[IGSREPORT-30198] Wk 2340 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 29 06:51:09 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2340 (Nov 10, 2024 - Nov 16, 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 2.2340.
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:
igl2340[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2340 in the SP3 format.
igl23407.sum Combination Report for GPS Week 2340.
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 | 5.5 ns
1 | 5.2 ns
2 | 7.0 ns
3 | 1.4 ns
4 | 4.8 ns
5 | 2.5 ns
6 | 7.0 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 | COD | R26
0 | EMR | R26
0 | ESA | R26
0 | GFZ | R26
0 | GRG | R26
0 | IAC | R26
0 | JGX | 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 1.2340, 1a.2340).
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 2.2340.0-6)
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 3.2340.0-6).
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 2340 summary. (Nov 10, 2024 - Nov 16, 2024)
Table 1.2340.a GPS week : 2340 MJD: 60624.0-60630.0
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 5 0 58 .16 23 17 | -69 -39 3496 10029
| 0 1 1 10 25 28 .03 | 1293 3130
esa n/a| 0 0 0 -30 19 15 -.11 25 17 | 6266 24 3406 7852
| 0 0 1 10 14 33 .02 | 7940 3001
gfz n/a| 0 0 -1 28 18 11 -.02 19 16 | 0 -64 3411 8053
| 1 0 1 16 5 24 .03 | 0 2785
grg n/a| 1 0 7 -14 -25 -19 .30 27 20 | 3575 -35 3501 9720
| 1 1 4 17 16 47 .04 | 1529 3108
iac n/a| 1 0 -6 14 -1 -14 -.08 16 15 | 6670 -180 3484 9741
| 1 0 1 12 23 48 .03 | 1685 1834
jgx n/a| -1 0 4 -8 -12 -7 -.13 23 23 | 3168 -221 3344 8033
| 1 1 1 10 12 36 .04 | 1489 2678
Table 1.2340.b GPS week : 2340 MJD: 60624.0-60630.0
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 | 14 14 15 13 15 13 15 |
R02 | 7 7 7 --- --- --- --- |
R03 | 5 6 6 9 6 6 7 |
R04 | 7 6 5 6 7 8 8 |
R05 | 7 8 6 8 6 6 7 |
R07 | 7 8 6 9 7 7 5 |
R08 | 6 7 6 8 8 6 6 |
R09 | 7 7 7 8 6 6 7 |
R11 | 6 6 6 7 5 7 7 |
R12 | 8 9 8 8 7 7 7 |
R14 | 7 6 7 8 7 7 7 |
R15 | 9 9 9 9 8 7 9 |
R16 | 8 8 11 10 8 8 7 |
R17 | 6 6 6 6 5 7 6 |
R18 | 7 8 7 8 10 7 8 |
R19 | 22 23 22 21 21 20 19 |
R20 | 18 17 14 23 20 22 20 |
R21 | 8 9 5 8 6 8 7 |
R22 | 7 6 6 6 6 7 7 |
R24 | 7 6 6 6 6 7 8 |
R26 | --- 31 28 26 38 31 33 |
Table 1.2340.c GPS week : 2340 MJD: 60624.0-60630.0
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 2340 0 | 25 13 3 -107 -1158 -7196 81.1 1626 1626 | 5490 0
brd 2340 1 | 54 -7 12 1325 -1735 -9930 81.9 1629 1629 | 5181 0
brd 2340 2 | 23 -45 -103 -1172 -1869 -8423 80.5 1492 1492 | 7027 0
brd 2340 3 | 11 3 -121 -1403 1002 -7901 80.7 1292 1292 | 1367 0
brd 2340 4 | 78 14 -13 -798 683 -6025 80.4 1274 1274 | 4749 0
brd 2340 5 | -29 18 -81 -1837 1085 1697 80.7 1360 1360 | 2482 0
brd 2340 6 | 33 63 -196 -2601 1281 -716 81.3 1274 1274 | 7015 0
-------------+------------------------------------------------------------+----------------
brd 2340 mean| 28 8 -71 -942 -101 -5499 81.0 1420 1420 | 4758 0
brd 2340 sdev| 33 32 76 1269 1417 4316 .5 160 160 | 2146 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 2.2340.0 GPS week: 2340 Day: 0 MJD: 60624
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 -8 1 93 .20 23 19 | -695 -797 3645 7365
esa n/a| 0 0 -3 -35 6 10 -.12 23 18 | 7575 -665 3639 6880
gfz n/a| -2 0 0 46 18 40 -.03 20 16 | 0 -595 3608 7328
grg n/a| 0 -1 9 -31 -31 -14 .27 24 19 | 5598 -510 3638 6712
iac n/a| 0 0 -5 10 16 -85 -.13 14 14 | 8492 -1946 3631 7778
jgx n/a| 0 0 7 -3 9 14 -.10 24 24 | 1088 -586 3653 7389
Table 2.2340.1 GPS week: 2340 Day: 1 MJD: 60625
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 7 34 .16 24 18 | -58 1533 3046 9388
esa n/a| 0 0 0 -32 22 -8 -.12 22 18 | 11889 1872 2991 9244
gfz n/a| 0 0 -2 50 14 36 .02 21 17 | 0 1426 3012 7543
grg n/a| 0 -1 6 -42 -32 -46 .31 23 16 | 3129 1454 3086 9048
iac n/a| 2 1 -8 16 -9 29 -.12 18 17 | 7544 -434 3055 9179
jgx n/a| 0 1 4 -5 -10 9 -.19 22 22 | 2777 1754 3013 7714
Table 2.2340.2 GPS week: 2340 Day: 2 MJD: 60626
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 -9 14 24 .16 23 16 | 2378 1885 3201 10773
esa n/a| 0 1 1 -17 29 34 -.16 25 16 | -10593 1892 3191 8277
gfz n/a| 0 2 -2 39 9 30 .01 16 13 | 0 1928 3200 8669
grg n/a| 0 -1 7 -4 -16 4 .26 24 17 | 4534 1805 3215 10336
iac n/a| 1 1 -3 3 -29 -38 -.07 14 12 | 8330 97 3187 10410
jgx n/a| -1 -3 3 -22 -26 -49 -.11 25 25 | 6002 1642 3154 9113
Table 2.2340.3 GPS week: 2340 Day: 3 MJD: 60627
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 10 43 27 .13 25 17 | 207 -2480 3172 10435
esa n/a| 1 0 1 -44 30 -40 -.09 22 17 | 3753 -2445 3151 8185
gfz n/a| 0 0 -1 21 26 -24 -.04 18 17 | 0 -2447 3153 7687
grg n/a| 2 -1 1 -14 -15 74 .31 30 21 | 866 -2569 3151 10270
iac n/a| 0 0 -7 25 -27 64 -.04 24 23 | 4472 -1585 3165 9817
jgx n/a| -2 0 5 4 -21 -66 -.16 21 21 | 3548 -2659 3164 7932
Table 2.2340.4 GPS week: 2340 Day: 4 MJD: 60628
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 15 -29 78 .12 21 19 | -103 2242 3211 10831
esa n/a| 0 0 1 -35 38 12 -.11 26 16 | 9853 2451 3183 8147
gfz n/a| 0 0 2 9 24 3 -.07 20 17 | 0 2257 3192 8660
grg n/a| 1 0 2 -17 1 -50 .37 30 22 | 2857 2213 3219 10597
iac n/a| 1 0 -6 15 -6 -21 -.07 14 13 | 5350 2371 3198 10357
jgx n/a| -1 0 4 -6 -2 -11 -.08 23 23 | 3441 2065 3181 8665
Table 2.2340.5 GPS week: 2340 Day: 5 MJD: 60629
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 2 13 -28 76 .17 20 16 | -261 -5662 4093 10538
esa n/a| 1 -1 1 -16 5 59 -.10 29 17 | 11782 -5356 3744 6837
gfz n/a| 1 0 -2 14 15 -6 .01 17 15 | 0 -5035 3773 7402
grg n/a| 1 0 11 11 -46 -64 .30 30 22 | 3487 -5644 4075 10443
iac n/a| 0 0 -6 -2 22 -16 -.06 14 12 | 4969 -1916 4062 10067
jgx n/a| -1 -1 4 -4 -12 31 -.14 23 23 | 2470 -4954 3766 7400
Table 2.2340.6 GPS week: 2340 Day: 6 MJD: 60630
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 4 -9 75 .18 22 17 | -1951 3004 4110 10873
esa n/a| 0 1 -1 -30 0 42 -.10 25 18 | 9607 2421 3949 7400
gfz n/a| 0 0 0 19 18 0 -.04 21 18 | 0 2014 3940 9087
grg n/a| 2 0 12 -3 -34 -41 .25 27 27 | 4555 3002 4127 10637
iac n/a| 2 1 -8 32 26 -36 -.10 16 15 | 7535 2151 4094 10585
jgx n/a| 0 -1 2 -24 -25 16 -.15 21 21 | 2851 1185 3482 8023
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 3.2340.0 GPS week: 2340 Day: 0 MJD: 60624
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 874 44 29 18 34 24 41 14 | 98 62 74 63 72 60 70
R02 | 2739 9 19 15 16 13 13 6 | 22 34 25 27 29 14 26
R03 | 2174 9 8 11 17 8 14 5 | 81 82 79 90 83 74 81
R04 | 846 18 10 11 15 14 17 6 | 92 87 89 88 82 76 85
R05 | 777 25 13 9 15 10 22 7 | 87 88 81 84 79 81 82
R07 | 1520 9 11 21 13 13 22 7 | 82 77 93 78 84 68 81
R08 | 762 14 9 14 9 14 15 5 | 75 79 81 75 83 74 78
R09 | 2753 18 9 20 18 10 12 6 | 31 44 51 29 42 34 38
R11 | 2015 15 9 11 17 13 10 5 | 33 43 46 38 44 37 40
R12 | 1222 15 19 14 15 18 23 8 | 72 68 63 60 73 50 63
R14 | 1284 10 15 17 19 10 25 7 | 66 73 73 59 68 51 65
R15 | 1304 18 14 10 22 23 26 8 | 74 56 64 53 76 44 61
R16 | 1187 28 16 15 20 11 15 8 | 72 53 51 46 53 39 50
R17 | 678 10 16 5 18 12 18 6 | 25 24 21 25 20 17 19
R18 | 683 8 24 9 16 10 20 7 | 24 23 22 29 22 19 21
R19 | 2313 52 63 37 64 13 55 21 | 60 34 46 40 45 45 43
R20 | 2051 37 53 54 38 21 33 18 | 49 35 52 34 46 50 40
R21 | 1330 14 16 21 20 9 27 8 | 25 22 36 28 24 23 23
R22 | 1942 15 10 24 12 10 10 6 | 44 44 51 50 48 23 46
R24 | 1310 15 15 13 16 18 14 7 | 26 25 21 26 26 18 20
------+-----------------------------------------+-------------------------------------
RMS | 1625 23 23 20 24 14 24 |T 56 52 55 51 56 44 52
WRMS | 1625 19 18 16 19 14 24 |NE 56 52 55 51 56 44 52
MEDI | 1304 15 15 14 17 13 18 |MD 60 44 51 46 53 44 50
Table 3.2340.1 GPS week: 2340 Day: 1 MJD: 60625
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 737 48 32 18 20 21 36 13 | 66 39 62 44 45 39 46
R02 | 3080 11 11 22 12 17 8 6 | 29 25 26 32 23 13 24
R03 | 1338 10 13 11 13 13 18 6 | 55 58 47 56 55 47 52
R04 | 953 14 10 11 13 13 16 6 | 68 59 66 64 62 54 61
XR05 | 803 20 9 20 11 15 --- 7 | 72 67 65 67 58 --- 64
R07 | 1802 9 12 29 10 14 21 7 | 52 51 75 56 55 45 54
R08 | 1028 13 6 12 19 15 18 6 | 52 50 60 42 56 44 49
R09 | 1915 13 14 19 15 17 7 6 | 19 31 29 21 34 24 24
R11 | 2790 17 13 17 10 12 11 6 | 18 28 46 30 38 28 30
R12 | 1027 11 14 14 24 23 27 9 | 48 49 47 39 57 30 43
R14 | 638 9 13 10 10 16 21 6 | 52 56 56 61 67 45 55
R15 | 1018 16 16 15 12 21 27 8 | 57 44 59 48 64 41 50
R16 | 1360 25 17 18 19 11 19 8 | 57 43 51 40 41 30 41
R17 | 656 10 12 8 9 14 19 5 | 18 19 19 20 18 14 16
R18 | 621 23 16 11 12 18 17 7 | 19 20 28 24 31 16 21
R19 | 1680 62 60 38 67 28 45 23 | 43 35 46 38 25 30 32
R20 | 1077 42 46 49 38 20 29 17 | 40 25 41 52 28 45 30
R21 | 1140 10 19 25 20 24 6 8 | 23 23 35 28 26 25 22
R22 | 3097 12 8 15 12 14 7 5 | 31 27 41 33 39 18 33
R24 | 1364 14 8 12 12 19 13 6 | 20 22 22 23 28 15 19
XR26 | 8743 34 --- --- 33 57 --- 31 | 25 --- --- 37 61 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1628 24 22 21 23 18 22 |T 41 38 46 40 43 31 38
WRMS | 1628 18 18 17 16 17 22 |NE 41 38 46 40 43 31 38
MEDI | 1140 14 13 15 13 17 18 |MD 43 35 46 39 41 30 38
Table 3.2340.2 GPS week: 2340 Day: 2 MJD: 60626
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 779 48 38 25 26 11 48 14 | 76 32 70 49 56 39 52
XR02 | 1375 19 14 9 10 11 --- 6 | 25 35 32 31 28 --- 28
R03 | 1149 9 10 12 22 14 14 6 | 55 52 59 67 57 51 56
R04 | 894 10 14 10 10 8 13 5 | 58 54 58 54 55 52 55
XR05 | 842 15 16 10 13 9 --- 6 | 51 55 62 63 60 --- 58
R07 | 1997 15 10 7 10 13 22 6 | 65 56 59 64 62 45 58
R08 | 1332 12 15 12 15 10 16 6 | 60 59 50 49 60 48 54
R09 | 1809 15 16 16 24 13 9 7 | 30 37 39 21 35 27 30
R11 | 2440 12 15 11 19 15 12 6 | 41 55 47 35 47 43 44
R12 | 1004 11 15 11 21 22 14 7 | 68 67 67 60 80 61 67
R14 | 690 18 17 13 14 8 22 6 | 57 69 65 59 58 43 58
R15 | 1391 20 17 21 13 10 35 9 | 74 66 78 63 59 44 64
R16 | 1439 19 23 28 18 10 37 10 | 72 63 85 55 64 41 63
R17 | 672 14 10 13 15 13 19 6 | 26 26 37 31 33 25 29
R18 | 826 16 16 13 12 8 22 6 | 32 29 38 29 29 25 29
R19 | 720 52 74 18 66 33 44 21 | 51 55 45 43 40 33 38
R20 | 2283 42 38 21 32 19 32 13 | 52 54 58 60 36 53 44
R21 | 797 12 13 9 13 7 14 5 | 28 30 25 32 26 25 26
R22 | 2888 14 9 15 16 8 13 5 | 57 68 60 63 60 39 62
R24 | 988 11 11 12 13 14 10 5 | 25 26 23 29 25 21 22
XR26 |13034 48 --- --- 30 39 --- 28 | 44 --- --- 46 63 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1491 23 25 16 24 14 25 |T 49 49 52 47 49 39 46
WRMS | 1491 16 16 13 17 12 25 |NE 49 49 52 47 49 39 46
MEDI | 1149 15 15 12 15 11 16 |MD 52 54 58 49 56 41 52
Table 3.2340.3 GPS week: 2340 Day: 3 MJD: 60627
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1079 51 18 25 28 13 18 12 | 81 39 39 41 53 46 46
R03 | 1266 13 16 11 19 30 26 9 | 60 54 66 74 79 47 61
R04 | 1077 13 14 16 17 14 7 6 | 57 42 45 62 54 48 49
R05 | 1060 12 16 17 18 22 16 7 | 47 58 56 60 44 43 49
R07 | 988 9 17 11 20 32 22 8 | 70 53 65 77 70 63 63
R08 | 949 17 9 19 12 24 13 7 | 64 62 55 63 75 52 60
R09 | 1997 18 17 18 19 23 9 8 | 26 41 37 38 46 31 33
R11 | 1594 14 13 14 17 22 12 7 | 29 39 34 44 52 32 36
R12 | 646 11 13 10 26 27 19 8 | 70 68 66 53 74 47 61
R14 | 689 10 23 10 24 17 15 7 | 52 68 50 43 60 42 51
R15 | 1076 25 13 9 12 22 30 8 | 70 60 54 56 71 38 56
R16 | 1508 26 17 13 13 31 31 10 | 67 59 58 57 69 30 54
R17 | 692 14 11 7 13 13 21 6 | 19 18 21 19 26 20 18
R18 | 771 9 26 11 16 16 15 7 | 19 19 25 22 24 17 18
R19 | 1577 60 51 18 72 37 36 21 | 41 48 48 39 34 47 40
R20 | 1711 46 51 45 83 40 36 22 | 43 69 52 36 37 51 38
R21 | 848 19 10 25 13 21 12 8 | 21 18 38 36 26 19 21
R22 | 2413 13 11 14 17 15 10 6 | 28 35 27 37 35 20 30
R24 | 948 8 7 10 15 16 20 6 | 21 20 27 28 30 18 21
XR26 |12433 28 --- --- 24 50 --- 25 | 25 --- --- 28 60 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1292 25 22 18 30 24 21 |T 45 45 45 45 50 37 41
WRMS | 1292 17 17 17 21 23 21 |NE 45 45 45 45 50 37 41
MEDI | 1076 14 16 14 17 22 18 |MD 43 48 48 41 52 42 40
Table 3.2340.4 GPS week: 2340 Day: 4 MJD: 60628
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1090 52 15 19 27 18 54 15 | 78 62 64 54 53 51 57
R03 | 763 7 13 15 11 14 16 5 | 74 65 75 70 81 63 72
R04 | 892 11 17 15 15 10 19 6 | 67 64 70 65 67 58 65
R05 | 1717 11 7 15 25 12 12 6 | 59 64 59 77 66 53 62
R07 | 922 15 18 14 12 13 22 7 | 73 64 71 78 79 59 70
R08 | 1133 12 13 25 31 13 7 8 | 69 69 80 88 64 70 71
R09 | 1715 18 11 14 19 12 10 6 | 38 46 49 48 49 40 44
R11 | 1932 13 12 15 12 9 10 5 | 58 61 59 64 60 54 58
R12 | 690 15 13 17 18 13 19 7 | 74 70 52 66 75 59 66
R14 | 1114 14 17 13 15 15 12 6 | 63 78 79 73 74 66 71
R15 | 987 17 13 14 22 10 28 7 | 81 76 74 65 75 59 72
R16 | 1130 16 19 23 18 15 20 8 | 66 66 76 74 59 51 63
R17 | 781 9 8 11 18 8 13 5 | 37 38 37 38 39 37 36
R18 | 996 13 31 20 21 24 14 9 | 39 45 45 37 45 44 40
R19 | 1871 45 74 30 73 17 41 20 | 42 68 59 39 56 45 48
R20 | 1585 33 60 47 73 22 32 19 | 58 55 59 49 45 62 48
R21 | 920 12 13 10 13 9 20 5 | 35 38 32 40 35 36 34
R22 | 1919 11 18 10 20 9 13 5 | 58 67 62 71 62 49 63
R24 | 634 12 17 14 15 8 19 6 | 35 32 32 36 33 30 31
XR26 |15417 47 --- --- 59 53 --- 37 | 44 --- --- 41 86 --- 60
------+-----------------------------------------+-------------------------------------
RMS | 1274 21 26 20 30 14 23 |T 57 59 59 58 60 51 56
WRMS | 1274 19 16 17 22 13 23 |NE 57 59 59 58 60 51 56
MEDI | 1090 13 15 15 18 13 19 |MD 58 64 59 64 60 53 60
Table 3.2340.5 GPS week: 2340 Day: 5 MJD: 60629
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 770 45 29 14 32 15 32 12 | 61 41 50 47 43 39 44
R03 | 823 14 9 14 15 9 13 5 | 55 48 60 46 50 45 51
R04 | 872 17 18 12 15 9 34 8 | 63 53 57 54 57 46 55
R05 | 1839 14 12 6 12 16 18 6 | 45 53 51 59 59 39 51
R07 | 781 11 15 15 10 12 21 6 | 59 56 58 49 55 50 54
R08 | 851 10 8 17 16 12 14 6 | 54 54 58 52 57 54 55
R09 | 840 15 17 10 16 10 9 5 | 20 31 35 29 31 25 27
R11 | 1902 17 15 13 15 10 16 6 | 30 31 45 29 39 37 34
R12 | 697 17 13 9 22 11 17 6 | 64 62 64 56 60 55 60
R14 | 787 10 14 13 19 17 12 6 | 47 55 43 47 58 44 48
R15 | 1074 9 11 12 22 19 21 7 | 57 53 61 52 67 47 57
R16 | 810 17 18 13 14 14 24 7 | 52 46 51 47 49 33 45
R17 | 884 6 15 20 13 8 21 6 | 23 29 26 25 23 22 21
R18 | 1151 12 24 16 15 11 21 7 | 22 24 22 21 20 17 17
R19 | 995 35 65 22 78 30 46 20 | 24 35 28 27 24 22 21
R20 | 3308 39 85 40 75 12 41 21 | 43 47 39 52 25 48 27
R21 | 824 16 21 13 23 10 26 8 | 21 24 20 25 20 20 18
R22 | 2400 13 20 16 13 13 9 6 | 68 76 64 64 74 40 68
R24 | 816 18 10 18 17 14 8 6 | 23 23 26 26 27 19 22
XR26 |17014 43 --- --- 43 45 --- 31 | 34 --- --- 34 62 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1360 20 29 17 30 14 23 |T 43 44 45 42 45 36 41
WRMS | 1360 16 17 15 22 12 23 |NE 43 44 45 42 45 36 41
MEDI | 851 15 15 14 16 12 21 |MD 45 47 50 47 49 39 45
Table 3.2340.6 GPS week: 2340 Day: 6 MJD: 60630
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 684 59 29 24 23 13 39 15 | 91 42 54 51 59 44 54
R03 | 419 15 11 19 17 17 12 7 | 76 67 77 67 70 62 69
R04 | 800 18 9 16 26 14 20 8 | 81 68 78 62 70 59 69
R05 | 1297 10 13 23 14 7 20 7 | 65 64 76 59 64 45 62
R07 | 934 12 12 12 12 9 10 5 | 76 73 79 74 73 66 73
R08 | 1365 10 11 14 9 18 15 6 | 67 75 66 66 78 64 69
R09 | 1086 15 22 16 13 11 11 6 | 26 41 36 30 39 32 32
R11 | 1496 14 15 18 17 15 17 7 | 32 45 44 38 42 39 38
R12 | 734 13 14 24 11 9 22 7 | 85 85 92 76 82 71 81
R14 | 848 10 16 12 24 16 16 7 | 70 79 67 61 83 58 70
R15 | 1322 17 10 10 25 25 23 9 | 89 76 80 70 95 62 79
R16 | 828 17 17 9 16 16 12 6 | 77 75 72 66 76 62 71
R17 | 814 7 11 10 13 16 16 5 | 31 27 30 28 30 25 27
R18 | 966 16 20 18 12 11 25 8 | 29 37 32 27 27 24 26
R19 | 1288 33 58 25 63 28 43 18 | 29 39 43 39 40 40 35
R20 | 3094 32 64 55 66 20 20 20 | 49 48 49 58 43 45 44
R21 | 1666 14 20 13 23 11 14 7 | 29 28 27 31 27 23 25
XR22 | 2088 14 11 11 19 10 --- 6 | 74 79 71 78 78 --- 75
R24 | 894 19 15 14 23 16 12 7 | 31 36 39 35 30 29 30
XR26 |14463 45 --- --- 36 52 --- 33 | 37 --- --- 32 90 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 1274 22 25 21 27 16 21 |T 57 57 58 52 59 47 54
WRMS | 1274 17 18 18 27 15 21 |NE 57 57 58 52 59 47 54
MEDI | 966 15 15 16 17 15 16 |MD 65 64 66 58 64 45 58
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