[IGSREPORT-16505] Wk 1489 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Aug 7 06:17:50 PDT 2008
******************************************************************************
IGS Electronic Report 07 Aug 06:18:06 PDT 2008 Message Number 16505
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1489 (Jul 20, 2008 - Jul 26, 2008)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
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 2.1489.
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:
igl1489[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1489 in the SP3 format.
igl14897.sum Combination Report for GPS Week 1489.
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 | 735.7 ns
1 | 799.5 ns
2 | 788.6 ns
3 | 781.8 ns
4 | 778.9 ns
5 | 711.8 ns
6 | 706.7 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 | ESX | R13
1 | ESX | R17
2 | ESX | R13
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 1.1489, 1a.1489).
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 2.1489.0-6)
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 3.1489.0-6).
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 1489 summary. (Jul 20, 2008 - Jul 26, 2008)
Table 1.1489.a GPS week : 1489 MJD: 54667.0-54673.0
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 64| 2 -1 -8 -15 1 24 -.09 34 32 | 0 -125 2326 2430
| 1 1 5 26 8 130 .04 | 0 125
cod 211| -5 0 -6 -4 24 3 -.08 31 25 | --- --- --- ---
| 2 4 5 24 41 106 .04 | --- ---
esx 118| 6 0 12 63 -39 -35 .47 195 58 | 4324 4436 6331 13756
| 2 6 13 84 43 94 .14 | 35298 5709
iac n/a| 1 1 15 -35 9 -45 -.01 34 34 | 757506 -1476 6129 13251
| 1 2 14 43 32 80 .04 | 38514 2470
mcc n/a| 0 3 78 59 26 -935 .86 469 469 | --- --- --- ---
| 20 10 12 210 131 1064 .77 | --- ---
Table 1.1489.b GPS week : 1489 MJD: 54667.0-54673.0
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 | --- --- 0 0 0 0 0 |
R04 | 14 23 24 16 23 26 22 |
R06 | 28 21 14 21 22 19 23 |
R07 | 32 25 24 31 24 24 38 |
R10 | 24 11 14 21 16 17 16 |
R11 | 24 29 21 24 20 19 20 |
R13 | 17 35 35 24 25 21 19 |
R14 | 12 19 16 17 18 14 9 |
R15 | 18 18 18 20 26 26 24 |
R17 | 36 20 50 41 44 49 37 |
R19 | 42 27 16 18 22 63 44 |
R20 | 17 12 17 18 17 19 33 |
R23 | 18 22 34 33 27 32 19 |
R24 | 15 12 20 15 14 15 9 |
Table 1.1489.c GPS week : 1489 MJD: 54667.0-54673.0
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 1489 0 | 306 -4 581 1729 2360 -11880 96.0 3749 3749 | 735662 0
brd 1489 1 | -195 -197 417 1000 3479 -16710 97.2 >>>>> >>>>> | 799487 0
brd 1489 2 | -173 -194 396 -445 -5370 -15400 99.7 3645 3645 | 788564 0
brd 1489 3 | 5 141 299 3198 -338 -13670 97.5 3401 3401 | 781809 0
brd 1489 4 | -65 -3 290 1420 -2824 -8240 102.1 3910 3910 | 778872 0
brd 1489 5 | 6 -56 182 192 -547 -11340 98.8 3417 3417 | 711809 0
brd 1489 6 | 134 -118 612 2975 -314 -13990 99.8 3766 3766 | 706725 0
-------------+------------------------------------------------------------+----------------
brd 1489 mean| 2 -61 397 1438 -507 -13032 98.7 >>>>> >>>>> | 757561 0
brd 1489 sdev| 175 120 156 1343 2977 2817 2.0 >>>>> >>>>> | 38553 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 2.1489.0 GPS week: 1489 Day: 0 MJD: 54667
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 64| 2 0 -2 -49 -2 67 -.10 31 30 | 0 -207 2288 2372
cod 211| -6 -6 -5 11 -20 -169 -.09 37 30 | --- --- --- ---
esx 118| 2 3 -5 137 -2 108 .54 313 61 | -42130 -2479 6100 11156
iac n/a| 2 -1 10 -36 -1 -52 -.04 32 32 | 737501 -4126 5833 11112
mcc n/a| 7 -3 72 -19 -246 -563 2.24 663 663 | --- --- --- ---
Table 2.1489.1 GPS week: 1489 Day: 1 MJD: 54668
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 64| 1 0 -6 -59 10 159 -.02 32 27 | 0 -10 2006 2066
cod 211| -4 -3 -4 0 12 -96 -.12 25 20 | --- --- --- ---
esx 118| 6 11 -1 37 -42 -130 .59 143 54 | 25912 9127 5578 13610
iac n/a| 3 3 14 5 35 29 .01 30 30 | 796222 2061 5476 12973
mcc n/a| -19 23 92 480 50 -368 1.47 859 859 | --- --- --- ---
Table 2.1489.2 GPS week: 1489 Day: 2 MJD: 54669
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 64| 2 0 -12 -1 10 -231 -.07 37 34 | 0 -151 2481 2566
cod 211| -2 -2 -1 12 -21 60 -.03 32 27 | --- --- --- ---
esx 118| 8 -2 15 -50 -51 86 .64 535 58 | 27737 10229 6409 14942
iac n/a| 0 1 13 -18 7 59 .02 29 29 | 791703 -2975 6239 15381
mcc n/a| 25 1 96 -138 38 -1168 .46 227 227 | --- --- --- ---
Table 2.1489.3 GPS week: 1489 Day: 3 MJD: 54670
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 64| 3 -3 -2 7 -12 -28 -.09 35 31 | 0 19 2173 2333
cod 211| -5 0 -8 18 62 135 -.11 33 24 | --- --- --- ---
esx 118| 7 5 20 -24 35 -59 .49 71 54 | 31421 9688 7906 14578
iac n/a| 0 3 8 -24 -12 -57 -.05 35 35 | 782535 -1831 7855 14309
mcc n/a| 4 12 78 -138 83 -306 .05 289 289 | --- --- --- ---
Table 2.1489.4 GPS week: 1489 Day: 4 MJD: 54671
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 64| 0 -1 -17 1 1 141 -.13 31 29 | 0 -3 2697 2766
cod 211| -2 5 -17 -2 80 -15 -.03 28 24 | --- --- --- ---
esx 118| 10 0 12 181 -94 -119 .23 81 59 | 43033 5478 6315 16078
iac n/a| 1 3 47 -126 -46 -136 -.05 42 42 | 777443 848 5887 15455
mcc n/a| -9 1 62 84 36 -374 .97 355 355 | --- --- --- ---
Table 2.1489.5 GPS week: 1489 Day: 5 MJD: 54672
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 64| 2 -3 -11 -3 7 44 -.06 36 36 | 0 -269 2361 2485
cod 211| -6 5 -2 -22 54 32 -.05 30 25 | --- --- --- ---
esx 118| 8 -1 32 110 -70 -73 .33 127 62 | -28284 -3226 6251 13742
iac n/a| 1 0 7 -41 30 -3 .04 37 37 | 711608 -4203 5912 12938
mcc n/a| -26 -4 69 41 186 -507 .57 444 444 | --- --- --- ---
Table 2.1489.6 GPS week: 1489 Day: 6 MJD: 54673
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 64| 1 -2 -5 -4 -3 15 -.15 36 36 | 0 -255 2276 2425
cod 211| -9 1 -3 -51 1 79 -.11 32 21 | --- --- --- ---
esx 118| 5 -9 12 52 -47 -56 .47 97 58 | -27421 2235 5764 12191
iac n/a| 2 3 6 -4 49 -156 .01 35 35 | 705532 -110 5703 10593
mcc n/a| 22 -4 78 106 34 -3258 .22 448 448 | --- --- --- ---
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 3.1489.0 GPS week: 1489 Day: 0 MJD: 54667
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3075 20 31 33 16 --- 14 | 137 145 146 148 --- 141
R06E | 2446 43 34 104 26 --- 27 | 122 124 207 142 --- 135
R07 | 3696 43 66 58 52 --- 31 | 35 60 59 51 --- 40
R10 | 4608 16 58 53 35 --- 23 | 22 49 42 31 --- 24
R11 | 6795 16 37 97 27 187 24 | 31 30 105 39 69 34
R13 | 3139 22 20 1088 27 --- 16 | 29 29 884 37 --- 23
R14 | 1495 12 21 34 18 --- 11 | 48 36 44 43 --- 38
R15 | 2648 29 24 53 29 174 18 | 35 21 49 31 50 25
R17 | 6968 56 41 108 57 --- 35 | 21 62 138 44 --- 36
R19 | 1888 18 41 200 33 --- 42 | 34 30 121 44 --- 30
R20 | 2957 32 17 44 26 --- 16 | 34 23 38 38 --- 27
R23 | 1017 28 29 52 24 --- 18 | 66 64 52 63 --- 55
R24 | 2266 33 16 35 18 1121 14 | 126 144 160 146 210 140
------+------------------------------------+--------------------------------
RMS | 3748 31 37 313 32 663 |T 56 62 157 65 109 57
WRMS | 3748 30 30 61 32 663 |NE 43 49 153 51 109 42
MEDI | 2957 28 31 53 27 187 |MD 35 49 105 44 69 36
Table 3.1489.1 GPS week: 1489 Day: 1 MJD: 54668
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |>>>>> 44 32 49 38 --- 22 | 104 148 120 114 --- 120
R06E |>>>>> 43 23 61 29 --- 20 | 84 106 123 90 --- 94
R07 | 2691 50 32 77 27 --- 24 | 69 34 65 33 --- 32
R10 |>>>>> 15 17 34 17 --- 11 | 25 44 39 27 --- 29
R11 |>>>>> 18 39 121 40 198 29 | 35 28 131 37 115 24
R13 |>>>>> 33 24 164 45 --- 34 | 35 23 523 44 --- 33
R14 |>>>>> 22 13 79 28 --- 18 | 49 34 83 27 --- 34
R15 |>>>>> 19 25 71 26 226 18 | 23 24 90 32 82 24
R17 |>>>>> 36 24 422 20 --- 19 | 14 28 389 49 --- 24
R19 |>>>>> 18 18 133 32 --- 27 | 12 22 170 25 --- 16
R20 |>>>>> 22 11 19 27 --- 11 | 18 23 22 21 --- 14
R23 |>>>>> 44 30 57 26 --- 21 | 59 35 71 50 --- 40
R24 |>>>>> 12 13 35 27 1457 11 | 107 109 114 118 483 109
------+------------------------------------+--------------------------------
RMS |>>>>> 32 25 143 30 859 |T 48 50 149 51 226 45
WRMS |>>>>> 27 20 54 30 859 |NE 40 36 154 42 226 34
MEDI |>>>>> 22 24 71 27 226 |MD 35 34 114 37 115 32
Table 3.1489.2 GPS week: 1489 Day: 2 MJD: 54669
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 4 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 1780 61 34 33 25 --- 23 | 81 125 107 103 --- 101
R06 | 3128 32 19 31 15 --- 13 | 108 122 134 119 --- 116
R07 | 2279 30 35 49 50 --- 23 | 53 39 43 54 --- 33
R10 | 4815 24 27 32 19 --- 14 | 30 33 45 29 --- 24
R11 | 2952 23 22 90 18 208 20 | 22 29 72 24 99 20
R13 | 8698 56 59 1902 27 --- 35 | 23 54 9999 41 --- 32
R14 | 1749 35 16 36 23 --- 15 | 38 22 33 24 --- 18
R15 | 3612 26 17 59 29 72 17 | 39 22 68 21 98 23
R17 | 3330 34 39 232 44 --- 49 | 43 44 245 62 --- 33
R19 | 1520 15 21 57 26 --- 16 | 10 26 56 29 --- 13
R20 | 1228 30 27 37 25 --- 16 | 31 41 39 21 --- 23
R23 | 1132 50 35 134 32 --- 33 | 77 75 105 61 --- 58
R24 | 3836 31 38 56 17 326 19 | 89 94 130 102 501 95
------+------------------------------------+--------------------------------
RMS | 3645 37 32 534 29 227 |T 49 55 89 53 232 45
WRMS | 3645 34 27 58 29 227 |NE 41 43 83 42 232 33
MEDI | 2952 31 27 56 25 208 |MD 39 41 68 41 99 32
Table 3.1489.3 GPS week: 1489 Day: 3 MJD: 54670
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 10 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 1939 29 16 43 23 --- 15 | 110 99 102 83 --- 95
R06 | 5857 44 16 26 44 --- 20 | 94 94 92 98 --- 91
R07 | 2417 26 38 110 46 --- 31 | 42 46 87 37 --- 33
R10 | 2671 25 42 50 24 --- 20 | 29 49 39 29 --- 27
R11 | 2206 36 20 69 46 233 24 | 29 24 83 55 100 26
R13 | 5281 42 29 78 22 --- 24 | 51 55 309 37 --- 45
R14 | 2828 42 17 33 17 --- 16 | 57 33 41 43 --- 40
R15 | 4791 18 16 67 38 39 20 | 32 28 86 27 57 29
R17 | 3640 55 50 147 44 --- 41 | 60 68 112 44 --- 28
R19 | 1780 29 23 38 35 --- 17 | 18 27 89 34 --- 14
R20 | 1140 30 17 50 29 --- 17 | 31 35 66 38 --- 32
R23 | 2705 29 68 81 47 --- 32 | 47 94 61 31 --- 37
R24 | 3249 27 28 30 14 442 14 | 86 86 112 82 210 85
------+------------------------------------+--------------------------------
RMS | 3401 35 33 71 35 289 |T 52 56 98 49 122 44
WRMS | 3401 31 24 54 35 289 |NE 43 49 98 41 122 36
MEDI | 2705 29 20 50 35 233 |MD 47 49 87 38 100 33
Table 3.1489.4 GPS week: 1489 Day: 4 MJD: 54671
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 11 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 4771 31 30 70 39 --- 22 | 71 65 79 93 --- 67
R06 | 1820 41 28 62 33 --- 22 | 105 106 142 102 --- 101
R07 | 9552 34 34 57 50 --- 24 | 40 67 82 37 --- 39
R10 | 1579 25 17 58 20 --- 16 | 33 32 80 40 --- 30
R11 | 1911 32 16 55 46 249 20 | 29 23 61 43 88 18
R13 | 3608 21 17 105 44 --- 25 | 24 40 244 38 --- 37
R14 | 2231 31 15 55 30 --- 17 | 40 35 54 42 --- 31
R15 | 3833 14 19 100 55 63 25 | 25 36 76 36 36 30
R17 | 2314 36 52 180 55 --- 43 | 24 62 159 56 --- 42
R19 | 2320 34 25 60 46 --- 22 | 21 32 95 77 --- 27
R20 | 1894 28 25 30 37 --- 17 | 17 41 63 52 --- 25
R23 | 5126 38 44 68 48 --- 27 | 38 64 46 49 --- 31
R24 | 1383 24 18 26 28 560 13 | 51 59 74 78 246 59
------+------------------------------------+--------------------------------
RMS | 3909 31 28 81 42 355 |T 39 50 96 57 123 41
WRMS | 3909 29 24 59 42 355 |NE 31 44 94 49 123 33
MEDI | 2314 31 19 60 44 249 |MD 33 41 79 49 88 31
Table 3.1489.5 GPS week: 1489 Day: 5 MJD: 54672
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 2757 43 39 75 35 --- 25 | 71 77 72 85 --- 71
R06 | 5816 41 21 33 34 --- 19 | 73 72 74 72 --- 69
R07 | 4225 34 47 49 33 --- 23 | 24 60 50 28 --- 23
R10 | 3766 20 21 54 33 --- 16 | 41 31 56 36 --- 30
R11 | 2906 16 20 89 18 247 18 | 26 16 95 41 126 25
R13 | 1802 33 24 50 43 --- 20 | 39 42 73 37 --- 31
R14 | 2409 25 13 46 21 --- 13 | 35 37 50 32 --- 31
R15 | 2066 47 19 89 39 82 25 | 22 38 89 21 39 28
R17 | 2101 35 37 244 47 --- 48 | 37 58 256 39 --- 45
R19 | 1707 61 26 329 41 --- 63 | 29 42 306 25 --- 41
R20 | 3344 30 23 49 35 --- 18 | 54 55 83 52 --- 51
R23 | 5135 40 55 82 60 --- 32 | 46 82 64 44 --- 45
R24 | 3406 24 17 44 24 723 14 | 82 71 98 81 542 78
------+------------------------------------+--------------------------------
RMS | 3416 36 30 127 37 443 |T 44 52 105 45 235 43
WRMS | 3416 36 25 62 37 443 |NE 39 48 110 39 235 38
MEDI | 2906 34 21 54 35 247 |MD 39 55 74 39 126 41
Table 3.1489.6 GPS week: 1489 Day: 6 MJD: 54673
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 8 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 4235 44 30 60 28 --- 22 | 98 103 104 106 --- 98
R06 | 2882 47 33 45 38 --- 23 | 105 122 119 110 --- 109
R07 | 1783 39 44 169 30 --- 38 | 34 51 125 28 --- 30
R10 | 1996 29 12 42 30 --- 15 | 30 34 46 31 --- 28
R11 | 3676 30 7 84 26 454 20 | 42 26 61 33 223 26
R13 | 3131 16 30 63 31 --- 19 | 34 36 101 27 --- 29
R14 | 4147 15 9 17 21 --- 9 | 39 36 59 38 --- 39
R15 | 1526 57 25 75 15 116 24 | 23 41 60 30 64 28
R17 | 2588 32 72 40 76 --- 36 | 27 71 99 47 --- 40
R19 | 1619 46 26 208 39 --- 44 | 22 39 141 36 --- 34
R20 | 5331 37 32 142 30 --- 32 | 51 48 118 55 --- 42
R23 | 3681 31 21 58 31 --- 18 | 39 52 64 37 --- 38
R24 | 7537 10 12 20 19 619 9 | 98 100 119 106 636 102
------+------------------------------------+--------------------------------
RMS | 3766 36 32 97 35 448 |T 49 58 93 52 307 49
WRMS | 3766 36 21 57 35 448 |NE 39 48 90 42 307 39
MEDI | 3131 32 25 60 30 454 |MD 39 48 101 37 223 38
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