[IGSREPORT-29080] Wk 2237 IGLOS Final Orbits
acc
acc at igs.org
Wed Dec 14 00:35:15 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2237 (Nov 20, 2022 - Nov 26, 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 2.2237.
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:
igl2237[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2237 in the SP3 format.
igl22377.sum Combination Report for GPS Week 2237.
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 | -1.2 ns
1 | -12.2 ns
2 | -1.3 ns
3 | -14.4 ns
4 | 0.8 ns
5 | 0.4 ns
6 | -2.3 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESX | R22
1 | ESX | R22
2 | ESX | R22
3 | ESX | R22
5 | ESX | R22
6 | ESX | R22
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 1.2237, 1a.2237).
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 2.2237.0-6)
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 3.2237.0-6).
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 2237 summary. (Nov 20, 2022 - Nov 26, 2022)
Table 1.2237.a GPS week : 2237 MJD: 59903.0-59909.0
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| 0 0 2 0 -8 23 .11 24 17 | 29465 -1568 3001 8445
| 1 1 2 9 13 25 .05 | 6707 2038
emx n/a| 0 1 -3 26 3 -6 -.00 43 27 | -12252 -1239 2998 8374
| 2 1 2 22 19 31 .05 | 12514 1601
esx n/a| 0 1 1 4 7 -6 -.11 32 23 | -19858 -784 3354 97015
| 1 0 1 11 9 33 .03 | 61600 1678
gfz n/a| 1 3 3 17 49 -87 .00 45 36 | 0 -1491 3003 8605
| 5 3 2 25 15 38 .17 | 0 2244
grg n/a| 0 -5 -1 -21 -3 -4 .18 28 21 | -42266 -795 9595 178973
| 1 0 3 29 16 25 .06 | 67711 2273
iac n/a| 1 2 0 -7 -12 19 -.22 31 28 | -39971 -50 7991 177218
| 1 1 1 20 26 74 .05 | 65128 1341
Table 1.2237.b GPS week : 2237 MJD: 59903.0-59909.0
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 | 17 18 14 18 15 13 17 |
R02 | 7 7 8 7 8 6 7 |
R03 | 7 7 8 8 9 7 8 |
R04 | 8 10 9 11 10 8 9 |
R05 | 9 8 10 11 13 10 9 |
R07 | 8 7 10 8 9 8 9 |
R08 | 9 10 10 9 9 9 9 |
R09 | 10 11 11 14 16 12 18 |
R11 | 11 8 10 15 13 8 9 |
R12 | 9 9 11 10 12 10 10 |
R13 | 16 18 18 18 16 19 17 |
R14 | 8 10 11 12 10 8 14 |
R15 | 9 12 13 12 12 9 9 |
R17 | 9 10 9 10 10 8 8 |
R18 | 9 9 10 13 11 10 9 |
R19 | 30 33 33 32 29 28 33 |
R20 | 36 32 32 34 28 24 28 |
R21 | 9 12 10 12 22 8 8 |
R22 | 22 13 16 31 39 18 12 |
R24 | 10 10 10 13 10 9 9 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2237.c GPS week : 2237 MJD: 59903.0-59909.0
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 2237 0 | 66 62 -6 1383 3358 2840 81.9 1570 1570 | -1195 0
brd 2237 1 | 19 47 -54 1867 682 6260 81.3 1642 1642 | -12151 0
brd 2237 2 | -56 43 -91 -138 1581 -2283 81.3 1530 1530 | -1274 0
brd 2237 3 | -83 -28 -152 1006 903 -4120 80.7 1698 1698 | -14424 0
brd 2237 4 | 34 -97 -70 830 106 -5847 80.0 1523 1523 | 842 0
brd 2237 5 | 35 -19 34 1105 483 -3766 82.2 1379 1379 | 406 0
brd 2237 6 | -12 62 34 521 565 -788 82.2 1645 1645 | -2282 0
-------------+------------------------------------------------------------+----------------
brd 2237 mean| 0 10 -43 939 1097 -1100 81.4 1569 1569 | -4296 0
brd 2237 sdev| 54 60 69 637 1095 4280 .8 106 106 | 6266 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 2.2237.0 GPS week: 2237 Day: 0 MJD: 59903
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 4 -12 -30 27 .11 22 14 | 36421 -3768 3334 8897
emx n/a| 0 0 -1 34 -10 -45 -.03 42 25 | -12950 -2942 3336 8827
esx n/a| -1 1 3 -5 0 -29 -.10 38 23 | 10130 -3079 3295 10863
gfz n/a| 5 0 1 13 69 -102 .10 35 27 | 0 -3051 3338 9068
grg n/a| 0 -4 -5 5 26 -19 .24 28 23 | -6 -3097 3310 8706
iac n/a| 3 3 0 7 -12 122 -.30 29 25 | 240 -1225 3249 9792
Table 2.2237.1 GPS week: 2237 Day: 1 MJD: 59904
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 1 -4 0 1 .07 24 17 | 22201 -1489 2664 9523
emx n/a| 4 0 -7 36 -11 -44 -.01 48 28 | -29127 -1753 2640 9504
esx n/a| -3 1 0 -5 0 0 -.13 37 22 | -11969 -1093 2718 6706
gfz n/a| -7 0 0 19 21 -60 .28 38 25 | 0 -1914 2655 9736
grg n/a| 0 -4 1 -2 4 20 .05 27 20 | -11543 -1719 2770 9100
iac n/a| 3 2 0 11 -32 41 -.22 26 24 | -11031 -203 2717 10257
Table 2.2237.2 GPS week: 2237 Day: 2 MJD: 59905
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 6 15 -8 26 .10 24 19 | 32915 -2774 3303 8019
emx n/a| 2 0 0 66 12 -2 .06 48 29 | 12145 -2024 3293 7869
esx n/a| 0 0 1 18 -1 52 -.12 31 27 | -1158 -1208 3240 7453
gfz n/a| 3 11 1 -7 48 -99 .05 43 39 | 0 -2781 3295 8147
grg n/a| -3 -4 -4 -18 3 -49 .16 30 21 | -269 -2363 3294 7288
iac n/a| -1 0 -1 -39 4 -47 -.18 30 29 | 652 -1665 3225 9107
Table 2.2237.3 GPS week: 2237 Day: 3 MJD: 59906
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 4 7 6 -4 .11 26 19 | 17998 -2175 3090 7486
emx n/a| 0 3 -3 2 -11 38 -.08 42 29 | -9514 -976 3103 7313
esx n/a| 0 2 1 15 10 9 -.16 35 28 | -158434 -1501 3142 623431
gfz n/a| 0 0 2 17 42 -64 .04 46 35 | 0 -1951 3102 7549
grg n/a| 0 -5 -4 -9 -23 14 .19 29 17 | -157304 -1835 3155 626066
iac n/a| 0 3 1 -15 22 -71 -.27 39 40 | -149516 -1030 3093 611567
Table 2.2237.4 GPS week: 2237 Day: 4 MJD: 59907
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 0 -22 54 .05 25 17 | 31748 1992 2983 8480
emx n/a| 0 1 -5 2 -13 1 .01 40 28 | -16609 1147 2965 8379
esx n/a| 0 0 0 8 25 -52 -.12 31 26 | 10081 1835 2972 11169
gfz n/a| -1 3 4 64 48 -150 -.05 50 40 | 0 2561 2985 8581
grg n/a| 1 -5 0 -54 -6 0 .21 25 20 | -122998 2488 46678 581568
iac n/a| 0 4 0 -28 12 99 -.18 44 36 | -118982 617 35891 577528
Table 2.2237.5 GPS week: 2237 Day: 5 MJD: 59908
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 0 1 -4 0 .16 23 18 | 33475 280 2895 8316
emx n/a| -2 0 -4 30 23 -12 -.01 37 25 | -11761 638 2888 8270
esx n/a| 0 1 0 10 10 -18 -.07 26 18 | 5142 1075 4173 11118
gfz n/a| 8 3 5 24 65 -32 -.18 51 49 | 0 500 2927 8554
grg n/a| 1 -6 2 -70 -14 -15 .21 23 18 | -2435 2388 4108 11275
iac n/a| 0 4 -2 6 -34 27 -.22 23 19 | -784 1803 3998 12223
Table 2.2237.6 GPS week: 2237 Day: 6 MJD: 59909
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 1 -5 2 56 .20 23 15 | 31500 -3045 2740 8397
emx n/a| 1 1 -2 14 33 20 .07 45 26 | -17948 -2765 2767 8460
esx n/a| 1 0 1 -12 9 -3 -.07 28 18 | 7201 -1520 3942 8365
gfz n/a| 1 4 7 -12 49 -105 -.22 50 36 | 0 -3803 2725 8600
grg n/a| 0 -5 0 2 -14 19 .20 36 25 | -1312 -1432 3852 8813
iac n/a| 0 1 -2 9 -48 -34 -.20 25 21 | -382 1347 3770 10052
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 3.2237.0 GPS week: 2237 Day: 0 MJD: 59903
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 824 40 24 49 39 29 33 16 | 158 154 153 144 146 135 147
R02 | 1232 13 11 15 16 16 20 7 | 52 47 55 45 41 52 47
R03M | 646 8 13 11 20 13 27 7 | 63 64 60 64 61 73 63
R04M | 1147 13 16 12 19 11 30 7 | 77 75 74 76 67 68 71
R05 | 763 14 17 20 32 9 21 8 | 62 57 57 76 55 49 56
R07 | 1034 6 12 12 36 13 18 7 | 65 60 64 80 60 73 64
R08 | 1059 12 15 21 30 20 22 9 | 60 59 76 83 60 78 66
R09E | 3843 16 23 20 34 19 18 9 | 87 84 91 102 83 93 87
R11E | 2566 14 17 16 30 37 30 11 | 23 30 32 35 42 39 28
R12E | 1290 10 22 15 39 16 15 8 | 155 145 148 155 148 152 150
R13E | 944 29 46 41 48 18 27 15 | 51 31 54 79 52 45 45
R14E | 2206 10 24 19 26 12 18 8 | 88 89 82 90 88 77 84
R15E | 1117 11 31 12 35 14 22 9 | 135 133 134 149 138 122 134
R17M | 1072 7 33 16 25 9 23 8 | 70 48 64 76 72 83 68
R18 | 470 10 20 29 24 19 18 9 | 59 51 72 72 59 68 61
R19 | 2295 39 127 58 52 69 43 29 | 109 46 62 120 111 112 90
R20 | 1222 62 88 125 63 67 67 35 | 142 65 94 131 127 134 107
R21M | 556 9 30 17 26 11 25 8 | 71 56 63 76 69 81 68
XR22 | 5305 --- --- 323 --- 20 22 21 | --- --- 110 --- 109 102 106
R24M | 1272 11 35 15 35 18 25 10 | 69 63 70 73 68 79 68
XR25M |12958 --- --- --- --- --- 8 0 | --- --- --- --- --- 44 44
------+-----------------------------------------+-------------------------------------
RMS | 1569 22 42 38 35 28 29 |T 84 71 80 90 82 83 78
WRMS | 1569 14 25 23 27 23 25 |NE 88 67 82 93 85 89 82
MEDI | 1147 12 23 17 32 16 22 |MD 70 60 70 79 68 78 68
Table 3.2237.1 GPS week: 2237 Day: 1 MJD: 59904
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1274 51 34 52 26 32 28 18 | 158 138 155 156 150 146 149
R02 | 563 14 10 13 21 9 24 7 | 38 40 43 33 34 35 34
R03M | 711 10 12 8 28 14 16 6 | 49 51 50 59 44 50 48
R04M | 1227 11 14 16 22 26 29 9 | 58 59 57 72 39 61 54
R05 | 604 11 16 13 34 8 23 8 | 43 49 41 67 37 38 41
R07 | 835 9 20 17 22 8 13 6 | 43 41 37 43 42 42 40
R08 | 1328 20 20 26 34 9 17 9 | 33 41 55 49 45 50 42
R09E | 4009 16 23 24 38 15 29 10 | 77 70 93 90 81 99 83
R11E | 2886 14 23 11 33 18 15 8 | 28 28 34 57 38 37 33
R12E | 1358 12 29 17 32 16 22 9 | 85 72 87 78 92 83 82
R13E | 1253 40 44 29 66 31 30 17 | 47 41 43 79 58 45 40
R14E | 2526 15 29 18 45 10 12 9 | 90 96 89 95 89 92 89
R15E | 1238 10 32 22 51 14 26 11 | 125 120 130 148 127 130 128
R17M | 627 9 37 17 32 22 15 9 | 36 25 35 52 47 39 37
R18 | 568 15 28 21 24 13 24 9 | 37 26 32 42 36 45 35
R19 | 2090 37 145 63 55 83 41 32 | 66 45 38 71 50 65 52
R20 | 1402 57 97 115 51 42 46 31 | 81 49 63 90 81 70 67
R21M | 800 9 38 21 30 12 42 11 | 41 34 36 42 43 76 43
XR22 | 3807 --- --- 319 --- 12 13 13 | --- --- 81 --- 77 66 72
R24M | 984 10 36 8 41 16 19 9 | 42 50 45 60 42 46 43
XR25M |15743 --- --- --- --- --- 4 0 | --- --- --- --- --- 49 50
------+-----------------------------------------+-------------------------------------
RMS | 1641 24 48 37 38 27 26 |T 61 56 62 72 62 64 60
WRMS | 1641 17 28 22 25 20 24 |NE 62 53 60 68 61 61 59
MEDI | 1253 14 29 18 33 14 23 |MD 47 49 45 67 45 50 48
Table 3.2237.2 GPS week: 2237 Day: 2 MJD: 59905
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1103 32 32 30 20 23 37 13 | 79 88 66 78 69 68 68
R02 | 792 14 15 16 22 15 23 7 | 38 31 42 51 35 31 34
R03M | 988 11 14 7 36 13 24 8 | 52 44 56 66 60 51 53
R04M | 553 13 11 8 36 17 26 8 | 59 51 51 56 50 62 53
R05 | 892 17 16 19 28 24 27 9 | 44 43 40 47 33 53 38
R07 | 846 13 18 10 35 15 41 10 | 45 40 46 72 54 84 53
R08 | 1054 20 18 16 37 15 25 9 | 40 33 46 63 43 58 44
R09E | 4009 17 24 13 23 19 48 11 | 70 82 82 87 78 87 77
R11E | 2676 14 25 11 44 26 20 10 | 16 24 27 58 40 31 24
R12E | 839 12 35 17 33 16 35 10 | 76 69 81 81 76 64 73
R13E | 642 43 45 31 65 39 25 18 | 49 28 42 73 41 42 36
R14E | 951 18 24 17 64 15 11 11 | 49 52 53 78 56 50 48
R15E | 1289 13 34 20 71 19 25 13 | 99 99 105 129 102 111 103
R17M | 901 11 33 11 36 20 15 9 | 46 34 46 62 49 48 45
R18 | 676 17 32 20 31 15 23 10 | 41 34 48 46 53 46 44
R19 | 2352 45 137 63 58 90 37 32 | 89 59 60 93 79 83 69
R20 | 1394 54 107 96 66 52 44 32 | 99 38 55 125 106 94 80
R21M | 1347 14 29 13 32 13 32 9 | 49 37 44 49 40 42 41
XR22 | 2107 --- --- 304 --- 16 15 16 | --- --- 86 --- 100 60 84
R24M | 1123 14 40 15 28 18 24 10 | 53 45 48 58 42 51 45
XR25M |12962 --- --- --- --- --- 4 0 | --- --- --- --- --- 34 34
------+-----------------------------------------+-------------------------------------
RMS | 1530 24 48 31 43 30 30 |T 57 49 56 72 60 59 54
WRMS | 1530 19 29 27 39 21 29 |NE 59 45 54 71 63 64 57
MEDI | 1054 14 29 16 36 17 25 |MD 49 43 48 66 53 53 48
Table 3.2237.3 GPS week: 2237 Day: 3 MJD: 59906
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1218 39 16 52 37 37 38 17 | 76 62 64 77 60 69 62
R02 | 662 4 10 11 24 12 30 6 | 37 34 41 38 35 50 36
R03M | 1871 7 10 15 32 12 29 7 | 45 44 46 56 55 43 46
R04M | 624 10 16 20 46 11 43 10 | 50 49 45 69 49 65 49
R05 | 1091 16 25 28 44 18 19 11 | 39 45 50 59 33 47 38
R07 | 901 12 15 17 27 10 24 7 | 47 45 35 57 40 46 42
R08 | 534 16 12 22 40 13 22 9 | 35 35 43 58 45 39 38
R09E | 4338 17 21 20 42 15 67 13 | 83 88 92 100 93 104 88
R11E | 3412 25 36 13 38 43 39 14 | 19 27 41 57 79 50 39
R12E | 1445 10 25 14 40 14 30 9 | 65 55 63 79 69 71 64
R13E | 1164 28 50 24 78 24 39 17 | 43 43 37 93 42 39 39
R14E | 783 14 24 18 61 19 23 11 | 34 33 38 63 43 28 31
R15E | 1794 17 25 20 53 15 38 12 | 146 139 157 172 149 147 149
R17M | 672 11 33 11 35 14 37 10 | 62 45 57 62 62 82 59
R18 | 1010 14 32 28 41 14 46 12 | 46 40 60 61 49 75 50
R19 | 1669 65 107 65 59 75 43 32 | 115 50 64 114 112 107 88
R20 | 1667 54 103 104 70 62 26 33 | 106 54 35 133 121 90 81
R21M | 1020 21 29 11 30 15 56 12 | 61 46 55 69 58 77 55
XR22 | 6147 --- --- 298 --- 22 41 30 | --- --- 98 --- 59 69 62
R24M | 915 9 42 13 23 13 60 12 | 54 51 58 60 58 86 55
XR25M |14193 --- --- --- --- --- 6 0 | --- --- --- --- --- 43 46
------+-----------------------------------------+-------------------------------------
RMS | 1697 26 42 35 46 29 39 |T 61 51 58 77 65 67 57
WRMS | 1697 19 29 28 35 17 40 |NE 62 45 54 74 61 65 55
MEDI | 1164 16 25 20 40 15 38 |MD 50 45 50 63 58 69 50
Table 3.2237.4 GPS week: 2237 Day: 4 MJD: 59907
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1113 38 27 43 36 30 24 15 | 77 83 83 78 69 68 71
R02 | 751 12 9 7 38 14 24 7 | 34 26 30 49 29 51 31
R03M | 2109 7 10 13 41 11 39 8 | 35 33 32 45 33 63 33
R04M | 644 15 26 21 44 10 28 10 | 54 60 38 55 45 51 46
R05 | 891 22 16 27 52 21 42 12 | 43 32 43 69 23 30 29
R07 | 1009 10 11 10 47 19 21 8 | 48 45 45 72 38 47 43
R08 | 660 12 14 26 30 9 33 9 | 35 41 53 56 33 41 38
R09E | 3013 22 28 22 79 23 52 15 | 78 71 82 93 83 88 74
R11E | 3316 14 17 14 68 33 36 13 | 14 21 26 64 60 32 25
R12E | 1459 14 27 15 68 14 19 11 | 65 62 70 92 64 66 64
R13E | 1173 23 57 28 52 23 43 16 | 32 44 35 65 34 45 28
R14E | 948 10 25 25 30 12 31 9 | 45 49 44 58 50 55 45
R15E | 760 15 26 19 73 11 28 12 | 117 113 125 140 119 108 117
R17M | 685 15 29 17 25 8 48 10 | 52 34 37 48 45 67 43
R18 | 1156 11 32 31 37 14 25 11 | 39 34 54 49 47 51 42
R19 | 1205 50 102 52 59 65 40 28 | 85 65 56 97 84 84 71
R20 | 1772 66 83 77 60 35 44 28 | 94 35 39 78 80 64 61
R21M | 1113 18 40 39 35 28 123 22 | 57 52 50 54 62 142 55
XR22 | 6925 --- --- --- --- 27 58 39 | --- --- --- --- 82 43 70
R24M | 1566 17 29 16 32 11 28 9 | 45 35 44 43 46 44 40
XR25M |21650 --- --- --- --- --- 7 0 | --- --- --- --- --- 28 28
------+-----------------------------------------+-------------------------------------
RMS | 1523 25 40 31 50 25 44 |T 55 49 51 68 56 60 50
WRMS | 1523 17 28 26 40 20 36 |NE 56 45 50 68 53 53 50
MEDI | 1156 15 27 22 44 14 33 |MD 48 44 44 64 47 51 43
Table 3.2237.5 GPS week: 2237 Day: 5 MJD: 59908
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 970 35 21 31 45 27 18 13 | 54 54 47 58 51 48 48
R02 | 1214 10 16 11 29 14 12 6 | 27 25 30 45 31 36 28
R03M | 1469 9 14 12 43 11 14 7 | 42 41 36 51 43 33 37
R04M | 678 9 18 14 51 11 12 7 | 49 48 58 69 52 56 51
R05 | 1282 18 18 19 58 13 16 9 | 34 32 38 58 34 33 29
R07 | 585 7 11 15 44 17 18 8 | 40 34 40 63 31 48 37
R08 | 715 10 16 12 42 21 22 8 | 33 33 37 60 27 38 32
R09E | 2559 26 24 27 46 24 26 12 | 88 87 97 111 102 93 91
R11E | 1968 15 20 9 38 18 15 8 | 17 25 24 44 24 20 19
R12E | 1036 9 22 18 58 15 23 10 | 101 100 104 122 109 87 100
R13E | 2020 27 48 32 107 33 32 18 | 31 41 32 93 39 42 24
R14E | 924 10 22 17 40 16 12 8 | 67 75 71 83 70 73 70
R15E | 779 14 26 14 28 17 20 8 | 165 165 166 168 164 168 165
R17M | 1066 11 31 12 35 11 17 8 | 38 28 35 54 34 32 33
R18 | 933 15 27 31 46 11 13 10 | 33 28 38 49 34 26 30
R19 | 945 50 105 42 68 67 41 27 | 40 41 61 79 48 44 42
R20 | 1717 53 67 68 66 18 46 23 | 50 50 59 79 39 47 44
R21M | 1595 12 30 16 35 15 13 8 | 44 39 42 58 46 43 41
XR22 | 6212 --- --- 312 --- 18 18 18 | --- --- 185 --- 166 166 162
R24M | 1777 18 31 14 40 14 17 9 | 68 71 75 84 72 67 69
XR25M |21658 --- --- --- --- --- 5 0 | --- --- --- --- --- 28 30
------+-----------------------------------------+-------------------------------------
RMS | 1379 23 37 26 51 23 23 |T 53 53 63 75 60 58 56
WRMS | 1379 18 25 18 49 18 19 |NE 38 37 59 61 51 54 50
MEDI | 1214 14 22 16 44 16 17 |MD 42 41 42 63 43 44 41
Table 3.2237.6 GPS week: 2237 Day: 6 MJD: 59909
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 888 39 35 27 30 54 32 16 | 89 85 75 86 80 81 78
R02 | 1527 9 15 9 36 21 12 7 | 39 36 39 42 29 39 35
R03M | 1441 7 14 14 31 23 15 7 | 113 110 111 116 121 128 115
R04M | 705 16 20 20 39 12 14 8 | 71 61 67 67 61 73 66
R05 | 1414 15 15 16 48 10 12 8 | 47 42 54 67 44 42 45
R07 | 910 10 15 13 55 17 20 9 | 60 57 55 92 52 73 60
R08 | 919 12 21 20 35 16 15 8 | 46 48 62 63 47 60 52
R09E | 2930 32 28 23 92 30 38 17 | 59 73 71 112 57 79 62
R11E | 2008 18 22 9 27 34 14 9 | 28 29 30 44 43 35 29
R12E | 696 11 28 11 38 18 27 9 | 142 134 139 137 140 145 140
R13E | 1410 35 55 27 51 49 27 17 | 34 51 31 53 49 36 28
R14E | 1838 17 37 20 79 32 23 14 | 102 104 100 127 104 103 100
R15E | 1063 12 24 17 34 19 25 9 | 157 151 161 156 162 167 159
R17M | 1523 8 26 16 32 23 12 8 | 69 47 62 76 74 72 65
R18 | 437 10 25 27 29 21 13 9 | 57 45 71 64 62 64 59
R19 | 834 42 141 64 81 90 44 33 | 110 54 79 131 125 108 95
R20 | 1511 44 82 76 68 65 44 27 | 123 95 105 149 120 112 103
R21M | 1330 10 23 10 42 12 10 7 | 80 61 76 91 79 83 76
XR22 | 5182 --- --- 317 --- 14 9 11 | --- --- 156 --- 192 180 184
R24M | 3896 13 23 10 36 21 21 8 | 157 156 150 155 155 160 154
XR25M |17204 --- --- --- --- --- 4 0 | --- --- --- --- --- 30 31
------+-----------------------------------------+-------------------------------------
RMS | 1645 23 45 28 50 36 25 |T 83 75 84 96 89 89 82
WRMS | 1645 15 26 18 36 25 21 |NE 71 57 77 86 83 84 79
MEDI | 1414 13 24 17 38 21 15 |MD 71 61 71 91 74 79 66
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