[IGSREPORT-30669] Wk 2389 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 7 03:26:19 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2389 (Oct 19, 2025 - Oct 25, 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 2.2389.
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:
igl2389[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2389 in the SP3 format.
igl23897.sum Combination Report for GPS Week 2389.
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 | 5.2 ns
1 | 6.9 ns
2 | 4.7 ns
3 | 3.8 ns
4 | 5.3 ns
5 | 3.9 ns
6 | 3.9 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
1 | GFZ | R20
1 | GRG | R27
2 | GFZ | R20
3 | ALL | R27
3 | GFZ | R20
4 | GFZ | R20
5 | ALL | R19
5 | GFZ | R20
6 | ALL | R19
6 | GFZ | R20
6 | GRG | R14
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 1.2389, 1a.2389).
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 2.2389.0-6)
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 3.2389.0-6).
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 2389 summary. (Oct 19, 2025 - Oct 25, 2025)
Table 1.2389.a GPS week : 2389 MJD: 60967.0-60973.0
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 -4 5 8 .15 14 13 | 458 -330 3276 7287
| 0 0 1 16 11 24 .03 | 1648 2242
esa n/a| -2 -1 0 1 12 39 -.11 20 20 | 2029 -491 3469 7521
| 1 1 1 13 18 28 .04 | 3715 1933
gfz n/a| 0 0 0 26 1 -9 .01 16 16 | 0 -326 3288 7148
| 1 1 2 10 14 30 .03 | 0 2072
grg n/a| 1 0 0 -12 -12 14 .29 19 14 | 4828 -689 3220 6717
| 0 1 2 17 15 41 .05 | 1019 2002
iac n/a| 0 0 -2 10 9 -43 -.17 17 18 | 6962 -810 3405 8253
| 2 1 1 16 19 100 .07 | 826 961
jgx n/a| 0 0 3 -15 0 0 -.18 14 14 | 2680 -651 3266 7301
| 0 1 2 14 17 24 .03 | 1109 2249
Table 1.2389.b GPS week : 2389 MJD: 60967.0-60973.0
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 7 6 7 7 7 7 |
R03 | 6 4 6 6 9 8 6 |
R04 | 7 6 6 6 8 10 7 |
R05 | 6 5 6 6 6 8 7 |
R07 | 8 9 7 7 7 6 5 |
R08 | 6 7 8 7 8 6 7 |
R09 | 6 7 6 6 7 12 7 |
R11 | 7 6 8 10 7 6 12 |
R12 | 8 6 7 6 6 6 11 |
R14 | 7 7 7 6 7 8 11 |
R15 | 6 7 8 8 7 8 10 |
R16 | 8 12 9 9 11 8 9 |
R17 | 7 7 6 6 6 7 5 |
R18 | 7 9 9 7 8 7 7 |
R19 | 10 10 8 7 25 --- --- |
R20 | 11 6 10 10 9 10 9 |
R21 | 7 7 7 7 8 7 7 |
R22 | 7 7 9 7 8 8 7 |
R24 | 7 7 8 7 7 7 7 |
R26 | 27 32 31 30 31 33 32 |
R27 | 28 28 62 --- 27 28 30 |
R28 | 47 64 80 57 63 81 53 |
Table 1.2389.c GPS week : 2389 MJD: 60967.0-60973.0
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 2389 0 | -130 111 -95 -480 1880 -16050 76.8 1814 1814 | 5233 0
brd 2389 1 | -46 18 -168 -3238 -742 -13950 81.3 1547 1547 | 6850 0
brd 2389 2 | 97 42 34 -3956 2459 -12070 79.0 1804 1804 | 4650 0
brd 2389 3 | -36 -48 11 -3488 269 -14400 77.6 2053 2053 | 3788 0
brd 2389 4 | 62 39 100 -1313 1076 -20390 78.8 1824 1824 | 5348 0
brd 2389 5 | 1 -8 57 -516 3858 -11870 81.0 1571 1571 | 3901 0
brd 2389 6 | 29 95 -26 -1205 1291 -9059 79.0 1510 1510 | 3943 0
-------------+------------------------------------------------------------+----------------
brd 2389 mean| -3 35 -12 -2028 1441 -13969 79.1 1731 1731 | 4816 0
brd 2389 sdev| 76 55 93 1482 1492 3602 1.6 196 196 | 1101 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 2.2389.0 GPS week: 2389 Day: 0 MJD: 60967
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 12 15 31 .16 13 12 | -2062 -2380 3053 7932
esa n/a| -3 -2 -1 8 17 22 -.11 19 20 | -657 -2173 3082 8072
gfz n/a| 0 -2 0 39 -10 -11 -.00 15 15 | 0 -2148 3065 7454
grg n/a| 1 0 0 -29 18 51 .26 15 12 | 5666 -2014 3083 6921
iac n/a| 0 2 -1 -6 -5 -58 -.16 13 13 | 7885 -2799 3161 8906
jgx n/a| 0 1 5 -26 5 -36 -.19 16 16 | 1116 -2320 3163 7294
Table 2.2389.1 GPS week: 2389 Day: 1 MJD: 60968
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 0 -7 11 -24 .17 14 13 | -1217 2233 3633 7104
esa n/a| -2 0 1 10 17 12 -.14 21 21 | 272 1390 3603 6882
gfz n/a| 1 -2 -3 17 12 -67 .03 16 17 | 0 2026 3667 6604
grg n/a| 1 0 1 -22 -30 67 .26 16 13 | 6236 429 3599 5609
iac n/a| 0 0 -3 28 -9 3 -.11 14 17 | 8375 -475 3682 8838
jgx n/a| 0 0 5 -28 32 0 -.20 16 16 | 2591 1037 3452 5870
Table 2.2389.2 GPS week: 2389 Day: 2 MJD: 60969
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 -2 12 20 .14 13 11 | 598 926 3286 8134
esa n/a| -1 0 -1 -5 22 73 -.06 20 18 | 484 399 3292 7979
gfz n/a| 0 0 -2 24 -3 -12 .06 14 14 | 0 1037 3255 7855
grg n/a| 0 0 0 -16 -21 46 .22 16 15 | 3780 1326 3259 7530
iac n/a| 0 1 -1 30 19 -78 -.12 17 16 | 6437 143 3303 8645
jgx n/a| 0 0 5 -18 -17 -17 -.19 15 15 | 2586 1086 3301 8300
Table 2.2389.3 GPS week: 2389 Day: 3 MJD: 60970
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 10 13 34 .12 14 13 | 1018 -2014 3731 7670
esa n/a| -3 0 -1 -1 5 49 -.07 20 18 | 10192 -2398 4937 9439
gfz n/a| 0 1 1 15 -11 34 .01 15 14 | 0 -2272 3725 7649
grg n/a| 2 -3 -5 5 -12 13 .29 14 14 | 4823 -2511 3273 7299
iac n/a| 3 -2 -3 -1 46 -174 -.19 17 17 | 6365 -948 3949 8800
jgx n/a| 1 0 4 -22 -18 35 -.13 12 12 | 1953 -3041 3382 7956
Table 2.2389.4 GPS week: 2389 Day: 4 MJD: 60971
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 -13 -17 -3 .11 15 14 | 285 2197 3265 6329
esa n/a| -2 -3 2 3 42 41 -.15 23 22 | 195 1417 3333 6562
gfz n/a| -2 0 1 30 17 -5 -.03 17 18 | 0 1738 3299 6404
grg n/a| 2 0 -2 -22 -24 -35 .30 13 12 | 4244 1390 3296 6144
iac n/a| -2 -2 0 22 -1 89 -.31 22 25 | 6434 -272 3590 6797
jgx n/a| 0 2 0 11 -2 -8 -.19 13 13 | 2263 2131 3307 6729
Table 2.2389.5 GPS week: 2389 Day: 5 MJD: 60972
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 7 0 -17 .15 14 13 | 2425 -23 3204 7266
esa n/a| -3 -2 -2 16 0 4 -.15 20 20 | 2059 886 3252 7964
gfz n/a| 0 0 -2 41 -14 -13 .02 19 16 | 0 245 3249 7399
grg n/a| 1 -1 0 -21 -7 -28 .32 19 14 | 3544 175 3252 7143
iac n/a| 0 0 -1 9 16 61 -.11 18 17 | 6856 -328 3342 8112
jgx n/a| 0 0 3 -20 7 0 -.21 14 14 | 4232 -1 3404 7833
Table 2.2389.6 GPS week: 2389 Day: 6 MJD: 60973
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 1 -2 -33 5 22 .22 16 14 | 2164 -3249 2765 6580
esa n/a| -1 -2 0 -25 -14 75 -.07 19 19 | 1660 -2959 2786 5754
gfz n/a| 0 1 1 18 21 5 .01 16 14 | 0 -2912 2756 6675
grg n/a| 2 -1 0 19 -8 -13 .37 41 15 | 5509 -3624 2783 6374
iac n/a| 4 0 -5 -10 0 -149 -.20 18 19 | 6385 -996 2809 7678
jgx n/a| 0 0 0 -1 -10 24 -.12 12 12 | 4024 -3449 2854 7126
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 3.2389.0 GPS week: 2389 Day: 0 MJD: 60967
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1278 9 25 21 11 10 11 6 | 45 55 41 40 45 40 43
R03M | 1934 10 20 12 9 7 16 5 | 82 74 83 84 80 75 80
R04M | 878 9 20 10 15 15 16 6 | 70 66 66 57 68 51 62
R05M | 1762 12 20 15 10 12 16 6 | 57 57 66 51 52 48 54
R07 | 939 6 29 23 12 12 15 7 | 73 56 77 67 74 60 68
R08 | 1638 13 14 14 8 13 11 5 | 59 67 66 66 73 60 64
R09E | 2826 14 11 14 18 8 9 5 | 47 45 54 37 50 47 46
R11E | 1942 13 15 15 16 14 17 6 | 31 37 41 30 33 29 32
R12E | 2969 17 18 17 17 21 18 8 | 41 42 43 47 44 37 41
R14E | 3151 10 23 9 20 17 10 7 | 95 94 97 93 104 96 96
R15E | 1382 12 15 12 19 12 7 6 | 121 125 120 128 116 119 120
R16E | 1496 19 15 18 23 11 15 7 | 69 67 71 66 68 63 65
R17 | 1274 14 17 14 16 8 17 6 | 34 26 33 35 31 27 29
R18 | 745 14 27 19 14 8 11 7 | 26 29 33 30 26 20 25
XR19 | 1505 16 10 13 --- 23 --- 10 | 98 22 104 --- 104 --- 100
XR20 | 1983 10 --- 353 --- 10 --- 10 | 269 --- 268 --- 276 --- 272
R21 | 1342 14 12 7 7 18 25 7 | 39 35 35 38 37 32 34
XR22 | 1668 11 14 11 13 17 --- 6 | 19 24 26 23 23 --- 20
R24 | 1082 15 18 13 13 10 25 7 | 33 40 35 36 37 37 33
XR26 | 8261 43 72 33 --- 39 --- 27 | 49 104 51 --- 78 --- 58
XR27M | 9142 42 55 --- 44 49 --- 27 | 77 98 --- 473 113 --- 89
XR28 |12849 46 --- --- --- 46 --- 46 | 67 --- --- --- 54 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1813 13 19 15 15 13 16 |T 68 58 70 77 72 52 67
WRMS | 1813 12 20 15 12 13 16 |NE 69 44 72 42 73 39 68
MEDI | 1638 13 18 14 14 12 15 |MD 57 55 54 47 54 47 54
Table 3.2389.1 GPS week: 2389 Day: 1 MJD: 60968
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1507 12 28 13 10 22 9 7 | 32 35 32 26 24 23 26
R03M | 1941 8 17 10 7 7 7 4 | 63 57 60 65 65 65 62
R04M | 837 13 20 10 11 7 14 5 | 50 40 49 52 38 38 44
R05M | 1591 7 17 15 13 10 8 5 | 47 48 50 35 43 44 43
R07 | 1425 10 24 28 12 11 27 8 | 47 37 62 40 45 26 42
R08 | 756 16 18 19 14 15 8 7 | 37 38 58 37 51 38 42
R09E | 2154 18 17 22 10 8 12 6 | 25 31 30 22 28 27 24
R11E | 1662 17 17 12 14 9 14 6 | 25 25 34 24 29 33 26
R12E | 2553 9 16 21 15 6 14 6 | 30 35 40 36 34 25 31
R14E | 1446 10 15 13 15 13 18 6 | 74 75 79 78 80 77 76
R15E | 1747 14 18 13 22 15 12 7 | 83 80 88 76 80 74 79
R16E | 1196 17 23 14 29 38 19 11 | 108 116 108 113 84 100 101
R17 | 958 12 25 13 20 9 14 7 | 20 29 29 33 20 21 22
R18 | 678 22 29 15 18 7 24 8 | 20 26 31 18 15 23 18
XR19 | 2100 13 20 14 --- 19 --- 9 | 44 23 48 --- 49 --- 45
XR20 | 2261 9 --- 359 9 7 --- 6 | 210 --- 193 158 216 --- 210
R21 | 1331 12 27 16 7 5 17 6 | 28 23 38 27 24 20 24
XR22 | 1753 14 17 11 7 17 --- 7 | 15 18 24 23 28 --- 18
R24 | 1655 9 10 14 17 10 21 6 | 26 22 30 34 25 20 23
XR26 |11372 32 98 41 --- 56 --- 32 | 41 74 39 --- 49 --- 37
XR27M | 7772 43 51 --- 2516 28 --- 28 | 88 96 --- 9999 77 --- 87
XR28 |14114 67 --- --- --- 59 --- 63 | 90 --- --- --- 72 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 1546 14 21 16 16 14 16 |T 54 46 56 49 53 40 51
WRMS | 1546 13 21 17 13 17 16 |NE 52 32 55 46 54 24 49
MEDI | 1655 13 18 14 14 10 14 |MD 41 35 40 35 43 27 42
Table 3.2389.2 GPS week: 2389 Day: 2 MJD: 60969
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1683 9 8 15 12 19 8 5 | 40 39 45 45 31 36 38
R03M | 1367 9 11 19 14 9 10 5 | 269 273 264 270 274 271 269
R04M | 1159 11 14 11 14 13 19 6 | 62 55 52 64 55 54 56
R05M | 1514 8 18 19 6 9 12 5 | 44 52 52 44 39 35 42
R07 | 1910 11 24 13 16 12 15 7 | 62 61 65 59 64 58 60
R08 | 1068 15 31 9 11 26 10 8 | 51 36 58 58 71 57 55
R09E | 1177 15 13 13 11 11 9 5 | 21 21 25 21 23 19 19
R11E | 1303 12 19 19 26 12 12 7 | 20 36 37 22 27 23 23
R12E | 3430 13 19 10 18 19 9 6 | 28 32 29 34 30 22 26
R14E | 1825 15 17 11 14 17 21 7 | 64 65 77 69 75 75 70
R15E | 3138 13 24 12 21 11 18 7 | 54 55 50 45 54 50 49
R16E | 1673 25 18 17 24 20 9 8 | 133 123 133 108 110 123 122
R17 | 759 11 18 7 9 14 15 5 | 30 20 25 29 32 23 25
R18 | 669 14 27 16 8 31 22 9 | 19 24 20 24 40 15 19
XR19 | 2113 16 13 11 --- 12 --- 7 | 109 25 119 --- 112 --- 111
XR20 | 4156 12 --- 328 8 18 --- 9 | 208 --- 222 150 194 --- 204
R21 | 1281 9 16 17 25 15 10 7 | 29 28 23 42 25 33 26
XR22 | 1588 17 15 14 12 23 --- 8 | 12 24 29 24 27 --- 19
R24 | 2328 13 29 14 12 10 21 7 | 25 36 29 24 28 27 25
XR26 | 8372 45 82 45 --- 47 --- 31 | 51 86 56 --- 67 --- 56
XR27M |12172 53 --- --- --- 70 --- 61 | 101 --- --- --- 135 --- 107
XR28 |18650 71 --- --- --- 90 --- 80 | 77 --- --- --- 89 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 1803 13 20 14 16 17 15 |T 68 57 70 62 72 57 67
WRMS | 1803 11 18 14 14 16 15 |NE 61 37 64 51 68 35 60
MEDI | 1673 13 18 14 12 15 12 |MD 51 36 50 44 54 35 49
Table 3.2389.3 GPS week: 2389 Day: 3 MJD: 60970
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1700 11 12 23 9 14 11 6 | 117 118 118 109 111 111 113
R03M | 1996 8 17 11 17 17 8 6 | 9999 9999 9999 9999 9999 9999 9999
R04M | 1335 12 8 10 10 21 12 5 | 277 272 280 270 265 273 272
R05M | 2409 8 18 8 12 15 10 5 | 208 201 214 207 195 208 205
R07 | 2107 13 23 15 12 12 10 6 | 70 57 52 64 59 63 60
R08 | 2043 11 33 17 11 11 9 7 | 59 73 55 68 67 61 61
R09E | 781 12 11 15 11 18 8 5 | 32 36 34 33 31 35 31
R11E | 2252 15 35 18 24 22 14 9 | 31 35 37 30 33 34 28
R12E | 3931 12 15 9 18 15 8 6 | 40 46 38 41 37 35 37
R14E | 2176 9 22 15 15 11 11 6 | 43 42 45 38 40 35 38
R15E | 2522 16 17 15 16 25 19 8 | 64 64 64 68 55 58 60
R16E | 1766 23 19 24 20 20 15 9 | 181 188 188 186 169 181 181
R17 | 666 16 15 7 10 11 11 5 | 38 35 33 40 32 34 34
R18 | 747 17 18 10 9 17 13 6 | 35 42 41 39 31 36 35
XR19 | 2204 11 12 10 --- 12 --- 6 | 124 25 120 --- 130 --- 120
XR20 | 5638 13 --- 347 11 16 --- 9 | 70 --- 164 99 78 --- 71
R21 | 1224 17 13 18 13 11 13 6 | 40 35 39 40 31 33 33
XR22 | 1130 12 15 13 10 14 --- 6 | 34 38 39 46 31 --- 36
R24 | 2552 15 22 12 11 17 15 7 | 37 41 36 38 35 35 35
XR26 | 7111 52 67 38 --- 51 --- 29 | 55 72 54 --- 68 --- 53
XR28 |16469 53 --- --- --- 61 --- 57 | 72 --- --- --- 36 --- 54
------+-----------------------------------------+-------------------------------------
RMS | 2053 14 20 15 14 17 12 |T 83 83 86 83 79 82 80
WRMS | 2053 13 18 14 14 17 12 |NE 57 46 63 54 54 43 53
MEDI | 2107 13 17 15 11 16 11 |MD 59 46 52 46 55 36 54
Table 3.2389.4 GPS week: 2389 Day: 4 MJD: 60971
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1304 9 15 25 15 16 11 7 | 179 181 188 184 191 174 182
R03M | 1937 10 22 33 10 23 17 9 | 9999 9999 9999 9999 9999 9999 9999
R04M | 1315 9 31 17 9 31 9 7 | 518 523 520 522 527 519 520
R05M | 2254 8 24 14 9 15 7 5 | 381 381 383 377 382 381 380
R07 | 1954 19 20 11 13 21 6 6 | 61 53 61 53 56 57 56
R08 | 1690 8 26 7 9 37 12 7 | 55 56 48 57 63 56 53
R09E | 880 16 19 19 16 12 10 7 | 25 34 39 31 32 32 29
R11E | 1666 14 17 13 14 25 13 7 | 31 35 35 28 38 32 29
R12E | 3248 15 14 10 16 15 11 6 | 36 33 33 35 35 27 30
R14E | 1173 11 18 15 20 19 8 6 | 56 55 54 48 62 50 52
R15E | 2386 16 22 12 18 13 12 7 | 57 51 54 51 59 62 54
R16E | 2183 22 35 19 16 43 18 11 | 82 111 97 89 65 92 87
R17 | 1289 14 11 11 7 15 17 6 | 34 34 28 35 44 31 32
R18 | 700 15 38 14 12 13 8 7 | 29 34 29 29 34 30 28
XR19 |11720 19 --- --- --- 31 --- 25 | 91 --- --- --- 125 --- 100
XR20 | 5342 9 --- 370 10 19 --- 9 | 198 --- 214 88 188 --- 196
R21 | 1065 20 26 18 11 11 15 7 | 31 32 32 31 36 28 28
XR22 | 906 17 19 18 8 10 --- 7 | 23 25 32 26 23 --- 22
R24 | 2245 22 10 9 8 19 20 7 | 34 44 35 34 42 37 35
XR26 | 6902 38 72 43 --- 68 --- 31 | 57 85 65 --- 93 --- 66
XR27M | 7755 30 --- --- 16 65 --- 26 | 120 --- --- 300 141 --- 124
XR28 |17214 48 --- --- --- 82 --- 63 | 69 --- --- --- 48 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1823 15 23 17 13 22 13 |T 103 103 108 112 108 107 102
WRMS | 1823 14 22 18 12 25 13 |NE 62 45 60 44 68 39 60
MEDI | 1937 15 20 15 12 19 11 |MD 57 51 48 48 59 50 53
Table 3.2389.5 GPS week: 2389 Day: 5 MJD: 60972
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1252 9 22 21 8 20 7 6 | 242 238 245 238 239 246 242
R03M | 1557 11 22 19 9 20 22 8 | 9999 9999 9999 9999 9999 9999 9999
R04M | 1321 20 30 21 11 26 18 9 | 740 745 740 746 770 747 746
R05M | 1391 12 23 24 10 17 13 7 | 538 535 528 536 546 533 536
R07 | 1449 11 12 16 15 11 10 5 | 50 53 52 45 46 43 46
R08 | 1020 10 22 16 9 17 8 6 | 42 56 43 44 37 40 42
R09E | 1388 12 18 14 53 28 21 12 | 33 40 40 67 41 40 38
R11E | 1319 12 15 16 11 15 9 5 | 57 53 58 55 51 52 53
R12E | 2235 14 17 17 15 9 9 6 | 63 61 56 72 57 65 62
R14E | 902 13 16 21 29 16 9 8 | 41 42 42 44 46 36 39
R15E | 1365 19 17 25 19 18 12 8 | 56 59 70 65 56 56 58
R16E | 3466 12 19 26 18 16 12 7 | 117 125 122 115 112 111 114
R17 | 1158 19 14 10 10 17 13 6 | 42 39 33 43 36 34 36
R18 | 596 14 28 11 13 10 15 7 | 42 44 42 44 38 39 40
XR20 | 4843 11 --- 390 11 17 --- 9 | 239 --- 220 177 237 --- 240
R21 | 926 9 22 15 13 12 14 6 | 45 50 48 49 40 42 44
XR22 | 1188 14 17 15 12 17 --- 7 | 45 48 53 51 52 --- 49
R24 | 1661 15 13 13 18 16 14 6 | 46 45 46 47 44 48 45
XR26 | 6651 40 65 60 --- 64 --- 32 | 57 86 41 --- 88 --- 63
XR27M | 5282 39 65 --- 40 50 --- 27 | 117 95 --- 281 122 --- 115
XR28 |10398 66 --- --- --- 97 --- 80 | 62 --- --- --- 65 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1571 14 20 19 19 17 14 |T 145 134 152 151 149 142 145
WRMS | 1571 13 20 16 14 17 14 |NE 96 52 98 62 99 41 95
MEDI | 1388 13 19 17 13 17 12 |MD 57 53 53 55 56 48 53
Table 3.2389.6 GPS week: 2389 Day: 6 MJD: 60973
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1277 9 28 13 12 23 8 7 | 355 362 355 353 353 353 354
R03M | 1406 14 17 11 7 14 9 5 | 9999 9999 9999 9999 9999 9999 9999
R04M | 1444 17 24 14 8 7 10 6 | 9999 9999 9999 9999 9999 9999 9999
R05M | 1116 6 24 24 11 9 12 7 | 747 741 748 744 746 745 745
R07 | 845 11 14 15 9 12 7 5 | 68 58 67 62 60 57 61
R08 | 1348 19 10 10 16 16 16 6 | 57 60 60 62 61 54 58
R09E | 2197 21 11 14 18 20 11 7 | 23 24 30 28 28 29 24
R11E | 1697 15 18 14 57 40 12 11 | 35 45 41 57 51 40 37
R12E | 1718 21 16 9 63 17 8 10 | 54 59 54 81 64 57 56
R14E | 1768 16 21 26 122 14 22 10 | 103 110 106 150 101 108 105
R15E | 1254 23 13 22 41 16 14 9 | 99 100 101 106 101 98 98
R16E | 2892 18 19 21 31 23 8 8 | 83 77 74 80 81 74 75
R17 | 759 11 12 10 14 12 6 4 | 34 29 25 32 29 30 27
R18 | 784 15 27 10 13 11 12 6 | 27 28 21 23 25 20 21
XR20 | 2731 13 --- 374 9 14 --- 9 | 278 --- 271 166 270 --- 275
R21 | 1072 14 19 17 17 9 11 6 | 35 31 26 36 33 27 29
XR22 | 1029 16 11 11 22 13 --- 7 | 22 31 29 33 31 --- 26
R24 | 959 18 14 11 18 11 14 6 | 30 32 27 31 26 27 26
XR26 | 7419 47 70 44 --- 58 --- 31 | 26 103 31 --- 83 --- 50
XR27M | 8697 46 71 --- 50 37 --- 30 | 306 261 --- 296 321 --- 314
XR28 |16474 48 --- --- --- 56 --- 52 | 80 --- --- --- 116 --- 88
------+-----------------------------------------+-------------------------------------
RMS | 1509 16 19 16 41 18 12 |T 145 126 140 137 152 122 146
WRMS | 1509 14 18 14 15 19 12 |NE 100 46 101 55 109 35 101
MEDI | 1406 16 18 14 17 14 11 |MD 57 59 54 62 64 54 58
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