[IGSREPORT-17902] Wk 1551 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Oct 15 05:32:35 PDT 2009
******************************************************************************
IGS Electronic Report 15 Oct 05:32:58 PDT 2009 Message Number 17902
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1551 (Sep 27, 2009 - Oct 03, 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 2.1551.
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:
igl1551[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1551 in the SP3 format.
igl15517.sum Combination Report for GPS Week 1551.
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 | 241.4 ns
1 | 248.3 ns
2 | 247.2 ns
3 | 246.1 ns
4 | 244.1 ns
5 | 184.2 ns
6 | 243.9 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
1 | IAC | R11
2 | IAC | R11
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 1.1551, 1a.1551).
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 2.1551.0-6)
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 3.1551.0-6).
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 1551 summary. (Sep 27, 2009 - Oct 03, 2009)
Table 1.1551.a GPS week : 1551 MJD: 55101.0-55107.0
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 103| 0 0 0 15 -1 26 -.16 26 24 | 0 -594 3606 4101
| 1 2 7 44 25 145 .05 | 0 1909
cod 224| -1 0 0 22 -27 60 -.14 16 15 | --- --- --- ---
| 1 2 6 24 13 46 .03 | --- ---
esx 124| 1 0 0 -32 38 -21 .44 26 23 | 139350 -668 4474 10901
| 2 1 7 41 29 48 .05 | 20940 2359
iac n/a| 0 0 43 -31 1 -120 -.15 87 87 | 127689 -3776 6511 151200
| 1 1 136 30 18 73 .08 | 287601 6761
mcc n/a| -3 -2 49 8 44 426 .04 141 141 | --- --- --- ---
| 6 5 33 114 113 708 .32 | --- ---
Table 1.1551.b GPS week : 1551 MJD: 55101.0-55107.0
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 | 14 21 17 19 15 12 10 |
R03 | 21 34 20 18 14 9 10 |
R07 | 12 24 16 17 12 8 13 |
R08 | 12 15 13 19 12 9 14 |
R10 | 11 12 13 19 11 9 11 |
R11 | 17 52 27 24 18 14 13 |
R13 | 12 11 10 19 11 10 10 |
R14 | 13 10 10 19 15 13 12 |
R15 | 9 10 13 20 15 12 14 |
R17 | 14 10 15 18 8 11 11 |
R18 | 10 9 12 20 10 10 10 |
R19 | 13 12 11 19 11 8 13 |
R20 | 13 14 14 19 15 10 12 |
R21 | 12 13 12 20 12 11 11 |
R23 | 11 14 13 25 18 15 11 |
R24 | 18 15 11 21 12 19 18 |
Table 1.1551.c GPS week : 1551 MJD: 55101.0-55107.0
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 1551 0 | -122 -4 235 -841 -241 -13020 93.1 3607 3607 | 241406 0
brd 1551 1 | ---- ---- -6507 -384700 76000 184100 <<<< >>>>> >>>>> | 248292 0
brd 1551 2 | -7 5 90 -1242 521 -8964 91.0 3333 3333 | 247171 0
brd 1551 3 | -38 99 98 -1277 -88 -14120 90.4 3259 3259 | 246120 0
brd 1551 4 | -15 76 155 -2091 -1340 -17770 86.6 2560 2560 | 244072 0
brd 1551 5 | -18 -32 184 1344 312 -17130 85.8 2605 2605 | 184224 0
brd 1551 6 | 81 2 210 -934 -2791 -12940 87.9 2316 2316 | 243904 0
-------------+------------------------------------------------------------+----------------
brd 1551 mean|-2915 -8224 -790 -55677 10338 14307 -65.7 >>>>> >>>>> | 236455 0
brd 1551 sdev| 7661 21825 2521 145089 28976 74928 409.7 >>>>> >>>>> | 23146 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 2.1551.0 GPS week: 1551 Day: 0 MJD: 55101
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 103| -2 3 4 68 22 230 -.13 30 24 | 0 932 2895 3416
cod 224| -2 0 6 -8 -29 40 -.12 17 17 | --- --- --- ---
esx 124| -2 -2 9 -60 48 -51 .44 25 25 | 139771 -1060 5053 11226
iac n/a| 2 0 -15 5 -22 -163 -.16 17 17 | -522486 -18703 19379 999999
mcc n/a| -7 -8 90 -45 37 -763 -.16 98 98 | --- --- --- ---
Table 2.1551.1 GPS week: 1551 Day: 1 MJD: 55102
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 103| 0 0 3 67 -29 123 -.19 28 25 | 0 -1349 2757 3312
cod 224| 0 0 5 -2 -9 3 -.09 20 17 | --- --- --- ---
esx 124| 2 0 6 -91 83 45 .44 47 28 | 147462 1637 3745 10060
iac n/a| 0 0 -16 -24 -26 -224 -.06 199 199 | 248173 627 3752 9805
mcc n/a| 8 -7 96 -3 -19 -253 .39 107 107 | --- --- --- ---
Table 2.1551.2 GPS week: 1551 Day: 2 MJD: 55103
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 103| 2 -4 5 13 -18 73 -.16 25 24 | 0 -895 2776 2940
cod 224| -1 4 0 52 -44 77 -.18 21 19 | --- --- --- ---
esx 124| 1 1 2 -27 45 -40 .43 27 26 | 151268 -2473 5048 16316
iac n/a| 0 -2 -4 -35 11 -177 -.02 174 174 | 248434 -4265 5019 9912
mcc n/a| 0 6 57 122 -106 395 -.27 145 145 | --- --- --- ---
Table 2.1551.3 GPS week: 1551 Day: 3 MJD: 55104
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 103| 0 1 -15 8 -30 53 -.12 26 24 | 0 1850 3500 3806
cod 224| 0 0 -13 14 -13 -2 -.17 14 12 | --- --- --- ---
esx 124| 0 0 -14 -23 57 -47 .33 19 19 | 146408 -1542 4079 10331
iac n/a| -2 -1 352 -60 3 -20 -.23 135 135 | 247718 -1724 4045 10040
mcc n/a| -9 1 15 186 39 632 -.21 170 170 | --- --- --- ---
Table 2.1551.4 GPS week: 1551 Day: 4 MJD: 55105
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 103| 1 0 3 0 8 -14 -.10 23 21 | 0 417 4048 4730
cod 224| -1 0 0 20 -20 102 -.12 15 15 | --- --- --- ---
esx 124| 1 -1 1 7 24 -35 .50 23 22 | 147034 90 4745 10360
iac n/a| 0 0 -7 -31 10 -119 -.22 34 34 | 243903 -1573 4754 10196
mcc n/a| -8 2 31 -21 -19 711 -.19 184 184 | --- --- --- ---
Table 2.1551.5 GPS week: 1551 Day: 5 MJD: 55106
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 103| 0 -1 2 14 6 -227 -.19 26 23 | 0 -1112 3719 4357
cod 224| -3 1 0 25 -31 109 -.13 12 11 | --- --- --- ---
esx 124| 4 -1 2 -59 9 48 .48 20 17 | 92643 -4080 4391 8529
iac n/a| -1 0 -2 2 13 -93 -.18 24 24 | 185429 -475 4367 8736
mcc n/a| -8 -4 31 -19 230 1033 .48 171 171 | --- --- --- ---
Table 2.1551.6 GPS week: 1551 Day: 6 MJD: 55107
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 103| 1 0 0 -62 33 -52 -.24 26 25 | 0 -4003 5553 6147
cod 224| -3 -2 3 53 -42 92 -.16 14 13 | --- --- --- ---
esx 124| 1 2 -1 29 0 -72 .42 22 21 | 150865 2751 4262 9488
iac n/a| 0 -1 -3 -75 18 -47 -.15 23 23 | 242657 -323 4262 9713
mcc n/a| 2 -5 22 -161 153 1227 .24 111 111 | --- --- --- ---
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 3.1551.0 GPS week: 1551 Day: 0 MJD: 55101
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1683 34 16 24 21 --- 13 | 31 39 34 46 --- 31
XR03 | 1900 38 20 --- 32 --- 21 | 62 64 --- 93 --- 66
R07 | 4379 38 13 12 17 --- 12 | 26 40 49 60 --- 37
R08 | 747 36 14 12 16 105 11 | 58 50 51 50 42 45
R10 | 1903 14 20 26 11 --- 10 | 41 39 35 43 --- 37
R11 |11795 50 24 29 17 --- 17 | 700 733 706 698 --- 717
R13 | 1337 20 20 19 19 --- 11 | 27 32 37 25 --- 25
R14 | 1767 24 21 27 15 --- 12 | 32 27 35 25 --- 22
R15 | 2953 22 13 15 12 49 9 | 33 36 33 36 29 31
R17 | 1065 15 15 40 18 --- 13 | 50 56 63 59 --- 54
R18 | 1545 18 15 21 16 --- 10 | 27 18 30 33 --- 23
R19 | 782 17 16 37 17 --- 13 | 29 26 57 43 --- 34
R20 | 1331 22 20 20 23 --- 12 | 32 36 55 46 --- 36
R21 | 1483 20 16 27 17 --- 11 | 49 49 36 54 --- 43
R23 | 975 22 14 20 18 125 10 | 96 105 110 106 34 105
R24 | 2660 55 17 30 16 --- 17 | 137 128 141 131 --- 132
------+------------------------------------+--------------------------------
RMS | 3606 30 17 25 17 98 |T 89 92 98 96 35 89
WRMS | 3606 24 17 25 17 98 |NE 89 92 98 96 35 89
MEDI | 1545 22 16 24 17 105 |MD 33 39 49 46 34 37
Table 3.1551.1 GPS week: 1551 Day: 1 MJD: 55102
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 52 23 37 34 --- 20 | 40 36 35 53 --- 27
XR03 |>>>>> 41 46 --- 55 --- 33 | 80 117 --- 72 --- 89
R07 |>>>>> 37 25 77 27 --- 24 | 29 37 75 61 --- 35
R08 |>>>>> 38 8 30 25 129 14 | 27 41 64 69 41 39
R10 |47993 25 11 31 15 --- 11 | 31 35 53 49 --- 35
R11 | ---- 40 48 131 765 --- 52 | 9999 9999 9999 689 --- 9999
R13 |>>>>> 12 15 26 19 --- 10 | 19 24 32 45 --- 19
R14 | ---- 13 15 26 17 --- 10 | 19 38 26 42 --- 24
R15 |>>>>> 19 14 13 19 43 9 | 18 33 35 47 21 28
R17 |>>>>> 13 11 26 16 --- 9 | 43 39 47 54 --- 41
R18 |>>>>> 13 12 18 20 --- 9 | 27 27 33 42 --- 26
R19 |>>>>> 19 16 23 26 --- 12 | 19 19 33 48 --- 19
R20 |>>>>> 19 21 32 22 --- 13 | 29 16 46 49 --- 16
R21 |>>>>> 22 17 18 28 --- 12 | 39 48 46 57 --- 41
R23 |>>>>> 21 14 33 28 126 13 | 56 64 65 71 23 61
R24 |>>>>> 39 10 30 28 --- 15 | 110 98 118 116 --- 106
------+------------------------------------+--------------------------------
RMS |>>>>> 28 20 47 199 107 |T 39 44 50 97 28 40
WRMS |>>>>> 25 17 28 199 107 |NE 39 44 50 97 28 40
MEDI |>>>>> 21 15 30 25 126 |MD 29 37 46 53 23 35
Table 3.1551.2 GPS week: 1551 Day: 2 MJD: 55103
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1000 41 17 27 27 --- 16 | 41 36 42 68 --- 34
R03 | 1258 30 29 42 38 --- 20 | 46 48 45 69 --- 50
R07 | 8950 31 20 33 21 --- 15 | 33 39 50 57 --- 32
R08 | 1042 29 21 12 21 131 12 | 18 37 33 51 41 22
R10 | 1894 17 16 30 23 --- 12 | 36 32 62 75 --- 39
R11 | 7675 41 34 41 692 --- 27 | 953 962 982 719 --- 962
R13 | 1155 13 18 15 18 --- 9 | 23 17 38 57 --- 23
R14 | 1371 12 20 22 15 --- 10 | 24 33 42 67 --- 27
R15 | 1048 15 25 20 24 45 12 | 29 47 30 75 28 32
R17 | 1552 20 24 36 23 --- 15 | 64 71 61 96 --- 60
R18 | 2032 14 18 27 17 --- 11 | 28 33 44 69 --- 30
R19 | 751 16 18 18 21 --- 10 | 21 23 25 70 --- 21
R20 | 1346 25 16 21 31 --- 13 | 21 28 45 68 --- 31
R21 | 2910 20 18 20 21 --- 11 | 34 37 37 66 --- 32
R23 | 1876 30 13 25 21 209 13 | 55 70 84 110 30 70
R24 | 2488 18 13 23 22 --- 11 | 138 135 149 167 --- 140
------+------------------------------------+--------------------------------
RMS | 3332 25 21 27 174 145 |T 97 103 110 117 33 100
WRMS | 3332 24 19 26 174 145 |NE 97 103 110 117 33 100
MEDI | 1371 20 18 23 21 131 |MD 33 37 44 69 30 32
Table 3.1551.3 GPS week: 1551 Day: 3 MJD: 55104
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 791 27 15 23 120 --- 18 | 35 44 51 236 --- 42
R03 | 1443 23 10 16 127 --- 17 | 74 107 35 248 --- 95
R07 | 6871 21 14 20 111 --- 16 | 39 43 55 219 --- 42
R08 | 798 26 17 14 128 88 18 | 36 50 48 212 91 44
R10 | 1474 13 14 15 142 --- 18 | 29 37 33 174 --- 26
R11 | 8573 44 22 20 138 --- 23 | 764 795 768 828 --- 779
R13 | 1878 22 13 15 134 --- 18 | 23 26 34 184 --- 26
R14 | 1976 25 12 21 126 --- 18 | 27 26 31 179 --- 27
R15 | 1156 26 14 15 139 66 19 | 29 44 41 175 40 33
R17 | 1830 18 9 15 134 --- 17 | 44 44 46 164 --- 39
R18 | 1668 28 9 19 139 --- 19 | 42 35 21 167 --- 27
R19 | 1607 20 15 10 141 --- 18 | 33 28 33 170 --- 27
R20 | 1876 25 9 19 139 --- 19 | 39 32 32 193 --- 35
R21 | 1817 18 13 23 143 --- 19 | 32 35 24 177 --- 25
R23 | 1049 37 20 30 156 273 25 | 67 69 87 150 30 68
R24 | 4271 27 17 18 144 --- 20 | 76 81 88 189 --- 79
------+------------------------------------+--------------------------------
RMS | 3258 26 14 19 135 170 |T 86 93 89 229 53 88
WRMS | 3258 24 12 19 135 170 |NE 86 93 89 229 53 88
MEDI | 1668 25 14 18 138 88 |MD 36 43 35 179 40 35
Table 3.1551.4 GPS week: 1551 Day: 4 MJD: 55105
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 926 13 24 23 40 --- 14 | 31 33 31 64 --- 25
R03 | 1266 23 17 23 34 --- 13 | 35 49 41 76 --- 43
R07 | 5655 13 14 19 38 --- 12 | 43 41 36 65 --- 35
R08 | 951 28 12 15 27 110 11 | 24 35 26 68 60 28
R10 | 1736 10 13 21 29 --- 10 | 36 37 42 73 --- 33
R11 | 6124 33 18 32 46 162 18 | 375 368 367 402 105 372
R13 | 1122 16 12 21 27 --- 10 | 29 28 27 75 --- 25
R14 | 1202 31 21 25 31 --- 15 | 33 37 34 79 --- 30
R15 | 1988 30 14 25 33 44 14 | 17 32 47 82 33 31
R17 | 1513 12 7 13 26 --- 8 | 51 52 46 89 --- 50
R18 | 888 17 9 9 32 --- 10 | 17 25 25 82 --- 23
R19 | 1281 18 9 16 35 --- 11 | 38 28 24 83 --- 30
R20 | 3382 20 15 30 39 --- 14 | 42 32 63 68 --- 36
R21 | 861 21 13 27 25 --- 12 | 28 27 39 69 --- 22
R23 | 1123 34 15 36 43 309 18 | 66 76 107 125 32 83
R24 | 2039 23 13 16 34 --- 12 | 134 130 139 148 --- 133
------+------------------------------------+--------------------------------
RMS | 2560 23 15 23 34 184 |T 62 64 68 103 57 62
WRMS | 2560 21 15 22 34 184 |NE 62 64 68 103 57 62
MEDI | 1266 20 13 21 33 110 |MD 35 35 39 76 33 31
Table 3.1551.5 GPS week: 1551 Day: 5 MJD: 55106
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1633 19 17 15 28 --- 11 | 28 29 34 50 --- 26
R03 | 1355 24 8 16 18 --- 9 | 45 67 24 61 --- 56
R07 | 7508 16 5 19 15 --- 8 | 26 27 44 47 --- 29
R08 | 944 15 13 18 16 116 9 | 33 43 43 56 60 37
R10 | 890 17 14 10 21 --- 9 | 24 33 35 46 --- 28
R11 | 2983 45 9 22 23 127 14 | 525 519 504 481 13 517
R13 | 1255 18 8 23 17 --- 9 | 27 31 42 50 --- 29
R14 | 2080 37 12 20 26 --- 13 | 19 24 38 43 --- 23
R15 | 2975 28 16 21 21 63 12 | 29 33 51 49 32 35
R17 | 1596 23 10 11 31 --- 10 | 32 39 34 55 --- 35
R18 | 986 18 9 17 28 --- 10 | 25 36 32 43 --- 30
R19 | 1336 11 7 16 16 --- 7 | 22 15 31 38 --- 17
R20 | 2773 25 13 14 19 --- 10 | 26 16 21 47 --- 16
R21 | 805 30 14 12 21 --- 11 | 24 27 26 41 --- 20
R23 | 1688 25 19 21 41 288 15 | 60 66 84 80 37 70
R24 | 2423 43 14 43 29 --- 18 | 104 122 162 133 --- 128
------+------------------------------------+--------------------------------
RMS | 2605 26 12 20 24 171 |T 65 70 75 82 35 68
WRMS | 2605 23 11 17 24 171 |NE 65 70 75 82 35 68
MEDI | 1596 23 12 17 21 116 |MD 27 33 35 49 32 29
Table 3.1551.6 GPS week: 1551 Day: 6 MJD: 55107
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1013 15 17 15 19 --- 9 | 28 39 38 43 --- 32
R03 | 2628 23 13 10 23 --- 10 | 44 54 40 57 --- 49
R07 | 4427 30 16 26 21 --- 13 | 23 39 42 39 --- 29
R08 | 1069 22 13 35 29 114 14 | 23 41 55 34 43 34
R10 | 871 18 11 21 27 --- 11 | 37 38 38 38 --- 34
R11 | 1228 28 10 28 22 135 12 | 495 507 510 470 12 505
R13 | 1169 18 10 19 22 --- 9 | 26 31 36 48 --- 31
R14 | 1629 25 19 21 20 --- 12 | 34 35 46 40 --- 34
R15 | 5532 39 20 16 23 76 14 | 26 42 46 42 30 36
R17 | 1087 24 10 18 26 --- 11 | 57 54 63 70 --- 59
R18 | 722 20 11 15 20 --- 9 | 16 29 27 36 --- 24
R19 | 920 18 11 31 28 --- 13 | 20 29 43 34 --- 27
R20 | 1462 29 14 21 19 --- 11 | 33 20 26 31 --- 18
R21 | 873 24 12 17 20 --- 10 | 28 26 24 28 --- 24
R23 | 3378 19 11 20 26 --- 10 | 80 92 102 95 --- 93
R24 | 1843 46 22 29 28 --- 17 | 117 125 136 127 --- 124
------+------------------------------------+--------------------------------
RMS | 2316 26 14 22 23 111 |T 67 75 79 77 28 72
WRMS | 2316 25 13 21 23 111 |NE 67 75 79 77 28 72
MEDI | 1169 23 12 20 22 114 |MD 28 39 42 40 30 34
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