[IGSREPORT-16349] Wk 1482 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 19 05:44:28 PDT 2008
******************************************************************************
IGS Electronic Report 19 Jun 05:44:35 PDT 2008 Message Number 16349
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1482 (Jun 01, 2008 - Jun 07, 2008)
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 2.1482.
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:
igl1482[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1482 in the SP3 format.
igl14827.sum Combination Report for GPS Week 1482.
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 | 958.9 ns
1 | 880.0 ns
2 | 889.6 ns
3 | 894.4 ns
4 | 859.5 ns
5 | 949.8 ns
6 | 940.8 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 1.1482, 1a.1482).
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 2.1482.0-6)
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 3.1482.0-6).
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 1482 summary. (Jun 01, 2008 - Jun 07, 2008)
Table 1.1482.a GPS week : 1482 MJD: 54618.0-54624.0
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 67| 2 0 -3 18 -25 16 -.17 43 38 | 0 39 2977 3089
| 2 2 5 23 43 170 .09 | 0 190
cod 202| -2 0 5 3 12 32 -.17 34 32 | --- --- --- ---
| 2 3 3 21 25 73 .06 | --- ---
esx 119| -1 0 7 16 11 -2 .42 59 44 | 10835 3560 9780 21274
| 6 3 8 37 49 85 .17 | 38793 8634
iac n/a| 2 -1 -8 -31 -31 -59 .09 50 50 | 909482 1224 9003 16860
| 1 4 5 14 23 133 .18 | 38121 5120
mcc n/a| -60 -33 143 -215 300 1519 2.29 711 711 | --- --- --- ---
| 86 38 147 1762 1084 4875 2.53 | --- ---
Table 1.1482.b GPS week : 1482 MJD: 54618.0-54624.0
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 | --- --- --- --- 0 0 242 |
R04 | 32 19 20 17 23 24 16 |
R06 | 19 23 26 45 66 22 20 |
R07 | 25 25 32 31 39 26 33 |
R08 | 26 32 38 30 34 36 21 |
R09 | --- --- 0 0 0 0 0 |
R10 | 13 19 19 17 22 14 19 |
R11 | 37 16 27 43 30 19 16 |
R13 | 18 22 25 24 23 24 23 |
R14 | 19 19 20 27 25 18 16 |
R15 | 27 36 26 29 22 23 26 |
R17 | 19 22 30 25 51 46 41 |
R19 | 21 16 21 13 27 19 46 |
R20 | 14 26 21 16 20 19 24 |
R23 | 25 16 20 27 22 22 24 |
R24 | 23 18 19 23 28 16 21 |
Table 1.1482.c GPS week : 1482 MJD: 54618.0-54624.0
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 1482 0 | -67 56 417 -435 1580 -21010 92.3 4191 4191 | 958920 0
brd 1482 1 |-1426 5736 645 8730 -5657 8679 <<<< >>>>> >>>>> | 879978 0
brd 1482 2 | 64 142 684 -1012 2956 -17210 94.8 7535 7535 | 889644 0
brd 1482 3 | -56 -131 500 2445 -4982 -25470 99.4 6923 6923 | 894370 0
brd 1482 4 | 130 -61 494 854 -762 -14640 98.9 4861 4861 | 859496 0
brd 1482 5 | 59 7 455 354 320 -28270 92.2 6479 6479 | 949825 0
brd 1482 6 | -299 149 554 -130 -1435 -20180 95.6 5665 5665 | 940820 0
-------------+------------------------------------------------------------+----------------
brd 1482 mean| -228 842 535 1543 -1140 -16871 <<<< >>>>> >>>>> | 910436 0
brd 1482 sdev| 546 2160 98 3356 3206 12178 657.1 >>>>> >>>>> | 38812 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 2.1482.0 GPS week: 1482 Day: 0 MJD: 54618
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 67| 2 1 -2 -25 -2 -47 -.26 40 37 | 0 -367 2876 3018
cod 202| -6 -1 0 4 -9 65 -.14 26 27 | --- --- --- ---
esx 119| 2 -1 7 41 87 -84 .57 50 37 | 46389 7952 11731 19897
iac n/a| 2 4 -4 -30 -78 -49 .11 53 53 | 952513 5413 11655 15573
mcc n/a| -170 0 17 -95 1443 410 1.38 685 685 | --- --- --- ---
Table 2.1482.1 GPS week: 1482 Day: 1 MJD: 54619
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 67| 5 0 -9 10 38 380 -.13 39 37 | 0 163 3514 3653
cod 202| -3 -3 9 37 -32 -38 -.23 29 26 | --- --- --- ---
esx 119| 0 2 5 35 27 -123 .28 47 45 | -24872 17583 9645 19167
iac n/a| 1 0 -14 -42 -43 -251 .27 44 44 | 877723 5531 9885 18596
mcc n/a| -198 -88 188 1781 2132 2083 7.09 1055 1055 | --- --- --- ---
Table 2.1482.2 GPS week: 1482 Day: 2 MJD: 54620
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 67| 3 -1 -7 28 -66 -19 -.18 37 33 | 0 176 3777 3916
cod 202| -2 -3 3 -23 28 -30 -.13 27 29 | --- --- --- ---
esx 119| -1 3 13 25 -42 45 .17 62 55 | 2267 -7737 11221 23833
iac n/a| 4 0 -8 -44 -27 139 .36 58 58 | 896675 -8589 11112 19159
mcc n/a| -40 -88 438 -3943 -969 12150 4.32 1287 1287 | --- --- --- ---
Table 2.1482.3 GPS week: 1482 Day: 3 MJD: 54621
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 67| 0 1 -7 35 -57 -35 -.25 57 42 | 0 57 2937 3016
cod 202| -2 3 9 -6 19 -32 -.25 38 32 | --- --- --- ---
esx 119| 4 -2 0 -6 64 13 .34 40 37 | -2688 -4127 8011 20526
iac n/a| 0 -1 -6 -30 -11 38 .12 58 58 | 891036 -2685 7448 12933
mcc n/a| 3 -15 12 340 -245 -2199 1.37 204 204 | --- --- --- ---
Table 2.1482.4 GPS week: 1482 Day: 4 MJD: 54622
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 67| -2 1 6 19 -15 -159 -.00 64 49 | 0 161 2534 2593
cod 202| 0 2 8 0 12 151 -.16 51 46 | --- --- --- ---
esx 119| 0 -4 0 9 -29 130 .42 74 42 | -45292 4068 8749 17462
iac n/a| 2 0 -6 -30 -17 -34 .00 43 43 | 857620 2386 7328 15253
mcc n/a| 8 -12 58 122 68 -484 1.38 736 736 | --- --- --- ---
Table 2.1482.5 GPS week: 1482 Day: 5 MJD: 54623
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 67| 3 0 -4 46 2 -36 -.22 34 35 | 0 82 2646 2692
cod 202| -1 5 5 -9 37 92 -.19 34 31 | --- --- --- ---
esx 119| -1 -2 22 -52 -21 -30 .64 63 43 | 52545 -1121 10116 27640
iac n/a| 3 -7 -17 -41 -13 -56 -.07 45 45 | 951902 3385 9829 25707
mcc n/a| -12 -10 129 319 -172 -81 -.25 445 445 | --- --- --- ---
Table 2.1482.6 GPS week: 1482 Day: 6 MJD: 54624
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 67| 2 -4 0 16 -80 33 -.11 31 31 | 0 3 2561 2735
cod 202| 0 2 2 25 33 22 -.08 35 32 | --- --- --- ---
esx 119| -14 0 7 62 -6 29 .51 73 49 | 47498 8306 8992 20395
iac n/a| 4 -8 0 -2 -26 -202 -.15 49 49 | 938905 3133 5767 10804
mcc n/a| -11 -16 156 -33 -151 -1245 .76 565 565 | --- --- --- ---
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 3.1482.0 GPS week: 1482 Day: 0 MJD: 54618
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 4885 49 37 91 46 --- 32 | 56 61 111 59 --- 60
R06 | 2809 36 19 49 29 --- 18 | 394 412 361 393 --- 393
R07 | 3344 54 38 48 34 --- 25 | 46 54 48 56 --- 37
R08 | 4730 30 23 82 34 --- 25 | 109 115 145 108 --- 116
R10E | 1395 21 9 18 38 --- 12 | 28 25 34 35 --- 24
R11E | 2713 38 29 56 123 --- 37 | 38 23 61 71 --- 25
R13E | 2354 33 16 34 43 --- 17 | 46 42 49 43 --- 37
R14E | 1889 46 20 30 34 --- 18 | 35 30 39 36 --- 26
R15E | 1846 44 27 38 78 483 26 | 34 43 44 83 154 36
R17 |11558 45 19 38 27 --- 18 | 46 50 53 37 --- 34
R19 | 1437 25 28 38 56 --- 21 | 35 72 75 41 --- 50
R20 | 1623 15 22 25 35 --- 14 | 24 49 35 44 --- 33
R23 | 1398 40 33 61 42 --- 25 | 42 46 68 71 --- 43
R24 | 4295 54 24 45 41 839 23 | 85 107 114 98 170 95
------+------------------------------------+--------------------------------
RMS | 4190 40 26 50 53 684 |T 72 80 88 83 162 72
WRMS | 4190 37 27 37 53 684 |NE 93 107 112 100 170 95
MEDI | 2354 38 23 38 38 483 |MD 42 49 53 56 154 37
Table 3.1482.1 GPS week: 1482 Day: 1 MJD: 54619
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |>>>>> 45 24 25 30 --- 18 | 62 81 53 74 --- 65
R06 |>>>>> 42 37 41 37 --- 22 | 374 407 405 427 --- 402
R07 |>>>>> 51 37 35 48 --- 24 | 62 44 63 42 --- 39
R08 |>>>>> 47 21 99 37 --- 31 | 127 113 95 116 --- 108
R10E |>>>>> 37 18 37 39 --- 18 | 32 25 54 51 --- 30
R11E |>>>>> 29 18 37 26 --- 15 | 30 27 59 81 --- 32
R13E |>>>>> 35 28 22 62 --- 22 | 39 46 38 65 --- 31
R14E |>>>>> 39 24 29 40 --- 19 | 31 25 40 34 --- 20
R15E |>>>>> 63 50 44 90 902 36 | 34 49 41 98 157 36
R17 |>>>>> 37 23 55 36 --- 22 | 22 41 85 42 --- 37
R19 |>>>>> 25 23 32 29 --- 15 | 23 49 61 26 --- 33
R20 |>>>>> 29 35 71 39 --- 26 | 16 53 82 67 --- 36
R23 |>>>>> 21 18 38 30 --- 15 | 34 41 60 38 --- 36
R24 |>>>>> 26 29 32 36 1187 17 | 59 64 64 82 504 59
------+------------------------------------+--------------------------------
RMS |>>>>> 39 29 47 44 1054 |T 67 76 85 88 330 68
WRMS |>>>>> 37 26 45 44 1054 |NE 86 99 107 101 504 90
MEDI |>>>>> 37 24 37 37 902 |MD 34 46 60 65 157 36
Table 3.1482.2 GPS week: 1482 Day: 2 MJD: 54620
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2187 38 27 44 35 --- 20 | 51 38 66 46 --- 42
R06 | 4959 48 25 72 42 --- 26 | 349 376 381 392 --- 370
R07 | 3128 47 23 106 42 --- 31 | 43 29 131 60 --- 35
R08 | 7511 59 35 120 45 --- 37 | 58 50 74 50 --- 39
XR09E |13470 --- --- 9 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 2258 23 27 46 43 --- 19 | 28 22 45 40 --- 16
R11E | 3985 48 22 31 81 --- 26 | 36 26 31 63 --- 24
R13E |23993 25 23 59 72 --- 24 | 34 33 91 97 --- 42
R14E | 6025 28 23 35 55 --- 19 | 48 56 44 57 --- 43
R15E | 5272 36 27 50 75 1287 26 | 50 37 63 90 634 43
R17 | 4848 22 36 37 105 --- 30 | 31 57 48 66 --- 33
R19 | 1183 28 27 54 38 --- 20 | 26 51 59 60 --- 42
R20 | 1975 25 31 55 41 --- 21 | 24 58 83 32 --- 41
R23 | 1689 24 19 41 59 --- 19 | 32 37 50 53 --- 29
R24 | 2614 38 26 37 30 --- 18 | 114 164 166 148 --- 145
------+------------------------------------+--------------------------------
RMS | 7534 37 27 62 58 1287 |T 66 73 95 89 634 67
WRMS | 7534 33 29 55 58 1287 |NE 80 95 117 100 --- 86
MEDI | 3985 28 26 46 43 1287 |MD 36 38 63 60 634 41
Table 3.1482.3 GPS week: 1482 Day: 3 MJD: 54621
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 4608 25 15 29 43 --- 16 | 42 76 58 74 --- 58
R06 | 1425 135 52 52 53 --- 44 | 315 403 416 414 --- 387
R07 | 2314 30 52 59 65 --- 31 | 31 53 51 67 --- 31
R08 | 8264 69 46 40 51 --- 29 | 146 158 143 147 --- 142
XR09E |15974 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 2122 31 26 21 37 --- 16 | 40 41 39 31 --- 30
R11E | 4337 63 47 58 123 --- 43 | 29 29 93 101 --- 45
R13E |17312 44 47 38 33 --- 24 | 46 54 48 40 --- 35
R14E | 5002 56 31 42 58 --- 26 | 41 39 44 67 --- 33
R15E |13901 69 30 46 55 204 28 | 79 37 77 70 524 55
R17 | 2193 35 45 35 52 --- 24 | 36 85 76 64 --- 50
R19 | 1150 26 17 22 28 --- 13 | 23 43 52 39 --- 33
R20 | 1909 37 22 24 29 --- 16 | 25 48 63 43 --- 39
R23 | 2402 24 36 44 74 --- 27 | 55 37 52 95 --- 42
R24 | 4155 55 39 27 36 --- 23 | 130 121 124 124 --- 121
------+------------------------------------+--------------------------------
RMS | 6923 57 38 40 58 204 |T 74 87 95 98 524 78
WRMS | 6923 42 32 37 58 204 |NE 89 113 115 118 --- 100
MEDI | 4155 37 36 38 51 204 |MD 41 48 58 67 524 42
Table 3.1482.4 GPS week: 1482 Day: 4 MJD: 54622
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 10 --- --- --- 0 | --- 839 --- --- --- 836
R04 | 5179 47 35 26 41 --- 22 | 33 50 51 50 --- 40
R06 | 1587 178 80 125 51 --- 65 | 319 482 523 443 --- 434
R07 | 1965 53 89 83 40 --- 39 | 28 87 71 47 --- 46
R08 |11965 52 78 72 27 --- 34 | 88 102 119 92 --- 95
XR09E |17048 --- --- 10 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 1021 50 28 31 41 --- 22 | 46 33 36 39 --- 26
R11E | 2668 70 26 55 50 --- 30 | 27 50 70 46 --- 38
R13E | 7295 14 35 54 45 --- 23 | 51 44 71 68 --- 47
R14E | 1971 63 36 34 33 --- 24 | 37 42 48 40 --- 27
R15E | 7696 28 33 53 37 117 22 | 56 41 67 61 159 38
R17 | 2421 48 42 169 59 --- 51 | 41 70 200 54 --- 70
R19 | 1189 40 41 67 36 --- 26 | 21 34 76 39 --- 27
R20 | 1255 30 38 45 24 --- 20 | 16 65 51 50 --- 38
R23 | 1482 27 40 34 43 --- 21 | 31 35 39 57 --- 34
R24 | 4350 24 60 26 58 1035 27 | 143 155 154 148 894 144
------+------------------------------------+--------------------------------
RMS | 4861 64 51 74 43 736 |T 66 141 112 88 526 129
WRMS | 4861 49 46 42 43 736 |NE 80 191 142 108 894 176
MEDI | 2421 47 38 53 41 117 |MD 37 50 70 50 159 40
Table 3.1482.5 GPS week: 1482 Day: 5 MJD: 54623
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 8 --- --- --- 0 | --- 872 --- --- --- 878
R04 | 3210 39 45 46 35 --- 24 | 40 51 46 36 --- 30
R06 | 1654 40 30 50 34 --- 22 | 183 191 166 175 --- 175
R07 | 3217 23 52 60 43 --- 25 | 27 65 57 75 --- 47
R08 |13934 28 61 115 38 --- 36 | 162 166 161 161 --- 159
XR09E |21367 --- --- 16 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 1662 16 20 35 26 --- 13 | 19 24 44 38 --- 20
R11E | 4885 28 26 55 25 --- 19 | 31 33 60 63 --- 35
R13E |14776 34 26 56 51 --- 23 | 54 28 63 65 --- 37
R14E | 2091 32 26 26 40 --- 18 | 30 21 42 47 --- 21
R15E | 6106 32 25 47 55 155 22 | 32 30 77 67 160 39
R17 | 7591 60 41 132 87 --- 45 | 38 62 134 50 --- 38
R19 | 1483 34 23 43 28 --- 18 | 16 33 71 25 --- 25
R20 | 1976 32 23 34 42 --- 19 | 19 31 36 46 --- 16
R23 | 1493 30 22 57 48 --- 22 | 36 35 75 64 --- 38
R24 | 4183 21 23 29 39 611 16 | 146 145 161 151 335 147
------+------------------------------------+--------------------------------
RMS | 6478 34 34 63 45 445 |T 59 119 85 75 247 113
WRMS | 6478 35 31 43 45 445 |NE 74 165 100 87 335 155
MEDI | 3217 32 26 47 39 155 |MD 32 35 63 63 160 38
Table 3.1482.6 GPS week: 1482 Day: 6 MJD: 54624
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 190 --- 305 --- 241 | --- 591 --- 32 --- 600
R04 | 2986 20 21 32 41 --- 16 | 48 43 64 65 --- 48
R06 | 2110 36 29 41 36 --- 20 | 302 331 329 333 --- 323
R07 | 1948 46 70 65 37 --- 32 | 24 90 71 46 --- 47
R08 | 7698 37 30 35 40 --- 20 | 152 106 144 154 --- 135
XR09E |25407 --- --- 12 --- --- 0 | --- --- 9999 --- --- 9999
R10E | 1955 30 19 26 53 --- 19 | 36 26 28 37 --- 23
R11E |10439 25 17 43 24 --- 15 | 33 44 67 55 --- 42
R13E |11484 24 43 49 48 --- 23 | 34 55 54 47 --- 32
R14E | 3722 23 16 46 27 --- 15 | 37 30 29 28 --- 19
R15E | 5395 27 21 47 79 185 25 | 48 44 65 84 151 45
R17 | 7263 38 55 144 36 --- 40 | 37 76 177 23 --- 49
R19 | 2374 35 38 174 58 --- 45 | 22 57 143 68 --- 45
R20 | 1893 21 33 40 67 --- 23 | 41 41 58 106 --- 48
R23 | 1985 36 31 44 58 --- 24 | 36 45 45 78 --- 41
R24 | 4381 24 19 55 51 777 21 | 154 145 156 149 627 147
------+------------------------------------+--------------------------------
RMS | 5664 31 35 73 49 564 |T 71 114 102 87 389 109
WRMS | 5664 31 32 49 49 564 |NE 90 152 131 105 627 148
MEDI | 3722 27 30 44 48 185 |MD 37 55 65 65 151 47
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