[IGSREPORT-30223] Wk 2342 IGLOS Final Orbits
acc
acc at igs.org
Mon Dec 16 00:09:32 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2342 (Nov 24, 2024 - Nov 30, 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 2.2342.
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:
igl2342[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2342 in the SP3 format.
igl23427.sum Combination Report for GPS Week 2342.
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 | 13.7 ns
1 | 16.8 ns
2 | 29.5 ns
3 | 27.8 ns
4 | 28.2 ns
5 | 25.5 ns
6 | 21.7 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 1.2342, 1a.2342).
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 2.2342.0-6)
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 3.2342.0-6).
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 2342 summary. (Nov 24, 2024 - Nov 30, 2024)
Table 1.2342.a GPS week : 2342 MJD: 60638.0-60644.0
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| -2 0 0 -9 -10 53 .17 21 17 | 6816 -1982 3436 9167
| 0 0 1 17 12 19 .03 | 1097 4989
esa n/a| 0 0 0 -5 7 34 -.12 29 21 | 30987 -2116 3454 8517
| 1 0 2 9 10 23 .03 | 9526 5338
gfz n/a| 1 0 1 36 16 13 -.01 18 14 | 0 -2045 3436 7946
| 1 1 1 15 17 17 .02 | 0 5200
grg n/a| 1 0 7 -18 -32 -27 .30 27 19 | 20474 -274 2925 7673
| 1 1 2 8 12 50 .03 | 10160 2787
iac n/a| 0 0 -7 -12 24 -37 -.10 16 14 | 24035 -806 3424 8964
| 1 1 1 11 28 25 .02 | 5696 1736
jgx n/a| -1 0 4 -14 -27 2 -.14 23 23 | 9042 -2040 3484 8127
| 1 1 2 11 14 34 .04 | 1057 5121
Table 1.2342.b GPS week : 2342 MJD: 60638.0-60644.0
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 | 16 14 16 15 14 12 16 |
R02 | 12 9 7 6 6 7 7 |
R03 | 6 8 6 6 6 6 10 |
R04 | 8 7 8 8 7 6 7 |
R05 | 7 7 7 8 6 6 6 |
R07 | 7 6 9 8 6 6 7 |
R08 | 6 5 6 8 7 7 6 |
R09 | 7 6 6 6 8 6 6 |
R11 | 6 8 7 7 5 5 6 |
R12 | 6 6 7 7 8 7 8 |
R14 | 6 6 6 7 5 7 6 |
R15 | 7 6 11 10 8 7 8 |
R16 | 6 7 7 9 10 8 8 |
R17 | 7 6 7 6 6 7 7 |
R18 | 8 6 9 8 8 8 5 |
R19 | 21 21 19 20 20 22 17 |
R20 | 22 20 19 19 21 20 21 |
R21 | 8 6 8 7 7 8 10 |
R22 | 7 6 6 7 6 6 7 |
R24 | 8 8 8 8 7 6 9 |
R26 | 38 39 37 31 29 32 32 |
Table 1.2342.c GPS week : 2342 MJD: 60638.0-60644.0
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 2342 0 | 46 -4 75 -355 3457 -1066 80.9 1292 1292 | 13662 0
brd 2342 1 | -50 47 -27 -1305 3087 3175 80.2 1053 1053 | 16815 0
brd 2342 2 | -53 45 0 -796 1535 -334 78.9 1242 1242 | 29519 0
brd 2342 3 | -11 -6 70 1425 -633 338 80.6 1446 1446 | 27750 0
brd 2342 4 | -1 129 -3 535 -195 -78 79.9 1291 1291 | 28192 0
brd 2342 5 | -23 37 0 398 -1238 -4033 79.0 1252 1252 | 25483 0
brd 2342 6 | 79 31 -81 709 -1428 -6124 79.4 1574 1574 | 21670 0
-------------+------------------------------------------------------------+----------------
brd 2342 mean| -1 39 4 87 654 -1160 79.9 1307 1307 | 23298 0
brd 2342 sdev| 49 45 54 947 2034 3049 .8 164 164 | 6120 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 2.2342.0 GPS week: 2342 Day: 0 MJD: 60638
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 -19 28 .17 19 15 | 8048 -5795 3200 9854
esa n/a| -1 0 0 -17 1 7 -.13 31 24 | 19015 -6003 3202 8157
gfz n/a| 1 2 -1 51 18 17 .00 22 16 | 0 -5700 3169 8354
grg n/a| 2 0 4 -4 -52 3 .32 25 20 | 15862 -5718 3234 9736
iac n/a| 2 -1 -8 -28 59 -10 -.10 16 14 | 14295 424 3195 9522
jgx n/a| 0 -1 4 -4 -29 -37 -.20 24 24 | 10421 -5576 3186 8501
Table 2.2342.1 GPS week: 2342 Day: 1 MJD: 60639
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 -14 9 71 .21 19 17 | 5723 -11471 3597 7971
esa n/a| 0 0 0 4 -1 30 -.13 30 23 | 17887 -12132 3631 6718
gfz n/a| 0 0 0 19 0 35 -.00 18 12 | 0 -12067 3574 6898
grg n/a| 1 -1 5 -19 -40 -105 .29 30 22 | --- --- --- ---
iac n/a| 0 1 -7 5 36 -8 -.13 14 13 | 18783 -3123 3568 7786
jgx n/a| 0 -1 4 -9 -20 -25 -.14 21 21 | 8331 -11881 3696 7173
Table 2.2342.2 GPS week: 2342 Day: 2 MJD: 60640
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 1 0 -41 -11 49 .21 22 17 | 6941 -1022 3214 8678
esa n/a| 0 0 0 -1 21 8 -.10 27 21 | 37998 -1386 3243 7391
gfz n/a| 1 0 0 57 42 27 .03 21 16 | 0 -952 3262 8076
grg n/a| 3 1 13 -27 -19 21 .24 25 22 | 29704 -1106 3209 8128
iac n/a| 0 0 -9 -11 11 -64 -.10 15 14 | 27721 1642 3212 8771
jgx n/a| 0 0 9 -26 -40 27 -.12 25 25 | 9495 -1196 3247 8043
Table 2.2342.3 GPS week: 2342 Day: 3 MJD: 60641
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 -17 -27 67 .16 21 16 | 5007 1797 4097 9372
esa n/a| 0 0 -1 -18 -4 48 -.16 27 21 | 40315 1001 4143 10861
gfz n/a| 2 0 3 31 0 21 -.02 18 14 | 0 1327 4099 8590
grg n/a| 0 1 6 -18 -23 -29 .30 22 15 | 26937 1641 4117 8694
iac n/a| 2 1 -9 -2 60 -70 -.10 19 18 | 28877 190 4086 9190
jgx n/a| -3 1 3 2 -31 0 -.18 24 24 | 7103 1204 4220 8936
Table 2.2342.4 GPS week: 2342 Day: 4 MJD: 60642
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 1 -4 -18 36 .14 23 17 | 6857 963 3411 9023
esa n/a| 1 0 -4 -6 17 73 -.14 32 20 | 32179 760 3417 8220
gfz n/a| 2 1 2 24 13 -5 -.02 16 13 | 0 1038 3424 8183
grg n/a| 1 -1 7 -28 -25 -41 .29 25 18 | 27063 1167 3381 8731
iac n/a| 0 0 -5 -16 13 -35 -.09 16 14 | 29239 -2108 3388 8822
jgx n/a| -1 -2 2 -25 -27 26 -.12 23 23 | 9072 1064 3487 8471
Table 2.2342.5 GPS week: 2342 Day: 5 MJD: 60643
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 -1 1 -3 42 .16 20 16 | 7781 2434 3549 9282
esa n/a| 1 1 0 1 14 25 -.08 31 18 | 29122 3845 3565 7246
gfz n/a| 0 0 2 21 4 -12 -.01 14 11 | 0 2974 3541 7711
grg n/a| 1 0 6 -8 -42 34 .31 33 20 | 23400 2913 3552 8759
iac n/a| 0 1 -5 -8 5 -19 -.08 14 13 | 26584 -341 3549 8937
jgx n/a| -1 0 2 -24 1 -27 -.15 21 21 | 9538 3059 3571 7786
Table 2.2342.6 GPS week: 2342 Day: 6 MJD: 60644
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 1 -1 9 -1 79 .16 20 16 | 7355 -782 2985 9991
esa n/a| 0 0 0 1 0 45 -.10 29 18 | 40395 -898 2982 11032
gfz n/a| 0 2 1 46 39 11 -.03 17 12 | 0 -936 2986 7812
grg n/a| 0 0 7 -19 -21 -72 .33 29 18 | 20358 -821 2988 9669
iac n/a| 1 -1 -5 -22 -12 -55 -.07 15 14 | 22748 -2326 2976 9722
jgx n/a| -1 -2 3 -10 -41 52 -.10 23 23 | 9335 -959 2986 7980
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 3.2342.0 GPS week: 2342 Day: 0 MJD: 60638
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1428 45 41 21 27 15 50 15 | 107 43 76 61 77 46 69
XR02 | 4111 16 --- 19 --- 15 --- 12 | 77 --- 79 --- 73 --- 75
R03 | 829 11 15 15 14 8 16 5 | 94 83 98 87 92 74 89
R04 | 995 20 11 14 16 9 27 7 | 100 86 85 84 88 75 86
XR05 | 1708 11 19 15 17 11 --- 7 | 90 82 93 81 91 --- 87
R07 | 954 8 28 12 14 16 17 7 | 85 70 88 85 97 69 83
R08 | 779 13 15 13 14 11 14 6 | 74 75 82 85 89 69 79
R09 | 2409 13 14 18 15 7 19 6 | 19 32 27 21 24 26 22
R11 | 1128 14 9 13 19 8 11 5 | 25 31 33 42 31 30 29
R12 | 724 11 18 11 13 10 14 5 | 56 60 50 49 57 40 52
R14 | 1157 9 19 13 14 12 10 5 | 69 78 71 63 68 66 68
R15 | 977 14 12 11 13 14 29 7 | 81 65 72 70 84 57 72
R16 | 723 14 19 11 8 11 21 6 | 86 73 70 76 79 63 74
R17 | 582 17 13 12 19 15 18 7 | 43 39 40 39 46 42 40
R18 | 723 12 20 14 11 18 26 7 | 27 38 33 28 33 23 28
R19 | 1976 39 71 27 54 40 44 20 | 44 38 56 50 47 43 45
R20 | 2216 17 82 69 63 22 29 22 | 53 44 68 64 50 47 51
R21 | 748 12 26 15 28 13 17 8 | 40 30 41 50 45 33 39
R22 | 1913 13 10 22 15 16 9 6 | 63 67 71 67 70 70 67
R24 | 695 14 19 18 16 19 20 8 | 38 35 39 41 38 33 35
XR26 | 8822 39 --- --- 51 62 --- 37 | 101 --- --- 95 127 --- 104
------+-----------------------------------------+-------------------------------------
RMS | 1292 19 31 22 25 16 24 |T 65 56 63 61 66 50 61
WRMS | 1292 15 24 16 20 14 24 |NE 65 56 63 61 66 50 61
MEDI | 995 14 19 14 15 14 18 |MD 69 60 70 63 70 46 68
Table 3.2342.1 GPS week: 2342 Day: 1 MJD: 60639
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1439 47 38 15 30 18 37 13 | 72 33 37 36 58 32 44
XR02 | 3136 16 19 15 23 18 --- 9 | 50 64 44 47 62 --- 50
R03 | 751 12 24 10 15 15 26 7 | 69 57 65 70 68 46 63
R04 | 670 17 10 10 25 9 21 7 | 78 76 71 71 77 67 72
XR05 | 1423 13 14 8 21 11 --- 6 | 73 66 69 66 70 --- 68
R07 | 1058 9 17 9 10 10 21 5 | 62 52 61 65 65 48 60
R08 | 933 11 13 12 14 9 12 5 | 53 49 44 58 51 50 49
R09 | 1911 16 25 11 16 9 7 6 | 24 44 37 35 30 32 31
R11 | 796 13 16 23 20 14 15 8 | 28 32 34 49 30 36 31
R12 | 818 13 16 9 11 8 18 5 | 47 46 46 41 44 34 42
R14 | 1006 15 16 10 16 8 10 5 | 55 53 47 40 54 45 48
R15 | 1074 12 13 8 13 10 19 5 | 62 51 57 57 66 52 58
R16 | 941 19 15 9 20 11 20 7 | 72 61 56 63 58 46 58
R17 | 762 22 15 10 12 7 11 6 | 27 26 25 26 25 22 23
R18 | 791 8 17 14 13 13 15 6 | 25 24 26 26 26 18 22
R19 | 1374 31 68 30 93 26 36 20 | 39 35 31 60 29 40 29
R20 | 1132 19 79 55 46 24 37 19 | 37 28 61 41 21 38 34
R21 | 1034 10 14 11 22 6 18 6 | 23 24 26 36 22 23 23
R22 | 1013 16 13 7 15 17 12 6 | 72 73 71 73 67 78 71
R24 | 634 12 19 14 27 18 16 7 | 26 30 28 28 21 22 21
XR26 | 8224 57 --- --- 49 56 --- 39 | 89 --- --- 86 107 --- 93
------+-----------------------------------------+-------------------------------------
RMS | 1053 19 30 18 30 14 21 |T 51 46 46 51 50 40 47
WRMS | 1053 17 23 12 22 13 21 |NE 51 46 46 51 50 40 47
MEDI | 1013 15 16 10 20 11 18 |MD 53 46 44 49 54 38 48
Table 3.2342.2 GPS week: 2342 Day: 2 MJD: 60640
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1327 52 38 25 37 20 36 15 | 79 44 52 42 57 39 49
XR02 | 2578 10 23 11 15 11 --- 7 | 54 51 47 43 54 --- 54
R03 | 1215 8 16 13 12 13 20 6 | 69 62 72 67 68 54 65
R04 | 639 24 14 14 17 12 20 7 | 77 67 57 55 60 50 60
XR05 | 1052 15 13 11 15 11 --- 6 | 72 68 63 67 79 --- 69
R07 | 976 16 14 29 23 10 29 9 | 64 46 73 39 61 37 54
R08 | 708 9 11 14 8 17 17 6 | 57 52 59 56 71 44 57
R09 | 1206 14 15 11 15 9 13 5 | 24 37 36 26 26 30 27
R11 | 859 17 13 14 16 13 15 6 | 20 29 35 23 30 22 24
R12 | 1304 11 13 15 17 9 27 7 | 51 49 51 60 51 35 49
R14 | 1157 8 21 9 17 12 6 6 | 61 73 56 63 51 59 59
R15 | 1881 15 12 7 30 31 34 10 | 69 59 62 43 88 47 63
R16 | 1231 21 13 12 18 10 23 7 | 72 59 67 56 70 53 63
R17 | 1118 22 9 13 16 8 27 7 | 36 35 37 33 33 30 32
R18 | 599 9 17 21 31 11 25 8 | 29 33 38 42 29 21 28
R19 | 1267 41 64 33 56 15 38 19 | 37 25 40 34 29 29 25
R20 | 1879 34 64 53 39 22 33 19 | 49 37 64 45 39 41 41
R21 | 1581 11 19 19 14 15 24 7 | 30 29 37 41 36 23 31
R22 | 1535 15 6 10 13 14 10 5 | 71 72 72 72 74 78 72
R24 | 863 12 17 12 26 12 20 7 | 34 33 38 39 28 29 31
XR26 | 7266 48 --- --- 50 56 --- 37 | 103 --- --- 93 124 --- 107
------+-----------------------------------------+-------------------------------------
RMS | 1241 22 27 21 25 15 25 |T 55 48 52 49 55 40 50
WRMS | 1241 17 21 16 22 14 25 |NE 55 48 52 49 55 40 50
MEDI | 1215 15 14 13 17 12 23 |MD 57 46 52 43 54 37 54
Table 3.2342.3 GPS week: 2342 Day: 3 MJD: 60641
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 681 47 40 23 29 20 39 15 | 77 27 57 39 60 27 47
R02 | 2722 12 15 10 11 13 9 5 | 52 50 43 50 44 31 48
R03 | 993 9 11 13 10 10 17 5 | 69 68 76 69 69 54 68
R04 | 1013 25 9 14 13 12 25 7 | 66 47 56 43 44 32 47
XR05 | 827 16 13 13 21 8 --- 7 | 68 62 53 49 61 --- 56
R07 | 1491 10 12 22 16 20 20 8 | 69 62 78 59 82 53 67
R08 | 833 10 10 15 14 28 12 7 | 59 57 59 51 83 51 59
R09 | 1256 12 14 13 16 8 8 5 | 21 28 27 17 26 20 20
R11 | 1444 15 19 12 10 21 17 7 | 25 43 37 30 48 28 33
R12 | 1657 6 10 9 15 26 21 7 | 55 56 50 46 70 41 52
R14 | 593 10 18 10 12 12 23 6 | 56 63 47 55 48 34 49
R15 | 1155 16 31 23 11 24 29 10 | 74 64 84 64 86 51 70
R16 | 731 23 17 13 27 13 19 8 | 71 69 62 39 67 48 58
R17 | 801 15 9 12 7 16 16 6 | 25 27 30 26 26 22 25
R18 | 632 11 22 13 18 10 28 7 | 28 33 36 30 28 19 27
R19 | 1405 45 69 19 56 29 34 19 | 32 43 34 42 31 38 32
R20 | 2250 34 54 46 42 32 44 19 | 51 38 44 70 41 68 46
R21 | 1796 13 19 15 9 16 19 6 | 27 30 35 29 33 25 28
R22 | 2450 16 9 17 11 10 19 6 | 24 32 43 41 34 33 33
R24 | 989 16 26 13 18 8 21 7 | 34 26 29 32 29 27 28
XR26 |12718 32 --- --- 34 59 --- 31 | 51 --- --- 42 70 --- 55
------+-----------------------------------------+-------------------------------------
RMS | 1446 21 27 18 22 19 24 |T 49 46 49 43 51 36 45
WRMS | 1446 16 21 14 15 18 24 |NE 49 46 49 43 51 36 45
MEDI | 1155 15 15 13 15 16 20 |MD 52 43 44 42 48 33 47
Table 3.2342.4 GPS week: 2342 Day: 4 MJD: 60642
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 973 51 45 15 30 12 36 14 | 70 27 51 36 47 38 43
R02 | 888 11 25 8 11 11 13 5 | 49 52 44 38 38 21 43
R03 | 600 9 14 8 17 11 17 5 | 60 54 55 75 65 52 60
R04 | 1412 18 14 16 10 10 23 7 | 70 66 65 64 59 56 62
XR05 | 1345 9 11 15 16 9 --- 6 | 62 61 65 54 58 --- 59
R07 | 954 19 12 11 15 12 12 6 | 65 57 52 52 61 50 55
R08 | 1038 12 19 14 10 16 13 6 | 61 62 66 61 72 57 63
R09 | 1449 19 34 14 25 10 8 8 | 19 34 24 28 16 18 16
R11 | 1693 13 12 10 15 10 11 5 | 17 35 24 27 33 21 25
R12 | 2245 10 20 15 21 23 12 8 | 55 68 51 48 73 46 55
R14 | 1052 10 16 11 10 7 18 5 | 55 62 56 59 50 51 54
R15 | 827 25 13 13 13 15 25 8 | 70 57 64 63 49 46 57
R16 | 685 22 28 20 15 10 35 9 | 76 70 82 63 75 48 69
R17 | 912 11 12 8 13 13 17 5 | 30 26 29 30 29 27 28
R18 | 735 18 20 13 24 16 22 8 | 23 27 31 35 18 20 23
R19 | 1170 55 74 23 65 27 34 20 | 37 48 35 35 27 29 29
R20 | 1869 29 77 40 52 40 46 20 | 40 45 70 38 28 58 40
R21 | 1069 12 20 8 18 11 22 6 | 30 26 27 31 28 19 26
R22 | 1502 14 12 11 13 11 13 5 | 55 61 61 59 64 64 60
R24 | 1920 12 25 15 12 7 21 7 | 34 25 35 32 27 25 28
XR26 |12816 33 --- --- 42 43 --- 28 | 107 --- --- 87 105 --- 100
------+-----------------------------------------+-------------------------------------
RMS | 1291 23 32 16 25 16 23 |T 51 48 49 48 48 39 47
WRMS | 1291 17 20 13 18 14 23 |NE 51 48 49 48 48 39 47
MEDI | 1069 14 19 13 15 11 18 |MD 55 52 51 48 49 46 54
Table 3.2342.5 GPS week: 2342 Day: 5 MJD: 60643
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 710 39 29 16 40 10 32 12 | 64 44 56 48 42 42 47
R02 | 1082 10 16 14 19 7 21 6 | 48 45 59 35 50 23 49
R03 | 645 9 20 12 11 10 20 6 | 59 49 63 61 63 48 58
R04 | 1534 18 15 9 16 7 19 6 | 65 56 55 66 55 49 56
R05 | 807 12 21 14 11 8 12 5 | 53 67 51 57 57 15 54
R07 | 884 20 19 9 16 10 11 6 | 57 44 38 48 46 41 44
R08 | 1491 14 12 15 21 16 13 6 | 57 54 51 40 62 51 52
R09 | 1167 16 14 12 16 9 9 5 | 21 24 22 15 20 22 17
R11 | 890 14 13 10 10 8 8 4 | 23 32 32 23 27 26 26
R12 | 1853 9 8 9 22 17 21 6 | 56 57 63 44 64 47 56
R14 | 645 8 23 13 21 14 8 6 | 57 65 55 42 52 52 53
R15 | 1004 24 10 8 19 14 16 7 | 64 51 54 58 41 49 50
R16 | 888 21 19 9 20 10 28 7 | 72 57 67 73 61 64 64
R17 | 1146 11 8 12 12 7 30 6 | 25 24 29 26 20 19 22
R18 | 569 18 14 8 24 18 18 7 | 22 20 23 30 25 19 20
R19 | 854 40 78 18 98 29 43 22 | 23 47 34 44 21 27 24
R20 | 1676 35 85 28 71 29 32 20 | 32 71 50 31 32 40 36
R21 | 1386 18 26 17 22 13 17 8 | 24 22 22 33 23 15 18
R22 | 960 14 6 13 17 8 12 5 | 47 53 55 53 50 52 51
R24 | 2722 17 16 13 10 11 15 6 | 35 28 31 23 24 32 26
XR26 |11287 46 --- --- 44 43 --- 31 | 81 --- --- 96 106 --- 96
------+-----------------------------------------+-------------------------------------
RMS | 1252 20 31 14 33 14 21 |T 46 45 45 45 44 36 43
WRMS | 1252 16 18 11 20 13 21 |NE 46 45 45 45 44 36 43
MEDI | 1004 17 16 12 19 10 17 |MD 53 47 51 44 46 40 49
Table 3.2342.6 GPS week: 2342 Day: 6 MJD: 60644
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 751 55 20 35 33 14 36 15 | 92 47 60 48 62 46 54
R02 | 1542 11 25 7 21 8 15 6 | 62 60 58 45 58 24 58
R03 | 973 11 21 28 17 11 32 9 | 81 63 91 71 84 57 76
R04 | 872 19 10 15 9 15 15 6 | 87 70 80 75 68 63 73
R05 | 545 9 18 7 12 17 15 6 | 76 87 78 78 75 15 76
R07 | 1960 19 19 11 14 13 19 7 | 75 62 61 64 74 53 64
R08 | 1472 11 18 12 20 9 15 6 | 70 70 77 80 86 67 75
R09 | 1376 13 11 17 13 14 8 6 | 22 30 34 23 21 27 23
R11 | 1599 16 20 12 17 9 7 6 | 25 36 29 23 26 21 24
R12 | 1115 9 12 21 23 14 17 7 | 73 77 76 60 83 60 72
R14 | 968 12 17 10 21 10 11 6 | 76 86 76 62 74 71 74
R15 | 1371 13 12 9 10 22 25 7 | 81 70 78 76 85 68 77
R16 | 1636 18 19 14 23 9 22 7 | 90 68 78 88 82 72 79
R17 | 1524 9 16 12 13 15 29 7 | 34 28 37 34 36 24 31
R18 | 786 11 15 8 9 6 18 5 | 24 24 24 25 22 19 21
R19 | 1376 33 73 15 60 20 26 17 | 34 34 37 47 37 27 32
R20 | 3220 28 70 31 87 20 42 20 | 40 42 56 57 43 47 40
R21 | 1897 17 26 15 13 25 29 9 | 34 30 36 37 39 26 30
R22 | 1191 15 17 17 19 12 12 7 | 68 81 81 67 67 66 71
R24 | 2673 20 24 12 26 15 29 9 | 47 33 37 48 43 35 39
XR26 | 9844 37 --- --- 46 48 --- 31 | 102 --- --- 98 122 --- 107
------+-----------------------------------------+-------------------------------------
RMS | 1573 20 29 17 29 15 23 |T 61 54 59 57 61 44 56
WRMS | 1573 16 18 12 18 14 23 |NE 61 54 59 57 61 44 56
MEDI | 1376 15 18 12 19 14 18 |MD 70 60 60 60 67 46 64
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