[IGSREPORT-18693] Wk 1586 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jun 17 06:59:37 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1586 (May 30, 2010 - Jun 05, 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 2.1586.
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:
igl1586[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1586 in the SP3 format.
igl15867.sum Combination Report for GPS Week 1586.
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 | 363.5 ns
1 | 446.6 ns
2 | 367.7 ns
3 | 451.4 ns
4 | 376.1 ns
5 | 378.4 ns
6 | 393.5 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 1.1586, 1a.1586).
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 2.1586.0-6)
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 3.1586.0-6).
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 1586 summary. (May 30, 2010 - Jun 05, 2010)
Table 1.1586.a GPS week : 1586 MJD: 55346.0-55352.0
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 121| 1 0 -9 -5 9 -6 -.08 28 28 | 0 -39 1756 1827
| 1 1 3 20 30 60 .06 | 0 158
cod 250| -2 -1 0 25 -54 26 -.09 17 15 | --- --- --- ---
| 1 0 3 8 11 17 .03 | --- ---
esx 132| 0 0 1 -8 65 10 .24 23 22 | 74092 698 4058 8123
| 1 1 4 14 37 57 .10 | 39641 1881
gfz 199| 0 -1 2 -75 59 33 -.33 32 32 | 228819 309 4034 8255
| 2 3 3 61 71 64 .16 | 37064 2020
iac n/a| 1 1 9 -52 -12 -40 -.12 31 31 | 396386 567 4057 8638
| 1 1 11 16 18 75 .07 | 37170 1540
mcc n/a| 14 7 8 -126 115 -616 .44 314 314 | --- --- --- ---
| 29 25 42 174 252 642 .70 | --- ---
Table 1.1586.b GPS week : 1586 MJD: 55346.0-55352.0
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 17 16 15 14 13 12 |
R02 | 12 12 17 15 15 15 15 |
R03 | 15 11 14 15 19 15 18 |
R04 | 10 12 14 14 18 15 16 |
R05 | 13 12 18 14 18 23 20 |
R07 | 18 16 16 15 12 18 0 |
R08 | 12 15 19 13 15 14 18 |
R10 | 14 13 16 10 11 14 14 |
R11 | 10 10 13 13 14 13 11 |
R13 | 16 13 11 9 8 12 13 |
R14 | 14 13 12 12 10 12 13 |
R15 | 17 14 15 11 13 12 15 |
R17 | 20 20 16 18 12 17 17 |
R18 | 10 10 13 10 11 15 12 |
R19 | 12 10 8 10 11 12 15 |
R20 | 18 14 19 13 13 15 10 |
R21 | 14 10 14 14 11 11 12 |
R22 | 14 17 11 15 20 10 13 |
R23 | 14 16 11 11 11 11 8 |
R24 | 12 11 16 13 10 10 11 |
Table 1.1586.c GPS week : 1586 MJD: 55346.0-55352.0
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 1586 0 | 83 42 315 191 1884 -19210 88.5 2362 2362 | 363489 0
brd 1586 1 | 49 88 281 199 1647 -6822 87.6 2225 2225 | 446615 0
brd 1586 2 | 37 78 399 -3648 -566 -9026 89.4 1845 1845 | 367704 0
brd 1586 3 | -14 14 387 68 378 -10120 90.1 1915 1915 | 451433 0
brd 1586 4 | -169 142 348 4534 -1173 -4770 91.8 7014 7014 | 376088 0
brd 1586 5 | 243 -15 211 -847 -1894 -3356 87.7 5521 5521 | 378450 0
brd 1586 6 | 74 -1 493 889 4936 -10680 86.2 2280 2280 | 393532 0
-------------+------------------------------------------------------------+----------------
brd 1586 mean| 43 49 348 198 744 -9140 88.8 3308 3308 | 396758 0
brd 1586 sdev| 123 56 90 2421 2315 5206 1.8 2075 2075 | 36965 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 2.1586.0 GPS week: 1586 Day: 0 MJD: 55346
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 121| 0 0 -15 38 -3 79 -.14 30 30 | 0 -17 1581 1648
cod 250| 0 -1 -5 8 -56 23 -.07 15 14 | --- --- --- ---
esx 132| -1 2 -1 6 114 -91 .31 27 25 | 38668 3054 3968 8956
gfz 199| 0 5 0 15 56 31 -.09 32 32 | 194620 2074 3959 8925
iac n/a| -1 0 25 -69 -4 14 -.05 28 28 | 363155 1146 3978 9378
mcc n/a| 16 -6 -3 -6 411 -561 .39 281 281 | --- --- --- ---
Table 2.1586.1 GPS week: 1586 Day: 1 MJD: 55347
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 121| 3 -1 -7 -14 18 -13 -.02 25 25 | 0 -57 1827 1891
cod 250| -1 0 1 31 -48 5 -.11 15 13 | --- --- --- ---
esx 132| -1 0 9 -3 87 -21 .29 26 24 | 129074 -2715 3638 7551
gfz 199| 3 -1 5 -85 44 -46 -.23 37 37 | 278971 -2431 3637 7650
iac n/a| 0 1 -3 -58 -9 53 -.15 30 30 | 446969 -2598 3632 8100
mcc n/a| 62 -8 -25 -289 91 -90 1.90 328 328 | --- --- --- ---
Table 2.1586.2 GPS week: 1586 Day: 2 MJD: 55348
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 121| 3 2 -4 -14 -25 -52 -.10 27 27 | 0 93 1735 1802
cod 250| -2 -2 3 23 -72 27 -.10 20 19 | --- --- --- ---
esx 132| 0 -1 1 2 110 8 .26 24 24 | 49223 525 3442 7144
gfz 199| -1 -2 6 -134 -32 -14 -.31 30 30 | 199810 -1295 3293 6954
iac n/a| 2 2 -4 -35 -7 25 -.15 30 30 | 367533 54 3461 7988
mcc n/a| 20 -5 -51 21 -244 401 -.02 397 397 | --- --- --- ---
Table 2.1586.3 GPS week: 1586 Day: 3 MJD: 55349
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 121| 1 -1 -6 -5 -23 42 -.10 27 26 | 0 61 1259 1327
cod 250| -3 0 0 26 -40 11 -.07 16 15 | --- --- --- ---
esx 132| 3 0 -4 -15 47 -1 .22 20 20 | 132521 2581 3071 7019
gfz 199| 0 -1 -1 -115 -5 -25 -.62 33 33 | 283143 1294 3066 7425
iac n/a| 1 0 16 -38 -5 -70 -.16 30 30 | 450973 1139 3070 7871
mcc n/a| 35 8 36 -423 368 -498 .67 310 310 | --- --- --- ---
Table 2.1586.4 GPS week: 1586 Day: 4 MJD: 55350
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 121| 1 1 -8 -24 9 -3 -.10 28 28 | 0 25 1468 1550
cod 250| -3 0 3 25 -52 29 -.04 19 16 | --- --- --- ---
esx 132| 0 0 0 1 34 65 .07 18 16 | 51728 430 3451 9609
gfz 199| -4 -3 5 -83 55 115 -.31 31 31 | 208822 -1226 3417 10246
iac n/a| 1 1 4 -31 -45 -122 -.08 31 31 | 376749 1129 3430 10103
mcc n/a| 8 49 -4 -179 -186 -1338 .09 261 261 | --- --- --- ---
Table 2.1586.5 GPS week: 1586 Day: 5 MJD: 55351
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 121| 1 0 -9 -9 61 -107 .01 32 32 | 0 -382 2587 2662
cod 250| -2 -1 0 30 -68 25 -.10 14 13 | --- --- --- ---
esx 132| 1 1 0 -18 25 75 .18 23 21 | 50183 104 6572 9415
gfz 199| 1 -3 2 -125 172 95 -.31 30 30 | 209836 632 6576 9562
iac n/a| 3 3 12 -61 10 -42 -.03 36 36 | 375887 2271 6552 9311
mcc n/a| -11 32 44 -11 206 -1371 -.14 301 301 | --- --- --- ---
Table 2.1586.6 GPS week: 1586 Day: 6 MJD: 55352
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 121| 0 0 -14 -11 28 8 -.13 26 25 | 0 0 1835 1910
cod 250| 0 -1 -5 35 -45 60 -.13 18 17 | --- --- --- ---
esx 132| 2 0 6 -34 37 37 .37 23 22 | 67252 908 4270 7167
gfz 199| 0 1 0 4 126 79 -.42 32 32 | 226535 3115 4290 7029
iac n/a| 0 1 17 -71 -26 -140 -.23 32 32 | 393436 831 4279 7720
mcc n/a| -28 -20 67 1 158 -857 .22 322 322 | --- --- --- ---
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 3.1586.0 GPS week: 1586 Day: 0 MJD: 55346
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2064 45 17 19 31 18 --- 14 | 17 13 24 27 24 --- 12
R02E | 894 21 11 26 48 23 --- 11 | 34 22 35 48 24 --- 22
R03E | 1159 29 15 36 34 29 --- 15 | 42 23 40 52 28 --- 25
R04E | 1663 23 10 20 36 18 --- 9 | 28 26 32 36 26 --- 22
R05E | 2404 27 16 16 40 30 --- 12 | 19 38 37 41 29 --- 25
R07E | 863 31 23 38 39 33 --- 17 | 30 22 43 39 36 --- 19
R08E | 1428 33 17 14 45 20 --- 12 | 59 59 53 54 48 --- 53
R10 | 1668 39 12 23 35 25 --- 14 | 48 37 37 32 50 --- 40
R11 | 1422 17 11 23 15 17 --- 9 | 42 37 52 42 34 --- 37
R13 | 1253 30 11 34 26 37 --- 16 | 23 25 43 39 21 --- 22
R14 | 2512 35 17 19 19 23 --- 13 | 33 29 34 26 42 --- 29
R15 | 2743 42 16 24 32 38 133 17 | 26 29 39 39 39 60 26
R17 | 3806 41 21 26 24 49 --- 19 | 61 74 65 56 38 --- 60
R18 | 6426 18 11 23 19 16 --- 9 | 50 63 62 60 50 --- 56
R19 | 1987 24 10 15 35 31 --- 11 | 31 44 53 55 32 --- 39
R20 | 2431 25 24 37 45 35 --- 17 | 26 33 48 52 38 --- 29
R21 | 1037 24 13 39 22 17 --- 13 | 43 53 77 66 58 --- 54
R22 | 1440 34 10 25 17 29 --- 13 | 50 69 77 76 71 --- 66
R23 | 1432 20 16 29 19 33 375 14 | 28 41 52 48 26 99 33
R24 | 1661 21 18 27 15 20 --- 12 | 64 57 78 68 60 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 2362 30 15 27 32 28 281 |T 37 39 49 47 38 79 36
WRMS | 2362 30 14 25 32 28 281 |NE 40 45 55 50 43 79 42
MEDI | 1661 27 15 24 31 25 133 |MD 33 37 43 48 36 60 29
Table 3.1586.1 GPS week: 1586 Day: 1 MJD: 55347
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2401 41 24 23 55 29 --- 17 | 17 40 31 66 31 --- 23
R02E | 1060 27 16 17 28 25 --- 12 | 18 33 27 37 27 --- 19
R03E | 1730 20 14 21 73 25 --- 11 | 20 28 43 57 29 --- 24
R04E | 1627 19 10 28 51 25 --- 11 | 36 29 37 48 28 --- 28
R05E | 2064 20 15 25 44 26 --- 12 | 22 30 51 54 29 --- 26
R07E | 1007 26 17 28 47 39 --- 15 | 14 24 42 43 29 --- 21
R08E | 2907 21 23 35 52 22 --- 15 | 55 65 58 74 52 --- 54
R10 | 1402 30 16 18 16 22 --- 12 | 39 41 47 29 34 --- 38
R11 | 1290 16 7 22 26 26 --- 10 | 23 37 43 40 35 --- 30
R13 | 2044 33 17 12 29 28 --- 13 | 21 24 26 33 23 --- 18
R14 | 2157 18 17 20 25 33 --- 12 | 18 24 34 22 27 --- 20
R15 | 1661 29 12 27 27 29 147 13 | 27 32 43 43 35 73 30
R17 | 4692 33 18 38 31 51 --- 19 | 25 52 75 43 24 --- 42
R18 | 4464 19 7 25 23 23 --- 10 | 30 38 58 55 32 --- 37
R19 | 1094 15 13 24 26 15 --- 9 | 19 31 24 36 20 --- 20
R20 | 2492 13 15 19 27 45 --- 13 | 15 27 39 40 33 --- 25
R21 | 1052 13 10 18 24 25 --- 9 | 31 33 46 31 23 --- 30
R22 | 2050 25 9 39 35 42 --- 16 | 51 48 77 59 46 --- 49
R23 | 929 32 11 42 26 27 440 16 | 19 17 62 40 19 187 23
R24 | 1400 20 15 22 23 20 --- 11 | 35 40 60 55 41 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 2224 25 15 26 37 30 328 |T 26 34 46 45 30 130 29
WRMS | 2224 25 13 24 37 30 328 |NE 27 34 48 40 30 130 31
MEDI | 1661 20 15 23 27 26 147 |MD 22 32 43 43 29 73 26
Table 3.1586.2 GPS week: 1586 Day: 2 MJD: 55348
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1030 28 19 29 41 35 --- 16 | 15 20 41 51 47 --- 21
R02E | 1804 34 31 20 35 27 --- 16 | 22 25 29 28 33 --- 15
R03E | 1207 26 20 19 41 29 --- 13 | 29 26 47 42 38 --- 27
R04E | 863 23 22 22 31 28 --- 13 | 28 31 25 26 30 --- 18
R05E | 1165 26 26 38 32 35 --- 18 | 22 27 47 46 38 --- 24
R07E | 1224 32 21 21 35 38 --- 16 | 29 27 36 28 40 --- 23
R08E | 3529 35 34 33 33 24 --- 18 | 44 66 36 50 34 --- 38
R10 | 1504 25 24 35 --- 20 --- 15 | 43 52 59 --- 38 --- 46
R11 | 1072 14 23 22 29 23 --- 12 | 30 34 50 41 24 --- 33
R13 | 2911 23 11 16 16 28 --- 11 | 30 22 28 21 36 --- 24
R14 | 687 24 17 18 --- 24 --- 12 | 30 26 35 --- 44 --- 28
R15 | 2207 25 11 29 27 34 161 14 | 29 26 45 36 41 75 30
R17 | 3814 34 15 15 19 41 --- 15 | 45 54 54 53 39 --- 47
R18 | 1116 24 16 28 14 16 --- 12 | 32 50 68 46 35 --- 46
R19 | 1338 13 9 15 38 20 --- 8 | 33 29 48 64 28 --- 34
R20 | 1383 37 15 25 33 49 --- 18 | 33 24 36 39 25 --- 18
R21 | 966 33 21 19 19 17 --- 13 | 20 47 49 40 29 --- 34
R22 | 1397 16 23 15 20 16 --- 10 | 39 50 52 49 46 --- 43
R23 | 1539 22 12 26 33 14 538 11 | 23 32 46 51 25 361 29
R24 | 2065 34 18 20 18 40 --- 16 | 32 46 38 49 67 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 1845 27 20 24 30 29 397 |T 30 35 43 42 36 218 31
WRMS | 1845 27 19 24 30 29 397 |NE 32 37 46 44 36 218 34
MEDI | 1338 25 19 21 31 27 161 |MD 30 29 45 42 36 75 29
Table 3.1586.3 GPS week: 1586 Day: 3 MJD: 55349
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1757 19 17 22 34 42 --- 14 | 20 23 29 32 36 --- 18
R02E | 1985 27 26 20 37 31 --- 15 | 19 23 25 44 25 --- 14
R03E | 1793 34 17 22 32 34 --- 15 | 21 26 22 31 35 --- 17
R04E | 1398 27 15 19 25 38 --- 13 | 28 36 27 37 41 --- 28
R05E | 1373 26 19 21 53 34 --- 14 | 21 21 34 54 40 --- 21
R07E | 2714 25 17 27 50 35 --- 15 | 28 19 40 37 40 --- 22
R08E | 2626 26 13 15 33 35 224 12 | 70 72 79 69 71 9999 71
R10 | 1536 20 16 16 36 17 --- 10 | 36 46 41 52 33 --- 38
R11 | 872 27 19 24 28 16 --- 12 | 24 37 45 50 36 --- 32
R13 | 2046 13 12 14 18 22 --- 9 | 29 38 36 40 34 --- 32
R14 | 853 22 15 19 13 25 --- 11 | 23 19 37 30 38 --- 23
R15 | 2434 18 11 13 29 31 160 10 | 23 20 34 42 30 160 23
R17 | 2543 42 16 28 39 41 --- 18 | 51 54 46 68 62 --- 48
R18 | 1245 20 14 10 39 21 --- 9 | 43 48 46 39 63 --- 47
R19 | 2916 16 14 20 25 19 --- 10 | 44 49 54 34 51 --- 47
R20 | 1554 22 17 20 23 34 --- 13 | 44 47 57 61 70 --- 50
R21 | 1074 40 18 13 44 25 --- 14 | 28 43 37 65 55 --- 35
R22 | 526 42 12 11 20 32 --- 14 | 33 61 60 64 80 --- 56
R23 | 1951 23 11 23 26 17 461 11 | 29 33 52 44 39 458 37
R24 | 2613 12 20 30 16 18 --- 12 | 48 43 62 48 48 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1914 26 16 20 33 30 310 |T 33 37 43 47 46 309 35
WRMS | 1914 26 15 20 33 30 310 |NE 35 41 46 49 49 309 39
MEDI | 1757 23 16 20 29 31 224 |MD 28 37 40 44 40 160 32
Table 3.1586.4 GPS week: 1586 Day: 4 MJD: 55350
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2809 14 15 19 30 43 --- 13 | 20 22 31 41 44 --- 23
R02E | 6856 22 23 16 25 43 --- 15 | 22 31 30 36 34 --- 22
R03E | 8503 27 26 32 43 50 --- 19 | 20 24 44 48 34 --- 20
R04E |13133 40 31 16 44 35 --- 17 | 16 25 29 43 35 --- 20
R05E | 9685 45 23 20 59 37 --- 17 | 23 34 38 58 48 --- 28
R07E | 5045 22 16 17 40 27 --- 11 | 19 23 32 46 35 --- 23
R08E | 6770 33 17 22 39 35 92 15 | 46 59 58 75 43 9999 50
R10 | 1759 23 16 20 18 17 --- 11 | 40 41 44 32 37 --- 37
R11 | 4012 21 23 24 31 28 --- 14 | 27 36 45 45 32 --- 29
R13 | 2490 13 14 12 17 14 --- 8 | 24 21 29 29 21 --- 21
R14 | 7432 13 17 14 26 24 --- 10 | 35 42 43 39 36 --- 36
R15 | 3120 32 8 15 20 34 322 13 | 33 18 24 29 37 55 21
R17 |10852 20 20 19 38 26 --- 12 | 51 55 46 48 47 --- 45
R18 |12668 24 16 18 21 16 --- 11 | 37 51 41 47 45 --- 41
R19 | 2931 26 14 16 26 20 --- 11 | 37 50 35 42 35 --- 37
R20 | 5738 16 25 14 24 31 --- 12 | 41 49 48 48 46 --- 44
R21 | 2165 23 16 15 27 20 --- 10 | 37 46 42 54 43 --- 40
R22 | 7318 57 10 24 20 40 --- 19 | 33 55 66 64 70 --- 51
R23 | 3450 18 16 9 19 30 304 10 | 24 39 31 43 30 245 29
R24 | 6224 21 12 14 18 22 --- 9 | 30 39 31 36 28 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 7013 28 19 18 31 31 261 |T 30 38 39 45 39 150 32
WRMS | 7013 28 16 16 31 31 261 |NE 34 41 40 42 39 150 35
MEDI | 5738 22 16 16 26 28 304 |MD 30 39 38 43 36 55 29
Table 3.1586.5 GPS week: 1586 Day: 5 MJD: 55351
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2117 23 12 22 37 38 --- 13 | 14 32 37 38 38 --- 24
R02E | 3777 28 18 23 36 36 --- 14 | 21 34 36 37 41 --- 26
R03E | 8421 22 14 29 25 43 --- 15 | 21 22 38 42 35 --- 19
R04E |14398 35 20 19 32 36 --- 15 | 22 26 29 38 29 --- 20
R05E | 3259 64 21 41 54 38 --- 23 | 27 31 38 58 39 --- 23
R07E | 2750 48 15 18 45 46 --- 17 | 38 23 35 57 39 --- 28
R08E | 6972 30 13 22 23 37 98 14 | 49 56 60 57 46 9999 50
R10 | 1774 36 10 25 15 32 --- 14 | 19 37 55 33 29 --- 33
R11 | 1551 30 11 19 24 37 --- 13 | 25 38 47 44 47 --- 35
R13 | 1548 26 13 23 19 22 --- 11 | 20 28 46 44 23 --- 26
R14 | 3370 29 16 17 21 20 --- 11 | 28 37 25 31 28 --- 26
R15 | 3608 22 9 17 24 41 494 12 | 22 19 32 29 27 81 18
R17 | 8402 27 15 16 43 62 --- 17 | 36 46 44 39 19 --- 38
R18 | 8858 41 18 23 27 24 --- 15 | 28 56 49 48 40 --- 43
R19 | 1539 35 12 15 22 21 --- 11 | 19 38 34 46 37 --- 28
R20 | 5402 27 12 27 29 42 --- 14 | 39 41 40 42 51 --- 37
R21 | 1433 26 14 20 18 19 --- 11 | 40 46 49 45 48 --- 43
R22 | 2555 11 10 20 13 26 --- 9 | 70 64 80 72 88 --- 71
R23 | 3234 14 12 25 25 27 136 11 | 32 32 27 45 35 86 25
R24 | 3706 14 8 17 25 31 --- 9 | 28 25 20 38 45 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 5520 32 14 23 30 36 301 |T 29 36 41 44 39 83 31
WRMS | 5520 32 13 21 30 36 301 |NE 31 39 42 42 39 83 34
MEDI | 3259 27 13 20 25 36 136 |MD 27 34 38 42 38 81 26
Table 3.1586.6 GPS week: 1586 Day: 6 MJD: 55352
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1344 14 16 18 26 33 --- 11 | 25 23 33 36 43 --- 25
R02E | 853 30 22 22 31 32 --- 15 | 27 32 37 34 38 --- 26
R03E | 2387 25 20 18 39 59 --- 18 | 23 24 27 32 42 --- 20
R04E | 4180 25 24 20 33 44 --- 16 | 31 22 33 33 36 --- 23
R05E | 1995 39 32 31 47 40 --- 20 | 29 29 49 50 40 --- 26
XR07E | ---- --- --- --- --- 15 --- 0 | --- --- --- --- 58 --- 55
R08E | 4192 43 15 30 36 36 122 18 | 60 60 59 61 59 9999 56
R10 | 1885 21 23 20 28 33 --- 14 | 28 41 50 55 55 --- 40
R11 | 1520 18 12 22 29 22 --- 10 | 26 30 30 36 27 --- 24
R13 | 1466 23 18 25 38 19 --- 12 | 21 27 30 42 23 --- 21
R14 | 2131 20 24 13 45 31 --- 13 | 32 34 39 32 35 --- 32
R15 | 2572 30 20 25 35 24 534 14 | 19 29 34 27 34 79 23
R17 | 1427 26 17 27 43 50 --- 17 | 58 63 69 51 35 --- 56
R18 | 3113 27 9 24 16 20 --- 11 | 54 60 73 54 63 --- 61
R19 | 1414 29 15 33 19 21 --- 14 | 32 55 70 47 50 --- 49
R20 | 3193 12 16 18 24 23 --- 10 | 33 33 49 51 52 --- 39
R21 | 1066 26 12 14 19 28 --- 11 | 45 66 65 69 68 --- 60
R22 | 1521 31 12 26 24 18 --- 13 | 60 75 88 74 87 --- 75
R23 | 1686 12 8 13 21 21 103 7 | 43 44 41 44 51 234 42
R24 | 1459 18 14 17 21 28 --- 11 | 58 55 57 69 76 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 2280 26 18 23 32 32 321 |T 37 42 49 47 48 156 40
WRMS | 2280 25 17 22 32 32 321 |NE 39 47 53 50 50 156 44
MEDI | 1686 25 16 22 29 28 122 |MD 32 34 49 47 43 79 39
More information about the IGSREPORT
mailing list