[IGSREPORT-30424] Wk 2362 IGLOS Final Orbits
acc
acc at igs.org
Fri May 2 06:12:01 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2362 (Apr 13, 2025 - Apr 19, 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 2.2362.
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:
igl2362[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2362 in the SP3 format.
igl23627.sum Combination Report for GPS Week 2362.
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 | 4.1 ns
1 | 6.8 ns
2 | 8.4 ns
3 | 6.3 ns
4 | 5.1 ns
5 | 7.2 ns
6 | 6.6 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 | GFZ | R12 R14 R15 R16
1 | ALL | R26
2 | ALL | R26
3 | ALL | R26
3 | ESA | R20
4 | ESA | R20
5 | 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 1.2362, 1a.2362).
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 2.2362.0-6)
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 3.2362.0-6).
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 2362 summary. (Apr 13, 2025 - Apr 19, 2025)
Table 1.2362.a GPS week : 2362 MJD: 60778.0-60784.0
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| 0 1 5 11 -7 27 .10 17 14 | 16545 1274 5297 58449
| 1 0 1 17 17 20 .06 | 12359 1776
esa n/a| -2 -2 2 11 -26 55 -.01 38 43 | 6832 -1053 4021 20988
| 1 2 1 18 17 58 .05 | 7342 2544
gfz n/a| 1 0 -1 10 -1 -39 .02 38 16 | 0 -362 3700 8086
| 0 1 1 10 20 18 .06 | 0 2036
grg n/a| 1 0 3 -44 6 -17 .26 25 19 | 6532 -618 3612 7749
| 1 1 3 22 17 46 .04 | 867 1658
iac n/a| 0 0 -3 -2 15 -1 -.16 17 16 | 21388 1091 5329 59666
| 1 1 2 9 13 43 .08 | 12309 988
jgx n/a| 0 0 -6 21 12 -4 -.19 24 24 | 3532 -648 3623 8062
| 0 1 1 12 15 17 .04 | 1192 1640
Table 1.2362.b GPS week : 2362 MJD: 60778.0-60784.0
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 6 5 6 8 |
R03 | 7 7 6 7 5 6 7 |
R04 | 7 8 6 8 6 7 5 |
R05 | 6 6 7 8 7 7 6 |
R07 | 6 6 5 8 8 7 6 |
R08 | 6 7 5 7 10 9 8 |
R09 | 19 7 7 7 9 7 6 |
R11 | 14 7 6 8 7 7 7 |
R12 | 13 8 7 6 9 9 7 |
R14 | 11 7 7 7 7 7 7 |
R15 | 10 9 7 6 7 7 7 |
R16 | 17 10 9 11 10 9 7 |
R17 | 6 7 7 10 6 7 7 |
R18 | 7 8 9 9 7 8 9 |
R19 | 22 24 20 17 20 19 16 |
R20 | 23 24 23 18 14 19 17 |
R21 | 9 9 7 7 9 8 8 |
R22 | 10 6 8 7 8 12 9 |
R24 | 8 9 8 8 9 9 9 |
R26 | 51 --- --- --- 31 33 30 |
R27 | 43 49 49 45 48 45 51 |
Table 1.2362.c GPS week : 2362 MJD: 60778.0-60784.0
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 2362 0 | 79 126 79 -280 1935 11140 79.2 1875 1875 | 4074 0
brd 2362 1 | -2 2 114 1004 1629 11250 80.1 1939 1939 | 6823 0
brd 2362 2 | -26 52 101 1077 -1459 12440 79.8 2117 2117 | 8401 0
brd 2362 3 | 25 -14 154 -266 -230 11780 79.2 1994 1994 | 6330 0
brd 2362 4 | 75 1 40 473 804 9972 82.2 1853 1853 | 5118 0
brd 2362 5 | -1 59 72 -1215 -242 7150 81.2 1851 1851 | 7242 0
brd 2362 6 | -20 -18 -20 -1008 746 9085 79.9 2130 2130 | 6633 0
-------------+------------------------------------------------------------+----------------
brd 2362 mean| 18 29 77 -30 454 10402 80.2 1965 1965 | 6374 0
brd 2362 sdev| 43 52 55 915 1182 1817 1.1 119 119 | 1414 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 2.2362.0 GPS week: 2362 Day: 0 MJD: 60778
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 3 -31 -4 .08 21 16 | 22639 -2002 7185 77274
esa n/a| -2 -4 1 24 -9 143 .07 36 27 | 4610 -4018 2932 7707
gfz n/a| 3 0 2 1 38 -39 .07 156 24 | 0 -3765 3169 7807
grg n/a| 3 0 1 -37 38 71 .23 34 28 | 5730 -3595 2944 7396
iac n/a| -1 1 -5 -14 2 -47 -.30 16 14 | 25503 239 7266 78988
jgx n/a| 0 0 -4 20 25 -20 -.14 27 27 | 4445 -3586 2956 7864
Table 2.2362.1 GPS week: 2362 Day: 1 MJD: 60779
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 -17 2 42 .07 16 12 | 15147 768 4191 57920
esa n/a| -3 -6 1 30 -13 79 -.00 36 38 | 4981 -3476 3129 7975
gfz n/a| 2 0 0 1 -23 -22 .05 21 13 | 0 -1652 3132 7274
grg n/a| 0 1 9 -33 -11 -49 .26 30 21 | 7249 -1339 3140 7185
iac n/a| 1 0 -5 10 7 -13 -.17 17 16 | 20362 1721 4207 59564
jgx n/a| 0 0 -7 46 -8 0 -.16 27 27 | 3762 -1381 3173 7483
Table 2.2362.2 GPS week: 2362 Day: 2 MJD: 60780
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 4 8 -10 42 .12 15 13 | 16720 2510 4811 64198
esa n/a| -2 -1 4 15 -31 17 .02 36 41 | 2602 1984 3252 8385
gfz n/a| 1 1 -3 4 -7 -61 .02 16 14 | 0 853 3244 8340
grg n/a| 0 -1 3 -42 5 -52 .26 25 21 | 7799 858 3263 8275
iac n/a| -1 -1 -3 2 30 28 -.19 16 15 | 22853 851 4879 65841
jgx n/a| 0 0 -6 25 10 5 -.18 27 27 | 3593 790 3228 8371
Table 2.2362.3 GPS week: 2362 Day: 3 MJD: 60781
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 5 17 -29 17 .10 17 14 | 18943 596 5484 70759
esa n/a| 0 -4 3 24 -19 -25 -.03 39 49 | 4782 -3124 4307 8097
gfz n/a| 1 0 0 16 -7 -23 -.02 18 18 | 0 -774 4288 7594
grg n/a| 0 0 3 -52 -6 -64 .21 22 20 | 6803 -1030 4303 7434
iac n/a| 0 1 -4 -4 36 32 -.04 15 15 | 23915 420 5522 72379
jgx n/a| 1 0 -7 15 -1 2 -.21 25 25 | 4118 -1126 4282 7804
Table 2.2362.4 GPS week: 2362 Day: 4 MJD: 60782
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 2 5 30 12 7 .21 18 15 | 37986 2055 7056 121045
esa n/a| -3 2 3 10 -56 113 -.10 41 48 | 23369 -1200 6884 100132
gfz n/a| 1 0 -1 32 -18 -20 -.09 17 14 | 0 -880 4382 9455
grg n/a| 2 -2 0 -82 2 11 .31 22 14 | 5243 -934 4354 9233
iac n/a| -1 0 -2 6 17 -71 -.14 20 20 | 43052 2235 7120 123193
jgx n/a| 1 -2 -6 9 36 -4 -.24 20 20 | 908 -868 4454 9622
Table 2.2362.5 GPS week: 2362 Day: 5 MJD: 60783
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 7 32 5 39 .03 18 17 | 2135 1414 3749 10343
esa n/a| -2 -1 0 -16 -12 31 -.00 38 46 | 4178 883 3707 7836
gfz n/a| 1 2 -1 8 3 -65 .06 18 14 | 0 1733 3742 8793
grg n/a| 3 -3 1 -53 21 -24 .30 22 15 | 6487 1267 3696 7749
iac n/a| -1 0 1 -14 7 23 -.21 20 19 | 7371 -121 3715 9613
jgx n/a| 1 0 -10 18 16 17 -.21 25 25 | 3773 1226 3675 8014
Table 2.2362.6 GPS week: 2362 Day: 6 MJD: 60784
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 5 2 -1 49 .11 17 14 | 2251 3581 4603 7607
esa n/a| -1 -1 3 -10 -39 29 -.05 38 53 | 3302 1576 3936 6787
gfz n/a| 2 0 -2 7 2 -44 .07 16 14 | 0 1948 3946 7340
grg n/a| 2 0 0 -8 -5 -11 .28 21 17 | 6414 442 3589 6975
iac n/a| 0 0 -4 -2 6 39 -.08 14 14 | 6661 2296 4599 8084
jgx n/a| 0 0 -4 11 7 -34 -.21 20 20 | 4125 407 3593 7281
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 3.2362.0 GPS week: 2362 Day: 0 MJD: 60778
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1080 13 19 7 15 16 12 6 | 54 58 54 59 59 47 54
R03 | 922 14 27 10 12 10 19 6 | 60 69 59 67 62 50 60
R04 | 1002 14 14 8 15 13 25 7 | 56 54 49 47 50 38 49
R05 | 1065 12 14 15 9 8 25 6 | 52 50 48 47 52 43 47
R07 | 2072 11 21 8 13 12 7 5 | 57 45 57 61 55 53 54
R08 | 919 10 16 12 16 11 14 5 | 49 54 53 58 54 46 51
R09E | 3798 21 24 100 23 14 21 19 | 60 59 128 57 58 48 62
R11E | 3502 12 16 67 28 16 19 13 | 33 39 75 41 37 39 36
R12E | 2065 11 26 330 49 22 18 13 | 134 143 328 147 131 141 135
R14E | 1059 12 22 316 43 10 23 11 | 32 36 289 56 37 30 34
R15E | 1753 10 24 344 29 18 19 9 | 43 49 306 45 51 44 43
R16E | 2168 29 19 343 69 14 19 17 | 60 49 308 81 60 51 54
R17 | 923 6 17 11 13 11 23 6 | 53 43 56 50 50 40 49
R18 | 949 13 14 21 18 12 17 7 | 39 46 46 36 40 37 39
R19 | 1257 67 59 25 60 34 42 22 | 60 44 72 60 51 73 54
R20 | 2329 19 107 28 61 16 75 23 | 86 44 98 112 94 76 88
R21 | 935 10 26 27 28 9 29 9 | 55 45 68 75 67 50 59
R22 | 2702 12 45 11 25 16 15 9 | 12 31 18 34 30 18 19
R24 | 813 17 31 10 20 13 18 8 | 52 38 51 54 57 43 49
XR26 |10081 56 --- --- --- 45 --- 51 | 60 --- --- --- 103 --- 79
XR27 |11012 47 --- --- --- 38 --- 42 | 50 --- --- --- 86 --- 66
------+-----------------------------------------+-------------------------------------
RMS | 1874 21 36 156 34 16 27 |T 55 52 113 62 61 50 56
WRMS | 1874 16 27 24 28 14 27 |NE 53 47 56 58 60 47 54
MEDI | 1257 13 22 21 23 14 19 |MD 54 46 59 57 55 46 54
Table 3.2362.1 GPS week: 2362 Day: 1 MJD: 60779
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1123 8 17 9 19 15 11 5 | 33 27 32 28 30 31 28
R03 | 1630 9 30 12 15 13 11 6 | 36 51 34 43 38 34 36
R04 | 664 8 24 23 23 11 23 8 | 44 57 55 33 45 35 44
R05 | 1740 10 17 14 14 15 13 6 | 41 54 50 40 57 46 47
R07 | 945 8 16 12 19 12 15 6 | 38 30 39 49 33 28 35
R08 | 805 10 12 8 23 19 23 7 | 33 34 40 49 49 28 37
R09E | 4398 12 20 16 18 16 9 6 | 45 46 47 47 43 36 43
R11E | 3588 14 21 14 13 15 13 6 | 25 37 35 30 35 25 28
R12E | 1128 13 21 29 17 16 12 8 | 81 77 112 85 83 80 82
R14E | 2737 10 26 14 14 14 10 6 | 34 43 63 40 36 34 34
R15E | 635 10 25 18 33 13 21 8 | 53 43 75 73 59 56 55
R16E | 1065 12 24 33 32 17 12 10 | 44 56 86 64 45 51 48
R17 | 1002 6 23 15 15 18 22 7 | 28 27 29 29 37 27 28
R18 | 893 11 19 17 14 16 28 7 | 22 27 27 26 23 16 21
R19 | 1201 54 75 55 66 17 48 23 | 38 55 76 39 33 34 36
R20 | 2261 14 104 27 74 31 78 23 | 30 20 36 60 32 44 29
R21 | 886 7 34 11 26 17 28 8 | 27 23 25 41 30 23 26
R22 | 3170 11 13 9 16 11 15 5 | 13 20 19 27 18 14 14
R24 | 873 10 31 13 20 25 22 8 | 32 29 23 27 38 23 26
XR27 |11968 41 --- --- --- 58 --- 49 | 45 --- --- --- 53 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1938 16 36 21 30 17 27 |T 37 39 47 43 41 35 37
WRMS | 1938 12 38 13 21 16 27 |NE 33 34 37 37 38 29 33
MEDI | 1123 10 23 14 19 16 15 |MD 36 37 39 40 38 34 36
Table 3.2362.2 GPS week: 2362 Day: 2 MJD: 60780
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1313 10 23 14 10 13 13 6 | 37 52 36 42 34 33 36
R03 | 1358 11 26 11 14 8 18 6 | 42 49 43 40 43 38 41
R04 | 936 18 11 7 15 11 18 6 | 39 36 27 28 27 27 29
R05 | 2810 7 23 12 13 18 13 6 | 38 38 39 37 44 53 40
R07 | 1501 7 11 11 7 8 21 5 | 48 40 44 47 40 32 42
R08 | 844 6 11 15 11 11 16 5 | 39 34 47 41 31 30 36
R09E | 3513 13 21 18 13 11 11 6 | 34 39 35 35 36 29 33
R11E | 3665 15 13 10 9 16 11 6 | 26 29 27 25 27 26 24
R12E | 1999 9 16 15 19 19 16 7 | 94 95 98 88 83 90 90
R14E | 2522 14 21 11 18 13 13 6 | 27 34 45 31 26 20 23
R15E | 1438 7 19 13 20 18 9 6 | 35 37 52 35 43 33 33
R16E | 1086 13 23 27 22 15 14 8 | 36 36 63 46 37 35 33
R17 | 1438 6 22 16 10 13 24 6 | 39 34 42 35 35 34 36
R18 | 765 12 17 9 17 19 37 8 | 31 34 34 30 32 31 30
R19 | 1417 39 69 25 62 19 55 19 | 46 32 39 40 32 46 33
R20 | 3151 20 104 32 67 31 71 23 | 54 33 65 81 56 55 56
R21 | 917 8 29 8 15 13 20 6 | 40 34 45 51 47 40 43
R22 | 3703 14 35 17 20 13 14 8 | 12 35 19 30 20 18 15
R24 | 1152 16 36 13 13 15 22 8 | 48 35 35 35 40 30 36
XR27 | 8678 46 --- --- --- 52 --- 49 | 36 --- --- --- 50 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 2117 15 36 16 25 16 27 |T 39 39 43 41 40 36 37
WRMS | 2117 13 41 14 21 15 27 |NE 37 37 39 41 39 35 36
MEDI | 1438 12 22 13 15 13 16 |MD 38 35 42 37 37 33 36
Table 3.2362.3 GPS week: 2362 Day: 3 MJD: 60781
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1202 8 18 13 14 9 19 6 | 44 45 46 47 39 34 41
R03 | 1192 10 21 23 15 13 10 7 | 45 56 56 52 45 48 48
R04 | 914 19 19 21 11 13 11 7 | 47 29 36 41 36 32 36
R05 | 2303 17 28 11 14 15 18 7 | 48 38 50 38 43 48 43
R07 | 1331 14 28 20 18 11 21 8 | 52 39 57 43 49 40 46
R08 | 782 10 24 15 8 11 18 6 | 48 58 52 48 46 36 46
R09E | 2306 15 22 15 15 10 11 6 | 18 31 29 29 23 23 21
R11E | 2719 10 11 21 18 21 14 7 | 23 28 31 26 29 25 23
R12E | 2003 7 16 11 18 13 12 5 | 103 101 111 110 105 106 105
R14E | 2709 12 18 12 23 13 14 7 | 27 33 46 33 26 21 23
R15E | 786 9 14 15 18 14 11 6 | 52 47 65 59 46 50 49
R16E | 740 23 19 30 26 18 20 10 | 38 49 59 62 37 45 42
R17 | 1795 9 24 26 18 12 38 9 | 43 34 49 44 42 28 38
R18 | 750 16 18 8 14 20 32 8 | 29 32 30 27 34 26 27
R19 | 3134 36 50 22 49 22 52 17 | 44 38 44 47 48 52 40
R20 | 3508 32 138 23 40 26 57 18 | 82 33 90 79 80 77 79
R21 | 761 4 30 14 15 15 18 7 | 38 26 38 47 44 37 38
R22 | 3427 17 23 9 18 8 9 6 | 13 26 24 29 19 16 18
R24 | 830 13 25 13 18 13 27 8 | 50 49 46 43 47 36 44
XR27 | 8744 44 --- --- --- 44 --- 44 | 22 --- --- --- 65 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1994 17 39 18 22 15 25 |T 42 41 50 47 46 41 42
WRMS | 1994 14 49 18 20 15 25 |NE 41 38 47 45 47 39 41
MEDI | 1331 13 22 15 18 13 18 |MD 44 38 46 44 44 36 41
Table 3.2362.4 GPS week: 2362 Day: 4 MJD: 60782
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 601 7 13 11 11 16 12 5 | 44 40 43 46 45 40 42
R03 | 1020 9 16 13 13 11 8 5 | 44 45 47 52 45 51 46
R04 | 868 15 12 12 9 13 14 5 | 41 36 39 37 36 32 35
R05 | 1363 13 13 16 14 18 8 6 | 42 42 35 36 36 38 36
R07 | 1529 15 26 17 14 24 14 8 | 52 53 56 45 66 45 51
R08 | 811 13 35 32 9 12 22 9 | 47 55 68 48 49 40 49
XR09E | 3580 20 22 17 15 15 --- 9 | 43 41 49 41 39 --- 41
R11E | 2459 14 20 18 14 17 14 7 | 33 47 39 35 31 38 33
R12E | 2906 14 18 13 13 36 14 8 | 102 105 108 102 69 98 94
R14E | 2445 14 28 11 17 12 10 6 | 34 38 47 37 33 33 32
R15E | 1067 14 20 12 25 13 10 7 | 41 43 56 64 41 46 44
R16E | 1307 18 22 22 22 26 17 9 | 42 44 57 56 43 43 42
R17 | 783 9 17 12 12 7 23 6 | 36 31 33 40 29 27 32
R18 | 626 10 26 16 18 13 11 7 | 29 34 35 30 29 32 29
R19 | 2036 47 59 14 59 31 51 20 | 59 39 52 64 53 42 50
R20 | 3038 24 134 30 35 25 24 14 | 73 29 78 62 77 82 71
R21 | 908 7 23 17 11 23 28 8 | 39 39 47 43 49 34 40
R22 | 3963 20 32 10 21 13 16 8 | 19 69 26 54 25 31 30
R24 | 739 17 35 18 12 17 14 8 | 35 32 37 38 31 32 31
XR26 | 6854 44 44 --- --- 43 --- 31 | 27 27 --- --- 50 --- 38
XR27 | 6800 43 --- --- --- 53 --- 48 | 39 --- --- --- 65 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 1853 18 41 17 22 20 20 |T 43 44 50 48 44 43 43
WRMS | 1853 15 48 14 14 20 20 |NE 41 40 45 45 45 40 41
MEDI | 1363 14 22 16 14 17 14 |MD 41 40 47 45 43 38 41
Table 3.2362.5 GPS week: 2362 Day: 5 MJD: 60783
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 780 12 17 8 17 11 12 5 | 31 29 30 34 27 23 27
R03 | 1086 8 15 11 12 19 8 5 | 31 27 25 31 34 24 26
R04 | 877 21 25 11 7 16 10 7 | 28 29 24 23 26 20 22
R05 | 1881 19 19 12 11 14 17 7 | 27 19 21 28 25 19 19
R07 | 1059 16 15 13 12 25 10 7 | 39 54 44 48 56 43 45
R08 | 715 18 35 11 18 18 15 8 | 36 46 39 28 51 47 39
R09E | 1834 17 18 11 12 24 11 7 | 50 52 49 54 48 55 48
R11E | 3769 12 21 15 18 17 15 7 | 33 46 40 44 35 35 35
R12E | 1379 13 14 16 16 32 19 8 | 115 114 123 122 111 126 117
R14E | 2518 10 16 20 17 13 11 6 | 31 33 39 31 29 26 26
R15E | 1693 14 14 12 26 10 11 7 | 47 43 47 40 37 42 39
R16E | 976 23 17 18 29 14 17 9 | 50 57 53 72 50 56 53
R17 | 975 7 17 13 18 10 20 6 | 26 24 29 36 23 25 25
R18 | 684 19 16 20 11 16 25 8 | 27 33 40 37 34 30 32
R19 | 954 37 55 14 50 31 61 19 | 49 45 56 72 44 53 49
R20 | 1810 25 129 40 34 24 60 19 | 48 31 74 48 55 42 53
R21 | 723 10 24 20 10 20 18 7 | 29 30 41 34 38 34 32
R22 | 4488 18 39 24 33 20 19 11 | 14 50 23 51 27 18 21
R24 | 1205 16 22 19 12 20 24 8 | 23 21 19 26 17 18 16
XR26 | 7934 31 --- 34 --- 68 --- 32 | 36 --- 17 --- 41 --- 43
XR27 |11077 40 --- --- --- 50 --- 45 | 35 --- --- --- 47 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1851 18 38 18 22 20 25 |T 38 41 41 45 40 38 38
WRMS | 1851 17 46 14 15 19 25 |NE 31 33 34 38 36 30 32
MEDI | 1205 17 18 14 17 19 17 |MD 33 33 39 37 37 34 35
Table 3.2362.6 GPS week: 2362 Day: 6 MJD: 60784
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1360 15 8 20 31 13 10 8 | 66 60 71 73 66 66 66
R03 | 896 8 21 10 18 11 20 6 | 65 61 61 66 62 56 61
R04 | 850 11 16 7 12 11 7 4 | 62 50 49 48 51 50 51
R05 | 1747 10 20 11 15 8 10 5 | 60 50 51 58 57 47 53
R07 | 920 11 15 17 7 13 8 5 | 69 68 72 72 70 65 68
R08 | 744 13 24 13 8 18 24 7 | 63 76 73 67 71 65 68
R09E | 1686 15 10 14 12 10 10 5 | 46 48 49 45 47 48 45
R11E | 5981 13 18 13 16 15 12 6 | 27 30 28 31 31 29 27
R12E | 1217 13 22 13 14 19 14 7 | 128 126 145 138 133 139 133
R14E | 1357 8 16 15 25 11 10 6 | 28 26 56 38 32 23 26
R15E | 2451 10 15 18 15 15 11 6 | 45 40 62 45 52 44 44
R16E | 2045 22 19 12 21 10 10 7 | 41 55 63 57 46 45 46
R17 | 831 8 23 18 9 12 15 6 | 42 36 46 43 40 30 39
R18 | 1108 22 20 13 21 15 22 8 | 41 45 40 48 42 39 40
R19 | 1034 44 43 18 46 19 33 15 | 56 46 57 70 58 57 55
R20 | 1196 26 139 29 24 23 52 16 | 94 45 97 96 101 75 89
R21 | 875 8 20 13 17 14 31 8 | 47 45 54 58 51 41 48
R22 | 4414 19 30 18 28 13 8 8 | 23 25 38 30 32 32 27
R24 | 1231 10 27 20 17 17 21 8 | 45 37 48 51 52 36 44
XR26 |12915 46 56 41 --- 60 --- 29 | 52 30 21 --- 87 --- 62
XR27 | 9509 53 --- --- --- 48 --- 51 | 49 --- --- --- 99 --- 71
------+-----------------------------------------+-------------------------------------
RMS | 2129 17 38 16 21 14 20 |T 54 49 59 59 60 51 55
WRMS | 2129 14 53 14 17 14 20 |NE 55 48 55 60 62 50 56
MEDI | 1231 13 20 14 17 14 12 |MD 49 45 54 57 52 47 51
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