[IGSREPORT-17313] Wk 1525 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Apr 16 05:54:44 PDT 2009
******************************************************************************
IGS Electronic Report 16 Apr 05:55:06 PDT 2009 Message Number 17313
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1525 (Mar 29, 2009 - Apr 04, 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 2.1525.
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:
igl1525[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1525 in the SP3 format.
igl15257.sum Combination Report for GPS Week 1525.
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 | 220.4 ns
1 | 219.0 ns
2 | 167.9 ns
3 | 211.6 ns
4 | 206.8 ns
5 | 200.2 ns
6 | 153.5 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
----+--------+---------------
2 | BKG | R24
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 1.1525, 1a.1525).
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 2.1525.0-6)
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 3.1525.0-6).
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 1525 summary. (Mar 29, 2009 - Apr 04, 2009)
Table 1.1525.a GPS week : 1525 MJD: 54919.0-54925.0
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 96| 2 0 -1 9 -7 -38 -.10 47 31 | 0 291 3496 3702
| 2 1 3 28 46 180 .08 | 0 1630
cod 241| -2 0 -5 7 8 67 -.12 22 18 | --- --- --- ---
| 1 1 3 26 41 57 .04 | --- ---
esx 123| -2 0 -5 -13 18 53 .39 32 26 | 92910 1520 6578 11963
| 1 1 2 36 21 42 .06 | 23976 6566
iac n/a| 4 0 19 -19 -47 -136 -.12 32 32 | 197148 110 6546 12363
| 3 2 10 38 34 47 .05 | 28350 4848
mcc n/a| 1 1 43 -86 -29 -417 -.19 76 76 | --- --- --- ---
| 6 6 16 103 109 528 .19 | --- ---
Table 1.1525.b GPS week : 1525 MJD: 54919.0-54925.0
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 19 14 18 14 11 18 |
R03 | 15 18 16 21 18 15 12 |
R04 | 21 14 13 25 19 12 11 |
R06 | 26 15 32 28 19 17 23 |
R07 | 15 16 14 20 12 12 16 |
R08 | 13 11 15 15 10 14 16 |
R10 | 12 17 9 11 20 18 22 |
R11 | 9 15 11 14 14 10 14 |
R13 | 15 15 15 14 15 12 11 |
R14 | 16 18 18 28 14 15 18 |
R15 | 11 14 17 28 21 10 12 |
R17 | 13 16 15 20 14 13 10 |
R18 | 13 12 9 33 14 12 12 |
R19 | 13 13 12 14 13 9 10 |
R20 | 14 12 14 11 13 14 15 |
R21 | 14 14 13 18 16 10 13 |
R22 | 12 11 14 16 16 14 12 |
R23 | 25 20 19 23 23 22 19 |
R24 | 16 34 39 --- --- --- --- |
Table 1.1525.c GPS week : 1525 MJD: 54919.0-54925.0
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 1525 0 | 6 18 360 1630 963 -11150 87.6 3166 3166 | 220415 0
brd 1525 1 | 97 21 304 -5891 3223 -15090 86.9 >>>>> >>>>> | 219013 0
brd 1525 2 | -18 -31 289 1229 1109 -23170 85.2 3723 3723 | 167887 0
brd 1525 3 | -105 -67 350 153 -2013 -23160 87.8 3161 3161 | 211645 0
brd 1525 4 | 29 -55 447 -361 -2041 -26330 89.3 2879 2879 | 206759 0
brd 1525 5 | -4 25 281 1028 -4005 -28760 88.4 3159 3159 | 200160 0
brd 1525 6 | 38 112 250 -2682 -737 -23570 91.5 3228 3228 | 153524 0
-------------+------------------------------------------------------------+----------------
brd 1525 mean| 6 3 326 -699 -500 -21604 88.1 >>>>> >>>>> | 197057 0
brd 1525 sdev| 61 61 65 2703 2435 6245 2.0 >>>>> >>>>> | 26109 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 2.1525.0 GPS week: 1525 Day: 0 MJD: 54919
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 96| 5 1 -3 -7 -84 108 -.05 33 29 | 0 -2706 5445 6039
cod 241| -3 2 -1 22 75 32 -.07 18 15 | --- --- --- ---
esx 123| -5 -3 -2 -24 28 28 .32 30 27 | 105444 7207 7181 12989
iac n/a| 7 -2 9 3 -41 -136 -.04 29 29 | 220692 2471 7185 13544
mcc n/a| 3 4 29 61 -62 36 -.21 80 80 | --- --- --- ---
Table 2.1525.1 GPS week: 1525 Day: 1 MJD: 54920
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 96| 1 -1 -6 59 25 149 -.05 34 31 | 0 2263 4237 4442
cod 241| -2 1 -5 -22 -42 2 -.12 26 21 | --- --- --- ---
esx 123| -3 0 -4 -38 21 45 .32 26 21 | 113525 -5360 6213 13226
iac n/a| 6 -1 17 34 -2 -170 -.19 30 30 | 223366 -7775 6219 13204
mcc n/a| 3 -3 26 60 178 -65 -.13 77 77 | --- --- --- ---
Table 2.1525.2 GPS week: 1525 Day: 2 MJD: 54921
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 96| 5 -1 0 6 23 -39 -.07 144 48 | 0 -3 2768 2858
cod 241| -2 -1 -3 3 -20 18 -.16 25 19 | --- --- --- ---
esx 123| -1 0 -5 19 -13 60 .39 27 21 | 57971 3508 7512 10898
iac n/a| 9 3 13 -31 -11 -68 -.12 31 31 | 164860 3391 7286 11666
mcc n/a| -7 0 54 -156 -3 -1155 -.48 110 110 | --- --- --- ---
Table 2.1525.3 GPS week: 1525 Day: 3 MJD: 54922
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 96| 3 -2 0 22 41 151 -.06 32 30 | 0 270 2507 2610
cod 241| -5 -2 -8 -33 24 44 -.09 27 22 | --- --- --- ---
esx 123| 0 0 -5 15 1 -21 .44 64 49 | 106627 282 6642 11280
iac n/a| 4 4 16 0 -73 -159 -.10 30 30 | 210940 -180 6580 11663
mcc n/a| 0 10 73 -147 -36 -1075 -.36 85 85 | --- --- --- ---
Table 2.1525.4 GPS week: 1525 Day: 4 MJD: 54923
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 96| 0 0 -2 22 -26 -229 -.08 30 28 | 0 94 2881 3031
cod 241| -1 0 -9 28 -7 93 -.16 21 19 | --- --- --- ---
esx 123| -2 0 -9 -69 47 110 .37 25 23 | 101970 9831 5428 11724
iac n/a| 0 0 39 -8 -93 -78 -.17 37 37 | 205236 3143 5462 12431
mcc n/a| 7 8 44 -152 -141 -213 .11 72 72 | --- --- --- ---
Table 2.1525.5 GPS week: 1525 Day: 5 MJD: 54924
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 96| 0 0 0 -10 -47 -131 -.13 21 19 | 0 2003 4080 4258
cod 241| -1 -1 -6 35 44 132 -.09 15 14 | --- --- --- ---
esx 123| 0 0 -3 -26 9 80 .42 27 24 | 106458 -8477 7185 11253
iac n/a| 2 0 26 -60 -76 -200 -.13 37 37 | 204937 -5294 7194 12365
mcc n/a| -5 -6 30 -104 3 128 -.06 60 60 | --- --- --- ---
Table 2.1525.6 GPS week: 1525 Day: 6 MJD: 54925
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 96| 3 -1 3 -25 15 -276 -.27 34 31 | 0 116 2556 2679
cod 241| -3 -1 -3 18 -11 147 -.14 18 16 | --- --- --- ---
esx 123| -1 2 -4 30 37 68 .48 22 19 | 58376 3655 5887 12377
iac n/a| 5 0 10 -76 -36 -142 -.07 34 34 | 150011 5015 5899 11674
mcc n/a| 9 -3 45 -170 -144 -581 -.22 49 49 | --- --- --- ---
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 3.1525.0 GPS week: 1525 Day: 0 MJD: 54919
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1032 18 14 14 25 --- 10 | 24 38 40 42 --- 34
R03 | 2162 32 15 37 23 --- 15 | 17 45 69 47 --- 40
R04 | 1035 40 20 27 54 --- 20 | 36 56 74 79 --- 58
R06 | 6642 65 28 39 54 --- 26 | 88 124 139 89 --- 105
R07 | 8833 29 26 20 29 --- 15 | 21 39 37 33 --- 32
R08 | 919 18 13 31 26 --- 12 | 16 30 44 30 --- 26
R10 | 976 26 14 15 28 --- 12 | 29 43 50 54 --- 40
R11 | 874 21 10 15 15 92 8 | 30 29 33 30 63 26
R13 | 1319 35 16 22 30 --- 14 | 30 23 35 31 --- 25
R14 | 3308 24 23 38 26 --- 16 | 44 34 41 33 --- 32
R15 | 1090 24 11 22 18 65 10 | 26 29 38 33 36 27
R17 | 806 25 15 32 22 --- 13 | 52 53 61 60 --- 52
R18 | 1365 26 12 34 18 --- 13 | 21 21 26 22 --- 14
R19 | 803 31 10 34 17 --- 13 | 33 44 41 40 --- 37
R20 | 1100 30 17 34 19 --- 14 | 55 64 73 61 --- 60
R21 | 1016 30 18 27 25 --- 14 | 22 26 35 34 --- 22
R22 | 1139 29 13 13 26 --- 11 | 24 17 18 29 --- 16
R23 | 979 54 33 52 37 --- 24 | 81 76 107 111 --- 87
R24 | 6113 30 19 38 28 --- 16 | 158 97 96 62 --- 98
------+------------------------------------+--------------------------------
RMS | 3166 33 18 30 29 80 |T 42 46 55 48 49 43
WRMS | 3166 29 15 27 29 80 |NE 42 46 55 48 49 43
MEDI | 1090 29 15 31 26 65 |MD 30 39 41 40 36 34
Table 3.1525.1 GPS week: 1525 Day: 1 MJD: 54920
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 47 22 20 38 --- 18 | 14 29 47 51 --- 30
R03 |>>>>> 43 30 18 34 --- 18 | 20 53 41 55 --- 37
R04 |>>>>> 26 16 14 36 --- 13 | 26 42 35 59 --- 38
R06 |>>>>> 25 29 19 26 --- 14 | 128 120 136 129 --- 126
R07 |>>>>> 33 37 20 17 --- 16 | 19 39 25 21 --- 19
R08 |>>>>> 22 13 20 17 --- 10 | 19 21 41 41 --- 26
R10 |>>>>> 21 30 28 34 --- 16 | 41 41 39 48 --- 35
R11 |>>>>> 19 33 21 23 97 14 | 32 33 36 30 93 24
R13 |>>>>> 32 23 20 28 --- 15 | 43 30 48 31 --- 33
R14 |>>>>> 46 22 25 29 --- 18 | 34 20 38 30 --- 20
R15 |>>>>> 29 23 20 22 47 13 | 24 26 42 37 26 27
R17 |>>>>> 11 32 34 25 --- 16 | 47 52 65 52 --- 48
R18 |>>>>> 15 15 22 26 --- 11 | 23 13 28 20 --- 17
R19 |>>>>> 22 21 21 25 --- 13 | 22 19 53 30 --- 27
R20 |>>>>> 23 19 21 21 --- 12 | 80 67 72 70 --- 70
R21 |>>>>> 27 14 20 33 --- 13 | 33 30 30 32 --- 28
R22 |>>>>> 19 13 17 27 --- 11 | 21 21 34 24 --- 21
R23 |>>>>> 44 32 25 38 --- 20 | 69 65 94 91 --- 77
R24 |>>>>> 79 44 63 45 --- 33 | 51 122 135 55 --- 113
------+------------------------------------+--------------------------------
RMS |>>>>> 34 26 26 30 77 |T 39 44 54 47 59 42
WRMS |>>>>> 31 21 21 30 77 |NE 39 44 54 47 59 42
MEDI |>>>>> 26 23 20 27 47 |MD 32 33 41 41 26 30
Table 3.1525.2 GPS week: 1525 Day: 2 MJD: 54921
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1915 21 21 20 32 --- 13 | 20 23 31 29 --- 18
R03 | 9828 38 17 23 30 --- 15 | 20 34 39 36 --- 26
R04 | 3011 24 22 26 16 --- 13 | 38 53 64 51 --- 49
R06 | 5244 77 40 52 50 --- 31 | 133 177 198 177 --- 170
R07 | 2953 26 25 18 28 --- 14 | 16 45 25 33 --- 27
R08 | 1088 22 24 24 30 --- 14 | 16 27 44 38 --- 26
R10 | 1326 12 14 16 16 --- 8 | 29 26 36 37 --- 28
R11 | 929 19 11 20 22 137 10 | 29 27 34 27 145 24
R13 | 1705 15 16 33 31 --- 14 | 31 20 50 27 --- 25
R14 | 1646 41 31 20 32 --- 18 | 39 34 45 28 --- 26
R15 | 2493 33 17 29 40 75 17 | 34 20 49 23 44 21
R17 | 1327 37 20 22 28 --- 15 | 42 43 65 74 --- 51
R18 | 1394 13 15 13 20 --- 9 | 16 24 43 25 --- 12
R19 | 1244 18 17 13 33 --- 12 | 19 19 29 31 --- 19
R20 | 2101 27 17 18 31 --- 13 | 54 39 52 32 --- 41
R21 | 1577 25 21 14 30 --- 13 | 36 29 34 33 --- 28
R22 | 1061 36 20 19 22 --- 14 | 20 30 33 23 --- 21
R23 | 3130 45 25 28 33 --- 19 | 68 67 90 98 --- 79
R24 | 8889 615 59 59 39 --- 38 | 176 249 251 56 --- 242
------+------------------------------------+--------------------------------
RMS | 3722 144 25 27 31 110 |T 44 51 63 46 94 49
WRMS | 3722 48 19 21 31 110 |NE 44 51 63 46 94 49
MEDI | 1705 26 20 20 30 75 |MD 31 30 44 33 44 26
Table 3.1525.3 GPS week: 1525 Day: 3 MJD: 54922
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1172 41 26 28 23 --- 17 | 35 31 33 32 --- 20
R03 |10635 43 25 59 28 --- 21 | 17 40 63 36 --- 26
R04 | 4359 37 11 99 22 --- 24 | 40 54 128 51 --- 52
R06 | 3045 47 51 72 30 --- 28 | 84 145 119 101 --- 108
R07 | 1618 38 30 37 32 --- 19 | 19 56 34 50 --- 35
R08 | 929 17 14 48 25 --- 14 | 35 34 60 36 --- 26
R10 | 1169 19 15 23 22 --- 11 | 39 27 37 29 --- 28
R11 | 1129 26 8 23 35 102 14 | 37 24 34 32 86 24
R13 | 927 12 22 36 29 --- 14 | 29 37 59 42 --- 33
R14 | 2278 32 53 78 39 --- 28 | 26 51 92 43 --- 29
R15 | 1656 28 41 104 29 65 28 | 45 32 123 45 32 45
R17 | 1088 27 21 63 37 --- 20 | 40 37 80 73 --- 48
R18 | 905 33 23 138 40 --- 33 | 31 18 105 44 --- 19
R19 | 1758 17 24 38 22 --- 14 | 22 30 40 25 --- 20
R20 | 1428 17 17 21 22 --- 11 | 44 39 47 45 --- 40
R21 | 2499 31 15 50 32 --- 17 | 45 39 57 36 --- 33
R22 | 1321 33 15 41 27 --- 16 | 27 27 44 24 --- 22
R23 | 2660 42 25 52 41 --- 22 | 55 57 97 93 --- 68
------+------------------------------------+--------------------------------
RMS | 3161 32 27 64 30 85 |T 37 43 69 46 59 37
WRMS | 3161 30 22 49 30 85 |NE 37 43 69 46 59 37
MEDI | 1428 31 22 48 29 65 |MD 35 37 59 42 32 29
Table 3.1525.4 GPS week: 1525 Day: 4 MJD: 54923
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1448 24 18 18 39 --- 14 | 24 24 27 37 --- 17
R03 | 6133 30 28 27 39 --- 17 | 23 32 42 32 --- 24
R04 | 4390 36 25 38 33 --- 19 | 38 37 46 44 --- 31
R06 | 5484 42 31 21 37 --- 19 | 117 151 163 148 --- 143
R07 | 3202 27 12 20 24 --- 12 | 27 41 54 27 --- 35
R08 | 1057 21 7 17 21 --- 9 | 24 31 43 23 --- 28
R10 | 1850 33 29 39 33 --- 19 | 46 34 57 41 --- 35
R11 | 2342 30 13 23 32 81 14 | 38 33 50 38 46 36
R13 | 695 9 22 28 39 --- 14 | 31 22 43 60 --- 31
R14 | 3359 19 21 18 42 --- 14 | 24 37 38 47 --- 28
R15 | 2629 27 27 30 61 62 20 | 23 31 59 44 26 25
R17 | 714 27 18 20 35 --- 14 | 32 33 52 61 --- 38
R18 | 633 35 15 14 32 --- 14 | 33 19 61 52 --- 24
R19 | 2413 29 21 13 26 --- 13 | 33 23 35 49 --- 26
R20 | 1426 25 15 26 26 --- 13 | 40 29 49 27 --- 32
R21 | 1819 27 19 23 41 --- 15 | 43 20 40 25 --- 23
R22 | 2862 25 19 33 32 --- 16 | 29 21 58 31 --- 29
R23 | 955 55 28 30 48 --- 22 | 41 64 57 101 --- 57
------+------------------------------------+--------------------------------
RMS | 2879 30 21 25 37 72 |T 37 37 54 49 36 36
WRMS | 2879 28 19 23 37 72 |NE 37 37 54 49 36 36
MEDI | 1850 27 19 23 33 62 |MD 32 31 49 41 26 29
Table 3.1525.5 GPS week: 1525 Day: 5 MJD: 54924
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3055 19 11 17 32 --- 11 | 22 30 33 37 --- 26
R03 | 6927 16 13 24 55 --- 15 | 40 27 28 42 --- 25
R04 | 2518 25 14 23 20 --- 11 | 33 41 51 36 --- 38
R06 | 5634 29 21 31 45 --- 17 | 43 56 62 75 --- 50
R07 | 5015 22 15 21 24 --- 11 | 8 24 30 22 --- 15
R08 | 1372 17 11 18 54 --- 14 | 26 31 24 68 --- 30
R10 | 1967 19 22 42 46 --- 17 | 22 37 46 40 --- 23
R11 | 2475 19 14 21 18 48 10 | 38 30 40 26 46 31
R13 | 739 19 9 32 22 --- 11 | 28 27 47 33 --- 27
R14 | 2678 14 16 24 55 --- 15 | 20 28 39 49 --- 22
R15 | 3403 12 12 23 29 70 10 | 36 36 49 65 28 40
R17 | 816 20 19 21 31 --- 12 | 20 29 35 44 --- 26
R18 | 2070 14 12 33 24 --- 11 | 10 14 37 29 --- 16
R19 | 1268 13 7 21 28 --- 9 | 25 23 33 33 --- 23
R20 | 2555 25 19 22 30 --- 13 | 26 34 31 36 --- 26
R21 | 2302 12 11 16 29 --- 9 | 28 31 36 38 --- 28
R22 | 2930 16 17 32 37 --- 14 | 26 27 53 30 --- 28
R23 | 952 41 21 46 50 --- 21 | 36 53 75 83 --- 50
------+------------------------------------+--------------------------------
RMS | 3159 21 15 27 37 60 |T 27 32 41 43 37 29
WRMS | 3159 19 14 24 37 60 |NE 27 32 41 43 37 29
MEDI | 2475 19 14 23 30 48 |MD 26 30 37 37 28 26
Table 3.1525.6 GPS week: 1525 Day: 6 MJD: 54925
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2406 35 13 18 56 --- 17 | 29 47 36 88 --- 45
R03 | 2809 18 13 16 33 --- 11 | 33 41 44 55 --- 40
R04 | 5373 16 17 22 21 --- 11 | 53 54 62 65 --- 54
R06 | 8117 59 25 44 32 --- 23 | 126 97 66 102 --- 91
R07 | 4178 29 13 24 43 --- 15 | 27 38 40 37 --- 29
R08 | 1454 46 20 23 23 --- 16 | 33 40 61 45 --- 40
R10 | 1844 35 33 11 65 --- 21 | 39 51 46 45 --- 40
R11 | 2457 40 16 16 25 28 13 | 56 37 42 40 77 38
R13 | 1355 26 8 21 19 --- 10 | 32 37 48 53 --- 39
R14 | 1809 35 23 33 38 --- 18 | 36 33 41 39 --- 26
R15 | 2171 23 21 11 26 63 11 | 46 30 42 59 47 36
R17 | 1804 24 11 12 25 --- 10 | 39 46 51 60 --- 46
R18 | 1849 24 19 13 25 --- 11 | 25 27 32 34 --- 24
R19 | 1210 25 11 17 17 --- 9 | 35 22 25 34 --- 22
R20 | 4229 44 16 18 30 --- 15 | 35 39 39 36 --- 33
R21 | 1584 29 15 10 38 --- 13 | 28 33 39 53 --- 34
R22 | 3178 24 15 23 18 --- 11 | 36 25 43 34 --- 28
R23 | 1256 49 17 35 28 --- 18 | 79 78 106 107 --- 86
------+------------------------------------+--------------------------------
RMS | 3227 34 18 22 34 49 |T 43 43 47 54 62 41
WRMS | 3227 31 16 19 34 49 |NE 43 43 47 54 62 41
MEDI | 1849 29 16 18 26 28 |MD 35 38 42 45 47 38
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