[IGSREPORT-15151] Wk 1426 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Tue Jun 5 23:51:37 PDT 2007
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IGS Electronic Report 05 Jun 23:51:42 PDT 2007 Message Number 15151
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1426 (May 06, 2007 - May 12, 2007)
Contact: Gerd Gendt (gendt at gfz-potsdam.de)
Thomas Nischan ( nisn at 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 2.1426.
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:
igl1426[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1426 in the SP3 format.
igl14267.sum Combination Report for GPS Week 1426.
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 | 872.7 ns
1 | 977.0 ns
2 | 935.7 ns
3 | 929.3 ns
4 | 962.4 ns
5 | 932.2 ns
6 | 998.8 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 | COD | R15
0 | ESX | R23
1 | COD | R15
1 | ESX | R23
2 | COD | R15
2 | ESX | R23
3 | COD | R15 R17
3 | ESX | R23
4 | COD | R15 R17
4 | ESX | R23
5 | COD | R15
5 | ESX | R23
5 | IAC | R22
6 | BKG | R15
6 | COD | R15
6 | ESX | R02 R08 R23 R24
6 | IAC | R22
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 1.1426, 1a.1426).
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 2.1426.0-6)
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 3.1426.0-6).
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 1426 summary. (May 06, 2007 - May 12, 2007)
Table 1.1426.a GPS week : 1426 MJD: 54226.0-54232.0
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 60| -3 -1 4 148 -72 27 -.12 57 42 | 0 174 5285 5599
| 5 1 11 77 54 181 .10 | 0 763
cod 168| 0 0 5 109 -23 165 -.07 51 41 | --- --- --- ---
| 2 2 14 52 68 213 .10 | --- ---
esx 46| 4 0 4 173 48 -287 -.54 426 99 | 1537882 -16245 16395 28773
| 4 12 22 193 108 292 .67 | 3937948 16436
iac n/a| -1 0 -11 -280 71 0 .26 57 57 | 946400 -4709 15506 27807
| 5 3 27 45 59 158 .12 | 35294 8541
mcc n/a| -18 4 -34 -17 -69 1638 .78 97 97 | --- --- --- ---
| 36 8 37 154 225 1593 .91 | --- ---
Table 1.1426.b GPS week : 1426 MJD: 54226.0-54232.0
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 | 30 20 32 26 60 137 104 |
R03 | 20 18 26 27 30 34 94 |
R04 | 14 17 19 18 30 46 35 |
R06 | 37 16 22 17 23 36 32 |
R07 | --- --- 0 113 121 76 60 |
R08 | 22 30 32 29 30 30 26 |
R10 | 17 16 20 27 40 108 88 |
R14 | 18 11 14 27 22 25 32 |
R18 | 25 21 23 26 19 29 128 |
R19 | 33 22 22 25 15 31 27 |
R21 | 28 22 35 18 30 34 114 |
R22 | 18 15 24 40 185 333 1075 |
R23 | 20 26 34 27 29 45 43 |
R24 | 173 178 201 72 263 196 128 |
Table 1.1426.c GPS week : 1426 MJD: 54226.0-54232.0
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 1426 0 | -11 -690 -240 2951 7155 -372500 91.8 7010 7010 | 872743 0
brd 1426 1 | -36 -129 137 6971 8298 -357200 75.8 8006 8006 | 977030 0
brd 1426 2 | -70 95 -724 -6031 1217 -346400 91.8 6170 6170 | 935661 0
brd 1426 3 | -908 322 818 425 5389 -339000 85.1 12350 12350 | 929255 0
brd 1426 4 | -445 150 -789 -13820 -11410 -299400 86.1 15720 15720 | 962388 0
brd 1426 5 | -225 -161 456 -2884 -3293 -340300 77.6 11850 11850 | 932211 0
brd 1426 6 | -933 -529 500 -5958 -7808 -328000 77.1 18590 18590 | 998809 0
-------------+------------------------------------------------------------+----------------
brd 1426 mean| -375 -134 22 -2620 -64 -340400 83.6 11385 11385 | 944013 0
brd 1426 sdev| 400 366 625 6838 7665 23041 6.9 4647 4647 | 40695 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 2.1426.0 GPS week: 1426 Day: 0 MJD: 54226
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 60| -11 -4 0 244 -85 126 -.26 50 40 | 0 496 6600 7079
cod 168| 0 2 6 140 -76 61 -.07 41 33 | --- --- --- ---
esx 46| 8 4 -5 -10 42 -58 -.11 144 62 | -999999 -36862 15870 40833
iac n/a| 0 -4 -2 -218 112 -45 .16 35 35 | 889755 -11921 16985 39037
Table 2.1426.1 GPS week: 1426 Day: 1 MJD: 54227
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 60| -4 -1 -2 72 9 -139 -.10 22 21 | 0 -51 3749 3956
cod 168| 0 0 -3 64 -65 378 -.05 45 43 | --- --- --- ---
esx 46| 2 -1 4 369 -134 47 -.23 135 59 | 21797 -15516 14159 22732
iac n/a| -3 2 0 -340 108 -38 .20 36 36 | 958565 9270 13644 23161
Table 2.1426.2 GPS week: 1426 Day: 2 MJD: 54228
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 60| -2 0 1 73 -74 -49 -.04 41 42 | 0 552 4385 4527
cod 168| 1 -2 0 184 -7 282 -.09 46 37 | --- --- --- ---
esx 46| 4 -8 1 143 29 -18 -.36 141 59 | -2590 -7443 11258 26996
iac n/a| -1 6 0 -288 59 -289 .28 41 41 | 938503 -5887 9998 27004
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1426.3 GPS week: 1426 Day: 3 MJD: 54229
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 60| -1 0 5 64 -66 64 -.14 29 28 | 0 932 6802 7154
cod 168| -2 -1 -5 24 -116 274 -.26 35 39 | --- --- --- ---
esx 46| 7 1 -8 403 146 -560 -.16 129 62 | -10773 13987 18656 32207
iac n/a| -1 0 -3 -291 65 -38 .43 43 43 | 930995 4931 16670 29616
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1426.4 GPS week: 1426 Day: 4 MJD: 54230
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 60| 0 -2 3 190 -128 -204 -.03 73 36 | 0 222 5033 5516
cod 168| 0 0 3 107 90 369 .05 64 42 | --- --- --- ---
esx 46| 5 23 12 201 209 -253 .01 163 88 | 2756741 -15805 12374 21565
iac n/a| -1 -2 -2 -329 14 161 .22 85 85 | 971295 -9606 11714 20593
mcc n/a| -16 11 -43 112 0 2103 .82 100 100 | --- --- --- ---
Table 2.1426.5 GPS week: 1426 Day: 5 MJD: 54231
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 60| 4 -2 -4 166 -21 50 .00 76 55 | 0 484 4864 5172
cod 168| 5 5 -1 137 6 -144 .02 47 46 | --- --- --- ---
esx 46| -3 -1 50 237 10 -473 -1.17 209 153 | 9999999 -23605 18444 29841
iac n/a| -10 -3 1 -236 -16 72 .10 58 58 | 934094 -6823 16891 28149
mcc n/a| 4 14 -91 -278 114 2489 .84 101 101 | --- --- --- ---
Table 2.1426.6 GPS week: 1426 Day: 6 MJD: 54232
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 60| -9 -1 29 227 -143 341 -.25 106 70 | 0 -1416 5568 5795
cod 168| 2 3 36 107 6 -65 -.09 78 45 | --- --- --- ---
esx 46| 9 -16 -21 -130 32 -695 -1.79 2060 210 | -999999 -28475 24006 27243
iac n/a| 9 -3 -72 -258 155 177 .39 99 99 | 1001596 -12931 22643 27094
mcc n/a| -83 -4 -36 80 -463 3600 2.23 284 284 | --- --- --- ---
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 3.1426.0 GPS week: 1426 Day: 0 MJD: 54226
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 9654 57 39 84 37 30 | 60 86 107 40 55
R03 |10385 25 20 58 36 20 | 38 32 92 30 27
R04 | 2547 25 16 36 24 14 | 40 48 63 42 36
R06 |11444 100 44 76 34 36 | 73 51 49 37 27
R08 | 3355 35 34 42 42 22 | 36 53 608 43 31
XR10 | 3279 26 20 --- 24 16 | 247 300 --- 287 280
XR14 | 6764 22 30 --- 22 17 | 29 36 --- 45 31
R18 | 3688 55 38 54 33 25 | 435 418 427 419 421
R19 | 5810 28 68 91 33 32 | 73 104 56 55 63
R21 | 4543 44 54 53 43 28 | 42 44 126 45 27
XR22 | 4202 37 18 --- 19 17 | 189 108 --- 959 107
R23 | 4942 35 27 391 24 20 | 57 59 104 80 59
XR24 | ---- --- 125 238 --- 173 | --- 595 521 --- 551
------+-------------------------------+---------------------------
RMS | 7009 50 41 144 35 |T 109 148 215 173 131
WRMS | 7009 40 33 62 35 |NE 109 148 215 173 131
MEDI | 4543 35 34 58 33 |MD 57 59 104 45 55
Table 3.1426.1 GPS week: 1426 Day: 1 MJD: 54227
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 7257 17 35 67 32 20 | 75 50 66 30 40
R03 | 8238 18 34 61 22 17 | 28 28 96 31 23
R04 | 7752 16 44 49 19 17 | 45 35 70 38 33
R06 |16733 23 29 31 29 15 | 35 34 45 47 22
R08 | 2659 15 86 82 40 30 | 34 69 529 34 28
XR10 | 6273 12 30 --- 27 15 | 279 337 --- 326 316
XR14 | 4285 9 18 --- 20 10 | 33 42 --- 27 33
R18 | 2676 24 41 54 40 21 | 339 347 378 333 343
R19 | 7564 16 44 70 35 21 | 60 76 74 60 55
R21 | 4982 29 31 37 53 22 | 31 39 83 52 27
XR22 | 5259 14 31 --- 21 14 | 117 123 --- 762 97
R23 | 4472 32 33 369 45 26 | 48 44 116 74 43
XR24 | ---- --- 148 212 --- 177 | --- 282 280 --- 252
------+-------------------------------+---------------------------
RMS | 8006 22 45 135 36 |T 93 115 173 151 100
WRMS | 8006 21 43 59 36 |NE 93 115 173 151 100
MEDI | 5259 16 34 61 29 |MD 45 50 83 47 40
Table 3.1426.2 GPS week: 1426 Day: 2 MJD: 54228
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2858 38 51 90 43 --- 31 | 80 78 117 38 --- 61
R03 | 9133 38 48 66 27 --- 25 | 35 49 106 43 --- 36
R04 | 4984 21 32 48 28 --- 18 | 42 39 28 42 --- 32
R06 | 7291 25 36 54 38 --- 22 | 32 53 47 45 --- 24
XR07 |11195 --- 19 --- --- --- 0 | --- 816 --- --- --- 825
R08 | 3700 45 73 73 31 --- 32 | 47 54 344 41 --- 36
XR10 | 9735 24 29 --- 29 --- 19 | 155 166 --- 176 --- 165
XR14 | 2497 20 18 --- 18 --- 13 | 34 46 --- 41 --- 33
R18 | 4380 41 35 47 33 --- 22 | 315 331 327 316 --- 322
R19 | 6018 24 53 29 38 --- 22 | 46 52 55 41 --- 28
R21 | 8321 77 18 72 58 --- 34 | 33 57 119 65 --- 47
XR22 | 3891 25 33 --- 40 --- 24 | 151 95 --- 777 --- 87
R23 | 5888 34 47 385 58 --- 34 | 35 46 106 77 --- 41
XR24 | ---- --- 166 245 --- 521 201 | --- 444 448 --- 252 436
------+------------------------------------+--------------------------------
RMS | 6169 41 46 141 41 0 |T 83 166 169 141 252 155
WRMS | 6169 42 37 59 41 0 |NE 83 166 169 141 252 155
MEDI | 5888 25 35 66 33 521 |MD 42 54 106 43 252 41
Table 3.1426.3 GPS week: 1426 Day: 3 MJD: 54229
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7843 31 38 91 24 --- 25 | 101 111 147 47 --- 80
R03 |12870 27 24 68 70 --- 27 | 38 36 125 60 --- 26
R04 |11933 16 33 47 36 --- 18 | 35 59 88 32 --- 27
R06 |10054 19 35 37 26 --- 16 | 34 46 66 42 --- 28
XR07 | ---- --- 113 --- 113 192 113 | --- 383 --- 67 10 334
R08 | 6522 43 29 85 49 --- 28 | 38 68 672 58 --- 33
XR10 |12521 34 38 --- 43 --- 27 | 327 381 --- 357 --- 358
XR14 |10531 38 16 --- 52 --- 27 | 29 41 --- 72 --- 38
R18 |15847 28 43 65 52 --- 25 | 261 268 293 265 --- 263
R19 |16847 34 44 65 38 --- 24 | 43 54 59 39 --- 31
R21 |16278 30 25 51 24 --- 18 | 33 47 105 56 --- 39
XR22 |11520 53 56 --- 59 --- 39 | 224 162 --- 948 --- 156
R23 | 7710 27 39 339 46 --- 26 | 39 54 71 69 --- 45
XR24 |12170 51 76 203 --- --- 72 | 326 436 321 --- --- 372
------+------------------------------------+--------------------------------
RMS |12349 29 35 129 43 0 |T 117 153 194 162 10 130
WRMS |12349 28 39 62 43 0 |NE 117 153 194 162 10 130
MEDI |11933 31 38 65 46 192 |MD 39 59 105 60 10 39
Table 3.1426.4 GPS week: 1426 Day: 4 MJD: 54230
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |28358 35 135 143 103 --- 60 | 131 124 170 42 --- 58
R03 | 9231 21 40 111 34 --- 29 | 27 35 126 57 --- 21
R04 | 9146 29 58 84 44 --- 30 | 34 48 109 64 --- 34
R06 |10198 29 39 59 38 --- 23 | 35 48 45 45 --- 26
R07 | ---- 213 91 315 221 100 121 | 115 217 204 65 13 258
R08 |14421 33 42 87 54 --- 30 | 25 31 649 58 --- 30
XR10 |11594 53 53 --- 65 --- 40 | 221 325 --- 322 --- 290
XR14 |12335 28 22 --- 39 --- 21 | 28 49 --- 67 --- 39
R18 |18340 27 43 31 25 --- 18 | 324 322 316 322 --- 320
R19 |12545 26 29 27 21 --- 15 | 35 54 117 61 --- 46
R21 |17378 39 57 87 34 --- 30 | 50 82 184 53 --- 41
XR22 | ---- 228 348 --- 186 --- 184 | 196 429 --- 9999 --- 156
R23 |11945 30 31 329 56 --- 28 | 62 54 95 70 --- 43
XR24 |18607 392 349 361 --- --- 262 | 188 688 634 --- --- 480
------+------------------------------------+--------------------------------
RMS |15718 73 64 163 85 100 |T 105 179 240 102 13 131
WRMS |15718 36 42 88 85 100 |NE 105 179 240 102 13 131
MEDI |12335 30 43 87 44 100 |MD 50 54 170 61 13 43
Table 3.1426.5 GPS week: 1426 Day: 5 MJD: 54231
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |12476 245 115 --- 216 --- 137 | 195 165 --- 70 --- 100
R03 |11952 25 64 129 45 --- 34 | 46 39 226 56 --- 40
R04 |11129 21 49 262 35 --- 45 | 29 33 195 74 --- 41
R06 |14754 29 51 136 63 --- 35 | 27 49 88 55 --- 21
R07 | ---- 187 49 230 109 101 75 | 78 160 218 83 9 170
R08 | 9481 24 32 160 31 --- 29 | 34 31 9999 56 --- 34
XR10 | 7080 196 157 --- 103 --- 107 | 453 587 --- 577 --- 538
XR14 |12797 27 37 --- 36 --- 24 | 32 55 --- 53 --- 40
R18 |15050 41 39 120 38 --- 28 | 328 330 320 353 --- 330
R19 | 9737 54 18 152 33 --- 30 | 55 39 97 49 --- 31
XR21 |24187 41 57 --- 42 --- 34 | 35 81 --- 41 --- 46
XR22 | ---- 403 273 --- 5229 --- 332 | 444 567 --- 9999 --- 395
R23 | 9350 70 57 363 64 --- 45 | 43 40 124 53 --- 22
XR24 |19490 413 240 --- 172 --- 195 | 289 744 --- 79 --- 650
------+------------------------------------+--------------------------------
RMS |11850 76 47 209 58 101 |T 149 208 181 123 9 175
WRMS |11850 55 46 153 58 101 |NE 149 208 181 123 9 175
MEDI |11952 41 51 152 45 101 |MD 46 55 195 56 9 41
Table 3.1426.6 GPS week: 1426 Day: 6 MJD: 54232
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |33465 272 141 252 91 --- 103 | 232 159 164 55 --- 66
R03 |15602 44 44 632 95 --- 93 | 57 30 321 70 --- 42
R04 |14249 57 30 159 59 --- 35 | 34 34 83 79 --- 40
R06 |14242 45 39 131 57 --- 32 | 45 57 129 45 --- 33
R07 | ---- 140 48 207 90 141 60 | 42 244 167 91 13 241
R08 |11655 36 28 6609 44 --- 26 | 33 22 9999 42 --- 25
XR10 | 8791 174 123 --- 66 --- 88 | 334 514 --- 449 --- 437
XR14 |14162 31 37 --- 60 --- 32 | 28 37 --- 72 --- 37
R18 |16496 74 76 893 59 --- 127 | 416 430 937 435 --- 441
R19 |10107 36 32 141 34 --- 27 | 52 38 104 49 --- 34
R21 |21184 32 66 791 78 --- 113 | 26 49 463 57 --- 24
XR22 | ---- 1287 899 --- 4847 --- 1074 | 671 673 --- 9999 --- 430
R23 | 9978 82 52 328 48 --- 43 | 81 66 93 70 --- 59
R24 |25059 85 158 941 244 376 127 | 156 645 568 108 282 580
------+------------------------------------+--------------------------------
RMS |18589 106 78 2059 99 284 |T 157 214 302 124 147 177
WRMS |18589 70 45 210 99 284 |NE 157 214 302 124 147 177
MEDI |14242 57 48 328 60 141 |MD 52 57 164 70 13 42
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