[IGSREPORT-30330] Wk 2352 IGLOS Final Orbits
acc
acc at igs.org
Tue Feb 25 01:51:07 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2352 (Feb 02, 2025 - Feb 08, 2025)
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 2.2352.
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:
igl2352[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2352 in the SP3 format.
igl23527.sum Combination Report for GPS Week 2352.
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.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
Starting 02-Feb-2025 (GPS week 2352) the IGS Analysis Centers started using
the IGS realization of the updated ITRF2020-u2023, called IGb20. The combined
GLONASS orbits from this date are therefore in IGb20 frame.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | 1.9 ns
1 | -1.4 ns
2 | -2.5 ns
3 | -2.3 ns
4 | -1.8 ns
5 | -1.6 ns
6 | -1.1 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
----+--------+---------------
2 | ALL | R19
3 | ALL | R19
4 | ALL | R19
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 1.2352, 1a.2352).
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 2.2352.0-6)
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 3.2352.0-6).
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 2352 summary. (Feb 02, 2025 - Feb 08, 2025)
Table 1.2352.a GPS week : 2352 MJD: 60708.0-60714.0
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 0 -2 13 32 .12 18 16 | 7413 -427 3411 8231
| 0 1 1 16 16 27 .02 | 891 1346
esa n/a| -1 -1 0 -38 -12 27 -.14 32 29 | 12703 -1007 3389 9116
| 1 1 3 11 25 53 .04 | 8889 1341
gfz n/a| 0 0 1 16 21 -29 -.02 21 16 | 0 -296 3418 8214
| 0 1 2 9 19 23 .04 | 0 1267
grg n/a| 1 0 -2 3 -48 40 .35 18 16 | -1317 -309 3412 7807
| 1 1 3 16 17 54 .04 | 1082 1297
iac n/a| -1 1 -3 -5 17 -10 -.15 16 15 | -486 -328 3373 8703
| 1 0 2 24 32 35 .03 | 1656 415
jgx n/a| 0 0 5 11 -14 -39 -.21 20 20 | 8138 -343 3406 8258
| 1 1 1 18 10 22 .03 | 980 1377
Table 1.2352.b GPS week : 2352 MJD: 60708.0-60714.0
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 | 14 14 14 13 15 12 12 |
R02 | 7 6 7 5 5 6 6 |
R03 | 7 7 7 7 7 9 6 |
R04 | 7 8 8 7 8 7 8 |
R05 | 8 8 6 8 9 8 8 |
R07 | 8 7 8 7 8 8 8 |
R08 | 8 6 7 8 6 8 10 |
R09 | 5 7 7 7 7 7 8 |
R11 | 7 8 8 9 8 8 9 |
R12 | 7 7 7 7 9 9 7 |
R14 | 6 5 6 6 7 7 6 |
R15 | 7 8 8 8 7 8 9 |
R16 | 9 9 8 9 9 6 6 |
R17 | 8 9 7 11 8 8 8 |
R18 | 7 7 6 7 6 7 6 |
R19 | --- 0 --- --- --- 9 7 |
R20 | 19 18 20 19 19 22 25 |
R21 | 7 7 8 10 10 9 10 |
R22 | 7 8 6 8 7 8 7 |
R24 | 9 8 9 10 10 8 9 |
R26 | 0 36 30 36 26 429 386 |
Table 1.2352.c GPS week : 2352 MJD: 60708.0-60714.0
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 2352 0 | -108 -63 63 2107 734 547 77.2 2001 2001 | 1856 0
brd 2352 1 | -41 36 39 742 1862 -8858 78.0 2308 2308 | -1412 0
brd 2352 2 | 179 0 80 -218 3634 -3078 78.5 2127 2127 | -2530 0
brd 2352 3 | -17 -67 42 -1178 830 1507 79.0 2183 2183 | -2344 0
brd 2352 4 | -9 60 106 -296 1200 2107 79.3 1752 1752 | -1815 0
brd 2352 5 | -76 104 89 -209 822 8039 81.0 1873 1873 | -1645 0
brd 2352 6 | 13 60 -17 -1239 1702 146 81.6 2001 2001 | -1134 0
-------------+------------------------------------------------------------+----------------
brd 2352 mean| -8 18 57 -41 1540 58 79.2 2035 2035 | -1289 0
brd 2352 sdev| 92 65 41 1160 1024 5157 1.6 188 188 | 1471 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 2.2352.0 GPS week: 2352 Day: 0 MJD: 60708
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 4 55 .14 18 16 | 8620 1219 3385 8325
esa n/a| -3 0 0 -32 22 134 -.07 31 26 | 10729 -1354 3373 9411
gfz n/a| 1 1 2 18 43 -38 -.03 20 16 | 0 1501 3385 8251
grg n/a| 3 -1 0 -19 -52 -9 .37 20 16 | 935 1497 3384 7888
iac n/a| 0 1 -2 39 -6 5 -.15 12 12 | 2940 -338 3383 8874
jgx n/a| 2 -1 5 -19 0 -75 -.15 21 21 | 9103 1585 3377 8382
Table 2.2352.1 GPS week: 2352 Day: 1 MJD: 60709
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 13 45 .13 18 16 | 7567 1336 2897 8494
esa n/a| -2 0 -1 -28 -14 44 -.17 31 27 | 8007 1728 2892 9510
gfz n/a| 1 1 1 32 19 -67 -.01 19 16 | 0 1194 2899 8437
grg n/a| 0 0 0 1 -78 91 .35 20 18 | -2410 1364 2891 7979
iac n/a| -1 0 -4 -30 21 -5 -.11 16 14 | -92 -933 2896 9176
jgx n/a| 0 1 4 19 -25 -47 -.21 16 16 | 8552 1434 2899 8449
Table 2.2352.2 GPS week: 2352 Day: 2 MJD: 60710
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 1 3 33 56 .13 19 18 | 8241 -1630 3678 7666
esa n/a| -2 -1 -4 -24 -13 5 -.19 32 29 | 30394 -1229 3626 9516
gfz n/a| 0 -1 0 2 37 -28 -.00 19 13 | 0 -1443 3667 7613
grg n/a| 2 1 -4 22 -37 29 .41 19 16 | -1989 -1607 3681 7293
iac n/a| 0 1 0 -24 -19 -1 -.15 16 15 | -2036 -514 3625 8199
jgx n/a| 0 -1 3 12 -19 -23 -.19 17 17 | 9285 -1571 3642 7669
Table 2.2352.3 GPS week: 2352 Day: 3 MJD: 60711
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 0 -6 27 45 .11 18 16 | 7791 -2310 3264 8961
esa n/a| 0 0 -2 -42 -10 1 -.12 31 28 | 18740 -1120 3232 11452
gfz n/a| 0 0 0 17 14 4 -.08 20 16 | 0 -1953 3264 8991
grg n/a| 0 0 -6 10 -39 12 .37 17 14 | -1682 -1784 3265 8555
iac n/a| -1 2 -1 -20 39 -34 -.14 21 20 | -1790 -359 3207 9195
jgx n/a| 0 0 5 37 -27 -34 -.24 18 18 | 8391 -1909 3255 8930
Table 2.2352.4 GPS week: 2352 Day: 4 MJD: 60712
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 0 12 24 15 .12 15 15 | 6968 -427 3720 8877
esa n/a| 0 -4 5 -56 4 -27 -.12 32 32 | 8116 -2552 3632 8694
gfz n/a| 0 0 -4 8 13 -10 -.06 23 17 | 0 -494 3741 8961
grg n/a| 2 0 2 3 -30 -11 .31 18 15 | -1621 -466 3722 8538
iac n/a| -3 1 -4 2 9 39 -.19 17 15 | -710 -566 3657 9216
jgx n/a| 0 0 4 -4 -7 -19 -.22 20 20 | 7821 -566 3733 8929
Table 2.2352.5 GPS week: 2352 Day: 5 MJD: 60713
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 0 -35 -15 31 .10 17 15 | 6422 -656 3378 7146
esa n/a| 0 -3 2 -38 -18 -6 -.15 31 29 | 6555 -707 3385 7136
gfz n/a| 0 0 3 17 36 -20 .00 23 15 | 0 -587 3402 7077
grg n/a| 3 0 -4 21 -39 38 .34 17 15 | -1417 -646 3373 6641
iac n/a| 0 1 -5 -11 -1 -6 -.14 16 15 | -1129 269 3337 7663
jgx n/a| 0 -2 6 14 -15 -16 -.25 23 23 | 7192 -1055 3405 7266
Table 2.2352.6 GPS week: 2352 Day: 6 MJD: 60714
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 -1 2 9 -20 .10 18 15 | 6282 -527 3560 8149
esa n/a| 0 -3 2 -47 -59 39 -.15 33 29 | 6386 -1817 3587 8095
gfz n/a| 1 0 3 19 -13 -43 .05 22 17 | 0 -292 3572 8169
grg n/a| 0 1 -3 -16 -64 134 .29 19 15 | -1035 -525 3569 7761
iac n/a| 0 0 -2 8 77 -74 -.18 16 16 | -589 142 3507 8598
jgx n/a| 0 0 5 22 -4 -57 -.22 25 25 | 6624 -324 3533 8183
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 3.2352.0 GPS week: 2352 Day: 0 MJD: 60708
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2431 37 58 18 22 17 40 14 | 126 67 109 110 95 95 100
R02 | 1730 9 19 18 22 14 14 7 | 78 83 82 72 79 67 76
R03 | 1418 11 24 20 16 7 23 7 | 91 83 95 88 83 69 84
R04 | 2282 13 27 15 14 9 14 6 | 96 95 104 100 96 91 96
R05 | 1258 15 24 16 15 12 24 7 | 85 81 90 87 84 67 82
R07 | 1984 20 29 13 12 15 19 7 | 96 81 88 87 85 68 83
R08 | 1658 17 18 11 14 11 26 7 | 92 92 93 98 89 81 90
R09 | 801 10 19 13 9 10 8 5 | 26 25 25 25 26 25 24
R11 | 1300 13 43 10 16 6 7 7 | 20 29 26 29 18 19 20
R12 | 1441 21 18 17 12 10 16 7 | 38 33 42 33 28 28 31
R14 | 1256 13 21 18 11 9 11 6 | 45 45 43 42 39 38 40
R15 | 810 21 19 17 19 8 13 7 | 59 46 58 43 47 40 47
R16 | 901 24 28 21 12 15 16 8 | 74 58 71 56 64 52 62
R17E | 1214 15 23 16 26 9 14 7 | 258 263 253 257 254 257 256
R18E | 1428 12 24 16 19 9 16 7 | 22 29 32 35 30 19 25
R20E | 5815 27 69 54 45 25 43 18 | 95 95 102 119 88 113 95
R21E | 1010 11 24 20 12 13 18 7 | 267 274 275 264 265 268 267
R22E | 1986 17 23 18 9 10 12 6 | 45 43 48 48 45 40 44
R24E | 1407 17 20 16 31 14 21 9 | 37 32 33 39 31 35 30
XR26 |11045 --- 8 --- --- --- --- 0 | --- 231 --- --- --- --- 118
------+-----------------------------------------+-------------------------------------
RMS | 2001 18 31 20 20 12 21 |T 86 89 87 85 81 77 83
WRMS | 2001 16 26 16 16 12 21 |NE 71 74 71 66 64 56 68
MEDI | 1418 15 23 17 15 10 16 |MD 78 67 82 72 79 67 76
Table 3.2352.1 GPS week: 2352 Day: 1 MJD: 60709
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1327 41 64 14 29 22 18 14 | 101 60 83 89 69 75 79
R02 | 2085 9 20 7 14 10 15 5 | 63 63 59 62 60 51 58
R03 | 1026 8 20 15 16 15 16 6 | 62 58 52 65 70 51 58
R04 | 2404 9 20 22 17 18 13 7 | 74 70 84 68 54 60 66
R05 | 1817 15 19 17 21 13 18 7 | 65 71 75 75 63 59 65
R07 | 1204 17 27 9 20 8 13 7 | 68 57 57 67 63 53 60
R08 | 2219 13 20 10 19 11 13 6 | 72 73 69 74 68 63 69
R09 | 665 11 28 11 10 19 14 7 | 26 35 30 26 32 26 26
R11 | 1080 11 33 15 18 19 9 7 | 11 18 22 19 16 14 13
R12 | 1458 19 18 19 10 13 15 7 | 28 41 45 30 25 20 29
R14 | 1201 6 19 14 8 11 11 5 | 34 23 35 30 34 28 30
R15 | 761 28 19 11 12 8 18 7 | 45 42 38 34 38 35 37
R16 | 1231 21 24 24 12 12 21 8 | 55 49 67 43 51 44 50
R17E | 1837 10 22 20 32 16 10 8 | 186 189 188 188 187 186 187
R18E | 1376 8 24 11 21 16 7 6 | 21 26 21 28 22 18 19
XR19E | 9014 3 --- --- --- --- --- 0 | 78 --- --- --- --- --- 80
R20E | 7675 29 69 50 30 35 34 18 | 68 79 85 76 63 79 68
R21E | 1110 12 21 14 16 12 14 6 | 208 215 212 200 208 207 208
R22E | 2338 17 25 18 24 16 12 8 | 24 29 35 44 34 27 29
R24E | 648 15 31 13 23 14 18 8 | 41 44 50 50 40 45 42
XR26 |11263 --- 53 --- --- 25 --- 35 | --- 174 --- --- 60 --- 84
------+-----------------------------------------+-------------------------------------
RMS | 2307 18 31 19 20 16 16 |T 66 70 68 66 62 60 64
WRMS | 2307 16 27 16 18 14 16 |NE 54 59 55 52 50 44 51
MEDI | 1376 12 22 14 18 14 14 |MD 62 57 57 62 54 51 58
Table 3.2352.2 GPS week: 2352 Day: 2 MJD: 60710
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 888 43 71 19 18 24 13 14 | 111 42 88 90 74 85 83
R02 | 2452 11 29 16 18 10 15 7 | 66 70 51 75 66 51 61
R03 | 1080 7 30 10 13 19 14 7 | 71 56 69 72 86 62 70
R04 | 1973 16 29 17 11 16 16 7 | 79 73 62 68 71 60 66
R05 | 1394 13 29 10 12 9 11 6 | 75 74 64 68 66 69 68
R07 | 1379 16 25 14 13 21 21 8 | 74 63 71 65 84 54 68
R08 | 2640 16 18 10 19 10 17 6 | 71 64 69 74 62 56 65
R09 | 575 12 24 10 20 13 12 6 | 10 23 16 24 14 19 14
R11 | 937 12 29 8 25 14 10 7 | 11 18 16 31 11 14 13
R12 | 1668 22 18 14 15 6 10 6 | 37 28 33 20 26 25 27
R14 | 863 8 17 13 14 13 8 5 | 33 38 38 40 29 31 32
R15 | 1373 25 17 15 9 14 23 8 | 40 34 37 35 21 14 26
R16 | 1226 27 20 14 19 16 13 8 | 49 38 36 30 44 29 35
R17E | 2036 10 27 13 25 12 12 7 | 205 200 203 195 208 197 201
R18E | 768 12 20 17 14 12 6 6 | 26 28 25 26 27 24 23
R20E | 5957 25 65 61 30 36 46 20 | 40 59 67 52 45 58 45
R21E | 979 17 31 14 21 12 10 7 | 158 147 152 155 153 150 152
R22E | 3543 19 17 8 12 12 13 6 | 47 37 45 55 51 39 45
R24E | 1161 12 32 21 26 14 18 9 | 39 36 36 42 37 36 33
XR26 |10691 --- 46 --- --- 19 --- 29 | --- 173 --- --- 46 --- 81
------+-----------------------------------------+-------------------------------------
RMS | 2126 19 32 19 19 16 17 |T 65 64 63 68 61 56 60
WRMS | 2126 18 29 13 16 15 17 |NE 55 56 50 53 50 43 50
MEDI | 1373 16 27 14 18 13 13 |MD 49 48 51 55 46 51 61
Table 3.2352.3 GPS week: 2352 Day: 3 MJD: 60711
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1367 34 69 22 15 12 19 13 | 125 58 110 105 99 90 101
R02 | 1504 8 23 8 11 11 7 5 | 69 77 67 75 73 68 71
R03 | 2888 13 21 7 10 16 25 7 | 88 73 81 87 92 64 81
R04 | 1752 12 15 11 19 11 16 6 | 92 82 85 89 81 76 84
R05 | 659 11 44 13 14 12 14 8 | 81 97 74 76 71 70 75
R07 | 1648 13 24 21 13 14 14 7 | 92 72 100 81 94 77 87
R08 | 1926 11 25 16 15 17 19 7 | 84 89 74 81 91 70 80
R09 | 719 14 18 12 15 16 20 7 | 17 27 26 20 18 30 19
R11 | 1375 16 31 18 17 20 18 8 | 15 16 34 25 14 29 19
R12 | 881 14 18 13 12 15 19 7 | 29 26 33 31 17 18 22
R14 | 1943 8 17 16 10 12 9 5 | 34 37 29 31 36 35 32
R15 | 1680 27 22 19 10 9 13 8 | 44 34 33 30 31 22 29
R16 | 2788 18 17 20 13 13 27 8 | 50 47 54 37 47 26 40
R17E | 1386 21 23 15 15 42 13 10 | 179 182 183 173 155 180 174
R18E | 745 8 24 18 15 12 14 6 | 27 33 24 26 24 27 23
R20E | 5797 34 51 58 26 44 35 18 | 42 55 73 40 44 48 38
R21E | 1867 13 28 14 19 36 12 9 | 111 104 104 119 91 110 106
R22E | 2680 17 24 11 22 21 13 8 | 29 35 28 30 28 32 26
R24E | 1949 11 40 14 31 12 13 9 | 33 46 35 43 30 36 31
XR26 | 9250 --- 47 --- --- 27 --- 35 | --- 255 --- --- 53 --- 84
------+-----------------------------------------+-------------------------------------
RMS | 2182 18 31 20 17 21 18 |T 64 71 65 63 61 58 60
WRMS | 2182 16 28 16 14 20 18 |NE 63 70 61 59 58 51 58
MEDI | 1680 13 24 15 15 14 14 |MD 50 58 65 43 53 48 56
Table 3.2352.4 GPS week: 2352 Day: 4 MJD: 60712
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2207 24 70 46 13 14 33 14 | 117 59 133 105 115 83 105
R02 | 1020 10 15 8 9 11 9 4 | 67 71 58 69 56 58 62
R03 | 2799 13 21 12 20 11 14 6 | 77 62 62 87 63 62 70
R04 | 937 11 32 13 17 19 15 7 | 84 71 81 91 86 74 81
R05 | 645 10 29 15 27 17 15 8 | 75 81 68 88 66 64 72
R07 | 1723 9 23 26 16 15 12 7 | 82 76 86 81 83 73 79
R08 | 757 8 23 15 12 11 18 6 | 85 95 74 88 87 74 82
R09 | 1756 11 34 17 8 11 16 7 | 17 35 27 22 22 26 19
R11 | 1368 15 39 12 13 13 11 7 | 12 17 17 21 9 15 11
R12 | 1175 21 19 14 19 15 25 8 | 37 31 29 26 33 29 27
R14 | 2240 9 26 14 15 14 10 6 | 34 26 31 25 35 35 29
R15 | 1636 19 32 10 10 12 9 7 | 38 30 36 35 28 29 31
R16 | 2142 19 22 27 9 11 23 8 | 53 54 67 46 50 44 50
R17E | 1555 16 24 20 18 15 17 8 | 188 187 174 182 189 183 184
R18E | 716 11 16 11 15 19 11 6 | 19 24 16 25 20 19 17
R20E | 1856 28 59 52 26 40 54 19 | 38 52 52 52 47 49 39
R21E | 2592 14 33 21 33 17 12 9 | 186 195 197 181 188 190 188
R22E | 2213 16 17 11 15 17 13 6 | 38 47 34 38 31 32 33
R24E | 1762 13 20 37 21 19 14 9 | 42 45 61 34 39 49 40
XR26 |11878 --- 39 --- --- 17 --- 26 | --- 367 --- --- 41 --- 123
------+-----------------------------------------+-------------------------------------
RMS | 1752 15 32 23 18 17 20 |T 65 81 67 67 65 62 65
WRMS | 1752 15 32 17 15 15 20 |NE 59 76 59 60 55 51 60
MEDI | 1723 13 24 15 15 15 14 |MD 42 54 58 52 50 49 50
Table 3.2352.5 GPS week: 2352 Day: 5 MJD: 60713
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2239 27 49 27 17 14 26 11 | 96 65 92 92 81 67 83
R02 | 1197 10 15 11 15 14 12 5 | 61 55 63 67 55 57 59
R03 | 1832 16 22 17 16 19 25 8 | 74 64 74 73 53 58 65
R04 | 1797 13 28 9 15 11 16 6 | 76 73 77 82 85 71 77
R05 | 729 7 33 17 19 10 21 8 | 68 67 80 76 63 59 68
R07 | 1269 7 32 11 13 17 22 7 | 72 58 70 81 82 61 72
R08 | 982 15 31 14 14 15 22 8 | 71 80 77 72 77 69 73
R09 | 2993 12 33 15 15 11 13 7 | 22 40 25 30 23 24 23
R11 | 1030 14 43 14 10 7 18 8 | 22 42 30 24 30 20 24
R12 | 1161 23 21 20 27 9 15 9 | 32 27 39 25 32 24 26
R14 | 1745 8 33 9 13 13 18 7 | 27 20 27 23 33 26 24
R15 | 1652 21 26 20 12 11 18 8 | 30 21 22 29 26 14 20
R16 | 1718 14 14 17 6 15 12 6 | 35 36 29 38 38 32 33
R17E | 1585 15 18 20 14 20 15 7 | 160 161 159 157 157 159 158
R18E | 1040 12 25 19 11 15 10 6 | 22 27 23 25 23 20 20
XR19E | 3711 15 16 19 20 18 --- 9 | 52 68 49 76 94 --- 47
R20E | 1186 37 57 65 32 38 69 22 | 59 69 81 83 61 75 65
R21E | 3544 17 22 18 26 20 18 9 | 164 156 158 154 152 157 156
R22E | 2814 17 32 13 16 12 14 7 | 46 33 51 59 49 44 47
R24E | 2216 10 19 29 17 15 11 8 | 41 40 52 50 41 42 42
XR26 |13986 --- 671 --- --- 272 --- 428 | --- 593 --- --- 68 --- 178
------+-----------------------------------------+-------------------------------------
RMS | 1872 17 31 23 17 16 23 |T 61 85 63 65 63 56 64
WRMS | 1872 15 29 15 15 15 23 |NE 52 88 54 54 53 44 58
MEDI | 1718 14 28 17 15 15 18 |MD 52 58 52 67 55 57 59
Table 3.2352.6 GPS week: 2352 Day: 6 MJD: 60714
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1206 38 45 22 14 14 20 11 | 139 77 113 116 110 105 112
R02 | 932 6 19 17 12 14 10 6 | 85 89 89 82 80 77 83
R03 | 852 9 19 8 12 10 18 5 | 96 87 93 97 92 86 92
R04 | 1629 10 27 15 18 19 16 7 | 104 89 108 106 116 98 105
R05 | 1072 11 31 10 19 8 29 8 | 92 87 94 98 90 75 90
R07 | 1125 11 35 11 15 16 23 8 | 103 99 99 107 107 85 100
R08 | 1616 17 24 29 21 13 24 9 | 103 112 93 104 100 89 98
R09 | 3302 15 30 12 13 20 12 7 | 26 40 28 36 37 34 30
R11 | 841 17 48 19 13 13 15 9 | 21 45 38 32 31 21 28
R12 | 943 20 19 12 12 10 15 6 | 43 48 41 34 34 33 36
R14 | 1238 10 21 12 11 15 10 6 | 33 27 34 33 35 30 31
R15 | 813 17 30 12 18 11 30 8 | 47 29 40 49 36 22 36
R16 | 1027 14 29 13 7 7 13 6 | 60 57 60 55 52 44 53
R17E | 1893 15 15 18 12 19 18 7 | 199 197 198 196 199 194 196
R18E | 998 7 22 12 11 10 16 5 | 20 26 17 22 21 21 17
R19E | 4815 12 19 16 21 10 15 7 | 36 44 44 52 99 9999 35
R20E | 1484 33 80 68 54 25 79 25 | 80 86 92 95 79 98 80
R21E | 3589 26 22 16 16 26 26 10 | 237 229 232 234 228 230 231
R22E | 2896 15 26 12 10 19 15 7 | 50 48 53 54 48 49 49
R24E | 1560 15 37 27 16 16 14 9 | 50 55 65 60 54 54 53
XR26 |17040 --- 621 --- --- 239 --- 385 | --- 406 --- --- 71 --- 112
------+-----------------------------------------+-------------------------------------
RMS | 2002 18 33 22 19 16 25 |T 81 94 81 83 81 76 79
WRMS | 2002 15 29 17 15 16 25 |NE 73 92 71 73 70 61 71
MEDI | 1238 15 27 13 13 14 16 |MD 60 77 65 60 79 75 80
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