[IGSREPORT-30756] Wk 2399 IGLOS Final Orbits
acc
acc at igs.org
Fri Jan 16 04:19:43 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2399 (Dec 28, 2025 - Jan 03, 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 2.2399.
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:
igl2399[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2399 in the SP3 format.
igl23997.sum Combination Report for GPS Week 2399.
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 | 2.6 ns
1 | -2.4 ns
2 | 2.8 ns
3 | 2.8 ns
4 | 3.5 ns
5 | 5.7 ns
6 | 5.9 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ALL | R26
0 | ESA | R06
0 | GFZ | R06 R20
1 | ALL | R26
1 | ESA | R06
1 | GFZ | R06 R20
2 | ALL | R26
2 | ESA | R06
2 | GFZ | R06 R20
3 | ALL | R26
3 | ESA | R06
3 | GFZ | R06 R20
4 | ALL | R26
4 | ESA | R06
4 | GFZ | R06 R20
5 | 126 | R11
5 | ESA | R06
5 | GFZ | R06 R20
6 | 126 | R11
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 1.2399, 1a.2399).
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 2.2399.0-6)
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 3.2399.0-6).
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 2399 summary. (Dec 28, 2025 - Jan 03, 2026)
Table 1.2399.a GPS week : 2399 MJD: 61037.0-61043.0
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 2 -9 5 15 .12 14 15 | 1719 -1490 3313 10165
| 0 1 2 12 12 19 .05 | 1204 1766
esa n/a| -2 0 -5 -29 -13 56 -.22 28 26 | 3535 -1229 3327 9832
| 1 1 2 11 12 58 .17 | 1468 1791
gfz n/a| 0 0 1 34 -5 29 .03 67 23 | 0 -1247 3430 9823
| 1 1 2 9 16 34 .08 | 0 1912
grg n/a| 2 0 1 -23 -19 -35 .30 15 15 | 3334 -1162 3378 8676
| 1 1 1 11 10 31 .06 | 2391 2063
iac n/a| 0 0 -3 22 19 -27 -.15 16 17 | 5354 -458 3490 10991
| 1 1 2 10 30 61 .07 | 2726 557
jgx n/a| 0 0 1 -10 18 -13 -.28 17 17 | 3543 -1118 3312 9111
| 1 0 1 18 14 14 .08 | 1438 2249
Table 1.2399.b GPS week : 2399 MJD: 61037.0-61043.0
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 7 7 6 6 8 7 |
R03 | 5 6 7 6 7 6 7 |
R04 | 8 7 7 6 8 6 8 |
R05 | 6 8 7 6 7 8 7 |
R06 | 44 44 53 45 43 47 51 |
R07 | 7 7 9 8 7 7 9 |
R08 | 6 8 7 8 7 7 8 |
R09 | 6 7 8 5 8 7 7 |
R11 | 6 6 6 7 31 --- --- |
R12 | 6 7 7 8 9 10 7 |
R14 | 8 9 7 7 6 7 6 |
R15 | 10 9 8 6 6 7 8 |
R16 | 8 9 9 7 8 8 9 |
R17 | 7 8 8 9 8 8 8 |
R18 | 7 8 7 8 7 6 8 |
R19 | 8 7 9 8 8 9 11 |
R20 | 15 13 17 15 14 14 14 |
R21 | 9 10 11 10 8 9 9 |
R22 | 6 6 7 7 7 7 8 |
R24 | 8 9 9 8 7 8 8 |
R28 | 0 73 46 45 43 32 0 |
Table 1.2399.c GPS week : 2399 MJD: 61037.0-61043.0
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 2399 0 | 65 21 -67 77 -1659 6177 77.6 2028 2028 | 2594 0
brd 2399 1 | 15 30 112 -713 -2281 4181 79.8 1924 1924 | -2376 0
brd 2399 2 | -72 52 27 -1416 -2520 6112 80.2 1785 1785 | 2834 0
brd 2399 3 | -9 61 173 -1522 -2469 3659 80.0 7870 7870 | 2819 0
brd 2399 4 | 22 -10 -62 -724 338 7819 80.4 1728 1728 | 3451 0
brd 2399 5 | 36 66 3 -904 3175 5813 79.2 1779 1779 | 5720 0
brd 2399 6 | 99 16 11 -157 4276 -2890 79.8 1596 1596 | 5901 0
-------------+------------------------------------------------------------+----------------
brd 2399 mean| 22 34 28 -765 -162 4410 79.6 2672 2672 | 2991 0
brd 2399 sdev| 55 27 87 591 2848 3500 1.0 2295 2295 | 2742 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 2.2399.0 GPS week: 2399 Day: 0 MJD: 61037
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 21 45 .06 14 16 | 3278 1118 3085 8749
esa n/a| -2 -2 -4 -44 -10 92 -.20 28 26 | 4309 2275 3102 8577
gfz n/a| -2 0 0 31 -33 76 .08 101 30 | 0 1383 3205 8583
grg n/a| 1 0 1 -18 -36 -24 .33 14 14 | 1520 1698 3154 6843
iac n/a| 2 -2 0 26 78 -145 -.14 19 19 | 3974 67 3081 9207
jgx n/a| 1 0 2 -18 5 -13 -.23 15 15 | 5118 1423 3075 6693
Table 2.2399.1 GPS week: 2399 Day: 1 MJD: 61038
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 0 7 -1 29 .05 13 13 | 550 -3345 3000 9601
esa n/a| -1 0 -10 -34 -24 -26 -.21 30 30 | 1257 -2045 3016 9344
gfz n/a| 0 0 4 38 10 13 .12 100 21 | 0 -2993 3070 9045
grg n/a| 0 0 0 -35 -26 -59 .26 15 15 | -1066 -3365 3109 7326
iac n/a| 3 -3 -2 17 -6 34 -.20 18 19 | 592 -1024 3400 10722
jgx n/a| 1 0 3 20 14 -15 -.26 15 15 | 2883 -3862 2960 7509
Table 2.2399.2 GPS week: 2399 Day: 2 MJD: 61039
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 0 12 30 .13 14 14 | 3128 -3479 3433 9314
esa n/a| 0 0 -4 -21 1 65 .06 27 25 | 5473 -3328 3444 9149
gfz n/a| 0 -2 2 30 -14 -27 -.03 17 14 | 0 -3442 3523 8933
grg n/a| 3 -1 5 -25 -15 -2 .24 16 17 | 4559 -3770 3510 7634
iac n/a| 0 0 -7 16 6 -14 -.27 15 16 | 5482 -1109 3740 10470
jgx n/a| 0 2 2 -23 44 -33 -.17 16 16 | 5067 -4243 3433 8332
Table 2.2399.3 GPS week: 2399 Day: 3 MJD: 61040
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 2 -5 9 1 .14 14 14 | 38 -1200 3497 10444
esa n/a| -1 -1 -5 -27 -35 4 -.12 22 19 | 2008 -1384 3540 10033
gfz n/a| 0 1 -3 47 10 2 -.09 17 18 | 0 -703 3644 10386
grg n/a| 4 0 3 -9 -5 -11 .35 16 17 | 3111 -837 3544 9575
iac n/a| -1 -1 -1 32 -11 -11 -.10 14 14 | 4404 -722 3578 10922
jgx n/a| 0 0 0 -32 8 -30 -.20 17 17 | 920 -60 3525 10417
Table 2.2399.4 GPS week: 2399 Day: 4 MJD: 61041
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 4 -31 -16 0 .12 13 13 | 1902 -2834 3135 10732
esa n/a| -3 -2 -4 -27 -6 17 -.23 24 23 | 3427 -2373 3089 10992
gfz n/a| 0 0 2 22 9 48 -.03 17 15 | 0 -3075 3181 10337
grg n/a| 1 0 0 -9 -20 -85 .23 16 15 | 4299 -2302 3052 9410
iac n/a| 0 0 -4 29 20 27 -.14 14 14 | 6463 288 3541 11546
jgx n/a| -2 1 0 -1 32 -5 -.36 18 18 | 3462 -1646 3024 10210
Table 2.2399.5 GPS week: 2399 Day: 5 MJD: 61042
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 5 -14 1 -5 .16 15 16 | 1673 -229 3806 11301
esa n/a| -1 0 -5 -41 -10 110 -.37 29 27 | 3731 -467 3842 10681
gfz n/a| 1 0 0 44 -15 43 .14 111 29 | 0 336 3986 10920
grg n/a| 3 -2 0 -27 -8 -56 .32 15 14 | 5189 712 3926 10295
iac n/a| -1 0 -4 5 19 -16 -.04 19 20 | 8888 -37 3860 12461
jgx n/a| -2 0 0 1 15 -2 -.37 15 15 | 3323 1085 3867 10693
Table 2.2399.6 GPS week: 2399 Day: 6 MJD: 61043
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 -6 10 7 .20 15 16 | 1465 -466 3238 11016
esa n/a| -4 1 -4 -12 -10 128 -.48 35 30 | 4543 -1287 3257 10049
gfz n/a| 1 0 0 24 -7 47 .03 104 31 | 0 -240 3407 10560
grg n/a| 1 -2 1 -38 -23 -6 .39 14 14 | 5729 -274 3353 9654
iac n/a| 0 0 -5 31 30 -66 -.17 16 14 | 7677 -670 3233 11613
jgx n/a| -2 0 3 -19 11 6 -.34 19 19 | 4030 -524 3302 9925
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 3.2399.0 GPS week: 2399 Day: 0 MJD: 61037
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 799 10 17 15 10 8 --- 6 | 29 31 38 35 30 --- 31
R03E | 2220 10 13 10 14 9 12 5 | 60 60 64 70 64 59 62
R04E | 1547 11 32 16 19 15 12 7 | 36 52 40 37 38 36 36
R05E | 1893 8 31 13 15 10 9 6 | 38 38 43 42 36 31 36
XR06E | 1043 41 985 988 --- 46 --- 43 | 82 423 366 --- 89 --- 86
R07E | 2820 15 38 14 9 10 14 7 | 73 74 75 71 73 70 71
R08E | 3112 13 15 14 12 15 14 6 | 35 36 35 38 37 31 33
R09 | 497 16 15 16 10 14 5 6 | 22 20 29 20 21 20 19
R11 | 2805 10 24 13 14 14 12 6 | 126 109 111 127 124 14 129
R12 | 669 17 18 7 11 10 14 5 | 40 45 33 28 38 25 32
R14 | 4194 11 21 12 23 10 23 7 | 52 61 51 47 54 56 51
R15 | 1014 25 28 13 21 25 19 9 | 65 57 57 50 60 46 52
R16 | 664 15 28 12 10 20 17 7 | 64 62 53 53 58 48 54
R17 | 1800 17 19 13 8 14 17 6 | 176 171 172 171 167 161 169
R18 | 1170 5 31 10 12 21 18 7 | 133 149 133 139 139 129 135
XR19 | 4152 15 23 14 --- 10 15 7 | 96 95 92 --- 88 17 90
R20 | 2151 13 39 416 17 47 22 14 | 57 62 167 62 86 45 63
R21 | 747 16 48 11 13 18 16 8 | 147 127 148 138 147 126 139
R22 | 1076 14 27 9 11 13 9 6 | 67 83 69 65 72 67 68
R24 | 1663 18 21 16 15 16 19 7 | 150 128 149 137 130 126 137
XR28 |13747 3 --- --- --- --- --- 0 | 126 --- --- --- --- --- 116
------+-----------------------------------------+-------------------------------------
RMS | 2027 14 28 101 14 19 15 |T 79 94 96 73 77 61 76
WRMS | 2027 16 26 30 14 19 15 |NE 94 89 97 86 91 67 89
MEDI | 1663 14 24 13 12 14 14 |MD 65 62 64 53 64 46 63
Table 3.2399.1 GPS week: 2399 Day: 1 MJD: 61038
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 897 10 22 11 7 17 --- 6 | 30 35 34 35 25 --- 29
R03E | 1754 8 23 14 12 12 8 5 | 60 66 63 63 53 59 59
R04E | 1728 12 26 16 12 14 14 6 | 25 38 32 35 29 25 26
R05E | 1094 9 23 16 24 17 12 7 | 36 38 38 39 39 32 34
XR06E | 1247 39 968 837 --- 48 --- 43 | 77 324 286 --- 85 --- 79
R07E | 3476 8 42 15 10 16 8 7 | 57 68 57 55 51 56 54
R08E | 3145 16 23 13 21 16 21 8 | 47 56 41 46 45 46 43
R09 | 1024 13 24 9 17 17 9 6 | 18 33 24 17 20 13 14
R11 | 1438 11 13 23 8 13 11 6 | 84 73 76 89 78 12 85
R12 | 946 8 40 13 14 10 12 7 | 29 55 31 23 28 25 27
R14 | 3566 6 37 35 11 24 8 9 | 40 63 58 40 43 43 41
R15 | 1158 16 28 30 14 14 20 9 | 50 41 61 41 46 37 44
R16 | 864 18 33 23 15 16 20 9 | 47 51 48 43 43 30 40
R17 | 1934 18 19 14 16 15 19 7 | 157 148 155 152 154 153 153
R18 | 1172 13 33 14 17 18 14 7 | 107 116 106 116 117 113 111
XR19 | 3350 12 21 13 --- 13 12 6 | 77 88 82 --- 78 17 79
R20 | 2639 11 42 405 14 39 21 12 | 58 62 104 64 71 60 60
R21 | 810 16 40 27 15 17 18 9 | 100 82 110 89 88 88 92
R22 | 980 14 22 10 10 11 9 5 | 62 66 62 66 58 61 61
R24 | 1073 20 23 26 14 18 19 9 | 95 83 91 81 80 79 83
XR28 |14843 65 --- --- --- 80 --- 72 | 126 --- --- --- 63 --- 97
------+-----------------------------------------+-------------------------------------
RMS | 1923 13 30 100 15 18 15 |T 65 79 77 60 61 52 62
WRMS | 1923 13 30 21 15 19 15 |NE 75 73 77 68 69 56 70
MEDI | 1247 13 24 15 14 16 12 |MD 58 63 61 46 53 43 59
Table 3.2399.2 GPS week: 2399 Day: 2 MJD: 61039
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1758 11 15 15 11 14 --- 6 | 28 31 36 37 27 --- 29
R03E | 2016 10 16 15 16 19 13 6 | 41 38 44 37 40 31 37
R04E | 770 9 25 13 15 14 14 6 | 33 26 29 40 32 26 29
R05E | 1670 13 23 19 15 9 15 7 | 25 31 32 35 28 19 25
XR06E | 1052 48 874 967 --- 57 --- 52 | 41 307 266 --- 43 --- 39
R07E | 3653 11 46 16 18 15 10 8 | 58 76 66 52 50 56 56
R08E | 2328 13 19 19 14 12 11 6 | 37 45 44 44 38 37 38
R09 | 1626 20 29 19 19 13 10 8 | 21 38 27 19 26 17 18
R11 | 1414 10 25 12 11 13 12 6 | 129 92 104 124 135 10 132
R12 | 910 15 21 11 7 15 24 7 | 35 35 26 29 38 18 28
R14 | 3263 6 22 14 18 16 12 6 | 45 58 55 52 41 50 48
R15 | 951 12 21 26 15 18 12 8 | 52 44 56 46 52 48 48
R16 | 617 20 24 22 22 13 16 8 | 57 58 66 44 60 46 53
R17 | 1620 15 17 10 18 17 20 7 | 107 97 99 90 110 92 99
R18 | 1387 11 29 8 13 11 18 6 | 90 92 85 87 86 77 85
XR19 | 2245 14 28 9 --- 15 --- 9 | 36 58 42 --- 45 --- 42
XR20 | 3333 18 25 409 20 42 --- 16 | 44 55 120 51 71 --- 52
R21 | 801 17 38 16 23 26 24 10 | 121 103 122 117 118 100 113
R22 | 1097 13 28 10 15 14 9 6 | 41 45 49 57 42 43 44
R24 | 971 16 25 23 14 16 26 9 | 135 120 142 132 129 125 130
XR28 |17484 42 --- --- --- 49 --- 46 | 87 --- --- --- 48 --- 73
------+-----------------------------------------+-------------------------------------
RMS | 1784 14 27 17 16 15 16 |T 60 72 75 60 59 49 58
WRMS | 1784 14 25 14 17 16 16 |NE 71 68 76 70 71 56 68
MEDI | 1620 13 25 15 15 15 13 |MD 44 55 55 46 45 43 48
Table 3.2399.3 GPS week: 2399 Day: 3 MJD: 61040
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 7221 12 10 11 9 11 --- 5 | 36 38 33 35 29 --- 32
R03E | 7794 12 13 14 15 14 12 6 | 58 56 63 63 62 61 60
R04E | 5659 11 23 12 12 11 16 6 | 42 48 42 51 38 41 41
R05E | 7864 10 23 15 9 10 17 6 | 47 52 50 45 44 43 44
XR06E | 5660 43 836 908 --- 45 --- 44 | 52 347 246 --- 54 --- 51
R07E | 6898 13 34 13 14 13 12 7 | 43 45 45 50 41 48 42
R08E | 6100 15 16 19 25 13 14 7 | 42 44 38 51 34 39 39
R09 | 7345 10 15 16 11 9 9 5 | 17 31 35 17 21 22 21
R11 | 5474 11 13 20 23 17 8 7 | 90 53 59 71 91 16 82
R12 | 5920 21 17 16 21 16 16 8 | 33 24 23 20 27 17 21
R14 | 5474 10 19 28 19 7 9 7 | 37 36 61 31 32 32 36
R15 | 3074 11 19 12 15 13 10 6 | 38 45 41 46 38 40 39
R16 | 4766 14 23 17 11 14 16 7 | 46 60 44 51 52 44 47
R17 | 8663 17 24 13 9 25 28 9 | 135 114 131 130 133 116 127
R18 |10723 15 20 13 16 15 19 7 | 76 87 84 83 90 71 81
XR19 |10319 14 16 11 --- 12 --- 7 | 39 51 44 --- 46 --- 44
XR20 |12481 15 23 412 23 36 --- 15 | 31 41 110 36 55 --- 38
R21 | 9361 9 32 25 14 16 28 9 | 104 94 119 107 109 83 102
R22 |15480 13 27 14 20 13 8 7 | 37 55 34 45 43 39 39
R24 | 7281 20 18 11 11 9 27 7 | 110 87 96 101 99 86 97
XR28 |21093 44 --- --- --- 45 --- 44 | 75 --- --- --- 71 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 7869 14 22 17 16 14 17 |T 56 70 69 57 57 49 54
WRMS | 7869 14 19 18 17 14 17 |NE 62 59 67 61 64 51 59
MEDI | 7281 13 19 14 14 13 14 |MD 43 51 45 50 46 41 44
Table 3.2399.4 GPS week: 2399 Day: 4 MJD: 61041
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 978 10 17 10 13 9 --- 5 | 40 42 41 42 38 --- 38
R03E | 1959 13 17 17 16 15 14 7 | 52 55 60 61 47 49 52
R04E | 1818 13 27 15 12 17 17 7 | 54 63 56 51 46 46 50
R05E | 3061 9 21 24 9 15 16 7 | 40 36 49 40 35 32 37
XR06E | 1346 39 860 1002 --- 45 --- 42 | 46 333 266 --- 51 --- 48
R07E | 1721 10 23 15 17 13 16 6 | 45 47 56 48 43 55 47
R08E | 2342 9 17 13 15 15 19 6 | 60 62 50 67 44 59 55
R09 | 1823 9 17 33 9 11 12 7 | 20 24 45 21 18 23 21
XR11 |12292 37 --- --- 53 39 --- 30 | 183 --- --- 146 173 --- 167
R12 | 958 21 24 12 28 14 21 9 | 45 49 37 40 40 29 37
R14 | 1149 9 16 17 13 8 10 5 | 49 53 45 49 42 49 46
R15 | 962 12 24 12 12 17 7 6 | 52 55 55 61 49 51 52
R16 | 1429 14 27 14 8 15 30 8 | 58 59 55 59 61 49 55
R17 | 1462 14 28 15 20 14 21 8 | 109 103 107 98 92 90 99
R18 | 1412 12 25 14 17 9 21 7 | 94 109 92 109 99 88 97
XR19 | 2842 11 22 14 --- 12 --- 8 | 48 57 50 --- 51 --- 50
XR20 | 1649 10 29 441 26 30 --- 13 | 41 37 143 42 48 --- 38
R21 | 1917 15 33 14 14 13 26 8 | 80 76 78 74 76 60 73
R22 | 883 13 32 13 13 14 10 7 | 36 56 47 41 38 37 39
R24 | 1637 10 22 13 21 14 14 7 | 78 71 78 76 80 71 76
XR28 |20160 39 --- --- --- 46 --- 42 | 107 --- --- --- 60 --- 96
------+-----------------------------------------+-------------------------------------
RMS | 1727 13 24 17 16 14 18 |T 63 73 74 62 58 52 60
WRMS | 1727 13 23 15 15 14 18 |NE 71 62 69 68 66 54 67
MEDI | 1649 12 24 14 14 14 16 |MD 52 56 55 51 48 49 50
Table 3.2399.5 GPS week: 2399 Day: 5 MJD: 61042
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1210 9 26 8 19 17 --- 7 | 44 48 42 52 36 --- 41
R03E | 1743 11 20 12 12 13 10 5 | 68 69 67 72 67 67 67
R04E | 2617 16 21 16 8 10 14 6 | 33 27 34 33 34 28 30
R05E | 4151 11 40 10 12 20 18 8 | 33 48 36 40 33 28 32
XR06E | 1129 45 945 1075 --- 49 --- 47 | 54 348 316 --- 59 --- 55
R07E | 2243 11 23 18 13 20 15 7 | 56 60 55 56 63 48 54
R08E | 989 17 21 15 10 15 13 6 | 39 34 36 38 29 33 33
R09 | 811 12 38 9 9 21 11 7 | 15 42 24 22 27 14 16
R12 | 595 16 34 16 31 19 15 10 | 35 49 41 23 42 24 31
R14 | 1572 10 14 27 6 22 5 7 | 46 46 45 47 54 44 45
R15 | 938 21 14 11 16 11 19 7 | 44 45 43 36 37 38 38
R16 | 2130 15 34 12 17 17 8 7 | 47 60 38 55 38 50 44
R17 | 1083 16 24 20 17 11 20 8 | 81 64 80 67 71 65 70
R18 | 768 7 30 13 13 10 14 6 | 65 68 50 72 64 55 61
XR19 | 2807 14 20 14 --- 12 --- 8 | 53 49 47 --- 49 --- 49
R20 | 1098 16 32 442 20 42 24 13 | 42 51 80 42 62 59 46
R21 | 1979 24 42 17 13 12 20 9 | 76 72 70 67 56 53 63
R22 | 788 15 34 7 14 13 12 7 | 31 43 33 38 30 37 32
R24 | 1052 17 26 22 14 15 16 8 | 83 68 84 71 76 71 75
XR28 |16735 31 --- --- --- 33 --- 32 | 100 --- --- --- 78 --- 104
------+-----------------------------------------+-------------------------------------
RMS | 1779 15 29 111 15 19 15 |T 58 74 72 56 56 44 55
WRMS | 1779 16 27 29 14 20 15 |NE 64 66 66 60 61 46 61
MEDI | 1129 15 26 15 13 15 14 |MD 47 49 45 47 54 44 46
Table 3.2399.6 GPS week: 2399 Day: 6 MJD: 61043
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 1310 9 26 14 16 10 --- 7 | 57 69 58 54 54 --- 55
R03E | 1574 10 29 13 18 11 12 6 | 67 68 73 74 72 66 69
R04E | 1820 16 27 23 14 10 21 8 | 32 41 43 38 33 33 34
R05E | 3429 10 40 13 9 8 15 6 | 42 55 43 48 41 44 43
XR06E | 1067 54 938 1062 --- 48 --- 51 | 50 362 361 --- 48 --- 48
R07E | 1460 19 25 23 16 18 18 8 | 89 91 95 95 89 89 90
R08E | 741 16 25 12 13 15 28 8 | 48 57 56 57 41 40 48
R09 | 764 12 29 14 8 15 13 6 | 24 31 26 22 18 23 20
R12 | 752 21 29 13 14 11 9 7 | 37 48 35 24 35 25 30
R14 | 1818 8 21 13 9 15 8 5 | 54 56 49 51 61 53 53
R15 | 808 22 30 16 11 20 16 8 | 58 66 54 49 57 46 51
R16 | 2090 17 51 14 14 13 17 8 | 64 93 59 63 59 52 60
R17 | 926 14 24 12 20 9 25 7 | 125 108 117 117 113 99 113
R18 | 583 11 27 19 16 13 24 8 | 91 108 96 102 96 84 94
XR19 | 2494 14 39 14 --- 20 --- 11 | 52 70 51 --- 47 --- 50
R20 | 1578 18 50 414 16 36 26 14 | 52 59 112 49 73 50 54
R21 | 2170 15 63 13 8 12 18 9 | 109 81 104 99 95 86 97
R22 | 934 20 36 9 16 13 11 7 | 40 55 37 37 32 33 35
R24 | 1333 7 29 22 17 14 24 8 | 111 101 117 103 112 102 108
XR28 |18263 4 --- --- --- --- --- 0 | 113 --- --- --- --- --- 111
------+-----------------------------------------+-------------------------------------
RMS | 1596 15 35 104 14 16 19 |T 71 88 87 69 67 57 68
WRMS | 1596 16 30 31 14 14 19 |NE 79 79 78 74 74 59 75
MEDI | 1333 14 29 14 14 13 17 |MD 57 68 58 54 57 50 54
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