[IGSREPORT-26415] Wk 2039 IGLOS Final Orbits
acc
acc at igs.org
Sat Feb 23 03:13:18 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2039 (Feb 03, 2019 - Feb 09, 2019)
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 2.2039.
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:
igl2039[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2039 in the SP3 format.
igl20397.sum Combination Report for GPS Week 2039.
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 | 6.0 ns
1 | 6.5 ns
2 | 8.1 ns
3 | 7.5 ns
4 | 7.4 ns
5 | 7.9 ns
6 | 8.1 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 1.2039, 1a.2039).
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 2.2039.0-6)
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 3.2039.0-6).
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 2039 summary. (Feb 03, 2019 - Feb 09, 2019)
Table 1.2039.a GPS week : 2039 MJD: 58517.0-58523.0
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| -1 0 -4 19 4 24 .05 30 27 | 5011 -353 3488 9379
| 0 0 1 22 21 16 .02 | 865 1692
cof n/a| -1 -1 -7 23 14 11 .02 32 28 | 5000 -338 3488 9379
| 1 0 2 33 14 12 .02 | 857 1665
emx n/a| 0 0 2 21 -17 -37 .05 22 22 | 4718 106 3474 9296
| 1 1 1 31 19 26 .04 | 4390 1014
esx n/a| 0 0 0 -6 -5 -19 .07 22 19 | 3110 -2463 3489 11201
| 0 0 2 11 18 33 .02 | 13385 2565
gfz n/a| 0 0 -7 1 19 -8 .10 27 20 | 0 -341 3446 9191
| 1 0 2 16 23 28 .03 | 0 1466
grg n/a| 1 0 5 -68 2 69 -.40 35 27 | 7554 -476 3491 8908
| 1 1 4 19 18 37 .05 | 547 1598
iac n/a| 0 0 7 37 0 -29 -.13 33 33 | 33889 1703 14238 145851
| 1 0 1 42 38 43 .03 | 32960 2079
Table 1.2039.b GPS week : 2039 MJD: 58517.0-58523.0
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 | 25 23 22 23 23 20 21 |
R02 | 8 7 10 7 8 8 9 |
R03 | 12 11 10 11 10 10 11 |
R04 | 10 10 9 9 10 9 10 |
R05 | 13 11 10 10 10 13 12 |
R07 | 10 11 12 12 11 10 10 |
R08 | 8 8 9 11 12 9 9 |
R09 | 7 6 8 7 7 8 7 |
R10 | 6 10 10 8 9 9 7 |
R11 | 6 6 6 6 6 8 7 |
R13 | 7 9 12 9 8 9 10 |
R14 | 7 10 9 8 9 9 11 |
R15 | 9 10 11 11 11 11 12 |
R16 | 15 14 13 13 14 11 11 |
R17 | 10 10 10 10 11 10 9 |
R18 | 7 6 7 9 7 8 9 |
R19 | 26 22 22 25 21 18 20 |
R20 | 20 17 15 16 16 18 12 |
R21 | 10 10 10 13 13 10 11 |
R22 | 13 10 10 11 12 14 11 |
R23 | 8 8 10 9 8 9 9 |
R24 | 24 24 17 16 19 20 16 |
R26 | 28 17 15 17 34 35 26 |
Table 1.2039.c GPS week : 2039 MJD: 58517.0-58523.0
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 2039 0 | -85 13 -78 -481 -628 202 82.0 1605 1605 | 6024 0
brd 2039 1 | -5 -36 -33 914 1002 -1132 81.7 1479 1479 | 6542 0
brd 2039 2 | 37 -30 -39 858 114 -1370 80.9 1327 1327 | 8053 0
brd 2039 3 | 10 -1 46 -682 -1110 -5108 83.0 1160 1160 | 7535 0
brd 2039 4 | 23 77 -4 -322 78 -6502 82.6 1172 1172 | 7420 0
brd 2039 5 | 54 39 56 -264 -181 -6069 81.7 1212 1212 | 7939 0
brd 2039 6 | 14 33 -6 -1058 396 -4109 82.8 1102 1102 | 8091 0
-------------+------------------------------------------------------------+----------------
brd 2039 mean| 7 13 -8 -147 -46 -3441 82.1 1293 1293 | 7372 0
brd 2039 sdev| 45 40 47 753 686 2658 .7 186 186 | 799 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 2.2039.0 GPS week: 2039 Day: 0 MJD: 58517
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 -3 50 -26 18 .07 28 23 | 6711 -2529 3744 9264
cof n/a| 0 0 -3 59 -3 9 .01 31 25 | 6692 -2501 3741 9263
emx n/a| 0 -2 2 6 -41 -6 .07 28 28 | 8325 -1271 3758 9111
esx n/a| 0 1 -1 -11 15 -10 .09 23 17 | -13331 -5590 3760 11060
gfz n/a| -1 1 -4 33 32 3 .15 30 19 | 0 -2175 3699 9086
grg n/a| 0 0 3 -71 -14 27 -.40 34 27 | 7296 -2715 3736 8802
iac n/a| 0 0 10 -12 15 -89 -.13 40 40 | 9110 62 5326 12700
Table 2.2039.1 GPS week: 2039 Day: 1 MJD: 58518
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 26 -12 20 .04 34 30 | 5273 -2069 3530 10930
cof n/a| 0 0 -6 41 18 19 -.01 35 31 | 5238 -1996 3532 10934
emx n/a| 0 0 4 -23 -6 -23 -.03 24 24 | -2913 -1025 3509 10793
esx n/a| 0 0 0 0 -11 -11 .08 19 16 | 6892 -4975 3541 12227
gfz n/a| 2 1 -12 0 37 -46 .12 27 18 | 0 -2188 3555 10861
grg n/a| 0 -1 8 -47 -13 75 -.37 37 25 | 7227 -2358 3535 10252
iac n/a| -1 1 7 93 37 -17 -.17 32 33 | 8162 -1220 4790 11137
Table 2.2039.2 GPS week: 2039 Day: 2 MJD: 58519
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 -4 20 6 22 .02 31 29 | 4398 2508 3911 9633
cof n/a| 0 -2 -8 -5 -5 22 -.00 34 31 | 4407 2476 3910 9633
emx n/a| -1 0 4 10 -8 -75 .05 21 21 | 945 1656 3886 9504
esx n/a| 0 0 0 0 -7 -25 .10 21 19 | -3709 2266 3901 12349
gfz n/a| 1 0 -6 -14 -12 7 .13 26 19 | 0 1707 3802 9452
grg n/a| 2 2 0 -41 32 133 -.41 33 25 | 6982 1809 3929 8852
iac n/a| 2 0 5 60 15 9 -.07 33 33 | 4267 2863 5703 18671
Table 2.2039.3 GPS week: 2039 Day: 3 MJD: 58520
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 -4 -19 -1 3 .05 30 27 | 4817 550 3250 7834
cof n/a| -1 0 -10 -33 9 19 .03 30 28 | 4806 565 3254 7834
emx n/a| 1 0 3 62 -44 -20 .08 22 22 | 8242 580 3229 7762
esx n/a| 0 1 0 9 17 -90 .04 24 20 | -738 -1610 3246 9966
gfz n/a| 0 0 -6 7 46 -20 .08 29 21 | 0 759 3197 7664
grg n/a| 0 0 5 -93 8 71 -.38 32 26 | 7432 260 3261 7612
iac n/a| -1 -1 6 -3 -75 30 -.12 32 32 | 60003 3746 21133 287005
Table 2.2039.4 GPS week: 2039 Day: 4 MJD: 58521
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 -1 -3 3 26 53 .03 28 26 | 5157 249 3378 9269
cof n/a| -1 -1 -5 20 25 18 .01 30 26 | 5156 240 3377 9268
emx n/a| -1 0 1 57 6 -31 .06 23 23 | 8900 395 3361 9201
esx n/a| -1 0 4 -21 -35 -13 .06 25 21 | 29205 -2705 3368 10672
gfz n/a| -1 0 -6 9 -13 -33 .11 24 19 | 0 375 3345 8983
grg n/a| 2 1 3 -83 -15 79 -.35 36 28 | 7312 398 3368 8519
iac n/a| 2 0 8 43 8 -36 -.16 31 31 | 71948 3639 27628 331755
Table 2.2039.5 GPS week: 2039 Day: 5 MJD: 58522
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 -7 23 3 39 .07 31 27 | 4717 -718 3570 9834
cof n/a| -3 -1 -8 22 25 -11 .04 31 27 | 4703 -687 3566 9834
emx n/a| 1 1 0 1 -23 -71 .02 20 20 | 5123 575 3556 9866
esx n/a| 0 1 2 -1 -4 9 .08 23 20 | 6432 -1992 3573 11470
gfz n/a| 0 0 -6 -12 17 -11 .06 24 24 | 0 -117 3529 9651
grg n/a| 0 -1 3 -79 5 79 -.39 37 28 | 8139 -32 3567 9400
iac n/a| -1 0 7 80 22 -26 -.11 28 28 | 74330 3043 31969 350531
Table 2.2039.6 GPS week: 2039 Day: 6 MJD: 58523
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 -5 32 37 15 .07 28 24 | 4004 -464 3037 8890
cof n/a| 0 -1 -10 58 28 4 .06 32 27 | 4003 -466 3041 8890
emx n/a| 0 0 0 31 -4 -29 .06 18 18 | 4409 -163 3021 8837
esx n/a| -1 0 1 -18 -9 5 .05 20 18 | -2980 -2637 3035 10666
gfz n/a| 1 0 -9 -9 26 38 .08 26 20 | 0 -749 2996 8644
grg n/a| 0 1 16 -62 17 21 -.50 35 27 | 8494 -697 3044 8923
iac n/a| 0 0 8 0 -26 -77 -.13 32 32 | 9408 -207 3122 9163
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 3.2039.0 GPS week: 2039 Day: 0 MJD: 58517
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 639 83 89 46 55 35 38 57 24 | 114 119 36 46 78 64 27 49
R02 | 1493 20 15 21 6 18 16 25 7 | 77 76 54 63 70 66 47 62
R03 | 1013 25 27 20 22 23 32 38 11 | 103 103 74 76 104 103 61 86
R04M | 499 19 21 17 18 15 30 30 9 | 84 85 60 56 84 82 46 68
R05M | 737 23 19 30 12 50 21 33 13 | 85 86 46 65 104 60 48 67
R07 | 1642 24 28 19 15 20 14 43 9 | 96 101 73 63 85 77 49 73
R08 | 1754 16 19 16 10 21 18 30 8 | 98 103 81 86 103 85 71 88
R09 | 1180 17 17 12 5 18 19 21 6 | 28 27 22 20 29 22 25 20
R10 | 2774 11 15 13 9 7 11 23 5 | 62 67 52 73 76 60 58 64
R11 | 767 9 15 12 7 12 10 32 6 | 57 60 48 50 60 57 40 51
R13M | 3868 20 25 16 16 13 15 14 7 | 49 46 41 63 56 58 51 52
R14M | 1327 17 16 13 9 21 15 24 7 | 68 66 50 49 66 57 39 53
R15 | 832 27 32 16 19 11 13 25 8 | 100 102 86 82 89 87 79 86
R16 | 2029 36 34 39 15 31 38 43 14 | 55 57 58 70 71 54 77 61
R17 | 698 22 16 17 19 22 19 47 10 | 30 27 25 16 28 27 19 21
R18 | 748 14 11 13 7 11 10 34 6 | 23 23 21 19 22 14 18 16
R19 | 1591 43 44 31 59 82 48 75 25 | 52 52 32 25 108 54 20 41
R20M | 781 23 27 40 26 42 79 50 19 | 29 35 31 35 42 41 22 27
R21M | 626 20 20 14 18 22 22 48 10 | 31 33 27 25 36 34 25 28
R22M | 1189 15 12 21 26 23 41 51 13 | 34 33 26 36 40 43 30 32
R23M | 853 8 14 23 14 19 11 24 7 | 17 18 18 26 24 27 29 19
R24 | 2916 34 49 79 15 31 85 55 23 | 40 49 64 34 45 37 20 38
XR26M | 3797 18 50 --- --- --- --- 41 27 | 38 48 --- --- --- --- 24 31
------+----------------------------------------------+------------------------------------------
RMS | 1605 28 31 28 23 30 34 40 |T 59 61 46 49 64 54 40 49
WRMS | 1605 23 25 28 17 19 27 40 |NE 66 69 51 51 69 57 43 54
MEDI | 1180 20 20 17 15 21 19 34 |MD 55 57 46 49 66 57 39 51
Table 3.2039.1 GPS week: 2039 Day: 1 MJD: 58518
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 852 90 90 44 35 52 22 55 22 | 89 96 36 43 74 50 32 42
R02 | 1692 21 32 19 10 11 7 16 6 | 70 76 61 61 66 57 60 61
R03 | 846 30 30 17 18 22 28 33 10 | 98 95 83 85 91 92 87 86
R04M | 696 26 28 19 16 25 22 27 9 | 78 80 70 69 87 63 61 70
R05M | 610 30 32 27 13 22 18 36 10 | 70 75 67 70 72 57 50 63
R07 | 911 32 29 21 18 24 14 37 10 | 96 96 86 80 88 92 70 83
R08 | 1673 15 13 17 10 22 13 24 7 | 96 100 87 88 99 92 86 90
R09 | 1493 18 12 12 11 15 12 19 6 | 16 13 13 15 25 11 20 13
R10 | 4174 20 17 22 13 30 17 23 9 | 49 51 45 53 65 52 47 50
R11 | 594 15 15 14 7 9 13 25 6 | 34 35 32 29 35 36 20 30
R13M | 1844 20 24 24 15 13 29 21 9 | 42 47 33 48 47 65 43 43
R14M | 1301 18 22 21 15 17 32 40 10 | 48 52 43 41 54 67 34 44
R15 | 876 36 33 19 12 21 18 26 9 | 73 73 65 63 58 56 52 60
R16 | 1984 47 50 33 20 30 38 26 14 | 51 63 56 64 75 44 67 58
R17 | 876 22 29 12 15 11 33 34 9 | 21 26 17 18 22 22 21 17
R18 | 657 17 18 13 5 11 15 20 5 | 20 19 24 22 23 23 18 19
R19 | 1201 69 70 26 47 53 42 60 22 | 32 33 30 30 72 28 21 28
R20M | 719 18 17 28 16 34 77 39 16 | 26 26 36 31 40 24 21 26
R21M | 486 23 25 13 15 24 19 37 9 | 21 21 22 20 17 20 20 18
R22M | 628 29 32 14 14 11 30 30 9 | 22 23 19 19 28 20 25 18
R23M | 676 9 15 19 22 13 19 13 7 | 30 34 28 32 36 26 32 29
R24 | 2296 29 31 47 14 45 118 26 23 | 35 38 32 23 38 47 30 26
XR26M | 1827 14 47 --- --- --- --- 19 17 | 24 59 --- --- --- --- 25 22
------+----------------------------------------------+------------------------------------------
RMS | 1479 34 35 24 19 27 37 32 |T 49 53 44 45 55 47 40 43
WRMS | 1479 30 31 24 16 18 25 33 |NE 55 58 47 48 59 50 45 47
MEDI | 876 22 29 19 15 22 19 26 |MD 42 51 36 41 54 47 32 42
Table 3.2039.2 GPS week: 2039 Day: 2 MJD: 58519
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 700 71 85 38 44 48 46 55 22 | 98 110 47 35 80 63 32 50
R02 | 942 22 16 26 13 15 22 29 9 | 82 77 67 75 82 58 45 68
R03 | 1111 33 32 15 17 19 20 32 10 | 109 109 92 92 104 84 80 93
R04M | 1365 22 23 15 10 22 23 27 8 | 66 69 51 52 71 61 34 55
R05M | 593 33 38 21 16 26 19 14 10 | 74 81 57 58 75 65 61 62
R07 | 903 32 37 20 15 30 21 39 11 | 83 87 60 64 86 67 40 66
R08 | 1075 21 22 16 14 22 19 38 9 | 76 75 61 70 77 72 67 68
R09 | 829 13 14 13 22 18 17 14 7 | 24 23 21 26 35 28 23 22
R10 | 3539 10 10 27 12 35 20 15 10 | 55 59 44 54 80 66 51 55
R11 | 774 11 12 13 7 10 12 27 6 | 48 50 42 42 47 48 27 42
R13M | 1853 13 17 23 21 29 51 13 12 | 70 71 63 81 60 103 80 72
R14M | 863 29 26 12 12 12 19 33 8 | 52 50 29 31 34 43 22 32
R15 | 769 31 32 17 18 18 17 44 10 | 69 69 52 51 65 66 51 56
R16 | 1283 38 43 18 26 14 49 21 12 | 59 66 50 61 50 34 55 49
R17 | 842 25 22 13 19 10 34 37 10 | 25 26 20 23 26 20 15 19
R18 | 812 18 21 16 12 18 17 19 7 | 18 21 20 23 28 14 14 17
R19 | 1436 66 71 25 47 48 48 58 21 | 47 49 40 44 75 44 28 40
R20M | 1108 25 26 28 11 33 52 45 14 | 30 50 28 26 33 43 19 25
R21M | 592 21 20 10 17 24 19 38 9 | 29 27 23 24 27 26 18 23
R22M | 549 21 20 15 18 17 31 33 9 | 39 38 35 36 40 39 25 34
R23M | 1021 19 22 21 28 12 24 20 9 | 40 40 49 48 57 46 35 46
R24 | 2306 29 40 31 19 37 69 29 16 | 36 47 38 34 37 36 19 30
XR26M | 2490 12 54 --- --- --- --- 17 14 | 31 55 --- --- --- --- 22 22
------+----------------------------------------------+------------------------------------------
RMS | 1326 31 34 21 21 26 33 33 |T 54 58 44 47 57 51 37 45
WRMS | 1326 29 31 21 19 19 25 33 |NE 59 62 46 49 62 50 39 48
MEDI | 942 22 23 17 17 19 21 29 |MD 52 55 44 44 57 46 32 46
Table 3.2039.3 GPS week: 2039 Day: 3 MJD: 58520
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 735 69 60 37 53 47 48 58 23 | 103 96 46 24 74 85 28 51
R02 | 1026 18 28 19 9 16 13 16 7 | 96 105 88 90 86 87 90 88
R03 | 953 30 32 27 19 19 15 30 10 | 119 119 93 103 107 105 97 102
R04M | 899 24 24 18 13 21 22 28 9 | 92 94 87 79 91 88 76 84
R05M | 663 36 32 17 15 19 24 20 10 | 81 77 50 62 66 52 47 57
R07 | 1227 38 40 24 21 31 20 30 12 | 120 124 100 102 112 109 90 103
R08 | 1035 25 25 27 16 31 17 26 11 | 120 116 109 106 119 109 92 108
R09 | 647 15 21 11 9 16 23 11 6 | 24 31 17 18 32 17 17 17
R10 | 1924 9 10 22 12 14 25 12 7 | 50 51 37 55 60 65 51 50
R11 | 827 13 16 11 8 12 17 16 5 | 49 53 41 39 41 45 40 41
R13M | 1948 19 22 20 18 19 27 20 9 | 130 133 116 133 127 135 125 126
R14M | 1002 25 28 15 11 17 13 25 8 | 55 58 30 42 46 34 24 37
R15 | 1165 28 26 16 23 24 21 35 10 | 63 61 39 37 65 58 30 45
R16 | 1104 20 19 31 26 30 42 22 13 | 54 69 52 74 83 59 47 59
R17 | 747 25 27 14 19 14 29 38 10 | 18 21 18 17 22 18 13 15
R18 | 652 15 21 25 12 25 13 23 9 | 18 22 16 20 26 19 14 15
R19 | 1721 61 54 28 48 79 54 67 25 | 42 45 31 38 96 38 18 32
R20M | 1585 25 35 35 28 33 58 37 16 | 37 48 44 40 45 35 42 35
R21M | 715 22 28 14 31 36 22 40 12 | 25 28 26 26 40 29 18 25
R22M | 531 21 24 15 19 18 32 40 10 | 53 55 57 55 54 46 44 51
R23M | 567 10 13 15 25 12 27 19 8 | 51 56 50 63 58 48 44 53
R24 | 1874 29 31 19 23 32 65 33 15 | 35 45 33 25 50 46 32 26
XR26M | 3752 13 65 --- --- --- --- 19 16 | 25 73 --- --- --- --- 23 20
------+----------------------------------------------+------------------------------------------
RMS | 1160 30 30 22 24 29 32 32 |T 63 68 53 56 68 60 47 53
WRMS | 1160 27 28 22 20 21 26 32 |NE 65 68 51 53 69 61 47 53
MEDI | 1002 24 27 19 19 19 23 26 |MD 53 58 44 42 60 48 42 50
Table 3.2039.4 GPS week: 2039 Day: 4 MJD: 58521
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 820 71 78 38 42 49 49 52 22 | 90 96 30 27 68 58 33 43
R02 | 1089 16 15 24 12 10 18 15 7 | 58 56 59 53 61 61 52 56
R03 | 634 31 26 21 21 14 15 26 9 | 91 89 74 78 79 71 63 76
R04M | 880 25 24 20 15 19 28 31 10 | 267 269 258 259 265 267 261 262
R05M | 809 32 40 20 18 12 28 21 10 | 66 76 43 53 54 53 42 50
R07 | 2058 37 34 22 22 16 24 30 11 | 85 85 57 49 72 81 50 63
R08 | 2187 26 31 30 19 32 11 32 12 | 80 89 61 70 95 67 56 71
R09 | 993 17 14 14 7 20 20 14 7 | 16 16 14 18 27 18 17 14
R10 | 982 11 12 21 21 23 20 17 8 | 51 50 48 64 68 36 44 52
R11 | 786 11 11 10 8 15 13 20 6 | 47 46 41 41 57 46 34 44
R13M | 1260 12 11 19 17 11 17 27 7 | 213 214 211 220 222 219 205 215
R14M | 982 30 28 18 16 13 18 19 8 | 51 51 30 32 43 42 30 35
R15 | 1101 32 29 18 24 12 26 34 11 | 76 75 57 52 65 63 56 59
R16 | 1081 21 30 33 30 22 52 23 13 | 37 51 53 67 61 63 61 54
R17 | 554 22 27 14 22 15 34 36 10 | 17 22 21 18 21 24 13 16
R18 | 601 15 15 18 7 12 13 24 7 | 16 20 18 19 21 14 14 15
R19 | 2218 46 43 26 50 46 62 58 21 | 29 30 27 34 50 27 23 20
R20M | 1142 18 32 25 36 30 62 44 16 | 38 56 70 31 39 30 28 38
R21M | 816 23 20 15 36 32 20 35 12 | 21 24 23 21 28 18 17 18
R22M | 549 24 16 14 26 15 42 37 11 | 69 68 65 69 68 70 76 68
R23M | 666 9 11 12 22 11 32 15 7 | 38 41 35 38 42 41 35 37
R24 | 1306 17 30 40 16 43 83 33 18 | 23 25 51 26 29 19 32 23
XR26M | 3517 28 55 --- --- --- --- 40 34 | 27 63 --- --- --- --- 22 23
------+----------------------------------------------+------------------------------------------
RMS | 1172 28 30 23 25 24 36 31 |T 65 70 61 60 69 63 54 58
WRMS | 1172 26 26 23 21 19 28 31 |NE 51 53 43 44 55 46 39 43
MEDI | 982 23 27 20 21 15 24 30 |MD 51 56 48 41 57 46 35 44
Table 3.2039.5 GPS week: 2039 Day: 5 MJD: 58522
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1043 82 77 28 41 28 33 50 20 | 84 82 38 41 49 49 36 39
R02 | 1209 19 21 18 12 15 26 20 8 | 80 80 72 80 80 66 74 74
R03 | 599 33 35 18 12 22 13 31 10 | 114 116 96 103 112 106 100 103
R04M | 1524 28 27 15 15 22 11 27 9 | 400 392 391 391 395 390 400 393
R05M | 689 31 28 31 22 33 29 28 13 | 61 61 45 59 77 51 39 51
R07 | 1757 35 37 17 19 23 16 20 10 | 110 111 101 98 101 105 92 100
R08 | 1028 24 26 23 13 20 23 16 9 | 103 101 94 97 105 112 94 99
R09 | 1186 17 17 16 10 29 15 13 8 | 21 20 22 23 35 24 22 20
R10 | 1903 16 15 16 24 28 13 17 9 | 42 42 38 55 41 41 35 40
R11 | 696 13 15 16 14 15 25 20 7 | 47 48 45 48 43 35 41 41
R13M | 2044 17 16 20 16 23 27 14 9 | 305 307 313 299 301 291 307 303
R14M | 1017 22 20 21 12 20 12 21 8 | 44 44 24 40 46 36 28 33
R15 | 1177 29 26 19 24 18 23 32 10 | 59 59 46 35 52 57 40 45
R16 | 718 26 38 17 29 15 44 11 11 | 35 39 44 59 40 61 44 44
R17 | 796 22 19 10 17 24 26 37 10 | 16 20 19 21 29 17 19 18
R18 | 531 20 20 16 14 15 17 15 7 | 17 21 16 21 29 19 16 16
R19 | 2056 51 43 17 50 34 46 43 18 | 23 33 21 39 31 16 23 18
R20M | 714 25 31 43 20 29 72 32 17 | 28 35 28 48 33 35 25 25
R21M | 781 20 27 12 20 25 21 32 9 | 17 23 19 24 26 21 21 18
R22M | 746 25 34 14 31 24 42 43 13 | 91 99 95 101 105 100 97 97
R23M | 704 12 15 13 25 21 25 19 9 | 36 41 42 42 41 24 31 36
R24 | 1590 28 22 19 27 31 103 23 19 | 28 48 45 40 50 69 27 38
XR26M | 2051 34 133 --- --- --- --- 36 35 | 25 109 --- --- --- --- 23 21
------+----------------------------------------------+------------------------------------------
RMS | 1212 31 31 20 23 24 37 28 |T 77 83 75 80 82 78 71 72
WRMS | 1212 27 27 20 20 24 28 28 |NE 55 58 49 54 56 55 47 49
MEDI | 1028 25 26 17 19 23 25 23 |MD 44 48 44 48 46 49 36 40
Table 3.2039.6 GPS week: 2039 Day: 6 MJD: 58523
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1155 73 84 26 48 53 21 46 20 | 107 115 34 41 83 54 34 45
R02 | 1107 23 21 15 10 26 20 28 9 | 80 85 71 80 92 77 60 76
R03 | 648 35 42 19 10 29 24 32 11 | 115 118 98 96 113 96 82 98
R04M | 894 29 26 16 16 17 19 36 9 | 373 375 372 368 374 372 359 370
R05M | 757 26 36 24 15 41 18 22 11 | 97 101 63 72 103 71 64 75
R07 | 1153 41 39 15 20 16 17 25 10 | 106 105 77 84 96 83 65 84
R08 | 1003 27 29 14 14 23 21 24 9 | 96 89 80 85 101 85 76 85
R09 | 2056 16 12 16 6 25 15 13 7 | 27 25 25 19 24 22 23 19
R10 | 1627 8 12 12 15 15 21 11 6 | 64 62 51 72 71 60 55 61
R11 | 774 12 10 13 11 14 12 27 6 | 64 63 57 58 65 53 48 57
R13M | 1147 15 15 17 26 17 32 14 9 | 395 394 391 395 398 407 392 395
R14M | 1132 24 30 20 22 25 25 27 10 | 68 75 41 47 67 65 34 51
R15 | 1157 27 33 16 25 26 20 45 11 | 91 96 71 60 86 77 53 70
R16 | 801 23 20 16 20 14 50 20 11 | 47 60 57 74 66 61 63 60
R17 | 695 22 27 9 13 11 22 39 8 | 22 24 22 20 22 23 12 19
R18 | 568 15 17 20 11 30 18 22 9 | 19 21 18 21 28 18 11 17
R19 | 1499 40 47 19 27 44 81 69 20 | 44 42 28 40 43 64 21 29
R20M | 741 16 15 24 6 20 54 27 11 | 56 57 67 53 66 60 57 58
R21M | 887 21 20 10 25 23 25 38 10 | 29 28 26 25 36 31 21 26
R22M | 1288 24 19 13 22 14 25 44 10 | 116 111 113 108 107 114 108 110
R23M | 1068 13 13 20 23 15 24 20 9 | 36 41 36 47 44 46 44 40
R24 | 880 22 32 27 21 30 79 26 16 | 40 53 34 37 45 43 24 26
XR26M | 2542 22 48 --- --- --- --- 30 25 | 21 52 --- --- --- --- 26 22
------+----------------------------------------------+------------------------------------------
RMS | 1102 28 32 18 20 26 35 32 |T 91 95 83 86 96 90 75 82
WRMS | 1102 24 27 18 18 20 27 32 |NE 65 68 51 56 66 58 44 53
MEDI | 1068 23 26 16 16 23 21 27 |MD 64 63 57 58 67 61 53 58
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