[IGSREPORT-16418] Wk 1485 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 10 06:55:26 PDT 2008
******************************************************************************
IGS Electronic Report 10 Jul 06:55:33 PDT 2008 Message Number 16418
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1485 (Jun 22, 2008 - Jun 28, 2008)
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 2.1485.
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:
igl1485[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1485 in the SP3 format.
igl14857.sum Combination Report for GPS Week 1485.
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 | 917.9 ns
1 | 864.1 ns
2 | 911.1 ns
3 | 906.8 ns
4 | 912.9 ns
5 | 829.9 ns
6 | 801.8 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 1.1485, 1a.1485).
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 2.1485.0-6)
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 3.1485.0-6).
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 1485 summary. (Jun 22, 2008 - Jun 28, 2008)
Table 1.1485.a GPS week : 1485 MJD: 54639.0-54645.0
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 67| 1 -1 -8 26 -35 39 -.05 42 37 | 0 -105 2559 2703
| 2 2 4 45 29 105 .11 | 0 177
cod 205| -2 0 -3 -11 1 74 -.11 30 27 | --- --- --- ---
| 2 2 3 71 45 87 .07 | --- ---
esx 120| 0 -1 1 0 91 -35 .37 56 43 | 26387 2727 7992 16610
| 3 4 5 21 42 134 .18 | 39230 9607
iac n/a| 3 1 10 9 -37 -96 -.12 37 37 | 878687 -1948 7778 14607
| 1 2 9 42 53 81 .17 | 45701 5613
mcc n/a| -5 0 42 18 -58 -1393 .33 247 247 | --- --- --- ---
| 14 11 37 162 206 878 .60 | --- ---
Table 1.1485.b GPS week : 1485 MJD: 54639.0-54645.0
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
------+------------------------------------+------------------------------------------
R04 | 23 25 23 27 19 25 28 |
R06 | 29 36 30 31 35 54 34 |
R07 | 35 27 33 42 22 36 45 |
R10 | 18 16 22 16 15 10 16 |
R11 | 23 16 18 19 18 16 18 |
R13 | 25 21 20 19 26 21 25 |
R14 | 12 13 13 12 15 10 10 |
R15 | 22 27 15 21 22 22 23 |
R17 | 22 26 38 29 17 16 15 |
R19 | 26 20 18 32 21 17 16 |
R20 | 18 27 16 14 11 14 17 |
R23 | 23 29 32 27 16 23 33 |
R24 | 19 19 13 18 19 19 19 |
Table 1.1485.c GPS week : 1485 MJD: 54639.0-54645.0
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 1485 0 | 128 -48 453 -967 -4498 -9843 96.4 5232 5232 | 917924 0
brd 1485 1 | -135 -209 494 -3368 1229 -19770 99.5 >>>>> >>>>> | 864106 0
brd 1485 2 | -384 291 686 -3062 -2951 -26840 90.0 5506 5506 | 911110 0
brd 1485 3 | -139 -87 440 3074 -549 -18170 99.3 5514 5514 | 906773 0
brd 1485 4 | 296 62 608 -2376 828 -21380 92.2 5470 5470 | 912934 0
brd 1485 5 | 187 -307 483 -5551 4936 -14640 96.1 4748 4748 | 829850 0
brd 1485 6 | 4 31 529 2295 4059 -9006 107.7 4122 4122 | 801786 0
-------------+------------------------------------------------------------+----------------
brd 1485 mean| -6 -38 527 -1422 436 -17092 97.3 >>>>> >>>>> | 877783 0
brd 1485 sdev| 232 194 89 3127 3438 6399 5.7 >>>>> >>>>> | 46651 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 2.1485.0 GPS week: 1485 Day: 0 MJD: 54639
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 67| 0 0 -7 12 -95 -111 .02 36 33 | 0 172 2964 3189
cod 205| 0 -2 -6 59 57 -28 -.14 28 27 | --- --- --- ---
esx 120| -1 -4 -3 -28 156 111 .71 55 55 | 46707 6507 8834 15098
iac n/a| 5 1 22 -5 -92 71 -.48 38 38 | 919593 -1438 9057 14654
mcc n/a| -20 -21 -37 -216 299 -454 -.69 271 271 | --- --- --- ---
Table 2.1485.1 GPS week: 1485 Day: 1 MJD: 54640
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 67| 2 -4 -2 79 -9 184 .07 40 40 | 0 -291 2051 2136
cod 205| -3 0 -1 4 -63 26 .01 33 30 | --- --- --- ---
esx 120| -4 2 4 -19 106 -50 .19 49 58 | 51 6394 8018 16014
iac n/a| 2 1 -4 3 -24 -168 -.11 34 34 | 860648 1867 7828 13234
mcc n/a| -12 -2 50 16 -176 71 .90 744 744 | --- --- --- ---
Table 2.1485.2 GPS week: 1485 Day: 2 MJD: 54641
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 67| 0 -4 -4 72 -14 -64 -.00 45 42 | 0 108 1907 2106
cod 205| -1 2 -2 -20 4 149 -.10 27 27 | --- --- --- ---
esx 120| 1 -4 -2 0 47 -71 .40 56 38 | 56893 2700 6917 14204
iac n/a| 1 -2 8 -9 -11 -79 -.01 40 40 | 911538 -1297 6812 12410
mcc n/a| 4 4 60 244 -223 -1430 -.08 109 109 | --- --- --- ---
Table 2.1485.3 GPS week: 1485 Day: 3 MJD: 54642
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 67| 2 -1 -15 56 -44 69 .05 34 35 | 0 -228 2638 2794
cod 205| -4 2 -7 -161 55 131 -.14 33 31 | --- --- --- ---
esx 120| 0 3 -6 37 108 -282 .22 71 42 | 61051 -13800 8223 17311
iac n/a| 4 -1 24 99 -112 -90 -.10 41 41 | 911652 -9932 8096 16370
mcc n/a| 16 4 65 200 -84 -1930 .64 113 113 | --- --- --- ---
Table 2.1485.4 GPS week: 1485 Day: 4 MJD: 54643
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 67| 4 1 -9 6 -23 0 -.18 36 33 | 0 -223 2236 2356
cod 205| 1 -2 -6 23 12 204 -.19 33 28 | --- --- --- ---
esx 120| -5 -7 4 -2 116 -13 .44 45 31 | 62735 18009 7055 17295
iac n/a| 3 3 8 -3 -62 -124 -.12 28 28 | 908138 7467 6838 13820
mcc n/a| 0 -5 77 -99 -224 -1873 .20 140 140 | --- --- --- ---
Table 2.1485.5 GPS week: 1485 Day: 5 MJD: 54644
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 67| -2 1 -9 -49 -38 140 -.15 48 35 | 0 -121 3426 3580
cod 205| -4 1 0 22 -44 46 -.03 29 22 | --- --- --- ---
esx 120| 0 -3 6 13 61 -62 .36 70 43 | -13818 47 8220 17854
iac n/a| 2 2 5 -32 10 -123 -.06 33 33 | 835786 -5816 8005 16877
mcc n/a| -3 6 41 33 -158 -2358 .25 182 182 | --- --- --- ---
Table 2.1485.6 GPS week: 1485 Day: 6 MJD: 54645
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 67| 2 -4 -11 6 -24 56 -.16 56 40 | 0 -158 2695 2760
cod 205| -4 0 0 -6 -8 -6 -.16 30 20 | --- --- --- ---
esx 120| 4 3 9 -6 41 119 .30 43 34 | -28910 -764 8682 18500
iac n/a| 1 1 10 13 33 -161 .02 46 46 | 803459 -4493 7816 14890
mcc n/a| -24 15 41 -51 160 -1784 1.05 171 171 | --- --- --- ---
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 3.1485.0 GPS week: 1485 Day: 0 MJD: 54639
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 6666 27 35 63 35 --- 22 | 22 38 105 39 --- 34
R06E | 2170 51 36 42 68 --- 29 | 95 94 112 126 --- 100
XR07E | ---- 41 44 --- 61 --- 34 | 24 43 --- 54 --- 28
R10 | 1451 31 31 25 35 --- 18 | 35 51 53 65 --- 45
R11 | 8070 36 28 64 36 123 23 | 30 31 86 41 47 30
R13 | 9227 35 23 82 33 --- 24 | 31 29 86 31 --- 29
R14 | 1301 14 17 24 26 --- 11 | 26 31 41 27 --- 26
R15 | 7840 34 24 60 37 98 21 | 32 38 69 31 26 32
R17 | 6705 34 32 59 33 --- 22 | 50 41 87 59 --- 44
R19 | 1391 44 35 75 21 --- 25 | 46 39 92 55 --- 35
R20 | 1784 37 27 45 18 --- 18 | 33 61 59 57 --- 49
R23 | 1075 47 31 32 47 --- 23 | 51 53 52 61 --- 42
R24 | 3543 29 11 53 35 442 18 | 57 43 74 71 4 52
------+------------------------------------+--------------------------------
RMS | 5232 36 28 55 38 270 |T 40 45 76 55 25 42
WRMS | 5232 33 27 55 38 270 |NE 39 41 69 49 25 38
MEDI | 2170 35 31 53 35 123 |MD 33 41 74 55 26 35
Table 3.1485.1 GPS week: 1485 Day: 1 MJD: 54640
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E |>>>>> 34 46 55 35 --- 25 | 23 61 73 41 --- 37
XR06E |>>>>> --- 41 50 57 --- 35 | --- 118 119 134 --- 112
R07E | 6838 46 37 59 44 --- 26 | 37 47 53 51 --- 37
R10 |>>>>> 17 32 36 21 --- 16 | 31 30 54 45 --- 36
R11 |>>>>> 32 17 34 26 102 16 | 25 21 53 26 54 22
R13 |>>>>> 35 41 26 35 --- 20 | 25 49 54 40 --- 29
R14 |>>>>> 20 21 23 21 --- 12 | 41 36 40 22 --- 28
R15 |>>>>> 36 35 81 25 101 27 | 29 30 76 28 32 21
R17 |>>>>> 50 26 66 37 --- 26 | 45 27 88 42 --- 30
R19 |>>>>> 27 15 43 46 --- 20 | 17 18 42 35 --- 18
R20 |>>>>> 61 41 38 40 --- 26 | 25 53 35 34 --- 24
R23 |>>>>> 54 40 64 42 --- 28 | 33 53 74 38 --- 35
R24 |>>>>> 47 28 20 27 1281 18 | 85 63 64 50 5 56
------+------------------------------------+--------------------------------
RMS |>>>>> 40 33 49 34 744 |T 34 46 63 45 30 37
WRMS |>>>>> 40 30 58 34 744 |NE 35 38 58 36 30 29
MEDI |>>>>> 35 35 43 35 102 |MD 29 47 54 40 32 30
Table 3.1485.2 GPS week: 1485 Day: 2 MJD: 54641
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3179 46 29 49 39 --- 23 | 61 51 78 73 --- 57
R06E | 9212 69 34 55 56 --- 30 | 109 74 129 115 --- 87
R07E | 2121 60 42 74 55 --- 32 | 41 59 72 67 --- 34
R10 | 2269 31 34 41 42 --- 21 | 30 28 66 52 --- 31
R11 | 8005 47 15 37 21 70 17 | 17 24 42 34 69 20
R13 | 7133 35 34 25 40 --- 20 | 22 69 60 51 --- 46
R14 | 4015 18 21 23 24 --- 12 | 41 43 46 29 --- 36
R15 | 7427 14 21 30 33 138 14 | 25 32 65 30 31 32
R17 | 7294 68 23 125 36 --- 38 | 26 34 119 39 --- 34
R19 | 1845 37 23 32 35 --- 18 | 19 31 50 54 --- 29
R20 | 2404 39 22 33 20 --- 16 | 37 54 40 39 --- 41
R23 | 1527 51 27 78 64 --- 31 | 56 61 46 62 --- 43
R24 | 6208 27 19 19 25 --- 13 | 29 64 70 61 --- 53
------+------------------------------------+--------------------------------
RMS | 5506 45 27 56 40 109 |T 39 48 67 54 50 41
WRMS | 5506 42 27 38 40 109 |NE 30 44 60 45 50 36
MEDI | 4015 39 23 37 36 70 |MD 30 51 65 52 31 36
Table 3.1485.3 GPS week: 1485 Day: 3 MJD: 54642
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4303 29 38 81 42 --- 26 | 36 57 98 48 --- 42
R06E | 6140 37 39 84 58 --- 30 | 119 151 178 173 --- 149
R07E | 3516 48 51 146 56 --- 42 | 33 35 136 60 --- 31
R10 | 2330 17 25 26 36 --- 15 | 50 42 39 69 --- 45
R11 | 5518 36 17 32 43 62 19 | 15 31 45 51 42 25
R13 | 4973 20 35 47 33 --- 19 | 40 48 69 52 --- 43
R14 | 2207 20 19 24 22 --- 12 | 29 51 50 24 --- 34
R15 | 5463 23 37 56 27 148 20 | 40 37 68 41 23 35
R17 |14230 61 29 82 26 --- 28 | 32 51 66 38 --- 35
R19 | 1331 30 20 101 67 --- 31 | 37 46 78 91 --- 38
R20 | 3465 23 16 31 25 --- 13 | 35 33 44 57 --- 37
R23 | 1489 34 50 53 47 --- 26 | 52 45 63 45 --- 32
R24 | 3573 40 21 46 15 --- 17 | 28 39 67 50 --- 36
------+------------------------------------+--------------------------------
RMS | 5513 34 33 71 41 113 |T 42 51 77 61 32 44
WRMS | 5513 35 31 42 41 113 |NE 35 42 58 51 32 36
MEDI | 3573 30 29 53 36 62 |MD 36 45 67 51 23 36
Table 3.1485.4 GPS week: 1485 Day: 4 MJD: 54643
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4802 47 30 32 20 --- 19 | 63 39 47 46 --- 34
R06E | 3370 60 61 57 59 --- 34 | 81 171 176 159 --- 140
R07E | 4576 32 37 54 31 --- 22 | 28 29 66 38 --- 25
R10 | 2964 21 22 24 31 --- 14 | 24 30 42 41 --- 29
R11 | 5837 43 22 36 23 74 18 | 24 27 50 44 27 32
R13 | 5781 26 42 82 21 --- 26 | 17 45 87 32 --- 27
R14 | 1644 29 29 17 25 --- 15 | 37 57 45 25 --- 35
R15 | 3432 29 42 55 27 183 22 | 37 53 84 35 19 41
R17 |14213 14 17 57 24 --- 17 | 38 53 98 43 --- 48
R19 | 2416 40 29 44 32 --- 20 | 84 44 44 57 --- 51
R20 | 4312 23 14 23 13 --- 10 | 35 39 42 43 --- 38
R23 | 2684 27 23 38 25 --- 16 | 80 66 60 47 --- 56
R24 | 3027 49 34 25 11 --- 18 | 44 69 68 52 --- 52
------+------------------------------------+--------------------------------
RMS | 5470 36 33 45 28 140 |T 45 55 69 50 23 46
WRMS | 5470 33 28 31 28 140 |NE 42 48 62 41 23 40
MEDI | 3432 29 29 38 25 74 |MD 37 45 60 43 19 38
Table 3.1485.5 GPS week: 1485 Day: 5 MJD: 54644
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2264 45 26 78 31 --- 24 | 48 31 67 44 --- 27
R06E | 4370 117 62 152 61 --- 53 | 151 294 344 255 --- 255
R07E | 2599 53 35 110 61 --- 35 | 34 53 92 81 --- 44
R10 | 3034 11 15 28 15 --- 10 | 41 40 57 41 --- 41
R11 | 2292 25 29 32 22 92 15 | 26 18 54 28 27 24
R13 |13211 18 27 76 23 --- 20 | 30 37 90 43 --- 31
R14 | 2522 20 18 18 15 --- 10 | 24 31 29 21 --- 23
R15 | 4136 42 30 59 30 240 22 | 49 43 53 41 16 38
R17 | 3389 38 19 42 19 --- 16 | 18 43 51 37 --- 34
R19 | 3018 42 23 30 23 --- 16 | 27 40 67 54 --- 40
R20 | 2792 27 16 34 23 --- 13 | 29 40 46 34 --- 31
R23 | 3816 28 28 71 39 --- 23 | 45 52 61 37 --- 40
R24 | 2577 54 12 41 24 --- 19 | 74 65 76 55 --- 60
------+------------------------------------+--------------------------------
RMS | 4748 48 29 70 33 182 |T 45 60 83 59 21 52
WRMS | 4748 35 22 43 33 182 |NE 36 40 58 39 21 36
MEDI | 3018 38 26 42 23 92 |MD 34 40 61 41 16 38
Table 3.1485.6 GPS week: 1485 Day: 6 MJD: 54645
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2263 71 26 61 32 --- 27 | 100 58 66 80 --- 65
R06E | 2504 88 42 51 54 --- 33 | 82 149 159 161 --- 136
R07E | 2849 118 56 58 80 --- 44 | 55 42 62 82 --- 37
R10 | 2711 24 29 21 32 --- 16 | 38 42 42 52 --- 42
R11 | 3641 29 25 37 33 89 18 | 27 24 46 29 37 24
R13 |10404 25 12 64 58 --- 24 | 26 27 53 34 --- 28
R14 | 2020 17 14 21 20 --- 10 | 31 45 37 38 --- 35
R15 | 5119 51 23 33 52 225 22 | 45 31 43 30 23 27
R17 | 1512 31 10 28 35 --- 15 | 32 49 59 56 --- 42
R19 | 3655 39 10 29 33 --- 16 | 33 41 54 54 --- 39
R20 | 1302 16 26 38 33 --- 17 | 30 39 54 61 --- 40
R23 | 3499 75 45 49 61 --- 32 | 37 51 61 58 --- 43
R24 | 3547 26 26 42 31 --- 18 | 84 90 114 92 --- 92
------+------------------------------------+--------------------------------
RMS | 4121 56 30 43 46 171 |T 47 52 65 63 30 50
WRMS | 4121 40 20 34 46 171 |NE 38 43 56 50 30 41
MEDI | 2849 31 26 38 33 89 |MD 37 42 54 56 23 40
More information about the IGSREPORT
mailing list