[IGSREPORT-18052] Wk 1558 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 3 05:10:17 PST 2009
******************************************************************************
IGS Electronic Report 03 Dec 05:10:40 PST 2009 Message Number 18052
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1558 (Nov 15, 2009 - Nov 21, 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 2.1558.
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:
igl1558[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1558 in the SP3 format.
igl15587.sum Combination Report for GPS Week 1558.
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 | 507.8 ns
1 | 440.7 ns
2 | 506.0 ns
3 | 446.9 ns
4 | 509.0 ns
5 | 504.8 ns
6 | 508.1 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
----+--------+---------------
5 | IAC | R08
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 1.1558, 1a.1558).
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 2.1558.0-6)
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 3.1558.0-6).
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 1558 summary. (Nov 15, 2009 - Nov 21, 2009)
Table 1.1558.a GPS week : 1558 MJD: 55150.0-55156.0
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 111| 2 0 10 7 31 -49 -.15 45 34 | 0 72 2868 3144
| 2 1 4 19 28 130 .08 | 0 721
cod 237| -1 0 -7 20 -7 75 -.15 19 16 | --- --- --- ---
| 1 1 3 23 27 31 .06 | --- ---
esx 125| -1 0 -7 -38 -15 -27 .34 31 24 | 114953 -194 4968 10075
| 1 1 4 29 28 42 .08 | 31386 2121
iac n/a| 1 1 15 0 8 -69 -.10 68 68 | 489267 -589 4939 9682
| 1 2 10 35 31 53 .08 | 30840 1938
mcc n/a| -1 0 27 238 -90 496 .81 156 156 | --- --- --- ---
| 10 17 29 346 223 1299 .55 | --- ---
Table 1.1558.b GPS week : 1558 MJD: 55150.0-55156.0
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 | 7 12 12 7 14 16 15 |
R03 | 11 12 13 12 16 12 17 |
R07 | 9 14 11 11 11 12 12 |
R08 | 8 13 18 23 39 73 19 |
R10 | 21 25 25 23 20 21 20 |
R11 | 24 23 19 46 79 24 19 |
R13 | 19 23 15 14 16 20 19 |
R14 | 20 20 24 22 18 15 19 |
R15 | 24 22 18 26 14 15 41 |
R17 | 16 16 15 14 17 15 14 |
R18 | 18 12 9 10 9 9 13 |
R19 | 12 17 11 10 12 8 9 |
R20 | 13 15 14 17 16 17 16 |
R21 | 15 16 10 10 13 12 13 |
R23 | 19 19 12 14 22 17 19 |
Table 1.1558.c GPS week : 1558 MJD: 55150.0-55156.0
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 1558 0 | -4 -161 -6 -1858 2473 -22150 90.1 2209 2209 | 507764 0
brd 1558 1 | 41 -25 -60 -1344 2353 -20710 89.0 2532 2532 | 440736 0
brd 1558 2 | -138 33 -48 61 486 -21790 90.1 2251 2251 | 505976 0
brd 1558 3 | -88 -50 97 -673 -1291 -23260 87.7 2602 2602 | 446901 0
brd 1558 4 | -118 -58 36 -752 -1784 -23370 88.7 2948 2948 | 509001 0
brd 1558 5 | 81 225 127 -2704 200 -22600 89.3 2711 2711 | 504809 0
brd 1558 6 | -16 -70 137 -1145 -1887 -20200 85.4 4468 4468 | 508125 0
-------------+------------------------------------------------------------+----------------
brd 1558 mean| -34 -15 40 -1202 78 -22011 88.6 2817 2817 | 489044 0
brd 1558 sdev| 82 120 82 893 1839 1210 1.7 771 771 | 30977 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 2.1558.0 GPS week: 1558 Day: 0 MJD: 55150
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 111| 0 0 9 -15 -19 172 -.30 37 34 | 0 -296 3547 3940
cod 237| 0 0 -11 23 -10 19 -.15 17 13 | --- --- --- ---
esx 125| -3 0 -12 -34 20 -105 .43 28 25 | 130991 -231 4668 10800
iac n/a| 2 0 31 -23 17 -85 .01 37 37 | 507214 -568 4660 10609
mcc n/a| 2 18 34 -155 -395 486 .58 126 126 | --- --- --- ---
Table 2.1558.1 GPS week: 1558 Day: 1 MJD: 55151
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 111| 1 0 4 31 53 -103 -.16 38 37 | 0 474 2788 3100
cod 237| -1 0 -8 8 -36 82 -.14 23 19 | --- --- --- ---
esx 125| -1 0 -11 -13 -40 4 .22 27 26 | 67536 3461 5233 10325
iac n/a| 2 2 18 -26 41 -47 -.02 35 35 | 441177 2514 5233 10133
mcc n/a| -1 -2 28 211 120 827 .51 101 101 | --- --- --- ---
Table 2.1558.2 GPS week: 1558 Day: 2 MJD: 55152
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 111| 4 0 8 -16 59 -121 -.18 34 34 | 0 -808 2653 2879
cod 237| -2 0 -9 48 -31 83 -.17 17 16 | --- --- --- ---
esx 125| 0 -2 0 -75 20 -23 .35 23 21 | 129893 -1735 4962 9718
iac n/a| 1 3 10 -36 -9 9 -.11 39 39 | 506343 -2857 5033 8364
mcc n/a| -6 8 10 430 -43 226 .10 123 123 | --- --- --- ---
Table 2.1558.3 GPS week: 1558 Day: 3 MJD: 55153
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 111| 2 -3 10 15 36 58 -.11 40 26 | 0 -870 2542 2719
cod 237| -3 1 -6 32 36 76 -.22 19 16 | --- --- --- ---
esx 125| 0 0 -5 -54 -48 -53 .39 28 20 | 71094 1083 4959 10197
iac n/a| 4 -2 14 -1 7 -159 -.18 54 54 | 447237 781 4993 9882
mcc n/a| -2 -16 -25 385 -369 -1784 .77 222 222 | --- --- --- ---
Table 2.1558.4 GPS week: 1558 Day: 4 MJD: 55154
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 111| 6 0 8 25 54 -212 -.14 68 34 | 0 544 2317 2515
cod 237| -1 0 -6 -13 -3 95 -.17 21 16 | --- --- --- ---
esx 125| 0 2 -4 1 -18 19 .24 33 24 | 139865 -1766 4803 9031
iac n/a| 0 -2 12 22 -32 -81 -.15 84 84 | 508020 337 4805 8916
mcc n/a| 13 -28 35 758 -160 -184 1.29 84 84 | --- --- --- ---
Table 2.1558.5 GPS week: 1558 Day: 5 MJD: 55155
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 111| 0 0 14 18 23 -17 -.14 63 41 | 0 546 3245 3594
cod 237| 0 -2 -1 -1 21 51 -.18 20 14 | --- --- --- ---
esx 125| -1 0 -4 -21 -38 -37 .36 34 20 | 130276 585 5310 10231
iac n/a| 0 4 -1 65 -17 -91 -.09 184 184 | 506487 -2003 5407 10493
mcc n/a| 2 11 70 283 103 1775 1.77 198 198 | --- --- --- ---
Table 2.1558.6 GPS week: 1558 Day: 6 MJD: 55156
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 111| 1 0 17 -5 13 -120 -.04 35 34 | 0 920 2985 3264
cod 237| -1 0 -10 42 -25 118 -.04 17 16 | --- --- --- ---
esx 125| -3 0 -11 -69 -4 2 .39 47 32 | 135022 -2755 4844 10227
iac n/a| 1 1 24 -3 55 -31 -.19 40 40 | 508392 -2331 4448 9382
mcc n/a| -20 15 40 -244 108 2127 .67 241 241 | --- --- --- ---
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 3.1558.0 GPS week: 1558 Day: 0 MJD: 55150
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 916 17 7 11 14 --- 7 | 84 87 90 86 --- 86
R03 | 982 13 12 12 34 --- 10 | 74 82 84 86 --- 81
R07 | 3798 17 12 15 21 --- 9 | 29 27 35 33 --- 27
R08 | 782 14 10 15 18 95 8 | 739 725 717 704 13 723
R10E | 1802 58 24 19 46 --- 21 | 44 34 29 46 --- 24
R11E | 1211 51 19 51 49 122 23 | 126 125 128 134 13 124
R13E | 2833 42 17 32 46 --- 19 | 61 43 54 61 --- 46
R14E | 2446 52 16 27 46 --- 19 | 84 71 76 74 --- 70
R15E | 4382 43 30 28 65 154 23 | 55 69 58 68 34 56
R17 | 895 24 18 35 35 --- 15 | 29 56 56 26 --- 43
R18 | 1909 48 13 36 27 --- 17 | 40 61 75 42 --- 51
R19 | 1163 31 10 28 16 --- 12 | 24 42 58 32 --- 37
R20 | 2898 21 8 22 37 --- 12 | 21 35 36 59 --- 34
R21 | 1414 40 21 18 26 --- 15 | 27 54 57 57 --- 48
R23 | 1488 41 22 33 43 --- 19 | 32 39 53 58 --- 38
------+------------------------------------+--------------------------------
RMS | 2209 37 17 28 37 126 |T 97 103 107 104 20 99
WRMS | 2209 34 13 25 37 126 |NE 109 120 126 118 13 116
MEDI | 1488 40 16 27 35 122 |MD 44 56 58 59 13 48
Table 3.1558.1 GPS week: 1558 Day: 1 MJD: 55151
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 632 28 15 15 25 --- 11 | 100 102 106 105 --- 102
R03 | 908 24 18 17 22 --- 11 | 89 104 107 106 --- 101
R07 | 5125 21 14 26 31 --- 13 | 26 23 41 28 --- 21
R08 | 1059 26 14 24 21 118 12 | 820 793 802 778 12 801
R10E | 1781 73 40 15 39 --- 25 | 58 15 25 42 --- 20
R11E | 1159 44 33 34 49 83 22 | 100 101 114 125 12 104
R13E | 1745 56 26 36 42 --- 22 | 35 51 62 59 --- 47
R14E | 1381 46 20 29 46 --- 20 | 76 81 95 102 --- 84
R15E | 3827 40 25 32 55 98 21 | 94 85 73 88 31 79
R17 | 760 18 28 29 28 --- 15 | 47 43 43 18 --- 30
R18 | 1352 25 22 15 19 --- 12 | 45 54 37 40 --- 41
R19 | 961 49 10 19 34 --- 16 | 43 33 39 28 --- 26
R20 | 6083 26 14 28 33 --- 14 | 28 33 46 40 --- 32
R21 | 694 24 26 28 30 --- 15 | 27 39 56 42 --- 38
R23 | 1612 31 27 39 32 --- 19 | 25 52 59 14 --- 33
------+------------------------------------+--------------------------------
RMS | 2532 38 23 27 35 101 |T 107 107 113 107 18 103
WRMS | 2532 37 19 26 35 101 |NE 125 127 133 119 12 122
MEDI | 1352 28 22 28 32 98 |MD 47 52 59 42 12 41
Table 3.1558.2 GPS week: 1558 Day: 2 MJD: 55152
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 692 23 7 22 28 --- 11 | 57 56 45 52 --- 51
R03 | 848 31 20 15 23 --- 12 | 68 67 58 65 --- 62
R07 | 2951 21 13 22 22 --- 11 | 26 28 31 43 --- 27
R08 | 1326 50 10 19 48 119 18 | 483 488 488 490 10 489
R10E | 2094 45 21 21 84 --- 24 | 47 26 35 66 --- 25
R11E | 1169 33 19 25 57 56 18 | 154 151 145 160 10 149
R13E | 887 29 20 22 33 --- 14 | 36 26 44 43 --- 31
R14E | 2636 67 21 37 43 --- 24 | 35 53 66 83 --- 54
R15E | 2826 40 18 31 41 167 18 | 58 77 91 90 95 77
R17 | 881 15 28 25 32 --- 15 | 30 55 31 21 --- 31
R18 | 2604 16 16 9 19 --- 9 | 49 55 46 49 --- 48
R19 | 966 17 13 20 23 --- 10 | 36 34 27 25 --- 25
R20 | 5044 34 9 22 36 --- 14 | 27 24 34 40 --- 26
R21 | 1017 24 12 18 14 --- 10 | 30 41 55 46 --- 42
R23 | 2809 21 17 23 25 --- 12 | 29 27 35 28 --- 21
------+------------------------------------+--------------------------------
RMS | 2251 34 17 23 39 123 |T 77 80 82 86 38 77
WRMS | 2251 34 16 21 39 123 |NE 83 87 85 85 10 82
MEDI | 1326 29 17 22 32 119 |MD 36 53 45 49 10 42
Table 3.1558.3 GPS week: 1558 Day: 3 MJD: 55153
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 857 16 7 11 19 --- 7 | 113 113 99 108 --- 107
R03 | 838 24 16 15 29 --- 11 | 127 131 142 149 --- 135
R07 | 3595 19 15 13 31 --- 11 | 29 29 32 48 --- 30
R08 | 696 68 27 32 23 --- 22 | 9999 9999 9999 9999 --- 9999
R10E | 1914 45 21 19 74 --- 22 | 62 33 28 68 --- 29
R11E | 982 66 31 63 156 --- 45 | 351 326 307 346 --- 321
R13E | 875 25 16 24 35 --- 14 | 43 56 52 56 --- 47
R14E | 4894 43 35 22 52 --- 21 | 85 72 69 57 --- 66
R15E | 1259 72 14 52 32 222 25 | 137 172 179 173 83 166
R17 | 789 27 18 27 29 --- 14 | 30 40 52 24 --- 35
R18 | 4672 20 12 20 15 --- 9 | 62 61 50 49 --- 54
R19 | 1435 17 13 16 26 --- 10 | 47 48 50 41 --- 43
R20 | 5296 31 16 16 53 --- 16 | 26 32 46 73 --- 38
R21 | 1172 20 10 16 25 --- 9 | 30 48 47 39 --- 41
R23 | 1363 31 19 22 26 --- 13 | 38 27 41 29 --- 24
------+------------------------------------+--------------------------------
RMS | 2602 40 19 28 54 222 |T 84 84 85 90 83 81
WRMS | 2602 26 16 20 54 222 |NE 55 58 62 62 --- 56
MEDI | 1259 27 16 20 29 222 |MD 47 48 50 56 83 43
Table 3.1558.4 GPS week: 1558 Day: 4 MJD: 55154
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 863 27 16 28 29 --- 14 | 72 78 99 93 --- 83
R03 | 969 49 17 26 23 --- 16 | 46 88 97 76 --- 80
R07 | 6171 19 10 14 36 --- 10 | 26 46 40 46 --- 38
R08 | 1386 39 29 27 169 --- 39 | 756 761 761 681 --- 747
R10E | 1260 60 22 17 44 --- 19 | 55 32 44 46 --- 32
R11E | 1342 225 41 80 248 --- 78 | 494 440 451 258 --- 413
R13E | 749 25 17 31 40 --- 15 | 14 37 60 45 --- 34
R14E | 6279 39 24 32 40 --- 18 | 48 49 41 44 --- 36
R15E | 2096 24 15 26 41 84 14 | 58 71 74 64 44 65
R17 | 884 41 19 27 42 --- 17 | 34 50 55 35 --- 41
R18 | 4185 20 11 19 13 --- 9 | 58 39 43 35 --- 40
R19 | 1284 32 17 17 15 --- 11 | 30 57 58 41 --- 48
R20 | 4123 28 21 28 39 --- 15 | 23 30 62 57 --- 38
R21 | 1823 12 14 26 36 --- 12 | 38 32 37 43 --- 30
R23 | 755 54 20 38 51 --- 21 | 26 26 54 56 --- 29
------+------------------------------------+--------------------------------
RMS | 2947 68 21 33 84 84 |T 118 122 131 108 44 116
WRMS | 2947 34 16 24 84 84 |NE 110 120 130 116 --- 117
MEDI | 1342 32 17 27 40 84 |MD 46 49 58 46 44 40
Table 3.1558.5 GPS week: 1558 Day: 5 MJD: 55155
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 975 54 14 22 28 --- 16 | 149 142 161 146 --- 148
R03 | 1059 29 12 20 30 --- 12 | 129 134 146 141 --- 137
R07 | 1906 18 15 18 34 --- 11 | 30 38 36 34 --- 33
R08 | 3948 182 55 101 700 --- 72 | 9999 9999 9999 9999 --- 9999
R10E | 2060 74 14 23 38 --- 20 | 33 23 30 43 --- 21
R11E | 1129 80 19 34 51 --- 24 | 249 213 201 235 --- 216
R13E | 768 61 17 19 51 --- 19 | 53 43 42 50 --- 38
R14E | 5959 35 17 18 40 --- 14 | 53 75 74 64 --- 67
R15E | 4817 33 16 34 21 198 15 | 87 101 114 96 49 97
R17 | 1162 32 11 27 39 --- 14 | 19 32 57 41 --- 35
R18 | 2678 22 12 16 16 --- 9 | 34 46 39 42 --- 39
R19 | 1107 14 10 16 15 --- 7 | 51 41 44 47 --- 42
R20 | 2907 37 18 19 51 --- 16 | 23 41 43 74 --- 40
R21 | 1149 18 17 18 35 --- 12 | 48 39 64 60 --- 48
R23 | 2140 39 19 16 53 --- 17 | 30 30 40 35 --- 26
------+------------------------------------+--------------------------------
RMS | 2711 63 20 34 184 198 |T 70 71 77 79 49 70
WRMS | 2711 41 14 20 184 198 |NE 57 60 70 68 --- 60
MEDI | 1906 35 16 19 38 198 |MD 48 41 44 50 49 40
Table 3.1558.6 GPS week: 1558 Day: 6 MJD: 55156
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1512 47 14 24 20 --- 15 | 120 161 164 169 --- 155
R03 | 899 41 11 32 40 --- 17 | 75 80 83 90 --- 80
R07 | 1900 22 16 18 26 --- 11 | 30 41 34 46 --- 33
R08 |14187 24 16 20 64 --- 18 | 738 722 727 739 --- 726
R10E | 1153 51 20 42 29 --- 19 | 39 24 45 36 --- 19
R11E | 876 34 21 41 39 --- 18 | 141 146 141 139 --- 141
R13E | 490 35 16 36 52 --- 19 | 25 22 43 55 --- 24
R14E | 4735 43 21 22 47 --- 18 | 39 63 56 72 --- 54
R15E | 6487 36 28 147 51 241 41 | 61 69 61 61 50 62
R17 | 1040 21 18 33 29 --- 14 | 28 49 57 34 --- 41
R18 | 2144 29 12 35 13 --- 13 | 37 63 77 50 --- 56
R19 | 692 21 9 18 18 --- 9 | 32 49 56 47 --- 46
R20 | 2811 20 18 19 50 --- 16 | 41 54 65 94 --- 58
R21 | 941 33 11 20 30 --- 13 | 34 56 57 70 --- 53
R23 | 3099 44 13 32 49 --- 19 | 45 33 62 44 --- 34
------+------------------------------------+--------------------------------
RMS | 4467 35 17 47 40 241 |T 99 108 115 116 50 105
WRMS | 4467 34 16 32 40 241 |NE 118 130 138 138 --- 128
MEDI | 1512 34 16 32 39 241 |MD 39 56 61 61 50 54
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