[IGSREPORT-16936] Wk 1508 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 18 05:23:29 PST 2008
******************************************************************************
IGS Electronic Report 18 Dec 05:23:32 PST 2008 Message Number 16936
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1508 (Nov 30, 2008 - Dec 06, 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 2.1508.
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:
igl1508[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1508 in the SP3 format.
igl15087.sum Combination Report for GPS Week 1508.
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 | 428.8 ns
1 | 395.0 ns
2 | 386.4 ns
3 | 419.4 ns
4 | 413.4 ns
5 | 413.3 ns
6 | 412.3 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
----+--------+---------------
1 | BKG | R06
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 1.1508, 1a.1508).
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 2.1508.0-6)
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 3.1508.0-6).
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 1508 summary. (Nov 30, 2008 - Dec 06, 2008)
Table 1.1508.a GPS week : 1508 MJD: 54800.0-54806.0
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 88| 1 0 13 28 36 -120 -.05 40 33 | 0 16 2453 2511
| 1 2 3 32 32 145 .08 | 0 219
cod 243| -2 0 -3 -3 0 7 -.12 21 17 | --- --- --- ---
| 1 1 4 13 12 53 .06 | --- ---
esx 135| 0 -2 -10 -22 -47 89 .48 40 34 | 115800 -1244 6526 13240
| 2 1 5 42 43 49 .12 | 15177 6115
iac n/a| 3 0 1 2 3 54 -.15 37 37 | 411610 -2787 6501 13765
| 1 1 6 32 34 58 .11 | 16392 4282
mcc n/a| 0 0 10 73 -34 1830 .44 126 126 | --- --- --- ---
| 15 19 31 124 96 790 .35 | --- ---
Table 1.1508.b GPS week : 1508 MJD: 54800.0-54806.0
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
------+------------------------------------+------------------------------------------
R04 | 18 23 18 10 14 15 14 |
R06 | 25 39 29 15 24 22 21 |
R07 | 11 13 10 12 15 12 20 |
R10 | 25 25 14 16 18 18 20 |
R11 | 21 22 23 26 21 22 17 |
R13 | 25 27 19 16 26 21 22 |
R14 | 19 22 17 23 18 19 22 |
R15 | 18 17 18 17 21 13 14 |
R17 | 15 13 13 16 16 16 18 |
R18 | 20 20 13 10 10 11 11 |
R19 | 10 14 15 12 12 13 11 |
R20 | 11 13 20 14 17 17 17 |
R21 | 14 12 14 14 16 13 17 |
R22 | 17 20 18 11 16 24 14 |
R23 | 30 18 21 26 20 18 29 |
R24 | 13 17 22 30 17 19 17 |
Table 1.1508.c GPS week : 1508 MJD: 54800.0-54806.0
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 1508 0 | 35 112 -37 -363 377 -15140 91.8 4158 4158 | 428765 0
brd 1508 1 | -42 125 -42 -139 1248 -9100 93.8 5372 5372 | 395038 0
brd 1508 2 | -114 -95 107 250 1746 -4588 92.9 5935 5935 | 386355 0
brd 1508 3 | -21 100 -333 -696 1683 -6406 97.3 6562 6562 | 419410 0
brd 1508 4 | 94 17 -34 882 4472 -8483 94.1 6446 6446 | 413426 0
brd 1508 5 | -50 -110 -62 1122 1133 -8720 91.3 4268 4268 | 413273 0
brd 1508 6 | 65 -87 -133 -838 -329 -14990 91.1 4070 4070 | 412278 0
-------------+------------------------------------------------------------+----------------
brd 1508 mean| -4 8 -76 31 1475 -9632 93.2 5258 5258 | 409792 0
brd 1508 sdev| 73 105 133 756 1512 4027 2.2 1094 1094 | 14439 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 2.1508.0 GPS week: 1508 Day: 0 MJD: 54800
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 88| 3 3 7 41 4 -93 -.12 37 34 | 0 -98 2230 2296
cod 243| -2 0 -9 -13 1 -38 -.13 26 21 | --- --- --- ---
esx 135| 1 -2 -7 -9 -51 151 .35 38 31 | 136123 -5294 8770 21267
iac n/a| 1 1 4 -19 38 -9 -.09 30 30 | 436206 -5864 8788 22226
mcc n/a| -1 16 -19 -159 30 633 .09 65 65 | --- --- --- ---
Table 2.1508.1 GPS week: 1508 Day: 1 MJD: 54801
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 88| 1 -3 15 81 31 -303 -.12 82 41 | 0 472 2787 2757
cod 243| -3 0 -3 -14 5 76 -.05 21 16 | --- --- --- ---
esx 135| 0 -1 -9 -101 5 107 .36 41 33 | 99099 4659 5743 10659
iac n/a| 2 0 -3 0 -18 59 -.02 45 45 | 393562 2821 5792 11447
mcc n/a| -2 3 -20 117 -136 2079 .42 137 137 | --- --- --- ---
Table 2.1508.2 GPS week: 1508 Day: 2 MJD: 54802
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 88| 1 -1 12 9 -7 151 -.07 35 31 | 0 76 2774 2844
cod 243| -2 -1 -4 1 7 -78 -.14 18 15 | --- --- --- ---
esx 135| 1 -3 -12 -45 -18 57 .42 45 38 | 96602 -1664 6342 15267
iac n/a| 4 0 9 48 -10 -24 -.07 37 37 | 388560 -4954 6238 15767
mcc n/a| 3 -4 -6 89 -15 2199 .57 136 136 | --- --- --- ---
Table 2.1508.3 GPS week: 1508 Day: 3 MJD: 54803
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 88| 1 -1 12 25 31 -242 -.07 34 32 | 0 31 2297 2395
cod 243| -4 0 -6 -14 16 17 -.06 18 15 | --- --- --- ---
esx 135| 1 -4 0 -32 -7 137 .44 38 37 | 127692 -8423 6379 10280
iac n/a| 3 -1 4 31 -51 138 -.12 37 37 | 422914 -5942 6395 11826
mcc n/a| -8 11 11 60 123 2575 .56 111 111 | --- --- --- ---
Table 2.1508.4 GPS week: 1508 Day: 4 MJD: 54804
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 88| 0 0 14 47 87 -79 .10 30 28 | 0 -108 2411 2502
cod 243| -1 -2 1 -8 -24 5 -.21 24 19 | --- --- --- ---
esx 135| 0 -3 -7 8 -117 69 .57 37 34 | 121918 -158 6207 10282
iac n/a| 1 1 -7 15 27 106 -.26 34 34 | 411949 530 6220 10734
mcc n/a| -8 21 22 5 -78 2618 .27 88 88 | --- --- --- ---
Table 2.1508.5 GPS week: 1508 Day: 5 MJD: 54805
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 88| 0 0 13 -18 52 -165 -.00 30 28 | 0 -74 2501 2558
cod 243| 0 1 2 20 0 61 -.19 20 19 | --- --- --- ---
esx 135| -4 0 -18 0 -69 98 .70 36 33 | 122945 -6314 6297 13046
iac n/a| 2 0 6 -46 -5 68 -.31 39 39 | 416346 -7708 6265 11715
mcc n/a| -17 -24 68 197 -151 858 1.09 172 172 | --- --- --- ---
Table 2.1508.6 GPS week: 1508 Day: 6 MJD: 54806
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 88| 2 -2 20 10 55 -111 -.04 36 34 | 0 -185 2171 2229
cod 243| 0 3 -2 4 -3 11 -.08 18 16 | --- --- --- ---
esx 135| -2 0 -13 24 -75 7 .53 42 37 | 106225 8481 5950 11881
iac n/a| 6 0 -3 -13 42 40 -.16 38 38 | 411736 1602 5814 12643
mcc n/a| 31 -27 20 202 -16 1849 .09 171 171 | --- --- --- ---
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 3.1508.0 GPS week: 1508 Day: 0 MJD: 54800
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1574 30 30 39 22 --- 17 | 27 37 46 32 --- 31
R06 | 9316 52 38 36 44 --- 24 | 277 328 357 350 --- 341
R07 | 1801 12 15 22 21 --- 10 | 23 31 31 41 --- 29
R10E | 1803 58 23 26 54 --- 24 | 33 33 43 61 --- 35
R11E | 1682 42 22 38 40 85 20 | 34 36 48 54 35 34
R13E | 974 33 40 51 43 --- 24 | 30 42 47 49 --- 31
R14E | 4666 38 23 30 37 --- 18 | 49 41 51 69 --- 48
R15E | 1509 28 31 29 33 36 17 | 32 39 30 30 123 27
R17 | 1630 35 22 23 24 --- 15 | 71 61 54 52 --- 56
R18 | 1986 42 24 45 24 --- 19 | 56 61 75 65 --- 55
R19 | 1458 19 14 19 13 --- 9 | 37 58 53 44 --- 48
R20 | 888 21 14 25 14 --- 10 | 33 43 48 48 --- 40
R21 | 629 27 23 26 18 --- 13 | 42 64 46 43 --- 48
R22 | 1203 49 8 33 19 --- 16 | 51 63 77 69 --- 62
R23 | 2122 37 49 87 19 --- 30 | 19 38 112 45 --- 36
R24 |11708 30 13 28 17 --- 12 | 107 109 98 105 --- 105
------+------------------------------------+--------------------------------
RMS | 4157 37 26 38 30 65 |T 57 67 76 72 79 64
WRMS | 4157 34 21 31 30 65 |NE 67 81 90 81 --- 77
MEDI | 1630 33 23 29 22 36 |MD 34 42 48 49 35 40
Table 3.1508.1 GPS week: 1508 Day: 1 MJD: 54801
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2545 57 22 51 19 --- 22 | 33 65 94 55 --- 56
R06 |19501 302 32 77 65 --- 39 | 103 251 285 217 --- 254
R07 | 2031 21 14 16 36 --- 12 | 18 25 33 37 --- 21
R10E | 957 40 30 40 65 --- 24 | 24 59 58 50 --- 38
R11E | 1925 34 24 36 64 125 22 | 27 37 50 77 30 33
R13E | 1652 50 33 52 63 --- 27 | 26 67 79 47 --- 41
R14E | 2205 34 22 45 57 --- 22 | 22 35 55 61 --- 33
R15E | 2491 24 23 33 40 149 17 | 34 40 43 47 49 29
R17 | 3418 26 14 28 18 --- 12 | 64 50 45 43 --- 48
R18 | 2101 32 17 52 38 --- 19 | 31 30 63 60 --- 39
R19 | 903 22 19 35 24 --- 14 | 29 44 34 48 --- 33
R20 | 914 27 9 17 37 --- 13 | 18 27 33 52 --- 25
R21 | 1427 29 13 21 16 --- 11 | 22 48 46 42 --- 38
R22 | 2286 38 11 29 61 --- 20 | 30 43 42 95 --- 44
R23 | 1853 42 19 36 29 --- 18 | 16 31 24 34 --- 12
R24 | 4903 19 19 41 37 --- 16 | 117 133 145 113 --- 127
------+------------------------------------+--------------------------------
RMS | 5372 82 21 41 45 137 |T 38 61 70 67 39 54
WRMS | 5372 41 16 33 45 137 |NE 43 67 76 72 --- 63
MEDI | 2031 32 19 36 37 125 |MD 27 43 46 50 30 38
Table 3.1508.2 GPS week: 1508 Day: 2 MJD: 54802
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3396 30 23 53 24 --- 18 | 43 62 79 45 --- 49
R06 |20884 64 27 81 39 --- 28 | 226 221 260 260 --- 226
R07 | 1951 22 8 21 21 --- 10 | 27 25 33 38 --- 24
R10E | 1941 26 16 29 30 --- 14 | 33 29 37 41 --- 23
R11E | 1466 24 29 44 62 150 23 | 28 33 41 63 30 25
R13E | 2100 25 17 60 35 --- 19 | 29 27 47 40 --- 19
R14E | 4228 27 15 50 32 --- 17 | 37 50 53 85 --- 50
R15E | 3226 38 11 56 27 120 18 | 34 33 59 45 63 34
R17 | 2031 12 17 39 18 --- 12 | 49 47 72 37 --- 46
R18 | 1881 26 12 35 22 --- 13 | 42 42 66 53 --- 46
R19 | 718 17 21 38 28 --- 14 | 49 58 36 35 --- 44
R20 | 992 33 17 24 60 --- 20 | 24 31 42 76 --- 33
R21 | 1749 30 15 41 16 --- 14 | 35 46 42 40 --- 35
R22 | 3388 39 13 45 35 --- 18 | 55 53 91 84 --- 63
R23 | 1685 47 20 36 48 --- 21 | 41 30 55 52 --- 34
R24 | 6843 56 16 36 47 --- 21 | 56 75 88 63 --- 63
------+------------------------------------+--------------------------------
RMS | 5934 35 18 45 37 136 |T 50 53 68 66 46 50
WRMS | 5934 31 15 38 37 136 |NE 58 62 78 71 --- 60
MEDI | 1951 27 16 39 30 120 |MD 37 42 53 45 30 35
Table 3.1508.3 GPS week: 1508 Day: 3 MJD: 54803
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2811 14 14 19 24 --- 10 | 66 78 63 83 --- 72
R06 |18573 30 10 38 28 --- 14 | 191 174 210 186 --- 181
R07 | 1702 15 15 21 31 --- 11 | 34 29 34 34 --- 27
R10E | 3160 32 16 30 34 --- 15 | 44 48 62 47 --- 43
R11E | 2993 38 25 67 59 141 26 | 39 39 83 58 34 41
R13E | 3318 30 17 26 40 --- 16 | 12 37 48 57 --- 29
R14E | 2047 49 21 50 45 --- 22 | 40 72 86 84 --- 64
R15E | 4592 28 16 47 32 70 17 | 33 33 45 45 75 30
R17 | 1023 23 19 38 31 --- 15 | 30 53 33 55 --- 40
R18 | 3186 16 9 27 21 --- 10 | 59 49 49 53 --- 49
R19 | 699 20 18 18 23 --- 11 | 44 65 46 42 --- 50
R20 | 1067 16 16 41 20 --- 13 | 29 38 49 51 --- 37
R21 | 3685 18 16 42 20 --- 14 | 44 47 48 26 --- 35
R22 | 5260 23 9 28 18 --- 10 | 44 64 71 57 --- 57
R23 | 816 60 13 25 71 --- 25 | 24 36 57 87 --- 39
R24 |14939 69 36 58 50 --- 29 | 143 157 145 131 --- 138
------+------------------------------------+--------------------------------
RMS | 6561 34 18 38 37 111 |T 54 63 70 68 54 58
WRMS | 6561 32 15 37 37 111 |NE 64 71 73 73 --- 65
MEDI | 2993 23 16 30 31 70 |MD 40 48 49 55 34 41
Table 3.1508.4 GPS week: 1508 Day: 4 MJD: 54804
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1033 22 20 31 27 --- 14 | 47 57 56 53 --- 49
R06 |19145 58 35 32 36 --- 24 | 131 137 146 137 --- 131
R07 | 2098 21 17 28 37 --- 15 | 18 35 34 36 --- 25
R10E | 4043 26 20 35 43 --- 17 | 33 36 44 45 --- 29
R11E | 2390 26 28 31 54 110 20 | 29 26 38 48 32 25
R13E | 1650 39 24 69 42 --- 25 | 29 32 88 50 --- 36
R14E | 1310 29 31 37 29 --- 18 | 25 50 60 51 --- 38
R15E | 4548 50 19 48 22 57 21 | 24 20 47 29 86 22
R17 | 1013 16 26 34 31 --- 15 | 31 41 43 54 --- 37
R18 | 2932 18 10 20 21 --- 9 | 36 48 56 55 --- 47
R19 | 886 16 12 31 21 --- 11 | 50 46 84 50 --- 54
R20 | 1135 29 29 31 28 --- 17 | 20 50 58 47 --- 41
R21 | 3127 18 20 40 32 --- 16 | 45 42 79 40 --- 45
R22 | 4527 20 33 23 28 --- 15 | 44 61 42 63 --- 47
R23 | 1073 31 15 48 40 --- 19 | 29 30 64 23 --- 29
R24 |14227 34 21 29 29 --- 16 | 52 53 58 72 --- 51
------+------------------------------------+--------------------------------
RMS | 6445 30 24 37 34 88 |T 40 47 62 53 59 44
WRMS | 6445 28 19 34 34 88 |NE 45 54 65 57 --- 50
MEDI | 2098 26 20 31 29 57 |MD 31 42 56 50 32 38
Table 3.1508.5 GPS week: 1508 Day: 5 MJD: 54805
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2101 24 12 37 33 --- 15 | 31 41 63 30 --- 36
R06 |11601 48 18 43 46 --- 22 | 139 151 162 151 --- 146
R07 | 3196 24 16 21 25 --- 12 | 16 23 29 34 --- 19
R10E | 6082 34 15 33 48 --- 18 | 18 25 34 43 --- 20
R11E | 1418 27 32 32 56 214 21 | 25 26 35 59 138 25
R13E | 964 23 25 35 61 --- 20 | 18 24 40 51 --- 18
R14E | 1279 34 22 36 40 --- 18 | 28 48 56 61 --- 40
R15E | 1655 28 20 22 20 115 13 | 22 26 44 33 85 23
R17 | 719 26 20 27 42 --- 16 | 23 37 46 18 --- 28
R18 | 3302 15 15 28 14 --- 11 | 36 44 57 34 --- 41
R19 | 1034 17 21 22 28 --- 12 | 20 38 47 17 --- 29
R20 | 619 21 21 31 46 --- 17 | 52 45 75 23 --- 45
R21 | 3346 24 15 31 22 --- 13 | 39 43 56 49 --- 42
R22 | 3114 21 16 76 43 --- 23 | 39 43 90 22 --- 44
R23 | 1013 37 23 39 29 --- 18 | 21 30 45 32 --- 20
R24 | 7945 48 17 36 30 --- 19 | 41 37 57 37 --- 32
------+------------------------------------+--------------------------------
RMS | 4268 30 20 36 39 172 |T 35 42 58 43 111 38
WRMS | 4268 28 19 33 39 172 |NE 41 48 66 40 --- 43
MEDI | 1655 24 18 32 33 115 |MD 25 37 47 34 85 29
Table 3.1508.6 GPS week: 1508 Day: 6 MJD: 54806
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1538 33 15 33 22 --- 14 | 30 35 40 30 --- 30
R06 |13275 51 13 49 38 --- 21 | 124 113 114 129 --- 114
R07 | 2907 34 14 58 35 --- 19 | 25 33 41 36 --- 27
R10E | 5289 42 14 50 36 --- 19 | 34 39 54 53 --- 32
R11E | 3545 16 15 41 46 163 17 | 31 44 53 47 97 36
R13E | 763 37 25 50 49 --- 22 | 35 47 82 42 --- 42
R14E | 2086 35 28 60 30 --- 21 | 34 41 69 53 --- 39
R15E | 1553 22 14 38 25 178 13 | 33 26 47 36 62 29
R17 | 659 26 16 38 46 --- 17 | 41 48 59 55 --- 47
R18 | 1405 17 8 27 25 --- 10 | 39 45 55 41 --- 43
R19 | 536 18 15 28 18 --- 11 | 41 63 51 56 --- 53
R20 | 1372 40 14 16 45 --- 16 | 31 51 53 59 --- 46
R21 | 1397 19 19 33 47 --- 16 | 47 56 75 50 --- 54
R22 | 2304 19 21 27 33 --- 14 | 50 71 76 60 --- 63
R23 | 677 68 23 60 63 --- 29 | 40 28 65 81 --- 30
R24 | 4215 48 21 26 21 --- 17 | 53 71 68 55 --- 57
------+------------------------------------+--------------------------------
RMS | 4069 36 18 42 38 171 |T 43 50 62 55 79 46
WRMS | 4069 34 16 37 38 171 |NE 47 55 63 59 --- 51
MEDI | 1538 33 15 38 35 163 |MD 35 45 55 53 62 42
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