[IGSREPORT-30786] Wk 2402 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 6 02:00:02 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2402 (Jan 18, 2026 - Jan 24, 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 2.2402.
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:
igl2402[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2402 in the SP3 format.
igl24027.sum Combination Report for GPS Week 2402.
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 | 5.6 ns
1 | 5.0 ns
2 | 5.0 ns
3 | 4.4 ns
4 | 5.4 ns
5 | 4.5 ns
6 | 4.0 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
1 | IAC | R08
2 | ALL | R26
2 | ESA | R06
2 | GFZ | R06
3 | ALL | R26
3 | ESA | R06
3 | GFZ | R06
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 1.2402, 1a.2402).
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 2.2402.0-6)
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 3.2402.0-6).
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 2402 summary. (Jan 18, 2026 - Jan 24, 2026)
Table 1.2402.a GPS week : 2402 MJD: 61058.0-61064.0
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 -1 -1 2 11 -4 .12 14 14 | 3413 -609 3542 10449
| 0 1 1 16 17 22 .05 | 545 636
esa n/a| -1 0 -1 -45 -13 26 -.08 33 30 | 6235 -617 3552 10377
| 2 2 1 25 9 24 .04 | 773 759
gfz n/a| 0 0 0 19 12 1 -.22 77 16 | 0 -636 3723 10186
| 0 0 2 16 10 36 .07 | 0 666
grg n/a| 0 0 -2 2 -36 20 .38 16 14 | 4999 -697 3659 9202
| 1 1 2 22 17 22 .05 | 494 953
iac n/a| 0 1 -2 5 30 -1 -.14 19 19 | 6988 -1141 3690 11390
| 1 1 3 23 28 45 .05 | 747 1493
jgx n/a| 0 0 4 -7 -12 -24 -.17 16 16 | 6120 -996 3574 9473
| 1 1 1 21 10 34 .06 | 450 951
Table 1.2402.b GPS week : 2402 MJD: 61058.0-61064.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R02 | 7 7 9 8 9 10 7 |
R03 | 7 8 8 8 6 6 8 |
R04 | 7 7 8 8 8 7 7 |
R05 | 9 9 7 9 8 8 8 |
R06 | 53 53 56 53 54 47 55 |
R07 | 7 8 8 10 11 7 7 |
R08 | 16 28 9 11 9 9 9 |
R09 | 10 8 11 9 7 9 8 |
R11 | 9 7 7 10 9 6 7 |
R12 | 8 8 9 11 7 8 8 |
R14 | 5 6 7 6 6 7 8 |
R15 | 8 7 7 8 8 8 8 |
R16 | 8 8 9 9 7 9 8 |
R17 | 8 9 7 8 7 7 7 |
R18 | 6 7 8 7 7 7 7 |
R19 | 9 10 11 12 9 10 9 |
R20 | 9 11 45 43 9 10 9 |
R21 | 9 10 10 10 10 11 10 |
R22 | 8 8 9 8 6 8 9 |
R24 | 10 12 10 10 9 10 8 |
R28 | 74 0 404 418 115 66 60 |
Table 1.2402.c GPS week : 2402 MJD: 61058.0-61064.0
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 2402 0 | -37 11 -107 -779 992 6064 81.8 1743 1743 | 5630 0
brd 2402 1 | -74 60 -54 -2052 1956 -669 78.7 1785 1785 | 4983 0
brd 2402 2 | -14 -62 8 -2395 -726 -2411 75.2 1617 1617 | 4995 0
brd 2402 3 | -63 52 36 -3615 -355 -4011 80.5 1660 1660 | 4388 0
brd 2402 4 | 84 36 47 -1693 737 -6750 80.8 1801 1801 | 5443 0
brd 2402 5 | 77 146 72 1054 -2841 -1942 80.0 1782 1782 | 4534 0
brd 2402 6 | -104 -16 -54 -882 -1977 -688 79.1 2037 2037 | 4003 0
-------------+------------------------------------------------------------+----------------
brd 2402 mean| -18 32 -7 -1480 -316 -1486 79.5 1775 1775 | 4853 0
brd 2402 sdev| 73 65 65 1474 1697 3946 2.1 134 134 | 581 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 2.2402.0 GPS week: 2402 Day: 0 MJD: 61058
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 -21 -12 -8 .11 14 14 | 2596 144 3777 8799
esa n/a| -4 3 -2 -55 -23 38 -.08 32 32 | 5316 116 3819 8792
gfz n/a| 0 0 2 15 4 -43 -.31 86 15 | 0 54 3975 8343
grg n/a| 2 0 -2 24 -41 27 .45 14 12 | 5099 524 3892 7645
iac n/a| -1 0 -5 2 67 41 -.09 19 19 | 6966 435 3882 9886
jgx n/a| 0 0 5 9 -18 -66 -.06 15 15 | 5594 -705 3669 8001
Table 2.2402.1 GPS week: 2402 Day: 1 MJD: 61059
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 10 -13 -47 .18 14 14 | 3558 -572 3122 11560
esa n/a| -4 1 -4 -58 -15 64 -.14 31 29 | 5902 -1167 2946 9538
gfz n/a| -1 1 -2 -10 13 16 -.22 86 15 | 0 -617 3357 11167
grg n/a| 2 -1 0 -31 -57 24 .31 16 15 | 5365 -1029 3233 10487
iac n/a| -1 0 -2 47 49 -52 -.08 15 15 | 7713 -1453 3106 12225
jgx n/a| 1 -1 5 -26 -13 21 -.14 17 17 | 6125 -2244 2930 9603
Table 2.2402.2 GPS week: 2402 Day: 2 MJD: 61060
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 -5 24 19 .05 15 14 | 3801 -860 3985 10770
esa n/a| -3 -3 -1 -6 -20 14 -.04 36 30 | 5194 -119 3989 10401
gfz n/a| 0 0 -1 9 18 -57 -.27 86 17 | 0 -393 4122 10744
grg n/a| 2 0 -2 31 -22 47 .38 17 15 | 5340 -906 4143 9534
iac n/a| 0 4 -3 -3 42 -3 -.20 19 19 | 7020 -1047 4283 11697
jgx n/a| 0 -1 5 -18 -29 -39 -.14 18 18 | 6665 -578 4212 10364
Table 2.2402.3 GPS week: 2402 Day: 3 MJD: 61061
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 -3 -1 30 9 -6 .07 15 15 | 3038 -1602 3292 10469
esa n/a| -1 0 -2 -26 -12 26 -.08 37 32 | 6575 -1011 3361 10870
gfz n/a| 1 0 0 31 10 9 -.22 76 19 | 0 -1819 3501 10295
grg n/a| 0 0 -6 -2 -7 0 .33 17 14 | 5205 -2231 3332 8984
iac n/a| 0 1 2 27 11 68 -.17 25 26 | 6771 -2124 3527 11334
jgx n/a| -1 1 7 -40 1 11 -.26 19 19 | 6297 -2257 3330 9432
Table 2.2402.4 GPS week: 2402 Day: 4 MJD: 61062
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 -1 -1 22 -2 .09 13 14 | 2980 186 3701 10163
esa n/a| 0 1 -1 -30 -4 42 -.02 30 26 | 6658 478 3756 10529
gfz n/a| 0 0 -2 36 -1 25 -.08 74 14 | 0 128 3874 9833
grg n/a| 0 0 0 -14 -28 16 .36 17 15 | 5089 147 3860 8999
iac n/a| -2 0 1 0 38 -46 -.22 20 20 | 6200 1105 3841 11012
jgx n/a| 0 1 3 14 -18 -8 -.18 14 14 | 5478 183 3768 9291
Table 2.2402.5 GPS week: 2402 Day: 5 MJD: 61063
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 -7 22 -2 .15 14 15 | 3868 -1025 3281 11103
esa n/a| 2 0 1 -57 0 7 -.07 34 31 | 6797 -1482 3307 11588
gfz n/a| 0 0 0 34 13 24 -.24 61 13 | 0 -944 3419 10976
grg n/a| 0 2 0 -1 -49 42 .43 17 14 | 4976 -1306 3390 9821
iac n/a| 0 0 -6 -16 23 16 -.13 19 19 | 8155 -3270 3533 12365
jgx n/a| 1 0 3 -8 -9 -62 -.18 15 15 | 6567 -1156 3340 10213
Table 2.2402.6 GPS week: 2402 Day: 6 MJD: 61064
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 14 27 17 .18 14 14 | 4054 -534 3638 10285
esa n/a| 1 0 0 -82 -22 -6 -.13 31 30 | 7204 -1135 3687 10926
gfz n/a| 0 0 -3 19 29 34 -.22 71 17 | 0 -865 3818 9950
grg n/a| 0 0 -3 14 -47 -14 .41 17 15 | 3925 -81 3767 8946
iac n/a| -1 1 -3 -16 -21 -32 -.12 17 17 | 6095 -1637 3660 11215
jgx n/a| 0 0 3 14 0 -25 -.20 15 15 | 6115 -217 3770 9412
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 3.2402.0 GPS week: 2402 Day: 0 MJD: 61058
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1805 18 31 9 17 11 13 7 | 82 68 64 72 66 57 67
R03 | 4577 12 18 9 17 13 21 7 | 86 85 89 93 87 71 84
R04 | 784 12 19 9 15 16 17 6 | 82 81 81 82 78 71 78
R05 | 2012 10 35 19 15 19 20 8 | 148 133 149 155 128 142 143
XR06 | 1121 45 1013 1279 --- 62 --- 53 | 69 464 721 --- 107 --- 81
R07M | 1609 20 17 15 12 12 18 7 | 89 78 74 78 85 67 78
XR08M | 3086 23 31 23 41 34 --- 15 | 85 82 72 112 108 --- 86
R09M | 803 16 69 8 10 11 12 9 | 109 113 110 101 111 109 107
R11M | 2350 9 29 18 12 40 7 9 | 25 24 29 27 40 23 22
R12M | 622 19 21 15 14 12 18 7 | 39 39 32 28 29 29 29
R14M | 1407 5 19 9 12 12 10 5 | 44 55 48 42 47 46 44
R15M | 731 13 25 22 16 21 10 8 | 53 41 40 55 57 36 45
R16M | 1133 18 27 21 13 15 16 8 | 59 56 45 50 51 39 48
R17E | 1549 10 24 13 20 20 16 7 | 108 110 111 108 110 106 108
R18E | 963 7 23 12 11 19 10 6 | 30 37 27 34 32 23 28
XR19E | 2086 11 25 10 --- 18 --- 8 | 59 54 56 --- 62 --- 58
R20E | 868 12 36 342 8 23 14 8 | 73 70 184 73 64 73 68
R21E | 888 13 46 19 15 17 14 8 | 159 169 154 152 150 159 155
R22E | 1385 17 36 14 10 17 13 7 | 46 63 46 51 55 43 47
XR24E | 2549 12 32 14 28 15 --- 10 | 54 53 54 69 57 --- 55
XR28E |16080 64 --- --- --- 85 --- 74 | 207 --- --- --- 9999 --- 186
------+-----------------------------------------+-------------------------------------
RMS | 1743 14 32 86 14 19 15 |T 81 93 109 76 76 68 77
WRMS | 1743 14 32 15 12 19 15 |NE 93 166 220 100 93 85 90
MEDI | 1407 13 27 14 14 17 14 |MD 73 68 64 72 64 57 68
Table 3.2402.1 GPS week: 2402 Day: 1 MJD: 61059
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1366 16 19 15 15 14 20 7 | 64 52 47 56 63 49 55
R03 | 4603 10 20 17 17 11 24 7 | 71 63 68 67 67 52 64
R04 | 1012 10 18 17 16 15 18 7 | 62 61 74 70 60 59 63
R05 | 2259 17 32 22 11 16 24 8 | 130 132 144 139 118 140 133
XR06 | 1071 53 979 1243 --- 51 --- 52 | 57 335 523 --- 75 --- 65
R07M | 1002 19 38 16 10 12 10 7 | 78 96 66 67 73 68 71
XR08M | 8011 25 --- 48 40 309 --- 27 | 99 --- 71 117 262 --- 93
R09M | 1256 14 53 13 14 10 9 8 | 92 87 90 93 98 91 92
R11M | 2027 10 34 9 11 15 13 6 | 22 40 25 24 28 21 21
R12M | 849 18 39 15 12 10 12 7 | 47 55 46 40 51 42 44
R14M | 2066 8 19 16 16 11 7 5 | 28 36 40 29 33 36 32
R15M | 996 17 22 12 7 9 23 6 | 38 50 44 32 39 23 35
R16M | 1198 11 26 15 17 17 21 7 | 42 58 44 33 47 34 40
R17E | 1449 7 23 19 26 14 21 8 | 79 82 78 79 82 79 78
R18E | 929 11 26 13 16 16 10 6 | 22 29 20 31 24 18 19
XR19E | 2164 11 31 14 --- 16 --- 9 | 36 33 37 --- 38 --- 36
R20E | 1018 7 41 341 20 26 17 10 | 61 59 125 65 52 62 61
R21E | 1400 15 40 19 14 24 19 9 | 141 153 142 143 143 136 141
R22E | 1310 20 26 11 19 14 16 7 | 26 40 27 33 35 31 29
XR24E | 1459 22 28 15 33 18 --- 11 | 71 70 63 56 56 --- 60
XR28E | ---- --- --- --- --- --- --- 0 | 161 --- --- --- 9999 --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1785 14 31 86 16 15 17 |T 67 80 88 65 72 58 61
WRMS | 1785 14 29 15 15 15 17 |NE 76 128 171 83 76 75 76
MEDI | 1310 14 28 15 16 15 17 |MD 62 59 63 56 56 49 60
Table 3.2402.2 GPS week: 2402 Day: 2 MJD: 61060
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 855 12 35 10 13 21 21 8 | 62 57 55 61 67 43 57
R03 | 3688 16 19 13 19 19 21 8 | 81 69 67 76 74 63 71
R04 | 1254 14 19 25 13 21 13 7 | 74 66 78 73 68 66 69
R05 | 1215 15 23 13 15 14 10 6 | 86 75 81 81 83 85 81
XR06 | 883 47 1036 1168 --- 65 --- 55 | 52 345 561 --- 100 --- 68
R07M | 1949 12 23 19 15 15 24 8 | 80 93 90 87 88 79 83
R08M | 1028 13 35 24 13 12 22 8 | 66 82 68 72 81 59 66
R09M | 777 19 60 19 16 21 15 11 | 85 84 86 78 75 82 79
R11M | 1806 9 36 21 10 8 14 7 | 30 45 34 30 33 44 32
R12M | 813 21 35 28 15 16 15 9 | 98 88 102 102 92 94 94
R14M | 2523 6 24 23 12 20 16 7 | 28 35 36 25 26 21 23
R15M | 1316 15 20 12 8 23 13 7 | 49 51 51 46 47 43 45
R16M | 2228 14 33 19 19 13 18 8 | 50 66 47 39 52 33 44
R17E | 1149 10 16 11 19 13 15 6 | 68 63 64 68 68 61 64
R18E | 960 10 28 15 11 21 16 7 | 27 33 26 34 34 29 26
XR19E | 1758 13 30 19 --- 18 --- 11 | 41 42 50 --- 37 --- 40
R20E | 723 22 74 347 30 35 33 44 | 69 69 174 72 74 76 68
R21E | 1194 11 43 18 28 18 15 10 | 70 73 61 89 72 69 71
R22E | 660 16 29 21 22 25 12 9 | 37 51 43 43 47 34 37
XR24E | 1078 16 27 14 23 16 --- 9 | 53 46 44 51 46 --- 45
XR28E |23028 345 --- --- --- 470 --- 403 | 111 --- --- --- 9999 --- 250
------+-----------------------------------------+-------------------------------------
RMS | 1617 15 36 86 17 19 18 |T 62 76 90 62 63 57 67
WRMS | 1617 14 30 17 15 19 18 |NE 71 122 168 72 78 64 69
MEDI | 1194 14 29 19 15 19 15 |MD 66 66 61 68 68 61 66
Table 3.2402.3 GPS week: 2402 Day: 3 MJD: 61061
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1234 14 27 26 14 16 20 8 | 79 71 56 79 81 58 71
R03 | 1313 10 22 13 12 18 26 7 | 85 73 83 86 91 64 80
R04 | 2103 14 18 32 11 22 20 8 | 83 72 100 77 65 62 75
R05 | 728 13 43 19 18 26 9 9 | 107 120 106 104 89 103 103
XR06 | 971 36 1036 1213 --- 79 --- 53 | 26 402 666 --- 87 --- 38
R07M | 2770 13 31 12 12 41 20 9 | 77 65 74 67 105 59 72
R08M | 1442 12 54 26 17 33 22 11 | 86 110 98 88 83 62 88
R09M | 991 14 53 13 9 18 9 8 | 208 204 216 201 211 209 206
R11M | 1673 9 50 24 10 24 26 10 | 56 72 58 60 59 43 53
R12M | 1141 26 50 13 18 27 8 10 | 180 202 188 185 189 195 187
R14M | 2518 5 21 17 6 19 16 5 | 58 59 61 59 59 61 58
R15M | 1669 17 19 14 8 22 21 7 | 32 32 25 29 12 13 21
R16M | 2935 19 22 14 11 28 20 8 | 45 31 38 30 40 24 31
R17E | 929 11 24 11 21 23 11 7 | 110 100 108 103 114 108 106
R18E | 866 9 29 17 17 16 13 7 | 27 30 28 23 31 18 21
XR19E | 2454 13 28 23 --- 27 --- 12 | 23 26 24 --- 28 --- 18
R20E | 1412 24 59 315 31 41 34 43 | 39 51 139 32 38 24 37
R21E | 1451 10 52 21 21 16 10 9 | 65 92 70 69 67 67 66
R22E | 1519 14 29 17 16 19 16 8 | 23 34 24 31 34 25 23
R24E | 888 12 26 20 28 29 18 10 | 42 56 54 57 40 39 47
XR28E |17417 280 --- --- --- 620 --- 417 | 821 --- --- --- 9999 --- 555
------+-----------------------------------------+-------------------------------------
RMS | 1660 15 37 76 17 25 19 |T 108 95 110 76 76 68 93
WRMS | 1660 15 32 19 14 26 19 |NE 76 147 202 86 82 71 73
MEDI | 1442 13 29 17 14 24 18 |MD 65 71 70 67 65 59 66
Table 3.2402.4 GPS week: 2402 Day: 4 MJD: 61062
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1693 24 25 31 9 14 12 9 | 70 63 37 60 58 45 53
R03 | 1258 11 16 9 14 12 15 5 | 83 76 71 84 83 66 76
R04 | 2543 15 17 13 19 25 15 7 | 85 72 82 84 56 67 74
R05 | 941 12 37 14 18 19 11 8 | 76 78 76 74 70 72 73
XR06 | 984 43 1011 1192 --- 67 --- 54 | 46 408 553 --- 80 --- 53
R07M | 2374 14 35 16 12 44 20 10 | 99 109 96 112 138 93 105
R08M | 1875 12 39 16 15 17 22 8 | 55 68 63 61 60 33 55
R09M | 1499 10 38 13 17 11 8 7 | 318 321 316 305 321 323 317
R11M | 2634 10 23 20 10 31 20 8 | 68 66 79 62 78 65 68
R12M | 983 17 15 16 16 13 16 7 | 280 271 274 274 275 276 276
R14M | 2636 8 25 12 13 15 8 6 | 102 89 101 98 94 106 100
R15M | 1399 21 24 16 12 12 18 7 | 46 43 42 38 39 39 39
R16M | 2401 10 29 9 9 20 15 6 | 64 70 61 64 53 60 60
R17E | 645 15 21 14 20 20 11 7 | 110 114 120 105 108 116 111
R18E | 992 9 36 15 17 13 11 7 | 22 40 25 24 23 21 21
XR19E | 1708 13 30 13 --- 26 12 9 | 31 36 30 --- 30 21 27
R20E | 2028 7 39 308 9 24 12 9 | 53 55 134 58 49 48 51
R21E | 1932 9 50 20 29 12 11 9 | 41 69 39 46 41 45 41
R22E | 1241 12 11 11 15 13 10 5 | 22 26 29 29 30 22 23
R24E | 1339 9 30 22 33 17 13 9 | 37 41 45 51 31 26 36
XR28E |16131 93 --- --- --- 143 --- 115 | 224 --- --- --- 9999 --- 173
------+-----------------------------------------+-------------------------------------
RMS | 1801 13 30 74 17 20 14 |T 92 105 113 90 85 81 87
WRMS | 1801 14 26 14 15 20 14 |NE 72 139 163 75 69 62 65
MEDI | 1693 12 29 15 15 17 12 |MD 68 69 71 62 58 60 60
Table 3.2402.5 GPS week: 2402 Day: 5 MJD: 61063
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1431 24 22 16 18 26 23 9 | 63 55 45 41 67 35 48
R03 | 2535 7 14 14 15 14 15 6 | 69 68 70 68 65 62 66
R04 | 1618 10 30 9 18 13 14 6 | 69 71 63 82 68 64 68
R05 | 1672 12 36 20 13 19 14 8 | 63 68 84 76 67 60 69
XR06 | 940 39 954 1106 --- 55 --- 46 | 33 327 429 --- 58 --- 42
R07M | 1413 12 22 16 12 22 13 7 | 94 94 83 95 99 83 90
R08M | 3763 11 39 21 14 21 14 8 | 73 83 64 71 73 51 69
R09M | 1052 20 45 7 10 19 16 8 | 355 371 358 361 351 358 357
R11M | 770 6 27 12 8 18 11 6 | 78 78 89 80 81 90 82
R12M | 986 16 30 15 16 13 16 7 | 342 346 345 344 351 342 344
R14M | 1852 15 23 9 18 18 12 7 | 124 127 127 125 125 119 124
R15M | 874 18 28 17 17 15 15 8 | 51 60 60 55 59 42 52
R16M | 1641 16 38 21 12 20 18 9 | 83 86 90 84 81 68 80
R17E | 934 15 19 13 15 24 13 7 | 206 208 210 195 208 207 205
R18E | 1163 7 29 10 17 22 13 7 | 20 30 19 27 21 21 18
XR19E | 1337 10 36 13 --- 21 20 9 | 40 26 47 --- 40 19 42
R20E | 2471 9 51 253 13 18 14 10 | 41 46 84 50 37 46 40
R21E | 2247 11 59 15 34 12 16 11 | 57 68 59 62 59 59 56
R22E | 1268 18 39 8 14 14 12 7 | 23 56 27 32 29 27 27
R24E | 1601 13 24 28 24 22 15 9 | 42 54 61 38 30 34 42
XR28E |12936 55 --- --- --- 78 --- 66 | 132 --- --- --- 9999 --- 110
------+-----------------------------------------+-------------------------------------
RMS | 1782 14 34 61 17 19 15 |T 98 116 120 104 98 94 96
WRMS | 1782 15 31 13 14 19 15 |NE 59 117 138 66 65 55 58
MEDI | 1431 13 30 15 15 19 14 |MD 69 68 70 71 67 60 68
Table 3.2402.6 GPS week: 2402 Day: 6 MJD: 61064
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1373 21 17 11 15 13 15 7 | 96 83 77 80 93 69 82
R03 | 3943 15 17 22 12 11 24 8 | 108 98 107 106 105 85 100
R04 | 1046 11 18 10 8 25 17 7 | 107 100 104 104 111 96 103
R05 | 1707 19 33 14 19 16 12 8 | 97 91 91 101 86 84 90
XR06 | 1017 50 943 1125 --- 58 --- 54 | 41 403 709 --- 81 --- 50
R07M | 1129 12 31 13 13 13 11 6 | 112 116 111 113 112 100 108
R08M | 4431 16 31 16 24 17 15 8 | 92 111 99 109 108 64 99
R09M | 1041 11 44 17 8 14 13 7 | 287 293 288 288 289 286 287
R11M | 1058 11 20 14 22 13 10 6 | 112 118 109 112 114 107 110
R12M | 594 16 30 21 19 14 6 7 | 361 361 363 361 361 364 361
R14M | 1259 9 34 20 16 18 14 8 | 97 99 95 94 99 93 95
R15M | 1140 16 31 18 10 10 20 7 | 40 54 43 39 42 25 37
R16M | 1090 13 42 14 12 13 15 7 | 49 69 56 54 47 49 50
R17E | 890 15 19 18 16 20 9 7 | 166 157 162 159 164 162 161
R18E | 1527 8 26 14 16 19 9 6 | 27 35 33 31 29 29 27
XR19E | 1281 12 23 12 --- 16 --- 9 | 66 54 73 --- 67 --- 66
R20E | 1785 13 28 294 13 23 17 9 | 71 60 139 71 67 75 69
R21E | 3242 9 55 15 21 20 17 10 | 65 64 64 65 68 70 64
R22E | 1263 15 35 19 18 21 11 8 | 40 58 41 48 46 36 40
R24E | 2714 14 15 22 23 14 17 8 | 35 39 46 47 39 34 37
XR28E |13879 55 --- --- --- 64 --- 59 | 150 --- --- --- 9999 --- 125
------+-----------------------------------------+-------------------------------------
RMS | 2038 14 31 71 16 17 15 |T 105 123 140 110 106 101 102
WRMS | 2038 14 30 17 15 17 15 |NE 89 155 217 97 95 83 85
MEDI | 1263 14 30 16 16 16 14 |MD 96 91 95 94 86 75 90
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