[IGSREPORT-29373] Wk 2265 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 26 07:39:23 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2265 (Jun 04, 2023 - Jun 10, 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 2.2265.
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:
igl2265[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2265 in the SP3 format.
igl22657.sum Combination Report for GPS Week 2265.
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 | -9.7 ns
1 | -7.2 ns
2 | -8.4 ns
3 | -7.4 ns
4 | -8.2 ns
5 | -12.1 ns
6 | -8.1 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
----+--------+---------------
1 | ESA | R20
3 | ESA | R20
6 | 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 1.2265, 1a.2265).
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 2.2265.0-6)
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 3.2265.0-6).
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 2265 summary. (Jun 04, 2023 - Jun 10, 2023)
Table 1.2265.a GPS week : 2265 MJD: 60099.0-60105.0
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 1 -3 -27 21 .04 19 16 | 17974 -25 2818 9049
| 0 0 1 9 15 21 .02 | 2237 1258
esa n/a| -2 0 -2 -13 5 -7 -.19 41 24 | -8649 995 2924 7081
| 1 0 2 14 13 18 .03 | 3661 1307
gfz n/a| 0 1 2 28 6 -19 -.20 22 13 | 0 281 2924 8278
| 1 1 2 20 17 20 .05 | 0 1138
grg n/a| 3 0 -3 -17 29 -18 .29 23 19 | -8954 75 2921 7741
| 1 0 2 22 20 29 .03 | 1573 1054
iac n/a| -1 2 -2 -6 -1 -19 -.21 23 21 | -6610 -704 2913 9157
| 1 1 3 22 53 60 .06 | 1854 556
Table 1.2265.b GPS week : 2265 MJD: 60099.0-60105.0
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 | 25 21 21 20 21 23 22 |
R02 | 8 8 7 8 6 7 6 |
R03 | 7 7 9 11 7 7 7 |
R04 | 7 10 8 10 8 10 7 |
R05 | 8 8 8 7 8 9 8 |
R07 | 10 7 7 7 6 7 10 |
R08 | 9 8 8 7 7 9 8 |
R09 | 10 10 9 11 13 12 9 |
R11 | 8 11 8 8 8 8 8 |
R12 | 9 7 6 8 7 8 10 |
R13 | 19 17 18 20 23 24 19 |
R14 | 9 8 9 6 6 5 7 |
R15 | 10 8 8 7 6 8 8 |
R16 | 21 19 21 23 21 27 23 |
R17 | 8 9 7 5 7 6 5 |
R18 | 8 10 10 6 7 7 8 |
R19 | 26 28 26 22 26 27 27 |
R20 | 39 16 37 30 34 36 26 |
R21 | 10 9 10 7 8 8 7 |
R22 | 10 7 8 9 6 9 7 |
R24 | 7 8 10 10 7 8 10 |
R25 | 11 15 15 15 14 9 12 |
Table 1.2265.c GPS week : 2265 MJD: 60099.0-60105.0
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 2265 0 | -56 -50 228 -707 -667 -7046 84.4 1662 1662 | -9656 0
brd 2265 1 | 55 20 317 288 -4 -6833 82.2 1616 1616 | -7197 0
brd 2265 2 | 8 -109 288 -526 -390 2816 83.0 1802 1802 | -8413 0
brd 2265 3 | 94 -12 302 -202 545 3847 80.8 1686 1686 | -7415 0
brd 2265 4 | 80 49 339 428 1550 4337 80.6 2053 2053 | -8232 0
brd 2265 5 | 60 57 177 -162 333 5432 79.7 1978 1978 | -12119 0
brd 2265 6 | 10 -38 304 849 1119 -248 79.5 1867 1867 | -8087 0
-------------+------------------------------------------------------------+----------------
brd 2265 mean| 36 -11 279 -4 355 329 81.5 1809 1809 | -8731 0
brd 2265 sdev| 52 59 56 552 793 5270 1.8 166 166 | 1692 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 2.2265.0 GPS week: 2265 Day: 0 MJD: 60099
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 -15 -11 8 .05 22 17 | 14242 1785 2697 9089
esa n/a| -4 0 0 12 21 -12 -.18 39 23 | -12535 2717 2899 6578
gfz n/a| 1 0 5 23 -31 -6 -.15 23 13 | 0 1887 2829 8870
grg n/a| 5 0 -7 -6 32 -30 .28 24 24 | -10728 1607 2842 8474
iac n/a| -2 1 4 -36 29 -34 -.18 25 26 | -7626 -928 2880 9760
Table 2.2265.1 GPS week: 2265 Day: 1 MJD: 60100
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 2 -25 21 .06 16 13 | 19432 739 2748 9041
esa n/a| -2 0 0 -5 6 -6 -.24 44 28 | -5958 1616 2893 8280
gfz n/a| 0 0 4 -11 0 -45 -.17 19 12 | 0 1139 2910 8273
grg n/a| 4 1 -4 22 50 26 .33 25 20 | -7790 610 2895 7899
iac n/a| -1 1 -3 24 84 -6 -.10 21 19 | -4925 -54 2902 9197
Table 2.2265.2 GPS week: 2265 Day: 2 MJD: 60101
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 3 -54 48 .06 17 16 | 18626 -1832 3149 9555
esa n/a| -3 0 -4 -29 12 -6 -.18 41 25 | -9334 -600 3131 7067
gfz n/a| 1 0 2 22 13 -14 -.22 22 14 | 0 -1464 3122 8884
grg n/a| 2 1 -2 -9 58 -61 .30 24 20 | -7901 -1336 3146 8231
iac n/a| -2 1 -3 -8 -11 57 -.19 23 21 | -5988 -1316 3126 9501
Table 2.2265.3 GPS week: 2265 Day: 3 MJD: 60102
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 -33 53 .01 18 15 | 19507 407 3136 8974
esa n/a| -3 0 -5 -27 -4 -45 -.16 46 24 | -9621 2035 3258 6912
gfz n/a| 0 2 2 51 16 -45 -.17 22 14 | 0 510 3301 8496
grg n/a| 2 0 -1 -38 34 6 .24 20 16 | -7768 453 3263 8148
iac n/a| 0 2 -4 -30 5 -76 -.29 23 21 | -4897 -1338 3225 9435
Table 2.2265.4 GPS week: 2265 Day: 4 MJD: 60103
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 -8 -11 10 .05 18 15 | 19958 -445 2607 9397
esa n/a| 0 0 -2 -9 -18 2 -.20 40 26 | -3504 721 2903 6779
gfz n/a| 0 1 4 36 17 4 -.30 24 16 | 0 277 2900 8175
grg n/a| 1 0 -3 -14 13 -27 .29 21 16 | -8470 79 2911 7713
iac n/a| -1 0 0 13 6 -59 -.24 23 20 | -6353 77 2897 9311
Table 2.2265.5 GPS week: 2265 Day: 5 MJD: 60104
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 -3 -21 7 .02 20 15 | 15372 -1339 2749 9267
esa n/a| 0 0 0 -18 11 8 -.19 39 23 | -13511 -776 2737 7409
gfz n/a| -1 1 -2 36 16 -4 -.24 25 13 | 0 -869 2752 8352
grg n/a| 3 0 -4 -41 3 -34 .25 25 17 | -11649 -1271 2750 7529
iac n/a| -2 2 -6 7 -43 -80 -.23 23 23 | -10249 -708 2737 9144
Table 2.2265.6 GPS week: 2265 Day: 6 MJD: 60105
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 4 9 -34 1 .04 21 16 | 18681 507 2641 8021
esa n/a| 0 0 -1 -14 12 9 -.18 42 22 | -6081 1258 2652 6548
gfz n/a| 1 0 0 41 10 -27 -.17 21 12 | 0 487 2657 6899
grg n/a| 4 0 0 -35 12 -5 .31 23 20 | -8372 387 2646 6194
iac n/a| -1 3 -4 -15 -82 62 -.27 23 21 | -6232 -664 2630 7755
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 3.2265.0 GPS week: 2265 Day: 0 MJD: 60099
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1128 52 67 24 22 41 25 | 99 39 76 65 90 69
R02 | 1570 8 19 10 15 16 7 | 77 65 76 83 79 75
R03 | 733 8 14 11 13 21 6 | 82 74 85 87 90 82
R04 | 935 16 8 9 13 16 7 | 75 65 61 57 63 64
R05 | 1472 9 6 13 18 16 7 | 66 62 69 56 59 62
R07 | 712 11 16 22 15 21 9 | 73 64 90 68 77 74
R08 | 956 16 18 14 16 23 9 | 63 61 78 75 83 69
R09 | 4041 13 26 15 15 14 9 | 36 50 40 31 31 36
R11 | 2604 13 12 14 16 20 8 | 72 69 81 69 78 72
R12 | 599 11 19 15 16 27 8 | 66 81 77 64 60 70
R13 | 1901 17 52 36 20 30 18 | 102 71 119 86 87 94
R14 | 2084 12 16 15 19 30 9 | 68 77 68 70 78 68
R15 | 1885 20 10 17 15 35 9 | 79 72 67 64 83 69
R16 | 1624 24 32 52 23 26 20 | 75 70 92 78 73 77
R17 | 884 12 9 11 19 17 8 | 30 27 32 30 35 28
R18 | 657 9 10 18 11 12 7 | 26 31 30 28 27 25
R19 | 1908 39 50 21 64 22 26 | 47 40 50 49 44 44
R20 | 1368 52 123 46 47 43 39 | 52 71 81 60 58 61
R21 | 1180 13 24 16 14 18 9 | 33 39 37 43 32 36
XR22 | 8254 --- 12 14 14 46 9 | --- 115 109 107 106 109
R24 | 856 9 20 10 11 25 7 | 33 30 27 29 28 27
XR25 |25620 8 15 --- --- 37 11 | 23 27 --- --- 29 24
------+------------------------------------+--------------------------------
RMS | 1661 22 39 23 24 25 |T 60 59 68 61 63 60
WRMS | 1661 17 23 13 24 26 |NE 60 59 68 61 63 60
MEDI | 1368 13 16 15 16 22 |MD 66 64 76 64 63 68
Table 3.2265.1 GPS week: 2265 Day: 1 MJD: 60100
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 829 30 64 17 23 16 20 | 64 35 59 72 52 55
R02 | 1090 11 23 6 16 12 8 | 53 38 48 54 46 48
R03 | 768 10 16 7 15 14 7 | 60 61 61 68 61 61
R04 | 802 10 14 7 31 21 9 | 60 66 62 45 62 58
R05 | 1440 8 9 15 19 19 7 | 51 45 59 43 46 50
R07 | 925 7 11 13 17 15 7 | 59 59 63 67 63 61
R08 | 836 15 12 7 17 26 7 | 46 55 49 60 64 50
R09 | 2908 13 24 14 20 21 10 | 28 37 28 20 21 25
R11 | 3671 13 20 25 12 19 10 | 44 39 59 46 50 45
R12 | 924 10 18 11 10 33 7 | 47 65 61 53 44 54
R13 | 1704 20 41 27 28 22 16 | 73 59 86 52 53 66
R14 | 1974 15 9 15 16 21 8 | 51 55 64 48 57 53
R15 | 1835 14 12 13 16 21 8 | 55 54 52 45 59 50
R16 | 1638 20 29 47 25 22 19 | 56 46 59 58 50 53
R17 | 700 3 16 19 19 13 8 | 21 22 27 22 19 20
R18 | 549 9 24 12 22 13 9 | 21 20 21 28 21 17
R19 | 1509 36 55 24 74 26 27 | 45 31 42 22 26 35
R20 | 1684 22 159 23 22 36 16 | 49 54 47 37 25 43
R21 | 1368 10 25 14 14 18 9 | 21 25 20 28 20 20
XR22 | 7425 --- 11 10 8 19 7 | --- 71 62 66 61 65
R24 | 1442 14 18 10 9 12 7 | 27 25 30 27 18 26
XR25 |23460 10 19 --- --- 41 14 | 22 28 --- --- 27 22
------+------------------------------------+--------------------------------
RMS | 1616 16 44 19 25 21 |T 45 45 50 45 42 44
WRMS | 1616 13 28 12 20 19 |NE 45 45 50 45 42 44
MEDI | 1440 13 18 14 17 19 |MD 49 45 59 46 46 50
Table 3.2265.2 GPS week: 2265 Day: 2 MJD: 60101
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 646 25 72 26 22 33 20 | 73 41 82 62 40 66
R02 | 892 10 14 10 12 19 6 | 57 48 55 66 42 57
R03 | 723 9 27 5 20 16 9 | 63 46 61 79 68 64
R04 | 946 10 12 12 19 13 8 | 55 56 55 48 50 52
R05 | 1193 9 14 14 17 22 7 | 50 61 60 46 49 52
R07 | 1157 8 18 9 11 24 6 | 68 50 63 69 79 64
R08 | 904 13 10 14 13 20 7 | 56 58 74 69 71 64
R09 | 2466 12 22 18 13 14 9 | 35 45 35 34 45 34
R11 | 4055 14 12 13 11 17 7 | 63 64 76 58 72 64
R12 | 1038 7 13 8 11 23 5 | 53 55 48 52 38 51
R13 | 598 28 51 28 23 26 18 | 85 56 74 75 63 71
R14 | 1499 10 11 23 15 15 9 | 58 56 80 55 60 62
R15 | 1169 9 16 15 14 18 7 | 56 55 64 55 58 56
R16 | 1465 24 30 56 23 31 21 | 62 54 62 64 73 60
R17 | 587 9 11 16 12 15 7 | 24 25 30 25 22 24
R18 | 531 10 33 8 20 31 10 | 25 31 30 34 21 26
R19 | 1053 41 59 19 57 34 26 | 44 49 43 50 32 42
R20 | 1526 21 128 46 62 31 36 | 44 37 49 44 42 42
R21 | 871 12 28 18 14 11 10 | 25 27 32 39 28 29
XR22 | 4073 --- 19 7 8 24 8 | --- 118 116 110 113 114
R24 | 4914 22 20 11 12 28 10 | 32 31 24 32 23 26
XR25 |18305 10 21 --- --- 20 14 | 29 30 --- --- 26 26
------+------------------------------------+--------------------------------
RMS | 1801 17 41 22 24 23 |T 50 49 57 55 50 52
WRMS | 1801 16 25 14 20 21 |NE 50 49 57 55 50 52
MEDI | 1053 10 19 14 14 20 |MD 55 49 60 55 45 52
Table 3.2265.3 GPS week: 2265 Day: 3 MJD: 60102
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1006 32 61 21 24 31 20 | 83 32 79 55 49 62
R02 | 602 10 22 8 14 21 8 | 66 57 73 75 75 68
R03 | 1220 16 27 7 20 22 10 | 65 55 77 89 78 73
R04 | 681 16 13 21 13 14 9 | 63 52 40 60 47 53
R05 | 873 12 16 10 10 21 6 | 55 61 50 54 43 54
R07 | 712 9 19 12 9 24 7 | 71 54 72 67 81 66
R08 | 738 8 17 12 12 37 7 | 68 57 63 70 89 64
R09 | 2210 15 29 17 13 16 10 | 18 35 21 30 25 21
R11 | 3295 9 12 18 15 14 8 | 46 47 37 55 42 45
R12 | 1588 10 11 16 15 17 8 | 55 55 61 50 45 54
R13 | 742 28 53 33 24 23 19 | 97 60 92 78 88 81
R14 | 1143 8 14 10 8 14 5 | 57 58 55 60 55 57
R15 | 862 8 16 14 12 17 7 | 60 58 74 61 51 62
R16 | 1662 26 28 62 27 30 22 | 60 57 67 53 53 57
R17 | 680 6 12 6 9 12 4 | 23 22 20 29 19 22
R18 | 689 12 13 8 8 18 6 | 22 22 22 25 18 22
R19 | 1076 32 61 30 35 28 22 | 31 27 36 33 29 22
R20 | 4530 31 162 35 53 38 29 | 50 60 45 37 29 31
R21 | 1227 13 20 8 5 14 6 | 20 25 32 25 20 24
XR22 | 2303 --- 18 9 9 17 8 | --- 80 85 85 82 83
R24 | 1991 19 14 18 14 19 9 | 28 23 24 26 27 22
XR25 |16170 11 20 --- --- 22 15 | 20 20 --- --- 21 16
------+------------------------------------+--------------------------------
RMS | 1686 18 46 22 20 23 |T 50 46 53 53 48 48
WRMS | 1686 15 24 14 16 21 |NE 50 46 53 53 48 48
MEDI | 1076 12 18 14 13 19 |MD 55 54 55 55 45 54
Table 3.2265.4 GPS week: 2265 Day: 4 MJD: 60103
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1361 36 72 20 15 29 21 | 80 34 64 61 52 60
R02 | 516 7 18 12 7 26 6 | 63 51 71 59 55 62
R03 | 1517 9 19 12 11 22 7 | 68 58 79 73 55 70
R04 | 510 13 14 13 11 20 7 | 58 56 55 63 45 57
R05 | 541 11 9 20 12 16 8 | 54 47 46 58 54 51
R07 | 951 7 20 5 11 16 6 | 69 61 66 66 73 65
R08 | 892 11 11 12 12 16 7 | 67 62 70 68 73 66
R09 | 2790 16 37 20 17 30 12 | 33 42 37 25 38 29
R11 | 4771 8 12 19 11 13 7 | 58 54 52 59 58 55
R12 | 1232 9 15 11 11 19 6 | 52 58 55 56 52 54
R13 | 1131 31 49 40 42 37 23 | 86 57 91 52 93 70
R14 | 705 7 17 8 8 23 5 | 54 62 54 55 70 55
R15 | 1083 8 9 10 10 19 5 | 59 50 62 56 66 56
R16 | 1899 23 32 60 21 29 21 | 59 53 57 52 49 54
R17 | 961 10 12 14 8 18 6 | 27 24 30 26 18 23
R18 | 626 8 11 14 12 25 6 | 24 22 27 28 23 23
R19 | 993 35 82 24 42 29 26 | 40 41 53 41 29 42
R20 | 5658 26 111 47 53 26 33 | 47 37 41 37 29 33
R21 | 985 5 18 19 13 14 8 | 21 23 23 31 20 22
XR22 | 2705 --- 8 9 9 29 6 | --- 115 114 118 113 116
R24 | 1928 12 15 10 9 21 6 | 25 28 30 24 19 23
XR25 |20072 9 21 --- --- 15 14 | 35 25 --- --- 26 31
------+------------------------------------+--------------------------------
RMS | 2053 18 40 24 21 23 |T 51 48 56 52 50 50
WRMS | 2053 15 26 16 16 20 |NE 51 48 56 52 50 50
MEDI | 1083 10 17 14 11 21 |MD 54 50 55 56 52 54
Table 3.2265.5 GPS week: 2265 Day: 5 MJD: 60104
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 866 46 58 21 29 31 22 | 68 35 47 42 39 45
R02 | 599 13 15 11 10 20 7 | 50 38 42 46 34 43
R03 | 1512 9 12 11 17 19 7 | 53 50 50 67 42 54
R04 | 707 19 14 13 18 24 9 | 51 41 37 47 32 43
R05 | 896 13 14 17 15 30 8 | 47 43 54 58 35 50
R07 | 860 8 19 9 12 29 7 | 64 53 63 63 80 61
R08 | 1386 17 12 20 10 20 9 | 55 62 74 65 66 63
R09 | 2834 15 28 20 20 25 11 | 24 35 31 25 27 23
R11 | 2221 10 10 18 15 18 8 | 100 101 101 102 107 100
R12 | 890 7 18 12 15 28 7 | 53 60 47 51 70 51
R13 | 1729 33 48 38 45 21 23 | 81 49 61 57 64 61
R14 | 1066 6 11 6 10 16 4 | 52 55 50 51 51 51
R15 | 1231 12 17 13 10 19 7 | 62 69 61 67 61 63
R16 | 1524 26 38 70 37 37 27 | 60 57 79 47 58 59
R17 | 1318 8 8 10 11 15 5 | 22 25 22 28 21 23
R18 | 639 12 19 4 9 16 6 | 21 23 21 22 16 21
R19 | 1645 38 66 25 58 26 27 | 31 52 45 40 21 34
R20 | 6491 18 123 45 49 21 35 | 39 44 57 40 29 30
R21 | 994 9 13 13 16 15 7 | 23 22 24 28 22 22
XR22 | 2389 --- 18 8 11 15 8 | --- 201 193 187 188 192
R24 | 1098 15 19 12 11 19 8 | 23 25 31 25 18 23
XR25 |16968 6 12 --- --- 21 9 | 22 29 --- --- 23 22
------+------------------------------------+--------------------------------
RMS | 1978 20 39 25 25 23 |T 47 53 56 55 50 51
WRMS | 1978 15 23 13 17 23 |NE 47 53 56 55 50 51
MEDI | 1231 13 17 13 15 20 |MD 51 44 50 47 35 45
Table 3.2265.6 GPS week: 2265 Day: 6 MJD: 60105
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 816 36 55 26 29 25 21 | 99 43 87 66 68 74
R02 | 787 8 11 7 11 12 5 | 72 56 66 69 61 66
R03 | 889 12 12 11 11 16 7 | 78 63 73 84 68 74
R04 | 700 14 8 11 11 23 6 | 73 67 57 61 55 64
R05 | 825 12 10 11 19 16 8 | 71 63 67 68 58 66
R07 | 936 14 26 7 20 19 10 | 91 69 84 97 99 85
R08 | 1742 13 12 17 14 40 8 | 84 79 95 91 114 87
R09 | 3870 16 17 14 14 22 9 | 36 41 36 29 28 32
R11 | 2081 10 9 17 15 21 8 | 113 112 120 112 122 114
R12 | 561 13 20 16 16 18 9 | 76 82 65 66 68 70
R13 | 1180 34 41 21 31 32 18 | 104 69 86 78 94 82
R14 | 673 10 14 10 10 15 6 | 73 81 69 80 74 75
R15 | 1020 14 10 14 12 12 7 | 86 79 80 78 81 80
R16 | 1183 26 36 58 24 25 22 | 77 64 74 61 72 67
R17 | 1589 8 9 6 9 13 5 | 28 25 25 29 25 26
R18 | 761 12 21 7 10 20 7 | 26 25 24 27 27 24
R19 | 1889 41 52 18 64 20 26 | 38 39 41 40 34 35
R20 | 5470 31 155 37 38 45 25 | 52 62 63 56 44 59
R21 | 839 15 12 12 10 25 7 | 29 26 36 33 27 29
XR22 | 1779 --- 9 10 11 16 7 | --- 215 209 205 205 209
R24 | 1157 23 8 18 11 19 9 | 30 29 40 34 28 31
XR25 |18430 10 13 --- --- 20 11 | 28 33 --- --- 26 29
------+------------------------------------+--------------------------------
RMS | 1867 21 42 21 23 23 |T 64 64 71 69 67 67
WRMS | 1867 16 22 12 20 21 |NE 64 64 71 69 67 67
MEDI | 1020 14 12 14 14 20 |MD 73 63 67 66 61 66
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