[IGSREPORT-30680] Wk 2390 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 14 05:51:12 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2390 (Oct 26, 2025 - Nov 01, 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 2.2390.
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:
igl2390[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2390 in the SP3 format.
igl23907.sum Combination Report for GPS Week 2390.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
Starting 02-Feb-2025 (GPS week 2352) the IGS Analysis Centers started using
the IGS realization of the updated ITRF2020-u2023, called IGb20. The combined
GLONASS orbits from this date are therefore in IGb20 frame.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 4.9 ns
1 | 4.5 ns
2 | 4.5 ns
3 | 2.0 ns
4 | 3.7 ns
5 | 1.6 ns
6 | 3.3 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 | GFZ | R20
1 | ESA | R26 R27
1 | GFZ | R20
2 | GFZ | R20 R26
3 | ESA | R26
3 | GFZ | R20
4 | GFZ | R20
5 | GFZ | R20
6 | ESA | R26 R27
6 | GFZ | 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 1.2390, 1a.2390).
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 2.2390.0-6)
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 3.2390.0-6).
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 2390 summary. (Oct 26, 2025 - Nov 01, 2025)
Table 1.2390.a GPS week : 2390 MJD: 60974.0-60980.0
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 -1 -1 11 5 .17 14 13 | 1246 -572 3401 7999
| 0 0 2 19 7 24 .03 | 707 1762
esa n/a| -3 0 0 8 -11 52 -.09 20 19 | 1347 -430 3410 7879
| 1 2 1 12 16 32 .03 | 1161 2170
gfz n/a| 0 1 -3 25 1 7 -.06 18 18 | 0 -411 3432 8109
| 2 1 2 21 10 32 .05 | 0 1773
grg n/a| 1 -1 2 -34 -24 -22 .29 16 14 | 3255 -332 3401 7952
| 1 1 4 19 29 38 .04 | 1013 1945
iac n/a| 0 0 -3 10 10 -3 -.15 15 15 | 5855 -887 3593 9077
| 1 2 2 15 29 82 .06 | 1447 1596
jgx n/a| 1 0 5 0 0 -29 -.18 16 16 | 3177 -397 3521 8647
| 1 1 1 10 19 36 .04 | 930 2577
Table 1.2390.b GPS week : 2390 MJD: 60974.0-60980.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R02 | 7 6 7 6 7 7 6 |
R03 | 6 5 9 6 7 7 8 |
R04 | 6 7 7 5 5 6 8 |
R05 | 6 7 7 7 5 5 6 |
R07 | 8 9 11 7 7 6 7 |
R08 | 6 6 6 6 9 8 6 |
R09 | 6 6 11 8 7 6 8 |
R11 | 10 9 9 8 8 7 11 |
R12 | 11 8 8 7 9 7 8 |
R14 | 12 7 8 8 8 7 7 |
R15 | 9 7 8 8 7 8 8 |
R16 | 12 7 7 8 7 7 8 |
R17 | 5 7 8 8 6 6 5 |
R18 | 8 8 7 7 9 7 8 |
R19 | 11 11 22 7 8 9 9 |
R20 | 11 11 7 12 8 6 10 |
R21 | 6 6 7 8 6 7 8 |
R22 | 8 7 13 7 11 8 8 |
R24 | 7 6 7 7 8 6 7 |
R26 | 34 31 45 30 30 33 31 |
R27 | 32 33 28 30 34 35 30 |
R28 | 38 51 53 30 30 74 42 |
Table 1.2390.c GPS week : 2390 MJD: 60974.0-60980.0
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 2390 0 | -20 65 66 -1649 1483 3536 81.6 1436 1436 | 4900 0
brd 2390 1 | -17 39 147 1983 114 4501 83.3 1453 1453 | 4468 0
brd 2390 2 | -23 -45 -32 -646 440 -2913 85.8 2121 2121 | 4487 0
brd 2390 3 | 51 48 -229 1192 -1190 1995 80.8 2112 2112 | 2042 0
brd 2390 4 | 43 43 -124 -746 -38 732 81.8 1878 1878 | 3706 0
brd 2390 5 | -121 154 -39 744 1389 -600 82.6 1804 1804 | 1612 0
brd 2390 6 | 43 40 75 1435 2937 1002 83.1 11820 11820 | 3286 0
-------------+------------------------------------------------------------+----------------
brd 2390 mean| -6 49 -19 330 733 1179 82.7 3232 3232 | 3500 0
brd 2390 sdev| 60 58 129 1347 1329 2496 1.6 3797 3797 | 1268 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 2.2390.0 GPS week: 2390 Day: 0 MJD: 60974
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 30 11 -29 .21 15 13 | 710 309 3081 6809
esa n/a| -4 -2 0 8 3 63 -.05 20 20 | 42 1475 3090 6796
gfz n/a| 1 2 0 34 6 18 -.03 16 15 | 0 728 3114 7094
grg n/a| 0 -2 -5 -36 -71 -93 .26 24 15 | 4152 766 3193 6675
iac n/a| 1 0 1 10 51 83 -.16 16 17 | 7270 329 3192 7894
jgx n/a| 0 0 4 -14 -21 -67 -.16 17 17 | 1378 1897 3245 7604
Table 2.2390.1 GPS week: 2390 Day: 1 MJD: 60975
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 1 -1 7 46 .19 13 13 | -3 -995 3990 7928
esa n/a| -3 1 0 18 -32 71 -.07 22 23 | 933 -1789 3923 8116
gfz n/a| 0 0 -5 30 1 -27 -.07 14 15 | 0 -744 4047 8254
grg n/a| 2 -2 0 -65 -18 -28 .25 13 13 | 4958 -1539 4068 8031
iac n/a| -1 1 0 26 1 -20 -.09 14 15 | 7567 -2491 4049 10606
jgx n/a| 1 0 6 -7 1 -35 -.22 16 16 | 3146 -2479 4245 9043
Table 2.2390.2 GPS week: 2390 Day: 2 MJD: 60976
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 -14 14 -2 .17 14 14 | 1906 1445 3010 7196
esa n/a| -2 0 0 11 -25 96 -.13 18 18 | 1766 1855 3040 7274
gfz n/a| -3 2 -3 48 20 51 -.14 40 37 | 0 2070 3011 7405
grg n/a| 2 -1 2 -31 -27 30 .26 11 11 | 3215 1764 3101 7337
iac n/a| 0 1 -6 26 7 -155 -.24 17 17 | 6493 -118 3087 7610
jgx n/a| 3 -3 7 0 -18 -12 -.26 14 14 | 2802 2894 3203 7818
Table 2.2390.3 GPS week: 2390 Day: 3 MJD: 60977
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 -3 4 14 .18 13 13 | 1303 -2398 3527 8010
esa n/a| -3 -1 1 10 -10 -4 -.10 18 18 | 739 -2732 3534 8062
gfz n/a| 3 -2 -7 23 1 -44 .02 17 16 | 0 -2560 3561 8092
grg n/a| 0 0 3 -54 -40 0 .28 15 15 | 2070 -1049 3276 8013
iac n/a| -1 3 -5 15 22 87 -.17 15 15 | 3469 -342 4005 8453
jgx n/a| 1 -1 4 -4 -7 -87 -.18 16 16 | 3380 -2249 3334 8372
Table 2.2390.4 GPS week: 2390 Day: 4 MJD: 60978
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 6 15 -12 .14 14 14 | 1250 313 3370 8269
esa n/a| -5 0 2 16 5 56 -.08 20 18 | 316 1356 3391 8180
gfz n/a| 2 0 -3 0 -7 32 -.09 13 13 | 0 268 3434 8301
grg n/a| 4 0 6 -16 25 -11 .35 20 20 | 3166 262 3382 7907
iac n/a| 0 0 -3 -11 -37 -19 -.08 13 11 | 5757 -1056 3643 9617
jgx n/a| 1 -1 3 9 38 -11 -.14 16 16 | 3591 398 3553 8630
Table 2.2390.5 GPS week: 2390 Day: 5 MJD: 60979
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 -2 6 25 18 .19 13 13 | 2053 -3379 3574 8323
esa n/a| -3 1 0 -17 4 58 -.10 17 16 | 3190 -3377 3610 8197
gfz n/a| 2 2 -5 -4 -7 8 -.05 15 15 | 0 -2834 3612 8080
grg n/a| 0 -2 8 -19 -12 -37 .30 15 12 | 2947 -3820 3561 8147
iac n/a| 1 -2 -3 17 -5 -20 -.12 12 12 | 5815 -3507 3896 9650
jgx n/a| 1 -1 3 0 1 15 -.15 14 14 | 4387 -4109 3750 8626
Table 2.2390.6 GPS week: 2390 Day: 6 MJD: 60980
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 -1 -32 4 7 .15 15 15 | 1504 700 3256 9463
esa n/a| -3 -3 0 13 -25 24 -.09 25 21 | 2449 197 3286 8529
gfz n/a| 0 1 -2 46 -7 12 -.06 15 15 | 0 190 3249 9537
grg n/a| 2 1 3 -16 -28 -13 .31 15 15 | 2280 1288 3228 9558
iac n/a| 1 -2 -5 -8 34 20 -.21 16 15 | 4616 972 3279 9712
jgx n/a| 0 0 5 18 7 -6 -.16 17 17 | 3555 869 3317 10436
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 3.2390.0 GPS week: 2390 Day: 0 MJD: 60974
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1107 11 28 18 12 9 11 7 | 45 68 53 58 53 47 53
R03 | 1283 12 17 9 16 11 16 6 | 65 71 70 78 69 59 70
R04 | 1595 14 16 12 11 10 12 5 | 77 87 92 89 84 84 88
R05 | 975 8 18 11 15 14 9 5 | 58 75 77 77 80 76 76
R07 | 703 13 20 20 20 16 14 7 | 61 56 76 71 69 55 65
R08 | 2200 19 13 15 11 8 15 6 | 54 68 75 70 67 65 67
R09 | 2557 12 15 15 10 16 7 5 | 18 35 25 22 27 24 23
R11 | 1414 16 25 13 31 26 19 10 | 21 37 26 36 33 19 23
R12 | 1078 14 27 16 37 16 32 11 | 49 47 53 67 47 47 49
R14 | 2069 18 27 17 42 34 17 12 | 43 50 51 64 59 34 44
R15 | 1361 19 14 15 31 18 18 8 | 72 75 69 90 76 66 74
R16 | 1420 27 13 24 44 20 16 11 | 87 79 67 105 69 64 76
R17 | 1009 11 16 14 10 10 10 5 | 25 24 29 27 25 19 22
R18 | 913 12 22 20 12 14 17 7 | 25 28 35 34 35 25 29
XR19 | 7166 14 18 23 --- 21 --- 11 | 14 33 35 --- 34 --- 29
XR20 | 1643 17 --- 357 12 16 --- 11 | 131 --- 219 225 225 --- 221
R21 | 670 11 13 8 9 8 22 5 | 25 33 27 32 26 30 27
XR22 | 982 15 21 12 15 12 --- 7 | 16 22 33 23 22 --- 20
R24 | 1063 16 23 15 15 12 15 7 | 25 38 30 24 28 28 27
XR26 | 5814 53 69 53 --- 59 --- 33 | 135 198 154 --- 183 --- 166
XR27 | 6321 51 80 --- 45 42 --- 32 | 168 193 --- 175 175 --- 171
XR28 |16802 36 --- --- --- 39 --- 38 | 30 --- --- --- 37 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 1436 15 20 16 24 16 17 |T 56 65 64 71 69 46 65
WRMS | 1436 13 20 15 15 17 17 |NE 56 65 64 71 69 46 65
MEDI | 1361 14 18 15 15 16 15 |MD 45 50 53 67 53 47 49
Table 3.2390.1 GPS week: 2390 Day: 1 MJD: 60975
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1445 8 28 8 11 12 11 5 | 26 41 32 29 33 22 30
R03 | 1212 10 16 8 14 9 11 5 | 40 51 57 59 51 50 52
R04 | 1575 14 19 13 13 18 21 7 | 59 64 69 68 74 57 67
R05 | 1562 10 18 16 14 18 11 6 | 38 66 65 57 69 57 59
R07 | 1765 12 35 18 14 17 19 8 | 38 31 58 44 53 31 44
R08 | 1454 13 15 12 8 14 16 5 | 37 46 58 51 55 46 50
R09 | 1153 13 14 13 12 14 13 6 | 23 33 35 20 29 25 24
XR11 | 1502 18 17 19 18 16 --- 9 | 24 28 23 34 37 --- 26
R12 | 2505 14 33 12 16 13 19 8 | 36 54 45 50 43 35 42
R14 | 1543 10 21 17 16 13 16 7 | 29 40 45 37 40 24 33
R15 | 1354 12 19 12 12 14 17 6 | 45 45 46 45 53 39 46
R16 | 1057 20 16 9 14 10 16 6 | 51 52 46 47 46 37 45
R17 | 996 19 23 12 11 10 16 6 | 21 22 25 26 28 15 21
R18 | 1178 10 22 22 17 20 13 8 | 22 17 30 37 25 17 22
XR19 | 3752 18 16 16 --- 20 --- 10 | 21 25 37 --- 29 --- 23
XR20 | 1581 11 --- 343 17 18 --- 11 | 109 --- 159 164 157 --- 159
R21 | 872 10 18 12 9 12 17 5 | 22 28 32 23 23 19 22
XR22 | 1050 14 18 12 11 12 --- 6 | 17 20 26 25 26 --- 20
R24 | 1370 14 18 13 10 11 14 6 | 26 32 32 25 28 35 28
XR26 |11748 29 111 32 --- 64 --- 31 | 145 179 148 --- 174 --- 164
XR27 | 8820 40 89 --- 25 65 --- 32 | 170 184 --- 172 174 --- 167
XR28 |13966 49 --- --- --- 52 --- 51 | 64 --- --- --- 46 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 1453 13 22 14 13 14 16 |T 48 52 53 53 58 33 53
WRMS | 1453 13 23 15 13 15 16 |NE 48 52 53 53 58 33 53
MEDI | 1454 13 18 13 14 14 16 |MD 36 40 45 44 43 35 42
Table 3.2390.2 GPS week: 2390 Day: 2 MJD: 60976
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1595 7 15 37 9 19 9 6 | 43 43 57 48 44 42 44
R03 | 2932 5 15 56 6 25 19 9 | 54 53 78 57 72 49 56
R04 | 2442 11 11 30 9 15 16 6 | 53 56 69 63 64 55 60
R05 | 2468 10 15 30 9 19 10 6 | 51 58 68 62 65 54 60
R07 | 3258 13 28 71 11 22 13 11 | 61 52 98 53 64 47 56
R08 | 1015 17 21 15 10 10 9 6 | 58 56 51 64 60 57 59
R09 | 1421 12 19 71 13 16 16 10 | 35 53 90 43 41 36 42
XR11 | 1920 15 20 34 14 18 --- 9 | 29 38 39 33 42 --- 31
R12 | 2655 20 20 28 17 18 12 8 | 51 52 55 51 43 46 47
R14 | 2804 11 25 41 9 18 16 8 | 51 64 64 58 43 49 51
R15 | 2829 17 13 44 9 14 20 8 | 50 52 74 55 45 45 50
R16 | 1458 21 13 17 14 18 13 7 | 60 54 54 53 56 48 53
R17 | 953 18 20 30 10 16 17 7 | 35 39 44 36 26 25 31
R18 | 775 13 12 33 12 12 10 6 | 33 34 35 38 29 31 32
XR19 | 3511 23 17 95 --- 16 --- 21 | 39 51 83 --- 43 --- 45
XR20 | 2029 10 --- 367 8 13 --- 7 | 93 --- 201 176 169 --- 176
R21 | 1312 17 21 20 10 17 10 7 | 34 45 44 41 33 40 38
XR22 | 743 16 20 76 12 17 --- 13 | 27 26 86 34 30 --- 29
R24 | 1518 14 19 20 8 14 17 6 | 32 31 39 34 26 31 30
XR26 |10348 65 79 161 --- 40 --- 45 | 66 138 152 --- 101 --- 105
XR27 | 6216 41 49 --- 38 67 --- 27 | 73 80 --- 57 81 --- 68
XR28 |13044 49 --- --- --- 56 --- 52 | 76 --- --- --- 50 --- 64
------+-----------------------------------------+-------------------------------------
RMS | 2120 14 18 40 11 17 14 |T 50 53 74 55 55 43 55
WRMS | 2120 14 18 37 11 17 14 |NE 50 53 74 55 55 43 55
MEDI | 2029 15 19 34 10 17 13 |MD 51 52 64 53 44 46 50
Table 3.2390.3 GPS week: 2390 Day: 3 MJD: 60977
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1308 4 25 11 9 12 9 5 | 37 57 43 39 36 35 41
R03 | 1219 7 9 16 13 20 10 6 | 47 55 50 60 64 52 55
R04 | 2131 10 12 11 9 15 8 5 | 49 47 54 45 46 52 48
R05 | 1551 8 12 22 10 14 20 6 | 42 50 67 53 43 32 47
R07 | 3471 10 19 21 14 11 19 7 | 50 64 75 53 64 47 59
R08 | 1106 13 20 13 11 14 11 6 | 47 53 68 61 66 59 59
R09 | 2067 15 19 15 23 18 11 7 | 18 33 30 25 26 20 18
R11 | 1915 14 21 11 28 14 13 8 | 18 38 30 17 28 23 21
R12 | 1972 12 15 11 20 17 14 6 | 52 50 52 40 58 39 48
R14 | 3337 8 12 17 15 21 24 7 | 35 47 50 47 43 36 41
R15 | 3732 13 16 23 11 11 30 8 | 49 38 63 52 42 33 44
R16 | 1356 20 12 21 13 13 19 7 | 55 48 60 50 41 35 46
R17 | 1125 20 12 19 21 14 15 8 | 22 18 28 21 20 14 15
R18 | 787 17 23 13 11 15 11 7 | 19 32 23 25 21 24 21
XR19 | 1221 12 11 15 --- 12 --- 7 | 21 35 51 --- 36 --- 34
XR20 | 4175 8 --- 342 20 19 --- 11 | 82 --- 154 83 65 --- 72
R21 | 1946 13 27 22 13 17 13 8 | 24 37 21 26 19 23 20
XR22 | 1306 13 14 11 14 15 --- 6 | 16 23 22 21 20 --- 16
R24 | 1880 15 18 14 9 16 19 7 | 21 24 25 23 23 22 19
XR26 |10401 30 120 35 --- 58 --- 30 | 101 123 114 --- 97 --- 90
XR27 | 6950 49 60 --- 36 56 --- 29 | 109 128 --- 111 129 --- 116
XR28 |13545 27 --- --- --- 32 --- 29 | 63 --- --- --- 74 --- 68
------+-----------------------------------------+-------------------------------------
RMS | 2112 13 18 17 15 15 16 |T 44 50 54 44 48 34 45
WRMS | 2112 13 18 16 15 15 16 |NE 44 50 54 44 48 34 45
MEDI | 1915 13 16 15 13 15 13 |MD 42 47 50 45 42 33 44
Table 3.2390.4 GPS week: 2390 Day: 4 MJD: 60978
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1497 9 21 15 17 9 14 6 | 36 45 47 34 46 37 41
R03 | 791 12 21 8 23 8 17 6 | 43 43 53 66 53 45 51
R04 | 1700 12 17 8 9 10 12 5 | 46 48 52 57 55 59 55
R05 | 696 13 14 10 11 11 10 5 | 44 56 52 57 54 53 54
R07 | 2061 14 20 14 14 12 12 6 | 45 50 48 49 56 43 50
R08 | 875 18 42 10 14 13 15 9 | 39 68 49 57 45 55 51
R09 | 2986 14 13 14 22 9 14 6 | 19 25 31 24 27 25 22
R11 | 2625 12 18 14 30 16 7 7 | 17 28 20 29 30 21 19
R12 | 1484 16 12 18 26 23 14 8 | 43 48 35 45 62 41 46
R14 | 1957 13 17 11 27 20 22 8 | 40 49 38 43 45 31 40
R15 | 3637 19 10 13 17 8 24 7 | 38 47 45 49 44 38 43
R16 | 1414 17 14 14 16 7 21 6 | 48 48 56 52 56 46 52
R17 | 1829 12 13 7 20 9 18 6 | 25 23 25 29 22 22 23
R18 | 676 15 22 19 24 18 19 8 | 27 21 26 27 31 15 22
XR19 | 2297 15 17 13 --- 13 --- 8 | 38 39 38 --- 49 --- 44
XR20 | 5119 12 --- 353 14 7 --- 7 | 132 --- 187 183 180 --- 179
R21 | 1838 13 18 11 20 10 10 6 | 30 40 31 38 29 31 30
XR22 | 1813 13 17 26 30 13 --- 10 | 21 27 37 29 20 --- 22
R24 | 934 19 21 13 17 18 20 8 | 24 29 26 27 26 23 23
XR26 | 8398 50 64 40 --- 57 --- 30 | 85 127 123 --- 125 --- 107
XR27 |10848 60 69 --- 55 48 --- 33 | 81 127 --- 101 109 --- 101
XR28 |15641 32 --- --- --- 26 --- 29 | 87 --- --- --- 44 --- 66
------+-----------------------------------------+-------------------------------------
RMS | 1877 14 20 13 20 13 16 |T 45 49 50 52 54 36 51
WRMS | 1877 14 18 13 20 11 16 |NE 45 49 50 52 54 36 51
MEDI | 1829 14 17 13 20 12 14 |MD 39 45 38 45 45 37 44
Table 3.2390.5 GPS week: 2390 Day: 5 MJD: 60979
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 891 11 18 16 18 12 12 6 | 48 39 42 34 31 34 35
R03 | 1988 9 24 23 9 12 18 7 | 64 38 54 41 45 36 43
R04 | 1717 12 21 13 7 8 9 5 | 69 52 61 58 59 63 59
R05 | 899 8 13 13 8 11 6 4 | 59 56 52 53 50 52 52
R07 | 1734 11 14 20 10 13 10 6 | 59 47 55 44 43 41 45
R08 | 1485 9 26 15 21 14 14 7 | 55 53 52 47 38 38 43
R09 | 2467 14 15 14 13 10 14 6 | 18 26 32 19 24 20 20
R11 | 3066 15 13 12 22 12 8 6 | 21 31 23 22 25 18 19
R12 | 1032 18 14 16 26 8 8 7 | 57 40 37 40 36 41 38
R14 | 1538 10 11 11 15 21 13 6 | 43 43 42 36 54 36 40
R15 | 3429 16 10 14 22 14 23 7 | 54 36 40 32 42 27 35
R16 | 960 13 20 17 12 9 18 6 | 60 43 58 46 45 32 43
R17 | 1830 12 15 18 10 11 9 5 | 20 18 22 22 17 14 16
R18 | 687 14 18 13 16 10 16 6 | 21 25 33 25 22 18 22
XR19 | 1394 13 19 10 --- 16 --- 8 | 29 41 36 --- 53 --- 41
XR20 | 5229 9 --- 364 7 9 --- 6 | 136 --- 147 157 161 --- 160
R21 | 876 17 18 16 11 11 17 6 | 23 28 27 24 20 20 20
XR22 | 1770 15 20 21 10 9 --- 7 | 16 29 23 23 17 --- 15
R24 | 1473 13 13 12 9 13 15 6 | 26 28 23 25 15 22 19
XR26 | 8912 57 62 51 --- 58 --- 33 | 87 90 52 --- 85 --- 62
XR27 | 9188 67 67 --- 45 59 --- 35 | 83 110 --- 81 99 --- 88
XR28 |22406 76 --- --- --- 71 --- 73 | 70 --- --- --- 81 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 1804 13 17 15 15 12 14 |T 50 43 45 43 48 32 44
WRMS | 1804 13 16 15 12 12 14 |NE 50 43 45 43 48 32 44
MEDI | 1717 13 18 15 12 12 13 |MD 54 39 40 36 42 32 40
Table 3.2390.6 GPS week: 2390 Day: 6 MJD: 60980
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 997 12 25 9 12 15 8 6 | --- 65 51 45 50 44 50
R03 | 3320 13 26 21 7 7 22 7 | --- 59 80 76 72 60 70
R04 | 1401 14 35 15 8 14 13 7 | --- 66 86 78 85 73 81
R05 | 846 13 20 14 7 16 12 6 | --- 68 75 73 68 67 71
R07 |46901 15 21 13 12 14 14 6 | --- 62 65 68 67 54 64
R08 | 1087 12 22 13 9 16 11 6 | --- 72 63 65 59 62 63
R09 | 1770 18 10 20 17 16 20 8 | --- 27 42 21 29 19 23
R11 | 2260 15 50 20 29 19 14 11 | --- 33 33 18 30 24 21
R12 | 921 18 17 9 25 15 9 7 | --- 52 52 45 58 48 52
R14 | 1241 11 17 21 17 11 18 7 | --- 60 68 59 62 45 56
R15 | 2048 8 21 12 9 26 19 7 | --- 52 66 62 74 49 61
R16 | 875 19 17 14 12 21 18 7 | --- 49 55 54 57 44 52
R17 | 1746 12 16 9 8 12 10 5 | --- 22 21 21 17 15 17
R18 | 632 14 15 16 21 12 25 8 | --- 19 22 27 19 17 17
XR19 | 1485 13 11 19 --- 16 --- 9 | --- 39 38 --- 41 --- 38
XR20 | 2027 11 --- 378 12 15 --- 9 | --- --- 211 210 213 --- 211
R21 | 783 14 36 9 13 14 23 8 | --- 38 23 27 20 22 21
XR22 | 1584 13 28 16 9 14 --- 8 | --- 33 28 23 20 --- 21
R24 | 1334 20 15 7 15 14 19 7 | --- 23 23 25 22 23 21
XR26 | 9165 31 102 28 --- 64 --- 30 | --- 117 68 --- 93 --- 66
XR27 | 8596 36 106 --- 24 62 --- 30 | --- 145 --- 104 126 --- 107
XR28 |17603 39 --- --- --- 44 --- 42 | --- --- --- --- 65 --- 54
------+-----------------------------------------+-------------------------------------
RMS |11824 15 25 14 15 16 17 |T --- 55 58 57 61 41 56
WRMS |11824 15 21 15 15 15 17 |NE --- 55 58 57 61 41 56
MEDI | 1485 14 21 14 12 15 14 |MD --- 52 52 54 58 44 52
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