[IGSREPORT-17483] Wk 1533 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 11 05:37:41 PDT 2009
******************************************************************************
IGS Electronic Report 11 Jun 05:38:03 PDT 2009 Message Number 17483
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1533 (May 24, 2009 - May 30, 2009)
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 2.1533.
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:
igl1533[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1533 in the SP3 format.
igl15337.sum Combination Report for GPS Week 1533.
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 | 234.5 ns
1 | 232.7 ns
2 | 229.8 ns
3 | 245.6 ns
4 | 234.1 ns
5 | 220.8 ns
6 | 232.9 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
3 | BKG | R23
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1533, 1a.1533).
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 2.1533.0-6)
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 3.1533.0-6).
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 1533 summary. (May 24, 2009 - May 30, 2009)
Table 1.1533.a GPS week : 1533 MJD: 54975.0-54981.0
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 96| 2 0 -20 16 -42 48 -.04 63 44 | 0 976 16971 21522
| 3 2 6 44 72 288 .15 | 0 14150
cod 235| -1 -1 2 15 13 68 -.11 26 19 | --- --- --- ---
| 1 1 2 20 25 78 .04 | --- ---
esx 142| 0 1 11 -25 69 43 .49 46 35 | 109573 869 6747 17260
| 2 2 4 55 70 93 .13 | 12500 4033
iac n/a| 0 0 -1 6 -51 -139 -.19 31 31 | -295021 6238 431868 436961
| 1 1 3 34 23 64 .07 | 659489 9710
mcc n/a| -4 1 55 -63 -117 1210 .68 272 272 | --- --- --- ---
| 13 11 20 204 189 853 1.38 | --- ---
Table 1.1533.b GPS week : 1533 MJD: 54975.0-54981.0
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
------+------------------------------------+------------------------------------------
R02 | 68 24 14 23 19 12 11 |
R03 | 46 22 17 31 19 16 17 |
R06 | 19 32 25 21 37 30 25 |
R07 | 11 12 61 --- --- --- 0 |
R08 | 78 53 23 13 20 17 15 |
R10 | 35 16 17 18 17 16 15 |
R11 | 22 19 22 21 22 24 19 |
R13 | 18 17 19 19 17 18 14 |
R14 | 22 15 16 19 16 21 14 |
R15 | 17 17 21 17 19 17 18 |
R17 | 16 19 20 20 23 23 14 |
R18 | 20 16 18 15 12 14 14 |
R19 | 16 14 13 14 13 13 14 |
R20 | 14 23 23 17 18 18 16 |
R21 | 15 12 16 15 14 14 16 |
R22 | 14 13 20 12 18 17 15 |
R23 | 95 70 97 39 52 31 35 |
R24 | 26 19 23 33 27 0 --- |
Table 1.1533.c GPS week : 1533 MJD: 54975.0-54981.0
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 1533 0 | 200 -153 379 848 -2522 -10370 84.1 4875 4875 | 234528 0
brd 1533 1 | -25 -25 328 -1298 -2133 -14900 88.0 7014 7014 | 232743 0
brd 1533 2 | -137 -5 343 -1746 1214 -19520 82.2 8277 8277 | 229836 0
brd 1533 3 | 82 88 523 -1445 1842 -15200 86.8 5863 5863 | 245628 0
brd 1533 4 | 39 -54 490 -1802 1700 -14370 92.8 5228 5228 | 234080 0
brd 1533 5 | -54 13 374 1373 729 -15730 93.0 4302 4302 | 220805 0
brd 1533 6 | 81 144 403 1391 1475 -15350 87.6 2824 2824 | 232861 0
-------------+------------------------------------------------------------+----------------
brd 1533 mean| 26 1 406 -382 329 -15062 87.8 5483 5483 | 232925 0
brd 1533 sdev| 109 96 73 1504 1853 2675 4.0 1788 1788 | 7322 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 2.1533.0 GPS week: 1533 Day: 0 MJD: 54975
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 96| -1 0 -23 62 -115 438 -.17 123 46 | 0 1799 4609 5133
cod 235| 0 0 7 26 31 59 -.08 39 20 | --- --- --- ---
esx 142| 0 5 5 -10 106 90 .60 53 36 | 97584 5972 7601 18946
iac n/a| 2 1 0 -28 -82 -229 -.23 38 38 | -999999 22738 999999 999999
mcc n/a| 0 -3 81 9 -76 692 1.15 103 103 | --- --- --- ---
Table 2.1533.1 GPS week: 1533 Day: 1 MJD: 54976
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 96| 4 -2 -26 -54 -147 172 -.22 76 43 | 0 1534 4859 5332
cod 235| -4 0 2 16 47 11 -.14 27 21 | --- --- --- ---
esx 142| -2 3 9 42 149 82 .62 34 30 | 111953 -621 8879 23497
iac n/a| 1 0 4 -38 -88 -180 -.23 29 29 | -999999 17631 999999 999999
mcc n/a| -9 -9 71 -97 -135 697 1.48 134 134 | --- --- --- ---
Table 2.1533.2 GPS week: 1533 Day: 2 MJD: 54977
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 96| 0 0 -19 41 -20 -92 -.01 53 52 | 0 165 6061 6663
cod 235| -1 -3 1 29 20 -25 -.11 24 19 | --- --- --- ---
esx 142| 2 0 19 -10 30 134 .30 65 40 | 103647 -1161 7602 15091
iac n/a| 0 2 -1 -11 -28 -43 -.12 35 35 | -999999 1915 999999 999999
mcc n/a| -2 11 22 -74 -150 744 -.83 311 311 | --- --- --- ---
Table 2.1533.3 GPS week: 1533 Day: 3 MJD: 54978
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 96| 0 2 -9 67 75 326 .18 46 38 | 0 21422 34527 43823
cod 235| 0 0 3 20 -31 -8 -.09 26 24 | --- --- --- ---
esx 142| 2 0 11 -112 46 -119 .41 43 33 | 131682 -4408 6131 16384
iac n/a| 1 0 -8 5 -39 -123 -.21 29 29 | 247936 -1536 6186 17909
mcc n/a| 2 -10 42 -403 91 597 -1.32 399 399 | --- --- --- ---
Table 2.1533.4 GPS week: 1533 Day: 4 MJD: 54979
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 96| 8 5 -16 24 -12 36 .14 52 45 | 0 2996 20408 26289
cod 235| 0 -1 0 -6 1 130 -.07 24 18 | --- --- --- ---
esx 142| -1 2 12 -12 107 36 .37 49 40 | 106916 5474 5913 12531
iac n/a| -1 3 -3 41 -41 -174 -.07 28 28 | 232300 894 5887 11845
mcc n/a| 17 20 51 -96 80 901 .14 296 296 | --- --- --- ---
Table 2.1533.5 GPS week: 1533 Day: 5 MJD: 54980
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 96| 4 2 -30 -18 -49 -140 -.03 57 49 | 0 -26547 27191 35519
cod 235| -2 -1 2 -18 7 147 -.18 23 18 | --- --- --- ---
esx 142| 3 0 8 14 107 -40 .57 36 30 | 96447 -2393 4515 19204
iac n/a| 0 0 -1 51 -40 -146 -.24 29 29 | 221855 185 4499 13618
mcc n/a| -20 9 51 -77 -154 2086 1.84 289 289 | --- --- --- ---
Table 2.1533.6 GPS week: 1533 Day: 6 MJD: 54981
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 96| 2 0 -21 -7 -27 -395 -.15 35 32 | 0 5468 21145 27898
cod 235| -3 0 1 39 16 162 -.10 21 16 | --- --- --- ---
esx 142| 0 2 13 -87 -59 122 .59 42 34 | 118785 3220 6590 15170
iac n/a| 2 0 -1 27 -36 -75 -.23 29 29 | 232753 1840 6513 15364
mcc n/a| -18 -6 70 294 -476 2756 2.33 374 374 | --- --- --- ---
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 3.1533.0 GPS week: 1533 Day: 0 MJD: 54975
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 5529 289 84 81 58 --- 68 | 511 230 232 325 --- 291
R03 | 2060 194 55 61 41 --- 46 | 405 242 228 324 --- 283
R06 | 3711 49 31 27 29 --- 18 | 163 226 222 205 --- 210
R07 |11040 21 16 22 17 --- 10 | 16 9999 61 12 --- 9999
R08 | 1429 303 99 111 86 --- 78 | 599 827 859 756 --- 781
R10E | 2155 152 33 42 36 --- 35 | 89 42 51 40 --- 40
R11E | 2323 68 14 38 40 102 21 | 44 28 46 45 43 31
R13E | 1082 36 26 31 34 --- 18 | 22 23 41 51 --- 26
R14E | 2023 34 24 55 36 --- 21 | 25 38 66 38 --- 32
R15E | 5843 43 19 32 28 103 16 | 23 27 42 40 44 23
R17 | 851 18 18 45 24 --- 15 | 51 50 85 47 --- 51
R18 | 594 38 20 50 30 --- 19 | 28 51 61 43 --- 42
R19 | 1200 39 24 36 17 --- 15 | 34 55 64 46 --- 45
R20M | 1398 44 19 25 20 --- 14 | 46 61 53 56 --- 53
R21M | 3055 39 14 39 22 --- 15 | 49 61 73 68 --- 58
R22M | 1637 21 11 31 30 --- 14 | 53 66 77 82 --- 68
XR23M | 9765 201 107 --- 132 --- 94 | 177 105 --- 106 --- 43
R24M |12864 49 19 80 28 --- 25 | 156 176 156 183 --- 172
------+------------------------------------+--------------------------------
RMS | 4874 123 39 53 38 102 |T 138 135 142 137 43 132
WRMS | 4874 46 20 36 38 102 |NE 225 240 226 219 --- 243
MEDI | 2060 43 20 39 30 102 |MD 49 61 66 51 43 51
Table 3.1533.1 GPS week: 1533 Day: 1 MJD: 54976
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |10161 91 25 34 29 --- 24 | 114 132 149 138 --- 131
R03 | 5631 81 19 29 35 --- 22 | 91 132 154 128 --- 128
R06 | 8480 128 30 47 31 --- 32 | 232 320 333 303 --- 306
R07 |11890 27 15 24 20 --- 12 | 17 9999 60 16 --- 9999
R08 | 3316 216 63 65 43 --- 52 | 595 530 553 564 --- 546
R10E | 1961 44 17 27 29 --- 16 | 25 37 42 37 --- 28
R11E | 2024 45 26 37 28 141 18 | 32 37 61 43 78 38
R13E | 809 25 22 35 30 --- 16 | 38 23 48 40 --- 28
R14E | 4724 38 20 19 28 --- 14 | 35 29 42 53 --- 33
R15E | 6462 34 21 39 25 126 16 | 26 22 50 44 80 29
R17 | 1032 41 33 31 33 --- 19 | 46 45 67 52 --- 45
R18 | 967 33 19 31 31 --- 16 | 21 35 64 25 --- 32
R19 | 923 42 13 29 21 --- 14 | 32 34 56 47 --- 39
R20 | 1186 74 29 33 34 --- 22 | 30 35 67 58 --- 44
R21 | 2736 35 17 19 17 --- 11 | 81 47 58 45 --- 50
R22 | 1318 34 11 25 22 --- 12 | 31 42 40 53 --- 40
XR23 |12417 183 91 --- 49 --- 69 | 120 86 --- 75 --- 58
R24 |19772 35 38 26 29 --- 18 | 210 258 259 233 --- 246
------+------------------------------------+--------------------------------
RMS | 7014 76 27 34 29 134 |T 98 108 123 108 79 107
WRMS | 7014 43 21 30 29 134 |NE 143 175 179 159 --- 175
MEDI | 2736 41 21 31 29 126 |MD 35 42 61 52 78 44
Table 3.1533.2 GPS week: 1533 Day: 2 MJD: 54977
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |11488 32 14 37 19 --- 14 | 250 201 215 238 --- 218
R03 | 4183 34 16 30 41 --- 17 | 256 227 220 240 --- 230
R06 | 4271 73 25 52 33 --- 25 | 166 220 249 213 --- 215
R07 |17186 103 55 211 48 --- 61 | 21 9999 183 13 --- 9999
R08 | 6571 64 14 59 32 342 23 | 359 342 395 365 63 359
R10E | 2725 18 23 49 29 --- 17 | 60 37 39 38 --- 29
R11E | 3179 44 26 41 47 401 22 | 39 30 49 62 109 33
R13E | 2137 38 20 50 34 --- 19 | 27 19 47 40 --- 20
R14E | 3300 35 19 28 31 --- 15 | 49 32 39 46 --- 30
R15E | 3557 62 16 32 40 115 21 | 35 26 51 40 87 27
R17 | 1721 18 24 33 51 --- 19 | 40 33 47 25 --- 25
R18 |11011 21 27 26 41 --- 17 | 29 41 48 44 --- 32
R19 | 1294 34 18 26 15 --- 13 | 36 53 61 35 --- 44
R20 | 1607 73 11 61 13 --- 23 | 47 46 91 53 --- 46
R21 | 1723 30 18 29 35 --- 16 | 43 48 73 86 --- 58
R22 | 1067 39 13 60 30 --- 19 | 35 54 114 69 --- 63
XR23 |14111 214 123 --- 91 --- 97 | 194 69 --- 65 --- 31
R24 |21913 79 26 30 26 --- 23 | 88 155 140 120 --- 127
------+------------------------------------+--------------------------------
RMS | 8277 53 24 65 35 311 |T 98 96 121 99 86 93
WRMS | 8277 52 19 40 35 311 |NE 144 159 177 146 63 160
MEDI | 3300 38 19 37 33 342 |MD 43 48 73 53 87 44
Table 3.1533.3 GPS week: 1533 Day: 3 MJD: 54978
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 5745 74 22 34 28 --- 22 | 135 181 183 179 --- 170
R03 | 2971 93 35 54 39 --- 31 | 106 206 218 163 --- 176
R06 | 7586 33 41 30 34 --- 20 | 185 251 241 217 --- 228
R08 | 4702 26 18 21 25 541 13 | 463 433 406 443 14 434
R10E | 3021 40 28 24 34 --- 18 | 26 46 50 42 --- 33
R11E | 1756 45 25 50 32 422 21 | 32 39 57 70 48 43
R13E | 2513 49 30 34 19 --- 19 | 55 27 49 28 --- 28
R14E | 2313 55 16 35 30 --- 19 | 23 50 72 74 --- 51
R15E | 2631 33 24 27 35 84 17 | 41 43 49 48 53 35
R17 | 2460 27 32 39 36 --- 19 | 40 44 48 24 --- 31
R18 | 2073 21 21 28 30 --- 14 | 21 33 56 41 --- 30
R19 | 2263 33 25 21 14 --- 13 | 51 57 44 30 --- 41
R20 | 1735 36 12 33 34 --- 16 | 29 37 43 41 --- 29
R21 | 1037 36 13 44 12 --- 15 | 29 54 83 49 --- 51
R22 | 957 27 14 18 23 --- 11 | 44 53 65 62 --- 54
XR23 | 3444 294 37 --- 40 --- 38 | 180 64 --- 41 --- 44
R24 |19422 46 32 107 29 --- 32 | 162 193 267 180 --- 197
------+------------------------------------+--------------------------------
RMS | 5863 46 26 43 29 399 |T 95 106 120 101 38 98
WRMS | 5863 38 24 33 29 399 |NE 143 172 170 156 14 158
MEDI | 2513 36 25 33 30 422 |MD 44 53 57 49 48 44
Table 3.1533.4 GPS week: 1533 Day: 4 MJD: 54979
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3149 60 19 44 23 --- 19 | 180 185 207 183 --- 184
R03 | 2006 50 30 25 27 --- 18 | 216 213 225 222 --- 216
R06 | 9642 115 32 99 38 --- 37 | 107 181 240 146 --- 164
R08 | 1918 34 12 62 32 239 19 | 183 222 256 199 15 214
R10E | 4098 44 25 39 20 --- 17 | 46 60 80 56 --- 56
R11E | 1091 48 19 68 28 451 21 | 32 41 83 64 42 47
R13E | 3671 35 24 39 28 --- 17 | 52 29 57 31 --- 29
R14E | 1464 44 13 43 22 --- 16 | 58 63 66 64 --- 58
R15E | 961 58 18 27 33 56 19 | 25 32 40 47 36 30
R17 | 1947 37 39 36 44 --- 23 | 27 55 53 30 --- 38
R18 | 1239 28 12 23 21 --- 11 | 31 39 41 51 --- 39
R19 | 2456 44 7 26 18 --- 13 | 29 28 47 39 --- 31
R20 | 2409 49 13 42 29 --- 17 | 30 32 57 33 --- 29
R21 | 1088 38 17 32 14 --- 13 | 38 53 51 42 --- 44
R22 | 1270 46 15 53 21 --- 18 | 27 41 78 39 --- 41
XR23 | 1831 132 31 --- 74 --- 51 | 97 86 --- 67 --- 69
R24 |16497 41 45 66 40 --- 27 | 113 121 145 103 --- 105
------+------------------------------------+--------------------------------
RMS | 5227 52 24 49 28 296 |T 75 87 107 83 31 82
WRMS | 5227 45 18 40 28 296 |NE 110 131 152 124 15 126
MEDI | 1947 44 19 39 28 239 |MD 46 55 66 56 36 47
Table 3.1533.5 GPS week: 1533 Day: 5 MJD: 54980
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1774 28 17 19 23 --- 12 | 134 167 160 164 --- 159
R03 | 4006 43 15 30 30 --- 16 | 149 193 198 169 --- 181
R06 |14290 112 28 50 36 --- 30 | 147 225 229 198 --- 206
R08 | 1936 46 30 17 24 204 16 | 391 379 386 396 16 386
R10E | 4786 65 14 17 16 --- 15 | 36 25 40 39 --- 27
R11E | 1518 64 28 49 34 447 23 | 49 76 82 88 32 72
R13E | 2517 30 24 46 25 --- 18 | 25 20 51 30 --- 21
R14E | 1534 59 27 39 28 --- 20 | 54 35 68 44 --- 35
R15E | 2607 51 19 29 26 99 16 | 28 41 51 41 28 35
R17 | 923 68 19 51 30 --- 22 | 21 48 82 47 --- 48
R18 | 949 40 7 22 29 --- 13 | 17 28 34 63 --- 34
R19 | 1487 22 11 20 33 --- 12 | 21 24 27 46 --- 25
R20 | 4104 46 21 20 38 --- 17 | 19 33 38 20 --- 22
R21 | 1568 48 14 24 17 --- 13 | 23 54 59 33 --- 43
R22 | 1474 52 18 32 21 --- 16 | 53 38 49 26 --- 33
R23 | 1652 75 46 63 38 --- 30 | 57 45 55 75 --- 47
XR24 | ---- --- --- --- 11 --- 0 | --- --- --- 88 --- 76
------+------------------------------------+--------------------------------
RMS | 4301 57 23 36 29 289 |T 76 89 100 92 25 85
WRMS | 4301 49 18 30 29 289 |NE 125 152 159 154 16 148
MEDI | 1652 48 19 29 28 204 |MD 36 41 55 47 28 43
Table 3.1533.6 GPS week: 1533 Day: 6 MJD: 54981
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2540 15 11 25 22 --- 10 | 124 149 177 143 --- 148
R03 | 3135 23 16 45 31 --- 16 | 136 167 206 170 --- 169
R06 | 7577 48 41 33 48 --- 25 | 95 148 150 118 --- 128
XR07 | ---- --- 9 --- --- --- 0 | --- 9999 --- --- --- 9999
R08 | 2640 30 22 29 21 210 14 | 272 270 267 278 21 271
R10E | 1422 36 15 29 24 --- 14 | 58 38 60 43 --- 41
R11E | 857 33 25 43 34 532 18 | 39 40 49 55 45 39
R13E | 1755 26 17 34 24 --- 14 | 39 32 43 34 --- 30
R14E | 1737 26 12 38 23 --- 13 | 41 31 59 43 --- 36
R15E | 2847 44 19 32 31 303 17 | 29 36 54 45 50 33
R17 | 816 36 20 24 14 --- 13 | 32 72 83 50 --- 60
R18 | 1220 24 13 33 27 --- 13 | 35 54 77 65 --- 55
R19 | 2446 22 12 44 17 --- 13 | 24 37 68 54 --- 41
R20 | 4215 35 7 44 27 --- 16 | 50 45 56 53 --- 44
R21 | 1265 35 15 41 20 --- 15 | 29 62 76 47 --- 53
R22 | 1114 32 27 19 20 --- 14 | 43 71 62 53 --- 57
R23 | 1105 65 34 100 55 --- 35 | 89 31 52 109 --- 56
------+------------------------------------+--------------------------------
RMS | 2824 35 21 42 29 374 |T 70 80 96 85 38 78
WRMS | 2824 32 16 34 29 374 |NE 102 128 146 125 21 124
MEDI | 1737 32 16 33 24 303 |MD 41 45 62 53 45 53
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