[IGSREPORT-18815] Wk 1592 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jul 29 05:31:01 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1592 (Jul 11, 2010 - Jul 17, 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 2.1592.
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:
igl1592[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1592 in the SP3 format.
igl15927.sum Combination Report for GPS Week 1592.
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 | 475.4 ns
1 | 392.2 ns
2 | 425.4 ns
3 | 421.2 ns
4 | 385.3 ns
5 | 413.6 ns
6 | 473.2 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 1.1592, 1a.1592).
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 2.1592.0-6)
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 3.1592.0-6).
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 1592 summary. (Jul 11, 2010 - Jul 17, 2010)
Table 1.1592.a GPS week : 1592 MJD: 55388.0-55394.0
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 118| 2 0 -8 -6 11 20 -.10 19 19 | 0 53 1776 1848
| 0 1 1 28 37 74 .05 | 0 199
cod 238| -3 0 -4 42 -2 -7 -.10 13 12 | --- --- --- ---
| 0 1 2 26 32 34 .04 | --- ---
esx 135| 0 0 -1 -31 2 50 .43 24 22 | 85743 -2068 3891 7902
| 0 1 1 32 34 34 .03 | 37819 4034
gfz 194| -2 -1 -3 -84 -12 77 -.14 26 25 | 263306 -2373 3851 7926
| 1 2 2 48 92 20 .06 | 35836 3383
iac n/a| 2 0 20 -44 13 -49 -.12 24 24 | 427009 -965 3886 8475
| 1 1 4 20 28 46 .06 | 35705 1783
mcc n/a| 1 4 73 -57 -43 -32 -.10 154 154 | --- --- --- ---
| 9 9 9 100 65 877 .24 | --- ---
Table 1.1592.b GPS week : 1592 MJD: 55388.0-55394.0
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 | 11 13 9 8 8 10 10 |
R02 | 12 10 10 8 9 12 11 |
R03 | 11 14 8 9 8 9 10 |
R04 | 10 11 8 13 8 8 10 |
R05 | 7 10 9 10 11 8 10 |
R07 | 10 10 10 9 12 10 13 |
R08 | 9 10 10 8 11 10 10 |
R10 | 12 10 10 15 8 8 8 |
R11 | 14 14 13 11 11 10 11 |
R13 | 9 12 9 12 9 10 12 |
R14 | 18 13 15 11 12 14 10 |
R15 | 14 12 12 14 17 20 16 |
R17 | 16 15 15 16 9 13 15 |
R18 | 11 21 9 11 12 10 7 |
R19 | 10 10 12 8 7 6 8 |
R20 | 13 12 12 21 10 14 14 |
R21 | 11 10 10 13 12 12 11 |
R22 | 12 11 10 10 11 15 12 |
R23 | 13 10 9 8 9 11 19 |
R24 | 12 10 8 8 9 11 11 |
Table 1.1592.c GPS week : 1592 MJD: 55388.0-55394.0
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 1592 0 | 42 -35 413 1507 1010 -20810 84.8 1787 1787 | 475355 0
brd 1592 1 | 31 27 541 35 1120 -23100 83.0 1829 1829 | 392240 0
brd 1592 2 | 70 77 455 1514 -266 -23000 85.4 2219 2219 | 425386 0
brd 1592 3 | -10 -20 350 -624 1351 -12480 85.6 2509 2509 | 421222 0
brd 1592 4 | -47 -98 678 -3260 1858 -33990 84.4 2590 2590 | 385270 0
brd 1592 5 | -22 -157 518 -16 -328 -28600 83.4 2378 2378 | 413648 0
brd 1592 6 | -23 -14 573 806 873 -31330 85.2 2260 2260 | 473229 0
-------------+------------------------------------------------------------+----------------
brd 1592 mean| 5 -31 504 -5 802 -24758 84.6 2224 2224 | 426621 0
brd 1592 sdev| 42 77 108 1644 815 7249 1.0 312 312 | 35679 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 2.1592.0 GPS week: 1592 Day: 0 MJD: 55388
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 118| 3 1 -7 1 8 127 -.03 21 21 | 0 -220 2014 2083
cod 238| -3 0 -1 32 6 -19 -.10 14 13 | --- --- --- ---
esx 135| 0 -2 0 -74 -2 26 .45 26 25 | 145073 -7067 4500 7257
gfz 194| 0 -1 -3 -16 -45 36 -.19 27 25 | 312120 -6025 4223 7366
iac n/a| 3 1 12 -34 7 -112 -.02 23 23 | 476252 -2477 4480 7968
mcc n/a| -10 12 59 145 -179 -533 -.48 167 167 | --- --- --- ---
Table 2.1592.1 GPS week: 1592 Day: 1 MJD: 55389
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 118| 2 -1 -7 -17 6 -7 -.07 19 19 | 0 -38 1853 1951
cod 238| -4 0 -4 13 22 -10 -.05 12 12 | --- --- --- ---
esx 135| 0 -1 -3 20 -45 45 .46 30 27 | 52131 -2252 3579 8324
gfz 194| -4 -3 -2 -57 -3 82 -.09 28 28 | 228256 -1754 3581 7970
iac n/a| 1 0 24 -59 0 17 -.13 26 26 | 392239 -947 3591 8481
mcc n/a| -9 4 75 -96 31 523 -.22 78 78 | --- --- --- ---
Table 2.1592.2 GPS week: 1592 Day: 2 MJD: 55390
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 118| 3 1 -6 44 8 -38 -.18 19 19 | 0 110 1747 1802
cod 238| -4 -2 -2 13 -8 -50 -.16 13 12 | --- --- --- ---
esx 135| 0 0 -3 -30 0 95 .45 17 15 | 86243 -4237 4063 6953
gfz 194| -1 -3 0 -37 -47 69 -.11 26 27 | 261660 -3653 4053 7138
iac n/a| 2 4 21 -11 28 -33 -.21 28 28 | 425790 -1040 4052 7745
mcc n/a| 7 -8 81 -57 -46 807 .17 107 107 | --- --- --- ---
Table 2.1592.3 GPS week: 1592 Day: 3 MJD: 55391
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 118| 2 -1 -9 5 -41 107 -.09 17 17 | 0 -119 1593 1653
cod 238| -3 0 -5 59 36 -29 -.08 14 14 | --- --- --- ---
esx 135| 0 0 -2 -57 31 19 .42 28 23 | 78037 -679 3794 7154
gfz 194| -1 2 -6 -101 -110 85 -.08 27 26 | 259099 -2834 3785 7162
iac n/a| 4 0 22 -29 -25 -85 -.11 23 23 | 421908 -1603 3794 7819
mcc n/a| 13 1 69 -182 -34 762 -.02 172 172 | --- --- --- ---
Table 2.1592.4 GPS week: 1592 Day: 4 MJD: 55392
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 118| 3 0 -6 -22 -18 47 -.09 19 19 | 0 318 1753 1830
cod 238| -1 0 -8 33 8 -18 -.07 11 11 | --- --- --- ---
esx 135| 0 1 -1 -1 55 79 .45 24 23 | 42716 4811 4143 7891
gfz 194| -3 1 -4 -111 -97 78 -.21 24 22 | 219727 3178 4170 8391
iac n/a| 1 -2 25 -45 -8 -28 -.10 20 20 | 384625 1672 4132 8879
mcc n/a| 1 -3 87 -36 -11 455 .04 260 260 | --- --- --- ---
Table 2.1592.5 GPS week: 1592 Day: 5 MJD: 55393
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 118| 3 -2 -11 -44 49 -31 -.09 21 21 | 0 283 1968 2039
cod 238| -2 0 -3 76 -22 21 -.12 13 12 | --- --- --- ---
esx 135| -1 2 1 -29 -33 7 .37 21 19 | 68672 -5549 4251 10036
gfz 194| -2 0 -3 -138 71 89 -.18 23 25 | 253408 -6077 4231 9994
iac n/a| 2 0 20 -70 39 -16 -.16 26 26 | 415789 -3341 4242 10448
mcc n/a| 1 9 76 -79 -14 -893 .13 137 137 | --- --- --- ---
Table 2.1592.6 GPS week: 1592 Day: 6 MJD: 55394
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 118| 2 0 -9 -14 66 -63 -.12 21 21 | 0 40 1504 1583
cod 238| -3 0 -5 71 -63 52 -.11 13 13 | --- --- --- ---
esx 135| -1 -1 -2 -44 12 80 .42 23 21 | 127335 497 2912 7700
gfz 194| -1 -1 -6 -131 145 101 -.10 26 25 | 308876 554 2919 7465
iac n/a| 3 0 15 -61 55 -90 -.08 24 24 | 472461 979 2915 7990
mcc n/a| 8 16 67 -94 -47 -1351 -.31 156 156 | --- --- --- ---
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 3.1592.0 GPS week: 1592 Day: 0 MJD: 55388
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1258 20 10 18 20 27 --- 10 | 19 19 30 22 27 --- 18
R02 | 2890 13 21 23 30 24 --- 12 | 16 21 32 34 25 --- 20
R03 | 884 23 14 20 22 23 --- 11 | 23 26 38 26 29 --- 24
R04 | 1425 20 9 20 22 21 --- 9 | 28 32 32 31 27 --- 27
R05 | 3096 14 8 13 32 15 --- 7 | 24 24 30 32 28 --- 23
R07 | 1984 15 10 16 17 27 --- 10 | 22 22 29 27 34 --- 22
R08 | 935 13 11 16 18 22 205 9 | 26 28 27 36 31 65 24
R10 | 1869 15 13 33 38 19 --- 11 | 30 35 48 35 39 --- 32
R11 | 1336 20 24 25 18 28 --- 14 | 13 27 29 21 10 --- 15
R13 | 1901 15 8 20 21 17 --- 8 | 17 15 26 23 23 --- 14
R14 | 1333 35 13 50 39 22 --- 17 | 19 19 43 26 20 --- 18
R15 | 2014 24 12 22 30 38 88 14 | 17 23 26 36 21 39 17
R17 | 1057 35 10 31 33 34 --- 15 | 34 38 38 40 37 --- 34
R18 | 964 23 11 25 31 18 --- 11 | 26 37 35 41 37 --- 30
R19 | 1617 21 8 14 31 22 --- 9 | 29 26 40 43 37 --- 29
R20 | 1344 22 16 37 26 15 --- 13 | 24 28 29 23 20 --- 22
R21 | 1655 19 11 30 17 16 --- 10 | 22 35 48 36 30 --- 31
R22 | 1879 19 18 26 31 22 --- 12 | 33 45 54 41 45 --- 41
R23 | 2895 24 17 33 19 20 183 13 | 21 25 23 21 27 144 16
R24 | 912 21 16 24 21 21 --- 11 | 48 55 43 40 45 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 1786 21 14 26 27 23 167 |T 24 29 35 31 29 82 25
WRMS | 1786 21 13 25 25 23 167 |NE 24 29 35 31 29 82 25
MEDI | 1425 20 11 23 22 22 183 |MD 23 26 32 32 28 65 23
Table 3.1592.1 GPS week: 1592 Day: 1 MJD: 55389
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1287 21 13 30 28 28 --- 12 | 22 29 41 40 32 --- 26
R02 | 2049 12 13 16 26 31 --- 10 | 21 21 31 39 18 --- 19
R03 | 1337 26 17 22 31 30 --- 13 | 16 34 39 34 30 --- 26
R04 | 1514 18 12 23 19 28 --- 11 | 25 32 36 33 36 --- 28
R05 | 3067 19 10 20 17 23 --- 10 | 29 30 28 27 22 --- 23
R07 | 1376 19 9 24 16 15 --- 9 | 38 25 40 34 27 --- 28
R08 | 1712 15 13 15 45 24 93 9 | 20 30 36 49 31 101 25
R10 | 2177 19 10 16 18 24 --- 9 | 25 36 40 42 44 --- 33
R11 | 2446 17 15 38 29 27 --- 13 | 19 23 36 23 15 --- 14
R13 | 1246 16 11 39 34 20 --- 12 | 20 26 48 45 21 --- 23
R14 | 2113 22 10 17 23 39 --- 12 | 13 25 30 32 21 --- 16
R15 | 1425 21 12 26 26 30 60 12 | 19 28 28 37 26 48 20
R17 | 2470 23 19 22 42 43 --- 15 | 28 41 44 43 33 --- 34
R18 | 1257 27 12 73 38 30 --- 21 | 22 26 71 51 35 --- 27
R19 | 2100 11 9 30 18 17 --- 9 | 21 23 35 31 36 --- 20
R20 | 1846 22 11 28 18 22 --- 11 | 16 29 33 23 23 --- 21
R21 | 1770 14 12 26 18 22 --- 10 | 34 36 49 32 32 --- 34
R22 | 1096 15 16 29 34 17 --- 11 | 48 34 52 54 46 --- 39
R23 | 1397 10 11 31 25 17 76 10 | 20 18 33 31 19 67 16
R24 | 1464 18 9 22 32 25 --- 10 | 39 50 39 39 37 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1828 19 12 30 28 26 78 |T 24 29 39 36 29 72 25
WRMS | 1828 19 12 27 28 26 78 |NE 24 29 39 36 29 72 25
MEDI | 1514 18 12 24 26 24 76 |MD 21 29 36 34 30 67 25
Table 3.1592.2 GPS week: 1592 Day: 2 MJD: 55390
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2352 12 9 10 13 28 --- 8 | 81 83 85 91 82 --- 83
R02 | 2123 13 13 18 21 26 --- 10 | 23 26 32 40 21 --- 22
R03 | 1594 12 9 7 30 26 --- 7 | 20 27 25 34 24 --- 23
R04 | 1049 11 14 13 19 15 --- 7 | 23 28 24 34 26 --- 23
R05 | 3440 15 13 18 18 17 --- 9 | 27 23 38 30 24 --- 25
R07 | 1029 17 12 20 23 21 --- 10 | 23 32 43 44 32 --- 28
R08 | 2905 16 13 16 22 26 68 9 | 29 40 32 33 28 56 30
R10 | 3115 13 13 19 31 24 --- 10 | 24 35 34 37 28 --- 27
R11 | 807 26 16 23 36 19 --- 12 | 15 32 43 45 26 --- 28
R13 | 1635 11 11 16 22 27 --- 9 | 17 21 28 31 35 --- 18
R14 | 3610 27 14 11 26 53 --- 15 | 23 22 26 32 25 --- 15
R15 | 1996 25 10 22 23 31 63 12 | 14 27 26 23 32 30 20
R17 | 2410 25 13 20 29 47 --- 14 | 29 34 42 57 34 --- 29
R18 | 1232 19 13 9 22 19 --- 8 | 33 37 51 43 27 --- 34
R19 | 1710 25 10 24 25 25 --- 12 | 23 25 49 45 33 --- 29
R20 | 3189 17 11 19 34 41 --- 12 | 40 30 38 24 25 --- 29
R21 | 2533 21 16 12 34 15 --- 9 | 15 22 23 39 18 --- 14
R22 | 1165 20 11 18 20 18 --- 9 | 27 27 43 38 37 --- 29
R23 | 1507 20 12 16 24 14 160 9 | 17 27 35 40 22 77 22
R24 | 1712 16 11 12 32 19 --- 8 | 23 28 28 38 28 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2219 19 13 17 26 28 106 |T 26 31 37 39 30 54 27
WRMS | 2219 19 12 15 27 28 106 |NE 26 31 37 39 30 54 27
MEDI | 1712 17 12 16 23 24 68 |MD 23 27 34 38 27 56 25
Table 3.1592.3 GPS week: 1592 Day: 3 MJD: 55391
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2078 14 6 10 31 20 --- 7 | 151 145 139 134 134 --- 143
R02 | 1858 11 10 16 16 18 --- 8 | 22 20 35 24 24 --- 21
R03 | 1848 10 11 18 21 21 --- 8 | 18 28 35 22 30 --- 24
R04 | 905 20 15 33 24 21 --- 12 | 17 28 54 39 29 --- 26
R05 | 3680 11 17 22 30 21 --- 10 | 40 39 35 46 25 --- 32
R07 | 1567 12 8 23 21 20 --- 9 | 35 34 45 37 43 --- 36
R08 | 2962 15 11 17 21 13 61 8 | 22 31 36 44 32 46 27
R10 | 2800 24 17 41 40 22 --- 15 | 31 39 56 55 45 --- 35
R11 | 2140 8 16 27 23 20 --- 10 | 19 22 31 24 19 --- 14
R13 | 2815 22 16 27 17 15 --- 11 | 47 57 56 56 47 --- 49
R14 | 4918 16 12 19 23 29 --- 11 | 18 24 31 26 21 --- 18
R15 | 1895 26 14 25 24 30 64 13 | 22 26 32 29 17 24 17
R17 | 2288 22 20 34 35 34 --- 15 | 31 42 55 50 49 --- 41
R18 | 1421 18 14 18 38 24 --- 10 | 21 35 34 42 35 --- 27
R19 | 1643 13 9 19 27 18 --- 8 | 30 36 39 50 35 --- 33
R20 | 3298 24 15 65 28 39 --- 21 | 24 18 70 30 26 --- 18
R21 | 2594 19 19 30 31 19 --- 12 | 28 41 47 36 29 --- 30
R22 | 828 16 16 16 24 20 --- 10 | 29 42 44 48 49 --- 38
R23 | 1340 9 14 21 15 12 285 8 | 33 26 35 32 36 123 28
R24 | 3305 13 13 16 35 14 --- 8 | 28 29 28 37 28 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2509 17 14 27 27 23 172 |T 33 38 46 43 37 64 34
WRMS | 2509 17 14 23 26 23 172 |NE 33 38 46 43 37 64 34
MEDI | 2078 15 14 21 24 20 64 |MD 28 31 36 37 30 46 27
Table 3.1592.4 GPS week: 1592 Day: 4 MJD: 55392
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1122 13 10 21 22 13 --- 8 | 178 174 182 167 172 --- 175
R02 | 2859 14 13 16 21 20 --- 9 | 21 19 33 30 31 --- 21
R03 | 1195 9 9 16 21 18 --- 7 | 16 19 32 24 20 --- 17
R04 | 806 12 8 17 27 17 --- 7 | 17 22 29 28 18 --- 18
R05 | 2684 26 11 15 16 23 --- 11 | 26 27 35 36 21 --- 23
R07 | 2017 16 12 30 35 25 --- 11 | 24 22 33 33 22 --- 18
R08 | 3296 21 10 31 17 16 60 11 | 31 27 31 30 25 84 24
R10 | 1883 13 9 22 29 14 --- 8 | 15 23 26 26 18 --- 17
R11 | 3414 14 12 28 22 25 --- 11 | 21 22 48 40 36 --- 25
R13 | 3833 12 10 28 17 14 --- 9 | 62 57 66 67 75 --- 61
R14 | 5023 18 11 35 18 22 --- 12 | 24 19 50 35 26 --- 22
R15 | 2797 41 18 28 19 34 66 17 | 17 34 26 17 28 35 21
R17 | 1173 15 9 19 28 20 --- 8 | 38 41 40 39 32 --- 37
R18 | 2488 19 9 27 25 28 --- 11 | 32 28 30 29 42 --- 30
R19 | 1553 11 8 14 19 14 --- 6 | 24 26 37 29 24 --- 26
R20 | 3528 16 14 16 36 19 --- 9 | 38 17 38 38 24 --- 23
R21 | 2377 23 9 31 32 21 --- 11 | 20 24 46 39 42 --- 28
R22 | 1552 22 13 24 26 17 --- 10 | 43 47 58 58 45 --- 45
R23 | 1245 16 9 18 20 22 441 9 | 22 20 24 24 26 232 17
R24 | 2337 16 13 19 19 11 --- 8 | 25 35 34 25 24 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 2589 19 11 24 24 20 260 |T 34 35 44 40 37 117 33
WRMS | 2589 19 11 23 22 20 260 |NE 34 35 44 40 37 117 33
MEDI | 2337 16 10 21 21 19 66 |MD 24 24 34 30 26 84 23
Table 3.1592.5 GPS week: 1592 Day: 5 MJD: 55393
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1526 17 14 20 26 21 --- 10 | 217 220 218 231 227 --- 220
R02 | 3304 11 15 20 20 39 --- 12 | 19 24 34 32 26 --- 20
R03 | 1064 10 10 22 18 23 --- 9 | 19 20 28 31 21 --- 17
R04 | 1378 12 10 13 11 18 --- 7 | 15 21 24 16 21 --- 15
R05 | 2889 11 11 15 16 17 --- 7 | 24 35 33 32 28 --- 28
R07 | 1951 16 10 25 30 12 --- 9 | 26 27 33 30 31 --- 23
R08 | 3016 17 17 19 28 14 143 10 | 28 38 33 41 38 43 31
R10 | 2521 14 8 17 17 16 --- 7 | 25 30 29 26 30 --- 26
R11 | 1351 18 17 16 25 15 --- 9 | 19 22 21 27 25 --- 17
R13 | 4013 20 8 24 25 21 --- 10 | 35 32 51 37 28 --- 34
R14 | 3755 36 11 16 23 28 --- 13 | 26 24 27 13 14 --- 19
R15 | 2047 37 19 34 34 50 73 19 | 15 21 28 39 34 31 12
R17 | 1547 22 9 19 19 37 --- 12 | 25 36 39 31 37 --- 30
R18 | 1883 13 11 16 21 29 --- 9 | 21 26 35 28 39 --- 25
R19 | 1274 7 7 9 22 19 --- 6 | 33 28 36 47 42 --- 31
R20 | 3415 31 12 21 23 34 --- 14 | 30 21 33 31 25 --- 17
R21 | 2323 22 16 24 28 23 --- 12 | 25 22 44 38 33 --- 24
R22 | 1751 29 12 38 18 17 --- 14 | 27 28 55 27 37 --- 31
R23 | 1179 18 12 16 18 32 175 11 | 36 30 38 35 42 301 31
R24 | 1965 19 14 19 26 24 --- 10 | 31 40 46 36 42 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 2377 21 13 21 23 26 137 |T 34 37 44 41 41 125 34
WRMS | 2377 21 12 19 25 26 137 |NE 34 37 44 41 41 125 34
MEDI | 1951 17 11 19 22 21 143 |MD 25 27 33 31 31 43 25
Table 3.1592.6 GPS week: 1592 Day: 6 MJD: 55394
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2681 21 15 15 11 16 --- 10 | 294 293 297 292 287 --- 293
R02 | 3865 17 12 19 31 29 --- 11 | 28 25 31 27 34 --- 25
R03 | 953 18 11 18 17 24 --- 10 | 23 23 27 27 22 --- 19
R04 | 2151 24 8 12 23 21 --- 9 | 18 20 25 29 32 --- 19
R05 | 1896 15 13 23 20 18 --- 10 | 22 25 36 32 30 --- 24
R07 | 1690 17 12 30 42 28 --- 12 | 23 31 47 49 27 --- 28
R08 | 2335 13 11 13 22 28 239 9 | 32 28 28 37 30 73 26
R10 | 1546 11 13 20 28 11 --- 8 | 24 33 32 35 28 --- 27
R11 | 2323 12 16 29 20 13 --- 10 | 19 20 42 27 23 --- 20
R13 | 2923 17 16 24 11 24 --- 11 | 77 84 89 86 84 --- 81
R14 | 2575 18 10 21 27 20 --- 9 | 21 23 23 26 24 --- 18
R15 | 3796 39 12 20 32 34 77 15 | 26 25 28 30 26 20 18
R17 | 1664 27 14 19 27 43 --- 15 | 41 45 48 47 57 --- 44
R18 | 1544 16 8 14 23 11 --- 7 | 24 34 28 32 36 --- 28
R19 | 1179 11 10 18 27 12 --- 7 | 31 34 42 46 38 --- 33
R20 | 2408 34 9 23 24 25 --- 13 | 28 22 27 24 21 --- 18
R21 | 1836 12 16 27 37 20 --- 11 | 26 31 28 30 39 --- 28
R22 | 1778 22 22 12 30 22 --- 11 | 43 40 37 51 40 --- 36
R23 | 1796 21 14 55 16 29 101 18 | 24 23 49 24 34 158 23
R24 | 1755 22 14 20 27 23 --- 11 | 40 30 41 41 38 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 2260 21 13 23 26 24 156 |T 43 44 50 49 47 83 42
WRMS | 2260 21 13 21 25 24 156 |NE 43 44 50 49 47 83 42
MEDI | 1836 17 12 20 24 22 101 |MD 26 28 32 32 32 73 26
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