[IGSREPORT-30266] Wk 2346 IGLOS Final Orbits
acc
acc at igs.org
Mon Jan 13 01:39:50 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2346 (Dec 22, 2024 - Dec 28, 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 2.2346.
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:
igl2346[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2346 in the SP3 format.
igl23467.sum Combination Report for GPS Week 2346.
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 | -1.4 ns
1 | 0.2 ns
2 | -0.5 ns
3 | -1.9 ns
4 | -0.2 ns
5 | 7.4 ns
6 | -0.2 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
----+--------+---------------
3 | ALL | R22
4 | ALL | R22
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 1.2346, 1a.2346).
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 2.2346.0-6)
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 3.2346.0-6).
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 2346 summary. (Dec 22, 2024 - Dec 28, 2024)
Table 1.2346.a GPS week : 2346 MJD: 60666.0-60672.0
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 0 0 3 -3 49 .15 18 15 | 6901 -838 3436 9485
| 1 1 1 9 16 27 .03 | 1939 2063
esa n/a| 0 0 0 -11 24 -22 -.14 38 30 | 1941 -1881 3374 7538
| 1 1 1 13 15 21 .03 | 4576 1910
gfz n/a| 0 -1 3 15 10 2 .02 23 15 | 0 -789 3390 7818
| 1 1 2 9 20 31 .04 | 0 2009
grg n/a| 0 0 3 0 -41 -25 .34 26 20 | -97 -356 2868 7824
| 1 1 3 26 35 40 .04 | 3080 2053
iac n/a| 0 0 -2 -4 10 -27 -.13 17 15 | 1005 -202 3430 9257
| 0 2 1 14 26 71 .06 | 2489 1284
jgx n/a| 0 0 -3 -12 2 -13 -.21 23 23 | 9745 -1185 3396 7886
| 0 0 1 15 17 38 .04 | 1914 2260
Table 1.2346.b GPS week : 2346 MJD: 60666.0-60672.0
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 | 13 12 15 16 15 15 14 |
R02 | 7 6 7 7 7 5 7 |
R03 | 6 6 8 8 6 7 7 |
R04 | 9 9 7 6 6 5 7 |
R05 | 6 6 7 6 6 6 7 |
R07 | 6 8 7 7 6 7 6 |
R08 | 8 7 9 8 7 8 5 |
R09 | 6 6 6 8 6 6 7 |
R11 | 8 9 9 7 12 10 10 |
R12 | 7 7 6 7 7 6 8 |
R14 | 5 6 6 4 6 8 6 |
R15 | 7 8 7 8 6 7 8 |
R16 | 8 7 9 9 10 9 8 |
R17 | 8 6 8 9 7 8 9 |
R18 | 7 7 7 7 8 6 8 |
R19 | 17 18 16 19 21 19 20 |
R20 | 25 26 24 25 26 25 25 |
R21 | 7 7 9 8 7 7 10 |
R22 | 5 6 12 --- --- 7 7 |
R24 | 10 9 11 9 8 9 8 |
R26 | 33 32 30 30 32 38 38 |
Table 1.2346.c GPS week : 2346 MJD: 60666.0-60672.0
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 2346 0 | 8 38 -58 -996 2252 -5816 79.5 1977 1977 | -1390 0
brd 2346 1 | 22 -39 -45 -794 1650 -11050 80.1 1654 1654 | 186 0
brd 2346 2 | 33 -26 103 -1043 1435 5384 82.2 1531 1531 | -522 0
brd 2346 3 | 19 -20 12 -114 4030 3334 83.8 1551 1551 | -1911 0
brd 2346 4 | -9 -21 49 -233 4141 2065 79.4 1546 1546 | -239 0
brd 2346 5 | -13 17 34 448 4067 -513 80.4 1809 1809 | 7372 0
brd 2346 6 | -47 -18 31 1294 105 -4630 81.4 2027 2027 | -209 0
-------------+------------------------------------------------------------+----------------
brd 2346 mean| 1 -10 18 -205 2525 -1603 81.0 1727 1727 | 469 0
brd 2346 sdev| 27 27 55 852 1588 5830 1.6 210 210 | 3130 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 2.2346.0 GPS week: 2346 Day: 0 MJD: 60666
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 12 -6 57 .12 18 14 | 5320 1100 3558 10196
esa n/a| 0 0 0 -16 12 5 -.13 34 23 | 1039 -165 3568 7111
gfz n/a| 0 0 3 17 -1 40 -.01 19 15 | 0 1277 3564 7459
grg n/a| 2 0 2 -46 -60 8 .38 24 17 | -3748 1195 3542 9919
iac n/a| 0 0 -1 8 23 -102 -.10 17 13 | -1356 29 3546 9718
jgx n/a| 0 0 0 -8 18 44 -.20 23 23 | 8114 709 3478 7481
Table 2.2346.1 GPS week: 2346 Day: 1 MJD: 60667
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 0 -15 2 64 .18 18 15 | 8504 129 3538 10091
esa n/a| 0 0 -1 16 26 -17 -.19 36 24 | -576 -1032 3328 7347
gfz n/a| 0 -2 0 6 32 -16 .05 23 14 | 0 53 3301 7977
grg n/a| -2 0 2 -13 6 -41 .35 27 20 | -1350 460 3534 9565
iac n/a| 0 0 -1 3 -38 18 -.14 16 14 | 560 1137 3523 9796
jgx n/a| 0 0 -4 -16 16 -33 -.18 19 19 | 10764 278 3181 8105
Table 2.2346.2 GPS week: 2346 Day: 2 MJD: 60668
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 -1 4 -11 45 .18 17 15 | 6903 -2384 3985 9425
esa n/a| 0 0 -2 -23 16 -4 -.12 39 25 | -3073 -3072 4039 7335
gfz n/a| 0 -1 5 7 10 -1 .05 21 16 | 0 -2333 3984 7786
grg n/a| -1 1 2 -7 -51 -3 .32 28 20 | --- --- --- ---
iac n/a| 0 -2 -1 -7 4 -85 -.21 19 19 | 266 -2013 3996 9187
jgx n/a| 0 0 -1 5 14 23 -.16 20 20 | 9274 -1785 3938 8096
Table 2.2346.3 GPS week: 2346 Day: 3 MJD: 60669
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 2 8 22 56 .13 18 16 | 5001 -870 3265 9165
esa n/a| 0 0 0 -20 2 -34 -.17 40 29 | 845 -1883 3214 9413
gfz n/a| 2 0 4 22 -16 -47 .04 19 13 | 0 -904 3266 7909
grg n/a| 0 2 5 7 -94 -40 .30 27 22 | -2452 -711 3276 8888
iac n/a| 0 -5 -4 -29 45 16 -.21 20 19 | -1072 -1107 3260 8917
jgx n/a| 1 0 -4 5 12 -10 -.24 24 24 | 8125 -1290 3192 7859
Table 2.2346.4 GPS week: 2346 Day: 4 MJD: 60670
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 0 5 4 -10 .18 18 14 | 8589 -4488 3088 9052
esa n/a| 0 2 0 -13 23 -40 -.14 38 33 | 2074 -5374 3267 7845
gfz n/a| -1 0 2 15 -8 -16 -.02 27 16 | 0 -4096 3038 8279
grg n/a| 1 0 3 34 -48 -14 .34 27 20 | 2001 -4483 3079 8537
iac n/a| 1 0 0 -10 24 46 -.11 17 14 | 1925 -1294 3077 9186
jgx n/a| 0 0 -2 -35 -26 -71 -.22 25 25 | 11376 -5611 3831 8279
Table 2.2346.5 GPS week: 2346 Day: 5 MJD: 60671
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 -6 60 .11 18 17 | 9345 1431 3510 9368
esa n/a| 2 1 2 -13 45 -54 -.10 39 34 | 11540 269 3145 7268
gfz n/a| 0 -2 0 8 14 25 -.03 24 15 | 0 1618 3542 7874
grg n/a| 0 1 -1 15 -41 -104 .40 26 21 | 5539 1827 3514 9081
iac n/a| -1 0 0 12 18 35 -.05 16 15 | 6062 1273 3507 9091
jgx n/a| -2 0 -3 -27 -3 -31 -.25 23 23 | 12752 1002 3117 7899
Table 2.2346.6 GPS week: 2346 Day: 6 MJD: 60672
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 -1 -31 71 .13 18 18 | 4650 -789 3114 9104
esa n/a| 2 -2 1 -7 41 -14 -.12 38 39 | 1742 -1916 3060 6451
gfz n/a| 0 -2 4 33 39 31 .06 27 17 | 0 -1138 3035 7445
grg n/a| 0 0 8 13 0 13 .30 25 22 | -672 -785 3134 8782
iac n/a| 0 1 -4 -7 -4 -120 -.10 16 14 | 653 560 3104 8910
jgx n/a| 0 0 -5 -9 -12 -18 -.25 25 25 | 7812 -1603 3035 7484
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 3.2346.0 GPS week: 2346 Day: 0 MJD: 60666
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1266 26 40 37 22 26 27 13 | 87 82 111 93 83 80 87
XR02E | 2067 11 10 16 16 9 --- 6 | 113 112 116 115 108 --- 112
R03E | 1021 14 11 14 12 9 12 5 | 50 50 51 55 53 48 50
R04E | 1158 28 18 14 19 13 17 8 | 145 140 146 146 144 148 144
R05E | 1528 11 12 11 14 10 16 5 | 130 129 126 133 125 128 128
R07E | 762 9 15 12 11 11 16 5 | 90 91 97 92 90 87 90
R08E | 1291 11 17 28 21 10 20 8 | 161 169 176 154 164 163 163
R09 | 2718 9 16 18 9 5 12 5 | 28 28 38 28 30 26 28
R11 | 960 18 13 10 30 12 9 7 | 27 35 31 34 28 32 27
R12 | 1827 17 11 12 27 13 12 7 | 60 58 56 52 53 56 54
R14 | 824 7 9 8 12 9 16 4 | 48 48 50 47 48 42 46
R15 | 1496 12 18 16 13 10 17 6 | 70 49 57 61 59 49 57
R16 | 966 16 21 16 13 15 20 7 | 62 52 59 54 60 50 55
R17 | 2426 16 25 9 10 23 22 8 | 82 67 88 85 94 68 81
R18 | 501 11 16 17 14 13 22 7 | 65 76 79 78 73 56 70
R19 | 2042 30 66 18 46 24 43 17 | 117 63 106 112 105 101 101
R20 | 6056 39 102 39 62 42 55 24 | 138 68 144 137 142 103 124
R21 | 559 8 28 12 18 11 11 6 | 89 73 90 96 92 79 87
R22 | 1442 13 12 16 7 10 10 5 | 49 47 48 50 47 20 47
R24 | 900 9 41 26 12 14 23 9 | 90 62 103 96 91 77 87
XR26E |10902 38 --- --- 41 54 --- 32 | 43 --- --- 41 36 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1977 18 34 19 24 17 23 |T 83 74 88 83 82 74 79
WRMS | 1977 14 23 15 17 13 23 |NE 71 55 73 71 70 58 66
MEDI | 1291 13 16 16 14 12 17 |MD 82 63 88 85 83 68 81
Table 3.2346.1 GPS week: 2346 Day: 1 MJD: 60667
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 652 23 30 39 24 24 20 12 | 82 85 97 89 79 83 81
XR02E | 1507 10 13 11 16 9 --- 5 | 90 90 92 94 88 --- 90
R03E | 880 9 14 14 13 14 12 5 | 45 45 51 56 46 43 46
R04E | 893 25 21 19 17 15 15 8 | 106 102 108 102 104 101 102
R05E | 2467 15 15 10 18 13 13 6 | 99 99 99 101 100 99 99
R07E | 874 9 18 14 20 20 18 7 | 55 50 53 54 58 55 52
R08E | 901 14 16 18 16 12 12 6 | 113 112 110 113 114 113 112
R09 | 2070 13 17 9 13 14 10 5 | 21 26 27 24 24 21 21
R11 | 871 14 18 11 32 14 22 8 | 18 28 29 52 29 22 24
R12 | 1015 10 12 20 18 11 18 6 | 44 41 45 39 36 33 38
R14 | 744 9 8 11 22 13 16 6 | 36 33 39 24 32 26 30
R15 | 1390 21 29 13 10 14 22 8 | 49 32 35 37 45 32 37
R16 | 946 18 24 14 13 9 12 6 | 45 32 31 39 40 36 36
R17 | 1265 8 11 17 13 7 20 6 | 51 45 55 54 42 42 47
R18 | 608 9 12 9 14 17 25 7 | 44 42 42 50 49 36 42
R19 | 1398 28 80 37 53 30 20 18 | 46 65 55 62 51 75 49
R20 | 4984 45 110 58 73 23 44 25 | 75 60 80 77 69 60 63
R21 | 850 6 28 20 13 15 16 7 | 44 34 51 37 52 36 42
R22 | 1105 13 8 20 13 11 12 6 | 33 29 35 29 37 18 29
R24 | 1460 16 35 21 20 14 17 9 | 55 40 60 58 56 45 52
XR26E | 5872 41 --- --- 34 53 --- 31 | 34 --- --- 29 27 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1653 18 36 23 27 16 19 |T 56 54 59 58 56 51 53
WRMS | 1653 15 24 14 20 14 19 |NE 43 39 44 44 43 37 39
MEDI | 1015 14 17 14 17 14 17 |MD 46 42 51 54 49 42 46
Table 3.2346.2 GPS week: 2346 Day: 2 MJD: 60668
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 751 24 44 53 17 27 28 15 | 92 95 122 93 86 89 94
XR02E | 821 9 13 9 19 15 --- 6 | 82 81 85 88 84 --- 83
R03E | 803 15 14 19 23 11 17 7 | 53 50 54 58 54 47 51
R04E | 831 13 13 16 10 15 17 6 | 59 62 59 63 48 60 57
R05E | 3611 13 16 17 15 16 13 6 | 67 71 72 67 59 63 65
R07E | 916 10 12 17 19 19 13 7 | 62 63 66 64 55 60 60
R08E | 988 10 17 16 35 22 13 8 | 121 121 130 126 124 118 122
R09 | 2261 11 12 8 18 19 7 6 | 21 24 28 24 36 25 24
R11 | 671 16 14 18 20 30 9 8 | 23 25 28 21 38 27 22
R12 | 801 9 11 19 15 13 15 6 | 50 51 57 45 43 45 48
R14 | 794 14 7 11 11 14 11 5 | 43 45 39 41 43 42 40
R15 | 2032 22 12 11 9 18 8 6 | 59 44 38 47 44 47 45
R16 | 571 19 27 11 26 12 22 8 | 48 34 40 55 38 34 39
R17 | 637 9 26 12 13 19 22 7 | 57 53 67 71 67 54 60
R18 | 584 11 12 11 13 14 25 7 | 57 65 67 68 64 51 60
R19 | 1955 23 83 21 41 17 27 16 | 93 53 86 104 82 78 81
R20 | 2796 35 113 38 82 18 32 24 | 110 62 108 123 91 105 97
R21 | 589 15 29 13 13 19 26 8 | 69 60 67 69 69 59 64
XR22 | 1065 22 21 35 22 15 --- 12 | 45 52 70 64 39 --- 50
R24 | 1190 19 36 25 22 19 28 11 | 65 59 83 75 71 60 67
XR26E | 7540 38 --- --- 29 52 --- 30 | 41 --- --- 38 28 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1531 17 39 21 28 19 20 |T 62 58 68 66 60 59 60
WRMS | 1531 15 25 16 20 19 20 |NE 56 48 59 62 55 52 53
MEDI | 831 15 14 16 19 18 17 |MD 59 53 67 64 55 54 60
Table 3.2346.3 GPS week: 2346 Day: 3 MJD: 60669
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1446 24 40 43 23 41 30 15 | 141 142 161 154 136 142 144
XR02E | 809 8 12 14 13 15 --- 6 | 93 89 87 93 94 --- 90
R03E | 1081 9 17 16 20 22 21 8 | 70 63 69 79 69 63 67
R04E | 696 13 13 14 11 12 14 6 | 71 79 84 75 79 75 76
R05E | 3712 14 14 12 13 14 15 6 | 53 57 63 66 57 53 57
R07E | 579 7 21 10 22 18 14 6 | 42 54 45 43 42 37 41
R08E | 1643 14 19 17 20 21 12 7 | 81 90 86 77 71 80 79
R09 | 814 10 27 14 18 18 14 7 | 26 38 34 25 32 30 27
R11 | 1468 12 15 9 12 20 16 6 | 18 24 26 25 26 24 21
R12 | 662 13 14 12 18 18 13 6 | 32 43 41 26 40 29 32
R14 | 735 8 10 10 10 10 8 4 | 35 41 39 37 41 34 37
R15 | 1949 22 20 13 11 14 20 7 | 51 39 44 40 36 32 40
R16 | 670 26 21 17 13 14 18 8 | 52 41 42 37 43 34 40
R17 | 828 12 29 10 15 29 22 8 | 56 40 52 52 68 36 51
R18 | 516 8 11 13 16 13 24 6 | 45 46 49 58 52 31 45
R19 | 2858 43 85 19 48 21 37 18 | 104 42 95 92 77 67 82
R20 | 1933 19 116 41 79 22 61 25 | 111 46 120 147 115 72 104
R21 | 735 8 31 18 22 14 14 8 | 63 52 73 77 57 57 62
R24 | 1133 14 30 14 16 21 20 8 | 64 42 56 63 63 49 56
XR26E |10526 32 --- --- 33 57 --- 30 | 23 --- --- 30 24 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1551 18 40 19 27 20 24 |T 59 55 65 63 59 52 57
WRMS | 1551 16 29 13 22 19 24 |NE 52 41 54 55 51 41 47
MEDI | 828 13 20 14 16 18 16 |MD 53 43 52 58 57 37 51
Table 3.2346.4 GPS week: 2346 Day: 4 MJD: 60670
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 2077 26 39 51 30 20 36 15 | 88 92 97 77 85 88 84
XR02E | 1235 11 12 17 19 7 --- 6 | 64 62 62 71 60 --- 62
R03E | 663 7 16 13 15 12 14 5 | 57 59 56 55 53 54 54
R04E | 1190 10 10 11 15 15 12 5 | 65 61 62 72 58 67 62
R05E | 1465 14 11 11 13 14 15 6 | 66 66 67 65 64 64 64
R07E | 629 11 16 13 19 12 13 6 | 62 63 60 62 61 65 60
R08E | 2774 12 19 11 23 17 14 7 | 107 115 103 99 106 110 105
R09 | 794 13 7 15 13 10 14 5 | 30 27 35 29 23 34 27
R11 | 818 10 17 20 57 9 25 11 | 31 29 36 47 27 34 26
R12 | 807 11 20 16 22 7 14 6 | 54 53 53 49 48 55 50
R14 | 760 9 13 13 17 10 15 5 | 51 51 38 36 39 51 42
R15 | 1308 13 19 13 13 9 16 6 | 67 73 69 56 60 56 62
R16 | 807 23 25 23 14 19 29 10 | 59 53 55 51 59 43 51
R17 | 732 9 19 9 12 15 21 6 | 49 42 44 49 45 43 44
R18 | 590 9 17 13 15 18 23 7 | 43 53 40 45 48 36 42
R19 | 3505 47 91 42 42 28 36 21 | 90 45 98 64 72 56 70
R20 | 2549 21 104 76 54 36 63 25 | 93 50 124 104 95 59 86
R21 | 506 12 22 14 21 14 18 7 | 56 42 50 60 52 46 50
R24 | 1334 12 30 22 19 10 19 8 | 54 43 58 57 51 40 49
XR26E | 9622 38 --- --- 40 52 --- 31 | 36 --- --- 29 32 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1546 18 38 27 27 17 25 |T 60 56 64 58 56 55 55
WRMS | 1546 14 33 16 20 14 25 |NE 56 46 59 53 50 46 49
MEDI | 818 12 19 14 19 14 16 |MD 57 53 58 56 53 54 51
Table 3.2346.5 GPS week: 2346 Day: 5 MJD: 60671
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 4078 24 45 44 35 17 37 15 | 99 118 122 114 99 99 104
XR02E | 1334 6 12 11 16 8 --- 5 | 104 107 111 112 103 --- 107
R03E | 967 10 16 14 18 12 17 6 | 55 61 57 69 59 52 57
R04E | 1840 7 13 11 19 9 11 5 | 80 77 83 83 76 82 79
R05E | 1241 9 15 10 14 12 16 5 | 83 85 82 91 80 89 84
R07E | 767 13 15 18 23 15 14 7 | 61 56 62 63 57 57 58
R08E | 2114 13 22 19 23 15 15 7 | 121 125 126 122 119 127 123
R09 | 1754 14 10 15 11 16 12 6 | 31 25 24 25 30 31 25
R11 | 1331 23 26 12 42 14 13 10 | 25 44 28 85 36 26 33
R12 | 1151 14 18 12 14 8 18 6 | 45 35 38 40 42 44 41
R14 | 1150 10 12 15 19 26 18 8 | 45 47 57 44 55 46 48
R15 | 557 18 9 19 9 14 13 6 | 56 54 40 56 54 50 51
R16 | 1342 18 14 17 15 14 34 9 | 51 55 60 47 52 39 49
R17 | 868 12 18 19 21 18 18 8 | 39 33 35 45 35 33 34
R18 | 505 14 16 12 13 14 12 6 | 32 41 36 41 37 37 35
R19 | 3595 35 87 32 51 21 31 18 | 76 33 82 80 56 55 61
R20 | 2110 34 114 62 50 28 53 25 | 70 35 96 87 67 59 67
R21 | 619 15 26 11 22 12 13 7 | 45 31 35 51 28 35 35
XR22 |10477 16 13 14 20 10 --- 7 | 29 33 33 48 33 --- 32
R24 | 1720 16 33 21 23 18 14 9 | 40 44 47 49 41 34 38
XR26E |13860 50 --- --- 49 59 --- 38 | 43 --- --- 35 25 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1809 18 39 24 26 16 23 |T 58 56 62 66 56 55 56
WRMS | 1809 17 34 15 21 15 23 |NE 44 39 47 53 43 40 42
MEDI | 1334 14 16 15 20 14 15 |MD 51 44 57 56 54 46 49
Table 3.2346.6 GPS week: 2346 Day: 6 MJD: 60672
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 4586 25 37 48 28 13 42 14 | 101 99 113 109 97 96 100
XR02E | 1979 10 14 26 13 9 --- 7 | 84 82 87 86 86 --- 84
R03E | 1281 11 15 19 24 8 14 6 | 53 51 53 65 55 48 52
R04E | 1150 8 14 21 16 17 19 7 | 76 82 81 82 82 80 79
R05E | 692 13 11 17 13 10 22 6 | 90 90 89 92 87 89 88
R07E | 611 13 12 17 16 11 15 6 | 59 60 60 63 63 58 60
R08E | 923 11 15 13 12 8 8 5 | 147 145 148 147 148 145 146
R09 | 839 10 15 23 11 10 19 6 | 37 42 38 39 35 42 36
R11 | 1769 19 19 10 45 11 18 10 | 17 29 24 47 27 18 22
R12 | 2431 24 20 9 17 12 18 8 | 56 45 50 43 50 49 48
R14 | 813 8 16 17 14 15 12 6 | 54 51 53 44 56 53 51
R15 | 509 20 17 16 19 14 20 8 | 70 51 54 54 60 50 56
R16 | 1038 21 11 24 13 11 15 7 | 64 56 56 49 57 51 54
R17 | 1361 9 21 15 19 22 23 8 | 65 63 68 71 80 49 66
R18 | 480 12 20 16 24 10 21 7 | 42 56 52 61 55 36 48
R19 | 1840 33 87 48 36 16 47 19 | 102 50 121 107 90 79 90
R20 | 5488 35 108 60 56 37 51 25 | 124 43 131 126 127 89 108
R21 | 678 12 36 27 16 20 27 10 | 71 49 82 75 71 54 66
XR22 | 9750 12 12 13 13 16 --- 7 | 38 38 38 46 36 --- 37
R24 | 687 13 29 23 18 10 12 7 | 70 53 76 73 69 54 66
XR26E |16394 44 --- --- 52 61 --- 38 | 34 --- --- 25 29 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2027 18 38 27 25 16 25 |T 69 61 73 71 69 63 65
WRMS | 2027 18 39 17 22 14 25 |NE 62 48 64 64 62 52 57
MEDI | 1150 13 16 17 17 12 19 |MD 65 51 60 65 63 53 60
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