[IGSREPORT-16807] Wk 1502 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Nov 6 06:48:13 PST 2008
******************************************************************************
IGS Electronic Report 06 Nov 06:48:16 PST 2008 Message Number 16807
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1502 (Oct 19, 2008 - Oct 25, 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 2.1502.
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:
igl1502[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1502 in the SP3 format.
igl15027.sum Combination Report for GPS Week 1502.
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 | 505.0 ns
1 | 508.2 ns
2 | 495.1 ns
3 | 540.9 ns
4 | 482.3 ns
5 | 548.0 ns
6 | 550.4 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 1.1502, 1a.1502).
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 2.1502.0-6)
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 3.1502.0-6).
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 1502 summary. (Oct 19, 2008 - Oct 25, 2008)
Table 1.1502.a GPS week : 1502 MJD: 54758.0-54764.0
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 64| 0 -1 2 -9 1 -102 -.08 33 29 | 0 -38 2332 2432
| 1 2 4 41 58 162 .08 | 0 265
cod 240| -3 1 5 7 -16 2 -.12 21 19 | --- --- --- ---
| 1 0 2 14 48 66 .04 | --- ---
esx 124| 2 0 3 45 30 118 .43 31 27 | 132392 809 6868 20676
| 2 2 4 32 33 90 .11 | 27522 7056
iac n/a| 1 -1 -13 -28 0 -62 -.09 26 26 | 520270 652 5915 14142
| 2 2 4 20 41 66 .05 | 28226 3984
mcc n/a| -3 7 27 -39 -84 344 -.37 217 217 | --- --- --- ---
| 16 12 12 186 190 758 .32 | --- ---
Table 1.1502.b GPS week : 1502 MJD: 54758.0-54764.0
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 | 21 22 18 24 13 13 14 |
R06 | 20 18 20 20 22 19 17 |
R07 | 10 14 15 14 14 11 10 |
R09 | --- --- --- --- 0 0 0 |
R10 | 14 14 15 19 13 14 12 |
R11 | 10 13 15 18 21 14 14 |
R13 | 11 13 12 24 16 14 16 |
R14 | 13 9 10 13 13 12 10 |
R15 | 18 14 13 19 16 14 17 |
R17 | 14 18 16 15 16 13 15 |
R18 | 0 103 53 44 53 27 33 |
R19 | 11 17 11 18 14 11 10 |
R20 | 13 15 16 8 12 19 15 |
R23 | 18 12 22 26 23 22 19 |
R24 | 15 16 17 17 14 20 20 |
Table 1.1502.c GPS week : 1502 MJD: 54758.0-54764.0
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 1502 0 | 85 103 164 2028 1575 -20870 93.5 3688 3688 | 505026 0
brd 1502 1 | 39 -34 226 1988 1490 -15560 88.5 4162 4162 | 508198 0
brd 1502 2 | -6 35 -68 -496 2096 -17070 94.5 3419 3419 | 495087 0
brd 1502 3 | 199 -7 214 -1295 997 -14440 93.5 3217 3217 | 540858 0
brd 1502 4 | 9 -69 236 -552 -1089 -3262 94.5 3880 3880 | 482253 0
brd 1502 5 | 74 112 61 -2954 2309 -5909 92.1 5364 5364 | 547960 0
brd 1502 6 | 112 -13 -22 1408 2885 -12280 94.7 3389 3389 | 550350 0
-------------+------------------------------------------------------------+----------------
brd 1502 mean| 73 17 115 17 1466 -12770 93.0 3874 3874 | 518533 0
brd 1502 sdev| 69 68 125 1870 1283 6223 2.2 731 731 | 27482 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 2.1502.0 GPS week: 1502 Day: 0 MJD: 54758
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 64| 0 0 3 28 11 49 -.16 28 25 | 0 185 2205 2307
cod 240| -1 0 1 -10 51 4 -.14 22 18 | --- --- --- ---
esx 124| 0 -2 3 41 22 39 .39 25 23 | 120179 11167 5772 15599
iac n/a| 3 0 -12 -26 -76 -138 -.10 26 26 | 502958 5385 5764 10497
mcc n/a| -1 -11 19 -81 -169 475 -.25 212 212 | --- --- --- ---
Table 2.1502.1 GPS week: 1502 Day: 1 MJD: 54759
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 64| 0 -1 10 -47 -2 -206 -.10 31 31 | 0 -276 2327 2418
cod 240| -2 0 4 16 7 61 -.13 18 18 | --- --- --- ---
esx 124| 0 -4 2 81 33 167 .40 31 28 | 130070 3360 5475 18058
iac n/a| 0 2 -18 -60 -13 -105 -.05 29 29 | 509324 -1402 5443 13693
mcc n/a| 24 2 39 -8 -288 373 -.24 88 88 | --- --- --- ---
Table 2.1502.2 GPS week: 1502 Day: 2 MJD: 54760
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 64| -1 -1 1 -17 -2 -40 -.09 31 30 | 0 208 2133 2208
cod 240| -2 1 8 14 -44 -77 -.13 22 23 | --- --- --- ---
esx 124| 0 0 1 43 22 213 .34 27 23 | 121670 1344 5128 18455
iac n/a| 0 -4 -14 -46 52 -108 -.01 28 28 | 498171 2510 5100 15930
mcc n/a| 0 11 42 -23 74 -98 -.24 209 209 | --- --- --- ---
Table 2.1502.3 GPS week: 1502 Day: 3 MJD: 54761
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 64| 0 -3 1 49 -22 17 .07 45 34 | 0 -200 2506 2617
cod 240| -3 1 7 -12 -42 -50 -.14 24 20 | --- --- --- ---
esx 124| 4 2 0 2 60 119 .33 35 36 | 166314 -8723 6613 14221
iac n/a| 0 0 -9 -13 27 -71 -.18 27 27 | 542954 -1512 6627 13131
mcc n/a| -24 12 21 300 -145 1696 -.46 411 411 | --- --- --- ---
Table 2.1502.4 GPS week: 1502 Day: 4 MJD: 54762
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 64| -1 3 2 -58 -46 50 -.05 31 29 | 0 293 2226 2365
cod 240| -5 1 4 8 23 10 -.05 22 20 | --- --- --- ---
esx 124| 1 0 5 58 -15 -44 .36 30 24 | 85654 2816 11736 35258
iac n/a| 1 -2 -19 -4 0 -32 -.13 30 30 | 484076 4389 6693 17871
mcc n/a| -23 25 10 -81 54 774 -.68 293 293 | --- --- --- ---
Table 2.1502.5 GPS week: 1502 Day: 5 MJD: 54763
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 64| -2 0 -1 -39 -52 -359 -.14 31 27 | 0 -380 2662 2726
cod 240| -2 2 3 6 -17 110 -.16 19 18 | --- --- --- ---
esx 124| 4 2 11 84 84 176 .63 35 27 | 141047 3865 7165 25567
iac n/a| 0 -3 -10 -12 -18 -41 -.08 23 23 | 550147 1337 6020 15861
mcc n/a| -4 -2 24 -338 -302 -629 -.86 138 138 | --- --- --- ---
Table 2.1502.6 GPS week: 1502 Day: 6 MJD: 54764
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 64| 0 -4 -1 15 123 -231 -.10 36 30 | 0 -100 2271 2383
cod 240| -5 1 6 29 -91 -43 -.13 20 17 | --- --- --- ---
esx 124| 4 2 0 6 6 158 .53 33 28 | 161810 -8161 6191 17578
iac n/a| 4 -1 -7 -32 25 60 -.08 19 19 | 554260 -6137 5760 12017
mcc n/a| 4 12 37 -41 186 -179 .11 165 165 | --- --- --- ---
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 3.1502.0 GPS week: 1502 Day: 0 MJD: 54758
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1399 31 46 28 35 --- 21 | 36 67 55 28 --- 40
R06 | 7381 51 17 33 35 --- 20 | 86 110 107 85 --- 97
R07 | 4378 16 10 21 22 --- 10 | 22 26 33 33 --- 24
R10 | 3066 27 9 25 32 --- 14 | 63 55 59 70 --- 57
R11 | 1905 16 11 19 18 44 9 | 58 72 74 71 59 68
R13 | 4716 25 19 11 15 --- 10 | 78 78 80 76 --- 76
R14 | 1661 21 12 27 24 --- 12 | 25 26 37 32 --- 26
R15 | 1449 26 28 43 17 58 17 | 66 71 67 70 50 65
R17 | 2940 22 18 25 31 --- 14 | 53 56 65 50 --- 54
XR18 | ---- --- 4 --- --- --- 0 | --- 184 --- --- --- 182
R19 | 1037 24 15 18 20 --- 11 | 38 34 47 36 --- 36
R20 | 2885 18 24 19 26 --- 13 | 21 16 22 40 --- 18
R23 | 1182 39 28 30 29 --- 18 | 84 89 99 109 --- 91
R24 | 6450 33 27 16 22 360 14 | 244 236 224 238 287 234
------+------------------------------------+--------------------------------
RMS | 3688 28 22 25 26 212 |T 67 80 74 72 132 76
WRMS | 3688 25 18 23 26 212 |NE 67 80 74 72 132 76
MEDI | 2885 25 17 25 24 58 |MD 58 67 65 70 59 57
Table 3.1502.1 GPS week: 1502 Day: 1 MJD: 54759
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 761 51 31 29 45 --- 22 | 41 49 50 20 --- 35
R06 |10509 45 21 37 23 --- 18 | 97 98 114 102 --- 100
R07 | 1627 31 11 28 27 --- 13 | 11 21 40 38 --- 23
R10 | 1995 33 10 26 27 --- 13 | 55 53 61 61 --- 54
R11 | 1043 20 13 37 21 77 13 | 56 76 89 86 62 74
R13 | 4704 21 12 28 27 --- 12 | 90 103 91 94 --- 93
R14 | 3843 19 10 15 18 --- 8 | 23 23 29 24 --- 21
R15 | 5172 29 14 35 22 46 14 | 54 81 84 79 50 74
R17 | 1620 20 31 21 40 --- 17 | 35 60 40 44 --- 42
XR18 |23928 146 71 --- --- --- 103 | 136 115 --- --- --- 112
R19 | 797 42 16 33 26 --- 16 | 28 33 48 26 --- 27
R20 | 1438 21 15 39 30 --- 15 | 43 35 44 34 --- 29
R23 | 2474 14 16 22 28 --- 11 | 36 46 50 53 --- 42
R24 | 5600 30 15 37 30 124 15 | 234 239 217 233 254 230
------+------------------------------------+--------------------------------
RMS | 4162 31 18 31 29 88 |T 67 73 73 68 122 68
WRMS | 4162 31 18 28 29 88 |NE 67 73 73 68 122 68
MEDI | 1995 29 15 29 27 77 |MD 43 53 50 53 62 42
Table 3.1502.2 GPS week: 1502 Day: 2 MJD: 54760
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2149 45 34 20 20 --- 18 | 23 56 44 42 --- 37
R06 | 8725 31 38 35 26 --- 19 | 84 107 104 91 --- 93
R07 | 1737 36 17 14 34 --- 15 | 24 23 17 34 --- 13
R10 | 2029 37 21 25 19 --- 15 | 49 48 51 42 --- 45
R11 | 1607 22 16 26 34 112 14 | 71 55 78 57 69 62
R13 | 1407 14 17 23 26 --- 12 | 122 115 125 125 --- 121
R14 | 1594 16 14 18 20 --- 10 | 22 21 28 29 --- 21
R15 | 4004 25 18 16 28 72 12 | 50 63 65 77 97 63
R17 | 2447 19 16 36 30 --- 15 | 43 41 66 70 --- 50
XR18 |14635 63 44 --- --- --- 53 | 134 131 --- --- --- 133
R19 | 860 21 17 15 25 --- 11 | 39 34 57 39 --- 37
R20 | 1356 29 23 16 37 --- 15 | 38 26 27 33 --- 22
R23 | 2000 43 23 51 27 --- 21 | 75 58 90 76 --- 66
R24 | 5322 39 21 26 33 337 17 | 162 185 178 183 505 176
------+------------------------------------+--------------------------------
RMS | 3418 31 22 27 28 209 |T 66 68 71 69 223 67
WRMS | 3418 30 23 23 28 209 |NE 66 68 71 69 223 67
MEDI | 2000 29 18 23 27 112 |MD 49 55 65 57 97 50
Table 3.1502.3 GPS week: 1502 Day: 3 MJD: 54761
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1877 58 25 48 37 --- 23 | 79 53 85 45 --- 54
R06 | 8218 44 22 40 35 --- 20 | 71 97 106 75 --- 83
R07 | 2829 40 21 20 16 --- 14 | 29 33 33 22 --- 20
R10 | 895 50 23 35 23 --- 18 | 99 100 108 91 --- 96
R11 | 1624 39 28 33 28 224 18 | 111 122 135 110 68 118
R13 | 1680 53 33 45 36 --- 23 | 159 193 179 145 --- 167
R14 | 1231 23 18 13 27 --- 12 | 29 26 27 39 --- 24
R15 | 2913 64 20 18 27 182 19 | 71 123 109 129 57 112
R17 | 1306 26 25 28 24 --- 15 | 33 53 51 39 --- 42
XR18 | 7035 38 71 --- 63 --- 44 | 95 94 --- 55 --- 69
R19 | 805 29 19 46 27 --- 17 | 26 45 42 38 --- 31
R20 | 1178 15 10 14 14 --- 7 | 45 30 38 42 --- 34
R23 | 1371 58 37 56 29 --- 25 | 104 63 74 72 --- 67
R24 | 5795 50 23 25 21 652 16 | 154 157 174 166 576 160
------+------------------------------------+--------------------------------
RMS | 3217 45 24 35 27 411 |T 78 84 89 76 233 76
WRMS | 3217 34 20 36 27 411 |NE 78 84 89 76 233 76
MEDI | 1624 40 23 33 27 224 |MD 71 63 85 55 68 67
Table 3.1502.4 GPS week: 1502 Day: 4 MJD: 54762
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2089 27 15 14 34 --- 13 | 35 28 38 30 --- 26
R06 |10591 18 33 60 30 --- 22 | 56 87 96 68 --- 72
R07 | 4199 24 23 18 32 --- 14 | 25 35 25 21 --- 18
XR09 |17200 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1096 28 13 22 25 --- 12 | 41 56 63 66 --- 53
R11 | 1276 48 12 38 42 276 20 | 85 114 124 131 37 111
R13 | 1932 30 28 21 33 --- 16 | 200 213 223 214 --- 212
R14 | 2475 25 19 20 27 --- 13 | 29 30 32 39 --- 26
R15 | 1683 41 23 20 21 129 15 | 55 78 86 81 30 72
R17 | 1729 30 23 30 26 --- 15 | 37 40 50 36 --- 33
XR18 |10526 46 83 --- 83 --- 53 | 104 137 --- 30 --- 130
R19 | 575 33 14 14 31 --- 13 | 44 46 38 53 --- 41
R20 | 1921 25 19 19 19 --- 12 | 34 21 41 35 --- 26
R23 | 1334 42 30 49 39 --- 23 | 93 77 101 88 --- 79
R24 | 6101 24 21 30 22 406 14 | 215 222 188 210 264 209
------+------------------------------------+--------------------------------
RMS | 3880 31 22 30 30 293 |T 75 84 85 78 110 79
WRMS | 3880 29 20 23 30 293 |NE 75 84 85 78 110 79
MEDI | 1932 28 21 20 30 276 |MD 44 56 63 53 37 53
Table 3.1502.5 GPS week: 1502 Day: 5 MJD: 54763
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2536 31 20 22 17 --- 13 | 40 31 25 30 --- 27
R06 |11472 36 21 48 27 --- 18 | 49 47 46 29 --- 34
R07 | 9971 16 19 21 15 --- 10 | 30 21 29 17 --- 16
XR09 |11546 --- --- 17 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1411 20 20 35 19 --- 13 | 91 74 88 90 --- 82
R11 | 6046 35 18 17 23 167 13 | 128 156 170 158 52 153
R13 | 1875 30 21 29 21 --- 14 | 219 241 235 229 --- 231
R14 | 1993 26 12 28 18 --- 11 | 34 21 35 29 --- 21
R15 | 1540 33 19 26 23 59 14 | 78 111 98 104 24 99
R17 | 8761 21 15 33 21 --- 12 | 35 39 36 52 --- 34
XR18 |13098 36 35 --- 42 --- 27 | 102 150 --- 36 --- 134
R19 | 945 24 9 28 17 --- 11 | 44 30 33 42 --- 33
R20 | 2135 33 18 54 27 --- 18 | 66 39 64 47 --- 43
R23 | 1292 48 30 37 35 --- 21 | 117 91 89 103 --- 95
R24 | 2074 40 21 56 23 162 19 | 121 118 96 121 171 112
------+------------------------------------+--------------------------------
RMS | 5364 31 19 35 23 138 |T 82 83 80 77 82 79
WRMS | 5364 27 18 27 23 138 |NE 82 83 80 77 82 79
MEDI | 2135 31 19 28 21 162 |MD 66 47 64 47 52 43
Table 3.1502.6 GPS week: 1502 Day: 6 MJD: 54764
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1576 44 23 21 13 --- 14 | 35 52 38 36 --- 38
R06 | 6218 39 26 35 23 --- 17 | 59 52 54 40 --- 45
R07 | 4203 17 13 28 15 --- 10 | 19 33 29 24 --- 19
XR09 |12881 --- --- 12 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1618 24 19 30 16 --- 12 | 71 81 77 75 --- 75
R11 | 2508 43 19 20 19 196 14 | 98 141 149 134 54 132
R13 | 2759 35 18 48 15 --- 16 | 227 241 276 241 --- 244
R14 | 1024 15 18 17 17 --- 10 | 30 32 37 39 --- 31
R15 | 1331 38 13 48 20 94 16 | 76 96 100 106 33 94
R17 | 7612 31 26 25 22 --- 14 | 64 55 62 67 --- 59
XR18 |14402 40 48 --- 47 --- 33 | 133 148 --- 30 --- 155
R19 | 1726 20 12 19 16 --- 9 | 64 50 51 50 --- 51
R20 | 2045 27 19 39 21 --- 14 | 46 33 71 38 --- 40
R23 | 1080 47 24 43 25 --- 19 | 92 101 130 112 --- 105
R24 | 2206 57 27 36 23 187 19 | 146 150 145 142 315 143
------+------------------------------------+--------------------------------
RMS | 3389 36 20 33 19 165 |T 82 90 93 81 134 87
WRMS | 3389 30 17 28 19 165 |NE 82 90 93 81 134 87
MEDI | 2206 35 19 28 19 187 |MD 64 55 71 50 54 59
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