[IGSREPORT-14849] Wk 1413 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Tue Mar 6 08:10:29 PST 2007
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IGS Electronic Report 06 Mar 08:10:36 PST 2007 Message Number 14849
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1413 (Feb 04, 2007 - Feb 10, 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 2.1413.
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:
igl1413[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1413 in the SP3 format.
igl14137.sum Combination Report for GPS Week 1413.
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 | 710.5 ns
1 | 788.8 ns
2 | 729.2 ns
3 | 692.3 ns
4 | 689.3 ns
5 | 682.5 ns
6 | 687.6 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 | BKG | R01
0 | COD | R01
0 | IAC | R01
1 | COD | R01
1 | ESX | R23
4 | BKG | R22
4 | COD | R22
4 | IAC | R22
5 | COD | R22
6 | COD | 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 1.1413, 1a.1413).
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 2.1413.0-6)
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 3.1413.0-6).
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 1413 summary. (Feb 04, 2007 - Feb 10, 2007)
Table 1.1413.a GPS week : 1413 MJD: 54135.0-54141.0
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 58| 0 0 0 114 -45 -6 -.02 70 42 | 0 73082 74045 98071
| 2 2 7 39 56 193 .11 | 0 152235
cod 171| -2 1 -1 141 -75 -18 -.14 82 44 | --- --- --- ---
| 2 8 14 116 76 114 .11 | --- ---
esx 45| 3 -1 14 157 136 149 -.33 138 61 | 632980 91800 83787 188069
| 7 4 3 146 115 130 .16 | 905496 129632
iac n/a| 0 -2 -4 -279 87 -48 .22 53 53 | 580844 -132883 575486 719738
| 2 5 7 28 26 120 .13 | 1352605 604175
mcc n/a| -7 -8 64 145 376 -305 1.51 246 246 | --- --- --- ---
| 26 43 86 553 870 2300 2.02 | --- ---
Table 1.1413.b GPS week : 1413 MJD: 54135.0-54141.0
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 | ---- 224 93 73 32 21 18 |
R02E | 17 25 21 20 17 19 19 |
R03E | 30 59 110 148 65 45 120 |
R04E | 26 24 25 21 21 17 18 |
R06E | 16 22 31 24 29 28 19 |
R07E | 0 257 262 147 45 19 16 |
R08E | 22 23 18 22 25 28 19 |
R14 | ---- ---- ---- 179 52 112 148 |
R18 | 24 25 39 28 26 20 20 |
R19 | 19 25 24 22 22 24 15 |
R21 | 41 47 38 28 31 46 46 |
R22 | 24 16 36 93 ---- ---- ---- |
R23 | 56 35 36 59 57 48 56 |
R24 | 109 114 51 94 58 71 75 |
Table 1.1413.c GPS week : 1413 MJD: 54135.0-54141.0
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 1413 0 | 0 0 0 -3 -16 -370 88.69 8 8 | 710536 0 0 0
brd 1413 1 | 0 0 0 -13 -8 -369 59.13 10 10 | 788793 0 0 0
brd 1413 2 | 0 0 -1 -10 -21 -361 91.39 14 14 | 729178 0 0 0
brd 1413 3 | 0 0 -1 -11 -18 -358121.90 11 11 | 692263 0 0 0
brd 1413 4 | 0 0 -1 -14 -24 -390108.00 11 11 | 689273 0 0 0
brd 1413 5 | 0 0 -1 -6 -3 -383 99.31 10 10 | 682521 0 0 0
brd 1413 6 | 0 0 -1 -12 -10 -376 92.55 7 7 | 687596 0 0 0
-------------+----------------------------------------------------+------------------------------
brd 1413 mean| 0 0 0 -10 -14 -372 94.42 10 10 | 711451 0 0 0
brd 1413 sdev| 0 0 0 3 7 11 19.38 2 2 | 37777 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 2.1413.0 GPS week: 1413 Day: 0 MJD: 54135
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 58| -3 4 8 174 -6 19 -.07 78 33 | 0 108182 118612 154708
cod 171| -3 -2 -11 39 -136 66 -.01 62 35 | --- --- --- ---
esx 45| 8 -5 12 340 178 175 -.16 153 65 | 38265 176126 177155 312766
iac n/a| -4 -1 1 -298 56 -135 .06 47 47 | 705989 179061 174588 309498
mcc n/a| 9 -8 159 -709 -715 233 -.66 185 185 | --- --- --- ---
Table 2.1413.1 GPS week: 1413 Day: 1 MJD: 54136
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 58| 0 2 1 123 -92 -168 -.08 87 38 | 0 405876 381105 512287
cod 171| -1 -5 7 135 -40 3 -.09 68 48 | --- --- --- ---
esx 45| -3 -1 17 252 214 307 -.37 147 59 | 164874 319530 286247 741709
iac n/a| 3 -4 -12 -259 74 -69 .33 50 50 | 836058 306124 293001 712551
mcc n/a| -37 -69 137 646 880 -3467 2.67 423 423 | --- --- --- ---
Table 2.1413.2 GPS week: 1413 Day: 2 MJD: 54137
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 58| 2 0 -4 73 16 -13 .06 90 65 | 0 -712 3411 3482
cod 171| -3 12 1 264 32 103 -.11 211 60 | --- --- --- ---
iac n/a| 3 -1 7 -320 80 -45 .02 86 86 | 845612 388575 548584 999999
mcc n/a| 22 -17 -42 171 159 2867 1.22 244 244 | --- --- --- ---
Table 2.1413.3 GPS week: 1413 Day: 3 MJD: 54138
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 58| 0 -1 -11 151 -29 92 .14 82 41 | 0 680 3249 3463
cod 171| 0 -1 18 167 -127 -126 -.24 75 45 | --- --- --- ---
esx 45| -6 5 10 -10 -18 180 -.18 133 54 | 1718522 21963 10372 20136
iac n/a| -2 0 -13 -271 122 -86 .25 59 59 | 2992744 192347 999999 999999
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1413.4 GPS week: 1413 Day: 4 MJD: 54139
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 58| 2 -4 -6 92 -140 205 .00 56 42 | 0 -376 3815 4070
cod 171| -5 10 8 89 13 -159 -.10 40 35 | --- --- --- ---
esx 45| 0 2 20 152 6 -66 -.61 126 63 | 1876600 31186 12542 16705
iac n/a| 0 -13 -12 -262 73 -12 .29 52 52 | 685503 3705 12238 16125
Table 2.1413.5 GPS week: 1413 Day: 5 MJD: 54140
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 58| 0 0 4 68 -65 -343 -.19 50 38 | 0 -1369 4017 4149
cod 171| -2 6 -16 310 -120 101 -.07 61 46 | --- --- --- ---
esx 45| 10 -2 13 -20 172 76 -.37 137 76 | 2676 -1310 7717 15040
iac n/a| 0 0 0 -302 77 191 .24 33 33 | -999999 -999999 999999 999999
Table 2.1413.6 GPS week: 1413 Day: 6 MJD: 54141
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 58| -2 2 6 119 -3 165 .03 43 38 | 0 -703 4108 4340
cod 171| 0 -8 -18 -15 -151 -118 -.33 59 38 | --- --- --- ---
esx 45| 7 -5 13 230 266 227 -.31 134 50 | -3054 3309 8692 22061
iac n/a| 0 5 -3 -240 128 -182 .38 44 44 | -999999 -999999 999999 999999
mcc n/a| -32 52 66 619 1557 -1159 4.33 377 377 | --- --- --- ---
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 3.1413.0 GPS week: 1413 Day: 0 MJD: 54135
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 4676 28 28 31 32 --- 17 | 40 35 75 37 --- 26
XR03E |37655 38 38 --- 51 --- 30 | 67 100 --- 98 --- 77
R04E | 6971 41 32 68 48 --- 25 | 54 43 87 53 --- 44
R06E |17238 20 24 45 30 --- 16 | 112 135 161 125 --- 124
XR07E | ---- --- 11 --- --- --- 0 | --- 573 --- --- --- 478
R08E | 8612 25 39 40 46 --- 22 | 71 56 483 54 --- 55
R18 | 7028 24 38 77 41 --- 24 | 456 449 503 459 --- 458
R19 | 4628 27 39 26 32 --- 19 | 34 39 220 42 --- 29
R21 | 6563 24 40 175 65 --- 41 | 56 70 9999 61 --- 53
R22 | 5660 34 30 97 22 185 24 | 391 9999 277 143 79 79
R23 | 3364 37 36 265 72 --- 56 | 50 58 138 51 --- 49
R24 | 6860 232 169 327 53 --- 108 | 292 566 554 460 --- 445
------+------------------------------------+--------------------------------
RMS | 8038 78 62 153 47 185 |T 147 217 277 160 79 159
WRMS | 8038 33 35 65 47 185 |NE 213 236 338 202 79 185
MEDI | 6860 28 36 68 46 185 |MD 67 70 220 61 79 55
Table 3.1413.1 GPS week: 1413 Day: 1 MJD: 54136
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01E | ---- 251 618 --- 199 --- 223 | 359 453 --- 214 --- 172
R02E |14299 34 45 46 47 --- 25 | 32 39 133 44 --- 27
XR03E |48119 66 68 --- 104 --- 58 | 69 96 --- 138 --- 81
R04E | 7552 23 49 32 47 --- 23 | 42 59 78 27 --- 33
R06E | 9607 19 25 66 43 --- 22 | 46 54 302 66 --- 53
XR07E | ---- --- 272 --- 242 321 257 | --- 329 --- 147 47 299
R08E |10386 29 53 35 31 --- 22 | 34 69 660 47 --- 37
R18 |12431 35 34 79 29 --- 24 | 364 361 491 367 --- 361
R19 | 6827 43 33 73 30 --- 24 | 50 33 425 37 --- 27
R21 |12153 35 64 140 86 --- 47 | 57 104 9999 45 --- 58
R22 | 7929 16 28 44 24 292 16 | 400 9999 371 142 105 73
R23 | 6883 49 55 293 44 --- 35 | 36 77 183 42 --- 33
R24 | 8952 258 167 296 78 521 114 | 347 445 466 350 208 367
------+------------------------------------+--------------------------------
RMS |10004 87 68 147 50 423 |T 153 176 345 128 120 124
WRMS |10004 38 48 59 50 423 |NE 209 204 387 163 156 153
MEDI | 9607 35 53 66 47 321 |MD 50 77 371 66 105 58
Table 3.1413.2 GPS week: 1413 Day: 2 MJD: 54137
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod iac mcc IGL | bkg cod iac mcc IGL
------+-------------------------------+---------------------------
R01E |24990 83 187 139 --- 93 | 716 210 174 --- 154
R02E | 8632 21 38 31 --- 20 | 36 54 38 --- 32
R03 |37599 88 265 131 --- 110 | 84 339 164 --- 114
R04E | 6187 28 39 41 --- 25 | 35 43 47 --- 36
R06E | 4900 33 38 54 --- 30 | 80 88 83 --- 79
R07E |14971 281 655 203 --- 262 | 83 475 215 --- 213
R08E |12690 15 34 28 --- 18 | 47 60 44 --- 40
R18 | 9071 46 95 28 --- 39 | 367 359 376 --- 367
R19 | 4167 26 50 28 --- 23 | 44 78 44 --- 43
R21 |13285 31 75 58 --- 37 | 33 112 61 --- 42
R22 | 2664 51 50 48 244 35 | 245 9999 137 111 60
R23 | 2900 34 86 37 --- 35 | 39 79 35 --- 40
R24 | 5181 51 119 57 --- 51 | 650 580 617 --- 610
------+-------------------------------+---------------------------
RMS |14881 90 211 86 244 |T 189 206 156 111 140
WRMS |14881 65 60 86 244 |NE 208 257 204 111 182
MEDI | 8632 34 75 48 244 |MD 80 88 83 111 60
Table 3.1413.3 GPS week: 1413 Day: 3 MJD: 54138
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |19130 154 110 112 119 --- 72 | 422 221 9999 230 --- 190
R02E |10635 28 34 36 36 --- 19 | 39 54 131 57 --- 46
XR03 |25807 219 180 --- 224 --- 148 | 193 296 --- 275 --- 178
R04E |10433 41 29 45 31 --- 20 | 55 52 66 50 --- 48
R06E | 8084 24 49 29 45 --- 23 | 91 131 135 109 --- 105
XR07E | 9062 190 126 --- 266 --- 146 | 68 262 --- 347 --- 236
R08E |13645 28 40 65 26 --- 22 | 43 53 490 42 --- 39
XR14 | ---- 191 168 --- --- --- 179 | 97 137 --- --- --- 71
R18 |12606 48 37 96 22 --- 28 | 341 332 358 335 --- 333
R19 | 6357 45 36 56 15 --- 21 | 67 61 463 34 --- 41
XR21 |12005 34 39 --- 43 --- 28 | 39 51 --- 54 --- 31
XR22 | 2313 127 171 --- 85 613 92 | 566 9999 --- 272 94 209
R23 | 2367 45 49 243 55 --- 58 | 47 42 153 49 --- 37
R24 | 6958 164 166 257 92 --- 93 | 227 506 374 288 --- 342
------+------------------------------------+--------------------------------
RMS |11019 82 75 133 59 0 |T 163 169 271 164 94 136
WRMS |11019 41 45 54 59 0 |NE 197 203 337 186 94 155
MEDI |10433 45 49 65 45 613 |MD 68 131 153 109 94 71
Table 3.1413.4 GPS week: 1413 Day: 4 MJD: 54139
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 |13939 52 39 97 55 32 | 260 121 9999 144 91
R02E |12086 25 30 26 34 17 | 55 76 71 55 56
XR03 |17592 90 80 --- 108 65 | 112 176 --- 117 125
R04E |15208 24 34 62 37 21 | 50 56 98 63 52
R06E |19613 59 36 68 43 28 | 87 156 152 138 126
R07 | 5175 94 55 100 77 45 | 75 216 36 153 124
R08 |11271 44 33 74 34 25 | 55 77 244 52 56
XR14 | ---- 60 45 --- --- 52 | 110 105 --- --- 101
R18 | 7665 42 44 45 48 26 | 383 356 304 362 362
R19 | 7401 31 29 53 47 22 | 37 52 304 49 32
XR21 | 4593 37 39 --- 53 30 | 29 78 --- 58 31
R23 | 2787 40 25 271 65 57 | 63 48 130 38 54
R24 | 6070 97 63 218 58 58 | 698 755 720 748 729
------+-------------------------------+---------------------------
RMS |11262 56 40 126 52 |T 187 174 228 192 149
WRMS |11262 42 35 63 52 |NE 221 198 289 224 170
MEDI | 7665 44 39 68 48 |MD 75 105 152 117 91
Table 3.1413.5 GPS week: 1413 Day: 5 MJD: 54140
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R01 | 9177 27 48 33 35 21 | 211 68 708 101 71
R02 |12037 22 41 43 29 18 | 53 61 92 55 52
XR03 |19933 48 75 --- 64 44 | 94 146 --- 114 96
R04 |10498 26 26 66 21 17 | 62 73 105 58 57
R06 |21458 51 48 81 36 28 | 96 141 136 133 114
R07 | 3428 32 20 80 14 18 | 49 148 38 59 84
R08 | 6987 61 38 71 32 27 | 57 67 195 52 44
XR14 | ---- 112 112 --- --- 112 | 141 155 --- --- 121
R18 |12149 23 25 83 28 19 | 389 369 351 378 380
R19 | 9804 23 31 86 44 24 | 53 51 205 79 51
R21 | 4032 46 112 156 38 46 | 42 136 9999 45 41
R23 | 3025 32 23 268 39 48 | 41 73 88 61 53
R24 | 2988 121 133 265 38 71 | 338 521 497 437 429
------+-------------------------------+---------------------------
RMS |10173 50 61 137 33 |T 125 154 241 131 122
WRMS |10173 38 46 76 33 |NE 125 154 241 131 122
MEDI | 9177 32 41 81 35 |MD 62 136 136 61 71
Table 3.1413.6 GPS week: 1413 Day: 6 MJD: 54141
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7407 26 28 31 38 --- 18 | 367 83 9999 128 --- 71
R02 | 9493 27 28 51 33 --- 18 | 51 71 90 73 --- 61
XR03 |44027 108 250 --- 138 --- 120 | 41 268 --- 101 --- 82
R04 | 8268 21 37 54 27 --- 18 | 54 65 61 51 --- 49
R06 | 9025 25 36 54 27 --- 18 | 88 90 100 83 --- 86
XR07 | 4188 16 23 --- 29 191 16 | 45 138 --- 78 26 96
R08 | 4701 14 27 69 33 --- 18 | 58 68 150 70 --- 60
XR14 | ---- 127 171 --- --- --- 147 | 112 250 --- --- --- 172
R18 |11636 23 42 45 33 --- 19 | 460 441 425 460 --- 456
R19 | 9870 16 31 28 29 --- 15 | 52 38 165 52 --- 42
R21 | 5256 52 123 86 42 --- 45 | 42 146 9999 34 --- 48
R23 | 2188 26 45 276 65 --- 56 | 58 65 106 69 --- 60
R24 | 3509 109 99 284 79 377 74 | 394 480 439 412 155 422
------+------------------------------------+--------------------------------
RMS | 7710 43 59 134 44 377 |T 140 169 192 134 90 131
WRMS | 7710 38 38 50 44 377 |NE 140 169 192 134 90 131
MEDI | 7407 26 37 54 33 191 |MD 58 90 106 73 26 71
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