[IGSREPORT-25964] Wk 2003 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 15 00:39:09 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2003 (May 27, 2018 - Jun 02, 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 2.2003.
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:
igl2003[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2003 in the SP3 format.
igl20037.sum Combination Report for GPS Week 2003.
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 | 7.3 ns
1 | 6.5 ns
2 | 5.0 ns
3 | 5.0 ns
4 | 3.2 ns
5 | 4.3 ns
6 | 5.9 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 | GRG | R05
5 | GRG | R05
6 | GRG | R05
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 1.2003, 1a.2003).
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 2.2003.0-6)
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 3.2003.0-6).
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 2003 summary. (May 27, 2018 - Jun 02, 2018)
Table 1.2003.a GPS week : 2003 MJD: 58265.0-58271.0
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 3 -31 19 .06 21 20 | 5525 -113 3666 10156
| 0 0 1 11 13 36 .03 | 1138 2365
cof n/a| 0 0 0 1 -14 10 .08 24 22 | 5514 -96 3669 10160
| 1 0 1 25 17 34 .04 | 1140 2372
emx n/a| -1 0 2 18 30 -36 -.07 23 23 | -7818 202 3672 9579
| 0 1 2 10 22 27 .05 | 6283 1483
esx n/a| 0 0 -1 -16 7 15 .19 17 15 | 11318 -323 3669 12251
| 1 0 1 16 36 29 .04 | 11242 2744
gfz n/a| 2 1 2 19 32 1 .03 23 19 | 0 -213 3682 10090
| 1 1 1 14 31 29 .08 | 0 2182
grg n/a| 0 0 1 -69 -30 -69 -.32 37 27 | 5286 -46 3679 9512
| 1 1 3 23 23 55 .03 | 1370 2221
iac n/a| 0 -1 0 15 -21 26 -.06 19 18 | 6937 100 3669 9532
| 1 1 1 23 54 73 .04 | 1034 1213
mcc n/a| 0 -3 -33 47 -62 -56 -.53 141 141 | --- --- --- ---
| 7 10 8 71 119 546 .31 | --- ---
Table 1.2003.b GPS week : 2003 MJD: 58265.0-58271.0
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 | 13 18 18 18 15 12 14 |
R02 | 6 7 7 7 6 8 5 |
R03 | 6 6 5 6 5 7 6 |
R04 | 5 5 6 7 7 8 5 |
R05 | 18 20 21 14 22 17 20 |
R07 | 6 7 6 5 8 6 6 |
R08 | 7 8 7 6 7 5 6 |
R09 | 6 7 7 7 5 7 7 |
R10 | 8 8 8 8 6 8 8 |
R11 | 7 9 9 8 8 8 8 |
R13 | 7 9 7 9 10 8 9 |
R14 | 8 9 9 10 10 9 8 |
R15 | 16 14 14 13 15 15 14 |
R16 | 18 14 15 12 14 13 13 |
R17 | 7 7 7 6 7 7 8 |
R18 | 6 6 7 7 6 10 7 |
R19 | 9 10 9 9 11 11 11 |
R20 | 10 9 13 9 12 12 12 |
R21 | 8 7 7 8 7 7 7 |
R22 | 7 7 7 7 8 7 8 |
R23 | 9 8 8 10 9 9 9 |
R24 | 13 12 10 13 13 12 16 |
R26 | 15 24 17 23 14 20 12 |
Table 1.2003.c GPS week : 2003 MJD: 58265.0-58271.0
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 2003 0 | -7 76 174 -577 977 4297 83.3 1291 1291 | 7251 0
brd 2003 1 | -88 8 188 1383 -180 2649 83.8 1573 1573 | 6548 0
brd 2003 2 | -53 -41 233 235 -291 3843 85.5 1418 1418 | 4988 0
brd 2003 3 | 15 -14 268 -876 409 5531 85.0 1654 1654 | 5050 0
brd 2003 4 | 112 32 168 559 1180 4350 84.8 1765 1765 | 3227 0
brd 2003 5 | 57 40 129 844 1198 5490 84.8 2071 2071 | 4329 0
brd 2003 6 | -5 49 88 -169 -1174 3060 85.3 1924 1924 | 5855 0
-------------+------------------------------------------------------------+----------------
brd 2003 mean| 4 21 178 199 302 4174 84.7 1670 1670 | 5321 0
brd 2003 sdev| 66 40 60 800 894 1102 .8 274 274 | 1358 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 2.2003.0 GPS week: 2003 Day: 0 MJD: 58265
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 1 -10 -34 .05 21 21 | 5820 1667 4283 10394
cof n/a| 0 0 -2 -9 15 -42 .03 27 23 | 5827 1641 4292 10402
emx n/a| 0 2 4 18 46 -31 -.07 20 20 | -8299 1273 4284 9831
esx n/a| 1 -1 0 -16 -7 3 .14 16 13 | 19527 956 4277 12512
gfz n/a| 2 0 3 10 -2 -2 .05 24 23 | 0 1448 4322 10040
grg n/a| -1 0 -5 -66 -10 -107 -.27 36 25 | 6491 1584 4265 10104
iac n/a| -1 0 -2 -1 -23 117 -.04 20 18 | 8059 889 4288 9764
mcc n/a| -12 4 -38 7 -143 210 -1.02 136 136 | --- --- --- ---
Table 2.2003.1 GPS week: 2003 Day: 1 MJD: 58266
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 11 -42 -17 .12 22 19 | 6579 2200 3230 10275
cof n/a| 2 0 0 1 -15 0 .08 26 22 | 6560 2229 3230 10279
emx n/a| -1 -1 1 12 45 -13 -.15 23 23 | -5081 1777 3243 9435
esx n/a| -1 0 0 -13 10 -34 .16 16 14 | 16404 3449 3227 11972
gfz n/a| 0 0 2 34 19 -36 -.01 20 15 | 0 2398 3250 10070
grg n/a| 1 2 2 -101 -32 -159 -.31 41 40 | 5189 2450 3219 9736
iac n/a| 0 -3 -1 7 -32 146 .01 19 19 | 8461 1211 3238 9801
mcc n/a| 9 -9 -28 98 -132 -57 -.68 150 150 | --- --- --- ---
Table 2.2003.2 GPS week: 2003 Day: 2 MJD: 58267
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 1 -9 -19 9 .05 18 19 | 3591 796 3494 10459
cof n/a| 0 -1 -1 -39 -19 38 .06 19 20 | 3569 834 3499 10463
emx n/a| 0 1 5 -1 30 -50 -.11 30 30 | -4114 1104 3502 9457
esx n/a| -1 0 0 -17 35 40 .16 17 17 | 7435 418 3500 12648
gfz n/a| 0 0 2 6 38 54 .12 22 16 | 0 265 3508 9982
grg n/a| 2 0 1 -72 -33 -73 -.34 36 29 | 4518 563 3489 9497
iac n/a| 0 0 -3 45 -40 -15 -.05 19 19 | 6553 -104 3498 9750
mcc n/a| 6 -16 -15 48 181 -1256 -.53 178 178 | --- --- --- ---
Table 2.2003.3 GPS week: 2003 Day: 3 MJD: 58268
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 1 1 -3 -28 51 .08 20 18 | 6169 1895 3815 9726
cof n/a| 0 0 2 46 -9 -5 .13 23 22 | 6144 1945 3821 9731
emx n/a| -1 -2 3 15 61 -59 -.07 25 25 | -13525 1084 3826 9484
esx n/a| 0 0 -3 12 30 44 .17 15 15 | 20419 1089 3815 12136
gfz n/a| 2 2 0 16 83 -6 .10 23 21 | 0 1612 3815 9450
grg n/a| 0 1 0 -38 -36 -55 -.36 38 26 | 4092 1808 3829 9014
iac n/a| 0 -1 1 0 -78 -22 -.08 19 18 | 6428 1026 3815 9071
mcc n/a| 0 12 -39 -74 -82 54 -.64 141 141 | --- --- --- ---
Table 2.2003.4 GPS week: 2003 Day: 4 MJD: 58269
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 1 -1 22 -47 20 .06 22 21 | 6434 -1027 3235 9829
cof n/a| 0 0 -2 -3 -12 8 .06 26 25 | 6423 -1009 3236 9830
emx n/a| -2 -1 0 28 27 10 -.05 19 19 | -15493 -769 3252 9325
esx n/a| 0 0 -1 -35 -19 24 .24 19 16 | -3799 -221 3252 11440
gfz n/a| 3 3 1 44 19 -12 -.08 25 20 | 0 -1726 3261 9569
grg n/a| 1 0 1 -40 -8 -41 -.30 35 23 | 3673 -1037 3240 8971
iac n/a| 0 0 1 -3 20 -8 -.08 20 19 | 5801 -617 3244 9257
mcc n/a| -7 -13 -40 97 -7 87 -.51 102 102 | --- --- --- ---
Table 2.2003.5 GPS week: 2003 Day: 5 MJD: 58270
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 10 -37 64 .06 22 21 | 5793 -2539 3888 10357
cof n/a| 0 -1 -2 12 -43 67 .12 23 22 | 5796 -2549 3883 10357
emx n/a| -2 1 0 24 -1 -68 -.06 21 21 | -11054 -795 3879 9958
esx n/a| -1 -1 -1 -38 -52 -8 .25 17 15 | -3281 -3831 3894 12390
gfz n/a| 4 2 1 7 5 -10 .08 24 18 | 0 -2348 3864 10739
grg n/a| 1 0 4 -87 -75 20 -.34 42 25 | 5486 -2489 3886 9604
iac n/a| 2 -1 0 53 78 -23 -.11 17 17 | 5940 522 3882 9688
mcc n/a| 0 -2 -37 16 -94 383 -.02 119 119 | --- --- --- ---
Table 2.2003.6 GPS week: 2003 Day: 6 MJD: 58271
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 -6 -38 39 .03 22 20 | 4292 -3784 3719 10052
cof n/a| -1 0 0 0 -18 8 .11 24 22 | 4280 -3766 3722 10061
emx n/a| -2 0 4 28 5 -40 .00 20 20 | 2837 -2258 3723 9565
esx n/a| 0 0 -3 -10 53 35 .21 15 13 | 22522 -4127 3721 12665
gfz n/a| 1 1 4 16 62 22 -.05 23 18 | 0 -3145 3760 10786
grg n/a| 0 1 4 -83 -13 -71 -.31 30 23 | 7555 -3202 3826 9663
iac n/a| 0 -1 -1 7 -72 -11 -.09 18 16 | 7323 -2222 3720 9396
mcc n/a| -2 0 -38 138 -161 183 -.34 165 165 | --- --- --- ---
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 3.2003.0 GPS week: 2003 Day: 0 MJD: 58265
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 716 30 35 24 25 22 25 42 --- 13 | 38 53 39 51 55 61 59 --- 43
R02 | 582 10 14 13 14 13 19 14 161 6 | 42 41 44 38 43 40 43 79 39
R03 | 958 8 9 18 14 10 12 13 81 6 | 60 61 58 60 59 64 59 27 59
R04 | 1141 8 18 6 7 14 12 13 --- 4 | 54 58 51 47 54 61 42 --- 49
R05 | 1677 19 23 23 22 32 99 44 --- 18 | 40 48 56 56 44 45 49 --- 43
R07 | 622 5 9 10 9 22 9 14 142 5 | 65 66 66 72 77 67 58 147 66
R08 | 2000 18 13 11 12 21 18 11 --- 6 | 57 55 59 61 62 66 53 --- 58
R09 | 2139 12 20 10 9 18 15 14 --- 5 | 31 34 37 40 37 31 42 --- 35
R10 | 862 12 14 15 18 22 29 14 --- 8 | 54 54 39 62 38 50 51 --- 49
R11 | 786 17 22 12 9 22 19 15 162 6 | 58 59 44 49 33 56 37 45 45
R13 | 2437 15 18 10 11 20 24 13 --- 6 | 79 78 73 82 67 82 78 --- 76
R14 | 1031 27 26 12 8 24 16 13 --- 7 | 79 78 63 65 50 74 58 --- 63
R15 | 1520 52 51 27 17 51 41 15 --- 15 | 91 92 60 53 43 78 46 --- 57
R16 | 1146 35 43 51 20 34 71 29 --- 17 | 82 93 50 71 61 98 68 --- 65
R17E | 1176 11 12 22 15 18 19 9 --- 7 | 63 64 63 61 66 70 54 --- 61
R18E | 1012 9 10 14 11 19 14 15 --- 6 | 32 37 29 37 40 38 31 --- 32
R19E | 971 21 26 13 19 17 41 17 --- 9 | 74 80 72 79 75 85 71 --- 73
R20E | 991 20 20 21 12 31 38 14 --- 9 | 58 64 65 60 64 51 58 --- 57
R21E | 957 21 26 15 13 18 19 14 117 7 | 44 48 49 52 52 44 51 63 47
R22E | 1475 21 23 13 8 21 24 15 --- 7 | 126 128 125 125 134 126 120 --- 125
R23E | 1244 16 38 19 22 19 28 12 --- 8 | 129 129 134 127 125 124 119 --- 126
R24E | 903 17 58 24 29 30 52 25 --- 12 | 47 82 43 60 45 57 32 --- 42
XR26E | ---- 13 65 --- --- --- --- 16 --- 15 | 23 54 --- --- --- --- 34 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1290 21 27 20 16 24 36 20 136 |T 62 67 59 64 60 66 57 72 58
WRMS | 1290 21 23 20 13 23 25 18 136 |NE 59 62 52 57 51 62 53 74 53
MEDI | 1012 17 22 14 13 21 19 14 142 |MD 58 61 56 60 54 61 53 63 57
Table 3.2003.1 GPS week: 2003 Day: 1 MJD: 58266
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 522 30 30 42 33 29 61 46 --- 17 | 40 71 49 69 68 40 48 --- 49
R02 | 776 16 17 12 15 13 19 16 191 6 | 45 45 40 35 34 38 38 137 36
R03 | 1117 8 9 9 12 15 20 12 88 5 | 48 47 48 59 49 63 54 29 52
R04 | 2124 6 10 7 10 11 22 14 --- 5 | 45 47 45 47 41 61 36 --- 43
R05 | 1553 19 21 61 23 18 114 22 --- 19 | 39 40 67 47 41 35 33 --- 37
R07 | 692 7 12 11 13 11 25 20 173 6 | 55 54 54 67 61 75 45 90 57
R08 | 2794 21 24 17 17 15 26 13 --- 8 | 50 46 55 62 62 71 47 --- 55
R09 | 2479 13 14 12 10 16 25 18 --- 6 | 36 33 34 43 45 37 38 --- 37
R10 | 1345 14 17 15 20 19 38 8 --- 8 | 41 44 33 50 41 33 36 --- 39
R11 | 698 18 22 16 18 24 30 14 173 8 | 44 44 41 52 44 53 31 51 42
R13 | 1839 18 24 16 14 24 38 17 --- 9 | 62 60 56 62 67 82 62 --- 61
R14 | 1366 32 36 16 10 16 21 16 --- 8 | 61 59 59 58 52 60 46 --- 54
R15 | 3118 49 50 19 13 37 41 22 --- 14 | 59 60 48 42 36 61 33 --- 41
R16 | 1037 21 48 33 16 25 71 25 --- 13 | 50 82 32 54 50 87 60 --- 47
R17E | 967 18 11 15 12 23 18 9 --- 7 | 66 69 65 73 71 70 59 --- 66
R18E | 791 12 15 12 13 17 18 13 --- 6 | 37 40 35 38 41 37 31 --- 34
R19E | 1141 29 19 16 20 22 34 15 --- 10 | 63 65 78 79 75 76 61 --- 69
R20E | 1584 18 19 19 15 22 31 21 --- 9 | 55 55 62 55 52 53 57 --- 52
R21E | 936 20 21 12 9 20 21 13 89 7 | 45 46 43 52 54 49 51 71 47
R22E | 1042 18 22 12 10 16 27 11 --- 6 | 132 135 134 130 138 148 132 --- 133
R23E | 841 18 21 17 14 18 30 13 --- 7 | 99 104 103 99 102 103 94 --- 98
R24E | 2126 23 43 42 12 18 32 29 --- 12 | 39 59 71 51 49 51 37 --- 43
XR26E | ---- 22 67 --- --- --- --- 25 --- 24 | 17 60 --- --- --- --- 25 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1572 22 26 23 16 20 41 19 150 |T 53 59 56 60 57 62 50 75 52
WRMS | 1572 19 22 23 14 15 40 19 150 |NE 48 52 47 53 49 56 43 76 46
MEDI | 1117 18 21 16 13 18 27 16 173 |MD 48 55 49 54 50 60 46 71 47
Table 3.2003.2 GPS week: 2003 Day: 2 MJD: 58267
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 543 22 23 87 18 31 51 36 --- 18 | 44 46 61 52 61 62 50 --- 45
R02 | 939 13 18 19 15 16 10 20 192 7 | 38 41 48 37 34 33 35 198 35
R03 | 1254 9 14 11 11 9 11 13 117 5 | 50 49 50 46 50 47 52 55 48
R04 | 1687 13 12 10 14 15 13 13 --- 6 | 45 39 42 34 40 45 41 --- 39
R05 | 1089 25 30 63 28 31 108 18 --- 20 | 39 44 52 64 54 32 53 --- 44
R07 | 1841 7 10 10 12 9 16 17 257 5 | 56 55 58 58 54 65 51 210 55
R08 | 1516 11 13 16 14 14 14 19 --- 6 | 45 45 48 52 52 56 39 --- 46
R09 | 2946 10 19 14 11 19 19 17 --- 6 | 23 31 27 25 33 24 33 --- 24
R10 | 1808 12 18 18 24 16 16 10 --- 7 | 36 36 35 49 31 41 43 --- 38
R11 | 734 19 14 23 15 26 26 15 169 9 | 44 40 28 40 23 23 34 93 32
R13 | 1859 8 11 17 10 21 27 12 --- 6 | 58 65 57 59 42 71 48 --- 54
R14 | 1489 28 27 19 15 24 11 10 --- 8 | 68 70 53 64 44 54 61 --- 57
R15 | 1506 43 41 23 16 32 31 25 --- 13 | 71 69 53 44 52 61 43 --- 52
R16 | 1430 11 15 52 24 27 67 25 --- 15 | 54 49 80 66 59 85 57 --- 60
R17E | 748 15 16 13 12 20 16 17 --- 7 | 38 37 42 44 41 39 47 --- 40
R18E | 814 7 8 13 16 16 16 17 --- 6 | 26 22 30 28 28 27 36 --- 27
R19E | 1103 24 18 23 13 27 20 16 --- 9 | 48 52 54 51 63 56 58 --- 51
R20E | 907 20 22 24 22 38 46 28 --- 13 | 35 42 42 40 60 56 49 --- 39
R21E | 1279 12 9 17 13 20 14 12 118 6 | 44 45 43 47 44 39 50 126 43
R22E | 694 13 15 18 14 20 16 13 --- 7 | 61 64 61 73 70 65 61 --- 64
R23E | 1149 18 18 16 15 16 31 16 --- 8 | 70 75 67 72 71 76 70 --- 69
R24E | 1608 18 22 21 21 18 35 21 --- 9 | 43 47 45 53 42 32 40 --- 40
XR26E | ---- 15 30 --- --- --- --- 17 --- 16 | 20 34 --- --- --- --- 29 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1418 18 19 30 17 22 36 19 178 |T 45 47 48 49 47 49 46 136 44
WRMS | 1418 19 20 30 16 16 29 19 178 |NE 47 48 49 49 44 49 45 139 44
MEDI | 1254 13 18 18 15 20 16 17 169 |MD 44 45 48 49 44 47 48 126 44
Table 3.2003.3 GPS week: 2003 Day: 3 MJD: 58268
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 1185 15 20 65 25 28 64 34 --- 18 | 41 35 26 39 45 74 52 --- 36
R02 | 815 7 14 17 13 24 14 13 224 6 | 37 31 48 36 40 42 44 217 38
R03 | 1635 12 16 11 9 17 9 16 97 5 | 52 53 51 49 51 53 56 38 50
R04 | 567 16 15 21 8 12 20 11 --- 6 | 45 39 48 31 33 27 28 --- 33
R05 | 923 33 32 45 21 14 136 20 --- 14 | 37 47 50 66 61 34 65 --- 54
R07 | 1605 10 13 9 8 9 13 13 137 4 | 55 58 57 61 61 54 62 188 58
R08 | 759 15 13 16 14 16 12 10 --- 6 | 48 48 49 45 39 38 39 --- 42
R09 | 3316 13 16 17 13 19 20 10 --- 6 | 29 32 29 25 36 16 21 --- 22
R10 | 1093 16 18 16 19 19 21 18 --- 8 | 48 50 46 56 37 57 45 --- 48
R11 | 815 22 26 14 13 26 16 12 121 7 | 53 55 37 47 34 26 35 84 38
R13 | 2110 6 9 19 15 20 35 16 --- 8 | 43 39 38 53 38 60 41 --- 44
R14 | 1132 25 33 19 14 31 23 17 --- 9 | 52 60 37 36 26 53 34 --- 37
R15 | 1669 43 49 20 14 36 26 26 --- 12 | 74 82 51 51 52 53 32 --- 49
R16 | 1554 16 38 28 18 17 46 24 --- 11 | 49 55 43 49 52 39 51 --- 43
R17E | 1512 14 9 14 11 17 13 12 --- 6 | 35 37 38 40 44 43 37 --- 37
R18E | 1067 12 16 11 13 19 16 23 --- 7 | 28 29 27 26 30 22 26 --- 23
R19E | 1706 28 33 20 10 23 18 21 --- 9 | 28 35 33 33 49 37 32 --- 30
R20E | 728 16 19 21 13 29 19 22 --- 9 | 43 44 37 42 52 38 38 --- 37
R21E | 1410 15 13 21 10 24 16 13 78 7 | 36 39 39 44 54 34 44 50 39
R22E | 823 16 16 18 11 24 14 12 --- 7 | 76 76 65 72 82 80 78 --- 74
R23E | 3004 25 22 22 28 15 22 13 --- 10 | 64 64 64 73 66 58 60 --- 62
R24E | 2956 23 27 39 18 37 23 28 --- 12 | 43 56 62 48 51 55 39 --- 42
XR26E | ---- 22 49 --- --- --- --- 24 --- 23 | 33 42 --- --- --- --- 40 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1653 20 23 25 15 23 38 19 141 |T 45 48 44 46 46 45 43 115 42
WRMS | 1653 18 22 25 15 21 26 18 141 |NE 47 48 43 46 43 44 43 131 42
MEDI | 1185 16 18 19 13 19 19 16 121 |MD 43 47 43 45 45 42 40 84 39
Table 3.2003.4 GPS week: 2003 Day: 4 MJD: 58269
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 906 24 33 30 28 24 55 39 --- 15 | 55 73 62 56 65 71 59 --- 53
R02 | 651 14 12 12 11 15 10 14 149 5 | 37 42 47 47 53 43 44 135 43
R03 | 1125 9 8 11 5 14 18 14 87 5 | 50 52 53 50 59 68 57 27 54
R04 | 472 12 17 15 8 17 16 20 --- 6 | 47 54 49 42 46 47 44 --- 44
R05 | 580 40 51 29 33 33 111 37 --- 21 | 47 49 60 55 39 25 59 --- 44
R07 | 1518 13 13 19 15 22 18 13 79 7 | 58 59 62 69 64 50 62 102 61
R08 | 943 11 17 11 18 15 20 17 --- 7 | 57 62 56 63 59 50 48 --- 55
R09 | 4086 8 12 11 7 15 12 14 --- 5 | 29 28 32 31 30 25 33 --- 28
R10 | 1404 9 11 9 11 19 15 13 --- 5 | 46 48 45 57 39 52 48 --- 47
R11 | 1208 23 33 10 14 27 14 12 101 7 | 51 59 34 41 28 41 36 53 37
R13 | 1779 13 16 31 17 25 16 17 --- 9 | 55 61 60 57 39 44 50 --- 50
R14 | 1324 24 24 20 16 28 24 18 --- 9 | 65 60 60 60 44 69 59 --- 57
R15 | 4885 51 55 18 19 41 33 26 --- 14 | 75 79 60 47 45 75 50 --- 54
R16 | 990 16 20 25 34 28 56 22 --- 13 | 59 59 67 61 51 54 60 --- 54
R17E | 1654 17 23 12 10 20 22 16 --- 7 | 51 52 55 50 50 61 42 --- 49
R18E | 769 8 10 15 13 17 17 12 --- 6 | 33 32 40 30 32 32 39 --- 32
R19E | 1520 27 28 22 24 36 24 17 --- 11 | 53 50 60 76 62 57 59 --- 58
R20E | 767 16 22 24 22 47 34 15 --- 12 | 46 53 47 54 52 53 45 --- 45
R21E | 1062 15 19 13 14 20 18 10 74 6 | 39 43 46 48 47 42 42 61 42
R22E | 1126 17 25 14 10 27 28 8 --- 7 | 66 68 71 75 84 56 66 --- 69
R23E | 1708 25 27 18 21 14 13 19 --- 8 | 72 71 77 83 72 73 82 --- 75
R24E | 888 29 33 25 30 20 30 32 --- 12 | 45 47 49 61 46 32 45 --- 42
XR26E | ---- 14 58 --- --- --- --- 13 --- 14 | 27 62 --- --- --- --- 29 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1764 22 26 19 19 25 35 20 102 |T 50 54 54 55 50 50 50 75 48
WRMS | 1764 21 25 19 16 20 23 19 102 |NE 52 56 53 52 47 51 50 79 48
MEDI | 1125 16 22 15 15 20 18 16 87 |MD 51 54 55 55 47 50 48 61 49
Table 3.2003.5 GPS week: 2003 Day: 5 MJD: 58270
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 617 19 22 28 24 23 53 18 --- 12 | 46 49 47 45 54 65 41 --- 45
R02 | 923 9 7 15 26 12 11 17 103 7 | 30 31 34 31 25 32 36 67 28
R03 | 1010 11 7 8 19 16 13 17 80 6 | 36 37 37 49 36 38 33 28 37
R04 | 862 5 9 9 11 29 9 23 --- 7 | 39 38 34 47 37 47 49 --- 40
R05 | 1080 47 40 41 27 30 153 14 --- 16 | 38 34 28 37 49 54 30 --- 27
R07 | 1219 13 15 14 9 8 13 18 197 6 | 44 43 47 39 39 43 38 67 40
R08 | 773 6 9 10 9 8 18 11 --- 4 | 41 41 40 37 42 44 34 --- 38
R09 | 4495 10 15 15 17 14 19 15 --- 6 | 28 33 28 41 41 30 33 --- 31
R10 | 1576 15 18 10 12 19 29 14 --- 7 | 40 43 34 43 36 55 34 --- 37
R11 | 1693 24 19 18 11 19 23 10 98 8 | 40 39 26 35 27 23 27 36 29
R13 | 1782 8 11 20 11 26 14 16 --- 7 | 44 43 40 47 47 42 43 --- 42
R14 | 1121 24 31 20 12 34 15 15 --- 9 | 60 70 55 64 66 57 47 --- 56
R15 | 6045 53 54 21 17 43 30 28 --- 15 | 61 63 38 41 49 55 32 --- 41
R16 | 825 18 17 32 23 32 46 26 --- 13 | 56 66 57 70 72 56 61 --- 59
R17E | 1643 14 23 21 13 21 15 8 --- 7 | 71 74 66 69 77 75 72 --- 70
R18E | 1301 9 14 17 15 18 52 15 --- 10 | 25 27 25 29 30 63 27 --- 27
R19E | 1008 27 23 22 15 25 36 14 --- 10 | 51 52 52 60 64 58 60 --- 55
R20E | 878 21 33 34 19 29 25 23 --- 11 | 51 56 59 39 45 42 39 --- 42
R21E | 981 16 19 13 14 22 19 8 72 7 | 37 37 34 38 39 42 39 60 36
R22E | 2057 14 14 16 11 22 20 9 --- 6 | 63 61 65 67 75 57 64 --- 64
R23E | 2556 21 23 13 23 14 24 15 --- 8 | 81 80 85 86 87 76 80 --- 81
R24E | 1717 22 22 23 24 30 34 26 --- 11 | 42 51 38 46 46 60 38 --- 38
XR26E | ---- 20 117 --- --- --- --- 19 --- 20 | 17 90 --- --- --- --- 32 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS | 2070 22 23 21 17 24 42 17 119 |T 45 50 44 48 49 50 43 51 42
WRMS | 2070 21 22 21 15 18 25 17 119 |NE 43 45 38 44 44 45 38 49 39
MEDI | 1121 16 19 17 15 22 20 15 98 |MD 42 43 38 43 45 54 38 60 40
Table 3.2003.6 GPS week: 2003 Day: 6 MJD: 58271
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
------+---------------------------------------------------+-----------------------------------------------
R01 | 735 28 29 50 14 29 42 17 --- 13 | 48 52 29 58 70 85 61 --- 53
R02 | 923 10 9 11 9 10 21 11 146 5 | 42 46 48 49 54 61 53 49 49
R03 | 1829 10 8 12 11 12 20 10 75 5 | 54 54 56 60 62 58 55 41 56
R04 | 902 7 10 8 5 7 25 12 --- 5 | 47 49 49 48 47 51 49 --- 47
XR05 | 1252 31 43 44 31 --- 137 31 --- 20 | 32 57 36 47 --- 43 42 --- 32
R07 | 574 12 12 12 9 18 13 17 300 6 | 61 59 65 60 56 57 51 130 57
R08 | 883 8 7 13 12 21 17 13 --- 6 | 55 54 56 53 49 62 47 --- 52
R09 | 4111 9 13 13 9 14 31 12 --- 6 | 30 32 35 33 32 25 35 --- 30
R10 | 738 9 14 15 17 17 20 23 --- 7 | 50 55 42 54 35 50 45 --- 45
R11 | 1545 23 30 16 10 15 28 14 100 7 | 62 67 44 50 38 36 36 36 43
R13 | 1232 15 19 26 19 18 31 14 --- 9 | 61 61 56 76 56 81 66 --- 65
R14 | 862 23 24 12 15 24 17 10 --- 7 | 77 76 63 74 59 68 65 --- 67
R15 | 5202 48 47 21 14 38 40 21 --- 13 | 83 84 54 49 47 69 46 --- 53
R16 | 857 22 30 25 18 34 59 22 --- 13 | 78 89 66 81 77 71 75 --- 72
R17E | 1707 19 18 17 14 23 14 16 --- 7 | 80 80 77 76 77 71 83 --- 77
R18E | 794 11 17 12 14 16 25 11 --- 6 | 31 35 30 33 29 37 35 --- 29
R19E | 1165 26 37 23 15 26 31 22 --- 10 | 62 66 61 61 61 64 67 --- 61
R20E | 1890 28 29 24 24 25 38 20 --- 11 | 52 58 57 57 55 51 53 --- 50
R21E | 975 22 25 13 11 22 11 14 97 7 | 45 51 45 50 52 46 46 75 46
R22E | 1833 19 18 20 13 23 23 13 --- 8 | 76 79 79 79 80 79 81 --- 78
R23E | 2344 20 21 21 19 13 22 20 --- 8 | 92 95 96 91 93 84 93 --- 91
R24E | 1708 38 32 24 32 39 44 36 --- 15 | 47 51 39 52 55 52 44 --- 41
XR26E | ---- 13 57 --- --- --- --- 11 --- 12 | 45 63 --- --- --- --- 42 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1924 22 24 20 15 23 30 18 165 |T 56 61 53 58 56 59 55 66 53
WRMS | 1924 20 22 20 13 18 23 16 165 |NE 55 59 49 56 52 58 51 64 51
MEDI | 1165 19 21 16 14 21 25 14 100 |MD 54 58 54 54 55 58 51 49 52
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