[IGSREPORT-17876] Wk 1550 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Oct 8 05:01:37 PDT 2009
******************************************************************************
IGS Electronic Report 08 Oct 05:01:39 PDT 2009 Message Number 17876
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1550 (Sep 20, 2009 - Sep 26, 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 2.1550.
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:
igl1550[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1550 in the SP3 format.
igl15507.sum Combination Report for GPS Week 1550.
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 | 248.6 ns
1 | 243.9 ns
2 | 241.7 ns
3 | 241.8 ns
4 | 249.5 ns
5 | 154.5 ns
6 | 152.3 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
----+--------+---------------
5 | ESX | R03
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 1.1550, 1a.1550).
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 2.1550.0-6)
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 3.1550.0-6).
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 1550 summary. (Sep 20, 2009 - Sep 26, 2009)
Table 1.1550.a GPS week : 1550 MJD: 55094.0-55100.0
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| 0 0 0 -38 -2 -125 -.15 32 22 | 0 627 3646 4081
| 0 2 2 42 19 105 .03 | 0 2552
cod 225| 0 0 1 38 -18 93 -.10 18 14 | --- --- --- ---
| 1 0 1 22 19 51 .03 | --- ---
esx 137| 1 1 5 -17 44 41 .45 41 25 | 114707 -927 7001 13041
| 1 1 3 49 38 77 .04 | 48542 2807
iac n/a| -1 1 -6 -4 -10 -56 -.15 24 24 | 125557 -3117 45942 153904
| 2 2 3 38 28 63 .04 | 276506 6369
mcc n/a| 0 -1 50 4 -51 463 -.02 157 157 | --- --- --- ---
| 8 8 17 101 117 494 .48 | --- ---
Table 1.1550.b GPS week : 1550 MJD: 55094.0-55100.0
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 | 10 14 13 13 12 11 9 |
R03 | 13 13 7 12 12 18 25 |
R07 | 10 10 10 11 11 10 9 |
R08 | 10 10 11 9 15 10 10 |
R10 | 14 14 9 11 15 10 13 |
R11 | 13 13 14 14 16 13 11 |
R13 | 7 11 13 11 11 10 11 |
R14 | 11 11 10 12 13 10 10 |
R15 | 10 10 12 10 10 14 11 |
R17 | 13 12 12 9 11 12 11 |
R18 | 16 10 9 14 10 10 11 |
R19 | 13 12 10 8 7 13 9 |
R20 | 15 11 7 9 11 10 17 |
R21 | 20 9 9 8 9 9 11 |
R23 | 17 16 17 16 12 18 15 |
R24 | 23 38 48 33 19 46 44 |
Table 1.1550.c GPS week : 1550 MJD: 55094.0-55100.0
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 1550 0 | 48 -62 280 133 626 -2796 89.5 3841 3841 | 248639 0
brd 1550 1 |14420 -7649 -154 -27450 -42950 91220 94.9 >>>>> >>>>> | 243918 0
brd 1550 2 | -84 12 156 -72 3555 -11670 91.1 4725 4725 | 241711 0
brd 1550 3 | 130 -105 117 1938 544 -16219 87.7 4937 4937 | 241819 0
brd 1550 4 | 198 -3 378 236 882 -16020 89.8 4549 4549 | 249489 0
brd 1550 5 | 39 -4 269 -1293 823 -13270 91.0 3801 3801 | 154462 0
brd 1550 6 | -389 602 523 -9335 -5373 -7448 93.9 12650 12650 | 152290 0
-------------+------------------------------------------------------------+----------------
brd 1550 mean| 2052 -1029 224 -5120 -5984 3399 91.1 >>>>> >>>>> | 218904 0
brd 1550 sdev| 5457 2928 215 10508 16521 39020 2.5 >>>>> >>>>> | 44871 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 2.1550.0 GPS week: 1550 Day: 0 MJD: 55094
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 -1 4 -54 -13 -158 -.13 28 23 | 0 -388 2919 3268
cod 225| 0 0 0 60 -43 68 -.11 16 15 | --- --- --- ---
esx 137| 3 0 0 -13 95 106 .43 29 24 | 150464 -3719 5262 12127
iac n/a| -4 1 -6 -23 5 -37 -.14 25 25 | 248030 -2845 5270 11246
mcc n/a| 0 -16 56 76 59 -169 .31 263 263 | --- --- --- ---
Table 2.1550.1 GPS week: 1550 Day: 1 MJD: 55095
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 1 -84 24 -304 -.14 28 16 | 0 -979 3580 3919
cod 225| -1 0 2 59 0 185 -.12 21 16 | --- --- --- ---
esx 137| 4 2 7 -59 -10 129 .53 32 26 | 145598 -89 6548 9322
iac n/a| 0 0 -9 56 -23 22 -.14 22 22 | 243681 -1580 6566 8990
mcc n/a| 16 4 72 -6 54 1072 .30 167 167 | --- --- --- ---
Table 2.1550.2 GPS week: 1550 Day: 2 MJD: 55096
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 1 -93 -15 -201 -.20 42 25 | 0 -198 2836 3272
cod 225| 0 -1 1 54 -23 89 -.11 19 13 | --- --- --- ---
esx 137| -1 2 8 -36 83 -8 .43 30 19 | 135601 2318 5298 11018
iac n/a| 0 0 -8 3 -35 12 -.17 25 25 | 241275 586 5306 10820
mcc n/a| 2 10 55 162 -80 1174 -.97 187 187 | --- --- --- ---
Table 2.1550.3 GPS week: 1550 Day: 3 MJD: 55097
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 -3 -4 -23 -3 1 -.12 32 23 | 0 391 3743 4099
cod 225| 2 0 0 23 0 110 -.13 15 12 | --- --- --- ---
esx 137| 1 4 2 55 4 -99 .47 28 22 | 138644 -2282 5709 9943
iac n/a| -3 1 0 -21 10 -108 -.20 22 22 | 244329 -4047 5754 9938
mcc n/a| -5 0 25 54 15 220 .01 119 119 | --- --- --- ---
Table 2.1550.4 GPS week: 1550 Day: 4 MJD: 55098
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 -1 0 -12 22 -55 -.13 24 23 | 0 313 3318 3634
cod 225| -2 0 1 37 -42 80 -.12 15 12 | --- --- --- ---
esx 137| 0 0 7 -31 42 49 .40 24 23 | 144566 -2039 8144 19259
iac n/a| 0 -2 -6 -27 35 -112 -.07 23 23 | 248313 -2989 8116 19080
mcc n/a| -1 1 27 -139 -46 439 .45 110 110 | --- --- --- ---
Table 2.1550.5 GPS week: 1550 Day: 5 MJD: 55099
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 2 -2 28 -9 -43 -.16 30 19 | 0 -1026 3367 3676
cod 225| 0 0 3 0 1 108 -.10 22 14 | --- --- --- ---
esx 137| 0 0 5 -75 41 33 .42 113 38 | 41141 3161 13221 18323
iac n/a| 0 2 -8 33 -23 -137 -.12 28 28 | 149525 4902 9264 17261
mcc n/a| -6 -1 49 -48 -77 402 -.19 120 120 | --- --- --- ---
Table 2.1550.6 GPS week: 1550 Day: 6 MJD: 55100
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 3 1 -27 -25 -112 -.20 40 23 | 0 6277 5762 6705
cod 225| 0 -1 1 33 -22 14 -.05 19 12 | --- --- --- ---
esx 137| 1 1 7 42 55 80 .44 28 21 | 46938 -3839 4827 11299
iac n/a| 1 5 -9 -56 -43 -31 -.19 25 25 | -496248 -15847 281323 999999
mcc n/a| -9 -7 65 -70 -282 102 -.02 131 131 | --- --- --- ---
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 3.1550.0 GPS week: 1550 Day: 0 MJD: 55094
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1269 10 14 12 27 --- 9 | 24 30 29 31 --- 23
R03 |13879 28 16 23 24 --- 13 | 31 32 48 26 --- 28
R07 | 3918 22 17 18 12 --- 10 | 27 40 39 32 --- 34
R08 | 619 18 11 27 11 115 9 | 25 33 51 34 29 33
R10 | 2159 33 16 26 26 --- 14 | 42 42 39 46 --- 38
R11 | 1162 31 13 28 22 127 13 | 35 46 56 39 32 42
R13 | 1061 8 11 13 15 --- 7 | 26 26 31 24 --- 24
R14 | 1235 16 13 27 19 --- 11 | 32 23 41 29 --- 27
R15 | 1282 16 12 14 24 68 9 | 27 32 33 37 29 29
R17 | 931 29 20 19 25 --- 13 | 50 61 52 57 --- 53
R18 | 887 16 10 47 27 --- 15 | 25 20 46 29 --- 20
R19 | 813 20 13 26 29 --- 12 | 41 33 29 58 --- 36
R20 | 2635 24 21 30 27 --- 14 | 36 42 74 51 --- 46
R21 | 1184 41 27 35 33 --- 19 | 49 37 29 37 --- 30
R23 | 1832 43 18 27 32 493 17 | 106 110 122 145 177 118
R24 | 1325 53 20 52 36 --- 23 | 510 492 492 508 --- 499
------+------------------------------------+--------------------------------
RMS | 3841 28 16 29 25 263 |T 67 68 75 73 66 67
WRMS | 3841 23 15 24 25 263 |NE 67 68 75 73 66 67
MEDI | 1235 22 14 26 25 115 |MD 32 33 41 37 29 33
Table 3.1550.1 GPS week: 1550 Day: 1 MJD: 55095
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 10 28 24 26 --- 13 | 19 24 27 32 --- 15
R03 |>>>>> 14 23 35 16 --- 13 | 34 32 58 18 --- 22
R07 |>>>>> 21 16 11 17 --- 10 | 25 36 43 34 --- 30
R08 |>>>>> 18 11 19 17 83 9 | 21 28 27 27 26 21
R10 | ---- 22 15 30 29 --- 14 | 30 38 52 31 --- 34
R11 |>>>>> 23 16 29 22 116 13 | 27 35 43 30 35 28
R13 |>>>>> 17 13 30 15 --- 11 | 24 28 33 21 --- 19
R14 |>>>>> 15 13 29 19 --- 11 | 31 29 47 34 --- 31
R15 |>>>>> 9 20 14 22 109 10 | 34 36 32 31 22 30
R17 |>>>>> 15 20 31 12 --- 11 | 45 48 56 46 --- 44
R18 |>>>>> 7 12 26 18 --- 9 | 28 22 36 21 --- 19
R19 |>>>>> 17 16 33 12 --- 11 | 27 31 41 30 --- 24
R20 |>>>>> 9 19 22 20 --- 10 | 26 27 46 26 --- 25
R21 |>>>>> 12 15 19 17 --- 9 | 38 26 20 24 --- 20
R23 |>>>>> 32 18 22 33 282 15 | 60 70 85 101 166 76
R24 |>>>>> 89 51 77 38 --- 38 | 510 531 540 505 --- 514
------+------------------------------------+--------------------------------
RMS |>>>>> 28 21 32 22 167 |T 61 65 74 63 62 59
WRMS |>>>>> 16 16 26 22 167 |NE 61 65 74 63 62 59
MEDI |>>>>> 15 16 26 18 109 |MD 28 31 43 30 26 25
Table 3.1550.2 GPS week: 1550 Day: 2 MJD: 55096
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1712 40 18 14 18 --- 13 | 21 35 43 34 --- 30
R03 |10028 17 11 12 11 --- 7 | 31 33 40 16 --- 25
R07 | 3069 23 17 18 13 --- 10 | 32 42 52 44 --- 40
R08 | 977 32 9 19 13 77 10 | 19 30 40 30 31 27
R10 | 2000 27 9 14 14 --- 9 | 30 26 39 30 --- 28
R11 | 749 29 17 28 24 92 14 | 35 45 52 34 54 38
R13 | 2371 31 14 28 16 --- 12 | 23 34 55 26 --- 31
R14 | 2583 24 9 20 18 --- 10 | 26 31 41 23 --- 26
R15 | 2645 29 18 17 19 124 11 | 25 33 30 30 33 24
R17 | 1959 23 11 27 18 --- 11 | 42 46 63 59 --- 50
R18 | 1919 13 15 12 19 --- 9 | 37 35 30 30 --- 29
R19 | 2410 19 16 15 16 --- 9 | 41 35 40 44 --- 36
R20 | 2070 11 12 8 16 --- 7 | 21 23 26 27 --- 20
R21 | 581 18 10 18 15 --- 8 | 23 18 33 27 --- 20
R23 |14087 32 23 32 34 331 17 | 65 64 88 106 214 80
R24 | 1739 138 53 90 68 --- 48 | 431 531 575 509 --- 513
------+------------------------------------+--------------------------------
RMS | 4724 42 19 30 25 187 |T 56 66 77 66 83 63
WRMS | 4724 25 13 19 25 187 |NE 56 66 77 66 83 63
MEDI | 2000 24 14 18 16 92 |MD 30 34 40 30 33 29
Table 3.1550.3 GPS week: 1550 Day: 3 MJD: 55097
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2991 29 23 23 9 --- 12 | 17 38 31 34 --- 26
R03 |15123 32 12 19 23 --- 12 | 20 43 67 48 --- 37
R07 | 3697 16 20 17 17 --- 10 | 40 63 49 47 --- 51
R08 | 1126 10 13 23 17 63 9 | 20 27 42 33 56 26
R10 | 2367 17 12 20 23 --- 10 | 48 45 50 40 --- 43
R11 | 1416 35 14 37 15 134 14 | 42 40 71 50 73 46
R13 | 2067 34 10 13 18 --- 11 | 29 35 34 26 --- 29
R14 | 4950 30 14 20 17 --- 11 | 34 35 35 35 --- 33
R15 | 2891 16 8 21 22 72 9 | 33 25 30 25 42 22
R17 | 1676 18 8 13 23 --- 9 | 44 55 56 57 --- 52
R18 | 8362 22 16 36 21 --- 13 | 36 36 33 34 --- 27
R19 | 766 11 10 17 17 --- 8 | 23 22 34 34 --- 25
R20 | 2839 19 6 22 18 --- 9 | 27 28 47 25 --- 28
R21 | 729 9 9 18 19 --- 8 | 32 33 33 32 --- 30
R23 | 1460 31 17 31 35 172 16 | 67 76 101 106 224 85
R24 | 2939 93 25 71 43 --- 32 | 426 490 526 491 --- 485
------+------------------------------------+--------------------------------
RMS | 4937 32 15 28 22 119 |T 58 68 77 69 98 65
WRMS | 4937 23 12 22 22 119 |NE 58 68 77 69 98 65
MEDI | 2367 19 12 20 18 72 |MD 33 36 42 34 56 30
Table 3.1550.4 GPS week: 1550 Day: 4 MJD: 55098
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3707 26 13 22 21 --- 11 | 13 20 37 30 --- 18
R03 |14247 29 14 17 25 --- 12 | 21 36 63 44 --- 33
R07 | 6061 26 9 21 22 --- 11 | 22 42 56 48 --- 40
R08 | 970 19 26 24 27 86 14 | 42 34 51 51 28 36
R10 | 3791 23 24 29 26 --- 14 | 36 27 46 47 --- 32
R11 | 2393 36 16 36 21 137 15 | 47 36 63 36 44 39
R13 | 3105 27 10 21 21 --- 11 | 23 30 38 24 --- 25
R14 | 3824 32 10 25 24 --- 13 | 19 26 35 20 --- 20
R15 | 4055 16 9 20 26 94 10 | 20 22 30 39 33 23
R17 | 1041 18 9 21 27 --- 10 | 32 38 50 56 --- 41
R18 | 1973 19 10 20 19 --- 9 | 21 33 46 35 --- 31
R19 | 1038 11 9 14 16 --- 7 | 32 29 26 33 --- 27
R20 | 1875 20 17 18 17 --- 10 | 33 31 50 37 --- 34
R21 | 1257 10 11 25 15 --- 9 | 15 21 42 23 --- 21
R23 | 1025 15 13 31 25 117 12 | 66 59 70 74 140 64
R24 | 1913 38 23 36 35 --- 18 | 482 460 440 466 --- 460
------+------------------------------------+--------------------------------
RMS | 4549 24 15 24 23 110 |T 57 59 71 66 61 59
WRMS | 4549 23 12 23 23 110 |NE 57 59 71 66 61 59
MEDI | 1973 20 11 21 22 94 |MD 23 31 46 37 33 32
Table 3.1550.5 GPS week: 1550 Day: 5 MJD: 55099
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2856 15 13 19 28 --- 11 | 17 28 26 44 --- 24
R03 | 8538 30 23 437 20 --- 17 | 19 31 232 20 --- 18
R07 | 9630 15 16 20 17 --- 9 | 19 25 33 22 --- 21
R08 | 778 12 20 21 14 87 10 | 26 27 42 21 19 24
R10 | 3805 19 12 21 17 --- 10 | 31 28 30 37 --- 28
R11 | 1856 20 15 35 18 156 13 | 34 34 63 38 22 36
R13 | 4143 16 9 27 15 --- 10 | 30 27 37 23 --- 24
R14 | 1623 20 15 10 18 --- 9 | 25 17 38 28 --- 25
R15 | 2221 29 17 24 28 91 14 | 31 27 31 36 29 25
R17 | 856 19 10 21 27 --- 11 | 40 44 36 58 --- 43
R18 | 1677 10 16 19 19 --- 9 | 18 25 23 23 --- 17
R19 | 798 21 14 26 28 --- 13 | 18 21 40 42 --- 25
R20 | 1527 13 14 22 20 --- 10 | 36 25 40 27 --- 25
R21 | 1833 18 9 16 16 --- 8 | 27 15 18 24 --- 17
R23 | 1194 23 18 51 27 131 17 | 69 63 85 73 120 67
R24 | 1673 96 69 81 73 --- 46 | 333 438 444 369 --- 394
------+------------------------------------+--------------------------------
RMS | 3801 30 22 113 28 120 |T 48 54 76 55 47 50
WRMS | 3801 19 14 38 28 120 |NE 48 54 76 55 47 50
MEDI | 1677 19 15 21 19 91 |MD 27 27 37 28 22 25
Table 3.1550.6 GPS week: 1550 Day: 6 MJD: 55100
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 9833 13 7 16 22 --- 8 | 39 36 32 45 --- 35
XR03 |11000 50 23 --- 37 --- 25 | 22 47 --- 52 --- 37
R07 |17040 14 11 20 14 --- 8 | 27 41 50 47 --- 39
R08 |17379 18 10 9 28 101 10 | 41 37 45 34 29 35
R10 |13340 20 17 34 20 --- 13 | 41 38 41 47 --- 39
R11 |13424 30 14 17 17 169 11 | 49 48 54 45 45 46
R13 | 8579 18 7 24 26 --- 11 | 29 26 44 24 --- 27
R14 | 8013 13 15 21 20 --- 10 | 27 27 38 32 --- 28
R15 |14216 30 9 13 25 76 11 | 37 33 40 38 37 33
R17 |10336 19 10 26 21 --- 11 | 58 55 50 66 --- 55
R18 |12286 17 11 27 21 --- 11 | 29 27 40 37 --- 29
R19 |13591 16 12 16 21 --- 9 | 31 34 32 40 --- 32
R20 |14280 35 16 45 21 --- 17 | 21 19 53 30 --- 24
R21 |13222 25 13 19 21 --- 11 | 21 20 31 35 --- 23
R23 | 8459 31 23 28 23 154 14 | 86 82 100 99 135 88
R24 |11004 131 55 60 57 --- 43 | 351 375 375 359 --- 363
------+------------------------------------+--------------------------------
RMS |12652 40 19 28 25 131 |T 56 59 68 64 61 58
WRMS |12652 23 12 21 25 131 |NE 56 59 68 64 61 58
MEDI |12286 19 12 21 21 101 |MD 31 36 44 40 37 35
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