[IGSREPORT-16829] Wk 1503 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Nov 13 07:29:04 PST 2008
******************************************************************************
IGS Electronic Report 13 Nov 07:29:17 PST 2008 Message Number 16829
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1503 (Oct 26, 2008 - Nov 01, 2008)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
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 2.1503.
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:
igl1503[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1503 in the SP3 format.
igl15037.sum Combination Report for GPS Week 1503.
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 | 513.8 ns
1 | 491.2 ns
2 | 488.0 ns
3 | 553.6 ns
4 | 496.3 ns
5 | 500.8 ns
6 | 570.1 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 | ESX | R18
2 | ESX | R18
3 | ESX | R18
4 | ESX | R18
5 | BKG | 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 1.1503, 1a.1503).
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 2.1503.0-6)
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 3.1503.0-6).
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 1503 summary. (Oct 26, 2008 - Nov 01, 2008)
Table 1.1503.a GPS week : 1503 MJD: 54765.0-54771.0
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 63| 0 0 4 4 24 0 -.10 33 29 | 0 25 2576 2670
| 3 2 4 48 51 109 .06 | 0 259
cod 240| -2 1 3 -14 -14 35 -.11 24 23 | --- --- --- ---
| 2 1 2 34 45 75 .04 | --- ---
esx 128| 2 0 0 41 42 39 .46 68 67 | 121715 -824 7055 23834
| 1 3 5 48 58 48 .09 | 24429 5800
iac n/a| 1 0 -8 -23 -4 -54 -.08 26 26 | 517927 -618 5881 12250
| 2 2 5 40 33 50 .08 | 31268 3610
mcc n/a| 0 -3 30 80 -18 190 -.34 339 339 | --- --- --- ---
| 16 10 18 276 242 877 .51 | --- ---
Table 1.1503.b GPS week : 1503 MJD: 54765.0-54771.0
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
------+------------------------------------+------------------------------------------
R04 | 16 17 17 16 11 15 16 |
R06 | 15 14 15 25 21 40 25 |
R07 | 10 12 16 24 18 16 15 |
R09 | 0 --- --- 0 --- 0 0 |
R10 | 12 15 11 19 16 11 14 |
R11 | 22 18 15 17 16 15 22 |
R13 | 19 15 17 12 22 21 17 |
R14 | 13 9 12 11 14 14 12 |
R15 | 17 15 15 15 12 11 14 |
R17 | 14 17 15 17 18 22 18 |
R18 | 19 15 11 20 19 50 46 |
R19 | 12 12 13 24 18 14 15 |
R20 | 14 16 12 12 12 14 14 |
R21 | --- 0 0 0 79 236 154 |
R23 | 22 15 14 21 23 28 --- |
R24 | 18 14 18 24 14 14 17 |
Table 1.1503.c GPS week : 1503 MJD: 54765.0-54771.0
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 1503 0 | -25 67 96 -223 311 -14650 94.2 2721 2721 | 513761 0
brd 1503 1 | -11 -155 -34 877 -3944 -16980 90.8 2330 2330 | 491202 0
brd 1503 2 | 55 -209 -82 696 -2756 -25030 89.8 3191 3191 | 488038 0
brd 1503 3 | 10 0 173 -4983 -4981 -22230 93.7 5067 5067 | 553570 0
brd 1503 4 | -42 -41 140 174 1349 -8795 89.1 5456 5456 | 496309 0
brd 1503 5 | -187 45 -38 910 -2979 -11970 92.1 6715 6715 | 500760 0
brd 1503 6 | -178 -134 0 3067 2193 -8129 99.5 8351 8351 | 570146 0
-------------+------------------------------------------------------------+----------------
brd 1503 mean| -54 -61 36 74 -1543 -15397 92.7 4833 4833 | 516255 0
brd 1503 sdev| 93 106 99 2461 2795 6464 3.5 2227 2227 | 32569 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 2.1503.0 GPS week: 1503 Day: 0 MJD: 54765
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 63| -4 0 6 85 96 170 -.09 37 33 | 0 311 2287 2407
cod 240| -4 1 1 -83 2 -85 -.14 24 23 | --- --- --- ---
esx 128| 1 -1 -5 4 21 3 .44 29 29 | 116301 3416 6118 23081
iac n/a| 0 -1 1 20 -9 28 -.21 22 22 | 514621 -799 5290 8767
mcc n/a| -1 -12 56 554 122 1349 -.01 476 476 | --- --- --- ---
Table 2.1503.1 GPS week: 1503 Day: 1 MJD: 54766
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 63| 4 1 9 -21 -36 -38 -.11 28 25 | 0 -158 2467 2608
cod 240| -2 -1 0 16 19 42 -.13 19 18 | --- --- --- ---
esx 128| 3 -1 1 61 44 69 .54 82 264 | 109894 -5575 6181 15619
iac n/a| 0 4 -10 -65 -20 -88 -.01 22 22 | 495659 -3866 6207 13679
mcc n/a| 28 -19 50 60 -379 781 -1.10 345 345 | --- --- --- ---
Table 2.1503.2 GPS week: 1503 Day: 2 MJD: 54767
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 63| -1 -4 1 -48 -15 -58 -.10 32 33 | 0 -266 3156 3199
cod 240| -2 1 5 17 59 117 -.17 19 19 | --- --- --- ---
esx 128| 4 -2 2 78 30 -8 .39 72 33 | 103411 486 6719 16734
iac n/a| 0 0 -7 -40 -1 -42 -.05 20 20 | 491494 -1894 6749 14971
mcc n/a| 3 7 42 -275 44 -433 -.73 416 416 | --- --- --- ---
Table 2.1503.3 GPS week: 1503 Day: 3 MJD: 54768
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 63| -1 -2 1 -37 7 -145 -.05 33 31 | 0 121 2483 2537
cod 240| 1 4 6 -11 -25 40 -.11 23 20 | --- --- --- ---
esx 128| 2 1 -1 70 -11 53 .35 87 38 | 159311 1258 10053 33183
iac n/a| -1 -2 -7 -38 17 -38 .05 30 30 | 557428 -3075 5549 12305
mcc n/a| -10 -6 9 -220 194 -1356 -.52 379 379 | --- --- --- ---
Table 2.1503.4 GPS week: 1503 Day: 4 MJD: 54769
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 63| 5 2 0 35 41 3 -.20 29 27 | 0 407 2112 2236
cod 240| -4 2 3 -20 -72 26 -.05 27 24 | --- --- --- ---
esx 128| 1 -3 6 -33 27 -12 .42 82 33 | 111212 1518 4758 15339
iac n/a| 5 -2 -11 5 42 -22 -.09 25 25 | 497713 2506 4773 11546
mcc n/a| -1 -3 27 176 132 110 .11 374 374 | --- --- --- ---
Table 2.1503.5 GPS week: 1503 Day: 5 MJD: 54770
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 63| 0 2 0 -13 -9 -52 -.02 38 27 | 0 -54 3096 3169
cod 240| 1 2 6 -2 -34 130 -.15 27 28 | --- --- --- ---
esx 128| 3 3 2 101 169 46 .51 60 32 | 98395 -11687 8941 34582
iac n/a| 0 0 -13 -72 -64 -110 -.11 36 36 | 501453 -3186 7416 13742
mcc n/a| 9 4 10 101 109 522 .34 235 235 | --- --- --- ---
Table 2.1503.6 GPS week: 1503 Day: 6 MJD: 54771
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 63| 1 -1 9 31 84 117 -.11 31 28 | 0 -181 2435 2538
cod 240| -2 2 2 -21 -52 -21 -.07 26 26 | --- --- --- ---
esx 128| 1 4 -8 7 12 122 .59 62 40 | 153482 4811 6619 28306
iac n/a| 3 -3 -7 27 5 -106 -.11 29 29 | 567126 5986 5185 10742
mcc n/a| -25 7 22 168 -355 361 -.48 148 148 | --- --- --- ---
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 3.1503.0 GPS week: 1503 Day: 0 MJD: 54765
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 903 43 25 27 17 --- 16 | 25 60 62 42 --- 44
R06 | 2975 23 30 22 23 --- 14 | 40 43 46 38 --- 36
R07 | 2991 22 17 14 12 --- 9 | 24 34 34 21 --- 25
XR09 |11393 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2448 20 13 26 21 --- 12 | 39 53 56 51 --- 48
R11 | 2447 47 15 56 25 166 21 | 38 80 99 57 60 69
R13 | 6580 57 27 32 17 --- 19 | 77 122 130 115 --- 109
R14 | 2128 18 27 24 21 --- 13 | 24 27 40 34 --- 26
R15 | 1496 38 33 24 20 125 16 | 61 80 75 79 41 72
R17 | 2716 30 28 24 15 --- 14 | 41 51 66 56 --- 51
XR18 | 4380 30 24 --- 25 --- 18 | 107 112 --- 108 --- 110
R19 | 1098 20 17 29 15 --- 12 | 94 74 77 83 --- 79
R20 | 1721 30 25 17 23 --- 13 | 33 45 50 34 --- 38
R23 | 1433 53 24 40 34 --- 21 | 55 83 77 68 --- 90
R24 | 1395 45 24 22 33 797 18 | 120 140 141 135 269 133
------+------------------------------------+--------------------------------
RMS | 2720 37 24 29 22 476 |T 55 71 73 65 123 66
WRMS | 2720 33 23 29 22 476 |NE 55 71 73 65 123 66
MEDI | 2447 30 24 24 21 166 |MD 40 60 66 56 60 51
Table 3.1503.1 GPS week: 1503 Day: 1 MJD: 54766
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1214 34 14 50 20 --- 17 | 24 32 64 36 --- 30
R06 | 4870 25 20 33 17 --- 13 | 41 47 63 53 --- 46
R07 | 3003 21 18 27 17 --- 12 | 22 30 41 27 --- 24
R10 | 2428 21 19 41 25 --- 15 | 33 39 30 38 --- 27
R11 | 1177 38 21 38 26 201 17 | 73 59 63 48 44 51
R13 | 1787 31 16 23 30 --- 14 | 136 129 137 132 --- 132
R14 | 1466 17 11 16 15 --- 8 | 31 30 35 28 --- 28
R15 | 1814 36 25 15 21 134 14 | 68 64 59 78 38 65
R17 | 2016 29 22 49 16 --- 17 | 21 30 58 46 --- 28
R18 | 2782 28 20 286 12 --- 15 | 99 92 200 107 --- 100
R19 | 908 29 14 24 16 --- 12 | 65 48 65 47 --- 53
R20 | 1445 18 28 26 32 --- 15 | 24 48 41 21 --- 29
XR21 | ---- --- 3 --- --- --- 0 | --- 422 --- --- --- 419
R23 | 1719 23 16 28 34 --- 15 | 31 61 31 62 --- 66
R24 | 2862 35 17 29 18 547 14 | 90 126 123 126 133 116
------+------------------------------------+--------------------------------
RMS | 2330 28 19 82 22 345 |T 54 83 72 60 71 80
WRMS | 2330 25 18 264 22 345 |NE 54 83 72 60 71 80
MEDI | 1787 28 18 28 18 201 |MD 33 48 59 47 44 51
Table 3.1503.2 GPS week: 1503 Day: 2 MJD: 54767
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1132 43 26 30 19 --- 16 | 22 49 69 33 --- 40
R06 | 4438 28 16 37 22 --- 14 | 32 40 64 37 --- 37
R07 | 2527 44 23 20 19 --- 15 | 18 28 33 35 --- 24
R10 | 2364 13 16 21 21 --- 10 | 27 32 25 29 --- 23
R11 | 1129 17 19 41 20 92 14 | 44 49 59 35 56 41
R13 | 2721 52 19 21 23 --- 17 | 64 74 86 75 --- 71
R14 | 1288 29 16 23 16 --- 12 | 42 20 28 33 --- 23
R15 | 7416 35 24 26 19 47 14 | 45 55 62 65 45 55
R17 | 2086 42 19 22 22 --- 15 | 28 51 62 55 --- 47
R18 | 3457 23 8 245 13 --- 10 | 73 95 144 93 --- 88
R19 | 1010 19 20 29 23 --- 13 | 84 75 65 75 --- 71
R20 | 1209 22 20 22 20 --- 12 | 25 35 37 26 --- 25
XR21 | ---- --- 8 --- --- --- 0 | --- 336 --- --- --- 340
R23 | 2707 27 21 28 17 --- 13 | 58 55 40 28 --- 54
R24 | 4255 29 15 53 26 713 18 | 188 182 208 187 232 187
------+------------------------------------+--------------------------------
RMS | 3190 32 19 72 20 416 |T 53 78 70 57 111 75
WRMS | 3190 33 19 33 20 416 |NE 53 78 70 57 111 75
MEDI | 2364 28 19 26 20 92 |MD 42 51 62 35 56 47
Table 3.1503.3 GPS week: 1503 Day: 3 MJD: 54768
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 886 22 28 43 21 --- 16 | 35 50 56 35 --- 36
R06 | 9195 35 30 73 40 --- 24 | 58 60 105 68 --- 61
R07 | 1857 44 26 69 34 --- 24 | 41 38 81 26 --- 33
XR09 |16440 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1525 19 26 45 42 --- 19 | 26 28 53 46 --- 28
R11 | 3809 32 19 50 18 108 16 | 62 40 71 39 116 43
R13 |11314 19 11 13 31 --- 11 | 113 114 124 118 --- 115
R14 | 1136 19 17 17 23 --- 11 | 27 35 38 33 --- 29
R15 | 3375 23 18 26 36 119 15 | 48 39 51 73 96 48
R17 | 6299 41 18 26 27 --- 16 | 33 56 60 64 --- 49
R18 | 6840 28 21 273 35 --- 20 | 51 57 121 86 --- 60
R19 | 1983 49 17 78 23 --- 24 | 43 65 119 54 --- 61
R20 | 924 17 18 18 27 --- 12 | 24 27 35 45 --- 27
XR21 | ---- --- 5 --- --- --- 0 | --- 364 --- --- --- 366
R23 | 2958 34 21 68 28 --- 21 | 54 51 85 50 --- 49
R24 | 3617 55 35 46 27 637 23 | 79 133 147 98 491 110
------+------------------------------------+--------------------------------
RMS | 5067 33 23 87 30 379 |T 49 77 81 59 234 74
WRMS | 5067 31 20 38 30 379 |NE 49 77 81 59 234 74
MEDI | 3375 28 19 45 27 119 |MD 43 51 71 50 116 49
Table 3.1503.4 GPS week: 1503 Day: 4 MJD: 54769
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 625 18 15 27 12 --- 10 | 43 44 51 43 --- 41
R06 |11904 36 38 35 33 --- 20 | 56 67 69 38 --- 47
R07 | 1488 42 23 31 26 --- 18 | 39 33 25 40 --- 27
R10 | 1849 22 32 21 28 --- 15 | 35 35 46 54 --- 37
R11 | 5591 23 35 36 14 126 16 | 43 44 78 27 62 41
R13 | 6541 26 18 65 33 --- 22 | 53 49 66 44 --- 41
R14 | 817 23 19 25 25 --- 13 | 37 28 39 40 --- 32
R15 | 3574 26 20 19 15 58 11 | 31 29 48 43 53 34
R17 | 8146 33 23 21 39 --- 17 | 54 63 47 57 --- 51
R18 | 9976 26 32 281 18 --- 18 | 72 97 151 85 --- 86
R19 | 2472 35 33 35 19 --- 17 | 103 80 127 85 --- 94
R20 | 963 18 20 15 25 --- 11 | 25 31 31 42 --- 28
XR21 |14593 --- 82 --- 76 --- 79 | --- 241 --- 100 --- 265
R23 | 1671 43 35 56 22 --- 22 | 103 93 62 42 --- 98
R24 | 2408 17 26 32 19 632 13 | 161 168 145 163 497 160
------+------------------------------------+--------------------------------
RMS | 5456 29 27 82 25 373 |T 61 73 70 60 204 72
WRMS | 5456 27 24 33 25 373 |NE 61 73 70 60 204 72
MEDI | 2472 26 26 31 25 126 |MD 43 49 51 43 62 41
Table 3.1503.5 GPS week: 1503 Day: 5 MJD: 54770
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |11884 29 27 23 22 --- 15 | 44 37 41 46 --- 40
R06 |13939 107 31 90 36 --- 40 | 96 85 128 55 --- 70
R07 | 1837 19 16 39 34 --- 15 | 21 33 57 32 --- 18
XR09 |20954 --- --- 15 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1960 19 17 14 20 --- 10 | 25 29 36 36 --- 26
R11 | 4561 19 24 32 28 136 14 | 19 28 36 26 57 19
R13 | 6952 37 26 52 29 --- 20 | 85 104 105 117 --- 98
R14 | 1234 32 13 25 23 --- 13 | 28 25 32 27 --- 20
R15 | 5057 27 17 16 14 79 11 | 42 33 38 44 33 35
R17 | 8523 30 34 34 48 --- 21 | 41 49 47 43 --- 30
R18 | 7808 27 58 168 75 --- 49 | 69 72 128 71 --- 64
R19 | 2524 18 18 26 35 --- 14 | 66 83 107 91 --- 81
R20 | 1694 14 19 27 34 --- 14 | 47 38 70 65 --- 50
XR21 |13183 --- 202 --- 275 --- 235 | --- 390 --- 121 --- 295
XR23 | 4932 743 16 --- 38 --- 27 | 135 242 --- 48 --- 243
R24 | 2087 18 17 34 27 374 13 | 96 91 126 101 196 98
------+------------------------------------+--------------------------------
RMS | 6715 38 27 60 36 234 |T 58 89 73 61 95 79
WRMS | 6715 27 28 32 36 234 |NE 58 89 73 61 95 79
MEDI | 4932 27 19 27 34 136 |MD 44 49 57 48 57 50
Table 3.1503.6 GPS week: 1503 Day: 6 MJD: 54771
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |16385 34 27 15 28 --- 16 | 39 45 47 42 --- 41
R06 |16566 54 41 46 26 --- 24 | 61 107 101 70 --- 76
R07 | 5153 25 26 34 21 --- 15 | 30 42 32 23 --- 25
XR09 |14430 --- --- 12 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2511 26 20 38 18 --- 14 | 50 45 49 58 --- 48
R11 | 8084 41 30 58 26 157 21 | 44 27 42 34 50 25
R13 | 6528 22 22 46 30 --- 16 | 89 89 88 90 --- 85
R14 | 1633 13 14 39 15 --- 11 | 23 29 38 40 --- 28
R15 | 5378 20 20 42 19 113 14 | 48 42 43 61 40 45
R17 |10175 25 27 18 41 --- 17 | 53 54 47 54 --- 49
R18 | 8557 35 37 181 53 --- 45 | 88 105 171 82 --- 98
R19 | 2779 30 14 30 30 --- 15 | 77 82 97 86 --- 82
R20 | 1019 22 15 33 26 --- 13 | 35 44 44 50 --- 41
XR21 | 9185 --- 141 --- 168 --- 154 | --- 369 --- 161 --- 358
R24 | 2388 36 24 32 24 170 16 | 97 112 121 119 254 109
------+------------------------------------+--------------------------------
RMS | 8351 31 26 62 29 148 |T 56 85 70 69 114 79
WRMS | 8351 28 26 40 29 148 |NE 56 85 70 69 114 79
MEDI | 6528 26 24 34 26 157 |MD 50 45 47 58 50 48
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