[IGSREPORT-18752] Wk 1589 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jul 8 04:17:33 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1589 (Jun 20, 2010 - Jun 26, 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 2.1589.
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:
igl1589[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1589 in the SP3 format.
igl15897.sum Combination Report for GPS Week 1589.
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 | 465.1 ns
1 | 366.7 ns
2 | 381.4 ns
3 | 463.8 ns
4 | 464.0 ns
5 | 360.8 ns
6 | 418.4 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 1.1589, 1a.1589).
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 2.1589.0-6)
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 3.1589.0-6).
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 1589 summary. (Jun 20, 2010 - Jun 26, 2010)
Table 1.1589.a GPS week : 1589 MJD: 55367.0-55373.0
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 120| 2 0 -6 -8 19 -32 -.14 23 23 | 0 22 1707 1782
| 1 0 1 25 27 129 .05 | 0 57
cod 243| -2 0 0 27 -28 6 -.13 15 14 | --- --- --- ---
| 0 0 2 17 17 50 .03 | --- ---
esx 146| 0 0 -2 3 -2 101 .39 27 25 | 69835 83 4339 8282
| 1 3 3 26 45 56 .04 | 48088 3137
gfz 199| 0 -1 -1 -48 -12 111 -.21 28 28 | 251297 -88 4353 8415
| 1 2 2 90 82 48 .07 | 47154 3107
iac n/a| 3 0 12 -54 36 -77 -.01 28 28 | 417407 -570 4346 8906
| 0 1 4 18 27 92 .05 | 47538 2266
mcc n/a| 13 -1 43 -56 27 -1660 .10 210 210 | --- --- --- ---
| 17 10 19 137 128 1097 .72 | --- ---
Table 1.1589.b GPS week : 1589 MJD: 55367.0-55373.0
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 | 11 14 14 12 10 15 11 |
R02 | 13 12 14 13 11 13 12 |
R03 | 16 14 14 13 12 14 15 |
R04 | 13 17 14 12 14 10 10 |
R05 | 20 22 18 16 13 16 11 |
R07 | 14 12 12 13 15 11 10 |
R08 | 18 16 15 16 15 12 13 |
R10 | 11 10 10 12 15 14 10 |
R11 | 11 12 9 10 11 12 14 |
R13 | 11 9 12 13 13 14 10 |
R14 | 11 11 14 15 13 15 9 |
R15 | 12 12 11 15 15 12 13 |
R17 | 17 17 13 20 17 17 20 |
R18 | 9 12 8 14 10 9 13 |
R19 | 10 14 9 10 9 10 14 |
R20 | 17 16 18 16 14 17 14 |
R21 | 15 15 14 13 15 10 13 |
R22 | 12 14 10 15 13 13 14 |
R23 | 10 10 12 12 11 12 14 |
R24 | 12 10 10 9 12 10 12 |
Table 1.1589.c GPS week : 1589 MJD: 55367.0-55373.0
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 1589 0 | 188 -29 432 2294 1494 -13980 88.5 2496 2496 | 465122 0
brd 1589 1 | 70 -5 361 1758 2056 -16110 87.0 2301 2301 | 366678 0
brd 1589 2 | -50 15 436 3435 -407 -20410 85.0 1759 1759 | 381435 0
brd 1589 3 | -80 -20 368 2630 -1875 -20590 87.2 1770 1770 | 463771 0
brd 1589 4 | 75 37 328 -1209 -1580 -19460 85.5 1717 1717 | 463961 0
brd 1589 5 | -121 9 349 -898 -1729 -29610 84.4 2047 2047 | 360840 0
brd 1589 6 | 55 -93 424 -1074 123 -30790 85.0 2597 2597 | 418384 0
-------------+------------------------------------------------------------+----------------
brd 1589 mean| 19 -12 385 990 -273 -21564 86.1 2098 2098 | 417170 0
brd 1589 sdev| 108 42 44 1984 1587 6374 1.5 369 369 | 47716 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 2.1589.0 GPS week: 1589 Day: 0 MJD: 55367
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 120| 1 0 -7 -32 40 -211 -.15 22 22 | 0 11 1768 1839
cod 243| -2 -1 0 57 -36 104 -.11 16 15 | --- --- --- ---
esx 146| 0 4 -3 23 -11 133 .36 24 23 | 131743 -575 4442 7581
gfz 199| 0 -5 -2 -172 61 97 -.21 28 28 | 300938 -536 4414 7214
iac n/a| 4 0 13 -74 26 -44 -.02 31 31 | 465494 -459 4423 7706
mcc n/a| 4 -8 46 29 209 -2188 -.33 159 159 | --- --- --- ---
Table 2.1589.1 GPS week: 1589 Day: 1 MJD: 55368
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 120| 3 0 -6 -26 28 9 -.10 23 22 | 0 -20 1631 1715
cod 243| -1 -1 -1 32 -15 -5 -.17 17 16 | --- --- --- ---
esx 146| 0 3 -1 5 33 87 .36 25 23 | 24908 -3346 4152 8286
gfz 199| 0 0 0 -99 81 144 -.25 30 30 | 203469 -4043 4201 8103
iac n/a| 2 2 11 -77 2 -91 .05 31 31 | 366853 -2468 4164 8815
mcc n/a| 22 15 18 -165 122 -1889 -.17 216 216 | --- --- --- ---
Table 2.1589.2 GPS week: 1589 Day: 2 MJD: 55369
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 120| 2 1 -6 -22 27 -61 -.14 18 18 | 0 -16 1735 1809
cod 243| -2 0 3 7 -39 35 -.17 16 15 | --- --- --- ---
esx 146| 0 0 -4 24 -16 3 .44 26 24 | 33217 3047 4265 9435
gfz 199| 1 0 -5 -52 43 157 -.15 28 28 | 216357 1703 4326 10011
iac n/a| 2 1 13 -55 31 58 -.06 30 30 | 381875 667 4251 10258
mcc n/a| -12 -15 27 47 -135 -1663 -.24 142 142 | --- --- --- ---
Table 2.1589.3 GPS week: 1589 Day: 3 MJD: 55370
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 120| 4 0 -8 40 7 -98 -.22 24 24 | 0 -51 1689 1756
cod 243| -1 -1 0 11 -9 -8 -.16 16 14 | --- --- --- ---
esx 146| -3 -2 -8 -47 -14 188 .43 26 26 | 111380 -3159 3835 8124
gfz 199| 0 -1 -1 119 14 158 -.15 28 28 | 299105 -2065 3852 8411
iac n/a| 4 0 19 -33 67 -106 -.03 30 30 | 465371 -3446 3865 8662
mcc n/a| 5 1 29 39 -80 -2784 -.41 114 114 | --- --- --- ---
Table 2.1589.4 GPS week: 1589 Day: 4 MJD: 55371
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 120| 0 0 -7 9 -29 199 -.09 25 24 | 0 116 1708 1789
cod 243| -2 0 1 24 -25 -52 -.10 13 12 | --- --- --- ---
esx 146| 1 0 0 17 71 86 .43 28 27 | 108284 2380 4760 7557
gfz 199| 0 0 -2 -10 -128 26 -.13 30 30 | 295841 2830 4758 7837
iac n/a| 3 0 6 -58 7 -216 -.06 28 28 | 463312 1333 4772 8177
mcc n/a| 41 4 44 -45 52 -2323 1.55 310 310 | --- --- --- ---
Table 2.1589.5 GPS week: 1589 Day: 5 MJD: 55372
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 120| 4 0 -6 -14 8 31 -.19 29 29 | 0 52 1543 1609
cod 243| -2 0 -1 17 -17 -8 -.09 13 13 | --- --- --- ---
esx 146| 1 -1 0 -17 -7 90 .38 27 26 | 10870 -2058 4203 8287
gfz 199| -1 0 1 -42 -96 79 -.34 26 27 | 195751 -2793 4215 8394
iac n/a| 4 0 10 -27 69 -145 .04 26 26 | 362452 -2321 4196 9311
mcc n/a| 23 2 70 18 -82 -1377 .57 238 238 | --- --- --- ---
Table 2.1589.6 GPS week: 1589 Day: 6 MJD: 55373
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 120| 1 1 -5 -10 55 -97 -.12 21 19 | 0 64 1875 1963
cod 243| -2 0 -4 41 -59 -17 -.11 17 15 | --- --- --- ---
esx 146| 0 -4 0 20 -73 117 .36 29 27 | 68445 4292 4720 8710
gfz 199| 1 -2 3 -83 -63 118 -.22 25 25 | 247619 4286 4711 8939
iac n/a| 2 0 10 -56 52 6 -.01 22 22 | 416497 2703 4753 9417
mcc n/a| 10 -9 67 -320 105 599 -.26 294 294 | --- --- --- ---
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 3.1589.0 GPS week: 1589 Day: 0 MJD: 55367
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1507 13 14 23 46 29 --- 11 | 13 18 36 40 27 --- 18
R02E | 1184 16 15 21 25 38 --- 13 | 16 16 32 27 34 --- 14
R03E | 1713 28 16 26 32 39 --- 15 | 23 25 27 32 41 --- 21
R04E | 1340 28 13 21 26 28 --- 13 | 22 30 43 38 38 --- 26
R05E | 2302 38 21 41 42 37 --- 19 | 27 58 82 64 44 --- 48
R07E | 1701 16 15 22 --- 42 --- 13 | 38 43 57 --- 39 --- 41
R08E | 1103 33 17 34 45 40 87 17 | 73 59 68 66 66 139 61
R10 | 1258 23 14 20 19 22 --- 11 | 26 32 27 26 26 --- 24
R11 | 1664 19 14 21 22 20 --- 10 | 28 23 37 34 27 --- 26
R13 | 981 13 12 20 19 30 --- 10 | 20 23 22 19 23 --- 18
R14 | 828 16 16 18 17 28 --- 11 | 30 35 35 42 29 --- 30
R15 | 9311 15 15 30 22 17 157 11 | 21 27 23 24 23 29 19
R17 | 702 20 21 20 24 50 --- 16 | 47 57 52 53 38 --- 47
R18 | 1399 16 13 16 27 17 --- 9 | 40 44 38 48 35 --- 37
R19 | 1649 12 8 27 36 18 --- 9 | 39 42 68 64 39 --- 45
R20 | 775 37 11 21 32 45 --- 16 | 23 28 39 36 28 --- 24
R21 | 1756 23 27 25 21 22 --- 14 | 69 85 72 78 72 --- 73
R22 | 845 21 13 26 16 21 --- 11 | 60 74 79 71 74 --- 71
R23 | 1195 14 18 15 18 22 210 10 | 24 35 34 38 33 69 29
R24 | 1753 18 16 25 19 20 --- 11 | 27 41 41 38 33 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2496 22 16 24 28 31 159 |T 33 39 45 44 38 79 35
WRMS | 2496 22 15 23 28 31 159 |NE 34 42 43 43 36 49 36
MEDI | 1340 18 15 21 24 28 157 |MD 27 35 38 38 34 69 29
Table 3.1589.1 GPS week: 1589 Day: 1 MJD: 55368
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2994 21 14 28 42 37 --- 14 | 20 18 40 44 32 --- 21
R02E | 3869 14 16 28 51 28 --- 12 | 15 21 35 47 25 --- 18
R03E | 3207 21 16 14 28 43 --- 14 | 20 22 30 43 51 --- 23
R04E | 764 31 20 18 30 48 --- 17 | 29 26 33 41 52 --- 28
R05E | 2502 38 31 35 48 47 --- 21 | 45 50 54 50 41 --- 42
R07E | 1038 19 14 24 --- 28 --- 12 | 23 26 32 --- 25 --- 21
R08E | 1116 29 12 29 30 38 244 15 | 55 58 72 63 71 161 59
R10 | 2388 18 14 17 18 14 --- 9 | 16 25 26 20 20 --- 17
R11 | 912 24 17 22 30 16 --- 11 | 39 25 31 33 28 --- 26
R13 | 871 13 11 17 21 19 --- 8 | 13 20 30 30 19 --- 16
R14 | 1249 16 10 18 15 31 --- 10 | 29 34 32 36 35 --- 30
R15 | 5891 25 13 23 38 24 198 12 | 26 29 28 17 15 62 19
R17 | 926 32 19 26 16 41 --- 17 | 25 31 23 28 20 --- 21
R18 | 1361 18 12 25 18 26 --- 11 | 26 32 50 38 41 --- 33
R19 | 935 13 14 40 34 21 --- 13 | 41 33 70 59 39 --- 42
R20 | 1274 27 16 27 20 42 --- 16 | 20 30 39 29 34 --- 24
R21 | 2485 21 14 35 30 29 --- 14 | 69 65 71 80 53 --- 62
R22 | 756 22 27 23 38 20 --- 13 | 53 64 61 82 55 --- 55
R23 | 1334 18 13 22 19 17 204 10 | 29 30 22 26 28 66 24
R24 | 2275 12 18 12 16 22 --- 9 | 22 39 32 29 19 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 2300 23 17 25 30 31 216 |T 30 33 40 41 35 96 30
WRMS | 2300 22 16 23 30 31 216 |NE 31 35 39 39 31 64 30
MEDI | 1274 21 14 23 30 28 204 |MD 26 30 32 38 32 66 24
Table 3.1589.2 GPS week: 1589 Day: 2 MJD: 55369
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1598 19 12 29 29 35 --- 13 | 15 14 37 33 35 --- 16
R02E | 3105 19 11 36 24 34 --- 14 | 24 21 46 33 25 --- 23
R03E | 2759 14 16 32 39 36 --- 14 | 19 23 48 42 39 --- 25
R04E | 1318 22 12 11 32 46 --- 14 | 23 25 33 37 47 --- 25
R05E | 1305 22 25 30 29 46 --- 17 | 34 50 55 48 53 --- 42
R07E | 1457 20 13 27 --- 23 --- 12 | 34 30 47 --- 31 --- 31
R08E | 2041 22 19 28 34 34 --- 14 | 64 64 82 76 78 --- 67
R10 | 2853 14 8 22 16 25 --- 9 | 29 21 38 33 31 --- 26
R11 | 1062 14 15 17 33 16 --- 9 | 30 27 35 35 27 --- 25
R13 | 1090 21 19 23 14 19 --- 12 | 18 30 39 25 22 --- 23
R14 | 1133 17 26 11 16 36 --- 13 | 20 41 32 30 19 --- 26
R15 | 1692 12 8 30 19 22 74 10 | 27 17 26 23 18 66 17
R17 | 989 16 18 18 30 36 --- 12 | 18 35 26 27 32 --- 23
R18 | 1368 16 10 13 23 9 --- 7 | 19 32 29 31 29 --- 25
R19 | 1930 12 14 20 24 18 --- 9 | 27 45 45 46 36 --- 37
R20 | 1299 26 12 41 33 45 --- 17 | 23 22 52 36 42 --- 23
R21 | 1924 20 10 41 47 22 --- 14 | 61 63 78 85 77 --- 65
R22 | 1033 16 14 20 20 19 --- 10 | 55 63 52 58 74 --- 59
R23 | 956 25 16 20 19 19 186 11 | 24 53 53 45 42 114 41
R24 | 1940 11 16 19 21 20 --- 9 | 35 39 32 29 30 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 1758 18 16 26 28 30 142 |T 29 35 44 40 39 90 32
WRMS | 1758 18 15 24 28 30 142 |NE 29 37 41 38 36 90 32
MEDI | 1368 17 14 22 24 23 74 |MD 24 30 39 35 32 66 25
Table 3.1589.3 GPS week: 1589 Day: 3 MJD: 55370
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1153 23 14 23 32 25 --- 12 | 18 22 39 38 24 --- 18
R02E | 2649 22 16 19 30 34 --- 13 | 31 29 33 32 30 --- 23
R03E | 2758 15 14 26 29 36 --- 13 | 23 19 42 44 33 --- 22
R04E | 1962 23 14 21 35 26 --- 11 | 34 17 42 51 40 --- 26
R05E | 1033 22 19 26 40 41 --- 15 | 24 27 41 47 46 --- 24
R07E | 2760 23 19 24 38 25 --- 13 | 32 55 65 43 30 --- 45
R08E | 1972 27 27 26 31 33 --- 16 | 44 57 69 57 58 --- 52
R10 | 1423 14 12 16 14 38 --- 11 | 24 26 47 43 34 --- 28
R11 | 1048 17 13 20 23 16 --- 9 | 35 31 43 41 32 --- 31
R13 | 1599 21 9 26 34 34 --- 13 | 19 31 42 36 23 --- 26
R14 | 1077 23 17 35 24 28 --- 14 | 41 33 26 36 32 --- 28
R15 | 2460 35 11 35 18 20 117 14 | 21 29 35 27 19 30 21
R17 | 987 37 21 32 24 53 --- 20 | 40 39 29 32 48 --- 34
R18 | 2449 27 14 39 29 12 --- 14 | 24 36 55 42 30 --- 32
R19 | 1018 16 8 14 27 29 --- 9 | 29 32 33 45 28 --- 28
R20 | 1007 32 20 32 33 28 --- 16 | 26 52 53 57 37 --- 39
R21 | 1273 15 17 18 19 36 --- 12 | 63 80 95 80 82 --- 77
R22 | 1845 29 16 32 24 25 --- 14 | 56 63 49 54 66 --- 56
R23 | 1323 25 10 25 19 26 111 12 | 25 42 41 45 49 71 36
R24 | 1239 22 8 14 20 15 --- 8 | 27 52 47 52 57 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 1769 24 16 26 28 30 114 |T 31 38 46 45 39 50 34
WRMS | 1769 24 14 26 28 30 114 |NE 33 42 45 45 41 50 37
MEDI | 1323 23 14 25 27 28 111 |MD 27 32 42 43 33 30 28
Table 3.1589.4 GPS week: 1589 Day: 4 MJD: 55371
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1106 21 11 21 38 18 --- 9 | 16 21 38 40 33 --- 22
R02E | 2518 21 13 23 27 24 --- 11 | 20 27 34 36 38 --- 25
R03E | 2361 18 14 23 34 29 --- 11 | 23 26 42 27 30 --- 22
R04E | 2044 20 12 33 36 32 --- 13 | 50 35 53 55 35 --- 35
R05E | 1745 21 14 34 39 26 --- 13 | 33 22 48 50 35 --- 27
R07E | 2242 23 18 33 31 31 --- 14 | 38 54 60 44 36 --- 44
R08E | 746 36 14 29 32 26 509 14 | 58 64 86 83 74 360 67
R10 | 1321 18 7 43 40 33 --- 14 | 23 26 29 38 24 --- 21
R11 | 886 13 13 21 29 29 --- 10 | 35 33 46 44 42 --- 35
R13 | 997 33 12 19 24 27 --- 12 | 19 27 35 40 30 --- 24
R14 | 1005 15 14 29 34 34 --- 12 | 29 32 49 39 35 --- 28
R15 | 3747 30 17 29 31 32 116 15 | 30 41 42 47 29 20 31
R17 | 1021 30 9 44 27 40 --- 17 | 40 55 91 57 40 --- 54
R18 | 989 20 9 18 16 24 --- 9 | 31 27 22 20 27 --- 19
R19 | 892 14 10 20 16 17 --- 8 | 31 40 36 40 22 --- 31
R20 | 1018 25 14 33 43 24 --- 13 | 23 36 57 35 40 --- 36
R21 | 736 34 16 18 13 36 --- 14 | 54 74 85 75 88 --- 72
R22 | 2306 30 7 29 30 25 --- 12 | 48 55 76 59 71 --- 58
R23 | 1279 33 10 15 29 17 122 11 | 22 44 43 45 44 60 37
R24 | 1751 27 10 25 16 24 --- 12 | 24 40 55 46 51 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1716 25 13 28 30 28 309 |T 32 38 51 46 41 146 36
WRMS | 1716 24 12 27 30 28 309 |NE 31 40 51 45 41 40 37
MEDI | 1106 21 12 25 30 26 122 |MD 30 35 46 44 35 60 31
Table 3.1589.5 GPS week: 1589 Day: 5 MJD: 55372
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1774 22 17 38 37 30 --- 15 | 18 28 49 35 28 --- 26
R02E | 2238 23 16 25 44 24 --- 12 | 18 26 35 49 26 --- 20
R03E | 1821 31 10 36 21 23 --- 13 | 18 30 39 42 28 --- 25
R04E | 1275 16 11 21 17 24 --- 10 | 25 28 42 33 31 --- 27
R05E | 2467 17 14 39 24 37 --- 15 | 34 41 61 43 35 --- 39
R07 | 1535 25 8 22 27 25 --- 11 | 46 51 63 32 50 --- 50
R08E | 2495 25 12 22 26 26 361 11 | 52 59 69 58 64 290 59
R10 | 1394 33 13 32 20 24 --- 14 | 15 22 33 25 31 --- 20
R11 | 2271 29 12 20 19 25 --- 11 | 22 31 39 27 31 --- 26
R13 | 1855 44 11 21 22 18 --- 13 | 17 28 37 25 27 --- 25
R14 | 1655 34 12 20 46 41 --- 15 | 18 28 42 56 35 --- 26
R15 | 3012 24 15 27 30 23 92 12 | 24 32 36 43 26 21 26
R17 | 1542 54 4 29 20 32 --- 17 | 45 48 60 49 39 --- 48
R18 | 1736 15 7 25 18 14 --- 8 | 14 19 30 23 17 --- 16
R19 | 1446 27 11 20 18 17 --- 10 | 29 29 34 32 23 --- 22
R20 | 2865 27 22 41 26 28 --- 16 | 45 48 33 42 37 --- 39
R21 | 2114 28 11 15 21 15 --- 9 | 79 90 92 82 90 --- 88
R22 | 2506 27 14 26 18 26 --- 12 | 50 58 76 69 67 --- 61
R23 | 1336 24 17 26 22 20 175 12 | 21 32 46 44 49 97 34
R24 | 2336 18 12 21 27 22 --- 10 | 30 32 52 42 45 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 2047 29 13 27 26 26 238 |T 31 38 48 42 38 136 35
WRMS | 2047 29 13 26 27 26 238 |NE 31 38 46 43 39 59 35
MEDI | 1821 25 12 25 22 24 175 |MD 24 31 42 42 31 97 26
Table 3.1589.6 GPS week: 1589 Day: 6 MJD: 55373
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2593 10 14 15 26 28 --- 10 | 23 30 40 30 26 --- 26
R02E | 2726 17 17 26 25 22 --- 11 | 26 35 44 42 30 --- 28
R03E | 1960 13 29 32 25 29 --- 15 | 20 35 40 35 27 --- 26
R04E | 1137 15 19 15 23 20 --- 10 | 40 43 46 40 28 --- 37
R05E | 1772 14 14 22 27 28 --- 11 | 33 38 52 45 25 --- 33
R07 | 2498 15 10 24 13 20 --- 10 | 51 59 61 33 43 --- 52
R08E | 4943 23 19 17 31 26 495 12 | 49 56 67 66 57 462 55
R10 | 2152 19 15 24 25 9 --- 10 | 29 32 28 29 25 --- 26
R11 | 2140 23 19 36 24 18 --- 13 | 29 35 41 36 30 --- 28
R13 | 2453 14 18 15 22 20 --- 10 | 21 35 38 37 36 --- 31
R14 | 2153 15 11 20 24 15 --- 8 | 24 26 29 27 31 --- 23
R15 | 5005 27 6 28 15 24 100 12 | 33 22 34 28 33 39 22
R17 | 1566 46 14 41 32 37 --- 20 | 60 55 60 57 40 --- 51
R18 | 2839 23 11 36 50 19 --- 13 | 21 28 34 54 32 --- 26
R19 | 1201 26 9 41 15 14 --- 13 | 32 24 44 32 20 --- 24
R20 | 3113 17 21 36 17 20 --- 13 | 35 44 50 39 37 --- 36
R21 | 1587 25 19 30 17 18 --- 13 | 76 91 87 82 83 --- 83
R22 | 2326 29 23 20 14 22 --- 14 | 80 69 72 73 77 --- 73
R23 | 1308 18 19 35 21 21 57 13 | 28 38 38 38 48 149 34
R24 | 2356 9 17 35 33 15 --- 11 | 37 42 52 53 45 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 2597 21 17 29 25 22 294 |T 37 41 47 43 38 216 37
WRMS | 2597 19 15 27 25 22 294 |NE 38 41 46 45 41 94 38
MEDI | 2153 17 17 26 24 20 100 |MD 32 35 44 38 32 149 31
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