[IGSREPORT-26004] Wk 2006 IGS Final Orbits
acc
acc at igs.org
Sun Jul 8 03:45:37 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2006 (Jun 17, 2018 - Jun 23, 2018)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs2006[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2006[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2006[0-6].cls IGS GPS clock combination summary report.
igs20067.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20067.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | FAA1 OUS2 TIXI ULAB FAA1 NAUR OUS2 SCUB TIXI ULAB
0 | EMR | 18 YAKT
0 | ESA | FAA1 MAL2 NRMD FAA1 MAL2 NRMD
0 | GFZ | 18 21 18 21 ALBH BJNM FAA1 GODE MAL2 REUN ALBH BJNM
0 | GFZ | CUSV FAA1 GODE MAL2 REUN
0 | GRG | 21 21 GLSV KIT3 LPGS RIO2 GLSV KIT3 LPGS RIO2 TONG
0 | JPL | LAUT POLV
0 | MIT | BAKE BJNM CEDU CHUR DARW DUBO MAL2 PIE1 SCH2 WHIT
0 | MIT | BAKE BJNM CEDU CHUR DARW DUBO FAA1 MAL2 PIE1 SCH2
0 | MIT | WHIT
1 | COD | MCIL MDVJ TLSE YELL
1 | EMR | YAKT
1 | ESA | FAA1 KIRI MAL2 FAA1 KIRI MAL2
1 | GFZ | 18 21 18 21 BJNM FAA1 GODE MAL2 REUN YELL BJNM FAA1
1 | GFZ | GODE MAL2 REUN YELL
1 | GRG | 1 2 3 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
1 | GRG | 21 22 23 24 25 26 27 28 29 30 31 32 1 2 3 5 6 7 8
1 | GRG | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
1 | GRG | 26 27 28 29 30 31 32 KIT3 KIT3
1 | JPL | 18 18 CHUR CHUR LAUT
1 | MIT | ALBH BAKE CHPI DRAO FALK HLFX HOB2 PIE1 WAB2 ALBH
1 | MIT | BAKE CHPI DRAO FALK HLFX HOB2 PIE1 WAB2
2 | COD | FAA1 GLSV TIXI FAA1 GLSV KIRI TIXI
2 | EMR | 18
2 | ESA | DAV1 MAL2 OUS2 TLSE DAV1 MAL2 OUS2 TLSE
2 | GFZ | 18 24 18 24 GODE MDVJ REUN GODE MDVJ REUN
2 | GRG | ARTU GLSV KIT3 LPGS WIND ARTU GLSV KIT3 KRGG LPGS
2 | GRG | QIKI TONG WIND
2 | JPL | 18 18 POLV LAUT POLV
2 | MIT | ALGO BAKE CEDU CHPI CHUR DRAO FLIN HOB2 SUTH WAB2
2 | MIT | ALGO BAKE CEDU CHPI CHUR DRAO FLIN HOB2 SUTH WAB2
3 | COD | TIXI TLSE KIRI TIXI TLSE
3 | ESA | 18 18 CUSV KOUR CUSV KOUR MAL2 WIND
3 | GFZ | 18 18 GODE MAL2 REUN GODE MAL2 REUN
3 | GRG | 18 18 GLSV KIT3 RABT SEYG BRST DAV1 GLSV KIT3 RABT
3 | GRG | SEYG TONG
3 | JPL | LAUT LMMF
3 | MIT | BAKE CHPI CHUR DRAO DUBO HLFX NRC1 STJO SUTH TWTF
3 | MIT | VILL YELL BAKE CHPI CHUR DRAO DUBO HLFX NRC1 STJO
3 | MIT | SUTH TWTF VILL YELL
4 | COD | MAL2 SEYG TIXI KIRI SEYG TIXI TLSE
4 | EMR | DAEJ HOB2 OPMT YAR2
4 | ESA | 19 20 21 22 28 LAUT MAL2 REUN TLSE TOW2 YELL REUN
4 | ESA | TLSE
4 | GFZ | 18 18 BJNM GODE MAL2 REUN BJNM GODE MAL2 REUN
4 | GRG | FAA1 KIT3 LHAZ MOBS SEYG WIND COCO FAA1 KIT3 LHAZ
4 | GRG | MAL2 MOBS SEYG TONG TOW2 WIND
4 | JPL | 18 FAA1 LAUT MAL2
4 | MIT | ALGO BAKE CEDU CHPI CHUR FLIN GRAZ HOB2 MAL2 WAB2
4 | MIT | WHIT ALGO BAKE CEDU CHPI CHUR FLIN GRAZ HOB2 MAL2
4 | MIT | MEDI WAB2 WHIT
5 | COD | DAV1 SEYG TIXI DAV1 NAUR SEYG TIXI
5 | EMR | PTBB
5 | ESA | 22 18 FAA1 FAA1
5 | GFZ | 18 18 FAA1 GODE KOUR REUN FAA1 GODE KOUR NRIL REUN
5 | GRG | 18 21 FAA1 KOUR FAA1 KOUR LHAZ TONG
5 | JPL | LAUT
5 | MIT | BAKE CHPI CHUR DUBO FAA1 FLIN GRAZ MAL2 SUTH ABPO
5 | MIT | BAKE CHPI CHUR DUBO FAA1 FLIN GRAZ MAL2 SUTH
6 | COD | FAA1 TIXI NAUR TIXI
6 | EMR | HOB2
6 | ESA | 18 18 FAA1 MAL2 MAL2
6 | GFZ | 18 21 18 21 BJNM GODE MAL2 REUN BJNM GODE LHAZ MAG0
6 | GFZ | MAL2 REUN
6 | GRG | 18 21 18 21 BRST SEYG TLSE BRST MAL2 SEYG TLSE TONG
6 | GRG | TUVA
6 | JPL | LAUT
6 | MIT | BAKE CHPI CHUR FAA1 FLIN GRAZ HARB HLFX SCH2 WAB2
6 | MIT | WHIT BAKE BJNM CHPI CHUR FLIN GRAZ HARB HLFX SCH2
6 | MIT | WAB2 WHIT
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. 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 G20 | | | | | | 4 | |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
8. 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 | -.2 .4 .7 12 12 -7 -.29
EMR | 0 | -3.8 -13.1 -5.1 -1 -30 40 -.05
ESA | 0 | -.3 .2 -.3 15 6 15 -.37
GFZ | 0 | .1 .1 .2 -8 -19 2 -.23
GRG | 0 | -.2 -4.8 -4.6 46 4 28 -.43
JPL | 0 | 4.4 -7.0 -5.9 3 10 5 -.34
MIT | 0 | -1.9 -3.5 5.5 -5 11 6 -.0
NGS | 0 | -1.4 -8.5 -3.6 32 5 -79 -.14
SIO | 0 | 2.6 1.3 -3.9 4 -11 -11 -.11
COD | 1 | .1 .3 .8 9 1 1 -.46
EMR | 1 | -3.4 -8.8 -2.6 1 -29 52 -.01
ESA | 1 | .1 -.0 -.4 10 -13 9 -.49
GFZ | 1 | .5 .3 .3 -3 -25 -12 -.29
GRG | 1 | .5 -5.1 5.0 56 -1 13 -.44
JPL | 1 | 1.2 -11.0 -7.8 8 -15 5 -.34
MIT | 1 | 1.8 -3.1 4.2 5 45 16 .12
NGS | 1 | 1.8 -7.9 6.5 -14 -73 -86 -.36
SIO | 1 | .6 -.7 .0 19 -30 6 -.24
COD | 2 | -.2 .2 .4 8 12 5 -.36
EMR | 2 | -3.9 -3.7 -1.1 -4 -1 39 -.19
ESA | 2 | -.1 -.3 .0 -4 -12 13 -.54
GFZ | 2 | .0 .0 -.0 -5 -24 1 -.23
GRG | 2 | 1.6 -2.2 -3.3 55 -24 40 -.49
JPL | 2 | -.5 -10.8 -5.3 -1 1 -10 -.50
MIT | 2 | -2.7 -1.2 8.8 -22 51 2 -.11
NGS | 2 | -1.6 -9.6 -6.0 -17 23 -93 -.18
SIO | 2 | -1.0 1.8 6.2 -24 15 -14 -.18
COD | 3 | -.2 .2 .3 9 10 -3 -.33
EMR | 3 | -4.4 1.8 -4.0 -4 5 43 -.09
ESA | 3 | .2 -.2 .3 3 -19 6 -.39
GFZ | 3 | .1 .5 .4 2 -27 -3 -.29
GRG | 3 | 1.3 -2.8 -2.3 44 6 5 -.25
JPL | 3 | 3.0 -1.0 -3.4 -4 6 -5 -.26
MIT | 3 | -.8 -2.5 6.8 -5 50 -8 -.10
NGS | 3 | 2.9 -4.7 -7.1 26 20 -57 -.18
SIO | 3 | -1.3 2.5 -2.0 6 11 -10 -.26
COD | 4 | -.2 .5 .9 22 14 -11 -.39
EMR | 4 | 5.8 -.3 -3.4 -13 -1 26 -.08
ESA | 4 | .5 .4 .5 14 -34 10 -.52
GFZ | 4 | .4 .4 .3 4 -32 -5 -.28
GRG | 4 | 1.8 -1.7 3.3 47 -25 12 -.30
JPL | 4 | 3.4 -3.5 -4.0 0 8 -3 -.22
MIT | 4 | 1.3 -4.4 8.5 -11 45 -7 -.02
NGS | 4 | .7 1.6 1.3 24 -42 -9 -.22
SIO | 4 | 3.0 -.1 4.2 -10 -6 -16 -.0
COD | 5 | -.3 .4 .6 16 14 1 -.41
EMR | 5 | 3.2 -3.2 .5 -7 -2 14 -.06
ESA | 5 | -.7 -.4 1.0 1 -12 7 -.25
GFZ | 5 | .3 -.2 .2 -19 -27 1 -.28
GRG | 5 | 3.0 -1.3 1.8 12 30 13 -.43
JPL | 5 | 7.6 -7.3 -4.3 0 10 -12 -.45
MIT | 5 | 2.2 -5.3 4.8 -36 41 -18 -.11
NGS | 5 | 1.2 -10.8 7.9 -41 -115 -68 -.38
SIO | 5 | .7 -2.8 4.4 -1 -16 -13 -.13
COD | 6 | -.4 .6 1.2 19 20 -9 -.54
EMR | 6 | -2.3 -4.0 1.0 14 4 30 -.18
ESA | 6 | .1 .4 1.7 4 -18 8 -.39
GFZ | 6 | .5 .3 .6 -3 -45 -2 -.41
GRG | 6 | .5 .1 -12.3 56 -26 30 -.47
JPL | 6 | 3.3 -6.9 -2.8 -14 -5 -20 -.46
MIT | 6 | .2 -6.1 3.8 -14 18 7 -.32
NGS | 6 | -1.4 -5.3 4.2 2 -56 -72 -.58
SIO | 6 | -2.1 1.4 14.0 -6 -21 -13 -.21
9. 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.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.2006.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2006.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 2.2006.[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 3.2006.[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 5.2006.0-6). 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 2006 summary. (Jun 17, 2018 - Jun 23, 2018)
Table 1.2006.a GPS week: 2006 MJD: 58286.000-58292.000
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| 1 -1 0 6 -19 -9 -.04 10 9 | -629 18 7 94
| 0 0 0 8 11 10 .03 | 526 580
emr 80| -1 -3 -1 -4 -7 45 .18 12 12 | 139187 124 14 95
| 0 0 1 15 8 9 .02 | 842 507
esa 150| 0 0 -2 0 0 -12 -.09 9 9 | -1523 -357 8 204
| 0 0 1 11 12 11 .03 | 1583 1500
gfz 180| 0 2 2 -15 -11 -14 .03 11 10 | -206 -61 12 126
| 0 0 1 22 12 11 .02 | 246 363
grg 107| 2 0 -2 -5 3 -20 -.08 13 12 | -16 119 142865 143000
| 1 0 4 6 16 25 .03 | 121 230
igr n/a| 0 0 0 -11 -5 -3 -.07 4 4 | 2187 204 10 68
| 0 0 0 7 6 9 .03 | 959 584
jpl 80| 0 0 0 8 13 23 .16 8 8 | 136207 384 8 111
| 0 0 0 10 11 10 .02 | 913 572
mit 349| 0 0 2 8 1 4 -.06 11 10 | 29 -77 48 521
| 0 0 1 25 22 10 .01 | 228 372
ngs 205| 0 0 1 -4 6 2 -.10 10 9 | -660 67 1027 2230
| 1 0 3 20 23 22 .02 | 491 552
sio 339| 0 0 3 12 5 -29 -.14 15 15 | --- --- --- ---
| 0 0 1 30 20 24 .04 | --- ---
Table 1.2006.b GPS week : 2006 MJD: 58286.000-58292.000
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 3 4 4 3 3 3 |
2 | 4 4 4 4 4 4 4 |
3 | 4 3 3 3 3 3 4 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 4 4 4 4 4 |
6 | 4 3 3 3 3 4 4 |
7 | 5 4 4 4 4 4 5 |
8 | 3 3 3 3 4 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 3 3 3 3 4 3 3 |
12 | 5 5 5 5 5 4 4 |
13 | 4 5 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 5 6 5 5 5 5 5 |
19 | 4 4 4 4 4 4 4 |
20 | 5 5 5 5 6 0 6 |
21 | 5 5 4 4 5 4 5 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 4 4 4 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 4 4 4 3 |
27 | 4 3 3 3 3 3 3 |
28 | 5 4 4 4 4 4 4 |
29 | 5 5 4 5 5 5 4 |
30 | 5 4 4 3 4 4 4 |
31 | 4 4 4 4 4 4 4 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2006.0 GPS week: 2006 Day: 0 MJD: 58286.000
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 -2 0 17 -15 -28 -.06 13 12 | -329 -211 8 89
emr 80| -1 -5 -1 0 -9 28 .20 12 12 | 138227 5 17 104
esa 150| 1 1 -3 10 7 -28 -.14 9 9 | -2752 -173 8 191
gfz 178| -1 4 3 -9 -28 -34 .03 11 10 | -249 -116 12 111
grg 103| 1 0 -4 -5 0 6 -.07 13 13 | 163 -119 10 125
igr n/a| 0 0 1 0 -3 -22 -.09 6 6 | 1255 -235 13 69
jpl 80| -1 0 0 -6 8 13 .14 8 8 | 134664 309 9 103
mit 349| 0 0 5 41 -18 8 -.08 12 10 | 231 -405 59 557
ngs 207| 0 0 3 -46 35 43 -.07 11 10 | -370 -189 1136 2392
sio 337| -1 0 3 50 5 -16 -.07 17 18 | --- --- --- ---
Table 2.2006.1 GPS week: 2006 Day: 1 MJD: 58287.000
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 -1 3 -18 -5 -.04 10 9 | -457 -320 7 117
emr 80| -3 -3 -4 20 -6 47 .23 12 12 | 138465 295 14 99
esa 150| 0 0 -2 -8 -4 -25 -.09 9 9 | 390 -2679 8 219
gfz 181| -1 2 3 6 3 -22 .01 11 10 | -286 -88 12 122
grg 106| 2 0 1 -1 3 0 -.05 11 11 | 0 0 999999 999999
igr n/a| 0 0 0 -9 0 3 -.07 5 5 | 1230 12 10 68
jpl 80| -2 0 0 25 2 5 .14 9 9 | 136188 536 9 126
mit 350| 1 0 3 -33 12 -7 -.07 12 11 | 235 -140 43 591
ngs 203| 0 1 3 3 13 -2 -.07 11 9 | -465 -317 1067 2056
sio 338| 0 0 1 -25 -8 -3 -.15 16 17 | --- --- --- ---
Table 2.2006.2 GPS week: 2006 Day: 2 MJD: 58288.000
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| 1 -1 0 6 -14 -3 .01 10 9 | -474 -314 6 75
emr 80| 0 -2 -1 5 0 49 .18 13 13 | 138768 1175 14 80
esa 150| 0 0 -1 -7 -15 -5 -.08 9 9 | -276 -1141 8 195
gfz 183| -1 2 4 0 -22 -13 .02 10 10 | -316 122 13 168
grg 110| 0 1 -1 1 -12 10 -.10 11 10 | -207 145 9 152
igr n/a| 0 0 0 -5 -10 -4 -.06 4 4 | 1232 1402 11 68
jpl 80| -1 0 0 0 14 22 .15 8 8 | 135600 1556 9 125
mit 349| 0 0 3 15 32 9 -.08 12 11 | -252 124 53 474
ngs 211| 0 0 -3 -12 13 -28 -.12 10 8 | -569 -160 925 2017
sio 337| 0 0 1 7 9 -48 -.11 16 16 | --- --- --- ---
Table 2.2006.3 GPS week: 2006 Day: 3 MJD: 58289.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 263| 1 -1 0 14 -35 -19 -.05 10 9 | -1802 1310 6 106
emr 80| -1 -2 -1 -17 -17 44 .16 12 12 | 140350 -103 14 81
esa 150| 1 0 0 -8 -1 -19 -.10 9 9 | -181 -1499 7 186
gfz 180| -1 2 3 -25 -2 -4 .02 12 11 | 78 -488 14 124
grg 112| 2 0 0 -11 -4 -52 -.05 12 12 | -52 491 9 180
igr n/a| 0 0 0 -15 -16 -5 -.08 4 4 | 2996 324 11 75
jpl 80| -1 0 0 5 18 31 .16 8 8 | 137050 288 8 84
mit 349| 0 0 2 20 -1 20 -.07 12 12 | -294 410 40 344
ngs 203| -1 0 -3 -2 20 -3 -.11 9 8 | -1758 1258 1196 2086
sio 344| -1 0 3 33 -17 -10 -.18 15 15 | --- --- --- ---
Table 2.2006.4 GPS week: 2006 Day: 4 MJD: 58290.000
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 -1 0 11 -32 -8 -.03 9 9 | -278 -156 8 92
emr 80| 0 -3 -2 -20 3 40 .18 13 13 | 140021 -265 15 104
esa 150| 1 0 -3 -9 -16 -4 -.06 9 9 | -3419 1449 9 231
gfz 180| -1 1 0 0 0 -9 .06 11 10 | -49 -396 12 119
grg 111| 0 0 1 -1 -9 -30 -.11 14 13 | 103 -6 10 185
igr n/a| 0 0 0 -17 -7 -6 -.08 4 4 | 3163 181 11 64
jpl 80| 0 0 0 19 31 29 .19 9 9 | 136996 108 7 94
mit 349| 0 0 2 -14 9 -5 -.05 10 9 | 178 -635 67 570
ngs 204| 0 1 2 6 3 -5 -.11 10 9 | -385 -84 909 2122
sio 339| -1 -1 1 -7 6 -12 -.14 14 14 | --- --- --- ---
Table 2.2006.5 GPS week: 2006 Day: 5 MJD: 58291.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 263| 1 -1 -2 -5 -20 1 -.04 9 8 | -540 16 7 87
emr 80| -1 -2 -1 -18 -18 56 .17 12 12 | 139782 -317 12 96
esa 150| 1 0 -1 18 10 -6 -.09 9 9 | -3208 1197 9 199
gfz 180| 0 2 1 -60 -15 -17 .06 11 10 | -641 619 14 119
grg 99| 2 0 -3 -15 34 -35 -.11 14 14 | -81 376 10 178
igr n/a| 0 1 0 -13 -1 3 -.01 4 4 | 3291 -400 10 69
jpl 80| 0 1 0 6 0 35 .17 8 8 | 137100 -275 9 118
mit 349| 0 0 0 6 14 -5 -.05 11 10 | -54 275 36 502
ngs 203| -2 0 5 15 -1 1 -.10 11 9 | -594 217 1040 2507
sio 340| 0 0 4 43 -5 -41 -.14 15 15 | --- --- --- ---
Table 2.2006.6 GPS week: 2006 Day: 6 MJD: 58292.000
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| 1 0 0 0 0 -3 -.06 9 9 | -526 -194 7 96
emr 80| -2 -3 0 0 -1 50 .17 13 13 | 138696 84 16 106
esa 150| 0 1 -2 0 16 0 -.06 9 9 | -1220 346 7 209
gfz 180| 0 1 2 -19 -12 -1 .02 10 10 | 19 -86 12 123
grg 110| 3 0 -11 -6 13 -43 -.08 15 13 | -43 -50 10 183
igr n/a| 0 0 1 -19 2 7 -.07 4 4 | 2144 145 10 65
jpl 80| 0 0 0 8 21 28 .17 8 8 | 135853 168 9 129
mit 350| 0 0 2 23 -36 8 -.04 10 10 | 161 -171 44 609
ngs 208| -1 0 3 3 -38 15 -.09 10 9 | -480 -253 920 2436
sio 342| 0 0 6 -15 46 -70 -.17 14 14 | --- --- --- ---
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 3.2006.0 GPS week: 2006 Day: 0 MJD: 58286.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 9 9 7 15 4 6 8 8 18 3 | 19 19 21 17 22 18 19 19 19 17 18
2E | 16 11 9 9 19 5 9 12 12 15 4 | 30 31 29 27 33 27 33 29 27 27 28
3 | 13 10 10 11 8 5 8 9 9 17 3 | 27 34 26 25 26 26 31 24 29 25 26
X4 | 2 --- --- --- --- 30 --- --- --- --- 0 | 29 --- --- --- --- 26 --- --- --- --- 29
5 | 8 9 12 11 12 6 10 14 14 19 4 | 50 53 52 40 50 45 54 38 43 43 47
6E | 8 8 11 9 20 5 5 7 7 18 3 | 21 24 26 19 28 21 23 23 22 20 22
7E | 10 14 8 12 22 7 11 10 12 17 4 | 50 47 48 51 51 49 45 52 53 53 48
8 | 9 9 6 7 10 4 5 9 8 13 3 | 26 28 24 25 31 24 26 22 26 33 25
9 | 7 5 9 7 9 6 7 6 6 10 2 | 38 41 38 40 36 38 42 39 40 41 39
10 | 8 7 12 9 5 5 7 10 8 11 3 | 16 22 15 19 16 16 21 19 18 18 16
11E | 6 8 11 7 10 3 6 9 7 17 3 | 30 32 31 31 30 30 28 31 32 36 30
12 | 11 16 7 14 15 6 9 19 13 20 4 | 32 32 31 38 29 33 31 40 35 41 32
13 | 12 8 9 11 10 7 10 13 12 21 4 | 23 30 23 32 24 28 30 32 30 35 27
14 | 13 10 10 12 9 6 7 13 11 22 4 | 33 38 35 38 36 35 37 35 35 34 35
15 | 11 12 9 13 7 6 10 13 10 22 4 | 42 49 43 35 38 37 46 31 35 44 40
16 | 16 23 7 14 15 7 8 12 10 21 4 | 30 25 26 37 21 30 25 34 32 36 27
17 | 15 11 8 14 10 7 7 9 12 15 3 | 27 28 23 27 28 23 26 24 25 25 24
18E | 17 13 14 14 11 6 12 14 18 19 5 | 109 100 95 98 108 99 106 98 99 98 101
19 | 12 16 7 13 11 7 6 8 11 15 4 | 29 31 27 25 27 23 27 23 23 24 25
20 | 12 12 11 15 8 7 9 25 13 15 5 | 21 20 15 24 13 23 19 30 21 21 22
21E | 16 9 10 14 17 6 8 14 11 18 4 | 29 29 24 28 34 24 28 24 24 24 25
22 | 14 8 10 12 8 7 7 16 14 20 4 | 31 37 30 41 33 38 35 36 43 38 34
23 | 10 18 10 12 15 8 6 10 11 20 4 | 32 32 29 37 30 34 32 36 37 40 32
24 | 11 13 7 7 12 3 7 10 6 21 3 | 21 23 20 22 22 19 21 23 19 24 20
25 | 10 9 6 9 7 4 7 10 11 15 3 | 29 35 32 33 33 30 35 34 33 37 32
26 | 15 9 6 7 9 3 5 7 7 12 3 | 57 59 56 57 52 56 56 56 55 50 55
27 | 19 8 7 8 10 4 7 11 9 10 3 | 29 24 22 20 26 20 23 17 22 25 21
28 | 17 14 7 15 13 8 8 9 13 20 4 | 24 25 22 28 22 22 24 23 21 25 21
29 | 10 18 8 13 15 8 9 16 14 15 4 | 29 31 24 23 31 23 29 27 26 24 25
30E | 28 16 9 7 23 5 8 7 9 14 5 | 38 29 31 28 32 26 28 30 27 30 27
31E | 18 10 6 13 16 6 8 11 11 17 4 | 55 58 53 56 57 55 55 56 56 55 55
32 | 13 6 12 7 5 5 5 7 8 17 3 | 25 30 24 26 21 23 28 23 24 30 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 9 11 13 6 8 12 11 17 |T 33 35 32 33 33 31 34 33 33 34 32
WRMS | 12 12 9 10 13 6 8 10 10 18 |NE 30 33 28 31 29 29 31 30 30 32 29
MEDI | 12 10 9 11 11 6 7 10 11 17 |MD 29 31 27 28 30 26 29 30 29 33 27
Table 3.2006.1 GPS week: 2006 Day: 1 MJD: 58287.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 9 7 7 10 3 6 9 9 13 3 | 20 20 20 19 21 18 20 18 21 14 18
2E | 11 11 8 10 15 4 11 13 11 19 4 | 35 32 30 30 34 29 31 31 30 31 30
3 | 8 10 10 10 7 3 8 11 8 13 3 | 22 32 23 24 25 23 29 23 27 22 24
X4 | 1 --- --- --- --- 25 --- --- --- --- 0 | 29 --- --- --- --- 21 --- --- --- --- 28
5 | 7 9 10 12 8 4 13 14 14 20 4 | 36 38 36 30 33 32 41 27 30 34 33
6E | 7 13 9 8 13 3 7 6 8 13 3 | 23 27 24 21 22 22 26 22 23 23 22
7E | 6 12 9 10 16 5 11 12 15 15 4 | 37 35 35 40 40 37 37 40 41 38 37
8 | 8 10 6 10 10 5 8 10 9 14 3 | 20 25 19 19 26 18 22 18 23 25 20
9 | 6 7 8 10 8 4 8 7 8 11 3 | 38 40 36 37 33 34 40 32 36 36 36
10 | 8 6 11 7 7 2 8 11 5 13 3 | 13 21 13 15 15 13 20 16 14 17 14
11E | 9 6 10 6 9 3 6 8 6 16 3 | 20 25 26 25 28 25 23 23 28 29 24
12 | 10 17 8 12 10 4 10 16 15 17 4 | 27 25 22 27 24 24 23 28 28 28 24
13 | 9 7 10 14 9 5 12 15 14 21 4 | 20 25 20 30 19 22 29 23 24 33 22
14 | 9 8 9 12 7 5 7 13 10 22 3 | 28 29 27 28 29 27 30 30 31 31 28
15 | 11 13 8 12 6 5 11 16 13 19 4 | 30 36 30 30 27 28 34 25 25 34 29
16 | 11 23 5 15 16 7 6 13 12 23 5 | 22 22 21 27 19 22 22 28 27 28 21
17 | 9 8 8 14 10 4 8 10 11 14 3 | 21 24 18 26 22 20 24 22 23 21 21
18E | 18 13 16 13 13 6 17 14 19 18 5 | 99 87 85 85 97 86 92 85 88 87 89
19 | 10 13 5 12 10 4 8 11 14 15 3 | 20 26 20 24 24 20 23 22 22 23 21
20 | 9 15 11 15 8 5 13 27 11 17 5 | 22 24 18 21 13 22 25 29 19 24 23
21E | 13 11 8 18 16 6 9 15 11 17 4 | 25 23 18 23 28 17 21 17 19 18 19
22 | 9 10 10 12 7 5 8 15 12 16 4 | 29 34 27 37 32 32 31 31 34 34 31
23 | 9 16 9 14 11 6 7 10 11 18 4 | 31 28 27 34 28 29 30 30 34 34 29
24 | 13 14 9 6 11 4 8 11 8 12 3 | 21 22 20 20 23 17 21 22 17 20 19
25 | 7 8 6 11 7 3 8 7 10 13 3 | 25 32 27 31 29 25 29 26 27 30 27
26 | 12 11 7 9 12 4 7 7 7 10 3 | 76 80 76 75 76 75 79 78 76 75 77
27 | 7 10 6 8 10 5 8 11 9 12 3 | 19 24 19 20 22 17 19 16 21 21 18
28 | 8 13 7 15 12 7 9 11 11 18 4 | 16 24 19 25 19 20 22 22 22 24 19
29 | 11 19 8 12 13 5 11 15 12 13 4 | 24 24 18 23 23 22 22 24 24 20 21
30E | 12 11 10 6 18 3 8 9 10 13 4 | 27 26 28 26 34 24 28 24 29 24 26
31E | 12 11 6 11 14 4 8 11 10 13 3 | 55 57 52 52 55 51 51 52 51 53 52
32 | 6 7 11 8 6 4 7 10 7 19 3 | 20 28 19 24 20 20 25 20 21 30 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 9 11 11 5 9 12 11 16 |T 29 32 28 30 30 27 31 29 30 31 28
WRMS | 9 12 9 10 11 5 9 11 9 17 |NE 26 30 25 28 26 25 29 26 27 29 26
MEDI | 9 11 8 11 10 4 8 11 11 15 |MD 24 26 23 26 26 22 26 24 27 28 24
Table 3.2006.2 GPS week: 2006 Day: 2 MJD: 58288.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 9 10 10 6 16 3 7 9 6 15 3 | 23 24 26 23 28 22 26 24 23 17 23
2E | 9 11 8 9 12 4 10 12 10 18 3 | 35 37 35 37 38 35 38 35 34 34 35
3 | 9 8 11 11 7 5 7 8 7 12 3 | 30 33 30 31 29 28 35 28 28 27 29
X4 | 1 --- --- --- --- 16 --- --- --- --- 0 | 22 --- --- --- --- 22 --- --- --- --- 22
5 | 8 10 10 10 7 4 11 13 10 19 4 | 37 40 39 34 38 36 43 30 35 35 36
6E | 8 11 10 8 8 2 6 7 6 13 3 | 23 26 26 23 23 22 25 23 22 24 23
7 | 11 13 7 11 15 5 9 13 13 14 4 | 41 40 42 42 38 41 38 42 43 39 40
8 | 8 11 8 9 8 2 7 9 7 14 3 | 24 25 22 24 25 22 26 21 22 24 22
9 | 8 8 10 7 6 5 8 6 7 14 3 | 39 44 41 41 40 40 45 38 39 41 40
10 | 10 8 11 10 5 4 8 10 5 12 3 | 22 24 21 21 20 19 24 21 19 24 20
11E | 6 8 11 7 9 3 6 10 6 16 3 | 26 28 30 27 27 26 28 28 27 30 27
12 | 11 19 9 13 14 4 9 15 15 19 4 | 26 24 21 27 22 23 24 24 26 23 22
13 | 10 10 11 9 8 4 10 12 10 24 4 | 22 29 19 26 20 22 29 26 21 33 23
14 | 9 8 10 13 8 5 7 12 10 20 3 | 21 22 18 22 18 19 19 21 19 27 19
15 | 7 13 9 10 5 4 8 14 10 23 3 | 36 44 39 35 37 35 41 32 36 41 37
16 | 10 23 8 11 12 6 8 14 12 23 4 | 24 21 19 24 20 19 19 23 20 26 19
17 | 8 8 8 16 13 5 7 10 9 14 3 | 22 27 20 28 24 21 27 23 22 22 22
18E | 14 15 14 13 12 5 14 14 16 16 5 | 93 88 82 84 92 85 91 83 84 83 86
19 | 9 15 5 14 11 4 8 10 12 15 4 | 23 28 22 23 23 21 24 22 22 21 22
20 | 9 14 12 15 9 6 9 25 11 17 4 | 22 22 20 25 15 22 21 31 21 24 22
21E | 10 8 9 11 16 5 7 12 10 15 3 | 31 30 28 28 34 26 30 27 26 22 27
22 | 9 8 11 11 8 6 7 14 11 15 3 | 37 37 33 41 36 37 39 40 37 37 36
23 | 11 17 11 11 10 6 6 10 10 16 4 | 35 32 34 38 33 35 35 34 34 33 33
24 | 10 12 7 7 12 3 8 10 9 16 3 | 24 27 23 23 25 21 22 23 21 23 22
25 | 6 16 4 6 7 3 7 6 9 11 3 | 33 38 35 33 32 33 36 33 36 35 34
26 | 10 11 8 6 10 5 6 9 6 15 3 | 59 57 57 55 58 55 59 57 58 65 58
27 | 7 8 7 7 9 3 8 10 8 11 3 | 25 25 23 22 24 21 25 19 20 25 22
28 | 10 11 7 12 14 5 7 11 10 20 4 | 22 25 22 24 23 22 26 23 20 25 21
29 | 8 21 6 10 13 4 9 15 11 17 4 | 24 23 22 24 26 21 23 24 22 23 22
30E | 12 11 10 6 18 3 9 8 8 13 4 | 34 31 33 29 37 30 31 30 31 27 30
31E | 16 14 7 13 15 5 6 12 11 14 4 | 62 66 61 63 65 62 64 64 64 60 62
32 | 6 8 11 9 4 3 7 9 8 16 3 | 17 26 18 23 19 18 25 19 20 25 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 9 10 11 4 8 12 10 16 |T 31 33 31 32 31 30 33 31 30 32 30
WRMS | 9 13 9 10 10 4 8 11 8 16 |NE 28 30 27 29 27 26 30 27 27 29 27
MEDI | 9 11 9 10 10 4 8 10 10 15 |MD 25 28 26 27 27 22 28 27 26 27 23
Table 3.2006.3 GPS week: 2006 Day: 3 MJD: 58289.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 9 10 8 16 3 7 8 9 11 3 | 22 23 25 20 30 20 22 21 22 17 21
2E | 11 10 7 9 12 5 9 10 9 15 3 | 26 24 23 22 26 21 24 25 22 21 22
3 | 7 8 11 11 6 4 6 8 8 12 3 | 21 28 23 22 22 21 28 22 23 22 23
X4 | 3 --- --- --- --- 18 --- --- --- --- 0 | 28 --- --- --- --- 22 --- --- --- --- 28
5 | 6 9 10 10 9 4 9 12 10 17 3 | 39 41 40 31 40 35 44 32 33 35 37
6E | 12 8 11 8 11 3 7 8 9 12 3 | 19 23 24 19 19 21 22 20 21 19 20
7 | 8 12 7 11 19 5 9 12 10 12 4 | 35 33 34 37 35 35 34 36 37 34 34
8 | 10 10 7 9 11 3 6 9 7 8 3 | 26 27 26 22 30 22 27 21 24 20 24
9 | 7 8 10 9 8 5 7 5 6 11 2 | 23 31 26 26 24 22 30 22 24 25 25
10 | 9 7 12 8 5 3 7 11 6 11 3 | 17 25 18 18 17 18 23 20 18 24 19
11E | 9 7 10 9 11 4 6 10 5 13 3 | 23 25 25 24 25 24 24 24 27 27 24
12 | 10 20 7 14 16 5 7 14 12 16 4 | 24 23 19 25 22 20 21 20 22 17 19
13 | 8 9 10 13 11 3 10 12 11 22 4 | 23 27 20 31 20 25 29 29 25 36 25
14 | 9 7 9 13 7 4 5 11 10 18 3 | 18 20 17 22 16 17 17 21 18 25 18
15 | 7 10 8 12 10 5 8 15 11 23 4 | 35 41 36 31 36 31 40 28 32 40 35
16 | 13 21 7 16 16 6 7 14 12 20 5 | 23 20 18 25 22 20 19 21 24 22 19
17 | 8 8 9 17 15 5 6 9 10 15 3 | 22 25 18 25 25 19 24 21 22 18 21
18E | 16 15 12 15 16 5 11 12 15 10 4 | 84 80 72 74 83 74 77 74 72 75 76
19 | 10 15 6 16 13 5 7 10 11 17 4 | 21 24 19 24 24 18 22 19 19 18 19
20 | 10 12 13 15 11 6 9 25 12 16 5 | 27 27 23 28 16 27 26 33 25 30 27
21E | 12 10 9 16 17 4 8 12 10 15 4 | 22 25 19 24 29 20 24 20 22 17 21
22 | 10 8 11 13 8 5 7 14 12 18 4 | 24 27 24 32 26 27 27 30 27 29 26
23 | 9 18 10 14 11 6 6 9 8 16 4 | 24 24 25 29 25 24 24 23 24 25 24
24 | 10 10 7 8 10 4 7 10 7 19 3 | 19 23 20 21 23 17 23 22 20 26 20
25 | 10 10 4 7 14 4 6 8 5 12 3 | 24 25 23 24 22 21 24 21 22 21 22
26 | 10 9 7 9 15 4 7 18 6 10 3 | 95 96 94 97 96 94 97 99 97 95 96
27 | 9 9 7 9 13 3 7 10 7 8 3 | 26 26 25 22 29 22 26 19 22 23 24
28 | 9 12 7 13 14 6 7 10 9 14 3 | 18 22 18 22 20 19 22 24 22 23 20
29 | 8 23 6 14 15 5 9 13 14 15 4 | 20 23 17 23 24 19 21 21 21 18 19
30E | 10 11 9 7 12 4 8 9 7 8 3 | 40 43 42 41 41 41 45 45 41 41 42
31 | 19 7 7 13 14 4 8 13 9 12 4 | 72 74 73 77 72 72 71 68 74 72 72
32 | 8 8 10 9 7 4 6 8 6 15 3 | 19 28 19 25 18 19 25 20 19 30 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 9 12 12 4 8 12 9 15 |T 29 32 29 31 30 28 31 29 29 30 29
WRMS | 9 12 9 11 12 4 8 12 8 15 |NE 26 29 25 28 27 25 29 26 26 28 26
MEDI | 9 10 9 11 12 4 7 10 9 15 |MD 23 25 23 25 25 21 24 22 23 25 23
Table 3.2006.4 GPS week: 2006 Day: 4 MJD: 58290.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 9 10 7 11 3 7 6 9 11 3 | 21 22 25 22 24 20 22 21 20 15 20
2E | 11 10 7 9 14 3 11 10 10 13 3 | 23 25 23 22 25 22 25 22 24 20 22
3 | 9 9 11 6 8 3 7 6 9 16 3 | 24 29 26 26 25 25 31 24 26 25 25
X4 | 2 --- --- --- --- 21 --- --- --- --- 0 | 24 --- --- --- --- 20 --- --- --- --- 24
5 | 7 10 9 12 11 4 12 12 11 17 4 | 40 40 36 34 35 34 41 32 32 36 36
6E | 6 7 10 9 15 3 8 7 9 10 3 | 19 23 25 19 25 21 24 20 23 22 21
7 | 6 15 9 12 16 5 13 11 12 14 4 | 28 27 29 29 30 28 27 33 32 28 28
8 | 10 10 8 10 12 4 8 8 8 13 3 | 22 26 22 21 27 19 26 21 21 25 22
9 | 7 10 11 10 9 6 8 5 7 13 3 | 36 38 38 35 33 36 42 35 37 38 36
10 | 11 7 12 9 7 3 7 7 6 9 3 | 18 24 17 19 16 16 23 18 18 19 17
11E | 10 11 11 7 10 3 7 10 5 12 3 | 28 30 30 30 25 27 27 27 27 28 27
12 | 6 20 7 14 14 6 11 13 12 18 4 | 26 25 23 29 23 25 24 24 28 26 23
13 | 9 10 10 11 9 5 10 12 11 18 4 | 25 30 23 35 24 26 31 30 29 35 28
14 | 9 7 10 11 6 3 7 11 10 19 3 | 25 26 24 24 24 23 24 25 24 26 24
15 | 7 13 8 10 10 4 11 11 12 18 4 | 29 37 29 29 29 28 32 27 31 33 29
16 | 10 23 8 13 17 5 10 12 12 19 4 | 20 18 17 22 21 18 19 21 22 22 18
17 | 7 9 9 15 16 4 7 9 11 12 3 | 17 22 15 25 22 19 24 21 22 16 19
X18E | 18 --- 14 11 15 4 15 10 13 13 5 | 90 --- 77 79 89 80 83 79 78 78 81
19 | 7 15 7 15 14 5 9 10 12 14 4 | 18 23 18 22 20 17 23 18 20 15 17
X20 | 9 13 13 16 --- 7 11 22 12 14 5 | 22 24 21 31 --- 21 24 35 24 26 22
21E | 9 11 8 17 32 4 8 12 13 13 5 | 25 27 23 27 41 22 26 22 26 18 23
22 | 13 9 12 10 7 5 8 13 13 17 4 | 28 31 24 34 32 30 33 34 33 32 29
23 | 10 19 11 12 12 6 8 10 9 16 4 | 29 26 30 33 28 31 29 31 31 30 29
24 | 11 11 8 6 10 2 8 9 9 13 3 | 19 23 20 17 20 17 21 20 20 17 18
25 | 8 11 5 8 13 4 8 7 7 14 3 | 32 32 29 31 28 29 29 30 32 30 29
26 | 11 11 9 8 14 4 7 7 8 9 3 | 48 49 45 48 48 47 47 47 49 44 47
27 | 10 8 8 8 13 4 9 9 9 11 3 | 24 25 24 22 27 20 26 20 23 27 23
28 | 9 14 6 11 12 5 9 10 8 15 3 | 17 23 17 20 20 16 21 20 18 17 17
29 | 11 21 6 15 14 6 12 14 11 16 4 | 23 22 16 22 22 18 22 21 22 21 19
30 | 8 16 11 6 24 5 10 8 8 9 4 | 30 30 32 30 34 30 33 31 32 28 30
31 | 12 10 6 12 20 3 7 11 10 13 4 | 53 57 53 57 56 54 56 54 55 53 54
32 | 6 7 9 7 4 3 7 8 7 15 2 | 16 24 14 17 17 15 25 16 17 23 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 11 14 4 9 10 10 14 |T 28 28 27 29 29 26 30 28 28 28 27
WRMS | 9 13 9 10 13 4 9 9 9 14 |NE 25 28 24 27 25 23 28 25 26 26 24
MEDI | 9 10 9 10 12 4 8 10 10 14 |MD 24 26 24 27 25 22 26 24 26 26 23
Table 3.2006.5 GPS week: 2006 Day: 5 MJD: 58291.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 9 9 8 10 4 5 9 10 13 3 | 20 22 24 20 23 21 23 23 23 19 20
2E | 13 9 9 11 13 5 10 13 11 14 4 | 25 21 22 17 23 19 22 24 22 20 20
3 | 7 8 11 7 8 4 6 9 8 12 3 | 18 26 19 20 18 19 26 20 21 22 20
X4 | 2 --- --- --- --- 14 --- --- --- --- 0 | 22 --- --- --- --- 21 --- --- --- --- 22
5 | 5 10 10 13 14 4 13 10 14 15 4 | 32 36 32 26 31 30 36 30 29 34 31
6E | 8 10 11 10 17 4 6 10 9 11 3 | 16 20 23 19 17 18 21 20 19 18 18
7 | 9 12 7 12 20 4 10 10 13 13 4 | 24 24 24 26 25 23 24 28 30 24 24
8 | 9 9 6 9 10 3 7 7 7 12 3 | 18 24 19 17 23 19 23 19 23 22 19
9 | 6 10 12 10 8 5 7 6 8 16 3 | 22 35 25 25 23 24 33 26 27 35 26
10 | 6 8 13 7 9 3 8 10 7 11 3 | 15 22 17 14 15 16 21 16 18 21 16
11E | 7 6 8 8 12 4 6 11 7 15 3 | 24 26 27 28 26 25 26 27 31 28 26
12 | 5 20 7 11 17 5 9 13 11 16 4 | 23 22 18 28 19 21 20 24 26 23 21
13 | 10 8 9 13 11 3 9 13 14 20 4 | 25 31 25 34 25 28 31 31 35 38 28
14 | 7 7 9 10 11 3 7 12 10 18 3 | 26 29 26 26 26 25 26 27 31 29 26
15 | 6 11 9 11 12 3 11 14 10 22 4 | 29 31 27 27 30 27 31 23 29 30 27
16 | 11 21 10 10 17 4 9 14 12 18 4 | 28 25 24 30 23 27 28 30 32 28 25
17 | 6 7 10 14 17 2 7 10 10 14 3 | 18 23 16 23 21 18 22 23 22 14 18
18E | 13 15 11 13 12 4 13 12 18 15 4 | 95 95 83 85 92 87 90 83 87 87 87
19 | 9 13 7 16 14 4 7 10 12 19 4 | 19 22 19 19 22 18 21 19 21 15 18
X20 | 2 --- --- --- --- 86 --- --- --- --- 0 | 20 --- --- --- --- 12 --- --- --- --- 20
21E | 11 7 8 13 19 3 10 13 11 15 4 | 21 22 19 20 31 18 22 18 23 13 19
22 | 11 9 11 11 9 3 7 16 13 16 4 | 17 22 16 24 19 18 22 23 26 24 19
23 | 8 17 9 11 11 4 7 9 10 15 3 | 16 17 18 22 16 16 17 20 22 24 17
24 | 7 10 11 5 12 3 9 11 9 18 3 | 18 21 18 17 20 17 19 21 18 23 17
25 | 7 12 7 6 13 4 7 7 13 11 3 | 21 23 25 24 22 20 24 22 25 24 22
26 | 13 10 9 9 17 2 7 9 6 9 3 | 82 80 81 79 81 81 81 80 80 81 80
27 | 9 10 6 9 11 3 8 9 7 11 3 | 22 27 23 22 24 22 24 22 25 24 22
28 | 9 15 8 15 16 3 10 10 12 11 4 | 13 20 15 17 19 16 21 20 23 16 15
29 | 9 22 6 13 16 4 10 13 11 12 4 | 22 21 18 24 22 20 21 22 22 20 19
30 | 10 13 9 7 17 3 7 6 7 7 3 | 21 21 25 22 24 21 24 23 24 20 21
31 | 9 10 7 13 24 4 8 11 11 12 4 | 43 44 42 42 47 42 43 42 43 40 42
32 | 6 8 9 8 10 4 7 9 8 15 3 | 16 25 18 21 14 19 25 18 23 28 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 9 11 14 4 8 11 11 15 |T 25 29 26 27 27 25 28 27 29 28 25
WRMS | 8 12 9 10 14 4 8 10 9 15 |NE 23 27 23 25 24 23 27 25 27 27 23
MEDI | 8 10 9 10 12 4 7 10 10 14 |MD 21 23 23 23 23 20 24 23 24 24 20
Table 3.2006.6 GPS week: 2006 Day: 6 MJD: 58292.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 9 10 7 12 3 8 7 10 10 3 | 24 24 27 21 25 21 26 23 23 21 23
2E | 10 10 8 10 10 5 11 10 10 11 3 | 28 26 25 27 31 25 27 26 24 27 25
3 | 11 8 12 10 9 4 8 9 10 11 3 | 23 30 25 24 23 23 30 22 22 27 24
X4 | 1 --- --- --- --- 19 --- --- --- --- 0 | 26 --- --- --- --- 20 --- --- --- --- 26
5 | 9 8 11 10 13 4 11 13 10 20 4 | 49 48 50 40 48 43 52 37 43 39 45
6E | 10 16 10 9 12 4 7 7 10 11 3 | 23 26 28 24 27 24 26 25 22 26 24
7 | 14 16 7 13 20 6 9 14 14 14 4 | 25 25 26 30 29 26 26 31 29 25 25
8 | 10 9 6 8 12 2 8 7 7 10 3 | 24 25 23 21 24 20 25 20 22 20 21
9 | 7 9 10 7 9 4 9 5 6 10 2 | 31 38 34 34 30 32 39 34 33 34 34
10 | 6 9 11 9 10 3 7 8 9 11 3 | 16 24 17 16 20 16 23 18 19 21 17
11E | 7 7 10 8 15 3 6 7 7 14 3 | 29 33 34 31 29 30 33 33 30 36 31
12 | 8 20 7 12 15 5 9 15 10 13 4 | 30 26 27 34 29 29 24 31 31 29 27
13 | 7 9 10 12 15 4 9 13 10 21 4 | 30 33 26 39 27 33 35 34 35 42 32
14 | 9 7 9 12 12 4 6 10 10 16 3 | 30 33 30 33 31 31 30 31 35 31 30
15 | 7 13 10 10 13 4 10 13 10 22 4 | 37 44 41 34 43 34 41 30 34 41 37
16 | 10 19 7 14 16 5 11 12 12 20 4 | 30 26 27 37 26 30 29 35 32 33 28
17 | 5 11 9 12 15 4 6 10 8 11 3 | 20 25 18 24 26 19 25 25 22 19 21
18E | 12 17 12 12 13 4 12 9 13 18 4 | 109 105 96 100 108 99 104 97 98 103 101
19 | 7 17 8 14 13 5 8 11 11 15 4 | 22 27 22 21 26 21 24 22 22 21 21
X20 | 9 15 8 16 14 6 10 24 --- 15 5 | 13 14 8 8 9 12 12 22 --- 15 12
21E | 14 8 7 14 36 4 7 11 14 13 5 | 28 27 23 25 38 22 26 22 22 17 23
22 | 12 10 12 11 10 5 9 14 12 16 4 | 27 30 23 32 28 28 30 31 33 29 28
23 | 9 19 10 12 11 4 6 10 9 14 3 | 22 22 23 31 21 24 23 28 26 28 23
24 | 6 11 8 5 15 5 8 10 8 11 3 | 19 21 20 20 24 19 20 23 17 21 19
25 | 6 11 7 9 11 4 7 9 9 17 3 | 29 28 30 28 31 28 30 30 27 37 29
26 | 9 7 7 11 13 3 6 9 8 10 3 | 75 75 76 74 79 74 78 78 74 77 76
27 | 10 9 7 8 12 2 7 8 7 10 3 | 25 25 22 22 25 21 24 20 21 23 22
28 | 9 20 8 11 16 4 7 13 8 13 4 | 20 24 19 21 23 18 22 24 21 22 19
29 | 8 21 7 12 12 5 10 12 12 13 4 | 26 29 24 24 28 23 26 26 24 25 24
30 | 13 15 10 5 19 4 8 10 7 9 3 | 26 28 30 27 31 26 30 31 29 27 27
31 | 12 9 8 13 19 5 6 11 11 15 4 | 51 54 51 53 55 52 54 56 54 53 53
32 | 7 7 10 9 10 4 7 9 9 14 3 | 22 28 19 22 19 21 29 23 24 28 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 10 15 4 8 10 10 14 |T 30 33 30 31 32 29 33 31 31 32 30
WRMS | 9 13 9 10 13 4 8 10 9 14 |NE 28 30 27 29 29 26 30 29 29 30 27
MEDI | 9 10 9 11 13 4 8 10 10 13 |MD 26 27 26 27 28 24 27 28 26 27 25
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 4.2006 GPS week: 2006 MJD: 58286.0-58292.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 |U 10 9 20 |U 9 15 25 |U 12 14 33 |
emr | emr 2945 |U 17 16 39 |U 13 15 42 | 13 16 40 |
esa | esa 2962 | 12 10 25 |U 8 13 28 | 12 15 31 |
gfz | gfz 2958 |U 10 8 20 |U 9 14 29 |U 12 16 32 |
grg | grg 2948 |U 11 11 24 |U 12 22 38 | 14 23 45 |
igr | igr 2946 | 9 8 20 | 8 13 24 | 11 15 30 |
igs | igs 2957 | 10 8 21 | 8 13 26 | 11 14 31 |
jpl | jpl 2962 |U 13 13 32 |U 10 14 34 |U 12 16 37 |
mit | mit 2962 |U 12 11 27 |U 12 17 38 |U 15 19 44 |
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 5.2006.0 GPS week: 2006 Day: 0 MJD: 58286.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 7 19 | 9 16 22 | 10 13 33 |
emr | emr 2972 | 20 19 28 | 11 17 49 | 12 17 38 |
esa | esa 2976 | 11 8 22 | 7 15 36 | 10 12 37 |
gfz | gfz 2972 | 9 6 19 | 12 19 44 | 10 13 32 |
grg | grg 2976 | 12 10 23 | 14 25 42 | 19 24 69 |
igr | igr 2958 | 9 6 17 | 8 14 26 | 10 13 31 |
igs | igs 2976 | 10 7 19 | 9 15 28 | 10 13 32 |
jpl | jpl 2976 | 13 13 30 | ---- ---- ---- | 11 16 38 |
mit | mit 2976 | 14 11 34 | 16 21 61 | 15 14 41 |
Table 5.2006.1 GPS week: 2006 Day: 1 MJD: 58287.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 7 17 | 9 18 24 | 13 15 38 |
emr | emr 2972 | 17 15 30 | 13 14 37 | 15 14 45 |
esa | esa 2976 | 12 11 20 | 8 16 24 | 14 14 34 |
gfz | gfz 2972 | 9 7 16 | 8 15 28 | 13 17 36 |
grg | grg 2976 | 10 9 22 | 14 26 36 | 16 30 67 |
igr | igr 2974 | 9 8 17 | 9 17 25 | 13 15 35 |
igs | igs 2975 | 10 7 18 | 9 16 24 | 12 14 36 |
jpl | jpl 2976 | 15 12 29 | 12 22 32 | 12 12 44 |
mit | mit 2976 | 12 8 25 | 9 15 33 | 15 20 40 |
Table 5.2006.2 GPS week: 2006 Day: 2 MJD: 58288.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 9 22 | 9 12 20 | 12 14 23 |
emr | emr 2972 | 16 16 39 | 11 13 28 | 15 21 32 |
esa | esa 2976 | 13 11 29 | 8 9 24 | 11 14 22 |
gfz | gfz 2971 | 10 8 22 | 7 8 23 | 11 14 21 |
grg | grg 2976 | 11 10 24 | 10 14 27 | 13 18 21 |
igr | igr 2975 | 11 9 24 | 8 9 19 | 11 13 19 |
igs | igs 2976 | 11 8 26 | 8 8 20 | 11 14 22 |
jpl | jpl 2976 | 14 13 36 | 10 10 31 | 11 15 34 |
mit | mit 2976 | 12 13 32 | 14 18 43 | 15 18 36 |
Table 5.2006.3 GPS week: 2006 Day: 3 MJD: 58289.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 11 20 | 9 13 28 | 13 14 42 |
emr | emr 2972 | 16 19 27 | 14 13 39 | 14 19 50 |
esa | esa 2976 | 11 11 22 | 8 11 29 | 13 17 39 |
gfz | gfz 2972 | 10 10 19 | 8 13 30 | 13 19 42 |
grg | grg 2976 | 10 13 23 | 10 16 29 | 15 21 41 |
igr | igr 2924 | 9 10 19 | 9 13 26 | 13 16 40 |
igs | igs 2962 | 10 10 18 | 8 11 28 | 12 17 40 |
jpl | jpl 2976 | 13 13 24 | 10 11 35 | 13 19 40 |
mit | mit 2976 | 10 11 24 | 8 11 34 | 16 19 44 |
Table 5.2006.4 GPS week: 2006 Day: 4 MJD: 58290.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 11 10 22 | 7 17 23 | 12 13 37 |
emr | emr 2880 | 17 14 64 | 14 16 51 | 12 15 43 |
esa | esa 2976 | 13 11 29 | 6 15 25 | 12 16 33 |
gfz | gfz 2973 | 11 10 23 | 7 15 23 | 13 15 35 |
grg | grg 2877 | 11 11 23 | 15 29 56 | 13 19 42 |
igr | igr 2975 | 10 9 24 | 7 14 21 | 12 15 34 |
igs | igs 2975 | 11 9 25 | 7 13 24 | 12 15 35 |
jpl | jpl 2976 | 14 14 37 | 8 11 32 | 14 20 42 |
mit | mit 2976 | 12 12 25 | 16 28 33 | 19 30 72 |
Table 5.2006.5 GPS week: 2006 Day: 5 MJD: 58291.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 10 9 22 | 9 14 31 | 11 16 32 |
emr | emr 2876 | 15 14 51 | 16 13 38 | 14 16 38 |
esa | esa 2880 | 10 10 25 | 9 13 31 | 11 17 26 |
gfz | gfz 2876 | 9 9 21 | 10 14 32 | 13 19 31 |
grg | grg 2880 | 14 15 33 | 11 19 37 | 11 33 53 |
igr | igr 2853 | 9 8 22 | 10 14 28 | 12 16 28 |
igs | igs 2868 | 8 8 21 | 9 13 30 | 11 16 28 |
jpl | jpl 2880 | 10 12 31 | 12 16 41 | 13 15 31 |
mit | mit 2880 | 10 9 20 | 9 13 31 | 14 18 36 |
Table 5.2006.6 GPS week: 2006 Day: 6 MJD: 58292.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 11 8 19 | 8 14 25 | 12 13 29 |
emr | emr 2972 | 19 14 32 | 15 19 50 | 13 13 34 |
esa | esa 2976 | 12 10 26 | 7 14 29 | 10 15 26 |
gfz | gfz 2972 | 10 8 21 | 8 14 25 | 12 16 29 |
grg | grg 2975 | 10 10 22 | 12 27 43 | 11 14 26 |
igr | igr 2964 | 11 8 21 | 8 13 25 | 11 13 27 |
igs | igs 2971 | 11 8 22 | 7 14 27 | 11 13 27 |
jpl | jpl 2976 | 14 14 34 | 9 16 32 | 11 14 34 |
mit | mit 2976 | 11 11 27 | 10 15 32 | 12 17 36 |
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 6.2006 GPS week: 2006 MJD: 58286.500-58292.500
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 -8 31 13 3 | 9 19
| 16 15 71 109 5 | 2
emr uuuuu | 31 -4 169 199 8 | 38 42
| 10 15 58 66 13 | 3
esa uuuuu | 6 8 -82 68 2 | 7 18
| 16 16 59 60 6 | 2
gfz uuuuu | 15 22 -7 37 -2 | 15 23
| 14 17 63 87 4 | 2
grg uuuuu | -17 -5 90 -180 -6 | 6 17
| 20 12 34 96 5 | 3
igr xxxxx | -7 6 59 -50 -2 | 0 16
| 8 12 43 22 2 | 2
irf xxxxx | 1 -7 -38 -37 0 | -1 15
| 7 10 32 15 2 | 1
jpl uuuuu | -9 -19 103 28 5 | 20 24
| 16 10 39 47 4 | 2
mit uuuuu | -10 6 -94 -85 -2 | 17 23
| 11 9 71 27 3 | 1
ngs uuuuu | -25 -7 -76 -112 -2 | 15 22
| 32 22 104 86 4 | 2
sio uuuux | 19 25 -197 51 2 | 68 70
| 18 18 68 61 6 | 1
Table 7.2006.0 GPS week: 2006 Day: 0 MJD: 58286.500
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 | 20 -36 42 236 -3 | 9 22
emr uuuuu | 48 1 107 234 15 | 33 39
esa uuuuu | -3 23 -129 15 -7 | 9 23
gfz uuuuu | 20 25 70 -11 1 | 15 27
grg uuuuu | -33 -16 76 -314 1 | 7 21
igr xxxxx | -8 -6 46 -74 -4 | 0 21
irf xxxxx | -2 -6 14 -37 -1 | 0 20
jpl uuuuu | 13 -14 81 36 9 | 16 24
mit uuuuu | -3 3 43 -49 -1 | 17 26
ngs uuuuu | -70 -23 -172 -132 -5 | 14 25
sio uuuux | 24 57 -177 -2 9 | 67 70
Table 7.2006.1 GPS week: 2006 Day: 1 MJD: 58287.500
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 | 18 -4 69 7 -2 | 8 22
emr uuuuu | 40 -12 77 330 32 | 35 40
esa uuuuu | 2 26 -178 66 -4 | 8 23
gfz uuuuu | -11 15 -4 -16 -4 | 15 27
grg uuuuu | -38 -6 134 -292 -2 | 7 21
igr xxxxx | -21 17 68 -23 -3 | -1 21
irf xxxxx | -8 2 -35 -55 -2 | -1 20
jpl uuuuu | 12 -23 45 -27 8 | 17 25
mit uuuuu | -22 5 -97 -107 -3 | 16 26
ngs uuuuu | -31 -12 96 -16 -4 | 14 25
sio uuuux | 52 19 -198 108 4 | 68 70
Table 7.2006.2 GPS week: 2006 Day: 2 MJD: 58288.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 3 6 -65 -13 12 | 11 20
emr uuuuu | 25 4 200 178 9 | 40 45
esa uuuuu | 29 -1 -7 68 4 | 10 22
gfz uuuuu | 29 11 -79 -73 -9 | 19 25
grg uuuuu | -23 -22 48 -179 -6 | 10 18
igr xxxxx | 1 -11 117 -61 -3 | 3 16
irf xxxxx | 9 5 -77 -20 -3 | 2 17
jpl uuuuu | -11 -2 109 95 0 | 21 24
mit uuuuu | -12 21 -152 -50 -3 | 19 25
ngs uuuuu | -35 -27 23 -31 -4 | 18 24
sio uuuux | 13 43 -190 1 4 | 71 72
Table 7.2006.3 GPS week: 2006 Day: 3 MJD: 58289.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 11 -17 -38 -24 2 | 10 17
emr uuuuu | 36 9 237 179 7 | 39 43
esa uuuuu | 9 12 -89 60 4 | 7 15
gfz uuuuu | 12 38 -102 47 -5 | 16 20
grg uuuuu | -4 -12 130 -126 -6 | 8 13
igr xxxxx | 3 7 71 -44 -4 | 1 13
irf xxxxx | 12 -16 -35 -40 2 | -1 12
jpl uuuuu | -11 -15 131 82 7 | 20 24
mit uuuuu | -8 14 -81 -109 1 | 18 22
ngs uuuuu | -32 -24 -59 -137 2 | 16 21
sio uuuux | 10 22 -213 -4 7 | 69 70
Table 7.2006.4 GPS week: 2006 Day: 4 MJD: 58290.500
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 | 21 -10 17 -36 6 | 8 17
emr uuuuu | 19 12 201 143 7 | 38 42
esa uuuuu | 24 12 -86 188 6 | 5 15
gfz uuuuu | 16 4 -6 160 1 | 14 20
grg uuuuu | -2 5 107 -132 -11 | 5 14
igr xxxxx | -5 7 40 -47 2 | -1 14
irf xxxxx | 4 -24 -26 -37 4 | -2 13
jpl uuuuu | -29 -23 144 -15 8 | 20 24
mit uuuuu | -24 -5 -79 -89 1 | 17 21
ngs uuuuu | -36 1 -112 -277 -5 | 15 21
sio uuuux | 31 22 -175 126 3 | 69 70
Table 7.2006.5 GPS week: 2006 Day: 5 MJD: 58291.500
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 | 0 5 150 34 -1 | 8 17
emr uuuuu | 28 -11 202 142 -4 | 39 42
esa uuuuu | -2 -23 -29 2 6 | 4 15
gfz uuuuu | 30 52 38 147 0 | 14 20
grg uuuuu | -32 8 65 -175 -6 | 4 15
igr xxxxx | -6 8 90 -21 -4 | -2 15
irf xxxxx | 1 -9 -78 -52 2 | -2 13
jpl uuuuu | -14 -23 69 -1 3 | 21 24
mit uuuuu | -9 3 -180 -113 -4 | 17 21
ngs uuuuu | -4 -3 -119 -93 3 | 14 20
sio uuuux | 9 4 -325 18 -5 | 68 69
Table 7.2006.6 GPS week: 2006 Day: 6 MJD: 58292.500
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 | -23 1 42 -115 5 | 6 16
emr uuuuu | 25 -31 158 185 -8 | 38 42
esa uuuuu | -18 9 -57 76 8 | 4 14
gfz uuuuu | 8 10 38 6 2 | 13 19
grg uuuuu | 16 4 70 -41 -11 | 2 15
igr xxxxx | -10 22 -17 -77 1 | -4 15
irf xxxxx | -5 1 -28 -16 0 | -2 13
jpl uuuuu | -22 -35 144 26 0 | 22 24
mit uuuuu | 10 0 -111 -80 -6 | 15 20
ngs uuuuu | 34 37 -187 -97 1 | 13 19
sio uuuux | -2 10 -97 113 -6 | 67 68
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