[IGSREPORT-26126] Wk 2016 IGLOS Final Orbits
acc
acc at igs.org
Sat Sep 15 04:17:11 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2016 (Aug 26, 2018 - Sep 01, 2018)
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 2.2016.
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:
igl2016[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2016 in the SP3 format.
igl20167.sum Combination Report for GPS Week 2016.
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 | 3.9 ns
1 | 2.7 ns
2 | 2.9 ns
3 | 6.7 ns
4 | 6.7 ns
5 | 3.7 ns
6 | 1.4 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
----+--------+---------------
2 | GRG | R18
2 | IAC | R18
4 | COD | R18
5 | IAC | R18
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 1.2016, 1a.2016).
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 2.2016.0-6)
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 3.2016.0-6).
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 2016 summary. (Aug 26, 2018 - Sep 01, 2018)
Table 1.2016.a GPS week : 2016 MJD: 58356.0-58362.0
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 -1 4 -2 -14 4 .03 33 32 | 2181745 849 169776 295081
| 1 1 2 14 12 39 .05 | 3741470 3827
cof n/a| 0 0 6 4 -17 6 .06 36 34 | 2194218 904 169777 295080
| 1 2 2 17 13 31 .03 | 3760486 3869
emx n/a| -2 0 -3 42 -22 0 .10 24 23 | 511 -719 3590 9254
| 1 0 2 24 24 75 .08 | 8135 1681
esx n/a| 0 0 -1 -1 3 11 .12 14 13 | 3160 117 3968 10980
| 0 0 0 14 16 23 .02 | 8873 2761
gfz n/a| 0 1 -6 20 28 28 .07 26 24 | 0 -19 3567 9419
| 1 1 1 13 25 20 .09 | 0 2123
grg n/a| 0 0 8 -73 6 -126 -.36 41 36 | 4017 -11 3552 9301
| 2 1 7 13 38 63 .06 | 1539 2410
iac n/a| 1 0 1 -16 6 23 -.17 21 21 | 2155131 964 289022 294446
| 1 0 2 49 54 67 .04 | 3672732 3093
mcc n/a| 2 1 22 -14 24 -152 -.68 173 173 | --- --- --- ---
| 6 12 16 123 60 635 .61 | --- ---
Table 1.2016.b GPS week : 2016 MJD: 58356.0-58362.0
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 15 15 15 18 19 21 |
R02 | 7 6 9 12 9 9 8 |
R03 | 9 10 10 12 11 10 9 |
R04 | 8 8 8 7 7 7 7 |
R05 | 20 19 19 12 9 8 10 |
R07 | 10 10 10 8 8 9 7 |
R08 | 8 8 10 8 9 7 8 |
R09 | 7 6 6 6 7 6 5 |
R10 | 7 7 6 7 8 6 8 |
R11 | 10 9 7 8 9 7 10 |
R13 | 12 11 8 9 8 8 7 |
R14 | 10 13 9 8 9 9 9 |
R15 | 14 16 15 15 13 13 12 |
R16 | 13 14 13 15 17 16 15 |
R17 | 10 11 9 9 9 9 11 |
R18 | 9 8 98 406 175 167 11 |
R19 | 17 16 16 19 17 16 13 |
R20 | 12 11 11 12 12 13 15 |
R21 | 9 10 12 11 11 10 10 |
R22 | 9 10 10 10 11 9 10 |
R23 | 10 10 7 7 8 7 9 |
R24 | 14 15 15 20 12 15 17 |
R26 | 25 25 19 14 17 16 12 |
Table 1.2016.c GPS week : 2016 MJD: 58356.0-58362.0
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 2016 0 | 66 -13 186 -305 245 971 81.4 1473 1473 | 3907 0
brd 2016 1 | 49 39 109 69 -366 -801 82.5 1388 1388 | 2671 0
brd 2016 2 | -94 -30 59 892 -506 -749 82.0 1313 1313 | 2891 0
brd 2016 3 | -102 3 144 -553 -449 166 83.3 1370 1370 | 6676 0
brd 2016 4 | 26 -42 116 558 -629 2311 83.4 1207 1207 | 6724 0
brd 2016 5 | 59 -1 93 401 469 2049 83.1 1461 1461 | 3717 0
brd 2016 6 | 3 19 126 945 412 -82 83.3 1611 1611 | 1449 0
-------------+------------------------------------------------------------+----------------
brd 2016 mean| 1 -3 119 286 -117 552 82.7 1403 1403 | 4005 0
brd 2016 sdev| 71 28 39 576 472 1264 .8 128 128 | 2007 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 2.2016.0 GPS week: 2016 Day: 0 MJD: 58356
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 6 -23 -14 37 -.00 32 30 | 2825 -15 3264 9153
cof n/a| -2 0 8 -26 -33 40 .06 34 32 | 2800 15 3266 9154
emx n/a| -3 0 0 30 -26 -23 .03 21 21 | -3410 -177 3272 8816
esx n/a| 0 0 -1 20 14 4 .10 15 14 | -1590 521 3273 11246
gfz n/a| 0 0 -8 29 62 63 .14 26 23 | 0 269 3271 9054
grg n/a| 0 0 -2 -56 15 -52 -.31 35 32 | 3965 194 3301 8676
iac n/a| 2 0 0 -25 -21 45 -.15 22 22 | 5321 -878 4478 9249
mcc n/a| 3 3 12 -129 -30 -453 -1.76 167 167 | --- --- --- ---
Table 2.2016.1 GPS week: 2016 Day: 1 MJD: 58357
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 4 -14 -10 16 .07 34 33 | 1495 418 3168 10037
cof n/a| 0 1 4 -6 -25 5 .11 36 34 | 1485 435 3168 10033
emx n/a| -3 0 -2 18 -48 -113 .03 22 22 | -4402 -450 3189 9778
esx n/a| 0 0 0 -17 27 -13 .09 14 13 | 13640 -1134 3190 12054
gfz n/a| 0 1 -5 27 40 3 .10 30 25 | 0 42 3198 9874
grg n/a| 3 0 7 -53 47 -45 -.33 45 38 | 2476 542 3167 9737
iac n/a| 0 1 -1 53 -38 108 -.15 20 20 | 1188 108 4929 18028
mcc n/a| 4 -13 34 103 -62 57 -.82 130 130 | --- --- --- ---
Table 2.2016.2 GPS week: 2016 Day: 2 MJD: 58358
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 0 -6 -22 -6 .05 33 32 | 2944 -4302 3396 9677
cof n/a| 0 0 4 12 1 0 .05 37 38 | 2962 -4346 3403 9679
emx n/a| 0 0 -1 94 -46 -77 -.00 22 22 | 8866 -3306 3439 9362
esx n/a| 0 0 -1 1 13 0 .13 13 12 | 4927 -2729 3420 11782
gfz n/a| -2 1 -6 3 12 42 .21 24 23 | 0 -3193 3351 9500
grg n/a| -3 0 16 -82 -45 -120 -.40 52 44 | 4854 -3522 3394 9635
iac n/a| 2 0 0 -77 52 88 -.21 21 21 | 7686 -1140 4220 12044
mcc n/a| 0 4 48 -30 -19 472 -.23 124 124 | --- --- --- ---
Table 2.2016.3 GPS week: 2016 Day: 3 MJD: 58359
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 -3 5 18 -17 45 .08 37 36 | -10900 3779 4255 26464
cof n/a| 0 -2 7 1 -32 6 .08 35 34 | -10923 3816 4250 26461
emx n/a| -1 0 -5 33 -43 48 .19 27 26 | -9540 1373 4073 10240
esx n/a| 0 -1 -2 -15 -17 -15 .09 14 12 | -6487 1638 4051 12529
gfz n/a| 0 2 -8 6 4 15 .05 26 19 | 0 3150 4018 10321
grg n/a| 2 -3 0 -81 -20 -225 -.47 45 34 | 4488 3583 3968 9972
iac n/a| 0 0 6 37 104 55 -.11 20 21 | 6446 858 5150 11746
mcc n/a| 13 26 -3 -129 89 715 .15 186 186 | --- --- --- ---
Table 2.2016.4 GPS week: 2016 Day: 4 MJD: 58360
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 -4 5 -1 -37 28 .06 31 30 | 7042340 2508 999999 999999
cof n/a| 0 -4 7 15 -16 50 .05 34 32 | 7129701 2849 999999 999999
emx n/a| -2 0 -1 29 0 95 .13 25 25 | -4339 -1704 3446 8636
esx n/a| 1 0 -1 -11 8 27 .14 14 13 | 3675 462 4487 9122
gfz n/a| 1 1 -7 10 60 22 .04 24 27 | 0 188 3421 8686
grg n/a| 3 0 9 -74 63 -160 -.31 39 39 | 6808 -174 3333 8894
iac n/a| 1 0 3 -1 -35 -63 -.21 23 23 | 7652386 5054 999999 999999
mcc n/a| -4 -6 16 151 59 -899 -.98 210 210 | --- --- --- ---
Table 2.2016.5 GPS week: 2016 Day: 5 MJD: 58361
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 5 0 2 -18 -.05 33 31 | 8229032 6646 170252 999999
cof n/a| -1 0 8 26 -6 -18 .04 35 34 | 8229030 6654 170250 999999
emx n/a| 0 0 -6 49 -6 53 .11 24 24 | 12942 1086 3821 8723
esx n/a| 0 1 -1 5 -6 33 .15 13 12 | 14984 5021 5460 9071
gfz n/a| -1 2 -4 38 14 16 .00 26 26 | 0 1528 3834 8851
grg n/a| 1 0 12 -78 -5 -125 -.37 37 31 | 2756 1774 3824 8698
iac n/a| 2 -1 1 -62 -32 -45 -.20 20 20 | 7408559 5360 999999 999999
mcc n/a| 1 -3 30 -140 85 -910 -.69 196 196 | --- --- --- ---
Table 2.2016.6 GPS week: 2016 Day: 6 MJD: 58362
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 2 10 -2 -68 .00 31 30 | 4479 -3086 4103 10238
cof n/a| 0 0 3 9 -10 -38 .03 38 32 | 4474 -3090 4107 10238
emx n/a| -2 0 -8 37 11 22 .19 25 24 | 3462 -1861 3892 9228
esx n/a| 0 -1 -1 8 -13 44 .13 16 13 | -7026 -2954 3897 11059
gfz n/a| -2 0 -5 27 4 39 -.05 27 24 | 0 -2119 3876 9647
grg n/a| -1 0 16 -87 -12 -154 -.35 38 35 | 2774 -2475 3880 9497
iac n/a| 2 -1 0 -41 12 -19 -.15 21 21 | 4333 -2612 4383 10063
mcc n/a| -3 0 16 75 49 -49 -.44 198 198 | --- --- --- ---
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 3.2016.0 GPS week: 2016 Day: 0 MJD: 58356
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 732 64 71 28 21 24 30 27 --- 14 | 62 63 95 82 95 81 82 --- 80
R02E | 914 16 27 19 13 18 21 12 139 7 | 153 154 151 157 155 154 151 153 153
R03E | 1418 42 44 15 7 23 14 12 109 8 | 106 110 93 97 94 103 98 186 96
R04E | 758 33 38 11 8 25 17 13 --- 7 | 56 59 54 52 55 58 55 --- 52
XR05E |12343 26 32 --- --- --- --- 14 --- 19 | 91 90 --- --- --- --- 84 --- 86
R07E | 757 39 44 15 7 26 28 19 246 9 | 70 71 59 62 69 67 60 113 61
R08E | 2006 26 27 15 10 26 23 12 --- 8 | 68 70 63 68 69 73 63 --- 65
R09 | 915 9 11 12 13 16 16 25 --- 7 | 61 64 59 63 64 60 69 --- 61
R10 | 1006 12 11 10 14 25 25 16 --- 7 | 70 74 69 73 67 75 68 --- 69
R11 | 672 20 16 27 15 14 37 20 195 10 | 82 82 67 82 76 88 71 62 75
R13 | 2486 13 13 10 14 23 67 14 --- 11 | 78 78 74 76 70 112 71 --- 75
R14 | 1010 29 33 16 18 26 35 22 --- 10 | 91 92 82 79 72 95 72 --- 78
R15 | 3056 49 51 32 26 23 23 36 --- 14 | 93 95 82 66 64 72 62 --- 68
R16 | 564 32 34 22 19 19 52 26 --- 12 | 86 85 67 80 77 98 72 --- 75
R17 | 660 32 32 14 11 27 29 27 --- 10 | 39 40 41 36 35 43 34 --- 35
R18 | 2215 27 26 8 16 25 18 20 --- 8 | 109 165 26 140 35 37 148 --- 124
R19 | 2256 50 53 37 21 58 35 29 --- 16 | 38 38 52 35 39 34 32 --- 35
R20 | 664 12 23 24 15 31 54 24 --- 12 | 34 35 46 45 40 50 29 --- 38
R21 | 831 23 27 16 9 20 25 26 99 8 | 49 47 43 54 58 50 53 74 49
R22 | 925 31 30 10 7 33 18 22 --- 8 | 29 28 31 34 39 27 34 --- 32
R23 | 897 16 17 28 23 16 21 14 --- 9 | 37 40 39 39 41 41 30 --- 35
R24 | 2145 31 20 33 18 19 64 23 --- 14 | 44 51 51 46 46 41 37 --- 41
XR26 | 2163 29 80 --- --- --- --- 21 --- 24 | 44 88 --- --- --- --- 32 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1473 32 34 21 15 26 35 22 167 |T 69 74 64 69 64 69 65 117 66
WRMS | 1473 30 32 21 14 23 32 22 167 |NE 61 68 55 63 54 61 57 68 57
MEDI | 925 29 30 16 14 24 25 21 139 |MD 68 71 59 66 64 67 63 113 65
Table 3.2016.1 GPS week: 2016 Day: 1 MJD: 58357
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1326 58 54 34 14 32 65 22 --- 15 | 62 61 87 81 86 80 74 --- 75
R02E | 1095 18 8 12 5 24 20 8 88 5 | 139 138 142 136 141 135 139 138 138
R03E | 2151 40 49 18 7 30 40 10 139 9 | 66 70 55 54 58 69 57 211 56
R04E | 838 28 31 19 9 22 24 16 --- 8 | 44 46 46 45 47 47 47 --- 44
XR05E | 2278 25 24 --- --- --- --- 14 --- 19 | 67 61 --- --- --- --- 69 --- 65
R07E | 941 39 39 15 9 30 29 19 173 9 | 55 55 49 53 55 60 51 73 51
R08E | 1674 32 33 13 9 23 24 12 --- 7 | 54 54 50 50 51 55 51 --- 50
R09 | 1420 9 11 9 11 16 9 20 --- 6 | 51 49 46 46 58 49 61 --- 50
R10 | 814 11 21 19 10 23 19 17 --- 7 | 51 48 42 53 49 56 57 --- 50
R11 | 797 19 15 18 8 36 35 16 141 8 | 56 54 47 55 57 66 58 67 54
R13 | 2861 10 17 18 13 19 73 10 --- 10 | 57 60 50 60 56 85 59 --- 57
R14 | 870 31 24 16 20 36 73 12 --- 12 | 61 60 55 60 57 88 58 --- 57
R15 | 1369 61 59 36 21 43 23 35 --- 16 | 63 63 54 49 47 49 52 --- 49
R16 | 670 30 42 40 21 15 68 24 --- 14 | 65 74 56 55 55 63 63 --- 56
R17 | 635 35 35 22 15 29 25 26 --- 10 | 37 39 38 36 31 34 36 --- 34
R18 | 2411 32 25 12 12 24 19 13 --- 7 | 107 175 24 183 34 36 156 --- 121
R19 | 1484 64 62 27 25 48 38 31 --- 16 | 30 29 30 36 43 33 27 --- 30
R20 | 950 22 20 24 18 27 53 18 --- 11 | 36 38 36 31 34 36 24 --- 28
R21 | 1045 30 29 21 10 33 42 19 88 10 | 46 46 45 44 49 43 50 56 45
R22 | 785 30 27 16 7 25 30 31 --- 9 | 32 27 31 35 34 46 36 --- 33
R23 | 926 17 18 26 20 17 31 17 --- 9 | 31 32 33 35 32 39 36 --- 32
R24 | 1407 31 63 26 13 42 93 26 --- 15 | 51 76 47 31 40 48 39 --- 35
XR26 | 2157 28 69 --- --- --- --- 22 --- 24 | 45 65 --- --- --- --- 33 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1387 34 36 22 14 30 45 20 130 |T 56 61 50 58 53 57 57 109 54
WRMS | 1387 33 34 22 13 25 38 20 130 |NE 51 58 42 53 45 51 52 61 47
MEDI | 1095 30 29 19 12 27 31 18 139 |MD 54 55 47 50 49 49 52 73 50
Table 3.2016.2 GPS week: 2016 Day: 2 MJD: 58358
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1986 50 45 38 13 23 53 42 --- 15 | 87 92 116 94 104 78 85 --- 92
R02E | 1423 15 21 21 11 18 52 23 60 9 | 135 134 135 136 134 139 135 171 134
R03E | 1142 43 41 15 9 27 36 17 135 10 | 131 128 114 114 111 126 117 241 116
R04E | 782 30 34 15 10 21 39 12 --- 8 | 49 48 41 38 42 61 36 --- 38
XR05E | 1155 37 55 --- --- 25 --- 18 --- 19 | 94 98 --- --- 69 --- 76 --- 80
R07E | 1163 37 33 16 9 25 53 17 185 10 | 58 59 53 52 56 82 46 84 51
R08E | 1798 28 30 17 11 22 59 19 --- 10 | 56 60 51 52 54 78 48 --- 50
R09 | 1531 9 15 11 7 17 27 11 --- 5 | 34 40 36 40 51 19 35 --- 36
R10 | 1118 19 25 13 13 13 20 12 --- 6 | 38 42 36 47 44 43 41 --- 41
R11 | 804 21 23 13 9 24 23 14 112 7 | 42 45 40 36 30 45 35 66 35
R13 | 2135 13 13 12 10 11 58 15 --- 7 | 47 47 44 45 43 78 39 --- 44
R14 | 1218 21 29 15 12 21 47 16 --- 8 | 50 57 43 43 39 67 38 --- 42
R15 | 1623 57 62 33 13 46 34 27 --- 15 | 56 60 40 30 33 39 26 --- 30
R16 | 654 29 37 40 24 19 58 20 --- 13 | 48 56 45 43 40 46 38 --- 41
R17 | 721 23 30 13 8 23 37 24 --- 8 | 19 23 21 26 26 31 23 --- 21
XR18 | 2101 99 427 --- --- 96 185 273 --- 97 | 150 384 --- --- 60 133 217 --- 118
R19 | 747 74 80 18 24 26 49 28 --- 16 | 23 32 28 25 23 27 21 --- 17
R20 | 1481 12 18 16 19 20 79 13 --- 10 | 39 45 36 26 22 37 21 --- 25
R21 | 987 28 35 21 8 37 59 27 90 11 | 31 32 27 30 32 65 35 50 31
R22 | 788 24 45 18 12 24 49 20 --- 9 | 26 30 19 29 21 34 19 --- 20
R23 | 1402 15 15 22 14 8 28 11 --- 7 | 22 23 21 16 23 17 15 --- 15
R24 | 1344 36 33 31 9 21 104 26 --- 14 | 50 47 53 32 34 21 31 --- 34
XR26 | 1382 21 48 --- --- --- --- 18 --- 19 | 23 44 --- --- --- --- 24 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1313 33 37 22 13 24 52 21 124 |T 56 70 49 47 49 60 52 122 49
WRMS | 1313 32 38 22 12 23 44 21 124 |NE 43 62 34 33 34 46 41 58 35
MEDI | 1218 28 33 16 11 22 49 18 112 |MD 48 47 40 38 40 46 36 84 38
Table 3.2016.3 GPS week: 2016 Day: 3 MJD: 58359
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1961 61 45 28 20 35 55 19 --- 15 | 49 50 68 76 85 70 69 --- 66
R02E | 1499 21 22 17 18 28 36 36 64 11 | 151 148 150 160 156 150 140 184 150
R03E | 1125 57 44 29 17 18 28 16 161 12 | 156 166 155 165 157 166 145 254 156
R04E | 930 26 21 13 9 19 19 13 --- 7 | 44 44 45 43 46 46 48 --- 43
R05E | 1388 26 38 38 21 22 26 19 --- 11 | 85 89 32 25 37 30 82 --- 80
R07E | 831 33 33 16 10 21 19 15 357 8 | 47 50 56 58 58 55 59 168 54
R08E | 1255 27 27 12 8 19 25 20 --- 7 | 48 54 46 47 56 47 54 --- 47
R09 | 1929 10 11 20 6 9 20 9 --- 5 | 25 28 29 28 32 27 30 --- 27
R10 | 1059 13 13 14 12 16 27 11 --- 6 | 42 38 41 50 40 67 47 --- 46
R11 | 612 13 12 12 13 14 23 23 80 7 | 50 51 41 55 54 50 45 61 47
R13 | 596 8 11 15 14 17 44 17 --- 8 | 50 53 45 56 40 73 43 --- 49
R14 | 1074 30 19 21 6 17 16 22 --- 8 | 58 53 49 40 36 49 34 --- 40
R15 | 2889 56 47 36 10 43 38 31 --- 15 | 71 65 57 37 43 45 31 --- 41
R16 | 714 50 59 38 16 30 66 18 --- 15 | 55 58 55 44 43 62 47 --- 46
R17 | 688 29 28 19 9 19 26 27 --- 9 | 31 32 39 34 34 38 28 --- 32
XR18 | 2715 563 1192 --- --- --- --- 294 --- 406 | 555 9999 --- --- --- --- 891 --- 774
R19 | 932 75 74 30 25 52 65 25 --- 18 | 34 37 42 41 42 47 27 --- 33
R20 | 1539 17 27 35 18 19 52 15 --- 11 | 43 60 44 46 29 31 29 --- 33
R21 | 730 42 40 26 9 36 24 20 93 11 | 31 35 32 39 45 49 33 63 36
XR22 | 833 35 38 17 7 25 --- 17 --- 9 | 34 41 35 37 35 --- 34 --- 35
R23 | 1797 15 18 15 13 16 19 16 --- 6 | 32 40 34 36 39 41 36 --- 33
R24 | 1420 31 33 55 17 22 121 17 --- 19 | 42 48 40 39 53 65 32 --- 35
XR26 | 1269 14 59 --- --- --- --- 13 --- 14 | 30 56 --- --- --- --- 33 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1369 37 35 27 14 26 45 20 185 |T 76 58 54 55 55 60 87 146 84
WRMS | 1369 36 34 26 12 19 34 21 185 |NE 73 46 41 41 40 49 88 62 83
MEDI | 1125 29 33 20 13 19 26 18 93 |MD 47 50 44 43 43 49 43 168 43
Table 3.2016.4 GPS week: 2016 Day: 4 MJD: 58360
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1389 55 65 47 25 39 52 39 --- 18 | 75 79 83 69 86 80 67 --- 69
R02E | 2000 24 34 21 9 21 37 19 165 9 | 193 202 198 195 196 192 189 244 193
R03E | 1017 38 24 22 12 21 38 14 393 10 | 97 102 101 99 100 90 100 326 97
R04E | 944 19 23 15 7 18 19 13 --- 6 | 39 41 34 38 38 40 39 --- 36
R05E | 1348 27 28 22 13 16 32 15 --- 9 | 76 79 31 23 29 27 64 --- 66
R07E | 678 29 41 21 8 21 19 16 100 8 | 62 63 65 62 68 66 66 204 63
R08E | 769 21 28 20 10 21 34 16 --- 8 | 52 55 54 54 53 56 54 --- 52
R09 | 2027 13 12 21 13 17 19 11 --- 7 | 35 33 35 42 45 31 45 --- 38
R10 | 1235 10 16 17 13 22 33 14 --- 8 | 40 38 32 44 36 57 39 --- 38
R11 | 656 14 12 16 12 18 32 27 115 8 | 42 40 37 48 45 51 44 107 42
R13 | 891 12 17 23 18 11 22 15 --- 8 | 50 48 42 63 48 49 49 --- 50
R14 | 901 23 22 17 9 34 29 16 --- 9 | 55 52 46 47 38 55 44 --- 44
R15 | 1917 45 44 35 9 28 19 38 --- 13 | 64 62 53 38 36 55 33 --- 40
R16 | 698 15 26 35 20 21 85 42 --- 16 | 53 56 47 58 50 82 50 --- 50
R17 | 874 25 27 13 9 13 17 34 --- 8 | 26 27 28 34 41 30 25 --- 27
XR18 | 2087 358 276 --- 128 --- --- 237 --- 174 | 125 205 --- 107 --- --- 244 --- 257
R19 | 1022 70 73 23 20 50 39 21 --- 16 | 23 23 27 35 34 22 22 --- 24
R20 | 1332 18 20 32 21 14 57 18 --- 12 | 30 38 36 34 35 27 26 --- 26
R21 | 525 36 33 22 13 18 31 32 127 11 | 36 37 39 35 38 35 49 33 36
XR22 | 711 39 31 14 8 29 --- 14 --- 10 | 29 22 24 24 32 --- 26 --- 24
R23 | 1400 9 14 12 18 25 30 11 --- 8 | 25 27 23 28 31 40 23 --- 23
R24 | 861 34 50 29 11 27 55 13 --- 12 | 34 51 31 33 39 77 28 --- 26
XR26 | 1657 19 81 --- --- --- --- 14 --- 16 | 36 77 --- --- --- --- 26 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1206 31 34 25 14 24 39 23 210 |T 56 63 50 55 53 58 58 182 58
WRMS | 1206 30 32 25 13 27 39 23 210 |NE 43 52 35 44 39 47 48 70 48
MEDI | 1017 24 28 21 12 21 32 16 127 |MD 42 51 37 42 39 51 44 204 40
Table 3.2016.5 GPS week: 2016 Day: 5 MJD: 58361
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 504 70 66 36 28 40 59 38 --- 19 | 54 55 54 64 72 53 64 --- 52
R02E | 3377 27 23 27 8 23 28 16 123 9 | 124 121 118 115 116 120 118 147 117
R03E | 1871 33 38 21 8 29 36 16 375 9 | 70 71 56 59 66 72 62 279 60
R04E | 873 24 23 19 8 22 19 12 --- 7 | 38 39 35 32 42 34 35 --- 32
R05E | 1336 25 29 18 13 16 23 13 --- 7 | 65 64 22 23 29 25 60 --- 61
R07E | 704 32 31 21 5 27 19 14 87 8 | 49 48 52 49 56 48 51 84 49
R08E | 679 20 25 20 8 22 21 13 --- 7 | 44 47 50 43 45 42 47 --- 43
R09 | 2498 8 12 9 10 17 14 17 --- 5 | 36 40 32 33 46 33 47 --- 36
R10 | 1515 11 16 13 6 27 21 9 --- 6 | 37 45 39 38 40 47 42 --- 38
R11 | 561 18 17 11 9 19 20 15 112 6 | 55 55 48 54 55 57 51 74 51
R13 | 713 16 18 19 9 13 44 12 --- 8 | 50 57 47 48 50 64 53 --- 49
R14 | 991 20 24 19 10 26 24 23 --- 8 | 55 57 53 54 50 55 51 --- 52
R15 | 2865 50 49 37 16 28 28 28 --- 13 | 51 52 47 36 39 42 37 --- 38
R16 | 710 13 15 52 9 33 75 17 --- 15 | 56 58 48 47 60 68 54 --- 51
R17 | 911 28 32 21 11 22 24 23 --- 9 | 27 29 27 31 30 31 22 --- 26
XR18 | 1035 287 279 --- 97 --- --- 289 --- 167 | 101 184 --- 152 --- --- 152 --- 227
R19 | 1574 69 69 19 21 31 25 39 --- 15 | 29 36 37 45 43 34 26 --- 32
R20 | 774 35 46 19 15 32 62 20 --- 13 | 43 47 48 24 22 23 26 --- 26
R21 | 838 30 39 22 6 29 21 29 131 9 | 28 31 23 24 24 28 25 50 23
R22 | 638 34 39 18 13 14 26 19 --- 9 | 19 20 27 24 19 26 20 --- 18
R23 | 1121 16 14 20 16 14 22 8 --- 7 | 22 22 21 23 22 27 15 --- 18
R24 | 901 21 24 27 24 40 72 13 --- 14 | 48 52 54 38 36 37 26 --- 34
XR26 | 1432 20 103 --- --- --- --- 11 --- 15 | 29 97 --- --- --- --- 30 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1461 33 35 24 13 26 37 20 196 |T 49 57 44 48 45 46 48 126 50
WRMS | 1461 31 34 24 12 26 31 20 196 |NE 42 55 39 44 38 40 42 62 46
MEDI | 911 25 29 20 10 26 24 16 123 |MD 48 52 47 38 43 42 47 84 38
Table 3.2016.6 GPS week: 2016 Day: 6 MJD: 58362
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 594 64 74 29 46 44 48 42 --- 20 | 51 53 65 78 81 57 64 --- 58
R02E | 3681 25 16 24 8 21 20 13 143 8 | 177 179 179 180 190 173 170 183 177
R03E | 1097 32 37 25 9 22 22 19 371 9 | 70 72 75 81 81 74 80 247 76
R04E | 973 22 24 18 8 19 23 14 --- 7 | 40 40 38 37 42 39 40 --- 36
R05E | 1090 31 20 24 7 22 34 15 --- 9 | 64 61 29 24 42 33 65 --- 58
R07E | 1311 27 25 21 5 20 18 9 128 7 | 47 50 54 52 60 57 57 115 52
R08E | 622 15 15 24 8 22 28 15 --- 8 | 44 43 47 45 54 49 51 --- 45
R09 | 3178 12 11 14 9 15 13 9 --- 5 | 52 51 47 50 52 47 53 --- 49
R10 | 2115 19 22 18 20 16 21 15 --- 8 | 58 58 55 61 50 69 54 --- 56
R11 | 1140 17 20 13 8 36 48 10 101 9 | 70 73 58 67 65 82 64 89 64
R13 | 813 10 14 19 6 16 31 9 --- 6 | 63 61 55 66 58 94 64 --- 63
R14 | 683 20 20 10 11 22 37 21 --- 8 | 77 78 74 72 60 87 62 --- 69
R15 | 2410 44 44 32 15 39 11 21 --- 12 | 81 78 71 52 51 61 45 --- 54
R16 | 597 13 23 26 19 38 68 35 --- 14 | 84 88 78 85 75 109 69 --- 79
R17 | 741 36 31 30 6 42 18 20 --- 11 | 27 30 24 31 44 40 28 --- 28
R18 | 1053 19 25 29 27 19 26 22 --- 11 | 92 167 51 142 42 51 139 --- 194
R19 | 2673 56 59 25 15 24 17 33 --- 13 | 36 37 37 33 34 51 33 --- 30
R20 | 939 43 77 30 15 20 69 27 --- 14 | 54 77 47 34 38 31 30 --- 33
R21 | 894 31 26 21 9 33 24 22 108 10 | 35 33 36 34 33 34 35 53 33
R22 | 1440 29 30 11 6 30 40 22 --- 10 | 27 27 25 26 26 26 27 --- 24
R23 | 918 23 30 23 16 15 21 16 --- 8 | 26 32 21 24 20 24 27 --- 21
R24 | 1074 26 69 47 26 24 82 12 --- 16 | 65 103 48 32 39 40 35 --- 36
XR26 | 2514 14 103 --- --- --- --- 10 --- 12 | 33 95 --- --- --- --- 30 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1610 31 38 25 16 27 38 21 198 |T 59 68 55 59 56 60 57 137 59
WRMS | 1610 30 32 24 13 24 35 21 198 |NE 55 68 48 53 45 56 49 71 53
MEDI | 1074 25 25 24 9 22 24 16 128 |MD 54 61 48 50 50 51 53 115 52
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