[IGSREPORT-15961] Wk 1464 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Tue Feb 19 12:02:17 PST 2008
******************************************************************************
IGS Electronic Report 19 Feb 12:02:28 PST 2008 Message Number 15961
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1464 (Jan 27, 2008 - Feb 02, 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 2.1464.
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:
igl1464[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1464 in the SP3 format.
igl14647.sum Combination Report for GPS Week 1464.
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 | 1292.3 ns
1 | 1292.8 ns
2 | 1315.5 ns
3 | 1299.3 ns
4 | 1293.2 ns
5 | 1273.5 ns
6 | 1241.3 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
----+--------+---------------
0 | ESX | R08
2 | ESX | R11 R17
3 | ESX | R08
5 | 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 1.1464, 1a.1464).
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 2.1464.0-6)
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 3.1464.0-6).
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 1464 summary. (Jan 27, 2008 - Feb 02, 2008)
Table 1.1464.a GPS week : 1464 MJD: 54492.0-54498.0
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 2 12 -31 6 -36 -.09 51 42 | 0 96 2927 3047
| 3 3 5 38 49 141 .05 | 0 84
cod 168| -2 0 0 33 23 30 -.10 34 26 | --- --- --- ---
| 2 2 4 22 50 71 .04 | --- ---
esx 107| 1 0 1 15 15 -39 .39 105 93 | -29320 1776 9006 22321
| 5 4 7 86 79 73 .16 | 19275 6250
iac n/a| 2 0 -11 -15 -12 -3 .03 43 43 | 1284038 239 8652 19314
| 3 2 11 42 39 104 .10 | 24105 5336
mcc n/a| -13 -29 -18 -173 77 -1100 -.46 416 416 | --- --- --- ---
| 33 75 25 379 88 4535 1.40 | --- ---
Table 1.1464.b GPS week : 1464 MJD: 54492.0-54498.0
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 | 14 20 19 22 26 20 32 |
R04 | 28 24 33 17 35 27 25 |
R06 | 23 31 18 20 18 24 29 |
R07 | 12 16 19 16 16 15 16 |
R08 | 35 40 46 31 59 68 56 |
R09 | 38 37 52 38 38 36 19 |
R10 | 21 21 21 16 15 26 16 |
R11 | 20 24 16 25 29 21 35 |
R13 | --- --- --- --- 0 0 0 |
R14 | 12 16 20 21 14 15 17 |
R15 | 30 25 25 42 23 20 30 |
R17 | 49 25 25 30 35 29 21 |
R19 | 17 21 30 44 35 40 25 |
R20 | 20 13 16 17 17 23 25 |
R23 | 33 26 29 25 25 25 22 |
R24 | 20 14 21 22 24 28 22 |
Table 1.1464.c GPS week : 1464 MJD: 54492.0-54498.0
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 1464 0 | 175 233 195 -571 -4798 -4910 101.0 7957 7957 | 1292257 0
brd 1464 1 | -233 -4 -62 4653 -7669 -13170 103.7 7119 7119 | 1292761 0
brd 1464 2 | -99 -57 -152 1143 -8855 -19820 101.4 5493 5493 | 1315520 0
brd 1464 3 | -89 -87 -4 -3227 -8695 -10900 98.8 7241 7241 | 1299254 0
brd 1464 4 | 214 -81 282 1644 -5851 -4997 104.0 7174 7174 | 1293248 0
brd 1464 5 | 250 249 405 -2569 -1805 -3271 93.3 9079 9079 | 1273521 0
brd 1464 6 | 9 -477 -68 4607 -1613 9711 97.4 11560 11560 | 1241302 0
-------------+------------------------------------------------------------+----------------
brd 1464 mean| 32 -32 84 811 -5612 -6765 99.9 7946 7946 | 1286837 0
brd 1464 sdev| 184 243 209 3152 3040 9298 3.8 1920 1920 | 23569 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 2.1464.0 GPS week: 1464 Day: 0 MJD: 54492
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 3 5 -23 82 -35 -.16 47 44 | 0 43 2819 2886
cod 168| 0 0 -4 36 0 -20 -.10 28 21 | --- --- --- ---
esx 107| -5 1 8 2 -66 -39 .59 142 97 | -27855 1164 8004 23495
iac n/a| 6 0 -5 -5 39 71 -.08 44 44 | 1290232 -416 7716 21359
mcc n/a| -78 -190 -58 -612 -60 ---- -3.42 719 719 | --- --- --- ---
Table 2.1464.1 GPS week: 1464 Day: 1 MJD: 54493
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 2 9 -21 32 -6 -.08 54 40 | 0 -31 4756 4917
cod 168| -6 1 0 -5 3 18 -.15 25 24 | --- --- --- ---
esx 107| 3 -5 -3 32 -3 29 .49 65 65 | -30936 5334 10727 25939
iac n/a| 7 -2 0 43 12 -67 -.13 38 38 | 1286751 3964 11021 22367
mcc n/a| -8 -21 -6 282 194 1979 .37 532 532 | --- --- --- ---
Table 2.1464.2 GPS week: 1464 Day: 2 MJD: 54494
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| 4 -5 6 0 -27 -314 -.03 56 43 | 0 136 2173 2278
cod 168| -4 1 -4 25 -43 137 -.07 36 32 | --- --- --- ---
esx 107| 2 4 1 -59 97 -61 .16 116 118 | -5034 -3198 9080 26086
iac n/a| 1 0 -2 7 8 154 .14 38 38 | 1312920 -6936 8848 22804
mcc n/a| -3 -24 5 310 75 1636 .33 415 415 | --- --- --- ---
Table 2.1464.3 GPS week: 1464 Day: 3 MJD: 54495
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 5 12 -23 6 -18 -.14 55 45 | 0 114 2495 2633
cod 168| -4 -2 6 47 0 -24 -.10 30 23 | --- --- --- ---
esx 107| 1 5 8 -42 77 0 .21 100 76 | -23133 11081 9309 19341
iac n/a| 5 4 -18 -90 -37 77 -.01 42 42 | 1294784 5387 8864 16512
mcc n/a| 26 31 13 -422 82 808 -.57 296 296 | --- --- --- ---
Table 2.1464.4 GPS week: 1464 Day: 4 MJD: 54496
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 3 17 6 41 -15 -.08 45 40 | 0 130 2982 3075
cod 168| -3 2 1 22 32 129 -.07 42 24 | --- --- --- ---
esx 107| -3 -3 8 27 88 -112 .49 85 74 | -12614 -8111 8667 17982
iac n/a| 0 0 -21 -8 -45 -53 .05 44 44 | 1295969 -5847 8242 15114
mcc n/a| -28 31 -34 -272 -4 -484 .77 281 281 | --- --- --- ---
Table 2.1464.5 GPS week: 1464 Day: 5 MJD: 54497
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 3 18 -109 -39 166 -.11 38 34 | 0 233 2541 2685
cod 168| 0 0 2 64 111 -18 -.14 50 33 | --- --- --- ---
esx 107| 7 -7 -9 194 17 -146 .38 163 111 | -42550 972 7056 22236
iac n/a| 0 1 -29 -46 -70 -140 .10 48 48 | 1269947 -1031 6623 20246
mcc n/a| -8 -14 -29 -519 164 462 -.58 303 303 | --- --- --- ---
Table 2.1464.6 GPS week: 1464 Day: 6 MJD: 54498
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| -5 3 19 -45 -53 -31 -.03 64 47 | 0 53 2727 2861
cod 168| -1 -2 0 45 62 -10 -.06 27 23 | --- --- --- ---
esx 107| 7 0 -7 -46 -106 55 .43 63 109 | -63119 5195 10201 21169
iac n/a| -2 -1 -5 -11 5 -63 .11 48 48 | 1237667 6557 9253 16797
mcc n/a| 4 -20 -19 22 92 -1004 -.11 364 364 | --- --- --- ---
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 3.1464.0 GPS week: 1464 Day: 0 MJD: 54492
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |17173 21 14 37 28 --- 13 | 89 104 95 91 --- 94
R04 | 2124 68 22 66 48 --- 28 | 87 63 90 66 --- 62
R06 | 4062 63 19 35 41 --- 23 | 44 44 48 51 --- 41
R07 | 6218 14 16 25 28 926 12 | 28 31 43 41 486 29
R08 |11857 72 41 472 33 --- 35 | 53 77 257 54 --- 54
R09 | 9330 36 36 136 54 --- 37 | 399 379 316 394 --- 374
R10 | 2320 43 28 40 37 --- 20 | 21 44 43 30 --- 28
R11 | 5254 28 16 66 31 --- 19 | 93 115 155 109 --- 107
R14 | 1565 25 12 28 19 --- 11 | 25 22 44 28 --- 21
R15 | 6653 44 35 80 56 724 29 | 32 33 66 40 133 27
R17 | 9660 83 24 169 72 --- 48 | 79 97 220 105 --- 97
R19 | 5446 23 16 54 32 --- 17 | 190 188 226 204 --- 196
R20 | 1190 31 21 32 55 --- 20 | 47 45 37 65 --- 45
R23 | 8925 55 49 81 54 --- 33 | 48 66 118 77 --- 55
R24 | 9140 34 34 31 37 413 20 | 565 578 557 568 9999 569
------+------------------------------------+--------------------------------
RMS | 7956 47 28 142 44 719 |T 120 125 154 128 309 119
WRMS | 7956 44 21 97 44 719 |NE 120 125 154 128 309 119
MEDI | 6218 36 22 54 37 724 |MD 53 66 95 66 133 55
Table 3.1464.1 GPS week: 1464 Day: 1 MJD: 54493
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |13507 42 26 49 26 --- 19 | 46 79 70 55 --- 58
R04 | 2239 55 27 50 44 --- 24 | 95 122 129 115 --- 110
R06 | 3836 104 33 27 39 --- 31 | 53 33 32 46 --- 26
R07 | 7163 17 12 49 30 142 15 | 31 28 36 40 397 24
R08 | 8106 120 41 72 50 --- 39 | 125 85 134 58 --- 60
R09 | 6135 37 25 133 56 --- 36 | 455 448 407 434 --- 436
R10 | 3594 44 20 65 26 --- 21 | 16 26 55 26 --- 22
R11 | 4120 44 24 64 44 --- 24 | 109 122 181 157 --- 125
R14 | 2292 29 20 23 37 --- 15 | 27 22 48 34 --- 15
R15 | 5815 33 16 69 59 309 25 | 31 23 65 61 105 23
R17 | 5315 26 24 92 26 --- 24 | 58 82 131 104 --- 84
R19 | 5534 46 24 63 22 --- 21 | 167 138 152 149 --- 145
R20 | 1319 29 8 29 25 --- 12 | 31 38 44 32 --- 29
R23 |10489 47 31 77 38 --- 26 | 56 42 84 46 --- 31
R24 |12798 16 23 21 29 857 13 | 392 398 400 410 567 399
------+------------------------------------+--------------------------------
RMS | 7119 54 25 65 38 532 |T 112 112 131 117 356 105
WRMS | 7119 40 24 65 38 532 |NE 112 112 131 117 356 105
MEDI | 5534 42 24 63 37 309 |MD 56 79 84 58 397 58
Table 3.1464.2 GPS week: 1464 Day: 2 MJD: 54494
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6969 32 17 60 26 --- 19 | 53 26 68 41 --- 31
R04 | 3800 56 62 35 62 --- 33 | 75 126 144 126 --- 113
R06 | 1527 38 31 35 24 --- 18 | 46 47 55 54 --- 39
R07 | 2045 32 30 51 17 92 18 | 31 24 36 36 233 24
R08 | 7437 119 51 88 58 --- 45 | 134 53 74 53 --- 50
R09 | 6786 119 56 137 61 --- 52 | 166 240 323 219 --- 220
R10 | 3167 40 23 50 33 --- 20 | 19 31 57 29 --- 25
R11 | 4305 23 26 303 18 --- 16 | 109 115 301 105 --- 110
R14 | 2179 29 28 61 20 --- 19 | 25 31 49 26 --- 22
R15 | 2807 44 34 72 31 248 25 | 51 33 99 53 68 41
R17 | 7240 26 32 212 41 --- 24 | 70 83 225 85 --- 74
R19 | 2636 20 23 111 42 --- 30 | 57 49 127 53 --- 43
R20 | 1143 29 21 32 28 --- 15 | 33 22 35 29 --- 19
R23 | 7151 67 30 61 43 --- 28 | 46 55 75 42 --- 42
R24 |11344 29 36 52 32 669 21 | 567 581 541 547 437 561
------+------------------------------------+--------------------------------
RMS | 5493 56 36 116 38 415 |T 98 101 147 99 246 94
WRMS | 5493 43 32 118 38 415 |NE 98 101 147 99 246 94
MEDI | 3800 32 30 61 32 248 |MD 53 49 75 53 233 42
Table 3.1464.3 GPS week: 1464 Day: 3 MJD: 54495
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3658 50 24 53 33 --- 22 | 106 77 63 74 --- 74
R04 | 5717 26 16 46 31 --- 16 | 185 158 198 223 --- 187
R06 | 8426 37 22 40 45 --- 20 | 34 53 68 55 --- 45
R07 | 2327 45 14 33 24 78 16 | 41 31 50 43 173 32
R08 |11761 57 31 286 48 --- 31 | 118 51 210 99 --- 84
R09 | 8626 111 42 63 46 --- 37 | 559 584 596 602 --- 585
R10 | 1967 25 17 20 41 --- 15 | 37 25 25 38 --- 25
R11 | 6087 50 24 60 45 --- 24 | 61 92 81 100 --- 80
R14 | 1494 26 16 66 40 --- 21 | 30 18 40 43 --- 19
R15 | 5346 58 59 139 32 196 42 | 33 93 163 57 43 62
R17 | 7724 88 39 43 30 --- 30 | 74 91 87 80 --- 71
R19 | 1309 27 35 150 77 --- 43 | 73 79 128 132 --- 66
R20 | 1074 29 18 43 35 --- 17 | 29 21 38 27 --- 18
R23 | 9406 63 28 36 44 --- 24 | 44 44 58 55 --- 38
R24 |15115 48 34 41 31 468 21 | 329 346 344 320 333 335
------+------------------------------------+--------------------------------
RMS | 7241 55 30 100 42 296 |T 116 117 143 129 183 114
WRMS | 7241 45 23 76 42 296 |NE 116 117 143 129 183 114
MEDI | 5717 48 24 46 40 196 |MD 61 77 81 74 173 66
Table 3.1464.4 GPS week: 1464 Day: 4 MJD: 54496
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2571 42 47 60 34 --- 25 | 86 87 127 99 --- 90
R04 | 8311 68 63 53 54 --- 35 | 41 94 110 92 --- 73
R06 | 5014 35 20 32 37 --- 18 | 30 48 51 55 --- 41
R07 | 1472 32 16 33 29 91 15 | 23 22 43 30 84 19
R08 |14890 31 106 204 56 --- 59 | 103 47 100 91 --- 72
R09 |14391 86 28 93 55 --- 37 | 165 211 203 234 --- 200
R10 | 1689 21 22 41 23 --- 14 | 18 27 45 44 --- 23
R11 | 9752 41 44 90 31 --- 28 | 87 81 162 102 --- 90
XR13 | ---- --- 8 --- --- --- 0 | --- 127 --- --- --- 128
R14 | 1688 22 19 28 27 --- 13 | 22 24 45 39 --- 25
R15 | 6546 33 18 74 41 164 23 | 25 47 77 65 91 39
R17 | 6604 59 28 88 70 --- 34 | 53 78 150 87 --- 68
R19 | 4047 28 41 128 51 --- 35 | 52 44 169 111 --- 68
R20 | 1451 21 14 52 35 --- 17 | 37 21 29 49 --- 25
R23 | 2031 43 25 63 46 --- 24 | 48 47 81 68 --- 44
R24 | 5490 52 30 52 37 449 24 | 568 569 586 550 328 564
------+------------------------------------+--------------------------------
RMS | 7173 45 42 85 44 281 |T 90 98 131 114 167 98
WRMS | 7173 40 24 74 44 281 |NE 90 98 131 114 167 98
MEDI | 5014 35 25 60 37 164 |MD 48 47 100 87 91 68
Table 3.1464.5 GPS week: 1464 Day: 5 MJD: 54497
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9569 32 26 57 26 --- 19 | 127 135 164 128 --- 129
R04 |11400 33 55 53 52 --- 27 | 100 169 112 151 --- 132
R06 |16955 29 28 90 25 --- 24 | 45 50 99 48 --- 39
R07 | 3841 18 29 38 25 78 15 | 26 27 48 26 136 20
R08 |10666 102 89 573 95 --- 68 | 93 63 389 88 --- 43
R09 |17176 28 44 140 43 --- 36 | 426 458 416 488 --- 450
R10 | 1953 39 12 43 65 --- 25 | 14 26 37 62 --- 26
R11 | 8661 22 22 58 43 --- 20 | 54 55 110 82 --- 62
XR13 | ---- --- 8 --- --- --- 0 | --- 224 --- --- --- 227
R14 | 1245 22 25 41 23 --- 15 | 22 22 46 38 --- 18
R15 | 8858 28 40 41 31 187 19 | 24 53 56 33 70 21
R17 | 8061 29 53 76 50 --- 28 | 135 121 141 127 --- 118
R19 | 4305 20 108 67 65 --- 39 | 55 77 92 77 --- 49
R20 | 1004 30 15 74 41 --- 23 | 56 41 60 32 --- 32
R23 | 4790 26 64 54 28 --- 24 | 82 42 100 81 --- 65
R24 | 6134 25 37 97 42 484 27 | 613 610 546 585 572 594
------+------------------------------------+--------------------------------
RMS | 9079 38 50 163 48 303 |T 124 135 161 136 259 126
WRMS | 9079 34 33 111 48 303 |NE 124 135 161 136 259 126
MEDI | 8061 28 29 58 42 187 |MD 56 55 100 81 136 49
Table 3.1464.6 GPS week: 1464 Day: 6 MJD: 54498
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |12490 60 41 62 67 --- 32 | 98 147 109 146 --- 128
R04 |10239 55 32 62 32 --- 25 | 112 95 106 111 --- 97
R06 |27642 56 31 78 45 --- 28 | 31 46 104 61 --- 47
R07 | 8161 30 16 27 39 182 15 | 37 36 41 46 163 32
R08 |16158 188 45 78 57 --- 55 | 88 50 96 66 --- 37
R09 |11067 20 22 27 52 --- 18 | 399 415 409 417 --- 409
R10 | 6346 41 15 25 31 --- 15 | 23 24 42 40 --- 22
R11 | 9152 43 17 109 72 --- 34 | 57 43 81 63 --- 44
XR13 | ---- --- 5 --- --- --- 0 | --- 153 --- --- --- 152
R14 | 6635 34 10 34 44 --- 17 | 30 21 57 36 --- 29
R15 | 7539 44 26 93 53 188 30 | 33 30 119 44 46 39
R17 | 7606 44 24 49 39 --- 21 | 164 180 217 162 --- 173
R19 | 7595 53 27 37 62 --- 25 | 46 89 80 85 --- 68
R20 | 5739 44 30 62 43 --- 24 | 52 48 91 56 --- 48
R23 | 7751 35 18 67 33 --- 21 | 67 51 103 63 --- 62
R24 | 9861 29 30 63 28 574 21 | 733 757 725 719 479 737
------+------------------------------------+--------------------------------
RMS |11564 64 27 63 48 364 |T 131 136 158 141 229 132
WRMS |11564 47 23 109 48 364 |NE 131 136 158 141 229 132
MEDI | 8161 44 24 62 44 188 |MD 57 50 103 63 163 48
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