[IGSREPORT-27192] Wk 2098 IGS Final Orbits
acc
acc at igs.org
Mon Apr 13 03:19:48 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2098 (Mar 22, 2020 - Mar 28, 2020)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs2098[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2098[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2098[0-6].cls IGS GPS clock combination summary report.
igs20987.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20987.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 | TIXI TIXI
0 | EMR | SYOG YELL SYOG YELL
0 | ESA | CHUR PTBB WIND CHUR PTBB WIND
0 | GFZ | 4 18 4 18 BJNM GODE NOVM POHN BJNM GODE NOVM POHN
0 | GFZ | WIND
0 | GRG | 13 13 XMIS XMIS
1 | COD | BJNM GUUG OHI3 WIND GUUG OHI3 WIND
1 | ESA | CHUR PTBB WIND CHUR PTBB WIND
1 | GFZ | 4 18 4 18 GODE MDVJ POHN GODE MDVJ POHN
1 | GRG | 17 DJIG
1 | JPL | NRIL
2 | ALL | 18
2 | COD | 14 14 BJNM GODE TIXI URUM BJNM BRFT TIXI URUM
2 | ESA | BAKE FAA1 PTBB PTBB
2 | GFZ | 4 4 18 BJNM POHN BJNM GODE POHN SOFI
2 | GRG | FAA1 FAA1
3 | COD | 17 17 LHAZ TIXI ZAMB LHAZ NRMD TIXI ZAMB
3 | EMR | STJO SYOG STJO SYOG
3 | ESA | PTBB DJIG PTBB WIND
3 | GFZ | 4 18 4 18 BJNM GODE POHN STJO BJNM FAA1 GODE POHN
3 | GFZ | STJO WIND
3 | GRG | DGAR KRGG DGAR LHAZ
3 | JPL | POLV
4 | COD | 13 29 13 29 ADIS BJNM CPVG SGOC TIXI URUM VOIM BJNM
4 | COD | CPVG SGOC TIXI URUM VOIM
4 | EMR | SYOG SYOG
4 | ESA | ANKR PTBB ULAB WIND ANKR PTBB ULAB WIND
4 | GFZ | 4 18 4 18 BARH BJNM FLRS GODE POHN BARH BJNM FLRS
4 | GFZ | GODE POHN
4 | GRG | CHPG FAA1 SFER SGOC CHPG DARW FAA1 SFER SGOC
4 | JPL | POLV
4 | MIT | BJNM
5 | COD | TIXI TIXI
5 | ESA | DJIG PTBB ULAB DJIG PTBB
5 | GFZ | 4 18 4 18 ANKR BJNM GODE POHN ULAB ANKR FAA1 GODE
5 | GFZ | POHN
5 | GRG | BRST FAA1 LHAZ SGOC SUTM BRST FAA1 LHAZ SUTM
5 | MIT | FAA1
6 | COD | ANKR DARW TIXI BRFT DARW TIXI
6 | EMR | SYOG SYOG
6 | ESA | PTBB ULAB PTBB ULAB
6 | GFZ | 4 18 4 18 BJNM POHN USN7 FAA1 POHN USN7
6 | GRG | FAA1
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. 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 G17 | 4 | | | | | | 4 |
PRN G29 | 4 | 4 | | | | | |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
8. 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 | -.8 .3 .2 17 23 9 .11
EMR | 0 | 7.4 -2.0 15.7 -31 -6 46 .54
ESA | 0 | .7 -1.0 -1.0 -17 43 56 .23
GFZ | 0 | .1 -.6 .2 11 17 54 .15
GRG | 0 | 5.6 .0 9.8 58 -11 105 .20
JPL | 0 | 12.0 -3.0 12.6 19 20 11 -.16
MIT | 0 | -.0 2.3 7.8 33 16 -24 .31
NGS | 0 | 4.2 -2.8 5.9 3 -9 -13 .14
SIO | 0 | 2.7 -2.9 1.4 23 -8 -12 .39
COD | 1 | -.7 .4 .2 11 10 8 -.20
EMR | 1 | 11.6 -1.5 15.8 -41 -11 28 .21
ESA | 1 | 1.2 -.7 -1.4 -24 47 78 -.05
GFZ | 1 | .0 -.2 .9 31 24 50 .01
GRG | 1 | 9.5 -3.2 3.4 44 -5 101 -.05
JPL | 1 | 15.5 -6.8 11.8 4 -4 -1 -.33
MIT | 1 | 3.1 -.4 7.8 6 1 -1 .15
NGS | 1 | 6.8 -1.9 3.4 -8 17 -45 .17
SIO | 1 | 1.7 -4.1 -15.1 16 0 -2 .0
COD | 2 | -.4 .3 .4 21 16 15 .01
EMR | 2 | 2.6 -4.2 9.1 -39 -32 68 .41
ESA | 2 | .9 -1.9 -1.2 -25 48 74 .12
GFZ | 2 | -.3 -.6 .6 13 30 45 .19
GRG | 2 | 6.3 -3.3 .2 56 -1 110 .22
JPL | 2 | 7.4 -5.9 9.1 9 9 -4 -.06
MIT | 2 | -.0 -.3 8.2 17 4 8 .30
NGS | 2 | 4.4 -9.2 4.1 -55 23 -30 .32
SIO | 2 | .8 -5.0 -20.3 39 7 -21 -.05
COD | 3 | -.9 -.0 .0 21 8 20 -.11
EMR | 3 | 5.8 -2.3 12.7 -47 -36 67 .11
ESA | 3 | 1.5 -1.7 -.4 -32 39 93 -.04
GFZ | 3 | .2 -.6 .4 21 15 54 -.08
GRG | 3 | 3.8 -4.8 1.8 59 -19 150 .21
JPL | 3 | 3.6 -3.4 9.2 5 6 2 -.02
MIT | 3 | .4 -.5 11.3 11 -4 -14 .05
NGS | 3 | 5.0 -3.6 12.3 0 -8 -26 .01
SIO | 3 | .1 -4.6 9.2 18 3 7 -.16
COD | 4 | -.7 .7 .6 26 19 15 -.10
EMR | 4 | .2 1.7 10.6 -61 -39 2 .01
ESA | 4 | .7 -.8 -1.6 -19 45 113 -.12
GFZ | 4 | .4 .1 -.1 9 -14 47 .03
GRG | 4 | 3.6 -2.7 9.5 66 22 86 .12
JPL | 4 | -.9 -.2 9.1 1 0 2 -.08
MIT | 4 | 1.9 -.5 9.6 29 -3 -27 .25
NGS | 4 | 8.7 -.5 10.7 18 -48 -16 -.01
SIO | 4 | 1.6 -2.3 -7.1 26 -15 5 -.09
COD | 5 | -.4 .1 .4 9 8 9 -.11
EMR | 5 | -2.4 .7 11.8 -50 -18 33 .31
ESA | 5 | 1.1 -1.9 -1.1 -28 41 82 -.05
GFZ | 5 | -.3 .3 -.6 31 1 51 .11
GRG | 5 | 5.3 .4 7.8 79 16 120 .06
JPL | 5 | 4.4 2.1 9.2 9 -1 -17 -.03
MIT | 5 | 3.6 2.2 12.7 -5 -16 -21 .17
NGS | 5 | .9 -.0 15.4 71 41 6 .13
SIO | 5 | 4.7 -5.8 -2.2 18 -26 -1 .21
COD | 6 | -.2 -.1 1.0 13 11 21 -.22
EMR | 6 | -1.8 -5.1 6.8 -45 -19 15 -.02
ESA | 6 | 1.7 -1.8 -1.4 -31 14 127 -.07
GFZ | 6 | -.7 -.1 .1 31 15 55 -.08
GRG | 6 | 4.4 -1.4 -.2 58 34 77 .12
JPL | 6 | 9.5 -3.5 7.4 19 -1 10 -.31
MIT | 6 | 3.3 -4.1 6.9 10 -4 -9 .15
NGS | 6 | 9.2 -5.4 8.6 -9 -38 -43 .14
SIO | 6 | 5.7 -9.4 -7.3 0 -11 12 .12
9. 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.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.2098.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2098.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 2.2098.[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 3.2098.[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 5.2098.0-6). 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 2098 summary. (Mar 22, 2020 - Mar 28, 2020)
Table 1.2098.a GPS week: 2098 MJD: 58930.000-58936.000
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 -2 1 -15 0 -.06 9 8 | -887 515 6 116
| 0 0 0 11 19 12 .03 | 253 424
emr 81| 1 1 3 -8 4 7 .19 12 12 | 206130 442 12 98
| 1 1 1 10 18 20 .03 | 3535 541
esa 149| 0 0 0 -24 2 7 -.05 10 10 | -1667 1642 8 91
| 0 0 1 12 11 21 .01 | 343 872
gfz 180| -1 0 0 -23 -12 0 .01 12 12 | 59 -130 12 94
| 0 0 1 22 16 16 .03 | 247 632
grg 94| 1 0 -4 -17 -8 37 -.15 10 9 | 30 50 9 129
| 0 0 2 11 10 35 .02 | 156 403
igr n/a| 0 0 -1 -13 -20 -18 .03 4 4 | 2274 101 10 67
| 0 0 0 10 15 25 .01 | 923 762
jpl 80| 0 0 3 15 3 20 .23 8 8 | 181445 434 8 99
| 1 1 0 9 24 33 .03 | 37951 487
mit 377| 0 0 0 26 5 -17 -.08 8 7 | 1915 69 57 1696
| 1 0 0 15 21 84 .01 | 1007 744
ngs 205| 0 0 2 19 5 -22 -.02 9 7 | -936 598 817 1937
| 1 0 1 12 13 19 .02 | 334 568
sio 394| -1 0 -3 -25 14 -38 .06 17 18 | --- --- --- ---
| 0 0 2 50 66 28 .03 | --- ---
Table 1.2098.b GPS week : 2098 MJD: 58930.000-58936.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 2 3 3 3 3 |
2 | 3 3 3 4 3 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 9 7 8 7 8 8 8 |
5 | 4 3 3 3 4 3 4 |
6 | 3 3 3 3 3 3 3 |
7 | 4 3 3 3 3 3 4 |
8 | 6 5 5 5 4 4 4 |
9 | 5 7 4 4 4 4 4 |
10 | 3 3 2 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 4 3 4 3 3 4 4 |
13 | 4 4 5 4 5 4 4 |
14 | 3 4 4 3 4 3 3 |
15 | 4 3 4 5 4 4 4 |
16 | 4 4 4 4 4 4 4 |
17 | 4 4 4 5 5 4 4 |
18 | 6 7 7 5 6 6 7 |
19 | 3 4 3 3 5 4 4 |
20 | 3 3 3 3 3 3 3 |
21 | 4 3 3 3 3 3 3 |
22 | 3 3 3 3 3 3 3 |
23 | 5 5 4 4 5 0 6 |
24 | 3 3 3 4 3 3 4 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 3 3 3 |
27 | 5 5 5 4 5 4 4 |
28 | 4 3 4 4 3 3 3 |
29 | 4 4 4 4 6 5 5 |
30 | 3 3 3 3 3 3 3 |
31 | 4 3 3 3 4 3 3 |
32 | 5 4 5 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2098.0 GPS week: 2098 Day: 0 MJD: 58930.000
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 -3 -6 -12 -13 -.06 10 8 | -626 -35 8 122
emr 81| 2 0 4 -16 11 -11 .16 12 12 | 211870 -311 14 106
esa 149| 1 0 1 -16 -1 -18 -.06 10 10 | -1440 755 9 93
gfz 180| -1 0 -1 -45 -4 -17 -.01 15 15 | 550 -1336 13 94
grg 95| 2 1 -1 -16 -9 19 -.18 10 9 | 170 -386 9 118
igr n/a| 0 0 -1 -18 0 -11 .04 4 4 | 3624 -1065 11 75
jpl 80| 1 -1 2 14 -6 35 .27 8 8 | 211877 -298 8 97
mit 377| -2 0 0 42 11 51 -.09 8 7 | 3538 -1038 38 1641
ngs 206| 0 0 0 0 5 -44 -.02 9 7 | -617 -59 1015 2031
sio 419| 0 -1 -1 7 -7 -71 .09 18 17 | --- --- --- ---
Table 2.2098.1 GPS week: 2098 Day: 1 MJD: 58931.000
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| 0 0 -2 2 4 18 -.08 9 8 | -717 430 6 109
emr 81| 2 2 6 1 -14 15 .19 15 15 | 204382 -111 12 107
esa 149| 0 0 0 -8 4 26 -.03 9 9 | -1902 2807 8 85
gfz 181| -2 -1 0 -33 -23 24 .06 13 12 | -120 329 13 130
grg 94| 1 0 -4 -22 -4 54 -.17 10 9 | 165 -112 9 114
igr n/a| 0 0 -1 -24 -19 -6 .04 4 4 | 3300 -503 11 75
jpl 80| 1 0 4 12 -25 51 .27 8 8 | 212135 -49 9 77
mit 377| -1 -1 0 14 11 -83 -.07 6 5 | 2907 -521 32 1699
ngs 207| 0 0 0 17 16 -19 .00 9 7 | -684 257 863 1820
sio 390| -1 0 -5 -17 14 -4 .04 17 18 | --- --- --- ---
Table 2.2098.2 GPS week: 2098 Day: 2 MJD: 58932.000
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| -1 0 0 -9 -4 -9 -.03 8 7 | -1252 1144 6 126
emr 81| 1 3 4 -12 12 25 .18 12 12 | 203987 396 12 98
esa 149| 0 0 0 -31 6 -10 -.05 10 10 | -1958 2247 9 115
gfz 179| -1 0 1 -47 7 -19 .00 13 10 | -164 553 11 81
grg 94| 1 0 -5 -14 -27 31 -.15 10 10 | -199 576 10 116
igr n/a| 0 0 -1 -22 -19 -23 .03 4 4 | 2496 -106 10 68
jpl 80| 0 0 4 16 -15 20 .22 8 8 | 211834 451 7 98
mit 377| 0 0 0 28 14 9 -.06 6 5 | 2196 -188 77 1668
ngs 205| 0 -1 0 35 -9 -17 -.01 8 7 | -1491 1481 653 1782
sio 389| -1 0 -6 16 1 -55 .02 17 19 | --- --- --- ---
Table 2.2098.3 GPS week: 2098 Day: 3 MJD: 58933.000
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 -1 1 3 -14 -.02 7 7 | -819 432 5 108
emr 80| 2 2 4 -3 22 13 .20 12 12 | 210621 1100 12 84
esa 149| 0 0 -1 -34 23 -13 -.05 9 9 | -2170 2570 8 86
gfz 182| -1 0 0 -37 -1 1 -.01 12 12 | 212 221 12 87
grg 97| 0 0 -7 -3 4 4 -.14 11 10 | -97 608 9 148
igr n/a| 0 0 -1 -13 -5 -55 .02 4 4 | 1796 430 10 71
jpl 80| 0 0 3 4 17 -38 .23 8 8 | 140083 872 8 101
mit 377| 0 -1 0 45 -20 85 -.08 7 6 | 1254 325 73 1475
ngs 208| 0 0 4 12 -16 -54 -.04 10 8 | -881 670 969 1757
sio 394| 0 0 -4 -4 -34 -30 .10 17 19 | --- --- --- ---
Table 2.2098.4 GPS week: 2098 Day: 4 MJD: 58934.000
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 -2 13 -28 7 -.09 9 8 | -701 309 6 111
emr 80| 0 3 2 8 -18 13 .24 11 11 | 203714 253 13 103
esa 149| -1 0 -2 -10 -11 32 -.06 10 10 | -1503 909 9 92
gfz 172| 0 0 0 -6 -28 10 .04 13 12 | -46 -239 13 86
grg 95| 1 -1 -1 -6 -5 30 -.17 10 9 | 214 -186 9 125
igr n/a| 0 0 -2 0 -45 -19 .02 4 4 | 1523 51 10 60
jpl 80| -2 2 2 28 -10 39 .20 9 9 | 140391 282 8 125
mit 377| 0 -2 0 3 25 -100 -.09 11 9 | 924 7 68 1872
ngs 208| 2 0 3 17 9 -5 -.05 9 8 | -647 148 669 2012
sio 383| 0 0 -2 -127 160 -3 .05 17 18 | --- --- --- ---
Table 2.2098.5 GPS week: 2098 Day: 5 MJD: 58935.000
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 248| -1 -1 -1 -8 -49 2 -.07 9 8 | -871 286 7 119
emr 84| 0 0 2 -16 -11 23 .18 11 11 | 203584 787 14 103
esa 149| 0 0 -2 -28 3 27 -.04 9 9 | -1481 904 9 85
gfz 183| 0 0 -1 1 -33 10 -.02 10 10 | -30 -458 12 91
grg 94| 1 0 0 -17 -12 109 -.16 10 9 | -39 -283 8 150
igr n/a| 0 0 -1 0 -29 24 .03 4 4 | 1110 661 10 66
jpl 80| -1 2 2 6 28 45 .21 8 8 | 211635 792 9 106
mit 377| 0 0 0 33 26 -126 -.06 7 7 | 979 771 48 1718
ngs 201| 1 0 3 18 18 -9 -.02 9 7 | -966 474 871 2335
sio 395| -1 -1 0 4 1 -34 .09 17 16 | --- --- --- ---
Table 2.2098.6 GPS week: 2098 Day: 6 MJD: 58936.000
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 0 21 -22 6 -.04 8 7 | -1226 1040 6 122
emr 81| -1 0 2 -19 27 -30 .15 12 12 | 204753 986 13 87
esa 149| 0 0 -1 -41 -9 12 -.07 10 10 | -1217 1304 8 87
gfz 185| -1 0 1 2 -1 -10 .01 9 9 | 12 20 11 92
grg 92| 2 0 -6 -38 -1 9 -.11 10 10 | -3 135 10 138
igr n/a| 0 0 -1 -15 -25 -37 .01 4 4 | 2072 1240 10 60
jpl 80| -1 1 3 27 38 -8 .20 7 7 | 142166 993 9 95
mit 377| 0 0 0 15 -26 42 -.08 9 8 | 1608 1128 63 1799
ngs 204| 2 -1 2 37 15 -4 -.03 10 8 | -1271 1221 685 1828
sio 390| 0 0 -1 -54 -34 -72 .05 17 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 3.2098.0 GPS week: 2098 Day: 0 MJD: 58930.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 7 9 9 7 4 5 7 6 12 2 | 21 28 22 21 23 23 27 19 20 23 21
2 | 8 7 10 12 8 4 7 7 7 19 3 | 28 26 25 27 25 25 27 24 24 30 25
3 | 7 7 10 11 8 3 6 5 7 10 2 | 26 27 28 26 24 26 28 25 27 26 25
X4E | 26 16 13 37 --- 8 27 14 13 41 8 | 34 34 31 44 --- 27 33 30 29 36 28
5 | 10 15 11 11 10 5 6 8 9 21 3 | 51 51 55 54 52 53 54 48 52 52 51
6 | 6 8 10 11 5 4 7 10 7 10 3 | 30 32 31 27 28 29 33 28 28 34 29
7 | 7 10 8 8 10 4 8 6 11 24 3 | 48 50 51 48 46 49 54 48 48 46 48
8E | 14 17 11 29 18 4 13 10 14 17 5 | 40 41 39 42 41 37 40 38 33 34 37
9E | 13 11 16 34 16 4 9 8 9 14 5 | 19 24 24 30 23 20 24 19 21 20 19
10 | 10 9 7 9 9 3 7 5 8 14 3 | 24 25 28 27 23 25 31 23 24 34 25
11 | 8 15 13 19 10 5 9 10 9 13 4 | 21 31 21 38 25 26 29 24 27 24 24
12 | 9 14 8 11 11 5 7 14 9 23 4 | 30 35 29 33 28 28 32 25 28 23 28
13E | 10 12 8 10 14 4 7 6 5 19 3 | 43 42 40 41 40 41 42 38 43 46 40
14E | 8 11 7 10 7 4 10 10 5 12 3 | 91 90 88 89 92 89 89 85 90 91 89
15E | 8 13 8 14 9 4 10 6 9 16 3 | 30 32 28 33 33 30 30 27 33 27 29
16 | 10 20 7 14 8 3 8 9 9 28 4 | 25 32 28 24 23 25 29 23 25 27 24
17E | 15 9 7 10 12 3 9 8 7 16 3 | 172 165 166 165 164 167 168 169 167 167 167
X18 | 13 --- 16 10 --- 6 --- 7 8 --- 5 | 57 --- 50 52 --- 54 --- 55 53 --- 53
19E | 10 13 8 15 7 4 7 8 6 14 3 | 71 66 73 71 69 70 71 69 71 73 70
20 | 10 9 6 9 9 3 7 7 9 22 3 | 17 20 17 17 16 17 21 19 16 24 16
21 | 9 9 6 10 9 4 7 5 10 24 3 | 29 34 32 33 33 31 35 31 27 43 31
22 | 8 9 8 10 9 4 6 5 5 20 3 | 15 23 16 19 15 17 23 17 17 23 17
X23E | 15 21 9 12 10 4 7 8 10 --- 4 | 34 44 44 39 35 41 43 38 40 --- 41
24 | 7 12 12 9 9 4 6 5 8 9 3 | 19 27 22 21 18 20 26 19 19 27 20
25 | 8 8 8 14 10 4 7 5 7 12 3 | 25 29 24 26 24 23 29 22 24 32 24
26 | 6 9 8 12 6 4 9 6 7 12 3 | 24 26 26 24 21 23 30 20 19 25 23
27E | 19 13 14 13 18 5 15 10 16 19 5 | 43 43 38 34 40 37 41 36 33 34 37
28 | 7 10 7 9 8 3 7 10 5 25 3 | 25 29 21 26 25 25 29 22 22 29 24
29E | 10 16 12 12 12 5 8 10 14 17 4 | 185 189 187 184 186 186 188 188 185 190 186
30 | 8 10 10 9 8 5 7 7 7 12 3 | 25 27 28 24 23 25 29 26 25 26 25
31 | 6 12 8 11 9 3 7 7 5 27 3 | 37 39 40 44 35 36 43 34 38 36 37
32E | 16 8 17 31 9 3 8 6 8 11 4 | 38 35 30 40 35 33 35 30 34 37 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 10 15 10 4 8 8 9 18 |T 43 45 43 44 42 42 45 41 41 44 42
WRMS | 8 12 10 15 9 4 8 7 7 17 |NE 28 31 29 30 26 29 32 27 28 30 28
MEDI | 9 11 8 11 9 4 7 7 8 16 |MD 30 32 29 33 28 28 32 27 28 32 28
Table 3.2098.1 GPS week: 2098 Day: 1 MJD: 58931.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 8 6 8 7 4 8 6 10 9 2 | 27 30 27 29 27 27 31 22 25 32 26
2 | 9 7 9 9 10 3 8 5 6 20 3 | 28 27 26 30 26 26 29 21 27 28 25
3 | 8 9 7 8 8 3 8 4 11 11 2 | 26 31 27 27 27 26 33 22 30 30 26
X4E | 13 13 12 30 --- 6 23 15 13 36 7 | 15 19 18 29 --- 15 18 22 18 31 15
5 | 5 9 10 10 9 4 6 5 6 24 3 | 40 42 40 45 39 39 42 34 41 45 39
6 | 6 10 10 8 8 4 7 8 7 12 2 | 30 34 31 35 30 31 35 23 30 37 29
7 | 7 15 9 8 8 5 6 4 6 21 3 | 38 42 41 42 39 41 44 35 40 39 39
X8E | 12 16 15 29 --- 5 8 8 12 12 5 | 18 22 18 23 --- 17 16 21 19 18 16
9E | 10 44 17 33 15 5 11 6 11 16 6 | 18 47 18 29 15 17 21 16 19 21 16
10 | 7 8 8 11 10 3 7 5 8 13 2 | 28 30 30 30 29 28 31 20 29 32 26
11 | 9 17 12 12 11 6 11 7 12 12 4 | 31 37 33 37 32 32 36 27 31 33 31
12 | 7 15 7 7 12 3 6 4 7 22 3 | 28 33 27 30 27 26 32 22 28 27 26
13E | 10 19 6 6 14 4 9 6 16 16 4 | 35 35 32 35 37 33 36 31 39 40 33
14E | 12 10 6 11 9 4 11 10 7 9 3 | 67 63 63 67 62 65 62 69 63 65 65
15E | 7 14 7 10 8 4 10 6 10 17 3 | 25 25 26 28 24 24 28 24 27 30 24
16 | 6 19 5 10 8 4 5 4 6 28 3 | 27 29 27 30 27 26 29 24 27 32 26
17E | 14 8 8 9 19 4 7 6 7 15 3 | 137 132 132 138 134 135 134 129 137 134 133
X18 | 13 --- 16 14 --- 6 --- 8 12 43 7 | 43 --- 46 45 --- 42 --- 39 43 42 43
19E | 9 14 9 11 11 4 6 7 10 14 3 | 60 60 62 65 60 61 60 56 60 66 59
20 | 9 9 6 9 10 4 8 4 8 19 3 | 20 23 21 24 21 21 23 16 23 24 19
21 | 8 12 4 10 8 3 9 5 8 24 3 | 37 39 34 39 36 35 34 29 37 40 34
22 | 9 10 6 7 8 4 7 4 8 22 3 | 20 25 20 22 22 21 27 16 24 27 20
23E | 12 28 12 10 6 5 8 9 14 19 4 | 27 29 25 27 18 28 24 31 29 18 27
24 | 9 8 10 9 8 3 8 4 8 9 2 | 27 32 28 28 25 26 30 21 27 33 25
25 | 9 8 7 10 10 3 5 4 7 9 2 | 29 34 30 30 31 29 34 23 30 31 28
26 | 7 14 6 10 7 3 9 6 7 11 2 | 22 29 24 25 25 23 29 18 22 25 22
27E | 14 13 15 31 14 4 10 7 12 13 5 | 18 19 18 20 19 17 17 20 18 18 16
28 | 7 10 7 6 8 5 7 6 6 26 3 | 27 32 23 27 28 27 32 22 29 33 25
29E | 8 13 13 14 14 4 8 9 12 18 4 | 164 170 168 166 167 167 167 163 169 171 166
30 | 6 14 9 6 7 3 6 4 5 9 2 | 28 32 28 28 28 29 33 23 28 28 27
31 | 7 11 5 10 8 3 9 5 6 24 3 | 33 33 30 35 32 30 34 26 30 26 30
32E | 6 10 14 29 9 3 9 4 12 12 4 | 13 18 14 20 16 15 17 18 17 20 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 9 13 10 4 8 6 9 17 |T 37 40 37 40 38 36 39 33 38 39 35
WRMS | 8 15 9 12 9 4 8 5 7 17 |NE 29 32 29 31 29 29 32 24 30 32 28
MEDI | 9 12 8 10 9 4 8 6 8 16 |MD 28 32 27 30 28 27 32 23 29 31 26
Table 3.2098.2 GPS week: 2098 Day: 2 MJD: 58932.000
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 8 7 7 5 3 6 6 7 10 2 | 21 26 23 22 20 21 25 19 21 25 21
2 | 7 9 9 11 8 5 8 5 6 22 3 | 20 21 17 22 17 18 20 17 18 22 17
3 | 9 7 7 8 6 3 6 5 7 9 2 | 40 43 44 39 42 40 44 42 39 43 41
X4E | 12 15 12 28 --- 4 23 16 19 38 7 | 20 26 26 32 --- 21 24 26 23 35 21
5 | 7 11 10 11 8 8 7 5 7 20 3 | 41 40 42 42 40 43 43 38 41 42 40
6 | 6 8 10 7 7 5 9 6 8 9 2 | 22 26 22 25 22 23 26 19 21 26 21
7 | 6 11 8 8 9 4 6 4 4 24 3 | 32 32 32 33 28 32 34 31 32 24 31
8E | 11 16 15 29 13 4 10 10 13 14 5 | 33 32 30 35 36 31 30 31 34 34 30
9E | 9 9 16 10 11 3 9 7 9 13 3 | 19 22 20 22 17 18 20 18 18 21 17
10 | 7 9 8 7 9 4 5 4 4 9 2 | 21 25 24 21 21 21 26 18 22 27 21
11 | 8 17 12 10 10 4 7 9 7 12 3 | 24 32 21 28 23 25 29 23 26 23 24
12 | 7 13 8 10 12 4 7 5 8 25 3 | 22 26 19 25 22 21 25 20 22 17 20
13E | 12 25 9 10 9 4 10 6 15 16 4 | 34 38 32 36 33 34 33 34 37 34 32
14E | 9 10 8 11 15 6 9 5 12 12 3 | 53 49 52 53 49 51 48 50 51 58 50
15E | 9 13 10 8 12 4 9 6 10 13 3 | 26 24 24 24 27 24 25 26 26 24 24
16 | 8 19 4 10 10 6 5 5 7 26 3 | 25 26 22 25 23 22 23 21 22 23 22
17E | 15 6 9 11 11 7 7 6 7 16 3 | 108 102 102 100 107 101 103 104 106 104 104
X18 | 13 --- 13 9 --- 6 --- 7 10 49 7 | 25 --- 23 31 --- 26 --- 26 24 45 26
19E | 10 12 8 11 11 4 7 6 8 14 3 | 36 35 36 38 33 35 36 36 38 40 35
20 | 7 10 7 6 9 4 5 3 6 20 2 | 27 30 26 27 27 25 26 23 25 31 25
21 | 8 9 5 6 10 4 6 4 7 27 3 | 21 25 17 22 20 19 21 18 20 25 19
22 | 8 9 5 7 8 3 7 4 7 20 2 | 19 26 22 21 21 21 27 21 22 26 21
23E | 9 22 12 11 9 5 8 8 9 18 4 | 21 25 22 21 22 22 23 21 23 17 22
24 | 7 9 11 11 11 3 9 4 9 10 3 | 23 25 23 24 20 20 25 19 21 24 20
25 | 7 10 7 12 13 4 6 5 4 12 3 | 16 22 19 19 18 17 22 17 17 21 17
26 | 6 8 6 10 9 3 6 5 7 10 2 | 26 29 28 29 26 25 28 24 22 27 25
27E | 9 13 16 24 13 3 9 8 9 14 4 | 35 34 31 30 35 31 31 32 32 36 31
28 | 8 11 7 7 9 3 7 8 8 29 3 | 24 29 20 21 23 22 28 20 20 29 21
29E | 9 13 12 14 15 4 8 5 12 15 3 | 107 104 106 106 101 106 104 109 108 103 105
30 | 7 11 10 6 8 4 8 6 9 11 2 | 20 28 25 22 22 22 26 21 23 25 22
31 | 6 11 6 7 9 3 7 5 9 21 3 | 32 34 32 36 30 32 36 29 34 25 31
32E | 8 11 14 33 11 4 9 7 9 12 4 | 27 29 27 36 26 27 27 25 28 30 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 10 13 10 4 8 6 8 17 |T 31 34 31 33 31 31 33 30 31 33 30
WRMS | 7 12 10 10 10 4 8 5 7 19 |NE 25 28 25 26 24 24 28 23 24 27 24
MEDI | 8 11 9 10 9 4 7 5 8 14 |MD 25 29 24 27 23 24 27 23 23 26 24
Table 3.2098.3 GPS week: 2098 Day: 3 MJD: 58933.000
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 | 5 7 8 6 6 3 6 7 8 10 2 | 21 27 22 19 22 21 28 17 20 25 20
2 | 10 9 8 10 9 5 10 6 9 21 3 | 22 22 21 22 20 20 24 18 19 23 19
3 | 7 7 6 7 6 4 6 7 5 10 2 | 28 30 28 25 28 28 31 22 25 27 26
X4E | 10 15 12 28 --- 5 22 12 15 39 7 | 15 27 23 27 --- 19 24 23 24 34 19
5 | 8 10 10 5 10 6 6 6 6 21 3 | 45 43 47 46 45 46 43 39 43 41 42
6 | 7 6 9 8 7 4 8 7 8 11 2 | 21 24 21 23 22 21 25 16 20 26 19
7 | 8 11 7 9 9 3 8 5 9 24 3 | 31 31 32 31 29 31 36 32 36 27 31
8E | 7 14 13 26 12 4 11 11 11 14 4 | 20 23 19 23 23 18 18 16 19 23 17
9E | 6 9 12 18 11 3 12 6 18 15 4 | 15 19 16 22 22 16 19 16 23 20 15
10 | 8 7 7 11 7 3 9 4 7 12 2 | 23 27 27 24 23 24 26 20 26 28 23
11 | 6 12 12 11 8 3 10 10 9 11 3 | 25 32 23 27 28 25 33 22 25 26 25
12 | 5 14 6 6 12 4 6 5 7 24 3 | 22 29 22 24 24 23 25 21 23 21 22
13E | 6 24 7 14 13 6 9 8 10 12 4 | 57 57 55 56 59 57 57 50 53 58 54
14E | 6 8 7 10 10 4 8 4 7 12 2 | 35 33 34 35 35 33 34 39 35 38 35
15E | 6 26 6 10 17 5 11 9 8 17 4 | 25 28 23 24 35 25 27 23 26 25 23
16 | 7 18 6 10 9 5 8 5 11 26 3 | 21 22 20 21 22 19 23 17 21 22 18
17E | 7 10 15 24 18 6 11 14 19 19 5 | 79 79 80 90 80 80 79 82 92 78 81
X18 | 11 --- 13 9 --- 7 --- 9 10 --- 5 | 26 --- 29 30 --- 25 --- 28 30 --- 27
19E | 8 13 9 11 9 4 7 7 8 14 3 | 34 34 37 36 31 36 35 34 37 37 34
20 | 6 9 6 8 8 4 8 5 8 20 2 | 20 22 21 19 21 20 23 17 22 24 19
21 | 7 12 6 8 12 4 5 7 7 24 3 | 22 27 19 23 25 22 26 18 23 29 21
22 | 7 8 6 9 7 4 6 5 7 20 2 | 20 26 20 20 21 21 26 15 22 26 19
X23E | 11 20 11 7 12 7 8 8 10 --- 4 | 18 23 22 22 27 22 21 25 19 --- 21
24 | 8 13 12 8 11 2 9 5 10 14 3 | 20 29 23 19 20 19 23 19 19 27 19
25 | 6 8 8 6 13 3 5 7 6 8 2 | 16 22 20 18 20 17 22 17 16 23 17
26 | 6 7 6 6 8 2 7 5 10 11 2 | 24 25 22 24 25 23 28 19 21 27 22
27E | 10 11 13 21 13 3 11 8 12 13 4 | 22 21 19 18 23 18 22 17 20 25 18
28 | 7 10 7 6 10 3 7 8 8 28 3 | 22 26 18 20 24 21 26 19 20 30 20
29E | 7 13 11 13 19 3 9 10 10 16 4 | 112 112 112 112 115 112 113 101 114 111 110
30 | 7 8 10 6 8 2 7 6 9 9 2 | 19 25 21 18 22 20 26 18 20 24 19
31 | 7 11 7 6 8 4 7 4 6 25 3 | 33 36 31 34 32 32 36 29 33 25 31
32E | 8 9 15 10 11 3 9 5 11 13 3 | 19 22 20 21 21 19 21 20 21 20 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 9 12 11 4 8 7 10 17 |T 29 32 29 30 31 29 32 27 30 32 28
WRMS | 7 12 9 12 10 4 8 6 8 19 |NE 24 27 24 24 24 23 27 21 24 26 22
MEDI | 7 10 8 9 10 4 8 7 9 14 |MD 22 27 22 23 24 22 26 20 23 26 21
Table 3.2098.4 GPS week: 2098 Day: 4 MJD: 58934.000
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 7 10 8 7 4 7 8 6 10 2 | 21 28 22 20 22 20 26 21 20 25 21
2 | 8 9 9 11 8 6 8 8 5 22 3 | 21 22 18 24 19 19 21 19 19 25 18
3 | 9 7 7 10 6 3 7 7 7 13 2 | 35 40 37 33 34 34 40 31 35 34 34
X4E | 13 18 14 33 --- 5 20 13 21 40 7 | 21 29 25 29 --- 20 25 21 25 37 21
5 | 8 21 12 10 9 7 10 8 6 19 4 | 43 48 46 49 41 44 42 39 42 43 42
6 | 8 8 11 9 5 5 9 9 5 13 3 | 22 27 22 25 21 23 26 21 22 30 22
7 | 5 8 9 11 9 4 8 6 9 23 3 | 30 31 32 35 30 31 32 33 31 27 30
8E | 12 9 16 21 10 4 8 9 9 12 4 | 29 38 29 32 32 29 31 27 31 33 29
9E | 9 10 15 11 10 4 11 5 12 18 4 | 17 22 18 21 15 16 19 13 17 19 15
10 | 8 8 8 10 9 4 7 7 7 14 3 | 21 25 24 21 19 21 25 18 21 31 21
11 | 8 12 15 13 12 4 8 11 11 11 4 | 26 34 22 31 30 27 32 27 31 28 27
12 | 6 10 7 7 10 4 7 5 10 23 3 | 21 29 21 24 25 23 25 22 26 25 22
13E | 17 13 8 25 12 5 14 7 14 16 5 | 30 33 30 41 31 31 37 34 36 34 32
14E | 8 10 10 13 9 3 7 11 8 14 3 | 49 53 50 51 53 50 52 49 51 56 50
15E | 9 13 7 12 12 5 10 15 8 15 4 | 23 25 23 26 25 23 26 33 27 29 24
16 | 7 18 5 11 8 5 10 7 8 26 3 | 24 27 23 22 23 21 24 20 24 25 21
17E | 22 10 7 13 17 4 10 19 10 13 5 | 110 109 109 110 110 110 111 115 110 111 110
X18 | 9 --- 16 11 --- 4 --- 12 12 --- 6 | 27 --- 25 26 --- 25 --- 30 30 --- 27
19E | 17 12 10 18 6 5 11 12 11 16 4 | 43 37 39 45 38 40 40 40 42 42 39
20 | 8 7 7 9 10 4 8 10 7 18 3 | 20 26 22 22 24 21 23 22 26 25 21
21 | 8 10 8 9 10 4 5 11 5 21 3 | 17 22 15 18 22 16 22 21 18 24 17
22 | 9 8 7 8 8 4 8 5 9 22 3 | 21 26 21 20 22 21 28 19 24 26 21
X23E | 8 18 8 12 --- 5 7 8 11 --- 4 | 25 32 33 29 --- 29 32 30 31 --- 28
24 | 6 9 13 6 9 4 8 10 9 12 3 | 18 25 22 20 19 19 23 20 19 26 19
25 | 7 9 10 8 9 4 6 8 7 12 3 | 17 24 20 18 19 19 23 19 19 26 19
26 | 6 8 7 9 7 3 7 6 7 15 2 | 23 29 24 25 24 22 27 20 24 32 23
27E | 7 8 15 28 16 3 8 7 12 11 4 | 32 36 30 30 37 30 32 29 29 36 30
28 | 6 8 8 9 7 2 8 8 8 23 3 | 19 27 17 23 21 21 27 19 21 26 20
29E | 6 11 11 21 19 10 12 32 11 15 6 | 114 111 115 116 114 115 111 138 114 118 116
30 | 6 10 11 9 7 3 7 6 9 12 3 | 19 23 22 23 20 19 23 17 20 26 19
31 | 7 13 6 7 8 5 9 6 10 24 3 | 31 32 26 29 29 25 34 27 29 24 28
32E | 8 11 16 9 12 3 11 6 8 11 3 | 22 28 23 26 26 24 28 21 26 30 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 10 13 10 4 9 11 9 17 |T 30 35 31 33 32 30 34 31 32 35 30
WRMS | 8 11 10 12 9 4 9 9 8 18 |NE 23 28 24 25 24 23 27 23 25 27 23
MEDI | 8 10 9 10 9 4 8 8 9 15 |MD 23 29 23 26 25 23 27 22 26 28 23
Table 3.2098.5 GPS week: 2098 Day: 5 MJD: 58935.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 7 8 7 9 3 7 7 10 13 3 | 18 24 20 18 20 20 25 21 22 24 19
2 | 8 8 9 9 9 4 9 5 10 19 3 | 20 21 18 21 18 18 21 21 22 21 18
3 | 7 6 7 8 7 3 7 6 6 13 2 | 25 29 25 22 25 26 30 24 23 26 24
X4E | 12 16 12 26 --- 6 22 15 17 44 7 | 16 24 21 27 --- 18 21 22 23 38 17
5 | 7 8 10 9 8 6 5 7 8 20 3 | 37 37 38 38 33 37 38 33 34 39 35
6 | 6 8 9 6 6 4 11 7 5 9 2 | 21 26 23 22 22 22 27 23 21 28 22
7 | 9 9 8 10 10 4 8 5 9 23 3 | 34 33 33 35 33 33 35 38 34 32 33
X8E | 9 --- 15 12 9 4 9 12 9 15 4 | 27 --- 30 32 29 28 27 27 24 27 26
9E | 12 11 14 11 10 4 10 6 12 15 4 | 15 16 17 20 15 14 16 16 19 19 13
10 | 6 7 7 6 6 3 8 4 5 14 2 | 17 24 21 19 18 19 23 18 18 27 18
11 | 8 12 11 11 15 5 9 8 7 12 3 | 22 30 22 29 27 25 30 26 29 27 25
12 | 6 14 8 7 11 3 7 6 7 26 3 | 21 27 20 21 18 20 26 20 23 20 20
13E | 15 12 8 8 12 3 8 5 11 13 3 | 59 57 56 60 59 60 60 54 59 58 57
14E | 9 8 8 13 11 4 7 7 7 14 3 | 50 52 55 52 56 54 54 48 53 56 52
15E | 8 16 10 10 11 5 10 8 14 16 4 | 24 23 23 24 27 24 26 25 25 26 23
16 | 6 18 4 9 9 6 10 5 6 26 3 | 21 24 24 24 21 21 25 21 23 24 21
17E | 13 8 9 9 15 4 10 16 9 12 4 | 114 114 113 113 110 112 113 119 114 115 114
X18 | 10 --- 14 10 --- 5 --- 7 13 --- 5 | 31 --- 35 36 --- 32 --- 36 31 --- 33
19E | 13 13 9 12 9 3 11 10 13 12 4 | 47 44 47 46 40 45 45 49 47 47 45
20 | 9 7 6 7 8 4 8 6 5 19 2 | 19 23 21 22 23 21 23 19 20 25 19
21 | 7 10 8 9 12 4 6 5 7 19 3 | 16 21 16 21 22 18 22 18 20 23 17
22 | 8 9 6 8 8 4 7 5 8 23 3 | 20 24 18 15 19 19 24 18 15 24 17
X23E | 3 --- --- --- --- 35 --- --- --- --- 0 | 15 --- --- --- --- 12 --- --- --- --- 17
24 | 10 12 13 8 10 3 7 4 7 12 3 | 20 26 23 20 18 20 24 22 20 30 20
25 | 7 10 10 8 11 4 7 6 10 9 3 | 18 26 22 19 21 18 23 24 19 25 20
26 | 6 8 7 8 8 5 8 6 8 13 2 | 21 25 25 24 22 22 27 20 21 27 22
27E | 9 8 16 20 13 2 8 6 8 13 4 | 31 32 33 26 35 31 33 27 29 31 29
28 | 8 8 7 8 5 3 7 6 8 26 3 | 22 24 20 20 18 21 26 22 23 27 20
29E | 11 16 8 13 19 9 10 15 8 11 4 | 93 94 92 94 92 94 90 100 96 97 93
30 | 6 9 10 10 8 3 6 6 10 15 3 | 22 24 23 25 23 22 25 25 23 27 22
31 | 6 13 5 6 9 3 8 5 7 22 3 | 28 33 26 28 26 27 34 24 29 24 27
32E | 7 9 13 12 11 4 10 6 8 11 3 | 18 24 22 22 23 22 24 17 21 23 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 9 10 10 4 8 7 9 17 |T 30 33 31 32 31 30 33 31 31 34 29
WRMS | 8 11 9 10 9 4 8 7 7 16 |NE 22 26 23 23 22 23 26 23 23 26 22
MEDI | 8 9 9 9 9 4 8 6 8 14 |MD 21 26 23 24 23 22 26 24 23 27 22
Table 3.2098.6 GPS week: 2098 Day: 6 MJD: 58936.000
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 8 9 10 8 4 8 8 9 9 3 | 21 27 24 22 24 22 30 21 20 25 22
2 | 9 9 8 10 9 4 6 7 7 22 3 | 28 26 23 28 26 25 27 24 21 29 24
3 | 8 10 7 9 8 5 9 9 7 14 3 | 33 35 35 29 32 32 35 32 30 35 31
X4E | 12 19 16 26 --- 7 21 20 23 42 8 | 26 32 27 42 --- 26 30 35 32 37 28
5 | 9 14 12 9 8 6 5 9 13 21 3 | 51 50 55 54 49 53 53 47 53 48 50
6 | 4 9 11 8 6 3 5 8 8 12 2 | 27 31 30 29 29 28 33 25 22 35 27
7 | 7 13 7 8 10 4 8 6 11 23 3 | 46 50 49 49 47 48 52 46 45 47 47
8E | 10 14 16 13 8 5 8 13 10 13 4 | 35 38 35 41 35 36 37 40 39 33 36
9E | 9 12 14 9 10 3 9 10 9 16 3 | 20 20 16 21 16 16 17 17 16 23 15
10 | 8 8 7 7 9 3 5 7 7 13 2 | 21 24 24 24 20 21 25 18 20 27 21
11 | 4 15 12 13 12 3 7 8 10 13 3 | 25 35 23 31 28 28 34 26 29 27 27
12 | 5 13 7 8 11 3 7 7 9 25 3 | 26 35 28 29 28 27 32 24 27 24 27
13E | 8 18 6 11 12 4 6 9 11 11 3 | 58 59 58 60 60 58 57 62 58 59 58
14E | 7 8 7 10 10 3 7 5 11 12 3 | 75 76 77 75 77 77 76 78 79 79 76
15E | 9 22 7 10 12 4 8 8 8 15 4 | 27 24 22 27 29 24 24 28 24 26 24
16 | 9 18 5 7 11 4 6 8 11 27 4 | 24 28 27 26 23 24 26 24 24 28 23
17E | 9 10 6 10 13 4 8 16 7 14 3 | 162 162 161 163 162 162 162 162 161 165 162
X18 | 10 --- 16 12 --- 5 --- 9 17 --- 6 | 52 --- 49 52 --- 50 --- 49 52 --- 50
19E | 5 14 7 7 11 3 9 11 10 13 3 | 68 65 70 72 67 68 69 63 67 70 67
20 | 8 12 6 10 10 3 5 5 8 19 3 | 24 27 24 25 26 25 25 22 23 28 23
21 | 8 9 7 9 13 3 5 6 8 20 3 | 17 24 17 23 23 19 22 18 19 24 18
22 | 8 11 7 7 8 4 6 8 6 21 3 | 23 29 21 20 23 22 27 24 25 28 22
X23E | 12 21 7 19 --- 8 11 9 9 --- 5 | 12 12 9 14 --- 13 12 10 11 --- 12
24 | 11 12 14 9 10 4 7 6 14 7 3 | 24 30 27 22 22 22 26 21 20 29 23
25 | 7 9 8 7 12 3 7 5 7 6 2 | 22 29 23 21 24 22 28 22 23 28 23
26 | 6 8 6 7 10 3 5 8 10 13 2 | 24 27 26 25 24 25 28 24 21 28 24
27E | 6 13 19 12 10 4 7 10 10 11 4 | 38 42 38 41 41 37 39 41 39 36 38
28 | 6 12 4 7 8 2 6 7 7 26 3 | 21 30 21 23 22 23 29 21 22 31 22
29E | 17 16 9 9 21 5 9 11 14 13 4 | 132 134 134 132 133 133 135 132 132 136 132
30 | 9 12 9 8 8 3 7 8 10 11 3 | 26 31 30 30 27 27 34 24 26 32 27
31 | 5 12 5 7 11 3 7 6 8 23 3 | 35 37 33 38 32 33 38 32 36 31 34
32E | 7 8 16 8 10 4 8 7 13 8 3 | 28 29 26 29 30 28 28 30 34 33 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 10 9 10 4 7 9 10 17 |T 39 41 39 41 40 39 41 38 39 42 38
WRMS | 7 12 10 9 10 4 7 8 8 18 |NE 28 31 29 30 27 28 31 27 27 30 28
MEDI | 8 12 7 9 10 4 7 8 9 13 |MD 26 31 27 29 28 27 30 25 26 31 27
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 4.2098 GPS week: 2098 MJD: 58930.0-58936.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 0 0 0 |U 0 0 0 |U 8 9 39 |
emr | emr 2948 |U 0 0 0 |U 0 0 0 |U 14 18 43 |
esa | esa 3058 | 0 0 0 |U 0 0 0 | 12 12 34 |
gfz | gfz 3057 |U 0 0 0 |U 0 0 0 |U 8 9 33 |
grg | grg 2824 |U 0 0 0 |U 0 0 0 | 9 9 39 |
igr | igr 3016 | 0 0 0 | 0 0 0 | 9 9 39 |
igs | igs 3058 | 0 0 0 | 0 0 0 | 9 9 38 |
jpl | jpl 2962 |U 0 0 0 |U 0 0 0 |U 15 14 45 |
mit | mit 3058 | 0 0 0 |U 0 0 0 |U 16 15 69 |
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 5.2098.0 GPS week: 2098 Day: 0 MJD: 58930.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | ---- ---- ---- | 8 9 38 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 14 17 43 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 14 11 37 |
gfz | gfz 3069 | ---- ---- ---- | ---- ---- ---- | 8 11 36 |
grg | grg 2872 | ---- ---- ---- | ---- ---- ---- | 10 9 42 |
igr | igr 3071 | ---- ---- ---- | ---- ---- ---- | 9 9 39 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 9 10 40 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 16 14 45 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 10 9 50 |
Table 5.2098.1 GPS week: 2098 Day: 1 MJD: 58931.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | ---- ---- ---- | 8 9 33 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 15 22 46 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 12 14 32 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 7 8 27 |
grg | grg 2784 | ---- ---- ---- | ---- ---- ---- | 9 10 33 |
igr | igr 3072 | ---- ---- ---- | ---- ---- ---- | 9 10 34 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 9 11 32 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 17 16 38 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 11 14 34 |
Table 5.2098.2 GPS week: 2098 Day: 2 MJD: 58932.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | ---- ---- ---- | 9 9 42 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 13 20 44 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 12 11 37 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 7 9 37 |
grg | grg 2880 | ---- ---- ---- | ---- ---- ---- | 9 9 41 |
igr | igr 3072 | ---- ---- ---- | ---- ---- ---- | 9 8 44 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 9 9 43 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 15 10 49 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 11 10 52 |
Table 5.2098.3 GPS week: 2098 Day: 3 MJD: 58933.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | ---- ---- ---- | 8 11 42 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 13 19 43 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 13 13 34 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 8 9 33 |
grg | grg 2880 | ---- ---- ---- | ---- ---- ---- | 10 9 38 |
igr | igr 2975 | ---- ---- ---- | ---- ---- ---- | 9 10 39 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 9 10 40 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 12 13 48 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 41 27 177 |
Table 5.2098.4 GPS week: 2098 Day: 4 MJD: 58934.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | ---- ---- ---- | 9 10 36 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 13 16 47 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 12 12 33 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 9 9 31 |
grg | grg 2784 | ---- ---- ---- | ---- ---- ---- | 11 9 40 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 9 11 39 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 10 10 38 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 16 16 41 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 20 25 68 |
Table 5.2098.5 GPS week: 2098 Day: 5 MJD: 58935.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | ---- ---- ---- | ---- ---- ---- | 8 6 37 |
emr | emr 2784 | ---- ---- ---- | ---- ---- ---- | 12 14 35 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 12 13 29 |
gfz | gfz 2976 | ---- ---- ---- | ---- ---- ---- | 7 8 30 |
grg | grg 2784 | ---- ---- ---- | ---- ---- ---- | 9 7 36 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 8 7 35 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 8 7 32 |
jpl | jpl 2880 | ---- ---- ---- | ---- ---- ---- | 14 13 42 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | 9 9 48 |
Table 5.2098.6 GPS week: 2098 Day: 6 MJD: 58936.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | ---- ---- ---- | 7 9 44 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 14 17 47 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 12 12 35 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 7 10 37 |
grg | grg 2784 | ---- ---- ---- | ---- ---- ---- | 9 10 47 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 8 10 41 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 8 9 42 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 16 13 49 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 9 9 53 |
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 6.2098 GPS week: 2098 MJD: 58930.500-58936.500
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 -13 49 -86 2 | 12 20
| 22 12 51 83 9 | 2
emr uuuux | 8 20 -14 3 62 | -5 46
| 36 28 118 69 20 | 23
esa uuuuu | 3 33 -54 -16 3 | 28 32
| 8 14 54 33 4 | 2
gfz uuuuu | 2 21 28 24 -3 | 26 31
| 16 21 35 101 5 | 2
grg uuuuu | 19 13 -15 -33 1 | -3 14
| 32 13 23 69 4 | 1
igr xxxxx | 26 18 7 -4 -2 | -2 16
| 8 17 67 47 5 | 3
irf xxxxx | 8 -20 -34 2 -5 | -3 18
| 8 14 26 28 6 | 4
jpl uuuuu | -6 -14 3 -44 -6 | 55 57
| 16 12 47 59 12 | 1
mit uuuuu | -11 -27 -44 19 -9 | 21 27
| 29 27 60 40 8 | 4
ngs uuuuu | 0 -13 54 97 0 | 14 22
| 76 32 47 121 3 | 1
sio uuuux | 15 28 76 76 -1 | 89 90
| 40 32 97 95 8 | 1
Table 7.2098.0 GPS week: 2098 Day: 0 MJD: 58930.500
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 | -27 -7 111 -208 1 | 15 23
emr uuuux | -29 45 -106 17 74 | -33 40
esa uuuuu | 9 30 -92 30 -4 | 31 36
gfz uuuuu | -5 26 25 7 -8 | 30 34
grg uuuuu | 30 -4 -31 48 4 | -3 12
igr xxxxx | 19 18 -42 34 0 | 3 18
irf xxxxx | -1 -29 -38 -18 -12 | 3 18
jpl uuuuu | -15 0 -42 -90 14 | 55 57
mit uuuuu | -39 -56 -50 21 -15 | 27 32
ngs uuuuu | 85 3 134 180 -4 | 16 22
sio uuuux | -25 29 142 -34 0 | 88 89
Table 7.2098.1 GPS week: 2098 Day: 1 MJD: 58931.500
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 -10 107 -107 -16 | 14 23
emr uuuux | -6 -14 132 -147 77 | -27 40
esa uuuuu | 6 8 -54 7 -1 | 28 34
gfz uuuuu | 1 3 40 -124 -3 | 27 32
grg uuuuu | 40 22 -25 -4 8 | -4 13
igr xxxxx | 30 31 -30 69 -11 | 0 18
irf xxxxx | 8 -20 -77 -23 -11 | -1 20
jpl uuuuu | -4 0 24 -56 -3 | 56 57
mit uuuuu | -27 -1 -134 -5 -19 | 25 31
ngs uuuuu | 65 -18 26 327 4 | 13 21
sio uuuux | -14 22 173 56 -12 | 89 90
Table 7.2098.2 GPS week: 2098 Day: 2 MJD: 58932.500
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 | -17 1 62 -28 4 | 12 21
emr uuuux | -17 28 60 37 73 | -18 46
esa uuuuu | -7 36 -94 2 3 | 28 33
gfz uuuuu | -30 38 91 18 -2 | 26 31
grg uuuuu | 53 5 -21 -31 2 | -3 16
igr xxxxx | 32 23 -15 -17 -4 | -1 16
irf xxxxx | 1 -1 -59 -6 -11 | -1 19
jpl uuuuu | 0 -12 1 -74 -9 | 56 58
mit uuuuu | -18 -20 -82 -1 -17 | 24 30
ngs uuuuu | 51 -41 78 98 2 | 15 24
sio uuuux | -13 36 7 30 -8 | 90 91
Table 7.2098.3 GPS week: 2098 Day: 3 MJD: 58933.500
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 | -13 -14 -26 38 10 | 11 18
emr uuuux | -5 23 -167 3 68 | -8 49
esa uuuuu | -2 53 -95 -19 4 | 26 30
gfz uuuuu | 18 50 43 83 -11 | 25 30
grg uuuuu | 39 5 -38 -9 0 | -3 15
igr xxxxx | 13 30 -60 4 -5 | -3 14
irf xxxxx | 7 -31 -24 -14 -3 | -4 17
jpl uuuuu | -2 -31 81 -47 -26 | 55 57
mit uuuuu | -30 -40 14 -11 -9 | 21 26
ngs uuuuu | 35 6 86 -23 -2 | 14 22
sio uuuux | -12 -15 177 12 0 | 89 90
Table 7.2098.4 GPS week: 2098 Day: 4 MJD: 58934.500
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 | 10 -5 23 -116 2 | 11 18
emr uuuux | 67 -25 56 64 75 | 4 47
esa uuuuu | 11 39 -86 -43 6 | 25 29
gfz uuuuu | 3 28 4 -2 4 | 23 29
grg uuuuu | -19 33 -20 -122 -1 | -3 15
igr xxxxx | 23 28 2 -78 2 | -5 15
irf xxxxx | 16 -37 -11 24 3 | -6 18
jpl uuuuu | 25 -23 -45 17 -8 | 53 56
mit uuuuu | -20 -65 41 48 -3 | 18 25
ngs uuuuu | -87 40 -3 56 -3 | 12 22
sio uuuux | 68 -5 78 233 14 | 88 89
Table 7.2098.5 GPS week: 2098 Day: 5 MJD: 58935.500
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 | 18 -20 59 -145 3 | 11 18
emr uuuux | 52 38 -133 26 36 | 20 48
esa uuuuu | -7 28 20 -22 8 | 27 31
gfz uuuuu | 8 -10 13 -18 3 | 25 30
grg uuuuu | -31 4 32 -133 -4 | -2 14
igr xxxxx | 25 -17 128 -33 4 | -3 14
irf xxxxx | 20 -4 -4 56 1 | -6 18
jpl uuuuu | -22 -16 -34 54 -10 | 54 56
mit uuuuu | 44 1 -17 95 -1 | 18 24
ngs uuuuu | -94 -30 31 9 3 | 14 22
sio uuuux | 65 48 48 179 1 | 90 91
Table 7.2098.6 GPS week: 2098 Day: 6 MJD: 58936.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 11 -37 7 -34 8 | 11 18
emr uuuux | -6 42 59 20 32 | 29 53
esa uuuuu | 11 38 25 -67 4 | 28 33
gfz uuuuu | 17 12 -21 207 -3 | 25 30
grg uuuuu | 22 23 -4 21 -4 | -1 14
igr xxxxx | 39 15 67 -3 0 | -3 14
irf xxxxx | 6 -15 -25 -1 0 | -7 17
jpl uuuuu | -22 -19 36 -111 -4 | 53 56
mit uuuuu | 11 -8 -76 -16 0 | 16 22
ngs uuuuu | -52 -51 27 36 -2 | 14 22
sio uuuux | 34 81 -89 59 -2 | 90 91
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