[IGSREPORT-26991] Wk 2083 IGS Final Orbits
acc
acc at igs.org
Fri Dec 27 14:44:54 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2083 (Dec 08, 2019 - Dec 14, 2019)
Contacts: acc at igs.org
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 at each SP3 epoch. 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 with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations 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 over each daily arc. 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 10 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:
igs2083[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2083[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2083[0-6].cls IGS GPS clock combination summary report.
igs20837.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20837.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
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 | TIXI TIXI
0 | EMR | 18 18 GRAZ GRAZ
0 | ESA | OHI3 PTBB OHI3 PTBB
0 | GFZ | 18 18 BJNM GODE POHN BJNM GODE POHN
0 | GRG | 18 18 POHN
0 | JPL | 31
1 | COD | ASCG TIXI TLSE TIXI TLSE
1 | EMR | 18 GRAZ GRAZ
1 | ESA | 3 3 18 DAV1 PTBB SEYG TLSE DAV1 PTBB TLSE
1 | GFZ | 18 BJNM GODE POHN BJNM CHTI GODE POHN
1 | GRG | DAV1 MCM4 DAV1 MAW1 MCM4
1 | MIT | BJNM BJNM
2 | COD | TIXI SCOR TIXI
2 | EMR | GRAZ
2 | ESA | CHUR HOFN NYA1 PTBB SCOR ANKR CHUR PTBB
2 | GFZ | 16 ANKR FLRS POHN YAR2 FLRS GODE HOFN POHN SCOR YAR2
2 | GRG | CCJ2 HOFN SCOR CCJ2 HOFN
2 | JPL | NYA1
2 | MIT | CHUR
3 | COD | 2 21 2 21 ASCG CPVG GUAT REUN TIXI ASCG GUAT TIXI
3 | EMR | 21 21
3 | ESA | 18 18 HOFN PTBB REUN HOFN PTBB
3 | GFZ | BJNM GODE POHN SOFI BJNM GODE POHN SOFI
3 | GRG | 18 26 1 18 26 FAA1 HOFN MCM4 STJO CKIS CPVG HOFN
3 | JPL | DAEJ
3 | MIT | 18
4 | COD | 18 18 ASCG FLRS TIXI ASCG TIXI
4 | ESA | 18 18 PTBB PTBB
4 | GFZ | 21 21 BJNM BOR1 GLSV GODE POHN BJNM GLSV GODE POHN
4 | GRG | 18 1 14 18 FAA1
4 | JPL | FLRS
5 | COD | ASCG BRFT LAUT NAUR TIXI ASCG BRFT LAUT NAUR TIXI
5 | EMR | 6 6
5 | ESA | 18 PTBB REUN TLSE PTBB REUN TLSE
5 | GFZ | GODE POHN DGAR GODE POHN
5 | GRG | 18 18 DARW
5 | JPL | 6 6
5 | MIT | MTKA
6 | COD | 1 18 21 1 18 21 ASCG DAV1 LAUT NAUR TIXI ASCG DAV1
6 | COD | LAUT NAUR TIXI
6 | EMR | 18 21 PRDS
6 | ESA | 1 1 DAV1 NANO PTBB SGOC DAV1 PTBB SGOC
6 | GFZ | BJNM GODE POHN BJNM GODE NANO POHN
6 | GRG | CKIS DARW
5. 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 AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. 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
----+--------+---------------
0 | SIO | 4
2 | SIO | 4
3 | GRG | 26
3 | SIO | 4
4 | SIO | 4
6 | SIO | 4
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G04 | | | | | 4 | 4 | 4 |
PRN G26 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. 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.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ 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]
-------+-----+---------------------------------------------------
COD | 0 | 1.0 -.3 1.0 2 5 -7 -.60
EMR | 0 | -1.2 3.4 3.9 -42 -15 -12 -.18
ESA | 0 | .1 -.5 -.3 -4 13 50 -.44
GFZ | 0 | .5 .5 .9 37 13 37 -.45
GRG | 0 | -.8 2.3 1.3 26 17 94 -.08
JPL | 0 | 6.6 3.4 2.9 11 -14 17 -.54
MIT | 0 | .6 4.8 -.8 5 26 20 -.17
NGS | 0 | 2.4 4.6 -.9 48 -17 -2 -.17
SIO | 0 | .4 5.6 1.6 -9 -35 9 -.27
COD | 1 | .6 .4 .7 3 9 -7 -.49
EMR | 1 | 4.3 9.7 2.7 -40 19 -44 -.14
ESA | 1 | .1 .1 -.1 -7 -2 62 -.35
GFZ | 1 | .4 .9 -.0 40 0 22 -.20
GRG | 1 | -2.7 5.7 8.2 -3 2 86 -.11
JPL | 1 | 10.6 3.4 2.8 5 -7 9 -.37
MIT | 1 | 2.7 5.8 .8 8 7 7 -.24
NGS | 1 | -1.9 1.4 -1.1 -12 47 -25 -.30
SIO | 1 | 2.1 3.2 -5.4 21 -10 -7 -.15
COD | 2 | .9 -.6 .4 1 9 15 -.41
EMR | 2 | 3.0 4.4 2.9 -53 17 -57 .07
ESA | 2 | .1 .5 -.5 -5 10 68 -.28
GFZ | 2 | .4 1.1 -.2 34 9 22 -.33
GRG | 2 | -2.2 3.9 8.7 -6 8 80 -.13
JPL | 2 | 10.7 4.2 5.6 -9 -5 31 -.38
MIT | 2 | 5.5 3.8 -1.5 -21 37 -19 -.24
NGS | 2 | 3.8 .3 .4 13 15 -44 .03
SIO | 2 | 3.9 1.1 -.3 6 -13 6 -.21
COD | 3 | 1.2 -.7 1.0 -6 10 2 -.50
EMR | 3 | 1.3 6.1 .4 -63 17 -67 .15
ESA | 3 | .4 -.2 -.2 0 17 59 -.33
GFZ | 3 | .7 .4 -.0 41 1 54 -.22
GRG | 3 | -7.7 1.3 12.7 6 -1 95 -.13
JPL | 3 | 10.8 6.3 6.7 6 -2 4 -.43
MIT | 3 | .0 7.1 -.5 -22 51 10 -.20
NGS | 3 | -2.1 2.6 -1.8 15 15 -24 -.19
SIO | 3 | -3.6 2.2 15.3 10 -13 8 -.24
COD | 4 | .4 -.1 1.1 3 18 1 -.49
EMR | 4 | 5.0 2.4 5.1 -62 22 -76 .06
ESA | 4 | -.2 -.2 -.9 12 16 57 -.45
GFZ | 4 | .3 .9 .1 39 16 31 -.31
GRG | 4 | .6 3.6 -1.1 21 18 74 .05
JPL | 4 | -.3 4.1 .9 5 -1 21 -.15
MIT | 4 | 2.9 5.4 2.9 -10 26 -24 -.16
NGS | 4 | 1.9 2.8 2.5 9 -1 -26 -.07
SIO | 4 | 1.1 .8 12.0 -1 -9 -4 -.14
COD | 5 | .5 .1 1.3 5 16 3 -.62
EMR | 5 | 7.5 16.1 3.2 -42 9 -33 .02
ESA | 5 | -.5 .5 -.3 5 24 55 -.31
GFZ | 5 | .3 1.1 .7 44 10 41 -.37
GRG | 5 | .3 1.2 4.9 20 -6 93 -.04
JPL | 5 | 17.5 5.2 3.4 -3 -3 24 -.58
MIT | 5 | 1.8 6.7 5.8 -28 16 -11 -.26
NGS | 5 | 3.0 1.4 .9 10 -1 -12 -.19
SIO | 5 | .3 5.8 .7 -2 -6 12 -.30
COD | 6 | .8 .5 1.5 13 15 1 -.71
EMR | 6 | 2.0 17.3 11.4 -33 9 -1 -.15
ESA | 6 | .3 .3 -.3 10 8 75 -.37
GFZ | 6 | .3 1.2 .8 50 19 49 -.39
GRG | 6 | -.5 6.0 -1.1 23 -8 101 -.08
JPL | 6 | 12.2 3.1 6.2 1 -5 13 -.62
MIT | 6 | 1.7 7.4 5.6 -9 10 9 -.30
NGS | 6 | .4 4.9 2.9 29 -2 -2 -.19
SIO | 6 | 2.1 7.1 5.8 20 5 -1 -.18
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. 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; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
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
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven 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 1.2083.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2083.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 2.2083.[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 3.2083.[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 part,
Table 5, is similar to Table 4 and contains daily precise navigation
statistics (Tables 5.2083.0-6). The sixth part, Table 6, is a weekly
summary of daily ERP combination statistics. The seventh part, Table 7,
contains the daily ERP statistics. But this is not the IGS official ERP
combination products (which come from the accompanying SINEX combination)
but provided to check combination consistency, etc.
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 2083 summary. (Dec 08, 2019 - Dec 14, 2019)
Table 1.2083.a GPS week: 2083 MJD: 58825.000-58831.000
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 245| -1 0 0 17 4 21 -.03 8 8 | -460 -185 6 94
| 0 0 0 9 8 9 .02 | 69 208
emr 79| 0 2 2 -16 0 7 .16 13 13 | 142651 323 16 93
| 2 3 1 17 16 7 .02 | 378 1060
esa 150| 0 0 1 -14 -18 3 -.04 10 10 | 295 -1975 7 76
| 0 0 1 7 22 20 .02 | 561 825
gfz 178| 0 0 1 8 1 6 .12 10 10 | -154 -45 10 111
| 0 0 1 15 11 13 .03 | 373 370
grg 98| 0 0 -1 -21 -9 -2 -.14 16 10 | 146 -163 10 130
| 0 0 3 8 13 28 .04 | 219 397
igr n/a| 0 0 0 -12 1 -16 .04 4 4 | 5139 312 10 62
| 0 0 0 12 8 5 .01 | 358 974
jpl 80| 0 0 1 6 19 -19 .12 9 9 | 213509 160 7 67
| 2 1 1 11 18 14 .04 | 301 884
mit 349| 0 0 -5 -10 -6 12 -.09 14 13 | 3983 -406 83 1705
| 0 0 0 22 18 15 .01 | 3048 1284
ngs 201| 0 0 0 3 0 -9 -.04 8 7 | -465 -188 1008 2054
| 0 0 1 20 17 11 .02 | 83 224
sio 315| 1 -1 -3 7 0 -4 -.04 15 14 | --- --- --- ---
| 0 0 1 31 33 40 .06 | --- ---
Table 1.2083.b GPS week : 2083 MJD: 58825.000-58831.000
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 | 4 5 4 5 5 6 6 |
2 | 4 4 4 4 4 4 4 |
3 | 3 6 3 3 3 3 3 |
4 | 11 14 14 11 12 14 8 |
5 | 4 4 4 4 4 4 4 |
6 | 5 5 5 5 5 6 6 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 3 4 3 3 3 |
9 | 3 3 3 3 3 4 3 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 4 4 4 4 4 4 4 |
13 | 3 4 3 4 3 4 3 |
14 | 3 3 3 3 3 3 3 |
15 | 3 3 3 3 3 3 3 |
16 | 5 5 4 4 4 4 4 |
17 | 3 4 3 3 4 4 3 |
18 | 6 8 8 10 9 8 7 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 3 4 3 4 4 3 3 |
22 | 4 4 4 3 4 4 4 |
23 | 4 4 3 4 3 4 3 |
24 | 4 3 3 3 3 4 3 |
25 | 4 4 4 4 4 4 4 |
26 | 4 5 4 8 4 4 4 |
27 | 4 4 4 4 3 4 4 |
28 | 4 3 3 4 3 4 4 |
29 | 4 4 4 4 5 4 4 |
30 | 4 4 4 4 3 4 4 |
31 | 4 4 4 4 4 4 4 |
32 | 3 3 3 3 3 4 3 |
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
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2083.0 GPS week: 2083 Day: 0 MJD: 58825.000
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 247| -1 0 1 14 -5 11 -.04 8 8 | -393 -383 7 92
emr 80| 0 0 2 -6 -13 10 .15 13 13 | 142293 438 13 87
esa 150| 0 0 1 -5 -4 13 -.04 10 10 | 166 -1807 7 77
gfz 177| 0 0 0 15 9 13 .16 10 10 | -172 465 10 104
grg 94| 0 0 0 -27 10 -4 -.09 9 9 | 100 247 9 123
igr n/a| 0 0 0 -2 -4 -17 .03 4 4 | 4596 576 10 56
jpl 80| -2 2 1 18 0 -2 .17 10 10 | 213551 328 8 66
mit 349| 0 0 -7 20 -20 32 -.09 14 13 | 4897 462 110 1839
ngs 210| 0 0 0 -24 17 -24 -.05 6 6 | -363 -364 1097 2205
sio 315| 2 0 -2 14 -42 -3 -.12 15 14 | --- --- --- ---
Table 2.2083.1 GPS week: 2083 Day: 1 MJD: 58826.000
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 249| 0 0 0 10 16 17 -.02 8 8 | -538 -113 7 86
emr 80| 0 3 1 0 11 18 .13 13 13 | 142454 1050 14 89
esa 150| 0 0 3 -20 -67 -11 -.09 14 12 | 641 -2264 11 81
gfz 184| 0 0 0 16 3 0 .10 10 9 | -90 86 10 109
grg 100| 1 0 0 -26 10 -29 -.11 12 11 | 86 99 11 133
igr n/a| 0 0 0 -21 0 -8 .03 4 4 | 4937 967 11 74
jpl 80| 0 0 0 0 32 -8 .14 8 8 | 213613 642 7 62
mit 350| 0 1 -6 -19 -11 33 -.09 14 14 | 5427 207 80 1512
ngs 210| 0 -1 0 0 -6 -17 -.04 7 6 | -531 -101 1046 1795
sio 316| 3 -1 -3 -4 0 25 -.07 17 16 | --- --- --- ---
Table 2.2083.2 GPS week: 2083 Day: 2 MJD: 58827.000
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 248| 0 0 1 3 -1 30 -.01 8 8 | -568 178 7 98
emr 80| 0 0 2 -13 14 -2 .14 12 12 | 143060 52 14 97
esa 150| -1 0 1 -20 -19 38 -.04 10 10 | -119 -1610 8 84
gfz 182| 0 0 0 20 -4 -15 .10 10 11 | -767 169 11 122
grg 100| 0 0 2 -26 -16 -25 -.15 11 10 | 178 -251 10 112
igr n/a| 0 0 -1 -17 3 -19 .05 3 3 | 5358 44 10 61
jpl 80| 0 1 0 25 26 -22 .11 8 8 | 213846 -80 8 70
mit 350| 0 0 -6 -14 -18 7 -.08 14 13 | 5366 375 106 1448
ngs 209| 1 -1 -1 0 7 -5 -.03 7 6 | -540 213 1070 2475
sio 322| 1 -2 -2 9 -19 -8 -.07 16 15 | --- --- --- ---
Table 2.2083.3 GPS week: 2083 Day: 3 MJD: 58828.000
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 247| -1 0 0 23 8 36 -.03 8 8 | -423 -329 7 93
emr 80| 2 -1 1 -24 -15 6 .14 13 12 | 142978 172 17 93
esa 150| -1 0 0 -13 -6 11 -.03 11 10 | -708 -383 7 71
gfz 183| 0 0 4 25 -8 2 .10 12 12 | -389 129 12 125
grg 99| 1 0 0 -9 -17 -30 -.12 51 12 | -7 -48 10 130
igr n/a| 0 0 0 11 -10 -14 .04 4 4 | 5252 372 11 64
jpl 80| 0 0 1 -3 -4 -30 .13 9 9 | 213617 107 7 69
mit 349| 0 0 -5 -20 32 15 -.11 15 13 | 5846 56 78 1831
ngs 209| 0 0 -2 0 -1 8 -.01 9 8 | -459 -298 893 2006
sio 320| 0 -2 -3 -15 37 -11 -.08 15 14 | --- --- --- ---
Table 2.2083.4 GPS week: 2083 Day: 4 MJD: 58829.000
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 244| -1 0 0 20 -4 26 .00 8 8 | -390 -361 6 93
emr 80| 0 -2 3 -52 22 7 .16 13 13 | 143100 -964 17 98
esa 150| 0 0 0 -14 -13 -6 -.02 10 10 | 470 -2933 7 72
gfz 176| 0 2 2 6 23 6 .09 10 11 | -227 -249 10 124
grg 97| 1 1 -4 -19 -13 11 -.10 11 10 | 297 -405 10 149
igr n/a| 0 0 0 -15 8 -11 .02 4 4 | 5697 -798 11 65
jpl 80| -1 -1 0 4 3 -42 .03 8 8 | 213667 -586 6 69
mit 349| 0 0 -4 22 -17 3 -.10 13 12 | 7083 -3193 78 1771
ngs 192| 0 0 1 -8 6 0 -.04 8 7 | -524 -288 905 2096
sio 313| 1 0 -2 38 -10 16 -.02 15 14 | --- --- --- ---
Table 2.2083.5 GPS week: 2083 Day: 5 MJD: 58830.000
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 243| 0 0 0 31 9 9 -.03 9 8 | -439 -268 7 103
emr 79| 3 8 0 -5 -18 12 .17 15 15 | 142443 -668 18 92
esa 150| 0 -1 0 -5 -6 -22 -.03 10 9 | 900 -2398 7 66
gfz 171| -2 0 2 -16 -4 7 .15 9 8 | 382 -667 10 99
grg 96| 0 0 0 -10 -18 21 -.18 9 9 | 528 -905 10 128
igr n/a| 0 0 -1 -14 -3 -16 .04 4 4 | 5230 -870 10 60
jpl 80| 5 0 0 -5 36 -26 .15 11 10 | 213366 -1013 8 68
mit 350| 0 0 -5 -31 -6 0 -.08 15 14 | -362 -679 77 1690
ngs 192| -1 0 0 37 11 -16 -.06 9 7 | -337 -434 929 1982
sio 312| 0 -1 -5 -40 -18 35 .07 15 14 | --- --- --- ---
Table 2.2083.6 GPS week: 2083 Day: 6 MJD: 58831.000
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 242| 0 -1 1 15 11 19 -.05 8 8 | -474 -20 5 96
emr 80| -2 6 3 -10 0 -3 .19 14 14 | 142233 2185 19 101
esa 150| 0 0 1 -22 -10 -1 -.03 8 9 | 718 -2431 8 81
gfz 173| 0 0 0 -7 -5 29 .16 10 9 | 179 -251 11 97
grg 101| 1 0 -6 -31 -20 41 -.20 10 9 | -154 119 11 135
igr n/a| 0 0 -2 -23 15 -23 .06 3 3 | 4908 1893 10 58
jpl 80| 0 0 2 3 39 -6 .13 8 8 | 212907 1722 8 70
mit 350| 0 0 -5 -30 -5 -4 -.11 15 13 | -371 -72 58 1844
ngs 188| 0 0 0 22 -35 -12 -.05 7 6 | -506 -49 1118 1819
sio 311| 2 -3 -4 51 52 -87 .03 15 13 | --- --- --- ---
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 3.2083.0 GPS week: 2083 Day: 0 MJD: 58825.000
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 | 6 12 17 13 7 4 9 10 6 11 3 | 39 40 43 43 38 42 41 41 43 43 41
2E | 7 14 6 9 8 3 14 15 8 13 3 | 65 67 64 68 63 65 61 63 65 64 64
3 | 11 10 7 9 8 3 7 11 6 14 3 | 28 30 31 27 26 24 27 28 28 30 26
X4 | 11 --- 9 --- --- 18 --- 26 --- 1281 10 | 38 --- 38 --- --- 40 --- 44 --- 634 37
5 | 6 7 12 10 8 4 10 28 4 19 4 | 43 46 43 46 45 44 50 39 44 40 43
X6E | 7 --- 19 16 14 3 10 11 6 13 4 | 40 --- 42 47 40 42 26 41 41 44 42
7 | 8 12 7 14 12 3 11 11 5 18 3 | 31 25 25 37 25 27 23 30 25 27 26
8 | 8 12 12 10 10 4 9 9 5 15 3 | 22 23 23 22 19 20 23 19 19 26 20
9 | 9 9 7 6 7 3 10 10 6 12 3 | 35 39 33 36 32 33 38 36 33 35 34
10 | 5 8 6 9 5 5 7 11 5 13 2 | 19 24 22 22 22 21 25 25 21 27 21
11E | 10 9 13 8 11 4 7 12 6 14 3 | 36 34 36 36 35 34 35 33 31 37 34
12 | 10 18 6 8 9 3 7 16 6 14 3 | 27 27 25 25 23 25 26 31 24 26 24
13 | 7 10 8 7 6 3 9 13 8 16 3 | 23 30 23 26 25 24 30 29 26 28 25
14 | 7 6 8 7 7 3 5 13 6 14 2 | 35 35 35 37 36 35 37 36 37 35 35
15 | 5 10 6 11 6 3 8 12 7 13 3 | 36 41 40 40 38 38 39 37 37 35 38
16 | 8 19 6 16 12 3 14 15 6 18 4 | 25 21 24 27 21 22 23 28 23 24 21
17 | 5 10 8 7 7 3 7 14 7 12 3 | 20 24 20 23 21 22 25 26 22 24 21
X18E | 13 17 16 16 13 6 --- 17 17 24 6 | 87 80 94 97 92 92 --- 93 86 103 90
19 | 5 21 9 9 9 3 7 16 7 15 3 | 23 29 25 27 24 24 25 21 23 20 23
20 | 9 6 7 12 10 6 6 24 6 23 4 | 27 28 26 29 30 26 28 40 30 39 28
21E | 7 12 7 7 7 4 7 14 4 13 3 | 49 49 49 50 51 50 50 51 49 53 49
22 | 6 10 10 8 6 4 9 15 6 21 3 | 31 33 28 32 30 31 31 38 33 35 30
23 | 8 19 9 9 9 3 7 11 7 15 3 | 30 24 27 32 27 29 27 36 30 29 28
24 | 10 10 14 9 9 3 9 9 9 14 3 | 25 27 31 24 26 24 26 27 23 25 24
25 | 7 15 13 10 10 5 11 8 5 7 3 | 17 23 21 20 18 18 20 19 16 19 17
26 | 9 11 13 11 11 2 12 11 7 12 3 | 797 793 797 795 785 794 794 796 791 794 794
27 | 10 12 13 11 13 5 11 9 7 14 4 | 31 29 32 31 22 30 32 30 31 30 29
28 | 8 15 8 9 9 3 8 11 8 13 3 | 18 25 20 22 16 18 21 19 18 15 17
29 | 10 17 6 10 10 4 8 19 7 19 4 | 26 28 25 27 24 24 25 26 28 25 25
30 | 8 15 17 13 11 3 10 8 6 9 4 | 24 20 24 27 25 22 23 23 21 19 21
31 | 9 13 7 12 10 5 19 13 8 15 4 | 23 27 23 28 27 23 31 28 23 23 24
32 | 8 12 4 7 9 5 11 7 6 14 3 | 24 34 27 25 28 26 35 29 29 33 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 10 9 4 10 14 6 15 |T 56 58 56 58 55 55 56 58 56 76 55
WRMS | 8 13 10 10 9 4 10 13 6 14 |NE 56 59 57 59 56 56 59 59 57 80 56
MEDI | 8 12 8 9 9 3 9 12 6 14 |MD 28 29 27 29 27 26 27 30 29 30 27
Table 3.2083.1 GPS week: 2083 Day: 1 MJD: 58826.000
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 | 5 11 20 11 26 4 8 12 7 13 4 | 43 44 45 46 56 45 43 45 43 47 44
2E | 6 12 8 7 8 3 11 13 10 16 3 | 44 42 45 46 44 43 43 42 42 39 43
3 | 7 10 44 9 13 4 9 11 7 13 5 | 21 28 44 20 20 21 29 22 21 27 22
X4 | 10 --- 14 --- --- 15 --- 32 --- --- 13 | 26 --- 30 --- --- 26 --- 40 --- --- 28
5 | 6 7 12 8 7 4 9 29 5 22 4 | 32 35 29 31 29 33 38 33 33 37 32
6E | 10 6 22 28 16 5 8 9 5 16 5 | 44 34 44 50 41 45 34 45 45 50 44
7 | 8 13 7 7 13 4 11 14 9 22 4 | 27 24 23 27 23 25 26 28 26 26 24
8 | 10 12 13 9 12 5 9 11 5 14 3 | 21 24 23 24 19 21 24 21 19 24 20
9 | 7 9 7 6 10 4 10 8 6 12 3 | 26 34 29 27 23 25 34 26 26 32 27
10 | 8 8 7 11 6 5 7 11 6 13 3 | 21 26 21 19 20 20 25 20 18 27 20
11E | 7 11 16 8 17 4 6 9 9 14 3 | 32 33 31 34 34 32 32 29 28 31 30
12 | 9 19 9 8 12 4 7 15 7 16 4 | 21 24 24 23 19 22 24 25 22 25 21
13 | 9 12 9 7 9 3 10 14 4 16 3 | 24 33 23 27 21 25 31 25 23 29 25
14 | 7 6 6 7 8 3 4 13 6 17 2 | 32 34 31 33 33 33 35 34 30 37 32
15 | 10 8 5 9 10 3 8 13 5 17 3 | 32 31 32 35 30 30 30 28 29 30 30
16 | 14 18 7 11 13 5 9 15 9 20 4 | 26 22 25 25 24 23 24 31 24 29 23
17 | 5 11 7 11 10 3 6 16 8 21 3 | 26 30 25 31 26 28 31 31 30 32 28
X18E | 15 18 24 19 21 8 --- 19 22 --- 8 | 69 67 82 76 76 73 --- 77 72 --- 73
19 | 7 19 8 9 12 3 8 18 7 19 4 | 26 33 28 32 29 28 31 25 31 27 28
20 | 7 9 8 10 10 4 7 24 6 21 4 | 23 25 24 24 23 22 26 29 24 31 23
21E | 7 9 8 6 19 3 8 14 8 16 3 | 42 41 42 44 39 43 43 45 44 44 42
22 | 7 9 9 9 13 3 8 18 7 25 4 | 22 25 19 21 20 21 25 27 19 29 20
23 | 7 21 11 6 11 2 7 11 6 16 3 | 26 18 25 26 20 22 21 27 24 24 22
24 | 8 7 16 9 10 5 8 8 5 13 3 | 24 26 31 21 23 22 25 23 23 25 23
25 | 7 24 15 8 9 4 9 12 7 13 4 | 19 29 21 19 17 18 21 17 18 20 17
26 | 10 13 14 19 12 5 11 11 8 13 4 | 819 815 818 817 812 816 816 818 812 818 816
27 | 8 12 13 8 12 5 9 9 7 16 3 | 26 28 30 29 24 28 27 28 26 32 26
28 | 7 12 9 8 10 3 6 12 6 16 3 | 24 28 24 29 22 25 27 24 26 27 24
29 | 10 16 6 10 12 3 7 20 6 17 4 | 24 25 22 27 20 24 24 24 26 25 23
30 | 7 10 16 8 12 3 8 8 8 14 3 | 25 26 25 25 23 23 24 23 24 20 22
31 | 8 14 7 13 12 3 8 14 6 19 3 | 28 28 24 33 26 27 29 28 27 28 26
32 | 9 11 5 7 8 4 10 6 6 13 3 | 21 34 23 22 22 23 34 24 23 31 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 14 10 12 4 8 14 7 17 |T 53 56 55 56 53 53 55 55 54 56 53
WRMS | 8 13 12 9 11 4 8 14 6 16 |NE 55 59 56 57 54 55 59 56 56 59 54
MEDI | 7 11 9 9 12 4 8 13 7 16 |MD 26 29 25 27 23 25 29 28 26 29 25
Table 3.2083.2 GPS week: 2083 Day: 2 MJD: 58827.000
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 | 5 12 17 16 14 3 8 10 7 11 4 | 22 22 25 27 23 22 25 21 22 21 21
2E | 16 9 8 9 15 5 7 17 9 17 4 | 68 68 66 65 64 65 67 66 65 68 66
3 | 7 9 8 8 9 5 8 10 7 13 3 | 29 33 28 31 30 32 35 28 31 38 30
X4 | 15 --- 14 --- --- 10 --- 33 --- 941 14 | 40 --- 38 --- --- 39 --- 59 --- 571 42
5 | 7 7 11 9 9 4 8 29 6 22 4 | 42 41 35 39 37 38 43 38 38 37 38
6E | 8 9 19 21 14 3 7 10 8 12 4 | 19 21 21 24 18 17 24 17 18 16 17
7 | 9 11 6 8 14 3 7 13 6 23 3 | 44 39 38 43 40 40 40 43 38 40 39
8 | 4 12 11 8 9 4 7 8 6 15 3 | 28 29 28 31 28 29 31 27 26 33 28
9 | 8 10 5 8 8 3 10 8 7 12 3 | 41 48 41 41 42 42 49 40 40 45 42
10 | 7 6 6 8 6 3 6 10 4 16 2 | 19 24 20 19 23 22 26 22 20 29 21
11E | 8 11 12 8 14 4 7 8 8 14 3 | 40 38 39 42 41 40 41 40 39 39 39
12 | 8 17 6 9 11 4 8 16 8 15 3 | 37 38 32 34 35 34 35 37 36 36 35
13 | 7 8 5 6 9 2 8 17 4 18 3 | 21 25 17 23 19 20 26 25 19 27 21
14 | 7 8 8 7 8 3 4 13 5 14 2 | 24 22 23 21 23 22 22 28 22 27 22
15 | 6 11 5 7 8 2 6 11 6 16 2 | 42 44 43 43 40 42 42 39 39 44 41
16 | 10 21 6 14 13 3 9 17 6 18 4 | 22 23 22 26 22 22 21 24 20 23 20
17 | 6 10 8 10 10 3 6 13 5 13 3 | 25 28 24 29 25 26 28 25 27 24 25
X18E | 12 18 26 22 18 7 --- 14 23 16 7 | 42 46 53 49 50 45 --- 51 41 47 44
19 | 6 20 9 9 10 4 7 15 7 15 3 | 22 26 23 28 23 24 25 24 25 26 23
20 | 7 8 5 9 10 4 5 24 7 25 4 | 33 35 32 35 34 35 35 39 35 43 34
21E | 7 13 6 7 7 2 8 8 8 11 3 | 52 48 48 51 48 51 49 51 51 52 50
22 | 6 12 10 6 10 4 7 15 7 21 3 | 39 38 37 41 36 39 40 41 38 44 38
23 | 8 19 8 6 9 2 6 10 6 15 3 | 43 37 38 42 40 41 42 44 39 41 40
24 | 6 8 13 10 9 2 7 8 6 11 3 | 36 36 36 35 35 35 37 34 36 34 35
25 | 9 15 13 13 7 2 9 10 7 10 3 | 28 32 28 31 29 27 30 27 26 31 27
26 | 8 10 14 16 10 3 12 11 8 12 4 | 704 706 705 704 699 705 706 703 708 704 705
27 | 6 14 13 8 10 3 9 9 7 14 3 | 20 24 22 23 22 22 24 23 21 25 21
28 | 7 9 4 9 11 4 5 12 7 12 3 | 27 29 24 30 23 25 28 23 27 25 26
29 | 14 19 4 9 12 3 7 19 8 18 4 | 33 31 29 32 31 31 30 29 29 33 29
30 | 9 10 16 7 24 3 10 9 7 10 4 | 36 33 33 35 34 34 36 33 34 32 33
31 | 9 17 6 13 12 3 8 14 11 21 4 | 31 32 28 33 31 31 32 32 34 33 30
32 | 7 11 5 11 9 4 11 7 7 14 3 | 27 35 27 26 27 29 36 28 27 36 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 10 10 11 3 8 14 7 16 |T 54 55 53 55 53 53 56 55 53 72 53
WRMS | 8 12 10 11 10 3 8 13 6 15 |NE 57 59 55 59 57 57 59 58 57 80 56
MEDI | 7 11 8 9 10 3 7 11 7 15 |MD 33 33 29 33 31 32 35 32 34 34 30
Table 3.2083.3 GPS week: 2083 Day: 3 MJD: 58828.000
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 | 10 12 16 24 17 6 8 15 9 10 5 | 23 26 30 32 23 26 25 26 26 28 24
2E | 9 12 9 11 10 4 9 18 12 20 4 | 49 51 48 49 48 48 47 43 48 53 47
3 | 5 10 8 7 9 3 6 9 6 9 2 | 24 31 26 28 23 26 31 24 27 27 26
X4 | 11 --- 11 --- --- 10 --- 27 --- 731 11 | 40 --- 36 --- --- 33 --- 44 --- 406 38
5 | 6 10 12 9 10 4 10 27 6 21 4 | 43 40 40 39 39 39 46 36 39 37 39
6E | 7 7 22 27 18 3 8 10 9 15 5 | 27 23 28 32 22 23 22 24 25 24 23
7 | 8 10 7 8 13 4 9 17 8 21 4 | 31 26 23 30 27 27 25 28 28 22 25
8 | 6 10 12 9 12 4 8 11 6 14 3 | 25 30 26 26 23 26 28 26 25 30 25
9 | 7 10 7 10 7 4 9 10 8 10 3 | 32 42 32 34 30 34 41 32 36 36 34
10 | 8 7 7 10 5 3 6 9 7 10 2 | 21 26 23 26 23 23 25 20 22 26 22
11E | 7 10 12 8 16 5 8 10 13 14 4 | 34 33 32 33 36 32 33 32 32 33 32
12 | 8 19 6 8 13 4 7 17 10 14 4 | 26 26 24 20 24 22 26 24 21 23 22
13 | 7 7 7 8 10 3 8 16 8 17 3 | 24 29 23 23 22 23 29 27 27 28 24
14 | 9 5 7 8 8 3 5 15 5 14 3 | 23 24 23 21 21 23 23 30 25 28 22
15 | 5 11 6 7 8 2 6 13 9 16 3 | 32 32 35 32 27 30 31 26 30 32 30
16 | 11 19 5 10 11 4 9 15 6 15 4 | 24 24 25 27 20 25 23 27 28 24 23
17 | 4 8 6 10 14 3 6 15 6 15 3 | 22 28 21 29 21 23 25 24 25 22 23
X18E | 19 18 18 48 18 10 --- 14 27 14 9 | 60 66 66 89 63 67 --- 69 68 69 66
19 | 8 15 7 10 14 3 6 17 7 17 4 | 22 24 22 24 19 22 22 23 24 21 21
20 | 9 7 6 12 10 3 6 25 7 24 4 | 21 24 23 25 21 22 22 28 23 28 21
21E | 17 8 7 12 9 5 9 11 7 11 3 | 47 50 49 51 52 51 52 55 52 52 50
22 | 6 10 8 7 7 3 8 16 6 19 3 | 28 31 23 28 26 28 29 31 26 32 27
23 | 6 19 10 10 8 3 8 11 8 13 3 | 28 20 26 30 24 27 25 29 32 24 26
24 | 6 8 14 9 10 3 6 7 9 8 3 | 24 25 29 22 23 23 26 23 21 24 23
25 | 9 19 14 12 8 4 12 11 8 11 4 | 21 27 25 23 22 22 25 23 18 24 21
26 | 15 28 21 17 275 9 30 17 15 17 8 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
27 | 8 12 13 7 13 4 10 11 7 14 3 | 22 27 26 24 20 24 26 23 25 28 23
28 | 8 12 6 9 12 4 6 15 9 14 3 | 22 24 22 26 19 22 21 18 26 20 21
29 | 10 18 6 6 11 3 6 17 9 18 4 | 33 32 30 30 26 28 29 29 27 32 29
30 | 8 9 16 8 10 4 8 11 8 9 3 | 28 26 27 25 26 26 27 24 29 22 25
31 | 9 16 5 12 12 4 7 15 9 19 4 | 28 28 26 29 26 25 28 30 29 25 26
32 | 6 11 5 14 8 4 10 9 7 11 3 | 23 36 28 21 27 26 35 28 26 30 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 11 11 51 4 9 15 9 15 |T 29 31 29 30 27 28 29 29 29 42 28
WRMS | 8 12 10 12 11 4 9 13 8 14 |NE 26 28 26 26 24 25 27 27 26 42 25
MEDI | 8 10 7 10 10 4 8 15 8 14 |MD 26 27 26 28 23 26 26 27 26 28 25
Table 3.2083.4 GPS week: 2083 Day: 4 MJD: 58829.000
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 11 18 14 21 6 8 10 13 10 4 | 30 31 34 35 29 32 29 31 35 31 31
2E | 9 12 8 13 9 5 9 14 13 18 4 | 51 53 49 51 49 50 47 48 55 53 50
3 | 7 7 7 7 7 3 6 6 8 11 2 | 23 26 24 24 21 24 27 21 23 27 23
X4 | 11 --- 10 --- --- 19 --- 28 --- 1156 11 | 43 --- 9999 --- --- 9999 --- 9999 --- 9999 9999
5 | 9 7 11 8 10 3 7 27 8 20 4 | 35 36 33 38 30 34 36 36 37 35 34
6E | 10 8 21 21 17 3 11 11 9 13 5 | 30 29 31 34 27 28 26 30 28 33 29
7 | 6 10 7 7 12 4 7 15 6 19 3 | 30 29 27 29 31 28 27 33 26 28 27
8 | 7 10 11 7 7 6 8 10 7 11 3 | 18 23 19 22 17 18 19 19 18 25 18
9 | 7 10 5 9 6 3 11 7 7 11 3 | 29 40 31 32 32 31 40 30 29 33 32
10 | 7 8 6 6 7 4 8 7 9 14 3 | 18 23 20 21 21 20 21 19 20 23 19
11E | 8 11 12 12 9 5 8 12 10 10 3 | 22 26 23 26 25 24 23 21 25 21 22
12 | 8 16 6 12 12 3 6 15 8 14 3 | 29 26 25 28 26 26 25 27 26 29 25
13 | 7 9 7 7 7 2 9 15 6 16 3 | 20 27 23 21 21 21 27 27 23 27 22
14 | 8 7 8 6 18 4 6 11 6 12 3 | 28 24 28 23 19 24 26 30 23 25 24
15 | 7 11 7 7 6 2 7 11 8 14 3 | 39 37 37 39 32 36 34 32 35 36 35
16 | 9 21 5 10 13 4 8 16 8 17 4 | 21 21 21 21 20 19 19 23 17 20 18
17 | 8 10 9 12 11 3 5 12 9 13 3 | 21 27 22 30 21 23 24 25 24 26 23
X18E | 27 22 15 22 19 15 --- 18 30 18 8 | 83 79 68 67 71 61 --- 62 62 54 66
19 | 8 23 9 11 12 4 6 16 9 15 4 | 21 27 23 25 21 21 21 20 23 21 20
20 | 11 9 6 11 10 5 7 24 6 24 4 | 22 23 21 26 23 22 24 29 23 31 22
21E | 10 10 8 7 15 5 7 12 6 13 3 | 41 40 39 40 41 40 41 38 39 41 39
22 | 7 10 9 7 5 3 9 17 8 21 3 | 28 28 23 28 26 25 29 31 26 31 26
23 | 7 20 8 5 7 3 7 10 5 14 3 | 31 26 29 31 30 30 29 33 30 28 29
24 | 6 8 13 10 9 4 7 6 9 9 3 | 28 27 31 26 28 25 28 26 27 29 26
25 | 11 18 14 11 7 4 9 10 7 11 4 | 22 24 22 23 18 19 21 20 20 25 19
26 | 8 11 12 10 15 5 10 12 7 11 3 | 825 821 827 824 829 823 823 827 822 824 824
27 | 9 10 13 7 10 5 8 9 7 11 3 | 19 22 23 22 20 20 19 21 19 22 19
28 | 7 12 6 10 10 4 5 11 6 12 3 | 19 22 22 24 20 19 21 19 22 19 19
29 | 14 20 6 8 11 5 7 19 10 23 4 | 23 21 18 20 17 18 18 19 21 28 18
30 | 5 11 14 6 12 3 7 10 8 9 3 | 25 26 25 23 28 24 26 24 23 22 23
31 | 9 16 6 14 14 5 8 14 11 17 4 | 25 27 23 29 24 23 24 24 25 20 22
32 | 5 13 4 12 7 4 12 6 7 16 3 | 20 32 24 16 23 21 30 21 17 28 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 10 11 4 8 13 8 15 |T 53 55 53 54 52 52 53 53 53 54 52
WRMS | 8 13 10 11 10 4 8 12 7 14 |NE 56 58 56 57 55 55 57 57 55 58 55
MEDI | 8 11 8 10 10 4 7 12 8 14 |MD 25 27 24 26 25 24 26 27 25 28 23
Table 3.2083.5 GPS week: 2083 Day: 5 MJD: 58830.000
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 17 16 5 19 17 17 15 5 | 38 43 34 40 40 33 36 33 37 35 35
2E | 14 14 7 10 7 3 9 18 15 16 4 | 49 47 50 53 48 50 50 50 51 55 49
3 | 8 9 8 7 9 3 9 9 9 10 3 | 21 25 22 22 19 20 29 20 20 27 21
X4 | 14 --- --- 12 --- 14 --- --- --- --- 13 | 17 --- --- 12 --- 9999 --- --- --- --- 9999
5 | 9 11 9 7 8 3 9 27 7 22 4 | 37 36 30 34 35 32 38 35 33 35 33
6E | 22 20 20 14 14 7 21 14 17 14 6 | 44 37 39 38 39 36 42 37 42 35 37
7 | 9 14 7 8 10 3 8 17 6 18 3 | 31 28 24 30 26 27 27 32 27 27 26
8 | 9 11 14 6 7 5 9 9 5 12 3 | 20 24 22 25 18 19 24 21 20 30 20
9 | 7 13 7 7 9 4 13 11 7 12 3 | 26 38 27 26 25 25 37 25 26 31 27
10 | 6 9 6 9 4 4 8 10 6 9 2 | 20 26 20 22 19 20 25 21 19 24 20
11 | 7 11 13 8 10 5 9 12 7 11 3 | 33 34 32 36 29 32 34 31 35 31 32
12 | 11 20 6 7 11 2 9 16 5 15 4 | 26 28 25 27 24 26 27 30 26 32 25
13 | 6 9 7 8 6 4 8 19 7 18 3 | 27 34 29 27 26 29 32 28 29 30 27
14 | 8 9 7 7 6 5 7 14 7 13 3 | 36 35 35 39 38 35 36 36 37 35 35
15 | 7 12 5 5 5 4 9 11 6 15 2 | 27 30 28 31 23 24 27 25 24 27 26
16 | 10 25 7 6 10 3 11 14 9 19 4 | 24 22 24 26 21 21 22 27 25 25 21
17 | 8 10 7 10 11 5 9 15 9 16 3 | 23 30 23 28 19 23 30 22 24 28 23
X18E | 13 --- 21 24 14 16 --- 22 19 21 8 | 84 --- 79 85 78 85 --- 78 79 76 80
19 | 8 19 8 9 11 5 9 16 9 16 4 | 22 26 25 27 19 22 27 19 23 24 21
20 | 8 9 6 10 10 5 8 25 6 23 4 | 21 22 20 25 22 21 22 25 22 28 20
21E | 8 9 6 6 9 5 11 12 6 12 3 | 62 66 63 66 66 66 65 67 64 69 65
22 | 7 10 10 9 8 3 8 15 8 21 3 | 18 24 18 22 18 20 23 24 20 25 19
23 | 6 19 10 5 9 4 6 14 7 12 3 | 23 19 22 22 21 21 21 28 23 25 21
24 | 10 11 12 9 9 6 9 10 8 11 3 | 23 30 28 23 21 21 25 23 21 27 22
25 | 9 18 15 10 8 4 12 10 7 14 4 | 18 24 21 21 18 18 21 18 16 24 17
26 | 9 12 16 9 8 4 13 13 8 12 4 | 476 476 475 473 466 475 475 477 474 480 476
27 | 7 11 12 8 9 5 10 9 7 15 3 | 22 26 25 24 20 23 25 24 24 29 22
28 | 9 17 8 9 10 3 9 14 10 15 4 | 24 27 22 25 17 20 24 18 21 25 20
29 | 11 19 5 7 10 4 8 18 10 16 4 | 19 19 18 21 17 18 19 19 19 27 18
30 | 7 12 16 7 10 3 8 13 6 10 3 | 25 25 24 24 25 23 26 22 23 25 23
31 | 10 13 6 7 11 3 9 17 9 21 4 | 23 28 22 26 23 22 28 26 24 23 22
32 | 6 16 5 11 7 5 12 9 7 13 3 | 15 34 21 16 15 18 29 18 15 24 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 10 9 9 4 11 15 9 15 |T 42 45 43 44 41 42 44 43 43 46 42
WRMS | 8 14 9 8 9 4 10 14 7 14 |NE 40 45 42 42 39 40 44 42 41 45 40
MEDI | 8 12 8 8 9 4 9 14 7 15 |MD 24 28 25 26 23 23 27 25 24 28 23
Table 3.2083.6 GPS week: 2083 Day: 6 MJD: 58831.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 10 28 17 12 11 7 --- 11 13 9 5 | 35 42 37 41 32 34 --- 30 29 31 31
2E | 10 10 6 8 9 4 10 17 9 16 3 | 74 74 75 79 75 76 74 75 75 76 75
3 | 8 12 8 7 11 2 8 10 10 10 3 | 28 30 28 30 23 26 30 23 26 31 26
X4 | 8 --- 9 12 --- 9 --- 25 --- 1332 7 | 11 --- 9999 13 --- 9999 --- 9999 --- 9999 9999
5 | 6 9 9 12 10 4 9 27 9 19 4 | 48 46 45 48 45 46 52 43 50 43 47
X6E | 10 13 16 26 13 10 --- 12 14 12 6 | 55 39 59 60 51 54 --- 54 50 59 54
7 | 6 15 7 12 11 5 7 17 6 20 3 | 29 29 26 28 28 28 29 34 28 31 27
8 | 6 12 10 9 8 4 7 10 7 10 3 | 19 23 24 23 20 20 22 18 20 27 20
9 | 9 13 4 8 9 4 11 12 6 10 3 | 33 43 36 33 36 34 43 37 32 38 35
10 | 6 10 7 10 7 4 6 8 6 7 2 | 17 27 21 20 20 20 21 17 21 21 19
11 | 7 13 13 10 11 4 7 12 9 11 3 | 34 36 35 36 34 33 34 32 34 31 33
12 | 7 19 6 7 11 3 7 15 6 14 3 | 29 32 28 29 27 29 30 32 30 32 29
13 | 6 9 7 7 6 3 8 15 6 14 3 | 28 33 28 29 29 30 34 32 30 37 29
14 | 7 9 7 7 9 3 5 12 5 13 2 | 39 43 40 42 43 40 41 41 39 40 40
15 | 6 12 5 9 6 2 9 11 4 16 3 | 32 38 35 35 29 33 35 30 32 32 32
16 | 10 22 6 8 12 5 9 17 6 18 4 | 25 27 27 23 23 24 23 29 26 27 23
17 | 8 13 6 13 10 3 5 14 6 13 3 | 19 25 19 25 19 22 24 22 21 22 20
X18E | 12 22 16 21 11 11 --- 18 23 16 6 | 103 102 100 109 105 106 --- 106 101 98 103
19 | 9 18 7 11 10 3 7 15 7 15 3 | 20 25 22 28 21 22 22 19 22 17 20
20 | 8 8 5 16 10 4 5 25 7 24 4 | 26 29 25 32 28 28 27 38 27 36 26
21E | 7 9 7 12 12 4 8 12 5 11 3 | 75 73 74 77 80 78 77 79 79 76 77
22 | 7 12 9 9 8 4 7 19 8 23 4 | 26 30 27 29 27 27 27 33 26 32 25
23 | 7 18 7 8 9 3 6 14 6 12 3 | 28 24 26 29 29 28 27 33 28 27 27
24 | 5 10 10 8 8 3 5 8 8 9 2 | 25 29 28 26 24 24 27 24 24 28 25
25 | 9 19 15 12 9 3 9 8 7 9 4 | 21 25 25 24 21 20 22 18 18 21 20
26 | 9 12 13 12 11 4 10 12 7 11 3 | 315 310 313 313 314 314 314 310 313 312 314
27 | 7 12 13 8 8 4 9 12 7 11 3 | 22 28 27 26 21 24 25 27 27 29 24
28 | 9 14 5 10 11 4 5 10 8 15 3 | 21 25 20 24 18 20 23 17 19 20 19
29 | 10 20 5 8 11 3 7 16 8 17 3 | 27 27 23 26 22 23 25 20 25 30 24
30 | 6 14 13 9 9 2 7 12 6 13 3 | 22 26 22 21 24 22 24 21 21 21 21
31 | 8 13 7 11 14 4 6 16 12 20 4 | 22 27 19 29 24 22 24 26 24 23 21
32 | 6 13 5 9 9 3 11 9 7 10 3 | 20 34 25 21 24 22 31 24 22 28 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 8 10 10 3 8 15 7 15 |T 41 45 43 44 42 42 42 43 42 44 42
WRMS | 8 14 9 9 9 3 8 13 6 13 |NE 36 41 38 38 37 37 40 38 38 40 37
MEDI | 7 13 7 9 10 4 7 12 7 13 |MD 27 30 27 29 27 28 27 30 27 31 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 4.2083 GPS week: 2083 MJD: 58825.0-58831.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 |U 11 10 20 |U 0 0 0 |U 11 10 31 |
emr | emr 2945 |U 18 16 55 |U 0 0 0 |U 21 12 45 |
esa | esa 3058 | 11 12 23 |U 0 0 0 | 16 11 37 |
gfz | gfz 2999 |U 12 11 22 |U 0 0 0 |U 11 10 33 |
grg | grg 2975 |U 11 12 21 |U 0 0 0 | 12 10 33 |
igr | igr 3011 | 10 11 20 | 0 0 0 | 12 10 34 |
igs | igs 3004 | 10 11 20 | 0 0 0 | 13 9 33 |
jpl | jpl 2852 |U 15 12 46 |U 0 0 0 |U 18 12 43 |
mit | mit 3058 |U 19 16 33 |U 0 0 0 |U 20 16 51 |
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 5.2083.0 GPS week: 2083 Day: 0 MJD: 58825.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 11 6 23 | ---- ---- ---- | 9 8 30 |
emr | emr 2876 | 15 14 29 | ---- ---- ---- | 19 12 42 |
esa | esa 3072 | 12 9 23 | ---- ---- ---- | 13 7 31 |
gfz | gfz 2972 | 13 9 23 | ---- ---- ---- | 10 9 30 |
grg | grg 2976 | 11 9 22 | ---- ---- ---- | 11 10 34 |
igr | igr 3021 | 11 6 18 | ---- ---- ---- | 11 8 32 |
igs | igs 3028 | 11 7 18 | ---- ---- ---- | 11 8 32 |
jpl | jpl 2880 | 14 8 23 | ---- ---- ---- | 16 10 39 |
mit | mit 3072 | 21 23 34 | ---- ---- ---- | 32 31 75 |
Table 5.2083.1 GPS week: 2083 Day: 1 MJD: 58826.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 10 24 | ---- ---- ---- | 11 9 35 |
emr | emr 2972 | 9 15 30 | ---- ---- ---- | 19 9 43 |
esa | esa 3072 | 12 14 24 | ---- ---- ---- | 16 9 37 |
gfz | gfz 2972 | 14 12 31 | ---- ---- ---- | 12 10 34 |
grg | grg 2976 | 13 13 23 | ---- ---- ---- | 9 10 35 |
igr | igr 2975 | 11 13 22 | ---- ---- ---- | 13 9 38 |
igs | igs 3047 | 10 12 20 | ---- ---- ---- | 13 8 36 |
jpl | jpl 2880 | 11 15 24 | ---- ---- ---- | 18 11 44 |
mit | mit 3072 | 17 15 27 | ---- ---- ---- | 15 11 37 |
Table 5.2083.2 GPS week: 2083 Day: 2 MJD: 58827.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 8 19 | ---- ---- ---- | 9 9 29 |
emr | emr 2972 | 13 12 27 | ---- ---- ---- | 21 11 41 |
esa | esa 3072 | 8 11 23 | ---- ---- ---- | 14 9 33 |
gfz | gfz 2972 | 10 9 23 | ---- ---- ---- | 10 8 31 |
grg | grg 2976 | 9 12 19 | ---- ---- ---- | 10 8 31 |
igr | igr 2990 | 8 9 17 | ---- ---- ---- | 11 9 35 |
igs | igs 2973 | 7 9 17 | ---- ---- ---- | 12 8 33 |
jpl | jpl 2880 | 10 11 23 | ---- ---- ---- | 17 10 42 |
mit | mit 3072 | 16 15 30 | ---- ---- ---- | 29 20 64 |
Table 5.2083.3 GPS week: 2083 Day: 3 MJD: 58828.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 10 8 19 | ---- ---- ---- | 10 8 22 |
emr | emr 2972 | 42 21 188 | ---- ---- ---- | 25 16 45 |
esa | esa 3072 | 12 11 17 | ---- ---- ---- | 15 7 29 |
gfz | gfz 2971 | 12 12 20 | ---- ---- ---- | 11 9 25 |
grg | grg 2975 | 13 11 20 | ---- ---- ---- | 12 8 23 |
igr | igr 3057 | 12 10 25 | ---- ---- ---- | 13 10 28 |
igs | igs 3055 | 12 12 27 | ---- ---- ---- | 16 12 30 |
jpl | jpl 2880 | 39 17 180 | ---- ---- ---- | 22 19 47 |
mit | mit 3072 | 11 8 20 | ---- ---- ---- | 15 11 32 |
Table 5.2083.4 GPS week: 2083 Day: 4 MJD: 58829.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2972 | 9 11 15 | ---- ---- ---- | 10 8 29 |
emr | emr 2972 | 14 14 33 | ---- ---- ---- | 18 9 46 |
esa | esa 3072 | 11 12 26 | ---- ---- ---- | 15 10 38 |
gfz | gfz 2972 | 12 12 17 | ---- ---- ---- | 12 12 45 |
grg | grg 2970 | 10 13 22 | ---- ---- ---- | 12 9 36 |
igr | igr 3031 | 10 13 14 | ---- ---- ---- | 11 8 35 |
igs | igs 3022 | 10 12 14 | ---- ---- ---- | 12 8 35 |
jpl | jpl 2880 | 11 11 20 | ---- ---- ---- | 16 9 39 |
mit | mit 3072 | 15 14 24 | ---- ---- ---- | 21 12 59 |
Table 5.2083.5 GPS week: 2083 Day: 5 MJD: 58830.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 12 11 20 | ---- ---- ---- | 11 11 32 |
emr | emr 2880 | 13 18 31 | ---- ---- ---- | 19 12 48 |
esa | esa 2976 | 12 14 22 | ---- ---- ---- | 16 12 37 |
gfz | gfz 3068 | 12 12 24 | ---- ---- ---- | 12 11 35 |
grg | grg 2976 | 12 14 21 | ---- ---- ---- | 10 12 30 |
igr | igr 2969 | 11 13 19 | ---- ---- ---- | 12 12 36 |
igs | igs 2937 | 10 12 26 | ---- ---- ---- | 12 10 35 |
jpl | jpl 2880 | 10 15 25 | ---- ---- ---- | 18 12 49 |
mit | mit 2976 | 44 25 74 | ---- ---- ---- | 14 14 45 |
Table 5.2083.6 GPS week: 2083 Day: 6 MJD: 58831.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 17 19 24 | ---- ---- ---- | 18 16 42 |
emr | emr 2972 | 18 16 44 | ---- ---- ---- | 24 13 47 |
esa | esa 3072 | 13 14 28 | ---- ---- ---- | 22 20 54 |
gfz | gfz 3068 | 11 13 19 | ---- ---- ---- | 12 11 34 |
grg | grg 2976 | 12 13 21 | ---- ---- ---- | 17 16 40 |
igr | igr 3039 | 11 13 23 | ---- ---- ---- | 13 12 35 |
igs | igs 2968 | 11 11 19 | ---- ---- ---- | 13 10 34 |
jpl | jpl 2688 | 14 11 24 | ---- ---- ---- | 17 12 40 |
mit | mit 3072 | 13 14 21 | ---- ---- ---- | 15 12 41 |
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 6.2083 GPS week: 2083 MJD: 58825.500-58831.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 4 -19 51 85 -1 | 7 17
| 15 15 65 97 2 | 2
emr uuuuu | -8 30 29 -54 6 | 29 33
| 24 31 96 60 10 | 2
esa uuuuu | 8 -2 114 -58 5 | 16 21
| 23 16 49 70 3 | 4
gfz uuuuu | -9 -23 86 -13 5 | 15 20
| 18 22 135 42 3 | 3
grg uuuuu | 23 9 -65 16 -2 | -1 11
| 22 24 53 33 3 | 1
igr xxxxx | 6 11 -17 40 3 | 1 14
| 10 14 58 36 3 | 3
irf xxxxx | -16 -28 -1 -55 0 | 0 14
| 13 14 25 39 3 | 2
jpl uuuuu | -23 9 -73 -38 -5 | 28 31
| 39 39 98 96 13 | 3
mit uuuuu | -1 -1 32 -90 -1 | 11 18
| 24 16 49 86 4 | 1
ngs uuxuu | 20 -7 -54 145 -1 | 9 16
| 57 25 286 90 3 | 2
sio uuuux | -19 41 -299 -197 2 | 41 44
| 36 22 86 56 10 | 2
Table 7.2083.0 GPS week: 2083 Day: 0 MJD: 58825.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 27 1 37 101 -3 | 4 14
emr uuuuu | 7 -4 148 -23 -1 | 27 29
esa uuuuu | -9 -3 162 -135 4 | 12 16
gfz uuuuu | -12 3 -106 -8 2 | 12 16
grg uuuuu | 3 20 -88 54 3 | -1 9
igr xxxxx | 9 -1 16 22 2 | -2 12
irf xxxxx | -12 -11 -18 -16 -3 | -1 10
jpl uuuuu | 25 -9 76 98 -13 | 33 35
mit uuuuu | 21 1 -21 3 -7 | 12 15
ngs uuxuu | -47 -19 300 -15 0 | 7 14
sio uuuux | 40 47 -359 -186 -14 | 41 42
Table 7.2083.1 GPS week: 2083 Day: 1 MJD: 58826.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -17 -11 73 -88 3 | 4 14
emr uuuuu | -7 23 -3 -19 1 | 27 29
esa uuuuu | 58 28 133 -118 3 | 12 16
gfz uuuuu | 0 -15 -65 38 6 | 11 16
grg uuuuu | -2 17 33 47 -6 | -1 9
igr xxxxx | 16 15 77 23 4 | -3 12
irf xxxxx | -3 -34 33 -11 5 | -2 11
jpl uuuuu | -10 3 -57 46 -13 | 29 32
mit uuuuu | 17 -10 56 17 4 | 10 15
ngs uuxuu | -3 -26 240 97 1 | 7 13
sio uuuux | -17 43 -265 -181 6 | 38 40
Table 7.2083.2 GPS week: 2083 Day: 2 MJD: 58827.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 13 -12 -4 120 -2 | 8 17
emr uuuuu | -16 -12 146 -42 -9 | 30 33
esa uuuuu | 11 6 37 -137 9 | 16 21
gfz uuuuu | 13 -39 221 -30 4 | 15 21
grg uuuuu | 25 26 -109 30 2 | 1 11
igr xxxxx | 0 21 -47 -3 6 | 1 15
irf xxxxx | -9 -33 -4 -37 -3 | 2 14
jpl uuuuu | -8 -24 -54 -16 -5 | 31 33
mit uuuuu | 2 -10 59 -56 -5 | 13 19
ngs uuxuu | -23 24 -206 92 -3 | 10 17
sio uuuux | -11 69 -440 -140 4 | 42 45
Table 7.2083.3 GPS week: 2083 Day: 3 MJD: 58828.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -11 -23 -57 -2 0 | 7 18
emr uuuuu | -9 64 -58 -139 10 | 28 32
esa uuuuu | -2 -12 157 -42 8 | 16 21
gfz uuuuu | 12 -62 189 36 2 | 14 21
grg uuuuu | 5 -33 -25 -20 -5 | 0 13
igr xxxxx | 18 -12 -13 55 3 | 1 15
irf xxxxx | -2 -47 6 -39 1 | 0 17
jpl uuuuu | 3 26 -68 7 -4 | 27 31
mit uuuuu | 20 1 9 -72 1 | 11 20
ngs uuxuu | -7 23 -388 192 2 | 9 18
sio uuuux | 1 26 -192 -137 -8 | 41 44
Table 7.2083.4 GPS week: 2083 Day: 4 MJD: 58829.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 12 -28 70 142 0 | 7 18
emr uuuuu | -55 48 79 -65 8 | 28 33
esa uuuuu | 13 -15 139 21 6 | 17 23
gfz uuuuu | -26 -27 138 -7 5 | 15 22
grg uuuuu | 41 -9 -106 -6 -1 | -1 12
igr xxxxx | 5 12 -114 112 6 | 1 16
irf xxxxx | -31 -8 -35 -80 1 | -1 16
jpl uuuuu | -24 -16 -98 -124 -19 | 26 29
mit uuuuu | -4 34 -12 -141 0 | 10 19
ngs uuxuu | 39 9 -353 206 1 | 8 18
sio uuuux | -24 65 -340 -230 4 | 40 43
Table 7.2083.5 GPS week: 2083 Day: 5 MJD: 58830.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -45 101 125 -3 | 11 18
emr uuuuu | 24 67 -22 32 7 | 32 36
esa uuuuu | -7 -19 114 -15 -1 | 21 25
gfz uuuuu | -33 -8 203 -78 4 | 19 23
grg uuuuu | 51 4 -102 32 -1 | 1 11
igr xxxxx | 8 27 -29 38 -2 | 6 14
irf xxxxx | -22 -32 -15 -85 -3 | 3 15
jpl uuuuu | -56 90 -256 -143 20 | 27 29
mit uuuuu | -21 -8 17 -188 0 | 13 20
ngs uuxuu | 59 -37 -137 223 -6 | 12 18
sio uuuux | -51 8 -221 -208 18 | 43 46
Table 7.2083.6 GPS week: 2083 Day: 6 MJD: 58831.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 3 -15 135 200 -2 | 8 16
emr uuuuu | 1 26 -87 -120 23 | 31 35
esa uuuuu | -4 5 59 18 6 | 20 23
gfz uuuuu | -18 -9 21 -44 11 | 18 22
grg uuuuu | 42 37 -58 -26 -3 | -2 11
igr xxxxx | -11 18 -11 33 4 | 4 13
irf xxxxx | -34 -30 28 -115 0 | 1 15
jpl uuuuu | -92 -7 -50 -134 1 | 27 30
mit uuuuu | -43 -12 120 -192 -1 | 11 19
ngs uuxuu | 121 -19 165 223 -5 | 10 17
sio uuuux | -73 27 -276 -300 5 | 43 46
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