[IGSREPORT-17718] Wk 1543 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Aug 20 06:01:46 PDT 2009
******************************************************************************
IGS Electronic Report 20 Aug 06:02:08 PDT 2009 Message Number 17718
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1543 (Aug 02, 2009 - Aug 08, 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 2.1543.
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:
igl1543[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1543 in the SP3 format.
igl15437.sum Combination Report for GPS Week 1543.
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 | 212.2 ns
1 | 208.0 ns
2 | 211.6 ns
3 | 135.0 ns
4 | 157.8 ns
5 | 154.4 ns
6 | 222.0 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 1.1543, 1a.1543).
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 2.1543.0-6)
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 3.1543.0-6).
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 1543 summary. (Aug 02, 2009 - Aug 08, 2009)
Table 1.1543.a GPS week : 1543 MJD: 55045.0-55051.0
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 110| 2 0 -13 5 0 -8 -.12 31 25 | 0 -253 3730 4337
| 1 1 5 31 30 167 .06 | 0 1075
cod 236| -3 0 -4 4 -3 65 -.15 16 13 | --- --- --- ---
| 1 1 1 19 22 51 .01 | --- ---
esx 129| 1 1 0 14 14 59 .44 24 21 | 76297 -109 5671 11155
| 1 1 3 33 28 64 .04 | 37564 3562
iac n/a| 3 0 15 -31 -12 -179 -.08 24 24 | 185670 -144 5662 11145
| 1 1 7 12 17 46 .05 | 34926 2822
mcc n/a| 1 4 35 -34 -26 0 .30 139 139 | --- --- --- ---
| 5 6 8 85 101 725 .29 | --- ---
Table 1.1543.b GPS week : 1543 MJD: 55045.0-55051.0
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 | 10 10 8 7 9 12 9 |
R03 | 9 13 8 9 11 11 11 |
R07 | 11 12 9 11 14 11 9 |
R08 | 9 10 9 11 12 11 11 |
R10 | 11 16 13 14 10 13 13 |
R11 | 13 12 11 13 15 15 10 |
R13 | 8 10 9 12 10 13 13 |
R14 | 10 9 10 11 13 10 12 |
R15 | 15 12 12 8 15 15 10 |
R17 | 13 14 12 20 12 16 16 |
R18 | 9 11 9 10 9 14 14 |
R19 | 9 8 9 9 9 15 14 |
R20 | 18 13 11 11 13 14 16 |
R21 | 12 11 10 14 14 16 23 |
R22 | 11 9 11 10 9 14 13 |
R23 | 16 15 18 17 15 15 16 |
R24 | 14 14 19 41 47 13 19 |
Table 1.1543.c GPS week : 1543 MJD: 55045.0-55051.0
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 1543 0 | 120 65 518 104 -1012 -17730 83.7 2639 2639 | 212191 0
brd 1543 1 |43020 ---- -1022 -33980 -32549 799000 10.8 >>>>> >>>>> | 207976 0
brd 1543 2 | 41 149 371 -2530 -1117 -19880 88.4 3718 3718 | 211638 0
brd 1543 3 | -7 -21 241 7 298 -26660 86.5 4078 4078 | 135016 0
brd 1543 4 | -67 70 424 -2021 -1209 -20180 88.5 3452 3452 | 157823 0
brd 1543 5 | 36 -173 424 2963 1233 -15490 89.4 2935 2935 | 154382 0
brd 1543 6 | -18 -7 418 -1416 -1309 -13250 88.3 3129 3129 | 222012 0
-------------+------------------------------------------------------------+----------------
brd 1543 mean| 6160 -6055 196 -5267 -5095 97972 76.5 >>>>> >>>>> | 185862 0
brd 1543 sdev|16253 16057 544 12791 12143 309152 29.1 >>>>> >>>>> | 35392 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 2.1543.0 GPS week: 1543 Day: 0 MJD: 55045
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 110| 4 0 -18 -25 9 44 -.17 22 22 | 0 -564 3161 3470
cod 236| -4 -1 -4 4 6 107 -.16 16 15 | --- --- --- ---
esx 129| 1 1 2 48 9 -56 .48 20 19 | 110351 845 5668 10752
iac n/a| 3 -1 20 -39 -8 -147 -.05 23 23 | 211448 -1598 5680 10323
mcc n/a| 7 0 26 -100 2 -1072 .03 157 157 | --- --- --- ---
Table 2.1543.1 GPS week: 1543 Day: 1 MJD: 55046
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 110| 1 2 -16 9 3 -2 -.14 25 25 | 0 -1259 3987 4771
cod 236| -5 0 -6 17 -7 56 -.14 13 13 | --- --- --- ---
esx 129| 2 2 0 -19 61 71 .44 24 22 | 106618 5373 5694 12657
iac n/a| 5 -1 24 -27 -12 -169 -.03 22 22 | 207528 4939 5655 13063
mcc n/a| 0 16 27 -161 -53 -709 .43 143 143 | --- --- --- ---
Table 2.1543.2 GPS week: 1543 Day: 2 MJD: 55047
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 110| 1 -1 -11 7 -47 100 -.09 20 19 | 0 -155 3949 4542
cod 236| -4 -1 -3 18 15 34 -.15 13 11 | --- --- --- ---
esx 129| 0 2 -6 6 36 22 .45 23 18 | 102702 1720 4455 13673
iac n/a| 3 1 23 -39 -44 -238 -.01 24 24 | 209229 1346 4458 13756
mcc n/a| -9 2 43 1 -225 -152 .59 137 137 | --- --- --- ---
Table 2.1543.3 GPS week: 1543 Day: 3 MJD: 55048
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 110| 2 -1 -7 -1 45 139 -.10 38 26 | 0 1828 4743 5768
cod 236| -2 -2 -2 21 3 28 -.13 20 14 | --- --- --- ---
esx 129| 0 0 -2 -7 4 112 .45 27 22 | 24581 -62 6020 10249
iac n/a| 1 2 8 -18 -21 -250 -.11 23 23 | 135545 116 6002 10742
mcc n/a| 0 -1 50 91 7 194 .04 145 145 | --- --- --- ---
Table 2.1543.4 GPS week: 1543 Day: 4 MJD: 55049
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 110| 1 -2 -7 26 16 138 .01 38 25 | 0 -1133 4321 4977
cod 236| -2 0 -3 -27 18 -8 -.16 18 12 | --- --- --- ---
esx 129| 1 1 -1 71 1 45 .37 29 23 | 47049 -4390 6933 10074
iac n/a| 3 -1 9 -51 -5 -146 -.07 31 31 | 158589 -3830 6905 9663
mcc n/a| 5 0 35 27 -36 40 -.03 151 151 | --- --- --- ---
Table 2.1543.5 GPS week: 1543 Day: 5 MJD: 55050
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 110| 1 0 -20 59 -30 -283 -.19 37 33 | 0 -845 2914 3503
cod 236| -4 1 -1 -18 -47 108 -.16 16 14 | --- --- --- ---
esx 129| 1 0 3 -14 20 82 .48 21 20 | 38892 648 4947 10020
iac n/a| 3 0 9 -23 -2 -135 -.14 25 25 | 154342 136 4948 9786
mcc n/a| 7 5 36 -17 12 787 .33 106 106 | --- --- --- ---
Table 2.1543.6 GPS week: 1543 Day: 6 MJD: 55051
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 110| 3 0 -12 -33 0 -195 -.12 37 27 | 0 352 3036 3332
cod 236| -3 0 -7 17 -12 130 -.13 17 12 | --- --- --- ---
esx 129| -2 1 -1 13 -28 140 .40 27 25 | 103887 -4899 5985 10663
iac n/a| 5 0 16 -17 10 -170 -.12 21 21 | 223013 -2117 5990 10685
mcc n/a| -1 9 32 -80 105 905 .69 134 134 | --- --- --- ---
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 3.1543.0 GPS week: 1543 Day: 0 MJD: 55045
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2974 13 13 23 18 --- 10 | 16 25 24 25 --- 18
R03 | 4647 19 14 12 13 --- 8 | 14 31 27 26 --- 21
R07 | 1409 18 19 14 20 --- 10 | 26 32 32 28 --- 25
R08 | 901 19 11 15 15 254 8 | 22 17 21 23 44 16
R10 | 2858 14 17 28 11 --- 11 | 19 20 31 21 --- 13
R11 | 901 25 12 28 26 155 13 | 22 22 45 11 31 20
R13 | 830 10 13 14 14 --- 7 | 11 20 25 16 --- 15
R14 | 4260 15 13 21 16 --- 9 | 9 17 34 17 --- 15
R15 | 4271 25 11 23 41 51 15 | 15 22 34 15 29 17
R17 | 1402 34 9 20 20 --- 12 | 33 54 60 53 --- 50
R18 | 1797 15 15 20 11 --- 9 | 13 25 20 25 --- 17
R19 | 1039 16 12 19 14 --- 9 | 71 70 72 69 --- 70
R20 | 2331 30 21 24 46 --- 17 | 31 33 34 39 --- 30
R21 | 1271 23 18 13 24 --- 11 | 30 35 32 34 --- 28
R22 | 1837 12 20 18 19 --- 10 | 69 70 71 63 --- 67
R23 | 3258 36 10 20 37 91 15 | 37 60 76 78 94 61
R24 | 3427 26 27 21 16 --- 13 | 297 298 303 291 --- 297
------+------------------------------------+--------------------------------
RMS | 2639 22 16 20 23 157 |T 43 50 55 49 49 45
WRMS | 2639 22 15 19 23 157 |NE 43 50 55 49 49 45
MEDI | 1837 19 13 20 18 91 |MD 22 31 34 26 31 21
Table 3.1543.1 GPS week: 1543 Day: 1 MJD: 55046
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 12 13 16 25 --- 10 | 17 26 36 29 --- 23
R03 |>>>>> 15 16 33 20 --- 12 | 15 27 23 27 --- 17
R07 |>>>>> 19 11 24 27 --- 11 | 33 29 33 29 --- 24
R08 |>>>>> 21 15 12 20 210 10 | 17 32 31 17 23 21
R10 | ---- 32 18 40 21 --- 16 | 15 23 51 22 --- 20
R11 |>>>>> 20 15 28 17 150 11 | 25 17 35 13 20 16
R13 |>>>>> 16 11 25 17 --- 10 | 14 19 39 23 --- 18
R14 |55074 20 10 12 18 --- 8 | 15 17 27 21 --- 14
R15 |>>>>> 20 11 19 29 81 11 | 19 18 33 22 24 17
R17 |>>>>> 40 13 15 30 --- 14 | 28 53 55 52 --- 46
R18 |>>>>> 29 9 20 16 --- 10 | 16 22 24 28 --- 19
R19 |>>>>> 13 11 19 14 --- 8 | 62 60 60 57 --- 58
R20 |>>>>> 30 12 24 26 --- 13 | 36 44 52 43 --- 42
R21 |>>>>> 21 15 22 20 --- 11 | 29 26 24 35 --- 22
R22 |>>>>> 19 9 18 15 --- 8 | 61 61 60 57 --- 59
R23 |>>>>> 38 17 26 24 94 15 | 26 45 59 52 67 42
R24 |>>>>> 35 17 27 19 --- 14 | 282 271 289 267 --- 276
------+------------------------------------+--------------------------------
RMS |>>>>> 25 13 24 22 143 |T 41 46 54 46 33 43
WRMS |>>>>> 25 13 22 22 143 |NE 41 46 54 46 33 43
MEDI |>>>>> 20 13 22 20 94 |MD 25 27 36 29 23 22
Table 3.1543.2 GPS week: 1543 Day: 2 MJD: 55047
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1835 14 7 14 21 --- 8 | 18 18 25 22 --- 17
R03 |12521 12 8 15 19 --- 7 | 20 19 35 25 --- 21
R07 | 1629 12 10 24 17 --- 9 | 23 23 37 32 --- 24
R08 | 1929 17 13 9 20 144 8 | 20 30 25 26 29 21
R10 | 3130 23 16 24 29 --- 12 | 17 25 30 21 --- 17
R11 | 830 19 16 26 15 118 11 | 21 27 34 17 36 21
R13 | 2780 17 11 15 23 --- 9 | 17 18 31 32 --- 17
R14 | 2837 14 11 10 32 --- 10 | 12 22 25 30 --- 17
R15 | 1054 23 9 16 31 114 11 | 15 24 40 27 31 23
R17 | 1086 21 16 21 25 --- 11 | 51 72 71 73 --- 68
R18 | 1430 17 12 18 15 --- 8 | 10 30 37 31 --- 25
R19 | 949 11 13 12 21 --- 8 | 65 76 71 63 --- 68
R20 | 2850 23 13 17 24 --- 11 | 46 54 43 45 --- 46
R21 | 3320 7 13 25 22 --- 10 | 30 21 46 35 --- 27
R22 | 1255 16 11 20 27 --- 10 | 52 59 63 52 --- 55
R23 | 2947 30 20 45 29 164 17 | 38 48 86 70 90 54
R24 | 2741 41 16 44 30 --- 19 | 304 306 317 308 --- 306
------+------------------------------------+--------------------------------
RMS | 3717 20 13 23 24 137 |T 44 51 59 53 46 48
WRMS | 3717 19 11 18 24 137 |NE 44 51 59 53 46 48
MEDI | 1929 17 13 18 23 118 |MD 21 27 37 32 31 24
Table 3.1543.3 GPS week: 1543 Day: 3 MJD: 55048
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2524 10 11 10 15 --- 7 | 16 19 24 26 --- 17
R03 |14641 16 12 15 20 --- 9 | 27 24 36 24 --- 25
R07 | 1672 23 14 24 16 --- 11 | 38 43 36 33 --- 35
R08 | 2196 22 9 28 17 96 11 | 22 22 36 26 34 21
R10 | 2034 36 12 26 22 --- 13 | 27 20 30 26 --- 13
R11 | 1130 13 23 28 20 100 12 | 22 27 29 25 47 14
R13 | 2637 32 12 28 9 --- 12 | 22 16 29 16 --- 11
R14 | 3691 31 9 21 13 --- 10 | 10 28 33 25 --- 23
R15 | 1915 23 7 14 14 115 8 | 26 20 36 28 46 23
R17 | 1071 46 23 44 26 --- 19 | 47 58 74 59 --- 58
R18 | 1411 18 11 24 18 --- 10 | 26 32 40 25 --- 27
R19 | 1074 16 13 15 14 --- 8 | 64 68 56 66 --- 63
R20 | 1864 16 12 20 26 --- 11 | 32 45 55 42 --- 40
R21 | 2787 24 12 23 35 --- 14 | 43 36 35 57 --- 39
R22 | 1879 14 18 19 17 --- 10 | 89 91 98 95 --- 92
R23 | 1802 29 23 23 40 226 17 | 51 48 62 86 217 58
R24 | 1541 122 57 58 42 --- 40 | 282 333 348 314 --- 316
------+------------------------------------+--------------------------------
RMS | 4078 38 20 27 23 145 |T 49 54 62 57 86 51
WRMS | 4078 26 14 22 23 145 |NE 49 54 62 57 86 51
MEDI | 1879 23 12 23 18 100 |MD 27 32 36 28 46 27
Table 3.1543.4 GPS week: 1543 Day: 4 MJD: 55049
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3176 19 12 13 20 --- 9 | 26 18 23 21 --- 16
R03 |11147 15 10 19 31 --- 11 | 19 21 25 26 --- 16
R07 | 3538 30 20 24 23 --- 13 | 22 38 45 24 --- 30
R08 | 2133 22 14 18 27 71 11 | 31 34 29 20 53 25
R10 | 2657 22 9 17 22 --- 10 | 17 17 24 21 --- 13
R11 | 993 15 12 45 26 146 15 | 35 34 71 36 54 39
R13 | 1723 24 7 18 18 --- 9 | 24 18 32 27 --- 20
R14 | 1847 30 8 36 12 --- 13 | 15 18 41 22 --- 19
R15 | 4152 35 12 35 20 60 14 | 22 27 46 22 39 24
R17 | 1059 35 9 12 24 --- 11 | 51 55 45 58 --- 50
R18 | 1322 23 8 11 18 --- 8 | 40 33 38 36 --- 33
R19 | 1132 25 10 14 16 --- 9 | 44 49 43 47 --- 44
R20 | 1626 28 19 25 22 --- 13 | 36 36 30 20 --- 24
R21 | 1658 19 16 31 31 --- 14 | 26 24 34 34 --- 18
R22 | 1345 20 11 15 20 --- 9 | 67 86 86 89 --- 83
R23 | 1572 26 16 17 44 247 15 | 52 40 56 68 206 47
R24 | 2375 119 55 75 85 --- 46 | 316 394 408 333 --- 363
------+------------------------------------+--------------------------------
RMS | 3452 38 18 29 31 150 |T 49 55 63 53 88 50
WRMS | 3452 25 12 23 31 150 |NE 49 55 63 53 88 50
MEDI | 1723 24 12 18 22 71 |MD 31 34 41 27 53 25
Table 3.1543.5 GPS week: 1543 Day: 5 MJD: 55050
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2127 28 10 16 29 --- 11 | 24 18 23 21 --- 15
R03 | 6035 18 13 16 30 --- 11 | 28 28 24 25 --- 23
R07 | 4895 20 11 15 29 --- 10 | 40 43 42 41 --- 39
R08 | 877 39 13 13 15 48 11 | 27 32 36 23 28 23
R10 | 2980 30 20 18 24 --- 13 | 15 28 27 21 --- 15
R11 | 2475 19 22 31 24 140 14 | 26 33 22 27 26 21
R13 | 1302 22 17 26 27 --- 13 | 22 28 31 25 --- 12
R14 | 1508 30 11 18 16 --- 10 | 17 35 56 33 --- 33
R15 | 4185 35 19 34 17 79 15 | 38 24 42 21 22 25
R17 | 1605 54 14 18 30 --- 16 | 30 52 53 42 --- 45
R18 | 1525 51 11 10 29 --- 14 | 21 38 35 42 --- 32
R19 | 1049 57 14 14 23 --- 15 | 121 125 106 109 --- 114
R20 | 2228 40 16 23 20 --- 13 | 50 53 49 54 --- 49
R21 | 773 37 19 30 28 --- 15 | 36 36 41 35 --- 27
R22 | 936 44 20 13 20 --- 13 | 189 207 209 208 --- 205
R23 | 2381 33 15 30 27 128 14 | 68 61 91 60 88 68
R24 | 5113 41 15 17 19 --- 12 | 210 203 214 208 --- 207
------+------------------------------------+--------------------------------
RMS | 2935 37 16 21 25 106 |T 56 61 64 58 41 56
WRMS | 2935 33 14 20 25 106 |NE 56 61 64 58 41 56
MEDI | 2127 35 15 18 24 79 |MD 30 36 42 35 26 32
Table 3.1543.6 GPS week: 1543 Day: 6 MJD: 55051
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1858 19 11 17 17 --- 9 | 19 15 24 21 --- 15
R03 | 6323 24 11 22 18 --- 10 | 19 18 29 27 --- 17
R07 | 2823 20 7 21 15 --- 8 | 28 31 44 31 --- 30
R08 | 825 18 13 26 18 67 10 | 26 41 24 32 47 30
R10 | 3570 28 14 31 21 --- 13 | 20 27 34 28 --- 21
R11 | 2568 14 11 30 15 146 10 | 21 24 40 26 31 23
R13 | 1589 30 14 30 23 --- 13 | 16 22 36 30 --- 21
R14 | 2296 32 15 19 16 --- 11 | 14 20 36 23 --- 18
R15 | 6705 26 8 16 19 98 9 | 9 16 37 11 18 15
R17 | 1709 47 21 17 27 --- 16 | 82 80 78 86 --- 79
R18 | 1677 41 20 18 17 --- 13 | 94 88 79 96 --- 86
R19 | 778 35 17 30 19 --- 13 | 137 171 166 156 --- 160
R20 | 1880 42 15 39 23 --- 16 | 39 61 80 62 --- 59
R21 | 999 72 34 27 31 --- 23 | 116 68 73 94 --- 81
R22 | 747 35 14 29 16 --- 13 | 177 218 227 198 --- 208
R23 | 3043 42 18 30 28 192 16 | 69 71 104 90 91 81
R24 | 4643 52 23 36 30 --- 19 | 205 185 192 200 --- 191
------+------------------------------------+--------------------------------
RMS | 3129 37 17 27 21 134 |T 64 68 76 71 46 66
WRMS | 3129 27 12 25 21 134 |NE 64 68 76 71 46 66
MEDI | 1880 32 14 27 19 98 |MD 28 41 44 32 31 30
More information about the IGSREPORT
mailing list