[IGSREPORT-17501] Wk 1534 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 18 05:03:21 PDT 2009
******************************************************************************
IGS Electronic Report 18 Jun 05:03:44 PDT 2009 Message Number 17501
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1534 (May 31, 2009 - Jun 06, 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 2.1534.
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:
igl1534[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1534 in the SP3 format.
igl15347.sum Combination Report for GPS Week 1534.
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 | 231.6 ns
1 | 236.7 ns
2 | 252.1 ns
3 | 245.4 ns
4 | 185.9 ns
5 | 166.8 ns
6 | 225.1 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
----+--------+---------------
4 | BKG | R07
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 1.1534, 1a.1534).
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 2.1534.0-6)
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 3.1534.0-6).
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 1534 summary. (May 31, 2009 - Jun 06, 2009)
Table 1.1534.a GPS week : 1534 MJD: 54982.0-54988.0
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 95| 1 0 -14 21 -18 98 .03 38 33 | 0 -1021 7039 8087
| 2 2 5 31 31 121 .44 | 0 4745
cod 231| -2 0 5 5 9 45 -.01 22 17 | --- --- --- ---
| 1 0 4 25 24 39 .06 | --- ---
esx 126| 0 0 11 7 27 65 .29 38 33 | 93131 -2086 8209 15953
| 2 1 6 43 40 89 .33 | 27482 10181
iac n/a| 1 0 -7 -21 -27 -190 -.15 32 32 | 226339 -925 8180 16588
| 2 1 8 31 31 56 .14 | 22223 10176
mcc n/a| 5 34 50 -153 164 -414 1.23 276 276 | --- --- --- ---
| 5 51 21 558 100 1894 .60 | --- ---
Table 1.1534.b GPS week : 1534 MJD: 54982.0-54988.0
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 | 15 18 13 13 13 10 15 |
R03 | 15 19 15 14 14 9 13 |
R06 | 29 24 51 22 25 31 40 |
R07 | 0 0 39 55 30 45 33 |
R08 | 14 11 12 14 14 13 17 |
R10 | 16 22 20 22 31 19 17 |
R11 | 21 14 15 17 21 24 13 |
R13 | 10 14 15 12 13 16 15 |
R14 | 16 13 14 20 22 15 16 |
R15 | 14 16 11 15 20 19 17 |
R17 | 18 17 15 19 15 16 17 |
R18 | 13 17 18 12 15 14 10 |
R19 | 11 10 14 15 15 18 14 |
R20 | 18 14 19 26 22 13 13 |
R21 | 13 12 12 15 15 13 12 |
R22 | 15 14 15 14 18 16 14 |
R23 | 25 27 34 31 18 25 29 |
Table 1.1534.c GPS week : 1534 MJD: 54982.0-54988.0
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 1534 0 | -200 -27 228 2520 -1760 -17760 86.6 3344 3344 | 231622 0
brd 1534 1 | 3 -128 313 1905 -2202 -21810 89.3 4510 4510 | 236742 0
brd 1534 2 | -15 -68 292 -768 -2296 -22690 90.5 3636 3636 | 252125 0
brd 1534 3 | 77 -85 367 -949 -851 -14430 86.6 3151 3151 | 245392 0
brd 1534 4 | -17 -177 295 1772 -2678 -16540 88.0 2294 2294 | 185941 0
brd 1534 5 | 80 43 197 -3845 1417 -19920 87.5 3087 3087 | 166777 0
brd 1534 6 | -46 55 404 -3181 -1056 -19010 83.7 3410 3410 | 225093 0
-------------+------------------------------------------------------------+----------------
brd 1534 mean| -17 -55 299 -363 -1346 -18880 87.5 3347 3347 | 220527 0
brd 1534 sdev| 94 85 72 2535 1387 2907 2.2 665 665 | 31908 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 2.1534.0 GPS week: 1534 Day: 0 MJD: 54982
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 95| 0 2 -15 51 -16 -83 -.53 39 34 | 0 -195 3679 4366
cod 231| -2 0 0 -13 31 85 -.03 15 12 | --- --- --- ---
esx 126| -1 3 14 -59 -13 132 .79 40 36 | 104567 -6871 6867 11197
iac n/a| 0 0 -2 8 -51 -213 -.04 35 35 | 232480 -2073 6979 10444
mcc n/a| -2 27 66 -1 44 129 1.58 270 270 | --- --- --- ---
Table 2.1534.1 GPS week: 1534 Day: 1 MJD: 54983
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 95| 0 3 -12 32 -51 83 -.34 37 38 | 0 245 5107 5927
cod 231| 0 0 7 3 37 22 .03 18 13 | --- --- --- ---
esx 126| 3 -1 17 -23 -19 60 .29 32 29 | 111886 -13500 6302 13255
iac n/a| -3 2 -16 -20 -75 -128 -.04 36 36 | 237373 -1248 6283 13940
mcc n/a| 7 -13 71 193 156 661 .64 232 232 | --- --- --- ---
Table 2.1534.2 GPS week: 1534 Day: 2 MJD: 54984
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 95| 0 -1 -10 -7 6 106 -.15 39 30 | 0 2025 4436 4960
cod 231| -4 0 7 41 8 27 .01 26 18 | --- --- --- ---
esx 126| 0 1 18 46 26 48 .42 41 33 | 116014 -9009 5519 20358
iac n/a| 3 0 -18 -56 -38 -232 -.16 40 40 | 248442 3722 5539 22211
mcc n/a| 6 17 36 173 290 776 .82 259 259 | --- --- --- ---
Table 2.1534.3 GPS week: 1534 Day: 3 MJD: 54985
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 95| 1 0 -24 38 33 247 .36 36 36 | 0 -11013 9740 10993
cod 231| -4 -1 14 -25 -19 3 .06 24 22 | --- --- --- ---
esx 126| -2 1 11 24 0 -82 -.03 33 27 | 103977 17910 13944 25255
iac n/a| 4 1 -14 -18 5 -192 -.14 33 33 | 242101 19246 13970 27634
Table 2.1534.4 GPS week: 1534 Day: 4 MJD: 54986
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 95| 3 -2 -17 59 -23 72 .78 39 34 | 0 -2519 10280 11637
cod 231| -2 0 3 -12 24 37 -.13 29 19 | --- --- --- ---
esx 126| -3 2 5 -24 41 168 .08 41 35 | 70995 -72 11049 15914
iac n/a| 0 0 0 20 -25 -115 -.24 25 25 | 208933 -8198 10986 16571
Table 2.1534.5 GPS week: 1534 Day: 5 MJD: 54987
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 95| 5 1 -8 -16 -55 11 .20 35 30 | 0 2954 9818 11720
cod 231| -3 -1 3 8 8 114 -.01 25 21 | --- --- --- ---
esx 126| -2 -1 0 55 79 137 -.10 41 36 | 40263 1326 6630 13355
iac n/a| 0 0 1 -18 -17 -172 -.01 26 26 | 184547 -11135 6588 13277
Table 2.1534.6 GPS week: 1534 Day: 6 MJD: 54988
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 95| 1 0 -15 -5 -22 254 -.09 40 31 | 0 1356 6216 7007
cod 231| -2 0 1 36 -25 29 .02 20 16 | --- --- --- ---
esx 126| -1 1 13 32 77 -8 .56 42 34 | 104217 -4389 7152 12340
iac n/a| 0 -2 -1 -67 14 -274 -.40 31 31 | 230500 -6790 6918 12041
mcc n/a| 9 107 27 -981 166 -3224 1.89 344 344 | --- --- --- ---
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 3.1534.0 GPS week: 1534 Day: 0 MJD: 54982
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2751 31 11 42 30 --- 15 | 22 26 50 39 --- 26
R03 | 7758 28 9 45 27 --- 14 | 56 54 43 64 --- 51
R06 | 7061 91 19 38 59 --- 28 | 129 81 79 74 --- 84
XR07 | ---- --- 5 --- --- --- 0 | --- 57 --- --- --- 58
R08 | 1417 28 15 25 34 142 13 | 20 24 35 39 10 21
R10E | 915 41 12 35 34 --- 16 | 68 83 101 92 --- 83
R11E | 692 29 20 69 32 --- 20 | 65 80 117 78 --- 78
R13E | 2605 22 12 25 18 --- 10 | 64 82 91 81 --- 78
R14E | 2167 28 15 51 21 --- 15 | 78 83 108 81 --- 83
R15E | 2421 31 10 33 32 354 14 | 51 59 66 52 37 53
R17 | 1008 26 17 38 51 --- 18 | 44 66 75 31 --- 52
R18 | 837 38 11 17 24 --- 12 | 49 76 72 76 --- 68
R19 | 3036 20 9 26 24 --- 10 | 49 53 64 41 --- 48
R20 | 4933 50 12 39 33 --- 17 | 58 47 71 55 --- 49
R21 | 1068 25 10 34 29 --- 13 | 50 67 79 67 --- 62
R22 | 1215 38 12 35 31 --- 15 | 43 79 99 68 --- 70
R23 | 1633 49 27 57 55 --- 25 | 46 46 82 98 --- 52
------+------------------------------------+--------------------------------
RMS | 3343 39 15 40 35 270 |T 55 62 77 64 23 59
WRMS | 3343 34 12 36 35 270 |NE 48 62 77 62 --- 57
MEDI | 1633 29 12 35 31 142 |MD 50 66 75 67 10 58
Table 3.1534.1 GPS week: 1534 Day: 1 MJD: 54983
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1286 43 14 35 40 --- 18 | 19 28 47 35 --- 25
R03 | 6503 60 13 31 30 --- 19 | 36 60 81 52 --- 56
R06 |14461 46 35 54 32 --- 23 | 83 101 87 94 --- 85
XR07 | ---- --- 5 --- --- --- 0 | --- 101 --- --- --- 98
R08 | 1361 29 14 12 19 120 10 | 18 28 28 25 13 21
R10E | 1564 33 28 50 40 --- 21 | 77 68 111 115 --- 84
R11E | 923 38 12 26 24 --- 13 | 57 64 68 55 --- 59
R13E | 4073 36 14 29 24 --- 14 | 61 78 91 85 --- 76
R14E | 3964 22 17 23 27 --- 12 | 45 55 64 53 --- 52
R15E | 891 24 17 26 45 305 16 | 29 37 35 38 34 29
R17 | 1478 18 22 39 38 --- 17 | 41 51 50 36 --- 40
R18 | 1246 53 16 33 21 --- 17 | 35 59 84 57 --- 56
R19 | 2324 21 10 25 14 --- 10 | 42 38 40 44 --- 36
R20 | 4360 32 11 20 32 --- 13 | 45 41 65 51 --- 47
R21 | 1135 29 13 25 20 --- 12 | 37 43 65 53 --- 47
R22 | 874 40 13 27 19 --- 14 | 29 53 61 47 --- 48
R23 | 1975 44 20 21 85 --- 26 | 24 25 38 89 --- 29
------+------------------------------------+--------------------------------
RMS | 4510 37 18 32 36 232 |T 42 54 63 58 23 52
WRMS | 4510 38 13 29 36 232 |NE 36 44 57 53 --- 43
MEDI | 1478 33 14 26 27 120 |MD 37 53 64 52 13 48
Table 3.1534.2 GPS week: 1534 Day: 2 MJD: 54984
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1579 23 15 13 36 --- 13 | 13 18 39 47 --- 22
R03 | 6582 30 19 25 31 --- 15 | 63 80 81 87 --- 75
R06 | 9977 112 71 76 98 --- 51 | 128 240 235 187 --- 191
XR07 | ---- --- 30 --- 49 --- 39 | --- 94 --- 46 --- 74
R08 | 1309 21 10 30 20 129 11 | 20 21 46 26 10 22
R10E | 1384 35 27 40 37 --- 19 | 56 62 77 72 --- 59
R11E | 1458 24 22 23 32 --- 14 | 65 67 75 58 --- 63
R13E | 2652 28 16 28 31 --- 14 | 42 53 73 69 --- 54
R14E | 5252 24 21 16 31 --- 13 | 65 58 62 63 --- 58
R15E | 861 16 17 19 20 343 10 | 43 50 42 36 37 40
R17 | 1751 10 24 30 34 --- 15 | 40 54 56 35 --- 44
R18 | 1516 38 19 33 32 --- 17 | 39 47 56 63 --- 45
R19 | 1769 12 13 37 29 --- 13 | 39 35 60 38 --- 35
R20 | 3030 33 20 36 41 --- 18 | 21 28 35 30 --- 24
R21 | 1175 21 10 31 21 --- 12 | 42 52 77 38 --- 49
R22 | 1037 34 20 30 19 --- 15 | 23 57 68 29 --- 42
R23 | 2214 49 34 96 55 --- 34 | 25 30 111 64 --- 41
------+------------------------------------+--------------------------------
RMS | 3636 39 26 41 40 259 |T 45 61 74 58 23 55
WRMS | 3636 30 18 33 40 259 |NE 32 43 66 42 --- 40
MEDI | 1579 24 20 30 32 129 |MD 40 53 62 47 10 45
Table 3.1534.3 GPS week: 1534 Day: 3 MJD: 54985
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R02 | 1587 29 15 18 26 13 | 28 22 34 40 24
R03 | 5358 27 17 16 34 14 | 50 37 42 60 42
R06 | 7555 45 32 33 42 21 | 152 195 178 206 182
XR07E | 8861 --- 47 --- 63 54 | --- 93 --- 42 68
R08 | 2058 22 20 30 26 14 | 22 22 38 33 20
R10E | 1264 30 45 39 30 21 | 68 93 93 93 81
R11E | 1590 30 24 31 31 16 | 86 95 92 75 86
R13E | 2983 27 14 17 23 11 | 74 86 86 93 83
R14E | 4728 52 24 26 34 19 | 91 97 108 108 96
R15E | 1146 36 20 20 25 14 | 37 59 67 47 51
R17 | 1609 11 32 21 49 18 | 51 66 64 27 52
R18 | 2034 24 21 17 21 12 | 31 56 45 39 39
R19 | 1425 30 15 32 25 14 | 38 55 73 46 49
R20 | 1721 40 27 67 39 25 | 37 34 93 51 45
R21 | 1675 14 17 31 36 15 | 62 60 51 79 60
R22 | 1859 28 16 31 20 14 | 41 69 83 50 60
R23 | 3402 79 24 54 53 30 | 38 45 95 93 61
------+-------------------------------+---------------------------
RMS | 3150 36 24 33 33 |T 56 69 77 69 64
WRMS | 3150 36 22 27 33 |NE 42 55 72 55 52
MEDI | 1859 29 21 30 31 |MD 41 60 73 51 60
Table 3.1534.4 GPS week: 1534 Day: 4 MJD: 54986
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R02 | 1654 37 13 20 20 13 | 20 21 34 36 23
R03 | 3453 30 18 24 24 13 | 35 42 59 42 39
R06 | 3835 42 41 50 43 25 | 111 152 148 114 127
XR07E | 2572 305 32 --- 26 29 | 98 62 --- 36 54
R08 | 2094 34 15 23 22 13 | 22 24 36 37 23
R10E | 1812 36 69 67 29 30 | 50 95 83 55 58
R11E | 1091 60 31 39 14 21 | 57 86 106 83 78
R13E | 1847 34 18 26 16 13 | 60 81 81 71 71
R14E | 3464 65 30 37 19 22 | 49 89 109 77 76
R15E | 1134 49 31 31 27 19 | 53 72 72 51 54
R17 | 1349 21 25 18 29 14 | 45 40 36 36 36
R18 | 2805 12 13 46 23 14 | 39 27 64 34 31
R19 | 1168 18 11 50 20 15 | 36 35 65 47 37
R20 | 1408 32 33 56 34 22 | 31 28 66 47 30
R21 | 1845 28 14 45 14 14 | 38 41 77 42 45
R22 | 2127 42 20 40 23 17 | 29 59 55 66 48
R23 | 2882 36 21 45 26 18 | 62 60 89 74 65
------+-------------------------------+---------------------------
RMS | 2294 39 29 41 25 |T 49 59 73 55 52
WRMS | 2294 34 19 35 25 |NE 40 41 64 49 41
MEDI | 1847 36 21 39 23 |MD 45 59 66 47 48
Table 3.1534.5 GPS week: 1534 Day: 5 MJD: 54987
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac IGL | bkg cod esx iac IGL
------+-------------------------------+---------------------------
R02 | 2362 19 15 24 12 10 | 25 22 23 25 17
R03 | 4642 16 10 19 16 8 | 38 22 33 38 28
R06E | 7654 76 50 48 40 31 | 87 124 115 95 92
XR07E | 4397 91 33 --- 64 44 | 83 66 --- 48 55
R08 | 1481 34 10 33 16 13 | 35 21 34 23 22
R10 | 3600 45 31 32 23 19 | 75 78 75 72 71
R11 | 1828 46 39 38 41 23 | 68 104 101 76 81
R13 | 1775 28 16 48 21 16 | 73 91 106 78 82
R14 | 3422 27 27 34 18 15 | 73 90 95 96 86
R15 | 1833 39 26 42 26 18 | 40 60 69 44 46
R17 | 2008 24 19 47 23 15 | 41 37 59 31 34
R18 | 2127 23 12 42 23 14 | 35 25 45 36 25
R19 | 1222 20 24 36 37 17 | 28 49 69 32 37
R20 | 1230 22 18 32 20 13 | 40 49 61 39 43
R21 | 2050 24 14 39 16 13 | 39 52 61 40 43
R22 | 2687 31 14 54 15 16 | 34 33 70 41 34
R23 | 2656 41 36 64 37 25 | 35 35 110 55 48
------+-------------------------------+---------------------------
RMS | 3087 35 25 41 26 |T 49 56 70 51 49
WRMS | 3087 30 21 36 26 |NE 36 40 67 39 37
MEDI | 2127 28 19 38 23 |MD 40 49 69 41 43
Table 3.1534.6 GPS week: 1534 Day: 6 MJD: 54988
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1610 31 23 22 27 --- 15 | 41 22 29 44 --- 22
R03E | 5883 21 16 25 25 --- 12 | 27 29 29 35 --- 21
R06E | 9961 113 46 81 44 --- 40 | 121 119 134 112 --- 108
XR07E | 2588 29 35 --- 68 --- 33 | 47 77 --- 61 --- 69
R08E | 1099 31 16 39 35 --- 16 | 25 33 55 45 --- 27
R10 | 2506 46 12 41 19 --- 16 | 77 78 74 67 --- 72
R11 | 1005 24 9 23 32 344 12 | 68 79 85 78 8 76
R13 | 1688 24 14 44 24 --- 14 | 83 91 91 95 --- 89
R14 | 2265 30 17 39 30 --- 15 | 73 67 90 69 --- 71
R15 | 1633 47 15 25 33 --- 17 | 29 34 44 31 --- 30
R17 | 3655 35 14 35 35 --- 16 | 46 65 72 42 --- 54
R18 | 1193 20 11 25 14 --- 9 | 37 58 63 50 --- 52
R19 | 1119 12 20 42 21 --- 14 | 38 59 70 47 --- 50
R20 | 1022 30 9 30 22 --- 12 | 50 48 70 51 --- 49
R21 | 2170 26 15 31 14 --- 12 | 51 66 74 54 --- 60
R22 | 2330 20 21 27 30 --- 14 | 55 73 70 58 --- 62
R23 | 1788 32 30 82 57 --- 28 | 58 35 107 87 --- 51
------+------------------------------------+--------------------------------
RMS | 3409 40 20 42 31 344 |T 54 60 72 60 8 56
WRMS | 3409 31 16 34 31 344 |NE 47 57 75 55 --- 54
MEDI | 1788 30 16 31 30 344 |MD 50 65 70 54 8 54
More information about the IGSREPORT
mailing list