[IGSREPORT-18434] Wk 1575 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 1 05:49:13 PDT 2010
******************************************************************************
IGS Electronic Report 01 Apr 05:49:26 PDT 2010 Message Number 18434
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1575 (Mar 14, 2010 - Mar 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 2.1575.
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:
igl1575[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1575 in the SP3 format.
igl15757.sum Combination Report for GPS Week 1575.
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 | 473.4 ns
1 | 473.0 ns
2 | 474.0 ns
3 | 471.0 ns
4 | 470.4 ns
5 | 470.6 ns
6 | 467.2 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
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 1.1575, 1a.1575).
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 2.1575.0-6)
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 3.1575.0-6).
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 1575 summary. (Mar 14, 2010 - Mar 20, 2010)
Table 1.1575.a GPS week : 1575 MJD: 55269.0-55275.0
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 133| 2 -1 4 16 20 18 -.04 27 26 | 0 5 1530 1592
| 2 0 4 37 39 152 .11 | 0 41
cod 244| -2 0 -4 11 -4 28 -.10 13 13 | --- --- --- ---
| 1 1 2 16 22 50 .03 | --- ---
esx 140| 0 0 0 -17 -23 -38 .37 25 24 | 134308 -853 3675 8069
| 1 1 2 24 41 54 .06 | 6720 2259
iac n/a| 2 0 7 -18 4 -35 -.17 23 23 | 472044 -1050 3666 8104
| 1 0 4 24 7 51 .06 | 2757 1035
mcc n/a| 2 -2 60 -61 22 -214 -.23 101 101 | --- --- --- ---
| 6 9 19 132 118 331 .23 | --- ---
Table 1.1575.b GPS week : 1575 MJD: 55269.0-55275.0
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 | 12 12 9 10 9 8 15 |
R02 | 14 10 13 12 9 11 12 |
R03 | 10 15 15 16 14 10 12 |
R04 | 12 7 12 14 16 12 9 |
R05 | 11 13 9 15 14 12 13 |
R07 | 11 12 12 14 10 11 12 |
R08 | 9 11 12 12 10 10 11 |
R10 | 15 10 13 13 10 13 12 |
R11 | 13 14 10 15 12 14 15 |
R13 | 12 13 13 12 11 11 10 |
R14 | 25 15 12 22 15 18 13 |
R15 | 11 10 11 14 40 --- --- |
R17 | 16 14 13 16 14 12 13 |
R18 | 11 12 11 11 11 15 10 |
R19 | 9 11 11 10 10 9 13 |
R20 | 12 9 12 10 11 13 11 |
R21 | 12 11 10 12 13 13 12 |
R22 | --- --- --- --- --- 0 0 |
R23 | 21 14 18 18 14 0 0 |
R24 | --- --- --- --- --- --- 0 |
Table 1.1575.c GPS week : 1575 MJD: 55269.0-55275.0
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 1575 0 | -2 152 248 -764 2719 -15630 88.6 1943 1943 | 473401 0
brd 1575 1 | 19 -14 110 -2507 -75 -17590 91.2 2232 2232 | 473023 0
brd 1575 2 | -63 -115 55 1690 2890 -19230 87.2 2517 2517 | 473983 0
brd 1575 3 | -119 90 205 -1316 1480 -21810 86.0 2829 2829 | 470975 0
brd 1575 4 | -86 -59 183 -131 -2866 -33080 86.3 2833 2833 | 470431 0
brd 1575 5 | 8 -16 286 2621 -1086 -35680 89.0 2270 2270 | 470615 0
brd 1575 6 | 191 -35 249 889 2062 -29290 86.9 2273 2273 | 467236 0
-------------+------------------------------------------------------------+----------------
brd 1575 mean| -7 0 191 68 731 -24615 87.9 2413 2413 | 471380 0
brd 1575 sdev| 101 91 82 1784 2153 7988 1.8 330 330 | 2323 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 2.1575.0 GPS week: 1575 Day: 0 MJD: 55269
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 133| 0 -2 11 63 -46 54 -.22 36 33 | 0 -48 1479 1550
cod 244| -1 0 -1 14 13 18 -.09 11 10 | --- --- --- ---
esx 140| 2 0 -2 -29 -20 -61 .38 27 24 | 134517 2151 4478 8523
iac n/a| 1 0 4 -43 5 3 -.06 23 23 | 474225 -768 4402 8732
mcc n/a| 6 14 84 -103 -190 -408 .05 112 112 | --- --- --- ---
Table 2.1575.1 GPS week: 1575 Day: 1 MJD: 55270
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 133| 0 -1 1 0 25 249 -.12 24 24 | 0 -10 1532 1597
cod 244| -2 -1 -3 20 -25 -28 -.11 14 12 | --- --- --- ---
esx 140| 0 0 3 12 32 -82 .38 24 21 | 131597 -3899 3219 7163
iac n/a| 2 0 1 -50 -7 -73 -.16 23 23 | 474557 -2494 3215 6858
mcc n/a| 0 0 60 44 13 -163 -.16 102 102 | --- --- --- ---
Table 2.1575.2 GPS week: 1575 Day: 2 MJD: 55271
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 133| 3 0 3 -19 76 131 -.03 25 23 | 0 3 1968 2009
cod 244| -2 1 -4 39 10 15 -.15 14 13 | --- --- --- ---
esx 140| -1 0 -3 -16 -81 -49 .38 22 21 | 136379 1330 4387 9035
iac n/a| 3 1 12 -15 3 -114 -.24 26 26 | 474329 154 4395 8977
mcc n/a| -1 -13 42 125 184 -20 -.16 99 99 | --- --- --- ---
Table 2.1575.3 GPS week: 1575 Day: 3 MJD: 55272
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 133| 4 -2 -1 -18 3 8 .08 29 27 | 0 -24 1563 1615
cod 244| -3 0 -7 0 7 13 -.08 17 16 | --- --- --- ---
esx 140| 0 -2 -1 -6 -35 -50 .33 30 27 | 121673 -176 3605 8477
iac n/a| 5 1 11 -12 14 20 -.24 23 23 | 471893 -1682 3613 8214
mcc n/a| 13 -12 34 39 49 153 -.08 109 109 | --- --- --- ---
Table 2.1575.4 GPS week: 1575 Day: 4 MJD: 55273
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 133| 2 0 7 -11 -1 21 -.03 29 28 | 0 52 1245 1300
cod 244| -4 -1 -3 16 14 -12 -.08 12 11 | --- --- --- ---
esx 140| 3 0 0 9 -34 72 .26 23 22 | 143009 -223 3203 8871
iac n/a| 1 0 5 -32 7 -77 -.20 26 26 | 470432 -1392 3196 9962
mcc n/a| 4 -5 83 -241 106 -817 -.33 87 87 | --- --- --- ---
Table 2.1575.5 GPS week: 1575 Day: 5 MJD: 55274
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 133| 0 0 7 40 41 -205 .08 25 26 | 0 70 1489 1561
cod 244| -1 0 -6 -3 -5 106 -.10 14 14 | --- --- --- ---
esx 140| 0 0 1 -43 -52 -15 .35 29 28 | 133808 -3191 3198 7582
iac n/a| 1 0 3 14 10 -10 -.13 21 21 | 471999 -1551 3212 7548
mcc n/a| 0 0 64 -166 34 -300 -.26 97 97 | --- --- --- ---
Table 2.1575.6 GPS week: 1575 Day: 6 MJD: 55275
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 133| 5 -1 0 62 41 -130 -.04 24 23 | 0 -3 1438 1518
cod 244| -4 2 -4 -10 -45 88 -.13 14 14 | --- --- --- ---
esx 140| 0 -1 -1 -49 26 -86 .47 25 24 | 139176 -1969 3641 6833
iac n/a| 4 0 9 6 0 0 -.18 24 24 | 466877 382 3631 6442
mcc n/a| -5 1 53 -124 -42 56 -.67 102 102 | --- --- --- ---
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 3.1575.0 GPS week: 1575 Day: 0 MJD: 55269
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2707 36 9 20 24 --- 11 | 38 62 63 60 --- 57
R02 | 1333 42 6 36 18 --- 13 | 29 52 71 38 --- 46
R03 | 1450 26 11 12 22 --- 9 | 31 45 40 34 --- 36
R04 | 2254 31 15 28 14 --- 12 | 32 49 38 35 --- 38
R05 | 1073 24 7 28 18 --- 10 | 36 42 52 38 --- 40
R07 | 842 34 10 21 14 --- 10 | 27 50 46 53 --- 44
R08 | 2356 30 9 11 16 78 9 | 35 39 43 52 39 39
R10 | 1689 34 12 41 23 --- 15 | 50 30 48 45 --- 34
R11 | 1527 35 13 32 19 98 13 | 51 47 55 48 74 46
R13 | 871 38 11 18 24 --- 12 | 42 37 44 27 --- 34
XR14 | 2259 51 19 --- 49 --- 25 | 31 29 --- 56 --- 31
R15 | 1278 23 7 26 24 149 10 | 28 21 24 17 52 20
R17 | 1769 58 14 18 28 --- 16 | 65 60 68 80 --- 62
R18 | 3522 39 7 14 20 --- 10 | 47 31 34 42 --- 34
R19 | 1584 23 10 15 18 --- 9 | 37 31 40 47 --- 34
R20 | 1371 27 12 29 21 --- 12 | 21 20 39 28 --- 21
R21 | 2053 37 7 16 25 --- 11 | 22 21 30 32 --- 21
R23 | 2957 50 14 52 43 --- 21 | 78 70 87 89 --- 76
------+------------------------------------+--------------------------------
RMS | 1943 36 11 27 23 112 |T 38 40 48 45 55 39
WRMS | 1943 33 10 24 23 112 |NE 38 40 48 45 55 39
MEDI | 1584 34 10 21 21 98 |MD 35 39 44 42 52 36
Table 3.1575.1 GPS week: 1575 Day: 1 MJD: 55270
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2185 24 13 22 27 --- 12 | 28 36 31 48 --- 33
R02 | 2057 18 14 19 20 --- 10 | 35 36 35 43 --- 34
R03 | 1477 20 15 32 32 --- 14 | 19 34 57 35 --- 31
R04 | 1813 15 9 13 13 --- 7 | 41 44 41 38 --- 39
R05 | 2485 22 14 34 19 --- 13 | 36 31 46 36 --- 29
R07 | 1959 29 15 23 13 --- 11 | 23 49 48 45 --- 40
R08 | 776 24 10 18 22 81 10 | 30 32 37 45 31 33
R10 | 992 21 15 13 16 --- 9 | 31 25 28 31 --- 23
R11 | 1995 31 15 26 25 98 13 | 43 35 52 39 28 37
R13 | 1906 27 14 26 23 --- 12 | 31 33 41 28 --- 28
R14 | 1139 27 18 25 36 --- 15 | 24 31 29 61 --- 36
R15 | 1611 20 9 24 18 121 10 | 14 25 28 20 58 22
R17 | 3182 21 15 36 23 --- 14 | 55 63 76 69 --- 63
R18 | 5309 27 13 21 23 --- 12 | 45 41 46 42 --- 40
R19 | 1429 26 9 18 24 --- 11 | 39 37 49 40 --- 38
R20 | 1451 14 12 17 17 --- 8 | 27 25 27 32 --- 24
R21 | 1877 22 12 21 20 --- 10 | 11 25 31 27 --- 20
R23 | 2468 31 20 24 25 --- 14 | 62 60 64 57 --- 56
------+------------------------------------+--------------------------------
RMS | 2232 24 14 24 23 102 |T 33 36 42 40 39 34
WRMS | 2232 24 12 21 23 102 |NE 33 36 42 40 39 34
MEDI | 1877 22 14 22 22 98 |MD 31 34 41 39 31 33
Table 3.1575.2 GPS week: 1575 Day: 2 MJD: 55271
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2230 16 8 16 20 --- 8 | 33 42 50 36 --- 39
R02 | 2620 31 20 17 24 --- 13 | 29 33 33 35 --- 28
R03 | 1940 20 20 32 34 --- 15 | 36 46 53 34 --- 39
R04 | 1504 22 13 28 18 --- 11 | 24 45 60 35 --- 40
R05 | 3533 21 8 13 21 --- 9 | 25 37 43 45 --- 35
R07 | 3564 16 11 31 23 --- 11 | 47 44 29 48 --- 39
R08 | 1371 22 11 18 34 75 12 | 25 31 54 57 38 38
R10 | 1960 13 13 15 41 --- 12 | 40 32 42 57 --- 36
R11 | 1326 25 9 13 19 121 9 | 44 35 43 43 31 38
R13 | 2326 18 14 30 25 --- 12 | 28 37 47 32 --- 31
R14 | 932 21 8 25 31 --- 12 | 22 22 34 48 --- 20
R15 | 1182 23 14 21 23 96 11 | 22 39 32 21 38 30
R17 | 3737 36 17 17 14 --- 12 | 71 57 58 72 --- 61
R18 | 4072 18 17 16 22 --- 10 | 47 54 49 52 --- 47
R19 | 1617 27 10 20 22 --- 11 | 27 34 47 42 --- 34
R20 | 3077 32 9 24 20 --- 12 | 41 41 39 26 --- 35
R21 | 1575 19 9 19 23 --- 10 | 21 29 25 26 --- 21
R23 | 3274 43 22 25 36 --- 17 | 59 68 83 84 --- 69
------+------------------------------------+--------------------------------
RMS | 2517 25 14 22 26 99 |T 35 40 45 44 35 37
WRMS | 2517 23 13 21 26 99 |NE 35 40 45 44 35 37
MEDI | 1960 21 11 19 23 96 |MD 29 37 43 42 38 36
Table 3.1575.3 GPS week: 1575 Day: 3 MJD: 55272
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 926 23 8 27 12 --- 10 | 37 48 66 42 --- 45
R02 | 4151 9 18 29 21 --- 11 | 30 45 46 40 --- 35
R03 | 2076 32 18 44 12 --- 15 | 34 54 80 52 --- 52
R04 | 2692 36 10 27 21 --- 13 | 38 61 76 60 --- 57
R05 | 1953 29 13 40 23 --- 15 | 50 48 81 65 --- 56
R07 | 3978 20 19 35 24 --- 14 | 41 47 36 36 --- 34
R08 | 2926 21 13 16 30 89 12 | 40 50 51 63 60 50
R10 | 1441 33 20 11 23 --- 13 | 28 40 34 30 --- 28
R11 | 1470 22 21 40 15 142 14 | 44 48 38 40 36 39
R13 | 1790 17 16 33 11 --- 11 | 36 35 58 43 --- 38
R14 | 1998 43 24 55 29 --- 21 | 31 35 48 37 --- 27
R15 | 3037 26 16 22 32 89 14 | 17 35 29 17 89 25
R17 | 3585 40 18 23 25 --- 15 | 81 84 96 102 --- 89
R18 | 3253 20 10 24 19 --- 10 | 37 31 50 48 --- 39
R19 | 1368 27 13 16 16 --- 10 | 46 53 48 50 --- 48
R20 | 3995 16 14 17 21 --- 10 | 34 28 42 26 --- 26
R21 | 1335 28 16 20 19 --- 12 | 15 38 28 49 --- 31
R23 | 4743 43 24 15 34 --- 17 | 44 53 48 71 --- 53
------+------------------------------------+--------------------------------
RMS | 2829 29 17 30 23 109 |T 37 46 53 48 61 42
WRMS | 2829 27 16 27 23 109 |NE 37 46 53 48 61 42
MEDI | 2076 26 16 24 21 89 |MD 37 47 48 43 60 39
Table 3.1575.4 GPS week: 1575 Day: 4 MJD: 55273
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1151 21 8 16 18 --- 8 | 36 45 56 52 --- 46
R02 | 2956 21 8 16 19 --- 8 | 21 36 43 28 --- 31
R03 | 1946 26 13 31 29 --- 13 | 37 54 66 34 --- 47
R04 | 2359 33 17 36 26 --- 15 | 32 49 66 65 --- 49
R05 | 1347 35 12 32 25 --- 14 | 31 53 69 64 --- 53
R07 | 3934 28 11 18 19 --- 10 | 25 46 42 46 --- 40
R08 | 3086 23 10 21 19 80 9 | 33 39 46 42 43 37
R10 | 2073 28 9 17 19 --- 9 | 38 28 29 25 --- 26
R11 | 1319 33 10 26 22 94 12 | 51 54 61 56 52 54
R13 | 2633 28 11 19 26 --- 11 | 38 39 42 46 --- 37
R14 | 1854 36 8 23 40 --- 14 | 32 27 53 33 --- 27
XR15 |12445 105 35 --- 41 353 40 | 29 81 --- 26 47 62
R17 | 2155 38 11 23 28 --- 13 | 63 52 68 68 --- 58
R18 | 2446 21 10 22 28 --- 11 | 47 47 48 38 --- 42
R19 | 1989 20 13 19 16 --- 9 | 29 34 33 32 --- 29
R20 | 4672 30 12 10 26 --- 11 | 36 40 41 36 --- 37
R21 | 1493 30 11 21 32 --- 12 | 43 31 56 50 --- 38
R23 | 5929 29 17 24 30 --- 13 | 62 72 86 95 --- 77
------+------------------------------------+--------------------------------
RMS | 2833 29 12 23 25 87 |T 37 45 53 46 47 43
WRMS | 2833 28 11 22 25 87 |NE 37 45 53 46 47 43
MEDI | 2155 28 11 21 26 94 |MD 36 45 53 42 47 40
Table 3.1575.5 GPS week: 1575 Day: 5 MJD: 55274
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1998 13 13 20 12 --- 8 | 39 41 34 38 --- 36
R02 | 1718 23 15 26 12 --- 10 | 31 43 50 39 --- 38
R03 | 1623 15 13 26 17 --- 10 | 35 42 48 30 --- 36
R04 | 1618 26 15 23 20 --- 12 | 18 42 41 21 --- 29
R05 | 1078 24 12 34 17 --- 12 | 34 45 54 53 --- 43
R07 | 2745 23 11 25 18 --- 10 | 30 44 60 36 --- 40
R08 | 2159 19 7 27 19 88 10 | 20 30 30 32 29 25
R10 | 2857 31 14 21 28 --- 13 | 25 24 31 27 --- 20
R11 | 1340 30 16 34 22 106 14 | 43 50 52 43 23 45
R13 | 1391 24 13 20 17 --- 10 | 25 34 41 26 --- 28
R14 | 1807 38 19 49 24 --- 18 | 28 37 53 38 --- 34
R17 | 1394 26 14 27 22 --- 12 | 69 63 80 70 --- 68
R18 | 1506 34 13 36 26 --- 15 | 34 32 46 23 --- 24
R19 | 2637 13 13 21 18 --- 9 | 48 52 34 37 --- 40
R20 | 4922 27 11 37 19 --- 13 | 18 30 58 28 --- 26
R21 | 2513 28 13 19 30 --- 13 | 34 25 35 44 --- 30
XR22 | ---- --- 7 --- --- --- 0 | --- 43 --- --- --- 43
XR23 | ---- --- --- --- --- --- 0 | 220 379 --- 3 --- 0
------+------------------------------------+--------------------------------
RMS | 2270 25 14 29 21 97 |T 44 58 46 34 31 35
WRMS | 2270 26 14 28 21 97 |NE 44 58 46 34 31 35
MEDI | 1718 24 13 26 19 88 |MD 34 42 46 36 29 36
Table 3.1575.6 GPS week: 1575 Day: 6 MJD: 55275
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1845 23 15 32 34 --- 14 | 33 64 59 69 --- 55
R02 | 2472 15 12 34 22 --- 12 | 42 50 41 53 --- 42
R03 | 2763 23 16 29 13 --- 11 | 40 56 61 40 --- 48
R04 | 2435 22 11 16 15 --- 9 | 21 48 50 37 --- 39
R05 | 1133 18 19 24 25 --- 12 | 28 47 42 44 --- 38
R07 | 2511 27 12 27 20 --- 12 | 30 52 58 43 --- 44
R08 | 1280 19 14 18 25 114 10 | 23 44 46 58 19 42
R10 | 3440 28 10 18 24 --- 11 | 22 32 35 37 --- 27
R11 | 1154 33 14 21 35 89 14 | 59 54 65 43 33 51
R13 | 1147 25 13 16 12 --- 9 | 39 37 43 39 --- 37
R14 | 1806 23 14 30 23 --- 12 | 26 30 26 33 --- 27
R17 | 1179 27 11 27 26 --- 12 | 59 60 75 78 --- 65
R18 | 1922 20 8 14 28 --- 10 | 31 28 29 26 --- 26
R19 | 1711 22 17 29 25 --- 13 | 40 36 43 30 --- 34
R20 | 4162 25 9 25 19 --- 11 | 33 35 44 27 --- 31
R21 | 2691 20 16 23 28 --- 12 | 30 38 40 31 --- 29
XR22 | ---- --- 6 --- --- --- 0 | --- 53 --- --- --- 52
XR23 | ---- --- --- --- --- --- 0 | 399 391 --- --- --- 0
XR24 | ---- --- 6 --- --- --- 0 | --- 7 --- --- --- 7
------+------------------------------------+--------------------------------
RMS | 2272 24 14 25 24 102 |T 56 61 47 43 28 38
WRMS | 2272 23 14 24 24 102 |NE 56 61 47 43 28 38
MEDI | 1845 23 12 24 24 89 |MD 33 47 43 39 32 38
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