[IGSREPORT-30640] Wk 2385 IGLOS Final Orbits
acc
acc at igs.org
Mon Oct 13 00:28:22 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2385 (Sep 21, 2025 - Sep 27, 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 2.2385.
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:
igl2385[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2385 in the SP3 format.
igl23857.sum Combination Report for GPS Week 2385.
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 | 1.2 ns
1 | 4.0 ns
2 | 2.4 ns
3 | 5.6 ns
4 | 1.6 ns
5 | 0.8 ns
6 | 3.3 ns
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 1.2385, 1a.2385).
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 2.2385.0-6)
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 3.2385.0-6).
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 2385 summary. (Sep 21, 2025 - Sep 27, 2025)
Table 1.2385.a GPS week : 2385 MJD: 60939.0-60945.0
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 44 .18 16 13 | 1496 -1065 4188 10759
| 1 0 1 20 4 21 .03 | 1381 2164
esa n/a| -3 -2 0 16 -12 51 -.06 31 33 | 2846 -1086 4187 10911
| 1 1 2 18 11 25 .05 | 1354 1959
gfz n/a| 0 0 1 33 8 -8 -.05 16 14 | 0 -1503 4722 9972
| 1 1 1 9 15 18 .04 | 0 2181
grg n/a| 1 0 -1 -38 -8 -1 .27 21 16 | 2312 -545 3564 8443
| 0 1 2 15 18 40 .05 | 1740 1901
iac n/a| 0 0 -2 19 14 -48 -.18 17 16 | 3730 -868 4160 11274
| 1 1 1 18 21 33 .04 | 792 1383
jgx n/a| 0 0 -3 -21 -30 -17 -.15 19 19 | 4486 -605 3677 7641
| 1 1 3 11 16 33 .04 | 2098 2021
Table 1.2385.b GPS week : 2385 MJD: 60939.0-60945.0
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 8 6 6 6 |
R03 | 8 7 6 8 8 5 5 |
R04 | 5 5 6 7 7 6 6 |
R05 | 6 4 6 6 6 5 6 |
R07 | 6 5 6 6 7 8 5 |
R08 | 6 7 6 8 9 8 6 |
R09 | 8 8 6 7 10 7 7 |
R11 | 8 10 8 9 9 7 12 |
R12 | 7 8 6 6 6 7 18 |
R14 | 6 6 7 7 11 9 10 |
R15 | 7 7 7 7 6 12 15 |
R16 | 7 6 7 8 8 11 11 |
R17 | 8 6 7 7 6 8 7 |
R18 | 7 8 7 8 8 8 8 |
R19 | 8 8 8 9 9 8 9 |
R20 | 21 19 18 24 20 19 25 |
R21 | 6 8 7 7 7 8 7 |
R22 | 10 10 7 10 8 7 8 |
R24 | 6 6 6 9 9 6 6 |
R25 | 52 61 85 95 41 52 63 |
R26 | 23 24 27 27 27 30 33 |
R27 | 27 34 27 24 25 22 24 |
Table 1.2385.c GPS week : 2385 MJD: 60939.0-60945.0
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 2385 0 | 65 144 30 -1948 820 -3317 76.7 1745 1745 | 1165 0
brd 2385 1 | -2 44 75 -810 372 490 80.9 1937 1937 | 4022 0
brd 2385 2 | -134 54 8 -2144 -2592 1297 82.5 2453 2453 | 2360 0
brd 2385 3 | 41 167 168 -3133 4094 7136 81.1 1663 1663 | 5610 0
brd 2385 4 | -205 -14 36 571 -2776 3186 78.3 2201 2201 | 1609 0
brd 2385 5 | 88 16 42 1494 3338 1077 79.2 2333 2333 | 819 0
brd 2385 6 | -70 50 -64 671 1912 3110 79.4 2033 2033 | 3344 0
-------------+------------------------------------------------------------+----------------
brd 2385 mean| -30 66 42 -756 738 1854 79.7 2052 2052 | 2704 0
brd 2385 sdev| 109 66 70 1725 2676 3182 1.9 294 294 | 1723 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 2.2385.0 GPS week: 2385 Day: 0 MJD: 60939
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 -13 9 45 .16 14 12 | 963 429 5973 15263
esa n/a| -2 -3 0 24 -15 28 -.12 30 24 | 3571 214 5952 14652
gfz n/a| -1 2 0 35 12 -24 -.06 16 16 | 0 -3585 9328 14832
grg n/a| 1 0 0 -28 -20 27 .34 19 15 | -353 1947 4410 9777
iac n/a| 0 0 0 6 36 -44 -.22 17 16 | 3760 -459 5460 15303
jgx n/a| 1 0 -6 -15 -23 -30 -.16 18 18 | 982 1966 4639 9561
Table 2.2385.1 GPS week: 2385 Day: 1 MJD: 60940
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 7 9 55 .21 15 13 | 2042 1648 5193 11361
esa n/a| -2 -3 -1 7 -30 74 -.01 29 23 | 4036 1044 5199 11559
gfz n/a| 1 0 2 36 -12 -2 .02 15 13 | 0 1983 5307 10349
grg n/a| 1 1 0 -53 15 -34 .30 18 16 | 3420 -362 3550 9431
iac n/a| 0 0 -3 34 41 -53 -.22 16 14 | 4134 401 5139 11916
jgx n/a| 0 1 -5 -32 -49 -5 -.20 17 17 | 7368 -286 3687 8489
Table 2.2385.2 GPS week: 2385 Day: 2 MJD: 60941
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 -6 7 28 .16 14 12 | 2101 -2495 4185 11935
esa n/a| -2 -2 -1 50 -11 77 -.00 30 34 | 3132 -2789 4187 12443
gfz n/a| 2 0 3 30 -9 -23 -.08 17 15 | 0 -1955 4285 10806
grg n/a| 2 0 0 -37 7 26 .28 15 15 | 2075 -680 3561 9145
iac n/a| -1 0 0 29 -3 -58 -.17 15 15 | 2923 -2559 4303 11985
jgx n/a| 0 0 -6 -30 -17 13 -.17 15 15 | 5210 -932 3650 8264
Table 2.2385.3 GPS week: 2385 Day: 3 MJD: 60942
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 1 -2 18 33 .17 17 14 | 4015 -980 3867 14041
esa n/a| -3 -1 -3 27 -15 46 -.02 32 34 | 4686 -1127 3863 14321
gfz n/a| 0 -2 2 33 1 -17 -.08 18 13 | 0 -859 3943 12763
grg n/a| 2 0 1 -21 -19 48 .25 18 18 | 4927 -92 3519 8368
iac n/a| 0 -1 -2 -9 17 -37 -.22 19 19 | 4879 -532 3876 13433
jgx n/a| 0 2 0 -24 -38 -86 -.15 22 21 | 6341 735 3722 7238
Table 2.2385.4 GPS week: 2385 Day: 4 MJD: 60943
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 41 14 86 .16 16 13 | 1109 -556 3968 7458
esa n/a| -5 -3 -2 13 -4 7 -.13 33 32 | 1333 -603 3979 7389
gfz n/a| 0 0 1 16 27 19 -.08 17 19 | 0 -1020 3919 7059
grg n/a| 2 0 0 -63 -8 12 .29 19 15 | 732 274 3806 7574
iac n/a| -1 1 -1 7 -6 -107 -.17 17 15 | 2713 357 4095 8259
jgx n/a| 3 0 -5 -32 -4 -9 -.18 25 22 | 3270 -677 3787 7049
Table 2.2385.5 GPS week: 2385 Day: 5 MJD: 60944
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 -21 18 27 .21 17 14 | 464 -5046 2976 7836
esa n/a| -2 -4 1 -5 -15 58 -.10 33 43 | 1327 -4549 2973 7927
gfz n/a| -1 0 2 41 14 12 -.00 18 14 | 0 -4671 3035 7319
grg n/a| 0 3 -6 -22 0 -47 .24 21 16 | 2408 -4361 2914 7682
iac n/a| 0 0 -1 41 -10 5 -.18 13 14 | 3317 -3063 3039 8895
jgx n/a| 0 -1 0 -11 -29 2 -.11 19 19 | 3875 -4590 2984 7077
Table 2.2385.6 GPS week: 2385 Day: 6 MJD: 60945
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 -11 18 33 .23 22 17 | -221 -458 3160 7424
esa n/a| -1 0 3 1 6 65 -.06 31 37 | 1843 207 3161 8088
gfz n/a| 2 0 0 44 22 -22 -.06 15 11 | 0 -417 3237 6679
grg n/a| 0 0 -3 -40 -38 -47 .18 36 16 | 2980 -544 3194 7127
iac n/a| 1 0 -5 27 27 -46 -.11 24 21 | 4385 -221 3214 9133
jgx n/a| 0 0 3 -2 -47 -7 -.09 19 19 | 4359 -454 3270 5815
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 3.2385.0 GPS week: 2385 Day: 0 MJD: 60939
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1175 8 24 20 12 18 18 7 | 37 35 42 36 37 35 36
R03 | 1947 11 35 16 19 13 16 8 | 16 40 16 21 15 17 13
R04 | 1008 8 15 9 11 10 8 4 | 17 19 16 19 17 24 16
R05 | 3014 7 13 11 6 15 17 5 | 20 23 19 20 23 20 17
R07M | 1360 8 13 19 10 8 16 5 | 18 30 26 19 20 18 19
R08M | 1161 9 25 8 17 8 13 6 | 21 30 23 26 23 25 21
R09E | 1330 16 12 17 21 24 6 7 | 103 103 107 101 114 106 105
R11M | 1038 13 29 17 21 15 8 7 | 50 60 50 46 50 41 47
R12 | 902 10 26 9 16 12 19 6 | 72 66 64 73 61 52 64
R14E | 1906 12 22 12 13 12 12 6 | 58 63 56 65 55 52 56
R15 | 2174 13 19 17 14 20 12 7 | 64 46 60 65 54 29 56
R16 | 2918 11 19 12 19 14 13 6 | 55 55 49 63 45 44 50
R17M | 1649 16 27 14 23 18 13 8 | 80 70 77 78 77 66 74
R18M | 1153 13 21 15 17 17 8 6 | 69 88 75 71 77 73 74
XR19 | 1570 14 20 11 --- 13 --- 8 | 26 45 41 --- 39 --- 35
R20 | 2436 37 89 36 45 40 46 21 | 77 69 67 54 54 55 58
R21 | 1122 11 17 9 13 10 19 6 | 82 69 78 81 78 65 75
XR22M | 993 13 21 14 20 30 --- 10 | 38 38 42 47 51 --- 39
R24 | 1213 6 11 15 13 14 16 5 | 72 75 74 74 69 67 71
XR25 |22667 45 --- --- --- 60 --- 52 | 94 --- --- --- 145 --- 109
XR26M | 9926 30 63 30 --- 46 --- 23 | 27 26 35 --- 33 --- 27
XR27 |13442 47 60 --- 25 54 --- 27 | 29 41 --- 36 28 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1744 14 30 16 19 17 18 |T 51 51 50 52 52 46 49
WRMS | 1744 12 24 16 15 16 18 |NE 52 49 48 50 52 41 49
MEDI | 1360 12 21 14 17 15 13 |MD 50 46 49 54 50 44 47
Table 3.2385.1 GPS week: 2385 Day: 1 MJD: 60940
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1557 10 22 12 17 21 13 7 | 163 164 159 161 159 163 161
R03 | 2011 7 20 14 15 14 25 7 | 16 18 22 22 17 20 15
R04 | 1155 9 13 15 11 7 15 5 | 17 13 21 16 11 17 12
R05 | 1751 7 12 6 6 8 8 3 | 20 17 19 15 16 13 14
R07M | 1218 8 15 14 7 12 11 5 | 21 18 28 19 22 18 18
R08M | 1211 14 22 13 16 12 11 6 | 42 44 40 40 48 39 40
R09E | 1712 17 12 12 20 25 10 7 | 84 87 87 85 92 89 86
R11M | 1118 23 40 14 24 14 15 9 | 41 59 38 43 40 40 39
R12 | 926 10 17 15 28 9 17 7 | 70 67 58 79 54 53 61
R14E | 2396 7 22 11 11 14 16 6 | 51 61 50 62 46 55 52
R15 | 1225 18 23 15 13 9 16 7 | 54 32 41 57 42 21 42
R16 | 3700 8 19 15 12 8 20 6 | 48 41 46 54 45 43 45
R17M | 2126 11 13 14 9 14 21 6 | 52 48 52 49 41 45 46
R18M | 1782 9 21 20 21 8 18 7 | 46 51 54 45 41 38 44
XR19 | 1510 15 16 11 --- 12 --- 7 | 23 31 31 --- 32 --- 27
R20 | 3472 38 87 25 32 39 28 18 | 54 47 61 50 42 52 46
R21 | 1326 14 23 12 23 11 20 7 | 51 42 48 55 43 41 45
XR22M | 1490 18 18 18 19 21 --- 9 | 30 34 29 44 48 --- 33
R24 | 1566 7 12 17 12 14 8 5 | 51 49 47 54 53 49 49
XR25 |16598 58 --- --- --- 64 --- 61 | 53 --- --- --- 54 --- 47
XR26M |11889 33 50 34 --- 47 --- 23 | 23 28 24 --- 20 --- 20
XR27 | 8629 61 50 --- 34 73 --- 34 | 28 26 --- 30 38 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1936 15 29 15 18 16 17 |T 47 46 47 51 45 46 43
WRMS | 1936 13 23 13 16 14 17 |NE 40 34 39 43 37 34 35
MEDI | 1566 11 20 14 16 14 16 |MD 46 42 41 49 42 41 42
Table 3.2385.2 GPS week: 2385 Day: 2 MJD: 60941
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1439 9 17 12 10 23 10 6 | 300 311 305 306 310 309 306
R03 | 1112 8 31 14 8 10 15 6 | 18 27 25 17 22 23 18
R04 | 2383 9 27 13 16 8 13 6 | 20 29 18 22 15 18 17
R05 | 1097 10 15 21 7 13 7 5 | 23 31 31 26 23 21 22
R07M | 1320 9 24 11 9 14 14 5 | 25 32 32 24 29 30 25
R08M | 1065 18 11 16 7 9 8 5 | 107 119 117 119 120 108 114
R09E | 1999 14 19 14 11 16 10 6 | 70 69 72 74 78 72 72
R11M | 1519 14 27 19 21 10 10 7 | 37 52 31 44 40 36 36
R12 | 954 8 15 16 11 13 12 5 | 63 60 50 62 58 56 57
R14E | 2109 8 21 8 21 12 19 6 | 59 70 59 67 64 46 58
R15 | 1095 11 22 19 11 11 16 6 | 69 59 74 75 65 41 67
R16 | 3024 14 20 20 15 12 14 7 | 56 43 47 55 43 48 47
R17M | 1778 12 12 15 15 23 7 6 | 62 60 57 58 59 60 57
R18M | 1226 9 16 14 13 12 21 6 | 50 58 58 55 51 41 50
XR19 | 2152 13 10 15 --- 13 --- 8 | 26 31 32 --- 28 --- 26
R20 | 7582 36 92 31 29 24 29 17 | 63 48 55 52 55 46 50
R21 | 1744 11 23 10 16 17 17 7 | 54 44 53 62 49 51 51
XR22M | 1783 16 20 12 11 10 --- 7 | 29 26 33 36 29 --- 28
R24 | 1410 10 22 13 11 9 10 5 | 46 46 40 46 40 42 41
XR25 |13870 77 --- --- --- 92 --- 84 | 89 --- --- --- 125 --- 89
XR26M | 8303 39 54 40 --- 53 --- 26 | 33 25 32 --- 26 --- 26
XR27 | 9700 47 56 --- 23 55 --- 26 | 16 35 --- 31 22 --- 20
------+-----------------------------------------+-------------------------------------
RMS | 2452 14 30 17 15 15 15 |T 59 60 61 64 61 61 58
WRMS | 2452 12 34 15 15 15 15 |NE 45 41 42 44 45 38 42
MEDI | 1744 11 21 14 11 13 13 |MD 50 46 47 55 43 46 47
Table 3.2385.3 GPS week: 2385 Day: 3 MJD: 60942
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1152 9 17 11 13 24 22 7 | 452 457 457 449 459 451 454
R03 | 1278 16 23 16 14 8 23 7 | 21 24 25 29 17 30 20
R04 | 2309 14 37 5 11 8 8 6 | 18 33 15 20 16 18 16
R05 | 1010 16 22 9 8 11 6 5 | 17 22 18 15 14 15 12
R07M | 1288 11 11 14 11 11 13 5 | 14 22 22 22 18 16 15
R08M | 1805 14 22 20 11 17 26 8 | 161 164 169 162 168 167 165
R09E | 1126 14 13 19 17 15 16 7 | 60 57 54 69 63 67 60
XR11M | 2134 17 15 13 21 21 --- 9 | 31 30 24 24 34 --- 24
R12 | 1074 6 17 13 10 20 16 6 | 66 66 56 65 74 56 63
R14E | 1644 8 15 13 19 15 22 7 | 45 50 41 54 52 31 44
R15 | 880 12 18 13 19 10 23 7 | 55 51 57 56 53 29 50
R16 | 1889 15 27 19 10 16 22 8 | 63 43 62 59 48 40 52
R17M | 1605 10 17 10 15 15 22 6 | 50 41 53 53 49 48 48
R18M | 918 13 25 21 16 20 18 8 | 47 60 43 58 61 49 51
XR19 | 2618 14 17 15 --- 13 --- 8 | 18 36 37 --- 21 --- 25
R20 | 3768 47 98 43 48 42 42 23 | 72 60 79 36 26 44 47
R21 | 1426 10 18 17 13 13 22 7 | 53 44 59 61 46 46 51
XR22M | 1465 18 23 10 17 26 --- 9 | 22 36 26 33 38 --- 26
R24 | 924 14 26 9 23 22 24 8 | 36 46 29 29 38 28 29
XR25 |11407 87 --- --- --- 103 --- 95 | 71 --- --- --- 160 --- 101
XR26M | 7414 35 47 37 --- 63 --- 26 | 28 26 30 --- 22 --- 22
XR27 | 8034 31 62 --- 31 45 --- 23 | 21 35 --- 19 19 --- 15
------+-----------------------------------------+-------------------------------------
RMS | 1662 17 32 18 18 19 22 |T 64 66 67 69 68 70 63
WRMS | 1662 14 34 13 18 19 21 |NE 42 41 43 38 44 34 40
MEDI | 1465 14 22 13 15 16 22 |MD 45 43 41 53 38 40 44
Table 3.2385.4 GPS week: 2385 Day: 4 MJD: 60943
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1277 10 15 14 7 8 21 5 | 576 580 569 573 572 576 574
R03 | 2086 7 26 14 19 13 25 7 | 17 24 19 26 13 16 12
R04 | 981 11 32 9 12 9 20 6 | 16 26 18 25 14 23 14
R05 | 2144 9 17 14 11 16 9 6 | 15 27 19 19 21 17 15
R07M | 1940 10 26 17 9 12 16 6 | 17 21 17 16 16 15 12
R08M | 1506 15 25 11 13 31 25 9 | 226 215 218 223 214 229 220
R09E | 1341 14 20 17 38 14 17 9 | 87 82 83 96 89 86 85
R11M | 3232 18 24 18 23 19 17 8 | 32 51 28 38 40 29 31
R12 | 1146 9 20 13 13 14 19 6 | 72 70 66 75 69 59 68
R14E | 1137 14 24 32 30 15 23 10 | 74 92 76 81 78 63 73
R15 | 857 10 12 13 18 13 16 6 | 50 46 38 58 54 35 45
R16 | 1421 12 20 21 21 12 19 7 | 49 52 65 57 58 42 52
R17M | 1878 7 20 11 14 13 22 6 | 51 51 54 52 50 40 49
R18M | 1019 8 36 16 16 17 23 8 | 41 61 35 42 45 32 40
XR19 | 2182 16 23 15 --- 12 --- 9 | 27 41 38 --- 31 --- 31
R20 | 6397 46 97 21 26 31 53 20 | 70 51 64 57 43 29 52
R21 | 871 12 23 13 11 14 27 7 | 55 47 60 55 60 39 53
XR22M | 721 16 19 11 17 16 --- 8 | 33 39 36 44 36 --- 34
R24 | 947 12 34 15 14 12 34 8 | 44 49 49 43 40 27 40
XR25 |15543 35 --- --- --- 46 --- 41 | 97 --- --- --- 122 --- 103
XR26M | 7807 40 81 30 --- 50 --- 27 | 34 24 41 --- 32 --- 30
XR27 | 7030 33 43 --- 33 59 --- 25 | 24 27 --- 27 18 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 2200 16 33 17 19 17 25 |T 77 79 79 84 77 79 75
WRMS | 2200 13 32 19 15 15 22 |NE 44 41 43 44 45 31 41
MEDI | 1421 12 24 14 16 14 21 |MD 44 49 41 52 43 35 40
Table 3.2385.5 GPS week: 2385 Day: 5 MJD: 60944
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1165 10 22 10 10 12 10 5 | 741 755 732 742 734 746 740
R03 | 2509 7 14 17 13 9 9 5 | 20 24 30 22 21 24 20
R04 | 1423 12 23 10 8 12 21 6 | 21 21 16 16 9 19 12
R05 | 3158 7 23 13 9 9 8 5 | 24 34 21 23 17 15 18
R07M | 2722 9 30 22 10 10 21 7 | 23 26 27 26 20 20 20
R08M | 1540 16 20 17 16 15 16 7 | 293 289 291 281 292 281 287
R09E | 1493 15 20 11 23 12 10 6 | 85 86 87 81 86 83 84
R11M | 2263 14 19 11 30 10 13 7 | 46 53 47 73 43 44 48
R12 | 899 13 13 18 13 12 22 7 | 71 76 82 80 67 69 72
R14E | 1516 10 21 16 33 20 18 8 | 60 59 59 80 67 53 61
XR15 | 741 12 18 27 41 13 --- 11 | 79 77 72 95 79 --- 77
R16 | 1174 17 35 15 48 15 19 11 | 95 91 96 106 98 99 95
R17M | 1537 9 26 12 16 14 25 7 | 51 47 52 63 53 42 51
R18M | 999 17 29 18 15 14 22 8 | 52 65 57 59 56 49 55
XR19 | 1186 13 14 13 --- 11 --- 7 | 32 39 33 --- 29 --- 30
R20 | 6376 50 98 34 31 12 30 19 | 71 52 45 52 65 46 53
R21 | 926 16 18 25 11 11 22 8 | 59 48 62 57 63 51 57
XR22M | 589 17 13 11 13 9 --- 6 | 40 44 43 46 44 --- 42
R24 | 979 12 18 17 10 11 14 6 | 55 57 46 53 47 51 50
XR25 |14852 55 --- --- --- 48 --- 51 | 81 --- --- --- 60 --- 56
XR26M | 4940 43 54 51 --- 56 --- 29 | 47 41 44 --- 38 --- 41
XR27 | 6357 37 45 --- 31 39 --- 22 | 18 36 --- 28 22 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 2333 17 33 18 21 13 19 |T 93 96 97 104 91 105 90
WRMS | 2333 14 43 14 16 14 19 |NE 52 50 50 53 48 46 46
MEDI | 1493 13 21 16 15 12 18 |MD 52 52 47 59 53 49 51
Table 3.2385.6 GPS week: 2385 Day: 6 MJD: 60945
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1256 11 20 10 10 14 9 5 | 897 910 897 894 902 899 900
R03 | 1320 12 14 10 9 7 11 4 | 20 27 25 23 26 20 22
R04 | 1000 12 14 9 18 15 18 6 | 23 26 27 21 19 25 22
R05 | 3985 11 19 9 11 15 10 5 | 26 28 20 22 23 20 19
R07M | 1539 8 17 12 17 7 11 5 | 31 28 31 34 31 34 30
R08M | 2522 14 23 9 11 12 8 6 | 367 368 368 374 375 372 370
R09E | 1338 13 17 16 15 16 13 6 | 119 122 117 120 124 120 119
R11M | 2415 14 14 18 69 28 12 12 | 66 74 62 105 63 66 65
R12 | 831 23 23 21 72 70 21 18 | 105 102 103 137 121 93 103
R14E | 1579 10 19 10 65 11 14 10 | 86 96 89 111 91 83 88
XR15 | 1440 22 25 14 57 31 --- 14 | 140 149 137 165 121 --- 138
R16 | 1422 25 20 17 42 24 21 10 | 189 180 180 191 172 169 178
R17M | 1037 8 15 18 8 13 23 7 | 71 64 76 72 73 53 67
R18M | 1102 23 17 12 12 13 20 7 | 79 95 85 86 90 81 85
XR19 | 1987 16 22 16 --- 9 --- 9 | 29 43 41 --- 37 --- 33
R20 | 4295 64 104 31 59 29 44 25 | 90 78 70 65 58 59 62
R21 | 1132 16 11 14 19 17 15 7 | 91 81 92 91 87 81 86
XR22M | 860 15 14 17 15 17 --- 8 | 57 54 59 60 54 --- 55
R24 | 1521 13 21 8 14 14 15 6 | 74 72 72 73 71 64 70
XR25 |12842 59 --- --- --- 67 --- 63 | 69 --- --- --- 113 --- 84
XR26M | 5830 47 63 42 --- 76 --- 32 | 29 32 28 --- 45 --- 26
XR27 | 5273 44 46 --- 27 40 --- 23 | 21 34 --- 27 24 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 2032 22 31 15 36 24 19 |T 121 126 128 140 123 139 120
WRMS | 2032 17 37 11 16 21 19 |NE 73 74 76 81 72 66 69
MEDI | 1440 14 19 14 17 15 14 |MD 71 74 72 86 71 66 67
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