[IGSREPORT-28939] Wk 2227 IGLOS Final Orbits
acc
acc at igs.org
Mon Oct 3 08:16:01 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2227 (Sep 11, 2022 - Sep 17, 2022)
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 2.2227.
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:
igl2227[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2227 in the SP3 format.
igl22277.sum Combination Report for GPS Week 2227.
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.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 0.5 ns
1 | -1.3 ns
2 | 0.1 ns
3 | -0.8 ns
4 | -0.7 ns
5 | -6.9 ns
6 | -0.7 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2227, 1a.2227).
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 2.2227.0-6)
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 3.2227.0-6).
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 2227 summary. (Sep 11, 2022 - Sep 17, 2022)
Table 1.2227.a GPS week : 2227 MJD: 59833.0-59839.0
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 -17 -26 35 .08 18 15 | 34373 -1593 2796 7908
| 1 1 1 11 5 31 .05 | 4469 1666
esx n/a| 0 2 4 25 31 25 -.16 31 23 | 5659 -898 2789 11115
| 1 0 1 28 18 24 .05 | 9520 1193
gfz n/a| -1 0 -1 13 -7 62 .05 28 16 | 0 -1523 2842 7785
| 0 0 1 22 13 13 .06 | 0 1300
grg n/a| 3 -2 6 0 70 -173 .23 26 22 | -861 -1400 2785 7354
| 1 1 1 15 14 60 .03 | 2713 1465
iac n/a| 0 0 -13 -18 -33 30 -.29 24 23 | 1906 -496 2850 9736
| 1 1 3 19 26 66 .05 | 2507 824
Table 1.2227.b GPS week : 2227 MJD: 59833.0-59839.0
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 19 19 22 20 18 19 |
R02 | 10 10 9 8 9 6 7 |
R03 | 9 7 8 6 8 7 9 |
R04 | 10 6 8 10 10 10 8 |
R05 | 9 10 12 10 8 9 9 |
R07 | 9 8 9 10 8 7 6 |
R08 | 9 8 12 12 12 10 8 |
R09 | 11 11 11 12 11 13 12 |
R11 | 11 10 13 11 9 10 12 |
R12 | 10 6 8 11 7 7 8 |
R13 | 17 14 18 17 19 17 14 |
R14 | 7 8 8 6 7 6 6 |
R15 | 11 7 9 8 8 10 8 |
R17 | 8 7 8 6 8 8 6 |
R18 | 8 8 9 8 10 9 8 |
R19 | 22 23 25 25 19 24 21 |
R20 | 23 22 27 23 24 26 29 |
R21 | 6 8 8 8 8 8 9 |
R24 | 9 10 7 10 8 8 9 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2227.c GPS week : 2227 MJD: 59833.0-59839.0
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 2227 0 | 58 -57 68 365 -23 -7448 82.6 1598 1598 | 504 0
brd 2227 1 | 75 64 121 -812 -816 12 82.6 1397 1397 | -1258 0
brd 2227 2 | -123 86 90 -530 -1575 5696 80.2 1474 1474 | 60 0
brd 2227 3 | -18 -32 105 -844 -411 3727 82.7 1560 1560 | -821 0
brd 2227 4 | -11 -5 182 -12 316 7006 82.3 1759 1759 | -679 0
brd 2227 5 | 93 35 131 -770 -52 5638 82.5 1698 1698 | -6916 0
brd 2227 6 | 56 53 104 -515 1127 6628 82.2 1661 1661 | -715 0
-------------+------------------------------------------------------------+----------------
brd 2227 mean| 18 20 114 -445 -205 3037 82.2 1592 1592 | -1403 0
brd 2227 sdev| 75 53 36 457 855 5196 .9 127 127 | 2500 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 2.2227.0 GPS week: 2227 Day: 0 MJD: 59833
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 -3 -22 14 .03 18 15 | 38159 -152 3146 7349
esx n/a| 0 1 4 27 29 46 -.14 33 24 | 10041 -27 3145 10510
gfz n/a| 0 0 0 20 -10 66 .00 27 16 | 0 -151 3201 7287
grg n/a| 1 -2 4 -21 52 -96 .20 24 22 | 178 67 3124 6797
iac n/a| 0 2 -7 -19 -70 -47 -.24 24 23 | 2752 -607 3140 8022
Table 2.2227.1 GPS week: 2227 Day: 1 MJD: 59834
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 1 2 -13 -30 -4 .02 13 11 | 38424 -3984 2668 7451
esx n/a| -1 4 2 49 20 32 -.11 30 24 | 8603 -2334 2657 10659
gfz n/a| -1 0 -1 27 -27 51 .06 28 16 | 0 -3084 2708 7374
grg n/a| 6 -1 5 -11 71 -95 .21 24 19 | 404 -3568 2665 6789
iac n/a| -2 -1 -14 -42 -28 20 -.33 27 26 | 3084 -1773 2732 9470
Table 2.2227.2 GPS week: 2227 Day: 2 MJD: 59835
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 -29 -35 80 .07 20 16 | 35968 -43 2625 8782
esx n/a| -3 2 6 2 17 12 -.09 31 21 | 8409 541 2628 11994
gfz n/a| -1 0 0 26 -5 69 .05 29 13 | 0 156 2656 8843
grg n/a| 4 -1 6 23 98 -188 .23 27 24 | -182 168 2601 8227
iac n/a| 1 0 -15 -8 3 12 -.34 26 26 | 2627 833 2631 10451
Table 2.2227.3 GPS week: 2227 Day: 3 MJD: 59836
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 4 -32 -25 19 .11 20 16 | 36427 -3255 2955 8161
esx n/a| 0 3 4 75 25 -4 -.18 29 21 | 7209 -2128 2940 10761
gfz n/a| -2 -1 -2 18 -10 50 .14 28 16 | 0 -2672 3006 7984
grg n/a| 3 -1 5 -10 69 -222 .25 28 23 | 322 -2507 2916 7724
iac n/a| 2 -1 -18 -12 -22 162 -.33 26 24 | 3007 -515 3064 10609
Table 2.2227.4 GPS week: 2227 Day: 4 MJD: 59837
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 1 -28 -22 56 .07 19 17 | 33521 -1583 3408 8160
esx n/a| 0 3 4 -2 35 -4 -.15 33 23 | 12341 -895 3391 11523
gfz n/a| -1 1 -2 35 17 72 -.01 23 18 | 0 -2004 3466 8035
grg n/a| 2 -4 9 1 64 -181 .24 27 20 | 89 -1843 3424 7776
iac n/a| 1 0 -10 -20 -38 27 -.23 22 21 | 2226 -493 3417 9716
Table 2.2227.5 GPS week: 2227 Day: 5 MJD: 59838
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 -5 -19 15 .14 19 14 | 25514 188 2318 7414
esx n/a| 1 2 3 25 72 39 -.24 31 26 | -15613 298 2297 10885
gfz n/a| -2 1 -2 -3 -14 83 .00 27 17 | 0 -603 2336 7064
grg n/a| 2 -1 7 7 78 -258 .27 28 24 | -7000 -82 2312 6845
iac n/a| 0 1 -12 -39 -63 52 -.26 23 19 | -3718 120 2422 9696
Table 2.2227.6 GPS week: 2227 Day: 6 MJD: 59839
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 -12 -26 64 .14 18 13 | 32603 -2325 2452 8040
esx n/a| 1 2 2 2 23 58 -.19 28 21 | 8626 -1742 2468 11473
gfz n/a| -1 0 -2 -27 0 47 .10 34 18 | 0 -2305 2526 7909
grg n/a| 3 -1 5 14 61 -170 .19 24 20 | 161 -2039 2453 7325
iac n/a| -1 1 -11 16 -14 -13 -.28 22 19 | 3370 -1038 2547 10188
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 3.2227.0 GPS week: 2227 Day: 0 MJD: 59833
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1353 30 86 12 17 19 19 | 134 49 111 119 124 110
R02 | 2126 7 16 23 18 30 10 | 109 99 111 106 122 109
R03 | 818 15 20 17 16 19 8 | 87 69 70 90 82 79
XR04 | 1052 10 22 --- 9 25 9 | 93 85 --- 92 103 93
R05 | 2081 14 24 20 18 15 9 | 84 85 90 95 92 87
R07 | 978 20 15 9 11 27 9 | 93 78 85 89 85 85
R08 | 2473 13 11 13 10 31 8 | 82 83 98 90 90 87
R09 | 1097 21 20 18 32 14 11 | 52 56 49 43 47 45
R11 | 1631 17 19 20 29 27 11 | 31 43 41 42 33 33
R12 | 981 13 16 21 12 31 9 | 73 71 77 74 73 72
R13 | 2884 15 46 26 52 19 16 | 74 58 74 93 83 75
R14 | 1107 11 23 7 14 16 7 | 54 69 57 57 49 55
R15 | 839 17 19 14 21 32 10 | 71 71 80 94 91 79
R17E | 1179 10 13 12 19 19 7 | 54 54 56 62 55 55
R18E | 934 7 13 14 18 22 7 | 66 67 69 75 63 67
R19E | 1177 39 46 60 32 38 22 | 72 83 110 93 80 80
R20E | 1206 21 59 70 39 28 23 | 96 94 137 101 97 99
R21E | 2142 9 12 13 12 14 6 | 156 156 160 161 159 158
R24E | 1664 9 15 28 18 17 9 | 138 138 143 142 142 139
XR25 |28035 --- --- --- --- 7 0 | --- --- --- --- --- 0
------+------------------------------------+--------------------------------
RMS | 1598 18 33 27 24 24 |T 85 79 89 90 87 84
WRMS | 1598 15 24 16 22 23 |NE 79 70 78 83 82 77
MEDI | 1179 14 19 17 18 19 |MD 82 71 80 92 85 80
Table 3.2227.1 GPS week: 2227 Day: 1 MJD: 59834
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 930 15 78 36 17 24 18 | 90 50 112 101 96 89
R02 | 1999 8 16 11 18 37 9 | 93 81 91 97 113 93
R03 | 1361 9 14 16 12 16 6 | 76 64 66 79 78 73
XR04 | 1646 7 11 --- 13 14 6 | 75 71 --- 81 73 75
R05 | 1172 15 21 16 21 32 10 | 61 71 77 85 84 71
R07 | 736 13 17 10 13 21 7 | 80 69 74 78 70 75
R08 | 1855 10 13 23 10 24 8 | 68 71 77 77 68 69
R09 | 1447 14 17 16 32 29 11 | 55 61 59 40 63 52
R11 | 1238 11 14 19 25 26 9 | 31 33 35 44 46 34
R12 | 793 9 13 9 15 14 6 | 63 58 60 63 69 62
R13 | 1811 11 38 24 42 20 14 | 67 55 66 73 69 64
R14 | 682 8 20 16 10 29 8 | 52 62 64 61 46 54
R15 | 628 9 11 11 18 18 6 | 63 69 69 71 66 67
R17E | 1040 8 14 20 13 20 7 | 66 64 70 62 77 66
R18E | 886 13 16 15 17 17 7 | 59 67 65 69 66 63
R19E | 873 27 48 65 42 45 22 | 77 91 110 82 93 81
R20E | 918 18 52 64 45 40 21 | 93 98 120 96 104 96
R21E | 1916 12 13 17 10 24 7 | 139 138 139 138 132 138
R24E | 2737 18 22 26 14 22 10 | 88 87 85 88 93 86
XR25 |24622 --- --- --- --- 10 0 | --- --- --- --- --- 0
------+------------------------------------+--------------------------------
RMS | 1396 13 30 28 24 27 |T 73 71 79 78 79 74
WRMS | 1396 11 24 16 19 26 |NE 67 62 70 73 72 67
MEDI | 1172 11 16 16 17 22 |MD 68 69 70 78 73 71
Table 3.2227.2 GPS week: 2227 Day: 2 MJD: 59835
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 713 34 70 19 26 21 18 | 96 52 75 89 71 75
R02 | 729 10 23 12 8 31 9 | 74 65 70 73 95 74
R03 | 939 5 21 15 15 21 8 | 72 62 63 80 86 71
XR04 | 943 10 15 --- 8 20 7 | 76 82 --- 76 91 79
R05 | 1344 14 22 21 14 39 11 | 61 65 55 66 93 64
R07 | 1271 11 25 15 13 20 8 | 76 65 80 81 95 78
R08 | 1095 19 14 40 15 13 11 | 64 67 100 71 64 72
R09 | 2254 14 10 13 37 22 10 | 53 56 54 37 64 50
R11 | 1083 23 30 18 30 26 12 | 23 50 29 64 58 39
R12 | 710 15 14 8 15 22 7 | 43 50 45 52 48 44
R13 | 743 28 44 19 57 23 18 | 64 28 60 72 49 51
R14 | 965 8 15 9 20 24 8 | 35 43 41 49 30 37
R15 | 954 15 9 16 22 18 8 | 50 63 49 68 67 57
R17E | 1038 9 14 17 12 20 7 | 62 62 63 68 56 61
R18E | 825 13 16 15 16 25 8 | 45 46 52 53 38 45
R19E | 1304 42 49 69 35 47 25 | 38 47 80 46 35 37
R20E | 1020 34 60 72 58 38 27 | 52 60 87 55 51 51
R21E | 1726 10 15 16 16 17 7 | 98 94 92 106 96 96
R24E | 3986 13 12 13 13 15 6 | 178 172 177 175 180 176
XR25 |17576 --- --- --- --- 10 0 | --- --- --- --- --- 0
------+------------------------------------+--------------------------------
RMS | 1473 20 31 29 27 26 |T 66 64 70 72 71 66
WRMS | 1473 16 21 13 24 26 |NE 60 57 60 67 70 60
MEDI | 1020 14 16 16 16 21 |MD 62 62 63 68 64 61
Table 3.2227.3 GPS week: 2227 Day: 3 MJD: 59836
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 953 41 73 25 24 31 21 | 112 59 90 94 108 89
R02 | 1247 13 20 9 16 15 7 | 65 58 66 78 71 66
R03 | 723 6 13 14 9 18 6 | 63 58 74 64 77 66
XR04 | 1297 12 13 --- 21 18 9 | 64 66 --- 50 72 62
R05 | 2200 14 17 28 20 18 10 | 60 75 87 57 71 67
R07 | 1980 9 23 15 22 24 9 | 81 69 75 96 95 81
R08 | 800 23 15 27 17 33 12 | 64 79 98 78 110 83
R09 | 2829 20 12 18 35 29 12 | 52 48 45 19 51 40
R11 | 1045 15 21 23 32 20 11 | 17 36 17 60 42 27
R12 | 521 17 18 27 15 29 11 | 36 46 55 52 33 41
R13 | 549 23 36 21 51 35 17 | 49 33 41 64 46 42
R14 | 758 6 10 11 16 15 6 | 38 40 37 47 36 38
R15 | 1100 7 12 15 18 23 7 | 55 52 56 68 54 55
R17E | 1230 9 12 11 11 16 6 | 68 70 75 65 73 69
R18E | 980 14 18 14 13 20 8 | 27 35 31 38 38 30
R19E | 1355 29 51 71 53 43 25 | 41 65 100 44 45 49
R20E | 935 39 50 50 57 33 23 | 56 51 81 58 48 47
R21E | 2263 10 14 21 13 15 7 | 76 81 87 79 85 80
R24E | 3106 17 11 19 14 33 10 | 101 105 109 100 83 98
XR25 |15074 --- --- --- --- 15 0 | --- --- --- --- --- 0
------+------------------------------------+--------------------------------
RMS | 1560 20 29 27 28 26 |T 59 59 68 63 65 59
WRMS | 1560 16 21 16 23 24 |NE 58 55 61 63 66 58
MEDI | 1100 14 17 19 18 20 |MD 60 58 74 64 71 62
Table 3.2227.4 GPS week: 2227 Day: 4 MJD: 59837
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 952 26 84 18 30 28 19 | 101 74 96 108 109 95
R02 | 1196 14 13 19 13 27 9 | 78 80 83 74 84 78
R03 | 627 12 14 10 17 20 7 | 76 70 73 74 76 73
XR04 | 1673 8 12 --- 24 21 10 | 84 82 --- 74 96 84
R05 | 2311 12 21 12 21 15 8 | 69 83 69 54 64 66
R07 | 1394 15 22 14 12 17 8 | 87 72 81 88 94 84
R08 | 703 26 25 17 16 31 12 | 78 71 87 92 98 84
R09 | 3097 19 16 19 36 16 11 | 45 50 51 28 44 40
R11 | 1611 21 13 10 18 25 9 | 27 35 29 38 39 28
R12 | 537 11 16 11 15 12 6 | 61 62 59 68 63 61
R13 | 824 33 52 41 41 11 18 | 59 45 50 54 54 48
R14 | 742 9 11 13 14 19 6 | 55 64 64 60 45 57
R15 | 1044 12 23 10 24 10 8 | 65 64 64 81 73 67
R17E | 1732 13 13 14 13 19 7 | 53 50 45 55 43 48
R18E | 702 16 17 20 20 25 10 | 57 63 65 59 60 60
R19E | 2382 23 52 49 42 24 19 | 50 83 84 74 63 62
R20E | 1883 36 56 45 61 42 23 | 74 79 104 90 70 76
R21E | 1943 13 21 16 18 16 8 | 131 125 131 126 128 128
R24E | 3723 13 13 17 17 19 8 | 125 120 122 128 127 124
XR25 |13390 --- --- --- --- 7 0 | --- --- --- --- --- 0
------+------------------------------------+--------------------------------
RMS | 1758 19 33 23 27 22 |T 72 72 75 75 75 71
WRMS | 1758 17 23 18 20 21 |NE 68 65 67 68 72 66
MEDI | 1394 14 17 16 18 19 |MD 69 71 69 74 70 67
Table 3.2227.5 GPS week: 2227 Day: 5 MJD: 59838
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 615 19 74 15 28 25 17 | 85 45 73 98 94 79
R02 | 1160 11 17 9 14 10 6 | 60 56 66 67 61 61
R03 | 690 6 16 12 17 14 6 | 59 53 65 70 62 61
XR04 | 1534 8 20 --- 25 13 9 | 70 69 --- 62 69 66
R05 | 1665 15 22 13 25 18 9 | 60 60 57 42 65 55
R07 | 562 6 21 12 11 20 7 | 63 58 67 67 70 64
R08 | 788 18 24 13 22 22 10 | 61 57 73 88 80 70
R09 | 3685 20 17 29 39 20 12 | 62 58 61 44 57 53
R11 | 2733 21 17 14 24 22 10 | 25 35 34 31 26 21
R12 | 631 9 21 11 14 12 6 | 48 45 47 50 41 44
R13 | 518 32 44 20 41 34 17 | 52 29 36 42 44 38
R14 | 843 10 14 11 12 12 6 | 34 31 30 33 30 29
R15 | 529 6 27 17 23 22 9 | 48 38 52 55 42 44
R17E | 1903 9 13 17 18 17 7 | 42 45 45 46 45 43
R18E | 798 12 22 23 15 20 9 | 49 52 58 58 40 49
R19E | 1697 33 42 65 54 38 23 | 36 59 70 62 47 42
R20E | 1440 39 53 67 55 42 25 | 71 54 86 70 48 57
R21E | 1995 13 19 14 16 14 7 | 145 155 144 149 149 147
R24E | 3178 17 14 16 16 17 8 | 108 108 110 113 112 110
XR25 |14527 --- --- --- --- 9 0 | --- --- --- --- --- 0
------+------------------------------------+--------------------------------
RMS | 1698 19 31 27 28 23 |T 62 58 65 65 62 59
WRMS | 1698 14 26 17 24 19 |NE 55 48 55 57 57 52
MEDI | 1160 13 21 14 22 18 |MD 60 54 61 62 57 55
Table 3.2227.6 GPS week: 2227 Day: 6 MJD: 59839
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac IGL | cod esx gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 521 22 68 23 20 33 18 | 132 70 127 124 143 120
R02 | 1299 10 15 9 15 18 7 | 89 85 91 100 104 93
R03 | 1047 9 18 20 26 12 8 | 85 76 75 102 81 83
XR04 | 1433 7 14 --- 18 13 7 | 90 89 --- 87 86 87
R05 | 833 15 20 22 10 18 8 | 79 69 64 72 87 74
R07 | 752 10 9 14 15 13 6 | 88 79 80 83 89 84
R08 | 1263 12 16 11 12 24 8 | 91 91 109 101 119 101
R09 | 2582 18 16 18 36 22 11 | 70 66 62 50 75 62
R11 | 3156 14 15 26 40 21 12 | 35 46 40 37 48 36
R12 | 849 14 10 19 9 20 7 | 66 64 76 68 71 67
R13 | 929 24 34 27 36 22 14 | 75 50 73 74 65 66
R14 | 742 11 12 14 12 11 6 | 52 54 47 55 42 48
R15 | 455 8 17 17 21 18 8 | 75 67 83 88 68 75
R17E | 1885 7 8 10 15 13 5 | 57 58 55 60 62 57
R18E | 809 16 16 18 12 17 8 | 64 71 71 72 70 68
R19E | 1016 35 37 64 34 37 20 | 73 67 103 80 71 71
R20E | 1530 39 59 103 44 40 29 | 114 103 148 112 104 106
R21E | 969 12 19 20 14 20 8 | 200 209 212 206 201 205
R24E | 4030 14 17 30 15 10 8 | 133 131 138 136 131 133
XR25 |11186 --- --- --- --- 8 0 | --- --- --- --- --- 0
------+------------------------------------+--------------------------------
RMS | 1661 18 28 34 24 22 |T 87 81 91 89 90 86
WRMS | 1661 13 21 18 20 19 |NE 79 69 77 80 82 76
MEDI | 1016 14 16 19 15 18 |MD 79 70 76 83 81 75
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