[IGSREPORT-17828] Wk 1548 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Sep 24 04:45:28 PDT 2009
******************************************************************************
IGS Electronic Report 24 Sep 04:46:06 PDT 2009 Message Number 17828
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1548 (Sep 06, 2009 - Sep 12, 2009)
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 2.1548.
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:
igl1548[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1548 in the SP3 format.
igl15487.sum Combination Report for GPS Week 1548.
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 | 223.3 ns
1 | 222.8 ns
2 | 169.3 ns
3 | 150.7 ns
4 | 230.4 ns
5 | 224.2 ns
6 | 229.4 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 1.1548, 1a.1548).
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 2.1548.0-6)
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 3.1548.0-6).
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 1548 summary. (Sep 06, 2009 - Sep 12, 2009)
Table 1.1548.a GPS week : 1548 MJD: 55080.0-55086.0
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 109| 0 -1 -4 20 -1 45 -.17 32 32 | 0 336 3812 4364
| 2 2 2 27 18 126 .07 | 0 1099
cod 230| -1 0 0 21 -5 115 -.15 17 15 | --- --- --- ---
| 1 1 1 15 15 42 .03 | --- ---
esx 137| 0 0 7 -35 40 -30 .44 36 27 | 125217 -1851 7200 11237
| 3 1 2 34 33 42 .05 | 38821 5457
iac n/a| 2 0 -3 -11 -14 -190 -.02 30 30 | 207653 -1480 6933 10817
| 1 2 6 23 19 67 .06 | 32760 4259
mcc n/a| 2 2 46 12 10 497 .08 104 104 | --- --- --- ---
| 6 4 4 38 103 459 .29 | --- ---
Table 1.1548.b GPS week : 1548 MJD: 55080.0-55086.0
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
------+------------------------------------+------------------------------------------
R02 | 22 12 12 13 13 15 15 |
R03 | 17 10 47 15 13 10 13 |
R07 | 11 13 11 11 17 12 17 |
R08 | 12 15 13 10 8 11 13 |
R10 | 12 13 11 22 12 10 11 |
R11 | 14 13 16 15 13 14 16 |
R13 | 11 12 13 8 11 10 12 |
R14 | 12 11 11 11 8 12 10 |
R15 | 12 15 11 37 13 10 10 |
R17 | 18 15 16 14 14 15 17 |
R18 | 18 12 19 19 20 18 21 |
R19 | 24 23 24 20 18 19 20 |
R20 | 26 24 22 18 24 21 20 |
R21 | 15 17 20 17 18 18 14 |
R23 | 19 18 21 22 20 20 16 |
R24 | 10 10 12 20 13 9 11 |
Table 1.1548.c GPS week : 1548 MJD: 55080.0-55086.0
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 1548 0 | 87 211 17 -2402 3859 10620 91.9 5517 5517 | 223287 0
brd 1548 1 |29840 ---- 1274 -72530 -16059 469800 114.0 >>>>> >>>>> | 222818 0
brd 1548 2 | 111 279 226 3592 4630 1229 100.0 4542 4542 | 169345 0
brd 1548 3 | -59 316 377 -3255 1699 -13510 86.2 3794 3794 | 150732 0
brd 1548 4 | -47 249 481 1872 3115 -17030 81.4 3925 3925 | 230368 0
brd 1548 5 | 99 -77 429 -677 1609 -19720 88.5 3969 3969 | 224200 0
brd 1548 6 | -142 110 182 -3850 -2765 -16810 92.5 3620 3620 | 229370 0
-------------+------------------------------------------------------------+----------------
brd 1548 mean| 4269 -3174 427 -11035 -558 59225 93.5 >>>>> >>>>> | 207160 0
brd 1548 sdev|11275 8880 406 27252 7244 181391 10.7 >>>>> >>>>> | 32765 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 2.1548.0 GPS week: 1548 Day: 0 MJD: 55080
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 109| 2 3 -3 40 -11 -105 -.22 34 35 | 0 -402 3722 4260
cod 230| 0 0 0 0 -3 140 -.13 14 12 | --- --- --- ---
esx 137| -4 1 10 -47 38 -21 .46 33 30 | 148788 -5152 11000 14899
iac n/a| 0 -1 -4 9 -10 -196 .09 34 34 | 224697 -7970 10685 14092
mcc n/a| -4 3 48 -16 -88 338 .05 97 97 | --- --- --- ---
Table 2.1548.1 GPS week: 1548 Day: 1 MJD: 55081
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 109| 2 -1 -1 -7 -5 145 -.26 35 31 | 0 469 3572 4085
cod 230| 0 0 -2 39 -16 39 -.21 16 15 | --- --- --- ---
esx 137| -2 -2 4 -36 35 -13 .39 23 21 | 136153 3739 5367 11700
iac n/a| 5 2 -5 -5 -18 -216 .02 31 31 | 222847 4149 5207 11763
mcc n/a| 11 1 52 -27 -100 53 .04 82 82 | --- --- --- ---
Table 2.1548.2 GPS week: 1548 Day: 2 MJD: 55082
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 109| 2 -1 -8 50 4 169 -.21 40 40 | 0 165 3704 4296
cod 230| 0 2 0 25 -27 158 -.14 20 17 | --- --- --- ---
esx 137| 1 -2 8 -74 49 -102 .43 53 28 | 83713 -6443 6699 9712
iac n/a| 2 1 1 1 2 -154 -.03 27 27 | 170254 -1197 6595 9758
mcc n/a| 0 8 37 48 77 756 .44 89 89 | --- --- --- ---
Table 2.1548.3 GPS week: 1548 Day: 3 MJD: 55083
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 109| -2 -4 -3 45 -20 146 -.12 31 31 | 0 -38 3127 3450
cod 230| 0 1 -1 10 0 96 -.12 16 13 | --- --- --- ---
esx 137| 3 1 2 -68 94 -74 .51 62 45 | 57252 -4475 7830 10244
iac n/a| 0 -3 3 -20 -35 -154 -.04 32 32 | 150781 -2983 7154 9492
mcc n/a| 0 4 43 -7 149 1261 -.13 114 114 | --- --- --- ---
Table 2.1548.4 GPS week: 1548 Day: 4 MJD: 55084
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 109| 2 -3 -1 24 18 30 -.11 29 29 | 0 -1291 4605 5033
cod 230| -4 2 3 24 -7 153 -.16 20 15 | --- --- --- ---
esx 137| 1 0 6 -27 20 13 .41 25 17 | 140127 7900 6920 9583
iac n/a| 1 1 -16 -4 -23 -284 -.09 31 31 | 229463 2039 6658 9114
mcc n/a| 0 1 50 35 116 800 -.41 142 142 | --- --- --- ---
Table 2.1548.5 GPS week: 1548 Day: 5 MJD: 55085
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 109| 0 -1 -4 -20 23 78 -.07 27 27 | 0 1670 4220 4916
cod 230| -1 -1 -1 8 -3 89 -.19 15 13 | --- --- --- ---
esx 137| 2 1 9 29 -15 -18 .51 27 23 | 155303 -5224 7180 11390
iac n/a| 0 -1 -4 -59 18 -246 -.06 33 33 | 227426 -5308 6972 11113
mcc n/a| 0 2 44 -16 -1 -8 .24 99 99 | --- --- --- ---
Table 2.1548.6 GPS week: 1548 Day: 6 MJD: 55086
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 109| -1 0 -6 10 -21 -147 -.17 29 29 | 0 1783 3738 4512
cod 230| -1 0 -2 39 21 128 -.14 18 17 | --- --- --- ---
esx 137| -2 2 9 -20 61 5 .39 30 28 | 155185 -3307 5410 11133
iac n/a| 2 0 -1 1 -33 -81 -.03 26 26 | 228106 905 5260 10393
mcc n/a| 11 -5 49 71 -75 280 .30 103 103 | --- --- --- ---
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 3.1548.0 GPS week: 1548 Day: 0 MJD: 55080
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 2789 --- --- 17 25 --- 22 | --- --- 28 42 --- 30
R03 | 5658 26 20 43 31 --- 16 | 53 61 76 49 --- 57
R07 | 2712 27 9 22 24 --- 11 | 27 39 53 36 --- 36
R08 | 4029 20 10 24 32 77 11 | 29 35 31 31 42 30
R10 | 2840 20 9 29 32 --- 12 | 24 23 37 33 --- 22
R11 | 2591 18 13 31 37 92 13 | 38 29 43 28 40 28
R13 | 5173 31 14 16 18 --- 11 | 30 28 38 23 --- 28
R14 | 2156 35 10 25 14 --- 11 | 38 24 29 24 --- 24
R15 | 4547 26 10 23 27 63 11 | 24 23 31 30 40 21
R17E | 2463 45 16 27 43 --- 17 | 31 26 42 34 --- 25
R18E | 1851 26 14 40 47 --- 17 | 42 47 50 55 --- 45
XR19E | 1679 54 19 --- 39 --- 24 | 20 21 --- 44 --- 21
R20E | 4733 68 18 61 50 --- 26 | 30 34 57 61 --- 33
R21E | 2152 35 10 24 37 --- 14 | 26 29 37 39 --- 27
R23E |16082 45 19 39 41 140 19 | 47 40 55 44 85 33
R24E | 2896 17 10 25 17 --- 9 | 56 69 59 52 --- 60
------+------------------------------------+--------------------------------
RMS | 5516 34 14 33 34 97 |T 34 35 44 39 51 32
WRMS | 5516 35 12 30 34 97 |NE 32 32 40 32 40 30
MEDI | 2789 27 13 25 32 77 |MD 30 29 42 36 40 28
Table 3.1548.1 GPS week: 1548 Day: 1 MJD: 55081
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 |>>>>> 18 --- 16 17 --- 12 | 18 --- 37 28 --- 27
R03 |>>>>> 14 16 19 18 --- 9 | 63 63 145 71 --- 80
R07 |>>>>> 31 14 18 28 --- 12 | 42 38 33 25 --- 32
R08 |>>>>> 31 16 27 32 74 14 | 32 18 28 17 55 15
R10 |34347 24 17 20 33 --- 13 | 34 25 55 45 --- 32
R11 |>>>>> 25 16 20 27 76 12 | 28 21 28 32 61 20
R13 |>>>>> 26 17 18 23 --- 11 | 27 34 37 22 --- 28
R14 |>>>>> 16 12 13 32 --- 10 | 39 32 39 40 --- 34
R15 |>>>>> 48 8 21 26 70 15 | 30 18 43 25 43 20
R17E |>>>>> 37 19 22 32 --- 15 | 30 26 42 32 --- 26
R18E |>>>>> 21 15 19 30 --- 12 | 31 38 43 46 --- 34
XR19E |>>>>> 37 27 --- 36 --- 22 | 25 22 --- 54 --- 25
R20E |>>>>> 70 19 37 43 --- 23 | 42 26 46 42 --- 26
R21E |>>>>> 44 15 27 38 --- 17 | 48 37 59 59 --- 44
R23E |>>>>> 33 19 35 40 103 17 | 25 39 30 37 51 23
R24E |>>>>> 20 11 15 28 --- 10 | 42 52 65 43 --- 49
------+------------------------------------+--------------------------------
RMS |>>>>> 35 16 23 31 82 |T 34 32 48 38 52 32
WRMS |>>>>> 31 15 21 31 82 |NE 34 31 49 33 53 32
MEDI |>>>>> 26 16 20 30 74 |MD 31 32 42 37 51 27
Table 3.1548.2 GPS week: 1548 Day: 2 MJD: 55082
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 3621 23 --- 12 13 --- 11 | 19 --- 41 40 --- 36
R03 | 5072 60 37 174 24 --- 47 | 36 52 181 50 --- 70
R07 | 3179 28 15 21 17 --- 11 | 22 30 47 33 --- 30
R08 | 1527 15 16 23 29 65 12 | 23 29 36 29 27 24
R10 | 1777 29 13 15 18 --- 10 | 27 22 34 28 --- 23
R11 | 6908 40 21 24 26 110 15 | 38 34 54 38 32 35
R13 | 2063 26 19 31 15 --- 12 | 30 27 48 26 --- 27
R14 | 6298 23 11 23 19 --- 10 | 23 24 25 17 --- 16
R15 | 4954 20 8 27 19 81 10 | 20 31 70 31 29 31
R17E | 1346 34 20 24 30 --- 15 | 41 32 28 34 --- 28
R18E | 4425 58 19 18 33 --- 19 | 34 40 34 57 --- 36
XR19E | 1022 46 26 --- 33 --- 24 | 19 31 --- 40 --- 25
R20E | 4779 45 20 53 41 --- 22 | 22 23 42 53 --- 28
R21E | 2600 57 26 20 30 --- 19 | 41 25 44 43 --- 29
R23E | 8380 54 27 35 36 92 21 | 28 37 55 44 42 32
R24E | 3168 20 13 13 30 --- 12 | 72 76 54 81 --- 73
------+------------------------------------+--------------------------------
RMS | 4541 40 20 53 27 89 |T 30 34 52 40 32 33
WRMS | 4541 40 17 28 27 89 |NE 26 31 59 32 29 32
MEDI | 3179 29 19 23 26 81 |MD 27 31 44 38 29 29
Table 3.1548.3 GPS week: 1548 Day: 3 MJD: 55083
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 3951 18 --- 19 15 --- 12 | 16 --- 27 28 --- 21
R03 | 2874 25 6 27 42 --- 14 | 58 64 34 76 --- 54
R07 | 3531 19 11 27 22 --- 10 | 32 30 37 33 --- 29
R08 | 1599 15 11 11 27 68 9 | 39 33 36 27 33 31
R10 | 1821 36 8 91 27 --- 22 | 27 27 86 39 --- 33
R11 | 5352 35 15 30 31 161 15 | 40 29 55 41 56 33
R13 | 2403 17 6 21 13 --- 7 | 18 21 31 30 --- 21
R14 | 6157 27 11 16 20 --- 10 | 48 41 38 38 --- 40
R15 | 4149 26 24 167 34 101 36 | 34 27 129 24 22 27
R17E | 4158 17 14 16 40 --- 13 | 25 42 39 45 --- 34
R18E | 2535 50 16 34 36 --- 19 | 35 33 49 65 --- 37
XR19E | 1031 41 19 --- 27 --- 19 | 46 26 --- 33 --- 29
R20E | 6803 38 23 37 32 --- 17 | 31 40 39 48 --- 31
R21E | 1592 33 18 42 36 --- 17 | 32 37 34 60 --- 37
R23E | 1489 47 25 55 39 105 22 | 48 48 66 53 60 39
R24E | 3254 27 14 83 26 --- 20 | 27 42 85 36 --- 36
------+------------------------------------+--------------------------------
RMS | 3794 31 16 62 31 114 |T 34 36 52 42 42 33
WRMS | 3794 31 13 45 31 114 |NE 34 34 52 37 37 32
MEDI | 2874 27 14 30 27 101 |MD 32 33 39 38 33 33
Table 3.1548.4 GPS week: 1548 Day: 4 MJD: 55084
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 6564 16 --- 19 19 --- 13 | 15 --- 36 24 --- 22
R03 | 7299 22 13 20 37 --- 13 | 23 34 50 38 --- 33
R07 | 2437 28 26 35 26 --- 17 | 24 29 39 21 --- 20
R08 | 1679 17 10 12 19 74 8 | 37 31 34 26 56 29
R10 | 3368 29 14 21 17 --- 12 | 18 26 44 22 --- 21
R11 | 5157 23 18 25 24 221 13 | 37 32 39 21 108 28
R13 | 1698 15 15 19 22 --- 10 | 21 23 37 26 --- 24
R14 | 5147 14 10 15 16 --- 8 | 19 22 28 28 --- 19
R15 | 3002 20 18 17 32 82 12 | 17 23 33 41 14 21
R17E | 6059 25 16 11 39 --- 13 | 28 33 31 37 --- 25
R18E | 1180 26 22 41 45 --- 19 | 31 36 53 58 --- 34
XR19E | 2250 24 21 --- 31 --- 17 | 34 18 --- 45 --- 24
R20E | 3853 59 32 34 36 --- 23 | 41 33 52 40 --- 29
R21E | 2282 38 27 30 31 --- 18 | 24 28 36 49 --- 20
R23E | 3088 39 29 25 43 140 19 | 32 47 58 45 65 37
R24E | 3092 19 17 26 23 --- 12 | 51 58 56 45 --- 49
------+------------------------------------+--------------------------------
RMS | 3924 29 20 25 31 142 |T 28 31 41 35 60 27
WRMS | 3924 29 15 17 31 142 |NE 23 27 37 27 59 24
MEDI | 3088 23 18 21 26 82 |MD 24 31 39 37 56 24
Table 3.1548.5 GPS week: 1548 Day: 5 MJD: 55085
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 6377 12 --- 21 28 --- 14 | 16 --- 41 19 --- 23
R03 | 9910 14 17 17 24 --- 10 | 42 47 45 40 --- 41
R07 | 1506 17 11 24 32 --- 11 | 17 27 51 24 --- 26
R08 | 963 18 13 23 27 102 11 | 46 34 23 23 58 30
R10 | 3690 19 12 16 24 --- 9 | 21 22 36 22 --- 21
R11 | 4330 17 17 39 22 99 14 | 39 31 73 25 51 38
R13 | 2013 17 11 21 23 --- 10 | 20 23 35 18 --- 21
R14 | 2470 25 12 17 32 --- 12 | 34 29 29 19 --- 24
R15 | 2885 13 9 18 29 43 9 | 25 19 48 24 24 22
R17E | 5027 29 18 23 37 --- 15 | 29 35 26 38 --- 26
R18E | 1055 27 12 38 50 --- 18 | 30 27 44 59 --- 30
XR19E | 4464 19 17 --- 44 --- 18 | 27 21 --- 47 --- 21
R20E | 3802 47 19 35 46 --- 20 | 32 26 38 49 --- 25
R21E | 2205 39 24 29 35 --- 18 | 36 34 49 32 --- 30
R23E | 4449 46 17 41 38 132 20 | 30 39 49 45 67 31
R24E | 1649 13 8 19 21 --- 8 | 37 38 56 28 --- 38
------+------------------------------------+--------------------------------
RMS | 3968 27 15 27 33 99 |T 30 30 42 32 50 27
WRMS | 3968 27 13 23 33 99 |NE 28 29 42 23 44 27
MEDI | 2885 18 13 23 29 99 |MD 30 29 44 25 51 26
Table 3.1548.6 GPS week: 1548 Day: 6 MJD: 55086
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 4112 --- --- 16 13 --- 15 | --- --- 33 45 --- 38
R03 | 8744 25 19 30 17 --- 13 | 33 51 49 43 --- 42
R07 | 1296 24 31 40 17 --- 17 | 23 52 34 31 --- 33
R08 | 952 29 17 17 27 95 13 | 30 43 42 28 16 32
R10 | 4051 29 9 22 16 --- 11 | 19 18 34 19 --- 17
R11 | 2581 30 24 35 19 97 15 | 41 47 64 40 57 46
R13 | 3133 20 14 25 23 --- 11 | 16 24 43 39 --- 28
R14 | 1646 24 10 20 13 --- 9 | 30 19 25 31 --- 23
R15 | 2273 16 11 21 18 60 9 | 27 20 34 27 21 22
R17E | 1258 41 18 29 30 --- 17 | 24 37 46 34 --- 28
R18E | 1469 41 21 48 39 --- 21 | 31 45 52 52 --- 37
XR19E | 2336 25 18 --- 38 --- 19 | 33 28 --- 49 --- 30
R20E | 2418 31 19 45 40 --- 19 | 32 26 61 52 --- 28
R21E | 1412 30 18 26 23 --- 13 | 30 25 44 43 --- 29
R23E | 6911 29 21 23 37 144 16 | 27 32 36 44 58 26
R24E | 2060 21 12 23 18 --- 10 | 52 44 46 48 --- 45
------+------------------------------------+--------------------------------
RMS | 3619 29 18 30 26 103 |T 29 34 42 39 38 31
WRMS | 3619 29 17 28 26 103 |NE 27 34 39 33 31 31
MEDI | 2273 29 18 25 19 95 |MD 30 32 43 40 21 29
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