[IGSREPORT-15449] Wk 1441 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Sep 6 05:50:05 PDT 2007
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IGS Electronic Report 06 Sep 05:50:16 PDT 2007 Message Number 15449
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1441 (Aug 19, 2007 - Aug 25, 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 2.1441.
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:
igl1441[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1441 in the SP3 format.
igl14417.sum Combination Report for GPS Week 1441.
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 | 1113.9 ns
1 | 1125.1 ns
2 | 1151.9 ns
3 | 1132.0 ns
4 | 1154.1 ns
5 | 1167.4 ns
6 | 1118.0 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 | R15
0 | ESX | R23 R24
1 | COD | R15
1 | ESX | R23 R24
2 | COD | R15
2 | ESX | R23 R24
3 | COD | R15
3 | ESX | R23 R24
4 | COD | R15
4 | ESX | R23 R24
5 | COD | R15
5 | ESX | R03 R23 R24
6 | COD | R15
6 | ESX | R23 R24
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 1.1441, 1a.1441).
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 2.1441.0-6)
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 3.1441.0-6).
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 1441 summary. (Aug 19, 2007 - Aug 25, 2007)
Table 1.1441.a GPS week : 1441 MJD: 54331.0-54337.0
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 57| 1 0 -7 -33 37 -111 -.07 48 35 | 0 420 4356 4683
| 3 3 3 47 31 160 .10 | 0 462
cod 167| 0 -7 0 12 -1 130 -.13 57 44 | --- --- --- ---
| 4 6 8 47 51 194 .08 | --- ---
esx 45| 3 0 -19 208 -53 -15 -.28 210 81 | 358935 5279 16564 35119
| 8 12 17 177 242 420 .22 | 701155 38445
iac n/a| 0 0 11 -14 3 6 .27 38 38 | 1138692 -2432 15782 32084
| 2 3 4 43 45 105 .13 | 20829 10738
mcc n/a| -1 0 88 68 35 1573 .36 155 155 | --- --- --- ---
| 15 7 14 129 143 342 .50 | --- ---
Table 1.1441.b GPS week : 1441 MJD: 54331.0-54337.0
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 | 17 18 20 15 27 24 18 |
R03 | 28 23 20 22 32 --- --- |
R04 | 21 18 16 20 24 32 34 |
R06 | 29 25 28 32 26 19 35 |
R07 | 18 20 22 16 18 19 15 |
R08 | 20 28 45 30 27 26 24 |
R10 | 21 22 22 19 31 22 29 |
R14 | 20 24 30 21 26 14 17 |
R21 | 25 21 18 26 16 25 22 |
R23 | 27 22 19 20 35 43 49 |
R24 | 131 123 41 31 33 21 23 |
Table 1.1441.c GPS week : 1441 MJD: 54331.0-54337.0
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 1441 0 | 979 -250 -435 4867 -7018 -385200 111.8 8381 8381 | 1113884 0
brd 1441 1 | -110 1260 -932 -13240 -175 -369500 97.2 5932 5932 | 1125138 0
brd 1441 2 | -279 -284 -127 -3782 -7609 -370900 104.4 6312 6312 | 1151902 0
brd 1441 3 | -52 180 -673 5723 -12910 -369300 86.1 6823 6823 | 1131960 0
brd 1441 4 | -393 -278 -593 -4636 -5515 -381400 101.5 6521 6521 | 1154061 0
brd 1441 5 | -355 -54 -180 745 -5909 -365500 93.8 6092 6092 | 1167361 0
brd 1441 6 | -15 -642 -794 -5819 -6767 -353200 95.9 5296 5296 | 1118013 0
-------------+------------------------------------------------------------+----------------
brd 1441 mean| -32 -9 -533 -2305 -6557 -370714 98.7 6479 6479 | 1137474 0
brd 1441 sdev| 470 613 302 6642 3740 10499 8.2 967 967 | 20389 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 2.1441.0 GPS week: 1441 Day: 0 MJD: 54331
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 57| 2 1 -11 -116 93 36 .09 85 42 | 0 29 3509 3737
cod 167| 0 -6 -2 -15 47 38 -.09 63 30 | --- --- --- ---
esx 45| 1 -2 -19 518 -354 -27 -.53 201 91 | 31748 -15511 11818 22403
iac n/a| 0 6 6 -38 56 1 .20 62 62 | 1117048 -1897 11132 21714
mcc n/a| 22 15 106 131 -142 1191 .96 344 344 | --- --- --- ---
Table 2.1441.1 GPS week: 1441 Day: 1 MJD: 54332
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 57| -3 3 -8 -39 30 -384 -.23 74 33 | 0 -170 3980 4390
cod 167| 0 -7 15 -12 -46 6 -.18 95 48 | --- --- --- ---
esx 45| 7 6 -33 107 274 416 -.46 221 74 | 22161 -31675 14169 44598
iac n/a| -3 0 9 -1 -7 150 .28 31 31 | 1122522 -16704 13516 41782
mcc n/a| -4 -2 105 34 -8 2080 -.26 54 54 | --- --- --- ---
Table 2.1441.2 GPS week: 1441 Day: 2 MJD: 54333
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 57| 5 3 -10 5 54 0 -.12 32 30 | 0 959 4232 4447
cod 167| -3 -12 4 -19 18 40 -.19 43 45 | --- --- --- ---
esx 45| 7 8 -15 143 -408 128 -.21 208 69 | 1545349 72356 31351 42972
iac n/a| 0 2 12 -41 10 -69 .48 34 34 | 1138467 16461 28017 38716
mcc n/a| 7 -6 91 -2 36 1472 -.25 110 110 | --- --- --- ---
Table 2.1441.3 GPS week: 1441 Day: 3 MJD: 54334
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 57| 0 1 -8 -46 35 -134 -.01 37 35 | 0 957 3982 4189
cod 167| 3 -8 -1 44 -44 92 -.05 30 30 | --- --- --- ---
esx 45| 15 -2 -9 70 0 399 -.51 183 63 | 1151503 43127 14523 38239
iac n/a| 1 0 14 -7 65 -146 .33 37 37 | 1139003 -985 14354 36784
mcc n/a| -5 4 92 79 198 1461 .15 116 116 | --- --- --- ---
Table 2.1441.4 GPS week: 1441 Day: 4 MJD: 54335
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 57| -1 1 -10 -46 6 -96 -.05 34 33 | 0 453 4789 5073
cod 167| 0 -13 4 15 -24 136 -.04 45 36 | --- --- --- ---
esx 45| 0 15 8 24 72 -142 -.10 195 67 | 32930 -19791 19489 33444
iac n/a| 2 -5 4 70 -52 10 .34 39 39 | 1164473 -8142 18400 26247
mcc n/a| -27 3 81 -132 248 1350 .95 115 115 | --- --- --- ---
Table 2.1441.5 GPS week: 1441 Day: 5 MJD: 54336
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 57| 2 1 0 -24 2 -251 -.07 27 27 | 0 45 5930 6386
cod 167| -8 -7 -5 103 -40 559 -.09 61 56 | --- --- --- ---
esx 45| 5 -8 -26 368 24 -830 -.19 231 122 | -357106 -17308 13994 31628
iac n/a| 0 1 12 -65 -48 133 .26 33 33 | 1168512 -9806 14208 29270
mcc n/a| -8 -5 71 76 12 2029 .50 91 91 | --- --- --- ---
Table 2.1441.6 GPS week: 1441 Day: 6 MJD: 54337
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 57| 6 -7 -4 35 40 48 -.10 46 48 | 0 667 4071 4562
cod 167| 5 6 -11 -27 81 37 -.25 62 60 | --- --- --- ---
esx 45| -12 -21 -43 224 14 -49 .02 229 81 | 85965 5759 10608 32549
iac n/a| -5 -1 15 -20 2 -29 .04 27 27 | 1120823 4044 10850 30075
mcc n/a| 6 -4 69 290 -95 1428 .49 254 254 | --- --- --- ---
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 3.1441.0 GPS week: 1441 Day: 0 MJD: 54331
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |16596 27 16 46 37 --- 17 | 47 40 75 27 --- 29
R03 |10438 60 44 57 41 --- 28 | 44 43 72 25 --- 25
R04 | 3296 26 20 88 28 --- 20 | 27 43 80 33 --- 29
R06 | 3603 62 19 117 25 --- 29 | 21 39 75 49 --- 30
R07 | 3993 36 21 58 24 44 18 | 25 30 65 31 45 22
R08 | 7088 24 25 60 39 --- 19 | 26 46 68 28 --- 26
XR10 | 2132 32 27 --- 29 --- 20 | 25 47 --- 31 --- 32
XR14 | 5942 31 26 --- 25 --- 19 | 17 35 --- 46 --- 25
R21 | 8682 32 13 116 30 --- 24 | 33 28 103 41 --- 26
R23 | 5650 29 31 384 51 --- 27 | 40 45 99 75 --- 48
R24 | 7102 231 174 413 158 484 131 | 311 482 512 420 138 389
------+------------------------------------+--------------------------------
RMS | 8381 85 63 201 62 344 |T 56 79 127 73 91 61
WRMS | 8381 42 30 91 62 344 |NE 56 79 127 73 91 61
MEDI | 5942 32 25 88 30 44 |MD 27 43 75 33 45 29
Table 3.1441.1 GPS week: 1441 Day: 1 MJD: 54332
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7880 35 26 41 23 --- 17 | 31 38 50 33 --- 25
R03 | 7480 19 60 47 37 --- 23 | 34 43 58 31 --- 18
R04 | 5034 28 41 42 21 --- 17 | 35 49 59 33 --- 24
R06 | 5648 41 58 66 23 --- 25 | 25 55 78 50 --- 30
R07 | 3415 25 49 54 20 54 19 | 33 35 80 37 63 30
R08 | 5182 42 26 106 23 --- 27 | 39 31 73 35 --- 29
XR10 | 1711 26 48 --- 20 --- 21 | 45 48 --- 52 --- 42
XR14 | 3287 42 29 --- 29 --- 24 | 16 33 --- 49 --- 31
R21 | 6860 18 43 67 27 --- 20 | 25 43 104 40 --- 29
R23 | 5656 35 29 353 27 --- 21 | 44 47 86 46 --- 38
R24 | 4878 203 257 535 58 --- 123 | 270 447 443 273 --- 275
------+------------------------------------+--------------------------------
RMS | 5932 74 95 221 31 54 |T 54 79 114 61 63 51
WRMS | 5932 33 48 74 31 54 |NE 54 79 114 61 63 51
MEDI | 5182 35 43 66 23 54 |MD 34 43 78 40 63 30
Table 3.1441.2 GPS week: 1441 Day: 2 MJD: 54333
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7766 39 34 43 24 --- 19 | 31 54 53 30 --- 25
R03 | 9673 30 26 77 23 --- 20 | 36 28 68 31 --- 22
R04 | 7119 25 32 46 21 --- 16 | 31 38 73 38 --- 31
R06 | 7768 33 54 63 51 --- 28 | 19 58 53 50 --- 23
R07 | 3186 23 45 50 37 110 21 | 27 37 61 26 63 22
R08 | 4154 39 58 221 19 --- 45 | 30 59 80 42 --- 33
XR10 | 1973 14 44 --- 31 --- 22 | 25 51 --- 48 --- 33
XR14 | 1344 44 21 --- 50 --- 30 | 36 35 --- 90 --- 53
R21 | 5777 15 26 79 17 --- 17 | 18 28 81 22 --- 18
R23 | 3221 24 29 355 28 --- 19 | 44 54 79 42 --- 36
R24 | 4744 48 66 438 60 --- 41 | 222 241 379 257 --- 239
------+------------------------------------+--------------------------------
RMS | 6312 32 43 208 34 110 |T 47 62 103 61 63 48
WRMS | 6312 30 45 69 34 110 |NE 47 62 103 61 63 48
MEDI | 4744 30 34 77 28 110 |MD 31 51 73 42 63 31
Table 3.1441.3 GPS week: 1441 Day: 3 MJD: 54334
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5156 19 24 37 23 --- 14 | 39 45 61 37 --- 34
R03 | 6623 31 24 73 29 --- 21 | 22 32 80 26 --- 18
R04 |13703 29 33 34 40 --- 20 | 61 49 61 37 --- 36
R06 | 6893 43 38 82 65 --- 32 | 21 59 75 56 --- 29
R07 | 3523 28 20 40 27 116 16 | 23 40 55 33 47 25
R08 | 5396 50 28 114 20 --- 30 | 33 52 108 51 --- 43
XR10 | 3319 21 31 --- 26 --- 18 | 49 54 --- 58 --- 52
XR14 | 1759 30 30 --- 28 --- 21 | 27 51 --- 48 --- 36
R21 | 5838 34 52 72 23 --- 25 | 27 41 74 27 --- 14
R23 | 2146 30 16 357 34 --- 19 | 40 61 54 73 --- 52
R24 | 5745 55 23 374 45 --- 30 | 249 302 293 301 --- 282
------+------------------------------------+--------------------------------
RMS | 6823 37 30 183 37 116 |T 53 71 95 67 47 56
WRMS | 6823 35 30 63 37 116 |NE 53 71 95 67 47 56
MEDI | 5396 30 28 73 28 116 |MD 33 51 74 48 47 36
Table 3.1441.4 GPS week: 1441 Day: 4 MJD: 54335
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3628 8 72 61 34 --- 26 | 37 64 44 38 --- 33
R03 | 9226 34 33 120 38 --- 32 | 31 21 63 36 --- 19
R04 |10755 30 29 56 50 --- 23 | 34 37 83 75 --- 45
R06 | 4307 43 45 58 39 --- 26 | 29 64 69 58 --- 40
R07 | 4223 21 24 46 37 115 18 | 20 31 39 37 27 21
R08 | 7908 50 43 57 36 --- 26 | 23 65 69 57 --- 40
XR10 | 4354 44 49 --- 38 --- 31 | 32 56 --- 49 --- 38
XR14 | 2469 37 28 --- 40 --- 25 | 38 43 --- 47 --- 33
R21 | 4431 17 33 45 16 --- 15 | 19 40 37 27 --- 19
R23 | 2208 39 50 404 56 --- 34 | 25 41 127 56 --- 27
R24 | 6728 44 59 386 37 --- 33 | 171 192 230 210 --- 187
------+------------------------------------+--------------------------------
RMS | 6520 34 45 195 39 115 |T 41 59 84 62 27 45
WRMS | 6520 33 36 67 39 115 |NE 41 59 84 62 27 45
MEDI | 4354 37 43 58 38 115 |MD 31 43 69 49 27 33
Table 3.1441.5 GPS week: 1441 Day: 5 MJD: 54336
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4270 27 52 96 32 --- 24 | 29 32 83 40 --- 27
R04 |10500 17 78 138 40 --- 31 | 37 38 149 57 --- 43
R06 | 4030 20 53 58 27 --- 19 | 34 70 68 66 --- 44
R07 | 3719 13 23 80 35 91 18 | 28 33 67 31 37 26
R08 | 6840 23 53 125 23 --- 25 | 41 50 58 52 --- 39
XR10 | 4582 25 45 --- 31 --- 22 | 37 34 --- 30 --- 30
XR14 | 1836 15 23 --- 22 --- 14 | 43 39 --- 41 --- 37
R21 | 5926 20 64 113 22 --- 25 | 39 28 79 28 --- 27
R23 | 2244 50 98 398 50 --- 43 | 41 66 106 54 --- 36
R24 | 7165 24 42 449 28 --- 21 | 212 227 289 232 --- 224
------+------------------------------------+--------------------------------
RMS | 6091 27 61 231 33 91 |T 54 61 112 63 37 53
WRMS | 6091 27 56 122 33 91 |NE 54 61 112 63 37 53
MEDI | 4270 20 52 113 28 91 |MD 37 38 79 41 37 36
Table 3.1441.6 GPS week: 1441 Day: 6 MJD: 54337
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5139 47 27 38 18 --- 18 | 52 45 43 29 --- 33
R04 | 6579 63 61 128 29 --- 33 | 32 38 92 46 --- 33
R06 | 4184 24 102 141 16 --- 35 | 28 77 64 46 --- 37
R07 | 4318 21 37 43 17 62 14 | 28 36 37 32 44 25
R08 | 6119 42 38 91 28 --- 24 | 26 48 36 56 --- 37
XR10 | 4081 38 51 --- 38 --- 29 | 21 41 --- 37 --- 23
XR14 | 3152 28 26 --- 21 --- 17 | 23 31 --- 52 --- 35
R21 | 4390 27 43 100 16 --- 22 | 29 29 63 32 --- 27
R23 | 3059 79 94 424 51 --- 49 | 35 40 97 87 --- 51
R24 | 7238 37 48 428 20 354 23 | 171 200 296 187 110 179
------+------------------------------------+--------------------------------
RMS | 5295 46 62 229 27 254 |T 44 58 91 60 77 48
WRMS | 5295 48 60 81 27 254 |NE 44 58 91 60 77 48
MEDI | 4318 37 43 100 20 62 |MD 28 40 63 46 44 33
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