[IGSREPORT-30901] Wk 2413 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 24 00:28:07 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2413 (Apr 05, 2026 - Apr 11, 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 2.2413.
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:
igl2413[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2413 in the SP3 format.
igl24137.sum Combination Report for GPS Week 2413.
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 | 4.3 ns
1 | 6.8 ns
2 | 5.4 ns
3 | 7.9 ns
4 | 3.0 ns
5 | 3.4 ns
6 | 5.7 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 | ESA | R06
1 | ESA | R06
2 | ESA | R06
3 | ESA | R06
3 | GRG | R12
4 | 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 1.2413, 1a.2413).
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 2.2413.0-6)
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 3.2413.0-6).
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 2413 summary. (Apr 05, 2026 - Apr 11, 2026)
Table 1.2413.a GPS week : 2413 MJD: 61135.0-61141.0
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 3 14 3 2 .09 14 14 | 2286 -444 3444 9681
| 0 1 1 13 7 16 .04 | 1265 3136
esa n/a| -2 -1 9 -5 -6 23 .00 30 29 | 3861 -850 3485 10151
| 2 2 3 21 17 23 .04 | 1591 2989
gfz n/a| 0 0 0 35 5 0 -.15 15 14 | 0 -768 3441 9405
| 1 1 2 20 16 29 .06 | 0 3108
grg n/a| 1 0 2 -47 -8 -32 .27 23 14 | 5386 -673 3581 9270
| 1 0 1 16 7 28 .06 | 670 3032
iac n/a| 1 0 -5 4 2 -24 -.06 18 18 | 6650 -796 3441 10033
| 1 1 3 25 20 54 .05 | 1344 1785
jgx n/a| 0 0 -5 4 1 24 -.12 14 14 | 5655 -874 3639 9826
| 0 0 1 9 15 22 .03 | 1501 3227
Table 1.2413.b GPS week : 2413 MJD: 61135.0-61141.0
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 6 5 6 6 5 |
R03 | 7 7 6 5 8 6 6 |
R04 | 8 6 8 6 7 6 6 |
R05 | 7 6 5 7 6 6 5 |
R06 | 32 34 34 34 23 26 34 |
R07 | 6 7 6 7 6 6 5 |
R08 | 11 11 12 11 10 9 11 |
R09 | 6 8 6 7 7 7 6 |
R11 | 9 9 7 6 6 7 7 |
R12 | 7 6 7 24 9 7 6 |
R14 | 8 7 7 7 7 6 6 |
R15 | 8 7 8 7 9 6 6 |
R16 | 7 9 9 8 8 8 8 |
R17 | 7 7 6 7 10 9 6 |
R18 | 7 7 7 8 8 8 6 |
R19 | 7 6 7 6 7 7 6 |
R20 | 6 6 6 7 6 5 7 |
R21 | 11 9 10 9 9 7 9 |
R22 | 9 6 5 6 7 7 7 |
R24 | 7 6 8 6 7 8 5 |
R26 | 23 31 26 32 28 28 26 |
Table 1.2413.c GPS week : 2413 MJD: 61135.0-61141.0
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 2413 0 | -185 -18 55 -623 -3780 9403 77.3 3720 3720 | 4275 0
brd 2413 1 | 48 -98 75 2656 -891 10020 79.2 1821 1821 | 6766 0
brd 2413 2 | 89 -55 140 1426 91 14830 78.2 1612 1612 | 5377 0
brd 2413 3 | 48 36 88 287 1018 15250 77.4 2025 2025 | 7884 0
brd 2413 4 | -67 48 -18 4 941 13650 79.3 2591 2591 | 3041 0
brd 2413 5 | -11 45 -21 -1098 1621 11790 79.8 2383 2383 | 3392 0
brd 2413 6 | 113 -31 150 3504 2817 7508 81.7 2050 2050 | 5728 0
-------------+------------------------------------------------------------+----------------
brd 2413 mean| 5 -10 67 879 259 11778 79.0 2314 2314 | 5209 0
brd 2413 sdev| 103 56 68 1714 2125 2939 1.5 700 700 | 1767 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 2.2413.0 GPS week: 2413 Day: 0 MJD: 61135
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -2 7 13 0 23 .07 13 14 | 1533 -1895 3727 10472
esa n/a| -2 -1 12 10 -16 -18 -.06 35 35 | 4234 -2383 3765 10689
gfz n/a| 0 0 -1 36 -11 12 -.24 14 11 | 0 -2475 3716 10218
grg n/a| 1 0 3 -32 0 -78 .32 14 13 | 5056 -1659 3913 10211
iac n/a| 3 0 -10 38 29 72 .01 23 24 | 7275 -2750 3711 10854
jgx n/a| 0 0 -6 -3 -21 25 -.10 14 14 | 4616 -2591 3926 10932
Table 2.2413.1 GPS week: 2413 Day: 1 MJD: 61136
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 1 14 3 9 .04 13 12 | 2709 1507 3084 9193
esa n/a| -3 -2 10 19 -16 19 -.00 33 33 | 6403 -1011 3139 9153
gfz n/a| 1 1 0 64 -18 20 -.18 16 16 | 0 1087 3079 9074
grg n/a| 2 0 1 -36 0 -7 .22 14 12 | 6141 828 3249 9171
iac n/a| 0 -1 -6 -24 -15 -74 -.05 19 18 | 8406 -645 3088 9754
jgx n/a| -1 1 -5 -6 0 43 -.10 13 13 | 5425 1411 3281 9688
Table 2.2413.2 GPS week: 2413 Day: 2 MJD: 61137
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 2 29 9 -27 .10 14 14 | 1795 -938 3376 8605
esa n/a| -2 -5 13 -7 17 18 .07 34 32 | 4008 -2210 3395 8844
gfz n/a| 1 0 0 25 4 -48 -.20 16 16 | 0 -1031 3376 8184
grg n/a| 0 1 3 -68 -14 -3 .33 15 12 | 5568 -958 3524 7678
iac n/a| 0 -2 -2 8 4 7 -.04 14 14 | 6167 -1043 3370 8851
jgx n/a| 0 0 -5 9 10 33 -.12 13 13 | 5542 -1050 3642 8150
Table 2.2413.3 GPS week: 2413 Day: 3 MJD: 61138
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 21 9 0 .11 14 11 | 3729 4328 3784 10227
esa n/a| 2 -2 9 -33 19 19 .01 38 34 | 4658 3368 3819 11418
gfz n/a| 0 1 0 8 7 -17 -.16 13 14 | 0 4075 3787 9944
grg n/a| -1 1 3 -49 -19 -17 .18 69 14 | 5735 3668 3889 9488
iac n/a| 0 0 -4 -3 10 -15 -.04 17 16 | 8160 1295 3788 10553
jgx n/a| 0 -1 -6 -5 -3 20 -.11 26 26 | 7314 3938 3967 10136
Table 2.2413.4 GPS week: 2413 Day: 4 MJD: 61139
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 -14 -11 5 .14 15 16 | 3962 -1795 3210 10771
esa n/a| -1 2 9 16 -17 57 -.03 32 33 | 3989 -1425 3241 11704
gfz n/a| 0 -1 4 56 21 -7 -.14 12 10 | 0 -2569 3203 10466
grg n/a| 2 0 3 -72 -12 -51 .32 18 15 | 4355 -2968 3346 10379
iac n/a| 3 0 -5 -10 0 -78 -.11 19 20 | 5797 -1413 3208 11002
jgx n/a| -1 0 -5 14 12 54 -.10 11 11 | 8004 -3156 3414 11087
Table 2.2413.5 GPS week: 2413 Day: 5 MJD: 61140
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 4 21 10 13 .14 13 13 | 1880 -5504 3807 8883
esa n/a| -3 -3 5 -21 -12 31 -.02 17 16 | 1919 -5090 3874 9299
gfz n/a| 1 0 2 17 4 -3 -.08 17 18 | 0 -5440 3807 8680
grg n/a| 1 0 2 -40 -7 -53 .28 17 17 | 6057 -5360 3977 8858
iac n/a| 1 -1 -8 37 16 -19 -.07 16 15 | 4714 -2780 3811 9311
jgx n/a| 0 0 -4 5 -10 0 -.15 11 11 | 4926 -5626 3998 9281
Table 2.2413.6 GPS week: 2413 Day: 6 MJD: 61141
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 4 14 2 -9 .05 14 16 | 398 1188 3122 9620
esa n/a| -4 -1 3 -22 -21 37 .04 20 17 | 1822 2795 3162 9951
gfz n/a| 3 0 -1 42 27 42 -.06 16 14 | 0 971 3119 9272
grg n/a| 0 -1 0 -35 -3 -15 .27 13 12 | 4791 1733 3175 9108
iac n/a| 0 2 -1 -15 -32 -65 -.16 17 16 | 6032 1761 3113 9908
jgx n/a| 0 0 -2 17 24 -10 -.18 11 11 | 3761 954 3247 9509
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 3.2413.0 GPS week: 2413 Day: 0 MJD: 61135
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 738 8 19 10 12 31 7 6 | 61 61 63 63 68 62 62
R03 | 1396 12 21 10 9 33 17 7 | 64 77 73 74 83 62 69
R04 | 826 9 25 15 9 18 25 7 | 66 76 66 65 63 55 62
R05 | 2999 13 29 10 14 31 9 7 | 57 63 53 59 49 51 53
XR06 | 967 26 614 21 --- 91 --- 31 | 24 128 38 --- 93 --- 41
R07 | 2483 10 33 9 11 14 8 5 | 61 68 63 65 58 62 62
R08 | 5242 23 74 14 15 13 13 10 | 44 99 55 59 50 53 53
R09E | 1187 12 30 9 11 15 14 6 | 57 64 54 53 56 57 55
R11E | 2407 14 36 17 24 15 11 8 | 41 66 42 63 42 50 47
R12E | 1493 9 25 16 15 10 12 6 | 772 769 773 778 773 764 773
R14E | 3188 11 19 18 22 17 11 7 | 43 50 45 62 42 45 46
XR15E | 2088 13 24 14 17 14 --- 7 | 54 62 58 64 58 --- 57
R16E |11953 13 35 11 18 14 13 7 | 140 150 141 146 136 141 141
XR17 | 1412 8 28 9 15 12 --- 6 | 43 38 41 48 42 --- 42
R18 | 774 18 16 10 16 17 15 7 | 40 43 42 47 42 34 40
XR19 | 1060 11 18 17 --- 18 9 7 | 19 26 33 --- 32 27 24
R20 | 1512 7 35 9 8 27 8 6 | 26 32 27 29 47 27 27
R21 | 1063 9 60 8 14 39 23 10 | 51 37 49 53 59 44 47
R22 | 1452 21 29 25 11 24 7 8 | 23 30 50 34 46 32 31
R24 | 2647 9 24 18 11 20 9 6 | 49 42 53 45 54 46 47
XR26 | 7801 25 72 28 --- 59 --- 23 | 35 60 55 --- 80 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 3720 13 35 14 14 23 14 |T 84 97 89 100 93 94 87
WRMS | 3720 14 35 11 13 24 14 |NE 44 58 50 53 57 46 47
MEDI | 1493 12 29 14 14 18 11 |MD 49 62 53 59 56 51 49
Table 3.2413.1 GPS week: 2413 Day: 1 MJD: 61136
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 591 12 17 26 10 31 14 8 | 45 45 64 51 62 49 51
R03 | 1873 10 26 16 10 22 15 7 | 45 50 59 53 61 43 50
R04 | 1178 11 23 10 14 11 14 6 | 47 56 49 51 43 42 46
R05 | 2439 12 24 13 7 14 10 5 | 42 48 42 40 29 33 37
XR06 | 1062 30 605 26 --- 82 --- 33 | 31 133 29 --- 57 --- 30
R07 | 1740 12 39 18 12 16 10 7 | 37 56 40 45 32 37 38
R08 | 2706 25 62 15 13 16 18 10 | 31 54 33 34 21 33 29
R09E | 2410 11 51 15 10 12 10 7 | 23 62 30 29 31 31 28
R11E | 1736 13 20 17 28 18 13 8 | 16 33 23 39 19 20 19
R12E | 1542 10 25 15 10 19 13 6 | 649 655 652 646 648 644 650
R14E | 2398 11 22 12 18 15 11 6 | 26 35 28 38 27 26 27
XR15E | 1394 8 20 9 18 17 --- 7 | 36 37 41 49 45 --- 41
R16E | 2219 19 26 23 20 18 14 8 | 79 89 87 91 80 77 82
XR17 | 1153 10 18 20 12 13 --- 7 | 23 27 21 25 16 --- 19
R18 | 944 13 23 10 15 16 14 6 | 29 38 32 33 22 25 27
XR19 | 857 11 12 13 --- 12 9 5 | 15 20 17 --- 19 17 13
R20 | 1480 9 32 14 8 15 8 5 | 17 25 32 25 29 22 21
R21 | 1476 10 53 13 11 27 18 9 | 25 19 27 26 22 20 20
R22 | 922 7 23 15 10 16 10 5 | 20 31 20 28 23 21 19
R24 | 1873 6 19 16 11 23 12 6 | 26 24 30 25 29 26 24
XR26 | 9435 27 --- 26 --- 74 --- 30 | 35 --- 40 --- 49 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1821 13 33 16 14 19 13 |T 61 76 66 73 64 68 62
WRMS | 1821 12 33 16 12 18 13 |NE 31 44 35 36 34 30 30
MEDI | 1542 11 23 15 11 16 13 |MD 31 38 32 38 29 31 29
Table 3.2413.2 GPS week: 2413 Day: 2 MJD: 61137
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 526 14 25 11 10 14 8 5 | 55 62 49 56 50 51 52
R03 | 2037 11 20 15 12 12 8 5 | 47 58 55 52 57 54 52
R04 | 1291 14 28 22 21 11 16 8 | 48 60 61 51 53 43 49
R05 | 1624 8 24 14 11 12 8 5 | 46 55 52 50 55 47 49
XR06 | 1125 40 595 34 --- 62 --- 34 | 31 147 30 --- 67 --- 40
R07 | 1461 10 24 16 14 9 8 5 | 43 45 38 38 36 33 36
R08 | 1241 27 65 25 22 12 26 12 | 36 70 32 48 43 51 41
R09E | 2156 11 24 15 18 11 9 6 | 21 26 17 31 27 25 21
R11E | 1737 14 33 13 16 8 9 6 | 23 35 25 27 24 27 23
R12E | 1688 9 32 16 16 12 10 6 | 631 630 639 634 634 627 632
R14E | 2052 17 32 12 16 16 12 7 | 26 45 38 43 34 29 31
XR15E | 1745 9 28 17 18 10 --- 7 | 34 34 32 31 33 --- 30
R16E | 2167 14 30 17 25 15 16 8 | 49 45 47 50 49 40 43
XR17 | 997 6 27 12 9 10 --- 5 | 31 29 36 34 28 --- 30
R18 | 1227 17 17 15 9 21 7 6 | 26 27 31 30 30 28 26
XR19 | 1203 11 29 14 --- 13 12 7 | 16 33 18 --- 20 26 19
R20 | 1368 12 29 13 15 10 10 6 | 21 36 27 25 25 28 24
R21 | 1891 11 67 20 12 17 19 10 | 35 34 38 35 31 24 29
R22 | 1108 11 30 9 8 10 5 5 | 16 30 21 27 22 23 20
R24 | 1245 12 28 21 10 20 15 7 | 36 42 41 39 52 39 40
XR26 | 5601 39 53 31 --- 56 --- 26 | 27 56 33 --- 57 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1612 14 34 16 15 14 13 |T 61 76 64 72 67 70 63
WRMS | 1612 14 32 16 12 14 13 |NE 34 52 37 40 41 37 36
MEDI | 1461 12 29 15 14 12 10 |MD 34 45 36 38 36 33 36
Table 3.2413.3 GPS week: 2413 Day: 3 MJD: 61138
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 625 7 17 10 5 11 12 4 | 37 45 40 38 30 41 36
R03 | 1314 7 34 7 10 10 8 5 | 53 70 53 60 49 54 54
R04 | 823 10 29 11 15 10 10 5 | 47 63 50 42 50 43 47
R05 | 2939 11 49 13 14 9 11 6 | 50 82 47 47 49 44 48
XR06 | 1128 32 597 33 --- 73 --- 33 | 26 146 49 --- 64 --- 38
R07 | 2075 11 39 8 14 16 14 6 | 58 57 52 62 61 46 54
R08 | 1028 21 42 14 14 33 29 11 | 40 65 51 49 60 33 43
R09E | 2067 12 30 14 19 16 12 7 | 22 28 19 27 27 23 19
R11E | 2781 9 25 14 12 11 10 5 | 19 32 21 23 25 22 19
R12E | 4029 30 43 21 271 32 86 23 | 9999 9999 9999 9999 9999 9999 9999
R14E | 1803 16 28 13 20 8 11 6 | 32 43 33 43 31 28 30
XR15E | 1727 9 21 13 22 9 --- 7 | 32 32 35 39 35 --- 32
R16E | 2378 11 32 15 26 21 10 8 | 38 46 43 53 35 36 38
XR17 | 1371 8 27 11 14 16 --- 6 | 30 29 22 29 31 --- 26
R18 | 1220 13 23 9 14 24 19 7 | 27 33 31 28 33 19 26
XR19 | 1165 10 24 8 --- 15 12 6 | 9 18 14 --- 23 22 13
R20 | 2104 9 43 14 15 10 12 6 | 12 44 17 18 20 19 13
R21 | 1975 9 72 20 17 9 14 9 | 31 34 48 46 33 33 36
R22 | 1079 10 27 14 11 11 15 6 | 12 24 17 25 20 23 15
R24 | 815 11 34 8 9 13 16 6 | 31 44 28 30 29 27 27
XR26 | 4681 38 72 38 --- 81 --- 32 | 19 73 31 --- 74 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2025 14 38 13 69 17 26 |T 31 50 35 38 38 32 32
WRMS | 2025 11 34 14 14 16 26 |NE 32 55 36 39 41 33 34
MEDI | 1727 11 32 13 14 13 12 |MD 31 44 33 39 33 28 32
Table 3.2413.4 GPS week: 2413 Day: 4 MJD: 61139
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 735 11 33 15 11 9 9 6 | 55 61 66 64 53 58 58
R03 | 2842 11 26 9 25 24 11 7 | 52 59 56 69 41 48 52
R04 | 864 18 30 6 20 18 10 7 | 56 68 49 49 44 44 48
R05 | 3730 15 19 10 9 14 12 5 | 52 50 50 47 46 40 45
XR06 | 1060 30 592 15 --- 53 --- 23 | 25 218 37 --- 44 --- 31
R07 | 2932 9 31 13 11 17 12 6 | 58 70 67 59 67 54 60
R08 | 1800 34 44 12 19 16 12 9 | 43 71 56 58 59 54 53
R09E | 1307 14 20 11 17 25 9 6 | 37 36 40 37 39 35 35
R11E | 1931 12 21 8 14 13 12 5 | 34 36 35 31 34 36 33
R12E | 4581 13 28 16 25 32 10 8 | 693 688 688 705 688 687 689
R14E | 4462 14 23 13 24 16 7 7 | 35 43 39 46 32 35 35
XR15E | 2796 10 31 13 19 19 --- 8 | 41 49 42 47 39 --- 40
R16E | 2417 17 27 14 25 16 12 7 | 79 80 81 76 75 70 75
XR17 | 2210 16 24 20 15 24 --- 9 | 29 25 35 25 31 --- 25
R18 | 1113 15 28 11 16 27 15 7 | 27 32 26 26 33 28 25
XR19 | 1101 8 28 13 --- 19 9 7 | 18 23 23 --- 27 23 21
R20 | 3663 9 34 11 11 18 11 6 | 24 39 29 24 33 37 28
R21 | 1802 8 67 10 12 23 7 8 | 30 32 31 37 35 32 30
R22 | 1106 11 32 16 16 8 9 6 | 21 35 26 28 24 26 22
R24 | 982 14 19 8 11 20 16 6 | 31 32 30 33 32 29 28
XR26 | 5943 28 52 34 --- 83 --- 28 | 32 48 27 --- 70 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2590 15 32 12 18 19 11 |T 70 85 73 81 73 78 69
WRMS | 2590 16 33 10 15 20 11 |NE 36 57 40 43 42 39 37
MEDI | 1931 14 28 13 16 19 11 |MD 35 48 39 46 39 37 35
Table 3.2413.5 GPS week: 2413 Day: 5 MJD: 61140
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 949 9 13 18 10 12 10 5 | 59 53 55 60 55 54 54
R03 | 3133 12 8 8 12 22 5 5 | 36 32 35 36 34 32 32
R04 | 657 13 6 17 14 15 8 5 | 48 44 34 52 41 41 42
R05 | 2763 14 16 7 7 14 13 5 | 41 48 40 44 42 44 42
XR06 | 1079 33 --- 19 --- 51 --- 26 | 21 --- 37 --- 40 --- 28
R07 | 2165 7 22 18 12 15 8 6 | 40 38 49 33 43 36 37
R08 | 2430 25 29 17 10 21 9 8 | 28 38 43 32 21 38 32
R09E | 2279 12 17 18 25 17 8 7 | 23 35 21 30 34 24 23
R11E | 1786 15 10 18 20 12 11 6 | 18 20 25 25 23 20 18
R12E | 5175 14 16 14 20 15 9 6 | 680 674 680 653 673 665 674
R14E | 3153 11 16 13 16 10 8 5 | 29 33 29 32 26 26 26
R15E | 2187 8 15 19 18 17 9 6 | 32 33 39 40 35 23 31
R16E | 1343 15 17 15 28 20 12 8 | 79 85 85 86 83 83 82
XR17 | 1503 9 18 25 18 14 --- 8 | 26 21 42 21 26 --- 24
R18 | 1201 17 23 18 10 15 19 8 | 23 24 18 25 23 21 19
XR19 | 970 7 16 19 --- 15 11 6 | 16 23 13 --- 21 21 15
R20 | 2626 13 15 13 7 8 11 5 | 19 24 19 21 21 19 17
R21 | 2155 6 21 15 10 25 9 6 | 26 43 31 34 24 24 25
R22 | 1064 12 8 21 25 15 8 7 | 17 23 26 24 19 17 16
R24 | 1160 6 23 31 17 9 19 8 | 31 22 34 31 32 39 29
XR26 | 5468 40 45 42 --- 63 --- 27 | 33 55 34 --- 49 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 2383 13 17 17 17 16 11 |T 63 68 66 71 65 68 62
WRMS | 2383 13 16 18 17 15 11 |NE 30 34 34 34 32 32 30
MEDI | 2155 12 16 18 14 15 9 |MD 29 33 34 32 34 26 29
Table 3.2413.6 GPS week: 2413 Day: 6 MJD: 61141
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 750 9 11 9 10 17 10 5 | 77 76 74 78 77 70 74
R03 | 1715 11 13 15 11 19 6 5 | 68 70 69 74 64 62 66
R04 | 1260 21 12 15 6 18 6 6 | 69 77 62 68 64 58 64
R05 | 1085 13 17 12 8 11 8 5 | 66 71 62 65 65 60 63
XR06 | 1108 33 --- 30 --- 74 --- 34 | 32 --- 36 --- 88 --- 45
R07 | 1135 8 27 9 8 11 7 5 | 74 71 72 72 76 70 72
R08 | 2591 36 37 18 18 22 14 11 | 61 93 74 64 58 71 66
R09E | 2917 8 14 14 11 22 11 6 | 30 35 32 35 32 30 30
R11E | 2458 9 13 16 21 15 14 7 | 22 25 30 27 28 22 22
R12E | 3045 8 17 18 17 13 7 6 | 781 783 792 769 785 773 781
R14E | 1982 9 18 12 15 15 6 5 | 29 35 32 35 26 25 27
R15E | 1652 8 15 17 14 14 11 5 | 45 41 50 47 42 20 42
R16E | 1953 17 29 17 16 15 9 7 | 108 120 116 122 112 108 113
XR17 | 1184 7 19 16 11 8 --- 6 | 39 28 44 39 38 --- 37
R18 | 1445 14 21 10 12 14 9 6 | 30 36 31 31 36 28 30
XR19 | 1195 8 18 12 --- 13 10 6 | 14 19 15 --- 22 21 16
R20 | 1951 12 21 15 13 12 15 6 | 27 22 26 28 29 30 25
R21 | 3379 9 27 28 10 23 20 9 | 42 40 54 49 48 34 41
R22 | 1688 7 13 25 15 19 11 7 | 12 22 26 25 23 17 15
R24 | 1637 11 17 13 8 15 9 5 | 47 40 40 44 47 48 43
XR26 | 7911 35 50 40 --- 57 --- 26 | 32 72 45 --- 83 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 2049 14 20 16 13 17 11 |T 81 88 84 92 87 85 81
WRMS | 2049 16 17 14 12 16 11 |NE 46 52 48 53 54 47 46
MEDI | 1688 9 17 15 11 15 9 |MD 42 40 45 47 48 34 43
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