[IGSREPORT-29418] Wk 2269 IGLOS Final Orbits
acc
acc at igs.org
Mon Jul 24 11:09:39 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2269 (Jul 02, 2023 - Jul 08, 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 2.2269.
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:
igl2269[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2269 in the SP3 format.
igl22697.sum Combination Report for GPS Week 2269.
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 | -9.0 ns
1 | -6.9 ns
2 | -8.7 ns
3 | -10.1 ns
4 | -10.5 ns
5 | -13.8 ns
6 | -11.8 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
----+--------+---------------
3 | ALL | R25
5 | ALL | R25
6 | ALL | R25
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 1.2269, 1a.2269).
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 2.2269.0-6)
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 3.2269.0-6).
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 2269 summary. (Jul 02, 2023 - Jul 08, 2023)
Table 1.2269.a GPS week : 2269 MJD: 60127.0-60133.0
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 -1 3 12 -21 12 .04 21 16 | 14419 432 2967 8479
| 1 1 1 15 8 20 .07 | 2245 2392
esa n/a| -1 0 -1 -22 -13 4 -.20 36 25 | -15185 1086 2985 7801
| 1 0 1 11 12 13 .04 | 5260 3033
gfz n/a| 0 0 -2 20 17 42 -.19 23 19 | 0 452 2982 8275
| 0 0 2 11 11 17 .07 | 0 2375
grg n/a| 2 0 0 -20 29 -69 .32 26 18 | -10537 399 2978 7884
| 1 0 2 12 5 26 .07 | 1934 2464
iac n/a| 0 0 -4 11 14 -20 -.27 27 25 | -7703 -592 2959 8834
| 1 1 2 19 24 57 .10 | 2044 1345
Table 1.2269.b GPS week : 2269 MJD: 60127.0-60133.0
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 | 19 36 23 19 18 19 20 |
R02 | 5 7 18 15 7 9 7 |
R03 | 9 7 14 13 8 8 9 |
R04 | 9 9 11 22 7 9 7 |
R05 | 9 11 9 23 8 10 8 |
R07 | 11 9 13 10 9 9 6 |
R08 | 12 12 9 10 7 8 9 |
R09 | 10 9 8 8 6 8 8 |
R11 | 8 8 8 10 7 10 8 |
R12 | 7 9 8 10 9 8 9 |
R13 | 17 19 19 18 14 16 15 |
R14 | 9 5 4 7 9 6 5 |
R15 | 10 12 7 7 8 7 8 |
R16 | 23 26 20 23 21 20 22 |
R17 | 6 6 8 6 8 12 7 |
R18 | 11 8 9 9 11 8 9 |
R19 | 29 36 30 30 29 32 27 |
R20 | 31 36 39 37 38 38 36 |
R21 | 9 7 9 7 6 9 8 |
R22 | 8 7 7 9 8 8 8 |
R24 | 8 9 9 9 10 9 7 |
R25 | 10 14 0 --- 0 --- --- |
Table 1.2269.c GPS week : 2269 MJD: 60127.0-60133.0
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 2269 0 | 62 82 275 -552 -1262 9077 80.4 1774 1774 | -8974 0
brd 2269 1 | 84 4 228 -1750 -1405 4432 80.9 1639 1639 | -6905 0
brd 2269 2 | -16 -32 193 -1481 942 11220 81.0 1616 1616 | -8653 0
brd 2269 3 | 14 -123 163 308 1726 9423 81.1 1520 1520 | -10062 0
brd 2269 4 | -20 -32 223 -759 -902 15410 79.6 1369 1369 | -10530 0
brd 2269 5 | -50 -59 235 517 -678 8554 80.9 1308 1308 | -13821 0
brd 2269 6 | -67 -13 210 566 -2480 6602 80.9 1367 1367 | -11787 0
-------------+------------------------------------------------------------+----------------
brd 2269 mean| 0 -24 218 -449 -579 9245 80.7 1513 1513 | -10104 0
brd 2269 sdev| 56 62 35 949 1443 3478 .5 172 172 | 2252 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 2.2269.0 GPS week: 2269 Day: 0 MJD: 60127
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 1 -17 -26 32 .04 19 16 | 10667 -1487 3137 8944
esa n/a| -1 1 -2 -24 -17 -5 -.24 34 25 | -17199 -909 3159 8051
gfz n/a| 0 1 -3 33 5 22 -.30 23 17 | 0 -1830 3170 8502
grg n/a| 3 0 3 -37 33 -63 .34 22 17 | -8518 -1908 3147 8002
iac n/a| -1 1 -7 35 -3 -38 -.17 27 23 | -7131 -1795 3157 8816
Table 2.2269.1 GPS week: 2269 Day: 1 MJD: 60128
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 17 -6 -11 .09 21 15 | 12097 4682 3316 9115
esa n/a| -1 0 -2 -16 10 2 -.15 36 24 | -16987 5132 3311 8366
gfz n/a| 0 1 0 22 12 25 -.19 25 22 | 0 4421 3396 8458
grg n/a| 4 1 4 -34 28 -24 .32 37 23 | -9305 4527 3361 7998
iac n/a| 0 0 -7 17 -3 -52 -.24 27 23 | -6131 1509 3303 9002
Table 2.2269.2 GPS week: 2269 Day: 2 MJD: 60129
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 26 -30 7 .13 20 15 | 17048 -1507 3017 9309
esa n/a| 0 0 -3 -23 -18 -6 -.14 39 25 | -8963 -276 3024 6311
gfz n/a| 0 0 -5 7 33 66 -.18 22 15 | 0 -1384 3025 8952
grg n/a| 1 0 1 -8 25 -93 .21 28 17 | -8145 -1315 3009 8757
iac n/a| 1 -2 -2 27 16 91 -.22 30 33 | -4478 -2130 2989 9746
Table 2.2269.3 GPS week: 2269 Day: 3 MJD: 60130
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 5 12 -22 -16 .07 28 19 | 14810 436 2663 7788
esa n/a| -3 0 2 -37 -28 -8 -.16 34 31 | -7457 2964 2670 7502
gfz n/a| 0 0 2 7 6 61 -.18 21 17 | 0 785 2657 7668
grg n/a| 3 1 -3 -5 28 -45 .41 32 18 | -10553 468 2711 7468
iac n/a| -1 0 -1 -24 26 -93 -.14 31 27 | -7633 -534 2664 8363
Table 2.2269.4 GPS week: 2269 Day: 4 MJD: 60131
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 3 15 -20 15 .01 22 15 | 14808 2582 3010 7537
esa n/a| -1 -1 0 -26 -19 18 -.23 34 21 | -21756 3611 3012 7136
gfz n/a| 0 0 0 13 19 47 -.24 21 26 | 0 2447 3008 7512
grg n/a| 0 0 -1 -13 40 -91 .38 21 18 | -12264 2864 2999 7011
iac n/a| 0 0 -5 6 15 -39 -.34 27 25 | -8366 368 2997 8056
Table 2.2269.5 GPS week: 2269 Day: 5 MJD: 60132
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 27 -15 22 -.07 19 15 | 15814 -1539 3027 9059
esa n/a| 0 0 0 -28 -12 26 -.24 37 28 | -19286 -3712 3124 7535
gfz n/a| -1 0 -4 22 15 43 -.15 26 18 | 0 -1874 3029 9146
grg n/a| 2 0 0 -18 26 -78 .24 22 17 | -13004 -1811 3004 8532
iac n/a| 0 0 0 3 60 -10 -.40 25 23 | -9995 -1687 3017 9667
Table 2.2269.6 GPS week: 2269 Day: 6 MJD: 60133
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 6 -28 37 -.02 16 14 | 15690 -139 2600 7603
esa n/a| -2 0 -3 -1 -6 0 -.21 35 22 | -14648 793 2597 9706
gfz n/a| 0 0 -2 34 31 28 -.09 24 15 | 0 602 2590 7693
grg n/a| 2 2 0 -26 25 -88 .31 23 16 | -11972 -28 2617 7422
iac n/a| 1 1 -3 15 -12 0 -.36 25 21 | -10190 122 2587 8191
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 3.2269.0 GPS week: 2269 Day: 0 MJD: 60127
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 745 32 43 23 30 62 18 | 58 71 62 75 65 60
R02E | 1682 6 9 8 10 22 4 | 135 135 135 143 134 136
R03E | 710 16 17 11 15 25 8 | 59 59 59 65 67 59
R04E | 2736 10 15 17 15 14 8 | 71 71 69 78 70 71
R05E | 1187 14 11 17 18 24 9 | 61 61 59 69 65 61
R07E | 1173 13 26 15 19 20 10 | 76 76 77 80 75 76
R08E | 3491 11 26 30 16 11 12 | 96 100 114 108 99 103
R09 | 2065 20 19 17 11 32 9 | 43 47 48 43 49 43
R11 | 1389 9 19 15 12 24 8 | 50 49 54 54 50 51
R12 | 1022 13 14 10 6 33 6 | 62 73 68 68 67 66
R13 | 1094 26 40 21 30 22 16 | 71 60 62 56 66 60
R14 | 1041 6 10 23 18 13 9 | 50 51 43 58 48 49
R15 | 1036 12 16 23 12 17 9 | 68 74 57 69 60 65
R16 | 1105 25 39 63 19 22 22 | 81 97 84 80 82 84
R17 | 1552 12 11 10 9 17 6 | 59 58 56 57 56 56
R18 | 1487 12 30 23 10 24 11 | 46 61 41 51 36 47
R19 | 1687 40 88 17 44 20 28 | 107 68 102 101 90 93
R20 | 2526 39 79 40 54 42 30 | 103 60 87 95 88 79
R21 | 1057 10 17 14 19 16 8 | 64 66 72 60 64 64
R22 | 3181 13 9 16 10 25 7 | 26 29 31 31 37 27
R24 | 1671 15 17 11 13 27 8 | 65 60 63 62 56 62
XR25 |23163 7 14 --- --- 37 10 | 46 24 --- --- 51 32
------+------------------------------------+--------------------------------
RMS | 1773 19 34 23 22 27 |T 68 65 68 71 67 65
WRMS | 1773 16 25 17 17 23 |NE 62 58 62 63 60 58
MEDI | 1389 13 17 17 15 22 |MD 62 61 62 68 65 61
Table 3.2269.1 GPS week: 2269 Day: 1 MJD: 60128
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1564 43 33 46 113 46 36 | 75 84 90 145 72 83
R02E | 777 10 10 15 14 10 7 | 113 113 117 120 109 115
R03E | 975 10 16 8 14 46 7 | 41 35 43 49 33 40
R04E | 2292 11 18 12 21 32 9 | 48 41 46 51 37 43
R05E | 1280 16 12 22 28 12 11 | 41 37 42 54 32 39
R07E | 843 11 19 13 19 19 8 | 61 60 65 62 48 60
R08E | 3066 18 20 18 24 22 11 | 85 89 99 103 87 91
R09 | 2828 13 13 15 16 22 8 | 29 36 40 41 31 34
R11 | 1907 15 10 16 13 27 8 | 37 36 31 42 29 35
R12 | 1367 10 16 12 23 23 8 | 44 53 47 45 41 45
R13 | 1544 16 23 33 54 29 18 | 51 49 59 37 55 48
R14 | 1399 5 9 8 11 15 4 | 30 29 36 36 34 31
R15 | 894 14 11 30 24 32 12 | 42 46 42 53 56 42
R16 | 756 24 39 69 29 24 25 | 50 59 65 47 56 53
R17 | 726 7 8 14 11 29 6 | 35 39 43 44 29 39
R18 | 1475 11 21 8 10 16 7 | 36 39 32 45 32 37
R19 | 2025 36 94 32 85 28 36 | 61 54 61 82 63 57
R20 | 1813 50 113 30 31 39 36 | 74 70 88 71 79 71
R21 | 785 9 16 13 11 17 7 | 34 38 36 37 35 34
R22 | 1909 11 10 9 16 22 6 | 29 38 39 36 32 33
R24 | 1356 19 15 14 10 18 9 | 39 36 39 37 31 36
XR25 |20422 10 17 --- --- 39 13 | 36 26 --- --- 38 28
------+------------------------------------+--------------------------------
RMS | 1639 21 36 25 37 27 |T 49 50 55 58 48 49
WRMS | 1639 15 24 22 23 23 |NE 41 43 47 46 42 41
MEDI | 1399 11 16 15 19 23 |MD 41 39 43 47 37 40
Table 3.2269.2 GPS week: 2269 Day: 2 MJD: 60129
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1748 30 38 47 38 37 22 | 83 78 89 90 73 79
R02E | 713 16 14 25 55 12 18 | 123 121 123 153 123 127
R03E | 760 16 17 15 41 20 14 | 51 44 42 67 53 46
R04E | 2459 14 12 17 28 50 11 | 98 99 99 129 75 105
R05E | 932 17 11 9 23 15 9 | 82 80 80 106 79 86
R07E | 847 19 11 16 35 38 13 | 73 70 67 102 59 76
R08E | 2244 12 15 14 21 50 9 | 107 103 107 122 83 109
R09 | 3386 14 14 15 12 15 8 | 30 37 50 34 45 36
R11 | 1966 12 16 13 11 24 7 | 31 46 45 30 34 36
R12 | 1362 16 11 15 11 16 8 | 53 51 50 53 50 51
R13 | 1606 30 42 19 38 19 18 | 74 43 54 47 60 55
R14 | 2157 6 7 7 6 15 4 | 39 40 43 42 38 41
R15 | 891 11 18 7 10 25 7 | 54 48 52 54 37 51
R16 | 731 23 32 48 21 21 19 | 57 51 55 58 51 54
R17 | 886 9 15 14 15 16 7 | 37 36 45 42 35 39
R18 | 1045 13 22 13 10 24 8 | 29 39 35 42 30 33
R19 | 2264 33 89 36 45 37 29 | 75 37 84 63 82 65
R20 | 1143 43 129 35 43 62 38 | 76 48 86 87 50 70
R21 | 854 9 25 14 11 28 8 | 50 46 57 60 53 52
R22 | 1478 12 7 13 12 27 6 | 30 33 37 35 38 32
R24 | 1001 18 14 13 17 20 9 | 50 39 37 43 36 40
XR25 |18598 3 --- --- --- 37 0 | 28 --- --- --- 33 22
------+------------------------------------+--------------------------------
RMS | 1615 20 39 22 28 30 |T 60 56 63 69 55 59
WRMS | 1615 15 25 15 17 33 |NE 47 42 52 49 44 45
MEDI | 1143 14 15 15 21 24 |MD 53 46 54 58 50 51
Table 3.2269.3 GPS week: 2269 Day: 3 MJD: 60130
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1107 42 35 32 16 35 19 | 81 96 103 93 93 89
R02E | 937 13 18 13 45 19 14 | 156 160 162 155 157 156
R03E | 1451 20 15 16 36 18 13 | 48 35 41 58 39 41
R04E | 2483 30 24 17 69 62 22 | 63 64 58 102 66 63
R05E | 1371 25 21 18 76 49 23 | 43 40 37 87 52 38
R07E | 942 17 12 13 24 19 10 | 60 53 56 65 54 56
R08E | 1477 11 14 19 19 30 9 | 92 89 98 94 105 92
R09 | 2746 10 8 17 16 13 8 | 21 31 41 25 24 29
R11 | 1509 15 22 16 14 15 9 | 16 36 25 23 26 22
R12 | 834 17 19 20 8 18 10 | 30 29 18 22 21 19
R13 | 1307 37 29 17 40 32 18 | 67 41 38 35 40 42
R14 | 1703 8 13 11 13 18 6 | 35 45 33 38 33 35
R15 | 1029 8 16 13 9 27 7 | 50 42 59 48 35 48
R16 | 738 30 42 51 26 37 23 | 55 34 45 62 41 46
R17 | 1046 14 11 6 11 10 6 | 56 47 45 50 47 48
R18 | 1416 12 24 10 12 21 8 | 41 53 39 46 35 43
R19 | 2383 43 81 34 42 34 29 | 88 44 92 81 89 76
R20 | 1800 77 101 29 34 57 37 | 113 55 75 86 67 77
R21 | 1343 13 10 11 11 10 6 | 54 47 48 56 47 50
R22 | 1370 14 19 16 12 28 9 | 38 41 44 51 51 42
R24 | 873 19 13 13 14 19 8 | 61 54 50 53 53 53
------+------------------------------------+--------------------------------
RMS | 1520 28 34 21 32 31 |T 58 54 57 63 54 55
WRMS | 1520 19 31 17 18 27 |NE 50 42 46 48 42 45
MEDI | 1370 17 19 16 16 21 |MD 54 45 45 56 47 48
Table 3.2269.4 GPS week: 2269 Day: 4 MJD: 60131
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1295 36 34 33 20 33 18 | 69 66 76 74 58 66
R02E | 1663 9 12 9 14 18 6 | 140 140 147 139 132 141
R03E | 2016 12 17 15 13 16 8 | 45 53 44 52 34 46
R04E | 1901 9 11 9 16 22 6 | 49 46 49 59 42 50
R05E | 934 9 12 12 17 12 7 | 58 59 54 61 54 57
R07E | 603 16 13 13 19 16 9 | 49 49 53 51 53 49
R08E | 1062 8 12 11 14 14 6 | 62 60 64 68 63 63
R09 | 1568 13 9 11 9 27 6 | 31 27 31 29 30 29
R11 | 1746 12 13 9 12 20 6 | 35 39 38 34 30 35
R12 | 976 11 18 20 13 37 9 | 48 48 49 50 57 47
R13 | 1053 18 32 13 32 31 14 | 53 37 41 40 31 41
R14 | 944 11 18 18 14 19 9 | 35 39 29 23 40 28
R15 | 1002 10 8 17 12 18 7 | 50 50 43 48 35 46
R16 | 715 24 27 57 23 46 21 | 60 61 68 58 68 61
R17 | 1157 7 17 10 19 27 8 | 49 47 48 47 56 46
R18 | 1696 12 31 11 22 11 11 | 40 50 40 44 41 40
R19 | 1987 35 76 36 51 21 28 | 72 46 66 76 74 64
R20 | 1420 72 112 30 32 53 38 | 92 50 72 76 70 67
R21 | 1073 13 7 9 10 20 6 | 61 55 53 51 50 54
R22 | 1477 10 9 17 16 32 8 | 34 35 34 43 41 34
R24 | 1166 16 15 12 22 22 9 | 52 55 52 43 45 48
XR25 |15590 2 --- --- --- 39 0 | 28 --- --- --- 52 19
------+------------------------------------+--------------------------------
RMS | 1369 22 34 21 21 27 |T 55 52 54 55 52 51
WRMS | 1369 15 21 26 18 25 |NE 49 45 47 47 48 43
MEDI | 1166 12 15 13 16 21 |MD 49 50 49 51 50 47
Table 3.2269.5 GPS week: 2269 Day: 5 MJD: 60132
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 822 26 38 38 28 39 18 | 76 76 98 76 73 78
R02E | 1553 13 12 18 18 21 9 | 123 127 132 124 123 125
R03E | 2306 14 11 13 14 15 7 | 42 37 39 39 33 38
R04E | 1383 11 13 16 19 28 9 | 44 38 40 44 37 40
R05E | 1499 13 12 21 17 10 9 | 39 38 42 41 39 38
R07E | 1166 10 17 20 15 19 9 | 45 42 50 46 44 44
R08E | 883 13 14 12 17 16 8 | 68 67 72 77 77 70
R09 | 1234 9 8 18 15 32 7 | 42 44 46 35 45 40
R11 | 1557 16 18 21 12 30 9 | 26 29 46 26 39 29
R12 | 846 14 12 19 6 36 8 | 47 56 54 52 58 50
R13 | 577 23 35 26 24 26 15 | 46 45 47 45 38 42
R14 | 1237 9 11 12 11 13 6 | 30 38 35 37 29 34
R15 | 1053 14 13 10 8 10 6 | 46 50 46 45 47 46
R16 | 650 24 21 60 16 39 19 | 59 60 57 58 78 56
R17 | 707 5 15 31 20 11 11 | 37 31 53 36 36 36
R18 | 1362 8 22 11 15 16 8 | 34 32 30 37 31 32
R19 | 1658 27 87 46 58 35 32 | 34 35 51 54 42 39
R20 | 1368 53 119 37 41 37 38 | 60 36 48 46 51 43
R21 | 1164 8 22 21 11 11 9 | 33 36 48 39 33 37
R22 | 1666 13 13 16 10 23 7 | 42 40 52 40 44 42
R24 | 1428 15 23 13 11 21 9 | 36 33 43 48 31 38
------+------------------------------------+--------------------------------
RMS | 1308 19 37 26 22 25 |T 47 47 53 49 48 47
WRMS | 1308 15 28 18 17 23 |NE 40 40 46 42 42 40
MEDI | 1237 13 15 19 15 21 |MD 42 38 48 45 40 40
Table 3.2269.6 GPS week: 2269 Day: 6 MJD: 60133
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1196 19 46 40 37 55 20 | 75 80 97 77 75 77
R02E | 1059 10 10 9 14 15 6 | 110 106 107 116 105 110
R03E | 1775 13 15 17 18 20 9 | 45 44 49 53 42 46
R04E | 904 9 13 11 14 14 7 | 47 48 49 56 43 49
R05E | 1312 13 11 11 16 18 7 | 41 43 44 43 44 41
R07E | 2034 10 11 11 9 24 6 | 52 45 48 51 44 48
R08E | 1223 12 15 18 18 16 9 | 54 53 56 58 53 54
R09 | 1081 7 11 16 19 29 7 | 67 62 73 65 69 66
R11 | 1516 10 22 11 12 21 8 | 38 36 46 34 38 37
R12 | 1112 14 13 22 12 16 9 | 58 68 69 62 69 62
R13 | 601 16 32 26 29 29 14 | 58 48 62 63 57 56
R14 | 1327 5 8 9 11 16 4 | 40 46 39 45 42 41
R15 | 1212 13 15 16 9 12 7 | 65 72 67 63 60 65
R16 | 660 24 20 64 25 32 21 | 77 82 75 70 87 74
R17 | 1013 8 17 11 10 19 6 | 69 64 75 64 69 67
R18 | 1552 9 21 12 18 38 8 | 59 71 61 61 51 61
R19 | 1022 25 80 39 43 27 27 | 109 58 114 107 116 98
R20 | 2419 38 114 33 55 32 35 | 120 55 103 108 104 94
R21 | 1197 8 18 18 10 13 8 | 80 70 88 81 77 79
R22 | 1903 13 14 16 14 17 8 | 49 55 57 57 57 53
R24 | 1108 10 18 8 12 16 7 | 75 71 73 72 68 72
------+------------------------------------+--------------------------------
RMS | 1366 16 35 24 23 25 |T 64 60 69 66 64 64
WRMS | 1366 14 22 15 16 21 |NE 66 61 71 68 67 66
MEDI | 1197 12 15 16 14 19 |MD 58 58 67 63 57 62
More information about the IGSREPORT
mailing list