[IGSREPORT-30612] Wk 2382 IGLOS Final Orbits
acc
acc at igs.org
Fri Sep 19 15:04:30 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2382 (Aug 31, 2025 - Sep 06, 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 2.2382.
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:
igl2382[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2382 in the SP3 format.
igl23827.sum Combination Report for GPS Week 2382.
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 | 4.5 ns
1 | 3.2 ns
2 | 2.3 ns
3 | 1.6 ns
4 | -1.2 ns
5 | 4.1 ns
6 | 3.2 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
----+--------+---------------
0 | ESA | R20
1 | ESA | R20
2 | ESA | R20
3 | ESA | R20
4 | ESA | R20
5 | ESA | R20
6 | ESA | R20
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 1.2382, 1a.2382).
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 2.2382.0-6)
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 3.2382.0-6).
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 2382 summary. (Aug 31, 2025 - Sep 06, 2025)
Table 1.2382.a GPS week : 2382 MJD: 60918.0-60924.0
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 -14 16 22 .14 15 13 | 2782 -2640 4339 10763
| 1 0 1 21 13 24 .04 | 1893 2765
esa n/a| -3 -2 1 16 -15 57 -.14 33 29 | 3678 -2744 4338 10032
| 1 1 1 9 19 50 .05 | 2044 3016
gfz n/a| 1 0 3 29 8 -17 -.04 18 15 | 0 -1968 3872 9886
| 0 0 2 13 13 26 .02 | 0 3403
grg n/a| 2 1 0 -24 -11 -22 .36 16 15 | 2809 -1807 3837 9705
| 1 0 1 13 11 30 .04 | 2086 2144
iac n/a| 0 0 -3 14 8 -5 -.19 16 15 | 5215 -2172 4424 11445
| 1 0 2 14 29 55 .04 | 2138 1896
jgx n/a| 0 0 -5 -27 -25 -34 -.18 18 18 | 3651 -1013 3281 8893
| 1 1 1 13 11 37 .02 | 1411 3015
Table 1.2382.b GPS week : 2382 MJD: 60918.0-60924.0
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
------+------------------------------------+------------------------------------------
R02 | 7 5 5 5 6 6 5 |
R03 | 6 4 5 6 6 7 7 |
R04 | 7 6 5 5 6 4 6 |
R05 | 5 7 5 6 5 5 5 |
R07 | 8 8 7 7 6 7 6 |
R08 | 8 8 11 7 9 8 8 |
R09 | 7 7 6 6 7 7 6 |
R11 | 8 8 9 7 9 8 7 |
R12 | 7 7 6 7 7 7 5 |
R14 | 7 7 7 6 6 5 5 |
R15 | 7 7 7 7 7 7 7 |
R16 | 7 7 7 5 8 7 6 |
R17 | 8 7 7 6 8 8 7 |
R18 | 8 10 8 7 7 7 8 |
R19 | 9 10 12 9 9 9 10 |
R20 | 22 20 19 22 21 20 26 |
R21 | 8 8 8 8 8 8 8 |
R22 | 9 9 8 8 8 9 8 |
R24 | 8 8 7 7 7 6 6 |
R25 | 44 59 70 86 106 71 72 |
R26 | --- 29 35 31 27 27 23 |
R27 | 28 28 25 29 31 31 27 |
Table 1.2382.c GPS week : 2382 MJD: 60918.0-60924.0
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 2382 0 | -46 33 55 -1614 852 -1396 81.5 3051 3051 | 4496 0
brd 2382 1 | 34 13 -17 -887 -455 -174 79.5 2189 2189 | 3234 0
brd 2382 2 | 39 66 -7 -711 -1135 131 77.0 1999 1999 | 2308 0
brd 2382 3 | -71 195 3 -2183 823 3188 77.9 1973 1973 | 1627 0
brd 2382 4 | 15 -14 4 511 2197 7227 80.8 1748 1748 | -1225 0
brd 2382 5 | -6 46 75 1071 1769 6347 79.7 1484 1484 | 4139 0
brd 2382 6 | 0 99 126 102 213 3773 78.6 1320 1320 | 3156 0
-------------+------------------------------------------------------------+----------------
brd 2382 mean| -5 62 34 -530 609 2728 79.3 1966 1966 | 2533 0
brd 2382 sdev| 41 69 53 1163 1176 3336 1.6 566 566 | 1928 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 2.2382.0 GPS week: 2382 Day: 0 MJD: 60918
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 10 2 -6 .14 17 14 | 4673 -3626 3267 8993
esa n/a| -5 -2 3 14 0 149 -.06 34 26 | 6182 -4309 3272 8677
gfz n/a| 1 0 2 19 22 28 -.06 19 16 | 0 -4574 3323 8443
grg n/a| 4 1 1 -13 6 -61 .39 16 17 | 6212 -3554 3252 8784
iac n/a| 1 0 0 -2 -7 -84 -.24 19 19 | 7793 -2546 3558 10967
jgx n/a| 0 0 -7 -14 -8 0 -.20 19 19 | 4421 -3873 3370 8750
Table 2.2382.1 GPS week: 2382 Day: 1 MJD: 60919
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 -7 10 13 .15 15 14 | 3993 1544 3205 10079
esa n/a| -6 -4 1 14 -18 -19 -.11 33 30 | 4614 1558 3086 9350
gfz n/a| 1 0 2 44 8 -40 -.02 17 13 | 0 2351 3138 10101
grg n/a| 3 0 -1 -32 -16 3 .35 17 16 | 2622 1395 3052 9477
iac n/a| 0 0 -1 5 23 93 -.18 17 18 | 7870 -785 3276 11497
jgx n/a| 0 2 -6 -29 -37 -44 -.19 19 19 | 3167 1789 3175 9796
Table 2.2382.2 GPS week: 2382 Day: 2 MJD: 60920
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 5 -25 23 6 .16 14 13 | 4336 -2974 5312 10029
esa n/a| -4 -3 2 1 -1 47 -.22 36 31 | 3578 -2788 5363 9017
gfz n/a| 1 0 1 21 11 4 -.05 22 15 | 0 -12 3038 9597
grg n/a| 3 0 0 -23 -3 -30 .38 15 15 | 2942 -2726 5505 9348
iac n/a| -1 0 -3 22 -38 5 -.17 15 14 | 5557 -2934 5289 10702
jgx n/a| 0 1 -3 -13 -27 -20 -.20 19 19 | 2012 556 2965 8658
Table 2.2382.3 GPS week: 2382 Day: 3 MJD: 60921
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 6 -22 35 50 .19 18 14 | 3896 -3093 6510 9871
esa n/a| 0 0 2 11 9 73 -.12 36 30 | 5400 -3555 6515 9613
gfz n/a| 0 0 2 49 -5 -43 -.06 20 15 | 0 -713 5275 9197
grg n/a| 1 1 0 -23 -15 -37 .36 16 12 | 1213 -596 5433 9385
iac n/a| 0 0 -5 5 -4 -52 -.19 13 13 | 5239 -4301 6422 10104
jgx n/a| -1 0 -5 -29 -15 12 -.16 17 17 | 2662 2620 3413 8536
Table 2.2382.4 GPS week: 2382 Day: 4 MJD: 60922
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 3 -54 31 50 .18 17 14 | 1686 -6727 5717 11513
esa n/a| -3 0 0 30 -39 36 -.20 36 29 | 2397 -6731 5710 11122
gfz n/a| 0 0 1 30 12 -36 -.01 17 15 | 0 -6992 5839 10209
grg n/a| 0 0 1 -3 -8 -29 .37 17 16 | -447 -4051 3150 10801
iac n/a| 1 0 -1 28 7 10 -.22 15 13 | 1905 -4236 5772 11866
jgx n/a| 0 0 -5 -20 -21 -58 -.15 20 20 | 2902 -3819 3292 9386
Table 2.2382.5 GPS week: 2382 Day: 5 MJD: 60923
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 3 1 3 2 .13 15 12 | 1037 318 3369 13107
esa n/a| -2 -1 0 24 -40 55 -.12 34 40 | 31 1036 3369 13220
gfz n/a| 1 0 4 26 21 -13 -.00 17 13 | 0 668 3459 11421
grg n/a| 0 0 -2 -44 -27 31 .37 17 16 | 3241 286 3458 10823
iac n/a| 1 0 -4 9 33 0 -.21 17 16 | 4256 888 3368 13055
jgx n/a| 0 0 -2 -53 -30 -98 -.15 19 19 | 6224 292 3569 9278
Table 2.2382.6 GPS week: 2382 Day: 6 MJD: 60924
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| -3 0 4 -1 6 39 .06 10 10 | -145 -3925 2997 11749
esa n/a| -1 -2 0 22 -18 62 -.13 19 18 | 3545 -4420 3057 9226
gfz n/a| 1 -1 7 11 -12 -20 -.05 15 14 | 0 -4508 3037 10238
grg n/a| 1 2 0 -29 -18 -29 .28 12 12 | 3881 -3406 3009 9322
iac n/a| 1 -1 -6 35 47 -13 -.11 15 14 | 3891 -1292 3283 11929
jgx n/a| 2 0 -6 -32 -39 -31 -.20 17 17 | 4175 -4661 3184 7852
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 3.2382.0 GPS week: 2382 Day: 0 MJD: 60918
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2005 6 17 19 11 18 18 7 | 58 59 60 57 65 52 57
R03 | 2819 12 19 14 11 16 7 6 | 66 70 60 63 66 55 62
R04 | 1120 8 18 15 11 20 15 6 | 73 69 70 68 74 66 69
R05 | 1149 8 11 6 12 13 8 4 | 65 64 65 67 64 62 64
R07 | 1391 12 28 20 15 19 9 7 | 69 61 75 69 68 61 66
R08 | 997 15 21 13 11 24 23 8 | 58 56 70 66 74 58 63
R09 | 1387 12 22 17 12 17 16 7 | 60 66 69 61 58 59 60
R11 | 1482 19 19 20 18 20 8 8 | 40 51 46 47 40 46 42
R12 | 1039 5 16 15 10 26 13 6 | 54 61 46 61 66 43 53
R14 | 864 9 17 16 15 19 18 7 | 54 62 56 57 64 43 54
R15 | 1462 7 27 12 15 12 15 6 | 73 61 73 79 76 60 70
R16 | 1487 14 20 15 17 11 16 7 | 66 55 67 61 60 47 58
R17 | 1695 12 21 16 23 17 14 7 | 87 75 89 77 72 66 77
R18 | 1098 23 15 13 14 17 17 8 | 71 84 85 78 85 74 78
XR19 | 2106 11 19 17 --- 15 --- 8 | 24 33 39 --- 33 --- 29
R20 |11152 50 115 47 25 32 48 21 | 81 97 81 61 65 65 66
R21 | 983 13 19 15 15 13 22 7 | 92 85 98 96 87 80 89
XR22 | 1620 19 22 17 13 8 --- 8 | 41 47 43 50 43 --- 42
R24 | 1038 10 35 14 24 13 13 8 | 83 89 84 81 86 73 80
XR25 |18327 34 --- --- --- 57 --- 44 | 97 --- --- --- 112 --- 89
XR27 |10156 42 69 --- 27 60 --- 28 | 36 110 --- 47 83 --- 57
------+-----------------------------------------+-------------------------------------
RMS | 3051 17 34 19 16 19 19 |T 63 67 66 65 68 59 62
WRMS | 3051 14 26 16 17 19 19 |NE 63 67 66 65 68 59 62
MEDI | 1462 12 19 15 15 17 15 |MD 65 62 67 63 66 60 62
Table 3.2382.1 GPS week: 2382 Day: 1 MJD: 60919
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1622 10 17 13 10 13 7 5 | 31 39 31 34 36 36 32
R03 | 1204 5 12 6 12 10 8 4 | 33 38 32 38 29 30 31
R04 | 1181 7 19 16 13 16 7 6 | 40 42 34 43 42 34 37
R05 | 1519 10 20 14 13 19 9 6 | 33 33 28 34 42 38 32
R07 | 1917 15 16 16 13 24 13 7 | 40 36 39 41 29 30 33
R08 | 970 11 19 13 10 22 22 7 | 37 41 32 38 35 31 33
R09 | 1359 15 24 15 13 11 11 6 | 40 43 44 44 37 36 39
R11 | 1321 18 17 13 14 27 9 7 | 33 42 41 32 37 34 34
R12 | 1325 13 13 11 20 6 19 6 | 43 51 50 57 41 33 44
R14 | 990 7 15 11 15 19 16 6 | 47 52 39 57 57 35 45
R15 | 1619 13 27 15 12 19 12 7 | 64 48 55 62 71 54 58
R16 | 810 16 13 13 17 8 17 6 | 55 47 48 52 52 37 46
R17 | 1920 15 14 13 23 14 13 7 | 48 52 42 45 35 40 41
R18 | 1157 23 33 21 26 19 15 10 | 42 58 54 48 54 48 47
XR19 | 2016 18 13 21 --- 8 --- 9 | 23 27 45 --- 27 --- 28
R20 | 7172 34 112 40 28 21 58 19 | 48 55 56 57 46 46 45
R21 | 1260 15 14 19 17 12 19 7 | 44 42 43 46 36 28 38
XR22 | 1924 19 26 10 18 15 --- 8 | 19 31 21 39 22 --- 22
R24 | 1162 8 33 10 18 19 16 8 | 40 53 35 48 50 39 40
XR25 |15571 48 --- --- --- 70 --- 58 | 73 --- --- --- 57 --- 55
XR26 |11706 44 68 37 --- 55 --- 29 | 37 47 46 --- 53 --- 40
XR27 | 9082 41 64 --- 38 52 --- 28 | 28 53 --- 33 42 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 2188 15 33 17 17 17 19 |T 40 44 40 44 42 37 38
WRMS | 2188 14 30 13 16 18 19 |NE 40 44 40 44 42 37 38
MEDI | 1359 15 19 13 15 19 13 |MD 40 43 41 44 41 36 38
Table 3.2382.2 GPS week: 2382 Day: 2 MJD: 60920
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2506 11 18 8 10 8 11 5 | 46 48 38 47 44 41 43
R03 | 1867 12 11 10 12 12 7 5 | 49 47 47 42 40 41 43
R04 | 1535 9 18 12 12 12 9 5 | 52 53 55 48 52 49 51
R05 | 1405 8 16 9 8 10 9 4 | 49 53 51 47 53 48 49
R07 | 1928 10 20 22 12 13 21 7 | 53 52 63 57 51 43 52
R08 | 1071 14 41 32 15 16 29 11 | 46 54 74 66 61 42 54
R09 | 1291 11 25 13 9 15 11 6 | 44 42 43 35 41 41 40
R11 | 1382 25 18 16 21 14 15 8 | 24 38 38 49 35 36 33
R12 | 1411 10 22 10 17 10 11 6 | 40 53 38 55 36 39 42
R14 | 1161 7 29 16 11 17 19 7 | 43 64 49 48 38 37 43
R15 | 1411 14 20 11 10 19 13 6 | 60 50 58 61 67 51 58
R16 | 1194 11 18 19 17 13 15 7 | 55 47 60 47 57 47 51
R17 | 1724 10 24 17 16 11 21 7 | 65 52 68 66 60 49 59
R18 | 1057 20 22 14 20 22 9 8 | 52 57 57 57 71 52 56
XR19 | 1438 18 18 19 --- 22 --- 11 | 22 39 40 --- 42 --- 31
R20 | 5697 30 118 59 27 25 42 18 | 63 84 81 48 63 49 58
R21 | 1066 11 19 24 12 7 24 7 | 68 59 72 69 62 52 63
XR22 | 1591 16 19 10 15 13 --- 7 | 31 34 34 44 37 --- 34
R24 | 952 7 25 15 17 13 17 7 | 56 64 59 52 58 52 54
XR25 |10147 64 --- --- --- 76 --- 70 | 73 --- --- --- 79 --- 69
XR26 |11794 35 84 70 --- 62 --- 35 | 31 35 48 --- 50 --- 34
XR27 | 5612 33 63 --- 33 46 --- 24 | 72 79 --- 50 72 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 1998 14 36 22 15 15 19 |T 49 52 53 52 53 45 49
WRMS | 1998 13 31 15 15 14 19 |NE 49 52 53 52 53 45 49
MEDI | 1411 11 20 15 15 13 15 |MD 49 52 51 49 52 47 51
Table 3.2382.3 GPS week: 2382 Day: 3 MJD: 60921
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1136 11 6 16 10 5 13 4 | 52 47 42 50 46 40 45
R03 | 2859 7 18 11 11 13 18 5 | 50 54 50 53 53 41 49
R04 | 1268 8 21 13 9 10 8 5 | 51 66 55 53 54 53 54
R05 | 1191 9 19 14 10 11 15 5 | 53 59 54 57 53 50 52
R07 | 1339 8 24 19 11 9 16 6 | 57 55 73 61 63 54 60
R08 | 1387 18 20 28 7 8 3 7 | 51 55 71 57 56 54 55
R09 | 2250 12 22 15 9 8 16 6 | 34 36 36 33 32 42 34
R11 | 1284 17 15 15 16 13 11 6 | 31 31 36 32 27 42 30
R12 | 1519 12 15 24 9 12 16 6 | 44 42 59 48 48 34 44
R14 | 1125 11 18 13 10 11 11 5 | 55 64 49 52 39 43 49
R15 | 1447 10 18 11 20 13 13 6 | 73 64 72 83 57 62 67
R16 | 1870 9 14 13 13 12 10 5 | 66 59 66 64 65 56 62
R17 | 1424 8 23 11 12 15 15 6 | 62 49 57 63 64 50 57
R18 | 1225 20 19 11 13 14 12 6 | 56 56 58 64 64 53 58
XR19 | 1468 18 15 16 --- 10 --- 8 | 26 34 38 --- 32 --- 30
R20 | 5355 55 131 46 43 29 43 22 | 46 58 45 52 40 45 33
R21 | 709 10 23 28 19 8 12 7 | 66 54 80 66 63 55 62
XR22 | 1163 17 14 15 16 12 --- 7 | 28 33 31 47 31 --- 31
R24 | 1158 11 21 11 12 16 22 7 | 59 61 49 58 57 49 54
XR25 |13328 86 --- --- --- 85 --- 86 | 96 --- --- --- 125 --- 91
XR26 |15186 37 55 66 --- 54 --- 30 | 36 48 30 --- 65 --- 44
XR27 |10209 45 74 --- 37 47 --- 28 | 47 103 --- 48 75 --- 59
------+-----------------------------------------+-------------------------------------
RMS | 1972 18 36 20 16 13 17 |T 51 53 52 54 54 48 50
WRMS | 1972 14 30 15 12 13 17 |NE 51 53 52 54 54 48 50
MEDI | 1387 11 19 15 12 12 13 |MD 51 55 50 53 54 50 52
Table 3.2382.4 GPS week: 2382 Day: 4 MJD: 60922
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1195 8 23 11 6 11 19 6 | 39 43 38 36 36 30 35
R03 | 2335 12 13 8 15 11 16 5 | 45 37 42 51 43 36 42
R04 | 1764 12 28 11 12 7 14 6 | 44 47 44 46 36 33 39
R05 | 1496 10 20 10 8 8 10 5 | 42 50 42 34 31 36 37
R07 | 1279 10 17 18 11 12 15 6 | 47 49 53 41 41 38 43
R08 | 967 15 36 8 12 24 8 8 | 36 41 42 37 53 46 41
R09 | 2527 14 16 14 13 18 11 6 | 36 36 42 31 46 35 36
R11 | 1766 19 29 18 17 12 23 8 | 32 45 31 37 35 24 31
R12 | 2118 10 13 19 18 12 15 6 | 51 47 39 59 47 39 45
R14 | 1491 13 17 16 15 11 11 6 | 54 62 65 56 58 48 56
R15 | 955 13 12 9 20 15 17 6 | 66 60 60 77 49 58 61
R16 | 1788 16 13 26 14 12 15 7 | 67 61 77 62 65 55 63
R17 | 1456 11 16 20 14 13 23 7 | 51 46 60 50 54 41 49
R18 | 1194 14 24 15 12 12 16 6 | 40 47 43 47 49 44 43
XR19 | 1567 16 13 17 --- 11 --- 8 | 22 27 26 --- 25 --- 22
R20 | 3396 50 123 31 39 30 50 20 | 57 63 54 54 57 58 50
R21 | 645 12 26 21 23 11 18 8 | 50 42 53 58 43 38 45
XR22 | 1075 14 11 17 18 12 --- 7 | 25 29 40 35 24 --- 26
R24 | 1151 14 17 18 17 13 17 7 | 43 42 40 42 36 26 35
XR25 |20628 107 --- --- --- 104 --- 106 | 63 --- --- --- 115 --- 52
XR26 |14481 41 61 39 --- 45 --- 26 | 40 38 48 --- 57 --- 50
XR27 |10220 57 74 --- 27 51 --- 30 | 72 106 --- 67 78 --- 74
------+-----------------------------------------+-------------------------------------
RMS | 1748 17 36 17 17 15 20 |T 46 48 46 48 49 40 44
WRMS | 1748 14 29 15 16 13 20 |NE 46 48 46 48 49 40 44
MEDI | 1496 14 17 17 15 12 16 |MD 44 46 42 47 46 38 43
Table 3.2382.5 GPS week: 2382 Day: 5 MJD: 60923
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1358 8 9 15 10 16 22 6 | 35 31 32 28 32 21 29
R03 | 1229 9 22 18 8 16 16 6 | 36 49 32 39 44 28 36
R04 | 905 7 12 8 9 13 8 4 | 47 44 43 45 49 48 45
R05 | 620 13 10 10 11 12 10 5 | 38 32 28 41 24 29 31
R07 | 1059 9 18 19 14 15 20 7 | 38 49 51 36 48 31 40
R08 | 944 9 23 7 19 29 11 7 | 36 33 33 37 49 36 36
R09 | 2369 12 13 12 16 22 9 6 | 38 41 39 37 38 42 37
R11 | 2472 15 18 11 27 15 15 7 | 23 30 31 28 32 24 25
R12 | 1296 9 17 13 19 14 24 7 | 45 38 30 45 39 44 38
R14 | 1158 10 16 12 12 10 8 5 | 45 45 49 42 40 45 42
R15 | 631 10 23 12 15 10 13 6 | 53 41 53 58 51 50 50
R16 | 1468 10 14 18 16 20 17 7 | 45 45 46 51 31 40 41
R17 | 1023 11 20 27 15 9 22 8 | 47 37 60 43 45 33 43
R18 | 991 9 16 13 15 15 18 6 | 39 43 44 43 38 29 38
XR19 | 1863 19 13 15 --- 9 --- 8 | 23 29 37 --- 28 --- 26
R20 | 2924 43 122 43 27 36 40 19 | 62 61 54 53 50 71 52
R21 | 739 13 22 10 25 8 22 7 | 58 49 55 64 56 44 53
XR22 | 1120 18 13 18 23 13 --- 8 | 26 33 33 42 34 --- 29
R24 | 1552 10 11 11 17 10 13 5 | 48 37 45 45 41 43 42
XR25 |24712 58 --- --- --- 85 --- 70 | 69 --- --- --- 144 --- 89
XR26 |13798 38 65 36 --- 50 --- 27 | 39 56 38 --- 44 --- 42
XR27 |11487 55 71 --- 27 51 --- 31 | 69 64 --- 64 74 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 1483 15 34 17 17 17 19 |T 43 42 41 44 46 38 42
WRMS | 1483 12 40 13 16 16 19 |NE 43 42 41 44 46 38 42
MEDI | 1229 10 17 13 16 15 16 |MD 39 41 39 43 41 40 40
Table 3.2382.6 GPS week: 2382 Day: 6 MJD: 60924
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1532 7 13 12 11 10 17 5 | 45 52 48 54 53 45 48
R03 | 1047 7 13 16 14 15 25 6 | 52 57 54 56 61 40 52
R04 | 762 8 10 13 10 18 13 5 | 60 57 52 55 62 55 57
R05 | 765 12 16 9 8 13 11 5 | 53 52 51 57 56 53 53
R07 | 1051 12 14 9 10 12 18 5 | 60 50 58 54 59 47 55
R08 | 1472 7 20 20 10 27 16 7 | 52 55 60 58 71 53 56
R09 | 1666 10 16 13 13 19 12 6 | 59 64 62 57 57 59 59
R11 | 2274 13 23 14 14 17 17 7 | 41 48 38 47 44 40 40
R12 | 985 10 18 7 12 11 11 5 | 66 66 61 70 69 57 64
R14 | 1481 7 16 14 10 15 11 5 | 68 70 65 69 66 60 66
R15 | 644 12 24 14 11 13 13 6 | 88 67 84 90 76 75 81
R16 | 929 11 17 17 13 13 9 6 | 76 73 87 77 67 65 74
R17 | 1207 13 23 18 12 9 23 7 | 70 54 75 67 64 50 64
R18 | 1265 12 13 26 15 14 22 7 | 56 62 72 63 56 53 58
XR19 | 2529 11 16 17 --- 23 --- 9 | 25 32 35 --- 25 --- 25
XR20 | 2672 51 105 33 --- 40 51 26 | 79 70 66 --- 63 71 63
R21 | 1201 8 30 19 12 13 23 8 | 76 70 86 77 75 57 73
XR22 | 980 14 16 15 16 15 --- 7 | 30 34 42 44 32 --- 34
R24 | 1757 13 21 13 13 8 11 6 | 75 64 63 75 66 69 69
XR25 |16851 58 --- --- --- 89 --- 72 | 82 --- --- --- 154 --- 106
XR26 |16107 26 --- 21 --- 47 --- 23 | 38 --- 47 --- 65 --- 47
XR27 | 8615 43 60 --- 24 57 --- 26 | 63 97 --- 64 94 --- 71
------+-----------------------------------------+-------------------------------------
RMS | 1319 10 19 15 12 15 17 |T 59 59 60 63 65 55 59
WRMS | 1319 10 18 14 12 14 17 |NE 59 59 60 63 65 55 59
MEDI | 1265 12 16 14 12 15 16 |MD 60 57 60 58 63 55 58
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