[IGSREPORT-25963] Wk 2003 IGS Final Orbits
acc
acc at igs.org
Thu Jun 14 17:50:12 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2003 (May 27, 2018 - Jun 02, 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:
igs2003[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2003[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2003[0-6].cls IGS GPS clock combination summary report.
igs20037.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20037.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 | MAL2 SOFI TIXI MAL2 SOFI TIXI
0 | ESA | FAA1
0 | GFZ | 8 18 8 16 18 GODE REUN YAKT GODE NRMD REUN YAKT
0 | GRG | 21 21 GLSV KIT3 MAL2 NRMD RIO2 TLSE GLSV KIT3 MAL2
0 | GRG | RIO2 TLSE TONG
1 | COD | 18 21 18 21 MAL2 TIXI MAL2 NRC1 TIXI
1 | EMR | 18
1 | ESA | ABMF DAV1 KOUR SFER ABMF DAV1 KOUR
1 | GFZ | 18 21 18 21 BJNM DAEJ FAA1 GODE KOUR MAL2 NICO REUN
1 | GFZ | SFER YAKT BJNM DAEJ FAA1 GODE MAL2 NICO REUN YAKT
1 | GRG | 13 13 GLSV KIT3 GLSV KIT3 TONG
1 | MIT | 18 18 SFER
2 | COD | MAL2 TIXI MAL2 NAIN TIXI
2 | ESA | HERS HERS YELL
2 | GFZ | 18 18 BJNM GODE MAL2 NAIN REUN SFER YELL BJNM GODE
2 | GFZ | MAL2 REUN SFER YELL
2 | GRG | ARTU GLSV KIT3 KRGG SEYG ARTU GLSV KIT3 KRGG SEYG
2 | GRG | TONG
3 | COD | 24 24 TIXI BRMU GLSV LHAZ TIXI
3 | EMR | 24 24 KIRU
3 | ESA | LHAZ MAL2 YAKT HARB MAL2 YAKT
3 | GFZ | 18 18 BJNM GODE HARB KERG MAL2 REUN GODE KERG LHAZ
3 | GFZ | MAL2 REUN
3 | GRG | DAV1 GLSV LHAZ MCIL SEYG WIND DAV1 GLSV MCIL SEYG
3 | GRG | TLSE TONG WIND
3 | JPL | SAVO SAVO
4 | COD | TIXI TIXI TLSE
4 | GFZ | 18 18 GODE MAL2 MCIL REUN GODE MAL2 MCIL REUN
4 | GRG | ADIS GLSV MAL2 SEYG GLSV SEYG TLSE TONG
4 | MIT | NYAL
5 | COD | SEYG
5 | EMR | CHUR CHUR
5 | ESA | 18 18 FLIN MAL2 MAW1 FLIN MAL2 MAW1
5 | GFZ | 18 18 GODE KOUR MAL2 GODE KOUR MAL2
5 | GRG | 5 5 GLSV RIO2 TLSE GLSV TLSE TONG
5 | JPL | SAVO SAVO
6 | COD | KOUR KOUR MAL2 TLSE
6 | EMR | 18 ALBH
6 | ESA | MAL2 WIND WIND
6 | GFZ | 18 21 24 18 21 24 GODE KOUR MAL2 GODE HARB MAL2
6 | GRG | GLSV KIT3 RIO2 GLSV KIT3 RIO2 TONG
6 | MIT | 18 18 BOR1 YELL BOR1 YELL
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 | .2 .5 .2 19 9 -14 -.23
EMR | 0 | 4.2 1.4 -.8 7 -22 29 -.10
ESA | 0 | .3 -.0 .5 9 8 7 -.13
GFZ | 0 | -.1 .4 -.0 4 -12 -2 -.14
GRG | 0 | 10.9 -2.2 -.5 64 36 22 -.10
JPL | 0 | 3.4 -1.8 2.4 0 0 1 -.25
MIT | 0 | 5.4 -1.2 1.3 -26 36 22 .09
NGS | 0 | 3.6 .3 -8.8 60 44 -1 .16
SIO | 0 | 6.2 -3.7 -14.4 -2 -13 3 -.07
COD | 1 | -.1 .2 .3 8 11 -16 -.32
EMR | 1 | 2.9 3.7 -2.0 10 2 38 -.09
ESA | 1 | .2 .5 -.1 14 15 10 -.18
GFZ | 1 | .4 -.1 -.4 -16 -25 6 -.07
GRG | 1 | 8.0 -1.3 6.4 30 26 2 -.28
JPL | 1 | 4.9 -9.3 3.3 8 1 -7 -.36
MIT | 1 | 3.0 -.7 4.9 -24 42 25 .10
NGS | 1 | -3.0 -.9 -7.2 53 27 -18 .05
SIO | 1 | 3.1 -6.1 -11.3 8 21 -8 .08
COD | 2 | -.2 .3 .5 16 16 -10 -.41
EMR | 2 | 4.6 -.3 4.5 20 14 36 .07
ESA | 2 | .3 -.2 .2 6 20 6 -.34
GFZ | 2 | .4 .3 .3 6 -10 0 -.20
GRG | 2 | 5.8 -4.0 8.3 55 30 47 -.20
JPL | 2 | 8.3 -6.1 5.9 2 13 -7 -.41
MIT | 2 | 3.7 -2.6 7.2 -19 39 7 -.17
NGS | 2 | 1.6 1.5 -1.1 39 5 -26 -.16
SIO | 2 | 4.5 -.8 -11.6 4 9 -5 .01
COD | 3 | -.5 .2 1.0 14 28 -23 -.32
EMR | 3 | -5.6 -.5 5.7 11 -9 56 .02
ESA | 3 | .4 -.4 .1 9 10 -6 -.39
GFZ | 3 | .0 .2 .4 -1 -17 -1 -.20
GRG | 3 | 6.5 -4.4 3.9 73 23 25 -.27
JPL | 3 | 2.5 -3.2 5.6 2 13 -13 -.52
MIT | 3 | 4.3 -1.4 7.5 -22 58 15 -.11
NGS | 3 | 1.9 -4.7 5.9 -7 -50 -47 -.23
SIO | 3 | 5.0 -6.2 -11.9 2 10 3 -.08
COD | 4 | -.2 .2 .2 13 5 0 -.31
EMR | 4 | -.5 2.4 -2.0 9 -15 29 .02
ESA | 4 | .4 .4 -.1 13 -17 12 -.31
GFZ | 4 | .0 -.1 .7 -7 0 12 -.18
GRG | 4 | 7.0 -5.7 5.8 64 20 39 -.21
JPL | 4 | 6.6 -6.0 .2 3 13 -10 -.28
MIT | 4 | 2.4 -6.2 3.4 -15 24 10 .01
NGS | 4 | .5 -6.0 -4.9 32 12 -61 -.08
SIO | 4 | 3.5 -5.2 -12.6 5 6 -15 -.07
COD | 5 | .1 .2 .8 3 11 -16 -.34
EMR | 5 | .1 -2.6 1.7 13 -21 35 -.04
ESA | 5 | -1.0 -.8 .8 10 10 23 -.22
GFZ | 5 | .3 .0 .3 -11 -18 -5 -.12
GRG | 5 | 3.2 -2.9 .3 78 22 17 -.17
JPL | 5 | 6.8 -10.5 -2.6 5 -2 1 -.28
MIT | 5 | .7 -5.3 3.1 -18 15 10 -.06
NGS | 5 | -.3 -5.7 -.3 22 -8 -65 -.23
SIO | 5 | 2.7 -3.8 -12.5 8 -7 3 -.17
COD | 6 | -.3 .4 .0 4 9 -11 -.25
EMR | 6 | -1.3 -6.2 3.1 -6 -2 31 .31
ESA | 6 | .0 -.4 .0 -4 -1 -2 -.42
GFZ | 6 | .2 .2 .2 0 -12 -3 -.13
GRG | 6 | 4.6 -3.0 9.9 46 41 14 -.38
JPL | 6 | 8.6 -7.9 -2.7 -3 26 8 -.10
MIT | 6 | .7 -5.3 8.4 -48 29 17 .0
NGS | 6 | 1.6 -3.6 -4.4 23 20 -40 -.13
SIO | 6 | 1.5 -4.1 -9.7 -5 20 -1 -.08
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 1.2003.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2003.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 2.2003.[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 3.2003.[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 5.2003.0-6). 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 2003 summary. (May 27, 2018 - Jun 02, 2018)
Table 1.2003.a GPS week: 2003 MJD: 58265.000-58271.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 261| 0 0 3 12 -8 1 -.05 10 9 | -648 28 11 108
| 0 0 2 12 6 7 .02 | 161 208
emr 79| -2 0 0 6 5 33 .17 14 14 | 139356 -209 16 137
| 2 1 1 9 10 9 .03 | 846 740
esa 150| 0 0 -6 -5 2 2 -.07 9 9 | -1242 -128 9 197
| 0 0 1 14 12 7 .02 | 504 797
gfz 183| -1 1 0 20 9 -1 .05 10 9 | -167 -88 10 124
| 0 1 1 11 13 6 .03 | 484 501
grg 106| 1 0 2 -20 5 -23 -.08 12 11 | -59 43 10 148
| 0 0 2 15 12 17 .03 | 203 262
igr n/a| 0 0 0 -11 -4 1 -.02 5 5 | 2595 167 13 80
| 0 0 0 12 9 8 .01 | 554 684
jpl 80| 0 0 1 23 0 23 .21 10 10 | 134599 -127 33 119
| 1 1 1 11 19 15 .04 | 680 624
mit 350| 1 0 3 -10 -9 1 -.01 12 10 | 66 -140 39 268
| 0 0 0 17 32 22 .01 | 233 234
ngs 208| 0 0 -2 6 2 7 .06 9 7 | -634 -11 1096 2377
| 0 0 1 8 10 9 .02 | 157 205
sio 345| 0 0 1 -16 -8 -21 -.05 12 13 | --- --- --- ---
| 0 0 1 15 22 22 .02 | --- ---
Table 1.2003.b GPS week : 2003 MJD: 58265.000-58271.000
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 4 3 4 4 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 3 4 3 4 4 4 3 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 3 3 3 4 3 |
6 | 3 3 3 3 3 3 3 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 4 4 4 3 4 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 3 4 3 4 3 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 4 4 5 5 5 5 |
14 | 4 5 4 5 5 5 4 |
15 | 5 5 5 5 5 5 5 |
16 | 7 8 8 8 8 8 7 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 3 4 4 4 4 |
19 | 4 4 4 5 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 5 4 5 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 6 6 5 5 5 4 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 4 3 3 3 |
27 | 4 4 4 4 4 4 4 |
28 | 5 5 5 4 5 5 4 |
29 | 5 6 6 6 5 5 5 |
30 | 4 4 4 4 4 5 5 |
31 | 4 4 4 4 4 3 4 |
32 | 3 3 3 3 3 3 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
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 2.2003.0 GPS week: 2003 Day: 0 MJD: 58265.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 259| 0 0 6 15 -4 6 -.03 9 9 | -790 315 11 120
emr 80| 0 0 0 -3 21 38 .18 14 14 | 139819 256 15 157
esa 150| 0 0 -4 -13 3 7 -.07 8 8 | -1025 -281 7 215
gfz 183| 0 1 0 38 -6 -6 .01 10 9 | -636 153 10 139
grg 111| 0 -1 -1 -13 19 -31 -.11 12 12 | -253 268 9 155
igr n/a| 0 0 0 -22 -14 12 -.02 4 4 | 1745 628 12 71
jpl 80| -1 0 2 1 -11 52 .22 10 10 | 134826 229 34 134
mit 350| 0 0 3 -4 -36 -38 -.02 13 11 | 7 67 35 266
ngs 207| 0 0 -3 -3 19 8 .07 8 6 | -788 231 1159 2691
sio 346| 0 -1 3 -31 -23 7 -.06 13 14 | --- --- --- ---
Table 2.2003.1 GPS week: 2003 Day: 1 MJD: 58266.000
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 264| 0 0 4 19 -18 3 -.04 10 10 | -588 -78 11 98
emr 80| 0 0 1 1 9 33 .22 13 13 | 139965 441 14 138
esa 150| 0 1 -6 17 20 -8 -.06 9 9 | -1565 1139 11 206
gfz 186| 0 0 1 12 0 1 .04 11 9 | -341 17 10 106
grg 104| 1 0 1 -47 3 -48 -.09 13 12 | -46 14 11 147
igr n/a| 0 0 0 -15 -14 3 -.02 5 4 | 2335 783 14 111
jpl 80| 1 0 2 23 6 8 .26 10 10 | 135215 287 33 111
mit 350| 1 -1 3 -15 4 20 -.02 12 10 | -6 -73 42 311
ngs 209| -1 0 -4 0 -15 -5 .06 9 7 | -597 -61 1037 2360
sio 352| 0 -1 0 -5 9 -16 -.05 13 13 | --- --- --- ---
Table 2.2003.2 GPS week: 2003 Day: 2 MJD: 58267.000
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| 0 0 4 -1 -9 0 -.06 9 9 | -453 -285 10 103
emr 80| 0 0 2 11 2 33 .17 13 13 | 140105 -978 16 144
esa 150| 0 0 -7 -11 12 7 -.04 8 8 | -2192 -610 9 202
gfz 184| -1 3 0 18 19 -3 .10 10 8 | 366 -755 11 115
grg 105| 2 0 3 -35 -11 -42 -.10 13 11 | 173 -451 11 151
igr n/a| 0 0 -1 -25 -12 9 -.01 4 4 | 2777 -550 14 84
jpl 80| 2 0 1 23 -14 16 .24 11 11 | 135251 -954 34 133
mit 350| 1 0 3 1 -16 -5 -.02 12 10 | 123 -627 45 258
ngs 209| 0 0 -1 10 6 11 .03 9 8 | -394 -386 1048 2301
sio 347| 0 0 0 4 -13 -9 -.05 13 13 | --- --- --- ---
Table 2.2003.3 GPS week: 2003 Day: 3 MJD: 58268.000
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 264| 0 0 4 30 -5 10 -.04 10 9 | -576 21 11 107
emr 79| -8 1 0 11 7 48 .14 15 15 | 139613 110 18 134
esa 150| 0 0 -6 0 1 12 -.10 9 9 | -829 -772 8 207
gfz 185| -1 2 0 25 25 -9 .04 10 8 | 87 -188 10 165
grg 110| 2 -1 0 -12 0 -16 -.10 13 11 | 119 -33 10 150
igr n/a| 0 0 0 -5 -1 5 -.03 4 4 | 2883 541 13 77
jpl 80| -1 0 1 36 28 17 .20 10 10 | 134707 144 30 129
mit 350| 2 -1 3 -35 -12 -13 .01 11 9 | 555 -89 44 240
ngs 213| 0 0 -1 11 5 19 .09 10 9 | -563 -14 1006 2273
sio 353| 1 -1 1 -39 -45 -42 -.01 12 12 | --- --- --- ---
Table 2.2003.4 GPS week: 2003 Day: 4 MJD: 58269.000
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 -1 2 -5 -5 -4 -.07 10 10 | -547 -27 12 111
emr 80| -2 0 0 1 12 36 .14 13 13 | 139714 -1525 16 149
esa 150| 0 0 -6 -29 -16 -5 -.09 9 9 | -1238 848 9 198
gfz 183| 0 2 1 33 13 10 .05 10 9 | 512 -726 13 130
grg 101| 1 0 4 -22 13 -9 -.04 12 11 | 116 -19 10 152
igr n/a| 0 0 0 -18 6 -8 -.02 5 5 | 3476 -1019 13 66
jpl 80| -2 1 0 20 -18 13 .15 10 10 | 134893 -1117 34 110
mit 350| 0 -1 1 19 3 16 -.00 11 10 | -165 -45 33 273
ngs 208| 0 0 -1 17 2 -6 .09 9 8 | -582 8 1461 2557
sio 349| 0 0 2 -10 -11 -27 -.07 13 12 | --- --- --- ---
Table 2.2003.5 GPS week: 2003 Day: 5 MJD: 58270.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 258| 0 0 0 11 -16 -10 -.03 10 10 | -931 280 11 107
emr 80| -2 -1 0 -1 -2 19 .14 13 13 | 138095 206 16 130
esa 150| 0 0 -5 1 -9 2 -.08 9 9 | -701 -857 10 182
gfz 182| -1 1 1 10 -7 -4 .07 11 10 | -649 532 12 108
grg 111| 1 0 4 -1 -7 -12 -.06 12 11 | -333 339 11 146
igr n/a| 0 0 -1 6 -3 -9 -.01 6 6 | 2220 559 15 77
jpl 80| 0 0 0 29 -8 18 .15 10 10 | 133520 321 34 114
mit 350| 0 0 2 -13 45 7 -.01 12 10 | 33 17 37 242
ngs 207| 0 0 -1 -1 3 9 .04 8 7 | -875 209 1107 2274
sio 338| 0 0 1 -10 11 -7 -.08 12 12 | --- --- --- ---
Table 2.2003.6 GPS week: 2003 Day: 6 MJD: 58271.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 263| 0 0 0 17 -3 6 -.08 9 9 | -656 -30 12 111
emr 80| -2 0 1 21 -11 27 .17 14 14 | 138185 26 17 113
esa 150| 0 0 -4 -6 2 2 -.08 9 9 | -1148 -364 9 173
gfz 182| -1 0 1 6 20 0 .07 10 8 | -509 349 9 106
grg 100| 1 0 4 -13 20 -2 -.06 13 12 | -195 184 9 135
igr n/a| 0 0 0 1 5 -2 -.02 4 4 | 2732 228 12 78
jpl 80| 0 4 0 31 23 37 .24 11 11 | 133785 200 35 107
mit 350| 0 -1 3 -24 -55 22 -.02 13 12 | -84 -235 37 289
ngs 206| 0 0 -3 10 -4 11 .05 8 7 | -640 -70 860 2187
sio 336| 0 0 0 -22 16 -57 -.04 11 12 | --- --- --- ---
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 3.2003.0 GPS week: 2003 Day: 0 MJD: 58265.000
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 10 6 10 11 4 7 6 6 10 3 | 28 31 29 30 29 27 31 28 28 29 28
2 | 7 11 7 9 11 3 10 9 9 15 3 | 25 25 26 28 24 24 25 26 26 26 24
3 | 8 11 10 5 9 2 10 8 6 11 3 | 33 41 32 36 33 34 41 33 34 38 34
X4 | 3 --- --- --- --- 38 --- --- --- --- 0 | 28 --- --- --- --- 39 --- --- --- --- 28
5 | 6 10 11 13 11 6 12 21 8 9 4 | 78 78 80 75 74 78 78 69 77 76 76
6 | 7 9 5 5 9 3 9 6 6 10 2 | 24 29 26 23 26 23 29 24 28 26 24
7E | 10 14 7 8 8 4 14 10 8 8 3 | 49 52 48 46 47 47 49 50 51 49 48
8 | 10 16 10 7 18 4 7 8 6 9 4 | 28 31 28 28 32 26 29 27 27 25 27
9 | 5 11 7 6 8 4 8 4 5 7 2 | 29 35 34 31 32 31 36 32 33 33 32
10 | 4 12 8 10 6 3 13 9 7 12 3 | 23 33 21 23 25 23 33 25 25 27 23
11E | 10 12 7 9 9 4 7 7 5 10 3 | 56 56 54 54 53 53 55 55 54 57 55
12 | 11 19 8 11 14 5 11 17 11 14 4 | 22 23 20 25 23 22 25 31 25 22 22
13 | 14 12 10 12 12 5 11 13 9 17 4 | 30 36 32 37 29 32 35 33 36 34 31
14 | 9 12 10 10 11 4 11 12 9 17 4 | 49 55 49 52 52 51 53 51 54 50 50
15 | 12 14 11 13 12 5 13 14 11 17 5 | 43 46 47 34 43 37 46 35 35 40 39
16 | 14 23 8 15 15 8 8 40 11 17 7 | 24 24 25 33 25 27 25 41 31 30 24
17E | 9 13 6 10 12 5 12 11 6 9 3 | 44 47 45 51 42 48 45 50 51 47 47
18 | 12 9 9 13 9 5 9 9 6 13 4 | 49 47 44 48 41 43 48 44 43 49 45
19E | 10 12 6 9 13 4 9 10 8 12 3 | 60 61 59 59 57 60 61 59 60 57 59
20 | 6 12 9 8 10 3 9 12 10 10 3 | 18 16 17 13 19 15 17 20 20 20 16
21 | 8 10 10 11 15 4 11 12 8 14 4 | 27 27 26 28 25 27 26 29 30 27 26
22 | 7 8 9 8 9 3 7 9 8 15 3 | 21 24 21 25 22 22 24 22 25 28 22
23 | 10 22 11 12 12 5 7 11 9 16 4 | 34 32 33 37 33 34 33 36 37 37 34
24E | 10 13 10 10 13 4 10 11 8 16 4 | 96 100 98 97 98 99 97 100 94 102 98
25 | 7 8 5 8 11 4 9 8 5 12 3 | 20 22 20 22 21 19 24 21 19 23 20
26 | 6 8 6 7 8 3 8 11 5 8 2 | 24 28 24 24 26 22 26 24 23 22 23
27 | 10 10 9 7 15 4 8 13 6 7 3 | 28 28 26 28 31 25 28 26 25 25 26
28 | 11 13 8 10 13 4 10 12 9 19 4 | 20 26 20 28 20 24 27 29 29 23 22
29E | 11 30 6 13 16 3 13 15 9 11 5 | 85 82 87 92 84 87 85 88 88 84 86
30E | 13 14 10 9 12 5 9 6 7 6 3 | 35 34 36 30 32 31 34 29 29 32 31
31E | 8 9 6 7 14 3 10 11 6 11 3 | 52 55 55 56 54 54 54 54 55 57 54
32 | 5 9 8 6 8 4 9 12 7 11 3 | 32 36 34 34 35 32 36 30 34 36 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 8 10 12 4 10 13 8 13 |T 37 40 38 39 38 38 40 39 39 39 37
WRMS | 9 14 8 9 12 4 10 11 6 14 |NE 30 33 31 32 31 30 33 32 32 32 30
MEDI | 9 12 8 9 11 4 9 11 8 11 |MD 29 34 32 33 32 31 34 32 33 33 31
Table 3.2003.1 GPS week: 2003 Day: 1 MJD: 58266.000
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 13 7 9 11 4 8 7 7 13 3 | 38 39 40 36 38 36 40 37 39 39 37
2 | 10 12 8 10 11 3 12 6 10 13 3 | 31 32 30 35 30 31 33 33 34 33 31
3 | 11 12 12 9 10 3 10 8 7 12 3 | 32 40 38 35 31 34 42 33 37 36 34
X4 | 3 --- --- --- --- 18 --- --- --- --- 0 | 28 --- --- --- --- 28 --- --- --- --- 28
5 | 7 7 10 8 11 5 11 12 8 9 3 | 57 54 58 56 54 55 57 52 56 55 55
6 | 5 9 8 8 11 3 10 5 9 8 3 | 31 36 31 33 34 31 36 31 34 32 32
7E | 11 14 8 7 12 4 15 12 9 8 3 | 47 48 43 45 46 44 46 46 46 47 45
8 | 12 11 10 7 17 4 9 7 6 11 4 | 34 36 36 33 36 32 35 33 35 31 33
9 | 6 12 7 7 9 3 10 3 6 9 2 | 37 42 36 37 37 36 39 35 37 38 37
10 | 6 10 8 8 8 3 13 11 7 10 3 | 24 33 25 24 26 25 34 26 27 28 25
11E | 9 10 9 10 9 4 8 7 5 11 3 | 67 69 70 66 66 67 68 68 67 66 67
12 | 12 18 8 13 17 5 11 16 12 17 5 | 28 29 22 28 27 25 28 29 27 25 25
13 | 8 10 13 12 11 4 11 12 7 13 4 | 35 38 35 40 32 35 40 36 36 39 35
14 | 10 10 11 14 14 4 11 11 9 19 4 | 57 61 59 59 57 58 60 60 59 57 57
15 | 9 15 14 13 13 4 11 14 11 17 5 | 34 36 38 31 35 30 37 29 29 36 32
16 | 15 21 9 17 20 9 9 40 14 19 7 | 27 29 29 33 27 30 28 46 32 31 27
17 | 9 15 9 12 12 4 13 9 9 10 4 | 39 42 38 42 38 40 42 43 44 42 40
18 | 11 13 8 10 10 7 9 6 7 16 4 | 46 47 48 46 43 44 49 45 46 48 45
19E | 9 11 7 11 15 4 11 8 9 14 4 | 61 61 59 58 59 58 61 61 59 61 59
20 | 7 12 9 10 11 4 11 13 7 9 3 | 25 24 25 22 27 23 27 23 25 26 23
21 | 11 8 10 12 11 5 10 12 9 15 4 | 32 34 32 36 32 33 32 35 33 32 32
22 | 11 16 10 7 11 3 6 8 9 15 4 | 28 32 30 30 27 28 31 29 32 33 29
23 | 12 21 10 13 14 6 9 12 10 15 5 | 40 40 40 44 40 42 41 41 44 43 40
24E | 13 15 15 18 27 7 13 10 14 15 6 | 55 54 58 54 57 53 55 54 50 58 54
25 | 7 8 6 8 12 2 9 8 7 9 3 | 26 29 24 27 26 24 28 24 24 27 25
26 | 10 10 6 8 10 3 6 9 5 10 3 | 28 33 30 28 30 27 30 29 28 25 28
27 | 14 10 10 7 14 4 8 9 8 7 3 | 35 35 33 32 35 30 34 30 30 29 31
28 | 9 10 10 14 15 4 10 11 9 17 4 | 25 29 25 31 24 28 30 31 35 27 27
29 | 15 22 9 14 16 7 13 16 10 11 5 | 92 87 93 96 90 91 89 91 95 96 92
30E | 12 14 11 8 12 5 9 9 10 6 4 | 19 22 22 19 19 17 22 23 19 21 19
31E | 13 10 7 9 15 3 10 11 8 13 4 | 54 56 57 57 55 56 57 58 58 55 55
32 | 6 7 10 5 9 4 8 8 6 8 2 | 37 40 37 37 39 37 39 36 39 38 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 9 11 13 5 10 12 9 13 |T 39 41 40 40 39 38 41 40 40 40 38
WRMS | 10 13 9 9 12 4 10 10 7 13 |NE 33 36 34 35 34 33 36 34 35 35 33
MEDI | 10 12 9 10 12 4 10 9 9 12 |MD 34 38 36 36 35 33 39 35 36 36 33
Table 3.2003.2 GPS week: 2003 Day: 2 MJD: 58267.000
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 10 6 8 8 4 8 6 8 11 3 | 26 29 26 28 31 25 28 26 26 29 26
2 | 10 10 8 13 12 3 11 7 12 13 4 | 30 26 28 32 26 27 28 28 29 27 27
3 | 8 13 10 7 7 3 12 7 4 11 3 | 33 41 32 37 36 32 41 34 33 37 34
X4 | 2 --- --- --- --- 19 --- --- --- --- 0 | 26 --- --- --- --- 24 --- --- --- --- 26
5 | 5 7 9 8 9 3 10 10 8 10 3 | 47 46 49 48 46 45 47 45 49 46 46
6 | 6 9 6 8 10 4 13 8 11 9 3 | 26 28 28 26 28 25 31 27 30 29 26
7E | 6 11 5 10 16 4 14 9 8 9 3 | 31 32 31 31 33 29 34 32 33 32 31
8 | 10 10 11 8 14 4 9 6 5 9 3 | 27 29 25 26 32 27 30 26 28 26 26
9 | 6 11 9 6 9 3 8 5 6 8 3 | 21 28 25 25 26 22 29 23 24 25 23
10 | 4 9 8 6 7 3 13 7 10 10 3 | 24 33 27 27 29 26 35 26 27 29 26
11E | 7 10 6 8 10 4 10 7 8 11 3 | 42 42 38 42 44 40 41 35 39 40 39
12 | 12 16 8 13 15 4 10 13 15 18 5 | 24 24 22 23 21 22 24 24 23 19 20
13 | 9 10 12 11 13 6 14 13 9 16 4 | 35 35 32 36 32 33 36 33 35 34 32
14 | 9 10 9 11 12 3 12 13 9 19 4 | 39 43 41 43 45 40 44 43 43 44 41
15 | 8 12 13 11 11 4 14 13 12 17 4 | 35 38 43 33 38 34 41 32 34 35 35
16 | 13 25 8 15 17 9 9 40 13 18 7 | 23 21 21 29 24 23 23 40 26 25 20
17 | 8 14 6 12 14 4 11 12 11 12 4 | 37 39 37 41 33 39 38 44 43 35 38
18 | 8 9 7 10 10 4 10 7 7 11 3 | 34 36 32 34 33 31 35 32 33 35 32
19E | 10 13 5 11 11 6 9 10 11 15 4 | 88 90 89 85 86 85 91 90 87 88 87
20 | 9 9 9 9 10 3 13 11 10 14 4 | 19 18 19 16 20 16 19 18 19 23 17
21 | 7 8 9 11 12 3 14 10 8 18 4 | 26 28 26 31 27 26 25 30 28 26 26
22 | 7 6 10 6 8 3 8 8 11 15 3 | 23 26 23 27 26 23 26 25 24 30 24
23 | 11 24 8 14 12 5 9 13 10 17 5 | 33 32 31 37 37 32 35 35 34 34 33
24E | 12 24 14 10 21 6 21 17 13 17 6 | 73 78 78 77 79 75 87 76 75 76 75
25 | 6 8 5 7 10 3 9 8 6 8 2 | 21 22 22 23 22 22 25 23 23 20 21
26 | 8 8 5 5 9 2 9 12 7 9 3 | 22 24 21 25 25 22 25 21 22 20 21
27 | 12 8 9 6 13 4 10 10 5 9 3 | 26 26 23 27 31 24 26 24 25 24 25
28 | 11 11 6 13 16 5 9 9 10 18 4 | 23 27 22 27 21 22 27 26 27 21 22
29 | 11 31 7 15 19 5 12 14 12 14 6 | 52 50 55 58 47 53 50 52 53 51 51
30E | 7 11 10 9 13 4 10 6 8 8 3 | 22 23 23 20 22 20 24 21 19 21 20
31E | 11 10 7 9 17 3 10 10 7 13 4 | 47 48 45 48 50 46 48 47 46 51 47
32 | 7 8 8 7 8 3 8 6 7 9 2 | 23 27 24 24 25 23 27 22 24 26 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 10 13 4 11 12 9 13 |T 33 35 33 35 34 32 36 34 34 34 32
WRMS | 9 13 8 8 11 4 11 10 8 13 |NE 27 29 27 29 29 26 30 28 28 28 27
MEDI | 8 10 8 9 12 4 10 10 9 12 |MD 26 29 28 31 31 26 31 30 29 29 26
Table 3.2003.3 GPS week: 2003 Day: 3 MJD: 58268.000
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 15 5 7 10 4 7 5 10 12 3 | 27 31 27 28 30 25 29 25 30 31 27
2 | 9 10 8 10 13 3 7 8 10 13 3 | 24 23 24 26 24 22 22 23 23 23 22
3 | 7 15 10 7 7 3 13 6 8 11 3 | 20 33 22 21 20 21 33 20 28 23 22
X4 | 3 --- --- --- --- 17 --- --- --- --- 0 | 27 --- --- --- --- 20 --- --- --- --- 26
5 | 6 10 11 8 6 4 11 9 7 11 3 | 27 25 30 27 27 26 29 27 29 28 27
6 | 7 10 6 8 10 4 9 6 8 9 3 | 26 31 28 25 27 24 32 25 29 30 26
7E | 6 15 7 8 13 4 12 10 9 7 3 | 31 33 30 27 31 28 32 31 32 32 30
8 | 10 11 10 8 15 3 9 7 8 9 3 | 26 28 26 27 31 25 28 24 29 23 25
9 | 4 11 7 7 8 4 9 4 8 7 2 | 22 28 24 23 24 21 30 22 27 24 23
10 | 10 11 10 7 6 3 12 6 6 10 3 | 26 31 23 23 26 24 30 25 27 26 24
11E | 10 12 8 8 12 4 9 8 7 8 3 | 104 106 103 101 103 101 103 99 102 102 102
12 | 16 18 8 12 14 5 12 11 14 16 5 | 26 26 20 23 24 20 24 23 22 21 20
13 | 9 12 14 11 11 4 13 11 10 16 4 | 23 29 22 31 22 27 31 27 31 28 25
14 | 10 13 12 10 13 3 9 11 10 19 4 | 31 35 33 32 31 31 32 34 33 33 31
15 | 9 20 14 13 12 5 16 11 12 16 5 | 38 42 42 33 41 32 42 29 30 38 34
16 | 14 24 11 18 19 10 9 39 14 18 8 | 24 24 21 28 23 23 21 39 26 24 19
17 | 7 17 5 8 15 4 11 8 7 10 3 | 30 36 31 31 31 31 32 34 36 31 31
18 | 11 13 7 9 10 4 11 6 9 13 3 | 30 34 30 30 31 30 34 28 31 34 29
19E | 20 16 8 7 20 6 9 8 9 10 5 | 129 134 129 130 127 128 130 124 128 124 127
20 | 6 15 11 9 7 3 11 11 9 12 3 | 21 23 22 23 22 22 20 22 23 22 20
21 | 9 12 10 12 12 4 14 11 11 15 4 | 23 27 27 26 25 23 24 24 25 22 22
22 | 8 12 9 7 7 4 5 9 9 14 3 | 18 23 18 19 19 20 21 19 24 24 19
23 | 10 24 11 12 13 6 8 12 11 15 5 | 23 26 23 27 24 25 25 27 30 26 24
24E | 9 21 15 8 11 4 --- 15 17 11 5 | 51 62 56 52 56 52 --- 52 56 53 52
25 | 9 13 7 7 7 3 8 8 10 8 3 | 22 26 20 22 23 19 22 20 19 21 20
26 | 9 11 5 9 10 4 7 10 10 9 3 | 23 27 21 24 25 21 23 21 24 20 21
27 | 13 12 9 6 19 4 9 9 7 8 4 | 27 29 27 28 32 25 28 25 28 24 26
28 | 8 15 6 12 16 5 8 9 10 13 4 | 20 29 22 27 21 23 27 27 29 24 23
29 | 10 25 7 15 21 6 11 14 9 13 5 | 37 39 39 45 39 40 39 42 42 39 38
30E | 9 11 11 9 17 4 10 9 9 7 4 | 29 26 31 28 24 26 29 28 27 30 27
31E | 8 15 8 11 15 4 8 9 9 11 4 | 33 34 31 33 32 31 32 33 31 34 31
32 | 7 11 10 6 7 4 6 5 8 11 3 | 26 31 29 28 30 27 30 24 27 30 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 9 10 13 4 10 11 10 12 |T 32 36 33 33 33 31 34 33 34 33 31
WRMS | 9 15 9 8 11 4 10 9 9 12 |NE 25 28 25 26 26 24 27 25 27 26 24
MEDI | 9 13 9 8 12 4 9 9 9 11 |MD 26 29 27 27 27 25 29 27 29 28 26
Table 3.2003.4 GPS week: 2003 Day: 4 MJD: 58269.000
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 11 11 6 7 9 7 11 3 | 30 34 32 34 35 31 33 33 30 34 32
2 | 11 9 8 10 12 3 10 9 11 12 4 | 34 34 29 34 32 32 35 33 32 34 32
3 | 9 12 10 8 7 4 12 7 6 12 3 | 31 39 33 35 34 34 41 35 36 37 34
X4 | 1 --- --- --- --- 22 --- --- --- --- 0 | 25 --- --- --- --- 23 --- --- --- --- 25
5 | 6 10 11 7 6 4 10 8 8 12 3 | 52 53 52 50 49 49 51 51 54 54 51
6 | 5 8 6 8 10 4 7 7 9 9 3 | 32 36 32 31 34 32 35 33 32 37 32
7E | 5 15 6 8 13 4 11 8 9 7 3 | 41 44 41 41 45 40 43 43 42 43 42
8 | 8 12 9 9 15 4 9 5 7 8 3 | 30 33 31 34 37 31 31 33 32 31 32
9 | 7 8 7 6 7 4 7 4 6 7 2 | 31 36 33 33 32 31 37 34 33 35 33
10 | 9 10 9 8 7 3 11 7 5 11 3 | 24 34 26 28 27 28 35 29 30 32 28
11E | 9 9 7 10 12 5 8 7 7 10 3 | 47 51 47 51 47 47 51 53 50 50 49
12 | 13 19 9 12 14 5 10 11 14 17 5 | 29 29 23 25 24 24 27 24 26 25 24
13 | 15 12 11 11 10 6 13 11 11 14 4 | 38 41 33 42 33 36 40 36 38 37 36
14 | 11 10 12 14 13 4 10 11 10 18 4 | 45 47 44 49 47 47 49 49 50 49 47
15 | 13 13 12 13 8 4 11 12 11 17 4 | 44 42 43 38 38 37 43 35 36 37 38
16 | 14 24 12 17 19 8 10 38 16 18 8 | 26 27 26 32 26 28 26 42 30 31 25
17 | 7 13 5 10 15 4 11 8 9 8 3 | 33 36 31 36 35 34 34 39 38 36 35
18 | 12 9 9 10 8 11 10 8 8 12 3 | 43 43 39 42 40 35 42 40 39 42 40
19 | 11 13 6 9 14 6 9 10 9 8 3 | 105 105 102 105 105 101 103 106 103 104 104
20 | 6 11 11 9 8 3 10 11 10 14 4 | 22 25 22 23 24 23 24 25 24 27 22
21 | 11 9 10 11 11 3 13 10 6 17 4 | 31 32 29 33 31 30 31 33 32 30 30
22 | 9 7 11 8 6 5 8 9 10 16 3 | 27 30 26 29 30 29 30 30 32 35 28
23 | 12 23 10 11 11 6 8 13 12 16 5 | 39 37 37 42 40 38 38 42 41 43 39
24E | 15 13 14 11 10 6 9 9 13 17 5 | 75 73 73 74 75 73 70 76 73 75 73
25 | 6 11 8 5 9 4 8 6 10 14 3 | 27 32 26 26 26 27 29 25 28 32 26
26 | 9 9 5 7 9 3 8 8 7 7 3 | 24 28 26 28 28 25 27 26 26 23 26
27 | 7 11 9 10 17 3 11 9 6 8 3 | 30 33 31 36 37 30 32 31 30 29 31
28 | 11 12 6 12 16 6 10 11 9 18 4 | 28 30 24 33 25 27 29 33 30 28 27
29 | 8 25 7 11 18 4 11 15 11 14 5 | 29 26 28 31 33 29 28 32 34 28 28
30E | 8 11 11 12 16 5 10 6 12 6 4 | 22 20 23 21 19 18 20 22 20 21 20
31E | 9 11 8 7 15 3 10 9 9 11 3 | 45 46 46 47 45 45 49 46 49 46 46
32 | 8 7 11 6 8 2 6 6 6 12 3 | 30 35 33 32 32 31 33 31 34 35 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 9 10 12 5 10 11 9 13 |T 36 39 36 38 37 35 38 38 38 38 36
WRMS | 10 13 9 9 11 5 10 10 8 12 |NE 32 35 31 34 33 31 34 34 33 34 32
MEDI | 9 11 9 10 11 4 10 9 9 12 |MD 31 35 32 34 34 31 35 33 33 35 32
Table 3.2003.5 GPS week: 2003 Day: 5 MJD: 58270.000
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 17 5 7 10 4 7 7 7 10 3 | 22 24 19 22 24 20 23 20 20 20 19
2 | 11 10 7 10 14 4 12 10 9 13 4 | 28 26 27 29 28 27 28 28 30 26 27
3 | 9 12 9 8 5 4 13 8 9 12 3 | 20 30 20 22 20 21 32 21 21 27 21
X4 | 1 --- --- --- --- 20 --- --- --- --- 0 | 29 --- --- --- --- 28 --- --- --- --- 30
5 | 6 8 11 8 6 4 7 10 7 13 3 | 43 43 44 43 44 42 43 42 43 44 43
6 | 8 10 6 8 8 5 9 9 6 8 3 | 22 25 22 20 25 21 26 20 24 25 22
7E | 7 12 6 10 17 5 10 6 7 6 3 | 39 42 36 39 43 38 40 39 40 39 39
8 | 6 11 8 8 14 5 10 7 7 8 3 | 19 20 19 23 23 19 19 20 20 20 19
9 | 5 10 7 8 8 4 9 7 7 10 3 | 30 32 28 29 29 28 32 29 30 31 29
10 | 8 10 9 9 5 4 13 8 5 10 3 | 13 25 12 15 13 15 25 16 15 17 14
11E | 8 14 8 9 11 4 9 8 7 10 3 | 75 81 76 76 81 76 79 78 75 77 77
12 | 10 17 8 13 12 4 9 11 11 15 4 | 25 22 19 24 22 22 23 24 22 21 21
13 | 13 14 11 11 9 5 13 12 8 14 4 | 21 31 22 29 23 25 29 25 26 26 24
14 | 8 10 11 13 11 6 10 12 9 17 4 | 24 28 24 28 27 26 26 29 32 29 26
15 | 12 12 13 14 9 8 11 14 10 17 4 | 35 37 36 32 33 28 36 30 29 35 32
16 | 15 24 10 19 19 11 11 39 13 20 7 | 21 19 20 29 18 23 20 41 28 27 19
17 | 9 13 6 11 10 7 14 9 5 10 3 | 26 26 24 28 25 27 23 28 28 26 25
18 | 13 14 10 8 9 5 11 7 6 12 3 | 33 31 27 30 29 29 32 28 27 32 28
19 | 10 12 7 10 11 7 11 10 6 11 3 | 51 52 48 48 47 48 53 50 49 48 49
20 | 9 12 11 11 7 5 11 11 10 14 4 | 18 20 20 20 21 21 20 20 19 22 18
21 | 16 11 10 13 11 8 11 12 12 14 4 | 23 22 18 26 21 21 22 25 24 21 20
22 | 9 8 8 7 7 4 9 11 8 15 3 | 19 18 15 19 17 17 20 19 18 25 17
23 | 12 22 8 14 13 8 9 12 11 17 5 | 27 25 24 30 27 28 25 30 29 32 26
24E | 14 11 10 16 10 5 8 13 7 14 4 | 68 63 70 73 70 68 63 63 64 69 67
25 | 6 9 6 9 7 4 8 5 5 9 2 | 16 23 18 16 19 15 21 17 17 20 17
26 | 9 11 6 11 8 5 8 9 6 8 3 | 20 21 21 21 20 17 20 18 22 20 19
27 | 9 10 8 7 16 5 10 7 8 8 3 | 20 21 21 25 23 19 19 21 24 22 21
28 | 11 11 7 15 15 7 10 12 7 16 4 | 19 23 18 25 18 20 23 21 20 17 18
29 | 9 21 7 15 18 7 11 13 9 12 5 | 30 31 31 37 32 34 32 34 33 31 31
30E | 11 12 12 15 17 5 16 7 10 9 4 | 31 31 32 30 30 28 33 31 29 32 30
31E | 8 11 6 9 13 4 10 8 5 11 3 | 39 42 42 43 40 40 41 44 45 45 41
32 | 10 7 10 8 6 6 6 5 7 11 3 | 34 35 32 34 33 33 36 32 37 37 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 9 11 11 6 10 12 8 12 |T 29 31 28 31 29 28 31 30 30 31 28
WRMS | 10 13 9 10 11 6 10 10 7 12 |NE 24 26 22 25 24 23 26 25 25 25 23
MEDI | 9 11 8 10 10 5 10 9 7 12 |MD 25 26 24 29 25 26 26 28 28 27 25
Table 3.2003.6 GPS week: 2003 Day: 6 MJD: 58271.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 20 4 8 9 3 8 12 6 11 3 | 24 27 22 26 26 22 26 24 22 25 22
2 | 7 9 6 7 14 3 11 10 8 10 3 | 34 33 33 32 29 31 32 31 31 29 31
3 | 9 12 8 6 6 3 11 9 7 8 3 | 30 40 30 35 31 31 40 31 32 34 32
X4 | 1 --- --- --- --- 20 --- --- --- --- 0 | 31 --- --- --- --- 27 --- --- --- --- 32
5 | 5 7 9 9 7 2 8 10 6 12 3 | 59 59 61 59 59 58 57 55 59 60 59
6 | 6 9 7 7 12 4 10 8 8 10 3 | 23 29 25 23 28 22 29 23 27 26 24
7E | 8 14 5 7 15 4 13 12 9 6 3 | 44 42 40 43 45 42 45 43 44 41 42
8 | 9 11 8 10 17 3 11 7 6 7 3 | 24 26 26 27 28 25 28 25 28 27 25
9 | 5 8 7 5 9 3 7 6 6 7 2 | 28 31 28 27 27 26 31 29 26 29 27
10 | 7 10 9 5 5 4 12 10 3 6 2 | 26 33 23 25 26 24 33 26 25 26 25
11E | 7 12 7 9 13 4 10 9 4 11 3 | 73 74 72 74 77 73 71 72 73 79 74
12 | 8 18 11 10 13 3 10 12 9 13 4 | 28 26 23 26 23 24 26 27 26 25 24
13 | 14 11 11 14 10 5 14 15 10 16 4 | 26 32 28 39 27 32 30 32 34 35 30
14 | 9 11 10 11 11 4 11 13 8 15 4 | 34 36 34 39 36 35 36 36 36 36 35
15 | 9 13 13 12 7 5 12 16 10 16 4 | 45 52 48 43 46 42 51 40 39 45 43
16 | 15 22 9 15 19 9 9 39 13 18 7 | 25 22 24 34 23 27 23 41 30 31 24
17 | 9 13 4 10 14 4 14 11 7 11 3 | 30 32 31 36 32 33 31 37 38 34 33
18 | 8 17 7 10 9 4 10 10 5 13 3 | 40 42 37 41 37 38 43 39 37 43 38
19 | 10 15 6 8 14 5 10 12 9 12 4 | 78 81 78 78 78 77 81 79 79 76 78
20 | 7 11 9 9 7 2 10 11 6 12 3 | 27 26 27 25 28 26 26 30 28 30 26
21 | 7 8 9 10 10 4 11 12 6 15 3 | 22 23 21 24 23 20 22 24 23 21 20
22 | 8 9 9 8 5 4 11 11 8 13 3 | 23 27 22 28 24 25 27 25 28 31 25
23 | 11 20 9 10 13 5 10 12 11 16 4 | 30 29 29 32 29 29 30 31 29 34 29
24E | 11 11 11 16 14 5 10 9 9 8 4 | 108 108 111 110 111 109 105 107 111 108 109
25 | 8 9 9 5 10 3 8 9 7 8 3 | 21 23 22 20 23 19 23 22 20 24 20
26 | 8 11 5 8 10 3 8 7 7 10 3 | 24 24 23 24 25 22 26 23 25 22 23
27 | 7 11 8 7 18 4 10 6 8 7 3 | 24 24 27 28 29 25 25 25 27 26 25
28 | 11 10 8 12 13 7 10 15 8 13 4 | 22 29 24 32 21 26 30 32 28 25 25
29 | 8 28 8 10 21 4 11 15 10 11 5 | 44 38 42 46 39 43 40 48 44 44 42
30E | 15 13 13 12 19 4 27 10 12 6 5 | 45 44 44 44 40 42 51 43 40 42 42
31E | 6 14 8 8 19 3 10 19 8 9 4 | 42 43 43 47 43 43 45 52 46 48 44
32 | 13 8 10 6 7 4 6 11 6 12 3 | 35 34 31 31 32 30 34 32 32 36 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 9 10 13 4 11 13 8 11 |T 36 38 36 38 36 35 38 38 37 38 36
WRMS | 9 14 9 8 12 4 11 12 7 12 |NE 29 31 29 31 29 28 31 30 30 31 29
MEDI | 8 11 8 9 12 4 10 11 8 11 |MD 30 32 29 32 29 29 31 32 31 34 30
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 4.2003 GPS week: 2003 MJD: 58265.0-58271.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 |U 11 10 30 |U 7 15 28 |U 11 13 33 |
emr | emr 2975 |U 16 21 29 |U 13 15 52 | 16 20 46 |
esa | esa 2976 | 11 10 25 |U 9 16 31 | 11 13 35 |
gfz | gfz 2975 |U 12 10 28 |U 12 19 43 |U 11 14 37 |
grg | grg 2975 | 12 12 27 | 11 18 34 | 13 16 42 |
igr | igr 2958 | 10 9 25 | 8 16 30 | 11 15 36 |
igs | igs 2975 | 10 10 23 | 9 14 32 | 11 13 34 |
jpl | jpl 2962 | 14 15 29 |U 9 14 37 |U 14 12 39 |
mit | mit 2976 | 13 13 29 |U 10 14 36 |U 56 30 67 |
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 5.2003.0 GPS week: 2003 Day: 0 MJD: 58265.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 13 14 33 | 7 12 27 | 12 15 35 |
emr | emr 2976 | 18 21 31 | 12 14 40 | 17 23 42 |
esa | esa 2976 | 11 14 24 | 7 15 28 | 11 14 36 |
gfz | gfz 2976 | 13 14 30 | 8 16 32 | 16 15 40 |
grg | grg 2976 | 12 13 25 | 9 22 38 | 12 19 49 |
igr | igr 2976 | 11 13 29 | 7 14 28 | 12 13 36 |
igs | igs 2976 | 11 13 25 | 7 13 27 | 12 14 35 |
jpl | jpl 2976 | 14 21 34 | 9 15 35 | 14 13 39 |
mit | mit 2976 | 12 16 30 | 9 13 32 | 18 20 44 |
Table 5.2003.1 GPS week: 2003 Day: 1 MJD: 58266.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 8 9 30 | 7 15 24 | 10 16 38 |
emr | emr 2976 | 14 17 26 | 12 16 43 | 18 26 54 |
esa | esa 2976 | 8 9 26 | 11 15 32 | 12 22 40 |
gfz | gfz 2976 | 7 7 25 | 11 14 35 | 11 21 43 |
grg | grg 2976 | 9 12 23 | 13 16 39 | 11 19 42 |
igr | igr 2976 | 6 8 24 | 9 15 30 | 11 19 41 |
igs | igs 2974 | 6 8 21 | 9 14 32 | 11 19 39 |
jpl | jpl 2976 | 13 18 29 | 11 12 37 | 15 18 49 |
mit | mit 2976 | 10 14 22 | 9 14 39 | 143 52 90 |
Table 5.2003.2 GPS week: 2003 Day: 2 MJD: 58267.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 15 12 25 | 8 18 30 | 11 11 29 |
emr | emr 2975 | 19 19 37 | 10 15 57 | 15 25 51 |
esa | esa 2976 | 16 10 22 | 8 18 30 | 10 10 28 |
gfz | gfz 2975 | 16 12 24 | 9 19 34 | 11 12 30 |
grg | grg 2975 | 19 13 22 | 10 19 34 | 12 14 31 |
igr | igr 2975 | 15 10 20 | 8 19 30 | 11 11 26 |
igs | igs 2975 | 16 11 19 | 8 16 32 | 11 10 29 |
jpl | jpl 2976 | 16 11 24 | 9 16 42 | 14 8 36 |
mit | mit 2976 | 20 14 24 | 8 15 33 | 17 28 49 |
Table 5.2003.3 GPS week: 2003 Day: 3 MJD: 58268.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 12 7 29 | 7 14 30 | 10 11 25 |
emr | emr 2976 | 14 24 30 | 21 17 74 | 15 14 37 |
esa | esa 2976 | 10 8 26 | 16 18 50 | 10 10 30 |
gfz | gfz 2974 | 14 7 28 | 29 37 102 | 10 12 29 |
grg | grg 2976 | 14 8 27 | 15 17 41 | 13 15 35 |
igr | igr 2967 | 11 6 24 | 13 16 40 | 11 24 38 |
igs | igs 2975 | 11 6 23 | 15 15 51 | 11 11 29 |
jpl | jpl 2880 | 14 16 25 | 10 12 50 | 17 14 41 |
mit | mit 2976 | 15 14 33 | 15 15 54 | 157 65 162 |
Table 5.2003.4 GPS week: 2003 Day: 4 MJD: 58269.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 13 12 34 | 8 16 27 | 11 13 33 |
emr | emr 2976 | 21 17 28 | 13 15 43 | 19 22 49 |
esa | esa 2976 | 13 11 29 | 9 19 24 | 11 13 37 |
gfz | gfz 2976 | 13 11 31 | 8 16 29 | 11 15 39 |
grg | grg 2976 | 12 13 32 | 10 19 28 | 13 14 39 |
igr | igr 2880 | 12 11 29 | 8 17 27 | 12 14 34 |
igs | igs 2976 | 12 11 30 | 9 16 28 | 12 14 34 |
jpl | jpl 2976 | 16 17 32 | 9 16 30 | 14 11 36 |
mit | mit 2976 | 11 13 37 | 10 15 29 | 21 18 37 |
Table 5.2003.5 GPS week: 2003 Day: 5 MJD: 58270.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 8 9 31 | 6 14 31 | 11 12 36 |
emr | emr 2976 | 16 24 24 | 11 11 55 | 16 15 45 |
esa | esa 2976 | 8 10 24 | 7 15 28 | 11 11 40 |
gfz | gfz 2976 | 8 10 28 | 6 15 32 | 11 13 40 |
grg | grg 2976 | 9 11 31 | 9 17 32 | 13 14 45 |
igr | igr 2976 | 7 9 24 | 6 17 30 | 11 11 38 |
igs | igs 2976 | 7 10 22 | 7 14 32 | 12 11 39 |
jpl | jpl 2976 | 11 14 26 | 8 14 34 | 14 9 39 |
mit | mit 2976 | 10 11 26 | 7 14 39 | 20 15 43 |
Table 5.2003.6 GPS week: 2003 Day: 6 MJD: 58271.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 11 9 29 | 8 13 23 | 10 10 35 |
emr | emr 2976 | 14 21 28 | 12 14 54 | 15 15 43 |
esa | esa 2976 | 10 8 26 | 9 12 23 | 10 10 35 |
gfz | gfz 2976 | 12 9 28 | 16 15 36 | 11 11 38 |
grg | grg 2976 | 12 12 29 | 10 15 26 | 15 19 51 |
igr | igr 2956 | 10 7 24 | 8 13 25 | 10 10 37 |
igs | igs 2976 | 10 8 23 | 8 13 23 | 11 10 36 |
jpl | jpl 2976 | 12 11 30 | 9 14 31 | 12 9 33 |
mit | mit 2976 | 13 9 32 | 11 10 26 | 17 16 45 |
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 6.2003 GPS week: 2003 MJD: 58265.500-58271.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -14 24 -4 -4 | 15 28
| 7 10 50 56 2 | 5
emr uuuuu | 29 2 56 72 -6 | 39 46
| 27 15 113 65 10 | 6
esa uuuuu | -5 0 -52 3 -9 | 23 33
| 13 14 40 70 4 | 5
gfz uuuuu | -4 5 -52 50 -1 | 25 31
| 8 23 70 104 4 | 4
grg uuuuu | -4 3 64 -130 7 | -1 22
| 15 19 37 42 2 | 2
igr xxxxx | 2 0 90 13 -11 | 5 25
| 14 13 71 57 3 | 7
irf xxxxx | -12 -12 -18 -55 -3 | 1 23
| 6 5 28 26 9 | 6
jpl xxxxx | 4 -27 112 13 5 | 27 32
| 26 8 77 53 15 | 2
mit uuuuu | -27 0 -45 -129 -4 | 30 37
| 18 6 76 66 5 | 5
ngs uuuuu | -6 -24 108 55 5 | 17 28
| 28 18 107 100 2 | 3
sio uuuux | 31 46 -117 73 -2 | 64 67
| 25 11 38 57 8 | 5
Table 7.2003.0 GPS week: 2003 Day: 0 MJD: 58265.500
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 | 6 -24 98 -7 -3 | 21 28
emr uuuuu | 1 8 63 79 -7 | 45 49
esa uuuuu | -1 6 -60 -129 -7 | 30 35
gfz uuuuu | 1 -39 87 -145 -2 | 29 33
grg uuuuu | -7 3 13 -73 6 | -2 20
igr xxxxx | 21 8 42 -51 -9 | 13 22
irf xxxxx | -14 -21 23 -50 -17 | 10 21
jpl xxxxx | 32 -19 122 70 2 | 29 33
mit uuuuu | -39 -2 84 -78 -11 | 37 40
ngs uuuuu | 7 8 -117 228 5 | 19 27
sio uuuux | 25 52 -86 64 -14 | 70 72
Table 7.2003.1 GPS week: 2003 Day: 1 MJD: 58266.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 12 -30 -51 36 -7 | 21 28
emr uuuuu | 22 -7 122 181 7 | 45 49
esa uuuuu | -22 -19 -41 24 -4 | 30 35
gfz uuuuu | -16 4 -19 32 -2 | 29 33
grg uuuuu | -4 36 69 -127 5 | 0 21
igr xxxxx | 5 -1 108 27 -15 | 13 22
irf xxxxx | -10 -9 -25 -69 -14 | 8 19
jpl xxxxx | 2 -35 237 0 17 | 30 34
mit uuuuu | -32 3 -74 -182 -10 | 36 40
ngs uuuuu | 29 -9 118 24 4 | 20 28
sio uuuux | 14 46 -135 -6 -10 | 70 71
Table 7.2003.2 GPS week: 2003 Day: 2 MJD: 58267.500
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 | -2 -6 26 -71 -7 | 18 28
emr uuuuu | -2 25 -80 -7 -18 | 44 48
esa uuuuu | -3 -10 10 54 -6 | 28 35
gfz uuuuu | -11 -3 -45 165 2 | 27 32
grg uuuuu | 14 16 32 -138 8 | 0 21
igr xxxxx | 12 14 43 115 -11 | 9 23
irf xxxxx | -5 -6 -5 -88 -6 | 3 21
jpl xxxxx | -9 -20 19 34 20 | 29 34
mit uuuuu | -23 2 -4 -199 -4 | 33 38
ngs uuuuu | 9 -41 75 117 4 | 19 28
sio uuuux | 27 58 -63 14 4 | 66 69
Table 7.2003.3 GPS week: 2003 Day: 3 MJD: 58268.500
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 | 9 -18 74 -4 -2 | 11 28
emr uuuuu | 70 -2 -71 104 -18 | 35 44
esa uuuuu | -14 -4 -24 -15 -15 | 20 33
gfz uuuuu | 0 23 -89 153 6 | 20 30
grg uuuuu | 10 4 85 -161 8 | -5 25
igr xxxxx | 6 4 36 -28 -10 | 1 27
irf xxxxx | -17 -15 -24 -84 4 | -5 26
jpl xxxxx | -18 -20 90 -65 8 | 25 31
mit uuuuu | -45 0 -54 -205 -1 | 26 36
ngs uuuuu | -5 -32 186 52 4 | 13 27
sio uuuux | 15 40 -150 102 0 | 60 64
Table 7.2003.4 GPS week: 2003 Day: 4 MJD: 58269.500
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 -13 29 -7 -5 | 12 28
emr uuuuu | 46 -1 59 23 -9 | 33 43
esa uuuuu | 18 26 -90 -19 -10 | 20 33
gfz uuuuu | -3 2 -119 4 -3 | 22 30
grg uuuuu | -26 -7 68 -139 6 | -2 22
igr xxxxx | -1 -2 81 -6 -12 | 1 27
irf xxxxx | -15 -12 -7 -38 4 | -4 25
jpl xxxxx | 39 -35 190 64 -18 | 27 32
mit uuuuu | -19 -10 -34 -66 0 | 26 36
ngs uuuuu | -26 -37 189 70 8 | 15 27
sio uuuux | 33 51 -121 161 -6 | 60 64
Table 7.2003.5 GPS week: 2003 Day: 5 MJD: 58270.500
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 | -2 -3 -3 91 -1 | 13 29
emr uuuuu | 50 14 52 105 -4 | 35 44
esa uuuuu | -6 -3 -111 11 -14 | 20 33
gfz uuuuu | -5 25 -76 66 -2 | 23 31
grg uuuuu | -19 -18 128 -192 10 | 1 23
igr xxxxx | -24 -26 238 -24 -11 | 0 27
irf xxxxx | -5 -15 -15 -18 2 | -3 26
jpl xxxxx | 13 -25 68 37 -9 | 27 32
mit uuuuu | 8 -3 -62 -50 -2 | 27 37
ngs uuuuu | -58 -17 134 -73 1 | 17 29
sio uuuux | 85 25 -93 103 -2 | 61 64
Table 7.2003.6 GPS week: 2003 Day: 6 MJD: 58271.500
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 -7 -4 -64 -3 | 11 27
emr uuuuu | 16 -21 250 19 4 | 33 42
esa uuuuu | -5 6 -50 93 -10 | 17 29
gfz uuuuu | 7 24 -106 74 -5 | 22 30
grg uuuuu | 5 -16 56 -82 6 | 1 23
igr xxxxx | -4 2 83 55 -6 | -3 24
irf xxxxx | -21 -7 -70 -37 5 | -5 24
jpl xxxxx | -32 -38 59 -50 19 | 25 29
mit uuuuu | -36 10 -169 -126 1 | 25 34
ngs uuuuu | 3 -37 169 -36 6 | 17 29
sio uuuux | 15 51 -168 75 10 | 59 62
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