[IGSREPORT-18414] Wk 1574 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 25 05:47:40 PDT 2010
******************************************************************************
IGS Electronic Report 25 Mar 05:47:53 PDT 2010 Message Number 18414
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1574 (Mar 07, 2010 - Mar 13, 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 2.1574.
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:
igl1574[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1574 in the SP3 format.
igl15747.sum Combination Report for GPS Week 1574.
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 | 485.8 ns
1 | 430.6 ns
2 | 487.5 ns
3 | 484.4 ns
4 | 481.7 ns
5 | 482.0 ns
6 | 477.4 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 1.1574, 1a.1574).
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 2.1574.0-6)
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 3.1574.0-6).
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 1574 summary. (Mar 07, 2010 - Mar 13, 2010)
Table 1.1574.a GPS week : 1574 MJD: 55262.0-55268.0
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 132| 2 1 9 24 -13 -61 -.15 29 28 | 0 -78 1707 1770
| 1 1 5 30 35 188 .07 | 0 155
cod 245| -2 0 -5 17 14 30 -.11 16 13 | --- --- --- ---
| 0 1 2 12 20 70 .03 | --- ---
esx 124| 0 0 -8 -21 -22 52 .39 27 24 | 130104 -440 4154 8187
| 1 1 5 29 28 56 .06 | 17763 2526
iac n/a| 3 1 9 -36 -2 -33 -.12 27 27 | 1523256 13130 168845 346604
| 1 1 4 10 26 74 .07 | 2657006 9896
mcc n/a| 2 -3 47 22 -11 316 -.03 150 150 | --- --- --- ---
| 3 9 14 92 122 430 .43 | --- ---
Table 1.1574.b GPS week : 1574 MJD: 55262.0-55268.0
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
------+------------------------------------+------------------------------------------
R01 | 15 13 15 12 10 13 14 |
R02 | 13 11 8 11 11 12 9 |
R03 | 12 12 12 10 10 11 14 |
R04 | 10 11 11 10 9 9 11 |
R05 | 10 11 14 12 10 14 12 |
R07 | 11 11 11 13 8 10 12 |
R08 | 12 12 11 10 10 9 9 |
R10 | 12 12 8 10 14 13 15 |
R11 | 11 11 14 13 16 15 11 |
R13 | 16 16 17 16 15 8 8 |
R14 | 46 43 24 33 39 42 29 |
R15 | 12 14 15 16 12 8 10 |
R17 | 15 15 14 16 12 20 14 |
R18 | 13 23 12 14 32 26 11 |
R19 | 14 20 16 15 8 11 10 |
R20 | 19 25 16 14 13 16 17 |
R21 | 19 13 16 13 14 12 12 |
R23 | 20 18 19 16 17 16 17 |
Table 1.1574.c GPS week : 1574 MJD: 55262.0-55268.0
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 1574 0 | -53 125 116 -785 1489 -17060 85.2 2625 2625 | 485788 0
brd 1574 1 | -44 -17 293 -999 1707 -17870 84.5 2595 2595 | 430643 0
brd 1574 2 | 0 119 225 951 2691 -18340 85.3 2512 2512 | 487513 0
brd 1574 3 | 126 49 83 2324 2268 -22250 87.5 2582 2582 | 484391 0
brd 1574 4 | -85 1 84 238 -773 -21860 87.3 3103 3103 | 481693 0
brd 1574 5 | -1 -48 75 -117 -3194 -17700 89.5 3323 3323 | 481982 0
brd 1574 6 | 51 42 250 -588 167 -15910 87.0 2306 2306 | 477368 0
-------------+------------------------------------------------------------+----------------
brd 1574 mean| -1 38 161 146 622 -18712 86.6 2720 2720 | 475625 0
brd 1574 sdev| 71 66 91 1168 2067 2411 1.7 357 357 | 20104 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 2.1574.0 GPS week: 1574 Day: 0 MJD: 55262
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 132| 4 2 16 41 -45 -173 -.09 30 29 | 0 -53 1485 1550
cod 245| -2 0 -7 0 44 33 -.12 13 11 | --- --- --- ---
esx 124| -1 -1 -12 -60 -30 41 .30 32 29 | 130975 1465 4189 7768
iac n/a| 5 3 13 -29 4 22 -.00 30 30 | 7548048 26646 999999 999999
mcc n/a| 6 3 54 28 -122 116 .30 122 122 | --- --- --- ---
Table 2.1574.1 GPS week: 1574 Day: 1 MJD: 55263
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 132| 1 0 4 -10 23 -300 -.18 27 25 | 0 -324 1679 1744
cod 245| -1 2 -1 12 2 105 -.16 17 13 | --- --- --- ---
esx 124| -2 -2 -7 1 -51 132 .37 32 26 | 91342 -2014 3955 7756
iac n/a| 3 0 3 -36 11 44 -.05 31 31 | 452735 1546 20093 112444
mcc n/a| 0 -14 61 14 23 -48 -.23 142 142 | --- --- --- ---
Table 2.1574.2 GPS week: 1574 Day: 2 MJD: 55264
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 132| 4 1 9 18 26 132 -.09 28 27 | 0 -131 1988 2034
cod 245| -3 0 -2 23 -16 -34 -.09 15 16 | --- --- --- ---
esx 124| -1 -1 -16 -56 -20 -43 .40 25 23 | 144085 -1014 4817 9493
iac n/a| 4 1 12 -55 38 -59 -.14 30 30 | 527038 16775 29921 215681
mcc n/a| 6 -14 59 28 107 231 -.76 155 155 | --- --- --- ---
Table 2.1574.3 GPS week: 1574 Day: 3 MJD: 55265
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 132| 2 3 17 24 14 82 -.13 26 26 | 0 -106 1559 1641
cod 245| -3 -2 -8 18 21 -75 -.11 15 13 | --- --- --- ---
esx 124| 0 0 -5 -14 -36 95 .33 24 21 | 141693 -2746 4154 7707
iac n/a| 1 0 6 -32 -18 -15 -.14 28 28 | 534419 9675 36790 271359
mcc n/a| 3 -7 42 -125 -186 955 .48 105 105 | --- --- --- ---
Table 2.1574.4 GPS week: 1574 Day: 4 MJD: 55266
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 132| 1 2 13 77 -15 120 -.13 31 26 | 0 18 1538 1606
cod 245| -2 0 -6 13 1 76 -.09 19 15 | --- --- --- ---
esx 124| 2 0 -9 -17 -32 31 .39 28 25 | 133845 4426 3781 8193
iac n/a| 2 0 5 -33 3 -184 -.13 20 20 | 556314 20241 39757 379995
mcc n/a| 2 7 46 -50 51 893 .33 140 140 | --- --- --- ---
Table 2.1574.5 GPS week: 1574 Day: 5 MJD: 55267
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 132| 2 2 5 -9 -40 -8 -.17 30 28 | 0 182 2010 2071
cod 245| -1 -1 -7 40 30 1 -.11 15 11 | --- --- --- ---
esx 124| 0 0 -7 22 -18 35 .45 26 24 | 136568 -1313 4080 8083
iac n/a| 2 2 15 -44 -10 -21 -.20 27 27 | 567910 17242 51282 438833
mcc n/a| -3 6 48 108 135 156 -.14 117 117 | --- --- --- ---
Table 2.1574.6 GPS week: 1574 Day: 6 MJD: 55268
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 132| 3 0 3 28 -57 -284 -.28 32 32 | 0 -138 1691 1748
cod 245| 0 0 -5 14 14 106 -.06 15 13 | --- --- --- ---
esx 124| 0 0 0 -25 36 77 .47 21 18 | 132225 -1886 4107 8311
iac n/a| 1 1 6 -26 -45 -19 -.20 21 21 | 476332 -214 4076 7922
mcc n/a| 2 -3 17 152 -86 -90 -.19 269 269 | --- --- --- ---
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 3.1574.0 GPS week: 1574 Day: 0 MJD: 55262
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2048 44 8 34 16 --- 14 | 28 51 72 57 --- 47
R02 | 1636 32 11 28 25 --- 13 | 25 50 61 64 --- 49
R03 | 1097 32 11 29 17 --- 12 | 29 43 57 41 --- 38
R04 | 1871 15 10 20 26 --- 10 | 26 48 44 38 --- 38
R05 | 525 15 12 26 13 --- 9 | 40 57 43 44 --- 47
R07 | 2640 28 11 20 17 --- 10 | 39 60 74 67 --- 59
R08 | 821 31 10 31 16 149 12 | 23 49 69 43 27 44
R10 | 2495 29 8 26 28 --- 12 | 27 38 41 36 --- 32
R11 | 1607 20 10 30 22 75 11 | 35 40 55 29 50 37
R13 | 961 31 8 50 29 --- 16 | 21 27 43 29 --- 24
XR14 |16656 83 44 --- 85 --- 46 | 89 42 --- 96 --- 53
R15 | 3534 26 12 23 25 131 11 | 22 23 31 27 25 21
R17E | 3026 25 17 23 42 --- 15 | 24 29 38 45 --- 28
R18E | 5789 19 14 21 39 --- 13 | 42 47 64 64 --- 49
R19E | 965 29 15 26 35 --- 14 | 163 186 195 204 --- 186
R20E | 4673 41 12 40 46 --- 18 | 39 43 67 63 --- 46
R21E | 2437 27 21 48 43 --- 19 | 44 33 46 64 --- 37
R23E | 2002 41 22 43 45 --- 20 | 51 61 66 91 --- 61
------+------------------------------------+--------------------------------
RMS | 2625 30 13 32 30 122 |T 42 51 62 61 34 49
WRMS | 2625 29 11 29 30 122 |NE 33 44 53 47 34 40
MEDI | 2002 29 11 28 26 131 |MD 29 43 57 45 27 44
Table 3.1574.1 GPS week: 1574 Day: 1 MJD: 55263
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1878 29 14 27 24 --- 13 | 14 30 47 28 --- 24
R02 | 892 19 11 25 25 --- 11 | 25 17 31 37 --- 20
R03 | 1976 17 16 26 23 --- 11 | 39 35 32 23 --- 26
R04 | 1602 11 16 17 26 --- 10 | 22 34 22 19 --- 18
R05 | 1153 17 18 16 23 --- 11 | 24 41 30 14 --- 26
R07 | 1789 20 12 23 22 --- 10 | 44 40 58 55 --- 45
R08 | 748 26 11 21 23 213 11 | 16 32 38 48 30 28
R10 | 1728 21 16 15 28 --- 11 | 31 26 31 36 --- 24
R11 | 984 28 9 18 24 65 11 | 32 29 34 29 41 24
R13 | 846 26 12 50 22 --- 16 | 21 27 54 22 --- 21
XR14 |20160 27 50 --- 98 --- 43 | 39 48 --- 61 --- 31
R15 | 3145 33 16 24 26 105 14 | 20 27 34 27 18 17
R17E | 3517 27 20 20 33 --- 14 | 24 27 39 42 --- 27
R18E | 6838 25 24 72 32 --- 23 | 31 39 88 43 --- 38
R19E | 2258 36 21 40 43 --- 19 | 155 183 203 181 --- 179
R20E | 3819 51 30 44 54 --- 25 | 42 50 73 49 --- 45
R21E | 1836 23 14 24 33 --- 13 | 25 33 38 44 --- 29
R23E | 1336 33 16 34 46 --- 18 | 39 55 72 84 --- 56
------+------------------------------------+--------------------------------
RMS | 2594 27 17 32 31 142 |T 35 42 54 46 29 37
WRMS | 2594 25 13 26 31 142 |NE 27 32 37 33 29 25
MEDI | 1789 26 16 24 26 105 |MD 25 33 38 37 30 26
Table 3.1574.2 GPS week: 1574 Day: 2 MJD: 55264
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 888 26 22 25 33 --- 15 | 19 35 50 28 --- 27
R02 | 897 12 12 18 15 --- 8 | 30 31 46 31 --- 31
R03 | 1734 19 11 24 28 --- 11 | 24 36 56 39 --- 35
R04 | 786 16 16 16 27 --- 11 | 30 45 37 45 --- 37
R05 | 1292 38 7 27 18 --- 13 | 28 46 69 51 --- 45
R07 | 927 17 13 26 16 --- 10 | 35 46 42 34 --- 37
R08 | 1015 26 15 13 25 236 11 | 21 34 41 47 69 31
R10 | 2314 14 11 13 21 --- 8 | 22 29 28 24 --- 21
R11 | 1742 20 22 24 27 83 13 | 28 46 51 33 56 34
R13 | 2001 32 18 42 19 --- 16 | 23 29 58 23 --- 25
XR14 |23735 34 22 --- 48 --- 23 | 63 55 --- 48 --- 49
R15 | 2224 45 16 17 26 97 15 | 26 23 33 29 30 16
R17E | 1569 27 12 26 36 --- 14 | 17 22 38 46 --- 24
R18E | 6534 20 14 26 24 --- 12 | 43 45 63 53 --- 46
R19E | 2644 34 18 22 39 --- 16 | 65 89 102 85 --- 83
R20E | 4856 34 14 24 38 --- 15 | 41 39 52 40 --- 37
R21E | 755 31 13 36 31 --- 15 | 26 31 53 39 --- 31
R23E | 2191 34 20 24 53 --- 18 | 51 49 40 59 --- 42
------+------------------------------------+--------------------------------
RMS | 2511 28 15 25 30 155 |T 32 40 50 41 51 36
WRMS | 2511 27 16 23 30 155 |NE 29 37 46 36 51 32
MEDI | 1734 26 14 24 27 97 |MD 28 36 50 39 56 34
Table 3.1574.3 GPS week: 1574 Day: 3 MJD: 55265
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 778 22 11 16 32 --- 11 | 37 53 57 71 --- 52
R02 | 1992 23 10 13 28 --- 10 | 17 35 46 58 --- 37
R03 | 2411 19 14 20 14 --- 9 | 39 49 54 42 --- 43
R04 | 820 19 13 15 22 --- 9 | 28 50 47 36 --- 40
R05 | 1619 29 16 19 16 --- 11 | 29 62 49 53 --- 49
R07 | 747 32 15 26 10 --- 12 | 29 57 66 55 --- 52
R08 | 1609 17 11 18 25 56 10 | 20 40 42 28 90 31
R10 | 2514 22 11 20 16 --- 9 | 23 21 32 29 --- 20
R11 | 2103 27 15 25 25 136 13 | 31 41 49 53 91 41
R13 | 2175 26 21 33 28 --- 15 | 22 30 47 31 --- 26
XR14 |27415 50 20 --- 71 --- 33 | 60 55 --- 85 --- 60
R15 | 1035 39 10 25 35 108 15 | 23 18 28 39 29 16
R17E | 750 30 18 34 31 --- 16 | 31 28 63 56 --- 38
R18E | 3579 30 17 25 29 --- 14 | 72 71 76 70 --- 69
R19E | 4468 18 21 38 21 --- 14 | 123 134 138 123 --- 128
R20E | 6605 18 19 21 36 --- 13 | 55 56 61 50 --- 52
R21E | 726 24 11 23 35 --- 13 | 28 39 49 38 --- 35
R23E | 1567 29 18 19 42 --- 15 | 51 59 44 60 --- 50
------+------------------------------------+--------------------------------
RMS | 2582 26 15 24 28 105 |T 39 49 55 54 70 46
WRMS | 2582 26 13 21 28 105 |NE 29 42 47 48 70 38
MEDI | 1619 24 15 21 28 108 |MD 29 49 49 53 90 41
Table 3.1574.4 GPS week: 1574 Day: 4 MJD: 55266
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 951 26 12 18 10 --- 9 | 33 52 52 55 --- 47
R02 | 3500 14 17 26 14 --- 10 | 41 40 74 54 --- 48
R03 | 1437 20 16 20 12 --- 10 | 36 53 48 49 --- 45
R04 | 940 11 11 23 14 --- 8 | 29 33 35 37 --- 31
R05 | 1471 22 9 19 18 --- 10 | 27 41 43 53 --- 39
R07 | 1285 17 13 16 7 --- 7 | 31 46 48 39 --- 39
R08 | 4003 20 19 16 15 66 10 | 31 48 37 40 44 39
R10 | 4114 40 11 23 20 --- 13 | 25 28 37 28 --- 23
R11 | 2510 42 17 35 15 213 15 | 47 50 47 36 54 40
R13 | 1299 26 14 34 27 --- 14 | 26 23 42 47 --- 28
XR14 |30997 72 32 --- 60 --- 38 | 43 49 --- 66 --- 37
R15 | 2822 30 11 24 17 95 11 | 20 23 34 23 28 20
R17E | 836 23 17 26 16 --- 11 | 31 35 63 51 --- 39
R18E | 1072 80 50 57 37 --- 32 | 57 103 122 75 --- 80
R19E | 5333 14 13 17 13 --- 8 | 79 74 87 79 --- 78
R20E | 7825 29 20 24 18 --- 13 | 48 60 75 53 --- 56
R21E | 1348 14 20 32 28 --- 14 | 35 46 57 44 --- 39
R23E | 1203 29 23 40 29 --- 17 | 46 44 68 55 --- 49
------+------------------------------------+--------------------------------
RMS | 3102 31 19 28 20 140 |T 38 47 57 49 42 43
WRMS | 3102 26 15 25 20 140 |NE 32 40 45 43 42 36
MEDI | 1437 23 16 24 16 95 |MD 33 46 48 49 44 39
Table 3.1574.5 GPS week: 1574 Day: 5 MJD: 55267
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2255 28 19 15 27 --- 12 | 29 55 46 37 --- 42
R02 | 4245 20 21 23 17 --- 11 | 20 43 29 32 --- 29
R03 | 841 27 9 15 22 --- 10 | 50 48 48 52 --- 46
R04 | 2050 17 8 16 20 --- 8 | 36 41 46 56 --- 42
R05 | 1309 35 11 31 17 --- 13 | 24 35 60 36 --- 36
R07 | 1915 20 14 18 14 --- 9 | 24 45 39 25 --- 33
R08 | 4535 18 14 14 15 90 8 | 27 32 33 21 28 26
R10 | 4644 29 10 17 35 --- 13 | 20 19 25 39 --- 19
R11 | 2426 38 14 24 27 166 14 | 31 40 53 26 29 35
R13 | 874 18 6 15 17 --- 8 | 23 29 42 37 --- 31
XR14 |33402 51 31 --- 91 --- 41 | 62 29 --- 80 --- 38
R15 | 5496 18 10 11 13 72 7 | 15 22 21 25 27 17
R17E | 1440 44 11 45 38 --- 19 | 30 53 94 45 --- 51
R18 | 990 47 31 53 54 --- 26 | 97 144 152 103 --- 122
R19E | 3723 18 11 28 13 --- 10 | 112 118 135 119 --- 120
R20E | 7164 47 17 23 23 --- 15 | 61 70 79 60 --- 65
R21 | 1803 22 19 17 27 --- 12 | 40 48 58 49 --- 46
R23E | 1963 31 13 29 38 --- 15 | 41 45 45 46 --- 40
------+------------------------------------+--------------------------------
RMS | 3323 30 15 26 27 117 |T 41 50 59 49 28 46
WRMS | 3323 28 11 24 27 117 |NE 30 36 40 38 28 32
MEDI | 2050 27 13 18 22 90 |MD 30 43 46 39 28 38
Table 3.1574.6 GPS week: 1574 Day: 6 MJD: 55268
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2716 38 13 25 22 --- 13 | 33 62 76 43 --- 55
R02 | 2491 21 12 11 20 --- 9 | 26 44 46 60 --- 43
R03 | 1287 30 22 28 13 --- 13 | 33 48 41 36 --- 35
R04 | 1655 33 13 16 19 --- 11 | 36 52 54 57 --- 49
R05 | 940 36 8 20 19 --- 11 | 30 54 59 43 --- 48
R07 | 1671 46 14 11 13 --- 12 | 33 64 56 52 --- 51
R08 | 4643 26 12 11 14 132 8 | 39 52 48 45 45 44
R10 | 3117 32 17 27 33 --- 15 | 32 29 38 45 --- 28
R11 | 983 23 15 22 19 444 11 | 42 52 62 38 57 47
R13 | 569 21 9 14 12 --- 7 | 39 33 38 40 --- 34
XR14 | 2633 61 29 --- 43 --- 29 | 72 42 --- 61 --- 46
R15 | 1684 19 15 7 24 51 9 | 39 25 35 36 36 30
R17 | 1498 34 11 28 24 --- 13 | 37 38 49 51 --- 38
R18 | 2195 34 11 17 16 --- 11 | 82 79 78 80 --- 77
R19 | 1888 31 13 14 15 --- 10 | 95 108 113 103 --- 105
R20 | 3644 30 28 29 30 --- 17 | 51 71 79 71 --- 67
R21 | 1334 27 12 22 26 --- 12 | 43 39 51 40 --- 40
R23 | 2763 45 21 31 28 --- 17 | 39 48 77 66 --- 55
------+------------------------------------+--------------------------------
RMS | 2306 32 15 21 21 269 |T 44 52 58 53 46 49
WRMS | 2306 32 13 18 21 269 |NE 37 46 50 46 46 42
MEDI | 1684 31 13 20 19 132 |MD 39 48 54 45 45 46
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