[IGSREPORT-14743] Wk 1409 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Feb 2 05:43:27 PST 2007
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IGS Electronic Report 02 Feb 05:43:36 PST 2007 Message Number 14743
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1409 (Jan 07, 2007 - Jan 13, 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 2.1409.
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:
igl1409[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1409 in the SP3 format.
igl14097.sum Combination Report for GPS Week 1409.
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 | 649.0 ns
1 | 620.9 ns
2 | 643.1 ns
3 | 603.7 ns
4 | 595.5 ns
5 | 566.9 ns
6 | 578.9 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 | COD | R03
0 | ESX | R22 R23 R24
1 | COD | R24
1 | ESX | R03 R23
1 | IAC | R06
2 | ESX | R23
2 | IAC | R06
3 | ESX | R23
3 | IAC | R06
4 | COD | R03
5 | COD | R03
6 | COD | R03
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 1.1409, 1a.1409).
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 2.1409.0-6)
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 3.1409.0-6).
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 1409 summary. (Jan 07, 2007 - Jan 13, 2007)
Table 1.1409.a GPS week : 1409 MJD: 54107.0-54113.0
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 0 12 69 -9 -115 .06 35 33 | -10 168 2902 3190
| 2 3 6 54 40 187 .13 | 28 313
cod 171| -3 1 9 93 -22 31 -.10 49 41 | --- --- --- ---
| 2 4 6 110 117 156 .18 | --- ---
esx 42| -1 -3 -15 252 26 67 -.21 166 122 | 5445955 13153 8245 12758
| 6 3 18 100 97 175 .23 | 4618422 4465
iac n/a| 1 0 -19 -286 63 75 .07 45 45 | -87403 1144857 433418 435663
| 3 2 9 49 48 110 .10 | 854009 3933301
mcc n/a| 0 8 110 -265 121 -865 -.12 122 122 | --- --- --- ---
| 24 18 37 274 265 1033 .46 | --- ---
Table 1.1409.b GPS week : 1409 MJD: 54107.0-54113.0
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 | 23 24 23 37 29 22 19 |
R02E | 23 17 22 15 19 16 15 |
R03E | ---- 0 191 0 ---- ---- ---- |
R04E | 18 28 25 25 32 31 23 |
R06E | 0 388 244 377 391 889 209 |
R07E | 30 16 34 30 35 40 26 |
R08E | 28 17 20 23 32 26 31 |
R18 | 22 37 40 23 22 23 27 |
R19 | 17 18 14 15 26 22 14 |
R21 | 45 33 28 24 32 22 21 |
R22 | 0 263 0 0 0 0 1425 |
R23 | 33 39 31 48 87 67 68 |
R24 | 15 219 128 208 124 51 79 |
Table 1.1409.c GPS week : 1409 MJD: 54107.0-54113.0
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 1409 0 | 0 0 -1 6 7 -328105.90 8 8 | 648983 0 0 0
brd 1409 1 | 0 0 -1 2 17 -342 85.77 9 9 | 620920 0 0 0
brd 1409 2 | 0 0 -1 1 13 -373 88.81 9 9 | 643108 0 0 0
brd 1409 3 | 0 0 -1 1 11 -395 85.70 8 8 | 603732 0 0 0
brd 1409 4 | 0 0 -1 0 10 -384 99.75 7 7 | 595460 0 0 0
brd 1409 5 | 0 0 -1 0 4 -386 93.31 7 7 | 566943 0 0 0
brd 1409 6 | 0 0 0 6 9 -391108.70 8 8 | 578919 0 0 0
-------------+----------------------------------------------------+------------------------------
brd 1409 mean| 0 0 -1 2 10 -371 95.42 8 8 | 608295 0 0 0
brd 1409 sdev| 0 0 0 2 4 25 9.49 0 0 | 31051 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 2.1409.0 GPS week: 1409 Day: 0 MJD: 54107
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| 3 -3 20 34 -43 -77 .05 25 27 | 0 -265 2645 3036
cod 171| -5 9 13 159 45 -36 -.07 48 35 | --- --- --- ---
esx 42| -6 -6 -14 255 145 10 -.48 204 66 | 7771804 17704 9423 13344
iac n/a| 2 2 -35 -301 -8 130 -.02 43 43 | 645787 5865 9491 13429
mcc n/a| -45 30 121 116 551 773 -.54 258 258 | --- --- --- ---
Table 2.1409.1 GPS week: 1409 Day: 1 MJD: 54108
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 12 35 -5 -350 -.14 26 28 | -76 35 2762 3084
cod 171| -1 -2 1 50 155 212 .04 50 51 | --- --- --- ---
esx 42| 1 -1 -23 161 -154 321 -.03 167 58 | 1935506 11384 7365 14701
iac n/a| -1 1 -18 -214 69 159 .23 47 47 | -999999 -999999 999999 999999
mcc n/a| -18 25 150 80 119 -131 .07 211 211 | --- --- --- ---
Table 2.1409.2 GPS week: 1409 Day: 2 MJD: 54109
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 -1 7 100 -77 164 .13 31 29 | 0 -178 2608 2722
cod 171| -4 3 1 39 -8 -21 .03 58 49 | --- --- --- ---
esx 42| -8 -5 -14 321 2 -216 -.39 152 131 | 8452205 8500 7058 10736
iac n/a| 0 -2 -6 -254 57 -106 .12 38 38 | -999999 9999999 999999 999999
mcc n/a| 19 -18 132 -276 327 -673 -.04 105 105 | --- --- --- ---
Table 2.1409.3 GPS week: 1409 Day: 3 MJD: 54110
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 -4 9 32 21 -50 .26 34 31 | 0 552 3558 3691
cod 171| -5 2 10 106 -98 -38 -.38 43 32 | --- --- --- ---
esx 42| 0 -2 -3 343 44 116 .03 178 286 | 9999999 18697 9854 15104
iac n/a| 0 2 -21 -363 89 3 -.05 47 47 | -999999 -999999 999999 999999
mcc n/a| 5 -7 149 -398 85 -1381 -.48 78 78 | --- --- --- ---
Table 2.1409.4 GPS week: 1409 Day: 4 MJD: 54111
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 5 12 180 42 -372 .01 43 39 | 0 223 2848 3338
cod 171| 0 0 17 -80 -191 285 .10 51 46 | --- --- --- ---
esx 42| 2 -3 -31 358 118 128 -.13 149 66 | 9999999 11579 8895 12123
iac n/a| 0 -3 -12 -276 79 230 -.03 53 53 | 596323 3327 9176 11773
mcc n/a| 1 23 85 -342 147 -1994 -.71 89 89 | --- --- --- ---
Table 2.1409.5 GPS week: 1409 Day: 5 MJD: 54112
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 2 57 9 -47 .12 37 40 | 0 426 2902 3189
cod 171| 0 2 7 102 -109 -28 -.14 38 37 | --- --- --- ---
esx 42| 9 -5 17 86 35 -66 -.03 125 61 | -32582 16507 6867 10636
iac n/a| 8 1 -26 -327 140 38 .12 52 52 | 565879 3922 7003 11772
mcc n/a| 27 5 49 -650 -199 -2097 .48 53 53 | --- --- --- ---
Table 2.1409.6 GPS week: 1409 Day: 6 MJD: 54113
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 21 44 -14 -75 -.03 50 38 | 0 384 2997 3270
cod 171| -4 -4 13 278 51 -152 -.26 53 40 | --- --- --- ---
esx 42| -9 3 -38 241 -1 182 -.47 187 185 | -5245 7705 8253 12666
iac n/a| -1 -1 -12 -268 20 71 .10 35 35 | 580181 885 8265 12676
mcc n/a| 4 1 86 -389 -182 -556 .36 61 61 | --- --- --- ---
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 3.1409.0 GPS week: 1409 Day: 0 MJD: 54107
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |13951 28 45 54 43 --- 23 | 65 84 69 75 --- 62
R02E |10503 32 53 42 34 --- 22 | 65 76 107 66 --- 66
R04E | 8079 24 35 43 29 --- 17 | 56 64 61 55 --- 51
XR06E |13481 --- 14 --- --- --- 0 | --- 9999 --- --- --- 9999
R07E | 2070 24 68 92 43 258 30 | 71 58 107 93 53 70
R08E |14881 29 61 88 33 --- 28 | 41 62 70 45 --- 38
R18 | 7962 22 20 97 24 --- 22 | 132 149 207 145 --- 145
R19 | 6513 22 30 48 24 --- 16 | 69 68 88 71 --- 67
R21 | 1633 19 63 171 78 --- 44 | 70 81 146 109 --- 78
XR22 | ---- --- 15 563 --- --- 0 | --- 509 284 --- --- 418
R23 | 4492 24 55 466 60 --- 32 | 54 60 435 86 --- 64
R24 | 3759 18 21 367 23 --- 14 | 9999 9999 386 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 8595 25 48 204 42 258 |T 69 154 178 82 38 105
WRMS | 8595 27 35 66 42 258 |NE 81 173 257 102 --- 154
MEDI | 7962 24 35 92 33 258 |MD 65 76 107 75 24 66
Table 3.1409.1 GPS week: 1409 Day: 1 MJD: 54108
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |11587 23 60 32 48 --- 23 | 61 95 60 71 --- 59
R02E |13108 16 30 36 43 --- 17 | 38 45 45 56 --- 37
XR03E | ---- --- 15 1872 --- --- 0 | --- 9999 71 --- --- 251
R04E |15032 33 37 100 36 --- 27 | 34 47 127 57 --- 40
XR06E | 6589 259 581 --- 1477 --- 388 | 151 891 --- 559 --- 9999
R07E | 3201 21 20 36 36 211 16 | 57 45 79 55 60 47
R08E |11517 18 26 51 34 --- 17 | 41 43 42 40 --- 28
R18 | 5267 17 93 120 45 --- 37 | 95 155 188 104 --- 111
R19 | 7913 10 23 68 33 --- 18 | 43 43 65 52 --- 37
R21 | 3597 34 64 100 55 --- 33 | 62 39 115 97 --- 64
XR22 | ---- --- 207 333 --- --- 263 | --- 517 265 --- --- 529
R23 | 5387 43 46 454 75 --- 38 | 55 54 305 129 --- 52
XR24 | 3966 161 814 --- 297 --- 218 | 9999 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 9471 26 50 167 47 211 |T 63 179 123 122 60 114
WRMS | 9471 28 51 58 47 211 |NE 63 161 187 95 --- 158
MEDI | 6589 23 46 100 45 211 |MD 55 47 79 57 60 52
Table 3.1409.2 GPS week: 1409 Day: 2 MJD: 54109
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8061 30 47 58 33 --- 22 | 48 65 76 36 --- 44
R02E |10996 23 50 41 41 --- 22 | 54 58 56 53 --- 43
XR03E | ---- --- 160 228 --- 281 191 | --- 498 72 --- 35 261
R04E |17887 27 67 60 30 --- 25 | 37 73 87 55 --- 40
XR06E | 5184 176 334 --- 832 --- 244 | 153 9999 --- 494 --- 9999
R07E | 2958 35 47 101 62 105 34 | 80 71 176 57 79 77
R08E | 8017 22 39 59 28 --- 20 | 47 54 33 47 --- 38
R18 | 4582 46 110 91 44 --- 40 | 103 151 89 71 --- 87
R19 | 6599 20 14 50 14 --- 14 | 51 43 59 47 --- 42
R21 | 6361 31 45 89 37 --- 27 | 51 77 89 63 --- 53
XR22 | ---- --- 4 --- --- --- 0 | --- 530 --- --- --- 529
R23 | 8428 39 57 410 35 --- 30 | 84 57 315 55 --- 59
XR24 | 9925 135 280 --- 142 --- 127 | 9999 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 9158 31 58 152 38 105 |T 70 152 105 97 57 115
WRMS | 9158 29 49 131 38 105 |NE 72 171 138 59 --- 154
MEDI | 8017 31 50 60 37 105 |MD 51 71 76 55 35 53
Table 3.1409.3 GPS week: 1409 Day: 3 MJD: 54110
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 6659 44 32 140 40 --- 36 | 95 72 72 71 --- 72
R02E | 8059 14 32 34 25 --- 14 | 46 46 63 48 --- 42
XR03E | ---- --- 12 --- --- 339 0 | --- 340 --- --- 47 255
R04E |18154 20 54 42 51 --- 24 | 37 68 72 52 --- 36
XR06E | 5822 313 450 --- 1371 --- 376 | 175 9999 --- 635 --- 910
R07E | 4484 40 60 52 58 78 30 | 74 88 87 78 59 69
R08E | 7852 24 43 56 44 --- 23 | 61 118 101 62 --- 76
R18 | 8010 41 48 43 25 --- 23 | 67 89 72 71 --- 63
R19 | 3565 20 19 38 31 --- 15 | 63 54 74 50 --- 53
R21 | 4806 19 31 91 30 --- 24 | 64 59 102 57 --- 56
XR22 |10430 --- 12 --- --- --- 0 | --- 747 --- --- --- 720
R23 | 5203 60 52 495 88 --- 47 | 71 38 372 75 --- 42
XR24 |29164 291 349 --- 227 --- 208 | 9999 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 8483 34 43 178 47 78 |T 75 156 112 119 53 199
WRMS | 8483 31 32 286 47 78 |NE 66 197 155 63 --- 186
MEDI | 6659 40 43 52 44 78 |MD 64 72 74 62 47 63
Table 3.1409.4 GPS week: 1409 Day: 4 MJD: 54111
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 7074 24 42 80 61 --- 28 | 45 56 74 42 --- 31
R02E | 5852 34 40 29 24 --- 19 | 54 46 52 42 --- 42
R04E |13657 41 71 52 51 --- 31 | 48 55 75 68 --- 37
XR06E | 6627 --- 385 --- 396 --- 390 | --- 9999 --- 352 --- 9999
R07E | 6332 64 69 61 46 89 35 | 58 68 83 58 49 35
R08E | 9260 63 55 55 42 --- 31 | 78 79 65 50 --- 45
R18 | 5284 36 35 53 31 --- 21 | 99 77 92 87 --- 84
R19 | 4060 34 37 87 37 --- 26 | 32 52 86 54 --- 34
R21 | 2619 38 51 110 37 --- 31 | 50 71 128 64 --- 48
XR22 |11205 --- 23 --- --- --- 0 | --- 715 --- --- --- 632
R23 | 3103 40 46 400 106 --- 86 | 50 59 299 56 --- 60
XR24 |41169 149 125 --- 236 --- 123 | 9999 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 7130 43 51 149 53 89 |T 57 178 106 87 52 104
WRMS | 7130 39 46 66 53 89 |NE 57 194 151 65 --- 171
MEDI | 6332 38 46 61 46 89 |MD 50 68 83 56 49 42
Table 3.1409.5 GPS week: 1409 Day: 5 MJD: 54112
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8442 36 20 41 53 --- 21 | 69 59 49 71 --- 59
R02E | 5494 27 25 31 31 --- 16 | 42 42 48 49 --- 38
R04E | 9654 38 58 59 60 --- 30 | 46 78 74 41 --- 42
XR06E |14091 --- --- 1272 622 --- 888 | --- --- 11 442 --- 718
R07E | 9487 47 37 166 49 53 40 | 41 54 149 64 53 40
R08E |12280 37 39 86 37 --- 26 | 65 59 64 32 --- 40
R18 | 3536 35 38 66 24 --- 22 | 92 106 109 91 --- 97
R19 | 3149 29 32 49 52 --- 22 | 51 39 56 69 --- 37
R21 | 3390 17 29 62 54 --- 22 | 49 50 76 69 --- 50
XR22 |13545 --- 10 --- --- --- 0 | --- 587 --- --- --- 386
R23 | 4280 54 50 299 86 --- 66 | 56 57 176 37 --- 57
XR24 |38493 83 71 --- 53 --- 51 | 9999 9999 --- 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 7361 37 38 125 52 53 |T 56 162 81 96 53 142
WRMS | 7361 40 37 61 52 53 |NE 62 167 104 66 --- 125
MEDI | 8442 36 37 62 53 53 |MD 51 59 64 64 53 50
Table 3.1409.6 GPS week: 1409 Day: 6 MJD: 54113
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |12520 33 22 69 27 --- 18 | 88 81 82 79 --- 76
R02E | 7756 20 27 52 22 --- 15 | 40 49 62 45 --- 39
R04E | 7713 27 38 86 33 --- 22 | 37 55 47 50 --- 37
XR06E | ---- --- 249 --- 174 --- 208 | --- 9999 --- 278 --- 9999
R07E | 9892 42 44 77 40 61 26 | 54 51 72 70 77 45
R08E |13585 26 68 33 56 --- 30 | 36 39 73 52 --- 37
R18 | 3455 27 42 133 24 --- 27 | 145 138 182 122 --- 131
R19 | 3026 22 22 46 20 --- 14 | 50 64 64 60 --- 51
R21 | 3478 33 42 55 26 --- 20 | 66 73 104 77 --- 68
XR22 |15236 --- 1702 --- 1194 1127 1425 | --- 9999 --- 89 4 832
R23 | 5198 86 59 382 31 --- 68 | 62 57 376 77 --- 62
R24 | 8441 105 104 402 50 --- 78 | 9999 896 368 968 --- 955
------+------------------------------------+--------------------------------
RMS | 8308 50 53 187 35 61 |T 64 150 143 163 45 212
WRMS | 8308 38 40 185 35 61 |NE 80 245 218 232 4 349
MEDI | 7756 27 42 69 31 61 |MD 54 57 73 77 56 62
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