[IGSREPORT-30565] Wk 2376 IGLOS Final Orbits [Resubmission]
acc
acc at igs.org
Fri Aug 15 04:06:22 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
----+--------+---------------
0 | ESA | R20
1 | ESA | R20
2 | ESA | R20
3 | ESA | R20
4 | ESA | R20
5 | 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| 0 0 3 6 -22 29 .18 15 14 | 1386 -1409 3913 16680
| 0 0 1 10 8 22 .04 | 2125 1012
esa n/a| -3 -3 8 20 8 27 -.12 35 37 | -798 -915 3915 16523
| 1 1 1 22 15 21 .08 | 3041 1057
gfz n/a| 0 0 -1 20 14 15 -.08 19 14 | 0 -1544 3956 16144
| 1 0 1 15 7 41 .03 | 0 1230
grg n/a| 2 0 1 -45 43 -7 .39 23 18 | 7566 -766 3575 10705
| 2 0 1 6 19 25 .04 | 1776 1313
iac n/a| 0 0 -8 5 -5 -24 -.14 17 16 | 8567 -1962 4031 16917
| 1 2 2 20 8 84 .10 | 1958 2102
jgx n/a| 0 0 -3 -15 -23 -25 -.16 19 19 | 3985 -982 3655 10874
| 0 0 1 14 16 39 .05 | 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 7 7 7 7 7 8 |
R03 | 8 8 6 7 7 8 7 |
R04 | 7 8 8 7 8 7 7 |
R05 | 7 7 7 6 7 6 6 |
R07 | 8 8 8 8 10 8 7 |
R08 | 8 9 10 9 7 10 7 |
R09 | 8 7 7 6 7 6 6 |
R11 | 7 7 9 6 9 6 9 |
R12 | 7 6 7 8 7 6 6 |
R14 | 5 9 7 6 6 5 4 |
R15 | 7 6 8 7 7 6 7 |
R16 | 8 9 8 7 6 8 6 |
R17 | 7 7 8 7 7 7 6 |
R18 | 8 8 6 6 6 6 6 |
R19 | 10 8 9 9 9 7 8 |
R20 | 25 22 20 26 20 23 22 |
R21 | 8 8 8 6 8 8 8 |
R22 | 9 8 8 7 9 8 7 |
R24 | 8 7 9 8 9 7 9 |
R25 | 54 34 43 68 51 84 97 |
R26 | 36 33 34 30 32 35 32 |
R27 | 28 29 27 30 31 32 33 |
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 | 25 -106 76 127 651 16570 83.5 1970 1970 | 6219 0
brd 2376 1 | 78 6 99 169 2713 9255 84.2 1989 1989 | 9303 0
brd 2376 2 | 39 118 120 -1375 326 10810 80.0 1974 1974 | 11332 0
brd 2376 3 | -137 29 192 -160 -1908 9733 79.4 2192 2192 | 8647 0
brd 2376 4 | -9 -41 109 -495 -754 7527 81.6 2149 2149 | 6165 0
brd 2376 5 | 52 -30 173 -93 161 6263 79.9 1504 1504 | 6074 0
brd 2376 6 | 62 -7 80 597 -994 10870 81.0 1567 1567 | 5787 0
-------------+------------------------------------------------------------+----------------
brd 2376 mean| 16 -4 121 -175 28 10146 81.4 1906 1906 | 7646 0
brd 2376 sdev| 73 69 45 626 1478 3294 1.9 268 268 | 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 1 3 18 -31 26 .23 19 16 | 1286 -2788 3573 13724
esa n/a| -1 -2 10 51 32 0 -.26 35 29 | -3760 -2095 3582 14000
gfz n/a| 0 0 -2 19 3 32 -.12 22 16 | 0 -3756 3471 13358
grg n/a| 0 0 2 -52 46 15 .46 26 17 | 8082 -3086 3598 13726
iac n/a| 0 3 -9 15 -2 -14 -.13 14 13 | 9913 -369 3555 14634
jgx n/a| 0 0 -1 -12 -30 -20 -.13 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 4 -4 -15 45 .23 16 15 | -1153 -2056 3973 17903
esa n/a| -2 -2 8 45 21 31 -.10 38 51 | -3889 -918 3967 17418
gfz n/a| 2 0 0 38 18 76 -.08 20 15 | 0 -2013 3954 17671
grg n/a| 0 -1 3 -37 39 -5 .40 23 18 | 9211 -233 3243 13749
iac n/a| -1 0 -9 -3 -6 -120 -.27 16 16 | 10301 -1442 4031 17905
jgx n/a| 0 1 -4 -29 -10 30 -.10 17 16 | 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| 0 2 4 0 -27 29 .16 16 15 | -464 -519 4759 24854
esa n/a| -4 0 9 7 7 65 -.03 38 49 | -3049 349 4752 24803
gfz n/a| -1 2 -4 19 18 -12 -.03 18 15 | 0 -743 4855 24158
grg n/a| 2 0 0 -49 59 5 .34 23 20 | 10114 1296 4106 12221
iac n/a| 0 -2 -6 -2 -4 18 -.26 19 17 | 11398 -5395 4872 24107
jgx n/a| 0 0 -2 -25 -39 -82 -.18 16 16 | 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 4 13 -24 -4 .16 14 13 | -371 -2295 4196 31916
esa n/a| -2 -3 8 4 -9 22 -.18 35 33 | -2049 -2544 4197 31868
gfz n/a| 0 0 0 11 19 -43 -.11 18 10 | 0 -2384 4283 31471
grg n/a| 6 0 3 -40 14 -50 .39 22 19 | 8100 -487 3462 8875
iac n/a| -1 0 -12 -10 8 133 -.05 19 16 | 6184 -4461 4421 30427
jgx n/a| 0 1 -5 1 -45 -73 -.15 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 1 11 -23 60 .12 15 14 | 4130 -1507 3857 10099
esa n/a| -4 -3 9 -6 14 6 -.16 33 28 | 2417 -451 3836 9722
gfz n/a| 0 0 -1 -6 4 -3 -.09 17 12 | 0 -969 3946 9758
grg n/a| 2 1 3 -46 65 -16 .36 21 18 | 5973 -1200 3925 10019
iac n/a| 1 2 -9 21 -18 -46 .01 19 17 | 7874 -1321 3863 10819
jgx n/a| -1 0 -6 -6 -4 -15 -.15 20 20 | 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 -8 -29 45 .17 13 11 | 2645 -303 2986 9028
esa n/a| -3 -3 9 33 -4 24 -.07 34 26 | 2623 -9 2995 8873
gfz n/a| 0 0 -1 30 14 53 -.09 19 14 | 0 -434 3054 8250
grg n/a| 4 0 -1 -53 59 -21 .41 25 17 | 5735 -546 3025 8189
iac n/a| 0 0 -6 -21 -9 -100 -.14 15 14 | 7255 -710 3076 10401
jgx n/a| 0 0 -4 -3 -26 -10 -.21 21 21 | 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| -1 0 3 13 -7 7 .16 13 12 | 3629 -397 4048 9237
esa n/a| -6 -4 5 11 -3 39 -.04 33 42 | 2119 -739 4076 8978
gfz n/a| -1 0 -2 31 22 2 -.06 17 13 | 0 -511 4134 8346
grg n/a| 2 0 3 -40 23 23 .40 20 16 | 5753 -1106 3666 8160
iac n/a| 1 -3 -7 35 -7 -40 -.17 19 17 | 7048 -40 4402 10130
jgx n/a| 0 0 -2 -34 -7 -5 -.22 18 18 | 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 iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1298 15 19 17 20 20 15 8 | 75 69 68 68 78 60 69
R03 | 981 16 16 19 17 19 20 8 | 77 57 72 68 70 52 65
R04 | 1413 15 17 12 16 9 16 6 | 72 63 65 72 69 52 64
R05 | 1711 10 15 12 16 15 17 6 | 62 53 61 63 68 45 57
R07 | 1738 22 18 8 23 13 13 7 | 59 40 45 48 52 33 44
R08M | 1566 19 13 13 21 9 23 7 | 58 39 48 47 46 30 42
R09M | 2567 16 25 18 16 15 10 7 | 101 106 106 99 92 103 99
R11M | 2686 16 28 15 17 11 9 7 | 40 39 39 45 37 35 37
R12M | 1178 15 16 20 16 9 15 6 | 35 35 27 30 23 24 26
R14M | 1542 10 11 13 13 10 11 5 | 40 38 43 41 34 43 39
R15M | 1800 16 17 24 10 11 9 6 | 49 51 43 41 43 40 42
R16M | 1880 16 16 30 15 15 13 8 | 51 60 58 48 39 52 48
R17E | 2511 15 20 19 19 13 13 7 | 126 122 123 134 123 127 125
R18E | 1682 10 26 27 13 9 13 7 | 47 49 50 52 45 42 44
XR19E | 1265 19 18 17 --- 15 --- 10 | 16 29 29 --- 27 --- 22
R20E | 3376 48 122 56 76 20 45 24 | 73 67 92 92 75 65 70
R21E | 1928 14 28 12 24 14 14 8 | 122 124 123 124 123 123 122
XR22E | 2330 17 20 17 19 15 --- 8 | 42 44 31 40 37 --- 36
R24E | 2075 14 19 22 31 14 9 8 | 140 137 138 154 135 136 138
XR25E |13880 61 --- --- --- 48 --- 54 | 109 --- --- --- 112 --- 102
XR26M | 5527 53 62 66 --- 67 --- 36 | 44 108 32 --- 84 --- 60
XR27 | 6236 50 45 --- 34 53 --- 27 | 40 90 --- 55 57 --- 54
------+-----------------------------------------+-------------------------------------
RMS | 1969 19 35 22 26 14 18 |T 67 67 64 69 66 62 63
WRMS | 1969 16 29 16 17 13 18 |NE 64 62 62 62 65 48 58
MEDI | 1800 16 19 17 17 14 13 |MD 58 57 50 55 57 52 54
Table 3.2376.1 GPS week: 2376 Day: 1 MJD: 60877
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1452 14 23 10 23 13 13 7 | 43 51 40 41 35 37 38
R03 | 1138 18 17 11 21 18 17 7 | 50 49 38 48 46 38 42
R04 | 1554 13 32 17 14 14 21 8 | 53 49 53 57 49 37 47
R05 | 1803 7 20 12 17 16 19 7 | 44 38 48 52 51 33 42
R07 | 1380 14 20 18 25 17 12 8 | 40 39 39 33 37 29 32
R08M | 1495 25 17 13 28 9 20 9 | 43 34 35 32 29 27 29
R09M | 1812 13 11 10 16 18 15 6 | 91 85 89 91 86 90 88
R11M | 4542 11 13 20 19 15 11 7 | 36 51 53 48 35 35 40
R12M | 1319 9 22 13 10 13 14 6 | 32 39 39 30 31 30 30
R14M | 1148 12 42 18 13 17 9 8 | 28 50 35 27 17 28 25
R15M | 1470 8 13 16 12 12 11 5 | 31 31 34 34 25 35 29
R16M | 1193 20 16 25 13 18 18 8 | 32 34 36 26 25 35 26
R17E | 2779 13 27 14 20 14 12 7 | 106 105 106 115 94 99 102
R18E | 1315 8 26 12 18 23 12 7 | 41 38 39 49 36 37 37
XR19E | 1203 14 15 14 --- 12 --- 8 | 20 27 29 --- 22 --- 22
R20E | 2947 34 124 57 55 30 39 21 | 54 46 77 64 51 47 48
R21E | 1302 18 35 15 23 12 9 8 | 87 77 92 95 77 88 85
XR22E | 2876 16 30 8 16 11 --- 8 | 23 26 27 34 23 --- 23
R24E | 1909 13 19 19 22 11 11 7 | 98 100 107 96 88 97 96
XR25E |17047 31 --- --- --- 36 --- 34 | 96 --- --- --- 110 --- 101
XR26M | 6827 48 66 41 --- 70 --- 32 | 40 74 44 --- 64 --- 50
XR27 | 7648 43 54 --- 34 60 --- 28 | 24 59 --- 37 32 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1989 16 38 20 23 16 17 |T 50 52 53 53 48 48 48
WRMS | 1989 15 51 15 18 16 16 |NE 42 47 43 44 41 34 39
MEDI | 1495 14 22 14 19 15 13 |MD 41 49 39 48 36 37 38
Table 3.2376.2 GPS week: 2376 Day: 2 MJD: 60878
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1371 15 12 9 25 16 15 7 | 47 45 46 45 48 32 41
R03 | 1360 14 17 12 14 11 9 6 | 58 39 53 52 47 48 49
R04 | 1405 10 17 9 17 22 21 7 | 59 53 55 62 68 48 55
R05 | 2317 10 19 14 14 15 16 6 | 52 48 59 53 47 37 48
R07 | 976 18 26 9 17 15 16 7 | 48 44 39 40 47 31 39
R08M | 1291 25 20 16 28 13 22 9 | 48 42 48 32 42 27 37
R09M | 1888 14 13 14 10 19 15 6 | 43 39 44 42 42 45 41
R11M | 4878 16 25 19 19 23 15 8 | 33 23 31 22 37 27 24
R12M | 1485 10 25 15 9 16 11 6 | 34 52 33 33 27 31 33
R14M | 930 10 11 21 17 19 6 6 | 38 33 42 25 25 33 31
R15M | 1330 10 13 15 17 31 17 8 | 37 38 37 31 44 29 32
R16M | 794 18 15 25 13 13 13 7 | 40 39 37 35 34 37 33
R17E | 2785 13 26 13 26 11 7 7 | 58 64 56 47 46 48 51
R18E | 1304 11 19 10 14 15 14 6 | 29 30 27 35 25 22 26
XR19E | 1065 15 19 14 --- 13 --- 9 | 18 29 24 --- 23 --- 21
R20E | 1716 34 136 46 52 31 30 19 | 40 26 60 42 43 29 35
R21E | 1878 9 22 19 21 19 11 7 | 60 67 73 64 58 60 62
XR22E | 2878 17 17 16 14 11 --- 7 | 20 30 34 33 23 --- 24
R24E | 1935 13 23 13 37 14 12 8 | 64 64 63 65 62 50 58
XR25E |22607 37 --- --- --- 49 --- 42 | 67 --- --- --- 88 --- 65
XR26M | 5984 40 72 51 --- 73 --- 34 | 20 85 24 --- 59 --- 36
XR27 |15550 38 52 --- 35 59 --- 27 | 33 75 --- 44 48 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1973 16 38 18 23 19 16 |T 43 45 44 42 44 37 40
WRMS | 1973 15 49 15 20 17 16 |NE 49 50 50 49 50 39 46
MEDI | 1485 14 19 14 17 16 15 |MD 40 42 42 42 44 33 37
Table 3.2376.3 GPS week: 2376 Day: 3 MJD: 60879
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2500 11 14 8 24 19 11 6 | 66 58 66 64 67 60 62
R03 | 2599 16 22 8 19 14 16 7 | 74 57 66 68 67 57 64
R04 | 834 11 17 11 23 16 19 7 | 76 61 74 61 74 62 68
R05 | 1991 12 17 15 14 14 12 6 | 67 62 60 68 68 62 62
R07 | 1118 13 19 9 16 18 31 8 | 69 57 68 67 72 46 62
R08M | 875 23 16 7 21 14 27 8 | 67 65 62 52 58 46 57
R09M | 1377 11 14 9 13 16 13 5 | 62 59 62 63 63 60 60
R11M | 3707 10 13 7 15 10 17 5 | 53 51 51 48 41 53 48
R12M | 1543 13 26 20 15 17 14 8 | 51 58 45 51 35 43 44
R14M | 880 9 28 11 10 14 10 6 | 51 50 55 51 49 48 50
R15M | 1246 14 17 13 13 13 20 6 | 58 53 55 50 44 49 50
R16M | 1020 10 20 15 15 15 12 6 | 63 73 69 66 51 66 63
R17E | 3077 10 21 11 30 9 10 6 | 74 73 80 81 69 76 74
R18E | 1506 7 24 11 21 8 12 6 | 47 41 47 57 42 44 44
XR19E | 1328 16 14 15 --- 13 --- 8 | 43 47 53 --- 41 --- 45
R20E | 2782 32 120 57 52 51 65 26 | 55 43 93 67 56 46 57
R21E | 2532 10 19 12 16 16 14 6 | 56 53 59 61 47 53 53
XR22E | 1762 15 11 13 13 14 --- 7 | 44 40 47 54 36 --- 42
R24E | 3832 12 30 9 27 18 11 8 | 67 78 68 65 66 70 66
XR25E |19889 59 --- --- --- 78 --- 68 | 64 --- --- --- 81 --- 37
XR26M |13400 45 63 32 --- 72 --- 30 | 46 95 61 --- 67 --- 57
XR27 |14662 46 62 --- 29 64 --- 30 | 46 92 --- 64 63 --- 60
------+-----------------------------------------+-------------------------------------
RMS | 2191 14 35 18 22 19 22 |T 59 60 62 60 57 55 55
WRMS | 2191 13 33 10 19 16 22 |NE 66 64 66 65 68 57 63
MEDI | 1762 12 19 11 16 15 14 |MD 58 58 61 63 58 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 iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1612 15 12 8 18 19 17 6 | 50 39 38 45 52 37 41
R03 | 3114 14 19 12 19 15 14 7 | 56 39 50 52 57 39 47
R04 | 1091 13 20 10 22 19 17 7 | 59 46 55 55 63 41 52
R05 | 927 9 12 13 21 17 14 6 | 55 53 52 47 64 43 51
R07 | 1779 16 17 19 13 18 33 9 | 55 45 63 60 58 33 50
R08M | 857 16 18 10 14 20 19 7 | 52 42 47 52 50 34 44
R09M | 1148 14 20 11 13 18 14 6 | 45 50 49 51 57 46 47
R11M | 3671 20 24 20 30 14 14 9 | 35 37 37 38 34 34 32
R12M | 1096 12 14 15 15 16 13 6 | 29 32 30 34 24 21 25
R14M | 913 8 15 12 12 19 7 5 | 36 34 38 42 42 34 37
R15M | 1569 10 13 9 17 24 19 7 | 39 48 47 43 58 31 43
R16M | 968 16 11 15 12 11 10 5 | 46 49 48 43 42 40 43
R17E | 2692 10 26 11 24 16 10 7 | 67 69 63 75 65 60 65
R18E | 1385 11 17 12 19 8 15 6 | 35 40 40 44 40 34 36
XR19E | 1355 15 14 13 --- 16 --- 8 | 24 27 32 --- 29 --- 25
R20E | 4699 33 116 45 28 36 49 20 | 49 38 80 53 49 47 48
R21E | 2621 11 18 15 26 16 14 7 | 63 66 69 65 60 58 62
XR22E | 1470 15 23 19 17 16 --- 9 | 29 37 32 40 30 --- 29
R24E | 1380 14 24 18 33 17 11 8 | 72 75 76 77 69 67 70
XR25E |19191 42 --- --- --- 61 --- 51 | 68 --- --- --- 90 --- 70
XR26M |12282 37 64 49 --- 74 --- 32 | 38 77 30 --- 58 --- 40
XR27 |14303 50 57 --- 37 61 --- 30 | 25 66 --- 49 41 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 2149 15 33 17 21 19 20 |T 46 48 48 50 51 41 45
WRMS | 2149 14 28 12 18 17 20 |NE 50 48 51 51 55 38 46
MEDI | 1470 14 18 13 19 17 14 |MD 46 45 47 49 52 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 iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1256 8 16 7 15 18 23 6 | 57 50 61 67 63 45 56
R03 | 1498 11 15 17 15 21 23 7 | 61 54 61 57 63 46 56
R04 | 926 12 14 15 22 11 12 6 | 64 55 65 55 52 57 58
R05 | 1483 5 12 9 15 18 19 6 | 53 50 53 58 57 41 51
R07 | 1415 12 20 12 16 18 24 7 | 56 52 58 49 61 44 52
R08M | 1043 9 24 32 12 11 34 10 | 55 55 83 66 58 45 58
R09M | 1033 16 11 8 10 13 7 5 | 197 184 199 186 196 195 193
R11M | 1602 14 13 13 14 10 12 5 | 137 136 139 142 133 131 136
R12M | 1013 9 14 15 11 15 11 5 | 34 38 42 37 28 27 32
R14M | 854 10 14 11 15 9 12 5 | 28 38 34 25 30 30 29
R15M | 1515 6 10 9 13 19 12 5 | 39 46 44 41 54 38 43
R16M | 816 10 20 14 27 15 15 7 | 49 64 68 43 61 51 55
R17E | 1880 8 29 9 23 11 13 7 | 68 72 64 73 59 62 65
R18E | 1434 11 23 8 15 9 7 5 | 30 36 25 33 30 27 28
XR19E | 2365 10 14 13 --- 13 --- 7 | 24 28 27 --- 26 --- 24
R20E | 2967 34 119 49 73 22 54 23 | 50 28 83 50 39 36 46
R21E | 1564 12 19 23 24 13 15 8 | 57 56 67 69 61 59 59
XR22E | 1092 14 21 16 20 12 --- 8 | 23 27 35 40 20 --- 25
R24E | 1809 7 21 17 29 9 10 7 | 68 71 66 75 65 61 66
XR25E |14275 68 --- --- --- 102 --- 83 | 94 --- --- --- 102 --- 83
XR26M |12700 32 70 66 --- 75 --- 34 | 31 78 35 --- 60 --- 38
XR27 | 8868 49 66 --- 35 64 --- 31 | 30 60 --- 23 35 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 1504 13 34 19 25 15 21 |T 59 60 65 62 61 58 58
WRMS | 1504 11 26 14 17 14 21 |NE 53 53 59 51 55 46 50
MEDI | 1483 11 19 13 15 13 13 |MD 53 54 61 55 58 45 52
Table 3.2376.6 GPS week: 2376 Day: 6 MJD: 60882
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1541 11 16 12 19 16 26 7 | 71 60 73 76 72 50 66
R03 | 1687 14 18 7 16 19 13 6 | 75 58 67 76 60 57 65
R04 | 961 14 10 11 20 16 20 7 | 87 76 80 71 85 65 77
R05 | 1769 11 13 12 14 15 13 5 | 77 70 74 77 84 66 74
R07 | 1755 16 25 11 15 13 17 7 | 79 63 73 67 77 55 69
R08M | 692 8 16 14 12 21 14 6 | 69 59 75 64 82 56 67
R09M | 1660 12 21 11 11 20 7 6 | 337 339 333 337 337 335 335
R11M | 1704 20 32 16 17 26 13 9 | 231 243 228 240 232 234 234
R12M | 1209 7 11 19 9 20 12 6 | 38 40 35 40 37 31 34
R14M | 1168 6 11 9 12 10 9 4 | 38 37 35 36 35 33 34
R15M | 994 12 15 15 14 20 9 6 | 51 47 44 49 50 45 46
R16M | 805 8 33 12 13 13 7 6 | 56 75 56 48 54 56 56
R17E | 1514 6 22 15 21 9 11 6 | 92 94 91 96 86 86 90
R18E | 1400 6 25 11 13 14 8 5 | 31 38 25 34 28 25 27
XR19E | 1970 11 16 15 --- 11 --- 7 | 22 31 35 --- 27 --- 27
R20E | 2051 25 106 43 48 34 51 22 | 55 46 83 65 67 47 56
R21E | 1677 14 20 18 23 15 12 7 | 93 88 100 106 100 96 96
XR22E | 1872 14 17 9 14 8 --- 6 | 20 24 28 34 19 --- 22
R24E | 2738 16 26 24 26 19 11 9 | 99 103 99 100 95 92 96
XR25E |19361 73 --- --- --- 128 --- 96 | 106 --- --- --- 135 --- 97
XR26M |14775 33 80 45 --- 74 --- 31 | 34 96 26 --- 65 --- 40
XR27 |11779 54 69 --- 26 75 --- 33 | 26 86 --- 40 52 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1567 13 33 17 20 18 18 |T 81 84 83 87 85 84 79
WRMS | 1567 12 42 13 16 17 18 |NE 69 68 73 67 71 58 64
MEDI | 1677 12 20 12 15 16 12 |MD 69 63 73 67 67 56 65
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