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[IGSREPORT-14962] Wk 1419 IGLOS Final Orbits
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IGS Electronic Report 05 Apr 06:02:47 PDT 2007 Message Number 14962
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1419 (Mar 18, 2007 - Mar 24, 2007)
Contact: Gerd Gendt (gendt @ gfz-potsdam.de)
Thomas Nischan ( nisn @ gfz-potsdam.de)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the centers
absolute deviation to the unweighted average orbit after removing small
differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1419.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed to
the values of the final IGS (GPS) combination.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl1419[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1419 in the SP3 format.
igl14197.sum Combination Report for GPS Week 1419.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 725.1 ns
1 | 811.6 ns
2 | 807.4 ns
3 | 839.8 ns
4 | 836.7 ns
5 | 830.4 ns
6 | 817.0 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESX | R24
4 | BKG | R23
5 | BKG | R23
6 | BKG | R23
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1419, 1a.1419).
Table 2 contains the complete ephemeris and clock correction transformation
parameters (includes both the apriori and a posteriori values) for each
centre and each day (Tables 2.1419.0-6)
Table 3 contains two types of daily RMS for each satellite and centre, along
with the computed satellite position sigmas for the combined orbits
(tables 3.1419.0-6).
The first type of satellite RMS is based on orbit combination and the
second RMS type is a result of the 7-day arc evaluation of each centre
ephemerides.
Table 1: Week 1419 summary. (Mar 18, 2007 - Mar 24, 2007)
Table 1.1419.a GPS week : 1419 MJD: 54177.0-54183.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 55| 0 0 -2 98 -3 -7 -.03 52 41 | 0 811 5702 6407
| 2 3 7 48 53 84 .13 | 0 2320
cod 166| -1 0 -3 129 -49 -16 -.08 46 34 | --- --- --- ---
| 3 4 7 113 100 129 .13 | --- ---
esx 45| 6 -2 7 59 35 -126 -.19 131 62 | 372379 3586 16303 30011
| 7 5 17 114 166 311 .15 | 1060144 20309
iac n/a| 0 1 2 -251 60 115 .22 74 74 | 811984 727 14991 27677
| 4 5 4 46 42 61 .08 | 43130 14234
mcc n/a| -16 -32 -30 211 -422 -2376 -2.07 759 759 | --- --- --- ---
| 27 51 329 896 864 1643 1.48 | --- ---
Table 1.1419.b GPS week : 1419 MJD: 54177.0-54183.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 21 16 14 23 22 20 19 |
R02 | 40 35 15 15 15 19 17 |
R03 | 24 36 27 23 24 44 27 |
R04 | 17 19 37 25 19 29 19 |
R06 | 27 34 33 29 29 19 29 |
R07 | 36 83 33 31 18 27 39 |
R08 | 33 22 63 20 22 18 21 |
R10 | 23 16 25 21 30 50 39 |
R14 | 23 18 34 45 35 28 44 |
R15 | 0 0 0 0 0 0 0 |
R19E | 43 69 23 23 25 23 24 |
R23E | 35 50 27 130 0 0 0 |
R24E | 29 102 89 111 91 56 61 |
Table 1.1419.c GPS week : 1419 MJD: 54177.0-54183.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 1419 0 | 604 -307 -504 6153 3328 -368500 94.4 11010 11010 | 725144 0
brd 1419 1 | 40 426 -512 421 -2490 -375100 88.3 11840 11840 | 811613 0
brd 1419 2 | 336 207 -309 -5379 2655 -386100 64.5 13340 13340 | 807417 0
brd 1419 3 | -551 23 -245 1756 3879 -399400 94.7 10600 10600 | 839820 0
brd 1419 4 | -456 231 -1442 -8994 -1952 -392500 104.7 10020 10020 | 836736 0
brd 1419 5 | -830 -645 -830 -3812 9449 -389200 91.6 10720 10720 | 830444 0
brd 1419 6 | -480 -255 -566 -3243 -4700 -365000 91.7 8952 8952 | 817004 0
-------------+------------------------------------------------------------+----------------
brd 1419 mean| -190 -45 -630 -1871 1452 -382257 90.0 10926 10926 | 809739 0
brd 1419 sdev| 525 374 404 5024 4826 12910 12.4 1386 1386 | 39328 0
Table 2: Daily transformation of each centre to the combined IGL orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1419.0 GPS week: 1419 Day: 0 MJD: 54177
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 55| 2 1 -1 63 82 29 .15 54 62 | 0 2333 6755 7573
cod 166| 4 1 -3 36 20 25 -.04 26 26 | --- --- --- ---
esx 45| 0 -5 16 122 45 -23 -.09 158 50 | -85185 11303 13028 20678
iac n/a| -5 -1 3 -302 13 53 .14 101 101 | 718222 6657 12130 18897
mcc n/a| 18 -104 440 701 -1394 -1231 -3.53 329 329 | --- --- --- ---
Table 2.1419.1 GPS week: 1419 Day: 1 MJD: 54178
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 55| -1 -6 -11 90 58 76 .11 52 43 | 0 1448 4383 4729
cod 166| -2 4 -13 -11 90 -290 .11 59 36 | --- --- --- ---
esx 45| 1 0 18 117 -183 42 -.29 128 57 | -101004 -7606 10773 19044
iac n/a| 8 13 5 -239 37 153 .30 196 196 | 815239 -5494 9853 16967
Table 2.1419.2 GPS week: 1419 Day: 2 MJD: 54179
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 55| 0 -2 4 85 -61 -128 -.05 53 36 | 0 3210 4996 5427
cod 166| -3 -5 -9 220 -28 -38 -.05 52 33 | --- --- --- ---
esx 45| 22 9 37 -160 -120 346 -.46 214 75 | 2773857 27128 8116 15638
iac n/a| 0 0 -5 -290 121 168 .18 59 59 | 809937 -1786 7775 14903
Table 2.1419.3 GPS week: 1419 Day: 3 MJD: 54180
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 55| 3 1 5 81 -32 -10 -.12 91 45 | 0 537 5007 5578
cod 166| 2 -8 -9 308 -58 6 -.06 60 39 | --- --- --- ---
esx 45| 0 -6 -8 33 0 -373 -.15 133 62 | -26836 -23518 13341 27088
iac n/a| -3 1 4 -249 59 136 .19 53 53 | 833940 -6009 12625 26437
Table 2.1419.4 GPS week: 1419 Day: 4 MJD: 54181
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 55| 1 -1 3 86 -22 -63 -.04 24 24 | 0 255 3732 4175
cod 166| -3 2 0 50 -56 97 -.04 33 33 | --- --- --- ---
esx 45| 4 -3 -11 14 17 -18 -.20 77 62 | -5952 25383 16971 19955
iac n/a| -5 -1 4 -160 50 72 .12 35 35 | 823664 23592 14316 17636
mcc n/a| -29 16 -326 883 -748 -700 -1.86 2331 2331 | --- --- --- ---
Table 2.1419.5 GPS week: 1419 Day: 5 MJD: 54182
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 55| -2 0 -13 77 -40 108 -.21 44 31 | 0 1820 4556 4871
cod 166| -4 3 7 174 -81 83 -.25 41 35 | --- --- --- ---
esx 45| 8 -7 8 95 198 -605 -.02 99 63 | 37425 10648 17249 46120
iac n/a| 1 -2 0 -250 23 33 .33 34 34 | 842073 9535 16149 42622
mcc n/a| -44 -21 -139 352 -192 -3819 -2.77 188 188 | --- --- --- ---
Table 2.1419.6 GPS week: 1419 Day: 6 MJD: 54183
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 55| -2 4 -5 207 -11 -66 -.02 46 42 | 0 -3926 10485 12501
cod 166| -2 -3 1 130 -234 -1 -.26 48 38 | --- --- --- ---
esx 45| 6 -1 -7 194 294 -256 -.13 110 64 | 14350 -18236 34645 61554
iac n/a| 1 3 9 -269 115 191 .28 38 38 | 840816 -21405 32094 56279
mcc n/a| -9 -21 -94 -1092 643 -3754 -.10 190 190 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGL orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1419.0 GPS week: 1419 Day: 0 MJD: 54177
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9960 41 26 29 62 --- 21 | 61 59 74 61 --- 55
R02 | 4650 42 20 38 184 --- 40 | 39 50 58 229 --- 63
XR03 | ---- --- 12 --- 46 --- 23 | --- 36 --- 41 --- 37
R04 | 2196 16 22 39 51 --- 17 | 59 58 65 46 --- 56
R06 | 3997 53 27 66 53 --- 27 | 47 59 71 67 --- 53
R07 |20416 95 25 77 55 233 36 | 43 39 67 87 222 28
R08 | 6655 42 31 107 29 --- 33 | 47 32 108 75 --- 43
XR10 | 2079 35 17 --- 57 --- 22 | 47 53 --- 52 --- 42
XR14 | 3920 18 22 --- 67 --- 23 | 38 49 --- 68 --- 40
XR15 | ---- --- 4 --- --- --- 0 | --- 247 --- --- --- 243
R19E | 7020 60 25 57 180 --- 43 | 263 241 270 269 --- 243
XR23E | 3854 36 30 --- 103 --- 35 | 443 98 --- 26 --- 111
R24E |17836 54 30 414 46 402 28 | 501 526 426 521 24 507
------+------------------------------------+--------------------------------
RMS |11012 54 26 158 101 329 |T 144 119 142 128 123 117
WRMS |11012 62 26 50 101 329 |NE 47 68 73 80 222 66
MEDI | 4650 42 25 57 55 233 |MD 47 58 71 67 24 55
Table 3.1419.1 GPS week: 1419 Day: 1 MJD: 54178
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 7853 24 19 37 42 16 | 67 72 93 83 69
R02 |10553 26 20 42 163 34 | 35 38 70 180 45
XR03 | ---- --- 25 --- 58 36 | --- 64 --- 43 56
R04 | 4346 36 30 25 38 19 | 42 36 85 29 37
R06 | 6184 52 57 63 66 33 | 37 56 62 75 29
R07 |17914 68 65 62 400 83 | 44 62 77 444 69
R08 | 2648 17 27 62 56 22 | 44 33 136 48 48
XR10 | 2479 17 25 --- 30 16 | 31 57 --- 44 38
XR14 | 1460 16 22 --- 47 17 | 50 50 --- 34 41
XR15 | ---- --- 19 --- --- 0 | --- 458 --- --- 454
R19E | 8290 50 67 77 315 68 | 176 166 168 361 171
XR23E | 4693 40 46 --- 159 49 | 305 133 --- 25 128
R24E |22228 93 114 332 99 101 | 578 632 524 625 607
------+-------------------------------+---------------------------
RMS |11837 52 59 128 196 |T 128 142 151 165 137
WRMS |11837 43 36 57 196 |NE 43 92 87 108 88
MEDI | 6184 36 27 62 58 |MD 44 62 85 48 56
Table 3.1419.2 GPS week: 1419 Day: 2 MJD: 54179
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 5610 11 22 58 24 14 | 70 79 82 72 68
R02 |11129 18 22 52 25 14 | 68 58 98 63 60
XR03 |23551 42 32 --- 36 26 | 67 38 --- 37 44
R04 | 7346 39 49 185 31 36 | 68 40 142 39 40
R06 | 4524 63 54 61 49 33 | 81 72 97 43 50
R07 |27766 20 37 129 72 32 | 64 67 71 112 60
R08 | 3610 47 49 368 40 62 | 76 58 383 81 74
XR10 | 3458 40 32 --- 33 25 | 42 56 --- 37 31
XR14 | 2988 40 59 --- 42 33 | 49 47 --- 62 38
XR15 | ---- --- 15 --- --- 0 | --- 486 --- --- 488
R19E | 9097 24 36 48 55 23 | 96 95 102 127 97
XR23E | 4655 20 33 --- --- 27 | 357 108 --- --- 97
R24E |18073 115 102 409 118 89 | 488 612 627 620 568
------+-------------------------------+---------------------------
RMS |13337 53 52 214 59 |T 127 139 200 117 131
WRMS |13337 36 33 75 59 |NE 65 100 145 60 95
MEDI | 5610 39 36 61 40 |MD 68 67 98 63 60
Table 3.1419.3 GPS week: 1419 Day: 3 MJD: 54180
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 3380 15 48 82 14 22 | 91 111 63 88 84
R02 | 9770 22 25 49 15 14 | 51 43 27 39 36
XR03 | ---- 38 26 --- 32 23 | 38 59 --- 81 67
R04 | 7692 37 56 31 38 24 | 42 46 63 43 32
R06 | 4274 59 42 85 32 29 | 55 66 52 46 45
R07 |18491 61 32 81 49 31 | 42 80 37 113 60
R08 | 4027 29 39 61 17 19 | 47 58 63 37 36
XR10 | 3843 34 37 --- 17 20 | 41 82 --- 49 50
XR14 | 4598 64 75 --- 55 45 | 46 70 --- 62 40
XR15 | ---- --- 20 --- --- 0 | --- 540 --- --- 547
R19E | 9081 28 46 46 37 22 | 110 111 131 133 117
XR23E | 3024 142 118 --- --- 130 | 919 95 --- --- 144
R24E |16527 235 129 336 124 110 | 325 465 504 647 386
------+-------------------------------+---------------------------
RMS |10595 91 60 133 53 |T 150 140 117 121 126
WRMS |10595 45 39 62 53 |NE 50 115 50 62 99
MEDI | 4598 37 42 61 32 |MD 47 80 63 62 60
Table 3.1419.4 GPS week: 1419 Day: 4 MJD: 54181
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2782 14 40 91 25 --- 22 | 34 51 89 31 --- 33
R02 | 5780 13 23 47 27 --- 14 | 33 43 53 52 --- 39
XR03 | ---- 25 35 --- 39 --- 23 | 38 57 --- 41 --- 38
R04 | 7729 24 32 27 43 --- 19 | 31 54 45 35 --- 31
R06 | 5279 37 22 132 25 --- 29 | 47 39 58 37 --- 28
R07 |21786 19 25 74 23 2330 18 | 43 43 67 49 133 37
R08 | 4698 27 47 59 31 --- 22 | 49 46 112 60 --- 49
XR10 | 3323 35 61 --- 27 --- 30 | 62 74 --- 48 --- 53
XR14 | 6171 40 67 --- 39 --- 34 | 51 65 --- 61 --- 48
XR15 | ---- --- 7 --- --- --- 0 | --- 336 --- --- --- 338
R19E | 8757 28 33 66 56 --- 25 | 100 97 116 112 --- 96
XR23E | 2705 2037 7 --- --- --- 0 | 784 207 --- --- --- 197
XR24E |14351 150 80 --- 133 --- 91 | 492 415 --- 505 --- 445
------+------------------------------------+--------------------------------
RMS |10015 24 33 77 35 2330 |T 147 117 77 93 133 110
WRMS |10015 24 33 62 35 2330 |NE 43 80 70 46 133 69
MEDI | 5780 27 33 66 31 2330 |MD 47 57 67 49 133 48
Table 3.1419.5 GPS week: 1419 Day: 5 MJD: 54182
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2200 34 34 64 19 --- 20 | 64 58 73 43 --- 44
R02 | 3738 20 30 60 28 --- 18 | 40 29 54 24 --- 22
XR03 | ---- 72 52 --- 61 --- 44 | 42 93 --- 95 --- 66
R04 | 6730 61 29 74 42 --- 28 | 63 33 64 27 --- 27
R06 | 9070 29 37 48 24 --- 18 | 30 51 57 31 --- 29
R07 |20601 31 68 33 35 188 26 | 37 78 49 50 98 37
R08 | 6164 29 21 66 20 --- 18 | 34 44 100 44 --- 40
XR10 | 3777 97 74 --- 33 --- 49 | 64 78 --- 43 --- 35
XR14 | 3994 36 48 --- 32 --- 27 | 47 47 --- 67 --- 43
XR15 | ---- --- 14 --- --- --- 0 | --- 233 --- --- --- 239
R19E | 7505 25 37 67 38 --- 23 | 94 103 123 117 --- 96
XR23E | 4452 4731 13 --- --- --- 0 | 9999 277 --- --- --- 288
R24E |15940 83 53 230 51 --- 56 | 213 265 338 317 --- 255
------+------------------------------------+--------------------------------
RMS |10719 44 41 99 34 188 |T 66 106 107 78 98 93
WRMS |10719 31 35 63 34 188 |NE 46 74 66 47 98 58
MEDI | 6164 34 37 64 33 188 |MD 47 78 64 44 98 43
Table 3.1419.6 GPS week: 1419 Day: 6 MJD: 54183
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3709 26 25 65 24 --- 18 | 57 64 61 57 --- 52
R02 | 3703 11 33 47 26 --- 16 | 39 57 55 25 --- 31
XR03 | ---- 30 49 --- 33 --- 26 | 67 58 --- 58 --- 53
R04 | 2838 29 36 59 18 --- 19 | 55 49 48 33 --- 37
R06 |11181 31 64 67 42 --- 28 | 37 84 63 31 --- 33
R07 |16054 76 88 69 35 190 39 | 37 75 65 38 87 38
R08 | 5608 31 28 81 20 --- 21 | 43 38 67 31 --- 26
XR10 | 3423 75 43 --- 43 --- 38 | 54 71 --- 49 --- 45
XR14 | 3404 89 37 --- 49 --- 43 | 75 69 --- 78 --- 47
XR15 | ---- --- 16 --- --- --- 0 | --- 287 --- --- --- 288
R19E | 6014 33 35 80 32 --- 23 | 194 193 202 219 --- 192
XR23E | 7444 4871 16 --- --- --- 0 | 9999 173 --- --- --- 172
R24E |12453 79 40 253 75 --- 61 | 438 391 333 387 --- 399
------+------------------------------------+--------------------------------
RMS | 8951 46 48 110 38 190 |T 99 123 111 91 87 108
WRMS | 8951 42 38 64 38 190 |NE 51 85 59 44 87 65
MEDI | 5608 31 36 67 33 190 |MD 55 71 63 49 87 47