[IGSREPORT-18191] Wk 1564 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jan 14 07:35:01 PST 2010
******************************************************************************
IGS Electronic Report 14 Jan 07:35:25 PST 2010 Message Number 18191
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1564 (Dec 27, 2009 - Jan 02, 2010)
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 2.1564.
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:
igl1564[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1564 in the SP3 format.
igl15647.sum Combination Report for GPS Week 1564.
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 | 435.4 ns
1 | 501.6 ns
2 | 504.9 ns
3 | 488.3 ns
4 | 492.4 ns
5 | 393.6 ns
6 | 507.8 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 1.1564, 1a.1564).
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 2.1564.0-6)
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 3.1564.0-6).
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 1564 summary. (Dec 27, 2009 - Jan 02, 2010)
Table 1.1564.a GPS week : 1564 MJD: 55192.0-55198.0
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 124| 0 0 8 -4 -34 66 -.13 28 25 | 0 -47 2441 2646
| 2 1 2 26 35 306 .08 | 0 847
cod 237| -1 0 0 55 11 25 -.11 15 14 | --- --- --- ---
| 1 1 1 13 25 58 .05 | --- ---
esx 138| -1 0 -1 -80 41 -21 .41 25 23 | 113488 2647 4494 10046
| 2 1 4 33 31 66 .05 | 41807 5304
iac n/a| 1 1 -7 -18 -33 -59 -.10 24 24 | 475467 -523 4452 9073
| 0 2 5 15 29 132 .07 | 43144 1892
mcc n/a| -5 6 20 0 -36 421 -.38 252 252 | --- --- --- ---
| 15 20 26 282 325 2500 .55 | --- ---
Table 1.1564.b GPS week : 1564 MJD: 55192.0-55198.0
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 | 16 15 15 16 16 13 10 |
R03 | 20 17 23 14 15 11 13 |
R07 | 15 13 17 13 11 12 10 |
R08 | 19 14 17 15 22 19 22 |
R10 | 7 11 11 12 10 10 9 |
R11 | 13 10 14 11 12 10 12 |
R13 | 10 11 13 11 10 6 7 |
R14 | 10 11 10 14 10 12 9 |
R15 | 11 12 14 12 7 8 10 |
R17 | 11 13 14 14 16 15 13 |
R18 | 10 10 12 10 8 10 10 |
R19 | 9 16 13 12 13 9 8 |
R20 | 15 18 19 13 13 15 12 |
R21 | 9 18 19 10 9 16 9 |
R23 | --- --- 0 0 0 67 46 |
Table 1.1564.c GPS week : 1564 MJD: 55192.0-55198.0
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 1564 0 | -120 136 85 -4493 -1002 -14230 86.6 3961 3961 | 435441 0
brd 1564 1 | 54 -146 205 -1585 -1166 -21140 87.3 2664 2664 | 501577 0
brd 1564 2 | -76 -55 386 2782 -2582 -21400 84.6 2627 2627 | 504874 0
brd 1564 3 | -69 -37 373 -88 -651 -11560 85.1 2668 2668 | 488253 0
brd 1564 4 | 153 41 355 205 2817 -10330 87.4 2354 2354 | 492448 0
brd 1564 5 | -67 58 303 -1428 -700 -11710 85.6 1865 1865 | 393630 0
brd 1564 6 | -16 45 462 1151 1320 -22020 90.2 2549 2549 | 507817 0
-------------+------------------------------------------------------------+----------------
brd 1564 mean| -20 5 310 -493 -280 -16055 86.7 2669 2669 | 474862 0
brd 1564 sdev| 94 92 126 2314 1782 5247 1.9 636 636 | 43477 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 2.1564.0 GPS week: 1564 Day: 0 MJD: 55192
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 124| 0 -2 8 40 34 275 -.20 32 28 | 0 -786 2601 2754
cod 237| -1 0 0 60 -4 16 -.14 12 11 | --- --- --- ---
esx 138| 0 -2 -3 -96 17 -67 .40 24 21 | 66503 -3893 3743 10286
iac n/a| 0 1 -7 -27 -26 -170 .02 28 28 | 437445 -1897 3730 9204
mcc n/a| -29 9 50 9 391 5937 -1.10 352 352 | --- --- --- ---
Table 2.1564.1 GPS week: 1564 Day: 1 MJD: 55193
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 124| 0 2 10 2 -60 -385 -.26 27 27 | 0 609 2034 2159
cod 237| -3 -1 0 53 60 153 -.19 18 18 | --- --- --- ---
esx 138| 4 0 0 -45 54 73 .49 25 24 | 135607 1248 4680 11474
iac n/a| 0 3 -9 -28 -53 61 -.06 25 25 | 501788 380 4674 9822
mcc n/a| 5 29 38 -420 174 -768 .60 312 312 | --- --- --- ---
Table 2.1564.2 GPS week: 1564 Day: 2 MJD: 55194
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 124| 5 0 4 -26 -37 502 -.10 31 31 | 0 905 2663 2875
cod 237| -2 0 1 35 28 16 -.08 20 19 | --- --- --- ---
esx 138| -3 1 -5 -52 61 -118 .40 31 27 | 137808 344 6124 11643
iac n/a| 0 2 0 -17 -64 -229 -.11 25 25 | 505157 -1523 6095 10026
mcc n/a| -21 32 8 -297 -142 -901 -.56 240 240 | --- --- --- ---
Table 2.1564.3 GPS week: 1564 Day: 3 MJD: 55195
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 124| 1 0 8 -6 -61 234 -.11 27 24 | 0 -1332 2893 3147
cod 237| -1 -1 0 42 1 -16 -.05 13 12 | --- --- --- ---
esx 138| -3 0 -1 -38 55 2 .35 25 24 | 126552 13175 4495 9960
iac n/a| 2 1 -8 -44 -51 -160 -.11 26 26 | 488118 474 4501 8490
mcc n/a| 14 -6 9 119 -619 -372 .03 219 219 | --- --- --- ---
Table 2.1564.4 GPS week: 1564 Day: 4 MJD: 55196
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 124| -1 1 11 -22 -67 -233 -.04 29 25 | 0 -359 2990 3419
cod 237| 1 0 -1 72 -9 21 -.14 14 13 | --- --- --- ---
esx 138| -3 -2 -4 -108 87 45 .41 23 21 | 130926 1031 4894 8503
iac n/a| 2 2 -3 -5 -49 107 -.14 24 24 | 494498 -3484 4630 8573
mcc n/a| 6 8 -24 363 -215 725 -.75 293 293 | --- --- --- ---
Table 2.1564.5 GPS week: 1564 Day: 5 MJD: 55197
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 124| 1 1 5 -33 -14 96 -.08 23 21 | 0 769 2060 2176
cod 237| 0 1 1 66 -8 3 -.09 16 13 | --- --- --- ---
esx 138| -2 -2 0 -105 22 -53 .35 26 25 | 42496 1820 4002 10535
iac n/a| 1 -3 -5 -7 -1 -65 -.09 21 21 | 394096 155 4014 10284
mcc n/a| -6 -27 14 257 88 -965 -.53 230 230 | --- --- --- ---
Table 2.1564.6 GPS week: 1564 Day: 6 MJD: 55198
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 124| -2 -1 10 15 -32 -23 -.11 24 19 | 0 -141 1850 1993
cod 237| 0 1 1 57 12 -16 -.08 13 10 | --- --- --- ---
esx 138| 0 1 8 -114 -6 -34 .44 23 21 | 154525 4806 3526 7921
iac n/a| 1 0 -16 1 12 44 -.20 22 22 | 507172 2229 3526 7112
mcc n/a| -3 0 47 -32 64 -704 -.31 118 118 | --- --- --- ---
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 3.1564.0 GPS week: 1564 Day: 0 MJD: 55192
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1406 26 18 34 34 --- 15 | 111 117 117 115 --- 113
R03E | 1471 51 21 34 42 --- 19 | 71 53 77 91 --- 65
R07E | 3063 32 10 36 33 --- 15 | 52 60 71 56 --- 58
R08E | 976 53 17 34 33 440 18 | 140 121 118 116 397 118
R10 | 794 20 7 10 15 --- 7 | 31 22 26 20 --- 20
R11 |13400 23 15 33 20 --- 13 | 28 24 46 37 --- 26
R13 | 976 26 9 23 15 --- 10 | 26 24 30 23 --- 20
R14 | 2263 16 10 20 24 --- 9 | 31 32 35 28 --- 28
R15 | 2821 27 11 10 32 232 11 | 33 23 28 23 139 22
R17 | 1643 32 11 11 22 --- 10 | 43 68 66 66 --- 61
R18 | 1273 23 9 17 27 --- 10 | 35 58 65 44 --- 52
R19 | 1288 29 9 11 19 --- 9 | 49 60 61 56 --- 55
R20 | 1928 44 8 13 43 --- 15 | 42 59 60 66 --- 56
R21 | 1096 24 9 19 15 --- 9 | 43 61 62 57 --- 56
------+------------------------------------+--------------------------------
RMS | 3960 32 12 24 28 352 |T 52 55 61 57 268 53
WRMS | 3960 28 11 21 28 352 |NE 36 43 47 42 139 39
MEDI | 1406 26 10 19 24 232 |MD 42 58 61 56 139 55
Table 3.1564.1 GPS week: 1564 Day: 1 MJD: 55193
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1512 28 13 21 35 --- 14 | 118 113 124 115 --- 114
R03E | 2287 26 16 37 35 --- 16 | 40 52 77 61 --- 49
R07E | 2505 22 20 18 25 --- 12 | 39 33 40 35 --- 31
R08E | 811 31 16 25 24 424 13 | 147 123 141 119 332 129
R10 | 2134 24 18 19 16 --- 11 | 55 51 46 34 --- 42
R11 | 5033 16 14 21 21 323 10 | 42 31 43 26 271 26
R13 | 1192 16 17 26 13 --- 11 | 31 24 31 23 --- 18
R14 | 3867 19 17 17 21 --- 10 | 44 38 47 25 --- 31
R15 | 5332 25 18 18 24 90 12 | 40 24 31 27 98 23
R17 | 917 19 23 23 25 --- 13 | 48 47 46 35 --- 39
R18 | 1784 19 18 13 13 --- 9 | 24 40 34 34 --- 27
R19 | 1848 31 18 39 15 --- 15 | 41 53 81 46 --- 48
R20 | 1456 50 18 29 24 --- 18 | 51 48 50 43 --- 40
R21 | 777 32 21 28 38 --- 17 | 66 53 42 42 --- 43
------+------------------------------------+--------------------------------
RMS | 2663 27 18 25 25 312 |T 56 52 59 47 233 47
WRMS | 2663 27 18 24 25 312 |NE 44 40 45 33 184 33
MEDI | 1784 24 18 21 24 323 |MD 42 47 46 35 271 39
Table 3.1564.2 GPS week: 1564 Day: 2 MJD: 55194
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1028 26 22 30 24 --- 14 | 107 89 114 100 --- 98
R03E | 1187 39 36 41 42 --- 23 | 48 69 73 53 --- 49
R07E | 916 31 12 45 25 --- 16 | 52 62 75 60 --- 57
R08E | 1359 34 15 27 37 361 16 | 98 87 99 92 164 87
R10 | 1538 28 11 21 18 --- 11 | 35 33 36 27 --- 26
R11 | 2829 28 15 26 24 187 13 | 30 25 44 39 55 27
R13 | 1682 25 21 25 20 --- 13 | 46 43 51 43 --- 40
R14 | 5423 18 15 18 15 --- 9 | 38 31 28 21 --- 20
R15 | 5753 23 26 25 17 83 13 | 36 33 46 29 64 28
R17 | 1359 25 21 28 25 --- 14 | 55 57 58 38 --- 47
R18 | 1082 23 20 19 16 --- 11 | 45 50 44 33 --- 38
R19 | 1897 32 15 20 22 --- 12 | 39 49 54 50 --- 43
R20 | 2819 47 16 35 31 --- 18 | 43 34 64 50 --- 40
R21 | 1063 42 23 51 14 --- 19 | 44 39 93 35 --- 45
XR23 | ---- --- 3 --- --- --- 0 | --- 350 --- --- --- 349
------+------------------------------------+--------------------------------
RMS | 2626 31 20 31 25 239 |T 51 70 62 47 94 66
WRMS | 2626 31 19 27 25 239 |NE 41 67 51 36 59 63
MEDI | 1359 28 16 26 22 187 |MD 44 49 54 39 64 43
Table 3.1564.3 GPS week: 1564 Day: 3 MJD: 55195
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 971 41 13 31 25 --- 15 | 112 120 133 121 --- 120
R03E | 778 34 14 26 29 --- 14 | 65 44 70 74 --- 57
R07E | 1434 28 15 24 26 --- 12 | 37 58 60 44 --- 49
R08E | 1335 31 15 33 32 347 15 | 181 170 180 184 112 176
R10 | 1404 25 17 18 21 --- 11 | 48 44 53 38 --- 42
R11 | 5091 18 8 28 26 105 11 | 34 42 46 32 46 35
R13 | 1245 22 11 15 27 --- 10 | 26 41 45 39 --- 35
R14 | 4474 26 12 35 24 --- 13 | 30 33 62 28 --- 33
R15 | 4735 17 10 30 24 114 11 | 24 27 42 30 82 23
R17 | 2709 32 12 14 36 --- 13 | 34 46 49 56 --- 43
R18 | 1067 21 13 21 14 --- 10 | 44 57 51 47 --- 49
R19 | 1261 23 10 30 22 --- 12 | 37 56 72 61 --- 53
R20 | 3415 25 11 21 34 --- 12 | 30 38 48 36 --- 35
R21 | 780 20 13 18 19 --- 9 | 43 49 47 57 --- 46
XR23 | ---- --- 3 --- --- --- 0 | --- 126 --- --- --- 124
------+------------------------------------+--------------------------------
RMS | 2667 27 13 25 26 219 |T 53 63 68 60 80 61
WRMS | 2667 24 12 24 26 219 |NE 35 50 51 42 64 47
MEDI | 1335 25 12 24 25 114 |MD 37 46 51 44 82 46
Table 3.1564.4 GPS week: 1564 Day: 4 MJD: 55196
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 817 43 15 28 23 --- 15 | 102 107 127 102 --- 107
R03E | 1180 37 10 26 33 --- 15 | 62 39 47 64 --- 47
R07 | 2740 27 9 24 15 --- 10 | 45 51 66 47 --- 49
R08E | 887 56 26 35 39 433 22 | 96 117 118 89 104 103
R10 | 1978 19 11 19 18 --- 9 | 37 29 46 26 --- 29
R11 | 5332 25 17 22 23 203 12 | 33 40 53 43 134 37
R13 | 949 20 11 20 17 --- 9 | 47 42 49 34 --- 40
R14 | 3863 19 13 19 22 --- 10 | 40 24 31 19 --- 22
R15 | 3089 15 9 14 12 173 7 | 30 24 32 23 132 23
R17 | 2422 41 18 30 25 --- 16 | 42 39 34 29 --- 31
R18 | 755 13 11 13 18 --- 8 | 34 42 39 40 --- 37
R19 | 1030 21 14 28 24 --- 12 | 31 43 59 39 --- 37
R20 | 1181 17 16 21 34 --- 13 | 38 29 51 29 --- 30
R21 | 762 22 7 14 21 --- 9 | 40 38 56 37 --- 39
XR23 | ---- --- 5 --- --- --- 0 | --- 70 --- --- --- 69
------+------------------------------------+--------------------------------
RMS | 2353 29 14 23 24 293 |T 48 48 57 44 123 46
WRMS | 2353 25 13 21 24 293 |NE 37 38 45 31 133 35
MEDI | 1180 21 11 21 22 203 |MD 40 40 49 37 132 37
Table 3.1564.5 GPS week: 1564 Day: 5 MJD: 55197
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1024 29 13 34 17 --- 13 | 94 84 93 93 --- 88
R03E | 1580 28 11 21 17 --- 11 | 62 49 57 52 --- 50
R07 | 1924 18 11 27 26 --- 12 | 39 39 48 43 --- 37
R08E | 1208 35 36 27 25 356 18 | 141 121 137 144 336 132
R10 | 1641 17 11 25 13 --- 9 | 27 27 26 24 --- 22
R11 | 2312 23 15 19 13 83 10 | 31 32 46 36 114 33
R13 | 1342 10 7 14 11 --- 6 | 38 40 44 41 --- 40
R14 | 2847 17 16 33 18 --- 12 | 21 20 35 19 --- 16
R15 | 2714 14 10 15 14 157 7 | 18 20 20 22 138 15
R17 | 1760 34 13 33 23 --- 14 | 19 28 62 37 --- 32
R18 | 1438 18 16 20 18 --- 10 | 25 20 35 27 --- 21
R19 | 816 13 13 21 16 --- 9 | 31 27 25 30 --- 23
R20 | 2472 29 20 23 31 --- 15 | 33 40 36 22 --- 29
R21 | 1650 23 12 35 36 --- 15 | 26 31 34 37 --- 28
XR23 | ---- --- 55 --- 79 --- 66 | --- 90 --- 30 --- 88
------+------------------------------------+--------------------------------
RMS | 1865 23 16 26 21 230 |T 43 44 49 43 196 43
WRMS | 1865 21 13 25 21 230 |NE 26 34 36 29 126 31
MEDI | 1641 18 13 23 18 157 |MD 31 32 36 36 138 32
Table 3.1564.6 GPS week: 1564 Day: 6 MJD: 55198
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1750 29 9 14 18 --- 10 | 103 102 106 110 --- 104
R03E | 1567 28 19 24 22 --- 13 | 93 86 95 78 --- 85
R07 | 4911 16 7 23 25 --- 10 | 33 36 52 40 --- 37
R08E | 1027 52 21 49 34 --- 22 | 119 129 140 118 --- 122
R10 | 1009 12 13 15 22 --- 9 | 27 28 28 26 --- 23
R11 | 1715 22 14 25 23 47 11 | 29 28 30 31 78 25
R13 | 1658 10 8 15 10 --- 6 | 30 30 37 31 --- 30
R14 | 4201 18 8 15 19 --- 8 | 22 18 27 23 --- 17
R15 | 3468 14 12 25 17 159 9 | 23 18 41 28 98 23
R17 | 1125 25 16 14 34 --- 13 | 33 60 57 52 --- 50
R18 | 2646 21 6 24 14 --- 9 | 31 43 48 24 --- 35
R19 | 948 15 6 21 15 --- 8 | 30 37 48 40 --- 37
R20 | 3288 28 15 21 22 --- 12 | 30 42 49 39 --- 38
R21 | 1963 14 14 16 16 --- 8 | 37 54 51 44 --- 46
XR23 | ---- --- 32 --- 62 --- 45 | --- 91 --- 28 --- 87
------+------------------------------------+--------------------------------
RMS | 2548 24 13 23 22 118 |T 45 53 57 47 88 50
WRMS | 2548 19 10 21 22 118 |NE 29 40 41 33 88 37
MEDI | 1715 18 13 21 22 47 |MD 30 42 48 39 78 37
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