[IGSREPORT-21425] Wk 1714 IGS Final Orbits [Resubmission]
IGS ACC
igs.acc at noaa.gov
Mon Dec 17 08:15:04 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1714 (Nov 11, 2012 - Nov 17, 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 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:
igs1714[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1714[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1714[0-6].cls IGS GPS clock combination summary report.
igs17147.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17147.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.
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 | 30 32 10 30 32 KOUC FLRS KOUC
0 | ESA | 10 30 32 10 30 32
0 | GFZ | 10 30 32 BOGT CRO1 LHAZ PIMO
0 | GRG | BOGT CAGZ THTI
1 | COD | 10 30 32 10 30 32 KOUC KOUC
1 | EMR | MATE
1 | ESA | 10 30 32 10 30 32 KELY
1 | GFZ | 10 30 32 ADIS BOGT LHAZ NRMD
1 | GRG | MATE MCM4 SCH2 WSRT ASPA MCM4 NYAL TRO1 WSRT
1 | JPL | 10
1 | MIT | 10 NYAL NYAL
2 | COD | 10 30 32 10 30 32 KOUC HNPT KOUC
2 | EMR | HERS SYOG
2 | ESA | 10 30 32 10 30 32
2 | GFZ | 10 30 32 BOGT BRFT JPLM LHAZ
2 | GRG | NTUS
2 | JPL | 24 30 SYOG
2 | MIT | 30 30
3 | COD | 30 32 30 32 KOUC HERT JOZ2 KOUC
3 | EMR | 10 10 WHIT WHIT WUHN
3 | ESA | 30 32 30 32 CHUR HOFN UNSA
3 | GFZ | 30 32 BOGT YAKT
3 | GRG | 10 10 LPGS MAC1 IISC LPGS
3 | JPL | 1 10 24 MAC1 TIXI WHIT
3 | MIT | SCH2 MAC1 SCH2
4 | COD | 30 32 30 32 KOUC
4 | ESA | 1 2 3 4 5 6 7 8 10 11 12 13 14 15 16 17 18 19 20
4 | ESA | 21 22 23 24 25 26 28 29 30 31 32 1 2 3 4 5 6 7 8
4 | ESA | 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26
4 | ESA | 28 29 30 31 32 AREQ AREQ
4 | GFZ | 12 30 32 BOGT
4 | GRG | LPGS MATE
4 | JPL | 10 12 24 32
4 | MIT | 6 12
5 | COD | 30 32 30 32 KOUC WROC KOUC WROC
5 | EMR | HERS TLSE HERS TLSE
5 | ESA | 30 32 30 32 DARW UNSA
5 | GFZ | 30 32 BOGT HOLM SOFI
5 | GRG | NICO ADIS ALIC AMC2 ARTU ASPA AUCK BARH BRUX CAS1
5 | GRG | CEDU CHTI COCO CONZ DARW DAV1 DUBO FAIR GOLD GOPE
5 | GRG | GUUG HOB2 HOFN IISC IRKT KARR KIT3 KOKB KOUC LAMA
5 | GRG | LHAZ MAC1 MAL2 MAR6 MAS1 MAW1 MBAR MCM4 MDVJ MKEA
5 | GRG | NICO NRIL NRMD NTUS NYAL OHI2 ONSA PALM PIMO POL2
5 | GRG | POTS QAQ1 RESO SEY1 SPT0 SYOG THU3 TIDB TIXI TNML
5 | GRG | TOW2 WSRT XMIS YELL ZECK
5 | JPL | 24
5 | MIT | 30 30 USNO USNO
6 | COD | 32 32 HERT KOUC HERT KOUC
6 | ESA | 32 32 UNSA
6 | GFZ | 30 32 BOGT COCO KERG METS NYAL RESO SCOR STJO WES2
6 | GFZ | YAKT
6 | GRG | USNO NRMD USNO
6 | JPL | 24 32
6 | MIT | 30 30
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
----+--------+---------------
1 | SIO | ALL (high Transformation - See Table 2)
6 | SIO | ALL (high Transformation - See Table 2)
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 G10 | | | | | 1 | 1 | |
PRN G30 | | | | 1 | | | |
PRN G32 | | | | | | | 1 |
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.
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 | -.7 1.5 -.8 -48 -9 9 -.13
EMR | 0 | 6.3 10.8 1.0 11 21 -7 .15
ESA | 0 | 3.8 6.8 -16.9 127 -295 132 -.32
GFZ | 0 | .4 .8 -.4 -60 -66 -27 -.05
GRG | 0 | -2.4 7.2 15.6 -11 24 -25 .25
JPL | 0 | 3.2 4.0 8.3 12 -29 4 .17
MIT | 0 | 4.3 8.9 -2.4 -9 3 -22 .06
NGS | 0 | -3.6 3.5 -1.8 11 13 -23 .44
SIO | 0 | 5.9 6.8 -43.4 147 -299 -134 -.06
COD | 1 | -.9 1.2 -1.4 -55 -14 -2 -.16
EMR | 1 | -.3 4.1 1.3 7 8 5 -.04
ESA | 1 | 1.4 2.1 -16.1 66 -246 117 -.10
GFZ | 1 | .4 1.0 -.5 -71 -84 -25 -.07
GRG | 1 | 4.6 4.0 6.9 -14 38 -27 -.09
JPL | 1 | 4.4 3.4 10.5 -29 6 1 -.01
MIT | 1 | 5.7 7.8 -1.9 2 2 -32 .04
NGS | 1 | 1.8 -1.2 4.6 -41 -7 16 .09
SIO | 1 | 4.2 4.2 -49.6 121 -376 -301 .07
COD | 2 | -1.1 1.1 -1.0 -56 3 -17 -.18
EMR | 2 | 1.6 8.0 1.8 11 19 5 .10
ESA | 2 | 3.5 3.6 -15.5 108 -266 126 -.18
GFZ | 2 | .7 1.4 -.9 -44 -68 -1 -.17
GRG | 2 | 5.3 -.6 17.2 -46 111 -85 -.05
JPL | 2 | 2.3 -.7 12.7 -73 4 -29 .02
MIT | 2 | 6.7 9.3 -.1 -3 1 -31 .03
NGS | 2 | -7.5 1.6 -5.3 30 32 -54 .58
SIO | 2 | 1.8 5.2 -50.5 172 -323 -197 .13
COD | 3 | -.7 1.0 -.3 -42 4 -5 -.03
EMR | 3 | 4.5 6.0 -2.5 -3 8 8 .20
ESA | 3 | 4.7 5.2 -12.9 112 -249 110 -.04
GFZ | 3 | .9 1.7 -.4 -23 -58 -11 .02
GRG | 3 | 2.7 8.2 15.6 -31 16 -26 .32
JPL | 3 | 7.0 5.2 11.0 -78 15 8 .43
MIT | 3 | 5.9 6.0 2.2 -5 5 -25 .06
NGS | 3 | 5.0 .4 3.3 -24 -20 43 .34
SIO | 3 | 2.6 8.3 -40.8 88 -314 -224 .23
COD | 4 | -.4 1.2 -1.0 -49 -13 13 .03
EMR | 4 | 3.4 10.1 -3.3 -1 9 -2 .01
ESA | 4 | 6.5 10.8 -16.2 204 -308 98 -.05
GFZ | 4 | .7 1.5 -.6 -37 -69 -19 -.07
GRG | 4 | 6.6 9.7 5.9 -25 52 -43 .35
JPL | 4 | -1.7 12.1 10.9 -15 17 -53 .40
MIT | 4 | 7.2 10.7 -2.0 -15 0 -19 .14
NGS | 4 | 9.0 8.5 -2.7 48 -38 94 .14
SIO | 4 | 2.3 8.8 -54.5 211 -325 -262 .09
COD | 5 | -.5 .5 -1.3 -59 2 16 .04
EMR | 5 | 3.5 6.8 -.3 -2 5 -3 .13
ESA | 5 | 4.0 5.7 -11.2 131 -238 120 .13
GFZ | 5 | .3 1.4 -.8 -42 -53 -36 -.08
GRG | 5 | -2.7 8.6 -1.6 -25 55 -49 .19
JPL | 5 | -2.8 8.0 6.3 -10 9 -9 .24
MIT | 5 | 5.3 7.6 .0 -6 -4 -24 .08
NGS | 5 | 2.8 4.3 -6.2 55 -5 35 .49
SIO | 5 | 3.8 10.0 -63.1 206 -370 -175 .08
COD | 6 | -.3 .5 -.3 -61 -3 3 -.10
EMR | 6 | 7.6 10.7 -1.9 -1 7 -1 .12
ESA | 6 | 6.2 5.5 -13.4 134 -291 115 -.04
GFZ | 6 | .4 1.1 -.8 -39 -59 -32 -.05
GRG | 6 | 1.1 4.6 1.5 -39 70 -53 .37
JPL | 6 | 2.2 2.3 10.5 -83 25 82 .28
MIT | 6 | 7.7 5.5 .2 -5 -3 -23 .11
NGS | 6 | 10.8 -2.0 -4.0 19 -36 100 .52
SIO | 6 | 6.9 2.5 -62.8 151 -450 -30 .12
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.
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 1.1714.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1714.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 2.1714.[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 3.1714.[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 5.1714.0-6). 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 1714 summary. (Nov 11, 2012 - Nov 17, 2012)
Table 1.1714.a GPS week: 1714 MJD: 56242.000-56248.000
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 261| 0 0 4 -7 71 18 -.41 11 10 | -250 -1005 18 81
| 0 0 1 17 13 14 .02 | 375 795
emr 79| -2 0 0 -28 60 -1 .27 16 16 | 2921 -690 16 102
| 0 1 1 15 15 18 .04 | 1944 731
esa 172| 1 0 1 99 -122 9 .07 7 6 | -1121 1070 25 113
| 0 0 1 30 20 12 .02 | 1273 1633
gfz 193| -1 -1 -3 -86 -42 16 -.43 12 11 | 60 5 20 127
| 0 0 1 48 70 24 .05 | 371 693
grg 130| 0 0 0 -14 101 -21 .40 16 15 | 10 22 18 164
| 1 1 4 30 36 26 .05 | 221 488
igr n/a| 0 0 0 -44 108 -28 -.17 5 4 | 12720 -508 18 83
| 0 0 0 28 18 15 .03 | 1211 709
jpl 80| 0 -1 0 -3 51 0 .33 15 14 | 3288 -564 18 113
| 0 1 1 18 22 14 .03 | 1487 721
mit 239| 0 0 -3 -32 50 -8 -.20 7 7 | -43 -63 20 188
| 0 0 0 27 23 31 .02 | 278 515
ngs 238| 0 0 0 -86 85 33 .39 10 9 | -242 -1053 1896 3469
| 0 0 1 43 23 20 .03 | 328 730
sio 276| -1 0 3 127 -271 -197 -.25 18 17 | --- --- --- ---
| 1 1 1 35 58 86 .04 | --- ---
Table 1.1714.b GPS week : 1714 MJD: 56242.000-56248.000
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 4 4 5 4 3 4 |
2 | 4 4 4 4 4 4 4 |
3 | 4 3 4 3 3 4 4 |
4 | 4 3 4 4 4 4 3 |
5 | 4 5 4 4 4 4 4 |
6 | 3 3 3 3 3 4 4 |
7 | 4 4 4 4 4 4 5 |
8 | 3 3 3 3 3 3 4 |
9 | 3 3 4 3 0 3 4 |
10 | 5 5 5 6 6 5 5 |
11 | 4 4 4 4 4 3 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 5 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 4 4 4 4 4 4 5 |
17 | 5 5 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 5 5 5 4 |
20 | 4 4 5 4 4 3 4 |
21 | 4 3 4 4 4 4 10 |
22 | 3 3 3 3 3 3 3 |
23 | 5 5 0 5 4 4 4 |
24 | 6 6 7 5 5 4 5 |
25 | 4 5 5 4 4 4 4 |
26 | 3 4 4 3 3 3 4 |
27 | 0 0 0 0 0 0 0 |
28 | 4 4 4 3 3 3 3 |
29 | 5 5 4 4 4 4 4 |
30 | 5 5 5 5 6 5 6 |
31 | 5 4 4 5 4 4 5 |
32 | 7 6 5 5 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 2.1714.0 GPS week: 1714 Day: 0 MJD: 56242.000
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 262| -1 -1 4 -7 61 27 -.42 11 10 | -398 -1169 21 83
emr 80| -1 0 0 -39 37 0 .30 16 16 | 5965 -406 13 87
esa 172| 2 0 0 115 -147 13 .05 6 6 | -387 831 11 104
gfz 192| -1 0 -2 -148 -26 10 -.47 11 10 | 437 -242 21 128
grg 130| 0 1 2 2 71 -2 .45 14 13 | 11 628 14 157
igr n/a| 0 0 0 -17 80 -29 -.18 5 5 | 14003 404 17 75
jpl 80| 0 0 0 -5 73 0 .38 15 15 | 5274 -141 16 107
mit 240| 0 0 -3 -65 65 -20 -.23 8 8 | 17 161 21 234
ngs 245| 0 0 0 -27 122 27 .36 10 8 | -459 -1076 1772 3478
sio 272| -1 -1 3 102 -221 -133 -.28 18 17 | --- --- --- ---
Table 2.1714.1 GPS week: 1714 Day: 1 MJD: 56243.000
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 259| 0 0 2 23 69 1 -.42 12 10 | -479 -766 20 85
emr 80| -2 -2 1 -4 57 -7 .22 16 16 | 4532 -1071 14 96
esa 172| 1 0 0 70 -91 10 .09 6 6 | -1673 932 11 96
gfz 194| -2 -1 -1 -62 -107 2 -.45 10 9 | 231 -631 20 113
grg 129| 0 0 4 39 77 20 .45 14 13 | 185 -244 18 178
igr n/a| 0 0 0 4 120 -44 -.17 4 4 | 13466 -256 19 78
jpl 80| 0 -1 0 14 78 -9 .30 14 13 | 4232 -665 16 106
mit 240| 0 0 -3 -16 32 -30 -.21 8 7 | 171 -392 20 191
ngs 241| 0 1 2 -124 68 23 .41 12 10 | -397 -853 1947 3610
sio 284| 0 -1 4 135 -326 -311 -.28 18 16 | --- --- --- ---
Table 2.1714.2 GPS week: 1714 Day: 2 MJD: 56244.000
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 261| 0 0 2 -30 67 23 -.40 10 9 | -401 -813 17 85
emr 80| -2 1 4 -36 57 4 .29 16 16 | 3619 -1073 16 111
esa 172| 1 0 0 71 -123 25 .05 5 5 | -2594 2379 12 105
gfz 196| -2 -1 -3 -52 -70 33 -.43 12 11 | -155 210 20 120
grg 130| 1 -1 4 -47 157 -50 .42 15 14 | 35 -425 18 167
igr n/a| 0 0 1 -62 131 -10 -.21 5 5 | 13703 -705 19 83
jpl 80| -1 0 0 -12 57 1 .32 14 14 | 4119 -672 18 110
mit 239| 0 0 -2 -42 73 -45 -.20 8 8 | 34 -163 18 153
ngs 239| 0 0 -3 -46 107 53 .41 10 9 | -334 -952 1753 3781
sio 275| -1 0 5 141 -241 -171 -.32 18 17 | --- --- --- ---
Table 2.1714.3 GPS week: 1714 Day: 3 MJD: 56245.000
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 261| 0 0 4 -2 99 28 -.38 10 9 | -262 -604 18 81
emr 80| -3 -1 -1 -15 73 12 .24 16 16 | 3115 -1763 18 117
esa 172| 2 0 2 92 -105 21 .10 6 6 | 1000 -986 11 99
gfz 193| -1 -1 -3 -78 -51 37 -.47 14 15 | 520 -202 21 136
grg 132| 0 1 0 -6 54 0 .43 16 15 | 159 87 15 160
igr n/a| 0 0 0 -44 119 -8 -.19 5 5 | 13537 -1640 18 85
jpl 80| 0 -1 -1 -3 59 29 .29 16 16 | 4102 -1910 21 132
mit 240| 0 0 -2 -33 25 -32 -.21 7 7 | -61 194 24 204
ngs 235| 1 0 0 -77 80 55 .44 11 10 | -324 -565 1955 3278
sio 260| 0 0 2 58 -254 -241 -.27 17 17 | --- --- --- ---
Table 2.1714.4 GPS week: 1714 Day: 4 MJD: 56246.000
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 265| 0 0 5 4 64 30 -.42 11 11 | -531 -496 17 82
emr 79| -1 0 -1 -18 86 16 .25 16 16 | 1198 349 17 104
esa 172| 1 0 1 151 -137 -2 .07 6 5 | -2520 3900 103 180
gfz 196| -2 0 -4 -161 51 43 -.44 11 11 | -490 1169 22 140
grg 131| 0 1 2 -44 125 -39 .36 16 15 | -463 738 15 136
igr n/a| 0 0 0 -49 120 -21 -.17 4 4 | 11676 210 20 93
jpl 80| -1 -3 0 14 20 5 .34 14 14 | 1895 309 21 109
mit 239| 0 0 -3 -64 65 9 -.19 8 7 | -640 870 20 170
ngs 238| 1 1 0 -137 81 54 .35 10 8 | -478 -635 2057 3839
sio 281| 0 0 2 144 -227 -270 -.22 17 16 | --- --- --- ---
Table 2.1714.5 GPS week: 1714 Day: 5 MJD: 56247.000
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 4 -21 61 26 -.38 10 9 | -250 -463 16 71
emr 80| 0 1 1 -50 54 2 .31 16 16 | 873 -925 18 103
esa 172| 1 0 3 73 -112 10 .10 6 6 | -607 -295 14 99
gfz 193| 0 0 -5 -71 43 17 -.37 11 11 | 123 -821 18 109
grg 131| -2 0 -8 -37 125 -38 .33 19 18 | 10 -473 32 187
igr n/a| 0 0 0 -68 94 -33 -.14 4 4 | 11246 -1049 18 66
jpl 80| 0 -2 2 -37 23 -4 .35 14 13 | 1486 -834 18 101
mit 240| 0 0 -2 -22 71 19 -.17 7 6 | -13 -525 19 172
ngs 238| 0 0 -2 -65 53 14 .40 11 10 | -172 -638 1768 3070
sio 282| -2 2 3 163 -252 -200 -.20 17 17 | --- --- --- ---
Table 2.1714.6 GPS week: 1714 Day: 6 MJD: 56248.000
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 261| 0 0 6 -15 80 -6 -.43 11 11 | 569 -2726 19 86
emr 80| -1 1 0 -32 55 -38 .31 16 16 | 1151 55 17 101
esa 172| 1 0 4 118 -140 -10 .06 12 7 | -1068 730 13 111
gfz 189| -2 -1 -5 -33 -134 -26 -.36 12 11 | -246 552 22 143
grg 131| 0 0 -3 -10 101 -36 .36 17 16 | 138 -151 17 165
igr n/a| 0 0 0 -70 94 -50 -.14 4 4 | 11412 -522 18 103
jpl 80| 0 -2 -2 6 50 -18 .31 14 14 | 1912 -38 18 130
mit 240| 0 0 -3 13 19 40 -.20 6 6 | 187 -590 22 197
ngs 236| 1 0 0 -127 82 7 .39 10 10 | 465 -2656 2020 3227
sio 279| -3 0 2 144 -377 -56 -.21 20 21 | --- --- --- ---
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 3.1714.0 GPS week: 1714 Day: 0 MJD: 56242.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 14 13 8 11 12 5 13 7 7 10 3 | 49 57 60 50 65 56 69 56 58 54 57
2 | 10 14 4 11 9 4 14 8 9 24 3 | 19 28 22 20 23 21 27 22 25 22 22
3 | 8 11 7 10 15 3 11 6 11 18 3 | 36 38 35 42 41 36 38 38 35 36 39
4 | 9 8 5 10 12 5 9 6 8 36 4 | 36 36 38 45 40 40 35 39 38 38 38
5E | 7 16 5 13 11 4 18 9 9 17 3 | 22 29 25 28 28 24 27 26 26 32 25
6 | 9 9 6 10 11 3 9 8 8 15 3 | 17 17 18 24 23 19 18 21 20 22 19
7 | 9 15 7 12 18 3 13 8 8 17 3 | 30 35 30 29 32 29 35 32 34 33 29
8 | 8 10 5 9 16 5 12 6 4 17 3 | 18 18 16 17 20 16 17 17 18 23 16
9 | 7 13 6 10 10 3 11 6 7 15 3 | 13 23 14 17 18 14 21 15 19 13 17
10E | 14 23 5 8 16 8 19 10 10 16 4 | 33 82 85 87 84 86 83 88 83 85 29
11 | 10 15 6 9 15 5 14 6 10 17 3 | 36 48 39 34 49 38 48 38 36 32 38
12E | 14 21 7 10 20 5 24 8 10 13 4 | 18 32 20 17 31 19 29 23 29 23 22
13 | 10 14 6 13 20 5 14 9 7 15 4 | 32 38 33 32 39 31 38 30 35 34 31
14 | 9 19 9 10 15 4 16 7 6 14 3 | 24 33 21 19 29 20 28 23 22 19 22
15 | 8 16 5 9 14 7 18 7 10 13 3 | 26 33 25 23 34 24 32 26 32 26 26
16E | 9 16 7 11 18 3 17 8 10 15 4 | 22 26 20 19 27 17 26 20 21 22 20
17 | 11 17 8 13 9 5 20 9 8 25 4 | 23 26 23 29 25 23 24 25 24 29 24
18E | 8 12 5 11 16 4 12 7 10 13 3 | 26 22 19 20 25 19 21 18 20 24 20
19 | 9 16 6 11 12 5 16 7 8 23 4 | 18 23 23 19 26 19 23 20 23 23 20
20E | 10 10 4 9 11 4 13 9 12 14 3 | 39 41 40 44 38 38 39 39 39 46 39
21 | 10 15 5 9 9 4 13 7 8 23 3 | 16 28 17 14 26 15 26 16 20 19 17
22E | 9 12 7 9 10 4 10 8 7 13 3 | 23 21 18 22 19 18 18 18 19 24 19
23 | 11 17 6 13 16 6 20 10 12 22 4 | 16 22 10 11 7 9 17 14 12 7 15
X24 | 13 --- 7 --- 15 8 --- 5 --- --- 5 | --- --- 56 --- 52 56 --- 55 --- --- 55
25E | 11 23 6 14 12 5 17 8 12 12 4 | 24 31 29 33 38 28 38 30 31 37 30
26 | 8 13 5 12 9 4 11 8 7 16 3 | 18 27 17 25 23 19 21 21 23 21 22
X27E | 8 --- --- --- --- 50 --- --- --- --- 0 | 41 --- --- --- --- 23 --- --- --- --- 44
28E | 8 16 6 10 19 5 13 9 7 13 3 | 21 31 21 21 32 23 27 26 27 24 24
29 | 13 18 9 12 11 6 17 8 8 26 4 | 25 26 18 20 20 20 22 24 24 23 20
30E | 14 16 7 12 15 5 17 8 15 14 4 | 21 25 19 28 22 17 26 22 19 22 19
31 | 13 19 5 11 18 5 19 10 11 14 4 | 19 28 14 17 25 13 25 15 22 17 14
32E | 30 21 12 13 16 8 19 15 19 14 6 | 135 146 139 133 140 138 145 136 143 134 138
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 6 11 14 5 15 8 10 18 |T 28 35 31 31 35 30 34 32 32 32 30
WRMS | 10 16 6 10 13 5 15 8 8 17 |NE 24 29 26 26 31 26 29 28 27 26 27
MEDI | 9 15 6 11 15 5 14 8 8 15 |MD 23 28 22 23 28 21 27 24 24 24 22
Table 3.1714.1 GPS week: 1714 Day: 1 MJD: 56243.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 17 8 8 12 4 14 6 12 9 4 | 34 39 45 35 52 39 55 40 48 39 42
2 | 7 15 4 11 10 3 14 7 13 24 3 | 11 20 16 16 17 12 21 14 23 21 14
3 | 6 10 6 9 13 3 10 6 8 16 3 | 19 19 20 16 20 16 21 16 22 18 16
4 | 9 9 6 10 9 5 9 7 13 31 3 | 30 30 31 37 30 30 28 31 25 30 30
5E | 12 15 5 12 14 4 17 10 17 19 4 | 28 28 24 28 28 23 26 24 31 27 25
6 | 8 10 5 7 10 2 9 9 8 16 3 | 17 15 15 23 17 16 15 21 16 19 16
7 | 8 16 6 9 15 4 14 6 12 16 3 | 34 36 31 34 41 31 33 33 37 34 33
8 | 9 12 5 5 15 3 13 6 10 16 3 | 20 19 18 20 20 18 17 18 23 23 17
9 | 7 12 5 7 11 5 14 6 9 14 3 | 11 19 14 19 16 11 18 13 19 16 14
10E | 16 24 7 9 12 7 19 8 10 15 4 | 38 82 83 84 76 85 80 84 79 83 32
11 | 6 15 5 8 14 4 13 5 15 17 3 | 26 39 29 27 41 28 39 30 28 26 30
12E | 15 20 6 7 20 4 23 8 12 14 5 | 17 29 19 19 24 15 25 17 27 19 18
13 | 14 14 6 10 20 4 13 8 11 14 4 | 38 44 38 38 49 37 42 38 43 41 38
14 | 9 18 7 9 12 4 14 7 13 13 4 | 18 27 19 15 23 18 23 18 27 15 16
15 | 10 15 5 9 15 4 18 8 12 16 4 | 30 36 29 29 35 29 34 29 36 32 29
16E | 10 19 5 12 17 4 14 8 9 16 4 | 19 25 18 18 24 15 22 16 23 19 16
17 | 15 18 8 12 9 4 17 11 15 25 4 | 26 26 21 22 19 19 25 20 25 23 19
18E | 8 10 6 10 23 3 13 6 10 14 4 | 23 20 17 22 25 18 21 18 18 23 17
19 | 10 13 5 9 10 4 13 7 13 24 3 | 15 20 16 19 18 12 20 17 21 20 15
20E | 12 12 4 10 14 4 10 9 9 14 3 | 58 60 57 59 60 58 58 58 59 63 57
21 | 6 12 4 9 9 3 12 5 10 24 3 | 14 21 17 12 20 14 21 13 18 16 13
22E | 8 12 5 6 10 4 8 6 10 9 2 | 19 22 24 19 26 20 22 20 22 22 19
X23 | 10 18 5 13 --- 6 --- 9 12 --- 4 | 22 22 14 10 --- 10 --- 14 14 --- 21
X24 | 12 --- 7 --- --- 9 --- 8 --- --- 6 | --- --- 52 --- --- 55 --- 51 --- --- 52
25E | 10 25 6 7 16 3 18 8 10 14 4 | 18 24 22 22 30 19 29 22 29 27 21
26 | 7 12 7 10 10 4 13 8 11 15 3 | 16 20 18 20 17 16 18 18 23 19 17
X27E | 8 --- --- --- --- 56 --- --- --- --- 0 | 43 --- --- --- --- 59 --- --- --- --- 47
28E | 9 15 5 7 13 4 10 8 12 10 3 | 22 25 21 20 25 19 24 21 28 21 20
29 | 14 20 6 13 12 4 16 8 12 26 4 | 24 26 18 20 17 19 23 20 26 17 17
30E | 18 19 6 11 18 5 16 8 15 18 5 | 20 26 20 24 21 18 22 20 23 17 17
31 | 16 16 6 12 17 3 13 6 11 15 4 | 25 29 24 22 31 20 28 21 32 21 22
32E | 23 25 12 14 18 6 17 12 15 15 6 | 113 132 118 109 119 114 125 114 121 112 117
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 10 14 4 14 8 12 18 |T 27 32 29 28 32 28 32 28 32 29 27
WRMS | 10 16 6 9 13 4 13 7 10 16 |NE 22 25 24 23 25 23 25 24 26 23 23
MEDI | 10 15 6 9 13 4 14 8 12 16 |MD 22 26 21 22 25 19 24 20 25 22 19
Table 3.1714.2 GPS week: 1714 Day: 2 MJD: 56244.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 14 7 12 10 4 13 5 8 11 3 | 42 47 51 44 55 46 59 46 58 44 49
2M | 7 14 5 12 10 5 14 7 7 24 3 | 22 29 24 24 25 22 27 23 24 32 23
3 | 7 12 3 11 15 5 12 10 8 16 3 | 29 31 27 29 33 27 33 26 36 31 28
4 | 6 10 6 10 10 5 10 7 7 28 3 | 35 32 37 39 36 36 34 36 36 33 35
5E | 8 17 6 12 12 4 17 8 8 16 3 | 27 30 26 30 31 25 32 25 25 32 27
6 | 8 17 4 12 12 5 9 7 8 15 3 | 18 21 19 23 21 16 22 19 27 18 19
7 | 8 15 5 13 17 4 12 7 9 20 3 | 31 34 29 32 40 27 33 28 36 29 30
8 | 6 11 4 10 17 5 12 7 12 15 3 | 15 17 13 20 21 13 17 14 20 19 13
9 | 7 14 7 9 9 4 11 9 12 13 3 | 10 18 13 13 17 13 17 11 21 15 13
10E | 12 24 7 12 21 7 22 9 12 21 5 | 39 80 79 83 82 81 75 81 76 75 34
11 | 6 16 5 11 14 5 15 6 14 17 3 | 29 36 30 35 36 29 37 31 37 29 31
12E | 13 20 8 9 19 5 24 9 9 14 4 | 27 34 29 26 30 27 29 26 34 26 26
13 | 10 14 4 10 20 5 13 7 8 15 3 | 30 40 30 36 47 30 39 31 37 30 33
14M | 10 17 6 12 17 5 13 6 8 13 3 | 24 28 20 20 25 21 27 19 24 20 20
15 | 10 15 4 10 17 4 16 11 10 21 4 | 35 38 32 30 41 31 38 35 39 28 34
16E | 7 15 4 11 17 6 14 6 9 16 3 | 19 28 20 20 28 19 27 20 28 23 21
17 | 12 18 6 13 11 5 17 8 8 22 4 | 27 26 19 26 21 20 24 20 26 22 21
18E | 13 12 5 12 19 4 11 9 10 21 4 | 36 38 35 38 40 35 38 30 42 42 36
19 | 9 15 4 11 15 5 14 8 7 21 3 | 19 23 19 23 24 16 24 20 26 22 20
20E | 17 13 4 14 13 9 16 10 12 19 4 | 106 109 106 114 110 105 107 108 112 100 108
21 | 9 14 5 11 12 4 13 6 10 29 4 | 15 23 14 17 18 12 24 13 17 16 15
22E | 8 12 7 10 12 4 9 5 9 15 3 | 27 26 28 29 25 25 30 26 30 25 27
X23M | 8 --- --- --- --- 65 --- --- --- --- 0 | 39 --- --- --- --- 37 --- --- --- --- 41
X24 | 17 --- 6 --- --- 9 18 10 --- --- 6 | --- --- 56 --- --- 54 45 52 --- --- 56
25E | 14 23 6 9 15 3 19 6 12 15 4 | 20 26 26 28 33 25 36 23 36 30 24
26 | 6 14 5 11 11 4 9 12 14 13 3 | 16 21 13 17 17 12 15 14 20 16 14
X27E | 8 --- --- --- --- 87 --- --- --- --- 0 | 37 --- --- --- --- 51 --- --- --- --- 39
28E | 6 15 4 9 17 5 12 9 10 10 3 | 14 22 15 16 23 14 21 14 26 15 16
29 | 9 17 5 14 14 6 15 7 11 23 4 | 20 25 17 23 20 19 24 21 26 21 19
30E | 16 20 6 16 19 7 17 7 18 18 5 | 22 29 19 27 25 21 27 21 24 22 19
31 | 13 18 4 12 18 3 14 7 10 13 4 | 23 32 21 23 30 19 26 18 30 19 21
32E | 18 20 7 17 18 9 16 12 13 16 5 | 124 135 127 123 132 125 137 121 131 121 127
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 5 12 15 5 14 8 10 18 |T 31 37 33 34 37 32 37 32 38 32 32
WRMS | 9 16 5 11 14 5 14 8 9 17 |NE 23 27 25 25 28 24 29 24 29 23 25
MEDI | 9 15 5 11 15 5 14 7 10 16 |MD 27 29 26 27 30 25 29 23 30 26 26
Table 3.1714.3 GPS week: 1714 Day: 3 MJD: 56245.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 16 8 13 8 5 29 8 13 14 4 | 43 53 54 47 60 52 70 53 54 52 52
2 | 8 13 5 17 13 3 13 6 9 23 3 | 18 26 20 26 24 20 29 23 30 28 22
3 | 6 10 4 16 17 3 9 4 10 18 3 | 16 24 19 29 25 18 21 21 21 16 19
4 | 7 10 5 14 10 6 10 6 11 24 3 | 32 32 31 42 36 37 34 35 37 32 33
5E | 9 15 8 13 10 6 17 7 10 17 3 | 31 38 35 36 37 34 40 38 41 37 35
6 | 6 10 4 16 13 3 9 4 9 17 3 | 18 17 16 24 25 16 20 20 16 16 16
7 | 9 15 6 12 18 3 14 7 8 11 3 | 18 22 19 20 27 17 24 21 22 17 18
8 | 9 10 6 12 13 5 16 7 10 9 3 | 23 21 21 28 23 18 21 22 23 19 21
9 | 8 10 6 12 13 3 12 4 14 11 3 | 10 21 14 14 21 12 22 13 23 12 15
10E | 13 27 10 14 21 7 26 10 10 19 5 | 58 119 123 126 122 124 117 122 120 118 55
11M | 8 16 5 13 13 4 19 6 14 17 4 | 38 48 42 38 50 41 51 41 42 36 41
12E | 16 22 5 14 22 4 25 7 8 12 4 | 18 29 20 22 27 18 30 21 24 18 19
13M | 10 15 6 14 22 5 15 9 16 14 4 | 41 46 42 38 49 40 48 40 45 42 40
14M | 9 19 9 13 17 5 17 7 10 10 4 | 25 30 22 20 27 21 28 21 26 18 20
15 | 8 15 5 11 17 5 20 7 7 15 3 | 21 30 20 21 32 20 32 22 26 24 21
16E | 6 13 5 14 22 6 13 6 11 17 3 | 22 28 23 29 27 21 24 22 24 23 23
17 | 8 19 8 17 12 5 20 6 9 20 4 | 19 25 18 26 21 20 25 19 21 24 18
18E | 11 13 7 15 20 3 12 8 9 15 4 | 22 23 25 26 25 22 22 19 25 21 20
19 | 19 13 5 15 13 6 15 7 11 22 4 | 18 23 18 24 24 20 27 24 22 23 19
20 | 8 10 5 13 24 8 12 6 13 16 3 | 56 60 58 56 57 58 58 57 59 61 56
21 | 6 12 7 14 10 4 14 6 11 25 3 | 14 23 16 16 21 13 23 14 18 14 14
22E | 8 11 7 12 11 4 10 5 10 17 3 | 28 25 26 27 27 24 29 25 27 22 24
X23M | 12 17 7 16 20 5 18 8 16 --- 5 | 30 32 25 20 31 28 34 24 37 --- 32
X24 | 12 --- 7 --- 18 11 18 7 14 --- 5 | --- --- 50 --- 52 50 38 49 27 --- 50
25E | 8 23 8 15 17 5 14 6 9 10 4 | 26 28 26 26 35 26 34 29 32 29 27
26 | 6 10 5 12 10 4 12 7 8 13 3 | 19 29 22 28 21 22 24 24 28 31 24
X27E | 9 --- --- --- --- 143 --- --- --- --- 0 | 41 --- --- --- --- 86 --- --- --- --- 46
28E | 5 13 4 11 19 3 12 4 7 10 3 | 27 30 26 26 31 24 31 24 29 23 25
29 | 11 17 5 18 14 5 18 5 11 19 4 | 27 28 22 29 25 24 26 25 27 21 23
30E | 12 25 6 19 22 11 19 8 14 24 5 | 21 31 21 29 25 24 30 23 27 20 20
31 | 12 19 7 15 17 6 17 8 14 16 4 | 20 31 18 21 27 18 29 18 22 15 17
32E | 13 19 7 13 19 7 16 9 12 14 4 | 132 144 135 129 139 134 147 134 137 133 135
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 6 14 16 5 16 7 11 17 |T 30 37 33 34 37 34 38 33 35 32 31
WRMS | 9 16 6 15 15 5 16 7 10 17 |NE 21 27 23 26 29 23 29 25 25 22 24
MEDI | 9 15 6 14 17 5 15 7 10 16 |MD 23 29 22 26 27 22 29 24 27 23 23
Table 3.1714.4 GPS week: 1714 Day: 4 MJD: 56246.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 15 17 10 8 10 4 14 8 11 13 4 | 46 53 55 48 59 51 62 53 54 50 53
2 | 9 13 4 13 11 5 16 9 8 21 3 | 17 22 16 15 18 13 27 19 20 16 17
3 | 7 10 4 10 14 2 6 5 6 21 3 | 37 37 35 36 37 35 39 37 39 33 36
4 | 10 9 6 8 11 6 11 9 9 25 3 | 31 33 34 37 35 35 35 37 37 34 34
5E | 8 18 7 13 13 5 16 8 8 17 4 | 26 37 29 38 31 29 36 32 33 36 30
6 | 9 12 4 10 13 2 6 7 7 15 3 | 24 24 21 29 26 22 28 27 24 22 24
7 | 8 17 6 11 17 4 15 8 9 15 3 | 26 28 23 23 28 22 29 24 27 19 23
8 | 9 10 4 10 15 4 12 7 7 11 3 | 26 23 22 24 25 23 28 26 25 23 24
X9 | 8 --- --- --- --- 38 --- --- --- --- 0 | 91 --- --- --- --- 74 --- --- --- --- 92
10E | 14 28 9 12 21 8 23 15 6 19 5 | 71 153 152 152 153 154 156 160 146 151 72
11 | 8 16 6 7 13 3 12 7 10 16 3 | 32 41 34 32 39 31 39 35 29 31 33
12E | 10 22 7 9 17 4 22 8 12 12 4 | 20 35 25 21 32 23 34 25 32 23 24
13 | 9 15 4 10 23 3 14 7 7 12 3 | 27 35 26 20 41 25 35 28 30 25 27
14 | 10 16 4 10 17 4 13 6 10 13 3 | 20 27 16 16 27 17 26 19 21 17 18
15 | 14 14 5 9 20 5 18 7 12 15 4 | 24 32 26 23 36 23 37 24 30 23 26
16E | 6 18 5 12 21 4 11 7 8 23 4 | 32 37 33 30 40 32 38 33 38 35 33
17 | 12 18 8 14 12 4 17 8 9 21 4 | 27 29 22 24 24 23 31 28 30 22 24
18E | 12 10 6 11 18 3 13 8 12 16 3 | 30 32 31 35 33 29 31 29 32 31 29
19 | 22 16 6 11 11 6 11 9 9 21 4 | 23 27 22 25 26 22 29 26 22 22 23
20 | 10 9 4 10 20 4 11 8 9 13 3 | 36 38 34 34 35 35 36 38 36 35 35
21 | 7 12 4 10 10 3 16 10 7 23 3 | 14 23 18 14 21 14 28 20 17 18 17
22E | 9 10 4 9 13 4 8 7 9 18 3 | 26 23 24 25 22 21 25 22 23 21 22
X23 | 10 18 5 11 20 6 15 8 12 --- 4 | 31 31 21 16 29 32 32 24 25 --- 31
X24 | 13 --- 9 13 17 7 20 6 12 --- 5 | --- --- 39 15 44 35 44 37 22 --- 37
25E | 10 23 5 12 15 3 15 7 8 11 4 | 23 30 28 27 38 26 37 29 34 29 28
26 | 8 11 5 9 13 4 11 7 12 9 3 | 16 26 17 23 24 17 29 21 23 25 21
X27E | 8 --- --- --- --- 90 --- --- --- --- 0 | 58 --- --- --- --- 58 --- --- --- --- 59
28E | 8 13 5 10 16 3 10 6 8 9 3 | 31 30 27 27 31 28 33 29 33 27 29
29 | 11 15 5 13 15 4 17 8 10 21 4 | 22 29 23 28 24 23 31 29 28 24 24
30E | 17 25 7 19 19 6 18 8 16 26 5 | 24 31 17 28 29 20 30 25 29 18 20
31 | 14 16 4 11 18 4 15 9 11 16 4 | 15 27 14 17 30 14 28 18 21 18 17
32E | 13 17 5 13 18 7 16 9 11 13 4 | 129 139 132 124 135 130 138 129 139 131 132
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 6 11 16 4 14 8 10 17 |T 34 39 33 33 39 35 41 36 36 34 34
WRMS | 11 16 5 11 15 4 14 7 8 16 |NE 30 30 26 26 31 28 34 29 28 25 31
MEDI | 10 16 5 10 15 4 14 8 9 16 |MD 26 31 25 25 31 25 32 28 29 24 27
Table 3.1714.5 GPS week: 1714 Day: 5 MJD: 56247.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 16 6 7 11 4 15 4 7 15 3 | 42 46 47 47 54 44 57 42 47 40 46
2 | 8 15 5 14 15 3 14 5 8 21 3 | 19 26 23 23 21 21 26 21 29 25 21
3 | 5 10 6 14 18 2 8 6 10 22 3 | 23 25 22 24 23 22 25 19 30 27 22
4 | 5 10 6 12 14 4 10 9 12 25 3 | 28 26 26 30 32 26 28 29 27 25 27
5 | 12 17 7 12 21 4 18 5 10 19 4 | 34 34 31 32 39 31 36 31 35 28 31
6 | 5 11 5 12 17 5 7 7 12 21 3 | 14 16 13 22 18 13 17 14 21 19 13
7 | 12 17 7 12 21 3 13 7 9 13 4 | 24 29 24 25 32 23 29 23 32 18 24
8 | 5 11 5 11 20 4 12 6 9 10 3 | 21 23 23 21 24 23 25 23 30 20 22
X9 | 7 15 5 6 15 3 --- 5 8 16 3 | 19 19 12 10 12 16 --- 11 18 15 21
10E | 7 23 8 13 22 5 23 13 12 18 5 | 31 92 91 92 98 91 95 95 86 88 32
11 | 6 13 5 8 12 4 12 4 13 17 3 | 27 34 25 31 35 25 33 24 26 21 26
12E | 9 24 5 8 20 4 26 6 9 14 4 | 19 32 23 18 21 22 31 21 32 19 20
13 | 12 14 5 10 27 2 12 7 8 11 3 | 28 37 30 29 49 30 36 28 34 27 30
14 | 8 19 6 8 24 4 12 5 8 13 3 | 17 27 15 17 32 15 20 15 19 17 15
15 | 8 15 6 9 27 5 17 4 15 16 4 | 27 32 25 21 41 23 34 25 37 24 26
16E | 6 19 5 13 17 4 12 7 12 16 3 | 28 33 29 25 32 26 30 26 33 27 27
17 | 11 19 5 14 10 4 16 6 14 20 4 | 20 28 16 20 19 18 25 20 24 15 19
18 | 11 12 4 10 20 3 13 10 10 19 3 | 21 23 20 26 31 19 24 21 22 24 21
19 | 17 16 9 14 13 4 14 7 11 22 4 | 17 22 16 23 18 14 22 17 23 14 16
20 | 8 9 4 11 14 4 10 5 12 14 3 | 34 34 32 33 37 31 32 31 38 32 33
21 | 7 11 5 9 11 4 12 5 11 25 3 | 12 23 23 14 20 15 24 15 22 14 16
22 | 7 10 4 7 19 3 9 6 10 18 3 | 25 25 24 27 32 24 27 27 30 24 25
23 | 12 17 4 12 24 4 13 7 9 14 4 | 20 28 18 18 32 18 24 16 24 9 18
X24 | 10 --- 5 9 20 4 19 6 8 --- 4 | --- --- 39 13 43 39 40 39 23 --- 39
25E | 8 22 6 9 16 3 15 6 12 14 3 | 17 21 24 15 27 20 28 20 27 20 19
26 | 7 12 7 9 16 4 10 8 12 12 3 | 17 25 21 21 25 20 24 20 24 24 21
X27E | 7 --- --- --- --- 105 --- --- --- --- 0 | 91 --- --- --- --- 38 --- --- --- --- 90
28E | 5 14 4 12 19 2 6 6 8 9 3 | 26 32 29 25 28 29 32 28 34 26 28
29 | 14 18 4 10 13 5 16 8 13 20 4 | 25 29 22 22 22 23 27 25 26 24 21
30E | 17 23 7 15 18 6 18 8 16 24 5 | 22 31 23 27 27 23 29 26 30 20 22
31 | 8 15 5 10 22 4 14 9 12 14 3 | 15 28 16 14 31 14 26 15 22 16 15
32E | 12 19 4 10 21 6 14 8 11 15 4 | 145 157 148 141 152 147 156 145 151 150 148
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 6 11 19 4 14 7 11 17 |T 29 34 30 29 35 29 35 29 34 28 29
WRMS | 9 16 6 11 18 4 13 6 10 17 |NE 21 26 23 21 27 22 28 22 27 21 23
MEDI | 8 15 5 10 18 4 13 6 11 16 |MD 23 28 23 23 31 23 28 23 29 24 22
Table 3.1714.6 GPS week: 1714 Day: 6 MJD: 56248.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 13 7 12 11 4 15 3 7 13 3 | 57 67 67 60 75 64 76 63 66 61 64
2 | 9 14 6 13 14 4 12 7 12 22 4 | 20 25 22 25 17 20 24 22 29 27 21
3 | 6 11 6 14 16 3 10 5 9 23 3 | 23 29 25 36 27 27 24 27 32 27 26
4 | 10 9 6 11 13 4 9 6 10 27 3 | 35 37 38 42 43 39 37 38 40 37 37
5 | 8 19 7 10 16 2 14 7 9 20 4 | 29 33 26 30 28 26 34 27 29 33 26
6 | 6 11 5 16 13 2 9 6 10 24 3 | 18 21 19 34 23 23 19 23 26 26 20
7 | 14 16 8 14 19 4 17 6 8 16 4 | 24 30 24 29 32 23 27 22 29 18 24
8 | 12 13 7 11 16 4 12 5 8 10 3 | 20 21 23 26 24 21 24 21 27 18 21
9 | 10 11 8 9 16 3 10 4 8 18 3 | 12 16 11 12 14 14 8 9 19 12 15
10 | 9 25 7 11 12 5 17 11 10 21 4 | 33 90 92 89 93 95 89 91 94 90 28
11 | 8 14 7 9 13 4 12 4 13 20 3 | 37 45 39 42 49 39 45 40 44 34 40
12E | 12 25 7 11 23 4 22 7 12 15 5 | 17 33 22 18 25 22 28 21 33 20 20
13 | 10 12 6 13 22 3 12 6 7 13 3 | 28 40 32 31 48 31 39 30 39 29 32
14 | 9 20 7 13 23 4 9 5 7 16 4 | 23 33 25 23 35 26 25 25 30 27 23
15 | 10 16 6 8 23 4 18 7 9 16 4 | 29 38 29 30 40 30 35 29 39 29 30
16E | 6 17 5 16 22 4 16 7 12 17 4 | 30 37 33 31 35 33 33 32 38 31 30
17 | 7 16 7 13 12 4 16 5 9 23 3 | 23 29 23 27 26 22 30 23 28 28 23
18 | 13 13 6 9 15 4 14 5 10 14 3 | 24 29 28 31 29 29 28 25 30 26 24
19 | 17 18 4 11 13 3 13 6 9 27 4 | 17 26 21 27 23 23 27 24 28 23 21
20 | 9 14 6 12 16 4 12 5 8 15 3 | 41 47 46 45 47 43 41 42 47 42 42
21 | 17 20 54 13 17 12 20 10 15 35 10 | 15 26 48 17 20 19 24 14 27 22 14
22 | 7 12 3 9 17 3 9 4 6 22 3 | 24 23 23 23 24 24 22 23 27 30 20
23 | 12 15 6 14 21 4 14 8 9 16 4 | 30 29 24 17 34 30 26 20 30 9 29
X24 | 12 --- 7 11 22 4 18 6 9 --- 4 | --- --- 43 16 44 42 37 41 25 --- 43
25E | 7 20 9 12 16 3 15 6 10 12 4 | 26 27 30 27 36 29 35 28 37 30 27
26 | 13 11 7 11 14 5 11 6 9 14 3 | 17 19 15 21 20 17 19 16 24 18 15
X27E | 9 --- --- --- --- 130 --- --- --- --- 0 | 72 --- --- --- --- 57 --- --- --- --- 71
28E | 10 15 4 8 13 3 8 5 8 9 3 | 33 37 32 31 34 30 39 30 34 30 32
29 | 8 16 12 13 17 5 17 6 9 24 4 | 21 26 27 24 25 24 26 21 31 26 21
30E | 18 18 10 15 17 6 17 9 17 24 5 | 26 26 24 27 26 21 28 21 29 18 20
31 | 13 17 7 14 23 4 11 9 11 15 4 | 19 30 20 18 30 17 23 15 27 17 16
32E | 12 14 6 13 20 5 17 7 8 21 4 | 132 141 135 129 135 135 141 133 138 143 134
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 12 12 17 4 14 6 10 20 |T 30 37 34 33 37 34 35 32 37 32 31
WRMS | 11 16 7 11 16 4 14 6 10 21 |NE 23 29 28 27 31 27 29 25 31 25 26
MEDI | 10 15 7 12 16 4 14 6 9 17 |MD 24 29 26 27 30 26 28 25 30 27 24
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 4.1714 GPS week: 1714 MJD: 56242.0-56248.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2998 |U 4 5 11 |U 8 9 30 |U 9 7 16 |
emr | emr 2841 | 9 9 19 |U 11 10 31 | 9 10 21 |
esa | esa 2948 | 5 7 11 |U 8 10 29 | 9 8 15 |
gfz | gfz 2881 |U 6 6 11 |U 8 10 31 |U 13 11 22 |
grg | grg 2907 |U 9 10 20 |U 9 12 34 | 13 14 26 |
igr | igr 2917 | 5 6 11 | 7 9 28 | 9 7 15 |
igs | igs 2934 | 7 8 13 | 8 9 28 | 9 9 18 |
jpl | jpl 2881 | 8 8 16 |U 8 11 31 |U 9 9 22 |
mit | mit 2948 | 8 9 16 |U 9 12 32 |U 11 9 21 |
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 5.1714.0 GPS week: 1714 Day: 0 MJD: 56242.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 4 3 10 | 10 8 34 | 8 7 14 |
emr | emr 2868 | 8 10 18 | 10 8 27 | 9 10 19 |
esa | esa 2976 | 5 6 11 | 8 9 26 | 8 8 13 |
gfz | gfz 2866 | 5 6 10 | 8 8 25 | 7 9 15 |
grg | grg 2976 | 11 12 29 | 9 9 34 | 11 12 22 |
igr | igr 2974 | 5 5 9 | 8 9 25 | 8 8 15 |
igs | igs 2973 | 11 13 18 | 8 9 26 | 8 9 17 |
jpl | jpl 2866 | 8 10 15 | 8 9 23 | 7 8 17 |
mit | mit 2976 | 12 14 18 | 8 9 26 | 9 8 19 |
Table 5.1714.1 GPS week: 1714 Day: 1 MJD: 56243.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 | 4 4 13 | 6 9 31 | 8 5 14 |
emr | emr 2868 | 8 8 20 | 8 9 33 | 7 8 18 |
esa | esa 2976 | 5 6 17 | 6 10 32 | 9 5 12 |
gfz | gfz 2869 | 6 6 14 | 6 8 32 | 11 8 18 |
grg | grg 2784 | 9 10 29 | 8 13 36 | 14 12 35 |
igr | igr 2976 | 5 6 14 | 6 9 29 | 8 4 14 |
igs | igs 2938 | 5 5 17 | 6 9 32 | 8 7 12 |
jpl | jpl 2771 | 9 7 18 | 8 12 33 | 9 6 23 |
mit | mit 2976 | 7 6 18 | 6 8 32 | 10 9 17 |
Table 5.1714.2 GPS week: 1714 Day: 2 MJD: 56244.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2949 | 4 9 11 | 8 9 32 | 9 9 20 |
emr | emr 2772 | 11 13 17 | 11 12 35 | 9 9 20 |
esa | esa 2880 | 6 11 12 | 8 11 29 | 9 9 16 |
gfz | gfz 2770 | 6 10 13 | 8 11 33 | 16 15 29 |
grg | grg 2784 | 10 10 20 | 9 14 35 | 12 14 22 |
igr | igr 2862 | 5 10 13 | 8 9 28 | 9 8 15 |
igs | igs 2859 | 9 11 13 | 9 10 32 | 11 10 24 |
jpl | jpl 2868 | 13 11 19 | 9 13 34 | 11 10 23 |
mit | mit 2880 | 9 11 13 | 9 13 35 | 13 10 20 |
Table 5.1714.3 GPS week: 1714 Day: 3 MJD: 56245.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 4 4 11 | 6 7 26 | 10 7 16 |
emr | emr 2868 | 11 9 21 | 12 13 33 | 8 6 17 |
esa | esa 2976 | 5 6 12 | 7 8 28 | 10 8 15 |
gfz | gfz 2869 | 6 7 11 | 7 9 29 | 17 14 23 |
grg | grg 2976 | 10 10 18 | 9 12 35 | 10 13 21 |
igr | igr 2975 | 5 6 11 | 6 7 27 | 10 7 14 |
igs | igs 2961 | 6 7 12 | 6 8 29 | 8 7 13 |
jpl | jpl 2964 | 9 8 16 | 8 11 36 | 8 6 19 |
mit | mit 2976 | 10 10 29 | 12 23 48 | 8 5 18 |
Table 5.1714.4 GPS week: 1714 Day: 4 MJD: 56246.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2926 | 5 8 13 | 8 8 37 | 10 9 17 |
emr | emr 2773 | 10 9 21 | 12 9 35 | 9 9 22 |
esa | esa 2880 | 6 8 11 | 10 9 39 | 9 8 13 |
gfz | gfz 2865 | 7 8 18 | 11 8 44 | 11 10 18 |
grg | grg 2879 | 8 9 15 | 8 9 40 | 22 20 34 |
igr | igr 2878 | 6 8 12 | 9 8 36 | 9 8 13 |
igs | igs 2874 | 6 9 12 | 8 7 33 | 9 9 16 |
jpl | jpl 2866 | 7 8 15 | 9 9 38 | 10 11 26 |
mit | mit 2880 | 6 9 14 | 10 8 31 | 9 10 18 |
Table 5.1714.5 GPS week: 1714 Day: 5 MJD: 56247.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3018 | 4 4 9 | 6 9 24 | 8 6 13 |
emr | emr 2872 | 9 7 15 | 9 8 24 | 9 12 22 |
esa | esa 2976 | 5 6 9 | 6 10 23 | 9 7 11 |
gfz | gfz 2963 | 5 5 8 | 6 10 24 | 13 10 21 |
grg | grg 2976 | 8 8 14 | 6 12 28 | 10 10 20 |
igr | igr 2880 | 5 6 9 | 6 9 24 | 9 7 11 |
igs | igs 2968 | 5 5 8 | 6 9 22 | 10 10 16 |
jpl | jpl 2872 | 7 5 16 | 6 12 23 | 9 10 20 |
mit | mit 2976 | 4 6 9 | 7 9 20 | 11 10 20 |
Table 5.1714.6 GPS week: 1714 Day: 6 MJD: 56248.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3015 | 4 3 8 | 10 11 26 | 10 8 21 |
emr | emr 2872 | 8 5 19 | 12 12 28 | 13 15 28 |
esa | esa 2976 | 5 4 7 | 10 12 28 | 10 9 23 |
gfz | gfz 2967 | 5 5 7 | 9 15 34 | 14 11 27 |
grg | grg 2976 | 9 9 13 | 11 14 28 | 11 19 28 |
igr | igr 2874 | 5 4 8 | 9 12 29 | 10 8 22 |
igs | igs 2968 | 5 5 9 | 10 12 26 | 11 13 26 |
jpl | jpl 2966 | 7 6 16 | 11 14 30 | 10 9 26 |
mit | mit 2976 | 5 6 9 | 10 15 29 | 14 14 33 |
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 6.1714 GPS week: 1714 MJD: 56242.500-56248.500
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 | -8 -26 111 3 2 | 1 17
| 20 21 36 138 2 | 3
emr uuuuu | -18 15 -128 -187 -13 | 26 35
| 18 32 102 162 15 | 4
esa uuuuu | -31 -25 -26 -69 5 | -1 18
| 27 30 53 97 2 | 3
gfz uuuuu | 100 49 25 8 1 | 1 16
| 17 27 116 57 4 | 2
grg uuuux | -18 -21 67 139 -18 | -5 22
| 27 27 60 118 37 | 6
igr xxxxx | -32 22 -6 21 2 | -1 16
| 17 21 61 59 5 | 2
irf xxxxx | 7 -5 33 15 1 | 2 14
| 11 13 16 41 4 | 3
jpl uuuuu | 15 -33 -90 34 -13 | 20 29
| 22 19 85 113 13 | 5
mit uuuuu | 26 1 32 80 2 | -1 14
| 16 18 43 83 9 | 3
ngs uuuuu | -45 53 -12 26 -1 | 3 16
| 39 53 128 64 3 | 2
sio xxuuu | 347 -166 -9 -114 -11 | 27 32
| 36 47 97 146 6 | 3
Table 7.1714.0 GPS week: 1714 Day: 0 MJD: 56242.500
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 | -34 -34 144 -80 7 | -2 18
emr uuuuu | 5 42 -93 -226 7 | 31 38
esa uuuuu | -4 -38 -101 -136 6 | -4 20
gfz uuuuu | 98 67 52 93 2 | 0 17
grg uuuux | 7 -8 83 204 11 | -15 33
igr xxxxx | -17 5 31 -12 10 | -3 18
irf xxxxx | 10 7 18 67 -1 | -1 15
jpl uuuuu | -7 -25 -93 -41 -6 | 27 36
mit uuuuu | 46 33 12 211 -11 | -4 14
ngs uuuuu | -105 -9 73 -2 5 | 3 17
sio xxuuu | 287 -155 -56 -76 -10 | 32 36
Table 7.1714.1 GPS week: 1714 Day: 1 MJD: 56243.500
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 -57 111 -57 2 | -2 19
emr uuuuu | -15 -47 79 -65 -31 | 31 38
esa uuuuu | -72 17 -75 -84 6 | -4 20
gfz uuuuu | 135 69 -138 -54 -2 | 0 17
grg uuuux | -7 -58 -4 184 25 | -12 32
igr xxxxx | -34 -16 -9 38 6 | -3 17
irf xxxxx | 9 -21 11 5 6 | -1 15
jpl uuuuu | 18 -47 -85 135 -33 | 26 34
mit uuuuu | 9 -14 48 33 10 | -4 14
ngs uuuuu | 3 80 167 69 -3 | 3 17
sio xxxxx | 343 -170 75 -173 -18 | 30 35
Table 7.1714.2 GPS week: 1714 Day: 2 MJD: 56244.500
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 -22 165 -154 0 | 0 18
emr uuuuu | -9 4 -129 -58 -24 | 27 36
esa uuuuu | -32 -1 -14 -154 5 | -4 20
gfz uuuuu | 97 51 -65 -21 1 | 0 17
grg uuuux | -29 -6 94 287 3 | -3 23
igr xxxxx | -39 40 -99 80 -4 | -2 17
irf xxxxx | 8 4 33 45 6 | 0 15
jpl uuuuu | 3 -36 -49 145 -15 | 21 31
mit uuuuu | 23 1 74 142 9 | -4 15
ngs uuuuu | -17 9 -65 85 -4 | 3 17
sio xxuuu | 347 -160 -167 20 -10 | 28 33
Table 7.1714.3 GPS week: 1714 Day: 3 MJD: 56245.500
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 | -33 -19 52 -27 2 | 1 18
emr uuuuu | -10 8 -176 -62 -30 | 25 35
esa uuuuu | -55 -16 43 -162 3 | -2 19
gfz uuuuu | 76 3 -40 -63 -3 | 0 17
grg uuuux | 26 0 5 186 -1 | 2 14
igr xxxxx | -42 30 -72 58 1 | -2 17
irf xxxxx | 29 -7 42 41 4 | 1 15
jpl uuuuu | 22 -33 -113 168 -8 | 17 29
mit uuuuu | 47 5 76 124 8 | -2 14
ngs uuuuu | -13 58 -80 9 1 | 1 16
sio xxuuu | 326 -73 -31 -63 -16 | 26 32
Table 7.1714.4 GPS week: 1714 Day: 4 MJD: 56246.500
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 | 8 -39 110 -53 -1 | 3 17
emr uuuuu | -38 43 -209 -147 -2 | 23 35
esa uuuuu | -15 -72 -17 -74 2 | 0 18
gfz uuuuu | 101 79 38 43 0 | 1 17
grg uuuux | -33 12 20 159 -30 | 2 14
igr xxxxx | -60 36 36 -94 2 | -1 17
irf xxxxx | -1 4 37 3 0 | 3 15
jpl uuuuu | 40 -14 -259 -37 6 | 16 28
mit uuuuu | 29 -21 48 69 1 | -1 14
ngs uuuuu | -86 121 108 101 -3 | 2 16
sio xxuuu | 348 -203 4 -18 -1 | 25 32
Table 7.1714.5 GPS week: 1714 Day: 5 MJD: 56247.500
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 | 14 -23 104 193 0 | 3 17
emr uuuuu | -14 38 -226 -242 -5 | 21 32
esa uuuuu | -38 -12 33 41 4 | 0 18
gfz uuuuu | 98 55 130 45 0 | 0 16
grg uuuux | -52 -40 124 -22 -71 | -2 14
igr xxxxx | -20 15 71 13 -4 | -1 16
irf xxxxx | -2 3 29 -2 1 | 3 15
jpl uuuuu | 42 -11 -39 -118 -11 | 14 25
mit uuuuu | 13 7 -47 -3 5 | 0 15
ngs uuuuu | -45 0 -107 -85 -1 | 1 16
sio xxuuu | 385 -216 -24 -74 -12 | 24 29
Table 7.1714.6 GPS week: 1714 Day: 6 MJD: 56248.500
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 | 7 11 93 201 2 | 8 11
emr uuuuu | -46 19 -141 -511 -5 | 25 32
esa uuuuu | 2 -50 -48 87 7 | 5 11
gfz uuuuu | 97 22 199 14 10 | 5 11
grg uuuux | -37 -50 146 -25 -60 | -6 23
igr xxxxx | -13 42 -1 61 4 | 4 10
irf xxxxx | -4 -25 59 -57 -5 | 8 9
jpl uuuuu | -16 -65 10 -13 -27 | 17 25
mit uuuuu | 13 -6 13 -15 -10 | 5 9
ngs uuuuu | -51 109 -180 6 0 | 6 10
sio xxxxx | 394 -185 138 -415 -8 | 27 30
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