[IGSREPORT-18924] Wk 1597 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 2 05:18:20 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1597 (Aug 15, 2010 - Aug 21, 2010)
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 2.1597.
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:
igl1597[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1597 in the SP3 format.
igl15977.sum Combination Report for GPS Week 1597.
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 | 368.3 ns
1 | 371.9 ns
2 | 398.5 ns
3 | 359.5 ns
4 | 447.2 ns
5 | 448.2 ns
6 | 358.0 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 1.1597, 1a.1597).
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 2.1597.0-6)
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 3.1597.0-6).
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 1597 summary. (Aug 15, 2010 - Aug 21, 2010)
Table 1.1597.a GPS week : 1597 MJD: 55423.0-55429.0
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 118| 3 -1 -6 24 -8 -76 -.15 34 32 | 0 -823 3350 3800
| 0 1 2 24 38 112 .03 | 0 2271
cod 231| -2 0 5 32 16 89 -.13 20 19 | --- --- --- ---
| 1 1 2 6 21 53 .03 | --- ---
esx 136| -1 0 0 -24 -8 17 .42 25 22 | 83227 -538 3815 7770
| 1 0 4 28 42 61 .02 | 38681 1310
gfz 197| 0 1 2 -57 -16 110 -.17 31 25 | 232720 -293 3827 7518
| 1 3 5 79 97 50 .04 | 36757 1497
iac n/a| 2 0 -2 -26 -11 -92 -.24 33 33 | 393341 -208 3828 8126
| 1 1 7 19 30 126 .05 | 39662 1003
mcc n/a| 1 0 46 -22 23 -353 -.13 113 113 | --- --- --- ---
| 6 7 19 71 140 369 .28 | --- ---
Table 1.1597.b GPS week : 1597 MJD: 55423.0-55429.0
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 | 17 12 9 16 14 18 10 |
R02 | 14 10 9 14 10 12 10 |
R03 | 11 13 12 11 9 16 11 |
R04 | 9 14 9 10 9 12 8 |
R05 | 11 15 12 12 11 11 12 |
R07 | 10 12 13 16 18 15 16 |
R08 | 12 11 16 13 12 14 14 |
R10 | 12 12 9 10 13 13 13 |
R11 | 17 23 27 23 23 20 18 |
R13 | 10 14 9 14 13 9 12 |
R14 | 12 15 15 15 12 13 10 |
R15 | 13 12 12 12 13 13 11 |
R17 | 12 16 17 18 19 24 24 |
R18 | 18 12 13 16 15 17 26 |
R19 | 14 14 14 16 17 15 21 |
R20 | 18 19 26 19 21 17 22 |
R21 | 20 20 21 22 20 18 16 |
R22 | 15 16 20 25 24 17 18 |
R23 | 13 13 23 19 24 29 20 |
R24 | 15 16 13 14 23 20 22 |
Table 1.1597.c GPS week : 1597 MJD: 55423.0-55429.0
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 1597 0 | 74 48 163 213 162 -9279 88.5 1698 1698 | 368278 0
brd 1597 1 | 54 95 292 -1326 -3988 -14260 87.8 1744 1744 | 371902 0
brd 1597 2 | 18 76 281 -1668 -3101 -8225 87.8 2125 2125 | 398516 0
brd 1597 3 | 99 -35 339 1130 -2021 -1934 90.1 2556 2556 | 359545 0
brd 1597 4 | 38 18 286 -3694 2418 -1489 91.8 2420 2420 | 447201 0
brd 1597 5 | 13 -136 395 674 1138 -5638 89.4 2281 2281 | 448215 0
brd 1597 6 | 11 -42 312 2603 -796 -9033 88.0 2291 2291 | 357988 0
-------------+------------------------------------------------------------+----------------
brd 1597 mean| 44 3 295 -295 -884 -7122 89.1 2159 2159 | 393092 0
brd 1597 sdev| 33 80 70 2086 2307 4496 1.5 327 327 | 39619 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 2.1597.0 GPS week: 1597 Day: 0 MJD: 55423
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 118| 3 0 -7 67 31 13 -.14 25 25 | 0 293 1883 1953
cod 231| -1 2 3 23 0 -7 -.07 20 20 | --- --- --- ---
esx 136| -1 0 -6 -65 -28 -37 .41 24 21 | 61426 412 3290 7411
gfz 197| -3 3 -4 82 124 43 -.20 29 24 | 209887 10 3330 7157
iac n/a| 1 1 9 -14 30 31 -.30 27 27 | 368427 304 3313 7714
mcc n/a| 1 12 21 -16 134 107 .13 120 120 | --- --- --- ---
Table 2.1597.1 GPS week: 1597 Day: 1 MJD: 55424
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 118| 2 -1 -5 27 -55 -93 -.14 26 25 | 0 -81 1704 1763
cod 231| 0 0 8 28 40 66 -.13 21 20 | --- --- --- ---
esx 136| -2 0 5 1 81 37 .43 25 23 | 64981 -1278 3820 6974
gfz 197| 1 -1 6 -3 -136 154 -.22 29 21 | 210775 -2743 3828 6237
iac n/a| 2 -2 -10 -34 -44 2 -.24 29 29 | 372281 -324 3825 6748
mcc n/a| -4 -8 25 -61 -119 -23 -.35 173 173 | --- --- --- ---
Table 2.1597.2 GPS week: 1597 Day: 2 MJD: 55425
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 118| 4 -2 -2 0 -20 -319 -.13 40 40 | 0 41 1705 1791
cod 231| -2 1 5 43 34 148 -.16 18 17 | --- --- --- ---
esx 136| 0 -1 -4 -59 -48 20 .45 25 19 | 83727 697 4166 8378
gfz 197| 0 0 -2 -70 -116 149 -.11 30 21 | 236711 -360 4125 8334
iac n/a| 5 -1 -3 -12 14 -25 -.23 31 31 | 398064 -103 4151 8754
mcc n/a| -4 4 30 -30 134 -918 -.36 109 109 | --- --- --- ---
Table 2.1597.3 GPS week: 1597 Day: 3 MJD: 55426
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 118| 4 -2 -10 0 -50 -54 -.17 41 41 | 0 199 1804 1894
cod 231| -4 0 4 36 25 114 -.11 16 15 | --- --- --- ---
esx 136| 0 0 3 -19 -27 -33 .40 27 26 | 44885 -2136 4067 7999
gfz 197| 1 2 4 -167 -80 58 -.13 31 27 | 203126 -590 4122 7910
iac n/a| 2 0 -3 -22 -30 -172 -.18 33 33 | 359151 1572 4066 7935
mcc n/a| -3 4 53 -107 -120 -567 -.20 91 91 | --- --- --- ---
Table 2.1597.4 GPS week: 1597 Day: 4 MJD: 55427
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 118| 4 -1 -5 45 -9 -11 -.16 43 38 | 0 -5960 13330 16037
cod 231| -2 1 3 27 3 144 -.17 22 20 | --- --- --- ---
esx 136| -2 0 -5 -5 4 94 .42 24 20 | 136568 662 3883 7306
gfz 197| 0 5 -4 -113 6 85 -.20 36 34 | 283762 722 3937 7213
iac n/a| 2 1 5 -14 -28 -267 -.30 30 30 | 447450 -224 3949 7939
mcc n/a| 12 -8 63 39 -79 -563 -.37 100 100 | --- --- --- ---
Table 2.1597.5 GPS week: 1597 Day: 5 MJD: 55428
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 118| 1 1 -7 21 4 -42 -.22 35 30 | 0 -113 1572 1644
cod 231| -3 0 5 35 29 89 -.12 20 19 | --- --- --- ---
esx 136| -2 0 2 -27 -28 -53 .39 24 22 | 137648 117 3419 7420
gfz 197| 0 -4 7 -63 23 107 -.17 31 26 | 283742 2054 3395 7362
iac n/a| 0 0 -5 -21 -39 16 -.22 39 39 | 448885 -1307 3405 8346
mcc n/a| 2 0 66 -78 -8 -437 -.07 107 107 | --- --- --- ---
Table 2.1597.6 GPS week: 1597 Day: 6 MJD: 55429
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 118| 3 0 -7 10 44 -24 -.11 30 26 | 0 -140 1453 1520
cod 231| -4 -1 10 32 -16 71 -.16 22 18 | --- --- --- ---
esx 136| -1 1 2 5 -15 91 .41 26 21 | 53360 -2244 4061 8904
gfz 197| -2 2 8 -63 63 175 -.13 29 23 | 201040 -1148 4057 8417
iac n/a| 2 2 -7 -66 15 -229 -.21 38 38 | 359134 -1380 4088 9446
mcc n/a| 8 0 63 98 225 -70 .34 91 91 | --- --- --- ---
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 3.1597.0 GPS week: 1597 Day: 0 MJD: 55423
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1875 26 30 27 28 31 --- 16 | 23 37 49 37 28 --- 26
R02 | 1201 21 18 18 21 35 --- 13 | 27 34 24 22 17 --- 19
R03 | 1353 21 21 12 18 22 --- 11 | 18 28 24 32 12 --- 17
R04 | 2661 20 12 15 26 15 --- 9 | 14 32 37 31 30 --- 26
R05 | 563 12 16 22 20 22 --- 10 | 15 31 34 21 20 --- 21
R07 | 1195 12 18 12 27 25 --- 10 | 23 43 36 32 21 --- 29
R08 | 2393 24 21 12 18 22 67 11 | 23 52 39 40 26 43 33
R10 | 1695 13 16 24 20 24 --- 11 | 16 22 28 24 33 --- 21
R11 | 1468 31 21 36 36 29 --- 17 | 33 31 38 34 26 --- 20
R13 | 1504 14 14 20 16 21 --- 10 | 20 24 28 25 17 --- 17
R14 | 1846 21 20 17 14 23 --- 11 | 29 35 30 25 24 --- 22
R15 | 1568 31 15 15 26 25 105 12 | 13 23 27 26 33 29 19
R17E | 2672 23 17 17 18 23 --- 11 | 30 30 44 35 45 --- 33
R18E | 1075 39 25 33 34 21 --- 17 | 30 31 60 49 41 --- 36
R19E | 709 25 22 27 35 24 --- 14 | 104 118 119 120 111 --- 111
R20E | 1418 33 19 37 54 36 --- 18 | 19 26 56 63 38 --- 28
R21E | 1104 38 19 28 38 46 --- 19 | 35 37 47 51 46 --- 35
R22E | 1937 27 23 25 29 31 --- 15 | 34 17 39 32 30 --- 20
R23E | 2150 16 27 23 34 23 166 13 | 43 23 42 32 37 95 30
R24E | 1661 28 16 32 27 23 --- 14 | 20 23 49 32 35 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1698 25 20 24 29 27 120 |T 28 34 42 38 33 55 29
WRMS | 1698 25 20 21 24 27 120 |NE 21 32 32 29 23 36 22
MEDI | 1504 23 19 22 26 23 105 |MD 23 31 38 32 30 43 25
Table 3.1597.1 GPS week: 1597 Day: 1 MJD: 55424
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1096 13 13 17 16 37 --- 12 | 13 21 29 22 25 --- 14
R02 | 2114 17 21 15 18 14 --- 10 | 21 28 30 25 14 --- 15
R03 | 1500 25 20 17 22 27 --- 13 | 20 28 37 28 14 --- 18
R04 | 1435 31 27 13 20 19 --- 13 | 27 26 19 18 18 --- 10
R05 | 784 27 28 24 17 18 --- 14 | 25 24 36 23 14 --- 14
R07 | 1243 10 20 9 27 36 --- 12 | 12 17 22 25 33 --- 11
R08 | 1295 10 21 12 30 29 100 11 | 13 24 25 39 23 42 13
R10 | 2169 12 20 26 18 20 --- 11 | 16 18 26 26 30 --- 15
R11 | 2593 51 22 30 34 51 --- 22 | 50 25 44 37 19 --- 28
R13 | 1006 24 14 29 23 26 --- 13 | 17 25 35 25 20 --- 18
R14 | 1055 33 17 29 22 22 --- 15 | 13 19 34 31 19 --- 14
R15 | 1444 17 20 20 26 25 145 12 | 15 23 22 38 17 62 15
R17E | 2790 19 24 39 26 26 --- 16 | 23 28 51 31 34 --- 25
R18E | 914 23 15 19 31 24 --- 11 | 32 24 35 36 43 --- 28
R19E | 1274 18 12 32 31 29 --- 13 | 80 80 86 86 84 --- 79
R20E | 1604 40 23 35 58 30 --- 18 | 15 28 60 67 39 --- 32
R21E | 1473 43 28 31 45 31 --- 19 | 21 24 43 36 39 --- 24
R22E | 2184 30 20 28 29 33 --- 16 | 28 31 36 32 44 --- 24
R23E | 3227 18 19 20 32 31 243 12 | 39 32 44 43 42 134 31
R24E | 1094 18 20 36 27 33 --- 16 | 18 17 45 30 33 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 1744 26 21 25 29 29 173 |T 24 27 37 34 30 79 22
WRMS | 1744 25 20 23 21 29 173 |NE 20 23 29 28 20 52 15
MEDI | 1435 19 20 24 26 27 145 |MD 20 24 35 31 25 62 17
Table 3.1597.2 GPS week: 1597 Day: 2 MJD: 55425
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1261 19 9 9 24 24 --- 9 | 34 27 24 28 16 --- 20
R02 | 2839 17 15 13 13 19 --- 9 | 18 17 18 15 14 --- 11
R03 | 3126 20 18 21 13 20 --- 11 | 23 29 24 22 14 --- 15
R04 | 1825 20 11 11 23 17 --- 8 | 16 25 19 32 20 --- 17
R05 | 1448 23 16 23 16 21 --- 11 | 21 17 27 25 17 --- 9
R07 | 950 20 21 20 26 31 --- 13 | 25 36 27 23 13 --- 22
R08 | 1037 24 23 14 17 43 104 15 | 38 34 26 29 29 35 21
R10 | 1974 17 13 14 19 18 --- 9 | 27 28 23 28 20 --- 19
R11 | 3374 82 16 41 37 47 --- 26 | 23 24 49 42 20 --- 21
R13 | 996 18 12 17 27 16 --- 9 | 20 27 28 22 17 --- 17
R14 | 1269 52 8 14 15 30 --- 15 | 27 18 25 18 18 --- 14
R15 | 1883 19 20 15 38 25 33 11 | 13 24 21 41 25 66 17
R17E | 3195 36 21 22 40 38 --- 16 | 31 28 41 27 33 --- 26
R18E | 1476 23 16 21 34 28 --- 12 | 27 27 41 44 27 --- 25
R19E | 3749 29 19 21 27 32 --- 14 | 100 82 83 89 94 --- 85
R20E | 1155 79 29 40 48 37 --- 26 | 31 31 53 57 29 --- 26
R21E | 1109 48 25 40 39 34 --- 20 | 30 32 52 41 40 --- 29
R22E | 1413 58 13 31 45 39 --- 19 | 27 16 35 49 53 --- 22
R23E | 3126 63 18 40 33 42 154 22 | 44 62 82 69 82 61 62
R24E | 1132 17 14 25 29 34 --- 13 | 20 16 40 27 35 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 2125 40 18 25 30 31 109 |T 29 30 36 36 30 54 24
WRMS | 2125 40 17 19 21 31 109 |NE 23 25 25 27 18 50 16
MEDI | 1448 23 16 21 27 30 104 |MD 27 27 27 28 20 61 20
Table 3.1597.3 GPS week: 1597 Day: 3 MJD: 55426
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1470 39 15 41 29 21 --- 16 | 50 40 34 25 24 --- 30
R02 | 1799 32 16 27 27 26 --- 13 | 33 24 23 23 16 --- 14
R03 | 2746 27 8 23 44 23 --- 11 | 25 21 32 54 18 --- 19
R04 | 3220 26 11 14 34 20 --- 9 | 24 39 39 58 19 --- 29
R05 | 2238 30 9 20 22 28 --- 12 | 36 36 50 34 18 --- 32
R07 | 1298 37 21 19 50 34 --- 15 | 20 39 45 50 26 --- 29
R08 | 1183 32 17 20 17 24 126 12 | 27 38 29 30 15 25 23
R10 | 1414 25 6 20 11 17 --- 9 | 21 15 23 18 16 --- 13
R11 | 3092 74 16 35 40 40 --- 22 | 22 32 36 33 17 --- 20
R13 | 1502 21 17 19 17 37 --- 13 | 20 26 33 29 23 --- 19
R14 | 1328 37 13 28 24 29 --- 14 | 23 19 29 29 23 --- 16
R15 | 1168 28 13 18 28 25 30 11 | 16 26 27 29 33 31 22
R17E | 3454 29 18 30 30 51 --- 18 | 42 27 46 37 40 --- 27
R18E | 4166 31 12 34 41 35 --- 15 | 36 26 41 53 32 --- 25
R19E | 5964 33 22 25 25 37 --- 16 | 101 95 120 105 110 --- 102
R20E | 1275 43 23 28 43 41 --- 18 | 37 19 49 47 41 --- 28
R21E | 2015 66 22 30 35 42 --- 22 | 33 24 37 42 43 --- 27
R22E | 930 82 22 34 34 38 --- 24 | 31 20 35 40 41 --- 19
R23E | 3059 48 14 34 21 41 90 18 | 48 69 73 69 72 40 60
R24E | 1234 22 13 25 27 39 --- 14 | 35 16 29 31 44 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 2556 41 16 27 31 33 91 |T 34 32 41 41 33 32 28
WRMS | 2556 41 15 26 27 33 91 |NE 26 29 33 34 20 28 22
MEDI | 1502 32 15 25 28 34 90 |MD 31 26 35 34 24 31 23
Table 3.1597.4 GPS week: 1597 Day: 4 MJD: 55427
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1503 31 17 28 21 24 --- 14 | 19 41 53 48 29 --- 35
R02 | 1144 22 18 10 16 16 --- 9 | 26 33 20 24 23 --- 22
R03 | 1733 30 8 9 15 15 --- 9 | 36 21 24 21 21 --- 19
R04 | 4106 17 16 10 25 19 --- 9 | 28 28 22 32 23 --- 20
R05 | 2461 22 19 16 22 21 --- 11 | 14 30 27 18 21 --- 17
R07 | 958 29 33 27 30 30 --- 17 | 17 40 34 39 21 --- 22
R08 | 1235 29 24 11 31 18 142 12 | 12 35 25 35 29 28 23
R10 | 1005 33 21 20 30 20 --- 13 | 21 28 35 31 20 --- 19
R11 | 2328 67 23 32 29 37 --- 22 | 32 38 38 33 27 --- 29
R13 | 1267 28 16 20 26 24 --- 12 | 19 24 38 29 25 --- 24
R14 | 1781 21 19 13 30 28 --- 12 | 17 18 19 38 25 --- 14
R15 | 1638 21 10 23 35 31 29 13 | 19 19 34 38 27 15 19
R17E | 2563 34 18 33 49 45 --- 19 | 37 31 49 33 62 --- 35
R18E | 4608 37 19 24 32 28 --- 15 | 35 18 35 34 42 --- 24
R19E | 3667 31 23 27 27 36 --- 17 | 89 76 85 84 77 --- 77
R20E | 3103 50 36 32 78 31 --- 21 | 24 49 52 87 37 --- 35
R21E | 2982 54 32 24 23 34 --- 20 | 26 18 37 40 42 --- 22
R22E | 1282 65 23 39 38 41 --- 23 | 29 21 43 53 50 --- 26
R23E | 2986 78 24 27 42 39 95 24 | 40 37 52 58 47 31 36
R24E | 960 71 16 34 54 40 --- 23 | 36 11 39 36 44 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 2419 43 22 24 36 30 100 |T 28 30 38 40 34 24 26
WRMS | 2419 38 20 20 34 30 100 |NE 21 29 30 32 24 21 21
MEDI | 1733 31 19 24 30 28 95 |MD 26 28 35 35 27 28 22
Table 3.1597.5 GPS week: 1597 Day: 5 MJD: 55428
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1831 38 26 28 27 29 --- 17 | 23 42 53 52 20 --- 30
R02 | 1424 26 18 15 27 27 --- 12 | 16 31 28 36 20 --- 20
R03 | 1159 38 18 16 34 38 --- 15 | 25 24 26 33 30 --- 14
R04 | 4331 17 12 22 17 28 --- 11 | 21 22 24 18 23 --- 18
R05 | 1525 20 17 16 31 26 --- 11 | 20 28 36 34 14 --- 21
R07 | 1439 30 19 20 28 34 --- 14 | 20 47 58 48 26 --- 38
R08 | 777 22 30 18 14 24 153 14 | 20 41 24 29 17 25 24
R10 | 1746 22 13 24 17 29 --- 12 | 24 17 29 22 35 --- 17
R11 | 1981 41 24 21 36 53 --- 19 | 37 50 48 33 36 --- 40
R13 | 1063 20 11 8 27 21 --- 8 | 24 23 20 39 20 --- 17
R14 | 1315 21 19 24 41 28 --- 13 | 11 20 31 36 14 --- 14
R15 | 2443 21 13 15 30 38 46 12 | 16 16 30 28 29 24 16
R17E | 1507 47 17 35 30 66 --- 23 | 47 39 48 37 60 --- 33
R18E | 4093 36 12 26 34 44 --- 17 | 31 27 48 33 48 --- 30
R19E | 2047 32 16 20 28 38 --- 15 | 115 118 125 133 134 --- 121
R20E | 2592 28 19 31 35 42 --- 17 | 35 43 62 74 31 --- 40
R21E | 4229 22 22 32 32 47 --- 17 | 32 29 37 37 34 --- 22
R22E | 2377 27 25 24 40 44 --- 17 | 16 31 36 45 34 --- 22
R23E | 1825 85 35 32 42 40 92 28 | 29 46 43 43 44 35 34
R24E | 972 47 20 28 38 46 --- 20 | 29 30 49 52 42 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 2281 35 20 24 31 39 107 |T 29 36 42 43 35 28 29
WRMS | 2281 30 19 22 26 39 107 |NE 21 30 33 34 23 24 22
MEDI | 1746 27 18 22 30 38 92 |MD 24 30 36 36 30 25 22
Table 3.1597.6 GPS week: 1597 Day: 6 MJD: 55429
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2199 22 14 14 25 20 --- 10 | 24 49 35 50 54 --- 38
R02 | 1884 23 12 11 12 17 --- 9 | 18 30 27 28 35 --- 23
R03 | 1177 21 19 15 23 21 --- 10 | 16 32 30 38 24 --- 22
R04 | 3300 12 14 12 19 19 --- 8 | 13 25 16 20 20 --- 15
R05 | 1285 17 20 20 26 25 --- 12 | 18 35 24 30 19 --- 19
R07 | 2019 9 32 25 22 36 --- 15 | 29 60 39 50 16 --- 35
R08 | 1416 29 15 18 23 31 104 13 | 37 52 49 35 24 60 41
R10 | 1698 33 17 18 21 12 --- 12 | 23 14 31 23 15 --- 14
R11 | 3210 15 40 25 41 37 --- 18 | 60 42 55 55 49 --- 47
R13 | 1906 16 20 20 12 22 --- 11 | 19 23 39 27 17 --- 22
R14 | 1285 19 17 10 37 24 --- 10 | 24 30 23 30 16 --- 19
R15 | 2358 17 18 15 15 24 42 10 | 14 20 27 22 24 21 17
R17E | 1035 57 21 31 33 58 --- 24 | 45 31 43 40 52 --- 32
R18E | 3323 63 21 36 43 52 --- 25 | 39 22 45 39 54 --- 28
R19E | 1361 37 22 30 30 57 --- 20 | 130 136 132 141 145 --- 131
R20E | 3333 32 21 46 33 50 --- 21 | 31 31 65 58 37 --- 34
R21E | 4176 26 20 29 32 38 --- 16 | 37 27 44 40 37 --- 30
R22E | 2599 18 28 29 36 48 --- 18 | 24 22 43 40 30 --- 22
R23E | 1319 33 27 25 21 55 111 20 | 21 26 30 23 47 59 23
R24E | 1228 36 14 42 39 56 --- 21 | 22 15 35 37 46 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 2291 30 22 26 29 38 91 |T 32 36 41 41 38 46 31
WRMS | 2291 26 18 21 23 38 91 |NE 24 34 32 34 26 40 26
MEDI | 1884 22 20 20 25 31 104 |MD 24 30 35 37 30 59 23
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