[IGSREPORT-30849] Wk 2408 IGLOS Final Orbits
acc
acc at igs.org
Mon Mar 23 00:27:56 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2408 (Mar 01, 2026 - Mar 07, 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 2.2408.
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:
igl2408[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2408 in the SP3 format.
igl24087.sum Combination Report for GPS Week 2408.
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 | 5.3 ns
2 | 5.2 ns
3 | 5.2 ns
4 | 5.5 ns
5 | 7.1 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 1.2408, 1a.2408).
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 2.2408.0-6)
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 3.2408.0-6).
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 2408 summary. (Mar 01, 2026 - Mar 07, 2026)
Table 1.2408.a GPS week : 2408 MJD: 61100.0-61106.0
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 -1 11 2 -17 .13 13 13 | 1493 -107 3407 9211
| 0 0 1 12 13 16 .03 | 791 2107
esa n/a| 0 -2 1 -21 -14 -10 -.00 37 35 | 3150 -355 3379 9618
| 2 1 3 20 19 65 .04 | 1072 2107
gfz n/a| 0 0 -4 9 8 16 -.20 16 15 | 0 -253 3320 9146
| 0 0 2 23 22 32 .03 | 0 2149
grg n/a| 1 0 5 8 -14 20 .30 16 15 | 5755 -108 3393 9145
| 1 0 1 11 15 42 .02 | 931 2080
iac n/a| 0 0 -8 -17 0 -40 -.17 22 24 | 7408 -488 3530 9912
| 1 1 2 36 65 27 .05 | 1050 1302
jgx n/a| 0 0 8 -3 0 30 -.07 17 17 | 3046 -211 3416 9630
| 1 0 2 13 17 19 .02 | 754 2022
Table 1.2408.b GPS week : 2408 MJD: 61100.0-61106.0
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 | 7 8 7 6 7 7 6 |
R03 | 7 8 7 5 5 6 6 |
R04 | 8 8 8 8 6 6 6 |
R05 | 7 8 8 8 6 5 7 |
R06 | 29 36 33 28 30 33 34 |
R07 | 7 7 9 8 8 9 8 |
R08 | 9 9 12 9 9 10 9 |
R09 | 7 8 7 6 6 6 6 |
R11 | 6 8 8 9 7 10 8 |
R12 | 8 7 7 7 9 9 9 |
R14 | 6 8 6 8 6 6 7 |
R15 | 9 7 7 8 8 8 6 |
R16 | 10 9 10 9 9 10 9 |
R17 | 8 9 7 8 7 11 9 |
R18 | 8 7 5 6 8 8 7 |
R19 | 7 8 8 8 8 8 9 |
R20 | 13 12 16 14 11 9 11 |
R21 | 12 10 9 9 9 8 10 |
R22 | 9 9 9 9 9 8 8 |
R24 | 11 11 9 9 11 10 12 |
R26 | 24 23 22 24 24 24 28 |
R28 | 75 58 64 106 80 56 51 |
Table 1.2408.c GPS week : 2408 MJD: 61100.0-61106.0
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 2408 0 | 68 -85 -45 112 -613 2446 75.9 1770 1770 | 6396 0
brd 2408 1 | -200 17 6 -2456 -2792 -448 78.2 1657 1657 | 5274 0
brd 2408 2 | 12 -26 -44 -544 579 3092 77.4 1685 1685 | 5185 0
brd 2408 3 | -88 -4 42 13 -773 -1877 79.4 1763 1763 | 5197 0
brd 2408 4 | -38 -9 17 -867 -895 -3870 79.8 1853 1853 | 5534 0
brd 2408 5 | -26 50 -137 764 2064 -3578 78.1 1791 1791 | 7139 0
brd 2408 6 | 5 79 -69 2209 1906 -2503 80.2 1418 1418 | 6570 0
-------------+------------------------------------------------------------+----------------
brd 2408 mean| -37 3 -33 -109 -75 -962 78.4 1705 1705 | 5899 0
brd 2408 sdev| 86 53 60 1441 1720 2793 1.5 142 142 | 791 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 2.2408.0 GPS week: 2408 Day: 0 MJD: 61100
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 0 3 -4 3 .08 14 13 | 2344 -619 3385 8737
esa n/a| 0 -2 -4 -17 1 3 -.04 37 36 | 4246 -425 3437 9643
gfz n/a| 0 0 -5 27 0 -10 -.21 17 15 | 0 -129 3377 8742
grg n/a| 2 0 3 9 -37 13 .31 13 12 | 6280 -37 3571 8660
iac n/a| -1 1 -13 -26 60 -41 -.19 25 22 | 8977 -1362 3476 9608
jgx n/a| 0 0 10 -18 -9 45 -.09 18 18 | 3602 65 3566 9277
Table 2.2408.1 GPS week: 2408 Day: 1 MJD: 61101
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 17 -15 -38 .14 15 15 | 1786 -2729 3067 9966
esa n/a| 1 -4 4 -14 -7 -20 -.02 34 34 | 4362 -3860 3123 10480
gfz n/a| 0 0 -5 24 1 -22 -.20 15 16 | 0 -3233 3057 9960
grg n/a| 0 -2 6 14 -21 60 .28 15 14 | 6654 -3124 3176 10084
iac n/a| 0 -2 -12 -2 2 -70 -.11 23 21 | 7736 -2414 3075 10769
jgx n/a| -1 1 11 -22 26 41 -.10 18 18 | 3850 -3171 3192 10645
Table 2.2408.2 GPS week: 2408 Day: 2 MJD: 61102
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 0 28 12 -9 .14 13 13 | -80 1732 3765 8944
esa n/a| 0 0 -2 -22 -31 -122 -.03 39 35 | 1340 1199 3805 9647
gfz n/a| -1 -1 -8 -37 22 0 -.22 16 16 | 0 1502 3769 9119
grg n/a| 1 -1 7 -10 0 80 .29 18 18 | 4217 1345 3548 8923
iac n/a| -1 1 -7 44 -63 -58 -.16 24 31 | 6631 -451 3969 10039
jgx n/a| 1 0 8 -2 -18 9 -.05 18 18 | 1854 1107 3578 9390
Table 2.2408.3 GPS week: 2408 Day: 3 MJD: 61103
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 4 4 -27 .17 13 12 | 1960 -563 3079 8659
esa n/a| 0 0 3 14 -9 18 .07 39 35 | 2356 -496 3140 9076
gfz n/a| 0 0 -3 23 18 65 -.16 16 15 | 0 -922 3066 8636
grg n/a| 0 0 5 11 1 17 .28 16 17 | 5142 -601 3188 8670
iac n/a| 0 1 -7 -62 -1 -66 -.18 22 28 | 6255 1172 3453 9592
jgx n/a| 0 0 5 14 -1 57 -.06 16 16 | 3409 -610 3249 9169
Table 2.2408.4 GPS week: 2408 Day: 4 MJD: 61104
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 24 -13 -35 .16 13 13 | 1104 -2512 3757 8578
esa n/a| 0 -3 2 -46 -31 -65 -.01 39 35 | 2989 -2245 3835 8388
gfz n/a| 0 1 -5 4 -27 30 -.15 14 14 | 0 -2727 3758 8812
grg n/a| 0 -1 6 5 -17 25 .31 17 16 | 6813 -2412 3850 8674
iac n/a| 1 0 -6 -46 105 -33 -.24 21 24 | 6641 -890 3759 9260
jgx n/a| 0 0 7 6 -16 22 -.08 15 15 | 2643 -2536 3893 9201
Table 2.2408.5 GPS week: 2408 Day: 5 MJD: 61105
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 5 16 0 .11 13 13 | 1523 1096 3345 9599
esa n/a| -3 -1 2 -42 -38 55 .04 33 32 | 3070 1393 3223 9527
gfz n/a| 0 0 -5 -3 -2 4 -.24 16 15 | 0 1564 3192 9488
grg n/a| 0 -1 4 1 -24 0 .31 15 14 | 5909 1941 3281 9701
iac n/a| -1 1 -8 7 -19 -14 -.17 21 22 | 8587 -648 3347 10183
jgx n/a| 0 0 8 4 18 2 -.06 17 17 | 2374 1958 3292 10129
Table 2.2408.6 GPS week: 2408 Day: 6 MJD: 61106
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 -2 16 -15 .09 12 12 | 1815 2843 3451 10000
esa n/a| -4 -2 0 -24 15 59 -.04 35 34 | 3689 1949 3090 10570
gfz n/a| 0 0 -1 27 45 47 -.19 16 16 | 0 2170 3027 9265
grg n/a| 3 0 5 25 0 -50 .33 18 16 | 5270 2129 3143 9304
iac n/a| 0 0 -6 -33 -80 2 -.11 20 22 | 7029 1176 3637 9933
jgx n/a| 0 0 9 -7 -4 31 -.04 17 17 | 3591 1710 3145 9599
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 3.2408.0 GPS week: 2408 Day: 0 MJD: 61100
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2184 11 30 17 10 15 12 6 | 32 35 36 32 29 27 29
R03 | 1352 19 30 14 12 15 13 7 | 39 51 37 40 32 32 35
R04 | 1123 14 32 13 12 24 13 7 | 42 51 33 33 34 41 34
R05 | 1448 10 37 10 9 19 11 6 | 39 40 28 33 26 30 30
XR06 | 856 31 613 20 --- 69 --- 29 | 20 244 39 --- 67 --- 32
R07 | 885 14 27 15 13 10 18 6 | 39 50 36 47 37 35 38
R08 | 1333 19 46 17 10 20 18 8 | 28 53 34 33 40 23 30
R09 | 1993 9 32 12 15 17 12 6 | 68 79 64 64 71 64 65
R11 | 871 10 16 16 10 12 11 5 | 84 81 92 80 90 85 85
R12 | 1306 19 22 17 9 30 10 8 | 79 78 68 62 57 64 66
R14 | 3018 7 43 11 8 15 9 6 | 136 136 135 131 135 127 132
R15 | 1072 20 44 12 17 16 18 8 | 123 136 118 105 111 105 113
R16 | 1500 17 45 27 15 13 26 10 | 121 85 130 102 116 93 109
XR17 | 1402 7 41 10 9 19 --- 7 | 54 37 55 54 64 --- 53
R18 | 804 11 35 10 20 17 15 7 | 48 59 44 42 48 34 42
XR19 | 1178 10 26 18 --- 12 11 7 | 21 33 28 --- 28 26 23
R20 | 3782 10 25 22 12 66 19 12 | 18 29 23 21 45 23 14
R21 | 735 8 58 29 16 27 29 11 | 67 44 75 62 77 50 62
R22 | 2028 12 36 21 11 30 14 8 | 25 45 29 35 44 27 27
R24 | 1466 12 47 18 15 15 39 10 | 61 47 65 59 62 40 54
XR26 |11566 26 47 31 --- 68 --- 24 | 99 105 112 --- 122 --- 107
XR28 |24599 53 --- --- --- 103 --- 74 | 104 --- --- --- 64 --- 85
------+-----------------------------------------+-------------------------------------
RMS | 1769 14 37 17 13 25 18 |T 61 72 61 57 63 51 57
WRMS | 1769 13 36 15 12 22 18 |NE 61 72 61 57 63 51 57
MEDI | 1352 12 36 17 12 17 13 |MD 48 51 44 47 57 35 42
Table 3.2408.1 GPS week: 2408 Day: 1 MJD: 61101
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1469 12 19 12 21 18 18 7 | 25 28 26 30 23 28 23
R03 | 2085 9 43 13 14 13 14 7 | 23 59 39 29 27 29 29
R04 | 1275 26 20 13 19 10 12 8 | 25 30 18 35 19 23 22
R05 | 1303 23 38 10 13 17 15 8 | 24 37 20 25 26 31 20
XR06 | 921 47 600 27 --- 73 --- 35 | 13 227 44 --- 40 --- 23
R07 | 902 6 42 11 11 14 13 6 | 24 32 25 20 31 25 23
R08 | 2606 19 41 13 12 29 17 9 | 19 30 21 17 35 29 20
R09 | 2118 8 39 18 15 13 10 7 | 64 69 48 58 63 54 56
R11 | 785 11 21 17 7 22 21 7 | 70 62 81 68 78 69 70
R12 | 1348 15 18 20 10 13 12 6 | 52 48 42 44 48 38 43
R14 | 1968 14 40 14 19 15 9 8 | 110 101 108 103 110 104 106
R15 | 1087 15 30 15 10 12 19 7 | 110 103 111 98 105 93 103
R16 | 1464 21 48 14 14 20 17 9 | 93 69 84 75 85 81 81
XR17 | 1329 7 38 22 11 13 --- 8 | 38 30 57 45 38 --- 41
R18 | 809 9 27 11 17 19 11 6 | 34 38 33 33 28 25 29
XR19 | 1743 11 21 15 --- 16 16 7 | 15 22 25 --- 22 19 16
R20 | 2666 10 24 16 10 60 17 12 | 13 24 14 16 39 21 9
R21 | 1049 13 40 13 17 28 24 9 | 48 45 43 42 55 32 41
R22 | 2022 14 38 16 19 24 18 9 | 20 34 30 29 38 24 23
R24 | 1474 15 36 24 13 14 36 10 | 45 36 52 44 43 32 41
XR26 | 9985 29 48 22 --- 62 --- 23 | 76 83 85 --- 89 --- 83
XR28 |21340 49 --- --- --- 68 --- 58 | 44 --- --- --- 118 --- 68
------+-----------------------------------------+-------------------------------------
RMS | 1657 15 34 15 15 23 18 |T 44 57 47 45 52 42 44
WRMS | 1657 15 34 16 14 21 18 |NE 44 57 47 45 52 42 44
MEDI | 1464 14 38 15 13 17 16 |MD 34 38 42 35 39 29 29
Table 3.2408.2 GPS week: 2408 Day: 2 MJD: 61102
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 976 13 24 14 18 8 17 6 | 22 28 22 26 19 17 18
R03 | 3957 11 21 12 18 14 18 6 | 34 39 29 35 28 28 30
R04 | 884 15 41 18 13 14 11 7 | 28 46 28 29 27 23 26
R05 | 2127 22 37 20 9 12 7 8 | 30 31 31 23 17 21 21
XR06 | 947 40 618 24 --- 69 --- 32 | 14 215 34 --- 52 --- 25
R07 | 1650 10 50 20 16 17 13 8 | 34 47 31 36 28 37 31
R08 | 2148 19 57 14 25 25 31 11 | 25 45 28 30 29 23 23
R09 | 1632 8 35 15 8 23 11 7 | 45 72 59 46 34 51 47
R11 | 658 12 32 17 20 20 17 8 | 67 48 76 54 74 62 65
R12 | 1608 8 23 20 19 14 16 7 | 65 60 77 53 73 53 63
R14 | 1306 10 28 14 17 10 14 6 | 125 123 113 115 113 120 117
R15 | 1546 9 35 16 12 9 17 6 | 81 95 63 74 81 73 74
R16 | 736 17 58 13 19 14 20 9 | 83 51 79 84 69 61 74
XR17 | 1312 8 29 12 16 14 --- 7 | 40 35 41 48 42 --- 40
R18 | 646 8 20 7 12 10 13 5 | 40 44 42 42 42 37 39
XR19 | 1456 10 16 21 --- 15 13 7 | 22 27 31 --- 24 25 22
R20 | 1541 9 22 22 27 78 19 16 | 17 20 28 32 58 21 18
R21 | 1322 13 54 9 15 14 21 8 | 53 45 48 48 46 44 46
R22 | 1397 11 55 11 25 16 12 8 | 13 48 21 33 21 19 16
R24 | 1470 19 32 15 15 12 28 9 | 46 36 44 40 39 28 37
XR26 |10187 30 40 18 --- 59 --- 21 | 99 95 96 --- 115 --- 100
XR28 |19027 53 --- --- --- 78 --- 64 | 119 --- --- --- 75 --- 94
------+-----------------------------------------+-------------------------------------
RMS | 1684 13 39 16 18 24 18 |T 50 59 48 47 50 41 46
WRMS | 1684 13 35 16 18 31 18 |NE 50 59 48 47 50 41 46
MEDI | 1456 11 35 15 16 14 16 |MD 40 46 41 40 42 28 37
Table 3.2408.3 GPS week: 2408 Day: 3 MJD: 61103
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 841 8 26 11 15 17 12 6 | 28 22 34 30 36 28 26
R03 | 2598 10 28 9 10 11 11 5 | 29 38 27 32 27 28 28
R04 | 845 10 28 11 19 18 21 7 | 32 45 30 39 30 31 30
R05 | 1740 8 36 16 9 19 19 7 | 34 42 43 39 29 38 35
XR06 | 962 29 653 25 --- 62 --- 28 | 25 192 32 --- 47 --- 28
R07 | 2198 8 54 12 24 15 10 8 | 42 45 40 46 34 36 38
R08 | 3587 11 59 14 16 14 23 9 | 27 51 28 33 33 28 27
R09 | 1974 10 24 16 6 17 11 5 | 49 60 51 52 49 48 48
R11 | 742 20 42 12 24 15 18 9 | 52 52 54 45 51 47 46
R12 | 2422 16 21 12 25 9 10 7 | 64 56 60 46 53 53 54
R14 | 1089 19 31 16 13 16 9 7 | 83 95 87 76 89 75 81
R15 | 1295 14 32 19 14 13 15 7 | 94 92 82 81 84 93 86
R16 | 761 17 55 17 16 16 12 9 | 82 57 71 79 71 65 72
XR17 | 1048 8 35 13 14 19 --- 8 | 53 46 59 49 55 --- 51
R18 | 739 7 16 14 10 20 17 6 | 44 45 45 51 53 33 43
XR19 | 1074 12 19 19 --- 15 15 7 | 23 26 27 --- 22 26 20
R20 | 1632 11 16 15 22 68 20 13 | 25 32 25 29 54 23 21
R21 | 1079 13 57 18 13 16 22 9 | 50 33 54 39 48 32 42
R22 | 2240 13 48 21 19 16 10 8 | 18 35 24 31 24 23 18
R24 | 878 10 45 29 11 9 25 9 | 63 42 79 57 60 46 58
XR26 |13060 36 49 20 --- 62 --- 24 | 35 54 41 --- 68 --- 42
XR28 |15514 87 --- --- --- 130 --- 106 | 134 --- --- --- 53 --- 83
------+-----------------------------------------+-------------------------------------
RMS | 1763 13 39 16 16 22 16 |T 49 55 47 47 48 41 44
WRMS | 1763 12 35 15 17 28 16 |NE 49 55 47 47 48 41 44
MEDI | 1089 11 35 16 14 16 15 |MD 42 45 43 45 49 33 42
Table 3.2408.4 GPS week: 2408 Day: 4 MJD: 61104
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 746 11 29 13 14 15 15 6 | 30 29 33 28 31 28 27
R03 | 2326 9 15 11 10 13 11 5 | 32 43 39 31 30 30 32
R04 | 1465 9 26 11 12 13 15 6 | 29 37 23 34 28 25 26
R05 | 1887 11 27 10 11 12 11 5 | 26 26 21 34 31 25 24
XR06 | 946 23 652 29 --- 70 --- 29 | 9 150 20 --- 42 --- 13
R07 | 3078 11 56 9 12 13 11 7 | 34 52 37 37 27 35 34
R08 | 3480 18 53 17 22 14 10 9 | 26 42 29 40 26 33 28
R09 | 1858 12 34 11 11 17 10 6 | 45 66 50 47 50 48 48
R11 | 1019 11 27 12 16 25 13 7 | 79 76 85 76 76 80 78
R12 | 2923 18 27 16 31 15 9 8 | 61 59 61 36 49 44 49
R14 | 1173 9 30 11 13 12 14 6 | 144 138 147 143 143 148 144
R15 | 1900 13 33 11 18 25 13 7 | 88 95 87 90 80 78 84
R16 | 766 20 52 20 14 13 18 9 | 82 50 63 72 69 61 66
XR17 | 891 12 30 9 12 11 --- 6 | 53 40 51 51 56 --- 50
R18 | 1013 15 21 14 17 32 8 8 | 45 49 51 47 74 52 51
XR19 | 1100 10 24 18 --- 13 18 8 | 18 27 30 --- 26 25 21
R20 | 1508 14 22 12 9 49 20 10 | 17 27 30 22 39 22 20
R21 | 990 12 57 17 21 10 20 9 | 61 39 63 53 54 48 53
R22 | 1205 11 54 17 28 16 11 9 | 16 38 23 30 24 15 15
R24 | 844 13 55 24 14 20 28 10 | 61 27 66 58 61 39 53
XR26 | 9825 26 46 33 --- 66 --- 24 | 95 106 95 --- 109 --- 96
XR28 |14277 66 --- --- --- 95 --- 79 | 119 --- --- --- 97 --- 99
------+-----------------------------------------+-------------------------------------
RMS | 1852 13 39 14 17 21 15 |T 53 57 52 51 55 46 50
WRMS | 1852 13 35 14 16 24 15 |NE 53 57 52 51 55 46 50
MEDI | 1205 12 30 13 14 15 13 |MD 45 43 50 40 49 35 48
Table 3.2408.5 GPS week: 2408 Day: 5 MJD: 61105
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 774 14 14 13 13 26 12 7 | 23 29 26 22 18 19 19
R03 | 2052 10 27 13 15 15 7 6 | 27 48 30 37 37 36 33
R04 | 1617 9 19 12 9 18 15 6 | 26 30 29 31 44 27 28
R05 | 1031 8 27 7 6 7 12 4 | 24 29 21 25 22 18 21
XR06 | 981 25 640 31 --- 80 --- 32 | 30 176 46 --- 46 --- 34
R07 | 3351 9 36 25 20 11 21 9 | 23 45 37 27 18 23 23
R08 | 3503 23 35 14 20 23 27 10 | 20 28 19 22 28 30 21
R09 | 1326 9 25 14 9 18 13 6 | 32 36 39 32 42 31 33
R11 | 2071 16 28 21 27 19 25 10 | 34 70 39 57 53 27 39
R12 | 1786 18 22 18 19 24 14 8 | 59 55 58 49 40 40 48
R14 | 1272 8 29 7 14 11 9 5 | 72 80 78 74 79 77 75
R15 | 1912 12 34 13 18 14 19 7 | 66 74 63 53 65 60 61
R16 | 462 14 66 21 9 12 19 10 | 74 53 85 68 76 58 70
XR17 | 1267 10 33 19 24 27 --- 10 | 42 31 56 44 62 --- 45
R18 | 1465 15 12 15 12 35 12 8 | 41 47 55 49 69 42 48
XR19 | 1183 12 33 13 --- 20 14 8 | 15 29 26 --- 32 18 19
R20 | 1343 15 18 13 8 42 15 9 | 11 18 23 23 27 18 14
R21 | 850 8 49 16 13 9 13 7 | 54 52 58 59 45 51 52
R22 | 1161 10 36 15 16 19 13 7 | 17 25 22 26 25 22 18
R24 | 1337 9 46 22 17 27 24 10 | 53 39 63 62 64 45 54
XR26 | 8875 22 60 31 --- 63 --- 24 | 87 82 85 --- 89 --- 84
XR28 |16276 42 --- --- --- 74 --- 56 | 67 --- --- --- 119 --- 65
------+-----------------------------------------+-------------------------------------
RMS | 1791 13 33 16 15 21 17 |T 40 51 45 42 50 35 41
WRMS | 1791 13 32 15 14 22 17 |NE 40 51 45 42 50 35 41
MEDI | 1337 12 33 15 14 19 14 |MD 32 45 39 37 44 30 34
Table 3.2408.6 GPS week: 2408 Day: 6 MJD: 61106
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 892 12 29 12 11 13 15 6 | 38 36 32 38 29 33 32
R03 | 1905 7 35 20 11 7 9 6 | 43 71 45 45 45 45 44
R04 | 983 11 23 13 17 11 9 5 | 46 57 36 43 46 41 42
R05 | 1060 10 32 14 11 12 17 6 | 40 52 48 44 48 42 42
XR06 | 940 26 623 41 --- 74 --- 33 | 38 183 65 --- 70 --- 48
R07 | 2602 10 25 7 23 10 29 8 | 46 47 42 53 39 43 43
R08 | 2134 16 41 19 19 14 22 9 | 31 65 40 41 39 35 36
R09 | 860 7 25 13 9 19 9 5 | 35 42 31 33 47 36 35
R11 | 1553 13 27 18 25 11 11 7 | 57 78 66 67 72 54 62
R12 | 1820 22 22 26 17 12 12 8 | 75 62 67 54 55 53 61
R14 | 825 13 36 17 13 9 11 6 | 87 98 76 82 81 79 81
R15 | 1122 9 26 9 13 8 17 5 | 88 97 79 83 79 73 81
R16 | 987 13 53 25 16 13 19 9 | 91 50 101 79 85 71 83
XR17 | 778 8 38 12 15 24 --- 8 | 71 49 75 74 89 --- 73
R18 | 1081 8 24 15 18 18 12 6 | 63 74 72 65 82 55 66
XR19 | 800 15 20 26 --- 13 11 8 | 24 29 42 --- 33 30 29
R20 | 1764 13 28 13 13 45 18 10 | 19 28 21 23 53 22 20
R21 | 850 10 49 10 30 15 28 10 | 78 51 83 88 74 58 73
R22 | 1107 12 49 9 13 19 10 7 | 26 53 29 30 32 26 26
R24 | 856 9 52 13 23 45 24 12 | 81 47 83 72 100 61 75
XR26 | 8252 30 39 37 --- 76 --- 27 | 113 105 109 --- 136 --- 113
XR28 |17431 41 --- --- --- 64 --- 51 | 84 --- --- --- 60 --- 65
------+-----------------------------------------+-------------------------------------
RMS | 1418 12 35 16 17 20 17 |T 57 65 59 56 63 47 55
WRMS | 1418 12 34 16 16 22 17 |NE 57 65 59 56 63 47 55
MEDI | 1060 12 32 14 15 13 12 |MD 46 53 65 53 55 43 48
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