[IGSREPORT-18348] Wk 1571 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 4 05:45:08 PST 2010
******************************************************************************
IGS Electronic Report 04 Mar 05:45:31 PST 2010 Message Number 18348
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1571 (Feb 14, 2010 - Feb 20, 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 2.1571.
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:
igl1571[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1571 in the SP3 format.
igl15717.sum Combination Report for GPS Week 1571.
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 | 553.0 ns
1 | 470.2 ns
2 | 368.0 ns
3 | 381.1 ns
4 | 380.6 ns
5 | 482.3 ns
6 | 489.6 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 1.1571, 1a.1571).
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 2.1571.0-6)
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 3.1571.0-6).
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 1571 summary. (Feb 14, 2010 - Feb 20, 2010)
Table 1.1571.a GPS week : 1571 MJD: 55241.0-55247.0
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 128| 0 1 -6 2 -21 -60 -.12 27 26 | 0 -75 1802 1919
| 1 1 3 32 33 113 .04 | 0 360
cod 243| -1 0 -5 11 -23 69 -.16 20 16 | --- --- --- ---
| 1 1 2 26 17 72 .05 | --- ---
esx 130| 0 0 -7 -5 55 12 .35 30 25 | 94348 -1399 4310 8968
| 2 2 4 42 27 59 .06 | 69842 4290
iac n/a| 0 1 22 -35 -14 -3 -.03 31 31 | 446666 -510 4312 8958
| 2 1 8 23 14 65 .07 | 70792 1681
mcc n/a| 0 2 41 -56 -52 -75 .55 149 149 | --- --- --- ---
| 8 5 11 150 102 751 .71 | --- ---
Table 1.1571.b GPS week : 1571 MJD: 55241.0-55247.0
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 | 13 15 10 11 8 9 13 |
R02 | 12 12 11 9 12 13 13 |
R03 | 16 14 10 14 10 12 14 |
R04 | 20 11 15 9 11 13 13 |
R05 | 16 15 18 19 13 15 10 |
R07 | 11 12 12 11 14 14 11 |
R08 | 16 10 12 14 13 14 12 |
R10 | 11 8 12 12 10 8 14 |
R11 | 18 13 15 11 14 14 11 |
R13 | 11 13 9 10 8 13 42 |
R14 | 14 11 14 10 8 9 11 |
R15 | 25 12 12 8 13 9 13 |
R17 | 14 14 14 21 15 17 26 |
R18 | 14 15 19 16 18 18 19 |
R19 | 14 16 19 15 21 21 20 |
R20 | 15 19 22 17 23 30 28 |
R21 | 13 11 12 17 19 21 19 |
R23 | 20 17 16 16 21 25 29 |
Table 1.1571.c GPS week : 1571 MJD: 55241.0-55247.0
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 1571 0 | 27 -32 166 -918 453 -22280 87.7 2560 2560 | 552961 0
brd 1571 1 | 88 183 263 -564 -1938 -17370 88.6 2384 2384 | 470182 0
brd 1571 2 | -149 -11 264 -3616 -629 -10780 87.5 2446 2446 | 368026 0
brd 1571 3 | -41 -109 37 -2009 -1450 -10160 86.1 2225 2225 | 381062 0
brd 1571 4 | 93 -58 60 -1705 -1223 -13770 89.3 2295 2295 | 380554 0
brd 1571 5 | 41 201 227 -889 178 -14630 90.3 2012 2012 | 482345 0
brd 1571 6 | 63 70 170 2005 -539 -12440 90.3 1876 1876 | 489596 0
-------------+------------------------------------------------------------+----------------
brd 1571 mean| 17 34 169 -1099 -735 -14489 88.5 2256 2256 | 446389 0
brd 1571 sdev| 86 120 91 1709 865 4207 1.5 241 241 | 70505 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 2.1571.0 GPS week: 1571 Day: 0 MJD: 55241
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 128| -2 2 -10 57 -46 -17 -.13 30 30 | 0 507 1928 2065
cod 243| -2 -1 -6 -43 7 33 -.17 22 18 | --- --- --- ---
esx 130| 3 -3 -2 -2 71 -12 .38 28 25 | 191908 3035 4316 9250
iac n/a| -2 4 19 2 -16 10 -.12 27 27 | 554313 -773 4320 9086
mcc n/a| -2 6 42 -340 -5 237 1.79 227 227 | --- --- --- ---
Table 2.1571.1 GPS week: 1571 Day: 1 MJD: 55242
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 128| 0 0 -2 32 -11 -54 -.14 22 21 | 0 -730 2055 2208
cod 243| -2 0 -2 36 -21 17 -.06 16 15 | --- --- --- ---
esx 130| 2 1 -5 -92 86 95 .32 27 26 | 119296 -6836 4064 10344
iac n/a| 0 3 17 -24 -23 -10 -.09 30 30 | 471100 -2813 4052 9084
mcc n/a| -8 4 31 94 -114 782 .61 165 165 | --- --- --- ---
Table 2.1571.2 GPS week: 1571 Day: 2 MJD: 55243
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 128| 2 -1 -3 -10 14 159 -.15 26 26 | 0 -100 2188 2396
cod 243| -2 0 -3 23 -32 -34 -.19 18 16 | --- --- --- ---
esx 130| -1 0 -8 15 21 -58 .39 26 23 | 17542 910 3888 10307
iac n/a| 3 0 22 -56 3 -2 -.06 31 31 | 367597 1640 3909 10004
mcc n/a| 12 -1 50 -94 23 409 .60 139 139 | --- --- --- ---
Table 2.1571.3 GPS week: 1571 Day: 3 MJD: 55244
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 128| 0 2 -8 -39 -7 -71 -.08 23 23 | 0 -39 1688 1741
cod 243| -1 0 -7 6 -40 72 -.12 16 14 | --- --- --- ---
esx 130| 2 -2 -9 29 92 -20 .36 28 25 | 18726 -4731 4036 8427
iac n/a| 0 1 30 -13 1 27 -.05 30 30 | 382544 -2530 4013 9122
mcc n/a| 7 1 29 -139 94 585 1.01 135 135 | --- --- --- ---
Table 2.1571.4 GPS week: 1571 Day: 4 MJD: 55245
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 128| 2 0 -4 -6 -10 -97 -.13 23 22 | 0 17 1594 1675
cod 243| 0 0 -4 6 -26 144 -.14 21 19 | --- --- --- ---
esx 130| -2 1 -3 31 44 94 .32 26 22 | 35479 4252 4747 7287
iac n/a| 0 0 11 -57 -25 -143 .02 32 32 | 379864 1068 4753 8037
mcc n/a| 0 7 46 7 -173 -948 -.36 137 137 | --- --- --- ---
Table 2.1571.5 GPS week: 1571 Day: 5 MJD: 55246
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 128| 0 2 -2 -13 -84 -197 -.04 27 27 | 0 -59 1720 1815
cod 243| 0 -3 -2 22 -9 172 -.20 20 16 | --- --- --- ---
esx 130| -3 1 -11 1 34 -11 .24 28 25 | 131607 -1441 4740 8223
iac n/a| 2 0 18 -45 -34 51 .04 39 39 | 482242 59 4721 8131
mcc n/a| -7 6 57 64 -170 -1004 .26 128 128 | --- --- --- ---
Table 2.1571.6 GPS week: 1571 Day: 6 MJD: 55247
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 128| 2 1 -11 -3 -2 -143 -.15 37 31 | 0 -126 1447 1535
cod 243| 0 1 -10 26 -42 82 -.22 23 18 | --- --- --- ---
esx 130| 2 -4 -12 -19 36 0 .41 43 29 | 145883 -4988 4383 8943
iac n/a| 0 3 36 -51 -8 40 .05 33 33 | 489005 -222 4417 9245
mcc n/a| -6 -7 28 12 -26 -587 -.07 112 112 | --- --- --- ---
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 3.1571.0 GPS week: 1571 Day: 0 MJD: 55241
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01M | 1108 30 14 25 21 --- 13 | 36 38 45 23 --- 31
R02 | 2038 25 10 22 20 --- 11 | 36 26 30 34 --- 28
R03 | 907 32 28 19 29 --- 15 | 44 52 66 63 --- 54
R04 | 3261 45 41 14 30 --- 20 | 34 47 39 40 --- 31
R05M | 1043 46 15 28 13 --- 15 | 27 34 40 45 --- 33
R07M | 4946 19 10 27 16 --- 11 | 34 46 49 42 --- 40
R08M | 2019 33 20 23 31 287 15 | 47 53 61 44 36 49
R10 | 2007 23 20 12 17 --- 10 | 34 24 25 18 --- 20
R11M | 2553 27 28 39 22 164 17 | 21 22 46 31 53 25
R13M | 3176 21 13 19 21 --- 10 | 22 37 36 22 --- 26
R14M | 1469 22 21 30 24 --- 14 | 33 38 36 36 --- 31
R15M | 4440 32 22 64 46 214 25 | 27 34 71 38 49 29
R17E | 1809 26 24 13 29 --- 13 | 25 36 33 39 --- 28
R18E | 1425 26 20 20 26 --- 13 | 28 48 46 41 --- 35
R19E | 978 27 24 19 28 --- 14 | 141 151 140 131 --- 140
R20E | 1076 25 15 26 32 --- 14 | 31 38 47 40 --- 33
R21E | 754 34 12 21 18 --- 12 | 52 25 33 38 --- 30
R23E | 4577 30 37 35 36 --- 20 | 43 58 46 52 --- 43
------+------------------------------------+--------------------------------
RMS | 2559 30 22 28 27 227 |T 39 44 49 43 46 39
WRMS | 2559 30 18 25 27 227 |NE 37 37 40 38 --- 33
MEDI | 1809 27 20 22 24 214 |MD 34 38 45 39 49 31
Table 3.1571.1 GPS week: 1571 Day: 1 MJD: 55242
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1432 28 10 33 28 --- 14 | 44 26 26 29 --- 25
R02 | 1613 29 8 23 23 --- 12 | 53 35 34 45 --- 38
R03 | 1669 17 14 32 36 --- 14 | 32 43 54 38 --- 36
R04 | 2621 26 12 11 23 --- 11 | 34 42 55 45 --- 42
R05 | 1069 18 22 33 29 --- 14 | 45 28 67 57 --- 44
R07 | 2951 12 18 29 26 --- 12 | 20 28 48 29 --- 27
R08 | 1814 11 17 12 24 114 9 | 35 47 53 46 30 43
R10 | 966 16 11 13 16 --- 8 | 19 15 26 19 --- 15
R11 | 3103 14 18 16 37 163 12 | 26 17 30 36 42 21
R13 | 3141 21 18 29 22 --- 12 | 28 32 31 33 --- 24
R14 | 3543 17 13 26 24 --- 11 | 17 22 45 26 --- 23
R15 | 4024 13 11 33 20 205 11 | 25 30 55 33 56 31
R17E | 2639 24 18 30 26 --- 14 | 12 23 38 30 --- 18
R18E | 1825 20 12 33 40 --- 15 | 27 33 54 52 --- 33
R19E | 964 30 26 28 27 --- 16 | 110 120 115 105 --- 111
R20E | 2242 37 19 37 41 --- 19 | 39 46 53 49 --- 39
R21E | 871 22 11 20 19 --- 10 | 25 25 52 36 --- 29
R23E | 2943 17 22 29 48 --- 16 | 47 47 46 44 --- 36
------+------------------------------------+--------------------------------
RMS | 2384 22 16 27 30 165 |T 35 36 49 41 42 35
WRMS | 2384 21 15 26 30 165 |NE 34 33 42 36 --- 32
MEDI | 1825 18 14 29 26 163 |MD 28 30 48 36 42 31
Table 3.1571.2 GPS week: 1571 Day: 2 MJD: 55243
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1749 16 13 11 26 --- 9 | 34 40 40 31 --- 33
R02 | 2031 23 9 13 28 --- 10 | 38 24 28 26 --- 23
R03 | 2207 20 17 12 16 --- 9 | 41 53 55 45 --- 48
R04 | 1937 23 22 34 25 --- 15 | 28 42 50 26 --- 32
R05 | 1162 36 22 23 45 --- 18 | 34 40 44 43 --- 34
R07 | 2454 14 17 23 30 --- 12 | 42 53 42 47 --- 42
R08 | 1563 20 20 15 24 91 11 | 32 45 46 28 29 37
R10 | 714 30 15 19 16 --- 11 | 22 27 25 25 --- 20
R11 | 1905 37 14 26 24 109 14 | 23 27 40 22 49 24
R13 | 2311 17 14 12 15 --- 8 | 25 30 32 24 --- 24
R14 | 4793 29 15 29 25 --- 14 | 24 38 52 34 --- 31
R15 | 3977 16 16 26 22 194 11 | 24 28 51 31 45 29
R17E | 2588 19 18 31 30 --- 14 | 17 28 48 40 --- 26
R18E | 2002 24 16 37 50 --- 18 | 22 31 49 39 --- 27
R19E | 1195 27 32 34 36 --- 18 | 99 107 84 86 --- 92
R20E | 3803 41 19 42 50 --- 22 | 28 26 67 43 --- 30
R21E | 916 19 18 21 27 --- 12 | 22 29 33 33 --- 23
R23E | 2523 30 17 33 33 --- 16 | 51 36 49 54 --- 41
------+------------------------------------+--------------------------------
RMS | 2446 26 18 26 31 139 |T 33 39 46 37 41 34
WRMS | 2446 26 16 23 31 139 |NE 32 36 39 30 --- 30
MEDI | 2002 23 17 23 26 109 |MD 28 31 46 33 45 30
Table 3.1571.3 GPS week: 1571 Day: 3 MJD: 55244
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 860 24 15 19 19 --- 11 | 30 36 42 22 --- 28
R02 | 2726 17 7 19 19 --- 9 | 53 37 41 36 --- 39
R03 | 2372 27 14 30 25 --- 13 | 40 31 28 29 --- 24
R04 | 1550 11 13 15 21 --- 8 | 50 48 53 35 --- 45
R05 | 582 39 17 27 49 --- 19 | 60 39 35 23 --- 34
R07 | 3511 23 13 22 21 --- 11 | 32 46 53 45 --- 41
R08 | 2443 24 12 34 29 113 14 | 42 33 39 31 49 28
R10 | 1945 26 15 22 22 --- 12 | 23 32 33 19 --- 20
R11 | 1234 16 12 30 19 102 11 | 44 41 53 47 92 42
R13 | 1853 16 16 15 19 --- 9 | 25 34 29 30 --- 25
R14 | 1584 16 18 16 17 --- 10 | 22 33 27 27 --- 23
R15 | 3544 15 9 15 15 177 8 | 39 46 43 49 102 42
R17E | 2344 30 15 57 36 --- 20 | 19 33 71 34 --- 31
R18E | 2393 17 15 31 46 --- 16 | 32 29 50 39 --- 28
R19E | 1950 27 22 17 37 --- 15 | 166 144 162 150 --- 153
R20E | 2693 25 18 28 47 --- 16 | 26 35 52 60 --- 34
R21E | 1135 18 30 37 32 --- 17 | 19 25 46 31 --- 18
R23E | 2619 30 21 27 33 --- 15 | 50 34 49 44 --- 36
------+------------------------------------+--------------------------------
RMS | 2224 23 16 28 30 135 |T 42 42 50 41 81 38
WRMS | 2224 23 14 25 30 135 |NE 41 37 38 29 --- 32
MEDI | 1950 23 15 22 22 113 |MD 32 34 43 34 92 31
Table 3.1571.4 GPS week: 1571 Day: 4 MJD: 55245
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1133 10 13 13 15 --- 7 | 27 33 31 33 --- 28
R02 | 2292 19 17 21 23 --- 11 | 40 26 45 29 --- 33
R03 | 2127 12 19 17 18 --- 9 | 27 35 37 37 --- 31
R04 | 1570 11 18 13 31 --- 11 | 18 31 26 24 --- 20
R05 | 868 23 20 15 31 --- 13 | 27 36 36 47 --- 29
R07 | 3910 22 26 27 23 --- 14 | 36 63 34 54 --- 42
R08 | 2383 30 17 17 24 110 13 | 33 45 45 55 60 40
R10 | 2454 13 19 19 12 --- 9 | 17 19 33 15 --- 17
R11 | 768 14 23 37 15 97 14 | 18 25 35 24 38 13
R13 | 790 12 16 10 12 --- 7 | 17 18 29 16 --- 16
R14 | 869 6 18 16 11 --- 8 | 22 26 21 22 --- 19
R15 | 3828 25 15 24 24 186 13 | 26 40 50 31 97 33
R17E | 1763 16 21 29 36 --- 15 | 28 32 29 39 --- 22
R18E | 1675 23 19 28 50 --- 17 | 27 26 39 46 --- 25
R19E | 2300 33 23 43 42 --- 20 | 90 115 133 112 --- 108
R20E | 1159 35 23 33 66 --- 23 | 17 26 38 53 --- 24
R21E | 1634 20 38 31 43 --- 19 | 22 37 40 41 --- 24
R23E | 4656 45 16 41 39 --- 21 | 39 31 27 62 --- 32
------+------------------------------------+--------------------------------
RMS | 2295 23 21 26 32 137 |T 29 36 40 41 65 30
WRMS | 2295 22 19 22 32 137 |NE 25 27 35 26 --- 25
MEDI | 1675 19 19 21 24 110 |MD 27 31 35 37 60 25
Table 3.1571.5 GPS week: 1571 Day: 5 MJD: 55246
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 655 15 15 15 14 --- 8 | 17 34 39 34 --- 29
R02 | 933 25 16 25 16 --- 12 | 36 28 51 41 --- 34
R03 | 1223 14 16 19 32 --- 11 | 14 16 30 22 --- 15
R04 | 2297 23 16 15 36 --- 13 | 29 31 28 32 --- 25
R05 | 1408 24 18 24 36 --- 14 | 27 31 22 27 --- 19
R07 | 1761 18 22 26 33 --- 14 | 37 54 64 23 --- 44
R08 | 1538 28 21 29 13 73 14 | 51 69 69 64 43 61
R10 | 3104 11 12 17 14 --- 8 | 16 27 32 19 --- 20
R11 | 1364 11 21 37 23 110 14 | 24 21 65 37 37 31
R13 | 541 26 15 19 27 --- 12 | 14 29 31 32 --- 20
R14 | 1821 14 10 16 22 --- 9 | 12 17 21 26 --- 13
R15 | 3086 17 10 16 17 178 8 | 29 31 24 30 60 25
R17E | 843 38 21 24 28 --- 16 | 32 26 40 29 --- 26
R18E | 1655 21 15 33 51 --- 17 | 27 25 36 51 --- 24
R19E | 2352 26 23 43 55 --- 21 | 241 221 243 210 --- 228
R20E | 1154 46 27 54 84 --- 30 | 41 37 66 74 --- 38
R21E | 2314 25 28 29 64 --- 21 | 23 26 39 47 --- 24
R23E | 4128 57 32 35 42 --- 24 | 30 38 38 41 --- 26
------+------------------------------------+--------------------------------
RMS | 2012 27 20 28 39 128 |T 38 42 52 46 46 39
WRMS | 2012 27 16 25 39 128 |NE 23 25 35 28 --- 23
MEDI | 1538 23 16 24 28 110 |MD 27 29 38 32 43 25
Table 3.1571.6 GPS week: 1571 Day: 6 MJD: 55247
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1219 17 22 25 26 --- 13 | 31 47 32 24 --- 31
R02 | 1022 18 12 15 35 --- 12 | 29 30 37 47 --- 31
R03 | 927 25 20 33 20 --- 14 | 30 29 31 16 --- 21
R04 | 1549 21 15 25 29 --- 13 | 20 35 42 22 --- 28
R05 | 861 21 11 15 21 --- 9 | 43 46 49 38 --- 40
R07 | 1962 25 15 18 13 --- 10 | 34 52 52 46 --- 45
R08 | 1108 19 23 19 22 66 12 | 43 44 48 37 48 39
R10 | 2353 23 17 15 35 --- 13 | 21 29 24 19 --- 17
R11 | 2306 18 15 18 24 130 11 | 33 27 35 28 33 26
R13 | 603 51 35 136 37 --- 41 | 17 31 110 26 --- 28
R14 | 1437 18 14 25 19 --- 10 | 16 20 27 26 --- 18
R15 | 3904 24 17 31 20 128 13 | 27 21 30 22 53 20
R17E | 830 64 46 35 28 --- 26 | 34 51 36 35 --- 25
R18E | 1954 23 29 43 35 --- 19 | 34 24 37 41 --- 26
R19E | 2301 49 22 27 39 --- 20 | 198 210 209 204 --- 204
R20E | 1112 61 24 50 56 --- 27 | 50 37 50 56 --- 35
R21E | 1636 26 21 31 49 --- 18 | 37 33 46 55 --- 36
R23E | 3073 75 24 51 44 --- 28 | 52 39 44 53 --- 40
------+------------------------------------+--------------------------------
RMS | 1875 37 23 43 33 112 |T 41 44 52 44 44 39
WRMS | 1875 31 18 29 33 112 |NE 25 30 33 26 --- 24
MEDI | 1437 23 20 25 28 128 |MD 33 33 37 35 48 28
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