[IGSREPORT-19191] Wk 1609 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Nov 25 07:25:13 PST 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1609 (Nov 07, 2010 - Nov 13, 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 2.1609.
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:
igl1609[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1609 in the SP3 format.
igl16097.sum Combination Report for GPS Week 1609.
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 | 485.2 ns
1 | 334.9 ns
2 | 349.9 ns
3 | 341.0 ns
4 | 354.1 ns
5 | 389.8 ns
6 | 357.0 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 1.1609, 1a.1609).
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 2.1609.0-6)
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 3.1609.0-6).
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 1609 summary. (Nov 07, 2010 - Nov 13, 2010)
Table 1.1609.a GPS week : 1609 MJD: 55507.0-55513.0
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 125| 1 0 12 36 44 -43 -.10 31 28 | 0 730 9231 11443
| 2 2 1 60 53 276 .16 | 0 3632
cod 229| -1 0 -8 11 -2 -29 -.10 17 16 | --- --- --- ---
| 1 1 1 28 24 47 .03 | --- ---
esx 145| 0 0 -14 -23 -67 35 .33 32 28 | 19624 -1454 4872 9205
| 2 3 4 45 46 84 .08 | 55527 2930
gfz 187| 0 0 -22 -50 -32 5 -.18 39 33 | 210280 -1093 4831 8960
| 2 3 3 53 40 94 .12 | 52816 2151
iac n/a| 3 0 20 -30 13 75 -.03 31 31 | 373705 -894 4868 9747
| 2 2 4 31 23 114 .09 | 53049 1603
mcc n/a| 8 -9 41 106 72 38 .07 261 261 | --- --- --- ---
| 19 18 19 299 267 790 .49 | --- ---
Table 1.1609.b GPS week : 1609 MJD: 55507.0-55513.0
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 | 12 16 11 14 13 12 13 |
R02 | 12 12 15 11 14 13 10 |
R05 | 10 13 17 16 14 17 14 |
R07 | 19 30 29 19 15 13 17 |
R08 | 15 12 13 12 14 17 11 |
R09 | 20 16 19 22 20 16 17 |
R10 | 17 14 16 12 19 14 10 |
R11 | 24 24 27 21 28 26 24 |
R12 | 17 17 20 18 13 13 15 |
R13 | 21 14 15 17 21 15 17 |
R15 | 16 20 17 17 20 15 16 |
R16 | 17 18 19 18 13 17 17 |
R17 | 14 16 12 13 10 12 13 |
R18 | 12 17 23 11 14 12 13 |
R19 | 17 11 15 12 14 12 13 |
R20 | 20 13 18 15 9 16 16 |
R21 | 14 11 11 7 10 11 13 |
R22 | 19 13 14 14 16 17 11 |
R23 | 13 14 11 15 10 11 12 |
R24 | 17 17 16 15 11 12 12 |
Table 1.1609.c GPS week : 1609 MJD: 55507.0-55513.0
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 1609 0 | -61 -4 -1 -2172 -1117 -9762 84.4 1918 1918 | 485168 0
brd 1609 1 | -17 -17 62 -1536 643 -9256 85.5 1680 1680 | 334927 0
brd 1609 2 | 41 -45 60 307 3961 -7951 87.0 1587 1587 | 349939 0
brd 1609 3 | -139 29 344 -803 0 -6121 85.2 45560 45560 | 340974 0
brd 1609 4 | -77 119 204 -2638 -153 -3341 86.5 42510 42510 | 354077 0
brd 1609 5 | 87 -12 259 -3071 273 -5842 86.2 1966 1966 | 389805 0
brd 1609 6 | -11 -50 316 -2333 -1779 -17060 86.6 1838 1838 | 356954 0
-------------+------------------------------------------------------------+----------------
brd 1609 mean| -25 2 177 -1749 261 -8476 85.9 13865 13865 | 373120 0
brd 1609 sdev| 76 57 137 1170 1832 4379 .9 20628 20628 | 52419 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 2.1609.0 GPS week: 1609 Day: 0 MJD: 55507
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 125| 0 2 11 -3 20 -55 -.22 31 30 | 0 5326 6915 7968
cod 229| 1 0 -6 19 18 -35 -.13 18 17 | --- --- --- ---
esx 145| 0 0 -18 34 -120 113 .34 34 32 | 140072 -3521 4502 8930
gfz 187| -1 0 -26 -153 -89 19 -.00 41 41 | 323123 -4988 4502 8569
iac n/a| 0 0 17 -59 11 26 .07 34 34 | 487292 -2940 4478 9671
mcc n/a| 5 -3 46 10 167 53 .17 131 131 | --- --- --- ---
Table 2.1609.1 GPS week: 1609 Day: 1 MJD: 55508
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 125| 1 1 12 124 156 -390 -.16 28 26 | 0 -5204 9139 11263
cod 229| -1 0 -11 -33 -44 59 -.09 17 15 | --- --- --- ---
esx 145| -1 0 -17 -95 -123 92 .35 36 29 | -22996 3196 4481 9628
gfz 187| 2 0 -17 -28 25 158 -.31 39 32 | 170869 1600 4479 9243
iac n/a| 2 -1 26 6 11 239 .04 31 31 | 334333 2267 4461 10266
mcc n/a| -20 8 63 429 84 809 .42 328 328 | --- --- --- ---
Table 2.1609.2 GPS week: 1609 Day: 2 MJD: 55509
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 125| -2 0 12 87 66 -265 -.17 33 30 | 0 4818 11899 14846
cod 229| 0 0 -9 -2 18 -45 -.05 20 19 | --- --- --- ---
esx 145| -4 2 -12 -37 -78 115 .41 36 31 | -10691 269 4777 8521
gfz 187| -1 2 -21 -77 -23 -1 -.07 37 30 | 187122 459 4780 8364
iac n/a| 2 -1 17 -22 -6 175 -.01 29 29 | 349780 -576 4796 9390
mcc n/a| -15 -45 6 600 591 -72 -.70 352 352 | --- --- --- ---
Table 2.1609.3 GPS week: 1609 Day: 3 MJD: 55510
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 125| 2 0 16 -13 7 -13 -.17 29 28 | 0 -614 8684 10940
cod 229| -2 0 -8 26 -9 -35 -.12 15 14 | --- --- --- ---
esx 145| 1 1 -13 -11 4 0 .44 30 28 | -3764 -3992 5611 9382
gfz 187| 5 0 -21 -26 -7 -90 -.18 42 26 | 179120 -966 5579 8932
iac n/a| 5 1 20 -56 2 41 -.01 33 33 | 342346 -980 5624 9787
mcc n/a| 31 -19 23 -77 -218 -1361 .78 336 336 | --- --- --- ---
Table 2.1609.4 GPS week: 1609 Day: 4 MJD: 55511
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 125| 3 4 13 -27 0 191 -.18 33 29 | 0 -1153 10194 12237
cod 229| -1 -1 -9 56 25 -87 -.12 18 14 | --- --- --- ---
esx 145| -1 -4 -8 12 -37 0 .34 27 24 | -690 -4949 5320 8589
gfz 187| -3 5 -20 -25 -29 -12 -.15 37 24 | 191503 -310 4978 8344
iac n/a| 1 4 22 -67 -4 24 .01 33 33 | 354565 -1771 5320 8959
mcc n/a| 22 4 50 -67 67 -291 .15 231 231 | --- --- --- ---
Table 2.1609.5 GPS week: 1609 Day: 5 MJD: 55512
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 125| 1 -1 12 83 35 418 .01 33 29 | 0 398 8769 11526
cod 229| -4 1 -7 -7 -12 -62 -.08 17 16 | --- --- --- ---
esx 145| 2 -5 -20 -66 -41 -121 .21 28 26 | 29763 -1710 4789 8104
gfz 187| 1 -4 -26 13 -16 -116 -.32 45 46 | 227305 -848 4811 8110
iac n/a| 5 1 22 9 17 -107 -.08 27 27 | 389797 -774 4777 8451
mcc n/a| 18 -5 50 80 -13 51 .05 264 264 | --- --- --- ---
Table 2.1609.6 GPS week: 1609 Day: 6 MJD: 55513
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 125| 2 -1 10 3 25 -187 .22 27 27 | 0 1544 9017 11326
cod 229| -2 0 -6 20 -14 2 -.14 18 16 | --- --- --- ---
esx 145| -1 1 -9 0 -76 48 .23 29 26 | 5679 529 4628 11285
gfz 187| -1 -2 -21 -52 -82 79 -.22 36 32 | 192922 -2598 4688 11161
iac n/a| 5 -2 13 -25 63 125 -.19 28 28 | 357823 -1486 4625 11708
mcc n/a| 16 -3 51 -232 -168 1076 -.40 186 186 | --- --- --- ---
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 3.1609.0 GPS week: 1609 Day: 0 MJD: 55507
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 831 16 15 21 17 30 --- 11 | 45 52 59 47 61 --- 52
R02 | 2091 27 11 24 21 18 --- 11 | 105 129 130 120 117 --- 122
R05 | 856 20 12 19 14 17 69 9 | 150 164 152 151 157 217 157
XR07 | 3332 34 22 --- --- 27 --- 19 | 26 38 --- --- 32 --- 26
R08 | 1343 31 23 27 50 20 240 14 | 48 47 50 57 63 165 49
R09E | 2324 32 21 35 28 53 --- 20 | 36 32 37 46 54 --- 30
R10E | 2378 33 15 29 51 43 --- 17 | 50 59 55 49 62 --- 53
R11E | 940 49 23 48 64 53 87 24 | 83 87 127 115 100 235 91
R12E | 2516 35 15 27 34 43 --- 17 | 47 29 34 40 57 --- 32
R13E | 1707 32 23 35 45 53 --- 20 | 58 39 52 53 76 --- 47
R15E | 2481 24 25 38 38 25 134 16 | 166 178 194 176 173 110 177
R16E | 1069 38 20 30 34 34 --- 17 | 21 16 39 44 41 --- 18
R17 | 840 19 20 27 26 29 --- 13 | 28 51 56 62 29 --- 39
R18 | 3270 21 12 23 35 26 106 11 | 40 48 61 76 61 119 49
R19 | 1239 44 13 38 55 20 --- 16 | 33 51 72 65 50 --- 47
R20 | 1317 39 21 50 30 30 --- 20 | 42 47 92 75 62 --- 56
R21 | 878 28 15 30 22 28 --- 14 | 60 60 56 76 68 --- 58
R22 | 3899 26 21 47 42 41 --- 19 | 49 77 61 80 68 --- 62
R23 | 1337 27 15 30 82 17 63 13 | 36 55 51 72 43 118 43
R24 | 1163 28 15 45 30 26 --- 16 | 31 39 77 63 57 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 1918 31 18 34 41 34 131 |T 57 64 76 77 71 160 62
WRMS | 1918 30 17 32 41 34 131 |NE 53 66 76 78 66 154 61
MEDI | 1337 28 15 30 34 28 87 |MD 45 51 59 65 61 119 49
Table 3.1609.1 GPS week: 1609 Day: 1 MJD: 55508
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1057 32 18 30 29 33 --- 15 | 34 51 50 53 45 --- 42
R02 | 2208 32 13 18 15 20 --- 12 | 119 132 145 126 144 --- 133
R05 | 856 30 13 31 32 19 339 13 | 170 189 199 193 188 80 186
XR07 | 3726 68 28 --- --- 28 --- 30 | 25 50 --- --- 31 --- 34
R08 | 1088 29 16 20 19 15 209 11 | 64 59 64 66 65 138 60
R09E | 760 21 22 23 32 43 --- 16 | 22 25 30 32 60 --- 23
R10E | 1251 29 12 27 43 32 --- 14 | 46 58 65 56 71 --- 56
R11E | 937 42 18 59 43 56 519 24 | 72 92 128 106 104 135 93
R12E | 1439 29 19 32 35 39 --- 16 | 50 25 38 40 69 --- 33
R13E | 1628 25 14 23 36 33 --- 13 | 64 53 51 63 71 --- 55
R15E | 3659 36 29 36 34 42 303 20 | 163 194 193 193 172 82 180
R16E | 1325 25 18 42 50 40 --- 17 | 21 19 42 40 45 --- 17
R17 | 1451 26 17 49 55 21 --- 16 | 16 46 61 75 36 --- 35
R18 | 1664 30 9 52 29 28 207 17 | 30 53 103 49 34 129 49
R19 | 1288 25 9 16 83 23 --- 10 | 55 47 54 72 34 --- 44
R20 | 1503 24 17 26 29 27 --- 13 | 52 46 42 56 53 --- 45
R21 | 1495 18 14 30 34 13 --- 10 | 37 36 65 46 33 --- 38
R22 | 2887 26 12 21 21 30 --- 12 | 32 49 49 45 55 --- 43
R23 | 1633 15 19 37 26 22 290 13 | 22 52 50 35 31 97 34
R24 | 864 18 15 59 36 22 --- 17 | 35 43 47 39 38 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 1679 28 17 36 39 31 328 |T 56 65 77 72 68 110 61
WRMS | 1679 26 15 29 32 31 328 |NE 53 65 77 71 60 111 59
MEDI | 1439 26 16 30 34 28 290 |MD 37 50 54 56 53 97 43
Table 3.1609.2 GPS week: 1609 Day: 2 MJD: 55509
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1691 25 12 11 23 22 --- 10 | 33 36 44 43 41 --- 36
R02 | 993 42 17 21 26 17 --- 14 | 83 111 113 120 111 --- 104
R05 | 1912 52 27 18 32 13 90 17 | 99 149 142 142 134 33 132
XR07 | 2502 66 29 --- --- 26 --- 28 | 30 49 --- --- 33 --- 32
R08 | 1563 24 16 22 24 31 124 13 | 38 53 56 63 66 61 49
R09E | 886 33 28 34 40 36 --- 18 | 24 40 52 45 54 --- 35
R10E | 934 34 20 34 23 21 --- 15 | 35 41 73 52 57 --- 46
R11E | 1304 49 26 74 55 41 427 27 | 63 60 87 88 61 111 61
R12E | 800 43 17 40 32 40 --- 20 | 37 39 48 33 59 --- 38
R13E | 1830 26 15 36 31 30 --- 15 | 46 42 58 55 55 --- 43
R15E | 1933 37 21 30 39 31 674 16 | 117 136 137 133 139 55 130
R16E | 1115 32 21 30 39 47 --- 19 | 21 30 40 47 57 --- 26
R17 | 2395 18 15 19 43 25 --- 11 | 36 38 34 56 35 --- 32
R18 | 1103 28 24 72 18 24 203 22 | 32 51 81 50 36 60 40
R19 | 1949 33 17 24 37 31 --- 15 | 32 48 48 49 30 --- 35
R20 | 1664 36 28 36 58 28 --- 18 | 19 50 58 88 36 --- 38
R21 | 1377 25 13 24 62 15 --- 11 | 43 53 70 78 54 --- 53
R22 | 1492 24 13 38 24 18 --- 13 | 45 47 84 74 51 --- 53
R23 | 1830 22 13 24 23 17 209 10 | 26 42 55 57 43 51 38
R24 | 2134 26 18 31 25 34 --- 15 | 20 49 53 48 42 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1586 33 20 36 37 29 352 |T 43 58 70 69 59 61 52
WRMS | 1586 30 19 31 30 29 352 |NE 41 59 69 72 54 51 52
MEDI | 1563 32 17 30 32 26 203 |MD 35 48 58 56 54 55 38
Table 3.1609.3 GPS week: 1609 Day: 3 MJD: 55510
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 613 26 7 39 29 27 --- 14 | 49 55 66 66 61 --- 53
R02 | 1007 28 13 17 17 18 --- 11 | 108 142 148 128 137 --- 134
R05 | 1431 47 18 25 25 19 137 16 | 176 209 216 219 195 74 200
XR07 | 3507 29 18 --- --- 37 --- 19 | 27 57 --- --- 64 --- 44
R08 | 1075 27 14 13 20 28 121 11 | 95 105 97 106 82 35 96
R09E | 1150 53 23 27 51 49 --- 21 | 28 34 40 47 58 --- 27
R10E | 1432 20 13 19 28 32 --- 11 | 71 79 82 87 91 --- 79
R11E | 716 33 19 53 71 41 293 20 | 100 100 118 132 114 137 104
R12E | 1391 33 20 38 39 41 --- 18 | 34 39 39 38 55 --- 33
R13E | 1653 32 12 35 22 40 --- 16 | 80 70 87 88 84 --- 75
R15E |>>>>> 26 14 36 34 42 692 16 | 145 145 158 160 136 64 145
R16E | 935 32 16 30 41 48 --- 17 | 22 22 40 41 52 --- 20
R17 | 3228 22 14 21 27 31 --- 12 | 32 47 41 47 34 --- 37
R18 | 1141 18 14 18 28 25 242 10 | 35 37 32 48 39 63 30
R19 | 1872 25 20 11 34 24 --- 12 | 40 47 40 57 34 --- 37
R20 | 3251 32 16 36 67 26 --- 15 | 25 38 55 75 24 --- 33
R21 | 1998 13 11 11 62 15 --- 7 | 33 49 46 84 42 --- 42
R22 | 821 22 11 31 75 32 --- 13 | 37 47 79 99 50 --- 51
R23 | 1263 19 16 40 20 26 150 14 | 46 43 89 41 41 25 51
R24 | 1514 20 16 39 18 30 --- 14 | 27 47 35 34 55 --- 36
------+-----------------------------------------+-------------------------------------
RMS |45558 29 15 30 42 33 336 |T 60 70 79 84 72 66 66
WRMS |45558 28 14 28 26 33 336 |NE 56 71 78 83 66 49 64
MEDI | 1391 26 14 30 29 30 150 |MD 37 47 66 75 55 63 44
Table 3.1609.4 GPS week: 1609 Day: 4 MJD: 55511
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 870 26 15 16 25 32 --- 12 | 33 48 45 47 61 --- 42
R02 | 1581 30 15 22 15 34 --- 14 | 70 102 96 86 93 --- 90
R05 | 913 39 9 17 24 30 230 13 | 110 136 138 127 136 165 130
R07 | 3383 24 23 30 --- 25 --- 14 | 29 42 19 --- 35 --- 27
R08 | 679 30 13 24 38 29 108 13 | 48 64 58 63 42 55 51
R09E | 1789 37 18 38 36 48 --- 19 | 45 31 54 43 64 --- 38
R10E | 4120 49 21 30 44 36 --- 19 | 44 75 83 94 67 --- 65
R11E | 1285 68 28 54 55 44 286 27 | 76 133 154 151 114 178 122
R12E | 2538 24 13 20 29 34 --- 12 | 42 42 60 60 53 --- 45
R13E | 1113 34 33 30 41 45 --- 20 | 32 72 59 69 43 --- 49
R15E |>>>>> 53 16 40 43 28 303 20 | 86 116 145 128 112 79 113
R16E | 1160 25 13 20 48 36 --- 13 | 23 24 35 48 40 --- 22
R17 | 3148 20 14 17 28 16 --- 9 | 42 48 42 48 38 --- 42
R18 | 2869 23 16 16 42 41 263 14 | 35 38 52 73 66 99 43
R19 | 984 21 13 23 20 39 --- 14 | 30 32 24 43 58 --- 31
R20 | 4170 21 11 14 19 19 --- 9 | 26 33 23 29 13 --- 21
R21 | 1913 19 10 20 45 21 --- 9 | 30 37 57 63 45 --- 41
R22 | 1374 32 20 28 25 32 --- 15 | 18 55 44 56 52 --- 41
R23 | 1600 16 12 17 63 27 117 10 | 32 51 49 63 50 29 45
R24 | 989 15 17 24 20 20 --- 11 | 38 37 59 47 42 --- 41
------+-----------------------------------------+-------------------------------------
RMS |42511 33 17 27 37 33 231 |T 44 60 64 70 61 100 54
WRMS |42511 29 14 24 24 33 231 |NE 41 55 54 62 56 87 49
MEDI | 1581 25 15 22 36 32 230 |MD 35 48 54 63 52 79 42
Table 3.1609.5 GPS week: 1609 Day: 5 MJD: 55512
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 948 27 13 21 30 24 --- 12 | 48 47 49 52 54 --- 47
R02 | 1132 34 17 21 40 21 --- 13 | 59 80 89 91 77 --- 75
R05 | 1475 52 21 15 36 23 240 16 | 70 109 110 112 87 181 95
R07 | 2182 23 17 20 --- 28 --- 12 | 22 43 31 --- 38 --- 35
R08 | 843 36 26 29 37 24 --- 16 | 32 58 67 52 52 --- 49
R09E | 1840 26 19 21 33 41 --- 15 | 30 27 30 33 51 --- 28
R10E | 2652 37 16 20 32 27 --- 14 | 37 47 58 61 58 --- 46
R11E | 2282 68 22 54 80 42 459 26 | 88 129 162 172 150 282 130
R12E | 2143 23 13 24 30 30 --- 13 | 53 38 59 51 56 --- 46
R13E | 1158 34 16 23 40 31 --- 14 | 72 87 79 87 83 --- 79
R15E | 1333 36 16 32 49 24 175 15 | 104 116 124 127 90 141 107
R16E | 2430 33 18 38 33 32 --- 17 | 16 19 44 37 37 --- 19
R17 | 1385 21 13 30 67 16 --- 11 | 24 34 69 88 38 --- 37
R18 | 1257 26 19 17 44 24 182 12 | 41 19 33 49 42 111 28
R19 | 909 22 17 18 69 28 --- 12 | 36 32 43 86 51 --- 36
R20 | 4956 27 20 26 28 37 --- 16 | 25 21 28 34 30 --- 15
R21 | 1863 20 16 27 22 14 --- 11 | 31 38 47 37 25 --- 31
R22 | 1028 35 14 44 34 26 --- 17 | 25 39 71 50 21 --- 33
R23 | 1087 21 15 27 24 14 124 11 | 35 31 56 47 34 35 34
R24 | 1901 20 12 31 61 22 --- 12 | 34 24 57 58 30 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1966 33 17 28 45 27 264 |T 44 51 65 69 55 150 50
WRMS | 1966 29 16 26 46 27 264 |NE 37 44 57 63 44 109 41
MEDI | 1385 27 16 24 36 24 182 |MD 35 38 57 52 51 141 36
Table 3.1609.6 GPS week: 1609 Day: 6 MJD: 55513
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1069 28 12 28 21 23 --- 13 | 43 49 52 52 61 --- 48
R02 | 2177 15 13 21 30 19 --- 9 | 47 43 50 59 49 --- 43
R05 | 1484 29 17 20 21 33 184 14 | 54 59 58 58 59 113 54
R07 | 1771 32 28 32 --- 20 --- 16 | 28 43 32 --- 32 --- 29
R08 | 540 27 14 15 34 15 --- 10 | 45 25 35 44 36 --- 29
R09E | 1884 27 23 38 41 33 --- 17 | 39 37 62 52 47 --- 39
R10E | 1109 18 9 13 27 27 --- 10 | 49 54 63 68 55 --- 53
R11E | 1230 39 26 61 61 41 --- 24 | 101 123 145 156 117 --- 118
R12E | 1933 32 16 25 26 29 --- 14 | 43 47 43 49 52 --- 41
R13E | 1533 32 16 38 39 30 --- 16 | 51 49 64 68 52 --- 48
R15E | 1866 21 23 39 48 26 87 16 | 70 74 89 102 63 61 72
R16E | 3660 34 16 34 40 32 --- 16 | 22 23 47 35 30 --- 21
R17 | 902 30 12 23 30 28 --- 13 | 35 47 54 58 32 --- 39
R18 | 1702 22 15 17 39 33 299 12 | 42 43 47 72 55 80 44
R19 | 1169 22 13 19 33 32 --- 12 | 40 52 45 56 62 --- 48
R20 | 3011 20 22 31 57 36 --- 15 | 26 29 56 76 44 --- 33
R21 | 2445 18 21 26 16 26 --- 13 | 47 51 61 61 57 --- 49
R22 | 1351 23 14 22 30 15 --- 10 | 35 55 69 74 49 --- 50
R23 | 1741 24 15 15 16 27 84 11 | 39 40 46 45 34 56 36
R24 | 1340 23 12 29 44 16 --- 11 | 26 39 52 67 41 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1838 27 17 29 36 28 186 |T 44 49 58 65 51 77 46
WRMS | 1838 27 16 26 32 28 186 |NE 39 44 50 60 47 83 41
MEDI | 1533 24 15 25 33 27 87 |MD 42 47 52 59 49 61 43
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