[IGSREPORT-30594] Wk 2380 IGLOS Final Orbits
acc
acc at igs.org
Fri Sep 5 05:57:56 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2380 (Aug 17, 2025 - Aug 23, 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 2.2380.
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:
igl2380[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2380 in the SP3 format.
igl23807.sum Combination Report for GPS Week 2380.
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 | 1.6 ns
1 | 2.0 ns
2 | 3.0 ns
3 | 5.4 ns
4 | 2.6 ns
5 | 2.9 ns
6 | 4.1 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
----+--------+---------------
1 | ESA | R20
2 | ESA | R20
3 | ESA | R20 R26
4 | ALL | R27
4 | 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 1.2380, 1a.2380).
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 2.2380.0-6)
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 3.2380.0-6).
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 2380 summary. (Aug 17, 2025 - Aug 23, 2025)
Table 1.2380.a GPS week : 2380 MJD: 60904.0-60910.0
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 5 -4 -4 37 .13 13 11 | 2535 -564 3695 10407
| 0 0 1 11 14 21 .04 | 2743 1416
esa n/a| -2 -1 5 24 -16 45 -.16 32 33 | 2502 -535 3555 9645
| 1 1 2 18 8 26 .03 | 1793 1588
gfz n/a| 0 0 -1 35 22 10 -.03 20 14 | 0 -591 3562 10273
| 1 0 3 19 10 24 .04 | 0 1320
grg n/a| 1 0 1 -45 -3 -39 .36 15 13 | 2245 -607 3888 8965
| 0 0 2 9 9 44 .04 | 2857 1376
iac n/a| 0 0 -2 23 15 -9 -.22 18 18 | 5977 -850 3632 11391
| 1 1 1 19 20 21 .05 | 2217 1109
jgx n/a| 0 0 -6 -19 -16 -33 -.21 16 16 | 2715 -643 3656 9087
| 0 0 2 20 6 27 .03 | 1631 1207
Table 1.2380.b GPS week : 2380 MJD: 60904.0-60910.0
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 | 5 6 7 6 6 6 7 |
R03 | 6 7 7 6 6 7 7 |
R04 | 5 5 6 6 6 7 8 |
R05 | 5 5 5 6 5 6 6 |
R07 | 8 6 6 7 5 7 7 |
R08 | 6 9 7 7 7 7 9 |
R09 | 6 6 5 8 6 6 7 |
R11 | 9 7 10 7 11 9 6 |
R12 | 5 6 6 7 6 6 8 |
R14 | 6 4 5 6 5 5 6 |
R15 | 6 5 5 5 6 6 6 |
R16 | 7 7 7 6 7 6 8 |
R17 | 6 6 6 6 8 6 7 |
R18 | 7 5 6 6 7 13 14 |
R19 | 9 7 9 9 11 10 9 |
R20 | 20 20 16 17 15 21 21 |
R21 | 6 6 6 7 6 7 7 |
R22 | 8 7 8 7 8 9 8 |
R24 | 6 6 6 8 6 9 9 |
R25 | 76 74 60 54 67 93 51 |
R26 | 29 32 32 30 31 30 31 |
R27 | 29 33 78 46 --- 24 25 |
Table 1.2380.c GPS week : 2380 MJD: 60904.0-60910.0
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 2380 0 | -42 125 70 1310 417 -4547 84.5 2149 2149 | 1631 0
brd 2380 1 | 100 35 136 481 2563 2007 78.7 1972 1972 | 1966 0
brd 2380 2 | -18 22 -66 -28 -1044 7811 77.7 1794 1794 | 2980 0
brd 2380 3 | -81 79 42 -301 -31 8749 79.2 1833 1833 | 5359 0
brd 2380 4 | 71 42 3 1835 99 7349 76.4 1883 1883 | 2604 0
brd 2380 5 | 88 9 39 800 936 7412 80.4 1721 1721 | 2936 0
brd 2380 6 | 37 -37 -78 -1214 -367 6561 78.9 1841 1841 | 4148 0
-------------+------------------------------------------------------------+----------------
brd 2380 mean| 22 39 21 411 367 5048 79.4 1884 1884 | 3089 0
brd 2380 sdev| 70 52 75 1027 1148 4757 2.6 139 139 | 1286 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 2.2380.0 GPS week: 2380 Day: 0 MJD: 60904
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 3 1 -6 31 .16 10 9 | -1531 -2286 4435 14503
esa n/a| -4 -1 9 15 -12 35 -.16 30 38 | 1598 -2595 3454 9070
gfz n/a| 2 1 -1 0 28 -4 -.01 24 15 | 0 -2239 3442 10060
grg n/a| 2 0 0 -45 0 29 .33 15 12 | -3898 -2015 5608 10988
iac n/a| 0 0 -2 17 -1 -18 -.27 16 14 | 2477 -2763 3863 11458
jgx n/a| 1 0 -5 7 -15 -54 -.24 16 16 | 1567 -1519 3496 9638
Table 2.2380.1 GPS week: 2380 Day: 1 MJD: 60905
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 5 -25 -12 39 .14 11 11 | 1364 -2013 3582 8084
esa n/a| -3 0 6 -3 -7 36 -.15 32 25 | 777 -1851 3588 7987
gfz n/a| 0 0 1 45 12 -22 -.01 22 14 | 0 -2112 3579 8616
grg n/a| 0 0 1 -38 -2 -20 .32 15 11 | 2787 -2154 3626 7794
iac n/a| 1 0 -4 -2 28 29 -.16 15 13 | 4384 -823 3560 9412
jgx n/a| 0 0 -6 1 -18 -58 -.23 15 15 | 1830 -2226 3705 8121
Table 2.2380.2 GPS week: 2380 Day: 2 MJD: 60906
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 -22 40 .18 12 13 | 980 277 4018 10517
esa n/a| -1 -1 6 15 -25 4 -.20 31 24 | 840 684 4014 10571
gfz n/a| 0 0 0 39 13 44 -.04 16 13 | 0 238 4015 11183
grg n/a| 1 0 1 -56 -9 -85 .38 17 14 | 2997 -619 4014 9350
iac n/a| 0 0 -2 27 36 -37 -.16 15 14 | 5418 -198 4000 11572
jgx n/a| 0 0 -6 -39 -9 -1 -.18 15 15 | 1092 -855 4127 9734
Table 2.2380.3 GPS week: 2380 Day: 3 MJD: 60907
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 6 5 2 66 .15 12 10 | 5004 45 3426 10545
esa n/a| -3 -4 6 28 -18 30 -.16 34 42 | 5074 546 3407 10639
gfz n/a| 1 0 0 29 29 6 -.11 17 14 | 0 -94 3430 11212
grg n/a| 1 1 1 -58 0 -58 .42 15 14 | 4650 1068 3252 8530
iac n/a| 0 1 -5 34 -12 -6 -.23 17 17 | 8611 107 3407 11787
jgx n/a| 0 1 -10 -15 -26 -20 -.18 16 16 | 3734 1303 3335 9154
Table 2.2380.4 GPS week: 2380 Day: 4 MJD: 60908
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 7 -15 48 .11 12 12 | 1910 -1311 3563 9587
esa n/a| -2 -1 2 52 -15 72 -.10 34 40 | 2001 -2103 3569 9469
gfz n/a| 1 0 0 28 39 -4 -.01 20 15 | 0 -1068 3555 10303
grg n/a| 1 0 3 -48 1 -50 .37 15 13 | 2815 -1262 3692 7942
iac n/a| 0 1 -3 12 5 -1 -.21 13 13 | 5516 -1545 3561 11222
jgx n/a| 0 1 -7 -16 -7 -61 -.20 16 16 | 1896 -1305 3720 8005
Table 2.2380.5 GPS week: 2380 Day: 5 MJD: 60909
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 5 -11 19 42 .07 15 12 | 3268 1741 4029 9805
esa n/a| -3 0 3 40 -7 64 -.15 30 38 | 2310 1317 4034 9542
gfz n/a| 0 0 -8 59 10 39 -.05 19 16 | 0 1460 4063 10412
grg n/a| 1 2 4 -38 -21 -91 .31 14 11 | 2060 1330 4103 9079
iac n/a| 1 0 0 13 43 -4 -.27 25 28 | 6942 480 4123 12496
jgx n/a| 0 1 -6 -23 -16 6 -.21 18 18 | 3118 401 4178 9583
Table 2.2380.6 GPS week: 2380 Day: 6 MJD: 60910
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 6 -10 3 -4 .15 17 13 | 6756 -402 2813 9808
esa n/a| -1 0 4 27 -29 77 -.16 33 27 | 4919 253 2820 10241
gfz n/a| -2 1 -3 49 25 12 -.00 19 14 | 0 -328 2853 10127
grg n/a| 1 0 -2 -34 8 0 .40 16 12 | 4309 -598 2922 9077
iac n/a| 2 -1 -2 59 10 -29 -.25 25 29 | 8493 -1214 2914 11796
jgx n/a| 0 0 -1 -49 -21 -43 -.24 16 16 | 5774 -301 3031 9375
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 3.2380.0 GPS week: 2380 Day: 0 MJD: 60904
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2113 10 17 11 9 8 13 5 | 68 61 71 67 69 60 66
R03M | 1306 3 18 12 10 14 16 5 | 73 63 72 73 81 64 71
R04 | 979 6 13 8 12 12 10 4 | 68 62 69 77 75 64 69
R05 | 1119 6 17 15 9 16 8 5 | 62 53 58 67 67 55 61
R07 | 2474 11 24 27 15 19 19 8 | 80 62 87 85 71 65 75
R08M | 1170 8 20 26 10 8 7 5 | 72 65 87 79 79 73 75
R09M | 4766 13 19 10 13 12 11 5 | 33 32 36 36 33 32 32
R11M | 1605 16 35 15 18 14 20 8 | 21 35 28 31 27 24 22
R12M | 1337 8 19 9 9 9 9 4 | 71 54 67 72 69 45 69
R14 | 1207 8 20 11 13 17 9 5 | 52 68 58 60 51 56 55
R15 | 1854 9 17 17 6 17 11 5 | 85 77 85 86 89 76 83
R16 | 1477 8 13 22 21 13 12 6 | 75 75 83 63 76 69 72
R17E | 1013 7 18 21 16 12 8 6 | 62 57 58 59 64 61 60
R18E | 1758 11 23 16 13 11 19 6 | 37 45 41 43 36 40 38
XR19E | 1431 12 16 16 --- 16 --- 8 | 28 33 40 --- 32 --- 30
R20E | 4318 16 89 73 34 36 43 20 | 87 82 115 97 82 96 88
R21E | 1344 8 23 13 16 16 14 6 | 39 43 46 48 34 34 39
XR22E | 1358 13 22 11 18 16 --- 8 | 20 31 29 36 22 --- 23
R24E | 1965 11 29 14 10 13 8 6 | 68 87 77 72 71 70 71
XR25E |16724 56 --- --- --- 101 --- 75 | 93 --- --- --- 37 --- 63
XR26M |10973 31 77 49 --- 64 --- 29 | 19 99 16 --- 77 --- 39
XR27 | 4869 27 --- --- 29 66 --- 29 | 571 --- --- 567 569 --- 570
------+-----------------------------------------+-------------------------------------
RMS | 2148 10 30 24 15 16 16 |T 81 59 61 90 82 57 80
WRMS | 2148 9 38 15 12 14 16 |NE 132 65 73 134 133 63 131
MEDI | 1477 10 19 15 13 14 11 |MD 68 61 58 67 69 61 63
Table 3.2380.1 GPS week: 2380 Day: 1 MJD: 60905
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1771 13 15 10 14 12 10 5 | 43 37 36 35 40 41 38
R03M | 2459 8 21 10 10 16 18 6 | 44 43 42 46 44 42 42
R04 | 1554 9 16 8 9 16 9 5 | 43 48 42 48 52 40 44
R05 | 1146 7 13 11 10 11 9 4 | 41 40 47 53 42 43 43
R07 | 2056 12 25 8 13 13 10 6 | 50 43 40 57 46 45 46
R08M | 1058 11 22 34 16 14 15 8 | 44 38 64 61 44 40 47
R09M | 4509 12 22 16 11 11 14 6 | 21 21 24 21 23 24 20
R11M | 1864 15 32 7 16 11 15 7 | 15 28 19 18 18 21 15
R12M | 1137 10 19 18 11 12 7 5 | 52 33 40 49 49 32 45
R14 | 1848 9 16 9 8 10 5 4 | 33 45 39 41 28 37 35
R15 | 1073 11 13 12 8 9 7 4 | 58 59 62 58 54 57 57
R16 | 1892 12 16 19 15 16 11 6 | 58 57 71 50 61 51 56
R17E | 1453 9 21 18 15 15 8 6 | 72 65 72 74 75 65 69
R18E | 1308 8 21 15 8 8 10 5 | 25 34 23 29 23 25 23
XR19E | 1106 11 16 14 --- 11 --- 7 | 36 38 40 --- 38 --- 37
R20E | 2932 16 105 67 36 32 41 20 | 80 80 104 91 88 102 86
R21E | 1030 10 23 17 11 11 9 5 | 41 45 43 42 40 34 39
XR22E | 1898 16 15 10 15 12 --- 7 | 24 30 31 36 26 --- 26
R24E | 1041 11 16 14 12 16 9 5 | 57 59 61 63 57 57 57
XR25E |11060 65 --- --- --- 84 --- 74 | 81 --- --- --- 52 --- 57
XR26M |11032 38 74 50 --- 63 --- 31 | 27 67 32 --- 58 --- 38
XR27 | 5908 40 --- --- 26 67 --- 33 | 465 --- --- 673 441 --- 456
------+-----------------------------------------+-------------------------------------
RMS | 1971 11 32 22 15 15 15 |T 64 45 46 81 63 44 62
WRMS | 1971 11 25 14 11 13 15 |NE 98 47 48 126 95 44 96
MEDI | 1771 11 19 14 12 12 10 |MD 43 43 40 49 44 41 43
Table 3.2380.2 GPS week: 2380 Day: 2 MJD: 60906
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1238 12 17 23 15 7 18 7 | 61 48 60 49 54 53 54
R03M | 1856 8 21 16 14 22 10 7 | 58 50 48 58 65 53 55
R04 | 1016 7 15 8 11 18 17 6 | 53 60 57 54 60 48 54
R05 | 1498 9 15 10 9 11 9 4 | 46 55 53 53 49 45 49
R07 | 1938 13 28 8 11 10 12 6 | 60 46 54 59 48 47 52
R08M | 1006 10 30 8 18 17 10 7 | 55 43 58 67 65 54 57
R09M | 2903 11 12 14 9 7 11 5 | 24 25 30 28 25 29 25
R11M | 3023 29 21 15 38 11 12 10 | 20 40 22 43 23 22 17
R12M | 1081 10 23 13 13 11 14 6 | 59 43 71 58 57 36 59
R14 | 2452 8 12 11 12 11 8 4 | 36 44 42 38 41 38 38
R15 | 1257 12 12 12 10 9 14 5 | 65 67 65 66 54 51 60
R16 | 1225 8 16 14 16 19 14 6 | 65 70 66 55 72 51 62
R17E | 1808 9 15 13 14 19 10 6 | 59 62 58 62 48 56 56
R18E | 1122 11 22 11 14 11 9 5 | 31 36 31 32 25 32 28
XR19E | 1326 14 15 21 --- 12 --- 9 | 17 25 35 --- 24 --- 21
R20E | 2256 17 102 41 23 32 36 15 | 48 40 69 52 60 58 50
R21E | 1318 11 17 11 14 13 11 5 | 45 38 41 44 43 36 39
XR22E | 1983 17 18 16 15 12 --- 7 | 20 24 31 32 24 --- 23
R24E | 1581 9 16 13 18 14 12 6 | 32 38 34 39 33 29 31
XR25E |15240 54 --- --- --- 66 --- 60 | 86 --- --- --- 67 --- 67
XR26M |10631 40 68 52 --- 61 --- 31 | 29 75 28 --- 70 --- 40
XR27 |16031 71 --- --- --- 86 --- 78 | 514 --- --- --- 536 --- 524
------+-----------------------------------------+-------------------------------------
RMS | 1794 12 31 16 17 15 15 |T 67 46 47 49 70 43 66
WRMS | 1794 13 24 13 14 14 15 |NE 112 55 56 53 114 47 111
MEDI | 1581 11 17 13 14 12 12 |MD 48 43 48 52 49 47 50
Table 3.2380.3 GPS week: 2380 Day: 3 MJD: 60907
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1823 8 15 9 16 13 19 6 | 61 56 61 73 69 54 61
R03M | 1390 9 13 15 10 16 18 6 | 63 62 61 63 71 54 61
R04 | 1198 10 22 14 5 16 9 5 | 56 51 49 53 53 51 51
R05 | 1686 8 20 8 7 15 16 5 | 51 53 46 54 57 45 49
R07 | 2531 6 23 21 17 15 6 6 | 58 56 76 55 68 60 61
R08M | 1230 12 30 8 15 22 8 7 | 61 62 70 68 77 62 65
R09M | 1301 13 20 14 14 27 10 7 | 19 18 24 15 33 16 17
R11M | 3879 18 14 11 14 14 10 6 | 26 27 23 24 25 25 22
R12M | 1150 7 18 15 9 8 23 6 | 48 45 54 50 45 30 45
R14 | 1842 7 16 11 9 22 14 6 | 39 47 47 42 48 30 41
R15 | 1131 8 9 13 17 6 7 5 | 54 55 56 67 56 52 56
R16 | 899 10 17 15 12 13 14 5 | 60 65 54 49 59 43 53
R17E | 1365 8 17 14 17 12 11 6 | 63 60 61 68 66 67 64
R18E | 1321 7 19 14 13 18 15 6 | 34 41 31 40 33 36 33
XR19E | 1488 14 15 16 --- 15 --- 8 | 25 28 32 --- 26 --- 25
R20E | 2764 25 115 44 28 29 41 17 | 47 34 65 47 40 54 41
R21E | 1574 10 30 12 14 11 10 6 | 37 57 46 47 38 40 41
XR22E | 2632 14 17 13 17 12 --- 7 | 22 28 29 33 24 --- 23
R24E | 1531 13 23 20 17 16 13 7 | 43 38 51 55 45 37 43
XR25E |24878 39 --- --- --- 73 --- 54 | 72 --- --- --- 55 --- 55
XR26M |11379 21 92 35 --- 71 --- 30 | 25 88 23 --- 67 --- 24
XR27 |14488 34 --- --- --- 61 --- 45 | 223 --- --- --- 240 --- 225
------+-----------------------------------------+-------------------------------------
RMS | 1832 12 34 17 15 17 16 |T 53 48 47 50 58 44 52
WRMS | 1832 10 42 14 14 17 16 |NE 75 54 55 56 81 47 74
MEDI | 1531 10 18 14 14 15 13 |MD 48 51 49 50 53 45 45
Table 3.2380.4 GPS week: 2380 Day: 4 MJD: 60908
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1969 11 20 13 13 13 10 5 | 55 54 68 71 71 66 64
R03M | 1387 8 15 18 12 13 19 6 | 58 57 60 65 61 56 59
R04 | 877 10 19 15 12 8 20 6 | 61 54 64 67 51 45 57
R05 | 1399 9 16 13 7 7 8 4 | 53 51 43 55 52 51 50
R07 | 2730 10 23 12 12 8 8 5 | 54 53 55 47 52 53 51
R08M | 1248 10 18 19 13 19 19 7 | 57 60 74 61 75 54 63
R09M | 1183 12 28 14 10 10 14 6 | 21 30 30 22 28 23 22
R11M | 3647 22 48 15 28 12 22 11 | 19 55 16 45 22 19 16
R12M | 1956 16 19 13 9 13 10 6 | 62 57 72 70 72 49 67
R14 | 1239 6 15 11 9 12 13 5 | 46 39 48 46 44 34 42
R15 | 884 9 24 16 13 8 10 5 | 60 60 76 70 62 57 63
R16 | 921 14 18 25 10 18 11 7 | 59 60 71 57 48 60 56
R17E | 1415 8 21 27 16 18 12 7 | 41 42 59 48 44 38 42
R18E | 1467 10 17 20 17 10 18 6 | 35 38 39 42 33 33 34
XR19E | 1371 22 23 17 --- 15 --- 11 | 26 28 27 --- 25 --- 21
R20E | 3710 19 106 46 27 22 32 14 | 55 50 77 53 45 53 52
R21E | 1212 9 26 12 13 10 13 6 | 43 41 38 45 37 40 39
XR22E | 3371 15 23 12 13 12 --- 7 | 16 27 26 34 25 --- 21
R24E | 1281 13 18 15 15 9 12 6 | 52 50 52 57 55 48 51
XR25E |17385 64 --- --- --- 68 --- 66 | 66 --- --- --- 49 --- 42
XR26M |10329 44 73 49 --- 53 --- 30 | 26 77 31 --- 58 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1883 12 34 20 15 13 16 |T 68 49 51 74 71 45 68
WRMS | 1883 12 40 15 13 13 16 |NE 117 53 60 109 118 52 117
MEDI | 1399 11 20 15 13 12 13 |MD 53 51 52 55 49 49 50
Table 3.2380.5 GPS week: 2380 Day: 5 MJD: 60909
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2481 7 12 12 10 21 21 6 | 47 47 54 57 60 37 50
R03M | 1498 6 23 15 15 24 14 7 | 62 55 70 56 70 59 61
R04 | 1593 8 14 21 6 8 21 6 | 54 46 65 55 53 48 53
R05 | 813 7 15 18 9 8 12 5 | 45 46 58 47 37 36 44
R07 | 1584 13 26 14 9 21 15 7 | 51 44 51 51 34 41 45
R08M | 1269 12 16 18 8 22 16 6 | 52 47 56 51 61 49 52
R09M | 1359 15 15 13 10 15 11 6 | 27 38 39 28 35 29 30
R11M | 2604 21 23 14 22 22 12 8 | 20 47 28 43 33 24 28
R12M | 1851 8 9 11 12 25 14 6 | 68 56 61 73 83 51 68
R14 | 1900 6 18 11 9 15 11 5 | 46 47 33 40 44 37 40
R15 | 1182 11 18 12 12 14 11 5 | 58 55 55 65 62 44 56
R16 | 1131 15 19 15 10 9 10 6 | 54 54 47 60 51 52 52
R17E | 1195 7 21 14 13 15 12 6 | 56 55 49 58 49 48 51
R18E | 1383 19 19 18 21 63 26 13 | 38 38 33 48 66 32 35
XR19E | 1113 15 21 16 --- 15 --- 9 | 20 29 32 --- 26 --- 23
R20E | 3086 36 98 52 25 36 40 21 | 70 55 90 70 73 78 68
R21E | 1165 7 24 19 14 13 17 7 | 28 29 41 34 29 24 29
XR22E | 2376 14 17 23 16 16 --- 8 | 12 25 30 32 21 --- 19
R24E | 1432 16 26 14 19 27 13 8 | 69 86 72 76 67 71 71
XR25E |17916 64 --- --- --- 135 --- 93 | 90 --- --- --- 72 --- 75
XR26M |11388 39 83 31 --- 62 --- 30 | 23 55 22 --- 38 --- 19
XR27 | 9735 27 59 --- 26 62 --- 23 | 369 20 --- 279 379 --- 378
------+-----------------------------------------+-------------------------------------
RMS | 1721 15 30 19 14 25 18 |T 61 46 49 64 65 44 61
WRMS | 1721 12 38 16 11 28 18 |NE 90 44 51 81 90 42 89
MEDI | 1498 13 19 15 12 21 14 |MD 51 47 49 55 51 44 50
Table 3.2380.6 GPS week: 2380 Day: 6 MJD: 60910
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 3120 9 24 16 11 19 15 6 | 74 75 85 83 91 71 78
R03M | 2477 6 22 8 12 25 16 6 | 70 69 70 68 85 66 70
R04 | 1502 14 22 18 15 19 15 7 | 77 68 70 75 78 63 71
R05 | 872 6 12 17 11 12 15 5 | 64 65 76 66 65 57 65
R07 | 1351 18 21 8 17 16 10 7 | 74 52 65 67 54 57 62
R08M | 1239 16 43 16 16 15 19 9 | 75 61 76 85 74 76 75
R09M | 1569 17 29 16 10 14 11 7 | 32 34 34 31 33 30 30
R11M | 1393 16 12 13 12 16 12 6 | 20 24 26 24 25 25 21
XR12M |16741 14 --- 15 7 18 --- 8 | 85 --- 86 85 95 --- 87
R14 | 2781 7 20 9 11 14 14 5 | 60 60 54 56 63 50 56
R15 | 1854 11 18 12 14 12 13 6 | 79 70 78 77 78 67 74
R16 | 1613 16 20 20 15 19 10 7 | 78 74 65 66 73 66 68
R17E | 1062 14 15 13 17 13 12 6 | 49 54 52 57 48 47 49
R18E | 1135 24 21 21 15 69 20 14 | 48 48 48 55 59 52 48
XR19E | 3233 12 22 13 --- 15 --- 8 | 32 39 38 --- 37 --- 35
R20E | 2877 41 95 49 31 35 31 20 | 107 94 113 110 109 111 104
R21E | 1312 8 19 20 11 11 17 6 | 32 28 40 39 25 23 29
XR22E | 1718 15 15 10 15 19 --- 7 | 20 28 32 36 25 --- 25
R24E | 1161 15 32 16 21 19 15 8 | 131 111 128 135 130 125 127
XR25E |14414 39 --- --- --- 63 --- 50 | 69 --- --- --- 51 --- 45
XR26M | 9268 44 92 33 --- 56 --- 31 | 30 101 40 --- 78 --- 46
XR27 |13213 27 57 --- 33 61 --- 24 | 488 19 --- 364 509 --- 498
------+-----------------------------------------+-------------------------------------
RMS | 1840 17 33 19 16 25 16 |T 81 58 63 83 85 61 80
WRMS | 1840 13 27 14 12 29 16 |NE 124 60 70 106 126 61 121
MEDI | 1613 15 21 16 15 18 15 |MD 69 60 65 67 65 57 62
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