[IGSREPORT-17529] Wk 1535 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 25 06:00:53 PDT 2009
******************************************************************************
IGS Electronic Report 25 Jun 06:01:15 PDT 2009 Message Number 17529
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1535 (Jun 07, 2009 - Jun 13, 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 2.1535.
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:
igl1535[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1535 in the SP3 format.
igl15357.sum Combination Report for GPS Week 1535.
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 | 226.3 ns
1 | 222.0 ns
2 | 222.9 ns
3 | 221.3 ns
4 | 216.1 ns
5 | 206.2 ns
6 | 213.7 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
----+--------+---------------
6 | ESX | 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 1.1535, 1a.1535).
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 2.1535.0-6)
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 3.1535.0-6).
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 1535 summary. (Jun 07, 2009 - Jun 13, 2009)
Table 1.1535.a GPS week : 1535 MJD: 54989.0-54995.0
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 97| 0 0 -20 1 -1 -7 .03 41 36 | 0 -790 5248 6051
| 1 1 4 40 37 144 .14 | 0 597
cod 233| -2 0 0 1 -10 78 -.12 20 16 | --- --- --- ---
| 0 2 4 14 15 64 .04 | --- ---
esx 122| 2 0 6 -17 64 21 .33 35 28 | 103617 481 6465 12067
| 2 3 4 38 29 65 .14 | 7290 6456
iac n/a| 0 1 9 0 -27 -146 -.14 35 35 | 217804 -1266 6372 11466
| 1 2 10 27 25 18 .08 | 6391 2821
mcc n/a| -8 3 34 -59 -46 418 .59 264 264 | --- --- --- ---
| 22 10 19 200 152 683 .58 | --- ---
Table 1.1535.b GPS week : 1535 MJD: 54989.0-54995.0
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 12 11 11 11 12 19 |
R03 | 13 12 17 14 13 16 12 |
R06 | 29 16 27 19 23 22 133 |
R07 | 32 31 35 17 18 21 30 |
R08 | 20 11 12 13 16 15 20 |
R10 | 15 20 18 15 12 17 13 |
R11 | 9 14 13 15 9 12 7 |
R13 | 10 11 9 11 15 12 12 |
R14 | 15 13 11 12 10 15 11 |
R15 | 15 16 12 11 17 24 20 |
R17 | 19 22 20 13 15 21 14 |
R18 | 16 18 18 15 16 13 13 |
R19 | 13 15 12 15 11 14 10 |
R20 | 18 18 17 12 18 23 14 |
R21 | 12 12 12 14 17 15 14 |
R22 | 10 11 15 15 13 13 20 |
R23 | 25 20 29 82 36 19 17 |
R24 | --- 0 0 154 80 115 227 |
Table 1.1535.c GPS week : 1535 MJD: 54989.0-54995.0
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 1535 0 | 152 70 494 -1444 5724 -17860 85.6 3565 3565 | 226276 0
brd 1535 1 | 24 -64 537 -421 1695 -19040 88.5 4011 4011 | 221970 0
brd 1535 2 | 51 -1 488 1463 499 -17540 88.3 4155 4155 | 222900 0
brd 1535 3 | -9 -19 485 -441 2636 -21590 87.7 4673 4673 | 221348 0
brd 1535 4 | -91 73 464 1932 505 -22240 87.7 3322 3322 | 216068 0
brd 1535 5 | -20 142 438 -295 -736 -25460 88.9 4470 4470 | 206221 0
brd 1535 6 | -95 30 466 -572 693 -19460 87.8 3015 3015 | 213692 0
-------------+------------------------------------------------------------+----------------
brd 1535 mean| 1 33 482 31 1573 -20455 87.8 3887 3887 | 218353 0
brd 1535 sdev| 86 68 31 1206 2112 2820 1.1 609 609 | 6826 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 2.1535.0 GPS week: 1535 Day: 0 MJD: 54989
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 97| 0 1 -15 5 -46 94 .25 43 41 | 0 -1000 5187 6046
cod 233| -3 1 4 -15 -5 2 -.13 20 16 | --- --- --- ---
esx 122| 0 0 5 -31 96 68 .25 33 28 | 104953 72 6407 10601
iac n/a| -3 -1 0 12 -1 -153 -.20 31 31 | 224960 -3289 6033 9784
mcc n/a| -45 13 24 -68 21 1467 1.41 440 440 | --- --- --- ---
Table 2.1535.1 GPS week: 1535 Day: 1 MJD: 54990
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 97| 0 0 -24 47 -37 0 .06 33 33 | 0 -1507 4393 4951
cod 233| -3 0 4 19 8 85 -.16 15 13 | --- --- --- ---
esx 122| 0 -4 8 -75 58 -42 .37 34 29 | 111770 2840 5826 11340
iac n/a| -1 0 4 16 -10 -162 -.24 40 40 | 221374 582 5726 11762
mcc n/a| -22 -13 4 -72 -144 689 .10 303 303 | --- --- --- ---
Table 2.1535.2 GPS week: 1535 Day: 2 MJD: 54991
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 97| -3 1 -18 -11 -13 45 .06 38 37 | 0 123 4993 5800
cod 233| -2 0 3 5 -6 91 -.05 22 17 | --- --- --- ---
esx 122| 5 0 10 -1 28 -3 .25 31 23 | 106447 -6518 5846 10839
iac n/a| 0 1 -2 -31 -19 -168 -.06 39 39 | 224381 -3262 5840 10704
mcc n/a| 7 7 50 -382 4 562 .21 243 243 | --- --- --- ---
Table 2.1535.3 GPS week: 1535 Day: 3 MJD: 54992
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 97| 0 1 -19 -70 63 72 .12 57 28 | 0 -1077 5297 5993
cod 233| -3 -3 -1 -3 -26 33 -.09 28 13 | --- --- --- ---
esx 122| 2 3 10 17 28 59 .18 53 31 | 106144 4659 7187 12955
iac n/a| 0 1 9 49 -55 -154 -.04 37 37 | 219859 3123 7205 13368
mcc n/a| 11 -10 15 266 -5 904 -.10 92 92 | --- --- --- ---
Table 2.1535.4 GPS week: 1535 Day: 4 MJD: 54993
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 97| 0 0 -26 25 12 109 -.06 44 35 | 0 -1265 4273 5012
cod 233| -1 -2 -6 22 4 28 -.16 15 13 | --- --- --- ---
esx 122| -2 3 10 -53 103 -38 .51 34 28 | 90347 8322 5884 10002
iac n/a| 1 3 16 -23 -66 -116 -.10 35 35 | 213388 -11 5866 9648
mcc n/a| 0 12 42 9 83 -441 .96 254 254 | --- --- --- ---
Table 2.1535.5 GPS week: 1535 Day: 5 MJD: 54994
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 97| 1 -1 -20 36 -9 -67 -.02 35 34 | 0 -136 5090 5580
cod 233| -1 2 -4 -9 -10 113 -.08 19 22 | --- --- --- ---
esx 122| 2 -3 0 -5 71 -19 .23 33 32 | 97401 3788 6338 13887
iac n/a| 0 0 26 -14 -33 -142 -.17 36 36 | 209204 -838 6361 13996
mcc n/a| 16 10 45 21 68 -271 1.15 244 244 | --- --- --- ---
Table 2.1535.6 GPS week: 1535 Day: 6 MJD: 54995
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 97| 2 -1 -14 -20 20 -306 -.20 39 41 | 0 -668 7505 8976
cod 233| -4 -1 -3 -9 -35 193 -.13 20 16 | --- --- --- ---
esx 122| 5 3 1 30 63 129 .54 31 26 | 108261 -9792 7770 14847
iac n/a| 0 4 13 -1 -3 -128 -.19 25 25 | 211463 -5170 7573 11001
mcc n/a| -25 4 55 -190 -349 22 .39 271 271 | --- --- --- ---
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 3.1535.0 GPS week: 1535 Day: 0 MJD: 54989
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2271 25 14 25 19 --- 11 | 39 46 54 36 --- 41
R03E | 2071 30 13 28 26 --- 13 | 40 56 63 43 --- 50
R06E |12584 85 38 52 28 --- 29 | 76 101 99 82 --- 107
R07E | 3216 100 22 51 50 --- 31 | 29 52 62 52 --- 38
R08E | 927 49 17 35 41 610 19 | 52 45 59 41 292 44
R10 | 1554 34 16 37 22 --- 15 | 47 54 58 58 --- 51
R11 | 1433 22 9 19 17 325 9 | 23 35 41 28 37 31
R13 | 1586 19 10 24 18 --- 10 | 21 19 36 23 --- 17
R14 | 1699 34 21 29 18 --- 14 | 35 28 42 24 --- 24
R15 | 1403 39 13 21 30 319 14 | 30 35 32 45 111 32
R17 | 3210 27 24 52 25 --- 18 | 45 58 73 38 --- 47
R18 | 1361 33 21 34 26 --- 16 | 54 63 73 47 --- 56
R19 | 1047 16 19 27 23 --- 12 | 44 63 64 54 --- 55
R20 | 1149 35 19 30 43 --- 18 | 51 55 66 69 --- 55
R21 | 1940 30 10 23 22 --- 12 | 48 67 86 72 --- 67
R22 | 1734 14 12 20 22 --- 9 | 39 60 67 53 --- 55
R23 | 1947 42 36 26 62 --- 25 | 208 237 260 236 --- 234
------+------------------------------------+--------------------------------
RMS | 3564 43 20 33 31 439 |T 51 63 72 58 146 59
WRMS | 3564 41 16 28 31 439 |NE 53 64 74 62 74 60
MEDI | 1699 33 17 28 25 325 |MD 44 55 63 47 111 50
Table 3.1535.1 GPS week: 1535 Day: 1 MJD: 54990
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2276 17 16 23 33 --- 12 | 22 25 35 30 --- 21
R03E | 2586 22 14 25 23 --- 11 | 28 45 49 29 --- 35
R06E |14567 33 9 41 31 --- 16 | 34 90 100 76 --- 92
R07E | 2994 74 21 36 85 --- 30 | 43 46 37 50 --- 34
R08E | 1467 23 11 20 28 388 11 | 32 32 39 23 87 27
R10 | 1356 31 20 50 46 --- 20 | 52 72 49 62 --- 54
R11 | 1732 33 12 30 26 309 14 | 26 31 49 24 28 29
R13 | 1652 18 9 16 32 --- 10 | 15 18 27 25 --- 16
R14 | 3194 24 15 30 23 --- 12 | 28 24 42 25 --- 22
R15 | 1132 33 13 22 44 174 15 | 18 31 28 37 25 24
R17 | 2628 36 16 58 49 --- 21 | 35 40 88 32 --- 41
R18 | 2240 28 19 50 29 --- 17 | 34 51 52 45 --- 35
R19 | 863 31 11 40 18 --- 14 | 20 39 78 32 --- 40
R20 | 829 34 12 25 54 --- 17 | 28 45 62 55 --- 42
R21 | 1135 27 11 25 27 --- 12 | 33 41 40 45 --- 35
R22 | 1403 18 18 21 23 --- 11 | 18 42 40 19 --- 29
R23 | 1626 41 24 29 51 --- 20 | 292 308 339 302 --- 310
XR24 | ---- --- 6 --- --- --- 0 | --- 103 --- --- --- 109
------+------------------------------------+--------------------------------
RMS | 4011 33 15 34 40 303 |T 44 60 67 53 46 55
WRMS | 4011 33 13 29 40 303 |NE 49 65 74 58 26 60
MEDI | 1652 31 13 29 31 309 |MD 28 41 49 32 28 35
Table 3.1535.2 GPS week: 1535 Day: 2 MJD: 54991
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 985 19 13 20 26 --- 11 | 41 43 50 43 --- 40
R03E | 8365 30 24 27 41 --- 17 | 22 41 52 32 --- 32
R06E |13697 69 25 50 48 --- 27 | 30 89 78 52 --- 84
R07E | 2647 74 30 49 91 --- 35 | 48 42 59 53 --- 35
R08E | 1356 22 16 25 20 335 12 | 37 32 51 27 146 31
R10 | 1174 28 26 40 25 --- 17 | 37 52 50 59 --- 44
R11 | 1102 36 14 20 22 236 13 | 37 46 61 53 36 47
R13 | 1422 21 15 11 18 --- 9 | 21 21 31 19 --- 18
R14 | 2261 24 13 21 21 --- 11 | 28 37 44 24 --- 30
R15 | 1235 32 11 15 25 91 12 | 26 35 34 39 29 31
R17 | 1886 28 23 33 52 --- 19 | 34 57 69 30 --- 42
R18 | 2290 38 16 38 35 --- 18 | 25 43 81 55 --- 49
R19 | 710 23 14 27 15 --- 11 | 48 47 28 34 --- 37
R20 | 936 33 17 32 36 --- 16 | 44 57 76 57 --- 58
R21 | 903 22 15 29 14 --- 11 | 37 54 50 50 --- 45
R22 | 1196 30 27 22 22 --- 15 | 23 47 29 39 --- 30
R23 | 1557 60 43 32 67 --- 29 | 247 257 234 254 --- 246
XR24 | ---- --- 6 --- --- --- 0 | --- 73 --- --- --- 82
------+------------------------------------+--------------------------------
RMS | 4155 38 22 31 39 243 |T 46 59 63 54 70 54
WRMS | 4155 37 17 23 39 243 |NE 50 63 65 59 32 58
MEDI | 1356 30 16 27 25 236 |MD 37 46 51 43 36 40
Table 3.1535.3 GPS week: 1535 Day: 3 MJD: 54992
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1055 22 12 27 20 --- 11 | 33 43 47 26 --- 32
R03E | 8711 21 16 35 26 --- 13 | 32 38 51 29 --- 30
R06E |11003 30 28 47 30 --- 18 | 35 86 73 42 --- 76
R07E | 2368 30 19 29 37 --- 16 | 25 43 55 46 --- 35
R08E | 1594 16 12 32 29 --- 12 | 35 30 57 31 --- 31
R10 | 1302 31 16 41 24 --- 15 | 43 61 78 49 --- 54
R11 | 1053 42 12 16 32 80 15 | 35 35 51 48 91 39
R13 | 1837 19 13 25 24 --- 11 | 15 23 42 29 --- 21
R14 | 825 24 10 21 25 --- 11 | 19 31 41 29 --- 26
R15 | 2161 22 13 26 21 102 11 | 18 27 45 39 41 28
R17 | 1035 23 12 27 28 --- 12 | 39 56 65 59 --- 52
R18 | 1650 36 10 33 30 --- 15 | 24 50 68 44 --- 45
R19 | 1064 25 14 50 18 --- 14 | 29 35 83 54 --- 43
R20 | 1046 16 13 33 24 --- 12 | 52 55 51 73 --- 56
R21 | 913 26 18 33 21 --- 13 | 58 74 92 79 --- 73
R22 | 1417 35 6 44 21 --- 14 | 38 61 82 69 --- 59
R23 |12024 210 100 174 112 --- 82 | 440 614 652 495 --- 551
XR24 | ---- 230 103 --- --- --- 154 | 236 145 --- --- --- 187
------+------------------------------------+--------------------------------
RMS | 4672 57 28 53 37 92 |T 67 83 96 73 66 79
WRMS | 4672 28 13 31 37 92 |NE 80 97 112 88 66 94
MEDI | 1417 25 13 33 25 80 |MD 35 43 57 46 41 43
Table 3.1535.4 GPS week: 1535 Day: 4 MJD: 54993
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1407 21 13 20 28 --- 11 | 33 53 45 56 --- 45
R03E | 6351 26 14 29 27 --- 13 | 21 36 56 35 --- 33
R06E |10029 48 17 57 47 --- 23 | 25 94 73 53 --- 90
R07E | 3231 58 12 24 37 --- 18 | 45 41 51 38 --- 36
R08E | 1576 19 15 34 41 239 15 | 24 35 44 41 153 29
R10 | 1265 24 11 32 17 --- 11 | 40 31 51 43 --- 36
R11 | 1281 24 11 12 17 349 8 | 40 42 46 41 136 41
R13 | 2269 39 10 32 28 --- 14 | 24 32 45 18 --- 25
R14 | 1324 21 10 20 22 --- 10 | 25 29 44 22 --- 26
R15 | 2755 58 12 33 22 123 17 | 22 21 40 28 29 19
R17 | 1530 32 17 21 40 --- 15 | 19 42 51 57 --- 41
R18 | 990 42 9 42 25 --- 16 | 22 40 70 26 --- 38
R19 | 942 28 9 26 17 --- 11 | 35 41 69 65 --- 49
R20 | 1020 29 19 44 40 --- 18 | 30 43 75 66 --- 47
R21 | 1128 33 25 29 35 --- 17 | 43 80 60 81 --- 68
R22 | 1481 27 13 26 28 --- 12 | 36 61 81 62 --- 60
R23 | 2308 117 24 57 71 --- 36 | 228 281 290 269 --- 265
XR24 | ---- 138 48 --- --- --- 80 | 108 148 --- --- --- 133
------+------------------------------------+--------------------------------
RMS | 3322 44 15 34 35 254 |T 45 63 70 58 106 60
WRMS | 3322 35 13 28 35 254 |NE 51 68 76 64 82 65
MEDI | 1481 29 13 29 28 239 |MD 30 41 51 43 136 41
Table 3.1535.5 GPS week: 1535 Day: 5 MJD: 54994
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1227 15 10 30 26 --- 12 | 46 40 46 33 --- 38
R03E | 9088 27 15 36 36 --- 16 | 18 26 43 40 --- 23
R06E |13010 48 24 37 46 --- 21 | 47 191 78 55 --- 195
R07E | 4539 49 26 34 41 --- 21 | 27 35 46 31 --- 23
R08E | 1740 22 19 28 35 288 14 | 32 34 42 34 55 30
R10 | 1367 41 19 32 30 --- 17 | 29 43 54 46 --- 39
R11 | 2094 17 14 32 22 272 12 | 31 34 55 42 54 36
R13 | 1994 26 11 27 15 --- 11 | 20 20 32 17 --- 17
R14 | 2082 22 17 32 31 --- 14 | 24 31 47 20 --- 24
R15 | 2917 66 24 45 29 150 23 | 14 21 40 23 33 15
R17 | 1833 20 32 38 49 --- 21 | 12 24 37 19 --- 14
R18 | 864 30 13 25 25 --- 13 | 13 22 34 30 --- 20
R19 | 846 29 19 22 30 --- 14 | 15 43 45 22 --- 30
R20 | 1661 30 21 38 68 --- 23 | 19 38 34 76 --- 34
R21 | 1653 34 18 35 18 --- 15 | 25 45 71 41 --- 42
R22 | 1737 28 11 32 20 --- 13 | 52 40 43 61 --- 42
R23 | 5127 40 16 20 52 --- 19 | 308 339 351 304 --- 327
XR24 | 8033 159 85 --- --- --- 115 | 145 168 --- --- --- 138
------+------------------------------------+--------------------------------
RMS | 4470 35 19 33 36 244 |T 48 66 64 52 47 60
WRMS | 4470 34 22 32 36 244 |NE 54 66 70 58 43 59
MEDI | 1833 29 18 32 30 272 |MD 25 35 45 34 54 30
Table 3.1535.6 GPS week: 1535 Day: 6 MJD: 54995
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2493 50 22 40 21 --- 18 | 33 38 44 37 --- 30
R03E | 8605 20 17 17 26 --- 11 | 38 34 51 38 --- 36
XR06E | 8998 --- 66 666 188 --- 132 | --- 489 105 36 --- 459
R07E | 2961 89 42 39 39 --- 30 | 24 42 52 41 --- 31
R08E | 1377 57 18 25 36 360 19 | 35 36 48 47 68 35
R10 | 1111 37 16 23 16 --- 13 | 44 49 53 44 --- 43
R11 | 1166 17 9 11 12 246 7 | 37 36 39 41 66 36
R13 | 1303 22 13 22 26 --- 12 | 24 26 26 25 --- 21
R14 | 2281 17 14 16 26 --- 11 | 27 34 35 29 --- 29
R15 | 1415 56 24 35 23 173 19 | 21 37 40 31 31 27
R17 | 1424 27 21 25 26 --- 14 | 33 55 45 41 --- 43
R18 | 975 35 13 16 26 --- 13 | 36 48 59 46 --- 45
R19 | 823 11 14 14 25 --- 10 | 41 48 54 46 --- 44
R20 | 2858 29 18 34 16 --- 14 | 37 47 77 77 --- 55
R21 | 1811 19 16 36 25 --- 14 | 56 78 95 76 --- 74
R22 | 818 27 25 55 25 --- 19 | 49 62 95 74 --- 65
R23 | 5214 24 20 47 21 --- 16 | 251 276 279 275 --- 269
XR24 | 8337 326 158 --- --- --- 227 | 202 123 --- --- --- 124
------+------------------------------------+--------------------------------
RMS | 3014 39 20 31 25 271 |T 58 86 70 59 55 81
WRMS | 3014 41 16 26 25 271 |NE 66 70 74 67 48 67
MEDI | 1424 27 18 25 25 246 |MD 37 47 52 41 66 43
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