[IGSREPORT-15695] Wk 1452 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Nov 23 03:49:03 PST 2007
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IGS Electronic Report 23 Nov 03:49:20 PST 2007 Message Number 15695
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1452 (Nov 04, 2007 - Nov 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 2.1452.
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:
igl1452[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1452 in the SP3 format.
igl14527.sum Combination Report for GPS Week 1452.
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 | 1321.5 ns
1 | 1364.9 ns
2 | 1365.1 ns
3 | 1360.1 ns
4 | 1406.6 ns
5 | 1438.9 ns
6 | 1418.0 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 | R04
0 | ESX | R10 R14 R23 R24
1 | ESX | R10 R14 R23 R24
2 | ESX | R10 R14 R23 R24
3 | ESX | R10 R14 R23 R24
4 | ESX | R10 R14 R23 R24
5 | ESX | R10 R14 R23 R24
6 | ESX | R10 R14 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 1.1452, 1a.1452).
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 2.1452.0-6)
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 3.1452.0-6).
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 1452 summary. (Nov 04, 2007 - Nov 10, 2007)
Table 1.1452.a GPS week : 1452 MJD: 54408.0-54414.0
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 -1 6 -3 6 -31 -.06 34 30 | 0 -333 4393 4918
| 3 3 10 80 45 177 .16 | 0 1881
cod 175| 2 0 1 34 -3 -1 -.06 34 30 | --- --- --- ---
| 5 3 6 61 61 77 .12 | --- ---
esx 52| 2 -5 -1 -142 41 -46 -.22 264 90 | -13265 -24399 8446 14614
| 5 8 7 123 162 196 .29 | 56608 14482
iac n/a| 0 -1 -6 10 -15 42 .05 33 33 | 1381941 -553 8212 14681
| 3 4 9 45 46 167 .09 | 41010 2284
mcc n/a| 0 -3 55 -3 -71 -174 -.06 502 502 | --- --- --- ---
| 11 8 18 81 158 1340 .26 | --- ---
Table 1.1452.b GPS week : 1452 MJD: 54408.0-54414.0
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 | 513 708 100 29 29 31 20 |
R04 | 0 281 147 43 27 21 20 |
R06 | 14 16 15 15 20 25 23 |
R07 | 17 18 16 14 21 17 20 |
R08 | 24 24 34 24 16 27 21 |
R10 | 23 24 18 15 26 23 24 |
R14 | 16 17 18 15 24 20 26 |
R15 | 82 42 67 83 49 39 46 |
R19 | --- --- --- --- 0 0 138 |
R21 | 17 17 15 15 34 34 22 |
R23 | 24 28 25 17 32 33 54 |
R24 | 17 17 23 28 24 32 20 |
Table 1.1452.c GPS week : 1452 MJD: 54408.0-54414.0
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 1452 0 | 265 20 291 -834 -6678 -17710 101.8 5653 5653 | 1321472 0
brd 1452 1 | 41 -44 320 -1252 -8022 -15860 93.5 5077 5077 | 1364884 0
brd 1452 2 | -387 366 216 -4765 -8750 -14920 98.8 4918 4918 | 1365114 0
brd 1452 3 | 156 -335 -1088 4541 8991 -3750 90.6 4551 4551 | 1360122 0
brd 1452 4 | 570 414 224 -847 -5493 485 101.6 6207 6207 | 1406615 0
brd 1452 5 | 442 421 -369 -3245 -8622 -23360 80.1 6396 6396 | 1438851 0
brd 1452 6 | 10 -66 -319 -3083 -6920 -17580 73.6 5741 5741 | 1418049 0
-------------+------------------------------------------------------------+----------------
brd 1452 mean| 157 110 -103 -1355 -5070 -13242 91.4 5506 5506 | 1382158 0
brd 1452 sdev| 314 293 521 2985 6308 8459 10.9 683 683 | 40533 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 2.1452.0 GPS week: 1452 Day: 0 MJD: 54408
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 12 0 44 -91 .03 19 19 | 0 973 3251 3510
cod 175| -4 -2 -4 43 -16 76 -.06 23 20 | --- --- --- ---
esx 52| 3 -6 9 -335 -55 -32 -.49 279 106 | -111342 -37242 10590 13308
iac n/a| 3 2 -24 -54 -18 238 .06 41 41 | 1317147 1951 10074 12977
mcc n/a| 1 -2 27 -146 -11 203 .16 327 327 | --- --- --- ---
Table 2.1452.1 GPS week: 1452 Day: 1 MJD: 54409
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 17 9 -28 -209 -.08 32 33 | 0 -4428 10975 13088
cod 175| 4 0 6 4 -55 -104 -.04 40 37 | --- --- --- ---
esx 52| 4 10 0 -210 312 81 -.54 285 104 | 51583 -8757 8181 15786
iac n/a| -6 -1 -9 8 18 86 .00 19 19 | 1361140 976 8118 15822
mcc n/a| 10 5 69 79 -183 334 -.32 472 472 | --- --- --- ---
Table 2.1452.2 GPS week: 1452 Day: 2 MJD: 54410
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 20 61 35 -89 -.39 50 37 | 0 301 3127 3308
cod 175| 7 1 -4 -62 123 59 .11 26 25 | --- --- --- ---
esx 52| -4 -1 -12 -141 -184 176 -.26 269 71 | 28799 233 7787 13498
iac n/a| 3 2 2 6 -18 -78 .09 28 28 | 1366190 1733 7574 13882
mcc n/a| -7 -1 82 89 -129 858 -.25 202 202 | --- --- --- ---
Table 2.1452.3 GPS week: 1452 Day: 3 MJD: 54411
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 4 -15 67 336 -.04 35 28 | 0 1117 3402 3582
cod 175| -4 1 4 32 -7 -79 .07 22 16 | --- --- --- ---
esx 52| 9 -2 -6 -68 -72 121 -.23 269 78 | 36581 -28636 6667 10802
iac n/a| 0 -2 -9 -7 -62 -249 .17 30 30 | 1366955 -4490 6484 12054
mcc n/a| 0 1 65 22 32 799 -.35 377 377 | --- --- --- ---
Table 2.1452.4 GPS week: 1452 Day: 4 MJD: 54412
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 -6 1 -142 8 -147 .05 27 23 | 0 -219 3053 3212
cod 175| 6 0 -3 136 22 23 -.21 36 32 | --- --- --- ---
esx 52| 7 -18 -7 37 69 -87 -.27 265 110 | -32879 -34316 7159 15143
iac n/a| 0 -11 -7 85 -68 -12 -.12 43 43 | 1405953 -1567 6866 13934
mcc n/a| 14 3 55 -8 214 703 -.09 645 645 | --- --- --- ---
Table 2.1452.5 GPS week: 1452 Day: 5 MJD: 54413
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 -45 -61 -16 .09 35 33 | 0 -245 3153 3455
cod 175| 8 3 13 72 -52 73 -.20 49 42 | --- --- --- ---
esx 52| -4 -10 -2 -63 113 -381 .33 241 93 | -32030 -26699 9559 20204
iac n/a| -1 0 -2 -16 67 141 .12 32 32 | 1436744 -1185 9075 19676
mcc n/a| -20 -14 46 -60 -216 -2551 .23 816 816 | --- --- --- ---
Table 2.1452.6 GPS week: 1452 Day: 6 MJD: 54414
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 -1 109 -16 -1 -.05 42 36 | 0 166 3794 4275
cod 175| -3 -6 0 14 -35 -57 -.10 40 39 | --- --- --- ---
esx 52| 2 -5 6 -213 109 -200 -.10 236 70 | -33569 -35379 9182 13557
iac n/a| 0 2 2 52 -26 170 .06 36 36 | 1419460 -1292 9297 14425
mcc n/a| 0 -16 43 -1 -206 -1570 .22 675 675 | --- --- --- ---
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 3.1452.0 GPS week: 1452 Day: 0 MJD: 54408
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |15556 466 565 --- --- --- 513 | 332 236 --- --- --- 144
XR04 | ---- 2853 6 --- --- --- 0 | 9999 228 --- --- --- 215
R06 | 2742 15 19 59 24 --- 13 | 32 32 68 38 --- 34
R07 | 1556 21 18 76 33 64 17 | 23 31 69 54 42 27
R08 | 3598 21 32 105 50 --- 24 | 43 50 52 61 --- 33
R10 | 2735 11 24 444 65 --- 23 | 65 72 169 94 --- 74
R14 | 4023 19 19 449 32 --- 15 | 30 33 195 37 --- 29
XR15 | 5570 49 136 --- 169 121 81 | 74 91 --- 126 97 81
R21 | 3585 16 18 78 31 --- 16 | 39 35 69 31 --- 29
R23 | 6415 27 27 340 52 --- 23 | 82 92 78 66 --- 76
R24 |12454 21 25 289 27 458 17 | 120 134 139 115 561 123
------+------------------------------------+--------------------------------
RMS | 5653 19 23 279 41 327 |T 84 94 104 69 233 78
WRMS | 5653 19 20 106 41 327 |NE 84 94 104 69 233 78
MEDI | 3598 21 24 105 33 121 |MD 43 72 69 61 97 74
Table 3.1452.1 GPS week: 1452 Day: 1 MJD: 54409
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 8996 659 760 --- --- --- 708 | 767 260 --- --- --- 352
XR04 | ---- 263 300 --- --- --- 280 | 9999 513 --- --- --- 453
R06 | 1310 12 31 72 9 --- 16 | 35 38 56 34 --- 30
R07 | 2667 21 24 85 14 56 18 | 44 46 69 48 52 43
R08 | 3748 55 55 42 22 --- 23 | 43 34 59 35 --- 26
R10 | 2831 20 60 518 19 --- 23 | 86 73 114 82 --- 85
R14 | 5710 32 25 404 18 --- 17 | 25 36 139 33 --- 25
XR15 | 3564 67 78 --- 43 173 41 | 53 79 --- 88 106 69
R21 | 2658 35 26 57 14 --- 16 | 35 37 36 35 --- 26
R23 | 5227 41 48 316 33 --- 27 | 66 81 94 54 --- 58
R24 |10408 23 36 320 14 665 16 | 59 66 117 60 608 56
------+------------------------------------+--------------------------------
RMS | 5077 32 40 285 19 472 |T 121 114 85 52 255 111
WRMS | 5077 33 37 104 19 472 |NE 121 114 85 52 255 111
MEDI | 3564 35 48 85 18 173 |MD 44 66 69 48 106 56
Table 3.1452.2 GPS week: 1452 Day: 2 MJD: 54410
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 8970 133 74 --- --- --- 99 | 318 267 --- --- --- 245
XR04 |12833 194 110 --- --- --- 146 | 588 185 --- --- --- 199
R06 | 1003 29 20 33 22 --- 15 | 26 47 65 29 --- 37
R07 | 4947 21 23 38 24 38 15 | 29 44 54 39 39 37
R08 | 3096 110 36 34 49 --- 34 | 63 30 53 45 --- 31
R10 | 2343 40 24 414 12 --- 18 | 73 66 137 64 --- 67
R14 | 3291 33 14 445 27 --- 17 | 43 27 176 41 --- 32
XR15 | 9199 75 79 --- 116 137 67 | 59 62 --- 154 59 74
R21 | 5482 18 20 44 14 --- 15 | 41 44 50 26 --- 37
R23 | 3386 47 29 332 32 --- 25 | 61 74 66 54 --- 62
R24 |10029 43 32 308 25 283 23 | 113 133 164 120 335 121
------+------------------------------------+--------------------------------
RMS | 4918 50 26 269 28 202 |T 128 89 95 63 144 85
WRMS | 4918 37 25 71 28 202 |NE 128 89 95 63 144 85
MEDI | 4947 43 29 44 25 137 |MD 61 62 65 45 59 62
Table 3.1452.3 GPS week: 1452 Day: 3 MJD: 54411
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4173 50 24 101 40 --- 28 | 177 177 59 31 --- 159
XR04 | 6945 47 52 --- 77 --- 42 | 353 145 --- 43 --- 132
R06 | 3030 19 14 50 26 --- 14 | 43 31 60 29 --- 29
R07 | 4204 10 19 38 32 34 14 | 62 54 73 37 75 46
R08 | 2689 62 28 42 34 --- 24 | 56 25 70 47 --- 34
R10 | 3139 17 18 459 25 --- 14 | 123 100 195 113 --- 111
R14 | 2443 26 9 428 27 --- 15 | 51 27 180 40 --- 31
XR15 |11883 63 109 --- 157 430 82 | 79 120 --- 142 90 81
R21 | 7386 13 25 48 23 --- 15 | 37 20 56 28 --- 21
R23 | 4530 29 17 316 24 --- 16 | 75 64 86 63 --- 59
R24 | 6630 50 35 374 31 533 27 | 73 111 165 107 502 94
------+------------------------------------+--------------------------------
RMS | 4550 35 22 269 30 377 |T 102 79 104 61 222 72
WRMS | 4550 28 16 78 30 377 |NE 102 79 104 61 222 72
MEDI | 4204 29 24 101 31 430 |MD 73 64 73 43 90 59
Table 3.1452.4 GPS week: 1452 Day: 4 MJD: 54412
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4708 25 27 148 38 --- 29 | 82 106 87 30 --- 71
XR04 | 6174 28 21 --- 59 --- 26 | 200 68 --- 54 --- 60
R06 | 3400 16 43 60 29 --- 19 | 21 40 55 33 --- 23
R07 | 2347 24 19 70 51 57 21 | 18 27 67 59 96 25
XR08 | 3620 18 25 --- 25 --- 16 | 35 30 --- 43 --- 21
R10 | 5793 29 40 405 39 --- 25 | 90 102 147 83 --- 86
R14 | 2358 20 34 376 48 --- 24 | 31 35 160 30 --- 24
XR15 |11461 41 69 --- 97 510 48 | 97 132 --- 114 107 105
XR19 | ---- --- 10 --- --- --- 0 | --- 382 --- --- --- 382
XR21 | 5238 30 42 --- 72 --- 34 | 28 32 --- 25 --- 17
R23 | 5961 38 50 251 48 --- 32 | 62 83 78 38 --- 46
R24 |12481 31 27 307 42 910 23 | 94 86 121 101 931 86
------+------------------------------------+--------------------------------
RMS | 6207 27 36 265 43 645 |T 68 93 102 55 378 78
WRMS | 6207 23 32 110 43 645 |NE 68 93 102 55 378 78
MEDI | 5238 28 27 251 48 510 |MD 62 68 87 43 107 46
Table 3.1452.5 GPS week: 1452 Day: 5 MJD: 54413
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2338 47 40 112 26 --- 30 | 63 117 56 34 --- 70
R04 | 2659 23 45 54 28 --- 20 | 224 148 38 47 --- 141
R06 | 5048 31 40 84 27 --- 24 | 31 51 67 44 --- 34
R07 | 3295 16 34 56 18 40 16 | 41 34 67 40 96 40
R08 | 4853 26 52 77 42 --- 27 | 27 47 33 36 --- 22
R10 | 3859 32 39 393 27 --- 22 | 65 75 147 82 --- 71
R14 | 3428 20 28 486 34 --- 20 | 26 41 180 33 --- 26
XR15 | 8691 25 69 --- 64 248 39 | 119 137 --- 133 125 118
XR19 | ---- --- 12 --- --- --- 0 | --- 108 --- --- --- 110
R21 | 5793 40 82 81 41 --- 33 | 17 59 75 43 --- 32
R23 | 5394 48 61 282 29 --- 33 | 37 85 83 51 --- 47
R24 |15727 45 49 275 40 1154 31 | 121 134 209 152 923 130
------+------------------------------------+--------------------------------
RMS | 6396 35 49 241 32 816 |T 70 86 95 63 381 70
WRMS | 6396 33 42 93 32 816 |NE 70 86 95 63 381 70
MEDI | 4853 31 40 84 29 248 |MD 41 75 67 44 125 47
Table 3.1452.6 GPS week: 1452 Day: 6 MJD: 54414
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1699 37 30 48 23 --- 20 | 82 101 86 40 --- 79
R04 | 2558 21 37 42 36 --- 20 | 355 137 39 28 --- 121
R06 | 3960 40 36 50 31 --- 22 | 37 42 59 48 --- 39
R07 | 5068 23 36 53 25 62 19 | 28 32 66 25 51 22
R08 | 4974 34 34 46 28 --- 20 | 37 44 51 41 --- 32
R10 | 2250 43 24 420 30 --- 24 | 85 82 184 91 --- 85
R14 | 3380 20 46 461 38 --- 25 | 30 31 212 34 --- 27
XR15 | 8112 52 77 --- 63 194 45 | 99 128 --- 101 85 100
XR19 | ---- --- 120 156 --- --- 137 | --- 116 20 --- --- 160
R21 | 5535 26 51 34 36 --- 21 | 19 65 36 28 --- 29
R23 | 2691 97 60 243 64 --- 53 | 61 128 99 109 --- 86
R24 |14131 21 29 310 33 953 20 | 58 72 95 76 469 65
------+------------------------------------+--------------------------------
RMS | 5741 42 40 236 36 675 |T 81 81 86 56 201 70
WRMS | 5741 36 39 70 36 675 |NE 81 81 86 56 201 70
MEDI | 3960 34 36 53 33 194 |MD 58 72 66 41 85 65
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