[IGSREPORT-25191] Wk 1941 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 7 21:14:42 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1941 (Mar 19, 2017 - Mar 25, 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 2.1941.
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:
igl1941[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1941 in the SP3 format.
igl19417.sum Combination Report for GPS Week 1941.
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 | -11.7 ns
1 | -12.4 ns
2 | -10.5 ns
3 | -11.9 ns
4 | -11.7 ns
5 | -9.9 ns
6 | -11.2 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 1.1941, 1a.1941).
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 2.1941.0-6)
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 3.1941.0-6).
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 1941 summary. (Mar 19, 2017 - Mar 25, 2017)
Table 1.1941.a GPS week : 1941 MJD: 57831.0-57837.0
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 2 -17 -20 30 .09 24 26 | -9991 601 3377 11516
| 0 0 2 14 17 49 .02 | 1191 1617
cof n/a| -1 0 3 -12 0 24 .12 26 28 | -9989 593 3376 11517
| 1 1 2 19 32 47 .02 | 1191 1605
emx n/a| 0 1 5 -34 -40 -72 .04 24 24 | -16836 1070 3371 10773
| 0 0 2 29 25 52 .04 | 9670 1333
esx n/a| 0 0 -2 20 27 -1 .15 16 15 | -10110 22 3378 13385
| 1 0 0 16 11 31 .03 | 3858 2301
gfz n/a| 0 0 -1 4 30 -20 -.00 23 21 | 0 759 3364 10884
| 1 1 2 23 24 19 .04 | 0 1526
grg n/a| -1 0 8 -103 32 64 -.45 32 31 | -11629 542 3402 11289
| 1 2 4 40 28 64 .07 | 788 1656
iac n/a| 1 0 -8 63 -27 -6 .01 20 20 | -11323 613 3375 10698
| 0 0 1 38 52 72 .02 | 1388 972
mcc n/a| 4 0 -15 152 -42 560 -.32 139 139 | --- --- --- ---
| 7 7 7 78 132 560 .17 | --- ---
Table 1.1941.b GPS week : 1941 MJD: 57831.0-57837.0
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 11 11 10 14 10 11 |
R02 | 8 8 7 7 7 6 7 |
R03 | 8 7 8 7 8 8 8 |
R04 | 7 8 7 7 7 7 7 |
R05 | 13 12 12 12 13 14 11 |
R07 | 9 8 8 8 8 8 6 |
R08 | 8 9 8 9 8 8 8 |
R09 | 8 9 19 8 8 9 7 |
R10 | 8 9 10 9 7 7 6 |
R11 | 10 8 9 10 9 7 8 |
R13 | 9 9 9 9 10 11 9 |
R14 | 13 13 11 12 11 13 13 |
R15 | 11 9 10 11 12 11 11 |
R16 | 12 15 14 14 11 10 14 |
R17 | 9 8 8 11 9 8 8 |
R18 | 7 11 9 8 8 8 5 |
R19 | 10 13 15 14 14 13 11 |
R20 | 16 15 12 15 14 14 14 |
R21 | 8 7 9 9 10 9 8 |
R22 | 8 7 8 8 9 12 11 |
R23 | 7 6 8 9 8 7 8 |
R24 | 14 19 11 11 14 18 12 |
R26 | 0 0 0 0 0 0 26 |
Table 1.1941.c GPS week : 1941 MJD: 57831.0-57837.0
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 1941 0 | 23 -1 100 -730 8 1379 85.1 1570 1570 | -11718 0
brd 1941 1 | 30 13 140 -1488 -1137 1103 86.6 1219 1219 | -12410 0
brd 1941 2 | -43 44 105 -802 127 2927 86.4 1022 1022 | -10549 0
brd 1941 3 | -34 25 41 -189 -304 3705 85.5 1040 1040 | -11875 0
brd 1941 4 | -7 -11 127 366 586 2665 85.8 1337 1337 | -11663 0
brd 1941 5 | -12 17 59 -616 1455 3480 86.5 1421 1421 | -9920 0
brd 1941 6 | -35 -21 -15 249 1295 2645 84.9 1446 1446 | -11175 0
-------------+------------------------------------------------------------+----------------
brd 1941 mean| -11 9 80 -458 290 2557 85.8 1293 1293 | -11330 0
brd 1941 sdev| 29 22 54 649 908 985 .7 208 208 | 851 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 2.1941.0 GPS week: 1941 Day: 0 MJD: 57831
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 0 -35 -19 65 .11 24 25 | -10436 2009 3708 11103
cof n/a| -2 0 3 -27 -15 14 .11 25 24 | -10434 2006 3699 11099
emx n/a| 0 0 7 -26 -83 -39 .12 21 21 | -25062 1786 3700 10513
esx n/a| 3 0 -1 -5 36 -28 .10 19 18 | -10910 1350 3699 12799
gfz n/a| 0 1 3 5 52 -44 .04 26 21 | 0 1657 3675 10408
grg n/a| -3 0 7 -57 19 -12 -.41 33 33 | -12954 2326 3741 10854
iac n/a| 0 0 -12 93 3 33 -.02 17 17 | -11313 788 3704 10174
mcc n/a| 8 -11 -12 169 -163 1353 -.35 165 165 | --- --- --- ---
Table 2.1941.1 GPS week: 1941 Day: 1 MJD: 57832
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 0 -19 -52 87 .12 25 27 | -10831 -875 3472 12350
cof n/a| -1 1 3 2 24 93 .13 27 29 | -10836 -884 3471 12348
emx n/a| 1 1 6 4 -42 -85 -.00 26 26 | -19323 -213 3470 11239
esx n/a| -1 0 -1 18 46 43 .15 19 17 | -13199 -1895 3489 14013
gfz n/a| 1 0 -1 -26 62 -15 .01 23 23 | 0 -425 3468 11607
grg n/a| 0 -5 14 -80 58 25 -.48 34 35 | -11902 -1064 3512 12234
iac n/a| 2 0 -8 32 -53 -85 .02 18 18 | -13028 -208 3472 11522
mcc n/a| 0 -8 -6 100 -270 2 -.40 166 166 | --- --- --- ---
Table 2.1941.2 GPS week: 1941 Day: 2 MJD: 57833
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 -3 0 5 -33 26 .07 25 27 | -8790 2681 3498 10920
cof n/a| 0 -1 0 -23 -34 81 .11 28 29 | -8775 2644 3494 10921
emx n/a| 0 2 4 -6 -56 -46 .02 23 23 | -30590 2447 3499 10153
esx n/a| 1 0 -2 29 17 29 .15 16 16 | -12554 1608 3509 12469
gfz n/a| 1 0 0 -8 34 -11 -.03 22 21 | 0 2504 3496 10149
grg n/a| -2 0 9 -89 -12 37 -.44 28 25 | -11921 2610 3508 10455
iac n/a| 1 0 -9 53 27 -75 .01 19 19 | -10453 1729 3487 10030
mcc n/a| 16 0 -18 70 83 -169 -.27 155 155 | --- --- --- ---
Table 2.1941.3 GPS week: 1941 Day: 3 MJD: 57834
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 4 -28 0 48 .07 24 27 | -8329 -1846 3614 11132
cof n/a| -1 0 0 -43 0 -23 .13 28 31 | -8329 -1835 3627 11134
emx n/a| 0 0 0 -45 1 -144 .08 24 24 | -8092 -1122 3608 10127
esx n/a| 0 1 -1 4 14 -37 .17 17 16 | -1651 -4268 3605 13081
gfz n/a| 1 -2 -1 -11 13 -26 -.04 22 20 | 0 -1920 3598 10541
grg n/a| -1 3 7 -112 71 117 -.43 31 32 | -11224 -1760 3644 10956
iac n/a| 1 1 -9 130 -64 99 .05 21 21 | -11018 -789 3601 10272
mcc n/a| 5 1 -23 297 -54 718 -.52 133 133 | --- --- --- ---
Table 2.1941.4 GPS week: 1941 Day: 4 MJD: 57835
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 -15 -21 -64 .08 23 25 | -11824 768 3029 11981
cof n/a| -3 0 5 13 60 -28 .15 24 26 | -11813 751 3029 11980
emx n/a| 0 1 6 -81 -32 -89 .02 25 25 | -3298 2360 3039 11520
esx n/a| 0 1 -1 28 22 10 .17 14 13 | -10959 1508 3033 13946
gfz n/a| 0 -2 -2 30 46 -45 .06 23 22 | 0 1937 3023 11493
grg n/a| -1 0 0 -75 44 70 -.51 30 28 | -11852 619 3032 11864
iac n/a| 1 0 -9 48 -115 48 .02 25 25 | -13035 1907 3039 11254
mcc n/a| 4 10 -23 160 -8 931 -.48 129 129 | --- --- --- ---
Table 2.1941.5 GPS week: 1941 Day: 5 MJD: 57836
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 2 -2 -6 7 .08 24 25 | -9774 1498 3266 11554
cof n/a| -1 -2 5 -5 -15 30 .14 24 27 | -9774 1486 3264 11555
emx n/a| 0 1 6 -25 -29 13 .01 24 24 | -19986 1383 3244 10965
esx n/a| 0 0 -2 44 33 2 .12 16 14 | -10577 1814 3265 13570
gfz n/a| 0 0 -1 40 10 -2 -.04 22 21 | 0 1058 3252 10936
grg n/a| 1 0 9 -175 13 35 -.51 39 37 | -10511 1283 3291 11207
iac n/a| 1 1 -6 15 19 -74 .01 19 19 | -9116 527 3267 10810
mcc n/a| 2 5 -18 187 39 191 -.05 96 96 | --- --- --- ---
Table 2.1941.6 GPS week: 1941 Day: 6 MJD: 57837
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 4 -26 -9 44 .12 23 25 | -9959 -23 3053 11578
cof n/a| 0 0 4 -1 -20 5 .11 27 28 | -9964 -15 3052 11585
emx n/a| 0 0 4 -58 -43 -113 .07 26 26 | -11503 851 3039 10896
esx n/a| 0 0 -3 26 22 -33 .17 14 13 | -10921 41 3049 13818
gfz n/a| -1 -1 -4 -1 -4 1 .00 22 19 | 0 502 3039 11057
grg n/a| -2 1 8 -132 30 180 -.33 30 27 | -11039 -215 3087 11454
iac n/a| 2 1 -7 73 -7 7 -.00 18 18 | -11301 337 3055 10827
mcc n/a| -7 5 -3 81 79 895 -.16 126 126 | --- --- --- ---
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 3.1941.0 GPS week: 1941 Day: 0 MJD: 57831
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 | 810 29 37 24 22 41 34 22 --- 12 | 7 9 7 13 13 22 5 --- 6
R02E | 588 11 13 22 12 17 30 8 78 7 | 7 8 7 8 9 14 4 13 3
R03E | 1664 17 16 24 11 17 25 9 142 7 | 7 7 7 9 9 9 4 10 4
R04E | 680 18 13 18 7 26 13 12 --- 7 | 7 7 7 8 9 13 4 --- 4
R05E | 732 22 26 25 24 36 42 22 --- 12 | 8 16 7 10 22 21 5 --- 5
R07E | 803 21 26 21 14 25 24 12 120 8 | 7 8 9 8 9 7 4 21 3
R08E | 3173 21 22 18 18 21 17 9 --- 7 | 7 7 8 9 9 10 5 --- 4
XR09 | 1416 18 17 17 16 19 --- 12 --- 8 | 7 7 7 7 7 --- 2 --- 1
R10 | 1382 28 23 15 11 21 22 13 --- 8 | 7 10 8 8 7 14 2 --- 2
R11 | 1168 24 23 20 15 34 30 17 305 10 | 7 7 7 7 7 9 1 12 1
R13 | 2054 31 32 14 16 21 16 19 --- 9 | 7 7 7 7 7 16 2 --- 2
R14 | 2441 36 29 27 34 16 32 26 --- 13 | 7 9 7 9 9 15 2 --- 3
R15 | 1747 28 22 15 14 26 38 22 --- 10 | 7 7 7 9 9 7 2 --- 2
R16 | 680 24 34 28 21 32 39 22 --- 12 | 7 8 8 8 8 7 4 --- 2
R17 | 1462 19 20 18 9 29 20 18 --- 8 | 7 7 7 8 7 12 2 --- 2
R18 | 1200 14 16 13 15 17 12 17 --- 6 | 7 7 7 8 8 20 2 --- 2
R19 | 1933 39 40 18 20 29 15 11 --- 10 | 7 7 7 7 8 11 2 --- 2
R20 | 867 20 38 33 33 22 82 18 --- 16 | 8 9 7 8 8 9 3 --- 2
R21 | 675 20 19 20 17 24 14 13 49 8 | 7 8 7 7 7 16 2 3 1
R22 | 659 23 18 16 13 14 17 16 --- 7 | 7 7 7 8 8 18 1 --- 2
R23 | 632 11 16 16 19 11 13 16 --- 7 | 7 7 7 8 8 10 2 --- 2
R24 | 3152 20 21 27 26 36 59 19 --- 13 | 7 10 8 9 7 9 3 --- 2
XR26 | ---- --- --- --- --- --- --- 9 --- 0 | --- --- --- --- --- --- 2 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS | 1570 24 25 21 19 26 33 17 165 |T 7 8 7 8 8 12 2 11 2
WRMS | 1570 25 24 21 18 21 33 17 165 |NE 7 7 7 7 7 12 2 7 1
MEDI | 1168 21 22 18 16 22 24 16 120 |MD 7 7 7 8 8 12 2 12 2
Table 3.1941.1 GPS week: 1941 Day: 1 MJD: 57832
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 | 1334 33 33 26 15 34 17 16 --- 10 | 9 10 11 14 15 19 6 --- 6
R02E | 1114 11 14 23 14 25 18 18 164 8 | 10 12 10 12 12 13 4 22 4
R03E | 1223 14 13 21 12 20 17 14 183 7 | 10 10 10 11 12 8 5 12 4
R04E | 691 14 15 21 10 18 26 13 --- 7 | 10 9 10 11 11 11 5 --- 4
R05E | 688 30 26 22 17 37 28 24 --- 11 | 10 15 10 12 20 20 5 --- 5
R07E | 516 19 12 24 12 21 20 11 170 8 | 9 10 11 11 11 7 4 34 3
R08E | 1840 18 11 17 12 21 35 18 --- 9 | 10 10 11 11 12 9 5 --- 4
XR09 | 1266 19 23 21 13 18 --- 16 --- 8 | 9 10 10 10 10 --- 4 --- 3
R10 | 1827 35 34 11 13 22 13 16 --- 8 | 10 12 10 11 10 12 3 --- 3
R11 | 604 29 33 17 10 17 19 16 205 8 | 10 10 10 11 10 7 1 19 2
R13 | 1253 30 31 17 9 20 19 20 --- 8 | 10 10 10 11 10 14 2 --- 3
R14 | 2008 42 50 26 20 23 28 27 --- 12 | 9 10 10 11 12 12 2 --- 3
R15 | 911 23 28 19 21 22 24 15 --- 9 | 9 10 10 11 11 6 2 --- 2
R16 | 758 23 31 23 35 20 68 23 --- 15 | 9 11 10 11 12 6 2 --- 3
R17 | 520 19 18 23 9 20 16 19 --- 8 | 9 10 10 11 12 10 1 --- 2
R18 | 776 31 25 29 11 29 29 18 --- 10 | 9 10 9 12 11 17 3 --- 3
R19 | 1638 37 33 24 27 29 31 24 --- 12 | 9 10 9 10 11 10 1 --- 2
R20 | 859 15 28 45 28 21 63 14 --- 14 | 10 15 10 15 11 8 4 --- 4
R21 | 590 11 16 16 15 23 18 10 83 7 | 10 11 10 10 11 13 3 6 2
R22 | 969 20 23 18 7 22 20 12 --- 7 | 10 12 10 11 11 15 2 --- 2
R23 | 556 9 12 10 15 14 22 12 --- 6 | 9 10 9 11 10 8 2 --- 3
R24 | 2336 32 42 62 37 24 76 21 --- 19 | 10 13 11 11 11 8 3 --- 3
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1218 25 27 26 19 23 34 18 166 |T 9 10 10 11 11 11 3 18 3
WRMS | 1218 27 29 26 17 23 35 18 166 |NE 9 10 9 11 10 10 2 12 2
MEDI | 911 20 25 21 13 21 22 16 170 |MD 10 10 10 11 11 10 3 19 3
Table 3.1941.2 GPS week: 1941 Day: 2 MJD: 57833
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 | 869 30 24 29 12 30 26 12 --- 10 | 12 13 13 15 16 7 6 --- 6
R02E | 1104 13 13 19 9 17 15 13 117 6 | 12 13 12 13 13 5 4 5 3
R03E | 742 17 17 23 9 22 15 13 175 7 | 12 13 12 13 13 6 6 5 4
R04E | 557 14 17 23 9 16 15 8 --- 6 | 12 12 13 12 13 5 4 --- 3
R05E | 840 30 34 28 20 28 35 28 --- 12 | 12 14 12 14 17 10 5 --- 5
R07E | 536 21 22 19 16 25 12 12 115 8 | 12 13 12 13 12 6 4 4 3
R08E | 1331 20 22 19 11 17 13 24 --- 8 | 12 12 13 13 13 4 6 --- 4
XR09 | 921 32 38 22 42 26 --- 47 --- 18 | 12 12 12 15 13 --- 7 --- 4
R10 | 1773 30 28 25 14 24 14 22 --- 9 | 12 13 13 13 12 2 2 --- 2
R11 | 925 30 30 12 12 16 17 23 238 8 | 12 12 13 13 12 4 2 3 2
R13 | 939 23 24 21 8 29 20 14 --- 8 | 12 12 12 13 13 6 3 --- 4
R14 | 772 26 26 22 17 16 36 26 --- 10 | 12 16 12 12 13 3 3 --- 2
R15 | 1341 30 34 16 17 26 23 19 --- 9 | 12 12 12 13 13 5 2 --- 2
R16 | 669 22 39 34 28 13 60 13 --- 13 | 12 13 12 13 13 3 2 --- 3
R17 | 662 20 21 18 12 25 24 14 --- 8 | 12 12 12 14 14 4 2 --- 2
R18 | 466 24 33 29 8 16 16 24 --- 9 | 12 13 12 13 14 4 2 --- 2
R19 | 1298 47 48 34 25 40 32 16 --- 14 | 12 13 12 14 14 3 2 --- 3
R20 | 961 21 40 30 16 19 53 15 --- 12 | 12 15 12 16 14 3 3 --- 4
R21 | 480 22 22 17 16 13 15 30 77 9 | 12 13 12 12 13 2 3 1 2
R22 | 1549 23 25 16 12 16 19 15 --- 7 | 12 13 12 13 12 3 2 --- 2
R23 | 806 9 12 13 24 10 30 13 --- 8 | 12 12 12 12 12 2 2 --- 2
R24 | 1438 29 35 23 19 15 34 24 --- 10 | 12 14 13 13 14 3 4 --- 3
XR26 | ---- --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1022 25 28 23 16 22 28 19 155 |T 12 12 12 13 13 4 3 3 3
WRMS | 1022 27 29 23 16 21 25 19 155 |NE 12 13 12 13 13 3 2 2 2
MEDI | 869 23 25 22 14 17 20 15 117 |MD 12 13 12 13 13 4 3 4 3
Table 3.1941.3 GPS week: 1941 Day: 3 MJD: 57834
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 | 635 26 18 29 11 23 28 15 --- 9 | 13 15 14 17 16 5 7 --- 5
R02E | 1772 12 14 23 10 19 18 10 70 7 | 14 15 14 14 15 4 4 5 3
R03E | 1013 16 20 19 10 19 16 15 116 7 | 13 13 14 14 14 6 5 5 4
R04E | 694 16 18 19 12 17 19 12 --- 7 | 13 14 13 14 14 6 4 --- 4
R05E | 749 14 17 38 21 25 31 27 --- 12 | 14 18 14 17 18 5 5 --- 5
R07E | 669 23 24 19 13 18 16 11 91 7 | 13 15 14 14 15 5 4 5 4
R08E | 1173 21 20 19 14 18 34 20 --- 9 | 13 14 13 15 14 4 5 --- 4
XR09 | 1791 23 30 12 15 13 --- 16 --- 8 | 13 13 13 16 14 --- 8 --- 4
R10 | 929 20 35 21 17 22 18 25 --- 9 | 13 15 14 15 14 4 2 --- 3
R11 | 909 34 36 12 11 24 18 24 242 9 | 13 13 14 13 13 5 2 3 2
R13 | 1196 24 18 18 12 20 29 18 --- 9 | 13 14 13 14 14 7 2 --- 3
R14 | 738 25 36 27 19 13 41 32 --- 12 | 13 17 14 14 14 3 3 --- 2
R15 | 1821 37 35 30 21 22 19 11 --- 11 | 14 14 13 16 16 4 2 --- 4
R16 | 583 26 27 36 23 19 53 27 --- 13 | 13 14 14 14 14 5 3 --- 3
R17 | 1238 24 25 15 24 20 46 15 --- 11 | 13 13 13 15 14 3 2 --- 2
R18 | 551 19 18 16 11 17 31 14 --- 8 | 13 14 13 15 15 6 3 --- 3
R19 | 1228 42 54 33 18 29 23 34 --- 13 | 13 14 14 17 17 4 3 --- 4
R20 | 768 33 37 25 20 41 53 23 --- 14 | 14 16 15 16 18 4 4 --- 5
R21 | 518 24 26 21 13 19 9 27 55 9 | 13 13 13 14 14 3 3 1 2
R22 | 1562 21 22 12 15 17 22 12 --- 7 | 13 13 13 14 13 5 2 --- 2
R23 | 611 16 21 16 22 11 25 18 --- 8 | 14 14 13 14 13 2 2 --- 2
R24 | 962 12 38 25 21 21 41 25 --- 11 | 14 15 14 15 14 5 4 --- 4
XR26 | ---- --- --- --- --- --- --- 11 --- 0 | --- --- --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1040 24 28 24 17 22 31 21 133 |T 13 14 13 14 14 4 3 3 3
WRMS | 1040 27 31 24 16 20 32 21 133 |NE 13 14 13 14 14 4 3 2 3
MEDI | 909 23 24 19 15 19 25 18 91 |MD 13 14 14 14 14 5 3 5 3
Table 3.1941.4 GPS week: 1941 Day: 4 MJD: 57835
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 | 1094 33 21 33 17 26 35 45 --- 13 | 16 16 15 17 17 4 8 --- 3
R02E | 3052 12 16 21 10 18 16 12 61 6 | 15 17 17 17 17 6 4 5 4
R03E | 1790 15 18 17 8 19 23 21 84 7 | 16 16 16 16 17 5 4 11 4
R04E | 715 11 13 16 9 17 21 15 --- 6 | 16 16 16 16 16 6 5 --- 4
R05E | 1671 20 22 33 20 34 32 39 --- 13 | 16 20 16 22 24 6 6 --- 7
R07E | 653 15 14 21 10 21 22 16 129 7 | 16 16 16 17 18 7 4 8 4
R08E | 913 13 15 24 10 25 28 11 --- 8 | 15 16 16 16 16 6 6 --- 4
XR09 | 3291 17 18 17 11 17 --- 13 --- 7 | 16 16 16 17 17 --- 3 --- 3
R10 | 1699 15 15 17 12 9 31 12 --- 7 | 16 16 15 16 16 5 2 --- 2
R11 | 780 20 24 16 10 26 20 29 228 9 | 15 15 15 16 16 5 2 6 2
R13 | 1837 25 33 25 9 19 17 30 --- 9 | 16 16 16 17 16 3 2 --- 1
R14 | 817 36 35 29 14 16 33 24 --- 11 | 16 17 17 18 17 4 4 --- 3
R15 | 1778 23 28 30 24 30 25 18 --- 11 | 16 16 15 17 17 3 2 --- 3
R16 | 1051 23 30 31 19 14 46 14 --- 11 | 16 17 16 16 16 5 2 --- 3
R17 | 1352 20 23 21 9 27 23 24 --- 9 | 16 16 16 17 16 3 1 --- 1
R18 | 936 21 23 18 11 17 20 17 --- 7 | 16 16 16 17 16 6 1 --- 3
R19 | 1209 43 27 28 20 19 26 43 --- 13 | 15 16 15 18 18 4 2 --- 3
R20 | 724 25 28 28 18 37 49 26 --- 13 | 16 18 17 17 19 5 3 --- 4
R21 | 671 25 27 23 7 24 23 30 64 9 | 16 16 16 17 17 3 3 2 2
R22 | 864 24 25 23 11 28 16 23 --- 9 | 15 16 16 17 16 6 3 --- 2
R23 | 1004 17 16 18 19 12 18 20 --- 8 | 16 16 15 16 16 4 2 --- 2
R24 | 744 19 27 38 19 11 64 25 --- 13 | 16 18 17 18 17 4 3 --- 3
XR26 | ---- --- --- --- --- --- --- 9 --- 0 | --- --- --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1337 23 24 25 14 23 30 25 129 |T 15 16 15 17 17 4 3 6 3
WRMS | 1337 25 26 25 13 22 28 25 129 |NE 15 16 15 16 16 4 2 4 2
MEDI | 1004 20 23 23 11 19 23 21 84 |MD 16 16 16 17 17 5 3 6 3
Table 3.1941.5 GPS week: 1941 Day: 5 MJD: 57836
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 | 1211 30 21 19 14 24 39 14 --- 10 | 16 17 17 17 18 7 8 --- 4
R02E | 2829 12 19 17 8 16 19 10 89 6 | 16 18 17 18 19 7 4 6 4
R03E | 716 17 10 16 11 17 27 15 56 7 | 17 17 17 18 18 6 5 18 4
R04E | 613 13 14 15 13 18 19 13 --- 6 | 17 17 17 17 17 5 4 --- 3
R05E | 2080 24 26 26 28 28 58 28 --- 13 | 17 18 18 21 23 6 6 --- 6
R07E | 745 12 13 19 9 17 36 11 152 7 | 17 18 18 19 18 6 4 13 4
R08E | 957 20 24 20 10 17 35 13 --- 8 | 17 17 17 17 17 6 4 --- 3
XR09 | 3961 17 13 20 22 13 --- 13 --- 9 | 17 17 17 17 17 --- 2 --- 2
R10 | 2896 8 16 15 15 11 24 14 --- 6 | 17 17 17 18 17 3 2 --- 2
R11 | 537 16 22 17 12 21 16 17 78 7 | 17 17 16 17 17 4 3 9 2
R13 | 1357 27 31 28 8 29 33 21 --- 10 | 17 17 17 17 17 5 2 --- 2
R14 | 799 41 32 27 24 30 39 19 --- 13 | 17 19 18 21 21 4 3 --- 6
R15 | 2439 35 31 30 21 20 17 21 --- 11 | 17 17 17 18 18 3 2 --- 3
R16 | 722 18 17 26 12 12 45 20 --- 9 | 17 19 17 17 17 4 2 --- 3
R17 | 1074 16 14 15 11 20 18 22 --- 7 | 17 17 17 17 17 3 2 --- 2
R18 | 1075 20 18 18 12 23 28 12 --- 8 | 17 17 17 18 18 5 2 --- 2
R19 | 1484 38 44 25 21 28 36 22 --- 12 | 17 17 17 18 17 3 2 --- 2
R20 | 1319 20 33 33 26 25 59 26 --- 13 | 17 18 17 17 18 4 3 --- 3
R21 | 522 23 22 17 11 20 32 24 78 9 | 17 17 17 18 18 3 3 3 2
R22 | 619 32 31 28 9 30 26 27 --- 11 | 17 17 17 18 18 4 3 --- 3
R23 | 949 14 19 12 18 12 29 12 --- 7 | 17 17 16 17 17 4 2 --- 2
R24 | 877 27 24 47 27 22 96 20 --- 17 | 17 19 17 20 18 2 3 --- 4
XR26 | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1420 24 24 24 16 22 39 19 96 |T 16 17 17 17 17 4 3 9 3
WRMS | 1420 25 27 24 14 21 37 19 96 |NE 17 17 16 17 17 3 2 6 2
MEDI | 957 20 21 19 12 20 32 17 78 |MD 17 17 17 18 18 4 3 9 3
Table 3.1941.6 GPS week: 1941 Day: 6 MJD: 57837
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 | 1419 27 27 30 14 20 30 30 --- 11 | 17 18 18 17 17 7 9 --- 5
R02E | 3541 16 10 19 10 20 19 12 122 7 | 17 18 17 17 18 5 4 5 3
R03E | 581 15 19 19 9 20 37 13 87 8 | 16 17 17 17 17 5 4 5 3
R04E | 683 11 17 13 11 18 23 16 --- 6 | 17 17 17 17 17 4 5 --- 4
R05E | 2478 13 20 26 21 35 31 13 --- 10 | 17 17 18 18 19 5 6 --- 5
R07E | 988 16 12 18 10 17 15 9 206 6 | 17 18 17 18 17 4 4 6 4
R08E | 1169 16 15 16 11 17 22 19 --- 7 | 17 17 17 18 18 5 5 --- 4
XR09 | 4087 14 18 17 17 10 --- 11 --- 7 | 17 16 17 17 17 --- 2 --- 1
R10 | 2413 14 21 18 9 15 10 11 --- 5 | 17 17 17 17 17 2 1 --- 2
R11 | 549 19 16 15 12 19 27 12 60 7 | 17 17 17 17 17 3 2 4 1
R13 | 600 23 27 18 11 28 20 16 --- 8 | 16 17 17 16 17 4 2 --- 1
R14 | 699 32 41 20 24 40 35 23 --- 13 | 17 18 17 19 19 3 3 --- 5
R15 | 1482 37 35 26 20 21 18 17 --- 10 | 17 17 17 17 17 2 2 --- 2
R16 | 834 20 38 55 13 14 52 22 --- 13 | 17 18 17 17 18 2 2 --- 2
R17 | 954 27 33 21 9 15 14 19 --- 8 | 17 17 17 17 17 3 1 --- 2
R18 | 1086 14 15 12 9 14 11 9 --- 5 | 17 17 17 17 17 3 2 --- 1
R19 | 1897 31 32 29 8 24 17 29 --- 10 | 17 17 17 17 17 2 2 --- 1
R20 | 1173 27 34 45 15 22 61 15 --- 13 | 17 17 17 18 17 3 3 --- 2
R21 | 458 20 30 15 10 19 20 17 103 7 | 17 17 16 17 17 3 2 2 1
R22 | 566 30 33 29 12 28 20 27 --- 10 | 17 17 17 18 18 3 2 --- 2
R23 | 1135 19 21 18 20 11 21 10 --- 7 | 17 17 17 17 17 3 2 --- 1
R24 | 1152 22 43 28 15 20 51 19 --- 11 | 17 18 17 18 17 2 4 --- 3
XR26 | ---- 29 115 --- --- --- --- 23 --- 26 | 9999 9999 --- --- --- --- 2 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS | 1446 23 27 25 14 22 30 18 126 |T 16 17 17 17 17 3 3 4 2
WRMS | 1446 25 28 25 13 19 27 18 126 |NE 16 17 16 17 17 2 2 3 1
MEDI | 1086 20 27 19 11 19 21 16 103 |MD 17 17 17 17 17 3 2 5 2
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