[IGSREPORT-25991] Wk 2005 IGS Final Orbits
acc
acc at igs.org
Thu Jun 28 21:41:17 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2005 (Jun 10, 2018 - Jun 16, 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:
igs2005[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2005[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2005[0-6].cls IGS GPS clock combination summary report.
igs20057.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20057.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 | KOUR NAUR TIXI WIND KOUR NAUR TIXI WIND
0 | ESA | 22 22 MAL2 MAL2 NOVM
0 | GFZ | 18 18 GODE KOUR MAL2 REUN GODE KOUR MAL2 REUN
0 | GRG | GLSV KIT3 MAL2 GLSV KIT3 MAL2 TONG
1 | COD | FAA1 TIXI ABPO BAKO TIXI
1 | EMR | USUD YAR2
1 | ESA | 22 22 MAL2 MAL2 YELL ZAMB
1 | GFZ | 18 18 ABPO FAA1 MAL2 REUN ABPO MAL2 REUN
1 | GRG | GLSV SCUB BRST GLSV SCUB TONG
1 | JPL | MAL2
1 | MIT | BAKE CHPI CHUR DRAO FALK FLIN GRAZ IISC KAT1 MBAR
1 | MIT | SUTH BAKE CHPI CHUR DRAO FALK FLIN GRAZ IISC KAT1
1 | MIT | MBAR PIE1 SUTH ZAMB
2 | COD | TIXI HARB SCUB TIXI
2 | EMR | MAR6
2 | ESA | 22 FAA1 FAA1
2 | GFZ | 18 18 MAL2 XMIS BJNM MAL2 XMIS
2 | GRG | FAA1 GLSV RABT SCUB SEYG FAA1 GLSV RABT SCUB SEYG
2 | GRG | TONG
2 | MIT | ALBH BAKE CHPI DUBO FAA1 FLIN IISC KIRU PIE1 STR1
2 | MIT | SUTH ALBH BAKE CHPI DUBO FAA1 FLIN IISC KIRU PIE1
2 | MIT | STR1 SUTH
3 | COD | 11 11 TIDB TIXI SEYG TIDB TIXI
3 | EMR | HOB2
3 | ESA | FAA1 REUN
3 | GFZ | 18 18 MAL2 MAL2 NYA1
3 | GRG | FAA1 GLSV KIT3 LPGS MAL2 SEYG BOGT GLSV KIT3 LPGS
3 | GRG | MAL2 SEYG TONG
3 | MIT | CEDU CHPI DARW DUBO FAA1 FLIN HOB2 OHI2 PIE1 SUTH
3 | MIT | WAB2 CEDU CHPI DARW DUBO FLIN HOB2 NYAL OHI2 PIE1
3 | MIT | SUTH WAB2
4 | COD | MAL2 NAUR TIXI LHAZ NAUR NNOR TIXI
4 | ESA | CHUR FAA1 MAL2 CHUR FAA1
4 | GFZ | 18 18 BJNM PRDS REUN TLSE BJNM COCO PRDS REUN
4 | GRG | FAA1 GLSV KIT3 PDEL ULAB COCO FAA1 GLSV KIT3 LHAZ
4 | GRG | NNOR PDEL SCUB TONG ULAB
4 | JPL | LAUT
4 | MIT | ALBH BAKE CEDU DUBO FLIN GRAZ HLFX KAT1 KIRU MAL2
4 | MIT | MAS1 PIE1 REDU TWTF ALBH BAKE CEDU DUBO FLIN GRAZ
4 | MIT | HLFX KAT1 KIRU MAS1 MKEA PIE1 REDU TWTF
5 | COD | NAUR TIXI TLSE HARB MAL2 NAUR SEYG TIXI TLSE
5 | EMR | HOB2 THTI
5 | ESA | MAL2 MDVJ
5 | GFZ | 18 18 BJNM HYDE REUN BAKO BJNM HYDE REUN
5 | GRG | FAA1 GLSV LPGS SCUB SEYG TONG ULAB FAA1 GLSV LPGS
5 | GRG | SCUB SEYG TLSE TONG ULAB
5 | JPL | LAUT
5 | MIT | BAKE BJNM DRAO DUBO GRAZ HOB2 KIRU MAS1 MKEA NNOR
5 | MIT | OHI2 PIE1 SCH2 STJO STR1 WAB2 YELL BAKE BJNM DRAO
5 | MIT | DUBO GRAZ HOB2 KIRU MAS1 MKEA NNOR OHI2 PIE1 SCH2
5 | MIT | STR1 WAB2 YELL
6 | COD | HARB NRC1 TIXI HARB NRC1 TIXI TLSE
6 | ESA | CUSV CUSV LMMF SCH2
6 | GFZ | 18 18 REUN GUAT MCIL REUN
6 | GRG | GLSV KOUR RIO2 WIND ALRT DARW GLSV KOUR MAL2 RIO2
6 | GRG | TONG WIND
6 | JPL | POLV
6 | MIT | ALBH BAKE CHUR DARW DRAO GRAZ HOB2 KAT1 KIRU NRC1
6 | MIT | OHI2 SCH2 VILL WAB2 WHIT ALBH BAKE CHUR DARW DRAO
6 | MIT | GRAZ HOB2 KAT1 KIRU NRC1 OHI2 SCH2 VILL 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. 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.
7. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These 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 | .5 .4 1.2 10 -8 -1 -.58
EMR | 0 | -3.4 -1.6 -1.9 -7 9 34 -.06
ESA | 0 | -.2 -.4 -.6 -5 5 2 -.46
GFZ | 0 | .5 .1 .9 -14 -24 1 -.33
GRG | 0 | 1.8 -3.3 -14.1 39 -25 52 -.21
JPL | 0 | 3.6 -7.9 -3.2 5 -16 -19 -.29
MIT | 0 | .1 -4.8 3.1 -14 37 16 -.12
NGS | 0 | 2.0 -9.1 -.7 2 -18 -30 -.20
SIO | 0 | -.4 -1.5 -6.4 1 6 0 -.14
COD | 1 | .3 .3 .9 13 7 -11 -.60
EMR | 1 | 5.5 -3.9 .6 -3 -18 31 -.25
ESA | 1 | -.6 -.2 .2 2 0 4 -.62
GFZ | 1 | .8 -.2 .8 -10 -27 10 -.51
GRG | 1 | 6.2 -5.9 -10.6 40 -17 36 -.45
JPL | 1 | 12.5 -4.9 -8.1 4 -2 -11 -.51
MIT | 1 | -1.4 -3.1 5.0 -30 41 6 -.21
NGS | 1 | -.6 -4.7 1.9 17 -33 -29 -.38
SIO | 1 | 1.9 -.7 -3.9 -5 4 -7 -.15
COD | 2 | -.4 .4 .8 25 27 -8 -.43
EMR | 2 | -1.3 -2.4 -2.0 14 -20 60 -.15
ESA | 2 | -1.2 .2 .0 8 -19 21 -.50
GFZ | 2 | -.1 -.1 .7 -7 -21 17 -.29
GRG | 2 | 4.8 -3.6 -10.5 46 22 22 -.17
JPL | 2 | 6.9 -7.4 -8.6 2 9 -10 -.23
MIT | 2 | -.9 -3.5 5.1 -35 41 25 -.35
NGS | 2 | -.4 -7.5 -8.0 32 8 -53 -.31
SIO | 2 | .1 -1.6 -.6 -7 12 -13 -.17
COD | 3 | -.1 .4 1.1 18 26 -9 -.49
EMR | 3 | 1.8 -8.0 -4.4 0 -7 53 .01
ESA | 3 | -1.0 .4 .5 9 10 4 -.59
GFZ | 3 | .5 .2 .3 4 -23 4 -.32
GRG | 3 | 4.7 .5 -6.1 50 29 -2 -.27
JPL | 3 | 5.1 -10.4 -8.6 -17 6 -11 -.29
MIT | 3 | -3.1 -1.7 .5 -16 65 9 -.15
NGS | 3 | -5.2 -11.1 -1.8 1 29 -114 -.15
SIO | 3 | -2.9 .0 -3.8 -8 5 1 -.09
COD | 4 | .2 .9 1.1 16 14 -21 -.38
EMR | 4 | -1.5 -12.4 -6.3 15 -9 72 .05
ESA | 4 | -.0 .0 .1 25 12 5 -.39
GFZ | 4 | .3 .2 .4 -1 -18 -1 -.30
GRG | 4 | 3.6 -1.7 -6.5 54 23 15 -.25
JPL | 4 | 2.1 -4.7 -10.7 1 -5 12 -.25
MIT | 4 | -4.2 -.9 5.0 -15 45 -5 -.20
NGS | 4 | -5.9 -7.2 -9.0 40 41 -89 -.27
SIO | 4 | -2.1 .8 .9 17 10 -7 -.20
COD | 5 | .5 .7 1.3 23 5 -10 -.47
EMR | 5 | -.3 -1.7 -1.2 -14 3 28 -.04
ESA | 5 | -.2 .3 .4 9 5 16 -.38
GFZ | 5 | .0 .1 .4 -9 -21 7 -.37
GRG | 5 | 1.8 -1.7 -2.0 56 21 26 -.34
JPL | 5 | 5.0 -6.4 -5.7 2 12 -7 -.50
MIT | 5 | -5.2 -1.6 4.4 -14 16 7 -.21
NGS | 5 | .9 -.7 3.7 4 -29 -12 -.26
SIO | 5 | -2.5 5.1 3.3 2 10 1 -.25
COD | 6 | .3 .3 1.2 12 3 -7 -.44
EMR | 6 | -3.3 -4.1 -.8 -14 -32 72 -.02
ESA | 6 | .2 -.4 -.1 6 -2 20 -.37
GFZ | 6 | .1 .1 .7 2 -21 7 -.36
GRG | 6 | 2.5 -4.4 2.8 51 21 22 -.38
JPL | 6 | 3.3 -6.0 -4.3 -3 7 -17 -.45
MIT | 6 | -1.8 -3.7 6.2 -20 21 7 -.13
NGS | 6 | .7 -4.3 -.1 -8 -35 -37 -.30
SIO | 6 | 1.0 2.4 3.1 -3 -6 18 -.26
8. 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.
9. 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 1.2005.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2005.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 2.2005.[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 3.2005.[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 5.2005.0-6). 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 2005 summary. (Jun 10, 2018 - Jun 16, 2018)
Table 1.2005.a GPS week: 2005 MJD: 58279.000-58285.000
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 262| 0 0 0 11 -15 -7 -.07 10 9 | -620 32 6 94
| 0 0 1 4 14 9 .02 | 264 353
emr 80| 0 -2 0 -1 1 20 .18 12 12 | 137576 92 17 116
| 1 1 1 10 13 17 .03 | 375 375
esa 150| 0 0 -4 -4 8 -5 -.10 9 9 | -1152 -273 8 222
| 0 0 0 7 10 9 .01 | 836 1126
gfz 179| -1 1 5 1 -12 -9 .01 11 10 | -145 -188 12 134
| 0 1 1 13 12 9 .01 | 174 257
grg 107| 1 1 -8 -4 1 -14 -.07 13 12 | -72 76 9 166
| 0 0 4 6 13 16 .02 | 169 186
igr n/a| 0 0 0 -12 -12 -1 -.06 4 4 | 2306 -394 10 69
| 0 0 1 7 9 8 .01 | 994 429
jpl 80| 0 0 0 -3 8 27 .15 8 8 | 133505 52 8 111
| 0 0 0 7 11 12 .01 | 299 398
mit 349| 0 0 2 -6 0 -7 -.05 11 10 | 149 -110 41 427
| 0 0 1 18 9 8 .01 | 350 335
ngs 208| -1 0 0 8 -2 11 -.01 9 8 | -610 7 1007 2184
| 0 0 1 10 12 16 .04 | 224 320
sio 339| 0 0 4 3 11 -35 -.12 14 14 | --- --- --- ---
| 0 0 1 10 31 18 .04 | --- ---
Table 1.2005.b GPS week : 2005 MJD: 58279.000-58285.000
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 | 3 3 3 4 4 3 3 |
2 | 4 4 4 4 4 4 5 |
3 | 3 3 3 3 3 3 3 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 4 4 4 4 4 |
6 | 3 3 3 3 3 3 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 3 3 3 3 3 3 3 |
12 | 4 4 4 4 4 4 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 3 4 |
18 | 4 4 4 4 4 5 5 |
19 | 4 4 4 4 4 3 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 5 4 5 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 4 4 4 4 |
25 | 3 3 3 3 3 4 3 |
26 | 3 3 3 3 3 3 3 |
27 | 3 4 3 3 3 3 3 |
28 | 4 4 4 4 4 4 4 |
29 | 4 5 5 5 5 5 4 |
30 | 4 4 4 4 4 4 3 |
31 | 4 4 3 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 2.2005.0 GPS week: 2005 Day: 0 MJD: 58279.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 263| 1 0 0 11 -10 -13 -.07 8 8 | -827 325 7 112
emr 80| -1 -2 0 -8 8 25 .23 12 12 | 137364 -536 14 111
esa 150| 0 0 -3 -13 -9 -20 -.07 8 9 | -572 -866 7 211
gfz 176| -1 1 6 1 1 -13 .02 11 10 | -59 -535 12 130
grg 102| 2 0 -13 -7 -19 -13 -.09 13 12 | -31 0 10 162
igr n/a| 0 0 1 -23 -8 -1 -.05 4 4 | 3912 -984 9 68
jpl 80| 0 0 1 -4 18 31 .17 8 8 | 133568 -577 9 121
mit 349| 0 0 2 -1 0 -3 -.03 11 11 | 742 -543 39 254
ngs 212| 0 0 1 21 10 21 -.08 9 7 | -742 179 799 1984
sio 342| 0 0 6 2 12 -18 -.20 14 15 | --- --- --- ---
Table 2.2005.1 GPS week: 2005 Day: 1 MJD: 58280.000
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 267| 0 0 2 1 -26 -4 -.06 9 9 | -606 -27 6 86
emr 80| 0 0 0 3 17 -15 .18 12 12 | 137087 550 15 127
esa 150| 0 0 -3 -7 18 -8 -.09 9 9 | -841 -582 10 236
gfz 183| 0 0 4 8 -19 -4 -.00 11 10 | -54 -43 11 120
grg 109| 1 0 -13 -1 -14 -11 -.07 13 12 | -183 141 10 192
igr n/a| -1 0 0 -12 0 0 -.08 4 4 | 3039 -168 11 63
jpl 80| 0 0 0 -11 23 29 .16 8 8 | 133239 339 9 112
mit 349| 0 -1 3 -1 -5 -12 -.04 11 10 | 254 -208 41 645
ngs 213| -2 1 1 15 4 22 -.04 9 8 | -602 -57 1485 2350
sio 344| -2 0 5 12 1 -22 -.10 15 14 | --- --- --- ---
Table 2.2005.2 GPS week: 2005 Day: 2 MJD: 58281.000
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 267| 0 0 -2 10 -12 1 -.07 9 9 | -303 -423 6 81
emr 80| 0 -1 1 -5 -6 25 .18 12 12 | 137647 -273 18 118
esa 150| 1 0 -5 -2 -2 -2 -.11 9 9 | -239 -1520 9 245
gfz 181| -2 1 5 7 9 10 .03 11 10 | -73 -126 13 195
grg 110| 2 1 -9 -7 13 -29 -.06 14 12 | 184 -239 11 183
igr n/a| 0 0 1 -8 -3 -1 -.04 4 4 | 2907 -948 10 81
jpl 80| 0 0 0 0 -6 18 .14 9 9 | 133664 -419 9 129
mit 349| 0 -1 4 -15 13 -3 -.05 10 9 | 212 -334 39 480
ngs 210| -1 0 -1 16 -11 7 .00 9 8 | -400 -386 1023 2139
sio 342| 0 -1 3 0 20 -48 -.12 14 13 | --- --- --- ---
Table 2.2005.3 GPS week: 2005 Day: 3 MJD: 58282.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 262| 1 -1 -1 11 12 10 -.10 9 9 | -424 -194 7 99
emr 80| 0 -1 0 2 10 32 .16 13 13 | 137277 334 19 129
esa 150| 0 0 -5 -11 14 -10 -.11 9 9 | -672 -1065 9 231
gfz 180| -1 2 4 -17 -21 -14 -.01 11 11 | -389 89 13 110
grg 112| 2 0 -5 7 1 -39 -.05 13 12 | -20 103 9 170
igr n/a| 0 0 0 -19 -24 2 -.06 4 4 | 1873 -188 10 76
jpl 80| 0 -1 0 -9 -1 26 .16 8 8 | 133127 230 8 109
mit 350| 0 0 1 12 -2 -20 -.03 11 10 | -44 105 43 447
ngs 210| -2 0 2 2 0 11 .01 9 8 | -568 98 651 2452
sio 338| -1 0 2 7 -31 -21 -.07 14 13 | --- --- --- ---
Table 2.2005.4 GPS week: 2005 Day: 4 MJD: 58283.000
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| 1 -1 0 10 -28 -14 -.10 12 12 | -493 -84 8 99
emr 80| 0 -3 0 15 -7 24 .15 12 12 | 137711 81 20 111
esa 150| 0 0 -4 10 11 1 -.10 9 9 | -1459 985 7 191
gfz 178| -1 0 6 15 -22 -17 .02 11 10 | 15 -235 12 130
grg 107| 1 1 -7 -5 7 -12 -.08 14 12 | -22 58 10 153
igr n/a| 0 0 2 -3 -23 11 -.07 4 4 | 1815 -511 10 59
jpl 80| 0 0 0 5 2 52 .15 8 8 | 133440 41 8 104
mit 349| 0 0 3 -35 10 -14 -.07 10 9 | 314 -309 41 355
ngs 205| 0 0 0 -5 8 -21 .03 9 8 | -360 -285 861 1822
sio 336| 0 0 4 -4 -3 -28 -.08 14 14 | --- --- --- ---
Table 2.2005.5 GPS week: 2005 Day: 5 MJD: 58284.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 261| 0 -1 -1 16 -31 -11 -.07 10 9 | -1090 653 6 87
emr 80| 1 -3 1 -16 5 16 .16 12 12 | 137721 266 18 104
esa 150| 0 0 -4 -1 15 -5 -.12 9 8 | -2710 1566 12 225
gfz 179| -1 2 4 -14 -17 -16 .01 12 11 | -55 -525 13 136
grg 110| 0 1 -4 -6 3 3 -.08 11 10 | -369 388 8 154
igr n/a| 0 0 0 -16 -12 -11 -.06 4 4 | 1227 -39 11 74
jpl 80| 0 0 0 -10 18 12 .13 8 8 | 133457 317 8 105
mit 348| 0 0 2 15 -12 -4 -.06 11 10 | -352 447 43 363
ngs 208| -1 0 0 -2 -5 26 .03 10 8 | -1027 580 1322 1996
sio 338| -1 0 3 19 12 -35 -.14 14 14 | --- --- --- ---
Table 2.2005.6 GPS week: 2005 Day: 6 MJD: 58285.000
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 -1 -1 15 -13 -17 -.04 10 9 | -599 -20 6 97
emr 80| -1 -2 -2 0 -21 35 .16 12 12 | 138229 228 17 112
esa 150| 0 0 -5 -2 8 7 -.11 9 9 | -1572 -434 8 216
gfz 178| -2 3 3 12 -17 -12 .02 11 10 | -405 56 12 120
grg 99| 2 1 -1 -12 16 4 -.09 12 11 | -66 82 8 148
igr n/a| 0 1 -1 -3 -12 -11 -.06 4 4 | 1374 76 10 68
jpl 80| 0 0 0 6 4 22 .14 8 8 | 134041 438 9 100
mit 349| 0 0 2 -18 -9 4 -.06 11 11 | -82 66 45 446
ngs 204| 0 0 2 11 -25 12 -.01 10 8 | -572 -78 914 2547
sio 335| 0 0 4 -10 71 -70 -.11 13 13 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.2005.0 GPS week: 2005 Day: 0 MJD: 58279.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 10 7 7 17 4 8 6 5 11 3 | 27 32 30 29 31 29 31 30 28 28 29
2 | 7 9 6 10 16 3 9 9 9 12 3 | 34 35 33 35 34 33 34 32 32 32 33
3 | 8 7 11 9 5 4 8 8 5 12 3 | 29 35 29 28 28 28 36 30 30 29 30
X4 | 1 --- --- --- --- 22 --- --- --- --- 0 | 35 --- --- --- --- 30 --- --- --- --- 36
5 | 5 7 9 11 10 4 12 9 11 18 3 | 45 49 47 39 51 43 53 42 42 45 45
6 | 8 10 8 7 13 3 7 7 7 10 3 | 35 42 37 37 37 37 40 37 36 39 37
7E | 12 13 6 13 15 4 10 11 10 12 4 | 26 26 30 33 32 29 26 34 31 28 28
8 | 8 8 6 8 9 3 6 7 7 7 2 | 25 30 28 27 28 26 29 26 25 27 27
9 | 5 7 8 8 10 4 6 7 5 13 2 | 23 29 27 25 24 23 30 25 24 31 25
10 | 6 8 11 8 8 2 6 10 6 10 3 | 25 33 27 26 26 26 32 30 27 31 27
11E | 6 13 6 8 18 3 7 8 5 9 3 | 125 126 124 124 125 125 125 122 122 125 124
12 | 9 16 7 12 12 3 10 12 11 14 4 | 30 33 30 33 31 31 31 34 31 31 30
13 | 8 10 10 13 13 3 12 13 12 20 4 | 37 42 36 45 37 40 40 45 43 47 40
14 | 8 8 9 12 11 4 8 12 11 20 4 | 20 22 21 25 20 21 21 23 22 24 20
15 | 7 13 10 15 12 5 11 23 12 21 5 | 44 51 47 41 49 42 50 43 40 47 44
16 | 10 24 6 15 14 6 7 14 12 18 4 | 28 28 25 35 25 30 28 32 31 30 28
17 | 9 11 8 14 11 4 9 12 9 11 3 | 29 33 28 31 29 30 30 33 30 29 29
18 | 13 9 8 11 11 4 8 7 6 13 3 | 58 56 50 50 49 52 55 51 51 55 52
19 | 7 16 7 12 8 3 8 12 8 16 3 | 29 36 30 31 31 31 34 32 30 30 30
20 | 9 9 9 9 12 4 8 13 11 17 3 | 37 39 37 38 37 38 37 43 36 43 37
21 | 7 11 8 12 16 3 9 12 10 15 4 | 40 41 40 43 41 40 39 41 40 38 39
22 | 9 6 10 9 6 5 6 14 9 19 3 | 23 26 20 26 19 23 25 23 24 29 22
23 | 8 20 8 14 12 6 7 11 10 18 4 | 18 20 19 29 18 19 19 22 20 27 19
24E | 7 12 10 8 21 3 9 11 9 18 4 | 76 77 80 75 75 76 75 77 75 74 75
25 | 7 8 6 5 8 2 10 7 11 9 3 | 26 32 28 26 28 26 30 27 26 29 27
26 | 8 8 6 8 10 3 6 8 6 10 2 | 27 28 25 27 28 24 28 24 25 27 26
27 | 6 9 5 8 11 2 7 8 6 8 2 | 25 26 24 24 25 23 26 23 21 26 23
28 | 11 9 7 14 13 5 8 12 9 15 3 | 21 25 20 23 20 20 24 24 20 20 20
29 | 9 21 6 12 13 4 11 11 12 13 4 | 35 35 33 39 33 34 32 36 36 35 34
30E | 12 14 13 8 18 3 6 7 10 8 4 | 22 25 29 26 24 24 26 24 25 19 23
31E | 13 10 5 12 14 4 8 10 7 12 3 | 32 36 31 33 30 31 35 32 31 29 31
32 | 5 8 10 7 8 3 7 10 7 12 3 | 37 41 38 38 38 37 41 35 36 39 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 8 11 13 4 8 11 9 14 |T 35 38 35 36 35 35 37 36 35 36 35
WRMS | 8 12 9 10 12 4 8 11 7 15 |NE 27 30 27 29 27 27 29 29 27 29 27
MEDI | 8 10 8 10 12 4 8 10 9 13 |MD 29 33 30 33 31 30 32 32 31 30 30
Table 3.2005.1 GPS week: 2005 Day: 1 MJD: 58280.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 12 7 8 15 3 8 7 7 12 3 | 23 26 25 21 26 22 26 25 23 25 23
2 | 7 10 6 11 18 4 9 8 9 12 3 | 31 32 31 34 32 31 31 30 31 32 30
3 | 7 8 11 9 5 4 9 6 6 13 3 | 19 29 21 18 20 20 30 21 23 22 22
X4 | 2 --- --- --- --- 23 --- --- --- --- 0 | 28 --- --- --- --- 19 --- --- --- --- 28
5 | 7 8 9 10 10 3 10 9 9 21 3 | 30 32 29 26 34 27 34 26 26 36 29
6 | 5 8 8 8 12 3 9 5 8 11 3 | 26 32 29 26 28 27 33 27 25 29 27
7E | 10 13 7 11 17 5 10 10 12 12 4 | 21 23 27 30 23 27 25 32 33 30 26
8 | 10 7 5 9 11 2 6 7 6 6 2 | 21 25 23 23 24 21 25 22 22 21 22
9 | 7 9 9 6 10 4 5 4 5 10 2 | 24 30 24 26 23 24 30 27 27 31 26
10 | 8 9 10 10 9 2 8 10 6 13 3 | 16 24 15 15 16 15 23 18 16 21 17
11E | 6 9 7 9 17 4 7 7 6 9 3 | 105 102 103 104 104 103 100 101 102 103 102
12 | 8 18 9 15 10 4 8 13 11 19 4 | 25 24 20 28 22 23 24 29 26 27 23
13 | 9 10 11 14 13 4 11 12 9 20 4 | 30 35 29 40 32 33 34 34 34 39 32
14 | 7 10 9 13 12 4 7 10 11 19 3 | 17 19 16 21 17 18 18 21 22 25 17
15 | 8 12 12 16 11 5 12 25 12 21 5 | 29 33 30 25 34 25 35 30 26 34 28
16 | 11 23 7 12 13 5 9 15 11 17 4 | 23 19 21 29 20 23 20 28 26 26 22
17 | 11 9 9 13 12 4 7 12 10 15 4 | 21 26 19 25 23 21 25 26 24 23 22
18 | 12 9 8 11 13 5 9 7 8 13 3 | 50 50 44 45 44 47 50 47 46 49 47
19 | 9 13 10 11 11 5 7 10 11 14 3 | 24 25 21 21 22 19 22 22 22 20 21
20 | 9 12 9 12 11 4 9 13 11 15 4 | 23 26 26 26 25 24 27 27 22 28 24
21 | 8 13 9 13 18 5 10 13 9 14 4 | 38 41 37 40 39 38 38 39 40 37 37
22 | 9 9 11 9 8 4 6 12 9 20 3 | 15 22 12 18 13 16 20 16 19 26 16
23 | 9 17 9 15 13 7 7 11 10 15 4 | 17 16 14 24 15 17 16 20 20 24 16
24E | 8 12 15 6 18 3 10 8 7 18 4 | 76 75 84 77 75 77 76 76 77 77 77
25 | 7 9 6 8 7 3 6 7 8 11 2 | 22 24 22 21 22 19 25 21 20 24 22
26 | 10 7 7 6 9 3 7 8 7 9 2 | 20 23 23 21 22 19 23 19 22 22 21
27 | 11 11 8 9 13 2 8 9 9 8 3 | 20 24 23 22 24 19 22 20 20 21 20
28 | 11 11 9 11 14 5 8 12 9 16 4 | 16 22 17 20 18 17 23 23 22 23 19
29 | 7 25 7 14 12 5 11 11 14 13 4 | 23 25 22 27 23 23 25 26 26 23 23
30E | 10 16 11 7 16 4 7 7 8 13 3 | 19 23 25 21 22 20 24 22 23 18 20
31E | 11 11 6 11 18 4 9 12 10 14 4 | 29 33 32 35 30 32 32 30 34 31 31
32 | 7 8 10 7 8 3 6 12 7 15 3 | 32 36 33 34 35 33 39 33 34 38 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 9 11 13 4 8 11 9 15 |T 28 31 28 30 29 28 31 30 30 31 28
WRMS | 9 12 9 10 12 4 8 10 8 14 |NE 21 24 20 23 21 20 23 23 22 24 21
MEDI | 8 10 9 11 12 4 8 10 9 14 |MD 23 26 24 26 23 23 25 26 25 26 23
Table 3.2005.2 GPS week: 2005 Day: 2 MJD: 58281.000
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 | 7 12 8 7 16 3 7 5 6 12 3 | 22 26 22 22 27 22 25 24 23 21 22
2 | 10 10 6 9 21 3 11 9 9 13 4 | 40 40 40 39 43 38 40 38 38 39 38
3 | 8 9 11 8 9 3 9 6 9 13 3 | 21 30 24 24 23 24 32 24 27 24 25
X4 | 2 --- --- --- --- 57 --- --- --- --- 0 | 28 --- --- --- --- 41 --- --- --- --- 29
5 | 8 9 8 10 9 4 10 9 9 15 3 | 34 34 32 29 35 30 36 27 31 33 31
6 | 7 11 10 8 13 3 8 6 10 10 3 | 25 34 31 27 30 28 33 28 28 31 28
7E | 10 15 8 11 19 6 10 12 10 12 4 | 22 23 25 29 25 25 21 30 30 22 24
8 | 7 8 6 9 10 3 6 6 7 7 2 | 21 24 24 25 26 22 25 22 23 21 22
9 | 6 10 9 9 11 5 7 5 4 10 2 | 22 27 24 26 24 22 28 23 24 28 24
10 | 10 8 10 10 8 4 7 8 9 10 3 | 17 24 15 19 15 16 23 17 18 20 17
11E | 11 12 6 9 13 5 10 6 6 7 3 | 63 63 63 61 58 62 62 62 61 61 61
12 | 8 17 9 14 15 4 9 11 11 15 4 | 25 26 20 25 25 23 24 26 26 21 23
13 | 8 9 12 11 12 3 11 13 10 20 4 | 30 36 30 38 30 32 36 35 34 39 33
14 | 7 9 11 12 11 4 7 10 11 18 3 | 17 19 16 19 14 18 17 23 24 26 18
15 | 11 11 12 13 11 5 10 24 11 20 5 | 35 37 35 30 37 30 37 33 32 34 33
16 | 14 22 7 15 13 6 9 13 11 17 4 | 21 21 19 27 20 22 18 24 23 22 19
17 | 8 9 9 13 16 3 9 11 8 12 3 | 23 24 17 22 24 20 24 25 24 18 21
18 | 12 9 9 12 12 5 9 7 8 13 3 | 51 50 46 45 46 47 49 45 45 50 46
19 | 8 14 7 12 16 4 8 10 8 13 3 | 20 22 18 19 22 17 22 21 21 16 18
20 | 10 12 10 13 11 4 10 11 11 14 4 | 26 26 27 29 25 25 27 27 28 27 26
21 | 10 11 8 14 30 7 20 10 10 12 5 | 44 44 40 42 39 41 44 39 39 39 39
22 | 9 8 12 10 9 4 7 11 9 19 3 | 14 22 13 23 14 18 20 19 18 25 17
23 | 9 18 9 12 13 6 7 11 9 17 4 | 16 15 16 23 15 17 16 19 19 24 16
24E | 8 11 11 8 13 4 9 7 9 14 3 | 64 67 69 68 69 66 69 69 68 69 67
25 | 5 8 8 6 10 2 7 5 9 11 2 | 19 26 21 20 23 20 24 22 21 22 21
26 | 7 8 8 8 9 3 7 6 8 9 2 | 23 23 23 25 25 22 22 22 21 23 22
27 | 8 8 6 9 13 3 8 6 8 8 3 | 22 25 23 22 26 20 22 21 24 22 22
28 | 9 9 7 14 15 5 9 9 7 17 3 | 17 24 19 23 20 19 24 21 21 23 19
29 | 8 22 8 15 12 5 12 11 10 14 4 | 24 23 20 26 23 22 22 23 23 21 21
30E | 10 10 11 8 16 5 9 7 8 11 3 | 19 24 25 24 25 21 23 22 22 19 21
31E | 10 9 5 11 17 2 7 7 8 10 3 | 27 30 29 30 26 28 27 29 29 28 27
32 | 6 7 12 6 8 2 6 8 8 17 3 | 26 31 26 27 27 26 31 24 30 35 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 9 11 14 4 9 10 9 14 |T 27 30 27 29 28 27 29 28 28 29 27
WRMS | 9 12 9 10 12 4 9 9 8 13 |NE 21 23 20 23 21 21 23 22 23 22 21
MEDI | 8 10 9 10 13 4 9 9 9 13 |MD 23 26 24 26 25 22 25 24 24 24 23
Table 3.2005.3 GPS week: 2005 Day: 3 MJD: 58282.000
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 14 9 9 16 3 7 7 6 14 3 | 24 27 25 25 27 23 27 23 23 27 24
2E | 13 11 7 9 15 6 8 15 9 17 4 | 50 48 52 54 52 50 49 45 50 48 49
3 | 10 9 11 11 8 3 9 7 6 12 3 | 18 28 18 19 20 19 30 20 23 23 21
X4 | 2 --- --- --- --- 24 --- --- --- --- 0 | 27 --- --- --- --- 32 --- --- --- --- 28
5M | 7 7 11 9 10 3 10 9 8 14 3 | 33 36 37 27 34 32 39 28 28 31 32
6M | 10 10 10 7 15 3 8 6 8 10 3 | 27 33 31 30 28 28 33 28 30 30 29
7E | 8 13 6 14 15 4 10 10 10 11 3 | 22 23 23 28 23 23 22 30 27 24 23
8 | 8 8 6 12 12 3 6 8 8 6 3 | 23 27 22 25 28 21 26 20 24 23 23
9M | 7 9 9 11 10 5 8 6 7 8 3 | 18 25 21 18 23 18 26 23 23 26 21
10 | 9 8 11 7 6 3 6 9 7 12 3 | 19 24 15 19 18 18 24 19 19 22 18
11E | 7 10 7 8 16 5 8 11 6 11 3 | 66 70 68 69 70 69 68 68 66 68 68
12 | 7 20 7 10 15 4 7 13 13 15 4 | 22 23 18 21 22 20 23 23 22 17 20
13M | 12 9 11 13 10 4 10 12 10 19 4 | 19 30 19 35 22 25 28 28 30 35 25
14 | 10 11 9 13 9 4 8 13 11 21 4 | 16 20 18 19 17 18 19 22 24 25 18
15M | 13 14 12 15 10 6 11 24 11 18 5 | 34 42 39 31 40 33 40 36 32 38 35
16 | 9 23 7 16 17 6 8 14 10 16 4 | 18 21 17 22 20 19 19 21 19 19 17
17 | 8 11 7 14 13 4 7 8 9 11 3 | 23 24 20 26 25 22 24 25 28 20 23
18 | 13 14 10 13 14 4 9 8 9 17 4 | 54 57 48 47 52 48 53 47 46 51 49
19 | 8 14 6 12 13 4 8 8 10 12 3 | 20 23 20 21 22 19 22 21 24 18 20
20 | 10 11 12 12 8 4 8 11 11 14 3 | 17 18 14 23 16 17 17 22 24 20 17
21 | 8 19 11 14 13 4 7 11 9 15 4 | 47 50 49 48 49 46 49 49 46 44 47
22 | 11 8 10 12 7 4 7 15 11 16 4 | 18 21 15 25 19 19 23 21 26 25 20
23 | 8 18 9 13 13 6 4 9 9 15 3 | 17 17 16 22 16 16 17 18 18 25 17
24E | 7 13 10 9 18 4 9 8 11 18 4 | 74 76 81 75 73 76 78 78 76 81 76
25 | 5 10 6 7 11 3 8 7 10 11 3 | 20 22 21 19 21 19 23 20 21 21 20
26 | 9 8 8 9 10 4 7 7 5 9 3 | 21 23 20 21 24 20 24 19 22 21 21
27 | 7 8 7 8 16 2 7 9 7 8 3 | 22 23 23 21 28 20 24 19 22 20 22
28 | 10 11 6 15 12 4 8 10 11 16 3 | 18 20 17 23 19 17 20 21 21 19 18
29 | 10 24 7 14 16 5 10 12 11 15 4 | 17 19 15 19 19 15 16 21 19 18 15
30E | 12 15 11 9 14 3 8 9 9 10 3 | 19 24 25 20 21 19 23 24 22 18 21
31E | 12 13 4 13 14 4 9 9 9 14 3 | 28 34 28 30 29 27 29 28 31 29 28
32 | 7 9 11 6 8 3 7 7 9 15 3 | 14 23 19 15 17 15 23 14 19 23 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 11 13 4 8 11 9 14 |T 27 30 27 28 28 26 30 28 29 29 27
WRMS | 9 13 9 11 12 4 8 10 8 13 |NE 19 22 18 21 20 19 22 20 22 21 19
MEDI | 9 11 9 12 13 4 8 9 9 14 |MD 21 24 21 23 23 20 24 23 24 24 21
Table 3.2005.4 GPS week: 2005 Day: 4 MJD: 58283.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 16 8 7 17 4 6 6 8 13 3 | 26 29 28 28 28 27 28 26 26 27 26
2E | 15 11 6 10 21 6 8 10 11 15 4 | 38 37 35 35 39 34 35 34 36 36 35
3 | 10 7 10 10 8 4 8 7 6 12 3 | 20 31 23 25 23 24 32 23 24 25 25
X4 | 2 --- --- --- --- 23 --- --- --- --- 0 | 27 --- --- --- --- 23 --- --- --- --- 27
5 | 16 9 11 11 10 5 9 11 11 16 4 | 28 32 31 24 31 26 36 27 30 31 29
6 | 9 10 9 6 13 3 7 4 7 8 3 | 29 35 35 32 32 32 35 32 30 34 32
7E | 10 14 6 11 14 5 11 10 9 13 3 | 25 27 29 31 28 28 27 33 31 27 28
8 | 9 7 6 9 15 2 7 7 7 9 3 | 23 26 24 25 26 22 25 22 23 23 23
9 | 9 7 9 10 9 5 8 3 7 9 2 | 20 27 22 20 21 20 29 21 23 25 23
10 | 11 7 12 8 6 3 6 9 7 9 3 | 18 25 16 18 16 15 24 18 18 21 18
11E | 9 8 6 7 14 3 6 8 7 12 3 | 55 55 51 53 51 52 53 51 51 52 52
12 | 9 18 8 11 14 3 8 13 11 14 4 | 23 24 19 22 23 21 23 26 26 20 21
13 | 12 9 12 11 9 4 9 11 10 18 4 | 32 36 32 38 31 34 36 34 35 38 34
14 | 16 10 9 13 11 3 8 11 12 20 4 | 19 20 15 17 15 17 17 19 21 23 15
15 | 12 12 13 13 9 6 11 24 12 19 5 | 42 46 44 34 42 36 45 41 40 40 41
16 | 12 24 7 15 14 6 8 12 12 17 4 | 22 18 18 24 18 19 17 21 23 21 18
17 | 13 11 6 14 14 4 7 8 9 11 3 | 21 25 20 27 25 22 24 24 26 18 22
18E | 15 10 12 11 15 4 9 10 10 15 4 | 65 63 56 59 63 58 63 58 56 60 59
19 | 12 17 6 13 12 4 7 8 8 15 3 | 20 22 18 23 21 19 23 22 22 19 20
20 | 19 9 12 12 10 4 9 12 11 14 4 | 25 27 21 27 24 23 24 26 25 29 24
21E | 16 16 8 14 18 6 8 13 10 12 4 | 51 46 47 45 47 46 45 44 48 45 45
22 | 11 7 10 10 9 5 7 15 11 18 4 | 15 21 14 22 14 18 21 22 19 24 17
23 | 7 19 9 12 11 6 7 10 9 15 4 | 17 18 16 21 16 17 17 19 20 23 17
24E | 10 12 9 7 27 5 6 8 7 19 4 | 72 77 78 73 75 72 75 75 76 70 74
25 | 9 8 6 8 12 3 9 9 9 10 3 | 22 29 25 23 25 22 27 26 24 24 24
26 | 11 8 6 8 10 3 7 6 7 8 2 | 22 22 19 19 22 18 21 18 21 20 19
27 | 10 8 7 7 14 2 8 9 9 9 3 | 24 23 23 21 25 20 22 20 20 19 21
28 | 13 10 6 12 16 4 8 9 10 13 3 | 18 22 18 22 20 17 22 19 20 19 18
29 | 13 21 7 14 16 5 12 13 12 17 5 | 21 23 19 24 25 20 22 25 26 23 21
30E | 15 14 11 6 15 4 13 8 10 12 4 | 17 23 23 20 21 18 24 19 20 15 19
31E | 17 10 5 12 13 5 9 9 10 12 3 | 24 29 28 30 27 27 27 28 26 25 26
32 | 10 8 10 7 8 3 5 7 7 12 3 | 27 34 28 27 28 26 33 26 30 34 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 9 11 14 4 8 10 9 14 |T 28 31 28 29 29 27 30 29 29 29 28
WRMS | 12 12 9 10 12 4 8 9 8 14 |NE 21 24 19 22 21 20 23 22 22 22 21
MEDI | 11 10 8 11 13 4 8 9 9 13 |MD 23 27 23 25 25 22 27 26 26 25 24
Table 3.2005.5 GPS week: 2005 Day: 5 MJD: 58284.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 9 8 8 13 4 6 7 7 9 3 | 21 23 22 22 26 20 24 23 20 21 21
2E | 8 11 6 12 21 4 9 13 10 16 4 | 32 30 30 32 38 30 31 31 31 28 30
3 | 9 8 11 10 5 4 8 7 6 10 3 | 23 30 22 22 21 22 30 24 26 24 24
X4 | 2 --- --- --- --- 35 --- --- --- --- 0 | 38 --- --- --- --- 25 --- --- --- --- 38
5 | 6 8 10 11 7 4 11 9 13 14 3 | 26 26 25 22 27 23 29 23 27 27 25
6 | 5 8 9 8 10 2 7 5 6 8 2 | 59 63 62 58 58 59 62 61 61 59 60
7E | 12 13 9 12 17 5 9 14 10 14 4 | 21 25 27 28 27 26 25 31 29 24 24
8 | 8 7 7 11 13 3 7 8 6 9 3 | 19 21 20 21 22 18 21 18 19 18 19
9 | 6 9 9 9 6 6 10 6 8 8 3 | 24 28 24 20 22 22 30 21 25 25 24
10 | 8 7 11 12 5 4 8 8 6 10 3 | 23 27 23 23 22 22 28 22 24 27 23
11E | 6 9 7 10 9 4 6 6 5 14 2 | 60 62 61 60 61 61 62 59 60 62 60
12 | 11 18 8 13 10 5 7 13 15 14 4 | 26 25 21 29 26 24 25 30 28 22 24
13 | 9 9 11 11 7 3 10 11 13 16 4 | 23 30 19 30 21 25 28 27 28 32 25
14 | 9 10 10 13 9 3 6 12 13 21 4 | 17 18 18 20 18 18 20 21 24 24 18
15 | 12 11 11 13 6 6 9 24 15 17 4 | 42 43 41 39 39 39 42 42 40 39 39
16 | 10 25 6 16 14 6 7 13 12 16 4 | 21 17 18 27 17 21 16 24 22 22 18
17 | 7 11 6 13 12 5 7 8 9 10 3 | 26 30 23 29 28 25 29 28 29 23 26
18E | 16 10 11 14 12 4 11 12 11 15 4 | 77 77 70 67 76 70 76 68 68 73 72
19 | 8 13 6 11 8 4 8 9 10 10 3 | 28 29 28 30 27 27 30 28 30 28 28
20 | 10 9 11 15 7 5 8 12 12 14 3 | 35 32 33 33 34 32 35 35 36 35 33
21E | 10 12 9 17 16 4 7 13 10 14 4 | 52 53 52 55 54 52 50 51 50 50 51
22 | 8 8 10 10 7 6 6 15 11 16 3 | 19 22 18 21 19 21 22 22 24 26 20
23 | 8 17 8 14 11 8 5 11 9 16 3 | 18 17 16 22 15 18 18 18 20 22 17
24E | 12 11 8 7 12 4 8 12 8 13 3 | 68 69 71 67 69 68 70 70 66 68 68
25 | 9 9 6 9 6 5 8 7 9 20 3 | 20 29 22 21 25 22 28 22 28 35 24
26 | 9 8 7 9 7 4 6 7 7 10 2 | 28 25 27 26 27 24 27 26 25 25 25
27 | 9 8 8 13 12 3 7 8 8 9 3 | 19 21 21 20 21 17 20 17 18 21 19
28 | 12 11 6 14 12 5 8 9 9 12 3 | 16 23 20 23 21 19 24 21 22 20 20
29 | 11 20 7 14 12 5 8 13 16 14 4 | 27 27 24 29 28 26 26 30 28 27 26
30E | 14 16 12 7 15 5 7 7 9 11 4 | 20 22 25 20 23 20 24 22 23 18 20
31E | 14 9 7 12 13 4 7 11 10 12 3 | 27 29 28 30 29 27 29 30 27 26 27
32 | 7 7 10 10 6 2 5 6 7 15 3 | 33 36 31 36 33 33 36 32 34 39 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 9 12 11 4 8 11 10 14 |T 30 32 30 31 31 29 32 31 32 31 30
WRMS | 9 12 8 11 10 4 8 10 8 14 |NE 24 25 22 25 23 23 25 24 25 25 24
MEDI | 9 9 8 12 10 4 7 9 9 14 |MD 26 28 24 28 27 24 28 27 28 26 25
Table 3.2005.6 GPS week: 2005 Day: 6 MJD: 58285.000
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 7 8 8 12 3 8 9 7 11 3 | 26 30 28 28 25 25 27 26 25 25 26
2E | 11 9 6 11 23 6 8 13 11 15 4 | 38 37 37 39 42 36 37 41 37 34 37
3 | 10 8 10 10 7 3 8 7 9 8 3 | 28 33 30 32 29 30 34 31 34 32 31
X4 | 2 --- --- --- --- 29 --- --- --- --- 0 | 33 --- --- --- --- 31 --- --- --- --- 33
5 | 9 9 11 11 8 5 10 13 12 18 4 | 43 46 46 34 44 37 48 33 36 37 40
6E | 12 7 11 8 17 4 7 9 8 7 3 | 56 62 60 58 56 59 63 63 59 60 59
7E | 8 15 8 11 17 4 10 11 10 12 4 | 34 35 37 41 34 36 33 41 41 39 36
8 | 8 8 6 10 10 2 8 7 6 10 3 | 23 24 22 23 24 21 24 21 21 21 22
9 | 9 8 8 9 8 4 9 6 7 7 2 | 35 39 38 35 36 34 39 34 33 36 35
10 | 6 7 12 9 6 2 7 8 6 8 3 | 18 24 19 21 18 18 24 21 20 21 19
11E | 9 6 9 7 7 3 6 6 6 15 3 | 77 76 74 75 75 75 76 73 76 77 75
12 | 10 18 8 12 12 4 9 14 13 17 4 | 34 33 31 39 33 34 33 37 37 37 33
13 | 13 10 11 13 7 5 9 11 13 19 4 | 33 38 30 41 33 36 36 36 37 44 35
14 | 9 9 11 12 9 4 7 12 12 18 4 | 18 20 16 26 18 21 18 26 27 26 20
15 | 12 12 12 14 6 6 10 25 13 17 5 | 53 58 56 46 51 48 54 48 44 48 50
16 | 8 23 7 13 14 6 8 13 11 18 4 | 27 28 27 37 27 31 29 34 32 31 28
17 | 9 9 7 13 13 6 9 10 9 12 3 | 23 28 22 27 26 23 26 26 25 23 24
18E | 19 11 14 13 12 5 12 16 15 17 5 | 120 120 113 115 121 115 119 113 115 109 116
19 | 11 15 6 11 12 5 8 11 11 14 3 | 25 29 23 26 25 24 27 25 26 24 24
20 | 7 12 11 14 8 4 9 12 11 16 4 | 33 32 32 36 35 31 36 37 35 35 33
21E | 10 7 10 15 18 5 7 12 9 13 4 | 62 64 61 67 64 64 64 65 65 62 63
22 | 9 8 11 10 8 5 9 14 14 15 4 | 17 22 15 25 18 22 22 25 27 25 20
23 | 10 17 9 12 12 6 6 13 9 16 4 | 23 21 21 27 22 21 21 22 23 30 21
24 | 16 12 9 10 12 4 7 10 6 12 3 | 80 83 87 84 84 82 85 84 83 83 83
25 | 8 10 8 10 7 4 8 7 10 13 3 | 26 31 29 27 27 26 29 28 26 30 27
26 | 8 8 8 8 8 4 5 6 6 7 2 | 30 32 30 31 33 28 32 29 29 30 30
27 | 10 10 7 8 10 3 8 6 9 8 3 | 20 22 18 19 22 17 19 17 18 19 18
28 | 10 14 7 10 12 5 9 12 10 10 3 | 21 26 22 24 24 20 25 22 20 21 21
29 | 9 17 7 11 12 3 9 12 12 15 4 | 32 32 30 35 27 31 31 31 32 29 30
30E | 9 14 10 6 12 4 7 7 6 10 3 | 23 26 28 24 23 22 26 23 24 20 23
31E | 15 11 7 14 15 5 8 12 10 10 4 | 42 41 41 43 42 39 41 38 39 40 40
32 | 7 6 12 6 5 3 7 8 10 11 3 | 38 40 39 39 39 38 42 38 40 41 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 9 11 12 4 8 11 10 13 |T 37 39 37 39 37 36 39 38 38 38 37
WRMS | 9 12 9 10 11 4 8 11 8 13 |NE 26 28 25 29 26 25 27 27 27 27 26
MEDI | 9 10 9 11 12 4 8 11 10 13 |MD 32 32 30 35 33 31 33 33 33 32 31
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 4.2005 GPS week: 2005 MJD: 58279.0-58285.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 |U 8 10 21 |U 8 12 25 |U 11 10 31 |
emr | emr 2975 |U 15 22 31 |U 11 15 36 | 13 11 42 |
esa | esa 2976 | 10 12 22 |U 8 13 28 | 11 11 36 |
gfz | gfz 2974 |U 7 10 20 |U 10 13 31 |U 12 11 31 |
grg | grg 2975 |U 11 15 22 |U 10 15 32 | 13 16 45 |
igr | igr 2975 | 8 9 19 | 8 12 26 | 11 10 36 |
igs | igs 2975 | 8 9 20 | 8 12 27 | 11 10 33 |
jpl | jpl 2976 |U 12 15 29 |U 9 14 31 |U 11 13 42 |
mit | mit 2976 | 9 11 20 |U 10 12 31 |U 14 13 37 |
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 5.2005.0 GPS week: 2005 Day: 0 MJD: 58279.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 10 24 | 7 12 22 | 11 10 34 |
emr | emr 2976 | 13 15 39 | 8 12 35 | 10 14 41 |
esa | esa 2976 | 9 9 23 | 6 13 24 | 11 12 39 |
gfz | gfz 2976 | 8 9 21 | 7 12 23 | 12 10 33 |
grg | grg 2975 | 10 16 24 | 8 15 26 | 12 10 36 |
igr | igr 2976 | 8 8 21 | 7 12 22 | 11 10 34 |
igs | igs 2976 | 8 7 22 | 6 12 22 | 10 10 34 |
jpl | jpl 2976 | 11 12 32 | 7 12 29 | 11 13 42 |
mit | mit 2976 | 9 9 24 | 8 11 31 | 11 10 37 |
Table 5.2005.1 GPS week: 2005 Day: 1 MJD: 58280.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 7 33 | 7 12 24 | 11 9 33 |
emr | emr 2976 | 17 18 48 | 9 17 36 | 13 8 44 |
esa | esa 2976 | 11 11 35 | 7 14 24 | 11 9 40 |
gfz | gfz 2976 | 9 8 31 | 7 13 26 | 12 9 33 |
grg | grg 2976 | 11 13 26 | 8 15 30 | 12 10 40 |
igr | igr 2976 | 9 6 30 | 7 12 25 | 11 7 34 |
igs | igs 2976 | 9 7 31 | 7 12 25 | 10 8 36 |
jpl | jpl 2976 | 13 16 42 | 8 13 24 | 11 13 45 |
mit | mit 2976 | 10 8 26 | 8 14 29 | 11 9 34 |
Table 5.2005.2 GPS week: 2005 Day: 2 MJD: 58281.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 11 20 | 8 12 24 | 9 10 31 |
emr | emr 2976 | 14 23 30 | 9 14 33 | 12 12 43 |
esa | esa 2976 | 12 11 24 | 8 13 28 | 9 11 39 |
gfz | gfz 2974 | 9 11 19 | 8 11 27 | 10 6 34 |
grg | grg 2976 | 11 16 18 | 9 14 26 | 11 10 40 |
igr | igr 2976 | 9 11 19 | 8 12 23 | 9 7 33 |
igs | igs 2976 | 9 10 19 | 8 12 24 | 9 9 35 |
jpl | jpl 2976 | 13 16 29 | 9 17 30 | 10 15 43 |
mit | mit 2976 | 9 12 18 | 9 11 24 | 28 30 59 |
Table 5.2005.3 GPS week: 2005 Day: 3 MJD: 58282.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 9 20 | 11 12 27 | 10 7 25 |
emr | emr 2976 | 14 24 26 | 17 17 37 | 13 13 39 |
esa | esa 2976 | 9 12 21 | 10 14 30 | 10 9 28 |
gfz | gfz 2975 | 7 9 16 | 9 11 29 | 12 10 23 |
grg | grg 2976 | 10 15 20 | 11 15 31 | 14 20 56 |
igr | igr 2974 | 7 9 17 | 10 11 26 | 14 12 59 |
igs | igs 2976 | 7 10 17 | 11 12 27 | 9 8 25 |
jpl | jpl 2976 | 12 16 25 | 11 15 31 | 10 14 34 |
mit | mit 2976 | 8 12 18 | 11 11 30 | 11 8 25 |
Table 5.2005.4 GPS week: 2005 Day: 4 MJD: 58283.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 12 18 | 8 13 26 | 10 8 29 |
emr | emr 2976 | 15 23 26 | 14 17 37 | 16 6 43 |
esa | esa 2976 | 9 16 19 | 8 14 29 | 10 7 34 |
gfz | gfz 2976 | 7 14 18 | 8 13 29 | 11 8 28 |
grg | grg 2976 | 11 14 21 | 10 18 33 | 13 25 66 |
igr | igr 2976 | 7 13 18 | 8 14 26 | 11 7 29 |
igs | igs 2975 | 7 14 18 | 9 14 27 | 11 7 31 |
jpl | jpl 2976 | 12 18 26 | 10 18 29 | 12 12 44 |
mit | mit 2976 | 9 15 18 | 10 16 32 | 12 10 33 |
Table 5.2005.5 GPS week: 2005 Day: 5 MJD: 58284.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 11 17 | 7 10 26 | 11 11 35 |
emr | emr 2974 | 16 23 27 | 11 15 40 | 14 10 40 |
esa | esa 2976 | 9 11 18 | 7 10 26 | 11 11 37 |
gfz | gfz 2972 | 7 10 17 | 7 8 30 | 11 13 35 |
grg | grg 2976 | 9 14 20 | 9 12 34 | 16 16 43 |
igr | igr 2976 | 7 10 16 | 7 9 26 | 11 12 35 |
igs | igs 2976 | 7 9 16 | 7 9 28 | 12 11 37 |
jpl | jpl 2976 | 12 12 25 | 9 12 32 | 12 11 42 |
mit | mit 2976 | 7 12 20 | 8 8 33 | 12 11 36 |
Table 5.2005.6 GPS week: 2005 Day: 6 MJD: 58285.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 9 18 | 10 14 29 | 13 14 31 |
emr | emr 2972 | 17 28 24 | 12 14 37 | 14 15 45 |
esa | esa 2976 | 11 11 17 | 10 13 35 | 13 15 35 |
gfz | gfz 2972 | 7 10 18 | 21 25 53 | 13 17 32 |
grg | grg 2976 | 12 14 28 | 13 18 44 | 16 19 38 |
igr | igr 2976 | 8 10 17 | 10 12 31 | 12 15 31 |
igs | igs 2976 | 9 9 18 | 10 12 32 | 13 14 33 |
jpl | jpl 2976 | 13 14 25 | 10 14 39 | 12 15 44 |
mit | mit 2976 | 9 12 18 | 13 13 41 | 14 15 34 |
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 6.2005 GPS week: 2005 MJD: 58279.500-58285.500
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 -12 41 -4 -3 | 11 25
| 20 11 90 56 6 | 0
emr uuuuu | 32 6 107 165 -4 | 35 42
| 15 22 78 37 9 | 1
esa uuuuu | 1 5 -58 81 -4 | 11 26
| 14 12 55 54 7 | 1
gfz uuuuu | -3 8 -27 -11 2 | 15 28
| 21 19 146 72 3 | 1
grg uuuuu | -8 -9 18 -249 0 | 7 22
| 24 17 16 40 2 | 1
igr xxxxx | -2 9 51 -26 5 | -3 23
| 12 8 36 42 7 | 3
irf xxxxx | -6 -15 -21 -42 -1 | 0 22
| 4 5 18 15 2 | 1
jpl uuuuu | 3 -12 66 30 3 | 15 25
| 6 7 47 18 8 | 2
mit uuuuu | -15 3 -24 -78 0 | 18 28
| 25 15 31 25 5 | 2
ngs uuuuu | -5 0 26 3 3 | 14 26
| 19 23 150 65 5 | 1
sio uuuux | -4 26 -207 29 -3 | 69 72
| 7 16 47 67 5 | 1
Table 7.2005.0 GPS week: 2005 Day: 0 MJD: 58279.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -4 -5 38 -6 2 | 11 25
emr uuuuu | 32 9 104 155 5 | 35 41
esa uuuuu | 20 12 -79 22 6 | 10 26
gfz uuuuu | -32 -1 118 -109 -1 | 16 30
grg uuuuu | 9 -14 27 -258 4 | 7 22
igr xxxxx | 2 25 73 -18 7 | -7 24
irf xxxxx | -8 -13 -23 -43 -6 | 1 23
jpl uuuuu | 2 -14 120 48 -2 | 17 27
mit uuuuu | -10 4 -59 -81 -9 | 21 31
ngs uuuuu | -18 0 -147 63 -7 | 16 28
sio uuuux | 10 9 -111 117 -1 | 69 72
Table 7.2005.1 GPS week: 2005 Day: 1 MJD: 58280.500
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 | 26 -7 -1 -11 3 | 11 25
emr uuuuu | 50 -1 152 183 -2 | 36 42
esa uuuuu | -14 -4 43 30 4 | 10 26
gfz uuuuu | -7 -4 -48 -61 -2 | 15 28
grg uuuuu | 9 -35 15 -257 -1 | 7 22
igr xxxxx | -13 7 74 -6 13 | -7 24
irf xxxxx | -7 -18 -38 -37 -3 | 0 22
jpl uuuuu | -7 0 101 41 -5 | 17 27
mit uuuuu | -8 21 -63 -87 -5 | 19 29
ngs uuuuu | -25 -9 -81 44 4 | 14 25
sio uuuux | -8 53 -187 92 3 | 69 72
Table 7.2005.2 GPS week: 2005 Day: 2 MJD: 58281.500
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 4 -57 -97 2 | 12 25
emr uuuuu | 34 1 184 178 -5 | 37 43
esa uuuuu | 14 14 -98 100 -1 | 11 26
gfz uuuuu | -25 8 -168 -42 4 | 15 28
grg uuuuu | -8 -16 26 -173 -1 | 7 22
igr xxxxx | -13 8 54 28 11 | -5 24
irf xxxxx | -10 -22 -32 -41 -1 | 0 22
jpl uuuuu | 1 -15 98 33 -8 | 17 27
mit uuuuu | -22 17 -33 -93 0 | 18 28
ngs uuuuu | 19 -35 198 43 6 | 14 26
sio uuuux | -9 38 -243 41 -6 | 71 74
Table 7.2005.3 GPS week: 2005 Day: 3 MJD: 58282.500
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 | -24 -16 53 -21 -10 | 11 25
emr uuuuu | 5 -30 165 127 -17 | 35 41
esa uuuuu | 13 15 -110 145 -5 | 10 26
gfz uuuuu | 28 44 -204 80 -1 | 13 27
grg uuuuu | 19 -4 -2 -245 1 | 5 22
igr xxxxx | 19 10 43 5 8 | -4 24
irf xxxxx | 0 -12 -44 -46 0 | -2 22
jpl uuuuu | 8 -13 -14 23 10 | 12 21
mit uuuuu | -60 7 -5 -81 2 | 16 26
ngs uuuuu | 23 -18 250 -34 7 | 12 24
sio uuuux | -8 33 -220 -54 -12 | 69 72
Table 7.2005.4 GPS week: 2005 Day: 4 MJD: 58283.500
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 | 19 -21 220 5 -12 | 11 25
emr uuuuu | 25 2 42 129 -3 | 34 41
esa uuuuu | -4 -2 -61 151 -10 | 11 26
gfz uuuuu | 6 10 -126 -53 5 | 14 28
grg uuuuu | -5 19 9 -234 0 | 7 22
igr xxxxx | 9 10 -5 -99 7 | -2 23
irf xxxxx | -9 -10 -3 -68 0 | 0 21
jpl uuuuu | 7 -13 36 -6 5 | 13 22
mit uuuuu | -27 -22 23 -109 2 | 17 27
ngs uuuuu | -7 22 65 43 9 | 13 25
sio uuuux | -6 14 -251 -30 0 | 69 72
Table 7.2005.5 GPS week: 2005 Day: 5 MJD: 58284.500
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 | 25 -28 61 92 -4 | 11 25
emr uuuuu | 25 43 -35 148 -10 | 35 41
esa uuuuu | -10 -14 -10 38 -12 | 12 26
gfz uuuuu | -2 14 96 52 0 | 16 29
grg uuuuu | -28 -15 6 -276 1 | 8 22
igr xxxxx | -13 2 19 -51 -6 | 0 23
irf xxxxx | -6 -19 -2 -41 0 | 1 22
jpl uuuuu | 2 -22 76 42 13 | 15 24
mit uuuuu | 11 3 -2 -68 4 | 18 27
ngs uuuuu | -21 28 -58 -16 0 | 15 26
sio uuuux | -3 19 -215 -31 -6 | 69 72
Table 7.2005.6 GPS week: 2005 Day: 6 MJD: 58285.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -8 -15 -27 8 -4 | 11 25
emr uuuuu | 49 14 140 234 8 | 34 41
esa uuuuu | -13 14 -87 80 -11 | 11 27
gfz uuuuu | 11 -16 147 56 5 | 16 29
grg uuuuu | -52 0 47 -303 -2 | 8 23
igr xxxxx | -3 -1 101 -41 -4 | 0 23
irf xxxxx | -2 -9 -4 -15 0 | 1 22
jpl uuuuu | 9 -8 44 28 6 | 15 24
mit uuuuu | 13 -13 -26 -28 2 | 18 27
ngs uuuuu | -4 11 -43 -121 1 | 15 26
sio uuuux | -7 12 -219 67 1 | 68 71
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