[IGSREPORT-19168] Wk 1608 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Nov 18 05:16:48 PST 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1608 (Oct 31, 2010 - Nov 06, 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 2.1608.
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:
igl1608[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1608 in the SP3 format.
igl16087.sum Combination Report for GPS Week 1608.
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 | 318.3 ns
1 | 332.4 ns
2 | 349.3 ns
3 | 337.4 ns
4 | 343.3 ns
5 | 342.1 ns
6 | 353.9 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 1.1608, 1a.1608).
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 2.1608.0-6)
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 3.1608.0-6).
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 1608 summary. (Oct 31, 2010 - Nov 06, 2010)
Table 1.1608.a GPS week : 1608 MJD: 55500.0-55506.0
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 128| 1 1 10 -28 19 -40 -.21 31 31 | 0 819 5457 6488
| 1 1 3 41 23 69 .05 | 0 3273
cod 231| -1 0 -9 31 4 -7 -.14 15 12 | --- --- --- ---
| 0 0 3 10 12 28 .04 | --- ---
esx 135| 0 -2 -8 -28 -44 61 .39 31 27 | -5384 -2497 5202 9854
| 1 2 5 38 41 33 .07 | 7906 3089
gfz 192| -1 0 -18 -47 -7 30 -.17 37 34 | 172052 -1603 5181 9499
| 2 2 4 74 117 67 .03 | 12357 3023
iac n/a| 2 1 27 -51 11 15 .20 43 43 | 340097 -703 5176 10375
| 2 1 12 34 31 87 .10 | 12150 1490
mcc n/a| 1 4 29 -13 41 61 .10 106 106 | --- --- --- ---
| 7 9 6 116 84 293 .24 | --- ---
Table 1.1608.b GPS week : 1608 MJD: 55500.0-55506.0
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 | 10 11 12 8 9 9 16 |
R02 | 9 10 11 7 10 10 12 |
R05 | 14 17 16 8 12 10 10 |
R07 | 214 --- --- 0 19 30 25 |
R08 | 10 10 9 8 10 12 18 |
R09 | 19 21 19 22 22 18 20 |
R10 | 22 23 23 17 21 15 16 |
R11 | 30 24 25 22 27 27 23 |
R12 | 21 21 25 20 17 19 21 |
R13 | 20 17 20 19 17 17 16 |
R15 | 20 20 18 18 18 17 14 |
R16 | 20 20 22 19 18 20 21 |
R17 | 14 10 18 11 10 16 12 |
R18 | 14 16 14 11 12 12 9 |
R19 | 10 12 14 15 12 12 9 |
R20 | 15 16 11 19 12 15 14 |
R21 | 11 12 11 13 19 12 11 |
R22 | 12 11 18 9 11 13 11 |
R23 | 13 10 13 12 26 17 21 |
R24 | 13 13 9 11 15 17 14 |
Table 1.1608.c GPS week : 1608 MJD: 55500.0-55506.0
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 1608 0 | 107 48 223 258 -392 -17130 85.7 1687 1687 | 318293 0
brd 1608 1 | 91 80 218 -574 94 -16320 85.2 1531 1531 | 332367 0
brd 1608 2 | 15 -30 108 -623 -1497 -22490 85.6 1732 1732 | 349260 0
brd 1608 3 | 72 47 216 939 1008 -23500 83.1 2192 2192 | 337360 0
brd 1608 4 | -8 140 205 1089 -2264 -17430 87.8 1776 1776 | 343304 0
brd 1608 5 | 176 -14 24 -290 -220 -14940 87.9 1689 1689 | 342051 0
brd 1608 6 | -53 -16 50 -1245 -1912 -10100 86.3 1848 1848 | 353868 0
-------------+------------------------------------------------------------+----------------
brd 1608 mean| 57 36 149 -63 -740 -17415 85.9 1779 1779 | 339500 0
brd 1608 sdev| 77 61 86 862 1184 4540 1.7 206 206 | 11746 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 2.1608.0 GPS week: 1608 Day: 0 MJD: 55500
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 128| 1 0 11 -41 -12 57 -.28 36 35 | 0 -2002 10704 13377
cod 231| -1 -1 -9 29 17 -26 -.20 16 12 | --- --- --- ---
esx 135| -1 2 -11 -3 0 33 .41 25 23 | -12209 -7044 5627 10001
gfz 192| -5 5 -16 -74 -34 -70 -.16 37 30 | 150191 -5999 5591 9675
iac n/a| 0 0 41 -43 -31 -25 .23 46 46 | 318870 -1010 5613 10525
mcc n/a| 3 -6 18 -52 -76 -332 .24 142 142 | --- --- --- ---
Table 2.1608.1 GPS week: 1608 Day: 1 MJD: 55501
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 128| 0 1 12 -114 12 -24 -.19 33 33 | 0 261 2121 2228
cod 231| 0 0 -8 40 13 -37 -.14 14 10 | --- --- --- ---
esx 135| 0 -3 -3 31 -40 107 .31 30 27 | -11707 -3496 4540 8896
gfz 192| -3 -1 -15 -171 70 39 -.16 33 40 | 163069 -2840 4545 8333
iac n/a| 0 1 23 -98 -6 19 .26 46 46 | 331425 279 4554 9359
mcc n/a| 8 -9 36 -180 58 183 .05 102 102 | --- --- --- ---
Table 2.1608.2 GPS week: 1608 Day: 2 MJD: 55502
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 128| 0 2 11 -6 51 -89 -.17 33 33 | 0 277 2254 2348
cod 231| -1 0 -3 31 5 30 -.12 13 11 | --- --- --- ---
esx 135| 0 -1 -4 -40 -108 47 .31 36 33 | 1866 -2391 5278 8597
gfz 192| 0 0 -13 -80 74 -26 -.19 39 30 | 180735 -3023 5262 8503
iac n/a| 6 4 3 -62 10 -28 .26 47 47 | 349866 -1109 5207 9126
mcc n/a| 9 0 31 68 36 347 .07 81 81 | --- --- --- ---
Table 2.1608.3 GPS week: 1608 Day: 3 MJD: 55503
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 128| 2 3 4 16 25 -63 -.18 24 24 | 0 -210 2151 2234
cod 231| 0 -1 -12 8 -17 32 -.06 14 10 | --- --- --- ---
esx 135| -2 -3 -1 -92 -43 71 .44 32 26 | -5867 -3446 4463 9416
gfz 192| 0 0 -15 30 25 44 -.18 36 31 | 169820 -1907 4482 9179
iac n/a| 1 0 37 2 10 -57 .20 44 44 | 339511 -1247 4453 10158
mcc n/a| 1 11 23 153 35 227 .43 88 88 | --- --- --- ---
Table 2.1608.4 GPS week: 1608 Day: 4 MJD: 55504
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 128| 1 -1 8 -16 42 47 -.24 27 27 | 0 -84 2445 2537
cod 231| -1 0 -13 34 0 -25 -.14 14 11 | --- --- --- ---
esx 135| 1 -1 -7 -26 -58 59 .51 38 27 | -15421 1320 4909 9708
gfz 192| -1 -2 -20 -49 69 55 -.10 39 38 | 175805 1525 4793 9401
iac n/a| 2 4 36 -84 67 -38 .31 44 44 | 341391 1620 4802 10210
mcc n/a| -7 12 30 -46 14 -361 -.30 120 120 | --- --- --- ---
Table 2.1608.5 GPS week: 1608 Day: 5 MJD: 55505
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 128| 0 2 12 -12 20 -121 -.24 30 30 | 0 8031 8494 10290
cod 231| 0 0 -6 38 14 -5 -.17 16 15 | --- --- --- ---
esx 135| 0 -3 -15 -51 -72 16 .37 29 26 | 3203 -4113 5528 10732
gfz 192| -1 -3 -24 52 2 26 -.17 40 35 | 177364 -2052 5498 10013
iac n/a| 0 1 28 -22 34 199 .13 39 39 | 343729 -3196 5512 10870
mcc n/a| -8 7 32 71 14 65 -.06 94 94 | --- --- --- ---
Table 2.1608.6 GPS week: 1608 Day: 6 MJD: 55506
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 128| 3 1 14 -24 -6 -88 -.15 34 34 | 0 -534 10033 12402
cod 231| -1 0 -9 34 1 -19 -.15 15 12 | --- --- --- ---
esx 135| 0 -4 -12 -18 11 99 .36 31 28 | 2443 1687 6075 11634
gfz 192| 0 1 -24 -39 -256 142 -.21 39 36 | 187381 3075 6097 11395
iac n/a| 4 0 24 -52 -4 39 .02 34 34 | 355889 -258 6094 12381
mcc n/a| 5 12 34 -107 206 300 .28 115 115 | --- --- --- ---
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 3.1608.0 GPS week: 1608 Day: 0 MJD: 55500
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 588 24 9 14 16 25 --- 9 | 25 33 37 34 42 --- 31
R02 | 520 14 9 13 25 32 --- 9 | 18 28 29 20 26 --- 24
R05 | 2309 22 11 30 45 33 97 13 | 21 22 40 48 26 43 22
XR07 | 6082 --- 66 --- --- 418 --- 214 | --- 9999 --- --- 9999 --- 9999
R08 | 1231 18 13 13 19 28 89 10 | 18 18 35 33 34 32 22
R09E | 2940 25 27 23 39 64 --- 19 | 36 31 39 45 64 --- 25
R10E | 1442 60 22 26 53 48 --- 21 | 46 33 30 28 70 --- 35
R11E | 704 61 24 53 36 82 73 29 | 47 54 63 60 77 21 46
R12E | 2470 55 12 34 28 52 --- 21 | 34 28 31 32 67 --- 29
R13E | 1304 48 13 26 40 59 --- 19 | 41 23 32 33 62 --- 25
R15E | 3470 52 14 25 35 56 117 20 | 45 25 30 30 50 22 25
R16E | 1265 45 20 17 28 64 --- 20 | 38 23 32 29 62 --- 25
R17 | 1686 24 16 25 49 37 --- 13 | 33 44 43 61 57 --- 42
R18 | 1841 38 10 11 36 43 278 14 | 24 44 46 70 62 64 41
R19 | 810 16 12 9 29 37 --- 10 | 32 32 34 43 45 --- 29
R20 | 1049 24 16 34 31 31 --- 14 | 29 40 53 56 47 --- 37
R21 | 853 16 13 23 31 27 --- 11 | 46 65 69 79 43 --- 58
R22 | 667 19 10 27 41 32 --- 12 | 49 62 61 58 69 --- 58
R23 | 706 14 20 19 61 38 82 13 | 33 49 45 70 45 42 40
R24 | 2064 31 12 15 34 35 --- 12 | 25 40 55 65 57 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1686 36 16 25 37 46 142 |T 33 36 42 47 52 37 34
WRMS | 1686 35 12 23 30 46 142 |NE 27 37 43 45 34 43 33
MEDI | 1265 24 13 23 35 37 89 |MD 33 33 39 45 57 32 31
Table 3.1608.1 GPS week: 1608 Day: 1 MJD: 55501
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 658 27 11 20 20 24 --- 11 | 22 27 50 38 37 --- 29
R02 | 542 20 10 19 21 27 --- 10 | 25 24 28 29 37 --- 23
R05 | 1514 18 11 42 21 49 90 16 | 19 23 39 32 31 30 17
R08 | 771 17 9 25 27 19 74 9 | 16 21 29 29 22 28 18
R09E | 2859 37 19 29 37 73 --- 21 | 39 30 28 31 63 --- 26
R10E | 2373 65 27 18 24 53 --- 23 | 41 37 26 38 52 --- 30
R11E | 801 39 23 57 58 60 58 24 | 44 31 57 68 71 18 35
R12E | 1003 42 16 44 34 58 --- 21 | 32 32 39 33 60 --- 30
R13E | 961 35 12 27 27 54 --- 16 | 41 25 32 29 55 --- 28
R15E | 2645 46 11 32 34 64 93 20 | 46 23 37 24 61 18 24
R16E | 723 30 18 33 25 72 --- 20 | 25 24 47 36 64 --- 25
R17 | 1956 15 9 26 20 23 --- 10 | 36 40 48 26 53 --- 40
R18 | 2122 48 5 23 39 39 187 16 | 27 32 51 52 49 49 34
R19 | 1176 23 11 20 43 37 --- 12 | 28 17 25 37 44 --- 18
R20 | 1803 34 11 29 28 45 --- 15 | 24 36 32 43 58 --- 30
R21 | 903 27 9 28 53 27 --- 12 | 22 45 62 81 31 --- 40
R22 | 701 20 7 14 24 40 --- 10 | 32 45 54 59 65 --- 46
R23 | 982 26 8 16 31 21 42 9 | 23 30 37 39 23 28 25
R24 | 1324 17 14 30 28 32 --- 12 | 22 27 32 35 36 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 1530 33 14 30 33 46 102 |T 29 29 39 39 48 28 28
WRMS | 1530 33 10 27 40 46 102 |NE 22 29 44 45 34 30 27
MEDI | 1003 27 11 27 28 40 74 |MD 27 30 37 36 52 28 28
Table 3.1608.2 GPS week: 1608 Day: 2 MJD: 55502
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 933 27 9 30 23 22 --- 11 | 25 35 33 25 32 --- 28
R02 | 1144 19 9 21 13 35 --- 10 | 25 26 36 28 45 --- 26
R05 | 1747 22 8 28 18 59 71 16 | 28 28 44 30 42 37 27
R08 | 2444 15 10 22 16 19 63 9 | 35 33 45 40 40 35 33
R09E | 2578 38 16 25 29 62 --- 19 | 26 40 48 41 70 --- 32
R10E | 3120 63 20 35 51 46 --- 22 | 57 44 37 26 68 --- 41
R11E | 822 28 26 76 75 51 51 25 | 44 44 69 73 66 26 42
R12E | 1590 55 19 53 39 62 --- 24 | 31 32 37 37 60 --- 27
R13E | 1532 34 10 52 48 56 --- 20 | 35 34 55 47 58 --- 33
R15E | 3306 42 14 24 43 50 89 17 | 49 29 30 22 60 22 25
R16E | 1808 34 9 34 38 85 --- 22 | 34 20 45 50 57 --- 25
R17 | 792 33 13 43 26 44 --- 17 | 50 41 30 47 54 --- 34
R18 | 743 33 11 23 41 36 122 13 | 35 43 57 66 57 63 41
R19 | 1912 16 12 23 23 53 --- 14 | 28 29 51 30 48 --- 32
R20 | 885 25 7 26 33 20 --- 10 | 36 29 32 43 53 --- 31
R21 | 1065 13 12 19 46 39 --- 11 | 42 45 41 68 45 --- 40
R22 | 1030 47 7 39 57 42 --- 18 | 25 43 68 80 87 --- 46
R23 | 946 22 13 30 31 30 70 12 | 44 34 63 55 41 30 37
R24 | 950 16 9 18 27 24 --- 8 | 32 39 32 50 48 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1731 33 13 36 39 47 81 |T 35 35 44 45 54 35 33
WRMS | 1731 33 11 33 30 47 81 |NE 30 33 38 37 41 37 30
MEDI | 1144 28 11 28 33 44 70 |MD 35 34 44 43 54 30 33
Table 3.1608.3 GPS week: 1608 Day: 3 MJD: 55503
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 915 18 10 13 17 18 --- 8 | 35 39 45 46 49 --- 38
R02 | 1841 12 9 15 24 16 --- 7 | 23 22 24 25 32 --- 21
R05 | 1604 13 6 17 21 26 66 8 | 17 27 34 29 59 46 27
XR07 | ---- --- 7 --- --- --- --- 0 | --- 9999 --- --- --- --- 9999
R08 | 2727 20 7 16 28 17 63 8 | 35 34 34 25 37 77 32
R09E | 3041 42 16 34 44 75 --- 22 | 35 38 53 55 59 --- 34
R10E | 2395 31 19 16 38 56 --- 16 | 37 31 34 20 70 --- 31
R11E | 1113 28 23 56 69 58 45 22 | 35 42 80 76 53 31 39
R12E | 1824 41 21 37 35 52 --- 20 | 36 29 39 39 53 --- 27
R13E | 1733 27 13 49 48 49 --- 18 | 33 31 34 33 57 --- 28
R15E | 5616 34 16 32 44 51 104 17 | 37 33 40 29 59 45 30
R16E | 2110 31 11 39 45 58 --- 18 | 29 33 39 42 58 --- 28
R17 | 801 22 7 18 29 30 --- 10 | 63 57 43 54 39 --- 51
R18 | 1178 16 12 18 33 34 119 10 | 35 33 29 57 46 85 32
R19 | 2030 12 9 30 19 59 --- 15 | 30 26 37 28 44 --- 24
R20 | 2577 15 18 58 32 42 --- 19 | 25 37 55 53 37 --- 30
R21 | 1055 11 9 31 22 42 --- 12 | 45 53 75 60 26 --- 49
R22 | 1455 12 10 24 15 22 --- 9 | 56 55 45 51 48 --- 49
R23 | 913 17 18 29 39 24 108 12 | 24 48 42 53 30 47 30
R24 | 1286 9 10 21 41 40 --- 10 | 31 36 39 60 35 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 2192 24 14 32 36 44 88 |T 34 37 43 43 46 55 33
WRMS | 2192 24 10 26 31 44 88 |NE 30 35 44 40 41 46 33
MEDI | 1733 18 10 29 33 42 66 |MD 35 34 39 46 48 46 30
Table 3.1608.4 GPS week: 1608 Day: 4 MJD: 55504
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 742 17 10 13 19 21 --- 8 | 27 23 27 28 35 --- 23
R02 | 2099 17 13 17 18 24 --- 9 | 25 35 28 26 34 --- 25
R05 | 832 27 7 15 38 35 129 11 | 22 26 29 35 33 98 21
XR07 | ---- --- 11 --- --- 32 --- 18 | --- 9999 --- --- 9999 --- 9999
R08 | 1806 15 14 23 24 21 154 10 | 52 72 68 74 53 80 62
R09E | 1938 54 15 30 34 60 --- 21 | 44 28 39 40 58 --- 31
R10E | 1286 36 18 34 30 66 --- 20 | 49 31 45 26 69 --- 33
R11E | 1187 31 21 67 70 79 66 26 | 47 46 94 97 65 26 47
R12E | 1694 18 15 40 30 51 --- 16 | 26 25 56 33 52 --- 28
R13E | 1290 19 21 40 46 44 --- 17 | 27 25 47 35 53 --- 26
R15E | 4488 39 15 33 47 48 113 18 | 35 34 33 35 64 20 33
R16E | 1143 27 15 38 39 53 --- 17 | 34 25 43 36 64 --- 30
R17 | 1055 13 12 23 19 25 --- 9 | 32 44 33 38 44 --- 37
R18 | 1031 23 10 22 31 33 114 11 | 33 43 31 54 47 106 34
R19 | 1024 23 10 23 23 35 --- 12 | 25 33 43 39 40 --- 31
R20 | 2518 12 12 24 39 37 --- 11 | 31 32 44 47 37 --- 32
R21 | 1128 25 11 56 31 45 --- 18 | 49 49 72 40 18 --- 41
R22 | 1457 21 7 19 18 37 --- 11 | 41 42 56 54 64 --- 45
R23 | 894 22 22 87 70 48 125 26 | 41 44 97 97 61 54 48
R24 | 2104 37 8 34 54 21 --- 14 | 28 52 66 65 41 --- 43
------+-----------------------------------------+-------------------------------------
RMS | 1776 27 14 38 39 44 120 |T 35 37 50 47 49 64 35
WRMS | 1776 27 11 27 38 44 120 |NE 30 33 39 32 30 98 27
MEDI | 1286 23 12 30 31 37 114 |MD 33 34 44 39 52 54 33
Table 3.1608.5 GPS week: 1608 Day: 5 MJD: 55505
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 600 20 9 17 26 21 --- 9 | 32 25 35 42 46 --- 29
R02 | 1892 14 11 21 16 20 --- 9 | 18 21 30 23 22 --- 18
R05 | 1518 20 10 13 26 26 88 9 | 21 22 22 28 17 50 15
XR07 |>>>>> --- 20 --- --- 47 --- 30 | --- 9999 --- --- 9999 --- 9999
R08 | 1375 29 14 23 35 20 136 12 | 50 70 70 79 48 43 60
R09E | 1890 37 15 31 48 44 --- 17 | 33 20 33 31 47 --- 21
R10E | 1776 31 14 16 40 46 --- 15 | 30 25 28 30 54 --- 25
R11E | 1670 51 24 57 75 66 66 27 | 37 35 90 81 55 28 42
R12E | 2058 25 16 19 29 66 --- 18 | 32 30 36 33 60 --- 29
R13E | 2645 25 23 26 37 47 --- 17 | 22 28 43 47 52 --- 25
R15E | 1356 35 16 36 31 32 107 16 | 35 30 32 36 38 28 24
R16E | 1389 36 16 36 33 55 --- 19 | 22 30 38 33 57 --- 27
R17 | 1554 34 14 24 23 42 --- 15 | 24 31 34 30 41 --- 25
R18 | 1403 16 17 32 59 14 61 12 | 45 29 64 69 35 45 38
R19 | 934 13 21 24 36 17 --- 11 | 30 39 40 55 25 --- 33
R20 | 1950 21 18 33 22 34 --- 15 | 26 17 49 44 35 --- 23
R21 | 871 19 11 27 23 27 --- 11 | 37 38 55 47 52 --- 41
R22 | 2753 26 16 26 17 20 --- 12 | 37 54 66 51 49 --- 51
R23 | 735 48 11 17 26 43 83 17 | 23 45 68 57 72 37 44
R24 | 1903 29 20 32 83 44 --- 17 | 23 40 61 88 66 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1689 30 16 29 40 39 94 |T 30 33 47 47 45 38 32
WRMS | 1689 30 15 26 35 39 94 |NE 27 26 35 35 34 50 25
MEDI | 1554 26 16 26 31 34 83 |MD 30 30 40 44 48 37 29
Table 3.1608.6 GPS week: 1608 Day: 6 MJD: 55506
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 634 27 24 37 46 24 --- 16 | 30 40 54 43 42 --- 35
R02 | 1116 38 11 14 28 17 --- 11 | 20 25 30 31 24 --- 21
R05 | 782 21 7 24 24 17 85 9 | 19 22 25 24 20 59 19
XR07M | 2749 34 29 --- --- 46 --- 24 | 4 9999 --- --- 9999 --- 9999
R08M | 1274 56 20 23 27 20 197 17 | 57 87 89 100 72 62 79
R09E | 1895 39 15 45 40 48 --- 20 | 27 21 37 25 51 --- 20
R10E | 1610 42 17 13 30 40 --- 16 | 31 24 24 24 48 --- 25
R11E | 1654 49 22 35 64 59 55 22 | 36 30 50 76 54 32 31
R12E | 1690 37 18 36 41 58 --- 20 | 26 19 35 44 59 --- 24
R13E | 3058 23 15 27 39 45 --- 15 | 36 27 36 38 49 --- 28
R15E | 1719 30 17 28 36 25 115 13 | 37 32 39 43 47 29 31
R16E | 1243 51 19 39 36 46 --- 21 | 21 30 29 31 50 --- 23
R17M | 2248 35 12 18 30 18 --- 11 | 32 46 39 55 35 --- 36
R18M | 2386 22 9 10 43 24 123 9 | 28 44 38 66 52 62 40
R19M | 1097 19 11 19 48 15 --- 9 | 34 45 57 79 44 --- 44
R20M | 1146 27 12 24 15 35 --- 13 | 28 39 53 48 51 --- 40
R21 | 670 12 8 28 48 26 --- 11 | 52 54 53 76 54 --- 50
R22M | 4548 29 8 16 47 27 --- 11 | 45 69 73 79 70 --- 65
R23M | 650 22 14 66 42 34 40 20 | 28 43 59 66 51 45 37
R24M | 705 33 19 29 21 17 --- 13 | 29 44 69 75 49 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 1847 34 15 31 39 34 115 |T 31 39 46 53 48 48 36
WRMS | 1847 34 12 28 36 34 115 |NE 30 35 40 43 35 59 31
MEDI | 1274 30 15 27 39 26 85 |MD 29 39 39 48 50 45 35
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