[IGSREPORT-30584] Wk 2379 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 29 03:47:22 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2379 (Aug 10, 2025 - Aug 16, 2025)
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 2.2379.
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:
igl2379[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2379 in the SP3 format.
igl23797.sum Combination Report for GPS Week 2379.
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.
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
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 | 5.8 ns
1 | 1.8 ns
2 | 4.7 ns
3 | 4.9 ns
4 | 2.8 ns
5 | 6.5 ns
6 | 5.1 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
----+--------+---------------
3 | ESA | R20
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 1.2379, 1a.2379).
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 2.2379.0-6)
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 3.2379.0-6).
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 2379 summary. (Aug 10, 2025 - Aug 16, 2025)
Table 1.2379.a GPS week : 2379 MJD: 60897.0-60903.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 3 0 -13 20 .15 12 11 | 1442 583 3985 9769
| 0 0 1 12 10 9 .02 | 1079 2919
esa n/a| -3 -2 6 23 -23 27 -.15 30 31 | 676 400 3984 9957
| 1 1 1 16 10 60 .06 | 1102 2804
gfz n/a| 0 0 -1 32 22 -3 -.02 19 14 | 0 439 3997 9840
| 0 0 2 13 16 29 .05 | 0 2558
grg n/a| 2 1 1 -48 -5 -29 .35 21 18 | 4483 40 3503 9094
| 1 0 3 21 21 39 .04 | 977 2337
iac n/a| 0 0 -2 8 23 -22 -.15 18 16 | 7810 53 4090 11797
| 1 1 1 16 31 55 .05 | 1187 1559
jgx n/a| 0 1 -6 -25 -18 -22 -.25 17 17 | 2185 -80 3533 9323
| 1 1 1 14 16 17 .03 | 1608 2405
Table 1.2379.b GPS week : 2379 MJD: 60897.0-60903.0
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 9 8 8 8 7 7 |
R03 | 6 6 6 10 8 7 6 |
R04 | 6 6 6 7 8 8 5 |
R05 | 6 6 6 5 9 7 5 |
R07 | 10 8 7 7 6 7 8 |
R08 | 11 10 10 10 9 7 7 |
R09 | 7 7 7 6 7 6 6 |
R11 | 9 10 7 8 7 10 6 |
R12 | 7 6 6 5 6 7 6 |
R14 | 6 5 5 6 6 7 6 |
R15 | 6 6 6 6 6 6 6 |
R16 | 6 7 6 6 6 7 6 |
R17 | 6 6 6 6 7 7 6 |
R18 | 7 5 6 7 8 8 7 |
R19 | 10 9 9 10 9 10 10 |
R20 | 22 20 19 15 23 24 19 |
R21 | 7 6 7 7 6 7 6 |
R22 | 9 8 9 7 8 7 8 |
R24 | 8 7 9 7 8 8 7 |
R25 | 52 87 79 68 87 67 46 |
R26 | 35 30 28 30 28 31 29 |
R27 | 27 32 28 31 27 26 27 |
Table 1.2379.c GPS week : 2379 MJD: 60897.0-60903.0
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 2379 0 | -16 106 -3 1550 -994 -805 76.5 1966 1966 | 5788 0
brd 2379 1 | -137 81 -53 -2515 270 -1376 80.4 2141 2141 | 1757 0
brd 2379 2 | 10 0 -53 1936 1016 843 80.9 2256 2256 | 4680 0
brd 2379 3 | -30 -28 31 -973 2131 1761 81.1 1877 1877 | 4855 0
brd 2379 4 | 226 21 69 -1755 2868 3717 80.9 1690 1690 | 2833 0
brd 2379 5 | -3 -4 64 -2523 3813 1779 81.0 2086 2086 | 6520 0
brd 2379 6 | 62 69 9 527 -1696 -2048 79.9 2115 2115 | 5098 0
-------------+------------------------------------------------------------+----------------
brd 2379 mean| 15 34 9 -536 1058 552 80.1 2018 2018 | 4504 0
brd 2379 sdev| 110 50 50 1876 2018 2057 1.6 189 189 | 1661 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 2.2379.0 GPS week: 2379 Day: 0 MJD: 60897
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 5 -4 -3 22 .15 14 11 | 934 4294 5203 9409
esa n/a| -1 -3 9 -4 -38 -10 -.06 27 30 | -97 4741 5209 9915
gfz n/a| 0 1 0 47 -8 34 .06 22 14 | 0 3680 5252 9119
grg n/a| 3 2 0 -50 -33 -109 .34 35 29 | 4922 1863 3403 8210
iac n/a| 1 1 -3 9 64 -4 -.09 15 14 | 7369 2443 5200 11123
jgx n/a| 0 0 -6 -26 -43 -29 -.25 16 16 | 2897 1154 3401 7802
Table 2.2379.1 GPS week: 2379 Day: 1 MJD: 60898
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 4 24 -2 14 .12 12 10 | 2581 -3954 3708 9198
esa n/a| -5 -3 6 14 -29 88 -.13 30 32 | 2248 -3856 3706 9372
gfz n/a| 0 0 -5 21 30 0 .03 18 15 | 0 -3311 3491 8600
grg n/a| 2 0 6 -62 -31 4 .38 23 21 | 3508 -3210 3502 9304
iac n/a| 0 2 -1 10 -2 -15 -.14 18 16 | 6818 -811 3978 11853
jgx n/a| 2 1 -5 -37 -14 -30 -.23 17 17 | 1313 -2497 3324 8755
Table 2.2379.2 GPS week: 2379 Day: 2 MJD: 60899
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 4 -1 0 26 .13 12 10 | 504 -86 3029 10763
esa n/a| -2 -1 5 45 -26 -51 -.26 30 35 | -944 320 3021 11184
gfz n/a| 1 0 -3 25 36 11 -.05 17 14 | 0 -303 3016 10707
grg n/a| 2 0 2 -31 -5 -36 .39 15 13 | 4732 31 3126 10837
iac n/a| 0 1 -2 -1 -12 0 -.15 20 17 | 7909 1041 3100 13878
jgx n/a| 0 2 -6 -3 -3 -13 -.27 18 18 | 231 -430 3139 11129
Table 2.2379.3 GPS week: 2379 Day: 3 MJD: 60900
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 3 -17 17 .14 11 10 | 868 1195 4402 11667
esa n/a| -2 -2 5 31 -21 -27 -.16 34 44 | 343 1199 4380 11897
gfz n/a| 1 0 -3 37 14 -43 -.07 20 18 | 0 1487 4470 11842
grg n/a| 2 1 3 -59 21 5 .32 18 15 | 3715 2646 4011 10487
iac n/a| 0 0 -3 -1 36 44 -.13 18 15 | 9432 -1976 4633 13362
jgx n/a| 1 1 -6 -20 -25 -51 -.26 16 16 | 538 3467 4169 10928
Table 2.2379.4 GPS week: 2379 Day: 4 MJD: 60901
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 -8 -21 19 .15 12 11 | 361 -1430 4418 10177
esa n/a| -5 0 6 22 -29 92 -.11 30 25 | 256 -1652 4420 10000
gfz n/a| 1 0 -1 41 14 21 -.02 19 14 | 0 -1521 4521 10739
grg n/a| 0 0 -1 -38 -6 -39 .31 22 20 | 4047 -2887 3596 8537
iac n/a| 3 -1 -2 39 61 -136 -.15 20 18 | 6131 -1482 4440 11327
jgx n/a| 0 1 -5 -47 -9 -3 -.28 18 18 | 3204 -3454 3602 9296
Table 2.2379.5 GPS week: 2379 Day: 5 MJD: 60902
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 -24 37 .18 15 14 | 3176 70 3459 8408
esa n/a| -3 -2 9 20 -18 13 -.12 28 22 | 1653 -493 3469 8549
gfz n/a| -1 0 2 9 36 -41 -.00 21 12 | 0 -330 3476 8793
grg n/a| 3 0 -2 -82 -1 -15 .42 22 17 | 6376 -78 3471 8003
iac n/a| 0 0 -4 17 15 -4 -.17 18 16 | 9157 330 3492 10346
jgx n/a| 0 1 -5 -24 1 -1 -.20 18 18 | 4767 -484 3554 8732
Table 2.2379.6 GPS week: 2379 Day: 6 MJD: 60903
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 -13 -21 6 .16 11 10 | 1672 3996 3679 8762
esa n/a| -3 -2 5 36 -4 85 -.18 27 30 | 1276 2541 3686 8782
gfz n/a| 0 0 0 41 32 -7 -.05 17 13 | 0 3375 3758 9081
grg n/a| 2 1 0 -18 18 -11 .31 15 11 | 4081 1920 3416 8283
iac n/a| -2 0 0 -12 -2 -39 -.24 17 16 | 7857 830 3787 10690
jgx n/a| 1 0 -8 -15 -33 -29 -.28 18 18 | 2349 1684 3543 8620
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 3.2379.0 GPS week: 2379 Day: 0 MJD: 60897
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1605 11 22 13 25 11 19 7 | 102 81 105 104 111 86 98
R03 | 2017 9 13 9 24 15 16 6 | 97 85 95 95 101 86 94
R04 | 1049 7 12 16 23 10 16 6 | 96 94 101 95 100 94 97
R05 | 1060 5 14 13 32 7 11 5 | 95 87 100 109 98 83 94
R07 | 1314 9 31 15 35 30 19 10 | 98 85 94 121 116 86 98
R08 | 1604 15 25 42 38 12 22 11 | 90 82 127 125 113 84 100
R09 | 1888 9 28 11 26 12 17 7 | 53 53 53 54 57 42 51
R11 | 1302 21 25 8 44 12 12 8 | 39 36 40 37 37 42 36
R12 | 1067 13 14 12 31 8 17 6 | 53 54 53 60 48 50 50
R14 | 869 5 10 13 39 12 9 6 | 44 45 48 63 43 43 45
R15 | 2552 12 15 15 26 9 11 6 | 70 72 75 76 71 74 71
R16 | 4391 10 24 16 18 12 6 6 | 69 69 64 66 71 64 67
R17E | 1688 8 19 13 24 13 6 5 | 68 70 68 63 60 61 64
R18E | 2063 10 21 14 39 6 7 6 | 62 64 61 66 62 61 61
XR19E | 6414 16 20 14 --- 17 --- 9 | 40 45 47 --- 46 --- 43
R20E | 2670 36 78 65 63 33 36 21 | 60 50 87 69 70 62 60
R21E | 1700 10 23 10 35 13 11 7 | 51 55 53 67 46 47 50
XR22E | 845 14 15 14 47 12 --- 9 | 30 35 37 66 34 --- 34
R24E | 1566 11 20 18 39 16 11 7 | 97 102 100 112 101 100 99
XR25E |15741 49 --- --- --- 54 --- 51 | 99 --- --- --- 79 --- 86
XR26 |15030 44 68 64 --- 66 --- 34 | 38 91 45 --- 80 --- 48
XR27 |15380 48 55 --- 34 45 --- 27 | 38 88 --- 47 71 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 1966 14 27 22 35 15 16 |T 67 68 72 78 73 68 68
WRMS | 1966 11 30 14 29 14 16 |NE 70 73 76 80 79 69 71
MEDI | 1688 11 21 14 34 12 12 |MD 62 70 64 67 71 64 61
Table 3.2379.1 GPS week: 2379 Day: 1 MJD: 60898
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1963 6 21 23 16 24 25 9 | 72 62 85 63 85 59 71
R03 | 2155 8 29 9 15 12 15 6 | 63 50 68 72 65 59 62
R04 | 1187 8 18 12 11 16 18 6 | 67 70 69 71 73 58 66
R05 | 1445 11 17 12 26 8 9 6 | 73 65 71 50 66 60 64
R07 | 1548 11 26 14 19 25 18 8 | 63 46 52 56 72 50 56
R08 | 1878 13 33 20 29 22 19 9 | 55 49 71 78 74 52 62
R09 | 1471 8 28 10 19 17 12 6 | 38 36 39 49 48 33 39
R11 | 1630 15 46 12 31 20 15 9 | 24 46 30 44 27 31 22
R12 | 2115 9 18 16 15 14 7 5 | 36 38 35 45 28 38 34
R14 | 948 11 11 11 13 15 9 5 | 26 35 36 36 41 27 30
R15 | 2050 8 17 11 22 16 12 6 | 48 45 46 49 46 40 44
R16 | 4195 8 27 17 25 11 12 7 | 43 56 51 37 44 40 43
R17E | 1788 7 18 11 21 11 8 5 | 55 54 53 57 50 46 51
R18E | 1645 11 18 8 17 11 9 5 | 40 42 40 40 37 39 38
XR19E | 6007 14 15 13 --- 16 --- 8 | 25 36 37 --- 33 --- 30
R20E | 3580 29 78 51 42 33 40 19 | 45 41 69 48 52 49 43
R21E | 1665 10 18 14 21 10 14 6 | 38 36 33 41 33 33 32
XR22E | 1260 13 18 11 24 9 --- 7 | 20 24 28 37 23 --- 22
R24E | 2543 12 12 10 30 16 11 6 | 74 82 73 80 77 72 73
XR25E |25162 64 --- --- --- 117 --- 87 | 90 --- --- --- 82 --- 77
XR26 |13333 36 86 36 --- 67 --- 30 | 32 71 29 --- 49 --- 32
XR27 |11440 41 78 --- 46 67 --- 32 | 33 58 --- 45 42 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 2140 12 30 18 23 18 17 |T 48 49 50 52 52 46 46
WRMS | 2140 10 32 15 21 16 17 |NE 48 51 52 53 54 45 46
MEDI | 1878 11 18 12 21 16 12 |MD 43 46 46 49 48 46 43
Table 3.2379.2 GPS week: 2379 Day: 2 MJD: 60899
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2668 6 22 23 12 27 20 8 | 82 69 101 78 100 73 84
R03 | 1471 10 18 12 12 11 20 6 | 82 74 79 79 70 65 75
R04 | 864 9 22 7 13 15 11 5 | 76 73 68 79 70 67 72
R05 | 1376 11 18 13 9 13 16 5 | 79 70 73 75 77 64 73
R07 | 1895 8 21 11 10 16 21 6 | 81 72 84 80 82 72 78
R08 | 2004 14 35 9 14 42 15 9 | 72 69 80 85 109 73 79
R09 | 1038 13 20 17 16 19 8 7 | 28 35 34 30 33 28 28
R11 | 2364 10 19 17 21 16 11 7 | 21 38 29 33 23 22 23
R12 | 1451 7 19 18 12 20 11 6 | 50 55 62 57 55 49 52
R14 | 1424 9 20 10 7 16 8 5 | 38 25 37 39 39 29 34
R15 | 1323 8 13 16 11 11 13 5 | 51 48 56 59 54 40 51
R16 | 3015 5 16 17 9 19 13 6 | 55 56 63 63 58 50 56
R17E | 2094 7 13 12 14 15 11 5 | 55 59 58 64 48 53 55
R18E | 1920 8 19 16 13 15 11 5 | 53 54 55 57 48 60 54
XR19E | 1083 14 16 17 --- 16 --- 9 | 29 37 39 --- 32 --- 32
R20E | 3705 27 89 38 28 32 46 18 | 57 43 62 51 43 67 49
R21E | 3217 12 30 14 16 8 17 7 | 44 50 47 53 40 39 43
XR22E | 1068 17 21 16 18 16 --- 8 | 25 29 39 41 28 --- 29
R24E | 3630 17 22 16 27 23 17 9 | 96 99 104 121 96 109 103
XR25E |22250 55 --- --- --- 113 --- 79 | 101 --- --- --- 90 --- 90
XR26 |10694 34 86 30 --- 61 --- 28 | 32 65 31 --- 34 --- 25
XR27 | 9792 38 82 --- 21 62 --- 27 | 33 67 --- 22 37 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2255 12 30 17 15 20 18 |T 56 56 60 61 57 56 55
WRMS | 2255 10 35 14 13 17 18 |NE 55 58 61 59 60 52 53
MEDI | 1920 10 20 16 13 16 13 |MD 53 56 58 59 48 60 52
Table 3.2379.3 GPS week: 2379 Day: 3 MJD: 60900
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2244 6 27 15 13 30 19 8 | 89 74 98 93 112 82 91
R03 | 1362 6 33 18 24 23 28 9 | 84 73 97 103 98 72 87
R04 | 975 13 26 11 12 13 14 6 | 80 83 72 82 72 70 76
R05 | 1965 10 15 17 8 9 7 5 | 83 75 71 80 79 76 78
R07 | 1321 6 19 29 16 11 12 7 | 84 84 105 77 77 75 82
R08 | 1509 14 16 25 21 33 23 10 | 84 87 114 104 119 82 96
R09 | 1106 8 25 13 13 9 14 6 | 34 32 37 31 26 35 31
R11 | 1712 12 29 17 23 15 16 8 | 23 31 29 26 25 23 19
R12 | 1207 9 23 13 6 9 10 5 | 35 52 46 40 39 41 39
R14 | 948 8 12 16 15 19 8 5 | 43 46 36 54 52 42 44
R15 | 1217 8 16 11 23 11 8 5 | 48 46 45 66 50 46 49
R16 | 2066 11 15 21 13 10 14 6 | 47 57 61 57 54 40 49
R17E | 1911 7 18 14 22 12 10 6 | 59 62 61 65 52 52 57
R18E | 1990 10 19 21 17 11 13 6 | 57 64 58 68 55 55 57
XR19E | 865 14 16 23 --- 11 --- 9 | 41 49 61 --- 43 --- 46
R20E | 2973 27 109 43 24 29 29 15 | 67 59 77 63 60 74 64
R21E | 2766 12 26 13 20 17 14 7 | 56 60 56 60 47 50 52
XR22E | 1131 13 18 12 16 11 --- 7 | 34 41 47 46 35 --- 37
R24E | 2787 8 18 19 22 12 10 6 | 58 57 61 74 60 60 60
XR25E |13204 49 --- --- --- 93 --- 68 | 109 --- --- --- 98 --- 100
XR26 | 9026 36 79 39 --- 63 --- 29 | 47 73 49 --- 45 --- 40
XR27 | 6866 47 69 --- 26 71 --- 31 | 30 68 --- 27 56 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1876 11 34 20 18 18 16 |T 58 60 64 64 61 57 58
WRMS | 1876 10 44 18 15 15 16 |NE 57 62 66 64 64 57 57
MEDI | 1712 10 19 17 17 12 14 |MD 56 60 61 65 54 55 52
Table 3.2379.4 GPS week: 2379 Day: 4 MJD: 60901
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2056 8 16 16 23 22 26 8 | 79 66 86 76 92 60 76
R03 | 1218 10 26 15 21 25 13 8 | 76 64 82 85 94 72 78
R04 | 1121 7 21 13 29 14 18 7 | 72 70 81 98 77 63 75
R05 | 951 11 16 20 28 16 23 8 | 71 64 75 65 75 52 66
R07 | 1725 10 21 11 11 11 13 5 | 74 57 70 75 61 61 66
R08 | 1084 12 26 14 20 28 17 8 | 68 58 72 76 88 64 70
R09 | 1110 14 16 11 18 19 13 6 | 36 38 41 42 33 37 36
R11 | 2011 12 19 8 16 11 23 6 | 18 21 22 16 20 32 18
R12 | 997 11 14 10 10 21 11 5 | 37 42 45 38 53 40 41
R14 | 2312 6 17 12 19 12 13 5 | 33 41 30 47 30 24 31
R15 | 1364 11 9 18 14 13 7 5 | 50 48 54 50 58 42 49
R16 | 1072 14 15 14 16 12 11 6 | 46 51 52 58 51 55 50
R17E | 1584 10 15 14 24 10 12 6 | 52 50 57 55 45 43 49
R18E | 1437 13 17 14 33 16 18 8 | 53 56 48 67 55 50 52
XR19E | 1087 15 17 14 --- 15 --- 9 | 28 41 43 --- 41 --- 35
R20E | 2950 24 100 56 33 46 42 22 | 62 46 87 53 54 64 58
R21E | 2111 10 15 11 16 16 12 6 | 37 39 41 47 41 34 37
XR22E | 1368 14 17 10 20 13 --- 7 | 20 30 29 40 23 --- 24
R24E | 2035 12 21 16 30 24 6 8 | 77 82 78 86 89 78 79
XR25E |12185 63 --- --- --- 119 --- 86 | 79 --- --- --- 75 --- 60
XR26 | 7446 39 75 30 --- 58 --- 28 | 18 70 27 --- 41 --- 23
XR27 | 6521 32 50 --- 41 67 --- 27 | 28 61 --- 27 62 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1689 12 30 19 22 20 18 |T 50 52 56 57 57 51 50
WRMS | 1689 11 25 14 20 18 18 |NE 50 53 56 57 59 50 51
MEDI | 1437 12 17 14 20 16 13 |MD 50 51 52 55 54 52 49
Table 3.2379.5 GPS week: 2379 Day: 5 MJD: 60902
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2301 9 13 14 18 14 23 7 | 64 65 62 70 62 53 61
R03 | 892 12 16 11 15 19 13 6 | 68 54 58 61 72 56 61
R04 | 959 12 18 15 17 24 15 7 | 66 58 63 64 81 62 65
R05 | 1042 7 18 12 16 14 18 6 | 59 63 70 76 70 54 64
R07 | 4628 14 23 13 14 10 12 6 | 64 46 49 66 55 49 54
R08 | 1007 11 16 11 13 14 22 6 | 56 47 53 57 57 44 52
R09 | 2125 14 21 8 13 9 9 5 | 44 42 42 41 44 40 41
R11 | 1825 25 29 14 38 14 9 10 | 21 36 28 36 21 25 20
R12 | 1007 11 19 9 14 21 17 7 | 38 55 43 50 49 31 42
R14 | 2621 13 21 9 15 12 17 6 | 32 35 32 38 23 23 27
R15 | 1189 8 14 10 17 9 15 5 | 43 42 48 40 42 38 41
R16 | 983 16 17 14 18 18 5 6 | 43 37 38 36 37 33 35
R17E | 1477 10 20 13 26 13 12 7 | 61 62 59 60 56 54 57
R18E | 1658 18 20 12 24 14 14 7 | 38 39 38 51 41 36 38
XR19E | 1028 16 20 14 --- 18 --- 9 | 28 35 35 --- 41 --- 33
R20E | 4030 31 86 70 42 42 43 23 | 44 41 80 45 47 58 44
R21E | 1674 13 23 15 24 9 11 7 | 40 47 47 42 34 38 38
XR22E | 2051 17 13 12 19 9 --- 7 | 21 28 31 36 27 --- 26
R24E | 1154 15 25 14 22 15 14 7 | 65 58 62 76 65 65 63
XR25E |12957 59 --- --- --- 74 --- 66 | 82 --- --- --- 95 --- 78
XR26 | 4084 44 67 37 --- 67 --- 30 | 21 57 25 --- 59 --- 30
XR27 | 7248 44 38 --- 33 54 --- 25 | 20 53 --- 52 53 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 2086 15 28 21 22 18 18 |T 46 47 48 52 51 44 45
WRMS | 2086 14 22 12 17 16 18 |NE 45 49 47 52 51 42 45
MEDI | 1658 14 20 13 18 14 14 |MD 43 47 47 51 49 44 41
Table 3.2379.6 GPS week: 2379 Day: 6 MJD: 60903
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1827 11 17 16 10 14 22 6 | 94 90 109 98 108 87 97
R03 | 1253 8 15 7 12 17 19 5 | 107 90 100 110 107 90 102
R04 | 891 4 20 8 7 13 13 4 | 103 94 105 104 105 95 101
R05 | 1059 6 19 16 10 9 8 5 | 93 88 104 96 96 90 95
R07 | 2320 7 23 19 23 12 15 7 | 95 73 88 107 92 82 91
R08 | 961 9 19 14 15 22 13 6 | 84 74 96 99 92 81 87
R09 | 2492 10 18 17 6 16 13 6 | 60 62 58 57 55 49 55
R11 | 2334 15 16 6 10 18 15 6 | 35 35 35 37 38 38 33
R12 | 1083 8 15 9 9 17 20 5 | 53 60 54 55 62 47 54
R14 | 2173 11 20 10 10 18 10 5 | 44 47 41 52 46 38 43
R15 | 2383 8 12 11 8 22 15 5 | 63 56 63 64 70 58 62
R16 | 1317 12 14 10 17 12 13 6 | 59 57 56 55 55 50 54
R17E | 1122 10 16 14 15 8 13 5 | 66 71 69 73 62 63 66
R18E | 1490 16 22 11 17 11 19 7 | 68 70 65 75 68 69 68
XR19E | 1593 13 18 19 --- 15 --- 9 | 41 50 54 --- 50 --- 46
R20E | 5257 20 86 49 28 34 44 19 | 71 60 94 71 79 82 75
R21E | 1941 9 22 12 15 16 14 6 | 55 55 62 62 52 47 54
XR22E | 1523 15 15 14 15 14 --- 7 | 29 32 42 47 36 --- 35
R24E | 1742 13 23 12 15 12 17 6 | 93 97 94 106 96 96 96
XR25E |17205 35 --- --- --- 60 --- 46 | 95 --- --- --- 74 --- 79
XR26 | 5669 34 59 43 --- 71 --- 29 | 27 85 32 --- 81 --- 39
XR27 | 6832 25 58 --- 43 68 --- 27 | 37 87 --- 37 84 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 2114 11 27 17 15 17 18 |T 66 68 71 73 73 68 67
WRMS | 2114 10 30 13 11 16 18 |NE 68 71 72 74 77 67 68
MEDI | 1742 11 19 12 15 16 15 |MD 63 70 63 71 70 69 62
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