[IGSREPORT-17198] Wk 1520 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 12 04:22:24 PDT 2009
******************************************************************************
IGS Electronic Report 12 Mar 04:22:46 PDT 2009 Message Number 17198
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1520 (Feb 22, 2009 - Feb 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 2.1520.
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:
igl1520[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1520 in the SP3 format.
igl15207.sum Combination Report for GPS Week 1520.
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 | 238.0 ns
1 | 236.4 ns
2 | 235.4 ns
3 | 243.4 ns
4 | 234.9 ns
5 | 241.2 ns
6 | 244.4 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
----+--------+---------------
3 | BKG | R06
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 1.1520, 1a.1520).
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 2.1520.0-6)
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 3.1520.0-6).
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 1520 summary. (Feb 22, 2009 - Feb 28, 2009)
Table 1.1520.a GPS week : 1520 MJD: 54884.0-54890.0
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| 0 1 -6 -3 -9 -47 -.14 30 26 | 0 21 2274 2333
| 1 1 4 39 31 173 .06 | 0 143
cod 238| 0 0 1 6 -10 91 -.10 19 15 | --- --- --- ---
| 1 1 4 23 18 71 .05 | --- ---
esx 130| 0 -1 2 14 32 41 .38 32 27 | 117708 -1043 5630 11782
| 1 1 5 33 56 49 .09 | 5073 3686
iac n/a| 0 1 2 -37 -5 -128 -.02 30 30 | 639627 78796 181770 293537
| 1 1 9 24 34 52 .09 | 690474 136702
mcc n/a| 5 -7 19 -126 117 1016 .09 203 203 | --- --- --- ---
| 19 10 34 173 138 353 .45 | --- ---
Table 1.1520.b GPS week : 1520 MJD: 54884.0-54890.0
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 | 8 13 10 13 9 14 10 |
R03 | 12 12 11 16 13 15 15 |
R04 | 11 11 15 11 11 8 16 |
R06 | 55 70 93 60 48 18 33 |
R07 | 8 11 9 9 11 11 12 |
R08 | 12 11 13 16 19 23 9 |
R10 | 11 11 11 10 11 11 9 |
R11 | 10 12 15 12 7 11 9 |
R13 | 11 10 15 10 12 11 11 |
R14 | 9 12 13 11 11 12 13 |
R15 | 16 12 17 13 10 11 12 |
R17 | 23 17 15 14 13 23 24 |
R18 | 22 11 17 17 16 18 17 |
R19 | 16 11 11 18 15 15 14 |
R20 | 15 15 24 21 22 22 26 |
R21 | 31 15 13 16 15 16 20 |
R22 | 13 12 14 18 17 18 19 |
R23 | 19 22 22 22 27 19 21 |
R24 | 0 28 21 19 29 17 21 |
Table 1.1520.c GPS week : 1520 MJD: 54884.0-54890.0
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 1520 0 | -4 66 78 528 -1646 -8644 105.8 >>>>> >>>>> | 237985 0
brd 1520 1 | -93 71 18 -884 264 -11340 91.0 >>>>> >>>>> | 236445 0
brd 1520 2 | -36 -489 39 -1335 -1038 -16400 106.7 >>>>> >>>>> | 235445 0
brd 1520 3 | -31 -119 204 -702 -635 -15180 111.9 >>>>> >>>>> | 243443 0
brd 1520 4 | -6 180 107 -449 322 -17620 97.4 >>>>> >>>>> | 234938 0
brd 1520 5 | 95 -57 163 913 840 -13660 86.0 >>>>> >>>>> | 241221 0
brd 1520 6 | -135 -96 343 -68 -1257 -16930 102.4 >>>>> >>>>> | 244361 0
-------------+------------------------------------------------------------+----------------
brd 1520 mean| -30 -63 136 -285 -449 -14253 100.2 >>>>> >>>>> | 239119 0
brd 1520 sdev| 73 216 112 796 934 3272 9.2 >>>>> >>>>> | 3873 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 2.1520.0 GPS week: 1520 Day: 0 MJD: 54884
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 4 -8 -76 37 147 -.14 31 26 | 0 154 1961 2023
cod 238| -2 0 0 24 -37 23 -.08 18 12 | --- --- --- ---
esx 130| 1 -1 8 48 -61 64 .51 32 25 | 112690 687 5460 10997
iac n/a| 1 1 -5 -57 10 -206 -.18 30 30 | 239427 995 5472 10764
mcc n/a| 3 -18 10 -11 90 571 .06 152 152 | --- --- --- ---
Table 2.1520.1 GPS week: 1520 Day: 1 MJD: 54885
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 0 -12 27 -29 -85 -.11 26 26 | 0 -157 2433 2493
cod 238| 0 0 8 16 -8 88 -.04 16 15 | --- --- --- ---
esx 130| -1 -1 10 -39 118 78 .32 31 28 | 115282 -2503 5746 11501
iac n/a| 0 0 -7 -24 -44 -104 -.04 20 20 | 235015 498 5739 9760
mcc n/a| 31 -20 -8 -218 181 1131 1.03 437 437 | --- --- --- ---
Table 2.1520.2 GPS week: 1520 Day: 2 MJD: 54886
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| 0 0 -3 3 -1 119 -.14 25 24 | 0 260 2476 2550
cod 238| -2 0 7 9 -13 24 -.09 21 20 | --- --- --- ---
esx 130| -2 -1 5 61 72 20 .35 32 27 | 113001 -4520 5363 12320
iac n/a| 3 0 -9 -69 8 -125 -.04 26 26 | 237604 -2295 5355 12022
mcc n/a| 27 -8 0 -469 327 1703 -.18 201 201 | --- --- --- ---
Table 2.1520.3 GPS week: 1520 Day: 3 MJD: 54887
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 3 -4 -9 23 -17 -.07 23 20 | 0 -19 1928 1985
cod 238| -1 0 0 32 -23 57 -.14 18 16 | --- --- --- ---
esx 130| 2 -3 -2 -7 7 -7 .49 32 31 | 121981 5199 4086 10409
iac n/a| -1 1 10 -41 53 -73 -.04 32 32 | 239557 4171 4132 9720
mcc n/a| 15 -13 80 -78 205 1038 -.36 209 209 | --- --- --- ---
Table 2.1520.4 GPS week: 1520 Day: 4 MJD: 54888
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| 0 0 -10 29 -14 -136 -.11 46 32 | 0 47 2180 2235
cod 238| 0 2 1 -40 -2 132 -.17 20 13 | --- --- --- ---
esx 130| 0 0 -4 7 7 -6 .28 31 25 | 122349 1149 6979 11951
iac n/a| 0 1 10 3 -32 -115 -.01 33 33 | 237772 -2535 6135 12496
mcc n/a| -21 0 54 59 -101 963 .12 202 202 | --- --- --- ---
Table 2.1520.5 GPS week: 1520 Day: 5 MJD: 54889
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| 0 0 -5 -25 -29 -365 -.24 28 24 | 0 -74 2661 2714
cod 238| -1 -2 0 -1 22 228 -.05 19 15 | --- --- --- ---
esx 130| 0 -2 -1 21 42 125 .31 31 26 | 124626 -5512 6041 12513
iac n/a| 0 3 10 -28 -34 -78 .04 32 32 | 1509960 319518 575543 999999
mcc n/a| -6 7 -2 -88 104 938 .03 103 103 | --- --- --- ---
Table 2.1520.6 GPS week: 1520 Day: 6 MJD: 54890
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| -2 0 1 31 -53 9 -.19 31 27 | 0 -59 2283 2332
cod 238| 1 -2 -4 2 -11 87 -.14 21 14 | --- --- --- ---
esx 130| -1 -2 0 10 42 16 .41 34 25 | 114029 -1803 5736 12789
iac n/a| -2 2 6 -45 -3 -193 .10 34 34 | 1778054 231226 670019 999999
mcc n/a| -10 0 0 -78 15 773 -.04 115 115 | --- --- --- ---
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 3.1520.0 GPS week: 1520 Day: 0 MJD: 54884
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 15 9 11 19 --- 7 | 24 27 33 24 --- 22
R03 |>>>>> 30 8 17 27 --- 12 | 24 39 52 40 --- 36
R04 |>>>>> 31 10 14 15 --- 10 | 24 24 23 29 --- 22
XR06 | ---- --- 42 --- 72 --- 54 | --- 173 --- 127 --- 151
R07 |>>>>> 15 12 19 12 --- 8 | 27 31 36 34 --- 30
R08 |>>>>> 25 14 26 23 --- 12 | 164 164 166 168 --- 164
R10 |>>>>> 15 16 15 24 --- 10 | 21 28 33 22 --- 22
R11 |>>>>> 19 14 20 18 107 10 | 23 24 31 26 189 20
R13 |>>>>> 22 11 20 21 --- 10 | 33 25 32 33 --- 24
R14 |>>>>> 20 9 16 18 --- 9 | 34 30 39 24 --- 29
R15 |>>>>> 23 20 33 33 187 15 | 25 29 44 36 64 25
R17 |>>>>> 51 22 55 29 --- 22 | 58 90 115 73 --- 77
R18E |>>>>> 47 25 50 35 --- 22 | 63 66 95 64 --- 67
R19E |>>>>> 22 15 29 45 --- 16 | 60 65 73 52 --- 59
R20E |>>>>> 26 13 20 40 --- 14 | 48 64 74 66 --- 60
R21E |>>>>> 63 36 66 55 --- 30 | 47 92 125 58 --- 75
R22E |>>>>> 20 16 30 25 --- 13 | 42 56 70 42 --- 47
R23E |>>>>> 27 26 38 41 --- 19 | 55 63 78 76 --- 62
XR24E | ---- --- 3 --- --- >>>> 0 | --- 121 --- --- 9999 121
------+------------------------------------+--------------------------------
RMS |>>>>> 31 18 32 30 152 |T 45 63 65 55 126 58
WRMS |>>>>> 26 12 25 30 152 |NE 24 58 36 50 --- 52
MEDI |>>>>> 23 14 20 25 187 |MD 34 56 52 40 64 47
Table 3.1520.1 GPS week: 1520 Day: 1 MJD: 54885
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 21 18 29 23 --- 13 | 21 32 40 20 --- 22
R03 |>>>>> 15 16 33 20 --- 12 | 35 30 42 43 --- 33
R04 |>>>>> 27 12 26 14 --- 11 | 41 44 35 33 --- 34
XR06 | ---- --- 61 --- 78 --- 69 | --- 175 --- 141 --- 152
R07 |>>>>> 29 9 20 20 --- 11 | 32 23 48 53 --- 34
R08 |>>>>> 19 13 29 17 --- 11 | 129 141 168 146 --- 144
R10 |>>>>> 16 14 26 16 --- 10 | 35 34 42 40 --- 34
R11 |>>>>> 25 17 25 16 437 11 | 34 34 47 26 235 32
R13 |>>>>> 22 8 23 19 --- 10 | 18 21 30 27 --- 18
R14 |>>>>> 20 15 18 25 --- 11 | 44 35 32 40 --- 33
XR15 |>>>>> --- 13 22 18 127 12 | --- 32 26 33 55 26
R17E |>>>>> 47 17 40 13 --- 16 | 42 51 71 47 --- 44
R18E |>>>>> 21 16 20 16 --- 10 | 44 48 45 29 --- 39
R19E |>>>>> 19 15 24 19 --- 10 | 25 38 44 31 --- 29
R20E |>>>>> 34 21 30 20 --- 14 | 28 58 49 65 --- 46
R21E |>>>>> 25 23 39 16 --- 14 | 35 55 74 41 --- 44
R22E |>>>>> 25 15 32 16 --- 12 | 28 44 62 36 --- 38
R23E |>>>>> 35 24 55 40 --- 21 | 80 98 123 96 --- 95
XR24E | ---- --- 24 --- 32 4906 28 | --- 53 --- 87 9999 62
------+------------------------------------+--------------------------------
RMS |>>>>> 26 16 31 20 437 |T 41 55 57 54 145 50
WRMS |>>>>> 26 15 28 20 437 |NE 32 60 41 58 --- 55
MEDI |>>>>> 22 16 26 19 437 |MD 35 44 45 40 55 34
Table 3.1520.2 GPS week: 1520 Day: 2 MJD: 54886
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 10 16 18 19 --- 9 | 33 24 34 34 --- 28
R03 |>>>>> 15 19 21 21 --- 11 | 30 39 35 36 --- 31
R04 |>>>>> 16 28 32 23 --- 14 | 14 21 32 31 --- 14
XR06 | ---- --- 85 --- 101 --- 93 | --- 277 --- 163 --- 211
R07 |>>>>> 13 11 21 18 --- 9 | 32 28 34 47 --- 32
R08M |>>>>> 14 22 33 15 --- 12 | 72 79 79 82 --- 75
R10 |>>>>> 15 11 26 22 --- 11 | 30 34 47 38 --- 34
R11 |>>>>> 28 24 32 22 265 15 | 17 24 47 33 198 22
R13M |>>>>> 35 9 32 21 --- 14 | 31 33 57 43 --- 35
R14M |>>>>> 29 18 27 13 --- 13 | 36 25 31 25 --- 23
R15M |>>>>> 36 25 37 19 105 17 | 44 21 57 24 66 25
R17E |>>>>> 24 16 41 22 --- 15 | 37 48 72 40 --- 43
R18E |>>>>> 30 18 41 26 --- 16 | 49 60 63 51 --- 49
R19E |>>>>> 15 16 17 24 --- 10 | 26 32 45 27 --- 29
R20E |>>>>> 36 28 39 57 --- 23 | 34 44 71 44 --- 40
R21E |>>>>> 27 20 19 19 --- 12 | 29 43 43 35 --- 34
R22E |>>>>> 23 24 25 24 --- 14 | 33 64 52 24 --- 41
R23E |>>>>> 31 30 51 39 --- 21 | 43 77 101 58 --- 64
XR24E | ---- --- 20 --- 22 566 21 | --- 72 --- 61 9999 76
------+------------------------------------+--------------------------------
RMS |>>>>> 25 21 32 26 201 |T 34 55 52 47 132 47
WRMS |>>>>> 24 20 27 26 201 |NE 27 77 33 62 --- 63
MEDI |>>>>> 24 20 32 22 265 |MD 33 39 47 38 66 34
Table 3.1520.3 GPS week: 1520 Day: 3 MJD: 54887
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 11 22 26 30 --- 13 | 28 32 51 42 --- 31
R03 |>>>>> 15 24 45 23 --- 16 | 29 34 64 45 --- 35
R04 |>>>>> 22 9 28 16 --- 11 | 37 38 61 62 --- 45
XR06 | 6857 250 42 --- 85 --- 60 | 109 138 --- 83 --- 109
R07 |>>>>> 10 8 21 22 --- 8 | 26 32 40 31 --- 28
R08 |>>>>> 26 14 43 31 --- 16 | 194 190 202 201 --- 194
R10M |>>>>> 21 15 13 20 --- 10 | 18 35 41 33 --- 29
R11M |>>>>> 20 14 29 26 246 12 | 37 35 44 43 206 34
R13M |>>>>> 16 8 21 25 --- 10 | 29 42 49 50 --- 39
R14M |>>>>> 17 8 33 16 --- 11 | 40 37 57 35 --- 39
R15M |>>>>> 19 12 37 17 164 12 | 35 37 45 33 123 33
R17E |>>>>> 27 15 20 36 --- 14 | 37 48 57 40 --- 41
R18E |>>>>> 22 15 43 39 --- 16 | 50 51 78 46 --- 50
R19E |>>>>> 29 19 45 29 --- 17 | 31 27 65 45 --- 32
R20E |>>>>> 31 17 35 60 --- 20 | 52 62 70 73 --- 57
R21E |>>>>> 19 15 38 40 --- 15 | 34 36 62 36 --- 35
R22E |>>>>> 24 27 27 43 --- 17 | 34 34 47 50 --- 32
R23E |>>>>> 43 37 21 39 --- 21 | 97 90 101 82 --- 88
XR24E | ---- --- 14 --- 26 432 19 | --- 93 --- 72 9999 87
------+------------------------------------+--------------------------------
RMS |>>>>> 23 18 32 32 209 |T 50 57 66 58 164 54
WRMS |>>>>> 20 16 31 32 209 |NE 45 54 54 52 --- 49
MEDI |>>>>> 21 15 29 29 246 |MD 35 37 57 45 123 39
Table 3.1520.4 GPS week: 1520 Day: 4 MJD: 54888
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 19 10 16 21 --- 9 | 34 37 51 38 --- 35
R03 |>>>>> 16 18 31 22 --- 13 | 39 36 52 34 --- 37
R04 |>>>>> 16 15 22 21 --- 10 | 24 15 31 26 --- 16
R06 |>>>>> 155 43 63 62 --- 48 | 67 109 50 90 --- 78
R07 |>>>>> 22 14 16 22 --- 10 | 45 29 39 36 --- 32
R08 |>>>>> 57 25 24 16 --- 18 | 109 153 153 142 --- 141
R10 |>>>>> 32 9 21 15 --- 11 | 27 28 42 38 --- 31
R11 |>>>>> 15 7 16 10 276 7 | 53 51 49 48 153 49
R13 |>>>>> 23 14 23 24 --- 12 | 20 35 50 35 --- 32
R14 |>>>>> 27 12 18 23 --- 11 | 27 41 52 36 --- 34
R15 |>>>>> 16 14 20 19 74 10 | 28 20 39 27 78 23
R17E |>>>>> 22 16 17 32 --- 12 | 32 47 57 60 --- 45
R18E |>>>>> 27 17 31 34 --- 15 | 51 67 76 62 --- 62
R19E |>>>>> 24 17 33 30 --- 14 | 32 32 58 34 --- 34
R20E |>>>>> 43 25 41 44 --- 21 | 24 28 70 52 --- 37
R21E |>>>>> 15 20 23 41 --- 15 | 34 35 58 46 --- 39
R22E |>>>>> 26 25 26 43 --- 17 | 29 39 47 36 --- 35
R23E |>>>>> 40 30 58 58 --- 26 | 45 36 76 48 --- 37
XR24E |19106 --- 21 --- 38 303 28 | --- 78 --- 72 9999 75
------+------------------------------------+--------------------------------
RMS |>>>>> 46 20 31 33 202 |T 40 48 58 50 115 45
WRMS |>>>>> 32 13 25 33 202 |NE 41 45 44 44 --- 39
MEDI |>>>>> 23 17 23 24 276 |MD 32 36 51 38 78 37
Table 3.1520.5 GPS week: 1520 Day: 5 MJD: 54889
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 20 11 28 34 --- 13 | 27 32 35 55 --- 31
R03 |>>>>> 24 19 29 29 --- 14 | 37 32 53 51 --- 37
R04 |>>>>> 14 10 15 14 --- 7 | 37 32 50 36 --- 36
R06 |>>>>> 34 16 42 28 --- 17 | 47 38 48 52 --- 34
R07 |>>>>> 19 14 21 20 --- 10 | 23 27 20 18 --- 17
R08 |>>>>> 61 27 38 27 --- 23 | 201 242 254 235 --- 231
R10 |>>>>> 22 16 21 17 --- 11 | 29 22 29 16 --- 18
R11 |>>>>> 16 16 25 18 143 11 | 39 39 54 41 115 39
R13 |>>>>> 15 14 24 22 --- 11 | 27 44 58 55 --- 42
R14 |>>>>> 23 14 26 20 --- 11 | 43 16 36 24 --- 21
R15 |>>>>> 16 12 25 23 32 11 | 40 33 50 42 38 40
R17E |>>>>> 43 24 51 39 --- 22 | 37 63 92 58 --- 56
R18E |>>>>> 28 24 31 41 --- 17 | 109 101 118 111 --- 107
R19E |>>>>> 24 18 30 33 --- 15 | 48 29 54 40 --- 36
R20E |>>>>> 38 29 40 47 --- 22 | 41 56 74 71 --- 52
R21E |>>>>> 25 22 23 36 --- 15 | 33 32 56 47 --- 36
R22E |>>>>> 15 26 29 50 --- 18 | 36 32 52 49 --- 35
R23E |>>>>> 30 23 36 46 --- 19 | 87 69 97 75 --- 76
XR24E | 4828 21 18 --- 31 443 16 | 21 59 --- 53 9999 58
------+------------------------------------+--------------------------------
RMS |>>>>> 28 19 31 32 103 |T 50 52 68 59 76 52
WRMS |>>>>> 24 15 26 32 103 |NE 34 32 41 42 --- 31
MEDI |>>>>> 23 18 28 29 143 |MD 37 33 53 51 38 37
Table 3.1520.6 GPS week: 1520 Day: 6 MJD: 54890
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 20 9 18 18 --- 9 | 28 32 41 24 --- 27
R03 |>>>>> 22 14 31 34 --- 14 | 31 31 49 37 --- 29
R04 |>>>>> 23 11 46 21 --- 15 | 32 23 47 34 --- 24
R06 |>>>>> 73 31 60 64 --- 32 | 93 61 54 81 --- 63
R07 |>>>>> 28 9 25 19 --- 12 | 42 34 39 27 --- 32
R08 |>>>>> 17 10 15 20 --- 9 | 245 255 253 244 --- 249
R10 |>>>>> 14 5 23 16 --- 8 | 28 19 31 26 --- 22
R11 |>>>>> 12 10 15 22 158 8 | 107 100 103 105 118 103
R13 |>>>>> 19 13 26 20 --- 11 | 33 28 39 31 --- 29
R14 |>>>>> 21 16 34 18 --- 13 | 41 30 48 25 --- 32
R15 |>>>>> 17 20 19 27 39 12 | 30 29 36 33 37 28
R17E |>>>>> 35 38 44 48 --- 23 | 45 73 62 56 --- 56
R18E |>>>>> 28 20 34 36 --- 16 | 64 64 81 61 --- 62
R19E |>>>>> 23 15 25 36 --- 14 | 41 33 49 43 --- 37
R20E |>>>>> 40 38 49 52 --- 25 | 50 56 75 68 --- 52
R21E |>>>>> 44 27 32 37 --- 20 | 42 45 58 51 --- 41
R22E |>>>>> 26 22 44 40 --- 19 | 44 37 52 56 --- 39
R23E |>>>>> 43 32 28 42 --- 21 | 82 81 88 87 --- 82
XR24E | 7443 36 26 --- 22 304 20 | 13 105 --- 83 9999 108
------+------------------------------------+--------------------------------
RMS |>>>>> 31 21 34 34 115 |T 57 59 66 61 77 58
WRMS |>>>>> 27 14 25 34 115 |NE 45 36 46 40 --- 35
MEDI |>>>>> 23 16 28 27 158 |MD 42 37 49 51 37 39
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