[IGSREPORT-15009] Wk 1421 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Apr 19 07:27:03 PDT 2007
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IGS Electronic Report 19 Apr 07:27:08 PDT 2007 Message Number 15009
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1421 (Apr 01, 2007 - Apr 07, 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 2.1421.
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:
igl1421[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1421 in the SP3 format.
igl14217.sum Combination Report for GPS Week 1421.
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 | 843.2 ns
1 | 868.1 ns
2 | 880.8 ns
3 | 861.5 ns
4 | 860.2 ns
5 | 873.8 ns
6 | 854.6 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 | R01
0 | ESX | R24
1 | ESX | R24
2 | ESX | R24
3 | ESX | R24
4 | BKG | R23
4 | ESX | R24
5 | BKG | R23
5 | ESX | R24
6 | BKG | R23
6 | ESX | 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 1.1421, 1a.1421).
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 2.1421.0-6)
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 3.1421.0-6).
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 1421 summary. (Apr 01, 2007 - Apr 07, 2007)
Table 1.1421.a GPS week : 1421 MJD: 54191.0-54197.0
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 56| 0 0 3 111 -54 -1 -.04 48 34 | 0 3093 7185 7521
| 3 6 6 55 41 182 .08 | 0 2953
cod 165| 0 0 8 143 -48 65 -.13 43 28 | --- --- --- ---
| 4 6 6 87 55 90 .10 | --- ---
esx 47| 4 1 2 -15 -113 -59 -.17 135 54 | 788101 17296 16890 26223
| 3 4 11 160 90 137 .10 | 2092379 28043
iac n/a| -2 -1 -10 -263 109 -38 .27 42 42 | 863771 3840 15642 24674
| 3 2 4 46 51 73 .08 | 15289 15947
mcc n/a| -1 0 7 -101 -31 218 -.07 196 196 | --- --- --- ---
| 3 1 13 172 78 379 .12 | --- ---
Table 1.1421.b GPS week : 1421 MJD: 54191.0-54197.0
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 | 70 42 25 22 16 20 17 |
R02 | 26 22 18 19 17 13 15 |
R03 | 57 40 24 28 28 21 37 |
R04 | 29 32 26 18 15 16 16 |
R06 | 25 25 22 14 22 22 22 |
R07 | --- 0 0 38 40 25 20 |
R08 | 23 29 28 14 12 17 20 |
R10 | 36 61 58 29 25 20 21 |
R14 | 32 24 34 20 21 21 22 |
R19E | 26 30 26 20 21 28 23 |
R23E | 0 0 0 0 0 0 0 |
R24E | 49 49 69 83 70 38 26 |
Table 1.1421.c GPS week : 1421 MJD: 54191.0-54197.0
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 1421 0 |-1204 -936 -1237 8248 -3493 -376900 76.0 10660 10660 | 843199 0
brd 1421 1 | 1 -551 -327 8354 -3892 -377600 65.2 13550 13550 | 868145 0
brd 1421 2 | 1046 363 -202 -7680 -8480 -357200 104.2 10260 10260 | 880753 0
brd 1421 3 | 441 258 380 3484 5843 -359600 82.0 10940 10940 | 861504 0
brd 1421 4 | 423 175 981 6886 7477 -415200 78.1 10200 10200 | 860172 0
brd 1421 5 | -301 260 463 -2048 2710 -397500 110.6 7988 7988 | 873788 0
brd 1421 6 | -156 159 269 -5566 -771 -373000 99.4 5760 5760 | 854582 0
-------------+------------------------------------------------------------+----------------
brd 1421 mean| 35 -38 46 1668 -86 -379571 87.9 9908 9908 | 863163 0
brd 1421 sdev| 709 498 714 6733 5732 20592 16.8 2449 2449 | 12456 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 2.1421.0 GPS week: 1421 Day: 0 MJD: 54191
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 56| -2 -3 6 110 -43 211 -.10 57 42 | 0 7384 14712 15523
cod 165| 1 -3 0 128 -113 70 -.26 56 26 | --- --- --- ---
esx 47| 2 7 9 -166 8 -16 -.10 166 63 | -18026 14199 18127 37882
iac n/a| 0 -2 -9 -251 6 -28 .28 31 31 | 838359 9353 15888 32888
mcc n/a| 0 0 0 0 0 0 .0 484 484 | --- --- --- ---
Table 2.1421.1 GPS week: 1421 Day: 1 MJD: 54192
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 56| -1 13 8 89 -91 127 .06 66 43 | 0 2237 5304 5985
cod 165| 0 -4 9 -1 -53 89 -.18 41 26 | --- --- --- ---
esx 47| 0 3 -7 136 -71 -226 -.06 130 56 | 14620 17529 24130 27769
iac n/a| -6 1 -11 -221 156 -105 .42 50 50 | 865517 17249 21232 24597
mcc n/a| 0 0 0 0 0 0 .0 713 713 | --- --- --- ---
Table 2.1421.2 GPS week: 1421 Day: 2 MJD: 54193
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 56| 3 -7 4 41 -71 149 -.18 55 36 | 0 3856 9372 8331
cod 165| -2 12 19 202 8 -32 -.06 53 36 | --- --- --- ---
esx 47| 7 -4 13 238 -71 -60 -.20 136 61 | -999999 -32139 18414 23860
iac n/a| 4 -4 -17 -305 89 -107 .34 42 42 | 889179 -26244 17739 24532
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1421.3 GPS week: 1421 Day: 3 MJD: 54194
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 56| 0 0 -3 137 -22 -171 .01 54 20 | 0 1058 4143 4341
cod 165| 7 -6 8 280 -78 -38 -.18 51 34 | --- --- --- ---
esx 47| 2 6 16 -152 -121 7 -.34 170 62 | -999999 30766 18730 28754
iac n/a| -1 0 -11 -290 95 105 .27 44 44 | 862888 18761 15878 25793
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1421.4 GPS week: 1421 Day: 4 MJD: 54195
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 56| -6 -1 9 93 20 73 -.08 32 23 | 0 181 6487 7065
cod 165| 3 2 0 115 -47 16 .03 41 26 | --- --- --- ---
esx 47| 4 -2 -14 48 -286 -222 -.12 123 45 | -43360 -2198 17008 33396
iac n/a| -4 0 -3 -301 134 -10 .24 58 58 | 871925 -3905 15460 29810
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
Table 2.1421.5 GPS week: 1421 Day: 5 MJD: 54196
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 56| 4 -1 -6 92 -76 -215 -.02 35 34 | 0 329 2967 3122
cod 165| 0 0 8 111 40 156 -.10 24 21 | --- --- --- ---
esx 47| 0 0 -5 -159 -127 -72 -.25 111 50 | 3709140 45290 10329 16093
iac n/a| -2 -1 -7 -289 140 -55 .17 48 48 | 859665 13583 11160 17194
mcc n/a| -8 3 23 -356 -9 881 -.30 82 82 | --- --- --- ---
Table 2.1421.6 GPS week: 1421 Day: 6 MJD: 54197
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 56| -2 0 7 219 -93 -188 -.00 38 37 | 0 6607 7312 8285
cod 165| -7 3 12 164 -92 198 -.19 33 30 | --- --- --- ---
esx 47| 10 1 3 -57 -124 171 -.14 112 39 | 3854336 47626 11498 15809
iac n/a| -3 -2 -12 -185 143 -69 .21 23 23 | 858866 -1915 12142 17907
mcc n/a| 0 -2 29 -351 -209 648 -.18 94 94 | --- --- --- ---
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 3.1421.0 GPS week: 1421 Day: 0 MJD: 54191
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- 74 799 --- 67 --- 70 | 136 396 --- 105 --- 133
R02 |10658 51 36 61 39 --- 25 | 43 37 64 25 --- 21
XR03 |21266 40 113 --- 66 --- 56 | 45 77 --- 39 --- 39
R04 | 6237 88 54 33 16 --- 28 | 65 49 27 24 --- 34
R06 |16036 27 60 58 25 --- 24 | 34 54 29 43 --- 27
R08 | 8874 29 17 90 18 --- 22 | 37 32 85 42 --- 39
XR10 |11199 89 23 --- 37 --- 35 | 49 35 --- 66 --- 35
XR14 |13480 67 52 --- 20 --- 31 | 35 76 --- 28 --- 32
R19E | 5131 57 38 66 30 --- 26 | 71 79 78 52 --- 60
XR23E | 9718 --- 11 --- --- --- 0 | --- 178 --- --- --- 177
R24E |12920 69 95 380 45 484 48 | 394 430 444 369 73 412
------+------------------------------------+--------------------------------
RMS |10659 57 56 166 31 484 |T 90 131 121 79 93 91
WRMS |10659 42 26 63 31 484 |NE 55 94 51 46 114 45
MEDI |10658 57 52 61 30 484 |MD 45 76 64 42 73 39
Table 3.1421.1 GPS week: 1421 Day: 1 MJD: 54192
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |19103 77 38 --- 61 --- 42 | 93 221 --- 88 --- 78
R02 | 4549 22 50 31 34 --- 21 | 37 40 47 30 --- 29
XR03 |28270 67 64 --- 32 --- 40 | 39 65 --- 64 --- 55
R04 | 6836 92 30 30 58 --- 32 | 56 31 34 26 --- 17
R06 |23588 41 39 49 43 --- 25 | 31 31 41 40 --- 23
XR07 |>>>>> --- 8 --- --- 472 0 | --- 230 --- --- 227 229
R08 | 7715 33 18 72 59 --- 29 | 40 41 63 61 --- 39
XR10 | 3591 81 93 --- 81 --- 61 | 96 87 --- 76 --- 48
XR14 | 9045 42 28 --- 30 --- 23 | 46 71 --- 48 --- 44
R19E | 6649 64 61 38 38 --- 30 | 62 70 68 72 --- 59
XR23E |10204 --- 9 --- --- --- 0 | --- 139 --- --- --- 137
R24E |19334 103 35 300 61 713 48 | 287 310 324 336 77 304
------+------------------------------------+--------------------------------
RMS |13548 66 41 130 50 713 |T 78 111 96 84 152 88
WRMS |13548 43 26 56 50 713 |NE 54 90 46 54 227 62
MEDI | 9045 64 35 38 43 472 |MD 46 70 47 61 77 48
Table 3.1421.2 GPS week: 1421 Day: 2 MJD: 54193
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |11503 29 38 83 28 --- 25 | 43 107 73 61 --- 37
R02 |11574 20 33 55 18 --- 17 | 30 70 87 34 --- 43
XR03 |43276 22 39 --- 35 --- 23 | 48 41 --- 43 --- 34
R04 | 5690 59 29 25 46 --- 25 | 35 50 47 38 --- 31
R06 | 6061 28 57 42 18 --- 21 | 37 46 67 33 --- 36
XR07 | 8560 --- 18 --- --- 217 0 | --- 134 --- --- 179 131
R08 | 4669 23 30 98 40 --- 27 | 52 66 83 68 --- 58
XR10 | 4182 84 80 --- 80 --- 57 | 43 59 --- 90 --- 38
XR14 | 7081 34 66 --- 40 --- 34 | 31 44 --- 30 --- 20
R19E | 8489 56 38 58 32 --- 26 | 65 62 106 80 --- 68
XR23E | 6742 --- 18 --- --- --- 0 | --- 262 --- --- --- 264
R24E |17542 111 103 322 79 --- 68 | 379 451 399 388 --- 417
------+------------------------------------+--------------------------------
RMS |10261 55 53 136 42 0 |T 76 116 123 86 179 98
WRMS |10261 36 36 61 42 0 |NE 39 68 71 49 179 47
MEDI | 7081 29 38 58 35 217 |MD 43 62 83 43 179 38
Table 3.1421.3 GPS week: 1421 Day: 3 MJD: 54194
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |13079 23 31 83 28 --- 21 | 75 105 75 82 --- 75
R02 |13664 16 39 66 22 --- 18 | 35 38 71 48 --- 28
XR03 |40258 41 45 --- 31 --- 27 | 53 93 --- 69 --- 65
R04 | 4065 17 35 65 22 --- 18 | 53 56 92 35 --- 37
R06 | 8168 17 23 42 21 --- 13 | 43 49 75 49 --- 41
XR07 | 6021 --- 51 87 38 112 37 | --- 58 36 35 110 52
R08 | 9025 18 17 45 23 --- 13 | 40 63 62 45 --- 44
XR10 | 2183 13 58 --- 45 --- 29 | 60 47 --- 66 --- 52
XR14 | 5184 16 34 --- 31 --- 19 | 50 53 --- 29 --- 36
R19E | 9920 30 38 54 25 --- 19 | 60 68 77 68 --- 61
XR23E | 4071 --- 20 --- --- --- 0 | --- 110 --- --- --- 107
R24E |14718 135 112 425 102 --- 83 | 312 378 439 442 --- 365
------+------------------------------------+--------------------------------
RMS |10938 54 51 170 44 0 |T 78 93 115 88 110 80
WRMS |10938 20 34 62 44 0 |NE 51 62 68 50 110 47
MEDI | 8168 17 35 65 28 112 |MD 53 58 75 49 110 52
Table 3.1421.4 GPS week: 1421 Day: 4 MJD: 54195
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8972 14 18 51 28 --- 16 | 40 57 65 54 --- 40
R02 |11307 24 22 47 27 --- 17 | 53 41 64 30 --- 37
XR03 |46706 46 41 --- 24 --- 27 | 27 61 --- 41 --- 34
R04 | 8750 24 29 32 19 --- 15 | 54 36 54 27 --- 34
R06 | 8768 28 25 65 35 --- 21 | 34 42 50 46 --- 35
XR07 | 5457 --- 59 74 34 112 39 | --- 105 38 24 53 59
R08 | 6114 17 20 32 16 --- 12 | 45 62 54 61 --- 52
XR10 | 4681 34 24 --- 47 --- 25 | 39 32 --- 39 --- 25
XR14 | 5224 30 37 --- 19 --- 21 | 29 45 --- 21 --- 24
R19E |13255 38 32 36 39 --- 21 | 44 49 45 71 --- 41
XR23E | 5086 295 7 --- --- --- 0 | 518 185 --- --- --- 185
R24E |12403 58 89 306 138 --- 70 | 251 278 296 356 --- 290
------+------------------------------------+--------------------------------
RMS |10203 32 41 123 58 0 |T 103 82 83 70 53 71
WRMS |10203 23 26 45 58 0 |NE 40 53 54 38 53 37
MEDI | 8750 30 25 47 28 112 |MD 44 49 54 41 53 37
Table 3.1421.5 GPS week: 1421 Day: 5 MJD: 54196
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2226 38 15 67 30 --- 20 | 73 83 34 67 --- 52
R02 | 8000 18 16 27 30 --- 12 | 30 36 44 38 --- 28
XR03 |60473 35 29 --- 24 --- 21 | 66 73 --- 65 --- 58
R04 | 5965 30 22 44 15 --- 15 | 48 34 51 18 --- 26
R06 | 5455 24 17 78 41 --- 22 | 40 50 61 34 --- 40
R07 | 3394 54 17 76 30 82 24 | 33 34 29 32 42 32
R08 | 5780 25 23 51 27 --- 17 | 30 46 29 39 --- 33
XR10 | 7738 22 22 --- 41 --- 20 | 35 40 --- 60 --- 38
XR14 | 6466 25 26 --- 36 --- 20 | 32 43 --- 27 --- 31
R19E |12313 49 24 35 77 --- 27 | 89 72 77 116 --- 83
XR23E | 3239 2163 12 --- --- --- 0 | 796 208 --- --- --- 210
R24E |13399 24 44 276 84 --- 38 | 272 285 314 302 --- 288
------+------------------------------------+--------------------------------
RMS | 7987 35 24 111 48 82 |T 128 83 79 72 42 76
WRMS | 7987 34 21 50 48 82 |NE 43 48 41 42 42 37
MEDI | 5965 25 22 51 30 82 |MD 40 46 44 39 42 38
Table 3.1421.6 GPS week: 1421 Day: 6 MJD: 54197
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2061 32 27 48 15 --- 17 | 45 62 63 36 --- 34
R02 | 4663 38 22 22 19 --- 14 | 48 29 42 42 --- 33
XR03 |54921 85 21 --- 45 --- 37 | 66 45 --- 43 --- 31
R04 | 6389 30 41 18 17 --- 16 | 51 41 34 25 --- 26
R06 | 3918 50 24 59 23 --- 21 | 49 29 46 44 --- 29
R07 | 2359 13 31 66 25 94 20 | 35 42 39 18 91 35
R08 | 4763 31 33 62 17 --- 20 | 48 66 39 45 --- 39
XR10 | 8537 41 26 --- 24 --- 21 | 47 44 --- 47 --- 33
XR14 | 3571 38 27 --- 29 --- 22 | 28 38 --- 33 --- 22
R19E | 9128 63 33 39 27 --- 23 | 88 114 110 102 --- 99
XR23E | 5610 9113 17 --- --- --- 0 | 880 352 --- --- --- 348
R24E | 8462 23 45 292 35 --- 25 | 320 323 389 346 --- 329
------+------------------------------------+--------------------------------
RMS | 5759 38 33 112 23 94 |T 142 98 95 71 91 88
WRMS | 5759 37 30 39 23 94 |NE 46 44 43 37 91 31
MEDI | 4763 38 27 48 24 94 |MD 48 44 42 43 91 33
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