[IGSREPORT-30174] Wk 2338 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 15 03:03:23 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2338 (Oct 27, 2024 - Nov 02, 2024)
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 2.2338.
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:
igl2338[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2338 in the SP3 format.
igl23387.sum Combination Report for GPS Week 2338.
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.
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 | 5.9 ns
1 | 7.2 ns
2 | 7.7 ns
3 | 5.6 ns
4 | 6.8 ns
5 | 5.3 ns
6 | 5.6 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2338, 1a.2338).
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 2.2338.0-6)
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 3.2338.0-6).
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 2338 summary. (Oct 27, 2024 - Nov 02, 2024)
Table 1.2338.a GPS week : 2338 MJD: 60610.0-60616.0
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 8 -11 36 .14 21 18 | 115 -587 4071 16147
| 1 0 2 10 23 39 .02 | 1260 1924
esa n/a| 0 0 -1 -40 19 18 -.06 25 20 | 12482 -828 3438 8413
| 0 0 1 11 17 22 .05 | 6328 1612
gfz n/a| 0 0 3 23 1 -9 .04 17 14 | 0 -740 3409 7799
| 1 0 1 13 16 28 .06 | 0 1747
grg n/a| 0 0 2 -3 -10 -8 .24 26 19 | 3544 -632 4053 15799
| 0 1 2 11 12 46 .03 | 965 1997
iac n/a| 1 0 -7 -1 5 -25 -.12 17 15 | 6990 -451 4058 15607
| 0 1 3 25 16 81 .06 | 1282 1071
jgx n/a| 0 0 4 0 -13 31 -.21 26 23 | 4404 -826 3416 7951
| 1 0 1 22 15 34 .06 | 1216 1748
Table 1.2338.b GPS week : 2338 MJD: 60610.0-60616.0
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 | 15 14 15 13 14 11 15 |
R02 | 11 7 8 7 6 6 7 |
R03 | 6 6 7 7 6 5 5 |
R04 | 5 6 8 7 8 6 7 |
R05 | 6 7 6 9 9 7 9 |
R07 | 7 4 8 7 6 5 7 |
R08 | 8 7 8 7 6 8 7 |
R09 | 5 5 7 7 8 6 5 |
R11 | 6 5 6 6 7 8 7 |
R12 | 7 8 7 6 8 7 8 |
R14 | 7 7 7 6 6 8 9 |
R15 | 8 8 8 7 8 9 7 |
R16 | 10 10 9 9 11 9 9 |
R17 | 6 6 6 5 5 7 7 |
R18 | 9 8 7 7 6 7 8 |
R19 | 23 26 22 22 21 22 24 |
R20 | 16 18 21 22 19 17 15 |
R21 | 7 6 6 8 8 8 8 |
R22 | 6 7 5 6 7 5 5 |
R24 | 8 6 7 7 7 8 7 |
R25 | 9 10 13 13 48 --- --- |
R26 | 27 23 31 32 34 33 29 |
Table 1.2338.c GPS week : 2338 MJD: 60610.0-60616.0
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 2338 0 | -107 44 80 -841 -222 -193 82.2 2648 2648 | 5869 0
brd 2338 1 | 50 -14 19 -2273 -902 -5407 81.9 2374 2374 | 7163 0
brd 2338 2 | 12 -16 -80 -513 -842 -10440 81.2 1828 1828 | 7713 0
brd 2338 3 | 62 75 -108 -1970 1472 -9205 82.6 1611 1611 | 5593 0
brd 2338 4 | 3 50 -101 -2931 532 -3745 82.0 1612 1612 | 6781 0
brd 2338 5 | -80 0 -67 -1683 664 -2430 81.3 2152 2152 | 5330 0
brd 2338 6 | 25 61 -40 -1064 858 1147 82.4 1823 1823 | 5646 0
-------------+------------------------------------------------------------+----------------
brd 2338 mean| -4 28 -42 -1610 222 -4324 82.0 2006 2006 | 6299 0
brd 2338 sdev| 64 38 69 857 899 4345 .5 396 396 | 915 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 2.2338.0 GPS week: 2338 Day: 0 MJD: 60610
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 4 25 -9 -34 .14 25 20 | 1476 -1161 3535 14041
esa n/a| -1 -1 -1 -56 0 -8 -.09 21 18 | 15595 -723 2978 8815
gfz n/a| 1 0 2 9 3 -49 .14 18 14 | 0 -1640 2944 7610
grg n/a| 0 -1 7 -24 -24 76 .23 23 19 | 4094 -1568 3581 14003
iac n/a| 2 1 -12 43 16 45 -.08 17 16 | 7809 60 3614 14523
jgx n/a| -3 0 5 1 -32 -13 -.21 23 21 | 5236 -1192 2880 7815
Table 2.2338.1 GPS week: 2338 Day: 1 MJD: 60611
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 0 1 1 49 .16 23 18 | 929 96 3844 14631
esa n/a| 0 0 1 -27 19 41 -.03 23 18 | 6003 281 3395 10424
gfz n/a| 0 0 5 42 28 -9 -.03 18 14 | 0 523 3118 7836
grg n/a| 0 -1 4 -6 -7 9 .23 30 19 | 4468 249 3611 14221
iac n/a| 1 -1 -9 -13 -24 -99 -.07 15 14 | 8818 -17 3817 14140
jgx n/a| 0 0 3 -5 -5 70 -.20 28 23 | 4081 496 3083 7884
Table 2.2338.2 GPS week: 2338 Day: 2 MJD: 60612
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 0 10 8 66 .13 23 21 | 590 1320 3741 15310
esa n/a| -2 -1 0 -40 26 18 .00 25 18 | 9357 -766 3144 7230
gfz n/a| 0 -1 2 13 4 -22 -.02 15 13 | 0 998 3138 7712
grg n/a| 1 0 1 -7 -22 -9 .28 28 17 | 4352 1384 3683 13721
iac n/a| 1 0 -8 3 19 -50 -.18 18 16 | 8175 -170 3711 14447
jgx n/a| 1 1 7 -11 -24 58 -.13 27 24 | 5551 989 3151 7806
Table 2.2338.3 GPS week: 2338 Day: 3 MJD: 60613
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 2 15 13 -4 .11 19 17 | -781 -1227 3928 17662
esa n/a| 0 0 -2 -36 3 35 -.06 26 20 | 8510 -1710 3165 7771
gfz n/a| 2 0 4 43 -10 -16 .06 17 13 | 0 -1983 3224 8465
grg n/a| 0 -1 0 9 8 -77 .22 27 20 | 3024 -1691 4037 17551
iac n/a| 0 -1 -6 -9 -4 72 -.11 19 17 | 5439 -1441 3892 16621
jgx n/a| -1 0 1 -38 -8 1 -.27 25 21 | 4846 -2131 3191 8419
Table 2.2338.4 GPS week: 2338 Day: 4 MJD: 60614
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 -2 -9 49 .15 18 17 | 485 900 4171 17400
esa n/a| -1 0 -4 -35 15 -9 -.16 28 21 | 25141 691 3359 9690
gfz n/a| 0 0 3 20 -12 -21 -.00 18 13 | 0 237 3374 6952
grg n/a| 0 2 2 8 0 -23 .21 26 18 | 2900 1063 4173 17405
iac n/a| 1 -2 -6 -38 25 57 -.06 18 16 | 6235 1221 4119 16449
jgx n/a| 1 0 4 33 -20 0 -.31 25 25 | 4673 225 3480 7215
Table 2.2338.5 GPS week: 2338 Day: 5 MJD: 60615
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 0 -52 63 .15 20 16 | 397 -4372 4949 18072
esa n/a| 0 -1 -3 -58 16 43 -.06 24 22 | 11851 -3959 4181 6838
gfz n/a| 0 0 5 17 16 30 .08 15 14 | 0 -3745 4190 7783
grg n/a| 0 0 2 2 -5 -23 .23 29 19 | 4100 -4263 4967 18046
iac n/a| 2 0 -4 10 8 -121 -.11 16 15 | 6621 -2022 4907 17225
jgx n/a| -2 0 4 3 -19 43 -.22 23 22 | 4583 -3981 4257 8183
Table 2.2338.6 GPS week: 2338 Day: 6 MJD: 60616
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 1 12 -31 66 .13 21 19 | -2288 331 4330 15919
esa n/a| 0 0 0 -30 53 7 -.06 25 21 | 10923 384 3848 8124
gfz n/a| -1 -1 3 20 -16 26 .08 21 19 | 0 430 3875 8239
grg n/a| 0 -1 0 -6 -22 -14 .26 23 18 | 1875 396 4319 15650
iac n/a| 1 0 -3 -4 -1 -80 -.23 15 14 | 5833 -789 4348 15846
jgx n/a| -1 0 3 15 15 59 -.16 28 28 | 1860 -190 3875 8339
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 3.2338.0 GPS week: 2338 Day: 0 MJD: 60610
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1714 43 36 14 27 22 52 15 | 82 50 65 56 74 38 60
XR02M | 1862 19 21 15 24 23 --- 10 | 142 163 155 140 133 --- 146
R03M | 503 13 8 10 13 12 15 5 | 52 59 65 61 69 52 60
R04M | 1266 8 14 9 12 14 10 5 | 46 46 48 41 56 38 45
R05M | 4338 13 7 8 12 16 15 5 | 42 46 43 36 53 22 42
R07M | 2407 8 13 15 16 10 19 6 | 78 82 85 68 80 71 77
R08M | 912 20 16 12 12 24 15 7 | 62 73 64 64 82 61 67
R09E | 2874 17 10 12 13 10 6 5 | 22 26 31 25 27 25 24
R11E | 4424 14 10 17 12 11 13 6 | 35 42 49 38 42 37 40
R12E | 983 10 12 12 17 21 11 6 | 87 85 88 91 95 84 88
R14E | 2105 14 11 8 20 13 18 6 | 78 80 82 79 78 83 79
R15E | 1853 16 12 17 26 13 18 7 | 125 121 123 122 122 118 121
R16E | 2573 23 18 20 27 23 22 10 | 55 62 61 71 48 62 57
R17M | 842 13 15 8 13 7 17 5 | 48 49 48 50 48 41 46
R18M | 952 13 24 8 22 20 21 8 | 37 51 39 44 42 34 39
R19M | 2169 66 59 36 54 27 57 22 | 79 72 82 72 76 55 68
R20M | 6646 52 26 46 38 27 19 16 | 81 44 80 78 63 57 64
R21 | 1206 8 23 12 17 10 10 6 | 54 47 52 55 51 50 50
R22 | 2734 17 12 10 17 11 15 6 | 37 39 39 40 38 37 37
R24 | 488 18 15 20 17 16 16 7 | 57 68 68 58 67 52 61
XR25 | 9745 15 11 --- --- 12 --- 9 | 31 28 --- --- 38 --- 32
XR26M |27399 25 --- --- 39 43 --- 26 | 53 --- --- 51 74 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 2647 25 21 18 23 17 23 |T 62 63 68 63 66 53 61
WRMS | 2647 20 18 14 19 16 21 |NE 44 45 53 51 48 46 45
MEDI | 1862 15 14 12 17 14 16 |MD 54 51 64 58 63 52 58
Table 3.2338.1 GPS week: 2338 Day: 1 MJD: 60611
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 2147 39 24 18 24 18 52 13 | 51 36 53 38 49 31 42
XR02M | 1193 14 13 12 12 14 --- 6 | 99 100 101 93 97 --- 97
R03M | 686 16 14 10 8 12 15 5 | 34 37 40 37 45 35 37
R04M | 1843 10 11 10 10 16 16 5 | 27 25 27 25 34 21 25
R05M | 3670 13 25 14 9 11 9 6 | 21 42 22 29 27 21 25
R07M | 1753 8 6 9 9 8 11 3 | 56 60 59 54 63 57 58
R08M | 970 20 16 15 10 13 10 6 | 40 46 36 35 49 40 41
R09E | 2169 12 8 11 11 11 12 5 | 17 24 31 19 25 18 21
R11E | 5813 13 7 9 13 11 9 4 | 29 33 34 35 37 31 32
R12E | 768 11 18 17 13 22 11 7 | 124 121 131 124 125 117 123
R14E | 2079 9 12 22 24 10 15 7 | 56 57 59 63 57 58 56
R15E | 1467 17 18 16 20 17 23 8 | 112 110 113 116 120 123 115
R16E | 2076 18 18 25 30 24 21 10 | 62 62 54 75 65 62 60
R17M | 495 7 9 11 25 9 14 6 | 29 31 32 44 30 25 28
R18M | 1619 12 32 16 17 11 14 8 | 23 35 20 30 25 21 22
R19M | 1354 62 59 35 91 23 81 26 | 38 56 57 42 35 38 38
R20M | 4269 45 45 28 60 26 43 18 | 32 58 46 43 27 50 32
R21 | 1462 13 10 10 10 12 19 5 | 35 34 29 35 33 26 30
R22 | 2421 13 13 17 24 10 11 6 | 42 39 48 41 44 45 42
R24 | 504 12 9 20 11 9 20 6 | 40 42 44 47 51 38 42
XR25 |10713 17 9 --- --- 14 --- 9 | 44 33 --- --- 49 --- 44
XR26M |28594 31 --- --- 29 34 --- 22 | 56 --- --- 46 51 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 2373 23 23 18 30 15 28 |T 48 51 51 51 51 45 48
WRMS | 2373 18 18 14 19 14 23 |NE 40 37 40 41 44 36 39
MEDI | 1753 13 13 15 13 12 15 |MD 40 42 44 42 45 38 41
Table 3.2338.2 GPS week: 2338 Day: 2 MJD: 60612
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1890 54 12 19 39 11 57 15 | 62 42 45 34 41 49 41
R02M | 1084 11 19 12 24 13 23 7 | 42 40 42 42 42 29 38
R03M | 696 8 17 16 9 16 21 6 | 44 46 56 46 53 36 47
R04M | 1128 11 22 14 11 23 13 7 | 42 31 40 43 50 31 38
R05M | 2645 15 17 8 9 13 12 5 | 32 38 32 30 37 26 32
R07M | 1304 8 21 15 16 17 28 8 | 59 58 59 57 64 48 56
R08M | 727 14 20 12 26 15 22 8 | 53 65 59 63 57 53 57
R09E | 2277 17 10 18 13 16 14 7 | 28 30 42 29 31 31 30
R11E | 5407 13 10 13 12 16 11 5 | 36 35 37 29 37 31 33
R12E | 472 10 11 12 19 19 19 7 | 116 118 122 123 111 112 116
R14E | 1858 14 18 13 21 17 12 7 | 39 47 37 53 38 39 39
R15E | 720 17 13 15 26 14 15 7 | 72 67 61 62 66 53 62
R16E | 930 24 20 16 21 22 23 9 | 67 64 66 73 62 63 63
R17M | 503 10 13 12 12 12 16 5 | 40 40 43 41 43 38 40
R18M | 1450 13 24 8 12 10 21 6 | 37 47 35 38 35 35 37
R19M | 1049 48 65 16 73 29 57 21 | 46 51 49 47 48 34 43
R20M | 1315 46 56 36 62 35 48 20 | 62 51 57 59 50 42 49
R21 | 1196 16 15 9 14 8 15 5 | 44 40 38 42 36 35 37
R22 | 2104 11 8 13 10 7 17 5 | 30 29 34 33 29 32 29
R24 | 734 15 13 10 14 18 27 7 | 42 46 38 47 47 38 41
XR25 |11558 18 15 --- --- 19 --- 12 | 31 30 --- --- 44 --- 33
XR26M |27926 33 --- --- 41 53 --- 31 | 75 --- --- 66 81 --- 72
------+-----------------------------------------+-------------------------------------
RMS | 1827 23 25 15 28 18 27 |T 49 48 49 50 50 42 46
WRMS | 1827 21 18 13 17 16 24 |NE 36 36 36 40 39 35 35
MEDI | 1196 14 17 13 16 16 19 |MD 42 46 42 46 44 36 40
Table 3.2338.3 GPS week: 2338 Day: 3 MJD: 60613
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 806 32 25 18 27 19 45 12 | 59 50 55 50 42 51 49
R02M | 791 6 24 14 21 14 16 7 | 38 46 40 36 40 30 37
R03M | 604 12 11 14 9 20 25 7 | 50 51 53 51 63 37 50
R04M | 1036 10 15 15 13 14 27 7 | 44 38 48 36 46 27 40
R05M | 2404 23 19 10 10 32 13 9 | 28 38 29 30 53 24 32
R07M | 1251 11 16 12 15 17 25 7 | 48 49 45 51 53 35 46
R08M | 941 18 13 13 19 17 13 7 | 46 57 54 62 49 54 51
R09E | 1974 17 16 14 14 14 23 7 | 21 26 37 28 28 31 27
R11E | 4553 14 12 13 15 11 17 6 | 42 41 47 34 42 42 40
R12E | 512 16 10 12 16 14 13 6 | 62 49 54 56 59 47 53
R14E | 963 15 16 11 14 11 12 6 | 61 53 55 53 50 57 53
R15E | 814 14 11 15 19 14 21 7 | 81 73 75 78 81 80 77
R16E | 1488 18 18 17 28 15 20 8 | 86 90 89 98 82 98 88
R17M | 502 9 14 9 7 10 21 5 | 44 41 42 44 41 33 40
R18M | 1338 10 23 12 17 10 23 7 | 41 49 42 36 36 34 38
R19M | 1218 29 65 22 68 46 58 21 | 60 48 70 65 79 53 60
R20M | 689 47 64 47 69 19 31 21 | 72 55 62 81 66 73 62
R21 | 1002 11 18 11 26 16 28 8 | 45 39 48 53 42 33 42
R22 | 2610 13 13 11 16 10 8 5 | 18 24 25 30 23 22 21
R24 | 658 10 13 15 17 22 11 7 | 38 38 37 47 43 35 37
XR25 |16529 18 21 --- --- 17 --- 13 | 34 32 --- --- 54 --- 40
XR26M |25346 26 --- --- 47 58 --- 32 | 43 --- --- 37 68 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1611 19 26 17 27 19 25 |T 48 47 50 50 51 44 46
WRMS | 1611 17 20 13 20 17 21 |NE 33 33 36 43 40 30 35
MEDI | 1002 14 16 13 17 15 21 |MD 44 48 48 50 49 35 42
Table 3.2338.4 GPS week: 2338 Day: 4 MJD: 60614
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 755 40 34 15 33 12 43 13 | 54 26 39 46 40 30 37
R02M | 2873 12 7 8 16 15 13 5 | 43 45 46 41 52 37 44
R03M | 1256 9 14 8 8 14 23 6 | 49 51 46 42 51 33 44
R04M | 660 10 9 6 13 23 33 7 | 51 51 46 38 57 31 45
XR05M | 767 19 18 15 12 18 --- 8 | 44 35 46 36 51 --- 41
R07M | 1038 8 13 12 12 12 18 5 | 45 46 40 41 48 38 42
R08M | 1168 19 20 10 12 11 9 6 | 37 54 43 44 39 37 41
R09E | 2204 14 14 17 11 19 21 7 | 25 31 34 23 31 33 27
XR11E | 3979 15 9 15 10 13 --- 6 | 37 40 44 37 41 --- 38
R12E | 540 16 20 16 19 23 13 8 | 83 79 86 69 69 72 76
R14E | 1195 13 14 10 18 8 11 5 | 39 36 32 42 32 34 34
R15E | 1256 10 17 21 20 18 18 8 | 60 57 66 65 50 65 58
R16E | 1213 20 26 36 13 24 17 11 | 112 125 134 124 109 129 121
R17M | 801 13 10 9 7 13 10 4 | 42 39 37 44 38 38 38
R18M | 809 8 17 8 8 15 20 5 | 36 40 38 39 38 30 36
R19M | 2532 22 63 16 78 29 62 20 | 51 39 56 61 60 57 53
R20M | 2500 37 71 46 35 24 19 18 | 71 47 73 63 58 64 61
R21 | 1166 12 18 7 23 13 29 7 | 39 40 41 52 46 29 41
R22 | 2840 13 19 10 20 13 15 6 | 24 30 32 34 30 26 27
R24 | 691 14 14 14 19 15 10 6 | 38 41 39 40 40 37 36
XR25 |16016 46 --- --- --- 49 --- 48 | 30 --- --- --- 65 --- 40
XR26M |28238 30 --- --- 44 61 --- 33 | 77 --- --- 67 101 --- 81
------+-----------------------------------------+-------------------------------------
RMS | 1612 18 28 18 26 18 25 |T 49 47 50 49 52 45 48
WRMS | 1612 17 21 13 18 16 25 |NE 32 37 37 42 45 30 36
MEDI | 1195 14 17 12 16 15 18 |MD 43 40 43 42 48 37 41
Table 3.2338.5 GPS week: 2338 Day: 5 MJD: 60615
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 634 35 19 10 16 17 40 10 | 58 45 38 54 44 35 44
R02M | 4251 10 12 15 14 13 15 6 | 62 68 62 65 60 34 61
R03M | 951 10 10 14 9 9 11 5 | 44 39 45 40 40 39 40
R04M | 660 13 9 11 16 17 12 6 | 43 39 30 30 43 35 35
XR05M | 871 10 9 19 7 13 --- 6 | 32 34 25 34 33 --- 29
R07M | 937 6 14 8 10 13 15 5 | 95 95 102 99 94 94 96
R08M | 1332 17 14 16 17 12 25 7 | 46 51 49 51 36 53 46
R09E | 1072 14 11 10 10 18 10 5 | 25 28 33 24 36 28 28
R11E | 4849 19 14 12 20 16 22 7 | 40 48 47 52 41 50 44
R12E | 1029 14 19 13 16 19 12 7 | 74 72 82 78 88 69 77
R14E | 1343 11 15 21 22 13 14 7 | 80 74 79 70 70 79 74
R15E | 830 19 13 12 35 17 26 9 | 96 93 100 110 95 96 96
R16E | 951 26 15 21 20 17 19 9 | 79 78 73 74 66 71 71
R17M | 1377 11 16 10 24 12 17 6 | 32 39 34 34 28 24 29
R18M | 490 13 16 11 12 16 25 7 | 27 24 25 30 26 18 23
R19M | 2546 39 66 21 86 23 48 21 | 56 47 47 65 40 47 45
R20M | 3987 31 57 25 55 17 29 16 | 56 49 73 78 58 48 57
R21 | 641 11 21 15 11 14 26 7 | 30 30 35 32 35 31 30
R22 | 3124 16 9 10 10 13 9 5 | 24 36 37 28 26 31 29
R24 | 1294 18 18 10 12 18 21 7 | 34 36 29 31 29 24 28
XR26M |10529 38 --- --- 41 54 --- 32 | 54 --- --- 56 89 --- 68
------+-----------------------------------------+-------------------------------------
RMS | 2151 20 24 15 28 16 23 |T 51 51 52 54 51 47 50
WRMS | 2151 16 22 14 19 15 22 |NE 29 34 33 30 30 28 29
MEDI | 1072 14 14 12 16 16 19 |MD 46 45 45 52 41 39 44
Table 3.2338.6 GPS week: 2338 Day: 6 MJD: 60616
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 978 34 30 27 36 23 54 15 | 76 57 59 55 60 51 58
R02M | 4319 10 20 19 18 13 15 7 | 54 65 68 51 57 27 57
R03M | 698 9 9 10 11 10 17 5 | 55 54 58 57 58 44 54
R04M | 550 14 13 12 11 12 24 6 | 51 47 48 41 57 34 46
XR05M | 757 24 18 16 15 10 --- 8 | 54 46 42 40 50 --- 43
R07M | 903 15 13 22 13 12 22 7 | 180 181 180 174 176 174 177
R08M | 1437 16 16 14 17 16 15 7 | 74 84 77 89 75 79 78
R09E | 1329 12 7 12 13 11 13 5 | 24 27 33 30 23 32 26
R11E | 3090 15 11 16 9 18 21 7 | 52 50 52 48 52 41 49
R12E | 813 13 19 19 21 12 23 8 | 109 111 109 118 110 113 111
R14E | 1244 14 17 29 24 14 19 9 | 94 97 89 98 87 93 91
R15E | 1220 15 14 17 19 12 19 7 | 130 135 135 129 129 125 130
R16E | 895 23 12 16 18 20 24 8 | 67 70 78 74 60 68 68
R17M | 2004 12 19 14 12 12 17 6 | 55 59 53 51 55 47 52
R18M | 524 14 24 11 24 14 23 8 | 49 59 50 47 46 38 47
R19M | 1805 51 70 43 55 27 74 23 | 85 50 83 85 85 64 74
R20M | 2794 32 54 35 33 13 26 15 | 88 56 80 92 78 77 77
R21 | 785 11 13 23 19 13 21 7 | 54 49 57 64 56 45 54
R22 | 2099 15 13 7 7 10 14 5 | 30 34 31 38 28 30 30
R24 | 1907 19 11 18 14 14 17 7 | 54 52 52 55 54 44 51
XR26M |13700 26 --- --- 47 46 --- 29 | 72 --- --- 66 109 --- 82
------+-----------------------------------------+-------------------------------------
RMS | 1822 21 25 21 23 15 28 |T 71 69 71 71 71 64 69
WRMS | 1822 18 21 19 18 14 28 |NE 46 45 46 52 46 39 45
MEDI | 1244 15 14 16 18 13 21 |MD 55 56 58 57 58 47 57
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