[IGSREPORT-17291] Wk 1524 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 9 05:00:09 PDT 2009
******************************************************************************
IGS Electronic Report 09 Apr 05:00:31 PDT 2009 Message Number 17291
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1524 (Mar 22, 2009 - Mar 28, 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 2.1524.
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:
igl1524[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1524 in the SP3 format.
igl15247.sum Combination Report for GPS Week 1524.
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 | 238.2 ns
1 | 235.0 ns
2 | 243.1 ns
3 | 237.4 ns
4 | 229.1 ns
5 | 231.5 ns
6 | 231.0 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 1.1524, 1a.1524).
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 2.1524.0-6)
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 3.1524.0-6).
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 1524 summary. (Mar 22, 2009 - Mar 28, 2009)
Table 1.1524.a GPS week : 1524 MJD: 54912.0-54918.0
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 98| 3 0 1 -5 -43 -5 -.19 29 26 | 0 -602 10158 12782
| 1 2 5 42 22 82 .04 | 0 4082
cod 237| -3 0 -4 20 25 47 -.13 18 15 | --- --- --- ---
| 1 1 2 29 24 35 .02 | --- ---
esx 122| -1 0 0 -21 2 35 .40 28 24 | 118013 102 6427 12643
| 2 2 4 38 39 56 .07 | 5701 6472
iac n/a| 3 0 6 -13 -21 -92 -.03 27 27 | 235423 27 6423 13182
| 1 1 5 30 29 48 .05 | 4185 3313
mcc n/a| 2 4 26 -57 -101 -25 .32 302 302 | --- --- --- ---
| 9 22 13 146 235 425 .52 | --- ---
Table 1.1524.b GPS week : 1524 MJD: 54912.0-54918.0
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 | 9 14 15 10 13 10 12 |
R03 | 14 13 10 10 11 13 11 |
R04 | 9 11 11 11 18 8 13 |
R06 | 16 25 27 23 18 18 18 |
R07 | 10 11 14 12 10 11 12 |
R08 | 15 9 9 9 11 10 11 |
R10 | 15 19 12 15 11 18 12 |
R11 | 8 15 8 8 12 12 15 |
R13 | 12 12 17 15 11 12 11 |
R14 | 9 14 11 14 15 10 10 |
R15 | 14 13 14 18 13 10 11 |
R17 | 29 29 17 13 12 12 13 |
R18 | 13 10 10 10 10 8 9 |
R19 | 12 14 9 14 14 10 10 |
R20 | 21 16 12 16 12 13 13 |
R21 | 19 18 14 12 13 15 16 |
R22 | 22 15 13 14 13 10 8 |
R23 | 21 27 24 22 23 25 25 |
R24 | 21 14 14 17 16 16 12 |
Table 1.1524.c GPS week : 1524 MJD: 54912.0-54918.0
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 1524 0 | -3 168 111 -1478 147 -27760 102.8 >>>>> >>>>> | 238236 0
brd 1524 1 | 251 -239 -2051 126300 1254 -19990 84.0 >>>>> >>>>> | 235014 0
brd 1524 2 | -64 -65 128 -699 -1596 -19880 88.9 3623 3623 | 243096 0
brd 1524 3 | -53 76 -27 -1279 -892 -12370 90.3 3074 3074 | 237430 0
brd 1524 4 | -85 30 -14 -182 -565 -9498 88.7 2871 2871 | 229082 0
brd 1524 5 | -15 -14 196 -1939 2916 -12190 89.6 2334 2334 | 231481 0
brd 1524 6 | -3 -88 262 174 2466 -10580 89.8 2704 2704 | 231014 0
-------------+------------------------------------------------------------+----------------
brd 1524 mean| 3 -18 -199 17271 532 -16038 90.6 >>>>> >>>>> | 235050 0
brd 1524 sdev| 113 130 823 48082 1725 6690 5.8 >>>>> >>>>> | 4919 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 2.1524.0 GPS week: 1524 Day: 0 MJD: 54912
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 98| 4 -5 8 -24 -1 64 -.22 30 27 | 0 1714 3932 4329
cod 237| -6 1 -4 13 6 52 -.12 22 15 | --- --- --- ---
esx 122| -1 1 -8 39 -41 5 .43 33 27 | 126339 88 6545 11814
iac n/a| 4 -1 6 -53 4 -167 .02 26 26 | 236902 2507 6533 12470
mcc n/a| 0 -8 29 -123 209 -29 -.29 359 359 | --- --- --- ---
Table 2.1524.1 GPS week: 1524 Day: 1 MJD: 54913
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 98| 4 -1 5 60 -76 43 -.15 40 37 | 0 -512 4099 4635
cod 237| -2 2 -3 -9 49 2 -.13 19 14 | --- --- --- ---
esx 122| -1 -2 6 -66 33 21 .41 28 25 | 119248 -7296 6002 13470
iac n/a| 4 -1 1 43 -75 -57 -.09 33 33 | 237082 -1813 6002 14460
mcc n/a| 5 7 11 -23 -36 -693 .26 336 336 | --- --- --- ---
Table 2.1524.2 GPS week: 1524 Day: 2 MJD: 54914
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 98| 3 1 3 -50 -51 -92 -.19 28 22 | 0 -4115 8995 11873
cod 237| -4 0 -6 17 31 101 -.16 20 18 | --- --- --- ---
esx 122| 0 1 0 23 -3 20 .35 22 19 | 112856 986 6678 12236
iac n/a| 0 1 4 -27 -33 -29 .00 31 31 | 240709 3332 6541 12872
mcc n/a| -1 -25 32 -137 -192 152 1.08 276 276 | --- --- --- ---
Table 2.1524.3 GPS week: 1524 Day: 3 MJD: 54915
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 98| 2 -1 0 28 -54 -115 -.21 30 29 | 0 -3229 7995 9237
cod 237| -1 0 -6 53 -14 57 -.16 19 16 | --- --- --- ---
esx 122| -2 1 1 -46 71 118 .44 24 23 | 122916 -2787 6595 15243
iac n/a| 2 0 9 -13 -10 -107 -.09 26 26 | 239323 -3341 6585 15454
mcc n/a| 13 20 21 201 -108 664 .44 293 293 | --- --- --- ---
Table 2.1524.4 GPS week: 1524 Day: 4 MJD: 54916
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 98| 1 1 -5 19 -43 -5 -.24 25 24 | 0 -224 10673 13313
cod 237| -3 1 -4 -18 28 75 -.13 16 15 | --- --- --- ---
esx 122| -5 -3 -3 -21 -13 45 .51 30 27 | 109816 11769 6122 15209
iac n/a| 2 1 14 -6 -35 -139 -.08 26 26 | 230020 3884 6256 15482
mcc n/a| 10 45 13 -91 161 169 .88 511 511 | --- --- --- ---
Table 2.1524.5 GPS week: 1524 Day: 5 MJD: 54917
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 98| 4 0 -3 -18 -32 108 -.19 26 23 | 0 6973 14889 18511
cod 237| -5 0 -3 29 22 24 -.12 16 13 | --- --- --- ---
esx 122| 0 0 0 -27 11 -53 .32 28 22 | 119160 -5963 6185 10195
iac n/a| 4 1 9 0 -3 -85 -.04 23 23 | 233356 -4355 6191 10503
mcc n/a| 3 -3 51 34 -433 -310 .11 163 163 | --- --- --- ---
Table 2.1524.6 GPS week: 1524 Day: 6 MJD: 54918
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 98| 2 0 0 -53 -41 -39 -.11 22 19 | 0 -4827 20527 27578
cod 237| -1 0 0 59 58 16 -.09 16 13 | --- --- --- ---
esx 122| 0 -4 3 -47 -37 90 .35 30 25 | 115762 3923 6866 10337
iac n/a| 3 0 -1 -36 5 -62 .04 26 26 | 230572 -23 6853 11039
mcc n/a| -15 -6 21 -259 -310 -135 -.23 180 180 | --- --- --- ---
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 3.1524.0 GPS week: 1524 Day: 0 MJD: 54912
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 19 10 15 17 --- 9 | 123 127 128 126 --- 126
R03 |>>>>> 26 11 38 16 --- 13 | 22 45 75 53 --- 45
R04 |>>>>> 19 12 18 11 --- 8 | 27 41 42 41 --- 36
R06 |>>>>> 28 20 39 23 --- 15 | 68 85 81 66 --- 74
R07 |>>>>> 12 19 22 15 --- 10 | 20 44 45 27 --- 31
R08 |>>>>> 27 12 27 34 --- 15 | 43 40 36 37 --- 32
R10 | 1857 16 27 16 35 --- 15 | 31 31 40 36 --- 30
R11 |>>>>> 14 7 15 17 115 7 | 30 33 36 38 106 32
R13 |>>>>> 17 13 34 17 --- 12 | 26 34 51 33 --- 32
R14 | 2858 15 17 17 14 --- 9 | 24 30 35 32 --- 25
R15 |>>>>> 15 26 29 23 39 14 | 24 33 46 31 56 27
R17E |>>>>> 50 39 71 37 --- 28 | 67 118 136 100 --- 97
R18E |>>>>> 20 19 23 23 --- 12 | 32 35 34 34 --- 28
R19E |>>>>> 17 18 24 24 --- 12 | 46 48 51 53 --- 46
R20E |>>>>> 51 24 42 25 --- 20 | 69 89 99 85 --- 84
R21E |>>>>> 41 26 36 27 --- 18 | 55 89 102 77 --- 76
R22E |>>>>> 48 30 34 37 --- 21 | 41 88 93 70 --- 68
R23E |>>>>> 38 35 32 36 --- 20 | 85 117 122 114 --- 107
R24E |>>>>> 44 22 41 40 610 21 | 48 69 79 48 577 56
------+------------------------------------+--------------------------------
RMS |>>>>> 30 22 33 26 359 |T 46 62 70 57 246 55
WRMS |>>>>> 27 15 27 26 359 |NE 39 49 55 47 81 44
MEDI |>>>>> 20 19 29 23 115 |MD 41 45 51 48 106 45
Table 3.1524.1 GPS week: 1524 Day: 1 MJD: 54913
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 35 17 11 36 --- 14 | 139 149 167 170 --- 154
R03 |>>>>> 21 10 23 36 --- 13 | 11 28 28 46 --- 22
R04 |>>>>> 19 17 18 24 --- 11 | 27 30 28 31 --- 25
R06 |>>>>> 55 33 49 40 --- 24 | 45 85 108 47 --- 71
R07 |>>>>> 20 17 18 21 --- 10 | 19 42 37 21 --- 30
R08 |>>>>> 16 8 19 19 --- 9 | 25 32 40 34 --- 32
R10 | 8371 36 15 26 52 --- 18 | 28 24 41 47 --- 27
R11 |>>>>> 15 9 37 38 100 15 | 38 41 38 55 99 38
R13 |>>>>> 12 18 18 30 --- 11 | 23 40 39 35 --- 33
R14 | 8052 23 23 29 13 --- 13 | 21 54 31 39 --- 36
R15 |>>>>> 28 11 23 31 65 13 | 34 36 54 46 60 39
R17 |>>>>> 85 34 45 38 --- 28 | 39 60 72 67 --- 50
R18 |>>>>> 20 11 22 15 --- 9 | 27 36 39 34 --- 31
R19 |>>>>> 34 16 23 30 --- 14 | 45 41 52 53 --- 40
R20 |>>>>> 36 13 36 27 --- 15 | 76 95 123 105 --- 96
R21 |>>>>> 52 11 31 33 --- 18 | 45 46 52 52 --- 39
R22 |>>>>> 40 18 21 31 --- 15 | 28 44 51 46 --- 38
R23 |>>>>> 81 30 33 42 --- 26 | 55 92 114 101 --- 90
R24 |>>>>> 27 16 22 36 569 14 | 27 31 44 39 389 23
------+------------------------------------+--------------------------------
RMS |>>>>> 40 19 28 33 336 |T 39 52 60 56 182 48
WRMS |>>>>> 37 14 25 33 336 |NE 37 51 55 51 79 46
MEDI |>>>>> 28 16 23 31 100 |MD 28 41 44 46 99 38
Table 3.1524.2 GPS week: 1524 Day: 2 MJD: 54914
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1578 40 15 26 15 --- 15 | 74 103 113 96 --- 95
R03 | 2318 12 13 8 32 --- 10 | 29 33 38 42 --- 31
R04 | 3106 18 11 21 24 --- 10 | 20 38 45 36 --- 33
R06 |11247 65 36 29 53 --- 26 | 64 73 85 49 --- 57
R07 | 2379 21 17 22 37 --- 14 | 25 43 38 53 --- 34
R08 | 823 14 14 12 18 --- 8 | 22 38 34 31 --- 29
R10 | 2935 13 13 26 24 --- 11 | 22 32 37 45 --- 28
R11 | 756 9 11 16 20 105 8 | 33 30 26 41 52 28
R13 | 2632 31 22 27 39 --- 17 | 18 24 48 32 --- 27
R14 | 2775 14 16 23 18 --- 10 | 26 41 42 39 --- 34
R15 | 2984 18 30 13 33 83 14 | 23 24 39 30 37 27
R17 | 1199 45 21 20 24 --- 16 | 57 75 84 79 --- 71
R18 | 2350 18 13 17 21 --- 9 | 17 27 38 37 --- 27
R19 | 2245 15 14 14 17 --- 8 | 36 36 33 46 --- 35
R20 | 1482 22 21 19 21 --- 12 | 49 51 64 56 --- 53
R21 | 1636 19 26 24 25 --- 14 | 61 70 79 78 --- 69
R22 | 1506 16 12 21 36 --- 12 | 29 34 20 53 --- 28
R23 | 3107 49 29 32 56 --- 23 | 86 81 87 114 --- 87
R24 | 6127 21 19 25 30 459 13 | 27 31 40 28 323 27
------+------------------------------------+--------------------------------
RMS | 3623 28 20 22 31 276 |T 37 46 52 51 137 43
WRMS | 3623 22 18 19 31 276 |NE 32 43 49 44 44 38
MEDI | 2350 18 16 21 24 105 |MD 29 38 40 45 52 33
Table 3.1524.3 GPS week: 1524 Day: 3 MJD: 54915
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1384 20 13 15 17 --- 9 | 124 131 135 142 --- 132
R03 | 3364 18 10 19 24 --- 10 | 24 42 45 27 --- 33
R04 | 2023 25 12 13 21 --- 10 | 46 48 51 70 --- 51
R06 | 7796 49 33 40 34 --- 22 | 50 89 90 38 --- 63
R07 | 3259 23 17 27 15 --- 12 | 20 31 37 19 --- 22
R08 | 1079 19 13 16 15 --- 9 | 32 51 49 40 --- 42
R10 | 2118 20 17 37 26 --- 15 | 29 36 46 38 --- 27
R11 | 1394 14 9 15 13 178 7 | 35 37 44 47 82 38
R13 | 1535 24 15 17 41 --- 14 | 33 42 38 51 --- 39
R14 | 2630 33 12 30 20 --- 14 | 16 32 42 39 --- 28
R15 | 1602 15 37 15 41 89 17 | 31 39 56 43 69 38
R17 | 1821 29 23 17 19 --- 13 | 39 54 62 62 --- 53
R18 | 2258 19 14 16 19 --- 9 | 25 40 51 41 --- 37
R19 | 2900 37 13 26 15 --- 13 | 26 29 44 32 --- 28
R20 | 1191 41 16 31 17 --- 15 | 42 58 75 69 --- 59
R21 | 2993 23 15 20 22 --- 11 | 38 46 59 52 --- 46
R22 | 2143 30 14 33 20 --- 14 | 30 35 72 46 --- 43
R23 | 2621 53 22 22 52 --- 22 | 45 63 54 96 --- 59
R24 | 5715 33 26 27 29 467 16 | 56 67 64 75 263 61
------+------------------------------------+--------------------------------
RMS | 3073 30 19 24 26 293 |T 39 51 58 54 138 47
WRMS | 3073 29 16 23 26 293 |NE 40 52 57 50 75 46
MEDI | 2143 24 15 20 20 178 |MD 33 42 51 46 82 42
Table 3.1524.4 GPS week: 1524 Day: 4 MJD: 54916
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3818 20 15 34 22 --- 13 | 43 69 69 62 --- 60
R03 | 1360 10 17 29 20 --- 11 | 38 50 32 47 --- 41
R04 | 1411 35 22 39 28 --- 17 | 31 51 78 49 --- 47
R06 | 6566 21 20 49 31 --- 17 | 66 66 94 61 --- 65
R07 | 1720 22 8 26 12 --- 9 | 27 38 61 28 --- 36
R08 | 863 24 9 26 17 --- 11 | 30 44 65 53 --- 45
R10 | 1042 23 11 27 17 --- 11 | 23 32 54 40 --- 33
R11 | 1642 19 16 24 22 273 11 | 37 41 50 33 83 34
R13 | 938 19 15 20 21 --- 10 | 29 34 46 30 --- 31
R14 | 2238 22 11 36 33 --- 14 | 48 41 38 54 --- 39
R15 | 2251 27 20 18 19 80 12 | 19 45 43 50 54 37
R17 | 1813 9 18 23 28 --- 11 | 42 53 55 71 --- 52
R18 | 1161 14 10 20 22 --- 9 | 15 27 36 33 --- 23
R19 | 1681 34 20 21 18 --- 14 | 23 39 44 36 --- 30
R20 | 1259 21 14 31 19 --- 12 | 40 42 66 39 --- 42
R21 | 3561 26 16 20 24 --- 12 | 75 75 69 68 --- 70
R22 | 2473 28 8 30 22 --- 12 | 33 38 52 53 --- 38
R23 | 2219 41 25 44 53 --- 23 | 62 61 68 94 --- 62
R24M | 6621 32 19 28 31 838 15 | 41 67 76 43 502 52
------+------------------------------------+--------------------------------
RMS | 2871 25 16 30 26 511 |T 38 48 57 49 213 44
WRMS | 2871 24 15 27 26 511 |NE 35 46 57 46 68 42
MEDI | 1720 22 16 27 22 273 |MD 37 44 55 49 83 41
Table 3.1524.5 GPS week: 1524 Day: 5 MJD: 54917
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2899 17 11 19 20 --- 9 | 94 96 79 103 --- 93
R03 | 1877 25 24 21 18 --- 13 | 27 52 39 34 --- 36
R04 | 2622 8 10 20 16 --- 8 | 34 39 37 41 --- 36
R06 | 4561 48 19 28 28 --- 18 | 65 65 65 51 --- 55
R07 | 2625 30 10 16 21 --- 11 | 30 30 38 35 --- 30
R08 | 924 21 15 13 16 --- 9 | 23 41 43 37 --- 35
R10 | 972 22 18 54 21 --- 17 | 31 32 58 29 --- 26
R11 | 726 31 6 27 19 148 12 | 40 35 45 40 101 34
R13 | 1521 25 14 26 15 --- 11 | 30 34 36 34 --- 28
R14 | 2001 18 13 12 25 --- 10 | 31 33 32 33 --- 29
R15 | 946 13 12 24 21 140 10 | 37 33 55 52 113 40
R17 | 1488 16 10 28 26 --- 11 | 43 46 54 65 --- 48
R18 | 1008 10 10 14 17 --- 7 | 23 28 22 33 --- 25
R19 | 418 18 10 24 20 --- 10 | 18 30 56 32 --- 31
R20 | 960 29 22 18 20 --- 13 | 36 55 53 43 --- 44
R21 | 3699 28 17 26 33 --- 14 | 43 43 63 57 --- 47
R22 | 2487 21 16 12 18 --- 10 | 41 52 58 56 --- 50
R23 | 1673 39 29 65 37 --- 24 | 75 64 107 83 --- 73
R24 | 4520 32 14 31 33 194 15 | 66 83 95 87 373 79
------+------------------------------------+--------------------------------
RMS | 2333 26 16 28 23 162 |T 41 46 54 49 195 44
WRMS | 2333 23 13 22 23 162 |NE 40 44 47 44 107 40
MEDI | 1673 22 14 24 20 148 |MD 36 41 54 41 113 36
Table 3.1524.6 GPS week: 1524 Day: 6 MJD: 54918
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1277 13 12 36 21 --- 12 | 75 74 94 77 --- 78
R03 | 2715 20 16 24 15 --- 10 | 38 56 53 53 --- 49
R04 | 2923 13 19 30 26 --- 12 | 33 47 40 46 --- 39
R06 | 5449 32 16 37 42 --- 18 | 53 68 82 82 --- 64
R07 | 3321 21 14 25 21 --- 11 | 23 40 46 27 --- 31
R08 | 795 22 15 21 21 --- 11 | 25 34 33 38 --- 29
R10 | 680 15 11 33 22 --- 11 | 24 35 55 34 --- 31
R11 | 708 12 23 34 30 95 14 | 30 34 64 36 69 36
R13 | 1467 24 10 26 20 --- 11 | 39 35 39 33 --- 34
R14 | 1628 15 14 17 24 --- 10 | 39 46 39 40 --- 39
R15 | 1387 17 12 23 26 57 11 | 25 34 43 43 52 33
R17 | 1356 23 11 31 25 --- 12 | 40 50 54 73 --- 49
R18 | 1183 8 11 25 19 --- 9 | 21 33 32 35 --- 27
R19 | 500 14 12 20 26 --- 10 | 19 38 47 43 --- 33
R20 | 807 24 14 31 24 --- 13 | 51 56 62 58 --- 53
R21 | 2330 29 12 17 44 --- 15 | 52 47 55 60 --- 50
R22 | 2454 19 8 15 16 --- 8 | 30 40 48 48 --- 39
R23 | 1290 44 36 63 33 --- 25 | 84 75 119 104 --- 84
R24 | 7418 22 15 27 18 293 11 | 55 65 64 54 235 57
------+------------------------------------+--------------------------------
RMS | 2703 22 16 30 26 180 |T 39 47 56 51 118 45
WRMS | 2703 19 13 25 26 180 |NE 36 45 53 46 60 42
MEDI | 1387 20 14 26 24 95 |MD 38 46 53 46 69 39
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