[IGSREPORT-30812] Wk 2405 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 27 02:50:02 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2405 (Feb 08, 2026 - Feb 14, 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 2.2405.
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:
igl2405[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2405 in the SP3 format.
igl24057.sum Combination Report for GPS Week 2405.
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 | 7.3 ns
1 | 6.3 ns
2 | 10.6 ns
3 | 6.5 ns
4 | 5.5 ns
5 | 5.1 ns
6 | 3.7 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
1 | ALL | R26
1 | ESA | R06
1 | GFZ | R11
2 | ALL | R26
2 | ESA | R06
3 | ALL | R11 R26
3 | ESA | R06
4 | ALL | R11 R26
4 | ESA | R06
5 | ALL | R11
5 | ESA | R06
6 | ESA | R06
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2405, 1a.2405).
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 2.2405.0-6)
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 3.2405.0-6).
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 2405 summary. (Feb 08, 2026 - Feb 14, 2026)
Table 1.2405.a GPS week : 2405 MJD: 61079.0-61085.0
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 10 2 -3 .09 13 13 | 3750 62 3550 9356
| 0 1 2 16 13 20 .02 | 1212 3215
esa n/a| -1 -1 -1 -35 23 23 -.17 38 36 | 4667 -306 3558 9598
| 1 2 2 25 7 48 .03 | 1932 2918
gfz n/a| 0 0 -1 6 15 29 -.18 16 15 | 0 100 3522 9254
| 1 0 2 12 13 37 .05 | 0 2994
grg n/a| 1 0 2 -15 -16 -28 .25 18 14 | 6128 150 3549 9061
| 0 0 2 15 15 49 .02 | 1171 3823
jgx n/a| 1 0 3 -5 -5 -14 -.14 15 15 | 5525 178 3486 9494
| 1 1 2 13 10 21 .05 | 1486 3311
Table 1.2405.b GPS week : 2405 MJD: 61079.0-61085.0
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 9 9 7 8 |
R03 | 7 7 7 8 8 9 10 |
R04 | 6 8 8 6 7 7 7 |
R05 | 8 7 9 10 7 7 10 |
R06 | 12 17 11 10 12 13 24 |
R07 | 8 10 10 11 10 8 9 |
R08 | 9 9 9 10 11 11 10 |
R09 | 8 10 11 10 9 8 9 |
R11 | 9 64 --- --- --- --- 12 |
R12 | 9 11 9 10 10 7 7 |
R14 | 7 8 9 7 10 11 9 |
R15 | 8 8 7 7 7 13 7 |
R16 | 12 8 8 10 9 9 8 |
R17 | 9 10 9 10 12 27 16 |
R18 | 6 7 7 7 8 9 16 |
R19 | 9 9 11 10 10 9 9 |
R20 | 11 8 8 8 9 9 9 |
R21 | 11 11 9 9 8 12 17 |
R22 | 8 8 8 9 8 9 11 |
R24 | 8 8 9 12 16 13 11 |
R26 | --- --- --- --- --- 9 23 |
R28 | 0 0 0 0 0 0 0 |
Table 1.2405.c GPS week : 2405 MJD: 61079.0-61085.0
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 2405 0 | -34 69 26 524 -656 5971 82.6 1707 1707 | 7265 0
brd 2405 1 | -55 -40 84 1423 -2211 12090 80.4 2039 2039 | 6256 0
brd 2405 2 | -33 123 27 -237 -2153 10750 78.0 1957 1957 | 10560 0
brd 2405 3 | 86 24 37 -1044 -944 6847 81.4 1832 1832 | 6522 0
brd 2405 4 | -75 -22 86 1302 -686 6053 82.4 2211 2211 | 5503 0
brd 2405 5 | 90 -19 3 588 23 5961 79.8 1666 1666 | 5132 0
brd 2405 6 | -13 -28 6 -535 155 8284 80.6 1935 1935 | 3662 0
-------------+------------------------------------------------------------+----------------
brd 2405 mean| -5 15 38 288 -924 7993 80.7 1906 1906 | 6414 0
brd 2405 sdev| 66 61 34 930 944 2508 1.6 190 190 | 2160 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 2.2405.0 GPS week: 2405 Day: 0 MJD: 61079
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 -3 29 15 16 .09 12 13 | 2448 -571 3594 10160
esa n/a| -2 -2 -2 -48 16 -57 -.16 35 33 | 5165 -563 3625 10787
gfz n/a| -1 1 -2 -10 31 10 -.26 16 16 | 0 -182 3591 10129
grg n/a| 1 0 0 -3 -41 -28 .27 14 12 | 7097 -63 3471 9313
jgx n/a| 2 0 6 4 -17 2 -.11 15 15 | 4582 -603 3526 9641
Table 2.2405.1 GPS week: 2405 Day: 1 MJD: 61080
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 0 -1 -6 2 -39 .09 12 12 | 3011 -2715 3943 8934
esa n/a| -3 1 2 -24 25 53 -.19 37 33 | 5303 -2555 3732 8345
gfz n/a| 0 0 -6 -1 12 -4 -.20 15 14 | 0 -2079 3763 8537
grg n/a| 1 0 1 -8 -28 71 .27 16 15 | 8008 -3231 3692 8238
jgx n/a| 1 0 4 5 2 -37 -.19 14 14 | 4328 -2806 3689 8813
Table 2.2405.2 GPS week: 2405 Day: 2 MJD: 61081
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 5 6 .05 12 11 | 2323 5993 4757 8653
esa n/a| -2 0 3 -45 23 75 -.18 35 34 | 5433 4776 4803 8248
gfz n/a| -2 -1 -1 -1 3 92 -.13 19 18 | 0 5722 4765 8818
grg n/a| 2 0 1 2 -18 -54 .22 13 12 | 6641 7283 4710 8655
jgx n/a| 2 2 5 -25 9 -33 -.21 14 14 | 3441 6570 4784 9068
Table 2.2405.3 GPS week: 2405 Day: 3 MJD: 61082
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 -11 0 -20 .09 14 14 | 4231 1523 2861 9560
esa n/a| -1 -2 -1 -7 32 57 -.18 44 43 | 2316 604 2919 10366
gfz n/a| 0 0 1 18 0 24 -.22 16 15 | 0 1115 2857 9605
grg n/a| 2 0 2 -7 3 -9 .23 15 13 | 5605 1184 2951 9708
jgx n/a| 0 0 0 11 -11 -28 -.13 15 15 | 5869 1486 2895 10158
Table 2.2405.4 GPS week: 2405 Day: 4 MJD: 61083
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 2 13 0 .06 13 12 | 4971 536 3408 9053
esa n/a| -2 -5 -1 -4 32 32 -.21 36 36 | 2005 584 3452 9809
gfz n/a| 0 0 1 6 18 12 -.14 18 16 | 0 173 3402 9126
grg n/a| 1 0 2 -36 -11 -62 .25 19 15 | 4973 488 3545 9177
jgx n/a| 1 0 2 -6 -19 3 -.15 15 15 | 6525 71 3458 9495
Table 2.2405.5 GPS week: 2405 Day: 5 MJD: 61084
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 29 9 17 .12 15 15 | 5426 -361 2930 10147
esa n/a| 0 -1 -3 -78 15 26 -.17 47 42 | 7586 -381 2953 9974
gfz n/a| 1 0 0 10 7 0 -.15 13 13 | 0 -107 2929 9895
grg n/a| 0 0 2 -31 -15 -40 .26 18 13 | 4799 161 3000 9490
jgx n/a| 1 -1 3 -12 1 15 -.14 16 16 | 7781 54 3023 9900
Table 2.2405.6 GPS week: 2405 Day: 6 MJD: 61085
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 -6 21 -24 -1 .11 16 14 | 3843 -3965 3359 8988
esa n/a| -2 0 -4 -40 19 -27 -.12 34 34 | 4861 -4611 3426 9658
gfz n/a| 0 0 0 24 34 69 -.13 15 15 | 0 -3938 3352 8670
grg n/a| 1 -1 8 -24 0 -75 .25 31 20 | 5775 -4767 3480 8850
jgx n/a| 0 0 2 -16 -4 -23 -.06 14 14 | 6149 -3520 3031 9385
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 3.2405.0 GPS week: 2405 Day: 0 MJD: 61079
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1354 14 28 15 11 19 8 | 81 68 72 72 66 72
R03 | 2284 9 10 10 13 19 6 | 95 101 90 94 80 90
R04 | 1211 9 11 7 15 14 6 | 105 117 108 111 103 107
R05 | 889 16 39 12 8 12 8 | 92 107 100 93 86 93
XR06 | 984 11 788 13 --- --- 12 | 48 172 65 --- --- 56
R07 | 1046 8 27 18 13 15 7 | 86 95 80 87 75 83
R08 | 616 16 38 15 14 15 9 | 65 95 65 73 64 67
R09 | 3272 12 45 10 11 9 8 | 38 30 35 33 34 32
R11 | 2622 8 34 24 14 11 8 | 69 43 230 72 10 59
R12 | 1372 15 34 15 16 10 8 | 73 72 78 71 61 70
R14 | 1532 7 37 12 7 7 6 | 54 63 48 47 47 49
R15 | 1119 9 29 9 13 21 7 | 65 83 64 68 56 64
R16 | 1647 18 52 17 16 27 12 | 70 80 70 69 53 64
XR17E | 827 11 21 14 15 --- 8 | 68 67 73 82 --- 72
R18E | 1287 7 26 10 11 10 5 | 44 50 43 46 40 42
XR19E | 1227 11 29 12 --- 15 8 | 27 41 30 --- 28 29
R20E | 2162 13 40 31 11 14 10 | 31 47 46 33 31 30
R21E | 1002 16 49 17 22 15 11 | 52 57 49 46 37 43
R22E | 1927 10 39 12 17 10 8 | 26 51 34 32 29 29
R24E | 1386 15 18 17 15 10 7 | 133 147 148 150 137 141
XR28E |15005 3 --- --- --- --- 0 | 95 --- --- --- --- 96
------+------------------------------------+--------------------------------
RMS | 1707 12 35 16 14 15 |T 77 79 76 71 57 76
WRMS | 1707 13 33 16 12 15 |NE 88 86 85 74 61 85
MEDI | 1354 11 34 13 13 14 |MD 68 68 65 71 53 64
Table 3.2405.1 GPS week: 2405 Day: 1 MJD: 61080
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 754 12 20 14 11 9 6 | 47 38 49 44 44 45
R03 | 4527 8 17 14 13 17 6 | 55 64 58 63 51 56
R04 | 2631 9 15 13 24 11 7 | 71 70 70 79 71 71
R05 | 1329 10 25 8 13 13 6 | 64 70 59 65 55 61
XR06 | 1262 15 777 18 --- --- 17 | 46 114 65 --- --- 54
R07 | 1486 16 53 15 14 14 10 | 48 60 41 37 36 40
R08 | 836 13 32 20 14 16 8 | 41 53 51 49 43 45
R09 | 2917 10 56 14 12 14 9 | 32 39 19 35 27 26
XR11 | 2574 56 --- 931 72 --- 63 | 50 --- 789 98 --- 27
R12 | 1155 15 36 24 27 13 11 | 58 68 74 52 48 56
R14 | 1894 6 42 13 17 12 8 | 41 55 51 38 36 41
R15 | 1879 13 33 9 9 20 8 | 51 68 55 46 45 49
R16 | 1767 15 40 14 11 8 8 | 56 68 59 58 58 57
XR17E | 1158 15 18 13 20 --- 9 | 61 49 58 55 --- 55
R18E | 1500 8 21 17 14 9 6 | 31 37 41 34 31 32
XR19E | 1191 11 30 11 --- 15 8 | 29 37 32 --- 30 30
R20E | 1056 11 32 12 10 21 8 | 30 52 34 37 27 31
R21E | 871 14 59 9 15 17 10 | 39 55 36 36 37 34
R22E | 2582 10 41 12 17 12 8 | 24 41 29 33 25 25
R24E | 1725 14 22 15 22 10 8 | 134 143 136 133 137 135
XR28E |15550 2 --- --- --- --- 0 | 79 --- --- --- --- 78
------+------------------------------------+--------------------------------
RMS | 2039 12 37 15 16 14 |T 61 62 90 55 47 59
WRMS | 2039 12 33 14 15 14 |NE 65 63 110 55 46 63
MEDI | 1500 12 32 14 14 13 |MD 48 55 51 46 43 45
Table 3.2405.2 GPS week: 2405 Day: 2 MJD: 61081
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 654 12 17 22 9 7 6 | 61 54 56 56 57 57
R03 | 3842 6 19 21 11 15 7 | 68 79 79 81 69 73
R04 | 2522 10 34 19 9 14 7 | 70 95 73 79 65 72
R05 | 1412 8 41 15 16 18 9 | 72 81 72 87 65 74
XR06 | 1166 7 748 15 --- --- 10 | 17 142 20 --- --- 15
R07 | 1873 9 49 23 13 14 9 | 64 67 56 72 57 62
R08 | 1708 5 38 23 15 18 9 | 45 65 41 53 56 48
R09 | 1459 13 60 22 8 12 10 | 13 40 38 23 27 22
R12 | 1342 22 25 13 16 8 8 | 70 74 58 67 61 64
R14 | 873 7 47 15 12 19 9 | 48 71 55 39 34 44
R15 | 2714 11 23 11 7 17 6 | 56 63 61 58 48 55
R16 | 1106 10 35 11 15 15 7 | 59 46 56 68 48 56
XR17E | 1484 10 19 15 17 --- 8 | 77 78 83 79 --- 78
R18E | 872 5 24 20 11 11 6 | 32 32 24 30 29 27
XR19E | 1237 12 44 11 --- 19 11 | 24 26 18 --- 23 19
R20E | 565 14 25 15 10 18 7 | 19 27 25 25 25 21
R21E | 2328 12 32 24 16 17 9 | 39 37 48 36 25 34
R22E | 2072 12 27 19 15 11 7 | 25 29 34 32 28 26
R24E | 2683 17 23 17 22 12 9 | 90 92 90 82 86 85
XR28E |12981 3 --- --- --- --- 0 | 88 --- --- --- --- 87
------+------------------------------------+--------------------------------
RMS | 1956 12 35 19 13 14 |T 60 63 51 56 47 59
WRMS | 1956 11 34 18 12 14 |NE 67 73 55 62 53 67
MEDI | 1459 10 32 17 13 15 |MD 59 65 56 58 48 56
Table 3.2405.3 GPS week: 2405 Day: 3 MJD: 61082
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1198 18 22 12 22 11 8 | 63 61 51 48 50 52
R03 | 1237 11 44 13 13 15 8 | 77 91 72 73 63 71
R04 | 962 9 21 17 10 8 6 | 67 69 76 69 68 69
R05 | 1779 12 55 11 14 23 10 | 64 63 73 75 54 65
XR06 | 1082 9 708 11 --- --- 10 | 35 114 33 --- --- 33
R07 | 953 11 51 12 21 25 10 | 68 90 59 82 49 65
R08 | 2743 11 61 18 9 16 10 | 48 80 48 48 50 48
R09 | 1929 6 76 11 12 11 10 | 21 48 19 23 24 20
R12 | 1955 22 47 16 16 9 9 | 50 55 27 38 31 36
R14 | 1393 11 36 9 16 10 7 | 49 63 45 34 39 42
R15 | 1336 19 26 15 8 9 7 | 55 60 46 50 45 48
R16 | 880 14 55 22 9 16 10 | 59 39 63 58 45 54
XR17E | 910 14 22 12 20 --- 9 | 71 65 71 73 --- 69
R18E | 892 8 29 16 14 12 7 | 33 43 33 40 32 33
XR19E | 1237 11 35 16 --- 19 10 | 24 23 22 --- 33 22
R20E | 695 11 45 15 9 15 8 | 19 33 25 22 27 20
R21E | 4192 18 37 10 15 21 9 | 30 37 24 34 17 24
R22E | 1896 12 40 18 15 17 9 | 17 40 25 32 23 21
R24E | 1920 23 25 27 27 12 11 | 199 214 206 215 209 206
XR28E |13780 2 --- --- --- --- 0 | 96 --- --- --- --- 96
------+------------------------------------+--------------------------------
RMS | 1831 14 44 16 15 15 |T 69 66 59 59 50 67
WRMS | 1831 14 43 15 13 15 |NE 74 67 60 54 47 71
MEDI | 1237 11 40 15 14 15 |MD 55 60 46 48 45 48
Table 3.2405.4 GPS week: 2405 Day: 4 MJD: 61083
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1894 14 33 12 18 14 8 | 50 58 44 38 38 42
R03 | 1667 11 28 19 15 15 8 | 65 70 64 56 57 60
R04 | 655 9 30 17 9 13 7 | 71 79 76 72 67 71
R05 | 1508 8 37 14 12 10 7 | 64 62 61 63 60 61
XR06 | 1089 9 716 15 --- --- 12 | 49 93 63 --- --- 54
R07 | 1412 15 28 21 18 18 9 | 58 54 41 60 36 49
R08 | 2454 7 49 14 12 30 10 | 40 63 48 43 29 39
R09 | 2921 8 51 15 10 12 8 | 27 37 31 23 34 27
R12 | 1889 17 39 24 11 12 9 | 63 66 55 52 53 55
R14 | 1062 17 47 14 20 15 10 | 52 63 41 36 33 41
R15 | 1472 9 26 15 15 12 7 | 66 68 68 54 54 61
R16 | 1469 10 30 23 9 19 8 | 63 58 72 56 50 59
XR17E | 1035 13 23 23 27 --- 12 | 60 57 64 64 --- 59
R18E | 871 7 33 13 23 8 8 | 30 34 27 39 23 28
XR19E | 1061 8 31 20 --- 16 9 | 26 37 37 --- 29 29
R20E | 782 8 38 22 13 13 8 | 20 40 36 26 23 24
R21E | 6028 15 32 12 16 13 8 | 30 39 34 33 21 27
R22E | 1653 10 29 14 16 14 7 | 23 31 31 37 24 24
R24E | 1754 23 23 30 52 18 16 | 154 165 159 175 156 158
XR28E |18616 1 --- --- --- --- 0 | 76 --- --- --- --- 75
------+------------------------------------+--------------------------------
RMS | 2210 13 36 18 19 15 |T 68 62 64 56 46 66
WRMS | 2210 12 36 16 15 15 |NE 77 65 69 53 46 73
MEDI | 1472 9 32 15 15 14 |MD 58 61 48 52 36 54
Table 3.2405.5 GPS week: 2405 Day: 5 MJD: 61084
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 2212 15 15 10 7 17 6 | 51 52 42 50 36 44
R03 | 2135 15 49 13 12 10 8 | 63 77 47 55 55 54
R04 | 999 6 44 11 10 10 7 | 70 99 71 67 73 71
R05 | 1469 8 32 14 12 8 6 | 64 68 66 57 62 62
XR06 | 992 14 740 11 --- --- 13 | 37 59 45 --- --- 40
R07 | 1109 11 40 8 12 17 7 | 61 65 58 52 48 54
R08 | 1557 12 59 15 14 21 10 | 40 74 55 50 30 44
R09 | 2306 9 56 10 11 12 8 | 22 34 20 24 18 19
R12 | 1135 9 33 12 12 10 6 | 61 75 62 72 70 65
R14 | 818 15 74 7 19 10 10 | 47 91 45 42 42 45
R15 | 1150 29 78 9 19 12 12 | 58 89 43 45 46 46
R16 | 1548 19 40 15 10 16 8 | 60 58 57 53 49 53
XR17E | 1524 29 24 30 78 --- 27 | 76 73 71 106 --- 73
R18E | 734 12 29 13 23 13 8 | 36 33 31 32 29 29
XR19E | 2029 11 31 14 --- 12 8 | 20 33 20 --- 22 19
R20E | 1041 8 44 16 15 14 8 | 16 41 24 18 18 17
R21E | 2901 16 45 21 33 19 12 | 32 45 36 40 27 28
R22E | 2053 13 36 14 22 10 8 | 17 42 24 32 23 20
R24E | 1698 23 30 14 29 37 13 | 134 142 133 142 133 134
XR26 | 8430 10 --- 7 --- --- 8 | 161 --- 25 --- --- 161
XR28E |21221 3 --- --- --- --- 0 | 90 --- --- --- --- 89
------+------------------------------------+--------------------------------
RMS | 1666 15 47 13 18 16 |T 63 65 56 57 45 61
WRMS | 1666 15 42 13 13 16 |NE 70 70 60 55 48 67
MEDI | 1548 12 40 13 14 12 |MD 58 65 45 50 42 46
Table 3.2405.6 GPS week: 2405 Day: 6 MJD: 61085
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R02 | 1938 13 27 11 21 12 7 | 71 61 68 76 62 66
R03 | 4545 12 34 21 13 20 10 | 87 90 79 83 70 79
R04 | 1744 15 20 9 18 7 6 | 99 109 100 96 93 97
R05 | 2637 12 39 16 19 16 9 | 83 85 81 72 74 78
XR06 | 1060 24 728 22 --- --- 23 | 38 215 50 --- --- 40
R07 | 1687 9 39 14 17 14 8 | 76 93 78 86 67 76
R08 | 1407 9 40 21 20 10 9 | 55 78 54 67 53 57
R09 | 1297 10 54 10 14 8 9 | 29 39 26 30 29 26
XR11 | 2918 8 48 19 11 --- 12 | 188 97 260 106 --- 182
R12 | 1329 17 19 13 12 7 6 | 78 78 77 77 73 75
R14 | 1561 8 33 18 25 12 8 | 58 79 56 49 51 54
R15 | 724 15 24 12 15 11 7 | 75 78 71 68 75 72
R16 | 2208 20 35 9 12 9 8 | 84 67 70 72 74 74
XR17E | 1867 11 34 16 51 --- 15 | 59 49 58 77 --- 56
R18E | 735 14 26 13 78 13 15 | 42 49 46 64 48 42
XR19E | 2567 13 26 13 --- 14 8 | 30 31 29 --- 39 31
R20E | 841 10 39 18 13 10 8 | 28 40 29 27 29 27
R21E | 970 36 33 15 67 15 16 | 38 37 35 60 30 29
R22E | 1188 12 39 22 33 11 10 | 19 41 29 34 19 19
R24E | 2395 18 18 15 30 27 11 | 128 132 126 136 129 128
XR26 | 9647 11 70 26 --- --- 23 | 214 32 25 --- --- 214
XR28E |19530 4 --- --- --- --- 0 | 133 --- --- --- --- 133
------+------------------------------------+--------------------------------
RMS | 1934 16 34 15 31 14 |T 77 75 68 71 59 75
WRMS | 1934 14 34 15 20 14 |NE 88 85 78 73 65 85
MEDI | 1687 12 34 15 18 12 |MD 71 78 58 72 62 66
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