[IGSREPORT-30774] Wk 2401 IGLOS Final Orbits
acc
acc at igs.org
Thu Jan 29 05:55:57 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2401 (Jan 11, 2026 - Jan 17, 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 2.2401.
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:
igl2401[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2401 in the SP3 format.
igl24017.sum Combination Report for GPS Week 2401.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
Starting 02-Feb-2025 (GPS week 2352) the IGS Analysis Centers started using
the IGS realization of the updated ITRF2020-u2023, called IGb20. The combined
GLONASS orbits from this date are therefore in IGb20 frame.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 5.7 ns
1 | 5.8 ns
2 | 5.2 ns
3 | 4.5 ns
4 | 4.3 ns
5 | 4.7 ns
6 | 4.2 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 | COD | R28
0 | ESA | R06
0 | GFZ | R06 R20
1 | ESA | R06
1 | GFZ | R06 R20
2 | ESA | R06
2 | GFZ | R06 R20
3 | ESA | R06
3 | GFZ | R06 R20
4 | ESA | R06
4 | GFZ | R06 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 1.2401, 1a.2401).
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 2.2401.0-6)
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 3.2401.0-6).
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 2401 summary. (Jan 11, 2026 - Jan 17, 2026)
Table 1.2401.a GPS week : 2401 MJD: 61051.0-61057.0
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 -5 9 32 .12 15 16 | 13320 -350 3617 15082
| 1 1 0 17 11 15 .05 | 6398 808
esa n/a| -1 0 -2 -38 -4 32 -.16 28 25 | 2208 18 3654 10106
| 2 2 1 14 25 70 .11 | 449 876
gfz n/a| 0 0 0 11 24 7 -.14 94 17 | 0 -331 3840 9921
| 1 1 1 15 18 38 .06 | 0 973
grg n/a| 1 -1 -2 1 -43 -10 .38 16 15 | 4813 -114 3794 9541
| 0 1 2 12 13 42 .02 | 544 990
iac n/a| 0 0 -2 6 15 -15 -.10 15 14 | 14079 -441 3830 13888
| 0 0 1 20 20 74 .04 | 4345 603
jgx n/a| 0 0 4 11 -1 -19 -.15 17 17 | 5796 -124 3728 9890
| 1 1 2 19 16 36 .06 | 482 1085
Table 1.2401.b GPS week : 2401 MJD: 61051.0-61057.0
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 6 7 7 7 8 7 |
R03 | 8 7 8 7 7 9 8 |
R04 | 8 8 8 8 9 6 7 |
R05 | 8 7 8 9 8 8 6 |
R06 | 51 52 50 52 48 50 49 |
R07 | 9 8 8 8 8 8 8 |
R08 | 7 7 8 8 8 9 9 |
R09 | 8 10 8 6 8 8 9 |
R11 | 6 7 6 7 6 6 8 |
R12 | 8 6 7 7 8 9 8 |
R14 | 6 6 7 7 6 7 6 |
R15 | 6 8 9 8 7 9 7 |
R16 | 7 9 7 9 10 8 6 |
R17 | 7 9 6 6 6 6 7 |
R18 | 6 9 6 7 7 7 6 |
R19 | 9 10 11 9 10 10 9 |
R20 | 11 11 12 11 11 9 9 |
R21 | 8 7 9 8 9 9 8 |
R22 | 8 8 6 6 7 7 7 |
R24 | 9 6 11 9 9 9 8 |
R26 | 48 50 47 45 43 49 42 |
R28 | 62 71 39 45 36 48 45 |
Table 1.2401.c GPS week : 2401 MJD: 61051.0-61057.0
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 2401 0 | -19 -10 -82 553 -3815 1552 78.9 1746 1746 | 5659 0
brd 2401 1 | -63 -57 7 48 -38 7755 78.1 1632 1632 | 5759 0
brd 2401 2 | -122 14 -10 253 121 9111 79.4 1398 1398 | 5210 0
brd 2401 3 | -25 51 46 748 -287 12200 79.9 1883 1883 | 4458 0
brd 2401 4 | 5 -6 -55 1478 1042 5755 80.0 1894 1894 | 4315 0
brd 2401 5 | 65 -47 -17 236 1344 7513 78.0 1710 1710 | 4721 0
brd 2401 6 | 69 -12 -73 -511 394 7138 80.7 1747 1747 | 4205 0
-------------+------------------------------------------------------------+----------------
brd 2401 mean| -12 -9 -26 400 -176 7289 79.3 1715 1715 | 4903 0
brd 2401 sdev| 68 36 46 620 1706 3240 1.0 168 168 | 640 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 2.2401.0 GPS week: 2401 Day: 0 MJD: 61051
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 -7 0 32 .21 15 16 | 22795 -46 3117 22230
esa n/a| -4 0 -3 -26 -27 90 -.37 24 22 | 2030 -1012 3164 9081
gfz n/a| 0 3 1 4 11 36 -.12 92 18 | 0 267 3416 9294
grg n/a| 3 -2 -2 -22 -25 -89 .35 17 17 | 5730 620 3633 9330
iac n/a| 0 0 0 14 5 18 -.12 14 14 | 20059 687 3484 17303
jgx n/a| 1 -1 4 20 0 -53 -.08 18 18 | 5770 -382 3234 9297
Table 2.2401.1 GPS week: 2401 Day: 1 MJD: 61052
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 -12 32 45 .09 14 15 | 9382 353 3437 11186
esa n/a| 0 -1 -2 -35 -6 52 -.16 27 27 | 2086 -48 3472 9288
gfz n/a| -1 0 1 0 9 -18 -.05 95 27 | 0 744 3693 9548
grg n/a| 2 0 0 14 -53 -19 .37 16 14 | 5382 148 3580 9311
iac n/a| 0 1 -3 -5 35 -60 -.12 17 15 | 13112 -1182 3812 12181
jgx n/a| 0 0 4 26 -22 7 -.18 15 15 | 6190 -52 3571 9684
Table 2.2401.2 GPS week: 2401 Day: 2 MJD: 61053
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| -3 -3 0 33 17 41 .15 17 18 | 15514 909 4048 15509
esa n/a| -3 0 0 -36 23 90 -.13 29 26 | 2294 1344 4073 9916
gfz n/a| 1 0 -1 30 19 -19 -.15 96 16 | 0 854 4226 9663
grg n/a| 0 0 -2 1 -59 25 .37 13 13 | 4321 1386 4111 9368
iac n/a| 0 1 -3 -29 21 -45 -.15 14 13 | 14709 -197 4150 13337
jgx n/a| 0 0 8 39 -2 -29 -.26 17 17 | 5652 2004 4151 9877
Table 2.2401.3 GPS week: 2401 Day: 3 MJD: 61054
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 -17 2 48 .09 14 16 | 17334 -915 3623 16369
esa n/a| 2 4 -1 -30 19 -90 -.01 32 29 | 1338 -2 3661 9251
gfz n/a| 1 -2 1 -3 18 -27 -.20 96 17 | 0 -995 3852 8709
grg n/a| 1 0 -6 4 -29 -27 .39 16 14 | 4606 -949 3768 8001
iac n/a| 0 0 0 30 -6 103 -.09 15 15 | 17962 -878 3919 15640
jgx n/a| 0 0 2 17 -7 -76 -.15 16 15 | 6634 -1064 3678 8086
Table 2.2401.4 GPS week: 2401 Day: 4 MJD: 61055
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 -9 5 29 .13 13 14 | 14167 -1323 3826 15427
esa n/a| 0 -1 -5 -52 15 74 -.22 32 28 | 2546 -1132 3871 10897
gfz n/a| 0 0 0 28 60 74 -.13 89 14 | 0 -1575 4034 10347
grg n/a| 1 -2 -1 2 -40 -17 .40 17 15 | 4835 -1525 3992 9977
iac n/a| 0 0 -1 2 11 -115 -.04 14 13 | 12289 -386 3973 13016
jgx n/a| 0 0 3 0 -16 30 -.17 18 18 | 5482 -1355 3977 10429
Table 2.2401.5 GPS week: 2401 Day: 5 MJD: 61056
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 1 -9 2 20 .10 14 15 | 11464 -388 3506 14998
esa n/a| -2 -2 -2 -23 -45 -42 -.18 27 23 | 2539 379 3540 13129
gfz n/a| 1 -1 0 21 15 -20 -.08 93 15 | 0 -402 3687 12369
grg n/a| 1 -1 0 -3 -57 36 .40 19 15 | 4401 150 3587 11882
iac n/a| 0 1 -3 10 47 45 -.08 16 16 | 13955 -767 3672 14894
jgx n/a| 0 1 3 -14 10 -14 -.12 17 17 | 5691 139 3576 12290
Table 2.2401.6 GPS week: 2401 Day: 6 MJD: 61057
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 -16 6 6 .07 15 16 | 2584 -1044 3768 9857
esa n/a| -1 3 -2 -63 -13 54 -.10 26 22 | 2628 599 3800 9184
gfz n/a| 0 1 0 -4 38 24 -.21 96 15 | 0 -1214 3975 9521
grg n/a| 1 -1 -1 11 -39 15 .35 15 15 | 4417 -630 3892 8920
iac n/a| 0 0 -3 26 -7 -55 -.09 14 13 | 6470 -369 3801 10845
jgx n/a| 0 0 6 -9 25 -3 -.08 17 17 | 5155 -164 3913 9571
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 3.2401.0 GPS week: 2401 Day: 0 MJD: 61051
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1320 17 22 16 20 13 19 8 | 143 142 135 135 139 132 137
R03 | 2296 17 19 22 18 11 21 8 | 86 72 73 75 68 58 71
R04 | 791 14 15 10 22 13 23 7 | 87 79 81 84 71 73 77
R05 | 2530 15 35 14 13 14 20 8 | 98 93 99 97 100 88 95
XR06 | 915 54 980 1260 --- 46 --- 50 | 54 549 516 --- 68 --- 58
R07 | 2233 12 17 22 16 18 24 8 | 84 75 86 82 66 59 74
R08 | 714 13 23 9 17 17 16 7 | 104 100 105 111 95 91 100
R09 | 932 16 40 12 11 13 15 8 | 38 45 40 39 35 41 38
R11 | 3048 8 22 13 9 17 9 6 | 25 34 27 29 28 26 24
R12 | 747 20 15 20 21 11 19 8 | 29 31 29 16 28 16 21
R14 | 2443 10 19 10 12 14 14 6 | 40 44 42 34 41 37 37
R15 | 845 24 14 13 8 9 8 6 | 51 45 43 44 43 40 43
R16 | 1380 18 16 13 13 14 19 7 | 60 68 60 59 61 47 57
R17E | 975 9 15 14 23 15 16 7 | 49 45 51 46 51 42 46
R18E | 706 12 19 13 16 9 16 6 | 27 31 34 37 29 20 28
XR19E | 1977 12 26 12 --- 11 --- 8 | 50 44 47 --- 52 --- 47
R20E | 669 12 39 388 16 23 16 11 | 37 37 137 33 40 39 34
R21E | 784 11 29 16 14 12 18 7 | 29 34 35 36 34 28 30
R22E | 937 18 24 16 21 12 20 8 | 29 44 35 43 33 27 32
R24E | 3551 14 22 16 22 19 27 9 | 48 45 54 46 44 33 43
XR26 | 6047 51 --- --- --- 44 --- 48 | 63 --- --- --- 82 --- 71
XR28E | 8861 166 --- --- 70 54 --- 62 | 43 --- --- 30 112 --- 115
------+-----------------------------------------+-------------------------------------
RMS | 1745 15 24 92 17 14 18 |T 57 82 86 56 60 49 58
WRMS | 1745 16 22 18 17 14 18 |NE 68 105 102 67 66 59 64
MEDI | 975 14 22 14 16 14 18 |MD 49 45 51 44 51 40 46
Table 3.2401.1 GPS week: 2401 Day: 1 MJD: 61052
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1261 14 18 9 15 13 15 6 | 112 114 109 111 110 113 111
R03 | 2270 19 20 11 18 12 15 7 | 56 52 45 52 44 42 46
R04 | 601 17 18 21 17 13 18 8 | 61 52 48 53 43 48 49
R05 | 1389 14 24 14 15 18 12 7 | 58 62 57 57 40 50 52
XR06 | 1470 48 1062 1215 --- 54 --- 51 | 51 373 321 --- 64 --- 54
R07 | 1545 16 21 15 16 11 24 8 | 57 56 55 59 46 36 50
R08 | 1359 14 16 12 21 8 20 7 | 72 66 57 78 62 60 65
R09 | 1077 14 54 13 10 20 10 9 | 33 40 35 33 32 38 32
R11 | 3452 8 30 15 7 14 15 6 | 21 34 13 23 20 28 19
R12 | 825 8 24 10 13 10 9 5 | 21 37 16 27 21 27 20
R14 | 966 6 19 17 12 10 8 5 | 30 29 45 31 40 31 33
R15 | 1137 27 16 12 15 11 14 7 | 36 39 34 29 34 25 29
R16 | 2019 18 43 14 11 18 18 9 | 41 61 47 38 45 34 41
R17E | 884 11 18 13 21 28 17 8 | 55 48 55 59 46 42 49
R18E | 757 12 23 21 23 18 21 9 | 28 32 39 35 34 17 27
XR19E | 1857 11 23 14 --- 18 --- 9 | 43 37 46 --- 49 --- 43
R20E | 840 8 42 401 10 30 18 11 | 39 39 145 36 46 35 36
R21E | 1737 10 31 18 15 14 9 7 | 30 36 32 32 34 23 28
R22E | 1621 16 21 15 20 19 12 7 | 26 34 27 36 28 26 26
R24E | 2625 10 14 13 19 14 13 6 | 49 48 46 48 42 35 44
XR26 | 5066 46 --- --- --- 52 --- 49 | 52 --- --- --- 59 --- 53
XR28E | 9496 68 --- --- --- 74 --- 71 | 77 --- --- --- 99 --- 78
------+-----------------------------------------+-------------------------------------
RMS | 1632 14 27 95 16 17 15 |T 47 64 63 46 47 39 44
WRMS | 1632 15 27 27 14 15 15 |NE 50 78 67 49 47 44 46
MEDI | 1389 14 21 14 15 14 15 |MD 43 40 46 36 43 35 43
Table 3.2401.2 GPS week: 2401 Day: 2 MJD: 61053
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 674 17 20 10 11 9 20 6 | 132 123 125 129 122 115 124
R03 | 1426 22 21 19 11 17 15 7 | 67 55 64 56 41 48 53
R04 | 719 23 28 17 17 13 17 8 | 72 59 61 54 54 52 56
R05 | 932 22 33 16 15 14 16 8 | 73 65 62 65 54 57 60
XR06 | 4238 61 1087 1259 --- 40 --- 49 | 44 440 505 --- 57 --- 48
R07 | 1105 17 33 16 15 11 20 8 | 67 64 66 55 64 47 59
R08 | 1261 15 21 23 14 13 25 8 | 112 118 114 111 107 102 109
R09 | 1084 15 45 13 10 13 15 8 | 34 40 38 43 30 38 34
R11 | 3374 10 34 10 9 12 10 6 | 28 42 27 33 29 22 26
R12 | 590 15 20 13 18 15 9 6 | 26 25 17 16 31 20 19
R14 | 1445 12 22 13 11 12 20 6 | 38 39 34 39 28 22 31
R15 | 648 27 18 21 8 14 30 9 | 41 28 47 25 38 20 29
R16 | 1850 21 17 16 8 13 15 6 | 44 39 45 32 31 25 33
R17E | 898 9 21 16 14 10 15 6 | 43 36 41 46 34 31 37
R18E | 1154 10 23 13 11 11 12 5 | 33 36 31 39 32 28 31
XR19E | 1961 17 26 19 --- 14 --- 10 | 31 41 47 --- 38 --- 38
R20E | 826 11 46 391 14 27 20 12 | 30 44 166 37 36 34 32
R21E | 1235 18 46 16 17 9 10 8 | 32 51 39 39 30 32 33
R22E | 1833 16 23 14 14 7 12 6 | 23 33 24 34 27 24 25
XR24E | 2579 19 32 18 22 17 --- 10 | 42 45 46 49 33 --- 39
XR26 | 4922 58 --- --- --- 38 --- 47 | 48 --- --- --- 73 --- 64
XR28E |17084 48 --- --- --- 30 --- 38 | 47 --- --- --- 66 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 1398 17 29 96 13 14 17 |T 50 71 79 50 47 42 46
WRMS | 1398 18 26 16 13 13 17 |NE 59 87 92 54 54 47 53
MEDI | 1235 17 23 16 14 13 15 |MD 42 42 46 39 36 32 37
Table 3.2401.3 GPS week: 2401 Day: 3 MJD: 61054
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 970 22 19 10 13 15 16 7 | 88 80 71 83 71 64 75
R03 | 2402 19 19 9 12 11 21 7 | 74 62 61 64 57 45 60
R04 | 911 15 24 15 18 14 22 8 | 71 63 72 74 54 51 62
R05 | 1049 14 39 23 19 16 17 9 | 70 77 78 63 52 55 63
XR06 | 1789 54 1083 1294 --- 50 --- 52 | 37 521 534 --- 53 --- 45
R07 | 1080 11 37 12 15 13 17 7 | 72 83 71 72 65 53 66
R08 | 946 14 26 15 15 11 25 8 | 99 101 93 92 79 88 90
R09 | 740 15 31 8 11 9 9 6 | 24 42 28 32 18 27 24
R11 | 5378 11 38 15 10 13 10 7 | 26 27 28 33 30 30 26
R12 | 635 8 25 18 22 10 10 7 | 29 33 40 19 32 31 28
R14 | 1467 16 29 12 12 16 10 6 | 40 48 30 29 24 37 31
R15 | 554 19 23 17 15 13 15 7 | 43 38 40 44 31 27 34
R16 | 1914 21 44 16 11 19 21 9 | 52 65 58 50 38 35 46
R17E | 1250 9 19 12 21 11 11 6 | 37 40 43 46 36 34 37
R18E | 1055 12 29 10 17 13 13 6 | 28 45 28 38 25 28 27
XR19E | 1907 15 25 18 --- 16 18 8 | 20 35 33 --- 27 11 23
R20E | 951 10 47 405 10 27 19 11 | 51 67 190 50 54 47 50
R21E | 1171 10 51 15 15 11 9 8 | 32 45 37 35 29 27 29
R22E | 1306 11 17 11 17 14 10 6 | 22 31 28 38 25 26 25
R24E | 3229 11 29 16 29 20 11 8 | 41 42 45 53 38 36 38
XR26 | 7538 47 --- --- --- 43 --- 45 | 36 --- --- --- 64 --- 49
XR28E |17866 46 --- --- --- 44 --- 45 | 57 --- --- --- 61 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 1882 14 32 96 16 15 16 |T 47 77 80 50 43 39 44
WRMS | 1882 16 29 17 14 15 15 |NE 54 95 92 54 47 45 49
MEDI | 1171 14 29 15 15 14 15 |MD 40 45 43 46 38 35 38
Table 3.2401.4 GPS week: 2401 Day: 4 MJD: 61055
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1228 18 22 13 9 14 20 7 | 138 125 135 128 122 128 129
R03 | 2858 16 21 12 9 12 25 7 | 60 51 53 52 52 34 50
R04 | 942 14 14 11 29 12 27 8 | 63 49 48 79 47 42 54
R05 | 2412 8 29 20 20 11 26 8 | 56 51 73 71 50 39 56
XR06 | 902 50 999 1162 --- 45 --- 47 | 41 422 406 --- 52 --- 45
R07 | 1588 15 30 12 17 11 20 7 | 59 61 57 61 47 40 52
R08 | 1286 14 21 18 22 16 20 8 | 77 74 79 91 75 76 77
R09 | 1474 14 46 12 8 12 13 7 | 33 29 32 31 41 33 32
R11 | 4632 13 35 8 5 9 8 5 | 27 29 25 29 27 23 24
R12 | 583 16 26 17 19 9 23 8 | 30 39 35 17 26 18 24
R14 | 1057 10 28 10 12 9 8 5 | 35 43 33 32 31 34 32
R15 | 510 16 17 13 16 17 8 6 | 37 40 35 43 24 40 34
R16 | 1270 19 32 27 18 14 29 10 | 48 64 67 55 47 35 49
R17E | 3046 10 20 10 19 9 10 5 | 46 45 45 50 44 38 43
R18E | 1204 11 28 17 11 14 12 6 | 33 45 38 38 34 30 32
XR19E | 1584 16 30 14 --- 14 --- 10 | 27 30 37 --- 32 --- 28
R20E | 773 9 53 373 11 23 16 11 | 36 48 147 36 43 35 35
R21E | 879 9 57 14 16 13 15 9 | 37 55 39 41 36 28 34
R22E | 772 11 24 13 15 15 15 6 | 22 35 25 36 30 24 24
R24E | 2079 12 33 25 23 16 14 9 | 44 62 53 48 45 39 43
XR26 |12240 45 --- --- --- 40 --- 42 | 64 --- --- --- 80 --- 72
XR28E |18145 39 --- --- --- 33 --- 36 | 58 --- --- --- 61 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 1893 13 32 89 17 14 18 |T 48 69 73 52 47 40 46
WRMS | 1893 14 27 14 15 13 18 |NE 54 82 82 57 51 45 52
MEDI | 1270 14 28 13 16 14 15 |MD 41 48 45 43 44 35 43
Table 3.2401.5 GPS week: 2401 Day: 5 MJD: 61056
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1858 26 14 12 10 13 21 8 | 91 75 87 82 84 72 82
R03 | 2366 16 14 16 15 26 28 9 | 61 49 60 56 62 37 52
R04 | 809 10 15 13 14 9 19 6 | 57 52 62 63 56 46 56
R05 | 2392 15 29 9 22 13 18 7 | 60 59 58 72 59 50 57
XR06 | 1027 47 991 1184 --- 53 --- 50 | 25 311 426 --- 46 --- 30
R07 | 2300 12 22 10 24 14 20 7 | 59 59 51 66 51 41 52
R08 | 2220 16 17 17 25 20 20 8 | 94 94 92 101 80 83 89
R09 | 1319 9 42 10 15 14 11 7 | 25 35 26 34 23 33 25
R11 | 1976 11 28 10 14 10 10 6 | 31 47 33 29 32 35 31
R12 | 694 23 30 18 15 11 21 8 | 26 31 22 18 24 19 18
R14 | 806 10 25 12 13 13 17 6 | 33 38 33 25 30 17 27
R15 | 614 23 20 22 14 20 8 8 | 29 34 26 24 27 28 24
R16 | 1410 15 31 16 21 19 8 8 | 39 56 44 41 38 42 40
R17E | 3243 8 19 12 14 12 13 5 | 42 41 38 48 40 35 39
R18E | 649 8 28 12 18 14 10 6 | 29 35 29 37 33 25 28
XR19E | 1669 13 22 12 --- 21 --- 9 | 40 31 41 --- 44 --- 38
R20E | 889 8 33 392 11 18 17 8 | 59 63 168 56 59 51 55
R21E | 911 9 42 14 19 11 19 8 | 36 37 37 40 32 31 31
R22E | 921 11 23 14 19 19 10 7 | 26 41 26 46 30 27 28
R24E | 2100 12 22 12 33 19 13 8 | 51 55 45 68 41 39 47
XR26 |13561 46 --- --- --- 52 --- 49 | 42 --- --- --- 74 --- 56
XR28E |15952 44 --- --- --- 51 --- 48 | 44 --- --- --- 60 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1709 14 27 93 19 16 17 |T 45 62 70 50 46 39 43
WRMS | 1709 15 23 15 15 16 17 |NE 48 72 78 50 49 41 45
MEDI | 1410 12 23 12 15 14 17 |MD 40 47 41 46 41 35 39
Table 3.2401.6 GPS week: 2401 Day: 6 MJD: 61057
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2187 24 15 11 13 8 19 7 | 108 97 98 100 97 89 97
R03 | 4320 18 11 15 21 16 19 7 | 73 60 56 59 74 47 61
R04 | 645 15 20 15 15 10 17 6 | 76 69 72 72 67 58 68
R05 | 1099 10 26 14 11 8 16 6 | 73 76 73 67 69 64 69
XR06 | 1021 53 1049 1218 --- 45 --- 49 | 39 474 651 --- 68 --- 51
R07 | 2124 17 27 11 15 13 26 8 | 79 76 74 76 67 49 69
R08 | 2433 10 17 16 18 26 23 8 | 102 101 107 107 93 89 98
R09 | 1360 16 53 10 8 13 11 9 | 35 51 38 33 33 36 34
R11 | 2212 9 23 15 18 20 16 7 | 38 40 37 34 47 30 35
R12 | 623 24 21 12 22 14 9 8 | 39 35 28 22 31 22 26
R14 | 1016 10 17 12 13 9 15 5 | 49 52 43 39 42 33 41
R15 | 685 15 18 11 14 12 19 6 | 50 42 39 43 45 32 40
R16 | 1530 15 19 20 11 4 10 6 | 58 62 54 57 55 54 54
R17E | 1491 9 16 11 21 17 16 7 | 63 58 62 74 57 51 60
R18E | 799 8 23 16 12 13 11 6 | 40 46 34 47 45 34 39
XR19E | 1179 16 25 14 --- 11 --- 9 | 66 69 70 --- 72 --- 68
R20E | 990 9 33 394 12 17 18 9 | 64 75 180 59 65 62 63
R21E | 884 13 35 18 12 8 18 7 | 38 57 43 41 41 35 39
R22E | 867 10 31 12 14 16 14 7 | 40 42 41 49 47 39 41
XR24E | 2892 11 20 11 22 10 --- 7 | 55 52 52 68 50 --- 54
XR26 |13188 45 --- --- --- 39 --- 42 | 59 --- --- --- 87 --- 72
XR28E |16571 50 --- --- --- 39 --- 44 | 95 --- --- --- 75 --- 80
------+-----------------------------------------+-------------------------------------
RMS | 1746 15 26 96 15 14 17 |T 60 81 92 58 60 48 57
WRMS | 1746 16 22 15 15 13 17 |NE 62 95 105 59 62 50 58
MEDI | 1179 15 21 14 14 13 16 |MD 58 58 54 57 57 47 54
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