[IGSREPORT-18647] Wk 1584 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jun 3 04:51:42 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1584 (May 16, 2010 - May 22, 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 2.1584.
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:
igl1584[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1584 in the SP3 format.
igl15847.sum Combination Report for GPS Week 1584.
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 | 463.5 ns
1 | 463.7 ns
2 | 463.1 ns
3 | 414.0 ns
4 | 409.9 ns
5 | 457.2 ns
6 | 378.3 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 1.1584, 1a.1584).
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 2.1584.0-6)
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 3.1584.0-6).
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 1584 summary. (May 16, 2010 - May 22, 2010)
Table 1.1584.a GPS week : 1584 MJD: 55332.0-55338.0
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 127| 1 1 -13 -10 13 -11 -.11 26 23 | 0 2 1751 1819
| 1 1 3 10 61 95 .05 | 0 83
cod 244| -3 -1 3 31 -45 20 -.12 15 14 | --- --- --- ---
| 1 0 1 10 33 30 .03 | --- ---
esx 131| 0 0 8 3 73 54 .49 25 23 | 98370 -1904 4054 7502
| 1 2 5 14 20 56 .06 | 36100 2948
gfz 198| 0 -2 6 -63 1 90 -.23 31 31 | 273100 -1339 4057 7728
| 1 3 4 44 31 56 .11 | 35759 2904
iac n/a| 2 1 0 -52 -4 -87 -.22 26 26 | 436318 -449 4062 8059
| 2 1 8 10 24 56 .05 | 34785 1262
mcc n/a| 0 -7 39 -106 109 1595 -.88 317 317 | --- --- --- ---
| 8 23 59 214 221 1805 .98 | --- ---
Table 1.1584.b GPS week : 1584 MJD: 55332.0-55338.0
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 11 9 10 10 7 10 |
R02 | 11 12 13 8 12 8 13 |
R03 | 11 13 14 14 12 14 13 |
R04 | 18 12 26 18 11 11 9 |
R05 | 22 28 15 15 10 12 13 |
R07 | 8 12 10 15 12 17 16 |
R08 | 8 13 9 12 11 10 10 |
R10 | 12 11 9 13 13 14 13 |
R11 | 23 15 14 13 15 12 12 |
R13 | 15 14 17 13 10 8 12 |
R14 | 14 8 11 9 11 12 26 |
R15 | 13 12 15 15 12 15 18 |
R17 | 15 15 12 15 18 14 23 |
R18 | 13 9 14 15 10 10 11 |
R19 | 10 11 11 7 10 10 10 |
R20 | 16 16 13 13 19 17 15 |
R21 | 12 15 11 13 11 14 10 |
R22 | 9 12 10 10 12 13 15 |
R23 | 14 15 9 10 8 11 9 |
R24 | 10 11 10 12 9 8 11 |
Table 1.1584.c GPS week : 1584 MJD: 55332.0-55338.0
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 1584 0 | 39 32 7 314 -1347 -14470 83.6 3940 3940 | 463511 0
brd 1584 1 | 1 178 214 -407 -116 -19120 85.1 3124 3124 | 463743 0
brd 1584 2 | -102 -9 200 1496 -1917 -23460 87.3 2590 2590 | 463120 0
brd 1584 3 | -43 77 251 435 -2021 -23170 82.2 2715 2715 | 414035 0
brd 1584 4 | -4 56 167 -2767 702 -20220 83.9 3040 3040 | 409861 0
brd 1584 5 | -10 -59 85 -1808 2511 -18750 91.0 2751 2751 | 457161 0
brd 1584 6 | -97 -6 216 -585 -2629 -22150 87.7 2554 2554 | 378334 0
-------------+------------------------------------------------------------+----------------
brd 1584 mean| -31 38 163 -474 -688 -20191 85.8 2959 2959 | 435680 0
brd 1584 sdev| 53 77 86 1436 1824 3145 3.0 482 482 | 34641 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 2.1584.0 GPS week: 1584 Day: 0 MJD: 55332
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 127| 1 3 -18 -12 -11 -93 -.07 34 27 | 0 -5 1672 1731
cod 244| -4 0 1 23 -48 59 -.11 15 15 | --- --- --- ---
esx 131| 0 0 5 -17 70 129 .38 24 22 | 131236 1880 3711 7249
gfz 198| 1 2 2 -130 20 193 -.21 32 32 | 301269 1904 3707 7682
iac n/a| 3 3 8 -61 5 -144 -.16 27 27 | 464181 935 3712 8077
mcc n/a| 4 7 -44 -237 -172 2217 -1.95 370 370 | --- --- --- ---
Table 2.1584.1 GPS week: 1584 Day: 1 MJD: 55333
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 127| 2 3 -15 -9 134 12 -.05 28 22 | 0 11 1844 1889
cod 244| -3 -1 2 38 -109 23 -.16 16 15 | --- --- --- ---
esx 131| 0 0 3 13 35 65 .49 26 23 | 128825 -4824 4241 6945
gfz 198| -2 -4 1 -100 58 96 -.44 34 34 | 304441 -5619 4243 7230
iac n/a| 2 0 9 -31 19 -109 -.17 26 26 | 465518 -1712 4249 7639
mcc n/a| -1 -15 12 -95 188 -831 .40 245 245 | --- --- --- ---
Table 2.1584.2 GPS week: 1584 Day: 2 MJD: 55334
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 127| 1 0 -9 8 26 0 -.06 22 17 | 0 -62 1772 1832
cod 244| -3 0 2 17 -42 32 -.11 16 14 | --- --- --- ---
esx 131| 0 -1 9 8 85 80 .51 27 25 | 115952 -3355 4344 6999
gfz 198| 0 -2 10 -39 -13 74 -.14 31 29 | 301356 -2240 4339 6998
iac n/a| 3 0 0 -44 -29 -141 -.24 26 26 | 462816 -755 4357 7557
mcc n/a| 16 -4 29 -198 289 673 -1.19 288 288 | --- --- --- ---
Table 2.1584.3 GPS week: 1584 Day: 3 MJD: 55335
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 127| 0 -1 -15 -15 -60 -23 -.12 24 22 | 0 122 1690 1783
cod 244| -3 -1 4 32 -14 14 -.11 14 12 | --- --- --- ---
esx 131| 1 2 9 15 77 76 .51 23 21 | 78762 1240 4014 7443
gfz 198| 0 0 9 -4 -27 79 -.17 29 28 | 251392 -535 4035 7738
iac n/a| 4 3 2 -55 -36 -51 -.30 28 28 | 415016 -397 4048 8044
mcc n/a| -3 21 27 -215 -52 1087 -2.08 449 449 | --- --- --- ---
Table 2.1584.4 GPS week: 1584 Day: 4 MJD: 55336
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 127| 0 0 -12 -12 -22 -139 -.17 22 22 | 0 104 1924 1982
cod 244| -2 -2 3 30 -9 49 -.07 15 14 | --- --- --- ---
esx 131| 0 3 12 17 63 7 .47 23 22 | 71596 305 4302 7682
gfz 198| -1 -6 5 -70 -9 68 -.10 28 28 | 244942 2631 4325 7932
iac n/a| 1 1 -10 -50 -20 16 -.25 23 23 | 409880 1356 4303 7983
mcc n/a| -7 -9 65 62 -81 1060 -.93 303 303 | --- --- --- ---
Table 2.1584.5 GPS week: 1584 Day: 5 MJD: 55337
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 127| 1 2 -12 -25 24 162 -.11 25 25 | 0 -81 1638 1718
cod 244| -3 0 6 48 -34 -27 -.10 13 12 | --- --- --- ---
esx 131| 1 0 15 -16 79 -43 .57 26 24 | 124734 -5020 3694 8611
gfz 198| 0 -1 12 -20 -30 5 -.30 29 29 | 293621 -2249 3688 8638
iac n/a| 2 1 -13 -59 12 -90 -.20 23 23 | 457999 -484 3683 8812
mcc n/a| -2 -2 30 284 446 1939 .33 200 200 | --- --- --- ---
Table 2.1584.6 GPS week: 1584 Day: 6 MJD: 55338
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 127| 2 0 -12 -10 0 0 -.17 28 25 | 0 -75 1722 1802
cod 244| 0 -1 5 29 -61 -6 -.16 17 17 | --- --- --- ---
esx 131| -1 -3 1 1 100 63 .51 25 23 | 37490 -3559 4076 7591
gfz 198| -3 -7 3 -80 10 116 -.21 34 34 | 214680 -3271 4062 7881
iac n/a| -2 1 1 -59 20 -95 -.20 28 28 | 378819 -2092 4082 8305
mcc n/a| -5 -52 152 -342 147 5025 -.74 361 361 | --- --- --- ---
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 3.1584.0 GPS week: 1584 Day: 0 MJD: 55332
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1008 18 17 26 26 22 --- 12 | 22 22 28 33 34 --- 22
R02 | 2879 20 14 19 25 22 --- 10 | 52 63 73 66 58 --- 61
R03 | 1724 22 14 12 22 26 --- 10 | 76 87 90 94 97 --- 88
R04 | 8886 57 12 29 31 23 --- 17 | 181 228 244 234 225 --- 222
R05 |11193 71 20 37 34 26 --- 22 | 140 214 228 225 193 --- 199
R07 | 876 13 9 11 20 23 --- 8 | 18 20 20 26 29 --- 18
R08 | 970 15 11 14 22 18 306 8 | 53 59 72 68 66 83 61
R10E | 5876 31 11 19 42 27 --- 12 | 66 55 46 67 58 --- 53
R11E | 3063 68 16 36 68 39 --- 22 | 45 38 58 75 54 --- 41
R13E | 2203 32 18 29 43 30 --- 15 | 26 46 57 63 49 --- 40
R14E | 1606 29 12 22 41 34 --- 13 | 50 56 61 50 41 --- 48
R15E | 1570 22 16 17 31 32 443 12 | 30 37 43 45 37 349 32
R17 | 1471 30 18 34 20 20 --- 14 | 45 60 46 43 42 --- 47
R18 | 4422 27 19 29 25 18 --- 13 | 33 43 66 50 66 --- 48
R19 | 879 15 13 18 12 22 --- 10 | 44 58 53 57 62 --- 53
R20 | 1351 31 17 31 27 36 --- 16 | 41 65 52 69 84 --- 58
R21 | 798 36 10 15 30 24 --- 12 | 34 58 62 59 64 --- 54
R22 | 2207 15 9 21 20 18 --- 9 | 33 43 56 49 49 --- 43
R23 | 1626 22 21 21 31 32 348 14 | 22 24 36 36 26 176 20
R24 | 2418 19 13 16 35 23 --- 10 | 35 37 45 56 36 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 3939 34 15 24 32 27 370 |T 52 65 71 73 68 202 62
WRMS | 3939 27 15 22 32 27 370 |NE 55 72 78 77 75 129 68
MEDI | 1626 22 14 21 27 23 348 |MD 41 55 56 57 54 176 48
Table 3.1584.1 GPS week: 1584 Day: 1 MJD: 55333
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1383 14 13 23 16 24 --- 10 | 19 25 32 27 24 --- 18
R02 | 1085 15 24 23 33 19 --- 12 | 42 67 39 67 52 --- 50
R03 | 1098 27 21 16 24 24 --- 13 | 104 114 116 112 111 --- 110
R04 | 6264 24 12 21 21 23 --- 11 | 275 271 274 278 299 --- 277
R05 | 7608 77 30 41 41 38 --- 27 | 103 175 176 167 154 --- 151
R07 | 1885 17 11 26 21 26 --- 11 | 20 27 43 23 26 --- 21
R08 | 965 27 20 19 33 25 254 13 | 29 62 44 69 42 50 43
R10E | 5221 21 10 22 26 22 --- 10 | 31 46 61 47 40 --- 43
R11E | 2102 27 13 34 52 25 --- 14 | 28 32 64 78 35 --- 34
R13E | 1517 32 17 24 45 24 --- 14 | 16 37 41 47 37 --- 27
R14E | 1962 16 10 10 40 19 --- 8 | 31 34 31 43 32 --- 29
R15E | 4405 10 15 19 67 34 287 12 | 18 31 38 56 28 183 22
R17 | 3306 34 15 27 32 23 --- 14 | 26 37 50 62 38 --- 35
R18 | 1531 17 11 17 33 18 --- 9 | 39 28 35 33 25 --- 27
R19 | 1000 13 13 19 29 27 --- 10 | 28 38 47 55 15 --- 30
R20 | 2648 32 15 16 43 42 --- 15 | 32 47 38 69 44 --- 38
R21 | 922 21 20 37 18 23 --- 14 | 28 38 34 24 31 --- 24
R22 | 1400 15 18 30 17 21 --- 12 | 17 38 46 35 22 --- 26
R23 | 1172 14 16 43 19 20 184 14 | 15 18 49 39 25 154 17
R24 | 2546 23 12 23 20 19 --- 11 | 15 25 42 31 32 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 3123 28 16 26 34 26 245 |T 45 59 65 68 55 129 52
WRMS | 3123 22 15 23 34 26 245 |NE 52 67 71 72 62 102 59
MEDI | 1531 21 15 23 29 23 254 |MD 28 37 43 47 32 154 29
Table 3.1584.2 GPS week: 1584 Day: 2 MJD: 55334
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 804 11 12 18 19 18 --- 8 | 19 26 24 23 29 --- 21
R02 | 1673 20 19 32 19 21 --- 13 | 66 76 85 82 78 --- 74
R03 | 2675 16 22 28 15 27 --- 13 | 84 102 101 98 107 --- 97
R04 | 1435 59 30 44 46 43 --- 25 | 122 195 200 210 184 --- 173
R05 | 3211 33 20 26 40 24 --- 15 | 176 206 216 208 212 --- 201
R07 | 2512 18 13 15 19 19 --- 9 | 18 19 20 23 26 --- 16
R08 | 2197 11 11 19 15 24 166 9 | 61 55 70 58 59 38 58
R10E | 4810 11 15 17 36 18 --- 9 | 35 36 36 44 33 --- 31
R11E | 2777 24 13 36 58 22 --- 13 | 29 33 57 64 36 --- 32
R13E | 2036 28 19 39 33 33 --- 16 | 21 35 52 45 47 --- 30
R14E | 1184 13 12 26 41 23 --- 10 | 41 50 57 49 49 --- 46
R15E | 3990 15 17 27 49 41 414 14 | 11 20 34 45 28 176 15
R17 | 4197 13 13 22 24 32 --- 11 | 56 52 73 50 31 --- 50
R18 | 3477 16 20 29 24 30 --- 13 | 31 28 66 57 64 --- 41
R19 | 1421 19 10 27 19 15 --- 10 | 45 41 28 37 42 --- 36
R20 | 2465 18 18 28 23 25 --- 12 | 40 45 41 40 44 --- 38
R21 | 1559 10 15 17 18 29 --- 10 | 26 30 38 36 26 --- 22
R22 | 1168 17 13 22 15 13 --- 9 | 15 27 40 32 29 --- 23
R23 | 1338 12 12 19 20 21 224 9 | 12 11 23 21 21 84 9
R24 | 2071 13 10 22 28 21 --- 9 | 26 28 40 34 20 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 2589 22 16 27 31 26 288 |T 46 55 65 62 58 99 51
WRMS | 2589 17 14 25 29 26 288 |NE 53 62 71 67 64 61 58
MEDI | 2071 16 13 26 23 23 224 |MD 31 35 41 45 36 84 32
Table 3.1584.3 GPS week: 1584 Day: 3 MJD: 55335
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 718 17 11 16 11 25 --- 9 | 21 23 26 25 35 --- 20
R02 | 2203 11 8 15 16 20 --- 7 | 30 37 46 38 31 --- 33
R03 | 1959 27 20 21 17 32 --- 14 | 80 96 88 89 85 --- 86
R04 | 4682 42 20 38 25 20 --- 17 | 285 286 300 297 276 --- 286
R05 | 1811 38 20 17 24 20 --- 14 | 62 92 90 81 79 --- 80
R07 | 2255 42 13 14 23 30 --- 14 | 20 22 23 25 32 --- 16
R08 | 3484 19 11 31 18 22 196 12 | 43 40 67 50 44 31 45
R10E | 3126 19 16 24 45 28 --- 12 | 38 46 52 59 45 --- 41
R11E | 1917 28 14 29 39 22 --- 13 | 42 42 67 69 53 --- 47
R13E | 2954 24 19 26 37 21 --- 13 | 26 47 62 71 52 --- 43
R14E | 2404 17 11 16 34 19 --- 9 | 47 45 50 49 51 --- 44
R15E | 3410 29 9 24 41 42 688 14 | 32 40 55 44 33 273 37
R17 | 3532 23 17 19 35 45 --- 15 | 29 46 46 30 23 --- 34
R18 | 4711 19 10 26 29 47 --- 15 | 29 37 39 48 61 --- 36
R19 | 2278 14 8 14 20 11 --- 6 | 35 43 40 54 43 --- 38
R20 | 2560 20 15 18 14 36 --- 12 | 37 39 61 49 72 --- 48
R21 | 1506 21 11 24 29 32 --- 12 | 26 53 67 68 28 --- 43
R22 | 1283 17 12 16 24 27 --- 10 | 41 52 43 55 68 --- 49
R23 | 2046 10 13 27 21 18 306 10 | 14 20 35 31 28 61 18
R24 | 1294 18 12 31 36 18 --- 11 | 12 26 41 42 37 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 2715 24 14 23 29 28 449 |T 47 56 64 63 58 121 53
WRMS | 2715 22 12 21 28 28 449 |NE 50 60 67 65 62 46 57
MEDI | 2255 19 12 21 24 22 306 |MD 32 42 50 49 44 61 41
Table 3.1584.4 GPS week: 1584 Day: 4 MJD: 55336
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1169 18 10 22 13 15 --- 9 | 14 18 27 25 29 --- 17
R02 | 1764 27 11 25 18 14 --- 11 | 46 41 45 52 54 --- 43
R03 | 729 21 17 15 23 28 --- 12 | 68 82 87 87 91 --- 80
R04 | 4460 19 14 27 22 18 --- 11 | 85 111 116 104 105 --- 104
R05 | 5985 12 20 15 26 20 --- 10 | 105 121 108 128 114 --- 112
R07 | 2706 31 13 17 24 22 --- 12 | 21 20 30 32 37 --- 21
R08 | 4321 20 8 24 18 20 157 10 | 29 39 41 44 38 24 33
R10E | 2883 27 17 20 42 21 --- 12 | 42 63 64 60 39 --- 50
R11E | 2406 22 19 36 31 23 --- 14 | 58 52 64 54 43 --- 50
R13E | 3521 16 13 26 34 14 --- 10 | 34 37 51 50 29 --- 34
R14E | 2983 22 15 20 33 20 --- 11 | 48 49 69 75 53 --- 52
R15E | 3451 27 16 24 36 18 --- 12 | 39 51 61 60 40 --- 45
R17 | 3279 32 27 18 37 42 --- 17 | 22 47 43 28 20 --- 29
R18 | 4388 16 14 25 19 13 --- 10 | 27 40 40 29 31 --- 31
R19 | 2038 18 8 25 15 14 --- 9 | 39 45 63 39 49 --- 47
R20 | 1940 34 15 31 23 47 --- 18 | 16 27 53 47 41 --- 29
R21 | 1163 16 7 23 34 28 --- 11 | 40 41 46 48 59 --- 43
R22 | 1386 22 15 25 32 22 --- 12 | 45 61 78 54 49 --- 56
R23 | 2794 9 10 20 30 15 399 8 | 24 27 40 26 17 112 23
R24 | 1306 9 13 15 21 23 --- 9 | 27 21 39 39 43 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 3039 22 15 23 28 23 303 |T 41 49 58 54 49 68 46
WRMS | 3039 22 14 22 28 23 303 |NE 40 49 57 52 51 68 46
MEDI | 2706 20 14 23 24 20 157 |MD 39 41 51 48 41 24 43
Table 3.1584.5 GPS week: 1584 Day: 5 MJD: 55337
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 877 8 7 13 27 19 --- 7 | 15 15 28 32 28 --- 16
R02 | 1627 10 12 13 15 20 --- 8 | 28 31 27 35 41 --- 29
R03 | 1451 27 12 36 19 23 --- 13 | 40 47 75 62 46 --- 47
R04 | 5522 22 12 20 13 26 --- 11 | 200 192 196 197 185 --- 192
R05 | 6009 20 13 22 21 28 --- 11 | 66 76 64 71 72 --- 69
R07 | 3240 36 24 34 35 24 --- 16 | 28 30 39 41 22 --- 23
R08 | 3165 19 13 18 29 18 80 9 | 25 39 44 47 29 32 31
R10E | 2614 31 16 31 25 25 --- 14 | 32 44 48 48 35 --- 35
R11E | 1577 31 15 18 39 20 --- 12 | 49 53 58 62 39 --- 48
R13E | 2678 12 11 18 28 15 --- 8 | 31 40 44 56 32 --- 34
R14E | 2964 30 16 21 27 20 --- 12 | 33 43 50 59 37 --- 38
R15E | 2736 37 13 28 40 25 --- 14 | 23 45 64 71 30 --- 37
R17 | 1711 30 17 19 15 30 --- 13 | 17 24 43 24 16 --- 19
R18 | 2132 22 8 13 24 23 --- 9 | 20 29 33 33 27 --- 23
R19 | 1817 15 11 27 29 19 --- 10 | 29 29 35 36 22 --- 25
R20 | 2205 38 12 33 34 36 --- 16 | 17 22 44 42 20 --- 17
R21 | 1270 24 15 44 36 17 --- 14 | 25 31 70 57 24 --- 31
R22 | 1186 21 11 34 27 26 --- 13 | 63 52 48 55 64 --- 53
R23 | 2100 17 7 31 29 17 272 10 | 40 38 47 39 29 84 34
R24 | 1693 15 6 19 45 16 --- 8 | 27 25 39 59 20 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2751 25 13 26 29 23 200 |T 40 45 54 56 40 58 41
WRMS | 2751 25 12 24 29 23 200 |NE 42 45 55 55 43 58 42
MEDI | 2100 22 12 21 27 20 80 |MD 28 38 44 48 29 32 31
Table 3.1584.6 GPS week: 1584 Day: 6 MJD: 55338
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1148 16 11 20 18 23 --- 10 | 18 22 32 21 33 --- 20
R02 | 1462 28 18 20 25 25 --- 13 | 39 52 48 59 45 --- 43
R03 | 2554 27 14 22 14 27 --- 12 | 34 39 37 32 44 --- 33
R04 | 4849 14 10 14 18 24 --- 9 | 148 147 154 157 141 --- 147
R05 | 4366 28 17 20 22 29 --- 13 | 77 80 76 78 76 --- 75
R07 | 3494 31 31 19 27 27 --- 16 | 19 31 22 30 31 --- 21
R08 | 2167 23 16 13 19 17 211 10 | 36 45 46 38 40 36 40
R10E | 2429 24 17 19 29 31 --- 13 | 53 77 77 73 49 --- 64
R11E | 1411 20 15 28 53 20 --- 12 | 75 79 96 96 78 --- 80
R13E | 1871 19 15 24 58 21 --- 11 | 57 60 78 93 58 --- 61
R14 | 3820 63 24 43 45 46 --- 25 | 91 116 126 133 86 --- 101
R15E | 3566 48 18 29 36 30 427 18 | 58 83 99 99 65 292 74
R17 | 1430 24 36 43 34 50 --- 22 | 32 52 48 29 31 --- 36
R18 | 1168 12 10 23 52 27 --- 10 | 37 40 44 76 50 --- 40
R19 | 947 17 12 18 35 17 --- 9 | 39 48 48 54 39 --- 42
R20 | 3082 31 11 32 39 29 --- 14 | 28 33 56 54 49 --- 35
R21 | 1027 15 11 24 27 19 --- 10 | 39 51 51 59 39 --- 44
R22 | 1856 32 11 26 30 36 --- 15 | 50 70 87 84 90 --- 71
R23 | 1277 10 11 13 34 24 404 8 | 37 43 39 53 40 77 39
R24 | 1532 24 11 18 29 22 --- 10 | 22 31 45 54 34 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2554 28 17 25 34 28 361 |T 49 59 65 68 55 135 54
WRMS | 2554 25 17 23 34 28 361 |NE 43 52 55 58 52 56 47
MEDI | 1856 24 14 20 29 25 404 |MD 39 51 48 59 45 77 42
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