[IGSREPORT-25100] Wk 1934 IGLOS Final Orbits
acc
acc at igs.org
Sun Feb 26 15:10:54 PST 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1934 (Jan 29, 2017 - Feb 04, 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 2.1934.
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:
igl1934[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1934 in the SP3 format.
igl19347.sum Combination Report for GPS Week 1934.
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 | -2.8 ns
1 | -4.1 ns
2 | -2.4 ns
3 | -6.6 ns
4 | -6.0 ns
5 | -6.7 ns
6 | -9.5 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 1.1934, 1a.1934).
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 2.1934.0-6)
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 3.1934.0-6).
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 1934 summary. (Jan 29, 2017 - Feb 04, 2017)
Table 1.1934.a GPS week : 1934 MJD: 57782.0-57788.0
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 0 -5 18 1 -6 .10 31 32 | -15285 -167 3032 11363
| 1 2 1 16 23 29 .04 | 1078 2373
cof n/a| -1 0 -6 11 -3 -27 .11 34 34 | -15296 -157 3031 11365
| 0 1 3 24 23 26 .08 | 1080 2356
emx n/a| 0 0 -4 37 -46 -51 .11 24 24 | -9129 92 3026 10474
| 0 1 2 26 26 29 .03 | 9145 1916
esx n/a| 0 0 0 -6 8 25 .13 18 16 | -11308 981 3026 13502
| 1 0 1 18 14 13 .03 | 11892 3091
gfz n/a| 0 0 5 0 49 52 -.09 29 27 | 0 303 3027 10812
| 1 1 3 15 36 35 .07 | 0 2275
grg n/a| 0 0 6 -54 14 -34 -.40 30 27 | -5544 381 3040 10878
| 1 1 6 21 31 83 .08 | 1617 2354
Table 1.1934.b GPS week : 1934 MJD: 57782.0-57788.0
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 | 12 11 15 13 14 12 11 |
R02 | 9 9 9 9 8 11 10 |
R03 | 9 7 11 12 11 11 13 |
R04 | 8 9 10 10 10 11 7 |
R05 | 16 15 15 14 15 17 19 |
R06 | 12 13 11 11 10 9 10 |
R07 | 12 10 12 11 12 12 13 |
R08 | 11 10 11 10 11 9 11 |
R09 | 7 8 8 9 9 7 8 |
R10 | 10 11 10 8 9 10 12 |
R11 | 9 8 8 7 8 7 13 |
R13 | 12 10 10 9 10 12 11 |
R14 | 17 21 16 13 14 16 16 |
R15 | 10 10 9 12 10 11 12 |
R16 | 14 13 14 17 14 13 14 |
R17 | 10 13 12 12 13 13 12 |
R18 | 9 10 13 11 9 9 10 |
R19 | 18 17 20 15 17 15 16 |
R20 | 14 19 19 19 15 15 21 |
R21 | 13 13 12 12 13 13 12 |
R22 | 12 11 15 14 15 13 12 |
R23 | 12 10 12 11 11 10 8 |
R24 | 21 21 19 34 14 27 22 |
Table 1.1934.c GPS week : 1934 MJD: 57782.0-57788.0
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 1934 0 | 76 4 55 -494 730 -1187 84.5 1086 1086 | -2752 0
brd 1934 1 | -3 26 12 -336 -879 772 84.9 992 992 | -4064 0
brd 1934 2 | 24 64 -21 -904 -1488 337 84.0 991 991 | -2368 0
brd 1934 3 | -24 -1 51 621 -1358 -198 84.4 1062 1062 | -6578 0
brd 1934 4 | 45 -3 115 696 -477 1254 84.1 995 995 | -5969 0
brd 1934 5 | -42 27 81 -153 -343 143 83.8 993 993 | -6740 0
brd 1934 6 | -23 -51 82 -677 -1229 320 84.9 1170 1170 | -9538 0
-------------+------------------------------------------------------------+----------------
brd 1934 mean| 7 9 53 -178 -720 206 84.4 1041 1041 | -5429 0
brd 1934 sdev| 43 35 46 620 773 770 .4 68 68 | 2536 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 2.1934.0 GPS week: 1934 Day: 0 MJD: 57782
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 33 20 -35 .03 28 30 | -13683 532 3028 11053
cof n/a| 0 1 -5 53 0 -70 .05 33 33 | -13681 519 3022 11052
emx n/a| 0 0 0 13 -28 -79 .10 23 22 | -7327 811 3023 10184
esx n/a| -2 0 0 0 2 33 .12 18 15 | -3264 3216 3017 12925
gfz n/a| 1 0 3 17 85 26 -.06 31 29 | 0 1315 3013 10466
grg n/a| 2 0 0 -84 -37 115 -.36 31 27 | -3225 1014 3051 10180
Table 2.1934.1 GPS week: 1934 Day: 1 MJD: 57783
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 -5 -11 3 -35 .08 31 32 | -14574 -731 2923 11417
cof n/a| 0 0 -7 -9 30 -9 .07 34 34 | -14589 -713 2925 11424
emx n/a| 0 0 -8 63 -65 -38 .16 20 20 | -9277 29 2932 10472
esx n/a| 0 0 -1 -13 8 23 .15 23 19 | 4145 -1560 2913 13485
gfz n/a| 0 1 6 -6 64 53 -.19 29 23 | 0 -595 2911 10865
grg n/a| 0 0 15 -73 63 8 -.37 27 24 | -4746 1629 2945 11241
Table 2.1934.2 GPS week: 1934 Day: 2 MJD: 57784
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 -3 11 0 15 .15 32 28 | -15339 2723 3041 11225
cof n/a| 0 0 -5 -2 -36 -32 .18 36 32 | -15349 2729 3043 11230
emx n/a| 0 -1 -5 62 -34 -33 .07 25 25 | 4412 1576 3025 10310
esx n/a| 1 0 0 10 -7 8 .17 17 15 | -14043 4677 3034 13275
gfz n/a| 2 -2 3 -17 -14 26 -.17 29 25 | 0 3348 3032 10673
grg n/a| -1 0 6 -64 34 -9 -.37 31 26 | -3730 2760 3042 10882
Table 2.1934.3 GPS week: 1934 Day: 3 MJD: 57785
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 2 -5 13 -40 -29 .17 33 32 | -17191 -1022 2762 11934
cof n/a| -1 2 -3 18 -18 -16 .19 35 34 | -17194 -1031 2752 11935
emx n/a| 0 -2 -6 9 -31 -96 .08 29 29 | -7091 261 2733 11207
esx n/a| 0 -1 0 13 5 41 .17 15 15 | -22959 1382 2733 14830
gfz n/a| 0 0 11 -3 27 67 -.09 26 29 | 0 -631 2746 11510
grg n/a| -1 0 0 -53 22 -64 -.34 24 23 | -6385 -371 2742 11481
Table 2.1934.4 GPS week: 1934 Day: 4 MJD: 57786
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 -3 24 -14 23 .08 32 36 | -15798 1045 3449 11451
cof n/a| 0 3 -2 13 -8 12 .00 33 36 | -15821 1068 3456 11453
emx n/a| 1 1 -3 10 -71 -47 .13 19 19 | -25597 1632 3436 10789
esx n/a| 0 -1 1 -10 14 22 .12 19 18 | -21383 726 3451 13777
gfz n/a| 0 0 10 25 91 8 -.10 28 26 | 0 1872 3449 10933
grg n/a| 1 -3 2 -45 18 -52 -.35 26 25 | -6684 1284 3505 10897
Table 2.1934.5 GPS week: 1934 Day: 5 MJD: 57787
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -8 22 12 -14 .11 30 30 | -15206 1031 2860 10194
cof n/a| -2 0 -11 26 23 -33 .10 35 33 | -15207 1019 2857 10196
emx n/a| 0 0 -4 63 -11 -6 .12 25 25 | -5067 349 2847 9358
esx n/a| 1 0 1 -40 -1 10 .13 18 17 | 1416 2801 2856 12122
gfz n/a| -3 2 5 -7 52 74 -.07 32 34 | 0 584 2855 9539
grg n/a| 0 1 11 -22 -3 -98 -.43 30 31 | -6930 875 2833 9397
Table 2.1934.6 GPS week: 1934 Day: 6 MJD: 57788
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 -4 -6 36 30 32 .09 33 34 | -15209 -4751 3167 12273
cof n/a| -2 -1 -9 -18 -15 -43 .20 35 38 | -15236 -4693 3165 12269
emx n/a| 0 0 -1 39 -80 -59 .14 26 26 | -13960 -4014 3190 11004
esx n/a| 1 0 0 -4 36 41 .07 16 16 | -23073 -4375 3184 14101
gfz n/a| 0 1 1 -3 40 113 .01 28 26 | 0 -3767 3184 11699
grg n/a| 0 -2 12 -40 1 -141 -.56 39 34 | -7111 -4520 3166 12070
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 3.1934.0 GPS week: 1934 Day: 0 MJD: 57782
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 503 38 40 18 18 19 19 11 | 2 5 2 7 7 3 3
R02 | 650 20 20 14 17 13 24 9 | 2 3 2 6 6 4 3
R03 | 697 21 25 13 11 25 20 8 | 2 2 2 2 3 3 2
R04 | 828 21 23 13 9 26 15 8 | 2 2 2 3 5 3 2
R05 | 790 29 32 33 31 39 32 16 | 2 3 5 5 5 4 3
R06 | 1830 34 32 16 15 20 36 12 | 2 2 3 4 5 3 2
R07 | 638 20 24 31 13 36 15 11 | 2 3 2 3 6 3 2
R08 | 1290 15 11 21 12 19 38 10 | 2 6 4 2 3 4 2
XR09E | 2602 17 14 14 7 13 --- 7 | 2 3 2 3 3 --- 2
R10E | 1010 17 19 24 15 21 22 10 | 4 7 4 8 6 5 4
R11E | 673 12 12 17 12 17 26 8 | 2 3 2 4 4 4 3
R13E | 1043 16 23 38 12 23 22 12 | 3 5 4 5 4 4 3
R14E | 1555 28 42 30 19 52 46 17 | 5 16 5 16 26 5 9
R15E | 2077 17 16 22 21 13 25 10 | 3 5 4 7 7 4 4
R16E | 1241 20 24 33 26 23 37 14 | 3 8 3 6 10 6 4
R17 | 463 29 34 15 13 26 23 10 | 3 4 3 5 3 2 3
R18 | 486 26 33 14 8 20 18 8 | 2 3 2 2 3 2 2
R19 | 1759 53 53 25 17 55 24 17 | 2 4 4 4 3 2 2
R20 | 1015 44 44 27 15 21 30 13 | 2 4 2 4 7 3 3
R21 | 649 37 37 16 10 36 34 13 | 2 3 2 3 7 3 3
R22 | 931 38 41 17 9 33 19 11 | 2 2 2 2 4 1 2
R23 | 626 18 26 15 28 22 33 12 | 2 4 2 6 5 5 3
R24 | 964 22 56 25 30 56 70 20 | 4 14 4 5 28 3 3
------+-----------------------------------------+-------------------------------------
RMS | 1085 28 33 23 18 31 31 |T 2 4 2 4 6 3 3
WRMS | 1085 30 33 22 15 29 27 |NE 2 4 2 3 6 3 2
MEDI | 931 21 26 18 15 23 24 |MD 2 4 2 4 5 3 3
Table 3.1934.1 GPS week: 1934 Day: 1 MJD: 57783
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 427 36 33 20 18 18 22 11 | 2 11 3 11 8 5 4
R02 | 665 19 20 14 15 17 23 8 | 1 7 4 7 7 5 4
R03 | 604 14 16 13 8 18 13 6 | 1 3 3 3 3 3 2
R04 | 690 22 26 18 12 22 11 8 | 2 4 2 4 4 3 2
R05 | 1050 37 47 13 31 32 30 14 | 2 6 5 10 7 3 4
R06 | 1955 17 19 18 29 27 33 13 | 1 3 2 5 6 2 3
R07 | 722 20 24 24 15 25 17 10 | 1 4 2 4 5 4 2
R08 | 832 16 23 23 16 22 22 10 | 2 6 4 3 4 3 2
XR09E | 2499 13 17 13 10 19 --- 7 | 1 4 3 4 4 --- 2
R10E | 946 17 19 21 20 30 19 10 | 3 7 4 9 7 5 4
R11E | 854 12 14 14 11 17 20 7 | 2 4 3 5 4 5 3
R13E | 611 19 14 25 18 17 15 9 | 2 4 5 5 5 4 3
R14E | 1121 52 33 35 50 43 27 21 | 6 15 12 21 25 8 13
R15E | 662 19 22 18 22 11 22 9 | 4 5 5 8 7 4 5
R16E | 541 23 42 22 18 22 38 12 | 3 9 3 6 9 5 4
R17 | 472 38 35 16 16 37 22 12 | 2 5 3 8 6 6 4
R18 | 766 32 35 15 8 25 16 9 | 2 4 2 2 4 2 2
R19 | 1562 56 66 14 26 47 26 16 | 1 4 4 5 4 4 2
R20 | 1084 58 58 28 20 39 44 18 | 2 6 3 4 6 5 3
R21 | 1003 34 35 14 15 41 27 13 | 2 5 2 3 6 4 2
R22 | 1751 36 36 19 20 24 14 11 | 1 2 2 6 7 4 4
R23 | 747 22 15 20 15 26 18 10 | 2 4 2 6 5 4 3
R24 | 1012 28 41 25 44 46 57 20 | 4 11 4 6 27 4 3
------+-----------------------------------------+-------------------------------------
RMS | 992 31 34 20 23 29 27 |T 2 5 3 6 7 4 3
WRMS | 992 32 34 20 19 23 24 |NE 1 5 2 5 6 3 2
MEDI | 832 22 26 18 18 25 22 |MD 2 5 3 5 6 4 3
Table 3.1934.2 GPS week: 1934 Day: 2 MJD: 57784
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 505 43 61 30 21 27 32 15 | 2 9 3 12 8 5 6
R02 | 849 19 24 20 8 14 29 9 | 1 6 3 6 6 7 4
R03 | 594 21 17 28 18 24 22 11 | 1 4 3 3 3 5 2
R04 | 1653 23 23 19 14 20 25 10 | 1 4 2 10 6 5 5
R05 | 1003 41 29 22 26 30 29 14 | 1 6 5 13 8 5 7
R06 | 1151 19 21 25 16 32 19 11 | 1 4 2 4 5 3 2
R07 | 512 28 33 30 17 23 23 12 | 1 3 3 5 7 3 3
R08 | 782 16 17 24 9 25 31 10 | 2 5 5 3 4 4 2
XR09E | 2776 18 15 13 7 21 --- 8 | 1 4 2 4 4 --- 2
R10E | 765 12 18 27 19 14 15 9 | 3 7 3 7 6 4 3
R11E | 615 16 16 12 11 23 15 7 | 2 3 3 4 6 5 3
R13E | 853 19 21 16 16 21 28 9 | 2 4 4 5 5 6 3
R14E | 710 35 31 21 22 31 47 15 | 4 10 11 14 13 9 9
R15E | 657 13 26 18 16 20 20 9 | 2 6 6 7 5 5 4
R16E | 552 24 33 39 17 24 28 13 | 3 15 4 9 11 6 5
R17 | 594 26 33 19 14 39 24 12 | 2 4 2 8 5 5 4
R18 | 906 32 34 17 14 34 29 12 | 2 4 3 4 4 5 3
R19 | 1288 68 65 28 22 38 41 19 | 1 4 4 4 5 6 2
R20 | 1609 61 86 41 15 35 34 18 | 2 8 4 3 3 4 2
R21 | 1592 30 38 20 11 36 23 11 | 2 5 2 5 5 4 3
R22 | 1352 37 36 27 15 45 27 14 | 2 4 3 6 6 4 3
R23 | 975 17 20 24 20 20 32 11 | 2 3 2 8 6 4 3
R24 | 815 28 28 28 19 45 66 19 | 3 8 2 6 26 5 4
------+-----------------------------------------+-------------------------------------
RMS | 991 32 36 25 17 29 31 |T 1 5 3 6 6 4 3
WRMS | 991 28 32 25 15 25 26 |NE 1 5 3 6 6 4 3
MEDI | 849 24 28 24 16 25 28 |MD 2 4 3 6 6 5 3
Table 3.1934.3 GPS week: 1934 Day: 3 MJD: 57785
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 579 53 68 36 13 17 8 13 | 2 6 2 9 6 7 5
R02 | 932 22 27 27 8 24 12 9 | 1 5 2 4 5 7 3
R03 | 1158 29 32 34 11 17 27 11 | 1 3 3 3 3 5 3
R04 | 1788 23 21 16 16 19 21 9 | 2 4 2 8 5 6 4
R05 | 744 49 51 23 20 29 28 14 | 1 5 4 12 8 5 6
R06 | 1267 22 27 18 12 32 23 10 | 1 4 3 4 7 3 2
R07 | 481 23 30 22 16 27 24 11 | 1 3 3 6 7 2 3
R08 | 998 19 18 26 12 28 17 10 | 1 5 4 5 6 4 2
XR09E | 2551 17 27 20 8 19 --- 9 | 1 6 2 4 4 --- 3
R10E | 769 14 17 20 15 13 13 7 | 3 5 2 4 5 4 3
R11E | 493 13 14 16 11 18 9 6 | 2 4 2 5 6 5 3
R13E | 607 25 30 23 8 18 20 9 | 2 3 3 6 7 5 4
R14E | 1081 28 33 21 21 27 32 12 | 3 7 4 7 11 7 5
R15E | 1659 18 23 30 22 17 27 11 | 3 8 6 6 5 5 4
R16E | 568 31 30 39 28 31 42 17 | 5 14 5 9 12 7 6
R17 | 582 38 38 29 10 22 25 12 | 1 3 3 5 3 4 3
R18 | 613 25 25 14 19 28 26 11 | 1 5 4 6 5 5 4
R19 | 889 55 53 28 9 40 26 15 | 2 5 6 7 4 5 3
R20 | 1364 48 52 64 13 27 34 18 | 1 6 6 3 5 3 2
R21 | 1403 42 37 20 12 33 14 11 | 1 3 2 6 7 3 3
R22 | 1544 39 39 24 9 43 26 13 | 1 3 3 4 4 2 2
R23 | 1175 25 22 32 21 14 17 11 | 2 4 2 8 6 2 4
XR24 | 1123 23 33 87 26 --- 78 33 | 2 9 5 7 --- 4 4
------+-----------------------------------------+-------------------------------------
RMS | 1062 33 35 29 15 26 24 |T 1 5 3 6 5 4 3
WRMS | 1062 32 34 29 15 29 23 |NE 1 4 3 6 5 4 3
MEDI | 998 25 30 24 13 24 24 |MD 1 5 3 6 5 5 3
Table 3.1934.4 GPS week: 1934 Day: 4 MJD: 57786
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 481 63 59 10 16 22 27 14 | 2 4 2 5 4 6 3
R02 | 697 17 25 13 12 18 24 8 | 2 4 2 4 3 4 2
R03 | 1185 23 26 21 12 24 27 10 | 1 3 4 4 5 4 3
R04 | 1386 24 26 21 8 18 28 10 | 2 4 2 4 4 4 2
R05 | 798 53 54 15 28 22 33 15 | 2 6 4 7 6 7 4
R06 | 1174 25 20 16 19 18 20 9 | 1 3 3 3 6 3 2
R07 | 479 33 28 24 14 24 23 11 | 1 3 2 4 6 3 2
R08 | 594 25 23 19 10 26 33 11 | 2 4 2 6 8 3 3
XR09E | 3596 19 13 15 11 15 --- 8 | 2 4 3 4 4 --- 2
R10E | 927 21 23 11 17 11 23 8 | 3 4 3 7 7 5 4
R11E | 631 16 11 13 11 12 22 7 | 2 3 2 4 4 4 3
R13E | 818 27 20 15 12 32 20 10 | 3 5 4 5 10 5 4
R14E | 656 22 25 27 24 30 33 13 | 4 8 3 6 12 7 4
R15E | 1812 15 27 17 22 16 25 10 | 3 6 4 6 5 4 3
R16E | 1482 21 24 31 28 26 29 14 | 3 5 6 6 9 6 4
R17 | 639 40 38 21 13 35 20 12 | 2 3 3 6 6 4 4
R18 | 484 28 32 14 13 20 16 8 | 2 5 3 5 4 3 3
R19 | 840 44 39 21 25 42 39 16 | 2 5 5 7 3 5 4
R20 | 783 35 23 24 18 45 32 15 | 3 10 6 4 5 3 3
R21 | 817 38 41 16 19 34 24 12 | 2 2 2 4 6 3 2
R22 | 549 47 52 14 29 35 26 14 | 2 3 3 3 4 3 2
R23 | 1912 21 26 24 27 16 11 11 | 2 6 3 6 5 2 3
R24 | 847 22 25 22 17 45 28 13 | 3 8 5 8 9999 3 4
------+-----------------------------------------+-------------------------------------
RMS | 995 32 33 19 19 28 26 |T 2 4 3 5 5 4 3
WRMS | 995 36 36 19 18 26 25 |NE 1 4 3 5 5 3 2
MEDI | 817 25 26 17 17 24 25 |MD 2 4 3 5 5 4 3
Table 3.1934.5 GPS week: 1934 Day: 5 MJD: 57787
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 556 42 54 10 10 37 20 12 | 2 7 2 5 4 4 2
R02 | 629 20 20 22 17 17 31 11 | 2 2 2 4 3 4 2
R03 | 1179 23 28 27 18 19 15 10 | 2 3 3 5 5 3 3
R04 | 1497 31 37 23 11 32 15 11 | 2 6 3 4 6 3 2
R05 | 771 41 45 12 30 36 49 17 | 2 7 4 9 15 8 6
R06 | 1152 17 19 14 16 12 24 8 | 1 3 2 2 3 5 2
R07 | 999 31 32 25 18 24 19 11 | 2 4 4 8 6 5 5
R08 | 762 12 20 13 12 16 27 8 | 2 5 5 4 8 4 3
XR09E | 3505 13 15 12 7 14 --- 6 | 2 4 2 3 4 --- 2
R10E | 860 27 20 18 15 18 24 10 | 4 4 5 6 6 6 4
R11E | 682 15 10 16 14 13 13 7 | 4 2 3 4 5 4 3
R13E | 627 28 33 19 22 30 27 12 | 3 7 5 8 8 6 5
R14E | 778 36 32 32 26 43 25 16 | 4 10 7 6 11 5 5
R15E | 1279 28 35 23 20 26 18 11 | 6 7 5 5 6 6 3
R16E | 779 19 28 30 22 25 30 13 | 4 6 5 8 9 6 4
R17 | 475 35 39 24 16 35 22 12 | 2 3 3 7 6 4 4
R18 | 526 24 30 14 9 24 24 9 | 2 4 3 5 7 2 3
R19 | 2169 48 56 23 18 42 28 15 | 2 5 3 4 4 6 3
R20 | 890 36 53 19 23 47 33 15 | 3 8 6 7 4 4 4
R21 | 620 38 33 15 10 44 19 12 | 2 3 2 3 4 4 2
R22 | 819 44 41 16 15 43 13 13 | 2 3 3 3 4 3 2
R23 | 1345 17 18 28 19 18 13 10 | 2 5 2 3 3 3 2
R24 | 745 16 32 63 24 57 84 27 | 3 7 4 5 9999 3 3
------+-----------------------------------------+-------------------------------------
RMS | 993 30 35 25 18 32 30 |T 2 5 3 5 5 4 3
WRMS | 993 30 33 25 17 34 31 |NE 2 4 3 4 5 4 3
MEDI | 779 28 32 19 17 26 24 |MD 2 5 3 5 5 4 3
Table 3.1934.6 GPS week: 1934 Day: 6 MJD: 57788
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 604 36 27 25 10 22 16 10 | 2 6 2 3 2 3 2
R02 | 851 19 22 19 14 27 29 10 | 1 2 2 2 3 3 2
R03 | 1672 39 41 29 15 34 19 13 | 2 3 3 4 4 3 3
R04 | 732 23 27 12 9 16 16 7 | 2 5 2 2 4 4 2
R05 | 951 23 34 18 24 44 74 18 | 2 5 3 7 11 5 4
R06 | 2010 26 25 11 12 14 33 9 | 1 2 2 2 2 4 2
R07 | 505 37 42 31 15 24 29 13 | 1 3 3 7 4 4 4
R08 | 599 20 17 17 14 20 41 10 | 1 2 4 2 6 3 2
XR09E | 2739 18 18 15 10 18 --- 8 | 2 3 2 3 4 --- 2
R10E | 838 34 33 27 17 17 31 12 | 3 6 4 4 3 7 3
R11E | 914 38 26 28 16 28 25 13 | 3 4 3 3 4 4 3
R13 | 1428 32 24 17 16 18 35 11 | 3 5 4 6 3 3 3
R14E | 1106 29 37 37 26 22 49 16 | 6 11 5 5 7 7 4
R15 | 1718 38 34 20 15 25 23 11 | 4 7 4 3 4 6 3
R16 | 760 26 18 34 25 24 25 13 | 6 6 3 6 6 3 3
R17 | 449 36 37 18 10 38 24 12 | 2 2 2 4 4 4 3
R18 | 655 24 18 14 7 30 31 10 | 2 3 2 4 5 3 3
R19 | 2480 52 60 27 21 34 27 15 | 2 4 3 3 4 4 2
R20 | 1076 53 68 37 19 29 76 20 | 2 4 4 6 3 4 3
R21 | 640 32 39 12 12 40 22 11 | 2 3 2 2 2 3 2
R22 | 986 43 43 13 7 39 19 12 | 2 2 2 2 3 3 2
R23 | 1119 14 18 17 13 17 23 8 | 2 3 2 3 2 3 2
R24 | 1093 31 37 54 15 29 88 22 | 3 5 3 2 9999 2 2
------+-----------------------------------------+-------------------------------------
RMS | 1169 33 35 26 16 28 39 |T 2 4 2 3 4 3 2
WRMS | 1169 34 38 26 16 26 34 |NE 1 3 2 3 3 3 2
MEDI | 951 32 33 19 15 25 27 |MD 2 4 3 3 4 3 3
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