[IGSREPORT-17269] Wk 1523 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 2 07:02:52 PDT 2009
******************************************************************************
IGS Electronic Report 02 Apr 07:03:15 PDT 2009 Message Number 17269
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1523 (Mar 15, 2009 - Mar 21, 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 2.1523.
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:
igl1523[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1523 in the SP3 format.
igl15237.sum Combination Report for GPS Week 1523.
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 | 240.3 ns
1 | 191.5 ns
2 | 234.4 ns
3 | 236.7 ns
4 | 239.0 ns
5 | 242.7 ns
6 | 240.7 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 1.1523, 1a.1523).
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 2.1523.0-6)
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 3.1523.0-6).
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 1523 summary. (Mar 15, 2009 - Mar 21, 2009)
Table 1.1523.a GPS week : 1523 MJD: 54905.0-54911.0
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 99| 5 0 4 -9 14 -75 -.14 28 26 | 0 800 3358 3582
| 1 1 2 36 36 87 .05 | 0 1083
cod 241| -4 0 -7 21 20 97 -.14 20 16 | --- --- --- ---
| 1 1 5 22 24 36 .04 | --- ---
esx 122| 0 0 -7 8 -36 78 .32 32 27 | 113729 -625 7003 12915
| 3 1 1 20 30 45 .09 | 19847 3675
iac n/a| 3 0 15 -31 15 -159 .11 33 33 | 233079 -1219 7003 12339
| 1 1 10 33 16 77 .10 | 19515 3921
mcc n/a| 5 -4 32 -67 -55 -562 .22 235 235 | --- --- --- ---
| 9 8 13 115 138 882 .18 | --- ---
Table 1.1523.b GPS week : 1523 MJD: 54905.0-54911.0
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 | 12 11 10 14 16 12 10 |
R03 | 12 10 13 10 12 12 13 |
R04 | 31 13 11 11 9 12 12 |
R06 | 19 18 24 22 15 19 15 |
R07 | 9 10 12 12 12 12 9 |
R08 | 6 9 10 16 11 14 13 |
R10 | 23 24 20 16 22 19 13 |
R11 | 11 11 9 9 11 13 12 |
R13 | 14 10 13 13 13 15 15 |
R14 | 17 13 21 21 15 15 11 |
R15 | 15 14 12 14 13 14 14 |
R17 | 22 24 24 20 14 18 17 |
R18 | 15 25 16 15 15 16 14 |
R19 | 14 17 15 17 15 16 16 |
R20 | 19 21 20 15 16 14 17 |
R21 | 18 19 16 14 13 13 15 |
R22 | 23 21 14 17 13 11 15 |
R23 | 29 23 17 24 30 24 27 |
R24 | 19 12 12 13 15 12 20 |
Table 1.1523.c GPS week : 1523 MJD: 54905.0-54911.0
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 1523 0 | 43 66 187 -1700 1928 -21540 104.2 >>>>> >>>>> | 240275 0
brd 1523 1 | -48 14 261 -1093 -599 -25190 89.3 4866 4866 | 191461 0
brd 1523 2 | 51 -64 269 -978 -335 -22940 100.1 >>>>> >>>>> | 234369 0
brd 1523 3 | 87 -64 233 2149 2263 -29050 89.7 >>>>> >>>>> | 236726 0
brd 1523 4 | 338 65 344 -3259 1559 -32630 110.0 >>>>> >>>>> | 238959 0
brd 1523 5 | 62 -92 132 -322 3592 -25460 101.4 >>>>> >>>>> | 242656 0
brd 1523 6 | -253 10 157 -2681 -2261 -27300 102.5 >>>>> >>>>> | 240708 0
-------------+------------------------------------------------------------+----------------
brd 1523 mean| 40 -9 226 -1126 877 -26301 99.6 >>>>> >>>>> | 232164 0
brd 1523 sdev| 175 64 73 1765 2014 3753 7.6 >>>>> >>>>> | 18154 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 2.1523.0 GPS week: 1523 Day: 0 MJD: 54905
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 99| 4 2 0 -12 13 -21 -.18 25 24 | 0 -648 3465 3613
cod 241| -2 -1 -14 8 -3 109 -.11 24 20 | --- --- --- ---
esx 122| -1 -1 -7 40 -49 34 .18 40 34 | 119297 -1792 5828 11551
iac n/a| 3 0 27 -11 43 -148 .19 40 40 | 245828 -6327 5801 10616
mcc n/a| 17 -6 15 -235 160 -1590 .26 305 305 | --- --- --- ---
Table 2.1523.1 GPS week: 1523 Day: 1 MJD: 54906
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 99| 1 -1 1 5 -23 -141 -.07 29 28 | 0 316 2677 2857
cod 241| -4 1 -11 0 44 80 -.21 23 18 | --- --- --- ---
esx 122| 4 1 -7 -13 11 155 .29 31 24 | 70149 3481 6813 13126
iac n/a| 2 -2 23 22 31 -132 .18 36 36 | 189699 -881 6835 11021
mcc n/a| 15 -8 38 -169 -39 -1014 .08 254 254 | --- --- --- ---
Table 2.1523.2 GPS week: 1523 Day: 2 MJD: 54907
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 99| 5 0 4 -6 -18 -64 -.17 28 25 | 0 1077 3138 3362
cod 241| -4 0 -10 6 62 24 -.15 19 17 | --- --- --- ---
esx 122| 1 0 -5 -14 -79 97 .26 30 26 | 117557 1779 7654 11895
iac n/a| 4 0 24 -20 9 -90 .17 35 35 | 237314 -379 7670 11198
mcc n/a| 7 -21 47 -20 -204 245 .37 149 149 | --- --- --- ---
Table 2.1523.3 GPS week: 1523 Day: 3 MJD: 54908
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 99| 6 0 3 -73 -7 94 -.09 29 28 | 0 1807 4022 4333
cod 241| -4 -1 -7 56 18 93 -.15 17 14 | --- --- --- ---
esx 122| 0 0 -4 25 -24 46 .34 32 27 | 119895 3730 6619 15801
iac n/a| 5 0 17 -61 8 -300 .13 34 34 | 233772 6476 6606 16563
mcc n/a| -9 -3 34 73 61 779 .33 131 131 | --- --- --- ---
Table 2.1523.4 GPS week: 1523 Day: 4 MJD: 54909
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 99| 5 -2 6 -31 29 -127 -.12 29 29 | 0 2539 4394 4728
cod 241| -4 1 -3 52 12 122 -.17 17 13 | --- --- --- ---
esx 122| -2 1 -5 11 -62 110 .31 31 24 | 116055 -2056 7478 12469
iac n/a| 5 0 7 -67 -1 -229 .13 33 33 | 242643 -3217 7478 12969
mcc n/a| -1 4 20 -144 -8 -1378 -.10 314 314 | --- --- --- ---
Table 2.1523.5 GPS week: 1523 Day: 5 MJD: 54910
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 99| 5 -1 8 11 82 -130 -.19 25 23 | 0 304 2760 2949
cod 241| -5 3 0 16 -2 130 -.10 20 18 | --- --- --- ---
esx 122| -4 1 -10 12 -22 75 .41 30 26 | 121826 -3790 6565 11137
iac n/a| 3 0 -1 -19 0 -108 -.05 29 29 | 241718 -2640 6580 10536
mcc n/a| 2 0 20 34 -163 -866 .43 201 201 | --- --- --- ---
Table 2.1523.6 GPS week: 1523 Day: 6 MJD: 54911
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 99| 7 -1 7 42 27 -134 -.17 29 26 | 0 205 3052 3236
cod 241| -4 1 -5 12 14 123 -.12 19 14 | --- --- --- ---
esx 122| -4 0 -8 -4 -29 31 .45 30 26 | 131324 -5728 8066 14431
iac n/a| 2 0 9 -62 16 -107 -.00 27 27 | 240581 -1565 8052 13473
mcc n/a| 7 -1 50 -10 -193 -114 .17 294 294 | --- --- --- ---
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 3.1523.0 GPS week: 1523 Day: 0 MJD: 54905
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 13 20 24 25 --- 11 | 29 48 33 41 --- 34
R03 |>>>>> 25 10 25 23 --- 12 | 24 41 44 45 --- 35
R04 |>>>>> 27 34 106 23 --- 30 | 37 46 102 35 --- 47
R06 |>>>>> 36 27 38 31 --- 19 | 95 98 107 98 --- 96
R07 |>>>>> 8 14 19 17 --- 8 | 32 38 23 25 --- 28
R08 |>>>>> 10 7 14 12 --- 6 | 41 36 31 25 --- 32
R10 | 1274 29 40 31 57 --- 23 | 30 42 37 34 --- 22
R11 |>>>>> 20 13 20 21 148 10 | 26 27 36 26 44 25
R13 |>>>>> 15 23 32 29 --- 14 | 28 30 40 38 --- 27
R14 | 2507 24 15 49 31 --- 17 | 30 27 35 44 --- 24
R15 |>>>>> 27 22 15 35 66 15 | 22 34 24 44 25 24
R17E |>>>>> 43 26 45 40 --- 22 | 48 72 69 85 --- 63
R18E |>>>>> 21 21 21 39 --- 14 | 56 59 69 71 --- 59
R19E |>>>>> 15 20 25 38 --- 14 | 43 28 41 37 --- 31
R20E |>>>>> 24 21 42 44 --- 18 | 46 39 68 62 --- 46
R21E |>>>>> 25 24 39 40 --- 18 | 40 39 62 64 --- 42
R22E |>>>>> 26 28 44 61 --- 22 | 45 40 66 72 --- 45
R23E |>>>>> 26 38 53 81 --- 28 | 75 67 89 94 --- 76
R24E |>>>>> 40 18 26 40 504 18 | 40 49 54 69 234 48
------+------------------------------------+--------------------------------
RMS |>>>>> 25 24 40 40 305 |T 41 45 54 53 101 42
WRMS |>>>>> 24 20 34 40 305 |NE 35 42 46 41 34 35
MEDI |>>>>> 25 21 31 35 148 |MD 40 40 44 44 44 35
Table 3.1523.1 GPS week: 1523 Day: 1 MJD: 54906
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1758 17 15 17 29 --- 11 | 29 42 48 18 --- 31
R03 | 1694 22 15 14 19 --- 10 | 22 37 51 36 --- 34
R04 | 1768 20 15 29 27 --- 13 | 23 33 58 37 --- 31
R06 | 5989 28 35 28 32 --- 18 | 81 76 91 87 --- 79
R07 | 7252 19 11 16 19 --- 9 | 21 35 33 30 --- 28
R08 | 2217 14 8 19 21 --- 9 | 36 28 25 34 --- 28
R10 | 1565 33 35 23 68 --- 24 | 25 51 39 31 --- 28
R11 | 1343 19 16 21 22 87 11 | 26 22 34 31 30 24
R13 | 1051 24 12 16 17 --- 10 | 24 29 27 19 --- 22
R14 | 927 20 15 27 24 --- 12 | 19 22 35 35 --- 20
R15 | 4655 25 24 23 24 75 14 | 21 36 50 32 19 30
R17E | 1365 48 26 40 50 --- 23 | 29 43 69 69 --- 44
R18E |11563 44 24 56 43 --- 24 | 31 48 93 76 --- 55
R19E | 3547 23 17 39 36 --- 17 | 26 25 48 29 --- 24
R20E | 1511 35 29 40 42 --- 20 | 37 54 52 40 --- 36
R21E | 2816 34 30 32 37 --- 19 | 41 37 65 48 --- 39
R22E | 4239 34 25 49 37 --- 21 | 39 37 63 56 --- 39
R23E | 4870 34 33 38 56 --- 23 | 52 53 67 55 --- 46
R24E |10924 23 17 15 24 424 11 | 43 42 51 43 124 42
------+------------------------------------+--------------------------------
RMS | 4865 29 23 31 36 254 |T 32 39 52 42 57 35
WRMS | 4865 28 18 24 36 254 |NE 29 37 44 35 24 32
MEDI | 2217 24 17 27 29 87 |MD 29 37 51 36 30 31
Table 3.1523.2 GPS week: 1523 Day: 2 MJD: 54907
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 13 18 19 19 --- 10 | 22 40 21 35 --- 27
R03 |>>>>> 27 18 21 22 --- 12 | 19 36 30 24 --- 24
R04 |>>>>> 17 6 27 21 --- 10 | 31 43 60 46 --- 40
R06 |>>>>> 57 34 38 34 --- 24 | 151 146 159 142 --- 146
R07 |>>>>> 20 14 29 23 --- 12 | 24 38 53 25 --- 31
R08 |>>>>> 20 11 18 22 --- 10 | 36 37 30 30 --- 31
R10 | 1480 23 21 51 42 --- 20 | 34 33 57 25 --- 23
R11 |>>>>> 13 12 13 20 81 8 | 25 30 35 28 25 27
R13 |>>>>> 30 15 18 23 --- 12 | 26 29 31 30 --- 23
R14 | 1438 35 22 26 60 --- 21 | 21 33 36 45 --- 27
R15 |>>>>> 22 11 25 26 99 12 | 25 30 44 36 23 26
R17E |>>>>> 30 32 40 63 --- 23 | 29 33 47 60 --- 29
R18E |>>>>> 17 20 30 43 --- 15 | 33 37 58 37 --- 35
R19E |>>>>> 28 17 26 34 --- 15 | 32 26 41 32 --- 26
R20E |>>>>> 36 21 39 43 --- 19 | 35 27 56 35 --- 29
R21E |>>>>> 27 15 35 34 --- 16 | 29 39 55 51 --- 36
R22E |>>>>> 14 16 32 34 --- 14 | 39 36 50 49 --- 35
R23E |>>>>> 33 18 33 36 --- 17 | 50 52 57 60 --- 49
R24E |>>>>> 25 16 21 16 223 11 | 45 48 59 50 179 47
------+------------------------------------+--------------------------------
RMS |>>>>> 28 19 30 35 149 |T 37 41 51 44 75 37
WRMS |>>>>> 25 17 26 35 149 |NE 37 45 50 42 24 38
MEDI |>>>>> 25 17 27 34 99 |MD 31 36 50 36 25 29
Table 3.1523.3 GPS week: 1523 Day: 3 MJD: 54908
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 31 15 18 34 --- 13 | 27 50 43 51 --- 39
R03 |>>>>> 23 7 19 17 --- 9 | 22 39 44 46 --- 36
R04 |>>>>> 17 15 21 22 --- 10 | 30 41 44 41 --- 35
R06 |>>>>> 49 20 48 36 --- 21 | 74 103 125 93 --- 96
R07 |>>>>> 28 10 28 17 --- 12 | 23 35 34 36 --- 29
R08 |>>>>> 23 20 36 30 --- 15 | 25 41 28 35 --- 27
R10 | 1402 39 17 27 26 --- 15 | 29 34 44 38 --- 26
R11 |>>>>> 14 9 11 28 110 9 | 27 32 30 46 51 30
R13 |>>>>> 30 20 22 19 --- 13 | 26 29 39 42 --- 25
R14 | 1298 42 15 33 59 --- 21 | 18 28 38 54 --- 25
R15 |>>>>> 22 17 14 39 100 13 | 25 33 40 41 39 31
R17E |>>>>> 38 23 41 41 --- 20 | 32 43 55 47 --- 35
R18E |>>>>> 22 16 29 35 --- 14 | 26 32 49 47 --- 28
R19E |>>>>> 37 14 24 44 --- 17 | 38 29 33 38 --- 28
R20E |>>>>> 24 16 31 37 --- 15 | 41 32 56 36 --- 34
R21E |>>>>> 15 16 29 37 --- 14 | 31 36 49 45 --- 36
R22E |>>>>> 19 20 33 44 --- 16 | 39 37 60 57 --- 40
R23E |>>>>> 32 30 65 35 --- 23 | 90 70 114 86 --- 81
R24E |>>>>> 16 16 36 23 172 13 | 38 44 77 48 342 48
------+------------------------------------+--------------------------------
RMS |>>>>> 29 17 32 34 131 |T 34 41 52 48 144 38
WRMS |>>>>> 28 14 27 34 131 |NE 29 42 46 47 45 36
MEDI |>>>>> 24 16 29 35 110 |MD 29 36 44 46 51 34
Table 3.1523.4 GPS week: 1523 Day: 4 MJD: 54909
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 32 14 13 48 --- 16 | 19 41 45 69 --- 38
R03 |>>>>> 26 13 14 30 --- 11 | 13 40 35 38 --- 30
R04 |>>>>> 20 12 15 17 --- 9 | 35 35 34 41 --- 34
R06 |>>>>> 32 19 32 19 --- 14 | 105 87 81 79 --- 84
R07 |>>>>> 29 10 24 22 --- 12 | 23 30 47 32 --- 26
R08 |>>>>> 29 8 22 18 --- 11 | 25 22 42 30 --- 24
R10 | 1685 61 19 37 38 --- 22 | 24 29 52 38 --- 23
R11 |>>>>> 22 7 25 24 79 11 | 20 19 37 29 63 17
R13 |>>>>> 26 10 27 28 --- 12 | 26 30 34 29 --- 22
R14 | 4618 25 12 19 48 --- 15 | 20 30 41 30 --- 24
R15 |>>>>> 33 13 26 17 72 12 | 16 30 52 32 77 27
R17E |>>>>> 26 18 25 32 --- 14 | 28 37 47 40 --- 31
R18E |>>>>> 15 19 35 30 --- 14 | 28 24 54 48 --- 29
R19E |>>>>> 21 20 32 33 --- 15 | 22 15 43 28 --- 19
R20E |>>>>> 19 20 29 42 --- 15 | 46 47 50 35 --- 39
R21E |>>>>> 20 14 22 37 --- 13 | 38 32 46 51 --- 36
R22E |>>>>> 20 15 21 38 --- 13 | 46 47 57 51 --- 46
R23E |>>>>> 44 37 80 49 --- 30 | 70 84 149 102 --- 91
R24E |>>>>> 26 20 35 25 533 15 | 37 38 62 44 354 40
------+------------------------------------+--------------------------------
RMS |>>>>> 29 17 31 33 314 |T 33 37 53 44 164 35
WRMS |>>>>> 29 13 24 33 314 |NE 29 35 45 40 70 31
MEDI |>>>>> 26 14 25 30 79 |MD 26 32 47 38 77 30
Table 3.1523.5 GPS week: 1523 Day: 5 MJD: 54910
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 26 18 18 20 --- 12 | 15 38 37 26 --- 26
R03 |>>>>> 19 18 27 18 --- 12 | 25 38 36 39 --- 29
R04 |>>>>> 13 21 21 28 --- 12 | 29 40 37 32 --- 30
R06 |>>>>> 42 29 18 38 --- 19 | 66 88 84 62 --- 71
R07 |>>>>> 14 14 28 29 --- 12 | 21 21 24 36 --- 19
R08 |>>>>> 34 18 18 20 --- 13 | 28 30 36 23 --- 19
R10 | 1204 18 17 49 43 --- 19 | 16 42 74 21 --- 29
R11 |>>>>> 24 15 24 24 69 12 | 34 30 44 19 23 28
R13 |>>>>> 23 15 34 29 --- 14 | 19 33 53 29 --- 26
R14 | 3742 21 20 38 20 --- 14 | 17 15 47 18 --- 15
R15 |>>>>> 32 21 21 15 57 13 | 22 26 35 22 29 21
R17E |>>>>> 27 21 40 37 --- 17 | 20 30 40 39 --- 24
R18E |>>>>> 19 22 33 35 --- 16 | 25 30 60 50 --- 33
R19E |>>>>> 25 24 34 26 --- 15 | 14 22 57 37 --- 22
R20E |>>>>> 15 18 31 32 --- 14 | 36 38 50 37 --- 35
R21E |>>>>> 16 13 21 34 --- 12 | 29 34 47 43 --- 32
R22E |>>>>> 17 12 26 18 --- 10 | 41 45 53 49 --- 44
R23E |>>>>> 41 38 40 43 --- 23 | 50 73 67 76 --- 61
R24E |>>>>> 12 19 23 25 336 11 | 49 46 63 50 165 48
------+------------------------------------+--------------------------------
RMS |>>>>> 24 20 30 29 201 |T 29 37 49 37 72 32
WRMS |>>>>> 23 18 26 29 201 |NE 26 36 46 29 26 28
MEDI |>>>>> 21 18 27 28 69 |MD 25 34 47 37 29 29
Table 3.1523.6 GPS week: 1523 Day: 6 MJD: 54911
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 15 14 23 15 --- 9 | 30 47 39 39 --- 37
R03 |>>>>> 27 17 29 12 --- 12 | 28 52 52 38 --- 41
R04 |>>>>> 12 14 23 28 --- 11 | 38 46 57 49 --- 44
R06 |>>>>> 30 15 21 35 --- 14 | 111 94 98 80 --- 93
R07 |>>>>> 21 10 9 17 --- 8 | 28 36 36 45 --- 35
R08 |>>>>> 18 16 18 31 --- 12 | 44 39 46 38 --- 36
R10 | 1084 20 13 32 23 --- 12 | 25 24 36 21 --- 16
R11 |>>>>> 21 15 21 24 80 11 | 19 26 38 22 30 22
R13 |>>>>> 36 7 40 17 --- 15 | 41 33 33 32 --- 31
R14 | 2851 26 9 24 17 --- 10 | 27 25 36 38 --- 26
R15 |>>>>> 18 22 26 31 49 14 | 26 46 37 45 41 34
R17E |>>>>> 33 23 29 30 --- 16 | 42 44 42 48 --- 39
R18E |>>>>> 19 19 31 29 --- 14 | 34 33 56 47 --- 36
R19E |>>>>> 26 21 39 23 --- 15 | 30 36 51 36 --- 32
R20E |>>>>> 36 21 36 28 --- 17 | 51 52 83 58 --- 56
R21E |>>>>> 32 22 30 23 --- 15 | 48 51 55 47 --- 47
R22E |>>>>> 35 15 29 24 --- 14 | 71 55 63 62 --- 58
R23E |>>>>> 63 31 49 48 --- 27 | 62 83 111 96 --- 79
R24E |>>>>> 30 32 39 37 502 20 | 49 77 70 61 220 62
------+------------------------------------+--------------------------------
RMS |>>>>> 29 19 30 27 294 |T 42 47 54 47 97 43
WRMS |>>>>> 26 14 26 27 294 |NE 37 42 46 40 35 37
MEDI |>>>>> 26 16 29 24 80 |MD 38 46 51 45 41 37
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