ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 4305.56
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 72.1
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.19
ET - UTC (sec) : 66.18
UT1 - UTC (sec) : 0.00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
044/07:19:00.000 0.0 0.0 0.0
N/A 0.0 0.0 197.2
000/00:00:00.000 0.0 0.0 186.8
Coasting Arc #1 (Orbit 2587)
---------------------------------------
Vector Time (GMT): 2009/040/13:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 624260.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 626373.65 A = 6734055.37 meter
Y = -5337462.87 meter E = .0012711
Z = 4043916.52 I = 51.34674
XDOT = 5643.657664 Wp = 60.56500
YDOT = 3572.187596 meter/sec RA = 239.69105 deg
ZDOT = 3837.792713 TA = 349.78263
MA = 349.80844
Ha = 196.880 n.mi
Hp = 187.671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2055031.66 X = 666367.54
Y = -17511361.11 feet Y = -5330234.77 meter
Z = 13267442.66 Z = 4047056.50
XDOT = 18515.937219 XDOT = 5584.650755
YDOT = 11719.775579 feet/sec YDOT = 3634.968340 meter/sec
ZDOT = 12591.183442 ZDOT = 3865.065340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9456412.18 X = 2882314.43
Y = -14870566.45 feet Y = -4532548.65 meter
Z = 13279249.98 Z = 4047515.39
XDOT = 10352.121059 XDOT = 3155.326499
YDOT = 17930.444548 feet/sec YDOT = 5465.199498 meter/sec
ZDOT = 12697.732395 ZDOT = 3870.268834
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09040.59644537 .00010596 00000-0 82463-4 0 9006
2 25544 51.6363 240.2749 0008689 4.2508 355.8726 15.70845073 25883
Satellite: ISS
Catalog Number: 25544
Epoch time: 09040.59644537 = yrday.fracday
Element set: 900
Inclination: 51.6363 deg
RA of node: 240.2749 deg
Eccentricity: .0008689
Arg of perigee: 4.2508 deg
Mean anomaly: 355.8726 deg
Mean motion: 15.70845073 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2588
Checksum: 329
Coasting Arc #2 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2009/041/13:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 624260.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5123610.23 A = 6733839.39 meter
Y = -1561822.10 meter E = .0010477
Z = -4084222.73 I = 51.36214
XDOT = -995.579801 Wp = 55.61437
YDOT = -6617.183361 meter/sec RA = 234.50752 deg
ZDOT = 3792.123784 TA = 253.46633
MA = 253.58146
Ha = 196.966 n.mi
Hp = 187.350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16809744.84 X = -5085925.07
Y = -5124088.24 feet Y = -1618906.70 meter
Z = -13399680.87 Z = -4109020.87
XDOT = -3266.337930 XDOT = -939.932253
YDOT = -21709.919165 feet/sec YDOT = -6628.005254 meter/sec
ZDOT = 12441.350996 ZDOT = 3787.422776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12994505.49 X = -3960725.27
Y = -11720251.38 feet Y = -3572332.62 meter
Z = -13496435.97 Z = -4113713.68
XDOT = 5302.810825 XDOT = 1616.296739
YDOT = -20136.640031 feet/sec YDOT = -6137.647881 meter/sec
ZDOT = 12422.491630 ZDOT = 3786.375449
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09041.55070713 .00010596 00000-0 82463-4 0 9013
2 25544 51.6363 235.3960 0008626 9.2747 350.8572 15.70844543 26037
Satellite: ISS
Catalog Number: 25544
Epoch time: 09041.55070713 = yrday.fracday
Element set: 901
Inclination: 51.6363 deg
RA of node: 235.3960 deg
Eccentricity: .0008626
Arg of perigee: 9.2747 deg
Mean anomaly: 350.8572 deg
Mean motion: 15.70844543 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2603
Checksum: 300
Coasting Arc #3 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2009/042/13:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 624260.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2357895.03 A = 6738415.07 meter
Y = 5807145.20 meter E = .0007879
Z = -2487944.76 I = 51.39626
XDOT = -5570.073951 Wp = 50.43020
YDOT = -4.408049 meter/sec RA = 229.42402 deg
ZDOT = -5295.425619 TA = 157.74154
MA = 157.70732
Ha = 197.168 n.mi
Hp = 187.175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7735876.08 X = 2304869.00
Y = 19052313.65 feet Y = 5833215.95 meter
Z = -8162548.43 Z = -2476619.49
XDOT = -18274.520837 XDOT = -5543.887122
YDOT = -14.462103 feet/sec YDOT = -66.549698 meter/sec
ZDOT = -17373.443631 ZDOT = -5322.420732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -652066.40 X = -198749.84
Y = 20570260.01 feet Y = 6269815.25 meter
Z = -8117933.45 Z = -2474346.12
XDOT = -15092.143349 XDOT = -4600.085293
YDOT = -7368.155596 feet/sec YDOT = -2245.813826 meter/sec
ZDOT = -17478.636353 ZDOT = -5327.488360
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09042.56857864 .00010596 00000-0 82463-4 0 9026
2 25544 51.6367 230.1926 0008835 13.3245 346.8148 15.70880454 26199
Satellite: ISS
Catalog Number: 25544
Epoch time: 09042.56857864 = yrday.fracday
Element set: 902
Inclination: 51.6367 deg
RA of node: 230.1926 deg
Eccentricity: .0008835
Arg of perigee: 13.3245 deg
Mean anomaly: 346.8148 deg
Mean motion: 15.70880454 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2619
Checksum: 325
Coasting Arc #4 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2009/043/13:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 624260.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4223249.88 A = 6730167.16 meter
Y = -1485059.39 meter E = .0013269
Z = 5022283.59 I = 51.38794
XDOT = 4282.731818 Wp = 31.85528
YDOT = 6147.348055 meter/sec RA = 224.25789 deg
ZDOT = -1770.391289 TA = 75.33418
MA = 75.18712
Ha = 197.188 n.mi
Hp = 187.087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13855806.68 X = 4215145.33
Y = -4872242.10 feet Y = -1437877.60 meter
Z = 16477308.37 Z = 5042780.11
XDOT = 14050.957407 XDOT = 4222.272918
YDOT = 20168.464749 feet/sec YDOT = 6194.901913 meter/sec
ZDOT = -5808.370372 ZDOT = -1749.733392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14569468.78 X = 4440774.08
Y = 904597.20 feet Y = 275721.23 meter
Z = 16557055.79 Z = 5046590.60
XDOT = 5129.111530 XDOT = 1563.353194
YDOT = 23010.290858 feet/sec YDOT = 7013.536653 meter/sec
ZDOT = -5727.351491 ZDOT = -1745.696734
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09043.58644534 .00010596 00000-0 82463-4 0 9038
2 25544 51.6364 224.9884 0008656 17.6913 342.4548 15.70828863 26350
Satellite: ISS
Catalog Number: 25544
Epoch time: 09043.58644534 = yrday.fracday
Element set: 903
Inclination: 51.6364 deg
RA of node: 224.9884 deg
Eccentricity: .0008656
Arg of perigee: 17.6913 deg
Mean anomaly: 342.4548 deg
Mean motion: 15.70828863 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2635
Checksum: 338
Coasting Arc #5 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2009/044/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030693.65 A = 6729782.99 meter
Y = -1866425.55 meter E = .0013430
Z = 5052552.29 I = 51.40891
XDOT = 4782.462495 Wp = 31.09345
YDOT = 5800.501967 meter/sec RA = 220.35032 deg
ZDOT = -1659.216415 TA = 74.98653
MA = 74.83793
Ha = 197.197 n.mi
Hp = 186.836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13224060.54 X = 4026720.79
Y = -6123443.39 feet Y = -1821373.94 meter
Z = 16576615.13 Z = 5072123.51
XDOT = 15690.493749 XDOT = 4725.304916
YDOT = 19030.518263 feet/sec YDOT = 5853.662575 meter/sec
ZDOT = -5443.623409 ZDOT = -1636.122735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1880171.66 X = 573076.32
Y = 14363431.27 feet Y = 4377973.85 meter
Z = 16652726.56 Z = 5075751.06
XDOT = -21837.616652 XDOT = -6656.105556
YDOT = 9115.208569 feet/sec YDOT = 2778.315572 meter/sec
ZDOT = -5353.136365 ZDOT = -1631.635964
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09044.34983749 .00010596 00000-0 82463-4 0 9048
2 25544 51.6412 221.0909 0009059 18.0034 342.1447 15.70917797 26470
Satellite: ISS
Catalog Number: 25544
Epoch time: 09044.34983749 = yrday.fracday
Element set: 904
Inclination: 51.6412 deg
RA of node: 221.0909 deg
Eccentricity: .0009059
Arg of perigee: 18.0034 deg
Mean anomaly: 342.1447 deg
Mean motion: 15.70917797 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2647
Checksum: 318
Coasting Arc #6 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2009/045/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5273545.86 A = 6740960.89 meter
Y = -4156088.89 meter E = .0021445
Z = 441273.39 I = 51.46965
XDOT = 3293.805844 Wp = 38.32588
YDOT = -3527.154967 meter/sec RA = 215.24185 deg
ZDOT = 6004.426800 TA = 326.48290
MA = 326.61841
Ha = 197.404 n.mi
Hp = 186.722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17301659.63 X = -5228823.44
Y = -13635462.23 feet Y = -4214810.67 meter
Z = 1447747.33 Z = 415763.64
XDOT = 10806.449620 XDOT = 3303.834254
YDOT = -11572.030733 feet/sec YDOT = -3490.265419 meter/sec
ZDOT = 19699.562993 ZDOT = 6020.452377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18003985.52 X = 5487614.79
Y = -12704672.00 feet Y = -3872384.03 meter
Z = 1347977.47 Z = 410863.53
XDOT = 7117.308600 XDOT = 2169.355661
YDOT = 12234.696727 feet/sec YDOT = 3729.135562 meter/sec
ZDOT = 19761.719292 ZDOT = 6023.372040
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09045.36769135 .00010596 00000-0 82463-4 0 9053
2 25544 51.6414 215.8876 0009097 21.9177 338.2372 15.70896155 26634
Satellite: ISS
Catalog Number: 25544
Epoch time: 09045.36769135 = yrday.fracday
Element set: 905
Inclination: 51.6414 deg
RA of node: 215.8876 deg
Eccentricity: .0009097
Arg of perigee: 21.9177 deg
Mean anomaly: 338.2372 deg
Mean motion: 15.70896155 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2663
Checksum: 337
Coasting Arc #7 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2009/046/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1475788.76 A = 6729066.16 meter
Y = 3973425.71 meter E = .0020948
Z = -5243236.57 I = 51.45419
XDOT = -6860.913937 Wp = 62.92545
YDOT = -3395.512897 meter/sec RA = 210.11852 deg
ZDOT = -634.657942 TA = 200.96746
MA = 201.05348
Ha = 197.490 n.mi
Hp = 186.455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4841826.64 X = -1494640.20
Y = 13036173.59 feet Y = 3956817.08 meter
Z = -17202219.73 Z = -5250451.73
XDOT = -22509.560162 XDOT = -6819.351817
YDOT = -11140.134175 feet/sec YDOT = -3472.003252 meter/sec
ZDOT = -2082.211097 ZDOT = -667.886827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11283749.89 X = -3439286.97
Y = -8068792.81 feet Y = -2459368.05 meter
Z = -17230004.11 Z = -5251705.25
XDOT = 16183.720100 XDOT = 4932.797886
YDOT = -17856.629253 feet/sec YDOT = -5442.700596 meter/sec
ZDOT = -2212.009122 ZDOT = -674.220380
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09046.32192233 .00010596 00000-0 82463-4 0 9060
2 25544 51.6410 211.0095 0009157 25.0538 335.1066 15.70916039 26780
Satellite: ISS
Catalog Number: 25544
Epoch time: 09046.32192233 = yrday.fracday
Element set: 906
Inclination: 51.6410 deg
RA of node: 211.0095 deg
Eccentricity: .0009157
Arg of perigee: 25.0538 deg
Mean anomaly: 335.1066 deg
Mean motion: 15.70916039 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2678
Checksum: 290
Coasting Arc #8 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2009/047/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6358515.74 A = 6739981.66 meter
Y = 1626262.63 meter E = .0017033
Z = 1522887.32 I = 51.51702
XDOT = 90.451367 Wp = 85.32810
YDOT = 5095.718488 meter/sec RA = 204.97593 deg
ZDOT = -5762.621439 TA = 77.88890
MA = 77.69811
Ha = 197.611 n.mi
Hp = 186.356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20861272.10 X = 6332460.20
Y = 5335507.31 feet Y = 1697221.56 meter
Z = 4996349.48 Z = 1553713.30
XDOT = 296.756454 XDOT = 61.456888
YDOT = 16718.236508 feet/sec YDOT = 5096.567845 meter/sec
ZDOT = -18906.238317 ZDOT = -5762.252464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10411455.72 X = -3173411.70
Y = 18816093.56 feet Y = 5735145.32 meter
Z = 5116642.76 Z = 1559552.71
XDOT = -14909.036321 XDOT = -4544.274271
YDOT = -3059.564666 feet/sec YDOT = -932.555310 meter/sec
ZDOT = -18904.368523 ZDOT = -5762.051526
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09047.33976308 .00010596 00000-0 82463-4 0 9076
2 25544 51.6410 205.8067 0009154 29.5171 330.6506 15.70892795 26948
Satellite: ISS
Catalog Number: 25544
Epoch time: 09047.33976308 = yrday.fracday
Element set: 907
Inclination: 51.6410 deg
RA of node: 205.8067 deg
Eccentricity: .0009154
Arg of perigee: 29.5171 deg
Mean anomaly: 330.6506 deg
Mean motion: 15.70892795 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2694
Checksum: 324
Coasting Arc #9 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2009/048/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1696079.83 A = 6731667.83 meter
Y = -4547111.25 meter E = .0012934
Z = 4652611.76 I = 51.51539
XDOT = 7168.080097 Wp = 71.32931
YDOT = 211.473288 meter/sec RA = 199.89033 deg
ZDOT = 2817.458629 TA = 350.80928
MA = 350.83293
Ha = 197.750 n.mi
Hp = 186.261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5564566.38 X = -1667708.44
Y = -14918344.00 feet Y = -4565919.23 meter
Z = 15264474.29 Z = 4644441.18
XDOT = 23517.323153 XDOT = 7151.496119
YDOT = 693.810000 feet/sec YDOT = 291.538165 meter/sec
ZDOT = 9243.630671 ZDOT = 2852.240366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15829258.46 X = 4824757.98
Y = -1984705.33 feet Y = -604938.18 meter
Z = 15232238.29 Z = 4642786.23
XDOT = -6338.591161 XDOT = -1932.002586
YDOT = 21487.631886 feet/sec YDOT = 6549.430199 meter/sec
ZDOT = 9379.237193 ZDOT = 2858.791497
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09048.35759581 .00010596 00000-0 82463-4 0 9082
2 25544 51.6403 200.6027 0009275 32.6181 327.5552 15.70891006 27108
Satellite: ISS
Catalog Number: 25544
Epoch time: 09048.35759581 = yrday.fracday
Element set: 908
Inclination: 51.6403 deg
RA of node: 200.6027 deg
Eccentricity: .0009275
Arg of perigee: 32.6181 deg
Mean anomaly: 327.5552 deg
Mean motion: 15.70891006 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2710
Checksum: 300
Coasting Arc #10 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2009/049/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5739693.44 A = 6736074.95 meter
Y = 1210071.81 meter E = .0012633
Z = -3312157.26 I = 51.55809
XDOT = -3715.788547 Wp = 53.20432
YDOT = -4829.408984 meter/sec RA = 194.72375 deg
ZDOT = 4694.516379 TA = 267.91096
MA = 268.05564
Ha = 197.603 n.mi
Hp = 186.069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18831015.24 X = -5736708.51
Y = 3970051.86 feet Y = 1145903.97 meter
Z = -10866657.67 Z = -3340032.92
XDOT = -12190.907308 XDOT = -3684.313839
YDOT = -15844.517663 feet/sec YDOT = -4870.785200 meter/sec
ZDOT = 15401.956625 ZDOT = 4676.541753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 226403.89 X = 69007.91
Y = -19181909.84 feet Y = -5846646.12 meter
Z = -10975234.48 Z = -3345251.47
XDOT = 16745.685789 XDOT = 5104.085028
YDOT = -8537.783684 feet/sec YDOT = -2602.316467 meter/sec
ZDOT = 15331.469339 ZDOT = 4673.031855
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09049.31180602 .00010596 00000-0 82463-4 0 9092
2 25544 51.6394 195.7242 0009145 35.2219 324.9546 15.70929662 27257
Satellite: ISS
Catalog Number: 25544
Epoch time: 09049.31180602 = yrday.fracday
Element set: 909
Inclination: 51.6394 deg
RA of node: 195.7242 deg
Eccentricity: .0009145
Arg of perigee: 35.2219 deg
Mean anomaly: 324.9546 deg
Mean motion: 15.70929662 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2725
Checksum: 319
Coasting Arc #11 (Orbit 2740)
---------------------------------------
Vector Time (GMT): 2009/050/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597477.36 A = 6735898.25 meter
Y = 3544098.44 meter E = .0012865
Z = -3433250.70 I = 51.58517
XDOT = -5527.924163 Wp = 56.45007
YDOT = 2741.629786 meter/sec RA = 189.65750 deg
ZDOT = -4577.649944 TA = 164.06928
MA = 164.02877
Ha = 197.740 n.mi
Hp = 186.071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15083587.14 X = 4574182.73
Y = 11627619.55 feet Y = 3595379.92 meter
Z = -11263945.86 Z = -3410973.13
XDOT = -18136.234132 XDOT = -5535.933746
YDOT = 8994.848379 feet/sec YDOT = 2679.768628 meter/sec
ZDOT = -15018.536561 ZDOT = -4604.523439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14443487.50 X = -4402374.99
Y = 12492312.34 feet Y = 3807656.80 meter
Z = -11176780.16 Z = -3406682.59
XDOT = -4259.097692 XDOT = -1298.172976
YDOT = -18439.057560 feet/sec YDOT = -5620.224744 meter/sec
ZDOT = -15123.088169 ZDOT = -4609.517274
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09050.32962469 .00010596 00000-0 82463-4 0 9106
2 25544 51.6385 190.5207 0009167 39.0542 321.1280 15.70933853 27415
Satellite: ISS
Catalog Number: 25544
Epoch time: 09050.32962469 = yrday.fracday
Element set: 910
Inclination: 51.6385 deg
RA of node: 190.5207 deg
Eccentricity: .0009167
Arg of perigee: 39.0542 deg
Mean anomaly: 321.1280 deg
Mean motion: 15.70933853 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2741
Checksum: 301
Coasting Arc #12 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2009/051/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3619854.82 A = 6731667.81 meter
Y = -3351465.82 meter E = .0017166
Z = 4573519.98 I = 51.60118
XDOT = 6479.661600 Wp = 53.47262
YDOT = 2889.135475 meter/sec RA = 184.49365 deg
ZDOT = -2993.579627 TA = 66.35675
MA = 66.17665
Ha = 197.656 n.mi
Hp = 185.849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11876164.12 X = 3634845.64
Y = -10995622.76 feet Y = -3310902.73 meter
Z = 15004986.81 Z = 4591141.18
XDOT = 21258.732283 XDOT = 6461.415146
YDOT = 9478.790929 feet/sec YDOT = 2961.492833 meter/sec
ZDOT = -9821.455470 ZDOT = -2962.146475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8627635.21 X = 2629703.21
Y = 13618099.65 feet Y = 4150796.77 meter
Z = 15073416.87 Z = 4594377.46
XDOT = -12261.126817 XDOT = -3737.191454
YDOT = 18567.362698 feet/sec YDOT = 5659.332150 meter/sec
ZDOT = -9698.629904 ZDOT = -2956.142395
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09051.34743521 .00010596 00000-0 82463-4 0 9116
2 25544 51.6389 185.3164 0009131 42.4119 317.7747 15.70965127 27577
Satellite: ISS
Catalog Number: 25544
Epoch time: 09051.34743521 = yrday.fracday
Element set: 911
Inclination: 51.6389 deg
RA of node: 185.3164 deg
Eccentricity: .0009131
Arg of perigee: 42.4119 deg
Mean anomaly: 317.7747 deg
Mean motion: 15.70965127 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2757
Checksum: 313
Coasting Arc #13 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2009/052/07:19:00.000
Vector Time (MET): N/A
Weight (LBS) : 637863.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6383338.60 A = 6739623.76 meter
Y = -1277650.16 meter E = .0022963
Z = 1697197.87 I = 51.65625
XDOT = 2442.478265 Wp = 57.55168
YDOT = -4548.386925 meter/sec RA = 179.41757 deg
ZDOT = 5718.538646 TA = 321.21144
MA = 321.37606
Ha = 197.812 n.mi
Hp = 185.749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20942711.93 X = -6376821.74
Y = -4191765.60 feet Y = -1348995.92 meter
Z = 5568234.50 Z = 1666204.27
XDOT = 8013.380134 XDOT = 2465.378666
YDOT = -14922.529280 feet/sec YDOT = -4520.945661 meter/sec
ZDOT = 18761.609732 ZDOT = 5730.459520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7652869.31 X = 2332594.57
Y = -19973342.70 feet Y = -6087874.85 meter
Z = 5447246.09 Z = 1660320.61
XDOT = 11927.298436 XDOT = 3635.440563
YDOT = 9739.451750 feet/sec YDOT = 2968.584893 meter/sec
ZDOT = 18807.710437 ZDOT = 5732.590141
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09052.36523955 .00010596 00000-0 82463-4 0 9127
2 25544 51.6379 180.1122 0009129 46.9069 313.2855 15.70971405 27738
Satellite: ISS
Catalog Number: 25544
Epoch time: 09052.36523955 = yrday.fracday
Element set: 912
Inclination: 51.6379 deg
RA of node: 180.1122 deg
Eccentricity: .0009129
Arg of perigee: 46.9069 deg
Mean anomaly: 313.2855 deg
Mean motion: 15.70971405 rev/day
Decay rate: 1.05960E-04 rev/day^2
Epoch rev: 2773
Checksum: 315
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