[IGSREPORT-19059] Wk 1603 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Oct 14 07:41:43 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1603 (Sep 26, 2010 - Oct 02, 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 2.1603.
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:
igl1603[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1603 in the SP3 format.
igl16037.sum Combination Report for GPS Week 1603.
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 | 445.4 ns
1 | 359.0 ns
2 | 438.1 ns
3 | 370.1 ns
4 | 371.8 ns
5 | 373.0 ns
6 | 575.1 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 1.1603, 1a.1603).
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 2.1603.0-6)
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 3.1603.0-6).
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 1603 summary. (Sep 26, 2010 - Oct 02, 2010)
Table 1.1603.a GPS week : 1603 MJD: 55465.0-55471.0
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 125| 0 2 0 -6 -2 23 -.16 22 21 | 0 47523 20028 28317
| 1 0 2 9 45 90 .04 | 0 125978
cod 233| 0 -1 2 41 -9 24 -.12 16 15 | --- --- --- ---
| 1 0 3 9 15 47 .04 | --- ---
esx 146| 0 0 2 -11 4 0 .46 22 21 | 90732 363 4237 8269
| 1 0 4 30 32 39 .03 | 73025 5853
gfz 195| 1 3 1 -86 22 6 -.14 29 27 | 241081 162 4245 8031
| 1 2 5 37 72 92 .08 | 79170 5551
iac n/a| 0 0 -5 -49 16 -60 -.21 27 27 | 419537 -875 4233 8481
| 1 0 12 18 8 62 .04 | 77339 1576
mcc n/a| 0 -8 20 -76 94 -47 -.39 107 107 | --- --- --- ---
| 13 11 12 161 145 551 .64 | --- ---
Table 1.1603.b GPS week : 1603 MJD: 55465.0-55471.0
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 | 13 15 11 13 13 16 14 |
R02 | 9 12 13 12 14 14 12 |
R04 | 12 16 13 14 12 0 --- |
R05 | 8 11 11 13 16 14 16 |
R07 | 11 12 11 12 13 16 13 |
R08 | 8 11 12 16 9 12 12 |
R09 | --- --- --- --- --- 0 147 |
R10 | 9 14 12 12 14 20 18 |
R11 | 23 22 20 17 20 18 19 |
R13 | 12 17 15 10 10 10 11 |
R14 | 12 11 18 16 15 16 15 |
R15 | 11 13 12 11 13 11 13 |
R16 | --- 0 0 0 0 --- --- |
R17 | 11 11 13 11 9 12 9 |
R18 | 12 11 11 10 9 9 10 |
R19 | 9 8 9 10 8 8 10 |
R20 | 11 14 14 14 12 12 8 |
R21 | 11 8 11 10 10 9 9 |
R22 | 8 16 8 9 8 9 10 |
R23 | 11 10 13 10 12 8 11 |
R24 | 11 11 12 10 10 10 11 |
Table 1.1603.c GPS week : 1603 MJD: 55465.0-55471.0
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 1603 0 | 9 14 156 -1018 652 -16940 84.8 2025 2025 | 445389 0
brd 1603 1 | -3 56 85 -833 2027 -14530 86.3 1930 1930 | 358967 0
brd 1603 2 | 50 -36 154 1167 1188 -11360 86.6 2313 2313 | 438053 0
brd 1603 3 | 163 34 167 1234 970 -16510 85.5 2687 2687 | 370057 0
brd 1603 4 | 48 40 211 -915 172 -17280 88.1 2978 2978 | 371762 0
brd 1603 5 | 4 -104 63 557 1959 -18750 88.1 2365 2365 | 373035 0
brd 1603 6 | 38 -44 99 -1193 -310 -20200 86.9 1822 1822 | 575068 0
-------------+------------------------------------------------------------+----------------
brd 1603 mean| 44 -5 134 -143 951 -16510 86.6 2302 2302 | 418904 0
brd 1603 sdev| 57 58 52 1083 867 2882 1.2 419 419 | 77201 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 2.1603.0 GPS week: 1603 Day: 0 MJD: 55465
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 125| 0 2 2 -12 -60 -13 -.10 21 20 | 0 -62 2071 2158
cod 233| 0 0 6 35 -2 32 -.11 15 14 | --- --- --- ---
esx 146| 1 -2 9 11 47 47 .46 23 20 | 108430 -894 4521 7924
gfz 195| 0 6 6 -86 -63 151 .00 29 28 | 264931 -602 4569 7390
iac n/a| 2 -1 -23 -48 22 -84 -.20 22 22 | 445790 -730 4515 7788
mcc n/a| 19 -23 10 -407 -129 -557 -1.58 151 151 | --- --- --- ---
Table 2.1603.1 GPS week: 1603 Day: 1 MJD: 55466
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 125| 0 2 2 -7 7 -64 -.17 20 20 | 0 -315 2147 2247
cod 233| -2 -2 4 46 -13 89 -.12 18 15 | --- --- --- ---
esx 146| 1 0 1 23 5 37 .46 22 20 | 32653 3580 3516 6758
gfz 195| 3 3 -2 -62 -9 42 -.17 29 25 | 177773 2681 3523 6381
iac n/a| 0 0 -12 -79 23 -85 -.20 31 31 | 359237 -2239 3517 6565
mcc n/a| -17 -16 0 -138 271 560 -.85 138 138 | --- --- --- ---
Table 2.1603.2 GPS week: 1603 Day: 2 MJD: 55467
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 125| -1 2 0 -2 15 175 -.16 20 20 | 0 -60 1716 1815
cod 233| 0 -2 6 48 13 -64 -.05 17 16 | --- --- --- ---
esx 146| 0 0 0 4 -16 4 .41 23 21 | 98514 5908 4326 7842
gfz 195| 0 0 4 -86 -8 -128 -.10 30 29 | 254329 5976 4339 7929
iac n/a| 0 0 -9 -48 23 -171 -.14 29 29 | 437948 -1514 4322 8462
mcc n/a| 16 2 34 -34 173 292 -.09 88 88 | --- --- --- ---
Table 2.1603.3 GPS week: 1603 Day: 3 MJD: 55468
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 125| 0 1 -2 -21 -54 112 -.19 24 23 | 0 -98 1686 1741
cod 233| 1 0 3 50 1 4 -.14 16 17 | --- --- --- ---
esx 146| -1 0 7 -57 48 -31 .47 20 20 | 48277 8568 4108 8985
gfz 195| 3 1 7 -39 -31 -43 -.13 29 22 | 187820 7743 4111 8781
iac n/a| 2 0 -13 -29 11 -28 -.22 24 24 | 369857 1572 4082 9328
mcc n/a| -6 9 33 -35 53 -215 -.37 84 84 | --- --- --- ---
Table 2.1603.4 GPS week: 1603 Day: 4 MJD: 55469
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 125| -2 2 0 -4 -23 28 -.17 24 23 | 0 102 2382 2470
cod 233| -1 0 0 33 -13 39 -.15 16 16 | --- --- --- ---
esx 146| -1 0 -1 3 7 -9 .45 21 19 | 58912 -1916 4535 9012
gfz 195| 3 0 -7 -58 117 38 -.15 29 27 | 197906 -4231 4538 8987
iac n/a| 2 0 9 -64 0 -56 -.27 24 24 | 374768 -3127 4528 9079
mcc n/a| -7 -11 27 -28 254 -805 .06 99 99 | --- --- --- ---
Table 2.1603.5 GPS week: 1603 Day: 5 MJD: 55470
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 125| 0 1 -5 8 61 -67 -.21 23 23 | 0 -120 2050 2149
cod 233| -1 0 -1 50 -29 29 -.15 15 13 | --- --- --- ---
esx 146| 3 -2 0 -25 -33 18 .51 22 22 | 44863 -5967 4867 9351
gfz 195| 1 6 -3 -119 124 51 -.25 28 26 | 200833 -3029 4847 9239
iac n/a| 0 1 10 -46 21 -11 -.23 29 29 | 372864 269 4856 9712
mcc n/a| 0 -14 18 19 36 -226 .32 84 84 | --- --- --- ---
Table 2.1603.6 GPS week: 1603 Day: 6 MJD: 55471
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 125| 0 2 -2 -4 37 -4 -.10 22 20 | 0 333215 128147 185641
cod 233| -2 -1 0 26 -25 42 -.15 15 14 | --- --- --- ---
esx 146| 1 0 0 -42 -23 -63 .49 22 21 | 243475 -6732 3789 8017
gfz 195| 3 3 1 -149 30 -63 -.19 29 30 | 403976 -7402 3792 7512
iac n/a| 0 0 0 -27 13 18 -.22 30 30 | 576296 -362 3811 8437
mcc n/a| 0 -4 22 92 2 621 -.23 103 103 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGL orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1603.0 GPS week: 1603 Day: 0 MJD: 55465
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1108 21 19 32 17 18 --- 13 | 55 54 50 52 38 --- 47
R02 | 572 21 8 11 21 22 --- 9 | 20 31 37 41 42 --- 30
R04 | 720 24 11 26 33 22 --- 12 | 26 30 40 28 42 --- 33
R05 | 968 15 11 12 21 16 --- 8 | 22 45 39 36 26 --- 33
R07 | 2933 18 17 20 14 20 --- 11 | 25 42 46 29 24 --- 33
R08 | 1985 8 10 11 24 22 154 7 | 30 35 38 40 23 27 31
R10 | 1025 16 10 15 15 23 --- 9 | 38 48 57 51 48 --- 47
R11 | 1741 39 30 47 39 44 --- 23 | 63 86 65 66 68 --- 69
R13 | 1245 20 17 28 32 17 --- 12 | 34 57 74 62 49 --- 52
R14 | 998 21 15 24 24 22 --- 11 | 41 39 31 35 37 --- 32
R15 | 4129 19 10 25 61 20 145 10 | 49 59 82 93 65 59 62
R17 | 2127 21 13 18 25 23 --- 11 | 39 45 57 46 60 --- 47
R18 | 3142 23 13 25 31 19 --- 11 | 15 31 25 17 31 --- 22
R19 | 1420 21 12 13 26 13 --- 8 | 34 30 38 50 41 --- 33
R20 | 1650 18 9 23 22 22 --- 10 | 30 33 45 45 33 --- 32
R21 | 2558 15 16 27 24 17 --- 11 | 40 46 57 46 46 --- 44
R22 | 1014 11 11 14 24 19 --- 8 | 30 24 27 27 26 --- 23
R23 | 1023 22 18 19 32 16 152 11 | 26 29 39 43 34 96 29
R24 | 3295 24 13 14 31 21 --- 10 | 20 25 37 35 44 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2024 21 15 23 29 22 151 |T 33 41 46 44 40 60 38
WRMS | 2024 20 14 20 28 22 151 |NE 33 41 46 44 40 60 38
MEDI | 1420 21 13 20 24 20 152 |MD 30 39 40 43 41 59 33
Table 3.1603.1 GPS week: 1603 Day: 1 MJD: 55466
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1063 19 27 16 21 42 --- 15 | 38 62 46 39 28 --- 41
R02 | 1197 24 19 19 17 24 --- 12 | 18 42 40 34 40 --- 30
R04 | 2396 20 18 19 15 52 --- 16 | 13 29 29 32 59 --- 24
R05 | 1154 24 9 14 24 23 --- 10 | 20 31 35 19 40 --- 28
R07 | 1812 18 17 24 29 25 --- 12 | 35 24 18 21 14 --- 17
R08 | 2160 23 9 20 30 20 176 10 | 27 26 38 40 22 58 26
R10 | 1672 28 8 23 43 32 --- 13 | 14 34 50 74 34 --- 30
R11 | 2545 31 30 37 35 53 --- 21 | 40 70 85 59 50 --- 59
R13 | 1276 32 19 35 49 23 --- 16 | 25 48 73 78 38 --- 43
R14 | 1113 15 13 24 33 27 --- 11 | 22 21 40 26 25 --- 21
R15 | 2345 14 28 23 27 23 94 13 | 23 55 36 35 29 44 33
XR16 | ---- --- 6 --- --- --- --- 0 | --- 79 --- --- --- --- 78
R17 | 2232 16 16 12 23 29 --- 10 | 34 39 45 40 53 --- 38
R18 | 1213 22 10 18 25 20 --- 10 | 21 24 24 21 24 --- 17
R19 | 1651 10 11 14 27 15 --- 7 | 24 34 37 29 26 --- 29
R20 | 2922 12 25 22 20 36 --- 14 | 24 42 35 31 26 --- 30
R21 | 2234 16 13 13 19 11 --- 8 | 24 30 38 35 28 --- 28
R22 | 1300 21 20 28 27 46 --- 16 | 45 44 45 57 22 --- 35
R23 | 1716 12 11 19 23 23 131 9 | 25 31 39 31 31 95 28
R24 | 2864 14 15 24 44 19 --- 10 | 24 40 48 51 43 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1930 20 18 22 29 31 138 |T 26 40 42 39 33 65 33
WRMS | 1930 20 15 20 25 31 138 |NE 26 40 42 39 33 65 33
MEDI | 1716 19 15 20 27 24 131 |MD 24 34 39 35 29 58 30
Table 3.1603.2 GPS week: 1603 Day: 2 MJD: 55467
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 950 10 14 18 22 30 --- 10 | 32 44 42 36 37 --- 36
R02 | 3494 28 23 19 47 17 --- 13 | 22 45 30 64 34 --- 28
R04 | 3377 25 13 23 27 25 --- 12 | 20 43 47 38 45 --- 38
R05 | 663 14 15 19 21 30 --- 11 | 26 42 28 45 46 --- 31
R07 | 1934 16 15 17 28 31 --- 11 | 30 23 24 31 21 --- 19
R08 | 3517 18 13 17 23 37 58 12 | 19 19 25 25 33 62 13
R10 | 3022 22 13 12 31 32 --- 11 | 44 44 46 57 41 --- 42
R11 | 3588 32 25 45 34 31 --- 19 | 37 71 80 72 58 --- 58
R13 | 1408 26 20 27 32 30 --- 14 | 42 53 77 73 64 --- 55
R14 | 867 20 21 29 29 56 --- 18 | 26 33 43 53 42 --- 24
R15 | 2115 20 17 22 32 25 67 12 | 46 72 75 68 70 79 63
XR16 |35022 --- 6 --- --- --- --- 0 | --- 39 --- --- --- --- 37
R17 | 2011 17 19 28 28 19 --- 12 | 40 42 66 42 56 --- 47
R18 | 937 24 12 18 33 22 --- 11 | 15 25 37 37 35 --- 21
R19 | 1922 9 14 22 25 13 --- 8 | 26 33 28 31 30 --- 25
R20 | 2146 14 16 27 32 37 --- 13 | 26 27 53 44 30 --- 29
R21 | 3257 20 11 21 32 20 --- 10 | 34 35 59 58 44 --- 40
R22 | 1227 14 11 11 38 22 --- 8 | 34 34 37 47 28 --- 31
R23 | 2052 18 18 30 32 25 125 13 | 25 33 49 42 25 65 28
R24 | 1353 18 17 15 17 31 --- 11 | 17 24 37 27 36 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 2313 20 17 23 30 29 88 |T 29 39 46 46 40 68 34
WRMS | 2313 20 16 21 29 29 88 |NE 29 39 46 46 40 68 34
MEDI | 2011 18 15 21 31 30 67 |MD 26 35 43 44 37 65 31
Table 3.1603.3 GPS week: 1603 Day: 3 MJD: 55468
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 802 16 20 9 26 36 --- 12 | 32 37 30 30 20 --- 27
R02 | 4811 17 17 19 20 30 --- 12 | 30 37 57 37 43 --- 39
R04 | 3616 22 12 35 25 26 --- 14 | 27 23 37 21 26 --- 19
R05 | 943 28 13 21 18 23 --- 12 | 16 42 54 43 32 --- 35
R07 | 1950 19 23 17 33 19 --- 11 | 20 33 30 38 24 --- 23
R08 | 4181 24 22 19 13 40 70 15 | 31 22 40 31 36 33 21
R10 | 4500 27 13 19 23 21 --- 11 | 30 26 24 26 34 --- 24
R11 | 1544 41 24 24 37 31 --- 17 | 41 61 79 66 57 --- 58
R13 | 1093 19 15 18 17 19 --- 10 | 37 44 51 55 48 --- 42
R14 | 1365 35 15 30 40 25 --- 15 | 31 27 34 33 37 --- 26
R15 | 4360 17 15 24 27 18 89 10 | 44 44 44 37 52 42 41
XR16 | 3947 --- 4 --- --- --- --- 0 | --- 35 --- --- --- --- 34
R17 | 1973 22 20 14 21 19 --- 11 | 37 53 32 36 58 --- 43
R18 | 2673 21 13 16 41 15 --- 9 | 20 28 33 38 36 --- 24
R19 | 1214 22 11 19 30 17 --- 10 | 20 28 47 42 33 --- 30
R20 | 2505 33 11 27 37 23 --- 13 | 33 36 47 49 24 --- 30
R21 | 2769 19 15 13 45 20 --- 9 | 28 39 45 47 48 --- 37
R22 | 1616 16 11 14 29 17 --- 8 | 39 43 42 55 53 --- 42
R23 | 1775 16 15 18 32 18 92 9 | 25 27 29 40 47 48 28
R24 | 1094 22 9 14 19 23 --- 10 | 23 26 35 30 52 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2687 24 16 20 29 24 84 |T 29 35 41 39 40 41 32
WRMS | 2687 23 17 20 22 24 84 |NE 29 35 41 39 40 41 32
MEDI | 1950 22 15 19 27 21 89 |MD 30 35 40 38 37 42 30
Table 3.1603.4 GPS week: 1603 Day: 4 MJD: 55469
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 806 18 23 16 16 29 --- 12 | 26 33 34 33 22 --- 25
R02 | 1585 26 19 22 23 31 --- 14 | 32 21 31 24 33 --- 15
R04 | 5201 27 16 18 --- 22 --- 12 | 18 32 26 --- 23 --- 20
R05 | 1409 23 26 28 29 28 --- 15 | 28 47 39 42 23 --- 30
R07 | 3561 27 19 18 28 24 --- 12 | 23 34 27 39 45 --- 27
R08 | 3996 22 11 19 34 11 103 9 | 17 23 36 35 33 22 23
R10 | 5105 26 16 22 33 34 --- 14 | 47 28 34 31 30 --- 30
R11 | 1477 38 16 48 38 25 --- 19 | 42 57 85 68 64 --- 57
R13 | 1157 17 17 14 19 16 --- 9 | 36 34 39 40 40 --- 34
R14 | 2139 28 20 16 21 37 --- 14 | 22 30 34 30 33 --- 26
R15 | 6670 29 18 14 51 27 123 12 | 34 50 46 57 52 40 43
XR16 | 5381 --- 3 --- --- --- --- 0 | --- 39 --- --- --- --- 39
R17 | 766 15 14 11 26 22 --- 9 | 41 49 47 52 52 --- 46
R18 | 3013 24 12 13 19 15 --- 9 | 14 23 27 20 19 --- 18
R19 | 1055 14 9 17 26 15 --- 8 | 22 18 28 25 23 --- 19
R20 | 1770 19 19 26 27 15 --- 12 | 33 34 38 36 25 --- 28
R21 | 1553 16 12 21 31 14 --- 9 | 29 35 42 45 32 --- 32
R22 | 1712 19 6 17 38 12 --- 8 | 27 26 39 52 30 --- 28
R23 | 2515 27 10 20 25 23 62 11 | 23 33 44 47 32 43 30
R24 | 1846 18 9 8 25 28 --- 9 | 19 21 26 26 39 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 2978 24 16 21 29 24 99 |T 28 33 38 39 34 35 29
WRMS | 2978 23 16 19 27 24 99 |NE 28 33 38 39 34 35 29
MEDI | 1770 23 16 18 26 23 103 |MD 27 33 36 36 32 40 28
Table 3.1603.5 GPS week: 1603 Day: 5 MJD: 55470
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 656 34 24 26 23 23 --- 15 | 26 25 40 25 16 --- 18
R02 | 1902 31 14 26 17 21 --- 13 | 27 22 22 25 16 --- 13
XR04 | 4363 --- --- --- --- 8 --- 0 | --- --- --- --- 36 --- 33
R05 | 1383 18 17 21 29 38 --- 13 | 9 22 39 39 20 --- 16
R07 | 4771 26 17 32 39 37 --- 16 | 15 33 63 57 20 --- 31
R08 | 2104 23 14 29 19 16 95 12 | 16 21 56 41 40 17 27
XR09 | 4563 --- 4 --- --- --- --- 0 | --- 21 --- --- --- --- 46
R10 | 4508 36 24 34 31 43 --- 19 | 39 34 41 40 31 --- 28
R11 | 1970 35 15 26 35 50 --- 18 | 45 50 52 55 48 --- 46
R13 | 806 16 12 21 22 19 --- 9 | 33 35 32 50 39 --- 31
R14 | 2488 27 13 20 20 49 --- 15 | 18 26 40 25 31 --- 24
R15 | 4445 19 12 17 21 25 82 10 | 30 40 37 39 43 23 35
R17 | 1104 21 15 26 20 16 --- 11 | 31 43 36 42 40 --- 34
R18 | 1563 17 8 17 26 18 --- 8 | 20 27 32 36 24 --- 23
R19 | 942 12 9 14 25 21 --- 8 | 17 17 29 26 25 --- 19
R20 | 1358 21 19 20 30 23 --- 12 | 28 27 33 33 28 --- 24
R21 | 1362 17 14 14 19 18 --- 9 | 33 46 38 48 45 --- 39
R22 | 757 9 13 16 40 21 --- 8 | 27 33 30 48 35 --- 27
R23 | 2069 10 9 10 35 21 74 7 | 20 19 30 42 28 27 20
R24 | 1885 21 10 14 32 23 --- 9 | 17 29 38 42 33 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 2364 23 15 22 28 29 84 |T 25 30 38 39 31 22 27
WRMS | 2364 23 13 22 26 29 84 |NE 25 30 38 39 31 22 27
MEDI | 1885 21 14 20 25 21 82 |MD 26 27 37 40 31 23 27
Table 3.1603.6 GPS week: 1603 Day: 6 MJD: 55471
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 604 17 23 16 25 38 --- 13 | 20 41 36 37 14 --- 26
R02 | 1652 17 12 29 28 24 --- 12 | 19 35 30 26 27 --- 25
R05 | 1970 9 30 23 51 44 --- 16 | 21 37 38 51 34 --- 29
R07 | 3706 19 15 30 30 27 --- 13 | 40 38 30 29 28 --- 31
R08 | 974 24 16 20 18 20 89 11 | 24 25 33 25 35 30 22
XR09 | 3232 --- 99 --- --- 216 --- 147 | --- 26 --- --- 11 --- 50
R10 | 2263 27 13 27 37 57 --- 18 | 31 25 33 35 37 --- 24
R11 | 1631 42 19 23 33 46 --- 18 | 50 65 63 55 59 --- 57
R13 | 1032 19 11 24 22 23 --- 11 | 41 35 52 40 40 --- 39
R14 | 2373 35 9 27 32 33 --- 15 | 29 21 32 33 35 --- 25
R15 | 2297 27 13 23 32 31 54 13 | 28 32 22 26 43 51 26
R17 | 1679 21 8 17 20 17 --- 9 | 45 57 53 55 59 --- 53
R18 | 2754 23 10 15 23 21 --- 10 | 23 30 32 38 32 --- 26
R19 | 709 12 10 24 26 21 --- 10 | 25 23 32 38 29 --- 25
R20 | 1371 14 9 17 20 16 --- 8 | 31 28 32 30 29 --- 28
R21 | 1573 12 16 17 34 15 --- 9 | 43 48 46 50 45 --- 43
R22 | 727 16 14 13 29 26 --- 10 | 29 35 39 44 41 --- 31
R23 | 836 14 17 19 27 28 145 11 | 37 39 42 55 44 58 37
R24 | 1343 19 15 21 24 21 --- 10 | 25 36 37 43 33 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1821 22 15 22 29 30 103 |T 31 35 37 39 35 46 33
WRMS | 1821 20 14 21 30 30 103 |NE 31 35 37 39 35 46 33
MEDI | 1631 19 14 21 27 26 89 |MD 29 35 33 38 35 51 29
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