[IGSREPORT-18949] Wk 1598 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 9 09:29:52 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1598 (Aug 22, 2010 - Aug 28, 2010)
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 2.1598.
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:
igl1598[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1598 in the SP3 format.
igl15987.sum Combination Report for GPS Week 1598.
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 | 449.6 ns
1 | 447.8 ns
2 | 344.1 ns
3 | 356.6 ns
4 | 443.4 ns
5 | 444.4 ns
6 | 449.6 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 1.1598, 1a.1598).
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 2.1598.0-6)
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 3.1598.0-6).
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 1598 summary. (Aug 22, 2010 - Aug 28, 2010)
Table 1.1598.a GPS week : 1598 MJD: 55430.0-55436.0
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 119| 1 0 -6 39 -53 -146 -.11 45 42 | 0 79 1789 1866
| 1 1 3 27 60 148 .07 | 0 256
cod 233| -1 0 9 15 20 51 -.18 20 17 | --- --- --- ---
| 0 1 4 19 30 39 .02 | --- ---
esx 134| 1 0 8 -17 11 67 .40 26 23 | 104449 154 3714 7892
| 1 1 6 19 16 72 .05 | 51824 2013
gfz 197| 0 0 11 -31 -64 107 -.22 29 26 | 263537 -1106 3709 7498
| 2 1 6 46 62 39 .05 | 47648 2211
iac n/a| 0 0 -25 -24 -12 -56 -.21 36 36 | 419564 -645 3718 8095
| 1 1 31 36 24 63 .08 | 47152 330
mcc n/a| 7 5 48 -21 31 -655 -.04 122 122 | --- --- --- ---
| 15 9 12 71 81 511 .47 | --- ---
Table 1.1598.b GPS week : 1598 MJD: 55430.0-55436.0
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
------+------------------------------------+------------------------------------------
R01 | 11 15 10 12 17 12 13 |
R02 | 15 13 14 8 10 12 13 |
R03 | 13 18 11 10 12 12 19 |
R04 | 11 12 16 12 12 9 13 |
R05 | 10 12 13 14 13 10 14 |
R07 | 9 10 13 12 13 13 15 |
R08 | 16 10 10 11 11 14 14 |
R10 | 10 12 11 10 14 11 17 |
R11 | 31 40 24 22 20 16 20 |
R13 | 12 11 13 12 12 11 15 |
R14 | 10 14 16 15 14 7 13 |
R15 | 8 11 11 15 12 11 12 |
R17 | 21 17 23 25 19 16 18 |
R18 | 25 26 25 23 20 16 17 |
R19 | 22 28 30 32 22 22 19 |
R20 | 22 23 25 25 35 25 23 |
R21 | 15 18 47 36 22 16 17 |
R22 | 18 16 23 25 24 31 20 |
R23 | 16 16 16 19 25 22 24 |
R24 | 16 20 19 22 22 28 27 |
Table 1.1598.c GPS week : 1598 MJD: 55430.0-55436.0
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 1598 0 | 98 -1 472 28 -326 -15320 87.5 5359 5359 | 449592 0
brd 1598 1 | 16 96 340 -716 -4326 -14260 88.3 2148 2148 | 447779 0
brd 1598 2 | -7 -21 262 430 -589 -16940 90.8 2155 2155 | 344078 0
brd 1598 3 | 20 45 303 -2280 -675 -11200 89.3 1975 1975 | 356576 0
brd 1598 4 | 17 -92 239 -1983 725 -8068 89.4 2124 2124 | 443440 0
brd 1598 5 | -43 -49 307 -144 85 -1872 92.7 2386 2386 | 444399 0
brd 1598 6 | 39 9 297 1453 814 -4872 90.0 2150 2150 | 449634 0
-------------+------------------------------------------------------------+----------------
brd 1598 mean| 20 -1 317 -458 -613 -10361 89.7 2613 2613 | 419356 0
brd 1598 sdev| 43 61 75 1322 1741 5645 1.7 1216 1216 | 47353 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 2.1598.0 GPS week: 1598 Day: 0 MJD: 55430
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 119| 3 -2 -7 36 25 -119 -.16 33 28 | 0 -46 1861 1921
cod 233| -2 0 8 -17 -17 99 -.15 21 17 | --- --- --- ---
esx 134| 0 1 2 -23 21 65 .44 31 24 | 142863 -75 3705 9165
gfz 197| -3 1 7 23 55 145 -.23 37 37 | 294641 -1823 3646 9004
iac n/a| 2 0 -9 31 -29 -83 -.14 33 33 | 449976 -1117 3701 9483
mcc n/a| 6 0 42 -3 139 -144 -.23 102 102 | --- --- --- ---
Table 2.1598.1 GPS week: 1598 Day: 1 MJD: 55431
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 119| 3 -1 -7 35 -76 -70 .01 44 44 | 0 339 1992 2069
cod 233| -2 0 8 22 33 32 -.20 17 14 | --- --- --- ---
esx 134| 1 0 1 -16 15 109 .38 25 23 | 136936 1366 4121 7920
gfz 197| -1 0 4 -9 -59 135 -.29 25 22 | 293520 -285 4135 7580
iac n/a| -2 0 -8 -39 -47 -121 -.23 36 36 | 447400 -282 4141 7761
mcc n/a| 1 0 34 106 35 -617 .06 90 90 | --- --- --- ---
Table 2.1598.2 GPS week: 1598 Day: 2 MJD: 55432
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 119| 1 2 -5 61 -166 96 -.08 42 39 | 0 312 1771 1829
cod 233| 0 1 6 18 66 33 -.16 21 17 | --- --- --- ---
esx 134| 1 0 5 -36 20 -81 .47 29 27 | 34720 1886 3732 8819
gfz 197| 0 0 9 -47 -28 105 -.24 29 22 | 188269 212 3731 7802
iac n/a| 0 2 -12 -68 14 -34 -.29 34 34 | 344903 -762 3737 8607
mcc n/a| -5 1 47 -43 -9 -947 .13 98 98 | --- --- --- ---
Table 2.1598.3 GPS week: 1598 Day: 3 MJD: 55433
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 119| 0 0 -10 8 -51 -76 -.09 54 43 | 0 270 1582 1670
cod 233| 0 0 8 15 4 -20 -.16 24 18 | --- --- --- ---
esx 134| 1 -2 10 10 -2 78 .39 27 24 | 23310 2090 3902 7841
gfz 197| 2 -2 12 -68 -130 126 -.18 31 28 | 199934 1176 3891 7885
iac n/a| 0 0 -16 -55 24 -32 -.29 37 37 | 356689 -389 3923 8581
mcc n/a| -14 1 41 -59 10 -265 -.17 99 99 | --- --- --- ---
Table 2.1598.4 GPS week: 1598 Day: 4 MJD: 55434
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 119| 0 1 -9 22 -10 -242 -.12 56 50 | 0 173 1613 1693
cod 233| -2 1 9 49 50 67 -.20 20 18 | --- --- --- ---
esx 134| 2 -2 4 4 -18 56 .46 27 24 | 129156 827 3554 7573
gfz 197| 5 -1 9 -100 -101 27 -.23 28 24 | 286072 859 3570 6969
iac n/a| 2 0 -15 -34 -20 12 -.24 34 34 | 443870 -295 3551 7672
mcc n/a| 8 3 41 -10 -3 -243 -.57 123 123 | --- --- --- ---
Table 2.1598.5 GPS week: 1598 Day: 5 MJD: 55435
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 119| 0 0 -6 21 -60 -277 -.22 46 45 | 0 -243 2148 2232
cod 233| 0 0 8 10 -6 76 -.21 22 21 | --- --- --- ---
esx 134| 0 0 10 -19 29 98 .35 22 19 | 131653 -1659 3235 6306
gfz 197| -1 0 16 -41 -87 92 -.20 27 22 | 288805 -3148 3243 5989
iac n/a| 2 -1 -19 -21 -15 12 -.21 31 31 | 444741 -726 3247 6804
mcc n/a| 25 7 60 -129 -87 -769 -.37 149 149 | --- --- --- ---
Table 2.1598.6 GPS week: 1598 Day: 6 MJD: 55436
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 119| 0 0 0 89 -31 -334 -.10 43 42 | 0 -251 1559 1651
cod 233| -1 -1 18 10 13 72 -.18 19 17 | --- --- --- ---
esx 134| 2 0 21 -43 13 148 .34 23 21 | 132510 -3355 3749 7624
gfz 197| 0 -2 23 22 -97 115 -.15 29 24 | 293520 -4737 3751 7263
iac n/a| 0 0 -96 13 -13 -149 -.06 45 45 | 449371 -950 3732 7759
mcc n/a| 29 25 69 -10 133 -1598 .88 192 192 | --- --- --- ---
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 3.1598.0 GPS week: 1598 Day: 0 MJD: 55430
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1571 23 17 18 33 19 --- 11 | 40 54 40 36 32 --- 41
R02 | 2545 29 13 33 30 27 --- 14 | 16 37 34 39 39 --- 26
R03 | 1207 35 9 25 16 18 --- 13 | 39 38 50 38 39 --- 35
R04 | 2897 23 15 26 29 11 --- 11 | 25 34 38 34 26 --- 27
R05 | 836 21 16 10 12 22 --- 10 | 17 43 37 35 27 --- 30
R07 | 2637 21 16 9 31 17 --- 9 | 28 51 40 57 37 --- 37
R08 | 2496 38 28 15 15 26 94 16 | 27 52 30 39 21 50 33
R10 | 1849 20 15 16 18 20 --- 10 | 28 40 46 48 33 --- 35
R11 |22125 38 51 75 112 38 --- 31 | 57 59 67 86 80 --- 47
R13 | 2307 13 20 22 16 20 --- 11 | 17 22 33 30 30 --- 21
R14 | 1212 19 11 18 26 24 --- 10 | 29 33 46 41 28 --- 33
R15 | 2531 12 8 12 25 20 68 7 | 24 17 23 22 21 34 16
R17E | 1946 49 20 38 38 43 --- 21 | 39 19 47 36 40 --- 23
R18E | 1494 68 20 42 34 40 --- 24 | 51 39 47 35 48 --- 36
R19E | 1835 48 19 38 34 49 --- 22 | 56 33 51 51 56 --- 35
R20E | 3539 49 19 32 51 55 --- 22 | 72 71 90 79 88 --- 76
R21E | 3063 14 18 27 33 38 --- 14 | 25 27 39 215 55 --- 31
R22E | 801 34 22 37 30 33 --- 18 | 36 45 40 33 47 --- 37
R23E | 1600 20 23 22 20 42 134 16 | 28 36 39 39 45 64 33
R24E | 1026 20 17 22 24 47 --- 16 | 32 27 43 34 47 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 5359 33 21 31 37 33 102 |T 34 38 44 51 41 49 34
WRMS | 5359 28 17 24 37 33 102 |NE 28 40 40 42 34 42 31
MEDI | 1849 23 17 22 29 26 94 |MD 28 37 40 38 39 50 33
Table 3.1598.1 GPS week: 1598 Day: 1 MJD: 55431
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2170 19 19 29 26 32 --- 14 | 36 29 60 37 20 --- 32
R02 | 2354 39 12 18 16 23 --- 12 | 23 26 33 26 18 --- 21
R03 | 1230 27 22 44 26 27 --- 18 | 25 31 50 38 32 --- 25
R04 | 1367 29 10 15 21 33 --- 12 | 26 32 39 31 23 --- 27
R05 | 689 27 12 20 18 27 --- 12 | 32 38 39 36 22 --- 32
R07 | 2639 25 12 15 22 18 --- 9 | 28 39 31 36 39 --- 32
R08 | 2801 26 15 12 20 20 105 10 | 24 37 36 40 26 22 31
R10 | 1489 30 11 17 20 32 --- 12 | 28 32 40 38 47 --- 34
XR11 | 8336 79 22 --- 44 81 --- 40 | 47 66 --- 109 92 --- 62
R13 | 2679 34 13 13 20 21 --- 11 | 17 30 47 37 38 --- 32
R14 | 1381 37 14 17 19 33 --- 14 | 41 32 33 33 32 --- 32
R15 | 1620 20 15 23 27 20 74 11 | 20 22 27 43 21 25 19
R17E | 1310 28 13 30 19 47 --- 16 | 34 33 50 30 36 --- 29
R18E | 3850 85 21 37 37 43 --- 26 | 33 28 40 42 42 --- 29
R19E | 2923 97 26 30 37 46 --- 28 | 31 22 35 42 48 --- 22
R20E | 2143 75 14 28 34 49 --- 23 | 42 33 42 46 53 --- 32
R21E | 2059 46 15 21 26 47 --- 17 | 58 50 57 451 92 --- 62
R22E | 1511 28 18 21 24 48 --- 16 | 33 18 36 35 47 --- 23
R23E | 1924 39 15 25 25 39 88 16 | 20 41 45 47 51 41 36
R24E | 2218 20 26 33 29 52 --- 19 | 21 19 42 34 29 --- 15
------+-----------------------------------------+-------------------------------------
RMS | 2148 44 17 25 25 36 90 |T 30 32 41 61 40 29 31
WRMS | 2148 44 14 23 22 36 90 |NE 28 34 39 42 34 23 31
MEDI | 2059 29 15 21 24 33 88 |MD 28 32 40 37 36 25 31
Table 3.1598.2 GPS week: 1598 Day: 2 MJD: 55432
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2679 16 10 17 24 24 --- 9 | 44 37 55 55 33 --- 38
R02 | 3300 16 21 33 26 19 --- 13 | 25 41 25 27 37 --- 28
R03 | 1222 29 14 15 29 15 --- 10 | 35 40 32 32 32 --- 32
R04 | 911 43 16 34 33 18 --- 16 | 53 31 26 36 34 --- 26
R05 | 882 17 13 29 24 27 --- 12 | 29 29 51 31 18 --- 27
R07 | 2347 31 19 22 17 14 --- 12 | 32 41 22 41 33 --- 29
R08 | 1829 23 9 14 17 20 130 9 | 29 31 41 39 38 57 29
R10 | 1930 19 11 22 24 25 --- 11 | 24 28 42 30 37 --- 28
R11 | 1641 49 28 25 28 59 --- 23 | 35 43 53 32 33 --- 27
R13 | 1624 25 20 25 15 21 --- 13 | 29 32 42 28 25 --- 25
R14 | 1748 31 24 31 20 24 --- 16 | 47 36 48 40 26 --- 33
R15 | 2822 23 11 15 23 25 64 10 | 23 29 26 28 21 46 22
R17E | 1302 35 29 45 29 47 --- 22 | 32 21 50 32 32 --- 20
R18E | 3917 70 33 28 30 36 --- 24 | 32 29 51 39 46 --- 35
R19E | 1391 84 31 48 33 47 --- 30 | 49 29 37 30 50 --- 27
R20E | 1165 72 23 40 50 37 --- 24 | 34 32 51 48 61 --- 38
XR21E |22714 --- 37 --- 3043 58 --- 46 | --- 72 --- 9999 92 --- 68
R22E | 2271 57 23 23 24 52 --- 22 | 49 44 50 44 56 --- 40
R23E | 2684 29 18 29 30 37 88 16 | 46 44 32 44 48 38 37
R24E | 2328 29 22 34 44 45 --- 19 | 36 18 44 37 38 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 2155 42 21 29 29 34 98 |T 35 35 40 36 39 47 31
WRMS | 2155 39 17 27 22 34 98 |NE 33 34 38 34 30 51 28
MEDI | 1829 29 20 28 26 25 88 |MD 34 32 42 36 34 46 28
Table 3.1598.3 GPS week: 1598 Day: 3 MJD: 55433
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2256 23 11 22 17 25 --- 11 | 37 45 53 55 55 --- 43
R02 | 3026 22 12 15 19 10 --- 8 | 34 44 38 39 44 --- 37
R03 | 1702 20 9 16 22 22 --- 9 | 38 46 52 59 33 --- 41
R04 | 942 37 15 15 23 19 --- 12 | 38 51 47 56 42 --- 42
R05 | 1312 49 21 8 20 14 --- 13 | 35 43 30 39 26 --- 29
R07 | 2970 38 15 16 50 16 --- 11 | 28 44 59 55 41 --- 42
R08 | 1304 18 15 14 25 28 93 11 | 33 35 29 39 26 38 27
R10 | 2610 23 9 18 27 19 --- 9 | 44 38 44 48 32 --- 37
R11 | 1963 80 20 26 21 32 --- 22 | 60 47 52 59 63 --- 51
R13 | 1266 21 21 14 28 25 --- 11 | 32 56 48 54 45 --- 44
R14 | 1023 44 18 14 18 32 --- 15 | 26 41 36 38 39 --- 32
R15 | 1594 27 25 25 42 24 57 14 | 31 39 31 53 36 62 32
R17E | 1050 50 21 47 31 58 --- 25 | 42 22 46 28 40 --- 18
R18E | 2790 65 25 34 33 43 --- 23 | 41 44 46 47 39 --- 37
R19E | 1951 112 42 25 35 50 --- 32 | 107 48 48 40 54 --- 49
R20E | 628 80 20 42 41 39 --- 25 | 48 64 55 58 67 --- 55
R21E | 1399 85 56 50 46 67 --- 35 | 101 30 85 736 103 --- 55
R22E | 1587 77 21 27 30 53 --- 24 | 36 28 33 31 57 --- 25
R23E | 2288 42 26 27 27 41 132 19 | 28 36 50 51 58 38 36
R24E | 3006 31 29 38 28 50 --- 21 | 25 29 49 35 49 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 1974 54 24 27 31 37 99 |T 43 41 46 81 47 46 38
WRMS | 1974 43 18 24 28 37 99 |NE 36 44 43 49 40 50 38
MEDI | 1594 38 20 22 27 28 93 |MD 36 43 47 48 42 38 37
Table 3.1598.4 GPS week: 1598 Day: 4 MJD: 55434
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1699 37 27 27 26 27 --- 16 | 49 39 28 28 25 --- 27
R02 | 2544 26 13 22 21 8 --- 10 | 23 38 45 45 38 --- 35
R03 | 2663 40 11 15 26 22 --- 12 | 31 44 62 65 58 --- 47
R04 | 2586 32 20 19 24 15 --- 12 | 33 42 35 47 35 --- 32
R05 | 1260 43 16 17 18 19 --- 12 | 32 42 37 40 30 --- 33
R07 | 2051 41 18 14 36 23 --- 13 | 26 48 38 34 41 --- 38
R08 | 2849 20 17 7 20 28 98 11 | 30 36 35 44 29 27 30
R10 | 1853 39 9 29 34 25 --- 14 | 39 27 54 59 22 --- 32
R11 | 1908 65 20 29 34 33 --- 19 | 39 40 51 62 45 --- 41
R13 | 2057 24 16 23 28 20 --- 11 | 28 22 41 42 37 --- 28
R14 | 816 33 18 24 16 23 --- 13 | 43 49 49 44 32 --- 40
R15 | 2019 25 18 15 18 27 61 12 | 23 32 28 32 24 38 26
R17E | 1153 38 21 35 28 42 --- 19 | 35 37 33 30 35 --- 24
R18E | 1920 69 13 33 15 35 --- 20 | 47 41 50 44 61 --- 45
R19E | 2829 60 27 29 26 45 --- 22 | 75 48 47 43 62 --- 47
R20E | 1365 136 34 41 49 43 --- 34 | 77 61 58 63 71 --- 55
R21E | 3023 51 26 27 34 53 --- 22 | 53 52 58 326 82 --- 57
R22E | 1391 83 18 30 19 44 --- 23 | 39 30 25 25 62 --- 27
R23E | 1108 57 20 46 32 54 179 24 | 37 29 62 46 64 34 35
R24E | 3149 69 17 30 37 47 --- 22 | 33 22 40 42 54 --- 20
------+-----------------------------------------+-------------------------------------
RMS | 2124 56 20 27 28 34 123 |T 39 38 43 58 45 33 35
WRMS | 2124 50 18 24 24 34 123 |NE 33 38 41 45 34 32 34
MEDI | 1920 40 18 27 26 27 98 |MD 35 39 41 44 38 34 33
Table 3.1598.5 GPS week: 1598 Day: 5 MJD: 55435
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1196 14 25 17 20 21 --- 12 | 24 44 37 31 36 --- 32
R02 | 2042 13 21 14 30 29 --- 12 | 34 44 36 58 35 --- 33
R03 | 2765 17 17 23 20 19 --- 11 | 22 37 24 31 41 --- 25
R04 | 2741 24 14 12 18 15 --- 9 | 22 33 40 37 36 --- 29
R05 | 1083 25 18 12 26 19 --- 10 | 24 38 36 35 39 --- 32
R07 | 2609 26 28 16 31 21 --- 13 | 17 31 21 34 20 --- 13
R08 | 2944 30 27 16 14 21 81 13 | 35 36 41 34 30 24 31
R10 | 2328 19 20 14 21 20 --- 10 | 21 27 19 30 34 --- 17
R11 | 3163 51 16 23 21 24 --- 16 | 50 55 44 54 56 --- 50
R13 | 2857 26 15 16 21 22 --- 11 | 39 35 47 54 43 --- 37
R14 | 915 19 7 9 21 15 --- 7 | 21 20 30 32 36 --- 23
R15 | 3255 21 15 15 30 23 103 10 | 39 44 34 56 35 32 35
R17E | 1164 21 25 18 26 43 --- 16 | 32 24 21 29 49 --- 20
R18E | 3234 37 17 21 19 37 --- 15 | 34 29 44 34 56 --- 34
R19E | 2553 69 23 30 27 30 --- 21 | 51 29 46 45 55 --- 33
R20E | 2619 61 34 33 35 47 --- 24 | 61 24 50 38 63 --- 37
R21E | 2641 34 23 18 24 38 --- 16 | 31 31 38 198 50 --- 32
R22E | 2151 98 25 44 44 53 --- 31 | 26 23 30 40 51 --- 22
R23E | 815 67 25 27 37 38 223 22 | 36 30 31 36 60 33 26
R24E | 1985 99 18 25 37 48 --- 27 | 30 20 31 36 60 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2386 46 22 22 27 31 149 |T 32 32 35 47 44 29 29
WRMS | 2386 45 21 19 22 31 149 |NE 29 37 34 40 36 28 29
MEDI | 2553 26 20 17 24 23 103 |MD 31 31 36 36 41 32 31
Table 3.1598.6 GPS week: 1598 Day: 6 MJD: 55436
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1907 28 19 21 22 28 --- 13 | 33 52 39 46 47 --- 40
R02 | 687 29 20 19 17 28 --- 13 | 25 45 39 43 36 --- 34
R03 | 1091 59 9 30 22 31 --- 18 | 49 45 33 41 45 --- 37
R04 | 1214 24 16 20 18 30 --- 12 | 31 52 33 45 45 --- 39
R05 | 1395 34 17 18 19 38 --- 14 | 22 56 43 50 56 --- 44
R07 | 978 40 16 23 44 29 --- 14 | 21 52 64 40 48 --- 48
R08 | 2861 31 23 19 22 28 134 14 | 28 46 35 41 34 30 34
R10 | 2013 34 21 21 27 47 --- 16 | 27 24 43 32 29 --- 26
R11 | 1854 60 11 21 25 52 --- 19 | 46 64 65 59 72 --- 61
R13 | 1952 26 13 15 20 52 --- 14 | 30 31 43 43 46 --- 33
R14 | 956 27 13 21 27 33 --- 12 | 30 29 51 51 30 --- 34
R15 | 3116 28 11 10 31 37 177 11 | 28 28 29 29 27 41 25
R17E | 897 39 18 15 26 57 --- 17 | 47 38 27 30 59 --- 34
R18E | 2879 34 16 22 28 53 --- 17 | 35 35 44 36 53 --- 34
R19E | 3894 37 21 27 25 50 --- 18 | 72 46 39 41 55 --- 42
R20E | 4423 66 27 26 29 51 --- 23 | 68 31 48 47 60 --- 39
R21E | 2412 35 19 28 29 45 --- 17 | 57 31 55 203 65 --- 47
R22E | 602 47 15 29 56 55 --- 19 | 41 20 28 42 47 --- 21
R23E | 814 48 19 38 33 68 249 23 | 33 31 39 36 61 44 27
R24E | 1391 80 30 28 30 56 --- 26 | 25 24 27 31 58 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2149 43 19 23 29 45 192 |T 37 39 41 49 48 38 36
WRMS | 2149 42 17 21 24 45 192 |NE 30 43 43 43 42 35 37
MEDI | 1395 34 17 21 26 45 177 |MD 31 35 39 41 47 41 34
More information about the IGSREPORT
mailing list