[IGSREPORT-18903] Wk 1596 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 26 09:52:03 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1596 (Aug 08, 2010 - Aug 14, 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 2.1596.
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:
igl1596[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1596 in the SP3 format.
igl15967.sum Combination Report for GPS Week 1596.
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 | 449.2 ns
1 | 365.4 ns
2 | 393.7 ns
3 | 387.5 ns
4 | 400.3 ns
5 | 452.9 ns
6 | 370.6 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 1.1596, 1a.1596).
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 2.1596.0-6)
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 3.1596.0-6).
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 1596 summary. (Aug 08, 2010 - Aug 14, 2010)
Table 1.1596.a GPS week : 1596 MJD: 55416.0-55422.0
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| 1 0 -1 1 3 -46 -.15 26 23 | 0 -35 1906 1985
| 1 1 6 33 26 118 .01 | 0 398
cod 233| -2 0 -1 43 3 41 -.11 17 14 | --- --- --- ---
| 0 0 3 20 10 41 .02 | --- ---
esx 130| 0 1 -2 -15 7 16 .47 25 22 | 86217 502 4129 8851
| 2 1 3 15 14 64 .04 | 34718 3248
gfz 195| -1 0 -2 -79 -20 57 -.15 28 25 | 238195 62 4120 8456
| 2 1 6 36 57 61 .07 | 34642 2393
iac n/a| 3 0 8 -52 -15 -21 -.21 28 28 | 403210 -773 4115 8851
| 1 0 9 17 15 60 .03 | 35325 849
mcc n/a| 4 0 37 -32 -35 385 .07 164 164 | --- --- --- ---
| 12 9 18 121 121 406 .34 | --- ---
Table 1.1596.b GPS week : 1596 MJD: 55416.0-55422.0
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 | 10 9 9 10 11 10 14 |
R02 | 10 8 8 10 11 12 11 |
R03 | 10 14 11 10 11 8 12 |
R04 | 10 9 8 8 13 11 16 |
R05 | 10 10 10 11 10 10 15 |
R07 | 11 16 13 12 11 12 10 |
R08 | 11 9 11 10 11 13 9 |
R10 | 8 8 11 12 13 10 11 |
R11 | 17 21 17 20 20 16 16 |
R13 | 11 12 14 12 7 8 12 |
R14 | 15 18 15 10 10 10 13 |
R15 | 12 14 12 14 13 12 10 |
R17 | 14 11 24 11 14 14 17 |
R18 | 8 9 15 9 13 14 18 |
R19 | 9 23 38 23 11 13 19 |
R20 | 13 14 25 28 16 16 19 |
R21 | 15 20 36 17 12 12 12 |
R22 | 13 11 15 12 11 12 16 |
R23 | 8 9 14 16 12 13 14 |
R24 | 11 9 14 11 11 12 10 |
Table 1.1596.c GPS week : 1596 MJD: 55416.0-55422.0
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 1596 0 | -42 -58 495 -1073 -2174 -21240 87.3 1833 1833 | 449178 0
brd 1596 1 | 19 -41 346 -2543 -2400 -13330 87.7 2146 2146 | 365442 0
brd 1596 2 | 67 -105 393 -1079 -1010 -10240 86.4 2054 2054 | 393727 0
brd 1596 3 | -25 -111 373 -456 -2487 -14680 85.8 2300 2300 | 387516 0
brd 1596 4 | 43 -37 334 755 -2464 -12070 87.4 1893 1893 | 400337 0
brd 1596 5 | -15 -31 311 -1886 -2257 -7709 88.9 1518 1518 | 452924 0
brd 1596 6 | 38 38 278 878 -147 -4318 88.5 1628 1628 | 370598 0
-------------+------------------------------------------------------------+----------------
brd 1596 mean| 12 -49 361 -771 -1848 -11941 87.4 1910 1910 | 402817 0
brd 1596 sdev| 40 50 70 1272 909 5398 1.1 279 279 | 35161 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 2.1596.0 GPS week: 1596 Day: 0 MJD: 55416
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 -6 22 13 -45 -.13 19 19 | 0 114 1825 1890
cod 233| -1 0 -3 30 2 31 -.15 14 14 | --- --- --- ---
esx 130| -1 1 -3 -20 7 81 .45 20 18 | 128162 4850 3943 8782
gfz 195| -1 2 -4 -51 6 85 -.08 21 20 | 282766 3675 3943 8371
iac n/a| 3 0 18 -32 -28 -84 -.20 26 26 | 449980 447 3916 8464
mcc n/a| -13 -11 67 -29 -142 411 .06 131 131 | --- --- --- ---
Table 2.1596.1 GPS week: 1596 Day: 1 MJD: 55417
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 -12 -14 7 65 -.17 28 24 | 0 55 2152 2224
cod 233| -3 0 -2 83 6 18 -.13 17 16 | --- --- --- ---
esx 130| -1 -1 -1 -34 20 -37 .40 23 20 | 46687 -103 5027 8839
gfz 195| -1 0 -2 -99 8 0 -.15 25 30 | 201137 -2897 5028 8279
iac n/a| 2 1 20 -70 -25 -58 -.16 27 27 | 365842 -575 5030 8717
mcc n/a| -13 3 24 2 -207 235 -.28 222 222 | --- --- --- ---
Table 2.1596.2 GPS week: 1596 Day: 2 MJD: 55418
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| 0 -3 0 64 52 98 -.15 38 29 | 0 -93 1621 1712
cod 233| -2 2 -2 20 -4 40 -.11 23 15 | --- --- --- ---
esx 130| 0 2 -2 -22 -10 -86 .48 32 24 | 73814 2916 4158 9683
gfz 195| 0 2 0 -68 4 -50 -.06 37 33 | 226549 2486 4138 9220
iac n/a| 1 0 10 -34 0 -22 -.24 32 32 | 394195 -2230 4179 9703
mcc n/a| 8 -6 19 -67 -72 426 -.12 369 369 | --- --- --- ---
Table 2.1596.3 GPS week: 1596 Day: 3 MJD: 55419
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 0 6 3 -2 17 -.14 30 25 | 0 660 2239 2327
cod 233| -3 0 -3 46 -3 7 -.12 17 13 | --- --- --- ---
esx 130| 5 0 -10 -29 23 27 .49 26 23 | 69109 -1724 4538 8662
gfz 195| -2 0 -13 -18 -10 71 -.19 31 24 | 222828 -461 4513 8187
iac n/a| 2 0 13 -62 -14 -42 -.24 26 26 | 389756 -373 4510 8946
mcc n/a| 14 4 22 55 -56 396 -.12 77 77 | --- --- --- ---
Table 2.1596.4 GPS week: 1596 Day: 4 MJD: 55420
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 0 3 -37 -28 -161 -.15 20 19 | 0 -671 2093 2203
cod 233| -2 0 -3 38 21 94 -.08 16 15 | --- --- --- ---
esx 130| -3 2 0 4 18 30 .48 25 22 | 78689 -2389 3774 9320
gfz 195| -5 0 2 -108 -142 114 -.17 28 22 | 236296 -1691 3761 9066
iac n/a| 3 0 5 -65 -18 -50 -.21 25 25 | 398371 -337 3756 9445
mcc n/a| 8 10 55 -86 140 913 .69 112 112 | --- --- --- ---
Table 2.1596.5 GPS week: 1596 Day: 5 MJD: 55421
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 -2 1 -25 -23 -224 -.16 19 19 | 0 -183 1738 1810
cod 233| -3 1 2 33 7 102 -.10 15 14 | --- --- --- ---
esx 130| 1 3 0 3 7 1 .53 24 23 | 140996 3477 3702 7998
gfz 195| 0 1 5 -126 -40 111 -.18 27 23 | 289123 893 3694 7452
iac n/a| 2 0 -4 -34 11 100 -.17 26 26 | 453742 -1238 3674 7667
mcc n/a| 5 -13 38 141 15 -383 .37 141 141 | --- --- --- ---
Table 2.1596.6 GPS week: 1596 Day: 6 MJD: 55422
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| 0 0 -3 -3 6 -78 -.16 25 23 | 0 -127 1674 1730
cod 233| -3 1 5 49 -7 -1 -.10 15 14 | --- --- --- ---
esx 130| 0 1 1 -11 -15 96 .46 26 24 | 66063 -3507 3763 8679
gfz 195| 0 0 -5 -80 30 74 -.25 29 23 | 208667 -1569 3765 8617
iac n/a| 6 0 -2 -68 -32 5 -.25 33 33 | 370584 -1105 3741 9020
mcc n/a| 19 7 34 -245 74 696 -.11 97 97 | --- --- --- ---
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 3.1596.0 GPS week: 1596 Day: 0 MJD: 55416
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2734 13 14 19 18 23 --- 10 | 28 39 45 44 34 --- 35
R02 | 1107 10 17 22 17 17 --- 10 | 29 29 42 30 28 --- 29
R03 | 1957 20 11 19 19 17 --- 9 | 42 42 44 42 44 --- 41
R04 | 2244 10 19 17 17 22 --- 10 | 25 29 36 29 25 --- 25
R05 | 2028 20 13 18 28 17 --- 10 | 31 34 35 41 26 --- 29
R07 | 3355 24 15 12 15 25 --- 11 | 32 50 40 38 27 --- 39
R08 | 1150 13 17 17 26 27 155 10 | 22 38 39 34 24 47 30
R10 | 1470 11 11 15 21 17 --- 7 | 18 36 33 33 30 --- 27
R11 | 2298 26 16 21 28 52 --- 16 | 44 36 45 45 18 --- 32
R13 | 1147 21 11 24 19 17 --- 10 | 19 20 27 27 30 --- 18
R14 | 1779 34 11 22 25 36 --- 15 | 42 55 61 69 58 --- 52
R15 | 1847 18 13 16 14 35 103 12 | 21 22 23 22 17 83 18
R17 | 2857 30 16 26 17 25 --- 14 | 103 93 103 102 103 --- 99
R18 | 1458 13 14 15 19 15 --- 8 | 68 65 74 69 67 --- 67
R19 | 1033 9 14 15 22 24 --- 9 | 92 81 84 90 84 --- 83
R20 | 1416 16 16 23 26 33 --- 12 | 64 70 76 78 77 --- 69
R21 | 1121 23 16 35 21 23 --- 14 | 90 96 113 104 102 --- 99
R22 | 976 23 16 23 23 26 --- 12 | 91 105 102 104 91 --- 97
R23 | 1073 12 8 16 20 19 130 7 | 83 88 91 89 86 192 86
R24 | 905 13 12 20 17 27 --- 10 | 74 74 89 80 78 --- 76
------+-----------------------------------------+-------------------------------------
RMS | 1832 19 14 20 21 26 131 |T 50 55 60 58 52 107 52
WRMS | 1832 19 14 18 20 26 131 |NE 25 35 36 33 25 65 29
MEDI | 1458 16 14 19 19 23 130 |MD 42 42 45 44 34 83 39
Table 3.1596.1 GPS week: 1596 Day: 1 MJD: 55417
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2745 10 10 16 14 21 --- 8 | 41 44 52 49 34 --- 42
R02M | 2002 12 13 14 25 12 --- 7 | 15 28 25 33 21 --- 19
R03 | 2616 15 16 33 25 31 --- 14 | 29 40 58 48 36 --- 38
R04 | 2044 17 13 10 26 22 --- 9 | 21 27 27 24 20 --- 21
R05 | 2278 9 18 14 26 21 --- 9 | 35 42 35 33 30 --- 34
R07 | 4172 38 24 19 19 30 --- 16 | 31 47 35 40 31 --- 34
R08 | 1245 16 13 11 19 23 87 9 | 21 28 34 35 21 56 24
R10 | 1818 9 10 14 18 21 --- 8 | 27 40 36 42 40 --- 34
R11 | 2524 48 15 38 30 41 --- 20 | 50 33 35 30 20 --- 24
R13 | 1453 19 22 14 27 25 --- 12 | 19 42 21 22 20 --- 22
R14 | 1472 46 18 30 27 32 --- 18 | 43 56 65 64 56 --- 54
R15 | 3985 17 24 24 21 28 88 13 | 23 17 25 32 23 69 17
R17 | 2536 15 16 16 21 27 --- 11 | 82 60 54 58 59 --- 60
R18 | 2014 12 12 13 19 21 --- 8 | 78 70 74 68 74 --- 72
R19 | 739 60 28 32 47 42 --- 23 | 47 104 113 110 71 --- 83
R20 | 1125 30 11 30 28 25 --- 14 | 59 74 93 85 75 --- 74
R21 | 1070 47 20 39 21 29 --- 19 | 85 96 118 97 112 --- 98
R22 | 687 19 11 24 27 20 --- 11 | 67 66 76 72 59 --- 65
R23 | 809 18 11 14 21 20 363 9 | 63 68 64 61 64 200 63
R24 | 970 18 12 16 19 20 --- 9 | 89 84 96 99 96 --- 89
------+-----------------------------------------+-------------------------------------
RMS | 2145 28 17 23 25 27 222 |T 46 53 56 55 48 108 48
WRMS | 2145 24 16 20 30 27 222 |NE 27 32 34 36 25 62 27
MEDI | 1818 17 13 16 21 23 88 |MD 41 44 52 48 36 69 38
Table 3.1596.2 GPS week: 1596 Day: 2 MJD: 55418
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1911 13 16 14 26 18 --- 9 | 23 37 34 44 20 --- 27
R02 | 1707 11 11 18 18 16 --- 8 | 32 34 37 36 32 --- 30
R03M | 2163 18 8 17 27 26 --- 10 | 42 43 57 59 40 --- 44
R04 | 1719 13 11 17 19 15 --- 8 | 24 31 35 30 26 --- 27
R05M | 2081 22 7 16 19 21 --- 9 | 29 31 36 31 23 --- 26
R07 | 2848 36 13 19 14 20 --- 13 | 29 41 39 40 33 --- 34
R08 | 1503 27 16 13 23 18 84 10 | 29 38 26 36 28 38 28
R10M | 1636 19 10 25 20 17 --- 10 | 25 40 49 50 32 --- 35
R11M | 2026 38 20 35 26 24 --- 16 | 29 41 41 29 32 --- 33
R13M | 1402 21 20 28 33 26 --- 13 | 30 27 28 33 29 --- 20
R14M | 1790 26 22 24 19 27 --- 14 | 55 80 73 76 62 --- 66
R15 | 5216 11 15 20 24 30 61 11 | 23 26 47 34 22 45 26
R17 | 2172 62 25 39 46 36 --- 23 | 88 125 154 155 124 --- 122
R18E | 1099 33 26 19 44 23 --- 15 | 44 80 82 93 64 --- 67
R19 | 827 73 50 73 85 69 --- 37 | 54 100 122 130 82 --- 74
R20E | 2285 39 32 37 36 62 --- 25 | 95 114 128 123 110 --- 105
R21 | 1580 93 47 65 72 40 --- 35 | 71 142 161 166 82 --- 109
R22E | 692 36 16 25 45 28 --- 15 | 65 69 84 85 71 --- 69
R23E | 746 27 17 24 30 28 631 13 | 46 68 73 68 63 369 60
R24E | 948 27 18 30 33 24 --- 14 | 65 85 101 90 69 --- 78
------+-----------------------------------------+-------------------------------------
RMS | 2053 38 23 32 37 32 369 |T 44 62 70 70 52 150 54
WRMS | 2053 29 15 24 33 32 369 |NE 25 34 36 36 25 41 28
MEDI | 1707 27 16 24 26 24 84 |MD 32 41 49 50 33 45 35
Table 3.1596.3 GPS week: 1596 Day: 3 MJD: 55419
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1421 22 14 16 19 14 --- 9 | 42 45 43 49 44 --- 41
R02 | 2105 16 10 20 26 25 --- 10 | 27 29 38 39 21 --- 25
R03 | 1336 16 11 23 16 19 --- 10 | 33 38 37 36 36 --- 33
R04 | 1388 16 9 19 27 14 --- 8 | 33 39 41 43 37 --- 36
R05 | 1532 24 15 11 21 22 --- 10 | 39 42 40 38 32 --- 36
R07 | 1782 28 15 21 17 17 --- 11 | 19 34 35 23 32 --- 27
R08 | 1137 27 10 15 20 15 96 9 | 24 35 32 22 31 47 28
R10 | 1808 12 19 29 19 16 --- 11 | 20 40 23 26 28 --- 25
R11 | 1791 42 22 35 24 42 --- 20 | 72 65 86 65 57 --- 65
R13 | 1699 20 10 19 28 31 --- 11 | 87 84 82 79 71 --- 80
R14 | 1479 19 11 15 23 25 --- 10 | 28 38 43 55 52 --- 38
R15 | 6447 15 16 22 32 37 50 14 | 27 30 32 36 31 54 25
R17E | 1631 22 11 24 31 23 --- 11 | 120 123 124 130 131 --- 123
R18E | 1380 25 8 13 17 15 --- 9 | 69 74 75 66 55 --- 67
R19E | 1831 54 29 39 76 37 --- 22 | 57 92 111 126 75 --- 81
R20E | 2534 60 33 52 50 51 --- 27 | 97 120 141 129 117 --- 113
R21E | 3286 47 15 30 30 26 --- 17 | 108 129 128 121 123 --- 121
R22E | 1027 23 13 26 27 22 --- 12 | 84 88 92 96 85 --- 86
R23E | 2779 28 23 38 22 14 --- 15 | 72 84 93 81 75 --- 79
R24E | 1337 28 11 23 29 17 --- 11 | 130 125 148 145 133 --- 131
------+-----------------------------------------+-------------------------------------
RMS | 2300 30 17 26 31 26 77 |T 59 67 72 70 63 50 63
WRMS | 2300 25 13 23 24 26 77 |NE 29 36 36 34 35 50 31
MEDI | 1631 23 13 22 24 22 50 |MD 42 45 43 55 52 47 41
Table 3.1596.4 GPS week: 1596 Day: 4 MJD: 55420
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1553 23 11 22 16 20 --- 11 | 22 28 44 36 29 --- 27
R02 | 2749 15 15 24 28 18 --- 10 | 28 39 45 38 35 --- 34
R03 | 981 20 14 13 19 29 --- 11 | 50 44 37 33 27 --- 38
R04 | 564 27 10 24 16 29 --- 13 | 19 24 47 38 29 --- 25
R05 | 836 14 16 14 25 21 --- 9 | 27 34 33 40 23 --- 27
R07 | 926 26 11 19 15 18 --- 11 | 23 37 47 32 30 --- 31
R08 | 1097 11 17 18 20 27 137 10 | 22 30 24 28 20 75 21
R10 | 1553 15 11 29 24 30 --- 12 | 25 37 37 42 37 --- 31
R11 | 1342 19 29 50 32 34 --- 19 | 114 132 129 123 127 --- 124
R13 | 1188 12 8 14 17 11 --- 6 | 117 120 119 117 120 --- 119
R14 | 1077 12 14 26 37 17 --- 10 | 36 38 47 53 37 --- 36
R15 | 4445 23 19 16 36 31 80 13 | 17 23 35 31 25 96 21
R17E | 884 27 12 21 37 35 --- 13 | 105 100 114 110 95 --- 103
R18E | 1233 17 21 24 30 29 --- 13 | 47 61 55 53 48 --- 51
R19E | 2668 23 8 19 31 23 --- 10 | 71 74 83 78 89 --- 76
R20E | 2637 27 20 34 37 32 --- 16 | 70 83 93 92 73 --- 78
R21E | 3197 19 18 26 34 15 --- 11 | 67 65 86 80 66 --- 68
R22E | 759 19 10 23 28 24 --- 11 | 61 75 80 79 70 --- 70
R23E | 1505 17 21 20 27 28 --- 12 | 58 67 63 67 65 --- 61
R24E | 1280 17 15 28 34 18 --- 11 | 64 67 75 73 60 --- 64
------+-----------------------------------------+-------------------------------------
RMS | 1892 20 16 25 28 25 112 |T 52 58 64 62 55 85 55
WRMS | 1892 19 15 22 22 25 112 |NE 20 28 39 33 26 85 25
MEDI | 1233 19 14 22 28 24 80 |MD 47 44 47 53 37 75 38
Table 3.1596.5 GPS week: 1596 Day: 5 MJD: 55421
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3127 16 13 22 20 17 --- 9 | 24 30 30 35 23 --- 24
R02 | 1570 19 13 31 28 14 --- 11 | 36 33 59 59 29 --- 37
R03 | 1231 13 11 18 25 15 --- 8 | 21 27 27 35 30 --- 23
R04 | 721 23 8 13 33 30 --- 11 | 34 33 30 29 29 --- 29
R05 | 1212 15 12 23 20 21 --- 10 | 31 24 36 23 20 --- 22
R07 | 1282 15 19 31 19 17 --- 12 | 16 24 32 29 16 --- 15
R08 | 832 20 13 22 16 36 72 13 | 33 37 42 35 18 55 26
R10 | 1655 15 9 22 15 23 --- 10 | 21 26 48 34 27 --- 27
R11 | 1075 26 22 27 36 37 --- 16 | 194 195 193 196 192 --- 193
R13 | 1261 13 9 13 26 17 --- 7 | 141 142 137 149 147 --- 141
R14 | 1367 12 11 19 26 23 --- 9 | 28 26 17 34 25 --- 18
R15 | 2260 25 15 15 22 28 72 12 | 20 30 33 30 30 67 25
R17E | 727 23 17 30 29 30 --- 14 | 78 77 88 80 72 --- 77
R18E | 916 23 16 29 27 33 --- 14 | 28 42 58 53 40 --- 36
R19E | 2610 17 16 19 26 34 --- 12 | 35 37 49 46 48 --- 35
R20E | 968 23 20 32 35 36 --- 15 | 76 75 90 91 76 --- 76
R21E | 1609 16 20 25 22 18 --- 11 | 53 63 66 62 56 --- 58
R22E | 1075 20 19 23 33 23 --- 12 | 37 35 47 50 38 --- 34
R23E | 1015 28 15 26 30 20 223 13 | 29 32 50 47 43 163 33
R24E | 1280 18 17 26 34 23 --- 12 | 107 88 105 113 108 --- 99
------+-----------------------------------------+-------------------------------------
RMS | 1518 19 15 24 27 26 141 |T 52 53 61 61 53 95 51
WRMS | 1518 19 14 23 23 26 141 |NE 25 30 33 31 23 61 23
MEDI | 1231 18 15 23 26 23 72 |MD 33 33 48 46 30 67 33
Table 3.1596.6 GPS week: 1596 Day: 6 MJD: 55422
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2388 22 9 24 18 40 --- 13 | 21 28 35 18 30 --- 21
R02 | 1234 17 10 13 19 33 --- 10 | 36 39 36 37 31 --- 32
R03 | 1274 25 13 20 21 25 --- 12 | 31 36 36 32 24 --- 28
R04 | 1933 32 19 31 22 29 --- 15 | 25 39 33 35 23 --- 27
R05 | 999 23 19 19 22 42 --- 14 | 29 36 25 26 35 --- 23
R07 | 1417 15 12 14 30 29 --- 10 | 23 37 31 31 24 --- 25
R08 | 1874 12 14 19 15 16 51 9 | 20 33 31 28 16 65 22
R10 | 1054 23 15 18 16 18 --- 10 | 16 26 29 23 26 --- 19
R11 | 985 19 16 27 28 50 --- 16 | 220 221 229 220 217 --- 221
R13 | 1972 16 14 26 18 30 --- 12 | 203 203 210 203 201 --- 203
R14 | 1867 21 16 30 19 24 --- 13 | 24 24 22 25 28 --- 17
R15 | 1482 21 11 16 20 24 82 10 | 25 29 22 18 18 50 21
R17E | 1564 13 23 25 21 55 --- 17 | 139 129 143 131 143 --- 136
R18E | 1538 41 16 41 40 20 --- 17 | 61 70 75 74 67 --- 65
R19E | 2022 42 16 39 44 31 --- 18 | 86 99 111 110 103 --- 95
R20E | 1577 27 19 34 52 54 --- 18 | 69 73 105 91 77 --- 78
R21E | 1353 23 8 23 41 31 --- 12 | 89 95 119 115 97 --- 98
R22E | 1758 33 15 29 32 34 --- 15 | 85 86 95 89 87 --- 86
R23E | 2010 28 18 29 31 24 138 14 | 78 93 91 86 95 110 87
R24E | 1367 14 16 21 23 20 --- 10 | 96 92 102 100 94 --- 95
------+-----------------------------------------+-------------------------------------
RMS | 1628 25 15 26 29 33 97 |T 68 74 79 74 71 75 69
WRMS | 1628 23 14 24 23 33 97 |NE 22 33 30 26 22 57 23
MEDI | 1538 22 15 24 22 29 82 |MD 36 39 36 37 35 65 32
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