[IGSREPORT-17684] Wk 1542 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Aug 13 05:55:08 PDT 2009
******************************************************************************
IGS Electronic Report 13 Aug 05:55:36 PDT 2009 Message Number 17684
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1542 (Jul 26, 2009 - Aug 01, 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 2.1542.
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:
igl1542[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1542 in the SP3 format.
igl15427.sum Combination Report for GPS Week 1542.
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 | 119.1 ns
1 | 129.6 ns
2 | 197.4 ns
3 | 201.7 ns
4 | 144.6 ns
5 | 203.7 ns
6 | 209.4 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 1.1542, 1a.1542).
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 2.1542.0-6)
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 3.1542.0-6).
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 1542 summary. (Jul 26, 2009 - Aug 01, 2009)
Table 1.1542.a GPS week : 1542 MJD: 55038.0-55044.0
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 105| 3 0 -11 -14 -19 7 -.15 24 23 | 0 -265 3847 4361
| 1 1 1 33 38 127 .04 | 0 633
cod 236| -3 0 -3 16 7 82 -.13 14 13 | --- --- --- ---
| 1 1 2 25 27 34 .02 | --- ---
esx 127| 0 1 -2 -1 26 21 .42 24 23 | 79750 -224 5257 12110
| 3 2 3 36 56 54 .03 | 36327 3676
iac n/a| 3 0 22 -33 -2 -187 -.09 25 25 | 172509 -538 5258 12443
| 2 1 6 33 51 52 .05 | 40151 1646
mcc n/a| -4 0 23 -16 -67 21 -.09 124 124 | --- --- --- ---
| 8 7 14 41 64 178 .32 | --- ---
Table 1.1542.b GPS week : 1542 MJD: 55038.0-55044.0
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 11 8 13 7 11 11 |
R03 | 12 21 12 13 13 11 11 |
R07 | 8 19 8 8 13 9 8 |
R08 | 10 10 8 12 12 10 8 |
R10 | 10 14 11 13 14 9 10 |
R11 | 14 16 11 9 14 13 11 |
R13 | 10 13 11 12 13 13 14 |
R14 | 10 8 12 11 16 14 13 |
R15 | 15 13 12 13 12 11 15 |
R17 | 18 19 17 10 13 10 12 |
R18 | 9 14 15 11 12 11 8 |
R19 | 10 12 14 9 8 9 9 |
R20 | 14 15 13 10 12 18 15 |
R21 | 9 12 13 12 13 12 9 |
R22 | 9 11 10 12 15 11 8 |
R23 | 12 14 14 18 14 15 19 |
R24 | 16 10 12 14 12 14 18 |
Table 1.1542.c GPS week : 1542 MJD: 55038.0-55044.0
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 1542 0 | -74 81 351 2217 -702 -21280 92.2 2417 2417 | 119084 0
brd 1542 1 |53680 ---- 7631 -86110 -77660 588000 484.7 >>>>> >>>>> | 129639 0
brd 1542 2 | 18 0 503 2599 -895 -18850 86.2 3181 3181 | 197420 0
brd 1542 3 | 132 2 351 1951 5280 -16180 85.2 2732 2732 | 201720 0
brd 1542 4 | 107 -52 501 3837 1542 -12450 86.2 2829 2829 | 144598 0
brd 1542 5 | 13 93 332 -771 2564 -7843 84.6 3394 3394 | 203675 0
brd 1542 6 | 91 5 288 478 1283 -14390 86.8 2402 2402 | 209365 0
-------------+------------------------------------------------------------+----------------
brd 1542 mean| 7710 -6562 1422 -10828 -9798 71001 143.7 >>>>> >>>>> | 172214 0
brd 1542 sdev|20270 17421 2738 33229 29996 228016 150.4 >>>>> >>>>> | 39314 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 2.1542.0 GPS week: 1542 Day: 0 MJD: 55038
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 105| 3 -1 -12 -32 0 83 -.13 23 21 | 0 -1250 4540 5084
cod 236| -6 0 -3 26 -21 80 -.13 13 12 | --- --- --- ---
esx 127| 3 1 1 -11 53 -5 .40 23 21 | 25611 3211 5380 11098
iac n/a| 8 1 17 -24 1 -188 -.10 25 25 | 115865 1888 5389 11498
mcc n/a| -6 -5 16 44 -52 -109 -.10 128 128 | --- --- --- ---
Table 2.1542.1 GPS week: 1542 Day: 1 MJD: 55039
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 105| 2 0 -13 -35 -69 -30 -.14 24 25 | 0 -507 2968 3370
cod 236| -4 -3 0 52 44 68 -.14 17 15 | --- --- --- ---
esx 127| 4 4 -3 23 77 49 .40 29 25 | 40698 4751 4682 11957
iac n/a| 2 0 17 -41 -73 -147 -.07 27 27 | 131937 -1909 4687 12263
mcc n/a| 6 2 7 -38 -148 33 -.01 112 112 | --- --- --- ---
Table 2.1542.2 GPS week: 1542 Day: 2 MJD: 55040
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 105| 5 2 -12 22 -62 -86 -.14 23 22 | 0 -197 4990 5692
cod 236| 0 -1 -2 30 37 138 -.12 15 14 | --- --- --- ---
esx 127| -3 3 1 -16 54 108 .40 22 22 | 104527 -918 5821 12852
iac n/a| 3 2 19 -59 -52 -259 -.16 25 25 | 198739 -2188 5814 13028
mcc n/a| 8 6 13 -63 -115 250 -.35 103 103 | --- --- --- ---
Table 2.1542.3 GPS week: 1542 Day: 3 MJD: 55041
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 105| 4 -1 -10 36 -36 -94 -.18 23 23 | 0 -374 4583 5141
cod 236| -2 0 -6 -22 26 98 -.12 13 11 | --- --- --- ---
esx 127| -3 1 -5 -69 14 37 .49 23 23 | 103105 1549 4967 11682
iac n/a| 0 1 30 21 -15 -179 -.06 26 26 | 200509 627 4974 11852
mcc n/a| -7 9 26 37 -75 1 -.51 143 143 | --- --- --- ---
Table 2.1542.4 GPS week: 1542 Day: 4 MJD: 55042
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 105| 4 -1 -12 -47 6 137 -.14 24 24 | 0 10 3188 3777
cod 236| -2 0 -4 24 -9 67 -.10 14 15 | --- --- --- ---
esx 127| -2 3 -5 13 -1 -67 .40 24 23 | 62165 -2807 4868 13508
iac n/a| 4 0 30 -82 36 -229 -.10 28 28 | 144269 808 4883 13991
mcc n/a| -6 -1 27 -43 -114 24 .19 109 109 | --- --- --- ---
Table 2.1542.5 GPS week: 1542 Day: 5 MJD: 55043
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 105| 1 0 -9 -40 34 -143 -.20 27 26 | 0 -399 3275 3591
cod 236| -3 0 -6 -12 -8 98 -.16 14 13 | --- --- --- ---
esx 127| 1 0 -4 46 -82 26 .40 22 21 | 107126 -1396 6777 15286
iac n/a| 2 0 25 -38 78 -100 -.12 22 22 | 205714 -878 6761 16318
mcc n/a| -9 -5 19 -25 4 218 .42 123 123 | --- --- --- ---
Table 2.1542.6 GPS week: 1542 Day: 6 MJD: 55044
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 105| 1 0 -9 -3 -5 183 -.08 23 20 | 0 862 3388 3872
cod 236| -3 1 -4 19 -18 26 -.15 14 12 | --- --- --- ---
esx 127| 0 -4 0 4 70 0 .44 27 24 | 115018 -5959 4310 8388
iac n/a| 3 1 15 -9 5 -204 .01 22 22 | 210536 -2117 4301 8152
mcc n/a| -14 -10 53 -28 26 -265 -.25 147 147 | --- --- --- ---
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 3.1542.0 GPS week: 1542 Day: 0 MJD: 55038
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2184 16 9 18 26 --- 10 | 23 24 38 27 --- 23
R03 | 4812 30 12 25 15 --- 12 | 60 56 56 51 --- 53
R07 | 1432 13 10 16 15 --- 7 | 24 28 37 26 --- 25
R08 | 4349 17 9 20 24 184 10 | 22 30 32 24 28 24
R10 | 1133 19 12 23 18 --- 10 | 11 23 35 20 --- 18
R11 | 2631 25 21 32 14 41 13 | 20 26 40 24 22 18
R13 | 2735 15 10 22 19 --- 9 | 13 14 27 21 --- 9
R14 | 2079 16 12 19 22 --- 9 | 11 13 27 13 --- 11
R15 | 1747 20 11 33 41 118 15 | 11 17 30 25 17 12
R17 | 2535 28 24 21 50 --- 18 | 28 36 48 43 --- 36
R18 | 1952 20 14 12 16 --- 9 | 25 21 25 26 --- 15
R19 | 974 23 12 20 15 --- 10 | 25 30 32 29 --- 25
R20 | 2023 33 9 21 30 --- 13 | 11 13 26 24 --- 11
R21 | 1277 15 13 16 17 --- 8 | 29 32 39 35 --- 31
R22 | 1386 17 13 21 12 --- 9 | 31 42 49 38 --- 37
R23 | 2388 24 11 20 30 --- 12 | 50 64 72 81 --- 64
R24 | 1674 42 16 34 20 --- 16 | 126 124 122 114 --- 120
------+------------------------------------+--------------------------------
RMS | 2417 23 13 23 25 128 |T 30 34 43 36 22 31
WRMS | 2417 21 12 21 25 128 |NE 30 34 43 36 22 31
MEDI | 2023 20 12 21 19 118 |MD 24 28 37 26 22 24
Table 3.1542.1 GPS week: 1542 Day: 1 MJD: 55039
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 18 11 19 27 --- 11 | 20 25 23 28 --- 18
R03 |>>>>> 34 31 51 29 --- 21 | 27 65 89 40 --- 51
R07 |>>>>> 23 11 54 34 --- 18 | 17 32 60 31 --- 24
R08 |>>>>> 12 11 20 24 145 9 | 17 27 22 30 25 17
R10 |>>>>> 18 23 26 26 --- 13 | 17 21 28 19 --- 13
R11 |>>>>> 32 17 38 23 35 15 | 17 40 55 25 15 31
R13 |>>>>> 28 18 28 10 --- 12 | 12 21 34 18 --- 13
R14 |52791 14 8 15 14 --- 7 | 9 18 27 13 --- 13
R15 |>>>>> 27 12 23 29 125 13 | 12 22 45 26 16 20
R17 |>>>>> 22 23 31 54 --- 19 | 31 34 48 40 --- 31
R18 |>>>>> 26 17 30 27 --- 14 | 24 27 34 21 --- 21
R19 |>>>>> 24 15 25 20 --- 12 | 20 27 44 31 --- 25
R20 |>>>>> 30 9 21 37 --- 14 | 20 15 32 26 --- 15
R21 |>>>>> 19 20 23 15 --- 11 | 29 24 32 33 --- 23
R22 |>>>>> 22 18 17 15 --- 10 | 39 35 46 37 --- 35
R23 |>>>>> 31 13 26 29 --- 14 | 36 50 65 68 --- 50
R24 |>>>>> 23 12 16 18 --- 10 | 130 139 134 126 --- 132
------+------------------------------------+--------------------------------
RMS |>>>>> 24 17 29 27 112 |T 28 36 48 36 18 31
WRMS |>>>>> 25 15 25 27 112 |NE 28 36 48 36 18 31
MEDI |>>>>> 23 15 25 26 125 |MD 20 27 44 30 16 23
Table 3.1542.2 GPS week: 1542 Day: 2 MJD: 55040
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3656 18 9 14 17 --- 8 | 24 28 34 29 --- 26
R03 | 6536 22 19 14 26 --- 11 | 51 74 57 54 --- 59
R07 | 1707 13 9 15 21 --- 8 | 19 26 33 34 --- 24
R08 | 5601 12 10 15 19 113 8 | 25 27 29 30 27 23
R10 | 6373 18 13 16 29 --- 11 | 13 16 26 28 --- 14
R11 | 1461 15 16 21 22 32 10 | 13 28 31 16 26 17
R13 | 2347 17 14 25 22 --- 11 | 17 22 35 29 --- 15
R14 | 2493 29 12 21 16 --- 11 | 17 16 26 15 --- 11
R15 | 1440 19 11 17 30 134 11 | 15 19 22 20 13 10
R17 | 1049 35 17 39 27 --- 17 | 23 30 28 24 --- 22
R18 | 1460 15 20 30 36 --- 15 | 15 24 38 31 --- 17
R19 | 1472 28 24 20 22 --- 13 | 27 32 48 23 --- 26
R20 | 1300 26 14 22 26 --- 12 | 25 28 23 27 --- 16
R21 | 1067 31 17 23 19 --- 13 | 23 34 45 35 --- 27
R22 | 515 14 12 16 23 --- 9 | 17 24 29 37 --- 22
R23 | 3558 25 14 27 33 --- 14 | 68 64 81 90 --- 71
R24 | 1983 26 20 17 19 --- 12 | 124 141 120 131 --- 129
------+------------------------------------+--------------------------------
RMS | 3181 23 15 22 25 103 |T 30 37 41 38 22 31
WRMS | 3181 22 14 22 25 103 |NE 30 37 41 38 22 31
MEDI | 1707 19 14 20 22 113 |MD 23 28 33 29 26 22
Table 3.1542.3 GPS week: 1542 Day: 3 MJD: 55041
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 4106 29 11 26 26 --- 12 | 20 30 41 33 --- 25
R03 | 5027 35 14 20 20 --- 12 | 30 41 43 45 --- 34
R07 | 3172 16 8 14 19 --- 8 | 24 23 32 33 --- 24
R08 | 3698 14 8 30 30 83 12 | 29 21 43 29 40 24
R10 | 4086 25 12 20 34 --- 12 | 13 18 30 35 --- 15
R11 | 1251 14 10 17 23 81 9 | 21 32 49 29 32 29
R13 | 1423 22 10 22 27 --- 11 | 15 17 36 21 --- 15
R14 | 2075 18 11 27 19 --- 10 | 15 12 30 13 --- 10
R15 | 2835 25 11 28 30 110 13 | 14 16 38 16 21 16
R17 | 1915 24 10 18 14 --- 9 | 25 25 35 40 --- 25
R18 | 1146 18 13 21 23 --- 10 | 24 18 24 16 --- 15
R19 | 1162 19 11 14 21 --- 9 | 17 25 27 25 --- 18
R20 | 1495 15 13 23 19 --- 10 | 13 15 28 26 --- 13
R21 | 1276 25 14 21 22 --- 11 | 28 29 37 31 --- 25
R22 | 1086 27 12 16 27 --- 11 | 21 27 33 43 --- 23
R23 | 3060 24 22 36 44 238 18 | 47 56 40 77 40 50
R24 | 2755 31 19 21 24 --- 13 | 135 143 148 137 --- 140
------+------------------------------------+--------------------------------
RMS | 2731 23 13 23 26 143 |T 28 32 42 38 33 29
WRMS | 2731 23 11 23 26 143 |NE 28 32 42 38 33 29
MEDI | 2075 24 11 21 23 83 |MD 21 25 36 31 32 24
Table 3.1542.4 GPS week: 1542 Day: 4 MJD: 55042
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3581 12 5 10 23 --- 7 | 23 18 26 29 --- 18
R03 | 3763 18 20 20 34 --- 13 | 29 49 42 43 --- 37
R07 | 2432 24 16 23 32 --- 13 | 19 31 24 32 --- 20
R08 | 1747 19 16 26 19 72 11 | 26 24 37 27 26 21
R10 | 3291 19 18 30 28 --- 13 | 17 33 37 20 --- 20
R11 | 2279 21 15 33 25 89 13 | 17 32 45 18 18 23
R13 | 954 16 13 32 28 --- 13 | 12 15 43 18 --- 16
R14 | 2983 43 11 26 28 --- 15 | 14 13 26 16 --- 10
R15 | 2609 25 12 24 24 129 12 | 15 12 30 13 13 8
R17 | 2103 16 22 19 31 --- 12 | 28 35 23 41 --- 26
R18 | 1085 27 8 20 32 --- 12 | 22 22 27 28 --- 19
R19 | 768 13 10 13 19 --- 7 | 21 24 35 30 --- 24
R20 | 1891 19 13 25 25 --- 11 | 14 23 41 37 --- 19
R21 | 1256 23 13 21 32 --- 12 | 24 24 30 26 --- 17
R22 | 1948 38 11 18 39 --- 15 | 27 29 34 50 --- 26
R23 | 2576 28 12 32 25 133 13 | 48 67 83 78 12 66
R24 | 6758 22 18 18 26 --- 12 | 144 140 109 112 --- 127
------+------------------------------------+--------------------------------
RMS | 2829 24 14 24 28 109 |T 29 34 40 36 17 29
WRMS | 2829 24 15 23 28 109 |NE 29 34 40 36 17 29
MEDI | 2279 21 13 23 28 89 |MD 22 24 35 29 13 20
Table 3.1542.5 GPS week: 1542 Day: 5 MJD: 55043
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3856 19 12 26 19 --- 11 | 27 21 47 29 --- 21
R03 | 2068 26 12 19 20 --- 10 | 22 28 30 25 --- 23
R07 | 2536 15 11 17 21 --- 9 | 20 21 22 20 --- 17
R08 | 2504 23 12 18 17 76 10 | 22 18 34 25 21 19
R10 | 1938 18 12 16 13 --- 8 | 14 22 31 22 --- 16
R11 | 1148 30 18 26 13 128 12 | 24 23 25 18 13 12
R13 | 2300 22 15 28 22 --- 12 | 15 17 51 25 --- 21
R14 | 4757 37 17 21 27 --- 14 | 17 16 35 25 --- 14
R15 | 2877 19 11 19 26 160 10 | 16 19 27 19 14 12
R17 | 1623 26 8 8 25 --- 10 | 25 26 30 29 --- 26
R18 | 1251 26 10 15 24 --- 10 | 30 20 21 16 --- 15
R19 | 773 11 9 10 26 --- 8 | 31 17 24 24 --- 19
R20 | 1481 48 23 33 26 --- 18 | 31 34 30 25 --- 17
R21 | 1061 18 12 28 24 --- 12 | 21 25 33 30 --- 18
R22 | 2070 20 12 21 24 --- 11 | 27 26 26 33 --- 23
R23 | 2239 35 14 31 27 112 15 | 56 66 94 60 11 68
R24 |10260 43 17 19 19 --- 14 | 87 93 86 79 --- 84
------+------------------------------------+--------------------------------
RMS | 3394 27 14 22 22 123 |T 28 28 38 29 14 25
WRMS | 3394 26 13 21 22 123 |NE 28 28 38 29 14 25
MEDI | 2070 23 12 19 24 112 |MD 24 22 30 25 13 19
Table 3.1542.6 GPS week: 1542 Day: 6 MJD: 55044
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 4024 16 16 27 15 --- 10 | 32 23 29 32 --- 25
R03 | 2843 17 11 31 18 --- 11 | 34 31 28 31 --- 28
R07 | 1627 11 10 17 17 --- 8 | 22 22 33 31 --- 22
R08 | 1798 10 10 22 16 80 8 | 21 19 28 29 34 19
R10 | 1012 16 17 24 10 --- 10 | 17 21 26 18 --- 14
R11 | 905 20 14 32 13 210 11 | 20 22 46 21 23 19
R13 | 1424 17 11 36 31 --- 13 | 18 17 36 24 --- 16
R14 | 4574 33 10 33 15 --- 13 | 16 17 31 21 --- 15
R15 | 4020 29 17 21 34 149 14 | 13 13 26 23 17 14
R17 | 1052 28 10 20 23 --- 11 | 26 33 37 39 --- 31
R18 | 2001 11 10 17 15 --- 7 | 29 26 36 24 --- 24
R19 | 959 16 11 19 16 --- 8 | 26 27 35 24 --- 23
R20 | 2247 29 15 33 29 --- 15 | 19 17 31 18 --- 13
R21 | 543 16 11 23 16 --- 9 | 36 29 40 36 --- 31
R22 | 1840 15 12 19 12 --- 8 | 22 23 38 39 --- 26
R23 | 2936 26 19 39 45 118 18 | 58 74 101 93 13 77
R24 | 1897 46 23 32 17 --- 17 | 156 159 162 159 --- 159
------+------------------------------------+--------------------------------
RMS | 2402 23 14 27 22 147 |T 33 33 44 38 21 32
WRMS | 2402 20 12 24 22 147 |NE 33 33 44 38 21 32
MEDI | 1840 17 11 24 16 118 |MD 22 23 35 29 17 23
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