[IGSREPORT-25261] Wk 1946 IGLOS Final Orbits
acc
acc at igs.org
Sun May 14 05:47:51 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1946 (Apr 23, 2017 - Apr 29, 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 2.1946.
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:
igl1946[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1946 in the SP3 format.
igl19467.sum Combination Report for GPS Week 1946.
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 | 0.5 ns
1 | 2.1 ns
2 | -0.2 ns
3 | 2.3 ns
4 | -1.6 ns
5 | -1.0 ns
6 | 0.6 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 1.1946, 1a.1946).
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 2.1946.0-6)
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 3.1946.0-6).
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 1946 summary. (Apr 23, 2017 - Apr 29, 2017)
Table 1.1946.a GPS week : 1946 MJD: 57866.0-57872.0
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 20 -37 -14 36 .13 39 37 | 5725 799 3326 11647
| 1 1 1 32 27 27 .03 | 3117 3347
cof n/a| 0 0 24 -38 5 39 .15 41 38 | 5724 796 3324 11645
| 1 1 2 33 33 42 .09 | 3113 3342
emx n/a| 0 0 0 -14 -35 2 .09 22 22 | 2520 1025 3310 10892
| 1 1 1 17 16 27 .04 | 11389 2324
esx n/a| -1 0 0 3 13 0 .11 16 15 | -3082 -605 3314 13900
| 1 1 1 15 15 28 .03 | 8703 4403
gfz n/a| -2 0 -12 6 45 11 .06 26 26 | 0 346 3316 11530
| 1 1 2 30 18 32 .06 | 0 3005
grg n/a| 1 0 5 -63 3 -83 -.33 32 30 | 57 629 3332 11093
| 1 1 5 33 19 110 .03 | 485 3408
iac n/a| 1 0 -5 63 -14 17 -.12 20 20 | 1288 -423 3317 10792
| 0 1 1 33 37 66 .03 | 1098 1643
mcc n/a| 0 2 34 64 -60 643 -.22 174 174 | --- --- --- ---
| 4 6 4 132 97 510 .41 | --- ---
Table 1.1946.b GPS week : 1946 MJD: 57866.0-57872.0
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 | 10 12 12 11 13 15 12 |
R02 | 5 6 8 7 10 7 7 |
R03 | 9 9 9 10 10 8 9 |
R04 | 9 9 9 10 9 9 7 |
R05 | 12 14 12 12 14 13 15 |
R06 | 9 8 8 6 7 8 9 |
R07 | 10 9 9 9 9 10 9 |
R08 | 7 9 9 8 7 7 8 |
R09 | 7 7 6 7 9 7 6 |
R10 | 9 8 7 7 9 10 9 |
R11 | 8 8 9 7 10 9 8 |
R13 | 8 8 9 8 8 8 11 |
R14 | 10 15 16 15 14 13 15 |
R15 | 11 11 9 10 9 9 12 |
R16 | 19 15 14 16 12 19 11 |
R17 | 9 10 9 10 13 10 9 |
R18 | 7 8 8 8 9 8 8 |
R19 | 14 15 17 12 14 15 14 |
R20 | 14 11 10 12 15 15 12 |
R21 | 13 11 10 9 13 10 9 |
R22 | 10 11 12 10 9 13 13 |
R23 | 12 12 10 10 11 11 9 |
R24 | 13 16 16 14 14 15 14 |
R26 | 10 12 17 17 17 19 15 |
Table 1.1946.c GPS week : 1946 MJD: 57866.0-57872.0
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 1946 0 | -20 28 172 -1757 1508 1953 84.0 1547 1547 | 524 0
brd 1946 1 | -22 -28 171 360 1020 -434 84.7 1304 1304 | 2060 0
brd 1946 2 | 31 5 222 -44 1112 -522 84.4 1049 1049 | -190 0
brd 1946 3 | 0 -19 173 -1110 435 -1824 83.7 945 945 | 2282 0
brd 1946 4 | 86 -24 167 420 -221 -562 83.1 984 984 | -1633 0
brd 1946 5 | -39 1 187 447 -615 -342 84.8 1014 1014 | -960 0
brd 1946 6 | -14 -25 216 -1113 -1044 1331 83.8 1012 1012 | 619 0
-------------+------------------------------------------------------------+----------------
brd 1946 mean| 3 -8 187 -399 313 -57 84.1 1122 1122 | 386 0
brd 1946 sdev| 42 21 23 908 963 1277 .6 220 220 | 1454 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 2.1946.0 GPS week: 1946 Day: 0 MJD: 57866
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 23 -92 -4 14 .14 41 41 | -58 432 3210 11428
cof n/a| 0 1 20 -89 49 10 .09 43 42 | -56 424 3209 11423
emx n/a| -1 1 0 -38 -19 1 .16 25 25 | 663 336 3178 10460
esx n/a| -2 0 -1 17 18 -57 .15 15 14 | -3328 -706 3204 13734
gfz n/a| -2 0 -14 72 66 -33 .02 27 24 | 0 1061 3195 11209
grg n/a| 3 0 4 -31 31 85 -.29 27 26 | 561 264 3237 10599
iac n/a| 1 0 -3 14 -48 31 -.09 19 19 | 1034 -1321 3196 10575
mcc n/a| 0 0 37 55 -111 1100 -.11 201 201 | --- --- --- ---
Table 2.1946.1 GPS week: 1946 Day: 1 MJD: 57867
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 21 -21 21 20 .10 39 37 | 4073 5741 3646 11704
cof n/a| 0 0 28 -50 15 12 .22 44 38 | 4085 5724 3643 11702
emx n/a| -1 2 -2 -5 -62 11 .10 23 23 | 3815 3673 3630 10982
esx n/a| 0 1 0 -4 25 -4 .08 15 14 | 8836 5061 3639 13698
gfz n/a| -2 -2 -15 2 33 -26 .16 26 30 | 0 4212 3643 11508
grg n/a| 1 -2 16 -70 -23 26 -.38 32 33 | -753 5753 3577 11188
iac n/a| 0 -1 -6 67 -10 -18 -.10 21 21 | 2729 1371 3629 10769
mcc n/a| -6 5 37 -164 -133 1153 .56 261 261 | --- --- --- ---
Table 2.1946.2 GPS week: 1946 Day: 2 MJD: 57868
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 21 -54 -4 6 .14 38 38 | 7063 -1483 3183 11011
cof n/a| -1 1 24 -46 42 7 .25 41 40 | 7061 -1483 3181 11008
emx n/a| 0 0 0 1 -20 0 .05 21 21 | 3374 -353 3161 10234
esx n/a| 0 2 0 28 35 11 .07 16 14 | -10844 -5106 3168 13362
gfz n/a| -2 -1 -15 3 53 43 .08 27 24 | 0 -1905 3165 10944
grg n/a| 0 0 3 -109 2 -61 -.35 34 31 | 623 -1887 3209 10698
iac n/a| 1 -1 -3 36 -46 -45 -.10 19 19 | 1603 -2176 3177 10086
mcc n/a| 0 12 31 -34 -81 521 .02 164 164 | --- --- --- ---
Table 2.1946.3 GPS week: 1946 Day: 3 MJD: 57869
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 20 -4 11 32 .08 39 38 | 8766 4068 3231 11982
cof n/a| -1 -1 24 -4 -6 8 .01 40 39 | 8761 4057 3231 11983
emx n/a| 0 0 0 -8 -36 -51 .05 21 21 | 21747 3679 3218 11242
esx n/a| -1 3 0 2 16 28 .11 16 15 | -2523 4719 3211 14618
gfz n/a| -3 0 -9 -12 34 4 .03 24 22 | 0 3409 3208 11932
grg n/a| 2 -2 0 -69 15 -157 -.29 33 28 | 174 4050 3236 11668
iac n/a| 1 -1 -3 43 -44 65 -.15 19 19 | 2064 1543 3222 11079
mcc n/a| 1 9 28 62 -157 776 -.48 142 142 | --- --- --- ---
Table 2.1946.4 GPS week: 1946 Day: 4 MJD: 57870
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 -26 -44 44 .14 38 37 | 9042 -3678 3577 12177
cof n/a| 1 0 24 8 -38 61 .12 39 38 | 9036 -3671 3577 12176
emx n/a| 0 -1 1 6 -27 11 .10 22 22 | 3809 -2504 3560 11421
esx n/a| -1 0 0 4 -7 -6 .09 17 17 | -6732 -5438 3552 14000
gfz n/a| 0 0 -9 -6 22 11 .07 27 27 | 0 -3862 3550 12114
grg n/a| 0 0 1 -99 15 -236 -.32 32 32 | 214 -3680 3620 11551
iac n/a| 1 1 -4 83 16 140 -.10 20 20 | 1156 -2587 3569 11408
mcc n/a| -2 -3 37 121 -94 882 -.46 127 127 | --- --- --- ---
Table 2.1946.5 GPS week: 1946 Day: 5 MJD: 57871
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 19 -58 -33 45 .14 38 33 | 5436 -1498 3255 11458
cof n/a| 0 1 25 -56 4 119 .14 41 33 | 5442 -1505 3257 11458
emx n/a| -1 0 2 -26 -53 40 .07 23 23 | 1727 -151 3263 10783
esx n/a| -1 -1 -2 -20 -3 5 .12 17 16 | 7419 -3734 3256 13940
gfz n/a| -3 -1 -11 -20 34 32 .09 27 26 | 0 -1961 3252 11295
grg n/a| 0 0 5 -24 -20 -137 -.30 34 33 | -169 -1747 3283 10855
iac n/a| 2 -2 -6 114 51 -15 -.15 21 21 | -804 42 3260 10592
mcc n/a| 6 -2 37 199 70 399 -.58 123 123 | --- --- --- ---
Table 2.1946.6 GPS week: 1946 Day: 6 MJD: 57872
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 21 -5 -45 90 .17 42 37 | 5754 2014 3183 11771
cof n/a| -1 0 23 -31 -28 55 .22 43 38 | 5745 2030 3175 11769
emx n/a| 0 -1 2 -28 -30 2 .10 21 21 | -17492 2496 3164 11127
esx n/a| -3 0 2 0 12 23 .14 15 13 | -14408 964 3172 13948
gfz n/a| -1 0 -13 7 71 49 -.01 26 27 | 0 1469 3200 11712
grg n/a| 3 0 6 -39 6 -100 -.35 32 31 | -248 1656 3163 11097
iac n/a| 1 0 -7 85 -16 -34 -.17 20 20 | 1237 167 3168 11039
mcc n/a| 3 -5 29 212 84 -328 -.47 202 202 | --- --- --- ---
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 3.1946.0 GPS week: 1946 Day: 0 MJD: 57866
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 | 4461 63 63 18 8 26 20 18 --- 10 | 3 5 2 5 5 5 3 --- 4
R02 | 528 18 18 12 10 17 12 8 93 5 | 2 4 3 3 2 3 2 2 2
R03 | 779 44 48 23 13 25 15 16 45 9 | 2 3 3 3 5 2 3 2 2
R04 | 825 40 58 18 13 24 15 19 --- 8 | 3 6 2 5 7 3 5 --- 3
R05 | 558 27 35 24 18 37 34 26 --- 12 | 3 10 5 8 7 3 4 --- 5
R06 | 2665 31 32 20 13 22 25 11 --- 8 | 3 4 3 5 3 4 2 --- 3
R07 | 662 44 46 16 18 22 29 17 235 10 | 3 3 3 3 4 4 2 3 2
R08 | 989 33 30 12 10 21 14 9 --- 6 | 2 3 2 5 5 2 3 --- 3
XR09 | 1882 20 18 17 8 17 --- 10 --- 6 | 1 3 1 3 3 --- 1 --- 2
R10 | 1414 41 37 19 7 29 17 16 --- 8 | 2 3 2 3 5 3 3 --- 3
R11 | 652 32 40 15 12 31 21 12 323 8 | 2 2 2 3 4 2 3 3 2
R13 | 1133 15 18 19 21 13 17 14 --- 8 | 1 2 2 5 2 3 4 --- 2
R14 | 2261 48 56 28 15 27 20 10 --- 10 | 2 6 3 5 5 8 4 --- 3
R15 | 1066 27 28 19 16 32 36 19 --- 10 | 2 4 3 8 6 6 2 --- 4
R16 | 1315 45 33 68 21 26 62 16 --- 19 | 3 7 4 4 3 3 2 --- 2
R17 | 1003 37 32 24 11 28 19 13 --- 9 | 3 3 4 3 2 4 2 --- 3
R18 | 680 30 34 16 9 20 13 15 --- 7 | 2 4 4 6 4 4 3 --- 4
R19 | 1456 75 77 26 7 25 27 34 --- 13 | 3 4 2 6 5 3 4 --- 4
R20 | 828 39 36 22 19 43 38 32 --- 13 | 3 7 3 8 8 3 4 --- 5
R21 | 1374 46 42 29 16 39 26 26 177 12 | 2 4 3 6 5 6 5 4 5
R22 | 1229 47 45 26 14 29 19 13 --- 10 | 3 3 3 9 9 3 3 --- 5
R23 | 1241 39 54 25 27 15 31 16 --- 11 | 3 5 2 5 4 2 3 --- 3
R24 | 1192 27 31 20 22 29 36 33 --- 12 | 4 9 3 5 7 3 3 --- 4
XR26 | ---- 16 177 --- --- --- --- 5 --- 9 | 4 32 --- --- --- --- 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1546 41 43 25 15 27 27 19 201 |T 2 5 2 5 4 3 3 2 3
WRMS | 1546 41 42 25 14 24 26 19 201 |NE 2 5 2 5 4 3 3 2 3
MEDI | 1133 37 36 20 13 26 20 16 177 |MD 3 4 3 5 5 3 3 3 3
Table 3.1946.1 GPS week: 1946 Day: 1 MJD: 57867
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 | 3614 59 60 23 14 35 28 16 --- 12 | 4 9 3 9 7 9 4 --- 6
R02 | 499 28 31 11 9 17 16 10 93 6 | 3 5 4 6 6 5 3 6 4
R03 | 623 38 27 20 10 24 23 15 68 9 | 2 5 3 4 5 2 3 3 2
R04 | 520 41 37 17 13 18 19 13 --- 8 | 3 5 3 6 6 3 4 --- 3
R05 | 669 29 35 28 20 28 52 32 --- 13 | 4 9 6 9 8 3 4 --- 6
R06 | 2568 24 28 16 14 20 25 11 --- 7 | 3 4 4 5 3 5 4 --- 2
R07 | 1138 41 44 18 9 22 20 14 331 8 | 2 3 4 3 3 4 2 17 2
R08 | 756 38 45 19 12 22 19 11 --- 8 | 3 4 3 5 5 4 3 --- 3
XR09 | 1925 21 26 9 9 14 --- 15 --- 6 | 2 4 2 6 5 --- 2 --- 3
R10 | 1487 23 20 12 14 19 19 17 --- 7 | 2 3 3 4 7 4 3 --- 3
R11 | 616 28 30 15 10 21 13 23 429 7 | 2 4 3 6 5 4 4 36 4
R13 | 771 26 31 11 9 21 26 16 --- 7 | 2 3 2 4 3 3 3 --- 2
R14 | 989 51 50 44 14 20 53 16 --- 14 | 3 6 4 9 5 7 6 --- 4
R15 | 760 28 27 31 20 20 24 22 --- 10 | 3 6 3 8 7 7 4 --- 5
R16 | 633 33 75 45 22 22 51 17 --- 14 | 3 11 4 4 5 5 3 --- 3
R17 | 1285 33 29 17 10 39 23 21 --- 10 | 3 5 5 4 4 5 3 --- 3
R18 | 725 35 32 14 13 29 16 11 --- 8 | 3 5 5 6 4 4 3 --- 4
R19 | 2191 64 75 23 14 32 40 41 --- 14 | 3 6 3 8 5 5 3 --- 4
R20 | 697 41 62 16 16 32 30 28 --- 11 | 4 10 4 11 10 4 4 --- 6
R21 | 672 38 44 21 11 34 23 26 183 10 | 3 5 6 9 11 6 5 15 7
R22 | 707 48 48 18 12 36 28 19 --- 11 | 3 4 4 10 10 5 4 --- 6
R23 | 706 44 43 24 18 14 36 25 --- 11 | 3 6 2 8 5 8 3 --- 5
R24 | 666 26 34 30 34 33 59 30 --- 16 | 4 9 5 10 8 4 4 --- 4
XR26 | ---- 17 123 --- --- --- --- 7 --- 11 | 6 33 --- --- --- --- 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1303 39 44 23 15 26 32 21 261 |T 3 6 3 6 5 4 3 15 3
WRMS | 1303 37 38 23 14 30 33 21 261 |NE 3 6 3 6 5 4 3 15 3
MEDI | 725 33 35 18 13 22 24 16 183 |MD 3 5 4 6 5 4 3 15 4
Table 3.1946.2 GPS week: 1946 Day: 2 MJD: 57868
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 | 1997 57 66 17 14 29 34 18 --- 11 | 3 7 4 9 8 8 3 --- 5
R02 | 641 28 33 14 12 23 16 14 89 7 | 2 4 4 5 5 4 3 9 4
R03 | 662 37 47 15 10 27 25 12 37 8 | 2 5 3 6 6 2 3 4 3
R04 | 425 44 41 19 12 26 15 13 --- 9 | 3 4 3 4 4 2 2 --- 2
R05 | 798 38 38 26 15 23 43 24 --- 12 | 4 5 4 6 8 4 4 --- 4
R06 | 1578 21 31 13 14 22 31 15 --- 8 | 2 2 4 5 5 3 3 --- 3
R07 | 655 36 38 18 12 24 28 19 180 9 | 2 4 3 4 6 4 2 28 2
R08 | 719 37 43 26 12 22 15 10 --- 9 | 3 5 4 6 4 3 3 --- 4
XR09 | 1692 16 22 11 9 18 --- 9 --- 6 | 2 4 2 5 4 --- 2 --- 3
R10 | 1408 18 23 13 15 18 19 7 --- 6 | 2 4 2 3 5 4 3 --- 2
R11 | 563 23 32 12 19 29 29 17 179 9 | 2 4 2 6 6 5 3 57 3
R13 | 1127 16 24 14 13 25 24 23 --- 8 | 2 4 3 4 4 4 2 --- 2
R14 | 930 61 59 37 21 34 62 16 --- 16 | 3 8 3 10 8 4 3 --- 4
R15 | 829 21 27 12 22 22 31 14 --- 9 | 2 6 2 3 5 5 3 --- 3
R16 | 922 34 27 33 21 32 45 24 --- 13 | 3 9 3 3 4 6 3 --- 2
R17 | 730 35 41 21 10 22 19 15 --- 8 | 2 4 3 3 5 4 3 --- 2
R18 | 619 29 31 17 8 20 15 16 --- 7 | 2 4 3 4 3 3 2 --- 2
R19 | 2435 70 60 33 21 44 45 29 --- 16 | 2 6 3 6 7 5 2 --- 3
R20 | 692 41 40 15 15 23 32 21 --- 10 | 3 7 3 9 9 4 3 --- 4
R21 | 539 39 37 21 11 29 26 19 245 10 | 2 4 5 6 8 5 4 25 5
R22 | 578 50 49 20 11 37 34 24 --- 12 | 2 3 4 7 8 6 4 --- 5
R23 | 609 32 38 23 24 18 16 20 --- 10 | 2 5 2 6 4 6 3 --- 3
R24 | 907 23 37 27 22 26 72 32 --- 15 | 3 11 5 8 6 4 5 --- 4
XR26 | ---- 27 115 --- --- --- --- 9 --- 16 | 6 21 --- --- --- --- 5 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1049 38 41 21 16 27 34 19 164 |T 2 5 3 5 5 4 3 24 3
WRMS | 1049 38 40 21 14 24 31 19 164 |NE 2 5 3 5 5 4 3 24 3
MEDI | 730 34 38 18 14 24 28 16 179 |MD 2 4 3 6 5 4 3 25 3
Table 3.1946.3 GPS week: 1946 Day: 3 MJD: 57869
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 | 1221 50 52 27 12 18 30 18 --- 10 | 5 8 5 6 7 4 4 --- 4
R02 | 635 29 26 12 14 19 15 14 77 7 | 4 5 4 5 6 5 5 4 4
R03 | 782 46 37 24 11 33 16 15 35 10 | 2 4 3 8 5 4 3 2 4
R04 | 895 50 54 25 10 29 12 17 --- 10 | 4 4 7 3 5 5 4 --- 4
R05 | 668 40 38 20 14 26 44 27 --- 12 | 6 6 5 3 12 6 5 --- 4
R06 | 1131 17 17 16 8 15 19 12 --- 6 | 4 6 4 6 5 3 4 --- 4
R07 | 711 42 45 17 12 28 22 15 96 9 | 3 6 4 5 6 3 3 4 2
R08 | 966 34 33 14 16 15 19 13 --- 7 | 4 7 6 9 7 5 5 --- 6
XR09 | 1928 17 14 12 9 21 --- 9 --- 6 | 5 7 4 5 5 --- 4 --- 5
R10 | 798 25 22 9 14 18 21 13 --- 7 | 5 4 4 3 4 5 4 --- 3
R11 | 576 29 34 10 7 15 21 18 162 7 | 3 4 2 5 5 3 2 3 3
R13 | 652 21 22 21 16 21 20 13 --- 8 | 5 5 6 6 4 4 5 --- 5
R14 | 1133 44 48 26 21 24 72 20 --- 15 | 3 8 8 7 7 4 3 --- 4
R15 | 893 24 27 16 21 16 34 17 --- 9 | 3 4 3 2 4 3 3 --- 2
R16 | 664 45 53 42 26 14 67 16 --- 16 | 4 6 4 4 5 5 3 --- 2
R17 | 671 47 44 23 13 29 23 16 --- 10 | 5 4 5 5 5 3 4 --- 3
R18 | 689 34 30 17 10 17 23 14 --- 8 | 4 3 4 5 5 3 4 --- 4
R19 | 2281 63 60 23 6 35 21 23 --- 12 | 3 4 3 7 8 6 4 --- 4
R20 | 810 37 37 16 19 26 46 23 --- 12 | 3 8 4 9 8 3 5 --- 4
R21 | 910 37 41 20 8 22 20 20 242 8 | 5 5 5 4 5 5 5 5 4
R22 | 548 48 54 20 9 34 14 16 --- 9 | 5 6 6 7 7 5 5 --- 5
R23 | 824 27 33 21 21 15 20 23 --- 9 | 3 5 4 7 6 5 3 --- 5
R24 | 816 25 30 25 30 28 49 32 --- 14 | 4 12 5 4 5 3 4 --- 3
XR26 | ---- 29 141 --- --- --- --- 10 --- 16 | 6 30 --- --- --- --- 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 945 39 40 21 16 24 33 19 142 |T 4 6 4 5 5 4 3 3 3
WRMS | 945 38 39 21 15 22 28 19 142 |NE 4 6 4 5 5 4 3 3 3
MEDI | 810 34 37 20 13 21 21 16 96 |MD 4 5 4 5 5 4 4 4 4
Table 3.1946.4 GPS week: 1946 Day: 4 MJD: 57870
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 | 1537 62 55 18 13 26 36 26 --- 12 | 4 10 4 8 9 6 5 --- 5
R02 | 1080 23 25 14 19 22 40 14 64 9 | 4 5 5 4 6 4 4 3 4
R03 | 1237 39 43 17 15 26 24 17 32 9 | 2 4 5 8 4 5 3 2 4
R04 | 953 40 42 15 10 26 20 14 --- 8 | 3 5 6 4 7 8 4 --- 4
R05 | 552 29 21 35 16 23 51 26 --- 13 | 5 7 7 9 11 5 5 --- 5
R06 | 1589 21 21 17 12 16 16 14 --- 7 | 4 6 3 5 4 5 4 --- 4
R07 | 505 34 36 20 14 23 24 12 74 9 | 3 5 4 5 6 5 3 4 3
R08 | 673 30 33 10 8 21 12 12 --- 6 | 4 5 4 7 6 5 4 --- 5
XR09 | 1600 22 26 19 11 28 --- 14 --- 9 | 4 6 4 5 5 --- 4 --- 4
R10 | 1214 19 21 19 24 16 19 16 --- 8 | 4 6 4 6 7 7 4 --- 4
R11 | 621 33 34 14 19 25 38 9 174 10 | 3 3 4 5 4 3 3 3 3
R13 | 646 18 20 20 16 25 15 16 --- 8 | 4 4 6 5 6 3 4 --- 4
R14 | 887 45 41 28 22 45 19 27 --- 13 | 3 10 8 7 7 4 3 --- 5
R15 | 711 32 41 19 10 28 15 20 --- 8 | 2 3 4 2 4 3 2 --- 2
R16 | 521 39 45 32 9 32 30 19 --- 11 | 4 7 3 5 4 5 3 --- 3
R17 | 894 45 51 28 19 29 34 26 --- 12 | 4 5 4 8 7 4 5 --- 4
R18 | 565 35 39 17 12 26 18 15 --- 8 | 4 4 4 8 9 4 4 --- 5
R19 | 1859 67 64 30 14 23 32 29 --- 14 | 3 4 4 5 7 5 4 --- 3
R20 | 1060 29 31 23 25 22 65 29 --- 15 | 3 9 3 7 9 3 5 --- 4
R21 | 767 47 54 25 20 36 39 17 199 12 | 4 7 5 5 6 7 4 5 4
R22 | 513 43 47 16 11 24 19 14 --- 9 | 4 7 6 7 6 5 4 --- 5
R23 | 850 29 26 23 23 23 30 15 --- 10 | 3 6 4 8 6 5 3 --- 4
R24 | 838 23 26 26 21 35 48 29 --- 13 | 3 8 3 6 8 5 3 --- 4
XR26 | ---- 21 56 --- --- --- --- 14 --- 17 | 4 22 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 984 38 39 22 17 27 32 20 127 |T 3 6 4 6 6 4 3 3 3
WRMS | 984 37 38 22 17 27 32 20 127 |NE 3 6 4 6 6 4 3 3 3
MEDI | 850 32 36 19 15 25 24 16 74 |MD 4 6 4 6 6 5 4 3 4
Table 3.1946.5 GPS week: 1946 Day: 5 MJD: 57871
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 | 1436 66 79 21 17 45 44 23 --- 15 | 3 7 3 7 9 5 4 --- 4
R02 | 612 18 22 13 15 13 18 19 71 7 | 3 4 4 4 5 5 2 4 3
R03 | 1183 33 34 13 9 26 21 14 37 8 | 2 4 4 5 5 4 3 4 3
R04 | 947 41 40 14 8 27 24 9 --- 8 | 2 4 3 4 5 8 3 --- 3
R05 | 750 36 39 23 22 24 36 35 --- 12 | 3 8 7 9 9 6 5 --- 5
R06 | 1442 25 22 19 10 20 20 16 --- 7 | 2 4 2 4 4 5 3 --- 2
R07 | 950 44 38 19 10 28 16 18 131 9 | 2 3 3 3 6 5 3 18 2
R08 | 629 26 23 12 14 14 13 15 --- 6 | 2 5 2 4 4 4 3 --- 2
XR09 | 1818 17 19 15 9 18 --- 9 --- 6 | 1 4 2 5 4 --- 2 --- 2
R10 | 1077 22 21 15 21 16 37 16 --- 9 | 2 5 4 7 6 5 4 --- 4
R11 | 1130 27 31 10 14 23 31 12 172 8 | 2 2 3 3 5 4 3 17 3
R13 | 1050 19 23 10 18 24 13 16 --- 7 | 2 3 2 3 5 2 2 --- 2
R14 | 867 43 49 24 29 24 42 18 --- 13 | 2 8 5 9 7 6 2 --- 4
R15 | 716 35 34 20 13 20 22 19 --- 9 | 2 2 3 3 4 4 2 --- 2
R16 | 543 14 17 61 20 39 60 26 --- 18 | 3 6 3 7 4 6 2 --- 3
R17 | 992 40 34 16 8 29 26 19 --- 9 | 3 5 2 7 8 5 4 --- 4
R18 | 600 32 29 17 10 25 16 14 --- 8 | 2 4 3 9 9 4 4 --- 5
R19 | 1188 75 86 28 23 32 28 25 --- 15 | 3 5 4 5 6 3 2 --- 2
R20 | 1363 31 33 28 24 29 63 25 --- 15 | 3 7 3 12 9 3 3 --- 5
R21 | 1207 43 38 19 9 19 17 23 151 9 | 2 6 3 3 4 6 3 11 2
R22 | 882 51 45 31 14 34 21 26 --- 12 | 3 6 5 5 4 7 3 --- 3
R23 | 1083 30 31 21 22 20 30 19 --- 10 | 3 7 5 5 5 3 2 --- 2
R24 | 911 30 45 22 18 30 61 33 --- 14 | 4 9 4 7 10 5 3 --- 4
XR26 | ---- 28 52 --- --- --- --- 13 --- 19 | 3 47 --- --- --- --- 5 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1014 38 41 23 17 27 34 21 123 |T 2 6 3 5 5 4 3 10 3
WRMS | 1014 33 33 23 16 26 33 21 123 |NE 2 6 3 5 5 4 3 10 3
MEDI | 992 31 34 19 14 24 24 18 131 |MD 2 5 3 5 5 5 3 11 3
Table 3.1946.6 GPS week: 1946 Day: 6 MJD: 57872
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 | 1035 57 58 16 13 30 37 22 --- 11 | 2 3 3 3 5 3 3 --- 3
R02 | 579 21 20 15 8 24 19 12 67 7 | 2 4 3 3 3 4 2 7 2
R03 | 715 37 32 16 10 29 19 17 60 8 | 2 4 2 3 3 2 2 7 2
R04 | 773 34 31 13 10 17 18 13 --- 7 | 2 3 2 3 2 5 2 --- 2
R05 | 544 50 54 21 27 23 54 35 --- 15 | 3 6 4 6 7 5 4 --- 4
R06 | 1896 20 29 24 16 22 22 14 --- 8 | 2 3 2 3 3 3 3 --- 2
R07 | 606 39 39 15 11 26 17 18 222 8 | 2 2 2 2 3 2 2 29 1
R08 | 679 25 23 18 10 21 25 19 --- 8 | 2 4 2 3 2 3 2 --- 2
XR09 | 1494 17 23 10 6 20 --- 13 --- 6 | 1 3 1 4 3 --- 2 --- 2
R10 | 1401 38 41 18 13 27 20 10 --- 8 | 2 3 4 4 4 2 3 --- 3
R11 | 932 28 27 12 12 28 25 7 379 7 | 2 2 2 2 3 3 2 30 2
R13 | 914 22 27 23 28 20 27 16 --- 10 | 2 3 2 3 2 2 2 --- 1
R14 | 764 71 66 22 21 24 56 21 --- 15 | 2 4 3 6 5 5 2 --- 2
R15 | 690 50 50 23 26 31 19 24 --- 12 | 2 3 2 2 3 3 3 --- 2
R16 | 666 39 39 25 11 31 34 18 --- 10 | 2 4 3 5 3 4 2 --- 2
R17 | 775 36 40 20 6 27 25 12 --- 8 | 2 3 2 4 6 4 3 --- 3
R18 | 575 29 28 15 11 29 14 11 --- 7 | 3 3 3 6 5 4 3 --- 3
R19 | 1551 78 71 24 12 36 29 27 --- 14 | 3 4 3 4 5 2 2 --- 2
R20 | 1235 27 46 26 18 28 42 24 --- 12 | 3 7 3 10 6 2 3 --- 4
R21 | 1638 40 40 19 12 15 19 25 52 9 | 2 3 2 3 3 3 3 17 2
R22 | 939 52 57 32 12 35 24 24 --- 12 | 2 3 3 3 3 5 4 --- 2
R23 | 1035 22 27 18 15 14 30 18 --- 8 | 2 4 4 2 4 3 3 --- 2
R24 | 769 37 44 28 15 19 62 25 --- 14 | 4 6 4 4 7 2 3 --- 3
XR26 | ---- 24 197 --- --- --- --- 9 --- 14 | 5 39 --- --- --- --- 6 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1011 42 43 21 15 26 32 20 202 |T 2 5 2 3 3 3 2 18 2
WRMS | 1011 37 38 21 13 27 31 20 202 |NE 2 5 2 3 3 3 2 18 2
MEDI | 775 36 39 19 12 26 25 18 67 |MD 2 3 3 3 3 3 3 17 2
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