[IGSREPORT-21421] Wk 1710 IGS Final Orbits [Resubmission]
IGS ACC
igs.acc at noaa.gov
Mon Dec 17 07:56:23 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1710 (Oct 14, 2012 - Oct 20, 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:
igs1710[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1710[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1710[0-6].cls IGS GPS clock combination summary report.
igs17107.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17107.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 | HOB2 KOUC MATE BRMU HOB2 KOUC MATE SUTM
0 | EMR | LPGS HOB2 LPGS YELL
0 | ESA | HOB2 MATE HOB2 MATE
0 | GFZ | ADIS AREQ BOGT LPGS MATE SANT TIXI
0 | GRG | 13 USNO WSRT BRMU MAC1 MAL2 USNO WIND WSRT
0 | MIT | 19 19 MAC1 SOFI
1 | COD | HNPT KOUC HNPT KOUC
1 | EMR | USNO
1 | ESA | ALRT
1 | GFZ | ALRT BOGT LHAZ SOFI
1 | GRG | 13 13 MCM4 WROC LPGS MCM4 NRMD SOFI VESL WROC WSRT
1 | JPL | NKLG
1 | MIT | 15 JOZ2 USNO ALRT JOZ2 USNO
2 | COD | HOB2 HERT HOB2 JOZ2
2 | EMR | HOB2
2 | ESA | NOVM
2 | GFZ | ARTU ASPA SANT
2 | GRG | AREQ WROC AREQ SOFI WROC
2 | JPL | ARTU
2 | MIT | 27 27 JOZ2 JOZ2
3 | COD | HERT HNPT JOZ2
3 | EMR | KERG MCM4 CRO1 KERG MCM4 YELL
3 | ESA | AREQ
3 | GFZ | BOGT KOSG LHAZ
3 | GRG | NRMD WROC NRMD SOFI THTI WROC
3 | MIT | 7 7 DARW MDVJ SOFI DARW REUN
4 | COD | KOUC MATE KOUC MATE
4 | EMR | 30 MCM4 MCM4
4 | GFZ | 30 BOGT MATE MIZU
4 | GRG | 9 HYDE MATE WROC ALIC ALRT AMC2 ANKR ARTU AUCK BAKE
4 | GRG | BARH BOGT BRFT BRMU BRUX BUCU CAGZ CAS1 CEDU CHPI
4 | GRG | CHTI CHUR COCO CONZ CRO1 DARW DAV1 DRAO DUBO FAIR
4 | GRG | GLSV GOLD GOPE GUAM GUAT GUUG HERT HNPT HOFN HOLM
4 | GRG | HYDE IISC IRKJ IRKT KARR KIT3 KOKB KOUC LAMA LHAZ
4 | GRG | LPGS MAC1 MAL2 MAR6 MAS1 MATE MAW1 MBAR MCM4 MDO1
4 | GRG | MDVJ MKEA NANO NOVM NRC1 NRIL NRMD NTUS NYAL OHI2
4 | GRG | ONSA PALM PDEL PIMO POTS QAQ1 RAMO RESO SCH2 SCOR
4 | GRG | SCUB SEY1 SFER SOFI SPT0 STJO STR1 SYOG THTI THU3
4 | GRG | TIDB TIXI TOW2 TRO1 UNSA URUM USN3 WES2 WHIT WIND
4 | GRG | WROC WSRT WTZR YEBE YELL ZECK
4 | JPL | 30
4 | MIT | 30 30 NICO GMAS NICO
5 | COD | 30 30 KOUC KOUC
5 | EMR | TLSE
5 | ESA | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
5 | ESA | 21 22 23 25 26 28 29 30 31 32 1 2 3 4 5 6 7 8 9 10
5 | ESA | 11 12 13 14 15 16 17 18 19 20 21 22 23 25 26 28 29
5 | ESA | 30 31 32 AREQ AREQ
5 | GFZ | 30 BOGT MDO1 METS SSIA THTI
5 | GRG | ARTU NICO
5 | JPL | 30
5 | MIT | NICO GMAS NICO
6 | COD | HERT KOUC HERT KOUC
6 | EMR | MCM4 TLSE
6 | ESA | AREQ
6 | GFZ | BOGT LHAZ SANT TLSE
6 | GRG | 6 6 MATE PDEL WROC MATE WROC
6 | MIT | MBAR MDVJ MBAR
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 | GRG | 27
6 | GRG | 27
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 G03 | | | | | | 2 | |
PRN G24 | 4 | 2 | 2 | 1 | | | 2 |
PRN G27 | | | | | 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.
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 .9 .6 -66 6 -4 -.16
EMR | 0 | -4.5 .1 13.7 11 6 -6 -.10
ESA | 0 | 2.9 9.4 -9.1 168 -191 92 -.37
GFZ | 0 | -1.0 .2 .6 -55 -22 -25 -.28
GRG | 0 | 4.0 3.0 14.7 -3 56 -18 .04
JPL | 0 | -1.2 10.1 14.6 -61 34 6 .04
MIT | 0 | 5.0 9.5 7.1 10 4 -21 -.17
NGS | 0 | 2.1 -8.7 14.1 -127 -17 -3 .23
COD | 1 | .4 1.0 1.3 -74 1 -2 -.24
EMR | 1 | -5.8 6.9 11.5 12 5 4 -.05
ESA | 1 | 2.5 10.7 -4.9 153 -191 88 -.39
GFZ | 1 | -.6 .1 1.1 -68 -28 -13 -.23
GRG | 1 | -4.1 8.6 10.3 -22 57 -23 -.07
JPL | 1 | -.1 11.5 15.5 7 -2 -7 .17
MIT | 1 | 2.7 9.0 11.0 4 2 -36 -.11
NGS | 1 | -6.9 1.4 8.7 -61 20 -62 -.02
COD | 2 | -.3 1.0 .2 -66 12 -2 -.30
EMR | 2 | -1.3 8.6 7.9 18 5 9 -.04
ESA | 2 | 2.8 13.2 -10.0 211 -200 69 -.34
GFZ | 2 | -.5 .2 .2 -58 -38 -16 -.13
GRG | 2 | -2.7 4.4 11.6 1 29 -25 -.06
JPL | 2 | 4.5 4.2 16.0 -23 -3 30 .41
MIT | 2 | 2.7 12.5 10.3 -5 -3 -22 -.03
NGS | 2 | 3.7 3.6 6.9 -33 -19 28 .28
COD | 3 | -.1 .6 .1 -71 9 -4 -.29
EMR | 3 | 3.5 3.2 11.0 23 5 3 -.07
ESA | 3 | 6.6 9.0 -5.9 185 -226 99 -.26
GFZ | 3 | -.4 1.0 .1 -54 -24 -35 -.10
GRG | 3 | 3.1 10.5 15.7 6 35 -42 -.19
JPL | 3 | .3 1.7 14.9 -21 -1 48 -.04
MIT | 3 | 7.3 6.1 7.8 -4 -6 -23 -.04
NGS | 3 | 3.1 -.2 14.2 -87 -17 19 .25
COD | 4 | -.3 1.2 .1 -56 3 11 -.21
EMR | 4 | 4.5 6.4 8.0 13 -2 8 .08
ESA | 4 | 5.7 1.5 -11.4 67 -264 146 -.20
GFZ | 4 | -.5 .9 .9 -59 -23 -36 -.15
GRG | 4 | 4.3 5.1 18.7 -8 54 -17 -.14
JPL | 4 | 6.2 11.2 18.4 -12 15 30 .13
MIT | 4 | 8.4 6.8 5.6 -2 0 -24 -.11
NGS | 4 | 4.6 1.5 7.3 -43 -24 35 .45
COD | 5 | -.3 1.3 .2 -43 -6 19 -.20
EMR | 5 | 3.9 1.8 5.8 4 0 4 -.05
ESA | 5 | 3.8 2.3 -13.0 103 -223 128 -.43
GFZ | 5 | -.6 .5 .4 -68 -21 -34 -.25
GRG | 5 | 2.9 5.1 8.5 -23 39 -44 -.17
JPL | 5 | 3.3 3.9 15.5 -15 13 48 -.31
MIT | 5 | 8.2 6.9 8.8 -1 3 -32 -.15
NGS | 5 | 2.6 -5.0 5.0 -56 -15 23 .22
COD | 6 | -.5 1.1 -.3 -45 8 15 -.45
EMR | 6 | 6.2 7.5 8.3 0 2 0 .02
ESA | 6 | 6.7 1.2 -7.1 61 -230 123 -.61
GFZ | 6 | -.4 .7 .1 -51 -30 -25 -.23
GRG | 6 | .8 -2.0 16.2 -16 64 -39 -.02
JPL | 6 | 6.9 4.1 20.5 -23 20 -20 .05
MIT | 6 | 9.0 7.8 8.7 -1 1 -32 -.17
NGS | 6 | -1.0 -4.9 10.6 -100 -3 -24 .39
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 1.1710.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1710.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 2.1710.[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 3.1710.[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 5.1710.0-6). 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 1710 summary. (Oct 14, 2012 - Oct 20, 2012)
Table 1.1710.a GPS week: 1710 MJD: 56214.000-56220.000
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 257| 0 0 0 8 50 8 -.45 10 10 | -923 174 19 88
| 0 0 1 26 17 11 .04 | 487 667
emr 79| -1 0 4 -17 31 5 .28 15 15 | 1674 162 20 99
| 1 1 1 13 25 13 .02 | 881 1180
esa 174| 0 0 0 117 -110 -8 .04 7 7 | -1327 1043 25 132
| 0 0 1 49 22 15 .04 | 1450 2339
gfz 189| -2 0 -4 -110 -25 13 -.41 12 12 | -87 293 22 153
| 1 1 1 57 73 25 .02 | 544 748
grg 130| 1 1 6 9 72 -11 .41 16 15 | -161 242 17 158
| 1 1 1 17 14 26 .05 | 277 635
igr n/a| 0 0 -1 -24 77 -24 -.17 4 4 | 4697 32 19 95
| 0 0 1 21 27 14 .02 | 1007 1231
jpl 80| 0 -1 -1 2 43 22 .42 13 13 | 2390 82 20 127
| 1 1 1 17 23 22 .02 | 963 1270
mit 240| 0 0 -3 -26 15 -10 -.18 7 7 | -250 323 21 202
| 0 0 1 26 23 22 .02 | 365 539
ngs 241| 0 0 1 -86 55 -3 .37 11 9 | -921 142 1799 3383
| 0 1 2 28 33 30 .02 | 353 501
sio 276| -1 0 -7 -23 71 -19 -.40 20 19 | --- --- --- ---
| 1 1 1 25 15 11 .03 | --- ---
Table 1.1710.b GPS week : 1710 MJD: 56214.000-56220.000
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 4 4 4 4 |
2 | 4 4 4 4 4 4 5 |
3 | 4 3 4 4 3 6 3 |
4 | 3 3 3 3 4 3 3 |
5 | 5 4 5 4 4 4 5 |
6 | 4 4 4 3 3 3 3 |
7 | 4 4 4 4 4 5 5 |
8 | 4 4 4 4 4 4 4 |
9 | 4 4 4 4 4 4 4 |
10 | 4 4 4 4 4 4 5 |
11 | 4 4 4 4 4 4 4 |
12 | 5 4 5 5 5 5 4 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 5 4 4 4 |
15 | 5 4 4 4 4 5 4 |
16 | 5 5 5 5 5 4 5 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 4 3 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 5 4 5 |
24 | 30 30 36 24 20 29 33 |
25 | 5 5 5 5 5 5 5 |
26 | 4 3 4 3 3 3 3 |
27 | 5 5 7 0 0 0 0 |
28 | 4 4 4 4 4 4 4 |
29 | 5 4 5 4 4 4 5 |
30 | 4 4 4 4 4 4 5 |
31 | 5 5 5 4 5 5 5 |
32 | 4 4 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1710.0 GPS week: 1710 Day: 0 MJD: 56214.000
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 255| 0 0 0 -10 40 1 -.46 9 9 | -995 99 19 107
emr 80| -4 -3 5 -25 22 12 .27 16 16 | 3472 -1891 13 89
esa 174| 0 0 1 123 -104 -14 -.03 7 7 | 280 -2535 11 130
gfz 189| -2 1 -4 -76 -88 11 -.45 13 12 | 991 -1188 19 145
grg 131| 2 0 5 21 67 0 .46 14 13 | 123 -193 15 176
igr n/a| 0 0 -2 -46 73 -31 -.19 4 4 | 6490 -1794 18 99
jpl 80| 0 -3 -2 -20 42 13 .41 14 13 | 4225 -1938 19 126
mit 240| 0 1 -5 3 37 -18 -.18 8 7 | -83 371 24 232
ngs 242| 1 0 2 -138 75 9 .40 10 9 | -971 6 2193 3512
sio 272| 1 0 -8 -12 52 -32 -.40 20 19 | --- --- --- ---
Table 2.1710.1 GPS week: 1710 Day: 1 MJD: 56215.000
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 255| 0 0 -1 23 62 29 -.52 10 10 | -752 328 18 78
emr 80| -1 0 6 -16 54 4 .24 14 14 | 1380 1265 14 82
esa 174| 0 0 3 136 -77 -23 .02 6 6 | -3007 4296 13 123
gfz 190| -2 -1 -4 -191 -114 46 -.40 12 12 | -656 1146 21 156
grg 131| 1 1 8 -20 75 18 .43 15 14 | -538 758 15 129
igr n/a| 0 0 -1 -17 87 -13 -.18 5 4 | 4496 1498 19 91
jpl 80| 1 -3 -2 16 65 42 .38 13 13 | 1958 1480 18 130
mit 240| 0 0 -3 -46 0 -29 -.15 7 7 | -707 1197 22 193
ngs 239| -1 0 -2 -57 41 -4 .36 10 7 | -946 500 1693 3366
sio 270| 1 1 -7 -52 68 -10 -.45 21 19 | --- --- --- ---
Table 2.1710.2 GPS week: 1710 Day: 2 MJD: 56216.000
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 258| 0 0 0 15 43 11 -.45 10 10 | -520 -266 20 80
emr 80| -1 1 5 -25 27 32 .26 15 15 | 1742 374 14 75
esa 174| 0 0 0 188 -110 -32 .02 7 7 | 593 -529 15 139
gfz 189| 0 0 -7 -170 8 48 -.43 12 12 | 181 56 23 153
grg 129| 2 1 6 -3 69 21 .43 15 15 | -67 123 16 163
igr n/a| 0 0 0 -7 63 -6 -.16 4 4 | 5073 404 19 96
jpl 80| 0 -1 -1 2 14 50 .42 13 13 | 2564 505 17 130
mit 240| 0 0 -2 -71 13 -43 -.16 6 6 | 163 -211 20 211
ngs 244| 1 0 2 -64 55 23 .37 11 10 | -569 -197 1542 3372
sio 266| -2 -1 -7 -62 60 -25 -.40 18 19 | --- --- --- ---
Table 2.1710.3 GPS week: 1710 Day: 3 MJD: 56217.000
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 257| 1 0 0 -40 30 0 -.45 9 9 | -709 -677 17 79
emr 79| 0 -1 4 -37 -6 -4 .30 16 16 | 1766 -211 18 93
esa 174| 0 0 0 155 -130 -7 .05 8 7 | -1205 527 14 152
gfz 192| -2 0 -4 -56 87 14 -.38 11 11 | -315 358 21 143
grg 130| 0 2 6 1 66 -49 .47 15 15 | 54 374 16 134
igr n/a| 0 0 -3 -46 42 -9 -.16 5 5 | 5217 -755 16 91
jpl 80| 0 0 0 -7 9 40 .44 14 14 | 2911 -631 17 128
mit 240| 0 0 -3 -29 38 -18 -.16 7 7 | -2 -193 23 194
ngs 245| 0 1 5 -92 -3 27 .38 11 11 | -825 -325 1692 3303
sio 271| -2 1 -9 -7 96 -3 -.41 19 18 | --- --- --- ---
Table 2.1710.4 GPS week: 1710 Day: 4 MJD: 56218.000
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 260| 1 0 1 11 77 -4 -.40 11 10 | -506 -216 25 84
emr 80| 0 -1 4 0 61 0 .25 15 15 | 1189 87 50 125
esa 174| 0 0 0 43 -129 0 .05 6 6 | -870 114 21 123
gfz 193| -3 0 -4 -39 -28 -4 -.43 12 12 | -239 271 27 160
grg 131| 0 0 7 20 87 -18 .36 16 15 | 38 -742 21 221
igr n/a| 0 0 -2 -46 97 -28 -.16 5 4 | 4198 -424 25 99
jpl 80| -1 -3 0 0 60 -10 .40 13 13 | 1957 -421 37 137
mit 240| 0 0 -3 -13 23 6 -.19 8 7 | 60 -164 24 155
ngs 243| 1 1 0 -85 79 10 .35 11 10 | -455 -442 2056 3523
sio 289| -1 1 -6 2 80 -34 -.39 18 20 | --- --- --- ---
Table 2.1710.5 GPS week: 1710 Day: 5 MJD: 56219.000
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 260| 0 0 1 23 62 14 -.46 10 10 | -1916 1355 19 93
emr 79| -1 0 4 -1 49 0 .30 15 15 | 1531 -254 17 130
esa 174| 0 0 0 103 -87 6 .08 7 7 | -2119 2353 93 154
gfz 189| -1 1 -2 -135 -78 -7 -.40 12 12 | -110 570 24 156
grg 130| 1 3 4 12 46 -12 .36 17 16 | -204 152 18 151
igr n/a| 1 0 0 -2 122 -39 -.14 4 4 | 4017 -323 19 100
jpl 80| -1 -1 0 35 69 13 .45 13 13 | 1834 -130 18 120
mit 240| 0 0 -2 -33 -27 5 -.17 6 6 | -628 594 19 209
ngs 242| 0 -2 2 -64 100 -29 .37 12 10 | -1486 708 1625 3257
sio 282| -1 0 -5 -29 61 -15 -.35 20 19 | --- --- --- ---
Table 2.1710.6 GPS week: 1710 Day: 6 MJD: 56220.000
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 256| 2 0 0 39 37 6 -.43 11 11 | -1069 596 21 95
emr 79| 0 0 3 -16 8 -8 .29 15 15 | 638 1766 16 100
esa 174| 1 0 1 72 -136 12 .06 7 7 | -2965 3080 10 106
gfz 185| -3 1 -3 -105 38 -14 -.39 12 12 | -465 842 23 161
grg 130| 0 0 6 31 91 -37 .38 17 17 | -537 1223 18 137
igr n/a| 0 0 0 -4 55 -43 -.16 4 4 | 3390 1623 17 91
jpl 80| -2 0 -3 -3 43 8 .44 14 13 | 1286 1714 17 122
mit 240| 0 0 -1 1 24 22 -.21 6 5 | -554 670 20 223
ngs 237| 0 -1 1 -99 41 -56 .35 10 8 | -1198 747 1798 3354
sio 286| -2 1 -6 0 79 -14 -.42 22 19 | --- --- --- ---
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 3.1710.0 GPS week: 1710 Day: 0 MJD: 56214.000
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 19 9 10 12 4 12 10 9 15 4 | 26 25 33 28 42 29 44 31 38 30 32
2 | 8 18 7 15 13 5 15 8 11 23 4 | 18 28 24 24 28 19 24 19 23 19 20
3 | 8 11 5 14 12 5 11 6 13 25 3 | 26 30 27 24 33 28 31 27 38 22 27
4 | 10 11 5 9 11 3 10 6 11 21 3 | 17 20 21 28 17 20 18 20 20 21 18
5 | 10 19 5 11 17 3 18 9 9 16 4 | 41 49 44 46 48 41 43 43 45 38 42
6 | 9 10 6 16 9 4 9 6 11 17 3 | 20 24 23 27 26 20 28 22 23 23 21
7 | 9 18 7 10 14 3 15 8 9 16 4 | 34 39 33 34 38 36 38 37 37 34 34
8 | 9 13 4 12 13 5 9 10 10 18 3 | 15 20 15 19 16 12 15 14 20 20 13
9 | 10 12 6 14 15 6 9 7 9 17 3 | 13 23 19 20 24 18 24 17 23 18 17
10 | 7 11 5 14 13 3 10 8 12 28 3 | 19 21 18 29 17 20 20 22 26 28 20
11 | 8 13 6 11 16 5 14 6 12 10 4 | 26 38 32 31 45 28 40 28 33 31 31
12 | 9 20 9 12 17 7 17 9 9 17 4 | 35 45 36 37 37 35 37 36 35 38 35
13 | 6 13 6 11 15 4 13 7 10 20 3 | 24 31 27 26 34 24 30 25 25 23 25
14 | 10 13 8 14 15 4 12 5 12 17 4 | 26 30 29 30 32 25 28 25 32 27 26
15 | 11 16 7 12 15 3 18 9 11 20 4 | 25 32 31 28 35 25 31 24 30 17 26
16 | 10 19 6 15 15 5 16 9 11 20 4 | 34 40 32 27 42 30 37 29 36 29 31
17 | 10 17 6 13 12 4 16 8 9 33 4 | 23 28 26 31 24 23 25 22 24 23 22
18 | 7 15 10 14 15 4 14 6 8 13 4 | 28 30 27 32 27 27 29 27 29 29 25
19 | 10 15 7 12 10 3 13 8 12 24 4 | 19 29 24 22 24 20 27 19 24 19 19
20 | 9 14 5 10 13 3 16 7 8 13 3 | 59 62 59 61 64 58 60 57 59 63 59
21 | 6 12 7 12 17 5 11 7 12 15 3 | 17 18 13 21 19 11 17 12 15 14 13
22 | 8 18 8 17 17 5 9 5 7 9 4 | 39 39 36 43 38 36 38 38 36 41 35
23 | 11 14 7 10 12 4 14 7 14 23 4 | 37 40 34 36 38 33 39 34 39 35 35
X24 | 21 --- --- --- 40 72 --- --- --- --- 29 | --- --- --- --- 51 40 --- --- --- --- 87
25 | 11 27 8 10 17 6 15 7 5 24 4 | 35 43 38 34 35 33 37 32 34 43 34
26 | 8 13 7 15 12 4 8 5 13 15 3 | 18 25 25 26 30 19 25 21 21 19 21
X27 | 9 16 9 17 16 7 10 9 --- --- 4 | 27 15 13 17 9999 25 16 13 --- --- 32
28 | 5 16 5 15 17 3 12 6 9 13 3 | 23 30 25 27 32 22 25 23 26 26 23
29 | 12 19 6 12 14 4 18 8 9 31 4 | 26 29 18 26 20 21 27 23 23 22 21
30 | 10 15 6 10 14 4 12 7 8 29 3 | 30 31 29 29 29 27 29 27 30 37 28
31 | 13 21 6 14 17 4 18 8 10 15 4 | 20 26 18 22 28 16 24 14 22 15 16
32 | 11 19 6 10 13 5 12 10 9 22 4 | 27 31 24 28 24 24 32 24 26 29 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 7 13 14 4 14 8 10 20 |T 26 31 27 29 32 26 30 25 29 27 28
WRMS | 9 16 7 12 13 4 13 7 9 19 |NE 20 26 24 25 30 22 27 21 25 21 27
MEDI | 9 15 6 12 14 4 13 7 10 17 |MD 26 30 27 28 32 25 29 24 26 26 25
Table 3.1710.1 GPS week: 1710 Day: 1 MJD: 56215.000
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 19 6 11 12 4 12 5 9 13 4 | 24 22 30 30 39 25 39 28 33 27 29
2M | 9 17 8 13 14 4 13 7 11 30 4 | 26 29 29 29 33 25 28 25 32 31 26
3M | 9 8 5 11 9 3 9 5 6 23 2 | 32 34 33 31 33 31 34 30 37 33 31
4 | 10 9 6 8 11 4 9 7 10 19 3 | 16 16 13 22 14 15 18 17 18 19 14
5 | 8 16 6 8 16 5 15 12 9 13 4 | 28 31 27 27 36 26 31 24 33 24 26
6M | 9 8 5 14 10 3 9 7 11 17 3 | 21 25 22 25 26 21 28 21 31 23 21
7M | 8 15 7 9 24 5 16 7 10 18 4 | 66 68 69 69 58 67 69 67 69 64 66
8 | 10 11 5 11 9 6 12 8 8 15 3 | 16 17 12 16 13 10 19 13 16 20 12
9 | 11 10 5 13 16 6 10 9 8 17 3 | 12 20 13 15 21 14 19 18 20 19 13
10 | 8 13 5 12 12 4 11 8 8 28 3 | 20 22 18 27 20 19 18 20 19 25 18
11 | 6 16 7 10 15 4 9 6 10 11 3 | 21 35 25 26 40 22 33 24 27 25 25
12M | 8 16 6 13 15 4 14 8 11 38 4 | 33 38 33 37 40 30 35 33 36 38 34
13M | 7 12 5 12 21 4 11 6 12 14 3 | 19 28 19 25 33 16 29 19 26 13 21
14M | 10 14 4 16 14 4 14 5 9 16 3 | 28 31 26 27 28 22 29 21 25 28 23
15 | 14 12 5 11 15 6 16 8 7 18 4 | 20 27 21 23 31 19 27 20 26 16 20
16M | 10 17 7 12 20 5 16 7 10 20 4 | 24 31 24 26 33 20 25 20 24 22 22
17 | 8 15 8 13 12 3 14 7 11 31 4 | 14 21 17 25 16 15 21 18 15 21 15
18 | 6 11 5 14 15 3 12 5 10 12 3 | 26 24 24 23 20 23 23 20 28 24 21
19 | 10 13 7 8 8 5 11 6 11 23 3 | 17 21 16 19 17 14 23 13 20 14 14
20E | 14 14 6 14 20 7 12 9 10 11 4 | 81 82 82 78 82 77 81 79 81 79 81
21M | 5 11 6 12 20 4 10 5 10 11 3 | 18 20 13 15 22 13 19 12 19 14 14
22 | 10 13 5 14 16 3 9 5 8 8 3 | 30 28 26 28 27 25 27 23 30 28 24
23M | 9 15 7 11 14 5 15 6 11 25 4 | 29 32 28 22 29 23 32 23 30 29 25
X24 | 20 --- --- --- 42 74 --- --- --- --- 29 | --- --- --- --- 50 52 --- --- --- --- 114
25M | 11 28 8 10 16 7 17 7 12 27 5 | 39 42 36 39 41 34 41 35 35 44 36
26 | 11 10 5 11 11 4 7 6 6 14 3 | 18 23 21 22 25 20 24 21 22 22 19
X27M | 14 14 8 15 >>>> 8 12 9 --- --- 5 | 27 14 15 14 9999 35 17 13 --- --- 29
28 | 6 14 6 16 17 5 10 8 9 10 3 | 19 22 19 26 27 16 20 19 20 21 18
29M | 15 15 7 11 14 4 15 7 6 33 4 | 25 22 16 18 14 16 23 17 20 19 16
30M | 10 13 8 12 15 3 14 6 12 21 4 | 54 51 51 54 54 48 50 52 50 52 52
31 | 11 18 9 14 17 4 19 7 12 11 4 | 17 24 19 20 26 11 27 14 24 16 14
32M | 8 17 6 10 11 5 12 8 8 25 3 | 29 30 29 28 25 25 30 24 30 35 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 6 12 15 5 13 7 10 21 |T 27 30 26 28 31 25 30 25 29 28 28
WRMS | 10 14 6 12 14 4 13 7 7 19 |NE 17 22 18 22 26 19 24 18 21 20 25
MEDI | 10 14 6 12 15 4 12 7 10 17 |MD 24 27 24 26 28 22 27 21 26 24 22
Table 3.1710.2 GPS week: 1710 Day: 2 MJD: 56216.000
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 | 9 18 6 11 15 3 11 6 10 15 3 | 25 24 30 26 39 27 41 29 35 29 29
2 | 8 19 8 14 16 5 16 6 11 23 4 | 23 28 24 26 27 24 27 25 28 27 22
3 | 9 11 5 10 12 3 10 5 14 22 3 | 30 36 31 35 30 30 35 32 33 25 30
4 | 8 12 6 9 12 3 8 6 9 17 3 | 20 21 20 23 18 21 22 25 26 23 19
5 | 10 18 8 11 18 6 17 8 12 15 4 | 29 35 24 27 29 26 32 29 30 29 25
6 | 11 10 6 13 10 3 11 5 15 15 3 | 26 31 26 27 28 23 33 26 23 21 24
7 | 11 14 7 12 17 5 17 8 11 13 4 | 27 32 24 29 33 28 31 33 32 25 26
8 | 9 17 5 12 13 5 11 9 10 14 4 | 16 22 15 20 15 14 20 17 22 22 13
9 | 10 10 8 13 15 5 10 6 6 18 3 | 14 20 20 16 21 15 22 19 22 22 15
10 | 8 16 5 13 14 3 10 7 10 26 3 | 22 25 22 29 19 22 24 24 24 27 21
11 | 9 14 10 7 18 3 9 5 11 15 3 | 23 38 30 29 41 27 38 29 31 31 28
12 | 11 17 6 13 17 5 16 9 11 17 4 | 33 37 35 34 39 31 35 35 34 33 32
13 | 8 13 7 12 17 4 11 4 11 15 3 | 21 30 19 21 35 21 31 23 25 16 21
14 | 10 13 7 10 16 3 13 6 12 16 3 | 26 32 24 25 28 23 30 27 28 29 24
15 | 12 14 7 11 16 4 17 6 9 19 4 | 21 29 24 22 31 21 30 24 29 19 23
16 | 13 18 7 13 16 5 15 7 11 18 4 | 29 35 25 26 33 25 31 27 33 28 26
17 | 13 17 8 13 10 4 16 7 10 28 4 | 22 27 21 28 23 22 27 27 23 26 20
18 | 10 13 5 12 17 4 13 5 12 15 3 | 25 29 25 25 30 28 28 28 33 29 25
19 | 10 13 7 8 10 3 14 6 12 22 3 | 21 26 19 20 20 17 28 22 25 17 18
20E | 8 15 7 11 14 7 14 7 10 13 3 | 59 63 60 58 63 58 63 59 59 61 58
21 | 8 13 5 11 18 4 11 4 12 11 3 | 17 21 14 15 21 13 19 17 20 20 12
22 | 10 13 6 11 18 3 10 6 8 15 3 | 28 25 21 24 28 24 25 25 23 25 22
23 | 10 15 8 10 13 5 16 4 11 21 3 | 33 35 30 30 36 31 39 31 32 31 30
X24 | 25 --- --- --- 48 56 --- --- --- --- 35 | --- --- --- --- 114 84 --- --- --- --- 113
25 | 11 25 8 8 17 4 16 8 11 18 4 | 32 32 35 30 37 31 37 33 36 39 31
26 | 10 10 7 11 12 4 9 6 10 12 3 | 14 19 18 14 22 15 20 17 19 19 15
X27 | 19 --- 8 16 --- 10 13 9 --- --- 6 | 39 --- 12 14 --- 45 21 12 --- --- 36
28 | 8 18 6 14 15 4 13 7 7 11 4 | 21 29 20 26 29 21 28 24 26 25 20
29 | 14 17 8 13 16 5 17 9 13 28 4 | 26 25 20 24 22 19 28 23 24 18 19
30 | 12 13 8 14 17 6 11 8 10 29 4 | 29 34 25 25 29 26 33 27 32 32 26
31 | 12 19 9 14 17 4 18 5 9 12 4 | 24 27 19 20 29 18 27 21 25 17 18
32 | 8 12 8 11 12 7 13 8 11 19 3 | 21 25 23 23 23 21 30 23 24 27 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 7 12 15 4 13 6 11 18 |T 25 29 24 25 32 26 30 26 28 26 26
WRMS | 10 15 7 12 15 4 13 6 10 19 |NE 20 25 21 22 33 25 27 23 25 22 27
MEDI | 10 14 7 12 16 4 13 6 11 16 |MD 25 29 24 25 29 23 30 25 26 25 23
Table 3.1710.3 GPS week: 1710 Day: 3 MJD: 56217.000
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 19 7 12 15 5 11 6 9 16 4 | 34 33 36 32 41 36 45 34 41 37 35
2 | 7 18 10 13 14 5 17 6 11 23 4 | 18 30 24 22 26 23 27 21 26 22 19
3 | 8 9 6 11 12 3 12 6 13 20 3 | 46 53 46 45 49 48 52 48 54 43 47
4 | 7 12 5 9 13 4 10 6 6 19 3 | 21 25 23 23 23 25 25 23 26 22 20
5 | 7 18 7 9 22 4 18 7 9 17 4 | 22 35 24 26 35 25 34 25 29 25 23
6 | 8 10 5 12 10 3 8 5 14 12 3 | 18 31 25 25 27 23 31 23 25 21 22
7 | 11 17 5 13 15 4 17 8 11 13 4 | 41 50 43 42 49 45 47 45 51 44 41
8 | 9 13 5 12 12 5 12 8 11 16 3 | 17 27 16 19 17 21 23 18 25 23 16
9 | 8 14 11 14 14 5 13 7 13 18 4 | 19 29 22 17 28 20 26 19 28 23 17
10 | 8 15 4 10 19 5 10 6 12 27 3 | 29 35 30 32 30 32 31 31 33 34 29
11 | 8 14 8 10 17 4 10 5 16 12 4 | 27 39 31 31 43 31 38 30 39 34 31
12 | 9 20 10 18 21 6 20 8 13 22 5 | 40 46 41 44 41 41 42 41 45 41 39
13 | 7 13 6 13 18 3 13 5 11 13 3 | 27 37 28 30 40 29 37 28 30 23 28
14 | 10 14 11 14 17 6 13 10 13 17 4 | 25 32 29 29 35 28 30 24 31 26 25
15 | 9 12 7 9 15 6 17 7 8 20 3 | 27 34 30 27 37 27 36 24 32 24 26
16 | 13 18 10 12 14 4 16 7 14 19 4 | 28 33 24 23 34 26 32 26 35 27 25
17 | 16 15 6 11 13 2 15 8 10 30 4 | 21 31 26 25 22 25 30 24 29 26 21
18 | 6 16 7 11 16 4 15 6 11 13 4 | 72 71 69 72 73 68 71 68 70 68 69
19 | 9 15 8 10 9 4 12 7 15 22 4 | 20 31 25 23 25 22 26 20 22 20 20
20E | 9 16 7 12 11 5 14 9 12 11 4 | 58 60 57 56 59 59 61 55 58 59 57
21 | 6 11 7 7 17 4 13 6 11 16 3 | 19 25 20 19 27 20 24 19 22 20 19
22 | 7 15 8 12 17 4 10 6 7 14 3 | 48 50 49 52 50 46 47 46 50 47 47
23 | 11 16 8 11 13 5 17 5 10 21 4 | 31 37 30 29 32 31 38 30 32 29 30
X24 | 14 --- --- --- 37 64 --- --- --- --- 24 | --- --- --- --- 141 157 --- --- --- --- 135
25 | 13 25 9 9 21 6 17 8 15 24 5 | 53 54 50 50 49 47 49 47 51 58 48
26 | 6 9 7 10 14 5 9 7 11 12 3 | 22 31 27 28 33 26 28 25 30 24 24
X27 | 7 --- --- --- --- 415 --- --- --- --- 0 | 79 --- --- --- --- 125 --- --- --- --- 82
28 | 7 16 5 13 15 3 13 6 11 12 3 | 23 34 26 26 30 27 32 25 29 24 24
29 | 9 15 8 10 16 5 17 7 12 31 4 | 29 34 31 30 30 30 35 30 32 28 29
30 | 11 12 7 10 14 6 11 6 9 27 3 | 44 43 43 41 40 39 41 41 47 42 42
31 | 9 17 6 12 18 3 18 7 8 15 4 | 20 29 18 19 28 20 27 19 26 18 18
32 | 8 20 8 10 13 4 12 6 10 18 4 | 29 36 26 27 25 29 36 27 32 34 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 8 11 15 5 14 7 11 19 |T 32 37 32 32 39 39 36 31 36 32 35
WRMS | 9 16 7 11 15 5 14 7 11 18 |NE 22 31 25 24 39 36 30 23 29 25 32
MEDI | 8 15 7 11 15 4 13 6 11 17 |MD 27 34 28 28 34 29 34 26 32 26 28
Table 3.1710.4 GPS week: 1710 Day: 4 MJD: 56218.000
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 | 13 20 6 11 15 5 14 6 12 11 4 | 28 21 29 25 40 27 40 29 36 30 31
2 | 8 20 6 14 15 6 16 5 9 22 4 | 18 29 19 20 25 19 26 19 27 21 19
3 | 11 7 2 11 12 4 9 6 10 24 3 | 45 47 47 42 46 45 49 45 47 45 44
4 | 7 12 7 9 15 4 10 8 5 20 3 | 16 19 17 20 15 16 15 18 18 17 16
5E | 9 17 6 9 11 5 19 10 9 18 4 | 31 39 33 34 39 33 41 34 40 36 32
6 | 11 8 4 12 11 3 9 7 12 17 3 | 21 28 24 24 26 22 28 24 28 20 25
7 | 11 16 5 11 18 4 15 8 11 14 4 | 17 25 20 22 30 18 26 19 28 15 20
8 | 7 14 5 13 14 6 14 10 12 18 4 | 13 21 14 14 15 13 18 17 22 22 14
9 | 9 12 7 14 15 5 14 6 11 15 3 | 18 23 19 17 22 16 24 17 24 16 17
10 | 7 17 5 11 21 4 11 7 9 29 4 | 25 29 20 25 31 22 24 25 23 28 23
11 | 8 14 6 10 19 3 9 7 15 8 4 | 23 34 25 26 39 24 34 26 27 26 28
12 | 11 19 6 11 19 6 17 9 14 16 4 | 30 39 35 32 32 35 37 38 38 34 34
13 | 9 14 6 12 18 3 12 7 11 16 4 | 24 29 26 24 35 23 30 26 23 15 24
14 | 11 14 5 20 14 5 12 9 9 15 4 | 23 28 22 28 27 22 28 23 24 20 22
15 | 10 11 6 13 17 4 15 6 13 19 4 | 18 25 21 20 31 18 26 19 25 17 19
16 | 12 21 6 12 15 6 15 10 10 18 4 | 21 28 20 25 29 19 26 26 26 19 22
17 | 10 18 8 12 13 3 16 9 8 28 4 | 17 22 20 24 17 20 22 21 21 22 18
18E | 18 9 5 13 13 9 11 7 10 12 4 | 104 105 104 105 104 101 105 106 103 102 102
19 | 9 12 5 10 10 3 13 8 12 23 3 | 19 25 20 22 18 17 27 21 18 16 20
20E | 11 13 5 11 22 3 14 7 8 13 4 | 36 35 35 35 36 34 35 33 33 35 33
21 | 9 12 4 10 16 3 10 7 11 19 3 | 18 20 14 19 21 15 18 17 19 24 16
22E | 11 10 5 13 16 5 8 7 6 7 3 | 69 72 73 75 75 71 75 74 72 73 70
23 | 14 16 9 12 15 4 16 7 12 23 4 | 25 28 23 23 27 22 28 24 23 15 22
X24 | 15 --- --- --- 27 75 --- --- --- --- 20 | --- --- --- --- 156 162 --- --- --- --- 150
25 | 17 25 7 12 19 4 16 7 11 19 5 | 37 40 38 37 36 38 38 38 39 37 35
26 | 9 9 4 10 13 3 7 6 14 10 3 | 17 21 18 20 26 17 23 19 20 19 17
X27 | 8 --- --- --- --- >>>> --- --- --- --- 0 | 447 --- --- --- --- 568 --- --- --- --- 447
28 | 8 15 6 13 17 4 13 8 9 11 4 | 19 25 21 23 28 21 25 23 23 23 20
29 | 9 15 7 9 15 7 18 10 11 28 4 | 23 28 24 23 20 25 28 29 28 21 24
30 | 11 11 7 10 13 3 10 9 12 24 3 | 29 32 29 31 29 29 30 36 29 31 30
31 | 10 16 6 13 22 4 17 9 13 15 4 | 18 25 18 22 29 17 26 19 25 18 17
32 | 11 13 5 10 16 4 11 7 9 17 3 | 24 27 18 20 21 18 25 20 21 25 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 12 16 5 13 8 11 18 |T 41 32 28 29 36 48 32 29 31 28 44
WRMS | 10 15 6 12 15 4 13 7 10 20 |NE 18 23 20 21 36 30 25 20 23 20 30
MEDI | 10 14 6 11 15 4 13 7 11 17 |MD 23 28 21 24 29 22 27 24 25 22 22
Table 3.1710.5 GPS week: 1710 Day: 5 MJD: 56219.000
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 | 9 19 8 11 14 5 12 6 12 14 4 | 30 30 37 30 42 32 43 32 41 37 36
2 | 11 16 6 14 17 5 15 6 10 22 4 | 20 21 17 20 23 15 22 15 24 22 17
3 | 17 19 8 12 37 8 16 7 17 31 6 | 73 68 69 62 60 66 68 64 67 68 65
4 | 7 13 6 10 12 4 9 5 10 18 3 | 17 18 16 22 17 14 16 17 15 16 16
5E | 8 16 5 10 11 3 15 7 8 12 3 | 32 33 32 34 33 29 33 29 34 31 30
6 | 10 9 6 11 12 2 9 4 10 13 3 | 18 25 24 15 22 21 28 18 26 17 19
7 | 12 14 9 11 23 4 18 5 10 14 4 | 36 40 38 34 44 35 43 35 39 37 35
8 | 8 17 8 13 18 4 12 9 13 16 4 | 16 22 16 16 16 10 20 13 18 20 13
9 | 8 16 6 14 14 4 10 6 10 22 3 | 14 23 12 18 21 10 20 15 20 17 14
10E | 10 18 6 15 17 4 13 7 13 31 4 | 29 35 29 39 33 29 32 32 29 34 31
11 | 8 14 8 8 16 5 10 6 14 12 3 | 22 40 27 24 40 23 38 26 31 27 28
12 | 8 18 9 13 15 4 17 6 12 14 4 | 29 32 32 32 34 29 31 29 38 24 30
13 | 9 13 8 11 20 5 13 5 8 18 3 | 24 29 23 23 34 21 31 23 23 13 24
14 | 9 12 6 12 18 4 13 8 12 16 4 | 23 27 26 21 25 21 28 18 25 21 20
15 | 14 13 9 12 18 2 13 7 13 23 4 | 22 24 21 24 32 18 28 18 25 18 21
16 | 9 15 8 12 20 4 14 6 13 18 4 | 20 24 20 21 26 18 26 19 25 19 19
17 | 9 16 7 12 14 4 14 5 8 29 3 | 19 21 15 21 19 14 20 17 15 17 17
18E | 7 13 7 12 16 4 14 6 10 12 3 | 48 47 46 40 46 47 51 45 46 44 43
19 | 12 12 8 8 13 3 11 5 15 24 3 | 18 25 19 18 20 15 26 17 25 15 17
20E | 10 12 6 11 14 4 13 7 14 10 4 | 29 31 30 25 31 26 31 26 30 23 28
21 | 8 12 7 11 18 4 12 6 8 27 3 | 17 25 17 19 25 16 25 18 19 32 16
22E | 8 13 7 11 15 4 12 7 8 7 3 | 30 31 27 27 28 28 31 27 27 28 25
23 | 11 14 8 14 16 6 15 7 13 23 4 | 24 26 22 19 25 18 28 19 21 11 19
X24 | 18 --- --- --- 43 50 --- --- --- --- 28 | --- --- --- --- 110 95 --- --- --- --- 98
25 | 17 23 8 9 18 3 16 7 13 21 5 | 31 27 25 26 29 24 29 26 33 28 24
26 | 9 9 5 10 14 3 8 6 15 14 3 | 24 26 23 27 30 21 29 24 25 26 24
X27 | 8 --- --- --- --- 70 --- --- --- --- 0 | 216 --- --- --- --- 257 --- --- --- --- 216
28 | 5 13 6 12 19 4 10 7 10 13 3 | 20 23 19 20 26 16 23 18 19 19 19
29 | 11 18 9 12 14 5 16 7 9 30 4 | 24 30 19 22 20 17 24 20 25 19 21
30 | 10 11 9 9 13 3 11 7 10 21 3 | 33 36 33 33 32 32 39 35 36 39 33
31 | 13 14 7 12 23 6 14 8 13 16 4 | 20 26 17 18 28 15 23 13 22 16 15
32 | 9 19 6 10 15 5 12 6 9 18 3 | 24 31 23 22 26 20 30 23 24 29 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 7 12 17 4 13 6 12 20 |T 32 29 25 25 32 32 30 24 28 25 33
WRMS | 10 15 7 12 16 4 13 6 10 19 |NE 20 25 20 21 33 23 26 19 23 20 26
MEDI | 9 14 7 11 16 4 13 6 10 18 |MD 24 27 23 22 28 21 28 20 25 22 24
Table 3.1710.6 GPS week: 1710 Day: 6 MJD: 56220.000
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 | 9 17 7 10 17 3 13 5 13 21 4 | 31 32 36 30 46 33 48 33 40 42 34
2 | 8 21 9 17 17 5 15 5 11 28 4 | 23 31 21 20 26 21 28 21 26 34 20
3 | 11 9 4 10 13 5 8 6 10 24 3 | 54 53 53 54 51 54 52 53 52 55 52
4 | 8 13 5 10 12 4 8 6 12 20 3 | 17 23 16 19 17 16 20 18 18 17 15
5E | 12 19 6 13 17 6 18 5 10 14 4 | 36 34 29 31 31 31 34 28 34 27 28
6 | 11 9 4 13 11 4 8 4 10 15 3 | 20 29 25 28 28 24 30 25 32 23 25
7 | 13 16 7 13 22 4 18 5 10 15 4 | 24 31 23 23 32 22 32 24 27 21 23
8 | 7 15 5 10 17 5 10 6 7 18 3 | 15 25 17 15 23 16 24 17 22 25 15
9 | 11 16 5 13 15 4 11 6 11 26 3 | 17 23 15 18 25 15 22 16 21 19 15
10E | 12 19 6 15 17 5 15 7 12 29 4 | 30 39 28 26 38 28 35 28 33 29 29
11 | 8 13 8 10 19 4 12 5 13 15 3 | 26 41 32 30 44 29 41 31 32 34 31
12 | 13 17 5 13 19 5 17 6 11 18 4 | 31 33 27 26 35 25 31 26 32 25 26
13 | 8 14 7 13 21 3 14 4 10 18 4 | 25 35 28 28 40 26 34 26 30 22 26
14 | 13 12 5 12 20 4 14 6 9 20 4 | 25 27 21 27 33 20 27 19 25 18 21
15 | 9 14 8 11 18 6 16 6 7 27 4 | 19 27 24 24 36 21 28 20 26 27 21
16 | 12 19 8 14 18 4 16 5 8 17 4 | 25 32 24 23 30 22 28 23 28 21 23
17 | 9 16 6 11 11 4 13 5 7 29 3 | 25 28 21 28 21 21 26 21 22 25 22
18E | 11 9 7 13 16 3 14 4 8 14 3 | 42 44 42 41 44 41 42 42 41 45 39
19 | 13 11 4 10 12 5 11 4 8 28 3 | 23 28 24 23 22 21 27 20 25 22 22
20E | 9 14 6 9 13 3 12 7 9 12 3 | 50 53 51 52 52 50 54 52 53 57 51
21 | 7 13 7 13 16 4 12 4 8 27 3 | 15 25 16 17 25 12 21 14 17 27 14
22E | 7 17 6 11 17 3 10 4 9 17 3 | 49 48 47 47 49 47 50 48 43 53 46
23 | 13 17 9 13 18 3 16 5 10 24 4 | 30 34 30 28 35 27 33 29 30 29 27
X24 | 23 --- --- --- 46 60 --- --- --- --- 32 | --- --- --- --- 146 107 --- --- --- --- 137
25 | 16 21 9 11 21 4 16 6 10 28 4 | 52 49 49 47 54 48 51 49 52 56 48
26 | 9 10 6 10 14 4 8 4 8 12 3 | 21 22 19 21 29 18 23 19 20 21 19
X27 | 7 --- --- --- >>>> 112 --- --- --- --- 0 | 209 --- --- --- 504 241 --- --- --- --- 209
28 | 7 12 6 12 18 4 10 6 8 10 3 | 22 26 22 21 28 21 27 21 29 23 21
29 | 14 13 11 13 14 4 16 7 12 33 4 | 23 27 29 29 24 22 26 23 27 20 23
30 | 15 15 8 13 25 8 14 9 11 36 4 | 63 67 61 55 69 56 67 57 64 61 59
31 | 14 15 8 14 25 5 14 7 10 16 4 | 16 24 15 17 32 15 23 14 22 17 13
32 | 10 12 6 10 18 4 14 5 10 24 3 | 23 29 21 20 31 21 31 20 24 34 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 7 12 17 4 14 6 10 22 |T 34 33 28 28 53 36 33 27 31 30 36
WRMS | 11 15 7 12 17 4 13 5 8 19 |NE 21 27 21 22 39 27 28 20 25 24 30
MEDI | 11 14 6 12 17 4 14 5 10 20 |MD 25 31 24 26 32 22 30 23 28 25 23
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 4.1710 GPS week: 1710 MJD: 56214.0-56220.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 |U 5 5 13 |U 6 9 22 |U 7 8 19 |
emr | emr 2906 | 7 6 18 |U 8 8 25 | 10 12 22 |
esa | esa 2921 | 5 5 15 |U 6 9 23 | 8 10 20 |
gfz | gfz 2919 |U 5 5 15 |U 6 8 23 |U 8 9 19 |
grg | grg 2989 |U 8 8 20 |U 8 12 29 | 10 11 26 |
igr | igr 2929 | 5 5 15 | 6 8 22 | 8 9 18 |
igs | igs 2989 | 5 6 15 | 6 8 22 | 8 10 20 |
jpl | jpl 2920 | 6 6 19 |U 7 8 24 | 10 11 22 |
mit | mit 2921 | 6 5 14 |U 6 9 24 |U 9 10 23 |
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 5.1710.0 GPS week: 1710 Day: 0 MJD: 56214.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 4 4 12 | 6 9 16 | 7 8 21 |
emr | emr 2976 | 5 5 16 | 6 8 16 | 8 8 23 |
esa | esa 2976 | 4 4 13 | 5 9 17 | 7 8 21 |
gfz | gfz 2975 | 4 3 12 | 6 8 17 | 7 7 21 |
grg | grg 3070 | 7 6 19 | 7 13 24 | 11 11 27 |
igr | igr 2976 | 4 4 13 | 5 9 17 | 7 7 19 |
igs | igs 3072 | 4 4 12 | 5 9 16 | 8 9 23 |
jpl | jpl 2976 | 4 4 18 | 6 7 17 | 8 9 21 |
mit | mit 2976 | 4 4 13 | 5 9 17 | 8 8 24 |
Table 5.1710.1 GPS week: 1710 Day: 1 MJD: 56215.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 6 4 14 | 6 8 21 | 5 8 18 |
emr | emr 2976 | 7 5 20 | 7 7 26 | 7 10 21 |
esa | esa 2976 | 6 4 16 | 6 9 24 | 6 10 18 |
gfz | gfz 2976 | 6 4 17 | 6 8 23 | 6 9 19 |
grg | grg 2976 | 11 10 19 | 8 12 29 | 11 11 24 |
igr | igr 2976 | 6 4 16 | 6 7 20 | 7 9 17 |
igs | igs 3072 | 6 4 14 | 6 8 23 | 6 9 18 |
jpl | jpl 2976 | 5 4 17 | 7 9 22 | 8 10 18 |
mit | mit 2976 | 6 4 16 | 6 8 27 | 7 8 21 |
Table 5.1710.2 GPS week: 1710 Day: 2 MJD: 56216.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 9 17 | 5 11 21 | 8 7 18 |
emr | emr 2880 | 7 8 20 | 8 9 23 | 10 12 24 |
esa | esa 2976 | 6 8 18 | 6 9 23 | 10 9 18 |
gfz | gfz 2975 | 6 8 17 | 6 8 24 | 9 8 18 |
grg | grg 2976 | 7 8 17 | 7 14 29 | 10 7 22 |
igr | igr 2976 | 6 8 17 | 6 8 22 | 10 9 18 |
igs | igs 3035 | 7 8 17 | 6 9 21 | 9 9 19 |
jpl | jpl 2976 | 6 9 20 | 6 8 24 | 10 10 22 |
mit | mit 2976 | 6 7 17 | 7 8 24 | 9 8 18 |
Table 5.1710.3 GPS week: 1710 Day: 3 MJD: 56217.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
emr | emr 2880 | 7 8 26 | 10 8 28 | 11 14 25 |
esa | esa 2880 | 5 5 20 | 7 12 25 | 8 11 24 |
gfz | gfz 2880 | 6 6 21 | 7 9 24 | 8 11 24 |
grg | grg 2975 | 6 6 22 | 8 13 25 | 8 10 28 |
igr | igr 2941 | 6 5 21 | 7 10 24 | 8 11 22 |
igs | igs 2976 | 5 5 21 | 7 10 24 | 9 13 26 |
jpl | jpl 2880 | 6 7 25 | 7 11 26 | 9 14 26 |
mit | mit 2880 | 8 6 21 | 8 10 26 | 9 12 35 |
Table 5.1710.4 GPS week: 1710 Day: 4 MJD: 56218.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 11 | 9 9 30 | 6 6 17 |
emr | emr 2880 | 6 5 16 | 11 8 30 | 10 10 18 |
esa | esa 2880 | 5 7 12 | 9 9 29 | 7 7 16 |
gfz | gfz 2878 | 6 4 11 | 9 7 30 | 7 6 15 |
grg | grg 2976 | 11 9 24 | 10 11 37 | 8 6 28 |
igr | igr 2880 | 5 6 12 | 9 9 30 | 7 6 16 |
igs | igs 2880 | 6 11 18 | 8 8 29 | 7 7 15 |
jpl | jpl 2880 | 8 7 23 | 8 9 30 | 9 8 21 |
mit | mit 2880 | 6 7 13 | 8 8 31 | 8 7 19 |
Table 5.1710.5 GPS week: 1710 Day: 5 MJD: 56219.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3019 | 4 4 11 | 6 7 22 | 9 13 24 |
emr | emr 2880 | 7 6 18 | 9 7 23 | 12 16 27 |
esa | esa 2880 | 5 5 13 | 6 9 23 | 10 14 23 |
gfz | gfz 2880 | 5 5 12 | 6 8 23 | 10 14 22 |
grg | grg 2976 | 6 9 16 | 7 11 29 | 12 13 34 |
igr | igr 2879 | 5 5 14 | 5 8 21 | 10 14 21 |
igs | igs 2933 | 4 5 12 | 6 8 21 | 10 12 25 |
jpl | jpl 2879 | 6 5 16 | 7 7 26 | 12 15 25 |
mit | mit 2880 | 4 5 11 | 6 8 22 | 12 13 24 |
Table 5.1710.6 GPS week: 1710 Day: 6 MJD: 56220.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3013 | 4 4 10 | 5 8 25 | 7 7 17 |
emr | emr 2876 | 9 6 13 | 7 6 26 | 11 15 20 |
esa | esa 2880 | 5 5 11 | 5 8 21 | 9 11 17 |
gfz | gfz 2873 | 6 6 13 | 5 6 22 | 9 10 16 |
grg | grg 2975 | 9 7 22 | 6 10 28 | 9 14 21 |
igr | igr 2880 | 5 5 12 | 5 7 21 | 9 11 16 |
igs | igs 2959 | 5 5 11 | 5 7 22 | 8 10 17 |
jpl | jpl 2876 | 8 7 13 | 6 7 22 | 11 13 20 |
mit | mit 2880 | 6 6 10 | 5 9 23 | 11 11 19 |
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 6.1710 GPS week: 1710 MJD: 56214.500-56220.500
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 | -75 -42 136 -252 -5 | 2 13
| 16 24 52 106 7 | 2
emr uuuxu | 40 -11 83 480 -11 | 21 26
| 19 23 70 84 5 | 3
esa uuuuu | -27 -35 -65 -225 -7 | 9 17
| 27 51 99 79 6 | 2
gfz uuuuu | 39 71 -37 20 0 | 4 12
| 19 35 111 62 3 | 2
grg uuuux | -7 -27 12 105 -30 | -7 31
| 34 45 73 42 51 | 10
igr xxxxx | -44 18 -26 43 2 | -3 12
| 11 13 74 70 4 | 3
irf xxxxx | 22 6 2 138 4 | 5 12
| 8 16 12 28 6 | 3
jpl uuuuu | 22 -24 -51 237 2 | 29 32
| 15 26 87 88 7 | 2
mit uuuuu | 44 7 11 212 11 | 0 13
| 10 11 83 66 10 | 5
ngs uuuuu | -27 73 -21 39 1 | 10 15
| 18 33 54 125 3 | 2
sio xxxxx | -27 4 77 -230 -4 | 20 24
| 19 21 162 115 6 | 2
Table 7.1710.0 GPS week: 1710 Day: 0 MJD: 56214.500
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 | -65 -19 53 -210 -5 | 2 12
emr uuuxu | 50 -46 221 487 -10 | 25 28
esa uuuuu | -45 -73 -91 -308 -9 | 9 16
gfz uuuuu | 78 99 -158 67 -2 | 1 13
grg uuuux | 16 -6 -100 149 29 | -23 51
igr xxxxx | -24 40 -112 152 0 | -7 15
irf xxxxx | 33 19 0 145 7 | 0 11
jpl uuuuu | 33 -9 51 351 -8 | 32 34
mit uuuuu | 41 4 108 233 14 | -7 13
ngs uuuuu | -26 112 -50 16 4 | 6 14
sio xxxxx | -32 7 -120 -151 -13 | 21 25
Table 7.1710.1 GPS week: 1710 Day: 1 MJD: 56215.500
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 | -49 -34 118 -240 -13 | 3 11
emr uuuxu | 45 8 47 560 -16 | 24 28
esa uuuuu | -59 -49 49 -260 -2 | 9 16
gfz uuuuu | 41 94 -190 53 2 | 3 11
grg uuuux | 24 34 -53 100 21 | -14 44
igr xxxxx | -48 15 -36 -52 3 | -5 12
irf xxxxx | 27 16 -8 180 10 | 2 11
jpl uuuuu | 28 -17 -135 328 -4 | 31 33
mit uuuuu | 36 -10 46 331 18 | -5 13
ngs uuuuu | 7 56 -47 -164 4 | 8 14
sio xxxxx | 3 15 -71 -109 -10 | 22 25
Table 7.1710.2 GPS week: 1710 Day: 2 MJD: 56216.500
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 | -79 -43 220 -357 -1 | 3 10
emr uuuxu | 54 16 56 564 -13 | 23 27
esa uuuuu | -46 -91 -30 -285 -3 | 11 16
gfz uuuuu | 43 79 -103 16 2 | 5 10
grg uuuux | 6 17 25 150 -2 | -3 30
igr xxxxx | -37 28 -97 38 10 | -2 10
irf xxxxx | 24 23 1 136 0 | 5 11
jpl uuuuu | 46 13 -155 207 1 | 31 33
mit uuuuu | 44 2 1 241 3 | -2 12
ngs uuuuu | -34 109 -32 148 1 | 11 14
sio xxxxx | -36 10 160 -138 -6 | 22 25
Table 7.1710.3 GPS week: 1710 Day: 3 MJD: 56217.500
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 | -91 -7 119 -240 -5 | 3 10
emr uuuxu | 50 -6 15 550 -13 | 22 26
esa uuuuu | -23 -81 -226 -292 -7 | 11 16
gfz uuuuu | 31 98 13 65 -5 | 5 10
grg uuuux | 0 -28 94 123 -10 | 5 14
igr xxxxx | -46 23 24 69 2 | -1 10
irf xxxxx | 31 16 21 151 10 | 5 11
jpl uuuuu | 25 -9 -25 173 4 | 29 31
mit uuuuu | 52 24 45 177 23 | -1 12
ngs uuuuu | -25 42 76 206 -4 | 11 14
sio xxxxx | -13 38 -63 -177 -4 | 21 24
Table 7.1710.4 GPS week: 1710 Day: 4 MJD: 56218.500
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 | -97 -58 119 -408 5 | -1 12
emr uuuxu | 0 -38 36 449 -14 | 16 23
esa uuuuu | 21 37 -155 -148 -3 | 7 15
gfz uuuuu | 28 67 75 71 0 | 1 11
grg uuuux | -27 -88 -13 27 -77 | 2 16
igr xxxxx | -46 11 8 97 -2 | -4 10
irf xxxxx | 12 -13 15 140 -3 | 5 11
jpl uuuuu | 8 -59 67 294 2 | 25 27
mit uuuuu | 42 5 62 213 -1 | 0 11
ngs uuuuu | -36 30 -6 77 1 | 8 13
sio xxxxx | -58 -28 120 -296 0 | 17 20
Table 7.1710.5 GPS week: 1710 Day: 5 MJD: 56219.500
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 | -66 -62 160 -228 -15 | 4 16
emr uuuxu | 31 -16 120 388 -5 | 19 25
esa uuuuu | -16 2 -39 -165 -18 | 11 18
gfz uuuuu | 15 56 51 -48 -1 | 6 15
grg uuuux | 8 -64 38 90 -87 | -2 21
igr xxxxx | -58 8 -64 25 -2 | 0 12
irf xxxxx | 17 -1 -9 124 5 | 9 14
jpl uuuuu | 14 -50 -107 192 9 | 29 32
mit uuuuu | 33 20 -42 164 19 | 5 14
ngs uuuuu | -21 69 -93 52 3 | 12 18
sio xxxxx | -25 -15 217 -327 -2 | 21 25
Table 7.1710.6 GPS week: 1710 Day: 6 MJD: 56220.500
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 | -77 -74 163 -79 -1 | 1 18
emr uuuxu | 52 3 85 358 -5 | 17 24
esa uuuuu | -22 10 34 -117 -4 | 8 20
gfz uuuuu | 35 1 56 -84 4 | 5 15
grg uuuux | -75 -56 94 92 -83 | -12 39
igr xxxxx | -48 3 97 -27 -1 | 0 12
irf xxxxx | 13 -18 -8 87 -2 | 9 14
jpl uuuuu | 2 -40 -55 114 10 | 29 32
mit uuuuu | 62 3 -145 126 1 | 7 14
ngs uuuuu | -54 96 5 -63 -4 | 12 18
sio xxxxx | -29 3 298 -414 7 | 19 24
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