[IGSREPORT-30654] Wk 2387 IGLOS Final Orbits
acc
acc at igs.org
Thu Oct 23 06:28:03 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2387 (Oct 05, 2025 - Oct 11, 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 2.2387.
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:
igl2387[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2387 in the SP3 format.
igl23877.sum Combination Report for GPS Week 2387.
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 | 3.4 ns
1 | 2.8 ns
2 | 4.0 ns
3 | 2.9 ns
4 | 4.9 ns
5 | 4.1 ns
6 | 2.2 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
----+--------+---------------
1 | 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 1.2387, 1a.2387).
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 2.2387.0-6)
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 3.2387.0-6).
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 2387 summary. (Oct 05, 2025 - Oct 11, 2025)
Table 1.2387.a GPS week : 2387 MJD: 60953.0-60959.0
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 2 8 2 34 .16 15 13 | 559 -1032 3650 10962
| 0 1 1 17 21 17 .03 | 1567 2088
esa n/a| -1 -1 0 16 -4 55 -.04 31 35 | 734 -609 3639 11008
| 1 1 2 20 13 54 .03 | 1656 1593
gfz n/a| 0 0 0 18 16 -10 -.02 17 14 | 0 -1105 3334 7672
| 1 1 1 18 11 16 .05 | 0 2237
grg n/a| 0 0 -1 -40 -18 -11 .31 20 15 | 3199 -1035 3388 8933
| 1 2 1 21 19 33 .04 | 757 2149
iac n/a| 1 0 -5 25 26 -19 -.13 16 15 | 5304 -466 3600 10916
| 1 0 2 26 15 49 .06 | 2065 538
jgx n/a| 1 0 3 -15 -24 -16 -.23 16 16 | 2639 -1252 3452 8009
| 1 0 0 12 10 23 .02 | 765 2159
Table 1.2387.b GPS week : 2387 MJD: 60953.0-60959.0
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 | 5 8 8 7 6 7 7 |
R03 | 5 4 6 8 7 7 6 |
R04 | 5 6 6 6 7 6 5 |
R05 | 6 5 6 6 5 6 6 |
R07 | 6 7 5 4 5 5 8 |
R08 | 7 7 7 7 7 7 6 |
R09 | 7 7 7 8 6 7 6 |
R11 | 6 8 7 6 8 10 7 |
R12 | 10 6 6 10 6 7 9 |
R14 | 7 7 7 6 7 8 10 |
R15 | 9 8 8 9 7 7 8 |
R16 | 9 7 9 9 8 11 10 |
R17 | 6 6 7 6 5 6 6 |
R18 | 8 8 6 8 6 8 9 |
R19 | 7 8 8 8 9 6 8 |
R20 | 22 21 20 18 17 20 13 |
R21 | 6 7 6 7 7 6 8 |
R22 | 7 7 6 8 7 8 8 |
R24 | 6 7 7 6 7 7 8 |
R25 | 97 83 57 68 152 --- --- |
R26 | 29 27 26 37 40 31 32 |
R27 | 25 28 29 28 27 26 26 |
Table 1.2387.c GPS week : 2387 MJD: 60953.0-60959.0
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 2387 0 | 17 -27 -193 -887 1999 -2819 78.4 1658 1658 | 3379 0
brd 2387 1 | 76 47 -172 -904 1229 -1024 82.3 1965 1965 | 2777 0
brd 2387 2 | -111 101 -91 -1202 1551 -1250 80.2 1829 1829 | 4008 0
brd 2387 3 | 84 43 -137 694 512 -3256 82.7 2017 2017 | 2882 0
brd 2387 4 | -195 9 -57 -160 2974 -3887 80.5 2047 2047 | 4890 0
brd 2387 5 | -17 31 -115 -405 1488 -7793 82.2 1814 1814 | 4112 0
brd 2387 6 | -40 31 -96 -1856 734 -6916 79.7 2152 2152 | 2157 0
-------------+------------------------------------------------------------+----------------
brd 2387 mean| -26 33 -123 -674 1498 -3849 80.9 1926 1926 | 3457 0
brd 2387 sdev| 100 39 47 814 822 2617 1.6 167 167 | 937 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 2.2387.0 GPS week: 2387 Day: 0 MJD: 60953
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 37 20 34 .17 19 15 | 1321 195 3288 8801
esa n/a| -1 -2 0 21 13 121 -.08 32 39 | 418 731 3250 9020
gfz n/a| 0 -2 0 -1 4 -15 .05 15 14 | 0 335 3333 8233
grg n/a| -2 3 -4 -49 -22 -16 .31 18 16 | 2666 299 3402 8717
iac n/a| 4 2 -6 34 22 -35 -.20 20 18 | 5006 430 3283 9235
jgx n/a| 0 0 4 1 -20 -9 -.23 13 13 | 3771 374 3544 8464
Table 2.2387.1 GPS week: 2387 Day: 1 MJD: 60954
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 -2 0 0 10 49 .15 17 14 | -519 -3005 3367 9018
esa n/a| -1 -2 -2 32 9 -35 -.05 34 30 | -1128 -2450 3356 9225
gfz n/a| -1 -1 1 29 10 -35 -.02 15 12 | 0 -2723 3441 8571
grg n/a| 0 3 -2 -38 13 -50 .39 19 15 | 3661 -2964 3437 9059
iac n/a| 0 0 -3 10 9 24 -.11 15 14 | 3290 -614 3354 9463
jgx n/a| 1 1 2 -17 -23 5 -.23 18 18 | 2228 -3190 3585 8969
Table 2.2387.2 GPS week: 2387 Day: 2 MJD: 60955
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 2 6 -2 44 .11 11 9 | -309 622 3006 8363
esa n/a| -3 0 -1 9 -6 52 .01 27 30 | 295 528 3018 8221
gfz n/a| 0 -1 3 13 9 -4 -.12 19 16 | 0 610 3049 7094
grg n/a| -1 0 0 -81 -50 46 .33 22 14 | 3374 -154 2987 8624
iac n/a| 2 0 -7 50 46 -82 -.11 16 13 | 6200 -383 3173 9362
jgx n/a| 2 1 3 -13 -40 -10 -.18 19 19 | 3157 57 3089 7536
Table 2.2387.3 GPS week: 2387 Day: 3 MJD: 60956
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 -1 -25 42 .16 13 12 | 3712 -3009 5395 23562
esa n/a| -2 0 -3 6 -2 68 -.04 30 34 | 4197 -2169 5394 23413
gfz n/a| 0 -1 0 -1 40 -21 -.00 17 13 | 0 -3940 3193 7193
grg n/a| 1 -1 0 -41 -6 8 .35 22 13 | 3985 -3824 3160 8794
iac n/a| 2 0 -2 64 9 -69 -.20 16 15 | 8960 -1070 4908 22040
jgx n/a| 1 1 3 -29 -14 0 -.26 16 16 | 1700 -3766 3251 7390
Table 2.2387.4 GPS week: 2387 Day: 4 MJD: 60957
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 1 -11 -12 8 .19 16 15 | -916 196 3695 9642
esa n/a| 0 -2 2 49 -4 7 .00 31 43 | -104 370 3667 9721
gfz n/a| 1 1 -1 17 18 -16 -.05 14 15 | 0 699 3731 8170
grg n/a| 0 -1 1 -20 -18 -46 .30 16 12 | 3815 928 3802 9948
iac n/a| 0 0 -3 7 29 55 -.14 14 14 | 6293 -1076 3682 9860
jgx n/a| 0 0 2 -2 -14 -2 -.22 13 13 | 1771 636 3918 8626
Table 2.2387.5 GPS week: 2387 Day: 5 MJD: 60958
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 4 29 -9 12 .13 15 13 | 269 1395 3403 9634
esa n/a| -1 0 2 9 -28 103 -.04 30 38 | 788 1001 3386 9406
gfz n/a| 0 0 0 49 13 13 -.02 20 13 | 0 984 3183 7657
grg n/a| 0 0 -1 -16 -20 -24 .26 18 14 | 1820 1432 3504 9804
iac n/a| 1 1 -8 -13 46 -4 -.04 17 16 | 4435 -52 3401 9101
jgx n/a| 2 0 2 -30 -24 -41 -.22 18 18 | 2963 787 3308 8033
Table 2.2387.6 GPS week: 2387 Day: 6 MJD: 60959
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 0 37 52 .17 14 13 | 359 -3624 3402 7719
esa n/a| 0 -3 0 -16 -12 70 -.06 32 30 | 675 -2277 3403 8053
gfz n/a| -2 1 -2 24 16 6 .03 19 17 | 0 -3705 3408 6789
grg n/a| 2 1 -3 -33 -26 1 .28 21 21 | 3078 -2964 3424 7585
iac n/a| 0 0 -4 23 17 -20 -.07 16 16 | 2950 -502 3401 7356
jgx n/a| 0 0 4 -16 -37 -56 -.24 15 15 | 2887 -3668 3472 7048
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 3.2387.0 GPS week: 2387 Day: 0 MJD: 60953
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2053 13 15 9 11 15 10 5 | 29 34 29 25 30 21 24
R03 | 1649 7 22 11 17 10 5 5 | 33 36 38 39 34 36 34
R04 | 1271 11 17 12 9 11 10 5 | 35 40 32 40 37 29 33
R05 | 1955 9 23 17 9 12 8 6 | 31 44 40 36 35 31 33
R07 | 993 12 21 9 8 17 16 6 | 42 44 44 46 47 40 42
R08 | 1409 13 19 15 16 15 11 6 | 39 42 47 38 42 35 39
R09E | 1423 16 14 14 17 15 10 6 | 59 68 69 64 58 66 63
R11E | 1051 13 17 14 14 15 8 6 | 63 60 58 62 64 57 60
R12E | 1975 13 23 20 18 42 15 10 | 157 167 170 169 145 159 160
R14E | 2411 10 24 16 21 11 8 6 | 56 48 57 67 53 54 55
R15E | 1261 21 19 10 29 20 14 8 | 74 79 72 91 71 71 74
R16E | 940 9 25 19 37 20 10 9 | 75 70 73 91 77 73 75
R17 | 1200 5 21 9 8 22 10 5 | 78 67 80 80 86 75 78
R18 | 975 19 20 14 14 18 15 7 | 67 80 73 74 66 64 68
XR19 | 1695 13 9 6 --- 15 --- 6 | 29 31 35 --- 33 --- 30
R20 | 3306 62 105 31 26 34 36 21 | 103 65 79 71 67 66 70
R21 | 998 8 24 8 21 15 8 6 | 78 71 76 81 66 72 73
XR22 | 1444 14 16 13 12 9 --- 6 | 102 104 104 108 101 --- 103
R24 | 1321 14 21 12 11 16 9 6 | 69 69 65 64 63 62 64
XR25 |22448 86 --- --- --- 109 --- 97 | 66 --- --- --- 72 --- 65
XR26 |11238 27 53 45 --- 70 --- 28 | 47 90 62 --- 84 --- 63
XR27 |13249 39 49 --- 29 57 --- 25 | 73 120 --- 85 111 --- 91
------+-----------------------------------------+-------------------------------------
RMS | 1658 19 32 15 18 20 13 |T 63 68 65 70 65 59 63
WRMS | 1658 15 39 14 16 18 13 |NE 57 62 57 60 60 48 56
MEDI | 1423 13 21 13 16 15 10 |MD 63 67 62 67 64 62 63
Table 3.2387.1 GPS week: 2387 Day: 1 MJD: 60954
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 2423 11 11 26 17 6 22 7 | 20 17 30 17 17 19 16
R03 | 2066 7 11 9 10 10 7 4 | 23 26 23 27 19 28 22
R04 | 2055 10 15 19 14 13 13 6 | 24 32 22 34 24 24 23
R05 | 2170 8 12 15 13 7 7 4 | 17 26 23 24 20 17 17
R07 | 3842 12 26 10 16 14 19 7 | 39 44 34 36 36 38 35
R08 | 1540 14 29 10 22 16 9 7 | 36 40 35 28 34 29 31
R09E | 1839 16 12 11 17 17 11 6 | 31 37 37 32 35 35 32
R11E | 974 13 24 17 23 16 15 7 | 32 26 28 20 32 31 26
R12E | 1515 10 17 14 17 12 9 5 | 110 116 116 111 104 106 109
R14E | 1605 12 27 13 25 12 8 7 | 30 39 27 33 27 28 26
R15E | 1645 14 23 12 19 15 22 8 | 47 46 46 48 43 45 44
R16E | 1429 11 21 14 23 12 9 6 | 43 46 44 45 43 43 42
R17 | 1476 8 12 9 12 18 14 5 | 38 40 42 45 52 36 41
R18 | 1358 12 40 12 13 12 8 7 | 34 56 33 38 36 37 36
XR19 | 3458 13 14 14 --- 14 --- 8 | 19 29 28 --- 25 --- 22
R20 | 2982 52 111 25 40 31 53 21 | 45 37 43 30 24 56 35
R21 | 1171 15 22 12 11 16 8 6 | 47 50 41 42 31 42 39
XR22 | 1313 12 12 19 18 9 --- 7 | 100 102 99 113 103 --- 102
R24 | 1082 19 21 15 9 11 11 6 | 36 39 29 37 32 31 31
XR25 |23383 80 --- --- --- 86 --- 83 | 83 --- --- --- 44 --- 55
XR26 | 7453 49 54 26 --- 52 --- 26 | 20 35 35 --- 32 --- 25
XR27 |15388 49 59 --- 33 48 --- 27 | 46 85 --- 59 75 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 1965 17 34 15 19 15 18 |T 41 46 40 43 40 37 39
WRMS | 1965 14 30 12 15 14 18 |NE 39 43 36 40 37 32 36
MEDI | 1645 12 21 14 17 14 11 |MD 36 39 34 36 32 35 32
Table 3.2387.2 GPS week: 2387 Day: 2 MJD: 60955
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1961 12 17 17 22 16 22 7 | 27 29 24 16 38 15 23
R03 | 1302 8 12 26 7 8 13 6 | 21 28 38 24 22 20 23
R04 | 1688 10 14 9 14 13 21 6 | 20 22 20 28 25 16 19
R05 | 1011 7 17 9 9 20 14 6 | 21 17 22 21 23 23 17
R07 | 3570 6 14 15 12 12 10 5 | 31 30 38 29 34 30 31
R08 | 1816 11 21 19 19 11 8 6 | 37 37 35 42 40 41 37
R09E | 1205 13 16 17 18 14 10 6 | 33 41 43 40 36 41 36
R11E | 1172 12 16 16 21 14 13 6 | 28 20 30 29 26 27 24
R12E | 1004 9 17 11 17 13 16 6 | 73 73 69 67 68 71 69
R14E | 1740 7 24 14 24 8 11 6 | 26 29 26 41 25 24 24
R15E | 1565 6 21 12 33 17 14 7 | 58 70 64 69 58 60 60
R16E | 2328 7 26 19 44 10 14 9 | 45 54 52 69 46 47 47
R17 | 1375 8 23 19 12 9 18 6 | 47 40 57 50 43 39 45
R18 | 988 9 21 15 13 13 17 6 | 39 48 48 45 32 40 39
XR19 | 3538 14 15 11 --- 15 --- 8 | 20 30 30 --- 35 --- 25
R20 | 3350 28 81 45 38 40 51 20 | 64 43 65 63 50 56 55
R21 | 1333 7 17 12 14 14 11 5 | 49 40 53 48 41 47 46
XR22 | 1850 12 12 11 13 13 --- 6 | 103 99 106 102 93 --- 100
R24 | 901 12 17 10 6 8 25 6 | 46 43 46 43 38 34 41
XR25 |18046 45 --- --- --- 71 --- 57 | 105 --- --- --- 71 --- 79
XR26 |12644 39 43 27 --- 62 --- 26 | 20 48 35 --- 41 --- 26
XR27 | 9922 47 65 --- 26 56 --- 29 | 84 96 --- 89 87 --- 85
------+-----------------------------------------+-------------------------------------
RMS | 1829 11 27 19 22 16 19 |T 45 44 45 48 44 37 43
WRMS | 1829 9 30 16 14 13 19 |NE 45 43 44 46 44 32 43
MEDI | 1688 10 17 15 17 13 14 |MD 37 40 38 43 38 39 37
Table 3.2387.3 GPS week: 2387 Day: 3 MJD: 60956
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1148 12 20 14 17 10 19 6 | 26 33 29 18 23 20 22
R03 | 1341 10 36 16 9 11 20 7 | 32 42 32 34 32 26 29
R04 | 1171 8 29 10 7 16 13 6 | 31 33 30 31 29 20 26
R05 | 829 9 26 10 8 10 13 5 | 22 25 24 24 20 22 20
R07 | 829 7 15 10 11 8 9 4 | 35 33 36 36 32 30 32
R08 | 2088 10 24 17 25 11 10 7 | 34 45 31 29 25 31 28
R09E | 1433 17 14 19 19 14 20 7 | 28 32 36 28 31 35 29
R11E | 1968 12 11 15 17 15 10 6 | 21 26 31 18 23 20 21
R12E | 1458 16 24 11 18 30 24 9 | 81 89 82 77 70 68 75
R14E | 1865 10 15 15 21 10 8 5 | 30 31 36 34 28 26 28
R15E | 2614 14 26 22 27 21 13 9 | 42 49 59 44 48 44 44
R16E | 2102 10 24 23 42 12 9 9 | 43 49 41 47 45 41 39
R17 | 1595 7 20 10 20 9 18 6 | 51 41 53 62 51 43 50
R18 | 1332 13 30 15 18 15 20 8 | 41 54 46 48 38 36 41
XR19 | 2222 13 11 17 --- 11 --- 7 | 21 22 32 --- 28 --- 24
R20 | 5464 25 85 32 48 35 24 17 | 68 44 55 78 51 70 58
R21 | 1203 15 19 14 13 11 19 6 | 56 42 47 52 51 44 49
XR22 | 2186 11 36 17 9 10 --- 8 | 44 65 46 41 41 --- 43
R24 | 714 17 9 14 10 10 12 6 | 45 48 42 49 49 44 44
XR25 |18505 60 --- --- --- 76 --- 68 | 64 --- --- --- 54 --- 40
XR26 |10238 51 45 --- --- 55 --- 36 | 22 56 --- --- 56 --- 35
XR27 | 9716 41 47 --- 38 61 --- 28 | 31 55 --- 23 50 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 2017 13 30 17 22 16 16 |T 39 43 41 40 39 36 36
WRMS | 2017 12 34 13 13 15 16 |NE 38 42 38 40 39 35 36
MEDI | 1595 12 24 15 18 11 13 |MD 34 42 36 36 38 35 35
Table 3.2387.4 GPS week: 2387 Day: 4 MJD: 60957
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1030 19 19 8 18 9 6 6 | 25 27 19 27 19 20 20
R03 | 1925 12 24 13 8 8 19 6 | 36 44 39 37 34 31 35
R04 | 1453 15 28 10 10 16 12 6 | 36 31 28 29 37 32 30
R05 | 1188 8 21 12 9 10 7 5 | 25 25 24 25 23 23 22
R07 | 1932 8 15 8 10 12 8 4 | 29 23 24 30 32 24 26
R08 | 2418 19 12 21 11 12 9 6 | 34 36 40 35 40 31 34
R09E | 2307 17 22 12 9 12 7 5 | 41 44 44 42 42 39 40
R11E | 2359 19 12 20 16 22 10 7 | 35 33 33 28 35 30 30
R12E | 1885 15 14 12 13 15 11 6 | 78 70 75 66 68 64 69
R14E | 1106 9 18 10 22 17 9 6 | 41 33 38 44 33 33 35
R15E | 2690 11 19 11 24 18 10 7 | 48 54 44 58 42 43 46
R16E | 1789 14 25 17 23 9 14 7 | 56 70 56 62 52 60 56
R17 | 1247 10 14 8 17 10 7 5 | 48 52 46 62 47 52 49
R18 | 1282 12 21 12 11 10 13 5 | 39 46 43 42 35 36 38
XR19 | 3446 17 13 12 --- 15 --- 8 | 20 23 24 --- 25 --- 19
R20 | 4721 32 95 27 27 24 28 16 | 65 39 61 57 57 58 54
R21 | 969 12 27 10 16 11 20 7 | 46 38 43 53 45 33 42
XR22 | 1272 14 20 14 16 11 --- 7 | 88 90 83 97 87 --- 88
R24 | 918 17 32 17 12 6 10 7 | 42 46 35 36 32 40 35
XR25 |24695 162 --- --- --- 143 --- 152 | 173 --- --- --- 92 --- 103
XR26 | 6059 44 59 84 --- 75 --- 40 | 22 42 75 --- 56 --- 33
XR27 | 5293 43 67 --- 39 44 --- 26 | 76 106 --- 81 96 --- 87
------+-----------------------------------------+-------------------------------------
RMS | 2047 16 31 14 16 14 13 |T 50 46 43 47 46 38 45
WRMS | 2047 15 43 15 12 14 13 |NE 50 44 41 47 47 34 44
MEDI | 1885 15 21 12 16 12 10 |MD 41 42 40 42 40 33 35
Table 3.2387.5 GPS week: 2387 Day: 5 MJD: 60958
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1698 9 24 14 13 17 16 6 | 26 29 25 20 27 27 22
R03 | 1408 6 28 10 14 21 16 7 | 31 38 21 34 35 27 27
R04 | 1500 8 22 9 14 11 13 5 | 30 35 30 27 28 24 27
R05 | 1208 10 18 14 14 14 10 6 | 32 25 31 27 36 26 27
R07 | 2003 9 16 12 5 19 5 5 | 28 31 28 28 34 29 27
R08 | 2860 16 19 14 15 12 21 7 | 33 38 29 31 30 31 28
R09E | 1946 15 18 13 22 17 9 7 | 74 77 78 79 68 72 73
R11E | 1644 15 32 24 22 19 18 9 | 53 39 58 42 50 55 49
R12E | 1639 11 17 12 17 15 16 6 | 96 106 101 102 104 103 101
R14E | 1785 9 17 14 26 22 17 8 | 55 45 45 55 51 52 49
R15E | 2299 13 17 20 16 16 13 7 | 65 60 64 63 56 62 60
R16E | 2009 17 26 45 22 18 12 11 | 60 54 73 64 60 60 59
R17 | 1262 15 20 18 11 11 10 6 | 45 43 35 45 37 38 39
R18 | 922 15 30 13 9 19 24 8 | 45 46 35 41 44 44 40
XR19 | 2080 11 14 7 --- 10 --- 6 | 24 27 25 --- 30 --- 25
R20 | 2889 37 89 38 39 26 40 19 | 63 39 68 35 42 48 47
R21 | 1120 12 16 10 12 13 17 6 | 47 41 41 45 44 37 41
XR22 | 1158 13 24 11 16 18 --- 8 | 68 65 69 75 63 --- 66
R24 | 1205 18 24 14 14 11 14 7 | 43 51 46 44 40 39 41
XR26 | 5543 47 60 36 --- 70 --- 31 | 31 52 44 --- 46 --- 36
XR27 | 3661 34 58 --- 37 55 --- 26 | 98 107 --- 89 93 --- 94
------+-----------------------------------------+-------------------------------------
RMS | 1814 15 30 20 18 17 18 |T 49 49 47 49 48 45 46
WRMS | 1814 13 38 13 14 16 18 |NE 42 44 37 41 41 33 39
MEDI | 1698 13 22 14 15 17 16 |MD 45 43 41 44 44 39 41
Table 3.2387.6 GPS week: 2387 Day: 6 MJD: 60959
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1367 14 15 11 11 23 8 6 | 32 42 40 28 39 28 32
R03 | 1576 8 16 12 13 21 12 6 | 45 47 49 49 46 39 44
R04 | 1681 9 14 11 11 10 12 5 | 43 44 39 40 44 34 39
R05 | 1294 8 12 23 14 16 7 6 | 42 36 44 35 34 36 36
R07 | 1879 14 18 19 13 16 19 7 | 40 34 36 37 44 35 36
R08 | 1824 12 15 11 20 12 14 6 | 38 41 38 45 41 38 38
R09E | 2023 15 7 17 10 13 14 6 | 55 56 62 56 52 63 56
R11E | 2087 15 21 14 15 17 10 7 | 36 27 32 35 38 38 34
R12E | 943 12 24 18 24 17 20 8 | 153 152 153 156 152 151 152
R14E | 2129 8 16 18 51 14 14 10 | 43 37 39 57 43 38 38
R15E | 1038 12 15 20 24 16 19 7 | 48 44 45 56 49 49 46
R16E | 1803 10 19 31 39 15 12 9 | 50 48 52 62 51 50 49
R17 | 1641 13 20 11 11 9 11 5 | 64 59 60 65 62 54 60
R18 | 1073 16 27 31 19 14 8 8 | 54 69 50 50 51 47 50
XR19 | 1128 11 16 16 --- 14 --- 8 | 36 36 33 --- 31 --- 31
R20 | 6093 32 110 18 15 25 21 12 | 89 52 74 66 68 58 71
R21 | 1697 13 20 20 11 13 26 8 | 59 46 59 56 59 47 53
XR22 | 1119 14 12 13 24 15 --- 8 | 84 88 85 94 84 --- 85
R24 | 968 14 21 19 15 13 19 7 | 58 50 56 55 49 39 49
XR26 | 8744 48 63 55 --- 60 --- 32 | 34 78 30 --- 70 --- 47
XR27 | 7429 37 47 --- 41 51 --- 25 | 106 133 --- 102 122 --- 113
------+-----------------------------------------+-------------------------------------
RMS | 2151 14 32 19 21 16 15 |T 57 58 53 60 58 49 55
WRMS | 2151 13 30 17 21 16 15 |NE 54 57 49 55 56 41 52
MEDI | 1681 13 18 18 15 15 14 |MD 48 47 45 56 49 39 47
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