[IGSREPORT-30729] Wk 2396 IGLOS Final Orbits
acc
acc at igs.org
Fri Dec 26 12:37:32 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2396 (Dec 07, 2025 - Dec 13, 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 2.2396.
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:
igl2396[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2396 in the SP3 format.
igl23967.sum Combination Report for GPS Week 2396.
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 | 5.7 ns
1 | 5.7 ns
2 | 7.7 ns
3 | 6.3 ns
4 | 3.4 ns
5 | 5.7 ns
6 | 5.6 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
0 | GRG | R05
1 | GFZ | R20
2 | GFZ | R20
3 | GFZ | R20
4 | GFZ | R20
5 | GFZ | R20
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 1.2396, 1a.2396).
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 2.2396.0-6)
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 3.2396.0-6).
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 2396 summary. (Dec 07, 2025 - Dec 13, 2025)
Table 1.2396.a GPS week : 2396 MJD: 61016.0-61022.0
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 -1 -22 14 44 .16 13 13 | 725 -914 3229 9000
| 1 1 2 12 16 12 .03 | 689 1529
esa n/a| -2 0 0 2 -12 35 -.20 22 21 | 2818 -633 3239 8753
| 1 1 1 24 21 34 .05 | 478 1182
gfz n/a| 0 0 -3 19 -5 2 -.03 16 14 | 0 -361 3268 7307
| 1 1 1 20 21 43 .05 | 0 1098
grg n/a| 0 0 6 -12 -39 -43 .31 22 18 | 4889 -494 3211 8819
| 1 1 4 28 11 59 .02 | 1252 1204
iac n/a| 0 0 0 -14 21 -31 -.18 16 16 | 7098 -836 3450 9069
| 1 1 3 19 9 25 .06 | 1358 1578
jgx n/a| 0 0 1 24 0 -36 -.18 17 17 | 3147 -1033 3006 7141
| 0 1 2 14 18 22 .03 | 788 1544
Table 1.2396.b GPS week : 2396 MJD: 61016.0-61022.0
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 | 21 7 8 7 6 7 7 |
R03 | 8 6 7 9 --- --- --- |
R04 | 14 7 9 7 8 6 7 |
R05 | 12 10 8 8 6 6 8 |
R07 | 8 12 8 6 7 7 8 |
R08 | 11 7 10 7 8 8 7 |
R09 | 7 6 7 6 6 6 6 |
R11 | 6 9 7 8 7 10 15 |
R12 | 6 8 8 8 7 7 6 |
R14 | 5 6 5 5 6 4 7 |
R15 | 7 7 8 6 8 8 7 |
R16 | 9 6 7 8 7 6 8 |
R17 | 8 7 6 9 9 7 7 |
R18 | 7 7 7 7 8 7 7 |
R19 | 9 8 8 10 8 8 11 |
R20 | 21 20 17 13 16 15 12 |
R21 | 8 7 7 6 8 7 8 |
R22 | 6 6 9 8 9 7 7 |
R24 | 10 8 9 10 9 8 7 |
R26 | 62 28 29 27 26 29 31 |
R27 | 25 25 23 27 26 26 25 |
R28 | 40 44 51 86 87 26 28 |
Table 1.2396.c GPS week : 2396 MJD: 61016.0-61022.0
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 2396 0 | 30 19 34 -31 -982 5439 81.4 1953 1953 | 5662 0
brd 2396 1 | 8 42 52 -3 415 4596 77.7 2358 2358 | 5730 0
brd 2396 2 | -32 32 65 -740 792 5714 80.7 2716 2716 | 7716 0
brd 2396 3 | -24 121 -93 -433 1362 8610 83.5 2178 2178 | 6344 0
brd 2396 4 | -60 137 -171 -591 1881 8600 79.4 2158 2158 | 3429 0
brd 2396 5 | 73 17 -369 1881 472 16000 79.4 2482 2482 | 5674 0
brd 2396 6 | 28 -92 -415 2126 -3817 17440 81.0 2774 2774 | 5614 0
-------------+------------------------------------------------------------+----------------
brd 2396 mean| 3 39 -128 315 17 9485 80.4 2374 2374 | 5738 0
brd 2396 sdev| 45 76 200 1186 1912 5192 1.8 303 303 | 1267 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 2.2396.0 GPS week: 2396 Day: 0 MJD: 61016
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 2 0 -27 18 47 .14 14 13 | 50 -1028 2972 8722
esa n/a| -2 1 -2 2 -23 24 -.14 19 19 | 3078 -1903 3030 8755
gfz n/a| 0 -1 -1 39 -13 -26 -.09 17 13 | 0 -1528 3011 7620
grg n/a| 2 1 14 -71 -49 -14 .29 44 20 | 5756 -1550 2951 8787
iac n/a| -1 0 -1 4 40 -19 -.08 16 19 | 7117 -1247 3009 8941
jgx n/a| 0 0 -1 33 -26 -26 -.12 19 19 | 2560 -2646 2932 7502
Table 2.2396.1 GPS week: 2396 Day: 1 MJD: 61017
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 -14 -12 61 .13 13 13 | 886 -1686 3139 8773
esa n/a| -3 -2 1 -21 -5 7 -.23 22 20 | 3389 -2105 3180 7724
gfz n/a| 0 0 -4 40 13 58 -.09 18 16 | 0 -1690 3199 7878
grg n/a| 0 0 9 3 -38 -76 .30 16 15 | 6260 -1837 3049 8094
iac n/a| 0 -1 -2 -43 22 -58 -.19 15 16 | 8338 -2311 3184 9232
jgx n/a| 1 -1 1 39 10 -22 -.15 21 21 | 2364 -1100 3027 7679
Table 2.2396.2 GPS week: 2396 Day: 2 MJD: 61018
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 -23 7 29 .13 11 9 | 505 1081 4201 8949
esa n/a| -2 0 1 -30 -26 -5 -.26 21 19 | 2487 452 4278 8555
gfz n/a| 0 0 -3 22 1 37 -.05 17 16 | 0 1044 4284 8207
grg n/a| 0 -1 4 -19 -22 -69 .32 17 17 | 6330 717 4095 8415
iac n/a| 0 -2 -6 14 19 -18 -.23 18 18 | 7380 1661 4189 9561
jgx n/a| 1 1 1 27 30 -63 -.20 19 19 | 3896 -1015 3095 6895
Table 2.2396.3 GPS week: 2396 Day: 3 MJD: 61019
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 -1 -34 13 45 .22 16 16 | 1152 1095 3155 8537
esa n/a| 0 0 0 36 -31 68 -.14 21 19 | 3102 659 3135 8220
gfz n/a| 0 -1 -5 8 17 -17 -.01 15 11 | 0 950 3234 7074
grg n/a| -2 0 5 -11 -28 -85 .29 20 19 | 4685 1495 3166 8301
iac n/a| 1 -1 0 -21 15 -16 -.14 14 14 | 9247 -1567 3906 9127
jgx n/a| 1 0 3 21 9 -25 -.19 15 15 | 2337 2151 3112 6944
Table 2.2396.4 GPS week: 2396 Day: 4 MJD: 61020
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 -21 38 29 .17 12 11 | -346 -1846 2996 9308
esa n/a| -1 2 -2 -5 -30 91 -.20 23 23 | 1949 -1039 2918 9833
gfz n/a| 1 0 0 -17 -15 38 .03 14 13 | 0 -948 3075 7642
grg n/a| -1 -1 7 20 -42 -114 .33 20 22 | 3094 -1055 3017 9361
iac n/a| 0 0 -2 -14 16 -74 -.19 16 15 | 5508 -2766 3491 8837
jgx n/a| 0 0 3 25 -11 -14 -.21 18 18 | 2889 -1547 2990 7813
Table 2.2396.5 GPS week: 2396 Day: 5 MJD: 61021
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 -36 7 58 .14 13 13 | 1563 -970 2871 8783
esa n/a| -3 0 0 12 1 19 -.16 24 22 | 2988 -1056 2862 8608
gfz n/a| 2 1 -3 27 0 -61 .03 11 12 | 0 -217 2871 5836
grg n/a| 0 0 4 0 -56 8 .33 19 16 | 4184 -707 2893 8711
iac n/a| 0 0 3 -13 23 -3 -.16 15 15 | 6288 306 3048 8230
jgx n/a| 0 1 2 -5 -11 -32 -.21 16 16 | 4166 -911 2883 5724
Table 2.2396.6 GPS week: 2396 Day: 6 MJD: 61022
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 0 28 39 .17 12 12 | 1268 -3046 3273 9933
esa n/a| 0 0 -2 24 26 39 -.27 22 23 | 2739 557 3270 9581
gfz n/a| 0 3 -4 14 -45 -13 -.05 17 15 | 0 -143 3204 6898
grg n/a| 0 -2 -1 -11 -37 50 .35 15 15 | 3920 -525 3310 10070
iac n/a| -1 2 4 -30 11 -28 -.27 17 19 | 5811 66 3323 9557
jgx n/a| 1 0 0 28 -5 -72 -.20 14 14 | 3819 -2167 3006 7434
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 3.2396.0 GPS week: 2396 Day: 0 MJD: 61016
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2759 14 16 20 84 55 --- 21 | 56 58 59 90 75 --- 56
R03E | 1676 12 16 22 19 12 22 7 | 59 46 58 60 64 42 58
R04E | 2389 21 13 14 84 20 17 14 | 143 143 148 164 140 142 143
R05E | 991 21 17 16 136 34 25 12 | 164 163 160 213 161 164 161
R07E | 1634 10 19 26 23 13 16 8 | 123 117 122 119 121 116 119
R08E | 2023 12 16 35 31 24 19 10 | 94 92 109 93 89 99 94
R09 | 3545 9 25 22 11 7 10 6 | 24 42 22 23 27 27 24
R11 | 1718 12 14 12 23 8 8 5 | 32 45 33 28 26 27 28
R12 | 2030 16 7 12 14 9 14 5 | 82 77 73 65 72 60 71
R14 | 612 13 13 12 12 9 10 5 | 69 71 71 68 76 68 70
R15 | 1026 13 13 9 16 14 20 6 | 95 82 82 85 89 72 84
R16 | 617 16 21 16 28 15 21 8 | 88 83 79 68 80 69 78
R17 | 723 14 25 6 15 12 25 7 | 43 30 36 46 39 25 35
R18 | 743 15 25 13 11 16 12 7 | 29 34 26 26 24 17 22
XR19 | 2115 13 24 9 --- 13 --- 9 | 28 40 29 --- 35 --- 30
XR20 | 7271 23 --- 378 26 34 --- 20 | 29 --- 233 30 45 --- 29
R21 | 723 11 18 18 19 18 24 8 | 42 36 56 55 52 27 43
R22 | 2535 11 14 13 17 8 18 6 | 20 26 30 31 26 13 23
R24 | 3907 14 33 8 28 19 26 9 | 48 29 45 63 58 31 44
XR26E |15721 62 --- --- --- 61 --- 62 | 47 --- --- --- 35 --- 40
XR27E | 7169 42 35 --- 39 51 --- 25 | 27 42 --- 39 34 --- 30
XR28 |19653 41 --- --- --- 39 --- 40 | 109 --- --- --- 80 --- 86
------+-----------------------------------------+-------------------------------------
RMS | 1953 14 19 17 44 16 19 |T 65 66 77 71 65 62 62
WRMS | 1953 13 19 13 20 19 19 |NE 52 49 62 49 52 39 47
MEDI | 2023 14 17 14 23 15 18 |MD 48 46 59 63 58 42 44
Table 3.2396.1 GPS week: 2396 Day: 1 MJD: 61017
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 3119 9 14 13 19 16 --- 7 | 58 59 61 57 58 --- 56
R03E | 3244 12 14 18 14 6 16 6 | 39 25 39 41 39 20 37
R04E | 3024 13 17 12 18 9 25 7 | 111 102 110 105 108 105 106
R05E | 1885 14 20 15 21 34 26 10 | 163 165 168 162 154 164 162
R07E | 2694 9 20 48 24 10 26 11 | 99 95 118 98 96 95 98
R08E | 1791 9 24 21 14 12 20 7 | 79 83 87 74 77 75 78
R09 | 4275 11 19 13 10 14 12 6 | 18 28 19 20 19 20 18
R11 | 1260 17 40 22 14 13 8 9 | 26 46 28 30 19 22 21
R12 | 1534 23 18 12 19 8 14 7 | 69 62 62 52 59 52 59
R14 | 814 11 13 9 14 16 21 6 | 50 46 55 40 52 39 47
R15 | 1091 14 17 10 12 14 22 6 | 64 61 63 58 52 47 57
R16 | 685 16 16 8 7 11 11 5 | 60 52 55 55 54 52 55
R17 | 767 10 15 8 15 11 35 7 | 34 28 30 37 32 23 31
R18 | 679 13 21 11 12 16 17 6 | 27 31 25 31 23 19 24
XR19 | 3159 15 14 10 --- 16 --- 8 | 24 33 27 --- 25 --- 25
XR20 | 6496 14 --- 393 27 37 --- 19 | 25 --- 137 24 48 --- 27
R21 | 788 8 28 10 16 14 21 7 | 37 30 31 40 33 28 32
XR22 | 983 12 17 11 10 12 --- 6 | 25 26 28 31 24 --- 24
R24 | 4849 7 30 8 13 19 22 7 | 38 25 31 48 42 28 35
XR26E |11558 33 52 55 --- 56 --- 28 | 32 39 45 --- 26 --- 23
XR27E |11062 34 41 --- 31 59 --- 24 | 28 46 --- 28 29 --- 27
XR28 |15590 42 --- --- --- 46 --- 44 | 95 --- --- --- 58 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 2358 13 22 18 16 15 21 |T 54 54 60 54 51 52 50
WRMS | 2358 13 20 16 15 16 21 |NE 42 39 45 38 38 33 37
MEDI | 1885 13 18 12 14 14 21 |MD 38 46 45 41 42 39 35
Table 3.2396.2 GPS week: 2396 Day: 2 MJD: 61018
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2301 10 13 16 21 16 --- 7 | 44 38 41 44 39 --- 40
R03E | 4507 10 14 16 12 20 16 6 | 44 44 44 45 41 41 42
R04E | 3231 15 20 16 28 14 22 8 | 68 66 69 70 65 64 65
R05E | 1737 18 16 15 19 14 21 7 | 109 106 106 125 114 114 111
R07E | 3306 9 20 22 17 18 22 8 | 60 66 66 62 70 63 62
R08E | 1694 10 20 39 19 11 23 10 | 61 66 79 67 64 57 63
R09 | 5081 10 19 12 10 30 13 7 | 16 27 26 18 28 19 17
R11 | 1831 8 24 13 15 15 13 6 | 23 37 31 23 29 30 24
R12 | 1329 8 18 15 25 17 22 7 | 67 76 72 61 76 52 66
R14 | 873 5 12 7 17 17 9 5 | 58 59 60 49 69 61 58
R15 | 2243 12 21 14 12 23 27 8 | 77 65 67 77 86 60 72
R16 | 556 12 16 19 10 18 17 6 | 66 70 63 66 68 54 64
R17 | 943 10 14 9 12 13 23 6 | 37 31 35 37 32 22 32
R18 | 876 5 24 17 13 18 16 6 | 25 32 36 28 25 24 25
XR19 | 3385 10 19 12 --- 16 --- 8 | 27 31 35 --- 35 --- 30
XR20 | 4131 10 --- 396 21 41 --- 16 | 24 --- 186 24 46 --- 21
R21 | 990 11 25 10 17 14 14 6 | 36 27 27 39 29 25 29
XR22 | 1071 14 15 26 13 11 --- 8 | 18 26 40 28 25 --- 23
R24 | 4834 7 38 10 18 27 22 9 | 41 36 34 50 52 30 39
XR26E | 8431 26 62 56 --- 63 --- 28 | 27 33 61 --- 22 --- 28
XR27E |10044 29 45 --- 31 61 --- 23 | 30 54 --- 41 37 --- 36
XR28 |13979 33 --- --- --- 76 --- 51 | 46 --- --- --- 66 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 2715 11 21 17 17 18 19 |T 45 49 58 50 50 47 44
WRMS | 2715 9 19 16 17 18 19 |NE 40 43 54 41 47 37 38
MEDI | 2243 10 19 15 17 17 21 |MD 41 38 44 45 41 52 39
Table 3.2396.3 GPS week: 2396 Day: 3 MJD: 61019
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1746 11 13 13 21 11 --- 7 | 47 50 52 54 44 --- 47
XR03E |11723 13 --- 11 23 14 --- 8 | 62 --- 63 60 66 --- 61
R04E | 3324 14 16 16 19 13 17 7 | 54 49 62 63 47 51 52
R05E | 1222 22 16 15 19 15 16 7 | 97 94 97 97 98 96 95
R07E | 3890 9 14 12 16 12 12 5 | 71 66 71 76 72 63 69
R08E | 2768 12 22 12 17 17 14 7 | 109 104 107 109 99 111 106
R09 | 2944 15 18 10 15 16 10 6 | 17 24 23 18 21 17 15
R11 | 2031 14 23 12 32 13 17 8 | 21 26 23 27 18 20 16
R12 | 598 10 26 13 37 10 9 8 | 47 64 57 29 51 41 47
R14 | 1014 10 15 9 12 15 7 5 | 56 65 63 54 65 62 60
R15 | 2007 13 17 11 9 19 12 6 | 70 67 69 63 79 61 68
R16 | 776 30 15 18 12 7 11 7 | 65 53 47 49 52 47 51
R17 | 1187 11 19 5 33 18 26 9 | 38 28 33 54 42 20 34
R18 | 1824 18 15 14 16 16 14 7 | 31 40 41 49 48 30 37
XR19 | 3133 17 23 13 --- 13 --- 9 | 18 20 31 --- 26 --- 22
XR20 | 1732 10 --- 414 20 23 --- 13 | 25 --- 202 30 34 --- 24
R21 | 1721 16 26 7 11 12 12 6 | 42 33 37 40 41 31 36
XR22 | 1056 19 18 13 20 10 --- 8 | 17 24 26 36 22 --- 21
R24 | 2130 12 40 31 13 15 18 10 | 44 39 69 53 58 43 50
XR26E | 9303 41 50 40 --- 53 --- 26 | 20 30 45 --- 24 --- 20
XR27E | 5210 45 40 --- 39 56 --- 27 | 27 43 --- 25 30 --- 26
XR28 |20306 89 --- --- --- 83 --- 86 | 62 --- --- --- 92 --- 65
------+-----------------------------------------+-------------------------------------
RMS | 2177 16 21 15 20 14 15 |T 47 48 60 51 51 49 46
WRMS | 2177 16 19 11 19 14 15 |NE 39 40 55 41 46 37 39
MEDI | 2007 14 18 13 19 15 12 |MD 44 43 52 53 47 43 47
Table 3.2396.4 GPS week: 2396 Day: 4 MJD: 61020
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2203 11 17 10 15 11 --- 6 | 46 44 42 44 46 --- 42
R04E | 1887 15 21 13 19 13 22 7 | 71 56 60 62 68 58 61
R05E | 1026 11 15 14 13 14 11 5 | 63 59 54 58 61 57 57
R07E | 3434 11 17 12 25 11 18 6 | 70 64 72 72 75 75 70
R08E | 4161 10 26 17 25 13 15 7 | 67 66 68 74 65 57 64
R09 | 1611 13 11 10 17 13 17 6 | 17 17 25 22 24 24 18
R11 | 2263 15 15 9 18 20 6 6 | 19 28 30 41 29 21 23
R12 | 1066 10 25 9 30 11 8 7 | 62 71 54 57 58 54 57
R14 | 1562 8 18 8 16 13 17 5 | 47 39 37 35 46 43 41
R15 | 2132 13 32 13 14 20 7 7 | 71 65 63 58 77 70 66
R16 | 1151 13 11 17 31 10 9 7 | 69 65 68 49 65 63 63
R17 | 1344 7 23 22 21 15 30 9 | 48 36 61 62 45 32 47
R18 | 2961 12 21 10 16 20 26 8 | 32 40 35 42 45 24 33
XR19 | 3961 12 13 11 --- 17 --- 7 | 19 21 27 --- 30 --- 21
XR20 | 1294 13 --- 391 18 32 --- 15 | 20 --- 155 24 39 --- 21
R21 | 854 11 26 19 15 15 23 8 | 50 39 60 55 53 38 49
XR22 | 1178 19 20 17 13 16 --- 9 | 18 27 27 28 25 --- 20
R24 | 1729 8 39 13 10 25 20 9 | 54 38 57 54 66 45 52
XR26E |10795 33 51 36 --- 62 --- 26 | 30 42 42 --- 25 --- 26
XR27E | 5182 33 45 --- 36 60 --- 25 | 32 33 --- 33 30 --- 26
XR28 |14180 71 --- --- --- 105 --- 86 | 66 --- --- --- 109 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 2158 12 23 14 20 16 18 |T 46 44 54 48 51 47 43
WRMS | 2158 11 23 13 22 15 18 |NE 42 40 53 43 50 41 41
MEDI | 1887 12 21 13 17 15 17 |MD 48 40 54 49 46 45 47
Table 3.2396.5 GPS week: 2396 Day: 5 MJD: 61021
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2800 11 19 15 11 15 --- 7 | 52 54 55 54 45 --- 51
R04E | 1804 9 22 9 18 13 13 6 | 85 88 89 95 86 87 87
R05E | 2705 13 14 14 16 15 9 6 | 110 111 116 112 107 109 110
R07E | 1880 8 14 15 19 19 14 6 | 90 91 95 90 96 92 91
R08E | 4129 15 22 14 25 9 18 7 | 102 110 108 103 106 107 104
R09 | 1470 14 15 12 16 13 10 6 | 19 20 21 15 18 16 14
R11 | 2533 10 45 11 37 16 15 10 | 20 64 22 53 25 21 24
R12 | 1236 19 18 12 14 8 20 7 | 49 47 41 36 40 28 39
R14 | 2087 6 19 7 12 7 7 4 | 41 47 46 37 40 40 41
R15 | 2526 21 21 11 15 13 20 7 | 62 40 55 47 50 43 50
R16 | 1404 17 15 8 15 13 14 6 | 63 50 57 49 55 52 54
R17 | 1394 9 20 14 16 17 11 6 | 35 38 33 38 35 32 32
R18 | 3201 8 24 8 12 17 23 7 | 29 30 23 31 31 23 25
XR19 | 5259 13 20 10 --- 13 --- 7 | 30 35 36 --- 41 --- 33
XR20 | 1722 14 --- 382 19 29 --- 15 | 31 --- 127 30 36 --- 28
R21 | 1033 10 26 11 20 20 15 7 | 35 26 32 44 41 28 32
XR22 | 1304 15 13 10 14 18 --- 7 | 16 30 23 30 27 --- 20
R24 | 4358 7 34 10 13 22 20 8 | 33 35 30 40 42 26 32
XR26E | 5240 44 59 43 --- 62 --- 29 | 24 36 56 --- 19 --- 26
XR27E | 7992 32 42 --- 40 59 --- 25 | 30 34 --- 25 27 --- 26
XR28 |14404 22 --- --- --- 29 --- 25 | 41 --- --- --- 51 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 2481 13 24 11 19 15 16 |T 47 51 56 51 48 50 45
WRMS | 2481 13 22 12 16 15 16 |NE 36 38 42 37 38 30 33
MEDI | 2526 13 20 11 16 16 14 |MD 35 40 46 40 41 32 33
Table 3.2396.6 GPS week: 2396 Day: 6 MJD: 61022
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 3077 12 23 11 9 14 --- 7 | 65 60 64 66 65 --- 63
R04E | 1777 7 18 15 18 25 13 7 | 133 139 138 137 131 138 135
R05E | 6096 11 12 30 15 10 14 7 | 132 134 141 143 130 142 136
R07E | 847 8 27 19 13 26 9 7 | 121 114 119 117 128 116 119
R08E | 3165 14 18 17 24 13 8 7 | 91 96 100 86 89 90 91
R09 | 1619 13 14 11 15 19 6 6 | 20 19 22 21 21 20 18
XR11 | 2390 18 64 27 17 20 --- 15 | 20 47 25 35 24 --- 22
R12 | 1005 12 19 9 11 17 15 6 | 64 64 65 61 57 52 59
R14 | 1440 4 18 19 18 14 12 6 | 54 62 63 41 57 48 53
R15 | 782 12 21 23 14 7 8 6 | 78 67 65 73 73 67 70
R16 | 1173 20 16 20 14 11 21 8 | 80 71 70 64 66 56 67
R17 | 1978 14 22 12 13 15 19 7 | 55 44 56 63 57 38 51
R18 | 3740 13 28 13 12 12 11 6 | 40 57 42 45 46 33 41
XR19 | 5576 12 12 15 --- 30 --- 10 | 37 38 37 --- 52 --- 39
XR20 | 1643 11 24 366 17 32 --- 12 | 31 14 226 32 46 --- 33
R21 | 1210 7 27 10 14 27 17 7 | 63 44 59 66 72 47 59
XR22 | 1124 13 14 14 13 16 --- 7 | 19 26 27 28 23 --- 21
R24 | 4676 10 31 11 11 12 16 7 | 60 43 66 71 73 51 61
XR26E | 5699 40 51 61 --- 67 --- 31 | 45 42 66 --- 31 --- 40
XR27E | 5681 29 45 --- 36 62 --- 24 | 40 48 --- 37 34 --- 36
XR28 |11622 22 --- --- --- 34 --- 27 | 97 --- --- --- 98 --- 94
------+-----------------------------------------+-------------------------------------
RMS | 2773 12 22 17 15 17 14 |T 64 61 76 65 65 69 62
WRMS | 2773 12 23 15 15 19 14 |NE 51 45 63 50 54 45 49
MEDI | 1978 12 21 15 14 17 13 |MD 60 48 65 63 57 52 59
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