[IGSREPORT-17132] Wk 1517 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Feb 19 05:35:30 PST 2009
******************************************************************************
IGS Electronic Report 19 Feb 05:35:32 PST 2009 Message Number 17132
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1517 (Feb 01, 2009 - Feb 07, 2009)
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 2.1517.
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:
igl1517[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1517 in the SP3 format.
igl15177.sum Combination Report for GPS Week 1517.
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 | 260.1 ns
1 | 243.7 ns
2 | 236.1 ns
3 | 235.4 ns
4 | 232.9 ns
5 | 229.2 ns
6 | 236.0 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
----+--------+---------------
6 | BKG | R18
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 1.1517, 1a.1517).
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 2.1517.0-6)
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 3.1517.0-6).
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 1517 summary. (Feb 01, 2009 - Feb 07, 2009)
Table 1.1517.a GPS week : 1517 MJD: 54863.0-54869.0
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 98| 0 -1 3 0 20 -48 -.08 40 28 | 0 -12 2182 2251
| 1 2 5 17 58 211 .06 | 0 199
cod 235| -1 0 -2 21 -18 87 -.13 18 15 | --- --- --- ---
| 1 1 2 20 20 62 .05 | --- ---
esx 128| 1 0 3 -7 11 -6 .40 31 26 | 112843 1116 5957 11648
| 0 2 3 25 52 127 .04 | 5920 4923
iac n/a| 0 0 -2 -30 -4 -86 -.08 24 24 | 238984 -523 5918 11089
| 1 1 4 14 21 92 .04 | 9599 2009
mcc n/a| -3 0 -5 -23 -43 1163 .34 215 215 | --- --- --- ---
| 17 7 9 94 169 670 .59 | --- ---
Table 1.1517.b GPS week : 1517 MJD: 54863.0-54869.0
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
------+------------------------------------+------------------------------------------
R02 | 22 28 17 13 9 13 11 |
R03 | 17 19 10 12 10 9 12 |
R04 | 20 11 13 10 16 18 13 |
R07 | 12 7 12 12 14 11 15 |
R08 | --- --- 0 0 0 74 101 |
R10 | 11 8 13 14 13 11 12 |
R11 | 14 15 12 10 13 14 10 |
R13 | 11 13 16 15 11 12 10 |
R14 | 9 12 14 10 12 10 11 |
R15 | 10 10 9 14 11 19 14 |
R17 | 16 21 14 14 13 16 14 |
R18 | 10 7 13 13 12 10 24 |
R19 | 10 9 9 14 11 13 24 |
R20 | 18 15 18 16 24 20 18 |
R21 | 9 9 11 11 15 16 37 |
R22 | 12 11 10 12 12 13 24 |
R23 | 18 17 17 20 15 22 21 |
R24 | 13 31 28 19 19 17 18 |
Table 1.1517.c GPS week : 1517 MJD: 54863.0-54869.0
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 1517 0 | 18 -102 29 -202 1306 -10830 91.3 2184 2184 | 260098 0
brd 1517 1 | 137 -81 -72 363 -401 -9639 91.6 1933 1933 | 243736 0
brd 1517 2 | 0 114 -161 41 -1538 -12910 92.2 1856 1856 | 236107 0
brd 1517 3 | 71 21 -138 -1996 -3533 -14850 89.7 1920 1920 | 235398 0
brd 1517 4 | -67 -148 -117 -3484 -2822 -16810 88.0 2025 2025 | 232860 0
brd 1517 5 | 213 -18 -4 -5 2466 -14610 87.8 2389 2389 | 229187 0
brd 1517 6 | -90 103 91 -2277 2261 -15810 90.0 2248 2248 | 235995 0
-------------+------------------------------------------------------------+----------------
brd 1517 mean| 40 -15 -53 -1079 -323 -13637 90.1 2079 2079 | 239054 0
brd 1517 sdev| 108 101 94 1489 2420 2633 1.7 197 197 | 10262 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 2.1517.0 GPS week: 1517 Day: 0 MJD: 54863
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 98| 1 1 -2 4 123 110 -.13 32 28 | 0 -350 2080 2130
cod 235| -3 0 -4 28 -31 48 -.12 16 13 | --- --- --- ---
esx 128| 0 -3 8 -23 -32 -13 .38 29 25 | 113055 3304 5650 12976
iac n/a| 3 1 0 -50 -10 -151 -.12 24 24 | 258042 -1405 5683 11380
mcc n/a| 7 5 -10 -26 -202 2213 .78 253 253 | --- --- --- ---
Table 2.1517.1 GPS week: 1517 Day: 1 MJD: 54864
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 98| -1 1 2 23 51 -17 -.05 30 23 | 0 -77 2223 2296
cod 235| -2 -1 -3 53 3 16 -.05 22 14 | --- --- --- ---
esx 128| 1 -1 5 -47 -26 -108 .46 38 27 | 103529 9954 6485 9803
iac n/a| 0 2 -1 -51 -18 34 -.09 22 22 | 243719 495 6500 10129
mcc n/a| -5 0 8 -68 21 1845 -.60 170 170 | --- --- --- ---
Table 2.1517.2 GPS week: 1517 Day: 2 MJD: 54865
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 98| 1 -1 6 11 -7 99 -.10 26 22 | 0 77 2350 2424
cod 235| 0 1 -2 12 0 40 -.14 17 16 | --- --- --- ---
esx 128| 2 -3 0 9 66 -123 .45 39 30 | 110489 2474 6415 12793
iac n/a| 1 0 0 -28 -25 -25 -.11 22 22 | 237966 -2388 6115 12728
mcc n/a| 3 12 -17 -157 -120 488 .85 339 339 | --- --- --- ---
Table 2.1517.3 GPS week: 1517 Day: 3 MJD: 54866
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 98| -1 -2 12 -8 -63 21 -.06 30 26 | 0 146 2194 2262
cod 235| -1 3 0 9 0 135 -.20 18 18 | --- --- --- ---
esx 128| 1 0 1 -3 53 -56 .41 22 20 | 118358 -1815 5228 11912
iac n/a| 0 0 -11 -18 -27 -124 -.10 24 24 | 237093 -1588 5245 9696
mcc n/a| 13 -7 -7 143 169 611 .53 212 212 | --- --- --- ---
Table 2.1517.4 GPS week: 1517 Day: 4 MJD: 54867
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 98| 1 -2 5 -28 -12 97 .02 33 28 | 0 -25 2422 2473
cod 235| -2 1 -3 34 -32 148 -.13 16 14 | --- --- --- ---
esx 128| 0 0 8 29 55 -77 .37 30 27 | 121524 -964 5794 10785
iac n/a| 1 0 -5 -16 13 -232 -.06 22 22 | 231420 -1295 5790 10078
mcc n/a| 11 2 -10 -67 -300 609 -.03 293 293 | --- --- --- ---
Table 2.1517.5 GPS week: 1517 Day: 5 MJD: 54868
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 98| 0 -3 3 8 13 -467 -.12 29 28 | 0 262 2200 2317
cod 235| 1 1 -1 24 -48 172 -.14 19 17 | --- --- --- ---
esx 128| 2 1 1 -23 28 219 .35 27 25 | 109416 641 6109 10340
iac n/a| -2 1 -1 -19 28 -11 -.01 27 27 | 229423 3589 6117 10676
mcc n/a| -22 -2 4 -21 104 1016 -.10 106 106 | --- --- --- ---
Table 2.1517.6 GPS week: 1517 Day: 6 MJD: 54869
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 98| -2 -2 -5 -14 40 -182 -.14 104 39 | 0 -123 1808 1860
cod 235| 0 -1 0 -10 -20 51 -.14 19 15 | --- --- --- ---
esx 128| 0 2 0 4 -66 117 .38 30 25 | 113536 -5780 6021 12928
iac n/a| 1 -1 3 -27 9 -95 -.08 29 29 | 235231 -1075 5979 12937
mcc n/a| -29 -6 -8 36 25 1362 .94 135 135 | --- --- --- ---
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 3.1517.0 GPS week: 1517 Day: 0 MJD: 54863
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 748 74 16 29 27 --- 22 | 125 132 150 131 --- 131
R03 | 4153 26 23 42 25 --- 16 | 40 46 44 35 --- 34
R04 | 1064 47 17 54 15 --- 19 | 35 33 61 36 --- 37
R07 | 1644 20 11 32 19 --- 11 | 25 29 48 29 --- 27
R10 | 2494 24 16 15 18 --- 10 | 36 26 34 26 --- 25
R11 | 1857 30 16 31 23 161 14 | 30 31 32 29 55 25
R13 | 1640 24 16 20 14 --- 10 | 22 20 27 25 --- 20
R14 | 1272 20 12 14 12 --- 8 | 23 25 28 24 --- 21
R15 | 4197 19 13 22 18 101 10 | 16 25 28 16 43 19
R17 | 1586 25 19 29 37 --- 16 | 40 55 57 47 --- 45
R18 | 1227 13 9 27 17 --- 9 | 49 40 37 36 --- 32
R19 | 2420 16 9 21 21 --- 9 | 34 31 35 43 --- 32
R20 | 2437 45 12 28 38 --- 17 | 18 26 41 23 --- 21
R21 | 604 18 11 13 17 --- 8 | 41 37 43 42 --- 38
R22 | 2410 18 9 33 23 --- 12 | 46 31 40 33 --- 32
R23 | 894 32 25 34 34 --- 18 | 73 86 88 88 --- 81
R24 | 2242 28 18 26 24 395 13 | 202 235 229 226 168 225
------+------------------------------------+--------------------------------
RMS | 2183 32 16 29 24 253 |T 50 53 60 52 88 49
WRMS | 2183 28 13 25 24 253 |NE 50 53 60 52 88 49
MEDI | 1644 24 16 28 21 161 |MD 36 31 41 35 55 32
Table 3.1517.1 GPS week: 1517 Day: 1 MJD: 54864
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 806 61 42 62 31 --- 27 | 211 247 254 237 --- 234
R03 | 2887 24 34 49 22 --- 18 | 21 43 45 30 --- 25
R04 | 1601 18 17 24 16 --- 10 | 23 33 45 35 --- 29
R07 | 1247 14 9 19 8 --- 7 | 21 18 29 21 --- 18
R10 | 2924 13 12 18 12 --- 7 | 15 18 29 18 --- 13
R11 | 2229 21 19 32 29 147 14 | 18 31 36 27 87 16
R13 | 1630 18 20 16 31 --- 13 | 15 15 22 26 --- 9
R14 | 1267 16 16 34 18 --- 12 | 11 16 34 23 --- 15
R15 | 3563 22 10 23 13 50 9 | 21 20 32 19 59 16
R17 | 1062 35 26 66 22 --- 21 | 38 60 71 44 --- 44
R18 | 836 12 9 20 10 --- 7 | 50 28 33 26 --- 26
R19 | 1130 21 11 12 13 --- 8 | 27 41 31 32 --- 30
R20 | 1946 36 13 31 21 --- 14 | 18 19 37 32 --- 20
R21 | 594 12 12 26 13 --- 9 | 29 29 46 35 --- 29
R22 | 1111 28 8 24 18 --- 11 | 20 22 37 20 --- 18
R23 | 2100 22 29 32 34 --- 17 | 64 73 86 78 --- 71
R24 | 2650 69 38 77 39 249 31 | 147 205 226 147 190 173
------+------------------------------------+--------------------------------
RMS | 1933 30 22 38 22 170 |T 44 54 64 50 112 46
WRMS | 1933 23 14 27 22 170 |NE 44 54 64 50 112 46
MEDI | 1601 21 16 26 18 147 |MD 21 29 37 30 87 25
Table 3.1517.2 GPS week: 1517 Day: 2 MJD: 54865
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1115 44 20 23 26 --- 16 | 119 125 116 119 --- 118
R03 | 2638 18 19 19 14 --- 10 | 39 37 31 28 --- 29
R04 | 1196 27 13 31 21 --- 12 | 32 31 47 29 --- 30
R07 | 1484 13 12 40 15 --- 11 | 20 26 56 28 --- 26
XR08 | ---- --- 3 --- --- --- 0 | --- 205 --- --- --- 204
R10 | 2119 17 17 35 22 --- 12 | 17 28 48 21 --- 22
R11 | 2269 17 12 33 23 116 12 | 18 23 44 30 81 21
R13 | 1285 22 17 50 25 --- 16 | 21 30 63 28 --- 27
R14 | 2106 30 19 29 22 --- 14 | 23 24 27 19 --- 17
R15 | 1434 21 12 16 11 115 9 | 29 20 27 13 83 17
R17 | 1766 17 19 42 20 --- 14 | 40 39 63 50 --- 42
R18 | 765 21 14 37 17 --- 12 | 61 41 21 34 --- 32
R19 | 664 20 8 18 17 --- 9 | 22 29 29 25 --- 23
R20 | 798 42 19 31 35 --- 18 | 35 33 38 37 --- 27
R21 | 880 23 14 21 17 --- 10 | 52 38 38 41 --- 38
R22 | 828 12 9 25 21 --- 10 | 22 34 32 40 --- 29
R23 | 2495 39 19 27 30 --- 16 | 53 69 82 82 --- 68
R24 | 4056 29 34 102 19 565 27 | 287 286 202 270 398 267
------+------------------------------------+--------------------------------
RMS | 1856 26 17 39 22 339 |T 52 62 56 52 187 57
WRMS | 1856 22 16 30 22 339 |NE 52 62 56 52 187 57
MEDI | 1434 21 14 31 21 116 |MD 32 33 44 30 83 29
Table 3.1517.3 GPS week: 1517 Day: 3 MJD: 54866
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1134 38 16 16 14 --- 12 | 135 142 150 145 --- 143
R03 | 2974 37 15 13 15 --- 12 | 23 31 32 37 --- 24
R04 | 1134 27 16 14 13 --- 10 | 31 29 43 31 --- 28
R07 | 839 19 10 20 29 --- 11 | 22 23 26 28 --- 20
XR08 | ---- --- 8 --- --- --- 0 | --- 217 --- --- --- 213
R10 | 1550 24 18 26 26 --- 13 | 19 18 49 39 --- 27
R11 | 2276 13 18 17 18 108 10 | 22 25 31 32 65 21
R13 | 1208 16 20 35 25 --- 14 | 26 31 53 25 --- 24
R14 | 2438 16 15 22 13 --- 10 | 19 27 47 29 --- 26
R15 | 1786 13 23 16 34 110 13 | 11 25 19 27 46 14
R17 | 1331 19 16 26 30 --- 13 | 30 38 48 51 --- 38
R18 | 775 29 19 22 18 --- 12 | 40 34 39 27 --- 27
R19 | 1005 27 20 25 24 --- 13 | 42 49 42 35 --- 35
R20 | 1080 35 23 25 29 --- 16 | 26 27 32 37 --- 24
R21 | 1862 29 15 13 19 --- 11 | 54 34 38 57 --- 41
R22 | 753 23 17 23 20 --- 12 | 38 24 41 47 --- 31
R23 | 2451 51 17 21 42 --- 19 | 46 76 67 92 --- 68
R24 | 4217 51 27 32 16 333 18 | 92 136 149 127 145 125
------+------------------------------------+--------------------------------
RMS | 1920 30 18 22 24 212 |T 39 54 53 50 85 51
WRMS | 1920 26 17 20 24 212 |NE 39 54 53 50 85 51
MEDI | 1331 27 17 22 20 110 |MD 30 31 42 37 65 27
Table 3.1517.4 GPS week: 1517 Day: 4 MJD: 54867
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1221 26 11 14 11 --- 8 | 63 59 66 62 --- 61
R03 | 1564 29 12 19 13 --- 10 | 43 34 26 31 --- 28
R04 | 1723 29 20 43 23 --- 16 | 37 31 65 34 --- 30
R07 | 1130 26 18 37 20 --- 14 | 32 27 36 24 --- 22
XR08 | ---- --- 9 --- --- --- 0 | --- 44 --- --- --- 46
R10 | 2511 37 9 30 18 --- 13 | 15 26 43 27 --- 25
R11 | 1988 19 16 34 18 53 12 | 11 20 49 24 25 20
R13 | 1445 22 10 31 16 --- 11 | 33 27 47 25 --- 25
R14 | 1841 16 20 19 24 --- 12 | 33 35 27 27 --- 24
R15 | 1530 17 10 25 21 131 10 | 23 19 52 43 28 26
R17 | 1389 33 11 21 28 --- 13 | 49 36 44 59 --- 41
R18 | 933 20 13 33 19 --- 12 | 64 26 40 35 --- 24
R19 | 1113 20 14 25 18 --- 11 | 43 34 43 33 --- 33
R20 | 1214 62 21 61 33 --- 24 | 54 43 51 33 --- 36
R21 | 845 41 15 31 23 --- 15 | 63 42 41 29 --- 33
R22 | 677 38 9 11 21 --- 11 | 40 25 27 34 --- 27
R23 | 4575 25 20 18 36 --- 14 | 66 63 60 87 --- 67
R24 | 3983 60 25 24 23 488 19 | 169 211 210 217 236 202
------+------------------------------------+--------------------------------
RMS | 2025 33 16 30 22 293 |T 49 44 54 48 96 42
WRMS | 2025 28 14 27 22 293 |NE 49 44 54 48 96 42
MEDI | 1445 26 13 25 21 131 |MD 43 34 44 33 28 28
Table 3.1517.5 GPS week: 1517 Day: 5 MJD: 54868
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2414 19 12 22 31 --- 12 | 92 103 112 120 --- 105
R03 | 1139 16 10 18 18 --- 9 | 29 15 22 24 --- 16
R04 | 2204 38 26 32 24 --- 17 | 24 25 36 32 --- 22
R07 | 2083 18 15 20 25 --- 11 | 35 21 31 25 --- 22
XR08 | ---- --- 59 --- 91 --- 73 | --- 99 --- 63 --- 62
R10 | 2766 22 17 17 21 --- 11 | 22 23 18 22 --- 12
R11 | 1773 28 20 18 28 110 13 | 20 17 32 34 48 15
R13 | 1372 16 18 29 15 --- 12 | 47 25 33 24 --- 24
R14 | 1405 15 16 16 22 --- 10 | 31 21 24 32 --- 16
R15 | 2622 44 16 36 36 101 19 | 23 25 55 37 24 23
R17 | 1361 39 17 19 32 --- 15 | 28 33 49 58 --- 35
R18 | 1353 17 10 15 26 --- 10 | 89 25 33 31 --- 19
R19 | 711 14 22 33 15 --- 13 | 54 30 54 35 --- 35
R20 | 1095 47 20 30 39 --- 19 | 30 24 26 18 --- 14
R21 | 683 25 26 35 21 --- 15 | 47 21 45 23 --- 15
R22 | 933 22 14 29 22 --- 12 | 24 28 33 24 --- 16
R23 | 4944 36 30 41 43 --- 21 | 47 54 68 55 --- 50
R24 | 5288 37 21 33 30 --- 17 | 142 125 120 124 --- 125
------+------------------------------------+--------------------------------
RMS | 2388 29 19 27 27 106 |T 46 39 46 43 36 34
WRMS | 2388 28 17 25 27 106 |NE 46 39 46 43 36 34
MEDI | 1405 22 17 29 25 101 |MD 31 25 33 32 24 22
Table 3.1517.6 GPS week: 1517 Day: 6 MJD: 54869
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3484 26 13 14 23 --- 10 | 104 103 115 119 --- 109
R03 | 1012 31 13 23 18 --- 11 | 42 28 31 38 --- 28
R04 | 1563 43 10 29 15 --- 13 | 29 20 51 25 --- 26
R07 | 3844 33 9 39 21 --- 14 | 42 30 59 34 --- 34
XR08 | ---- --- 78 --- 130 --- 101 | --- 66 --- 48 --- 67
R10 | 2406 23 14 28 22 --- 12 | 26 20 36 23 --- 20
R11 | 1071 29 16 13 17 167 10 | 38 24 32 28 50 26
R13 | 1221 15 16 23 15 --- 10 | 32 26 28 24 --- 23
R14 | 2300 22 12 23 24 --- 11 | 28 19 35 22 --- 21
R15 | 2189 27 16 24 30 91 13 | 17 24 32 31 40 21
R17 | 1171 38 15 23 30 --- 14 | 57 49 51 66 --- 52
R18 | 1904 362 29 30 44 --- 24 | 261 59 46 40 --- 41
R19 | 800 88 13 43 35 --- 24 | 128 74 79 92 --- 81
R20 | 1369 37 13 29 48 --- 18 | 35 25 28 32 --- 24
R21 | 810 148 39 40 39 --- 36 | 146 41 29 36 --- 37
R22 | 1933 94 30 15 27 --- 23 | 87 38 29 32 --- 27
R23 | 3077 45 21 46 36 --- 20 | 54 69 101 79 --- 72
R24 | 3951 35 23 43 23 --- 17 | 200 203 193 188 --- 196
------+------------------------------------+--------------------------------
RMS | 2248 104 19 30 29 135 |T 78 51 57 53 45 50
WRMS | 2248 39 15 25 29 135 |NE 78 51 57 53 45 50
MEDI | 1904 35 15 28 24 91 |MD 42 30 36 34 40 28
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