[IGSREPORT-29394] Wk 2267 IGLOS Final Orbits
acc
acc at igs.org
Sun Jul 9 23:24:55 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2267 (Jun 18, 2023 - Jun 24, 2023)
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 2.2267.
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:
igl2267[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2267 in the SP3 format.
igl22677.sum Combination Report for GPS Week 2267.
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. The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
3. 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).
4. 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
5. 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 | -13.1 ns
1 | -11.2 ns
2 | -8.9 ns
3 | -12.5 ns
4 | 0.4 ns
5 | -10.5 ns
6 | -12.1 ns
6. 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 | ESA | R20
1 | ESA | R20
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 1.2267, 1a.2267).
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 2.2267.0-6)
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 3.2267.0-6).
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 2267 summary. (Jun 18, 2023 - Jun 24, 2023)
Table 1.2267.a GPS week : 2267 MJD: 60113.0-60119.0
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 1 7 -26 11 .01 21 16 | 16130 -728 2854 8765
| 0 0 1 10 16 22 .03 | 4607 1015
esa n/a| -1 0 0 -13 -6 -4 -.19 37 22 | -8283 178 2865 7285
| 1 1 0 14 14 14 .02 | 5870 1134
gfz n/a| -1 0 1 35 7 21 -.20 22 16 | 0 -844 2887 8341
| 1 1 2 11 9 27 .04 | 0 1512
grg n/a| 3 0 -3 -28 20 -39 .30 21 17 | -9432 -941 2890 7838
| 1 1 1 9 15 33 .02 | 4426 1353
iac n/a| -1 0 -2 10 18 10 -.21 23 20 | -6982 -697 2848 8801
| 1 1 2 23 39 68 .05 | 4732 613
Table 1.2267.b GPS week : 2267 MJD: 60113.0-60119.0
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 | 20 21 24 23 26 25 25 |
R02 | 7 13 8 8 8 9 8 |
R03 | 8 10 9 8 7 7 8 |
R04 | 7 9 8 10 8 12 7 |
R05 | 10 9 10 9 9 8 10 |
R07 | 8 10 9 9 9 10 9 |
R08 | 8 10 14 9 8 10 10 |
R09 | 9 9 7 8 9 9 10 |
R11 | 6 7 6 8 6 6 7 |
R12 | 6 8 8 7 9 7 8 |
R13 | 19 14 16 19 15 17 21 |
R14 | 8 8 8 7 6 6 8 |
R15 | 5 7 11 10 10 6 10 |
R16 | 23 21 21 21 22 24 26 |
R17 | 7 7 7 6 8 6 7 |
R18 | 9 7 9 12 9 6 7 |
R19 | 27 24 29 27 25 23 27 |
R20 | 24 28 37 35 41 28 27 |
R21 | 8 5 6 7 6 6 9 |
R22 | 7 6 8 7 7 7 7 |
R24 | 9 11 7 9 8 10 11 |
R25 | 16 15 9 11 12 12 13 |
Table 1.2267.c GPS week : 2267 MJD: 60113.0-60119.0
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 2267 0 | 48 -6 296 -568 -80 -647 80.2 1169 1169 | -13057 0
brd 2267 1 | 35 82 280 -1101 -886 -1361 79.4 1321 1321 | -11194 0
brd 2267 2 | 10 1 370 -1294 -1862 -1585 79.3 1350 1350 | -8924 0
brd 2267 3 | -13 -8 320 -534 -3544 -1623 80.8 1471 1471 | -12454 0
brd 2267 4 | 8 -6 348 319 -1674 -1450 80.1 1379 1379 | 378 0
brd 2267 5 | 20 0 284 -222 -3949 -1370 80.0 1337 1337 | -10461 0
brd 2267 6 | 73 120 257 -1012 -1799 3000 80.7 1512 1512 | -12135 0
-------------+------------------------------------------------------------+----------------
brd 2267 mean| 26 26 308 -630 -1970 -719 80.1 1362 1362 | -9692 0
brd 2267 sdev| 29 52 40 561 1370 1672 .6 111 111 | 4650 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 2.2267.0 GPS week: 2267 Day: 0 MJD: 60113
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 3 -2 -12 -15 .02 19 14 | 13641 -2197 2595 8915
esa n/a| -2 0 0 -23 -10 -13 -.21 44 23 | 669 -750 2603 8068
gfz n/a| 0 2 1 27 -3 -1 -.26 19 13 | 0 -2846 2632 8725
grg n/a| 3 0 -2 -20 31 10 .32 20 15 | -11834 -2777 2621 8259
iac n/a| -2 0 1 39 11 36 -.23 22 19 | -10778 -504 2591 9157
Table 2.2267.1 GPS week: 2267 Day: 1 MJD: 60114
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 -42 4 -.03 20 16 | 14122 -339 3110 9009
esa n/a| -2 2 0 -14 9 14 -.21 43 24 | -7062 256 3128 8273
gfz n/a| -2 0 1 50 0 -13 -.21 24 17 | 0 344 3151 8649
grg n/a| 3 0 -1 -33 26 -9 .27 16 12 | -11285 -265 3146 8142
iac n/a| -2 0 1 24 -2 91 -.23 22 18 | -8521 -866 3101 9151
Table 2.2267.2 GPS week: 2267 Day: 2 MJD: 60115
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 -11 -3 22 .01 25 20 | 17155 -1466 2626 8009
esa n/a| -2 0 0 6 -15 -19 -.18 37 24 | -8404 -94 2630 6153
gfz n/a| -2 1 5 50 6 45 -.22 22 19 | 0 -978 2622 7329
grg n/a| 5 0 -4 -30 -7 -64 .30 21 18 | -8600 -1211 2655 6856
iac n/a| -1 0 -2 -29 95 99 -.15 24 20 | -6130 -667 2607 7976
Table 2.2267.3 GPS week: 2267 Day: 3 MJD: 60116
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -1 2 17 -31 0 .03 18 14 | 12621 -814 2826 8822
esa n/a| -1 -2 0 -38 4 8 -.19 38 23 | -13441 -965 2851 7046
gfz n/a| -3 1 0 28 1 33 -.16 24 18 | 0 -2515 2859 8196
grg n/a| 6 1 -5 -23 23 -53 .29 23 18 | -11742 -2013 2876 7658
iac n/a| -1 -1 -2 14 22 -43 -.17 23 20 | -9673 -1603 2827 8704
Table 2.2267.4 GPS week: 2267 Day: 4 MJD: 60117
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 15 -48 52 .04 21 16 | 26097 -167 2808 9135
esa n/a| -2 0 0 -12 -1 0 -.16 37 20 | -2428 1162 2819 7381
gfz n/a| 0 0 1 25 23 -2 -.14 20 15 | 0 336 2851 8733
grg n/a| 4 1 -1 -19 20 -73 .29 25 22 | 282 -72 2828 8275
iac n/a| 0 0 -5 -11 -1 -78 -.19 23 21 | 3230 -441 2804 9149
Table 2.2267.5 GPS week: 2267 Day: 5 MJD: 60118
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 3 11 -19 17 -.02 23 18 | 14563 969 2971 8464
esa n/a| 0 0 0 -1 -31 0 -.20 30 19 | -11872 2178 2963 7267
gfz n/a| -1 0 1 38 16 57 -.20 24 16 | 0 1115 3011 8018
grg n/a| 1 0 -1 -28 8 -67 .27 17 16 | -11300 1261 3021 7782
iac n/a| 0 0 -1 24 32 0 -.30 22 20 | -7911 352 2957 8392
Table 2.2267.6 GPS week: 2267 Day: 6 MJD: 60119
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 0 11 -29 -4 .04 21 15 | 14713 -1088 3045 9005
esa n/a| 0 0 1 -9 1 -25 -.20 32 24 | -15448 -535 3063 6811
gfz n/a| 0 0 -2 25 3 30 -.23 24 15 | 0 -1367 3083 8742
grg n/a| 3 0 -2 -46 41 -15 .33 22 19 | -11551 -1516 3085 7900
iac n/a| -2 2 -6 9 -30 -33 -.20 23 21 | -9097 -1151 3054 9083
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 3.2267.0 GPS week: 2267 Day: 0 MJD: 60113
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1187 38 58 19 22 37 19 | 104 105 105 104 98 100
R02 | 643 14 12 9 12 25 7 | 74 60 75 68 79 69
R03 | 1422 12 22 10 11 26 7 | 109 100 110 112 119 108
R04 | 1295 13 12 8 11 16 6 | 72 61 64 65 62 65
R05 | 1107 10 16 15 25 18 10 | 64 55 64 51 52 57
R07 | 1251 12 27 9 11 20 8 | 97 86 101 103 107 97
R08 | 638 10 18 9 17 22 8 | 95 86 101 106 109 97
R09M | 2024 13 22 16 8 13 8 | 17 37 30 25 28 23
R11 | 1848 10 14 11 9 19 6 | 27 26 31 24 29 25
R12 | 912 9 17 7 9 11 6 | 62 68 55 59 62 59
R13 | 1144 30 52 17 31 33 18 | 103 76 90 78 90 86
R14 | 1014 13 22 11 8 16 7 | 64 77 63 68 65 66
R15 | 1095 10 10 8 8 14 5 | 83 80 81 79 76 80
R16 | 599 27 41 55 22 30 22 | 88 89 96 91 97 90
R17 | 1192 12 15 10 10 19 6 | 30 28 29 29 23 28
R18 | 691 15 23 14 8 19 8 | 28 29 33 31 22 29
R19 | 953 35 77 21 53 19 26 | 41 48 43 42 41 38
R20 | 1043 29 150 37 35 39 24 | 64 60 70 82 66 76
R21 | 1118 9 20 13 10 11 7 | 41 43 49 48 44 45
R22 | 1010 13 10 15 8 10 7 | 25 27 38 35 29 31
R24 | 1250 16 17 12 15 19 8 | 38 32 36 34 29 33
XR25 |13254 11 21 --- --- 27 15 | 24 24 --- --- 27 21
------+------------------------------------+--------------------------------
RMS | 1169 19 44 19 20 22 |T 61 58 64 63 61 60
WRMS | 1169 14 23 13 15 19 |NE 63 60 66 65 63 61
MEDI | 1107 13 20 12 11 19 |MD 64 60 64 65 62 59
Table 3.2267.1 GPS week: 2267 Day: 1 MJD: 60114
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 974 42 53 22 26 27 20 | 86 104 98 99 96 94
R02 | 621 12 23 34 15 11 12 | 54 48 83 61 57 60
R03 | 2503 9 28 18 15 15 10 | 109 100 116 119 113 111
R04 | 1162 20 12 17 9 16 8 | 64 49 47 58 52 53
R05 | 916 13 13 14 18 11 8 | 52 47 48 43 42 45
R07 | 1358 14 24 12 17 25 9 | 85 75 82 92 89 83
R08 | 516 16 18 13 17 24 9 | 81 78 78 83 74 80
R09M | 1136 13 26 18 6 14 9 | 16 31 27 20 22 19
R11 | 1608 10 15 15 8 11 7 | 21 27 32 23 23 24
R12 | 848 8 21 17 11 12 8 | 44 56 50 42 40 45
R13 | 1328 20 32 26 18 32 13 | 71 69 72 70 53 68
R14 | 660 8 21 17 10 15 8 | 43 52 40 47 46 43
R15 | 1466 14 10 15 8 20 7 | 52 51 45 51 41 49
R16 | 769 22 34 61 17 21 20 | 57 58 56 58 54 57
R17 | 1867 14 11 10 13 16 7 | 23 24 29 22 21 21
R18 | 953 16 18 7 7 16 7 | 21 23 21 21 19 20
R19 | 1016 43 69 21 32 27 24 | 27 25 29 25 19 22
R20 | 2290 35 153 52 29 48 27 | 51 75 32 35 56 40
R21 | 907 9 11 10 7 12 5 | 32 38 28 39 32 33
R22 | 1321 9 6 13 8 26 5 | 17 18 24 22 31 18
R24 | 1389 25 20 20 10 14 11 | 24 23 30 26 15 20
XR25 |14736 11 18 --- --- 29 14 | 22 22 --- --- 23 19
------+------------------------------------+--------------------------------
RMS | 1320 20 43 24 16 22 |T 47 49 50 50 46 46
WRMS | 1320 16 24 17 12 18 |NE 49 50 52 51 47 47
MEDI | 1136 14 20 17 13 16 |MD 44 48 45 43 41 43
Table 3.2267.2 GPS week: 2267 Day: 2 MJD: 60115
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 699 51 59 28 26 22 24 | 102 99 88 101 96 92
R02 | 649 10 20 10 16 11 8 | 64 51 61 69 58 61
R03 | 2943 8 24 13 17 19 9 | 116 117 129 118 130 119
R04 | 1444 18 15 12 11 15 8 | 60 43 58 53 53 52
R05 | 710 16 9 18 18 20 9 | 59 49 62 51 41 53
R07 | 1056 10 18 15 19 27 9 | 124 121 123 129 140 124
R08 | 614 24 21 29 18 14 13 | 118 124 139 140 129 130
R09M | 675 12 12 13 8 29 6 | 19 30 30 23 24 23
R11 | 2050 6 18 9 7 21 6 | 25 28 31 26 38 26
R12 | 844 12 15 15 10 14 7 | 53 60 48 54 50 52
R13 | 1791 22 27 33 26 24 16 | 74 70 79 61 73 68
R14 | 698 9 22 9 14 10 8 | 60 75 60 58 60 61
R15 | 976 21 17 23 12 20 11 | 72 69 62 64 67 64
R16 | 1343 21 32 55 25 38 21 | 72 67 80 72 63 72
R17 | 1833 15 14 11 10 20 7 | 33 34 40 42 26 36
R18 | 1292 14 25 11 14 17 9 | 31 35 31 40 32 32
R19 | 1331 57 63 27 53 24 29 | 33 32 47 36 34 31
R20 | 1432 53 125 24 44 55 37 | 43 65 54 40 35 38
R21 | 828 13 7 10 7 8 5 | 30 30 34 35 24 31
R22 | 1474 12 8 19 9 19 7 | 28 33 45 34 33 32
R24 | 1028 15 10 11 11 24 7 | 42 37 40 45 26 41
XR25 |19401 7 11 --- --- 19 9 | 23 25 --- --- 26 22
------+------------------------------------+--------------------------------
RMS | 1349 25 37 22 21 24 |T 58 58 63 61 57 57
WRMS | 1349 20 24 19 18 20 |NE 60 60 65 63 58 58
MEDI | 1056 14 18 15 14 20 |MD 53 49 58 53 41 52
Table 3.2267.3 GPS week: 2267 Day: 3 MJD: 60116
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 596 44 56 22 35 44 23 | 65 83 55 57 71 56
R02 | 600 12 14 14 12 16 7 | 65 51 62 55 63 59
R03 | 3051 7 22 9 16 18 8 | 85 81 84 85 87 83
R04 | 1416 10 13 16 26 19 10 | 58 53 66 43 53 53
R05 | 1268 9 18 21 15 12 9 | 60 48 69 54 52 57
R07 | 1369 11 18 21 14 17 9 | 75 68 93 75 82 77
R08 | 1048 8 22 19 13 19 8 | 73 76 85 77 83 77
R09M | 821 11 16 17 12 18 8 | 18 27 19 22 24 19
R11 | 3251 11 13 15 16 12 8 | 24 22 21 31 27 21
R12 | 588 4 21 13 8 16 7 | 39 46 32 39 30 37
R13 | 1486 21 39 37 35 22 19 | 71 50 65 62 65 61
R14 | 838 7 17 11 11 21 6 | 46 58 51 44 39 48
R15 | 793 16 15 22 13 13 10 | 60 54 37 53 54 50
R16 | 731 21 20 59 26 28 20 | 69 58 59 64 74 63
R17 | 1360 5 11 13 12 10 6 | 25 22 27 29 25 24
R18 | 1471 11 37 14 17 19 11 | 21 29 24 30 22 20
R19 | 1856 32 66 34 59 19 27 | 31 30 38 22 29 26
R20 | 1186 34 123 37 36 56 34 | 42 41 45 44 34 34
R21 | 663 12 9 10 12 15 6 | 30 29 28 31 30 27
R22 | 1614 11 13 12 11 17 6 | 19 26 28 32 23 23
R24 | 1108 15 24 12 11 12 9 | 26 26 20 36 25 24
XR25 |18425 7 15 --- --- 17 10 | 24 18 --- --- 21 19
------+------------------------------------+--------------------------------
RMS | 1470 18 38 24 23 23 |T 46 45 48 46 46 43
WRMS | 1470 14 23 18 18 20 |NE 48 46 49 48 47 44
MEDI | 1186 11 18 16 14 17 |MD 42 46 45 44 34 37
Table 3.2267.4 GPS week: 2267 Day: 4 MJD: 60117
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 511 52 47 28 51 38 26 | 102 100 106 106 102 99
R02 | 1209 13 10 11 20 12 8 | 56 47 55 52 51 51
R03 | 1176 12 15 8 11 23 6 | 118 110 121 120 125 117
R04 | 836 15 10 10 17 17 8 | 54 45 49 48 52 48
R05 | 1285 14 10 17 19 20 9 | 51 47 59 44 57 49
R07 | 1755 14 18 14 16 19 9 | 115 109 113 112 111 112
R08 | 1174 9 20 15 13 18 8 | 118 119 123 128 122 122
R09M | 2038 14 17 16 14 20 9 | 20 31 22 28 22 22
R11 | 3586 12 12 9 7 26 6 | 28 33 30 30 28 28
R12 | 745 9 15 19 13 16 8 | 51 50 34 54 40 45
R13 | 792 25 46 12 13 26 14 | 81 47 58 73 65 64
R14 | 955 6 8 9 13 31 5 | 56 53 53 49 35 52
R15 | 857 12 13 17 21 15 9 | 60 57 70 57 57 60
R16 | 647 27 27 53 32 37 21 | 68 59 57 51 75 58
R17 | 1348 5 16 15 13 14 7 | 29 24 35 31 27 29
R18 | 1059 14 22 12 15 16 9 | 23 23 26 32 22 24
R19 | 1195 33 69 26 43 21 24 | 39 31 35 33 28 30
R20 | 1116 38 127 41 65 30 40 | 62 60 52 32 37 46
R21 | 1046 7 16 9 8 14 6 | 20 20 21 27 21 21
R22 | 1500 11 5 12 13 26 6 | 22 24 31 29 33 24
R24 | 891 17 15 7 12 10 7 | 35 31 26 30 19 28
XR25 |10585 9 15 --- --- 15 12 | 16 20 --- --- 20 14
------+------------------------------------+--------------------------------
RMS | 1379 21 37 20 25 23 |T 55 51 56 55 52 51
WRMS | 1379 16 20 15 22 21 |NE 57 52 57 56 53 53
MEDI | 1116 13 15 14 14 19 |MD 51 47 52 48 37 46
Table 3.2267.5 GPS week: 2267 Day: 5 MJD: 60118
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 649 59 48 29 34 27 25 | 68 76 63 83 69 67
R02 | 1673 12 12 14 18 18 8 | 49 47 51 51 42 48
R03 | 1136 11 12 12 10 8 6 | 64 61 54 69 60 62
R04 | 891 21 16 29 10 17 11 | 53 48 42 47 49 44
R05 | 1178 14 12 11 14 23 7 | 52 50 46 44 59 45
R07 | 2216 14 25 19 15 14 10 | 81 62 74 78 75 73
R08 | 746 9 22 18 14 19 9 | 82 77 80 77 75 78
R09M | 2115 12 16 20 12 23 9 | 20 30 25 27 23 23
R11 | 3126 11 14 11 8 23 6 | 37 42 38 32 36 35
R12 | 661 12 15 12 9 13 7 | 57 70 69 58 59 62
R13 | 1046 28 37 27 26 39 16 | 72 55 58 65 78 59
R14 | 600 11 12 8 9 25 5 | 64 69 72 62 60 65
R15 | 1044 9 14 11 9 10 6 | 68 69 80 79 73 74
R16 | 892 26 32 67 26 30 23 | 71 77 89 70 79 73
R17 | 967 11 9 11 9 13 6 | 38 43 43 34 34 38
R18 | 1088 12 9 12 7 17 5 | 40 32 40 39 29 37
R19 | 971 34 64 29 27 35 22 | 40 32 32 31 35 33
R20 | 920 48 80 33 33 34 28 | 44 49 50 54 40 46
R21 | 888 8 12 15 7 14 6 | 28 24 26 30 31 26
R22 | 1410 14 10 15 7 20 6 | 32 33 34 36 40 32
R24 | 797 24 11 19 14 16 10 | 37 41 29 44 34 36
XR25 |11234 10 14 --- --- 16 12 | 42 35 --- --- 47 38
------+------------------------------------+--------------------------------
RMS | 1336 23 30 24 17 22 |T 51 51 52 52 51 49
WRMS | 1336 18 19 16 16 20 |NE 53 52 53 54 52 51
MEDI | 971 12 14 15 12 18 |MD 49 48 50 51 47 45
Table 3.2267.6 GPS week: 2267 Day: 6 MJD: 60119
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 975 47 52 31 39 35 24 | 87 94 76 96 86 80
R02 | 1504 12 18 14 12 17 8 | 57 50 59 54 55 54
R03 | 952 8 14 16 15 20 8 | 81 74 87 84 77 81
R04 | 819 14 14 8 13 20 7 | 57 46 40 54 47 48
R05 | 798 16 11 21 17 19 9 | 54 56 60 56 65 55
R07 | 1599 16 19 9 15 16 8 | 94 77 86 85 90 85
R08 | 627 10 17 22 17 21 9 | 94 85 100 90 94 91
R09M | 2162 14 22 15 16 26 9 | 25 43 38 26 33 29
R11 | 2293 10 11 14 12 16 7 | 34 25 29 30 31 28
R12 | 684 12 18 14 9 18 7 | 71 81 64 67 63 69
R13 | 864 34 34 40 38 27 21 | 97 71 73 78 86 78
R14 | 675 8 24 12 9 22 8 | 70 84 69 68 62 70
R15 | 1370 15 18 13 19 31 9 | 85 91 84 84 79 84
R16 | 894 26 41 71 24 25 25 | 88 99 112 94 94 96
R17 | 1113 8 11 9 14 16 6 | 38 38 42 37 34 38
R18 | 965 10 17 11 10 17 7 | 33 31 31 34 30 31
R19 | 932 35 80 23 41 40 27 | 47 51 50 42 51 40
R20 | 3361 38 75 32 37 31 26 | 65 48 61 60 56 54
R21 | 1098 8 18 16 18 17 9 | 32 30 29 39 32 30
R22 | 2828 10 11 9 16 16 7 | 38 37 38 46 35 39
R24 | 1345 17 18 22 14 22 10 | 42 50 55 43 35 43
XR25 |12886 10 16 --- --- 28 12 | 32 28 --- --- 30 28
------+------------------------------------+--------------------------------
RMS | 1512 21 32 24 22 23 |T 60 58 61 60 57 56
WRMS | 1512 15 24 15 19 21 |NE 61 59 62 62 58 58
MEDI | 975 12 18 15 16 20 |MD 57 50 60 56 55 54
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