[IGSREPORT-25103] Wk 1935 IGLOS Final Orbits
acc
acc at igs.org
Mon Feb 27 18:02:20 PST 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1935 (Feb 05, 2017 - Feb 11, 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 2.1935.
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:
igl1935[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1935 in the SP3 format.
igl19357.sum Combination Report for GPS Week 1935.
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 | -6.1 ns
1 | -9.1 ns
2 | -9.9 ns
3 | -10.1 ns
4 | -5.9 ns
5 | -6.0 ns
6 | -6.3 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 1.1935, 1a.1935).
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 2.1935.0-6)
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 3.1935.0-6).
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 1935 summary. (Feb 05, 2017 - Feb 11, 2017)
Table 1.1935.a GPS week : 1935 MJD: 57789.0-57795.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 -6 0 -21 -25 .08 31 29 | -17475 -506 3147 11361
| 1 1 1 22 16 29 .02 | 1929 709
cof n/a| 0 0 -10 0 -2 -26 .09 34 31 | -17485 -498 3146 11363
| 1 0 2 10 22 25 .04 | 1928 710
emx n/a| 0 -1 -1 27 -23 -32 .12 21 21 | -12350 153 3134 10344
| 1 1 1 16 12 32 .02 | 12801 1014
esx n/a| 1 0 0 -1 0 24 .15 20 18 | -8801 -956 3144 13535
| 1 1 1 17 9 29 .02 | 10589 882
gfz n/a| -1 0 6 30 23 27 -.01 32 30 | 0 -118 3127 10712
| 2 2 1 21 26 54 .05 | 0 742
grg n/a| 0 1 4 -54 33 0 -.40 26 25 | -1 -14532 3179 11132
| 1 1 4 12 18 79 .05 | 19188 35680
Table 1.1935.b GPS week : 1935 MJD: 57789.0-57795.0
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 | 13 20 12 14 13 16 14 |
R02 | 12 12 10 10 8 7 12 |
R03 | 15 12 12 13 12 13 10 |
R04 | 14 14 13 12 11 11 12 |
R05 | 18 18 16 18 14 14 15 |
R06 | 11 9 11 12 11 11 11 |
R07 | 10 10 13 13 13 12 12 |
R08 | 11 10 10 10 10 12 8 |
R09 | 8 10 8 14 --- 0 0 |
R10 | 11 10 10 9 9 10 11 |
R11 | 10 8 10 8 8 8 7 |
R13 | 8 11 11 10 8 11 9 |
R14 | 17 15 17 13 14 14 12 |
R15 | 11 11 11 10 11 10 11 |
R16 | 10 11 10 13 13 12 14 |
R17 | 12 13 13 12 10 13 12 |
R18 | 10 9 10 11 10 8 11 |
R19 | 17 16 16 19 15 16 14 |
R20 | 15 16 17 15 13 15 16 |
R21 | 9 13 12 11 11 10 12 |
R22 | 13 10 14 14 12 11 10 |
R23 | 11 10 12 13 11 10 10 |
R24 | 17 19 20 29 16 15 18 |
Table 1.1935.c GPS week : 1935 MJD: 57789.0-57795.0
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 1935 0 | 0 23 132 458 -518 603 85.1 1271 1271 | -6102 0
brd 1935 1 | 60 -60 131 167 1012 3291 82.7 1825 1825 | -9112 0
brd 1935 2 | 30 -70 63 258 1797 1704 82.2 1647 1647 | -9873 0
brd 1935 3 | 52 -51 31 -69 1466 909 82.8 1355 1355 | -10059 0
brd 1935 4 | 19 53 68 383 1584 3429 82.8 1388 1388 | -5857 0
brd 1935 5 | -35 -5 -16 333 -118 1804 83.0 1208 1208 | -5955 0
brd 1935 6 | -46 -77 -82 217 -391 997 84.1 1176 1176 | -6303 0
-------------+------------------------------------------------------------+----------------
brd 1935 mean| 11 -27 46 249 690 1819 83.3 1410 1410 | -7608 0
brd 1935 sdev| 41 51 77 172 1001 1136 1.0 240 240 | 1965 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 2.1935.0 GPS week: 1935 Day: 0 MJD: 57789
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 3 -4 -34 -35 -41 .04 33 31 | -19049 568 2993 12553
cof n/a| 0 1 -6 -6 -13 -53 .09 33 31 | -19062 573 2990 12555
emx n/a| 2 0 -3 30 -7 -54 .15 23 23 | -16998 1870 2984 11305
esx n/a| 0 0 -2 6 20 47 .13 19 19 | -23475 -862 2976 14273
gfz n/a| -3 0 2 34 -2 50 .04 31 28 | 0 -116 2979 11861
grg n/a| 0 0 9 -50 6 -47 -.42 27 26 | -5167 -2018 2972 12153
Table 2.1935.1 GPS week: 1935 Day: 1 MJD: 57790
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 -4 -10 6 -30 .07 30 29 | -18375 -294 3165 10965
cof n/a| 0 1 -6 -19 -12 8 .10 36 33 | -18372 -304 3162 10961
emx n/a| 0 -3 2 7 -42 26 .14 22 22 | 4728 502 3130 9973
esx n/a| 0 0 0 3 -3 57 .17 18 17 | -7033 -880 3156 12584
gfz n/a| -1 4 6 59 41 88 .02 35 32 | 0 362 3137 10379
grg n/a| 2 0 -3 -30 51 -141 -.41 26 25 | -7711 -2521 3296 11283
Table 2.1935.2 GPS week: 1935 Day: 2 MJD: 57791
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 -6 1 -34 -17 .10 31 28 | -18522 -580 3288 10675
cof n/a| 0 0 -9 0 -37 11 .09 34 30 | -18524 -589 3291 10684
emx n/a| 0 0 -1 13 -36 -21 .13 18 18 | -27763 -465 3278 9643
esx n/a| 1 -3 0 23 -1 39 .14 24 21 | -15256 -1127 3283 12543
gfz n/a| -1 0 7 13 61 63 .06 35 30 | 0 257 3261 10041
grg n/a| 0 1 2 -58 50 46 -.41 28 26 | -9840 20 3314 10781
Table 2.1935.3 GPS week: 1935 Day: 3 MJD: 57792
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 -7 2 -19 12 .11 33 31 | -19865 -536 3022 10877
cof n/a| -2 0 -9 5 12 -40 .05 34 31 | -19890 -499 3012 10879
emx n/a| 0 0 0 18 -15 -42 .11 25 25 | -18535 -262 3011 10248
esx n/a| 2 0 -3 2 -3 1 .13 19 18 | 1901 21 3032 13673
gfz n/a| -1 0 8 17 2 -29 -.05 31 26 | 0 665 3001 10286
grg n/a| -2 3 8 -62 53 -11 -.48 33 28 | -9483 -838 3030 10716
Table 2.1935.4 GPS week: 1935 Day: 4 MJD: 57793
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 -7 21 -3 -54 .05 30 26 | -15240 -89 3578 12017
cof n/a| -1 0 -10 8 31 -31 .16 36 30 | -15251 -80 3584 12018
emx n/a| -1 0 -1 21 -27 -22 .12 19 19 | -24670 1015 3566 10749
esx n/a| 1 0 -1 2 -7 -28 .18 18 17 | -4726 -2538 3574 14933
gfz n/a| 1 -1 7 26 30 8 -.02 30 29 | 0 246 3567 11281
grg n/a| 0 2 5 -58 19 42 -.44 22 22 | -5852 161 3594 11040
Table 2.1935.5 GPS week: 1935 Day: 5 MJD: 57794
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 -6 31 -35 15 .07 31 30 | -15144 -890 3164 11428
cof n/a| -3 0 -12 11 -8 -39 .08 35 33 | -15168 -853 3159 11425
emx n/a| 0 -1 0 51 -14 -79 .08 19 19 | -4022 -694 3160 10317
esx n/a| 2 0 0 -20 -7 33 .13 20 18 | 5133 49 3151 13621
gfz n/a| 0 0 6 3 36 -55 -.08 32 35 | 0 -821 3133 10746
grg n/a| -1 3 4 -72 19 108 -.30 23 23 | -5254 -1112 3234 11161
Table 2.1935.6 GPS week: 1935 Day: 6 MJD: 57795
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 -10 -11 -27 -58 .10 29 27 | -16132 -1727 2823 11015
cof n/a| 0 0 -13 -3 12 -43 .05 30 28 | -16133 -1736 2827 11022
emx n/a| 1 0 -1 47 -22 -30 .14 20 20 | 805 -892 2809 10174
esx n/a| 2 0 -2 -26 -2 23 .16 20 18 | -18152 -1361 2837 13123
gfz n/a| -5 -4 6 57 -7 65 -.01 32 28 | 0 -1422 2815 10393
grg n/a| 0 1 7 -51 31 3 -.37 23 22 | 43294 -95417 2814 10792
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 3.1935.0 GPS week: 1935 Day: 0 MJD: 57789
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 776 31 47 28 25 29 19 13 | 3 4 4 7 7 9999 3
R02 | 888 30 23 29 18 26 19 12 | 2 9 2 6 4 3 3
R03 | 789 31 30 25 18 39 39 14 | 2 5 2 5 4 4 1
R04 | 1056 41 35 28 13 36 26 14 | 2 3 2 2 2 4 1
R05 | 917 31 41 30 31 30 53 18 | 2 9 2 6 6 4 3
R06 | 1686 20 24 19 18 25 25 10 | 2 7 3 3 2 4 1
R07 | 575 27 26 17 11 28 19 9 | 1 5 2 3 4 5 2
R08 | 936 18 21 10 18 16 40 11 | 2 2 3 5 6 7 2
XR09 | 1759 15 23 13 7 17 --- 7 | 9999 9999 2 4 5 --- 9999
R10 | 654 25 21 26 21 17 22 11 | 3 5 3 7 4 4 4
R11 | 946 25 18 19 16 20 22 10 | 3 5 3 3 3 4 2
R13 | 1184 22 17 18 11 17 17 8 | 2 7 3 5 4 2 3
R14 | 3104 25 29 38 27 40 39 17 | 4 6 3 5 5 4 3
R15 | 2913 28 27 13 19 24 23 10 | 3 5 5 4 3 4 2
R16 | 795 13 20 22 22 14 20 10 | 3 8 2 3 3 3 2
R17 | 511 39 49 15 15 32 25 12 | 2 2 3 3 4 3 2
R18 | 595 24 29 10 9 36 19 9 | 2 3 2 2 3 4 2
R19 | 1315 51 44 21 21 55 24 16 | 2 8 2 3 5 2 2
R20 | 1197 50 34 20 15 43 23 14 | 3 6 3 2 5 3 2
R21 | 593 30 31 13 11 20 18 9 | 2 2 2 4 3 4 2
R22 | 844 38 42 16 18 40 17 12 | 2 3 3 5 4 2 2
R23 | 588 32 34 18 22 27 13 11 | 2 3 2 2 4 4 2
R24 | 914 51 52 34 20 29 36 16 | 3 4 3 5 2 3 2
------+-----------------------------------------+-------------------------------------
RMS | 1271 33 33 23 19 31 27 |T 2 5 2 4 4 3 2
WRMS | 1271 31 31 23 19 28 26 |NE 2 5 2 4 4 3 2
MEDI | 914 30 29 19 18 28 22 |MD 2 5 3 4 4 4 2
Table 3.1935.1 GPS week: 1935 Day: 1 MJD: 57790
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
XR01 | 479 52 40 30 29 36 --- 20 | 2 7 3 8 8 --- 4
R02 | 903 25 39 24 21 26 23 11 | 1 9 2 8 7 4 4
R03 | 1369 34 35 26 16 32 20 12 | 2 4 3 5 6 4 3
R04 | 1990 34 38 25 13 53 19 13 | 2 4 2 3 5 5 2
R05 | 976 35 30 35 35 45 32 18 | 2 8 5 6 5 4 3
R06 | 2206 20 18 13 16 26 22 9 | 2 8 4 4 3 4 2
R07 | 593 25 25 21 10 25 23 10 | 2 5 2 4 4 4 2
R08 | 881 27 22 17 11 30 20 9 | 1 5 3 5 5 6 2
XR09 | 1559 11 19 21 14 16 --- 9 | 9999 9999 3 4 5 --- 9999
R10 | 836 22 22 17 16 25 20 9 | 3 5 3 6 4 5 3
R11 | 1030 22 22 14 12 19 17 8 | 3 5 3 3 3 4 2
R13 | 1214 29 33 21 16 22 22 10 | 3 8 5 6 5 4 3
R14 | 4859 22 32 31 23 39 31 14 | 4 17 4 13 14 5 6
R15 | 4643 20 24 18 21 21 26 10 | 3 5 4 6 6 3 3
R16 | 1041 18 22 24 22 18 21 10 | 3 9 3 6 7 5 3
R17 | 602 41 47 17 12 43 23 12 | 2 4 3 3 5 4 2
R18 | 695 26 35 12 10 23 19 8 | 2 3 2 2 3 4 2
R19 | 1072 45 53 23 17 57 27 15 | 2 7 3 3 5 2 2
R20 | 689 42 77 26 23 45 32 15 | 2 8 4 5 7 3 2
R21 | 909 37 41 19 19 33 24 12 | 2 3 2 6 6 3 3
R22 | 767 30 30 17 10 38 12 10 | 2 4 3 6 5 3 2
R23 | 1045 19 27 17 11 28 27 10 | 2 5 2 4 6 6 2
R24 | 1374 40 43 31 24 41 56 19 | 2 4 3 10 8 6 5
------+-----------------------------------------+-------------------------------------
RMS | 1825 30 36 22 18 35 26 |T 2 6 3 5 5 4 2
WRMS | 1825 29 33 22 17 32 25 |NE 2 6 3 5 5 4 2
MEDI | 1030 27 32 21 16 30 23 |MD 2 5 3 5 5 4 2
Table 3.1935.2 GPS week: 1935 Day: 2 MJD: 57791
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 529 43 59 13 22 30 16 12 | 2 9 3 10 7 1 4
R02 | 799 21 21 17 14 30 15 9 | 2 5 2 6 6 4 3
R03 | 1130 25 28 22 25 32 18 12 | 2 3 4 5 6 5 3
R04 | 1726 33 34 24 14 30 27 12 | 2 3 3 5 7 3 3
R05 | 987 49 55 7 32 47 25 15 | 2 5 4 9 6 3 4
R06 | 1705 23 24 13 8 45 23 11 | 1 5 3 3 4 3 2
R07 | 568 26 28 21 30 35 24 13 | 1 3 3 4 5 3 2
R08 | 609 21 31 19 11 25 22 9 | 1 7 4 4 3 3 2
XR09 | 1090 12 19 13 12 20 --- 8 | 9999 9999 2 2 4 --- 9999
R10 | 1439 20 25 16 19 19 24 9 | 2 4 3 6 5 6 4
R11 | 574 22 35 15 15 25 25 10 | 2 6 3 4 3 4 2
R13 | 1359 29 22 18 19 22 20 10 | 3 4 5 4 4 3 2
R14 | 4814 33 42 23 39 40 36 16 | 3 17 4 17 21 8 9
R15 | 3492 16 16 16 24 19 27 10 | 3 4 4 7 5 3 4
R16 | 1154 20 33 12 26 19 24 10 | 3 9 3 6 8 4 3
R17 | 573 29 30 13 11 56 24 13 | 2 6 3 3 5 4 2
R18 | 707 24 26 18 11 31 19 10 | 2 4 3 2 4 2 2
R19 | 1816 39 54 22 30 45 32 16 | 2 4 3 4 6 3 2
R20 | 563 44 30 15 25 40 48 16 | 3 8 5 5 5 3 3
R21 | 837 38 33 13 14 42 22 12 | 2 2 3 5 6 3 3
R22 | 668 34 33 21 27 30 31 13 | 2 4 2 6 7 3 2
R23 | 1384 19 18 15 27 10 40 12 | 2 5 3 4 5 5 2
R24 | 1203 35 37 22 48 53 42 19 | 2 5 3 10 7 5 5
------+-----------------------------------------+-------------------------------------
RMS | 1646 31 34 18 24 35 28 |T 2 5 3 5 6 3 3
WRMS | 1646 28 30 18 21 29 26 |NE 2 5 3 5 6 3 3
MEDI | 1090 26 30 16 22 30 24 |MD 2 5 3 5 5 3 3
Table 3.1935.3 GPS week: 1935 Day: 3 MJD: 57792
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 532 53 51 21 15 24 26 13 | 2 9 5 10 7 1 4
R02 | 684 11 12 19 14 25 30 10 | 2 2 2 5 2 4 2
R03 | 1533 33 33 31 15 32 24 13 | 2 3 4 4 6 3 2
R04 | 1026 28 31 23 15 24 30 11 | 2 3 3 8 6 2 3
R05 | 644 60 52 20 34 37 28 17 | 2 9 5 10 6 2 5
R06 | 952 23 26 14 19 45 16 12 | 2 4 4 4 5 2 2
R07 | 630 34 32 27 8 43 24 13 | 1 3 3 4 4 4 2
R08 | 807 24 20 14 14 23 26 9 | 2 6 4 3 6 2 2
XR09 | 7073 20 26 10 --- 27 --- 13 | 9999 9999 1 --- 4 --- 9999
R10 | 1751 17 15 15 18 15 18 8 | 3 4 3 5 4 7 3
R11 | 959 15 11 12 12 25 16 8 | 2 5 3 3 2 4 2
R13 | 675 27 25 20 15 15 24 10 | 3 3 3 3 3 3 2
R14 | 3146 23 30 17 21 33 32 12 | 3 10 6 12 15 7 7
R15 | 1954 15 17 22 23 16 15 10 | 3 4 5 5 3 5 3
R16 | 1653 28 51 19 22 27 38 13 | 3 13 5 7 6 7 4
R17 | 618 29 33 17 17 41 21 12 | 2 6 3 5 5 6 4
R18 | 674 19 25 15 10 43 19 10 | 2 4 4 5 4 3 3
R19 | 1855 65 52 28 30 36 31 18 | 2 5 4 6 7 3 3
R20 | 895 30 44 33 27 20 37 15 | 2 6 5 5 2 4 3
R21 | 601 30 29 13 12 32 22 10 | 2 3 3 4 5 3 2
R22 | 600 38 42 21 15 42 23 13 | 2 4 3 5 6 3 2
R23 | 1623 22 22 26 19 15 37 12 | 2 3 2 6 3 5 2
R24 | 2124 41 39 67 23 37 99 29 | 2 5 12 7 5 3 5
------+-----------------------------------------+-------------------------------------
RMS | 1354 33 34 25 19 31 33 |T 2 5 4 5 5 3 3
WRMS | 1354 31 31 25 18 26 28 |NE 2 5 4 5 5 3 3
MEDI | 952 28 30 20 15 27 24 |MD 2 4 4 5 5 3 3
Table 3.1935.4 GPS week: 1935 Day: 4 MJD: 57793
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 872 53 69 19 18 20 16 12 | 2 7 5 7 7 1 3
R02 | 850 16 18 17 10 22 18 8 | 1 5 2 5 2 4 2
R03 | 1165 31 35 22 17 31 25 12 | 2 4 3 3 4 2 2
R04 | 1378 33 30 21 13 27 17 10 | 2 3 4 6 4 2 3
R05 | 620 40 47 23 24 32 26 13 | 2 11 5 10 9 2 4
R06 | 1792 19 18 16 19 33 20 10 | 2 5 4 3 5 2 2
R07 | 902 32 34 23 10 49 15 12 | 1 5 4 3 3 3 2
R08 | 1287 24 22 16 11 32 19 9 | 2 5 3 3 7 3 2
R10 | 2472 20 31 20 16 14 17 8 | 3 6 4 3 4 4 2
R11 | 690 20 22 13 16 18 16 8 | 2 4 3 2 3 6 2
R13 | 819 27 26 13 11 17 16 8 | 3 6 4 4 3 4 3
R14 | 3053 25 29 23 24 36 29 13 | 4 8 5 5 12 4 4
R15 | 903 24 21 21 24 16 18 10 | 2 4 4 3 4 4 3
R16 | 1765 35 50 15 27 29 22 12 | 4 10 4 7 9 7 4
R17 | 772 29 33 19 15 21 15 9 | 1 4 3 5 5 5 3
R18 | 704 20 26 8 17 28 21 9 | 2 4 3 5 4 4 3
R19 | 1182 46 60 27 18 45 20 15 | 2 6 4 6 5 3 3
R20 | 1132 27 31 24 14 20 39 13 | 2 7 5 5 4 7 3
R21 | 574 24 30 14 20 32 23 11 | 2 4 3 3 4 2 2
R22 | 620 31 31 17 10 47 15 11 | 2 4 4 3 4 2 2
R23 | 1193 14 20 21 28 19 19 11 | 2 3 3 7 5 4 2
R24 | 2266 35 48 23 22 38 42 15 | 2 5 10 9 5 2 5
------+-----------------------------------------+-------------------------------------
RMS | 1387 30 36 19 18 30 22 |T 2 5 4 4 5 3 2
WRMS | 1387 26 30 19 17 29 22 |NE 2 5 4 4 5 3 2
MEDI | 903 27 30 19 17 28 19 |MD 2 5 4 5 4 3 3
Table 3.1935.5 GPS week: 1935 Day: 5 MJD: 57794
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 615 62 68 24 13 41 21 15 | 2 6 3 5 5 1 3
R02 | 1426 14 24 11 10 21 17 7 | 2 5 3 5 4 5 3
R03 | 610 32 32 22 14 44 26 13 | 2 4 3 3 5 2 2
R04 | 848 35 40 22 13 31 16 11 | 2 6 5 3 4 2 2
R05 | 638 40 52 19 26 33 29 14 | 2 10 4 7 8 4 3
R06 | 698 25 30 16 26 18 16 10 | 2 6 3 3 5 4 2
R07 | 615 36 35 22 20 36 15 12 | 2 5 3 6 5 3 3
R08 | 1333 22 26 21 16 37 22 11 | 2 4 2 5 6 2 2
XR09 | ---- 4 1584 --- --- --- --- 0 | 1 1 --- --- --- --- 1
R10 | 2327 24 31 17 19 18 22 10 | 3 6 4 3 3 2 2
R11 | 515 18 20 14 15 16 18 8 | 2 4 3 3 3 5 2
R13 | 833 24 25 18 13 25 30 11 | 3 5 4 4 4 4 3
R14 | 3288 16 23 21 34 21 28 13 | 3 9 6 5 11 5 3
R15 | 873 25 32 16 15 21 24 10 | 3 6 2 4 5 2 2
R16 | 1274 31 30 19 21 22 24 11 | 4 8 5 6 7 5 3
R17 | 810 38 42 21 21 33 20 12 | 2 4 2 5 5 5 3
R18 | 819 13 20 14 14 25 14 8 | 2 4 2 3 4 3 2
R19 | 846 51 48 22 21 49 29 16 | 2 6 3 6 6 5 3
R20 | 1213 28 30 22 26 40 31 14 | 3 10 5 9 7 6 5
R21 | 617 28 28 17 15 30 17 10 | 2 3 3 4 4 2 2
R22 | 581 29 31 17 16 35 21 11 | 2 3 3 3 3 2 1
R23 | 626 13 19 18 25 23 20 10 | 2 4 4 5 4 4 2
R24 | 1156 29 44 19 21 47 35 14 | 2 5 3 7 4 3 3
------+-----------------------------------------+-------------------------------------
RMS | 1208 31 35 19 20 32 23 |T 2 5 3 4 5 3 2
WRMS | 1208 30 33 19 18 35 23 |NE 2 5 3 4 5 3 2
MEDI | 819 28 31 19 16 30 21 |MD 2 5 3 5 5 3 2
Table 3.1935.6 GPS week: 1935 Day: 6 MJD: 57795
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 653 40 46 17 12 53 21 13 | 2 4 3 3 4 1 2
R02 | 825 25 23 24 10 37 20 11 | 2 3 2 4 4 4 3
R03 | 1631 27 36 17 11 33 15 9 | 3 3 2 2 4 2 2
R04 | 1321 32 29 18 11 25 29 11 | 2 5 4 3 3 3 2
R05 | 989 39 36 20 30 35 31 15 | 3 5 3 2 4 3 2
R06 | 944 27 27 24 16 27 18 11 | 2 4 2 3 3 3 2
R07 | 885 36 38 21 24 30 13 12 | 3 4 2 5 4 3 3
R08 | 983 20 21 10 7 23 16 7 | 2 3 2 4 3 2 2
XR09 | ---- 7 19 --- --- --- --- 0 | 1 1 --- --- --- --- 1
R10 | 1979 27 26 18 17 21 22 10 | 3 4 3 3 2 2 3
R11 | 548 11 13 14 14 18 14 7 | 3 3 3 3 3 2 2
R13 | 739 17 16 13 18 16 21 8 | 3 3 3 3 3 3 3
R14 | 2613 17 23 19 31 20 26 12 | 3 6 4 4 6 4 3
R15 | 985 22 24 11 20 32 21 10 | 3 5 3 4 3 2 2
R16 | 711 34 26 22 30 26 24 13 | 5 6 4 4 3 4 2
R17 | 1259 32 35 18 9 44 18 11 | 2 3 2 3 3 4 2
R18 | 979 25 20 23 13 32 17 10 | 2 3 2 3 2 2 2
R19 | 819 41 44 21 26 28 25 13 | 2 3 2 4 5 3 3
R20 | 763 35 38 30 29 38 34 16 | 3 8 3 7 5 4 4
R21 | 704 28 33 17 12 46 19 11 | 2 3 2 3 3 3 2
R22 | 530 29 23 19 15 28 12 10 | 2 2 2 3 3 2 2
R23 | 635 16 14 20 26 13 15 10 | 2 3 3 3 2 3 2
R24 | 1789 34 33 30 34 37 43 18 | 3 6 3 3 3 3 2
------+-----------------------------------------+-------------------------------------
RMS | 1175 29 30 20 20 32 23 |T 2 3 2 3 3 2 2
WRMS | 1175 27 28 20 18 28 22 |NE 2 3 2 3 3 2 2
MEDI | 885 27 26 19 16 28 20 |MD 2 3 3 3 3 3 2
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