[IGSREPORT-17463] Wk 1532 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 4 08:48:34 PDT 2009
******************************************************************************
IGS Electronic Report 04 Jun 08:48:56 PDT 2009 Message Number 17463
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1532 (May 17, 2009 - May 23, 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 2.1532.
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:
igl1532[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1532 in the SP3 format.
igl15327.sum Combination Report for GPS Week 1532.
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 | 227.2 ns
1 | 233.3 ns
2 | 183.4 ns
3 | 245.7 ns
4 | 254.4 ns
5 | 172.3 ns
6 | 252.5 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 | BKG | R23
6 | BKG | R23
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 1.1532, 1a.1532).
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 2.1532.0-6)
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 3.1532.0-6).
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 1532 summary. (May 17, 2009 - May 23, 2009)
Table 1.1532.a GPS week : 1532 MJD: 54968.0-54974.0
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 96| 2 0 -19 13 -4 95 -.10 55 41 | 0 -1322 15958 19418
| 2 3 4 32 32 115 .06 | 0 6786
cod 235| -1 0 3 0 8 61 -.15 22 16 | --- --- --- ---
| 0 2 2 23 22 36 .04 | --- ---
esx 125| 0 0 11 12 14 17 .45 37 28 | 89751 -2780 8610 14493
| 1 3 3 28 28 47 .08 | 35744 11115
iac n/a| 1 0 -5 -27 -30 -185 -.13 39 39 | -123676 4783 291468 296099
| 1 2 4 31 40 66 .07 | 599141 12807
mcc n/a| 2 2 61 -28 -2 193 .57 109 109 | --- --- --- ---
| 7 7 11 131 106 500 .30 | --- ---
Table 1.1532.b GPS week : 1532 MJD: 54968.0-54974.0
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 7 13 10 10 27 107 |
R03 | 15 12 13 12 10 28 90 |
R04 | 30 40 33 26 51 39 0 |
R06 | 21 16 16 16 14 22 21 |
R07 | 12 10 14 15 15 12 12 |
R08 | 15 15 19 15 13 11 51 |
R10 | 24 24 21 27 18 24 32 |
R11 | 21 23 26 29 22 22 20 |
R13 | 24 23 19 19 18 17 17 |
R14 | 21 17 25 22 22 30 27 |
R15 | 20 22 19 21 18 15 20 |
R17 | 20 17 17 15 14 16 18 |
R18 | 12 11 15 18 13 13 18 |
R19 | 8 15 12 14 9 11 12 |
R20 | 16 17 15 18 13 15 12 |
R21 | 16 17 19 14 12 12 12 |
R22 | 10 14 16 18 15 15 11 |
R23 | 15 20 28 72 0 114 146 |
R24 | 17 14 21 20 19 19 17 |
Table 1.1532.c GPS week : 1532 MJD: 54968.0-54974.0
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 1532 0 | -59 143 347 -1936 -1195 -14770 86.0 3039 3039 | 227180 0
brd 1532 1 | 313 -217 ---- 2045 53780 -11130 323.6 >>>>> >>>>> | 233259 0
brd 1532 2 | 11 34 309 -1018 -602 -9845 90.8 5834 5834 | 183431 0
brd 1532 3 | 181 -70 391 -546 2751 -12800 87.9 5513 5513 | 245725 0
brd 1532 4 | 127 173 518 -111 2020 -9767 87.5 5489 5489 | 254400 0
brd 1532 5 | 22 -60 460 858 1145 -3829 86.6 4435 4435 | 172301 0
brd 1532 6 | 92 -46 372 931 401 -9490 88.3 5788 5788 | 252503 0
-------------+------------------------------------------------------------+----------------
brd 1532 mean| 98 -6 -3344 31 8328 -10233 121.5 >>>>> >>>>> | 224114 0
brd 1532 sdev| 123 135 9906 1346 20090 3413 89.1 >>>>> >>>>> | 33223 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 2.1532.0 GPS week: 1532 Day: 0 MJD: 54968
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 96| 3 3 -21 64 -33 274 -.21 44 43 | 0 -2240 30828 39721
cod 235| -3 1 2 0 33 13 -.12 18 14 | --- --- --- ---
esx 125| 0 -4 14 6 58 4 .57 31 28 | 106380 5067 8040 17324
iac n/a| 3 3 -3 -12 -115 -261 -.23 34 34 | 230077 2815 8063 17270
mcc n/a| -4 5 76 -98 69 -552 1.05 103 103 | --- --- --- ---
Table 2.1532.1 GPS week: 1532 Day: 1 MJD: 54969
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 96| 0 1 -17 -21 -27 90 -.04 43 40 | 0 5048 6791 7398
cod 235| -1 1 3 13 33 70 -.07 19 18 | --- --- --- ---
esx 125| 1 -1 8 31 17 19 .38 30 29 | 110939 -23347 11772 14681
iac n/a| 1 0 -4 -23 -40 -173 -.15 31 31 | 237283 -16011 11794 14636
mcc n/a| 12 0 46 -46 23 79 .47 101 101 | --- --- --- ---
Table 2.1532.2 GPS week: 1532 Day: 2 MJD: 54970
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 96| 5 1 -14 14 37 140 -.08 41 38 | 0 -15676 25288 31257
cod 235| -1 0 7 -7 -12 65 -.14 22 22 | --- --- --- ---
esx 125| -1 -3 17 18 -8 38 .40 35 29 | 45695 377 5188 12782
iac n/a| 1 3 -8 -60 -15 -209 -.05 35 35 | 174759 6984 5171 13560
mcc n/a| -3 9 71 -65 109 274 .12 93 93 | --- --- --- ---
Table 2.1532.3 GPS week: 1532 Day: 3 MJD: 54971
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 96| 0 -5 -18 -22 -46 55 -.06 40 39 | 0 1265 3790 4272
cod 235| 0 2 1 -42 25 25 -.17 22 16 | --- --- --- ---
esx 125| 0 3 9 62 11 -33 .36 29 26 | 116938 -6516 8538 12214
iac n/a| 0 -5 -5 -25 12 -51 -.05 41 41 | 243078 2325 5705 9075
mcc n/a| 0 8 65 -112 68 101 .70 86 86 | --- --- --- ---
Table 2.1532.4 GPS week: 1532 Day: 4 MJD: 54972
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 96| 2 -1 -25 10 -5 184 -.07 41 41 | 0 308 8146 9203
cod 235| -1 0 0 0 -9 60 -.19 15 12 | --- --- --- ---
esx 125| 0 0 8 3 39 -34 .48 25 23 | 111802 -9027 9519 17586
iac n/a| 1 0 1 25 -15 -227 -.15 34 34 | 249066 -2650 9547 18157
mcc n/a| 8 9 53 -160 -125 667 .73 117 117 | --- --- --- ---
Table 2.1532.5 GPS week: 1532 Day: 5 MJD: 54973
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 96| 6 3 -23 -1 14 -42 -.12 63 47 | 0 3094 20119 24811
cod 235| -2 -4 3 34 5 66 -.16 17 14 | --- --- --- ---
esx 125| 1 4 12 -27 14 21 .46 36 30 | 30505 8178 9989 15519
iac n/a| 1 2 -12 -69 -22 -166 -.16 33 33 | -999999 23015 999999 999999
mcc n/a| -6 -3 49 60 -172 944 .34 136 136 | --- --- --- ---
Table 2.1532.6 GPS week: 1532 Day: 6 MJD: 54974
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 96| 3 0 -14 46 29 -36 -.14 115 40 | 0 -1058 16749 19270
cod 235| -2 -3 5 1 -17 125 -.16 43 16 | --- --- --- ---
esx 125| 2 0 8 -4 -27 105 .52 75 35 | 106002 5803 7224 11347
iac n/a| 3 1 -7 -22 -13 -206 -.08 64 64 | -999999 17005 999999 999999
mcc n/a| 9 -11 67 226 9 -162 .58 128 128 | --- --- --- ---
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 3.1532.0 GPS week: 1532 Day: 0 MJD: 54968
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1803 21 12 11 26 --- 10 | 105 65 61 86 --- 73
R03 | 4471 22 12 34 36 --- 14 | 72 42 50 51 --- 46
XR04 | ---- --- 20 --- 42 --- 29 | --- 37 --- 42 --- 31
R06 | 9291 60 27 28 38 --- 21 | 130 87 89 88 --- 92
R07 | 3604 21 13 25 26 --- 12 | 33 25 29 36 --- 25
R08 | 1275 51 12 24 23 111 15 | 49 21 44 35 99 26
R10E | 1035 46 23 59 42 --- 23 | 44 28 57 46 --- 26
R11E | 1379 59 17 43 35 107 20 | 36 48 73 47 76 47
R13E | 1526 77 25 26 46 --- 24 | 49 45 37 47 --- 36
R14E | 1551 56 16 22 54 --- 21 | 43 32 26 55 --- 25
R15E | 1782 43 14 33 51 90 19 | 30 21 28 56 29 21
R17 | 1817 30 28 34 49 --- 20 | 64 73 43 72 --- 62
R18 | 1102 27 12 23 23 --- 11 | 70 92 89 80 --- 83
R19 | 848 22 6 18 15 --- 8 | 35 45 56 49 --- 45
R20 | 1682 31 17 37 32 --- 16 | 67 82 75 90 --- 77
R21 | 1529 45 14 35 24 --- 16 | 42 71 72 72 --- 64
R22 | 812 30 9 21 15 --- 10 | 41 64 73 58 --- 59
R23 | 2868 45 18 26 22 --- 15 | 198 85 20 53 --- 75
R24 | 3438 54 25 16 22 --- 17 | 63 92 90 72 --- 80
------+------------------------------------+--------------------------------
RMS | 3038 44 18 31 34 103 |T 65 55 56 59 68 52
WRMS | 3038 43 14 28 34 103 |NE 74 62 60 63 99 59
MEDI | 1551 43 16 26 32 107 |MD 49 48 56 55 76 47
Table 3.1532.1 GPS week: 1532 Day: 1 MJD: 54969
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 17 7 12 13 --- 6 | 127 70 60 78 --- 77
R03 |>>>>> 22 14 22 26 --- 12 | 86 38 43 57 --- 46
XR04 | ---- --- 30 --- 52 --- 40 | --- 31 --- 39 --- 28
R06 |>>>>> 39 18 27 29 --- 15 | 89 116 117 105 --- 109
R07 |>>>>> 23 11 20 16 --- 9 | 28 25 32 23 --- 22
R08 |>>>>> 34 18 36 15 99 14 | 52 26 45 34 69 28
R10E |16667 58 20 49 45 --- 24 | 60 46 65 52 --- 42
R11E |>>>>> 74 24 35 33 133 23 | 46 46 66 58 52 49
R13E |>>>>> 70 22 25 44 --- 22 | 47 37 45 34 --- 28
R14E |>>>>> 34 17 25 43 --- 17 | 31 28 37 56 --- 28
R15E |>>>>> 57 17 38 46 53 21 | 37 29 36 53 22 24
R17 |>>>>> 24 17 28 43 --- 16 | 44 57 40 50 --- 46
R18 |>>>>> 12 16 15 25 --- 10 | 68 79 69 57 --- 69
R19 |>>>>> 26 19 35 26 --- 15 | 46 34 72 36 --- 41
R20 |>>>>> 40 17 36 28 --- 16 | 58 50 69 59 --- 53
R21 |>>>>> 48 25 28 18 --- 17 | 37 59 50 50 --- 46
R22 |>>>>> 36 18 24 24 --- 14 | 32 57 47 45 --- 44
R23 |>>>>> 47 28 36 32 --- 19 | 154 73 31 61 --- 71
R24 |>>>>> 46 14 22 21 --- 14 | 46 67 74 71 --- 62
------+------------------------------------+--------------------------------
RMS |>>>>> 43 19 30 31 101 |T 60 50 55 53 47 48
WRMS |>>>>> 40 18 29 31 101 |NE 66 55 57 54 69 53
MEDI |>>>>> 36 18 27 28 99 |MD 46 46 47 53 52 46
Table 3.1532.2 GPS week: 1532 Day: 2 MJD: 54970
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 949 30 15 21 27 --- 13 | 94 65 65 85 --- 72
R03 | 8659 25 19 17 27 --- 12 | 62 42 42 64 --- 46
XR04 | ---- --- 24 --- 42 --- 33 | --- 40 --- 42 --- 35
R06 | 4797 34 21 34 26 --- 16 | 57 84 96 77 --- 74
R07 | 7936 24 18 34 18 --- 13 | 21 26 48 34 --- 27
R08 | 2054 28 19 50 28 102 18 | 35 31 55 41 51 31
R10E | 1807 41 27 40 40 --- 21 | 52 51 81 71 --- 54
R11E | 1593 71 23 44 46 110 26 | 49 44 64 69 41 50
R13E |10927 36 19 47 31 --- 19 | 58 49 66 51 --- 48
R14E | 1614 53 28 46 47 --- 24 | 36 22 61 51 --- 22
R15E | 1517 39 21 35 41 56 19 | 28 39 41 60 26 31
R17 | 1247 17 33 34 27 --- 17 | 44 39 39 27 --- 30
R18 | 1042 37 21 24 25 --- 15 | 68 75 86 76 --- 71
R19 | 999 11 18 9 33 --- 11 | 32 31 32 31 --- 24
R20 | 978 24 18 35 29 --- 15 | 71 74 90 89 --- 77
R21 | 2027 50 14 45 16 --- 18 | 20 56 94 51 --- 53
R22 | 985 44 20 31 11 --- 16 | 31 74 68 58 --- 57
R23 | 3491 52 31 17 76 --- 27 | 222 95 19 115 --- 93
R24 |17163 62 25 34 21 --- 21 | 66 74 97 67 --- 68
------+------------------------------------+--------------------------------
RMS | 5834 41 22 35 35 93 |T 58 53 63 61 39 50
WRMS | 5834 38 22 29 35 93 |NE 63 57 63 61 51 54
MEDI | 1614 36 21 34 28 102 |MD 49 49 64 60 41 50
Table 3.1532.3 GPS week: 1532 Day: 3 MJD: 54971
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1202 19 11 19 24 --- 10 | 117 80 69 101 --- 86
R03 | 7879 25 12 20 28 --- 11 | 73 31 47 50 --- 41
XR04 | ---- --- 17 --- 37 --- 25 | --- 51 --- 40 --- 37
R06 | 9413 20 13 21 50 --- 15 | 108 107 102 165 --- 104
R07 | 5875 20 15 37 28 --- 15 | 27 34 63 39 --- 37
R08 | 2208 41 8 14 41 127 15 | 23 23 35 49 35 23
R10E | 2306 33 47 27 76 --- 27 | 39 72 39 52 --- 39
R11E | 1672 84 30 41 50 65 29 | 61 75 84 79 32 68
R13E | 1188 36 27 32 37 --- 18 | 38 35 44 45 --- 28
R14E | 1972 48 27 44 32 --- 21 | 34 29 49 43 --- 21
R15E | 1662 62 20 13 48 46 21 | 36 38 33 43 20 28
R17 | 964 17 29 26 30 --- 15 | 30 55 32 46 --- 36
R18 | 580 42 17 24 45 --- 18 | 34 48 66 80 --- 51
R19 | 1046 27 20 15 32 --- 13 | 31 49 41 51 --- 40
R20 | 1052 20 19 37 45 --- 17 | 38 52 51 62 --- 45
R21 | 1799 24 13 26 34 --- 13 | 64 58 78 47 --- 59
R22 | 1806 46 16 32 33 --- 18 | 26 63 81 41 --- 55
XR23 |11718 --- 27 --- 120 --- 71 | --- 117 --- 141 --- 114
R24 |17289 53 21 33 32 --- 19 | 100 136 133 109 --- 120
------+------------------------------------+--------------------------------
RMS | 5512 40 22 29 41 86 |T 51 60 61 67 29 54
WRMS | 5512 39 16 26 41 86 |NE 55 64 66 72 35 60
MEDI | 1799 33 19 26 37 65 |MD 38 52 51 50 32 41
Table 3.1532.4 GPS week: 1532 Day: 4 MJD: 54972
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1041 23 11 10 24 --- 9 | 205 120 108 154 --- 136
R03 | 3925 19 10 19 20 --- 9 | 149 81 62 99 --- 87
XR04 | ---- --- 33 --- 76 --- 50 | --- 57 --- 36 --- 44
R06 | 3082 38 11 22 33 --- 14 | 52 52 50 54 --- 45
R07 | 6700 46 14 23 30 --- 15 | 33 27 36 23 --- 22
R08 | 1336 22 20 18 28 182 12 | 33 37 41 58 31 34
R10E | 2942 38 23 34 36 --- 18 | 60 36 59 60 --- 45
R11E | 2152 65 21 38 42 79 22 | 49 55 63 64 39 49
R13E | 1237 45 19 33 35 --- 17 | 46 37 61 46 --- 41
R14E | 1676 51 22 33 56 --- 21 | 35 29 53 51 --- 23
R15E | 1724 64 9 14 42 46 18 | 18 24 27 47 28 22
R17 | 1768 32 9 32 28 --- 14 | 51 42 63 45 --- 47
R18 | 665 45 15 14 20 --- 13 | 63 69 64 69 --- 64
R19 | 833 20 9 15 21 --- 8 | 26 44 52 57 --- 44
R20 | 1841 42 15 17 22 --- 13 | 85 83 84 84 --- 81
R21 | 1749 19 11 27 30 --- 12 | 32 42 43 34 --- 38
R22 | 1945 26 11 30 38 --- 14 | 65 54 55 53 --- 52
XR23 |13451 --- 4 --- --- --- 0 | --- 334 --- --- --- 326
R24 |20108 55 19 26 40 --- 18 | 104 142 162 160 --- 143
------+------------------------------------+--------------------------------
RMS | 5488 41 15 25 34 117 |T 65 71 63 66 32 70
WRMS | 5488 41 12 23 34 117 |NE 74 84 68 71 31 83
MEDI | 1768 38 14 23 30 79 |MD 51 52 59 54 31 45
Table 3.1532.5 GPS week: 1532 Day: 5 MJD: 54973
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1238 123 17 22 31 --- 26 | 144 113 112 121 --- 113
R03 | 1617 123 13 26 47 --- 28 | 88 77 76 105 --- 79
XR04 | ---- --- 27 --- 56 --- 39 | --- 53 --- 41 --- 55
R06 | 4321 94 16 26 28 --- 21 | 111 103 101 85 --- 98
R07 |10104 32 12 14 30 --- 12 | 38 33 37 44 --- 33
R08 | 1302 28 11 17 26 205 11 | 60 33 34 24 27 26
R10E | 2059 79 20 38 47 --- 23 | 81 43 54 59 --- 38
R11E | 1342 56 22 47 44 100 22 | 46 47 51 52 37 39
R13E | 2244 36 17 34 39 --- 17 | 41 27 36 53 --- 28
R14E | 1837 25 33 90 40 --- 29 | 25 44 78 52 --- 37
R15E | 2595 52 14 25 25 61 15 | 28 30 37 33 27 23
R17 | 2683 45 14 27 34 --- 15 | 55 53 77 45 --- 55
R18 | 967 36 11 31 21 --- 13 | 60 83 87 65 --- 76
R19 | 682 38 14 15 16 --- 11 | 22 47 41 54 --- 41
R20 | 1380 15 14 29 39 --- 14 | 67 57 63 84 --- 63
R21 | 827 33 13 18 25 --- 11 | 35 46 37 26 --- 35
R22 | 1984 51 7 37 19 --- 15 | 18 40 67 37 --- 40
XR23 | 6762 781 79 --- 162 --- 113 | 547 115 --- 165 --- 115
R24 |13091 59 20 36 30 --- 18 | 165 183 172 182 --- 176
------+------------------------------------+--------------------------------
RMS | 4434 63 17 36 33 136 |T 90 64 68 69 30 61
WRMS | 4434 47 14 30 33 136 |NE 108 74 75 77 27 71
MEDI | 1837 45 14 27 31 100 |MD 55 47 63 53 27 41
Table 3.1532.6 GPS week: 1532 Day: 6 MJD: 54974
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1206 299 118 205 178 --- 106 | 593 452 399 582 --- 477
R03 | 2714 254 98 182 141 --- 90 | 485 324 272 439 --- 348
XR04 | ---- --- --- --- 11 --- 0 | --- --- --- 59 --- 82
R06 | 4241 56 25 30 42 --- 21 | 99 135 120 112 --- 122
R07 |11848 29 13 27 19 --- 12 | 28 25 37 33 --- 22
R08 | 1481 208 47 25 54 181 50 | 156 53 42 48 40 27
R10E | 1117 106 23 44 56 --- 31 | 54 47 51 76 --- 47
R11E | 1614 44 20 45 40 106 20 | 44 38 52 57 39 36
R13E | 1708 33 19 30 35 --- 16 | 33 25 42 40 --- 25
R14E | 2057 36 29 79 40 --- 26 | 34 42 79 40 --- 36
R15E | 4818 27 26 41 40 71 19 | 24 38 39 43 23 27
R17 | 1439 43 16 34 36 --- 17 | 68 69 84 59 --- 66
R18 | 658 31 32 33 25 --- 17 | 84 110 103 100 --- 100
R19 | 759 23 16 33 12 --- 12 | 25 51 53 43 --- 43
R20 | 1535 36 8 23 19 --- 11 | 65 70 76 70 --- 68
R21 | 3000 16 9 31 24 --- 11 | 47 53 70 58 --- 55
R22 | 2239 33 7 14 22 --- 10 | 36 62 70 62 --- 59
XR23 | 8375 618 118 --- 178 --- 145 | 503 104 --- 78 --- 84
R24 |18614 21 16 33 42 --- 17 | 173 195 201 178 --- 187
------+------------------------------------+--------------------------------
RMS | 5788 115 43 75 64 128 |T 141 105 105 114 34 100
WRMS | 5788 40 16 35 64 128 |NE 181 131 127 137 40 124
MEDI | 1708 36 20 33 40 106 |MD 54 53 70 59 39 59
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