[IGSREPORT-16571] Wk 1492 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Aug 28 06:22:30 PDT 2008
******************************************************************************
IGS Electronic Report 28 Aug 06:22:33 PDT 2008 Message Number 16571
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1492 (Aug 10, 2008 - Aug 16, 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 2.1492.
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:
igl1492[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1492 in the SP3 format.
igl14927.sum Combination Report for GPS Week 1492.
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 | 659.4 ns
1 | 733.9 ns
2 | 693.2 ns
3 | 673.5 ns
4 | 669.9 ns
5 | 661.4 ns
6 | 711.5 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 | R07 R11 R19
1 | ESX | R07
3 | ESX | R04
4 | ESX | R11 R13
6 | ESX | R17
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 1.1492, 1a.1492).
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 2.1492.0-6)
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 3.1492.0-6).
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 1492 summary. (Aug 10, 2008 - Aug 16, 2008)
Table 1.1492.a GPS week : 1492 MJD: 54688.0-54694.0
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 2 -7 -5 27 53 -.13 35 34 | 0 -155 2611 2741
| 2 2 4 42 34 102 .06 | 0 227
cod 214| -4 -2 -8 -12 -4 16 -.11 28 26 | --- --- --- ---
| 3 2 4 27 36 39 .04 | --- ---
esx 113| -3 -3 9 -13 -87 84 .45 172 53 | -19081 -2008 14838 28342
| 4 3 8 96 69 165 .11 | 31716 6211
iac n/a| 4 3 11 3 32 -63 -.04 30 30 | 687026 -3293 9424 20048
| 3 1 5 36 38 43 .09 | 28511 4628
mcc n/a| 3 -5 86 8 -8 428 .27 241 241 | --- --- --- ---
| 12 18 15 185 276 1484 .58 | --- ---
Table 1.1492.b GPS week : 1492 MJD: 54688.0-54694.0
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 0 0 |
R04 | 19 22 18 21 16 16 16 |
R06 | 25 20 32 19 25 14 25 |
R07 | 18 28 23 27 32 26 31 |
R09 | 0 0 0 0 0 0 0 |
R10 | 21 16 19 16 15 16 18 |
R11 | 16 20 18 22 18 18 21 |
R13 | 17 24 21 25 20 24 26 |
R14 | 14 18 12 13 10 20 20 |
R15 | 20 19 21 19 27 18 22 |
R17 | 26 18 21 17 23 25 20 |
R19 | 15 28 20 20 11 15 18 |
R20 | 22 21 13 20 18 19 16 |
R23 | 22 24 22 20 27 34 34 |
R24 | 18 15 18 17 15 17 21 |
Table 1.1492.c GPS week : 1492 MJD: 54688.0-54694.0
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 1492 0 | -121 201 308 -5866 -585 -33700 98.8 3310 3310 | 659425 0
brd 1492 1 | 369 -12 531 -1781 1213 -30250 100.9 >>>>> >>>>> | 733874 0
brd 1492 2 | -308 -177 305 313 -751 -37800 91.0 3410 3410 | 693168 0
brd 1492 3 | -27 -36 137 -1599 1010 -32119 96.1 4215 4215 | 673482 0
brd 1492 4 | -333 -225 293 1126 -3002 -38100 95.5 3747 3747 | 669897 0
brd 1492 5 | 225 172 345 -2670 1193 -33400 99.2 5218 5218 | 661358 0
brd 1492 6 | -157 226 289 -3736 -138 -27920 93.0 5507 5507 | 711547 0
-------------+------------------------------------------------------------+----------------
brd 1492 mean| -50 21 315 -2030 -151 -33327 96.4 >>>>> >>>>> | 686107 0
brd 1492 sdev| 263 183 116 2371 1510 3721 3.5 >>>>> >>>>> | 28063 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 2.1492.0 GPS week: 1492 Day: 0 MJD: 54688
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| 4 0 -6 22 27 -96 -.20 34 30 | 0 -628 2885 3045
cod 214| -10 -6 -8 -46 44 27 -.18 25 26 | --- --- --- ---
esx 113| -2 0 10 -51 1 147 .38 603 66 | -52150 -4514 9981 20131
iac n/a| 8 4 10 17 4 -15 .13 28 28 | 664520 -9663 9286 15276
mcc n/a| 18 -40 93 222 487 3706 1.26 282 282 | --- --- --- ---
Table 2.1492.1 GPS week: 1492 Day: 1 MJD: 54689
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 2 -18 -36 -16 134 -.03 36 34 | 0 -57 2622 2725
cod 214| -7 -3 -5 -20 42 -11 -.09 29 28 | --- --- --- ---
esx 113| -2 0 19 182 -57 140 .43 86 65 | 25719 -1809 8853 20400
iac n/a| 5 2 6 28 3 -93 -.01 26 26 | 736039 -4022 6966 14807
mcc n/a| 10 2 114 -269 -103 -778 .15 338 338 | --- --- --- ---
Table 2.1492.2 GPS week: 1492 Day: 2 MJD: 54690
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| 4 0 -5 45 37 40 -.16 30 28 | 0 -172 2866 3019
cod 214| -6 -4 -4 -10 -21 52 -.10 27 23 | --- --- --- ---
esx 113| -9 -5 -4 -86 -132 103 .67 62 57 | -13478 -7368 26449 38396
iac n/a| 1 2 11 -17 42 -48 -.03 27 27 | 691266 2692 7714 19334
mcc n/a| -21 4 84 -45 -407 -304 .72 244 244 | --- --- --- ---
Table 2.1492.3 GPS week: 1492 Day: 3 MJD: 54691
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 3 -7 -2 7 0 -.15 29 28 | 0 78 2728 2872
cod 214| -4 -4 -5 -39 -3 -14 -.08 32 31 | --- --- --- ---
esx 113| 4 -6 18 -103 -157 364 .34 162 43 | -40952 6385 11225 21957
iac n/a| 1 2 4 30 27 -125 -.04 29 29 | 673740 2088 7652 12411
mcc n/a| -2 20 80 78 -138 -53 -.07 182 182 | --- --- --- ---
Table 2.1492.4 GPS week: 1492 Day: 4 MJD: 54692
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 1 -8 0 34 0 -.18 36 37 | 0 -5 2434 2533
cod 214| 0 -1 -7 -11 -26 -20 -.09 28 25 | --- --- --- ---
esx 113| -3 -3 7 -22 -119 21 .52 160 47 | -33320 -6011 14094 25269
iac n/a| 3 4 12 36 59 -20 -.10 31 31 | 673394 -6787 12167 18995
mcc n/a| 7 -10 74 -138 141 238 -.35 188 188 | --- --- --- ---
Table 2.1492.5 GPS week: 1492 Day: 5 MJD: 54693
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 -3 -81 93 218 -.12 38 38 | 0 -159 2382 2494
cod 214| -2 0 -9 29 -55 0 -.12 25 23 | --- --- --- ---
esx 113| -1 -5 13 -45 -151 -172 .38 50 41 | -41682 -7605 22040 55358
iac n/a| 7 0 14 -6 98 -36 -.12 35 35 | 656997 -5934 14967 47048
mcc n/a| 4 -7 65 -25 31 140 -.29 288 288 | --- --- --- ---
Table 2.1492.6 GPS week: 1492 Day: 6 MJD: 54694
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 5 -5 18 7 78 -.09 43 39 | 0 -147 2364 2499
cod 214| -2 0 -16 13 -7 83 -.09 30 27 | --- --- --- ---
esx 113| -6 -1 2 32 3 -13 .44 77 49 | 22293 6862 11226 16885
iac n/a| 7 4 21 -66 -10 -104 -.10 31 31 | 713229 -1427 7217 12470
mcc n/a| 6 -7 90 236 -72 53 .45 166 166 | --- --- --- ---
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 3.1492.0 GPS week: 1492 Day: 0 MJD: 54688
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 10 --- --- --- 0 | --- 616 --- --- --- 616
R04 | 2197 45 34 34 19 --- 19 | 58 50 53 24 --- 33
R06 | 4024 54 28 64 34 --- 24 | 78 92 78 80 --- 79
R07 | 1943 18 28 198 26 --- 18 | 42 51 121 32 --- 33
XR09 |28818 --- --- 12 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 2990 20 24 82 23 --- 21 | 14 39 48 25 --- 17
R11 | 1440 25 23 2146 21 169 16 | 20 30 9999 45 32 28
R13 | 6328 22 19 53 27 --- 16 | 33 37 68 22 --- 28
R14 | 3160 14 25 32 27 --- 14 | 16 31 42 23 --- 22
R15 | 2652 30 19 73 22 313 19 | 20 25 74 26 100 24
R17 | 1951 49 27 80 36 --- 26 | 45 52 59 39 --- 40
R19 | 3657 20 19 241 21 --- 14 | 55 43 105 47 --- 44
R20 | 3672 27 32 54 40 --- 21 | 13 33 41 40 --- 17
R23 | 1896 34 25 63 37 --- 21 | 76 89 109 97 --- 87
R24 | 3903 48 23 39 17 335 18 | 165 180 186 175 567 173
------+------------------------------------+--------------------------------
RMS | 3309 34 25 603 28 282 |T 48 97 82 51 233 88
WRMS | 3309 30 26 66 28 282 |NE 48 97 82 51 233 88
MEDI | 2990 27 24 63 26 313 |MD 42 43 68 39 100 33
Table 3.1492.1 GPS week: 1492 Day: 1 MJD: 54689
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 6 --- --- --- 0 | --- 881 --- --- --- 880
R04 |>>>>> 54 30 46 30 --- 22 | 64 51 74 19 --- 33
R06 |>>>>> 35 34 50 24 --- 19 | 75 100 132 82 --- 84
R07 | 1408 35 47 215 31 --- 27 | 27 49 158 32 --- 27
XR09 |>>>>> --- --- 19 --- --- 0 | --- --- 9999 --- --- 9999
R10 |>>>>> 39 20 27 26 --- 16 | 13 18 22 26 --- 13
R11 |>>>>> 34 14 70 27 127 19 | 21 28 399 38 72 24
R13 |>>>>> 22 30 88 29 --- 23 | 14 27 106 30 --- 21
R14 |>>>>> 29 25 58 17 --- 17 | 14 17 52 21 --- 10
R15 |>>>>> 35 38 40 19 78 18 | 31 38 66 21 64 23
R17 |>>>>> 24 25 49 31 --- 18 | 62 56 58 44 --- 47
R19 |>>>>> 50 18 109 22 --- 27 | 64 38 54 48 --- 39
R20 |>>>>> 32 19 75 26 --- 20 | 19 20 71 34 --- 19
R23 |>>>>> 34 33 77 33 --- 23 | 62 87 89 77 --- 73
R24 |>>>>> 34 23 36 19 566 15 | 126 123 143 123 430 124
------+------------------------------------+--------------------------------
RMS |>>>>> 36 29 86 26 338 |T 45 109 109 45 188 101
WRMS |>>>>> 34 28 65 26 338 |NE 45 109 109 45 188 101
MEDI |>>>>> 34 25 50 26 127 |MD 31 38 74 34 72 27
Table 3.1492.2 GPS week: 1492 Day: 2 MJD: 54690
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 | 2961 26 24 46 34 --- 18 | 47 52 163 22 --- 37
XR06 | 3369 55 39 --- 42 --- 31 | 85 129 --- 120 --- 107
R07 | 1751 29 35 80 25 --- 22 | 28 44 68 31 --- 26
XR09 |52937 --- --- 16 --- --- 0 | --- --- 9999 --- --- 9999
XR10 | 2583 27 20 --- 33 --- 19 | 14 33 --- 31 --- 17
R11 | 1976 31 23 60 23 163 18 | 30 25 268 24 26 22
R13 | 3144 26 31 51 42 --- 21 | 19 32 70 27 --- 20
R14 | 6885 25 18 30 14 --- 12 | 16 18 41 23 --- 16
R15 | 3322 25 29 67 34 80 21 | 25 33 59 35 46 19
R17 | 1676 31 17 87 18 --- 20 | 20 31 83 29 --- 26
R19 | 2355 26 15 86 19 --- 20 | 43 44 56 37 --- 34
XR20 | 2799 21 13 --- 19 --- 12 | 22 14 --- 28 --- 13
R23 | 2953 46 35 43 31 --- 22 | 44 57 73 79 --- 55
R24 | 3892 33 33 45 20 381 18 | 155 192 177 160 249 168
------+------------------------------------+--------------------------------
RMS | 3410 30 27 62 27 244 |T 42 54 105 49 107 43
WRMS | 3410 28 23 57 27 244 |NE 42 54 105 49 107 43
MEDI | 2953 27 23 51 25 163 |MD 28 33 70 31 46 26
Table 3.1492.3 GPS week: 1492 Day: 3 MJD: 54691
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 5 --- --- --- 0 | --- 9999 --- --- --- 9999
R04 | 2081 29 20 555 35 --- 21 | 43 34 408 30 --- 24
R06 | 2837 41 27 38 25 --- 19 | 95 105 99 114 --- 100
R07 | 1794 30 47 72 42 --- 26 | 28 41 59 36 --- 21
XR09 |29807 --- --- 26 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 1848 18 40 23 24 --- 16 | 10 50 25 22 --- 19
R11 | 6680 33 20 69 30 182 21 | 20 23 249 44 42 20
R13 | 1409 15 47 54 48 --- 24 | 37 53 88 28 --- 33
R14 | 4363 10 23 37 17 --- 12 | 17 22 43 34 --- 21
R15 | 2890 12 36 63 22 80 19 | 38 33 68 24 38 25
R17 | 8978 30 32 38 21 --- 17 | 29 45 81 28 --- 39
R19 | 1452 35 19 69 15 --- 20 | 43 29 86 25 --- 25
R20 | 2626 34 27 53 30 --- 20 | 13 26 50 27 --- 17
R23 | 5713 42 26 42 30 --- 20 | 33 59 75 61 --- 46
R24 | 3958 23 32 49 17 246 17 | 139 144 166 148 136 145
------+------------------------------------+--------------------------------
RMS | 4215 29 32 162 29 182 |T 41 51 115 47 72 41
WRMS | 4215 28 31 43 29 182 |NE 41 51 115 47 72 41
MEDI | 2837 30 27 49 25 182 |MD 33 41 81 30 42 25
Table 3.1492.4 GPS week: 1492 Day: 4 MJD: 54692
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 5 --- --- --- 0 | --- 373 --- --- --- 373
R04 | 1826 22 13 60 16 --- 16 | 26 28 192 39 --- 32
R06 | 4646 36 30 76 35 --- 24 | 85 85 134 88 --- 87
R07 | 2087 46 50 67 58 --- 31 | 55 61 65 57 --- 32
XR09 |24035 --- --- 11 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 3956 21 24 39 21 --- 15 | 23 45 38 24 --- 27
R11 | 3604 27 27 135 20 224 17 | 33 56 230 40 93 40
R13 | 1837 19 28 534 32 --- 19 | 37 46 458 20 --- 30
R14 | 4262 16 15 27 16 --- 10 | 26 27 40 26 --- 23
R15 | 3335 58 28 38 58 84 27 | 19 20 50 33 36 21
R17 | 3536 52 34 60 16 --- 23 | 35 41 51 36 --- 25
R19 | 1627 21 13 26 17 --- 10 | 51 47 64 34 --- 40
R20 | 2631 46 18 36 25 --- 17 | 18 27 44 25 --- 19
R23 | 5836 43 28 90 25 --- 26 | 37 61 119 60 --- 58
R24 | 5978 26 32 25 19 221 15 | 153 162 155 144 160 152
------+------------------------------------+--------------------------------
RMS | 3746 36 28 160 31 188 |T 46 77 126 48 96 68
WRMS | 3746 37 25 47 31 188 |NE 46 77 126 48 96 68
MEDI | 3536 27 27 39 21 221 |MD 35 46 65 36 93 32
Table 3.1492.5 GPS week: 1492 Day: 5 MJD: 54693
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 7 --- --- --- 0 | --- 212 --- --- --- 210
R04 | 3221 33 23 30 28 --- 16 | 28 34 61 26 --- 25
R06 | 3603 22 22 36 18 --- 14 | 70 91 74 79 --- 80
R07 | 1099 48 26 63 51 --- 26 | 26 40 96 53 --- 37
XR09 |43250 --- --- 16 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 4963 33 22 30 28 --- 16 | 25 39 24 21 --- 21
R11 | 6673 27 23 37 36 149 17 | 37 44 211 44 45 35
R13 |11744 36 25 60 45 --- 23 | 14 40 91 50 --- 22
R14 | 7157 44 16 42 38 --- 19 | 13 33 67 59 --- 36
R15 | 4892 32 13 28 48 41 18 | 31 30 57 29 40 29
R17 | 3569 50 23 73 32 --- 25 | 21 42 85 24 --- 34
R19 | 2104 21 13 45 25 --- 15 | 34 43 87 31 --- 37
R20 | 995 40 27 34 27 --- 18 | 21 44 53 18 --- 24
R23 | 3993 45 54 95 33 --- 33 | 39 42 91 53 --- 41
R24 | 3601 43 18 30 27 475 17 | 250 274 298 284 149 275
------+------------------------------------+--------------------------------
RMS | 5217 37 25 50 35 288 |T 46 72 99 59 78 64
WRMS | 5217 38 23 41 35 288 |NE 46 72 99 59 78 64
MEDI | 3603 36 22 36 32 149 |MD 28 42 85 44 45 35
Table 3.1492.6 GPS week: 1492 Day: 6 MJD: 54694
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 | ---- --- 10 --- --- --- 0 | --- 234 --- --- --- 235
R04 | 3766 19 29 36 23 --- 15 | 32 47 48 26 --- 31
R06 | 4012 54 43 50 23 --- 24 | 146 90 112 100 --- 107
R07 | 2833 66 21 97 29 --- 30 | 45 44 112 28 --- 37
XR09 |15631 --- --- 7 --- --- 0 | --- --- 9999 --- --- 9999
R10 | 4211 26 25 52 21 --- 17 | 23 54 41 23 --- 33
R11 |14013 56 15 40 33 161 21 | 29 24 237 34 37 20
R13 | 4179 37 20 85 42 --- 26 | 18 31 80 24 --- 26
R14 | 7790 55 17 26 35 --- 20 | 25 53 41 60 --- 40
R15 | 4407 35 32 54 32 64 21 | 22 48 49 46 35 29
R17 | 3556 33 25 188 29 --- 20 | 30 42 104 34 --- 30
R19 | 1879 32 19 54 25 --- 18 | 42 37 72 44 --- 38
R20 | 1333 34 16 21 35 --- 16 | 20 31 31 23 --- 17
R23 | 2096 37 62 86 48 --- 34 | 53 91 106 86 --- 72
R24 | 4682 47 27 54 19 230 20 | 249 287 301 284 148 279
------+------------------------------------+--------------------------------
RMS | 5507 43 30 77 31 166 |T 56 79 102 62 73 71
WRMS | 5507 39 27 49 31 166 |NE 56 79 102 62 73 71
MEDI | 4012 37 21 52 29 161 |MD 30 47 80 34 37 33
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