[IGSREPORT-30857] Wk 2409 IGLOS Final Orbits
acc
acc at igs.org
Fri Mar 27 06:13:36 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2409 (Mar 08, 2026 - Mar 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 2.2409.
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:
igl2409[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2409 in the SP3 format.
igl24097.sum Combination Report for GPS Week 2409.
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 | 4.6 ns
1 | 6.0 ns
2 | 4.9 ns
3 | 4.1 ns
4 | 6.2 ns
5 | 5.4 ns
6 | 6.6 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 1.2409, 1a.2409).
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 2.2409.0-6)
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 3.2409.0-6).
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 2409 summary. (Mar 08, 2026 - Mar 14, 2026)
Table 1.2409.a GPS week : 2409 MJD: 61107.0-61113.0
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 0 6 3 -15 .12 13 13 | 2392 -682 3878 9209
| 0 1 1 21 12 12 .05 | 833 1595
esa n/a| -1 -3 1 -18 -5 -3 -.06 35 33 | 5019 -54 3931 9646
| 2 1 3 13 23 59 .05 | 706 1217
gfz n/a| 1 0 -3 -6 10 15 -.18 16 15 | 0 -709 3875 9061
| 1 1 1 16 9 29 .02 | 0 1348
grg n/a| 0 0 4 14 -23 20 .30 15 14 | 5579 -652 3584 8749
| 1 0 0 14 21 43 .03 | 1087 2374
iac n/a| 0 0 -8 -6 12 -92 -.20 19 19 | 6647 -221 4033 10237
| 1 1 2 31 26 81 .10 | 1032 888
jgx n/a| 0 0 5 -6 1 43 -.08 17 17 | 3993 -679 3541 8967
| 1 0 1 12 10 26 .05 | 1415 2888
Table 1.2409.b GPS week : 2409 MJD: 61107.0-61113.0
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 7 6 6 5 6 5 |
R03 | 8 8 7 8 7 6 8 |
R04 | 8 7 9 6 5 7 5 |
R05 | 6 6 7 8 8 6 6 |
R06 | 29 30 32 32 32 27 30 |
R07 | 6 6 7 9 9 7 7 |
R08 | 13 8 10 14 10 12 9 |
R09 | 7 8 9 6 9 6 7 |
R11 | 6 9 9 8 7 7 8 |
R12 | 8 7 6 7 7 9 7 |
R14 | 7 5 6 6 5 6 8 |
R15 | 7 8 10 7 7 6 8 |
R16 | 8 10 10 10 8 9 10 |
R17 | 10 9 9 8 9 10 8 |
R18 | 7 8 7 7 8 8 8 |
R19 | 7 7 8 7 7 6 7 |
R20 | 9 10 10 7 9 7 7 |
R21 | 9 9 11 10 9 8 11 |
R22 | 8 8 8 8 9 10 8 |
R24 | 11 10 10 8 8 10 10 |
R26 | 26 24 23 26 30 24 30 |
R28 | 50 91 86 31 29 69 54 |
Table 1.2409.c GPS week : 2409 MJD: 61107.0-61113.0
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 2409 0 | 9 -10 88 1949 -3 -800 78.8 1928 1928 | 4591 0
brd 2409 1 | -12 -13 38 -118 2936 4594 81.0 2311 2311 | 6041 0
brd 2409 2 | 51 13 50 -312 2110 2662 80.9 2381 2381 | 4943 0
brd 2409 3 | 53 -107 -97 -2268 -1236 -298 80.1 1930 1930 | 4116 0
brd 2409 4 | 3 7 -129 -856 -3794 -4694 77.7 1814 1814 | 6170 0
brd 2409 5 | 10 150 102 -735 2591 -3006 79.5 1671 1671 | 5377 0
brd 2409 6 | -43 33 67 363 864 835 79.7 1782 1782 | 6615 0
-------------+------------------------------------------------------------+----------------
brd 2409 mean| 10 10 17 -282 495 -101 79.7 1973 1973 | 5407 0
brd 2409 sdev| 34 76 92 1284 2406 3178 1.1 270 270 | 912 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 2.2409.0 GPS week: 2409 Day: 0 MJD: 61107
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 -14 -6 -9 .09 13 13 | 2410 -403 3740 9083
esa n/a| -5 -3 -3 -14 38 27 -.09 35 35 | 4287 -259 3782 9504
gfz n/a| -1 0 -3 -9 17 -17 -.21 14 13 | 0 -787 3737 9133
grg n/a| 2 0 4 31 -29 29 .32 15 14 | 4173 162 3916 9428
iac n/a| 2 0 -6 25 11 -88 -.12 20 21 | 7943 -1658 4140 12026
jgx n/a| -1 1 4 -22 2 39 -.02 16 16 | 2324 569 3909 8469
Table 2.2409.1 GPS week: 2409 Day: 1 MJD: 61108
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 5 -7 -20 .19 11 10 | 3003 721 3571 8677
esa n/a| 0 -2 -2 -39 -7 57 -.02 34 34 | 4306 724 3606 9152
gfz n/a| 0 1 0 5 -1 -1 -.21 16 13 | 0 617 3563 8660
grg n/a| 0 0 3 5 -15 55 .33 14 15 | 5920 184 3760 8825
iac n/a| -1 -1 -4 24 45 -154 -.26 20 19 | 6721 50 3582 9315
jgx n/a| -2 0 7 8 -19 76 -.15 20 20 | 5624 48 3603 9330
Table 2.2409.2 GPS week: 2409 Day: 2 MJD: 61109
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 1 0 18 -3 -33 .20 14 13 | 3543 -380 2855 8340
esa n/a| 0 -3 0 -14 -8 -12 -.05 35 33 | 6225 22 2901 8807
gfz n/a| 2 -2 -5 -14 -1 -16 -.20 17 19 | 0 -733 2850 8258
grg n/a| 1 0 2 0 19 66 .34 15 15 | 5362 -1173 2920 8039
iac n/a| 1 -1 -7 -32 -1 -119 -.36 23 23 | 6170 -157 3038 8904
jgx n/a| -1 1 4 -2 8 71 -.07 17 17 | 5317 -1029 2896 8741
Table 2.2409.3 GPS week: 2409 Day: 3 MJD: 61110
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 -2 44 12 -29 .12 13 14 | 2824 -3007 3263 8206
esa n/a| 0 -2 0 -1 0 -36 -.14 36 31 | 4960 -1827 3306 8574
gfz n/a| 3 0 -3 -24 6 42 -.17 16 15 | 0 -2695 3249 8072
grg n/a| 0 -1 4 6 -19 -40 .27 13 13 | 5240 -2509 3312 8006
iac n/a| 1 1 -9 -31 -15 36 -.22 18 17 | 5225 187 3521 9092
jgx n/a| 0 0 5 -20 13 10 -.09 16 16 | 3415 -2920 3348 8216
Table 2.2409.4 GPS week: 2409 Day: 4 MJD: 61111
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -2 -10 28 -13 .07 14 14 | 2007 384 4855 10351
esa n/a| 1 -1 4 -12 -4 -102 -.09 36 33 | 5130 1186 4925 10637
gfz n/a| 2 2 -3 18 19 44 -.15 16 16 | 0 472 4853 10068
grg n/a| 0 0 4 38 -41 -29 .28 15 14 | 4758 2599 3563 9241
iac n/a| 0 0 -10 -51 -17 -23 -.08 14 14 | 7854 -1029 4905 11676
jgx n/a| 0 1 7 -10 -3 25 -.08 16 16 | 2946 3498 3475 9876
Table 2.2409.5 GPS week: 2409 Day: 5 MJD: 61112
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 15 0 -6 .09 12 12 | 1967 -2824 5496 11029
esa n/a| -1 -6 1 -35 -21 -28 -.05 36 36 | 4631 -1447 5557 11260
gfz n/a| 1 2 -3 -25 18 48 -.18 15 13 | 0 -2285 5513 10436
grg n/a| -1 0 4 3 -39 60 .28 14 13 | 7568 -4652 4132 8682
iac n/a| 1 -1 -11 12 19 -211 -.11 19 18 | 5687 -41 5486 10987
jgx n/a| 0 0 4 -6 5 17 -.11 15 15 | 5453 -5547 4047 8854
Table 2.2409.6 GPS week: 2409 Day: 6 MJD: 61113
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 2 -13 3 1 .10 12 12 | 995 732 3368 8780
esa n/a| -2 -6 6 -9 -36 68 .03 31 31 | 5594 1218 3445 9590
gfz n/a| 1 0 -5 5 13 8 -.17 16 14 | 0 444 3360 8801
grg n/a| 1 0 3 12 -41 3 .32 15 13 | 6038 822 3487 9023
iac n/a| -1 -3 -10 5 46 -86 -.24 20 19 | 6929 1101 3560 9664
jgx n/a| -1 0 2 7 4 60 -.03 17 17 | 2873 622 3513 9286
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 3.2409.0 GPS week: 2409 Day: 0 MJD: 61107
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1581 20 32 20 10 15 12 8 | 26 45 44 38 30 27 32
R03 | 1188 9 23 17 24 12 16 7 | 32 32 33 35 29 26 29
R04 | 781 15 38 9 13 13 20 7 | 37 43 36 34 34 29 33
R05 | 833 11 25 13 11 16 13 6 | 96 104 111 100 97 105 101
XR06 | 890 28 638 25 --- 69 --- 29 | 50 166 68 --- 53 --- 56
R07 | 2812 10 22 9 8 16 21 6 | 38 46 38 38 37 36 36
XR08 | 1555 28 41 22 18 24 --- 12 | 27 43 37 34 36 --- 30
R09 | 751 9 36 15 18 19 8 7 | 41 56 44 37 41 41 40
R11 | 1774 12 26 11 9 13 10 5 | 52 65 56 58 51 57 54
R12 | 2572 19 36 16 15 16 8 7 | 72 75 57 65 59 61 62
R14 | 3478 9 29 12 15 15 15 6 | 116 130 121 107 112 105 113
R15 | 997 12 31 13 17 12 18 7 | 138 150 135 128 128 120 131
R16 | 1549 13 41 19 11 11 18 8 | 97 69 102 88 90 74 89
XR17 | 872 9 35 21 21 20 --- 10 | 77 53 85 69 86 --- 76
R18 | 946 14 27 13 17 20 12 7 | 61 79 72 59 73 61 65
XR19 | 2134 9 23 11 --- 19 11 6 | 37 41 40 --- 47 38 39
R20 | 3363 7 30 12 12 44 16 9 | 39 41 40 41 56 43 40
R21 | 1660 15 55 9 17 17 19 9 | 94 67 95 89 95 76 88
R22 | 1457 10 40 13 19 10 21 7 | 37 63 39 49 44 35 40
R24 | 1850 11 46 17 15 38 25 10 | 78 48 83 75 89 56 73
XR26 | 7799 17 51 41 --- 70 --- 25 | 28 34 46 --- 44 --- 33
XR28 |12344 38 --- --- --- 65 --- 50 | 44 --- --- --- 50 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1927 13 35 14 15 20 16 |T 59 69 65 63 62 58 58
WRMS | 1927 13 35 13 14 21 16 |NE 59 69 65 63 62 58 58
MEDI | 1555 12 35 13 15 16 16 |MD 44 56 56 58 51 56 40
Table 3.2409.1 GPS week: 2409 Day: 1 MJD: 61108
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1249 12 25 18 9 13 21 7 | 29 34 30 25 25 29 25
R03 | 616 7 35 11 13 14 28 7 | 28 36 19 29 25 25 23
R04 | 2046 10 18 19 12 15 16 6 | 29 28 31 31 30 25 27
R05 | 2570 6 30 11 12 20 6 6 | 84 84 86 81 82 87 83
XR06 | 895 31 602 27 --- 67 --- 29 | 62 201 73 --- 56 --- 63
R07 | 1896 10 27 13 9 13 15 6 | 30 30 35 37 32 35 31
R08 | 1940 11 36 15 18 20 21 8 | 27 27 28 36 24 29 25
XR09 | 1158 11 22 14 16 21 --- 8 | 38 39 39 34 45 --- 36
R11 | 2219 10 16 24 25 16 16 8 | 52 63 69 60 54 54 56
R12 | 2039 14 37 15 13 15 8 7 | 66 68 57 61 65 60 61
R14 | 4115 5 20 12 9 10 14 4 | 105 105 109 108 101 100 105
R15 | 852 15 41 13 16 13 23 8 | 107 113 92 108 95 85 99
R16 | 1312 19 52 17 18 21 21 10 | 91 76 93 78 86 72 83
XR17 | 1112 5 38 18 15 20 --- 8 | 56 44 57 56 56 --- 53
R18 | 1819 10 27 15 18 15 24 7 | 53 58 54 46 50 54 50
XR19 | 3233 7 21 17 --- 17 10 7 | 45 50 45 --- 43 48 44
R20 | 5453 8 19 9 12 51 21 10 | 45 48 41 47 57 47 44
R21 | 1044 9 55 23 12 12 19 9 | 72 64 81 67 67 63 70
R22 | 1183 13 30 11 12 24 17 7 | 35 40 37 46 47 44 39
R24 | 1162 10 45 22 14 19 31 9 | 52 47 62 63 55 44 54
XR26 | 7180 23 44 34 --- 68 --- 24 | 41 36 32 --- 31 --- 32
XR28 |13422 66 --- --- --- 124 --- 90 | 90 --- --- --- 143 --- 89
------+-----------------------------------------+-------------------------------------
RMS | 2311 11 34 16 14 20 20 |T 56 61 55 56 57 53 54
WRMS | 2311 10 34 13 15 19 20 |NE 56 61 55 56 57 53 54
MEDI | 1819 10 30 15 13 17 19 |MD 52 48 54 47 54 48 50
Table 3.2409.2 GPS week: 2409 Day: 2 MJD: 61109
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 593 7 18 12 17 13 13 6 | 23 30 33 33 29 29 26
R03 | 1389 12 23 15 14 10 18 6 | 24 33 30 25 23 21 22
R04 | 3262 20 23 16 12 25 27 9 | 28 38 26 25 30 30 24
R05 | 4089 18 33 12 10 14 10 7 | 37 37 43 37 33 30 34
XR06 | 902 38 599 25 --- 69 --- 31 | 26 220 38 --- 35 --- 25
R07 | 1147 10 42 13 12 12 10 7 | 28 32 33 29 33 32 29
R08 | 2140 15 37 22 23 31 8 9 | 20 28 22 25 24 17 16
XR09 | 830 12 23 17 13 25 --- 8 | 22 34 29 27 29 --- 22
R11 | 1478 12 35 21 21 20 13 8 | 30 35 50 32 44 40 33
R12 | 1816 9 18 12 9 22 13 6 | 40 41 41 42 40 38 38
R14 | 3341 8 22 16 15 13 8 6 | 64 66 65 63 66 61 63
R15 | 1184 24 35 10 20 20 22 9 | 114 121 100 96 91 99 100
R16 | 681 23 44 18 13 22 20 9 | 80 58 66 71 72 55 66
XR17 | 1088 8 39 16 11 22 --- 8 | 57 43 67 65 60 --- 58
R18 | 2092 9 21 17 15 18 16 7 | 47 58 55 45 50 40 45
XR19 | 2961 13 21 20 --- 15 10 7 | 24 25 32 --- 24 26 24
R20 | 5222 8 32 12 19 48 13 10 | 25 34 25 28 48 26 23
R21 | 1058 10 58 28 14 28 23 11 | 66 48 72 64 77 50 61
R22 | 1437 18 34 14 12 22 17 8 | 25 44 39 39 45 28 32
R24 | 1348 12 50 23 15 15 30 10 | 55 37 63 65 54 36 51
XR26 | 3801 29 42 24 --- 63 --- 22 | 21 34 26 --- 29 --- 21
XR28 |15445 63 --- --- --- 115 --- 86 | 50 --- --- --- 102 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 2381 14 35 17 15 23 17 |T 41 52 45 45 47 38 38
WRMS | 2381 13 33 19 15 23 17 |NE 41 52 45 45 47 38 38
MEDI | 1437 12 34 16 14 22 13 |MD 28 37 39 37 40 32 32
Table 3.2409.3 GPS week: 2409 Day: 3 MJD: 61110
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1735 12 17 12 8 19 18 6 | 25 15 24 18 19 16 18
R03 | 1322 10 22 16 15 19 22 7 | 25 32 22 30 30 23 23
R04 | 2502 17 22 11 12 7 14 6 | 28 30 25 31 22 22 23
R05 | 3020 20 36 16 7 18 10 7 | 37 41 34 29 40 28 31
XR06 | 1003 37 614 31 --- 63 --- 31 | 50 175 60 --- 53 --- 52
R07 | 850 9 64 13 11 17 15 8 | 32 59 31 29 23 28 27
XR08 | 1433 20 55 18 26 37 --- 14 | 27 45 32 28 39 --- 27
R09 | 779 12 28 14 11 15 13 6 | 29 42 33 27 37 28 30
XR11 | 2251 17 19 14 11 22 --- 8 | 32 34 34 34 41 --- 31
R12 | 1440 11 26 16 18 17 10 7 | 54 44 57 50 49 46 49
R14 | 2126 7 18 14 15 16 9 6 | 61 66 58 70 62 54 60
R15 | 1125 15 28 14 12 17 13 6 | 87 96 81 79 77 70 79
R16 | 2130 18 51 14 13 21 27 9 | 74 37 60 65 78 37 59
XR17 | 787 12 47 10 13 10 --- 8 | 61 37 63 77 66 --- 64
R18 | 1662 10 14 18 7 17 18 6 | 56 55 66 62 66 48 58
XR19 | 1682 15 24 15 --- 12 9 7 | 27 28 17 --- 23 21 19
R20 | 3431 17 22 16 17 15 10 7 | 30 24 25 27 21 25 20
R21 | 1579 14 65 11 15 30 16 10 | 67 32 51 57 77 45 55
R22 | 2037 10 48 18 14 16 17 8 | 24 54 21 35 35 22 25
R24 | 904 13 30 26 12 11 19 8 | 63 42 73 55 56 41 55
XR26 | 6878 35 42 33 --- 65 --- 26 | 40 36 24 --- 23 --- 27
XR28 |15372 27 --- --- --- 36 --- 31 | 91 --- --- --- 81 --- 81
------+-----------------------------------------+-------------------------------------
RMS | 1930 13 36 16 13 18 16 |T 46 48 42 44 46 34 41
WRMS | 1930 14 31 15 13 17 16 |NE 46 48 42 44 46 34 41
MEDI | 1662 14 28 15 12 17 14 |MD 37 41 34 34 40 28 31
Table 3.2409.4 GPS week: 2409 Day: 4 MJD: 61111
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2668 8 22 8 9 15 10 5 | 24 29 30 29 28 34 27
R03 | 2100 7 23 20 14 12 23 7 | 21 27 25 22 19 16 17
R04 | 1850 12 20 9 9 15 6 5 | 23 22 21 26 19 25 20
R05 | 1439 21 28 14 7 13 20 7 | 44 48 47 44 40 48 43
XR06 | 992 39 661 33 --- 59 --- 32 | 22 123 38 --- 36 --- 30
R07 | 1216 19 62 15 16 8 8 8 | 31 44 34 38 30 28 30
R08 | 1536 24 55 11 17 21 20 10 | 29 41 33 38 29 36 30
R09 | 742 18 29 21 18 17 17 8 | 34 40 38 32 41 29 32
R11 | 2105 14 26 13 18 13 13 7 | 37 46 36 34 41 37 34
R12 | 1016 13 18 13 23 14 9 6 | 56 53 54 49 55 44 50
R14 | 1600 7 25 12 10 10 13 5 | 71 81 73 70 76 64 71
R15 | 831 10 30 10 12 9 20 6 | 85 100 87 88 79 69 82
R16 | 2660 16 41 18 15 8 16 7 | 78 59 84 76 77 63 73
XR17 | 1082 13 40 9 14 21 --- 9 | 53 41 58 56 69 --- 57
R18 | 1634 14 14 13 21 12 20 7 | 49 44 56 73 56 45 54
XR19 | 1332 10 22 12 --- 14 12 6 | 32 29 40 --- 30 39 33
R20 | 2721 12 29 20 17 22 17 8 | 29 33 27 32 29 30 26
R21 | 1787 14 60 14 13 14 17 8 | 67 53 67 64 71 62 65
R22 | 2137 9 50 24 17 12 10 8 | 33 58 27 46 29 40 34
R24 | 920 10 39 24 13 16 14 8 | 56 38 64 58 45 44 52
XR26 | 8673 47 47 37 --- 64 --- 29 | 29 36 52 --- 27 --- 32
XR28 |15981 31 --- --- --- 27 --- 29 | 112 --- --- --- 71 --- 86
------+-----------------------------------------+-------------------------------------
RMS | 1813 14 36 16 15 14 16 |T 46 49 47 48 45 41 44
WRMS | 1813 14 33 16 14 14 16 |NE 46 49 47 48 45 41 44
MEDI | 1600 13 29 14 14 14 14 |MD 34 44 40 44 40 39 34
Table 3.2409.5 GPS week: 2409 Day: 5 MJD: 61112
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1923 7 21 8 11 17 16 5 | 19 25 25 24 20 27 21
R03 | 3279 8 18 16 11 13 16 6 | 19 26 25 26 17 21 20
R04 | 1500 13 34 10 9 16 18 6 | 18 27 18 21 18 17 16
R05 | 731 8 15 17 14 13 14 6 | 28 36 42 37 23 26 30
XR06 | 927 25 655 20 --- 66 --- 26 | 41 117 44 --- 37 --- 40
R07 | 1309 9 45 12 8 13 11 6 | 20 33 22 19 16 16 17
XR08 | 3365 22 53 20 21 13 --- 12 | 21 31 22 33 27 --- 21
R09 | 896 12 26 14 9 19 9 6 | 14 35 21 25 35 22 20
R11 | 2507 12 27 14 18 16 16 7 | 33 40 26 33 37 33 29
R12 | 1205 21 24 14 27 16 12 8 | 56 50 50 45 52 44 46
R14 | 1558 6 26 10 18 18 10 6 | 55 64 51 53 49 46 50
R15 | 1452 11 24 14 9 14 16 6 | 72 75 65 71 67 56 66
R16 | 1764 8 50 24 13 14 20 8 | 65 68 80 71 59 52 64
XR17 | 1291 8 37 11 17 33 --- 9 | 47 33 38 39 65 --- 43
R18 | 885 15 12 16 13 32 8 7 | 42 47 54 46 68 48 48
XR19 | 1294 9 21 13 --- 12 11 6 | 25 32 36 --- 38 31 30
R20 | 1335 11 30 12 12 16 17 6 | 29 36 31 34 32 31 29
R21 | 1072 11 61 8 13 11 14 8 | 49 28 41 52 54 42 45
R22 | 1214 18 57 25 15 20 8 9 | 24 36 31 29 30 27 22
R24 | 2076 10 48 17 11 37 26 10 | 54 31 51 48 74 37 49
XR26 |15359 28 71 25 --- 60 --- 23 | 34 41 36 --- 25 --- 28
XR28 |10737 51 --- --- --- 95 --- 69 | 100 --- --- --- 139 --- 101
------+-----------------------------------------+-------------------------------------
RMS | 1670 12 36 15 14 19 15 |T 39 43 38 39 44 33 37
WRMS | 1670 12 36 13 13 18 15 |NE 39 43 38 39 44 33 37
MEDI | 1335 11 30 14 13 16 14 |MD 33 36 36 34 37 31 30
Table 3.2409.6 GPS week: 2409 Day: 6 MJD: 61113
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1489 6 16 10 6 22 9 5 | 26 27 26 24 28 22 24
R03 | 3353 10 21 11 24 14 20 7 | 25 40 24 33 24 30 25
R04 | 1135 8 23 11 6 14 9 5 | 26 28 23 24 23 22 22
R05 | 2139 7 29 10 9 17 16 6 | 38 47 41 40 34 37 37
XR06 | 931 18 668 35 --- 74 --- 30 | 40 203 43 --- 55 --- 39
R07 | 701 9 24 16 13 19 7 6 | 35 39 39 36 32 32 33
R08 | 3954 18 33 11 23 13 25 9 | 31 43 33 39 37 25 31
R09 | 1464 11 21 15 11 22 12 6 | 26 37 31 26 44 27 28
R11 | 1507 10 28 23 15 17 21 8 | 41 51 54 38 45 41 41
R12 | 1729 17 20 13 13 17 13 7 | 64 66 57 55 61 50 57
R14 | 1429 13 36 12 18 19 13 7 | 77 90 78 76 81 71 76
R15 | 1120 11 26 13 19 19 15 7 | 101 104 94 99 99 87 96
R16 | 1490 20 40 16 13 23 26 10 | 95 73 92 82 78 64 82
XR17 | 683 8 24 13 18 22 --- 8 | 72 49 73 68 85 --- 71
R18 | 737 11 21 14 18 30 12 7 | 58 70 65 58 81 58 62
XR19 | 2174 13 18 12 --- 19 11 7 | 31 40 41 --- 48 37 37
R20 | 878 10 25 13 11 17 16 6 | 33 37 39 41 40 36 35
R21 | 833 6 54 26 19 15 28 10 | 77 46 91 83 87 61 76
R22 | 998 13 38 23 11 15 9 7 | 30 42 30 32 28 29 27
R24 | 1618 6 44 15 11 32 25 9 | 76 47 83 76 92 55 73
XR26 | 9524 33 86 33 --- 75 --- 30 | 34 67 33 --- 42 --- 32
XR28 | 9814 39 --- --- --- 75 --- 54 | 75 --- --- --- 110 --- 83
------+-----------------------------------------+-------------------------------------
RMS | 1782 12 31 16 15 20 17 |T 50 59 51 51 57 43 49
WRMS | 1782 12 31 14 13 19 17 |NE 50 59 51 51 57 43 49
MEDI | 1464 11 26 13 13 19 13 |MD 38 47 41 40 45 37 37
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