[IGSREPORT-30764] Wk 2400 IGLOS Final Orbits
acc
acc at igs.org
Thu Jan 22 03:26:36 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2400 (Jan 04, 2026 - Jan 10, 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 2.2400.
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:
igl2400[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2400 in the SP3 format.
igl24007.sum Combination Report for GPS Week 2400.
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 | 5.5 ns
1 | 6.7 ns
2 | 7.1 ns
3 | 7.4 ns
4 | 4.4 ns
5 | 4.6 ns
6 | 3.8 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 | R11
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 1.2400, 1a.2400).
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 2.2400.0-6)
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 3.2400.0-6).
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 2400 summary. (Jan 04, 2026 - Jan 10, 2026)
Table 1.2400.a GPS week : 2400 MJD: 61044.0-61050.0
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 3 6 -2 31 .24 17 17 | 2695 -1590 4136 15286
| 1 0 3 22 33 37 .06 | 3499 1791
esa n/a| -2 0 -4 -35 -11 66 -.27 28 27 | 1246 -2055 4046 14429
| 1 2 0 10 27 42 .11 | 629 1777
gfz n/a| 0 0 0 23 59 -29 .04 95 25 | 0 -1599 4212 13856
| 1 1 2 31 137 151 .15 | 0 1769
grg n/a| 2 0 0 -15 -57 4 .29 29 19 | 5852 -810 3352 10142
| 1 1 5 17 35 52 .13 | 1519 1366
iac n/a| 0 0 -1 26 10 -7 -.17 20 21 | 8655 -2205 4241 15848
| 1 1 1 14 36 51 .19 | 3081 1374
jgx n/a| 0 0 2 -13 -10 -24 -.21 16 16 | 4242 -538 3210 10449
| 1 1 2 19 22 33 .06 | 1290 1424
Table 1.2400.b GPS week : 2400 MJD: 61044.0-61050.0
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 | 6 8 13 9 7 7 11 |
R03 | 6 8 14 10 8 9 12 |
R04 | 7 7 14 11 8 8 8 |
R05 | 5 8 8 9 9 9 12 |
R06 | 51 50 43 51 47 46 44 |
R07 | 8 7 13 12 9 8 13 |
R08 | 7 8 15 9 9 10 15 |
R09 | 7 7 6 7 8 7 9 |
R11 | --- 8 8 7 10 7 7 |
R12 | 7 9 7 10 8 10 9 |
R14 | 6 7 9 7 8 8 6 |
R15 | 7 7 8 9 10 10 10 |
R16 | 11 10 8 7 13 8 9 |
R17 | 7 7 9 13 16 6 11 |
R18 | 8 7 8 7 10 14 7 |
R19 | 10 11 9 11 9 9 11 |
R20 | 14 14 16 14 12 14 16 |
R21 | 8 10 11 12 10 12 10 |
R22 | 7 7 6 7 7 12 6 |
R24 | 8 11 12 13 7 7 9 |
R26 | 29 31 30 29 46 47 42 |
R28 | 0 49 56 43 48 49 61 |
Table 1.2400.c GPS week : 2400 MJD: 61044.0-61050.0
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 2400 0 | -19 93 167 3620 3824 6493 77.4 1598 1598 | 5546 0
brd 2400 1 | -101 -1 -28 625 2675 4886 79.5 1691 1691 | 6651 0
brd 2400 2 | -42 -29 -43 -700 119 12610 82.2 1575 1575 | 7112 0
brd 2400 3 | 116 11 -140 -447 1385 5456 78.4 1774 1774 | 7374 0
brd 2400 4 | 41 -29 -127 811 -1168 -2416 78.6 1895 1895 | 4370 0
brd 2400 5 | 46 20 -63 732 1031 -3018 78.6 2080 2080 | 4616 0
brd 2400 6 | -59 -86 -38 289 -3373 -1531 80.8 2065 2065 | 3809 0
-------------+------------------------------------------------------------+----------------
brd 2400 mean| -2 -3 -39 704 641 3211 79.4 1811 1811 | 5639 0
brd 2400 sdev| 74 55 101 1413 2402 5772 1.6 208 208 | 1427 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 2.2400.0 GPS week: 2400 Day: 0 MJD: 61044
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 5 -3 -55 105 .22 18 19 | -1116 -3997 4441 19909
esa n/a| -3 0 -5 -35 -49 145 -.20 25 25 | 495 -3930 4483 19620
gfz n/a| -3 0 -2 57 367 -365 .09 106 16 | 0 -3579 4547 18884
grg n/a| 3 -1 0 7 -121 99 .39 15 14 | 6117 -1665 2835 10747
iac n/a| 0 -1 -1 7 -47 44 -.41 17 16 | 4819 -3807 4446 19373
jgx n/a| 0 0 1 -18 -51 43 -.19 14 14 | 3989 -1725 2741 10773
Table 2.2400.1 GPS week: 2400 Day: 1 MJD: 61045
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 7 41 8 43 .29 20 19 | 1338 -477 4357 14080
esa n/a| -3 -2 -5 -45 10 39 -.38 29 29 | 2460 -302 4370 14103
gfz n/a| 0 1 0 52 -11 65 -.02 111 18 | 0 -278 4511 13336
grg n/a| 2 0 0 -5 -45 -49 .34 14 13 | 6483 -141 3493 10825
iac n/a| 0 -3 -3 12 6 10 -.32 20 18 | 8404 -852 4331 15035
jgx n/a| -2 0 1 -54 12 -50 -.20 14 14 | 4627 1062 3070 11020
Table 2.2400.2 GPS week: 2400 Day: 2 MJD: 61046
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 5 26 -3 -2 .29 17 17 | 785 -3848 5187 21538
esa n/a| 0 0 -4 -19 17 66 -.11 27 27 | 784 -4060 5213 21441
gfz n/a| 0 1 0 -24 -13 54 -.04 22 21 | 0 -3575 5310 20520
grg n/a| 0 0 -3 -33 -29 -25 .21 49 21 | 7712 -1755 3340 10207
iac n/a| 2 -1 0 43 -1 20 -.07 25 32 | 7277 -3747 5124 21426
jgx n/a| 0 0 0 -8 10 -24 -.21 13 13 | 6530 -2046 3248 10966
Table 2.2400.3 GPS week: 2400 Day: 3 MJD: 61047
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 1 -2 17 .21 16 15 | 1338 -1563 4289 16029
esa n/a| -1 0 -4 -36 -5 91 -.16 26 28 | 1203 -2443 4303 15740
gfz n/a| 0 0 3 18 11 3 .00 100 19 | 0 -2029 4479 15094
grg n/a| 1 0 9 -29 -56 17 .05 42 25 | 7314 -195 3375 10043
iac n/a| 0 0 -1 45 21 -23 .11 26 26 | 7617 -1817 4764 16701
jgx n/a| 2 -1 -2 -3 -16 -40 -.27 17 17 | 4775 226 3318 10341
Table 2.2400.4 GPS week: 2400 Day: 4 MJD: 61048
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 3 -28 -16 46 .29 16 16 | 5567 971 3778 11331
esa n/a| 0 -5 -4 -23 -42 10 -.39 30 27 | 1335 717 2987 9689
gfz n/a| -1 2 0 48 -4 30 .01 102 27 | 0 1309 3223 9727
grg n/a| 3 1 6 -37 -56 26 .28 34 24 | 3376 1759 3014 9251
iac n/a| 0 0 -3 31 74 -90 .01 20 19 | 11079 -289 3932 13290
jgx n/a| 2 -1 4 -10 -3 -58 -.29 20 20 | 2398 1405 2986 9495
Table 2.2400.5 GPS week: 2400 Day: 5 MJD: 61049
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 3 14 -3 14 .22 15 15 | 9213 -1339 3589 12413
esa n/a| -2 1 -2 -42 -19 50 -.29 27 24 | 1463 -2670 3617 9151
gfz n/a| 0 0 0 -7 48 31 -.10 101 20 | 0 -2050 3821 9328
grg n/a| 2 -3 -4 1 -80 9 .38 32 22 | 5239 -1707 3731 8815
iac n/a| -1 0 -1 27 21 -57 -.20 19 19 | 14233 -1914 3579 12971
jgx n/a| 0 1 5 -7 -25 -13 -.09 17 17 | 3334 -1715 3656 8979
Table 2.2400.6 GPS week: 2400 Day: 6 MJD: 61050
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 -4 59 -1 .15 16 16 | 1741 -877 3313 11702
esa n/a| -4 0 -4 -46 12 64 -.34 29 26 | 983 -1698 3351 11263
gfz n/a| 0 -3 6 18 15 -24 .35 123 54 | 0 -997 3593 10106
grg n/a| 1 -2 -5 -12 -10 -49 .42 17 14 | 4723 -1971 3681 11110
iac n/a| 0 1 1 17 1 45 -.29 16 16 | 7159 -3015 3512 12145
jgx n/a| -1 1 5 9 1 -29 -.22 17 17 | 4042 -975 3456 11570
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 3.2400.0 GPS week: 2400 Day: 0 MJD: 61044
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1134 9 18 12 9 11 --- 5 | 78 78 86 78 78 --- 78
R03E | 1890 13 15 13 14 9 12 5 | 62 53 64 65 58 53 57
R04E | 1915 11 22 17 16 10 11 6 | 74 71 74 81 76 71 72
R05E | 3076 9 18 13 10 10 8 5 | 89 89 91 90 94 86 88
XR06E | 1333 55 998 997 --- 46 --- 50 | 45 506 327 --- 54 --- 52
R07E | 1332 22 26 18 15 11 14 7 | 108 102 108 109 107 102 104
R08E | 824 15 18 14 16 17 16 7 | 77 76 90 83 78 77 77
R09 | 884 13 33 14 14 14 11 7 | 41 43 61 42 46 39 42
R12 | 1334 19 26 17 7 21 8 7 | 40 38 39 37 42 41 34
R14 | 1635 8 25 18 13 14 7 6 | 46 52 62 46 52 51 49
R15 | 776 22 21 12 11 14 4 6 | 41 45 50 37 43 42 39
R16 | 1718 37 26 33 6 19 20 11 | 52 57 80 52 58 48 53
R17E | 1411 20 18 13 17 13 16 7 | 38 36 53 42 33 29 33
R18E | 669 13 30 12 20 17 17 8 | 76 86 78 86 82 66 76
XR19E | 2794 15 24 18 --- 15 --- 10 | 50 57 60 --- 55 --- 53
R20E | 2051 12 37 420 26 37 19 13 | 28 42 140 20 52 27 29
R21E | 898 18 30 13 11 13 17 7 | 91 63 93 86 84 69 80
R22E | 575 19 24 10 12 17 11 6 | 60 67 61 64 55 58 58
R24E | 2257 22 17 15 16 18 16 8 | 138 141 144 141 138 141 139
XR26E | 5721 39 57 50 --- 55 --- 29 | 113 36 72 --- 112 --- 122
XR28 |21778 7 --- --- --- --- --- 0 | 102 --- --- --- --- --- 93
------+-----------------------------------------+-------------------------------------
RMS | 1597 18 25 106 15 17 14 |T 67 86 89 66 68 62 66
WRMS | 1597 19 25 16 14 16 14 |NE 51 47 56 42 46 44 49
MEDI | 1411 15 24 14 14 14 12 |MD 60 57 74 64 58 53 57
Table 3.2400.1 GPS week: 2400 Day: 1 MJD: 61045
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1293 13 21 15 11 17 --- 7 | 74 70 70 74 73 --- 71
R03E | 1921 24 17 14 18 18 14 7 | 46 50 55 55 50 42 48
R04E | 1372 10 26 11 12 15 16 6 | 87 90 87 85 84 78 83
R05E | 1884 12 32 13 18 16 12 7 | 76 79 78 85 77 74 77
XR06E | 1450 54 1040 1113 --- 45 --- 49 | 48 349 313 --- 53 --- 48
R07E | 1662 19 20 15 13 9 14 6 | 126 124 140 127 128 124 128
R08E | 1141 16 24 17 16 16 14 7 | 83 81 85 84 84 82 82
R09 | 765 19 34 9 7 16 14 7 | 27 32 35 26 39 28 28
XR11 | 5935 12 18 21 15 15 --- 8 | 17 39 18 29 23 --- 18
R12 | 1269 29 26 19 8 28 10 9 | 19 37 19 18 37 20 17
R14 | 2405 8 25 17 11 11 14 6 | 23 33 27 30 34 36 27
R15 | 671 24 29 12 13 10 10 7 | 23 45 33 32 43 37 32
R16 | 1500 32 32 26 11 23 8 9 | 32 55 56 47 36 49 43
R17E | 1854 18 19 17 15 11 11 6 | 39 46 40 42 31 41 37
R18E | 878 10 29 13 17 15 12 7 | 51 62 51 60 56 49 52
XR19E | 2692 17 28 15 --- 16 --- 10 | 33 48 35 --- 43 --- 36
R20E | 1810 19 41 440 13 45 21 14 | 29 46 153 37 55 29 34
R21E | 1378 15 48 17 14 14 20 9 | 59 46 59 69 57 46 55
R22E | 794 18 25 12 14 13 10 6 | 44 51 37 57 40 44 43
R24E | 3439 23 25 24 24 27 21 10 | 158 163 156 160 155 203 155
XR26E |10399 33 55 54 --- 64 --- 31 | 100 41 51 --- 89 --- 97
XR28 |19849 54 --- --- --- 45 --- 49 | 72 --- --- --- 104 --- 75
------+-----------------------------------------+-------------------------------------
RMS | 1690 20 29 111 14 20 14 |T 57 75 76 62 63 61 58
WRMS | 1690 19 29 18 13 18 14 |NE 30 40 31 30 45 34 34
MEDI | 1500 18 26 17 13 16 14 |MD 46 50 55 55 53 44 48
Table 3.2400.2 GPS week: 2400 Day: 2 MJD: 61046
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1188 21 16 13 62 19 --- 12 | 120 114 125 152 126 --- 123
R03E | 3380 11 14 37 90 34 12 13 | 84 77 92 143 68 82 82
R04E | 1967 16 28 19 73 58 11 14 | 90 95 90 126 78 84 85
R05E | 847 13 30 19 33 17 11 8 | 127 132 128 141 123 123 125
XR06E | 1555 36 1068 1146 --- 52 --- 43 | 52 464 293 --- 57 --- 53
R07E | 1914 20 35 13 86 28 11 13 | 76 93 87 137 69 80 80
R08E | 1036 22 20 12 92 43 25 15 | 80 82 98 142 82 83 83
R09 | 1560 11 23 15 10 16 10 6 | 38 48 38 34 29 40 36
XR11 | 2296 11 25 18 9 14 --- 8 | 30 27 29 33 39 --- 30
R12 | 1037 16 25 14 12 11 13 7 | 25 36 39 31 26 31 28
R14 | 1599 16 32 29 17 12 7 8 | 24 47 43 28 30 32 30
R15 | 509 23 23 25 12 10 9 8 | 21 31 35 25 28 31 25
R16 | 880 23 26 12 6 12 15 8 | 31 44 46 32 46 43 39
R17E | 1088 25 18 15 32 21 15 9 | 43 38 41 44 38 37 34
R18E | 751 9 37 21 21 11 10 8 | 62 81 53 52 63 55 59
XR19E | 2195 15 18 17 --- 14 --- 9 | 38 53 42 --- 49 --- 42
XR20E | 1480 20 31 421 21 37 --- 16 | 24 34 113 25 56 --- 32
R21E | 1916 17 40 35 22 14 17 10 | 71 52 86 76 64 53 63
R22E | 1198 15 17 14 12 12 7 5 | 40 47 43 47 41 44 42
XR24E | 4200 15 19 18 31 40 --- 12 | 203 186 198 202 178 --- 192
XR26E |13056 23 58 48 --- 77 --- 30 | 118 64 64 --- 101 --- 117
XR28 |19463 44 --- --- --- 69 --- 55 | 70 --- --- --- 68 --- 64
------+-----------------------------------------+-------------------------------------
RMS | 1574 17 27 22 49 25 13 |T 66 87 84 81 66 58 66
WRMS | 1574 17 27 21 21 32 13 |NE 34 38 38 30 38 35 36
MEDI | 1555 16 25 18 21 17 11 |MD 52 53 64 47 57 44 53
Table 3.2400.3 GPS week: 2400 Day: 3 MJD: 61047
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1047 11 25 10 42 16 --- 9 | 189 191 195 195 198 --- 191
R03E | 2957 15 12 15 67 21 19 10 | 42 41 46 70 39 42 38
R04E | 1151 15 17 14 60 30 20 10 | 85 95 87 113 74 93 86
R05E | 1491 16 25 15 38 18 17 8 | 174 176 179 176 165 170 171
XR06E | 1571 39 1001 1179 --- 66 --- 51 | 57 424 371 --- 58 --- 58
R07E | 848 12 31 14 77 17 17 11 | 88 98 95 102 83 89 88
R08E | 1331 11 13 14 47 28 20 9 | 73 80 68 83 76 71 70
R09 | 3342 8 22 15 9 11 16 6 | 34 32 39 33 36 33 33
R11 | 1931 10 36 10 13 17 9 7 | 33 45 35 34 42 30 36
R12 | 568 21 18 12 26 23 28 9 | 38 39 36 34 51 39 37
R14 | 1313 18 27 11 13 10 5 6 | 38 51 40 32 39 35 37
R15 | 554 20 13 13 28 35 15 9 | 36 41 34 38 43 41 34
R16 | 1163 17 20 12 13 9 15 6 | 44 53 52 47 51 46 47
R17E | 1330 20 23 16 32 56 20 12 | 96 99 98 108 62 91 91
R18E | 741 6 30 13 19 11 14 7 | 77 92 77 93 73 69 77
XR19E | 1555 13 31 16 --- 14 --- 10 | 46 53 51 --- 55 --- 48
R20E | 1465 15 33 409 24 46 15 13 | 29 43 115 33 66 31 36
R21E | 1981 15 49 26 32 16 20 11 | 97 79 99 110 92 78 90
R22E | 888 13 25 11 25 17 12 7 | 60 72 66 77 73 59 65
R24E | 3302 22 17 20 85 23 23 13 | 198 187 181 183 187 144 186
XR26E | 8445 26 49 52 --- 73 --- 29 | 68 47 75 --- 75 --- 70
XR28 |14935 33 --- --- --- 56 --- 43 | 78 --- --- --- 88 --- 81
------+-----------------------------------------+-------------------------------------
RMS | 1773 16 26 100 42 26 17 |T 76 97 97 86 78 68 75
WRMS | 1773 15 28 19 25 26 17 |NE 43 43 39 36 50 37 43
MEDI | 1331 15 25 14 28 18 17 |MD 60 72 75 77 66 59 65
Table 3.2400.4 GPS week: 2400 Day: 4 MJD: 61048
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 962 6 17 10 23 13 23 6 | 105 112 102 113 112 22 106
R03E | 1414 17 17 10 23 11 24 7 | 37 43 42 46 42 40 38
R04E | 1260 12 14 15 33 16 18 7 | 65 67 64 78 70 71 66
R05E | 1774 14 20 13 43 20 17 9 | 92 100 88 115 91 93 92
XR06E | 1360 43 995 1181 --- 51 --- 47 | 36 382 393 --- 45 --- 38
R07E | 946 16 24 15 27 17 21 8 | 69 71 76 81 76 79 73
R08E | 1050 19 22 15 26 10 28 9 | 62 61 73 68 62 68 62
R09 | 5062 10 40 16 8 16 12 8 | 44 67 56 46 49 44 47
R11 | 1975 14 52 12 17 19 14 9 | 26 62 29 25 32 19 26
R12 | 726 20 25 11 24 12 22 8 | 31 38 24 25 32 22 25
R14 | 761 6 30 19 19 18 12 7 | 32 50 41 26 30 30 32
R15 | 627 28 17 20 26 13 23 10 | 35 35 37 37 26 35 31
R16 | 933 32 59 28 11 16 13 13 | 42 89 48 39 41 54 46
R17E | 1073 10 17 15 86 47 25 15 | 49 41 52 81 59 35 41
R18E | 900 10 22 12 49 20 23 9 | 63 77 73 118 54 58 68
XR19E | 2194 16 32 11 --- 18 15 9 | 50 62 50 --- 38 18 47
R20E | 776 14 31 429 18 30 20 11 | 32 44 128 42 55 33 37
R21E | 1195 18 36 12 36 21 22 10 | 93 69 83 105 73 75 81
R22E | 776 13 21 10 32 12 14 7 | 88 98 94 117 92 87 92
R24E | 4295 14 27 14 24 10 13 7 | 176 182 184 177 175 149 180
XR26E |10698 42 --- --- --- 50 --- 46 | 86 --- --- --- 81 --- 86
XR28 |12448 43 --- --- --- 52 --- 48 | 75 --- --- --- 74 --- 68
------+-----------------------------------------+-------------------------------------
RMS | 1894 16 30 102 34 20 20 |T 63 87 86 74 64 54 62
WRMS | 1894 16 27 27 24 19 20 |NE 40 56 39 33 40 34 39
MEDI | 1073 14 24 14 24 17 20 |MD 50 67 64 68 55 44 47
Table 3.2400.5 GPS week: 2400 Day: 5 MJD: 61049
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 1134 14 14 15 17 16 12 6 | 122 120 119 130 119 21 121
R03E | 1803 11 19 19 18 14 31 8 | 33 35 40 38 34 35 31
R04E | 1364 13 19 25 16 16 20 8 | 71 68 72 77 71 71 70
R05E | 1248 11 36 19 19 18 15 8 | 123 121 139 127 128 122 125
XR06E | 1278 40 1043 1291 --- 51 --- 45 | 47 332 500 --- 48 --- 47
R07E | 1872 17 19 10 21 18 16 7 | 66 68 76 70 71 67 67
R08E | 1968 14 35 17 22 16 24 9 | 60 54 82 60 57 57 56
R09 | 4739 9 37 17 10 11 9 7 | 32 34 43 30 31 36 33
R11 | 2270 13 28 11 17 8 13 6 | 21 38 23 18 21 20 20
R12 | 559 22 38 14 22 8 19 9 | 20 49 28 16 27 23 22
R14 | 889 11 28 21 15 23 12 8 | 24 34 32 27 28 20 21
R15 | 926 23 29 19 17 25 15 9 | 26 39 39 36 36 29 28
R16 | 922 23 23 23 10 6 12 8 | 28 56 43 42 39 56 40
R17E | 1726 14 17 8 19 10 12 6 | 43 44 46 42 39 39 40
R18E | 781 12 24 14 73 39 16 14 | 82 92 89 97 94 74 82
XR19E | 1634 18 20 16 --- 21 16 9 | 63 67 72 --- 73 17 65
R20E | 713 11 29 424 45 25 28 13 | 28 41 113 55 37 29 28
R21E | 756 12 30 26 62 19 14 12 | 105 100 106 102 109 93 100
R22E | 827 13 26 20 60 21 17 11 | 121 133 134 143 127 126 127
R24E | 5169 11 19 13 16 14 16 6 | 125 126 125 119 118 106 122
XR26E | 7216 42 --- --- --- 53 --- 47 | 83 --- --- --- 92 --- 89
XR28 |12122 43 --- --- --- 55 --- 48 | 84 --- --- --- 82 --- 79
------+-----------------------------------------+-------------------------------------
RMS | 2079 15 27 101 32 19 17 |T 63 82 96 68 67 54 64
WRMS | 2079 15 24 20 22 19 17 |NE 33 41 34 28 37 30 34
MEDI | 1278 13 26 17 18 18 16 |MD 60 56 72 55 57 39 56
Table 3.2400.6 GPS week: 2400 Day: 6 MJD: 61050
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 1452 15 26 92 16 12 16 10 | 123 113 164 134 131 25 126
R03E | 2380 12 17 121 14 10 23 12 | 42 41 123 55 42 41 44
R04E | 1254 16 21 46 13 9 23 8 | 76 75 82 81 75 75 75
R05E | 2463 11 31 122 11 10 14 12 | 114 111 165 120 117 111 115
XR06E | 938 42 1061 1305 --- 44 --- 43 | 47 478 516 --- 49 --- 48
R07E | 2259 11 22 105 21 22 24 12 | 66 70 115 72 75 71 69
R08E | 2623 19 19 139 19 20 23 14 | 70 64 100 80 63 75 70
R09 | 2106 20 44 13 12 12 12 8 | 46 42 49 38 39 39 40
R11 | 3320 18 29 15 9 11 16 7 | 39 38 45 37 43 24 39
R12 | 730 24 26 24 24 12 12 9 | 45 48 37 33 42 31 37
R14 | 2797 10 16 24 8 13 13 5 | 49 57 59 47 47 54 50
R15 | 921 19 38 18 18 21 13 9 | 53 45 45 50 47 42 45
R16 | 807 15 26 20 16 20 19 8 | 67 72 66 66 66 69 64
R17E | 2182 17 19 93 14 16 12 10 | 39 41 43 41 39 35 35
R18E | 839 10 21 26 12 15 12 6 | 71 85 76 71 76 71 73
XR19E | 2096 15 25 25 --- 15 --- 10 | 94 93 80 --- 88 --- 89
R20E | 735 21 48 430 39 25 27 16 | 42 47 149 48 56 37 41
R21E | 707 16 40 61 9 15 14 9 | 89 75 106 81 85 81 82
R22E | 732 12 28 16 14 9 7 6 | 91 100 92 89 96 92 92
R24E | 4120 10 25 46 15 22 13 8 | 131 120 135 145 132 113 132
XR26E | 5691 41 --- --- --- 43 --- 42 | 102 --- --- --- 101 --- 103
XR28 |14803 100 --- --- 76 82 --- 61 | 101 --- --- 15 122 --- 104
------+-----------------------------------------+-------------------------------------
RMS | 2064 16 29 123 17 16 17 |T 72 90 112 68 74 60 71
WRMS | 2064 16 26 54 14 16 17 |NE 57 50 50 40 58 43 54
MEDI | 2096 16 26 46 14 15 14 |MD 67 70 82 66 66 54 69
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