[IGSREPORT-25992] Wk 2005 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 29 05:33:39 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2005 (Jun 10, 2018 - Jun 16, 2018)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's 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 2.2005.
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:
igl2005[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2005 in the SP3 format.
igl20057.sum Combination Report for GPS Week 2005.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
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. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
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.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 2.4 ns
1 | 2.5 ns
2 | 3.6 ns
3 | 3.4 ns
4 | -1.8 ns
5 | 4.3 ns
6 | 2.5 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 1.2005, 1a.2005).
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 2.2005.0-6)
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 3.2005.0-6).
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 2005 summary. (Jun 10, 2018 - Jun 16, 2018)
Table 1.2005.a GPS week : 2005 MJD: 58279.0-58285.0
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 11 -35 -8 .12 25 20 | 9808 58 3843 10582
| 1 1 1 18 16 26 .11 | 1516 2704
cof n/a| 0 0 -2 12 -13 -18 .14 29 23 | 9796 56 3844 10606
| 1 1 1 16 19 39 .08 | 1521 2695
emx n/a| -1 0 6 13 5 -27 -.03 24 24 | -4585 -177 3854 9985
| 1 1 1 14 17 55 .08 | 10750 1812
esx n/a| 0 0 0 6 25 24 .09 20 17 | 4390 -305 3844 12698
| 1 1 1 13 22 16 .08 | 12616 2527
gfz n/a| 1 0 5 21 29 45 .02 31 22 | -321 -139 3844 10543
| 0 1 2 14 8 40 .17 | 759 2853
grg n/a| 0 0 -6 -30 -22 -103 -.30 38 30 | 1848 189 3858 10318
| 0 2 5 19 26 98 .09 | 1362 2819
iac n/a| 0 0 -3 -27 -12 40 -.19 26 25 | 3897 -259 3847 9917
| 1 1 3 34 43 56 .07 | 1647 1227
mcc n/a| 0 0 -21 -45 -42 725 -.13 215 215 | --- --- --- ---
| 5 7 18 157 121 518 .55 | --- ---
Table 1.2005.b GPS week : 2005 MJD: 58279.0-58285.0
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 | 19 21 20 25 27 21 22 |
R02 | 6 6 6 9 9 8 8 |
R03 | 6 5 7 9 9 6 8 |
R04 | 6 6 7 6 9 8 8 |
R05 | 23 29 30 22 20 24 23 |
R07 | 8 6 8 8 6 8 6 |
R08 | 10 9 12 16 10 10 9 |
R09 | 6 8 8 7 7 7 7 |
R10 | 7 6 8 9 10 7 6 |
R11 | 7 7 7 8 9 7 6 |
R13 | 9 10 11 10 7 8 10 |
R14 | 7 8 7 9 9 9 9 |
R15 | 13 13 14 14 16 12 13 |
R16 | 14 18 17 13 12 14 12 |
R17 | 9 7 8 10 10 10 10 |
R18 | 7 7 8 10 11 8 8 |
R19 | 14 14 14 13 16 17 14 |
R20 | 14 20 15 16 20 16 16 |
R21 | 10 9 10 12 12 10 11 |
R22 | 8 9 11 11 11 9 9 |
R23 | 10 11 12 12 12 11 11 |
R24 | 18 15 16 14 16 17 17 |
R26 | 26 12 18 21 29 23 25 |
Table 1.2005.c GPS week : 2005 MJD: 58279.0-58285.0
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 2005 0 | 539 -1346 20250 2821 -5785 -8105 145.9 >>>>> >>>>> | 2358 0
brd 2005 1 | -205 1390 -526 6328 -5792 -9269 <<<< >>>>> >>>>> | 2528 0
brd 2005 2 | 639 174 178 -374 -7600 -2808 83.3 >>>>> >>>>> | 3610 0
brd 2005 3 | 4175 -3942 80 -1142 -15860 -69860 87.7 >>>>> >>>>> | 3380 0
brd 2005 4 | 133 448 137 1704 98 2135 81.9 >>>>> >>>>> | -1766 0
brd 2005 5 | -87 17 198 1871 344 4173 84.0 1970 1970 | 4262 0
brd 2005 6 | 694 150 49 3456 -23830 5654 86.9 >>>>> >>>>> | 2529 0
-------------+------------------------------------------------------------+----------------
brd 2005 mean| 841 -443 2909 2094 -8346 -11154 66.3 >>>>> >>>>> | 2414 0
brd 2005 sdev| 1512 1739 7650 2485 8724 26529 79.0 >>>>> >>>>> | 1969 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 2.2005.0 GPS week: 2005 Day: 0 MJD: 58279
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -1 1 3 -19 0 -.05 26 20 | 8059 -894 3660 8501
cof n/a| 0 0 -1 8 -21 -4 .03 28 21 | 8046 -884 3661 8521
emx n/a| -2 1 8 0 -6 -60 -.01 23 23 | -1776 -1215 3679 8013
esx n/a| 1 0 -1 10 -12 29 .22 17 14 | -12922 -2174 3662 10945
gfz n/a| 0 1 7 43 31 90 -.07 28 18 | -983 -1808 3630 8394
grg n/a| 0 -1 -12 -54 -5 -152 -.30 44 32 | 1818 -1099 3649 8550
iac n/a| 2 -1 -1 -3 8 35 -.19 24 21 | 3398 -1361 3674 7796
mcc n/a| -1 -10 -1 51 -51 671 -1.14 296 296 | --- --- --- ---
Table 2.2005.1 GPS week: 2005 Day: 1 MJD: 58280
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 18 -47 -48 .13 23 17 | 8293 -998 4045 11112
cof n/a| 0 -2 -2 15 -33 -100 .24 30 21 | 8290 -1003 4041 11125
emx n/a| 0 0 4 0 -5 -93 -.05 22 22 | -11349 -1344 4064 10476
esx n/a| 0 1 1 -12 34 3 .13 21 16 | 5890 -1504 4039 12573
gfz n/a| 1 -1 5 28 17 -2 -.16 30 19 | -534 -1121 4139 11137
grg n/a| 0 0 -10 -42 -43 -11 -.17 31 27 | 1705 -883 4049 11692
iac n/a| 0 -1 -2 18 19 119 -.15 24 24 | 3503 -752 4050 10437
mcc n/a| -7 0 -1 193 -37 510 .04 166 166 | --- --- --- ---
Table 2.2005.2 GPS week: 2005 Day: 2 MJD: 58281
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 0 0 3 -63 -40 .03 23 18 | 9613 1517 3574 11418
cof n/a| 0 0 -2 -1 -42 -5 .09 26 19 | 9604 1513 3573 11447
emx n/a| -1 -1 4 12 20 -56 -.19 24 23 | -3514 1550 3593 10676
esx n/a| 0 1 0 19 18 42 .14 22 19 | 1122 326 3593 13494
gfz n/a| 1 0 9 15 39 75 .16 42 26 | -748 1666 3597 12012
grg n/a| 1 2 -8 -41 -40 -93 -.24 39 30 | 2546 1603 3562 10800
iac n/a| 1 0 -4 -5 25 76 -.34 28 27 | 4217 154 3596 10631
mcc n/a| -2 -1 -25 -103 32 304 -.01 191 191 | --- --- --- ---
Table 2.2005.3 GPS week: 2005 Day: 3 MJD: 58282
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 2 -1 36 -23 21 .10 25 22 | 12125 3498 3621 10965
cof n/a| 0 0 -2 30 6 24 .07 31 22 | 12105 3482 3627 11010
emx n/a| 1 -2 7 24 20 34 .07 22 22 | 12111 1394 3642 10515
esx n/a| -1 0 -1 -10 41 0 .08 19 18 | 11368 2601 3624 12972
gfz n/a| 1 0 7 -1 21 33 .11 28 23 | 287 3714 3630 10772
grg n/a| 0 3 1 -38 -51 -152 -.44 38 34 | 1369 4376 3629 10880
iac n/a| 0 0 -11 -50 -92 -24 -.18 30 29 | 5366 1630 3622 10396
mcc n/a| 5 -1 -50 -286 -49 1683 .72 167 167 | --- --- --- ---
Table 2.2005.4 GPS week: 2005 Day: 4 MJD: 58283
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -1 -1 8 -17 2 .25 24 18 | 9228 -4622 4199 13152
cof n/a| -3 0 -5 19 -7 -5 .24 28 22 | 9196 -4588 4196 13194
emx n/a| 0 0 7 13 4 -42 -.05 22 22 | -21229 -3083 4191 12472
esx n/a| 0 0 -1 6 57 40 -.01 21 19 | 13998 -3630 4192 14893
gfz n/a| 1 0 3 28 29 95 .26 27 23 | -1197 -4874 4145 12906
grg n/a| 0 1 -5 -4 16 -247 -.36 41 30 | -797 -4263 4323 12980
iac n/a| 2 0 -4 -70 -47 91 -.15 30 31 | 638 -1470 4179 12530
mcc n/a| -7 2 -20 8 -290 1012 -.00 293 293 | --- --- --- ---
Table 2.2005.5 GPS week: 2005 Day: 5 MJD: 58284
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -2 29 -39 -3 .21 25 23 | 9892 2437 4076 9590
cof n/a| 0 1 -5 28 1 -19 .18 30 24 | 9857 2457 4081 9599
emx n/a| -2 2 7 7 -20 63 -.01 27 27 | -9448 1658 4088 9042
esx n/a| -1 0 0 6 13 30 .09 17 15 | -10147 3294 4082 11822
gfz n/a| 2 2 1 27 23 21 -.18 27 21 | 0 1964 4048 9432
grg n/a| 2 -3 -6 -2 -35 -122 -.35 41 33 | 3234 2345 4073 8939
iac n/a| -1 -2 0 -63 15 4 -.17 27 26 | 4754 1053 4100 8980
mcc n/a| 6 -3 -13 -171 0 104 -.32 255 255 | --- --- --- ---
Table 2.2005.6 GPS week: 2005 Day: 6 MJD: 58285
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 -2 -19 -35 10 .20 26 26 | 11449 -528 3731 9340
cof n/a| -1 0 0 -14 0 -17 .14 33 28 | 11476 -582 3731 9348
emx n/a| -1 0 4 40 28 -35 .04 30 30 | 3110 -203 3721 8702
esx n/a| 1 -1 2 24 24 21 -.02 21 18 | 21422 -1049 3719 12187
gfz n/a| 0 2 3 10 41 5 .04 30 22 | 927 -515 3723 9148
grg n/a| 0 1 -1 -32 5 52 -.27 33 27 | 3066 -755 3724 8385
iac n/a| 0 0 -2 -15 -18 -16 -.12 21 20 | 5403 -1073 3708 8652
mcc n/a| 1 12 -41 -8 98 790 -.21 136 136 | --- --- --- ---
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 3.2005.0 GPS week: 2005 Day: 0 MJD: 58279
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M |>>>>> 49 44 42 27 66 51 28 --- 19 | 128 139 135 143 151 95 137 --- 134
R02M |>>>>> 13 17 12 16 9 12 13 285 6 | 26 34 29 33 25 22 19 127 23
R03M | ---- 8 7 17 13 11 19 10 201 6 | 82 84 79 82 84 79 77 130 80
R04 |>>>>> 11 9 14 11 12 23 15 --- 6 | 24 29 22 32 30 29 22 --- 24
R05 |>>>>> 31 33 48 36 36 125 47 --- 23 | 26 32 44 48 46 60 25 --- 29
R07M |>>>>> 9 14 20 10 16 31 18 528 7 | 111 115 105 113 114 107 107 338 108
R08M |>>>>> 20 16 21 22 24 13 22 --- 9 | 25 33 28 45 49 37 20 --- 31
R09E |>>>>> 8 13 9 6 17 28 12 --- 5 | 24 27 23 26 27 36 26 --- 23
R10E |>>>>> 13 16 14 12 19 19 17 --- 7 | 70 73 69 79 70 79 73 --- 72
R11E |>>>>> 15 20 18 10 21 22 14 106 7 | 69 70 64 67 62 63 63 71 64
R13E |>>>>> 12 15 20 12 17 40 21 --- 8 | 88 87 88 88 90 95 88 --- 88
R14E |>>>>> 18 22 17 12 17 13 18 --- 7 | 140 142 135 141 137 134 137 --- 138
R15E |>>>>> 41 41 22 17 36 43 22 --- 13 | 129 132 121 119 113 124 111 --- 118
R16 |>>>>> 30 27 19 21 35 64 30 --- 13 | 87 92 84 92 96 82 91 --- 86
R17E | ---- 21 20 14 9 26 33 19 --- 8 | 31 33 24 26 35 33 23 --- 24
R18E |>>>>> 12 14 16 14 19 19 18 --- 7 | 56 57 61 59 63 59 61 --- 58
R19E |>>>>> 48 60 25 12 33 44 26 --- 13 | 55 64 48 48 60 58 41 --- 45
R20E |>>>>> 33 42 34 23 27 45 29 --- 13 | 124 123 135 117 124 124 129 --- 122
R21E |>>>>> 28 34 17 10 25 48 16 162 10 | 69 72 70 68 73 67 69 150 67
R22E |>>>>> 27 28 16 7 21 19 19 --- 8 | 102 102 104 104 106 108 101 --- 103
R23E | ---- 24 22 23 18 16 25 22 --- 9 | 97 96 98 100 99 97 97 --- 96
R24E | ---- 33 31 32 24 50 67 45 --- 17 | 52 65 39 59 63 57 54 --- 49
XR26E | ---- 27 91 --- --- --- --- 25 --- 26 | 43 93 --- --- --- --- 51 --- 45
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 26 28 23 17 28 44 24 296 |T 72 78 72 76 78 74 70 163 70
WRMS |>>>>> 20 21 23 14 18 32 21 296 |NE 45 51 50 57 57 57 46 --- 46
MEDI |>>>>> 21 22 18 12 21 28 19 201 |MD 69 73 69 68 70 67 69 130 67
Table 3.2005.1 GPS week: 2005 Day: 1 MJD: 58280
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | ---- 37 72 43 51 60 36 46 --- 20 | 108 139 116 148 140 90 124 --- 121
R02M |>>>>> 12 16 11 13 15 16 14 264 6 | 15 19 14 26 22 14 17 189 15
R03M |>>>>> 10 20 11 12 12 12 10 124 5 | 63 68 59 64 69 53 53 101 59
R04 | ---- 6 19 8 14 18 19 11 --- 5 | 17 27 19 20 23 26 13 --- 16
XR05 |>>>>> 34 54 31 34 --- 118 63 --- 29 | 36 56 48 51 --- 87 27 --- 37
R07M |>>>>> 8 16 7 11 20 14 16 --- 5 | 82 80 83 88 90 75 81 --- 83
R08M |>>>>> 19 17 15 25 18 16 19 --- 8 | 14 19 15 29 20 23 14 --- 15
R09E |>>>>> 10 16 20 15 15 30 17 --- 8 | 27 28 28 31 33 36 26 --- 25
R10E |>>>>> 6 12 15 14 18 17 10 --- 6 | 56 61 51 59 53 55 52 --- 53
R11E |>>>>> 12 14 17 13 19 21 10 123 7 | 50 50 50 57 48 60 47 68 50
R13E |>>>>> 13 18 24 16 22 38 15 --- 9 | 66 66 72 69 71 69 69 --- 68
R14E |>>>>> 18 24 17 10 28 26 13 --- 8 | 122 127 122 121 123 118 123 --- 121
R15E |>>>>> 35 32 29 15 44 35 14 --- 13 | 94 93 93 87 81 89 86 --- 88
R16 |>>>>> 26 46 27 22 32 84 32 --- 17 | 79 93 72 81 84 62 78 --- 72
R17E | ---- 20 23 16 10 25 14 11 --- 7 | 28 31 25 28 28 29 26 --- 24
R18E | ---- 13 14 12 15 18 13 22 --- 7 | 50 49 48 51 53 49 50 --- 49
R19E |>>>>> 47 46 23 19 42 23 19 --- 13 | 55 56 49 51 56 52 46 --- 48
R20E |>>>>> 37 39 31 45 60 26 55 --- 19 | 123 128 120 149 140 132 111 --- 124
R21E |>>>>> 28 23 17 13 28 17 17 100 9 | 59 57 56 55 55 60 58 123 55
R22E |>>>>> 28 30 17 10 21 19 19 --- 8 | 102 105 104 107 105 104 99 --- 103
R23E |>>>>> 18 26 30 23 16 31 21 --- 10 | 87 86 89 86 86 99 93 --- 88
R24E | ---- 26 33 29 25 33 50 40 --- 15 | 50 49 55 46 45 57 48 --- 43
XR26E | ---- 12 62 --- --- --- --- 11 --- 11 | 36 49 --- --- --- --- 42 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 23 30 22 21 30 31 24 166 |T 61 66 63 68 67 65 60 120 60
WRMS |>>>>> 17 21 22 16 19 27 24 166 |NE 44 58 46 50 53 58 39 --- 41
MEDI |>>>>> 18 23 17 15 21 21 17 123 |MD 56 57 55 57 56 60 52 101 53
Table 3.2005.2 GPS week: 2005 Day: 2 MJD: 58281
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M |>>>>> 38 38 47 42 44 35 61 --- 20 | 117 130 113 130 117 63 121 --- 115
R02M |>>>>> 9 14 13 11 23 15 11 301 6 | 18 19 21 27 23 25 17 260 19
R03M |>>>>> 16 15 12 19 15 18 7 201 6 | 72 69 71 65 67 72 70 140 69
R04 |>>>>> 10 8 9 21 14 15 16 --- 6 | 14 20 11 35 28 23 19 --- 18
R05 | ---- 28 53 40 33 135 123 41 --- 30 | 37 74 45 41 133 67 20 --- 29
R07M |>>>>> 9 11 8 10 38 12 24 --- 7 | 108 107 105 112 117 99 99 --- 106
R08M |>>>>> 18 7 19 34 39 14 27 --- 11 | 13 20 15 47 46 20 21 --- 21
R09E |>>>>> 14 8 17 11 19 27 17 --- 7 | 22 26 31 29 36 35 25 --- 25
R10E |>>>>> 7 9 19 15 18 27 11 --- 7 | 46 47 43 49 40 47 52 --- 45
R11E |>>>>> 9 11 19 12 18 23 17 96 7 | 49 54 47 50 45 55 35 59 45
R13E |>>>>> 20 16 19 19 27 37 33 --- 11 | 96 100 104 106 105 104 90 --- 99
R14E |>>>>> 15 14 12 11 19 21 16 --- 6 | 124 120 116 121 115 122 120 --- 119
R15E |>>>>> 35 37 22 19 47 43 22 --- 13 | 112 110 95 98 91 104 107 --- 100
R16 |>>>>> 32 30 32 30 42 53 41 --- 16 | 105 106 92 90 87 100 100 --- 92
R17E | ---- 22 24 18 9 25 14 15 --- 7 | 35 36 32 35 35 30 32 --- 31
R18E | ---- 19 11 17 13 19 16 21 --- 8 | 78 78 80 76 77 77 76 --- 76
R19E | ---- 43 43 23 26 38 25 21 --- 13 | 49 46 40 38 39 40 34 --- 35
R20E |>>>>> 28 32 25 21 55 53 29 --- 15 | 92 93 108 105 111 98 108 --- 100
R21E |>>>>> 28 32 18 10 36 15 19 81 9 | 75 76 72 77 75 75 77 80 74
R22E |>>>>> 27 27 19 14 26 25 37 --- 11 | 112 113 116 116 116 110 101 --- 111
R23E |>>>>> 17 28 30 21 25 18 36 --- 11 | 126 125 121 129 129 124 115 --- 122
R24E | ---- 12 28 40 41 26 49 40 --- 16 | 55 64 70 53 62 63 71 --- 57
XR26E | ---- 15 90 --- --- --- --- 21 --- 18 | 41 100 --- --- --- --- 60 --- 47
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 23 26 24 22 42 39 28 191 |T 69 75 70 74 77 70 68 134 67
WRMS |>>>>> 18 19 23 19 26 30 27 191 |NE 52 66 49 55 82 63 46 --- 46
MEDI |>>>>> 18 24 19 19 26 23 21 96 |MD 72 76 71 65 75 67 71 80 69
Table 3.2005.3 GPS week: 2005 Day: 3 MJD: 58282
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
XR01M |>>>>> 32 45 64 31 25 --- 79 --- 24 | 58 87 76 58 42 --- 41 --- 53
R02M |>>>>> 16 65 11 9 32 33 20 --- 8 | 20 65 16 20 32 25 19 --- 15
R03M |>>>>> 7 12 10 15 30 38 22 240 9 | 38 43 40 45 45 51 42 137 39
R04 |>>>>> 10 8 8 14 16 15 17 --- 6 | 16 21 17 30 25 33 15 --- 21
R05 |>>>>> 36 32 42 32 33 108 35 --- 21 | 26 38 49 48 35 26 26 --- 33
R07M |>>>>> 15 15 15 18 18 23 17 --- 8 | 39 39 42 38 28 37 48 --- 36
R08M |>>>>> 33 25 31 36 36 41 42 --- 16 | 11 17 18 58 53 59 12 --- 31
R09E |>>>>> 16 16 13 9 15 15 25 --- 6 | 25 25 19 26 31 31 38 --- 23
R10E |>>>>> 18 19 18 20 12 23 20 --- 8 | 43 59 55 58 49 56 56 --- 51
R11E |>>>>> 13 20 14 13 22 23 21 144 7 | 47 49 46 47 46 49 48 69 44
R13E |>>>>> 17 22 18 15 18 22 36 --- 9 | 75 73 76 78 77 73 75 --- 73
R14E |>>>>> 21 24 13 8 23 24 33 --- 9 | 109 114 104 105 103 102 100 --- 102
R15E |>>>>> 42 42 17 16 42 39 32 --- 13 | 112 115 104 106 100 106 98 --- 103
R16 |>>>>> 24 41 27 19 24 45 39 --- 12 | 99 111 101 99 95 90 83 --- 92
R17E |>>>>> 27 28 20 8 24 24 26 --- 9 | 32 33 35 30 31 36 34 --- 28
R18E | ---- 24 19 24 14 22 26 29 --- 10 | 71 78 71 75 74 83 60 --- 69
R19E | ---- 44 52 21 22 29 24 22 --- 12 | 72 79 65 69 72 71 70 --- 67
R20E | ---- 26 31 31 20 53 55 28 --- 15 | 77 75 81 72 76 92 81 --- 74
R21E |>>>>> 27 31 19 18 31 24 37 69 11 | 57 60 58 57 68 65 58 81 56
R22E |>>>>> 31 34 17 9 32 25 33 --- 11 | 83 86 88 85 94 89 84 --- 84
R23E |>>>>> 22 22 26 28 18 25 35 --- 11 | 84 86 85 93 85 93 92 --- 86
R24E |>>>>> 24 22 31 26 32 38 31 --- 13 | 59 69 90 66 71 65 63 --- 65
XR26E | ---- 19 105 --- --- --- --- 23 --- 21 | 41 111 --- --- --- --- 52 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 25 31 22 19 28 38 30 166 |T 56 66 60 61 60 63 56 95 55
WRMS |>>>>> 22 22 22 18 23 34 29 166 |NE 47 56 55 59 51 49 41 --- 48
MEDI |>>>>> 24 25 18 16 24 25 29 144 |MD 57 69 58 58 53 65 56 81 53
Table 3.2005.4 GPS week: 2005 Day: 4 MJD: 58283
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
XR01M |>>>>> 37 27 69 43 34 --- 77 --- 27 | 112 105 112 127 113 --- 122 --- 111
R02M |>>>>> 16 17 17 17 24 24 24 --- 9 | 16 21 33 32 31 20 20 --- 22
R03M |>>>>> 17 23 16 20 22 23 16 405 8 | 88 94 87 84 84 70 82 379 82
R04 |>>>>> 16 43 17 26 21 21 21 --- 9 | 20 53 15 32 30 28 17 --- 16
R05 |>>>>> 37 47 36 22 32 110 26 --- 20 | 34 53 47 50 42 95 32 --- 39
R07M | ---- 6 11 14 14 12 18 14 391 5 | 113 111 112 110 116 108 120 223 112
R08M |>>>>> 12 12 15 23 32 20 26 --- 9 | 21 22 16 30 35 20 14 --- 15
R09E |>>>>> 13 15 13 9 13 22 19 --- 6 | 23 25 27 27 33 34 34 --- 26
R10E |>>>>> 19 17 20 18 20 28 32 --- 10 | 69 68 57 67 57 62 57 --- 59
R11E |>>>>> 18 20 15 16 24 29 19 136 8 | 88 89 78 79 69 77 73 101 76
R13E |>>>>> 12 17 22 13 14 24 11 --- 7 | 101 105 116 107 109 105 112 --- 107
R14E |>>>>> 14 17 19 18 20 22 27 --- 8 | 160 162 155 160 149 151 159 --- 155
R15E |>>>>> 37 44 26 16 32 54 46 --- 15 | 130 136 124 123 117 117 131 --- 122
R16 |>>>>> 16 22 30 19 31 29 35 --- 12 | 55 55 56 54 68 44 77 --- 55
R17E |>>>>> 28 35 17 17 23 23 28 --- 10 | 52 57 48 55 53 52 35 --- 47
R18E |>>>>> 17 22 22 17 22 41 27 --- 10 | 79 88 83 90 93 96 76 --- 83
R19E | ---- 47 59 24 24 39 31 38 --- 15 | 75 84 81 95 100 87 70 --- 81
R20E | ---- 36 19 32 33 53 45 64 --- 19 | 72 69 64 77 91 73 90 --- 67
R21E | ---- 28 20 17 8 30 45 30 86 11 | 69 69 69 68 68 81 63 85 65
R22E |>>>>> 26 25 18 7 33 47 21 --- 11 | 85 86 88 89 98 90 90 --- 88
R23E |>>>>> 25 27 29 29 15 30 23 --- 11 | 89 91 88 93 91 98 89 --- 89
R24E |>>>>> 22 21 29 36 30 60 39 --- 15 | 58 67 60 63 61 66 71 --- 56
XR26E | ---- 26 55 --- --- --- --- 32 --- 29 | 57 108 --- --- --- --- 66 --- 57
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 24 28 22 21 27 41 30 293 |T 72 79 73 77 77 74 73 197 70
WRMS |>>>>> 18 22 22 19 23 30 31 293 |NE 36 53 39 45 46 55 42 --- 36
MEDI |>>>>> 19 22 19 18 24 29 27 136 |MD 72 84 69 77 69 77 73 101 67
Table 3.2005.5 GPS week: 2005 Day: 5 MJD: 58284
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | 882 38 38 67 34 26 56 52 --- 20 | 83 98 69 110 102 149 92 --- 89
R02M | 955 19 16 17 22 15 13 15 455 8 | 15 18 15 37 27 35 24 258 22
R03M | 899 8 8 14 7 23 21 9 268 6 | 82 81 81 88 93 87 87 272 86
R04 | 1153 9 30 16 8 26 21 21 --- 7 | 23 28 17 30 38 34 22 --- 24
R05 | 1174 39 35 53 28 40 121 43 --- 23 | 37 42 41 38 61 51 38 --- 32
R07M | 2202 13 32 18 15 11 27 28 198 8 | 99 103 99 103 105 97 104 237 100
R08M | 1850 13 19 18 11 35 26 28 --- 9 | 19 26 18 22 35 29 25 --- 18
R09E | 3840 13 13 13 10 15 34 15 --- 7 | 18 16 17 21 25 27 20 --- 17
R10E | 1748 15 21 17 15 12 19 14 --- 6 | 50 49 44 54 48 47 56 --- 50
R11E | 2606 13 12 16 13 23 18 12 62 7 | 144 147 143 144 142 131 143 146 141
R13E | 2697 9 17 17 13 20 35 19 --- 8 | 107 107 110 107 116 102 104 --- 107
R14E | 2902 21 21 23 11 25 15 23 --- 9 | 89 91 87 93 85 93 88 --- 88
R15E | 2622 32 45 26 12 29 39 29 --- 12 | 140 143 135 126 129 124 124 --- 129
R16 | 817 19 37 24 26 39 49 31 --- 13 | 70 80 55 74 78 53 73 --- 65
R17E | 2359 34 27 17 10 25 18 14 --- 9 | 40 41 38 38 36 39 27 --- 33
R18E | 1232 15 13 18 11 22 22 16 --- 7 | 80 78 81 77 78 80 88 --- 79
R19E | 1908 48 55 31 22 38 57 34 --- 16 | 90 93 90 77 86 104 76 --- 81
R20E | 1997 31 55 25 21 43 51 51 --- 16 | 106 122 116 107 118 115 88 --- 104
R21E | 818 27 31 15 9 29 31 23 66 9 | 83 82 76 79 87 80 76 96 79
R22E | 1104 26 23 16 7 31 26 12 --- 9 | 93 94 98 100 106 95 99 --- 98
R23E | 1894 29 25 29 27 15 18 14 --- 11 | 89 90 87 92 93 87 86 --- 88
XR24E | 2518 31 44 31 31 --- 27 40 --- 16 | 33 52 34 48 --- 39 42 --- 32
XR26E | ---- 20 85 --- --- --- --- 24 --- 22 | 41 64 --- --- --- --- 50 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1970 25 30 27 17 27 41 27 255 |T 70 75 70 75 80 77 70 201 69
WRMS | 1970 23 24 27 15 21 33 26 255 |NE 43 50 37 47 59 46 44 --- 40
MEDI | 1850 20 27 18 13 25 26 23 198 |MD 82 81 76 77 86 80 76 237 79
Table 3.2005.6 GPS week: 2005 Day: 6 MJD: 58285
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01M | ---- 24 45 96 41 34 24 34 --- 21 | 118 145 110 151 139 127 128 --- 126
R02M |>>>>> 19 15 15 22 10 17 14 217 7 | 21 27 26 39 34 36 22 220 26
R03M |>>>>> 12 16 9 15 29 17 15 105 7 | 88 89 91 94 98 95 87 106 90
R04 |>>>>> 11 18 15 11 27 31 12 --- 8 | 18 21 23 21 27 32 25 --- 18
R05 |>>>>> 44 74 52 24 56 91 42 --- 23 | 49 70 57 49 75 58 42 --- 43
R07M |>>>>> 14 14 13 16 16 12 8 133 6 | 124 124 125 131 130 123 121 196 125
R08M |>>>>> 12 15 12 25 15 25 22 --- 8 | 23 21 18 23 28 19 30 --- 17
R09E |>>>>> 17 12 14 13 18 24 12 --- 7 | 41 43 41 42 47 49 41 --- 41
R10E |>>>>> 10 15 14 12 14 12 17 --- 6 | 59 64 58 63 62 55 63 --- 59
R11E |>>>>> 11 17 16 12 17 16 7 107 6 | 93 93 92 91 95 99 93 96 93
R13E |>>>>> 16 21 21 19 23 36 17 --- 9 | 100 98 105 98 101 96 97 --- 98
R14E |>>>>> 16 11 18 16 28 23 13 --- 8 | 109 107 108 108 110 108 110 --- 108
R15E |>>>>> 36 44 24 16 43 40 17 --- 13 | 152 154 151 147 141 143 148 --- 146
R16 |>>>>> 18 33 30 18 34 33 28 --- 12 | 46 53 58 50 56 47 66 --- 49
R17E |>>>>> 35 41 18 16 24 20 17 --- 10 | 50 54 45 44 42 41 38 --- 40
R18E |>>>>> 9 11 21 20 15 19 14 --- 7 | 91 94 92 88 95 86 97 --- 91
R19E |>>>>> 46 43 21 21 35 38 21 --- 13 | 62 62 64 63 66 63 61 --- 57
R20E |>>>>> 30 56 30 37 39 48 32 --- 16 | 89 96 87 80 84 88 88 --- 81
R21E | ---- 32 30 18 13 30 27 22 67 10 | 91 89 88 89 89 90 93 90 89
R22E | ---- 26 28 17 10 26 30 11 --- 9 | 86 86 93 89 98 89 89 --- 89
R23E | ---- 34 39 27 24 17 10 19 --- 10 | 91 92 92 96 95 95 93 --- 92
R24E |>>>>> 37 27 35 32 56 43 30 --- 17 | 59 59 49 62 71 51 58 --- 51
XR26E | ---- 28 76 --- --- --- --- 22 --- 25 | 41 76 --- --- --- --- 51 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 26 33 30 21 30 33 21 136 |T 73 79 76 78 81 76 75 141 72
WRMS |>>>>> 26 28 30 18 22 27 20 136 |NE 37 48 46 40 52 45 44 --- 36
MEDI |>>>>> 19 27 18 16 26 24 17 107 |MD 86 86 87 80 84 86 87 106 81
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