[IGSREPORT-30748] Wk 2398 IGLOS Final Orbits
acc
acc at igs.org
Fri Jan 9 04:27:13 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2398 (Dec 21, 2025 - Dec 27, 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 2.2398.
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:
igl2398[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2398 in the SP3 format.
igl23987.sum Combination Report for GPS Week 2398.
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 | 1.5 ns
1 | -2.2 ns
2 | 3.2 ns
3 | 1.2 ns
4 | 3.1 ns
5 | 5.6 ns
6 | 4.3 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 | GFZ | R20
2 | GFZ | R20
3 | GFZ | R20
4 | GFZ | R20
5 | ESA | R06
5 | GFZ | R06 R20
6 | ESA | R06
6 | GFZ | R06 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 1.2398, 1a.2398).
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 2.2398.0-6)
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 3.2398.0-6).
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 2398 summary. (Dec 21, 2025 - Dec 27, 2025)
Table 1.2398.a GPS week : 2398 MJD: 61030.0-61036.0
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 0 -6 6 34 .14 14 14 | 3578 -771 3493 12736
| 0 0 1 12 10 11 .05 | 2302 3847
esa n/a| -2 0 -4 -26 -30 42 -.11 22 21 | 2290 -625 3486 12340
| 1 1 1 11 17 33 .12 | 1772 3590
gfz n/a| 0 0 0 29 -5 10 .00 29 15 | 0 -730 3556 10193
| 1 1 1 17 13 26 .05 | 0 4042
grg n/a| 1 -1 0 -25 -16 -18 .26 16 15 | 3305 -603 3666 12065
| 2 0 2 17 25 24 .01 | 1360 3926
iac n/a| 0 0 -2 14 16 -20 -.05 15 16 | 5429 -935 3574 13048
| 1 0 2 20 26 37 .05 | 1249 1344
jgx n/a| 1 0 1 -1 15 -30 -.24 14 14 | 4970 -590 3262 7733
| 1 0 2 16 2 33 .03 | 1596 3907
Table 1.2398.b GPS week : 2398 MJD: 61030.0-61036.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R02 | 8 7 8 8 7 9 6 |
R03 | 14 10 7 5 6 6 7 |
R04 | 7 9 6 6 6 6 6 |
R05 | 6 8 7 7 6 8 7 |
R06 | --- --- --- --- 204 51 47 |
R07 | 8 9 7 8 7 7 8 |
R08 | 8 7 7 7 6 6 8 |
R09 | 6 5 6 7 6 8 6 |
R11 | 8 6 6 7 7 7 5 |
R12 | 6 7 7 6 8 10 8 |
R14 | 7 5 6 6 7 6 5 |
R15 | 7 7 7 8 9 7 8 |
R16 | 9 10 6 7 7 7 8 |
R17 | 7 8 8 8 7 7 8 |
R18 | 7 6 7 8 6 7 8 |
R19 | 9 9 9 7 8 10 8 |
R20 | 17 14 14 10 19 18 18 |
R21 | 7 9 9 8 10 10 9 |
R22 | 6 7 6 7 7 8 7 |
R24 | 10 8 7 9 10 8 7 |
R26 | 31 29 28 28 28 29 32 |
R27 | 30 27 24 --- --- --- --- |
R28 | 55 86 82 67 51 0 0 |
Table 1.2398.c GPS week : 2398 MJD: 61030.0-61036.0
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 2398 0 | 46 30 -20 -478 -331 2546 80.7 1074 1074 | 1472 0
brd 2398 1 | 173 -20 8 450 785 2470 79.9 1313 1313 | -2227 0
brd 2398 2 | -72 0 94 907 -1934 2128 78.7 1425 1425 | 3210 0
brd 2398 3 | 199 106 9 399 1297 4254 80.1 1798 1798 | 1169 0
brd 2398 4 | 33 44 -8 806 1843 1631 80.2 1741 1741 | 3099 0
brd 2398 5 | -86 161 -39 -702 452 6387 79.4 1977 1977 | 5611 0
brd 2398 6 | 0 -35 -29 -576 -68 5206 80.6 1994 1994 | 4316 0
-------------+------------------------------------------------------------+----------------
brd 2398 mean| 42 40 2 115 291 3517 79.9 1617 1617 | 2378 0
brd 2398 sdev| 110 71 44 682 1235 1786 .7 352 352 | 2546 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 2.2398.0 GPS week: 2398 Day: 0 MJD: 61030
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 -8 4 25 .16 16 16 | 5144 6237 3375 23084
esa n/a| -2 0 -4 -15 -17 41 -.08 20 20 | 4264 5192 3362 23341
gfz n/a| 0 0 1 17 7 24 -.07 17 13 | 0 6473 3952 19859
grg n/a| -2 0 0 -4 29 -15 .27 15 16 | 1661 6627 3441 23661
iac n/a| 0 0 0 20 -39 -54 -.00 13 12 | 6924 1723 3629 23540
jgx n/a| 0 1 0 -37 16 29 -.26 14 14 | 3676 6294 3408 7963
Table 2.2398.1 GPS week: 2398 Day: 1 MJD: 61031
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 -18 26 36 .21 15 15 | 7568 -5867 4464 21644
esa n/a| -2 0 -3 -15 -63 11 .12 23 22 | 4652 -6403 4460 20881
gfz n/a| 0 1 1 55 -5 36 -.07 16 15 | 0 -6413 4098 10869
grg n/a| 0 0 5 -16 3 -12 .26 17 16 | 3292 -5647 5120 22253
iac n/a| 0 1 -5 -21 11 -70 -.08 16 17 | 4048 -2167 4212 21391
jgx n/a| 0 1 -2 0 12 -32 -.24 13 13 | 6726 -5504 2936 7344
Table 2.2398.2 GPS week: 2398 Day: 2 MJD: 61032
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 -5 13 47 .05 12 13 | 4727 -3282 3082 9566
esa n/a| -1 1 -3 -32 -38 10 -.10 19 18 | 1851 -2435 3082 8567
gfz n/a| 0 1 0 0 9 34 .03 15 15 | 0 -2641 3153 7881
grg n/a| 1 0 3 -36 -46 -6 .28 17 15 | 4098 -3109 3142 8852
iac n/a| -2 0 -1 43 22 14 -.11 15 16 | 5105 -1268 3082 9902
jgx n/a| 3 0 -1 15 14 -66 -.22 13 13 | 7079 -3076 2955 7994
Table 2.2398.3 GPS week: 2398 Day: 3 MJD: 61033
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 -24 2 34 .11 14 14 | 2425 -2184 3372 8556
esa n/a| -5 -3 -3 -12 -25 11 -.11 18 17 | 108 -1415 3367 7927
gfz n/a| 2 2 -1 38 -29 -16 -.01 106 17 | 0 -2792 3391 8131
grg n/a| 4 0 -1 -5 -22 18 .26 16 16 | 2152 -2298 3479 7457
iac n/a| 0 0 1 27 20 -34 -.08 17 19 | 4505 -2384 3463 8829
jgx n/a| 1 1 4 -2 17 -27 -.28 15 15 | 4202 -2724 3384 7732
Table 2.2398.4 GPS week: 2398 Day: 4 MJD: 61034
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 5 6 22 .17 14 15 | 1367 -947 3498 9114
esa n/a| -3 -1 -5 -35 -7 60 -.21 22 21 | 221 -724 3435 8370
gfz n/a| 0 0 0 26 -2 -16 .04 17 17 | 0 -918 3526 8780
grg n/a| 2 -1 0 -39 -30 -15 .26 16 16 | 3228 -694 3584 8183
iac n/a| 0 0 -2 13 44 38 .01 16 16 | 5042 -807 3989 10104
jgx n/a| 1 1 4 8 12 -61 -.24 14 14 | 2883 953 3254 8702
Table 2.2398.5 GPS week: 2398 Day: 5 MJD: 61035
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 12 -5 24 .16 15 15 | 2309 -908 3513 8480
esa n/a| -3 2 -3 -34 -29 70 -.24 24 23 | 2279 -453 3530 8735
gfz n/a| -2 0 3 29 -16 30 .05 16 16 | 0 -519 3554 7718
grg n/a| 2 -1 -1 -50 -21 -36 .27 17 15 | 5809 -864 3651 7021
iac n/a| 0 0 -5 12 29 -13 -.03 14 14 | 7406 -759 3504 8884
jgx n/a| 4 0 1 0 20 -48 -.22 15 15 | 5856 -1815 3665 7267
Table 2.2398.6 GPS week: 2398 Day: 6 MJD: 61036
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 0 49 .10 13 14 | 1506 1550 3152 8711
esa n/a| -1 0 -6 -40 -31 94 -.13 25 25 | 2658 1859 3167 8563
gfz n/a| 2 1 0 39 2 -18 .04 15 14 | 0 1694 3223 8116
grg n/a| 3 -1 0 -26 -29 -61 .25 15 14 | 2900 1759 3250 7030
iac n/a| 0 0 0 7 26 -26 -.08 16 16 | 4978 -883 3145 8690
jgx n/a| 0 0 1 1 15 -6 -.21 15 15 | 4373 1742 3237 7135
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 3.2398.0 GPS week: 2398 Day: 0 MJD: 61030
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1956 12 21 16 16 15 --- 8 | 30 33 23 34 32 --- 27
XR03E | 7911 16 35 32 39 15 --- 14 | 38 40 42 62 42 --- 38
R04E | 1097 12 16 17 16 14 9 6 | 42 43 45 50 41 44 42
R05E | 1050 12 14 12 18 12 13 6 | 28 31 30 37 29 30 28
R07E | 1795 16 22 20 20 14 6 7 | 71 77 81 79 77 75 75
R08E | 949 18 16 29 13 12 8 7 | 36 45 43 42 29 41 37
R09 | 589 18 17 7 13 8 9 5 | 31 39 38 41 37 31 34
XR11 | 1861 15 19 20 10 14 --- 7 | 38 50 41 43 41 --- 40
R12 | 626 10 21 17 12 10 13 6 | 37 37 29 37 29 26 29
R14 | 1588 8 18 18 13 16 11 6 | 39 49 50 36 41 51 42
R15 | 957 14 18 14 9 14 19 6 | 47 48 48 40 50 33 42
R16 | 861 26 16 22 14 15 19 8 | 53 42 50 36 38 28 38
R17 | 691 17 25 10 13 9 16 6 | 75 60 62 72 69 60 66
R18 | 692 13 22 14 19 7 10 6 | 109 120 116 108 108 108 110
XR19 | 1581 15 19 19 --- 10 --- 9 | 66 81 79 --- 64 --- 69
XR20 | 2713 23 28 383 17 41 --- 17 | 80 83 191 84 87 --- 80
R21 | 820 9 20 11 15 19 17 7 | 64 48 68 66 73 49 61
R22 | 1481 14 17 10 11 13 8 5 | 60 60 57 66 63 61 60
R24 | 988 20 32 22 21 8 24 9 | 81 60 83 84 72 61 72
XR26E |12388 41 41 61 --- 59 --- 30 | 41 48 36 --- 34 --- 29
XR27E |13307 45 24 --- 60 59 --- 30 | --- --- --- --- --- --- 0
XR28 |17084 62 --- --- --- 48 --- 55 | 150 --- --- --- 96 --- 143
------+-----------------------------------------+-------------------------------------
RMS | 1074 16 20 17 15 13 14 |T 57 54 60 56 54 49 55
WRMS | 1074 16 20 13 16 12 14 |NE 66 59 70 59 62 50 63
MEDI | 1097 15 20 17 15 14 11 |MD 47 48 48 43 42 44 42
Table 3.2398.1 GPS week: 2398 Day: 1 MJD: 61031
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2045 13 13 16 17 12 --- 7 | 44 40 45 45 43 --- 42
XR03E | 5886 9 19 19 17 28 --- 9 | 33 34 32 38 38 --- 29
R04E | 977 17 25 25 23 18 8 8 | 45 50 58 57 44 42 46
R05E | 1091 13 19 17 15 18 17 7 | 42 45 44 44 38 42 40
R07E | 2368 10 16 27 24 25 12 9 | 61 69 75 59 54 67 62
R08E | 895 14 19 14 16 19 16 7 | 26 26 30 31 26 30 25
R09 | 808 11 15 10 14 11 8 5 | 29 35 35 30 35 32 31
R11 | 1226 11 15 12 10 15 10 5 | 36 38 44 41 34 37 36
R12 | 889 16 18 14 13 13 11 6 | 40 39 28 29 33 31 31
R14 | 1130 6 13 9 15 11 8 4 | 42 49 45 45 45 50 45
R15 | 1058 14 26 10 11 18 12 6 | 48 45 45 40 45 43 43
R16 | 1466 24 38 21 22 15 16 10 | 49 59 54 40 43 33 41
R17 | 789 19 25 11 18 18 14 7 | 63 53 54 50 62 48 53
R18 | 807 12 18 12 12 14 8 5 | 87 91 84 83 82 90 85
XR19 | 1248 15 20 12 --- 16 --- 9 | 77 92 81 --- 69 --- 78
XR20 | 1890 13 17 391 15 39 --- 13 | 79 77 128 80 87 --- 79
R21 | 810 11 31 17 13 22 20 8 | 53 44 58 58 59 47 52
R22 | 2116 17 16 17 18 8 8 6 | 62 64 59 75 65 60 63
R24 | 1840 14 29 15 19 12 20 8 | 63 51 56 67 53 50 56
XR26E |13354 36 39 58 --- 61 --- 29 | 28 39 65 --- 23 --- 31
XR27E |11226 32 38 --- 47 64 --- 27 | --- --- --- --- --- --- 0
XR28 |13525 79 --- --- --- 92 --- 85 | 142 --- --- --- 74 --- 94
------+-----------------------------------------+-------------------------------------
RMS | 1312 15 23 16 17 16 13 |T 54 52 56 50 50 46 50
WRMS | 1312 15 22 15 16 17 13 |NE 62 56 59 53 56 47 56
MEDI | 1226 14 19 15 16 18 12 |MD 48 45 54 45 45 43 45
Table 3.2398.2 GPS week: 2398 Day: 2 MJD: 61032
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2466 14 15 19 20 12 --- 8 | 34 37 41 41 32 --- 35
XR03E | 2395 9 14 18 16 16 --- 7 | 45 47 53 48 40 --- 45
R04E | 1165 7 15 12 16 13 17 6 | 35 42 38 41 33 41 36
R05E | 1102 9 13 12 28 11 16 7 | 33 35 32 47 29 34 32
R07E | 2460 9 24 15 16 11 11 6 | 76 73 80 80 74 83 78
R08E | 1729 8 15 18 25 16 10 7 | 26 30 28 33 28 27 25
R09 | 766 8 14 16 20 13 10 6 | 28 34 33 33 24 31 28
R11 | 1039 7 14 17 12 16 9 5 | 38 33 43 39 45 30 38
R12 | 850 17 16 9 19 13 11 6 | 32 31 24 16 18 26 23
R14 | 939 8 13 13 15 7 16 5 | 26 31 39 28 32 29 29
R15 | 1169 17 21 13 8 15 12 6 | 29 32 30 20 18 17 22
R16 | 1274 16 19 10 12 19 6 6 | 34 43 36 26 23 30 30
R17 | 820 15 28 18 13 16 15 7 | 81 85 75 81 81 75 78
R18 | 888 11 24 11 14 14 14 6 | 111 125 112 113 112 106 112
XR19 | 1269 16 18 16 --- 13 --- 9 | 42 41 37 --- 42 --- 39
XR20 | 1226 9 18 404 28 36 --- 14 | 54 51 176 50 61 --- 51
R21 | 760 8 25 20 13 21 24 8 | 52 42 67 59 68 38 53
R22 | 2394 11 13 16 13 18 9 6 | 48 47 47 55 58 46 48
R24 | 2187 17 25 14 15 13 10 7 | 65 55 59 67 60 60 60
XR26E | 8990 47 43 35 --- 61 --- 27 | 27 41 58 --- 31 --- 30
XR27E | 9149 35 27 --- 37 58 --- 24 | --- --- --- --- --- --- 0
XR28 |14185 71 --- --- --- 94 --- 82 | 135 --- --- --- 73 --- 110
------+-----------------------------------------+-------------------------------------
RMS | 1424 12 19 15 17 15 13 |T 50 47 55 48 46 44 47
WRMS | 1424 13 18 15 15 16 13 |NE 55 50 59 48 51 44 51
MEDI | 1226 11 18 16 16 15 11 |MD 38 41 41 41 40 34 38
Table 3.2398.3 GPS week: 2398 Day: 3 MJD: 61033
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1883 14 20 16 14 8 --- 7 | 26 35 27 29 28 --- 26
R03E | 3292 7 15 14 13 13 8 5 | 31 34 37 41 31 28 32
R04E | 2287 13 13 17 10 17 10 6 | 52 53 50 47 45 49 48
R05E | 864 12 12 21 10 10 15 6 | 31 35 24 35 26 31 28
R07E | 1816 14 21 17 19 17 10 7 | 55 57 60 46 47 54 51
R08E | 1971 14 19 16 20 12 14 7 | 26 34 26 27 25 30 24
R09 | 1452 11 17 26 12 10 9 7 | 18 23 40 20 22 21 22
R11 | 1456 11 16 16 17 14 12 6 | 20 25 26 24 23 11 19
R12 | 934 16 14 7 19 10 10 6 | 31 29 24 17 22 16 22
R14 | 888 8 13 16 13 11 19 6 | 32 27 38 31 31 22 28
R15 | 818 17 16 16 19 19 22 8 | 38 39 40 44 22 18 30
R16 | 1900 19 18 12 10 7 17 6 | 41 38 34 37 32 33 33
R17 | 957 20 15 12 23 18 16 8 | 106 98 91 93 99 88 94
R18 | 831 13 20 11 19 15 20 7 | 106 115 100 111 92 97 102
XR19 | 2078 15 11 16 --- 9 13 6 | 48 55 43 --- 46 14 46
R20 | 2699 5 14 433 19 32 16 9 | 33 32 194 28 43 13 30
R21 | 955 17 22 14 14 17 19 7 | 59 50 50 57 55 52 52
R22 | 1486 14 22 13 16 14 8 6 | 45 43 47 43 48 42 43
R24 | 2958 11 27 12 16 30 21 9 | 77 64 68 79 81 70 71
XR26E | 8950 46 42 36 --- 61 --- 27 | 33 51 40 --- 28 --- 28
XR28 |14350 62 --- --- --- 71 --- 66 | 78 --- --- --- 104 --- 93
------+-----------------------------------------+-------------------------------------
RMS | 1797 14 18 106 16 17 15 |T 46 46 52 44 45 38 43
WRMS | 1797 14 17 17 16 19 15 |NE 52 49 61 48 51 38 48
MEDI | 1816 14 16 16 16 14 14 |MD 38 38 40 37 32 30 32
Table 3.2398.4 GPS week: 2398 Day: 4 MJD: 61034
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2174 11 12 15 21 12 --- 7 | 45 47 52 54 42 --- 46
R03E | 3373 8 23 16 18 13 7 6 | 37 35 40 42 37 37 35
R04E | 1400 12 15 15 9 15 15 6 | 58 53 54 56 49 51 52
R05E | 1631 9 20 20 13 12 11 6 | 36 41 43 44 38 37 37
XR06 | 888 --- 247 168 --- --- --- 204 | --- --- --- --- --- --- 0
R07E | 1027 12 22 16 14 17 16 7 | 40 38 45 39 46 36 39
R08E | 3195 12 13 14 12 16 11 6 | 36 40 34 36 35 31 33
R09 | 1938 14 21 12 13 13 9 6 | 23 33 26 32 27 30 26
R11 | 1910 7 27 10 21 12 10 6 | 31 46 37 33 40 28 34
R12 | 766 10 21 14 20 18 17 7 | 38 38 45 29 42 27 34
R14 | 1124 9 20 19 15 14 9 6 | 46 54 62 44 43 51 48
R15 | 883 27 10 20 15 15 19 8 | 54 40 35 47 39 37 40
R16 | 1593 15 20 13 12 16 12 6 | 51 51 50 46 47 38 46
R17 | 1224 13 24 13 20 13 14 7 | 91 86 89 94 92 84 88
R18 | 766 10 24 16 12 8 14 6 | 102 114 109 110 107 105 106
XR19 | 1977 12 14 16 --- 8 --- 7 | 41 54 48 --- 41 --- 44
XR20 | 3169 18 28 454 29 48 --- 19 | 50 57 191 48 73 --- 53
R21 | 1138 17 33 31 22 15 18 10 | 68 61 80 59 62 53 61
R22 | 894 19 19 15 18 12 9 7 | 66 71 70 68 64 65 66
R24 | 2116 11 32 17 20 29 25 10 | 113 100 112 114 121 96 108
XR26E | 7828 37 56 46 --- 57 --- 28 | 36 49 40 --- 27 --- 25
XR28 |15215 47 --- --- --- 55 --- 51 | 123 --- --- --- 136 --- 121
------+-----------------------------------------+-------------------------------------
RMS | 1741 14 22 17 16 15 14 |T 56 55 63 55 57 50 54
WRMS | 1741 15 21 17 16 16 14 |NE 64 61 73 60 66 55 62
MEDI | 1593 12 21 16 15 15 12 |MD 46 49 48 46 43 37 46
Table 3.2398.5 GPS week: 2398 Day: 5 MJD: 61035
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1735 8 30 15 24 10 --- 8 | 33 48 38 37 33 --- 33
R03E | 2853 11 20 15 18 11 8 6 | 37 43 38 42 38 31 36
R04E | 1451 11 15 15 16 10 17 6 | 75 78 75 73 69 77 73
R05E | 1973 13 29 18 15 13 13 7 | 42 51 32 42 29 38 36
XR06 | 1052 51 858 755 --- 50 --- 50 | --- --- --- --- --- --- 0
R07E | 2301 11 17 12 20 18 14 7 | 52 63 55 61 47 57 53
R08E | 2943 14 24 9 11 11 14 6 | 26 35 25 27 26 25 24
R09 | 1342 12 26 13 17 21 14 7 | 26 34 23 30 23 25 21
R11 | 4235 17 21 13 19 12 10 6 | 33 36 36 36 36 24 33
R12 | 726 12 21 17 32 24 14 9 | 20 33 32 19 33 14 19
R14 | 1740 10 18 20 13 11 8 6 | 28 25 23 27 30 26 23
R15 | 1203 22 19 10 12 10 13 6 | 41 25 27 30 30 25 29
R16 | 979 16 24 13 15 11 19 7 | 37 47 30 35 38 28 33
R17 | 1291 15 17 13 17 13 21 7 | 53 46 53 48 46 35 46
R18 | 858 11 19 9 16 18 21 7 | 54 66 60 69 57 56 59
XR19 | 2797 15 22 15 --- 15 --- 9 | 27 45 33 --- 32 --- 31
XR20 | 1236 20 32 417 23 41 --- 17 | 62 70 95 66 68 --- 63
R21 | 1513 20 38 25 14 13 22 10 | 65 66 69 56 52 54 58
R22 | 1096 21 27 12 17 13 14 7 | 31 31 30 34 33 32 29
R24 | 1681 11 32 26 12 10 13 8 | 74 67 85 78 70 67 73
XR26E | 8363 38 63 50 --- 53 --- 29 | 22 61 42 --- 25 --- 23
XR28 |11380 2 --- --- --- --- --- 0 | 108 --- --- --- --- --- 112
------+-----------------------------------------+-------------------------------------
RMS | 1976 15 24 16 17 14 15 |T 45 48 45 45 40 38 43
WRMS | 1976 15 23 16 15 14 15 |NE 47 45 45 44 42 35 44
MEDI | 1513 13 24 15 16 13 14 |MD 37 46 36 37 33 31 33
Table 3.2398.6 GPS week: 2398 Day: 6 MJD: 61036
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1015 11 16 13 11 13 --- 6 | 37 39 45 47 44 --- 41
R03E | 1038 10 23 16 14 18 8 6 | 51 59 55 55 46 41 50
R04E | 1456 7 20 14 15 15 13 6 | 61 70 59 60 60 66 61
R05E | 2287 7 25 16 14 16 14 6 | 44 44 50 42 50 42 43
XR06 | 1087 40 902 912 --- 55 --- 47 | --- --- --- --- --- --- 0
R07E | 2915 11 28 15 17 23 15 8 | 70 65 66 64 69 66 65
R08E | 2325 12 16 13 21 19 19 7 | 39 40 37 40 35 35 36
R09 | 740 9 24 13 12 14 11 6 | 32 35 29 34 27 31 28
R11 | 3627 8 19 5 13 9 10 4 | 42 45 41 40 43 26 40
R12 | 1036 13 37 10 10 13 21 7 | 29 45 27 16 30 19 23
R14 | 4225 6 18 14 12 13 9 5 | 36 45 40 37 42 36 37
R15 | 1228 25 34 14 13 16 7 8 | 52 34 36 37 38 33 36
R16 | 1122 19 15 16 20 18 9 7 | 54 47 45 38 52 42 44
R17 | 1365 17 22 19 14 18 19 8 | 98 80 95 91 93 74 89
R18 | 955 7 28 9 15 17 25 7 | 71 79 74 78 77 56 71
XR19 | 3828 10 20 13 --- 14 --- 7 | 28 43 35 --- 29 --- 30
XR20 | ---- 15 32 422 25 48 --- 18 | 74 81 202 75 80 --- 72
R21 | 970 11 34 20 12 16 25 8 | 83 67 93 79 85 64 78
R22 | 1013 17 22 9 19 12 10 6 | 46 44 44 48 45 49 44
R24 | 1069 12 27 22 11 11 16 7 | 105 89 110 104 104 91 101
XR26E | 8416 43 65 56 --- 64 --- 32 | 25 52 70 --- 30 --- 30
XR28 | 8835 3 --- --- --- --- --- 0 | 285 --- --- --- --- --- 276
------+-----------------------------------------+-------------------------------------
RMS | 1994 13 25 15 15 16 15 |T 64 55 62 54 53 48 61
WRMS | 1994 14 25 14 14 16 15 |NE 73 56 67 56 57 47 69
MEDI | 1228 11 24 14 14 16 13 |MD 51 45 45 47 45 42 44
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