[IGSREPORT-18145] Wk 1562 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 31 05:21:02 PST 2009
******************************************************************************
IGS Electronic Report 31 Dec 05:21:26 PST 2009 Message Number 18145
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1562 (Dec 13, 2009 - Dec 19, 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 2.1562.
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:
igl1562[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1562 in the SP3 format.
igl15627.sum Combination Report for GPS Week 1562.
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 | 521.6 ns
1 | 526.6 ns
2 | 514.2 ns
3 | 531.4 ns
4 | 520.8 ns
5 | 459.1 ns
6 | 536.6 ns
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 1.1562, 1a.1562).
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 2.1562.0-6)
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 3.1562.0-6).
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 1562 summary. (Dec 13, 2009 - Dec 19, 2009)
Table 1.1562.a GPS week : 1562 MJD: 55178.0-55184.0
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 127| 2 0 10 34 14 -63 -.19 37 36 | 0 74 2320 2530
| 1 1 2 33 65 110 .07 | 0 517
cod 240| -2 0 -3 42 13 74 -.16 16 13 | --- --- --- ---
| 1 2 2 17 31 57 .04 | --- ---
esx 125| 0 -1 -3 -67 -4 -10 .35 22 21 | 140198 -446 4434 10770
| 1 2 2 36 29 48 .04 | 27835 2276
iac n/a| 3 0 8 -4 -9 -80 -.11 38 38 | 516323 -1078 4439 9175
| 2 2 3 22 31 57 .09 | 26369 1315
mcc n/a| -1 8 -13 -61 40 808 -.07 101 101 | --- --- --- ---
| 8 23 19 265 221 1078 .26 | --- ---
Table 1.1562.b GPS week : 1562 MJD: 55178.0-55184.0
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 | 20 22 21 22 24 21 17 |
R03 | 19 21 22 23 25 25 19 |
R07 | 24 22 23 22 17 20 16 |
R08 | 23 23 19 23 25 21 21 |
R10 | 9 10 14 10 10 10 9 |
R11 | 16 11 9 11 11 13 13 |
R13 | 14 11 10 15 14 10 11 |
R14 | 10 8 9 8 7 9 10 |
R15 | 11 10 11 10 9 11 13 |
R17 | 13 12 15 16 16 16 12 |
R18 | 12 11 10 9 7 10 12 |
R19 | 11 14 13 14 12 11 8 |
R20 | 13 13 15 18 18 16 10 |
R21 | 11 9 5 12 16 14 12 |
R23 | 19 18 14 22 16 17 23 |
Table 1.1562.c GPS week : 1562 MJD: 55178.0-55184.0
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 1562 0 | -131 85 298 782 -3691 -15890 87.9 2522 2522 | 521603 0
brd 1562 1 | 0 108 116 -2707 -90 -14920 87.5 2111 2111 | 526625 0
brd 1562 2 | -2 15 -27 -2713 -1302 -17850 89.6 2295 2295 | 514192 0
brd 1562 3 | 27 -51 57 -28 1613 -16480 87.6 2033 2033 | 531442 0
brd 1562 4 | 16 117 94 -1353 1546 -14700 86.2 2259 2259 | 520800 0
brd 1562 5 | -30 -99 160 2302 146 -17680 90.7 2345 2345 | 459067 0
brd 1562 6 | -51 39 -13 -381 -155 -20620 89.7 2247 2247 | 536641 0
-------------+------------------------------------------------------------+----------------
brd 1562 mean| -24 30 98 -585 -276 -16877 88.5 2259 2259 | 515767 0
brd 1562 sdev| 54 82 111 1833 1817 2053 1.6 158 158 | 26064 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 2.1562.0 GPS week: 1562 Day: 0 MJD: 55178
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 127| 0 0 11 12 -114 -74 -.23 35 36 | 0 971 2514 2765
cod 240| -1 -2 0 54 68 69 -.14 18 14 | --- --- --- ---
esx 125| -1 1 -8 -48 20 17 .37 24 23 | 144747 -1802 4972 10560
iac n/a| 3 0 3 -16 -53 -156 -.21 35 35 | 523464 -1982 4959 8801
mcc n/a| -6 57 -18 -648 -30 -1318 -.40 358 358 | --- --- --- ---
Table 2.1562.1 GPS week: 1562 Day: 1 MJD: 55179
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 127| 1 0 7 -12 -24 152 -.15 29 26 | 0 -30 2607 2898
cod 240| -1 -1 -4 18 25 -13 -.13 18 13 | --- --- --- ---
esx 125| 0 0 -4 0 -16 5 .37 20 20 | 155027 429 5167 11080
iac n/a| 2 0 9 -34 32 -146 -.23 42 42 | 524873 1080 5155 8938
mcc n/a| -1 0 -37 78 -251 96 .14 64 64 | --- --- --- ---
Table 2.1562.2 GPS week: 1562 Day: 2 MJD: 55180
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 127| 2 -1 5 30 23 -54 -.09 35 34 | 0 -156 2532 2897
cod 240| -2 1 -2 65 -2 61 -.14 14 12 | --- --- --- ---
esx 125| 1 0 -4 -78 -24 34 .36 23 22 | 142139 -2902 4302 12243
iac n/a| 1 0 13 -20 20 -82 -.19 37 37 | 516178 -2806 4326 10371
mcc n/a| 12 13 -40 124 -37 994 -.45 54 54 | --- --- --- ---
Table 2.1562.3 GPS week: 1562 Day: 3 MJD: 55181
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 127| 2 -2 12 14 65 -115 -.19 47 47 | 0 600 2079 2243
cod 240| -3 3 -4 48 -5 163 -.14 17 14 | --- --- --- ---
esx 125| 0 -4 -3 -59 -33 -78 .27 22 22 | 158264 -2680 3926 9900
iac n/a| 0 0 6 20 -5 -97 -.06 37 37 | 532113 -478 3941 8484
mcc n/a| 0 -6 2 18 174 1710 -.13 62 62 | --- --- --- ---
Table 2.1562.4 GPS week: 1562 Day: 4 MJD: 55182
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 127| 2 1 11 65 40 -170 -.15 37 36 | 0 -407 2320 2449
cod 240| -3 1 -2 53 18 131 -.23 16 14 | --- --- --- ---
esx 125| 0 -1 -2 -85 -24 -17 .35 21 20 | 142627 3004 4421 11597
iac n/a| 5 -2 6 -17 1 -29 .02 43 43 | 520902 -1075 4440 10085
mcc n/a| -9 -1 9 -47 302 1587 .11 69 69 | --- --- --- ---
Table 2.1562.5 GPS week: 1562 Day: 5 MJD: 55183
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 127| 3 1 12 82 74 -19 -.30 40 35 | 0 -384 1938 2041
cod 240| -5 -2 -7 23 -29 65 -.19 16 13 | --- --- --- ---
esx 125| 0 0 -2 -91 48 -73 .37 22 21 | 79304 1842 4380 10270
iac n/a| 7 2 12 18 -41 -13 -.05 38 38 | 458790 -265 4375 9264
mcc n/a| -9 3 -10 -17 296 1394 .10 62 62 | --- --- --- ---
Table 2.1562.6 GPS week: 1562 Day: 6 MJD: 55184
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 127| 2 0 13 50 37 -160 -.25 37 37 | 0 -76 2252 2421
cod 240| -2 0 -5 37 22 45 -.17 14 11 | --- --- --- ---
esx 125| 2 -2 0 -113 -4 37 .36 21 21 | 159282 -1017 3876 9742
iac n/a| 3 3 8 17 -23 -34 -.07 34 34 | 537945 -2025 3881 8285
mcc n/a| 5 -8 -1 60 -175 1195 .15 41 41 | --- --- --- ---
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 3.1562.0 GPS week: 1562 Day: 0 MJD: 55178
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 3380 46 22 23 52 --- 20 | 59 34 47 64 --- 43
R03E | 1102 34 17 27 55 --- 19 | 47 54 61 58 --- 48
R07E | 4903 66 29 21 54 --- 24 | 30 25 26 52 --- 22
R08E | 3629 58 25 28 52 486 22 | 43 60 51 56 29 48
R10 | 1417 22 8 16 20 --- 9 | 42 45 49 55 --- 45
R11 | 4710 23 15 40 30 --- 16 | 35 42 78 36 --- 47
R13 | 1519 29 12 33 19 --- 13 | 48 55 72 53 --- 56
R14 | 830 14 12 20 18 --- 9 | 23 28 33 25 --- 23
R15 | 720 15 16 18 28 144 11 | 20 25 32 31 50 22
R17 | 973 38 15 15 19 --- 12 | 34 70 64 62 --- 58
R18 | 1611 23 21 13 25 --- 12 | 41 70 62 63 --- 60
R19 | 1872 26 11 19 18 --- 10 | 52 70 83 65 --- 69
R20 | 1756 36 11 24 22 --- 13 | 31 56 64 61 --- 53
R21 | 2436 22 13 18 23 --- 10 | 50 67 73 75 --- 66
R23 | 1340 29 24 30 48 --- 18 | 27 31 63 48 --- 35
------+------------------------------------+--------------------------------
RMS | 2522 35 18 24 35 358 |T 38 48 57 53 39 46
WRMS | 2522 36 14 23 35 358 |NE 34 52 54 49 50 46
MEDI | 1611 29 15 21 25 144 |MD 41 54 62 56 29 48
Table 3.1562.1 GPS week: 1562 Day: 1 MJD: 55179
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2209 43 25 29 58 --- 21 | 48 48 57 67 --- 47
R03E | 708 40 18 24 66 --- 20 | 51 47 47 62 --- 42
R07E | 3491 50 20 25 64 --- 22 | 41 29 26 50 --- 25
R08E | 1307 48 31 24 59 --- 22 | 40 48 57 67 --- 47
R10 | 1953 14 12 19 24 --- 9 | 45 43 45 44 --- 42
R11 | 4033 10 16 20 27 --- 10 | 33 40 38 28 --- 33
R13 | 1000 21 14 23 18 --- 11 | 65 63 74 68 --- 66
R14 | 2427 12 8 12 22 --- 7 | 29 31 31 27 --- 27
R15 | 930 13 14 20 18 64 9 | 24 24 34 23 48 23
R17 | 715 29 14 10 27 --- 11 | 32 37 36 46 --- 32
R18 | 857 30 12 14 17 --- 10 | 29 50 48 35 --- 40
R19 | 674 11 13 25 49 --- 14 | 56 60 59 56 --- 53
R20 | 2611 29 8 14 39 --- 12 | 24 31 45 30 --- 30
R21 | 2479 16 13 13 16 --- 8 | 38 49 45 37 --- 41
R23 | 2247 18 28 20 59 --- 17 | 23 29 36 46 --- 21
------+------------------------------------+--------------------------------
RMS | 2111 29 18 20 42 64 |T 38 41 45 45 48 37
WRMS | 2111 26 13 20 42 64 |NE 34 40 41 37 48 35
MEDI | 1953 21 14 20 27 64 |MD 38 43 45 46 48 40
Table 3.1562.2 GPS week: 1562 Day: 2 MJD: 55180
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2755 50 15 31 56 --- 20 | 50 45 40 68 --- 42
R03E | 696 54 26 27 53 --- 21 | 57 80 81 75 --- 70
R07E | 3906 55 19 31 61 --- 22 | 33 31 32 44 --- 23
R08E | 3546 54 13 27 47 --- 19 | 41 38 50 66 --- 42
R10 | 2387 18 15 34 33 --- 14 | 35 44 72 45 --- 46
R11 | 3454 13 10 16 21 --- 8 | 37 43 49 33 --- 39
R13 | 509 25 11 16 18 --- 9 | 61 72 61 66 --- 65
R14 | 3920 16 6 17 22 --- 8 | 25 22 34 19 --- 22
R15 | 1345 17 12 18 32 54 11 | 21 29 30 39 61 23
R17 | 541 40 14 28 22 --- 14 | 31 44 64 26 --- 40
R18 | 808 27 11 19 11 --- 10 | 43 47 48 43 --- 44
R19 | 889 32 14 18 28 --- 12 | 72 77 70 48 --- 67
R20 | 1136 30 13 16 46 --- 14 | 49 49 47 59 --- 48
R21 | 2017 9 6 9 11 --- 5 | 59 55 60 57 --- 56
R23 | 967 33 15 17 35 --- 13 | 35 22 42 49 --- 28
------+------------------------------------+--------------------------------
RMS | 2295 35 14 23 37 54 |T 43 46 52 49 61 43
WRMS | 2295 34 12 22 37 54 |NE 38 43 49 35 61 39
MEDI | 1345 30 13 18 32 54 |MD 41 44 49 48 61 42
Table 3.1562.3 GPS week: 1562 Day: 3 MJD: 55181
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 2198 59 19 26 58 --- 22 | 36 29 37 68 --- 33
R03E | 1238 59 21 30 57 --- 22 | 79 68 56 73 --- 62
R07E | 3338 66 22 22 53 --- 22 | 35 22 33 52 --- 20
R08E | 3870 68 29 20 47 --- 22 | 31 67 57 50 --- 51
R10M | 1311 22 12 13 21 --- 9 | 52 52 54 64 --- 53
R11M | 3395 19 13 16 25 --- 10 | 33 49 46 39 --- 41
R13M | 688 52 18 18 24 --- 15 | 118 153 154 137 --- 143
R14 | 2223 15 8 19 16 --- 8 | 29 27 35 28 --- 26
R15 | 1174 26 11 14 23 62 10 | 25 18 23 30 55 17
R17 | 655 44 20 24 28 --- 15 | 35 52 65 36 --- 46
R18 | 652 31 11 11 13 --- 9 | 30 40 43 37 --- 36
R19 | 1062 43 16 23 22 --- 14 | 56 90 76 72 --- 76
R20M | 1751 58 18 30 29 --- 18 | 33 50 76 70 --- 57
R21M | 1402 31 13 23 17 --- 11 | 57 69 88 64 --- 71
R23M | 1578 57 13 31 60 --- 22 | 35 32 38 48 --- 29
------+------------------------------------+--------------------------------
RMS | 2033 47 17 22 37 62 |T 45 54 58 57 55 50
WRMS | 2033 47 14 22 37 62 |NE 35 45 48 40 55 40
MEDI | 1402 44 16 22 25 62 |MD 35 50 54 52 55 46
Table 3.1562.4 GPS week: 1562 Day: 4 MJD: 55182
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1365 61 21 29 63 --- 23 | 43 35 36 54 --- 30
R03E | 2269 47 31 24 79 --- 25 | 74 67 75 96 --- 71
R07E | 2048 30 11 26 56 --- 17 | 29 24 30 59 --- 23
R08E | 5506 48 14 27 84 --- 24 | 66 51 62 74 --- 51
R10 | 2317 20 15 16 22 --- 10 | 42 43 45 53 --- 42
R11 | 3144 22 12 21 22 --- 10 | 29 37 52 29 --- 36
R13 | 1064 38 12 23 24 --- 13 | 71 84 100 82 --- 84
R14 | 2128 12 6 14 18 --- 7 | 32 25 33 22 --- 26
R15 | 1531 12 11 18 23 69 9 | 26 25 36 38 40 28
R17 | 840 46 21 17 27 --- 15 | 25 63 56 34 --- 48
R18 | 769 15 6 12 17 --- 7 | 36 34 42 40 --- 36
R19 | 706 38 12 16 17 --- 12 | 32 58 63 49 --- 52
R20 | 2911 53 10 24 38 --- 17 | 23 47 56 71 --- 47
R21 | 829 42 19 25 23 --- 15 | 57 67 78 57 --- 65
R23 | 880 33 24 16 41 --- 16 | 60 55 71 63 --- 59
------+------------------------------------+--------------------------------
RMS | 2258 37 16 21 43 69 |T 43 47 55 54 40 46
WRMS | 2258 36 14 20 43 69 |NE 30 41 46 36 40 38
MEDI | 1531 38 12 21 24 69 |MD 36 47 56 54 40 47
Table 3.1562.5 GPS week: 1562 Day: 5 MJD: 55183
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1133 61 19 23 51 --- 20 | 44 26 29 53 --- 28
R03E | 2467 80 22 33 50 --- 25 | 66 66 63 75 --- 60
R07E | 3538 33 16 34 57 --- 19 | 32 21 29 51 --- 17
R08E | 3945 44 18 24 67 --- 21 | 27 53 49 70 --- 40
R10 | 2576 22 8 17 22 --- 9 | 49 42 53 54 --- 46
R11 | 3517 34 16 23 22 --- 13 | 28 41 40 29 --- 30
R13 | 2663 31 10 15 18 --- 10 | 108 113 122 117 --- 114
R14 | 2243 23 8 16 18 --- 8 | 37 33 35 33 --- 32
R15 | 1534 14 11 15 35 62 10 | 25 32 30 36 22 26
R17 | 1466 27 18 13 53 --- 16 | 43 54 44 43 --- 43
R18 | 829 33 10 12 18 --- 10 | 18 34 33 30 --- 27
R19 | 846 35 11 12 18 --- 10 | 19 44 39 44 --- 36
R20 | 2773 52 10 20 35 --- 16 | 20 31 40 36 --- 29
R21 | 1052 39 18 21 20 --- 13 | 56 77 64 81 --- 68
R23 | 1094 23 27 32 34 --- 16 | 135 123 130 131 --- 126
------+------------------------------------+--------------------------------
RMS | 2345 40 16 22 38 62 |T 47 52 53 58 22 48
WRMS | 2345 35 13 21 38 62 |NE 28 39 36 37 22 32
MEDI | 2243 33 16 20 34 62 |MD 37 42 40 51 22 36
Table 3.1562.6 GPS week: 1562 Day: 6 MJD: 55184
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02E | 1426 36 16 19 51 --- 17 | 54 41 35 54 --- 35
R03E | 1427 53 21 19 47 --- 19 | 82 65 62 68 --- 63
R07E | 5260 37 14 30 38 --- 16 | 28 20 48 46 --- 27
R08E | 1282 54 18 29 53 --- 20 | 35 41 46 71 --- 39
R10 | 1372 19 9 15 20 --- 8 | 48 46 49 61 --- 48
R11 | 2802 23 13 29 27 --- 13 | 28 47 71 38 --- 47
R13 | 3427 35 9 17 22 --- 11 | 96 93 94 93 --- 93
R14 | 1562 34 9 16 15 --- 10 | 31 27 35 25 --- 27
R15 | 1254 30 13 21 31 41 13 | 34 32 50 39 38 36
R17 | 2750 26 16 25 20 --- 12 | 38 67 75 52 --- 60
R18 | 1344 31 9 25 24 --- 12 | 35 62 65 58 --- 58
R19 | 877 27 10 9 16 --- 8 | 36 63 62 52 --- 56
R20 | 1706 33 6 6 23 --- 9 | 23 42 52 50 --- 41
R21 | 1043 39 11 12 23 --- 11 | 61 86 96 84 --- 84
R23 | 1642 57 23 29 59 --- 22 | 206 214 217 211 --- 211
------+------------------------------------+--------------------------------
RMS | 2246 37 14 21 34 41 |T 55 63 70 66 38 61
WRMS | 2246 37 11 21 34 41 |NE 34 50 57 45 38 47
MEDI | 1427 34 13 19 24 41 |MD 36 47 62 54 38 48
More information about the IGSREPORT
mailing list