[IGSREPORT-18213] Wk 1565 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Fri Jan 22 05:37:09 PST 2010
******************************************************************************
IGS Electronic Report 22 Jan 05:37:31 PST 2010 Message Number 18213
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1565 (Jan 03, 2010 - Jan 09, 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 2.1565.
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:
igl1565[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1565 in the SP3 format.
igl15657.sum Combination Report for GPS Week 1565.
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 | 415.9 ns
1 | 497.9 ns
2 | 403.8 ns
3 | 484.9 ns
4 | 485.8 ns
5 | 498.5 ns
6 | 499.0 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 1.1565, 1a.1565).
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 2.1565.0-6)
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 3.1565.0-6).
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 1565 summary. (Jan 03, 2010 - Jan 09, 2010)
Table 1.1565.a GPS week : 1565 MJD: 55199.0-55205.0
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 125| 0 1 11 7 -32 -4 -.09 19 19 | 0 -191 2196 2376
| 2 1 3 20 33 162 .04 | 0 677
cod 236| -1 -1 -1 63 -11 27 -.12 14 13 | --- --- --- ---
| 1 1 3 21 21 52 .04 | --- ---
esx 124| 0 0 -6 -79 69 22 .42 21 21 | 114473 148 4467 9862
| 1 2 3 19 34 89 .03 | 44369 2464
iac n/a| 2 1 -4 -16 -15 -85 -.11 25 25 | 465295 -943 4454 9558
| 2 2 5 30 19 73 .02 | 42778 1283
mcc n/a| 9 -1 36 2 -78 -107 .29 200 200 | --- --- --- ---
| 12 15 32 118 137 1137 .51 | --- ---
Table 1.1565.b GPS week : 1565 MJD: 55199.0-55205.0
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 | 11 13 11 10 7 8 8 |
R03 | 12 10 12 11 9 11 10 |
R05 | 0 0 0 0 31 31 28 |
R07 | 9 9 8 9 8 10 10 |
R08 | 14 10 9 9 8 8 11 |
R10 | 9 12 11 11 13 9 15 |
R11 | 14 16 18 13 9 12 15 |
R13 | 7 9 13 11 11 11 8 |
R14 | 12 11 10 9 8 9 10 |
R15 | 10 10 10 14 12 13 13 |
R17 | 15 13 12 15 13 14 12 |
R18 | 11 13 13 13 11 8 10 |
R19 | 9 8 12 12 10 10 10 |
R20 | 12 18 13 13 19 20 15 |
R21 | 8 12 14 11 8 9 12 |
R23 | 47 69 85 197 0 0 0 |
Table 1.1565.c GPS week : 1565 MJD: 55199.0-55205.0
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 1565 0 | 42 -29 341 636 880 -24140 86.7 2434 2434 | 415875 0
brd 1565 1 | 138 -177 288 1659 2130 -22240 85.0 2364 2364 | 497853 0
brd 1565 2 | 75 148 222 -866 -612 -22410 85.0 2148 2148 | 403804 0
brd 1565 3 | 197 5 187 449 3046 -21360 88.2 1637 1637 | 484903 0
brd 1565 4 | -127 -11 274 -1355 1949 -19040 87.6 1443 1443 | 485818 0
brd 1565 5 | 69 148 127 1142 4133 -20120 88.6 1816 1816 | 498453 0
brd 1565 6 | -101 -141 106 -1129 1475 -19150 84.9 2230 2230 | 499046 0
-------------+------------------------------------------------------------+----------------
brd 1565 mean| 42 -8 221 76 1857 -21208 86.6 2010 2010 | 469393 0
brd 1565 sdev| 118 126 86 1189 1520 1881 1.6 380 380 | 41251 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 2.1565.0 GPS week: 1565 Day: 0 MJD: 55199
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 125| 0 1 13 17 -28 -128 -.06 18 18 | 0 -1030 2222 2325
cod 236| -2 0 -4 61 -12 3 -.09 13 11 | --- --- --- ---
esx 124| -2 -3 -1 -89 90 142 .44 24 23 | 57609 1315 4482 10447
iac n/a| 5 1 -7 -23 -34 36 -.08 22 22 | 417357 -430 4504 9769
mcc n/a| 32 -28 48 77 -19 -1423 .43 431 431 | --- --- --- ---
Table 2.1565.1 GPS week: 1565 Day: 1 MJD: 55200
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 125| 0 0 9 -11 -64 157 -.09 17 17 | 0 -485 2016 2181
cod 236| -2 -2 -4 95 25 -38 -.09 18 17 | --- --- --- ---
esx 124| 1 -1 -8 -70 65 -93 .40 23 22 | 144312 -2293 4607 9937
iac n/a| 1 0 0 -50 -26 -68 -.13 25 25 | 499302 -3322 4615 9646
mcc n/a| 9 6 -20 -129 -139 -1430 1.08 286 286 | --- --- --- ---
Table 2.1565.2 GPS week: 1565 Day: 2 MJD: 55201
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 125| -1 3 11 -26 -72 154 -.11 22 22 | 0 381 2142 2321
cod 236| 0 -1 -6 88 -14 -17 -.06 14 14 | --- --- --- ---
esx 124| 1 -3 -6 -43 138 -4 .45 25 23 | 44445 3127 4130 9002
iac n/a| 0 2 2 -41 -26 -152 -.09 24 24 | 404511 -1243 4129 9127
mcc n/a| -9 20 11 11 -59 -707 -.03 98 98 | --- --- --- ---
Table 2.1565.3 GPS week: 1565 Day: 3 MJD: 55202
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 125| 4 1 16 5 -41 -166 -.02 20 20 | 0 878 2507 2718
cod 236| -3 0 -3 53 -1 98 -.12 13 13 | --- --- --- ---
esx 124| 0 -3 -1 -92 56 91 .44 22 21 | 129757 -2426 4273 9269
iac n/a| 4 4 -10 3 -12 -121 -.14 27 27 | 485543 -78 4252 8998
mcc n/a| 5 -4 38 -190 184 -221 .58 100 100 | --- --- --- ---
Table 2.1565.4 GPS week: 1565 Day: 4 MJD: 55203
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 125| 4 0 12 31 -3 182 -.12 17 17 | 0 -861 2734 3130
cod 236| -1 -2 0 33 -17 6 -.18 13 12 | --- --- --- ---
esx 124| -2 2 -6 -68 35 -79 .40 17 17 | 127104 2668 4323 11498
iac n/a| 3 0 -8 32 19 -156 -.11 30 30 | 485215 267 4340 9912
mcc n/a| 14 -9 62 54 -122 674 -.15 124 124 | --- --- --- ---
Table 2.1565.5 GPS week: 1565 Day: 5 MJD: 55204
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 125| 0 1 13 27 -40 -57 -.09 20 20 | 0 -230 1905 2001
cod 236| 0 -2 3 61 -12 54 -.13 14 13 | --- --- --- ---
esx 124| 1 2 -10 -99 48 84 .38 20 20 | 148347 -2398 4913 10220
iac n/a| 0 0 -6 -19 -12 -48 -.10 23 23 | 499847 -852 4887 9900
mcc n/a| 4 0 75 56 -256 1153 -.40 162 162 | --- --- --- ---
Table 2.1565.6 GPS week: 1565 Day: 6 MJD: 55205
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 125| 0 2 5 9 22 -171 -.12 19 19 | 0 9 1846 1957
cod 236| 0 0 1 49 -46 87 -.14 11 10 | --- --- --- ---
esx 124| 0 0 -6 -88 53 13 .39 19 19 | 149739 1043 4544 8663
mcc n/a| 9 4 40 136 -133 1203 .53 202 202 | --- --- --- ---
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 3.1565.0 GPS week: 1565 Day: 0 MJD: 55199
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3510 16 18 26 18 --- 11 | 24 23 39 30 --- 21
R03 | 1125 18 16 21 25 --- 11 | 23 33 34 36 --- 27
XR05 | ---- --- 5 --- --- --- 0 | --- 80 --- --- --- 81
R07 | 2328 9 9 23 20 --- 9 | 28 27 37 34 --- 26
R08 | 2261 32 13 22 23 728 13 | 27 28 29 40 107 25
R10 | 1234 14 6 26 11 --- 8 | 26 27 32 24 --- 24
R11 | 698 27 14 37 21 70 14 | 30 32 46 18 22 27
R13 | 1981 13 10 11 12 --- 6 | 29 30 39 25 --- 29
R14 | 4539 22 15 26 20 --- 11 | 32 24 42 24 --- 26
R15 | 2773 14 9 24 22 152 10 | 29 24 30 21 40 22
R17 | 1198 15 21 23 42 --- 15 | 33 59 53 35 --- 43
R18 | 3029 18 15 28 11 --- 10 | 24 46 47 27 --- 34
R19 | 901 12 9 19 23 --- 9 | 28 40 44 27 --- 34
R20 | 2279 21 12 26 25 --- 11 | 27 33 33 26 --- 27
R21 | 2821 11 9 20 13 --- 7 | 33 43 48 35 --- 39
XR23 |14917 --- 34 --- 62 --- 46 | --- 9999 --- 43 --- 9999
------+------------------------------------+--------------------------------
RMS | 2433 18 13 24 22 431 |T 28 36 39 29 56 32
WRMS | 2433 18 11 23 22 431 |NE 28 36 39 29 56 32
MEDI | 2279 15 12 23 21 152 |MD 28 32 39 27 40 27
Table 3.1565.1 GPS week: 1565 Day: 1 MJD: 55200
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3397 14 17 33 23 --- 12 | 25 20 40 34 --- 25
R03 | 1636 11 17 22 21 --- 10 | 21 25 40 32 --- 23
XR05 | ---- --- 7 --- --- --- 0 | --- 70 --- --- --- 74
R07 | 1107 9 10 23 17 --- 9 | 32 40 52 28 --- 38
R08 | 2656 12 10 22 22 439 9 | 23 31 41 29 128 27
R10 | 1632 14 13 20 34 --- 12 | 17 21 30 30 --- 20
R11 | 849 18 28 25 36 118 15 | 27 41 45 22 44 30
R13 | 1920 15 13 19 11 --- 8 | 25 25 37 26 --- 27
R14 | 4345 16 15 22 21 --- 10 | 26 33 37 26 --- 24
R15 | 1631 13 20 19 19 196 10 | 25 35 41 21 94 27
R17 | 2419 23 24 20 19 --- 12 | 19 51 34 38 --- 33
R18 | 1847 26 20 24 12 --- 12 | 28 36 52 19 --- 28
R19 | 1110 16 13 16 8 --- 8 | 18 32 36 19 --- 24
R20 | 2073 29 20 19 50 --- 18 | 21 32 37 29 --- 25
R21 | 3509 12 16 27 24 --- 11 | 22 33 44 23 --- 25
XR23 | 2505 --- 58 --- 82 --- 69 | --- 899 --- 37 --- 911
------+------------------------------------+--------------------------------
RMS | 2364 17 18 23 25 286 |T 23 89 40 27 88 85
WRMS | 2364 17 17 22 25 286 |NE 23 89 40 27 88 85
MEDI | 1920 14 16 22 21 196 |MD 23 33 40 28 94 27
Table 3.1565.2 GPS week: 1565 Day: 2 MJD: 55201
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3567 18 11 18 28 --- 11 | 24 23 30 36 --- 22
R03 | 1357 18 15 29 22 --- 12 | 27 35 41 36 --- 31
XR05 | ---- --- 6 --- --- --- 0 | --- 60 --- --- --- 63
R07 | 2232 10 13 15 19 --- 8 | 27 33 36 29 --- 29
R08 | 2675 15 11 19 18 70 9 | 29 20 42 32 149 26
R10 | 1667 20 16 15 22 --- 10 | 24 31 31 34 --- 25
R11 | 660 33 17 46 32 96 18 | 24 24 67 29 41 27
R13 | 823 27 17 30 12 --- 13 | 29 34 52 28 --- 32
R14 | 3648 12 13 24 21 --- 10 | 29 37 52 37 --- 35
R15 | 2284 15 12 15 25 121 9 | 30 28 33 25 81 26
R17 | 2134 26 16 23 21 --- 12 | 36 59 63 33 --- 48
R18 | 1082 19 17 20 32 --- 12 | 27 42 49 30 --- 34
R19 | 1121 27 11 27 18 --- 12 | 27 38 50 22 --- 28
R20 | 1309 26 14 24 26 --- 13 | 26 29 35 30 --- 22
R21 | 2599 25 15 26 32 --- 14 | 34 35 37 38 --- 29
XR23 | 1693 --- 62 --- 113 --- 84 | --- 790 --- 26 --- 800
------+------------------------------------+--------------------------------
RMS | 2147 22 14 25 24 98 |T 28 82 44 31 90 79
WRMS | 2147 22 14 23 24 98 |NE 28 82 44 31 90 79
MEDI | 1693 19 14 23 22 96 |MD 27 34 41 30 81 29
Table 3.1565.3 GPS week: 1565 Day: 3 MJD: 55202
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1852 21 10 18 20 --- 9 | 37 24 30 35 --- 27
R03 | 546 20 12 18 28 --- 11 | 25 34 29 46 --- 29
XR05 | ---- --- 7 --- --- --- 0 | --- 70 --- --- --- 72
R07 | 1642 15 10 16 25 --- 9 | 35 44 39 31 --- 38
R08 | 2183 18 10 13 22 89 8 | 34 37 36 36 79 34
R10 | 2124 18 8 13 33 --- 10 | 27 33 42 31 --- 30
R11 | 556 21 20 29 21 87 13 | 35 41 47 33 31 32
R13 | 996 17 11 22 30 --- 11 | 37 27 42 27 --- 29
R14 | 2784 19 11 19 11 --- 9 | 25 29 45 26 --- 28
R15 | 2168 18 12 33 30 121 13 | 24 32 63 23 51 31
R17 | 1097 25 11 31 36 --- 14 | 37 51 67 36 --- 47
R18 | 1201 18 15 20 37 --- 12 | 17 36 32 34 --- 26
R19 | 877 18 17 16 29 --- 11 | 25 33 30 30 --- 27
R20 | 806 23 15 27 23 --- 12 | 41 34 39 24 --- 27
R21 | 1995 26 13 20 18 --- 11 | 36 41 39 34 --- 34
XR23 | 1163 --- 75 --- 334 --- 196 | --- 9999 --- 31 --- 9999
------+------------------------------------+--------------------------------
RMS | 1637 20 13 22 27 100 |T 31 37 41 31 53 34
WRMS | 1637 20 13 21 27 100 |NE 31 37 41 31 53 34
MEDI | 1201 18 11 19 28 89 |MD 34 34 39 31 51 30
Table 3.1565.4 GPS week: 1565 Day: 4 MJD: 55203
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2205 15 6 12 13 --- 6 | 26 19 30 23 --- 20
R03 | 1183 18 6 13 24 --- 8 | 20 37 44 34 --- 33
XR05 | 4268 46 29 --- 64 --- 31 | 34 61 --- 25 --- 49
R07 | 2124 15 11 14 19 --- 8 | 28 25 28 22 --- 24
R08 | 950 11 14 10 19 147 7 | 26 26 32 25 69 26
R10 | 784 16 16 26 31 --- 12 | 25 22 39 23 --- 20
R11 | 488 13 14 16 16 61 8 | 23 28 32 22 19 22
R13 | 1117 16 12 21 27 --- 10 | 22 26 37 22 --- 24
R14 | 1803 11 11 13 16 --- 7 | 20 23 29 20 --- 21
R15 | 2224 22 14 23 28 143 12 | 27 30 40 20 28 24
R17 | 928 18 20 16 41 --- 13 | 24 45 33 47 --- 35
R18 | 2032 16 13 21 27 --- 10 | 21 28 32 40 --- 27
R19 | 699 19 10 15 23 --- 9 | 29 41 51 34 --- 39
R20 | 938 24 19 18 71 --- 18 | 27 26 32 35 --- 25
R21 | 900 16 5 14 23 --- 8 | 31 27 47 30 --- 30
XR23 | 8423 --- 4 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 1443 17 13 17 30 124 |T 25 30 36 28 38 27
WRMS | 1443 17 12 17 30 124 |NE 25 30 36 28 38 27
MEDI | 1117 16 12 15 24 143 |MD 26 27 32 25 28 25
Table 3.1565.5 GPS week: 1565 Day: 5 MJD: 55204
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 664 13 11 17 14 --- 8 | 22 20 32 30 --- 22
R03 | 577 16 11 29 15 --- 10 | 27 28 37 43 --- 28
XR05 | 5532 46 30 --- 57 --- 30 | 21 56 --- 45 --- 52
R07 | 1299 15 12 21 21 --- 9 | 23 31 32 33 --- 28
R08 | 1680 17 13 9 15 223 8 | 21 18 27 33 66 20
R10 | 1568 21 13 16 13 --- 9 | 25 28 28 23 --- 23
R11 | 2178 21 14 26 17 67 11 | 21 27 41 26 18 23
R13 | 737 16 14 19 23 --- 10 | 27 29 39 30 --- 25
R14 | 3804 16 9 19 18 --- 9 | 18 20 35 25 --- 20
R15 | 2509 27 20 23 18 156 13 | 34 30 29 25 27 22
R17 | 983 32 12 29 23 --- 14 | 18 20 33 43 --- 21
R18 | 2261 13 11 18 12 --- 8 | 19 21 38 36 --- 21
R19 | 760 23 15 13 17 --- 10 | 28 34 38 33 --- 30
R20 | 770 30 20 16 60 --- 19 | 29 30 33 22 --- 22
R21 | 2255 12 13 19 18 --- 9 | 18 23 26 37 --- 20
XR23 | ---- --- 5 --- --- --- 0 | --- 9999 --- --- --- 9999
------+------------------------------------+--------------------------------
RMS | 1815 20 14 20 23 162 |T 23 27 33 32 37 25
WRMS | 1815 20 13 20 23 162 |NE 23 27 33 32 37 25
MEDI | 1568 17 13 19 18 156 |MD 22 28 33 33 27 22
Table 3.1565.6 GPS week: 1565 Day: 6 MJD: 55205
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL
------+-------------------------------+---------------------------
R02 | 1421 13 10 10 --- 7 | 24 25 28 --- 25
R03 | 605 19 11 13 --- 10 | 32 42 45 --- 39
XR05 | 5433 37 20 --- --- 28 | 18 51 --- --- 46
R07 | 3051 13 11 20 --- 10 | 38 35 51 --- 39
R08 | 2770 15 13 19 270 11 | 37 31 49 76 35
R10 | 2778 29 14 20 --- 14 | 23 25 31 --- 22
R11 | 1898 26 15 23 139 14 | 27 41 46 27 36
R13 | 1461 12 5 14 --- 7 | 27 30 46 --- 33
R14 | 4393 19 7 18 --- 10 | 23 28 38 --- 28
R15 | 1967 14 19 20 174 13 | 26 33 32 41 27
R17 | 1307 19 6 23 --- 11 | 23 40 51 --- 37
R18 | 919 18 12 13 --- 10 | 24 32 33 --- 27
R19 | 524 16 12 13 --- 10 | 28 42 42 --- 36
R20 | 2117 26 9 28 --- 15 | 28 32 31 --- 27
R21 | 2511 21 7 23 --- 12 | 24 37 46 --- 33
XR23 | ---- --- 6 --- --- 0 | --- 9999 --- --- 9999
------+-------------------------------+---------------------------
RMS | 2230 19 11 19 202 |T 26 34 40 48 32
WRMS | 2230 19 10 19 202 |NE 26 34 40 48 32
MEDI | 1967 19 11 19 174 |MD 26 33 42 41 33
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