[IGSREPORT-19102] Wk 1605 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Oct 28 05:14:55 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1605 (Oct 10, 2010 - Oct 16, 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 2.1605.
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:
igl1605[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1605 in the SP3 format.
igl16057.sum Combination Report for GPS Week 1605.
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 | 367.3 ns
1 | 373.1 ns
2 | 424.1 ns
3 | 428.2 ns
4 | 426.6 ns
5 | 375.6 ns
6 | 369.9 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 1.1605, 1a.1605).
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 2.1605.0-6)
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 3.1605.0-6).
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 1605 summary. (Oct 10, 2010 - Oct 16, 2010)
Table 1.1605.a GPS week : 1605 MJD: 55479.0-55485.0
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 124| 0 2 -6 31 -82 -12 -.15 27 25 | 0 21 2086 2171
| 0 1 2 42 141 170 .04 | 0 259
cod 230| 0 -1 -3 22 18 35 -.15 17 14 | --- --- --- ---
| 1 1 0 29 40 51 .03 | --- ---
esx 137| 0 0 0 -47 45 18 .38 25 23 | 65309 -3279 4300 8982
| 0 0 1 34 51 60 .04 | 27699 3161
gfz 193| 2 1 -3 -3 -3 2 -.24 36 28 | 247735 -3915 4209 7853
| 1 2 3 49 38 60 .05 | 29002 2783
iac n/a| 0 2 14 -51 16 -20 -.01 31 31 | 395369 -647 4279 8617
| 1 1 7 20 42 61 .06 | 29360 1442
mcc n/a| -13 7 -18 18 -208 379 .75 209 209 | --- --- --- ---
| 31 10 53 165 450 1611 1.45 | --- ---
Table 1.1605.b GPS week : 1605 MJD: 55479.0-55485.0
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 | 16 13 14 15 14 8 11 |
R02 | 11 8 12 10 8 10 10 |
R05 | 12 13 12 15 11 11 16 |
R07 | 16 13 12 11 13 11 11 |
R08 | 13 15 11 9 8 10 9 |
R09 | 15 15 12 13 13 11 15 |
R10 | 12 11 12 13 14 16 21 |
R11 | 20 25 28 31 24 32 27 |
R12 | 24 14 16 15 16 14 14 |
R13 | 13 15 13 13 14 16 23 |
R14 | 17 20 17 15 13 12 17 |
R15 | 14 15 15 13 13 14 17 |
R16 | 30 20 13 14 14 17 18 |
R17 | 11 10 11 11 12 16 14 |
R18 | 16 13 14 9 8 9 17 |
R19 | 9 11 11 8 9 13 14 |
R20 | 10 16 15 11 11 10 12 |
R21 | 12 10 14 11 10 12 13 |
R22 | 11 12 16 13 10 12 9 |
R23 | 12 10 12 11 10 11 11 |
R24 | 10 10 9 10 7 6 11 |
Table 1.1605.c GPS week : 1605 MJD: 55479.0-55485.0
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 1605 0 | 13 8 152 -250 -876 -12470 88.1 45490 45490 | 367332 0
brd 1605 1 | -38 -29 94 -480 -445 -14660 86.3 3872 3872 | 373094 0
brd 1605 2 | -24 -6 78 -1382 -1256 -14440 85.0 2450 2450 | 424068 0
brd 1605 3 | 19 -22 96 -49 -2652 -12400 86.7 2334 2334 | 428205 0
brd 1605 4 | 3 95 31 -2464 -2861 -14560 88.8 2289 2289 | 426573 0
brd 1605 5 | 6 -86 119 -1841 -1281 -15910 89.5 2033 2033 | 375581 0
brd 1605 6 | 70 -64 114 -2525 -1566 -13340 89.0 2048 2048 | 369950 0
-------------+------------------------------------------------------------+----------------
brd 1605 mean| 7 -15 98 -1284 -1562 -13968 87.6 8645 8645 | 394971 0
brd 1605 sdev| 35 58 37 1040 891 1285 1.7 16259 16259 | 29423 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 2.1605.0 GPS week: 1605 Day: 0 MJD: 55479
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 124| -1 3 -6 5 19 11 -.21 31 27 | 0 178 1966 2065
cod 230| 0 -4 -3 75 -15 2 -.14 21 19 | --- --- --- ---
esx 137| 0 0 3 -56 -12 82 .42 26 24 | 46456 1676 4572 9791
gfz 193| 1 1 -5 -11 -11 -94 -.25 37 25 | 224756 1651 4194 7021
iac n/a| 2 4 5 -46 2 -29 -.07 27 27 | 367121 2274 4539 7957
mcc n/a| 2 0 38 -51 47 -363 -.26 65 65 | --- --- --- ---
Table 2.1605.1 GPS week: 1605 Day: 1 MJD: 55480
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 124| 0 2 -10 -9 -1 171 -.14 31 30 | 0 197 2402 2502
cod 230| 1 -1 -3 38 10 -8 -.14 18 15 | --- --- --- ---
esx 137| 0 0 0 0 11 8 .38 24 24 | 54678 -5988 4134 9001
gfz 193| 2 2 0 -23 -5 33 -.22 36 32 | 227013 -5674 3849 6961
iac n/a| -1 1 8 -66 1 -99 -.04 26 26 | 373676 -1274 4104 8114
mcc n/a| 2 21 13 -229 -260 -226 -.43 169 169 | --- --- --- ---
Table 2.1605.2 GPS week: 1605 Day: 2 MJD: 55481
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 124| 0 3 -5 41 -44 101 -.16 29 27 | 0 -145 1980 2046
cod 230| 0 -2 -2 4 -8 4 -.11 14 13 | --- --- --- ---
esx 137| 0 0 0 -61 68 -11 .46 28 25 | 96060 -2077 4364 8735
gfz 193| 0 5 -1 32 55 21 -.23 34 22 | 277829 -4719 4375 8233
iac n/a| 0 4 13 -45 17 -71 -.04 32 32 | 424903 74 4335 8899
mcc n/a| -16 7 11 217 -137 1008 .83 186 186 | --- --- --- ---
Table 2.1605.3 GPS week: 1605 Day: 3 MJD: 55482
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 124| 1 2 -2 59 -29 126 -.09 26 24 | 0 129 1930 1977
cod 230| 0 0 -3 22 4 12 -.10 13 12 | --- --- --- ---
esx 137| 2 0 0 -90 64 -76 .35 29 23 | 98990 -4842 4147 9157
gfz 193| 0 2 0 82 35 -40 -.29 39 34 | 280740 -5082 4147 8161
iac n/a| 0 1 13 -15 -33 -50 -.06 30 30 | 427548 -786 4145 8933
mcc n/a| -18 -10 0 -37 201 3148 1.96 334 334 | --- --- --- ---
Table 2.1605.4 GPS week: 1605 Day: 4 MJD: 55483
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 124| 0 0 -5 2 -66 -192 -.12 23 22 | 0 -265 1894 1963
cod 230| 0 -2 -3 11 18 58 -.17 16 14 | --- --- --- ---
esx 137| 0 -1 -1 -3 32 70 .35 21 19 | 86469 -13 4118 9415
gfz 193| 5 0 -4 -3 -30 57 -.17 36 29 | 277155 -3102 4126 9069
iac n/a| 0 2 13 -48 -15 71 .00 28 28 | 427287 -1239 4127 9480
mcc n/a| -79 10 -125 146 -1173 -2149 3.42 307 307 | --- --- --- ---
Table 2.1605.5 GPS week: 1605 Day: 5 MJD: 55484
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 124| 0 1 -4 111 -396 -288 -.20 25 22 | 0 366 2269 2343
cod 230| -1 0 -4 -17 106 139 -.17 16 14 | --- --- --- ---
esx 137| 0 0 0 -73 142 79 .36 24 22 | 41343 -5504 4343 8490
gfz 193| 2 -1 -2 -23 -57 74 -.33 37 27 | 227646 -7005 4359 8232
iac n/a| 0 1 15 -81 93 44 .08 32 32 | 376909 -1963 4314 8906
mcc n/a| 7 5 -25 -98 -6 833 -.07 267 267 | --- --- --- ---
Table 2.1605.6 GPS week: 1605 Day: 6 MJD: 55485
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 124| 0 1 -7 10 -55 -18 -.14 28 25 | 0 -308 2166 2305
cod 230| -1 -1 -4 17 9 36 -.18 17 13 | --- --- --- ---
esx 137| 0 -1 0 -46 14 -19 .35 27 24 | 33167 -6209 4425 8286
gfz 193| 2 1 -10 -77 -11 -31 -.20 33 28 | 219007 -3476 4414 7300
iac n/a| 0 1 29 -56 49 -7 .06 40 40 | 370141 -1617 4391 8031
mcc n/a| 8 16 -40 180 -135 404 -.21 136 136 | --- --- --- ---
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 3.1605.0 GPS week: 1605 Day: 0 MJD: 55479
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1164 22 36 17 29 26 --- 15 | 26 51 33 44 29 --- 31
R02 | 1761 13 13 26 22 20 --- 11 | 29 27 34 31 28 --- 27
R05 | 845 18 16 11 19 31 --- 11 | 40 39 40 44 40 --- 38
R07 | 1943 32 20 33 49 21 --- 15 | 29 37 38 42 33 --- 28
R08 | 2521 21 21 16 31 30 74 13 | 20 36 33 46 43 125 29
R09E | 2086 23 14 28 37 34 --- 14 | 48 58 62 66 61 --- 54
R10E | 1620 15 18 19 39 26 --- 11 | 58 64 67 84 50 --- 59
R11E | 733 37 26 31 44 45 --- 20 | 82 100 102 105 78 --- 88
R12E |>>>>> 30 46 42 --- 38 --- 23 | 43 48 65 --- 49 --- 44
R13E | 992 25 15 20 36 26 --- 12 | 47 47 63 54 43 --- 48
R14E | 1435 39 18 23 41 38 --- 17 | 36 44 42 58 31 --- 33
R15E | 2573 25 19 22 31 29 --- 13 | 41 27 32 38 45 --- 30
R16E | 3397 81 30 57 --- 23 --- 29 | 84 87 70 --- 82 --- 78
R17 | 1312 28 14 14 18 15 --- 10 | 32 34 41 37 31 --- 33
R18 | 1176 35 14 27 27 31 --- 15 | 39 31 38 32 28 --- 30
R19 | 704 16 16 14 39 16 --- 9 | 38 46 44 49 36 --- 38
R20 | 2201 20 18 13 31 20 --- 10 | 31 31 24 27 27 --- 22
R21 | 1577 26 13 20 66 20 --- 11 | 28 27 29 42 27 --- 21
R22 | 756 11 16 27 32 11 --- 10 | 29 35 38 40 31 --- 30
R23 | 931 26 13 24 22 21 55 12 | 22 28 34 37 19 156 23
R24 | 2171 25 14 9 48 17 --- 9 | 28 26 33 40 24 --- 24
------+-----------------------------------------+-------------------------------------
RMS |45491 31 21 26 37 27 65 |T 39 43 45 48 39 140 38
WRMS |45491 27 19 24 25 27 65 |NE 30 34 35 39 30 140 28
MEDI | 1577 25 16 22 32 26 55 |MD 36 37 38 42 33 125 31
Table 3.1605.1 GPS week: 1605 Day: 1 MJD: 55480
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 797 21 24 22 21 18 --- 12 | 26 39 28 31 37 --- 29
R02 | 1416 17 10 13 24 16 --- 8 | 33 37 40 39 32 --- 34
R05 | 986 25 17 27 24 23 --- 13 | 36 23 24 18 18 --- 16
R07 | 4409 16 23 26 41 21 --- 13 | 23 31 50 54 17 --- 28
R08 | 3018 18 25 23 25 35 96 15 | 13 40 37 33 38 91 27
R09E | 1687 36 19 26 23 22 --- 14 | 39 41 57 58 48 --- 40
R10E | 3529 16 12 18 30 25 --- 10 | 37 36 38 41 33 --- 33
R11E | 1089 62 28 29 49 56 --- 25 | 63 87 75 70 65 --- 69
R12E |14326 24 21 21 --- 28 --- 13 | 43 45 53 --- 46 --- 42
R13E | 957 38 11 33 59 22 --- 15 | 53 38 47 76 41 --- 40
R14E | 995 55 21 25 32 34 --- 19 | 31 33 31 28 26 --- 25
R15E | 2525 23 13 32 52 32 205 14 | 41 25 30 49 38 144 26
R16E | 4960 49 29 28 49 33 --- 20 | 45 53 51 76 41 --- 43
R17 | 1794 24 11 19 26 16 --- 10 | 18 20 29 20 15 --- 16
R18 | 909 35 12 20 26 19 --- 12 | 38 18 30 39 20 --- 20
R19 | 1228 22 9 19 27 22 --- 10 | 38 30 31 34 28 --- 27
R20 | 2760 35 21 36 51 20 --- 16 | 21 27 53 60 24 --- 24
R21 | 2222 21 14 14 22 21 --- 10 | 14 22 31 37 20 --- 16
R22 | 636 25 16 26 29 16 --- 12 | 24 38 48 38 35 --- 33
R23 | 903 21 9 16 34 22 187 9 | 20 21 19 40 28 52 17
R24 | 2951 16 14 22 36 10 --- 9 | 23 22 30 36 19 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 3872 31 18 24 36 26 169 |T 32 34 39 43 31 95 29
WRMS | 3872 30 15 24 32 26 169 |NE 25 28 34 36 25 71 23
MEDI | 1687 24 16 23 29 22 187 |MD 33 33 37 39 32 91 27
Table 3.1605.2 GPS week: 1605 Day: 2 MJD: 55481
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1115 37 14 24 40 26 --- 14 | 33 40 41 51 43 --- 35
R02 | 1120 18 12 30 17 22 --- 11 | 38 33 45 29 32 --- 31
R05 | 611 35 11 11 23 26 --- 12 | 39 24 36 37 37 --- 28
R07 | 5090 14 19 28 30 17 --- 11 | 24 24 31 42 28 --- 20
R08 | 2942 17 15 10 19 31 150 10 | 34 42 34 36 27 107 30
R09E | 770 24 11 19 24 32 --- 12 | 34 39 50 50 47 --- 39
R10E | 3016 21 12 15 34 38 --- 12 | 46 51 45 55 45 --- 43
R11E | 981 63 18 54 56 68 --- 28 | 60 74 119 118 71 --- 77
R12E | 2375 22 18 42 55 29 --- 16 | 28 43 63 63 37 --- 39
R13E | 727 20 16 28 40 29 --- 13 | 38 46 56 55 41 --- 40
R14E | 784 46 16 23 54 37 --- 17 | 25 33 29 46 26 --- 24
R15E | 2709 28 13 29 45 39 182 15 | 32 19 30 46 36 129 21
R16E | 5368 20 16 22 37 36 --- 13 | 57 54 56 51 59 --- 52
R17 | 2699 25 13 16 31 22 --- 10 | 29 36 37 46 30 --- 32
R18 | 1994 34 16 16 32 30 --- 13 | 27 36 26 24 42 --- 28
R19 | 1100 25 8 12 19 32 --- 10 | 53 46 52 53 45 --- 46
R20 | 3747 19 11 38 22 33 --- 14 | 24 22 56 45 22 --- 27
R21 | 1563 29 14 32 24 19 --- 13 | 23 27 39 34 24 --- 21
R22 | 767 23 16 43 19 28 --- 16 | 26 35 57 35 25 --- 32
R23 | 871 18 18 22 21 22 220 11 | 29 45 40 30 28 85 34
R24 | 2160 21 7 16 34 21 --- 9 | 29 34 37 63 39 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 2449 29 14 28 34 32 186 |T 34 38 46 48 37 107 34
WRMS | 2449 27 13 25 22 32 186 |NE 31 34 40 40 32 96 30
MEDI | 1563 23 14 23 31 29 182 |MD 32 36 41 46 37 107 32
Table 3.1605.3 GPS week: 1605 Day: 3 MJD: 55482
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2385 36 18 30 32 27 --- 15 | 30 42 59 54 30 --- 35
R02 | 761 17 9 25 22 14 --- 9 | 36 39 42 48 43 --- 36
R05 | 990 33 11 36 29 26 --- 14 | 34 33 39 34 39 --- 29
R07 | 1137 17 9 31 22 18 --- 10 | 18 15 30 24 22 --- 15
R08 | 2199 18 12 15 20 16 341 8 | 29 37 35 24 34 248 32
R09E | 1355 17 11 30 38 31 --- 12 | 37 42 69 56 48 --- 44
R10E | 3193 19 14 21 35 35 --- 12 | 58 45 55 67 48 --- 46
R11E | 964 53 22 73 55 73 --- 30 | 69 80 139 111 82 --- 84
R12E | 1189 24 11 30 49 41 --- 14 | 39 39 57 41 43 --- 39
R13E | 1444 17 16 25 33 32 --- 12 | 34 36 48 52 32 --- 32
R14E | 782 34 13 30 50 29 --- 14 | 21 22 37 38 33 --- 22
R15E | 2995 28 14 24 79 30 --- 13 | 27 23 29 68 45 --- 24
R16E | 5776 33 12 23 36 28 --- 13 | 59 51 58 55 55 --- 52
R17 | 2362 20 14 13 48 30 --- 11 | 46 33 41 35 59 --- 40
R18 | 4637 19 11 14 36 16 --- 8 | 30 40 40 40 36 --- 34
R19 | 782 14 12 9 34 21 --- 8 | 44 37 36 48 36 --- 36
R20 | 2932 20 7 24 22 28 --- 11 | 34 25 34 35 20 --- 24
R21 | 974 24 10 23 21 21 --- 10 | 37 27 39 37 25 --- 28
R22 | 1038 19 19 29 47 22 --- 12 | 36 41 28 51 25 --- 29
R23 | 1037 16 12 25 21 24 326 10 | 24 23 36 33 25 118 21
R24 | 1493 27 7 23 25 13 --- 10 | 30 30 46 45 32 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2334 26 13 29 39 30 334 |T 36 36 47 47 38 183 34
WRMS | 2334 24 12 23 34 30 334 |NE 32 32 38 39 32 183 29
MEDI | 1355 20 12 25 34 27 326 |MD 34 37 40 45 36 118 32
Table 3.1605.4 GPS week: 1605 Day: 4 MJD: 55483
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3158 35 15 19 32 22 --- 13 | 22 34 38 46 27 --- 27
R02 | 1019 14 13 15 16 13 --- 8 | 19 27 23 28 14 --- 18
R05 | 2366 14 15 26 27 17 --- 10 | 35 35 50 43 31 --- 35
R07 | 2891 18 24 23 23 20 --- 12 | 15 35 28 25 24 --- 20
R08 | 2625 15 14 11 12 17 --- 8 | 23 22 26 26 29 --- 21
R09E | 2157 19 21 25 37 27 --- 13 | 28 36 49 57 45 --- 35
R10E | 1592 30 20 17 33 28 --- 13 | 49 49 54 49 45 --- 46
R11E | 1362 41 22 36 40 67 --- 23 | 74 85 79 85 80 --- 74
R12E | 1073 25 18 22 27 45 --- 16 | 31 33 47 38 44 --- 31
R13E | 2955 19 14 29 27 36 --- 14 | 27 28 46 38 33 --- 26
R14E | 1511 21 17 16 38 34 --- 12 | 21 21 28 26 33 --- 18
R15E | 3007 30 12 20 68 29 --- 13 | 20 17 28 49 41 --- 19
R16E | 3919 32 19 23 57 21 --- 14 | 37 30 51 67 43 --- 36
R17 | 1033 25 13 23 33 15 --- 11 | 35 25 51 45 36 --- 32
R18 | 4276 14 10 13 27 20 --- 8 | 51 40 41 40 24 --- 38
R19 | 744 15 11 18 25 19 --- 9 | 46 45 57 51 36 --- 45
R20 | 2213 14 18 16 27 25 --- 10 | 25 20 23 32 16 --- 17
R21 | 1287 21 11 13 17 21 --- 9 | 23 34 34 34 21 --- 27
R22 | 1579 18 12 20 50 15 --- 9 | 33 34 33 64 29 --- 28
R23 | 1436 17 16 19 54 17 307 10 | 28 29 40 67 24 239 27
R24 | 1221 13 7 8 23 19 --- 7 | 39 28 34 35 25 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 2288 23 16 21 36 28 307 |T 32 33 40 45 33 239 30
WRMS | 2288 22 14 19 29 28 307 |NE 30 31 36 41 25 239 28
MEDI | 1592 19 15 19 27 21 307 |MD 28 33 40 43 31 239 28
Table 3.1605.5 GPS week: 1605 Day: 5 MJD: 55484
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1898 11 8 16 12 21 --- 8 | 43 15 26 28 19 --- 19
R02 | 1039 21 12 12 24 24 --- 10 | 45 22 25 29 34 --- 25
R05 | 3204 21 8 26 23 18 --- 11 | 45 27 43 36 27 --- 30
R07 | 1308 16 17 13 41 31 --- 11 | 35 22 21 33 30 --- 14
R08 | 1076 12 16 17 28 23 165 10 | 38 21 35 32 26 188 22
R09E | 2464 14 13 23 74 28 --- 11 | 41 33 50 63 45 --- 34
R10E | 1016 37 19 20 44 32 --- 15 | 61 52 53 67 51 --- 48
R11E | 2283 55 34 52 62 83 --- 31 | 91 122 140 141 91 --- 107
R12E | 1863 21 14 21 31 40 --- 13 | 35 27 39 33 45 --- 26
R13E | 3232 26 18 23 31 45 --- 16 | 43 23 43 42 46 --- 28
R14E | 1524 21 9 17 39 35 --- 12 | 39 20 28 30 31 --- 18
R15E | 2353 25 13 28 51 34 394 14 | 38 29 30 43 47 380 21
R16E | 4295 38 27 28 33 24 --- 17 | 42 40 43 43 44 --- 31
R17 | 811 24 12 37 35 34 --- 15 | 37 28 53 36 19 --- 29
R18 | 1471 16 13 15 20 19 --- 9 | 37 26 35 28 18 --- 23
R19 | 857 36 12 15 28 26 --- 13 | 56 37 39 39 40 --- 38
R20 | 1042 13 14 21 30 20 --- 10 | 46 30 45 44 30 --- 33
R21 | 1730 18 13 24 23 28 --- 11 | 46 35 28 45 23 --- 28
R22 | 1839 21 20 21 21 20 --- 12 | 36 40 26 36 26 --- 29
R23 | 1364 18 16 25 40 11 177 10 | 34 23 25 43 18 234 18
R24 | 1872 7 9 10 21 12 --- 5 | 36 24 26 23 22 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2032 25 16 24 37 32 267 |T 44 33 40 43 34 267 30
WRMS | 2032 22 14 22 27 32 267 |NE 41 26 32 34 25 211 25
MEDI | 1730 21 13 21 31 26 177 |MD 41 27 35 36 30 234 28
Table 3.1605.6 GPS week: 1605 Day: 6 MJD: 55485
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1250 21 11 21 42 23 --- 10 | 26 29 34 36 22 --- 26
R02 | 1896 15 9 23 23 21 --- 9 | 23 28 38 40 26 --- 26
R05 | 3054 37 17 28 17 29 --- 15 | 26 41 47 32 33 --- 33
R07 | 2872 23 12 21 35 21 --- 11 | 25 31 33 43 30 --- 25
R08 | 1154 10 10 17 22 23 120 8 | 26 28 29 27 26 93 25
R09E | 2509 23 14 27 36 47 --- 15 | 37 39 55 57 60 --- 39
R10E | 978 53 25 22 44 43 --- 20 | 63 64 65 65 61 --- 60
R11E | 1475 42 29 47 48 80 --- 27 | 121 135 138 127 130 --- 127
R12E | 1214 17 11 26 37 44 --- 13 | 29 30 48 35 42 --- 30
R13E | 2600 46 32 25 39 58 --- 22 | 37 38 52 54 50 --- 34
R14E | 895 21 19 26 40 56 --- 17 | 23 23 26 30 55 --- 20
R15E | 3677 22 20 23 31 58 48 17 | 31 28 32 33 62 41 28
R16E | 2076 20 19 31 53 58 --- 18 | 57 56 56 63 60 --- 51
R17 | 778 30 12 13 22 38 --- 13 | 39 46 45 46 51 --- 43
R18 | 2619 29 12 45 25 24 --- 16 | 55 37 42 39 46 --- 39
R19 | 807 37 12 18 25 31 --- 14 | 50 43 48 52 44 --- 44
R20 | 1360 20 10 26 26 26 --- 11 | 29 34 30 40 40 --- 30
R21 | 1464 15 18 29 26 26 --- 12 | 40 51 57 39 42 --- 45
R22 | 1525 11 12 21 39 20 --- 9 | 36 51 52 65 43 --- 44
R23 | 2378 20 12 23 20 18 197 10 | 21 26 38 35 25 176 23
R24 | 2756 17 14 27 19 17 --- 11 | 34 25 34 31 30 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2047 28 17 27 33 40 136 |T 39 42 47 47 46 103 38
WRMS | 2047 25 13 24 28 40 136 |NE 33 36 40 40 35 134 33
MEDI | 1525 21 12 25 31 29 120 |MD 34 37 45 40 43 93 33
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