[IGSREPORT-17946] Wk 1553 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Oct 29 11:56:26 PDT 2009
******************************************************************************
IGS Electronic Report 29 Oct 11:56:49 PDT 2009 Message Number 17946
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1553 (Oct 11, 2009 - Oct 17, 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 2.1553.
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:
igl1553[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1553 in the SP3 format.
igl15537.sum Combination Report for GPS Week 1553.
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 | 108.9 ns
1 | 195.0 ns
2 | 193.4 ns
3 | 189.1 ns
4 | 187.4 ns
5 | 180.5 ns
6 | 117.1 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 1.1553, 1a.1553).
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 2.1553.0-6)
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 3.1553.0-6).
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 1553 summary. (Oct 11, 2009 - Oct 17, 2009)
Table 1.1553.a GPS week : 1553 MJD: 55115.0-55121.0
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 102| 0 0 -1 18 5 58 -.16 25 22 | 0 151 3970 4649
| 1 2 2 47 34 131 .03 | 0 1634
cod 226| -2 0 -1 8 -5 97 -.13 16 15 | --- --- --- ---
| 1 1 1 25 33 27 .02 | --- ---
esx 120| 2 -2 1 -16 -11 -45 .45 24 22 | 121167 557 4654 10023
| 2 1 3 26 47 91 .05 | 38258 4851
iac n/a| 0 0 2 -20 21 -167 -.11 24 24 | 167999 -994 4647 9938
| 1 1 5 43 25 70 .03 | 38008 2473
mcc n/a| -1 2 21 1 12 417 -.12 96 96 | --- --- --- ---
| 10 8 11 129 111 297 .29 | --- ---
Table 1.1553.b GPS week : 1553 MJD: 55115.0-55121.0
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 9 14 14 11 9 9 |
R03 | 13 13 11 17 10 13 12 |
R07 | 11 11 10 9 11 12 10 |
R08 | 12 12 9 9 12 18 13 |
R10 | 13 13 11 12 10 11 9 |
R11 | 12 14 10 16 13 11 13 |
R13 | 11 11 10 16 14 10 10 |
R14 | 12 11 9 9 11 13 10 |
R15 | 13 11 10 12 12 14 13 |
R17 | 14 12 13 9 18 12 10 |
R18 | 13 9 9 12 13 14 14 |
R19 | 9 8 9 10 8 11 8 |
R20 | 11 10 11 10 8 13 16 |
R21 | 15 12 14 11 14 9 8 |
R23 | 15 13 13 14 17 16 15 |
R24 | 26 30 20 22 25 13 11 |
Table 1.1553.c GPS week : 1553 MJD: 55115.0-55121.0
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 1553 0 | -69 86 107 -2984 -72 -9075 89.5 3013 3013 | 108874 0
brd 1553 1 | 2916 -7017 -582 -29550 3981 151700 60.4 >>>>> >>>>> | 194973 0
brd 1553 2 | 6 -2 162 -2400 879 -3969 86.6 2535 2535 | 193378 0
brd 1553 3 | -19 -126 229 902 2053 -9678 88.2 2334 2334 | 189120 0
brd 1553 4 | 25 61 102 -727 2879 -7774 93.1 2323 2323 | 187434 0
brd 1553 5 | 86 58 80 763 325 -15470 90.6 2096 2096 | 180541 0
brd 1553 6 | 3 98 53 1131 -460 -20420 87.5 1782 1782 | 117115 0
-------------+------------------------------------------------------------+----------------
brd 1553 mean| 421 -977 21 -4694 1369 12187 85.1 >>>>> >>>>> | 167347 0
brd 1553 sdev| 1101 2664 272 11081 1649 61754 11.1 >>>>> >>>>> | 37493 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 2.1553.0 GPS week: 1553 Day: 0 MJD: 55115
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 102| 1 2 -4 36 -24 -17 -.17 28 23 | 0 -789 4898 5788
cod 226| -2 0 1 -5 27 96 -.11 18 15 | --- --- --- ---
esx 120| 2 -3 3 -40 -5 -67 .37 28 26 | 61247 957 5105 9985
iac n/a| 1 0 0 13 0 -85 -.10 23 23 | 109343 921 5007 9730
mcc n/a| 11 3 22 -192 -174 894 -.12 106 106 | --- --- --- ---
Table 2.1553.1 GPS week: 1553 Day: 1 MJD: 55116
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 102| 1 0 1 90 -10 205 -.17 28 21 | 0 3099 5191 6371
cod 226| -2 0 0 -25 13 98 -.13 17 15 | --- --- --- ---
esx 120| -1 -1 -3 -49 10 -168 .43 23 18 | 154412 -5930 5462 11645
iac n/a| 0 0 2 51 13 -179 -.09 24 24 | 197222 -5418 5458 11511
mcc n/a| -7 -12 35 207 -2 293 -.04 93 93 | --- --- --- ---
Table 2.1553.2 GPS week: 1553 Day: 2 MJD: 55117
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 102| -2 2 -1 -2 -28 123 -.10 22 21 | 0 790 3475 4137
cod 226| -2 1 -4 30 12 108 -.15 15 15 | --- --- --- ---
esx 120| 4 -4 7 -27 15 -99 .45 22 19 | 139413 8625 4985 12846
iac n/a| 0 0 2 -4 -3 -221 -.12 21 21 | 193619 91 4985 13103
mcc n/a| -4 5 19 109 -5 543 .25 88 88 | --- --- --- ---
Table 2.1553.3 GPS week: 1553 Day: 3 MJD: 55118
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 102| 0 -3 0 -33 32 61 -.14 23 18 | 0 -1303 3082 3608
cod 226| -4 0 0 26 -60 106 -.15 20 17 | --- --- --- ---
esx 120| 3 -1 2 6 0 73 .53 23 21 | 141418 647 4431 8632
iac n/a| -2 0 -6 -58 64 -280 -.07 23 23 | 191881 -2662 4501 8284
mcc n/a| 7 10 36 -87 37 350 -.42 65 65 | --- --- --- ---
Table 2.1553.4 GPS week: 1553 Day: 4 MJD: 55119
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 102| -1 0 -2 44 60 -39 -.17 27 21 | 0 -186 4119 4774
cod 226| 0 0 -4 -12 -8 121 -.14 16 15 | --- --- --- ---
esx 120| 3 -2 4 -5 -110 49 .51 29 26 | 145867 4154 4111 9095
iac n/a| 0 2 4 -31 47 -180 -.07 23 23 | 186585 259 4116 9160
mcc n/a| 5 -2 13 -29 204 224 -.16 91 91 | --- --- --- ---
Table 2.1553.5 GPS week: 1553 Day: 5 MJD: 55120
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 102| 1 2 -2 37 27 213 -.21 26 26 | 0 1039 3624 4032
cod 226| 0 -2 -1 6 -41 38 -.13 14 13 | --- --- --- ---
esx 120| 0 -1 -2 -25 34 -117 .41 21 21 | 135056 -708 4099 8877
iac n/a| 1 1 12 -37 17 -137 -.15 28 28 | 180722 1695 4089 9031
mcc n/a| -17 9 6 -4 41 630 -.54 120 120 | --- --- --- ---
Table 2.1553.6 GPS week: 1553 Day: 6 MJD: 55121
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 102| 2 0 -2 -42 -15 -137 -.14 22 21 | 0 -1590 3402 3839
cod 226| -1 0 -2 42 18 110 -.10 13 12 | --- --- --- ---
esx 120| 1 -2 0 26 -25 12 .42 22 21 | 70762 -3843 4388 9087
iac n/a| 1 0 2 -74 12 -87 -.15 25 25 | 116623 -1844 4377 8753
mcc n/a| -1 6 13 7 -13 -11 .17 113 113 | --- --- --- ---
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 3.1553.0 GPS week: 1553 Day: 0 MJD: 55115
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2127 12 13 22 23 --- 10 | 16 21 21 27 --- 15
R03 | 898 24 13 33 17 --- 12 | 14 30 22 21 --- 19
R07 | 7756 16 18 23 20 --- 11 | 24 33 35 25 --- 24
R08 | 887 18 22 11 28 82 12 | 15 32 26 33 53 22
R10 | 4775 27 15 29 21 --- 13 | 58 60 43 60 --- 53
R11 | 1024 23 12 28 20 123 11 | 67 68 58 69 36 64
R13 | 1894 23 14 19 22 --- 11 | 62 63 68 67 --- 63
R14 | 2889 33 17 11 16 --- 12 | 29 32 29 25 --- 26
R15 | 2839 24 11 33 22 110 13 | 48 46 52 49 40 47
R17 | 2637 23 20 16 33 --- 14 | 56 53 66 86 --- 62
R18 | 1435 17 17 35 21 --- 13 | 30 41 58 51 --- 40
R19 | 645 16 8 21 18 --- 9 | 33 31 34 40 --- 32
R20 | 750 24 15 23 17 --- 11 | 42 37 36 39 --- 36
R21 | 1388 29 17 36 21 --- 14 | 33 38 45 43 --- 36
R23 | 853 29 19 39 18 --- 15 | 71 91 98 87 --- 85
R24 | 4742 64 35 47 37 --- 26 | 133 207 209 156 --- 177
------+------------------------------------+--------------------------------
RMS | 3013 28 18 28 23 106 |T 45 55 56 54 43 50
WRMS | 3013 23 15 26 23 106 |NE 45 55 56 54 43 50
MEDI | 1435 23 15 23 21 110 |MD 33 38 43 43 40 36
Table 3.1553.1 GPS week: 1553 Day: 1 MJD: 55116
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 12 16 13 19 --- 9 | 26 26 30 29 --- 24
R03 |>>>>> 18 17 28 23 --- 12 | 13 23 31 28 --- 15
R07 |>>>>> 25 7 19 21 --- 10 | 19 18 29 18 --- 17
R08 |>>>>> 16 16 14 33 121 12 | 12 23 25 30 73 17
R10 |>>>>> 16 16 25 27 --- 12 | 35 45 37 34 --- 34
R11 |>>>>> 32 14 30 22 84 14 | 40 62 76 48 42 54
R13 |>>>>> 18 10 27 20 --- 11 | 85 83 81 86 --- 82
R14 |>>>>> 18 13 19 26 --- 11 | 22 29 33 33 --- 24
R15 |>>>>> 15 17 16 27 64 11 | 41 44 39 33 44 37
R17 |>>>>> 24 22 15 23 --- 12 | 52 41 51 57 --- 47
R18 |>>>>> 15 15 13 15 --- 8 | 24 28 30 25 --- 23
R19 |>>>>> 11 10 16 14 --- 7 | 23 19 25 22 --- 18
R20 |>>>>> 22 15 12 17 --- 9 | 33 43 48 40 --- 39
R21 |>>>>> 29 9 23 18 --- 11 | 24 29 35 29 --- 25
R23 |>>>>> 29 13 19 29 --- 13 | 52 60 66 65 --- 58
R24 |>>>>> 78 42 45 35 --- 30 | 104 172 175 119 --- 142
------+------------------------------------+--------------------------------
RMS |>>>>> 28 17 23 24 93 |T 37 46 50 43 53 41
WRMS |>>>>> 21 15 18 24 93 |NE 37 46 50 43 53 41
MEDI |>>>>> 18 15 19 22 84 |MD 26 29 35 33 44 25
Table 3.1553.2 GPS week: 1553 Day: 2 MJD: 55117
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2890 26 25 18 26 --- 14 | 12 31 37 27 --- 22
R03 | 1388 20 10 15 24 --- 10 | 13 23 29 20 --- 15
R07 | 4141 23 15 12 19 --- 10 | 21 24 26 32 --- 23
R08 | 1315 17 12 12 20 81 9 | 24 19 24 21 105 16
R10 | 4632 23 14 13 21 --- 10 | 32 38 37 48 --- 35
R11 | 811 22 12 21 12 98 10 | 60 64 74 61 38 63
R13 | 1442 15 11 21 21 --- 10 | 63 77 93 73 --- 75
R14 | 2070 12 13 16 22 --- 9 | 27 34 33 36 --- 30
R15 | 2539 10 16 20 19 84 9 | 51 51 55 48 51 49
R17 | 1049 31 15 26 14 --- 13 | 50 45 51 48 --- 45
R18 | 1829 14 14 15 18 --- 8 | 29 33 45 35 --- 33
R19 | 1391 15 12 17 17 --- 9 | 29 33 33 30 --- 27
R20 | 1283 16 14 26 20 --- 11 | 35 35 37 43 --- 34
R21 | 917 23 18 31 20 --- 13 | 31 45 46 38 --- 37
R23 | 2964 20 17 23 25 --- 12 | 62 75 61 80 --- 69
R24 | 4586 42 20 46 31 --- 20 | 104 100 94 76 --- 87
------+------------------------------------+--------------------------------
RMS | 2534 22 15 22 21 88 |T 40 45 48 44 64 41
WRMS | 2534 21 15 19 21 88 |NE 40 45 48 44 64 41
MEDI | 1442 20 14 18 20 84 |MD 31 35 37 38 51 34
Table 3.1553.3 GPS week: 1553 Day: 3 MJD: 55118
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1671 12 21 26 31 --- 13 | 30 30 44 33 --- 29
R03 | 1671 17 36 27 34 --- 17 | 17 41 31 47 --- 24
R07 | 1906 16 14 17 16 --- 9 | 17 29 43 26 --- 24
R08 | 1353 11 17 13 18 41 8 | 24 42 46 35 67 34
R10 | 3321 20 19 22 21 --- 11 | 36 38 38 43 --- 31
R11 | 1289 28 24 26 29 96 15 | 37 53 58 29 42 40
R13 | 1550 27 17 32 28 --- 15 | 130 152 152 130 --- 140
R14 | 3241 12 11 13 21 --- 8 | 24 24 25 26 --- 21
R15 | 5812 20 14 24 22 45 11 | 28 30 41 32 46 27
R17 | 1004 18 13 15 16 --- 9 | 47 54 67 58 --- 54
R18 | 937 22 13 23 21 --- 11 | 35 35 37 42 --- 33
R19 | 1774 12 17 15 21 --- 9 | 29 28 41 41 --- 29
R20 | 1690 15 14 21 16 --- 9 | 37 45 42 35 --- 37
R21 | 719 15 16 22 18 --- 10 | 36 43 55 48 --- 42
R23 | 1714 26 25 20 22 --- 13 | 51 83 66 63 --- 63
R24 | 2313 52 32 32 25 --- 21 | 164 191 208 183 --- 184
------+------------------------------------+--------------------------------
RMS | 2333 23 20 23 23 65 |T 46 57 62 54 51 50
WRMS | 2333 18 17 21 23 65 |NE 46 57 62 54 51 50
MEDI | 1671 17 17 22 21 45 |MD 35 41 43 41 46 33
Table 3.1553.4 GPS week: 1553 Day: 4 MJD: 55119
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2947 16 15 17 27 --- 11 | 15 31 34 23 --- 22
R03 | 2251 14 9 16 24 --- 9 | 26 26 26 29 --- 22
R07 | 1718 22 11 20 20 --- 10 | 38 28 37 44 --- 33
R08 | 1545 20 12 31 21 71 12 | 30 20 48 19 28 17
R10 | 4016 13 15 24 19 --- 10 | 23 31 41 28 --- 26
R11 | 728 22 17 23 30 109 13 | 42 51 53 39 56 43
R13 | 1096 23 23 24 25 --- 14 | 93 98 109 98 --- 97
R14 | 4432 15 14 21 24 --- 10 | 41 30 35 43 --- 31
R15 | 4237 19 18 20 25 88 12 | 30 44 48 43 41 38
R17 | 1040 46 14 40 19 --- 17 | 76 54 38 56 --- 53
R18 | 900 19 16 36 20 --- 13 | 34 39 66 38 --- 40
R19 | 1375 18 9 13 17 --- 8 | 26 33 31 37 --- 29
R20 | 2045 14 8 19 17 --- 8 | 38 34 44 34 --- 34
R21 | 768 14 18 31 28 --- 13 | 56 59 36 67 --- 53
R23 | 1225 41 17 40 22 --- 17 | 51 42 56 39 --- 40
R24 | 1302 59 30 51 31 --- 24 | 77 135 154 107 --- 116
------+------------------------------------+--------------------------------
RMS | 2322 27 16 29 23 91 |T 43 47 53 46 41 43
WRMS | 2322 21 15 26 23 91 |NE 43 47 53 46 41 43
MEDI | 1375 19 15 23 22 88 |MD 38 34 41 39 41 34
Table 3.1553.5 GPS week: 1553 Day: 5 MJD: 55120
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1184 17 15 12 18 --- 9 | 33 23 33 34 --- 26
R03 | 1143 37 9 19 19 --- 12 | 22 29 40 29 --- 23
R07 | 1998 24 17 24 20 --- 12 | 31 28 29 27 --- 21
R08 | 1740 54 12 26 25 94 17 | 27 32 49 39 51 30
R10 | 3606 11 11 20 30 --- 10 | 37 30 33 33 --- 27
R11 | 754 18 13 15 28 129 10 | 41 48 49 31 81 40
R13 | 938 22 12 14 19 --- 9 | 146 141 153 152 --- 147
R14 | 3459 16 12 32 26 --- 12 | 30 25 44 32 --- 25
R15 | 3570 17 17 16 45 133 14 | 20 28 28 36 65 21
R17 | 1466 20 15 24 23 --- 11 | 46 40 49 52 --- 42
R18 | 908 30 15 18 36 --- 14 | 42 36 47 65 --- 42
R19 | 893 11 11 23 27 --- 10 | 36 41 59 40 --- 42
R20 | 1867 20 11 13 41 --- 12 | 26 31 28 31 --- 24
R21 | 1672 20 9 20 12 --- 8 | 31 46 61 42 --- 43
R23 | 2332 37 18 29 30 --- 16 | 21 50 41 51 --- 38
R24 | 2427 28 18 16 24 --- 12 | 186 198 215 203 --- 199
------+------------------------------------+--------------------------------
RMS | 2096 26 14 21 28 120 |T 48 51 59 56 65 49
WRMS | 2096 26 13 21 28 120 |NE 48 51 59 56 65 49
MEDI | 1672 20 12 19 25 129 |MD 31 32 44 36 65 30
Table 3.1553.6 GPS week: 1553 Day: 6 MJD: 55121
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 663 11 18 17 16 --- 9 | 20 27 27 21 --- 17
R03 | 948 12 20 20 26 --- 11 | 14 27 31 31 --- 22
R07 | 1620 23 11 16 17 --- 9 | 31 33 39 37 --- 32
R08 | 1013 31 12 27 20 158 13 | 18 27 34 20 76 21
R10 | 3281 13 8 12 30 --- 9 | 43 35 36 38 --- 35
R11 | 1136 34 12 18 27 105 13 | 43 49 50 47 103 46
R13 | 1166 18 9 17 23 --- 9 | 109 111 115 111 --- 111
R14 | 1617 18 10 23 22 --- 10 | 31 30 33 34 --- 28
R15 | 3462 25 12 21 33 46 13 | 19 27 34 46 50 27
R17 | 1206 15 12 21 20 --- 9 | 55 63 55 55 --- 56
R18 | 699 33 13 28 24 --- 14 | 35 33 46 43 --- 32
R19 | 708 8 9 11 25 --- 8 | 44 44 49 54 --- 45
R20 | 1111 20 23 35 35 --- 16 | 25 29 35 35 --- 23
R21 | 2866 10 9 13 23 --- 8 | 42 49 50 34 --- 42
R23 | 1662 29 13 32 29 --- 14 | 55 62 57 72 --- 59
R24 | 1763 21 9 25 20 --- 10 | 186 181 185 196 --- 185
------+------------------------------------+--------------------------------
RMS | 1781 22 13 22 25 113 |T 48 51 54 54 76 48
WRMS | 1781 21 12 21 25 113 |NE 48 51 54 54 76 48
MEDI | 1166 18 12 20 23 105 |MD 35 33 39 38 76 32
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