[IGSREPORT-15408] Wk 1438 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Aug 24 04:45:14 PDT 2007
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IGS Electronic Report 24 Aug 04:45:21 PDT 2007 Message Number 15408
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Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1438 (Jul 29, 2007 - Aug 04, 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 2.1438.
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:
igl1438[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1438 in the SP3 format.
igl14387.sum Combination Report for GPS Week 1438.
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 | 1076.2 ns
1 | 1079.0 ns
2 | 1038.9 ns
3 | 1036.5 ns
4 | 1088.8 ns
5 | 1082.2 ns
6 | 1056.3 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 | 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 | 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 1.1438, 1a.1438).
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 2.1438.0-6)
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 3.1438.0-6).
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 1438 summary. (Jul 29, 2007 - Aug 04, 2007)
Table 1.1438.a GPS week : 1438 MJD: 54310.0-54316.0
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 54| 0 2 -14 -60 25 32 .01 58 46 | 0 -855 5130 5722
| 2 6 6 32 57 166 .15 | 0 1269
cod 171| 1 -9 14 37 3 13 -.06 55 42 | --- --- --- ---
| 4 8 6 30 58 118 .13 | --- ---
esx 41| 0 4 -3 118 -22 27 -.43 172 73 | 15689 12698 13277 23716
| 8 4 12 162 154 219 .26 | 21575 24620
iac n/a| 0 3 1 -21 -14 -88 .25 45 45 | 1062408 4510 12178 22936
| 1 6 9 52 65 117 .18 | 20887 8560
mcc n/a| 4 0 18 -244 64 -1692 -.09 245 245 | --- --- --- ---
| 15 12 24 333 108 2252 .18 | --- ---
Table 1.1438.b GPS week : 1438 MJD: 54310.0-54316.0
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 | 27 28 25 27 59 29 39 |
R03E | 32 46 29 29 40 48 42 |
R04E | 30 25 33 21 24 18 19 |
R06E | 57 91 26 23 30 30 38 |
R07E | 35 29 33 28 22 18 25 |
R08E | 20 30 28 33 30 20 17 |
R10 | 25 21 18 21 28 35 32 |
R14 | 23 23 23 31 25 22 14 |
R21 | 22 27 26 38 33 34 19 |
R23 | 41 42 50 27 36 22 33 |
R24 | 17 22 25 46 37 31 26 |
Table 1.1438.c GPS week : 1438 MJD: 54310.0-54316.0
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 1438 0 | 160 169 -874 -1776 469 -352800 104.9 7314 7314 | 1076234 0
brd 1438 1 | -591 -243 -1719 13250 -2811 -350200 96.6 6999 6999 | 1078977 0
brd 1438 2 | -612 950 -1751 5950 -335 -328900 109.0 7365 7365 | 1038948 0
brd 1438 3 | -209 -670 -2051 -19360 12990 -314100 104.9 7245 7245 | 1036452 0
brd 1438 4 |-1669 -124 -1081 -19460 -10440 -360600 93.1 6264 6264 | 1088812 0
brd 1438 5 | 1222 131 -1025 -1371 7638 -366000 95.8 6002 6002 | 1082199 0
brd 1438 6 | 77 224 -125 4890 7503 -384500 101.8 7225 7225 | 1056259 0
-------------+------------------------------------------------------------+----------------
brd 1438 mean| -231 62 -1232 -2553 2144 -351014 100.9 6916 6916 | 1065411 0
brd 1438 sdev| 885 499 657 12568 7835 23428 5.8 552 552 | 21421 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 2.1438.0 GPS week: 1438 Day: 0 MJD: 54310
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 54| 0 -2 -20 -28 52 -26 .08 59 53 | 0 289 3396 3627
cod 171| -1 -1 11 49 5 205 -.09 54 38 | --- --- --- ---
esx 41| -9 0 7 -68 -72 -186 -.42 177 61 | 38686 13486 12157 21155
iac n/a| 0 -1 -6 -20 55 -22 .55 52 52 | 1076418 11248 11157 20597
mcc n/a| -17 -17 51 -334 8 -2665 -.38 150 150 | --- --- --- ---
Table 2.1438.1 GPS week: 1438 Day: 1 MJD: 54311
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 54| -2 3 -24 -57 56 147 .07 58 56 | 0 -931 3023 3482
cod 171| -5 -20 26 30 -22 -31 -.07 102 42 | --- --- --- ---
esx 41| 16 6 12 346 263 -309 -.49 188 77 | 19752 -4828 10783 23625
iac n/a| 0 16 -5 -71 -123 -14 .30 53 53 | 1081497 -3965 10074 22498
mcc n/a| 34 -3 46 -564 209 -3813 .07 83 83 | --- --- --- ---
Table 2.1438.2 GPS week: 1438 Day: 2 MJD: 54312
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 54| 0 9 -17 -28 117 338 -.24 53 45 | 0 -2028 5002 5503
cod 171| 1 -20 7 54 -104 -32 -.06 45 42 | --- --- --- ---
esx 41| 2 3 1 75 -31 -16 -.31 172 72 | -20797 27959 18544 25637
iac n/a| 2 2 4 -19 37 -317 .22 45 45 | 1031964 14076 16011 24119
mcc n/a| 11 23 34 -809 235 -5373 -.29 105 105 | --- --- --- ---
Table 2.1438.3 GPS week: 1438 Day: 3 MJD: 54313
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 54| 0 1 -9 -103 8 -56 .11 38 34 | 0 -1242 5628 6085
cod 171| 1 -5 19 2 -4 -13 -.02 45 43 | --- --- --- ---
esx 41| -3 6 -9 110 18 310 -.50 154 65 | 32267 -9537 11259 21354
iac n/a| -3 2 -8 78 -23 -169 .31 57 57 | 1042910 -5490 11203 20773
mcc n/a| 0 0 0 0 0 0 .0 337 337 | --- --- --- ---
Table 2.1438.4 GPS week: 1438 Day: 4 MJD: 54314
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 54| -3 6 -10 -106 13 -3 .15 49 41 | 0 479 5060 5609
cod 171| 1 -5 11 62 53 133 -.23 53 54 | --- --- --- ---
esx 41| 0 13 1 37 -7 170 -.81 189 99 | 33674 -9398 11332 25924
iac n/a| 1 -2 2 -19 -74 -84 .31 41 41 | 1084965 -2137 10400 24984
mcc n/a| 0 0 0 0 0 0 .0 474 474 | --- --- --- ---
Table 2.1438.5 GPS week: 1438 Day: 5 MJD: 54315
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 54| 3 -8 -7 -37 -3 9 -.19 81 51 | 0 -2809 7982 9320
cod 171| 8 -9 14 70 19 -150 -.15 48 42 | --- --- --- ---
esx 41| -2 0 -20 337 -257 36 .04 172 77 | 4214 12535 17046 28415
iac n/a| -1 2 2 -84 35 9 -.04 24 24 | 1070161 4028 15445 27611
mcc n/a| 0 0 0 0 0 0 .0 569 569 | --- --- --- ---
Table 2.1438.6 GPS week: 1438 Day: 6 MJD: 54316
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 54| -1 7 -14 -61 -67 -183 .05 68 45 | 0 252 5820 6433
cod 171| 4 -2 8 -8 77 -20 .18 37 31 | --- --- --- ---
esx 41| -7 0 -15 -5 -67 191 -.55 151 57 | 2030 58674 11821 19908
iac n/a| 0 5 20 -16 -13 -18 .12 44 44 | 1048947 13811 10962 19971
mcc n/a| 0 0 0 0 0 0 .0 0 0 | --- --- --- ---
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 3.1438.0 GPS week: 1438 Day: 0 MJD: 54310
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 5921 38 44 46 54 --- 26 | 99 114 120 139 --- 114
R03E | 4648 65 39 64 46 --- 31 | 115 97 100 102 --- 96
R04E |14600 44 70 25 52 --- 29 | 57 81 52 83 --- 60
R06E | 5665 116 110 94 64 --- 56 | 53 110 69 64 --- 48
R07E | 2035 61 38 65 70 150 34 | 42 36 79 74 16 49
R08E |11008 37 32 33 35 --- 19 | 39 31 45 54 --- 32
XR10 | 3643 35 36 --- 32 --- 24 | 28 40 --- 35 --- 24
XR14 | 5580 31 35 --- 29 --- 22 | 29 48 --- 40 --- 34
R21 | 6482 25 33 50 38 --- 21 | 41 44 55 39 --- 38
R23 | 1708 65 40 375 65 --- 40 | 72 43 218 54 --- 46
R24 | 3045 25 21 343 25 --- 17 | 92 94 205 92 --- 89
------+------------------------------------+--------------------------------
RMS | 7314 59 54 177 52 150 |T 60 67 104 70 16 57
WRMS | 7314 53 38 61 52 150 |NE 52 53 159 52 --- 46
MEDI | 5580 38 38 64 46 150 |MD 53 48 79 64 16 48
Table 3.1438.1 GPS week: 1438 Day: 1 MJD: 54311
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 4999 52 45 59 42 --- 28 | 70 82 108 79 --- 70
R03E | 3849 106 43 77 69 --- 46 | 66 99 112 102 --- 85
R04E |14143 38 24 61 47 --- 25 | 71 89 115 102 --- 87
R06E | 9468 51 282 171 86 --- 90 | 20 178 61 62 --- 46
R07E | 2627 47 37 55 56 83 28 | 29 44 61 56 14 36
R08E | 5931 54 42 76 32 --- 29 | 46 36 59 47 --- 29
XR10 | 6237 21 36 --- 31 --- 20 | 27 48 --- 26 --- 30
XR14 | 4328 34 36 --- 28 --- 23 | 25 43 --- 42 --- 31
R21 | 6885 32 40 73 42 --- 26 | 36 46 86 82 --- 49
R23 | 2614 72 55 394 47 --- 42 | 32 42 229 51 --- 33
R24 | 3881 30 38 327 24 --- 21 | 129 125 178 136 --- 128
------+------------------------------------+--------------------------------
RMS | 6999 58 102 188 53 83 |T 50 75 112 71 14 56
WRMS | 6999 56 42 77 53 83 |NE 49 60 164 67 --- 54
MEDI | 4999 47 40 76 42 83 |MD 36 48 108 62 14 46
Table 3.1438.2 GPS week: 1438 Day: 2 MJD: 54312
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 8142 43 42 53 37 --- 24 | 75 93 99 100 --- 85
R03E | 4889 67 44 48 33 --- 28 | 87 64 98 103 --- 80
R04E | 9491 58 43 81 47 --- 32 | 112 126 188 168 --- 142
R06E |10472 36 31 64 48 --- 25 | 46 62 39 57 --- 29
R07E | 2974 43 63 81 43 105 32 | 31 80 65 62 14 44
R08E | 6330 45 55 60 38 --- 28 | 39 70 51 53 --- 40
XR10 | 7374 29 22 --- 23 --- 17 | 29 33 --- 41 --- 28
XR14 | 6110 38 27 --- 30 --- 22 | 31 38 --- 38 --- 25
R21 | 9061 31 32 75 44 --- 26 | 47 46 101 45 --- 45
R23 | 6157 84 50 376 71 --- 49 | 53 50 233 61 --- 31
R24 | 5411 45 33 307 26 --- 25 | 142 153 171 175 --- 155
------+------------------------------------+--------------------------------
RMS | 7364 53 45 172 45 105 |T 62 74 116 82 14 64
WRMS | 7364 45 42 72 45 105 |NE 60 64 168 72 --- 56
MEDI | 6330 43 42 75 38 105 |MD 47 64 99 61 14 44
Table 3.1438.3 GPS week: 1438 Day: 3 MJD: 54313
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E | 9858 48 23 78 32 --- 27 | 87 109 106 115 --- 97
R03E | 7508 39 49 52 62 --- 28 | 53 82 127 117 --- 79
R04E | 4779 29 28 45 44 --- 20 | 60 82 121 124 --- 88
R06E | 8582 31 31 34 61 --- 23 | 59 62 66 65 --- 43
R07E | 4854 29 41 79 49 --- 28 | 52 58 66 66 --- 51
R08E | 6186 34 60 56 76 --- 32 | 29 60 45 57 --- 31
XR10 | 7677 28 22 --- 36 --- 20 | 34 55 --- 57 --- 45
XR14 | 5978 37 48 --- 45 --- 30 | 30 59 --- 44 --- 36
R21 | 8557 31 46 126 56 --- 37 | 62 68 135 65 --- 53
R23 | 5187 33 39 291 42 --- 27 | 52 57 119 56 --- 40
R24 | 7772 56 67 305 71 337 45 | 228 232 237 266 9 233
------+------------------------------------+--------------------------------
RMS | 7245 38 45 154 57 337 |T 67 84 113 93 9 72
WRMS | 7245 34 43 65 57 337 |NE 81 94 163 97 9 81
MEDI | 7508 33 41 78 49 337 |MD 53 62 119 65 9 51
Table 3.1438.4 GPS week: 1438 Day: 4 MJD: 54314
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |12083 26 48 299 51 --- 59 | 116 120 158 123 --- 113
R03E | 5454 71 44 99 72 --- 40 | 61 74 84 70 --- 55
R04E | 3639 38 35 89 20 --- 23 | 100 104 74 94 --- 95
R06E | 4528 31 66 82 44 --- 30 | 39 88 63 43 --- 33
R07E | 2672 40 30 68 29 --- 22 | 48 62 66 64 --- 55
R08E | 7759 31 63 95 38 --- 30 | 26 52 62 43 --- 32
XR10 | 5044 40 31 --- 45 --- 28 | 38 50 --- 60 --- 42
XR14 | 3784 21 52 --- 29 --- 25 | 35 65 --- 31 --- 26
R21 | 5212 59 69 76 35 --- 33 | 69 56 67 45 --- 38
R23 | 3040 60 62 315 24 --- 35 | 73 54 105 45 --- 41
R24 | 6310 66 49 296 36 474 36 | 184 259 269 208 14 213
------+------------------------------------+--------------------------------
RMS | 6263 49 53 189 41 474 |T 71 89 105 75 14 67
WRMS | 6263 41 54 99 41 474 |NE 79 96 147 77 14 72
MEDI | 5044 40 49 95 36 474 |MD 61 65 74 60 14 42
Table 3.1438.5 GPS week: 1438 Day: 5 MJD: 54315
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01E |14059 74 60 70 25 --- 28 | 79 81 101 89 --- 80
R03 | 4977 189 39 96 35 --- 47 | 102 119 115 88 --- 96
R04E | 2557 31 46 44 17 --- 18 | 79 64 74 75 --- 64
R06E | 4837 44 70 91 29 --- 29 | 44 67 78 49 --- 39
R07E | 2745 45 32 57 14 --- 17 | 39 49 74 51 --- 50
R08E | 4255 34 46 50 23 --- 20 | 28 38 62 36 --- 30
XR10 | 4578 60 64 --- 36 --- 34 | 24 57 --- 56 --- 41
XR14 | 4430 44 38 --- 24 --- 22 | 30 29 --- 30 --- 25
R21 | 5350 59 52 147 16 --- 33 | 50 71 102 31 --- 32
R23 | 1915 56 34 342 18 --- 22 | 45 46 69 41 --- 35
R24 | 3730 72 42 315 32 569 30 | 227 271 237 245 10 246
------+------------------------------------+--------------------------------
RMS | 6002 81 48 172 24 569 |T 67 81 101 71 10 67
WRMS | 6002 51 42 77 24 569 |NE 79 98 130 81 10 79
MEDI | 4430 56 46 91 24 569 |MD 45 64 78 51 10 41
Table 3.1438.6 GPS week: 1438 Day: 6 MJD: 54316
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 |14206 116 32 41 70 --- 39 | 142 152 136 172 --- 151
R03 | 5990 124 53 55 56 --- 42 | 167 103 96 94 --- 100
R04E | 7127 34 23 49 22 --- 18 | 84 89 96 83 --- 84
R06E | 3817 43 69 94 42 --- 37 | 46 74 85 59 --- 46
R07 | 3074 23 24 67 49 --- 25 | 64 78 85 74 --- 69
R08 |10557 26 27 34 30 --- 17 | 39 48 48 39 --- 37
XR10 | 3983 32 46 --- 51 --- 32 | 31 47 --- 41 --- 34
XR14 | 3055 20 18 --- 22 --- 14 | 31 49 --- 41 --- 37
R21 | 5586 26 30 55 16 --- 19 | 51 53 73 37 --- 42
R23 | 2546 71 23 286 45 --- 32 | 67 33 127 51 --- 28
R24 | 2858 55 18 315 38 --- 26 | 303 290 327 300 --- 295
------+------------------------------------+--------------------------------
RMS | 7225 68 37 151 44 0 |T 93 92 119 90 --- 83
WRMS | 7225 45 31 57 44 0 |NE 99 94 127 94 --- 88
MEDI | 3983 34 27 55 42 0 |MD 64 74 96 59 --- 46
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