[IGSREPORT-30554] Wk 2376 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 8 06:23:01 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2376 (Jul 20, 2025 - Jul 26, 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 2.2376.
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:
igl2376[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2376 in the SP3 format.
igl23767.sum Combination Report for GPS Week 2376.
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 | 6.2 ns
1 | 9.3 ns
2 | 11.3 ns
3 | 8.6 ns
4 | 6.2 ns
5 | 6.1 ns
6 | 5.8 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 | 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 1.2376, 1a.2376).
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 2.2376.0-6)
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 3.2376.0-6).
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 2376 summary. (Jul 20, 2025 - Jul 26, 2025)
Table 1.2376.a GPS week : 2376 MJD: 60876.0-60882.0
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 2 1 -21 24 .13 15 14 | 1386 -1409 3913 16680
| 0 0 1 10 5 16 .04 | 2125 1012
esa n/a| -3 -2 7 26 2 18 -.16 32 35 | -798 -915 3915 16523
| 1 1 1 21 13 30 .09 | 3041 1057
gfz n/a| 0 0 -3 25 11 10 -.11 20 14 | 0 -1544 3956 16144
| 1 0 1 15 9 28 .03 | 0 1230
grg n/a| 2 0 0 -45 41 -17 .35 23 17 | 7566 -766 3575 10705
| 2 1 1 9 14 35 .05 | 1776 1313
jgx n/a| 0 0 -5 -13 -23 -25 -.19 18 18 | 3985 -982 3655 10874
| 0 0 2 16 17 26 .04 | 1488 1345
Table 1.2376.b GPS week : 2376 MJD: 60876.0-60882.0
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 | 8 8 8 7 7 7 9 |
R03 | 9 8 7 8 8 8 7 |
R04 | 8 10 8 8 8 8 8 |
R05 | 7 8 7 7 7 6 6 |
R07 | 9 9 9 9 11 8 8 |
R08 | 10 11 11 10 8 12 6 |
R09 | 8 7 7 6 7 6 6 |
R11 | 8 8 9 6 11 7 10 |
R12 | 8 7 7 9 7 6 6 |
R14 | 6 10 7 7 5 6 5 |
R15 | 8 6 7 8 7 5 7 |
R16 | 9 10 9 7 7 8 8 |
R17 | 8 8 9 9 8 8 8 |
R18 | 9 7 7 7 8 7 6 |
R19 | 12 10 11 11 10 8 10 |
R20 | 33 29 23 30 26 31 24 |
R21 | 9 10 8 7 8 9 9 |
R22 | 10 10 10 8 10 10 8 |
R24 | 10 8 10 9 10 9 10 |
R25 | 0 0 0 0 0 0 0 |
R26 | 34 30 36 28 31 34 34 |
R27 | 24 26 27 27 31 32 35 |
Table 1.2376.c GPS week : 2376 MJD: 60876.0-60882.0
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 2376 0 | 14 -90 83 238 691 17300 84.9 1966 1966 | 6219 0
brd 2376 1 | 85 -47 41 -741 999 9166 86.1 1983 1983 | 9303 0
brd 2376 2 | 41 125 117 -1346 303 10780 79.7 1974 1974 | 11332 0
brd 2376 3 | -156 31 155 -8 -2242 9767 78.3 2192 2192 | 8647 0
brd 2376 4 | 26 -22 108 -267 -482 8382 81.8 2145 2145 | 6165 0
brd 2376 5 | 87 -5 199 322 -111 6599 81.2 1503 1503 | 6074 0
brd 2376 6 | 48 -19 61 838 -671 11680 80.5 1566 1566 | 5787 0
-------------+------------------------------------------------------------+----------------
brd 2376 mean| 20 -4 109 -137 -215 10524 81.8 1904 1904 | 7646 0
brd 2376 sdev| 82 68 54 726 1077 3408 2.8 268 268 | 2140 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 2.2376.0 GPS week: 2376 Day: 0 MJD: 60876
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 2 0 9 -26 33 .19 18 16 | 1286 -2788 3573 13724
esa n/a| -1 -2 7 61 23 -15 -.31 31 26 | -3760 -2095 3582 14000
gfz n/a| 1 0 -4 26 -1 19 -.14 22 16 | 0 -3756 3471 13358
grg n/a| 0 0 0 -58 44 13 .44 26 17 | 8082 -3086 3598 13726
jgx n/a| 0 0 -3 -4 -33 -7 -.12 18 18 | 2258 -3668 3562 13756
Table 2.2376.1 GPS week: 2376 Day: 1 MJD: 60877
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 2 -6 -19 5 .16 15 15 | -1153 -2056 3973 17903
esa n/a| -1 -3 6 42 17 7 -.19 34 45 | -3889 -918 3967 17418
gfz n/a| 3 1 -1 40 16 51 -.15 20 15 | 0 -2013 3954 17671
grg n/a| 0 -1 3 -37 35 -47 .33 23 18 | 9211 -233 3243 13749
jgx n/a| 0 0 -6 -34 -10 0 -.17 17 17 | 1654 -473 3323 14167
Table 2.2376.2 GPS week: 2376 Day: 2 MJD: 60878
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 -2 -25 32 .12 16 15 | -464 -519 4759 24854
esa n/a| -3 0 8 6 0 66 -.08 37 48 | -3049 349 4752 24803
gfz n/a| 0 1 -5 24 17 -8 -.08 18 14 | 0 -743 4855 24158
grg n/a| 2 0 -1 -41 50 8 .29 23 20 | 10114 1296 4106 12221
jgx n/a| 1 0 -3 -23 -39 -77 -.22 15 15 | 3999 545 3988 12941
Table 2.2376.3 GPS week: 2376 Day: 3 MJD: 60879
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 2 5 -16 6 .09 13 13 | -371 -2295 4196 31916
esa n/a| -2 -3 5 9 -2 36 -.21 32 30 | -2049 -2544 4197 31868
gfz n/a| -1 0 -1 10 19 -13 -.12 19 11 | 0 -2384 4283 31471
grg n/a| 4 0 1 -34 20 -32 .34 21 18 | 8100 -487 3462 8875
jgx n/a| 0 2 -6 2 -48 -34 -.20 22 22 | 5364 -452 3641 8993
Table 2.2376.4 GPS week: 2376 Day: 4 MJD: 60880
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 5 -28 46 .07 15 14 | 4130 -1507 3857 10099
esa n/a| -4 -3 7 9 -2 -7 -.19 30 26 | 2417 -451 3836 9722
gfz n/a| 0 0 -2 0 -3 -14 -.09 19 12 | 0 -969 3946 9758
grg n/a| 3 1 1 -45 57 -27 .31 20 17 | 5973 -1200 3925 10019
jgx n/a| 0 0 -8 3 -2 -6 -.18 18 18 | 4614 -1400 4108 10086
Table 2.2376.5 GPS week: 2376 Day: 5 MJD: 60881
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 1 -14 -21 32 .13 13 11 | 2645 -303 2986 9028
esa n/a| -3 -2 8 38 -15 -2 -.12 30 23 | 2623 -9 2995 8873
gfz n/a| 0 0 -2 34 12 46 -.11 20 14 | 0 -434 3054 8250
grg n/a| 2 0 -2 -58 54 -66 .39 25 16 | 5735 -546 3025 8189
jgx n/a| 0 0 -4 -3 -22 -17 -.22 20 20 | 4503 -235 3110 8133
Table 2.2376.6 GPS week: 2376 Day: 6 MJD: 60882
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 15 -14 12 .15 14 12 | 3629 -397 4048 9237
esa n/a| -5 -3 5 16 -2 41 -.04 34 44 | 2119 -739 4076 8978
gfz n/a| 0 0 -4 44 18 -6 -.07 17 13 | 0 -511 4134 8346
grg n/a| 3 1 1 -44 27 29 .38 20 15 | 5753 -1106 3666 8160
jgx n/a| 0 0 -3 -34 -6 -37 -.21 17 17 | 5508 -1192 3858 8045
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 3.2376.0 GPS week: 2376 Day: 0 MJD: 60876
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1317 16 16 19 18 12 8 | 75 69 68 68 60 67
R03 | 988 16 13 20 14 18 8 | 77 57 72 68 52 64
R04 | 1404 13 17 12 15 17 7 | 72 63 65 72 52 63
R05 | 1697 11 13 10 18 14 6 | 62 53 61 63 45 55
R07 | 1746 23 18 7 21 13 8 | 59 40 45 48 33 43
R08M | 1552 20 13 13 20 22 9 | 58 39 48 47 30 42
R09M | 2572 15 24 16 16 10 8 | 101 106 106 99 103 102
R11M | 2665 14 28 15 17 9 8 | 40 39 39 45 35 37
R12M | 1186 14 17 20 17 14 8 | 35 35 27 30 24 27
R14M | 1571 12 11 11 14 8 5 | 40 38 43 41 43 40
R15M | 1792 14 15 25 10 10 8 | 49 51 43 41 40 42
R16M | 1867 17 14 29 16 12 9 | 51 60 58 48 52 51
R17E | 2501 13 18 21 18 12 8 | 126 122 123 134 127 125
R18E | 1678 10 25 27 13 13 9 | 47 49 50 52 42 44
XR19E | 1279 15 16 17 --- --- 11 | 16 29 29 --- --- 21
R20E | 3359 44 103 55 81 52 33 | 73 67 92 92 65 68
R21E | 1929 12 29 13 25 10 9 | 122 124 123 124 123 122
XR22E | 2365 17 18 14 19 --- 10 | 42 44 31 40 --- 36
R24E | 2072 14 18 22 30 10 9 | 140 137 138 154 136 139
XR25E |13856 4 --- --- --- --- 0 | 109 --- --- --- --- 108
XR26M | 5546 30 78 34 --- --- 34 | 44 108 32 --- --- 50
XR27 | 6240 31 51 --- 15 --- 24 | 40 90 --- 55 --- 53
------+------------------------------------+--------------------------------
RMS | 1965 18 31 22 26 18 |T 67 67 64 69 62 63
WRMS | 1965 16 26 16 17 18 |NE 64 62 62 62 48 57
MEDI | 1792 14 18 17 17 12 |MD 58 57 50 55 52 51
Table 3.2376.1 GPS week: 2376 Day: 1 MJD: 60877
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1446 13 24 10 22 12 8 | 43 51 40 41 37 39
R03 | 1138 19 17 9 21 14 8 | 50 49 38 48 38 42
R04 | 1567 15 30 17 16 19 9 | 53 49 53 57 37 47
R05 | 1796 7 18 14 18 16 7 | 44 38 48 52 33 41
R07 | 1371 14 19 17 24 13 8 | 40 39 39 33 29 33
R08M | 1503 24 18 12 28 20 10 | 43 34 35 32 27 30
R09M | 1835 13 11 10 16 13 6 | 91 85 89 91 90 89
R11M | 4536 12 12 18 18 13 7 | 36 51 53 48 35 41
R12M | 1313 8 21 13 11 14 6 | 32 39 39 30 30 31
R14M | 1184 13 40 17 15 9 9 | 28 50 35 27 28 29
R15M | 1457 9 13 16 11 9 6 | 31 31 34 34 35 31
R16M | 1223 17 17 28 14 14 9 | 32 34 36 26 35 28
R17E | 2781 12 26 16 20 13 8 | 106 105 106 115 99 104
R18E | 1314 8 23 12 18 11 7 | 41 38 39 49 37 39
XR19E | 1242 12 13 15 --- --- 9 | 20 27 29 --- --- 22
R20E | 2846 29 107 56 58 47 29 | 54 46 77 64 47 49
R21E | 1296 17 36 15 22 9 9 | 87 77 92 95 88 87
XR22E | 2870 16 31 8 15 --- 10 | 23 26 27 34 --- 24
R24E | 1919 12 18 18 24 11 8 | 98 100 107 96 97 98
XR25E |17034 2 --- --- --- --- 0 | 96 --- --- --- --- 97
XR26M | 6826 28 81 19 --- --- 30 | 40 74 44 --- --- 44
XR27 | 7644 28 61 --- 19 --- 25 | 24 59 --- 37 --- 32
------+------------------------------------+--------------------------------
RMS | 1982 15 34 20 23 17 |T 50 52 53 53 48 48
WRMS | 1982 15 45 15 18 17 |NE 42 47 43 44 34 39
MEDI | 1503 13 21 15 18 13 |MD 41 49 39 48 37 39
Table 3.2376.2 GPS week: 2376 Day: 2 MJD: 60878
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1373 15 12 10 25 13 7 | 47 45 46 45 32 40
R03 | 1359 14 18 11 15 9 6 | 58 39 53 52 48 49
R04 | 1405 12 16 8 19 17 7 | 59 53 55 62 48 54
R05 | 2320 10 17 15 16 15 7 | 52 48 59 53 37 48
R07 | 976 20 23 11 16 14 8 | 48 44 39 40 31 38
R08M | 1292 26 18 16 27 22 11 | 48 42 48 32 27 36
R09M | 1888 13 14 14 10 13 6 | 43 39 44 42 45 41
R11M | 4878 17 24 17 18 15 9 | 33 23 31 22 27 24
R12M | 1486 10 24 14 8 12 7 | 34 52 33 33 31 34
R14M | 929 7 10 19 19 5 6 | 38 33 42 25 33 33
R15M | 1331 10 12 14 17 14 6 | 37 38 37 31 29 33
R16M | 794 18 14 25 13 13 9 | 40 39 37 35 37 34
R17E | 2785 12 24 13 26 9 8 | 58 64 56 47 48 52
R18E | 1303 12 17 9 15 13 6 | 29 30 27 35 22 26
XR19E | 1063 14 18 15 --- --- 11 | 18 29 24 --- --- 21
R20E | 1717 31 133 45 53 32 23 | 40 26 60 42 29 40
R21E | 1879 9 21 18 22 10 8 | 60 67 73 64 60 62
XR22E | 2877 17 17 16 15 --- 9 | 20 30 34 33 --- 25
R24E | 1937 14 23 14 36 11 10 | 64 64 63 65 50 58
XR25E |22605 3 --- --- --- --- 0 | 67 --- --- --- --- 66
XR26M | 5991 28 80 37 --- --- 35 | 20 85 24 --- --- 31
XR27 |15558 31 54 --- 23 --- 27 | 33 75 --- 44 --- 46
------+------------------------------------+--------------------------------
RMS | 1974 16 37 18 23 15 |T 43 45 44 42 37 40
WRMS | 1974 15 48 14 20 15 |NE 49 50 50 49 39 45
MEDI | 1486 14 18 14 18 13 |MD 40 42 42 42 33 38
Table 3.2376.3 GPS week: 2376 Day: 3 MJD: 60879
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 2501 13 14 9 21 9 6 | 66 58 66 64 60 62
R03 | 2593 15 24 8 18 17 8 | 74 57 66 68 57 65
R04 | 839 12 16 11 22 18 8 | 76 61 74 61 62 67
R05 | 1987 10 15 17 14 11 6 | 67 62 60 68 62 63
R07 | 1118 14 18 11 16 29 9 | 69 57 68 67 46 61
R08M | 873 24 16 7 20 26 10 | 67 65 62 52 46 57
R09M | 1367 8 17 9 10 13 5 | 62 59 62 63 60 60
R11M | 3705 9 12 9 13 18 6 | 53 51 51 48 53 50
R12M | 1544 10 24 22 12 15 8 | 51 58 45 51 43 46
R14M | 891 8 27 12 10 10 6 | 51 50 55 51 48 50
R15M | 1256 13 16 15 12 19 7 | 58 53 55 50 49 52
R16M | 1030 11 20 16 15 11 7 | 63 73 69 66 66 65
R17E | 3079 10 22 12 28 11 8 | 74 73 80 81 76 75
R18E | 1509 6 26 10 20 12 7 | 47 41 47 57 44 45
XR19E | 1326 13 14 16 --- --- 10 | 43 47 53 --- --- 46
R20E | 2779 25 104 63 50 67 30 | 55 43 93 67 46 58
R21E | 2532 9 19 13 14 14 6 | 56 53 59 61 53 55
XR22E | 1765 14 10 13 11 --- 7 | 44 40 47 54 --- 44
R24E | 3836 10 31 9 26 12 8 | 67 78 68 65 70 66
XR25E |19875 2 --- --- --- --- 0 | 64 --- --- --- --- 63
XR26M |13408 31 75 17 --- --- 27 | 46 95 61 --- --- 54
XR27 |14667 29 70 --- 13 --- 27 | 46 92 --- 64 --- 56
------+------------------------------------+--------------------------------
RMS | 2192 13 32 19 21 22 |T 59 60 62 60 55 57
WRMS | 2192 13 30 11 18 22 |NE 66 64 66 65 57 62
MEDI | 1765 11 19 12 15 14 |MD 58 58 61 63 53 57
Table 3.2376.4 GPS week: 2376 Day: 4 MJD: 60880
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1615 17 11 7 15 16 7 | 50 39 38 45 37 40
R03 | 3133 16 19 11 18 13 7 | 56 39 50 52 39 46
R04 | 1081 14 19 12 20 16 8 | 59 46 55 55 41 50
R05 | 895 11 13 14 19 12 7 | 55 53 52 47 43 49
R07 | 1803 15 17 19 14 33 10 | 55 45 63 60 33 49
R08M | 846 14 19 11 12 18 7 | 52 42 47 52 34 44
R09M | 1159 12 21 11 13 14 7 | 45 50 49 51 46 46
R11M | 3646 19 26 19 30 13 10 | 35 37 37 38 34 32
R12M | 1099 10 15 17 13 12 6 | 29 32 30 34 21 27
R14M | 927 7 13 11 13 7 5 | 36 34 38 42 34 36
R15M | 1554 9 17 12 15 15 6 | 39 48 47 43 31 40
R16M | 987 16 12 15 11 10 6 | 46 49 48 43 40 43
R17E | 2677 11 27 11 22 9 8 | 67 69 63 75 60 65
R18E | 1393 11 19 13 18 15 7 | 35 40 40 44 34 36
XR19E | 1384 12 13 14 --- --- 9 | 24 27 32 --- --- 26
R20E | 4674 29 98 56 32 45 26 | 49 38 80 53 47 50
R21E | 2612 10 20 16 23 14 8 | 63 66 69 65 58 62
XR22E | 1501 15 21 19 15 --- 10 | 29 37 32 40 --- 29
R24E | 1410 14 26 18 31 12 10 | 72 75 76 77 67 71
XR25E |19211 3 --- --- --- --- 0 | 68 --- --- --- --- 69
XR26M |12282 20 78 32 --- --- 30 | 38 77 30 --- --- 36
XR27 |14298 38 66 --- 23 --- 30 | 25 66 --- 49 --- 35
------+------------------------------------+--------------------------------
RMS | 2145 15 30 19 20 18 |T 46 48 48 50 41 44
WRMS | 2145 14 26 12 17 18 |NE 50 48 51 51 38 44
MEDI | 1501 14 19 14 18 14 |MD 46 45 47 49 39 43
Table 3.2376.5 GPS week: 2376 Day: 5 MJD: 60881
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1258 11 13 8 16 20 7 | 57 50 61 67 45 55
R03 | 1509 14 13 17 13 20 8 | 61 54 61 57 46 55
R04 | 924 11 15 14 23 13 7 | 64 55 65 55 57 59
R05 | 1480 7 11 10 14 17 6 | 53 50 53 58 41 50
R07 | 1418 15 19 12 13 21 8 | 56 52 58 49 44 51
R08M | 1032 9 23 33 13 32 11 | 55 55 83 66 45 58
R09M | 1042 14 12 9 10 8 5 | 197 184 199 186 195 193
R11M | 1596 12 13 14 15 12 6 | 137 136 139 142 131 136
R12M | 1015 7 13 16 11 13 6 | 34 38 42 37 27 34
R14M | 855 10 14 11 14 11 6 | 28 38 34 25 30 29
R15M | 1514 4 12 11 12 8 4 | 39 46 44 41 38 40
R16M | 823 11 23 15 24 12 8 | 49 64 68 43 51 53
R17E | 1883 8 29 9 24 13 8 | 68 72 64 73 62 66
R18E | 1435 10 24 8 15 7 6 | 30 36 25 33 27 27
XR19E | 2384 8 14 14 --- --- 8 | 24 28 27 --- --- 23
R20E | 2956 31 101 58 74 54 30 | 50 28 83 50 36 44
R21E | 1562 10 18 22 25 16 9 | 57 56 67 69 59 59
XR22E | 1115 13 20 16 20 --- 9 | 23 27 35 40 --- 27
R24E | 1801 7 21 17 29 10 8 | 68 71 66 75 61 66
XR25E |14295 3 --- --- --- --- 0 | 94 --- --- --- --- 94
XR26M |12704 16 86 46 --- --- 34 | 31 78 35 --- --- 32
XR27 | 8876 34 78 --- 18 --- 32 | 30 60 --- 23 --- 26
------+------------------------------------+--------------------------------
RMS | 1502 13 30 20 25 20 |T 59 60 65 62 58 58
WRMS | 1502 11 23 14 16 20 |NE 53 53 59 51 46 49
MEDI | 1480 10 18 14 15 13 |MD 53 54 61 55 45 51
Table 3.2376.6 GPS week: 2376 Day: 6 MJD: 60882
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1573 11 15 14 19 24 8 | 71 60 73 76 50 64
R03 | 1664 13 18 7 15 13 6 | 75 58 67 76 57 66
R04 | 978 17 11 12 17 17 7 | 87 76 80 71 65 75
R05 | 1785 12 12 12 14 10 6 | 77 70 74 77 66 71
R07 | 1740 20 21 11 14 14 8 | 79 63 73 67 55 67
R08M | 696 9 13 16 12 11 6 | 69 59 75 64 56 64
R09M | 1644 10 19 14 10 7 6 | 337 339 333 337 335 336
R11M | 1691 18 29 19 13 15 9 | 231 243 228 240 234 234
R12M | 1203 9 10 18 10 11 6 | 38 40 35 40 31 35
R14M | 1168 6 11 8 14 8 4 | 38 37 35 36 33 34
R15M | 997 14 13 14 14 8 6 | 51 47 44 49 45 46
R16M | 822 9 30 10 15 9 7 | 56 75 56 48 56 57
R17E | 1503 6 22 15 21 12 7 | 92 94 91 96 86 90
R18E | 1405 6 24 11 13 8 6 | 31 38 25 34 25 27
XR19E | 1998 12 16 14 --- --- 10 | 22 31 35 --- --- 28
R20E | 2070 30 117 40 47 47 24 | 55 46 83 65 47 56
R21E | 1674 13 18 18 24 11 8 | 93 88 100 106 96 95
XR22E | 1907 15 16 9 15 --- 8 | 20 24 28 34 --- 22
R24E | 2722 17 23 23 28 10 10 | 99 103 99 100 92 96
XR25E |19401 3 --- --- --- --- 0 | 106 --- --- --- --- 105
XR26M |14771 30 82 33 --- --- 34 | 34 96 26 --- --- 37
XR27 |11778 46 73 --- 20 --- 34 | 26 86 --- 40 --- 34
------+------------------------------------+--------------------------------
RMS | 1566 14 34 17 20 17 |T 81 84 83 87 84 79
WRMS | 1566 12 44 13 15 17 |NE 69 68 73 67 58 62
MEDI | 1664 12 18 14 15 11 |MD 69 63 73 67 56 64
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