[IGSREPORT-30805] Wk 2404 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 20 03:27:35 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2404 (Feb 01, 2026 - Feb 07, 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 2.2404.
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:
igl2404[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2404 in the SP3 format.
igl24047.sum Combination Report for GPS Week 2404.
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 | 4.0 ns
1 | 4.7 ns
2 | 5.3 ns
3 | 5.7 ns
4 | 6.1 ns
5 | 3.7 ns
6 | 3.2 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
2 | ESA | R06
3 | ALL | R28
3 | ESA | R06
4 | ALL | R28
4 | ESA | R06
5 | ALL | R26
5 | ESA | R06
6 | ALL | R26
6 | ESA | R06
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 1.2404, 1a.2404).
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 2.2404.0-6)
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 3.2404.0-6).
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 2404 summary. (Feb 01, 2026 - Feb 07, 2026)
Table 1.2404.a GPS week : 2404 MJD: 61072.0-61078.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -1 16 -3 -20 .11 14 14 | 4283 -1013 3534 9955
| 0 0 0 11 18 19 .04 | 698 2047
esa n/a| 0 0 0 -35 13 38 -.13 31 29 | 7786 -1171 3579 10167
| 2 2 1 11 24 41 .04 | 489 1940
gfz n/a| -1 0 0 19 9 26 -.16 23 14 | 0 -988 3542 10020
| 0 1 1 23 12 21 .05 | 0 2036
grg n/a| 2 0 1 6 -22 -12 .33 17 14 | 5014 -1116 3642 9359
| 0 1 3 21 18 33 .04 | 494 2078
iac n/a| 0 0 -2 -14 18 0 -.16 16 16 | 6766 -893 3633 10725
| 1 0 2 27 10 29 .04 | 672 1142
jgx n/a| 1 0 3 -22 -14 -23 -.09 16 16 | 6861 -1024 3605 9711
| 1 0 1 14 13 23 .03 | 500 2026
Table 1.2404.b GPS week : 2404 MJD: 61072.0-61078.0
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 9 8 7 6 |
R03 | 6 9 7 5 7 6 7 |
R04 | 6 7 8 5 6 6 7 |
R05 | 8 7 8 7 7 7 7 |
R06 | 57 43 34 37 32 30 30 |
R07 | 8 9 9 8 8 8 7 |
R08 | 8 7 10 10 9 8 10 |
R09 | 7 7 8 8 7 8 8 |
R11 | 10 7 8 8 8 7 6 |
R12 | 8 10 8 7 8 7 8 |
R14 | 7 6 5 7 6 6 5 |
R15 | 8 7 7 6 7 7 8 |
R16 | 8 8 7 9 9 8 9 |
R17 | 6 7 9 6 7 11 10 |
R18 | 6 7 6 7 7 6 7 |
R19 | 8 7 8 7 8 8 7 |
R20 | 10 12 9 12 9 13 9 |
R21 | 11 10 10 9 9 9 9 |
R22 | 8 7 7 7 7 7 7 |
R24 | 7 8 9 8 9 9 7 |
R26 | --- --- 45 46 52 --- --- |
R28 | 56 56 81 --- --- 52 61 |
Table 1.2404.c GPS week : 2404 MJD: 61072.0-61078.0
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 2404 0 | -69 4 39 839 -1591 7564 79.2 1213 1213 | 4038 0
brd 2404 1 | -30 46 -122 368 440 8868 78.8 1436 1436 | 4691 0
brd 2404 2 | -48 -44 -81 -341 -879 7568 79.4 1434 1434 | 5293 0
brd 2404 3 | 78 -65 -204 259 -11 1870 79.5 1530 1530 | 5702 0
brd 2404 4 | 44 39 -97 -640 859 1526 78.4 1629 1629 | 6103 0
brd 2404 5 | 32 -12 -57 -1846 -500 3598 77.3 1419 1419 | 3670 0
brd 2404 6 | 139 136 9 -386 151 988 81.8 1527 1527 | 3221 0
-------------+------------------------------------------------------------+----------------
brd 2404 mean| 20 14 -73 -249 -218 4568 79.2 1455 1455 | 4674 0
brd 2404 sdev| 74 67 81 871 834 3335 1.4 130 130 | 1080 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 2.2404.0 GPS week: 2404 Day: 0 MJD: 61072
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 -1 -12 .14 14 15 | 4287 -1567 3422 10118
esa n/a| 0 1 1 -18 -29 -32 -.12 34 29 | 7861 -2309 3469 10784
gfz n/a| 0 2 0 11 5 32 -.10 61 14 | 0 -1943 3534 10255
grg n/a| 1 1 5 12 -23 -39 .31 19 16 | 4944 -2159 3507 9539
iac n/a| 0 0 -3 -7 16 -6 -.17 17 17 | 7262 -2302 3551 10729
jgx n/a| 2 0 2 -27 -1 0 -.08 15 15 | 6591 -1758 3483 9809
Table 2.2404.1 GPS week: 2404 Day: 1 MJD: 61073
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 13 -27 -48 .11 14 15 | 3616 855 3739 8924
esa n/a| -1 2 1 -39 27 83 -.07 28 25 | 7633 49 3791 8733
gfz n/a| -2 0 1 0 2 9 -.15 18 14 | 0 613 3740 8934
grg n/a| 3 0 1 17 -21 45 .33 17 13 | 4195 600 3886 8348
iac n/a| -1 0 -4 -19 30 -9 -.18 15 14 | 7093 161 3804 9842
jgx n/a| 1 0 3 -21 -19 -30 -.06 18 18 | 6504 337 3808 8574
Table 2.2404.2 GPS week: 2404 Day: 2 MJD: 61074
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 25 -16 -41 .17 14 15 | 3793 -648 3400 9183
esa n/a| -2 2 1 -27 3 68 -.15 32 29 | 7498 -1214 3470 8446
gfz n/a| -1 0 2 -7 -6 42 -.21 14 12 | 0 -704 3409 9247
grg n/a| 3 -2 -1 23 4 10 .34 21 18 | 5585 -1245 3495 8651
iac n/a| 0 1 -3 13 26 -47 -.07 17 15 | 6511 899 3607 10484
jgx n/a| 3 0 2 -21 -37 -32 -.05 16 16 | 6575 -782 3442 8909
Table 2.2404.3 GPS week: 2404 Day: 3 MJD: 61075
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 11 -9 11 .15 13 12 | 3574 -378 3215 9607
esa n/a| -2 -2 0 -37 16 2 -.18 31 31 | 7087 -836 3289 10202
gfz n/a| -2 0 0 23 8 35 -.16 19 18 | 0 -643 3218 9718
grg n/a| 1 -1 1 -34 -2 -50 .36 18 15 | 5457 -53 3286 9080
iac n/a| 1 2 -2 29 7 -1 -.16 14 14 | 6899 -1161 3209 10389
jgx n/a| 2 0 5 -37 -10 -34 -.08 16 16 | 6412 -503 3267 9299
Table 2.2404.4 GPS week: 2404 Day: 4 MJD: 61076
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 18 18 -23 .07 14 15 | 4902 1572 3154 10226
esa n/a| -2 0 -1 -32 15 44 -.12 33 32 | 8416 1829 3207 10468
gfz n/a| -1 -2 -1 32 20 20 -.09 15 14 | 0 2035 3158 10290
grg n/a| 1 0 4 4 -38 -6 .31 15 12 | 4990 1717 3268 9519
iac n/a| 0 0 -3 -30 24 34 -.18 15 15 | 7567 -477 3143 10832
jgx n/a| 1 1 3 -29 -22 -32 -.13 16 16 | 7618 1763 3195 9860
Table 2.2404.5 GPS week: 2404 Day: 5 MJD: 61077
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 35 -11 -18 .06 16 16 | 5445 -2434 3799 11505
esa n/a| 2 0 0 -32 8 29 -.12 30 29 | 8420 -1281 3763 11682
gfz n/a| -1 0 -3 63 29 -7 -.18 18 16 | 0 -1950 3716 11457
grg n/a| 2 -2 0 -6 -24 -6 .25 13 11 | 4601 -2147 3881 10806
iac n/a| 0 0 1 -48 1 42 -.18 16 16 | 6525 -1775 3961 12223
jgx n/a| 1 1 3 -25 3 -52 -.11 17 17 | 7528 -1468 3849 11333
Table 2.2404.6 GPS week: 2404 Day: 6 MJD: 61078
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 12 21 -12 .08 13 13 | 4368 -4494 4012 10126
esa n/a| 3 -4 0 -55 51 71 -.16 32 30 | 7592 -4438 4069 10854
gfz n/a| -1 -1 0 11 5 54 -.23 17 15 | 0 -4328 4020 10240
grg n/a| 1 -1 -4 26 -49 -39 .38 15 14 | 5328 -4529 4174 9573
iac n/a| -2 1 0 -35 25 -8 -.19 17 17 | 5509 -1599 4159 10582
jgx n/a| 0 1 2 6 -16 15 -.09 13 13 | 6801 -4761 4195 10194
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 3.2404.0 GPS week: 2404 Day: 0 MJD: 61072
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 938 14 24 16 12 14 17 7 | 48 38 54 49 50 38 46
R03 | 1166 9 17 12 14 11 19 6 | 62 59 64 65 54 45 57
R04 | 1357 13 14 8 17 11 16 6 | 75 74 74 77 71 71 73
R05 | 1575 15 33 10 17 18 17 7 | 71 72 65 67 56 50 61
XR06 | 1090 51 859 1057 --- 63 --- 56 | 64 221 827 --- 126 --- 84
R07 | 1144 17 43 14 13 16 15 8 | 73 76 65 66 68 59 65
R08 | 860 19 41 12 23 14 11 8 | 40 66 46 58 38 41 42
R09 | 1573 9 36 10 18 16 11 6 | 53 59 53 49 54 55 52
R11 | 921 14 46 20 23 24 9 9 | 46 41 45 39 55 43 42
R12 | 693 23 37 7 15 11 12 7 | 85 62 82 68 85 75 77
R14 | 694 5 44 14 10 17 10 7 | 67 84 69 61 56 59 64
R15 | 1280 13 33 12 18 19 17 7 | 78 86 70 82 68 63 72
R16 | 2239 17 40 8 22 18 15 8 | 87 88 80 84 79 70 79
R17E | 1149 7 16 12 18 11 11 5 | 125 123 126 129 126 32 125
R18E | 716 9 21 9 16 17 10 5 | 32 35 36 37 31 35 32
XR19E | 1357 15 33 11 --- 16 14 8 | 45 60 51 --- 49 43 46
R20E | 1176 15 29 256 12 21 24 10 | 59 66 166 58 62 53 59
R21E | 996 12 55 15 34 19 15 10 | 92 101 85 100 88 88 89
R22E | 750 14 37 15 22 18 14 8 | 35 44 36 42 36 42 35
R24E | 1470 13 15 16 24 16 12 7 | 83 86 89 84 78 76 81
XR28E |19456 50 --- --- --- 62 --- 56 | 121 --- --- --- 69 --- 84
------+-----------------------------------------+-------------------------------------
RMS | 1213 14 34 61 19 16 15 |T 70 77 109 67 69 54 67
WRMS | 1213 15 29 14 16 17 15 |NE 67 78 122 63 70 55 66
MEDI | 1149 14 33 12 17 17 14 |MD 67 66 65 65 62 53 64
Table 3.2404.1 GPS week: 2404 Day: 1 MJD: 61073
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 856 20 18 24 17 10 14 8 | 44 36 38 40 42 39 37
R03 | 1294 12 19 21 9 17 29 8 | 46 49 56 44 49 34 45
R04 | 681 14 19 10 13 17 21 7 | 60 65 61 61 61 58 60
R05 | 2216 11 23 8 16 10 24 7 | 55 49 53 57 50 45 51
XR06 | 1141 63 872 46 --- 66 --- 42 | 42 204 285 --- 88 --- 63
R07 | 1062 9 30 13 17 10 32 8 | 61 54 58 63 62 46 56
R08 | 1450 13 25 14 12 17 17 7 | 42 48 40 48 48 39 43
R09 | 1163 10 40 12 7 17 8 7 | 37 53 39 41 44 41 40
R11 | 1085 9 35 11 14 19 11 7 | 22 21 22 23 32 19 20
R12 | 680 28 33 16 22 20 10 9 | 69 55 60 54 70 60 61
R14 | 591 12 25 15 15 10 9 6 | 50 55 32 35 45 38 41
R15 | 1494 13 17 14 16 10 19 6 | 56 45 47 56 53 42 50
R16 | 2866 18 25 17 14 13 19 7 | 58 52 52 46 52 41 49
R17E | 1379 11 22 16 19 15 15 7 | 115 111 111 113 104 49 110
R18E | 840 6 23 17 19 21 11 7 | 32 34 32 41 34 33 31
XR19E | 1154 10 22 11 --- 12 14 6 | 27 31 32 --- 30 33 29
R20E | 1399 14 24 46 12 20 28 11 | 36 41 90 38 39 35 35
R21E | 1060 15 52 18 29 12 13 10 | 77 95 79 81 77 78 77
R22E | 1921 12 30 12 16 9 11 6 | 20 37 27 34 24 22 23
R24E | 1707 14 22 15 25 11 11 7 | 77 74 70 70 68 67 70
XR28E |19537 55 --- --- --- 56 --- 55 | 102 --- --- --- 67 --- 74
------+-----------------------------------------+-------------------------------------
RMS | 1435 14 28 18 17 15 18 |T 54 60 64 52 55 43 52
WRMS | 1435 15 25 14 13 14 18 |NE 51 60 64 47 56 41 49
MEDI | 1163 13 24 15 16 15 14 |MD 50 49 52 46 50 41 49
Table 3.2404.2 GPS week: 2404 Day: 2 MJD: 61074
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 920 23 20 15 22 17 15 8 | 49 36 39 32 32 38 36
R03 | 898 11 24 12 24 18 11 7 | 53 61 55 64 49 51 53
R04 | 910 8 18 11 12 24 23 7 | 50 64 56 59 67 45 54
R05 | 2566 11 40 11 23 12 19 8 | 46 48 50 60 39 38 45
XR06 | 1217 52 836 21 --- 67 --- 34 | 58 219 212 --- 107 --- 79
R07 | 1421 15 35 17 18 16 19 8 | 61 67 47 65 54 46 53
R08 | 2249 16 45 13 23 20 21 9 | 39 58 43 31 43 39 38
R09 | 1591 11 48 11 11 16 17 8 | 47 55 53 53 42 51 48
R11 | 970 12 37 8 31 18 11 8 | 43 73 45 71 46 44 48
R12 | 935 25 29 15 9 14 9 8 | 62 49 50 57 49 48 51
R14 | 681 8 21 10 11 13 8 5 | 49 56 51 51 41 49 48
R15 | 1443 9 29 12 22 10 20 7 | 62 49 59 78 65 50 59
R16 | 1593 17 32 13 12 13 15 7 | 70 45 61 57 67 55 60
R17E | 1237 13 29 14 23 22 18 8 | 104 93 101 99 103 50 98
R18E | 1187 15 23 6 13 16 13 6 | 28 38 32 37 34 40 32
XR19E | 1086 18 30 8 --- 15 13 7 | 43 31 37 --- 34 39 37
R20E | 732 6 38 23 16 24 18 9 | 44 60 71 50 42 44 48
R21E | 1346 12 37 13 37 17 18 9 | 48 60 51 59 51 46 48
R22E | 1775 15 29 11 17 11 15 7 | 36 32 31 40 32 29 31
R24E | 1724 14 24 20 32 16 11 8 | 34 36 39 38 34 26 30
XR26 |12562 39 --- --- --- 51 --- 45 | 113 --- --- --- 118 --- 111
XR28E |24775 73 --- --- --- 90 --- 81 | 126 --- --- --- 65 --- 78
------+-----------------------------------------+-------------------------------------
RMS | 1433 14 32 14 21 17 16 |T 57 61 59 55 55 43 53
WRMS | 1433 15 29 12 18 15 16 |NE 57 67 63 56 58 46 55
MEDI | 1237 14 29 12 18 16 15 |MD 49 55 50 57 46 45 48
Table 3.2404.3 GPS week: 2404 Day: 3 MJD: 61075
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1086 19 26 21 20 18 13 8 | 52 39 39 35 47 36 40
R03 | 976 8 22 10 12 11 8 5 | 62 64 63 62 56 59 60
R04 | 827 8 20 12 10 8 15 5 | 59 63 68 71 66 61 63
R05 | 2019 9 29 13 18 10 23 7 | 51 49 53 61 52 39 49
XR06 | 1032 41 799 37 --- 70 --- 36 | 27 160 145 --- 87 --- 43
R07 | 1042 11 20 9 25 12 25 8 | 59 61 55 74 54 39 55
R08 | 1128 15 43 26 15 15 27 10 | 40 72 61 40 52 26 44
R09 | 2089 9 43 16 18 12 12 7 | 32 36 41 31 34 34 32
R11 | 1535 13 39 18 21 12 11 8 | 21 46 25 46 26 20 23
R12 | 783 17 37 12 7 11 15 7 | 43 25 30 37 35 23 31
R14 | 2600 10 30 14 11 20 7 6 | 51 62 56 53 38 47 48
R15 | 1026 11 28 14 13 9 13 6 | 58 64 47 48 59 45 52
R16 | 1343 11 36 20 15 17 19 8 | 72 62 71 61 76 55 66
R17E | 1330 11 23 14 17 14 10 6 | 100 100 94 98 91 49 96
R18E | 1853 10 27 11 17 17 19 7 | 24 32 24 30 28 29 24
XR19E | 1090 14 28 13 --- 12 10 7 | 22 41 28 --- 26 24 24
R20E | 725 11 37 46 19 23 19 12 | 29 45 43 50 31 33 33
R21E | 1699 16 31 13 26 17 14 8 | 34 51 38 46 40 35 35
R22E | 2400 14 24 13 15 12 13 6 | 25 33 25 38 24 25 25
R24E | 1241 14 23 21 25 14 12 8 | 33 32 39 35 32 27 29
XR26 |11670 43 --- --- --- 49 --- 46 | 98 --- --- --- 108 --- 100
------+-----------------------------------------+-------------------------------------
RMS | 1530 13 31 19 18 14 16 |T 50 56 52 50 52 37 48
WRMS | 1530 12 31 18 15 14 16 |NE 51 61 58 51 56 40 50
MEDI | 1241 11 28 14 17 14 13 |MD 43 49 43 46 47 35 43
Table 3.2404.4 GPS week: 2404 Day: 4 MJD: 61076
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 858 21 27 11 15 14 21 8 | 54 47 48 44 48 37 45
R03 | 959 10 20 12 18 9 23 7 | 60 55 62 60 48 54 56
R04 | 857 12 25 12 9 12 8 5 | 64 72 63 71 60 67 64
R05 | 689 10 32 9 18 15 7 6 | 61 65 60 80 56 69 64
XR06 | 956 36 847 31 --- 62 --- 32 | 58 197 94 --- 89 --- 62
R07 | 1102 13 21 14 11 9 32 8 | 62 54 62 67 57 45 57
R08 | 996 18 42 19 15 10 23 9 | 37 67 55 55 42 34 45
R09 | 1281 12 46 9 12 11 9 7 | 43 54 41 41 46 41 42
R11 | 1819 9 41 18 16 15 11 7 | 31 26 42 20 32 31 28
R12 | 1429 16 40 16 8 25 9 8 | 52 50 54 45 46 51 47
R14 | 3843 7 25 14 8 13 15 6 | 46 62 53 49 48 41 47
R15 | 820 21 30 17 7 8 11 7 | 53 48 30 37 45 37 39
R16 | 1451 21 42 14 12 18 16 8 | 66 61 57 47 59 48 54
R17E | 2283 11 19 17 19 15 10 6 | 70 62 71 60 73 54 65
R18E | 1859 7 27 9 19 14 15 6 | 33 35 35 41 36 35 34
XR19E | 1346 12 29 13 --- 17 12 8 | 34 44 38 --- 33 36 34
R20E | 1344 7 44 21 10 23 15 8 | 31 42 33 28 29 30 28
R21E | 1246 15 44 11 26 18 14 9 | 50 68 52 52 51 45 48
R22E | 1932 15 25 13 12 13 13 6 | 26 31 26 32 29 30 26
R24E | 1533 16 21 20 20 16 22 8 | 38 42 49 44 34 26 36
XR26 | 8476 51 --- --- --- 51 --- 51 | 124 --- --- --- 114 --- 117
------+-----------------------------------------+-------------------------------------
RMS | 1628 14 33 15 15 15 16 |T 54 59 51 48 52 42 49
WRMS | 1628 15 32 14 12 15 16 |NE 57 66 55 51 56 46 54
MEDI | 1344 13 29 14 12 15 14 |MD 52 54 52 45 48 41 47
Table 3.2404.5 GPS week: 2404 Day: 5 MJD: 61077
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1089 19 17 11 15 15 20 7 | 43 48 43 53 39 40 43
R03 | 1370 11 18 10 11 9 19 5 | 56 47 49 57 52 43 51
R04 | 1001 18 11 15 14 10 9 6 | 64 67 71 62 63 66 64
R05 | 631 16 33 13 11 15 8 6 | 57 66 55 50 51 54 52
XR06 | 944 49 831 27 --- 47 --- 30 | 56 188 104 --- 79 --- 74
R07 | 1959 7 19 17 14 20 26 8 | 76 76 75 68 83 61 72
R08 | 865 11 32 16 11 18 27 8 | 37 42 38 36 44 32 36
R09 | 841 11 53 10 8 13 8 7 | 27 46 29 27 23 26 25
R11 | 1543 13 37 11 5 15 9 6 | 34 42 47 43 43 41 40
R12 | 1162 24 29 11 8 8 8 6 | 56 47 54 48 55 47 51
R14 | 1897 12 21 12 8 10 18 5 | 47 54 44 48 43 40 44
R15 | 1243 18 28 12 9 12 18 7 | 60 67 53 63 58 48 57
R16 | 956 18 29 16 15 16 20 8 | 64 65 60 54 55 48 55
XR17E | 1675 15 24 30 21 13 --- 10 | 128 131 125 132 126 --- 127
R18E | 2602 11 20 12 9 18 13 6 | 31 32 33 34 31 30 30
XR19E | 1281 11 25 18 --- 18 10 8 | 34 44 41 --- 40 38 37
R20E | 998 17 40 49 7 28 16 12 | 34 42 54 33 37 33 33
R21E | 1332 17 46 16 21 16 12 9 | 64 84 69 79 67 70 70
R22E | 1915 14 22 13 16 16 16 7 | 25 33 24 31 31 26 26
R24E | 1200 23 21 16 20 13 20 8 | 50 52 52 54 48 42 47
XR28E |14149 55 --- --- --- 49 --- 52 | 57 --- --- --- 86 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 1418 16 30 18 13 16 17 |T 58 63 56 54 61 43 58
WRMS | 1418 16 29 16 11 16 17 |NE 62 65 55 50 63 45 61
MEDI | 1243 16 25 13 11 15 16 |MD 56 48 52 50 51 41 51
Table 3.2404.6 GPS week: 2404 Day: 6 MJD: 61078
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1767 12 28 13 11 16 8 6 | 67 55 61 62 59 59 61
R03 | 1341 12 27 10 15 16 20 7 | 83 84 78 81 81 67 77
R04 | 1298 16 21 9 18 10 17 7 | 92 98 88 93 88 81 88
R05 | 663 12 32 18 17 13 10 7 | 81 87 83 77 82 75 78
XR06 | 942 39 801 20 --- 58 --- 29 | 60 295 182 --- 107 --- 76
R07 | 1685 15 26 15 11 16 10 6 | 112 120 104 105 110 101 106
R08 | 883 17 39 28 11 25 17 9 | 56 79 62 57 67 47 57
R09 | 2154 9 49 18 8 14 10 7 | 32 42 33 33 29 32 30
R11 | 1779 10 21 12 7 19 9 5 | 28 38 35 35 40 28 31
R12 | 831 18 27 19 24 8 11 8 | 68 53 69 51 61 57 59
R14 | 1484 5 23 12 10 16 6 5 | 53 66 60 54 46 51 53
R15 | 1271 17 26 22 11 16 12 7 | 70 78 74 72 64 61 67
R16 | 1033 16 29 13 14 23 22 8 | 77 71 78 78 69 68 72
XR17E | 1347 13 17 14 24 25 --- 9 | 185 176 185 187 168 --- 180
R18E | 2196 9 25 18 13 16 14 6 | 38 38 40 42 40 34 36
XR19E | 1389 11 29 11 --- 11 14 7 | 39 45 45 --- 45 44 42
R20E | 1524 8 42 27 10 22 12 8 | 39 51 31 44 39 39 38
R21E | 894 11 44 13 28 14 11 8 | 110 110 112 121 109 109 111
R22E | 1757 11 34 15 19 17 9 7 | 30 40 26 42 37 33 32
R24E | 2133 14 30 14 18 20 9 7 | 90 95 95 91 88 95 91
XR28E |10731 51 --- --- --- 72 --- 61 | 117 --- --- --- 88 --- 98
------+-----------------------------------------+-------------------------------------
RMS | 1527 13 32 17 15 17 13 |T 78 86 77 73 78 60 76
WRMS | 1527 13 30 15 14 17 13 |NE 77 89 77 66 80 60 75
MEDI | 1389 12 28 14 13 16 11 |MD 68 71 69 62 67 57 67
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