[IGSREPORT-14942] Wk 1418 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Mar 30 09:05:08 PDT 2007
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IGS Electronic Report 30 Mar 09:05:14 PDT 2007 Message Number 14942
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1418 (Mar 11, 2007 - Mar 17, 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 2.1418.
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:
igl1418[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1418 in the SP3 format.
igl14187.sum Combination Report for GPS Week 1418.
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 | 760.8 ns
1 | 752.7 ns
2 | 793.9 ns
3 | 753.5 ns
4 | 791.1 ns
5 | 806.0 ns
6 | 726.7 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
----+--------+---------------
1 | BKG | R23
4 | BKG | R03
4 | ESX | 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 1.1418, 1a.1418).
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 2.1418.0-6)
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 3.1418.0-6).
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 1418 summary. (Mar 11, 2007 - Mar 17, 2007)
Table 1.1418.a GPS week : 1418 MJD: 54170.0-54176.0
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 0 122 -11 -53 -.12 63 47 | 0 1120 4930 5314
| 0 4 10 72 50 276 .14 | 0 1072
cod 166| 0 -1 5 90 -47 100 -.15 64 45 | --- --- --- ---
| 6 5 9 62 53 117 .18 | --- ---
esx 44| 2 -2 12 230 76 0 -.28 123 55 | 113985 -3073 14941 30003
| 8 2 9 82 106 141 .08 | 653668 13348
iac n/a| 0 0 -9 -244 33 -18 .28 41 41 | 769137 2853 11568 25397
| 4 2 4 27 66 111 .04 | 26602 8081
mcc n/a| -2 -4 -12 -158 -162 1152 1.14 233 233 | --- --- --- ---
| 43 28 74 374 329 1592 1.63 | --- ---
Table 1.1418.b GPS week : 1418 MJD: 54170.0-54176.0
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 | 36 89 47 54 29 19 21 |
R02 | 19 25 16 16 25 15 15 |
R03 | 58 29 40 46 54 69 36 |
R04 | 41 17 35 19 21 21 17 |
R06 | 23 22 20 25 31 18 37 |
R07 | 43 23 24 23 34 25 37 |
R08 | 26 23 27 24 15 30 31 |
R10 | 28 22 28 24 37 28 31 |
R14 | 34 33 22 32 17 25 24 |
R15 | 0 0 0 0 0 0 0 |
R18E | 53 44 48 74 45 129 --- |
R19E | 27 29 22 23 20 23 25 |
R21E | 53 20 27 24 36 57 --- |
R22E | 45 37 31 32 42 108 --- |
R23E | 16 123 159 32 39 87 63 |
R24E | 23 37 37 89 48 92 73 |
Table 1.1418.c GPS week : 1418 MJD: 54170.0-54176.0
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 1418 0 | 304 -204 913 148 -7617 -394900 79.7 6383 6383 | 760791 0
brd 1418 1 | 415 46 763 1124 5538 -388900 88.6 5940 5940 | 752672 0
brd 1418 2 | 70 144 78 2277 3023 -369300 93.1 5979 5979 | 793859 0
brd 1418 3 | 356 -141 -767 5486 5489 -371600 102.3 6753 6753 | 753474 0
brd 1418 4 | -273 215 -477 1870 11910 -354100 82.5 9008 9008 | 791114 0
brd 1418 5 | -354 82 -668 -2217 5422 -360100 98.9 8076 8076 | 805990 0
brd 1418 6 | -655 29 176 97 5261 -351900 83.7 10060 10060 | 726651 0
-------------+------------------------------------------------------------+----------------
brd 1418 mean| -19 24 2 1255 4146 -370114 89.8 7457 7457 | 769221 0
brd 1418 sdev| 413 149 673 2379 5866 16626 8.6 1617 1617 | 28411 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 2.1418.0 GPS week: 1418 Day: 0 MJD: 54170
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 -2 9 45 -30 -278 -.09 66 68 | 0 1008 4309 4574
cod 166| 2 8 11 132 -32 -1 -.15 58 42 | --- --- --- ---
esx 44| -6 -3 5 343 -113 145 -.36 132 75 | -999999 8673 19327 48611
iac n/a| 0 -1 -6 -291 153 19 .24 43 43 | 766564 8499 15436 39653
mcc n/a| -25 -6 10 -590 -4 839 .43 84 84 | --- --- --- ---
Table 2.1418.1 GPS week: 1418 Day: 1 MJD: 54171
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| -3 0 7 71 -70 231 -.25 48 36 | 0 1193 4074 4308
cod 166| 1 -1 -9 2 -10 32 .16 65 56 | --- --- --- ---
esx 44| -4 2 19 164 76 -172 -.36 43 39 | 941828 -8645 14711 21527
iac n/a| 5 3 -13 -246 22 39 .30 43 43 | 753479 -5304 11888 17930
mcc n/a| 3 4 6 -352 185 401 -.25 111 111 | --- --- --- ---
Table 2.1418.2 GPS week: 1418 Day: 2 MJD: 54172
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 1 -4 87 9 93 .05 41 39 | 0 86 4084 4407
cod 166| 6 -2 1 107 -76 75 -.27 62 49 | --- --- --- ---
esx 44| 3 0 19 111 32 -148 -.24 58 40 | 11047 13738 13171 24287
iac n/a| 1 0 -15 -249 91 -12 .34 49 49 | 792295 7661 11574 20133
mcc n/a| 1 0 9 -340 17 416 -.10 156 156 | --- --- --- ---
Table 2.1418.3 GPS week: 1418 Day: 3 MJD: 54173
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 5 3 135 -79 -546 -.15 97 57 | 0 -15 5699 5995
cod 166| -6 0 6 48 -110 251 -.30 57 44 | --- --- --- ---
esx 44| 0 -2 16 316 74 -17 -.27 56 39 | -21837 -11649 18450 37036
iac n/a| -1 -1 -5 -211 7 108 .27 34 34 | 755015 -1994 14703 29834
Table 2.1418.4 GPS week: 1418 Day: 4 MJD: 54174
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 -3 156 31 -40 -.04 55 45 | 0 483 3200 3333
cod 166| -10 -5 20 46 -116 115 -.06 45 43 | --- --- --- ---
esx 44| 0 -3 1 194 226 -66 -.23 178 60 | 868580 9632 9209 34341
iac n/a| 1 0 -5 -231 -37 52 .25 39 39 | 791074 9201 8742 31852
mcc n/a| 75 -43 -132 101 -391 3269 3.91 422 422 | --- --- --- ---
Table 2.1418.5 GPS week: 1418 Day: 5 MJD: 54175
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| -2 3 9 97 51 196 -.35 78 43 | 0 2725 8950 10123
cod 166| -1 -8 0 187 16 -34 -.06 114 45 | --- --- --- ---
esx 44| 16 -5 2 219 79 195 -.32 201 65 | 78417 -19362 20570 23773
iac n/a| 2 0 -12 -219 -11 -205 .24 41 41 | 799484 10940 9822 18740
mcc n/a| -55 -20 85 452 -713 -869 .55 414 414 | --- --- --- ---
Table 2.1418.6 GPS week: 1418 Day: 6 MJD: 54176
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 -7 -20 264 9 -27 -.00 58 41 | 0 2361 4196 4463
cod 166| 3 0 9 111 -2 260 -.35 49 39 | --- --- --- ---
esx 44| 12 -1 26 264 161 60 -.15 195 67 | -80141 -13899 9151 20452
iac n/a| -7 3 -8 -264 7 -133 .31 37 37 | 726051 -9027 8817 19638
mcc n/a| -13 41 -57 -222 -71 2858 2.28 209 209 | --- --- --- ---
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 3.1418.0 GPS week: 1418 Day: 0 MJD: 54170
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9005 95 43 48 48 --- 36 | 42 45 123 48 --- 63
R02 | 6186 35 38 36 23 --- 18 | 44 29 37 43 --- 30
XR03 | ---- --- 65 --- 50 --- 57 | --- 70 --- 58 --- 50
R04 | 3841 38 42 180 33 --- 40 | 44 27 131 36 --- 32
XR06 | 9532 20 40 --- 32 --- 23 | 52 46 --- 44 --- 47
R07 | 4234 46 94 100 59 95 42 | 36 86 112 38 64 45
R08 |12012 46 30 90 30 --- 26 | 40 34 62 43 --- 26
XR10 | 4462 46 28 --- 41 --- 28 | 33 44 --- 56 --- 39
XR14 | 3691 64 57 --- 17 --- 34 | 41 69 --- 33 --- 31
XR15 | ---- --- 11 --- --- --- 0 | --- 488 --- --- --- 488
R18 | 4535 119 60 155 56 --- 52 | 97 138 241 45 --- 145
R19 | 6105 64 39 40 39 --- 27 | 132 153 153 142 --- 139
R21 | 2056 27 57 242 41 --- 52 | 76 56 179 71 --- 56
R22 | 2865 66 86 135 43 72 44 | 57 119 59 29 135 31
XR23 | 3740 25 25 --- 18 --- 16 | 983 9999 --- 9999 --- 9999
XR24 | 4925 36 32 --- 27 204 22 | 9999 9999 --- 9999 908 9999
------+------------------------------------+--------------------------------
RMS | 6382 66 58 132 43 84 |T 129 100 121 52 369 87
WRMS | 6382 68 42 75 43 84 |NE 129 100 121 52 369 87
MEDI | 4462 46 40 100 39 95 |MD 44 56 123 44 135 45
Table 3.1418.1 GPS week: 1418 Day: 1 MJD: 54171
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 141 158 71 --- 89 | --- 109 157 54 --- 64
R02 | 5865 29 80 34 26 --- 25 | 52 52 48 50 --- 36
XR03 | ---- --- 37 --- 21 --- 28 | --- 44 --- 61 --- 52
R04 | 5053 38 31 20 26 --- 17 | 50 32 106 56 --- 46
XR06 |10290 20 47 --- 26 --- 22 | 35 46 --- 38 --- 23
R07 | 2130 30 47 33 47 108 23 | 24 56 53 33 67 30
R08 |10189 39 36 56 13 --- 22 | 39 30 46 32 --- 22
XR10 | 2697 39 29 --- 24 --- 22 | 33 35 --- 37 --- 31
XR14 | 2838 53 54 --- 33 --- 33 | 32 56 --- 30 --- 23
XR15 | ---- --- 6 --- --- --- 0 | --- 433 --- --- --- 434
R18 | 3057 97 81 41 76 --- 44 | 92 107 119 26 --- 98
R19 | 8465 39 57 56 49 --- 29 | 95 107 113 103 --- 100
R21 | 3224 29 35 39 32 --- 19 | 53 77 109 62 --- 64
R22 | 4748 43 111 55 43 114 37 | 63 118 102 36 97 26
XR23 | 3493 519 155 --- 96 --- 122 | 804 9999 --- 9999 --- 9999
XR24 | 3829 59 64 --- 33 206 37 | 9999 9999 --- 9999 820 9999
------+------------------------------------+--------------------------------
RMS | 5939 48 65 43 43 111 |T 114 93 94 47 328 74
WRMS | 5939 36 56 39 43 111 |NE 114 93 94 47 328 74
MEDI | 3829 39 47 41 33 114 |MD 50 56 106 38 97 36
Table 3.1418.2 GPS week: 1418 Day: 2 MJD: 54172
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | 7793 --- 58 86 49 --- 47 | --- 99 127 101 --- 95
R02 | 5828 16 39 21 31 --- 15 | 31 61 34 38 --- 29
XR03 | ---- --- 51 --- 29 --- 40 | --- 65 --- 54 --- 48
R04 | 8073 68 45 47 67 --- 34 | 32 29 69 46 --- 24
XR06 | 6649 31 26 --- 23 --- 19 | 59 39 --- 47 --- 44
R07 | 3900 25 64 48 31 158 24 | 29 39 47 30 152 26
R08 | 6252 21 69 65 24 --- 26 | 29 70 76 41 --- 37
XR10 | 3919 35 26 --- 49 --- 27 | 26 49 --- 73 --- 39
XR14 | 3238 27 40 --- 26 --- 21 | 28 50 --- 35 --- 26
XR15 | ---- --- 10 --- --- --- 0 | --- 771 --- --- --- 773
R18 | 3426 68 73 106 80 --- 47 | 84 131 163 35 --- 130
R19 | 9949 34 36 26 48 --- 21 | 90 96 117 99 --- 96
R21 | 4048 29 67 52 41 --- 27 | 65 109 59 52 --- 74
R22 | 2315 33 86 56 40 153 31 | 33 87 79 34 171 27
XR23 |10381 228 196 --- 239 --- 159 | 9999 9999 --- 9999 --- 9999
XR24 | 5570 48 37 --- 66 471 37 | 9999 9999 --- 9999 828 9999
------+------------------------------------+--------------------------------
RMS | 5978 41 62 58 49 156 |T 46 121 85 52 383 104
WRMS | 5978 39 49 40 49 156 |NE 46 121 85 52 383 104
MEDI | 5570 33 45 52 41 158 |MD 32 65 76 46 171 39
Table 3.1418.3 GPS week: 1418 Day: 3 MJD: 54173
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
XR01 |17500 --- 79 112 40 53 | --- 78 180 67 86
R02 | 5782 22 28 33 24 15 | 53 39 34 36 33
XR03 | ---- --- 64 --- 31 46 | --- 52 --- 65 52
R04 | 9558 48 29 34 21 18 | 42 49 73 40 43
XR06 | 6187 53 42 --- 13 24 | 75 55 --- 44 45
R07 | 5800 29 51 52 22 22 | 41 54 85 38 37
R08 | 4441 42 55 51 22 24 | 56 50 62 47 34
XR10 | 2645 43 45 --- 19 24 | 41 63 --- 47 44
XR14 | 3309 27 63 --- 37 31 | 36 69 --- 27 25
XR15 | ---- --- 18 --- --- 0 | --- 400 --- --- 400
R18 | 5128 242 108 93 68 73 | 124 168 151 37 117
R19 |10452 63 38 32 29 22 | 73 82 74 77 67
R21 | 6805 40 58 41 29 24 | 102 134 86 52 99
R22 | 2192 71 45 77 29 31 | 48 63 86 39 31
XR23 |10594 56 45 --- 37 31 | 727 774 --- 861 801
XR24 | 7544 181 167 --- 43 89 | 797 824 --- 803 800
------+-------------------------------+---------------------------
RMS | 6753 97 57 56 34 |T 170 184 92 152 169
WRMS | 6753 57 44 39 34 |NE 170 184 92 152 169
MEDI | 5800 48 45 51 29 |MD 56 63 85 47 45
Table 3.1418.4 GPS week: 1418 Day: 4 MJD: 54174
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |16487 80 27 63 25 --- 29 | 96 66 70 75 --- 70
R02 | 3596 29 47 44 48 --- 25 | 35 33 54 37 --- 24
XR03 |38700 423 59 --- 48 --- 53 | 24 46 --- 51 --- 28
R04 |10384 43 28 52 22 --- 20 | 65 43 60 26 --- 28
R06 | 2370 42 61 83 26 --- 30 | 69 72 72 53 --- 58
R07 | 5754 58 30 113 31 422 33 | 30 46 115 36 271 38
R08 | 3199 27 29 32 19 --- 15 | 40 52 45 43 --- 33
XR10 | 3898 71 44 --- 38 --- 36 | 54 60 --- 49 --- 32
XR14 | 2929 20 27 --- 24 --- 17 | 44 35 --- 42 --- 31
XR15 | ---- --- 17 --- --- --- 0 | --- 241 --- --- --- 245
XR18 | 6016 --- 62 61 64 --- 44 | --- 210 227 30 --- 180
R19 | 4194 35 42 30 31 --- 20 | 97 122 119 92 --- 102
R21 |16826 54 69 63 59 --- 35 | 167 150 69 87 --- 145
R22 | 4760 83 49 114 49 --- 41 | 83 76 95 30 --- 36
R23 | 6819 67 47 518 51 --- 39 | 924 988 130 982 --- 962
XR24 |10809 92 68 --- 39 --- 47 | 9999 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 9008 55 45 178 39 422 |T 132 149 96 116 271 134
WRMS | 9008 45 43 60 39 422 |NE 132 149 96 116 271 134
MEDI | 5754 54 44 63 38 422 |MD 65 66 72 43 271 38
Table 3.1418.5 GPS week: 1418 Day: 5 MJD: 54175
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4176 37 31 56 20 --- 18 | 68 42 93 43 --- 58
R02 | 2481 24 40 14 16 --- 14 | 39 32 32 47 --- 33
XR03 |43897 136 84 --- 69 --- 68 | 25 50 --- 75 --- 75
R04 | 6899 22 60 37 28 --- 21 | 36 50 56 30 --- 24
R06 | 9544 35 26 50 21 --- 17 | 61 51 40 41 --- 42
R07 | 4320 53 29 70 28 292 24 | 41 39 53 44 128 32
R08 | 2518 54 49 54 49 --- 29 | 68 47 54 63 --- 40
XR10 | 2997 50 44 --- 28 --- 28 | 43 42 --- 51 --- 35
XR14 | 4032 48 26 --- 28 --- 24 | 41 39 --- 31 --- 24
XR15 | ---- --- 12 --- --- --- 0 | --- 184 --- --- --- 184
XR18 |10301 --- 194 376 69 --- 129 | --- 515 491 45 --- 489
R19E | 3054 43 47 52 31 --- 23 | 154 156 161 166 --- 156
XR21 |21118 85 119 --- 46 --- 56 | 111 139 --- 150 --- 90
R22 |12604 160 304 266 64 508 108 | 123 192 89 45 264 61
R23E | 3172 84 86 402 70 --- 86 | 808 882 239 893 --- 867
R24E |16928 132 132 393 46 --- 92 | 9999 9999 118 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 8075 78 114 201 41 414 |T 124 164 129 123 196 147
WRMS | 8075 43 45 65 41 414 |NE 59 109 113 55 196 91
MEDI | 4320 50 47 56 31 292 |MD 61 50 89 45 128 58
Table 3.1418.6 GPS week: 1418 Day: 6 MJD: 54176
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7244 50 25 50 28 --- 20 | 54 51 52 47 --- 45
R02 | 3207 26 27 40 18 --- 14 | 40 37 47 44 --- 35
XR03 | ---- --- 42 --- 30 --- 36 | --- 40 --- 47 --- 49
R04 | 3448 28 29 69 16 --- 17 | 47 30 76 27 --- 25
R06 |12622 58 76 54 58 --- 37 | 74 111 31 61 --- 65
XR07 |29499 --- 63 66 37 288 36 | --- 35 66 39 166 31
R08 | 7451 63 48 92 37 --- 30 | 69 42 69 62 --- 39
XR10 | 2609 52 32 --- 45 --- 30 | 38 51 --- 66 --- 44
XR14 | 4492 44 31 --- 28 --- 23 | 27 56 --- 27 --- 29
XR15 | ---- --- 17 --- --- --- 0 | --- 220 --- --- --- 220
R19E | 4309 53 36 65 38 --- 25 | 165 164 173 163 --- 161
R23E | 3467 65 57 351 33 --- 62 | 9999 9999 189 9999 --- 9999
R24E |22116 95 65 398 45 209 73 | 9999 9999 148 9999 9999 9999
------+------------------------------------+--------------------------------
RMS |10057 58 49 195 37 209 |T 64 76 94 58 192 67
WRMS |10057 41 39 67 37 209 |NE 49 67 56 46 166 58
MEDI | 4492 52 36 66 33 209 |MD 47 51 69 47 166 44
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