[IGSREPORT-17642] Wk 1540 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 30 05:11:11 PDT 2009
******************************************************************************
IGS Electronic Report 30 Jul 05:11:33 PDT 2009 Message Number 17642
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1540 (Jul 12, 2009 - Jul 18, 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 2.1540.
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:
igl1540[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1540 in the SP3 format.
igl15407.sum Combination Report for GPS Week 1540.
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 | 32.8 ns
1 | 122.5 ns
2 | 188.2 ns
3 | 189.1 ns
4 | 184.3 ns
5 | 185.9 ns
6 | 111.2 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 1.1540, 1a.1540).
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 2.1540.0-6)
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 3.1540.0-6).
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 1540 summary. (Jul 12, 2009 - Jul 18, 2009)
Table 1.1540.a GPS week : 1540 MJD: 55024.0-55030.0
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 103| 1 0 -12 6 0 87 -.09 27 26 | 0 13 3847 4458
| 1 1 3 47 32 189 .05 | 0 765
cod 233| -3 0 -1 -11 -24 51 -.12 17 14 | --- --- --- ---
| 1 1 2 30 16 28 .04 | --- ---
esx 129| 2 0 5 28 62 39 .41 27 24 | 62144 1343 5681 11741
| 1 1 2 29 18 118 .05 | 63226 4285
iac n/a| 1 0 8 -4 -6 -181 -.06 26 26 | 145398 -2117 5654 11804
| 1 1 4 34 28 95 .04 | 60392 1817
mcc n/a| -3 4 41 -22 -140 -378 .31 1871 1871 | --- --- --- ---
| 8 11 33 269 92 309 .59 | --- ---
Table 1.1540.b GPS week : 1540 MJD: 55024.0-55030.0
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 | 9 15 12 10 10 10 9 |
R03 | 13 12 15 11 10 11 11 |
R07 | 9 13 9 9 10 10 10 |
R08 | 10 16 12 11 10 7 8 |
R10 | 18 13 13 13 15 16 28 |
R11 | 17 10 11 12 12 9 11 |
R13 | 9 11 11 11 10 13 12 |
R14 | 12 15 16 9 15 14 12 |
R15 | 12 13 11 17 19 18 16 |
R17 | 18 10 11 19 14 15 16 |
R18 | 15 11 11 9 10 9 11 |
R19 | 11 9 7 9 9 12 23 |
R20 | 18 14 17 12 19 16 18 |
R21 | 9 15 12 12 11 11 11 |
R22 | 10 12 13 15 13 14 11 |
R23 | 25 17 17 15 24 24 19 |
R24 | 36 22 14 15 16 13 20 |
Table 1.1540.c GPS week : 1540 MJD: 55024.0-55030.0
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 1540 0 | 8 28 657 -1724 -1901 -21090 87.9 2410 2410 | 32783 0
brd 1540 1 | 120 26 569 -1476 756 -18520 85.3 3015 3015 | 122495 0
brd 1540 2 | 115 9 430 -240 -1525 -12110 90.0 3194 3194 | 188246 0
brd 1540 3 | 47 -26 480 634 247 -7992 87.4 3455 3455 | 189112 0
brd 1540 4 | 16 -90 406 -1043 -2574 -6164 83.5 3535 3535 | 184300 0
brd 1540 5 | 62 80 468 406 -2170 -13510 87.4 3228 3228 | 185935 0
brd 1540 6 | 31 -139 420 -1326 1989 -18240 87.4 2785 2785 | 111202 0
-------------+------------------------------------------------------------+----------------
brd 1540 mean| 57 -15 490 -681 -739 -13946 87.0 3088 3088 | 144867 0
brd 1540 sdev| 44 76 91 946 1733 5626 2.1 392 392 | 59550 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 2.1540.0 GPS week: 1540 Day: 0 MJD: 55024
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 103| 0 -1 -10 -21 -46 -184 -.14 32 24 | 0 -135 3895 4588
cod 233| -2 2 1 27 3 81 -.12 20 15 | --- --- --- ---
esx 129| 2 -2 6 4 74 235 .39 32 24 | -52335 -3456 8699 21188
iac n/a| 0 -1 0 -9 -40 -151 -.07 30 30 | 31078 -5903 8685 20956
mcc n/a| 0 -2 -9 -197 -289 173 .69 194 194 | --- --- --- ---
Table 2.1540.1 GPS week: 1540 Day: 1 MJD: 55025
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 103| 3 0 -13 44 2 84 .00 29 28 | 0 -236 3401 3774
cod 233| -2 0 0 -27 -27 66 -.08 14 13 | --- --- --- ---
esx 129| 1 1 2 17 56 77 .45 31 24 | 29506 7988 6027 9749
iac n/a| 0 0 5 0 -9 -249 -.07 25 25 | 124105 -2346 5991 9823
mcc n/a| 4 29 57 -267 -62 -235 -.52 237 237 | --- --- --- ---
Table 2.1540.2 GPS week: 1540 Day: 2 MJD: 55026
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 103| 3 0 -10 50 61 398 -.11 26 26 | 0 1405 4384 4986
cod 233| -1 -1 -2 -35 -39 49 -.07 14 12 | --- --- --- ---
esx 129| 1 0 3 -2 92 -99 .47 25 23 | 109007 1749 5190 10484
iac n/a| 1 1 13 40 -14 -336 -.12 25 25 | 190467 -2149 5183 10696
mcc n/a| -12 5 49 -22 -32 -593 -.16 189 189 | --- --- --- ---
Table 2.1540.3 GPS week: 1540 Day: 3 MJD: 55027
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 103| 0 0 -15 -26 -3 58 -.07 24 22 | 0 -418 3153 3793
cod 233| -2 0 0 26 -28 40 -.14 16 15 | --- --- --- ---
esx 129| 2 0 4 44 74 66 .39 23 22 | 105276 2851 4790 10004
iac n/a| 1 -2 10 -32 -32 -221 -.09 25 25 | 189563 -871 4790 10285
mcc n/a| -2 4 74 175 -100 -544 .07 130 130 | --- --- --- ---
Table 2.1540.4 GPS week: 1540 Day: 4 MJD: 55028
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 103| 1 1 -15 52 -2 163 -.10 27 27 | 0 -1069 3816 4448
cod 233| -7 -1 -2 -33 -29 65 -.17 20 16 | --- --- --- ---
esx 129| 5 0 4 9 35 -36 .47 25 24 | 109295 -786 4177 9210
iac n/a| 3 0 10 9 46 -164 -.04 24 24 | 185535 -1511 4151 9590
mcc n/a| 5 0 70 -42 -170 -183 .20 104 104 | --- --- --- ---
Table 2.1540.5 GPS week: 1540 Day: 5 MJD: 55029
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 103| 1 0 -7 15 -1 178 -.12 27 26 | 0 251 3236 3688
cod 233| -3 1 -3 -41 -40 -5 -.15 15 13 | --- --- --- ---
esx 129| 3 -1 4 45 48 -76 .36 24 22 | 108875 -3637 5408 10320
iac n/a| 1 0 8 23 -6 -67 .02 31 31 | 185593 -1767 5389 10121
mcc n/a| -1 -9 47 470 -230 -559 1.24 >>>> >>>> | --- --- --- ---
Table 2.1540.6 GPS week: 1540 Day: 6 MJD: 55030
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 103| 0 0 -14 -70 -12 -87 -.07 26 25 | 0 295 5048 5931
cod 233| -4 2 -3 4 -8 64 -.10 20 17 | --- --- --- ---
esx 129| 0 0 10 79 58 107 .35 31 25 | 25384 4693 5477 11234
iac n/a| 3 -1 12 -62 8 -81 -.04 25 25 | 111449 -274 5394 11160
mcc n/a| -17 5 -1 -275 -101 -703 .67 490 490 | --- --- --- ---
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 3.1540.0 GPS week: 1540 Day: 0 MJD: 55024
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1297 6 10 11 27 --- 8 | 41 44 54 53 --- 45
R03 | 4953 20 16 29 24 --- 12 | 19 25 35 24 --- 17
R07 | 3185 20 7 20 15 --- 9 | 27 19 26 26 --- 20
R08 | 2467 10 10 17 25 --- 9 | 25 28 36 47 --- 31
R10 | 2829 34 25 34 33 --- 18 | 37 31 35 24 --- 22
R11 | 1667 20 14 41 41 133 17 | 32 27 57 24 818 26
R13 | 2809 16 13 18 18 --- 9 | 24 24 28 26 --- 21
R14 | 1825 16 17 19 28 --- 11 | 28 26 33 23 --- 24
R15 | 1813 26 10 24 23 142 12 | 19 27 39 18 77 22
R17 | 828 46 6 29 39 --- 18 | 31 48 47 56 --- 44
R18 | 865 27 24 20 27 --- 14 | 14 39 38 24 --- 22
R19 | 1413 14 12 22 25 --- 10 | 29 40 35 43 --- 37
R20 | 3032 21 28 28 45 --- 18 | 38 35 47 41 --- 33
R21 | 674 16 14 18 13 --- 9 | 39 29 41 33 --- 31
R22 | 1797 24 13 15 16 --- 10 | 45 36 35 30 --- 32
R23 | 1224 30 37 67 31 275 24 | 28 36 53 38 183 23
R24 | 3631 92 38 67 48 --- 35 | 112 85 75 75 --- 75
------+------------------------------------+--------------------------------
RMS | 2410 32 20 32 30 194 |T 34 35 42 35 359 30
WRMS | 2410 24 15 24 30 194 |NE 34 35 42 35 359 30
MEDI | 1813 20 14 22 27 142 |MD 29 31 38 30 183 26
Table 3.1540.1 GPS week: 1540 Day: 1 MJD: 55025
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 644 27 12 24 39 --- 14 | 46 34 50 43 --- 37
R03 | 2554 24 12 16 31 --- 12 | 29 38 35 17 --- 27
R07 | 5294 26 12 19 34 --- 13 | 24 22 34 27 --- 18
R08 | 2665 35 16 40 24 103 15 | 35 25 54 35 125 27
R10 | 3363 27 14 20 29 --- 12 | 27 27 32 33 --- 20
R11 | 693 23 8 23 16 --- 9 | 28 23 36 24 --- 22
R13 | 2375 34 6 20 18 --- 11 | 16 18 34 34 --- 21
R14 | 3023 27 15 38 25 --- 14 | 18 27 59 27 --- 27
R15 | 1735 24 11 28 32 145 13 | 21 24 48 26 63 23
R17 | 1526 23 8 16 26 --- 10 | 33 33 34 45 --- 32
R18 | 992 28 14 16 20 --- 11 | 34 29 23 23 --- 24
R19 | 996 19 11 18 17 --- 9 | 27 37 27 30 --- 29
R20 | 1986 32 14 32 20 --- 13 | 46 34 46 24 --- 30
R21 | 851 26 16 45 16 --- 15 | 24 37 48 27 --- 28
R22 | 2382 27 15 26 12 --- 11 | 25 34 30 16 --- 22
R23 | 1558 38 13 43 28 369 16 | 21 27 52 21 89 23
R24 | 8113 37 26 62 27 --- 21 | 63 69 93 70 --- 66
------+------------------------------------+--------------------------------
RMS | 3015 29 14 31 25 236 |T 30 31 43 30 92 28
WRMS | 3015 28 13 24 25 236 |NE 30 31 43 30 92 28
MEDI | 1986 27 13 24 25 145 |MD 27 29 36 27 89 27
Table 3.1540.2 GPS week: 1540 Day: 2 MJD: 55026
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 560 17 13 18 34 --- 12 | 23 27 40 38 --- 27
R03 | 1784 30 10 30 34 --- 14 | 35 17 40 30 --- 20
R07 | 6925 19 9 14 18 --- 8 | 20 23 21 25 --- 17
R08 | 2639 34 15 21 14 68 12 | 38 24 48 34 59 29
R10 | 3764 19 21 28 17 --- 12 | 24 38 35 20 --- 21
R11 | 922 25 12 26 17 --- 11 | 40 32 40 26 --- 27
R13 | 2629 26 10 15 23 --- 10 | 22 14 29 22 --- 14
R14 | 3405 29 17 38 26 --- 15 | 32 34 65 44 --- 36
R15 | 1461 23 9 23 24 132 11 | 26 19 29 22 38 18
R17 | 1629 26 9 20 22 --- 10 | 34 34 47 40 --- 36
R18 | 1132 21 12 17 24 --- 10 | 31 31 29 38 --- 26
R19 | 670 15 9 10 17 --- 7 | 29 21 27 32 --- 23
R20 | 689 19 22 30 42 --- 16 | 26 33 34 32 --- 22
R21 | 1022 23 15 24 20 --- 11 | 25 43 53 37 --- 36
R22 | 1956 36 14 25 17 --- 13 | 23 38 41 40 --- 30
R23 | 1083 43 17 33 30 292 17 | 30 37 40 27 49 23
R24 | 8272 21 10 33 32 --- 13 | 107 115 124 131 --- 118
------+------------------------------------+--------------------------------
RMS | 3194 26 14 25 25 189 |T 33 34 43 37 48 30
WRMS | 3194 26 12 23 25 189 |NE 33 34 43 37 48 30
MEDI | 1629 23 12 24 23 132 |MD 29 32 40 32 49 26
Table 3.1540.3 GPS week: 1540 Day: 3 MJD: 55027
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 867 14 12 20 23 --- 10 | 48 30 37 27 --- 30
R03 | 4031 17 16 21 23 --- 11 | 20 27 28 18 --- 16
R07 | 1944 14 13 11 20 --- 8 | 11 22 28 22 --- 17
R08 | 1974 15 13 24 21 51 10 | 15 23 32 34 108 18
R10 | 3344 25 24 22 19 --- 13 | 26 32 31 27 --- 19
R11 | 886 26 11 29 15 --- 12 | 28 27 41 22 --- 24
R13 | 2811 26 11 21 21 --- 11 | 25 30 40 29 --- 28
R14 | 1605 13 15 20 15 --- 9 | 20 34 41 32 --- 29
R15 | 1203 37 21 22 38 95 17 | 17 23 22 20 34 14
R17 | 900 44 12 13 48 --- 18 | 45 31 32 40 --- 32
R18 | 979 14 14 18 17 --- 9 | 17 19 36 23 --- 18
R19 | 928 9 13 19 16 --- 8 | 19 22 29 26 --- 20
R20 | 1143 20 19 24 20 --- 12 | 24 19 45 24 --- 23
R21 | 1783 11 18 29 21 --- 12 | 27 27 37 15 --- 17
R22 | 776 17 11 37 30 --- 14 | 16 30 56 36 --- 26
R23 | 1179 37 12 29 22 198 14 | 22 22 47 42 55 23
R24 |12052 31 25 16 24 --- 14 | 62 82 77 76 --- 71
------+------------------------------------+--------------------------------
RMS | 3455 24 16 23 25 130 |T 26 29 38 30 65 25
WRMS | 3455 22 15 22 25 130 |NE 26 29 38 30 65 25
MEDI | 1203 17 13 21 21 95 |MD 22 27 37 27 55 23
Table 3.1540.4 GPS week: 1540 Day: 4 MJD: 55028
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2167 19 16 17 18 --- 10 | 21 24 38 22 --- 21
R03 | 7066 14 13 27 14 --- 10 | 20 29 39 29 --- 26
R07 | 2614 12 12 20 20 --- 9 | 16 24 38 18 --- 20
R08 | 1609 16 13 22 12 92 9 | 24 23 38 33 154 25
R10 | 1490 33 16 30 24 --- 15 | 20 28 42 23 --- 20
R11 | 1271 18 22 27 16 --- 12 | 19 30 38 26 --- 24
R13 | 2421 20 16 11 18 --- 9 | 28 36 34 23 --- 27
R14 | 1892 31 20 29 21 --- 14 | 25 23 52 29 --- 26
R15 | 2312 48 14 20 39 82 18 | 22 34 33 32 50 27
R17 | 1534 33 13 18 28 --- 13 | 27 41 43 45 --- 38
R18 | 742 17 13 18 17 --- 9 | 13 20 31 25 --- 18
R19 | 1302 12 12 19 18 --- 9 | 22 19 32 31 --- 24
R20 | 2733 39 25 41 22 --- 18 | 30 33 45 24 --- 25
R21 | 1467 20 12 24 19 --- 11 | 31 35 41 25 --- 28
R22 | 549 24 27 20 16 --- 13 | 17 44 32 18 --- 24
R23 | 2374 43 41 36 45 131 24 | 34 23 58 48 87 29
R24 |10469 27 25 28 29 --- 15 | 124 134 145 152 --- 137
------+------------------------------------+--------------------------------
RMS | 3535 27 20 25 24 104 |T 29 35 45 35 97 31
WRMS | 3535 27 16 24 24 104 |NE 29 35 45 35 97 31
MEDI | 1892 20 16 22 19 92 |MD 22 29 38 26 87 25
Table 3.1540.5 GPS week: 1540 Day: 5 MJD: 55029
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2856 18 10 24 15 --- 10 | 39 31 41 25 --- 29
R03 | 8771 12 12 26 23 --- 10 | 15 33 51 28 --- 29
R07 | 5816 21 10 20 20 --- 10 | 17 17 23 21 --- 14
R08 | 1011 10 9 10 20 456 7 | 15 17 18 24 259 13
R10 | 1869 37 16 30 28 --- 15 | 26 26 45 18 --- 21
R11 | 1322 23 9 20 11 >>>> 9 | 22 24 29 25 9999 20
R13 | 3034 20 19 17 32 --- 12 | 22 26 27 20 --- 19
R14 | 1975 26 12 26 34 --- 13 | 18 27 33 24 --- 19
R15 | 1214 38 17 35 41 159 18 | 17 34 53 21 51 27
R17 | 2283 43 12 13 32 --- 14 | 19 28 26 20 --- 20
R18 | 718 16 13 15 14 --- 8 | 16 24 27 17 --- 18
R19 | 1467 23 14 22 25 --- 12 | 24 29 29 24 --- 22
R20 | 2438 22 19 39 30 --- 16 | 39 53 69 50 --- 49
R21 | 650 19 16 22 19 --- 10 | 27 31 44 31 --- 29
R22 | 561 31 18 22 29 --- 14 | 19 28 42 26 --- 21
R23 | 2734 31 28 29 74 126 23 | 23 41 38 64 116 29
R24 | 3909 34 15 24 18 --- 13 | 57 53 58 58 --- 52
------+------------------------------------+--------------------------------
RMS | 3227 27 15 24 31 >>>> |T 24 30 38 29 142 25
WRMS | 3227 26 13 22 31 >>>> |NE 24 30 38 29 142 25
MEDI | 1975 23 14 22 25 159 |MD 22 28 38 24 116 21
Table 3.1540.6 GPS week: 1540 Day: 6 MJD: 55030
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1697 16 12 18 17 --- 9 | 32 23 35 28 --- 25
R03 | 3270 14 15 22 20 --- 10 | 16 28 34 23 --- 21
R07 | 6756 15 13 20 21 --- 10 | 23 24 39 30 --- 25
R08 | 955 13 9 16 15 950 7 | 22 26 32 32 216 24
R10 | 1083 48 33 81 22 --- 28 | 43 41 85 29 --- 26
R11 | 1394 12 13 34 13 115 11 | 21 22 49 27 9999 23
R13 | 3479 20 25 16 20 --- 12 | 21 26 32 24 --- 22
R14 | 3532 14 17 22 27 --- 11 | 30 27 34 22 --- 25
R15 | 2080 30 21 31 28 182 16 | 24 20 44 23 43 21
R17 | 2147 25 25 22 38 --- 16 | 32 52 46 41 --- 41
R18 | 1316 23 15 21 17 --- 11 | 25 24 34 17 --- 19
XR19 |14151 18 35 --- 38 --- 22 | 30 31 --- 46 --- 31
R20 | 2144 43 23 29 22 --- 17 | 41 55 51 46 --- 43
R21 | 1014 20 13 24 20 --- 11 | 25 31 37 34 --- 28
R22 | 563 15 15 25 16 --- 10 | 20 22 30 24 --- 19
R23 | 3068 27 25 31 45 110 18 | 22 27 34 41 88 19
R24 | 3194 36 30 29 39 --- 19 | 84 77 78 78 --- 74
------+------------------------------------+--------------------------------
RMS | 2784 26 20 31 25 490 |T 30 32 43 33 115 28
WRMS | 2784 25 17 25 25 490 |NE 30 32 43 33 115 28
MEDI | 2144 20 17 22 21 115 |MD 25 27 35 29 88 25
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