[IGSREPORT-21948] Wk 1745 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jul 5 08:56:41 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1745 (Jun 16, 2013 - Jun 22, 2013)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1745[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1745[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1745[0-6].cls IGS GPS clock combination summary report.
igs17457.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17457.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 | 21 21 FLRS KOUC MIZU MOBS REYK FLRS KOUC MIZU MOBS
0 | COD | REYK XMIS
0 | EMR | 26 26
0 | ESA | IRKJ KOUC CAGZ IRKJ KOUC
0 | GFZ | 26 26
0 | GRG | 26 26 BOGT IRKJ TNML BOGT IRKJ TNML
0 | JPL | 6 8 26
0 | MIT | 13 23 26 13 23 26 MDVJ MDVJ
1 | COD | 14 14 HERT JOZ2 KOUC REYK HERT JOZ2 KOUC REYK
1 | EMR | 26 26
1 | ESA | IRKJ KOUC IRKJ KOUC UNSA
1 | GFZ | 26 26
1 | GRG | 26 26 ALIC FAA1 IRKJ ALIC FAA1 IRKJ
1 | JPL | 26
1 | MIT | 26 26 MDVJ
2 | COD | 26 26 KOUC KOUC MOBS REYK
2 | ESA | IRKJ KOUC IRKJ KOUC MATE
2 | GFZ | KOUR MATE KOUR MATE
2 | GRG | 26 26 BARH IRKJ KOUR REUN BARH IRKJ KOUR RESO REUN
2 | JPL | 26 29
2 | MIT | 26 10 26 GOPE KOSG MDVJ PRDS SYDN USNO
3 | COD | JOZ2 KOUC REYK CONZ JOZ2 KOUC REYK RIOP
3 | ESA | IRKJ KOUC IRKJ KOUC UNSA
3 | GFZ | NYAL NYAL
3 | GRG | 26 26 ABMF FAA1 IRKJ NICO NYAL USNO ABMF FAA1 IRKJ
3 | GRG | NICO NYAL USNO
3 | JPL | 26
3 | MIT | 10 26 10 26 KOSG MDVJ KOSG MDVJ
4 | COD | 26 26 KOSG KOUC MDVJ HERT KOUC
4 | EMR | 26 26 HERS IRKT YAKT
4 | ESA | KOUC KOUC MDVJ UNSA
4 | GFZ | ONSA ONSA
4 | GRG | 26 26 MDVJ ONSA POLV REUN USNO MDVJ ONSA POLV REUN
4 | GRG | USNO
4 | MIT | 6 26 6 26 SYDN USNO GOPE SYDN TWTF USNO
5 | COD | 26 CONZ JOZ2 KOUC CONZ JOZ2 KOUC
5 | EMR | 26 YELL YELL
5 | ESA | 26 IRKJ KOUC IRKJ KOUC UNSA
5 | GFZ | 26 ARTU ARTU
5 | GRG | 17 26 17 IRKJ NYAL SPT0 IRKJ NYAL SPT0
5 | MIT | 3 7 18 26 3 7 18 22 KOSG NYAL KOSG MDVJ NYAL
6 | ALL | 32 32
6 | COD | 26 26 DAV1 DAV1 FAA1
6 | ESA | 26 26 IRKJ MAW1 IRKJ MAW1 UNSA
6 | GFZ | KELY NRMD KELY NRMD
6 | GRG | CAGZ FAA1 IRKJ IRKT CAGZ FAA1 IRKJ IRKT NYAL
6 | MIT | 3 6 7 16 3 6 7 16 DAEJ MDVJ MOBS NYAL STR1 SYDN TLSE
6 | MIT | TOW2 USNO
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
6 | MIT | ~02:46 | ~ -0.06 ns
6. 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.
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
2 | NGS | 26
4 | NGS | 26
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G26 | | | | | | | 4 |
9. 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.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.1 .0 -1.1 -25 30 -6 .15
EMR | 0 | 8.6 -5.1 4.3 -52 -16 -26 .24
ESA | 0 | 4.5 -1.1 .5 56 -3 -23 .05
GFZ | 0 | .2 .0 -.6 -13 -23 -16 -.32
GRG | 0 | 10.2 -9.1 26.3 -27 52 -23 .28
JPL | 0 | 2.1 -7.4 14.9 -57 -24 -56 .46
MIT | 0 | 5.6 -4.2 8.9 -12 0 -45 .22
NGS | 0 | -.4 -2.4 17.6 -64 -20 -5 .46
SIO | 0 | 9.4 -4.6 -3.2 -104 -120 -174 .18
COD | 1 | .1 .5 -1.2 -27 21 -14 .06
EMR | 1 | 7.9 -4.9 9.0 -57 -23 -27 .56
ESA | 1 | 2.0 -2.2 .9 44 3 -32 .15
GFZ | 1 | .3 -.9 -.7 -20 -21 -6 -.02
GRG | 1 | 8.3 -5.3 31.7 -27 33 -40 .29
JPL | 1 | 4.1 -5.6 15.6 -10 71 -45 .57
MIT | 1 | 5.2 -4.6 9.5 -10 11 -52 .27
NGS | 1 | 5.2 -1.5 18.9 -67 -41 26 .06
SIO | 1 | 2.9 -5.6 .1 -94 -52 -74 .26
COD | 2 | .1 .1 -1.4 -16 25 -27 .29
EMR | 2 | 5.2 -10.1 7.4 -52 -30 -32 .53
ESA | 2 | -1.2 -3.4 2.3 50 4 -29 .33
GFZ | 2 | .0 -.6 -1.2 -13 -35 -11 .15
GRG | 2 | 8.3 -3.0 30.1 -20 30 -43 .44
JPL | 2 | -.5 .1 9.5 -41 106 -33 .56
MIT | 2 | 3.8 -4.8 14.9 -7 7 -44 .38
NGS | 2 | 2.7 -1.7 22.6 -96 -44 10 .56
SIO | 2 | 2.6 -4.5 9.2 -45 -21 -102 .36
COD | 3 | .1 -.2 -.9 -32 24 -24 .38
EMR | 3 | .6 -1.0 6.8 -38 -28 -36 .35
ESA | 3 | 4.0 -4.9 -3.0 49 12 -36 .31
GFZ | 3 | .1 -.9 -.8 -21 -27 -20 .18
GRG | 3 | 8.2 -5.8 22.3 -16 10 -10 .30
JPL | 3 | -.9 4.3 15.1 -46 58 -20 .57
MIT | 3 | 6.2 -2.3 10.3 -33 -24 -47 .44
NGS | 3 | .1 -9.2 25.4 -193 -32 -32 .27
SIO | 3 | 4.5 -2.8 10.5 -19 -24 -31 .37
COD | 4 | -.4 -.4 -1.1 -30 41 -37 .25
EMR | 4 | 4.6 2.0 6.8 -40 -25 -41 .38
ESA | 4 | .9 -3.7 -1.3 45 18 -42 .28
GFZ | 4 | -.3 -.7 -1.5 -7 -32 -17 .37
GRG | 4 | 7.8 -2.4 27.1 -4 23 -39 .50
JPL | 4 | -1.3 1.9 19.0 -67 62 -4 .50
MIT | 4 | 5.4 .6 15.7 -29 -13 -55 .33
NGS | 4 | .1 -3.8 22.2 -126 -35 -8 .45
SIO | 4 | 5.1 -1.9 24.5 40 -5 87 .19
COD | 5 | .2 .6 -1.1 -24 23 -47 .27
EMR | 5 | .2 -2.0 8.1 -46 -22 -29 .32
ESA | 5 | -.5 -3.8 4.6 42 16 -52 .20
GFZ | 5 | .1 -.3 -1.3 -6 -29 -2 .01
GRG | 5 | 4.3 -9.8 15.8 -31 31 -29 .66
JPL | 5 | 2.1 -5.1 5.1 -75 1 -10 .62
MIT | 5 | 4.5 -2.8 16.6 -28 -11 -51 .23
NGS | 5 | 2.5 -1.7 25.0 -115 -70 14 .46
SIO | 5 | 5.7 -.3 6.8 47 -73 180 .09
COD | 6 | .7 -.4 -.9 -34 23 -54 .15
EMR | 6 | -3.4 -2.7 16.7 -32 -27 -13 .24
ESA | 6 | 4.1 -7.1 -1.7 25 -13 -51 .36
GFZ | 6 | -.1 -.7 -1.0 4 -13 -10 -.18
GRG | 6 | -1.2 -9.8 18.6 -23 21 -17 .46
JPL | 6 | 3.9 -7.7 19.3 51 72 -8 .39
MIT | 6 | 4.0 -5.4 17.1 -33 -25 -47 .36
NGS | 6 | .1 -5.5 18.3 -119 -34 0 .29
SIO | 6 | 7.3 -2.9 13.7 27 -72 250 .17
11. 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.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1745.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1745.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 2.1745.[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 3.1745.[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 5.1745.0-6). 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 1745 summary. (Jun 16, 2013 - Jun 22, 2013)
Table 1.1745.a GPS week: 1745 MJD: 56459.000-56465.000
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 272| 0 0 -7 17 36 5 -.40 10 10 | -1051 -282 17 86
| 1 0 1 8 17 9 .03 | 132 327
emr 79| 0 -3 -1 -11 -22 5 .38 14 14 | 3558 -490 15 100
| 1 1 0 23 21 14 .03 | 1240 507
esa 150| 1 0 0 16 33 -11 .10 5 5 | 56 -1876 15 123
| 0 0 0 24 15 12 .02 | 482 539
gfz 201| -1 0 0 -28 -55 7 -.47 9 8 | 75 -197 12 76
| 0 0 0 63 49 14 .03 | 164 540
grg 141| 2 0 13 0 10 24 .77 14 13 | 18 -213 21 149
| 0 0 2 20 13 19 .08 | 95 308
igr n/a| 0 0 -3 9 20 5 -.22 6 5 | 1873 -779 14 70
| 0 0 0 16 18 12 .01 | 1718 633
jpl 80| -1 1 -5 8 -38 -32 .36 14 13 | 3106 -455 16 103
| 1 1 2 60 30 22 .02 | 1188 623
mit 236| 0 0 -1 -1 12 3 -.58 12 10 | 59 -191 25 200
| 0 0 0 43 30 15 .02 | 134 399
ngs 242| 0 0 2 -37 -49 0 .35 14 10 | -1065 -293 1578 3181
| 0 1 2 58 32 20 .03 | 129 341
sio 429| 1 2 -6 -14 -64 24 -.56 20 19 | --- --- --- ---
| 1 1 0 64 50 161 .08 | --- ---
Table 1.1745.b GPS week : 1745 MJD: 56459.000-56465.000
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 4 3 |
2 | 5 4 4 4 4 4 4 |
3 | 3 4 4 4 4 5 5 |
4 | 4 3 3 3 3 3 3 |
5 | 4 5 4 4 4 5 5 |
6 | 3 3 3 3 4 4 4 |
7 | 4 3 4 4 3 4 4 |
8 | 3 3 3 3 3 3 3 |
9 | 4 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 3 3 3 3 4 4 4 |
12 | 5 5 5 5 5 6 6 |
13 | 4 4 4 4 3 3 4 |
14 | 5 4 4 3 4 4 4 |
15 | 5 5 5 5 6 6 6 |
16 | 5 4 4 5 4 5 5 |
17 | 4 4 4 4 4 4 5 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 5 5 |
20 | 4 4 3 4 4 4 4 |
21 | 3 3 4 4 3 4 4 |
22 | 4 4 4 3 4 4 4 |
23 | 4 3 4 4 4 4 3 |
24 | 5 4 4 4 4 4 3 |
25 | 4 4 4 4 4 5 4 |
26 | 6 7 8 11 8 9 7 |
27 | 0 0 0 0 0 0 0 |
28 | 3 3 4 4 3 4 4 |
29 | 5 4 4 5 6 6 6 |
30 | 0 0 0 0 0 0 0 |
31 | 4 4 4 4 3 4 4 |
32 | 3 3 3 3 4 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 2.1745.0 GPS week: 1745 Day: 0 MJD: 56459.000
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 276| -1 0 -5 12 51 15 -.42 9 9 | -1334 155 17 88
emr 79| 3 -2 -1 -13 -30 0 .35 14 14 | 4889 -699 11 103
esa 150| 0 0 1 10 18 -7 .12 5 5 | -309 -1697 12 126
gfz 204| 0 0 0 -23 -25 5 -.46 9 8 | 178 -827 11 77
grg 142| 2 0 12 -21 26 -4 .69 14 12 | -3 -216 28 176
igr n/a| 0 0 -4 26 33 -11 -.20 5 5 | 3627 -1028 14 71
jpl 80| 1 2 -3 9 -61 -51 .39 13 12 | 4191 -858 14 104
mit 236| -1 -1 -1 3 -4 28 -.59 12 10 | 153 -457 23 194
ngs 244| -1 1 0 -4 -21 0 .32 12 10 | -1311 83 1578 2949
sio 438| 0 0 -7 -107 -154 -193 -.45 20 18 | --- --- --- ---
Table 2.1745.1 GPS week: 1745 Day: 1 MJD: 56460.000
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 273| -1 1 -7 7 11 -11 -.35 9 9 | -944 -203 18 81
emr 80| 2 -2 0 -17 -63 7 .34 14 14 | 4278 239 12 92
esa 150| 0 0 1 18 6 6 .11 5 5 | -299 -1761 14 119
gfz 205| 0 0 0 36 32 1 -.42 8 7 | -128 -467 12 71
grg 144| 1 0 15 16 -7 -2 .71 14 12 | 48 -494 20 139
igr n/a| 0 0 -2 19 10 -1 -.20 5 5 | 2752 414 14 81
jpl 80| 0 2 -5 13 -53 -33 .35 13 12 | 3439 552 16 100
mit 236| 0 0 -1 -16 64 14 -.56 10 9 | 86 -483 22 219
ngs 246| 0 -2 -1 -145 -80 -31 .37 14 10 | -1090 -58 1584 3122
sio 428| 0 2 -6 -81 -44 -53 -.47 19 17 | --- --- --- ---
Table 2.1745.2 GPS week: 1745 Day: 2 MJD: 56461.000
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 273| -1 1 -6 16 36 7 -.37 10 10 | -1056 -350 15 119
emr 80| 0 -5 -1 -36 -28 -1 .39 16 16 | 4854 -1331 13 95
esa 150| 0 0 0 -13 48 -23 .10 5 4 | 926 -2914 16 109
gfz 200| -1 0 0 4 -65 40 -.47 10 9 | 286 -638 13 72
grg 143| 2 0 10 28 8 28 .71 14 12 | 188 -629 17 132
igr n/a| 0 1 -4 -6 4 0 -.23 7 5 | 3662 -1614 15 73
jpl 80| -1 0 -4 -34 -9 4 .39 14 13 | 4445 -1204 17 100
mit 237| 0 0 -1 75 -31 8 -.59 11 10 | 234 -493 32 198
ngs 244| 0 0 4 -35 -83 -10 .35 17 11 | -1087 -357 1715 3050
sio 430| 0 1 -6 16 -87 -104 -.53 18 20 | --- --- --- ---
Table 2.1745.3 GPS week: 1745 Day: 3 MJD: 56462.000
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 274| -1 1 -9 28 29 9 -.41 11 10 | -945 -905 14 77
emr 80| 0 -3 0 37 -19 8 .41 14 14 | 3546 -644 14 101
esa 150| 1 0 0 62 33 -12 .08 5 5 | -158 -1727 16 142
gfz 202| 0 -1 2 -154 -50 1 -.47 10 9 | 109 -395 13 82
grg 143| 2 0 10 -28 -1 40 .75 13 12 | -56 -347 17 138
igr n/a| 0 1 -2 29 22 0 -.22 6 5 | 2130 -966 16 77
jpl 80| -3 0 -5 4 -28 -34 .36 14 12 | 3336 -514 16 107
mit 236| 0 1 0 -61 32 -4 -.60 12 10 | 141 -526 22 193
ngs 244| 0 -1 2 13 -62 -2 .33 15 10 | -928 -984 1801 3526
sio 431| 3 3 -5 -48 -15 -25 -.64 20 19 | --- --- --- ---
Table 2.1745.4 GPS week: 1745 Day: 4 MJD: 56463.000
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 274| 0 0 -9 21 21 6 -.40 11 10 | -1034 -240 18 90
emr 80| 0 -2 -1 -9 -12 25 .39 15 15 | 3467 -652 19 116
esa 150| 0 0 0 20 36 -19 .10 5 5 | 469 -2152 16 108
gfz 202| -1 0 0 -62 -63 1 -.47 9 8 | 177 43 13 84
grg 142| 1 1 17 -6 18 32 .82 15 13 | -118 281 20 159
igr n/a| -1 1 -3 -3 -7 17 -.20 6 5 | 1764 -1105 14 65
jpl 80| -1 1 -8 -45 -24 -28 .35 15 13 | 3370 -1011 15 95
mit 237| 1 0 0 26 11 -7 -.59 12 10 | -108 298 21 174
ngs 243| -1 0 4 15 -43 5 .34 16 8 | -1069 -242 1575 3485
sio 425| 1 3 -6 59 -5 108 -.56 19 19 | --- --- --- ---
Table 2.1745.5 GPS week: 1745 Day: 5 MJD: 56464.000
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 270| 0 0 -6 26 39 0 -.41 11 10 | -1009 -366 19 67
emr 80| 0 -2 0 -15 -6 15 .38 15 15 | 1915 -91 18 106
esa 150| 1 0 0 20 40 -25 .08 6 6 | -345 -1169 16 137
gfz 197| -1 0 0 -9 -90 0 -.49 9 8 | -160 727 13 74
grg 140| 2 0 15 11 24 34 .85 15 14 | 50 -21 25 145
igr n/a| -1 0 -3 -12 26 24 -.21 6 5 | -122 -614 14 66
jpl 80| -2 3 -7 -23 -89 -65 .34 16 16 | 1508 -88 19 105
mit 237| 1 0 0 -23 23 4 -.60 13 11 | 29 -73 24 196
ngs 236| -2 0 2 -23 5 36 .35 13 9 | -1046 -334 1487 2955
sio 421| 2 4 -7 36 -73 190 -.63 21 19 | --- --- --- ---
Table 2.1745.6 GPS week: 1745 Day: 6 MJD: 56465.000
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 269| 0 1 -6 10 62 12 -.44 11 11 | -1035 -70 18 81
emr 80| -1 -4 0 -23 4 -19 .40 14 14 | 1960 -256 18 91
esa 150| 1 0 0 -6 50 4 .08 5 5 | 111 -1713 15 125
gfz 199| -2 0 0 8 -122 3 -.51 10 10 | 64 176 12 75
grg 138| 2 0 14 1 6 43 .89 15 13 | 20 -66 26 154
igr n/a| 0 0 -2 15 49 11 -.24 5 5 | -700 -541 16 60
jpl 80| -1 0 -3 135 -6 -18 .34 15 14 | 1458 -66 17 113
mit 237| 0 0 -2 -16 -5 -17 -.56 12 11 | -120 397 31 232
ngs 239| 0 0 4 -86 -59 0 .40 14 11 | -924 -159 1312 3185
sio 431| 0 4 -7 26 -72 248 -.61 20 18 | --- --- --- ---
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 3.1745.0 GPS week: 1745 Day: 0 MJD: 56459.000
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 10 5 5 7 6 16 9 10 25 3 | 38 46 45 43 52 39 50 43 42 35 42
2 | 7 12 8 19 10 6 9 15 10 20 4 | 21 25 27 37 27 24 26 30 26 22 23
3 | 9 12 4 7 11 5 12 8 9 21 3 | 29 36 28 29 33 28 35 26 35 30 29
4 | 8 11 5 10 9 5 8 12 11 14 3 | 24 30 32 35 37 29 31 36 35 29 30
5 | 13 15 6 7 11 6 14 13 7 21 4 | 45 49 41 38 42 41 49 41 40 44 41
6 | 8 9 4 7 7 3 11 7 9 19 2 | 16 25 15 14 21 15 24 14 23 16 15
7 | 10 12 5 7 15 5 13 9 8 26 3 | 33 28 25 26 31 25 30 24 30 32 25
8 | 8 7 4 6 12 3 10 7 9 24 3 | 23 25 22 25 22 23 29 23 28 28 23
9 | 10 8 5 6 10 4 10 14 11 34 3 | 25 27 26 25 26 26 29 29 26 36 25
10 | 7 7 3 6 11 5 6 10 10 15 2 | 11 18 14 14 22 12 19 17 19 20 14
11 | 6 12 4 4 11 3 10 9 9 13 3 | 59 67 63 62 73 63 65 62 65 59 63
12 | 10 25 6 15 17 6 17 11 12 18 5 | 20 37 21 21 32 18 30 19 27 20 20
13E | 7 13 5 6 16 6 11 13 11 19 3 | 38 39 36 36 45 35 41 40 41 37 37
14E | 10 12 5 7 19 4 12 23 14 27 4 | 22 24 23 20 23 20 22 30 29 26 21
15E | 8 20 6 10 19 5 18 15 12 11 4 | 16 23 16 17 21 15 22 18 21 21 15
16 | 10 20 5 12 15 6 13 12 13 18 4 | 25 33 21 16 28 22 29 17 24 19 20
17 | 8 13 5 8 17 3 15 8 10 13 3 | 18 25 20 25 35 20 25 20 30 17 21
18 | 8 15 7 9 15 5 13 8 12 23 4 | 14 22 15 18 23 13 19 17 14 17 11
19 | 6 12 5 9 17 4 13 11 9 19 3 | 15 24 15 21 32 17 24 14 25 17 17
20 | 9 13 4 10 11 4 12 11 8 20 3 | 19 21 19 24 27 21 21 23 19 17 19
21 | 8 10 5 6 14 4 11 6 11 26 3 | 19 26 25 23 34 22 27 22 21 20 23
22 | 10 12 5 7 13 3 12 9 12 27 3 | 20 25 22 24 35 22 24 23 23 31 21
23E | 9 13 3 9 12 5 10 11 9 15 3 | 22 22 19 18 25 17 23 20 23 20 18
24 | 11 13 6 8 18 5 13 21 10 10 4 | 29 27 23 26 28 21 30 17 26 24 22
25 | 8 14 6 6 17 4 15 11 13 13 4 | 22 30 22 22 30 20 27 20 25 20 21
26E | 14 20 10 13 14 9 18 17 29 17 6 | 82 76 80 80 77 78 78 86 78 82 78
X27 | 8 --- --- --- --- 33 --- --- --- --- 0 | 98 --- --- --- --- 99 --- --- --- --- 100
28 | 6 12 6 7 16 4 11 6 8 13 3 | 23 31 22 21 34 22 28 20 29 21 23
29 | 14 18 4 8 13 4 16 13 11 20 4 | 26 23 19 21 25 16 23 20 20 19 18
X30 | 8 --- --- --- --- 63 --- --- --- --- 0 | 49 --- --- --- --- 26 --- --- --- --- 49
31 | 13 12 7 7 17 6 11 11 12 19 4 | 25 28 22 23 38 24 28 20 26 18 22
32 | 8 6 3 6 11 5 7 12 8 16 2 | 12 18 12 11 19 10 18 11 15 14 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 5 9 14 5 13 12 12 20 |T 29 31 26 27 33 27 30 26 29 27 28
WRMS | 9 14 5 8 12 5 12 10 10 18 |NE 28 29 24 25 32 26 29 24 27 24 27
MEDI | 8 12 5 7 13 5 12 11 10 19 |MD 23 26 22 23 30 22 27 20 26 21 22
Table 3.1745.1 GPS week: 1745 Day: 1 MJD: 56460.000
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 7 3 7 9 5 14 10 11 23 3 | 25 33 28 26 36 24 38 26 24 21 26
2 | 9 11 6 13 10 4 10 13 12 21 3 | 20 18 19 20 22 16 21 20 22 15 16
3 | 9 12 7 9 12 5 11 8 11 22 3 | 23 30 26 23 31 22 30 18 30 23 24
4 | 8 8 4 5 6 3 7 11 14 16 3 | 21 24 25 21 28 21 28 25 25 23 22
5 | 13 17 5 10 13 5 17 10 16 19 4 | 24 31 23 25 32 23 32 23 27 26 23
6 | 9 11 5 8 12 4 10 8 12 19 3 | 13 19 14 13 21 9 19 10 20 16 11
7 | 9 12 3 7 13 5 11 6 12 23 3 | 19 25 18 17 28 15 25 17 25 27 17
8 | 8 10 4 6 11 4 8 7 9 24 2 | 16 22 16 16 17 15 23 17 20 24 15
9 | 8 10 5 7 9 6 8 8 14 33 3 | 19 20 20 20 19 18 24 20 22 32 18
10 | 6 9 4 6 10 4 7 7 13 9 2 | 14 18 15 14 21 13 20 14 17 16 14
11 | 7 11 4 5 12 5 11 9 12 13 3 | 36 45 40 40 48 39 44 40 36 38 39
12 | 9 22 6 12 16 7 17 8 10 15 4 | 20 30 20 19 27 18 28 17 25 19 18
13E | 9 11 4 7 12 5 13 12 10 20 3 | 25 27 25 19 26 23 26 27 27 25 23
14E | 10 12 5 7 14 4 11 13 15 19 3 | 24 25 23 22 25 20 26 25 25 22 21
15E | 9 18 4 11 13 4 19 13 13 9 4 | 18 25 16 19 22 18 26 22 26 22 17
16 | 8 17 5 9 16 6 14 9 14 22 4 | 13 24 17 15 23 14 24 13 26 18 15
17 | 6 16 4 8 16 3 16 8 14 14 4 | 16 19 14 15 31 13 23 13 22 14 14
18 | 9 14 6 8 15 4 14 9 11 23 3 | 18 21 13 19 23 15 24 17 17 14 13
19 | 6 12 4 9 18 4 13 9 9 18 3 | 7 21 14 14 30 11 22 12 19 15 12
20 | 8 13 4 9 11 4 11 8 13 20 3 | 18 19 15 18 20 15 21 19 16 15 14
21 | 6 10 3 5 13 2 9 8 14 25 3 | 16 21 19 18 25 15 22 17 23 13 17
22 | 9 14 6 8 16 5 12 8 10 23 3 | 19 22 16 20 29 17 23 18 15 23 16
23E | 8 15 3 10 9 4 10 9 10 14 3 | 18 22 14 14 22 13 22 14 21 16 14
24 | 14 14 3 8 13 6 12 11 8 13 3 | 15 21 16 13 24 13 25 12 21 14 13
25 | 10 15 5 6 21 5 14 10 12 12 4 | 20 25 18 19 25 16 25 16 22 16 17
26E | 18 25 10 15 14 13 20 17 39 18 7 | 61 55 61 61 58 58 58 60 74 61 58
X27 | 7 --- --- --- --- 25 --- --- --- --- 0 | 115 --- --- --- --- 117 --- --- --- --- 114
28 | 8 12 4 6 14 5 9 7 13 11 3 | 16 23 17 16 28 14 24 13 23 16 16
29 | 13 16 4 8 15 3 15 11 8 17 4 | 18 21 16 18 27 15 21 16 20 16 15
X30 | 7 --- --- --- --- 78 --- --- --- --- 0 | 38 --- --- --- --- 25 --- --- --- --- 39
31 | 8 12 4 8 19 5 10 9 18 18 3 | 17 26 19 18 37 18 27 16 26 16 18
32 | 9 7 3 6 14 4 6 9 7 13 2 | 17 19 13 13 21 12 21 14 18 14 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 5 8 14 5 13 10 14 19 |T 23 25 20 20 27 21 26 19 24 21 22
WRMS | 9 14 5 7 12 5 12 9 10 17 |NE 22 23 18 18 26 20 25 17 22 19 21
MEDI | 8 12 4 8 13 5 11 9 12 18 |MD 18 22 17 18 25 16 24 17 22 16 17
Table 3.1745.2 GPS week: 1745 Day: 2 MJD: 56461.000
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 9 4 6 7 5 15 10 12 20 3 | 31 37 34 32 41 30 44 33 35 27 33
2 | 6 13 6 14 11 5 12 13 10 20 3 | 17 24 23 24 22 17 23 21 25 15 19
3 | 10 18 4 9 11 6 12 8 14 19 3 | 26 34 27 22 30 23 31 21 26 26 25
4 | 5 10 5 8 9 7 7 11 11 17 3 | 22 27 27 27 30 21 29 25 31 18 25
5 | 13 20 4 9 10 7 16 11 13 20 4 | 35 44 36 27 37 34 39 32 31 37 33
6 | 8 12 4 8 10 6 13 7 14 16 3 | 17 25 18 13 24 14 24 15 20 16 16
7 | 12 13 4 10 16 5 16 7 10 24 4 | 31 25 24 25 32 22 25 20 25 28 22
8 | 8 10 3 8 12 3 9 7 8 25 2 | 22 21 23 22 23 22 24 21 20 26 21
9 | 7 13 3 7 10 4 9 9 11 33 3 | 26 23 24 22 25 22 26 23 21 34 22
10 | 7 8 4 9 11 5 11 9 9 11 3 | 13 17 18 14 19 14 17 15 18 17 14
11 | 6 12 3 9 11 5 11 10 13 13 3 | 47 51 50 47 58 49 53 49 50 46 49
12 | 10 27 6 16 16 8 18 9 9 15 5 | 20 32 21 20 32 17 26 16 22 20 18
13E | 7 11 5 10 10 4 13 20 9 18 4 | 39 37 39 42 35 38 39 39 35 37 37
14E | 7 14 5 8 14 5 15 8 9 13 3 | 20 26 25 20 31 19 24 20 26 17 21
15E | 9 23 4 12 12 6 18 13 14 11 4 | 19 25 18 17 21 15 23 16 17 21 15
16 | 9 21 5 13 13 6 15 11 12 15 4 | 22 33 25 15 28 18 27 18 25 18 21
17 | 9 16 4 11 14 4 18 9 12 13 4 | 13 23 22 18 32 17 24 17 28 15 18
18 | 9 18 5 10 11 5 15 7 13 22 4 | 17 24 17 19 20 18 22 15 14 14 14
19 | 7 14 5 11 14 5 13 12 13 17 3 | 17 24 21 17 30 16 23 16 22 19 18
20 | 7 13 4 9 10 4 13 9 10 21 3 | 17 18 18 19 19 16 17 20 19 15 16
21 | 7 15 3 6 18 6 11 9 17 25 3 | 24 31 26 23 34 22 26 20 21 18 23
22 | 9 15 5 8 13 4 14 6 17 18 3 | 18 25 22 20 29 20 25 18 19 21 19
23E | 6 15 3 10 13 4 12 11 10 13 3 | 24 26 23 20 24 20 23 22 23 22 21
24 | 14 13 4 10 15 7 14 11 10 9 4 | 18 23 21 15 31 20 28 18 24 17 18
25 | 8 17 5 9 18 6 13 10 9 9 4 | 25 31 24 20 34 21 26 20 25 20 22
26E | 22 26 10 12 25 28 25 26 68 23 8 | 84 80 77 78 79 81 79 86 92 84 78
X27 | 7 --- --- --- --- 31 --- --- --- --- 0 | 87 --- --- --- --- 84 --- --- --- --- 89
28 | 7 12 4 10 19 3 15 10 12 15 4 | 25 29 26 20 36 22 29 20 28 26 24
29 | 12 20 4 8 13 6 17 8 11 15 4 | 25 25 20 19 23 18 23 19 22 17 18
X30 | 7 --- --- --- --- 75 --- --- --- --- 0 | 47 --- --- --- --- 42 --- --- --- --- 49
31 | 9 12 5 6 19 4 13 8 19 18 4 | 22 32 26 20 40 23 27 22 32 20 24
32 | 8 8 4 9 9 3 7 12 12 16 3 | 14 18 17 14 20 12 20 12 17 13 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 5 10 14 7 14 11 17 18 |T 27 29 26 23 31 25 28 23 27 24 26
WRMS | 10 16 4 9 12 5 13 10 11 20 |NE 25 27 24 21 29 24 26 21 24 21 25
MEDI | 8 13 4 9 12 5 13 9 12 17 |MD 22 25 23 20 30 20 25 20 24 20 21
Table 3.1745.3 GPS week: 1745 Day: 3 MJD: 56462.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 14 7 4 8 9 4 16 12 8 20 3 | 30 39 37 33 45 34 44 34 36 31 35
2 | 8 12 6 15 10 5 11 9 9 20 3 | 25 28 27 29 27 24 28 26 32 21 24
3 | 8 11 5 11 12 8 12 13 12 21 3 | 33 41 36 36 39 33 39 32 42 38 35
4 | 9 9 4 8 8 5 8 10 10 17 3 | 27 36 33 30 39 31 35 33 40 28 31
5 | 12 16 6 7 12 6 16 10 13 21 4 | 40 45 36 33 41 33 45 34 39 38 36
6 | 7 11 4 10 8 6 13 8 10 19 3 | 17 27 18 14 22 15 25 13 26 19 16
7 | 6 13 4 12 13 4 15 7 10 21 3 | 28 31 26 26 33 24 28 22 35 31 25
8 | 11 7 4 9 14 5 8 10 7 25 3 | 26 30 27 28 28 28 31 24 37 30 26
9 | 9 9 4 9 11 5 10 8 7 34 3 | 25 31 26 24 26 24 28 23 36 34 25
10 | 10 7 4 7 11 4 7 9 10 9 3 | 15 20 15 15 22 17 21 19 24 19 15
11 | 8 13 4 8 13 4 9 11 9 14 3 | 46 58 51 52 62 51 54 52 54 49 51
12 | 9 22 6 13 14 8 19 11 13 13 5 | 23 34 23 22 31 19 30 20 33 24 21
13E | 10 10 5 11 10 5 12 12 9 15 3 | 31 28 23 21 27 25 28 28 32 23 23
14E | 8 11 4 5 11 5 11 8 11 14 3 | 27 32 27 21 32 26 31 22 36 22 25
15E | 12 18 6 11 12 5 23 16 15 12 5 | 21 26 19 16 24 16 27 18 26 22 16
16 | 9 22 5 11 14 6 13 11 12 17 4 | 23 35 22 15 28 18 29 17 32 19 20
17 | 8 14 5 9 17 5 18 10 10 13 4 | 18 25 18 16 33 17 24 13 29 12 17
18 | 9 13 6 11 11 4 12 7 11 20 3 | 18 24 18 22 23 17 22 18 26 16 16
19 | 7 12 5 11 16 5 14 14 13 17 4 | 14 25 16 17 31 14 23 15 27 14 15
20 | 9 13 5 12 12 5 13 7 8 21 3 | 22 28 22 22 26 22 27 23 31 19 21
21 | 9 11 4 4 14 4 10 9 15 27 3 | 25 30 24 25 30 23 28 23 37 21 25
22 | 9 12 5 9 12 3 10 6 10 15 3 | 25 29 25 27 33 24 27 24 31 24 24
23E | 10 12 4 11 14 3 13 7 7 13 3 | 24 23 21 16 21 18 25 17 25 18 18
24 | 10 12 5 9 12 7 12 11 9 12 3 | 16 25 16 15 26 13 25 15 26 16 15
25 | 6 13 4 8 16 7 14 14 9 14 3 | 21 31 23 24 29 21 29 26 28 27 22
26E | 35 24 11 10 20 19 20 36 57 49 10 | 76 69 62 56 63 69 66 68 91 71 62
X27 | 8 --- --- --- --- 25 --- --- --- --- 0 | 101 --- --- --- --- 105 --- --- --- --- 103
28 | 11 12 4 12 15 5 12 10 10 12 3 | 25 31 25 19 30 24 27 19 39 18 23
29 | 15 20 5 9 15 3 18 13 11 13 4 | 29 25 20 21 26 20 26 21 27 18 19
X30 | 8 --- --- --- --- 59 --- --- --- --- 0 | 37 --- --- --- --- 29 --- --- --- --- 36
31 | 9 12 6 6 14 6 12 7 11 19 3 | 28 31 25 20 39 25 29 21 37 17 24
32 | 8 8 4 7 11 6 7 9 11 18 3 | 19 24 17 14 23 15 25 15 30 11 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 5 10 13 6 14 12 15 20 |T 29 32 25 24 31 27 30 24 34 25 27
WRMS | 10 14 5 9 12 5 12 10 10 19 |NE 27 30 24 23 31 26 29 22 33 23 27
MEDI | 9 12 5 9 12 5 12 10 10 17 |MD 25 30 23 22 29 24 28 22 32 21 23
Table 3.1745.4 GPS week: 1745 Day: 4 MJD: 56463.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 7 4 7 12 5 17 10 7 22 3 | 24 36 33 31 45 27 39 29 33 26 31
2 | 10 8 5 15 8 3 11 10 7 20 3 | 17 23 22 25 28 20 23 25 24 18 20
3 | 9 14 5 9 21 7 14 10 8 23 4 | 37 46 38 39 49 36 44 36 43 40 38
4 | 9 6 4 6 9 5 11 8 8 17 2 | 18 28 24 23 33 22 26 25 27 23 23
5 | 14 16 5 7 11 6 18 10 12 21 4 | 32 41 34 34 37 33 45 32 35 36 34
6 | 8 11 4 8 12 6 13 8 12 21 3 | 19 23 19 16 26 14 26 19 23 23 17
7 | 9 12 4 7 13 4 14 7 9 22 3 | 26 26 20 19 30 19 25 20 29 27 20
8 | 9 8 3 7 16 2 8 8 10 24 3 | 18 21 20 19 21 18 23 19 25 24 18
9 | 8 11 5 6 13 4 9 8 7 32 3 | 19 23 21 19 21 21 24 20 27 33 19
10 | 9 6 3 5 12 5 10 8 7 13 2 | 13 19 16 17 27 15 18 19 21 21 16
11 | 9 12 5 8 16 5 10 13 8 13 3 | 40 47 43 44 58 42 43 41 46 41 43
12 | 10 24 6 14 12 6 20 13 14 14 5 | 16 32 18 19 27 16 29 20 28 19 18
13E | 7 11 4 5 12 6 13 9 8 12 3 | 24 23 22 22 24 21 25 23 28 24 22
14E | 9 10 5 7 14 4 14 11 11 12 3 | 19 22 19 21 26 19 22 21 23 22 19
15E | 11 24 6 11 16 5 25 25 13 17 6 | 21 31 23 26 29 22 32 34 27 32 24
16 | 8 20 4 10 14 5 13 12 9 19 4 | 16 28 20 15 26 18 25 17 25 15 17
17 | 10 15 5 7 20 5 22 6 7 14 4 | 15 24 18 20 36 16 26 16 26 15 18
18 | 9 16 7 9 11 6 13 8 12 17 3 | 19 24 13 21 26 17 21 18 20 12 14
19 | 9 13 4 9 19 5 11 13 6 15 3 | 13 22 15 14 34 13 21 15 22 14 14
20 | 10 13 5 12 14 4 12 6 7 21 3 | 17 20 19 20 26 17 21 20 19 16 17
21 | 10 12 3 4 12 5 13 9 9 27 3 | 20 26 21 22 31 22 24 24 24 17 21
22 | 9 13 5 7 12 5 13 9 11 17 3 | 25 27 21 26 35 24 22 25 25 27 22
23E | 8 12 4 10 19 5 12 9 10 14 3 | 23 24 20 17 24 18 25 19 27 19 19
24 | 13 13 4 5 13 4 15 12 9 16 3 | 16 21 17 14 24 14 24 17 22 18 14
25 | 5 16 4 5 15 7 14 18 11 10 4 | 13 26 16 14 24 16 24 24 22 17 15
26E | 22 31 12 9 21 22 22 27 72 35 8 | 136 132 133 133 134 131 134 134 137 134 131
X27 | 8 --- --- --- --- 42 --- --- --- --- 0 | 94 --- --- --- --- 82 --- --- --- --- 96
28 | 7 13 4 10 14 4 12 8 8 12 3 | 17 27 18 16 30 16 24 19 27 18 18
29 | 18 22 6 9 17 4 24 17 15 13 5 | 24 25 17 17 30 15 28 26 24 20 17
X30 | 8 --- --- --- --- 34 --- --- --- --- 0 | 32 --- --- --- --- 18 --- --- --- --- 32
31 | 10 12 4 8 13 4 11 7 8 18 3 | 20 26 19 17 33 18 25 17 25 16 18
32 | 9 8 5 14 16 4 6 7 7 20 3 | 15 19 16 18 26 13 20 16 20 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 5 9 15 6 15 12 16 19 |T 26 30 25 25 34 25 30 26 30 26 26
WRMS | 10 15 5 8 13 5 13 10 8 19 |NE 23 26 20 20 30 21 26 21 25 21 23
MEDI | 9 12 4 8 13 5 13 9 9 17 |MD 19 25 20 19 28 18 25 20 25 20 19
Table 3.1745.5 GPS week: 1745 Day: 5 MJD: 56464.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 15 8 7 9 13 6 17 13 11 26 4 | 22 32 29 26 42 21 42 23 24 24 26
2 | 8 8 7 11 10 5 13 9 10 20 3 | 15 23 20 18 25 17 24 18 28 14 17
3E | 15 13 4 10 19 7 15 16 10 31 4 | 62 63 60 63 66 58 62 59 58 60 61
4 | 8 8 7 6 10 6 8 6 10 19 3 | 22 31 27 23 34 25 31 21 33 21 26
5 | 15 17 8 8 12 7 18 9 9 23 4 | 35 40 32 29 38 27 40 29 33 33 31
6 | 9 12 5 9 15 6 11 12 8 24 3 | 15 25 15 15 30 13 22 19 21 25 16
7 | 11 11 4 7 13 5 18 8 9 23 3 | 24 27 20 20 32 20 25 20 28 27 20
8 | 11 8 4 6 14 3 13 9 7 26 3 | 22 23 21 20 22 21 26 19 26 24 20
9 | 8 9 6 6 14 3 14 9 5 33 3 | 21 23 23 21 21 20 26 17 22 30 19
10 | 10 7 5 7 12 6 9 8 7 14 3 | 11 17 14 13 22 12 17 15 19 19 12
11 | 10 11 5 7 16 5 14 15 8 16 4 | 32 39 35 35 48 31 39 31 33 30 33
12 | 16 24 6 14 14 8 23 14 11 16 5 | 22 30 19 18 30 16 29 17 26 21 18
13E | 8 10 3 6 11 4 12 12 6 16 3 | 21 22 20 21 24 19 26 19 20 23 19
14E | 8 13 5 6 13 5 13 11 10 14 3 | 20 29 24 19 29 21 25 22 29 22 22
15E | 12 24 6 11 17 7 26 19 11 16 5 | 28 33 30 27 32 30 35 32 29 33 27
16 | 10 23 8 12 14 6 14 14 7 21 4 | 19 32 17 15 27 16 26 19 24 18 17
17 | 6 13 5 10 21 4 18 8 7 15 4 | 15 21 17 17 38 15 26 16 26 15 17
18 | 7 16 7 8 13 6 13 10 8 18 3 | 16 21 16 17 25 16 18 17 18 14 12
19 | 8 13 6 12 21 4 15 18 7 16 4 | 15 23 17 17 37 13 24 17 23 15 16
20 | 10 11 6 12 12 5 14 6 11 22 3 | 12 17 14 17 21 13 22 15 18 12 12
21 | 8 16 6 7 11 4 17 12 14 28 4 | 21 25 22 17 27 18 26 20 23 16 19
22 | 8 13 5 5 14 6 13 9 8 21 3 | 19 25 22 20 32 18 22 20 22 27 19
23E | 10 13 5 10 12 4 12 8 10 15 3 | 25 26 19 21 27 21 28 23 25 26 20
24 | 9 12 6 7 12 7 15 16 9 20 4 | 15 20 20 15 25 15 23 14 20 15 15
25 | 12 16 7 7 11 5 15 23 7 16 4 | 18 25 20 15 24 15 22 22 22 19 16
26E | 22 23 12 10 26 10 29 22 47 23 9 | 143 139 144 143 140 146 140 141 152 141 142
X27 | 8 --- --- --- --- 35 --- --- --- --- 0 | 85 --- --- --- --- 84 --- --- --- --- 86
28 | 7 12 4 7 13 4 13 12 9 14 3 | 20 27 19 18 30 17 26 20 30 19 19
29 | 15 26 6 11 19 6 19 20 12 18 5 | 18 25 16 17 30 14 24 22 23 19 14
X30 | 8 --- --- --- --- 39 --- --- --- --- 0 | 41 --- --- --- --- 20 --- --- --- --- 43
31 | 10 14 4 13 10 7 20 10 10 20 4 | 23 30 24 22 34 22 27 20 29 20 22
32 | 10 7 4 9 15 2 7 6 11 17 3 | 14 19 16 15 25 13 22 14 23 14 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 9 15 6 16 13 13 21 |T 27 31 26 25 34 25 31 25 30 26 27
WRMS | 10 15 6 8 14 5 16 11 9 19 |NE 22 25 20 19 29 20 26 19 24 20 22
MEDI | 10 13 6 8 13 6 14 11 9 19 |MD 21 25 20 18 30 18 26 20 24 21 19
Table 3.1745.6 GPS week: 1745 Day: 6 MJD: 56465.000
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 8 4 7 10 6 14 10 13 31 3 | 38 47 43 43 57 38 51 39 39 38 42
2 | 7 11 6 15 13 5 17 9 12 21 4 | 21 27 25 30 35 22 26 26 31 19 24
3E | 13 15 5 10 15 8 17 16 13 25 4 | 36 44 36 35 46 35 42 31 38 36 35
4 | 11 6 4 8 9 5 10 6 9 20 3 | 26 36 33 34 44 30 34 30 36 25 32
5 | 12 16 7 9 14 6 20 11 17 22 4 | 42 49 42 37 43 39 54 43 38 47 41
6 | 9 13 4 10 13 8 12 10 9 21 3 | 20 26 18 18 29 19 25 20 21 25 17
7 | 9 11 4 9 15 6 20 7 10 27 3 | 28 28 26 29 32 25 30 23 27 30 24
8 | 8 7 2 7 20 3 10 7 11 25 3 | 18 22 19 24 24 20 27 19 21 22 19
9 | 8 9 4 7 16 5 12 8 11 33 3 | 23 25 23 24 25 23 27 21 25 30 22
10 | 8 7 4 8 13 3 10 5 13 14 3 | 15 22 22 23 32 20 19 24 22 27 20
11 | 9 12 5 7 14 5 11 15 12 18 3 | 54 65 58 60 73 59 61 56 56 54 58
12 | 12 27 7 15 14 6 21 10 13 12 5 | 21 35 19 20 32 17 29 19 25 22 19
13E | 10 13 3 7 14 5 13 10 8 10 3 | 22 25 19 24 27 22 29 26 23 21 21
14E | 9 12 5 9 16 5 13 12 10 17 3 | 28 31 29 24 30 25 29 25 33 25 26
15E | 10 25 6 12 14 5 24 15 15 15 5 | 35 34 29 30 36 28 32 30 34 32 28
16 | 18 20 6 16 13 7 16 14 15 19 5 | 20 31 20 17 26 19 30 17 28 18 18
17 | 11 14 5 8 22 4 19 12 11 15 4 | 17 23 21 24 42 19 26 22 27 17 20
18 | 8 16 6 12 14 6 15 13 11 19 4 | 20 26 19 27 32 22 21 23 19 21 18
19 | 9 14 5 11 19 4 11 17 11 15 4 | 17 27 20 20 39 18 23 19 24 17 18
20 | 10 10 4 9 15 4 12 6 17 22 3 | 23 26 22 26 32 24 24 25 18 22 22
21 | 13 14 4 8 11 4 14 12 15 31 4 | 26 32 26 24 37 24 30 26 26 22 25
22 | 9 14 6 8 14 5 14 8 9 23 3 | 30 32 30 34 43 32 28 32 29 39 29
23E | 7 10 4 11 12 5 10 9 9 12 3 | 19 21 22 20 25 17 25 19 21 27 19
24 | 11 13 3 6 11 6 12 9 9 14 3 | 17 24 19 14 24 19 21 15 21 11 16
25 | 11 16 6 7 12 4 14 15 8 14 4 | 24 28 22 18 25 19 23 23 23 20 20
26E | 20 19 7 9 15 10 17 13 39 18 6 | 166 159 161 157 166 157 163 151 158 144 158
X27 | 8 --- --- --- --- 22 --- --- --- --- 0 | 95 --- --- --- --- 89 --- --- --- --- 99
28 | 8 11 2 8 16 5 14 16 13 17 4 | 23 25 21 20 29 19 27 27 25 25 20
29 | 16 22 7 11 19 5 21 19 14 17 5 | 25 26 19 18 28 17 24 24 20 21 18
X30 | 8 --- --- --- --- 60 --- --- --- --- 0 | 57 --- --- --- --- 24 --- --- --- --- 56
31 | 11 13 5 13 13 5 14 12 10 20 4 | 24 31 19 20 34 22 27 23 24 21 20
32 | 10 9 3 9 15 4 6 8 16 16 3 | 16 22 16 17 30 14 20 17 20 18 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 5 10 15 5 15 12 14 20 |T 32 34 29 30 39 30 34 29 31 29 31
WRMS | 11 14 5 10 13 5 14 11 11 18 |NE 28 30 25 25 35 26 29 25 26 25 28
MEDI | 10 13 5 9 14 5 14 10 11 18 |MD 23 27 22 24 32 22 27 24 25 22 21
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 4.1745 GPS week: 1745 MJD: 56459.0-56465.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 |U 8 7 22 |U 6 9 24 |U 8 7 20 |
emr | emr 2875 | 10 9 26 |U 8 15 25 | 9 8 25 |
esa | esa 2880 | 8 7 25 |U 6 10 22 | 8 7 21 |
gfz | gfz 2875 |U 8 7 24 |U 6 16 28 |U 8 7 21 |
grg | grg 2880 |U 11 10 36 |U 12 26 45 | 13 10 30 |
igr | igr 2879 | 8 7 25 | 6 9 20 | 9 8 21 |
igs | igs 2854 | 8 7 24 | 6 11 22 | 9 7 20 |
jpl | jpl 2874 | 10 8 27 | 8 16 27 | 10 9 27 |
mit | mit 2880 | 9 9 27 |U 8 21 33 |U 10 8 22 |
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 5.1745.0 GPS week: 1745 Day: 0 MJD: 56459.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3019 | 7 5 18 | 6 10 21 | 7 6 18 |
emr | emr 2876 | 9 8 25 | 7 16 26 | 6 5 25 |
esa | esa 2880 | 7 6 21 | 5 9 14 | 7 6 20 |
gfz | gfz 2876 | 7 5 20 | 7 23 32 | 7 5 18 |
grg | grg 2880 | 11 10 35 | 10 34 64 | 17 9 29 |
igr | igr 2880 | 7 6 21 | 5 8 14 | 6 5 19 |
igs | igs 2867 | 7 6 20 | 5 8 16 | 6 4 20 |
jpl | jpl 2876 | 8 6 23 | 7 20 29 | 10 9 45 |
mit | mit 2880 | 7 4 18 | 8 27 45 | 7 5 21 |
Table 5.1745.1 GPS week: 1745 Day: 1 MJD: 56460.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 6 6 25 | 4 9 25 | 10 6 19 |
emr | emr 2876 | 9 8 20 | 8 16 23 | 10 8 26 |
esa | esa 2880 | 7 7 23 | 6 8 21 | 10 8 21 |
gfz | gfz 2876 | 7 6 22 | 6 21 42 | 10 8 20 |
grg | grg 2880 | 11 13 40 | 11 27 52 | 16 9 36 |
igr | igr 2880 | 7 7 23 | 4 7 18 | 10 9 21 |
igs | igs 2853 | 7 6 21 | 5 7 22 | 10 8 21 |
jpl | jpl 2874 | 9 7 21 | 8 15 26 | 11 11 27 |
mit | mit 2880 | 6 6 20 | 9 26 48 | 13 8 23 |
Table 5.1745.2 GPS week: 1745 Day: 2 MJD: 56461.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 5 5 15 | 5 9 26 | 8 9 21 |
emr | emr 2876 | 7 6 20 | 7 19 28 | 10 11 28 |
esa | esa 2880 | 4 5 15 | 5 19 28 | 9 11 24 |
gfz | gfz 2876 | 5 5 16 | 5 21 30 | 9 12 25 |
grg | grg 2880 | 8 8 35 | 10 22 37 | 14 12 41 |
igr | igr 2877 | 4 5 15 | 6 18 26 | 9 12 27 |
igs | igs 2877 | 5 5 15 | 5 19 28 | 8 11 24 |
jpl | jpl 2876 | 9 9 22 | 7 21 33 | 9 12 27 |
mit | mit 2880 | 5 5 16 | 7 18 27 | 10 9 25 |
Table 5.1745.3 GPS week: 1745 Day: 3 MJD: 56462.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3003 | 10 8 25 | 6 8 25 | 9 7 25 |
emr | emr 2876 | 11 9 26 | 7 6 24 | 10 7 32 |
esa | esa 2880 | 9 9 28 | 6 7 22 | 9 6 28 |
gfz | gfz 2876 | 10 8 26 | 6 7 23 | 10 6 29 |
grg | grg 2880 | 13 12 39 | 10 23 32 | 13 10 22 |
igr | igr 2880 | 9 8 27 | 6 7 22 | 9 6 29 |
igs | igs 2879 | 10 8 27 | 6 6 21 | 9 6 29 |
jpl | jpl 2874 | 10 9 27 | 8 20 29 | 10 6 33 |
mit | mit 2880 | 9 10 26 | 7 18 29 | 11 9 28 |
Table 5.1745.4 GPS week: 1745 Day: 4 MJD: 56463.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3016 | 12 8 36 | 6 7 22 | 8 7 14 |
emr | emr 2876 | 15 12 46 | 8 14 17 | 8 8 20 |
esa | esa 2880 | 15 10 44 | 5 6 20 | 8 6 15 |
gfz | gfz 2876 | 14 10 43 | 5 8 20 | 8 6 16 |
grg | grg 2880 | 17 12 53 | 10 24 45 | 11 11 29 |
igr | igr 2880 | 15 10 44 | 5 6 20 | 8 7 16 |
igs | igs 2876 | 15 10 44 | 5 6 19 | 8 6 14 |
jpl | jpl 2876 | 15 10 47 | 5 8 18 | 8 6 18 |
mit | mit 2880 | 15 10 42 | 8 20 29 | 10 8 15 |
Table 5.1745.5 GPS week: 1745 Day: 5 MJD: 56464.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3051 | 7 6 16 | 7 12 21 | 8 6 18 |
emr | emr 2876 | 9 7 22 | 10 16 24 | 10 8 17 |
esa | esa 2880 | 6 4 20 | 8 11 21 | 8 6 16 |
gfz | gfz 2876 | 7 5 20 | 8 12 19 | 7 5 15 |
grg | grg 2880 | 7 7 27 | 19 19 39 | 10 12 28 |
igr | igr 2880 | 6 5 21 | 8 11 19 | 8 7 14 |
igs | igs 2846 | 6 5 19 | 8 14 21 | 8 7 15 |
jpl | jpl 2875 | 8 6 22 | 7 11 24 | 9 7 14 |
mit | mit 2880 | 6 4 18 | 8 15 23 | 10 8 19 |
Table 5.1745.6 GPS week: 1745 Day: 6 MJD: 56465.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 7 8 20 | 9 9 31 | 8 11 23 |
emr | emr 2875 | 10 12 25 | 11 18 34 | 11 8 26 |
esa | esa 2880 | 8 8 22 | 10 9 32 | 10 8 23 |
gfz | gfz 2873 | 7 8 22 | 8 21 28 | 9 9 25 |
grg | grg 2880 | 10 10 25 | 13 32 44 | 10 10 26 |
igr | igr 2876 | 7 9 22 | 8 8 24 | 10 9 23 |
igs | igs 2780 | 8 9 23 | 9 19 30 | 10 7 21 |
jpl | jpl 2872 | 8 9 27 | 14 16 32 | 10 9 25 |
mit | mit 2880 | 12 24 49 | 8 21 30 | 10 8 24 |
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 6.1745 GPS week: 1745 MJD: 56459.500-56465.500
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 | -53 -10 -52 60 5 | 2 15
| 10 17 89 29 4 | 2
emr uuuuu | 56 21 -85 87 17 | 24 30
| 14 22 87 86 10 | 2
esa uuuuu | -12 -26 71 55 2 | 9 17
| 13 6 26 25 2 | 3
gfz uuuuu | -11 20 -23 -98 -9 | 5 17
| 16 27 99 97 3 | 5
grg uuuux | 7 -19 77 -193 62 | 5 37
| 18 10 75 101 43 | 9
igr xxxxx | -1 1 -23 -17 -3 | -1 17
| 16 19 59 48 4 | 4
irf xxxxx | -11 6 -68 -57 -3 | 3 15
| 5 6 27 18 2 | 3
jpl uuuuu | 30 -19 75 -11 -4 | 18 24
| 27 55 76 41 8 | 5
mit uuuuu | -41 18 -161 -78 -4 | 22 27
| 15 26 106 35 4 | 3
ngs uuuuu | 86 58 23 71 -1 | 11 17
| 47 50 157 119 4 | 3
sio xxxxx | 62 24 169 126 -1 | 36 39
| 44 73 126 65 4 | 2
Table 7.1745.0 GPS week: 1745 Day: 0 MJD: 56459.500
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 | -59 -7 -41 114 2 | 3 16
emr uuuuu | 29 32 -80 -33 10 | 22 29
esa uuuuu | 8 -15 82 68 3 | 12 19
gfz uuuuu | -14 2 17 -50 -6 | 10 18
grg uuuux | -24 -20 113 -271 9 | 1 32
igr xxxxx | -1 -21 8 20 -8 | 3 17
irf xxxxx | -4 10 -98 -70 -3 | 5 17
jpl uuuuu | 50 -31 153 26 -4 | 23 29
mit uuuuu | -16 19 -279 -92 1 | 22 28
ngs uuuuu | 35 45 -80 34 -2 | 14 20
sio xxxxx | 145 125 12 140 4 | 36 40
Table 7.1745.1 GPS week: 1745 Day: 1 MJD: 56460.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -33 -28 91 54 8 | 2 16
emr uuuuu | 55 64 -239 30 -1 | 22 29
esa uuuuu | -1 -30 97 101 0 | 11 18
gfz uuuuu | -37 -15 -10 -218 -5 | 8 18
grg uuuux | 1 -22 19 -227 33 | -1 32
igr xxxxx | -11 -27 49 -12 -7 | 1 17
irf xxxxx | -9 3 -63 -70 -3 | 5 18
jpl uuuuu | 31 -1 35 -27 -13 | 22 29
mit uuuuu | -31 -10 -185 -49 -2 | 23 29
ngs uuuuu | 72 152 -10 228 1 | 12 19
sio xxxxx | 87 92 137 169 2 | 37 40
Table 7.1745.2 GPS week: 1745 Day: 2 MJD: 56461.500
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 | -55 -26 -39 86 0 | 3 16
emr uuuuu | 53 18 -7 37 25 | 22 29
esa uuuuu | -7 -20 91 64 -2 | 11 18
gfz uuuuu | -5 4 19 -132 -13 | 9 18
grg uuuux | 5 -36 146 -252 33 | -2 30
igr xxxxx | 23 5 -99 -28 -7 | 1 17
irf xxxxx | -13 10 -101 -63 -2 | 5 17
jpl uuuuu | -9 6 85 36 8 | 20 27
mit uuuuu | -55 56 -324 -113 -2 | 24 29
ngs uuuuu | 146 37 -50 130 3 | 13 19
sio xxxxx | 41 80 -6 154 1 | 38 41
Table 7.1745.3 GPS week: 1745 Day: 3 MJD: 56462.500
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 | -63 2 -22 52 4 | 3 17
emr uuuuu | 55 -2 -88 222 27 | 25 30
esa uuuuu | -20 -30 77 30 5 | 9 19
gfz uuuuu | -17 9 112 -223 -8 | 7 20
grg uuuux | 5 -3 -48 -307 40 | -2 30
igr xxxxx | -20 -2 -21 -7 -1 | 0 19
irf xxxxx | -7 0 -32 -81 -1 | 5 18
jpl uuuuu | 17 9 -76 27 -12 | 20 27
mit uuuuu | -38 -18 -69 -42 -5 | 25 29
ngs uuuuu | 132 93 -78 216 -6 | 12 19
sio xxxxx | 39 -21 255 204 -3 | 39 41
Table 7.1745.4 GPS week: 1745 Day: 4 MJD: 56463.500
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 | -59 -22 -37 48 8 | 1 15
emr uuuuu | 64 14 -18 162 24 | 25 30
esa uuuuu | -12 -30 59 56 2 | 7 17
gfz uuuuu | -12 28 13 -69 -13 | 4 19
grg uuuux | 16 -19 57 -148 94 | 3 31
igr xxxxx | 17 21 -16 -87 2 | -3 18
irf xxxxx | -12 4 -41 -40 -7 | 2 16
jpl uuuuu | 23 23 90 -73 -2 | 15 23
mit uuuuu | -41 30 -86 -55 -10 | 22 27
ngs uuuuu | 68 16 -115 -35 -4 | 10 18
sio xxxxx | 10 -33 208 81 -4 | 36 39
Table 7.1745.5 GPS week: 1745 Day: 5 MJD: 56464.500
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 | -46 -13 -109 37 11 | 0 13
emr uuuuu | 59 1 -157 108 15 | 26 32
esa uuuuu | -26 -28 20 37 3 | 6 13
gfz uuuuu | 16 54 -133 -19 -5 | 0 12
grg uuuux | 10 -20 81 -135 104 | 14 49
igr xxxxx | -5 19 22 -59 -3 | -5 15
irf xxxxx | -16 0 -56 -38 0 | -1 11
jpl uuuuu | 77 0 117 -24 -8 | 12 17
mit uuuuu | -56 10 -58 -61 -5 | 20 23
ngs uuuuu | 30 8 279 -19 -6 | 9 14
sio xxxxx | 69 -64 300 125 0 | 35 36
Table 7.1745.6 GPS week: 1745 Day: 6 MJD: 56465.500
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 | -53 21 -203 32 1 | -1 13
emr uuuuu | 76 21 -4 80 22 | 27 33
esa uuuuu | -25 -29 69 32 1 | 5 13
gfz uuuuu | -8 56 -178 27 -10 | -3 13
grg uuuux | 35 -15 170 -14 121 | 22 58
igr xxxxx | -12 8 -104 56 2 | -7 16
irf xxxxx | -16 17 -83 -37 -4 | -3 12
jpl uuuuu | 23 -137 119 -41 2 | 11 17
mit uuuuu | -52 38 -126 -131 -7 | 17 21
ngs uuuuu | 119 57 215 -54 5 | 6 14
sio xxxxx | 46 -11 281 6 -6 | 33 35
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