"GEOTAIL POST MANEUVER ELEMENTS" These Cartesian GEI elements are in Mean Equator/Equinox of 1950. EPOCH X Y Z (km) YYMMDDHHMMSS VX VY VZ (km/s) 920725144500 89803.35654 -163131.5707 -65006.79863 .9195422870 -.9584426991 -.3043759517 920729140000 240447.6620 -252467.2869 -80322.67033 .7712495858D-01 .1983615615 .1161496891 920802150000 32392.95791 662.9659949 6686.354254 -4.248545171 1.994859015 .1726752809 920807150000 250968.0163 -275734.8351 -89816.26339 .1644766905 .1044344644 .8358924749D-01 920812143000 31681.79815 1636.361178 6821.427611 -4.356040830 1.925606059 .1333313783 920814120000 145499.5225 -228387.6391 -86159.18831 .7136131234 -.6425465651 -.1852006003 920821120000 263265.6063 -214488.8664 -58155.68966 -.3449561491 .5450606904 .2165856071 920826113000 174359.3377 -244882.8867 -92965.82385 .6484115375 -.5032930271 -.1319417639 920902113000 265026.7136 -196406.6470 -50345.05216 -.3976434207 .59400951532 .22675314315 920926120000 861583.5869 -6480.721113 113946.4111 -.1172597672D-01 .3182823365 .1313233078 921014235004 165980.0935 303257.5893 138314.7964 -.9257916654 -.4622533383 -.3034258057 921028210000 353297.9461 331292.7346 166788.4758 -.3775029267 .1274215264 .0097965437 921107130000 310198.3383 51151.03597 53296.03047 .7669739743 .6783692565 .3453123839 921210120000 -32860.21956 1111456.364 423122.3302 -.2433002444 .8952052571D-02 -.2280370565D-01 930108130000 -323160.6308 374575.6284 121335.9462 .2117638828 -.8444760704 -.2977071041 930110104716 -264685.7176 217921.5685 67262.28878 .6307874986 -.9862117046 -.3272890434 930129120000 -324901.1002 326909.7708 109142.2792 .2458232392 -.5551881089 -.1962647545 930209103000 -375572.4340 499205.6262 198729.3002 -.6262706917 .2886088104 .1517124006 930307120000 -1075885.180 443000.3301 236559.7704 -.9820414662D-01 -.1842538371 -.9759926898D-01 930402140000 -691600.6626 -130850.7159 -72558.28222 .5972831313 -.2844379815 -.1511861275 930510120000 -666807.1085 -350696.4696 -224343.9724 -.1748659066 -.5335050148 -.2587270107 930618130000 -159802.5265 -1211455.913 -531759.2851 .2709462884 -.4302852009D-01 .2137056718D-01 930727140000 639430.9155 -600297.8202 -167815.9427 .0306488761 .5196923201 .2101185893 930915130000 443389.9740 -185295.2589 -40681.93583 .1590162987 .2908924810 .1160941743 930925100000 158104.7531 -206090.7889 -65210.03820 1.127496685 -.4351576423 -.8991394092D-01 930927015408 299241.0535 -244085.9782 -70399.49056 1.067703492 -.1713140445 .1630861928D-01 931115120000 740372.4970 1037367.032 432811.2313 -.1959720978 .1308274514 .2270087191D-01 931231120243 -257612.1025 246282.2109 78141.50019 .2912217702 -1.083235167 -.3846645242 940114120000 -191965.4258 547183.0431 206106.9126 -.3009947722 -.6866406235D-01 -.4973132668D-01 940220201057 59691.75746 350161.7376 140429.2043 -.5083639286 .9819383947 .3390450402 940304103000 -564844.6084 691421.9254 211238.0143 -.4995107912 .3195428225D-01 -.3238524704D-01 940425140000 -1056934.689 -652401.8413 -270787.7440 .2153198480 -.3522698016 -.1100193993 940519150000 -417905.3678 -1124980.139 -409655.5940 .3657187366 -.1012107687 -.2597576469D-01 940624170000 464199.4192 -369586.0053 -141119.9412 -.8442173702D-01 .7758420495 .2709917840 940628100519 367406.9207 -87276.28213 -39103.10568 -.6437294134 .9337035379 .3825057304 940723143000 459840.8254 -672852.7776 -307862.4954 .3081204527 .1810125997 .1008962812 940809153000 403711.3456 -25649.33969 5925.931336 -.7388551541 .6818902920 .3009295003 940919123000 1078426.851 -324983.7977 -53453.75394 .9105828637D-01 .3598420253 .1357275494 941017130000 480414.3384 511054.7191 199553.5340 -.6766039868 .1426509060 .6803885652D-02 941104180000 55191.74336 381922.1848 108345.8776 -.4923563809 .2129588010 .4156956942D-01 941112034000 -27205.23774 -53331.62416 -15702.00355 3.199683160 -.8904640225 -.1452023636 941112063000 6906.839014 -57203.01188 -15686.60898 3.351385190 .1623278521 .1514570416 941112092000 39473.72220 -50435.23429 -12771.54895 2.942844226 1.103508152 .3997362468 950219181000 -33634.62700 -57655.42315 -15977.37437 2.908745203 -.9112130830 -.2713030625 950219210000 -2372.236585 -62805.26086 -17591.67310 3.120665642 -.6529303128D-01 -.3541464356D-01 950219235000 28867.69956 -58896.95542 -16667.45835 2.918510051 .8067476981 .2101028740 950226201000 -33408.19245 -57629.46801 -15905.52119 2.825034586 -.9182853367 -.2765261098 950226231000 -1145.971311 -62877.68736 -17596.71610 3.045421951 -.1983189496D-01 -.2569077193D-01 950227021000 30958.31494 -57993.43049 -16441.52445 2.794526126 .8949612800 .2328556796 950302140000 -77958.53901 149517.2846 42443.97304 -.8141939453 -.8805600247 -.2408292444 950713070000 -11224.51356 187037.6747 53680.93505 -1.001944895 -.3980601490D-01 .1529560720D-01 950810080000 -109603.1792 114438.4703 36063.39031 -.4878753016 -1.213523335 -.3316235836 950824010000 67850.75142 150376.8794 40764.06657 -.8504040687 .8889126030 .2819499404 950928080000 -90790.10837 -20458.12770 -2765.360836 1.419174774 -1.773756800 -.5580317329 951026190000 91387.24210 119372.2070 31187.35043 -.6342124802 1.247831210 .3833816195 951123210000 -19965.60201 185136.3131 54586.43799 -1.007443859 -.9552966010D-01 -.1216589480D-01 951214140000 35237.99010 173106.5268 48894.42256 -.9791353989 .5131152476 .1915427335 951220133000 -19858.19321 185684.3977 55011.30355 -1.002399729 -.4152139805D-01 -.1943543564D-01 960215000000 65562.91805 -30588.34339 -9108.682083 1.887820301 1.982558069 .5841976582 960301000000 -117171.0016 14076.47553 4456.172602 .7312155518 -1.692630658 -.5017563829 960306210000 -37967.30563 -59569.31239 -17502.43010 2.683228757 -.7777036160 -.2363805794 960325000000 18221.25145 173289.7166 51196.73263 -1.049373800 .4300431000 .1287222000 960401000000 -113677.5693 126452.2261 37780.39666 -.5696000650 -1.034441652 -.3036599436 960501000000 45360.45845 158502.5592 46756.07239 -.9818517887 .7370874236 .2234036817 960530150000 -111049.6304 2718.832732 1681.606255 .9414168987 -1.711126639 -.5155118469 960624090000 -56937.11937 177899.4593 43465.12173 -.9532299932 -.3023605037 -.7903189627D-01 960701000000 -129548.0845 87044.80138 27414.32901 -.1715153036 -1.323789048 -.3907813453 961072503000 49221.35811 149067.0307 43429.41843 -0.960083472 0.896444629 0.280058108 960801000000 -85713.97246 165219.3750 50264.17305 -0.848039341 -0.552098401 -0.150016858 960829090000 -112141.8338 -9221.254214 -714.2291409 1.104819612 -1.591536283 -.4899771858 960901000000 -883.8135551 174251.9255 51503.52259 -1.082296313 0.321838648 0.114562343 960926220000 65010.67102 126134.6851 36163.85916 -.8848409218 1.194338053 0.369900959 961031220000 -134631.1303 47065.19217 16757.54820 .2409902023 -1.481395646 -.4442456583 961128020000 -98902.45034 -23302.68614 -4633.100059 1.450116499 -1.545597705 -.4927894735 961205180000 12178.78446 168924.5373 49933.56103 -1.075764859 .4834260937 .1693574780 961206153000 -68383.60483 173135.3538 53113.92430 -.9476200375 -.3401344321 -.7832504532D-01 970116140000 63285.97965 118484.2395 37965.81023 -.8648373339 1.306733289 .3958294660 970201000000 85524.17930 36610.00234 12486.49476 .1033717137 2.214636582 .6911060229 970226230000 -10766.94119 -64515.37426 -20111.69598 2.919944619 .1347264659 .7262749949D-01 970301000000 -20001.21489 172015.1102 53106.58363 -1.113833533 .2383071699 .6209997784D-01 970327140000 -21226.19380 170909.5154 52635.06837 -1.127516574 .2246856734 .5864349596D-01 970401000000 62085.60350 114365.8588 35953.83610 -.9127474295 1.343439676 .4066091205 970424150000 -133961.8157 117016.0656 34973.14766 -.4789585658 -.9832654658 -.3080682732 970501000000 -125402.4457 -1049.099598 -1409.966308 .9112073856 -1.489746383 -.4525215427 970522170000 -57202.55498 -55775.72461 -17622.49587 2.391689918 -.9150710230 -.2656919669 970626100000 -104957.1114 156176.3987 47676.64436 -.7823950283 -.5578575800 -.1743285324 970701000000 -57903.24787 173105.3794 53040.64510 -1.014436161 -.8221816157D-01 -.2842560083D-01 970724140000 -27903.85837 -59665.53317 -18230.18774 2.904946552 -.2544706891 -.7774131422D-01 970828070000 -146354.4579 102787.8873 31665.98673 -.2958925810 -1.023751467 -.3094535217 970901000000 -53313.70138 169331.8870 51513.31641 -1.073346098 .2679826548D-01 .1188358760D-01 970925220000 41908.14742 121865.5337 36669.54063 -1.069584079 1.226389831 .3753936172 971001000000 52894.18239 107258.0216 32129.05193 -.9904752849 1.450826650 .4428056950 971030040000 -139357.2148 14530.68806 5208.479727 .6547297012 -1.388500449 -.4228196421 971101000000 59460.67647 99027.87441 29532.16024 -.9154590831 1.571031571 .4795386027 971127200000 -34681.87266 165900.3052 50268.16352 -1.144131999 .2025734663 .7036164672D-01 971201000000 -35243.69209 -61681.82073 -18285.25002 2.750882414 -.3569010314 -.1304989247 971225210000 -149648.0734 44831.43207 15187.56565 .2913371527 -1.296560674 -.3919731900 980101000000 -51803.65878 -57354.97174 -16526.71721 2.532178188 -.6779587931 -.2342685427 980201000000 -75111.91246 -51021.92387 -13879.79856 2.118883958 -.9651481439 -.3211433198 980226200000 -89870.17467 -45419.25982 -11662.32968 1.849609715 -1.077629664 -.3523972181 980323130000 -159438.8211 75986.42386 25523.62305 -.9828131240D-01 -1.096042106 -.3198008943 980423140000 -159431.3778 74177.18587 25165.76901 -.1025901189 -1.10574563 -.3222176296 Planned elements 980501000000 68466.19675 63457.31326 17164.97015 -.6184770108 2.111754499 .6333742601 980601000000 69837.97394 45402.49634 11485.98103 -.3321942741 2.389669982 .7063069921 980701000000 -99844.21093 -42271.86182 -9330.830439 1.672579896 -1.111652646 -.3711901329 980801000000 -112448.5507 -35158.01791 -6338.393489 1.458128352 -1.155095415 -.3797580941 Please respond to matu@d1.nas.nec.co.jp To: len.efron@jpl.nasa.gov, kevin.criddle@jpl.nasa.gov, earl.higa@jpl.nasa.gov, Joan.L.Pojman@jpl.nasa.gov, john.f.adams-jr@jpl.nasa.gov, istpfds@listserv.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp (bcc: Heather Franz/SSD/CSC) Subject: [Weekly] GEOTAIL Latest orbit data(7/17) To: Dr. L. Efron, Dr. K. Criddle, Dr. E.higa To: istpfds@listserv.gsfc.nasa.gov, john.f.adams-jr@jpl.nasa.gov ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ The following data is updated orbit solution based on 3-path data. (J2000.0EQ orbit elements) Best regards, Masatoshi Matsuoka --------------------------------------------------------- GEOTAIL STATE VECTOR for JPL FORMAT( Cartesian ) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ ( Unit is UTC, KM, KM/Sec ) ITIM= '16-Jul-1998 06:00:00.000 UTC', IC= -132535.580444, -14565.956968, -334.167350, 1.0520352150, -1.2510294464, -0.3915213342, DYNAMIC MODELING PARAMETERS ~~~~~~~~~~~~~~~~~~~~~~~~~~~ =========================================================================== ==== (Discriptions) =========================================================================== ==== S/C cross sectional area for drag cal. : NOT USE : 4.2170 [m**2] Dimensionless drag coefficient : NOT USE : 0.0000 [ -- ] Dimensionless drag scaling parameter : NOT USE : 00.000 [ -- ] S/C cross sectional area for S.R.F. cal.: USE : 4.2170 [m**2] Dimensionless solar reflectivity coefficient: USE : 1.3220 [ -- ] F10.7 solar flux at epoch : USE : 200.00 [1e-22*W/m**2/Hz] Dimensionless geomagnetic index : NOT USE : 000.00 [ -- ] =========================================================================== ==== ======================================================================= (DATA) (FREQ.) (STAT.) (First point[UTC]) -> (Last point[UTC]) ======================================================================= range S/S UDSC 98-07-14 00:16:36 -> 98-07-16 05:16:02 range rate S/S UDSC 98-07-14 00:02:30 -> 98-07-16 05:25:30 ======================================================================= GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1998 07 16 06 00 00.0000 [UTC] S/C MASS : 655.504 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -132535.580444 [km] Vx: 1.0520352150 [km/s] Y: -14565.956968 [km] Vy: -1.2510294464 [km/s] Z: -334.167350 [km] Vz: -0.3915213342 [km/s] (Keplerian) a: 126385.974918 [km] an: 5.776415148 [deg] e: 0.542242322160 [ - ] ap: 308.111539233 [deg] i: 16.1666279623 [deg] ma: 295.089234452 [deg] ORIGIN OF COORDINATE AND REFERENCE PLANE: [ @ ] 1= Geocentric, Earth equator [ ] 2= Heliocentric, Earth equator [ ] 3= Heliocentric, ecliptic [ ] 4= Selenocentric, Earth equator [ ] 5= Selenocentric, Moon equator COORDINATE SYSTEM: [ ] 1= Greenwich true of date rotating [ ] 2= Greenwich true of date nonrotating [ ] 3= EME50 [ @ ] 4= EME2000 [ ] 5= true of date (B1950.0) [ ] 6= true of date (J2000.0) [ ] 7= Selenographic VECTOR TYPE: [ @ ] 1= Routine on-orbit [ ] 2= Special on-orbit update [ ] 3= Spare [ ] 4= Maneuver ignition [ ] 5= Maneuver cut off [ ] 6= Reentry [ ] 7= Powered flight [ ] 8= Stationary From: AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 24-JUL-1998 07:44:59.04 To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia CC: d1.nas.nec.co.jp::matu Subj: [Monthly] GEOTAIL Latest Orbit Data(7/24) To: Waldherr-san, Valencia-san To: Dr. Sardi ^^^^^^^^^^^^^^~~~~~~~~~~~~~~~~ =================================================== Follow data is change coordinate system from EME50 to J2000.0 EQ. =================================================== The following data is updated orbit solution based on 3-path data. Attached orbit elements every one month to the last of this mail. Best regards, Masatoshi Matsuoka (E-mail: matu@d1.nas.nec.co.jp(in office)) (backup: matu@net203.newslan.isas.ac.jp(in ISAS)) --------------------------------------------------------- GEOTAIL STATE VECTOR(J2000EQ:GEOCENTRIC COORDINATE) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1998 07 22 22 00 00.0000 [UTC] S/C MASS : 655.504 [kg] ~~~~~~~~~~ (Cartesian) X: 55022.259302 [km] Vx: -0.9427484016 [km/s] Y: 82779.511792 [km] Vy: 1.8602411966 [km/s] Z: 22216.622766 [km] Vz: 0.5639867976 [km/s] (Keplerian) a: 126146.055351 [km] an: 5.885847567 [deg] e: 0.546354006990 [ - ] ap: 307.740112148 [deg] i: 16.1538312325 [deg] ma: 40.064278705 [deg] ===================================================================== <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> ^^^^^^^^^ EPOCH : 1998/07/22 22:00:00 (UTC) R(KM) V(KM/S) 55022.2593022800 -0.9427484015861000 82779.5117922200 1.8602411965600001 22216.6227656700 0.5639867976469000 EPOCH : 1998/08/01 00:00:00 (UTC) R(KM) V(KM/S) -112010.9916514838 1.4728940279232690 -36415.4833561601 -1.1386678667349523 -6885.3337852232 -0.3726327950144916 EPOCH : 1998/09/01 00:00:00 (UTC) R(KM) V(KM/S) -125396.1703894752 1.2452912664746048 -28140.5912409490 -1.1627622354635827 -3658.4900704168 -0.3729335201767809 EPOCH : 1998/10/01 00:00:00 (UTC) R(KM) V(KM/S) -167760.4470153365 -0.1392313205336155 73337.3677845155 -1.0263541414519435 26783.5983533663 -0.2855086209162156 EPOCH : 1998/11/01 00:00:00 (UTC) R(KM) V(KM/S) -166889.7003409113 -0.1825918366783869 75235.9598125775 -1.0208326309095348 27530.2385335464 -0.2821984347090732 % ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ====== % Received: Fri, 24 Jul 1998 04:43:59 -0700 from TYO203.gate.nec.co.jp by mg.nsi.net (8.9.0/1.3) with ESMTP % Received: from mailsv.nec.co.jp ([192.168.1.90]) by TYO203.gate.nec.co.jp (8.8.8+2.7Wbeta7/3.6Wbeta698070820) with ESMTP id UAA24008; Fri, 24 Jul 1998 20:44:54 +0900 (JS % Received: from india.d1.nas.nec.co.jp (india.d1.nas.nec.co.jp [10.52.9.1]) by mailsv.nec.co.jp (8.8.8+2.7Wbeta7/3.6Wbeta6-98070819) with SMTP id UAA01726; Fri, 24 Jul 1998 20:44:54 +0900 (JST % Received: from ayame.d1.nas.nec.co.jp by india.d1.nas.nec.co.jp (SMI-8.6/6.4JAIN-NAS-d1-1.3) id UAA07030; Fri, 24 Jul 1998 20:41:39 +090 % Received: by ayame.d1.nas.nec.co.jp (5.x/3.4Wbeta5) id AA15421; Fri, 24 Jul 1998 20:44:53 +090 % Date: Fri, 24 Jul 1998 20:44:53 +0900 % Message-Id: <9807241144.AA15421@ayame.d1.nas.nec.co.jp> % From: Masatoshi Matsuoka % To: ncf.span.nasa.gov::sardi % To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia % Cc: d1.nas.nec.co.jp::matu % Subject: [Monthly] GEOTAIL Latest Orbit Data(7/24) % Mime-Version: 1.0 % Content-Type: text/plain; charset=US-ASCII From: AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 17-JUL-1998 13:01:01.06 To: ncf.span.nasa.gov::sardi CC: d1.nas.nec.co.jp::matu Subj: Re: [Monthly] Geotail Latest Orbit Data Dear Dr. sardi I send Geotail Orbit Elements(monthly data) on June 26......... Resend same data the last of this e-mail. This data is EME50 GEOCENTRIC coordinate. I will next monthly data on July 24. The coordinate is changed to J2000.0EQ from next monthly data. Best regards, Masatoshi Matsuoka >>>>> "r" == r parthasarathy,nssdc/wdc-a-r&s writes: r> Looking into our Geotail collection, I notice that r> we have not received any more after your email dated 24 April 98. Do you r> think you could continue this help? We have no problem about the change r> from EME50 to J2000. Thanks very much for your help. r> sardi r> R. "Sardi" Parthasarathy ------ Return-Path: Date: Sat, 27 Jun 1998 00:05:01 +0900 From: Masatoshi Matsuoka To: sardi@ncf.span.nasa.gov Cc: matu@d1.nas.nec.co.jp Reply-To: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(6/26) Mime-Version: 1.0 Content-Type: text/plain; charset=US-ASCII Content-Length: 2691 To: Dr. Sardi ^^^^^^^^^^^^^^ The following data is updated orbit solution based on 3-path data. Attached orbit elements every one month to the last of this mail. Best regards, Masatoshi Matsuoka (E-mail: matu@d1.nas.nec.co.jp(in office)) (backup: matu@net203.newslan.isas.ac.jp(in ISAS)) --------------------------------------------------------- GEOTAIL STATE VECTOR(EME-50,GEOCENTRIC-COORDINATE) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1998 06 25 13 00 00.0000 [UTC] S/C MASS : 655.504 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: ( Cartesian )X: -131715.042901 [km] Vx: 1.0243218971 [km/s] Y: -10618.523507 [km] Vy: -1.2862530591 [km/s] Z: 641.370524 [km] Vz: -0.4028622499 [km/s] (Keplerian) a: 125866.832029 [km] an: 5.561347965 [deg] e: 0.544811658426 [ - ] ap: 306.317552152 [deg] i: 16.2800171395 [deg] ma: 295.832267101 [deg] ===================================================================== <<< S/C ORBITAL ELEMENTS (CARTESIAN;EME50;GEO-CENTRIC) >>> EPOCH : 1998/06/25 13:00:00 (UTC) R(KM) V(KM/S) -131715.0429010000 1.0243218971099999 -10618.5235069000 -1.2862530591400001 641.3705242020 -0.4028622499000001 EPOCH : 1998/07/01 00:00:00 (UTC) R(KM) V(KM/S) -99842.3458051911 1.6726288375644358 -42271.8218952288 -1.1116323861330368 -9331.3709407963 -0.3711816685331337 EPOCH : 1998/08/01 00:00:00 (UTC) R(KM) V(KM/S) -112446.1655800417 1.4581876940803937 -35158.7650557653 -1.1550725746791863 -6339.1904562338 -0.3797503455565049 EPOCH : 1998/09/01 00:00:00 (UTC) R(KM) V(KM/S) -125728.7484909494 1.2302290887133149 -26731.8362538046 -1.1766035621548567 -3046.4167440500 -0.3789357269159996 EPOCH : 1998/10/01 00:00:00 (UTC) R(KM) V(KM/S) -166800.3481653421 -0.1521713562571646 75209.9181934389 -1.0246849076211311 27596.7159617072 -0.2847793831889281 EPOCH : 1998/11/01 00:00:00 (UTC) R(KM) V(KM/S) -165903.6845624952 -0.1954871111333344 77097.9354866683 -1.0186824938898373 28338.7419161138 -0.2812595351290520 % ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ====== % Received: Thu, 16 Jul 1998 21:17:12 -0700 from TYO203.gate.nec.co.jp by mg.nsi.net (8.9.0/1.3) with ESMTP % Received: from mailsv.nec.co.jp ([192.168.1.90]) by TYO203.gate.nec.co.jp (8.8.8+2.7Wbeta7/3.6Wbeta698070820) with ESMTP id NAA24815; Fri, 17 Jul 1998 13:16:56 +0900 (JS % Received: from india.d1.nas.nec.co.jp (india.d1.nas.nec.co.jp [10.52.9.1]) by mailsv.nec.co.jp (8.8.8+2.7Wbeta7/3.6Wbeta6-98070819) with SMTP id NAA11090; Fri, 17 Jul 1998 13:16:54 +0900 (JST % Received: from ayame.d1.nas.nec.co.jp by india.d1.nas.nec.co.jp (SMI-8.6/6.4JAIN-NAS-d1-1.3) id NAA13594; Fri, 17 Jul 1998 13:13:50 +090 % Received: by ayame.d1.nas.nec.co.jp (5.x/3.4Wbeta5) id AA05227; Fri, 17 Jul 1998 13:16:53 +090 % Date: Fri, 17 Jul 1998 13:16:53 +0900 % Message-Id: <9807170416.AA05227@ayame.d1.nas.nec.co.jp> % From: Masatoshi Matsuoka % To: ncf.span.nasa.gov::sardi % Cc: d1.nas.nec.co.jp::matu % In-Reply-To: <199807161522.IAA00790@mg.nsi.net> (sardi@ncf.span.nasa.gov) % Subject: Re: [Monthly] Geotail Latest Orbit Data % Mime-Version: 1.0 % Content-Type: text/plain; charset=US-ASCII From: AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 28-AUG-1998 07:29:14.95 To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia CC: d1.nas.nec.co.jp::matu Subj: [Monthly] GEOTAIL Latest Orbit Data(8/28) To: Waldherr-san, Valencia-san To: Dr. Sardi ^^^^^^^^^^^^^^~~~~~~~~~~~~~~~~ The following data is updated orbit solution based on 3-path data. Attached orbit elements every one month to the last of this mail. Best regards, Masatoshi Matsuoka (E-mail: matu@d1.nas.nec.co.jp(in office)) (backup: matu@net203.newslan.isas.ac.jp(in ISAS)) --------------------------------------------------------- GEOTAIL STATE VECTOR(J2000EQ:GEOCENTRIC COORDINATE) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1998 08 27 21 00 00.0000 [UTC] S/C MASS : 655.504 [kg] ~~~~~~~~~~ (Cartesian) X: 64499.674870 [km] Vx: 0.6768522923 [km/s] Y: 3619.542645 [km] Vy: 2.8475746967 [km/s] Z: -1186.253679 [km] Vz: 0.7853068278 [km/s] (Keplerian) a: 126349.178280 [km] an: 6.893046443 [deg] e: 0.542766442799 [ - ] ap: 310.522727634 [deg] i: 15.9609114141 [deg] ma: 12.270003712 [deg] ==== <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1998/08/27 21:00:00 (UTC) R(KM) V(KM/S) 64499.6748696400 0.6768522923467000 3619.5426453540 2.8475746966830000 -1186.2536789550 0.7853068278027000 EPOCH : 1998/09/01 00:00:00 (UTC) R(KM) V(KM/S) -125404.0300444560 1.2451860486597834 -28138.8187370686 -1.1627334177140676 -3658.8439793931 -0.3729016973673931 EPOCH : 1998/10/01 00:00:00 (UTC) R(KM) V(KM/S) -167764.5244982436 -0.1392333026874613 73334.2866127447 -1.0263333735376210 26780.6928399403 -0.2854972262414144 EPOCH : 1998/11/01 00:00:00 (UTC) R(KM) V(KM/S) -166893.9362467496 -0.1825856860749385 75231.7792525536 -1.0208173702064127 27527.0285667714 -0.2821888600846592 % ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ====== % Received: Fri, 28 Aug 1998 04:27:13 -0700 from TYO203.gate.nec.co.jp by mg.nsi.net (8.9.0/1.3) with ESMTP % Received: from mailsv.nec.co.jp (mailsv-le1 [192.168.1.90]) by TYO203.gate.nec.co.jp (8.9.1a/3.7W98082117) with ESMTP id UAA11112; Fri, 28 Aug 1998 20:28:58 +0900 (JS % Received: from india.d1.nas.nec.co.jp (india.d1.nas.nec.co.jp [10.52.9.1]) by mailsv.nec.co.jp (8.9.1a/3.7W-MAILSV-NEC) with SMTP id UAA17181; Fri, 28 Aug 1998 20:28:57 +0900 (JST % Received: from ayame.d1.nas.nec.co.jp by india.d1.nas.nec.co.jp (SMI-8.6/6.4JAIN-NAS-d1-1.3) id UAA13028; Fri, 28 Aug 1998 20:24:54 +090 % Received: by ayame.d1.nas.nec.co.jp (SMI-8.6/3.4Wbeta5) id UAA08280; Fri, 28 Aug 1998 20:28:56 +090 % Date: Fri, 28 Aug 1998 20:28:56 +0900 % Message-Id: <199808281128.UAA08280@ayame.d1.nas.nec.co.jp> % From: Masatoshi Matsuoka % To: ncf.span.nasa.gov::sardi % To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia % Cc: d1.nas.nec.co.jp::matu % Subject: [Monthly] GEOTAIL Latest Orbit Data(8/28) % Mime-Version: 1.0 % Content-Type: text/plain; charset=US-ASCII From: AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 23-OCT-1998 05:43:07.98 To: csc.com::hfranz CC: d1.nas.nec.co.jp::matu Subj: [Monthly] GEOTAIL Latest Orbit Data(10/23) The following data is updated orbit solution based on 3 path data.(DV maneuver data included) We execute DV-maneuver on 10/18 at 9:00UT. (about 1.2m/s) After DV maneuver, SC weight is 655.017 kg. Best regards, Masatoshi Matsuoka ----- GEOTAIL STATE VECTOR for JPL FORMAT( Cartesian ) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ ( Unit is UTC, KM, KM/Sec ) ITIM= '22-Oct-1998 04:00:00.000 UTC', IC= -164103.924824, 26963.875218, 13676.896381, 0.3486328740, -1.1779966922, -0.3461541410, DYNAMIC MODELING PARAMETERS ~~~~~~~~~~~~~~~~~~~~~~~~~~~ =============================================================================== (Discriptions) =============================================================================== S/C cross sectional area for drag cal. : NOT USE : 4.2170 [m**2] Dimensionless drag coefficient : NOT USE : 0.0000 [ -- ] Dimensionless drag scaling parameter : NOT USE : 00.000 [ -- ] S/C cross sectional area for S.R.F. cal.: USE : 4.2170 [m**2] Dimensionless solar reflectivity coefficient: USE : 1.3220 [ -- ] F10.7 solar flux at epoch : USE : 200.00 [1e-22*W/m**2/Hz] Dimensionless geomagnetic index : NOT USE : 000.00 [ -- ] =============================================================================== ======================================================================= (DATA) (FREQ.) (STAT.) (First point[UTC]) -> (Last point[UTC]) ======================================================================= range S/S UDSC 98-10-19 15:24:16 -> 98-10-22 03:15:47 range rate S/S UDSC 98-10-19 15:00:30 -> 98-10-22 03:25:30 ======================================================================= GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1998 10 22 04 00 00.0000 [UTC] S/C MASS : 655.504 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -164103.924824 [km] Vx: 0.3486328740 [km/s] Y: 26963.875218 [km] Vy: -1.1779966922 [km/s] Z: 13676.896381 [km] Vz: -0.3461541410 [km/s] (Keplerian) a: 126602.021504 [km] an: 7.420843295 [deg] e: 0.524559359674 [ - ] ap: 311.709875532 [deg] i: 15.9251994123 [deg] ma: 256.579456977 [deg] RIGIN OF COORDINATE AND REFERENCE PLANE: [ @ ] 1= Geocentric, Earth equator [ ] 2= Heliocentric, Earth equator [ ] 3= Heliocentric, ecliptic [ ] 4= Selenocentric, Earth equator [ ] 5= Selenocentric, Moon equator COORDINATE SYSTEM: [ ] 1= Greenwich true of date rotating [ ] 2= Greenwich true of date nonrotating [ ] 3= EME50 [ @ ] 4= EME2000 [ ] 5= true of date (B1950.0) [ ] 6= true of date (J2000.0) [ ] 7= Selenographic VECTOR TYPE: [ @ ] 1= Routine on-orbit [ ] 2= Special on-orbit update [ ] 3= Spare [ ] 4= Maneuver ignition [ ] 5= Maneuver cut off [ ] 6= Reentry [ ] 7= Powered flight [ ] 8= Stationary ===== <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1998/10/22 04:00:00 (UTC) R(KM) V(KM/S) -164103.9248244000 0.3486328739792000 26963.8752183900 -1.1779966922480001 13676.8963814800 -0.3461541410122000 EPOCH : 1998/11/01 00:00:00 (UTC) R(KM) V(KM/S) -166522.0909012324 -0.2225565332313001 79515.6884919814 -0.9996775776787369 28722.3009656265 -0.2747417212629504 EPOCH : 1998/12/01 00:00:00 (UTC) R(KM) V(KM/S) -98322.6119678065 -1.0418416374684625 149130.4510275833 -0.2894260379523370 46059.4644173390 -0.0397352776671313 EPOCH : 1999/01/01 00:00:00 (UTC) R(KM) V(KM/S) -86278.8304690682 -1.1086983372282224 152554.3858726213 -0.1472404388413603 46575.0421535129 0.0090121943970104 EPOCH : 1999/02/01 00:00:00 (UTC) R(KM) V(KM/S) -78662.2234578588 -1.1632751655033187 151989.8999569704 -0.0508550606438207 45866.0966080847 0.0431990277035393 % ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ====== % Received: Fri, 23 Oct 1998 02:39:48 -0700 from TYO203.gate.nec.co.jp by mg.nsi.net (8.9.0/1.3) with ESMTP % Received: from mailsv.nec.co.jp (mailsv-le1 [192.168.1.90]) by TYO203.gate.nec.co.jp (8.9.1a/3.7W98092815) with ESMTP id SAA06147; Fri, 23 Oct 1998 18:42:53 +0900 (JS % Received: from india.d1.nas.nec.co.jp (india.d1.nas.nec.co.jp [10.52.9.1]) by mailsv.nec.co.jp (8.9.1a/3.7W-MAILSV-NEC) with SMTP id SAA25919; Fri, 23 Oct 1998 18:42:52 +0900 (JST % Received: from ayame.d1.nas.nec.co.jp by india.d1.nas.nec.co.jp (SMI-8.6/6.4JAIN-NAS-d1-1.3) id SAA27232; Fri, 23 Oct 1998 18:37:35 +090 % Received: by ayame.d1.nas.nec.co.jp (SMI-8.6/3.4Wbeta5) id SAA08279; Fri, 23 Oct 1998 18:42:51 +090 % Date: Fri, 23 Oct 1998 18:42:51 +0900 % Message-Id: <199810230942.SAA08279@ayame.d1.nas.nec.co.jp> % From: Masatoshi Matsuoka % To: ncf.span.nasa.gov::sardi % To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia % To: csc.com::hfranz % Cc: d1.nas.nec.co.jp::matu % Subject: [Monthly] GEOTAIL Latest Orbit Data(10/23) % Mime-Version: 1.0 % Content-Type: text/plain; charset=US-ASCII From: AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 27-NOV-1998 04:23:21.24 To: csc.com::hfranz CC: d1.nas.nec.co.jp::matu Subj: [Monthly] GEOTAIL Latest Orbit Data(11/27) The following data is updated orbit solution based on 3 path data. Best regards, Masatoshi Matsuoka(matu@d1.nas.nec.co.jp) == GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1998 11 26 22 00 00.0000 [UTC] S/C MASS : 655.504 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -165024.895104 [km] Vx: -0.2851936009 [km/s] Y: 85798.488241 [km] Vy: -0.9666553380 [km/s] Z: 30829.914062 [km] Vz: -0.2614544378 [km/s] (Keplerian) a: 126769.105527 [km] an: 8.075663395 [deg] e: 0.524962963887 [ - ] ap: 311.086150548 [deg] i: 15.9137898788 [deg] ma: 213.056014447 [deg] ======= <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1998/11/26 22:00:00 (UTC) R(KM) V(KM/S) X -165024.8951044000 -0.2851936008809000 Y 85798.4882408000 -0.9666553379743000 Z 30829.9140615200 -0.2614544378346000 EPOCH : 1998/12/01 00:00:00 (UTC) R(KM) V(KM/S) -98320.8783845109 -1.0418640951901483 149127.9489900977 -0.2894684741963401 46058.6013929629 -0.0397445817641774 EPOCH : 1999/01/01 00:00:00 (UTC) R(KM) V(KM/S) -86278.5749215878 -1.1087135335713625 152552.2078403555 -0.1472968983039445 46574.3591421458 0.0089983606500025 EPOCH : 1999/02/01 00:00:00 (UTC) R(KM) V(KM/S) -78663.0612135076 -1.1632846501342691 151988.3083533658 -0.0509230994619007 45865.6715100533 0.0431815555351659 EPOCH : 1999/03/01 00:00:00 (UTC) R(KM) V(KM/S) -173628.6679565991 0.2575071004631999 31877.6920100749 -1.0901325019025465 17873.8694310293 -0.3104730472576567 EPOCH : 1999/04/01 00:00:00 (UTC) R(KM) V(KM/S) -176411.9647095202 0.1132552837979275 41587.0086057190 -1.0610280088979831 20876.8763636268 -0.2946330141193896 % ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ====== % Received: Fri, 27 Nov 1998 01:19:46 -0800 from TYO203.gate.nec.co.jp by mg.nsi.net (8.9.0/1.3) with ESMTP % Received: from mailsv.nec.co.jp (mailsv-le1 [192.168.1.90]) by TYO203.gate.nec.co.jp (8.9.1a/3.7W98092815) with ESMTP id SAA05767; Fri, 27 Nov 1998 18:23:50 +0900 (JS % Received: from india.d1.nas.nec.co.jp (india.d1.nas.nec.co.jp [10.52.9.1]) by mailsv.nec.co.jp (8.9.1a/3.7W-MAILSV-NEC) with SMTP id SAA12603; Fri, 27 Nov 1998 18:23:49 +0900 (JST % Received: from ayame.d1.nas.nec.co.jp by india.d1.nas.nec.co.jp (SMI-8.6/6.4JAIN-NAS-d1-1.3) id SAA11734; Fri, 27 Nov 1998 18:17:50 +090 % Received: by ayame.d1.nas.nec.co.jp (SMI-8.6/3.4Wbeta5) id SAA20819; Fri, 27 Nov 1998 18:23:48 +090 % Date: Fri, 27 Nov 1998 18:23:48 +0900 % Message-Id: <199811270923.SAA20819@ayame.d1.nas.nec.co.jp> % From: Masatoshi Matsuoka % To: ncf.span.nasa.gov::sardi % To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia % To: csc.com::hfranz % Cc: d1.nas.nec.co.jp::matu % Subject: [Monthly] GEOTAIL Latest Orbit Data(11/27) % Mime-Version: 1.0 (generated by tm-edit 7.106) % Content-Type: text/plain; charset=US-ASCII From: AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 25-DEC-1998 04:18:57.71 To: csc.com::hfranz CC: d1.nas.nec.co.jp::matu Subj: [Monthly] GEOTAIL Latest Orbit Data(12/25) The following data is updated orbit solution based on 3-path data. Attached orbit elements every one month to the last of this mail. I wish you a Merry Christmas and a Happy New Year! Best regards, Masatoshi Matsuoka (E-mail: matu@d1.nas.nec.co.jp(in office)) --------------------------------------------------------- GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1998 12 23 22 00 00.0000 [UTC] S/C MASS : 655.504 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -144819.545878 [km] Vx: 0.8907304671 [km/s] Y: -11651.286396 [km] Vy: -1.1847998009 [km/s] Z: 3128.826735 [km] Vz: -0.3710641400 [km/s] (Keplerian) a: 126501.819585 [km] an: 8.956835246 [deg] e: 0.539083744483 [ - ] ap: 310.665972259 [deg] i: 15.8261708311 [deg] ma: 283.668373087 [deg] RIGIN OF COORDINATE AND REFERENCE PLANE: [ @ ] 1= Geocentric, Earth equator [ ] 2= Heliocentric, Earth equator [ ] 3= Heliocentric, ecliptic [ ] 4= Selenocentric, Earth equator [ ] 5= Selenocentric, Moon equator COORDINATE SYSTEM: [ ] 1= Greenwich true of date rotating [ ] 2= Greenwich true of date nonrotating [ ] 3= EME50 [ @ ] 4= EME2000 [ ] 5= true of date (B1950.0) [ ] 6= true of date (J2000.0) [ ] 7= Selenographic VECTOR TYPE: [ @ ] 1= Routine on-orbit [ ] 2= Special on-orbit update [ ] 3= Spare [ ] 4= Maneuver ignition [ ] 5= Maneuver cut off [ ] 6= Reentry [ ] 7= Powered flight [ ] 8= Stationary == <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1998/12/23 22:00:00 (UTC) R(KM) V(KM/S) -144819.5458780000 0.8907304671361000 -11651.2863957000 -1.1847998009050000 3128.8267353630 -0.3710641399863000 EPOCH : 1999/01/01 00:00:00 (UTC) R(KM) V(KM/S) -86271.5898224555 -1.1087423420830518 152552.9328654141 -0.1472795141741827 46575.9692373514 0.0090026320650926 EPOCH : 1999/02/01 00:00:00 (UTC) R(KM) V(KM/S) -78653.3078603960 -1.1633225833498364 151989.0059135459 -0.0508785350632679 45867.1476625561 0.0431942524797548 EPOCH : 1999/03/01 00:00:00 (UTC) R(KM) V(KM/S) -173626.9066355908 0.2574547350708813 31880.4188893832 -1.0901547762370007 17874.6786336214 -0.3104900030836084 EPOCH : 1999/04/01 00:00:00 (UTC) R(KM) V(KM/S) -176409.8675219867 0.1131671919556104 41593.3597851221 -1.0610388406552871 20878.7420756734 -0.2946447574881907 % ====== Internet headers and postmarks (see DECWRL::GATEWAY.DOC) ====== % Received: Fri, 25 Dec 1998 01:15:29 -0800 from TYO203.gate.nec.co.jp by mg.nsi.net (8.9.0/1.3) with ESMTP % Received: from mailsv.nec.co.jp (mailsv-le1 [192.168.1.90]) by TYO203.gate.nec.co.jp (8.9.1a/3.7W98121813) with ESMTP id SAA19899; Fri, 25 Dec 1998 18:20:12 +0900 (JS % Received: from india.d1.nas.nec.co.jp (india.d1.nas.nec.co.jp [10.52.9.1]) by mailsv.nec.co.jp (8.9.1a/3.7W-MAILSV-NEC) with SMTP id SAA19713; Fri, 25 Dec 1998 18:20:11 +0900 (JST % Received: from ayame.d1.nas.nec.co.jp by india.d1.nas.nec.co.jp (SMI-8.6/6.4JAIN-NAS-d1-1.3) id SAA19495; Fri, 25 Dec 1998 18:13:39 +090 % Received: by ayame.d1.nas.nec.co.jp (SMI-8.6/3.4Wbeta5) id SAA00379; Fri, 25 Dec 1998 18:20:08 +090 % Date: Fri, 25 Dec 1998 18:20:08 +0900 % Message-Id: <199812250920.SAA00379@ayame.d1.nas.nec.co.jp> % From: Masatoshi Matsuoka % To: ncf.span.nasa.gov::sardi % To: jpl.nasa.gov::stefan.waldherr, jpl.nasa.gov::jose.valencia % To: csc.com::hfranz % Cc: d1.nas.nec.co.jp::matu % Subject: [Monthly] GEOTAIL Latest Orbit Data(12/25) % Mime-Version: 1.0 (generated by tm-edit 7.106) % Content-Type: text/plain; charset=US-ASCII From: AMES::"matu@d1.nas.nec.co.jp" "Masatoshi Matsuoka" 29-JAN-1999 06:41:14.91 To: csc.com::hfranz CC: d1.nas.nec.co.jp::matu Subj: [Monthly] GEOTAIL Latest Orbit Data(1/29) The following data is updated orbit solution based on 3-path data. We executed attitude maneuver on Jan 26 (at 10:00 utc). After attitude maneuver, SC weight is 654.917kg. Attached orbit elements every one month to the last of this mail. Best regards, Masatoshi Matsuoka (E-mail: matu@d1.nas.nec.co.jp) == GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1999 01 28 21 00 00.0000 [UTC] S/C MASS : 654.917 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -166085.505835 [km] Vx: 0.3824063525 [km/s] Y: 25663.310202 [km] Vy: -1.1444062454 [km/s] Z: 15201.297217 [km] Vz: -0.3350011367 [km/s] (Keplerian) a: 126289.918453 [km] an: 10.015161599 [deg] e: 0.551074097393 [ - ] ap: 310.866834942 [deg] i: 15.6791520393 [deg] ma: 257.430351113 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1999/01/28 21:00:00 (UTC) R(KM) V(KM/S) -166085.5058350000 0.3824063525054000 25663.3102024300 -1.1444062453740000 15201.2972173200 -0.3350011366958000 EPOCH : 1999/02/01 00:00:00 (UTC) R(KM) V(KM/S) -78657.5256728291 -1.1632625537208110 151991.7420957299 -0.0509739196952565 45866.8982183420 0.0431624020640268 EPOCH : 1999/03/01 00:00:00 (UTC) R(KM) V(KM/S) -173608.6490101967 0.2579987117946700 31834.9634169662 -1.0903091265359073 17860.7524110667 -0.3105527519714410 EPOCH : 1999/04/01 00:00:00 (UTC) R(KM) V(KM/S) -176393.6125990544 0.1140985868233876 41510.2914644479 -1.0613193970538803 20854.6438101712 -0.2947644450239202 EPOCH : 1999/05/01 00:00:00 (UTC) R(KM) V(KM/S) -137307.4915406731 -0.8237525720591180 124665.5466938838 -0.5910229137654954 41652.0242471504 -0.1151243043768270 ------- foward message ------------------------------------------- The following data is updated orbit solution based on 3-path data. Attached orbit elements every one month to the last of this mail. Best regards, Masatoshi Matsuoka (E-mail: matu@d1.nas.nec.co.jp) == == GEOTAIL STATE VECTOR for JPL FORMAT( Cartesian ) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ ( Unit is UTC, KM, KM/Sec ) ITIM= '27-Apr-1999 14:00:00.000 UTC', IC= -149280.749092, -21871.558078, 2349.432890, 0.8962068606, -1.1028793414, -0.3504388694, DYNAMIC MODELING PARAMETERS ~~~~~~~~~~~~~~~~~~~~~~~~~~~ =============================================================================== (Discriptions) =============================================================================== S/C cross sectional area for drag cal. : NOT USE : 4.2170 [m**2] Dimensionless drag coefficient : NOT USE : 0.0000 [ -- ] Dimensionless drag scaling parameter : NOT USE : 00.000 [ -- ] S/C cross sectional area for S.R.F. cal.: USE : 4.2170 [m**2] Dimensionless solar reflectivity coefficient: USE : 1.3220 [ -- ] F10.7 solar flux at epoch : USE : 200.00 [1e-22*W/m**2/Hz] Dimensionless geomagnetic index : NOT USE : 000.00 [ -- ] =============================================================================== ======================================================================= (DATA) (FREQ.) (STAT.) (First point[UTC]) -> (Last point[UTC]) ======================================================================= range S/S UDSC 99-04-24 06:55:02 -> 99-04-27 13:35:26 range rate S/S UDSC 99-04-24 06:32:30 -> 99-04-27 13:41:30 ======================================================================= GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1999 04 27 14 00 00.0000 [UTC] S/C MASS : 654.917 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -149280.749092 [km] Vx: 0.8962068606 [km/s] Y: -21871.558078 [km] Vy: -1.1028793414 [km/s] Z: 2349.432890 [km] Vz: -0.3504388694 [km/s] (Keplerian) a: 126906.805523 [km] an: 11.544714386 [deg] e: 0.526356285014 [ - ] ap: 314.801285863 [deg] i: 15.5434932437 [deg] ma: 277.102882538 [deg] RIGIN OF COORDINATE AND REFERENCE PLANE: [ @ ] 1= Geocentric, Earth equator [ ] 2= Heliocentric, Earth equator [ ] 3= Heliocentric, ecliptic [ ] 4= Selenocentric, Earth equator [ ] 5= Selenocentric, Moon equator COORDINATE SYSTEM: [ ] 1= Greenwich true of date rotating [ ] 2= Greenwich true of date nonrotating [ ] 3= EME50 [ @ ] 4= EME2000 [ ] 5= true of date (B1950.0) [ ] 6= true of date (J2000.0) [ ] 7= Selenographic VECTOR TYPE: [ @ ] 1= Routine on-orbit [ ] 2= Special on-orbit update [ ] 3= Spare [ ] 4= Maneuver ignition [ ] 5= Maneuver cut off [ ] 6= Reentry [ ] 7= Powered flight [ ] 8= Stationary <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1999/04/27 14:00:00 (UTC) R(KM) V(KM/S) -149280.7490918000 0.8962068606238000 -21871.5580783100 -1.1028793413930000 2349.4328897750 -0.3504388693866000 EPOCH : 1999/05/01 00:00:00 (UTC) R(KM) V(KM/S) -137301.1045249201 -0.8237348142263734 124681.4649050949 -0.5909403531571857 41653.0274478543 -0.1150988081287263 EPOCH : 1999/06/01 00:00:00 (UTC) R(KM) V(KM/S) -124147.8657201431 -0.9386359862730519 132960.0557889145 -0.4807854225104943 43489.7100664334 -0.0754749113708513 EPOCH : 1999/07/01 00:00:00 (UTC) R(KM) V(KM/S) 1323.4952686999 -1.4741554939135211 123020.4499070225 0.9077654756403560 33005.8195753125 0.3375461625150198 From: SMTP%"hfranz@csc.com" 16-FEB-2000 10:20:30.61 To: SARDI CC: Subj: [Monthly] GEOTAIL Latest Orbit Data(6/25) X-Lotus-FromDomain: CSC From: hfranz@csc.com To: sardi@nssdca.gsfc.nasa.gov Message-ID: <85256887.00527C93.00@csc.com> Date: Wed, 16 Feb 2000 10:00:46 -0500 Subject: [Monthly] GEOTAIL Latest Orbit Data(6/25) Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline ---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:55 AM --------------------------- matu@d1.nas.nec.co.jp on 06/25/99 10:41:18 AM To: sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC, FERRIER@nssdca.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(6/25) The following data is updated orbit solution based on 3 path data. Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp -- GEOTAIL STATE VECTOR for JPL FORMAT( Cartesian ) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ ( Unit is UTC, KM, KM/Sec ) ITIM= '24-Jun-1999 20:00:00.000 UTC', IC= 27404.489657, -53386.651366, -16103.161038, 2.4937590539, 1.8306356745, 0.3368893854, DYNAMIC MODELING PARAMETERS ~~~~~~~~~~~~~~~~~~~~~~~~~~~ =============================================================================== (Discriptions) =============================================================================== S/C cross sectional area for drag cal. : NOT USE : 4.2170 [m**2] Dimensionless drag coefficient : NOT USE : 0.0000 [ -- ] Dimensionless drag scaling parameter : NOT USE : 00.000 [ -- ] S/C cross sectional area for S.R.F. cal.: USE : 4.2170 [m**2] Dimensionless solar reflectivity coefficient: USE : 1.3220 [ -- ] F10.7 solar flux at epoch : USE : 200.00 [1e-22*W/m**2/Hz] Dimensionless geomagnetic index : NOT USE : 000.00 [ -- ] =============================================================================== ======================================================================= (DATA) (FREQ.) (STAT.) (First point[UTC]) -> (Last point[UTC]) ======================================================================= range S/S UDSC 99-06-22 01:11:31 -> 99-06-24 19:19:47 range rate S/S UDSC 99-06-22 01:00:30 -> 99-06-24 19:36:30 ======================================================================= GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1999 06 24 20 00 00.0000 [UTC] S/C MASS : 654.917 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: 27404.489657 [km] Vx: 2.4937590539 [km/s] Y: -53386.651366 [km] Vy: 1.8306356745 [km/s] Z: -16103.161038 [km] Vz: 0.3368893854 [km/s] (Keplerian) a: 126656.639835 [km] an: 13.100313746 [deg] e: 0.532485362857 [ - ] ap: 313.721373722 [deg] i: 15.4638636319 [deg] ma: 351.960351100 [deg] RIGIN OF COORDINATE AND REFERENCE PLANE: [ @ ] 1= Geocentric, Earth equator [ ] 2= Heliocentric, Earth equator [ ] 3= Heliocentric, ecliptic [ ] 4= Selenocentric, Earth equator [ ] 5= Selenocentric, Moon equator COORDINATE SYSTEM: [ ] 1= Greenwich true of date rotating [ ] 2= Greenwich true of date nonrotating [ ] 3= EME50 [ @ ] 4= EME2000 [ ] 5= true of date (B1950.0) [ ] 6= true of date (J2000.0) [ ] 7= Selenographic VECTOR TYPE: [ @ ] 1= Routine on-orbit [ ] 2= Special on-orbit update [ ] 3= Spare [ ] 4= Maneuver ignition [ ] 5= Maneuver cut off [ ] 6= Reentry [ ] 7= Powered flight [ ] 8= Stationary <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1999/06/24 20:00:00 (UTC) R(KM) V(KM/S) 27404.4896567600 2.4937590539349999 -53386.6513655600 1.8306356744660000 -16103.1610378900 0.3368893854097000 EPOCH : 1999/07/01 00:00:00 (UTC) R(KM) V(KM/S) 1318.0276348595 -1.4741580556807234 123021.6275368300 0.9077089865686897 33008.7674934192 0.3375507437378745 EPOCH : 1999/08/01 00:00:00 (UTC) R(KM) V(KM/S) 14372.7915331505 -1.4809330424789520 110284.5948428321 1.1932737181693294 28309.6126282420 0.4164757614741601 EPOCH : 1999/09/01 00:00:00 (UTC) R(KM) V(KM/S) 38709.9946308732 -1.3476864856309085 83132.9716308857 1.7958980893698600 19207.5535721281 0.5669941087347343 EPOCH : 1999/10/01 00:00:00 (UTC) R(KM) V(KM/S) -94689.5471381356 1.7685113663800349 -69069.5403990595 -0.6412114680369356 -11419.0761797389 -0.2947538685737059 EPOCH : 2000/01/01 00:00:00 (UTC) R(KM) V(KM/S) -182214.0596469779 -0.1439921765522321 52965.4757122789 -0.9625781645605903 28645.5226553743 -0.2386928341048419 From: SMTP%"hfranz@csc.com" 16-FEB-2000 09:59:31.52 To: SARDI CC: Subj: [Monthly] GEOTAIL Latest Orbit Data(7/30) X-Lotus-FromDomain: CSC From: hfranz@csc.com To: sardi@nssdca.gsfc.nasa.gov Message-ID: <85256887.00528754.00@csc.com> Date: Wed, 16 Feb 2000 10:01:14 -0500 Subject: [Monthly] GEOTAIL Latest Orbit Data(7/30) Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline ---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:56 AM --------------------------- matu@d1.nas.nec.co.jp on 07/30/99 05:54:35 AM To: sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC, FERRIER@nssdca.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(7/30) The following data is updated orbit solution based on 3 path data. Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp -- GEOTAIL STATE VECTOR(J2000.0EQ GEO CENTRIC) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1999 07 29 06 00 00.0000 [UTC] S/C MASS : 654.917 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -179073.779827 [km] Vx: -0.0614619441 [km/s] Y: 56678.456195 [km] Vy: -0.9902871537 [km/s] Z: 27113.381570 [km] Vz: -0.2589567920 [km/s] (Keplerian) a: 126570.457395 [km] an: 14.219136963 [deg] e: 0.550693957041 [ - ] ap: 313.708764094 [deg] i: 15.3267823691 [deg] ma: 218.233495139 [deg] EPOCH : 1999/07/29 06:00:00 (UTC) R(KM) V(KM/S) -179073.7798269000 -0.0614619440672100 56678.4561947200 -0.9902871536955000 27113.3815701800 -0.2589567920332000 EPOCH : 1999/08/01 00:00:00 (UTC) R(KM) V(KM/S) 14372.1253905781 -1.4809438238210437 110283.8406880362 1.1932816841380645 28308.9213312332 0.4164870317851314 EPOCH : 1999/09/01 00:00:00 (UTC) R(KM) V(KM/S) 38711.7828251135 -1.3476638726211816 83128.9353223974 1.7959878255785213 19205.7645498786 0.5670217996393809 EPOCH : 1999/10/01 00:00:00 (UTC) R(KM) V(KM/S) -94697.8635463013 1.7684048716421221 -69066.9733367061 -0.6412736235148507 -11416.8292779320 -0.2947756394585940 From: SMTP%"hfranz@csc.com" 16-FEB-2000 09:59:49.30 To: SARDI CC: Subj: [Monthly] GEOTAIL Latest Orbit Data(8/27) X-Lotus-FromDomain: CSC From: hfranz@csc.com To: sardi@nssdca.gsfc.nasa.gov Message-ID: <85256887.00529135.00@csc.com> Date: Wed, 16 Feb 2000 10:01:40 -0500 Subject: [Monthly] GEOTAIL Latest Orbit Data(8/27) Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline ---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:57 AM --------------------------- matu@d1.nas.nec.co.jp on 08/27/99 07:41:56 AM To: sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC, FERRIER@nssdca.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(8/27) The following data is updated orbit solution based on 3 path data. We will be planning next DV on Oct. 27. (about 0.75m/s) Its purpose is eclipse start time change.(eclipse on next winter) Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp -- GEOTAIL STATE VECTOR(J2000.0EQ:GEO CENTRIC) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1999 08 26 20 00 00.0000 [UTC] S/C MASS : 654.917 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: 33073.272878 [km] Vx: -1.4051782643 [km/s] Y: 90132.145356 [km] Vy: 1.6423509953 [km/s] Z: 21440.735640 [km] Vz: 0.5303080985 [km/s] (Keplerian) a: 126509.859985 [km] an: 14.789221412 [deg] e: 0.549859630621 [ - ] ap: 315.241495402 [deg] i: 15.2389007589 [deg] ma: 37.329248409 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1999/08/26 20:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) 33073.2728775600 -1.4051782642849999 0.0000000000000000 90132.1453560900 1.6423509952510000 0.0000000000000000 21440.7356396400 0.5303080985010000 0.0000000000000000 EPOCH : 1999/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) 38709.9521214787 -1.3476997870198715 0.0000000000000000 83129.9497958064 1.7959616246576726 0.0000000000000000 19206.5196512819 0.5669951935636464 0.0000000000000000 EPOCH : 1999/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) -94695.7657752747 1.7684338222142038 0.0000000000000000 -69068.2450587733 -0.6412433257824663 0.0000000000000000 -11418.3646302641 -0.2947442035971555 0.0000000000000000 EPOCH : 1999/10/22 12:53:28 (UTC) R(KM) V(KM/S) DV(KM/S) 52156.9442799988 1.4534371041796454 0.0003370521499224 -24579.2359144661 2.8185382515826314 0.0006536191862741 -10276.9831423541 0.6349021819726980 0.0001472338533322 EPOCH : 1999/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) -118930.7016344239 1.4380134118733252 0.0000000000000000 -58288.9260947654 -0.8277543969018609 -0.0000000000000000 -6486.2734703003 -0.3244911084521494 0.0000000000000000 From: SMTP%"hfranz@csc.com" 16-FEB-2000 10:00:25.76 To: SARDI CC: Subj: [Monthly] GEOTAIL Latest Orbit Data(10/01) X-Lotus-FromDomain: CSC From: hfranz@csc.com To: sardi@nssdca.gsfc.nasa.gov Message-ID: <85256887.00529CCD.00@csc.com> Date: Wed, 16 Feb 2000 10:02:09 -0500 Subject: [Monthly] GEOTAIL Latest Orbit Data(10/01) Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline ---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:57 AM --------------------------- matu@d1.nas.nec.co.jp on 10/03/99 10:04:39 AM To: sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC, FERRIER@nssdca.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(10/01) The following data is updated orbit solution based on 3 path data. We will be planning next DV on Oct. 22. (about 0.76m/s) Its purpose is eclipse start time change.(eclipse on next winter) Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp -- <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 1999/09/30 05:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -170382.0837587000 0.5538921647400999 0.0000000000000000 Y: -5112.5381738350 -1.0559590693670000 0.0000000000000000 Z: 10796.0754213100 -0.3170686727022000 0.0000000000000000 EPOCH : 1999/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) -94694.8430001265 1.7684382222553701 0.0000000000000000 -69069.8434441794 -0.6412174085488236 -0.0000000000000000 -11417.7998517875 -0.2947611363500793 0.0000000000000000 EPOCH : 1999/10/22 12:53:28 (UTC) R(KM) V(KM/S)=pre-DV= DV(KM/S) 52156.6300602233 1.4534568241881800 0.0003517929223928 -24580.2052293450 2.8185199027993444 0.0006187645258989 -10277.9207894127 0.6348854498872206 0.0002664060833454 EPOCH : 1999/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) -118929.6522626079 1.4380267002818359 0.0000000000000000 -58289.5499531694 -0.8277359322336789 -0.0000000000000000 -6489.4916002066 -0.3245121363049182 0.0000000000000000 EPOCH : 1999/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) -182572.9442141713 -0.0360813339676075 0.0000000000000000 43661.8778211241 -1.0035835828206550 0.0000000000000000 25577.6540157757 -0.2615762471806082 0.0000000000000000 EPOCH : 2000/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) -179449.3542731727 -0.2858906266224348 0.0000000000000000 66352.5293385251 -0.9152771830574199 0.0000000000000000 31903.5281878539 -0.2149480634894784 0.0000000000000000 From: SMTP%"hfranz@csc.com" 16-FEB-2000 10:00:38.51 To: SARDI CC: Subj: [Monthly] GEOTAIL Latest Orbit Data(10/29) X-Lotus-FromDomain: CSC From: hfranz@csc.com To: sardi@nssdca.gsfc.nasa.gov Message-ID: <85256887.0052A504.00@csc.com> Date: Wed, 16 Feb 2000 10:02:30 -0500 Subject: [Monthly] GEOTAIL Latest Orbit Data(10/29) Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline ---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:58 AM --------------------------- matu@d1.nas.nec.co.jp on 10/29/99 03:39:33 AM To: sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC, FERRIER@nssdca.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(10/29) The following data is updated orbit solution based on 3 path data.(post DV24 data) Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp = GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1999 10 28 21 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -48396.740964 [km] Vx: -1.4684710550 [km/s] Y: 133970.206270 [km] Vy: 0.2689644141 [km/s] Z: 38891.757592 [km] Vz: 0.1787913471 [km/s] (Keplerian) a: 127013.204067 [km] an: 15.558703695 [deg] e: 0.532324410349 [ - ] ap: 318.051746937 [deg] i: 15.3125305935 [deg] ma: 78.735138283 [deg] RIGIN OF COORDINATE AND REFERENCE PLANE: [ @ ] 1= Geocentric, Earth equator [ ] 2= Heliocentric, Earth equator [ ] 3= Heliocentric, ecliptic [ ] 4= Selenocentric, Earth equator [ ] 5= Selenocentric, Moon equator COORDINATE SYSTEM: [ ] 1= Greenwich true of date rotating [ ] 2= Greenwich true of date nonrotating [ ] 3= EME50 [ @ ] 4= EME2000 [ ] 5= true of date (B1950.0) [ ] 6= true of date (J2000.0) [ ] 7= Selenographic VECTOR TYPE: [ @ ] 1= Routine on-orbit [ ] 2= Special on-orbit update [ ] 3= Spare [ ] 4= Maneuver ignition [ ] 5= Maneuver cut off [ ] 6= Reentry [ ] 7= Powered flight [ ] 8= Stationary <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>> EPOCH : 1999/10/28 21:00:00 (UTC) (Cartesian) X: -48396.740964 [km] Vx: -1.4684710550 [km/s] Y: 133970.206270 [km] Vy: 0.2689644141 [km/s] Z: 38891.757592 [km] Vz: 0.1787913471 [km/s] EPOCH : 1999/11/01 00:00:00 (UTC) (Cartesian) X: -118869.626618 [km] Vx: 1.4388332009 [km/s] Y: -58322.653619 [km] Vy: -0.8273672342 [km/s] Z: -6504.961756 [km] Vz: -0.3244327975 [km/s] EPOCH : 1999/12/01 00:00:00 (UTC) (Cartesian) X: -182572.615070 [km] Vx: -0.0345488234 [km/s] Y: 43512.595100 [km] Vy: -1.0039908907 [km/s] Z: 25533.555650 [km] Vz: -0.2617908097 [km/s] EPOCH : 2000/01/01 00:00:00 (UTC) (Cartesian) X: -179519.502132 [km] Vx: -0.2833091439 [km/s] Y: 66108.452701 [km] Vy: -0.9162476365 [km/s] Z: 31840.828588 [km] Vz: -0.2154039101 [km/s] From: SMTP%"hfranz@csc.com" 16-FEB-2000 10:01:30.58 To: SARDI CC: Subj: [Monthly] GEOTAIL Latest Orbit Data(11/26) X-Lotus-FromDomain: CSC From: hfranz@csc.com To: sardi@nssdca.gsfc.nasa.gov Message-ID: <85256887.0052AFEE.00@csc.com> Date: Wed, 16 Feb 2000 10:02:59 -0500 Subject: [Monthly] GEOTAIL Latest Orbit Data(11/26) Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline ---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:58 AM --------------------------- matu@d1.nas.nec.co.jp on 11/26/99 06:48:06 AM To: sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC, FERRIER@nssdca.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(11/26) The following data is updated orbit solution based on 3 path data. Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp = GEOTAIL STATE VECTOR(J2000.0EQ) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1999 11 24 22 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -149808.827675 [km] Vx: -0.7674824089 [km/s] Y: 109740.984047 [km] Vy: -0.6634718121 [km/s] Z: 40391.553064 [km] Vz: -0.1167657307 [km/s] (Keplerian) a: 126462.181898 [km] an: 16.086992712 [deg] e: 0.529730103567 [ - ] ap: 316.920844000 [deg] i: 15.3685867978 [deg] ma: 152.089803368 [deg] ==== <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>> EPOCH : 1999/11/24 22:00:00 (UTC) (Cartesian) X: -149808.827675 [km] Vx: -0.7674824089 [km/s] Y: 109740.984047 [km] Vy: -0.6634718121 [km/s] Z: 40391.553064 [km] Vz: -0.1167657307 [km/s] EPOCH : 1999/12/01 00:00:00 (UTC) (Cartesian) X: -182569.726439 [km] Vx: -0.0345454178 [km/s] Y: 43513.365822 [km] Vy: -1.0040055825 [km/s] Z: 25538.240597 [km] Vz: -0.2618077656 [km/s] EPOCH : 2000/01/01 00:00:00 (UTC) (Cartesian) X: -179496.994407 [km] Vx: -0.2835556341 [km/s] Y: 66152.352621 [km] Vy: -0.9162043491 [km/s] Z: 31867.551997 [km] Vz: -0.2153401581 [km/s] EPOCH : 2000/02/01 00:00:00 (UTC) (Cartesian) X: -173640.233520 [km] Vx: -0.4790466712 [km/s] Y: 84088.525970 [km] Vy: -0.8097390485 [km/s] Z: 36511.792920 [km] Vz: -0.1666270576 [km/s] From: SMTP%"hfranz@csc.com" 16-FEB-2000 10:01:40.24 To: SARDI CC: Subj: [Monthly] GEOTAIL Latest Orbit Data(12/24) X-Lotus-FromDomain: CSC From: hfranz@csc.com To: sardi@nssdca.gsfc.nasa.gov Message-ID: <85256887.0052BD92.00@csc.com> Date: Wed, 16 Feb 2000 10:03:18 -0500 Subject: [Monthly] GEOTAIL Latest Orbit Data(12/24) Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline ---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:59 AM --------------------------- matu@net203.newslan.isas.ac.jp on 12/24/99 01:09:27 AM To: sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC, FERRIER@ndadsb-f.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(12/24) The following data is updated orbit solution based on 3 path data. Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp - GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 1999 12 21 20 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -181664.213493 [km] Vx: -0.0365793794 [km/s] Y: 44267.722053 [km] Vy: -1.0031620547 [km/s] Z: 26005.932740 [km] Vz: -0.2608925597 [km/s] (Keplerian) a: 126653.358643 [km] an: 16.737517813 [deg] e: 0.529076710241 [ - ] ap: 316.331929922 [deg] i: 15.3542391651 [deg] ma: 213.367690708 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>> EPOCH : 1999/12/21 20:00:00 (UTC) (Cartesian) X: -181664.213493 [km] Vx: -0.0365793794 [km/s] Y: 44267.722053 [km] Vy: -1.0031620547 [km/s] Z: 26005.932740 [km] Vz: -0.2608925597 [km/s] EPOCH : 2000/01/01 00:00:00 (UTC) (Cartesian) X: -179512.857094 [km] Vx: -0.2833286793 [km/s] Y: 66114.620375 [km] Vy: -0.9162688538 [km/s] Z: 31850.352313 [km] Vz: -0.2154026608 [km/s] EPOCH : 2000/02/01 00:00:00 (UTC) (Cartesian) X: -173662.529384 [km] Vx: -0.4787899002 [km/s] Y: 84048.569720 [km] Vy: -0.8098754970 [km/s] Z: 36495.103727 [km] Vz: -0.1667202794 [km/s] EPOCH : 2000/03/01 00:00:00 (UTC) (Cartesian) X: 50552.758524 [km] Vx: -1.0818702050 [km/s] Y: 53601.240695 [km] Vy: 2.4302948824 [km/s] Z: 9266.473748 [km] Vz: 0.7164188819 [km/s] EPOCH : 2000/04/01 00:00:00 (UTC) (Cartesian) X: 50404.592576 [km] Vx: 1.4397792749 [km/s] Y: -26593.401496 [km] Vy: 2.8532576126 [km/s] Z: -11321.532474 [km] Vz: 0.6037138898 [km/s] From: SMTP%"hfranz@csc.com" 16-FEB-2000 10:02:28.59 To: SARDI CC: Subj: [Monthly] GEOTAIL Latest Orbit Data(1/28) X-Lotus-FromDomain: CSC From: hfranz@csc.com To: sardi@nssdca.gsfc.nasa.gov Message-ID: <85256887.0052C1C7.00@csc.com> Date: Wed, 16 Feb 2000 10:03:43 -0500 Subject: [Monthly] GEOTAIL Latest Orbit Data(1/28) Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline ---------------------- Forwarded by Heather Franz/CIV/CSC on 02/16/2000 09:59 AM --------------------------- matu@d1.nas.nec.co.jp on 01/28/2000 01:48:19 AM To: sardi@ncf.span.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, Heather Franz/CIV/CSC@CSC, FERRIER@ndadsb-f.gsfc.nasa.gov cc: matu@d1.nas.nec.co.jp Subject: [Monthly] GEOTAIL Latest Orbit Data(1/28) The following data is updated orbit solution based on 3 path data. Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp - GEOTAIL STATE VECTOR(J2000.0EQ) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 01 27 22 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -173128.041204 [km] Vx: 0.5539363428 [km/s] Y: -8107.069096 [km] Vy: -1.0195963126 [km/s] Z: 12703.691122 [km] Vz: -0.3089826594 [km/s] (Keplerian) a: 126722.835941 [km] an: 18.403943034 [deg] e: 0.551252144767 [ - ] ap: 317.021488242 [deg] i: 15.1354000055 [deg] ma: 250.991236413 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>> EPOCH : 2000/01/27 22:00:00 (UTC) (Cartesian) X: -173128.041204 [km] Vx: 0.5539363428 [km/s] Y: -8107.069096 [km] Vy: -1.0195963126 [km/s] Z: 12703.691122 [km] Vz: -0.3089826594 [km/s] EPOCH : 2000/02/01 00:00:00 (UTC) (Cartesian) X: -173690.233269 [km] Vx: -0.4785223705 [km/s] Y: 83998.426912 [km] Vy: -0.8100201478 [km/s] Z: 36476.506074 [km] Vz: -0.1668267795 [km/s] EPOCH : 2000/03/01 00:00:00 (UTC) (Cartesian) X: 50548.402022 [km] Vx: -1.0821438234 [km/s] Y: 53593.136735 [km] Vy: 2.4304166549 [km/s] Z: 9268.851443 [km] Vz: 0.7164626772 [km/s] EPOCH : 2000/04/01 00:00:00 (UTC) (Cartesian) X: 50375.615386 [km] Vx: 1.4415836918 [km/s] Y: -26652.868948 [km] Vy: 2.8522390274 [km/s] Z: -11331.784191 [km] Vz: 0.6034232197 [km/s] From: SMTP%"hfranz@csc.com" 16-FEB-2000 10:03:54.13 To: SARDI CC: Subj: Re: Geotail elements X-Lotus-FromDomain: CSC From: hfranz@csc.com To: SARDI@nssdca.gsfc.nasa.gov Message-ID: <85256887.0052EF99.00@csc.com> Date: Wed, 16 Feb 2000 10:05:42 -0500 Subject: Re: Geotail elements Mime-Version: 1.0 Content-type: text/plain; charset=us-ascii Content-Disposition: inline Sardi, I've forwarded to you all Geotail monthly element sets since May 1999. It looks like both you and Frank were in the distribution list for the original messages, so maybe Mr. Matsuoka has an incorrect e-mail address for you. Heather SARDI@nssdca.gsfc.nasa.gov on 02/16/2000 08:50:06 AM To: Heather Franz/CIV/CSC@CSC cc: SARDI@nssdca.gsfc.nasa.gov Subject: Geotail elements Dear Heather, As you may have known, we used to store in an FTP site the orb elemnts of Geotail and many others. A Russian colleague of mine has alerted me that the site carries Geotail elements only up to May 99. Looks like Masutoshi Matsuoka (Matu@d1.nas.nec.co.jp) forgot to include my name since May 99! If you have received sets after May 99, could you transmit them to me? Many thanx, sardi --------------- From: SMTP%"matu@d1.nas.nec.co.jp" 23-FEB-2000 06:03:40.43 To: SARDI CC: Subj: Re: Geotail Elements To: SARDI@nssdca.gsfc.nasa.gov CC: matu@d1.nas.nec.co.jp Subject: Re: Geotail Elements X-Mailer: Mew version 1.94.1 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20000223200603I.matu@d1.nas.nec.co.jp> Date: Wed, 23 Feb 2000 20:06:03 +0900 (JST) From: Masatoshi Matsuoka X-Dispatcher: imput version 990905(IM130) Lines: 17 Dear Dr. Sardi I apologazed that not quickly response. I send updated elements to "sardi@ncf.span.nasa.gov" in last year and this january. I change your address to "SARDI@nssdca.gsfc.nasa.gov" from the next distribution(perhaps this weekend) . Best regards, Masatosi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka From: SMTP%"matu@d1.nas.nec.co.jp" 25-FEB-2000 06:07:24.48 To: SARDI CC: Subj: [MONTHLY] GEOTAIL Latest Orbit Data(2/25) To: SARDI@nssdca.gsfc.nasa.gov, stefan.waldherr@jpl.nasa.gov, jose.valencia@jpl.nasa.gov, hfranz@csc.com, FERRIER@nssdca.gsfc.nasa.gov CC: matu@d1.nas.nec.co.jp Subject: [MONTHLY] GEOTAIL Latest Orbit Data(2/25) X-Mailer: Mew version 1.94.1 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20000225200951C.matu@d1.nas.nec.co.jp> Date: Fri, 25 Feb 2000 20:09:51 +0900 (JST) From: Masatoshi Matsuoka X-Dispatcher: imput version 990905(IM130) Lines: 70 The following data is updated orbit solution based on 3 path data. GEOTAIL survive the longest eclipse(Feb. 21) in this season. The next eclipse seaon start on June 3. Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp - GEOTAIL STATE VECTOR ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 02 23 22 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -64579.923567 [km] Vx: 2.1132219202 [km/s] Y: -79479.223708 [km] Vy: -0.2042324164 [km/s] Z: -14676.837658 [km] Vz: -0.2369919347 [km/s] (Keplerian) a: 126854.082490 [km] an: 18.877248291 [deg] e: 0.551040931412 [ - ] ap: 318.322327923 [deg] i: 15.1224797409 [deg] ma: 319.307816473 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2000/02/23 22:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -64579.9235672970 2.1132219201885998 0.0000000000000000 Y: -79479.2237079450 -0.2042324164141900 0.0000000000000000 Z: -14676.8376576800 -0.2369919347179200 0.0000000000000000 EPOCH : 2000/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 50535.7663861721 -1.0827747180945251 0.0000000000000000 Y: 53604.8282230864 2.4301232303228812 0.0000000000000000 Z: 9279.1944772004 0.7164025121963487 0.0000000000000000 EPOCH : 2000/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 50354.5470083164 1.4428538847143442 0.0000000000000000 Y: -26695.8495470231 2.8515209384223414 0.0000000000000000 Z: -11336.6919724865 0.6033154633573529 0.0000000000000000 EPOCH : 2000/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -152459.3378483584 0.9687763119604939 0.0000000000000000 Y: -47774.2606547474 -0.8990093616893475 -0.0000000000000000 Z: 1567.8113994270 -0.3203899329910120 0.0000000000000000 EPOCH : 2000/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -165534.0786320254 0.7381808655591339 0.0000000000000000 Y: -32688.5135982581 -0.9646919852796298 -0.0000000000000000 Z: 7150.3181899096 -0.3193975107998843 0.0000000000000000 Date: Fri, 26 May 2000 15:41:33 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 60 The following data is updated orbit solution based on 3 path data. Best regards, == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp - GEOTAIL STATE VECTOR(J2000.0EQ GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 05 25 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -177672.577796 [km] Vx: -0.4450592736 [km/s] Y: 69568.147760 [km] Vy: -0.8576838050 [km/s] Z: 34675.506384 [km] Vz: -0.1800011254 [km/s] (Keplerian) a: 126756.242023 [km] an: 19.958394987 [deg] e: 0.533187936455 [ - ] ap: 321.102319420 [deg] i: 15.3828137685 [deg] ma: 170.337236124 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2000/05/25 14:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -177672.5777963500 -0.4450592736050900 0.0000000000000000 Y: 69568.1477602230 -0.8576838050045700 0.0000000000000000 Z: 34675.5063842400 -0.1800011253597900 0.0000000000000000 EPOCH : 2000/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -165444.7203934217 0.7402724152370578 0.0000000000000000 Y: -32898.2230994869 -0.9638620955318317 -0.0000000000000000 Z: 7045.7882209187 -0.3192958160587813 0.0000000000000000 EPOCH : 2000/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -178203.1166074168 -0.4202099953155641 0.0000000000000000 Y: 68238.5955734169 -0.8647577694454093 0.0000000000000000 Z: 35068.4154299961 -0.1817844572346023 0.0000000000000000 EPOCH : 2000/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -166734.9402774003 -0.6769593884577420 0.0000000000000000 Y: 88038.5943908276 -0.7395811162445709 0.0000000000000000 Z: 39441.9079346983 -0.1194516350567001 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 30-JUN-2000 02:58:54.32 To: SARDI CC: Subj: [MONTHLY] GEOTAIL Latest Orbit Data(2000/6)@hanako.d1.nas.nec.co.jp To: gtl_month@ayame.d1.nas.nec.co.jp Subject: [MONTHLY] GEOTAIL Latest Orbit Data(2000/6)@hanako.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20000630160026B.matu@d1.nas.nec.co.jp> Date: Fri, 30 Jun 2000 16:00:26 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 65 The following data is updated orbit solution based on 3 path data. Best regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp - GEOTAIL STATE VECTOR(J2000.0EQ Geo centric) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 06 29 07 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -16026.268566 [km] Vx: -1.6895826205 [km/s] Y: 115241.332844 [km] Vy: 0.7062637285 [km/s] Z: 31324.704435 [km] Vz: 0.3471259292 [km/s] (Keplerian) a: 126856.087094 [km] an: 20.681937028 [deg] e: 0.533089316038 [ - ] ap: 320.153076447 [deg] i: 15.4321591323 [deg] ma: 54.192901048 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2000/06/29 07:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -16026.2685661920 -1.6895826205180000 0.0000000000000000 Y: 115241.3328441500 0.7062637284708200 0.0000000000000000 Z: 31324.7044346450 0.3471259291507900 0.0000000000000000 EPOCH : 2000/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -178230.2082027560 -0.4199024855768000 0.0000000000000000 Y: 68183.9645378976 -0.8648797428720826 0.0000000000000000 Z: 35041.5034502900 -0.1818816754309352 0.0000000000000000 EPOCH : 2000/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -166767.5121746208 -0.6767173574459242 0.0000000000000000 Y: 87990.2830864244 -0.7397563906435861 0.0000000000000000 Z: 39418.1845145209 -0.1195731585832706 0.0000000000000000 EPOCH : 2000/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -155265.3300107649 -0.8425608695798874 0.0000000000000000 Y: 95438.7820766874 -0.6340770083477916 0.0000000000000000 Z: 40216.1075317566 -0.0716613245000603 0.0000000000000000 EPOCH : 2000/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -12018.1272230547 -1.8194428555958930 0.0000000000000000 Y: 105134.8189803709 0.8168626092326485 0.0000000000000000 Z: 28198.1739244996 0.4014350206395152 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 28-JUL-2000 08:54:18.04 To: SARDI CC: Subj: [MONTHLY] GEOTAIL Latest Orbit Data(2000/7) To: gtl_month@ayame.d1.nas.nec.co.jp Subject: [MONTHLY] GEOTAIL Latest Orbit Data(2000/7) X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20000728215807M.matu@d1.nas.nec.co.jp> Date: Fri, 28 Jul 2000 21:58:07 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 65 The following data is updated orbit solution based on 3 path data. Best regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp - GEOTAIL STATE VECTOR(J2000.0EQ) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 07 23 13 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -126132.061569 [km] Vx: 1.3384702286 [km/s] Y: -67861.885495 [km] Vy: -0.7286557322 [km/s] Z: -4751.108949 [km] Vz: -0.3205646898 [km/s] (Keplerian) a: 127037.614298 [km] an: 21.351520333 [deg] e: 0.539160088581 [ - ] ap: 320.697379306 [deg] i: 15.3727812602 [deg] ma: 286.265877023 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2000/07/23 13:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -126132.0615694900 1.3384702285554999 0.0000000000000000 Y: -67861.8854951020 -0.7286557321839900 0.0000000000000000 Z: -4751.1089493680 -0.3205646897885200 0.0000000000000000 EPOCH : 2000/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -166793.9512368931 -0.6764694418656109 0.0000000000000000 Y: 87953.1999213346 -0.7399100926319286 0.0000000000000000 Z: 39404.3581487753 -0.1196900991014213 0.0000000000000000 EPOCH : 2000/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -155308.1370518884 -0.8421786577153415 0.0000000000000000 Y: 95397.1473126282 -0.6343564578683484 0.0000000000000000 Z: 40203.5319948237 -0.0718304815562822 0.0000000000000000 EPOCH : 2000/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -12089.5823790962 -1.8195092646967186 0.0000000000000000 Y: 105154.5190039808 0.8156683387476464 0.0000000000000000 Z: 28211.8561225323 0.4010510942268438 0.0000000000000000 EPOCH : 2000/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 37576.2702376218 -1.5955728523851911 0.0000000000000000 Y: 67797.3663458333 1.9924794340142529 0.0000000000000000 Z: 13585.7334302363 0.6896713613950787 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 25-AUG-2000 01:55:20.11 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/08) To: gtl_month@ayame.d1.nas.nec.co.jp Reply-to: matu@d1.nas.nec.co.jp Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/08) X-Mailer: Mew version 1.94.2 on Emacs 20.7 / Mule 4.0 =?iso-2022-jp?B?KBskQjJWMWMbKEIp?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20000825145833W.matu@d1.nas.nec.co.jp> Date: Fri, 25 Aug 2000 14:58:33 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 49 The following data is updated orbit solution based on 3 path data. Best regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(J2000.0EQ GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 08 24 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -3517.711469 [km] Vx: 2.4436499169 [km/s] Y: -75550.246522 [km] Vy: 1.0562299802 [km/s] Z: -18804.391963 [km] Vz: 0.0164735823 [km/s] (Keplerian) a: 126871.372042 [km] an: 22.080493147 [deg] e: 0.551698322793 [ - ] ap: 322.142877539 [deg] i: 15.3107167629 [deg] ma: 336.959092697 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2000/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -155345.0570315008 -0.8419495568748547 0.0000000000000000 Y: 95354.6991883666 -0.6345751085568405 0.0000000000000000 Z: 40185.9613697864 -0.0720030369350585 0.0000000000000000 EPOCH : 2000/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -12046.4811327411 -1.8199348668338988 0.0000000000000000 Y: 105116.1140742100 0.8165106832364836 0.0000000000000000 Z: 28199.0804069839 0.4011740803618901 0.0000000000000000 EPOCH : 2000/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 37700.4222046518 -1.5934186092103138 0.0000000000000000 Y: 67624.2450642905 1.9971017824172499 0.0000000000000000 Z: 13532.0439286193 0.6905454073462305 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 29-SEP-2000 07:34:24.31 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/09/29) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/09/29) To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20000929204023M.matu@d1.nas.nec.co.jp> Date: Fri, 29 Sep 2000 20:40:23 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 48 The following data is updated orbit solution based on 3 path data. Best regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR J2000.0EQ ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 09 25 22 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -39207.066878 [km] Vx: -1.7158720540 [km/s] Y: 114254.276297 [km] Vy: 0.4266028008 [km/s] Z: 33151.801988 [km] Vz: 0.2888693738 [km/s] (Keplerian) a: 126352.316025 [km] an: 22.490283244 [deg] e: 0.559697508677 [ - ] ap: 323.277602952 [deg] i: 15.3749942612 [deg] ma: 57.051170811 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>> EPOCH : 2000/10/01 00:00:00 (UTC) (Cartesian) X: -12153.727136 [km] Vx: -1.8201695983 [km/s] Y: 105138.215381 [km] Vy: 0.8146963081 [km/s] Z: 28218.981363 [km] Vz: 0.4006051892 [km/s] EPOCH : 2000/11/01 00:00:00 (UTC) (Cartesian) X: 37570.322587 [km] Vx: -1.5962624399 [km/s] Y: 67761.482667 [km] Vy: 1.9929970589 [km/s] Z: 13587.164982 [km] Vz: 0.6897094371 [km/s] EPOCH : 2000/12/01 00:00:00 (UTC) (Cartesian) X: -98012.567240 [km] Vx: 1.6196900980 [km/s] Y: -88328.847715 [km] Vy: -0.4066979539 [km/s] Z: -12241.541033 [km] Vz: -0.2854274707 [km/s] EPOCH : 2001/01/01 00:00:00 (UTC) (Cartesian) X: -122474.516939 [km] Vx: 1.3597014809 [km/s] Y: -78789.029567 [km] Vy: -0.6099927723 [km/s] Z: -6513.779652 [km] Vz: -0.3144177263 [km/s] From: SMTP%"matu@d1.nas.nec.co.jp" 28-OCT-2000 03:46:56.99 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/10/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/10/28) To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20001028165512H.matu@d1.nas.nec.co.jp> Date: Sat, 28 Oct 2000 16:55:12 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 65 The following data is updated orbit solution based on 3 path data. Best regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(J2000.0EQ GEO CENTRIC) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 10 26 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: 57888.155011 [km] Vx: -0.4501396236 [km/s] Y: 20755.391067 [km] Vy: 2.9903790446 [km/s] Z: -811.515787 [km] Vz: 0.8227183447 [km/s] (Keplerian) a: 126928.335469 [km] an: 22.424109842 [deg] e: 0.538874195377 [ - ] ap: 326.739198463 [deg] i: 15.6539327312 [deg] ma: 7.949714780 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC)>>> EPOCH : 2000/10/26 14:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 57888.1550110470 -0.4501396236334300 0.0000000000000000 Y: 20755.3910673410 2.9903790446309002 0.0000000000000000 Z: -811.5157872424 0.8227183447002100 0.0000000000000000 EPOCH : 2000/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 37555.6838862227 -1.5967655096362259 0.0000000000000000 Y: 67763.9902856239 1.9927586420378196 0.0000000000000000 Z: 13593.5378430966 0.6896272654166792 0.0000000000000000 EPOCH : 2000/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -98122.5781249820 1.6184593854261726 0.0000000000000000 Y: -88320.5864301659 -0.4074910298909200 -0.0000000000000000 Z: -12236.0875268722 -0.2853881338284940 0.0000000000000000 EPOCH : 2001/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -122669.2836982022 1.3574235520302611 0.0000000000000000 Y: -78724.6646694285 -0.6112107421066895 -0.0000000000000000 Z: -6485.1952530096 -0.3143853315531645 0.0000000000000000 EPOCH : 2001/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147368.3030592013 1.0596491315544585 0.0000000000000000 Y: -66182.6482833296 -0.7547694051174465 -0.0000000000000000 Z: -15.8263456787 -0.3202808456137621 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 24-NOV-2000 01:35:52.46 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/11/24) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/11/24) To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20001124154239H.matu@d1.nas.nec.co.jp> Date: Fri, 24 Nov 2000 15:42:39 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 56 The following data is updated orbit solution based on 3 path data. Best regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(J2000.0EQ GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 11 22 21 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -108270.499191 [km] Vx: -1.3116329423 [km/s] Y: 109915.209210 [km] Vy: -0.3514581349 [km/s] Z: 40474.759345 [km] Vz: 0.0522905715 [km/s] (Keplerian) a: 126487.270969 [km] an: 22.837409154 [deg] e: 0.537484895763 [ - ] ap: 326.756274149 [deg] i: 15.7700565757 [deg] ma: 92.136787886 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC)>>> EPOCH : 2000/11/22 21:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -108270.4991906800 -1.3116329423234001 0.0000000000000000 Y: 109915.2092098000 -0.3514581349018800 0.0000000000000000 Z: 40474.7593446920 0.0522905715020210 0.0000000000000000 EPOCH : 2000/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -97914.6395304702 1.6205004375616885 0.0000000000000000 Y: -88386.5938778840 -0.4054338206792317 -0.0000000000000000 Z: -12285.9871002636 -0.2849829046664799 0.0000000000000000 EPOCH : 2001/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -122379.3567022445 1.3606955504258467 0.0000000000000000 Y: -78870.6711594872 -0.6089650754610271 -0.0000000000000000 Z: -6567.7370644962 -0.3141043559833094 0.0000000000000000 EPOCH : 2001/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147084.4712708795 1.0633102017413949 0.0000000000000000 Y: -66404.6197707129 -0.7530157205685637 -0.0000000000000000 Z: -119.4089614638 -0.3202060309669246 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 22-DEC-2000 00:31:02.65 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/12/22) To: gtl_month@ayame.d1.nas.nec.co.jp Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2000/12/22) X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20001222143810P.matu@d1.nas.nec.co.jp> Date: Fri, 22 Dec 2000 14:38:10 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 56 The following data is updated orbit solution based on 3 path data. This update is the last data in this year. Merry Xmas and a happy new millennium. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(J2000.0EQ GEO centric) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2000 12 20 22 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -177901.973711 [km] Vx: 0.5526232646 [km/s] Y: -31806.182065 [km] Vy: -0.9272061796 [km/s] Z: 11779.409753 [km] Vz: -0.3041149844 [km/s] (Keplerian) a: 126771.256206 [km] an: 23.399303609 [deg] e: 0.536143114055 [ - ] ap: 325.439996473 [deg] i: 15.8602880369 [deg] ma: 235.379303618 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2000/12/20 22:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -177901.9737112200 0.5526232645969600 0.0000000000000000 Y: -31806.1820652060 -0.9272061795555300 0.0000000000000000 Z: 11779.4097533230 -0.3041149844461800 0.0000000000000000 EPOCH : 2001/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -122341.7887655387 1.3610716639697471 0.0000000000000000 Y: -78910.7258429261 -0.6084834627152037 -0.0000000000000000 Z: -6595.7530348898 -0.3139288246124629 0.0000000000000000 EPOCH : 2001/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147043.6456928062 1.0638605616306531 0.0000000000000000 Y: -66485.1680474847 -0.7524150686794925 -0.0000000000000000 Z: -173.6107897305 -0.3199911821514207 0.0000000000000000 EPOCH : 2001/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 3703.4544375961 -1.9349284728264726 0.0000000000000000 Y: 90877.3251328459 1.1516049577696952 0.0000000000000000 Z: 23295.4620891984 0.5296154977050683 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 26-JAN-2001 07:22:48.77 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/01/26) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/01/26) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010126213449A.matu@d1.nas.nec.co.jp> Date: Fri, 26 Jan 2001 21:34:49 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 107 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(J2000.0EQ) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 01 25 21 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -191759.270086 [km] Vx: 0.1193769981 [km/s] Y: 4797.972269 [km] Vy: -0.9498225982 [km/s] Z: 23603.070470 [km] Vz: -0.2613020009 [km/s] (Keplerian) a: 126934.849149 [km] an: 24.111539873 [deg] e: 0.543511165749 [ - ] ap: 324.852750044 [deg] i: 15.9261788664 [deg] ma: 204.522927645 [deg] ------ <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/01/25 21:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -191759.2700857000 0.1193769980987800 0.0000000000000000 Y: 4797.9722693602 -0.9498225981833500 0.0000000000000000 Z: 23603.0704702840 -0.2613020009311900 0.0000000000000000 EPOCH : 2001/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147042.6260562211 1.0638639340322678 0.0000000000000000 Y: -66485.0561954937 -0.7524289520365113 -0.0000000000000000 Z: -173.4159335023 -0.3199938289275155 0.0000000000000000 EPOCH : 2001/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 3706.8452433258 -1.9349022897327812 0.0000000000000000 Y: 90877.2307053570 1.1516508613841534 0.0000000000000000 Z: 23294.7806473035 0.5296225648491727 0.0000000000000000 EPOCH : 2001/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 38889.8496212090 -1.6162585975451182 0.0000000000000000 Y: 56441.8318227780 2.2619600414453056 0.0000000000000000 Z: 10246.9344139590 0.7918209824057376 0.0000000000000000 EPOCH : 2001/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -193281.1405626627 -0.0226371662035535 0.0000000000000000 Y: 2489.5423282521 -0.9336998378920764 -0.0000000000000000 Z: 25590.0221355299 -0.2536202738644504 0.0000000000000000 EPOCH : 2001/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -70997.7868776831 -1.7644231976105873 0.0000000000000000 Y: 97535.1531778735 -0.0716195542466095 0.0000000000000000 Z: 37407.0911436053 0.2181671501992647 0.0000000000000000 EPOCH : 2002/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -66014.4207481950 1.7268425934732039 0.0000000000000000 Y: -108406.4966527833 0.1001476683363375 0.0000000000000000 Z: -23275.9726685247 -0.2199052742291963 0.0000000000000000 EPOCH : 2002/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -25366.7571800792 -2.1971888824455297 0.0000000000000000 Y: 85448.3288868046 0.4797242943125729 0.0000000000000000 Z: 31415.4816791690 0.4898915959501698 0.0000000000000000 EPOCH : 2002/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -179526.7721449895 0.4972936775741232 0.0000000000000000 Y: -69191.5128887443 -0.7938440595047991 -0.0000000000000000 Z: 5561.3827512375 -0.3528765669538315 0.0000000000000000 EPOCH : 2002/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -141894.4216305260 -1.1376502419400512 0.0000000000000000 Y: 52556.2954745165 -0.7844533718631631 0.0000000000000000 Z: 43222.7222370163 -0.0916133259811976 0.0000000000000000 EPOCH : 2003/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 2481.4700794918 1.7518590898197879 0.0000000000000000 Y: -97235.4083763263 1.1753856836240306 0.0000000000000000 Z: -38928.5093190676 0.1421533655304170 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 23-FEB-2001 05:51:08.66 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/02/23) To: gtl_month@ayame.d1.nas.nec.co.jp Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/02/23) X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010223195238N.matu@d1.nas.nec.co.jp> Date: Fri, 23 Feb 2001 19:52:38 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 56 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(J2000.0EQ) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 02 21 20 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -154921.011975 [km] Vx: 0.9659376889 [km/s] Y: -64101.597759 [km] Vy: -0.7633932404 [km/s] Z: 1612.385516 [km] Vz: -0.3131717070 [km/s] (Keplerian) a: 126910.729417 [km] an: 24.404003072 [deg] e: 0.552847898264 [ - ] ap: 327.106012454 [deg] i: 15.9705461898 [deg] ma: 260.271190310 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/02/21 20:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -154921.0119754400 0.9659376889403700 0.0000000000000000 Y: -64101.5977589690 -0.7633932403526900 0.0000000000000000 Z: 1612.3855164872 -0.3131717070296600 0.0000000000000000 EPOCH : 2001/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 3707.5227096325 -1.9348844345654130 0.0000000000000000 Y: 90878.4197927416 1.1516590443000909 0.0000000000000000 Z: 23293.4487978360 0.5295971946364487 0.0000000000000000 EPOCH : 2001/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 38889.3336228970 -1.6162728495706866 0.0000000000000000 Y: 56444.2614421910 2.2619086800644213 0.0000000000000000 Z: 10246.7274385486 0.7917645604455970 0.0000000000000000 EPOCH : 2001/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -93382.7709317840 1.6235297861339613 0.0000000000000000 Y: -95674.2217600322 -0.2658865115064815 -0.0000000000000000 Z: -14320.3926595605 -0.2708601324199389 0.0000000000000000 ********NOTE: THESE VECTORS BELOW REPLACE Sep 94 - Mar 95 VECTORS.****** From: SMTP%"matu@d1.nas.nec.co.jp" 16-MAR-2001 12:16:40.91 To: SARDI CC: Subj: Re: Geotail To: SARDI@nssdca.gsfc.nasa.gov Cc: matu@d1.nas.nec.co.jp Reply-To: matu@d1.nas.nec.co.jp Subject: Re: Geotail In-Reply-To: <010312151106.16464ac@nssdca.gsfc.nasa.gov> References: <010312151106.16464ac@nssdca.gsfc.nasa.gov> X-Mailer: Mew version 1.94.2 on Emacs 19.28 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010317021751J.matu@net203.newslan.isas.ac.jp> Date: Sat, 17 Mar 2001 02:17:51 +0900 (JST) From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 131 From: "r.parthasarathy,nssdc/wdc/gsfc/nasa" Subject: Re: Geotail Date: Mon, 12 Mar 2001 15:11:06 -0500 Dear Sardi, The Geotail state vector is attached the end of this mail. I expect this data makes good result. Masatoshi. == Masatoshi Matsuoka(matu@d1.nas.nec.co.jp) NEC Aerospace Systems. -------- data ----------------------------------------- The executed maneuver dates are shown as Table-1 and Table-2 shows each state vector(J2000.0EQ). Table-1: delta-v epoch between from Sep.'94 to Mar.'95 ------------------------------------------------- DV14 EPOCH : 1994/09/19 12:30:00 (UTC) DVT14 EPOCH : 1994/10/17 13:00:00 (UTC) DV15 EPOCH : 1994/11/04 18:00:00 (UTC) DV16-1 EPOCH : 1994/11/12 03:40:00 (UTC) -2 EPOCH : 1994/11/12 06:30:00 (UTC) -3 EPOCH : 1994/11/12 09:20:00 (UTC) DV17-1 EPOCH : 1995/02/19 18:10:00 (UTC) -2 EPOCH : 1995/02/19 21:00:00 (UTC) -3 EPOCH : 1995/02/19 23:50:00 (UTC) DV18-1 EPOCH : 1995/02/26 20:10:00 (UTC) -2 EPOCH : 1995/02/26 23:10:00 (UTC) -3 EPOCH : 1995/02/27 02:10:00 (UTC) -------------------------------------------------- Table-2: state vector(post delta-v) <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000.0EQ;GEO-CENTRIC) >>> EPOCH : 1994/09/19 12:30:00 (UTC) (Cartesian) X: 1082240.234720 [km] Vx: 0.0863684506 [km/s] DV14 Y: -312903.617553 [km] Vy: 0.3608340098 [km/s] Z: -48204.212859 [km] Vz: 0.1361586227 [km/s] EPOCH : 1994/10/17 13:00:00 (UTC) (Cartesian) X: 473694.652648 [km] Vx: -0.6781818101 [km/s] DVT14 Y: 516389.094928 [km] Vy: 0.1350763672 [km/s] Z: 201871.627797 [km] Vz: 0.0035123081 [km/s] EPOCH : 1994/11/04 18:00:00 (UTC) (Cartesian) X: 50390.731944 [km] Vx: -0.4949029707 [km/s] DV15 Y: 382512.491517 [km] Vy: 0.2074390861 [km/s] Z: 108602.398491 [km] Vz: 0.0391709310 [km/s] EPOCH : 1994/11/12 03:40:00 (UTC) (Cartesian) X: -26530.593081 [km] Vx: 3.2100075006 [km/s] DV16-1 Y: -53632.058531 [km] Vy: -0.8546183261 [km/s] Z: -15832.559500 [km] Vz: -0.1296296688 [km/s] EPOCH : 1994/11/12 06:30:00 (UTC) (Cartesian) X: 7621.161579 [km] Vx: 3.3485851169 [km/s] DV16-2 Y: -57121.792211 [km] Vy: 0.1997870475 [km/s] Z: -15651.314070 [km] Vz: 0.1677352363 [km/s] EPOCH : 1994/11/12 09:20:00 (UTC) (Cartesian) X: 40096.786221 [km] Vx: 2.9275856905 [km/s] DV16-3 Y: -49990.359652 [km] Vy: 1.1341213113 [km/s] Z: -12578.224871 [km] Vz: 0.4135420144 [km/s] EPOCH : 1994/11/17 22:00:00 (UTC) (Cartesian) X: -55748.289425 [km] Vx: -0.5990302798 [km/s] (no-DV) Y: 275699.594619 [km] Vy: -0.4094083856 [km/s] Z: 75170.079524 [km] Vz: -0.1327402848 [km/s] EPOCH : 1994/12/07 22:00:00 (UTC) (Cartesian) X: -130671.519130 [km] Vx: -0.0641957102 [km/s] (no-DV) Y: 133949.074835 [km] Vy: -1.3657863425 [km/s] Z: 34442.840722 [km] Vz: -0.3834089758 [km/s] EPOCH : 1994/12/21 19:00:00 (UTC) (Cartesian) X: 47447.441485 [km] Vx: -0.5949022213 [km/s] (no-DV) Y: 286225.525471 [km] Vy: 0.3218517292 [km/s] Z: 81044.412737 [km] Vz: 0.0800823760 [km/s] EPOCH : 1995/01/04 20:00:00 (UTC) (Cartesian) X: -112750.551321 [km] Vx: 0.9369749920 [km/s] (no-DV) Y: 26328.048500 [km] Vy: -1.8864272023 [km/s] Z: 6276.399976 [km] Vz: -0.5195396910 [km/s] EPOCH : 1995/01/26 14:00:00 (UTC) (Cartesian) X: 75388.486725 [km] Vx: -0.5745492167 [km/s] (no-DV) Y: 265946.166071 [km] Vy: 0.5315081528 [km/s] Z: 74827.097324 [km] Vz: 0.1479010870 [km/s] EPOCH : 1995/02/09 18:00:00 (UTC) (Cartesian) X: -136611.608923 [km] Vx: 0.2506669450 [km/s] (no-DV) Y: 84531.604940 [km] Vy: -1.5748725548 [km/s] Z: 24071.502522 [km] Vz: -0.4417214861 [km/s] EPOCH : 1995/02/19 18:10:00 (UTC) (Cartesian) X: -32909.819989 [km] Vx: 2.9200359999 [km/s] DV17-1 Y: -58027.469845 [km] Vy: -0.8786246634 [km/s] Z: -16139.050014 [km] Vz: -0.2571414978 [km/s] EPOCH : 1995/02/19 21:00:00 (UTC) (Cartesian) X: -1584.326302 [km] Vx: 3.1213358652 [km/s] DV17-2 Y: -62827.381866 [km] Vy: -0.0303943170 [km/s] Z: -17601.285694 [km] Vz: -0.0202491253 [km/s] EPOCH : 1995/02/19 23:50:00 (UTC) (Cartesian) X: 29605.096659 [km] Vx: 2.9082516193 [km/s] DV17-3 Y: -58570.037037 [km] Vy: 0.8393248285 [km/s] Z: -16525.393072 [km] Vz: 0.2242595254 [km/s] EPOCH : 1995/02/26 20:10:00 (UTC) (Cartesian) X: -32684.041615 [km] Vx: 2.8364360614 [km/s] DV18-1 Y: -57998.986402 [km] Vy: -0.8866323420 [km/s] Z: -16066.098147 [km] Vz: -0.2627710415 [km/s] EPOCH : 1995/02/26 23:10:00 (UTC) (Cartesian) X: -357.317825 [km] Vx: 3.0455421956 [km/s] DV18-2 Y: -62886.092241 [km] Vy: 0.0142223772 [km/s] Z: -17600.368233 [km] Vz: -0.0108922131 [km/s] EPOCH : 1995/02/27 02:10:00 (UTC) (Cartesian) X: 31684.356099 [km] Vx: 2.7831799942 [km/s] DV18-3 Y: -57643.198552 [km] Vy: 0.9261459535 [km/s] Z: -16289.328079 [km] Vz: 0.2464072272 [km/s] From: SMTP%"matu@d1.nas.nec.co.jp" 30-MAR-2001 03:59:44.21 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/03/30) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/03/30) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010330180345V.matu@d1.nas.nec.co.jp> Date: Fri, 30 Mar 2001 18:03:45 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 53 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(J2000.0EQ) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 03 29 13 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -192761.972509 [km] Vx: 0.2363189984 [km/s] Y: -14570.240923 [km] Vy: -0.9107876426 [km/s] Z: 19242.539414 [km] Vz: -0.2683988695 [km/s] (Keplerian) a: 126692.170116 [km] an: 24.430501283 [deg] e: 0.558804887790 [ - ] ap: 329.854828788 [deg] i: 16.1479393599 [deg] ma: 206.897820514 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/03/29 13:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -192761.9725085400 0.2363189983785100 0.0000000000000000 Y: -14570.2409232780 -0.9107876425722300 0.0000000000000000 Z: 19242.5394141180 -0.2683988694681300 0.0000000000000000 EPOCH : 2001/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 38888.4263303645 -1.6162846777580686 0.0000000000000000 Y: 56446.3740448053 2.2618864328590131 0.0000000000000000 Z: 10245.8713283412 0.7916885219445409 0.0000000000000000 EPOCH : 2001/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -93376.2544459542 1.6236040931547437 0.0000000000000000 Y: -95674.0245180715 -0.2658445284733292 -0.0000000000000000 Z: -14318.5840008279 -0.2708453486492977 0.0000000000000000 EPOCH : 2001/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -132348.6712789652 1.2033562630388095 0.0000000000000000 Y: -87742.7913923098 -0.5787192253184295 -0.0000000000000000 Z: -7459.2038216575 -0.3104926082147613 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 27-APR-2001 04:38:38.88 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/04/27) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/04/27) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010427173358D.matu@d1.nas.nec.co.jp> Date: Fri, 27 Apr 2001 17:33:58 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 58 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(GEO CENTRIC J2000.0EQ) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 04 25 18 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -101466.299591 [km] Vx: 1.5420722518 [km/s] Y: -94991.888702 [km] Vy: -0.3366543636 [km/s] Z: -13208.574020 [km] Vz: -0.2787480049 [km/s] (Keplerian) a: 126909.411229 [km] an: 24.363365699 [deg] e: 0.546382192083 [ - ] ap: 331.039959606 [deg] i: 16.4706071898 [deg] ma: 290.213959549 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/04/25 18:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -101466.2995907200 1.5420722517612000 0.0000000000000000 Y: -94991.8887016430 -0.3366543636079200 0.0000000000000000 Z: -13208.5740195590 -0.2787480049472100 0.0000000000000000 EPOCH : 2001/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -93381.9665606042 1.6235597019430938 0.0000000000000000 Y: -95671.4962877457 -0.2658955436552801 -0.0000000000000000 Z: -14322.9606320805 -0.2708508771446435 0.0000000000000000 EPOCH : 2001/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -132356.9783998700 1.2032730132644445 0.0000000000000000 Y: -87737.4760712862 -0.5787729712147291 -0.0000000000000000 Z: -7462.4455390525 -0.3105121252209154 0.0000000000000000 EPOCH : 2001/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -193280.8127246245 -0.0225935500264003 0.0000000000000000 Y: 2490.4256756047 -0.9337060889516217 -0.0000000000000000 Z: 25587.2769618233 -0.2536275916963927 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 25-MAY-2001 03:39:43.19 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/05/25) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/05/25) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010525163804M.matu@d1.nas.nec.co.jp> Date: Fri, 25 May 2001 16:38:04 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 64 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp GEOTAIL STATE VECTOR(J2000.0EQ:GEOCENTRIC) ~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 05 24 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -157165.789985 [km] Vx: -0.8692038102 [km/s] Y: 74454.030857 [km] Vy: -0.7466569804 [km/s] Z: 40050.180731 [km] Vz: -0.0960147368 [km/s] (Keplerian) a: 126747.275420 [km] an: 24.512748257 [deg] e: 0.533248164682 [ - ] ap: 331.675761577 [deg] i: 16.7644320223 [deg] ma: 120.247793315 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/05/24 14:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -157165.7899846100 -0.8692038101983000 0.0000000000000000 Y: 74454.0308570130 -0.7466569803563200 0.0000000000000000 Z: 40050.1807310170 -0.0960147367607310 0.0000000000000000 EPOCH : 2001/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -132360.2771281240 1.2032500078924508 0.0000000000000000 Y: -87734.1712331426 -0.5787859213694646 -0.0000000000000000 Z: -7463.9027621221 -0.3105321249243183 0.0000000000000000 EPOCH : 2001/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -193281.7084619936 -0.0226488187305108 0.0000000000000000 Y: 2496.5159982823 -0.9336872613877825 -0.0000000000000000 Z: 25589.1188166683 -0.2536457745966253 0.0000000000000000 EPOCH : 2001/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -192699.3452419016 -0.1704576659239707 0.0000000000000000 Y: 16421.9629606947 -0.9180332368224438 0.0000000000000000 Z: 29953.0005416006 -0.2308962974130619 0.0000000000000000 EPOCH : 2001/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -188395.3585412372 -0.3885251390293857 0.0000000000000000 Y: 32327.1171153287 -0.8854698512199350 0.0000000000000000 Z: 34202.6935287402 -0.1959851615969169 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 29-JUN-2001 05:01:18.49 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/06/29) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/06/29) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010629180001G.matu@d1.nas.nec.co.jp> Date: Fri, 29 Jun 2001 18:00:01 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 65 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------ GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 06 27 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -65344.872011 [km] Vx: 1.8362728518 [km/s] Y: -100303.984685 [km] Vy: 0.0587194625 [km/s] Z: -19128.072119 [km] Vz: -0.2203392063 [km/s] (Keplerian) a: 126457.952306 [km] an: 25.124762513 [deg] e: 0.543485397615 [ - ] ap: 332.113305358 [deg] i: 16.8719389979 [deg] ma: 305.411704875 [deg] -- <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/06/27 14:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -65344.8720105490 1.8362728518039999 0.0000000000000000 Y: -100303.9846853000 0.0587194625314660 0.0000000000000000 Z: -19128.0721193520 -0.2203392062930700 0.0000000000000000 EPOCH : 2001/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -193282.6009458281 -0.0225946044168878 0.0000000000000000 Y: 2491.6330773662 -0.9336827697403455 -0.0000000000000000 Z: 25590.4268998259 -0.2536191086523167 0.0000000000000000 EPOCH : 2001/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -192701.7790050232 -0.1703538737377509 0.0000000000000000 Y: 16412.6874818409 -0.9180370473806765 0.0000000000000000 Z: 29952.9618540212 -0.2308775542208566 0.0000000000000000 EPOCH : 2001/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -188401.3960254153 -0.3883845694948563 0.0000000000000000 Y: 32314.7827701464 -0.8854886829141377 0.0000000000000000 Z: 34201.7656309735 -0.1959745119294151 0.0000000000000000 EPOCH : 2001/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -71027.8629697369 -1.7641580925740166 0.0000000000000000 Y: 97536.2640157485 -0.0718975361870519 0.0000000000000000 Z: 37410.9921594857 0.2180485107448029 0.0000000000000000 ayame{matu}102: From: SMTP%"matu@d1.nas.nec.co.jp" 27-JUL-2001 00:45:42.87 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/07/27) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/07/27) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010727134902I.matu@d1.nas.nec.co.jp> Date: Fri, 27 Jul 2001 13:49:02 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 63 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------ GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 07 26 10 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -182349.108393 [km] Vx: -0.5009108601 [km/s] Y: 45161.139889 [km] Vy: -0.8578156750 [km/s] Z: 36268.012712 [km] Vz: -0.1695396565 [km/s] (Keplerian) a: 126492.207510 [km] an: 25.541391096 [deg] e: 0.552734120379 [ - ] ap: 331.202646298 [deg] i: 16.9002895800 [deg] ma: 146.167841991 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/07/26 10:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -182349.1083927900 -0.5009108601100000 0.0000000000000000 Y: 45161.1398886320 -0.8578156749566400 0.0000000000000000 Z: 36268.0127117130 -0.1695396564645400 0.0000000000000000 EPOCH : 2001/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -192702.6517339308 -0.1703585486093077 0.0000000000000000 Y: 16412.5927889689 -0.9180257402249031 0.0000000000000000 Z: 29953.4731003370 -0.2308808360168667 0.0000000000000000 EPOCH : 2001/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -188401.2771230069 -0.3884117601287677 0.0000000000000000 Y: 32316.5551285676 -0.8854739386367032 0.0000000000000000 Z: 34202.7748891391 -0.1959735159669719 0.0000000000000000 EPOCH : 2001/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -71018.9093127686 -1.7642381892963832 0.0000000000000000 Y: 97535.5926228040 -0.0717940933573059 0.0000000000000000 Z: 37410.5385688973 0.2180905459730865 0.0000000000000000 EPOCH : 2001/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -37832.7395158337 -2.0262115114668973 0.0000000000000000 Y: 93663.1021730650 0.3334853646874665 0.0000000000000000 Z: 32543.1210650033 0.3768680700963247 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 30-AUG-2001 03:49:19.55 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/08/30) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/08/30) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010830165103G.matu@d1.nas.nec.co.jp> Date: Thu, 30 Aug 2001 16:51:03 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 63 The following data is updated orbit solution based on 2 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------ GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 08 28 07 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: (Cartesian) X: -149886.193816 [km] Vx: 1.0095754575 [km/s] Y: -79702.858928 [km] Vy: -0.6594014635 [km/s] Z: -2311.753108 [km] Vz: -0.3191139566 [km/s] (Keplerian) a: 126953.812385 [km] an: 25.483810670 [deg] e: 0.551060247802 [ - ] ap: 333.069218905 [deg] i: 17.2199370088 [deg] ma: 257.226446604 [deg] _ <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/08/28 07:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -149886.1938159900 1.0095754575345000 0.0000000000000000 Y: -79702.8589276990 -0.6594014634990100 0.0000000000000000 Z: -2311.7531083139 -0.3191139566226700 0.0000000000000000 EPOCH : 2001/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -188402.4838399479 -0.3884002881853749 0.0000000000000000 Y: 32314.4383327133 -0.8854731174795087 0.0000000000000000 Z: 34201.7786452258 -0.1959682516651505 0.0000000000000000 EPOCH : 2001/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -71019.2089613694 -1.7642525691642248 0.0000000000000000 Y: 97534.5249049002 -0.0717946193354440 0.0000000000000000 Z: 37409.3638671748 0.2180903452477491 0.0000000000000000 EPOCH : 2001/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -37831.1603884128 -2.0262436347331469 0.0000000000000000 Y: 93661.7296900384 0.3335166901700938 0.0000000000000000 Z: 32541.6905871179 0.3768762726359720 0.0000000000000000 EPOCH : 2001/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -21063.6961362875 1.9865782726036785 0.0000000000000000 Y: -98562.8240141603 0.7490214670686353 0.0000000000000000 Z: -26483.6298191449 -0.0574098379810612 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 28-SEP-2001 03:30:40.10 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/09/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/09/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20010928163618G.matu@d1.nas.nec.co.jp> Date: Fri, 28 Sep 2001 16:36:18 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 64 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 09 25 21 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -82516.621616 [km] Vx: -1.6631136078 [km/s] Y: 97438.634200 [km] Vy: -0.1898974174 [km/s] Z: 38886.047839 [km] Vz: 0.1707117379 [km/s] (Keplerian) a: 126880.633199 [km] an: 25.398691226 [deg] e: 0.559891812655 [ - ] ap: 335.852485486 [deg] i: 17.4890149407 [deg] ma: 63.384783090 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/09/25 21:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -82516.6216155780 -1.6631136078186000 0.0000000000000000 Y: 97438.6342001280 -0.1898974173621500 0.0000000000000000 Z: 38886.0478390760 0.1707117379260700 0.0000000000000000 EPOCH : 2001/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -71025.4785192835 -1.7642158565992654 0.0000000000000000 Y: 97532.8104218100 -0.0718738736508330 0.0000000000000000 Z: 37409.6212311423 0.2180890428255920 0.0000000000000000 EPOCH : 2001/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -37850.4136420035 -2.0261411263495024 0.0000000000000000 Y: 93663.7017933759 0.3332130444557059 0.0000000000000000 Z: 32544.5229977691 0.3768000432140207 0.0000000000000000 EPOCH : 2001/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -21037.9450494227 1.9866576910569693 0.0000000000000000 Y: -98553.8590537961 0.7494879177052426 0.0000000000000000 Z: -26483.4138778524 -0.0573184399590028 0.0000000000000000 EPOCH : 2002/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -65976.0718150615 1.7271536296858840 0.0000000000000000 Y: -108401.1105655195 0.1006348243621514 0.0000000000000000 Z: -23277.9611424616 -0.2198257284093545 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 26-OCT-2001 01:46:51.60 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/10/26) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/10/26) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20011026144657G.matu@d1.nas.nec.co.jp> Date: Fri, 26 Oct 2001 14:46:57 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 55 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 10 25 08 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -69602.473875 [km] Vx: 1.7392126973 [km/s] Y: -105300.237800 [km] Vy: 0.0877632235 [km/s] Z: -21026.870734 [km] Vz: -0.2137781502 [km/s] (Keplerian) a: 126474.699724 [km] an: 25.332868585 [deg] e: 0.560409514978 [ - ] ap: 337.541181693 [deg] i: 17.8249926608 [deg] ma: 300.898044431 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/10/25 08:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -69602.4738753820 1.7392126972937001 0.0000000000000000 Y: -105300.2377996100 0.0877632234807500 0.0000000000000000 Z: -21026.8707335540 -0.2137781502143000 0.0000000000000000 EPOCH : 2001/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -37837.5005941474 -2.0262316458334317 0.0000000000000000 Y: 93660.8930535618 0.3334021206082446 0.0000000000000000 Z: 32543.4219324282 0.3768491609191370 0.0000000000000000 EPOCH : 2001/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -21059.2091448278 1.9865622254194115 0.0000000000000000 Y: -98562.5444689138 0.7491041304462079 0.0000000000000000 Z: -26485.2346169084 -0.0573787602731171 0.0000000000000000 EPOCH : 2002/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -66004.0092240701 1.7269451177976467 0.0000000000000000 Y: -108403.3354471999 0.1003068800305830 0.0000000000000000 Z: -23277.5403326351 -0.2198696259842990 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 30-NOV-2001 00:59:40.78 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/11/30) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/11/30) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20011130150026Y.matu@d1.nas.nec.co.jp> Date: Fri, 30 Nov 2001 15:00:26 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 61 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 11 27 20 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -144593.427214 [km] Vx: -1.0604860684 [km/s] Y: 71243.769667 [km] Vy: -0.7172718330 [km/s] Z: 41652.370406 [km] Vz: -0.0639548451 [km/s] (Keplerian) a: 126734.020855 [km] an: 25.360060968 [deg] e: 0.542829412431 [ - ] ap: 338.430093236 [deg] i: 18.2508570576 [deg] ma: 99.915401690 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/11/27 20:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -144593.4272138100 -1.0604860683638000 0.0000000000000000 Y: 71243.7696666860 -0.7172718329533200 0.0000000000000000 Z: 41652.3704057520 -0.0639548450579790 0.0000000000000000 EPOCH : 2001/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -21057.2048743864 1.9865493440201143 0.0000000000000000 Y: -98563.5171031845 0.7491167980159703 0.0000000000000000 Z: -26485.1314973257 -0.0573454388848248 0.0000000000000000 EPOCH : 2002/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -66001.0097133015 1.7269527208285815 0.0000000000000000 Y: -108404.6198723152 0.1003279211622809 0.0000000000000000 Z: -23278.2742771797 -0.2198347105722727 0.0000000000000000 EPOCH : 2002/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -110688.6694561604 1.3724809826588189 0.0000000000000000 Y: -104273.9347504846 -0.2975821187502091 -0.0000000000000000 Z: -15464.8396626942 -0.2926955383147746 0.0000000000000000 EPOCH : 2002/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -87912.9616178469 -1.6671060507998579 0.0000000000000000 Y: 89592.6923328633 -0.2848737210382391 0.0000000000000000 Z: 40609.1819334092 0.1600294705433400 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 28-DEC-2001 01:15:00.76 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/12/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2001/12/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20011228150958J.matu@d1.nas.nec.co.jp> Date: Fri, 28 Dec 2001 15:09:58 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 63 The following data is updated orbit solution based on 3 path data. And.... A Happy New Year!! regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2001 12 27 05 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: 1373.016912 [km] Vx: 2.0141622150 [km/s] Y: -88833.527031 [km] Vy: 1.1763429995 [km/s] Z: -27108.594169 [km] Vz: 0.0652317302 [km/s] (Keplerian) a: 127043.449350 [km] an: 25.506937155 [deg] e: 0.532752822662 [ - ] ap: 338.719954277 [deg] i: 18.5539030465 [deg] ma: 326.660269415 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2001/12/27 05:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 1373.0169118890 2.0141622149690002 0.0000000000000000 Y: -88833.5270311180 1.1763429994857999 0.0000000000000000 Z: -27108.5941689420 0.0652317301575720 0.0000000000000000 EPOCH : 2002/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -66000.8491716926 1.7269405191580438 0.0000000000000000 Y: -108405.5305271847 0.1003260101982927 0.0000000000000000 Z: -23278.0876857966 -0.2198649845775018 0.0000000000000000 EPOCH : 2002/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -110692.3353542197 1.3724357382400278 0.0000000000000000 Y: -104274.0132343242 -0.2976181492886654 -0.0000000000000000 Z: -15463.2087173751 -0.2927277933151250 0.0000000000000000 EPOCH : 2002/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -87899.4084328946 -1.6672167790004697 0.0000000000000000 Y: 89594.7897442367 -0.2847686078260768 0.0000000000000000 Z: 40610.2894263358 0.1601061529357743 0.0000000000000000 EPOCH : 2002/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -25374.4315033607 -2.1971739878714831 0.0000000000000000 Y: 85448.3104252539 0.4795972607006960 0.0000000000000000 Z: 31417.0667489073 0.4898506560473496 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 27-JAN-2002 20:39:54.94 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/1/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/1/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20020128103923P.matu@d1.nas.nec.co.jp> Date: Mon, 28 Jan 2002 10:39:23 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 57 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 01 24 18 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -181891.733107 [km] Vx: -0.5026843955 [km/s] Y: 29813.348520 [km] Vy: -0.8991527448 [km/s] Z: 35748.016004 [km] Vz: -0.2003881365 [km/s] (Keplerian) a: 126754.062800 [km] an: 25.681728867 [deg] e: 0.544931846628 [ - ] ap: 338.939731800 [deg] i: 18.6864974244 [deg] ma: 137.373819704 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/01/24 18:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -181891.7331065900 -0.5026843954806300 0.0000000000000000 Y: 29813.3485203600 -0.8991527447877800 0.0000000000000000 Z: 35748.0160039740 -0.2003881364554500 0.0000000000000000 EPOCH : 2002/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -110687.4798690657 1.3724719288649068 0.0000000000000000 Y: -104276.3978652514 -0.2976036028907410 -0.0000000000000000 Z: -15460.8292379962 -0.2926949952803237 0.0000000000000000 EPOCH : 2002/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -87902.5207058663 -1.6671886069794575 0.0000000000000000 Y: 89596.5396495918 -0.2848010421249924 0.0000000000000000 Z: 40605.4902789652 0.1600853195745784 0.0000000000000000 EPOCH : 2002/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -25381.9994500968 -2.1971333362753138 0.0000000000000000 Y: 85451.8936993664 0.4794709046950659 0.0000000000000000 Z: 31414.5197538315 0.4897513361339627 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 28-FEB-2002 09:17:23.35 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/2/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/2/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20020228231745A.matu@d1.nas.nec.co.jp> Date: Thu, 28 Feb 2002 23:17:45 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 62 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ------- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 02 21 20 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -100408.920192 [km] Vx: 1.4594544508 [km/s] Y: -106938.298931 [km] Vy: -0.1975554419 [km/s] Z: -18032.433111 [km] Vz: -0.2770844303 [km/s] (Keplerian) a: 126611.882514 [km] an: 25.711225020 [deg] e: 0.561531928851 [ - ] ap: 339.591434266 [deg] i: 18.8596894990 [deg] ma: 283.379215827 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/02/21 20:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -100408.9201922100 1.4594544507633000 0.0000000000000000 Y: -106938.2989312100 -0.1975554418860600 0.0000000000000000 Z: -18032.4331112860 -0.2770844303229500 0.0000000000000000 EPOCH : 2002/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -87903.8751836299 -1.6671554625116345 0.0000000000000000 Y: 89596.1318203727 -0.2848165738349846 0.0000000000000000 Z: 40610.8738110017 0.1600700566872250 0.0000000000000000 EPOCH : 2002/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -25391.8538558743 -2.1970451133069639 0.0000000000000000 Y: 85454.2099060148 0.4792640558027703 0.0000000000000000 Z: 31421.3830951033 0.4897066311159488 0.0000000000000000 EPOCH : 2002/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -51955.3496109652 1.7323022098877636 0.0000000000000000 Y: -111735.4971951975 0.3621247362311183 0.0000000000000000 Z: -28875.0342708175 -0.1501957745502525 0.0000000000000000 EPOCH : 2002/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -71861.6155008759 1.5935306603385739 0.0000000000000000 Y: -115420.6639603829 0.1151686021853982 0.0000000000000000 Z: -27423.0485454493 -0.2156106702201837 0.0000000000000000 From: SMTP%"matu@d1.nas.nec.co.jp" 28-MAR-2002 23:14:16.24 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/3/29) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/3/29) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20020329131323E.matu@d1.nas.nec.co.jp> Date: Fri, 29 Mar 2002 13:13:23 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 61 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka matu@d1.nas.nec.co.jp ** e-mail addres will be changed. (from Apr. 1st) The new address is m-matsuoka@ps.jp.nec.com ------- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 03 28 19 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -196785.837834 [km] Vx: 0.0647107191 [km/s] Y: -26676.770065 [km] Vy: -0.8883318055 [km/s] Z: 21129.295303 [km] Vz: -0.2923987847 [km/s] (Keplerian) a: 128042.155697 [km] an: 25.314497408 [deg] e: 0.560095571027 [ - ] ap: 342.569289070 [deg] i: 19.3916306217 [deg] ma: 176.618891316 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/03/28 19:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -196785.8378341300 0.0647107191258140 0.0000000000000000 Y: -26676.7700645060 -0.8883318054555500 0.0000000000000000 Z: 21129.2953031170 -0.2923987847442900 0.0000000000000000 EPOCH : 2002/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -25390.5674677362 -2.1970248149690663 0.0000000000000000 Y: 85455.5287520052 0.4792920472373352 0.0000000000000000 Z: 31420.6919860320 0.4897154015165374 0.0000000000000000 EPOCH : 2002/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -51958.0614654219 1.7322974340659287 0.0000000000000000 Y: -111735.6748267773 0.3620808064524170 0.0000000000000000 Z: -28873.1648849800 -0.1502207130547424 0.0000000000000000 EPOCH : 2002/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -71866.4974963291 1.5935086737688169 0.0000000000000000 Y: -115420.3600596352 0.1151060588646520 0.0000000000000000 Z: -27420.5417851551 -0.2156362261757563 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 26-APR-2002 04:36:21.50 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/4/26) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/4/26) To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20020426173219I.m-matsuoka@ps.jp.nec.com> Date: Fri, 26 Apr 2002 17:32:19 +0900 From: Masatoshi Matsuoka X-Dispatcher: imput version 20000228(IM140) Lines: 56 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 04 22 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -129352.794058 [km] Vx: -1.2733339712 [km/s] Y: 70191.463566 [km] Vy: -0.6714497829 [km/s] Z: 42877.787643 [km] Vz: -0.0229933891 [km/s] (Keplerian) a: 127434.297366 [km] an: 25.269228201 [deg] e: 0.555684917335 [ - ] ap: 344.635214423 [deg] i: 19.8623681660 [deg] ma: 81.773901800 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/04/22 14:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -129352.7940580100 -1.2733339712092000 0.0000000000000000 Y: 70191.4635661270 -0.6714497828991600 0.0000000000000000 Z: 42877.7876434860 -0.0229933891086420 0.0000000000000000 EPOCH : 2002/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -51957.4539242512 1.7323135679673030 0.0000000000000000 Y: -111734.5288632976 0.3620929167485530 0.0000000000000000 Z: -28872.3689278735 -0.1502377130143913 0.0000000000000000 EPOCH : 2002/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -71862.0104324533 1.5935497279586923 0.0000000000000000 Y: -115418.9755005818 0.1151575815449473 0.0000000000000000 Z: -27420.1204623231 -0.2156425465427596 0.0000000000000000 EPOCH : 2002/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -179516.9357438168 0.4974904576955032 0.0000000000000000 Y: -69203.3424093769 -0.7937831205808664 -0.0000000000000000 Z: 5557.4926069857 -0.3528854899908411 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 31-MAY-2002 00:38:46.39 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/5/31) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/5/31) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20020531133748P.m-matsuoka@ps.jp.nec.com> Date: Fri, 31 May 2002 13:37:48 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 62 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 05 30 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -187464.399226 [km] Vx: 0.3200481065 [km/s] Y: -54662.970317 [km] Vy: -0.8438420381 [km/s] Z: 11499.293901 [km] Vz: -0.3352729666 [km/s] (Keplerian) a: 126597.784021 [km] an: 25.347787197 [deg] e: 0.550809463038 [ - ] ap: 345.870498537 [deg] i: 20.4396008911 [deg] ma: 192.757839882 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/05/30 14:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -187464.3992257200 0.3200481065227200 0.0000000000000000 Y: -54662.9703170510 -0.8438420380659299 0.0000000000000000 Z: 11499.2939007310 -0.3352729665961300 0.0000000000000000 EPOCH : 2002/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -71867.3316157834 1.5935362911004021 0.0000000000000000 Y: -115418.0678224160 0.1150971774923633 0.0000000000000000 Z: -27416.5552287573 -0.2156466524616490 0.0000000000000000 EPOCH : 2002/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -179518.9933808602 0.4974766647608256 0.0000000000000000 Y: -69199.8538926187 -0.7937931788644710 -0.0000000000000000 Z: 5559.0735816359 -0.3528594184185433 0.0000000000000000 EPOCH : 2002/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -189620.5856929055 0.2298120046960128 0.0000000000000000 Y: -48476.8320626448 -0.8697507020468487 -0.0000000000000000 Z: 14448.7179096230 -0.3409496992426257 0.0000000000000000 EPOCH : 2002/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -193320.0182661938 0.0203874565735930 0.0000000000000000 Y: -32930.7812603797 -0.8906933322355072 -0.0000000000000000 Z: 20617.0302115303 -0.3197272956714408 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 30-JUN-2002 18:53:52.30 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/6/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/6/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20020701075404X.m-matsuoka@ps.jp.nec.com> Date: Mon, 01 Jul 2002 07:54:04 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 61 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 06 27 18 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: 44377.353521 [km] Vx: 1.4252974333 [km/s] Y: -50147.782505 [km] Vy: 2.3820633669 [km/s] Z: -24399.943207 [km] Vz: 0.5834350055 [km/s] (Keplerian) a: 126965.216086 [km] an: 25.443701460 [deg] e: 0.538948608604 [ - ] ap: 345.738060577 [deg] i: 20.7656714983 [deg] ma: 342.420868755 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/06/27 18:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 44377.3535207760 1.4252974333068000 0.0000000000000000 Y: -50147.7825054870 2.3820633668904998 0.0000000000000000 Z: -24399.9432065870 0.5834350055049100 0.0000000000000000 EPOCH : 2002/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -179521.1025121388 0.4974529104145448 0.0000000000000000 Y: -69198.2157469335 -0.7937825384972783 -0.0000000000000000 Z: 5556.6502755467 -0.3528783691812422 0.0000000000000000 EPOCH : 2002/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -189622.3819334857 0.2297769278187672 0.0000000000000000 Y: -48474.3289644241 -0.8697405064906216 -0.0000000000000000 Z: 14447.1478816667 -0.3409704477308761 0.0000000000000000 EPOCH : 2002/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -193321.1075260315 0.0203422373892621 0.0000000000000000 Y: -32927.5593662301 -0.8906823743138976 -0.0000000000000000 Z: 20616.0595080732 -0.3197479619633695 0.0000000000000000 EPOCH : 2002/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -141929.0438782010 -1.1372181464387030 0.0000000000000000 Y: 52537.5431881604 -0.7845635557785239 0.0000000000000000 Z: 43220.4758069736 -0.0917367331203813 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 30-AUG-2002 03:12:06.08 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/8/30) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/8/30) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20020830161201U.m-matsuoka@ps.jp.nec.com> Date: Fri, 30 Aug 2002 16:12:01 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 54 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 08 28 11 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -90374.670539 [km] Vx: 1.4454987893 [km/s] Y: -117188.608023 [km] Vy: -0.0377603591 [km/s] Z: -26456.957919 [km] Vz: -0.2549678877 [km/s] (Keplerian) a: 126663.851789 [km] an: 25.231556709 [deg] e: 0.563565881005 [ - ] ap: 347.783511474 [deg] i: 21.4077786645 [deg] ma: 281.096290450 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/08/28 11:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -90374.6705394490 1.4454987892535001 0.0000000000000000 Y: -117188.6080225200 -0.0377603591126980 0.0000000000000000 Z: -26456.9579185860 -0.2549678877208100 0.0000000000000000 EPOCH : 2002/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -193323.0338282719 0.0202821467014314 0.0000000000000000 Y: -32924.1741613844 -0.8906732959537671 -0.0000000000000000 Z: 20617.7085453202 -0.3197338905473004 0.0000000000000000 EPOCH : 2002/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -141921.3214346362 -1.1373347199542043 0.0000000000000000 Y: 52541.5420122392 -0.7845152147585234 0.0000000000000000 Z: 43220.6794549391 -0.0916982453938796 0.0000000000000000 EPOCH : 2002/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -100651.8204057457 -1.6203673973055279 0.0000000000000000 Y: 71062.2155793009 -0.5699020088059458 0.0000000000000000 Z: 44329.7616414200 0.0691806723166424 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 27-SEP-2002 03:48:23.03 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/9/27) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/9/27) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20020927164511F.m-matsuoka@ps.jp.nec.com> Date: Fri, 27 Sep 2002 16:45:11 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 64 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 09 26 07 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -178158.593669 [km] Vx: -0.5880680243 [km/s] Y: 16218.415463 [km] Vy: -0.9062291175 [km/s] Z: 36061.341101 [km] Vz: -0.2285977699 [km/s] (Keplerian) a: 126578.269062 [km] an: 25.070195051 [deg] e: 0.572582764785 [ - ] ap: 349.055796213 [deg] i: 21.7952854267 [deg] ma: 119.615844006 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/09/26 07:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -178158.5936694000 -0.5880680243023100 0.0000000000000000 Y: 16218.4154628600 -0.9062291175094200 0.0000000000000000 Z: 36061.3411012330 -0.2285977699228600 0.0000000000000000 EPOCH : 2002/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -141922.7623276110 -1.1373160622887086 0.0000000000000000 Y: 52538.9040405956 -0.7845319945133493 0.0000000000000000 Z: 43220.9558746790 -0.0916929575747145 0.0000000000000000 EPOCH : 2002/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -100655.6166213353 -1.6203302380118119 0.0000000000000000 Y: 71059.4789753512 -0.5699453882276329 0.0000000000000000 Z: 44330.0517139620 0.0691757913626176 0.0000000000000000 EPOCH : 2002/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 17989.4012043788 1.7170718849286126 0.0000000000000000 Y: -82787.8128009563 1.5755874032298964 0.0000000000000000 Z: -35503.7214018452 0.3033062298392557 0.0000000000000000 EPOCH : 2003/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 2513.0833854556 1.7519008317250415 0.0000000000000000 Y: -97208.8287696448 1.1760860836739815 0.0000000000000000 Z: -38923.5517166961 0.1424175456806917 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 25-OCT-2002 01:34:34.05 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/10/25) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/10/25) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20021025143402Z.m-matsuoka@ps.jp.nec.com> Date: Fri, 25 Oct 2002 14:34:02 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 56 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 10 24 06 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -137001.403518 [km] Vx: 1.0255393704 [km/s] Y: -113050.378591 [km] Vy: -0.4116352740 [km/s] Z: -18526.357177 [km] Vz: -0.3330360611 [km/s] (Keplerian) a: 127272.332480 [km] an: 24.918523562 [deg] e: 0.560796644040 [ - ] ap: 351.539542049 [deg] i: 22.4651665250 [deg] ma: 246.366154906 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/10/24 06:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -137001.4035179000 1.0255393704114999 0.0000000000000000 Y: -113050.3785905100 -0.4116352739731600 0.0000000000000000 Z: -18526.3571774740 -0.3330360610773100 0.0000000000000000 EPOCH : 2002/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -100653.2293700212 -1.6203656005771239 0.0000000000000000 Y: 71059.1644591831 -0.5699333527436349 0.0000000000000000 Z: 44329.7873060555 0.0691610343948895 0.0000000000000000 EPOCH : 2002/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 17984.6353590809 1.7170841302275495 0.0000000000000000 Y: -82792.7455180099 1.5754464460681541 0.0000000000000000 Z: -35505.9114715730 0.3032917673861703 0.0000000000000000 EPOCH : 2003/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 2505.9901669043 1.7518892436347586 0.0000000000000000 Y: -97214.2245967906 1.1759314059773467 0.0000000000000000 Z: -38925.8152555026 0.1423952326500926 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 29-NOV-2002 01:44:21.36 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/11/29) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/11/29) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20021129154304X.m-matsuoka@ps.jp.nec.com> Date: Fri, 29 Nov 2002 15:43:04 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 62 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 11 27 20 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -170031.447672 [km] Vx: -0.6859320555 [km/s] Y: 16745.573052 [km] Vy: -0.9472246858 [km/s] Z: 37024.658261 [km] Vz: -0.2433926022 [km/s] (Keplerian) a: 127220.183436 [km] an: 24.897393891 [deg] e: 0.553187923749 [ - ] ap: 353.862305292 [deg] i: 23.1075034268 [deg] ma: 109.213324408 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/11/27 20:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -170031.4476719500 -0.6859320555165400 0.0000000000000000 Y: 16745.5730518200 -0.9472246858100000 0.0000000000000000 Z: 37024.6582610020 -0.2433926021927700 0.0000000000000000 EPOCH : 2002/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 17987.3072111164 1.7170526241739075 0.0000000000000000 Y: -82792.0480307550 1.5754839966322292 0.0000000000000000 Z: -35505.5914400583 0.3033101768626114 0.0000000000000000 EPOCH : 2003/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 2508.9642389089 1.7518682003611552 0.0000000000000000 Y: -97214.0079004594 1.1759656664196867 0.0000000000000000 Z: -38925.7274098168 0.1424126889934607 0.0000000000000000 EPOCH : 2003/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -33233.3237294712 1.6823194369983190 0.0000000000000000 Y: -114508.1054075284 0.6050066140338355 0.0000000000000000 Z: -39864.6263873757 -0.0708695852010221 0.0000000000000000 EPOCH : 2003/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -122904.3328745191 -1.3644398880470237 0.0000000000000000 Y: 54873.9730937330 -0.7763164519564361 0.0000000000000000 Z: 45988.5074124274 -0.0617391190363026 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 27-DEC-2002 00:32:03.60 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/12/27) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2002/12/27) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20021227142807D.m-matsuoka@ps.jp.nec.com> Date: Fri, 27 Dec 2002 14:28:07 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 58 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2002 12 24 22 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -182726.687998 [km] Vx: 0.3537394213 [km/s] Y: -71171.854885 [km] Vy: -0.8009925854 [km/s] Z: 5428.302484 [km] Vz: -0.3788657388 [km/s] (Keplerian) a: 126399.397609 [km] an: 24.948276309 [deg] e: 0.553695044369 [ - ] ap: 353.608341795 [deg] i: 23.4011614694 [deg] ma: 186.942391606 [deg] -- <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2002/12/24 22:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -182726.6879978200 0.3537394212694600 0.0000000000000000 Y: -71171.8548852130 -0.8009925854078600 0.0000000000000000 Z: 5428.3024838119 -0.3788657388416600 0.0000000000000000 EPOCH : 2003/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 2510.7332387665 1.7518521353363448 0.0000000000000000 Y: -97214.0227034799 1.1759866128968006 0.0000000000000000 Z: -38925.9486376164 0.1423974671154053 0.0000000000000000 EPOCH : 2003/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -33228.5076700973 1.6823250428879399 0.0000000000000000 Y: -114507.4803985163 0.6050655631243974 0.0000000000000000 Z: -39864.6962728362 -0.0708715356177962 0.0000000000000000 EPOCH : 2003/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -122907.9344360723 -1.3643817620052086 0.0000000000000000 Y: 54871.1267112785 -0.7763551650660787 0.0000000000000000 Z: 45989.7934552709 -0.0617462497716712 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 31-JAN-2003 00:40:05.12 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/01/31) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/01/31) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030131143726W.m-matsuoka@ps.jp.nec.com> Date: Fri, 31 Jan 2003 14:37:26 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 55 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 01 30 21 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -155176.651133 [km] Vx: 0.7987216627 [km/s] Y: -103756.500645 [km] Vy: -0.5770165988 [km/s] Z: -12752.880047 [km] Vz: -0.3814188370 [km/s] (Keplerian) a: 126766.957724 [km] an: 24.909544088 [deg] e: 0.543990115685 [ - ] ap: 353.697848275 [deg] i: 23.9239506486 [deg] ma: 224.052209794 [deg] -- <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/01/30 21:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -155176.6511325800 0.7987216626838800 0.0000000000000000 Y: -103756.5006452700 -0.5770165988299000 0.0000000000000000 Z: -12752.8800472270 -0.3814188370138300 0.0000000000000000 EPOCH : 2003/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -33224.8567434505 1.6823349204912754 0.0000000000000000 Y: -114506.9432503641 0.6050904778448120 0.0000000000000000 Z: -39865.3900361024 -0.0708540365264221 0.0000000000000000 EPOCH : 2003/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -122908.9906172153 -1.3643594142519526 0.0000000000000000 Y: 54871.5133530998 -0.7763681771752939 0.0000000000000000 Z: 45989.4256063686 -0.0617632368166384 0.0000000000000000 EPOCH : 2003/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -95890.0311350079 -1.7151031743884810 0.0000000000000000 Y: 62573.7298044762 -0.6151849140298892 0.0000000000000000 Z: 45140.1746672890 0.0705898079901253 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 28-FEB-2003 00:39:48.92 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/02/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/02/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030228143741P.m-matsuoka@ps.jp.nec.com> Date: Fri, 28 Feb 2003 14:37:41 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 69 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 02 26 21 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -68553.185066 [km] Vx: 1.4899043820 [km/s] Y: -123693.204333 [km] Vy: 0.2067721114 [km/s] Z: -38064.681694 [km] Vz: -0.1974721313 [km/s] (Keplerian) a: 126868.986914 [km] an: 24.690068939 [deg] e: 0.556344155285 [ - ] ap: 355.159032290 [deg] i: 24.4419904257 [deg] ma: 284.515898684 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/02/26 21:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -68553.1850662140 1.4899043819675000 0.0000000000000000 Y: -123693.2043330800 0.2067721113935600 0.0000000000000000 Z: -38064.6816938020 -0.1974721313382900 0.0000000000000000 EPOCH : 2003/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -122906.0383468873 -1.3643871934536480 0.0000000000000000 Y: 54874.0974028830 -0.7763522666954851 0.0000000000000000 Z: 45990.4681927020 -0.0617455007060016 0.0000000000000000 EPOCH : 2003/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -95884.0575354112 -1.7151625639585641 0.0000000000000000 Y: 62576.8347592873 -0.6151376791954182 0.0000000000000000 Z: 45140.7737636366 0.0706286250771159 0.0000000000000000 EPOCH : 2003/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 27473.4335939146 1.5755172514361875 0.0000000000000000 Y: -74751.4342137471 1.7850530679002061 0.0000000000000000 Z: -38069.0470808543 0.4657448398631284 0.0000000000000000 EPOCH : 2003/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -15158.3192366725 1.6126252938372929 0.0000000000000000 Y: -112715.3541307837 0.8556162192429070 0.0000000000000000 Z: -47393.8988543710 0.0534078005426741 0.0000000000000000 EPOCH : 2003/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147310.5539136669 0.8109891961384464 0.0000000000000000 Y: -116566.3371274310 -0.5016296164756094 -0.0000000000000000 Z: -22492.9733479244 -0.3968085475795344 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 28-MAR-2003 00:44:00.49 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/03/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/03/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030328144134G.m-matsuoka@ps.jp.nec.com> Date: Fri, 28 Mar 2003 14:41:34 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 62 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 03 26 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -57041.440729 [km] Vx: -2.1422329276 [km/s] Y: 72296.930614 [km] Vy: -0.2149187784 [km/s] Z: 41634.950771 [km] Vz: 0.3227244771 [km/s] (Keplerian) a: 126598.724333 [km] an: 24.515017103 [deg] e: 0.571395221268 [ - ] ap: 356.637330526 [deg] i: 24.9603861246 [deg] ma: 38.698885900 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/03/26 14:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -57041.4407287170 -2.1422329276366998 0.0000000000000000 Y: 72296.9306141990 -0.2149187784027800 0.0000000000000000 Z: 41634.9507709450 0.3227244770571600 0.0000000000000000 EPOCH : 2003/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -95882.1159758327 -1.7151812411956264 0.0000000000000000 Y: 62578.9289885522 -0.6151105161957178 0.0000000000000000 Z: 45140.3975642715 0.0706338945129513 0.0000000000000000 EPOCH : 2003/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 27472.3876179640 1.5755383894501416 0.0000000000000000 Y: -74752.9388233435 1.7850125659516722 0.0000000000000000 Z: -38068.9917422960 0.4657272321419722 0.0000000000000000 EPOCH : 2003/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -15160.2447156907 1.6126316018591660 0.0000000000000000 Y: -112716.2410737233 0.8555780455368275 0.0000000000000000 Z: -47393.4901758050 0.0533976926844558 0.0000000000000000 EPOCH : 2003/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147313.0428312802 0.8109689527967024 0.0000000000000000 Y: -116563.6742940341 -0.5016591377076175 -0.0000000000000000 Z: -22491.7959229082 -0.3968090122473529 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 25-APR-2003 04:30:33.84 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/04/25) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/04/25) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030425172829T.m-matsuoka@ps.jp.nec.com> Date: Fri, 25 Apr 2003 17:28:29 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 56 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 04 24 14 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -124406.558165 [km] Vx: 1.0692326496 [km/s] Y: -124216.296464 [km] Vy: -0.2747003118 [km/s] Z: -29389.043161 [km] Vz: -0.3309856873 [km/s] (Keplerian) a: 126769.510407 [km] an: 24.470375103 [deg] e: 0.567645833531 [ - ] ap: 358.338065274 [deg] i: 25.5321208416 [deg] ma: 247.060524672 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/04/24 14:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -124406.5581650000 1.0692326495930999 0.0000000000000000 Y: -124216.2964636400 -0.2747003117544200 0.0000000000000000 Z: -29389.0431606600 -0.3309856873225100 0.0000000000000000 EPOCH : 2003/05/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 27475.3976105677 1.5755227997459673 0.0000000000000000 Y: -74748.2689468139 1.7850902034743790 0.0000000000000000 Z: -38068.5553582951 0.4658292873768680 0.0000000000000000 EPOCH : 2003/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -15147.2910249003 1.6126724290164329 0.0000000000000000 Y: -112707.7035722191 0.8557648877768769 0.0000000000000000 Z: -47394.6505035379 0.0535205989390840 0.0000000000000000 EPOCH : 2003/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147301.5864874207 0.8111041854024811 0.0000000000000000 Y: -116569.0280635647 -0.5015564997085311 -0.0000000000000000 Z: -22501.6267468508 -0.3967815261773558 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 30-MAY-2003 01:20:35.33 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/05/30) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/05/30) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030530141912B.m-matsuoka@ps.jp.nec.com> Date: Fri, 30 May 2003 14:19:12 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 56 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 05 29 11 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -182061.859721 [km] Vx: -0.2648083284 [km/s] Y: -29365.277789 [km] Vy: -0.9668894750 [km/s] Z: 24036.918068 [km] Vz: -0.3786151939 [km/s] (Keplerian) a: 127013.214220 [km] an: 24.528071824 [deg] e: 0.552722225805 [ - ] ap: 0.967659604 [deg] i: 26.1924659378 [deg] ma: 129.937343556 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/05/29 11:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -182061.8597212500 -0.2648083283637200 0.0000000000000000 Y: -29365.2777891660 -0.9668894749620400 0.0000000000000000 Z: 24036.9180675070 -0.3786151938622800 0.0000000000000000 EPOCH : 2003/06/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -15159.1031742196 1.6126634008213481 0.0000000000000000 Y: -112713.5859884153 0.8556025724957176 0.0000000000000000 Z: -47392.7234653395 0.0534305085801981 0.0000000000000000 EPOCH : 2003/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147311.7334391318 0.8110050372813228 0.0000000000000000 Y: -116562.9065716514 -0.5016389848680755 -0.0000000000000000 Z: -22494.2508533407 -0.3967916430196947 0.0000000000000000 EPOCH : 2003/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -159633.0079054511 0.6776165625848094 0.0000000000000000 Y: -106846.2838022506 -0.5913193606136212 -0.0000000000000000 Z: -16055.4216835024 -0.4148756975613954 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 29-JUN-2003 22:37:10.64 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/06/30) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/06/30) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030630113733J.m-matsuoka@ps.jp.nec.com> Date: Mon, 30 Jun 2003 11:37:33 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 62 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 06 26 11 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -88963.648644 [km] Vx: 1.2758567934 [km/s] Y: -132229.884135 [km] Vy: 0.0051260581 [km/s] Z: -41744.623598 [km] Vz: -0.2624899920 [km/s] (Keplerian) a: 126854.966138 [km] an: 24.505450663 [deg] e: 0.547684230823 [ - ] ap: 1.803125865 [deg] i: 26.5844762909 [deg] ma: 263.249289979 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/06/26 11:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -88963.6486439620 1.2758567933974001 0.0000000000000000 Y: -132229.8841353400 0.0051260581386550 0.0000000000000000 Z: -41744.6235984890 -0.2624899919914100 0.0000000000000000 EPOCH : 2003/07/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -147317.3344831952 0.8109618700144792 0.0000000000000000 Y: -116559.0622931692 -0.5016729353330850 -0.0000000000000000 Z: -22492.8927024160 -0.3967894005664519 0.0000000000000000 EPOCH : 2003/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -159640.5451488573 0.6775385631495288 0.0000000000000000 Y: -106839.8745372603 -0.5913677791826103 -0.0000000000000000 Z: -16052.5661003555 -0.4148742748006616 0.0000000000000000 EPOCH : 2003/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -172458.7725325015 0.4939070019716303 0.0000000000000000 Y: -95714.2152746789 -0.6953572895331427 -0.0000000000000000 Z: -8874.3598739683 -0.4345780326534560 0.0000000000000000 EPOCH : 2003/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -160217.2723430087 -0.7671775627011665 0.0000000000000000 Y: 2994.4887870258 -1.0029466586840505 0.0000000000000000 Z: 36670.5924648676 -0.3244879556595968 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 28-JUL-2003 01:15:36.80 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/07/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/07/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030728141535N.m-matsuoka@ps.jp.nec.com> Date: Mon, 28 Jul 2003 14:15:35 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 62 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 07 22 15 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -66540.597515 [km] Vx: 1.4135000279 [km/s] Y: -129271.000618 [km] Vy: 0.2252735085 [km/s] Z: -45640.656090 [km] Vz: -0.1915088187 [km/s] (Keplerian) a: 126699.637185 [km] an: 24.395823478 [deg] e: 0.548095551310 [ - ] ap: 1.329825337 [deg] i: 26.8276035853 [deg] ma: 277.466782700 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/07/22 15:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -66540.5975151120 1.4135000278747001 0.0000000000000000 Y: -129271.0006179900 0.2252735084713800 0.0000000000000000 Z: -45640.6560901240 -0.1915088187346300 0.0000000000000000 EPOCH : 2003/08/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -159642.8744668194 0.6775113017727963 0.0000000000000000 Y: -106839.1187795001 -0.5913648657302313 -0.0000000000000000 Z: -16049.1426007386 -0.4148924122872250 0.0000000000000000 EPOCH : 2003/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -172461.0678975371 0.4938731110637306 0.0000000000000000 Y: -95712.8347359438 -0.6953554343229427 -0.0000000000000000 Z: -8870.2795903037 -0.4345932254562548 0.0000000000000000 EPOCH : 2003/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -160214.2624842977 -0.7672365995367815 0.0000000000000000 Y: 2997.0619268971 -1.0029353199638718 0.0000000000000000 Z: 36675.5413584964 -0.3244673363549022 0.0000000000000000 EPOCH : 2003/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -145925.5748304756 -1.0048905757884810 0.0000000000000000 Y: 16300.6885105568 -0.9983493602360588 0.0000000000000000 Z: 40966.8038151896 -0.2766491291877320 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 3-SEP-2003 08:26:44.96 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/09/03) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/09/03) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030903212649Q.m-matsuoka@ps.jp.nec.com> Date: Wed, 03 Sep 2003 21:26:49 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 61 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 08 28 08 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -28413.264840 [km] Vx: 1.5927515584 [km/s] Y: -116622.815572 [km] Vy: 0.6845004599 [km/s] Z: -48787.631271 [km] Vz: -0.0145481227 [km/s] (Keplerian) a: 126658.531371 [km] an: 24.189813922 [deg] e: 0.554009544475 [ - ] ap: 0.929913012 [deg] i: 27.2468415394 [deg] ma: 299.336958224 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/08/28 08:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -28413.2648404180 1.5927515583794001 0.0000000000000000 Y: -116622.8155722500 0.6845004599093700 0.0000000000000000 Z: -48787.6312713640 -0.0145481226754770 0.0000000000000000 EPOCH : 2003/09/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -172460.7854155054 0.4938893024193393 0.0000000000000000 Y: -95714.8220907560 -0.6953309367911410 -0.0000000000000000 Z: -8877.3949990577 -0.4345895979246677 0.0000000000000000 EPOCH : 2003/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -160218.1680560665 -0.7671778821841000 0.0000000000000000 Y: 2990.9773230944 -1.0029283142856646 0.0000000000000000 Z: 36669.5776968691 -0.3245157364359423 0.0000000000000000 EPOCH : 2003/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -145933.5034027580 -1.0047763875629623 0.0000000000000000 Y: 16291.6886921333 -0.9983577435462686 0.0000000000000000 Z: 40960.6517431657 -0.2767227102022765 0.0000000000000000 EPOCH : 2003/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 56779.9116269509 -0.8224381984810115 0.0000000000000000 Y: 11995.9533928325 2.7096849063516122 0.0000000000000000 Z: -6863.1673583548 1.5759731698752082 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 26-SEP-2003 07:31:57.81 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/09/26) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/09/26) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20030926202904S.m-matsuoka@ps.jp.nec.com> Date: Fri, 26 Sep 2003 20:29:04 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 62 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 09 25 03 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -95121.235826 [km] Vx: -1.7228523558 [km/s] Y: 56491.724813 [km] Vy: -0.7162007293 [km/s] Z: 47757.483037 [km] Vz: 0.0260441332 [km/s] (Keplerian) a: 127187.565884 [km] an: 24.086943253 [deg] e: 0.556160997234 [ - ] ap: 2.800824942 [deg] i: 27.8486648292 [deg] ma: 52.851768815 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/09/25 03:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -95121.2358263400 -1.7228523557758000 0.0000000000000000 Y: 56491.7248126610 -0.7162007293358200 0.0000000000000000 Z: 47757.4830366550 0.0260441331923410 0.0000000000000000 EPOCH : 2003/10/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -160216.4172374131 -0.7671978687479230 0.0000000000000000 Y: 2991.6935233639 -1.0029368961143543 0.0000000000000000 Z: 36675.8787328696 -0.3244577863238539 0.0000000000000000 EPOCH : 2003/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -145929.6674936821 -1.0048240441635350 0.0000000000000000 Y: 16294.0803147601 -0.9983613823188900 0.0000000000000000 Z: 40966.7426086068 -0.2766481093106551 0.0000000000000000 EPOCH : 2003/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 56781.6549227890 -0.8220410070333809 0.0000000000000000 Y: 11987.7430666392 2.7097977497953645 0.0000000000000000 Z: -6870.5303922079 1.5759217651404047 0.0000000000000000 EPOCH : 2004/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 47699.9503322699 1.1438949542813748 0.0000000000000000 Y: -58953.0419815666 2.0318669765787409 0.0000000000000000 Z: -41782.2629028880 0.7917930368649504 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 30-OCT-2003 23:31:03.65 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/10/31) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/10/31) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20031031133016D.m-matsuoka@ps.jp.nec.com> Date: Fri, 31 Oct 2003 13:30:16 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 61 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 10 30 05 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: 11301.664866 [km] Vx: 1.5519388877 [km/s] Y: -94873.724350 [km] Vy: 1.3163969313 [km/s] Z: -50260.442136 [km] Vz: 0.3135665441 [km/s] (Keplerian) a: 126755.376977 [km] an: 24.062895323 [deg] e: 0.567428800054 [ - ] ap: 5.829170045 [deg] i: 28.8493473750 [deg] ma: 316.531623008 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/10/30 05:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 11301.6648663020 1.5519388876527000 0.0000000000000000 Y: -94873.7243503110 1.3163969313135999 0.0000000000000000 Z: -50260.4421358400 0.3135665441228900 0.0000000000000000 EPOCH : 2003/11/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -145931.3537798052 -1.0047932633901464 0.0000000000000000 Y: 16290.1076452654 -0.9983735761395549 0.0000000000000000 Z: 40964.3489925381 -0.2766828155039200 0.0000000000000000 EPOCH : 2003/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 56781.9619129829 -0.8220305629558933 0.0000000000000000 Y: 11986.6219299766 2.7097848959980362 0.0000000000000000 Z: -6870.5806176159 1.5759440964398483 0.0000000000000000 EPOCH : 2004/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 47699.4871671712 1.1438954925880724 0.0000000000000000 Y: -58955.1420405452 2.0318154165395055 0.0000000000000000 Z: -41783.6179789744 0.7918017135518784 0.0000000000000000 EPOCH : 2004/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 22364.7156036033 1.4592629344446792 0.0000000000000000 Y: -90532.0748535578 1.4109722996406167 0.0000000000000000 Z: -53083.6664741560 0.4048052618837562 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 28-NOV-2003 03:43:02.37 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/11/28) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/11/28) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20031128174128O.m-matsuoka@ps.jp.nec.com> Date: Fri, 28 Nov 2003 17:41:28 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 62 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 11 26 20 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -124906.597606 [km] Vx: -1.3065585811 [km/s] Y: 32428.294071 [km] Vy: -0.9729847185 [km/s] Z: 45191.207930 [km] Vz: -0.1986055559 [km/s] (Keplerian) a: 127057.191710 [km] an: 24.111987616 [deg] e: 0.550385699038 [ - ] ap: 7.678424261 [deg] i: 29.2708397066 [deg] ma: 66.720332734 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/11/26 20:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -124906.5976059800 -1.3065585810608999 0.0000000000000000 Y: 32428.2940714820 -0.9729847184579899 0.0000000000000000 Z: 45191.2079297220 -0.1986055558644700 0.0000000000000000 EPOCH : 2003/12/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 56782.1803990425 -0.8220612485856645 0.0000000000000000 Y: 11986.9034962733 2.7098187961898308 0.0000000000000000 Z: -6871.4997847693 1.5758416629161820 0.0000000000000000 EPOCH : 2004/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 47702.0710565203 1.1438166416345159 0.0000000000000000 Y: -58953.7431934558 2.0318962603344839 0.0000000000000000 Z: -41781.1741830741 0.7917549892371668 0.0000000000000000 EPOCH : 2004/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 22370.5688789074 1.4592078409001228 0.0000000000000000 Y: -90530.0430493508 1.4110881046660992 0.0000000000000000 Z: -53079.9817014144 0.4047972589919092 0.0000000000000000 EPOCH : 2004/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -173714.3503288695 0.3061761106463290 0.0000000000000000 Y: -89214.6009322878 -0.7745128320439968 -0.0000000000000000 Z: -7101.1189838175 -0.4892243371907344 0.0000000000000000 From: SMTP%"m-matsuoka@ps.jp.nec.com" 25-DEC-2003 23:43:25.71 To: SARDI CC: Subj: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/12/26) Subject: [MONTHLY] GEOTAIL LATEST ORBIT DATA(2003/12/26) From: Masatoshi Matsuoka To: gtl_month@ayame.d1.nas.nec.co.jp X-Mailer: Mew version 1.94.2 on Emacs 19.34 / Mule 2.3 =?iso-2022-jp?B?KBskQkt2RSYyVhsoQik=?= Mime-Version: 1.0 Content-Type: Text/Plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20031226134122O.m-matsuoka@ps.jp.nec.com> Date: Fri, 26 Dec 2003 13:41:22 +0900 X-Dispatcher: imput version 20000228(IM140) Lines: 63 The following data is updated orbit solution based on 3 path data. regards, Masatoshi == NEC Aerospace Systems,Ltd Masatoshi Matsuoka m-matsuoka@ps.jp.nec.com ----- GEOTAIL STATE VECTOR(J2000.0EQ;GEO-CENTRIC) ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ EPOCH : 2003 12 25 05 00 00.0000 [UTC] S/C MASS : 654.612 [kg] ~~~~~~~~~~ ORBIT ELEMENTS: GM=398600.4415[km**3/sec**2] (Cartesian) X: -128553.735733 [km] Vx: 0.9097694453 [km/s] Y: -131065.246395 [km] Vy: -0.3500346718 [km/s] Z: -38219.554031 [km] Vz: -0.3938072425 [km/s] (Keplerian) a: 126703.674375 [km] an: 24.120475392 [deg] e: 0.540891182079 [ - ] ap: 9.129202474 [deg] i: 29.6700890359 [deg] ma: 221.729612497 [deg] <<< S/C ORBITAL ELEMENTS (CARTESIAN;J2000EQ;GEO-CENTRIC) >>> EPOCH : 2003/12/25 05:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -128553.7357326600 0.9097694453117000 0.0000000000000000 Y: -131065.2463954300 -0.3500346717816000 0.0000000000000000 Z: -38219.5540306700 -0.3938072425491600 0.0000000000000000 EPOCH : 2004/01/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 47704.0899050717 1.1437870050338297 0.0000000000000000 Y: -58951.6063886564 2.0318794785523133 0.0000000000000000 Z: -41781.6366320001 0.7918486562564666 0.0000000000000000 EPOCH : 2004/02/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: 22373.5471294516 1.4591956446983370 0.0000000000000000 Y: -90527.2894059196 1.4110954516667953 0.0000000000000000 Z: -53081.7972371544 0.4048839574166222 0.0000000000000000 EPOCH : 2004/03/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -173713.8228567744 0.3061913804616233 0.0000000000000000 Y: -89213.3591272777 -0.7745061607245813 -0.0000000000000000 Z: -7107.5027891565 -0.4892424929779011 0.0000000000000000 EPOCH : 2004/04/01 00:00:00 (UTC) R(KM) V(KM/S) DV(KM/S) X: -177891.1389899360 0.0867522492058356 0.0000000000000000 Y: -72688.6509738762 -0.8661772713538958 -0.0000000000000000 Z: 2662.7388220795 -0.4984663869541716 0.0000000000000000