[IGSREPORT-15932] Wk 1463 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Mon Feb 11 05:21:56 PST 2008
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IGS Electronic Report 11 Feb 05:22:05 PST 2008 Message Number 15932
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1463 (Jan 20, 2008 - Jan 26, 2008)
Contact: Gerd Gendt (gendt at gfz-potsdam.de)
Thomas Nischan ( nisn at gfz-potsdam.de)
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 2.1463.
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:
igl1463[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1463 in the SP3 format.
igl14637.sum Combination Report for GPS Week 1463.
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 | 1316.1 ns
1 | 1370.8 ns
2 | 1344.7 ns
3 | 1360.6 ns
4 | 1366.6 ns
5 | 1337.2 ns
6 | 1337.2 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
----+--------+---------------
0 | ESX | R08 R15 R17
1 | ESX | R08
1 | IAC | R04
2 | ESX | R15 R17 R19
2 | IAC | R04
3 | ESX | R08
4 | ESX | R08
6 | ESX | R08
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 1.1463, 1a.1463).
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 2.1463.0-6)
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 3.1463.0-6).
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 1463 summary. (Jan 20, 2008 - Jan 26, 2008)
Table 1.1463.a GPS week : 1463 MJD: 54485.0-54491.0
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 65| 0 0 11 25 -32 -54 -.12 41 34 | 0 55 2594 2729
| 3 2 6 30 53 144 .07 | 0 208
cod 169| -3 0 -1 -7 -1 -14 -.12 30 22 | --- --- --- ---
| 2 4 4 48 48 43 .05 | --- ---
esx 106| 8 -1 -10 -10 104 -19 .44 152 127 | 5895 -1126 9355 26283
| 8 7 10 57 102 120 .15 | 17675 8970
iac n/a| 0 0 -4 12 -34 86 -.00 44 44 | 1345779 -2701 8833 23293
| 5 2 10 42 66 75 .08 | 19448 5352
mcc n/a| 15 0 -15 123 54 -2959 .39 623 623 | --- --- --- ---
| 15 33 51 320 387 3486 1.67 | --- ---
Table 1.1463.b GPS week : 1463 MJD: 54485.0-54491.0
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
------+------------------------------------+------------------------------------------
R01E | 28 27 24 23 32 19 17 |
R04E | 36 79 135 45 38 41 29 |
R06E | 19 19 22 25 23 30 35 |
R07E | 25 22 17 13 27 17 11 |
R08E | 31 24 43 24 34 35 43 |
R09 | --- --- 0 0 116 21 25 |
R10 | 19 19 16 11 16 19 13 |
R11 | 0 0 31 35 65 76 50 |
R14 | 13 19 15 14 15 10 14 |
R15 | 30 32 36 26 25 25 23 |
R17 | 25 34 21 25 24 20 48 |
R19 | 25 36 36 27 31 20 22 |
R20 | 30 15 18 23 15 18 16 |
R23 | 28 31 24 23 22 26 23 |
R24 | 17 15 18 20 20 21 32 |
Table 1.1463.c GPS week : 1463 MJD: 54485.0-54491.0
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 1463 0 | 292 190 284 717 -1796 -17900 94.5 8471 8471 | 1316058 0
brd 1463 1 | -85 -111 169 -3477 -871 -8233 97.2 7971 7971 | 1370848 0
brd 1463 2 | 24 -60 -1 2325 -4969 -14970 95.0 7345 7345 | 1344712 0
brd 1463 3 | -90 93 243 -4745 -6814 -10020 99.7 5537 5537 | 1360641 0
brd 1463 4 | 212 -165 30 253 -6773 -11610 94.5 6034 6034 | 1366589 0
brd 1463 5 | 48 -18 -4 -4532 -4091 -11290 99.1 7132 7132 | 1337235 0
brd 1463 6 | -12 4 138 -6536 -7608 -21380 100.7 7617 7617 | 1337209 0
-------------+------------------------------------------------------------+----------------
brd 1463 mean| 55 -9 122 -2284 -4703 -13629 97.3 7158 7158 | 1347613 0
brd 1463 sdev| 145 121 117 3349 2606 4686 2.6 1042 1042 | 19535 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 2.1463.0 GPS week: 1463 Day: 0 MJD: 54485
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 65| -1 1 14 -16 -24 -199 .02 50 41 | 0 87 2538 2611
cod 169| -3 -1 -5 -34 -23 28 -.17 22 15 | --- --- --- ---
esx 106| 6 4 -13 32 75 39 .46 124 115 | -21037 -17411 7784 16673
iac n/a| -5 -2 8 45 45 88 -.04 62 62 | 1319325 -7950 7036 12599
mcc n/a| 9 30 28 704 -665 668 -2.35 631 631 | --- --- --- ---
Table 2.1463.1 GPS week: 1463 Day: 1 MJD: 54486
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 65| -2 0 2 25 -24 -192 -.14 39 40 | 0 -110 2877 3105
cod 169| -3 -4 2 -32 59 -5 -.12 28 25 | --- --- --- ---
esx 106| 17 8 -23 -94 119 91 .66 108 92 | 21966 1735 8394 22083
iac n/a| 0 0 6 65 -89 168 .06 41 41 | 1369104 76 8360 19635
mcc n/a| 9 -3 0 199 68 -341 .65 557 557 | --- --- --- ---
Table 2.1463.2 GPS week: 1463 Day: 2 MJD: 54487
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 65| 6 -1 13 72 -41 148 -.20 39 32 | 0 261 3188 3446
cod 169| -5 5 -5 21 69 -7 -.13 31 26 | --- --- --- ---
esx 106| -4 -7 -10 -9 -20 -132 .19 316 324 | -6540 2112 7687 26862
iac n/a| 8 -1 -2 -15 -70 3 .16 40 40 | 1341766 282 7312 26046
mcc n/a| 6 -23 -115 -119 66 -3298 1.14 424 424 | --- --- --- ---
Table 2.1463.3 GPS week: 1463 Day: 3 MJD: 54488
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 65| -1 0 18 -1 -38 -36 -.14 40 31 | 0 -268 2554 2671
cod 169| -4 4 -2 -41 2 4 -.13 28 22 | --- --- --- ---
esx 106| 3 -12 4 64 84 -28 .40 97 82 | 18150 1545 12277 22901
iac n/a| 1 0 -17 13 -60 57 -.06 35 35 | 1360313 586 11507 19379
mcc n/a| 23 -39 -16 327 232 -2240 -.83 230 230 | --- --- --- ---
Table 2.1463.4 GPS week: 1463 Day: 4 MJD: 54489
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 65| 0 0 1 14 -136 -76 -.16 40 32 | 0 -27 2541 2619
cod 169| -2 -4 6 86 -24 -57 -.06 36 20 | --- --- --- ---
esx 106| 17 -4 -2 14 268 113 .37 253 127 | 25376 -9037 11229 33121
iac n/a| -6 4 -15 -47 -121 5 -.06 44 44 | 1365791 -12603 11194 31407
mcc n/a| 46 -3 42 70 478 -1022 .14 640 640 | --- --- --- ---
Table 2.1463.5 GPS week: 1463 Day: 5 MJD: 54490
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 65| -2 0 15 33 -3 128 -.13 35 31 | 0 329 2094 2223
cod 169| 1 1 -5 -49 -34 -89 -.06 31 24 | --- --- --- ---
esx 106| 14 4 -21 -7 199 -221 .43 70 68 | -7569 8861 10927 44656
iac n/a| -3 0 0 50 29 82 -.01 44 44 | 1328741 702 9842 40665
mcc n/a| 17 56 -13 -235 390 -4800 2.97 982 982 | --- --- --- ---
Table 2.1463.6 GPS week: 1463 Day: 6 MJD: 54491
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 65| 3 -4 14 52 39 -155 -.08 45 30 | 0 114 2368 2433
cod 169| -3 1 0 0 -58 28 -.17 34 22 | --- --- --- ---
esx 106| 2 -2 -6 -77 5 3 .55 95 77 | 10919 4307 7189 17686
iac n/a| 4 3 -5 -20 26 201 -.06 41 41 | 1335415 -2 6580 13325
mcc n/a| -2 -21 -37 -80 -190 -9679 1.00 896 896 | --- --- --- ---
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 3.1463.0 GPS week: 1463 Day: 0 MJD: 54485
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9647 64 20 85 41 --- 27 | 86 97 112 99 --- 93
R04E | 6976 44 37 39 125 --- 36 | 163 183 154 462 --- 156
R06E |10884 31 18 42 50 --- 18 | 46 39 52 58 --- 40
R07E | 4122 58 16 63 61 564 25 | 95 78 75 99 223 79
R08E |10393 76 26 223 42 --- 31 | 97 113 179 110 --- 111
R10 | 991 36 19 44 43 --- 18 | 34 33 45 33 --- 27
XR11 |15322 --- 5 --- --- --- 0 | --- 256 --- --- --- 260
R14 | 2266 20 9 27 43 --- 13 | 24 30 45 33 --- 26
R15 |15866 29 27 267 77 83 29 | 28 45 260 77 51 37
R17 | 7395 40 25 208 53 --- 25 | 63 103 232 58 --- 84
R19 | 1210 32 23 59 73 --- 25 | 398 372 371 399 --- 383
R20 | 725 80 15 84 54 --- 30 | 67 56 97 85 --- 56
R23 |13497 45 20 85 62 --- 27 | 66 65 101 48 --- 58
R24 | 7136 51 10 38 28 932 16 | 135 150 156 139 196 144
------+------------------------------------+--------------------------------
RMS | 8471 50 22 124 62 631 |T 100 115 144 130 156 111
WRMS | 8471 41 15 115 62 631 |NE 101 123 163 109 123 119
MEDI | 7136 44 19 63 53 564 |MD 67 78 112 85 196 79
Table 3.1463.1 GPS week: 1463 Day: 1 MJD: 54486
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8188 46 34 65 51 --- 26 | 64 78 113 65 --- 69
XR04E |13969 99 61 --- 1174 --- 78 | 69 122 --- 368 --- 95
R06E |13782 29 22 58 33 --- 18 | 37 40 91 53 --- 39
R07E | 1638 32 25 68 43 444 22 | 45 28 51 72 179 41
R08E | 7733 46 22 244 32 --- 23 | 70 58 134 79 --- 69
R10 | 1162 16 27 50 39 --- 18 | 34 33 53 35 --- 27
XR11 |16218 --- 5 --- --- --- 0 | --- 170 --- --- --- 178
R14 | 1832 16 21 84 19 --- 19 | 26 27 50 23 --- 20
R15 | 5474 41 46 94 55 102 31 | 44 45 135 57 33 44
R17 | 9650 70 27 126 28 --- 33 | 27 69 166 59 --- 58
R19 | 901 44 34 151 46 --- 36 | 269 240 312 263 --- 253
R20 | 734 29 13 22 34 --- 14 | 50 52 41 67 --- 51
R23 |14836 46 32 98 62 --- 31 | 29 67 134 44 --- 50
R24 | 9672 21 18 37 30 851 14 | 112 119 113 117 45 112
------+------------------------------------+--------------------------------
RMS | 7970 39 28 108 41 557 |T 67 82 116 100 85 79
WRMS | 7970 40 25 92 41 557 |NE 73 91 125 83 39 88
MEDI | 7733 41 25 68 39 444 |MD 45 58 113 65 45 51
Table 3.1463.2 GPS week: 1463 Day: 2 MJD: 54487
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 5266 47 30 61 33 --- 24 | 63 54 69 74 --- 59
XR04E |11720 165 110 --- 2871 --- 134 | 299 133 --- 9999 --- 185
R06E |13987 29 36 35 47 --- 22 | 30 35 53 44 --- 31
R07E | 2109 31 22 42 27 320 17 | 60 47 68 67 174 53
R08E | 4832 67 30 158 34 --- 43 | 79 60 204 73 --- 74
XR09 |>>>>> --- 7 --- --- --- 0 | --- 562 --- --- --- 562
R10 | 1437 31 21 35 27 --- 16 | 26 28 42 50 --- 25
XR11 | 6983 --- 28 --- 32 --- 30 | --- 125 --- 74 --- 129
R14 | 1866 26 20 39 23 --- 15 | 23 31 49 43 --- 27
R15 | 5091 18 50 268 65 221 35 | 48 43 209 72 55 40
R17 | 7624 33 25 317 29 --- 20 | 77 78 294 72 --- 72
R19 | 912 54 34 995 63 --- 36 | 331 355 9999 388 --- 362
R20 | 1243 40 13 51 19 --- 17 | 32 48 68 61 --- 45
R23 |14608 24 42 33 52 --- 24 | 36 61 72 45 --- 46
R24 | 9526 38 26 37 22 623 17 | 58 98 91 79 81 78
------+------------------------------------+--------------------------------
RMS | 7344 39 31 316 40 424 |T 89 117 110 87 103 119
WRMS | 7344 32 26 324 40 424 |NE 78 142 117 98 68 138
MEDI | 5266 33 28 42 32 320 |MD 58 60 69 72 81 59
Table 3.1463.3 GPS week: 1463 Day: 3 MJD: 54488
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9035 34 31 61 39 --- 22 | 92 81 116 89 --- 87
R04E | 2714 47 41 186 38 --- 45 | 152 104 240 385 --- 137
R06E | 3892 28 35 35 59 --- 24 | 51 41 56 53 --- 39
R07E | 2253 22 18 31 21 291 12 | 85 76 94 83 324 80
R08E | 6445 46 23 227 31 --- 23 | 125 107 106 121 --- 110
XR09 | ---- --- 5 --- --- --- 0 | --- 278 --- --- --- 271
R10 | 1309 19 15 25 21 --- 11 | 17 35 39 42 --- 29
XR11 |14110 --- 33 --- 36 --- 34 | --- 149 --- 59 --- 157
R14 | 1697 26 19 28 23 --- 13 | 17 31 46 53 --- 29
R15 | 2766 21 20 96 40 172 25 | 28 37 105 57 89 37
R17 | 6460 63 35 48 29 --- 25 | 46 79 76 76 --- 59
R19 | 728 53 32 68 43 --- 27 | 298 308 300 318 --- 312
R20 | 1733 28 35 67 33 --- 22 | 33 45 58 37 --- 25
R23 |13028 44 22 77 26 --- 23 | 50 50 62 73 --- 45
R24 | 4536 51 16 40 31 209 20 | 44 74 85 83 136 65
------+------------------------------------+--------------------------------
RMS | 5537 40 28 97 35 230 |T 79 99 106 109 183 98
WRMS | 5537 31 22 82 35 230 |NE 66 108 96 88 112 102
MEDI | 2766 34 23 61 31 209 |MD 50 76 85 73 136 65
Table 3.1463.4 GPS week: 1463 Day: 4 MJD: 54489
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |10946 39 47 86 52 --- 32 | 76 111 134 78 --- 93
R04E | 3842 45 61 101 55 --- 38 | 101 121 151 214 --- 118
R06E | 7660 36 21 56 44 --- 22 | 62 62 98 64 --- 63
R07E | 1187 30 32 57 67 1081 27 | 58 85 104 77 470 68
R08E | 7236 60 46 891 24 --- 33 | 88 85 675 92 --- 82
XR09 |96917 132 100 --- --- --- 115 | 66 195 --- --- --- 173
R10 | 1778 23 24 39 19 --- 15 | 19 39 75 19 --- 30
XR11 | 6772 --- 52 --- 79 --- 64 | --- 95 --- 94 --- 89
R14 | 806 22 10 48 19 --- 14 | 28 29 76 30 --- 35
R15 | 6116 36 35 43 57 203 24 | 18 47 52 60 82 29
R17 | 7650 36 33 61 34 --- 23 | 40 55 98 32 --- 43
R19 | 793 65 53 31 50 --- 30 | 330 354 472 353 --- 347
R20 | 2306 23 17 27 33 --- 14 | 35 38 43 46 --- 35
R23 |10626 31 25 50 50 --- 22 | 91 47 109 51 --- 69
R24 | 2767 46 17 35 38 133 20 | 90 103 116 124 121 102
------+------------------------------------+--------------------------------
RMS | 6034 40 36 253 44 640 |T 78 97 169 95 224 91
WRMS | 6034 32 20 127 44 640 |NE 79 100 130 89 101 95
MEDI | 6116 36 33 50 44 203 |MD 62 85 104 64 121 69
Table 3.1463.5 GPS week: 1463 Day: 5 MJD: 54490
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |10331 24 29 43 40 --- 19 | 96 86 93 79 --- 85
R04E | 5414 68 52 101 77 --- 41 | 117 97 120 242 --- 99
R06E | 8467 57 45 59 43 --- 29 | 44 50 78 69 --- 43
R07E | 1293 20 15 44 39 1641 16 | 83 85 97 69 339 78
R08E |11316 47 44 92 73 --- 35 | 121 115 344 80 --- 101
XR09 |13889 22 23 --- 44 --- 21 | 45 110 --- 92 --- 99
R10 | 1557 20 24 67 24 --- 18 | 20 38 63 31 --- 29
XR11 | 4572 --- 64 --- 90 --- 76 | --- 138 --- 66 --- 123
R14 | 1590 17 11 26 19 --- 10 | 24 32 60 29 --- 31
R15 | 5191 22 24 92 39 368 24 | 21 24 112 41 43 25
R17 | 9463 29 29 60 25 --- 19 | 22 38 70 39 --- 27
R19 | 1432 25 26 44 48 --- 20 | 587 592 647 635 --- 601
R20 | 2126 22 24 60 25 --- 18 | 48 35 53 44 --- 34
R23 |13711 22 19 101 44 --- 26 | 72 52 135 47 --- 59
R24 | 2782 29 34 64 27 254 21 | 137 142 160 122 54 132
------+------------------------------------+--------------------------------
RMS | 7132 35 31 70 44 982 |T 102 108 156 112 145 104
WRMS | 7132 31 24 68 44 982 |NE 107 117 154 111 48 113
MEDI | 5191 22 26 60 40 368 |MD 48 85 97 69 54 78
Table 3.1463.6 GPS week: 1463 Day: 6 MJD: 54491
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |13504 35 19 37 27 --- 16 | 112 108 102 82 --- 101
R04E | 4609 54 41 75 36 --- 29 | 157 157 132 246 --- 145
R06 | 2722 73 57 29 61 --- 34 | 108 141 131 98 --- 111
R07 | 2417 21 12 17 24 1375 11 | 96 83 85 68 336 81
R08 |13370 67 43 247 72 --- 43 | 121 106 246 105 --- 104
XR09 |12094 27 30 --- 47 --- 25 | 50 150 --- 89 --- 152
R10 | 2107 22 19 38 16 --- 13 | 21 24 34 22 --- 19
XR11 | 4794 31 65 --- 96 --- 49 | 5 149 --- 74 --- 135
R14 | 1570 19 15 44 15 --- 13 | 33 30 44 24 --- 24
R15 | 6201 18 17 79 36 600 22 | 23 25 108 30 40 30
R17 |11886 64 38 174 47 --- 47 | 37 72 193 51 --- 61
R19 | 4056 36 19 52 43 --- 21 | 576 598 681 620 --- 599
R20 | 943 33 18 35 23 --- 15 | 37 52 56 58 --- 46
R23 |12231 15 36 61 44 --- 23 | 59 54 110 37 --- 53
R24 | 2234 60 59 43 47 394 31 | 149 113 121 153 43 125
------+------------------------------------+--------------------------------
RMS | 7616 45 34 95 41 896 |T 105 124 157 117 139 119
WRMS | 7616 30 22 77 41 896 |NE 101 121 159 107 139 117
MEDI | 4609 33 30 44 43 600 |MD 59 106 110 74 43 101
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