[IGSREPORT-18028] Wk 1557 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Nov 26 04:39:20 PST 2009
******************************************************************************
IGS Electronic Report 26 Nov 04:39:43 PST 2009 Message Number 18028
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1557 (Nov 08, 2009 - Nov 14, 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 2.1557.
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:
igl1557[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1557 in the SP3 format.
igl15577.sum Combination Report for GPS Week 1557.
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 | 502.5 ns
1 | 500.0 ns
2 | 497.7 ns
3 | 500.5 ns
4 | 505.0 ns
5 | 504.2 ns
6 | 504.2 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 1.1557, 1a.1557).
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 2.1557.0-6)
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 3.1557.0-6).
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 1557 summary. (Nov 08, 2009 - Nov 14, 2009)
Table 1.1557.a GPS week : 1557 MJD: 55143.0-55149.0
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 113| 1 0 3 30 7 -53 -.25 37 34 | 0 -67 2469 2693
| 1 0 3 29 27 180 .08 | 0 963
cod 237| -2 -1 -9 9 9 65 -.20 20 16 | --- --- --- ---
| 1 1 3 36 20 59 .05 | --- ---
esx 127| 0 0 -4 -21 -5 15 .38 26 23 | 131611 -725 4415 9320
| 1 1 6 19 28 81 .07 | 6659 3844
iac n/a| 1 1 24 -20 -13 -102 -.01 39 39 | 502332 -491 4424 8481
| 1 1 8 60 25 86 .09 | 2839 2142
mcc n/a| 2 -3 23 -27 43 577 .89 111 111 | --- --- --- ---
| 9 14 22 134 138 204 .59 | --- ---
Table 1.1557.b GPS week : 1557 MJD: 55143.0-55149.0
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 | 11 11 14 13 7 10 11 |
R03 | 10 10 11 12 10 12 16 |
R07 | 12 13 13 10 14 7 12 |
R08 | 9 13 10 12 11 10 6 |
R10 | 23 20 24 30 32 37 22 |
R11 | 21 24 22 31 24 27 27 |
R13 | 22 23 20 20 22 22 19 |
R14 | 20 17 19 20 18 19 26 |
R15 | 20 21 18 28 23 17 19 |
R17 | 11 10 10 15 13 14 11 |
R18 | 9 11 12 12 15 14 14 |
R19 | 13 14 13 12 10 12 11 |
R20 | 14 12 11 16 13 12 12 |
R21 | 12 14 13 15 16 12 17 |
R23 | 17 16 18 17 17 11 17 |
Table 1.1557.c GPS week : 1557 MJD: 55143.0-55149.0
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 1557 0 | 112 -72 88 1274 2226 -11990 90.1 1610 1610 | 502456 0
brd 1557 1 |31360 -3751 -7813 -755 -230800 135800 71.4 >>>>> >>>>> | 499969 0
brd 1557 2 | -113 22 210 3234 -308 -10710 90.1 2029 2029 | 497725 0
brd 1557 3 | -154 -136 80 518 459 -16110 90.7 2095 2095 | 500480 0
brd 1557 4 | 109 -22 100 -2703 1587 -20130 89.1 1831 1831 | 505017 0
brd 1557 5 | 78 5 22 -371 1875 -21730 86.3 1988 1988 | 504185 0
brd 1557 6 | -64 34 57 -1400 1249 -20300 87.0 2004 2004 | 504162 0
-------------+------------------------------------------------------------+----------------
brd 1557 mean| 4475 -559 -1036 -29 -31958 4975 86.4 >>>>> >>>>> | 501999 0
brd 1557 sdev|11855 1408 2988 1928 87684 57844 6.8 >>>>> >>>>> | 2691 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 2.1557.0 GPS week: 1557 Day: 0 MJD: 55143
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 113| 1 0 2 -16 28 -32 -.24 31 29 | 0 1196 2400 2520
cod 237| -3 -3 -1 60 -20 41 -.13 21 19 | --- --- --- ---
esx 127| -2 0 -10 2 -6 54 .24 25 23 | 135692 -3163 4400 9833
iac n/a| 2 3 11 -101 19 -80 .01 32 32 | 503301 -2177 4412 9075
mcc n/a| 0 8 -3 -226 59 668 .21 67 67 | --- --- --- ---
Table 2.1557.1 GPS week: 1557 Day: 1 MJD: 55144
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 113| -1 0 2 31 7 -142 -.24 32 29 | 0 -1044 1989 2152
cod 237| -2 -2 -13 20 25 66 -.16 17 15 | --- --- --- ---
esx 127| 0 0 7 4 2 34 .43 27 26 | 134940 7809 3705 8249
iac n/a| 4 0 20 -85 -56 -9 .06 38 38 | 499011 1668 3731 7149
mcc n/a| 4 8 3 -42 -17 461 .38 84 84 | --- --- --- ---
Table 2.1557.2 GPS week: 1557 Day: 2 MJD: 55145
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 113| 3 0 0 11 39 -37 -.32 38 38 | 0 -1107 2710 2912
cod 237| -4 0 -8 -2 20 113 -.24 18 13 | --- --- --- ---
esx 127| 0 1 -7 -27 -14 -9 .37 20 19 | 125290 -2318 4359 9142
iac n/a| 1 2 33 4 0 -77 .06 39 39 | 499839 -3007 4385 7661
mcc n/a| 2 7 7 -6 313 576 .40 130 130 | --- --- --- ---
Table 2.1557.3 GPS week: 1557 Day: 3 MJD: 55146
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 113| 2 -2 4 69 12 317 -.10 31 25 | 0 100 2079 2189
cod 237| -4 0 -12 -49 -1 -46 -.20 23 16 | --- --- --- ---
esx 127| 1 0 -3 -36 3 -142 .42 33 28 | 139469 -974 4204 10115
iac n/a| 2 3 31 33 -28 -274 .03 49 49 | 500241 718 4217 9120
mcc n/a| 17 -10 22 -155 -29 271 .80 109 109 | --- --- --- ---
Table 2.1557.4 GPS week: 1557 Day: 4 MJD: 55147
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 113| 2 -1 8 61 9 -59 -.20 44 43 | 0 1085 2398 2691
cod 237| -3 -1 -6 -18 19 56 -.26 19 16 | --- --- --- ---
esx 127| 1 0 -8 -14 -31 -5 .41 25 22 | 137193 -2738 4295 9710
iac n/a| 0 3 26 53 8 -39 -.04 40 40 | 505517 -133 4286 9038
mcc n/a| -9 -5 41 -13 64 598 1.58 110 110 | --- --- --- ---
Table 2.1557.5 GPS week: 1557 Day: 5 MJD: 55148
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 113| 0 0 2 41 -46 -207 -.28 44 42 | 0 108 2738 3103
cod 237| 0 0 -10 25 -11 95 -.24 20 17 | --- --- --- ---
esx 127| 0 0 0 -43 46 114 .43 23 20 | 124231 -1235 5127 8119
iac n/a| 2 -1 17 9 -10 -97 -.19 38 38 | 502132 2194 5133 7728
mcc n/a| -6 -31 41 166 -137 523 1.47 97 97 | --- --- --- ---
Table 2.1557.6 GPS week: 1557 Day: 6 MJD: 55149
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 113| 0 0 7 16 -1 -214 -.35 39 34 | 0 -810 2970 3285
cod 237| 0 0 -11 28 34 134 -.17 19 14 | --- --- --- ---
esx 127| -1 -2 -8 -32 -40 59 .38 25 24 | 124466 -2458 4815 10075
iac n/a| 0 0 29 -57 -24 -140 .02 39 39 | 506286 -2705 4809 9598
mcc n/a| 8 1 54 89 52 941 1.43 182 182 | --- --- --- ---
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 3.1557.0 GPS week: 1557 Day: 0 MJD: 55143
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 805 15 20 15 21 --- 10 | 22 26 35 36 --- 26
R03 | 1683 17 9 22 15 --- 9 | 22 24 39 30 --- 25
R07 | 1217 31 17 20 15 --- 12 | 24 29 38 43 --- 28
R08 | 688 13 19 14 15 73 9 | 20 28 30 37 36 23
R10E | 969 51 34 31 47 --- 23 | 29 30 37 68 --- 30
R11E | 2003 46 21 32 48 82 21 | 57 60 72 70 55 56
R13E | 1343 44 24 39 48 --- 22 | 72 41 45 61 --- 44
R14E | 3129 34 23 25 51 --- 19 | 52 29 32 60 --- 32
R15E | 3093 32 24 25 55 38 20 | 35 34 49 74 46 40
R17 | 1010 23 17 22 13 --- 11 | 32 45 31 28 --- 33
R18 | 673 16 12 20 16 --- 9 | 32 45 51 44 --- 42
R19 | 1267 25 13 12 34 --- 12 | 35 43 46 39 --- 40
R20 | 1199 34 13 30 15 --- 14 | 23 31 45 38 --- 29
R21 | 1235 20 18 27 14 --- 12 | 39 60 54 47 --- 49
R23 | 1127 30 32 26 23 --- 16 | 30 44 43 41 --- 32
------+------------------------------------+--------------------------------
RMS | 1609 31 21 25 32 67 |T 34 37 43 47 45 35
WRMS | 1609 29 19 23 32 67 |NE 27 37 41 38 36 32
MEDI | 1217 30 19 25 21 73 |MD 32 34 43 43 46 32
Table 3.1557.1 GPS week: 1557 Day: 1 MJD: 55144
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 13 14 22 27 --- 10 | 15 29 36 38 --- 25
R03 |>>>>> 19 10 21 22 --- 10 | 12 22 39 39 --- 22
R07 |>>>>> 16 18 29 21 --- 12 | 19 31 40 30 --- 24
R08 |>>>>> 26 17 22 26 121 13 | 16 24 37 34 59 21
R10E |24375 41 19 26 54 --- 19 | 48 30 26 56 --- 27
R11E |>>>>> 49 29 37 60 78 24 | 65 64 70 71 94 57
R13E |>>>>> 63 23 29 38 --- 22 | 36 44 53 52 --- 40
R14E |25432 22 24 24 50 --- 17 | 51 30 35 57 --- 34
R15E |>>>>> 44 15 40 51 27 21 | 35 23 53 57 64 29
R17 |>>>>> 17 14 21 17 --- 10 | 18 24 29 23 --- 19
R18 |>>>>> 22 8 26 19 --- 10 | 24 18 37 19 --- 17
R19 |>>>>> 21 8 27 43 --- 14 | 25 25 27 40 --- 22
R20 |>>>>> 31 7 22 24 --- 12 | 19 21 38 30 --- 21
R21 |>>>>> 19 22 23 29 --- 13 | 26 49 38 26 --- 34
R23 |>>>>> 25 18 25 48 --- 16 | 23 25 47 29 --- 25
------+------------------------------------+--------------------------------
RMS |>>>>> 32 17 27 38 84 |T 28 30 40 40 72 27
WRMS |>>>>> 29 15 26 38 84 |NE 19 26 36 30 59 23
MEDI |>>>>> 22 17 25 29 78 |MD 24 25 38 38 64 25
Table 3.1557.2 GPS week: 1557 Day: 2 MJD: 55145
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1470 25 10 31 26 --- 13 | 22 18 50 20 --- 26
R03 | 1586 19 11 17 28 --- 10 | 16 28 31 28 --- 22
R07 | 1799 24 14 13 41 --- 12 | 19 21 28 37 --- 22
R08 | 1707 19 9 12 29 114 9 | 21 20 26 33 68 18
R10E | 1152 53 29 26 66 --- 23 | 32 36 45 73 --- 34
R11E | 2227 60 25 25 54 156 22 | 46 101 84 80 93 79
R13E | 2032 65 21 19 37 --- 20 | 30 52 47 50 --- 37
R14E | 2572 48 27 14 50 --- 19 | 42 44 39 46 --- 34
R15E | 2356 42 20 20 52 114 18 | 31 35 48 69 65 36
R17 | 2511 24 12 18 17 --- 10 | 35 24 28 24 --- 23
R18 | 2082 28 15 17 29 --- 12 | 25 35 35 37 --- 30
R19 | 1853 31 14 23 18 --- 12 | 33 41 59 43 --- 42
R20 | 1702 19 14 16 27 --- 10 | 20 30 36 34 --- 28
R21 | 1756 31 14 15 32 --- 12 | 34 55 51 37 --- 45
R23 | 2888 46 19 25 43 --- 18 | 30 25 36 25 --- 22
------+------------------------------------+--------------------------------
RMS | 2030 38 18 20 39 129 |T 29 37 42 42 75 33
WRMS | 2030 38 13 19 39 129 |NE 25 29 38 31 68 27
MEDI | 1853 31 14 18 32 114 |MD 30 35 39 37 68 30
Table 3.1557.3 GPS week: 1557 Day: 3 MJD: 55146
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 885 20 14 27 29 --- 12 | 20 26 30 50 --- 21
R03 | 1044 22 12 23 27 --- 12 | 16 28 37 36 --- 22
R07 | 2266 18 11 16 27 --- 10 | 18 39 41 47 --- 30
R08 | 2556 18 10 10 42 114 11 | 23 18 28 33 51 18
R10E | 1598 63 42 35 66 --- 29 | 52 39 59 73 --- 46
R11E | 2652 42 37 46 99 49 31 | 85 84 86 101 53 78
R13E | 1102 40 19 30 56 --- 20 | 44 67 78 72 --- 59
R14E | 3011 30 31 32 54 --- 20 | 30 61 40 52 --- 36
R15E | 3231 44 28 73 47 141 28 | 64 55 68 58 33 49
R17 | 1371 18 20 28 36 --- 14 | 17 37 26 33 --- 20
R18 | 2004 13 19 27 20 --- 11 | 47 48 61 39 --- 46
R19 | 2213 19 10 22 35 --- 12 | 37 43 47 46 --- 37
R20 | 2351 14 23 25 50 --- 16 | 34 40 48 70 --- 39
R21 | 2039 30 14 18 46 --- 15 | 23 51 52 52 --- 40
R23 | 1212 26 15 36 41 --- 16 | 42 37 60 48 --- 31
------+------------------------------------+--------------------------------
RMS | 2094 31 23 33 49 109 |T 36 44 50 54 45 38
WRMS | 2094 25 16 28 49 109 |NE 27 36 43 45 51 30
MEDI | 2039 22 19 27 42 114 |MD 34 40 48 50 51 37
Table 3.1557.4 GPS week: 1557 Day: 4 MJD: 55147
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1632 15 8 10 16 --- 7 | 23 26 29 34 --- 25
R03 | 1224 26 13 14 21 --- 10 | 27 39 40 39 --- 34
R07 | 820 19 20 23 33 --- 13 | 23 27 30 30 --- 23
R08 | 2590 24 14 17 26 99 11 | 21 26 30 28 33 23
R10E | 1983 111 31 26 54 --- 32 | 49 56 57 65 --- 50
R11E | 2385 43 26 27 75 43 23 | 47 37 59 70 39 39
R13E | 1121 65 20 20 51 --- 21 | 33 37 47 63 --- 33
R14E | 2523 41 20 21 50 --- 18 | 44 48 58 57 --- 43
R15E | 1478 48 22 49 38 157 22 | 98 84 108 91 23 89
R17 | 1244 30 15 15 34 --- 12 | 24 35 39 25 --- 28
R18 | 1269 22 19 36 24 --- 15 | 39 40 80 24 --- 47
R19 | 1359 22 16 17 15 --- 10 | 33 41 49 36 --- 38
R20 | 2692 29 15 15 35 --- 13 | 19 47 32 55 --- 36
R21 | 2457 33 19 27 34 --- 15 | 29 40 39 55 --- 34
R23 | 1005 23 21 28 50 --- 17 | 30 37 40 45 --- 27
------+------------------------------------+--------------------------------
RMS | 1831 44 19 25 40 110 |T 35 41 49 47 31 37
WRMS | 1831 43 16 22 40 110 |NE 26 35 40 37 33 31
MEDI | 1478 29 19 21 34 99 |MD 30 39 40 45 33 34
Table 3.1557.5 GPS week: 1557 Day: 5 MJD: 55148
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1221 21 10 20 18 --- 10 | 22 22 21 32 --- 19
R03 | 1105 14 21 17 28 --- 12 | 15 42 32 36 --- 28
R07 | 1766 15 9 8 14 --- 6 | 23 25 36 39 --- 27
R08 | 1296 11 15 15 23 100 9 | 20 16 22 24 25 15
R10E | 1823 125 41 35 52 --- 37 | 39 66 59 70 --- 52
R11E | 1020 64 26 41 61 78 26 | 61 59 57 70 51 50
R13E | 998 32 20 33 68 --- 22 | 30 46 64 75 --- 44
R14E | 1928 35 15 21 61 --- 19 | 23 46 48 59 --- 36
R15E | 2758 49 14 23 35 111 17 | 53 71 69 72 21 64
R17 | 2173 21 24 25 27 --- 14 | 26 35 44 37 --- 34
R18 | 2780 30 21 15 33 --- 13 | 18 53 26 52 --- 36
R19 | 910 17 21 25 13 --- 11 | 30 37 27 24 --- 25
R20 | 2064 21 19 20 24 --- 12 | 41 51 58 47 --- 48
R21 | 2284 35 16 12 20 --- 12 | 44 71 54 72 --- 59
R23 | 3512 16 15 19 21 --- 10 | 33 34 36 42 --- 30
------+------------------------------------+--------------------------------
RMS | 1988 44 20 23 38 97 |T 31 44 43 50 32 37
WRMS | 1988 42 17 20 38 97 |NE 27 38 35 40 25 32
MEDI | 1823 21 19 20 27 100 |MD 30 46 44 47 25 36
Table 3.1557.6 GPS week: 1557 Day: 6 MJD: 55149
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 882 17 10 19 32 --- 11 | 20 23 30 32 --- 23
R03 | 1013 34 17 26 39 --- 16 | 23 37 47 33 --- 33
R07 | 2686 27 16 17 29 --- 12 | 22 39 34 34 --- 29
R08 | 922 11 8 7 17 96 6 | 21 22 25 26 47 21
R10E | 1663 64 25 27 37 --- 21 | 62 44 44 54 --- 41
R11E | 1178 73 25 41 56 163 26 | 71 65 69 90 59 65
R13E | 1737 40 20 23 55 --- 19 | 48 44 48 67 --- 42
R14E | 1960 45 32 31 76 --- 26 | 45 60 62 66 --- 48
R15E | 4559 49 21 24 43 252 19 | 116 86 90 83 26 89
R17 | 1318 25 9 21 23 --- 11 | 32 52 59 44 --- 47
R18 | 1225 40 7 25 23 --- 13 | 25 48 58 50 --- 45
R19 | 898 18 18 18 23 --- 11 | 37 58 44 37 --- 45
R20 | 2242 31 10 13 31 --- 11 | 37 57 50 69 --- 52
R21 | 1657 33 22 37 24 --- 16 | 58 77 106 78 --- 79
R23 | 2599 34 22 31 37 --- 17 | 42 40 62 64 --- 44
------+------------------------------------+--------------------------------
RMS | 2004 39 19 25 39 182 |T 43 50 55 55 44 46
WRMS | 2004 34 14 24 39 182 |NE 31 45 51 46 47 41
MEDI | 1657 34 18 24 32 163 |MD 37 48 50 54 47 45
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