[IGSREPORT-17782] Wk 1546 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Sep 10 06:01:24 PDT 2009
******************************************************************************
IGS Electronic Report 10 Sep 06:01:48 PDT 2009 Message Number 17782
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1546 (Aug 23, 2009 - Aug 29, 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 2.1546.
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:
igl1546[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1546 in the SP3 format.
igl15467.sum Combination Report for GPS Week 1546.
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 | 226.2 ns
1 | 142.6 ns
2 | 152.8 ns
3 | 150.5 ns
4 | 212.8 ns
5 | 214.8 ns
6 | 216.2 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
----+--------+---------------
1 | IAC | R23
2 | IAC | R23
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 1.1546, 1a.1546).
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 2.1546.0-6)
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 3.1546.0-6).
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 1546 summary. (Aug 23, 2009 - Aug 29, 2009)
Table 1.1546.a GPS week : 1546 MJD: 55066.0-55072.0
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 105| 1 0 -3 26 2 -38 -.14 26 24 | 0 167 3204 3701
| 1 1 6 16 27 172 .04 | 0 328
cod 231| -3 0 4 -5 -19 117 -.13 18 16 | --- --- --- ---
| 2 0 2 19 13 64 .02 | --- ---
esx 135| 0 2 4 -46 8 -14 .49 28 24 | 102468 2930 6107 10574
| 1 2 6 61 42 70 .05 | 40101 5862
iac n/a| 2 0 -5 16 20 -107 -.11 27 27 | 187714 -784 6101 10375
| 1 1 6 27 28 114 .05 | 38051 3918
mcc n/a| 0 1 27 8 16 640 -.16 102 102 | --- --- --- ---
| 12 4 10 89 78 512 .32 | --- ---
Table 1.1546.b GPS week : 1546 MJD: 55066.0-55072.0
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 11 11 9 12 10 |
R03 | 9 11 11 9 12 12 13 |
R07 | 13 10 15 13 12 8 12 |
R08 | 9 12 12 15 13 11 12 |
R10 | 13 8 9 12 11 12 15 |
R11 | 13 12 14 17 16 18 12 |
R13 | 10 12 10 12 9 14 13 |
R14 | 13 11 10 10 9 14 11 |
R15 | 10 12 13 8 8 10 9 |
R17 | 13 14 12 18 19 16 16 |
R18 | 15 14 12 15 17 17 22 |
R19 | 11 14 16 17 14 15 21 |
R20 | 10 13 17 17 19 20 25 |
R21 | 13 11 12 14 15 16 18 |
R22 | 13 14 15 15 20 20 16 |
R23 | 18 360 1572 18 25 18 20 |
R24 | 20 19 15 25 17 20 12 |
Table 1.1546.c GPS week : 1546 MJD: 55066.0-55072.0
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 1546 0 | -58 -57 358 -1419 900 -12600 87.3 2974 2974 | 226236 0
brd 1546 1 |-6530 ---- 4038 -253200 65260 23420 21.1 >>>>> >>>>> | 142588 0
brd 1546 2 | 97 -87 284 1461 -1046 -9357 88.9 3477 3477 | 152812 0
brd 1546 3 | -93 208 234 -1060 -961 -11590 92.6 5652 5652 | 150527 0
brd 1546 4 | -34 14 403 -1308 -1386 -11140 89.4 4792 4792 | 212841 0
brd 1546 5 | 35 -194 312 1105 771 -12530 88.2 4181 4181 | 214803 0
brd 1546 6 | 84 -100 176 684 1658 -13100 89.4 3811 3811 | 216189 0
-------------+------------------------------------------------------------+----------------
brd 1546 mean| -928 -3059 829 -36248 9313 -6699 79.5 >>>>> >>>>> | 187999 0
brd 1546 sdev| 2471 8000 1417 95674 24697 13339 25.8 >>>>> >>>>> | 37185 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 2.1546.0 GPS week: 1546 Day: 0 MJD: 55066
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 105| 2 1 4 8 -33 84 -.12 23 19 | 0 409 2855 3215
cod 231| -2 0 1 0 -4 85 -.12 16 14 | --- --- --- ---
esx 135| 0 1 -8 -3 -27 42 .46 26 23 | 145517 769 6599 10301
iac n/a| 3 0 -2 11 15 -252 -.03 23 23 | 226188 -3093 6587 9766
mcc n/a| 10 2 46 173 -120 611 .53 104 104 | --- --- --- ---
Table 2.1546.1 GPS week: 1546 Day: 1 MJD: 55067
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 105| 2 -1 3 18 50 40 -.15 23 22 | 0 342 3031 3554
cod 231| -4 1 5 6 -29 63 -.15 16 15 | --- --- --- ---
esx 135| 0 -1 1 -33 -16 -105 .43 22 21 | 51126 12099 6827 11888
iac n/a| 1 0 -10 13 28 -6 -.20 26 26 | 138710 3969 6821 11019
mcc n/a| 13 5 23 54 71 1385 -.17 104 104 | --- --- --- ---
Table 2.1546.2 GPS week: 1546 Day: 2 MJD: 55068
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 105| 0 0 -1 40 19 -149 -.06 20 20 | 0 221 3480 4299
cod 231| -2 0 4 -42 -31 107 -.17 17 15 | --- --- --- ---
esx 135| 1 2 5 -36 15 -17 .47 28 25 | 73688 2429 4372 10255
iac n/a| 4 -3 -6 4 44 22 -.13 25 25 | 153073 -2928 4367 9204
mcc n/a| -18 -4 23 -23 -3 1245 -.37 111 111 | --- --- --- ---
Table 2.1546.3 GPS week: 1546 Day: 3 MJD: 55069
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 105| 1 0 -11 26 -11 29 -.13 29 25 | 0 -418 4077 4771
cod 231| -6 0 0 -16 -6 58 -.13 21 18 | --- --- --- ---
esx 135| 2 1 4 28 90 -33 .45 29 23 | 57792 3327 4677 8249
iac n/a| 2 0 4 -24 -40 -79 -.13 25 25 | 150997 300 4686 8876
mcc n/a| -8 7 30 -79 45 148 -.22 106 106 | --- --- --- ---
Table 2.1546.4 GPS week: 1546 Day: 4 MJD: 55070
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 105| 1 -2 -11 22 15 204 -.11 28 24 | 0 545 3105 3410
cod 231| -3 0 4 -2 -26 95 -.12 19 14 | --- --- --- ---
esx 135| 0 5 9 -83 28 -98 .49 29 25 | 123016 -6715 6034 10266
iac n/a| 1 0 0 44 27 -275 -.12 29 29 | 214539 -4140 6041 10432
mcc n/a| -13 4 31 27 125 16 -.20 90 90 | --- --- --- ---
Table 2.1546.5 GPS week: 1546 Day: 5 MJD: 55071
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 105| 3 -3 -3 57 -18 -244 -.18 26 25 | 0 168 2663 2936
cod 231| -3 0 6 0 -31 233 -.13 21 18 | --- --- --- ---
esx 135| -3 3 9 -162 3 79 .57 30 28 | 128602 7487 7371 12539
iac n/a| 2 1 -13 60 43 -99 -.10 28 28 | 211941 4956 7346 12556
mcc n/a| 8 -3 12 -8 23 552 -.39 92 92 | --- --- --- ---
Table 2.1546.6 GPS week: 1546 Day: 6 MJD: 55072
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 105| 0 0 -2 12 -1 -234 -.19 34 34 | 0 -98 3221 3723
cod 231| 0 -1 5 17 -4 177 -.11 18 15 | --- --- --- ---
esx 135| 0 6 9 -37 -32 28 .54 29 25 | 137538 1118 6870 10524
iac n/a| 0 0 -9 9 25 -64 -.07 29 29 | 218554 -4557 6864 10772
mcc n/a| 5 -2 26 -87 -28 525 -.32 106 106 | --- --- --- ---
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 3.1546.0 GPS week: 1546 Day: 0 MJD: 55066
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3890 12 11 16 12 --- 7 | 22 31 29 24 --- 24
R03 | 5662 11 15 20 16 --- 9 | 18 25 28 20 --- 19
R07 | 3558 13 19 25 28 --- 12 | 26 46 50 25 --- 35
R08 | 1590 12 12 19 19 58 9 | 18 34 29 26 28 23
R10 | 883 12 13 33 25 --- 12 | 19 23 41 21 --- 19
R11 | 1272 29 8 22 27 136 12 | 26 25 28 17 25 20
R13 | 1687 14 16 20 15 --- 9 | 23 38 25 21 --- 25
R14 | 4443 25 18 21 21 --- 12 | 16 27 36 25 --- 18
R15 | 2049 16 11 19 24 --- 10 | 27 22 21 31 --- 21
R17E | 1363 14 15 31 25 --- 12 | 24 27 38 35 --- 26
R18E | 1960 35 14 16 34 --- 15 | 25 40 45 35 --- 33
R19E | 682 18 13 27 21 --- 11 | 49 47 60 54 --- 49
R20E | 1303 19 10 18 22 --- 10 | 53 60 74 72 --- 62
R21E | 618 17 12 29 27 --- 12 | 23 37 48 45 --- 34
R22E | 1040 21 21 28 18 --- 13 | 35 39 63 60 --- 44
R23E | 4734 30 24 41 27 --- 17 | 9999 9999 9999 9999 --- 9999
R24E | 5197 52 25 39 17 --- 20 | 158 181 185 170 --- 172
------+------------------------------------+--------------------------------
RMS | 2973 23 16 26 23 104 |T 35 43 50 42 26 39
WRMS | 2973 19 14 23 23 104 |NE 21 30 31 23 26 22
MEDI | 1687 17 14 22 22 58 |MD 24 34 38 26 25 25
Table 3.1546.1 GPS week: 1546 Day: 1 MJD: 55067
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 19 17 31 20 --- 12 | 18 25 46 20 --- 22
R03 |>>>>> 24 10 22 20 --- 11 | 18 30 48 30 --- 28
R07 |>>>>> 14 15 20 16 --- 9 | 37 34 40 33 --- 32
R08 |>>>>> 24 12 17 29 44 12 | 20 28 27 23 34 20
R10 |>>>>> 13 8 14 22 --- 8 | 19 22 30 32 --- 24
R11 |>>>>> 23 16 17 24 140 11 | 27 27 40 25 25 26
R13 |>>>>> 16 20 29 17 --- 12 | 11 23 30 12 --- 14
R14 |>>>>> 16 14 17 25 --- 10 | 22 34 35 27 --- 25
R15 |>>>>> 14 13 22 31 --- 12 | 20 22 29 26 --- 18
R17E |>>>>> 21 18 29 31 --- 14 | 29 25 57 41 --- 30
R18E |>>>>> 32 15 18 29 --- 13 | 26 28 32 35 --- 24
R19E |>>>>> 26 18 23 29 --- 13 | 42 45 62 59 --- 48
R20E |>>>>> 25 17 27 16 --- 12 | 34 53 61 44 --- 45
R21E |>>>>> 15 12 21 26 --- 10 | 21 34 45 37 --- 32
R22E |>>>>> 29 13 17 38 --- 14 | 18 28 33 35 --- 23
XR23E |>>>>> --- 301 429 2633 --- 360 | --- 9999 9999 9999 --- 9999
R24E |>>>>> 38 31 26 31 --- 18 | 120 100 106 116 --- 105
------+------------------------------------+--------------------------------
RMS |>>>>> 23 16 22 26 104 |T 30 34 45 37 29 32
WRMS |>>>>> 22 15 21 26 104 |NE 21 27 36 25 29 23
MEDI |>>>>> 21 15 22 26 44 |MD 21 28 40 32 25 25
Table 3.1546.2 GPS week: 1546 Day: 2 MJD: 55068
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 5662 20 9 26 18 --- 10 | 24 23 28 16 --- 17
R03 | 5061 10 9 33 22 --- 11 | 24 20 23 31 --- 17
R07 | 6475 13 25 42 22 --- 15 | 22 33 39 18 --- 16
R08 | 1232 21 16 13 31 54 12 | 34 25 30 18 42 21
R10 | 924 18 11 18 16 --- 9 | 23 20 31 21 --- 19
R11 | 971 22 20 33 19 147 13 | 33 27 32 22 37 21
R13 | 1411 13 11 25 21 --- 10 | 22 19 23 13 --- 14
R14 | 1029 9 18 20 19 --- 9 | 24 27 23 16 --- 18
R15 | 4664 24 18 22 23 --- 12 | 41 28 36 25 --- 23
R17E | 1838 17 11 27 30 --- 12 | 28 29 51 50 --- 31
R18E | 1889 23 19 23 18 --- 12 | 36 31 42 34 --- 31
R19E | 1803 29 17 29 37 --- 16 | 32 23 41 39 --- 25
R20E | 4683 34 21 40 22 --- 17 | 42 51 63 50 --- 46
R21E | 763 14 15 27 26 --- 11 | 28 29 33 41 --- 28
R22E | 1384 19 15 25 39 --- 14 | 34 37 47 57 --- 38
XR23E |26034 --- 1177 2098 3291 --- 1571 | --- 9999 9999 9999 --- 9999
R24E | 5568 18 25 35 24 --- 14 | 137 147 146 166 --- 147
------+------------------------------------+--------------------------------
RMS | 3476 20 17 28 25 111 |T 36 35 43 38 39 32
WRMS | 3476 20 15 25 25 111 |NE 27 24 29 20 39 18
MEDI | 1838 18 17 27 22 54 |MD 28 27 33 25 37 21
Table 3.1546.3 GPS week: 1546 Day: 3 MJD: 55069
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2417 16 21 17 20 --- 11 | 15 35 32 30 --- 22
R03 | 3192 10 16 15 15 --- 8 | 39 35 51 40 --- 37
R07 | 4314 27 11 32 13 --- 12 | 34 55 84 50 --- 53
R08 | 1634 12 33 30 21 124 15 | 20 38 25 20 108 18
R10 | 1687 14 13 34 18 --- 12 | 33 25 31 43 --- 27
R11 | 889 23 25 37 31 76 17 | 31 31 40 29 44 21
R13 | 1429 15 16 20 29 --- 12 | 22 28 26 22 --- 18
R14 | 4183 23 18 15 12 --- 10 | 23 27 32 19 --- 20
R15 | 3156 13 13 11 16 112 8 | 18 18 29 19 55 17
R17E | 3088 32 20 33 37 --- 17 | 37 44 60 43 --- 34
R18E | 1570 31 20 31 23 --- 15 | 26 30 39 35 --- 26
R19E | 2478 33 28 32 23 --- 16 | 36 29 53 53 --- 36
R20E | 2642 45 17 30 26 --- 17 | 33 34 59 39 --- 37
R21E | 1235 29 16 17 28 --- 13 | 26 33 43 45 --- 31
R22E | 605 18 18 40 23 --- 14 | 24 37 47 32 --- 26
R23E |20974 48 18 20 35 --- 18 | 752 9999 9999 9999 --- 9999
R24E | 2375 55 29 46 40 --- 24 | 103 148 159 130 --- 133
------+------------------------------------+--------------------------------
RMS | 5651 29 20 29 25 106 |T 74 40 50 40 69 34
WRMS | 5651 25 18 23 25 106 |NE 26 32 38 30 69 25
MEDI | 2417 23 18 30 23 112 |MD 31 33 40 35 55 26
Table 3.1546.4 GPS week: 1546 Day: 4 MJD: 55070
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1566 17 13 16 13 --- 8 | 25 29 36 21 --- 23
R03 |13961 21 18 29 12 --- 12 | 32 42 34 28 --- 28
R07 | 2941 20 8 22 28 --- 11 | 41 39 56 30 --- 36
R08 | 1219 21 24 16 26 80 13 | 38 40 45 26 45 32
R10 | 2006 14 15 24 23 --- 11 | 38 32 49 18 --- 30
R11 | 795 23 26 25 33 63 15 | 42 39 42 21 25 31
R13 | 1924 17 10 20 16 --- 9 | 28 19 33 20 --- 19
R14 | 4718 17 12 19 16 --- 9 | 30 24 24 13 --- 16
R15 | 2159 17 11 11 16 92 8 | 30 19 25 18 8 19
R17E | 1748 23 29 44 34 --- 19 | 29 25 57 43 --- 23
R18E | 956 25 17 41 35 --- 17 | 38 20 53 39 --- 25
R19E | 1843 32 16 23 26 --- 14 | 23 22 42 46 --- 27
R20E | 1021 31 27 43 32 --- 19 | 31 27 69 41 --- 31
R21E | 2333 26 16 32 33 --- 15 | 36 24 43 41 --- 28
R22E | 765 38 20 25 49 --- 19 | 42 36 38 54 --- 36
R23E |11496 62 32 29 42 117 24 | 604 9999 9999 9999 14 9999
R24E | 953 31 18 41 23 --- 16 | 164 139 124 144 --- 140
------+------------------------------------+--------------------------------
RMS | 4791 28 19 29 29 90 |T 74 36 48 37 23 34
WRMS | 4791 24 14 25 29 90 |NE 33 31 38 21 26 26
MEDI | 1843 23 17 25 26 80 |MD 36 27 42 28 14 28
Table 3.1546.5 GPS week: 1546 Day: 5 MJD: 55071
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 791 14 17 33 19 --- 12 | 22 21 30 22 --- 17
R03 |14565 24 22 21 15 --- 12 | 34 30 33 20 --- 21
R07 | 2153 13 9 13 19 --- 8 | 37 33 37 29 --- 31
R08 | 1528 12 23 15 24 58 11 | 31 42 35 15 28 30
R10 | 2774 20 18 23 24 --- 12 | 32 30 41 24 --- 27
R11 | 901 37 20 32 31 66 17 | 41 31 33 19 13 23
R13 | 1320 19 15 38 18 --- 13 | 19 14 42 16 --- 13
R14 | 5541 17 19 30 27 --- 13 | 23 18 41 25 --- 13
R15 | 850 15 15 16 19 100 9 | 15 15 21 16 7 10
R17E | 695 22 22 32 36 --- 16 | 33 27 51 46 --- 31
R18E | 712 33 17 33 32 --- 16 | 23 31 39 39 --- 26
R19E | 885 21 18 33 30 --- 14 | 31 21 51 48 --- 29
R20E | 1299 39 27 42 31 --- 20 | 41 36 70 38 --- 37
R21E | 2113 22 26 31 32 --- 16 | 28 24 46 42 --- 27
R22E | 1829 39 20 42 34 --- 19 | 21 26 45 38 --- 21
R23E | 4372 29 27 23 43 128 18 | 481 9999 9999 897 14 9999
R24E | 2304 43 26 31 34 --- 19 | 104 129 134 110 --- 116
------+------------------------------------+--------------------------------
RMS | 4180 26 21 30 28 92 |T 59 33 46 84 15 29
WRMS | 4180 25 18 28 28 92 |NE 28 26 34 20 16 20
MEDI | 1528 22 20 31 30 66 |MD 31 27 41 29 13 26
Table 3.1546.6 GPS week: 1546 Day: 6 MJD: 55072
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1064 21 10 25 17 --- 10 | 29 22 25 19 --- 19
R03 | 9918 17 21 24 24 --- 12 | 20 36 22 22 --- 21
R07 | 4375 21 18 27 14 --- 11 | 39 35 35 27 --- 31
R08 | 1325 28 13 17 26 79 12 | 49 37 36 17 55 29
R10 | 2611 20 14 37 30 --- 14 | 28 23 39 26 --- 20
R11 | 1058 23 10 28 20 73 11 | 40 30 34 26 22 27
R13 | 867 22 14 27 24 --- 12 | 24 19 27 15 --- 12
R14 | 4288 20 12 23 18 --- 10 | 24 17 29 20 --- 15
R15 | 1040 17 8 18 19 84 8 | 20 18 29 22 8 17
R17E | 787 26 13 24 42 --- 15 | 37 29 34 42 --- 27
R18E | 726 63 26 26 31 --- 21 | 39 21 37 31 --- 22
R19E | 1118 57 21 33 35 --- 20 | 26 40 48 52 --- 35
R20E | 1726 48 28 62 38 --- 25 | 36 30 74 46 --- 35
R21E | 1842 40 21 33 32 --- 17 | 24 20 42 47 --- 25
R22E | 2456 39 21 22 31 --- 16 | 29 24 37 42 --- 26
R23E | 8621 46 23 22 46 162 19 | 725 9999 9999 9999 14 9999
R24E | 3033 25 12 24 22 --- 11 | 177 180 177 185 --- 179
------+------------------------------------+--------------------------------
RMS | 3811 34 18 29 29 106 |T 80 36 45 39 24 33
WRMS | 3811 34 15 25 29 106 |NE 30 26 30 21 28 21
MEDI | 1726 25 14 25 26 79 |MD 29 24 35 26 14 25
More information about the IGSREPORT
mailing list