[IGSREPORT-24951] Wk 1925 IGLOS Final Orbits
acc at igs.org
acc at igs.org
Mon Dec 19 15:13:16 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1925 (Nov 27, 2016 - Dec 03, 2016)
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 2.1925.
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:
igl1925[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1925 in the SP3 format.
igl19257.sum Combination Report for GPS Week 1925.
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
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 | 7.6 ns
1 | -10.5 ns
2 | -9.1 ns
3 | -11.9 ns
4 | -10.9 ns
5 | -12.1 ns
6 | -15.0 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 1.1925, 1a.1925).
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 2.1925.0-6)
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 3.1925.0-6).
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 1925 summary. (Nov 27, 2016 - Dec 03, 2016)
Table 1.1925.a GPS week : 1925 MJD: 57719.0-57725.0
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 -9 2 -37 -15 .24 25 22 | --- --- --- ---
| 1 1 4 22 23 20 .04 | --- ---
cof n/a| 0 0 -10 2 -33 -12 .30 28 25 | --- --- --- ---
| 1 1 3 33 13 42 .05 | --- ---
emx n/a| -1 0 0 -79 -18 -59 .21 22 22 | -7363 -753 3006 10544
| 1 0 2 17 25 33 .03 | 11784 1005
esx n/a| 0 -1 0 32 31 27 -.18 20 18 | -12075 808 3010 13218
| 0 0 1 16 11 28 .03 | 11483 2175
gfz n/a| 0 0 4 40 83 39 .00 27 24 | 0 196 2999 10803
| 0 1 3 20 39 30 .04 | 0 1884
grg n/a| 0 1 4 7 -28 -2 -.28 27 25 | -8902 197 3018 11335
| 1 1 3 14 20 25 .10 | 7644 1792
Table 1.1925.b GPS week : 1925 MJD: 57719.0-57725.0
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 | 16 14 12 17 13 12 10 |
R02 | 7 9 9 8 8 8 10 |
R03 | 11 10 8 7 8 9 10 |
R04 | 9 10 11 7 7 6 6 |
R05 | 14 16 14 10 12 12 16 |
R06 | 7 11 10 12 9 10 8 |
R07 | 9 11 10 9 10 9 7 |
R08 | 11 8 7 10 10 9 14 |
R09 | 22 23 23 18 16 18 22 |
R10 | 11 8 9 9 10 9 9 |
R11 | 16 11 10 13 11 8 9 |
R13 | 11 13 13 13 12 16 12 |
R14 | 14 20 15 17 15 15 20 |
R15 | 10 8 10 9 12 12 10 |
R16 | 16 16 15 18 17 13 17 |
R17 | 10 13 12 10 10 13 10 |
R18 | 9 12 11 9 8 9 10 |
R19 | 15 15 20 15 16 12 14 |
R20 | 15 16 17 17 18 14 16 |
R21 | 11 12 11 12 11 11 11 |
R22 | 11 12 9 9 10 13 11 |
R23 | 13 12 12 12 11 10 9 |
R24 | 15 17 15 15 15 12 14 |
R26 | 0 0 0 0 0 0 0 |
Table 1.1925.c GPS week : 1925 MJD: 57719.0-57725.0
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 1925 0 | 28 -16 -89 185 514 -1263 82.9 1121 1121 | 7562 0
brd 1925 1 | 44 41 -144 -171 1067 -1325 82.8 1208 1208 | -10507 0
brd 1925 2 | -27 -21 -49 1633 2036 -1415 84.2 1086 1086 | -9066 0
brd 1925 3 | -33 -3 -70 -122 1014 -1898 84.3 1203 1203 | -11881 0
brd 1925 4 | 45 19 -6 127 -99 -3145 84.2 1251 1251 | -10869 0
brd 1925 5 | -36 69 19 248 -1703 -4898 84.1 1319 1319 | -12123 0
brd 1925 6 | 73 -81 -20 1220 -58 -3556 85.3 1321 1321 | -14975 0
-------------+------------------------------------------------------------+----------------
brd 1925 mean| 13 1 -51 445 395 -2500 84.0 1215 1215 | -8837 0
brd 1925 sdev| 45 48 55 697 1182 1398 .9 90 90 | 7456 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 2.1925.0 GPS week: 1925 Day: 0 MJD: 57719
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 -14 -1 -6 2 .29 28 29 | --- --- --- ---
cof n/a| 0 0 -14 -19 -14 -35 .24 31 32 | --- --- --- ---
emx n/a| 0 0 0 -53 -42 -73 .22 21 21 | -5985 -972 2725 10708
esx n/a| 0 -1 0 18 36 55 -.15 18 15 | 12083 -889 2732 13056
gfz n/a| 1 -2 8 24 43 47 .00 27 26 | 0 -452 2772 11355
grg n/a| -2 3 3 31 2 -36 -.42 30 29 | 7922 -581 2737 11289
Table 2.1925.1 GPS week: 1925 Day: 1 MJD: 57720
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 -7 5 -69 -56 .29 30 25 | --- --- --- ---
cof n/a| 0 0 -14 35 -53 48 .39 31 24 | --- --- --- ---
emx n/a| -1 0 -3 -70 -13 -124 .23 23 23 | -5460 -408 2836 10133
esx n/a| 0 -2 -2 25 44 62 -.12 21 17 | -8131 -516 2834 13143
gfz n/a| 0 0 9 29 62 47 .03 31 26 | 0 -1115 2809 10322
grg n/a| 0 0 5 6 -42 30 -.42 25 24 | -9991 -965 2856 10797
Table 2.1925.2 GPS week: 1925 Day: 2 MJD: 57721
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 -14 38 -25 -23 .22 29 23 | --- --- --- ---
cof n/a| -1 0 -14 57 -29 -76 .25 34 28 | --- --- --- ---
emx n/a| -1 0 0 -103 7 -55 .21 22 22 | -3954 -1356 3597 11655
esx n/a| 0 -1 0 24 31 33 -.21 20 15 | -15610 -245 3628 14493
gfz n/a| 0 -3 4 61 69 -13 .01 27 25 | 0 -970 3565 11856
grg n/a| 0 2 6 11 -49 11 -.23 24 23 | -8729 -665 3616 12634
Table 2.1925.3 GPS week: 1925 Day: 3 MJD: 57722
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 -8 -34 -61 -22 .27 27 24 | --- --- --- ---
cof n/a| 0 0 -8 -35 -33 9 .27 27 23 | --- --- --- ---
emx n/a| -1 0 2 -71 18 -55 .22 22 22 | -9640 -923 3008 10942
esx n/a| 1 -1 -1 60 18 9 -.21 21 18 | -18614 2227 3000 13411
gfz n/a| 1 -1 0 69 98 60 -.00 26 25 | 0 903 3001 11076
grg n/a| 1 3 4 -16 -19 14 -.24 25 24 | -12289 893 3027 11837
Table 2.1925.4 GPS week: 1925 Day: 4 MJD: 57723
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 -6 -12 -22 -5 .21 20 19 | --- --- --- ---
cof n/a| -1 -2 -7 -24 -19 -14 .32 26 25 | --- --- --- ---
emx n/a| -4 0 1 -75 -49 -53 .24 24 24 | -27772 175 2822 9782
esx n/a| 0 -1 0 34 46 -20 -.18 17 17 | -22412 3543 2842 12286
gfz n/a| 0 0 3 10 43 77 -.08 26 24 | 0 2526 2847 9875
grg n/a| 2 3 7 9 -8 0 -.17 32 29 | -11801 2143 2854 10633
Table 2.1925.5 GPS week: 1925 Day: 5 MJD: 57724
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 7 -52 -1 .20 19 20 | --- --- --- ---
cof n/a| -1 -1 -7 6 -39 21 .32 24 22 | --- --- --- ---
emx n/a| 0 0 2 -82 -13 -21 .16 22 22 | -10912 623 2934 9717
esx n/a| 0 -1 2 16 22 23 -.18 19 19 | -15466 3334 2925 12484
gfz n/a| 0 0 3 40 143 10 .02 26 23 | 0 2681 2894 9788
grg n/a| 0 0 -4 0 -41 -35 -.23 24 22 | -13394 2756 2936 10552
Table 2.1925.6 GPS week: 1925 Day: 6 MJD: 57725
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 -6 11 -23 -2 .21 19 17 | --- --- --- ---
cof n/a| 0 0 -7 -2 -45 -39 .31 23 22 | --- --- --- ---
emx n/a| -1 0 -1 -101 -37 -29 .16 23 24 | 12177 -2412 3122 10874
esx n/a| 0 0 0 50 22 25 -.18 23 23 | -16377 -1796 3115 13654
gfz n/a| 0 1 2 46 123 46 .03 26 22 | 0 -2195 3106 11351
grg n/a| 0 -1 7 11 -43 -5 -.28 26 22 | -14036 -2202 3101 11604
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 3.1925.0 GPS week: 1925 Day: 0 MJD: 57719
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 659 28 42 31 25 44 29 15 | 71 77 69 34 26 63 48
R02 | 690 22 15 10 8 20 14 7 | 63 61 48 45 38 48 46
R03 | 996 21 28 24 8 23 31 10 | 70 76 67 49 41 45 52
R04 | 594 20 21 20 10 22 22 9 | 71 73 67 49 44 38 52
R05 | 640 22 22 23 35 20 36 14 | 52 46 60 49 43 42 47
R06 | 1354 19 22 13 7 17 13 6 | 45 51 46 45 38 46 43
R07 | 740 27 29 17 14 17 18 9 | 80 82 73 53 49 52 60
R08 | 613 19 28 16 17 16 36 10 | 78 83 75 68 53 61 66
XR09 | 2547 23 31 --- --- 19 --- 21 | 51 51 --- --- 52 --- 49
R10 | 1268 22 22 8 19 21 32 10 | 40 36 30 41 33 32 31
R11 | 1102 28 35 22 12 43 55 16 | 42 46 37 34 31 38 30
R13 | 964 36 39 12 11 34 16 11 | 61 67 42 46 41 46 42
R14 | 2070 29 35 14 33 22 39 14 | 42 53 38 59 34 32 38
R15 | 2567 29 30 16 14 29 17 10 | 44 44 27 32 24 25 27
R16 | 590 52 62 32 17 33 27 16 | 53 59 33 41 39 38 34
R17 | 564 25 26 18 16 22 21 10 | 110 107 107 101 103 115 105
R18 | 845 22 18 17 12 22 22 9 | 102 102 105 106 116 117 107
R19 | 1319 45 40 23 14 38 27 14 | 101 98 105 107 121 119 108
R20 | 841 21 23 21 27 28 46 14 | 93 100 100 97 110 91 96
R21 | 522 28 17 19 11 27 21 10 | 134 134 142 145 150 132 140
R22 | 802 27 31 18 14 29 28 11 | 67 69 74 75 87 75 73
R23 | 1321 21 19 26 28 17 28 12 | 160 164 161 165 166 160 162
R24 | 1035 35 39 31 17 25 41 14 | 63 62 71 57 58 76 61
XR26 | ---- 9 128 --- --- --- --- 0 | 105 92 --- --- --- --- 107
------+-----------------------------------------+-------------------------------------
RMS | 1120 28 31 21 18 27 30 |T 74 76 71 68 65 67 67
WRMS | 1120 29 32 21 15 26 29 |NE 57 60 50 46 39 43 44
MEDI | 845 23 28 18 14 22 27 |MD 67 69 67 49 44 48 52
Table 3.1925.1 GPS week: 1925 Day: 1 MJD: 57720
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 1417 35 21 23 23 42 18 14 | 53 38 39 29 30 37 32
R02 | 861 20 17 13 9 31 14 8 | 36 34 33 29 22 31 27
R03 | 629 24 21 18 13 26 19 9 | 44 46 40 34 21 21 29
R04 | 628 22 22 21 7 14 28 9 | 55 61 52 40 38 33 41
R05 | 699 29 14 31 31 24 40 16 | 33 36 47 27 33 25 22
R06 | 851 26 22 22 11 33 22 11 | 31 29 36 19 26 37 24
R07 | 855 32 27 21 21 22 14 11 | 53 55 45 27 26 33 33
R08 | 758 15 14 13 13 17 21 8 | 51 55 48 40 40 51 44
XR09 | 3288 22 24 --- --- 22 --- 22 | 43 47 --- --- 52 --- 46
R10 | 784 15 17 14 17 14 16 7 | 31 30 27 30 24 21 25
R11 | 839 24 20 17 11 36 16 10 | 40 36 30 31 30 25 26
R13 | 981 30 33 19 11 43 29 13 | 41 42 35 27 26 37 28
R14 | 2848 35 30 26 45 36 46 19 | 43 59 51 59 49 31 42
R15 | 2730 19 26 14 11 25 12 8 | 32 37 23 23 23 25 22
R16 | 1368 50 40 25 20 39 26 15 | 49 41 26 27 30 23 21
R17 | 706 39 38 28 18 24 24 13 | 164 161 149 157 163 163 157
R18E | 579 29 24 19 16 22 29 11 | 73 94 78 92 88 96 84
R19 | 1488 52 58 22 18 38 18 15 | 113 120 110 120 126 124 115
R20 | 774 26 49 26 21 53 35 16 | 94 99 97 94 104 108 95
R21E | 526 25 38 27 20 24 23 12 | 136 138 127 143 144 139 136
R22E | 832 25 25 26 19 30 19 11 | 62 65 59 66 76 70 61
R23E | 1179 22 18 24 26 14 21 11 | 96 97 95 95 92 96 93
R24E | 558 31 55 33 38 29 32 16 | 57 72 54 69 64 48 54
XR26E | ---- 8 170 --- --- --- --- 0 | 87 199 --- --- --- --- 91
------+-----------------------------------------+-------------------------------------
RMS | 1208 30 31 23 21 31 25 |T 63 70 59 58 57 57 56
WRMS | 1208 25 24 23 17 26 24 |NE 42 43 38 31 31 30 30
MEDI | 839 25 24 22 18 26 21 |MD 51 55 47 34 38 37 41
Table 3.1925.2 GPS week: 1925 Day: 2 MJD: 57721
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 712 27 46 21 24 22 19 11 | 52 77 48 38 35 52 42
R02 | 793 13 19 16 12 20 25 9 | 49 54 37 34 33 62 41
R03 | 805 13 17 17 11 28 13 8 | 51 53 50 40 29 46 41
R04 | 652 22 28 24 8 16 31 10 | 57 62 54 35 31 30 38
R05 | 875 28 42 28 31 15 25 13 | 41 52 46 51 36 35 38
R06 | 1076 22 19 18 17 27 15 9 | 37 44 44 32 29 36 34
R07 | 1208 22 25 21 12 34 14 10 | 65 69 63 54 41 57 54
R08 | 865 15 12 11 13 17 16 7 | 63 59 54 46 40 59 50
XR09 | 3153 25 26 --- --- 19 --- 22 | 51 54 --- --- 53 --- 50
R10 | 841 26 33 14 9 27 13 9 | 33 41 36 29 25 24 26
R11 | 663 23 33 16 11 27 19 9 | 32 39 28 25 20 29 20
R13 | 1166 34 34 18 10 41 28 13 | 43 45 36 30 32 25 27
R14 | 1833 21 37 22 41 28 24 15 | 38 57 32 60 47 34 37
R15 | 2528 15 18 11 18 26 27 10 | 31 30 25 37 28 35 26
R16 | 1213 46 75 23 22 28 33 15 | 55 91 34 41 32 26 33
R17E | 587 34 16 16 12 37 25 12 | 109 117 118 117 130 120 116
R18E | 741 20 17 20 16 21 27 10 | 88 91 104 91 96 111 97
R19E | 1261 63 64 38 29 32 35 19 | 136 171 146 178 173 171 159
R20E | 968 47 37 32 26 39 30 17 | 131 151 141 168 175 170 155
R21E | 511 30 16 18 15 24 19 10 | 100 102 106 101 113 109 104
R22E | 713 18 19 18 16 20 18 9 | 52 54 59 55 57 58 53
R23E | 1127 16 19 26 25 20 20 11 | 78 83 83 80 79 74 77
R24E | 632 32 37 30 23 30 31 14 | 53 65 61 63 72 76 61
XR26E | ---- 9 99 --- --- --- --- 0 | 88 179 --- --- --- --- 87
------+-----------------------------------------+-------------------------------------
RMS | 1085 29 34 22 20 27 24 |T 63 76 63 63 61 65 61
WRMS | 1085 23 28 22 15 25 23 |NE 46 55 41 39 34 39 37
MEDI | 865 22 26 18 16 27 24 |MD 52 59 50 46 40 52 42
Table 3.1925.3 GPS week: 1925 Day: 3 MJD: 57722
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 663 34 25 27 35 35 32 16 | 56 47 65 43 54 59 48
R02 | 552 18 18 7 16 11 22 8 | 53 52 43 45 45 38 42
R03 | 702 10 18 6 16 17 14 6 | 60 57 56 61 46 67 58
R04 | 902 14 19 11 13 21 13 7 | 61 64 45 56 40 47 48
R05 | 705 21 12 19 24 21 13 10 | 45 50 55 59 36 45 47
R06 | 1821 19 20 22 28 20 20 11 | 47 47 57 51 47 49 49
R07 | 1855 21 22 16 11 20 18 8 | 72 64 63 60 48 58 59
R08 | 1600 18 25 17 12 28 23 10 | 66 73 53 61 46 78 59
XR09 | 4099 19 16 --- --- 16 --- 18 | 22 26 --- --- 40 --- 28
R10 | 570 22 19 15 11 24 12 8 | 38 35 29 31 25 28 26
R11 | 573 30 21 20 12 38 24 12 | 37 35 35 29 31 41 28
R13 | 2963 34 34 15 15 33 26 12 | 50 51 40 40 41 30 34
R14 | 1646 32 30 24 33 29 46 17 | 36 45 49 48 39 30 36
R15 | 1293 17 20 15 18 23 20 9 | 38 39 32 36 32 27 29
R16 | 936 54 55 34 23 27 38 18 | 64 53 38 50 43 38 36
R17E | 640 21 23 18 15 23 24 10 | 61 62 56 65 68 79 63
R18E | 561 13 19 18 17 21 16 8 | 74 75 77 76 83 88 78
R19E | 661 42 40 28 25 27 21 14 | 143 144 145 145 149 154 145
R20E | 987 39 39 34 32 30 38 17 | 160 168 177 174 170 170 169
R21E | 585 24 26 22 13 33 22 11 | 87 91 86 89 95 86 86
R22E | 649 22 21 16 11 27 12 9 | 59 61 62 58 68 54 58
R23E | 1197 22 13 25 26 20 23 12 | 82 84 93 85 84 78 82
R24E | 959 25 27 36 25 27 31 14 | 55 61 60 51 47 60 51
XR26E | ---- 7 219 --- --- --- --- 0 | 66 238 --- --- --- --- 66
------+-----------------------------------------+-------------------------------------
RMS | 1202 27 27 22 21 26 25 |T 63 71 64 64 59 63 59
WRMS | 1202 24 23 22 18 25 24 |NE 49 49 47 47 40 45 41
MEDI | 902 21 21 18 16 24 22 |MD 59 57 56 56 46 54 49
Table 3.1925.4 GPS week: 1925 Day: 4 MJD: 57723
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 694 15 18 28 21 30 31 12 | 43 41 50 35 34 54 37
R02 | 1288 18 23 15 12 18 19 8 | 48 51 42 28 24 35 34
R03 | 1084 14 15 17 14 16 13 7 | 53 54 53 38 39 47 44
R04 | 1027 12 14 16 8 13 24 7 | 52 51 54 48 40 45 47
R05 | 799 25 34 26 25 15 22 11 | 38 31 69 52 45 40 47
R06 | 1658 13 18 20 18 21 20 9 | 34 44 39 49 38 25 37
R07 | 959 23 29 14 5 19 34 9 | 63 71 57 49 52 36 50
R08 | 1576 18 15 16 13 25 25 9 | 59 55 54 44 40 45 48
XR09 | 3576 15 18 --- --- 16 --- 15 | 23 27 --- --- 29 --- 22
R10 | 670 14 19 27 14 21 17 9 | 38 39 36 34 23 29 29
R11 | 654 23 40 17 18 27 18 10 | 48 62 35 27 29 31 29
R13 | 2399 31 41 18 6 34 18 11 | 50 57 29 32 22 30 29
R14 | 1971 15 18 33 17 26 52 14 | 36 43 38 40 38 18 31
R15 | 1566 16 25 15 22 23 37 11 | 38 47 35 44 28 30 30
R16 | 542 30 34 30 25 37 48 16 | 38 61 40 48 37 45 36
R17E | 609 18 26 20 8 25 24 9 | 47 51 48 47 51 58 46
R18E | 897 11 12 20 14 16 22 8 | 50 54 50 49 56 53 49
R19E | 1066 28 18 41 15 35 40 15 | 137 139 142 146 147 146 141
R20E | 899 20 35 22 21 42 67 17 | 143 140 142 144 152 156 144
R21E | 712 24 26 26 19 22 17 11 | 61 60 56 61 60 59 57
R22E | 884 23 30 20 8 32 16 10 | 57 58 56 55 68 58 55
R23E | 2151 19 26 21 20 29 23 11 | 61 66 64 65 61 61 59
R24E | 968 18 24 41 23 28 39 15 | 46 49 55 44 50 52 42
XR26E | ---- 5 587 --- --- --- --- 0 | 61 507 --- --- --- --- 62
------+-----------------------------------------+-------------------------------------
RMS | 1250 20 26 24 17 26 31 |T 55 77 56 53 50 52 50
WRMS | 1250 19 25 24 17 24 29 |NE 44 48 45 40 34 36 36
MEDI | 968 18 24 20 15 25 23 |MD 48 54 50 47 40 45 44
Table 3.1925.5 GPS week: 1925 Day: 5 MJD: 57724
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 849 18 23 21 28 25 20 11 | 37 44 43 33 34 44 35
R02 | 1542 19 13 14 13 21 13 8 | 42 41 39 31 32 41 35
R03 | 1181 13 16 18 17 20 15 8 | 42 49 46 47 48 53 45
R04 | 1416 9 12 12 15 12 12 6 | 47 50 50 41 46 60 47
R05 | 1173 17 15 28 20 25 23 11 | 35 46 53 46 51 47 43
R06 | 1067 13 21 23 24 20 13 9 | 34 40 41 33 35 47 36
R07 | 593 12 18 15 10 21 25 8 | 57 59 58 56 47 42 52
R08 | 1700 11 13 12 19 20 23 8 | 49 56 47 61 54 56 53
XR09 | 2799 16 17 --- --- 21 --- 18 | 20 22 --- --- 35 --- 23
R10 | 821 11 28 15 19 16 21 8 | 35 44 27 43 31 23 30
R11 | 878 15 19 11 14 21 12 7 | 34 34 26 35 27 31 28
R13 | 1470 43 41 17 13 44 29 15 | 48 48 27 30 35 31 26
R14 | 2903 23 33 36 16 38 37 15 | 35 41 39 45 38 26 31
R15 | 1151 20 24 13 14 34 31 11 | 38 38 31 35 46 29 30
R16 | 501 17 29 14 20 30 38 12 | 32 37 44 34 30 23 26
R17E | 618 22 23 33 16 28 32 13 | 44 44 38 46 52 50 39
R18E | 1551 13 11 16 22 21 18 9 | 53 55 50 56 61 61 53
R19E | 1012 25 33 23 18 28 23 11 | 138 146 142 157 156 145 146
R20E | 905 18 21 37 20 33 30 14 | 148 159 138 152 153 160 148
R21E | 611 20 32 19 24 27 17 11 | 62 61 51 55 56 55 53
R22E | 1125 27 27 28 27 23 16 12 | 47 50 33 46 39 46 38
R23E | 2163 15 21 18 24 16 19 9 | 56 54 56 60 52 52 53
R24E | 1190 14 23 30 20 19 28 11 | 48 52 52 45 50 42 44
XR26E | ---- 5 162 --- --- --- --- 0 | 34 209 --- --- --- --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1318 19 24 22 19 26 24 |T 50 61 51 53 52 52 47
WRMS | 1318 20 22 22 19 23 22 |NE 39 43 40 40 39 39 36
MEDI | 1151 16 21 18 19 21 21 |MD 42 48 44 45 46 46 38
Table 3.1925.6 GPS week: 1925 Day: 6 MJD: 57725
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 852 18 17 23 20 15 21 10 | 80 72 75 62 74 78 72
R02 | 1081 20 33 22 20 15 13 9 | 67 77 56 50 45 51 53
R03 | 1214 13 7 15 21 28 20 9 | 70 66 73 48 39 73 60
R04 | 1485 11 17 14 13 12 10 6 | 69 73 65 55 56 62 61
R05 | 1560 12 28 33 31 23 49 15 | 62 60 65 64 62 58 61
R06 | 2327 17 16 12 18 11 17 8 | 40 44 39 47 33 42 39
R07 | 867 9 18 12 16 21 9 7 | 70 73 70 69 57 60 64
R08 | 788 9 13 10 46 23 34 13 | 73 72 69 102 68 56 72
XR09 | 2692 19 29 --- --- 25 --- 22 | 21 30 --- --- 38 --- 23
R10 | 870 10 23 9 30 18 17 9 | 37 43 39 46 30 30 33
R11 | 717 12 10 15 20 21 17 8 | 42 42 35 40 31 30 31
R13 | 1179 30 38 13 15 32 17 11 | 57 62 40 36 25 32 35
R14 | 1496 35 20 29 35 46 53 20 | 40 42 40 45 30 25 31
R15 | 969 15 19 18 17 32 10 9 | 44 49 34 48 31 40 37
R16 | 498 31 40 40 22 36 38 17 | 42 50 38 44 43 42 35
R17E | 730 19 13 19 13 29 14 9 | 56 55 60 59 69 61 58
R18E | 1875 15 13 22 18 23 17 9 | 71 76 79 82 89 76 77
R19E | 2063 28 38 26 13 41 28 14 | 189 186 198 205 199 206 199
R20E | 1142 19 24 41 24 27 40 15 | 166 166 192 167 174 179 174
R21E | 796 19 18 22 17 24 23 10 | 88 88 85 92 91 92 87
R22E | 1557 19 33 25 23 25 20 11 | 68 70 69 65 75 68 66
R23E | 1365 19 13 16 24 14 13 9 | 88 94 94 94 92 87 90
R24E | 1713 14 20 35 24 27 36 14 | 60 66 62 60 59 52 54
XR26E | ---- 5 328 --- --- --- --- 0 | 69 282 --- --- --- --- 71
------+-----------------------------------------+-------------------------------------
RMS | 1320 19 23 23 23 26 26 |T 69 80 71 71 65 68 65
WRMS | 1320 17 22 24 23 22 22 |NE 54 57 52 54 44 48 47
MEDI | 1179 17 19 19 20 24 17 |MD 67 66 65 59 57 58 60
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