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[IGSREPORT-15320] Wk 1435 IGLOS Final Orbits
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IGS Electronic Report 26 Jul 01:33:47 PDT 2007 Message Number 15320
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1435 (Jul 08, 2007 - Jul 14, 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 2.1435.
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:
igl1435[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1435 in the SP3 format.
igl14357.sum Combination Report for GPS Week 1435.
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 | 1096.7 ns
1 | 1083.7 ns
2 | 1059.0 ns
3 | 1077.7 ns
4 | 1125.2 ns
5 | 1092.3 ns
6 | 1065.5 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
----+--------+---------------
2 | ESX | R23
5 | BKG | R24
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 1.1435, 1a.1435).
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 2.1435.0-6)
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 3.1435.0-6).
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 1435 summary. (Jul 08, 2007 - Jul 14, 2007)
Table 1.1435.a GPS week : 1435 MJD: 54289.0-54295.0
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 57| -2 -2 -17 21 89 82 -.04 58 53 | 0 95 3791 4072
| 5 4 7 96 49 117 .15 | 0 484
cod 170| 3 -1 0 -7 -59 76 -.12 46 44 | --- --- --- ---
| 2 6 7 51 112 76 .14 | --- ---
esx 43| 0 0 16 101 8 -77 -.50 171 71 | 880462 10507 13569 26208
| 6 8 22 161 164 323 .33 | 2018314 30117
iac n/a| 0 -1 15 -35 -3 -231 .53 60 60 | 1083464 1807 13124 25782
| 6 2 6 24 81 102 .19 | 21401 11596
mcc n/a| 5 -4 21 11 36 667 .54 76 76 | --- --- --- ---
| 14 13 35 198 153 541 .33 | --- ---
Table 1.1435.b GPS week : 1435 MJD: 54289.0-54295.0
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
------+------------------------------------+------------------------------------------
R01E | 22 26 23 47 16 22 44 |
R03E | 27 28 28 20 65 23 34 |
R04E | 19 18 28 18 37 24 30 |
R06E | 25 31 26 21 23 22 57 |
R07E | 25 21 27 27 47 50 24 |
R08E | 32 73 20 28 46 32 41 |
R10 | 29 19 20 28 16 19 27 |
R14 | 17 32 27 19 26 27 68 |
R15 | 0 0 0 0 0 0 0 |
R21 | 52 25 23 25 68 31 46 |
R22 | 0 0 --- --- --- --- 0 |
R23 | 74 70 26 69 34 47 116 |
R24 | 0 167 187 142 180 235 171 |
Table 1.1435.c GPS week : 1435 MJD: 54289.0-54295.0
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 1435 0 | -245 273 -46 8500 4721 -364600 84.7 7637 7637 | 1096675 0
brd 1435 1 | 651 -161 -869 1771 1357 -315500 92.7 7421 7421 | 1083655 0
brd 1435 2 | -210 -281 -1517 4204 7939 -305500 89.7 13080 13080 | 1059015 0
brd 1435 3 | 205 -30 -793 627 1812 -337900 105.9 11220 11220 | 1077663 0
brd 1435 4 | 477 458 -3 -561 952 -332900 97.2 8735 8735 | 1125214 0
brd 1435 5 | 248 499 129 7005 6324 -342400 76.9 7795 7795 | 1092253 0
brd 1435 6 | -970 363 -662 3313 6161 -331400 94.6 10380 10380 | 1065531 0
-------------+------------------------------------------------------------+----------------
brd 1435 mean| 22 160 -537 3551 4180 -332885 91.7 9466 9466 | 1085715 0
brd 1435 sdev| 547 314 594 3304 2796 19043 9.2 2153 2153 | 22031 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 2.1435.0 GPS week: 1435 Day: 0 MJD: 54289
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 57| -4 1 -12 -70 90 85 -.18 35 34 | 0 716 2729 2991
cod 170| 2 -3 -1 -27 -44 107 .02 38 36 | --- --- --- ---
esx 43| 1 3 22 401 -79 -179 .04 175 67 | 4531423 35569 9481 16276
iac n/a| 2 -3 27 -58 15 -318 .26 68 68 | 1097040 8509 9709 17988
mcc n/a| 4 2 11 94 284 878 .70 45 45 | --- --- --- ---
Table 2.1435.1 GPS week: 1435 Day: 1 MJD: 54290
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 57| 1 -5 -16 103 97 56 .01 44 38 | 0 129 3304 3644
cod 170| 2 10 5 -92 -231 -46 -.19 49 44 | --- --- --- ---
esx 43| 2 -9 8 191 193 307 -.41 227 86 | 2876504 2398 10641 16617
iac n/a| -9 -5 16 -22 41 -240 .41 60 60 | 1089791 -5519 12131 19890
mcc n/a| 12 -5 40 -65 177 1355 .86 85 85 | --- --- --- ---
Table 2.1435.2 GPS week: 1435 Day: 2 MJD: 54291
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 57| 1 -1 -22 148 105 97 .19 54 55 | 0 490 3743 3831
cod 170| 7 -5 2 -14 -12 198 -.34 41 43 | --- --- --- ---
esx 43| -3 7 -13 -54 -65 -284 -.60 196 73 | -233173 4519 10126 21255
iac n/a| -1 0 8 -16 11 -84 .39 24 24 | 1060411 9690 9958 21680
mcc n/a| 24 -22 44 170 71 1324 .82 87 87 | --- --- --- ---
Table 2.1435.3 GPS week: 1435 Day: 3 MJD: 54292
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 57| 3 4 -24 -47 63 148 -.20 44 40 | 0 -164 3441 3629
cod 170| 2 -7 3 38 -54 119 -.07 27 26 | --- --- --- ---
esx 43| 10 0 44 157 273 -568 -.49 235 104 | 55901 -34991 8557 15684
iac n/a| -3 2 19 -57 76 -219 .62 48 48 | 1082906 -14011 9990 19779
mcc n/a| 0 -17 64 -150 -149 517 -.10 64 64 | --- --- --- ---
Table 2.1435.4 GPS week: 1435 Day: 4 MJD: 54293
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 57| -3 0 -12 23 181 -135 -.13 66 56 | 0 -491 3363 3867
cod 170| 7 -4 -16 -35 -147 60 -.04 45 43 | --- --- --- ---
esx 43| -11 12 45 46 -93 354 -1.08 190 79 | -999999 -8948 13361 35809
iac n/a| -1 0 16 -34 48 -259 .75 74 74 | 1118097 -10023 12518 31418
mcc n/a| 4 5 39 95 -36 -89 .56 86 86 | --- --- --- ---
Table 2.1435.5 GPS week: 1435 Day: 5 MJD: 54294
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 57| -13 -6 -7 95 23 71 -.11 69 61 | 0 -474 4424 4590
cod 170| 4 0 5 25 -54 61 .04 46 49 | --- --- --- ---
esx 43| -1 0 -2 -36 7 -78 -.49 41 35 | -23104 17416 31615 51254
iac n/a| -2 1 10 1 -54 -123 .74 59 59 | 1080543 7098 26801 44340
mcc n/a| 13 -8 -32 -314 -101 401 .38 83 83 | --- --- --- ---
Table 2.1435.6 GPS week: 1435 Day: 6 MJD: 54295
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 57| -6 -9 -28 -98 60 254 .12 96 90 | 0 460 5538 5957
cod 170| 0 3 -3 55 129 33 -.23 72 63 | --- --- --- ---
esx 43| -4 -10 8 7 -175 -96 -.49 137 51 | -44317 57586 11203 26563
iac n/a| 11 -1 10 -63 -163 -377 .56 86 86 | 1055464 16907 10766 25380
mcc n/a| -20 17 -15 252 9 288 .56 81 81 | --- --- --- ---
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 3.1435.0 GPS week: 1435 Day: 0 MJD: 54289
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |10894 21 31 85 39 --- 21 | 59 65 80 92 --- 63
R03E | 5336 38 37 100 38 --- 26 | 43 48 118 65 --- 52
R04E | 6137 27 36 55 24 --- 19 | 44 37 81 47 --- 40
R06E |11099 22 51 45 53 --- 24 | 30 73 77 34 --- 39
R07E | 4820 41 40 67 35 45 24 | 63 46 71 42 21 40
R08E |11338 45 36 43 87 --- 31 | 77 66 106 73 --- 55
XR10 | 7012 42 24 --- 54 --- 28 | 29 30 --- 50 --- 27
XR14 | 6426 19 26 --- 29 --- 17 | 23 22 --- 39 --- 20
XR15 | ---- --- 7 --- --- 6780 0 | --- 9999 --- --- 141 9999
R21 | 1531 37 36 279 56 --- 52 | 70 58 206 73 --- 61
XR22 | ---- --- 7 --- --- --- 0 | --- 9999 --- --- --- 9999
R23 | 2090 42 33 372 135 --- 73 | 86 75 363 63 --- 73
XR24 | ---- --- 7 --- --- 2690 0 | --- 545 --- --- 14 540
------+------------------------------------+--------------------------------
RMS | 7636 35 38 175 68 45 |T 52 96 137 57 58 91
WRMS | 7636 34 36 67 68 45 |NE 52 146 284 56 77 144
MEDI | 6137 37 33 67 39 2690 |MD 44 58 81 50 21 52
Table 3.1435.1 GPS week: 1435 Day: 1 MJD: 54290
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8593 31 38 103 44 --- 25 | 68 70 69 85 --- 66
R03E |10338 24 25 149 41 --- 27 | 29 38 135 44 --- 38
R04E | 5173 22 27 56 34 --- 17 | 44 33 49 47 --- 35
R06E | 3232 32 70 96 38 --- 31 | 25 97 66 29 --- 38
R07E | 4754 35 36 41 39 85 21 | 55 48 49 52 20 38
R08E |11070 73 71 419 64 --- 73 | 76 64 284 65 --- 45
XR10 | 8300 21 23 --- 37 --- 19 | 34 25 --- 46 --- 27
XR14 | 7600 33 44 --- 61 --- 32 | 22 43 --- 63 --- 27
XR15 | ---- --- 17 --- --- 3723 0 | --- 9999 --- --- 167 9999
XR21 | 4834 31 36 --- 40 --- 25 | 49 48 --- 45 --- 39
XR22 | ---- --- 16 --- --- --- 0 | --- 9999 --- --- --- 9999
R23 | 4732 65 55 371 115 --- 69 | 48 78 184 73 --- 45
XR24 | ---- --- 76 366 --- 300 166 | --- 498 566 --- 10 495
------+------------------------------------+--------------------------------
RMS | 7421 44 49 226 60 85 |T 45 94 175 54 65 81
WRMS | 7421 38 44 86 60 85 |NE 38 138 375 56 88 126
MEDI | 5173 31 36 103 40 300 |MD 44 48 69 47 20 38
Table 3.1435.2 GPS week: 1435 Day: 2 MJD: 54291
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 7025 48 42 46 31 --- 22 | 62 58 107 68 --- 58
R03E |33594 57 32 112 19 --- 28 | 41 56 151 62 --- 60
R04E | 5619 71 27 104 17 --- 28 | 44 38 91 60 --- 49
R06E | 3166 45 56 68 26 --- 26 | 36 51 65 39 --- 25
R07E | 4026 73 43 69 22 87 26 | 59 41 66 59 22 42
R08E | 8727 32 26 73 25 --- 20 | 74 56 111 59 --- 51
XR10 | 7658 35 27 --- 24 --- 19 | 31 35 --- 31 --- 26
XR14 |10745 54 44 --- 25 --- 27 | 33 47 --- 44 --- 23
XR15 | ---- --- 13 --- --- 2319 0 | --- 9999 --- --- 136 9999
R21 | 6501 44 55 48 21 --- 23 | 46 60 97 42 --- 35
R23 | 3896 48 35 514 31 --- 25 | 49 37 338 41 --- 32
XR24 | ---- --- 120 289 --- 661 187 | --- 595 500 --- 16 597
------+------------------------------------+--------------------------------
RMS |13083 54 41 196 24 87 |T 47 97 169 50 58 90
WRMS |13083 55 43 73 24 87 |NE 39 154 311 39 76 142
MEDI | 6501 48 35 73 24 661 |MD 44 51 107 44 22 42
Table 3.1435.3 GPS week: 1435 Day: 3 MJD: 54292
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |10289 58 28 307 28 --- 46 | 55 50 166 67 --- 49
R03E |24184 39 23 64 34 --- 19 | 44 69 99 57 --- 47
R04E | 5779 24 25 66 35 --- 18 | 43 48 91 65 --- 48
R06E | 2808 29 34 75 30 --- 20 | 40 46 56 51 --- 35
R07E | 2576 56 28 107 37 64 26 | 54 35 75 52 20 28
XR08E | 9568 33 28 --- 55 --- 27 | 46 47 --- 75 --- 45
XR10 | 5616 52 15 --- 47 --- 27 | 42 29 --- 47 --- 24
XR14 | 5845 32 11 --- 34 --- 18 | 25 26 --- 53 --- 28
XR15 | ---- --- 9 --- --- 2419 0 | --- 9999 --- --- 407 9999
XR21 | 4797 35 24 --- 49 --- 25 | 39 28 --- 41 --- 23
R23 | 4119 45 23 459 91 --- 69 | 49 68 338 98 --- 52
XR24 | ---- --- 51 392 --- --- 142 | --- 493 442 --- --- 500
------+------------------------------------+--------------------------------
RMS |11222 44 27 235 48 64 |T 43 85 181 60 213 79
WRMS |11222 40 26 104 48 64 |NE 38 128 390 59 407 125
MEDI | 5616 35 24 107 35 64 |MD 43 47 99 53 20 45
Table 3.1435.4 GPS week: 1435 Day: 4 MJD: 54293
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9311 19 25 42 32 --- 16 | 63 53 112 51 --- 44
R03E |18339 92 65 291 57 --- 64 | 77 68 284 48 --- 59
R04E | 3628 63 32 116 76 --- 36 | 53 59 99 74 --- 50
R06E | 4080 23 24 95 41 --- 22 | 45 44 79 51 --- 41
R07E | 3150 80 36 68 132 86 47 | 52 38 58 80 21 36
R08E | 6815 94 68 126 44 --- 46 | 89 51 132 61 --- 51
XR10 | 6525 21 19 --- 30 --- 16 | 32 30 --- 31 --- 24
XR14 | 3371 36 21 --- 54 --- 26 | 22 35 --- 59 --- 27
XR15 | ---- --- 14 --- --- 3728 0 | --- 9999 --- --- 372 9999
R21 | 4986 42 43 351 87 --- 68 | 51 40 371 67 --- 48
XR23 | 3932 52 48 --- 38 --- 33 | 70 45 --- 66 --- 58
XR24 | ---- --- 86 377 --- --- 179 | --- 547 452 --- --- 546
------+------------------------------------+--------------------------------
RMS | 8735 66 45 190 74 86 |T 55 91 198 58 196 89
WRMS | 8735 56 43 79 74 86 |NE 43 139 411 55 372 140
MEDI | 4080 42 32 116 44 86 |MD 52 45 112 59 21 48
Table 3.1435.5 GPS week: 1435 Day: 5 MJD: 54294
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8691 69 27 14 43 --- 22 | 50 58 62 68 --- 51
R03E |15044 70 25 32 31 --- 22 | 49 61 67 68 --- 52
R04E | 3919 67 29 35 37 --- 23 | 39 56 61 51 --- 40
R06E | 6382 33 45 37 32 --- 21 | 36 57 71 44 --- 35
R07E | 3770 112 47 45 129 83 49 | 73 49 58 75 18 42
R08E | 6980 55 74 45 38 --- 31 | 66 57 87 66 --- 44
XR10 | 6820 34 22 --- 24 --- 18 | 16 20 --- 26 --- 18
XR14 | 3811 49 21 --- 43 --- 26 | 29 21 --- 46 --- 18
XR15 | ---- --- 6 --- --- 3855 0 | --- 9999 --- --- 136 9999
R21 | 2109 53 56 62 34 --- 31 | 34 42 104 49 --- 33
XR23 | 3972 49 78 --- 62 --- 47 | 46 113 --- 49 --- 74
XR24 | 8907 373 252 218 --- --- 235 | 33 448 370 --- --- 487
------+------------------------------------+--------------------------------
RMS | 7795 69 46 41 59 83 |T 42 89 110 54 77 81
WRMS | 7795 61 49 35 59 83 |NE 31 128 237 42 136 126
MEDI | 6382 55 29 37 37 83 |MD 39 57 67 49 18 42
Table 3.1435.6 GPS week: 1435 Day: 6 MJD: 54295
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8931 134 54 47 47 --- 44 | 69 64 84 75 --- 55
R03E |19396 73 42 46 67 --- 33 | 46 87 61 77 --- 58
R04E |15076 78 34 40 53 --- 30 | 36 43 75 65 --- 46
R06E | 5765 110 128 81 49 --- 57 | 46 145 46 44 --- 55
R07E | 7347 56 23 54 37 81 24 | 56 46 55 61 21 37
R08E | 7482 111 46 67 52 --- 40 | 86 73 71 68 --- 52
XR10 | 6075 51 24 --- 41 --- 27 | 29 32 --- 40 --- 29
XR14 | 5628 67 73 --- 133 --- 68 | 15 26 --- 179 --- 56
XR15 | ---- --- 9 --- --- 3483 0 | --- 9999 --- --- 278 9999
R21 | 3197 42 55 69 123 --- 46 | 51 40 53 123 --- 50
XR22 | ---- --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
R23 | 5021 125 119 356 169 --- 115 | 45 62 314 218 --- 89
XR24 |13476 270 113 345 --- --- 170 | 43 629 545 --- --- 620
------+------------------------------------+--------------------------------
RMS |10380 96 72 137 86 81 |T 47 113 144 95 149 104
WRMS |10380 90 63 51 86 81 |NE 36 157 304 140 278 168
MEDI | 7347 78 46 67 52 81 |MD 46 62 71 68 21 55