[IGSREPORT-17595] Wk 1538 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 16 06:06:37 PDT 2009
******************************************************************************
IGS Electronic Report 16 Jul 06:07:00 PDT 2009 Message Number 17595
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1538 (Jun 28, 2009 - Jul 04, 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 2.1538.
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:
igl1538[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1538 in the SP3 format.
igl15387.sum Combination Report for GPS Week 1538.
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 | 130.9 ns
1 | 135.7 ns
2 | 126.5 ns
3 | 138.0 ns
4 | 115.3 ns
5 | 196.6 ns
6 | 196.6 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 1.1538, 1a.1538).
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 2.1538.0-6)
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 3.1538.0-6).
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 1538 summary. (Jun 28, 2009 - Jul 04, 2009)
Table 1.1538.a GPS week : 1538 MJD: 55010.0-55016.0
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 -10 -27 -17 16 -.16 30 29 | 0 169 3469 3936
| 2 2 3 28 28 202 .04 | 0 502
cod 236| -2 0 0 12 -3 77 -.13 19 17 | --- --- --- ---
| 1 2 1 20 17 61 .03 | --- ---
esx 123| 2 0 3 42 34 47 .31 27 25 | 55573 872 4725 9872
| 1 2 3 31 26 32 .05 | 34879 3123
iac n/a| 1 0 6 -49 -10 -211 .00 32 32 | 148547 -1117 4721 10004
| 2 2 3 21 25 89 .05 | 33577 2031
mcc n/a| 7 -4 72 100 -184 1229 .04 204 204 | --- --- --- ---
| 26 23 31 268 178 890 .86 | --- ---
Table 1.1538.b GPS week : 1538 MJD: 55010.0-55016.0
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 | 17 17 23 15 20 19 14 |
R03 | 18 19 22 20 18 18 16 |
R07 | 17 19 20 16 15 18 14 |
R08 | 17 20 18 14 15 14 13 |
R10 | 10 10 16 14 15 18 17 |
R11 | 12 12 10 12 12 11 13 |
R13 | 11 12 14 11 9 11 11 |
R14 | 13 11 12 9 10 9 12 |
R15 | 16 15 16 14 13 12 12 |
R17 | 15 17 12 16 17 15 18 |
R18 | 15 12 14 12 12 13 12 |
R19 | 13 9 13 8 11 10 13 |
R20 | 18 14 15 14 13 16 17 |
R21 | 14 18 15 16 14 12 10 |
R22 | 23 17 17 13 14 16 9 |
R23 | 21 25 17 19 22 21 17 |
R24 | 12 23 14 17 14 17 15 |
Table 1.1538.c GPS week : 1538 MJD: 55010.0-55016.0
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 1538 0 | -178 78 360 -1724 2248 -20370 89.6 2290 2290 | 130893 0
brd 1538 1 | 77 -55 512 920 1440 -22490 86.7 2365 2365 | 135720 0
brd 1538 2 | 37 -40 466 1375 -1873 -21110 89.4 2660 2660 | 126506 0
brd 1538 3 | 65 -67 449 -398 -1920 -15590 88.6 2394 2394 | 137995 0
brd 1538 4 | 6 48 297 -489 -2171 -18320 88.5 2316 2316 | 115283 0
brd 1538 5 | -83 -55 240 -1154 80 -23250 90.6 2048 2048 | 196574 0
brd 1538 6 | 11 -3 460 -2084 -2301 -20450 87.5 2517 2517 | 196591 0
-------------+------------------------------------------------------------+----------------
brd 1538 mean| -8 -13 398 -507 -642 -20225 88.7 2370 2370 | 148508 0
brd 1538 sdev| 91 57 100 1289 1890 2589 1.3 191 191 | 33651 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 2.1538.0 GPS week: 1538 Day: 0 MJD: 55010
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 -1 -14 -56 -30 195 -.16 30 30 | 0 214 3357 3817
cod 236| 0 0 1 5 3 22 -.11 17 17 | --- --- --- ---
esx 123| 2 0 9 75 45 29 .25 29 28 | 35683 771 4917 9690
iac n/a| -1 3 1 -23 -4 -313 .02 37 37 | 129894 145 4883 9061
mcc n/a| -8 27 28 -370 -117 -116 -.23 217 217 | --- --- --- ---
Table 2.1538.1 GPS week: 1538 Day: 1 MJD: 55011
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 11 -26 288 -.11 36 35 | 0 1009 3305 3630
cod 236| -3 0 0 -23 -32 -2 -.15 19 17 | --- --- --- ---
esx 123| 3 0 2 71 59 37 .38 29 25 | 35249 -673 3594 9416
iac n/a| 1 -1 3 -37 -18 -302 -.03 33 33 | 137468 -4282 3593 9854
mcc n/a| -12 -7 53 -112 -102 210 .70 206 206 | --- --- --- ---
Table 2.1538.2 GPS week: 1538 Day: 2 MJD: 55012
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 4 -8 -13 20 -154 -.15 31 31 | 0 -581 3099 3694
cod 236| -3 -2 2 11 0 127 -.17 22 21 | --- --- --- ---
esx 123| 4 -4 1 19 26 95 .36 28 27 | 42029 3506 4654 9872
iac n/a| 1 1 7 -29 -35 -130 -.01 31 31 | 126001 136 4647 10382
mcc n/a| -9 -6 105 234 -175 1171 -1.10 182 182 | --- --- --- ---
Table 2.1538.3 GPS week: 1538 Day: 3 MJD: 55013
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 2 -5 -28 -22 -13 -.18 25 24 | 0 84 3973 4531
cod 236| -3 -3 -1 42 -17 68 -.12 17 15 | --- --- --- ---
esx 123| 2 0 5 53 26 5 .28 30 29 | 50478 -1383 4346 8971
iac n/a| 0 3 9 -82 31 -70 .06 31 31 | 139394 -3451 4338 8962
mcc n/a| -18 -47 107 245 78 1704 -.68 188 188 | --- --- --- ---
Table 2.1538.4 GPS week: 1538 Day: 4 MJD: 55014
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 0 -11 -26 22 148 -.21 29 29 | 0 114 3191 3627
cod 236| -3 3 1 11 -5 36 -.16 22 20 | --- --- --- ---
esx 123| 2 -1 3 30 -10 30 .30 23 22 | 16769 -3353 4288 9955
iac n/a| 1 0 1 -52 12 -182 -.07 27 27 | 114599 -1529 4301 10183
mcc n/a| 17 -14 59 29 -193 2241 .81 196 196 | --- --- --- ---
Table 2.1538.5 GPS week: 1538 Day: 5 MJD: 55015
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 -6 -30 -74 -.13 29 28 | 0 -171 3402 3872
cod 236| -3 0 0 15 19 152 -.12 20 18 | --- --- --- ---
esx 123| 0 0 1 -11 24 48 .28 24 21 | 102568 5984 5512 10326
iac n/a| 3 0 7 -51 -18 -252 -.04 32 32 | 195628 908 5522 10299
mcc n/a| 46 2 99 289 -507 2029 1.21 226 226 | --- --- --- ---
Table 2.1538.6 GPS week: 1538 Day: 6 MJD: 55016
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| 5 -1 -7 -70 -52 -273 -.20 30 29 | 0 514 3960 4382
cod 236| -2 0 0 24 11 138 -.08 14 13 | --- --- --- ---
esx 123| 0 1 -1 56 71 86 .31 26 24 | 106240 1252 5770 10874
iac n/a| 5 -1 11 -68 -40 -230 .07 33 33 | 196845 251 5768 11292
mcc n/a| 37 13 51 390 -271 1366 -.40 215 215 | --- --- --- ---
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 3.1538.0 GPS week: 1538 Day: 0 MJD: 55010
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 4555 33 14 36 40 --- 17 | 42 43 53 56 --- 43
R03E | 4553 30 15 37 47 --- 18 | 37 33 41 47 --- 31
R07E | 2731 31 20 26 40 --- 16 | 27 26 37 37 --- 25
R08E | 2491 42 17 30 32 255 17 | 27 34 43 45 24 33
R10 | 1760 18 10 21 24 --- 10 | 28 28 34 26 --- 24
R11 | 1282 19 17 26 21 --- 12 | 28 36 38 23 --- 30
R13 | 1747 16 14 22 26 --- 11 | 25 26 32 29 --- 23
R14 | 1090 22 19 20 31 --- 13 | 44 45 38 37 --- 38
R15 | 2098 30 17 39 28 172 16 | 33 30 49 31 28 28
R17 | 1629 24 24 23 31 --- 14 | 43 62 67 37 --- 53
R18 | 1711 32 14 32 22 --- 14 | 35 43 75 61 --- 49
R19 | 1853 31 10 28 22 --- 13 | 50 57 69 53 --- 56
R20 | 1535 35 25 23 45 --- 18 | 74 67 68 70 --- 66
R21 | 1756 32 16 28 24 --- 14 | 49 68 65 48 --- 56
R22 | 1004 45 19 21 69 --- 22 | 44 58 53 109 --- 58
R23 | 1370 33 16 39 61 --- 21 | 28 28 37 68 --- 25
R24 | 1801 23 15 22 28 --- 12 | 110 120 117 98 --- 112
------+------------------------------------+--------------------------------
RMS | 2289 30 17 29 37 217 |T 42 47 53 51 26 44
WRMS | 2289 30 17 28 37 217 |NE 45 51 57 53 28 47
MEDI | 1756 31 16 26 31 172 |MD 37 43 49 47 24 38
Table 3.1538.1 GPS week: 1538 Day: 1 MJD: 55011
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2043 31 14 26 45 --- 16 | 56 56 55 57 --- 52
R03E | 3349 47 18 33 39 --- 19 | 37 21 36 52 --- 26
R07E | 1737 40 18 38 40 --- 19 | 31 27 43 36 --- 25
R08E | 1693 58 22 15 40 225 19 | 37 35 43 60 21 39
R10 | 3390 24 8 13 22 --- 9 | 22 16 25 16 --- 16
R11 | 1349 23 17 23 17 --- 11 | 24 22 36 24 --- 20
R13 | 814 23 15 18 25 --- 11 | 24 23 27 29 --- 19
R14 | 4395 24 13 24 13 --- 11 | 33 31 42 29 --- 28
R15 | 2396 39 11 21 30 185 14 | 27 19 35 26 33 20
R17 | 1156 24 19 20 48 --- 16 | 38 44 51 20 --- 37
R18 | 1280 31 11 23 15 --- 11 | 27 33 37 34 --- 29
R19 | 2243 21 9 13 19 --- 8 | 40 49 55 41 --- 46
R20 | 1045 32 18 20 30 --- 14 | 70 53 53 38 --- 50
R21 | 1514 24 36 31 28 --- 18 | 45 49 55 20 --- 35
R22 | 1521 40 17 30 37 --- 17 | 39 37 64 77 --- 49
R23 | 1784 39 33 53 44 --- 24 | 44 32 55 37 --- 21
R24 | 4229 54 24 51 34 --- 23 | 115 94 107 85 --- 92
------+------------------------------------+--------------------------------
RMS | 2365 36 19 29 33 206 |T 41 37 48 40 27 35
WRMS | 2365 35 17 25 33 206 |NE 42 38 49 36 33 35
MEDI | 1737 31 17 23 30 185 |MD 37 33 43 36 21 29
Table 3.1538.2 GPS week: 1538 Day: 2 MJD: 55012
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1169 49 27 33 48 --- 22 | 35 55 76 55 --- 48
R03E | 4575 36 25 42 48 --- 21 | 33 42 32 54 --- 28
R07E | 2043 43 26 30 38 --- 19 | 44 22 32 41 --- 26
R08E | 1166 37 22 26 36 204 17 | 41 29 37 43 24 29
R10 | 1007 26 19 33 33 --- 16 | 27 33 45 21 --- 23
R11 | 1320 16 15 18 21 --- 10 | 30 28 38 31 --- 27
R13 | 831 27 16 25 24 --- 13 | 32 45 52 34 --- 36
R14 | 4940 26 12 26 14 --- 11 | 47 28 44 31 --- 32
R15 | 2918 31 17 33 26 157 15 | 33 20 54 33 69 28
R17 | 1047 30 12 20 20 --- 12 | 42 50 54 50 --- 47
R18 | 1620 24 26 21 23 --- 14 | 39 17 41 45 --- 29
R19 | 1163 23 18 17 30 --- 13 | 30 40 39 25 --- 29
R20 | 2155 22 26 30 25 --- 15 | 36 39 59 38 --- 39
R21 | 1623 39 25 16 19 --- 15 | 32 53 38 38 --- 35
R22 | 1380 15 25 40 31 --- 17 | 38 42 58 34 --- 32
R23 | 2076 24 24 26 39 --- 16 | 44 50 52 28 --- 36
R24 | 6121 29 24 20 23 --- 14 | 77 94 89 101 --- 87
------+------------------------------------+--------------------------------
RMS | 2659 31 22 28 31 182 |T 38 40 49 41 46 35
WRMS | 2659 31 21 27 31 182 |NE 39 41 51 39 69 36
MEDI | 1620 27 24 26 26 157 |MD 36 40 45 38 24 32
Table 3.1538.3 GPS week: 1538 Day: 3 MJD: 55013
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1083 24 18 29 37 --- 15 | 63 61 67 73 --- 62
R03E | 4263 37 17 46 43 --- 20 | 36 37 37 53 --- 35
R07E | 2153 33 14 33 29 --- 15 | 34 24 43 37 --- 28
R08E | 1134 18 13 33 35 182 14 | 29 31 51 53 37 34
R10 | 1086 19 19 26 31 --- 13 | 23 34 46 25 --- 27
R11 | 1105 24 14 25 24 --- 12 | 28 38 59 42 --- 37
R13 | 810 19 15 20 19 --- 10 | 38 39 29 28 --- 31
R14 | 5709 19 12 14 19 --- 9 | 40 42 42 36 --- 38
R15 | 1509 29 7 23 36 193 13 | 25 31 44 27 82 28
R17 | 1720 30 15 39 29 --- 16 | 53 59 84 51 --- 58
R18 | 1858 20 13 20 34 --- 12 | 25 28 45 48 --- 29
R19 | 743 10 8 17 21 --- 8 | 33 31 43 28 --- 30
R20 | 2444 18 18 30 34 --- 14 | 48 41 67 35 --- 44
R21 | 1342 27 24 36 25 --- 16 | 36 64 67 49 --- 51
R22 | 1252 19 20 19 33 --- 13 | 29 41 48 30 --- 32
R23 | 1986 29 26 31 46 --- 18 | 40 47 35 51 --- 36
R24 | 3740 30 17 44 24 --- 16 | 78 93 106 84 --- 87
------+------------------------------------+--------------------------------
RMS | 2394 25 17 30 31 188 |T 38 43 53 44 59 40
WRMS | 2394 24 15 29 31 188 |NE 38 45 55 41 82 40
MEDI | 1509 24 15 29 31 182 |MD 36 39 46 42 37 35
Table 3.1538.4 GPS week: 1538 Day: 4 MJD: 55014
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1108 45 26 23 41 --- 19 | 35 35 39 44 --- 31
R03E | 5632 33 18 33 37 --- 17 | 24 33 40 36 --- 27
R07E | 3828 31 18 33 19 --- 15 | 27 24 50 30 --- 23
R08E | 1782 22 20 24 33 197 14 | 25 25 40 46 27 27
R10 | 1282 34 21 24 22 --- 14 | 19 39 51 31 --- 32
R11 | 1352 21 24 13 25 --- 12 | 25 27 30 35 --- 26
R13 | 803 22 18 11 12 --- 9 | 17 38 32 28 --- 28
R14 | 1847 25 15 16 14 --- 10 | 30 41 36 33 --- 33
R15 | 1802 35 15 10 22 196 12 | 19 32 31 32 37 27
R17 | 1512 34 22 33 23 --- 16 | 33 52 61 28 --- 45
R18 | 1418 17 24 25 12 --- 12 | 22 31 46 33 --- 32
R19 | 894 20 13 21 18 --- 10 | 17 32 36 33 --- 27
R20 | 1973 22 24 21 22 --- 13 | 44 49 60 53 --- 47
R21 | 1916 25 24 18 29 --- 14 | 41 65 52 49 --- 51
R22 | 1039 18 18 25 30 --- 13 | 20 33 44 31 --- 25
R23 | 2987 44 40 20 41 --- 21 | 34 51 61 53 --- 45
R24 | 2639 20 23 21 26 --- 13 | 105 128 130 113 --- 118
------+------------------------------------+--------------------------------
RMS | 2316 29 22 23 27 196 |T 31 43 49 41 32 37
WRMS | 2316 29 20 22 27 196 |NE 32 47 51 42 37 41
MEDI | 1782 25 21 21 23 196 |MD 25 35 44 33 27 31
Table 3.1538.5 GPS week: 1538 Day: 5 MJD: 55015
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1464 39 21 20 48 --- 18 | 39 35 44 55 --- 38
R03E | 1831 30 21 24 47 --- 17 | 19 27 32 46 --- 18
R07E | 3431 35 18 37 34 --- 18 | 32 30 51 23 --- 28
R08E | 3123 22 19 26 31 246 14 | 16 23 38 34 26 19
R10 | 1414 26 27 18 49 --- 17 | 16 29 25 35 --- 19
R11 | 1375 14 19 19 21 --- 10 | 20 24 33 24 --- 20
R13 | 1659 25 11 22 14 --- 11 | 21 27 29 18 --- 18
R14 | 3423 15 15 14 17 --- 9 | 28 28 28 32 --- 26
R15 | 1454 28 18 11 27 203 12 | 22 27 29 24 40 21
R17 | 990 29 19 13 42 --- 15 | 29 45 44 26 --- 34
R18 | 1135 33 11 24 20 --- 13 | 16 27 34 23 --- 19
R19 | 1007 14 17 14 23 --- 10 | 20 22 22 39 --- 20
R20 | 1726 34 15 29 31 --- 15 | 33 34 41 35 --- 31
R21 | 1713 24 17 20 20 --- 11 | 23 30 44 47 --- 32
R22 | 815 25 32 22 27 --- 15 | 20 37 33 25 --- 19
R23 | 2660 34 27 37 44 --- 20 | 30 39 46 29 --- 28
R24 | 2619 45 18 31 19 --- 17 | 58 94 89 69 --- 78
------+------------------------------------+--------------------------------
RMS | 2048 29 20 24 32 226 |T 26 34 38 34 33 27
WRMS | 2048 28 18 21 32 226 |NE 25 35 38 32 40 28
MEDI | 1659 28 18 22 27 203 |MD 22 29 34 32 26 21
Table 3.1538.6 GPS week: 1538 Day: 6 MJD: 55016
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1568 32 10 22 38 --- 14 | 40 40 47 49 --- 40
R03E | 5011 31 12 22 51 --- 16 | 29 30 35 57 --- 31
R07E | 5084 28 15 28 33 --- 14 | 32 30 40 28 --- 28
R08E | 2889 19 8 30 33 218 12 | 26 24 37 36 30 25
R10 | 1841 29 23 35 37 --- 17 | 15 37 46 32 --- 31
R11 | 1386 20 11 34 27 --- 13 | 28 31 53 28 --- 30
R13 | 1467 25 8 22 25 --- 10 | 30 31 39 32 --- 30
R14 | 2836 24 10 22 29 --- 11 | 28 32 39 34 --- 30
R15 | 2869 29 14 15 32 212 12 | 27 33 34 35 38 30
R17 | 621 42 16 30 44 --- 17 | 44 65 58 37 --- 53
R18 | 1081 16 10 28 31 --- 12 | 28 42 56 60 --- 42
R19 | 1305 37 8 24 18 --- 12 | 33 44 45 50 --- 40
R20 | 2455 46 19 23 38 --- 17 | 52 43 46 40 --- 39
R21 | 1374 21 8 18 30 --- 10 | 26 51 49 54 --- 42
R22 | 798 15 11 19 22 --- 9 | 35 51 48 35 --- 41
R23 | 1083 32 22 28 40 --- 16 | 35 37 60 59 --- 41
R24 | 3033 38 18 33 18 --- 15 | 112 85 99 84 --- 91
------+------------------------------------+--------------------------------
RMS | 2517 30 14 26 33 215 |T 36 41 48 44 34 39
WRMS | 2517 29 13 24 33 215 |NE 37 44 51 44 38 41
MEDI | 1568 29 11 24 32 212 |MD 30 37 46 37 30 39
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