[IGSREPORT-22882] Wk 1799 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jul 18 07:09:34 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1799 (Jun 29, 2014 - Jul 05, 2014)
Contacts: igs.acc 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:
igs1799[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1799[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1799[0-6].cls IGS GPS clock combination summary report.
igs17997.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17997.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 | EMR | 3
0 | ESA | WUHN UNSA WUHN
0 | GFZ | 1 2 6 30 1 6 30 YELL
0 | GRG | 3 6 3 6 HYDE WUHN HYDE WUHN
0 | JPL | 3
0 | MIT | 3 3 9 MDVJ
1 | EMR | 3 WUHN
1 | ESA | REUN REUN UNSA
1 | GFZ | 1 2 3 6 30 1 3 6 30 WUHN ZECK WUHN
1 | GRG | 3 6 3 6 BOR1 FAA1 IRKJ MAL2 NYAL FAA1 MAL2 NYAL
1 | JPL | NOVM
1 | MIT | 9 3 9 MDVJ TNML
2 | EMR | 27 3 27 WUHN
2 | ESA | UNSA
2 | GFZ | 1 2 3 6 30 1 3 6 30
2 | GRG | 3 6 3 6 KOUC NRMD NYAL QAQ1 SOFI WUHN XMIS KOUC NYAL
2 | GRG | QAQ1 SOFI WUHN XMIS
2 | JPL | 3 27
2 | MIT | 9 3 9 TLSE MDVJ TLSE
3 | COD | 3 WUHN WUHN
3 | ESA | 3 HOB2 HOB2 WUHN
3 | GFZ | 1 2 3 6 30 1 3 6 30 BOR1 IRKJ
3 | GRG | 6 6 FAA1 FAA1 IRKJ
3 | JPL | UNSA
3 | MIT | 9 27 6 9 27 SYOG MDVJ
3 | NGS | 9
4 | ALL | 30 9 30
4 | COD | 3 BRAZ KARR MDVJ
4 | EMR | 6
4 | ESA | 3 UNSA WUHN
4 | GFZ | 1 3 6 1 3 6 BJFS REUN WUHN BJFS CAS1 REUN WUHN
4 | GRG | 6 6 BRST IRKJ KOUC MDVJ NNOR NRMD BRST KOUC NNOR
4 | GRG | NRMD WES2
4 | MIT | FLIN KOUR MDVJ TLSE
5 | EMR | 9
5 | ESA | 3 FAA1
5 | GFZ | 1 2 3 6 30 1 3 6 30 DUBO KOUC MCM4 SCOR DUBO IRKJ
5 | GFZ | KOUC MCM4 NOVM SCOR
5 | GRG | 6 6 DUBO FAA1 IRKJ WUHN DUBO FAA1 SOFI WUHN
5 | JPL | 3
5 | MIT | 3 CORD FLIN IRKJ MDVJ
6 | ALL | 9
6 | COD | 3
6 | EMR | WUHN
6 | ESA | 3 BRFT UNSA
6 | GFZ | 1 2 6 30 1 3 6 30 BAKE BAKE
6 | GRG | 6 6 FAA1 QAQ1 FAA1 WUHN
6 | JPL | 3 8
6 | MIT | 9 HLFX RBAY
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
----+--------+---------------
0 | GRG | 6
1 | GRG | 6
2 | GRG | 6
3 | GRG | 6
4 | GRG | 6
5 | GRG | 6
6 | GRG | 6
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 G27 | 4 | 4 | 4 | 4 | 4 | 4 | 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 | -.4 1.4 -.2 -18 21 -39 .25
EMR | 0 | 4.0 -1.8 7.9 -15 10 -69 .24
ESA | 0 | .1 .8 -1.8 -2 -20 35 .09
GFZ | 0 | .0 .5 -2.1 -22 -22 -16 .36
GRG | 0 | 13.5 -17.2 27.0 7 17 -4 .70
JPL | 0 | -3.0 -6.7 19.2 -67 88 -42 -.44
MIT | 0 | -1.0 -6.3 20.8 10 2 -43 .26
NGS | 0 | -.4 -8.6 29.6 -125 -54 -33 .53
SIO | 0 | 1.2 -5.1 12.4 7 12 -4 .21
COD | 1 | -.4 .7 -.3 -40 18 -39 .32
EMR | 1 | 1.0 -7.5 9.0 -6 -5 -48 .16
ESA | 1 | -.2 .4 -2.0 -1 -20 34 .12
GFZ | 1 | -.2 .7 -1.6 -10 -23 -4 .13
GRG | 1 | 12.1 -19.7 27.4 -7 15 -8 .59
JPL | 1 | -2.5 -5.1 15.2 -92 5 -2 -.50
MIT | 1 | -1.0 -8.2 20.2 8 1 -46 .32
NGS | 1 | -5.0 -7.8 28.6 -118 -35 -58 .57
SIO | 1 | .4 -6.2 10.0 16 18 -2 .41
COD | 2 | -.4 .2 -.4 -55 21 -64 .38
EMR | 2 | 4.9 4.0 11.2 -3 12 -57 .33
ESA | 2 | .1 .5 -2.0 7 -23 33 .13
GFZ | 2 | .5 .1 -1.6 -23 -30 -14 .35
GRG | 2 | 16.7 -19.4 21.3 -3 14 -25 .85
JPL | 2 | -.7 1.5 12.5 -96 15 5 -.61
MIT | 2 | .4 -4.7 19.6 6 4 -44 .42
NGS | 2 | 3.2 -8.3 28.5 -114 -65 -12 .71
SIO | 2 | 3.9 -2.6 16.3 10 12 -10 .49
COD | 3 | -.2 .1 .0 -49 12 -54 .43
EMR | 3 | 5.9 -4.5 6.4 -11 4 -69 .28
ESA | 3 | .4 .4 -1.8 13 -4 22 .14
GFZ | 3 | .5 .2 -.7 -13 -25 -18 -.03
GRG | 3 | 20.4 -16.0 29.6 -4 -1 -26 .71
JPL | 3 | -3.8 5.6 10.5 -54 -18 37 -.47
MIT | 3 | 5.4 -7.8 17.1 6 11 -46 .47
NGS | 3 | 6.5 -6.0 25.7 -90 -68 15 .45
SIO | 3 | 8.8 -4.1 10.8 28 26 -15 .41
COD | 4 | -.8 -.5 -.1 -65 44 -55 .38
EMR | 4 | 4.1 -6.0 7.0 5 26 -84 .20
ESA | 4 | .5 .7 -2.2 -14 -19 20 .08
GFZ | 4 | .2 .1 -1.2 -13 -25 -23 .06
GRG | 4 | 11.3 -16.3 11.4 -8 8 -21 .84
JPL | 4 | -.5 3.1 4.8 -17 -1 43 -.32
MIT | 4 | 5.1 -10.8 17.9 -1 10 -46 .62
NGS | 4 | 6.3 -4.0 23.0 -97 -64 19 .66
SIO | 4 | 6.2 -8.6 6.7 4 35 -32 .52
COD | 5 | -.9 -.4 -.6 -53 21 -45 .21
EMR | 5 | 7.3 -4.9 3.1 0 10 -63 -.06
ESA | 5 | .3 .7 -1.8 -7 0 40 -.02
GFZ | 5 | .3 .4 -.5 -24 -34 -8 -.27
GRG | 5 | 24.9 -21.9 24.2 -26 21 -18 .66
JPL | 5 | .2 -5.3 8.5 -84 56 18 -.53
MIT | 5 | 7.4 -9.6 13.8 1 8 -48 .19
NGS | 5 | -1.3 -7.5 21.4 -85 -33 -32 .58
SIO | 5 | 1.2 -8.6 8.4 2 33 -11 .08
COD | 6 | -.9 .3 .3 -44 6 -33 .06
EMR | 6 | 7.9 -11.3 5.5 1 5 -76 -.01
ESA | 6 | -.3 1.3 -1.7 -6 -4 23 -.06
GFZ | 6 | -.7 .5 -.7 -29 -14 -32 -.19
GRG | 6 | 10.9 -21.0 30.5 -20 3 -6 .49
JPL | 6 | -3.0 -4.9 13.1 -103 18 19 -.62
MIT | 6 | 6.6 -15.0 19.0 13 1 -42 .19
NGS | 6 | 9.1 -13.1 22.8 -104 -56 13 .53
SIO | 6 | 3.3 -10.9 3.1 3 36 -41 .17
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 1.1799.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1799.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 2.1799.[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 3.1799.[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 5.1799.0-6). 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 1799 summary. (Jun 29, 2014 - Jul 05, 2014)
Table 1.1799.a GPS week: 1799 MJD: 56837.000-56843.000
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 250| -1 0 0 5 10 -5 .09 10 10 | -1410 524 15 106
| 0 0 2 22 15 11 .04 | 598 772
emr 80| 0 -1 -4 -26 -20 17 .18 12 12 | 2399 -164 15 127
| 1 0 1 21 15 13 .03 | 839 821
esa 150| 0 0 -7 5 6 -1 -.29 11 11 | -1009 -124 11 175
| 0 0 1 10 26 14 .03 | 1586 1563
gfz 198| 0 0 0 13 -11 -18 .04 11 10 | 13 108 13 144
| 0 0 1 17 13 14 .03 | 272 545
grg 188| 4 -1 13 37 -37 2 .24 17 15 | -252 297 17 154
| 1 0 2 16 21 11 .02 | 297 483
igr n/a| 0 0 -3 4 -1 -8 -.20 5 5 | -23 128 16 95
| 0 0 0 14 13 16 .03 | 955 664
jpl 80| 0 0 -8 -29 -1 7 -.06 13 12 | 2004 -189 18 147
| 0 0 1 21 16 21 .04 | 852 728
mit 300| 0 -1 5 -9 -11 17 -.07 12 10 | -326 191 20 205
| 0 0 1 27 20 15 .01 | 1160 2180
ngs 235| 0 1 6 6 37 -20 -.04 10 9 | -1118 305 1491 3096
| 0 0 1 54 44 23 .06 | 289 715
sio 481| 0 1 -6 -11 -9 12 -.78 16 15 | --- --- --- ---
| 0 0 2 19 23 18 .04 | --- ---
Table 1.1799.b GPS week : 1799 MJD: 56837.000-56843.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 5 4 4 4 |
2 | 5 5 5 5 5 5 5 |
3 | 6 6 6 5 6 5 6 |
4 | 3 4 4 4 4 4 3 |
5 | 4 5 4 4 4 4 4 |
6 | 9 10 8 12 12 9 10 |
7 | 5 5 4 5 5 4 5 |
8 | 3 3 3 4 4 3 3 |
9 | 9 15 17 18 16 12 17 |
10 | 3 4 3 3 3 3 4 |
11 | 5 5 4 5 5 4 5 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 5 5 5 |
14 | 4 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 5 4 5 5 5 4 5 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 3 4 4 |
21 | 5 5 5 5 5 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 5 4 5 |
24 | 5 5 4 5 5 5 6 |
25 | 4 4 4 4 4 4 5 |
26 | 4 5 4 4 3 4 4 |
27 | 5 5 7 8 6 5 5 |
28 | 4 4 4 5 4 4 5 |
29 | 5 5 4 5 5 6 5 |
30 | 4 4 4 4 49 4 4 |
31 | 5 5 5 4 5 5 5 |
32 | 3 3 3 3 3 4 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1799.0 GPS week: 1799 Day: 0 MJD: 56837.000
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 250| -1 0 -2 -5 12 1 .06 9 8 | -945 -281 14 89
emr 80| 0 0 -3 -8 -25 25 .18 11 11 | 1312 919 16 111
esa 150| 0 0 -8 1 11 -1 -.32 11 11 | -865 1102 12 188
gfz 196| -1 2 0 8 -3 -18 .05 11 11 | -395 309 17 175
grg 185| 3 -1 14 44 -31 12 .27 15 15 | -406 266 18 164
igr n/a| 0 0 -3 -3 -1 -16 -.23 5 5 | -1574 953 17 89
jpl 80| -1 0 -8 -8 4 -7 -.09 12 10 | 1354 716 18 157
mit 300| 0 0 7 -10 -23 10 -.08 13 11 | 714 -2303 19 208
ngs 236| 1 0 9 -8 36 -24 .03 10 9 | -1332 1080 1310 2945
sio 483| 1 1 -5 -13 -48 1 -.80 16 14 | --- --- --- ---
Table 2.1799.1 GPS week: 1799 Day: 1 MJD: 56838.000
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 252| 0 0 -3 -1 -19 -11 .08 10 11 | -1908 1076 16 105
emr 80| 0 -1 -3 -11 -41 21 .16 11 11 | 1931 645 16 120
esa 150| 0 0 -8 -1 -4 0 -.34 11 11 | 215 -1575 11 169
gfz 201| 0 0 -1 15 -25 -9 .01 11 10 | -187 46 13 131
grg 187| 3 -1 16 45 -40 -2 .26 15 15 | -397 508 17 159
igr n/a| 0 0 -4 9 0 -14 -.20 5 5 | -978 951 17 95
jpl 80| -1 0 -8 -57 0 9 -.13 12 11 | 1856 663 18 153
mit 300| 0 0 6 -21 11 -3 -.05 12 11 | -1648 1698 19 184
ngs 237| 0 1 7 25 99 -19 .04 11 10 | -752 -407 1510 2977
sio 479| 0 2 -5 -11 9 -21 -.80 16 16 | --- --- --- ---
Table 2.1799.2 GPS week: 1799 Day: 2 MJD: 56839.000
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 251| -1 0 0 -21 7 -12 .09 9 9 | -1290 492 16 100
emr 80| -2 0 -4 -56 -7 36 .14 12 12 | 3297 -91 16 121
esa 150| 0 0 -6 4 -9 12 -.28 10 10 | 391 -1953 9 150
gfz 198| 0 0 0 7 6 -5 .08 10 10 | 335 -459 14 143
grg 189| 4 -1 9 42 4 21 .24 15 15 | 195 -401 16 134
igr n/a| 0 0 -4 -21 12 -2 -.16 5 4 | 674 266 17 84
jpl 80| -1 0 -9 -48 -4 17 -.07 12 12 | 2967 -47 18 148
mit 300| 0 0 6 28 -10 16 -.05 12 10 | -148 -1194 19 209
ngs 237| 1 1 8 36 9 -58 -.05 9 8 | -852 508 1392 3571
sio 481| 0 1 -8 8 -23 13 -.81 16 16 | --- --- --- ---
Table 2.1799.3 GPS week: 1799 Day: 3 MJD: 56840.000
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 251| -1 1 -1 42 13 -16 .12 10 10 | -2404 1853 14 111
emr 80| 0 -1 -5 -4 -39 17 .17 14 12 | 3486 -239 14 127
esa 150| 0 2 -7 13 -16 -4 -.26 12 11 | -3232 1158 11 196
gfz 200| -1 0 0 9 -2 -28 .06 12 11 | 209 -237 13 167
grg 191| 4 0 15 25 -30 -9 .22 23 15 | -562 645 18 176
igr n/a| -1 0 -3 2 -17 -18 -.21 5 5 | 1069 -49 16 104
jpl 80| 1 0 -9 -9 -21 3 -.06 16 13 | 3000 -190 18 144
mit 300| 0 -1 4 -60 10 16 -.08 11 9 | -1641 3197 18 194
ngs 238| 0 1 5 -3 40 10 -.07 10 9 | -1246 -124 1192 2756
sio 480| -1 2 -6 -17 -8 28 -.82 16 15 | --- --- --- ---
Table 2.1799.4 GPS week: 1799 Day: 4 MJD: 56841.000
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 249| 0 0 1 26 27 5 .18 10 9 | -644 -317 17 124
emr 80| 0 -1 -5 -41 -10 0 .23 15 12 | 2956 -386 16 152
esa 150| 0 1 -6 -2 -15 -16 -.29 11 11 | -3021 1364 9 162
gfz 200| 0 1 0 21 -18 -13 .02 11 10 | -206 1217 13 129
grg 190| 4 -2 9 51 -49 -2 .25 22 16 | -492 997 16 155
igr n/a| -1 1 -4 20 7 25 -.19 6 5 | 658 -121 17 92
jpl 80| 0 0 -7 -8 -12 -6 -.04 14 13 | 2507 -466 18 154
mit 300| 0 -1 5 11 -22 24 -.08 11 9 | 971 -1995 19 206
ngs 234| 1 2 4 -49 63 -6 -.11 11 10 | -1484 1396 1744 3220
sio 485| 0 2 -9 16 10 32 -.76 16 14 | --- --- --- ---
Table 2.1799.5 GPS week: 1799 Day: 5 MJD: 56842.000
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 251| -1 0 0 -12 5 -14 .08 10 10 | -1547 677 17 102
emr 80| 1 -1 -7 -50 -18 21 .21 12 12 | 2071 -382 14 142
esa 150| 0 0 -5 -3 24 19 -.28 12 12 | 607 -1823 14 190
gfz 197| 0 0 0 -12 -30 -5 .01 9 10 | 189 33 13 138
grg 187| 6 -2 13 3 -59 -7 .25 17 16 | -212 277 18 134
igr n/a| -1 0 -2 7 -20 -4 -.16 6 5 | 100 -193 17 101
jpl 80| 0 1 -9 -44 29 -12 -.04 12 11 | 1600 -674 18 127
mit 300| 1 -1 5 -15 -45 47 -.07 11 10 | -1214 2212 24 227
ngs 236| 0 0 4 104 52 -37 -.06 9 8 | -859 -403 1636 3238
sio 486| 0 1 -3 -44 -20 16 -.71 14 14 | --- --- --- ---
Table 2.1799.6 GPS week: 1799 Day: 6 MJD: 56843.000
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 247| -1 0 2 14 24 12 .05 12 11 | -1135 170 17 111
emr 80| 0 0 -6 -13 -2 -3 .19 12 12 | 1746 -1618 14 122
esa 150| 0 0 -8 23 56 -19 -.27 11 11 | -1159 859 11 175
gfz 195| -2 1 -2 43 -5 -45 .06 11 10 | 152 -149 12 126
grg 190| 4 -2 14 47 -52 3 .23 16 14 | 109 -212 17 161
igr n/a| -1 0 -3 19 12 -25 -.24 6 5 | -112 -909 17 101
jpl 80| 0 1 -6 -30 -4 49 -.01 12 11 | 745 -1331 18 147
mit 300| 1 -1 5 0 -2 10 -.08 12 10 | 684 -274 23 213
ngs 232| 0 0 4 -56 -40 -3 -.08 10 9 | -1305 91 1658 2967
sio 475| 0 2 -5 -20 17 18 -.76 14 15 | --- --- --- ---
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 3.1799.0 GPS week: 1799 Day: 0 MJD: 56837.000
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 | 6 9 13 13 10 6 12 10 9 10 4 | 21 24 25 25 32 20 24 23 28 18 22
2 | 11 12 15 10 17 5 9 15 12 16 4 | 33 36 31 38 42 33 35 46 41 34 36
3E | 12 19 11 14 16 7 17 23 17 19 6 | 68 74 68 68 71 65 70 72 75 68 68
4 | 7 9 12 8 10 4 7 9 8 10 3 | 39 37 35 41 46 36 37 42 41 32 39
5 | 8 9 10 9 12 4 10 11 11 21 3 | 39 39 35 39 39 34 38 40 39 39 37
X6 | 15 --- 11 18 79 12 31 27 11 31 9 | 43 --- 44 38 71 36 37 40 35 38 36
7 | 8 12 9 13 15 5 16 12 9 14 4 | 29 30 23 35 34 26 28 28 30 25 27
8 | 8 8 8 10 7 4 7 8 9 21 3 | 25 31 25 27 26 24 27 23 29 31 25
X9 | 11 12 --- --- --- 30 --- 20 16 --- 8 | 26 28 --- --- --- 30 --- 31 24 --- 24
10 | 7 8 9 8 13 5 5 10 7 8 3 | 27 27 23 28 35 25 26 31 32 26 27
11 | 9 9 16 9 19 5 10 12 11 14 4 | 47 45 41 47 59 43 45 48 50 41 46
12 | 11 11 10 16 18 5 10 16 11 16 4 | 27 33 26 28 32 27 31 32 32 26 27
13 | 7 12 9 9 20 5 11 9 9 12 4 | 23 30 27 24 36 24 31 24 29 24 25
14 | 7 9 9 11 17 5 9 14 7 18 4 | 31 31 30 31 36 29 31 28 31 24 29
15 | 9 12 12 10 20 3 13 11 10 20 4 | 29 31 26 28 30 25 31 26 26 26 26
16 | 10 14 9 14 13 7 13 11 10 24 4 | 27 30 24 24 28 22 27 23 28 28 24
17E | 10 8 8 11 13 5 17 13 11 17 4 | 52 52 50 55 58 50 48 52 57 52 51
18 | 7 7 13 17 11 5 9 17 9 21 4 | 20 25 23 22 26 20 24 32 29 23 22
19E | 6 11 5 11 13 4 11 11 6 15 3 | 35 37 31 38 42 32 31 35 38 27 34
20 | 8 7 9 9 11 6 8 9 12 16 3 | 22 20 21 23 24 21 19 21 27 19 20
21 | 9 12 15 9 15 6 11 14 10 19 4 | 38 41 32 41 48 37 39 45 43 33 39
22 | 6 6 12 12 12 5 9 12 9 13 3 | 22 24 21 25 29 20 23 31 28 23 23
23 | 9 11 8 11 14 6 13 11 10 18 4 | 27 32 30 25 31 26 33 26 33 26 27
24 | 10 8 14 11 13 5 14 13 10 10 4 | 30 32 32 31 31 29 34 31 29 28 30
25 | 10 10 13 10 15 5 12 12 8 12 4 | 24 29 29 29 30 26 28 27 28 24 26
26 | 7 9 13 11 12 5 8 16 12 14 4 | 26 33 27 27 26 25 29 30 27 27 27
X27E | 6 10 16 16 --- 6 10 8 13 12 4 | 252 249 251 254 --- 250 249 253 254 253 251
28 | 8 11 11 16 17 5 11 7 10 19 4 | 25 30 21 26 34 21 24 22 27 24 23
29E | 10 14 8 11 17 6 20 10 12 9 5 | 49 49 46 54 49 46 47 51 52 42 48
X30 | 6 8 12 9 --- 5 13 12 9 13 4 | 28 33 31 24 --- 28 33 31 29 31 28
31 | 9 10 10 10 19 6 15 15 8 11 4 | 29 31 23 31 36 26 29 28 28 24 27
32 | 6 8 9 11 9 4 6 11 10 16 3 | 24 21 21 19 24 19 21 24 26 23 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 11 11 15 5 12 13 10 16 |T 38 40 37 40 38 36 39 40 41 37 37
WRMS | 8 11 11 11 15 5 10 11 9 14 |NE 28 30 27 29 35 27 30 30 31 27 28
MEDI | 8 10 11 11 14 5 11 12 10 16 |MD 28 31 29 29 34 26 31 31 29 27 27
Table 3.1799.1 GPS week: 1799 Day: 1 MJD: 56838.000
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 12 12 10 11 4 12 8 11 12 4 | 23 26 19 22 32 19 25 21 29 14 22
2 | 11 13 14 9 16 7 11 16 9 17 4 | 24 36 28 31 38 28 33 37 33 26 30
3E | 12 20 13 15 14 7 16 20 18 22 6 | 60 69 61 62 67 58 61 59 63 55 61
4 | 6 7 12 5 12 4 9 12 10 11 3 | 36 40 38 38 44 39 39 42 46 31 39
5 | 17 10 11 10 14 4 12 12 11 18 4 | 35 29 22 29 29 23 29 26 27 23 26
X6 | 16 --- 13 18 80 10 37 29 14 30 10 | 41 --- 40 37 48 32 40 33 35 39 32
7 | 8 16 9 12 16 5 15 10 11 16 4 | 27 32 20 30 34 25 29 26 30 21 26
8 | 9 8 8 10 11 4 8 7 8 20 3 | 25 26 21 21 23 20 25 19 27 26 22
X9 | 21 18 --- --- --- 18 --- 18 37 --- 14 | 24 29 --- --- --- 26 --- 28 39 --- 24
10 | 10 9 8 9 14 5 5 7 11 10 3 | 27 22 20 24 25 19 20 23 23 18 21
11 | 8 8 16 9 21 4 11 9 11 15 4 | 33 38 32 37 50 34 35 37 42 29 36
12 | 9 12 9 14 20 4 13 12 12 16 4 | 25 31 25 26 32 23 29 29 28 24 26
13 | 9 12 11 9 21 5 12 8 10 15 4 | 25 29 25 25 37 23 30 22 27 22 24
14 | 18 9 8 14 20 4 13 13 10 14 5 | 35 32 27 30 37 28 32 30 31 24 29
15 | 10 14 11 11 21 4 14 10 13 19 5 | 27 34 23 28 37 24 28 25 26 22 26
16 | 11 13 10 13 15 7 13 7 12 26 4 | 27 28 22 26 28 21 25 21 27 21 23
17E | 9 10 10 9 17 6 14 17 10 15 4 | 46 45 42 46 56 44 42 42 52 36 45
18 | 7 9 13 14 11 3 10 16 8 15 4 | 26 26 22 16 29 20 22 30 20 21 22
19E | 6 10 7 12 14 5 9 9 11 17 3 | 32 34 27 36 40 29 31 30 36 23 31
20 | 10 8 10 9 11 3 8 8 13 20 3 | 25 21 19 24 22 20 18 19 32 14 20
21 | 13 13 16 9 16 5 13 14 12 18 5 | 36 37 31 34 42 32 37 35 34 28 33
22 | 9 8 12 12 10 3 11 11 10 11 4 | 26 23 20 18 27 20 22 24 19 16 20
23 | 11 11 10 10 14 5 13 10 10 18 4 | 25 30 22 20 31 21 27 22 28 23 23
24 | 10 11 14 11 14 4 16 11 10 12 4 | 33 33 35 30 34 29 33 31 30 27 31
25 | 10 8 12 10 15 4 12 11 8 12 4 | 23 30 30 30 31 25 30 26 27 26 27
26 | 10 11 12 13 13 6 9 20 11 19 5 | 29 34 29 27 29 25 28 27 28 26 27
X27E | 10 11 16 17 --- 6 12 9 12 17 5 | 296 297 301 299 --- 297 293 295 298 295 297
28 | 11 11 10 13 12 5 10 6 12 19 4 | 31 29 21 23 32 21 26 23 26 20 24
29E | 12 12 7 13 15 5 16 9 11 12 4 | 43 43 41 46 47 41 43 43 48 33 43
X30 | 6 8 12 7 --- 3 11 12 8 14 4 | 32 29 33 28 --- 29 36 27 33 28 30
31 | 12 8 8 12 19 4 13 11 9 14 4 | 28 29 23 27 38 23 29 24 27 22 25
32 | 7 6 9 8 9 4 5 7 8 15 3 | 24 21 18 17 24 17 19 20 25 14 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 11 11 15 5 12 12 11 16 |T 39 40 36 38 35 35 39 37 40 33 37
WRMS | 11 11 11 10 15 5 11 11 10 16 |NE 28 29 25 26 33 24 28 26 29 23 26
MEDI | 10 11 11 11 14 4 12 11 11 16 |MD 27 30 25 28 34 25 29 27 29 24 26
Table 3.1799.2 GPS week: 1799 Day: 2 MJD: 56839.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 12 12 15 11 6 11 10 11 9 4 | 22 27 24 24 31 21 25 22 28 16 22
2 | 9 14 13 9 15 5 12 14 10 16 4 | 30 35 28 31 33 29 31 37 28 28 29
3E | 11 18 11 12 15 9 16 20 15 18 5 | 61 69 62 62 72 58 61 61 63 57 62
4 | 6 8 10 8 11 4 11 10 9 11 3 | 32 32 31 32 36 29 33 35 32 27 32
5 | 7 9 9 7 11 4 12 10 8 15 3 | 31 35 28 32 33 29 33 32 31 32 30
X6 | 16 --- 13 20 81 10 --- 22 11 35 8 | 39 --- 35 32 57 30 --- 32 27 32 32
7 | 8 16 9 10 15 5 16 10 7 16 4 | 27 32 21 29 33 23 27 26 23 22 25
8 | 9 8 8 9 11 4 7 8 8 20 3 | 25 28 24 24 25 22 24 21 20 28 23
X9 | 24 25 --- --- --- 36 --- 18 40 --- 16 | 27 26 --- --- --- 26 --- 27 52 --- 27
10 | 9 8 7 7 14 3 6 8 7 11 3 | 28 24 22 23 28 22 23 26 23 23 23
11 | 8 11 15 10 20 4 7 9 10 11 4 | 40 44 38 42 52 37 40 41 42 35 40
12 | 11 16 9 13 17 5 13 13 13 17 5 | 27 34 25 27 33 25 30 30 29 26 27
13 | 9 11 10 8 21 3 11 9 6 13 4 | 23 29 23 23 37 22 28 21 22 22 23
14 | 9 13 10 12 20 4 16 14 8 17 4 | 31 40 28 26 32 30 34 26 28 26 28
15 | 7 11 10 11 18 4 16 11 13 22 4 | 29 31 26 29 33 26 33 25 28 29 26
16 | 11 15 8 15 17 8 13 9 9 25 4 | 30 32 25 26 30 23 28 24 27 25 25
17E | 9 11 7 9 16 5 17 15 9 12 4 | 46 45 41 49 51 42 46 37 47 36 44
18 | 8 11 11 11 11 3 10 19 10 20 4 | 25 28 25 22 24 23 24 29 28 21 24
19E | 5 10 6 9 12 5 9 12 10 14 3 | 34 34 31 37 39 31 31 34 37 27 33
20 | 9 8 8 10 12 3 9 7 8 18 3 | 23 19 19 24 20 18 18 18 23 17 19
21 | 9 15 12 10 16 4 14 13 11 18 4 | 39 43 33 40 39 35 35 37 43 32 37
22 | 8 9 10 8 11 4 11 11 7 12 3 | 26 27 24 22 25 22 26 26 27 21 24
23 | 9 14 10 8 14 4 12 11 7 19 4 | 22 29 23 22 27 22 27 23 22 24 22
24 | 9 11 14 11 13 3 14 9 11 9 4 | 29 29 32 25 32 25 26 26 24 25 26
25 | 11 10 12 7 14 3 13 9 10 11 4 | 23 30 29 26 31 25 31 24 26 23 26
26 | 10 9 9 7 10 5 9 18 6 16 4 | 24 29 28 26 26 24 26 28 24 28 25
X27E | 10 18 13 19 --- 7 19 22 19 17 7 | 242 242 244 243 --- 243 235 242 246 234 243
28 | 12 16 10 13 16 5 9 7 6 19 4 | 26 33 21 25 33 21 25 22 23 23 23
29E | 10 13 6 9 15 5 19 9 9 10 4 | 47 47 42 48 46 43 41 46 50 39 45
X30 | 7 8 12 8 --- 5 11 11 10 14 4 | 27 28 32 27 --- 24 31 22 24 24 26
31 | 9 11 9 9 23 7 16 9 10 9 4 | 24 31 20 26 40 24 29 25 22 23 24
32 | 8 6 7 9 10 5 8 9 9 15 3 | 22 23 20 19 24 16 20 22 19 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 10 10 15 5 12 12 9 16 |T 36 39 35 36 35 34 37 35 37 33 35
WRMS | 9 12 10 10 15 4 12 10 8 16 |NE 27 30 26 27 32 24 28 26 27 25 26
MEDI | 9 11 10 9 15 5 12 10 9 16 |MD 27 31 28 26 33 25 29 26 27 26 26
Table 3.1799.3 GPS week: 1799 Day: 3 MJD: 56840.000
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 13 14 12 10 5 12 10 12 9 4 | 19 27 21 26 32 20 25 20 27 16 22
2 | 9 14 15 9 16 4 13 12 10 17 4 | 38 39 31 37 42 35 33 42 37 29 36
3E | 8 14 11 12 15 8 17 13 13 15 5 | 56 65 58 55 64 54 62 53 61 55 58
4 | 8 9 13 8 12 3 8 6 7 13 3 | 36 36 33 37 46 35 33 37 37 27 36
5 | 6 11 11 9 12 3 9 8 8 13 3 | 33 36 31 36 36 31 34 35 33 34 33
6 | 21 42 18 20 87 11 56 23 13 33 12 | 36 47 35 37 54 30 63 33 33 37 32
7 | 9 15 11 13 17 5 16 8 9 16 4 | 35 33 27 38 36 28 30 31 31 26 30
8 | 9 8 10 9 13 4 9 6 10 19 3 | 26 28 24 26 23 20 26 21 24 27 23
X9 | 30 24 --- --- --- 17 --- 21 43 --- 18 | 24 38 --- --- --- 26 --- 31 58 --- 27
10 | 9 8 9 12 13 2 5 6 6 9 3 | 27 23 20 21 31 20 21 24 25 18 22
11 | 10 10 18 9 21 6 10 10 11 12 4 | 41 44 38 45 55 41 41 43 45 38 42
12 | 9 12 12 15 20 5 14 10 9 17 4 | 29 36 27 27 32 25 32 30 28 29 27
13 | 9 11 12 10 20 5 12 6 8 14 4 | 30 31 31 23 36 24 33 24 27 24 26
14 | 10 12 9 13 18 5 16 11 8 16 4 | 31 36 30 32 35 29 35 31 30 29 30
15 | 7 10 13 12 20 5 15 10 9 16 4 | 31 33 26 31 32 24 30 26 29 24 27
16 | 10 16 10 16 19 8 13 9 10 22 4 | 30 32 24 28 28 22 27 23 25 25 24
17E | 8 12 8 11 26 6 12 10 11 12 4 | 52 46 46 52 69 47 48 45 53 42 49
18 | 9 10 11 18 10 4 10 20 10 19 5 | 20 23 23 21 26 15 23 29 22 22 20
19E | 8 12 8 13 16 5 11 9 8 10 4 | 35 37 33 40 41 33 31 36 37 29 35
20 | 11 9 10 8 10 4 7 9 11 15 3 | 23 18 16 20 22 17 16 18 23 13 16
21 | 10 14 13 11 18 5 16 16 11 18 5 | 37 40 33 41 46 34 40 42 40 33 37
22 | 8 8 10 11 12 6 9 10 8 15 3 | 19 24 20 25 26 16 19 24 22 19 20
23 | 10 13 10 11 16 4 13 10 9 18 4 | 32 34 31 23 31 26 34 26 33 27 28
24 | 8 16 15 11 13 4 14 8 8 12 4 | 29 34 32 28 32 26 31 29 28 23 28
25 | 10 10 12 10 14 4 14 9 8 8 4 | 26 33 31 31 33 26 32 28 28 25 28
26 | 11 9 11 6 11 6 7 14 8 17 3 | 28 34 28 27 25 25 28 27 31 26 26
X27E | 15 19 20 10 --- 12 25 16 19 25 7 | 401 405 400 405 --- 398 400 402 409 405 403
28 | 11 14 13 15 19 4 10 6 10 22 4 | 28 29 22 27 31 20 25 21 24 23 23
29E | 8 13 6 11 17 4 20 7 11 9 4 | 52 48 44 52 42 44 45 50 55 41 48
X30 | 8 10 14 10 --- 4 11 8 10 16 4 | 33 28 34 32 --- 24 32 27 30 28 27
31 | 9 10 9 11 21 5 14 7 10 9 4 | 30 34 25 31 42 27 30 26 26 28 27
32 | 9 7 9 9 14 4 8 7 7 17 3 | 20 18 16 16 22 13 20 17 18 15 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 12 12 23 5 16 11 10 16 |T 43 45 41 44 36 39 44 42 44 39 41
WRMS | 10 12 11 11 15 5 13 9 9 15 |NE 29 32 27 29 34 25 30 28 30 25 27
MEDI | 9 12 11 11 16 5 12 9 10 16 |MD 30 34 31 31 33 26 32 29 30 27 27
Table 3.1799.4 GPS week: 1799 Day: 4 MJD: 56841.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 9 14 13 13 5 11 9 9 8 4 | 18 25 20 19 29 16 25 19 24 13 19
2 | 9 12 13 9 18 5 11 11 10 19 4 | 32 37 32 36 37 31 33 40 39 27 34
3E | 13 19 13 11 20 7 17 13 10 16 5 | 56 66 58 56 57 55 63 51 58 57 56
4 | 7 8 11 8 11 4 12 7 13 11 3 | 34 34 30 33 34 28 32 32 30 22 32
5 | 9 10 10 9 12 4 9 9 10 15 3 | 37 36 32 37 36 31 34 34 34 32 34
6 | 19 53 13 21 83 14 37 27 17 33 12 | 33 60 34 36 50 26 41 36 25 32 31
7 | 10 14 9 10 15 6 18 10 9 17 4 | 30 32 24 32 36 28 31 29 32 26 28
8 | 9 8 8 11 10 6 7 8 11 18 3 | 24 29 24 25 24 22 25 21 31 26 23
X9 | 32 17 --- --- --- 20 --- 26 33 --- 16 | 33 33 --- --- --- 23 --- 30 45 --- 28
10 | 8 10 7 7 15 5 7 6 6 12 3 | 28 28 24 28 26 22 25 23 22 20 24
11 | 10 10 18 10 23 6 10 8 10 11 4 | 38 42 33 40 51 36 40 37 40 32 38
12 | 9 12 11 13 19 5 12 8 11 19 4 | 29 34 26 28 32 26 30 31 32 28 28
13 | 9 16 9 10 21 4 12 9 6 12 4 | 23 31 25 21 37 22 31 24 27 22 24
14 | 11 12 9 10 16 4 16 9 12 13 4 | 30 33 29 27 36 27 33 27 26 21 28
15 | 8 13 11 12 19 5 14 11 15 17 4 | 30 35 26 31 36 26 32 28 32 27 29
16 | 12 16 12 14 19 9 12 12 15 21 5 | 29 33 27 25 27 21 28 22 23 24 24
17E | 12 12 8 10 20 5 14 12 12 15 4 | 56 55 52 56 67 52 53 54 57 52 54
18 | 6 8 10 15 12 5 8 18 8 13 4 | 28 29 29 24 25 25 28 33 28 21 27
19E | 8 12 7 10 17 4 12 13 8 9 4 | 36 36 31 37 37 30 32 34 36 24 33
20 | 10 9 9 6 13 4 7 9 6 19 3 | 27 22 19 22 19 18 19 22 20 19 20
21 | 13 15 13 11 16 5 11 13 10 18 4 | 39 39 32 41 41 33 39 40 35 28 36
22 | 7 10 10 9 10 3 7 10 10 9 3 | 29 28 26 25 28 23 27 25 27 20 25
23 | 11 14 10 10 15 4 13 10 9 17 4 | 25 31 26 21 29 22 31 24 26 23 24
24 | 10 16 14 11 16 4 13 6 14 13 4 | 35 36 34 32 37 30 35 32 32 31 32
25 | 10 9 12 10 14 5 11 10 9 10 4 | 28 33 31 32 31 27 32 29 29 25 29
26 | 7 9 9 7 13 8 9 6 11 21 3 | 28 33 28 26 26 23 30 26 23 34 26
X27E | 8 12 15 17 --- 6 13 12 13 13 5 | 171 169 171 171 --- 168 165 171 168 169 169
28 | 10 12 12 12 18 4 14 7 7 21 4 | 26 30 22 26 31 21 28 24 23 20 23
29E | 8 13 6 11 21 4 19 7 10 9 4 | 46 45 40 47 46 41 41 47 48 40 44
X30 | 48 --- --- 50 --- 32 --- --- --- --- 49 | 37 --- --- 68 --- 24 --- --- --- --- 33
31 | 11 9 12 10 23 5 13 8 11 12 4 | 34 37 26 33 39 27 33 28 26 26 30
32 | 8 7 11 6 10 4 7 9 10 13 3 | 22 24 21 18 22 18 21 21 23 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 11 11 22 6 14 11 11 16 |T 36 39 34 37 35 31 37 35 36 32 34
WRMS | 9 12 11 10 16 5 13 9 10 14 |NE 29 33 27 30 32 25 30 28 29 24 27
MEDI | 9 12 11 10 16 5 12 9 10 13 |MD 30 33 28 32 36 26 32 29 30 26 28
Table 3.1799.5 GPS week: 1799 Day: 5 MJD: 56842.000
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 | 6 10 12 8 12 5 11 9 9 10 3 | 17 21 19 18 25 14 25 15 23 10 18
2 | 10 15 16 9 18 7 12 12 10 16 4 | 26 31 25 29 29 25 26 28 32 19 25
3E | 11 16 14 7 15 7 16 19 8 19 5 | 55 64 57 54 61 51 59 48 58 57 55
4 | 7 10 12 8 11 3 11 9 10 10 3 | 33 30 30 30 33 30 29 29 34 24 30
5 | 8 13 11 8 15 6 10 8 11 15 4 | 32 35 26 30 27 26 27 26 35 25 28
X6 | 13 --- 11 20 83 8 35 25 10 29 9 | 31 --- 29 34 41 26 37 34 30 30 26
7 | 8 14 10 12 15 4 14 10 9 12 4 | 28 29 20 29 32 23 26 26 30 18 24
8 | 7 8 10 7 12 5 10 9 8 16 3 | 22 25 22 20 21 18 24 18 27 22 20
X9 | 25 19 --- --- --- 27 --- 14 20 --- 12 | 30 26 --- --- --- 29 --- 28 38 --- 23
10 | 8 8 11 8 14 4 6 4 6 8 3 | 24 20 19 22 20 19 19 19 25 15 19
11 | 7 14 16 7 21 5 10 10 7 11 4 | 29 33 26 31 42 28 30 30 29 27 28
12 | 10 16 10 12 19 7 13 12 11 16 4 | 22 33 23 24 32 21 28 24 30 21 24
13 | 11 11 11 12 19 6 15 10 10 13 4 | 25 26 24 19 34 20 29 21 31 18 22
14 | 12 12 11 11 20 4 10 10 10 12 4 | 32 32 28 31 37 28 29 26 29 22 28
15 | 9 11 12 11 19 5 14 10 12 17 4 | 27 27 22 27 33 19 25 22 24 19 22
16 | 13 13 12 10 19 8 11 9 10 22 4 | 23 26 21 19 25 18 23 18 29 17 20
17E | 11 12 8 10 22 5 13 13 9 13 4 | 57 50 48 55 50 50 50 48 54 45 51
18 | 12 8 12 10 12 6 8 16 7 14 4 | 21 21 21 13 21 15 19 24 23 15 17
19E | 7 12 8 8 18 5 12 10 10 13 4 | 27 28 26 30 31 24 24 27 30 19 26
20 | 10 10 9 13 14 5 8 11 7 16 4 | 24 16 19 27 18 18 15 16 23 14 17
21 | 12 18 14 11 17 7 14 15 9 14 5 | 22 32 23 25 35 21 32 27 27 20 24
22 | 10 7 11 7 12 5 9 12 8 10 3 | 15 18 18 13 21 14 18 15 23 11 14
23 | 9 12 10 8 15 4 14 11 8 17 4 | 25 28 25 20 27 19 26 20 30 20 22
24 | 12 18 13 8 19 5 13 9 9 10 4 | 29 34 32 29 34 28 31 30 31 29 29
25 | 7 11 14 7 16 5 12 13 7 12 4 | 22 29 28 25 29 22 28 20 24 21 23
26 | 10 10 12 6 15 6 9 7 7 15 3 | 24 31 22 22 24 19 24 23 25 23 22
X27E | 8 9 15 13 --- 6 11 9 9 16 4 | 238 237 241 237 --- 236 233 235 240 236 237
28 | 10 13 12 14 15 4 11 6 9 18 4 | 24 29 20 28 27 19 24 21 28 18 22
29E | 10 15 9 9 18 7 18 19 15 15 5 | 55 53 47 50 51 46 44 55 51 47 49
X30 | 6 9 12 7 --- 4 12 10 8 13 3 | 29 29 33 44 --- 32 31 28 36 27 35
31 | 17 10 13 9 22 8 16 8 7 12 5 | 30 28 16 20 39 21 27 21 25 13 22
32 | 13 8 11 5 12 4 9 7 8 12 3 | 22 16 16 15 19 14 18 15 24 13 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 12 9 17 6 12 11 9 14 |T 35 36 33 34 31 31 34 32 37 29 32
WRMS | 10 12 12 10 16 5 11 10 8 14 |NE 25 27 23 24 29 21 25 23 28 19 22
MEDI | 10 12 12 9 16 5 12 10 9 14 |MD 26 29 24 27 31 21 27 24 29 20 23
Table 3.1799.6 GPS week: 1799 Day: 6 MJD: 56843.000
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 | 11 9 13 11 11 4 10 7 8 10 3 | 26 26 22 25 32 19 25 21 22 14 23
2 | 14 16 12 8 16 6 13 13 9 18 4 | 38 43 36 43 47 38 36 48 44 35 40
3E | 13 14 14 10 16 8 14 24 10 18 5 | 59 67 62 54 66 56 64 54 56 61 58
4 | 5 10 10 8 10 4 9 7 7 9 3 | 37 36 34 38 44 34 34 38 37 30 36
5 | 9 12 9 9 9 5 10 10 14 16 4 | 39 42 36 42 42 37 40 41 38 41 38
X6 | 15 --- 12 19 80 11 37 22 13 25 9 | 37 --- 34 35 60 29 45 32 27 33 29
7 | 9 16 8 10 15 7 16 11 9 12 4 | 34 35 28 37 39 33 34 32 32 29 31
8 | 8 8 8 9 11 5 7 9 10 18 3 | 23 29 25 25 24 23 30 21 23 25 23
X9 | 30 14 --- --- --- 35 --- 31 33 --- 16 | 28 31 --- --- --- 21 --- 34 43 --- 29
10 | 16 9 7 7 10 4 7 5 8 9 3 | 36 24 24 29 31 23 23 26 23 21 25
11 | 11 10 15 9 21 7 10 10 12 11 4 | 44 44 40 47 57 42 45 45 45 40 44
12 | 12 16 11 16 16 8 13 10 9 16 5 | 29 35 30 33 34 29 31 30 30 29 29
13 | 16 16 10 10 22 5 14 14 11 14 5 | 25 35 31 24 38 26 35 26 30 27 26
14 | 10 8 10 13 19 7 10 10 14 11 4 | 32 34 33 31 32 33 35 28 34 27 31
15 | 10 12 13 11 18 4 16 10 11 16 4 | 29 33 28 29 33 27 35 26 28 27 28
16 | 11 14 13 11 17 5 11 11 8 18 4 | 29 31 27 25 29 23 29 23 26 21 25
17E | 12 11 8 13 19 6 14 12 13 9 4 | 60 58 55 62 65 54 55 54 63 51 57
18 | 12 6 12 16 12 5 8 14 8 17 4 | 22 25 24 23 28 21 26 31 24 22 23
19E | 9 13 8 9 15 5 13 8 10 7 4 | 42 39 38 41 43 36 34 38 41 29 38
20 | 7 9 8 12 12 5 10 11 7 16 3 | 21 17 19 29 22 18 20 19 18 16 18
21 | 14 14 13 10 17 6 14 13 8 18 5 | 41 44 37 46 51 40 43 45 42 36 42
22 | 10 6 10 8 11 5 6 13 9 10 3 | 22 24 22 23 28 19 24 26 21 20 22
23 | 16 14 10 10 17 4 15 11 9 19 4 | 26 36 33 25 32 27 38 25 26 28 27
24 | 15 14 15 12 16 8 14 17 10 11 5 | 76 73 72 73 76 68 75 76 71 72 73
25 | 12 11 14 12 12 10 13 10 8 12 4 | 29 34 33 34 33 29 34 29 29 27 30
26 | 12 10 9 10 12 4 10 15 9 17 4 | 25 35 27 27 24 25 30 29 30 28 27
X27E | 15 9 14 17 --- 6 11 7 10 14 5 | 223 227 228 225 --- 227 224 226 227 228 226
28 | 11 12 10 16 16 6 12 8 12 18 4 | 25 29 22 28 32 20 26 22 24 22 22
29E | 12 16 8 9 18 6 18 12 14 13 5 | 59 54 52 56 53 52 49 59 57 52 54
X30 | 7 8 11 8 --- 7 11 11 13 13 4 | 26 28 31 31 --- 27 33 26 28 25 28
31 | 10 8 11 11 24 6 15 8 9 13 4 | 37 36 27 35 42 32 37 30 31 27 32
32 | 10 7 10 7 13 5 7 8 6 13 3 | 20 21 19 19 24 17 21 18 18 15 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 11 11 16 6 12 12 10 14 |T 40 42 39 41 40 37 42 39 40 37 39
WRMS | 11 12 11 10 14 5 11 10 9 15 |NE 31 33 30 32 37 28 34 31 31 28 30
MEDI | 11 11 10 10 16 6 12 11 9 14 |MD 29 35 31 33 34 29 34 30 30 28 29
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 4.1799 GPS week: 1799 MJD: 56837.0-56843.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 |U 7 6 19 |U 21 33 80 |U 10 12 19 |
emr | emr 2980 | 9 8 25 |U 22 33 82 | 11 11 22 |
esa | esa 2962 | 10 9 24 |U 21 33 80 | 10 12 21 |
gfz | gfz 2966 |U 9 8 20 |U 21 32 79 |U 10 12 20 |
grg | grg 2784 |U 10 8 23 |U 10 11 36 |U 12 12 24 |
igr | igr 3011 | 8 6 20 | 21 32 78 | 10 13 21 |
igs | igs 2971 | 9 8 20 | 21 32 80 | 10 12 21 |
jpl | jpl 2944 | 11 9 26 |U 21 33 80 |U 11 12 25 |
mit | mit 3058 | 21 20 56 |U 21 33 82 |U 11 13 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 5.1799.0 GPS week: 1799 Day: 0 MJD: 56837.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 8 8 20 | 5 6 18 | 8 5 18 |
emr | emr 2966 | 9 5 27 | 5 6 19 | 10 5 21 |
esa | esa 2976 | 7 7 25 | 5 6 18 | 8 5 18 |
gfz | gfz 2971 | 8 7 22 | 5 5 15 | 8 5 21 |
grg | grg 2784 | 10 6 20 | 7 10 21 | 9 6 22 |
igr | igr 3032 | 7 8 23 | 4 4 15 | 8 6 19 |
igs | igs 3013 | 8 6 23 | 4 5 16 | 8 5 19 |
jpl | jpl 2972 | 8 6 30 | 5 6 18 | 9 7 22 |
mit | mit 3072 | 18 27 97 | 5 5 20 | 10 7 23 |
Table 5.1799.1 GPS week: 1799 Day: 1 MJD: 56838.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3038 | 8 6 17 | 7 8 25 | 10 11 18 |
emr | emr 2972 | 11 8 25 | 7 6 25 | 9 9 20 |
esa | esa 2976 | 9 7 17 | 6 8 24 | 9 11 17 |
gfz | gfz 2972 | 8 4 16 | 6 5 21 | 9 11 18 |
grg | grg 2784 | 14 9 23 | 8 7 27 | 12 12 25 |
igr | igr 3021 | 8 6 18 | 5 5 22 | 10 12 19 |
igs | igs 2990 | 9 6 16 | 6 5 23 | 9 11 18 |
jpl | jpl 2972 | 11 9 16 | 6 5 23 | 9 10 20 |
mit | mit 3072 | 22 12 25 | 7 7 25 | 10 11 18 |
Table 5.1799.2 GPS week: 1799 Day: 2 MJD: 56839.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3018 | 6 4 13 | 6 7 18 | 8 15 19 |
emr | emr 2969 | 9 7 20 | 7 7 23 | 8 9 22 |
esa | esa 2976 | 7 4 20 | 5 7 19 | 8 14 21 |
gfz | gfz 2973 | 6 4 15 | 6 7 19 | 8 12 20 |
grg | grg 2784 | 9 8 21 | 8 9 22 | 11 13 25 |
igr | igr 3009 | 7 3 15 | 5 6 17 | 8 14 21 |
igs | igs 2957 | 6 4 15 | 6 6 21 | 8 13 20 |
jpl | jpl 2876 | 11 15 27 | 6 7 21 | 9 12 24 |
mit | mit 3072 | 35 40 97 | 5 6 22 | 8 13 21 |
Table 5.1799.3 GPS week: 1799 Day: 3 MJD: 56840.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 6 9 12 | 112 190 422 | 19 20 28 |
emr | emr 3066 | 8 7 15 | 113 192 423 | 19 19 29 |
esa | esa 2976 | 19 21 21 | 112 191 423 | 18 20 29 |
gfz | gfz 2972 | 18 21 15 | 112 188 420 | 18 21 29 |
grg | grg 2784 | 7 6 14 | 22 24 85 | 18 19 30 |
igr | igr 3032 | 7 7 12 | 112 189 421 | 18 21 30 |
igs | igs 2993 | 18 21 15 | 112 190 421 | 18 21 30 |
jpl | jpl 2972 | 7 5 17 | 111 188 416 | 19 22 36 |
mit | mit 3072 | 22 13 36 | 111 189 418 | 18 21 27 |
Table 5.1799.4 GPS week: 1799 Day: 4 MJD: 56841.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2995 | 6 5 23 | 8 10 34 | 11 13 17 |
emr | emr 2958 | 8 8 31 | 7 9 36 | 11 12 21 |
esa | esa 2880 | 7 6 25 | 7 9 35 | 11 14 23 |
gfz | gfz 2930 | 6 5 21 | 8 9 33 | 11 14 19 |
grg | grg 2784 | 8 8 26 | 10 11 36 | 11 13 25 |
igr | igr 2920 | 7 6 24 | 7 9 32 | 11 14 21 |
igs | igs 2877 | 7 6 22 | 7 10 36 | 11 13 20 |
jpl | jpl 2876 | 9 9 28 | 8 8 36 | 12 13 26 |
mit | mit 2976 | 20 12 46 | 8 10 37 | 13 13 24 |
Table 5.1799.5 GPS week: 1799 Day: 5 MJD: 56842.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3021 | 9 6 27 | 7 6 21 | 10 10 18 |
emr | emr 2968 | 11 11 29 | 7 6 21 | 10 8 21 |
esa | esa 2976 | 12 11 33 | 7 6 21 | 9 9 18 |
gfz | gfz 2972 | 9 6 28 | 6 7 22 | 9 9 18 |
grg | grg 2784 | 11 8 33 | 9 9 31 | 12 11 21 |
igr | igr 3028 | 9 6 25 | 6 7 21 | 9 10 20 |
igs | igs 3008 | 9 7 26 | 6 6 24 | 10 10 19 |
jpl | jpl 2972 | 14 8 28 | 7 7 22 | 11 11 22 |
mit | mit 3072 | 21 27 63 | 6 7 30 | 10 13 20 |
Table 5.1799.6 GPS week: 1799 Day: 6 MJD: 56843.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 8 7 23 | 4 5 21 | 8 12 18 |
emr | emr 2967 | 9 7 30 | 5 6 25 | 8 13 20 |
esa | esa 2976 | 8 8 25 | 5 5 20 | 9 13 22 |
gfz | gfz 2972 | 8 8 24 | 5 6 21 | 9 14 18 |
grg | grg 2784 | 11 9 27 | 7 9 33 | 11 13 19 |
igr | igr 3039 | 9 8 25 | 5 5 20 | 8 14 19 |
igs | igs 2961 | 8 7 25 | 5 6 21 | 8 13 19 |
jpl | jpl 2972 | 13 13 35 | 5 7 22 | 10 11 25 |
mit | mit 3072 | 9 10 29 | 5 6 23 | 8 14 21 |
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 6.1799 GPS week: 1799 MJD: 56837.500-56843.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -21 5 -55 -23 3 | 13 20
| 27 18 93 97 5 | 2
emr uuuuu | 49 -2 118 113 -2 | 29 35
| 22 14 99 69 13 | 5
esa uuuuu | -10 -3 -40 -27 1 | 9 18
| 28 14 40 59 2 | 2
gfz uuuuu | -10 2 -22 -62 5 | 1 17
| 29 22 115 53 5 | 4
grg uuuuu | 38 -31 -35 239 -1 | 34 38
| 22 22 51 92 4 | 2
igr xxxxx | -6 -5 9 -35 2 | 1 16
| 11 19 59 50 1 | 2
irf xxxxx | 10 -8 -8 -42 -1 | 1 15
| 8 17 51 46 4 | 2
jpl uuuuu | -10 24 2 15 2 | 4 23
| 23 26 56 41 11 | 3
mit uuuuu | 17 10 -35 -103 -4 | 19 24
| 16 29 93 69 6 | 2
ngs uuuuu | -37 -12 69 -35 -8 | 11 19
| 58 65 85 82 7 | 2
sio xxxxx | 9 19 63 -84 -3 | 37 40
| 12 23 57 77 6 | 3
Table 7.1799.0 GPS week: 1799 Day: 0 MJD: 56837.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -12 24 -74 -70 6 | 14 19
emr uuuuu | 68 -9 -9 147 -7 | 36 41
esa uuuuu | -20 -9 16 -45 1 | 11 17
gfz uuuuu | -6 -5 129 24 10 | -2 15
grg uuuuu | 24 -52 -10 201 -3 | 38 40
igr xxxxx | -1 -14 68 -45 1 | 2 14
irf xxxxx | 3 -8 58 -83 0 | 2 13
jpl uuuuu | 0 -20 1 -3 -14 | 7 20
mit uuuuu | -4 17 81 -183 -4 | 21 25
ngs uuuuu | -43 24 -72 -2 -6 | 16 20
sio xxxxx | 28 0 156 -141 -11 | 42 43
Table 7.1799.1 GPS week: 1799 Day: 1 MJD: 56838.500
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 | -5 14 -101 -144 2 | 13 19
emr uuuuu | 81 5 9 176 -13 | 32 36
esa uuuuu | -4 2 -11 -115 0 | 9 16
gfz uuuuu | -4 2 56 -82 4 | -1 15
grg uuuuu | 42 -37 2 218 -1 | 35 38
igr xxxxx | 5 -25 82 -82 0 | 0 14
irf xxxxx | 10 -19 -6 -86 2 | 0 14
jpl uuuuu | 9 45 64 92 -11 | 4 21
mit uuuuu | 14 -13 -25 -128 2 | 20 23
ngs uuuuu | -124 -26 27 80 2 | 14 19
sio xxxxx | 11 21 14 -133 -7 | 39 41
Table 7.1799.2 GPS week: 1799 Day: 2 MJD: 56839.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 8 17 1 84 -2 | 12 19
emr uuuuu | 49 -2 212 145 -14 | 26 34
esa uuuuu | -3 0 -63 -81 6 | 7 18
gfz uuuuu | -51 23 -217 -116 8 | -3 17
grg uuuuu | -1 -13 -73 137 8 | 32 36
igr xxxxx | -18 22 45 15 3 | -2 17
irf xxxxx | -3 8 -63 -86 3 | -2 16
jpl uuuuu | 19 38 66 22 0 | 0 24
mit uuuuu | -6 41 -108 -179 4 | 17 23
ngs uuuuu | -4 -91 166 47 -17 | 11 20
sio xxxxx | 9 25 50 -156 -8 | 35 39
Table 7.1799.3 GPS week: 1799 Day: 3 MJD: 56840.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -19 -19 -191 120 -1 | 11 19
emr uuuuu | 26 -6 137 -28 -10 | 24 31
esa uuuuu | 17 -10 -20 21 0 | 7 18
gfz uuuuu | -38 19 -36 -32 10 | -2 17
grg uuuuu | 32 -15 -126 129 0 | 31 36
igr xxxxx | 3 2 4 -82 0 | -2 16
irf xxxxx | 19 -14 37 -54 -2 | -1 16
jpl uuuuu | -9 44 14 0 7 | -1 23
mit uuuuu | 33 -4 47 -122 -3 | 18 23
ngs uuuuu | -29 0 135 -31 -8 | 9 18
sio xxxxx | 14 11 49 -135 -6 | 34 38
Table 7.1799.4 GPS week: 1799 Day: 4 MJD: 56841.500
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 | -40 -17 -90 5 13 | 12 20
emr uuuuu | 54 25 63 119 16 | 24 31
esa uuuuu | 22 4 -43 56 0 | 9 19
gfz uuuuu | -1 -24 56 -93 6 | 1 18
grg uuuuu | 45 -45 28 349 -6 | 32 37
igr xxxxx | -17 -23 -15 20 3 | 0 16
irf xxxxx | 13 -9 24 9 -8 | 0 16
jpl uuuuu | -8 7 -23 -43 6 | 2 23
mit uuuuu | 22 16 13 -58 -14 | 19 25
ngs uuuuu | -67 15 15 -141 -17 | 10 18
sio xxxxx | 13 30 77 33 -2 | 34 38
Table 7.1799.5 GPS week: 1799 Day: 5 MJD: 56842.500
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 | -5 21 -39 -58 -2 | 16 23
emr uuuuu | 48 -8 248 152 14 | 28 35
esa uuuuu | -24 20 -109 -26 1 | 12 20
gfz uuuuu | 39 27 -38 -20 -2 | 6 18
grg uuuuu | 61 1 -24 306 -3 | 35 39
igr xxxxx | 2 18 -78 16 2 | 3 17
irf xxxxx | 14 21 -81 4 -4 | 3 16
jpl uuuuu | -49 8 -6 26 18 | 6 24
mit uuuuu | 29 47 -185 -57 -9 | 21 25
ngs uuuuu | -58 -93 137 -114 -7 | 11 18
sio xxxxx | -5 60 -12 5 7 | 37 40
Table 7.1799.6 GPS week: 1799 Day: 6 MJD: 56843.500
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 | -73 -6 106 -100 3 | 16 23
emr uuuuu | 20 -17 164 84 1 | 30 36
esa uuuuu | -61 -27 -54 1 2 | 12 20
gfz uuuuu | -7 -28 -103 -111 0 | 6 18
grg uuuuu | 64 -54 -41 336 -3 | 35 39
igr xxxxx | -17 -17 -45 -83 2 | 3 16
irf xxxxx | 15 -32 -23 3 0 | 2 16
jpl uuuuu | -30 44 -100 15 8 | 8 24
mit uuuuu | 31 -33 -68 4 -4 | 20 25
ngs uuuuu | 65 89 75 -82 -6 | 9 18
sio xxxxx | -7 -11 108 -59 3 | 37 40
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