[IGSREPORT-25482] Wk 1962 IGLOS Final Orbits
acc
acc at igs.org
Sun Sep 3 20:28:53 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1962 (Aug 13, 2017 - Aug 19, 2017)
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 2.1962.
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:
igl1962[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1962 in the SP3 format.
igl19627.sum Combination Report for GPS Week 1962.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://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 | 1.3 ns
1 | -0.7 ns
2 | 1.4 ns
3 | -0.8 ns
4 | 0.8 ns
5 | 0.2 ns
6 | -1.1 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 1.1962, 1a.1962).
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 2.1962.0-6)
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 3.1962.0-6).
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 1962 summary. (Aug 13, 2017 - Aug 19, 2017)
Table 1.1962.a GPS week : 1962 MJD: 57978.0-57984.0
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 11 -19 -8 -4 .01 40 38 | 11567 -250 3092 11229
| 1 2 2 24 12 49 .04 | 1270 2379
cof n/a| -1 1 14 -16 -3 9 .02 43 39 | 11569 -265 3092 11229
| 1 1 5 22 23 69 .05 | 1271 2392
emx n/a| -1 0 0 6 -14 57 .07 24 23 | 3244 -633 3116 10486
| 1 1 1 27 27 32 .04 | 4923 1392
esx n/a| 0 0 -2 -12 19 1 .18 16 14 | -3429 -506 3108 13302
| 1 0 1 13 10 27 .01 | 8260 2578
gfz n/a| 0 0 -8 -17 41 44 .13 26 21 | 0 -15 3111 11131
| 0 0 1 11 25 10 .06 | 0 1897
grg n/a| 0 0 5 -61 2 -119 -.35 28 25 | 101 29 3100 10395
| 0 0 4 14 21 58 .05 | 198 2022
iac n/a| 0 0 -1 81 -41 7 -.15 21 21 | 1273 -493 3111 10386
| 0 1 1 44 46 41 .02 | 816 1095
mcc n/a| 1 -2 29 91 -127 314 -.29 117 117 | --- --- --- ---
| 5 9 7 64 80 388 .21 | --- ---
Table 1.1962.b GPS week : 1962 MJD: 57978.0-57984.0
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 16 13 16 16 14 15 |
R02 | 11 13 10 9 10 10 11 |
R03 | 9 9 11 11 9 9 9 |
R04 | 10 9 9 10 8 8 9 |
R05 | 16 12 15 12 11 13 15 |
R06 | 11 11 11 10 10 11 10 |
R07 | 11 11 10 11 10 11 12 |
R08 | 11 9 10 11 9 9 10 |
R09 | 9 8 8 7 6 7 6 |
R10 | 9 9 8 7 7 8 8 |
R11 | 7 8 8 7 7 7 7 |
R13 | 10 8 7 8 8 9 7 |
R15 | 10 9 9 10 11 11 12 |
R16 | 14 11 14 11 14 15 17 |
R17 | 11 11 10 9 11 10 9 |
R18 | 7 7 8 8 8 7 9 |
R19 | 13 12 12 11 13 10 13 |
R20 | 13 14 14 16 14 11 14 |
R21 | 11 9 10 9 8 10 9 |
R22 | 10 9 10 9 8 9 11 |
R23 | 7 8 8 11 9 10 7 |
R24 | 15 14 14 13 16 16 21 |
R26 | 15 16 0 23 36 16 19 |
Table 1.1962.c GPS week : 1962 MJD: 57978.0-57984.0
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 1962 0 | 0 13 106 128 178 839 85.2 1435 1435 | 1272 0
brd 1962 1 | 26 -11 172 290 278 1595 85.2 1494 1494 | -703 0
brd 1962 2 | 22 -20 180 -94 1075 1424 84.4 1142 1142 | 1372 0
brd 1962 3 | -21 47 133 196 870 2880 82.4 1107 1107 | -779 0
brd 1962 4 | 28 76 140 174 -825 3102 82.6 1246 1246 | 786 0
brd 1962 5 | -1 -31 218 334 -2157 2278 84.5 1311 1311 | 201 0
brd 1962 6 | 71 21 162 336 -2492 3741 83.2 1329 1329 | -1062 0
-------------+------------------------------------------------------------+----------------
brd 1962 mean| 18 13 159 195 -438 2265 83.9 1294 1294 | 155 0
brd 1962 sdev| 29 39 36 151 1427 1036 1.2 142 142 | 1018 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 2.1962.0 GPS week: 1962 Day: 0 MJD: 57978
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 9 -28 -15 57 .08 39 36 | 9826 1674 3161 10299
cof n/a| -4 1 7 -17 -20 45 .11 45 38 | 9820 1685 3165 10297
emx n/a| -2 0 1 7 -12 37 .12 22 21 | 4968 -195 3193 9425
esx n/a| 2 0 -4 -3 15 38 .19 19 17 | 1215 2924 3192 11761
gfz n/a| -1 1 -8 -9 33 38 .02 26 23 | 0 1652 3184 10188
grg n/a| 0 0 4 -47 -6 -164 -.29 27 24 | 235 1866 3162 9120
iac n/a| 1 -1 -3 78 -42 15 -.13 23 22 | 2206 -75 3187 9588
mcc n/a| -2 -6 36 103 -9 118 -.04 118 118 | --- --- --- ---
Table 2.1962.1 GPS week: 1962 Day: 1 MJD: 57979
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 13 -22 -20 64 .03 41 40 | 10554 -2220 2928 11692
cof n/a| -2 0 22 6 5 142 .05 46 43 | 10571 -2264 2926 11695
emx n/a| -1 -1 0 -32 17 95 .06 24 24 | 7901 -2046 2948 11042
esx n/a| 0 0 -3 1 34 34 .20 16 15 | -4353 -3877 2945 13423
gfz n/a| 0 0 -5 -11 75 62 .14 25 20 | 0 -1936 2945 11655
grg n/a| -1 0 0 -51 38 -192 -.37 26 26 | 261 -1980 2931 10802
iac n/a| 0 0 0 81 -123 -36 -.17 18 18 | 1012 -2215 2941 10885
mcc n/a| 5 -4 43 36 -221 320 -.21 120 120 | --- --- --- ---
Table 2.1962.2 GPS week: 1962 Day: 2 MJD: 57980
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 13 -27 4 4 .06 38 37 | 11535 3126 3045 11736
cof n/a| 0 1 15 -37 40 -34 .04 39 37 | 11526 3130 3048 11738
emx n/a| -3 0 -4 14 5 41 .11 23 23 | 368 2143 3062 10843
esx n/a| 2 0 -1 -4 21 -16 .17 17 15 | 7468 2843 3037 13920
gfz n/a| 0 0 -8 -18 8 38 .11 24 19 | 0 2217 3048 11630
grg n/a| 0 0 7 -64 23 -56 -.39 28 25 | -175 2842 3048 10972
iac n/a| 1 0 -3 33 -47 10 -.16 19 19 | 2269 58 3049 10900
mcc n/a| 2 14 32 77 -74 -194 -.22 158 158 | --- --- --- ---
Table 2.1962.3 GPS week: 1962 Day: 3 MJD: 57981
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 14 -38 -5 -41 -.00 39 35 | 13453 -3788 2767 10667
cof n/a| 0 4 20 -38 -24 -41 .03 43 36 | 13458 -3808 2763 10666
emx n/a| 0 -1 -1 25 -18 87 .10 21 21 | 9812 -1730 2779 10131
esx n/a| 0 0 0 -5 4 5 .18 15 13 | 2130 -2708 2783 13102
gfz n/a| 0 0 -10 -9 21 32 .14 27 17 | 0 -2102 2787 10567
grg n/a| 0 0 9 -48 -13 -183 -.42 28 26 | 313 -2243 2777 9898
iac n/a| 0 0 -1 24 27 55 -.17 21 21 | 1015 -1461 2788 9894
mcc n/a| -4 5 22 61 -64 72 -.68 113 113 | --- --- --- ---
Table 2.1962.4 GPS week: 1962 Day: 4 MJD: 57982
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 3 11 -19 -21 -33 -.01 39 36 | 11850 357 3357 11165
cof n/a| 0 1 9 -31 -26 -30 -.01 43 38 | 11846 343 3351 11163
emx n/a| 0 0 0 43 4 89 .09 21 19 | -106 -434 3387 10447
esx n/a| -1 0 -3 -31 11 2 .18 16 14 | -15247 -995 3369 13543
gfz n/a| 0 0 -10 -8 26 45 .15 27 19 | 0 1320 3384 11039
grg n/a| 0 0 6 -54 -5 -101 -.30 26 21 | 211 974 3381 10635
iac n/a| 0 0 0 89 -3 -59 -.14 22 22 | 824 826 3382 10338
mcc n/a| -3 -9 26 78 -188 223 -.43 86 86 | --- --- --- ---
Table 2.1962.5 GPS week: 1962 Day: 5 MJD: 57983
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 8 -36 -10 -18 -.02 43 39 | 12824 559 3000 12838
cof n/a| -2 0 11 -18 5 32 .01 44 40 | 12833 535 3006 12843
emx n/a| -1 -1 0 12 -59 21 .05 25 23 | 4100 -870 3021 12057
esx n/a| 0 0 0 -32 29 -32 .18 14 12 | -2008 -1192 3016 15507
gfz n/a| -1 0 -8 -41 68 53 .20 26 26 | 0 649 3016 12766
grg n/a| 0 0 0 -81 -1 -71 -.35 27 26 | -21 444 3010 12030
iac n/a| 1 2 -2 155 -50 46 -.16 19 19 | 1617 414 3020 11807
mcc n/a| 10 -12 24 230 -200 894 -.19 102 102 | --- --- --- ---
Table 2.1962.6 GPS week: 1962 Day: 6 MJD: 57984
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| -5 -2 8 34 9 -63 -.04 43 41 | 10927 -1458 3386 10209
cof n/a| -3 -1 16 21 -2 -51 -.06 45 43 | 10933 -1477 3386 10207
emx n/a| -1 1 0 -29 -38 26 .00 29 27 | -4334 -1300 3425 9459
esx n/a| 0 0 -3 -9 18 -22 .18 15 13 | -13212 -539 3416 11861
gfz n/a| 0 0 -10 -18 54 42 .17 24 20 | 0 -1907 3413 10075
grg n/a| 0 1 9 -78 -20 -68 -.37 32 28 | -112 -1698 3392 9314
iac n/a| 0 0 -1 110 -48 17 -.15 23 23 | -26 -998 3411 9293
mcc n/a| 3 -4 22 54 -133 768 -.24 121 121 | --- --- --- ---
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 3.1962.0 GPS week: 1962 Day: 0 MJD: 57978
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 817 73 81 22 19 50 37 34 --- 16 | 90 101 45 37 37 62 28 --- 38
R02 | 1042 54 59 19 15 25 20 24 75 11 | 95 96 60 47 37 65 41 50 52
R03 | 1428 37 38 16 6 25 19 25 64 9 | 86 85 60 54 44 65 37 62 54
R04 | 901 34 39 16 12 23 14 31 --- 9 | 78 81 56 50 40 56 33 --- 48
R05 | 1758 54 48 15 36 31 50 31 --- 16 | 77 74 39 47 32 55 31 --- 39
R06 | 2047 13 14 28 31 9 27 16 --- 11 | 55 60 44 82 58 40 59 --- 57
R07 | 1025 46 53 17 9 24 31 25 162 11 | 98 103 65 54 44 68 44 63 57
R08 | 1341 36 47 21 14 37 27 18 --- 11 | 95 103 73 63 47 75 52 --- 64
R09E | 2407 13 16 15 24 17 21 21 --- 8 | 21 24 26 28 36 22 29 --- 23
R10E | 921 11 14 21 21 13 26 11 --- 8 | 55 52 44 63 41 48 50 --- 49
R11E | 1061 22 21 10 15 15 15 10 172 6 | 74 75 55 56 46 61 53 116 55
R13E | 1620 27 24 22 22 16 28 19 --- 10 | 68 66 43 63 51 60 52 --- 53
R15E | 3123 54 59 14 12 29 11 18 --- 10 | 67 72 37 31 34 30 22 --- 30
R16E | 1260 25 24 35 26 26 39 25 --- 13 | 74 79 54 73 62 56 61 --- 58
R17 | 949 43 50 14 13 27 29 24 --- 10 | 54 60 36 40 26 42 21 --- 32
R18 | 745 21 27 14 17 10 15 14 --- 6 | 46 50 32 45 38 25 26 --- 33
R19 | 1444 55 46 25 22 27 13 29 --- 12 | 67 64 55 53 34 47 28 --- 43
R20 | 809 36 64 38 24 16 33 12 --- 12 | 64 70 53 43 37 37 36 --- 38
R21 | 950 39 44 22 10 29 14 29 68 10 | 58 61 49 37 31 39 38 52 38
R22 | 1403 42 39 16 14 23 14 24 --- 9 | 62 63 46 43 34 38 31 --- 38
R23 | 650 11 16 14 13 29 14 12 --- 7 | 30 41 34 45 45 26 29 --- 33
R24 | 1141 36 72 37 16 38 43 28 --- 15 | 54 72 58 40 38 42 26 --- 38
XR26 | ---- 20 47 --- --- --- --- 10 --- 14 | 16 34 --- --- --- --- 29 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1434 39 45 22 19 26 27 23 118 |T 64 68 48 49 40 48 37 68 43
WRMS | 1434 36 38 21 17 23 24 22 118 |NE 66 71 50 48 38 48 34 56 42
MEDI | 1061 36 44 17 15 25 21 24 75 |MD 67 70 46 47 38 47 33 62 39
Table 3.1962.1 GPS week: 1962 Day: 1 MJD: 57979
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 955 76 64 32 20 39 40 22 --- 15 | 70 61 35 40 39 48 22 --- 32
R02 | 1135 50 49 28 14 38 28 24 117 12 | 68 69 53 39 30 59 30 84 41
R03 | 1911 34 33 22 9 24 22 19 64 9 | 61 63 53 38 40 49 31 66 41
R04 | 872 34 37 21 9 21 18 19 --- 8 | 56 56 45 36 33 40 27 --- 35
R05 | 1384 45 59 19 17 30 39 19 --- 12 | 50 71 32 42 37 42 25 --- 33
R06 | 1842 21 21 24 29 11 35 11 --- 11 | 48 47 37 58 45 31 43 --- 42
R07 | 1460 52 54 26 12 32 21 14 148 10 | 76 78 56 47 34 38 35 46 43
R08 | 1613 41 36 21 7 15 19 22 --- 8 | 76 73 55 53 51 55 43 --- 51
R09E | 2145 13 18 17 12 16 22 17 --- 7 | 22 31 23 22 30 25 18 --- 18
R10E | 713 15 19 30 23 16 17 10 --- 9 | 34 38 29 44 33 37 31 --- 33
R11E | 1098 32 37 13 14 23 24 11 161 8 | 59 60 47 37 46 53 42 125 43
R13E | 651 17 16 13 18 20 23 12 --- 8 | 47 50 33 51 53 31 32 --- 39
R15E | 3349 50 45 19 9 30 17 10 --- 9 | 38 40 21 29 32 28 21 --- 22
R16E | 1197 23 37 28 19 26 32 21 --- 11 | 40 58 44 43 46 34 39 --- 37
R17 | 647 48 54 25 14 33 16 19 --- 10 | 27 35 21 32 32 23 19 --- 20
R18 | 867 25 34 15 11 18 16 14 --- 7 | 30 37 28 31 32 28 17 --- 25
R19 | 1387 48 55 25 16 23 23 33 --- 12 | 39 49 37 44 47 44 20 --- 35
R20 | 620 68 97 42 18 29 33 11 --- 14 | 53 77 48 44 48 35 31 --- 36
R21 | 1187 38 43 15 16 25 13 24 80 9 | 28 31 27 30 23 25 22 58 22
R22 | 2438 41 52 17 11 19 12 26 --- 9 | 35 39 34 29 32 24 21 --- 26
R23 | 669 13 22 17 20 14 17 13 --- 7 | 23 21 33 30 31 25 14 --- 24
R24 | 1318 41 41 38 20 29 45 14 --- 13 | 39 66 51 43 48 24 25 --- 33
XR26 | ---- 23 55 --- --- --- --- 12 --- 15 | 26 52 --- --- --- --- 31 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1493 41 46 24 16 25 26 18 120 |T 45 52 38 39 38 36 27 75 33
WRMS | 1493 40 43 24 15 20 26 18 120 |NE 47 54 40 39 37 36 26 63 33
MEDI | 1187 38 41 21 14 23 22 17 117 |MD 40 52 35 39 34 34 27 66 33
Table 3.1962.2 GPS week: 1962 Day: 2 MJD: 57980
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 670 69 80 21 17 20 33 19 --- 12 | 76 87 31 41 36 55 33 --- 36
R02 | 1137 42 43 22 8 29 22 17 146 9 | 69 69 42 43 29 52 31 96 39
R03 | 1440 38 37 22 12 38 23 22 69 11 | 63 62 43 38 30 56 25 42 36
R04 | 565 36 31 11 15 25 22 12 --- 8 | 57 55 36 42 33 44 32 --- 37
R05 | 907 48 43 31 22 32 55 16 --- 15 | 77 73 41 55 45 64 48 --- 50
R06 | 1395 18 20 29 25 11 32 14 --- 10 | 49 53 34 69 51 48 56 --- 52
R07 | 1585 45 45 25 8 22 18 26 153 10 | 75 76 50 47 33 54 31 65 43
R08 | 1006 38 40 15 11 26 33 22 --- 10 | 74 76 48 47 45 62 39 --- 46
R09E | 2034 15 16 20 14 14 21 15 --- 7 | 19 18 21 26 25 22 22 --- 18
R10E | 659 14 17 21 21 19 13 13 --- 8 | 48 47 34 52 40 43 36 --- 41
R11E | 1221 24 30 19 12 21 22 7 261 7 | 52 62 33 44 35 56 35 165 39
R13E | 1840 15 15 19 15 16 17 10 --- 7 | 54 50 41 49 39 58 48 --- 46
R15E | 697 41 44 14 9 25 21 16 --- 8 | 47 52 31 30 21 27 25 --- 26
R16E | 687 27 36 24 32 16 47 27 --- 13 | 68 74 44 71 51 51 47 --- 52
R17 | 580 40 39 18 16 28 22 20 --- 10 | 32 33 28 32 20 21 17 --- 20
R18 | 874 28 31 13 16 24 12 17 --- 8 | 31 36 23 33 24 23 17 --- 22
R19 | 957 57 58 28 20 22 24 23 --- 12 | 56 54 43 40 38 39 29 --- 35
R20 | 854 61 53 39 19 26 36 19 --- 14 | 64 53 54 45 34 42 41 --- 41
R21 | 726 41 42 17 15 30 13 18 87 9 | 38 40 33 34 25 30 25 62 27
R22 | 1276 34 38 13 16 28 16 24 --- 9 | 43 44 33 40 24 40 22 --- 31
R23 | 839 13 20 24 11 16 21 21 --- 8 | 35 36 38 35 40 46 36 --- 35
R24 | 1495 17 22 42 17 24 49 17 --- 13 | 50 38 48 43 40 21 20 --- 32
XR26 | ---- --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 34 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1142 38 39 23 17 24 28 19 158 |T 53 54 37 43 34 43 32 86 36
WRMS | 1142 37 37 23 15 19 25 19 158 |NE 55 55 39 42 34 43 31 66 36
MEDI | 907 36 37 21 15 24 22 17 146 |MD 52 53 36 42 34 44 32 65 36
Table 3.1962.3 GPS week: 1962 Day: 3 MJD: 57981
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 659 80 88 17 22 51 45 15 --- 16 | 91 101 34 31 36 63 31 --- 33
R02 | 776 36 44 15 12 23 21 18 127 8 | 77 85 43 48 42 61 43 69 47
R03 | 993 34 40 24 12 30 18 30 78 10 | 73 77 49 49 32 56 31 38 43
R04 | 708 39 47 17 8 28 15 28 --- 9 | 68 74 40 40 24 49 27 --- 36
R05 | 785 35 51 20 15 35 35 27 --- 11 | 73 92 61 57 64 57 35 --- 52
R06 | 1801 25 27 19 26 15 23 10 --- 9 | 46 46 51 78 58 48 65 --- 60
R07 | 1151 47 41 25 10 21 28 29 90 11 | 86 80 57 53 37 50 33 38 48
R08 | 847 33 30 14 9 30 39 26 --- 11 | 85 86 58 63 60 83 45 --- 61
R09E | 1935 12 17 13 8 13 24 13 --- 6 | 29 32 24 29 33 43 25 --- 26
R10E | 846 11 11 19 9 17 17 16 --- 6 | 50 54 45 47 41 56 44 --- 44
R11E | 1207 26 22 11 13 25 14 13 171 7 | 61 56 41 45 39 50 38 101 42
R13E | 1608 14 23 22 14 26 17 16 --- 8 | 54 60 46 59 41 57 57 --- 51
R15E | 822 42 28 17 14 28 30 18 --- 10 | 54 50 30 30 28 39 23 --- 25
R16E | 752 33 43 17 17 20 35 27 --- 10 | 74 80 52 60 46 45 52 --- 50
R17 | 589 37 42 13 11 19 17 24 --- 8 | 46 48 39 44 45 29 31 --- 36
R18 | 1346 27 28 17 18 18 15 14 --- 8 | 29 30 26 36 33 24 25 --- 26
R19 | 1179 50 46 25 8 40 14 24 --- 11 | 47 48 36 36 36 40 29 --- 33
R20 | 862 65 77 31 15 33 55 22 --- 15 | 63 72 39 44 43 36 29 --- 36
R21 | 565 44 44 16 11 22 19 13 61 8 | 44 44 38 43 37 34 32 41 35
R22 | 1513 46 43 19 9 26 16 16 --- 9 | 46 42 30 34 31 31 28 --- 29
R23 | 796 10 18 24 28 13 31 16 --- 10 | 26 32 26 34 25 30 30 --- 24
R24 | 1107 26 43 40 16 21 44 18 --- 13 | 37 64 34 32 40 28 24 --- 25
XR26 | ---- 34 131 --- --- --- --- 15 --- 22 | 35 138 --- --- --- --- 52 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 1106 39 43 21 15 27 28 21 113 |T 56 64 40 45 39 45 36 57 39
WRMS | 1106 35 36 21 13 17 26 21 113 |NE 57 68 41 45 40 44 34 46 39
MEDI | 847 34 42 17 12 23 21 18 90 |MD 54 60 39 44 37 45 31 41 36
Table 3.1962.4 GPS week: 1962 Day: 4 MJD: 57982
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 778 89 90 19 15 38 42 35 --- 16 | 114 117 76 77 76 90 70 --- 76
R02 | 533 49 43 18 6 34 11 22 107 9 | 104 103 83 85 83 90 76 75 83
R03 | 1969 34 39 18 11 18 25 25 85 9 | 94 97 84 79 74 89 72 74 79
R04 | 1280 36 45 17 7 24 14 15 --- 7 | 82 89 68 75 78 73 70 --- 72
R05 | 917 36 29 16 19 31 33 24 --- 11 | 85 81 75 84 79 85 69 --- 77
R06 | 1354 33 32 18 25 13 18 18 --- 9 | 70 68 71 81 75 78 81 --- 75
R07 | 887 49 57 22 12 26 15 22 65 10 | 102 105 84 80 75 80 73 70 79
R08 | 1045 32 39 14 16 17 15 24 --- 8 | 101 106 83 95 82 90 75 --- 86
R09E | 2354 10 11 15 6 11 16 19 --- 6 | 74 73 83 77 82 72 75 --- 77
R10E | 1095 19 24 18 15 17 16 13 --- 7 | 76 76 69 76 75 76 70 --- 72
R11E | 1252 30 31 14 8 24 16 14 108 7 | 83 81 74 72 73 75 73 81 73
R13E | 854 23 17 14 16 22 18 14 --- 7 | 91 89 88 101 99 85 81 --- 91
R15E | 1862 49 52 19 13 26 25 22 --- 10 | 72 78 74 73 70 66 68 --- 69
R16E | 683 26 29 34 19 27 42 31 --- 13 | 79 86 76 80 72 70 72 --- 72
R17 | 599 45 45 23 12 39 22 24 --- 11 | 73 75 68 68 75 73 62 --- 67
R18 | 674 28 29 16 19 20 15 12 --- 8 | 69 70 66 66 64 63 60 --- 63
R19 | 1588 43 43 35 17 42 18 26 --- 13 | 75 77 72 71 61 72 67 --- 68
R20 | 714 45 57 23 19 33 40 35 --- 13 | 90 91 76 85 79 85 58 --- 76
R21 | 792 38 53 13 10 26 13 13 50 7 | 78 84 74 80 82 75 68 62 75
R22 | 1786 31 35 10 10 12 18 25 --- 7 | 68 73 67 73 76 73 63 --- 69
R23 | 1122 11 18 20 21 22 22 13 --- 9 | 61 61 63 67 54 68 60 --- 62
R24 | 1123 33 45 34 24 35 55 24 --- 15 | 74 76 70 75 71 63 65 --- 65
XR26 | ---- 55 92 --- --- --- --- 21 --- 35 | 70 102 --- --- --- --- 72 --- 69
------+---------------------------------------------------+-----------------------------------------------
RMS | 1245 39 43 21 16 27 26 22 86 |T 81 85 74 78 75 76 69 72 73
WRMS | 1245 36 38 19 14 19 21 22 86 |NE 82 86 73 77 74 77 68 70 73
MEDI | 1045 34 39 18 15 24 18 22 85 |MD 78 81 74 77 75 75 70 74 73
Table 3.1962.5 GPS week: 1962 Day: 5 MJD: 57983
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 619 98 96 19 8 36 33 20 --- 14 | 148 145 126 132 139 138 122 --- 130
R02 | 673 52 52 22 8 25 17 25 123 10 | 141 143 129 138 134 135 122 118 132
R03 | 1875 40 35 24 4 32 14 15 107 8 | 137 136 131 134 133 135 125 122 131
R04 | 1769 32 28 13 7 21 24 12 --- 7 | 140 139 129 134 142 143 125 --- 134
R05 | 803 41 45 31 20 28 35 25 --- 12 | 146 154 139 152 153 141 126 --- 142
R06 | 771 36 43 29 28 14 23 11 --- 11 | 132 137 133 146 139 130 128 --- 136
R07 | 1287 53 54 19 10 27 31 18 99 10 | 148 148 138 137 138 141 124 133 135
R08 | 1764 45 41 13 7 32 21 15 --- 8 | 148 146 130 135 137 136 127 --- 133
R09E | 2321 12 15 15 7 17 20 17 --- 6 | 116 119 116 118 125 122 119 --- 119
R10E | 660 22 19 25 15 11 16 12 --- 7 | 138 137 121 134 133 131 128 --- 130
R11E | 1561 25 26 15 10 21 17 10 112 6 | 133 133 125 134 135 131 123 138 130
R13E | 1970 18 22 15 14 35 17 23 --- 9 | 131 132 132 134 141 129 121 --- 131
R15E | 1048 62 61 20 15 29 20 25 --- 11 | 137 138 129 139 145 132 124 --- 133
R16E | 973 43 43 48 17 25 48 26 --- 15 | 143 135 136 142 134 138 132 --- 137
R17 | 743 39 44 24 9 35 16 22 --- 9 | 129 130 129 125 124 126 119 --- 124
R18 | 584 26 38 19 10 22 15 11 --- 7 | 132 131 135 130 130 130 124 --- 130
R19 | 1468 43 40 23 10 29 20 22 --- 9 | 128 126 125 124 125 131 123 --- 125
R20 | 673 32 22 24 22 22 28 22 --- 10 | 123 128 130 129 130 131 122 --- 127
R21 | 1285 41 33 19 12 36 27 20 55 10 | 134 133 130 133 134 129 122 130 129
R22 | 1749 42 46 26 11 24 16 19 --- 9 | 140 142 139 144 142 133 127 --- 137
R23 | 1016 11 17 24 24 8 35 11 --- 10 | 127 129 118 128 133 134 124 --- 126
R24 | 921 45 64 47 20 21 52 24 --- 15 | 132 136 114 136 130 119 117 --- 124
XR26 | ---- 23 42 --- --- --- --- 13 --- 16 | 119 137 --- --- --- --- 123 --- 126
------+---------------------------------------------------+-----------------------------------------------
RMS | 1310 43 44 25 14 26 27 19 102 |T 134 136 128 134 135 132 123 128 130
WRMS | 1310 39 40 23 12 26 26 19 102 |NE 135 137 129 134 135 133 123 125 130
MEDI | 1016 40 41 22 10 25 20 19 107 |MD 134 136 129 134 134 131 124 130 130
Table 3.1962.6 GPS week: 1962 Day: 6 MJD: 57984
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 656 89 85 34 20 29 29 23 --- 15 | 215 215 170 188 188 187 180 --- 184
R02 | 1279 58 61 29 9 20 21 16 108 10 | 202 200 193 188 189 193 180 193 188
R03 | 895 46 43 18 8 26 17 20 104 9 | 194 192 189 184 181 184 175 169 183
R04 | 1276 32 38 20 7 30 21 14 --- 8 | 190 194 176 185 184 180 175 --- 181
R05 | 941 41 37 21 12 27 54 42 --- 14 | 211 216 201 213 218 208 193 --- 206
R06 | 1034 25 25 28 20 8 34 16 --- 10 | 187 187 188 197 192 179 184 --- 189
R07 | 1103 54 55 23 8 30 23 31 122 11 | 195 197 185 182 179 182 172 173 180
R08 | 1414 49 45 23 10 29 22 14 --- 10 | 200 200 185 181 180 183 176 --- 181
R09E | 1371 14 15 12 8 12 21 9 --- 5 | 168 165 175 175 180 178 175 --- 175
R10E | 740 17 32 20 17 16 24 13 --- 8 | 182 190 175 187 184 185 178 --- 182
R11E | 1144 30 29 12 12 18 16 11 180 6 | 191 190 180 184 183 177 181 198 182
R13E | 720 19 21 20 12 13 15 18 --- 7 | 196 194 186 194 191 189 187 --- 190
R15E | 3384 62 71 19 12 32 23 24 --- 11 | 185 188 180 178 180 182 175 --- 178
R16E | 857 56 60 59 27 22 44 28 --- 17 | 207 204 197 192 192 192 185 --- 191
R17 | 783 37 37 25 9 21 19 23 --- 9 | 187 186 192 188 184 179 178 --- 184
R18 | 616 18 15 24 14 25 20 17 --- 8 | 181 182 182 187 182 172 171 --- 180
R19 | 1049 57 61 30 11 33 25 27 --- 12 | 198 195 187 184 184 191 180 --- 185
R20 | 917 27 32 41 19 24 57 18 --- 14 | 194 195 186 178 180 191 177 --- 181
R21 | 2122 40 47 19 7 28 20 19 57 9 | 176 176 181 178 176 183 177 175 178
R22 | 1830 48 50 27 10 23 30 19 --- 10 | 181 180 184 184 187 178 174 --- 181
R23 | 1037 16 13 21 16 13 16 12 --- 7 | 190 191 194 197 198 196 185 --- 193
R24 | 912 34 38 63 32 25 76 43 --- 21 | 183 179 175 194 186 186 178 --- 183
XR26 | ---- 29 89 --- --- --- --- 12 --- 18 | 182 206 --- --- --- --- 177 --- 181
------+---------------------------------------------------+-----------------------------------------------
RMS | 1328 43 45 29 15 24 32 23 121 |T 191 192 184 187 186 185 178 181 184
WRMS | 1328 41 43 27 13 20 28 23 121 |NE 192 193 185 188 186 185 178 177 184
MEDI | 1034 37 38 23 12 24 22 18 108 |MD 190 192 185 185 184 183 178 175 182
More information about the IGSREPORT
mailing list