[IGSREPORT-17551] Wk 1536 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 2 06:06:13 PDT 2009
******************************************************************************
IGS Electronic Report 02 Jul 06:06:34 PDT 2009 Message Number 17551
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1536 (Jun 14, 2009 - Jun 20, 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 2.1536.
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:
igl1536[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1536 in the SP3 format.
igl15367.sum Combination Report for GPS Week 1536.
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 | 214.7 ns
1 | 208.8 ns
2 | 204.7 ns
3 | 200.2 ns
4 | 198.6 ns
5 | 200.8 ns
6 | 198.5 ns
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 1.1536, 1a.1536).
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 2.1536.0-6)
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 3.1536.0-6).
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 1536 summary. (Jun 14, 2009 - Jun 20, 2009)
Table 1.1536.a GPS week : 1536 MJD: 54996.0-55002.0
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 106| 1 0 -11 6 -16 14 -.14 37 35 | 0 600 4950 5645
| 1 1 4 36 35 122 .08 | 0 1687
cod 236| -2 -1 1 -2 -4 84 -.10 18 16 | --- --- --- ---
| 1 1 3 16 28 38 .02 | --- ---
esx 136| 3 0 11 -1 50 70 .41 32 29 | 97027 1948 5459 11520
| 2 1 6 44 34 65 .11 | 3959 4237
iac n/a| 1 2 -6 -7 -19 -217 -.12 34 34 | 203313 131 5380 10649
| 3 1 6 25 31 92 .07 | 5193 2633
mcc n/a| 2 1 36 -85 5 903 .21 270 270 | --- --- --- ---
| 21 14 20 212 278 676 .38 | --- ---
Table 1.1536.b GPS week : 1536 MJD: 54996.0-55002.0
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 | 18 19 22 21 18 16 20 |
R03 | 16 17 23 22 21 18 20 |
R06 | 572 20 17 20 0 --- --- |
R07 | 22 19 15 13 17 20 29 |
R08 | 21 18 15 17 18 19 35 |
R10 | 16 17 19 20 17 15 14 |
R11 | 11 10 12 9 13 11 11 |
R13 | 11 9 9 11 15 12 9 |
R14 | 18 18 12 11 13 14 11 |
R15 | 15 14 14 15 12 14 17 |
R17 | 15 16 18 14 15 14 21 |
R18 | 10 10 12 13 12 11 11 |
R19 | 9 9 9 8 15 12 12 |
R20 | 12 15 14 16 18 14 15 |
R21 | 11 17 12 10 12 11 13 |
R22 | 11 19 10 10 14 11 11 |
R23 | 24 26 27 20 20 25 19 |
R24 | 127 46 22 27 13 20 12 |
Table 1.1536.c GPS week : 1536 MJD: 54996.0-55002.0
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 1536 0 | 53 -96 231 1129 -655 -13520 89.6 2230 2230 | 214650 0
brd 1536 1 | -92 73 330 -497 -387 -11340 90.5 7416 7416 | 208829 0
brd 1536 2 | 17 -52 397 -420 758 -7271 89.6 8206 8206 | 204709 0
brd 1536 3 | 91 -75 390 1812 2845 -10830 88.8 11630 11630 | 200225 0
brd 1536 4 | 119 13 443 2117 2215 -11070 88.1 3563 3563 | 198605 0
brd 1536 5 | 5 81 330 1944 2636 -9894 88.5 2431 2431 | 200762 0
brd 1536 6 | -41 0 218 -357 335 -13810 88.2 1903 1903 | 198530 0
-------------+------------------------------------------------------------+----------------
brd 1536 mean| 22 -8 334 818 1106 -11105 89.0 5339 5339 | 203758 0
brd 1536 sdev| 73 70 84 1203 1451 2215 .9 3768 3768 | 6063 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 2.1536.0 GPS week: 1536 Day: 0 MJD: 54996
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 106| 4 1 -7 -7 -40 -27 -.26 44 46 | 0 -759 5605 6479
cod 236| -7 -1 1 -15 -25 88 -.06 14 11 | --- --- --- ---
esx 136| 4 1 5 35 76 174 .45 30 25 | 103124 5998 6562 14213
iac n/a| 6 2 -5 12 23 -340 -.24 31 31 | 211076 3461 6380 10569
mcc n/a| 23 -13 5 -238 -27 -129 .65 170 170 | --- --- --- ---
Table 2.1536.1 GPS week: 1536 Day: 1 MJD: 54997
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 106| 1 1 -14 20 -48 194 -.06 44 38 | 0 1088 6740 7980
cod 236| -1 -2 -2 -6 -25 88 -.09 19 18 | --- --- --- ---
esx 136| -1 0 12 -57 87 57 .39 43 47 | 93002 4305 5254 12189
iac n/a| 5 0 2 1 -22 -329 -.08 34 34 | 208439 -1170 5064 10226
mcc n/a| -12 5 46 47 -53 290 -.03 192 192 | --- --- --- ---
Table 2.1536.2 GPS week: 1536 Day: 2 MJD: 54998
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 106| 0 0 -11 -7 -62 -94 -.20 29 27 | 0 -468 3674 4299
cod 236| -2 -1 1 10 26 96 -.10 18 16 | --- --- --- ---
esx 136| 3 -1 15 8 63 85 .52 35 30 | 96233 -3103 5376 11841
iac n/a| 1 2 -2 -12 -48 -92 -.14 35 35 | 206245 -1534 5230 11702
mcc n/a| -23 -3 49 -6 1 664 .52 211 211 | --- --- --- ---
Table 2.1536.3 GPS week: 1536 Day: 3 MJD: 54999
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 106| 1 1 -6 -1 14 88 -.11 36 33 | 0 -480 4689 5287
cod 236| -1 -1 0 -5 -22 15 -.11 17 14 | --- --- --- ---
esx 136| 3 2 19 33 -14 55 .27 27 24 | 92907 650 5000 11294
iac n/a| -1 1 -18 -32 26 -196 -.05 36 36 | 198787 605 4968 10673
mcc n/a| 3 -15 59 307 -102 1435 -.50 229 229 | --- --- --- ---
Table 2.1536.4 GPS week: 1536 Day: 4 MJD: 55000
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 106| 2 2 -13 55 32 132 -.16 32 31 | 0 3298 4575 5112
cod 236| -3 -1 2 -7 -12 79 -.10 18 16 | --- --- --- ---
esx 136| 6 0 16 -62 57 -42 .59 32 30 | 101587 -517 5351 9453
iac n/a| 0 2 -9 21 -46 -207 -.19 30 30 | 200993 -2481 5333 9606
mcc n/a| -3 8 12 -234 529 1757 .29 190 190 | --- --- --- ---
Table 2.1536.5 GPS week: 1536 Day: 5 MJD: 55001
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 106| 3 -3 -20 42 0 -90 -.13 36 33 | 0 2400 4272 4843
cod 236| -1 2 7 -19 -18 79 -.14 19 18 | --- --- --- ---
esx 136| 1 0 4 -16 27 57 .30 21 19 | 95524 -1826 4619 11514
iac n/a| 0 3 -1 3 -32 -130 -.08 37 37 | 199367 -1934 4629 11267
mcc n/a| 39 26 42 -219 92 1388 .23 505 505 | --- --- --- ---
Table 2.1536.6 GPS week: 1536 Day: 6 MJD: 55002
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 106| 0 0 -8 -53 -14 -101 -.04 39 35 | 0 -878 5095 5521
cod 236| -2 -4 4 29 44 145 -.11 21 15 | --- --- --- ---
esx 136| 5 0 3 45 56 108 .38 33 30 | 96816 8133 6054 10139
iac n/a| -2 2 -6 -48 -37 -227 -.06 33 33 | 198284 3970 6057 10505
mcc n/a| -8 2 42 -252 -401 916 .34 394 394 | --- --- --- ---
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 3.1536.0 GPS week: 1536 Day: 0 MJD: 54996
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2837 65 13 30 30 --- 18 | 37 40 42 45 --- 36
R03E | 4416 50 14 22 31 --- 15 | 34 21 33 35 --- 22
XR06E |12267 --- 380 860 --- --- 572 | --- 777 69 --- --- 539
R07E | 2935 62 20 43 43 --- 22 | 30 31 58 50 --- 32
R08E | 1450 69 20 31 39 218 21 | 32 30 47 44 124 26
R10 | 1869 60 17 16 22 --- 16 | 34 54 40 38 --- 42
R11 | 677 18 14 22 22 130 10 | 33 43 52 39 8 39
R13 | 1869 26 12 19 25 --- 11 | 29 32 37 30 --- 28
R14 | 2822 42 15 35 41 --- 17 | 38 43 54 30 --- 36
R15 | 1355 49 12 25 29 149 15 | 35 38 36 43 174 33
R17 | 1200 41 13 28 30 --- 14 | 53 60 83 59 --- 60
R18 | 896 31 9 22 14 --- 10 | 41 50 58 55 --- 49
R19 | 815 25 6 18 20 --- 9 | 40 36 55 43 --- 39
R20 | 2325 30 11 22 24 --- 11 | 34 39 55 35 --- 36
R21 | 1399 23 8 22 28 --- 10 | 42 49 66 40 --- 46
R22 | 784 25 10 29 17 --- 11 | 50 45 75 49 --- 50
R23 | 3629 33 18 62 55 --- 23 | 60 64 62 81 --- 53
XR24 |21102 379 106 --- 85 --- 127 | 135 62 --- 79 --- 53
------+------------------------------------+--------------------------------
RMS | 2230 44 14 30 31 170 |T 44 84 54 46 102 67
WRMS | 2230 46 11 25 31 170 |NE 48 47 56 47 91 43
MEDI | 1869 41 13 25 29 149 |MD 37 43 55 43 124 39
Table 3.1536.1 GPS week: 1536 Day: 1 MJD: 54997
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2276 53 21 33 24 --- 18 | 29 32 56 39 --- 32
R03E | 9288 42 17 24 37 --- 17 | 31 20 45 46 --- 24
R06E |28302 48 15 39 40 --- 19 | 15 263 65 26 --- 173
R07E | 2322 50 20 22 40 --- 19 | 28 21 34 48 --- 24
R08E | 1315 37 21 24 43 92 18 | 41 16 28 45 64 17
R10 | 1811 50 22 19 23 --- 17 | 33 44 30 48 --- 34
R11 | 687 23 14 15 19 --- 10 | 38 36 34 29 --- 32
R13 | 1175 19 11 19 18 --- 9 | 26 34 43 29 --- 29
R14 | 2468 23 21 48 31 --- 17 | 31 44 56 36 --- 36
R15 | 1403 36 10 26 28 255 14 | 21 27 35 27 89 23
R17 | 1118 44 12 35 24 --- 16 | 42 46 58 37 --- 43
R18 | 1102 23 11 20 18 --- 10 | 35 41 29 49 --- 38
R19 | 1145 15 9 28 13 --- 9 | 16 19 39 26 --- 20
R20 | 1220 29 16 36 23 --- 14 | 25 29 37 20 --- 25
R21 | 1019 17 13 44 38 --- 16 | 22 24 55 16 --- 21
R22 | 872 18 28 52 28 --- 19 | 25 16 78 48 --- 32
R23 | 1535 43 27 48 63 --- 25 | 32 51 60 43 --- 35
R24 | 8227 113 35 117 60 --- 45 | 69 87 134 98 --- 75
------+------------------------------------+--------------------------------
RMS | 7416 44 19 43 34 192 |T 31 47 50 39 76 39
WRMS | 7416 38 18 47 34 192 |NE 31 38 52 38 89 34
MEDI | 1315 36 16 28 28 92 |MD 29 32 43 37 64 32
Table 3.1536.2 GPS week: 1536 Day: 2 MJD: 54998
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1467 51 30 34 38 --- 22 | 29 36 55 46 --- 32
R03E | 9572 46 21 53 43 --- 22 | 20 32 45 42 --- 21
R06E |32628 20 21 46 32 --- 17 | 10 178 54 19 --- 126
R07E | 1512 32 16 24 31 --- 14 | 32 17 32 32 --- 20
R08E | 1415 28 16 25 37 146 15 | 30 17 35 48 73 24
R10 | 1835 31 23 44 36 --- 18 | 31 39 50 31 --- 31
R11 | 2014 14 12 30 25 --- 11 | 35 31 46 26 --- 28
R13 | 747 18 15 14 10 --- 8 | 37 37 32 24 --- 31
R14 | 1863 19 13 26 24 --- 11 | 30 27 36 29 --- 22
R15 | 1831 24 12 36 27 260 14 | 28 27 47 36 59 26
R17 | 912 14 14 42 50 --- 18 | 41 48 76 24 --- 41
R18 | 2285 25 10 29 21 --- 12 | 36 51 58 57 --- 48
R19 | 1999 14 15 19 13 --- 8 | 38 22 37 34 --- 27
R20 | 749 28 10 32 32 --- 14 | 47 35 67 33 --- 40
R21 | 679 19 15 22 25 --- 11 | 33 43 53 30 --- 34
R22 | 489 15 9 23 20 --- 9 | 27 38 49 35 --- 35
R23 | 1446 51 21 42 74 --- 27 | 58 44 46 68 --- 37
R24 | 4612 19 34 59 33 --- 21 | 96 89 123 95 --- 87
------+------------------------------------+--------------------------------
RMS | 8206 29 18 35 35 211 |T 36 45 52 39 66 39
WRMS | 8206 27 16 30 35 211 |NE 41 40 55 40 59 37
MEDI | 1512 20 15 30 31 146 |MD 32 36 47 33 59 31
Table 3.1536.3 GPS week: 1536 Day: 3 MJD: 54999
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1261 52 23 30 48 --- 21 | 54 47 47 61 --- 45
R03E |10866 47 23 33 57 --- 22 | 34 42 42 43 --- 25
R06E |47394 50 15 29 45 --- 19 | 15 176 52 25 --- 124
R07E | 1432 26 13 23 31 --- 12 | 38 24 38 43 --- 26
R08E | 826 46 19 19 38 236 17 | 39 22 35 33 84 21
R10 | 2115 38 15 49 41 --- 20 | 39 49 71 61 --- 48
R11 | 2667 15 11 21 17 --- 9 | 30 41 48 43 --- 38
R13 | 1097 23 13 19 21 --- 10 | 47 56 60 57 --- 53
R14 | 1739 21 15 19 20 --- 10 | 34 32 39 29 --- 28
R15 | 1990 25 19 24 34 223 14 | 25 29 39 47 61 28
R17 | 1858 22 17 21 39 --- 14 | 58 49 50 21 --- 40
R18 | 2525 29 9 28 28 --- 13 | 39 54 83 60 --- 56
R19 | 2563 14 12 10 15 --- 7 | 42 40 47 32 --- 40
R20 | 1130 22 14 36 37 --- 15 | 41 44 79 21 --- 44
R21 | 1168 16 10 21 23 --- 10 | 46 42 58 64 --- 48
R22 | 486 14 13 20 23 --- 10 | 37 39 48 22 --- 35
R23 | 1263 35 19 33 56 --- 20 | 41 41 42 74 --- 40
R24 | 4822 76 31 34 43 --- 26 | 79 151 162 122 --- 133
------+------------------------------------+--------------------------------
RMS |11625 36 17 27 36 229 |T 41 54 57 47 72 48
WRMS |11625 33 14 24 36 229 |NE 42 51 63 50 61 48
MEDI | 1739 25 15 23 34 223 |MD 39 42 48 43 61 40
Table 3.1536.4 GPS week: 1536 Day: 4 MJD: 55000
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 731 34 16 24 45 --- 17 | 29 30 37 61 --- 33
R03E |12408 44 20 32 48 --- 20 | 42 33 39 40 --- 28
XR06E | ---- --- --- --- 11 --- 0 | --- --- --- 32 --- 146
R07E | 1360 33 23 26 39 --- 17 | 30 24 45 57 --- 26
R08E | 929 29 27 31 37 252 18 | 38 17 46 48 194 23
R10 | 1378 31 19 45 24 --- 17 | 33 37 77 49 --- 40
R11 | 1266 29 16 22 25 --- 13 | 30 40 47 36 --- 35
R13 | 2096 39 12 26 26 --- 14 | 40 35 51 34 --- 34
R14 | 1007 16 14 35 23 --- 12 | 23 28 64 28 --- 30
R15 | 2420 26 16 21 24 96 12 | 21 26 42 35 92 26
R17 | 2187 21 16 42 27 --- 15 | 25 38 75 32 --- 38
R18 | 2818 29 12 24 19 --- 11 | 25 50 62 47 --- 44
R19 | 2149 31 16 35 21 --- 14 | 25 43 71 47 --- 42
R20 | 1493 31 23 42 32 --- 18 | 22 42 37 35 --- 27
R21 | 1953 22 9 34 18 --- 12 | 32 39 74 42 --- 43
R22 | 700 33 16 30 16 --- 13 | 27 48 74 47 --- 46
R23 | 1108 43 19 45 36 --- 20 | 42 44 80 68 --- 51
R24 | 4322 35 21 15 17 --- 13 | 60 83 80 68 --- 72
------+------------------------------------+--------------------------------
RMS | 3562 32 18 32 30 190 |T 32 38 58 44 143 43
WRMS | 3562 31 16 30 30 190 |NE 31 42 64 43 92 40
MEDI | 1493 31 16 31 24 96 |MD 30 38 62 42 92 35
Table 3.1536.5 GPS week: 1536 Day: 5 MJD: 55001
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1472 22 24 14 49 --- 16 | 36 40 51 59 --- 40
R03E | 6567 42 19 21 50 --- 18 | 36 24 40 42 --- 27
R07E | 1650 48 14 24 59 --- 20 | 39 36 37 51 --- 33
R08E | 784 47 24 23 41 711 18 | 36 31 53 47 194 36
R10 | 1465 23 20 27 36 --- 15 | 41 45 67 52 --- 47
R11 | 1178 30 13 9 25 --- 11 | 25 29 34 32 --- 27
R13 | 2976 19 20 22 22 --- 12 | 52 48 41 42 --- 42
R14 | 1351 29 14 16 39 --- 13 | 40 44 47 34 --- 38
R15 | 2248 35 21 12 28 60 13 | 22 31 40 30 46 25
R17 | 998 22 18 22 38 --- 14 | 20 28 27 34 --- 22
R18 | 2272 31 17 13 16 --- 11 | 27 41 27 37 --- 29
R19 | 1183 18 20 24 17 --- 12 | 49 54 62 53 --- 53
R20 | 1880 36 10 18 37 --- 14 | 27 32 42 41 --- 30
R21 | 1406 24 17 13 22 --- 10 | 18 28 25 24 --- 18
R22 | 664 27 14 20 13 --- 11 | 17 42 46 40 --- 36
R23 | 1824 69 26 30 57 --- 25 | 98 97 106 100 --- 95
R24 | 3958 51 15 34 40 --- 19 | 45 47 65 32 --- 44
------+------------------------------------+--------------------------------
RMS | 2430 36 19 21 37 505 |T 36 41 47 44 120 37
WRMS | 2430 33 18 19 37 505 |NE 37 43 48 42 46 38
MEDI | 1472 30 18 21 37 60 |MD 36 40 42 41 46 36
Table 3.1536.6 GPS week: 1536 Day: 6 MJD: 55002
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1079 48 24 31 37 --- 19 | 57 34 39 44 --- 35
R03E | 2698 42 25 28 44 --- 19 | 51 34 41 47 --- 35
R07E | 1537 74 31 52 46 --- 28 | 38 37 63 53 --- 38
R08E | 701 88 44 52 59 555 34 | 62 41 53 86 142 50
R10 | 1548 30 11 27 31 --- 14 | 39 41 59 65 --- 45
R11 | 1803 13 15 25 23 --- 11 | 32 32 45 36 --- 34
R13 | 3128 20 9 12 19 --- 8 | 41 48 50 43 --- 43
R14 | 1796 18 9 27 22 --- 11 | 32 37 51 33 --- 33
R15 | 1395 32 15 46 24 60 16 | 32 42 50 41 68 36
R17 | 884 39 34 27 45 --- 21 | 34 55 48 38 --- 40
R18 | 2587 18 11 25 20 --- 10 | 44 64 69 56 --- 57
R19 | 1304 25 15 26 20 --- 12 | 39 56 68 40 --- 49
R20 | 1112 29 22 34 23 --- 15 | 33 47 45 38 --- 38
R21 | 1186 20 13 31 24 --- 12 | 39 49 68 51 --- 50
R22 | 680 25 12 18 19 --- 10 | 35 49 59 41 --- 44
R23 | 2367 33 17 38 43 --- 18 | 133 130 141 150 --- 134
R24 | 3429 27 15 25 19 --- 12 | 53 74 71 41 --- 56
------+------------------------------------+--------------------------------
RMS | 1902 39 21 33 33 394 |T 46 51 60 53 105 48
WRMS | 1902 35 15 30 33 394 |NE 45 55 63 51 68 50
MEDI | 1537 29 15 27 24 60 |MD 39 47 53 43 68 43
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