[IGSREPORT-30358] Wk 2355 IGLOS Final Orbits
acc
acc at igs.org
Fri Mar 14 05:44:21 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2355 (Feb 23, 2025 - Mar 01, 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 2.2355.
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:
igl2355[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2355 in the SP3 format.
igl23557.sum Combination Report for GPS Week 2355.
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 | 3.5 ns
1 | 7.1 ns
2 | 5.2 ns
3 | 3.4 ns
4 | 1.5 ns
5 | 4.4 ns
6 | 1.4 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 | GFZ | R26
1 | GFZ | R26
2 | GFZ | R26
3 | GFZ | R26
4 | GFZ | R26
5 | GFZ | R26
6 | ALL | R26
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 1.2355, 1a.2355).
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 2.2355.0-6)
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 3.2355.0-6).
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 2355 summary. (Feb 23, 2025 - Mar 01, 2025)
Table 1.2355.a GPS week : 2355 MJD: 60729.0-60735.0
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 -1 -5 -9 34 .13 18 16 | 4523 124 3418 12500
| 1 1 1 21 19 13 .05 | 2420 1843
esa n/a| -1 -1 -2 -26 3 45 -.12 25 22 | 7208 -3611 3416 11981
| 1 1 2 15 9 28 .05 | 3927 5352
gfz n/a| 0 0 1 35 14 -16 .02 19 16 | 0 -19 3497 10960
| 1 0 2 18 16 20 .06 | 0 1867
grg n/a| 1 0 3 -23 -15 -8 .29 22 18 | 3514 87 3443 7453
| 1 1 2 16 17 48 .05 | 1751 1928
iac n/a| 0 1 -2 -7 2 -33 -.22 20 18 | 3358 -650 3415 11913
| 0 1 2 21 25 56 .06 | 2010 643
jgx n/a| 0 -1 1 25 -4 -6 -.15 20 20 | 7617 184 3423 7952
| 1 1 2 12 20 26 .04 | 2091 1945
Table 1.2355.b GPS week : 2355 MJD: 60729.0-60735.0
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
------+------------------------------------+------------------------------------------
R01 | 11 11 14 15 14 14 11 |
R02 | 7 7 7 6 7 7 9 |
R03 | 7 7 6 6 6 8 7 |
R04 | 7 9 8 6 7 8 6 |
R05 | 7 7 8 8 7 7 9 |
R07 | 7 8 8 7 8 7 7 |
R08 | 7 8 8 10 8 9 6 |
R09 | 6 9 7 7 7 5 7 |
R11 | 9 8 7 7 8 7 8 |
R12 | 7 10 8 8 9 6 10 |
R14 | 7 7 6 7 6 8 5 |
R15 | 8 8 6 8 8 8 8 |
R16 | 8 8 9 11 9 7 9 |
R17 | 8 7 8 8 9 13 12 |
R18 | 6 6 7 8 11 13 14 |
R19 | 8 6 7 7 9 8 8 |
R20 | 20 18 18 21 17 19 24 |
R21 | 8 7 6 7 8 13 12 |
R22 | 8 7 7 7 7 7 7 |
R24 | 7 9 7 11 12 14 10 |
R26 | 38 40 43 44 37 36 --- |
Table 1.2355.c GPS week : 2355 MJD: 60729.0-60735.0
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 2355 0 | -104 -15 -87 -1117 -119 -131 81.7 1949 1949 | 3496 0
brd 2355 1 | 55 -19 95 1156 -643 -3661 81.1 1835 1835 | 7075 0
brd 2355 2 | 42 61 89 214 -789 -2536 79.5 1558 1558 | 5202 0
brd 2355 3 | -114 52 111 -756 -2215 158 81.6 1408 1408 | 3350 0
brd 2355 4 | 62 58 36 -1844 -1709 1275 80.3 1289 1289 | 1501 0
brd 2355 5 | -19 29 45 -1060 -2159 665 80.3 1438 1438 | 4394 0
brd 2355 6 | 46 -53 38 -735 -1157 7043 79.8 1448 1448 | 1368 0
-------------+------------------------------------------------------------+----------------
brd 2355 mean| -4 16 46 -591 -1255 401 80.6 1560 1560 | 3769 0
brd 2355 sdev| 76 45 66 984 799 3425 .9 241 241 | 2022 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 2.2355.0 GPS week: 2355 Day: 0 MJD: 60729
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 -2 18 -6 52 .09 18 16 | 645 -495 4078 11808
esa n/a| 0 -3 -2 -46 -13 23 -.14 25 23 | 1550 -60 4062 10743
gfz n/a| 0 -1 2 40 -16 -3 .15 17 14 | 0 -688 4128 10258
grg n/a| 1 0 3 -28 -12 40 .27 19 16 | 3745 -723 4071 7476
iac n/a| 0 3 -3 -21 31 -92 -.25 17 16 | 2553 -767 4058 11226
jgx n/a| 2 -1 2 14 -3 9 -.20 20 20 | 3507 -591 4055 7993
Table 2.2355.1 GPS week: 2355 Day: 1 MJD: 60730
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 -15 -37 15 .06 17 16 | 4715 1700 3845 12395
esa n/a| -3 1 -1 -30 10 72 -.17 25 21 | 5764 1667 3830 11757
gfz n/a| 2 0 1 45 21 -21 .02 17 14 | 0 1741 3918 10768
grg n/a| 2 0 1 -24 -50 66 .30 20 17 | 5792 2023 3832 7633
iac n/a| 0 0 0 -9 -4 -61 -.21 17 16 | 7024 -520 3836 11750
jgx n/a| 1 -1 0 28 31 -3 -.16 20 20 | 7968 2170 3835 8103
Table 2.2355.2 GPS week: 2355 Day: 2 MJD: 60731
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 -2 -5 -23 19 .18 18 15 | 4415 -112 3574 13172
esa n/a| -2 -1 -3 -22 -1 40 -.12 24 20 | 5438 133 3575 13573
gfz n/a| 1 0 2 50 6 12 .03 16 13 | 0 -309 3675 11249
grg n/a| 2 0 0 -35 -9 -14 .33 19 20 | 5079 -126 3706 7524
iac n/a| 0 0 1 3 40 -79 -.23 18 17 | 4538 -1277 3577 12428
jgx n/a| 0 -3 1 8 -27 -27 -.16 18 18 | 8054 69 3600 7954
Table 2.2355.3 GPS week: 2355 Day: 3 MJD: 60732
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 11 -24 34 .16 17 14 | 2735 3404 3252 13086
esa n/a| -3 -3 -4 -13 17 78 -.18 29 25 | 5586 15 3278 12780
gfz n/a| 0 0 6 5 24 5 -.00 22 18 | 0 3166 3377 11203
grg n/a| 1 0 4 -24 -23 -56 .34 19 17 | 1323 3371 3273 6612
iac n/a| 0 0 -3 16 4 -14 -.28 21 18 | 2135 716 3262 12278
jgx n/a| 1 0 0 24 8 -2 -.16 19 19 | 6819 3397 3270 7040
Table 2.2355.4 GPS week: 2355 Day: 4 MJD: 60733
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 -1 -21 5 44 .16 17 16 | 4412 -723 3077 14442
esa n/a| -1 -1 -2 -39 7 -1 -.07 25 24 | 7441 -5668 3071 13614
gfz n/a| -1 0 0 32 33 -36 .01 19 16 | 0 -980 3179 12630
grg n/a| 4 0 6 -7 -2 -67 .30 22 18 | 1725 -983 3074 8092
iac n/a| 0 0 -3 -45 -27 73 -.27 20 20 | 736 -941 3072 13634
jgx n/a| 1 0 0 28 -1 -49 -.16 20 21 | 7893 -740 3054 8567
Table 2.2355.5 GPS week: 2355 Day: 5 MJD: 60734
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 -1 15 14 35 .12 19 18 | 6817 -742 3189 15019
esa n/a| 0 0 -5 -33 4 45 -.10 23 20 | 12420 -10685 3178 13492
gfz n/a| 0 -1 2 19 16 -35 -.02 19 19 | 0 -626 3277 13077
grg n/a| 0 0 5 -46 0 -26 .22 29 20 | 4633 -747 3230 7810
iac n/a| 0 1 -5 10 -18 -6 -.10 23 20 | 2829 -909 3186 14172
jgx n/a| 0 0 4 27 -24 -7 -.09 21 21 | 10216 -719 3234 8394
Table 2.2355.6 GPS week: 2355 Day: 6 MJD: 60735
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 0 -39 4 35 .17 17 15 | 7927 -2164 2913 7578
esa n/a| 0 -2 0 -3 0 59 -.06 26 21 | 12257 -10683 2920 7912
gfz n/a| 3 0 -3 56 19 -33 -.04 23 16 | 0 -2441 2930 7537
grg n/a| 1 -3 4 2 -11 0 .23 27 19 | 2304 -2204 2916 7026
iac n/a| -2 1 -5 -7 -10 -51 -.17 21 22 | 3697 -854 2920 7907
jgx n/a| 0 0 4 48 -16 35 -.11 24 24 | 8867 -2297 2915 7614
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 3.2355.0 GPS week: 2355 Day: 0 MJD: 60729
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2148 28 51 16 13 13 14 10 | 112 58 91 96 91 94 91
R02 | 817 13 24 11 18 11 13 6 | 66 52 57 63 58 57 58
R03M | 3012 14 16 10 11 18 24 7 | 83 77 83 85 84 64 79
R04 | 951 12 21 15 13 16 14 6 | 93 94 95 88 90 84 90
R05 | 1611 10 22 12 18 20 12 7 | 78 78 83 84 74 75 78
R07M | 1044 15 16 17 13 18 15 7 | 85 72 76 85 80 66 76
R08M | 736 13 24 13 10 12 15 6 | 71 80 75 72 70 64 71
R09M | 2094 11 19 12 12 12 13 5 | 32 31 40 30 31 33 31
R11M | 1588 10 32 13 27 19 16 8 | 47 51 51 50 53 45 48
R12 | 1282 16 22 8 24 11 10 7 | 73 79 75 68 70 70 71
R14 | 709 9 26 13 16 12 15 6 | 91 95 93 84 92 82 89
R15 | 1866 26 20 12 7 11 19 7 | 77 74 70 71 73 64 70
R16 | 1769 26 17 18 10 14 14 7 | 67 65 63 55 63 59 60
R17E | 949 7 14 17 27 22 16 8 | 94 88 93 98 94 90 92
R18E | 640 11 15 12 14 15 11 6 | 48 50 47 53 52 42 47
R19E | 504 14 24 13 15 21 14 7 | 54 51 57 59 59 48 54
R20E | 1695 39 49 45 32 39 58 19 | 122 114 126 122 112 131 118
R21E | 4589 14 17 18 17 15 20 7 | 50 51 53 47 44 43 46
R22E | 3811 15 21 15 28 10 15 8 | 26 33 42 39 34 27 30
R24E | 893 17 19 10 21 13 11 7 | 123 125 125 135 128 133 127
XR26M |>>>>> 62 53 964 --- 43 --- 38 | 129 155 637 --- 138 --- 134
------+-----------------------------------------+-------------------------------------
RMS | 1949 18 25 17 19 17 20 |T 77 74 101 74 75 68 74
WRMS | 1949 16 23 14 16 16 20 |NE 82 74 78 76 76 73 75
MEDI | 1588 14 21 13 15 15 14 |MD 77 74 75 71 73 64 71
Table 3.2355.1 GPS week: 2355 Day: 1 MJD: 60730
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2485 28 34 22 22 19 17 10 | 62 41 59 46 46 52 49
R02 | 675 18 11 15 10 18 16 7 | 44 37 34 38 26 46 36
R03M | 2365 11 18 12 16 19 20 7 | 45 41 54 49 49 40 46
R04 | 1215 15 30 14 16 21 19 8 | 57 50 44 58 67 44 52
R05 | 896 12 24 16 15 15 13 7 | 49 44 46 50 53 40 46
R07M | 1423 14 31 11 21 15 19 8 | 64 56 63 61 63 54 59
R08M | 607 16 16 10 16 17 29 8 | 48 49 46 49 59 46 48
R09M | 3288 17 27 20 14 19 17 8 | 28 43 44 29 31 33 31
R11M | 969 10 26 8 22 14 18 7 | 52 57 50 51 60 55 52
R12 | 1170 25 35 12 26 14 8 9 | 68 74 60 63 61 59 62
R14 | 767 7 21 10 18 19 13 6 | 69 73 70 60 77 61 67
R15 | 1624 17 23 19 11 10 19 7 | 62 54 69 63 56 50 58
R16 | 1342 12 23 19 12 19 14 7 | 56 51 60 56 43 52 52
R17E | 645 11 15 14 21 15 12 6 | 77 74 70 77 68 76 72
R18E | 534 7 14 14 20 13 11 6 | 31 33 32 31 30 29 29
R19E | 1185 6 18 13 16 13 14 6 | 35 40 41 40 39 32 36
R20E | 1726 38 49 37 38 30 48 18 | 84 82 94 80 88 81 81
R21E | 3741 11 18 14 16 14 19 7 | 29 36 34 35 31 26 29
R22E | 3457 13 20 16 20 14 14 7 | 27 42 37 43 28 29 32
R24E | 1102 20 18 14 33 14 15 9 | 108 101 102 100 102 102 101
XR26M |>>>>> 59 63 964 --- 45 --- 39 | 139 150 328 --- 139 --- 139
------+-----------------------------------------+-------------------------------------
RMS | 1834 17 25 17 20 17 20 |T 58 58 68 53 57 50 56
WRMS | 1834 16 21 14 17 16 20 |NE 58 53 55 54 53 50 52
MEDI | 1215 14 23 14 16 15 16 |MD 56 50 54 50 56 46 52
Table 3.2355.2 GPS week: 2355 Day: 2 MJD: 60731
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1778 43 41 12 35 20 30 14 | 77 39 55 62 51 56 54
R02 | 666 17 17 11 19 18 12 7 | 52 48 50 45 40 45 45
R03M | 1465 8 15 9 12 15 14 5 | 65 70 63 70 62 59 63
R04 | 1281 11 22 11 14 26 18 8 | 74 65 71 74 84 62 71
R05 | 600 10 30 12 9 20 15 7 | 59 60 63 60 71 54 60
R07M | 1397 14 16 13 23 16 16 7 | 71 62 69 80 66 62 68
R08M | 581 20 20 18 15 17 14 7 | 63 65 59 68 55 64 61
R09M | 2407 15 17 9 13 23 17 7 | 23 35 36 35 28 31 29
R11M | 1476 13 24 11 20 16 10 7 | 48 51 51 48 39 45 45
R12 | 1218 21 20 11 17 14 17 7 | 59 56 57 53 48 49 52
R14 | 604 13 18 16 11 9 10 6 | 80 90 76 83 77 80 79
R15 | 755 10 13 10 17 8 19 6 | 66 60 64 73 59 60 63
R16 | 706 15 40 23 9 12 15 9 | 60 37 67 57 57 53 55
R17E | 615 18 15 12 27 15 14 7 | 53 53 53 54 52 46 49
R18E | 634 10 20 14 18 17 7 6 | 43 47 45 48 42 38 42
R19E | 994 10 17 16 19 11 13 6 | 37 40 38 45 35 38 36
R20E | 2031 30 45 43 31 40 47 18 | 60 71 76 54 59 60 56
R21E | 2695 15 15 8 12 11 18 6 | 40 35 34 44 36 30 34
R22E | 3387 18 24 12 11 15 14 7 | 25 47 35 38 30 24 30
R24E | 1714 14 13 15 22 15 12 7 | 144 138 143 142 141 142 142
XR26M |>>>>> 72 53 1020 --- 49 --- 42 | 167 162 554 --- 163 --- 161
------+-----------------------------------------+-------------------------------------
RMS | 1557 18 24 16 19 18 18 |T 65 63 83 61 61 54 61
WRMS | 1557 15 20 13 20 17 18 |NE 65 56 62 63 60 57 59
MEDI | 1281 15 20 12 17 16 14 |MD 60 56 59 54 55 53 55
Table 3.2355.3 GPS week: 2355 Day: 3 MJD: 60732
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 483 37 57 34 32 17 27 15 | 91 53 72 86 74 75 74
R02 | 770 12 25 13 17 8 9 6 | 51 49 54 43 42 45 45
R03M | 1226 8 9 15 7 13 17 5 | 62 64 74 68 68 64 65
R04 | 870 10 16 21 9 15 12 6 | 72 58 85 78 70 70 72
R05 | 573 11 30 20 8 18 17 7 | 59 43 69 59 64 46 55
R07M | 1238 14 16 21 15 13 14 7 | 76 64 64 78 72 63 69
R08M | 608 15 28 16 24 22 23 9 | 66 75 67 80 57 51 63
R09M | 1850 11 22 23 13 12 9 6 | 21 23 35 25 22 22 22
R11M | 1722 10 24 12 13 25 12 7 | 61 62 60 56 69 54 59
R12 | 1532 21 25 13 10 17 14 7 | 39 36 26 31 24 25 27
R14 | 674 7 29 15 14 17 13 7 | 58 64 51 56 55 52 54
R15 | 622 19 18 14 21 19 10 7 | 56 46 38 37 50 42 42
R16 | 853 6 47 26 11 29 19 10 | 67 38 79 66 85 59 66
R17E | 701 15 14 17 26 13 12 7 | 86 90 82 107 92 84 89
R18E | 720 12 30 16 19 13 11 7 | 33 36 27 40 35 29 30
R19E | 1586 16 21 19 17 9 12 7 | 33 38 44 41 34 34 35
R20E | 2166 28 52 50 34 49 57 20 | 45 55 72 57 47 54 42
R21E | 1734 18 19 14 13 14 10 6 | 34 35 34 41 33 29 32
R22E | 3050 14 26 14 16 13 15 7 | 25 30 35 40 27 30 28
R24E | 1869 21 21 26 24 34 14 10 | 125 126 127 121 112 130 122
XR26M |>>>>> 67 61 1056 --- 57 --- 44 | 180 180 580 --- 151 --- 165
------+-----------------------------------------+-------------------------------------
RMS | 1408 17 29 22 19 21 19 |T 63 60 84 60 61 52 59
WRMS | 1408 14 25 18 17 18 19 |NE 61 48 59 57 58 51 54
MEDI | 1226 14 25 17 15 17 13 |MD 59 53 64 56 57 51 55
Table 3.2355.4 GPS week: 2355 Day: 4 MJD: 60733
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 661 29 52 15 34 27 27 14 | 78 39 59 85 48 83 64
R02 | 909 14 26 13 12 11 12 6 | 43 47 47 38 34 33 38
R03M | 1182 11 17 10 13 11 18 6 | 53 50 47 55 51 42 49
R04 | 681 13 24 9 11 16 13 6 | 68 64 68 64 58 65 63
R05 | 799 10 21 22 12 15 7 6 | 54 54 71 58 48 55 55
R07M | 1036 9 19 9 17 23 19 7 | 53 47 53 48 60 43 49
R08M | 627 15 22 9 21 11 22 7 | 52 59 56 58 51 51 53
R09M | 1664 13 26 17 10 11 12 7 | 27 34 42 36 32 40 32
R11M | 855 14 24 13 13 22 11 7 | 45 40 56 58 42 51 47
R12 | 1927 22 19 18 10 18 25 8 | 53 49 46 46 44 53 46
R14 | 903 7 25 12 13 14 10 6 | 89 92 86 87 90 89 87
R15 | 645 20 17 18 21 14 11 7 | 66 65 57 58 54 53 57
R16 | 805 18 29 10 20 26 20 9 | 69 53 63 56 72 58 60
R17E | 659 18 17 14 38 15 10 9 | 63 55 60 54 49 57 53
R18E | 1061 12 17 25 28 39 19 11 | 36 34 32 47 44 32 33
R19E | 1746 17 31 18 27 11 15 9 | 36 42 35 41 34 33 34
R20E | 1987 37 28 37 27 33 51 16 | 61 61 69 62 55 54 55
R21E | 1122 13 18 19 22 14 11 7 | 30 27 42 36 33 32 30
R22E | 2696 15 17 15 15 20 13 7 | 27 35 33 41 33 28 30
R24E | 1341 12 19 35 36 12 33 12 | 124 123 136 118 120 133 124
XR26M |>>>>> 58 59 1032 --- 37 --- 36 | 238 241 431 --- 230 --- 235
------+-----------------------------------------+-------------------------------------
RMS | 1289 17 25 19 22 20 20 |T 65 62 75 57 61 54 61
WRMS | 1289 16 24 16 18 20 21 |NE 65 57 62 61 56 61 58
MEDI | 1036 14 22 15 17 15 13 |MD 53 50 56 55 49 51 53
Table 3.2355.5 GPS week: 2355 Day: 5 MJD: 60734
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 452 38 41 31 38 24 14 14 | 73 36 44 75 38 63 53
R02 | 936 18 17 12 8 12 13 6 | 43 41 31 37 34 37 36
R03M | 1312 10 29 12 8 19 16 7 | 51 57 48 52 59 47 50
R04 | 755 15 30 13 15 17 15 8 | 69 53 66 57 64 57 61
R05 | 1091 10 23 11 17 13 10 6 | 50 52 54 39 40 52 47
R07M | 1103 12 16 11 14 15 24 7 | 57 54 58 56 50 44 52
R08M | 838 12 16 18 23 12 27 8 | 54 53 68 67 53 49 56
R09M | 1339 11 14 11 12 12 10 5 | 22 24 26 22 28 22 22
R11M | 1048 12 18 18 21 15 7 7 | 129 135 130 129 118 128 128
R12 | 1862 17 17 12 10 13 13 6 | 52 56 52 47 56 38 48
R14 | 945 14 22 14 13 19 17 7 | 106 113 112 113 101 107 108
R15 | 1228 22 11 14 12 8 26 8 | 67 70 65 69 73 62 66
R16 | 880 16 18 12 17 20 12 7 | 57 53 52 52 58 49 52
R17E | 512 13 15 21 60 33 22 13 | 136 140 137 162 130 135 137
R18E | 858 18 24 19 40 46 16 12 | 52 49 58 62 54 41 47
R19E | 1007 16 27 14 26 12 10 8 | 46 51 50 43 47 42 45
R20E | 3805 40 38 51 37 33 49 19 | 96 96 92 102 92 89 90
R21E | 1131 23 23 18 38 44 23 12 | 58 50 55 67 59 54 52
R22E | 2121 16 9 15 19 17 12 6 | 20 30 31 31 29 26 24
R24E | 1742 16 18 20 62 33 31 14 | 108 99 103 118 103 104 102
XR26M |>>>>> 53 52 958 --- 44 --- 35 | 198 210 624 --- 191 --- 199
------+-----------------------------------------+-------------------------------------
RMS | 1437 19 23 19 29 23 21 |T 73 72 93 70 70 62 70
WRMS | 1437 18 20 19 20 20 21 |NE 64 59 59 61 58 58 58
MEDI | 1091 16 18 14 17 17 15 |MD 57 53 58 57 58 49 52
Table 3.2355.6 GPS week: 2355 Day: 6 MJD: 60735
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 816 25 40 25 26 11 17 11 | 95 53 86 90 78 73 79
R02 | 1358 18 26 18 22 15 14 8 | 53 37 43 53 45 38 43
R03M | 1338 7 13 10 19 16 20 6 | 64 68 67 77 71 56 66
R04 | 619 9 20 10 12 12 15 6 | 79 76 76 77 69 74 74
R05 | 933 13 40 15 19 9 13 8 | 63 56 61 66 55 53 57
R07M | 894 12 7 13 18 18 21 7 | 91 85 87 95 88 78 86
R08M | 889 8 15 11 13 9 19 5 | 80 77 75 78 75 67 75
R09M | 2280 13 11 18 16 15 11 6 | 27 25 30 26 27 26 24
R11M | 1229 16 30 14 13 12 9 7 | 433 427 436 427 434 434 432
R12 | 1260 17 21 29 25 10 21 9 | 69 68 78 54 68 52 64
R14 | 1156 8 16 10 13 15 6 5 | 121 125 121 121 119 119 120
R15 | 1766 19 20 14 16 16 23 8 | 90 95 93 87 90 76 87
R16 | 1061 15 30 12 20 15 23 8 | 79 57 77 78 78 58 70
R17E | 768 17 18 21 50 22 29 12 | 111 122 122 127 106 111 113
R18E | 620 10 22 22 65 31 28 14 | 59 64 55 97 73 58 62
R19E | 624 14 27 13 22 14 15 8 | 54 54 52 52 47 53 50
R20E | 3803 39 49 74 37 44 68 24 | 125 135 140 133 129 131 125
R21E | 899 20 27 15 23 45 20 12 | 72 72 65 70 60 65 65
R22E | 1466 13 15 14 24 18 11 7 | 19 29 34 35 28 27 25
R24E | 1458 17 23 16 29 26 28 10 | 137 137 138 136 139 141 136
------+-----------------------------------------+-------------------------------------
RMS | 1448 17 26 23 27 21 24 |T 95 94 96 98 94 89 92
WRMS | 1448 15 21 16 18 22 24 |NE 81 70 79 78 75 67 74
MEDI | 1061 14 21 14 20 15 19 |MD 79 72 76 78 75 65 74
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