[IGSREPORT-30574] Wk 2378 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 22 00:37:43 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2378 (Aug 03, 2025 - Aug 09, 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 2.2378.
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:
igl2378[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2378 in the SP3 format.
igl23787.sum Combination Report for GPS Week 2378.
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 | 2.3 ns
1 | 6.3 ns
2 | 7.8 ns
3 | 3.2 ns
4 | 6.4 ns
5 | 2.2 ns
6 | 2.4 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 | R20
1 | ALL | R19
2 | ALL | R19
6 | GFZ | R18 R19 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 1.2378, 1a.2378).
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 2.2378.0-6)
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 3.2378.0-6).
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 2378 summary. (Aug 03, 2025 - Aug 09, 2025)
Table 1.2378.a GPS week : 2378 MJD: 60890.0-60896.0
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 -4 -6 31 .15 12 10 | 976 -579 3595 8103
| 0 0 1 11 16 12 .03 | 1412 2440
esa n/a| -3 -2 8 22 0 -4 -.13 31 28 | 388 -728 3663 8256
| 1 1 2 18 11 58 .04 | 1894 2176
gfz n/a| 1 0 -5 18 34 -9 -.06 33 17 | 0 -619 3720 8545
| 0 0 2 19 19 27 .03 | 0 2590
grg n/a| 2 1 1 -33 2 -32 .34 23 16 | 4381 -517 3592 7791
| 0 0 2 16 20 51 .04 | 1568 2178
iac n/a| 0 0 -7 11 2 -2 -.13 17 15 | 7035 -388 3680 9500
| 1 1 3 6 28 39 .05 | 1980 1118
jgx n/a| 0 1 -3 -9 -22 -10 -.23 19 19 | 1188 -804 3746 8387
| 0 0 3 19 11 16 .03 | 1347 2590
Table 1.2378.b GPS week : 2378 MJD: 60890.0-60896.0
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 10 8 7 7 8 |
R03 | 7 8 9 6 7 7 7 |
R04 | 7 6 7 7 7 6 6 |
R05 | 5 7 5 8 6 6 7 |
R07 | 7 8 8 8 7 8 8 |
R08 | 7 8 6 7 8 8 9 |
R09 | 5 6 6 6 6 6 8 |
R11 | 9 8 10 11 9 11 9 |
R12 | 6 6 5 6 6 7 7 |
R14 | 5 5 4 6 6 6 6 |
R15 | 5 7 6 5 6 6 6 |
R16 | 6 6 7 8 6 7 8 |
R17 | 6 8 10 7 7 7 16 |
R18 | 5 8 6 7 7 7 13 |
R19 | 30 --- --- 9 7 8 11 |
R20 | 21 22 20 23 22 21 25 |
R21 | 8 7 7 10 7 6 12 |
R22 | 9 8 8 8 11 9 15 |
R24 | 7 8 8 6 8 6 10 |
R25 | 70 79 124 66 66 101 115 |
R26 | 33 32 29 29 32 32 32 |
R27 | 30 29 31 29 29 26 28 |
Table 1.2378.c GPS week : 2378 MJD: 60890.0-60896.0
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 2378 0 | 18 133 -61 584 4440 17070 80.4 1680 1680 | 2275 0
brd 2378 1 | 6 33 44 778 1637 16100 82.7 1941 1941 | 6325 0
brd 2378 2 | -42 66 82 170 2441 15670 78.9 1956 1956 | 7771 0
brd 2378 3 | 95 59 62 1889 2965 16590 79.7 2254 2254 | 3250 0
brd 2378 4 | 98 -13 -32 2187 2222 5547 79.6 2093 2093 | 6397 0
brd 2378 5 | 81 -35 -72 2251 1105 7018 77.7 1965 1965 | 2182 0
brd 2378 6 | 30 75 18 -217 1548 2050 77.7 1796 1796 | 2401 0
-------------+------------------------------------------------------------+----------------
brd 2378 mean| 41 45 5 1091 2336 11435 79.5 1954 1954 | 4371 0
brd 2378 sdev| 52 56 61 1008 1115 6328 1.7 186 186 | 2373 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 2.2378.0 GPS week: 2378 Day: 0 MJD: 60890
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 3 -5 20 47 .13 11 9 | -18 -3813 2906 7360
esa n/a| -4 -4 13 -9 -10 -39 -.16 35 25 | -571 -3329 2919 8177
gfz n/a| 2 0 -2 5 11 -30 -.09 19 14 | 0 -4149 2963 7856
grg n/a| 0 0 0 -28 20 -55 .33 19 12 | 4154 -3904 2961 7004
iac n/a| 0 1 -9 10 -51 17 -.10 16 14 | 5989 -1356 2938 9120
jgx n/a| 0 1 -4 24 -5 -11 -.24 18 18 | 659 -5262 2888 7598
Table 2.2378.1 GPS week: 2378 Day: 1 MJD: 60891
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 6 4 -11 27 .16 11 10 | -19 1377 3128 7232
esa n/a| -1 -2 6 6 -12 -69 -.16 34 29 | -480 1687 3154 7442
gfz n/a| 1 0 -5 36 13 7 -.01 25 16 | 0 1548 3190 7599
grg n/a| 2 0 2 -18 11 36 .34 18 15 | 5473 1681 3199 7098
iac n/a| 0 0 -9 6 -7 -50 -.15 16 15 | 7966 555 3125 8721
jgx n/a| 1 0 -1 5 -12 0 -.26 21 21 | -720 1121 3329 7341
Table 2.2378.2 GPS week: 2378 Day: 2 MJD: 60892
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 6 7 -30 31 .15 11 11 | 3230 1087 3526 7310
esa n/a| -3 -2 7 31 18 -4 -.08 32 24 | 3751 784 3547 7298
gfz n/a| 1 0 -9 -8 39 -40 -.03 23 18 | 0 1156 3595 7692
grg n/a| 2 0 1 -63 21 43 .32 20 15 | 7090 1074 3606 7202
iac n/a| 1 2 -11 12 0 -9 -.23 18 17 | 10431 -84 3479 8048
jgx n/a| 0 0 0 -13 -15 -37 -.23 17 17 | 2986 1677 3749 7808
Table 2.2378.3 GPS week: 2378 Day: 3 MJD: 60893
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 2 -24 2 46 .20 15 13 | -634 -386 4258 9008
esa n/a| -1 0 8 26 -2 -72 -.08 31 23 | -283 -1553 4264 8776
gfz n/a| 1 -1 -2 40 25 1 -.08 16 14 | 0 -479 4353 9541
grg n/a| 2 1 1 -34 -6 -88 .35 24 16 | 3224 -1038 4432 9137
iac n/a| 0 0 -9 5 3 49 -.09 18 16 | 5374 -688 4730 10029
jgx n/a| 0 0 -1 -26 -29 6 -.23 20 20 | 307 -1344 4677 9864
Table 2.2378.4 GPS week: 2378 Day: 4 MJD: 60894
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 -3 0 36 .13 13 11 | 2314 2578 3277 9045
esa n/a| -6 -1 6 46 10 42 -.13 31 35 | 2363 1974 3319 9322
gfz n/a| 1 -1 -3 33 35 0 -.09 21 15 | 0 2724 3344 9411
grg n/a| 3 2 5 -44 -7 -49 .30 18 12 | 4890 1990 3261 8407
iac n/a| 1 0 -8 23 9 -27 -.15 15 13 | 8437 1359 3332 9893
jgx n/a| 0 0 -4 -33 -37 -16 -.17 21 21 | 2872 1951 3351 8915
Table 2.2378.5 GPS week: 2378 Day: 5 MJD: 60895
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 4 -16 -12 15 .13 10 10 | 462 -1534 3722 7853
esa n/a| -4 -2 7 30 -1 42 -.14 27 29 | -716 -1881 4098 7827
gfz n/a| 2 0 -3 23 47 -35 -.05 20 18 | 0 -1806 4094 8411
grg n/a| 2 1 0 -15 -36 -55 .31 22 14 | 2532 -1377 3435 7667
iac n/a| 2 0 -3 5 34 42 -.13 18 17 | 4904 -562 3739 9886
jgx n/a| 0 2 -9 -8 -32 7 -.22 21 21 | 873 -1500 3722 8427
Table 2.2378.6 GPS week: 2378 Day: 6 MJD: 60896
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 5 -17 16 .15 12 9 | 1499 -3367 4350 8918
esa n/a| -3 -4 8 30 -1 73 -.19 28 31 | -1342 -2782 4346 8951
gfz n/a| 1 0 -8 1 65 34 -.06 106 24 | 0 -3328 4507 9308
grg n/a| 2 1 1 -30 10 -56 .43 38 28 | 3307 -2049 4255 8027
iac n/a| 1 2 -3 16 31 -40 -.09 17 16 | 6150 -1942 4421 10807
jgx n/a| 1 1 -4 -13 -23 -24 -.23 19 19 | 1342 -2271 4508 8756
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 3.2378.0 GPS week: 2378 Day: 0 MJD: 60890
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1083 6 19 11 15 9 24 6 | 79 63 83 81 88 55 75
R03 | 1579 13 17 12 14 12 27 7 | 79 61 71 74 80 54 70
R04 | 1817 8 17 17 11 16 21 6 | 71 65 75 69 71 52 67
R05 | 1106 7 18 14 14 11 9 5 | 74 66 84 73 72 67 73
R07 | 1704 13 35 13 13 10 16 7 | 73 49 71 65 72 55 65
R08 | 1118 10 27 16 10 19 13 6 | 66 64 82 78 80 60 71
R09 | 1334 9 13 17 9 8 12 5 | 35 30 44 33 39 41 36
R11 | 1459 13 43 10 25 9 25 9 | 35 49 34 40 34 32 33
R12 | 1066 6 22 13 8 20 7 5 | 53 58 47 54 58 51 53
R14 | 1066 5 13 18 12 8 5 4 | 45 49 47 46 47 46 46
R15 | 1190 9 16 11 11 11 9 5 | 68 68 58 65 55 61 62
R16 | 1631 7 25 13 15 18 8 6 | 64 80 67 63 54 63 63
R17E | 1447 9 19 14 12 12 10 5 | 77 72 76 79 74 79 76
R18E | 1139 5 27 12 13 9 8 5 | 61 52 69 65 61 64 61
XR19E |10156 25 --- 65 --- 35 --- 29 | 49 --- 66 --- 53 --- 44
R20E | 3227 25 108 53 54 39 43 21 | 102 95 133 116 108 100 104
R21E | 1707 15 27 20 25 14 13 8 | 43 38 49 57 48 40 44
XR22E | 721 14 32 17 22 9 --- 9 | 40 48 48 48 40 --- 41
R24E | 2944 11 24 14 16 16 11 6 | 36 29 31 40 40 35 33
XR25E |11529 54 --- --- --- 89 --- 69 | 114 --- --- --- 66 --- 78
XR26 | 8324 32 81 63 --- 68 --- 32 | 27 108 34 --- 78 --- 41
XR27 | 6766 48 79 --- 23 61 --- 30 | 30 109 --- 46 77 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1680 11 35 19 19 16 18 |T 60 62 63 62 63 56 58
WRMS | 1680 9 25 14 12 14 18 |NE 57 65 61 60 64 53 57
MEDI | 1459 10 24 14 14 12 12 |MD 61 61 66 65 61 55 61
Table 3.2378.1 GPS week: 2378 Day: 1 MJD: 60891
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 940 6 26 14 10 20 26 7 | 51 45 51 51 60 36 49
R03 | 1496 10 23 12 11 12 31 7 | 61 43 59 59 59 34 54
R04 | 1911 14 11 17 14 12 15 6 | 53 47 41 50 43 38 45
R05 | 1207 9 17 24 15 17 14 7 | 50 52 67 61 48 48 52
R07 | 1453 10 28 11 13 15 24 7 | 50 32 43 48 55 30 44
R08 | 1073 9 39 26 13 14 13 8 | 41 40 52 51 47 38 43
R09 | 1567 10 26 12 15 14 9 6 | 28 35 30 28 33 29 28
R11 | 1499 15 32 8 23 13 20 8 | 27 56 26 48 27 24 28
R12 | 1067 5 17 21 12 14 8 5 | 40 45 29 48 38 37 38
R14 | 1069 5 17 14 14 14 9 5 | 33 26 31 34 31 29 30
R15 | 1168 12 15 21 17 21 9 7 | 45 34 32 43 32 39 36
R16 | 1967 8 14 22 11 12 12 5 | 46 42 53 41 32 42 41
R17E | 1574 14 26 20 19 14 12 7 | 77 81 95 92 78 87 83
R18E | 1450 9 28 31 16 14 13 7 | 47 34 58 49 43 56 45
R20E | 5496 24 103 72 39 30 52 22 | 87 78 119 102 92 99 92
R21E | 1955 9 26 17 20 9 22 7 | 35 46 46 40 36 28 35
XR22E | 1102 15 18 16 18 13 --- 8 | 22 33 29 34 28 --- 25
R24E | 1309 10 29 18 23 21 14 8 | 31 44 33 29 36 30 30
XR25E |14609 62 --- --- --- 100 --- 78 | 78 --- --- --- 51 --- 52
XR26 | 6022 39 84 50 --- 66 --- 32 | 19 73 15 --- 56 --- 28
XR27 | 5777 39 82 --- 27 60 --- 28 | 21 71 --- 25 42 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1941 11 34 25 18 16 21 |T 44 47 47 49 45 42 42
WRMS | 1941 10 29 16 15 15 21 |NE 40 45 40 45 43 35 38
MEDI | 1496 10 26 18 15 14 14 |MD 41 44 43 48 42 37 38
Table 3.2378.2 GPS week: 2378 Day: 2 MJD: 60892
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 996 7 26 18 20 36 17 9 | 62 49 72 52 90 49 61
R03 | 1083 7 29 30 19 11 26 9 | 67 48 86 73 69 48 64
R04 | 1102 12 19 24 12 11 17 7 | 66 59 79 54 56 47 59
R05 | 1396 8 10 15 13 10 9 4 | 53 51 57 49 45 43 48
R07 | 2031 12 32 12 18 18 12 7 | 60 45 60 51 63 47 53
R08 | 1140 9 18 19 15 15 11 6 | 49 49 67 60 59 45 53
R09 | 1564 13 23 15 12 15 10 6 | 25 24 26 26 26 28 23
R11 | 1272 19 38 19 32 19 10 10 | 28 46 28 43 27 26 21
R12 | 1359 7 13 14 13 11 9 5 | 43 36 39 47 34 39 39
R14 | 957 7 17 8 8 6 8 4 | 41 33 30 36 35 37 36
R15 | 1091 8 16 18 13 18 10 6 | 47 53 46 49 41 44 44
R16 | 1997 12 10 28 12 15 14 7 | 44 44 42 37 36 48 40
R17E | 1991 7 15 19 41 13 21 9 | 49 48 58 65 49 53 50
R18E | 2451 9 21 9 15 14 10 5 | 41 45 55 46 43 44 43
R20E | 5326 21 101 55 32 29 43 20 | 86 77 84 82 62 71 73
R21E | 1559 8 26 19 17 15 8 6 | 28 41 42 38 29 28 30
XR22E | 1530 14 21 11 19 8 --- 7 | 22 37 30 30 24 --- 24
R24E | 1209 14 16 18 18 27 8 7 | 34 30 29 36 27 26 28
XR25E |19633 96 --- --- --- 161 --- 124 | 88 --- --- --- 94 --- 63
XR26 | 8839 34 71 40 --- 62 --- 28 | 27 85 30 --- 53 --- 39
XR27 | 5667 41 70 --- 36 71 --- 30 | 28 82 --- 35 71 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1955 11 32 23 20 18 17 |T 46 49 49 47 47 42 43
WRMS | 1955 11 24 18 15 17 17 |NE 45 50 50 47 50 41 44
MEDI | 1530 12 21 18 17 15 10 |MD 43 46 42 47 43 44 41
Table 3.2378.3 GPS week: 2378 Day: 3 MJD: 60893
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1555 6 22 12 11 23 24 7 | 69 56 74 70 83 54 68
R03 | 2250 12 20 9 14 10 20 6 | 74 59 69 74 72 59 67
R04 | 1113 7 22 12 21 7 24 7 | 73 59 78 83 72 53 69
R05 | 2433 8 17 12 23 17 22 7 | 63 57 66 50 76 45 60
R07 | 1618 10 31 9 19 18 16 7 | 62 51 58 49 69 46 55
R08 | 1365 10 19 15 13 15 16 6 | 63 50 66 62 64 56 60
R09 | 1314 14 13 11 12 9 12 5 | 15 29 19 19 16 20 16
R11 | 1468 23 45 15 33 12 17 10 | 18 57 12 44 17 17 17
R12 | 1428 9 16 15 17 17 8 6 | 36 48 46 30 52 40 41
R14 | 1028 9 17 8 11 19 11 5 | 38 39 36 40 24 28 33
R15 | 1147 7 14 11 14 18 6 5 | 46 55 52 52 43 46 48
R16 | 1489 21 19 21 13 16 12 8 | 45 43 45 45 26 39 38
R17E | 1657 13 17 17 19 16 10 7 | 48 42 56 59 46 51 49
R18E | 1554 11 13 13 18 10 21 6 | 28 31 35 34 25 30 27
XR19E | 2181 16 17 12 --- 13 --- 8 | 26 18 34 --- 25 --- 21
R20E | 6232 37 91 37 56 40 54 22 | 64 51 93 70 54 50 55
R21E | 2692 13 21 23 41 12 16 9 | 31 32 40 47 27 23 26
XR22E | 3144 18 15 13 13 12 --- 7 | 29 34 39 39 35 --- 33
R24E | 2342 11 19 10 20 16 7 6 | 26 30 22 30 23 23 22
XR25E |18687 58 --- --- --- 76 --- 66 | 88 --- --- --- 87 --- 73
XR26 | 8889 38 79 34 --- 60 --- 29 | 16 88 33 --- 56 --- 35
XR27 | 7724 39 61 --- 39 61 --- 28 | 27 85 --- 29 69 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 2254 15 30 16 24 18 20 |T 44 48 48 48 48 40 43
WRMS | 2254 13 23 14 16 15 20 |NE 46 55 50 49 52 41 46
MEDI | 1618 12 19 12 18 16 16 |MD 38 50 45 47 46 45 41
Table 3.2378.4 GPS week: 2378 Day: 4 MJD: 60894
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1643 9 15 12 12 17 29 7 | 67 55 68 58 74 47 62
R03 | 1775 8 25 14 11 12 20 6 | 75 58 76 75 77 60 72
R04 | 1145 7 27 13 19 15 19 7 | 73 63 80 79 83 67 75
R05 | 1788 6 18 22 14 9 14 6 | 65 62 71 63 64 59 63
R07 | 1931 13 31 12 11 6 18 6 | 70 52 66 67 61 52 62
R08 | 1382 11 23 19 10 11 28 7 | 61 52 65 57 53 45 55
R09 | 2689 10 23 15 10 10 9 5 | 23 27 27 26 27 33 24
R11 | 2038 20 38 15 18 7 14 8 | 22 67 29 51 26 23 29
R12 | 1011 7 16 21 11 9 17 6 | 41 52 56 48 40 34 43
R14 | 1321 7 17 19 10 14 11 5 | 42 42 39 44 40 36 40
R15 | 2154 8 15 12 12 15 17 5 | 48 46 51 55 56 44 49
R16 | 1126 16 19 15 8 10 6 5 | 44 42 37 40 33 37 37
R17E | 2822 8 22 15 22 13 9 6 | 47 54 50 62 50 51 51
R18E | 1430 13 23 11 8 13 19 6 | 43 44 47 43 51 50 44
XR19E | 2998 12 14 16 --- 10 --- 7 | 22 17 27 --- 19 --- 20
R20E | 4667 34 90 55 45 40 51 22 | 80 64 70 79 75 81 70
R21E | 1556 10 19 24 19 12 12 7 | 34 39 40 38 32 27 32
XR22E | 5334 18 --- 19 22 16 --- 11 | 27 --- 36 33 31 --- 29
R24E | 2041 7 26 18 23 18 11 7 | 26 36 34 38 24 26 25
XR25E |18104 58 --- --- --- 73 --- 65 | 92 --- --- --- 63 --- 62
XR26 | 8527 40 77 49 --- 63 --- 31 | 23 76 26 --- 57 --- 31
XR27 |14773 45 60 --- 30 62 --- 28 | 26 72 --- 44 57 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 2093 13 31 21 18 15 21 |T 47 51 49 52 49 45 46
WRMS | 2093 11 35 15 12 13 21 |NE 48 54 53 54 53 44 48
MEDI | 1931 10 23 15 12 13 17 |MD 43 52 47 51 51 45 43
Table 3.2378.5 GPS week: 2378 Day: 5 MJD: 60895
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1204 6 16 21 11 18 19 6 | 59 54 75 58 65 52 60
R03 | 1746 6 18 12 12 20 23 6 | 63 52 68 59 76 52 62
R04 | 1345 6 15 14 17 17 18 6 | 56 49 54 67 60 44 55
R05 | 1827 6 15 14 17 18 16 6 | 48 42 43 49 57 47 46
R07 | 1809 11 19 20 14 19 19 7 | 60 44 68 64 40 47 55
R08 | 1009 5 26 21 15 14 25 7 | 50 36 60 61 46 42 48
R09 | 1133 12 16 16 11 10 8 5 | 33 35 35 36 36 37 33
R11 | 2218 21 42 26 32 15 13 11 | 24 54 35 35 23 25 23
R12 | 1061 7 22 16 15 14 18 6 | 34 44 34 36 25 24 30
R14 | 1348 10 14 12 10 23 12 6 | 37 33 42 32 51 29 36
R15 | 2982 6 14 14 12 18 17 6 | 46 39 48 43 47 41 43
R16 | 1509 9 17 25 17 18 14 7 | 41 48 55 28 32 30 37
R17E | 1708 5 17 22 15 20 17 7 | 48 42 52 45 42 53 45
R18E | 1934 13 20 16 17 11 21 7 | 35 37 47 44 36 39 37
XR19E | 2665 10 15 19 --- 12 --- 8 | 34 23 46 --- 34 --- 32
R20E | 3030 20 75 46 64 36 52 21 | 81 60 107 76 88 78 74
R21E | 1959 8 17 12 17 13 14 6 | 36 47 39 43 43 35 37
XR22E | 2761 13 13 14 26 15 --- 8 | 32 49 37 61 36 --- 36
R24E | 3415 7 25 11 15 13 9 5 | 30 40 25 33 28 29 27
XR25E |19094 68 --- --- --- 150 --- 101 | 102 --- --- --- 82 --- 87
XR26 |12313 36 89 46 --- 69 --- 32 | 17 69 27 --- 52 --- 21
XR27 |16352 30 64 --- 31 65 --- 26 | 29 67 --- 28 54 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1964 10 27 20 22 18 21 |T 45 45 49 47 47 41 43
WRMS | 1964 10 29 18 14 17 21 |NE 42 47 49 45 47 39 41
MEDI | 1827 9 17 16 15 18 17 |MD 37 44 46 44 43 41 37
Table 3.2378.6 GPS week: 2378 Day: 6 MJD: 60896
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1198 7 21 18 31 20 18 8 | 85 67 95 95 91 71 82
R03 | 1435 5 25 14 33 12 13 7 | 95 74 101 98 103 87 93
R04 | 1249 8 17 13 20 14 14 6 | 90 80 95 96 96 74 88
R05 | 1067 7 15 13 29 12 22 7 | 83 74 89 85 86 74 81
R07 | 1275 10 20 14 25 19 25 8 | 84 63 89 80 85 60 77
R08 | 1279 8 14 24 35 25 22 9 | 72 64 92 80 90 61 74
R09 | 1287 10 26 20 30 8 15 7 | 45 51 47 37 47 49 44
R11 | 1610 13 40 18 28 12 14 9 | 33 31 37 22 38 31 29
R12 | 1081 10 16 20 26 15 17 7 | 46 50 45 54 50 41 46
R14 | 993 7 9 14 30 9 7 5 | 46 47 48 50 51 48 48
R15 | 2645 9 11 13 21 15 7 5 | 63 61 61 64 64 62 62
R16 | 3660 9 29 20 22 16 15 7 | 61 66 64 56 52 49 56
R17E | 1700 17 22 104 35 15 13 15 | 67 62 121 69 58 67 64
R18E | 1570 13 38 179 50 10 25 12 | 62 62 161 69 60 66 60
XR19E | 5641 12 21 178 --- 17 --- 11 | 29 21 152 --- 26 --- 25
R20E | 2946 27 72 369 98 38 40 25 | 102 94 303 153 103 110 104
R21E | 1484 11 25 73 36 13 13 12 | 38 46 84 52 43 40 42
XR22E | 1127 16 16 69 42 10 --- 14 | 32 35 75 44 37 --- 34
R24E | 1522 17 16 56 30 11 14 10 | 27 32 63 39 28 27 27
XR25E |14271 92 --- --- --- 143 --- 115 | 111 --- --- --- 81 --- 85
XR26 |16256 41 74 54 --- 58 --- 31 | 26 102 24 --- 71 --- 44
XR27 |15443 37 64 --- 35 56 --- 27 | 39 105 --- 47 77 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 1795 12 28 106 38 17 19 |T 60 61 92 67 65 59 60
WRMS | 1795 9 31 24 28 16 19 |NE 62 66 68 66 71 58 63
MEDI | 1484 10 21 20 30 15 15 |MD 61 62 84 64 60 61 58
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