[IGSREPORT-17663] Wk 1541 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Aug 6 06:24:07 PDT 2009
******************************************************************************
IGS Electronic Report 06 Aug 06:24:30 PDT 2009 Message Number 17663
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1541 (Jul 19, 2009 - Jul 25, 2009)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the centers
absolute deviation to the unweighted average orbit after removing small
differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1541.
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:
igl1541[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1541 in the SP3 format.
igl15417.sum Combination Report for GPS Week 1541.
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 | 121.5 ns
1 | 112.0 ns
2 | 183.5 ns
3 | 187.4 ns
4 | 188.1 ns
5 | 193.4 ns
6 | 194.3 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 1.1541, 1a.1541).
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 2.1541.0-6)
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 3.1541.0-6).
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 1541 summary. (Jul 19, 2009 - Jul 25, 2009)
Table 1.1541.a GPS week : 1541 MJD: 55031.0-55037.0
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 107| 2 0 -12 -2 -7 49 -.12 34 25 | 0 158 4170 4812
| 2 1 3 25 28 185 .04 | 0 1007
cod 235| -2 0 -3 -5 -12 75 -.12 19 15 | --- --- --- ---
| 1 2 3 10 23 59 .04 | --- ---
esx 131| 0 0 0 5 45 1 .42 31 24 | 84774 -2302 5680 11685
| 2 1 4 45 28 48 .04 | 32423 2816
iac n/a| 2 0 14 0 -6 -167 -.03 29 29 | 168357 -86 5685 11286
| 1 1 3 31 24 60 .04 | 35239 1338
mcc n/a| 0 0 1 -82 -137 -691 .30 205 205 | --- --- --- ---
| 14 9 25 108 164 508 .46 | --- ---
Table 1.1541.b GPS week : 1541 MJD: 55031.0-55037.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R02 | 10 8 11 11 10 8 11 |
R03 | 10 11 9 13 13 13 9 |
R07 | 11 8 9 18 10 10 11 |
R08 | 12 79 59 45 14 11 8 |
R10 | 16 14 16 14 14 11 14 |
R11 | 17 10 13 10 13 16 12 |
R13 | 14 15 12 13 12 9 10 |
R14 | 15 15 18 15 15 13 14 |
R15 | 13 11 10 12 14 15 17 |
R17 | 19 19 8 14 19 17 10 |
R18 | 13 12 9 12 9 11 13 |
R19 | 16 12 9 10 8 10 12 |
R20 | 12 12 14 17 17 16 17 |
R21 | 10 9 10 13 12 10 14 |
R22 | 11 14 12 14 13 12 13 |
R23 | 21 22 20 18 13 17 21 |
R24 | 20 18 13 12 12 16 10 |
Table 1.1541.c GPS week : 1541 MJD: 55031.0-55037.0
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 1541 0 | 55 84 473 -2069 1763 -19780 85.6 2655 2655 | 121503 0
brd 1541 1 | 135 -86 604 -1187 1871 -23190 86.8 2541 2541 | 112007 0
brd 1541 2 | 68 90 430 -79 -381 -17520 87.4 2972 2972 | 183473 0
brd 1541 3 | 19 17 279 -1361 -2220 -12020 90.3 3180 3180 | 187386 0
brd 1541 4 | -133 -46 153 -2109 -716 -12780 90.4 3058 3058 | 188056 0
brd 1541 5 | 72 -105 211 4458 1248 -10070 90.1 2403 2403 | 193403 0
brd 1541 6 | -42 106 324 800 82 -15040 88.7 2330 2330 | 194328 0
-------------+------------------------------------------------------------+----------------
brd 1541 mean| 25 8 353 -220 235 -15771 88.5 2734 2734 | 168593 0
brd 1541 sdev| 88 88 158 2315 1492 4658 1.9 335 335 | 35708 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 2.1541.0 GPS week: 1541 Day: 0 MJD: 55031
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 107| 5 1 -15 13 14 263 -.10 26 26 | 0 722 3158 3728
cod 235| -3 -2 -2 -24 8 5 -.10 20 15 | --- --- --- ---
esx 131| 2 0 4 -42 18 -40 .39 28 24 | 35363 -1862 4808 12552
iac n/a| 2 2 13 22 -3 -192 -.08 25 25 | 121888 -1450 4860 9752
mcc n/a| -6 0 23 -133 -67 -856 .30 159 159 | --- --- --- ---
Table 2.1541.1 GPS week: 1541 Day: 1 MJD: 55032
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 107| 2 0 -8 30 -22 -72 -.15 52 26 | 0 -131 4716 5543
cod 235| 0 -4 -3 -4 -42 141 -.11 32 20 | --- --- --- ---
esx 131| 1 0 -8 -39 62 42 .42 40 21 | 39839 -4265 4580 9754
iac n/a| 0 2 17 23 -2 -140 -.02 37 37 | 112483 -799 4554 8739
mcc n/a| -9 -12 -3 -39 -293 -356 -.16 158 158 | --- --- --- ---
Table 2.1541.2 GPS week: 1541 Day: 2 MJD: 55033
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 107| 3 1 -17 -42 -21 -63 -.17 43 26 | 0 -234 3171 3444
cod 235| -4 0 -1 7 15 97 -.18 21 12 | --- --- --- ---
esx 131| -1 0 1 72 76 47 .44 41 26 | 105403 -862 5806 10299
iac n/a| 5 0 14 -29 -38 -149 .05 31 31 | 183862 -355 5833 10715
mcc n/a| 0 -13 0 -244 22 -1204 .01 159 159 | --- --- --- ---
Table 2.1541.3 GPS week: 1541 Day: 3 MJD: 55034
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 107| 3 0 -10 -14 -58 356 -.16 42 27 | 0 1641 6904 8101
cod 235| -2 -2 1 -3 9 22 -.07 17 13 | --- --- --- ---
esx 131| -5 -4 1 -4 81 -82 .48 34 27 | 106445 -4859 6610 14038
iac n/a| 1 1 8 1 -41 -295 -.02 31 31 | 186391 -1062 6615 14235
mcc n/a| 19 9 29 -104 -189 -1182 -.28 161 161 | --- --- --- ---
Table 2.1541.4 GPS week: 1541 Day: 4 MJD: 55035
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 107| 1 0 -9 -2 18 37 -.08 24 23 | 0 -1352 3632 4440
cod 235| -2 0 -2 -8 -30 15 -.11 14 15 | --- --- --- ---
esx 131| 1 0 0 -2 34 39 .43 25 24 | 102504 -2066 5610 10327
iac n/a| 2 0 14 18 8 -141 -.07 30 30 | 187998 -221 5589 10257
mcc n/a| 18 10 25 -132 -391 -1052 .60 138 138 | --- --- --- ---
Table 2.1541.5 GPS week: 1541 Day: 5 MJD: 55036
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 107| 1 0 -10 18 8 -67 -.10 25 25 | 0 -490 3686 4160
cod 235| -2 0 -6 -8 -22 137 -.17 15 15 | --- --- --- ---
esx 131| 3 1 3 -8 38 -7 .44 25 22 | 96995 2900 5287 13050
iac n/a| 2 0 14 21 19 -131 -.02 25 25 | 190748 2468 5292 13428
mcc n/a| -6 -1 -28 -22 59 -276 .95 262 262 | --- --- --- ---
Table 2.1541.6 GPS week: 1541 Day: 6 MJD: 55037
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 107| -1 -2 -12 -22 10 -109 -.06 24 25 | 0 954 3926 4269
cod 235| -4 0 -8 4 -27 106 -.13 16 15 | --- --- --- ---
esx 131| 0 0 3 65 6 10 .34 26 24 | 106870 -5100 7064 11779
iac n/a| 1 -1 18 -55 15 -124 -.01 25 25 | 195131 815 7058 11876
mcc n/a| -16 2 -33 99 -101 86 .68 400 400 | --- --- --- ---
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 3.1541.0 GPS week: 1541 Day: 0 MJD: 55031
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1984 16 8 19 21 --- 9 | 15 22 33 24 --- 19
R03 | 2535 20 12 19 19 --- 10 | 24 27 24 32 --- 23
R07 | 4734 16 10 20 27 --- 10 | 29 24 29 25 --- 22
R08 | 774 13 11 24 31 --- 12 | 199 223 229 227 --- 217
R10 | 1104 28 20 42 20 --- 16 | 45 35 46 41 --- 35
R11 | 928 30 16 44 21 96 16 | 23 33 47 27 29 28
R13 | 2842 21 29 15 26 --- 14 | 26 32 22 14 --- 18
R14 | 1503 28 15 30 27 --- 14 | 31 38 49 38 --- 34
R15 | 2226 32 13 19 20 164 12 | 13 19 29 17 36 14
R17 | 1200 28 28 19 49 --- 19 | 19 47 42 34 --- 34
R18 | 1974 23 22 22 15 --- 12 | 27 43 35 31 --- 32
R19 | 6067 22 27 37 18 --- 15 | 40 41 55 40 --- 37
R20 | 2042 29 13 13 27 --- 12 | 17 20 18 22 --- 14
R21 | 1177 20 16 16 13 --- 9 | 38 38 35 35 --- 35
R22 | 576 16 15 24 18 --- 10 | 27 30 42 26 --- 28
R23 | 3066 40 23 52 22 199 20 | 41 41 64 54 131 41
R24 | 3408 38 35 31 35 --- 20 | 145 117 128 135 --- 128
------+------------------------------------+--------------------------------
RMS | 2654 26 20 28 25 159 |T 44 48 54 48 65 44
WRMS | 2654 26 15 24 25 159 |NE 44 48 54 48 65 44
MEDI | 1984 23 16 22 21 164 |MD 27 35 42 32 36 32
Table 3.1541.1 GPS week: 1541 Day: 1 MJD: 55032
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2519 14 10 10 18 --- 7 | 22 19 26 21 --- 19
R03 | 6998 24 13 19 17 --- 10 | 22 29 40 26 --- 25
R07 | 2435 17 11 15 12 --- 8 | 37 27 25 25 --- 24
R08 | 1114 185 103 138 124 --- 78 | 305 380 420 376 --- 359
R10 | 1853 21 24 27 21 --- 13 | 38 42 44 32 --- 35
R11 | 1056 13 18 20 16 63 10 | 18 27 29 23 36 20
R13 | 1745 17 18 33 27 --- 14 | 33 25 45 16 --- 22
R14 | 2756 24 24 27 28 --- 15 | 27 37 25 27 --- 21
R15 | 4174 19 18 16 21 148 11 | 11 25 24 20 52 13
R17 | 1226 48 22 31 26 --- 18 | 25 41 24 29 --- 27
R18 | 2126 15 23 19 20 --- 11 | 26 38 43 40 --- 32
R19 | 1373 25 16 18 19 --- 11 | 29 45 45 46 --- 38
R20 | 874 15 23 22 19 --- 12 | 30 30 20 24 --- 20
R21 | 820 9 14 20 13 --- 8 | 57 43 59 53 --- 51
R22 | 639 27 22 20 26 --- 14 | 31 33 33 21 --- 23
R23 | 1731 48 28 30 46 221 22 | 48 63 61 53 225 50
R24 | 1381 44 33 26 20 --- 18 | 138 152 145 131 --- 140
------+------------------------------------+--------------------------------
RMS | 2541 52 32 40 37 157 |T 52 62 65 56 104 54
WRMS | 2541 26 20 21 37 157 |NE 52 62 65 56 104 54
MEDI | 1731 21 22 20 20 148 |MD 30 37 40 27 52 25
Table 3.1541.2 GPS week: 1541 Day: 2 MJD: 55033
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2771 24 10 16 25 --- 10 | 25 20 23 31 --- 17
R03 | 9000 18 9 21 17 --- 9 | 27 26 34 30 --- 25
R07 | 4130 20 10 23 14 --- 9 | 36 35 44 30 --- 31
R08 | 1534 151 67 124 87 --- 59 | 176 339 399 253 --- 289
R10 | 2022 37 16 41 23 --- 16 | 50 57 52 40 --- 43
R11 | 1146 15 14 33 25 123 12 | 29 29 47 28 29 27
R13 | 1587 23 15 28 20 --- 12 | 22 31 45 44 --- 30
R14 | 4020 25 17 47 38 --- 18 | 28 34 71 49 --- 36
R15 | 1339 16 10 21 22 77 9 | 21 26 36 24 56 22
R17 | 1802 22 8 14 13 --- 8 | 36 37 43 35 --- 33
R18 | 1624 14 13 13 18 --- 8 | 24 30 35 23 --- 24
R19 | 1062 27 9 15 15 --- 9 | 38 44 46 37 --- 39
R20 | 868 26 13 32 27 --- 13 | 26 16 33 20 --- 10
R21 | 596 25 10 20 13 --- 9 | 29 41 39 42 --- 36
R22 | 519 27 10 29 20 --- 12 | 34 27 43 27 --- 23
R23 | 2578 38 23 45 39 233 20 | 45 51 67 54 125 49
R24 | 1046 17 20 31 17 --- 12 | 80 88 100 93 --- 87
------+------------------------------------+--------------------------------
RMS | 2971 43 21 41 31 158 |T 42 54 68 50 70 48
WRMS | 2971 26 12 26 31 158 |NE 42 54 68 50 70 48
MEDI | 1587 24 13 28 20 123 |MD 29 34 44 35 56 31
Table 3.1541.3 GPS week: 1541 Day: 3 MJD: 55034
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 5030 17 10 29 18 --- 10 | 33 28 39 30 --- 28
R03 |10044 21 7 35 25 --- 12 | 35 23 38 22 --- 23
R07 | 3581 41 17 44 25 --- 17 | 65 37 40 37 --- 33
R08 | 1530 133 45 75 71 --- 45 | 312 374 403 366 --- 360
R10 | 995 33 13 26 30 --- 14 | 32 34 53 32 --- 27
R11 | 736 19 11 21 22 97 10 | 31 29 29 24 23 23
R13 | 2297 22 11 19 34 --- 12 | 49 39 46 56 --- 42
R14 | 1886 21 19 38 22 --- 14 | 35 48 39 32 --- 33
R15 | 673 22 12 16 31 113 11 | 33 23 34 30 56 20
R17 | 2149 29 14 17 37 --- 14 | 37 44 32 39 --- 36
R18 | 1175 21 13 27 22 --- 11 | 23 30 38 32 --- 26
R19 | 1204 20 10 16 22 --- 9 | 24 35 43 29 --- 29
R20 | 1120 25 19 35 38 --- 16 | 34 20 48 28 --- 16
R21 | 2185 29 9 34 17 --- 12 | 65 56 77 50 --- 57
R22 | 481 38 15 26 18 --- 13 | 32 38 35 24 --- 26
R23 | 1675 38 21 49 20 235 18 | 35 57 79 44 197 48
R24 | 1771 21 13 21 29 --- 11 | 105 90 88 96 --- 91
------+------------------------------------+--------------------------------
RMS | 3179 42 17 34 31 161 |T 57 59 68 57 92 54
WRMS | 3179 27 13 27 31 161 |NE 57 59 68 57 92 54
MEDI | 1675 22 13 27 25 113 |MD 35 37 40 32 56 29
Table 3.1541.4 GPS week: 1541 Day: 4 MJD: 55035
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 5988 12 10 25 21 --- 9 | 22 20 32 20 --- 17
R03 | 7018 14 16 18 43 --- 13 | 21 23 29 36 --- 19
R07 | 3174 19 12 18 20 --- 9 | 29 26 47 21 --- 26
R08 | 1181 37 18 15 26 --- 14 | 188 191 198 211 --- 195
R10 | 1528 19 19 26 32 --- 13 | 36 38 50 45 --- 36
R11 | 1574 25 11 33 16 92 12 | 21 24 50 27 19 26
R13 | 2637 24 10 23 30 --- 12 | 17 22 36 28 --- 20
R14 | 1363 23 22 29 35 --- 15 | 96 82 92 103 --- 90
R15 | 1567 23 13 21 39 125 13 | 25 12 41 17 18 17
R17 | 3210 43 12 22 54 --- 18 | 33 30 24 19 --- 23
R18 | 2826 18 10 15 22 --- 9 | 29 31 37 37 --- 31
R19 | 1325 12 11 15 18 --- 8 | 43 37 30 35 --- 34
R20 | 1878 24 14 44 35 --- 16 | 19 17 55 34 --- 20
R21 | 2738 12 17 32 15 --- 11 | 32 25 57 29 --- 29
R22 | 1053 25 11 31 23 --- 12 | 28 22 46 27 --- 24
R23 | 2749 29 9 23 29 183 12 | 30 43 45 46 97 36
R24 | 2556 29 13 17 28 --- 12 | 51 59 64 53 --- 54
------+------------------------------------+--------------------------------
RMS | 3058 24 14 25 30 138 |T 42 41 54 46 44 41
WRMS | 3058 23 15 24 30 138 |NE 42 41 54 46 44 41
MEDI | 2556 23 12 23 28 125 |MD 29 26 46 34 19 26
Table 3.1541.5 GPS week: 1541 Day: 5 MJD: 55036
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 4809 10 13 12 14 --- 7 | 24 20 30 25 --- 21
R03 | 2884 14 13 27 30 --- 12 | 25 32 38 29 --- 27
R07 | 1180 20 12 11 23 --- 9 | 42 29 35 26 --- 30
R08 | 1958 27 10 11 25 --- 10 | 204 195 196 205 --- 200
R10 | 1916 27 13 16 21 --- 11 | 23 25 34 23 --- 23
R11 | 1757 24 16 41 29 83 16 | 17 25 56 14 19 23
R13 | 2806 18 9 14 20 --- 8 | 30 23 31 24 --- 24
R14 | 1484 21 21 18 31 --- 13 | 109 122 127 106 --- 116
R15 | 1947 33 12 37 21 188 15 | 17 17 46 18 28 17
R17 | 2931 35 18 22 39 --- 16 | 26 29 25 32 --- 22
R18 | 2717 22 16 20 21 --- 11 | 30 38 32 33 --- 29
R19 | 1058 10 16 21 18 --- 9 | 26 25 29 24 --- 20
R20 | 2113 29 20 40 21 --- 16 | 14 21 37 16 --- 11
R21 | 3249 25 10 17 19 --- 10 | 38 43 53 47 --- 42
R22 | 1357 16 17 30 20 --- 12 | 43 24 44 24 --- 26
R23 | 1660 33 20 29 35 405 16 | 31 27 45 34 73 28
R24 | 2034 36 20 32 26 --- 16 | 38 62 66 48 --- 49
------+------------------------------------+--------------------------------
RMS | 2403 25 15 25 25 262 |T 43 44 54 42 40 41
WRMS | 2403 25 15 22 25 262 |NE 43 44 54 42 40 41
MEDI | 1958 24 16 21 21 188 |MD 30 27 38 26 28 26
Table 3.1541.6 GPS week: 1541 Day: 6 MJD: 55037
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3057 17 19 13 20 --- 10 | 24 23 24 19 --- 20
R03 | 5472 19 11 14 14 --- 8 | 26 26 35 25 --- 23
R07 | 1484 16 11 25 22 --- 10 | 30 27 26 28 --- 23
R08 | 3305 8 10 20 15 --- 8 | 200 215 226 222 --- 216
R10 | 1153 25 13 35 24 --- 14 | 29 31 44 23 --- 23
R11 | 1829 24 17 20 25 110 12 | 20 18 27 23 20 17
R13 | 2325 22 15 20 14 --- 10 | 20 21 24 14 --- 16
R14 | 1776 18 21 35 23 --- 14 | 193 190 188 195 --- 191
R15 | 1522 24 20 41 33 319 17 | 22 19 54 18 35 18
R17 | 1832 23 9 11 23 --- 10 | 25 40 40 39 --- 35
R18 | 1941 27 13 25 23 --- 12 | 47 45 55 42 --- 44
R19 | 986 25 13 14 26 --- 11 | 30 31 38 31 --- 29
R20 | 1941 35 17 41 25 --- 17 | 17 31 40 30 --- 20
R21 | 2572 28 19 32 15 --- 13 | 23 40 43 26 --- 28
R22 | 1422 31 15 24 23 --- 13 | 58 60 42 64 --- 54
R23 | 1529 30 19 31 56 605 20 | 32 35 53 59 107 35
R24 | 1190 20 12 17 18 --- 9 | 37 33 30 38 --- 32
------+------------------------------------+--------------------------------
RMS | 2329 24 16 26 25 400 |T 49 52 58 52 54 48
WRMS | 2329 25 15 24 25 400 |NE 49 52 58 52 54 48
MEDI | 1829 24 15 24 23 319 |MD 29 31 40 30 35 28
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