[IGSREPORT-30646] Wk 2386 IGLOS Final Orbits
acc
acc at igs.org
Thu Oct 16 06:11:25 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2386 (Sep 28, 2025 - Oct 04, 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 2.2386.
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:
igl2386[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2386 in the SP3 format.
igl23867.sum Combination Report for GPS Week 2386.
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 | 3.7 ns
1 | 5.0 ns
2 | 2.5 ns
3 | 6.2 ns
4 | 2.8 ns
5 | 2.5 ns
6 | 3.4 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
6 | 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 1.2386, 1a.2386).
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 2.2386.0-6)
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 3.2386.0-6).
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 2386 summary. (Sep 28, 2025 - Oct 04, 2025)
Table 1.2386.a GPS week : 2386 MJD: 60946.0-60952.0
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 4 1 -4 42 .17 15 13 | 1416 -206 4737 10035
| 1 0 1 10 29 28 .04 | 1532 2699
esa n/a| -3 -2 0 8 -4 51 -.12 32 35 | 2211 -503 4735 10126
| 1 1 1 15 11 13 .05 | 1762 2574
gfz n/a| 0 0 1 21 18 -17 -.04 17 15 | 0 -30 4868 9468
| 0 1 1 19 11 20 .07 | 0 2528
grg n/a| 1 0 -3 -48 -12 -11 .29 17 14 | 3485 -637 3288 7902
| 1 0 2 10 11 36 .03 | 2072 3290
iac n/a| 0 0 -5 44 31 -29 -.17 17 17 | 4893 -186 4900 10691
| 1 0 2 22 37 78 .07 | 1962 2732
jgx n/a| 0 0 1 -10 -18 -26 -.23 17 17 | 3895 -434 3319 7506
| 1 1 2 15 6 43 .03 | 2043 3225
Table 1.2386.b GPS week : 2386 MJD: 60946.0-60952.0
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 6 6 7 8 6 6 |
R03 | 6 5 6 7 8 6 5 |
R04 | 5 5 7 6 7 6 8 |
R05 | 5 8 8 7 7 7 5 |
R07 | 7 5 5 6 6 6 7 |
R08 | 8 7 7 7 7 7 7 |
R09 | 6 8 7 9 8 8 6 |
R11 | 6 8 7 7 9 8 7 |
R12 | 11 7 7 8 10 8 8 |
R14 | 6 7 5 7 7 7 7 |
R15 | 9 6 7 7 9 7 8 |
R16 | 8 8 9 9 9 8 9 |
R17 | 7 7 8 6 7 6 7 |
R18 | 7 7 9 8 7 7 7 |
R19 | 7 10 8 8 8 9 7 |
R20 | 20 21 20 19 19 17 11 |
R21 | 6 6 8 8 8 7 9 |
R22 | 8 7 7 8 9 8 8 |
R24 | 7 7 7 7 7 7 8 |
R25 | 57 45 70 117 96 81 67 |
R26 | 29 28 26 28 30 27 26 |
R27 | 28 31 30 23 25 23 24 |
Table 1.2386.c GPS week : 2386 MJD: 60946.0-60952.0
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 2386 0 | 36 -64 -203 51 1674 1645 78.7 2055 2055 | 3704 0
brd 2386 1 | -20 77 -213 266 -145 4576 78.6 1845 1845 | 4995 0
brd 2386 2 | 140 83 -232 -396 -1626 22830 77.0 2081 2081 | 2516 0
brd 2386 3 | -108 48 -459 -58 -490 14850 83.2 2501 2501 | 6190 0
brd 2386 4 | -66 -62 -190 -139 -1755 -2878 81.8 2193 2193 | 2819 0
brd 2386 5 | -197 12 -308 -1695 410 -3209 79.9 2107 2107 | 2484 0
brd 2386 6 | -25 45 -261 -81 1598 -5930 76.5 1604 1604 | 3371 0
-------------+------------------------------------------------------------+----------------
brd 2386 mean| -34 20 -267 -293 -47 4554 79.4 2055 2055 | 3725 0
brd 2386 sdev| 107 61 93 649 1384 10597 2.4 279 279 | 1392 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 2.2386.0 GPS week: 2386 Day: 0 MJD: 60946
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 -50 6 .19 17 14 | 202 1744 3471 8573
esa n/a| -4 -1 -3 -23 -7 65 -.16 35 28 | 2261 1263 3462 8848
gfz n/a| 0 2 3 0 13 11 -.08 17 15 | 0 1453 3539 7839
grg n/a| 1 0 -6 -48 -10 17 .28 18 14 | 2689 954 3445 8372
iac n/a| -2 0 0 64 83 -48 -.14 17 17 | 5375 -341 3660 11105
jgx n/a| 1 0 -1 -27 -9 -24 -.18 18 18 | 4418 1182 3613 7863
Table 2.2386.1 GPS week: 2386 Day: 1 MJD: 60947
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 7 -33 1 .17 13 11 | 4579 -2519 3378 9129
esa n/a| -1 -3 0 6 5 41 -.17 27 23 | 5789 -1619 3383 9353
gfz n/a| 0 1 2 33 26 -38 -.17 18 17 | 0 -2030 3472 8067
grg n/a| -1 0 -2 -35 -15 -41 .30 19 14 | 5020 -1385 3183 8137
iac n/a| 0 0 -3 13 36 69 -.08 17 16 | 6432 -2076 3650 8843
jgx n/a| 0 0 0 -25 -15 -44 -.21 19 17 | 6553 -1382 3341 7733
Table 2.2386.2 GPS week: 2386 Day: 2 MJD: 60948
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 8 1 66 .11 15 13 | 481 -2399 2984 8988
esa n/a| -4 -3 -2 19 -13 43 -.09 28 37 | 2112 -3549 2969 9706
gfz n/a| 0 0 0 20 9 -45 -.02 18 16 | 0 -2468 3032 7983
grg n/a| 0 0 -2 -70 -29 48 .26 18 15 | 3375 -2817 3006 8753
iac n/a| 1 0 -6 44 36 -120 -.12 16 16 | 3016 688 3564 9243
jgx n/a| 0 0 3 -24 -14 15 -.26 18 18 | 4191 -3047 3114 8044
Table 2.2386.3 GPS week: 2386 Day: 3 MJD: 60949
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 -15 17 42 .23 14 12 | 471 4610 6766 12061
esa n/a| -3 -2 0 23 0 43 -.04 31 49 | 1325 4078 6755 12319
gfz n/a| 0 0 4 36 17 0 -.02 18 15 | 0 4583 6894 11606
grg n/a| 1 0 0 -51 -8 -5 .29 17 14 | 5713 46 3716 7229
iac n/a| 1 0 -5 61 -13 -109 -.30 17 19 | 6032 4772 6792 13115
jgx n/a| -2 -1 1 -10 -17 43 -.25 17 17 | 3059 978 3404 6680
Table 2.2386.4 GPS week: 2386 Day: 4 MJD: 60950
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 3 -13 25 59 .20 18 15 | 2016 838 8294 12625
esa n/a| -3 0 0 1 14 41 -.17 34 41 | 2535 187 8292 12766
gfz n/a| -1 0 0 48 41 -5 .02 18 15 | 0 1047 8515 12245
grg n/a| 0 0 -2 -42 -6 -33 .35 18 17 | -638 5598 3316 8214
iac n/a| 2 0 -7 13 -15 67 -.21 19 19 | 7504 -4055 8204 12522
jgx n/a| 2 0 4 9 -15 -86 -.24 15 15 | 93 5414 3407 8329
Table 2.2386.5 GPS week: 2386 Day: 5 MJD: 60951
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 0 7 7 22 76 .16 13 13 | 1446 -1852 5330 11914
esa n/a| -3 -2 0 17 -18 47 -.10 33 29 | 1250 -2456 5346 11179
gfz n/a| 0 0 0 -1 16 -19 -.06 14 12 | 0 -1505 5651 12101
grg n/a| 2 1 -8 -47 5 -58 .32 16 13 | 4204 -4477 3430 7847
iac n/a| 0 0 -5 54 21 1 -.19 17 18 | 2141 516 5480 12155
jgx n/a| 0 2 3 8 -28 -39 -.27 17 17 | 5423 -4027 3343 7617
Table 2.2386.6 GPS week: 2386 Day: 6 MJD: 60952
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 9 -12 44 .15 14 13 | 719 -1868 2940 6957
esa n/a| -1 0 1 14 -9 75 -.07 34 39 | 208 -1425 2938 6712
gfz n/a| 0 0 2 12 5 -27 .01 16 13 | 0 -1290 2976 6436
grg n/a| 2 0 -3 -44 -23 -8 .26 16 12 | 4033 -2378 2922 6763
iac n/a| 1 0 -7 59 70 -68 -.16 18 18 | 3751 -808 2954 7857
jgx n/a| 0 0 1 -3 -26 -46 -.21 14 14 | 3529 -2160 3014 6280
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 3.2386.0 GPS week: 2386 Day: 0 MJD: 60946
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1876 10 13 19 8 16 17 6 | 38 38 38 37 34 33 34
R03 | 1153 6 10 10 16 23 7 5 | 34 42 36 38 36 34 34
R04 | 1665 8 12 14 10 14 6 5 | 37 40 40 40 37 38 37
R05 | 2982 9 10 11 7 10 11 4 | 31 38 34 34 30 30 31
R07 | 2378 12 21 10 17 16 12 6 | 39 49 45 42 41 43 42
R08 | 2120 16 25 18 20 13 11 7 | 36 34 41 34 33 40 34
R09E | 1282 14 13 19 12 13 8 6 | 85 92 89 88 87 69 87
R11E | 1597 10 17 11 11 12 14 5 | 46 54 54 53 52 39 50
R12E | 1235 17 22 27 40 27 13 11 | 120 121 117 126 116 119 118
R14E | 1641 13 19 9 16 10 11 6 | 106 117 112 107 111 112 110
R15E | 1076 16 21 26 17 15 20 8 | 68 76 75 78 81 76 74
R16E | 1244 15 14 26 15 11 18 8 | 86 92 94 91 92 95 90
R17 | 1050 7 26 16 14 20 11 7 | 46 35 49 43 52 38 42
R18 | 866 15 20 10 16 20 10 7 | 35 49 36 45 48 36 39
XR19 | 2549 11 9 10 --- 13 --- 6 | 16 19 21 --- 25 --- 18
R20 | 5242 50 123 18 30 25 53 20 | 69 49 48 58 47 68 56
R21 | 1589 15 18 13 10 13 9 6 | 50 51 58 53 46 41 48
XR22 | 1035 14 14 11 14 19 --- 7 | 16 31 27 31 29 --- 22
R24 | 1458 12 22 13 9 13 17 6 | 38 38 40 39 32 35 34
XR25 |10385 49 --- --- --- 64 --- 56 | 89 --- --- --- 101 --- 90
XR26 | 3950 37 54 47 --- 59 --- 28 | 39 55 46 --- 39 --- 39
XR27 | 6856 46 50 --- 35 58 --- 27 | 85 101 --- 95 99 --- 92
------+-----------------------------------------+-------------------------------------
RMS | 2055 17 35 17 18 17 18 |T 54 58 55 59 57 55 55
WRMS | 2055 14 28 15 14 17 18 |NE 43 44 39 45 45 39 43
MEDI | 1597 14 19 13 15 15 11 |MD 39 49 45 45 46 40 42
Table 3.2386.1 GPS week: 2386 Day: 1 MJD: 60947
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1737 11 19 11 13 10 18 6 | 25 18 19 21 14 16 16
R03 | 2019 6 17 13 6 10 13 5 | 21 22 20 18 22 15 17
R04 | 2008 8 10 12 8 14 9 4 | 23 22 26 26 15 36 22
R05 | 1515 13 22 22 19 12 9 7 | 18 27 29 20 19 17 16
R07 | 2968 8 12 12 11 11 10 4 | 24 25 24 23 26 22 23
R08 | 1352 7 24 10 21 12 15 6 | 23 28 30 32 26 27 24
R09E | 1194 14 19 18 16 19 13 7 | 57 63 61 58 67 49 59
R11E | 1714 16 17 18 14 17 16 7 | 38 39 38 42 48 29 39
R12E | 1010 10 17 12 21 19 16 7 | 102 99 101 96 86 100 96
R14E | 2371 10 19 18 23 12 15 7 | 70 73 70 76 67 66 69
R15E | 1329 8 20 15 18 13 11 6 | 78 78 82 84 82 78 79
R16E | 1362 10 24 27 15 18 16 8 | 117 117 117 119 112 112 114
R17 | 1281 12 21 15 10 15 24 7 | 29 25 32 31 29 19 25
R18 | 1052 9 23 15 18 19 12 7 | 26 28 24 32 32 22 24
XR19 | 1219 16 28 9 --- 17 --- 10 | 18 24 17 --- 24 --- 16
R20 | 3707 33 81 36 43 41 51 20 | 27 28 40 40 30 46 25
R21 | 1348 10 15 9 17 8 22 6 | 38 38 34 36 33 35 34
XR22 | 1170 14 19 19 9 10 --- 7 | 18 29 23 28 22 --- 19
R24 | 932 11 22 12 11 15 21 7 | 30 27 32 29 30 22 25
XR25 |14768 36 --- --- --- 54 --- 44 | 103 --- --- --- 64 --- 77
XR26 | 6374 46 47 28 --- 62 --- 27 | 26 35 40 --- 37 --- 30
XR27 | 5566 51 48 --- 26 73 --- 31 | 73 74 --- 72 81 --- 72
------+-----------------------------------------+-------------------------------------
RMS | 1845 13 27 18 19 17 19 |T 44 43 42 46 43 41 41
WRMS | 1845 11 23 17 14 16 17 |NE 32 30 27 31 31 25 29
MEDI | 1362 11 20 15 16 15 15 |MD 27 28 32 32 30 29 25
Table 3.2386.2 GPS week: 2386 Day: 2 MJD: 60948
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1865 8 18 11 13 16 7 5 | 31 30 22 27 31 31 27
R03 | 1833 8 23 16 10 9 9 5 | 28 32 37 27 31 28 29
R04 | 2339 7 17 21 9 9 21 6 | 28 29 43 31 27 21 28
R05 | 2450 17 26 9 11 17 17 7 | 23 28 24 22 24 24 21
R07 | 1865 9 15 8 8 8 14 4 | 22 26 25 25 20 19 20
R08 | 1903 8 19 13 20 11 16 6 | 23 25 35 31 33 33 27
R09E | 2749 14 19 18 19 13 15 7 | 41 48 47 46 42 40 42
R11E | 2046 14 13 14 11 21 19 7 | 29 35 36 34 37 22 31
R12E | 1141 13 23 14 14 18 13 7 | 106 105 105 103 117 101 105
R14E | 2430 8 16 9 16 10 11 5 | 52 52 49 68 49 54 53
R15E | 1583 12 25 14 20 15 15 7 | 50 53 48 65 45 53 50
R16E | 1450 15 23 17 25 23 11 8 | 87 85 87 99 78 82 84
R17 | 2628 9 20 17 12 21 21 7 | 38 34 48 38 48 24 37
R18 | 1972 19 19 20 16 18 21 8 | 25 38 40 33 36 22 29
XR19 | 2033 12 11 15 --- 14 --- 7 | 20 36 29 --- 32 --- 25
R20 | 2811 40 84 42 45 25 39 20 | 56 29 43 51 45 41 39
R21 | 1501 8 28 14 16 17 20 7 | 38 31 43 50 49 31 39
XR22 | 1589 14 21 11 11 14 --- 7 | 17 33 24 29 32 --- 22
R24 | 1924 14 14 17 16 10 20 7 | 40 42 36 40 40 30 36
XR25 |17216 63 --- --- --- 75 --- 69 | 82 --- --- --- 127 --- 97
XR26 | 8493 39 43 36 --- 59 --- 26 | 27 29 31 --- 22 --- 23
XR27 |10785 55 56 --- 27 60 --- 30 | 58 53 --- 53 58 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 2081 15 28 18 18 16 18 |T 41 41 42 45 46 38 41
WRMS | 2081 13 37 16 15 16 18 |NE 34 33 34 35 40 27 34
MEDI | 1972 13 20 14 16 16 16 |MD 31 34 37 38 37 31 31
Table 3.2386.3 GPS week: 2386 Day: 3 MJD: 60949
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2988 11 17 9 14 22 14 6 | 38 28 36 37 31 35 33
R03 | 1824 8 30 13 12 17 8 6 | 39 47 38 37 37 38 37
R04 | 1612 11 23 8 11 12 12 5 | 44 53 48 45 44 50 45
R05 | 3460 9 26 22 4 12 10 6 | 36 45 43 39 36 38 37
R07 | 2824 10 15 17 11 18 9 6 | 42 38 42 39 40 43 39
R08 | 2738 14 19 15 8 10 26 7 | 41 44 49 48 40 50 43
XR09E | 4186 14 23 15 20 14 --- 8 | 40 47 45 44 42 --- 40
R11E | 1726 17 22 19 9 13 12 7 | 37 55 44 43 34 36 40
R12E | 1780 15 17 13 12 29 11 7 | 116 100 110 112 113 110 110
R14E | 3163 9 15 18 24 10 12 6 | 96 97 105 98 92 88 95
R15E | 2391 10 21 18 17 14 19 7 | 126 124 125 133 123 139 128
R16E | 1602 12 20 27 27 19 13 9 | 146 138 139 149 150 147 144
R17 | 2529 8 13 15 9 17 17 6 | 57 60 51 55 55 46 52
R18 | 2138 8 28 18 18 11 23 8 | 47 60 55 46 48 40 46
XR19 | 2486 13 15 15 --- 15 --- 8 | 29 31 41 --- 35 --- 32
R20 | 3473 35 94 34 38 26 31 18 | 75 51 64 65 71 64 64
R21 | 1574 9 28 13 10 18 22 7 | 55 38 58 58 53 51 52
XR22 | 1964 15 23 16 19 12 --- 8 | 30 39 39 36 32 --- 33
R24 | 2793 15 22 13 17 17 13 7 | 46 44 36 44 37 38 38
XR25 |14230 96 --- --- --- 141 --- 116 | 112 --- --- --- 165 --- 110
XR26 | 5966 41 47 34 --- 69 --- 28 | 47 38 35 --- 43 --- 36
XR27 | 9459 29 63 --- 28 46 --- 22 | 47 56 --- 61 60 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 2500 14 31 18 17 17 17 |T 61 58 60 62 62 63 59
WRMS | 2500 12 49 15 14 19 17 |NE 49 44 45 46 51 44 46
MEDI | 2529 12 22 15 14 17 13 |MD 46 47 45 46 43 46 43
Table 3.2386.4 GPS week: 2386 Day: 4 MJD: 60950
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 4630 8 18 20 12 25 17 7 | 26 32 26 27 30 21 22
R03 | 1776 12 26 18 9 23 12 7 | 26 24 19 21 36 18 19
R04 | 1125 15 25 10 10 14 16 6 | 26 26 24 26 31 18 21
R05 | 1826 13 34 16 12 12 11 7 | 25 23 26 28 26 20 21
R07 | 1620 10 21 16 12 16 6 6 | 24 28 26 25 28 22 22
R08 | 1631 16 14 13 16 10 20 7 | 28 23 27 31 26 29 25
XR09E | 2466 17 17 16 15 15 --- 8 | 33 40 43 39 37 --- 36
R11E | 1250 22 28 20 27 11 14 9 | 22 49 31 42 31 33 28
R12E | 2064 24 16 16 14 30 20 9 | 154 150 158 141 142 148 147
R14E | 2787 9 25 12 24 13 11 7 | 52 59 57 47 55 44 49
R15E | 1516 15 30 19 14 19 19 8 | 82 85 88 71 81 61 75
R16E | 2131 14 24 21 23 17 16 8 | 75 88 84 79 80 83 79
R17 | 1326 14 14 13 15 12 15 6 | 37 36 25 36 33 27 29
R18 | 1091 9 39 15 8 17 9 7 | 29 48 27 34 29 29 27
XR19 | 2224 19 13 10 --- 12 --- 8 | 21 32 32 --- 37 --- 27
R20 | 3195 41 95 32 38 32 27 19 | 65 41 54 41 36 42 44
R21 | 1744 15 21 15 19 18 13 7 | 40 38 45 50 38 33 39
XR22 | 2109 19 22 16 18 17 --- 9 | 19 23 28 23 27 --- 18
R24 | 2415 18 24 16 15 15 10 7 | 33 45 33 29 35 22 28
XR25 |15797 90 --- --- --- 102 --- 96 | 85 --- --- --- 104 --- 82
XR26 | 9888 43 52 40 --- 70 --- 30 | 35 35 36 --- 36 --- 29
XR27 | 9700 41 58 --- 28 47 --- 24 | 59 55 --- 46 60 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 2193 18 34 18 18 19 15 |T 45 46 44 44 47 40 41
WRMS | 2193 15 41 15 17 19 15 |NE 36 33 30 32 38 25 31
MEDI | 2064 15 24 16 15 17 14 |MD 33 38 31 36 36 29 28
Table 3.2386.5 GPS week: 2386 Day: 5 MJD: 60951
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 3745 8 18 13 9 10 16 5 | 32 35 38 38 32 34 33
R03 | 1230 9 18 10 9 19 16 6 | 32 36 35 33 32 34 32
R04 | 1049 6 24 7 11 10 17 5 | 33 37 34 38 29 32 33
R05 | 1411 15 21 12 17 17 16 7 | 36 41 27 43 33 30 32
R07 | 2195 11 19 9 13 15 14 6 | 35 35 37 33 37 34 34
R08 | 1780 14 22 12 13 13 14 6 | 37 38 38 44 39 37 37
XR09E | 1266 15 15 14 15 17 --- 7 | 83 78 82 87 77 --- 81
XR11E | 2246 13 23 13 17 13 --- 7 | 60 59 69 62 64 --- 62
R12E | 1413 12 19 14 21 25 19 8 | 128 128 127 132 137 131 129
R14E | 2190 9 16 14 20 19 9 6 | 100 107 109 108 95 99 102
R15E | 1990 11 16 11 17 20 13 6 | 124 126 124 131 123 121 123
R16E | 3053 10 22 14 27 20 12 8 | 132 132 121 131 127 136 129
R17 | 1355 13 16 14 10 15 12 6 | 42 38 43 50 44 42 42
R18 | 1204 15 29 14 16 10 17 7 | 46 50 50 46 44 51 46
XR19 | 1777 17 15 15 --- 16 --- 9 | 30 30 39 --- 33 --- 32
R20 | 2320 25 100 25 20 26 35 16 | 56 44 72 53 68 44 57
R21 | 1581 15 15 11 9 13 21 6 | 45 42 42 40 39 39 40
XR22 | 2119 15 28 14 13 14 --- 8 | 31 38 39 39 39 --- 34
R24 | 2952 17 30 13 8 15 11 7 | 44 52 43 47 40 40 42
XR25 |15559 63 --- --- --- 102 --- 80 | 101 --- --- --- 127 --- 104
XR26 |11178 31 82 34 --- 56 --- 27 | 43 46 47 --- 43 --- 42
XR27 |13652 29 44 --- 30 59 --- 23 | 43 44 --- 48 40 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 2107 13 33 14 16 17 17 |T 59 58 60 63 61 60 59
WRMS | 2107 13 29 12 13 18 17 |NE 42 40 41 42 44 37 42
MEDI | 1990 14 21 13 15 16 16 |MD 43 44 43 47 40 40 42
Table 3.2386.6 GPS week: 2386 Day: 6 MJD: 60952
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1547 9 12 17 7 12 13 5 | 33 33 38 34 36 37 32
R03 | 1309 7 17 10 12 16 7 5 | 36 35 34 37 38 31 33
R04 | 1125 16 18 16 8 19 22 7 | 36 38 37 35 38 33 33
R05 | 1147 12 13 8 14 11 6 5 | 34 38 31 34 30 31 31
R07 | 1518 5 37 6 13 15 8 6 | 37 39 42 45 38 37 38
R08 | 1637 14 24 17 7 15 11 6 | 37 34 45 40 40 36 37
R09E | 1425 13 14 13 10 19 9 6 | 90 95 97 93 97 105 93
R11E | 1968 15 18 14 12 13 13 6 | 56 59 57 56 64 68 57
R12E | 1335 14 21 20 16 26 10 8 | 142 131 141 133 130 136 136
R14E | 1760 11 14 12 23 13 9 6 | 98 102 100 108 96 96 99
R15E | 1310 17 19 14 22 19 13 7 | 95 99 106 112 100 99 101
R16E | 1329 9 23 18 35 21 10 9 | 127 114 115 150 118 123 124
R17 | 1350 9 21 7 14 19 16 6 | 52 44 47 53 55 40 47
R18 | 1031 15 21 13 16 22 11 7 | 44 60 45 50 53 49 48
XR19 | 1703 11 13 12 --- 11 --- 6 | 11 21 24 --- 20 --- 14
R20 | 3043 30 111 19 11 18 24 11 | 90 55 65 71 71 62 72
R21 | 1326 10 31 27 8 18 24 9 | 59 46 70 60 62 45 55
XR22 | 1413 15 21 19 14 14 --- 8 | 24 31 37 30 29 --- 26
R24 | 1970 17 22 19 9 22 13 7 | 50 47 46 41 43 34 41
XR25 |16594 52 --- --- --- 85 --- 67 | 86 --- --- --- 116 --- 91
XR26 |13612 27 54 47 --- 55 --- 26 | 39 46 38 --- 45 --- 34
XR27 |11908 28 54 --- 35 53 --- 24 | 46 49 --- 50 41 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 1604 14 34 16 16 18 14 |T 60 57 60 64 61 62 58
WRMS | 1604 13 39 13 12 18 14 |NE 44 41 42 44 47 39 42
MEDI | 1425 14 21 14 13 18 11 |MD 46 46 45 50 45 45 42
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