[IGSREPORT-30877] Wk 2411 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 10 00:51:16 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2411 (Mar 22, 2026 - Mar 28, 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 2.2411.
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:
igl2411[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2411 in the SP3 format.
igl24117.sum Combination Report for GPS Week 2411.
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 | 7.4 ns
1 | 6.2 ns
2 | 6.6 ns
3 | 3.8 ns
4 | 6.7 ns
5 | 2.3 ns
6 | 8.0 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
4 | ESA | R06
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 1.2411, 1a.2411).
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 2.2411.0-6)
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 3.2411.0-6).
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 2411 summary. (Mar 22, 2026 - Mar 28, 2026)
Table 1.2411.a GPS week : 2411 MJD: 61121.0-61127.0
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| -2 0 3 17 0 6 .05 13 12 | 2506 -490 3915 11460
| 0 0 0 9 16 25 .04 | 480 3408
esa n/a| 0 -2 8 -29 0 15 -.09 34 33 | 5786 -868 3919 11867
| 2 1 4 13 17 43 .04 | 792 3552
gfz n/a| 0 0 -3 3 11 10 -.14 17 15 | 0 -538 3888 10967
| 1 1 4 20 14 19 .06 | 0 3564
grg n/a| 0 -1 3 -16 -7 -6 .28 18 15 | 5618 212 3699 9495
| 1 1 0 15 21 54 .07 | 888 3019
iac n/a| 1 0 -5 -11 -2 -54 -.11 21 21 | 7170 -824 3974 11843
| 1 2 2 34 35 63 .09 | 831 2396
jgx n/a| 0 0 -3 9 3 9 -.13 14 14 | 5421 141 3686 9548
| 0 1 1 11 11 15 .02 | 1208 2722
Table 1.2411.b GPS week : 2411 MJD: 61121.0-61127.0
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 | 5 6 8 8 8 7 7 |
R03 | 7 6 6 5 7 6 5 |
R04 | 7 6 6 6 8 8 7 |
R05 | 8 11 8 7 7 8 6 |
R06 | 34 35 32 29 31 29 32 |
R07 | 7 9 9 9 10 8 7 |
R08 | 11 16 23 13 10 16 18 |
R09 | 7 7 7 6 6 5 7 |
R11 | 10 6 6 7 6 6 9 |
R12 | 11 8 7 8 9 7 7 |
R14 | 9 7 6 7 8 6 7 |
R15 | 7 9 7 7 7 8 8 |
R16 | 9 8 16 11 8 9 8 |
R17 | 11 10 8 7 12 10 8 |
R18 | 8 7 8 9 9 7 8 |
R19 | 8 9 8 9 7 7 8 |
R20 | 8 8 6 6 7 7 7 |
R21 | 11 11 9 8 9 11 9 |
R22 | 6 6 9 7 7 8 7 |
R24 | 11 8 10 10 8 6 5 |
R26 | 26 29 17 21 28 21 24 |
R28 | 117 89 90 91 --- --- --- |
Table 1.2411.c GPS week : 2411 MJD: 61121.0-61127.0
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 2411 0 | -38 -63 33 -715 -896 -2323 79.4 2352 2352 | 7408 0
brd 2411 1 | 54 12 254 192 -2008 -342 79.2 2878 2878 | 6241 0
brd 2411 2 | -43 -56 395 -329 -490 -4017 76.0 2734 2734 | 6550 0
brd 2411 3 | -2 -86 212 -2497 -507 743 77.9 2574 2574 | 3755 0
brd 2411 4 | 37 -69 68 -2948 -2272 3908 77.5 2898 2898 | 6717 0
brd 2411 5 | 95 -28 178 742 741 1889 80.2 4005 4005 | 2257 0
brd 2411 6 | 114 201 132 -1172 -366 468 80.4 3779 3779 | 8028 0
-------------+------------------------------------------------------------+----------------
brd 2411 mean| 31 -12 182 -961 -828 46 78.7 3031 3031 | 5850 0
brd 2411 sdev| 62 99 121 1356 1030 2621 1.6 620 620 | 2076 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 2.2411.0 GPS week: 2411 Day: 0 MJD: 61121
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 17 29 14 .03 13 12 | 3253 1016 3461 12955
esa n/a| -1 0 15 -27 8 42 -.02 35 37 | 6608 489 3332 11774
gfz n/a| 0 0 -5 -7 12 28 -.12 16 14 | 0 911 3288 11144
grg n/a| 1 -3 3 -3 -46 -81 .31 19 17 | 6426 1157 3446 11051
iac n/a| 0 1 -5 16 17 21 -.10 21 21 | 8292 80 3429 12917
jgx n/a| 0 2 -1 17 -7 -12 -.12 16 16 | 5131 855 3469 11109
Table 2.2411.1 GPS week: 2411 Day: 1 MJD: 61122
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 5 0 0 32 .04 15 12 | 2431 -807 3003 10713
esa n/a| 0 -4 14 -34 19 43 -.12 40 36 | 7031 -1656 3020 12246
gfz n/a| -1 0 -4 9 12 30 -.15 17 15 | 0 -737 2998 10355
grg n/a| 2 -2 3 1 24 -35 .22 19 17 | 6030 -179 3134 9652
iac n/a| 2 -3 -3 -12 -36 -48 -.08 20 20 | 7705 -1529 3095 11636
jgx n/a| 0 1 -3 0 -3 -1 -.14 15 15 | 5822 -489 3166 9753
Table 2.2411.2 GPS week: 2411 Day: 2 MJD: 61123
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 19 -17 -11 .04 15 10 | 1919 2523 3047 10074
esa n/a| 0 -3 10 -48 20 5 -.15 35 34 | 5413 1933 3070 10958
gfz n/a| 0 -1 -3 2 21 -15 -.25 21 17 | 0 2488 3041 9659
grg n/a| 3 0 3 -20 -8 45 .29 24 17 | 5214 2311 3187 8343
iac n/a| 2 2 -8 -9 -41 -99 .04 29 27 | 6331 889 3204 10149
jgx n/a| 1 0 -2 11 10 13 -.10 17 17 | 5410 2598 3223 8391
Table 2.2411.3 GPS week: 2411 Day: 3 MJD: 61124
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 3 11 -15 -39 .09 12 10 | 2555 -4081 3953 11452
esa n/a| -4 -1 8 -6 -17 86 -.05 30 29 | 5333 -4083 3985 11997
gfz n/a| 2 -1 -6 -27 21 -14 -.16 18 18 | 0 -4194 3955 11068
grg n/a| 0 1 2 -16 2 71 .23 15 12 | 5823 -4128 4184 10020
iac n/a| 2 3 -7 25 -13 -58 -.07 22 22 | 5890 -1073 4160 12238
jgx n/a| 1 -2 -2 16 13 24 -.17 13 13 | 4886 -3244 4079 9877
Table 2.2411.4 GPS week: 2411 Day: 4 MJD: 61125
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 24 -11 18 .02 15 16 | 1918 1394 3441 11125
esa n/a| 2 -1 3 -34 -25 -38 -.09 34 34 | 5464 1781 3459 11849
gfz n/a| 1 -1 -5 12 20 28 -.12 16 15 | 0 1666 3429 10834
grg n/a| -2 -1 3 -46 1 -49 .21 15 13 | 5880 2389 3552 9464
iac n/a| 0 2 -5 -44 -27 -11 -.13 19 19 | 7117 723 3420 11354
jgx n/a| 0 -1 -3 25 14 6 -.14 14 14 | 5781 2042 3511 9877
Table 2.2411.5 GPS week: 2411 Day: 5 MJD: 61126
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 1 3 31 -1 30 .03 12 13 | 2625 -6138 6834 11462
esa n/a| 0 -2 5 -39 0 -12 -.11 32 33 | 5908 -6969 6846 11243
gfz n/a| 1 0 -3 40 9 9 -.11 15 14 | 0 -6574 6837 11574
grg n/a| 0 -2 2 -10 -12 13 .37 17 15 | 3789 -3607 4611 8832
iac n/a| 1 0 -1 -68 49 -169 -.18 19 18 | 7178 -5791 6836 12077
jgx n/a| 1 0 -3 -8 -14 33 -.11 12 12 | 3447 -3694 4644 8636
Table 2.2411.6 GPS week: 2411 Day: 6 MJD: 61127
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 0 2 18 10 2 .12 12 11 | 2841 2661 3666 12444
esa n/a| 1 0 4 -19 -6 -18 -.07 29 29 | 4748 2426 3721 13007
gfz n/a| 1 3 6 -3 -19 3 -.08 15 16 | 0 2670 3668 12135
grg n/a| 1 -2 2 -17 -10 -12 .36 17 13 | 6165 3542 3783 9103
iac n/a| 0 0 -6 10 32 -18 -.23 19 19 | 7680 932 3679 12531
jgx n/a| 0 0 -5 4 9 3 -.15 10 10 | 7472 2922 3711 9195
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 3.2411.0 GPS week: 2411 Day: 0 MJD: 61121
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1878 8 18 15 9 17 6 5 | 24 33 30 27 29 22 24
R03 | 1911 10 19 12 17 17 15 6 | 31 41 37 39 35 32 33
R04 | 1621 9 40 14 14 12 9 6 | 32 48 33 34 31 27 31
R05 | 1606 12 46 11 16 12 15 7 | 34 45 31 28 30 24 29
XR06 | 953 31 674 27 --- 82 --- 34 | 71 231 64 --- 87 --- 69
R07 | 1194 10 38 9 13 22 10 7 | 40 58 48 38 50 35 40
R08 | 1620 28 40 13 22 22 23 10 | 744 774 754 737 746 459 746
R09E | 2512 10 36 12 13 21 13 7 | 35 53 36 38 42 38 36
R11E | 1609 15 33 23 25 16 19 9 | 24 39 35 33 33 19 27
R12E | 1299 14 32 26 21 34 16 10 | 171 175 171 170 165 170 169
R14E | 4253 14 28 18 26 18 15 8 | 130 134 137 133 133 129 131
R15E | 2149 9 25 16 22 12 15 7 | 100 105 101 105 96 94 98
R16E | 2496 11 30 20 23 16 20 8 | 639 629 638 641 625 626 634
XR17 | 2633 8 42 18 19 26 --- 10 | 62 42 64 59 64 --- 59
R18 | 803 21 16 12 17 20 11 7 | 45 52 50 51 53 47 47
XR19 | 936 12 30 15 --- 18 14 8 | 23 25 29 --- 34 29 26
R20 | 5869 11 21 12 24 13 20 7 | 16 26 23 32 20 19 18
R21 | 807 11 66 17 20 22 20 10 | 63 32 72 79 76 54 64
R22 | 958 11 28 10 10 21 8 6 | 16 32 16 32 24 20 19
R24 | 1187 10 49 17 19 43 17 11 | 63 46 71 56 82 51 61
XR26 | 4125 13 66 47 --- 63 --- 26 | 51 80 58 --- 68 --- 55
XR28 |17645 90 --- --- --- 150 --- 116 | 42 --- --- --- 140 --- 72
------+-----------------------------------------+-------------------------------------
RMS | 2352 13 35 16 19 21 16 |T 111 128 118 129 121 105 113
WRMS | 2352 12 37 14 17 21 16 |NE 84 104 92 101 98 68 87
MEDI | 1620 11 33 15 19 20 15 |MD 42 48 50 39 53 35 47
Table 3.2411.1 GPS week: 2411 Day: 1 MJD: 61122
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1658 14 19 15 7 17 12 6 | 17 26 33 26 33 18 20
R03 | 4250 13 25 11 9 20 10 6 | 18 38 31 24 26 33 24
R04 | 1425 10 34 14 17 12 6 6 | 17 34 25 20 18 19 18
R05 | 1285 15 78 16 15 18 20 11 | 20 54 16 18 28 14 15
XR06 | 936 31 667 32 --- 83 --- 35 | 61 171 67 --- 67 --- 63
R07 | 1299 11 32 17 8 27 22 8 | 21 39 23 25 33 20 22
R08 | 2150 38 69 23 32 31 30 15 | 358 362 358 361 348 306 357
R09E | 1588 12 29 11 9 23 12 6 | 23 27 30 24 38 27 26
R11E | 1357 9 21 15 17 15 12 6 | 20 31 26 29 20 21 19
R12E | 1831 14 23 23 18 19 12 7 | 145 147 150 140 133 138 142
R14E | 5587 9 25 14 23 11 14 6 | 86 87 92 94 87 82 87
R15E | 1986 15 28 26 25 13 10 8 | 62 67 78 65 63 64 64
R16E | 3576 11 27 20 19 15 16 7 | 763 770 766 765 752 758 761
XR17 | 1052 13 44 12 13 24 --- 9 | 45 33 40 39 45 --- 40
R18 | 737 15 27 14 12 23 7 7 | 30 35 34 31 30 37 31
XR19 | 728 6 28 17 --- 30 10 9 | 12 18 16 --- 30 17 15
R20 | 6322 10 40 15 23 17 10 7 | 11 36 13 24 20 13 12
R21 | 780 9 69 14 26 20 18 10 | 33 21 43 56 46 33 38
R22 | 1924 11 29 10 13 18 10 6 | 15 21 18 29 24 17 17
R24 | 3082 12 28 16 22 23 16 8 | 36 33 37 29 38 27 31
XR26 | 5267 20 49 44 --- 80 --- 28 | 43 55 48 --- 65 --- 47
XR28 |15916 69 --- --- --- 114 --- 88 | 50 --- --- --- 73 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 2878 15 39 17 19 20 15 |T 85 100 92 99 91 91 85
WRMS | 2878 12 36 15 17 20 15 |NE 49 65 53 56 57 46 49
MEDI | 1658 12 29 15 17 20 12 |MD 30 36 34 29 38 27 31
Table 3.2411.2 GPS week: 2411 Day: 2 MJD: 61123
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 938 9 36 19 13 15 16 7 | 23 44 36 21 21 19 22
R03 | 3945 9 32 13 17 14 6 6 | 24 40 29 30 24 27 24
R04 | 1143 9 26 17 12 15 8 6 | 24 28 18 26 24 29 23
R05 | 1195 9 47 15 21 21 10 8 | 20 42 31 18 36 23 23
XR06 | 1000 31 658 15 --- 85 --- 31 | 33 193 38 --- 53 --- 36
R07 | 3518 10 27 23 8 29 20 8 | 28 37 37 25 38 27 28
R08 | 1796 44 62 46 72 43 39 22 | 553 576 569 524 555 470 549
R09E | 1920 10 34 12 14 14 9 6 | 24 28 25 26 29 24 23
R11E | 1492 10 22 14 13 18 11 6 | 19 33 22 19 31 22 20
R12E | 2035 12 32 21 12 20 8 7 | 94 114 105 98 93 94 97
R14E | 5485 8 22 14 19 17 10 6 | 57 59 57 66 55 57 57
R15E | 3466 9 31 15 15 16 12 6 | 42 43 42 50 44 38 41
R16E | 4717 20 25 29 32 77 23 15 | 708 703 719 691 680 700 700
XR17 | 932 8 31 18 14 14 --- 7 | 51 54 55 56 45 --- 51
R18 | 1171 12 27 18 16 28 14 8 | 36 41 39 34 44 26 33
XR19 | 635 10 22 15 --- 31 10 8 | 39 34 41 --- 58 49 42
R20 | 3370 7 28 14 10 17 14 6 | 14 21 11 16 22 23 14
R21 | 751 8 49 20 13 24 19 9 | 46 35 56 53 56 42 47
R22 | 1356 10 41 18 22 19 18 8 | 19 39 38 37 34 25 25
R24 | 1638 17 34 15 24 31 16 9 | 45 33 36 45 55 33 38
XR26 | 5930 14 45 24 --- 44 --- 16 | 33 34 33 --- 54 --- 34
XR28 |12035 59 --- --- --- 136 --- 90 | 38 --- --- --- 56 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2733 15 35 21 24 29 17 |T 89 106 97 101 95 96 88
WRMS | 2733 10 34 17 17 27 17 |NE 64 83 71 73 73 66 63
MEDI | 1638 10 32 17 14 20 12 |MD 33 40 38 34 44 27 33
Table 3.2411.3 GPS week: 2411 Day: 3 MJD: 61124
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1884 13 26 22 8 20 15 7 | 31 29 46 36 34 32 32
R03 | 3411 8 25 11 11 13 9 5 | 31 34 29 36 38 34 31
R04 | 1173 8 20 12 13 19 8 5 | 30 37 28 27 23 32 28
R05 | 2418 10 36 11 11 24 11 7 | 30 41 29 29 26 29 28
XR06 | 894 28 580 22 --- 73 --- 28 | 23 198 43 --- 48 --- 31
R07 | 3084 9 30 22 13 30 20 8 | 40 31 45 43 54 34 39
XR08 | 1824 22 61 23 15 20 --- 13 | 386 404 383 389 388 --- 388
R09E | 2228 14 17 10 9 20 13 6 | 26 36 27 28 36 27 26
R11E | 2627 13 24 15 12 18 13 6 | 22 35 31 35 30 23 26
R12E | 2156 10 39 19 15 23 13 8 | 169 183 179 163 175 167 170
R14E | 4550 8 26 16 23 11 12 7 | 45 60 54 46 50 50 46
R15E | 3050 10 35 12 21 14 10 7 | 46 50 50 62 45 42 47
R16E | 3577 25 23 14 24 46 16 11 | 892 885 888 890 869 881 886
XR17 | 1212 11 34 8 8 10 --- 6 | 37 29 34 36 34 --- 33
R18 | 1640 13 29 19 19 26 20 8 | 37 53 44 35 48 29 36
XR19 | 705 10 31 23 --- 22 11 8 | 24 31 29 --- 30 28 25
R20 | 1201 11 23 16 13 16 11 6 | 20 28 27 25 24 23 20
R21 | 1647 8 49 14 10 18 10 7 | 51 50 59 56 60 50 52
R22 | 2545 9 31 14 20 20 6 7 | 18 34 20 38 25 27 21
R24 | 1187 12 29 36 12 19 18 9 | 53 49 84 59 51 47 56
XR26 | 8782 17 42 24 --- 67 --- 20 | 37 54 39 --- 49 --- 40
XR28 |12750 57 --- --- --- 142 --- 90 | 97 --- --- --- 150 --- 75
------+-----------------------------------------+-------------------------------------
RMS | 2573 12 30 18 15 22 13 |T 97 111 103 112 103 91 97
WRMS | 2573 10 29 18 12 22 13 |NE 59 73 62 67 67 33 58
MEDI | 2156 11 30 16 13 20 12 |MD 37 41 43 36 45 32 33
Table 3.2411.4 GPS week: 2411 Day: 4 MJD: 61125
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1549 18 26 11 16 32 12 8 | 26 24 32 43 45 26 31
R03 | 2090 11 21 21 15 19 5 6 | 24 34 30 29 28 23 24
R04 | 1131 27 28 13 8 13 10 7 | 25 35 27 24 25 28 23
R05 | 2427 23 22 12 9 22 7 7 | 23 32 21 22 26 17 18
XR06 | 1013 36 594 26 --- 68 --- 31 | 36 152 48 --- 50 --- 40
R07 | 2695 13 64 15 14 28 13 10 | 23 44 23 28 39 26 26
R08 | 2928 23 50 19 10 12 21 9 | 197 211 196 204 199 342 202
R09E | 931 8 27 13 8 16 10 5 | 25 41 23 25 34 25 24
R11E | 2674 10 28 13 11 12 13 6 | 19 31 25 21 24 21 20
R12E | 2055 15 18 20 12 32 16 8 | 142 137 147 136 110 130 134
R14E | 1693 12 23 16 26 13 11 7 | 58 67 67 65 60 65 61
R15E | 1972 11 26 16 22 15 11 7 | 59 67 58 64 54 54 57
R16E | 7371 20 37 9 23 12 12 8 | 420 411 408 401 414 405 409
XR17 | 1812 10 54 24 8 25 --- 11 | 51 41 62 59 53 --- 53
R18 | 1003 13 19 24 20 15 23 9 | 39 49 51 35 51 33 39
XR19 | 1058 7 22 14 --- 10 13 6 | 33 33 35 --- 33 42 34
R20 | 1064 7 32 11 16 19 14 7 | 24 30 24 21 31 38 24
R21 | 2771 9 58 10 14 24 15 9 | 47 24 49 51 56 44 46
R22 | 5139 10 32 13 12 12 16 6 | 13 30 18 24 23 15 15
R24 | 1843 8 31 23 11 13 18 7 | 43 35 54 58 42 36 44
XR26 |>>>>> 30 54 37 --- 74 --- 27 | 28 50 36 --- 46 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 2897 15 34 16 15 19 14 |T 64 75 68 72 68 76 64
WRMS | 2897 16 34 15 13 19 14 |NE 42 54 47 49 49 55 43
MEDI | 1972 12 28 15 12 16 13 |MD 33 41 36 35 45 33 34
Table 3.2411.5 GPS week: 2411 Day: 5 MJD: 61126
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 954 14 21 12 9 26 7 6 | 23 30 31 33 30 28 26
R03 | 4219 9 15 13 9 24 10 6 | 22 32 28 28 24 24 23
R04 | 1112 24 22 19 14 18 8 8 | 22 29 31 29 17 24 22
R05 | 1895 18 42 12 10 17 12 7 | 21 23 23 23 16 23 19
XR06 | 1179 34 618 25 --- 64 --- 29 | 49 118 54 --- 50 --- 48
R07 | 3519 10 47 11 18 20 12 8 | 25 34 22 27 23 23 22
XR08 | 6263 30 71 17 23 22 --- 15 | 185 200 187 184 183 --- 186
R09E | 1600 8 26 11 9 11 9 5 | 37 38 37 37 35 39 36
R11E | 2907 11 24 11 13 15 10 5 | 23 26 26 26 29 20 22
R12E | 1506 7 22 18 12 17 15 6 | 222 234 229 227 220 218 224
R14E | 1917 7 21 14 23 14 10 6 | 85 93 86 91 88 82 85
R15E | 1066 9 22 18 29 25 11 8 | 65 64 65 85 56 63 64
R16E |11702 19 27 17 26 14 18 9 | 602 596 595 598 596 593 597
XR17 | 2626 11 39 12 27 19 --- 10 | 39 39 47 55 39 --- 41
R18 | 882 11 14 19 19 16 16 7 | 36 36 35 43 43 30 34
XR19 | 1082 7 18 15 --- 19 11 6 | 34 38 25 --- 30 34 30
R20 | 1431 9 33 17 12 14 12 6 | 32 34 42 29 23 34 30
R21 | 2436 8 74 16 22 30 8 11 | 38 38 35 52 49 41 38
R22 | 6684 9 35 16 15 23 12 7 | 19 34 25 30 34 24 22
R24 | 3493 8 20 15 14 17 12 6 | 30 32 31 36 31 31 29
XR26 |>>>>> 27 41 15 --- 58 --- 20 | 21 28 30 --- 31 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 4005 12 32 15 17 19 12 |T 77 85 80 90 78 78 77
WRMS | 4005 13 33 14 15 18 12 |NE 39 49 43 47 41 28 39
MEDI | 1917 10 26 15 14 19 11 |MD 34 36 35 36 34 31 30
Table 3.2411.6 GPS week: 2411 Day: 6 MJD: 61127
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 728 7 14 19 15 26 11 7 | 43 38 45 44 47 44 42
R03 | 4267 8 15 12 7 20 8 5 | 43 42 41 42 45 38 40
R04 | 960 16 20 10 12 23 12 6 | 40 44 31 34 38 34 34
R05 | 1500 13 22 8 10 22 9 6 | 41 53 35 40 38 34 36
XR06 | 1079 28 680 26 --- 77 --- 31 | 67 193 65 --- 94 --- 70
R07 | 4929 11 42 10 20 16 7 7 | 47 51 43 50 54 50 46
XR08 | 8083 28 75 29 28 24 --- 17 | 383 412 387 388 390 --- 389
R09E | 1429 11 31 15 9 12 13 6 | 23 32 26 30 30 27 25
XR11E | 2106 11 36 18 8 18 --- 8 | 36 45 44 40 43 --- 38
R12E | 1591 10 28 10 13 24 11 6 | 195 206 196 194 187 186 192
R14E | 1475 7 20 14 30 14 11 7 | 156 154 158 160 159 154 156
R15E | 1115 12 23 15 31 24 9 8 | 106 113 107 108 107 104 105
R16E |10246 17 31 15 24 15 8 7 | 604 611 613 620 607 606 609
XR17 | 2774 10 31 13 16 13 --- 7 | 59 48 57 64 52 --- 56
R18 | 1485 13 16 17 26 18 12 7 | 51 65 58 63 62 50 54
XR19 | 1105 9 20 22 --- 20 14 8 | 42 41 41 --- 47 45 41
R20 | 2217 10 34 17 10 17 10 6 | 36 45 42 36 40 34 36
R21 | 1187 14 55 21 10 15 15 9 | 66 43 70 70 72 60 63
R22 | 3966 9 38 19 9 16 9 7 | 24 35 33 36 34 31 28
R24 | 5549 10 20 9 7 12 5 4 | 58 49 67 62 61 51 57
XR26 |12033 35 56 20 --- 60 --- 24 | 47 57 63 --- 66 --- 52
------+-----------------------------------------+-------------------------------------
RMS | 3779 12 29 15 17 19 10 |T 103 113 105 115 108 96 103
WRMS | 3779 11 29 16 13 19 10 |NE 69 81 71 77 76 42 69
MEDI | 1591 11 31 15 12 18 10 |MD 47 49 57 50 54 45 52
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