[IGSREPORT-15843] Wk 1458 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Sat Jan 12 05:49:27 PST 2008
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IGS Electronic Report 12 Jan 05:49:30 PST 2008 Message Number 15843
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1458 (Dec 16, 2007 - Dec 22, 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 2.1458.
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:
igl1458[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1458 in the SP3 format.
igl14587.sum Combination Report for GPS Week 1458.
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 | 1489.1 ns
1 | 1428.3 ns
2 | 1479.6 ns
3 | 1419.9 ns
4 | 1470.3 ns
5 | 1469.8 ns
6 | 1444.2 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 | ALL | R24
0 | BKG | R14 R21
0 | ESX | R19 R20 R20 R23
0 | IAC | R10
1 | ALL | R24
1 | BKG | R14 R15 R21
1 | ESX | R19 R20 R20 R23
1 | IAC | R10
2 | ALL | R24
2 | BKG | R15 R21
2 | ESX | R19 R20 R20 R23
2 | IAC | R10
3 | ALL | R24
3 | BKG | R14 R21
3 | ESX | R19 R20 R20 R23
4 | ALL | R24
4 | BKG | R21
4 | ESX | R19 R20 R20 R23
4 | IAC | R15
5 | ALL | R24
5 | ESX | R19 R20 R20 R23
6 | ALL | R24
6 | ESX | R19 R20 R20 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 1.1458, 1a.1458).
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 2.1458.0-6)
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 3.1458.0-6).
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 1458 summary. (Dec 16, 2007 - Dec 22, 2007)
Table 1.1458.a GPS week : 1458 MJD: 54450.0-54456.0
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 2 0 -68 -2 -18 .03 39 34 | 0 26 2711 2874
| 7 3 7 89 88 117 .13 | 0 100
cod 177| -6 -3 0 -15 -97 -37 -.05 43 35 | --- --- --- ---
| 4 8 9 47 86 97 .16 | --- ---
esx 50| 4 0 -3 161 123 -45 -.28 266 67 | 62415 8012 9466 20062
| 5 8 10 145 119 151 .18 | 171646 7179
iac n/a| 5 5 -1 -38 16 113 .26 45 45 | 1455400 1633 8442 17419
| 4 15 5 68 131 131 .18 | 26272 4849
mcc n/a| 15 2 -2 534 -673 -6358 -3.38 436 436 | --- --- --- ---
| 53 165 178 1728 1026 6508 4.40 | --- ---
Table 1.1458.b GPS week : 1458 MJD: 54450.0-54456.0
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 | 19 20 35 26 23 24 25 |
R04 | 27 22 25 21 21 26 25 |
R06 | 26 26 16 21 18 23 32 |
R07E | 13 15 17 14 14 20 31 |
R08E | 23 25 26 24 27 24 35 |
R10E | 101 107 63 93 44 57 55 |
R14E | 121 48 85 105 42 19 23 |
R15E | 93 45 80 77 42 36 37 |
R17 | 73 46 69 36 29 71 56 |
R19 | 17 25 23 21 21 22 28 |
R20 | 26 17 21 21 16 26 23 |
R21 | 29 66 44 34 41 --- --- |
R23 | 31 26 40 49 38 47 76 |
Table 1.1458.c GPS week : 1458 MJD: 54450.0-54456.0
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 1458 0 | 49 -268 -99 3134 101 -51250 102.3 6273 6273 | 1489053 0
brd 1458 1 | 95 -118 80 397 -1521 -48910 91.3 5402 5402 | 1428268 0
brd 1458 2 | 2 -41 76 -952 -6128 -44300 98.5 7885 7885 | 1479582 0
brd 1458 3 | -746 -240 87 -2176 -7068 -31290 120.2 8264 8264 | 1419909 0
brd 1458 4 | 383 -471 195 5579 -9162 -43150 101.5 8055 8055 | 1470323 0
brd 1458 5 | 114 -152 729 -3667 -5196 -30070 102.5 8889 8889 | 1469842 0
brd 1458 6 | -446 -267 677 5742 -213 -40880 99.0 8691 8691 | 1444159 0
-------------+------------------------------------------------------------+----------------
brd 1458 mean| -78 -222 249 1151 -4169 -41407 102.2 7637 7637 | 1457305 0
brd 1458 sdev| 384 138 322 3739 3631 8121 8.8 1301 1301 | 26599 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 2.1458.0 GPS week: 1458 Day: 0 MJD: 54450
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 3 -7 -167 -94 -249 .18 34 30 | 0 77 2529 2712
cod 177| 0 4 0 -49 -13 -17 -.07 33 25 | --- --- --- ---
esx 50| -5 -12 2 244 134 185 -.39 222 51 | 6523 18539 11885 13507
iac n/a| 2 0 0 -64 -97 70 .41 42 42 | 1484849 6613 10286 11959
mcc n/a| -7 11 108 265 -182 -228 .79 135 135 | --- --- --- ---
Table 2.1458.1 GPS week: 1458 Day: 1 MJD: 54451
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| -7 -2 14 -89 -103 52 .09 42 43 | 0 139 2211 2258
cod 177| 0 -5 -9 16 -58 -71 -.09 29 26 | --- --- --- ---
esx 50| 11 0 -9 24 188 -132 -.04 291 48 | -64147 8922 7141 14051
iac n/a| 3 7 -1 17 -20 221 .15 36 36 | 1425589 3312 6168 12801
mcc n/a| -14 -13 56 -35 23 -436 1.35 140 140 | --- --- --- ---
Table 2.1458.2 GPS week: 1458 Day: 2 MJD: 54452
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| 4 0 0 120 36 27 -.05 36 30 | 0 18 2285 2378
cod 177| -9 -9 -13 -74 -98 -186 .11 47 44 | --- --- --- ---
esx 50| 8 12 4 -98 140 -18 -.35 261 61 | 443801 7416 9867 25888
iac n/a| 2 -2 3 13 -22 69 .42 42 42 | 1482240 2746 8300 21790
mcc n/a| 17 6 13 115 250 -370 .79 119 119 | --- --- --- ---
Table 2.1458.3 GPS week: 1458 Day: 3 MJD: 54453
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| -12 2 0 -104 -78 54 .18 40 33 | 0 -7 3536 3846
cod 177| -7 4 0 -52 -217 24 -.36 56 48 | --- --- --- ---
esx 50| 3 -1 -7 218 204 18 -.49 291 80 | -25397 5794 11717 23003
iac n/a| 8 -5 2 -2 19 -5 .12 27 27 | 1422381 -3400 11290 21251
mcc n/a| 61 68 58 -328 232 ---- -9.54 931 931 | --- --- --- ---
Table 2.1458.4 GPS week: 1458 Day: 4 MJD: 54454
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| 1 0 1 -87 33 -108 .07 31 27 | 0 -162 2513 2573
cod 177| -1 0 0 30 -59 66 -.04 31 26 | --- --- --- ---
esx 50| 2 2 -3 238 261 65 -.13 286 79 | 25137 -5418 9091 13248
iac n/a| -1 -1 3 10 -24 -10 .35 39 39 | 1471403 -6660 7756 12154
mcc n/a| 112 169 232 -984 -1882 ---- -5.99 657 657 | --- --- --- ---
Table 2.1458.5 GPS week: 1458 Day: 5 MJD: 54455
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| 7 5 -9 -75 81 53 -.13 46 44 | 0 5 2713 2947
cod 177| -13 -1 3 50 -20 -135 .09 36 27 | --- --- --- ---
esx 50| 7 3 8 185 20 -239 -.43 230 68 | 38739 10891 8609 32319
iac n/a| 10 3 -2 -166 -42 91 .38 43 43 | 1462376 3257 7832 25599
mcc n/a| -24 115 -217 396 -931 -6870 -3.98 571 571 | --- --- --- ---
Table 2.1458.6 GPS week: 1458 Day: 6 MJD: 54456
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 6 -2 -75 109 42 -.10 40 28 | 0 117 3190 3408
cod 177| -9 -18 15 -27 -216 56 .05 71 52 | --- --- --- ---
esx 50| 3 -9 -22 320 -89 -197 -.11 284 85 | 12252 9944 7953 18418
iac n/a| 11 38 -13 -77 304 355 -.05 84 84 | 1438965 5569 7464 16383
mcc n/a| -38 -341 -267 4313 -2221 -7412 -7.10 497 497 | --- --- --- ---
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 3.1458.0 GPS week: 1458 Day: 0 MJD: 54450
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7658 41 13 21 44 --- 18 | 172 173 209 186 --- 178
R04 | 7288 49 33 64 31 --- 26 | 52 88 83 76 --- 69
R06 | 4048 36 52 41 45 --- 25 | 31 56 53 56 --- 43
R07 | 2428 15 22 17 31 135 12 | 33 30 45 34 181 26
R08 | 5908 30 38 43 43 --- 22 | 33 36 46 68 --- 38
XR10E | 8105 111 91 --- 429 --- 101 | 92 93 --- 211 --- 98
XR14E | 9137 789 107 --- 137 --- 121 | 433 72 --- 78 --- 116
XR15E |15357 125 124 --- 146 262 92 | 129 145 --- 102 75 78
XR17 |10677 128 80 --- 94 --- 72 | 107 83 --- 70 --- 68
R19 | 2757 23 21 399 28 --- 17 | 58 70 422 76 --- 86
XR20 | 4717 38 22 --- 50 --- 26 | 48 65 --- 81 --- 67
XR21 | ---- >>>> 22 --- 36 --- 29 | 9999 89 --- 79 --- 81
R23 | 9943 32 36 422 60 --- 30 | 67 62 406 51 --- 63
------+------------------------------------+--------------------------------
RMS | 6273 34 33 222 42 135 |T 104 81 180 89 128 77
WRMS | 6273 30 25 51 42 135 |NE 66 75 180 77 181 71
MEDI | 7288 41 36 43 45 135 |MD 58 72 83 76 75 69
Table 3.1458.1 GPS week: 1458 Day: 1 MJD: 54451
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6930 38 16 39 44 --- 20 | 141 153 172 153 --- 150
R04 | 7601 54 35 38 24 --- 22 | 35 94 58 70 --- 64
R06 | 2258 51 48 28 46 --- 26 | 27 68 75 43 --- 45
R07 | 1919 30 15 42 14 140 15 | 23 33 46 31 279 18
R08 | 5647 36 20 55 56 --- 24 | 44 50 45 53 --- 42
XR10E | 2884 139 80 --- 293 --- 106 | 61 132 --- 186 --- 103
XR14E | 3572 1108 40 --- 56 --- 48 | 688 59 --- 85 --- 94
XR15E | 7665 317 37 --- 54 269 45 | 274 71 --- 76 74 96
XR17 |11604 83 30 --- 79 --- 45 | 147 83 --- 58 --- 90
R19 | 2026 48 33 456 20 --- 24 | 20 49 281 22 --- 38
R20 | 3386 23 20 512 30 --- 17 | 33 59 390 38 --- 54
XR21 | ---- >>>> 56 --- 76 --- 65 | 9999 92 --- 57 --- 65
R23 | 8447 49 28 446 34 --- 25 | 40 38 268 30 --- 23
------+------------------------------------+--------------------------------
RMS | 5401 42 29 291 36 140 |T 127 75 166 69 176 67
WRMS | 5401 43 26 48 36 140 |NE 56 71 166 55 279 58
MEDI | 3572 51 33 42 46 140 |MD 40 68 75 57 74 64
Table 3.1458.2 GPS week: 1458 Day: 2 MJD: 54452
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |15763 52 55 84 46 --- 34 | 135 179 206 140 --- 148
R04 | 7324 16 52 39 59 --- 24 | 52 80 72 47 --- 54
R06 | 2712 22 36 32 18 --- 16 | 29 48 62 51 --- 38
R07 | 1317 11 41 33 28 119 16 | 36 39 51 47 416 33
R08 | 7920 44 27 52 51 --- 25 | 43 58 87 65 --- 46
XR10E | 4116 52 74 --- 340 --- 62 | 72 82 --- 182 --- 84
XR14E |10096 89 75 --- 181 --- 85 | 315 68 --- 173 --- 69
XR15E | 5891 506 81 --- 78 257 80 | 336 76 --- 77 111 125
XR17 |12382 111 82 --- 87 --- 68 | 101 57 --- 34 --- 48
R19 | 1589 23 42 508 32 --- 23 | 38 62 399 36 --- 58
XR20 | 1696 24 41 --- 18 --- 20 | 47 87 --- 31 --- 50
XR21 | ---- >>>> 44 --- 42 --- 43 | 9999 163 --- 105 --- 144
R23 | 7661 57 67 452 43 --- 40 | 59 61 320 47 --- 52
------+------------------------------------+--------------------------------
RMS | 7884 36 47 261 42 119 |T 105 81 171 79 263 73
WRMS | 7884 30 44 61 42 119 |NE 60 83 171 60 416 67
MEDI | 5891 52 52 52 46 119 |MD 52 68 87 51 111 54
Table 3.1458.3 GPS week: 1458 Day: 3 MJD: 54453
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |14526 51 58 57 24 --- 25 | 125 177 176 162 --- 153
R04 |10160 35 56 29 26 --- 20 | 30 53 47 45 --- 36
R06 | 4522 34 31 75 14 --- 21 | 49 54 60 57 --- 49
R07 | 2976 24 29 37 15 931 14 | 29 45 48 29 770 29
R08 |11829 39 53 69 18 --- 24 | 54 87 95 80 --- 67
XR10E | 7824 154 126 --- 118 --- 92 | 63 100 --- 112 --- 69
XR14E | 7415 357 163 --- 67 --- 104 | 263 81 --- 241 --- 125
XR15E | 9527 149 116 --- 76 942 77 | 159 114 --- 129 158 64
XR17 | 6011 63 49 --- 43 --- 35 | 122 71 --- 53 --- 60
R19 | 1356 29 44 488 22 --- 21 | 38 56 380 38 --- 56
R20 | 936 28 48 524 19 --- 21 | 46 73 371 47 --- 65
XR21 | ---- >>>> 53 --- 22 --- 34 | 9999 94 --- 62 --- 89
R23 | 7751 66 98 389 53 --- 48 | 67 100 313 57 --- 61
------+------------------------------------+--------------------------------
RMS | 8263 40 56 291 27 931 |T 87 85 186 85 464 71
WRMS | 8263 33 48 80 27 931 |NE 62 81 186 63 770 66
MEDI | 7415 51 53 69 24 931 |MD 54 81 95 57 158 64
Table 3.1458.4 GPS week: 1458 Day: 4 MJD: 54454
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |11627 28 42 40 45 --- 22 | 130 112 127 158 --- 128
R04 |13136 24 16 86 35 --- 21 | 77 90 111 82 --- 81
R06 | 1810 25 17 69 27 --- 18 | 53 50 72 76 --- 55
R07 | 5216 13 16 49 26 657 13 | 35 50 78 39 296 39
R08 |11910 42 37 78 47 --- 27 | 97 79 117 80 --- 84
XR10E | 2569 62 68 --- 47 --- 43 | 69 112 --- 152 --- 92
XR14E | 3879 57 65 --- 51 --- 41 | 132 47 --- 65 --- 31
XR15E |15929 44 40 --- 423 821 42 | 110 61 --- 231 72 92
XR17 | 8131 45 40 --- 34 --- 29 | 72 92 --- 61 --- 75
R19 | 2400 33 31 429 22 --- 21 | 28 52 301 40 --- 46
R20 | 1608 17 21 489 28 --- 15 | 38 64 327 50 --- 60
XR21 | ---- >>>> 16 --- 63 --- 40 | 9999 304 --- 83 --- 303
R23 | 5529 52 47 459 64 --- 37 | 84 60 356 71 --- 57
------+------------------------------------+--------------------------------
RMS | 8054 31 31 286 39 657 |T 77 90 186 91 184 87
WRMS | 8054 27 26 79 39 657 |NE 68 95 186 74 296 92
MEDI | 5216 42 37 78 45 657 |MD 72 64 117 76 72 75
Table 3.1458.5 GPS week: 1458 Day: 5 MJD: 54455
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |10153 24 45 63 27 --- 23 | 54 82 108 70 --- 65
R04 |14654 41 27 77 42 --- 26 | 61 60 57 65 --- 56
R06 | 979 43 25 47 44 --- 22 | 44 62 43 102 --- 63
R07 | 1076 43 30 36 21 571 19 | 20 72 89 36 291 36
R08 |14695 36 31 48 49 --- 23 | 47 70 102 53 --- 53
XR10E | 1204 73 91 --- 72 --- 56 | 55 121 --- 92 --- 66
XR14E | 4633 22 21 --- 35 --- 18 | 99 28 --- 35 --- 28
XR15E | 7634 54 47 --- 50 478 36 | 36 45 --- 135 89 58
XR17 | 6899 138 37 --- 108 --- 71 | 36 81 --- 134 --- 76
XR19 | 2132 35 30 --- 26 --- 22 | 71 67 --- 70 --- 60
R20 | 1876 48 16 499 40 --- 25 | 21 43 253 63 --- 51
R23 | 3692 74 58 328 64 --- 46 | 134 62 238 98 --- 92
------+------------------------------------+--------------------------------
RMS | 8888 46 36 230 43 571 |T 56 66 127 79 190 58
WRMS | 8888 44 27 68 43 571 |NE 54 66 127 76 291 61
MEDI | 3692 43 30 63 42 478 |MD 47 62 102 70 89 58
Table 3.1458.6 GPS week: 1458 Day: 6 MJD: 54456
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9308 35 55 44 36 --- 24 | 69 98 83 82 --- 64
R04 |15633 36 36 40 73 --- 24 | 76 97 105 100 --- 87
R06 | 2102 24 61 37 121 --- 31 | 46 66 56 99 --- 59
R07E | 2411 26 77 37 88 497 30 | 36 104 76 67 447 56
R08E |15661 15 43 96 107 --- 35 | 52 68 52 92 --- 49
XR10E | 1878 57 89 --- 112 --- 54 | 69 96 --- 97 --- 73
XR14E | 6030 19 41 --- 47 --- 22 | 106 27 --- 44 --- 34
XR15E | 9865 34 41 --- 106 697 37 | 46 70 --- 83 88 35
XR17 | 9205 63 72 --- 135 --- 56 | 103 126 --- 138 --- 115
R19 | 2005 27 50 486 49 --- 27 | 85 83 475 80 --- 110
R20 | 1638 27 37 459 42 --- 23 | 91 65 404 89 --- 105
R23 | 3309 85 143 428 107 --- 76 | 194 41 446 67 --- 121
------+------------------------------------+--------------------------------
RMS | 8690 40 71 284 84 497 |T 81 78 212 86 267 75
WRMS | 8690 28 52 85 84 497 |NE 99 79 297 95 --- 99
MEDI | 3309 27 50 44 88 497 |MD 69 70 83 83 88 64
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