[IGSREPORT-19124] Wk 1606 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Nov 4 05:47:48 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1606 (Oct 17, 2010 - Oct 23, 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 2.1606.
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:
igl1606[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1606 in the SP3 format.
igl16067.sum Combination Report for GPS Week 1606.
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 | 348.4 ns
1 | 430.4 ns
2 | 436.5 ns
3 | 427.0 ns
4 | 433.3 ns
5 | 373.8 ns
6 | 327.4 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 1.1606, 1a.1606).
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 2.1606.0-6)
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 3.1606.0-6).
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 1606 summary. (Oct 17, 2010 - Oct 23, 2010)
Table 1.1606.a GPS week : 1606 MJD: 55486.0-55492.0
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 129| 0 1 -1 19 -17 -41 -.20 29 28 | 0 17 2065 2145
| 1 3 3 21 21 97 .06 | 0 179
cod 227| 0 0 -4 17 5 6 -.15 16 13 | --- --- --- ---
| 1 1 3 11 12 46 .03 | --- ---
esx 143| 0 0 -2 -35 12 37 .38 29 25 | 55348 474 4400 9321
| 1 1 4 22 36 44 .05 | 42476 2893
gfz 195| 0 0 -4 -34 -9 25 -.19 35 33 | 239245 755 4414 8450
| 1 1 5 58 19 69 .10 | 48209 2686
iac n/a| 0 0 17 -36 -10 18 .14 39 39 | 396997 -695 4387 9085
| 2 2 15 10 12 36 .06 | 45548 1170
mcc n/a| 2 1 6 -102 -26 242 -.12 79 79 | --- --- --- ---
| 6 10 22 67 69 391 .29 | --- ---
Table 1.1606.b GPS week : 1606 MJD: 55486.0-55492.0
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 14 15 12 13 11 10 |
R02 | 8 12 8 14 8 10 12 |
R05 | 11 12 10 8 9 12 11 |
R07 | 15 13 14 11 11 8 9 |
R08 | 17 11 14 11 10 11 8 |
R09 | 15 15 17 17 19 17 25 |
R10 | 21 20 17 17 16 19 25 |
R11 | 23 24 30 34 37 29 31 |
R12 | 11 12 15 13 18 23 18 |
R13 | 17 16 22 20 18 21 23 |
R14 | 17 14 21 24 29 19 23 |
R15 | 18 16 16 19 19 17 21 |
R16 | 17 18 18 17 17 19 22 |
R17 | 10 12 10 14 13 10 16 |
R18 | 12 13 9 12 9 9 12 |
R19 | 15 10 7 10 11 8 8 |
R20 | 11 11 10 12 16 13 10 |
R21 | 8 7 21 13 13 13 14 |
R22 | 12 9 7 19 9 11 15 |
R23 | 14 12 14 11 9 10 14 |
R24 | 10 9 9 9 9 12 12 |
Table 1.1606.c GPS week : 1606 MJD: 55486.0-55492.0
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 1606 0 | 78 -79 168 -791 -251 -12270 86.7 2041 2041 | 348383 0
brd 1606 1 | 49 43 196 734 2012 -6957 88.3 1931 1931 | 430357 0
brd 1606 2 | -39 51 87 -773 -1204 -9437 86.3 2262 2262 | 436540 0
brd 1606 3 | -34 14 48 439 55 -11250 87.6 2172 2172 | 427023 0
brd 1606 4 | -53 -55 53 289 -135 -11310 87.2 1913 1913 | 433330 0
brd 1606 5 | -73 75 179 -439 -360 -10390 87.8 1889 1889 | 373814 0
brd 1606 6 | 137 -83 100 251 -410 -10810 86.5 1899 1899 | 327406 0
-------------+------------------------------------------------------------+----------------
brd 1606 mean| 8 -4 119 -41 -41 -10346 87.2 2015 2015 | 396693 0
brd 1606 sdev| 79 66 61 617 988 1730 .7 148 148 | 45900 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 2.1606.0 GPS week: 1606 Day: 0 MJD: 55486
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 129| 0 5 0 -6 2 -74 -.17 26 26 | 0 339 2125 2216
cod 227| -1 -1 -4 24 0 -4 -.18 15 13 | --- --- --- ---
esx 143| 0 -1 -5 -8 20 -13 .41 25 23 | 10011 -222 4985 10338
gfz 195| 0 -1 -13 -12 -15 34 -.23 32 27 | 197306 -191 4996 9832
iac n/a| 3 3 18 -36 -18 71 .04 38 38 | 349335 917 4970 10169
mcc n/a| 8 -7 -4 -128 -85 112 -.53 80 80 | --- --- --- ---
Table 2.1606.1 GPS week: 1606 Day: 1 MJD: 55487
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 129| 0 1 0 12 -15 -104 -.24 25 25 | 0 -169 2295 2384
cod 227| 0 -2 -2 19 11 -19 -.10 15 12 | --- --- --- ---
esx 143| 1 0 3 -17 6 126 .33 26 25 | 87904 -5303 5655 8898
gfz 195| 1 0 2 -112 -31 160 -.27 35 33 | 279766 -4630 5665 8424
iac n/a| 0 0 2 -46 -4 19 .11 32 32 | 430845 -1588 5652 9445
mcc n/a| 6 2 11 -41 8 676 -.30 69 69 | --- --- --- ---
Table 2.1606.2 GPS week: 1606 Day: 2 MJD: 55488
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 129| -2 1 -1 31 -18 -9 -.13 25 24 | 0 -65 2383 2486
cod 227| 0 0 -4 4 3 3 -.17 18 18 | --- --- --- ---
esx 143| 1 0 -5 -38 48 49 .36 29 25 | 92362 4254 4171 9123
gfz 195| -2 0 -4 -42 0 2 -.24 37 34 | 282156 2972 4189 8176
iac n/a| 0 0 19 -32 1 31 .16 37 37 | 435786 477 4172 8735
mcc n/a| 6 15 9 -54 -98 -37 .22 59 59 | --- --- --- ---
Table 2.1606.3 GPS week: 1606 Day: 3 MJD: 55489
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 129| 0 1 -7 0 -21 138 -.17 25 22 | 0 9 1776 1855
cod 227| -2 1 -6 22 23 -71 -.12 17 14 | --- --- --- ---
esx 143| 0 -4 0 -58 -13 5 .35 33 25 | 86658 1306 3918 10364
gfz 195| 0 -2 -8 -70 -5 -45 -.12 37 33 | 269747 1451 3932 9175
iac n/a| 1 0 34 -30 -21 -21 .20 44 44 | 427377 -412 3900 9687
mcc n/a| -10 11 15 -82 0 351 .13 67 67 | --- --- --- ---
Table 2.1606.4 GPS week: 1606 Day: 4 MJD: 55490
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 129| 1 0 -2 21 -31 -128 -.17 31 29 | 0 73 2047 2124
cod 227| 0 0 -9 19 -11 50 -.16 16 12 | --- --- --- ---
esx 143| 1 -1 -8 -25 41 41 .33 30 24 | 84246 1483 4116 9085
gfz 195| 0 -2 -6 -51 10 16 -.27 37 29 | 272659 3293 4136 8004
iac n/a| 0 2 38 -49 -13 57 .19 44 44 | 433129 -331 4111 8590
mcc n/a| 1 3 28 -36 -2 732 -.06 67 67 | --- --- --- ---
Table 2.1606.5 GPS week: 1606 Day: 5 MJD: 55491
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 129| 0 2 -2 26 14 -130 -.25 35 36 | 0 -175 1762 1827
cod 227| -1 0 -6 0 15 69 -.17 13 11 | --- --- --- ---
esx 143| 0 0 3 -30 -52 31 .42 29 23 | 35036 965 3677 8967
gfz 195| 0 -1 1 -25 10 50 .01 34 25 | 210005 1967 3662 7847
iac n/a| -1 0 11 -38 7 -11 .11 37 37 | 374845 -1894 3621 8567
mcc n/a| 2 -5 23 -151 89 244 -.39 56 56 | --- --- --- ---
Table 2.1606.6 GPS week: 1606 Day: 6 MJD: 55492
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 129| -1 -5 2 56 -50 19 -.30 38 35 | 0 107 2071 2125
cod 227| 0 1 0 31 -7 18 -.17 19 13 | --- --- --- ---
esx 143| -1 0 -2 -70 39 21 .45 27 27 | -8780 840 4283 8478
gfz 195| 0 1 -4 77 -39 -42 -.18 36 51 | 163080 424 4319 7694
iac n/a| 3 -3 -1 -19 -23 -15 .15 40 40 | 327664 -2037 4287 8406
mcc n/a| 1 -12 -37 -220 -95 -379 .09 155 155 | --- --- --- ---
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 3.1606.0 GPS week: 1606 Day: 0 MJD: 55486
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 925 28 11 11 18 21 --- 10 | 27 40 37 45 34 --- 34
R02 | 1026 16 9 9 13 24 --- 8 | 21 33 33 34 43 --- 30
R05 | 2838 20 12 16 18 28 --- 10 | 32 42 41 39 41 --- 38
R07 | 2479 29 17 33 33 24 --- 14 | 31 36 66 47 41 --- 38
R08 | 1193 38 11 38 20 26 71 16 | 30 35 53 38 34 17 33
R09E | 1862 14 15 26 25 52 --- 15 | 22 22 37 30 52 --- 22
R10E | 1813 51 25 28 46 44 --- 20 | 30 29 40 42 48 --- 28
R11E | 3026 41 29 39 68 59 --- 23 | 46 56 63 63 63 --- 49
R12E | 1204 15 13 21 19 26 --- 10 | 28 30 36 23 42 --- 29
R13E | 2012 27 13 35 37 45 --- 16 | 31 18 39 37 51 --- 25
R14E | 1350 31 14 26 32 53 --- 17 | 50 62 54 52 77 --- 56
R15E | 4439 17 17 24 44 64 85 17 | 19 24 34 32 64 21 24
R16E | 609 24 15 33 38 51 --- 17 | 19 20 43 42 44 --- 22
R17 | 921 11 13 20 21 25 --- 10 | 38 51 44 53 48 --- 44
R18 | 1787 21 15 26 37 27 --- 12 | 36 40 48 46 39 --- 36
R19 | 1002 24 14 30 33 41 --- 15 | 24 31 33 39 37 --- 26
R20 | 1855 27 11 20 26 15 --- 10 | 42 39 39 41 42 --- 37
R21 | 931 14 12 12 22 15 --- 7 | 28 39 33 44 34 --- 33
R22 | 910 28 12 18 19 26 --- 11 | 33 40 45 45 45 --- 38
R23 | 2650 24 16 19 23 42 82 14 | 28 37 32 49 46 45 31
R24 | 3062 15 12 19 30 24 --- 9 | 41 42 49 61 51 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 2040 26 15 25 32 38 80 |T 31 36 42 42 46 27 34
WRMS | 2040 26 13 23 27 38 80 |NE 31 38 42 44 41 31 35
MEDI | 1787 24 13 24 26 27 82 |MD 30 37 40 42 44 21 33
Table 3.1606.1 GPS week: 1606 Day: 1 MJD: 55487
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 936 33 21 19 38 18 --- 13 | 22 37 40 50 30 --- 28
R02 | 1637 15 17 28 29 25 --- 12 | 25 32 38 39 48 --- 30
R05 | 1816 30 11 23 22 17 --- 11 | 24 30 38 40 41 --- 28
R07 | 1671 14 16 33 38 19 --- 12 | 33 33 39 50 32 --- 27
R08 | 1270 23 14 22 26 20 68 11 | 31 32 35 38 52 29 32
R09E | 815 18 11 34 36 42 --- 15 | 21 17 33 35 46 --- 16
R10E | 2092 44 18 37 43 44 --- 20 | 41 15 25 25 54 --- 21
R11E | 5516 44 31 44 62 56 --- 24 | 52 67 58 79 63 --- 49
R12E | 1615 23 16 18 50 29 --- 12 | 21 25 36 42 43 --- 25
R13E | 1045 30 18 32 36 37 --- 16 | 20 13 43 25 45 --- 20
R14E | 1574 29 13 24 41 31 --- 13 | 50 54 53 50 65 --- 51
R15E | 3421 18 15 26 34 48 64 15 | 29 26 31 30 64 30 25
R16E | 1786 20 18 29 26 56 --- 18 | 28 21 32 27 54 --- 21
R17 | 1035 13 22 15 17 30 --- 12 | 32 37 27 37 21 --- 25
R18 | 748 34 9 27 41 20 --- 13 | 48 23 36 36 24 --- 22
R19 | 1754 20 9 19 35 23 --- 10 | 27 23 39 48 23 --- 23
R20 | 1098 17 7 27 26 23 --- 10 | 38 51 69 63 59 --- 51
R21 | 847 12 9 15 25 14 --- 7 | 20 20 36 33 31 --- 22
R22 | 782 11 11 22 33 17 --- 9 | 38 26 27 46 38 --- 28
R23 | 629 25 5 15 33 35 75 11 | 18 24 28 46 45 44 24
R24 | 1672 21 12 16 18 14 --- 9 | 26 41 52 65 43 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1930 25 15 26 35 32 69 |T 30 30 38 43 43 34 28
WRMS | 1930 25 12 25 33 32 69 |NE 29 31 38 45 37 36 29
MEDI | 1574 21 14 24 34 25 68 |MD 28 26 36 40 45 30 25
Table 3.1606.2 GPS week: 1606 Day: 2 MJD: 55488
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1019 20 30 29 17 17 --- 14 | 30 42 20 21 31 --- 28
R02 | 1613 13 10 18 14 16 --- 8 | 26 29 29 25 32 --- 25
R05 | 913 14 17 24 16 11 --- 10 | 24 30 20 26 30 --- 21
R07 | 1075 23 17 27 32 29 --- 13 | 34 36 50 34 31 --- 33
R08 | 1716 15 23 23 26 36 28 14 | 31 29 26 40 46 40 27
R09E | 1091 19 16 26 32 57 --- 17 | 30 25 31 28 58 --- 23
R10E | 4879 31 17 24 26 46 --- 16 | 36 29 28 31 58 --- 27
R11E | 5950 45 22 58 51 86 --- 29 | 45 42 63 54 83 --- 39
R12E | 1900 19 16 29 41 40 --- 14 | 35 26 47 36 53 --- 32
R13E | 949 52 28 27 50 37 --- 21 | 32 24 33 46 43 --- 18
R14E | 1588 51 26 25 39 38 --- 21 | 51 58 54 54 70 --- 53
R15E | 4066 21 16 25 36 51 67 16 | 40 28 30 27 61 33 31
R16E | 1252 23 25 28 37 48 --- 17 | 30 27 35 31 56 --- 22
R17 | 946 14 12 22 37 19 --- 9 | 41 40 34 40 26 --- 34
R18 | 1088 14 12 11 37 25 --- 9 | 27 31 31 46 36 --- 26
R19 | 1518 8 10 13 27 19 --- 7 | 17 21 19 29 26 --- 17
R20 | 2095 15 11 25 54 19 --- 10 | 52 51 68 92 55 --- 55
R21 | 1629 18 20 67 37 28 --- 20 | 22 37 71 47 28 --- 31
R22 | 663 14 7 17 28 11 --- 7 | 44 34 50 37 33 --- 38
R23 | 652 24 17 25 39 35 72 14 | 26 27 26 50 37 45 21
R24 | 987 14 12 17 59 19 --- 8 | 23 36 34 59 35 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2261 25 18 29 37 37 59 |T 33 33 38 40 44 39 30
WRMS | 2261 24 18 25 34 37 59 |NE 30 34 36 42 34 42 29
MEDI | 1252 19 17 25 37 29 67 |MD 31 30 33 37 37 40 28
Table 3.1606.3 GPS week: 1606 Day: 3 MJD: 55489
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1453 18 22 23 24 16 --- 11 | 44 55 57 67 46 --- 48
R02 | 1293 27 9 36 35 21 --- 13 | 23 30 53 51 34 --- 26
R05 | 1149 14 8 13 29 23 --- 8 | 38 32 38 47 39 --- 32
R07 | 1862 18 15 20 16 26 --- 10 | 23 37 41 35 49 --- 34
R08 | 1558 17 14 11 25 38 38 11 | 36 40 41 44 60 23 40
R09E | 1120 18 18 34 38 55 --- 17 | 41 34 37 31 63 --- 30
R10E | 3977 20 16 24 36 61 --- 16 | 39 27 26 40 65 --- 27
R11E | 5573 48 29 72 56 104 --- 34 | 46 53 93 76 84 --- 50
R12E | 971 15 12 20 39 49 --- 13 | 37 39 50 39 67 --- 42
R13E | 979 25 25 35 45 58 --- 19 | 28 25 52 32 55 --- 28
R14E | 2007 53 26 34 36 52 --- 23 | 58 67 73 58 81 --- 64
R15E | 3493 39 19 32 53 49 91 19 | 24 21 28 36 58 31 21
R16E | 1212 18 14 44 39 48 --- 17 | 47 24 57 42 55 --- 33
R17 | 649 31 11 10 25 41 --- 14 | 36 51 45 52 46 --- 42
R18 | 1416 23 11 17 24 36 --- 12 | 54 47 55 58 38 --- 45
R19 | 2216 10 17 22 23 20 --- 10 | 44 40 39 50 25 --- 35
R20 | 2206 14 15 31 42 27 --- 12 | 27 43 38 41 37 --- 32
R21 | 2213 13 17 34 54 25 --- 12 | 37 43 51 68 33 --- 34
R22 | 1041 21 13 65 37 27 --- 19 | 44 35 65 46 33 --- 34
R23 | 795 21 10 25 21 24 61 11 | 36 30 49 48 23 33 31
R24 | 1209 17 10 16 51 19 --- 8 | 28 48 44 69 48 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 2171 25 17 33 37 44 67 |T 37 39 49 49 49 29 36
WRMS | 2171 22 14 25 33 44 67 |NE 36 40 47 52 39 28 36
MEDI | 1416 18 15 25 36 36 61 |MD 37 39 49 47 48 31 34
Table 3.1606.4 GPS week: 1606 Day: 4 MJD: 55490
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1896 22 14 27 28 34 --- 13 | 41 48 54 44 53 --- 45
R02 | 1098 12 11 15 19 17 --- 8 | 20 27 34 36 33 --- 24
R05 | 815 16 12 14 19 23 --- 9 | 24 34 32 38 40 --- 30
R07 | 1199 24 15 14 31 21 --- 10 | 29 38 32 46 40 --- 33
R08 | 1110 17 14 12 25 25 42 9 | 38 42 37 39 47 23 40
R09E | 1243 36 14 36 38 50 --- 18 | 31 36 46 34 60 --- 34
R10E | 3520 29 15 21 28 50 --- 16 | 44 27 31 21 58 --- 29
R11E | 4020 63 22 74 73 110 --- 37 | 42 46 97 93 81 --- 44
R12E | 914 32 17 30 25 54 --- 18 | 43 29 47 39 49 --- 32
R13E | 762 13 20 22 35 67 --- 18 | 33 31 39 36 65 --- 33
R14E | 1798 70 33 41 63 65 --- 29 | 59 92 87 84 75 --- 73
R15E | 2801 45 24 19 42 44 96 19 | 45 27 40 47 62 27 33
R16E | 930 33 17 33 33 43 --- 17 | 24 17 45 27 49 --- 22
R17 | 911 24 13 26 45 34 --- 13 | 50 50 77 84 49 --- 53
R18 | 848 16 11 17 20 19 --- 8 | 40 51 38 42 41 --- 43
R19 | 2697 14 11 30 27 20 --- 10 | 33 39 32 42 22 --- 29
R20 | 3252 32 10 43 22 26 --- 16 | 32 39 73 60 44 --- 41
R21 | 1658 23 9 32 38 29 --- 13 | 24 30 49 43 31 --- 26
R22 | 733 10 7 16 49 29 --- 8 | 39 37 39 28 35 --- 32
R23 | 1226 14 7 23 29 23 48 9 | 26 31 46 39 18 31 27
R24 | 1003 21 9 19 29 15 --- 9 | 24 37 44 39 34 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1912 31 16 30 37 44 67 |T 35 38 48 45 46 27 35
WRMS | 1912 29 12 24 29 44 67 |NE 32 38 45 44 37 27 34
MEDI | 1199 23 14 23 29 29 48 |MD 33 37 44 39 47 27 33
Table 3.1606.5 GPS week: 1606 Day: 5 MJD: 55491
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2587 16 13 30 31 12 --- 10 | 46 37 54 59 50 --- 41
R02 | 1167 29 8 17 21 18 --- 9 | 27 16 28 34 25 --- 18
R05 | 865 24 15 22 32 28 --- 12 | 26 39 45 43 26 --- 33
R07 | 1263 17 9 13 35 16 --- 7 | 25 32 34 47 33 --- 29
R08 | 521 25 7 26 18 22 32 10 | 34 17 27 22 19 49 16
R09E | 788 43 11 30 30 42 --- 17 | 25 26 25 19 53 --- 24
R10E | 1077 55 19 23 37 44 --- 19 | 37 27 24 31 57 --- 25
R11E | 1816 63 23 52 57 78 --- 29 | 48 41 56 57 81 --- 38
R12E | 1887 50 17 44 30 57 --- 22 | 44 38 68 35 72 --- 48
R13E | 859 27 16 36 44 68 --- 21 | 30 28 42 45 62 --- 27
R14E | 1841 42 17 29 29 50 --- 18 | 42 89 99 80 83 --- 76
R15E | 3307 32 10 37 46 47 84 17 | 36 30 36 37 62 37 29
R16E | 1362 48 17 39 38 38 --- 19 | 43 32 38 31 56 --- 30
R17 | 1188 25 14 13 25 14 --- 9 | 59 46 45 49 27 --- 43
R18 | 1020 20 7 21 37 15 --- 8 | 60 54 57 45 39 --- 52
R19 | 2035 17 7 21 25 12 --- 8 | 56 54 66 66 49 --- 55
R20 | 4536 27 12 18 23 35 --- 12 | 31 52 46 43 49 --- 45
R21 | 955 41 14 23 17 14 --- 13 | 36 47 46 58 39 --- 39
R22 | 747 29 10 23 50 17 --- 10 | 39 31 34 51 28 --- 28
R23 | 2083 15 9 30 28 17 37 10 | 36 29 46 43 23 52 30
R24 | 2385 34 9 19 22 24 --- 11 | 26 30 36 32 18 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1888 35 13 29 34 37 56 |T 38 37 45 44 45 46 35
WRMS | 1888 36 10 23 25 37 56 |NE 38 37 43 45 32 50 34
MEDI | 1263 29 12 23 30 24 37 |MD 36 32 45 43 49 49 30
Table 3.1606.6 GPS week: 1606 Day: 6 MJD: 55492
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 535 16 10 19 20 21 --- 9 | 42 41 51 50 47 --- 42
R02 | 2805 36 9 18 22 23 --- 12 | 29 25 38 34 34 --- 25
R05 | 1820 20 14 20 25 23 --- 10 | 28 45 43 45 41 --- 38
R07 | 1606 19 14 9 64 18 --- 8 | 30 37 29 48 36 --- 30
R08 | 741 12 11 18 27 16 238 8 | 31 29 41 30 34 53 30
R09E | 934 67 23 40 38 47 --- 24 | 46 20 32 28 63 --- 25
R10E | 1055 79 15 37 38 34 --- 24 | 51 25 26 23 53 --- 28
R11E | 766 40 33 55 53 86 --- 30 | 45 42 82 76 86 --- 46
R12E | 1360 38 19 27 29 44 --- 17 | 56 34 49 42 66 --- 42
R13E | 1797 44 31 27 29 61 --- 23 | 34 41 40 35 60 --- 33
R14E | 1384 35 32 32 38 63 --- 23 | 59 85 61 58 93 --- 70
R15E | 1206 38 20 26 24 60 55 20 | 80 71 72 56 95 69 73
R16E | 957 49 30 28 38 45 --- 21 | 40 15 46 41 59 --- 28
R17 | 857 38 15 28 39 35 --- 16 | 37 56 65 55 36 --- 47
R18 | 1149 32 13 21 15 21 --- 12 | 39 62 68 52 43 --- 54
R19 | 1801 17 8 14 29 18 --- 8 | 43 53 66 69 51 --- 52
R20 | 3161 22 15 11 38 21 --- 9 | 47 62 57 46 52 --- 55
R21 | 2483 28 14 30 36 24 --- 13 | 41 63 62 68 34 --- 51
R22 | 903 32 12 24 54 38 --- 15 | 28 29 35 55 36 --- 27
R23 | 2654 28 13 33 36 20 109 13 | 42 33 36 46 19 57 25
R24 | 4454 24 14 21 29 24 --- 11 | 27 32 26 32 21 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1898 37 19 27 36 40 155 |T 41 42 48 47 50 59 40
WRMS | 1898 35 13 27 51 40 155 |NE 35 43 47 48 37 55 38
MEDI | 1360 32 14 26 36 24 109 |MD 41 41 46 46 47 57 38
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