[IGSREPORT-15346] Wk 1436 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Tue Aug 7 00:56:34 PDT 2007
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IGS Electronic Report 07 Aug 00:56:38 PDT 2007 Message Number 15346
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1436 (Jul 15, 2007 - Jul 21, 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 2.1436.
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:
igl1436[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1436 in the SP3 format.
igl14367.sum Combination Report for GPS Week 1436.
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 | 1061.6 ns
1 | 1047.0 ns
2 | 997.9 ns
3 | 989.1 ns
4 | 988.5 ns
5 | 1015.5 ns
6 | 1038.0 ns
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 1.1436, 1a.1436).
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 2.1436.0-6)
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 3.1436.0-6).
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 1436 summary. (Jul 15, 2007 - Jul 21, 2007)
Table 1.1436.a GPS week : 1436 MJD: 54296.0-54302.0
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 56| 1 0 -11 -36 21 -60 -.09 125 68 | 0 272 4433 4727
| 6 1 10 86 103 251 .12 | 0 1345
cod 170| 1 -1 0 1 4 -98 -.26 52 49 | --- --- --- ---
| 3 1 5 32 51 81 .14 | --- ---
esx 42| -6 6 10 61 -45 50 -.52 187 81 | 14273 8607 13571 24276
| 10 8 16 144 202 184 .20 | 23240 15120
iac n/a| 0 2 0 -26 -9 86 .56 62 62 | 1021263 1487 13093 23194
| 4 4 5 35 45 118 .17 | 29833 4640
mcc n/a| -20 -2 41 348 84 924 .79 111 111 | --- --- --- ---
| 32 20 26 354 217 804 .69 | --- ---
Table 1.1436.b GPS week : 1436 MJD: 54296.0-54302.0
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 | 28 30 32 46 122 34 29 |
R03E | 30 35 39 31 47 38 36 |
R04E | 27 43 43 54 37 110 121 |
R06E | 33 21 24 24 20 25 38 |
R07E | 38 36 20 27 48 58 33 |
R08E | 50 81 53 30 55 33 28 |
R10 | 26 30 20 26 27 32 25 |
R14 | 30 23 18 16 32 38 28 |
R15 | 0 0 0 0 0 0 0 |
R21 | 24 22 21 22 42 38 21 |
R22 | 0 0 --- --- --- --- --- |
R23 | 83 84 71 76 77 77 97 |
R24 | 92 77 80 64 72 79 75 |
Table 1.1436.c GPS week : 1436 MJD: 54296.0-54302.0
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 1436 0 | -343 -674 -755 1538 244 -327600 92.1 8315 8315 | 1061558 0
brd 1436 1 | -10 280 -716 5142 -2410 -329100 83.9 8816 8816 | 1046961 0
brd 1436 2 | 371 62 -526 10060 5233 -345000 78.1 6907 6907 | 997851 0
brd 1436 3 | 684 671 -518 -9167 805 -349200 105.0 7455 7455 | 989142 0
brd 1436 4 | -203 -45 225 172 179 -370100 89.1 7610 7610 | 988534 0
brd 1436 5 | -177 -161 -254 -3104 -3170 -384800 91.3 10020 10020 | 1015531 0
brd 1436 6 | -287 583 176 10670 -10140 -398700 85.6 13130 13130 | 1038018 0
-------------+------------------------------------------------------------+----------------
brd 1436 mean| 4 102 -338 2187 -1322 -357785 89.3 8893 8893 | 1019656 0
brd 1436 sdev| 383 462 403 7118 4735 27467 8.4 2129 2129 | 29525 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 2.1436.0 GPS week: 1436 Day: 0 MJD: 54296
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 56| -6 0 -9 -73 -33 175 -.16 71 66 | 0 532 3728 4002
cod 170| 4 -2 -10 13 -50 -152 -.34 59 52 | --- --- --- ---
esx 42| 1 -1 39 199 309 157 -.34 221 75 | 2238 29635 10834 27531
iac n/a| 0 7 6 -25 5 -130 .41 55 55 | 1069378 1055 10273 25910
mcc n/a| -44 -5 17 469 278 1380 1.72 109 109 | --- --- --- ---
Table 2.1436.1 GPS week: 1436 Day: 1 MJD: 54297
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 56| 0 0 -9 -58 84 -38 .15 102 67 | 0 -596 4268 4398
cod 170| 0 0 -2 19 -55 18 -.15 51 45 | --- --- --- ---
esx 42| 0 0 21 316 -50 -145 -.63 191 79 | 11151 26553 13088 16835
iac n/a| -2 -3 0 -64 -40 110 .76 63 63 | 1045561 9491 12313 15868
mcc n/a| -82 -40 31 980 265 2402 1.60 316 316 | --- --- --- ---
Table 2.1436.2 GPS week: 1436 Day: 2 MJD: 54298
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 56| -6 1 0 -119 -57 25 -.02 96 58 | 0 456 3649 3955
cod 170| 4 -2 2 -27 35 -42 -.25 43 38 | --- --- --- ---
esx 42| 11 -4 9 -68 -109 160 -.19 193 79 | 11420 6653 14448 23841
iac n/a| 4 0 -9 16 -70 4 .54 49 49 | 999924 1137 13307 21459
mcc n/a| -1 0 9 36 195 899 .24 51 51 | --- --- --- ---
Table 2.1436.3 GPS week: 1436 Day: 3 MJD: 54299
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 56| 7 2 0 -46 77 -354 -.14 88 57 | 0 2229 4341 4531
cod 170| -3 0 1 -9 39 -25 -.40 41 40 | --- --- --- ---
esx 42| -14 15 -9 -56 -63 263 -.45 161 65 | 10886 8558 13717 27523
iac n/a| 3 -1 0 -23 -17 183 .71 53 53 | 991442 -1554 13759 27356
mcc n/a| 7 3 37 48 -91 819 .04 70 70 | --- --- --- ---
Table 2.1436.4 GPS week: 1436 Day: 4 MJD: 54300
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 56| 1 0 -11 -112 -112 -448 -.18 209 69 | 0 -795 4664 5176
cod 170| 2 0 0 7 59 -123 -.23 49 52 | --- --- --- ---
esx 42| -12 14 0 -4 -370 -72 -.64 171 93 | -22522 88 19048 32723
iac n/a| 1 4 0 21 72 228 .70 77 77 | 990214 -989 17812 30373
mcc n/a| 4 6 42 77 130 274 .42 96 96 | --- --- --- ---
Table 2.1436.5 GPS week: 1436 Day: 5 MJD: 54301
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 56| 12 0 -19 121 194 210 -.17 155 77 | 0 1611 4786 5039
cod 170| 2 -2 5 -45 -45 -202 -.02 49 43 | --- --- --- ---
esx 42| -20 10 7 55 55 189 -.79 182 93 | 40252 -13570 11202 20552
iac n/a| -7 7 -1 -59 12 103 .52 83 83 | 1019916 -4264 10655 19228
mcc n/a| -23 25 88 601 -323 -94 1.14 79 79 | --- --- --- ---
Table 2.1436.6 GPS week: 1436 Day: 6 MJD: 54302
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 56| 4 -2 -28 37 -4 7 -.13 157 84 | 0 -1529 5599 5989
cod 170| -1 -1 3 52 45 -160 -.40 71 70 | --- --- --- ---
esx 42| -8 10 3 -12 -85 -198 -.61 193 85 | 46488 2334 12663 20928
iac n/a| -2 1 6 -54 -30 104 .29 54 54 | 1032408 5537 13532 22168
mcc n/a| -1 -8 59 224 135 793 .37 55 55 | --- --- --- ---
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 3.1436.0 GPS week: 1436 Day: 0 MJD: 54296
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 4494 61 32 55 48 --- 28 | 66 55 70 76 --- 57
R03E | 8028 52 36 83 52 --- 30 | 80 65 77 104 --- 75
R04E | 7493 58 47 55 33 --- 27 | 168 86 77 111 --- 103
R06E | 3031 36 74 72 44 --- 32 | 47 86 36 49 --- 39
R07E | 7825 47 47 154 53 109 38 | 41 41 104 46 101 29
R08E | 7197 121 98 56 36 --- 50 | 80 68 72 68 --- 50
XR10 | 5052 43 27 --- 38 --- 25 | 44 49 --- 58 --- 46
XR14 | 4538 46 26 --- 50 --- 30 | 35 27 --- 44 --- 26
XR15 | ---- --- 12 --- --- 4096 0 | --- 9999 --- --- 193 9999
R21 | 4288 35 40 94 21 --- 24 | 49 36 108 39 --- 38
XR22 | ---- --- 12 --- --- --- 0 | --- 19 --- --- --- 19
R23 | 2095 63 69 433 61 --- 82 | 76 66 375 112 --- 75
R24 |18340 109 54 444 105 --- 92 | 220 198 432 184 --- 192
------+------------------------------------+--------------------------------
RMS | 8314 71 59 221 55 109 |T 82 66 150 81 147 62
WRMS | 8314 66 52 75 55 109 |NE 84 65 305 87 193 66
MEDI | 5052 52 40 83 48 109 |MD 66 55 77 68 101 46
Table 3.1436.1 GPS week: 1436 Day: 1 MJD: 54297
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 3989 83 26 72 36 --- 30 | 88 92 110 120 --- 91
R03E | 3537 64 40 94 62 --- 34 | 52 47 61 34 --- 24
R04E | 5612 114 61 71 43 --- 42 | 115 76 65 68 --- 67
R06E | 2598 45 28 36 40 --- 21 | 29 48 44 59 --- 26
R07E | 6619 59 66 91 35 107 35 | 37 51 60 34 51 33
R08E | 9154 236 96 79 104 --- 80 | 119 68 87 78 --- 40
XR10 | 6017 50 22 --- 53 --- 29 | 57 63 --- 53 --- 55
XR14 | 4915 29 27 --- 40 --- 23 | 26 32 --- 36 --- 19
XR15 | ---- --- 4 --- --- 2393 0 | --- 9999 --- --- 72 9999
R21 | 2832 19 19 86 34 --- 21 | 39 42 69 50 --- 38
XR22 | ---- --- 4 --- --- --- 0 | --- 28 --- --- --- 28
R23 | 3692 66 43 396 81 --- 84 | 46 71 237 75 --- 62
R24 |21988 52 37 360 84 433 77 | 171 164 286 181 2 176
------+------------------------------------+--------------------------------
RMS | 8815 101 51 191 63 315 |T 70 65 113 71 41 54
WRMS | 8815 67 45 79 63 315 |NE 67 66 197 79 37 63
MEDI | 4915 59 28 86 43 433 |MD 52 51 69 59 51 38
Table 3.1436.2 GPS week: 1436 Day: 2 MJD: 54298
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 5448 91 33 70 45 --- 32 | 138 89 79 110 --- 85
R03E | 4502 79 47 117 61 --- 39 | 32 39 94 60 --- 33
R04E | 4482 137 41 70 54 --- 43 | 185 81 70 55 --- 79
R06E | 4002 39 39 64 38 --- 24 | 46 34 60 36 --- 27
R07E | 7145 46 19 59 31 51 20 | 32 44 63 45 41 26
R08E |12825 171 70 103 26 --- 53 | 99 61 70 95 --- 64
XR10 | 5871 35 20 --- 30 --- 19 | 33 53 --- 49 --- 46
XR14 | 4063 33 16 --- 29 --- 18 | 32 25 --- 33 --- 23
XR15 | ---- --- 6 --- --- 1441 0 | --- 513 --- --- 77 512
R21 | 4491 23 32 55 37 --- 20 | 24 43 44 25 --- 25
R23 | 3157 76 37 346 87 --- 71 | 62 58 189 104 --- 47
R24 | 9879 97 46 414 38 --- 79 | 186 245 347 239 --- 223
------+------------------------------------+--------------------------------
RMS | 6906 96 43 193 49 51 |T 79 107 112 77 59 99
WRMS | 6906 58 38 79 49 51 |NE 67 156 193 90 77 146
MEDI | 4502 76 33 70 38 51 |MD 46 53 70 55 41 46
Table 3.1436.3 GPS week: 1436 Day: 3 MJD: 54299
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 5512 143 46 34 62 --- 46 | 84 73 81 63 --- 58
R03E | 4237 68 25 85 54 --- 31 | 61 60 78 79 --- 55
R04E | 3344 165 40 84 71 --- 53 | 198 53 53 65 --- 72
R06E | 3940 29 44 39 44 --- 23 | 30 37 52 47 --- 22
R07E | 5935 40 31 103 23 70 26 | 38 36 50 50 44 29
R08E |16933 86 40 36 32 --- 29 | 105 56 58 62 --- 52
XR10 | 5312 26 31 --- 45 --- 25 | 52 41 --- 54 --- 43
XR14 | 3651 32 12 --- 23 --- 15 | 24 44 --- 25 --- 28
XR15 | ---- --- 7 --- --- 974 0 | --- 570 --- --- 64 569
R21 | 5702 17 43 60 32 --- 22 | 28 47 42 34 --- 24
R23 | 2953 69 39 348 75 --- 76 | 91 55 205 103 --- 56
R24 | 7868 53 54 285 57 --- 63 | 205 243 284 229 --- 226
------+------------------------------------+--------------------------------
RMS | 7454 88 41 161 53 70 |T 83 109 100 73 54 102
WRMS | 7454 57 40 65 53 70 |NE 80 166 177 89 64 157
MEDI | 5312 53 39 84 45 70 |MD 61 53 58 62 44 52
Table 3.1436.4 GPS week: 1436 Day: 4 MJD: 54300
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 4881 544 88 47 92 --- 122 | 341 86 86 94 --- 86
R03E | 5604 153 61 99 38 --- 46 | 121 81 136 90 --- 77
R04E | 4506 117 23 95 54 --- 36 | 237 80 93 96 --- 90
R06E |12364 46 22 57 30 --- 20 | 36 40 78 49 --- 33
R07E | 6076 53 58 70 126 96 47 | 34 42 65 86 43 32
R08E |13279 196 35 92 91 --- 54 | 154 60 98 68 --- 50
XR10 | 3751 25 31 --- 50 --- 26 | 34 38 --- 45 --- 32
XR14 | 2898 31 37 --- 61 --- 32 | 22 35 --- 28 --- 26
XR15 | ---- --- 8 --- --- 1487 0 | --- 9999 --- --- 62 9999
R21 | 7421 28 37 147 77 --- 41 | 34 27 118 49 --- 15
R23 | 2581 98 32 326 80 --- 76 | 72 43 173 56 --- 38
R24 | 4219 76 47 313 57 --- 72 | 160 188 297 192 --- 189
------+------------------------------------+--------------------------------
RMS | 7610 209 49 171 77 96 |T 113 65 127 77 52 60
WRMS | 7610 69 52 92 77 96 |NE 64 66 196 74 62 60
MEDI | 4881 76 35 95 61 96 |MD 72 43 98 68 43 38
Table 3.1436.5 GPS week: 1436 Day: 5 MJD: 54301
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 5314 74 44 69 65 --- 34 | 171 74 83 61 --- 67
R03E | 5318 88 44 56 80 --- 37 | 75 50 106 69 --- 47
R04E | 4594 412 87 83 105 --- 110 | 215 108 77 88 --- 82
R06E |24837 35 31 67 51 --- 25 | 26 43 42 45 --- 27
R07E | 7644 90 66 85 148 79 57 | 35 72 42 85 38 44
R08E | 8582 97 35 68 41 --- 32 | 71 70 64 52 --- 47
XR10 | 3571 43 34 --- 59 --- 32 | 46 59 --- 41 --- 37
XR14 | 2104 37 47 --- 71 --- 38 | 25 39 --- 45 --- 31
XR15 | ---- --- 12 --- --- 2817 0 | --- 9999 --- --- 54 9999
R21 | 7697 54 40 146 38 --- 37 | 55 29 120 29 --- 21
R23 | 3027 80 20 338 95 --- 77 | 62 51 143 71 --- 45
R24 | 2889 63 41 363 67 --- 79 | 126 122 218 127 --- 121
------+------------------------------------+--------------------------------
RMS |10018 154 49 182 83 79 |T 82 65 99 64 46 51
WRMS |10018 77 43 93 83 79 |NE 62 60 160 62 54 51
MEDI | 5314 74 40 83 67 79 |MD 62 59 83 61 38 45
Table 3.1436.6 GPS week: 1436 Day: 6 MJD: 54302
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 4687 52 70 40 32 --- 29 | 110 93 97 100 --- 89
R03E |22810 76 61 68 51 --- 35 | 93 46 63 66 --- 47
R04E | 5556 434 121 125 82 --- 121 | 229 86 78 86 --- 88
R06E |25426 57 92 57 47 --- 38 | 18 41 35 56 --- 32
R07E |14966 41 58 77 55 55 33 | 32 58 64 66 32 36
R08E | 6103 82 48 28 25 --- 27 | 76 73 62 59 --- 51
XR10 | 4084 40 38 --- 29 --- 24 | 29 51 --- 33 --- 24
XR14 | 3447 42 40 --- 36 --- 27 | 22 27 --- 49 --- 31
XR15 | ---- --- 11 --- --- 2606 0 | --- 9999 --- --- 59 9999
R21 | 7054 41 42 60 16 --- 21 | 36 42 48 24 --- 22
R23 | 2308 78 65 430 87 --- 97 | 74 56 322 74 --- 41
R24 | 3852 81 49 339 46 --- 75 | 123 123 354 133 --- 135
------+------------------------------------+--------------------------------
RMS |13127 157 71 193 54 55 |T 76 63 124 67 45 54
WRMS |13127 84 70 85 54 55 |NE 56 59 241 62 59 50
MEDI | 5556 57 49 68 46 55 |MD 74 56 64 66 32 41
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