[IGSREPORT-29970] Wk 2320 IGLOS Final Orbits
acc
acc at igs.org
Fri Jul 12 07:16:25 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2320 (Jun 23, 2024 - Jun 29, 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 2.2320.
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:
igl2320[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2320 in the SP3 format.
igl23207.sum Combination Report for GPS Week 2320.
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 | 5.1 ns
1 | 6.3 ns
2 | 12.4 ns
3 | 11.6 ns
4 | 9.2 ns
5 | 14.2 ns
6 | 8.4 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
1 | IAC | R26
2 | IAC | 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 1.2320, 1a.2320).
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 2.2320.0-6)
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 3.2320.0-6).
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 2320 summary. (Jun 23, 2024 - Jun 29, 2024)
Table 1.2320.a GPS week : 2320 MJD: 60484.0-60490.0
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 3 18 -40 26 .10 21 16 | -9774 -3943 4659 42929
| 1 1 2 12 9 31 .05 | 5256 2087
esa n/a| -1 0 0 -32 -26 -13 -.10 32 22 | 155 -3078 4681 41110
| 1 1 1 10 19 29 .04 | 6096 2116
gfz n/a| 0 0 3 24 11 14 -.02 20 14 | 0 -2311 3132 7838
| 1 1 2 11 22 36 .04 | 0 2396
grg n/a| 1 0 2 -36 -4 -48 .42 28 19 | 10181 -2382 3098 8555
| 1 1 1 30 15 37 .05 | 2493 2184
iac n/a| 0 0 -1 9 -2 -9 -.15 17 16 | 3629 -2489 4617 42058
| 1 0 1 24 26 84 .05 | 2807 1457
jgx n/a| 0 0 -10 -19 83 16 -.20 31 29 | 919 -2439 3093 8081
| 1 0 1 17 41 63 .05 | 2641 2227
Table 1.2320.b GPS week : 2320 MJD: 60484.0-60490.0
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 | 18 15 14 18 20 18 16 |
R02 | 12 8 7 6 6 8 9 |
R03 | 7 6 6 7 6 6 6 |
R04 | 9 6 6 7 7 9 6 |
R05 | 11 7 7 7 7 6 6 |
R07 | 7 7 7 6 9 7 7 |
R08 | 7 6 8 6 7 6 6 |
R09 | 6 7 7 7 9 5 6 |
R11 | 6 6 10 7 7 8 5 |
R12 | 6 6 8 7 6 6 8 |
R13 | 12 13 15 17 16 13 13 |
R14 | 5 6 6 4 6 7 7 |
R15 | 7 7 7 8 7 8 6 |
R16 | 7 10 9 8 9 7 8 |
R17 | 6 6 6 7 6 7 5 |
R18 | 7 8 9 8 7 6 8 |
R19 | 15 19 19 22 23 23 23 |
R20 | 28 24 23 23 27 29 31 |
R21 | 6 7 7 8 7 5 7 |
R22 | 7 6 7 7 6 6 7 |
R24 | 5 6 9 7 6 8 6 |
R25 | 10 10 9 11 9 22 16 |
R26 | 36 15 19 33 31 31 34 |
Table 1.2320.c GPS week : 2320 MJD: 60484.0-60490.0
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 2320 0 | 36 63 254 -219 197 8233 80.2 1869 1869 | 5070 0
brd 2320 1 | -16 -13 86 -803 -504 8337 80.2 1747 1747 | 6284 0
brd 2320 2 | -80 114 66 -1672 1050 9218 79.7 1954 1954 | 12411 0
brd 2320 3 | -80 50 41 1195 938 12600 80.1 1904 1904 | 11641 0
brd 2320 4 | -38 24 110 -543 1916 7490 81.4 2121 2121 | 9193 0
brd 2320 5 | -56 35 226 648 1456 944 80.2 1836 1836 | 14248 0
brd 2320 6 | 10 -63 195 193 -263 -682 82.6 1874 1874 | 8380 0
-------------+------------------------------------------------------------+----------------
brd 2320 mean| -32 30 140 -171 684 6591 80.6 1900 1900 | 9603 0
brd 2320 sdev| 44 56 84 954 899 4731 1.0 116 116 | 3337 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 2.2320.0 GPS week: 2320 Day: 0 MJD: 60484
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 8 20 -31 33 .21 20 17 | -2559 -7938 4224 22030
esa n/a| -1 0 2 -19 -1 -25 -.07 32 20 | -2607 -7016 4290 19245
gfz n/a| 1 -1 5 27 30 -31 -.06 18 13 | 0 -6308 3461 7957
grg n/a| 1 2 0 8 -6 -98 .46 36 25 | 7884 -6176 3395 8222
iac n/a| 1 1 -3 8 -8 28 -.11 14 12 | 4420 -4687 4209 21246
jgx n/a| -1 0 -9 -41 41 47 -.14 29 29 | 2522 -6379 3461 8313
Table 2.2320.1 GPS week: 2320 Day: 1 MJD: 60485
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 7 24 -54 59 .12 23 18 | -7513 -3652 4268 31008
esa n/a| 0 -1 0 -36 -25 -20 -.04 25 20 | -5831 -2192 4243 28553
gfz n/a| 2 0 6 37 21 44 .00 19 12 | 0 -2190 3063 7082
grg n/a| 1 0 1 -9 17 -48 .46 29 20 | 6867 -1937 3059 7490
iac n/a| -2 0 -3 -19 -3 -77 -.09 14 13 | 3092 -1430 4160 30008
jgx n/a| 2 1 -10 -39 42 71 -.19 30 30 | -401 -1884 2958 7365
Table 2.2320.2 GPS week: 2320 Day: 2 MJD: 60486
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 2 5 -52 14 .08 23 18 | -6560 -2795 4440 40749
esa n/a| -1 1 0 -18 -44 26 -.16 27 22 | 380 -1884 4477 38759
gfz n/a| -1 0 4 8 -10 57 -.05 19 14 | 0 -521 2702 7018
grg n/a| 0 -1 3 -23 -24 -73 .48 24 17 | 12451 -798 2688 7585
iac n/a| 1 -1 0 -7 55 -31 -.15 17 17 | 5897 -628 4404 39911
jgx n/a| -1 0 -12 -8 67 57 -.28 29 29 | 3319 -628 2609 7386
Table 2.2320.3 GPS week: 2320 Day: 3 MJD: 60487
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -1 1 -1 -33 -33 .10 19 16 | -10263 -4244 4867 53592
esa n/a| 0 -1 1 -36 -23 -21 -.06 36 28 | -1784 -3366 4897 50903
gfz n/a| 1 1 0 17 45 -13 .04 17 14 | 0 -2485 3015 7922
grg n/a| 2 0 2 -51 0 -25 .43 32 20 | 12221 -2466 2961 8303
iac n/a| 0 1 0 4 -6 42 -.20 17 15 | 4640 -3302 4840 52496
jgx n/a| 0 0 -7 7 59 20 -.25 32 32 | 3202 -2871 2995 7959
Table 2.2320.4 GPS week: 2320 Day: 4 MJD: 60488
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 -2 2 25 -39 13 .06 20 15 | -17145 -4354 5753 64035
esa n/a| 0 0 -1 -31 -10 -3 -.13 35 25 | -5603 -3905 5578 62909
gfz n/a| 0 0 2 19 12 2 -.05 26 19 | 0 -2268 3043 7960
grg n/a| 3 1 5 -51 9 12 .35 25 19 | 9900 -2444 2997 8532
iac n/a| 0 0 0 12 -16 -48 -.14 19 19 | -851 -3586 5710 63065
jgx n/a| 1 0 -11 -17 97 38 -.21 31 29 | -1921 -2438 2986 8140
Table 2.2320.5 GPS week: 2320 Day: 5 MJD: 60489
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 35 -31 44 .10 22 14 | -16192 -1046 5796 78873
esa n/a| -4 -1 0 -39 -20 13 -.10 35 21 | 5922 -180 6007 79251
gfz n/a| 2 -1 4 22 -13 54 -.04 19 12 | 0 1325 3349 9003
grg n/a| 0 1 0 -45 -3 -31 .37 25 15 | 13255 775 3314 10081
iac n/a| 1 0 0 8 -18 -116 -.23 20 18 | 968 -2520 5739 77565
jgx n/a| -1 0 -11 -9 123 -5 -.15 32 26 | 2711 620 3316 9186
Table 2.2320.6 GPS week: 2320 Day: 6 MJD: 60490
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 3 17 -37 53 .06 20 17 | -8190 -3578 3266 10220
esa n/a| 0 -1 2 -46 -57 -64 -.14 34 20 | 10611 -3006 3275 8151
gfz n/a| -1 0 4 40 -5 -8 .01 23 13 | 0 -3730 3297 7928
grg n/a| 2 2 2 -82 -20 -77 .38 25 16 | 8693 -3628 3274 9674
iac n/a| -1 0 -1 58 -15 134 -.15 19 17 | 7243 -1276 3261 10121
jgx n/a| 0 0 -11 -25 149 -115 -.19 31 31 | -2995 -3495 3332 8222
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 3.2320.0 GPS week: 2320 Day: 0 MJD: 60484
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1116 35 41 39 59 33 48 18 | 64 59 91 65 68 58 62
XR02E | 1391 12 16 14 60 15 --- 11 | 84 79 77 76 85 --- 79
R03E | 1119 13 9 17 18 17 10 6 | 79 74 73 82 74 74 74
R04E | 2105 15 15 17 47 15 16 9 | 28 19 27 50 31 23 24
R05E | 802 12 14 25 59 14 12 10 | 36 35 40 66 37 36 35
R07E | 1144 13 15 16 32 11 15 7 | 66 66 66 73 59 60 62
R08E | 950 10 21 18 21 12 16 7 | 84 84 84 97 90 81 86
R09 | 1584 14 16 15 17 10 12 6 | 102 103 109 103 96 99 101
R11 | 3998 16 15 11 14 7 11 5 | 33 28 35 31 27 26 27
R12 | 950 20 8 11 17 10 14 6 | 50 57 48 51 51 45 49
R13 | 1330 27 14 22 46 7 46 12 | 72 59 58 64 58 50 58
R14 | 1194 7 14 9 8 7 18 4 | 43 50 43 41 42 31 41
R15 | 1101 13 25 15 12 8 18 6 | 64 84 69 64 61 56 64
R16 | 1160 11 18 9 36 10 14 7 | 74 79 76 61 66 74 70
R17 | 1200 8 19 13 12 10 18 6 | 50 47 47 52 50 44 47
R18 | 1289 13 28 12 15 10 19 7 | 35 54 31 38 33 27 34
R19 | 2721 30 66 20 34 18 28 14 | 93 30 88 94 83 62 76
R20 | 3577 48 97 29 96 28 87 27 | 91 52 89 99 78 64 71
R21 | 1383 14 10 14 16 7 20 6 | 56 51 60 57 54 46 54
R22 | 2848 22 10 17 13 12 17 7 | 28 30 34 37 33 30 29
R24 | 1259 16 14 10 10 9 12 5 | 53 56 49 57 53 51 51
XR25 |16632 16 17 --- --- 10 --- 10 | 10 27 --- --- 18 --- 15
XR26E |16600 54 --- --- 49 47 --- 35 | 34 --- --- 39 287 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1869 20 32 18 36 14 29 |T 57 55 61 63 66 51 54
WRMS | 1869 17 20 13 25 12 29 |NE 56 53 59 60 53 50 52
MEDI | 1289 14 15 15 18 10 16 |MD 56 54 60 61 58 50 54
Table 3.2320.1 GPS week: 2320 Day: 1 MJD: 60485
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1263 37 35 37 28 28 36 15 | 51 55 71 58 55 52 51
XR02E | 2317 15 18 13 21 11 --- 7 | 50 48 47 51 42 --- 45
R03E | 830 13 12 14 16 10 18 6 | 71 67 69 71 67 71 68
R04E | 1053 12 12 14 15 12 17 6 | 26 22 23 36 25 20 21
R05E | 840 18 11 11 15 13 20 6 | 44 37 38 53 39 37 38
R07E | 1915 14 9 16 22 12 13 6 | 47 47 56 53 49 46 49
R08E | 1222 10 10 15 17 11 17 6 | 107 113 113 117 112 110 111
R09 | 1370 17 16 12 16 11 18 6 | 74 70 79 76 64 69 71
R11 | 4005 15 17 7 10 12 17 5 | 22 20 23 21 16 22 18
R12 | 1111 17 7 7 13 16 17 6 | 42 48 39 46 43 41 41
R13 | 1193 32 23 17 47 12 51 13 | 51 45 40 49 40 43 39
R14 | 1676 6 11 11 10 12 22 5 | 31 35 34 34 35 24 31
R15 | 1589 19 19 15 15 12 20 7 | 51 61 50 55 42 49 48
R16 | 943 17 22 28 20 18 23 9 | 52 70 77 44 45 52 54
R17 | 849 8 13 13 18 11 23 6 | 31 32 37 46 25 32 30
R18 | 1524 16 28 16 15 15 20 8 | 23 29 22 35 24 26 22
R19 | 1527 42 69 27 60 21 32 19 | 46 32 42 51 27 32 31
R20 | 1209 58 54 34 82 21 88 24 | 54 40 43 43 36 34 31
R21 | 1024 7 17 20 16 8 24 7 | 32 27 41 43 38 30 33
R22 | 4047 15 8 10 11 10 20 5 | 21 24 30 27 22 38 24
R24 | 835 14 14 15 13 6 19 6 | 35 31 24 39 34 25 29
XR25 |14369 17 11 --- --- 12 --- 9 | 19 18 --- --- 18 --- 15
XR26E |15221 13 --- --- 16 642 --- 15 | 24 --- --- 26 310 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 1747 23 25 19 29 14 30 |T 43 44 47 48 52 42 40
WRMS | 1747 18 20 12 20 13 30 |NE 38 38 41 43 33 36 34
MEDI | 1263 15 14 15 16 12 20 |MD 44 37 41 46 39 37 33
Table 3.2320.2 GPS week: 2320 Day: 2 MJD: 60486
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1058 32 38 32 29 25 33 14 | 54 69 73 51 65 51 56
XR02E | 1107 12 17 13 13 14 --- 7 | 28 33 32 37 27 --- 28
R03E | 1013 14 13 10 12 9 16 5 | 82 78 81 86 84 85 82
R04E | 1195 13 16 11 12 12 20 6 | 28 32 32 39 29 31 29
R05E | 795 18 12 16 13 9 19 6 | 35 36 37 41 32 31 33
R07E | 1910 13 16 12 18 11 22 6 | 38 39 39 43 36 40 37
R08E | 2209 21 17 12 20 13 19 7 | 79 68 79 86 70 78 75
R09 | 944 16 15 11 15 16 23 7 | 108 105 106 99 106 111 104
R11 | 3172 23 17 31 11 20 17 9 | 33 37 39 28 29 36 29
R12 | 1354 13 16 13 11 18 28 7 | 48 41 40 46 46 38 41
R13 | 1209 29 25 20 49 18 52 14 | 64 45 58 53 50 45 50
R14 | 1538 12 8 14 11 19 15 6 | 36 38 39 48 46 37 39
R15 | 1755 12 15 15 11 21 16 7 | 50 46 48 53 48 42 46
R16 | 1121 22 23 19 15 16 21 8 | 57 67 70 65 52 46 58
R17 | 799 15 13 12 10 17 16 6 | 42 42 31 43 30 33 34
R18 | 1792 12 35 21 10 13 15 8 | 29 35 29 31 28 31 26
R19 | 3903 39 74 14 50 26 41 19 | 65 45 54 72 65 47 53
R20 | 2302 60 53 39 58 26 67 22 | 68 43 75 58 59 41 49
R21 | 1230 11 14 16 13 9 24 6 | 49 44 53 51 46 46 47
R22 | 3971 14 14 13 12 17 23 7 | 23 23 39 31 34 36 28
R24 | 985 19 18 16 11 20 26 8 | 42 40 35 36 31 39 32
XR25 |19411 12 13 --- --- 10 --- 8 | 13 23 --- --- 26 --- 19
XR26E |16912 18 --- --- 19 625 --- 18 | 26 --- --- 37 340 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1953 23 27 19 24 17 29 |T 47 46 51 51 59 47 44
WRMS | 1953 18 22 14 17 17 29 |NE 48 44 51 51 46 44 43
MEDI | 1354 15 16 14 13 17 21 |MD 42 41 40 46 46 40 39
Table 3.2320.3 GPS week: 2320 Day: 3 MJD: 60487
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1238 38 57 36 29 24 55 17 | 71 94 85 66 61 75 69
XR02E | 994 10 10 14 16 12 --- 6 | 67 62 74 64 63 --- 65
R03E | 1171 13 15 13 19 14 15 6 | 68 72 70 62 61 72 65
R04E | 1155 8 16 16 19 13 15 6 | 31 28 31 36 30 25 28
R05E | 1177 16 14 15 18 10 23 7 | 55 56 61 53 46 58 52
R07E | 1564 13 13 15 15 10 17 6 | 46 45 52 46 43 52 45
R08E | 2635 8 18 15 15 11 18 6 | 115 118 110 112 120 119 115
R09 | 1491 13 14 16 14 16 17 6 | 50 57 61 49 55 54 53
R11 | 1954 14 13 14 19 19 14 7 | 20 28 27 31 16 30 19
R12 | 956 10 23 12 14 16 16 6 | 35 44 25 25 31 31 29
R13 | 1354 35 36 19 62 15 64 17 | 66 57 57 54 48 55 55
R14 | 1919 8 7 6 9 9 14 4 | 43 38 41 40 39 34 38
R15 | 2009 19 12 18 16 14 21 7 | 53 40 38 52 43 39 42
R16 | 937 17 26 10 11 21 18 8 | 49 50 46 48 64 49 49
R17 | 1172 8 14 14 13 14 25 6 | 42 35 49 43 43 28 39
R18 | 1151 13 41 12 8 15 15 8 | 29 45 26 33 23 23 26
R19 | 3023 24 85 22 79 35 58 22 | 82 45 91 96 91 73 79
R20 | 4779 33 97 23 73 21 64 23 | 63 32 66 80 62 49 52
R21 | 1068 14 15 21 16 9 30 8 | 39 30 46 37 29 36 34
R22 | 1628 17 11 9 14 21 14 6 | 26 26 32 35 31 28 26
R24 | 1269 19 11 15 17 10 21 7 | 42 32 30 31 30 38 31
XR25 |12763 14 13 --- --- 17 --- 11 | 21 27 --- --- 20 --- 15
XR26E |15529 41 --- --- 37 54 --- 32 | 21 --- --- 26 160 --- 20
------+-----------------------------------------+-------------------------------------
RMS | 1904 19 36 17 32 17 32 |T 49 48 53 50 52 48 45
WRMS | 1904 16 28 14 20 15 32 |NE 44 39 45 46 41 40 39
MEDI | 1354 14 14 15 16 15 18 |MD 46 44 49 46 43 39 42
Table 3.2320.4 GPS week: 2320 Day: 4 MJD: 60488
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1059 33 51 67 17 29 55 19 | 59 79 112 72 58 63 66
XR02E | 922 9 11 10 13 11 --- 5 | 57 58 55 57 47 --- 53
R03E | 1427 11 12 15 12 13 15 6 | 81 79 70 80 84 82 78
R04E | 1537 12 16 18 17 15 14 7 | 37 25 40 46 33 31 35
R05E | 1088 11 13 23 18 11 12 6 | 48 51 44 64 57 45 51
R07E | 1151 12 20 19 14 30 17 9 | 84 87 87 80 83 88 82
R08E | 2086 10 18 14 19 14 13 6 | 61 65 64 53 61 52 58
R09 | 1565 22 17 29 17 13 16 8 | 106 113 124 95 104 111 107
R11 | 1585 10 21 14 17 20 13 7 | 27 48 31 31 34 33 31
R12 | 818 12 17 9 14 10 12 5 | 30 37 41 28 40 35 34
R13 | 1051 30 21 26 45 16 66 16 | 65 56 43 52 63 51 54
R14 | 1760 9 11 14 9 16 12 5 | 42 41 35 41 37 31 36
R15 | 2814 15 13 11 13 12 27 7 | 53 49 53 55 40 29 45
R16 | 1677 16 29 25 14 12 24 9 | 59 54 54 66 56 62 55
R17 | 981 10 10 16 10 10 16 5 | 37 34 40 36 29 36 34
R18 | 689 11 32 18 8 13 10 7 | 27 36 25 26 22 26 23
R19 | 1780 45 83 33 52 33 57 22 | 76 33 81 72 79 47 65
R20 | 6696 42 97 48 68 39 64 26 | 72 46 89 94 45 63 60
R21 | 1335 14 14 15 15 16 23 7 | 36 35 39 47 35 40 35
R22 | 1181 13 11 18 11 12 12 6 | 19 26 36 29 32 23 25
R24 | 2086 13 9 14 16 7 18 6 | 50 42 48 44 46 39 44
XR25 | 9996 12 15 --- --- 13 --- 9 | 23 26 --- --- 19 --- 18
XR26E |13943 32 --- --- 38 55 --- 31 | 30 --- --- 30 118 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2120 20 35 26 25 19 31 |T 51 50 57 54 53 49 48
WRMS | 2120 15 25 19 19 19 29 |NE 48 45 52 51 45 44 44
MEDI | 1537 12 16 18 15 13 16 |MD 50 46 48 52 46 40 45
Table 3.2320.5 GPS week: 2320 Day: 5 MJD: 60489
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1072 39 53 42 21 38 39 17 | 60 67 81 66 62 57 60
XR02E | 953 11 13 22 17 15 --- 8 | 97 105 109 94 93 --- 98
R03E | 1081 10 17 11 17 13 13 6 | 76 76 74 74 71 68 72
XR04E | 3413 18 --- 16 17 15 22 9 | 51 --- 47 57 46 50 48
R05E | 2220 10 12 9 13 16 11 5 | 82 94 82 90 84 86 85
R07E | 1087 15 19 15 17 17 13 7 | 99 101 109 108 105 104 104
R08E | 1589 9 16 16 14 12 15 6 | 91 88 83 99 89 82 88
R09 | 920 10 10 9 11 12 10 4 | 125 127 129 129 138 124 129
R11 | 1960 19 21 11 8 22 18 7 | 28 27 25 26 30 26 23
R12 | 726 10 15 10 12 15 7 5 | 43 50 47 42 37 42 42
R13 | 1041 21 20 25 32 22 44 12 | 53 52 72 60 47 52 54
R14 | 1061 8 15 16 14 19 13 6 | 42 50 32 47 35 51 40
R15 | 2739 6 13 11 7 32 21 7 | 57 64 63 54 67 50 57
R16 | 960 14 16 13 10 16 18 6 | 62 66 62 59 57 69 60
R17 | 1015 14 15 12 14 14 20 6 | 36 31 29 37 33 31 31
R18 | 753 7 16 11 14 16 19 6 | 34 35 39 40 36 30 34
R19 | 1034 39 88 42 53 17 61 23 | 55 58 76 62 43 49 53
R20 | 5565 60 96 20 70 33 99 29 | 67 59 47 60 37 55 47
R21 | 1022 7 11 10 9 16 10 5 | 47 51 49 52 37 46 46
R22 | 1280 12 10 16 9 17 13 6 | 39 41 43 44 26 43 37
R24 | 934 16 17 18 19 16 12 7 | 50 46 48 58 45 46 46
XR25 |12482 20 34 --- --- 39 --- 22 | 37 57 --- --- 23 --- 33
XR26E | 9747 31 --- --- 33 60 --- 30 | 24 --- --- 30 78 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 1835 22 35 19 25 20 32 |T 58 64 64 63 57 58 56
WRMS | 1835 14 21 12 15 18 26 |NE 51 54 54 55 46 51 48
MEDI | 1072 14 16 15 14 16 15 |MD 53 58 62 58 46 50 48
Table 3.2320.6 GPS week: 2320 Day: 6 MJD: 60490
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 899 31 39 45 20 23 48 15 | 57 68 90 77 57 62 63
XR02E | 907 11 14 25 14 21 --- 9 | 61 59 63 56 53 --- 57
R03E | 1267 9 13 12 22 14 10 6 | 66 64 71 87 61 72 68
R04E | 1110 9 12 10 16 15 13 5 | 60 63 61 58 62 57 58
R05E | 3507 11 14 15 13 9 12 5 | 64 58 61 67 61 62 61
R07E | 2714 9 14 17 20 16 14 6 | 65 69 73 69 74 67 67
R08E | 1730 8 13 20 15 12 13 6 | 114 114 114 124 106 118 114
R09 | 1210 13 15 11 12 8 12 5 | 157 156 161 154 163 154 157
R11 | 2460 12 10 14 11 11 11 5 | 38 37 34 31 32 38 33
R12 | 846 10 21 18 15 18 18 7 | 56 62 51 55 45 60 53
R13 | 936 14 17 30 53 22 30 13 | 75 73 66 74 59 64 66
R14 | 726 10 13 16 13 20 15 6 | 62 66 54 59 63 57 59
R15 | 1834 8 12 14 16 17 12 6 | 78 85 75 71 75 76 75
R16 | 792 9 24 11 12 25 12 7 | 85 87 88 84 78 86 83
R17 | 978 12 9 11 13 13 12 5 | 61 55 57 61 57 54 57
R18 | 767 10 21 16 26 17 21 8 | 46 60 44 49 47 41 44
R19 | 1099 39 85 43 46 37 57 23 | 103 61 104 105 93 65 87
R20 | 4938 62 103 54 61 26 100 31 | 101 52 101 103 64 62 73
R21 | 947 14 12 12 12 22 15 7 | 60 60 63 67 53 56 58
R22 | 1301 11 12 13 9 24 13 6 | 41 44 37 48 47 49 41
R24 | 752 9 14 15 7 15 16 6 | 64 64 60 64 61 58 60
XR25 |13817 23 14 --- --- 27 --- 16 | 34 44 --- --- 34 --- 35
XR26E | 6953 33 --- --- 36 66 --- 33 | 53 --- --- 66 105 --- 59
------+-----------------------------------------+-------------------------------------
RMS | 1874 20 34 23 25 19 31 |T 69 68 72 74 67 67 66
WRMS | 1874 17 20 13 16 17 31 |NE 70 67 71 73 64 65 65
MEDI | 1110 11 14 15 15 18 13 |MD 62 62 63 67 61 62 60
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