[IGSREPORT-21197] Wk 1705 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Sep 28 05:30:56 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1705 (Sep 09, 2012 - Sep 15, 2012)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data. This is primarily intended
for testing clock solution precision as well as the orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility, no satellite L1/L2 delay calibration should be
applied.
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.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite. Note that each file contains all the
satellites that appear in any of the centre ephemeris files. If a satellite or
centre was excluded from combination, a note in the REMARKS section of this
report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to
the last non-predicted day of Bulletin A. AC LOD biases are removed and the
new AC bias-free LODs are used to compute a weighted IGS LOD which in turn
is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as
Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and
UT1-UTC values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1705[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1705[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1705[0-6].cls IGS GPS clock combination summary report.
igs17057.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17057.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and
JPL. The other centres are excluded because of poorer consistency (GRG),
they provide broadcast clocks (NGS), or clock corrections are not provided
(SIO). The clock information not used is still compared to combination for
completeness. Starting 12-Aug-2012 (GPS Week 1701, day 0, MJD 56151), GRG clocks
are included after changing their procedures to generate estimates in the
center-of-figure frame instead of the center-of-mass frame.
The value of 999999.999999 microseconds, according to the sp3 format
convention, is used to signify that no clock solution is available and
therefore must not be used.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 9 31 KOUC GUAT KOUC
0 | EMR | 8 8 CHUR CHUR MATE
0 | ESA | 9 GUAT
0 | GFZ | IRKJ PIMO
0 | GRG | 13 USNO WROC GUAT USNO WROC
0 | JPL | 8 9
0 | MIT | GUAT IRKJ MAS1 USNO IRKJ MAS1 USNO
1 | COD | 30 9 30 JOZ2 KOUC JOZ2 KOUC
1 | EMR | 8 4 8
1 | ESA | 9 IRKJ
1 | GFZ | 8 BOGT MAS1 WSRT
1 | GRG | MAR6 MAS1 NTUS IRKJ LHAZ MAR6 NOVM SPT0
1 | JPL | 8 NICO
1 | MIT | IRKJ NICO SPT0 MAR6 NICO SPT0
2 | COD | 9 HERT KOUC MAW1 HERT KOUC MAW1
2 | EMR | 9 8 9
2 | ESA | IRKJ MAW1 NNOR
2 | GFZ | LHAZ MAS1
2 | GRG | THTI YEBE IRKJ SPT0 THTI YEBE
2 | JPL | 8
2 | MIT | IRKJ TOW2 TOW2
3 | COD | 9
3 | ESA | 9
3 | GFZ | IRKJ
3 | GRG | LHAZ WROC
3 | JPL | 8
3 | MIT | IRKJ IRKJ
4 | COD | DARW KOUC DARW KOUC
4 | EMR | 11 2 8 11
4 | ESA | ZECK IRKJ WES2
4 | GFZ | DARW WSRT
4 | GRG | GUAT IRKJ NICO
4 | JPL | 2 4 8 NNOR
4 | MIT | 29 IRKJ
4 | NGS | 30
5 | COD | 4 9 21 4 9 21 KOUC KOUC
5 | EMR | 8 8 YEBE YEBE
5 | ESA | 4 9 4 9
5 | GFZ | 4 IRKJ NKLG
5 | GRG | 13 13 WROC DARW KARR NOVM WROC
5 | JPL | 8 27
5 | MIT | 21 21 27 IRKJ REUN IRKJ REUN
6 | COD | 4 9 4 8 9
6 | EMR | 9 HERS HERS THTI
6 | ESA | 4 9 4 8 9 HOB2
6 | GFZ | 4 8 SUTM
6 | GRG | 21 27 HOB2 YEBE ADIS HOB2 YEBE
6 | JPL | 8 27 REUN
6 | MIT | 28 27 28 IRKJ
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average (generally indicated by long arc RMS).
They were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
1 | NGS | ALL (high Transformation - See Table 2)
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) all IGS products, including the IGS
combined orbits, are based on the IGS realization of the ITRF2005 reference
frame (IGS05). For more information see IGSMAIL #5447. The IGS05 frame
is also the basis for 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) all IGS products,
are based on the IGS realization of the ITRF2008 reference frame (IGS08).
For more information see IGSMAIL #6354.
7. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the current IGS reference frame. These rotations were
estimated in the IGS SINEX combination process, performed by the IGS Reference
Frame Coordinator at the Institut Geographique National (IGN). Starting on
19-Aug-2012 (GPS Week 1702; mjd=56158), ACs began contributing products based
on 1d SINEX integrations. As a result, the SINEX combinations are now done
daily instead of weekly, and the associated daily rotations are applied here
to the orbits and ERPs. The estimated 7 transformations, from which only the
3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
EMR | 0 | 2.9 -2.9 4.7 -2 -4 5 -.13
ESA | 0 | -1.0 5.9 15.6 66 39 107 .0
GFZ | 0 | -.5 1.5 -1.0 -50 -23 -19 -.08
GRG | 0 | -8.2 -1.7 16.5 -27 28 -22 .23
JPL | 0 | 3.3 5.0 9.4 14 13 -52 .32
MIT | 0 | .0 .4 12.6 -11 2 -42 -.01
NGS | 0 | -4.4 -7.5 22.9 -141 37 -30 .16
EMR | 1 | -3.1 3.6 5.0 -2 0 4 -.06
ESA | 1 | -2.4 4.6 17.6 63 96 52 -.29
GFZ | 1 | -.7 1.0 -.2 -48 -20 -1 -.25
GRG | 1 | -.2 -.3 17.7 -35 43 -45 .02
JPL | 1 | 4.6 .2 11.4 -22 6 -76 -.13
MIT | 1 | .8 1.0 17.0 -7 4 -38 -.15
NGS | 1 | -3.1 -10.3 34.1 -192 37 -18 -.04
EMR | 2 | -1.4 6.5 8.9 -5 5 6 -.33
ESA | 2 | 1.6 8.1 22.0 138 38 50 -.54
GFZ | 2 | -.3 1.3 .1 -49 -8 0 -.61
GRG | 2 | -3.4 .6 23.0 -64 50 -36 -.36
JPL | 2 | 6.5 3.0 8.6 -34 17 -26 -.29
MIT | 2 | -1.1 3.8 19.4 -9 10 -39 -.25
NGS | 2 | -3.8 -4.1 24.8 -126 39 -30 -.14
EMR | 3 | -1.5 -1.3 7.3 -5 9 8 -.35
ESA | 3 | .9 3.7 19.5 89 21 91 -.42
GFZ | 3 | -.5 .9 .2 -53 -13 0 -.27
GRG | 3 | -5.8 -3.8 16.7 -41 48 -28 -.14
JPL | 3 | -2.5 3.8 10.3 -70 12 -33 -.08
MIT | 3 | -.9 3.1 14.8 -13 5 -43 -.27
NGS | 3 | -4.4 -1.0 24.5 -92 34 -31 -.15
EMR | 4 | 1.9 2.7 9.7 -5 15 20 -.20
ESA | 4 | -.9 7.2 17.3 105 34 66 -.28
GFZ | 4 | -.2 2.1 .2 -37 -26 -3 -.13
GRG | 4 | -4.8 -3.9 14.3 -51 43 -37 -.22
JPL | 4 | -7.1 -.7 12.8 -74 -6 -36 -.10
MIT | 4 | 2.5 5.3 19.7 -14 7 -40 -.26
NGS | 4 | -10.2 3.9 17.5 -45 56 -49 -.05
EMR | 5 | -2.1 3.3 11.3 -4 8 9 -.15
ESA | 5 | 2.5 3.8 17.6 65 5 110 -.62
GFZ | 5 | .5 .7 .5 -38 0 -4 -.61
GRG | 5 | -3.4 -3.1 13.0 -72 68 -31 -.20
JPL | 5 | 1.6 5.8 15.4 -60 16 -38 -.42
MIT | 5 | 3.0 6.2 14.1 -19 11 -46 -.36
NGS | 5 | 5.2 -2.8 25.2 -92 -25 15 .0
EMR | 6 | -4.1 10.8 3.5 3 10 11 -.34
ESA | 6 | -4.1 5.3 19.0 51 100 68 -.66
GFZ | 6 | -.6 1.8 .6 -53 5 -31 -.54
GRG | 6 | -5.4 .3 14.1 -64 33 -16 -.51
JPL | 6 | -2.7 1.8 13.7 -17 0 -24 -.08
MIT | 6 | 1.1 5.1 13.8 -25 19 -46 -.45
NGS | 6 | -.8 -4.3 20.6 -68 -1 -11 -.11
8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used.
The navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and ERPs
as generated by IGN). For more information see IGSMAIL #2750. Because of this
change in alignment, Table 2 has been enhanced with one additional line per AC.
This additional line shows daily X- and Y-rotations, i.e. RX_sp3(ac) and
RY_sp3(ac), used to align each daily AC orbit to the combined SINEX prior to
the orbit combination. These a-priori rotations are derived from three sources:
the daily AC polar motion estimates, XPO(ac) and YPO(ac), provided in their ERP
files; the combined polar motion values, XPO(cmb) and YPO(cmb), from the SINEX
combination; along with the AC TRF rotations, RX_snx(ac) and RY(ac), also from
the SINEX combination:
RX_sp3(ac) = YPO(ac) - YPO(cmb) + RX_snx(ac)
RY_sp3(ac) = XPO(ac) - XPO(cmb) + RY_snx(ac)
Thus, the total rotation of the individual AC orbits w.r.t. the IGS combined
orbit is the sum of the values in the two lines of Table 2.
Starting on 19-Aug-2012 (GPS Week 1702; mjd=56158), the AC TRF rotations are
daily values, instead of weekly ones, based on the combination of daily AC
SINEX files.
10. 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
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five parts. The first, 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 (table 1.1705.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1705.b).
The second part, 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 2.1705.[0-6]).
The third part, 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 3.1705.[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. The fourth part, Table 4, is a
weekly summary of the daily precise navigation summaries for centres
providing both orbit and clock solutions. It contains weekly station RMS
w.r.t. the initial coordinates for the Latitude, Longitude and Height
components for up to three IGS stations (table 4.1307). The fifth and final
part, Table 5, is similar to Table 4 and contains daily precise navigation
statistics (tables 5.1705.0-6).
In tables 1-3, the most important statistic which is meaningful for intra
centre/satellite analysis is labeled WRMS. It is a weighted RMS where
normalized weights are based on accuracy codes given in the SP3 files, and
should not be affected by downweighted/problem satellites when acknowledged
by individual centres in their SP3 file.
Table 1: Week 1705 summary. (Sep 09, 2012 - Sep 15, 2012)
Table 1.1705.a GPS week: 1705 MJD: 56179.000-56185.000
Mean and standard deviations of transformation parameters to the
combined IGS 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 263| -1 0 -1 -37 17 17 -.55 12 11 | -181 -299 30 75
| 0 0 1 16 32 28 .04 | 147 424
emr 78| 0 0 -1 -54 31 14 .25 19 18 | 607 -219 23 113
| 1 2 1 41 35 19 .02 | 830 866
esa 170| 1 0 0 -161 -18 -18 -.01 8 8 | -1164 1215 28 132
| 0 1 0 66 72 24 .03 | 685 1267
gfz 188| 1 1 0 81 45 19 -.46 11 10 | 133 75 24 95
| 0 1 1 36 58 12 .05 | 248 576
grg 120| 1 0 3 70 -44 28 .44 16 15 | 25 -18 26 158
| 0 1 1 34 39 2 .09 | 182 459
igr n/a| 0 0 0 -12 3 -11 -.21 5 5 | 2934 -212 22 74
| 0 0 1 16 26 13 .03 | 905 984
jpl 80| 0 1 -2 52 8 -7 .34 15 15 | 2043 -154 20 92
| 1 1 1 72 26 20 .04 | 926 996
mit 240| 0 -1 -1 -1 3 -10 -.23 8 8 | 60 1171 29 170
| 0 0 1 36 32 8 .03 | 797 2208
ngs 244| -2 0 7 203 -49 -6 .22 14 11 | -313 -1598 2051 3623
| 0 0 2 106 76 28 .03 | 709 2529
sio 271| 0 0 -5 -22 17 -17 -.33 20 20 | --- --- --- ---
| 1 0 1 26 38 17 .03 | --- ---
Table 1.1705.b GPS week : 1705 MJD: 56179.000-56185.000
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
------+------------------------------------+------------------------------------------
1 | 5 6 5 5 6 13 6 |
2 | 4 4 4 4 5 5 5 |
3 | 4 4 5 4 4 5 4 |
4 | 6 6 7 6 6 6 6 |
5 | 5 5 5 5 5 5 5 |
6 | 4 4 4 4 4 4 4 |
7 | 5 4 5 5 5 5 5 |
8 | 5 5 6 7 7 7 6 |
9 | 6 6 6 5 5 6 7 |
10 | 4 4 4 4 4 4 5 |
11 | 4 4 4 4 4 5 4 |
12 | 5 6 5 5 5 6 6 |
13 | 5 5 5 5 5 5 5 |
14 | 5 6 5 5 5 6 5 |
15 | 5 5 5 5 5 5 5 |
16 | 6 6 6 6 5 5 6 |
17 | 5 5 5 5 5 5 5 |
18 | 5 6 5 5 5 6 5 |
19 | 5 5 5 5 5 6 5 |
20 | 5 7 5 5 5 5 5 |
21 | 4 10 4 5 5 5 6 |
22 | 5 6 5 5 5 6 5 |
23 | 5 6 5 6 5 5 6 |
25 | 5 6 5 5 5 6 5 |
26 | 4 4 4 4 4 5 4 |
27 | 6 6 6 5 6 6 6 |
28 | 5 5 5 5 5 5 5 |
29 | 5 6 6 5 5 5 6 |
30 | 4 5 6 6 5 5 4 |
31 | 5 5 5 5 5 5 6 |
32 | 4 5 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS 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 2.1705.0 GPS week: 1705 Day: 0 MJD: 56179.000
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 263| -1 0 0 -48 5 2 -.50 10 10 | -196 -617 32 74
| 113 36 |
emr 79| 2 -2 -2 -52 81 -21 .25 18 18 | 2076 -1951 21 90
| 21 -43 |
esa 170| 1 0 0 -138 -16 25 .04 8 8 | -719 550 29 137
| 84 29 |
gfz 188| 0 2 0 78 69 10 -.44 11 10 | 302 213 26 105
| -4 8 |
grg 124| 2 0 0 5 -27 24 .32 16 15 | 86 -118 28 137
| 14 0 |
igr n/a| 0 0 0 -31 0 -9 -.17 4 4 | 4561 -2092 23 75
| -14 35 |
jpl 80| 0 0 -1 -64 8 -28 .38 15 14 | 3556 -1924 19 93
| 17 19 |
mit 240| 0 0 0 -10 -19 0 -.20 6 6 | -46 99 29 150
| -24 11 |
ngs 245| -4 -1 5 261 -51 -36 .19 13 11 | 80 -1124 1715 3442
| -107 15 |
sio 277| 0 -1 -3 -34 -17 10 -.31 20 20 | --- --- --- ---
| -40 -10 |
Table 2.1705.1 GPS week: 1705 Day: 1 MJD: 56180.000
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 263| -1 0 0 -22 -9 43 -.50 12 12 | 11 -761 30 79
| 72 83 |
emr 80| 0 -2 0 -6 39 6 .25 18 17 | 38 -450 18 89
| -19 -18 |
esa 170| 0 0 0 -97 -154 -31 -.00 10 9 | -39 -589 32 121
| 48 81 |
gfz 191| 2 1 0 60 129 9 -.44 12 11 | -63 619 26 96
| 9 15 |
grg 122| 0 0 3 62 -67 23 .39 13 13 | 195 -463 31 170
| -16 31 |
igr n/a| 0 0 1 -4 -20 3 -.18 6 6 | 2533 -617 22 85
| -2 32 |
jpl 80| 0 1 -2 60 -8 22 .39 15 14 | 1726 -633 24 92
| -12 5 |
mit 240| 0 0 0 -23 49 -10 -.22 7 7 | -916 2383 29 142
| -3 4 |
ngs 245| -4 -1 11 395 -98 17 .19 16 13 | 663 -3502 1685 3706
| -117 46 |
sio 268| 0 0 -2 0 50 -3 -.33 20 21 | --- --- --- ---
| -55 -27 |
Table 2.1705.2 GPS week: 1705 Day: 2 MJD: 56181.000
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 263| -1 0 0 -50 35 25 -.53 11 11 | -84 -554 35 71
| 124 18 |
emr 80| 1 0 0 -57 47 12 .22 18 18 | -258 -339 19 86
| 22 -22 |
esa 170| 1 -1 -2 -290 24 -38 -.00 9 8 | -1665 1042 37 123
| 131 33 |
gfz 191| 2 2 -3 142 28 27 -.48 12 12 | 253 -415 24 92
| -24 30 |
grg 124| 1 0 3 86 -45 32 .36 16 15 | -4 -125 28 173
| -13 -4 |
igr n/a| 0 0 0 -25 12 -2 -.21 5 5 | 2542 -582 22 88
| 6 34 |
jpl 80| -2 1 -1 43 13 -7 .36 15 14 | 1693 -711 23 85
| 0 28 |
mit 240| 0 0 -1 21 -9 -8 -.22 8 7 | -336 512 32 152
| -12 -3 |
ngs 247| -2 -1 9 211 -63 25 .24 13 10 | -108 -600 2265 3504
| -42 42 |
sio 273| 0 0 -5 -5 5 -19 -.36 19 19 | --- --- --- ---
| -46 -29 |
Table 2.1705.3 GPS week: 1705 Day: 3 MJD: 56182.000
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 263| 0 0 -1 -28 -4 57 -.54 11 10 | -341 355 36 84
| 70 49 |
emr 78| 0 0 -1 -22 4 11 .23 18 18 | -120 653 32 95
| 20 -21 |
esa 170| 2 -1 -1 -158 39 -21 .00 7 7 | -2180 3484 31 123
| 89 -8 |
gfz 188| 1 1 0 44 76 27 -.42 11 10 | 121 645 24 95
| -14 26 |
grg 121| 1 1 4 60 -64 29 .44 16 15 | -207 722 25 162
| -16 3 |
igr n/a| 0 0 0 3 -13 -6 -.21 4 4 | 2037 686 22 64
| -7 27 |
jpl 80| -1 0 -2 132 -4 3 .33 15 15 | 964 793 21 99
| -31 28 |
mit 240| 0 0 -3 -41 -27 -26 -.24 8 8 | -490 1254 28 176
| 0 -3 |
ngs 245| -3 1 8 199 -69 17 .24 13 10 | -65 -593 2679 4108
| -133 122 |
sio 270| 0 0 -6 -66 -9 -21 -.37 19 21 | --- --- --- ---
| -37 -17 |
Table 2.1705.4 GPS week: 1705 Day: 4 MJD: 56183.000
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 263| 0 0 -2 -25 -3 -15 -.57 13 11 | -42 -354 36 87
| 135 32 |
emr 78| 1 1 -2 -51 -18 13 .25 20 18 | 653 -146 41 217
| 24 -14 |
esa 170| 1 -2 0 -204 1 -41 -.03 7 7 | -973 1088 36 149
| 106 23 |
gfz 189| 1 1 0 82 68 36 -.45 11 11 | 505 -939 25 99
| -13 63 |
grg 118| 2 2 3 67 -52 29 .50 15 14 | 301 -610 26 140
| -8 -14 |
igr n/a| 0 0 0 -13 -9 -8 -.20 4 4 | 2410 185 26 79
| -4 13 |
jpl 80| -2 4 -3 124 26 5 .27 17 16 | 1442 213 20 95
| -18 21 |
mit 240| 0 -1 -2 53 45 -7 -.22 7 7 | 1335 5385 34 204
| -15 -27 |
ngs 243| -2 0 6 83 -161 -3 .23 12 8 | -1236 -6275 2053 3455
| -69 101 |
sio 269| 1 0 -7 11 54 -21 -.37 20 21 | --- --- --- ---
| -72 -53 |
Table 2.1705.5 GPS week: 1705 Day: 5 MJD: 56184.000
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 263| -1 0 -2 -22 16 24 -.59 12 10 | -257 214 24 68
| 60 10 |
emr 77| 1 2 -1 -52 4 35 .28 20 19 | 639 462 19 116
| -6 -6 |
esa 170| 1 0 0 -127 48 0 -.02 8 7 | -1241 910 21 153
| 55 -14 |
gfz 187| 0 0 0 43 -24 20 -.48 11 10 | -250 363 22 87
| -11 42 |
grg 116| 0 0 5 114 -88 28 .54 17 16 | -36 130 30 182
| -48 -20 |
igr n/a| 0 0 -1 9 -2 -37 -.24 5 5 | 2636 678 21 70
| -50 21 |
jpl 80| 1 1 -4 85 -29 -38 .32 17 17 | 1845 861 20 90
| -54 42 |
mit 240| 0 -1 -3 -39 -23 -12 -.28 11 10 | 927 -1532 30 192
| -10 16 |
ngs 243| -2 0 7 186 31 -44 .25 18 12 | -1288 1511 2149 3370
| -132 36 |
sio 270| 0 0 -5 -21 -26 -46 -.30 21 19 | --- --- --- ---
| -76 4 |
Table 2.1705.6 GPS week: 1705 Day: 6 MJD: 56185.000
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 263| -1 0 -4 -63 81 -17 -.61 11 11 | -364 -380 19 68
| 121 -1 |
emr 80| 0 4 -2 -139 62 39 .26 18 18 | 1222 238 16 101
| 80 -22 |
esa 170| 1 0 0 -116 -74 -23 -.04 8 8 | -1332 2024 16 123
| 34 66 |
gfz 184| 0 0 0 115 -31 3 -.55 11 11 | 69 39 22 96
| -26 24 |
grg 119| 1 -1 5 94 33 28 .56 16 15 | -158 337 20 144
| -49 -54 |
igr n/a| 0 -2 -1 -28 58 -19 -.23 5 5 | 3824 256 19 63
| -34 24 |
jpl 80| 0 0 -1 -16 52 -6 .32 15 15 | 3078 320 19 95
| -9 21 |
mit 240| 0 -1 -2 30 8 -6 -.24 10 9 | -50 100 23 178
| -30 28 |
ngs 243| -1 -1 5 88 66 -25 .19 15 13 | -241 -608 1814 3779
| -143 -1 |
sio 271| -1 0 -6 -35 66 -20 -.31 21 19 | --- --- --- ---
| -66 -25 |
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 IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS 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 IGS 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 3.1705.0 GPS week: 1705 Day: 0 MJD: 56179.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 21 10 8 14 4 10 9 13 17 4 | 115 121 127 118 130 122 122 122 124 124 123
2E | 8 14 8 10 14 4 16 5 12 14 4 | 37 37 37 34 38 36 38 37 37 35 36
3 | 9 11 6 9 19 4 10 5 11 22 4 | 18 18 17 23 24 14 18 16 17 20 17
4E | 13 20 10 8 20 3 15 8 19 15 5 | 28 45 33 29 40 31 43 32 38 36 34
5 | 12 19 11 11 15 4 15 8 14 18 5 | 23 30 25 24 29 22 29 23 26 20 23
6 | 9 11 7 7 18 4 9 4 12 22 3 | 21 23 22 23 28 17 22 20 21 25 20
7E | 9 13 5 7 21 5 15 6 14 12 4 | 20 22 20 17 24 20 25 19 31 25 19
8E | 12 16 8 10 17 5 12 8 20 16 5 | 29 43 31 31 36 32 40 32 43 34 33
9E | 13 17 9 10 19 5 19 9 18 20 5 | 20 25 21 22 26 21 27 23 27 23 21
10 | 7 11 7 11 15 4 10 5 11 15 3 | 24 25 30 29 35 25 26 25 28 28 27
11E | 11 14 9 8 13 3 11 7 9 13 4 | 28 28 29 28 31 28 28 28 32 30 28
12 | 9 22 10 12 15 6 17 7 11 23 5 | 22 27 25 28 26 20 26 21 21 24 22
13 | 7 16 7 11 18 5 13 6 10 28 4 | 19 32 24 24 36 19 31 19 28 24 23
14 | 9 18 8 12 12 4 16 6 14 31 4 | 18 27 25 25 31 22 28 22 27 22 23
15 | 9 19 7 11 10 4 19 5 9 16 4 | 23 27 24 27 25 21 25 22 23 18 22
16 | 11 20 9 18 15 4 19 7 14 23 5 | 20 26 21 32 27 21 28 20 24 21 21
17 | 11 15 9 12 18 5 15 6 14 32 4 | 21 31 25 22 31 23 32 24 33 26 25
18 | 7 23 7 14 12 4 17 5 11 22 5 | 23 42 30 23 35 26 38 28 29 26 29
19 | 11 18 8 12 20 4 16 6 11 28 5 | 24 30 17 16 23 18 28 19 27 26 18
20 | 13 18 8 15 14 4 16 5 11 25 4 | 26 32 27 32 35 27 33 27 31 25 28
21E | 7 16 8 11 12 5 14 4 14 10 4 | 36 40 42 36 45 38 42 38 44 37 39
22 | 7 17 6 13 12 3 15 6 12 22 4 | 24 35 30 26 36 25 35 25 29 24 27
23 | 9 22 8 15 16 4 17 4 9 25 5 | 24 32 24 28 32 23 30 22 29 25 25
25 | 13 28 9 6 16 4 13 6 10 18 5 | 28 28 30 25 37 25 36 25 23 26 26
26 | 7 12 8 7 12 5 9 6 6 16 3 | 20 19 22 22 25 19 19 20 25 23 20
27E | 11 15 10 13 19 6 17 10 14 14 5 | 16 26 20 21 27 19 26 20 27 24 20
28 | 9 16 9 12 15 3 15 5 13 24 4 | 24 30 32 32 35 28 32 27 28 27 29
29 | 16 23 10 10 13 6 18 10 11 21 5 | 22 42 30 25 36 27 37 27 36 25 30
30 | 11 14 8 10 15 5 7 5 13 11 4 | 18 20 20 19 24 19 15 16 22 12 18
31E | 14 18 6 11 14 5 14 7 14 12 4 | 24 30 22 27 28 26 30 30 30 33 26
32 | 13 17 6 12 14 5 9 5 9 20 4 | 26 28 27 32 35 27 28 29 32 31 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 8 11 16 4 15 6 13 20 |T 26 32 29 29 34 27 32 27 32 29 28
WRMS | 10 18 8 10 15 4 14 6 11 20 |NE 22 28 25 25 30 22 28 22 26 23 23
MEDI | 9 17 8 11 15 4 15 6 12 20 |MD 23 30 25 26 31 23 29 24 28 25 25
Table 3.1705.1 GPS week: 1705 Day: 1 MJD: 56180.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 22 12 13 12 7 11 8 13 17 5 | 93 94 105 96 106 100 100 98 105 97 100
2E | 8 11 4 13 10 4 15 4 16 12 4 | 26 30 30 31 30 28 30 30 34 32 29
3 | 12 10 6 8 15 7 7 7 13 22 4 | 10 15 12 12 17 12 17 12 18 20 13
4E | 17 18 8 11 16 8 15 8 22 16 5 | 30 43 30 27 35 28 39 27 37 32 31
5 | 13 15 13 9 12 6 15 7 17 18 5 | 15 29 20 18 29 18 29 20 27 18 21
6 | 11 10 8 8 14 6 7 6 16 20 4 | 12 20 17 13 20 13 20 13 20 24 16
7E | 7 12 8 7 12 8 14 6 14 14 4 | 10 20 16 10 17 15 19 14 25 21 15
8E | 16 23 8 12 12 5 11 6 26 18 5 | 26 47 32 29 35 30 37 29 44 31 32
9E | 18 15 10 11 14 6 15 10 21 19 5 | 17 25 24 20 21 23 26 24 28 23 21
10 | 8 10 6 10 13 5 9 6 8 13 4 | 14 24 16 19 24 17 21 18 24 23 19
11E | 8 12 6 8 10 4 9 4 17 12 3 | 21 24 24 26 27 22 23 20 25 21 23
12 | 11 21 11 12 13 6 15 7 15 24 5 | 17 27 21 20 21 17 25 17 24 19 19
13 | 8 16 8 12 14 5 16 7 15 28 5 | 11 28 19 16 30 16 29 14 19 21 19
14 | 9 19 9 12 12 5 17 8 11 29 5 | 13 26 22 18 27 15 26 14 21 21 18
15 | 11 19 9 9 14 5 17 6 14 20 5 | 16 24 20 18 18 18 23 18 19 16 17
16 | 12 19 10 14 12 5 17 8 17 24 5 | 17 27 20 22 23 19 26 17 22 19 20
17 | 9 14 8 12 14 5 19 6 16 29 5 | 16 30 24 19 30 21 30 20 30 17 23
18 | 10 24 11 14 11 5 18 6 17 24 6 | 18 39 30 16 34 24 40 25 26 25 27
19 | 13 16 10 10 16 5 14 8 15 26 5 | 15 23 13 11 21 14 23 15 22 22 14
20 | 14 18 7 24 12 6 18 8 15 20 6 | 15 24 20 26 25 18 26 18 24 16 19
21E | 12 37 28 16 18 7 18 7 14 15 9 | 21 59 40 24 34 26 31 25 35 28 29
22 | 10 20 9 11 13 7 17 6 15 25 5 | 17 36 27 15 35 21 34 24 26 25 25
23 | 10 20 10 17 13 4 19 6 14 25 6 | 15 26 21 21 24 17 26 15 18 21 18
25 | 10 27 5 8 14 4 13 6 12 15 5 | 19 27 22 15 28 18 32 17 22 22 20
26 | 8 9 9 8 10 4 11 7 16 17 4 | 14 20 19 17 19 18 21 16 21 21 18
27E | 14 14 10 11 13 7 15 11 17 14 5 | 10 25 21 16 19 21 25 22 27 23 19
28 | 10 14 9 12 13 4 17 5 19 23 5 | 19 31 27 28 30 25 30 24 30 22 27
29 | 21 19 11 13 14 8 16 9 16 21 6 | 23 37 28 26 35 25 34 27 39 23 29
X30 | 12 11 9 11 13 8 --- 7 17 --- 5 | 20 23 18 19 21 21 --- 20 28 --- 20
31E | 8 18 7 11 16 5 13 7 13 9 5 | 19 29 26 23 27 23 25 23 30 25 24
32 | 12 17 5 12 12 7 10 6 8 19 4 | 25 26 26 25 28 23 27 24 25 28 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 18 10 12 13 6 15 7 16 20 |T 19 30 25 22 28 22 29 22 28 25 24
WRMS | 12 17 9 11 13 6 14 7 13 21 |NE 16 26 21 18 25 18 26 18 24 21 20
MEDI | 11 17 9 11 13 5 15 7 15 19 |MD 17 27 22 19 27 21 26 20 25 22 20
Table 3.1705.2 GPS week: 1705 Day: 2 MJD: 56181.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 12 20 10 11 16 6 9 8 14 19 5 | 84 85 88 84 90 87 86 85 84 82 85
2E | 8 14 7 8 16 4 14 7 9 14 4 | 35 37 37 37 37 37 37 39 38 40 37
3 | 7 12 7 13 15 5 10 9 16 19 4 | 11 15 15 17 17 10 15 15 17 20 12
4E | 17 19 12 9 23 7 17 11 23 15 6 | 30 42 33 32 43 31 41 35 37 35 34
5 | 10 18 10 11 14 4 14 6 11 17 4 | 19 30 23 21 31 22 29 21 25 20 23
6 | 7 11 6 10 17 4 8 7 15 19 4 | 12 21 19 16 20 13 20 15 19 24 15
7E | 9 15 5 8 18 4 16 10 12 15 4 | 13 21 18 13 17 15 20 21 23 23 16
8E | 15 23 7 14 19 7 11 9 18 16 5 | 27 50 34 29 39 31 39 32 41 33 34
9E | 15 16 11 14 11 4 16 11 19 18 5 | 15 23 20 20 20 17 23 23 23 21 17
10 | 6 12 8 9 17 6 11 8 6 15 4 | 22 26 25 25 32 24 28 25 32 29 26
11E | 8 11 7 9 14 4 11 6 11 9 3 | 25 24 26 22 25 23 25 22 31 25 23
12 | 15 19 7 11 17 5 16 5 8 22 4 | 24 26 18 24 25 20 25 19 20 20 19
13 | 7 18 7 12 17 4 15 9 10 27 4 | 16 29 20 20 32 18 28 19 29 22 21
14 | 10 18 7 12 13 5 14 7 9 26 4 | 14 27 23 22 28 18 25 18 23 20 20
15 | 12 21 12 11 12 4 19 7 12 15 5 | 19 25 24 18 23 18 24 18 22 18 18
16 | 9 21 10 18 14 4 19 9 15 26 6 | 14 24 23 25 21 16 24 13 20 20 17
17 | 11 16 9 10 17 5 15 6 15 25 4 | 20 32 26 21 33 25 35 25 37 19 27
18 | 9 18 6 13 14 3 12 6 15 23 4 | 20 37 28 17 33 24 36 25 32 24 26
19 | 9 19 9 17 17 5 15 7 9 24 5 | 19 29 19 12 24 17 27 18 23 22 17
20 | 12 18 6 11 14 3 17 6 9 18 4 | 17 25 23 21 30 21 27 20 28 17 21
21E | 9 13 8 10 14 9 13 5 12 10 4 | 29 38 34 30 36 33 36 33 38 32 33
22 | 10 19 6 12 13 5 15 8 12 21 4 | 21 35 28 19 36 24 35 25 30 26 26
23 | 9 21 10 14 13 3 18 8 12 26 5 | 17 27 18 22 24 18 24 18 26 21 18
25 | 10 29 7 8 15 5 13 6 12 14 5 | 24 29 23 23 35 22 33 23 21 23 23
26 | 6 13 8 9 13 4 11 7 10 16 4 | 14 19 18 16 22 17 18 19 19 22 17
27E | 17 15 12 15 16 5 17 11 18 15 5 | 12 26 20 19 25 20 25 23 27 28 19
28 | 9 17 11 13 15 4 16 7 11 25 5 | 16 28 30 29 32 23 30 22 22 19 25
29 | 17 21 9 10 17 5 18 7 16 21 5 | 18 36 27 22 31 24 31 26 34 25 27
X30 | 13 16 10 10 16 8 --- 8 18 --- 5 | 16 19 19 19 18 18 --- 16 27 --- 16
31E | 11 17 8 11 15 4 16 9 14 12 5 | 13 23 20 17 24 16 20 17 24 19 17
32 | 14 18 7 7 16 5 10 5 8 20 4 | 20 20 20 22 27 20 22 18 22 20 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 9 12 15 5 15 8 13 19 |T 21 29 25 23 30 23 29 24 28 25 24
WRMS | 11 18 8 12 15 5 14 7 10 19 |NE 17 26 22 20 27 19 26 19 25 21 20
MEDI | 10 18 8 11 15 5 15 7 12 18 |MD 19 27 23 21 28 20 27 21 26 22 21
Table 3.1705.3 GPS week: 1705 Day: 3 MJD: 56182.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 15 19 9 12 16 4 13 9 13 21 5 | 102 103 109 100 113 105 105 106 107 105 105
2E | 12 15 5 7 16 2 17 6 10 13 4 | 37 37 38 32 41 36 37 36 40 33 36
3 | 7 11 5 8 19 4 8 7 11 20 4 | 13 18 14 15 18 12 18 17 17 19 15
4E | 23 23 8 11 18 7 18 8 18 15 5 | 27 46 33 26 39 30 42 32 35 32 32
5 | 9 17 9 11 16 4 16 6 10 16 4 | 20 28 22 18 32 20 29 22 23 18 22
6 | 7 12 4 6 19 4 8 7 12 19 3 | 16 24 18 18 21 16 22 21 22 25 19
7E | 9 18 7 8 20 7 13 8 11 13 4 | 13 24 16 12 18 15 22 20 23 21 16
8E | 13 28 6 11 20 7 13 10 28 14 6 | 27 52 35 29 41 32 40 34 39 32 35
9E | 14 16 10 9 13 5 16 10 16 15 5 | 18 26 19 19 20 21 26 27 26 25 20
10 | 9 11 5 10 15 4 10 6 11 15 3 | 21 26 26 25 34 24 28 23 27 27 26
11E | 6 12 6 9 13 4 12 8 13 9 4 | 25 26 26 28 31 26 27 24 32 27 26
12 | 10 18 9 12 15 5 17 7 10 23 5 | 20 27 23 27 25 20 26 23 20 21 22
13 | 8 16 7 12 18 4 15 8 13 27 4 | 16 30 24 24 35 18 30 19 25 18 23
14 | 8 18 6 11 14 4 16 6 10 25 4 | 16 27 21 22 29 17 28 19 25 21 20
15 | 7 20 8 11 12 6 17 8 11 16 4 | 21 28 20 22 27 18 26 22 21 19 20
16 | 11 20 8 17 14 4 18 12 13 24 5 | 21 27 20 30 27 21 27 25 24 20 23
17 | 13 14 8 12 16 3 16 9 12 24 4 | 22 32 28 24 31 26 34 29 33 19 28
18 | 9 20 6 12 11 4 18 8 10 20 4 | 21 39 28 22 34 25 38 27 32 23 28
19 | 9 19 10 10 19 4 15 9 13 24 5 | 20 28 17 16 23 18 27 22 26 22 19
20 | 10 19 5 11 13 3 18 7 9 16 4 | 19 27 21 21 29 20 27 20 23 14 21
21E | 7 21 8 10 20 5 14 8 13 11 5 | 32 39 35 32 46 33 39 35 43 33 36
22 | 11 20 6 12 15 3 20 5 10 22 5 | 21 35 27 26 36 24 35 25 30 25 27
23 | 10 22 8 14 15 3 19 8 12 25 5 | 21 30 25 27 28 20 28 22 23 22 22
25 | 12 30 6 9 15 4 18 7 10 15 5 | 29 31 26 26 35 25 38 29 27 23 27
26 | 8 12 6 8 14 2 11 8 11 13 4 | 18 22 18 20 26 18 25 19 19 23 20
27E | 14 16 10 11 14 5 17 11 14 15 5 | 16 28 21 16 25 20 29 28 26 28 21
28 | 8 14 6 11 15 4 16 7 11 23 4 | 22 30 27 30 33 25 33 26 26 22 27
29 | 18 20 8 9 15 4 16 8 12 22 4 | 27 42 32 29 37 31 39 33 40 30 33
X30 | 11 14 6 12 20 9 --- 10 17 --- 5 | 21 23 23 23 24 23 --- 26 29 --- 23
31E | 14 17 7 8 14 5 15 9 10 11 4 | 19 24 20 18 26 21 25 23 25 23 21
32 | 11 15 5 7 15 4 9 7 7 19 3 | 24 27 26 30 31 25 26 26 28 28 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 7 11 16 4 15 8 13 19 |T 24 32 27 26 32 25 32 27 30 26 27
WRMS | 10 18 7 10 15 4 15 8 10 21 |NE 20 28 23 23 29 21 29 23 25 21 23
MEDI | 10 18 7 11 15 4 16 8 11 16 |MD 21 28 24 24 31 21 28 25 26 23 23
Table 3.1705.4 GPS week: 1705 Day: 4 MJD: 56183.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 37 29 11 11 16 4 19 9 15 22 6 | 96 98 103 95 99 99 98 99 100 97 99
2E | 10 17 7 10 18 4 18 6 12 22 4 | 48 51 48 49 55 47 52 50 50 55 49
3 | 8 13 4 10 17 5 12 5 11 19 3 | 13 18 12 18 19 13 20 15 20 19 15
4E | 23 25 6 10 17 6 19 7 22 14 6 | 51 49 41 42 46 41 47 43 45 41 43
5 | 7 18 7 11 15 5 15 8 9 18 4 | 16 30 21 22 31 20 27 22 27 19 23
6 | 7 15 5 9 13 4 11 4 11 19 3 | 14 24 17 18 22 16 23 17 23 24 18
7E | 9 13 7 8 19 5 18 8 13 13 4 | 14 22 15 12 21 16 22 17 24 20 16
8E | 17 33 7 11 21 6 16 8 22 16 6 | 27 56 32 28 43 31 38 32 40 31 34
9E | 15 16 10 12 16 4 18 10 16 20 5 | 19 27 22 21 25 23 27 25 32 26 22
10 | 10 11 5 12 15 3 11 6 6 18 3 | 23 28 29 30 33 28 25 27 32 28 28
11E | 9 13 7 9 15 4 13 5 10 13 4 | 29 29 30 27 30 28 31 28 26 26 27
12 | 10 21 8 12 14 6 17 5 12 23 4 | 22 30 23 23 26 23 28 24 28 22 24
13 | 9 16 8 12 14 3 16 9 10 27 4 | 17 32 20 21 36 19 32 20 23 18 22
14 | 10 21 6 11 12 4 20 6 8 27 4 | 15 27 22 20 29 17 28 19 23 22 20
15 | 12 20 7 12 12 4 21 6 10 19 4 | 18 29 18 24 29 21 25 19 27 21 21
16 | 11 22 8 16 11 4 20 7 11 27 5 | 16 27 18 25 24 20 26 20 26 25 20
17 | 16 18 9 10 16 3 18 6 11 24 4 | 25 29 24 22 31 24 34 24 32 15 25
18 | 10 25 6 13 12 4 20 8 11 21 5 | 20 41 27 21 35 25 39 27 28 26 28
19 | 9 18 9 16 17 4 17 5 10 25 5 | 18 26 16 17 22 16 25 16 21 19 16
20 | 10 17 6 9 13 3 17 7 12 17 4 | 16 26 21 18 29 20 28 18 28 19 21
21E | 10 15 6 11 20 5 17 7 12 11 4 | 29 38 35 29 47 32 37 33 37 30 34
22 | 9 22 6 11 11 3 20 6 8 20 4 | 18 35 25 22 36 23 35 25 29 27 26
23 | 9 18 8 15 12 3 18 7 10 23 4 | 16 27 19 21 28 18 27 16 22 19 19
25 | 11 28 6 9 14 5 13 6 10 15 4 | 26 27 24 20 35 26 34 25 31 20 25
26 | 11 14 4 8 12 4 11 7 9 15 3 | 14 26 19 19 26 19 19 19 22 23 20
27E | 13 17 10 15 19 4 15 10 15 17 5 | 16 31 22 22 31 23 27 24 31 26 23
28 | 11 16 8 12 14 5 17 8 8 25 4 | 19 32 25 28 34 25 31 26 27 25 26
29 | 12 21 8 9 11 5 19 7 12 24 4 | 22 34 23 19 31 21 31 22 33 17 24
X30 | 15 16 8 10 17 4 --- 5 19 --- 5 | 17 21 17 20 19 19 --- 21 30 --- 20
31E | 11 19 6 10 15 4 17 10 10 13 4 | 14 25 19 19 28 18 26 22 28 24 21
32 | 13 16 6 7 17 5 9 6 6 20 3 | 26 24 25 25 32 26 26 24 30 30 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 20 7 11 15 4 17 7 12 20 |T 23 32 26 25 33 25 32 26 31 27 26
WRMS | 11 18 7 11 14 4 16 7 8 21 |NE 18 28 21 21 28 20 28 21 26 21 22
MEDI | 10 18 7 11 15 4 17 7 11 19 |MD 18 29 22 22 31 23 28 24 28 24 23
Table 3.1705.5 GPS week: 1705 Day: 5 MJD: 56184.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 22 34 21 12 37 12 20 17 66 23 12 | 117 134 137 131 133 127 131 122 142 130 129
2E | 10 16 5 9 16 4 15 11 12 15 4 | 39 45 43 40 48 41 44 45 42 43 42
3 | 7 16 5 10 18 5 10 10 12 18 4 | 13 21 15 18 17 13 21 21 19 23 16
4E | 26 23 7 9 18 6 18 9 21 21 5 | 50 52 45 44 52 43 51 44 50 54 45
5 | 6 18 7 12 16 3 17 11 14 18 5 | 16 28 21 20 32 19 29 23 26 21 21
6 | 8 16 5 7 15 3 9 8 12 18 4 | 18 25 21 21 24 19 24 22 24 27 21
7E | 10 13 5 10 18 7 15 11 13 10 4 | 14 23 16 14 20 16 22 23 24 21 17
8E | 17 30 8 14 17 7 15 13 20 18 6 | 26 55 35 31 43 32 42 36 42 32 36
9E | 12 16 10 16 16 7 14 14 18 21 6 | 18 23 16 22 23 20 23 30 27 24 19
10 | 8 10 5 9 19 4 10 9 9 17 4 | 21 28 28 26 30 25 28 30 28 30 27
11E | 9 10 7 10 15 3 17 11 15 15 4 | 26 28 26 24 30 22 29 26 25 24 24
12 | 10 21 11 11 17 5 21 9 9 25 5 | 20 26 22 22 27 19 26 23 22 18 20
13 | 7 17 7 12 16 3 18 11 14 28 5 | 13 29 19 18 36 14 30 18 20 17 20
14 | 13 22 7 12 13 5 23 9 13 28 5 | 13 28 21 21 30 17 29 23 26 20 20
15 | 11 19 6 12 14 8 22 9 12 23 5 | 16 26 20 23 24 17 27 20 23 18 19
16 | 10 21 6 14 11 5 17 10 9 22 5 | 18 28 20 25 26 21 28 24 25 24 22
17 | 14 17 9 10 17 5 14 11 13 27 5 | 16 31 26 25 32 22 33 25 33 14 26
18 | 8 24 6 12 13 5 21 12 10 20 5 | 18 38 26 22 36 25 39 30 31 20 28
19 | 8 19 7 13 17 4 22 10 15 26 5 | 16 28 16 15 25 15 30 21 18 19 17
20 | 10 17 5 7 15 6 18 10 15 21 4 | 15 24 18 14 28 16 27 19 26 14 18
21E | 8 17 7 8 24 4 17 12 10 18 5 | 39 45 41 37 49 38 44 39 46 35 40
22 | 9 23 6 11 15 4 22 11 9 21 5 | 19 36 28 24 40 25 37 28 33 26 28
23 | 8 20 5 11 12 4 18 10 14 26 5 | 15 25 17 17 25 13 24 17 18 18 16
25 | 12 34 8 9 15 4 17 9 13 18 6 | 24 32 26 21 34 22 34 26 26 19 24
26 | 10 13 5 11 14 5 13 9 13 11 4 | 13 20 17 20 24 17 22 22 26 21 18
27E | 12 18 10 12 22 8 16 15 15 15 6 | 15 26 17 20 31 20 25 28 28 24 20
28 | 9 16 7 12 18 3 14 11 11 24 5 | 18 30 23 25 35 22 31 24 29 21 25
29 | 16 21 7 8 13 4 21 9 12 25 5 | 22 39 26 22 34 25 37 27 34 22 28
X30 | 10 18 5 5 19 7 --- 9 16 --- 5 | 20 24 20 22 24 21 --- 25 30 --- 22
31E | 11 17 6 10 14 5 17 13 13 16 5 | 24 33 26 29 36 29 34 36 33 31 30
32 | 13 16 6 7 17 6 9 11 11 20 4 | 20 20 17 19 23 15 18 19 17 18 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 20 8 11 17 5 17 11 18 21 |T 23 33 27 26 34 25 33 29 32 27 27
WRMS | 10 18 7 10 16 5 17 10 12 19 |NE 17 27 21 20 28 19 28 23 25 20 21
MEDI | 10 18 7 11 16 5 17 11 13 20 |MD 18 28 21 22 30 21 29 25 26 21 22
Table 3.1705.6 GPS week: 1705 Day: 6 MJD: 56185.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 20 12 14 16 9 13 13 16 13 5 | 113 118 118 116 118 115 114 112 116 117 114
2E | 10 14 8 11 17 5 14 10 18 18 5 | 51 52 54 52 57 52 54 57 57 52 54
3 | 10 15 6 9 16 5 11 9 10 23 4 | 16 24 20 20 24 17 22 17 20 28 18
4E | 16 23 7 10 18 6 17 10 26 23 6 | 66 77 71 67 71 67 75 73 70 71 71
5 | 12 19 10 10 15 5 15 10 12 20 5 | 23 36 29 28 42 26 35 25 34 26 29
6 | 9 17 6 7 17 4 11 7 10 20 4 | 18 29 26 21 29 21 26 21 23 30 22
7E | 10 15 5 11 13 4 16 11 10 10 4 | 15 21 17 16 25 17 23 21 28 21 18
8E | 16 26 9 13 15 6 16 14 16 14 6 | 30 52 35 31 48 34 41 37 46 34 37
9E | 13 17 12 9 23 5 16 14 25 17 6 | 21 26 20 23 30 20 27 27 28 28 21
10 | 8 11 5 12 16 4 12 10 13 16 4 | 27 32 33 34 43 30 33 28 35 34 32
11E | 10 9 7 9 16 5 8 9 16 10 4 | 30 34 33 31 39 30 35 28 34 30 31
12 | 11 20 12 15 17 5 15 8 24 27 6 | 25 30 28 33 29 26 28 28 31 28 26
13 | 10 16 6 14 16 3 15 11 14 29 5 | 18 33 23 27 37 22 31 25 25 24 24
14 | 12 19 8 9 12 5 20 8 16 27 5 | 15 29 24 22 31 20 30 22 29 23 23
15 | 11 20 7 13 12 5 17 11 13 22 5 | 21 29 23 28 31 23 26 27 30 26 23
16 | 11 20 9 13 14 5 20 9 10 25 5 | 21 30 24 29 29 22 28 22 23 21 23
17 | 10 15 9 11 15 5 14 10 13 26 5 | 20 33 27 29 35 26 36 27 35 22 29
18 | 10 28 8 11 14 4 14 8 11 20 5 | 24 43 30 26 41 29 40 33 34 27 32
19 | 10 21 10 10 10 5 16 9 11 28 5 | 21 34 18 16 28 20 32 19 26 24 20
20 | 13 19 6 12 13 4 15 9 16 24 5 | 20 29 24 21 32 23 28 23 27 19 23
21E | 11 16 8 10 31 7 14 9 13 12 5 | 48 56 52 48 74 52 60 54 59 51 55
22 | 11 19 8 11 14 5 18 7 12 20 5 | 26 44 31 27 46 30 41 32 36 32 33
23 | 10 19 6 16 12 4 17 10 14 25 5 | 18 28 20 26 29 18 24 21 23 19 20
25 | 8 21 7 9 14 6 13 10 11 19 4 | 25 27 29 31 37 30 38 32 32 28 30
26 | 12 13 4 10 15 4 10 10 9 11 4 | 18 23 21 26 34 21 23 22 25 24 23
27E | 12 16 11 7 23 6 16 14 18 19 6 | 17 27 20 21 31 20 28 29 30 31 22
28 | 12 16 7 12 11 5 15 9 11 25 4 | 23 32 30 33 38 27 34 29 26 28 30
29 | 16 25 9 14 15 4 18 13 14 26 6 | 29 43 30 28 35 29 39 36 38 34 33
30 | 9 15 7 9 17 8 11 8 9 19 4 | 19 25 19 20 25 17 18 20 23 20 20
31E | 11 19 6 11 14 6 21 11 21 14 6 | 24 30 26 23 34 26 30 26 34 28 27
32 | 11 14 7 9 14 6 10 8 13 19 4 | 19 21 17 23 29 19 22 17 24 20 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 8 11 16 5 15 10 15 21 |T 27 37 31 31 39 29 36 31 35 32 31
WRMS | 11 18 8 11 15 5 15 9 13 19 |NE 21 31 25 26 33 23 30 25 28 25 25
MEDI | 11 19 7 11 15 5 15 10 13 20 |MD 21 30 26 27 34 26 31 27 30 28 26
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1705 GPS week: 1705 MJD: 56179.0-56185.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 |U 6 7 18 |U 6 7 24 |U 26 25 56 |
emr | emr 2959 | 13 11 28 |U 17 16 50 | 31 29 67 |
esa | esa 2976 | 7 7 19 |U 6 9 29 | 24 24 53 |
gfz | gfz 2959 |U 8 7 21 |U 16 12 38 |U 22 18 56 |
grg | grg 2975 |U 10 10 23 |U 17 19 43 | 28 27 55 |
igr | igr 2973 | 7 7 20 | 6 8 27 | 25 24 55 |
igs | igs 2972 | 8 7 19 | 15 15 38 | 29 25 66 |
jpl | jpl 2891 | 10 9 24 |U 19 20 45 | 94 41 65 |
mit | mit 2976 | 9 8 19 |U 17 16 40 |U 30 28 64 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1705.0 GPS week: 1705 Day: 0 MJD: 56179.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 7 15 | 5 6 28 | 37 51 36 |
emr | emr 2960 | 10 10 18 | 13 10 31 | 38 55 33 |
esa | esa 2976 | 8 7 18 | 6 8 27 | 37 52 36 |
gfz | gfz 2960 | 8 7 14 | 16 11 37 | 12 12 25 |
grg | grg 2975 | 9 7 18 | 14 17 42 | 40 52 34 |
igr | igr 2974 | 8 6 17 | 5 7 24 | 37 52 35 |
igs | igs 2974 | 8 6 15 | 12 12 30 | 38 53 31 |
jpl | jpl 2960 | 9 8 17 | 17 12 39 | 39 54 34 |
mit | mit 2976 | 11 10 16 | 14 12 32 | 38 50 34 |
Table 5.1705.1 GPS week: 1705 Day: 1 MJD: 56180.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 6 20 | 7 8 22 | 7 6 15 |
emr | emr 2960 | 8 10 19 | 19 16 43 | 8 8 17 |
esa | esa 2976 | 6 6 19 | 6 9 27 | 6 7 17 |
gfz | gfz 2953 | 5 7 18 | 18 16 45 | 6 6 17 |
grg | grg 2976 | 8 9 18 | 17 18 46 | 9 10 20 |
igr | igr 2974 | 6 6 19 | 6 9 25 | 6 5 19 |
igs | igs 2976 | 5 6 17 | 17 11 41 | 7 7 18 |
jpl | jpl 2864 | 8 9 22 | 17 17 45 | 8 8 21 |
mit | mit 2976 | 6 7 19 | 18 15 40 | 7 8 19 |
Table 5.1705.2 GPS week: 1705 Day: 2 MJD: 56181.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 12 26 | 6 8 18 | 36 14 129 |
emr | emr 2960 | 10 12 31 | 16 8 31 | 37 16 149 |
esa | esa 2976 | 10 12 27 | 7 9 25 | 27 10 113 |
gfz | gfz 2960 | 10 11 30 | 16 12 33 | 31 15 135 |
grg | grg 2976 | 11 10 34 | 17 14 39 | 30 13 106 |
igr | igr 2972 | 9 11 29 | 6 9 23 | 30 11 120 |
igs | igs 2976 | 10 12 27 | 14 11 31 | 33 14 131 |
jpl | jpl 2864 | 11 11 23 | 22 25 47 | 37 36 145 |
mit | mit 2976 | 10 11 22 | 16 15 35 | 31 20 135 |
Table 5.1705.3 GPS week: 1705 Day: 3 MJD: 56182.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 18 | 5 8 21 | 15 16 27 |
emr | emr 2960 | 9 6 21 | 14 17 42 | 10 17 23 |
esa | esa 2976 | 6 7 19 | 5 9 27 | 14 15 30 |
gfz | gfz 2960 | 7 6 24 | 14 11 33 | 15 12 28 |
grg | grg 2976 | 8 11 26 | 16 18 39 | 26 26 22 |
igr | igr 2975 | 6 7 21 | 5 7 24 | 14 15 26 |
igs | igs 2976 | 6 6 19 | 13 13 37 | 14 14 27 |
jpl | jpl 2863 | 9 8 29 | 20 13 48 | 21 8 37 |
mit | mit 2976 | 7 7 22 | 15 16 38 | 17 21 36 |
Table 5.1705.4 GPS week: 1705 Day: 4 MJD: 56183.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 8 18 | 6 6 23 | 13 5 19 |
emr | emr 2957 | 25 22 45 | 21 24 108 | 32 16 42 |
esa | esa 2976 | 7 9 19 | 5 7 33 | 13 9 17 |
gfz | gfz 2961 | 10 8 21 | 17 11 39 | 14 8 18 |
grg | grg 2975 | 12 14 24 | 15 14 33 | 17 12 23 |
igr | igr 2971 | 8 9 20 | 5 6 26 | 14 7 20 |
igs | igs 2976 | 11 11 17 | 14 12 35 | 19 6 22 |
jpl | jpl 2864 | 14 13 19 | 18 18 41 | 10 13 20 |
mit | mit 2976 | 10 11 20 | 19 16 40 | 31 9 37 |
Table 5.1705.5 GPS week: 1705 Day: 5 MJD: 56184.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 20 | 8 8 28 | 64 69 137 |
emr | emr 2960 | 14 10 31 | 19 19 59 | 74 71 159 |
esa | esa 2976 | 10 7 21 | 8 10 32 | 61 66 121 |
gfz | gfz 2960 | 10 7 24 | 21 14 42 | 64 66 138 |
grg | grg 2975 | 8 8 21 | 19 17 50 | 55 69 133 |
igr | igr 2973 | 7 6 22 | 7 9 32 | 64 70 131 |
igs | igs 2970 | 10 6 21 | 18 13 42 | 65 69 136 |
jpl | jpl 2864 | 11 8 28 | 24 32 60 | 528 143 144 |
mit | mit 2976 | 10 6 20 | 22 15 49 | 68 74 142 |
Table 5.1705.6 GPS week: 1705 Day: 6 MJD: 56185.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 4 12 | 6 7 26 | 8 10 28 |
emr | emr 2960 | 15 8 33 | 14 19 35 | 19 15 43 |
esa | esa 2976 | 5 5 14 | 8 8 36 | 7 10 35 |
gfz | gfz 2960 | 5 4 15 | 14 11 36 | 11 9 34 |
grg | grg 2976 | 10 10 23 | 22 34 48 | 18 11 48 |
igr | igr 2972 | 5 4 13 | 8 8 35 | 9 7 31 |
igs | igs 2961 | 6 5 18 | 18 30 51 | 25 13 95 |
jpl | jpl 2960 | 12 6 26 | 19 21 35 | 18 28 56 |
mit | mit 2976 | 7 5 15 | 19 23 44 | 16 17 44 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1705 GPS week: 1705 MJD: 56179.500-56185.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -15 -99 -100 -22 1 | 10 22
| 27 28 107 47 9 | 2
emr uuuux | 38 -20 63 -22 23 | 39 46
| 11 37 86 76 12 | 7
esa uuuuu | -13 -78 98 157 7 | 18 30
| 32 25 55 50 7 | 3
gfz uuuuu | -13 12 -69 39 -3 | 18 28
| 18 16 56 37 6 | 1
grg uuuux | 25 20 -56 -103 58 | 0 41
| 26 16 45 71 71 | 10
igr xxxxx | -10 15 0 -15 5 | -4 20
| 10 10 68 48 6 | 2
irf xxxxx | 17 0 -6 -9 3 | -2 14
| 4 12 16 11 2 | 2
jpl uuuuu | -6 16 -18 5 5 | 51 55
| 14 20 52 55 13 | 1
mit uuuuu | 13 14 -14 -57 -3 | -1 14
| 19 13 32 37 5 | 3
ngs uuuuu | -35 107 -57 -131 4 | 11 20
| 44 28 66 148 4 | 2
sio xxxxx | 39 56 -127 -135 1 | 74 76
| 21 15 80 35 7 | 2
Table 7.1705.0 GPS week: 1705 Day: 0 MJD: 56179.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -25 -111 -7 -4 10 | 10 22
emr uuuux | 54 -19 -7 15 28 | 29 39
esa uuuuu | -18 -82 206 123 6 | 18 30
gfz uuuuu | 3 6 -45 16 1 | 20 29
grg uuuux | 11 -12 -86 -37 -44 | 4 30
igr xxxxx | -24 16 18 65 5 | -3 20
irf xxxxx | 11 2 -17 -2 1 | 1 13
jpl uuuuu | -8 -15 -66 26 13 | 52 55
mit uuuuu | 0 26 -52 -87 -3 | 5 14
ngs uuuuu | -4 109 -45 -28 2 | 14 22
sio xxxxx | 21 42 -134 -163 7 | 73 75
Table 7.1705.1 GPS week: 1705 Day: 1 MJD: 56180.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -61 -67 -30 54 6 | 10 22
emr uuuux | 40 24 -75 53 20 | 33 41
esa uuuuu | -59 -43 29 129 -1 | 17 29
gfz uuuuu | 7 -4 35 57 -2 | 19 28
grg uuuux | -9 21 27 -71 -11 | -3 35
igr xxxxx | -10 7 102 35 4 | -4 20
irf xxxxx | 22 5 14 -7 2 | -2 14
jpl uuuuu | 17 17 -34 38 11 | 51 55
mit uuuuu | 18 8 -7 -121 0 | 2 14
ngs xxxxx | -24 122 -12 68 1 | 13 22
sio xxxxx | 49 60 -14 -91 3 | 73 75
Table 7.1705.2 GPS week: 1705 Day: 2 MJD: 56181.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -2 -108 -171 -79 0 | 8 20
emr uuuux | 38 -6 36 -67 5 | 36 43
esa uuuuu | -17 -115 79 184 5 | 14 27
gfz uuuuu | -14 40 -120 105 -7 | 17 27
grg uuuux | 20 29 -50 -145 33 | -10 32
igr xxxxx | -18 10 -14 -26 7 | -7 20
irf xxxxx | 16 16 9 4 2 | -3 13
jpl uuuuu | -12 16 -12 29 6 | 50 53
mit uuuuu | 19 28 35 -36 -6 | 0 14
ngs uuuuu | -26 58 -50 -235 11 | 10 18
sio xxxxx | 45 62 -95 -100 -2 | 71 74
Table 7.1705.3 GPS week: 1705 Day: 3 MJD: 56182.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -32 -70 56 -13 7 | 8 20
emr uuuux | 38 -20 109 -31 12 | 38 44
esa uuuuu | 25 -89 91 118 19 | 15 27
gfz uuuuu | -9 14 -47 27 2 | 17 27
grg uuuux | 14 16 -35 -175 57 | -11 32
igr xxxxx | -10 7 46 -55 10 | -6 19
irf xxxxx | 17 0 -2 -26 2 | -4 13
jpl uuuuu | -11 31 -96 78 5 | 51 54
mit uuuuu | 20 0 -8 -67 -9 | -2 14
ngs uuuuu | -105 133 -75 -73 5 | 10 18
sio xxxxx | 34 37 -67 -127 13 | 72 74
Table 7.1705.4 GPS week: 1705 Day: 4 MJD: 56183.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -12 -125 -133 -73 -2 | 10 21
emr uuuux | 34 -14 118 -162 26 | 42 47
esa uuuuu | -3 -96 117 194 5 | 18 30
gfz uuuuu | -43 23 -119 12 -7 | 17 27
grg uuuux | 34 18 -56 -181 89 | -6 36
igr xxxxx | 7 14 19 -39 -4 | -4 19
irf xxxxx | 20 10 -2 -20 7 | -4 13
jpl uuuuu | -1 28 58 2 -19 | 52 56
mit uuuuu | 47 25 -58 -26 2 | -4 14
ngs uuuuu | -81 79 -56 -102 -1 | 10 19
sio xxxxx | 73 82 -130 -173 -3 | 75 77
Table 7.1705.5 GPS week: 1705 Day: 5 MJD: 56184.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 2 -74 -232 -42 0 | 13 23
emr uuuux | 18 -8 76 -15 29 | 45 51
esa uuuuu | 26 -69 67 107 14 | 20 32
gfz uuuuu | -30 -3 -108 -2 5 | 18 28
grg uuuux | 32 34 -112 5 144 | 4 48
igr xxxxx | -9 36 -90 -68 13 | -3 20
irf xxxxx | 12 -14 -34 -2 0 | -2 15
jpl uuuuu | -30 40 18 -70 21 | 51 55
mit uuuuu | -4 -4 -12 -13 -10 | -3 14
ngs uuuuu | -24 118 26 -164 9 | 11 20
sio xxxxx | 8 62 -252 -175 -2 | 76 78
Table 7.1705.6 GPS week: 1705 Day: 6 MJD: 56185.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 22 -137 -182 0 -17 | 13 23
emr uuuux | 43 -96 183 54 43 | 49 57
esa uuuuu | -45 -50 95 242 2 | 22 34
gfz uuuuu | -3 10 -79 60 -14 | 18 27
grg uuuux | 75 33 -78 -115 139 | 19 71
igr xxxxx | -3 18 -79 -17 0 | -2 21
irf xxxxx | 21 -16 -13 -12 3 | -2 14
jpl uuuuu | 0 -7 6 -67 -3 | 53 57
mit uuuuu | -7 14 1 -52 1 | -4 13
ngs uuuuu | 22 127 -185 -386 4 | 10 18
sio xxxxx | 46 50 -200 -116 -7 | 75 78
More information about the IGSREPORT
mailing list