[IGSREPORT-14764] Wk 1411 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Feb 8 03:52:21 PST 2007
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IGS Electronic Report 08 Feb 03:52:32 PST 2007 Message Number 14764
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1411 (Jan 21, 2007 - Jan 27, 2007)
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 2.1411.
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:
igl1411[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1411 in the SP3 format.
igl14117.sum Combination Report for GPS Week 1411.
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 | 573.6 ns
1 | 604.7 ns
2 | 579.1 ns
3 | 585.7 ns
4 | 635.8 ns
5 | 571.7 ns
6 | 558.9 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 1.1411, 1a.1411).
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 2.1411.0-6)
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 3.1411.0-6).
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 1411 summary. (Jan 21, 2007 - Jan 27, 2007)
Table 1.1411.a GPS week : 1411 MJD: 54121.0-54127.0
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 55| 0 2 8 70 -44 21 -.15 63 48 | 0 -207 3237 3423
| 3 3 6 57 58 175 .10 | 0 328
cod 170| 0 -1 -4 147 -8 -84 -.16 50 36 | --- --- --- ---
| 3 4 5 59 44 98 .07 | --- ---
esx 45| -1 4 -24 69 30 86 -.33 178 72 | -38295 -2275 11932 22550
| 3 4 16 166 185 86 .07 | 85093 11335
iac n/a| 0 -1 4 -279 48 42 .40 56 56 | 588583 1897 11878 23440
| 2 2 8 48 38 119 .12 | 24926 8458
mcc n/a| -11 11 31 -175 207 452 .34 190 190 | --- --- --- ---
| 20 27 28 291 432 1086 1.93 | --- ---
Table 1.1411.b GPS week : 1411 MJD: 54121.0-54127.0
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 | 143 246 140 66 40 28 22 |
R02E | 19 32 18 27 22 18 16 |
R03E | ---- ---- ---- ---- 124 25 45 |
R04E | 40 45 55 31 26 20 19 |
R06E | 23 25 27 15 15 18 18 |
R07E | 29 58 53 44 19 31 28 |
R08E | 33 25 23 24 34 24 30 |
R18 | ---- ---- 0 108 49 53 32 |
R19 | 17 21 21 22 18 18 19 |
R21 | 35 27 24 27 34 16 16 |
R22 | 236 572 707 123 71 38 20 |
R23 | 48 62 69 64 56 61 62 |
R24 | 68 74 68 67 63 85 74 |
Table 1.1411.c GPS week : 1411 MJD: 54121.0-54127.0
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 SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
-------------+----------------------------------------------------+------------------------------
brd 1411 0 | 0 0 0 -12 1 -378101.60 7 7 | 573557 0 0 0
brd 1411 1 | 0 0 -1 -1 -6 -376107.40 7 7 | 604741 0 0 0
brd 1411 2 | 0 0 -1 -1 5 -377 93.79 7 7 | 579113 0 0 0
brd 1411 3 | 0 0 -1 -6 5 -367 97.33 8 8 | 585739 0 0 0
brd 1411 4 | 0 0 -1 -1 5 -384 84.28 8 8 | 635771 0 0 0
brd 1411 5 | 0 0 -1 -8 3 -367 92.59 8 8 | 571680 0 0 0
brd 1411 6 | 0 0 -2 -5 0 -353107.70 9 9 | 558935 0 0 0
-------------+----------------------------------------------------+------------------------------
brd 1411 mean| 0 0 -1 -5 2 -372 97.81 8 8 | 587076 0 0 0
brd 1411 sdev| 0 0 0 4 4 10 8.47 0 0 | 25691 0 0 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 2.1411.0 GPS week: 1411 Day: 0 MJD: 54121
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 55| 2 7 6 61 -15 63 -.29 92 62 | 0 -792 2781 2934
cod 170| -5 0 -2 184 7 -4 -.18 43 33 | --- --- --- ---
esx 45| 0 4 -20 55 92 36 -.33 159 67 | -7789 15159 9644 13141
iac n/a| 1 -2 -2 -193 -9 6 .28 33 33 | 571407 8576 9685 13681
mcc n/a| 17 34 66 -548 -242 1434 1.88 111 111 | --- --- --- ---
Table 2.1411.1 GPS week: 1411 Day: 1 MJD: 54122
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 55| -1 0 1 -24 -133 329 .02 78 72 | 0 200 3748 3948
cod 170| 4 0 2 257 7 -165 -.30 52 46 | --- --- --- ---
esx 45| -1 2 -32 298 343 204 -.38 151 78 | -223752 2302 10386 18407
iac n/a| -2 2 -3 -272 39 -123 .58 58 58 | 606806 3846 10470 19167
mcc n/a| -6 20 -12 273 -122 888 2.53 131 131 | --- --- --- ---
Table 2.1411.2 GPS week: 1411 Day: 2 MJD: 54123
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 55| 0 2 2 110 -12 14 -.09 83 57 | 0 -19 4404 4520
cod 170| -3 -10 -4 145 -88 -254 -.18 88 52 | --- --- --- ---
esx 45| -8 13 -8 205 -29 38 -.34 227 93 | -4377 -17599 16920 25246
iac n/a| -3 0 5 -300 116 99 .32 81 81 | 584212 -11547 17633 28556
mcc n/a| -22 21 9 -306 253 26 1.91 107 107 | --- --- --- ---
Table 2.1411.3 GPS week: 1411 Day: 3 MJD: 54124
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 55| 4 -2 14 46 -84 -192 -.13 45 40 | 0 -462 3056 3379
cod 170| 0 2 -15 84 26 6 -.13 53 35 | --- --- --- ---
esx 45| 0 3 1 129 -114 95 -.33 156 62 | -8111 -14309 8347 15047
iac n/a| -2 -4 3 -292 31 141 .56 73 73 | 589446 -6057 8285 15140
mcc n/a| 6 -3 51 -335 -11 78 .94 100 100 | --- --- --- ---
Table 2.1411.4 GPS week: 1411 Day: 4 MJD: 54125
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 55| 1 0 19 85 -6 -138 -.18 48 35 | 0 -63 2876 3040
cod 170| 1 0 -7 88 44 -7 -.11 33 24 | --- --- --- ---
esx 45| 3 0 -39 -128 -156 34 -.42 204 79 | 38118 -2204 8897 12930
iac n/a| 1 -5 14 -350 41 194 .38 64 64 | 634060 4006 9171 12966
mcc n/a| -13 -22 54 -144 1077 -1552 -1.45 272 272 | --- --- --- ---
Table 2.1411.5 GPS week: 1411 Day: 5 MJD: 54126
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 55| -5 5 5 54 -88 126 -.14 53 33 | 0 -244 3136 3297
cod 170| 1 -3 -4 125 -24 -54 -.15 43 31 | --- --- --- ---
esx 45| -3 3 -44 82 190 -6 -.27 169 62 | -23469 -4762 9758 15664
iac n/a| 1 0 16 -297 51 -98 .35 46 46 | 573705 1083 8614 14590
mcc n/a| -47 -18 14 -316 256 588 -1.21 317 317 | --- --- --- ---
Table 2.1411.6 GPS week: 1411 Day: 6 MJD: 54127
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 55| -1 4 9 160 30 -54 -.22 43 39 | 0 -75 2661 2845
cod 170| 0 -1 0 144 -34 -108 -.10 36 30 | --- --- --- ---
esx 45| -1 3 -27 -160 -113 206 -.22 179 63 | -38685 5485 19576 57416
iac n/a| -2 1 -1 -252 72 78 .31 36 36 | 560448 13374 19292 59983
mcc n/a| -17 51 38 150 240 1707 -2.25 291 291 | --- --- --- ---
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 3.1411.0 GPS week: 1411 Day: 0 MJD: 54121
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01E |29568 337 130 158 --- --- 143 | 121 131 236 --- --- 152
R02E | 9191 51 28 41 24 --- 18 | 46 46 56 35 --- 33
R04E | 5697 161 36 67 33 --- 39 | 128 59 68 72 --- 64
R06E | 3446 41 43 59 28 --- 22 | 26 38 63 37 --- 27
R07E | 8294 76 39 57 46 111 28 | 37 36 71 109 19 39
R08E |14441 96 42 118 27 --- 33 | 56 47 76 39 --- 32
R19 | 2742 21 36 46 20 --- 17 | 43 54 45 38 --- 37
R21 | 6630 63 22 182 26 --- 35 | 63 50 132 54 --- 42
XR22 |17559 --- 273 --- 203 --- 235 | --- 258 --- 224 --- 161
R23 | 3569 62 35 266 21 --- 47 | 39 59 280 48 --- 61
R24 | 9752 150 80 306 53 --- 68 | 521 513 598 510 --- 511
------+------------------------------------+--------------------------------
RMS | 7926 92 43 158 33 111 |T 108 117 162 116 19 105
WRMS | 7926 62 33 67 33 111 |NE 166 186 263 174 --- 162
MEDI | 8294 63 39 67 27 111 |MD 46 54 71 48 19 42
Table 3.1411.1 GPS week: 1411 Day: 1 MJD: 54122
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01E | ---- 301 243 --- 454 --- 246 | 109 136 --- 371 --- 169
R02E | 9327 83 49 49 37 --- 32 | 49 54 63 38 --- 30
R04E | 6904 139 58 66 27 --- 45 | 113 72 64 63 --- 61
R06E | 7320 38 37 46 48 --- 24 | 24 34 52 45 --- 22
R07E | 5390 110 57 115 120 131 57 | 35 36 117 120 16 51
R08E |12678 44 29 68 41 --- 24 | 39 48 81 39 --- 31
R19 | 2673 25 15 71 39 --- 20 | 38 46 58 51 --- 38
R21 | 6847 26 30 96 43 --- 26 | 42 45 105 62 --- 37
XR22 |15921 --- 555 --- 589 --- 572 | --- 335 --- 950 --- 448
R23 | 3520 62 46 285 37 --- 61 | 29 45 184 46 --- 54
R24 | 9366 91 99 288 68 --- 73 | 447 487 557 495 --- 480
------+------------------------------------+--------------------------------
RMS | 7690 78 52 151 58 131 |T 92 121 142 207 16 129
WRMS | 7690 72 46 78 58 131 |NE 139 191 226 320 --- 211
MEDI | 6904 62 49 71 43 131 |MD 39 48 81 62 16 51
Table 3.1411.2 GPS week: 1411 Day: 2 MJD: 54123
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | ---- 175 222 532 169 --- 140 | 102 200 422 197 --- 80
R02E |11473 21 35 48 28 --- 17 | 40 85 86 55 --- 55
R04E |10137 129 67 62 82 --- 55 | 114 62 48 45 --- 55
R06E | 3894 21 58 101 22 --- 27 | 24 47 63 32 --- 22
R07E | 3329 80 39 78 129 107 52 | 31 36 71 96 17 36
R08E |11175 22 45 50 46 --- 23 | 59 55 74 31 --- 41
XR18 | ---- --- 19 --- --- --- 0 | --- 192 --- --- --- 181
R19 | 3897 15 36 70 35 --- 20 | 25 49 64 33 --- 24
R21 | 5599 19 43 100 21 --- 24 | 43 29 111 38 --- 38
XR22 |23729 --- 760 --- 658 --- 707 | --- 198 --- 9999 --- 610
R23 | 2706 54 68 350 43 --- 69 | 34 47 237 60 --- 53
R24 | 9380 100 88 264 79 --- 68 | 523 544 568 556 --- 539
------+------------------------------------+--------------------------------
RMS | 7655 83 88 227 80 107 |T 99 128 174 114 17 144
WRMS | 7655 57 52 93 80 107 |NE 156 176 245 171 --- 240
MEDI | 5599 22 45 78 46 107 |MD 40 55 74 45 17 53
Table 3.1411.3 GPS week: 1411 Day: 3 MJD: 54124
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | ---- 58 125 158 137 --- 66 | 97 141 116 77 --- 64
R02E |12574 54 49 46 25 --- 27 | 36 74 76 58 --- 49
R04E |12924 54 35 73 60 --- 30 | 98 67 87 61 --- 57
R06E | 5173 17 23 28 33 --- 14 | 31 41 46 33 --- 27
R07E | 3878 64 28 86 120 100 43 | 47 41 56 61 17 34
R08E | 5426 27 37 35 60 --- 23 | 54 61 78 54 --- 43
XR18 | ---- --- 67 178 --- --- 107 | --- 109 169 --- --- 108
R19 | 7073 22 28 77 38 --- 21 | 37 35 49 27 --- 22
R21 | 4529 23 46 71 57 --- 26 | 30 46 56 50 --- 32
XR22 |19927 --- 102 --- 147 --- 123 | --- 126 --- 240 --- 127
R23 | 4121 52 47 305 35 --- 64 | 43 53 233 69 --- 61
R24 |10692 51 31 315 76 --- 67 | 445 451 521 442 --- 446
------+------------------------------------+--------------------------------
RMS | 8153 45 53 156 73 100 |T 91 103 135 106 17 89
WRMS | 8153 40 35 62 73 100 |NE 138 136 205 165 --- 132
MEDI | 5426 51 37 77 60 100 |MD 43 61 78 61 17 49
Table 3.1411.4 GPS week: 1411 Day: 4 MJD: 54125
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8415 79 40 80 92 --- 40 | 86 64 114 65 --- 49
R02E |11574 44 27 69 30 --- 21 | 47 66 85 72 --- 57
XR03E |25458 146 105 --- --- --- 123 | 33 109 --- --- --- 69
R04E |13400 49 18 49 65 --- 25 | 65 54 60 58 --- 46
R06E | 8818 18 19 60 28 --- 15 | 29 47 54 39 --- 26
R07E | 5157 26 11 59 50 --- 18 | 38 40 54 57 --- 36
R08E | 4146 26 37 76 101 --- 33 | 47 57 51 52 --- 39
XR18 | ---- --- 24 116 --- --- 49 | --- 104 155 --- --- 111
R19 | 9785 28 15 90 20 --- 18 | 54 38 48 31 --- 32
R21 | 6257 23 23 178 59 --- 33 | 46 35 182 73 --- 37
R22 | 3643 38 55 407 89 272 70 | 24 151 244 113 10 59
R23 | 3627 38 31 342 46 --- 56 | 44 69 280 72 --- 73
R24 |10738 94 50 329 60 --- 63 | 418 439 468 415 --- 422
------+------------------------------------+--------------------------------
RMS | 8434 48 33 204 64 272 |T 77 97 149 95 10 81
WRMS | 8434 35 24 79 64 272 |NE 117 139 229 140 10 122
MEDI | 8415 38 27 80 59 272 |MD 46 64 85 65 10 49
Table 3.1411.5 GPS week: 1411 Day: 5 MJD: 54126
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 6018 29 52 75 47 --- 27 | 52 83 54 61 --- 37
R02E | 7017 25 30 36 36 --- 18 | 32 56 66 62 --- 45
XR03E |23831 24 24 --- --- --- 24 | 35 52 --- --- --- 36
R04E |12309 35 33 46 28 --- 19 | 77 44 57 49 --- 46
R06E |15736 23 29 63 26 --- 18 | 24 52 68 36 --- 31
R07E | 7209 46 40 76 63 --- 30 | 49 44 49 76 --- 30
R08E | 6991 48 40 43 31 --- 23 | 52 58 56 55 --- 38
XR18 | ---- --- 29 104 --- --- 52 | --- 100 118 --- --- 101
R19 | 4471 14 24 60 35 --- 17 | 36 38 63 16 --- 25
R21 | 6586 28 18 37 32 --- 15 | 41 38 71 48 --- 37
R22 | 4440 47 57 158 43 317 38 | 25 106 97 60 10 67
R23 | 2511 23 25 337 70 --- 61 | 52 40 223 49 --- 48
R24 |13600 140 80 390 66 --- 85 | 604 605 646 615 --- 602
------+------------------------------------+--------------------------------
RMS | 8841 53 43 169 46 317 |T 89 101 130 102 10 87
WRMS | 8841 33 31 62 46 317 |NE 151 154 203 157 10 146
MEDI | 6991 28 30 63 36 317 |MD 41 52 66 55 10 38
Table 3.1411.6 GPS week: 1411 Day: 6 MJD: 54127
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 6190 38 31 89 25 --- 22 | 60 50 73 63 --- 29
R02E | 2684 30 18 57 22 --- 15 | 25 37 55 49 --- 32
XR03E |25075 50 55 --- 77 --- 45 | 31 42 --- 24 --- 34
R04E | 9766 26 40 37 26 --- 18 | 59 93 72 65 --- 69
R06E |14731 22 33 41 30 --- 17 | 24 53 41 36 --- 28
R07E |10280 36 37 70 57 --- 27 | 35 42 43 68 --- 33
R08E |12879 64 62 49 27 --- 30 | 46 78 68 31 --- 43
XR18 | 4752 37 20 105 --- --- 31 | 13 133 176 --- --- 128
R19 | 2901 37 29 55 23 --- 18 | 47 40 59 29 --- 30
R21 | 3895 22 19 75 17 --- 15 | 64 49 111 72 --- 60
R22 | 8127 39 9 91 22 291 20 | 27 92 101 71 9 46
R23 | 1989 31 21 371 57 --- 61 | 39 56 327 56 --- 59
R24 |14365 83 59 419 54 --- 74 | 713 760 852 739 --- 740
------+------------------------------------+--------------------------------
RMS | 9192 43 36 178 36 291 |T 91 117 164 108 9 102
WRMS | 9192 39 30 63 36 291 |NE 150 188 271 193 9 177
MEDI | 8127 37 31 70 26 291 |MD 39 53 72 56 9 43
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