[IGSREPORT-21638] Wk 1728 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Mar 8 08:31:09 PST 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1728 (Feb 17, 2013 - Feb 23, 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:
igs1728[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1728[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1728[0-6].cls IGS GPS clock combination summary report.
igs17287.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17287.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 | 9 9
0 | EMR | 8 8
0 | ESA | 9 9 BRMU MATE BRMU MATE UNSA
0 | GFZ | 8 ALRT AREQ BOGT BRMU MCIL NKLG NRMD YELL
0 | GRG | 21 21 BRMU BRMU
0 | JPL | 8 ALRT AREV
0 | MIT | 1 7 8 11 19 26 1 7 8 11 19 26 STJO TLSE USNO POLV
0 | MIT | STJO TLSE USNO
1 | COD | 9 9 HERT HERT
1 | EMR | 8 8 HERS
1 | ESA | 9 9 UNSA
1 | GFZ | BOGT NTUS SUTM
1 | GRG | LPGS LHAZ LPGS
1 | JPL | 8 FAA1
1 | MIT | 3 3 NTUS GODE KELY NTUS
2 | COD | 9 9 NKLG SOFI HNPT MIZU SOFI SUTM WTZR
2 | EMR | 8 8 STJO
2 | ESA | 9 9 FAA1 MATE NOVM STJO UNSA
2 | GFZ | 8 BOGT GRAS
2 | GRG | HYDE ABMF ADIS CHPI HYDE LHAZ NRMD RAMO WIND
2 | JPL | 8
2 | MIT | 7 14 22 7 14 22 WTZR GRAZ WTZR
3 | COD | 9 9 SOFI SOFI
3 | EMR | 8 8
3 | ESA | 9 9 STJO STJO SYDN
3 | GFZ | 8 30 BOGT BRAZ KERG LHAZ MATE SFER STJO TLSE
3 | GRG | CHUR NRMD NYAL CHUR NKLG NRMD NYAL
3 | JPL | 8 NKLG
3 | MIT | 14 14 MDVJ
4 | COD | 9 9 KOUC KOUC NKLG
4 | EMR | 4 8 4 8
4 | ESA | 9 9 CHUR LPGS NKLG NOVM
4 | GFZ | 8 BOGT BRAZ REUN SFER SUTM
4 | GRG | LPGS KOUC LPGS
4 | JPL | 4 8
4 | MIT | 16 19 22 5 16 19 22 24 SPT0 BAKO SPT0
5 | COD | 4 9 24 HOB2 KOUC REUN FLRS HOB2 KOUC REUN
5 | EMR | 8 8 24
5 | ESA | 4 9 21 MATE
5 | GFZ | 4 8 BOGT KOSG LHAZ NKLG
5 | GRG | ADIS AREQ POLV TIXI
5 | JPL | 8 21 AREV
5 | MIT | 21 24 15 21 24 KOUC WROC WROC
6 | COD | 4 9 4 9 KOUC KOUC
6 | EMR | 8 8
6 | ESA | 4 9 4 9 UNSA
6 | GFZ | 4 8 9 BOGT KERG LHAZ MATE
6 | GRG | ARTU ADIS ARTU KOUC NRMD WES2
6 | JPL | 8
6 | MIT | 24 24 GMAS
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
5 | MIT | 24
6 | EMR | 24
6 | MIT | 24
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G04 | | | | | 1 | 1 | |
PRN G24 | | | | | | | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.9 .3 -.6 -52 3 13 -.04
EMR | 0 | 15.5 -1.2 24.5 1 -3 5 -.10
ESA | 0 | 1.8 1.8 .5 39 -153 175 .16
GFZ | 0 | -.4 -.1 -1.0 -42 -7 9 -.12
GRG | 0 | .9 .9 13.6 -14 37 4 .28
JPL | 0 | -5.1 2.1 19.0 -81 -23 -19 -.17
MIT | 0 | 1.7 3.3 17.5 8 -4 -12 -.23
NGS | 0 | 2.9 -.3 4.3 -22 -23 24 .41
SIO | 0 | 6.4 1.6 -31.7 42 -305 -15 -.33
COD | 1 | -.7 .1 -1.4 -55 6 32 .04
EMR | 1 | 11.0 -.4 21.6 7 6 8 -.08
ESA | 1 | 6.1 6.9 -6.1 101 -247 136 .10
GFZ | 1 | -.3 .1 -1.0 -42 -21 -3 -.10
GRG | 1 | 2.8 1.8 9.8 -14 31 31 .16
JPL | 1 | 3.8 5.8 19.1 -75 15 -10 -.02
MIT | 1 | 1.1 6.4 15.3 1 -2 -10 -.07
NGS | 1 | 4.1 3.2 14.4 -62 -33 29 .47
SIO | 1 | 5.4 .8 -18.5 -10 -219 -179 -.01
COD | 2 | .3 .0 -.8 -54 -4 49 .01
EMR | 2 | 9.3 -1.1 19.0 1 -7 0 .17
ESA | 2 | 3.4 3.1 -3.4 57 -197 154 .24
GFZ | 2 | .0 .3 -.9 -40 -26 11 .12
GRG | 2 | .1 -5.9 7.7 -10 28 15 .23
JPL | 2 | 1.7 5.3 16.5 -74 -10 -43 -.03
MIT | 2 | 1.9 2.9 11.0 -3 -9 -6 .13
NGS | 2 | 8.8 .0 16.0 -72 -64 64 .50
SIO | 2 | 5.8 -1.3 -22.0 13 -227 -88 .21
COD | 3 | -.6 .5 -.3 -61 -10 33 -.05
EMR | 3 | 16.8 1.6 14.0 14 10 -6 .10
ESA | 3 | 3.6 7.5 -7.5 129 -242 134 .05
GFZ | 3 | -.8 .6 -.9 -31 -6 -10 .08
GRG | 3 | 1.5 -2.2 19.2 -36 25 2 .47
JPL | 3 | .0 3.1 18.4 3 -7 42 .08
MIT | 3 | 1.4 4.9 14.4 -4 -4 -13 -.12
NGS | 3 | 5.7 10.1 8.3 22 -39 62 .57
SIO | 3 | 4.2 1.1 -18.9 76 -187 93 .09
COD | 4 | -.4 .8 -1.0 -52 -8 19 -.01
EMR | 4 | 10.0 3.0 16.9 13 5 2 -.30
ESA | 4 | 4.2 4.7 -.8 88 -198 142 .32
GFZ | 4 | -.9 .2 -1.3 -39 -14 -17 .12
GRG | 4 | 1.0 -2.0 13.6 -7 43 22 .27
JPL | 4 | 5.3 .8 16.9 -90 -2 -17 -.06
MIT | 4 | -.1 6.4 16.7 -6 -5 -10 .28
NGS | 4 | 4.4 8.1 11.7 -10 -44 66 .45
SIO | 4 | .3 3.5 2.3 122 -64 93 .23
COD | 5 | -1.3 .4 -1.2 -52 8 13 -.12
EMR | 5 | 9.4 .6 16.7 4 8 0 -.06
ESA | 5 | -4.2 5.1 -6.9 86 -99 140 -.03
GFZ | 5 | -.7 .0 -.6 -41 -13 -14 -.17
GRG | 5 | 1.5 -7.3 14.9 -38 29 6 .19
JPL | 5 | 4.3 -.6 18.8 0 67 -18 -.16
MIT | 5 | -.5 .4 15.4 -1 2 -8 .07
NGS | 5 | 1.5 -3.0 5.3 -54 -8 16 .38
SIO | 5 | -1.2 .4 31.9 11 72 -10 .10
COD | 6 | -1.4 .4 -1.7 -60 -10 23 .02
EMR | 6 | 6.8 3.0 12.8 8 16 2 .0
ESA | 6 | -9.9 2.9 -2.8 37 -29 153 .25
GFZ | 6 | -1.2 -.1 -.4 -46 1 -1 -.17
GRG | 6 | -.3 -8.4 12.2 -21 5 4 .18
JPL | 6 | .3 1.6 15.2 -70 -7 -37 -.15
MIT | 6 | 2.8 -2.5 17.7 1 -3 -10 .09
NGS | 6 | 3.3 5.5 9.1 -11 -29 62 .29
SIO | 6 | -1.7 -.5 34.4 -10 82 -9 .25
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1728.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1728.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 2.1728.[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 3.1728.[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 5.1728.0-6). 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 1728 summary. (Feb 17, 2013 - Feb 23, 2013)
Table 1.1728.a GPS week: 1728 MJD: 56340.000-56346.000
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 264| -1 1 -4 4 37 14 -.39 11 10 | -582 -533 19 90
| 0 0 1 24 21 15 .04 | 787 1146
emr 80| 3 -1 6 -12 17 0 .20 17 17 | 3890 -644 13 102
| 1 1 2 27 17 13 .04 | 902 506
esa 171| 0 1 2 60 -43 2 .09 6 6 | -21 -372 11 114
| 0 0 1 22 42 10 .02 | 1170 1122
gfz 198| 1 -1 -4 -52 -18 -13 -.40 10 9 | 188 -518 20 126
| 0 0 1 32 39 4 .05 | 843 804
grg 140| 0 0 0 -20 32 10 .69 14 14 | 35 -214 17 135
| 0 1 2 23 26 16 .06 | 467 786
igr n/a| 0 0 -2 -31 69 -33 -.11 4 4 | 3700 -934 17 92
| 0 0 0 18 22 8 .02 | 1306 590
jpl 80| 0 0 2 -14 15 -28 .44 16 16 | 5054 -622 17 114
| 1 2 2 20 22 18 .04 | 752 568
mit 238| 0 -1 0 22 26 6 -.58 11 10 | -271 339 25 210
| 0 0 0 11 24 15 .03 | 667 1158
ngs 244| 0 0 0 -56 0 8 .34 11 9 | -616 -518 1787 3363
| 0 0 2 47 69 16 .05 | 703 1042
sio 257| 0 -2 -3 -7 -89 -68 -.16 20 18 | --- --- --- ---
| 1 1 1 44 141 92 .05 | --- ---
Table 1.1728.b GPS week : 1728 MJD: 56340.000-56346.000
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 | 5 5 5 7 5 5 5 |
2 | 4 4 5 4 4 5 5 |
3 | 4 4 3 3 4 4 3 |
4 | 4 4 5 5 6 5 5 |
5 | 4 4 4 4 4 5 5 |
6 | 4 4 4 3 4 4 3 |
7 | 4 4 5 4 4 4 4 |
8 | 7 6 7 6 7 7 8 |
9 | 9 8 9 7 8 9 9 |
10 | 4 3 3 4 3 3 4 |
11 | 3 4 4 4 5 4 4 |
12 | 4 5 5 5 5 6 6 |
13 | 4 4 4 4 4 4 5 |
14 | 4 4 5 4 8 5 5 |
15 | 5 4 4 5 5 5 6 |
16 | 4 4 5 4 5 5 4 |
17 | 4 5 5 4 4 5 5 |
18 | 5 4 5 4 5 5 5 |
19 | 4 4 4 4 5 4 4 |
20 | 4 4 5 4 4 4 5 |
21 | 4 4 5 4 4 4 4 |
22 | 4 5 4 4 4 4 5 |
23 | 4 5 4 4 5 4 4 |
24 | 6 5 5 6 7 16 29 |
25 | 4 4 4 4 4 4 5 |
26 | 4 3 4 4 4 4 4 |
27 | 0 0 0 0 0 0 0 |
28 | 5 5 5 5 5 5 5 |
29 | 6 5 5 5 5 4 5 |
30 | 4 3 4 3 3 4 4 |
31 | 4 4 4 4 4 4 5 |
32 | 4 3 4 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
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1728.0 GPS week: 1728 Day: 0 MJD: 56340.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 267| -1 0 -6 7 19 11 -.34 10 9 | -1011 69 18 96
emr 80| 5 -3 9 -21 12 3 .18 18 18 | 4256 -1123 12 103
esa 171| -1 2 2 21 -38 23 .10 6 6 | 1857 -2100 10 103
gfz 202| 1 0 -3 13 -3 -8 -.39 9 9 | 1452 -1578 20 133
grg 142| 0 0 -1 -11 22 -13 .66 14 14 | 678 -1091 14 136
igr n/a| 0 0 -1 -9 71 -44 -.10 4 4 | 4967 -1522 17 74
jpl 80| 1 0 6 -19 10 -44 .48 15 15 | 5457 -1188 17 106
mit 239| 0 -1 0 30 -4 -16 -.57 11 10 | 193 -570 29 219
ngs 243| 0 0 -3 -60 38 6 .33 11 9 | -1066 173 2119 3476
sio 269| 0 -4 -4 11 -268 -76 -.13 21 19 | --- --- --- ---
Table 2.1728.1 GPS week: 1728 Day: 1 MJD: 56341.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 267| 0 1 -4 0 42 4 -.36 10 10 | 475 -2057 21 90
emr 80| 4 -1 8 -48 0 -7 .27 17 17 | 4466 -641 12 103
esa 171| 0 2 0 70 -87 -3 .12 6 5 | 446 -1055 10 100
gfz 201| 1 -1 -5 -34 38 -10 -.38 9 9 | 868 -1438 19 125
grg 142| 0 0 0 -19 56 14 .67 14 13 | 508 -922 13 133
igr n/a| 0 0 -2 -45 84 -34 -.11 3 3 | 4755 -871 16 88
jpl 80| 0 -3 3 -49 -11 -14 .50 15 15 | 5686 -541 17 100
mit 239| 0 -1 0 20 42 0 -.55 10 9 | 404 -564 24 177
ngs 242| -1 0 2 -67 28 27 .33 11 8 | 349 -1924 1742 3325
sio 267| -2 -2 -2 -35 -186 -218 -.15 19 16 | --- --- --- ---
Table 2.1728.2 GPS week: 1728 Day: 2 MJD: 56342.000
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 266| -1 0 -4 -17 27 42 -.39 12 12 | -929 -362 22 86
emr 80| 1 -2 7 6 5 2 .15 17 17 | 4209 -147 12 87
esa 171| 0 2 0 80 -73 -2 .11 6 6 | 474 -838 12 110
gfz 199| 0 -1 -3 -86 8 -10 -.40 10 10 | -287 -319 21 115
grg 143| 0 0 -2 -22 50 8 .62 14 13 | -187 33 18 124
igr n/a| 0 0 -2 -8 69 -33 -.11 5 5 | 4261 -476 20 91
jpl 80| 0 0 4 -20 3 -46 .43 16 16 | 5456 -269 17 117
mit 239| 0 -1 0 0 31 -6 -.61 11 10 | -1478 2481 27 189
ngs 245| 0 0 2 -8 18 34 .26 11 9 | -819 -585 1744 3597
sio 258| 0 -2 -2 -27 -189 -137 -.23 19 18 | --- --- --- ---
Table 2.1728.3 GPS week: 1728 Day: 3 MJD: 56343.000
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 266| -3 1 -6 -15 39 29 -.36 12 12 | -810 -339 16 90
emr 80| 5 0 4 -40 39 17 .17 18 18 | 4955 -476 14 107
esa 171| 0 0 1 80 -78 1 .09 5 5 | -309 -182 10 116
gfz 198| 2 -1 -4 -70 -6 -17 -.45 9 9 | 719 -805 20 134
grg 143| 0 0 4 -60 38 6 .66 14 14 | -169 427 16 134
igr n/a| 0 0 -2 -51 89 -37 -.12 4 4 | 4671 -781 16 103
jpl 80| -1 -1 4 3 44 -29 .43 16 15 | 5903 -569 18 124
mit 239| 1 -1 0 31 51 8 -.56 12 9 | -303 411 26 220
ngs 244| -1 0 -1 -77 28 2 .36 12 10 | -919 -105 2172 3535
sio 256| 0 -2 -3 31 -135 39 -.19 18 18 | --- --- --- ---
Table 2.1728.4 GPS week: 1728 Day: 4 MJD: 56344.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 261| -1 2 -3 17 82 10 -.39 11 10 | -1804 1403 20 98
emr 80| 2 0 5 14 40 -24 .22 18 18 | 3959 114 12 95
esa 171| 0 0 3 75 -47 4 .10 8 6 | -7 -213 12 146
gfz 195| 0 -1 -5 -57 -29 -14 -.29 8 8 | -978 574 19 127
grg 141| 0 -1 -2 1 61 36 .70 15 14 | -728 1090 17 126
igr n/a| 0 0 -3 -49 89 -18 -.08 4 4 | 3162 37 17 91
jpl 80| 0 1 0 -5 42 -23 .44 17 17 | 4578 391 16 126
mit 239| 0 -1 0 27 54 16 -.56 11 10 | -833 1208 25 252
ngs 248| 0 0 1 -124 -143 -11 .42 13 11 | -1665 1136 1554 3262
sio 255| 0 0 -4 65 -11 40 -.19 19 17 | --- --- --- ---
Table 2.1728.5 GPS week: 1728 Day: 5 MJD: 56345.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 262| -1 2 -2 -15 25 4 -.46 10 9 | -196 -760 20 86
emr 80| 3 0 3 -20 26 6 .23 18 17 | 3090 -1191 14 111
esa 171| -1 2 3 47 -5 1 .07 6 6 | -659 332 11 109
gfz 197| 1 -1 -3 -59 -74 -16 -.42 10 10 | -257 -283 21 119
grg 138| 1 -2 0 -38 -3 -1 .77 14 13 | 77 -315 21 148
igr n/a| 0 0 -1 -38 54 -27 -.12 4 4 | 2537 -1434 20 98
jpl 80| 0 3 0 -23 -6 -44 .42 16 16 | 4370 -984 17 110
mit 238| 1 -2 0 31 7 15 -.60 12 11 | -16 64 24 217
ngs 246| 0 -1 -2 19 61 8 .37 11 9 | -276 -755 1444 3179
sio 246| 0 -3 -3 -37 78 -72 -.10 20 18 | --- --- --- ---
Table 2.1728.6 GPS week: 1728 Day: 6 MJD: 56346.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 261| -2 2 -2 51 27 -1 -.42 12 11 | 198 -1688 21 85
emr 80| 2 -1 3 24 0 7 .21 17 17 | 2295 -1046 15 113
esa 171| 0 1 3 50 28 -8 .07 7 7 | -1955 1452 13 120
gfz 196| 2 -1 -3 -69 -61 -20 -.45 11 11 | -197 222 20 134
grg 137| 2 0 -1 6 2 21 .77 14 14 | 68 -726 25 148
igr n/a| 0 0 -1 -19 26 -39 -.14 5 4 | 1551 -1495 18 102
jpl 80| 0 0 0 12 25 3 .39 16 17 | 3934 -1196 17 116
mit 239| 1 -1 0 14 4 31 -.61 13 11 | 132 -655 24 200
ngs 245| 0 0 -2 -74 -39 -7 .35 11 9 | 84 -1569 1735 3171
sio 251| 1 -2 -5 -57 88 -51 -.11 22 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 3.1728.0 GPS week: 1728 Day: 0 MJD: 56340.000
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 31 5 9 13 4 15 8 10 27 4 | 44 43 48 39 52 46 55 41 53 57 44
2 | 10 19 5 7 14 4 14 8 8 14 3 | 42 39 39 42 42 39 37 42 39 42 39
3 | 7 12 6 8 14 4 11 10 12 9 3 | 15 20 16 14 18 14 19 16 19 19 14
4 | 10 16 7 9 18 3 15 8 12 18 4 | 28 35 30 29 36 28 38 28 28 38 29
5 | 8 20 5 10 11 3 17 10 10 22 4 | 28 32 27 31 34 27 30 26 26 30 26
6 | 6 12 5 10 13 4 12 14 9 29 3 | 11 19 13 15 19 11 17 17 17 32 12
7E | 10 20 7 7 14 4 16 11 10 12 4 | 17 21 18 17 32 15 22 18 27 20 17
8E | 21 26 8 10 24 6 20 12 26 19 6 | 31 36 27 30 40 25 36 27 41 26 28
X9E | 21 27 10 13 28 10 --- 21 37 17 9 | 41 59 44 41 55 44 --- 44 64 42 45
10 | 9 9 4 8 13 2 11 12 9 14 3 | 31 27 30 36 37 32 28 33 33 36 31
11E | 7 14 5 9 11 3 13 7 8 11 3 | 49 51 50 48 55 50 54 47 52 50 49
12 | 9 17 5 9 19 4 16 13 9 21 4 | 23 27 25 26 39 23 29 27 31 23 26
13 | 8 18 5 7 16 5 16 8 7 16 3 | 21 34 24 21 43 21 34 20 25 20 24
14 | 7 22 5 12 11 5 17 11 7 36 4 | 26 27 25 30 34 25 28 25 27 34 25
15 | 10 19 7 9 16 5 16 10 13 22 4 | 24 31 26 26 39 26 31 21 34 24 25
16 | 9 19 8 11 12 3 19 9 9 23 4 | 15 21 22 21 29 16 24 20 20 18 18
17 | 10 15 5 10 18 4 18 9 11 14 4 | 25 29 18 17 30 18 29 18 25 21 19
18 | 9 19 6 12 13 4 15 9 14 28 4 | 24 27 27 32 31 25 27 26 28 29 26
19 | 7 15 5 9 15 4 18 12 12 17 4 | 25 31 23 21 29 23 35 20 23 26 23
20 | 9 17 7 14 9 3 15 10 8 26 4 | 21 30 27 26 29 23 30 22 25 19 22
21 | 8 16 7 8 17 5 13 7 11 17 3 | 32 35 35 33 49 32 38 33 41 33 34
22 | 7 17 7 8 8 6 15 14 11 31 4 | 31 26 30 33 32 29 30 31 25 36 28
23 | 10 18 7 8 10 3 16 10 8 26 4 | 23 32 25 24 34 22 31 20 26 21 24
24E | 12 26 10 13 15 7 16 20 15 --- 5 | 75 82 79 73 75 74 42 73 70 --- 76
25 | 10 17 6 7 14 3 13 8 10 19 3 | 17 25 29 19 38 22 33 27 28 20 24
26 | 7 14 5 8 12 4 9 11 11 18 3 | 20 21 21 20 26 20 22 19 25 19 19
X27 | 6 --- --- --- --- 19 --- --- --- --- 0 | 24 --- --- --- --- 29 --- --- --- --- 25
28 | 11 17 7 7 13 4 13 15 13 19 4 | 19 30 26 26 35 24 29 33 22 25 24
29 | 19 19 7 9 19 4 22 10 14 17 5 | 19 29 22 20 30 19 33 18 30 22 21
30 | 10 12 6 11 11 3 11 10 8 19 3 | 13 16 18 19 20 13 22 19 20 25 15
31E | 10 17 9 11 11 4 14 9 12 11 4 | 17 20 17 17 26 14 20 14 24 17 15
32 | 10 13 6 8 12 3 9 11 9 19 3 | 24 26 31 30 33 26 29 27 29 27 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 9 14 4 15 11 11 21 |T 26 31 28 28 36 26 31 27 31 28 27
WRMS | 9 18 6 9 14 4 15 10 9 19 |NE 21 26 24 24 31 22 28 23 25 25 22
MEDI | 9 17 6 9 13 4 15 10 10 19 |MD 24 29 26 26 34 24 30 26 27 25 25
Table 3.1728.1 GPS week: 1728 Day: 1 MJD: 56341.000
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 31 4 8 15 4 15 7 7 23 4 | 43 45 47 44 53 45 53 50 50 52 46
2 | 11 19 4 9 14 3 14 8 7 13 3 | 37 40 34 34 42 34 37 37 33 38 37
3 | 6 12 5 7 13 3 11 10 13 11 3 | 14 20 13 11 18 11 20 15 17 17 14
4 | 11 15 6 8 15 3 14 7 7 17 3 | 29 37 30 30 33 28 37 30 34 37 31
5 | 7 18 6 10 11 4 16 9 10 20 4 | 21 29 20 24 30 21 27 23 21 24 23
6 | 8 13 5 8 10 3 11 12 10 28 3 | 13 18 11 13 16 10 20 15 13 30 13
7E | 11 16 6 7 17 4 15 9 10 12 4 | 14 22 17 13 35 14 25 15 24 21 17
8E | 17 21 7 9 23 5 23 11 27 19 6 | 21 34 20 21 35 20 38 19 36 20 23
X9E | 18 26 9 9 28 6 --- 15 34 22 8 | 35 54 39 34 49 36 --- 41 52 37 39
10 | 8 10 3 9 13 3 9 7 6 13 3 | 23 23 19 25 27 21 23 26 20 29 23
11E | 10 14 3 6 11 3 11 10 10 10 3 | 35 44 42 38 51 41 48 38 45 42 41
12 | 11 17 7 11 16 4 17 13 15 21 4 | 17 24 18 19 32 18 28 20 29 17 20
13 | 6 16 6 7 17 4 18 10 8 14 4 | 19 34 23 18 39 19 34 18 25 19 23
14 | 7 20 7 11 12 4 17 9 10 26 4 | 18 26 20 23 27 19 26 19 19 28 20
15 | 14 18 5 9 17 3 17 10 9 20 4 | 23 30 20 20 32 19 29 21 28 21 22
16 | 7 18 6 7 12 3 18 8 8 24 3 | 16 22 16 15 24 14 26 16 18 16 17
17 | 13 16 6 11 18 4 19 9 7 15 4 | 20 29 19 16 28 17 32 16 20 19 19
18 | 7 19 6 14 9 3 17 9 15 26 4 | 16 25 22 24 23 19 27 17 20 24 20
19 | 9 15 6 9 15 3 18 11 10 17 4 | 16 23 15 17 24 14 28 15 18 18 15
20 | 8 17 6 11 9 2 17 10 10 26 4 | 18 30 22 23 28 20 33 21 25 21 22
21 | 7 16 4 8 13 3 12 9 10 14 3 | 27 36 32 33 43 31 35 29 40 31 33
22 | 6 17 7 10 9 3 16 16 15 30 4 | 19 24 22 24 24 20 25 21 13 27 19
23 | 9 20 7 10 12 3 21 11 10 23 4 | 21 30 23 21 30 19 31 17 23 19 21
24E | 11 22 7 15 17 5 12 10 15 --- 5 | 61 65 61 61 64 57 36 61 54 --- 61
25 | 12 15 4 8 15 2 15 10 12 19 4 | 16 23 21 16 33 18 34 18 24 16 20
26 | 9 13 4 8 12 3 10 8 9 15 3 | 24 22 16 20 23 19 21 21 18 19 19
X27 | 6 --- --- --- --- 71 --- --- --- --- 0 | 30 --- --- --- --- 30 --- --- --- --- 32
28 | 13 16 6 8 15 2 15 12 13 15 4 | 18 29 19 21 31 20 31 22 25 19 21
29 | 18 20 4 8 15 3 19 12 9 16 4 | 14 29 20 21 30 17 30 16 25 20 20
30 | 7 10 4 8 11 2 9 9 8 19 3 | 13 18 14 14 18 11 21 16 18 24 14
31E | 7 14 6 7 12 4 15 8 11 11 3 | 13 21 14 15 26 12 21 15 22 18 15
32 | 9 14 5 9 10 3 12 8 8 18 3 | 24 26 23 29 25 23 28 29 26 30 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 6 9 14 3 15 10 11 19 |T 22 30 23 23 32 22 30 23 26 25 24
WRMS | 10 17 5 9 13 3 15 9 8 16 |NE 18 25 18 19 26 18 27 19 21 21 20
MEDI | 9 16 6 9 13 3 15 10 10 18 |MD 19 29 20 21 30 19 28 20 24 21 21
Table 3.1728.2 GPS week: 1728 Day: 2 MJD: 56342.000
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 28 6 8 16 5 13 14 8 19 5 | 26 37 28 30 36 27 30 26 29 37 28
2 | 16 19 5 10 22 7 14 8 13 11 5 | 104 102 104 104 102 102 103 103 105 104 103
3 | 8 11 5 7 12 4 12 11 7 9 3 | 17 21 16 14 18 15 23 17 18 18 16
4 | 13 15 7 9 19 5 18 9 7 17 4 | 39 44 40 39 51 40 46 40 38 47 41
5 | 10 18 7 11 10 5 16 10 11 21 4 | 27 26 23 25 28 22 26 26 21 25 23
6 | 9 13 6 8 9 5 11 12 8 31 3 | 17 21 17 19 17 16 22 18 15 32 16
7E | 11 17 7 9 14 5 14 12 13 13 4 | 18 22 20 15 33 16 24 17 28 22 18
8E | 21 29 8 10 20 7 21 16 21 23 6 | 20 42 22 22 33 21 37 17 34 19 24
X9E | 22 26 12 11 21 6 --- 19 36 25 8 | 59 70 61 59 65 57 --- 63 68 61 61
10 | 12 10 5 9 9 3 11 7 7 15 3 | 28 23 27 28 31 28 24 29 26 31 27
11E | 10 14 5 7 12 5 13 9 8 13 3 | 31 40 35 37 38 35 36 36 35 40 35
12 | 10 16 5 10 15 3 16 15 9 19 4 | 13 23 17 19 32 16 24 23 22 19 19
13 | 13 17 7 7 15 5 18 7 9 13 4 | 25 32 26 20 39 23 35 21 26 21 25
14 | 7 18 5 12 12 4 18 11 11 24 4 | 21 24 24 26 31 21 26 21 24 25 22
15 | 13 16 7 11 14 4 15 9 11 18 4 | 21 26 20 23 30 19 26 20 26 20 21
16 | 12 18 7 10 13 4 21 10 10 23 4 | 18 23 19 23 25 15 26 18 18 17 18
17 | 18 14 6 12 18 5 17 10 8 16 4 | 25 28 20 19 29 17 29 20 22 23 20
18 | 9 18 5 13 9 4 17 12 13 25 4 | 19 24 22 26 26 19 25 19 24 20 21
19 | 8 14 7 9 13 4 19 11 8 18 4 | 27 31 20 23 28 23 33 20 24 23 22
20 | 8 16 9 11 11 4 16 13 12 26 4 | 20 28 23 23 26 21 28 19 22 22 21
21 | 11 14 6 10 17 4 13 10 15 11 4 | 26 28 27 33 38 26 27 24 25 28 27
22 | 7 18 6 10 9 6 17 15 9 25 4 | 22 21 25 27 24 21 25 25 20 25 21
23 | 13 17 6 8 11 5 21 8 9 23 4 | 26 30 26 22 32 24 31 20 25 19 24
24E | 17 20 8 13 17 7 14 13 8 15 5 | 73 73 73 66 69 70 29 71 52 70 70
25 | 12 12 5 8 14 5 14 10 7 14 3 | 18 23 23 18 33 19 32 22 23 16 22
26 | 12 12 5 10 10 4 9 11 11 14 3 | 20 19 17 17 22 16 19 24 18 18 18
X27 | 7 --- --- --- --- 51 --- --- --- --- 0 | 43 --- --- --- --- 28 --- --- --- --- 44
28 | 20 19 6 8 16 4 17 16 10 13 5 | 25 30 22 23 34 19 28 26 25 21 23
29 | 17 20 6 10 13 5 19 15 10 15 5 | 16 29 21 26 30 19 31 20 26 22 22
30 | 8 12 7 5 12 3 12 11 8 21 3 | 15 19 17 16 19 15 24 20 19 25 17
31E | 7 15 7 7 12 6 15 9 14 14 4 | 18 22 17 17 26 15 23 20 28 21 18
32 | 8 15 6 7 12 4 9 8 12 21 3 | 26 26 27 28 31 25 30 28 26 30 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 6 10 14 5 16 11 11 19 |T 28 32 28 28 34 26 30 28 29 29 28
WRMS | 12 17 6 10 13 5 16 10 9 18 |NE 22 25 21 22 27 20 27 21 22 22 22
MEDI | 11 16 6 10 13 5 15 11 10 18 |MD 22 26 23 23 31 21 27 21 25 23 22
Table 3.1728.3 GPS week: 1728 Day: 3 MJD: 56343.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 32 11 12 14 6 17 35 11 14 7 | 54 57 54 54 55 53 57 65 55 57 54
2E | 11 20 4 10 13 7 16 10 14 12 4 | 68 75 71 70 73 69 72 70 72 73 71
3 | 11 11 4 7 11 3 11 7 9 10 3 | 21 19 16 16 21 14 19 15 21 15 15
4E | 13 22 6 9 21 7 20 10 13 16 5 | 55 57 58 52 57 48 59 55 50 60 52
5 | 16 18 4 11 11 4 17 6 10 19 4 | 28 23 19 24 23 19 23 22 22 21 20
6 | 7 13 4 6 10 3 11 8 8 29 3 | 12 17 12 15 19 10 16 15 16 29 12
7E | 11 18 5 8 13 4 16 10 10 12 4 | 20 23 20 17 33 18 27 16 26 23 19
8E | 21 22 6 10 22 5 20 15 23 20 6 | 27 37 23 24 35 23 37 22 34 23 25
X9E | 17 32 7 9 19 5 --- 19 26 21 7 | 59 72 61 64 68 60 --- 65 73 61 63
10 | 12 12 4 10 12 3 9 8 10 12 3 | 28 24 26 30 27 26 25 27 29 29 26
11E | 8 19 4 6 12 3 11 13 15 11 4 | 45 50 49 47 54 49 53 48 50 49 48
12 | 13 18 5 13 16 3 16 13 13 20 4 | 23 24 21 23 35 20 28 22 27 22 21
13 | 10 18 5 9 16 3 17 7 10 13 4 | 26 34 25 18 40 22 35 21 28 19 24
14 | 10 19 4 11 14 4 16 8 11 17 4 | 23 26 24 28 32 24 27 24 26 23 23
15 | 18 18 5 10 16 5 17 11 10 19 4 | 28 27 22 24 34 22 29 19 27 19 22
16 | 9 18 7 8 11 3 20 7 10 23 4 | 12 18 20 18 29 14 24 16 20 14 15
17 | 13 14 4 8 16 3 20 11 8 19 4 | 22 24 18 16 26 14 24 15 22 19 17
18 | 11 18 6 11 12 3 17 9 12 23 4 | 25 25 23 28 26 22 26 22 23 22 23
19 | 10 16 5 9 13 4 16 9 12 15 4 | 19 27 18 19 23 17 27 17 22 23 17
20 | 7 17 6 9 11 3 18 11 12 27 4 | 19 25 21 20 24 19 27 20 24 21 19
21 | 8 15 3 10 15 3 13 9 10 10 3 | 36 37 37 40 39 35 36 34 38 39 35
22 | 8 17 4 7 10 5 16 10 9 24 3 | 31 26 27 29 28 25 26 28 24 26 25
23 | 10 17 5 8 11 4 17 7 11 23 3 | 24 27 26 21 31 22 31 19 28 17 23
24E | 21 20 8 15 17 4 15 13 14 16 5 | 94 92 98 93 97 93 33 99 70 82 96
25 | 12 14 4 10 14 3 15 9 12 16 4 | 19 21 24 20 37 19 32 21 25 15 22
26 | 9 13 3 8 15 3 15 8 7 15 3 | 23 20 17 20 23 16 22 19 23 17 19
X27 | 7 --- --- --- --- 54 --- --- --- --- 0 | 25 --- --- --- --- 47 --- --- --- --- 27
28 | 16 16 5 7 17 2 15 14 10 12 4 | 17 26 21 21 34 19 30 27 21 19 21
29 | 18 20 6 10 15 4 17 12 12 15 5 | 17 25 18 17 26 15 27 13 23 19 16
30 | 7 12 5 6 10 3 11 6 10 17 3 | 11 16 17 14 21 13 21 14 20 21 13
31E | 9 13 5 7 14 4 14 10 13 13 3 | 16 19 17 16 23 15 20 15 28 19 15
32 | 8 14 4 6 10 4 11 7 8 18 3 | 23 20 24 24 23 21 24 24 23 25 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 18 5 9 14 4 16 12 12 18 |T 29 32 29 29 36 28 31 29 31 29 28
WRMS | 12 18 5 9 14 4 15 9 10 18 |NE 21 23 20 21 27 20 25 20 23 20 20
MEDI | 10 18 5 9 14 4 16 10 11 16 |MD 23 25 23 23 31 21 27 22 26 22 22
Table 3.1728.4 GPS week: 1728 Day: 4 MJD: 56344.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 30 6 10 11 6 18 12 16 19 5 | 25 31 25 24 26 22 32 24 33 17 23
2E | 9 19 7 8 12 5 17 13 8 13 4 | 44 47 46 41 46 45 46 47 53 43 45
3 | 12 13 6 8 13 4 11 7 15 9 4 | 15 18 16 11 17 11 18 14 24 15 11
4E | 19 17 8 11 22 6 20 14 12 29 5 | 56 57 59 58 60 58 57 56 60 59 56
5 | 9 20 5 9 10 5 18 8 12 19 4 | 16 21 15 20 21 15 20 19 20 18 14
6 | 7 13 6 8 14 4 11 8 15 27 3 | 12 16 16 13 16 11 16 15 23 28 12
7E | 12 18 5 7 11 5 16 8 11 15 4 | 22 22 19 15 28 15 24 18 29 22 17
8E | 19 23 7 9 32 4 21 13 24 17 6 | 26 35 23 23 41 21 35 20 36 21 24
X9E | 15 32 10 12 17 9 --- 26 23 20 7 | 59 70 61 53 62 54 --- 69 66 55 60
10 | 10 12 4 8 10 4 13 7 9 13 3 | 22 17 17 27 23 20 19 25 27 27 21
11E | 10 20 4 9 13 5 13 19 16 11 4 | 48 57 52 53 61 51 57 54 51 47 52
12 | 9 19 6 8 20 3 21 14 11 20 5 | 20 23 20 21 32 17 26 19 27 18 19
13 | 7 18 5 9 14 5 18 8 12 14 4 | 22 34 21 19 39 18 37 19 27 15 22
14 | 11 20 31 9 21 7 19 15 13 19 7 | 25 25 51 25 30 23 28 25 25 23 27
15 | 15 17 6 8 16 5 18 12 17 18 5 | 20 28 22 18 30 18 28 17 31 19 18
16 | 8 19 7 11 12 5 22 8 13 23 4 | 15 23 22 18 29 16 24 15 26 15 17
17 | 11 14 5 9 19 4 16 11 13 23 4 | 19 22 14 17 27 14 25 16 22 20 15
18 | 14 23 9 10 12 3 19 12 8 24 5 | 23 27 23 27 27 20 27 18 32 21 23
19 | 10 15 7 7 12 4 19 10 17 15 4 | 16 23 15 16 24 13 27 15 27 17 15
20 | 9 15 7 9 8 5 16 14 14 29 4 | 21 27 20 21 28 19 29 19 22 18 18
21E | 9 17 4 7 12 4 14 7 10 13 3 | 24 28 25 27 31 23 28 25 38 30 26
22 | 7 18 5 7 14 5 17 15 12 25 4 | 27 24 24 29 29 23 26 24 30 26 24
23 | 11 20 6 8 10 4 18 9 15 24 4 | 23 30 23 19 30 18 31 17 27 13 20
X24E | 13 29 9 15 23 8 --- 14 17 19 6 | 84 85 88 83 92 86 --- 86 66 78 87
25 | 9 16 6 7 17 4 15 9 7 15 3 | 15 20 23 19 33 19 29 19 27 13 20
26 | 10 14 4 8 14 5 12 8 12 14 3 | 15 17 14 16 20 14 17 18 28 16 15
X27 | 8 --- --- --- --- 59 --- --- --- --- 0 | 30 --- --- --- --- 40 --- --- --- --- 32
28 | 14 17 5 11 16 3 17 13 15 13 4 | 20 27 23 21 32 19 27 26 35 19 22
29 | 13 21 6 8 16 4 21 13 13 16 5 | 11 25 15 18 25 13 26 12 28 17 15
30 | 9 12 5 7 12 4 10 7 12 19 3 | 18 19 21 15 20 15 20 17 23 23 16
31E | 11 13 6 7 16 4 13 10 12 11 4 | 21 20 22 12 25 16 22 20 24 20 16
32 | 9 10 3 7 11 4 8 7 13 21 3 | 18 17 17 18 23 15 22 17 19 20 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 8 8 15 4 17 11 13 19 |T 26 30 27 25 33 24 28 25 32 25 25
WRMS | 10 18 6 8 14 4 17 10 11 17 |NE 19 23 20 19 26 17 24 18 26 19 18
MEDI | 10 18 6 8 14 4 17 11 13 19 |MD 21 25 22 20 29 18 27 19 27 20 20
Table 3.1728.5 GPS week: 1728 Day: 5 MJD: 56345.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 30 6 9 13 5 15 12 10 21 4 | 33 38 31 31 34 30 37 33 32 33 30
2E | 12 20 5 7 15 3 18 12 8 11 4 | 38 40 37 39 44 37 40 35 40 35 38
3 | 9 16 5 9 14 4 11 9 11 10 3 | 16 21 18 17 21 14 20 15 21 15 15
4E | 16 17 7 11 18 6 19 11 7 19 4 | 25 30 29 28 35 28 31 28 26 31 26
5 | 12 19 7 11 11 3 19 9 10 22 4 | 23 25 18 22 20 17 23 22 20 20 17
6 | 6 17 6 10 14 3 12 9 9 26 3 | 10 18 17 16 19 12 16 12 17 27 12
7E | 11 14 6 9 15 3 16 11 10 12 4 | 18 19 16 12 31 13 21 14 26 21 15
8E | 18 26 7 11 23 5 22 17 24 22 6 | 24 38 24 22 38 21 36 18 41 20 24
X9E | 11 36 11 22 17 9 --- 37 20 22 9 | 72 89 77 76 81 75 --- 77 85 79 76
10 | 10 11 3 11 10 4 13 8 6 12 3 | 24 19 21 24 21 21 19 25 22 25 21
11E | 8 16 6 7 15 6 10 9 9 11 3 | 67 73 72 69 80 72 73 67 74 71 70
12 | 10 19 8 12 17 3 22 17 16 21 5 | 22 27 26 26 33 23 28 26 26 23 23
13 | 7 18 6 8 15 4 15 11 10 15 4 | 16 33 21 15 39 17 34 18 25 10 20
14 | 7 17 6 12 16 4 18 11 10 22 4 | 23 26 29 26 29 23 27 23 23 20 23
15 | 12 19 7 11 15 3 18 17 10 22 4 | 19 27 20 20 31 18 27 22 26 21 18
16 | 7 20 8 9 11 3 24 9 7 25 4 | 13 22 22 17 27 16 26 13 18 13 15
17 | 15 16 5 11 16 4 17 13 10 18 4 | 25 24 18 18 28 13 25 16 19 18 16
18 | 11 20 5 14 13 3 18 11 11 32 4 | 19 28 22 22 25 19 29 15 21 20 19
19 | 9 14 6 9 11 3 17 11 9 15 4 | 15 25 20 18 24 17 29 16 19 20 16
20 | 9 16 6 13 10 4 15 15 11 31 4 | 17 23 18 17 25 16 25 19 27 19 16
21E | 7 19 5 11 18 4 14 9 10 12 4 | 26 29 28 27 33 26 27 25 37 28 26
22 | 7 18 5 11 11 4 18 12 10 30 4 | 21 24 23 25 27 21 27 20 20 22 20
23 | 8 20 6 9 12 4 16 9 11 25 4 | 17 28 21 15 30 16 27 16 25 10 18
X24E | 32 49 21 30 40 16 --- 71 53 40 16 | 109 119 115 110 122 99 --- 139 113 90 107
25 | 10 14 7 8 15 4 17 11 15 16 4 | 15 20 26 18 33 21 31 21 26 13 21
26 | 8 15 4 12 11 4 12 11 11 15 3 | 13 17 16 13 16 12 16 20 19 15 12
X27 | 7 --- --- --- --- 48 --- --- --- --- 0 | 57 --- --- --- --- 35 --- --- --- --- 57
28 | 12 17 7 8 13 2 16 16 12 18 4 | 15 27 18 18 30 14 27 20 20 17 16
29 | 9 17 8 9 16 4 16 12 9 16 4 | 15 20 18 16 27 14 23 13 20 20 15
30 | 5 12 7 9 17 3 11 10 8 19 3 | 13 18 22 13 21 14 18 12 20 22 15
31E | 11 14 7 7 13 4 16 13 11 9 4 | 19 19 21 12 25 14 17 16 20 18 14
32 | 8 11 4 9 13 3 9 8 10 25 3 | 14 17 16 19 21 15 19 18 20 23 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 10 14 4 16 12 11 20 |T 26 31 28 26 34 25 27 26 30 26 26
WRMS | 9 17 6 10 13 4 16 11 9 18 |NE 19 23 20 18 26 17 24 18 21 18 19
MEDI | 9 17 6 10 15 4 16 11 10 19 |MD 19 25 21 19 29 17 27 20 23 20 18
Table 3.1728.6 GPS week: 1728 Day: 6 MJD: 56346.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 26 7 9 14 4 14 10 7 22 4 | 21 36 26 30 26 25 27 26 28 36 24
2E | 13 15 7 11 13 3 14 15 13 14 4 | 43 44 40 39 48 39 43 41 41 42 40
3 | 12 10 5 6 13 3 10 9 8 12 3 | 23 18 18 15 23 14 20 16 24 17 17
4E | 18 12 7 15 16 4 17 14 10 25 5 | 29 30 24 28 33 22 33 28 23 35 24
5 | 13 16 7 10 10 6 18 14 11 24 4 | 26 24 21 30 27 22 22 28 21 26 21
6 | 6 12 4 8 14 3 7 11 8 25 3 | 16 18 17 16 23 13 18 16 17 27 14
7E | 10 18 5 9 13 4 15 13 8 15 4 | 21 23 21 22 34 18 26 21 28 23 21
8E | 21 27 10 11 27 8 17 17 26 22 7 | 28 45 27 29 44 25 37 24 40 24 28
X9E | 10 33 11 17 19 7 --- 35 19 25 8 | 107 101 104 104 100 100 --- 122 102 96 104
10 | 12 11 4 8 12 4 13 12 12 15 4 | 29 26 27 32 34 28 28 32 29 31 27
11E | 10 11 6 9 14 4 12 11 7 15 3 | 67 74 73 73 76 74 74 75 79 77 73
12 | 15 19 9 16 18 5 21 15 18 23 6 | 26 25 29 29 35 24 26 29 30 27 25
13 | 6 17 8 10 14 5 19 13 12 17 4 | 25 34 24 22 42 23 36 25 26 18 25
14 | 11 16 9 10 14 4 16 17 7 23 4 | 32 31 35 32 36 31 33 34 31 28 31
15 | 16 20 8 15 14 7 20 28 13 26 6 | 22 30 21 25 33 22 31 37 27 24 21
16 | 8 19 7 10 15 4 20 9 8 27 4 | 20 23 22 22 32 18 28 22 19 20 19
17 | 15 20 10 15 14 6 22 10 7 16 5 | 30 30 17 21 31 17 30 18 23 20 20
18 | 13 19 7 15 14 6 20 10 10 35 5 | 25 26 26 29 31 22 30 21 21 27 22
19 | 12 16 5 7 12 4 16 9 7 16 3 | 20 29 18 20 23 18 29 22 22 25 19
20 | 9 17 9 10 15 6 19 12 10 36 4 | 21 28 23 26 30 21 29 24 24 31 21
21E | 6 20 9 12 11 3 14 10 11 11 4 | 21 26 22 29 29 23 27 24 30 28 23
22 | 9 17 5 13 11 5 18 15 8 31 4 | 32 27 29 33 34 29 30 30 25 28 27
23 | 9 19 8 10 10 4 18 11 9 29 4 | 27 31 24 25 33 22 32 23 25 20 23
X24E | 58 83 38 51 63 30 --- 242 --- 49 29 | 168 160 175 163 183 162 --- 190 --- 147 169
25 | 10 16 8 9 14 4 17 12 10 17 4 | 18 23 30 22 38 24 32 27 27 16 25
26 | 6 14 6 10 10 5 12 13 8 17 3 | 21 19 20 21 23 18 21 28 21 19 19
X27 | 7 --- --- --- --- 54 --- --- --- --- 0 | 30 --- --- --- --- 30 --- --- --- --- 31
28 | 9 20 6 12 12 4 19 14 10 20 4 | 21 29 25 28 37 23 29 29 30 25 24
29 | 14 18 6 9 13 3 18 15 14 18 5 | 15 24 16 19 26 16 28 13 24 22 16
30 | 8 10 6 8 16 4 11 7 9 18 3 | 18 24 22 19 24 20 22 15 24 24 19
31E | 10 15 8 10 16 4 16 11 12 10 4 | 26 26 26 21 32 24 25 23 28 26 23
32 | 11 12 6 7 14 4 11 8 8 21 3 | 26 25 22 28 29 22 24 26 23 27 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 7 11 14 5 16 13 11 22 |T 32 35 33 33 40 30 30 35 30 33 31
WRMS | 11 17 7 11 14 4 17 11 9 18 |NE 23 25 23 24 30 21 27 24 24 23 22
MEDI | 10 17 7 10 14 4 17 12 10 21 |MD 25 27 24 28 33 22 29 26 25 26 23
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1728 GPS week: 1728 MJD: 56340.0-56346.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 |U 3 4 11 |U 11 12 35 |U 6 5 15 |
emr | emr 2966 | 7 6 15 |U 12 13 35 | 9 8 17 |
esa | esa 2976 | 4 4 11 |U 11 12 36 | 6 5 18 |
gfz | gfz 2965 |U 5 4 12 |U 11 12 35 |U 7 6 18 |
grg | grg 2976 |U 8 9 15 |U 12 14 41 | 9 8 20 |
igr | igr 2973 | 5 5 13 | 11 12 34 | 6 5 18 |
igs | igs 2971 | 4 4 10 | 11 12 35 | 8 7 16 |
jpl | jpl 2833 | 6 7 13 |U 11 13 36 |U 9 9 19 |
mit | mit 2976 | 5 5 14 |U 11 13 37 |U 8 8 19 |
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 5.1728.0 GPS week: 1728 Day: 0 MJD: 56340.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 3 4 11 | 10 8 29 | 6 5 16 |
emr | emr 2968 | 6 5 13 | 10 8 31 | 8 7 19 |
esa | esa 2976 | 4 4 12 | 10 8 30 | 6 6 18 |
gfz | gfz 2969 | 5 5 13 | 10 10 34 | 7 7 16 |
grg | grg 2976 | 7 6 17 | 17 25 58 | 7 7 20 |
igr | igr 2976 | 4 4 10 | 10 8 29 | 6 5 17 |
igs | igs 2975 | 4 4 10 | 10 8 29 | 8 7 17 |
jpl | jpl 2875 | 5 5 11 | 11 11 33 | 7 8 14 |
mit | mit 2976 | 4 5 16 | 13 11 45 | 8 8 19 |
Table 5.1728.1 GPS week: 1728 Day: 1 MJD: 56341.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 4 5 13 | 9 10 22 | 5 3 12 |
emr | emr 2968 | 7 6 13 | 10 11 28 | 7 6 18 |
esa | esa 2976 | 5 6 12 | 8 10 28 | 6 4 16 |
gfz | gfz 2967 | 5 6 12 | 8 10 26 | 6 5 17 |
grg | grg 2976 | 8 8 17 | 8 12 34 | 8 6 19 |
igr | igr 2974 | 5 6 11 | 8 11 28 | 5 3 16 |
igs | igs 2974 | 5 5 11 | 9 10 28 | 7 5 17 |
jpl | jpl 2876 | 5 6 10 | 10 10 25 | 5 4 14 |
mit | mit 2976 | 5 6 12 | 9 10 31 | 7 6 16 |
Table 5.1728.2 GPS week: 1728 Day: 2 MJD: 56342.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 3 4 9 | 13 14 46 | 5 5 16 |
emr | emr 2968 | 6 6 14 | 12 13 38 | 8 8 15 |
esa | esa 2976 | 3 5 10 | 13 13 48 | 5 4 16 |
gfz | gfz 2968 | 4 4 12 | 12 14 41 | 6 5 16 |
grg | grg 2976 | 8 8 16 | 13 13 50 | 11 9 25 |
igr | igr 2976 | 3 4 10 | 12 13 41 | 5 4 18 |
igs | igs 2974 | 4 4 12 | 13 13 44 | 7 6 16 |
jpl | jpl 2876 | 5 6 14 | 12 14 38 | 7 8 16 |
mit | mit 2976 | 4 4 13 | 13 13 39 | 10 9 27 |
Table 5.1728.3 GPS week: 1728 Day: 3 MJD: 56343.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 | 5 4 14 | 14 12 40 | 5 4 15 |
emr | emr 2968 | 5 7 14 | 14 11 42 | 8 7 15 |
esa | esa 2976 | 4 4 11 | 14 10 39 | 6 5 18 |
gfz | gfz 2966 | 4 4 13 | 14 10 40 | 6 7 19 |
grg | grg 2976 | 10 11 16 | 12 10 41 | 8 8 19 |
igr | igr 2966 | 5 5 14 | 15 11 41 | 6 5 15 |
igs | igs 2971 | 3 4 9 | 14 10 40 | 6 6 15 |
jpl | jpl 2876 | 6 8 11 | 14 13 42 | 8 9 15 |
mit | mit 2976 | 4 3 12 | 15 10 34 | 6 6 16 |
Table 5.1728.4 GPS week: 1728 Day: 4 MJD: 56344.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 3 2 10 | 12 24 52 | 6 6 14 |
emr | emr 2966 | 10 7 23 | 14 24 45 | 8 9 18 |
esa | esa 2976 | 4 3 13 | 12 24 54 | 6 6 17 |
gfz | gfz 2962 | 5 3 15 | 12 22 47 | 8 5 18 |
grg | grg 2976 | 8 9 16 | 11 23 52 | 9 9 18 |
igr | igr 2976 | 4 3 11 | 12 22 45 | 6 6 20 |
igs | igs 2967 | 5 3 13 | 12 24 52 | 7 5 15 |
jpl | jpl 2777 | 7 6 15 | 14 25 54 | 10 11 22 |
mit | mit 2976 | 8 7 22 | 12 25 55 | 9 8 20 |
Table 5.1728.5 GPS week: 1728 Day: 5 MJD: 56345.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 3 4 9 | 7 8 23 | 7 6 19 |
emr | emr 2964 | 8 7 14 | 9 10 25 | 12 12 22 |
esa | esa 2976 | 4 4 9 | 7 8 23 | 6 7 21 |
gfz | gfz 2961 | 5 3 10 | 7 8 25 | 8 6 22 |
grg | grg 2976 | 8 8 13 | 8 8 25 | 11 7 21 |
igr | igr 2972 | 9 11 24 | 7 8 25 | 7 6 23 |
igs | igs 2968 | 4 4 9 | 7 8 22 | 11 10 17 |
jpl | jpl 2776 | 7 7 14 | 7 9 23 | 12 10 18 |
mit | mit 2976 | 5 5 12 | 8 10 26 | 12 9 15 |
Table 5.1728.6 GPS week: 1728 Day: 6 MJD: 56346.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 3 4 14 | 13 10 31 | 6 6 14 |
emr | emr 2964 | 6 6 13 | 13 12 36 | 9 8 15 |
esa | esa 2976 | 3 4 8 | 10 11 30 | 8 8 19 |
gfz | gfz 2962 | 4 3 10 | 12 11 33 | 7 6 18 |
grg | grg 2976 | 7 12 14 | 14 11 29 | 9 8 21 |
igr | igr 2973 | 4 4 10 | 13 11 31 | 8 8 17 |
igs | igs 2971 | 4 4 9 | 12 10 32 | 8 7 16 |
jpl | jpl 2776 | 7 8 15 | 13 12 36 | 16 11 35 |
mit | mit 2976 | 4 3 13 | 11 12 32 | 8 10 18 |
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 6.1728 GPS week: 1728 MJD: 56340.500-56346.500
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 | -50 -8 -42 -103 -2 | 8 18
| 25 24 77 115 6 | 3
emr uuuuu | 13 -24 58 185 1 | 5 16
| 25 37 51 104 10 | 2
esa uuuuu | -3 -18 97 -6 0 | 13 18
| 54 28 42 101 3 | 3
gfz uuuuu | 20 20 15 -57 4 | 13 19
| 35 14 37 63 5 | 4
grg uuuux | -17 2 -22 -25 39 | -10 37
| 23 21 41 87 47 | 6
igr xxxxx | -48 18 7 -7 0 | 10 16
| 22 19 41 38 5 | 3
irf xxxxx | 1 -13 -16 49 -3 | 11 18
| 24 14 21 14 4 | 3
jpl uuuuu | -5 -23 77 92 -4 | 66 68
| 32 21 76 118 9 | 4
mit uuuuu | 30 -2 -194 145 -2 | 16 22
| 45 20 61 52 7 | 4
ngs uuuuu | 13 58 -47 -115 0 | 7 10
| 84 49 41 111 4 | 1
sio xxxxx | 118 1 -259 -9 19 | 52 57
| 140 50 55 63 14 | 12
Table 7.1728.0 GPS week: 1728 Day: 0 MJD: 56340.500
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 | -35 -29 -19 -107 11 | 3 18
emr uuuuu | 56 2 -38 343 -19 | 5 16
esa uuuuu | -19 13 90 -90 4 | 8 16
gfz uuuuu | 25 3 -36 -48 8 | 7 15
grg uuuux | 3 -3 28 30 0 | -1 42
igr xxxxx | -45 -7 6 -24 9 | 6 15
irf xxxxx | 11 -26 16 52 3 | 6 17
jpl uuuuu | 20 -9 5 170 9 | 59 63
mit uuuuu | 35 -13 -105 114 6 | 10 20
ngs uuuuu | -32 23 -10 -79 -3 | 6 10
sio xxxxx | 308 -26 -187 20 38 | 33 42
Table 7.1728.1 GPS week: 1728 Day: 1 MJD: 56341.500
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 | -67 -11 -168 -168 -4 | 5 19
emr uuuuu | 18 28 29 260 8 | 2 16
esa uuuuu | 45 -49 155 -67 2 | 10 17
gfz uuuuu | 12 40 50 58 8 | 8 16
grg uuuux | -43 -2 11 -52 -10 | -6 39
igr xxxxx | -73 29 -20 38 3 | 7 16
irf xxxxx | -19 -11 -8 47 3 | 7 17
jpl uuuuu | 22 11 116 253 9 | 61 64
mit uuuuu | 9 10 -248 89 8 | 11 21
ngs uuuuu | -43 43 -24 -113 -7 | 5 10
sio xxxxx | 197 51 -287 27 39 | 39 47
Table 7.1728.2 GPS week: 1728 Day: 2 MJD: 56342.500
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 | -56 26 -131 -211 0 | 8 18
emr uuuuu | 8 -29 82 216 2 | 6 14
esa uuuuu | 20 -10 81 -110 1 | 13 17
gfz uuuuu | 23 4 38 -65 9 | 12 17
grg uuuux | -26 -6 -26 -9 2 | -11 37
igr xxxxx | -49 -3 -2 0 -2 | 11 16
irf xxxxx | -10 -29 -32 41 -4 | 11 17
jpl uuuuu | 22 -24 185 180 -6 | 65 68
mit uuuuu | 1 -30 -211 168 -5 | 16 21
ngs uuuuu | -14 52 -32 57 -3 | 6 10
sio xxxxx | 211 -9 -349 47 21 | 48 54
Table 7.1728.3 GPS week: 1728 Day: 3 MJD: 56343.500
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 | -69 8 -19 -228 -1 | 10 19
emr uuuuu | -5 -1 117 229 -5 | 8 16
esa uuuuu | 53 -48 96 -68 -3 | 15 19
gfz uuuuu | -23 17 20 -34 1 | 15 20
grg uuuux | -32 30 -51 123 23 | -16 32
igr xxxxx | -72 37 -9 -75 -7 | 12 17
irf xxxxx | -17 5 -38 73 -5 | 13 18
jpl uuuuu | -23 -49 146 88 -11 | 67 69
mit uuuuu | 5 11 -220 162 -2 | 18 23
ngs uuuuu | -6 93 -134 -45 4 | 8 11
sio xxxxx | 176 -21 -212 61 19 | 56 60
Table 7.1728.4 GPS week: 1728 Day: 4 MJD: 56344.500
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 | -83 -21 -6 -103 -7 | 10 19
emr uuuuu | -23 -38 93 101 4 | 6 16
esa uuuuu | 25 -36 30 145 -5 | 15 19
gfz uuuuu | -21 35 34 -134 4 | 15 20
grg uuuux | -36 -8 13 -21 57 | -17 32
igr xxxxx | -54 43 66 23 -1 | 12 17
irf xxxxx | -20 -15 -30 43 -6 | 13 18
jpl uuuuu | -55 -20 57 53 -13 | 68 70
mit uuuuu | -19 -18 -151 78 -5 | 18 23
ngs uuuuu | 195 127 -37 -202 2 | 7 11
sio xxxxx | 31 -81 -246 -55 8 | 59 62
Table 7.1728.5 GPS week: 1728 Day: 5 MJD: 56345.500
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 | -16 10 44 80 -5 | 13 18
emr uuuuu | 18 -51 56 75 5 | 7 16
esa uuuuu | -52 -13 145 87 -4 | 17 19
gfz uuuuu | 67 28 -38 -54 4 | 18 21
grg uuuux | -1 29 -40 -126 100 | -13 35
igr xxxxx | -29 18 -48 -24 -1 | 14 18
irf xxxxx | 24 4 -30 57 -6 | 15 18
jpl uuuuu | 16 -21 -27 -85 -7 | 71 72
mit uuuuu | 80 29 -274 193 -7 | 21 23
ngs uuuuu | -41 -19 -33 -290 2 | 9 12
sio xxxxx | -48 58 -240 -60 7 | 65 66
Table 7.1728.6 GPS week: 1728 Day: 6 MJD: 56346.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -25 -42 6 19 -6 | 10 18
emr uuuuu | 23 -82 67 73 8 | 4 15
esa uuuuu | -94 19 80 59 1 | 13 18
gfz uuuuu | 60 15 39 -120 -5 | 16 20
grg uuuux | 15 -26 -87 -123 100 | -8 40
igr xxxxx | -14 10 59 12 -2 | 11 17
irf xxxxx | 39 -21 7 30 -6 | 11 17
jpl uuuuu | -33 -46 55 -14 -11 | 68 70
mit uuuuu | 102 -4 -151 211 -12 | 17 22
ngs uuuuu | 31 85 -60 -131 2 | 6 11
sio xxxxx | -49 36 -292 -105 3 | 64 65
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