[IGSREPORT-30796] Wk 2403 IGLOS Final Orbits
acc
acc at igs.org
Thu Feb 12 05:35:41 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2403 (Jan 25, 2026 - Jan 31, 2026)
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 2.2403.
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:
igl2403[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2403 in the SP3 format.
igl24037.sum Combination Report for GPS Week 2403.
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.
Starting 11-Jan-2026 (GPS Week 2401, day 0, MJD 61051), all IGS products
are based on the IGS realization of the second yearly update of ITRF2020
called ITRF2020-u2024. This IGS realization is called IGc20.
For more information see IGSMAIL #8634.
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
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.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 | 4.2 ns
1 | 3.9 ns
2 | 5.3 ns
3 | 4.3 ns
4 | 3.6 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 | ALL | R26
0 | ESA | R06
0 | GFZ | R06 R20
1 | ALL | R26
1 | ESA | R06
1 | GFZ | R06 R20
2 | ALL | R26
2 | ESA | R06
2 | GFZ | R06 R20
3 | ALL | R26
3 | ESA | R06
3 | GFZ | R06 R20
4 | ALL | R26
4 | ESA | R06
4 | GFZ | R06 R20
5 | ALL | R26
5 | ESA | R06
5 | GFZ | R06 R20
6 | ALL | R26
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 1.2403, 1a.2403).
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 2.2403.0-6)
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 3.2403.0-6).
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 2403 summary. (Jan 25, 2026 - Jan 31, 2026)
Table 1.2403.a GPS week : 2403 MJD: 61065.0-61071.0
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 0 2 -28 .13 14 14 | 4896 -318 3326 10318
| 0 0 1 12 8 15 .05 | 457 1722
esa n/a| 0 0 0 -32 -3 57 -.11 30 28 | 7896 -308 3381 10270
| 2 1 1 26 22 48 .06 | 1348 1550
gfz n/a| 0 0 0 13 13 23 -.18 50 15 | 0 -246 3467 10106
| 1 0 1 14 14 11 .04 | 0 1379
grg n/a| 1 0 0 25 -25 22 .30 18 15 | 4427 -324 3429 9090
| 1 1 2 15 22 42 .04 | 743 1740
iac n/a| 0 0 -2 -16 22 -38 -.11 19 19 | 6057 -166 3595 11531
| 1 2 2 33 20 34 .06 | 596 1213
jgx n/a| 0 0 3 -5 -20 -22 -.15 17 17 | 7552 -371 3378 9383
| 1 1 1 19 10 29 .06 | 317 1580
Table 1.2403.b GPS week : 2403 MJD: 61065.0-61071.0
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 8 8 8 9 8 6 |
R03 | 7 8 8 8 8 7 6 |
R04 | 8 7 6 7 6 8 5 |
R05 | 9 10 9 8 8 7 7 |
R06 | 53 46 43 45 43 50 46 |
R07 | 9 8 9 8 8 7 7 |
R08 | 8 9 10 11 11 9 8 |
R09 | 8 8 9 9 9 8 7 |
R11 | 8 8 6 9 7 6 8 |
R12 | 9 10 8 7 8 6 8 |
R14 | 7 6 8 6 6 6 6 |
R15 | 9 8 9 10 9 6 7 |
R16 | 8 8 10 10 10 8 9 |
R17 | 7 10 10 8 9 8 7 |
R18 | 7 7 11 7 8 6 6 |
R19 | 8 8 8 9 9 7 8 |
R20 | 8 9 9 9 10 9 8 |
R21 | 9 14 12 8 9 9 9 |
R22 | 7 9 10 8 7 7 9 |
R24 | 10 11 9 9 9 7 7 |
R28 | 123 99 136 78 98 86 70 |
Table 1.2403.c GPS week : 2403 MJD: 61065.0-61071.0
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 2403 0 | -22 9 40 1872 -397 297 79.7 2008 2008 | 4218 0
brd 2403 1 | 79 -3 -119 -361 -1436 6040 80.3 1912 1912 | 3890 0
brd 2403 2 | -149 -161 -87 1871 -384 7851 81.3 1569 1569 | 5316 0
brd 2403 3 | -38 -29 170 206 -244 2633 84.2 1637 1637 | 4267 0
brd 2403 4 | 76 -105 -19 226 2669 1566 81.0 1566 1566 | 3569 0
brd 2403 5 | 139 35 135 1004 1436 3516 77.3 1689 1689 | 5585 0
brd 2403 6 | 94 10 23 610 1748 3240 80.6 1618 1618 | 4323 0
-------------+------------------------------------------------------------+----------------
brd 2403 mean| 25 -34 20 775 484 3591 80.6 1714 1714 | 4452 0
brd 2403 sdev| 100 71 107 856 1473 2586 2.0 175 175 | 733 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 2.2403.0 GPS week: 2403 Day: 0 MJD: 61065
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 -7 1 -25 .05 15 16 | 4652 1566 3318 11141
esa n/a| -3 0 1 -1 -23 35 -.00 28 26 | 7871 403 3373 10980
gfz n/a| -2 -1 0 25 20 19 -.16 53 16 | 0 945 3486 10951
grg n/a| 1 0 -3 4 -55 66 .35 16 14 | 2939 1853 3343 9789
iac n/a| 1 -3 1 -53 39 -41 -.06 19 19 | 6191 1008 3535 13632
jgx n/a| 1 1 3 27 -10 -33 -.13 16 16 | 7136 1353 3381 10014
Table 2.2403.1 GPS week: 2403 Day: 1 MJD: 61066
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 -3 -4 -10 -40 .15 16 16 | 5268 -1888 3127 10600
esa n/a| -2 0 0 -25 11 123 -.14 32 30 | 7774 -1398 3180 9771
gfz n/a| 0 -1 0 -1 13 22 -.23 59 20 | 0 -1364 3313 10219
grg n/a| 1 1 -1 24 -50 60 .32 22 22 | 4983 -2111 3246 9389
iac n/a| 0 0 -1 11 35 -8 -.09 18 18 | 5492 -986 3284 11189
jgx n/a| 0 0 4 -8 -12 -52 -.16 16 16 | 7992 -2016 3205 9567
Table 2.2403.2 GPS week: 2403 Day: 2 MJD: 61067
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 11 -2 -48 .16 15 15 | 4334 1690 3787 10104
esa n/a| -3 0 0 -38 8 110 -.14 31 30 | 8326 1754 3827 9388
gfz n/a| 0 0 -1 16 21 36 -.25 49 15 | 0 1355 3893 9827
grg n/a| 2 0 2 9 -34 17 .32 23 16 | 4256 1701 3938 8508
iac n/a| 0 0 0 9 15 -99 -.05 21 21 | 7295 -1009 4462 11376
jgx n/a| 1 0 4 -22 -11 -23 -.09 18 18 | 7516 1588 3845 8886
Table 2.2403.3 GPS week: 2403 Day: 3 MJD: 61068
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 -2 21 10 -38 .19 15 15 | 5518 -843 3289 11200
esa n/a| 0 1 -1 -3 24 56 -.10 27 27 | 10243 -1093 3358 10550
gfz n/a| -1 0 0 -5 29 2 -.19 54 14 | 0 -662 3450 11120
grg n/a| 1 -1 2 36 -26 35 .24 15 13 | 4709 -1490 3409 9862
iac n/a| 0 2 -4 -46 5 -20 -.22 21 22 | 5863 -461 3762 12182
jgx n/a| 1 0 3 -32 -34 -62 -.22 20 20 | 7920 -1013 3371 10143
Table 2.2403.4 GPS week: 2403 Day: 4 MJD: 61069
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 0 -11 1 -3 .10 14 14 | 5184 -2847 3045 9627
esa n/a| 3 2 2 -27 -1 75 -.13 31 31 | 8365 -2728 3119 9734
gfz n/a| -1 0 1 12 -13 22 -.15 44 14 | 0 -2304 3181 9560
grg n/a| 2 0 0 31 2 -61 .31 17 14 | 4640 -2385 3133 8169
iac n/a| 0 4 -5 -10 51 2 -.17 21 21 | 5942 -1675 3262 11169
jgx n/a| 0 0 4 -8 -11 11 -.22 19 19 | 7582 -2469 3031 8588
Table 2.2403.5 GPS week: 2403 Day: 5 MJD: 61070
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 14 -13 .12 10 10 | 4378 687 3168 10008
esa n/a| 1 0 0 -69 -1 8 -.17 29 26 | 6037 1107 3211 10649
gfz n/a| 1 -1 0 11 15 37 -.19 42 15 | 0 1008 3294 9786
grg n/a| 0 -1 1 25 -8 2 .25 16 13 | 5208 408 3266 9149
iac n/a| -1 0 -4 25 -8 -41 -.11 17 17 | 5596 247 3199 10485
jgx n/a| -1 1 2 6 -32 -13 -.18 16 16 | 7247 435 3198 9457
Table 2.2403.6 GPS week: 2403 Day: 6 MJD: 61071
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 8 0 -30 .14 13 14 | 4941 -596 3548 9548
esa n/a| -1 -2 0 -60 -43 -4 -.08 32 28 | 6659 -204 3600 10819
gfz n/a| 1 1 1 35 4 20 -.12 49 11 | 0 -702 3658 9285
grg n/a| 2 1 0 48 -7 32 .30 16 14 | 4257 -248 3671 8767
iac n/a| -1 0 0 -50 16 -59 -.10 14 14 | 6023 1714 3666 10686
jgx n/a| 0 -3 1 -1 -27 14 -.09 15 15 | 7476 -480 3621 9031
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 3.2403.0 GPS week: 2403 Day: 0 MJD: 61065
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1043 20 12 14 10 15 14 6 | 71 63 61 62 54 56 60
R03 | 4084 11 10 16 12 17 24 7 | 85 77 94 88 84 67 82
R04 | 1499 13 21 21 13 22 16 8 | 87 89 99 93 101 82 91
R05 | 2022 12 38 21 14 18 17 8 | 76 82 87 80 79 68 77
XR06 | 1063 48 986 1165 --- 58 --- 53 | 82 380 744 --- 114 --- 126
R07 | 1111 14 31 12 25 10 25 9 | 91 84 79 95 94 71 84
R08 | 2888 15 28 10 15 17 18 7 | 67 89 79 76 80 67 74
R09 | 1446 12 50 9 12 15 9 8 | 16 46 19 19 25 15 17
R11 | 3565 11 32 9 13 26 11 7 | 46 43 46 46 48 43 43
R12 | 571 28 26 14 23 16 8 9 | 44 34 41 32 40 32 33
R14 | 1212 9 30 11 11 18 15 7 | 47 59 46 43 53 43 46
R15 | 1171 23 26 16 12 18 19 8 | 56 41 55 46 36 39 45
R16 | 1098 17 18 16 14 23 13 7 | 60 52 59 57 48 49 53
R17E | 1068 14 14 11 11 26 17 7 | 86 85 92 83 81 87 85
R18E | 1787 11 26 11 12 16 13 6 | 20 20 19 23 26 18 17
XR19E | 870 10 25 12 --- 13 15 7 | 101 94 105 --- 103 105 102
R20E | 1681 11 24 215 14 21 13 8 | 86 86 145 87 84 83 85
R21E | 2177 15 34 18 20 18 21 9 | 31 49 29 37 29 36 30
R22E | 1518 11 21 13 18 13 12 6 | 57 65 61 65 62 63 61
R24E | 2351 15 35 28 25 18 14 10 | 44 48 59 61 51 41 47
XR28E |16421 112 --- --- --- 135 --- 123 | 102 --- --- --- 149 --- 78
------+-----------------------------------------+-------------------------------------
RMS | 2008 15 28 53 16 19 16 |T 64 79 100 60 68 56 63
WRMS | 2008 16 26 16 14 19 16 |NE 63 87 116 61 65 52 63
MEDI | 1499 14 26 14 13 18 15 |MD 67 63 61 61 62 56 61
Table 3.2403.1 GPS week: 2403 Day: 1 MJD: 61066
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1038 24 22 14 17 14 10 7 | 50 44 41 35 36 36 37
R03 | 4048 9 24 25 12 10 21 7 | 58 58 73 59 55 48 55
R04 | 1141 15 17 17 10 22 15 7 | 56 60 71 67 74 56 62
R05 | 2134 13 44 8 16 27 21 9 | 54 52 49 56 65 41 51
XR06 | 957 41 928 1196 --- 50 --- 46 | 73 291 531 --- 78 --- 200
R07 | 2151 10 23 14 19 19 24 8 | 67 74 61 74 77 49 66
R08 | 2006 12 31 22 12 23 15 8 | 48 58 47 45 65 50 49
R09 | 1845 11 51 16 10 9 10 8 | 15 33 19 17 24 20 18
R11 | 2253 16 32 13 8 28 11 8 | 43 33 46 34 49 31 37
R12 | 642 20 39 19 18 24 20 10 | 36 25 40 28 44 27 29
R14 | 1303 13 25 15 12 13 9 6 | 32 32 31 34 29 30 30
R15 | 800 20 24 24 10 11 15 7 | 39 29 43 31 22 25 29
R16 | 1089 21 25 17 15 11 14 7 | 42 28 38 33 35 35 33
R17E | 1673 21 28 26 24 19 11 9 | 126 135 143 136 124 126 128
R18E | 818 9 24 20 17 14 8 6 | 18 21 24 27 20 17 18
XR19E | 1301 14 31 9 --- 12 13 7 | 89 81 89 --- 87 89 87
R20E | 3194 10 43 238 13 15 14 9 | 63 63 165 70 67 65 63
R21E | 1821 22 34 21 52 23 22 13 | 43 44 36 59 31 40 35
R22E | 1477 14 36 28 19 19 13 9 | 47 40 57 59 43 50 46
R24E | 1482 8 24 22 46 10 17 10 | 33 33 30 51 29 30 30
XR28E |10506 91 --- --- --- 107 --- 99 | 105 --- --- --- 162 --- 89
------+-----------------------------------------+-------------------------------------
RMS | 1911 16 32 59 22 18 16 |T 54 61 81 50 57 45 56
WRMS | 1911 16 30 20 22 18 16 |NE 47 62 83 42 50 37 53
MEDI | 1482 14 28 19 15 19 14 |MD 48 44 46 45 49 40 46
Table 3.2403.2 GPS week: 2403 Day: 2 MJD: 61067
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1566 23 19 17 18 14 13 8 | 55 42 39 39 45 36 41
R03 | 2360 13 23 17 16 15 22 8 | 73 64 67 76 58 54 65
R04 | 1015 7 21 11 13 15 17 6 | 66 77 73 79 81 61 71
R05 | 1748 7 37 15 13 30 17 9 | 53 54 61 66 64 47 56
XR06 | 1049 36 890 1162 --- 49 --- 42 | 59 278 616 --- 78 --- 81
R07 | 2104 15 26 16 16 23 25 9 | 72 69 59 76 82 53 66
R08 | 1118 11 42 10 11 27 30 10 | 55 77 61 61 73 44 57
R09 | 885 11 57 13 7 13 9 8 | 7 41 15 12 13 13 8
R11 | 1763 9 23 10 9 14 12 5 | 28 34 32 35 29 41 31
R12 | 671 14 29 17 18 15 10 7 | 36 30 38 24 35 27 30
R14 | 1021 13 31 12 10 21 15 7 | 46 51 36 43 40 43 41
R15 | 1004 23 26 17 19 14 17 8 | 48 45 44 33 37 33 38
R16 | 1043 18 26 26 19 19 18 9 | 52 57 60 39 35 37 45
R17E | 1866 16 21 16 19 37 20 10 | 115 111 119 106 90 108 108
R18E | 1266 18 23 22 43 18 17 11 | 20 24 21 47 23 13 17
XR19E | 2084 12 22 9 --- 19 16 7 | 53 50 53 --- 60 60 54
R20E | 2207 13 37 197 11 19 16 9 | 37 32 133 30 32 37 33
R21E | 1933 18 37 9 54 18 15 12 | 27 33 31 76 29 30 31
R22E | 1455 19 25 12 34 15 19 9 | 32 33 27 44 31 32 29
R24E | 1786 18 23 15 26 27 15 9 | 41 37 37 45 41 27 34
XR28E | 8464 118 --- --- --- 157 --- 136 | 96 --- --- --- 220 --- 117
------+-----------------------------------------+-------------------------------------
RMS | 1568 15 31 49 23 21 18 |T 51 61 81 51 56 41 50
WRMS | 1568 15 30 15 16 21 18 |NE 50 70 92 48 51 40 48
MEDI | 1566 15 26 15 16 19 17 |MD 52 45 44 44 41 37 41
Table 3.2403.3 GPS week: 2403 Day: 3 MJD: 61068
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1553 16 20 11 12 29 16 7 | 64 66 60 57 46 46 55
R03 | 1266 17 14 19 14 21 10 7 | 75 64 57 75 50 64 64
R04 | 828 11 18 15 17 18 18 7 | 77 79 86 80 81 90 81
R05 | 1723 10 25 12 14 25 18 7 | 66 68 66 81 77 55 68
XR06 | 987 34 937 1104 --- 57 --- 45 | 27 289 631 --- 64 --- 51
R07 | 1531 11 20 17 9 20 28 7 | 71 71 66 70 77 47 66
R08 | 1599 18 42 23 10 18 34 10 | 49 77 71 69 50 38 58
XR09 | 779 13 44 11 10 13 --- 9 | 15 28 14 15 15 --- 11
R11 | 2226 8 42 14 10 17 23 8 | 18 43 16 22 29 29 19
R12 | 607 17 36 8 6 11 14 7 | 29 23 19 18 20 24 17
R14 | 1170 13 20 7 9 17 15 6 | 42 45 35 34 33 28 34
R15 | 2407 21 26 23 14 25 23 9 | 47 41 41 30 36 23 33
R16 | 1407 13 36 23 19 17 28 10 | 52 63 58 36 55 32 46
R17E | 2605 16 14 14 13 23 21 7 | 149 147 150 134 138 142 143
R18E | 1309 10 24 11 15 27 11 7 | 29 31 25 26 33 25 24
XR19E | 1224 16 26 11 --- 20 12 8 | 65 62 68 --- 57 64 62
R20E | 2249 12 32 217 15 18 15 9 | 36 45 185 45 34 42 38
R21E | 1468 14 18 16 19 21 12 7 | 28 39 29 38 28 26 27
R22E | 1130 18 22 10 23 19 13 8 | 41 45 38 49 40 36 38
R24E | 1232 22 17 11 21 26 21 9 | 41 44 44 45 52 40 41
XR28E |15425 60 --- --- --- 100 --- 78 | 94 --- --- --- 100 --- 74
------+-----------------------------------------+-------------------------------------
RMS | 1637 15 27 54 15 21 20 |T 53 68 87 51 53 47 50
WRMS | 1637 15 27 14 13 22 20 |NE 48 73 93 48 48 43 46
MEDI | 1407 16 24 14 14 20 16 |MD 47 45 57 45 50 38 46
Table 3.2403.4 GPS week: 2403 Day: 4 MJD: 61069
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1552 7 26 13 16 21 30 8 | 60 61 63 73 76 40 61
R03 | 1143 13 30 12 14 26 20 8 | 74 60 76 74 55 56 67
R04 | 739 11 19 10 12 21 9 6 | 75 65 67 72 63 65 68
R05 | 1693 10 34 13 16 16 19 7 | 66 63 69 62 65 57 62
XR06 | 909 33 932 1111 --- 56 --- 43 | 73 306 594 --- 92 --- 79
R07 | 1024 17 24 15 12 14 23 7 | 67 65 64 58 65 51 60
R08 | 1625 11 43 23 22 35 23 11 | 45 69 46 50 48 37 43
XR09 | 837 9 33 8 15 25 --- 8 | 18 25 13 22 34 --- 17
R11 | 1265 15 30 14 11 13 17 7 | 34 42 44 38 36 34 35
R12 | 914 12 45 9 9 21 8 7 | 28 29 26 22 38 22 24
R14 | 1434 9 29 10 8 14 13 6 | 41 51 44 40 44 36 41
R15 | 2612 24 32 15 9 13 27 9 | 46 23 35 35 46 25 33
R16 | 1131 17 32 21 26 21 16 9 | 52 57 56 31 50 39 44
R17E | 2805 9 17 19 21 30 18 8 | 57 69 59 55 78 56 58
R18E | 1006 12 25 13 21 17 15 7 | 30 38 29 36 22 33 28
XR19E | 904 14 32 9 --- 20 19 9 | 37 42 32 --- 37 38 33
R20E | 2369 9 40 171 12 23 16 9 | 66 59 107 61 67 64 62
R21E | 1238 11 38 22 21 17 12 9 | 32 37 37 40 34 28 30
R22E | 850 14 14 16 14 17 16 7 | 41 40 47 56 40 43 44
R24E | 1235 18 17 15 24 20 27 9 | 30 27 29 36 35 31 27
XR28E |17010 76 --- --- --- 127 --- 98 | 206 --- --- --- 149 --- 174
------+-----------------------------------------+-------------------------------------
RMS | 1566 14 31 44 17 21 19 |T 56 61 76 47 55 41 51
WRMS | 1566 14 31 14 14 21 19 |NE 52 70 92 48 54 42 48
MEDI | 1235 12 30 14 14 21 17 |MD 46 51 46 40 48 38 44
Table 3.2403.5 GPS week: 2403 Day: 5 MJD: 61070
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 839 11 13 28 13 23 18 8 | 56 52 39 58 62 42 50
R03 | 1552 9 18 13 13 15 20 6 | 65 72 63 73 65 52 64
R04 | 966 8 17 9 25 22 22 8 | 70 70 68 83 51 55 66
R05 | 2392 9 35 16 15 9 12 6 | 60 66 71 61 57 57 60
XR06 | 899 36 910 1094 --- 69 --- 50 | 37 286 464 --- 75 --- 43
R07 | 1007 9 29 9 15 16 13 6 | 64 79 66 68 58 60 64
R08 | 1501 12 41 24 12 20 23 9 | 49 69 57 53 36 45 47
R09 | 1517 11 39 16 6 17 19 7 | 18 30 24 21 28 24 18
R11 | 2192 9 19 10 8 22 16 6 | 30 43 30 43 23 37 31
R12 | 920 7 25 17 7 15 10 5 | 35 36 40 38 37 36 36
R14 | 1479 6 23 15 16 12 8 5 | 36 39 43 31 30 29 33
R15 | 2006 11 26 15 10 10 13 6 | 44 45 41 47 42 41 42
R16 | 2222 13 40 9 8 12 24 7 | 48 64 36 43 47 39 43
R17E | 2319 10 20 18 25 20 16 8 | 61 66 73 59 64 59 61
R18E | 1443 8 27 15 14 11 10 6 | 20 25 20 24 18 16 16
XR19E | 999 8 34 11 --- 13 13 7 | 43 38 47 --- 44 41 41
R20E | 2588 10 38 167 10 21 19 9 | 59 66 106 65 63 55 58
R21E | 1706 11 38 24 27 17 13 9 | 36 39 44 50 32 35 36
R22E | 1013 11 26 15 17 17 13 7 | 37 38 42 39 36 34 35
R24E | 1038 15 22 14 24 12 10 7 | 39 40 43 44 46 44 40
XR28E |15779 62 --- --- --- 118 --- 85 | 125 --- --- --- 72 --- 103
------+-----------------------------------------+-------------------------------------
RMS | 1688 10 29 42 16 17 16 |T 49 63 70 50 46 42 47
WRMS | 1688 10 26 15 12 17 16 |NE 47 73 80 51 47 43 45
MEDI | 1501 10 26 15 13 17 13 |MD 44 45 43 47 46 41 43
Table 3.2403.6 GPS week: 2403 Day: 6 MJD: 61071
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 843 18 20 9 14 9 13 6 | 75 60 56 69 63 52 62
R03 | 1087 11 12 10 13 11 18 5 | 91 79 91 88 79 72 84
R04 | 1688 6 16 10 12 10 16 5 | 96 91 98 102 93 85 94
R05 | 2682 9 36 13 9 10 19 7 | 82 85 89 83 81 70 80
XR06 | 880 46 872 1060 --- 45 --- 45 | 47 366 739 --- 82 --- 64
R07 | 851 14 24 8 17 15 13 6 | 95 98 83 93 84 75 85
R08 | 2267 15 30 11 20 13 24 8 | 65 87 70 74 72 53 66
R09 | 2880 10 39 14 16 13 14 7 | 19 26 20 28 22 18 17
R11 | 1305 8 27 16 19 18 14 7 | 39 48 43 44 44 41 40
R12 | 594 21 37 14 12 11 12 7 | 46 29 42 33 48 32 38
R14 | 658 17 29 12 14 8 8 6 | 49 49 41 42 41 39 42
R15 | 804 17 28 8 9 19 8 6 | 53 62 50 52 47 50 49
R16 | 1622 15 50 18 16 15 18 9 | 61 86 69 61 59 52 60
R17E | 1944 15 21 13 15 16 14 6 | 76 74 83 81 78 71 76
R18E | 658 8 24 11 17 11 13 6 | 33 39 29 36 30 29 30
XR19E | 1505 17 30 14 --- 9 17 8 | 73 62 78 --- 71 75 71
R20E | 2103 8 37 201 7 16 14 8 | 82 73 139 84 82 82 80
R21E | 1875 12 48 15 29 11 15 9 | 34 52 39 45 30 33 32
R22E | 1302 13 47 16 21 16 13 8 | 37 59 33 52 34 38 37
R24E | 1170 11 23 13 19 14 15 6 | 50 49 58 55 57 53 52
XR28E |22174 70 --- --- --- 69 --- 70 | 84 --- --- --- 67 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 1617 13 32 49 16 14 15 |T 61 78 97 62 60 53 58
WRMS | 1617 14 28 11 14 14 15 |NE 62 89 114 64 62 53 60
MEDI | 1305 14 29 13 15 13 14 |MD 61 62 58 55 63 52 62
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