[IGSREPORT-18994] Wk 1600 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 23 08:39:48 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1600 (Sep 05, 2010 - Sep 11, 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 2.1600.
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:
igl1600[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1600 in the SP3 format.
igl16007.sum Combination Report for GPS Week 1600.
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 | 364.1 ns
1 | 458.3 ns
2 | 458.7 ns
3 | 459.2 ns
4 | 413.6 ns
5 | 421.1 ns
6 | 463.4 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
----+--------+---------------
3 | BKG | R03
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 1.1600, 1a.1600).
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 2.1600.0-6)
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 3.1600.0-6).
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 1600 summary. (Sep 05, 2010 - Sep 11, 2010)
Table 1.1600.a GPS week : 1600 MJD: 55444.0-55450.0
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 124| 0 0 -7 -14 -34 -16 -.11 26 25 | 0 -29 1978 2101
| 1 1 7 21 24 178 .06 | 0 158
cod 232| -1 0 2 38 -6 5 -.12 19 18 | --- --- --- ---
| 1 1 4 37 19 68 .03 | --- ---
esx 129| -1 0 6 9 37 2 .47 27 23 | 91864 -201 4474 8903
| 1 1 6 26 22 71 .04 | 35432 3707
gfz 195| 0 0 6 -44 -46 68 -.17 32 27 | 280828 141 4497 8567
| 2 3 8 41 73 58 .13 | 35856 3386
iac n/a| 0 0 -4 -60 -9 20 -.24 28 28 | 434051 -867 4488 8923
| 1 1 7 28 23 116 .06 | 37242 1896
mcc n/a| 4 -1 9 15 43 234 -.55 181 181 | --- --- --- ---
| 10 17 21 138 188 307 .50 | --- ---
Table 1.1600.b GPS week : 1600 MJD: 55444.0-55450.0
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 | 53 39 38 30 16 14 17 |
R02 | 15 14 15 13 12 13 10 |
R03 | 13 17 17 174 --- --- --- |
R04 | 11 10 14 12 12 12 10 |
R05 | 10 14 9 15 13 13 16 |
R07 | 11 11 11 15 13 14 15 |
R08 | 15 16 15 12 9 11 13 |
R10 | 10 11 16 14 11 9 10 |
R11 | 14 17 19 20 21 23 21 |
R13 | 12 9 9 12 10 12 12 |
R14 | 14 12 14 14 13 14 13 |
R15 | 12 13 11 12 12 10 11 |
R17 | 11 15 18 13 14 12 13 |
R18 | 11 10 12 14 9 11 11 |
R19 | 14 14 13 14 12 7 8 |
R20 | 14 13 15 20 15 12 10 |
R21 | 14 13 11 11 16 9 9 |
R22 | 11 13 15 18 11 11 11 |
R23 | 14 12 16 11 12 9 10 |
R24 | 11 11 9 13 10 12 10 |
Table 1.1600.c GPS week : 1600 MJD: 55444.0-55450.0
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 1600 0 | -48 -66 202 448 -3373 -15670 85.8 2265 2265 | 364065 0
brd 1600 1 | -27 44 270 -2546 866 -16570 87.1 2186 2186 | 458349 0
brd 1600 2 | -57 -141 472 -1218 -2887 -12610 86.4 2011 2011 | 458725 0
brd 1600 3 | 83 -12 426 1830 280 -7922 88.3 1902 1902 | 459212 0
brd 1600 4 | -85 49 266 -186 673 -11190 87.4 1714 1714 | 413574 0
brd 1600 5 | -104 -35 201 1438 -1571 -15700 85.3 2109 2109 | 421093 0
brd 1600 6 | 71 86 302 -613 769 -14900 84.6 2437 2437 | 463412 0
-------------+------------------------------------------------------------+----------------
brd 1600 mean| -23 -10 305 -120 -748 -13508 86.4 2089 2089 | 434061 0
brd 1600 sdev| 73 78 105 1521 1831 3113 1.3 239 239 | 36922 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 2.1600.0 GPS week: 1600 Day: 0 MJD: 55444
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 124| 2 1 -11 7 -42 38 -.18 32 24 | 0 -96 1678 1761
cod 232| -3 0 -2 0 -1 21 -.07 23 20 | --- --- --- ---
esx 129| 0 -2 13 13 52 54 .40 30 22 | 29479 -1721 4803 9321
gfz 195| 1 -4 13 -89 -86 84 -.25 31 26 | 214665 -1271 4795 8978
iac n/a| 1 0 1 -26 -51 -159 -.14 32 32 | 363904 516 4808 9400
mcc n/a| 5 -1 2 24 -140 66 -.96 174 174 | --- --- --- ---
Table 2.1600.1 GPS week: 1600 Day: 1 MJD: 55445
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 124| 1 0 -10 -36 3 94 -.08 28 29 | 0 151 1784 1836
cod 232| -2 -1 5 22 -20 -6 -.12 18 20 | --- --- --- ---
esx 129| -2 1 10 27 2 -22 .46 30 27 | 118622 3346 4997 8973
gfz 195| 3 0 17 -42 64 151 -.26 43 26 | 308721 758 5057 8358
iac n/a| 0 1 -14 -50 0 -101 -.22 31 31 | 458277 1245 5028 8882
mcc n/a| 1 -4 -17 -20 -212 -130 .08 171 171 | --- --- --- ---
Table 2.1600.2 GPS week: 1600 Day: 2 MJD: 55446
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 124| 0 -1 -9 13 -37 232 -.07 28 25 | 0 -42 1895 1969
cod 232| -3 -1 8 -10 -18 -106 -.11 20 18 | --- --- --- ---
esx 129| 0 -1 9 -32 52 -133 .50 33 26 | 118539 -4471 4257 7219
gfz 195| -2 5 11 11 -88 -25 -.26 38 25 | 310281 -2650 4300 7134
iac n/a| 2 -2 -11 -24 -21 49 -.25 29 29 | 459577 -2597 4245 7693
mcc n/a| 5 -5 2 117 2 553 -.29 293 293 | --- --- --- ---
Table 2.1600.3 GPS week: 1600 Day: 3 MJD: 55447
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 124| 0 -1 -18 0 -69 -304 -.04 32 32 | 0 -70 1838 1909
cod 232| -1 2 8 45 8 72 -.13 20 19 | --- --- --- ---
esx 129| -1 0 10 4 35 -1 .47 28 24 | 115762 -3155 4713 10609
gfz 195| -2 2 10 -67 -38 108 -.32 29 33 | 307485 -2573 4756 10394
iac n/a| 0 -1 -8 -63 24 189 -.32 27 27 | 460849 -3491 4791 10972
mcc n/a| 6 32 15 262 172 529 -.97 308 308 | --- --- --- ---
Table 2.1600.4 GPS week: 1600 Day: 4 MJD: 55448
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 124| -1 0 3 -42 -17 65 -.12 24 24 | 0 108 1776 1848
cod 232| 1 0 -1 60 -36 -35 -.15 17 17 | --- --- --- ---
esx 129| 0 0 -1 38 65 -10 .52 25 23 | 72882 -1913 5460 9900
gfz 195| -2 1 -3 -96 16 81 -.03 28 27 | 261152 -1791 5489 9437
iac n/a| -1 0 -2 -95 -5 37 -.29 22 22 | 413291 -2140 5453 9848
mcc n/a| -7 5 2 -107 -22 351 -.18 100 100 | --- --- --- ---
Table 2.1600.5 GPS week: 1600 Day: 5 MJD: 55449
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 124| -1 0 0 -22 -56 -84 -.07 21 21 | 0 62 1654 1749
cod 232| 0 -1 -1 96 -1 -6 -.18 17 17 | --- --- --- ---
esx 129| -1 0 -4 -16 36 44 .48 21 18 | 68649 618 3640 7743
gfz 195| 0 1 -4 -17 -32 15 -.01 24 26 | 264546 1645 3629 7377
iac n/a| 0 -1 6 -85 -3 65 -.25 27 27 | 419891 -649 3651 7438
mcc n/a| -3 -6 3 -23 291 435 -.28 106 106 | --- --- --- ---
Table 2.1600.6 GPS week: 1600 Day: 6 MJD: 55450
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 124| 0 -1 -6 -18 -20 -152 -.18 17 17 | 0 -321 3227 3639
cod 232| -1 0 2 57 22 97 -.12 20 18 | --- --- --- ---
esx 129| 0 0 5 31 15 84 .49 23 21 | 119118 5884 3450 8559
gfz 195| -4 0 2 -6 -159 65 -.05 30 27 | 298951 6871 3453 8293
iac n/a| 1 -1 -2 -79 -7 66 -.20 25 25 | 462568 1046 3446 8234
mcc n/a| 24 -27 53 -141 217 -168 -1.26 117 117 | --- --- --- ---
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 3.1600.0 GPS week: 1600 Day: 0 MJD: 55444
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1747 115 60 90 49 97 --- 52 | 85 57 101 71 81 --- 49
R02 | 1517 25 31 18 21 21 --- 14 | 16 39 26 28 15 --- 19
R03 | 3187 19 21 29 17 16 --- 12 | 27 189 27 24 23 --- 193
R04 | 827 20 11 20 23 25 --- 11 | 30 41 38 33 37 --- 33
R05 | 1166 17 10 20 26 19 --- 9 | 30 55 44 51 42 --- 42
R07 | 2604 21 15 17 30 19 --- 10 | 38 50 55 61 35 --- 43
R08 | 1401 26 29 17 21 26 89 14 | 38 72 46 45 45 57 49
R10 | 791 15 16 20 14 15 --- 9 | 32 39 37 28 43 --- 34
R11 | 1076 19 21 27 45 27 --- 13 | 51 65 81 82 56 --- 61
R13 | 4359 13 22 19 21 29 --- 12 | 24 32 31 38 33 --- 25
R14 | 2277 19 20 28 23 30 --- 14 | 30 35 39 29 35 --- 30
R15 | 3978 18 13 18 28 31 71 12 | 29 33 42 40 34 48 31
R17E | 1271 16 18 11 44 28 --- 11 | 48 63 61 74 63 --- 57
R18E | 3969 17 11 20 29 24 --- 10 | 46 55 64 68 60 --- 53
R19E | 1193 28 12 29 41 23 --- 13 | 92 113 133 109 99 --- 109
R20E | 1159 18 27 19 26 31 --- 14 | 55 72 74 77 58 --- 62
R21E | 702 20 21 31 20 24 --- 14 | 42 56 53 57 45 --- 46
R22E | 1402 12 16 25 41 18 --- 10 | 49 56 66 58 57 --- 55
R23E | 2795 22 20 24 26 27 280 13 | 47 53 57 61 55 184 50
R24E | 2006 17 15 18 35 25 --- 11 | 40 48 47 47 45 --- 43
------+-----------------------------------------+-------------------------------------
RMS | 2264 32 23 30 31 32 174 |T 42 61 56 54 48 96 54
WRMS | 2264 24 20 22 26 32 174 |NE 35 58 47 44 39 52 50
MEDI | 1402 19 18 20 26 25 89 |MD 38 55 47 51 45 57 46
Table 3.1600.1 GPS week: 1600 Day: 1 MJD: 55445
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2237 85 34 66 87 85 --- 38 | 32 56 86 116 83 --- 52
R02 | 1794 21 27 15 25 29 --- 14 | 26 34 31 30 27 --- 24
R03 | 2592 32 24 37 39 29 --- 17 | 24 220 35 41 21 --- 226
R04 | 804 16 12 22 25 20 --- 10 | 26 32 35 46 31 --- 28
R05 | 1193 18 15 32 17 30 --- 13 | 30 41 30 31 42 --- 32
R07 | 4231 19 15 24 29 14 --- 10 | 31 41 51 58 36 --- 38
R08 | 1533 30 30 18 31 25 36 15 | 47 51 48 38 29 38 42
R10 | 1568 19 13 20 26 23 --- 10 | 25 37 42 38 30 --- 30
R11 | 1043 25 25 28 43 41 --- 17 | 51 48 69 74 47 --- 51
R13 | 3300 21 9 20 25 13 --- 9 | 26 37 41 42 34 --- 31
R14 | 1862 17 15 10 23 34 --- 11 | 23 34 32 32 28 --- 27
R15 | 2410 18 13 25 27 31 87 12 | 33 28 47 51 30 40 29
R17E | 1317 22 17 41 47 21 --- 14 | 39 36 45 29 45 --- 34
R18E | 2969 16 10 24 49 18 --- 10 | 58 56 64 88 65 --- 58
R19E | 2434 20 18 26 36 32 --- 13 | 117 129 128 125 136 --- 125
R20E | 1713 15 15 32 33 27 --- 13 | 35 46 61 50 44 --- 42
R21E | 1578 27 14 33 98 17 --- 13 | 41 56 63 118 59 --- 53
R22E | 866 18 13 39 46 18 --- 13 | 49 49 69 68 51 --- 52
R23E | 3023 27 11 24 26 23 282 12 | 77 72 74 86 81 147 73
R24E | 1666 15 13 29 31 18 --- 11 | 29 32 45 37 25 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 2186 28 18 30 43 31 171 |T 40 56 54 59 47 75 53
WRMS | 2186 29 20 27 26 31 171 |NE 31 54 45 49 36 39 50
MEDI | 1713 19 15 25 31 23 87 |MD 32 41 47 46 36 40 38
Table 3.1600.2 GPS week: 1600 Day: 2 MJD: 55446
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2095 62 26 94 92 75 --- 37 | 45 73 142 102 93 --- 77
R02 | 1383 27 25 25 25 22 --- 14 | 20 32 25 27 26 --- 18
R03 | 1376 40 28 22 36 19 --- 16 | 35 293 30 26 10 --- 292
R04 | 739 13 26 32 17 19 --- 13 | 35 44 43 42 26 --- 32
R05 | 1100 15 14 17 28 11 --- 8 | 43 47 45 45 37 --- 41
R07 | 4810 20 13 21 29 19 --- 10 | 32 48 47 52 47 --- 40
R08 | 1597 19 32 29 29 17 56 15 | 43 49 33 50 22 31 34
R10 | 1980 23 18 29 35 38 --- 16 | 33 46 53 54 44 --- 39
R11 | 1608 32 28 26 49 40 --- 18 | 47 45 64 65 51 --- 47
R13 | 1965 14 11 24 19 14 --- 9 | 32 35 43 41 33 --- 31
R14 | 1417 18 19 16 29 38 --- 14 | 23 32 35 37 31 --- 26
R15 | 2469 17 14 21 24 24 68 11 | 35 35 39 33 29 33 30
R17E | 1885 32 25 38 26 29 --- 17 | 49 64 61 51 71 --- 55
R18E | 2088 23 15 26 50 17 --- 11 | 51 58 78 94 55 --- 57
R19E | 2306 25 11 30 26 21 --- 12 | 70 87 98 90 83 --- 82
R20E | 1450 30 17 31 46 24 --- 14 | 62 67 83 80 60 --- 62
R21E | 1837 20 11 19 17 22 --- 10 | 47 57 62 65 49 --- 51
R22E | 1608 33 17 30 53 22 --- 15 | 46 57 76 93 49 --- 54
R23E | 1659 33 20 30 27 26 500 15 | 48 54 61 67 54 105 50
R24E | 1647 19 10 20 31 13 --- 9 | 38 51 59 54 42 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 2011 28 20 33 38 29 293 |T 41 63 58 58 45 56 58
WRMS | 2011 25 18 26 25 29 293 |NE 35 64 49 47 37 32 58
MEDI | 1647 23 17 26 29 22 68 |MD 43 49 53 52 44 33 45
Table 3.1600.3 GPS week: 1600 Day: 3 MJD: 55447
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3611 72 41 44 47 49 --- 29 | 35 69 83 69 60 --- 46
R02 | 1763 24 20 20 36 26 --- 13 | 30 48 50 29 39 --- 37
XR03 | ---- 2058 89 --- --- 247 --- 174 | 42 343 --- --- 21 --- 361
R04 | 2073 22 21 14 35 22 --- 11 | 69 51 44 28 30 --- 44
R05 | 736 24 21 32 21 22 --- 14 | 42 46 51 43 36 --- 38
R07 | 2363 14 19 41 26 21 --- 15 | 47 42 35 46 35 --- 32
R08 | 1414 25 20 21 19 14 100 11 | 79 53 57 60 49 43 55
R10 | 1632 18 13 32 22 28 --- 13 | 43 31 48 36 33 --- 30
R11 | 1183 29 32 18 31 50 --- 20 | 75 51 58 60 68 --- 58
R13 | 1479 35 14 17 25 14 --- 12 | 45 46 58 57 40 --- 43
R14 | 1568 30 18 13 33 31 --- 13 | 37 36 36 45 32 --- 31
R15 | 1178 29 14 21 26 19 66 12 | 64 41 48 66 44 48 46
R17E | 2216 31 12 20 25 22 --- 12 | 65 55 69 63 46 --- 54
R18E | 1142 30 16 25 18 24 --- 13 | 84 58 61 62 77 --- 65
R19E | 2824 26 11 30 29 26 --- 13 | 129 109 123 109 112 --- 115
R20E | 1788 45 14 48 36 25 --- 19 | 50 70 94 78 61 --- 65
R21E | 1086 17 11 19 35 24 --- 10 | 50 44 54 60 47 --- 45
R22E | 2162 34 20 42 32 25 --- 17 | 59 73 96 76 69 --- 70
R23E | 2270 29 16 8 21 18 520 10 | 52 55 52 55 47 256 48
R24E | 1276 27 22 19 20 23 --- 13 | 37 46 58 47 29 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1901 32 20 28 29 27 308 |T 56 68 61 57 48 115 66
WRMS | 1901 32 19 24 33 27 308 |NE 50 71 51 49 40 45 68
MEDI | 1632 29 18 21 26 24 100 |MD 50 51 57 60 44 48 46
Table 3.1600.4 GPS week: 1600 Day: 4 MJD: 55448
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1839 31 31 23 15 17 --- 15 | 37 53 50 46 49 --- 40
R02 | 975 17 20 27 12 15 --- 11 | 16 29 37 28 20 --- 17
R04 | 1724 29 12 17 26 23 --- 12 | 44 37 29 32 26 --- 30
R05 | 727 14 24 24 32 23 --- 13 | 33 46 40 33 26 --- 33
R07 | 1644 18 15 27 29 26 --- 12 | 39 37 55 41 24 --- 34
R08 | 1076 21 15 13 29 9 114 8 | 34 40 35 46 31 22 34
R10 | 1411 7 12 26 26 23 --- 10 | 47 37 51 54 49 --- 42
R11 | 969 51 19 26 35 41 --- 20 | 42 53 54 62 53 --- 46
R13 | 1464 16 17 17 24 17 --- 9 | 33 37 47 45 33 --- 35
R14 | 1449 23 17 24 19 23 --- 12 | 52 42 47 33 36 --- 38
R15 | 3049 13 15 31 38 21 83 12 | 32 27 39 46 27 27 28
R17 | 2034 34 15 23 24 19 --- 13 | 52 60 57 57 51 --- 52
R18 | 2379 20 7 12 21 20 --- 9 | 51 50 52 61 56 --- 49
R19E | 2261 19 16 21 28 24 --- 11 | 57 76 85 77 62 --- 68
R20E | 1256 19 19 34 46 29 --- 14 | 63 71 100 98 75 --- 73
R21 | 1571 16 19 46 23 18 --- 15 | 49 56 64 60 50 --- 50
R22 | 1426 16 19 20 29 21 --- 11 | 42 51 63 65 56 --- 50
R23 | 2392 28 13 20 22 22 --- 12 | 42 63 65 63 52 --- 53
R24 | 944 20 9 20 36 20 --- 10 | 40 41 59 50 41 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 1713 24 17 25 28 22 100 |T 42 47 54 52 43 24 42
WRMS | 1713 24 17 23 27 22 100 |NE 37 39 44 42 34 24 34
MEDI | 1464 19 16 23 26 21 83 |MD 42 46 52 50 49 22 42
Table 3.1600.5 GPS week: 1600 Day: 5 MJD: 55449
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1547 14 16 28 12 38 --- 14 | 47 48 48 42 41 --- 39
R02 | 2035 17 28 23 23 19 --- 13 | 26 41 46 40 35 --- 32
R04 | 1137 23 23 10 32 18 --- 11 | 27 33 32 24 33 --- 29
R05 | 578 17 18 26 15 27 --- 12 | 31 31 28 28 22 --- 22
R07 | 1712 19 30 22 33 22 --- 14 | 15 38 28 30 19 --- 19
R08 | 2304 11 22 12 19 28 102 11 | 50 48 44 46 28 35 41
R10 | 1158 11 8 14 21 24 --- 8 | 28 28 34 32 35 --- 28
R11 | 1002 50 16 41 30 48 --- 23 | 44 46 75 59 56 --- 52
R13 | 1516 19 19 20 13 29 --- 12 | 22 42 35 36 27 --- 28
R14 | 1889 28 20 14 29 32 --- 13 | 35 42 42 49 31 --- 34
R15 | 4654 17 10 13 29 31 110 10 | 35 28 42 37 41 38 33
R17 | 1612 24 10 17 36 30 --- 12 | 44 40 48 51 39 --- 40
R18 | 4059 23 10 23 13 19 --- 11 | 54 47 56 44 40 --- 48
R19 | 2548 10 11 11 10 16 --- 7 | 93 89 94 83 91 --- 91
R20 | 2406 19 10 21 22 34 --- 12 | 71 77 83 85 69 --- 73
R21 | 1812 18 13 17 31 15 --- 9 | 31 36 37 43 26 --- 31
R22 | 1281 15 20 19 35 17 --- 10 | 32 39 43 52 36 --- 35
R23 | 1055 10 11 19 16 19 --- 8 | 29 32 43 37 32 --- 31
R24 | 913 17 13 26 15 23 --- 11 | 33 40 50 36 31 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 2109 21 17 21 24 27 106 |T 39 43 47 44 38 36 39
WRMS | 2109 21 17 18 26 27 106 |NE 32 38 41 38 33 36 32
MEDI | 1612 17 16 19 22 24 102 |MD 33 40 43 42 35 35 34
Table 3.1600.6 GPS week: 1600 Day: 6 MJD: 55450
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1604 14 36 22 24 40 --- 16 | 51 75 61 69 58 --- 53
R02 | 2300 15 19 16 29 16 --- 9 | 24 49 41 34 24 --- 32
R04 | 2177 11 13 18 34 23 --- 9 | 30 39 45 35 43 --- 36
R05 | 1042 26 8 44 34 22 --- 16 | 32 48 72 47 44 --- 44
R07 | 1691 24 29 25 31 26 --- 15 | 28 48 31 45 30 --- 29
R08 | 3940 18 31 16 35 19 85 13 | 35 51 41 51 33 31 36
R10 | 1165 14 12 23 28 22 --- 10 | 33 33 32 32 38 --- 30
R11 | 1168 26 30 32 32 56 --- 21 | 57 69 80 67 67 --- 65
R13 | 1220 17 19 23 21 22 --- 11 | 28 34 47 40 28 --- 31
R14 | 1598 21 14 29 43 21 --- 12 | 40 47 41 42 35 --- 39
R15 | 4278 18 22 15 35 18 141 11 | 30 27 33 38 29 33 27
R17 | 1551 24 14 24 30 26 --- 13 | 42 43 50 53 49 --- 43
R18 | 3373 15 14 28 22 16 --- 11 | 37 44 49 49 38 --- 40
R19 | 1832 14 10 14 23 14 --- 7 | 82 78 83 82 76 --- 79
R20 | 3709 16 14 16 24 21 --- 9 | 71 70 73 76 69 --- 69
R21 | 1772 11 15 19 25 17 --- 9 | 39 43 45 45 42 --- 39
R22 | 2758 9 23 21 35 18 --- 10 | 38 42 53 57 48 --- 43
R23 | 3659 11 13 24 23 21 --- 10 | 42 57 57 60 49 --- 49
R24 | 824 13 18 18 30 21 --- 10 | 35 37 49 49 37 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 2437 17 20 23 30 25 116 |T 40 49 51 51 44 32 43
WRMS | 2437 17 18 21 27 25 116 |NE 35 47 47 45 39 32 38
MEDI | 1772 15 15 22 30 21 85 |MD 37 47 49 49 42 31 39
More information about the IGSREPORT
mailing list