[IGSREPORT-29417] Wk 2268 IGLOS Final Orbits [Resubmission]
acc
acc at igs.org
Mon Jul 24 10:27:11 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2268 (Jun 25, 2023 - Jul 01, 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 2.2268.
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:
igl2268[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2268 in the SP3 format.
igl22687.sum Combination Report for GPS Week 2268.
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 | -8.1 ns
1 | -11.1 ns
2 | -11.0 ns
3 | -8.6 ns
4 | -10.1 ns
5 | -6.9 ns
6 | -9.3 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 | ALL | R17
2 | ALL | R17
3 | GFZ | R17
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 1.2268, 1a.2268).
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 2.2268.0-6)
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 3.2268.0-6).
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 2268 summary. (Jun 25, 2023 - Jul 01, 2023)
Table 1.2268.a GPS week : 2268 MJD: 60120.0-60126.0
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 2 11 -16 9 .02 20 16 | 15091 -1353 3212 9630
| 1 0 0 8 8 26 .02 | 1773 1453
esa n/a| -2 0 1 -10 -4 4 -.18 34 22 | -13489 117 3110 7779
| 0 1 1 15 7 18 .05 | 9364 1460
gfz n/a| -1 0 -1 33 3 6 -.21 22 16 | 0 -1095 3052 8210
| 1 0 1 17 7 19 .04 | 0 1498
grg n/a| 4 0 -2 -40 20 -29 .33 24 19 | -8704 -1372 3149 7757
| 1 1 2 11 9 33 .04 | 1685 1257
iac n/a| 0 0 -7 14 24 -22 -.20 24 22 | -7004 -842 3212 9274
| 1 1 1 30 33 95 .05 | 1586 1297
Table 1.2268.b GPS week : 2268 MJD: 60120.0-60126.0
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 | 21 19 21 21 23 23 23 |
R02 | 8 6 10 10 7 7 10 |
R03 | 10 7 9 9 9 7 8 |
R04 | 9 7 9 10 9 7 6 |
R05 | 10 10 8 9 9 11 7 |
R07 | 11 8 9 11 8 8 10 |
R08 | 11 7 9 8 12 9 7 |
R09 | 8 7 10 6 7 9 7 |
R11 | 10 7 8 9 8 7 6 |
R12 | 7 7 8 6 8 8 7 |
R13 | 20 21 17 17 22 15 18 |
R14 | 5 6 7 8 6 7 7 |
R15 | 9 7 6 7 9 8 6 |
R16 | 23 25 20 24 23 21 23 |
R17 | 6 --- --- 15 7 7 6 |
R18 | 13 8 7 10 10 9 6 |
R19 | 27 26 26 27 31 24 22 |
R20 | 32 37 34 37 34 36 29 |
R21 | 7 6 7 8 9 8 7 |
R22 | 7 10 7 7 6 7 7 |
R24 | 7 6 8 6 14 8 7 |
R25 | 10 16 11 14 8 9 11 |
Table 1.2268.c GPS week : 2268 MJD: 60120.0-60126.0
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 2268 0 | 14 -13 275 -286 1114 6014 81.0 1519 1519 | -8052 0
brd 2268 1 | -36 -10 232 -1594 419 7337 79.0 1406 1406 | -11067 0
brd 2268 2 | -4 62 339 -1776 131 3564 79.4 1336 1336 | -11017 0
brd 2268 3 | 93 -58 384 376 -1236 686 79.5 1199 1199 | -8610 0
brd 2268 4 | 80 -55 279 11 331 2206 81.8 1288 1288 | -10124 0
brd 2268 5 | 32 59 328 -1054 -855 4407 80.9 1442 1442 | -6890 0
brd 2268 6 | 43 36 300 -190 383 6326 80.9 1542 1542 | -9296 0
-------------+------------------------------------------------------------+----------------
brd 2268 mean| 31 2 305 -644 41 4362 80.4 1390 1390 | -9293 0
brd 2268 sdev| 45 50 49 832 810 2388 1.0 124 124 | 1559 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 2.2268.0 GPS week: 2268 Day: 0 MJD: 60120
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 13 -12 38 .03 18 15 | 17712 -1422 3043 8279
esa n/a| -2 2 2 -8 -11 6 -.20 37 23 | -14878 139 3061 5951
gfz n/a| 0 1 0 25 -1 -6 -.19 24 18 | 0 -1365 3061 7680
grg n/a| 2 -1 -1 -48 8 -83 .30 23 17 | -7609 -1059 3053 7649
iac n/a| 0 0 -6 -34 -14 -59 -.24 19 18 | -5888 -967 3042 8276
Table 2.2268.1 GPS week: 2268 Day: 1 MJD: 60121
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 2 17 -20 3 .06 17 15 | 14437 -1071 3410 8647
esa n/a| -1 0 1 -19 -1 -16 -.22 37 24 | -9825 168 3390 6507
gfz n/a| -1 0 -1 3 11 10 -.19 21 11 | 0 -345 3470 7966
grg n/a| 5 -1 -3 -27 20 -9 .31 27 19 | -10722 -922 3459 7403
iac n/a| 0 0 -5 36 68 -21 -.12 23 22 | -8773 -133 3376 8421
Table 2.2268.2 GPS week: 2268 Day: 2 MJD: 60122
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 0 3 16 -11 -17 .01 23 17 | 13651 -409 2731 10385
esa n/a| -3 0 3 -21 -4 -13 -.25 34 23 | -32106 1109 2729 8477
gfz n/a| -1 0 1 28 11 35 -.20 20 13 | 0 -572 2750 9069
grg n/a| 3 1 -5 -37 13 11 .31 20 14 | -11033 -569 2772 8265
iac n/a| -1 0 -6 47 7 -71 -.22 23 21 | -8687 -1268 2705 9831
Table 2.2268.3 GPS week: 2268 Day: 3 MJD: 60123
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 10 -31 -30 -.01 24 19 | 17247 -2090 3871 10717
esa n/a| -2 0 1 22 -8 3 -.14 35 23 | -13297 536 3180 8358
gfz n/a| -2 1 -2 31 -5 16 -.22 23 13 | 0 -342 3239 8043
grg n/a| 5 0 -1 -41 28 -4 .37 21 16 | -7185 -2212 3892 8107
iac n/a| -2 0 -8 -10 -18 -64 -.22 24 22 | -5093 -2514 3873 10061
Table 2.2268.4 GPS week: 2268 Day: 4 MJD: 60124
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 18 -6 12 .04 22 16 | 14220 -4212 2780 11112
esa n/a| -1 0 0 -16 9 37 -.16 33 19 | -8904 -2841 2794 8626
gfz n/a| -1 0 -3 41 -3 4 -.20 23 18 | 0 -4374 2797 8234
grg n/a| 4 0 0 -28 29 -63 .35 27 24 | -8352 -3875 2829 7496
iac n/a| 0 1 -5 26 35 -139 -.14 22 24 | -7932 -2232 2866 10353
Table 2.2268.5 GPS week: 2268 Day: 5 MJD: 60125
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 10 -10 42 .02 16 15 | 15292 -48 3567 8391
esa n/a| -1 0 1 -20 0 2 -.18 34 19 | -13889 -93 3576 7529
gfz n/a| 0 1 -1 48 0 -27 -.17 21 24 | 0 -545 2951 7239
grg n/a| 4 1 -5 -58 31 -24 .31 27 25 | -6794 -547 2925 6959
iac n/a| 1 1 -9 0 36 44 -.24 26 23 | -5219 131 3565 8167
Table 2.2268.6 GPS week: 2268 Day: 6 MJD: 60126
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 -5 -24 14 .02 19 15 | 13080 -225 3087 9885
esa n/a| -1 0 0 -9 -9 15 -.11 31 22 | -1530 1802 3042 9007
gfz n/a| -1 0 -1 56 10 15 -.28 21 17 | 0 -125 3098 9239
grg n/a| 2 0 0 -45 14 -34 .39 19 15 | -9233 -426 3118 8425
iac n/a| -2 1 -9 37 57 154 -.24 28 24 | -7438 1088 3061 9810
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 3.2268.0 GPS week: 2268 Day: 0 MJD: 60120
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 897 37 56 22 31 23 21 | 109 50 93 63 69 80
R02 | 1224 10 12 12 17 12 7 | 88 89 86 82 91 85
R03 | 678 11 17 23 15 13 9 | 102 85 107 90 100 96
R04 | 1551 11 15 12 20 16 8 | 90 86 82 79 75 83
R05 | 709 13 11 16 26 12 10 | 87 83 79 71 79 79
R07 | 1393 12 23 19 23 21 11 | 101 80 106 92 94 95
R08 | 644 15 23 19 22 25 11 | 97 92 114 115 113 104
R09 | 2617 11 16 14 12 21 7 | 18 23 33 27 36 22
R11 | 2116 12 17 26 10 13 10 | 20 24 38 25 27 23
R12 | 676 9 19 10 10 15 7 | 56 58 52 55 54 54
R13 | 807 28 34 36 41 32 20 | 63 36 52 37 56 45
R14 | 697 5 9 8 9 20 4 | 36 44 38 38 33 38
R15 | 1380 10 17 21 16 13 9 | 62 70 61 66 63 63
R16 | 1049 25 33 66 20 22 23 | 69 76 75 63 68 69
R17 | 888 12 8 5 10 10 5 | 85 48 9999 85 90 64
R18 | 931 14 33 24 21 21 13 | 71 80 70 70 71 71
R19 | 1203 36 75 27 50 18 27 | 119 83 107 110 117 105
R20 | 3509 23 113 32 42 29 31 | 128 78 128 131 114 118
R21 | 1370 5 14 14 12 16 6 | 86 90 95 89 88 89
R22 | 2510 9 12 12 12 20 6 | 55 64 62 56 57 58
R24 | 928 13 19 9 8 11 7 | 90 85 90 86 90 88
XR25 |10811 6 15 --- --- 26 10 | 48 48 --- --- 49 48
------+------------------------------------+--------------------------------
RMS | 1518 18 37 24 23 19 |T 76 66 78 72 74 71
WRMS | 1518 15 23 18 17 18 |NE 76 66 78 72 74 71
MEDI | 1049 12 17 19 17 18 |MD 85 76 79 71 71 71
Table 3.2268.1 GPS week: 2268 Day: 1 MJD: 60121
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1243 26 46 28 37 27 19 | 65 44 72 48 49 58
R02 | 1552 10 10 8 14 15 6 | 57 54 53 60 63 55
R03 | 735 12 14 8 12 22 6 | 72 59 64 66 79 66
R04 | 1434 11 12 10 15 23 7 | 68 63 67 65 57 65
R05 | 1282 15 15 8 27 15 9 | 70 59 57 54 56 59
R07 | 831 8 20 11 12 17 7 | 68 56 70 69 70 66
R08 | 711 11 12 10 16 28 7 | 67 68 62 72 84 66
R09 | 1899 11 14 13 7 24 6 | 18 21 23 20 28 18
R11 | 1919 11 15 10 11 20 6 | 17 29 29 21 23 22
R12 | 761 9 19 11 11 21 7 | 48 59 49 47 53 49
R13 | 842 24 42 24 53 12 20 | 47 32 42 44 33 38
R14 | 630 11 12 5 11 19 5 | 29 39 31 34 27 31
R15 | 1535 11 12 11 11 18 6 | 47 56 53 53 46 50
R16 | 893 29 33 62 30 29 24 | 54 57 50 52 51 50
R18 | 776 14 17 8 14 17 7 | 25 31 38 40 26 30
R19 | 1269 34 74 23 51 31 25 | 63 54 47 53 63 51
R20 | 3577 32 120 39 59 40 36 | 60 67 74 76 50 64
R21 | 871 8 16 10 11 20 6 | 34 33 32 40 32 34
R22 | 1244 15 9 19 21 16 10 | 42 48 58 50 41 47
R24 | 826 11 13 8 11 16 6 | 46 37 38 36 39 39
XR25 | 7607 11 21 --- --- 40 15 | 37 23 --- --- 31 30
------+------------------------------------+--------------------------------
RMS | 1406 17 37 21 27 23 |T 48 47 50 49 47 47
WRMS | 1406 15 24 11 19 22 |NE 48 47 50 49 47 47
MEDI | 1243 11 15 10 14 20 |MD 47 54 50 50 46 50
Table 3.2268.2 GPS week: 2268 Day: 2 MJD: 60122
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 794 45 35 35 28 39 21 | 85 42 58 55 77 56
R02 | 1467 14 14 17 20 23 9 | 74 74 83 75 89 75
R03 | 737 16 20 11 16 10 9 | 84 67 74 70 75 72
R04 | 1354 12 9 14 20 21 8 | 75 70 77 60 65 69
R05 | 915 10 9 12 20 12 8 | 70 68 72 60 58 66
R07 | 934 10 16 15 16 12 8 | 77 68 78 74 66 74
R08 | 1644 8 21 15 17 37 9 | 79 67 84 88 104 80
R09 | 1630 17 13 24 10 22 10 | 16 22 38 22 34 22
R11 | 1476 14 18 12 9 16 7 | 17 29 25 20 25 20
R12 | 784 14 17 11 11 16 7 | 42 47 45 41 45 42
R13 | 684 26 24 22 38 22 16 | 51 42 45 27 27 38
R14 | 938 10 14 10 13 20 7 | 33 38 29 29 38 30
R15 | 1109 8 7 12 8 13 5 | 53 50 51 49 48 50
R16 | 745 24 28 52 21 28 20 | 57 55 60 50 46 54
R18 | 719 14 20 9 7 19 7 | 53 58 51 59 51 54
R19 | 1355 46 78 20 27 30 25 | 81 54 84 80 83 74
R20 | 3525 53 106 25 42 43 34 | 95 70 78 85 90 78
R21 | 694 12 17 9 10 17 7 | 59 56 60 59 62 58
R22 | 1035 14 17 11 6 19 7 | 27 38 32 39 38 33
R24 | 1083 10 18 9 15 14 7 | 63 58 62 62 61 60
XR25 |12693 8 12 --- --- 28 10 | 38 38 --- --- 40 37
------+------------------------------------+--------------------------------
RMS | 1335 23 34 20 20 23 |T 58 52 59 55 58 54
WRMS | 1335 17 23 13 14 21 |NE 58 52 59 55 58 54
MEDI | 1035 14 17 12 16 20 |MD 57 55 60 59 58 56
Table 3.2268.3 GPS week: 2268 Day: 3 MJD: 60123
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 661 45 42 33 27 36 21 | 92 39 69 53 55 61
R02 | 1393 18 17 12 21 25 10 | 87 83 71 67 86 75
R03 | 808 18 17 10 17 18 9 | 95 80 84 82 79 84
R04 | 1356 22 11 13 16 15 9 | 81 66 59 64 66 66
R05 | 985 14 12 16 16 14 8 | 74 62 72 63 72 67
R07 | 687 11 22 25 16 13 11 | 77 68 97 77 70 79
R08 | 810 12 14 9 16 24 7 | 78 77 85 94 89 84
R09 | 2592 13 6 11 11 13 6 | 20 22 30 26 26 23
R11 | 1367 12 13 16 16 17 8 | 22 34 33 29 35 27
R12 | 751 8 14 10 10 16 6 | 30 30 24 35 23 29
R13 | 825 29 25 22 34 22 16 | 59 36 49 33 43 40
R14 | 1093 10 19 11 12 16 7 | 32 42 27 34 35 31
R15 | 1252 13 10 11 11 12 6 | 46 42 31 39 31 38
R16 | 835 29 35 63 22 40 23 | 53 46 70 66 53 58
XR17 | 849 16 --- 355 13 24 14 | 64 --- 9999 66 74 74
R18 | 989 12 27 17 14 13 10 | 58 66 57 62 55 59
R19 | 1393 47 66 25 46 35 27 | 85 61 73 82 87 75
R20 | 1487 55 114 41 38 53 37 | 95 63 94 101 92 84
R21 | 651 12 12 10 17 14 7 | 73 71 77 75 71 74
R22 | 1039 11 15 14 7 17 7 | 36 33 46 43 49 38
R24 | 1361 12 9 10 10 23 6 | 64 62 63 62 70 61
XR25 |16908 12 15 --- --- 31 13 | 39 47 --- --- 44 42
------+------------------------------------+--------------------------------
RMS | 1199 24 35 23 21 24 |T 61 53 60 59 59 57
WRMS | 1199 19 23 13 16 22 |NE 61 53 60 59 59 57
MEDI | 989 13 15 14 16 17 |MD 64 61 63 63 55 61
Table 3.2268.4 GPS week: 2268 Day: 4 MJD: 60124
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 802 41 51 24 39 31 22 | 77 43 56 47 36 50
R02 | 1409 14 9 12 13 33 7 | 68 61 58 62 88 61
R03 | 1002 15 19 9 17 26 8 | 77 57 70 73 81 69
R04 | 870 14 11 12 20 14 8 | 69 60 56 54 54 59
R05 | 755 15 11 13 18 10 8 | 59 52 56 54 54 54
R07 | 726 10 19 12 13 18 8 | 64 46 61 65 61 59
R08 | 966 13 20 27 19 12 12 | 59 58 84 73 58 67
R09 | 2531 13 9 14 8 18 6 | 17 22 27 27 32 22
R11 | 1543 11 14 8 20 10 8 | 22 28 26 30 28 24
R12 | 1026 13 10 19 12 19 8 | 41 43 45 38 41 40
R13 | 628 36 34 32 51 22 22 | 53 31 38 31 27 32
R14 | 610 7 13 9 11 17 5 | 29 34 26 22 28 26
R15 | 1188 19 9 13 14 17 8 | 53 45 42 41 50 44
R16 | 1776 23 21 60 33 35 22 | 59 53 56 48 62 53
R17 | 874 10 9 9 19 23 7 | 45 65 9999 37 50 48
R18 | 1344 13 28 12 14 14 10 | 35 42 32 37 37 34
R19 | 1210 36 69 40 65 32 30 | 60 35 64 53 56 52
R20 | 1717 49 99 28 44 37 34 | 74 47 73 77 67 64
R21 | 1074 17 10 15 13 23 8 | 49 48 45 45 40 44
R22 | 1616 10 7 12 12 10 6 | 33 40 35 39 33 35
R24 | 1572 17 26 21 30 17 13 | 48 38 52 55 46 45
XR25 |18980 7 9 --- --- 20 8 | 33 41 --- --- 32 36
------+------------------------------------+--------------------------------
RMS | 1287 22 33 23 27 22 |T 51 44 50 48 48 46
WRMS | 1287 16 19 18 24 24 |NE 51 44 50 48 48 46
MEDI | 1074 14 13 13 18 18 |MD 53 43 52 47 46 45
Table 3.2268.5 GPS week: 2268 Day: 5 MJD: 60125
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1354 32 46 35 48 49 23 | 72 55 73 51 45 59
R02 | 1873 10 10 10 19 25 7 | 63 62 65 69 63 64
R03 | 1026 12 9 13 13 27 7 | 67 61 61 60 78 62
R04 | 864 10 11 14 14 17 7 | 68 64 53 66 66 62
R05 | 782 17 11 23 21 23 11 | 56 59 74 55 57 59
R07 | 795 14 20 9 11 18 8 | 65 54 61 63 58 60
R08 | 1218 6 20 17 16 24 8 | 67 58 71 80 58 68
R09 | 2262 11 12 24 10 29 9 | 20 22 40 23 34 24
R11 | 1269 12 14 15 7 16 7 | 31 33 38 30 34 30
R12 | 1018 9 18 18 8 16 8 | 50 55 44 51 49 48
R13 | 939 16 36 16 36 41 15 | 53 55 42 44 45 47
R14 | 843 7 11 15 12 16 6 | 36 37 46 35 32 37
R15 | 1144 11 17 13 16 20 8 | 55 64 62 48 56 56
R16 | 1874 25 20 57 29 30 21 | 51 58 49 39 65 47
R17 | 704 7 20 8 12 22 7 | 33 34 9999 45 42 36
R18 | 1738 8 23 8 20 17 8 | 39 37 33 37 41 35
R19 | 1394 26 59 25 56 31 23 | 31 29 31 36 44 28
R20 | 2066 33 113 31 65 34 36 | 46 57 54 39 50 45
R21 | 1103 8 18 15 10 17 7 | 37 36 45 44 34 39
R22 | 2521 12 11 10 14 25 7 | 28 35 33 34 25 30
R24 | 1512 12 20 7 13 20 7 | 45 47 42 49 35 44
XR25 |14729 7 12 --- --- 17 9 | 24 28 --- --- 24 25
------+------------------------------------+--------------------------------
RMS | 1441 16 34 21 27 26 |T 47 47 50 47 47 45
WRMS | 1441 15 19 24 25 23 |NE 47 47 50 47 47 45
MEDI | 1218 11 18 15 14 22 |MD 46 54 46 45 45 45
Table 3.2268.6 GPS week: 2268 Day: 6 MJD: 60126
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1307 39 50 35 37 41 23 | 85 43 77 43 42 57
R02 | 1923 10 16 18 20 31 9 | 73 73 81 72 63 73
R03 | 684 9 15 14 15 22 8 | 82 66 79 80 84 77
R04 | 1274 11 10 9 9 26 6 | 73 61 62 69 79 66
R05 | 540 8 15 9 14 15 7 | 65 66 64 67 64 63
R07 | 1034 17 25 13 15 17 10 | 77 53 71 66 61 66
R08 | 2119 10 16 8 11 20 6 | 79 65 79 79 78 76
R09 | 1540 10 10 14 13 28 7 | 40 37 47 36 45 39
R11 | 1180 7 16 9 8 34 6 | 27 27 33 31 39 28
R12 | 960 9 12 11 11 15 6 | 61 68 59 61 60 61
R13 | 1120 20 27 29 40 37 17 | 62 55 53 56 59 53
R14 | 1032 11 17 5 10 27 6 | 48 59 50 53 42 51
R15 | 1232 9 11 11 10 25 6 | 74 77 80 75 67 76
R16 | 1279 29 33 58 22 26 22 | 77 77 92 66 75 77
R17 | 892 9 16 9 9 15 6 | 72 57 9999 74 78 70
R18 | 1589 9 15 9 10 21 6 | 56 64 57 57 56 58
R19 | 1271 30 69 27 19 39 21 | 92 56 92 88 92 83
R20 | 2455 43 84 29 43 50 29 | 111 55 91 106 102 90
R21 | 949 6 19 12 10 14 7 | 81 70 80 81 80 78
R22 | 3540 13 15 13 7 22 7 | 44 45 48 49 49 45
R24 | 1426 12 12 9 11 30 6 | 77 70 73 74 68 73
XR25 |17598 8 13 --- --- 43 10 | 41 43 --- --- 54 41
------+------------------------------------+--------------------------------
RMS | 1542 19 31 21 19 28 |T 68 58 68 65 65 63
WRMS | 1542 15 22 17 15 24 |NE 68 58 68 65 65 63
MEDI | 1271 10 16 12 11 26 |MD 73 59 71 67 63 66
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