[IGSREPORT-18548] Wk 1580 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu May 6 05:31:29 PDT 2010
******************************************************************************
IGS Electronic Report 06 May 05:31:48 PDT 2010 Message Number 18548
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1580 (Apr 18, 2010 - Apr 24, 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 2.1580.
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:
igl1580[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1580 in the SP3 format.
igl15807.sum Combination Report for GPS Week 1580.
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 | 400.8 ns
1 | 379.5 ns
2 | 461.7 ns
3 | 463.2 ns
4 | 465.4 ns
5 | 405.0 ns
6 | 404.0 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 | IAC | R11
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 1.1580, 1a.1580).
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 2.1580.0-6)
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 3.1580.0-6).
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 1580 summary. (Apr 18, 2010 - Apr 24, 2010)
Table 1.1580.a GPS week : 1580 MJD: 55304.0-55310.0
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| 1 0 4 4 3 -15 -.16 21 20 | 0 -105 1722 1786
| 1 0 3 18 20 122 .03 | 0 124
cod 243| -2 0 10 43 -26 12 -.10 16 14 | --- --- --- ---
| 1 1 2 24 29 42 .02 | --- ---
esx 142| 0 0 5 -52 43 25 .48 25 23 | 95716 -765 3993 8665
| 1 2 2 28 19 64 .07 | 39229 3424
gfz 195| 0 -1 10 -78 -32 75 -.11 27 27 | 272989 -1568 4015 8853
| 2 1 3 39 40 55 .07 | 36277 1727
iac n/a| 0 1 -33 -26 0 -11 -.13 30 30 | 7296 -97 218247 292594
| 1 0 9 24 27 99 .07 | 688562 1978
mcc n/a| 2 6 67 -131 -72 217 -.01 157 157 | --- --- --- ---
| 8 11 17 194 156 568 .51 | --- ---
Table 1.1580.b GPS week : 1580 MJD: 55304.0-55310.0
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 | 11 7 9 9 9 13 12 |
R02 | 9 11 9 12 12 10 9 |
R03 | 10 10 11 10 16 11 10 |
R04 | 8 9 8 9 10 11 10 |
R05 | 11 10 11 8 9 9 11 |
R07 | 8 9 14 13 13 9 12 |
R08 | 8 11 11 8 9 9 9 |
R10 | 12 18 15 14 22 26 18 |
R11 | 19 140 0 46 26 40 23 |
R13 | 14 12 13 15 21 21 24 |
R14 | 16 14 16 20 15 17 18 |
R15 | 15 16 17 16 18 13 14 |
R17 | 10 11 14 15 13 15 13 |
R18 | 10 9 10 13 13 10 7 |
R19 | 11 11 10 12 13 10 12 |
R20 | 11 10 13 13 13 15 12 |
R21 | 13 11 12 15 17 18 17 |
R22 | 10 10 13 11 14 14 10 |
R23 | 13 11 12 10 14 16 15 |
R24 | 10 11 9 9 10 11 12 |
Table 1.1580.c GPS week : 1580 MJD: 55304.0-55310.0
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 1580 0 | -8 -20 272 -21 -969 -17100 86.0 1680 1680 | 400772 0
brd 1580 1 | -25 -13 427 -302 -1411 -12470 86.1 1688 1688 | 379483 0
brd 1580 2 | -5 -87 387 233 -1168 -6995 89.4 1889 1889 | 461714 0
brd 1580 3 | 117 31 362 -1146 243 -9524 90.9 2096 2096 | 463193 0
brd 1580 4 | 51 -92 313 905 1477 -12570 88.2 1920 1920 | 465427 0
brd 1580 5 | 19 -24 270 1278 -306 -9060 87.2 2051 2051 | 405013 0
brd 1580 6 | 0 81 251 -3282 1979 -12330 85.7 2420 2420 | 403971 0
-------------+------------------------------------------------------------+----------------
brd 1580 mean| 21 -17 326 -333 -22 -11435 87.6 1963 1963 | 425653 0
brd 1580 sdev| 48 61 66 1522 1325 3272 2.0 257 257 | 36374 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 2.1580.0 GPS week: 1580 Day: 0 MJD: 55304
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 4 25 29 198 -.19 21 19 | 0 45 1695 1755
cod 243| -2 2 9 44 -63 -53 -.10 15 14 | --- --- --- ---
esx 142| 0 -5 7 -69 38 -44 .52 23 22 | 68490 -193 4394 9978
gfz 195| 1 -2 14 -32 14 3 -.23 27 27 | 250615 473 4409 10507
iac n/a| 2 1 -25 -22 26 -91 -.14 22 22 | 401905 2147 4397 11110
mcc n/a| -10 25 84 -439 -364 1294 .28 267 267 | --- --- --- ---
Table 2.1580.1 GPS week: 1580 Day: 1 MJD: 55305
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 0 1 8 -3 -96 -.14 17 17 | 0 -165 1811 1865
cod 243| -2 0 10 55 0 40 -.11 13 11 | --- --- --- ---
esx 142| -1 0 5 -48 16 73 .55 23 21 | 52431 -4149 3544 7964
gfz 195| 0 1 11 -76 -69 104 -.08 24 24 | 229478 -2390 3670 8474
iac n/a| 0 0 -36 -65 -15 10 -.14 30 30 | 379577 -844 3542 8691
mcc n/a| -9 1 69 -275 -132 -432 -.21 149 149 | --- --- --- ---
Table 2.1580.2 GPS week: 1580 Day: 2 MJD: 55306
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 2 13 -27 28 -.13 18 17 | 0 -78 1744 1803
cod 243| 0 1 7 54 5 16 -.07 15 14 | --- --- --- ---
esx 142| 0 0 2 -77 57 25 .43 28 26 | 135543 -1457 5134 9301
gfz 195| 1 -3 11 -66 -86 65 -.04 27 27 | 309825 -371 5142 8944
iac n/a| 0 2 -21 -34 -38 -81 -.03 28 28 | 461374 1081 5143 9100
mcc n/a| 5 8 75 171 -117 138 1.02 118 118 | --- --- --- ---
Table 2.1580.3 GPS week: 1580 Day: 3 MJD: 55307
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 0 1 20 -12 57 -.13 17 17 | 0 -95 1497 1579
cod 243| -2 0 8 6 -7 -1 -.09 15 14 | --- --- --- ---
esx 142| 2 2 5 -53 49 -22 .58 28 26 | 138677 3138 3521 8052
gfz 195| 2 -1 7 -39 -29 45 -.03 29 29 | 309164 -1659 3535 8453
iac n/a| 1 0 -27 13 4 -150 -.10 30 30 | -999999 -3564 950533 999999
mcc n/a| 7 13 77 -83 -60 346 -.20 138 138 | --- --- --- ---
Table 2.1580.4 GPS week: 1580 Day: 4 MJD: 55308
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 0 8 -18 25 -156 -.16 21 21 | 0 5 1663 1714
cod 243| -1 0 9 65 -54 63 -.11 19 16 | --- --- --- ---
esx 142| 1 0 4 -49 69 92 .44 26 23 | 136986 795 3511 7774
gfz 195| -2 -3 10 -119 -17 173 -.17 28 28 | 313878 -2822 3500 8064
iac n/a| 0 0 -38 -39 12 23 -.25 35 35 | -999999 -790 555586 999999
mcc n/a| 6 10 74 -165 61 332 -.25 175 175 | --- --- --- ---
Table 2.1580.5 GPS week: 1580 Day: 5 MJD: 55309
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 0 5 -23 13 -20 -.21 25 25 | 0 -337 1966 2044
cod 243| -4 -1 14 11 -56 50 -.14 19 17 | --- --- --- ---
esx 142| 2 1 6 7 19 -49 .45 23 20 | 73961 -6133 4301 9369
gfz 195| 2 -1 3 -141 18 97 -.08 24 24 | 251489 -4282 4302 9356
iac n/a| 0 2 -42 -24 33 99 -.10 32 32 | 405307 -562 4966 10341
mcc n/a| 9 -12 51 -118 108 189 -.52 131 131 | --- --- --- ---
Table 2.1580.6 GPS week: 1580 Day: 6 MJD: 55310
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 -1 8 3 0 -115 -.18 27 25 | 0 -111 1684 1746
cod 243| -1 0 11 67 -7 -26 -.10 17 14 | --- --- --- ---
esx 142| 0 0 10 -73 51 99 .38 23 21 | 63929 2642 3548 8217
gfz 195| -1 0 12 -73 -55 35 -.13 28 28 | 246474 70 3551 8179
iac n/a| 2 0 -45 -16 -26 110 -.12 32 32 | 402912 1851 3567 8921
mcc n/a| 9 2 35 -8 -2 -349 -.19 123 123 | --- --- --- ---
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 3.1580.0 GPS week: 1580 Day: 0 MJD: 55304
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1354 11 17 25 25 19 --- 10 | 26 31 28 32 27 --- 25
R02 | 1885 14 10 19 19 17 --- 8 | 24 26 35 35 25 --- 24
R03 | 2579 21 15 12 29 16 --- 9 | 20 27 27 28 35 --- 20
R04 | 2010 11 8 18 26 18 --- 8 | 25 27 37 27 35 --- 26
R05 | 796 15 17 23 25 21 --- 11 | 41 37 28 38 44 --- 34
R07 | 2031 14 11 17 26 14 --- 8 | 39 32 34 36 31 --- 32
R08 | 1124 11 12 19 24 13 170 8 | 36 33 26 37 43 69 31
R10E | 2301 20 11 21 22 27 --- 11 | 62 60 66 64 56 --- 59
R11E | 958 45 21 28 50 35 --- 19 | 9999 9999 152 503 9999 --- 9999
R13E | 830 30 19 23 34 19 --- 13 | 32 24 39 46 43 --- 29
R14E | 1407 26 21 26 38 35 --- 15 | 34 30 52 31 45 --- 31
R15E | 1559 30 17 33 34 23 402 14 | 31 22 20 29 28 327 17
R17 | 1068 14 16 15 22 22 --- 10 | 36 48 43 37 35 --- 40
R18 | 2929 18 10 19 20 23 --- 10 | 24 34 22 26 20 --- 22
R19 | 1804 15 14 22 18 23 --- 10 | 25 29 32 31 28 --- 23
R20 | 1727 12 18 19 32 22 --- 10 | 35 36 28 39 26 --- 27
R21 | 2014 13 12 37 28 25 --- 13 | 32 35 42 37 40 --- 30
R22 | 678 15 17 23 16 14 --- 10 | 51 55 45 51 43 --- 47
R23 | 1052 29 13 24 17 18 150 12 | 17 24 38 28 29 50 20
R24 | 1190 12 16 15 17 23 --- 9 | 51 53 56 63 49 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1679 21 15 23 27 22 267 |T 33 34 42 60 35 148 30
WRMS | 1679 19 14 22 27 22 267 |NE 32 35 34 36 34 59 30
MEDI | 1407 15 15 21 25 21 170 |MD 32 32 35 36 35 69 29
Table 3.1580.1 GPS week: 1580 Day: 1 MJD: 55305
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1274 10 6 14 11 18 --- 6 | 21 21 25 24 20 --- 19
R02 | 1427 9 8 23 24 37 --- 10 | 29 21 36 27 31 --- 23
R03 | 2787 17 9 21 24 23 --- 9 | 20 22 37 36 31 --- 20
R04 | 3034 14 10 17 21 24 --- 8 | 19 24 29 16 27 --- 20
R05 | 1701 18 12 14 19 25 --- 9 | 25 33 39 23 37 --- 29
R07 | 1335 13 11 18 23 24 --- 9 | 37 29 30 37 28 --- 28
R08 | 2216 15 10 23 23 29 135 10 | 29 30 33 43 23 36 25
R10E | 1567 23 30 19 27 49 --- 17 | 50 48 42 48 54 --- 41
XR11E | 1846 --- 47 --- 1727 257 --- 139 | --- 9999 --- 563 9999 --- 9999
R13E | 487 23 8 23 37 34 --- 12 | 27 28 43 42 33 --- 26
R14E | 796 20 17 24 30 41 --- 14 | 27 21 36 37 39 --- 20
R15E | 1064 31 13 34 29 32 167 15 | 21 29 35 25 32 204 20
R17 | 1349 19 16 17 25 28 --- 11 | 28 26 29 22 36 --- 23
R18 | 1275 9 9 21 15 21 --- 8 | 12 22 31 19 22 --- 15
R19 | 2019 13 8 32 29 21 --- 10 | 14 17 33 33 19 --- 11
R20 | 2230 14 10 22 18 25 --- 9 | 24 19 29 21 29 --- 17
R21 | 1881 12 15 18 21 30 --- 10 | 28 24 32 33 42 --- 26
R22 | 1075 12 12 22 12 30 --- 10 | 37 41 39 31 30 --- 34
R23 | 1209 19 9 19 18 34 144 11 | 16 19 25 18 35 61 14
R24 | 870 11 12 33 30 17 --- 10 | 51 41 49 54 51 --- 43
------+-----------------------------------------+-------------------------------------
RMS | 1687 17 13 22 24 30 149 |T 27 27 34 57 32 100 23
WRMS | 1687 17 11 21 24 30 149 |NE 26 25 33 29 30 48 23
MEDI | 1349 14 10 21 23 28 144 |MD 27 24 33 31 31 61 23
Table 3.1580.2 GPS week: 1580 Day: 2 MJD: 55306
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 671 12 9 20 20 20 --- 8 | 28 28 27 30 25 --- 23
R02 | 1359 8 8 16 18 28 --- 8 | 18 22 22 19 46 --- 20
R03 | 3749 15 19 14 19 25 --- 10 | 15 24 29 18 33 --- 18
R04 | 3109 14 8 17 23 19 --- 8 | 22 27 32 26 28 --- 24
R05 | 2578 16 11 26 24 28 --- 11 | 20 28 32 31 41 --- 23
R07 | 1052 11 13 31 43 40 --- 13 | 35 31 62 67 27 --- 33
R08 | 1298 17 10 30 31 20 105 11 | 24 27 32 34 25 21 23
R10E | 1324 25 14 36 24 31 --- 14 | 53 37 60 43 51 --- 43
XR11E |31303 --- 5 --- --- --- --- 0 | --- 9999 --- --- --- --- 9999
R13E | 1046 19 14 32 42 27 --- 12 | 25 15 40 40 25 --- 17
R14E | 687 14 18 26 27 54 --- 16 | 20 21 42 37 39 --- 19
R15E | 2139 35 26 31 32 25 127 17 | 21 38 32 27 27 114 22
R17 | 2057 25 16 31 41 29 --- 14 | 22 32 32 38 38 --- 27
R18 | 1503 11 14 19 19 23 --- 9 | 17 31 33 30 42 --- 25
R19 | 1856 13 14 28 27 19 --- 10 | 17 20 36 22 30 --- 18
R20 | 2709 12 14 47 26 14 --- 13 | 27 24 52 35 15 --- 19
R21 | 1340 16 15 29 22 29 --- 12 | 23 29 35 41 42 --- 25
R22 | 1061 17 19 21 22 33 --- 12 | 54 55 45 49 42 --- 47
R23 | 1226 21 15 25 17 26 121 12 | 17 20 31 20 26 35 14
R24 | 1638 13 8 27 17 18 --- 9 | 23 30 43 35 25 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1888 18 15 28 27 28 118 |T 25 28 37 33 33 56 24
WRMS | 1888 17 14 26 27 28 118 |NE 24 28 36 33 32 28 24
MEDI | 1359 15 14 27 24 26 121 |MD 22 28 33 34 30 35 23
Table 3.1580.3 GPS week: 1580 Day: 3 MJD: 55307
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 848 12 11 17 22 25 --- 9 | 32 32 40 37 32 --- 31
R02 | 1032 21 11 20 25 31 --- 11 | 34 28 28 29 38 --- 25
R03 | 4009 9 10 32 31 21 --- 10 | 20 20 31 35 36 --- 19
R04 | 1449 12 13 16 22 22 --- 8 | 22 28 19 23 37 --- 23
R05 | 2831 7 14 18 30 19 --- 8 | 24 25 21 36 23 --- 20
R07 | 2787 11 18 28 23 35 --- 12 | 41 39 47 38 44 --- 37
R08 | 2314 12 10 13 21 19 89 7 | 31 33 39 41 27 26 30
R10E | 1425 22 15 28 47 36 --- 14 | 35 25 23 42 46 --- 21
XR11E | 9570 45 45 --- --- 281 --- 45 | 9999 9999 --- --- 9999 --- 9999
R13E | 2719 18 23 29 35 37 --- 15 | 24 23 36 33 32 --- 18
R14E | 1009 21 20 44 35 56 --- 19 | 28 28 54 41 33 --- 23
R15E | 2620 23 14 48 39 30 128 16 | 23 24 39 30 25 108 17
R17 | 1955 23 19 30 30 35 --- 14 | 34 61 69 41 30 --- 46
R18 | 2523 8 23 38 25 21 --- 13 | 13 28 43 29 15 --- 14
R19 | 1540 19 7 16 24 36 --- 11 | 14 20 30 34 37 --- 19
R20 | 1593 16 17 25 24 32 --- 12 | 20 31 17 27 49 --- 22
R21 | 928 23 19 39 29 26 --- 15 | 34 33 32 32 37 --- 26
R22 | 1297 16 13 29 23 23 --- 11 | 43 48 51 44 65 --- 45
R23 | 1143 20 13 14 24 17 180 9 | 17 19 28 33 31 59 16
R24 | 2474 13 12 16 17 23 --- 9 | 33 38 39 40 38 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2096 17 15 28 29 30 138 |T 27 30 36 35 35 64 25
WRMS | 2096 17 14 26 29 30 138 |NE 27 32 35 34 35 42 27
MEDI | 1593 16 14 28 25 26 128 |MD 28 28 36 35 36 59 23
Table 3.1580.4 GPS week: 1580 Day: 4 MJD: 55308
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 749 11 14 18 18 19 --- 9 | 29 42 45 35 36 --- 35
R02 | 1032 12 16 18 19 35 --- 11 | 28 39 35 44 36 --- 31
R03 | 4141 28 12 32 27 36 --- 15 | 28 20 33 30 33 --- 17
R04 | 1245 20 12 17 24 22 --- 10 | 25 27 31 28 27 --- 23
R05 | 1717 14 11 18 16 17 --- 8 | 20 20 31 21 23 --- 19
R07 | 4024 14 17 21 51 37 --- 12 | 24 24 35 37 46 --- 24
R08 | 1343 9 10 19 32 24 95 9 | 25 31 40 41 26 45 27
R10E | 1150 41 24 39 21 48 --- 21 | 35 41 54 43 54 --- 37
XR11E |14263 32 22 --- --- 57 --- 25 | 519 9999 --- --- 514 --- 9999
R13E | 3090 39 27 41 43 42 --- 21 | 25 23 48 43 31 --- 19
R14E | 922 17 12 20 26 51 --- 14 | 23 24 24 27 37 --- 19
R15E | 2173 13 29 20 44 57 139 17 | 26 36 33 41 35 96 22
R17 | 814 21 13 28 23 33 --- 13 | 37 51 71 40 25 --- 45
R18 | 1344 17 19 20 15 36 --- 13 | 17 30 34 24 33 --- 19
R19 | 1576 11 10 28 17 36 --- 12 | 22 15 26 29 41 --- 13
R20 | 1222 14 23 21 21 33 --- 13 | 26 29 43 37 35 --- 24
R21 | 722 20 30 33 26 35 --- 17 | 17 35 48 31 35 --- 22
R22 | 1554 27 12 29 30 24 --- 13 | 46 44 40 38 41 --- 36
R23 | 860 21 24 31 19 17 251 14 | 21 20 28 22 20 148 13
R24 | 1472 18 14 13 29 26 --- 10 | 29 32 33 46 41 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 1919 21 19 26 28 35 175 |T 51 30 38 34 58 96 24
WRMS | 1919 21 16 23 28 35 175 |NE 26 30 38 33 33 96 25
MEDI | 1343 17 14 21 24 35 139 |MD 25 30 35 37 35 96 23
Table 3.1580.5 GPS week: 1580 Day: 5 MJD: 55309
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1500 23 20 25 23 24 --- 13 | 21 31 37 34 27 --- 23
R02 | 1553 13 18 17 26 20 --- 10 | 29 34 42 50 32 --- 32
R03 | 4329 18 10 20 23 27 --- 11 | 28 22 35 32 19 --- 19
R04 | 1147 13 11 18 14 33 --- 11 | 18 15 25 20 29 --- 16
R05 | 1655 15 10 18 20 16 --- 8 | 16 14 24 25 20 --- 15
R07 | 4321 10 15 19 21 20 --- 9 | 19 24 32 32 20 --- 20
R08 | 721 18 10 14 28 21 60 9 | 23 21 24 33 21 31 16
R10E | 2179 62 33 27 18 48 --- 25 | 27 35 25 28 40 --- 19
XR11E |12866 69 33 --- --- 69 --- 40 | 338 9999 --- --- 372 --- 9999
R13E | 2956 48 24 33 37 38 --- 21 | 30 23 40 35 40 --- 22
R14E | 1124 20 16 26 26 54 --- 17 | 28 32 40 40 38 --- 27
R15E | 3158 19 19 13 31 35 137 12 | 18 37 23 27 32 101 21
R17 | 892 26 20 10 23 42 --- 14 | 51 54 41 58 29 --- 42
R18 | 1036 13 13 18 20 22 --- 9 | 20 29 30 25 18 --- 21
R19 | 542 14 10 21 20 25 --- 10 | 24 25 41 31 21 --- 23
R20 | 1082 18 15 37 33 30 --- 14 | 16 20 46 46 16 --- 14
R21 | 1324 24 22 38 23 38 --- 17 | 28 43 45 37 46 --- 32
R22 | 1292 23 18 27 18 32 --- 14 | 62 70 59 65 65 --- 59
R23 | 726 24 31 21 27 31 172 15 | 19 29 31 29 33 147 18
R24 | 1124 13 19 19 19 22 --- 10 | 26 30 24 35 29 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2051 25 19 23 24 32 131 |T 42 30 34 35 47 93 24
WRMS | 2051 25 17 20 24 32 131 |NE 26 30 35 36 28 89 24
MEDI | 1292 18 18 20 23 30 137 |MD 24 29 35 33 29 101 21
Table 3.1580.6 GPS week: 1580 Day: 6 MJD: 55310
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1954 21 15 25 18 19 --- 11 | 31 41 37 37 35 --- 33
R02 | 1405 10 14 13 20 22 --- 8 | 35 47 38 43 38 --- 38
R03 | 2720 14 15 16 15 23 --- 9 | 28 31 32 31 35 --- 28
R04 | 2143 11 13 20 19 20 --- 9 | 22 27 34 29 40 --- 26
R05 | 1555 25 9 16 22 27 --- 11 | 25 27 32 28 35 --- 27
R07 | 2861 19 12 19 14 32 --- 11 | 31 24 42 30 38 --- 28
R08 | 910 12 13 18 20 22 55 9 | 29 33 35 33 30 23 29
R10E | 2165 24 23 21 41 54 --- 17 | 31 26 33 24 41 --- 23
R11E | 3966 50 33 36 52 41 --- 23 | 315 9999 108 259 342 --- 9999
R13E | 2062 61 24 30 47 49 --- 23 | 34 21 48 31 44 --- 25
R14E | 1073 37 20 25 25 45 --- 17 | 51 29 28 29 40 --- 27
R15E | 7002 20 18 19 27 43 139 14 | 38 36 22 29 37 101 27
R17 | 2260 27 15 22 39 24 --- 12 | 58 63 47 43 39 --- 51
R18 | 1470 14 11 11 15 15 --- 7 | 23 32 27 24 15 --- 24
R19 | 652 21 7 26 23 26 --- 11 | 31 40 48 32 23 --- 34
R20 | 1010 21 14 22 28 23 --- 11 | 12 25 27 24 23 --- 14
R21 | 1310 25 18 39 14 38 --- 17 | 37 52 61 41 57 --- 45
R22 | 941 20 11 15 15 19 --- 9 | 67 79 80 78 65 --- 72
R23 | 799 31 17 26 29 30 153 14 | 29 32 41 39 55 63 32
R24 | 1037 18 18 20 26 29 --- 12 | 41 36 40 37 46 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 2419 27 17 23 28 32 123 |T 48 36 43 46 53 62 32
WRMS | 2419 25 14 21 28 32 123 |NE 33 39 41 36 38 43 34
MEDI | 1470 21 15 20 22 26 139 |MD 31 32 37 31 38 63 28
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