[IGSREPORT-30870] Wk 2410 IGLOS Final Orbits
acc
acc at igs.org
Sat Apr 4 02:09:26 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2410 (Mar 15, 2026 - Mar 21, 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 2.2410.
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:
igl2410[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2410 in the SP3 format.
igl24107.sum Combination Report for GPS Week 2410.
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 | 6.4 ns
1 | 6.9 ns
2 | 4.1 ns
3 | 5.1 ns
4 | 5.8 ns
5 | 6.2 ns
6 | 6.4 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 1.2410, 1a.2410).
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 2.2410.0-6)
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 3.2410.0-6).
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 2410 summary. (Mar 15, 2026 - Mar 21, 2026)
Table 1.2410.a GPS week : 2410 MJD: 61114.0-61120.0
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 1 1 8 -6 6 .13 13 13 | 2662 -221 3335 9540
| 0 0 1 21 17 24 .06 | 1088 2195
esa n/a| -1 -2 4 -25 -2 7 -.06 34 32 | 7728 -519 3334 10074
| 1 1 4 23 15 50 .05 | 2523 2163
gfz n/a| 1 0 -4 -2 8 31 -.18 15 14 | 0 -280 3284 9249
| 1 1 2 15 14 43 .05 | 0 1963
grg n/a| 0 0 6 -9 -20 -19 .26 23 16 | 5646 75 3356 9145
| 1 1 2 10 28 30 .04 | 636 2210
iac n/a| 0 0 -5 -6 3 -14 -.10 16 16 | 7153 -349 3603 10329
| 1 1 2 21 31 45 .06 | 1091 1189
jgx n/a| 0 0 0 10 8 1 -.03 15 15 | 4741 -44 3379 9714
| 1 1 3 14 18 32 .04 | 1111 2431
Table 1.2410.b GPS week : 2410 MJD: 61114.0-61120.0
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 7 8 6 8 7 |
R03 | 7 6 5 7 5 6 8 |
R04 | 5 7 8 6 6 5 6 |
R05 | 8 6 8 8 8 8 8 |
R06 | 37 31 25 30 39 38 31 |
R07 | 7 7 7 7 7 8 8 |
R08 | 9 10 7 8 13 12 11 |
R09 | 6 7 8 12 7 6 7 |
R11 | 6 6 7 7 11 10 7 |
R12 | 7 6 7 7 8 11 7 |
R14 | 8 7 6 10 15 7 7 |
R15 | 7 8 7 8 11 14 7 |
R16 | 9 9 8 11 12 14 11 |
R17 | 8 8 8 9 8 7 9 |
R18 | 8 8 7 6 7 7 6 |
R19 | 8 7 5 6 8 7 8 |
R20 | 7 7 5 7 8 6 7 |
R21 | 9 9 8 9 9 9 10 |
R22 | 8 8 7 6 7 8 8 |
R24 | 9 10 9 9 8 7 12 |
R26 | 24 25 32 27 22 20 18 |
R28 | 47 80 57 35 69 55 93 |
Table 1.2410.c GPS week : 2410 MJD: 61114.0-61120.0
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 2410 0 | 30 -5 15 394 -230 5977 82.5 1965 1965 | 6401 0
brd 2410 1 | -129 21 63 -1833 362 2722 78.1 2261 2261 | 6891 0
brd 2410 2 | 44 142 85 1949 -1845 2579 79.3 2484 2484 | 4106 0
brd 2410 3 | 70 19 -46 2234 1483 9552 78.3 2260 2260 | 5135 0
brd 2410 4 | -37 31 -55 925 1799 1504 82.1 1735 1735 | 5755 0
brd 2410 5 | -1 -80 -54 3169 786 3430 82.4 1781 1781 | 6184 0
brd 2410 6 | 205 78 -9 294 1205 -149 79.0 1821 1821 | 6433 0
-------------+------------------------------------------------------------+----------------
brd 2410 mean| 26 29 0 1018 508 3659 80.2 2043 2043 | 5843 0
brd 2410 sdev| 102 69 57 1634 1243 3197 2.0 290 290 | 948 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 2.2410.0 GPS week: 2410 Day: 0 MJD: 61114
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 9 -1 -12 .11 11 11 | 1960 -790 3299 10040
esa n/a| 0 -4 -2 -55 5 107 -.01 33 31 | 7468 45 3329 11104
gfz n/a| 0 0 -9 -2 1 17 -.22 17 16 | 0 -250 3291 9947
grg n/a| 0 1 10 -4 -73 -18 .32 18 18 | 6042 122 3459 10240
iac n/a| 1 1 -7 16 33 -1 -.14 17 16 | 8338 -1477 3506 10766
jgx n/a| -1 0 3 -5 6 11 -.07 12 12 | 3623 154 3457 10541
Table 2.2410.1 GPS week: 2410 Day: 1 MJD: 61115
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 0 -29 0 1 .11 14 14 | 3053 3921 3311 10364
esa n/a| -4 -4 2 -36 0 -15 .04 34 33 | 8768 3411 3337 10700
gfz n/a| 1 -1 -4 -23 25 -4 -.16 13 12 | 0 3567 3299 10180
grg n/a| 1 -1 7 -7 -6 -15 .21 17 17 | 4560 4095 3447 10347
iac n/a| 4 0 -6 9 -47 31 -.08 15 15 | 7973 999 3521 11907
jgx n/a| -1 1 2 9 15 -18 -.02 15 15 | 4748 4652 3424 10614
Table 2.2410.2 GPS week: 2410 Day: 2 MJD: 61116
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 1 18 -31 3 .09 14 14 | 4363 -2073 3090 9341
esa n/a| -2 -4 2 -38 4 -26 -.06 32 32 | 12421 -2976 3138 10161
gfz n/a| 1 0 -4 27 8 68 -.26 15 15 | 0 -2211 3080 9053
grg n/a| 2 1 3 -10 -15 -36 .24 15 14 | 5136 -2401 3214 8682
iac n/a| 0 -2 -6 -39 30 -51 -.09 13 12 | 5994 -2185 3637 9724
jgx n/a| 0 0 5 8 27 60 -.03 14 14 | 6569 -2180 3205 9309
Table 2.2410.3 GPS week: 2410 Day: 3 MJD: 61117
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 1 11 -30 -17 .15 14 14 | 3622 -2250 2950 9004
esa n/a| 1 0 3 2 -37 9 -.12 33 32 | 8688 -2962 2992 10083
gfz n/a| 2 -2 0 -10 -12 -12 -.18 14 13 | 0 -1818 2950 8766
grg n/a| 0 0 5 -17 -15 2 .26 24 15 | 6172 -2246 3001 8196
iac n/a| 0 1 -7 -17 3 0 -.06 17 17 | 5349 456 3524 9490
jgx n/a| -2 2 0 33 16 23 .05 15 15 | 5881 -2654 3140 8993
Table 2.2410.4 GPS week: 2410 Day: 4 MJD: 61118
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 5 -8 -5 -9 .24 16 16 | 2500 -745 3524 9692
esa n/a| 0 -2 10 1 8 -7 -.06 34 31 | 6056 -364 3580 10528
gfz n/a| 3 0 -3 2 27 20 -.15 14 12 | 0 -698 3523 9568
grg n/a| 0 0 6 -29 13 0 .26 32 18 | 5502 240 3097 9247
iac n/a| 0 1 -6 -14 -33 2 -.09 15 14 | 7604 291 3873 11539
jgx n/a| 1 -1 -1 24 24 -36 -.02 17 17 | 4566 -697 3279 10131
Table 2.2410.5 GPS week: 2410 Day: 5 MJD: 61119
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 0 19 13 51 .15 13 12 | 1912 -1089 3427 9113
esa n/a| -1 0 5 -8 3 31 -.08 36 33 | 5348 -761 3481 9276
gfz n/a| 0 1 -3 -6 6 110 -.12 18 14 | 0 -1292 3427 8968
grg n/a| 0 -1 8 1 -42 -79 .25 37 19 | 6372 -493 3640 9084
iac n/a| -1 -1 -2 15 18 -98 -.04 17 19 | 7673 -957 3426 9572
jgx n/a| 0 0 -3 3 -18 -12 -.07 12 12 | 3692 -647 3524 9721
Table 2.2410.6 GPS week: 2410 Day: 6 MJD: 61120
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 35 6 26 .07 12 13 | 1229 1473 3747 9227
esa n/a| -1 -3 8 -41 -2 -43 -.09 33 31 | 5353 -28 3485 8671
gfz n/a| 0 -1 -7 -2 2 22 -.19 16 16 | 0 739 3419 8261
grg n/a| 0 -2 6 -1 -2 10 .32 17 14 | 5743 1213 3636 8221
iac n/a| 0 1 -1 -18 19 17 -.23 21 22 | 7140 426 3739 9308
jgx n/a| 0 1 -3 -3 -13 -17 -.07 17 17 | 4112 1061 3629 8694
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 3.2410.0 GPS week: 2410 Day: 0 MJD: 61114
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 833 8 21 9 12 11 7 4 | 54 65 55 54 57 56 55
R03 | 4826 12 24 12 25 16 7 6 | 21 31 22 27 19 22 19
R04 | 1391 6 19 14 17 12 5 5 | 19 21 24 18 20 25 20
R05M | 1844 9 46 14 13 18 12 7 | 29 42 26 38 28 23 26
XR06M | 990 30 650 44 --- 79 --- 36 | 44 93 60 --- 36 --- 45
R07 | 736 8 24 16 22 13 9 6 | 16 33 22 21 13 17 14
R08M | 1914 14 37 16 21 25 14 8 | 16 51 29 21 21 21 19
R09E | 1973 9 19 14 13 13 10 5 | 52 58 58 53 57 52 54
R11E | 2313 12 26 12 9 16 11 6 | 35 37 30 33 41 32 33
R12E | 2432 10 23 15 12 17 15 6 | 75 78 71 70 79 63 71
R14E | 1526 12 29 15 20 26 11 8 | 282 295 291 279 290 288 286
R15E | 1403 10 25 19 19 19 14 7 | 118 127 123 110 112 107 115
R16E | 918 16 38 25 18 14 17 8 | 191 189 192 181 184 178 184
XR17M | 1057 10 39 10 11 17 --- 8 | 79 57 85 77 85 --- 79
R18 | 883 12 27 22 19 20 14 8 | 68 84 80 65 81 63 70
XR19 | 2214 13 28 18 --- 17 11 8 | 35 43 46 --- 42 36 37
R20M | 2371 13 40 17 10 16 10 7 | 31 52 43 37 38 47 38
R21M | 1168 8 54 16 27 10 17 9 | 93 59 99 101 93 75 89
R22 | 1408 10 35 21 21 18 13 8 | 35 49 31 45 32 32 33
R24M | 1436 18 49 26 13 13 14 9 | 80 52 90 78 84 66 77
XR26 |11340 32 45 21 --- 63 --- 24 | 52 67 60 --- 57 --- 55
XR28M |17593 36 --- --- --- 59 --- 46 | 114 --- --- --- 70 --- 88
------+-----------------------------------------+-------------------------------------
RMS | 1965 11 33 17 18 17 12 |T 69 75 73 72 69 66 68
WRMS | 1965 11 31 16 18 16 12 |NE 37 49 42 38 40 35 37
MEDI | 1436 12 29 16 17 17 11 |MD 52 57 58 53 57 47 54
Table 3.2410.1 GPS week: 2410 Day: 1 MJD: 61115
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 890 15 29 10 11 12 14 6 | 44 66 54 48 48 44 47
R03 | 3683 10 27 14 14 9 6 5 | 24 34 28 22 26 21 22
R04 | 1155 15 38 13 14 14 8 7 | 21 37 30 18 24 22 21
R05M | 1571 10 36 14 13 12 8 6 | 26 35 26 26 29 24 25
XR06M | 929 34 649 27 --- 63 --- 30 | 25 167 27 --- 24 --- 22
R07 | 802 6 30 15 20 17 14 7 | 18 29 24 16 18 18 16
R08M | 1790 28 38 10 16 22 17 9 | 25 30 20 21 21 16 17
R09E | 2635 13 27 14 20 14 10 7 | 41 38 41 34 41 36 36
R11E | 1882 13 26 8 14 12 12 6 | 16 33 17 18 23 18 15
R12E | 2093 15 20 10 17 14 9 6 | 51 43 38 45 45 40 42
R14E | 1315 6 26 10 17 11 20 6 | 258 269 264 258 264 253 259
R15E | 1127 15 39 11 26 10 16 8 | 101 113 98 92 98 95 96
R16E | 846 19 29 17 27 12 21 9 | 163 173 162 146 154 147 156
XR17M | 1552 11 38 14 17 9 --- 8 | 50 42 55 51 51 --- 50
R18 | 788 14 29 14 21 16 12 7 | 44 54 40 40 39 43 40
XR19 | 1672 10 15 13 --- 18 15 7 | 26 27 20 --- 29 21 21
R20M | 6237 14 30 10 6 18 18 7 | 21 34 29 27 24 37 24
R21M | 979 8 61 15 15 11 14 8 | 52 46 56 60 53 47 52
R22 | 1723 12 35 20 19 17 17 8 | 26 39 27 39 28 29 26
R24M | 1681 16 37 14 10 23 29 9 | 47 38 49 45 50 33 43
XR26 |12249 28 40 32 --- 62 --- 24 | 47 57 49 --- 48 --- 48
XR28M |22512 75 --- --- --- 83 --- 79 | 120 --- --- --- 53 --- 79
------+-----------------------------------------+-------------------------------------
RMS | 2260 14 34 13 17 15 15 |T 56 66 54 55 54 52 52
WRMS | 2260 14 33 12 17 15 15 |NE 31 42 34 30 32 28 30
MEDI | 1571 14 30 14 16 14 14 |MD 41 39 38 39 39 33 36
Table 3.2410.2 GPS week: 2410 Day: 2 MJD: 61116
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1473 9 25 18 10 14 16 6 | 53 63 58 59 62 52 56
R03 | 4376 10 24 10 8 12 8 5 | 18 34 21 24 25 22 19
R04 | 1951 16 20 26 16 11 14 7 | 21 24 23 21 21 26 17
R05M | 1008 21 34 22 10 10 7 7 | 23 31 28 28 27 22 24
XR06M | 949 34 592 26 --- 42 --- 25 | 29 173 33 --- 42 --- 29
R07 | 932 15 34 14 11 8 13 6 | 19 30 27 26 19 26 20
R08M | 926 17 31 12 11 15 17 7 | 19 24 16 17 20 20 15
R09E | 3684 18 18 12 29 14 12 8 | 74 80 81 94 84 78 80
R11E | 1593 18 29 14 14 13 13 7 | 18 35 28 26 22 21 21
R12E | 1676 7 21 16 21 14 15 7 | 80 78 83 72 82 72 77
R14E | 2270 12 24 13 10 9 11 5 | 260 252 246 254 256 255 254
R15E | 2661 11 36 8 15 11 20 7 | 108 123 102 108 105 93 104
R16E | 1591 20 26 13 19 10 19 7 | 199 183 185 195 186 179 188
XR17M | 1151 5 36 16 14 14 --- 8 | 58 40 57 53 61 --- 54
R18 | 938 13 28 16 16 9 15 6 | 49 59 52 44 42 41 45
XR19 | 1317 9 13 13 --- 9 7 5 | 36 38 43 --- 37 36 37
R20M | 5838 10 16 10 8 14 10 5 | 21 20 14 20 33 21 19
R21M | 995 7 58 12 8 19 13 8 | 72 54 76 73 83 63 72
R22 | 2041 9 42 15 9 14 8 6 | 26 49 25 36 27 34 28
R24M | 1791 13 49 20 14 11 24 9 | 58 35 72 68 57 51 58
XR26 |13330 29 36 62 --- 71 --- 32 | 50 65 72 --- 53 --- 53
XR28M |22032 60 --- --- --- 54 --- 57 | 130 --- --- --- 76 --- 99
------+-----------------------------------------+-------------------------------------
RMS | 2484 14 32 15 15 13 14 |T 64 70 63 67 64 61 62
WRMS | 2484 14 32 15 14 12 14 |NE 34 45 40 35 35 33 34
MEDI | 1593 13 29 14 11 13 13 |MD 49 49 52 44 42 36 45
Table 3.2410.3 GPS week: 2410 Day: 3 MJD: 61117
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1038 11 30 7 17 22 17 7 | 41 35 35 35 34 37 35
R03 | 5901 9 32 18 19 12 11 7 | 21 44 33 26 24 22 23
R04 | 1599 16 13 14 13 9 14 6 | 18 37 25 23 19 24 20
R05M | 910 16 22 21 8 16 19 8 | 26 35 34 25 31 33 28
XR06M | 1006 42 606 21 --- 60 --- 30 | 24 153 49 --- 25 --- 29
R07 | 1163 12 44 8 12 12 13 7 | 20 40 25 25 26 28 23
R08M | 1206 16 45 13 13 19 14 8 | 25 30 25 31 29 36 26
R09E | 1893 11 23 16 60 19 14 11 | 92 89 97 117 100 91 95
R11E | 1716 11 20 17 12 16 11 6 | 22 26 29 20 26 20 20
R12E | 1950 10 17 11 19 17 14 6 | 57 63 59 61 53 51 55
R14E | 2016 13 24 12 47 18 19 10 | 192 190 192 224 192 193 195
XR15E | 2830 8 23 10 21 21 --- 7 | 86 84 83 98 86 --- 86
R16E | 2510 27 35 10 33 26 17 10 | 134 117 116 133 114 120 121
XR17M | 800 9 44 16 11 9 --- 8 | 66 41 72 65 66 --- 65
R18 | 603 17 21 7 15 12 12 6 | 53 66 47 50 55 48 50
XR19 | 1010 9 20 15 --- 12 7 6 | 35 31 32 --- 32 33 32
R20M | 2247 10 30 20 14 14 9 7 | 19 22 27 22 27 22 19
R21M | 1034 12 61 11 12 19 16 9 | 77 42 74 71 83 66 71
R22 | 3086 9 33 11 13 9 10 5 | 30 54 31 42 39 32 33
R24M | 1700 14 47 8 15 21 18 8 | 66 40 60 70 70 49 59
XR26 | 9848 30 43 31 --- 75 --- 27 | 21 30 30 --- 27 --- 21
XR28M |24801 31 --- --- --- 38 --- 34 | 64 --- --- --- 45 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 2259 14 33 14 24 17 15 |T 54 60 55 63 54 53 52
WRMS | 2259 14 32 13 15 17 15 |NE 29 42 32 33 32 32 29
MEDI | 1700 12 30 13 14 17 14 |MD 35 41 35 42 34 36 33
Table 3.2410.4 GPS week: 2410 Day: 4 MJD: 61118
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1631 14 16 6 15 14 17 6 | 59 74 63 64 62 57 60
R03 | 2196 7 18 11 11 6 11 4 | 22 24 19 22 17 23 18
R04 | 2319 15 28 13 9 8 14 6 | 20 36 29 17 19 30 23
R05M | 1161 14 38 14 10 18 9 7 | 210 221 223 211 209 210 213
XR06M | 970 52 614 35 --- 70 --- 38 | 91 145 84 --- 96 --- 88
R07 | 788 10 51 9 12 10 9 7 | 22 52 22 21 21 27 21
R08M | 1123 25 51 18 30 28 27 12 | 21 36 22 22 29 31 21
R09E | 1761 12 29 16 19 10 12 7 | 41 52 41 55 46 42 43
XR11E | 1452 9 24 22 41 15 --- 11 | 25 39 38 48 26 --- 26
R12E | 2079 12 14 10 39 14 20 8 | 79 73 77 85 82 75 77
R14E | 1163 14 23 15 92 12 20 14 | 339 339 336 337 342 340 338
XR15E | 2867 12 22 11 44 18 --- 10 | 128 131 126 162 123 --- 129
R16E | 1818 26 28 17 47 16 30 11 | 229 219 219 242 219 207 219
XR17M | 1384 18 29 11 15 13 --- 8 | 57 36 41 43 45 --- 44
R18 | 513 16 15 19 12 15 16 7 | 49 53 69 55 66 51 58
XR19 | 805 10 19 18 --- 18 11 8 | 34 41 36 --- 41 35 35
R20M | 1945 11 28 18 21 15 9 7 | 19 29 36 23 21 27 22
R21M | 692 19 64 12 12 11 7 9 | 60 35 40 53 48 49 47
R22 | 2924 12 28 11 18 16 14 7 | 29 45 35 35 48 34 35
R24M | 1966 13 37 12 15 15 22 8 | 53 41 57 58 54 44 52
XR26 |11811 37 46 23 --- 45 --- 21 | 53 65 74 --- 62 --- 62
XR28M |19116 73 --- --- --- 65 --- 69 | 125 --- --- --- 74 --- 84
------+-----------------------------------------+-------------------------------------
RMS | 1734 16 34 14 32 15 17 |T 80 85 80 86 79 80 77
WRMS | 1734 16 31 12 18 14 17 |NE 36 48 43 35 42 36 39
MEDI | 1631 14 28 14 15 15 14 |MD 53 52 41 53 48 42 47
Table 3.2410.5 GPS week: 2410 Day: 5 MJD: 61119
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2480 15 29 20 13 21 15 8 | 52 61 63 49 60 58 56
R03 | 1026 9 18 8 21 13 11 5 | 21 19 19 20 21 17 16
R04 | 3122 9 20 18 9 11 8 5 | 19 17 23 18 17 14 15
R05M | 1474 17 23 15 7 17 16 7 | 460 460 454 468 469 468 464
XR06M | 976 39 683 38 --- 77 --- 38 | 199 216 195 --- 201 --- 198
R07 | 844 7 52 15 26 14 11 8 | 22 44 22 36 26 26 22
R08M | 1178 21 72 20 18 18 19 11 | 23 47 37 33 29 27 26
R09E | 2040 10 27 12 16 11 11 5 | 35 46 39 36 39 34 36
XR11E | 2019 11 30 16 39 13 --- 10 | 29 32 34 59 42 --- 33
R12E | 1882 12 22 15 59 27 9 10 | 158 159 165 189 158 161 161
R14E | 1337 11 21 15 26 22 7 7 | 241 245 241 234 232 236 238
R15E | 2231 17 30 15 91 16 15 14 | 179 183 172 155 172 193 172
R16E | 1889 19 26 32 84 21 9 14 | 251 263 259 228 236 249 247
XR17M | 1967 9 21 14 8 14 --- 6 | 54 48 49 48 41 --- 47
R18 | 727 14 13 17 12 22 10 7 | 39 48 41 53 55 41 43
XR19 | 1137 8 20 16 --- 15 10 6 | 34 29 33 --- 41 33 33
R20M | 2630 9 31 12 12 8 11 5 | 24 25 24 25 24 26 23
R21M | 678 9 57 26 11 14 10 9 | 54 35 64 54 43 49 49
R22 | 1073 9 44 25 11 12 9 7 | 29 48 29 37 35 35 30
R24M | 1555 9 34 11 17 19 9 6 | 49 40 43 47 43 46 44
XR26 | 9456 18 48 29 --- 45 --- 19 | 35 44 32 --- 38 --- 33
XR28M |18517 48 --- --- --- 62 --- 55 | 61 --- --- --- 35 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1781 13 36 18 37 17 12 |T 94 100 97 99 93 100 92
WRMS | 1781 12 33 14 19 19 12 |NE 31 38 32 35 36 32 31
MEDI | 1555 11 29 16 16 16 10 |MD 39 47 41 48 41 41 43
Table 3.2410.6 GPS week: 2410 Day: 6 MJD: 61120
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2382 6 16 14 13 23 14 6 | 71 77 74 68 75 67 70
R03 | 1177 12 24 12 23 19 20 8 | 25 29 28 29 31 22 24
R04 | 1748 9 30 12 8 15 15 6 | 21 22 17 18 19 19 17
R05M | 1464 18 23 11 12 24 16 7 | 728 727 737 729 721 726 728
XR06M | 954 28 680 20 --- 78 --- 30 | 350 364 350 --- 355 --- 351
R07 | 1025 15 45 18 8 10 8 7 | 24 49 25 32 22 23 22
R08M | 1086 22 57 14 13 17 23 10 | 27 39 25 30 26 44 27
R09E | 2091 13 26 17 10 17 14 7 | 46 40 46 53 49 45 45
R11E | 2223 8 24 17 14 16 14 6 | 27 35 37 38 32 33 30
R12E | 1545 13 20 12 15 16 16 6 | 163 148 157 158 162 148 157
R14E | 2186 8 28 12 18 16 12 6 | 306 306 308 313 302 306 306
R15E | 1413 11 21 17 20 11 13 7 | 212 222 210 197 211 195 210
R16E | 2763 11 37 26 29 21 21 10 | 307 303 310 284 310 287 300
XR17M | 2960 11 38 17 10 17 --- 8 | 82 61 83 78 79 --- 78
R18 | 710 13 15 8 11 20 7 5 | 57 63 57 58 71 60 60
XR19 | 1048 11 29 15 --- 19 14 8 | 41 41 50 --- 50 43 44
R20M | 3400 7 29 17 8 18 22 7 | 27 25 35 25 27 32 27
R21M | 542 8 57 11 21 21 25 10 | 77 44 78 80 79 62 72
R22 | 914 9 29 19 15 27 10 7 | 37 47 41 38 44 37 36
R24M | 1605 8 42 22 28 48 21 12 | 82 55 92 77 106 67 80
XR26 | 7478 21 66 15 --- 39 --- 18 | 39 50 46 --- 48 --- 39
XR28M |20625 64 --- --- --- 132 --- 92 | 63 --- --- --- 83 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1821 12 33 16 17 21 17 |T 127 130 133 128 131 123 126
WRMS | 1821 13 31 16 14 22 17 |NE 39 47 42 40 45 38 39
MEDI | 1545 11 29 15 13 19 14 |MD 57 50 57 58 71 45 49
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