[IGSREPORT-30127] Wk 2334 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 18 04:03:34 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2334 (Sep 29, 2024 - Oct 05, 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 2.2334.
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:
igl2334[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2334 in the SP3 format.
igl23347.sum Combination Report for GPS Week 2334.
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 | 6.5 ns
1 | 7.5 ns
2 | 7.1 ns
3 | 4.4 ns
4 | 7.0 ns
5 | 4.4 ns
6 | 4.1 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 1.2334, 1a.2334).
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 2.2334.0-6)
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 3.2334.0-6).
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 2334 summary. (Sep 29, 2024 - Oct 05, 2024)
Table 1.2334.a GPS week : 2334 MJD: 60582.0-60588.0
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 3 -1 2 49 .15 21 17 | -2238 -678 3823 17523
| 1 0 2 10 16 21 .02 | 1505 1785
esa n/a| 0 0 -2 -28 -16 11 -.03 23 18 | 10675 -278 3027 7113
| 1 1 1 15 8 42 .02 | 3552 1954
gfz n/a| 0 0 4 46 18 -36 -.02 19 14 | 0 -400 3025 7620
| 0 1 1 11 12 24 .05 | 0 1959
grg n/a| 0 0 0 -14 -3 7 .28 22 19 | 2749 -607 3881 17713
| 1 1 1 10 19 52 .04 | 1185 2061
iac n/a| 0 0 -3 26 14 -47 -.20 23 20 | 5488 -698 3769 16660
| 1 1 1 17 22 79 .12 | 1578 1152
jgx n/a| -1 0 -5 -58 -26 42 -.19 27 25 | 2638 -533 3033 7700
| 1 0 2 18 10 21 .06 | 1331 2079
Table 1.2334.b GPS week : 2334 MJD: 60582.0-60588.0
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 11 14 11 14 14 16 |
R02 | 4 7 5 6 5 6 6 |
R03 | 6 6 5 6 8 8 7 |
R04 | 6 7 6 5 6 7 6 |
R05 | 5 6 6 5 6 7 9 |
R07 | 7 5 6 6 6 7 5 |
R08 | 7 8 9 8 7 7 8 |
R09 | 7 6 6 8 6 6 7 |
R11 | 8 6 7 9 6 6 6 |
R12 | 8 7 6 8 9 6 6 |
R14 | 7 7 6 7 6 6 6 |
R15 | 6 7 8 8 7 7 8 |
R16 | 7 7 9 8 10 8 7 |
R17 | 7 6 7 8 10 8 8 |
R18 | 7 8 9 8 9 9 10 |
R19 | 27 25 22 24 22 27 25 |
R20 | 19 18 18 19 20 18 20 |
R21 | 8 8 8 10 8 6 8 |
R22 | 6 6 7 8 7 6 7 |
R24 | 8 7 8 9 9 7 7 |
R25 | 9 12 9 16 15 9 11 |
R26 | 26 38 30 29 34 33 26 |
Table 1.2334.c GPS week : 2334 MJD: 60582.0-60588.0
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 2334 0 | -3 132 161 -471 2302 -3130 82.0 1777 1777 | 6541 0
brd 2334 1 | -83 -35 144 523 621 -1042 80.2 1967 1967 | 7512 0
brd 2334 2 | -35 -77 164 -594 79 -6713 79.4 1863 1863 | 7056 0
brd 2334 3 | 100 -16 157 -643 -592 -4448 78.8 1486 1486 | 4425 0
brd 2334 4 | 33 16 158 -1408 475 -6599 80.9 1603 1603 | 7000 0
brd 2334 5 | -64 43 150 -1354 96 -5274 82.7 1488 1488 | 4379 0
brd 2334 6 | -90 -137 142 -872 716 -3858 82.4 1373 1373 | 4115 0
-------------+------------------------------------------------------------+----------------
brd 2334 mean| -20 -10 154 -688 528 -4437 80.9 1650 1650 | 5861 0
brd 2334 sdev| 69 86 8 648 897 2005 1.5 221 221 | 1484 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 2.2334.0 GPS week: 2334 Day: 0 MJD: 60582
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 6 19 2 60 .14 19 17 | -3242 -1372 4312 17521
esa n/a| 0 0 -3 -13 -28 -21 -.03 25 18 | 8901 544 3351 6888
gfz n/a| 0 2 2 64 27 -29 -.04 21 15 | 0 98 3392 7681
grg n/a| 1 0 -1 -25 -6 -45 .31 21 16 | 3694 -1220 4407 17544
iac n/a| -1 0 -3 4 35 18 -.19 21 24 | 6238 -1641 4223 16314
jgx n/a| 0 1 -5 -62 -34 77 -.22 26 27 | 1032 -125 3373 7683
Table 2.2334.1 GPS week: 2334 Day: 1 MJD: 60583
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 5 -2 30 11 .16 20 16 | -2148 -1425 4040 20952
esa n/a| -1 0 -1 -49 -26 18 -.01 23 15 | 15765 -1144 2988 6645
gfz n/a| 1 0 6 43 9 -24 .00 19 12 | 0 -1697 3000 7887
grg n/a| 0 0 -1 -6 -35 -56 .30 22 18 | 4405 -1733 4166 21255
iac n/a| 1 0 -3 39 45 -4 -.10 18 15 | 7104 -1931 3985 20119
jgx n/a| 0 0 -5 -66 -26 66 -.22 26 27 | 3652 -1700 2999 8001
Table 2.2334.2 GPS week: 2334 Day: 2 MJD: 60584
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 13 76 .14 18 18 | -3242 3265 3949 17715
esa n/a| 0 0 -1 -46 -11 77 -.01 25 21 | 15918 3514 2893 7377
gfz n/a| 1 0 5 29 35 -12 .01 18 16 | 0 3379 2945 7133
grg n/a| 0 -1 0 -3 -22 64 .24 21 21 | 1644 3932 4119 17953
iac n/a| 0 2 -3 37 -6 -183 -.19 18 17 | 5854 1480 3879 16891
jgx n/a| -1 -1 -5 -81 -23 30 -.18 28 26 | 1973 3628 2925 7159
Table 2.2334.3 GPS week: 2334 Day: 3 MJD: 60585
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 4 1 4 52 .16 20 18 | -1825 -1431 3395 15006
esa n/a| 0 0 -3 -11 -5 41 -.02 25 20 | 8957 -1604 2861 6895
gfz n/a| 0 0 5 37 1 -42 .05 20 11 | 0 -1790 2827 7475
grg n/a| 2 0 0 -1 4 10 .24 18 14 | 2451 -2006 3386 15147
iac n/a| -2 2 -4 42 -10 -75 -.48 31 27 | 3984 -581 3357 14240
jgx n/a| -3 0 -9 -78 -16 21 -.31 25 25 | 2474 -2283 2875 7666
Table 2.2334.4 GPS week: 2334 Day: 4 MJD: 60586
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 -7 -23 31 .17 25 19 | 792 -1095 4019 18892
esa n/a| -1 0 -2 -15 -13 -51 -.01 22 19 | 8032 -104 3328 6844
gfz n/a| 0 0 3 55 22 -80 -.02 18 13 | 0 540 3183 7905
grg n/a| 0 1 1 -30 10 54 .23 22 18 | 3679 -552 3993 19164
iac n/a| 1 0 -2 40 -7 36 -.16 24 21 | 7497 -1262 4004 18077
jgx n/a| 0 0 -4 -51 -13 21 -.15 23 23 | 5072 247 3196 8013
Table 2.2334.5 GPS week: 2334 Day: 5 MJD: 60587
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 -14 -8 46 .10 21 16 | -2277 -671 3277 14898
esa n/a| 1 -2 0 -31 -18 -4 -.04 22 18 | 9054 -589 2819 8217
gfz n/a| 0 1 3 52 23 -14 -.07 17 15 | 0 -1029 2833 8273
grg n/a| 0 2 -2 -16 2 59 .32 24 24 | 2112 -1001 3271 15095
iac n/a| 0 0 -2 0 19 -112 -.15 21 18 | 4111 -41 3214 14316
jgx n/a| 0 0 -2 -40 -44 37 -.18 29 24 | 2380 -1274 2854 8368
Table 2.2334.6 GPS week: 2334 Day: 6 MJD: 60588
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 -3 -3 65 .16 24 18 | -3727 -2017 3769 17681
esa n/a| 0 0 0 -27 -11 19 -.07 21 16 | 8102 -2566 2950 6926
gfz n/a| 0 0 4 45 8 -53 -.11 17 16 | 0 -2303 2995 6990
grg n/a| -1 0 0 -14 18 -34 .33 25 18 | 1262 -1672 3825 17833
iac n/a| 0 -3 -4 22 22 -11 -.15 25 22 | 3632 -914 3721 16664
jgx n/a| -1 0 -2 -31 -24 41 -.11 27 21 | 1886 -2230 3009 7013
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 3.2334.0 GPS week: 2334 Day: 0 MJD: 60582
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 900 31 10 21 35 17 49 13 | 31 34 36 23 30 30 26
R02 | 1186 9 11 8 12 7 8 4 | 24 29 23 25 22 23 22
R03 | 3278 9 16 14 11 17 16 6 | 23 31 27 28 23 20 23
R04M | 1626 9 13 14 17 11 14 6 | 30 33 34 29 29 29 29
R05M | 947 8 12 10 11 12 17 5 | 24 23 23 24 23 26 21
R07 | 1177 10 16 11 12 17 24 6 | 25 28 25 27 27 30 24
R08 | 1404 16 13 16 12 20 13 7 | 24 28 27 24 18 22 21
R09 | 3835 14 14 15 11 20 17 7 | 82 90 94 84 89 83 86
R11 | 1068 15 11 21 18 21 10 7 | 49 48 43 34 58 47 44
R12 | 2254 14 15 20 18 20 16 7 | 116 115 110 115 119 104 112
R14M | 960 11 14 12 16 12 24 6 | 100 98 96 99 93 78 94
R15M | 490 14 14 12 11 11 16 6 | 104 85 95 100 94 84 94
R16 | 1053 20 16 16 13 13 17 7 | 131 129 123 120 120 118 123
R17M | 1210 7 24 10 13 19 20 7 | 34 41 36 34 39 30 32
R18M | 893 14 15 14 13 18 23 7 | 37 41 38 40 35 31 34
R19 | 835 38 73 57 60 59 68 26 | 51 52 77 42 62 47 42
R20 | 1870 50 56 47 22 20 34 18 | 51 70 52 40 38 57 39
R21M | 834 9 20 11 15 20 27 8 | 39 36 41 47 47 40 39
R22M | 3206 13 13 10 14 13 17 6 | 26 31 34 30 29 36 28
R24 | 1625 9 19 14 23 18 17 7 | 47 53 46 53 39 49 45
XR25M |12148 12 15 --- --- 13 --- 9 | 28 29 --- --- 25 --- 24
XR26 |12216 29 --- --- 29 50 --- 26 | 50 --- --- 47 65 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1777 19 25 21 21 21 26 |T 51 53 54 50 51 49 47
WRMS | 1777 17 18 15 16 24 27 |NE 54 58 56 50 54 52 50
MEDI | 1186 13 15 14 14 17 17 |MD 37 41 38 40 38 36 34
Table 3.2334.1 GPS week: 2334 Day: 1 MJD: 60583
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1772 26 14 19 30 10 47 11 | 28 32 29 23 30 28 23
R02 | 897 14 13 17 15 10 14 6 | 26 30 22 26 24 26 22
R03 | 1566 9 18 10 10 13 15 5 | 27 32 29 34 22 26 25
R04M | 1162 6 10 8 16 16 26 6 | 21 22 23 22 24 21 19
R05M | 1477 9 12 11 12 17 19 6 | 22 27 27 26 24 23 23
R07 | 1028 12 9 11 15 5 17 5 | 22 24 23 23 22 20 18
R08 | 2985 13 9 10 19 24 20 7 | 26 27 28 34 24 17 24
R09 | 4237 15 8 9 15 11 13 5 | 61 64 70 61 69 59 64
R11 | 1057 13 11 10 21 12 17 6 | 29 33 38 18 36 26 29
R12 | 1377 13 15 13 18 11 25 7 | 119 114 122 120 110 101 114
R14M | 953 11 13 17 16 12 21 6 | 83 79 74 81 81 62 77
R15M | 474 13 12 13 22 15 17 7 | 83 73 83 74 66 66 74
R16 | 1714 20 18 11 20 8 15 7 | 109 113 112 95 100 96 104
R17M | 1547 9 17 14 14 10 17 6 | 29 34 29 31 27 25 27
R18M | 615 26 15 12 13 14 14 7 | 32 34 37 44 28 29 32
R19 | 1837 22 71 54 64 43 70 24 | 39 45 54 33 31 28 27
R20 | 1792 61 46 33 21 34 28 18 | 43 48 36 33 47 36 29
R21M | 1214 10 24 11 22 13 27 8 | 29 33 23 37 29 27 25
R22M | 4193 15 11 16 11 14 15 6 | 22 26 37 33 23 25 25
R24 | 1996 12 16 10 17 15 22 6 | 53 48 43 47 39 54 44
XR25M |13945 15 20 --- --- 13 --- 11 | 19 36 --- --- 22 --- 22
XR26 |11009 44 --- --- 40 66 --- 37 | 41 --- --- 42 48 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 1966 20 23 19 22 18 26 |T 43 46 46 44 42 39 40
WRMS | 1966 16 15 12 18 15 27 |NE 47 50 50 45 46 43 43
MEDI | 1547 13 14 11 17 13 17 |MD 29 34 36 34 29 27 27
Table 3.2334.2 GPS week: 2334 Day: 2 MJD: 60584
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2338 17 22 17 43 23 57 13 | 37 40 38 21 23 46 29
R02 | 1750 8 14 10 12 5 10 4 | 27 26 26 27 18 24 23
R03 | 1390 11 14 10 10 10 15 5 | 26 32 21 28 23 26 22
R04M | 1018 9 12 10 8 20 22 6 | 36 42 38 39 34 37 36
R05M | 2072 10 12 13 20 9 6 5 | 30 26 37 25 22 28 26
R07 | 1335 9 13 14 17 10 19 6 | 31 31 29 40 23 32 28
R08 | 2075 21 11 13 13 27 22 8 | 27 30 36 25 20 31 25
R09 | 2156 14 12 12 10 14 13 5 | 54 59 58 52 54 58 54
R11 | 1768 16 12 12 13 15 18 6 | 45 45 42 35 46 43 41
R12 | 749 7 9 16 12 9 23 6 | 73 71 83 76 77 64 74
R14M | 977 8 10 17 18 15 12 6 | 82 82 73 84 90 74 80
R15M | 783 12 16 11 21 18 23 7 | 86 69 75 97 83 65 79
R16 | 857 15 15 22 27 15 26 9 | 119 117 113 100 115 105 111
R17M | 1655 8 14 11 11 22 26 7 | 34 35 30 36 33 27 30
R18M | 749 17 21 10 25 21 17 8 | 35 38 35 44 29 34 32
R19 | 2393 32 68 43 51 42 66 22 | 45 55 57 38 51 33 38
R20 | 3584 49 62 33 21 13 40 17 | 45 61 49 41 41 48 40
R21M | 813 13 25 15 12 7 25 7 | 35 36 35 38 31 38 31
R22M | 2889 13 13 11 16 19 20 7 | 46 51 46 54 49 56 48
R24 | 2442 14 20 21 11 18 23 8 | 34 36 40 40 31 32 32
XR25M |10923 11 13 --- --- 12 --- 8 | 28 38 --- --- 27 --- 29
XR26 |12874 28 --- --- 32 59 --- 29 | 30 --- --- 37 44 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1862 18 25 18 21 18 28 |T 45 48 48 46 43 45 42
WRMS | 1862 18 21 16 21 17 26 |NE 45 50 49 43 43 45 42
MEDI | 1750 13 14 13 16 15 22 |MD 35 40 38 39 33 37 32
Table 3.2334.3 GPS week: 2334 Day: 3 MJD: 60585
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 923 21 15 17 21 30 40 10 | 36 42 41 41 38 40 36
R02 | 1132 12 18 10 9 16 16 5 | 36 40 36 38 36 42 36
R03 | 732 9 17 11 5 15 17 5 | 45 46 50 45 43 45 45
R04M | 641 6 11 8 5 16 14 4 | 48 48 46 46 53 52 47
R05M | 1336 11 11 10 14 11 12 5 | 38 40 40 46 43 40 40
R07 | 1507 8 8 10 12 16 19 5 | 39 43 40 36 45 43 39
R08 | 669 14 20 12 20 17 23 8 | 43 52 44 40 45 39 41
R09 | 1408 13 18 12 11 32 18 7 | 60 67 67 60 49 54 59
XR11 | 3871 16 20 11 21 21 --- 9 | 51 51 44 39 50 --- 44
R12 | 575 8 22 20 14 23 24 8 | 89 81 100 101 94 72 90
R14M | 564 7 13 15 11 30 17 6 | 84 86 74 83 93 72 80
R15M | 700 12 14 17 7 35 18 7 | 96 82 77 90 104 81 86
R16 | 899 9 22 18 14 29 17 8 | 107 97 110 102 102 92 102
R17M | 1332 8 24 8 14 29 30 8 | 40 41 40 43 47 45 39
R18M | 753 18 24 12 14 18 23 8 | 40 34 34 42 37 33 35
R19 | 2067 57 62 51 48 56 48 24 | 50 49 64 38 61 29 37
R20 | 3517 42 49 35 26 58 45 18 | 52 62 63 49 70 57 46
XR21M | 1004 20 24 14 23 21 --- 10 | 51 58 54 51 49 --- 49
R22M | 2172 16 13 10 20 28 12 7 | 40 42 37 39 41 39 36
R24 | 2120 12 17 22 13 44 16 9 | 48 42 46 46 60 41 43
XR25M |12336 14 15 --- --- 41 --- 16 | 46 42 --- --- 48 --- 41
XR26 |12622 12 --- --- 29 86 --- 28 | 44 --- --- 42 65 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1485 20 25 20 18 31 25 |T 53 54 55 53 57 50 50
WRMS | 1485 18 20 11 14 27 25 |NE 53 56 58 52 58 50 51
MEDI | 1132 12 18 12 14 28 18 |MD 46 48 46 45 49 43 43
Table 3.2334.4 GPS week: 2334 Day: 4 MJD: 60586
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 668 37 24 12 24 30 48 13 | 44 46 45 35 30 38 37
R02 | 857 12 13 10 10 11 15 5 | 26 34 34 30 30 34 29
R03 | 1516 13 9 10 18 30 20 7 | 28 35 32 32 37 35 29
R04M | 719 11 16 14 8 9 12 5 | 30 42 38 26 27 32 31
R05M | 1441 10 17 7 11 13 14 5 | 27 30 27 25 21 32 25
R07 | 2595 10 13 7 14 19 10 5 | 39 40 41 35 34 44 37
R08 | 813 17 8 10 11 25 12 6 | 29 38 31 29 28 35 28
R09 | 1412 14 12 11 10 15 8 5 | 62 59 57 55 55 56 56
R11 | 3955 15 14 11 15 14 9 6 | 50 53 47 40 37 40 44
R12 | 966 8 19 21 12 27 27 9 | 80 74 90 78 95 73 80
R14M | 656 7 13 12 16 11 16 5 | 95 99 95 97 85 93 93
R15M | 1179 15 13 14 12 15 17 6 | 98 86 81 90 89 84 87
R16 | 861 24 27 16 21 28 13 9 | 110 95 89 97 120 99 98
R17M | 633 8 23 15 21 29 32 10 | 35 32 39 42 45 29 33
R18M | 505 24 20 13 17 29 13 8 | 50 51 47 58 52 46 48
R19 | 2026 48 62 42 51 44 50 22 | 46 53 69 44 55 45 42
R20 | 1981 74 21 39 52 35 30 20 | 42 51 74 81 40 60 50
R21M | 1327 8 24 11 16 22 19 7 | 157 148 166 161 156 151 158
R22M | 1901 16 14 16 15 9 21 7 | 40 46 46 43 28 39 38
R24 | 1644 10 20 20 20 15 23 8 | 36 38 41 37 30 34 33
XR25M |18389 25 11 --- --- 26 --- 15 | 105 88 --- --- 74 --- 89
XR26 |13663 27 --- --- 35 73 --- 33 | 31 --- --- 34 41 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1602 25 22 18 22 24 23 |T 57 58 59 55 54 54 54
WRMS | 1602 18 19 13 18 21 23 |NE 47 51 54 48 48 49 45
MEDI | 1327 14 16 12 16 22 16 |MD 42 51 46 42 40 40 38
Table 3.2334.5 GPS week: 2334 Day: 5 MJD: 60587
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 936 25 27 19 32 35 51 14 | 31 30 41 26 32 33 27
R02 | 815 9 16 20 13 10 10 6 | 16 26 16 16 18 21 15
R03 | 2373 12 16 9 32 13 17 7 | 20 28 16 26 23 22 17
R04M | 862 11 15 15 10 17 17 6 | 21 23 30 24 30 21 22
R05M | 820 14 16 10 15 19 8 6 | 26 31 23 18 25 21 19
R07 | 1961 12 18 12 19 18 13 7 | 22 24 19 32 25 22 19
R08 | 815 11 15 12 17 19 10 6 | 24 25 23 28 34 31 23
R09 | 1441 12 11 13 13 13 13 5 | 59 63 66 58 67 62 62
R11 | 3356 12 15 13 18 12 14 6 | 36 41 34 27 37 32 34
R12 | 869 14 12 10 11 12 14 5 | 66 61 55 53 54 55 56
R14M | 962 10 13 14 13 18 16 6 | 127 131 130 125 125 118 126
R15M | 1024 11 18 9 15 13 23 6 | 67 61 64 64 69 52 62
R16 | 858 18 25 11 18 20 16 8 | 111 113 109 100 100 106 106
R17M | 492 6 21 13 20 10 26 7 | 32 36 35 38 30 32 31
R18M | 864 21 20 13 17 27 19 8 | 117 120 122 123 113 117 118
R19 | 1612 55 55 49 68 46 89 26 | 50 63 69 39 40 52 43
R20 | 1253 52 38 22 33 40 47 17 | 48 58 62 55 43 69 51
R21M | 1411 11 14 13 14 11 22 6 | 269 262 267 266 273 256 266
R22M | 1752 13 13 15 12 14 11 6 | 30 31 40 40 34 34 33
R24 | 2026 15 16 9 11 15 23 6 | 36 41 34 36 39 37 34
XR25M | 8956 14 10 --- --- 12 --- 8 | 150 154 --- --- 167 --- 155
XR26 |11153 39 --- --- 27 62 --- 32 | 18 --- --- 35 24 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1487 21 22 17 24 21 29 |T 62 67 62 58 63 59 61
WRMS | 1487 16 18 15 24 18 24 |NE 41 47 45 40 41 45 39
MEDI | 1024 12 16 13 17 15 16 |MD 36 41 40 38 37 34 34
Table 3.2334.6 GPS week: 2334 Day: 6 MJD: 60588
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 611 36 22 16 42 36 59 16 | 34 45 42 34 28 46 35
R02 | 1004 13 13 8 13 13 13 5 | 24 26 23 27 23 23 22
R03 | 1279 15 16 13 17 15 16 6 | 23 31 24 26 23 23 22
R04M | 842 14 13 11 14 20 8 6 | 149 148 144 143 151 144 146
R05M | 941 15 11 17 13 39 8 8 | 79 80 83 73 79 73 77
R07 | 1616 13 13 8 8 10 13 5 | 31 28 26 30 33 30 28
R08 | 1329 10 9 17 18 29 16 7 | 33 33 39 33 33 38 32
R09 | 911 16 12 17 19 20 7 7 | 81 85 86 82 86 80 82
R11 | 2528 11 12 14 14 13 8 5 | 46 53 48 44 48 40 46
R12 | 656 9 11 9 16 16 19 6 | 90 86 83 81 94 73 84
R14M | 1802 17 14 14 12 12 12 6 | 172 171 163 171 167 169 168
R15M | 996 12 21 22 14 11 23 8 | 103 96 109 101 107 87 100
R16 | 819 18 17 13 17 14 17 7 | 121 113 117 109 117 108 113
R17M | 758 10 16 21 9 13 25 7 | 42 40 43 46 45 38 39
R18M | 995 17 22 20 15 33 17 9 | 156 157 154 152 158 155 154
R19 | 1737 59 56 31 73 47 62 24 | 54 62 72 52 60 46 47
R20 | 1641 58 39 29 40 50 56 20 | 53 76 63 60 51 76 55
R21M | 1078 7 15 24 14 11 26 8 | 409 420 412 415 409 404 413
R22M | 2001 15 15 11 13 24 16 7 | 32 34 40 44 47 33 35
R24 | 1924 12 16 15 11 16 23 7 | 46 42 43 47 48 44 42
XR25M |15132 14 10 --- --- 22 --- 11 | 215 220 --- --- 220 --- 218
XR26 |10901 22 --- --- 27 55 --- 25 | 43 --- --- 43 56 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 1373 24 21 17 24 25 27 |T 92 97 90 86 94 86 91
WRMS | 1373 18 16 16 18 22 21 |NE 52 56 55 51 53 52 50
MEDI | 1078 14 15 15 14 16 16 |MD 53 76 63 52 56 46 47
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