[IGSREPORT-15410] Wk 1439 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Aug 24 11:53:44 PDT 2007
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IGS Electronic Report 24 Aug 11:53:53 PDT 2007 Message Number 15410
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1439 (Aug 05, 2007 - Aug 11, 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 2.1439.
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:
igl1439[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1439 in the SP3 format.
igl14397.sum Combination Report for GPS Week 1439.
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 | 1027.9 ns
1 | 988.3 ns
2 | 1066.3 ns
3 | 1004.4 ns
4 | 1052.5 ns
5 | 1077.5 ns
6 | 1054.6 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 | 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 1.1439, 1a.1439).
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 2.1439.0-6)
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 3.1439.0-6).
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 1439 summary. (Aug 05, 2007 - Aug 11, 2007)
Table 1.1439.a GPS week : 1439 MJD: 54317.0-54323.0
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 -17 -54 6 0 -.06 41 38 | 0 62 4459 4770
| 3 5 5 61 37 151 .09 | 0 1498
cod 172| -2 -8 2 -7 10 170 -.15 50 49 | --- --- --- ---
| 6 7 5 54 71 122 .15 | --- ---
esx 40| 0 4 -8 138 13 -66 -.32 169 82 | -94102 -1822 13840 28818
| 8 6 9 143 185 204 .21 | 406942 20695
iac n/a| 1 2 17 -30 -9 -65 .22 40 40 | 1039535 942 13376 28344
| 1 6 7 35 43 119 .15 | 29654 8273
mcc n/a| 0 0 79 14 -21 -42 .40 143 143 | --- --- --- ---
| 5 11 8 148 90 1328 .51 | --- ---
Table 1.1439.b GPS week : 1439 MJD: 54317.0-54323.0
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 | 23 17 27 24 23 25 25 |
R03 | 33 29 25 24 35 33 48 |
R04 | 24 26 20 23 30 29 20 |
R06E | 31 31 39 21 39 28 25 |
R07 | 23 21 15 20 24 20 20 |
R08 | 36 26 28 19 30 38 22 |
R10 | 19 23 20 17 19 18 22 |
R14 | 21 27 37 42 28 22 27 |
R21 | 21 33 27 21 22 22 29 |
R23 | 18 25 31 61 52 41 30 |
R24 | 20 22 30 28 38 20 51 |
Table 1.1439.c GPS week : 1439 MJD: 54317.0-54323.0
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 1439 0 | 337 -624 -536 6389 -3817 -348800 99.9 6133 6133 | 1027860 0
brd 1439 1 | 433 -74 -435 1598 985 -348200 87.2 4432 4432 | 988327 0
brd 1439 2 | -186 37 -489 12510 264 -342600 99.9 5090 5090 | 1066295 0
brd 1439 3 | 98 299 -516 -2522 -202 -335100 88.7 6229 6229 | 1004403 0
brd 1439 4 | 356 76 -83 -4301 1973 -334000 80.7 8249 8249 | 1052528 0
brd 1439 5 | 145 -362 209 2097 535 -325200 85.8 18000 18000 | 1077468 0
brd 1439 6 | -167 88 532 -3521 1442 -317300 101.1 8674 8674 | 1054602 0
-------------+------------------------------------------------------------+----------------
brd 1439 mean| 145 -79 -188 1750 168 -335885 91.9 8115 8115 | 1038783 0
brd 1439 sdev| 249 312 422 6056 1902 11742 8.2 4623 4623 | 33014 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 2.1439.0 GPS week: 1439 Day: 0 MJD: 54317
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 -1 -25 -62 -1 120 .11 46 42 | 0 2067 5176 5372
cod 172| -7 -3 4 -47 57 191 -.10 41 38 | --- --- --- ---
esx 40| 7 0 -7 123 -70 68 -.30 146 60 | 53662 65 11650 18788
iac n/a| 0 1 21 -21 -67 -281 .14 41 41 | 1040372 -941 10820 19383
mcc n/a| 1 0 77 -120 -63 359 .48 105 105 | --- --- --- ---
Table 2.1439.1 GPS week: 1439 Day: 1 MJD: 54318
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 -19 -88 -43 -287 -.06 35 33 | 0 -1082 4696 4942
cod 172| -5 -1 -6 5 -3 246 .03 48 49 | --- --- --- ---
esx 40| 2 4 -18 207 56 -53 -.34 164 64 | -28365 -24946 15578 28613
iac n/a| 4 -1 31 -9 21 63 .18 34 34 | 986726 -1379 15211 26605
mcc n/a| -6 4 93 193 29 700 .70 342 342 | --- --- --- ---
Table 2.1439.2 GPS week: 1439 Day: 2 MJD: 54319
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| 4 11 -11 -66 -18 -87 -.12 35 34 | 0 -2285 5289 5855
cod 172| -11 -20 3 30 146 115 -.13 50 40 | --- --- --- ---
esx 40| 7 2 -21 134 -180 38 -.30 164 74 | 29544 8595 12919 20706
iac n/a| 2 7 18 -95 -17 25 .26 40 40 | 1060154 3778 12059 20614
mcc n/a| -1 4 85 115 -8 1273 -.53 174 174 | --- --- --- ---
Table 2.1439.3 GPS week: 1439 Day: 3 MJD: 54320
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 0 -16 -117 3 65 -.08 31 31 | 0 -478 3607 3882
cod 172| 6 -13 10 45 -67 5 -.04 55 60 | --- --- --- ---
esx 40| -3 2 -3 228 -233 179 -.17 156 63 | -9314 15043 8457 27975
iac n/a| 1 4 15 -59 64 -69 .29 44 44 | 1010526 3060 8822 28610
mcc n/a| 7 9 80 -80 101 1552 -.09 254 254 | --- --- --- ---
Table 2.1439.4 GPS week: 1439 Day: 4 MJD: 54321
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 3 -9 31 42 -27 -.06 38 34 | 0 818 3727 3968
cod 172| 0 2 9 -91 -44 387 -.43 64 61 | --- --- --- ---
esx 40| -12 11 -4 0 107 -459 -.62 171 133 | 207977 -36759 16529 33088
iac n/a| 1 -10 6 -27 -29 25 .37 50 50 | 1061226 -15412 15964 32838
mcc n/a| -6 -23 68 -131 7 -1520 .76 51 51 | --- --- --- ---
Table 2.1439.5 GPS week: 1439 Day: 5 MJD: 54322
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| -4 -4 -14 -107 67 65 -.17 49 52 | 0 1391 4274 4685
cod 172| 0 -8 -1 -42 -5 151 -.20 47 53 | --- --- --- ---
esx 40| 5 -3 -11 351 123 -124 .00 177 96 | 87776 13148 20636 48543
iac n/a| 2 5 18 11 5 -91 -.05 35 35 | 1059819 8730 19482 45072
mcc n/a| 0 -5 70 -74 -25 -1546 .68 39 39 | --- --- --- ---
Table 2.1439.6 GPS week: 1439 Day: 6 MJD: 54323
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 -23 29 -6 153 -.02 56 42 | 0 4 4446 4689
cod 172| 1 -10 0 50 -7 96 -.19 43 41 | --- --- --- ---
esx 40| -8 12 6 -74 291 -116 -.52 208 81 | -999999 12099 11114 24014
iac n/a| 0 7 11 -13 -41 -133 .36 32 32 | 1057928 8762 11277 25288
mcc n/a| 7 9 79 198 -189 -1118 .77 37 37 | --- --- --- ---
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 3.1439.0 GPS week: 1439 Day: 0 MJD: 54317
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7910 36 55 25 35 --- 23 | 56 78 50 57 --- 52
R03 | 7826 67 36 79 42 --- 33 | 79 39 71 41 --- 39
R04 | 6100 44 32 50 36 --- 23 | 67 60 77 58 --- 53
R06E | 2771 44 47 75 42 --- 30 | 38 54 68 75 --- 52
R07 | 2856 27 41 54 36 105 23 | 21 33 31 39 54 23
R08 |10453 69 60 37 73 --- 36 | 72 146 116 121 --- 109
XR10 | 4530 23 30 --- 25 --- 18 | 32 38 --- 26 --- 26
XR14 | 5253 29 28 --- 31 --- 21 | 35 30 --- 48 --- 30
R21 | 4468 50 29 39 24 --- 21 | 20 58 57 40 --- 34
R23 | 3118 23 24 308 28 --- 18 | 26 30 148 42 --- 26
R24 | 4758 24 27 275 31 --- 19 | 176 212 240 214 --- 202
------+------------------------------------+--------------------------------
RMS | 6132 46 41 145 41 105 |T 56 70 95 69 54 58
WRMS | 6132 42 38 60 41 105 |NE 58 72 98 68 54 59
MEDI | 4758 36 32 54 35 105 |MD 38 54 71 48 54 39
Table 3.1439.1 GPS week: 1439 Day: 1 MJD: 54318
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4763 28 36 31 22 --- 17 | 45 67 62 48 --- 47
R03 | 5384 41 34 103 27 --- 29 | 40 48 65 35 --- 33
R04 | 5246 52 43 35 41 --- 26 | 62 66 72 57 --- 48
R06 | 2503 33 66 75 49 --- 31 | 58 68 117 123 --- 83
R07 | 2447 17 32 64 34 51 20 | 24 25 41 42 45 22
R08 | 4488 32 48 76 31 --- 25 | 77 84 59 45 --- 53
XR10 | 3370 25 50 --- 21 --- 23 | 31 35 --- 38 --- 27
XR14 | 4651 40 32 --- 40 --- 27 | 42 36 --- 40 --- 28
R21 | 4377 42 70 83 40 --- 32 | 26 77 80 17 --- 31
R23 | 3377 22 48 340 35 --- 25 | 21 59 168 60 --- 28
R24 | 5879 33 37 304 20 481 21 | 199 200 256 228 8 209
------+------------------------------------+--------------------------------
RMS | 4431 35 48 164 34 342 |T 56 69 102 66 26 55
WRMS | 4431 33 49 64 34 342 |NE 56 69 102 66 26 55
MEDI | 4488 33 43 76 34 51 |MD 42 66 72 45 8 33
Table 3.1439.2 GPS week: 1439 Day: 2 MJD: 54319
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5294 49 36 59 43 --- 26 | 70 57 75 33 --- 44
R03 | 7880 38 30 75 37 --- 25 | 35 52 90 34 --- 27
R04 | 2117 30 35 58 16 --- 19 | 47 57 66 38 --- 40
R06 | 4568 37 96 76 61 --- 39 | 22 128 65 76 --- 44
R07 | 2730 18 32 35 21 76 14 | 24 31 40 32 50 22
R08 | 3469 25 52 84 39 --- 27 | 51 85 76 42 --- 53
XR10 | 3134 30 28 --- 24 --- 19 | 21 28 --- 22 --- 17
XR14 | 5382 63 45 --- 44 --- 36 | 49 59 --- 58 --- 49
R21 | 6030 42 39 85 28 --- 27 | 19 58 90 51 --- 26
R23 | 3116 35 42 327 49 --- 30 | 14 55 128 50 --- 26
R24 | 7219 28 52 320 47 234 30 | 198 166 260 205 8 190
------+------------------------------------+--------------------------------
RMS | 5090 35 50 164 40 174 |T 50 70 98 58 29 48
WRMS | 5090 34 40 74 40 174 |NE 50 70 98 58 29 48
MEDI | 4568 35 39 76 39 76 |MD 35 57 76 42 8 40
Table 3.1439.3 GPS week: 1439 Day: 3 MJD: 54320
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6320 28 31 95 21 --- 24 | 48 46 65 55 --- 45
R03 |12709 29 52 64 32 --- 23 | 38 40 105 70 --- 46
R04 | 2525 19 50 76 26 --- 22 | 39 62 115 55 --- 46
R06 | 2649 18 54 43 34 --- 20 | 44 98 122 68 --- 69
R07 | 2680 29 41 41 31 94 19 | 30 57 73 49 94 27
R08 | 4555 26 35 57 20 --- 18 | 95 117 44 93 --- 84
XR10 | 2694 18 29 --- 26 --- 17 | 23 32 --- 22 --- 22
XR14 | 5839 64 61 --- 50 --- 41 | 37 54 --- 40 --- 19
R21 | 5997 18 36 58 42 --- 21 | 35 46 58 65 --- 37
R23 | 2179 54 112 287 98 --- 61 | 22 63 68 94 --- 36
R24 | 8105 37 39 328 42 346 28 | 310 332 372 332 8 324
------+------------------------------------+--------------------------------
RMS | 6229 31 55 156 44 254 |T 65 86 113 85 51 68
WRMS | 6229 31 60 63 44 254 |NE 65 86 113 85 51 68
MEDI | 4555 28 41 64 32 94 |MD 38 57 73 65 8 45
Table 3.1439.4 GPS week: 1439 Day: 4 MJD: 54321
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6958 31 31 85 31 --- 22 | 61 49 75 41 --- 39
R03 |19301 34 85 42 73 --- 35 | 46 56 92 60 --- 32
R04 | 5196 42 41 89 53 --- 30 | 49 36 103 72 --- 51
R06 | 3407 50 54 158 41 --- 38 | 40 48 66 48 --- 37
R07 | 2520 24 36 91 36 51 24 | 28 46 95 54 68 36
R08 | 3301 32 74 106 25 --- 30 | 47 80 52 43 --- 39
XR10 | 3238 24 31 --- 26 --- 18 | 28 46 --- 61 --- 42
XR14 | 4303 26 70 --- 27 --- 28 | 30 64 --- 24 --- 24
R21 | 6873 12 44 88 28 --- 21 | 26 38 95 41 --- 25
R23 | 3356 41 96 327 87 --- 52 | 17 53 38 65 --- 33
R24 | 8779 55 76 296 33 --- 38 | 213 264 281 245 --- 232
------+------------------------------------+--------------------------------
RMS | 8249 38 64 171 50 51 |T 53 70 99 68 68 53
WRMS | 8249 34 61 133 50 51 |NE 53 70 99 68 68 53
MEDI | 4303 32 54 91 33 51 |MD 40 49 92 54 68 37
Table 3.1439.5 GPS week: 1439 Day: 5 MJD: 54322
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6983 64 33 61 29 --- 25 | 36 61 62 53 --- 47
R03 |51133 69 44 64 55 --- 32 | 33 49 80 40 --- 28
R04 | 5006 57 39 102 28 --- 28 | 41 37 63 36 --- 32
R06 | 5294 53 43 93 32 --- 28 | 47 83 66 61 --- 60
R07 | 3238 40 26 58 27 39 19 | 30 33 68 35 39 29
R08 | 5352 40 77 142 24 --- 37 | 79 107 63 56 --- 71
XR10 | 4672 28 31 --- 20 --- 18 | 25 37 --- 29 --- 25
XR14 | 4905 42 31 --- 25 --- 22 | 49 36 --- 44 --- 36
R21 | 9254 39 28 83 22 --- 21 | 30 36 64 55 --- 36
R23 | 4259 33 71 390 55 --- 40 | 18 29 70 40 --- 24
R24 | 7572 30 30 271 26 --- 20 | 405 402 440 424 --- 408
------+------------------------------------+--------------------------------
RMS |18002 49 47 177 35 39 |T 72 82 108 79 39 72
WRMS |18002 52 53 96 35 39 |NE 72 82 108 79 39 72
MEDI | 5294 40 33 93 27 39 |MD 36 37 66 44 39 36
Table 3.1439.6 GPS week: 1439 Day: 6 MJD: 54323
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 8666 33 41 75 38 --- 24 | 58 57 57 43 --- 44
R03 |17006 84 34 236 32 --- 48 | 47 70 106 55 --- 52
R04 | 4146 56 22 37 25 --- 20 | 57 33 68 58 --- 46
R06 | 6667 42 38 99 25 --- 25 | 61 77 91 61 --- 64
R07 | 4111 33 37 61 26 37 20 | 32 42 73 40 36 29
R08 | 6483 33 37 65 32 --- 21 | 49 68 78 69 --- 58
XR10 | 6706 33 30 --- 30 --- 22 | 36 28 --- 40 --- 27
XR14 | 6027 56 34 --- 27 --- 27 | 43 41 --- 37 --- 32
R21 |11291 24 47 137 21 --- 29 | 30 32 87 36 --- 25
R23 | 4392 50 29 417 47 --- 30 | 28 42 97 60 --- 30
R24 | 6741 99 80 342 38 --- 50 | 322 395 396 375 --- 362
------+------------------------------------+--------------------------------
RMS | 8673 56 43 208 32 37 |T 69 80 117 79 36 69
WRMS | 8673 42 41 81 32 37 |NE 69 80 117 79 36 69
MEDI | 6667 42 37 99 30 37 |MD 47 42 87 55 36 44
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