[IGSREPORT-25290] Wk 1948 IGLOS Final Orbits
acc
acc at igs.org
Sun May 28 04:06:41 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1948 (May 07, 2017 - May 13, 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 2.1948.
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:
igl1948[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1948 in the SP3 format.
igl19487.sum Combination Report for GPS Week 1948.
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 | 0.2 ns
1 | 0.9 ns
2 | -0.7 ns
3 | -13.1 ns
4 | -12.2 ns
5 | 0.3 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 1.1948, 1a.1948).
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 2.1948.0-6)
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 3.1948.0-6).
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 1948 summary. (May 07, 2017 - May 13, 2017)
Table 1.1948.a GPS week : 1948 MJD: 57880.0-57886.0
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 19 0 0 7 .15 38 36 | 4751 903 3243 11756
| 1 1 0 14 45 41 .06 | 7860 1935
cof n/a| 0 1 22 -4 9 17 .16 39 36 | 4748 901 3244 11758
| 2 1 1 16 45 50 .06 | 7861 1947
emx n/a| 0 0 4 -4 -16 16 .10 23 22 | -9063 884 3241 11051
| 1 0 2 16 29 28 .04 | 10595 1066
esx n/a| 0 0 0 12 13 -12 .10 15 14 | -18961 -356 3236 14060
| 0 1 1 15 19 28 .03 | 14807 2441
gfz n/a| -1 0 -9 -1 68 27 .02 25 24 | 0 322 3247 11527
| 1 1 1 40 20 33 .08 | 0 1899
grg n/a| 1 0 0 -81 3 -74 -.33 28 25 | -3074 -708 3252 11185
| 0 1 2 13 8 40 .05 | 5950 3203
iac n/a| 1 0 -7 59 -45 57 -.10 21 21 | -2268 -146 3235 10933
| 1 1 2 47 34 66 .02 | 6603 824
mcc n/a| 4 -2 15 94 -46 207 -.33 155 155 | --- --- --- ---
| 9 5 24 66 107 719 .33 | --- ---
Table 1.1948.b GPS week : 1948 MJD: 57880.0-57886.0
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 | 14 12 13 12 10 11 11 |
R02 | 8 9 6 7 8 7 7 |
R03 | 12 11 9 9 10 10 8 |
R04 | 8 10 10 9 9 10 9 |
R05 | 15 15 16 14 14 15 14 |
R06 | 8 8 8 10 7 7 8 |
R07 | 10 10 10 8 11 12 9 |
R08 | 8 8 8 9 10 10 9 |
R09 | 9 6 6 6 7 8 8 |
R10 | 10 11 10 8 9 10 8 |
R11 | 9 7 7 9 10 9 8 |
R13 | 9 10 7 7 9 9 10 |
R14 | 17 15 14 15 16 15 16 |
R15 | 12 9 9 9 10 11 8 |
R16 | 14 14 18 15 14 21 16 |
R17 | 9 10 8 8 8 9 9 |
R18 | 8 7 8 7 7 7 9 |
R19 | 14 13 12 13 12 12 12 |
R20 | 13 13 14 14 12 14 12 |
R21 | 9 9 9 9 8 7 9 |
R22 | 10 9 10 10 10 8 9 |
R23 | 10 11 10 9 11 11 11 |
R24 | 11 13 13 13 15 16 11 |
R26 | 37 28 19 23 16 14 14 |
Table 1.1948.c GPS week : 1948 MJD: 57880.0-57886.0
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 1948 0 | 24 -5 277 -571 -1042 2931 86.5 1151 1151 | 158 0
brd 1948 1 | -8 -31 250 -339 -1914 2442 86.1 1159 1159 | 903 0
brd 1948 2 | 55 -7 307 422 1601 4280 86.5 1226 1226 | -723 0
brd 1948 3 | 28 28 252 109 -346 3479 86.6 1236 1236 | -13129 0
brd 1948 4 | 36 10 230 -167 -1276 3924 84.9 1189 1189 | -12235 0
brd 1948 5 | -18 -4 226 -827 -963 1273 87.8 1049 1049 | 264 0
brd 1948 6 | 9 34 319 -619 -827 3264 88.5 1047 1047 | 722 0
-------------+------------------------------------------------------------+----------------
brd 1948 mean| 18 3 266 -284 -681 3084 86.7 1151 1151 | -3434 0
brd 1948 sdev| 25 22 36 440 1112 1003 1.2 77 77 | 6343 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 2.1948.0 GPS week: 1948 Day: 0 MJD: 57880
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 2 19 20 5 34 .06 38 35 | 7874 -544 3124 11528
cof n/a| -3 2 21 -2 44 62 .07 36 34 | 7876 -553 3123 11529
emx n/a| 1 1 6 -19 -42 3 .13 23 20 | -7795 352 3120 10886
esx n/a| -1 -2 0 0 25 -1 .13 15 13 | -25959 -3525 3128 13803
gfz n/a| -2 0 -12 -52 99 46 -.12 26 22 | 0 -938 3130 11437
grg n/a| 2 0 1 -70 15 -72 -.30 32 30 | 223 -748 3128 11442
iac n/a| 3 0 -12 109 -95 -19 -.09 24 24 | 1306 -819 3122 10753
mcc n/a| -9 2 -15 128 -162 -1195 -.91 206 206 | --- --- --- ---
Table 2.1948.1 GPS week: 1948 Day: 1 MJD: 57881
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 20 -14 39 21 .09 39 36 | 8083 1529 3328 12703
cof n/a| 0 -1 22 11 49 43 .07 42 38 | 8083 1519 3329 12707
emx n/a| -1 0 1 -3 -34 50 .03 22 21 | -20345 1471 3327 11680
esx n/a| 0 0 0 39 30 -5 .07 15 14 | -7767 -766 3319 14928
gfz n/a| -3 0 -9 45 84 43 .03 26 25 | 0 905 3321 12522
grg n/a| 1 0 1 -101 5 -75 -.38 31 26 | 316 1132 3316 12141
iac n/a| 3 0 -8 2 -83 -15 -.10 24 24 | 1739 137 3315 11823
mcc n/a| 10 -8 -8 10 11 -251 -.50 240 240 | --- --- --- ---
Table 2.1948.2 GPS week: 1948 Day: 2 MJD: 57882
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 19 -13 62 5 .17 38 35 | 8232 -1173 3128 11442
cof n/a| 0 0 22 -35 47 33 .17 40 36 | 8233 -1181 3129 11445
emx n/a| -2 0 2 9 -35 15 .07 24 24 | -21359 -505 3126 10526
esx n/a| -1 1 2 -1 -15 -19 .09 13 11 | 10354 -3687 3124 13402
gfz n/a| 2 0 -12 -1 82 -10 -.01 25 23 | 0 -2072 3126 11182
grg n/a| 0 0 -2 -80 2 -62 -.37 29 28 | 383 -2033 3210 10589
iac n/a| 1 -1 -3 49 -19 41 -.07 19 19 | 940 -536 3124 10492
mcc n/a| 16 -6 -8 125 89 330 .09 143 143 | --- --- --- ---
Table 2.1948.3 GPS week: 1948 Day: 3 MJD: 57883
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 2 20 -3 25 -79 .11 37 37 | -6383 923 2923 11359
cof n/a| 3 3 22 -3 35 -86 .17 38 37 | -6381 915 2917 11360
emx n/a| 0 0 2 1 -37 0 .09 26 24 | -8975 1001 2916 10840
esx n/a| 0 0 1 12 -10 -31 .08 12 11 | -26959 1126 2913 13765
gfz n/a| -2 0 -7 -22 60 -14 .15 26 25 | 0 119 2910 10731
grg n/a| 1 1 0 -82 0 -54 -.37 31 29 | -9418 -6891 2932 10856
iac n/a| 1 -2 -7 39 0 108 -.09 19 19 | -12423 868 2908 10581
mcc n/a| -4 2 24 200 -48 331 -.28 118 118 | --- --- --- ---
Table 2.1948.4 GPS week: 1948 Day: 4 MJD: 57884
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 2 18 19 -30 0 .23 38 38 | -6742 4744 3252 12133
cof n/a| -1 4 20 -3 -21 8 .22 41 40 | -6757 4767 3258 12133
emx n/a| 0 0 5 -33 31 55 .15 26 25 | 5798 2868 3266 11443
esx n/a| -1 0 0 12 19 30 .13 17 16 | -27512 2564 3250 14336
gfz n/a| -1 -2 -9 -33 45 59 .03 27 24 | 0 3958 3252 11482
grg n/a| 1 2 3 -97 11 -150 -.29 23 21 | -13760 3364 3204 11532
iac n/a| 0 -1 -4 123 -55 48 -.08 18 18 | -11393 734 3256 11303
mcc n/a| 1 2 35 106 -215 826 -.42 132 132 | --- --- --- ---
Table 2.1948.5 GPS week: 1948 Day: 5 MJD: 57885
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| -4 0 20 -1 -32 44 .19 36 34 | 10352 -66 3866 11917
cof n/a| -1 0 24 -14 -57 56 .20 37 34 | 10352 -83 3864 11918
emx n/a| 0 0 6 13 -15 14 .11 22 22 | 3147 378 3858 11279
esx n/a| 0 1 1 24 13 -1 .12 17 17 | -28139 357 3851 14291
gfz n/a| 0 0 -9 56 48 65 .02 26 24 | 0 -437 3919 12139
grg n/a| 1 0 -3 -62 -2 -89 -.25 24 22 | 329 -275 3927 11865
iac n/a| 1 0 -4 10 -30 73 -.11 21 21 | 1778 -1398 3847 11063
mcc n/a| 4 -10 41 20 17 789 -.09 111 111 | --- --- --- ---
Table 2.1948.6 GPS week: 1948 Day: 6 MJD: 57886
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 18 -10 -65 29 .20 38 34 | 11843 908 3084 11215
cof n/a| -1 1 24 14 -32 1 .22 40 36 | 11832 926 3094 11217
emx n/a| 0 1 5 -2 14 -26 .08 20 20 | -13913 628 3074 10704
esx n/a| 0 0 0 0 33 -60 .09 16 15 | -26748 1437 3069 13895
gfz n/a| -1 -1 -7 0 60 0 .03 22 24 | 0 720 3075 11200
grg n/a| 0 0 0 -78 -7 -14 -.34 26 24 | 404 493 3050 9874
iac n/a| 1 1 -8 85 -36 166 -.13 20 20 | 2176 -8 3074 10520
mcc n/a| 10 -1 38 69 -17 622 -.18 135 135 | --- --- --- ---
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 3.1948.0 GPS week: 1948 Day: 0 MJD: 57880
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 | 637 66 40 22 15 35 32 35 --- 14 | 2 4 3 3 5 3 5 --- 3
R02 | 904 16 13 15 6 25 30 21 270 8 | 3 6 4 4 4 5 4 9999 3
R03 | 1312 33 32 24 11 35 33 30 118 11 | 2 4 3 7 7 6 3 3 4
R04 | 1089 27 30 17 7 20 22 17 --- 7 | 2 2 2 2 6 3 2 --- 2
R05 | 771 30 24 25 22 25 65 28 --- 14 | 2 3 2 3 3 6 3 --- 2
R06 | 1322 25 30 18 15 23 20 15 --- 8 | 3 4 3 8 5 4 2 --- 4
R07 | 799 39 42 24 10 34 16 18 234 10 | 2 3 3 5 4 3 2 22 3
R08 | 1417 31 31 16 4 21 13 20 --- 7 | 2 2 2 2 4 1 2 --- 1
XR09 | 1912 18 19 12 16 20 --- 22 --- 9 | 2 3 3 2 3 --- 2 --- 2
R10 | 1341 30 17 18 11 17 34 22 --- 9 | 2 6 3 7 3 7 4 --- 3
R11 | 1398 30 24 9 11 23 28 25 215 8 | 2 3 3 5 4 5 4 16 4
R13 | 1211 25 28 17 17 24 13 23 --- 8 | 3 3 2 3 2 4 2 --- 2
R14 | 1354 54 53 43 29 30 47 30 --- 16 | 3 5 5 5 3 2 3 --- 3
R15 | 2060 40 39 31 18 26 30 16 --- 11 | 3 3 2 3 2 3 3 --- 2
R16 | 658 41 26 34 16 26 52 22 --- 13 | 2 9 3 6 4 11 4 --- 2
R17 | 1168 37 35 17 13 27 15 17 --- 8 | 2 3 3 4 4 3 5 --- 3
R18 | 1017 21 20 20 13 20 21 13 --- 7 | 2 4 2 5 7 5 4 --- 3
R19 | 1162 72 79 22 13 30 33 27 --- 13 | 4 5 3 5 6 22 4 --- 4
R20 | 803 30 26 20 21 41 41 28 --- 12 | 3 8 3 3 6 912 4 --- 2
R21 | 576 34 34 21 11 22 19 23 156 9 | 3 4 2 4 5 2 3 29 3
R22 | 728 51 52 19 10 26 22 17 --- 10 | 3 3 3 2 3 4 3 --- 2
R23 | 852 21 15 24 17 15 25 28 --- 9 | 3 4 3 2 4 4 2 --- 2
R24 | 1507 28 32 18 23 14 34 28 --- 11 | 4 10 3 10 20 3 4 --- 4
XR26 | ---- 51 158 --- --- --- --- 27 --- 37 | 8 28 --- --- --- --- 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1150 38 36 23 15 26 32 24 206 |T 2 5 2 4 4 46 3 17 2
WRMS | 1150 35 34 20 13 22 30 24 206 |NE 2 5 2 4 4 46 3 17 2
MEDI | 1162 30 30 20 13 25 28 22 215 |MD 2 4 3 4 4 4 3 16 3
Table 3.1948.1 GPS week: 1948 Day: 1 MJD: 57881
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 | 565 59 60 23 15 19 35 24 --- 12 | 2 4 2 4 6 4 4 --- 3
R02 | 1186 22 29 20 10 32 29 16 426 9 | 3 5 4 4 5 5 3 9999 3
R03 | 722 38 42 21 15 34 32 24 86 11 | 3 4 4 8 8 6 3 3 4
R04 | 822 30 30 22 9 26 23 24 --- 9 | 2 3 2 3 6 4 3 --- 2
R05 | 882 34 31 15 21 33 62 31 --- 14 | 2 7 5 6 10 6 3 --- 4
R06 | 1500 26 22 18 12 19 14 15 --- 7 | 3 4 3 7 6 3 2 --- 4
R07 | 1099 41 35 26 15 30 13 14 187 10 | 3 3 3 5 7 5 3 3 3
R08 | 801 25 23 10 14 26 17 18 --- 7 | 2 3 3 6 4 1 2 --- 3
XR09 | 2002 19 24 11 9 17 --- 9 --- 6 | 2 3 3 2 3 --- 3 --- 2
R10 | 975 44 69 20 18 25 34 12 --- 10 | 3 7 3 6 2 7 2 --- 3
R11 | 1673 26 27 14 8 13 27 15 234 7 | 2 3 3 5 5 5 4 3 4
R13 | 984 17 18 22 19 29 29 13 --- 9 | 3 2 3 5 3 9 2 --- 3
R14 | 1255 55 54 31 21 26 40 36 --- 14 | 3 7 6 7 5 5 3 --- 5
R15 | 1383 34 32 17 12 30 16 18 --- 9 | 3 4 2 3 2 3 3 --- 2
R16 | 673 40 69 35 19 23 55 21 --- 14 | 3 9 3 10 8 10 4 --- 4
R17 | 1514 40 48 23 12 23 16 31 --- 10 | 3 7 6 4 4 4 4 --- 3
R18 | 677 24 29 13 9 18 22 17 --- 7 | 2 4 3 5 6 4 4 --- 3
R19 | 2226 68 56 30 12 37 21 23 --- 13 | 4 4 4 6 7 19 4 --- 4
R20 | 742 43 42 22 18 33 35 37 --- 13 | 3 6 7 7 7 906 5 --- 5
R21 | 514 40 35 21 12 26 19 13 92 9 | 3 4 4 5 5 3 3 3 3
R22 | 784 44 47 19 11 17 21 18 --- 9 | 3 4 4 4 4 4 3 --- 3
R23 | 723 25 39 26 16 17 29 28 --- 10 | 3 4 3 4 4 5 3 --- 3
R24 | 1851 38 40 26 19 19 32 39 --- 12 | 4 11 3 10 22 3 4 --- 4
XR26 | ---- 41 89 --- --- --- --- 18 --- 27 | 6 35 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1159 39 42 22 15 26 31 24 240 |T 2 6 3 5 6 46 3 3 3
WRMS | 1159 36 38 21 14 25 26 24 240 |NE 2 6 3 5 6 46 3 3 3
MEDI | 975 38 35 21 14 26 27 18 187 |MD 3 4 3 5 5 5 3 3 3
Table 3.1948.2 GPS week: 1948 Day: 2 MJD: 57882
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 | 590 57 77 30 11 32 40 15 --- 12 | 3 8 6 7 4 4 3 --- 4
R02 | 1848 24 22 18 7 13 9 17 --- 6 | 3 3 3 3 4 4 2 --- 2
R03 | 773 36 37 19 14 21 19 19 76 8 | 3 3 3 5 7 3 3 2 3
R04 | 484 34 36 21 10 31 29 18 --- 9 | 3 3 4 4 6 4 3 --- 3
R05 | 1059 40 51 43 18 27 58 27 --- 15 | 3 9 6 9 12 4 4 --- 6
R06 | 1704 25 25 25 7 22 22 9 --- 7 | 2 3 3 2 7 4 2 --- 2
R07 | 529 33 32 20 9 29 21 27 156 9 | 2 3 3 5 8 5 3 2 3
XR08 | 723 31 31 15 10 26 --- 10 --- 8 | 2 3 3 6 5 --- 3 --- 3
XR09 | 1172 17 22 14 7 17 --- 10 --- 6 | 2 3 2 3 3 --- 2 --- 2
R10 | 1609 48 41 29 11 24 14 13 --- 9 | 3 4 2 3 4 5 3 --- 2
R11 | 1554 23 25 11 12 26 10 13 215 6 | 3 5 3 5 5 4 2 3 3
R13 | 1487 19 24 15 11 15 29 11 --- 7 | 2 4 3 4 4 8 3 --- 3
R14 | 840 55 49 38 16 28 42 16 --- 13 | 3 10 5 9 7 6 5 --- 6
R15 | 2092 28 36 23 9 37 21 13 --- 9 | 3 3 7 7 5 4 3 --- 4
XR16 | 731 36 35 57 28 31 --- 20 --- 17 | 3 4 5 7 7 --- 4 --- 4
R17 | 1697 40 38 17 8 29 14 13 --- 8 | 3 6 5 3 4 4 4 --- 3
R18 | 734 26 25 15 10 21 18 19 --- 7 | 3 5 5 3 4 4 3 --- 3
XR19 | 2490 52 61 28 10 23 --- 16 --- 11 | 3 4 4 6 6 --- 3 --- 3
R20 | 890 41 53 21 21 32 45 32 --- 13 | 4 10 5 11 11 858 4 --- 6
R21 | 693 34 36 17 13 22 24 18 71 8 | 3 4 4 4 6 7 5 3 4
R22 | 645 52 51 21 9 22 26 9 --- 9 | 3 4 3 6 5 4 4 --- 4
R23 | 1033 42 37 31 21 10 17 14 --- 10 | 2 4 2 6 3 3 4 --- 3
R24 | 1071 25 32 23 18 19 43 38 --- 12 | 4 9 4 9 22 4 5 --- 4
XR26 | ---- 30 62 --- --- --- --- 11 --- 18 | 5 26 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1225 38 40 24 13 25 29 19 143 |T 2 5 3 5 6 49 3 2 3
WRMS | 1225 35 36 24 11 23 28 19 143 |NE 2 5 3 5 6 49 3 2 3
MEDI | 1033 34 36 21 11 24 22 15 76 |MD 3 4 4 5 5 4 3 2 3
Table 3.1948.3 GPS week: 1948 Day: 3 MJD: 57883
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 | 551 58 52 25 15 28 28 20 --- 11 | 2 10 7 11 8 4 3 --- 6
R02 | 1165 30 36 16 8 26 13 14 --- 7 | 2 4 3 5 6 3 2 --- 3
R03 | 620 41 44 27 7 13 16 21 72 8 | 2 2 2 5 6 5 3 2 3
R04 | 640 29 33 18 10 18 23 24 --- 8 | 2 3 3 4 5 3 3 --- 3
R05 | 1343 30 19 31 16 28 61 24 --- 13 | 3 7 5 10 11 7 5 --- 7
R06 | 2001 17 21 24 13 28 34 20 --- 9 | 2 4 4 5 7 4 3 --- 2
R07 | 545 31 33 20 7 16 21 19 115 7 | 2 3 4 4 9 4 2 4 3
XR08 | 616 36 30 22 9 23 --- 14 --- 9 | 2 3 3 5 5 --- 3 --- 2
XR09 | 1397 19 17 10 9 19 --- 10 --- 6 | 2 5 2 3 3 --- 2 --- 2
R10 | 1153 32 42 25 12 20 13 12 --- 8 | 2 5 3 6 5 3 2 --- 3
R11 | 1131 33 39 14 13 32 13 24 171 9 | 2 5 3 7 7 3 3 11 3
R13 | 998 24 23 14 9 16 18 15 --- 6 | 2 3 3 3 6 4 3 --- 2
R14 | 1384 57 55 53 16 22 42 22 --- 14 | 2 13 4 13 10 4 6 --- 7
R15 | 1584 38 31 19 11 34 24 11 --- 9 | 2 3 6 6 5 5 4 --- 4
R16 | 700 44 49 51 18 40 47 19 --- 15 | 4 8 6 5 3 9999 4 --- 4
R17 | 1626 40 32 14 7 22 20 18 --- 8 | 2 5 4 3 4 3 3 --- 3
R18 | 616 24 26 15 9 22 13 14 --- 6 | 3 4 4 3 5 3 3 --- 3
R19 | 2667 55 50 25 14 29 40 23 --- 12 | 3 6 3 7 4 9999 3 --- 4
XR20 | 721 45 46 16 17 33 --- 34 --- 13 | 4 10 6 10 13 --- 4 --- 6
R21 | 556 32 33 21 8 28 22 15 90 8 | 3 4 4 4 5 6 5 7 4
R22 | 712 43 47 19 13 27 27 17 --- 9 | 3 3 2 6 5 3 5 --- 4
R23 | 1371 33 33 26 15 16 24 17 --- 9 | 2 4 3 6 2 4 4 --- 3
R24 | 796 24 41 18 16 29 56 27 --- 12 | 3 9 6 8 23 5 4 --- 5
XR26 | ---- 35 63 --- --- --- --- 15 --- 22 | 5 10 --- --- --- --- 5 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1236 37 38 26 12 26 31 19 118 |T 2 5 3 6 6 4 3 6 3
WRMS | 1236 37 37 24 11 25 29 19 118 |NE 2 5 3 6 6 4 3 6 3
MEDI | 998 33 33 20 12 26 23 18 90 |MD 2 4 4 5 5 4 3 4 3
Table 3.1948.4 GPS week: 1948 Day: 4 MJD: 57884
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 | 1022 46 50 27 19 15 21 13 --- 10 | 2 7 5 10 7 3 3 --- 5
R02 | 539 31 31 20 12 24 14 10 213 7 | 3 3 3 4 8 6 3 9999 3
R03 | 585 37 43 25 12 39 21 13 107 10 | 2 3 2 4 5 5 3 3 3
R04 | 757 31 34 20 10 21 19 26 --- 9 | 2 3 2 3 5 3 2 --- 2
R05 | 1749 44 43 29 26 22 38 25 --- 13 | 3 6 5 7 11 7 4 --- 5
R06 | 2056 16 18 14 13 16 13 19 --- 6 | 3 3 4 4 4 5 5 --- 3
R07 | 508 38 36 27 10 28 18 28 55 10 | 3 2 3 4 8 6 3 6 3
XR08 | 792 26 27 25 11 15 --- 23 --- 10 | 2 4 3 6 5 --- 3 --- 3
XR09 | 1599 19 34 16 9 15 --- 11 --- 6 | 3 6 3 3 3 --- 3 --- 2
R10 | 629 33 30 17 22 17 21 13 --- 9 | 3 5 4 5 5 3 3 --- 3
R11 | 954 33 35 19 16 35 23 12 146 9 | 3 4 4 5 5 6 4 19 3
R13 | 927 26 33 21 11 28 23 11 --- 8 | 3 5 4 4 4 4 4 --- 2
R14 | 1345 66 64 39 29 38 32 17 --- 15 | 3 11 4 16 19 6 4 --- 8
R15 | 1699 37 43 23 18 26 22 8 --- 9 | 3 3 2 3 4 6 3 --- 3
R16 | 894 35 59 45 23 24 35 19 --- 13 | 4 8 6 5 5 9999 3 --- 4
R17 | 1367 31 36 21 8 19 18 13 --- 7 | 3 5 4 9 12 5 5 --- 6
R18 | 799 21 18 17 9 21 15 10 --- 6 | 3 4 3 4 6 6 3 --- 4
R19 | 2283 65 68 22 11 35 16 18 --- 11 | 3 6 4 6 5 9999 3 --- 3
XR20 | 637 42 31 24 13 28 --- 26 --- 12 | 3 7 6 9 9 --- 4 --- 4
R21 | 716 33 39 18 10 27 11 14 79 7 | 3 4 4 5 4 4 4 9 4
R22 | 1248 44 39 24 9 29 18 19 --- 9 | 2 4 3 6 6 2 4 --- 3
R23 | 784 40 42 36 23 11 14 16 --- 10 | 3 4 3 4 4 6 4 --- 3
R24 | 621 20 27 40 23 43 38 33 --- 15 | 4 8 6 7 20 5 5 --- 4
XR26 | ---- 25 41 --- --- --- --- 12 --- 16 | 7 9 --- --- --- --- 5 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1188 38 41 26 17 27 23 18 132 |T 3 5 3 5 7 4 3 9 3
WRMS | 1188 38 40 25 16 24 21 18 132 |NE 3 5 3 5 7 4 3 9 3
MEDI | 894 33 36 23 12 24 19 14 107 |MD 3 4 4 5 5 5 3 6 3
Table 3.1948.5 GPS week: 1948 Day: 5 MJD: 57885
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 | 1234 46 48 25 14 12 35 17 --- 11 | 3 6 2 8 9 5 4 --- 4
R02 | 539 23 23 14 11 14 17 14 93 6 | 5 4 3 2 6 6 4 9999 3
R03 | 994 36 32 26 16 32 11 10 106 9 | 3 4 2 4 3 4 4 3 2
R04 | 695 36 34 21 8 37 14 20 --- 9 | 2 3 2 2 4 3 2 --- 2
R05 | 860 36 39 32 13 19 55 29 --- 14 | 3 5 3 6 8 5 4 --- 3
R06 | 1915 14 17 20 13 14 12 17 --- 6 | 4 4 4 5 6 5 5 --- 4
R07 | 615 39 39 29 12 39 22 25 85 11 | 4 3 4 5 7 5 4 3 3
R08 | 797 25 23 23 20 23 15 26 --- 9 | 2 6 4 7 4 1 3 --- 3
XR09 | 2793 22 19 11 10 23 --- 13 --- 7 | 4 5 5 3 3 --- 3 --- 3
R10 | 702 30 35 12 22 23 20 25 --- 9 | 5 4 4 2 4 4 4 --- 3
R11 | 881 32 33 16 15 23 18 15 131 8 | 4 4 3 4 3 5 4 4 2
R13 | 1028 28 30 19 13 31 23 14 --- 9 | 4 7 4 4 4 5 4 --- 3
R14 | 813 56 54 22 26 36 33 31 --- 14 | 4 6 3 11 15 7 4 --- 6
R15 | 911 31 34 19 24 28 27 13 --- 10 | 4 3 4 2 3 7 4 --- 3
XR16 | 1423 35 30 70 17 27 --- 37 --- 20 | 4 9 5 6 5 --- 4 --- 4
R17 | 929 43 37 18 12 31 15 14 --- 9 | 3 4 4 8 10 5 7 --- 5
R18 | 930 22 20 14 11 17 11 20 --- 7 | 4 5 4 5 5 6 5 --- 4
R19 | 2142 60 51 26 11 30 20 26 --- 12 | 4 4 3 8 7 9999 5 --- 5
R20 | 697 31 41 28 29 26 33 35 --- 13 | 3 8 6 7 8 9999 5 --- 4
R21 | 589 30 34 11 7 21 16 17 132 7 | 3 3 4 4 3 3 4 3 3
R22 | 1412 35 46 19 10 21 13 10 --- 7 | 5 6 4 6 8 3 5 --- 4
R23 | 565 38 37 36 23 14 20 16 --- 11 | 4 4 4 6 5 5 5 --- 4
XR24 | 830 19 34 34 28 --- 40 28 --- 15 | 3 9 6 5 --- 4 6 --- 3
XR26 | ---- 21 29 --- --- --- --- 9 --- 13 | 7 11 --- --- --- --- 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1048 36 37 22 17 26 24 21 111 |T 3 5 3 5 5 4 4 3 3
WRMS | 1048 34 34 22 17 24 22 21 111 |NE 3 5 3 5 5 4 4 3 3
MEDI | 881 31 34 21 13 23 20 17 106 |MD 4 4 4 5 5 5 4 3 3
Table 3.1948.6 GPS week: 1948 Day: 6 MJD: 57886
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 | 892 58 62 15 10 30 30 18 --- 11 | 2 4 2 5 6 4 3 --- 3
R02 | 613 18 18 12 10 11 21 19 106 6 | 4 4 3 2 3 4 3 1 2
R03 | 1039 23 23 19 12 11 24 15 106 7 | 3 3 2 3 4 1 3 2 2
R04 | 683 32 36 25 10 24 19 12 --- 8 | 2 2 2 2 3 2 3 --- 2
R05 | 919 36 45 17 22 26 54 34 --- 14 | 2 3 2 5 3 3 3 --- 2
R06 | 1788 18 26 13 12 22 25 16 --- 7 | 3 4 3 4 6 4 3 --- 3
R07 | 788 34 38 23 11 14 16 19 137 8 | 3 3 3 3 5 2 4 2 2
XR08 | 1199 24 29 18 10 17 --- 23 --- 9 | 2 5 3 4 2 --- 3 --- 2
XR09 | 3466 23 28 16 9 21 --- 13 --- 7 | 3 3 3 2 2 --- 3 --- 2
R10 | 753 25 29 20 16 17 14 19 --- 8 | 3 3 2 2 2 3 3 --- 2
R11 | 968 34 41 11 14 26 16 10 116 8 | 3 3 2 3 3 2 2 3 2
R13 | 1008 31 30 22 14 26 35 14 --- 10 | 3 5 3 4 3 4 3 --- 3
R14 | 789 79 86 25 31 33 38 18 --- 15 | 3 3 3 5 4 5 6 --- 4
R15 | 1067 25 32 21 19 15 14 12 --- 8 | 3 2 3 2 3 4 3 --- 3
XR16 | 1992 34 46 53 23 22 --- 12 --- 16 | 3 4 3 5 2 --- 3 --- 2
R17 | 1360 37 33 16 12 26 22 17 --- 9 | 3 3 3 3 2 3 3 --- 2
R18 | 1401 24 26 16 11 23 24 19 --- 8 | 4 4 3 4 3 3 4 --- 3
R19 | 1964 61 53 28 12 26 22 22 --- 12 | 3 3 3 6 5 9999 5 --- 4
R20 | 582 26 27 17 23 18 33 34 --- 11 | 2 7 4 4 7 1 5 --- 3
R21 | 637 36 30 19 8 28 19 15 192 8 | 3 3 3 2 3 2 4 3 2
R22 | 1002 43 40 13 9 27 17 13 --- 8 | 4 5 3 5 5 3 4 --- 4
R23 | 743 31 33 33 20 12 24 25 --- 11 | 3 3 3 5 3 2 3 --- 3
R24 | 523 27 29 22 26 18 23 23 --- 10 | 3 6 3 3 9999 3 4 --- 2
XR26 | ---- 20 64 --- --- --- --- 11 --- 14 | 3 8 --- --- --- --- 7 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1047 38 40 20 16 22 26 20 135 |T 2 3 2 3 3 2 3 2 2
WRMS | 1047 34 36 20 15 24 24 20 135 |NE 2 3 2 3 3 2 3 2 2
MEDI | 968 31 32 19 12 22 22 17 116 |MD 3 3 3 4 3 3 3 2 2
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