[IGSREPORT-14744] Wk 1410 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Feb 2 06:17:41 PST 2007
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IGS Electronic Report 02 Feb 06:17:56 PST 2007 Message Number 14744
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1410 (Jan 14, 2007 - Jan 20, 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 2.1410.
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:
igl1410[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1410 in the SP3 format.
igl14107.sum Combination Report for GPS Week 1410.
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 | 577.3 ns
1 | 600.7 ns
2 | 543.7 ns
3 | 594.2 ns
4 | 583.8 ns
5 | 610.3 ns
6 | 583.1 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 | R22
0 | ESX | R23 R24
1 | COD | R22
1 | ESX | R23 R24
2 | ESX | R23 R24
3 | BKG | R01
3 | ESX | R23 R24
4 | ESX | R23 R24
5 | ESX | R23 R24
6 | ESX | R23 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 1.1410, 1a.1410).
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 2.1410.0-6)
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 3.1410.0-6).
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 1410 summary. (Jan 14, 2007 - Jan 20, 2007)
Table 1.1410.a GPS week : 1410 MJD: 54114.0-54120.0
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 -1 84 -9 13 -.00 60 49 | 0 78 3203 3555
| 4 4 11 68 58 128 .19 | 0 252
cod 176| 0 0 7 110 -26 -63 -.21 64 46 | --- --- --- ---
| 7 6 8 95 92 116 .12 | --- ---
esx 44| -2 4 -3 205 -28 39 -.29 194 79 | 2688358 -144457 292013 295661
| 4 6 9 176 137 201 .40 | 4876785 377341
iac n/a| -1 -6 -5 -280 21 59 .53 74 74 | 1936412 -142008 150523 156008
| 5 6 13 51 187 109 .20 | 3555732 378381
mcc n/a| -9 -9 78 -282 157 398 1.06 116 116 | --- --- --- ---
| 13 27 14 235 109 879 1.09 | --- ---
Table 1.1410.b GPS week : 1410 MJD: 54114.0-54120.0
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 | 23 19 104 84 65 0 0 |
R02E | 23 20 20 22 24 33 27 |
R04E | 21 18 23 33 31 54 34 |
R06E | 127 278 331 246 106 33 31 |
R07E | 40 43 29 23 24 42 40 |
R08E | 26 23 19 39 36 48 22 |
R18 | 35 40 42 35 45 48 103 |
R19 | 18 23 26 24 48 72 22 |
R21 | 21 26 57 33 40 70 20 |
R22 | 0 424 61 40 41 100 278 |
R23 | 22 18 20 21 22 44 27 |
R24 | 29 36 86 63 44 86 32 |
Table 1.1410.c GPS week : 1410 MJD: 54114.0-54120.0
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 SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
-------------+----------------------------------------------------+------------------------------
brd 1410 0 | 0 0 -1 -1 3 -379 88.41 8 8 | 577349 0 0 0
brd 1410 1 | 0 0 0 -3 4 -395 81.79 9 9 | 600685 0 0 0
brd 1410 2 | 0 0 0 -2 6 -389 80.16 9 9 | 543695 0 0 0
brd 1410 3 | 0 0 0 -5 -2 -384 86.31 6 6 | 594220 0 0 0
brd 1410 4 | 0 0 -1 -5 8 -394 82.74 8 8 | 583774 0 0 0
brd 1410 5 | 0 0 0 -4 -12 -387 93.28 8 8 | 610291 0 0 0
brd 1410 6 | -1 0 0 -5 -14 -362 98.44 8 8 | 583071 0 0 0
-------------+----------------------------------------------------+------------------------------
brd 1410 mean| 0 0 0 -4 0 -384 87.30 8 8 | 584726 0 0 0
brd 1410 sdev| 0 0 0 1 9 11 6.64 1 1 | 21369 0 0 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 2.1410.0 GPS week: 1410 Day: 0 MJD: 54114
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| -6 -3 1 114 55 -136 -.02 33 35 | 0 -24 3055 3459
cod 176| 0 6 11 111 -80 -7 -.15 38 40 | --- --- --- ---
esx 44| -6 0 -12 -72 -244 49 -.09 164 68 | -3700 -7005 7899 13077
iac n/a| 6 -5 -16 -316 161 114 .68 45 45 | 579257 -4129 7995 13563
mcc n/a| -6 16 64 -323 179 -109 .33 71 71 | --- --- --- ---
Table 2.1410.1 GPS week: 1410 Day: 1 MJD: 54115
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 3 6 -12 -51 4 .00 33 30 | 0 35 2427 2814
cod 176| 0 2 4 99 -55 19 -.16 41 39 | --- --- --- ---
esx 44| -9 -3 4 417 -38 -106 -.36 195 65 | 435167 7331 8721 14013
iac n/a| 1 -6 -20 -285 53 96 .62 48 48 | 597896 552 8518 14351
mcc n/a| -18 17 58 -280 141 295 -.17 96 96 | --- --- --- ---
Table 2.1410.2 GPS week: 1410 Day: 2 MJD: 54116
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 -1 5 134 -32 100 -.05 67 49 | 0 519 4205 4399
cod 176| 0 8 7 31 -55 -83 -.11 76 34 | --- --- --- ---
esx 44| -1 0 7 173 62 -179 -.49 196 64 | 9999999 -999999 999999 999999
iac n/a| -4 0 -6 -227 91 250 .42 88 88 | 9999999 -999999 999999 999999
mcc n/a| -28 1 88 -569 31 578 1.14 134 134 | --- --- --- ---
Table 2.1410.3 GPS week: 1410 Day: 3 MJD: 54117
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 -6 126 -72 130 .32 65 45 | 0 -73 3642 3848
cod 176| -6 -2 9 78 108 -63 -.12 53 35 | --- --- --- ---
esx 44| 1 6 4 430 -34 273 -.72 187 89 | 9593956 -11478 9681 15671
iac n/a| 0 -1 -5 -269 23 44 .18 38 38 | 588553 1398 9523 16632
mcc n/a| -17 -37 102 137 231 -1168 3.06 213 213 | --- --- --- ---
Table 2.1410.4 GPS week: 1410 Day: 4 MJD: 54118
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| 4 1 -1 78 57 10 -.07 39 30 | 0 -80 3102 3467
cod 176| -9 -3 4 -15 -171 -4 -.38 61 48 | --- --- --- ---
esx 44| -2 13 -13 203 -74 62 .33 202 106 | -999999 -2038 999999 999999
iac n/a| 1 -3 14 -262 195 -92 .66 102 102 | 582193 12259 9770 19986
mcc n/a| 12 -12 84 -369 335 458 1.35 106 106 | --- --- --- ---
Table 2.1410.5 GPS week: 1410 Day: 5 MJD: 54119
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 -3 8 -6 -62 -171 .10 72 65 | 0 340 2717 3364
cod 176| 14 -9 20 260 43 -313 -.38 90 85 | --- --- --- ---
esx 44| 0 10 -12 92 203 326 .05 212 99 | -234579 9872 8757 15358
iac n/a| -8 -21 -14 -372 -370 -25 .73 160 160 | 619677 1314 8685 15626
mcc n/a| -5 -55 78 -106 24 1343 1.54 88 88 | --- --- --- ---
Table 2.1410.6 GPS week: 1410 Day: 6 MJD: 54120
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| 7 7 -24 156 42 155 -.30 110 88 | 0 -166 3277 3540
cod 176| 4 -3 -7 204 24 6 -.19 92 38 | --- --- --- ---
esx 44| 3 3 -2 190 -76 -152 -.75 204 63 | 27666 -7887 9040 11516
iac n/a| -6 -4 10 -228 -3 27 .40 39 39 | 587313 -5452 9174 11903
mcc n/a| -2 0 72 -465 156 1392 .14 102 102 | --- --- --- ---
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 3.1410.0 GPS week: 1410 Day: 0 MJD: 54114
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |14314 28 34 68 36 --- 22 | 48 159 81 57 --- 104
R02E | 9945 42 40 43 30 --- 22 | 46 30 44 50 --- 27
R04E | 7076 36 45 30 29 --- 21 | 96 85 80 63 --- 76
XR06E | ---- --- 178 212 161 --- 126 | --- 227 60 351 --- 258
R07E | 8314 43 55 118 76 71 39 | 32 52 81 56 25 32
R08E |13649 37 53 51 39 --- 25 | 42 43 43 46 --- 34
R18 | 2988 22 37 133 56 --- 34 | 85 99 162 90 --- 85
R19 | 4371 22 17 58 36 --- 18 | 84 92 121 71 --- 87
R21 | 3680 24 22 78 32 --- 21 | 230 217 191 211 --- 215
XR22 |16084 --- >>>> --- 27 --- 0 | --- 9999 --- 446 --- 469
R23 | 3114 22 28 326 42 --- 22 | 41 62 284 61 --- 48
R24 | 8146 43 30 332 48 --- 29 | 308 287 489 310 --- 298
------+------------------------------------+--------------------------------
RMS | 8526 33 38 164 45 71 |T 101 123 148 151 25 144
WRMS | 8526 35 40 68 45 71 |NE 149 151 249 198 --- 200
MEDI | 8146 28 37 78 36 71 |MD 48 92 81 63 25 85
Table 3.1410.1 GPS week: 1410 Day: 1 MJD: 54115
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |14787 27 38 27 39 --- 19 | 42 120 92 47 --- 102
R02E | 9861 17 40 74 17 --- 20 | 26 49 59 43 --- 34
R04E | 6907 32 37 28 26 --- 18 | 29 57 56 62 --- 38
XR06E | ---- --- 287 --- 268 --- 278 | --- 365 --- 281 --- 207
R07E | 4534 43 33 123 103 96 42 | 35 40 33 79 24 33
R08E |11361 30 42 31 50 --- 22 | 32 41 49 37 --- 26
R18 | 3405 45 51 155 49 --- 40 | 52 73 141 85 --- 63
R19 | 6041 27 33 64 45 --- 22 | 90 102 146 76 --- 96
R21 | 3307 22 39 98 32 --- 25 | 192 210 191 181 --- 188
XR22 | 7785 207 >>>> --- 621 --- 424 | 281 9999 --- 467 --- 296
R23 | 3547 24 19 439 31 --- 18 | 41 24 255 32 --- 27
R24 |15638 48 65 354 34 --- 35 | 135 180 262 128 --- 137
------+------------------------------------+--------------------------------
RMS | 9107 33 41 195 48 96 |T 86 114 128 126 24 103
WRMS | 9107 30 39 65 48 96 |NE 131 117 199 161 --- 134
MEDI | 6907 30 39 74 39 96 |MD 42 73 92 76 24 63
Table 3.1410.2 GPS week: 1410 Day: 2 MJD: 54116
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |21999 120 170 174 243 --- 104 | 84 264 137 94 --- 198
R02E | 8830 33 25 36 45 --- 20 | 44 38 45 41 --- 32
R04E | 5312 36 40 48 37 --- 23 | 84 84 82 117 --- 89
XR06E | ---- --- 295 --- 369 --- 330 | --- 506 --- 418 --- 387
R07E | 3742 49 33 47 67 134 28 | 34 57 55 60 56 40
R08E | 9523 26 27 49 35 --- 19 | 49 46 73 25 --- 28
R18 | 2567 43 34 168 30 --- 41 | 34 69 151 50 --- 62
R19 | 4289 30 27 63 59 --- 25 | 56 46 91 72 --- 50
R21 | 3713 64 42 230 29 --- 56 | 231 238 243 207 --- 219
XR22 | 9566 90 104 --- 46 254 60 | 94 9999 --- 169 175 123
R23 | 5462 27 27 313 31 --- 20 | 31 56 159 63 --- 45
R24 |10777 132 144 405 60 --- 85 | 174 222 355 167 --- 155
------+------------------------------------+--------------------------------
RMS | 9378 67 76 196 88 134 |T 83 147 139 123 115 119
WRMS | 9378 49 34 64 88 134 |NE 103 126 199 121 175 109
MEDI | 5462 43 34 63 45 134 |MD 56 69 91 72 56 62
Table 3.1410.3 GPS week: 1410 Day: 3 MJD: 54117
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01E |23056 436 92 --- 76 --- 84 | 74 294 --- 72 --- 149
R02E | 4724 45 32 36 40 --- 22 | 38 62 70 42 --- 40
R04E | 7627 86 44 31 55 --- 33 | 104 152 106 155 --- 135
XR06E | ---- --- 266 --- 226 --- 245 | --- 215 --- 387 --- 259
R07E | 5425 30 23 74 33 148 22 | 39 36 68 54 67 35
R08E |10257 78 47 119 39 --- 38 | 67 51 115 33 --- 43
R18 | 5342 45 43 135 19 --- 35 | 50 63 119 83 --- 60
R19 | 3632 55 29 54 36 --- 24 | 100 115 170 75 --- 108
R21 | 3937 56 34 117 34 --- 33 | 267 262 240 233 --- 250
R22 | 2352 86 71 103 27 263 40 | 130 9999 15 141 209 98
R23 | 5562 39 34 340 17 --- 21 | 66 89 277 70 --- 73
R24 | 7331 91 112 407 58 --- 62 | 216 293 453 190 --- 222
------+------------------------------------+--------------------------------
RMS | 6021 65 53 187 38 213 |T 104 148 163 127 138 122
WRMS | 6021 45 35 89 38 213 |NE 138 164 212 132 209 135
MEDI | 5425 56 43 103 36 148 |MD 74 115 115 75 67 98
Table 3.1410.4 GPS week: 1410 Day: 4 MJD: 54118
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |11209 69 105 149 176 --- 64 | 81 257 182 55 --- 294
R02E | 5164 25 38 58 63 --- 23 | 46 63 71 53 --- 44
R04E |10157 40 51 91 57 --- 31 | 46 106 59 89 --- 67
XR06E |14401 --- 108 135 213 --- 106 | --- 112 138 243 --- 136
R07E | 7478 19 40 77 50 105 23 | 45 58 54 72 31 43
R08E | 9394 32 73 120 41 --- 36 | 44 40 57 48 --- 34
R18 | 7604 30 46 177 101 --- 45 | 92 90 206 143 --- 96
R19 | 3366 32 53 79 179 --- 47 | 57 84 87 207 --- 64
R21 | 6282 40 56 77 128 --- 40 | 232 236 194 251 --- 218
XR22 | 2983 41 70 --- 70 361 40 | 95 9999 --- 81 132 91
R23 | 3395 19 29 334 52 --- 21 | 33 42 209 63 --- 35
R24 |13115 53 83 445 35 --- 44 | 291 293 516 301 --- 289
------+------------------------------------+--------------------------------
RMS | 8317 39 61 202 102 105 |T 96 125 161 133 81 117
WRMS | 8317 30 48 106 102 105 |NE 133 149 242 174 132 132
MEDI | 7478 32 53 120 63 105 |MD 57 90 138 81 31 67
Table 3.1410.5 GPS week: 1410 Day: 5 MJD: 54119
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01E |22801 --- --- 24 --- --- 0 | --- --- 146 --- --- 648
R02E | 7224 49 74 35 75 --- 33 | 61 87 54 59 --- 49
R04E |10742 122 74 73 72 --- 53 | 75 76 96 55 --- 66
XR06E |14515 --- 40 47 55 --- 33 | --- 101 75 179 --- 105
R07E |10082 81 48 77 74 88 41 | 35 35 42 51 23 23
R08E |12503 66 106 80 82 --- 48 | 68 65 95 39 --- 63
R18 | 6962 42 62 93 151 --- 48 | 92 124 159 177 --- 117
R19 | 3180 22 107 68 295 --- 72 | 138 126 168 293 --- 128
R21 | 7135 31 91 80 285 --- 70 | 312 352 312 361 --- 308
XR22 | 6096 99 78 --- 269 583 99 | 132 9999 --- 217 226 124
R23 | 4593 44 61 322 98 --- 44 | 42 46 175 77 --- 27
R24 |11604 115 143 512 86 --- 85 | 238 286 402 241 --- 232
------+------------------------------------+--------------------------------
RMS | 8761 72 90 212 160 88 |T 119 129 156 159 124 157
WRMS | 8761 65 85 99 160 88 |NE 159 186 243 227 226 156
MEDI | 7224 49 74 77 86 88 |MD 75 87 146 177 23 105
Table 3.1410.6 GPS week: 1410 Day: 6 MJD: 54120
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01E | ---- --- 14 --- --- --- 0 | --- 362 --- --- --- 819
R02E | 7030 96 36 44 24 --- 26 | 64 47 53 49 --- 42
R04E | 7035 127 34 47 39 --- 34 | 82 75 47 75 --- 72
XR06E | 9824 --- 44 60 31 --- 30 | --- 89 66 109 --- 66
R07E |11706 136 39 66 52 102 40 | 40 50 48 90 33 53
R08E |15872 60 38 46 21 --- 21 | 57 51 62 47 --- 40
R18 |10845 224 255 210 68 --- 103 | 141 353 260 162 --- 227
R19 | 2270 43 35 56 27 --- 22 | 91 85 78 84 --- 74
R21 | 5425 53 26 47 25 --- 20 | 284 284 263 287 --- 280
XR22 |11423 --- 394 --- 196 307 277 | --- 9999 --- 200 127 146
R23 | 4123 59 37 347 29 --- 26 | 34 36 285 62 --- 39
R24 | 7852 60 50 440 36 --- 32 | 389 392 565 361 --- 373
------+------------------------------------+--------------------------------
RMS | 8936 110 92 204 39 102 |T 131 165 172 138 80 185
WRMS | 8936 88 38 63 39 102 |NE 187 230 290 192 127 189
MEDI | 7852 60 37 56 31 102 |MD 82 85 66 90 33 72
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