[IGSREPORT-17245] Wk 1522 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 26 05:52:20 PDT 2009
******************************************************************************
IGS Electronic Report 26 Mar 05:52:43 PDT 2009 Message Number 17245
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1522 (Mar 08, 2009 - Mar 14, 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 2.1522.
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:
igl1522[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1522 in the SP3 format.
igl15227.sum Combination Report for GPS Week 1522.
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 | 237.7 ns
1 | 239.7 ns
2 | 249.8 ns
3 | 208.9 ns
4 | 208.0 ns
5 | 247.4 ns
6 | 246.4 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 | R14
3 | ESX | R14 R19
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 1.1522, 1a.1522).
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 2.1522.0-6)
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 3.1522.0-6).
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 1522 summary. (Mar 08, 2009 - Mar 14, 2009)
Table 1.1522.a GPS week : 1522 MJD: 54898.0-54904.0
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 100| 0 1 2 -9 -28 -74 -.25 69 40 | 0 79 2892 3425
| 2 2 8 59 53 214 .14 | 0 569
cod 239| -1 0 -7 1 7 57 -.19 24 16 | --- --- --- ---
| 1 1 2 20 32 55 .04 | --- ---
esx 122| -3 0 -3 22 -7 74 .28 42 29 | 114639 -3598 8086 14776
| 1 1 7 39 37 80 .09 | 19541 5686
iac n/a| 3 0 16 -48 24 -158 .22 42 42 | 234736 -1460 7760 14659
| 2 2 5 23 28 88 .04 | 17874 2876
mcc n/a| 2 1 10 -49 -33 -489 .11 233 233 | --- --- --- ---
| 13 6 17 103 99 525 .63 | --- ---
Table 1.1522.b GPS week : 1522 MJD: 54898.0-54904.0
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 | 13 10 11 11 15 14 13 |
R03 | 13 12 11 12 13 17 11 |
R04 | 11 7 11 13 12 19 11 |
R06 | 20 15 23 20 15 25 15 |
R07 | 17 15 12 13 13 16 14 |
R08 | 14 16 12 10 19 21 11 |
R10 | 11 11 14 27 20 17 14 |
R11 | 12 7 9 13 16 17 12 |
R13 | 13 13 10 12 14 16 14 |
R14 | 16 7 12 26 63 19 10 |
R15 | 13 13 12 10 13 16 15 |
R17 | 30 29 32 40 34 27 26 |
R18 | 21 24 24 22 20 21 18 |
R19 | 29 24 35 30 23 22 17 |
R20 | 24 26 26 22 31 30 22 |
R21 | 24 19 22 28 24 30 21 |
R22 | 20 15 19 26 21 26 29 |
R23 | 72 24 29 32 34 33 28 |
R24 | 20 15 16 16 15 19 19 |
Table 1.1522.c GPS week : 1522 MJD: 54898.0-54904.0
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 1522 0 | -149 -178 228 -976 140 -21080 87.6 11400 11400 | 237690 0
brd 1522 1 | -362 -147 -277 1614 -19330 -11020 353.3 >>>>> >>>>> | 239655 0
brd 1522 2 | 66 18 534 268 954 -11150 90.0 13180 13180 | 249763 0
brd 1522 3 | 3 376 739 -2165 -7 -7684 107.7 >>>>> >>>>> | 208919 0
brd 1522 4 | -96 4 128 -634 1000 -8600 102.5 >>>>> >>>>> | 207964 0
brd 1522 5 | 154 -160 138 2674 1506 -11670 112.2 >>>>> >>>>> | 247425 0
brd 1522 6 | 43 1 37 2457 -132 -13870 95.1 >>>>> >>>>> | 246350 0
-------------+------------------------------------------------------------+----------------
brd 1522 mean| -48 -12 218 462 -2266 -12153 135.5 >>>>> >>>>> | 233966 0
brd 1522 sdev| 171 191 332 1844 7548 4430 96.5 >>>>> >>>>> | 17952 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 2.1522.0 GPS week: 1522 Day: 0 MJD: 54898
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 100| 1 1 -4 -1 6 277 -.46 37 36 | 0 -26 2399 2472
cod 239| 0 0 -9 -25 -19 64 -.18 48 19 | --- --- --- ---
esx 122| -5 -1 -4 41 -2 -41 .36 33 27 | 121016 -4609 8210 17699
iac n/a| 1 2 27 -51 31 -331 .19 47 47 | 241037 -2018 7991 18227
mcc n/a| -3 -1 20 130 79 -642 -.56 158 158 | --- --- --- ---
Table 2.1522.1 GPS week: 1522 Day: 1 MJD: 54899
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 100| 0 1 -1 -55 23 76 -.27 29 29 | 0 -118 2070 2122
cod 239| -1 -1 -7 35 -51 37 -.20 18 17 | --- --- --- ---
esx 122| -3 0 0 16 58 45 .39 30 28 | 127911 -1114 8100 14759
iac n/a| 3 -1 17 -47 39 -194 .21 43 43 | 238991 1888 7720 15286
mcc n/a| -15 6 -3 -167 -108 51 -.04 304 304 | --- --- --- ---
Table 2.1522.2 GPS week: 1522 Day: 2 MJD: 54900
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 100| 1 0 4 -38 -52 -80 -.08 232 38 | 0 -184 2300 2352
cod 239| -3 0 -7 16 18 25 -.22 19 13 | --- --- --- ---
esx 122| -3 2 -4 94 -27 117 .22 33 29 | 138314 -3631 7832 13324
iac n/a| 4 0 12 -85 17 -169 .30 39 39 | 250011 -3514 7628 12330
mcc n/a| 4 1 3 -115 -63 136 -.61 408 408 | --- --- --- ---
Table 2.1522.3 GPS week: 1522 Day: 3 MJD: 54901
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 100| 0 3 0 5 -51 -208 -.22 35 37 | 0 1279 3726 6790
cod 239| -1 -2 -9 -9 19 97 -.14 21 13 | --- --- --- ---
esx 122| -2 3 6 -7 16 106 .36 98 28 | 90013 -201 9166 13058
iac n/a| 2 0 13 -44 -20 -106 .17 38 38 | 210063 1981 7707 14056
mcc n/a| 0 -4 -19 -113 -168 -1347 .23 171 171 | --- --- --- ---
Table 2.1522.4 GPS week: 1522 Day: 4 MJD: 54902
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 100| -1 1 19 -29 -37 7 -.40 50 41 | 0 21 2439 2551
cod 239| -1 0 -3 -2 26 -11 -.15 23 16 | --- --- --- ---
esx 122| -2 0 -17 36 -39 71 .17 33 27 | 87247 -8216 8812 13870
iac n/a| 0 1 14 -63 73 -154 .23 44 44 | 208767 -2995 8746 13969
mcc n/a| 10 1 20 -61 -44 -888 .97 105 105 | --- --- --- ---
Table 2.1522.5 GPS week: 1522 Day: 5 MJD: 54903
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 100| -3 4 4 113 -121 -252 -.18 64 63 | 0 122 2581 2697
cod 239| -2 0 -5 -10 46 31 -.27 23 19 | --- --- --- ---
esx 122| 0 -2 -5 -21 -1 13 .22 31 27 | 126713 -12483 7177 14927
iac n/a| 4 -3 12 -38 11 -71 .27 45 45 | 251315 -5631 7233 14580
mcc n/a| 28 11 25 -63 -43 -261 .87 179 179 | --- --- --- ---
Table 2.1522.6 GPS week: 1522 Day: 6 MJD: 54904
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 100| 4 -2 -4 -59 30 -343 -.14 37 33 | 0 -537 4733 4994
cod 239| -2 3 -10 8 10 158 -.19 19 14 | --- --- --- ---
esx 122| -3 0 3 -5 -55 210 .23 35 34 | 111265 5062 7305 15798
iac n/a| 6 -3 18 -9 16 -82 .21 38 38 | 242972 66 7300 14166
mcc n/a| -3 -6 26 44 114 -472 -.07 306 306 | --- --- --- ---
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 3.1522.0 GPS week: 1522 Day: 0 MJD: 54898
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 911 25 20 18 25 --- 12 | 43 53 41 47 --- 42
R03 | 2482 23 18 19 30 --- 13 | 47 41 40 52 --- 42
R04 | 2093 18 13 26 15 --- 11 | 49 46 49 48 --- 45
R06 | 7655 45 27 27 41 --- 20 | 74 80 61 65 --- 65
R07 | 2687 40 10 33 22 --- 16 | 72 50 30 46 --- 45
R08 | 6288 29 24 26 17 --- 14 | 51 39 31 32 --- 32
R10 | 1099 23 16 19 18 --- 11 | 37 30 27 27 --- 23
R11 | 1311 26 8 21 19 152 11 | 28 24 31 27 23 23
R13 | 3445 20 14 26 23 --- 12 | 38 25 27 36 --- 26
R14 | 3264 30 18 33 22 --- 15 | 123 36 58 37 --- 33
R15 | 2255 33 21 15 16 110 13 | 45 29 31 27 32 27
R17E | 1847 53 36 47 69 --- 29 | 31 31 38 61 --- 25
R18E | 1189 35 24 32 50 --- 20 | 38 29 54 55 --- 35
XR19E | 1186 30 29 --- 59 --- 28 | 70 87 --- 86 --- 77
R20E | 2397 38 33 37 58 --- 24 | 66 69 57 79 --- 60
R21E | 1913 26 19 36 71 --- 23 | 34 28 27 34 --- 22
R22E | 851 24 20 29 57 --- 19 | 34 28 36 65 --- 30
R23E |38679 84 182 76 122 --- 72 | 61 177 66 70 --- 63
R24E |26057 45 35 23 28 199 19 | 45 49 61 48 143 48
------+------------------------------------+--------------------------------
RMS |11395 37 48 33 47 158 |T 51 50 42 49 66 40
WRMS |11395 36 19 27 47 158 |NE 55 41 38 40 27 36
MEDI | 2255 30 20 26 28 152 |MD 45 39 38 48 32 35
Table 3.1522.1 GPS week: 1522 Day: 1 MJD: 54899
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 22 9 17 19 --- 9 | 44 51 58 64 --- 53
R03 |>>>>> 15 14 23 29 --- 11 | 26 27 37 24 --- 24
R04 |>>>>> 10 10 15 11 --- 6 | 35 34 42 43 --- 37
R06 |>>>>> 28 17 32 29 --- 15 | 58 81 82 51 --- 69
R07 |>>>>> 18 21 40 16 --- 14 | 30 33 39 28 --- 24
R08 |>>>>> 19 25 35 30 --- 16 | 37 35 45 37 --- 31
R10 |>>>>> 23 17 14 16 --- 10 | 23 28 35 25 --- 24
R11 |>>>>> 13 8 11 18 150 7 | 20 26 26 29 40 22
R13 |>>>>> 22 23 26 18 --- 13 | 26 31 36 34 --- 28
XR14 |>>>>> --- 7 9 13 --- 7 | --- 23 112 22 --- 23
R15 |>>>>> 24 20 17 27 121 12 | 33 35 39 32 48 31
R17E |>>>>> 51 25 44 82 --- 28 | 49 23 50 48 --- 19
R18E |>>>>> 50 15 39 61 --- 23 | 32 28 37 48 --- 24
XR19E |>>>>> 35 27 --- 43 --- 24 | 40 73 --- 71 --- 60
R20E |>>>>> 38 26 46 74 --- 26 | 46 45 81 77 --- 54
R21E |>>>>> 27 15 37 54 --- 18 | 19 30 46 40 --- 25
R22E |>>>>> 23 17 24 43 --- 15 | 40 32 31 45 --- 30
R23E |>>>>> 38 21 35 73 --- 23 | 32 66 64 52 --- 37
R24E |>>>>> 26 19 30 27 489 14 | 28 47 51 42 122 38
------+------------------------------------+--------------------------------
RMS |>>>>> 29 18 30 43 303 |T 34 39 50 42 70 34
WRMS |>>>>> 29 17 28 43 303 |NE 33 36 50 35 44 33
MEDI |>>>>> 23 17 26 29 150 |MD 32 33 42 42 48 30
Table 3.1522.2 GPS week: 1522 Day: 2 MJD: 54900
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2251 19 9 32 17 --- 11 | 45 43 36 40 --- 38
R03 | 4380 14 10 20 28 --- 10 | 47 42 43 41 --- 39
R04 | 2196 25 12 25 15 --- 11 | 37 33 54 38 --- 36
R06 | 3929 66 18 45 33 --- 23 | 105 144 156 140 --- 135
R07 | 1745 28 12 27 17 --- 12 | 49 43 52 38 --- 41
R08 | 4505 21 15 22 24 --- 11 | 21 36 41 20 --- 25
R10 | 942 28 14 28 26 --- 13 | 40 44 63 29 --- 39
R11 | 1398 12 7 18 21 114 8 | 17 21 26 29 36 18
R13 | 2190 18 17 16 20 --- 10 | 19 31 26 20 --- 19
R14 | 4141 969 11 14 27 --- 12 | 857 32 316 25 --- 23
R15 | 2843 20 17 17 30 123 12 | 22 34 37 19 50 27
R17E | 698 76 38 43 71 --- 32 | 76 25 47 47 --- 26
R18E | 1256 39 23 38 66 --- 23 | 37 31 41 46 --- 31
XR19E | 978 68 34 --- 52 --- 34 | 60 79 --- 102 --- 75
R20E | 4253 42 31 49 64 --- 26 | 68 61 84 78 --- 64
R21E | 1072 54 20 30 53 --- 22 | 42 30 30 44 --- 22
R22E | 665 28 21 35 52 --- 19 | 33 34 38 44 --- 27
R23E |50511 75 25 61 44 --- 29 | 30 53 62 60 --- 38
R24E |21318 44 18 29 23 687 16 | 39 38 64 45 347 39
------+------------------------------------+--------------------------------
RMS |13183 232 19 33 39 408 |T 86 44 67 47 144 40
WRMS |13183 38 13 29 39 408 |NE 114 45 77 39 43 40
MEDI | 2196 28 17 28 28 123 |MD 40 36 43 41 50 36
Table 3.1522.3 GPS week: 1522 Day: 3 MJD: 54901
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 20 14 18 26 --- 11 | 54 65 53 54 --- 55
R03 |>>>>> 21 14 20 26 --- 11 | 45 51 39 26 --- 40
R04 |>>>>> 29 8 33 13 --- 12 | 74 49 60 56 --- 55
R06 |>>>>> 52 18 39 31 --- 19 | 99 138 130 149 --- 127
R07 |>>>>> 23 12 22 36 --- 13 | 48 49 49 79 --- 51
R08 |>>>>> 22 9 21 21 --- 10 | 77 55 54 67 --- 59
XR10 |>>>>> 31 --- --- 19 --- 26 | 23 --- --- 28 --- 27
R11 |>>>>> 36 13 24 16 58 13 | 34 41 50 41 71 38
R13 |>>>>> 25 14 28 20 --- 12 | 36 27 37 42 --- 29
XR14 |>>>>> 23 --- 1276 27 --- 25 | 240 --- 9999 36 --- 33
R15 |>>>>> 23 11 21 15 77 9 | 75 56 62 60 114 59
XR17E |>>>>> 64 --- 60 39 --- 39 | 48 --- 74 41 --- 48
R18E |>>>>> 43 21 38 54 --- 21 | 42 28 41 44 --- 24
R19E |>>>>> 49 34 356 47 --- 29 | 58 53 9999 53 --- 48
R20E |>>>>> 44 25 37 53 --- 22 | 50 33 41 67 --- 35
XR21E |>>>>> 31 --- --- 24 --- 28 | 38 --- --- 43 --- 41
R22E |>>>>> 45 24 46 67 --- 25 | 52 41 30 65 --- 39
R23E |>>>>> 32 40 86 61 --- 32 | 71 60 109 50 --- 51
R24E |>>>>> 37 21 28 22 280 15 | 34 41 55 39 382 37
------+------------------------------------+--------------------------------
RMS |>>>>> 35 21 98 38 171 |T 63 52 58 54 189 47
WRMS |>>>>> 37 13 28 38 171 |NE 73 59 59 58 92 52
MEDI |>>>>> 31 14 33 26 77 |MD 50 49 53 50 114 41
Table 3.1522.4 GPS week: 1522 Day: 4 MJD: 54902
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 34 16 32 20 --- 14 | 40 40 59 33 --- 39
R03 |>>>>> 33 17 18 24 --- 12 | 50 51 47 43 --- 45
R04 |>>>>> 39 11 16 15 --- 11 | 46 25 36 25 --- 27
R06 |>>>>> 50 14 14 31 --- 15 | 84 103 98 92 --- 91
R07 |>>>>> 36 12 21 22 --- 12 | 43 51 69 56 --- 52
R08 |>>>>> 43 16 40 33 --- 18 | 31 35 85 50 --- 45
R10 | 2985 51 20 31 39 --- 19 | 62 43 65 30 --- 45
R11 |>>>>> 40 16 31 23 67 15 | 42 21 41 22 27 21
R13 |>>>>> 31 14 27 29 --- 14 | 31 28 40 30 --- 24
XR14 | 9727 156 62 --- 48 --- 62 | 216 45 --- 43 --- 41
R15 |>>>>> 47 11 18 16 84 13 | 35 33 39 33 43 30
R17E |>>>>> 111 35 20 67 --- 33 | 103 36 32 68 --- 31
R18E |>>>>> 39 24 40 41 --- 20 | 38 28 64 36 --- 28
R19E |>>>>> 42 28 33 57 --- 22 | 43 68 9999 79 --- 62
R20E |>>>>> 55 41 52 73 --- 31 | 63 31 55 65 --- 38
R21E |>>>>> 44 25 23 74 --- 24 | 47 26 27 60 --- 27
R22E |>>>>> 47 30 30 40 --- 20 | 47 43 50 43 --- 33
R23E |>>>>> 70 31 66 74 --- 33 | 70 65 106 48 --- 60
R24E |>>>>> 26 21 30 23 146 14 | 45 34 56 33 158 35
------+------------------------------------+--------------------------------
RMS |>>>>> 50 23 33 44 105 |T 59 42 57 46 76 40
WRMS |>>>>> 41 16 27 44 105 |NE 61 43 57 41 35 41
MEDI |>>>>> 43 20 30 33 84 |MD 46 36 55 43 43 38
Table 3.1522.5 GPS week: 1522 Day: 5 MJD: 54903
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 48 16 17 25 --- 14 | 62 46 38 43 --- 39
R03 |>>>>> 51 22 28 27 --- 17 | 64 39 50 36 --- 36
R04 |>>>>> 54 25 31 27 --- 18 | 76 51 44 55 --- 46
R06 |>>>>> 89 21 39 33 --- 24 | 108 94 85 79 --- 80
R07 |>>>>> 53 14 21 32 --- 16 | 67 36 37 32 --- 30
R08 |>>>>> 53 23 23 53 --- 20 | 78 36 52 67 --- 48
R10 | 2903 63 14 25 20 --- 16 | 54 32 32 17 --- 23
R11 |>>>>> 59 17 22 26 102 16 | 71 27 46 31 41 33
R13 |>>>>> 57 15 17 25 --- 15 | 52 32 39 28 --- 28
R14 | 8817 51 16 30 44 --- 19 | 101 38 193 33 --- 30
R15 |>>>>> 62 16 23 14 104 16 | 65 35 27 33 63 31
R17E |>>>>> 68 27 31 70 --- 26 | 76 41 38 48 --- 33
R18E |>>>>> 60 18 30 45 --- 20 | 69 23 37 38 --- 26
R19E |>>>>> 71 19 32 42 --- 22 | 58 31 9999 36 --- 22
R20E |>>>>> 76 29 46 70 --- 29 | 68 47 61 71 --- 46
R21E |>>>>> 68 35 31 83 --- 30 | 67 19 27 59 --- 15
R22E |>>>>> 85 31 26 54 --- 26 | 62 45 32 56 --- 36
R23E |>>>>> 71 40 67 54 --- 32 | 86 62 89 36 --- 50
R24E |>>>>> 67 21 23 27 274 18 | 72 46 47 31 136 41
------+------------------------------------+--------------------------------
RMS |>>>>> 64 23 31 45 179 |T 71 41 54 43 80 36
WRMS |>>>>> 63 19 27 45 179 |NE 72 42 58 41 52 38
MEDI |>>>>> 62 21 28 33 104 |MD 68 38 39 36 63 33
Table 3.1522.6 GPS week: 1522 Day: 6 MJD: 54904
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 21 14 25 29 --- 12 | 44 63 60 36 --- 51
R03 |>>>>> 23 13 25 15 --- 10 | 36 50 36 44 --- 41
R04 |>>>>> 19 18 18 21 --- 11 | 33 47 34 37 --- 36
R06 |>>>>> 40 11 28 26 --- 15 | 76 53 55 58 --- 56
R07 |>>>>> 24 14 36 20 --- 13 | 42 49 30 52 --- 42
R08 |>>>>> 19 11 28 19 --- 11 | 40 35 34 41 --- 32
R10 | 2993 26 19 29 21 --- 13 | 29 39 38 16 --- 24
R11 |>>>>> 31 7 25 17 97 11 | 31 26 28 23 31 20
R13 |>>>>> 35 13 33 19 --- 14 | 39 31 36 22 --- 24
XR14 | 3878 15 9 --- 19 --- 10 | 78 31 --- 28 --- 26
R15 |>>>>> 26 17 33 28 89 14 | 25 35 47 28 50 30
R17E |>>>>> 24 32 49 70 --- 26 | 35 25 45 56 --- 23
R18E |>>>>> 27 15 39 45 --- 18 | 25 24 39 42 --- 20
R19E |>>>>> 22 17 31 45 --- 16 | 25 31 9999 51 --- 27
R20E |>>>>> 34 27 48 46 --- 21 | 53 37 60 48 --- 37
R21E |>>>>> 33 24 27 56 --- 20 | 30 37 24 46 --- 25
R22E |>>>>> 63 29 53 63 --- 29 | 31 37 43 61 --- 34
R23E |>>>>> 80 23 46 43 --- 27 | 71 55 56 54 --- 51
R24E |>>>>> 53 18 38 28 514 19 | 47 63 82 56 186 58
------+------------------------------------+--------------------------------
RMS |>>>>> 37 19 35 38 306 |T 41 40 43 42 89 34
WRMS |>>>>> 33 14 34 38 306 |NE 43 41 39 35 40 34
MEDI |>>>>> 26 17 31 28 97 |MD 36 37 39 44 50 32
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