[IGSREPORT-30545] Wk 2375 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 1 02:09:27 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2375 (Jul 13, 2025 - Jul 19, 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 2.2375.
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:
igl2375[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2375 in the SP3 format.
igl23757.sum Combination Report for GPS Week 2375.
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 | 7.2 ns
1 | 7.7 ns
2 | 5.5 ns
3 | 5.2 ns
4 | 7.0 ns
5 | 8.6 ns
6 | 6.8 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
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 1.2375, 1a.2375).
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 2.2375.0-6)
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 3.2375.0-6).
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 2375 summary. (Jul 13, 2025 - Jul 19, 2025)
Table 1.2375.a GPS week : 2375 MJD: 60869.0-60875.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 1 -13 17 .25 18 17 | 545 387 3373 8745
| 1 1 1 9 16 46 .06 | 1449 1389
esa n/a| -3 -3 6 13 0 33 -.06 35 36 | -1147 -407 3378 8656
| 1 1 2 10 12 41 .16 | 1913 2023
gfz n/a| 0 0 0 28 24 17 -.06 22 16 | 0 315 3441 8808
| 1 1 2 25 8 47 .11 | 0 1423
grg n/a| 3 0 0 -52 28 -20 .33 30 21 | 6308 422 3462 8596
| 2 1 4 26 14 40 .10 | 618 1335
iac n/a| 0 0 -4 13 -26 -29 -.25 24 24 | 9164 -22 3375 9527
| 1 1 3 15 20 137 .49 | 1553 1522
jgx n/a| 0 0 -1 -7 -8 -13 -.18 18 18 | 917 500 3539 9077
| 0 0 1 13 10 49 .09 | 1472 1603
Table 1.2375.b GPS week : 2375 MJD: 60869.0-60875.0
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 | 11 12 8 9 7 7 8 |
R03 | 12 9 9 8 8 7 8 |
R04 | 9 10 7 8 8 7 7 |
R05 | 8 12 7 7 7 6 6 |
R07 | 15 10 8 10 8 9 7 |
R08 | 18 14 8 8 9 7 7 |
R09 | 7 7 7 7 7 6 6 |
R11 | 9 8 7 10 8 8 8 |
R12 | 7 7 7 7 8 6 7 |
R14 | 6 8 6 5 8 6 5 |
R15 | 9 8 7 7 8 7 5 |
R16 | 12 11 8 10 9 8 10 |
R17 | 8 11 9 13 10 9 7 |
R18 | 7 7 8 10 13 8 7 |
R19 | 11 11 9 11 10 11 8 |
R20 | 31 27 24 24 28 22 23 |
R21 | 9 8 6 9 13 9 9 |
R22 | 10 10 8 8 9 12 7 |
R24 | 10 15 11 7 10 8 10 |
R25 | 62 47 63 43 74 74 44 |
R26 | 31 31 33 30 33 31 32 |
R27 | 31 29 29 26 26 30 30 |
Table 1.2375.c GPS week : 2375 MJD: 60869.0-60875.0
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 2375 0 | 175 -27 195 949 3073 12060 79.9 3135 3135 | 7229 0
brd 2375 1 | -74 128 -79 54 -3096 3966 80.4 2090 2090 | 7747 0
brd 2375 2 | 31 22 126 1359 -1016 3206 85.9 1981 1981 | 5512 0
brd 2375 3 | -100 39 9 -723 371 8350 82.4 2163 2163 | 5217 0
brd 2375 4 | 19 113 107 -808 -1227 11910 82.4 2027 2027 | 7047 0
brd 2375 5 | 93 101 229 -652 2508 15820 80.8 2009 2009 | 8557 0
brd 2375 6 | -118 56 54 -144 1803 15220 79.3 1964 1964 | 6790 0
-------------+------------------------------------------------------------+----------------
brd 2375 mean| 3 61 91 4 345 10076 81.6 2195 2195 | 6871 0
brd 2375 sdev| 108 55 106 853 2251 5070 2.3 419 419 | 1180 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 2.2375.0 GPS week: 2375 Day: 0 MJD: 60869
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 -2 -1 -7 11 105 .31 25 23 | -2145 1363 2892 7141
esa n/a| -1 -3 3 13 20 -24 -.01 33 32 | -875 1118 2889 7220
gfz n/a| 2 1 0 -3 14 82 .12 28 16 | 0 1628 2945 7512
grg n/a| 3 2 4 -3 17 -46 .38 45 27 | 6363 1292 2990 7182
iac n/a| 0 -2 -3 20 -13 -186 -.29 25 28 | 9005 439 2876 8296
jgx n/a| 1 1 -2 -26 -22 17 -.12 20 20 | -1066 1174 2990 7407
Table 2.2375.1 GPS week: 2375 Day: 1 MJD: 60870
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 0 12 0 45 .29 19 16 | 221 1151 3528 7445
esa n/a| -2 -3 4 33 4 42 .25 36 50 | 1100 164 3555 7179
gfz n/a| 0 0 0 72 32 74 .01 24 19 | 0 1591 3575 7591
grg n/a| 2 -1 -5 -37 21 -52 .40 34 21 | 6509 1794 3630 7416
iac n/a| 2 -1 -2 2 -17 -64 -1.06 39 40 | 10122 -1858 3543 8265
jgx n/a| 1 1 1 -27 -10 -10 -.17 16 16 | 700 2970 3721 7501
Table 2.2375.2 GPS week: 2375 Day: 2 MJD: 60871
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 0 3 -8 -7 .33 18 16 | 1498 -1345 3367 7562
esa n/a| -5 -2 7 2 0 109 -.02 37 39 | 1561 -3635 3373 7178
gfz n/a| 0 0 -4 37 22 -31 -.05 20 17 | 0 -1724 3430 7434
grg n/a| 8 0 -7 -41 9 -72 .29 26 20 | 5894 -1677 3502 7433
iac n/a| 0 1 1 23 -35 186 -.37 22 20 | 8538 -2119 3383 8082
jgx n/a| 0 2 0 0 4 -109 -.14 17 17 | 2266 -2169 3625 7818
Table 2.2375.3 GPS week: 2375 Day: 3 MJD: 60872
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 -40 -11 .24 16 14 | -146 -721 3283 8337
esa n/a| -2 -4 8 18 0 15 -.20 33 35 | -2903 -1224 3281 7354
gfz n/a| 0 1 -2 0 16 -13 -.16 18 13 | 0 -478 3354 7826
grg n/a| 1 -1 0 -67 45 -38 .19 28 16 | 5219 -714 3402 7356
iac n/a| 1 1 -3 10 -65 111 .42 24 24 | 6096 1334 3259 8625
jgx n/a| 0 1 0 0 4 -38 -.37 21 21 | -1002 -645 3555 7834
Table 2.2375.4 GPS week: 2375 Day: 4 MJD: 60873
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 12 -17 26 .18 19 17 | 905 -662 3818 10166
esa n/a| -2 -4 6 3 -13 19 -.22 31 30 | -1299 -2098 3829 10402
gfz n/a| 0 1 3 30 24 34 -.19 23 19 | 0 -552 3905 10311
grg n/a| 3 0 1 -82 48 18 .25 32 20 | 6692 137 3783 10300
iac n/a| 2 1 -9 -13 -30 -156 .29 26 27 | 9644 116 3795 11005
jgx n/a| 1 0 -3 4 -2 18 -.24 19 19 | 1240 676 3902 10857
Table 2.2375.5 GPS week: 2375 Day: 5 MJD: 60874
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 0 -9 -20 -3 .21 17 19 | 1076 2560 3296 9439
esa n/a| -4 -5 7 17 6 20 -.06 36 36 | -3471 2234 3303 9445
gfz n/a| 1 -1 0 27 22 5 -.11 18 16 | 0 2021 3378 9581
grg n/a| 2 2 3 -62 32 25 .32 23 23 | 7174 1920 3376 9291
iac n/a| -2 2 -7 34 -25 -96 -.41 18 17 | 9832 1993 3348 10463
jgx n/a| 1 0 -2 1 -8 41 -.14 17 17 | 1690 1118 3359 9899
Table 2.2375.6 GPS week: 2375 Day: 6 MJD: 60875
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 3 5 -19 -33 .18 15 13 | 2407 365 3431 11131
esa n/a| -2 -2 9 7 -17 52 -.13 39 33 | -2145 591 3422 11817
gfz n/a| 0 0 -1 34 38 -28 -.06 25 17 | 0 -281 3504 11401
grg n/a| 2 0 1 -71 24 19 .49 21 17 | 6305 202 3556 11200
iac n/a| 0 0 -7 19 0 0 -.29 16 16 | 10913 -61 3421 11959
jgx n/a| 1 0 -1 -3 -20 -13 -.10 18 18 | 2597 376 3625 12226
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 3.2375.0 GPS week: 2375 Day: 0 MJD: 60869
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1550 10 13 15 50 13 --- 10 | 83 85 81 92 79 --- 82
R03 | 859 19 17 16 68 24 16 11 | 78 66 76 75 74 57 66
R04E | 3962 20 19 19 44 17 9 9 | 107 110 112 122 100 99 105
R05E | 1404 16 17 14 42 18 10 8 | 72 69 70 77 68 59 66
R07E | 2271 15 13 41 91 26 13 15 | 148 134 146 164 149 126 139
R08 | 1329 22 25 21 102 53 16 18 | 105 103 101 140 107 101 100
R09 | 2638 17 12 14 11 19 10 6 | 56 50 56 51 47 49 50
R11 | 2973 10 19 20 20 31 14 8 | 56 52 63 52 40 58 52
R12 | 1269 13 17 17 10 21 12 7 | 54 48 56 57 51 48 50
R14 | 1704 14 14 11 12 16 9 5 | 58 61 61 57 56 56 57
R15 | 990 22 19 20 20 27 14 9 | 66 67 60 59 59 57 59
R16 | 1324 41 12 39 20 18 11 11 | 67 72 71 66 70 64 63
R17E | 2553 22 16 11 15 14 17 7 | 185 180 184 181 179 182 181
R18E | 1359 10 26 11 15 17 8 6 | 87 90 85 94 80 85 85
XR19E | 1147 15 22 17 --- 17 --- 10 | 56 64 62 --- 60 --- 60
R20 | 9710 60 112 70 46 35 62 31 | 115 78 122 80 78 67 83
R21E | 1851 26 18 16 27 14 13 8 | 123 109 112 119 109 114 113
XR22E | 2216 18 19 13 24 25 --- 10 | 81 80 81 86 84 --- 81
R24E | 1654 17 22 35 24 19 14 9 | 158 157 162 159 151 165 155
XR25 |18158 61 --- --- --- 63 --- 62 | 121 --- --- --- 149 --- 123
XR26 | 8351 43 49 43 --- 75 --- 31 | 90 104 99 --- 79 --- 91
XR27E | 8269 43 30 --- 77 62 --- 30 | 76 91 --- 115 83 --- 85
------+-----------------------------------------+-------------------------------------
RMS | 3134 25 33 28 45 25 20 |T 92 89 93 97 88 86 88
WRMS | 3134 23 32 16 27 27 20 |NE 78 70 76 70 73 61 72
MEDI | 1704 18 19 17 24 19 13 |MD 81 80 81 86 79 64 82
Table 3.2375.1 GPS week: 2375 Day: 1 MJD: 60870
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1360 13 16 16 48 26 --- 12 | 108 108 110 132 104 --- 110
R03 | 1971 17 14 23 32 32 13 9 | 62 66 63 82 68 58 60
R04E | 1559 15 20 13 46 28 15 10 | 73 81 91 110 84 79 81
R05E | 1895 11 21 19 59 29 20 12 | 56 52 63 92 67 52 56
R07E | 1474 15 24 16 38 34 15 10 | 90 95 92 118 73 80 87
R08 | 1240 17 20 18 51 71 17 13 | 94 101 105 99 108 95 93
R09 | 2761 13 9 25 9 20 12 7 | 44 41 39 39 48 46 40
R11 | 2712 9 16 21 21 45 7 8 | 42 32 48 41 64 42 39
R12 | 877 8 20 12 19 34 7 6 | 44 52 43 44 62 48 43
R14 | 1872 14 17 17 9 44 14 8 | 50 57 58 51 62 49 49
R15 | 990 13 18 16 10 41 13 7 | 57 55 49 51 66 42 47
R16 | 1444 23 14 41 10 35 12 10 | 54 45 57 49 60 40 43
R17E | 2269 15 25 17 40 36 17 10 | 154 154 157 153 151 150 151
R18E | 1105 9 24 15 14 37 8 7 | 66 64 66 76 62 65 64
XR19E | 1168 12 16 14 --- 39 --- 10 | 55 58 57 --- 64 --- 54
R20 | 4591 49 120 51 56 47 35 27 | 87 65 75 61 71 55 63
R21E | 1445 15 20 17 20 22 13 7 | 92 93 90 96 85 88 89
XR22E | 1269 16 25 18 18 27 --- 10 | 63 64 74 77 59 --- 64
XR24E | 1787 16 27 21 57 29 --- 15 | 137 138 141 141 135 --- 135
XR25 |13662 25 --- --- --- 87 --- 47 | 91 --- --- --- 150 --- 101
XR26 | 8322 25 61 51 --- 97 --- 30 | 69 70 68 --- 62 --- 62
XR27E |13246 26 46 --- 64 84 --- 29 | 74 77 --- 90 68 --- 68
------+-----------------------------------------+-------------------------------------
RMS | 2089 19 36 24 34 39 16 |T 75 74 77 84 80 65 72
WRMS | 2089 16 50 19 21 40 16 |NE 63 58 60 57 74 52 58
MEDI | 1559 15 20 17 32 35 13 |MD 66 65 66 82 67 55 63
Table 3.2375.2 GPS week: 2375 Day: 2 MJD: 60871
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 1406 14 18 14 35 17 13 8 | 71 79 73 65 66 48 68
R03 | 1462 19 17 25 28 18 18 9 | 64 56 71 62 45 49 54
R04E | 1553 11 12 15 22 15 12 6 | 73 67 74 80 61 64 68
R05E | 1840 9 17 16 26 19 12 7 | 55 57 69 81 57 55 59
R07E | 1904 20 14 17 16 19 15 7 | 74 62 75 70 63 56 65
R08 | 1949 21 20 10 20 15 17 8 | 55 58 55 48 38 46 47
R09 | 2135 23 12 16 6 17 9 6 | 54 45 49 52 47 49 48
R11 | 2704 9 20 18 22 16 9 7 | 58 58 64 50 44 61 55
R12 | 920 13 16 15 20 23 9 7 | 48 51 56 52 52 48 48
R14 | 1903 9 16 19 11 18 10 6 | 47 49 52 46 51 50 48
R15 | 1125 15 12 19 14 20 14 7 | 51 53 49 54 53 53 50
R16 | 1175 19 18 19 18 28 7 8 | 53 52 54 55 66 59 54
R17E | 1887 15 19 19 32 24 17 9 | 188 179 189 191 166 184 182
R18E | 1357 13 23 14 28 16 14 8 | 67 70 72 89 56 74 69
XR19E | 1636 14 17 17 --- 15 --- 9 | 45 48 42 --- 42 --- 44
R20 | 4528 39 134 46 53 49 50 23 | 77 59 80 66 62 54 61
R21E | 1475 9 16 16 16 13 12 6 | 80 78 84 87 68 73 76
XR22E | 1335 17 18 12 14 17 --- 8 | 46 48 51 57 43 --- 48
R24E | 1509 22 33 17 40 26 13 11 | 177 175 179 170 168 174 173
XR25 |12137 55 --- --- --- 72 --- 63 | 61 --- --- --- 70 --- 36
XR26 |10507 39 60 45 --- 81 --- 32 | 60 89 66 --- 54 --- 64
XR27E |10092 37 44 --- 40 74 --- 29 | 49 65 --- 56 44 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1980 18 37 20 26 22 17 |T 70 71 75 75 64 70 66
WRMS | 1980 16 39 17 20 20 17 |NE 57 57 59 53 52 52 51
MEDI | 1636 15 18 17 22 18 13 |MD 58 58 66 62 54 55 54
Table 3.2375.3 GPS week: 2375 Day: 3 MJD: 60872
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 1617 23 18 8 18 25 18 8 | 81 77 75 76 75 56 74
R03 | 2305 10 12 13 24 25 22 8 | 90 89 93 90 94 78 87
R04E | 1743 15 20 11 17 21 18 7 | 97 84 92 88 95 85 90
R05E | 2584 11 14 10 20 17 16 6 | 84 79 80 85 83 72 79
R07E | 2480 17 23 16 21 25 31 10 | 93 98 100 90 99 87 92
R08 | 1732 13 12 11 14 30 23 8 | 87 85 81 84 97 77 83
R09 | 3643 16 20 9 8 22 16 7 | 72 68 65 73 71 74 69
R11 | 1499 16 43 22 17 22 12 10 | 72 66 70 63 68 71 65
R12 | 984 10 30 15 9 23 12 7 | 75 92 80 77 80 78 77
R14 | 1286 7 12 11 12 20 8 5 | 72 82 76 73 69 75 73
R15 | 1146 10 18 12 23 20 6 6 | 76 75 79 74 71 74 74
R16 | 1245 14 16 25 21 42 10 10 | 78 86 82 84 87 86 80
R17E | 2116 24 18 15 65 24 15 13 | 183 179 184 182 171 180 178
R18E | 1500 11 29 11 39 17 21 9 | 101 100 101 120 91 105 101
XR19E | 1507 17 17 20 --- 17 --- 10 | 74 76 80 --- 75 --- 75
R20 | 3976 30 107 44 42 29 56 23 | 104 93 103 100 87 86 94
R21E | 1445 7 17 17 38 14 19 8 | 143 147 143 153 133 129 139
XR22E | 1515 13 23 11 17 20 --- 8 | 80 82 87 90 68 --- 80
R24E | 2663 10 22 13 25 19 13 7 | 146 147 144 143 137 138 142
XR25 |12501 30 --- --- --- 61 --- 42 | 86 --- --- --- 68 --- 69
XR26 | 8893 25 67 43 --- 83 --- 30 | 78 96 68 --- 72 --- 74
XR27E |10158 29 44 --- 34 72 --- 25 | 78 96 --- 79 76 --- 79
------+-----------------------------------------+-------------------------------------
RMS | 2163 16 33 18 28 24 21 |T 93 95 94 96 89 91 89
WRMS | 2163 14 35 13 16 24 21 |NE 80 83 79 79 78 77 76
MEDI | 1732 14 20 13 21 22 16 |MD 81 86 81 85 80 78 79
Table 3.2375.4 GPS week: 2375 Day: 4 MJD: 60873
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 2132 18 10 14 19 17 16 7 | 69 61 56 58 60 38 58
R03 | 1813 13 12 26 19 17 19 8 | 60 55 72 48 52 38 52
R04E | 2659 10 15 23 19 20 20 8 | 68 67 83 66 74 52 66
R05E | 2392 7 14 11 21 24 12 6 | 64 61 69 62 77 55 62
R07E | 2480 19 22 9 20 25 11 8 | 68 59 59 57 74 59 61
R08 | 1332 17 24 9 21 25 21 9 | 58 49 51 56 69 43 50
R09 | 3229 15 13 14 17 25 5 6 | 33 34 38 34 44 32 32
R11 | 1803 18 24 15 17 17 14 8 | 38 37 32 31 29 34 28
R12 | 1185 18 9 29 13 21 9 8 | 33 29 42 34 36 28 29
R14 | 1142 16 7 30 14 25 9 8 | 30 33 54 30 57 28 35
R15 | 1150 16 26 18 20 16 7 7 | 36 59 58 36 42 44 43
R16 | 1716 18 25 17 19 28 16 9 | 37 59 59 39 50 37 43
R17E | 1658 11 27 15 29 31 17 9 | 191 188 191 200 189 190 190
R18E | 1786 9 27 13 59 44 18 13 | 66 63 59 66 86 58 60
XR19E | 2081 13 11 16 --- 26 --- 9 | 38 42 40 --- 50 --- 40
R20 | 2693 48 105 60 49 42 53 27 | 69 46 48 54 56 31 45
R21E | 1483 15 15 26 72 18 16 13 | 115 117 117 121 103 111 111
XR22E | 1448 14 16 12 31 18 --- 9 | 60 64 60 67 71 --- 62
R24E | 2291 16 12 16 34 33 16 9 | 166 162 164 169 152 158 162
XR25 |14036 57 --- --- --- 96 --- 74 | 71 --- --- --- 152 --- 66
XR26 | 6399 30 67 55 --- 77 --- 32 | 46 76 41 --- 52 --- 45
XR27E | 7943 33 36 --- 39 67 --- 25 | 29 53 --- 48 53 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 2027 19 31 23 32 26 19 |T 65 67 69 67 74 60 62
WRMS | 2027 17 30 19 20 27 19 |NE 46 47 49 40 58 35 42
MEDI | 1813 16 16 16 20 25 16 |MD 60 59 58 56 57 43 50
Table 3.2375.5 GPS week: 2375 Day: 5 MJD: 60874
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 2329 9 17 13 19 22 17 7 | 79 83 83 85 87 73 81
R03 | 2253 17 13 12 16 14 14 6 | 66 58 56 67 51 55 58
R04E | 2476 12 9 15 20 16 13 6 | 70 63 72 63 69 65 66
R05E | 2126 10 14 9 17 18 15 6 | 65 58 60 69 61 55 60
R07E | 1538 23 22 12 22 17 17 8 | 76 68 63 65 73 59 65
R08 | 978 12 15 13 16 24 13 7 | 60 59 59 62 70 58 59
R09 | 3039 11 23 15 12 10 11 6 | 57 57 64 56 49 53 54
R11 | 1755 10 26 22 10 25 13 8 | 59 63 61 51 51 63 56
R12 | 1059 9 20 18 15 9 11 6 | 45 53 52 50 45 51 48
R14 | 1160 7 15 20 13 16 7 6 | 42 45 37 41 37 39 38
R15 | 1146 13 21 17 13 18 9 6 | 42 45 50 44 44 51 44
R16 | 2352 15 36 14 11 12 9 7 | 43 65 57 55 50 57 51
R17E | 2469 11 24 21 26 12 20 8 | 127 133 133 120 125 130 127
R18E | 1860 6 30 16 26 13 9 7 | 86 95 82 97 88 92 88
XR19E | 1945 15 10 21 --- 22 --- 10 | 52 54 58 --- 61 --- 55
R20 | 2758 46 117 40 54 29 45 22 | 57 61 63 46 60 47 49
R21E | 1578 20 25 20 28 22 12 9 | 140 142 141 128 126 136 135
XR22E | 1194 20 16 17 41 15 --- 11 | 82 81 82 85 73 --- 78
R24E | 1697 10 28 16 29 12 13 8 | 128 135 135 131 130 131 130
XR25 | 7337 60 --- --- --- 90 --- 73 | 52 --- --- --- 93 --- 41
XR26 | 8392 27 70 49 --- 71 --- 30 | 50 66 48 --- 46 --- 47
XR27E |10604 46 42 --- 30 73 --- 29 | 29 52 --- 37 43 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 2009 17 36 18 23 18 17 |T 68 73 72 71 69 71 66
WRMS | 2009 19 36 16 23 17 17 |NE 52 57 54 52 54 52 49
MEDI | 1945 12 22 16 19 17 13 |MD 59 63 61 63 61 58 56
Table 3.2375.6 GPS week: 2375 Day: 6 MJD: 60875
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 2628 13 12 18 13 23 16 7 | 74 72 71 64 77 57 69
R03 | 1661 20 14 14 16 15 14 7 | 80 59 69 61 64 53 65
R04E | 1235 12 19 11 16 12 17 6 | 85 74 82 79 79 63 76
R05E | 1275 6 13 21 14 17 11 6 | 76 77 71 76 83 66 73
R07E | 1522 12 21 14 18 12 16 6 | 93 77 87 88 87 70 83
R08 | 1466 9 27 13 18 14 12 6 | 77 66 74 75 85 61 72
R09 | 2004 8 19 19 17 15 9 6 | 43 48 47 41 44 45 42
R11 | 1278 7 37 19 18 13 9 7 | 53 53 55 50 47 51 50
R12 | 1189 11 13 23 22 13 15 7 | 41 46 47 49 47 37 41
R14 | 2516 9 16 10 14 11 11 5 | 37 36 35 37 39 37 36
R15 | 1844 10 12 16 10 10 11 5 | 44 50 48 43 42 41 42
R16 | 3045 20 35 32 13 19 14 10 | 53 77 71 53 58 64 57
R17E | 3016 10 25 14 21 16 10 7 | 151 142 147 153 145 150 147
R18E | 1994 8 26 17 19 9 11 6 | 64 62 62 70 59 68 63
XR19E | 1483 13 19 13 --- 12 --- 8 | 29 36 37 --- 37 --- 33
R20 | 2103 38 136 70 45 28 49 23 | 79 56 89 57 57 47 58
R21E | 1559 17 19 19 29 10 19 8 | 131 130 131 116 122 125 125
XR22E | 1472 14 17 13 18 7 --- 7 | 50 46 54 57 51 --- 50
R24E | 1502 11 28 27 28 21 24 10 | 149 149 149 156 147 148 149
XR25 |12530 38 --- --- --- 49 --- 43 | 65 --- --- --- 89 --- 53
XR26 | 8189 38 75 52 --- 63 --- 32 | 44 72 50 --- 36 --- 38
XR27E | 6608 46 44 --- 38 68 --- 29 | 25 57 --- 39 32 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 1963 15 39 25 21 16 18 |T 70 70 73 71 69 69 65
WRMS | 1963 13 33 17 17 16 18 |NE 56 56 58 51 55 48 50
MEDI | 1661 12 19 17 18 14 14 |MD 64 62 69 61 58 61 57
More information about the IGSREPORT
mailing list