[IGSREPORT-28415] Wk 2190 IGS Final Orbits
acc
acc at igs.org
Fri Jan 14 05:27:57 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2190 (Dec 26, 2021 - Jan 01, 2022)
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:
igs2190[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2190[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2190[0-6].cls IGS GPS clock combination summary report.
igs21907.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21907.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 | BRFT NOVM
0 | ESA | PTBB PTBB
0 | GFZ | 5 POHN BRFT POHN
0 | GRG | LHAZ SVTL LHAZ SVTL
0 | JPL | MCM4 MCM4
1 | COD | BRFT IENG IQAL WHIT WIND IENG
1 | EMR | NLIB WHIT
1 | ESA | WHIT
1 | GFZ | POHN SFER WHIT BRFT POHN SFER
1 | GRG | 13 13 SVTL XMIS SVTL
1 | JPL | BADG BADG IQAL MCM4 WHIT
1 | MIT | SFER
2 | COD | CAS1 CKIS CPVG MCIL CPVG
2 | ESA | SVTL PTBB SVTL
2 | GFZ | POHN POHN
2 | GRG | 20 22 CPVG NLIB CPVG HYDE
2 | JPL | MCM4 CAS1 MCM4 RIOP
2 | MIT | 11 11
3 | COD | ASCG CAS1 CKIS DAV1 FAA1 MAYG MQZG POHN SEYG TUVA
3 | COD | DAV1
3 | EMR | WARK
3 | ESA | BAKE NRMD PTBB BAKE NRMD PTBB
3 | GFZ | NVSK POHN DAV1 NVSK POHN
3 | GRG | 13 13 MCM4 SCRZ SVTL MCM4 SCRZ SVTL
3 | JPL | CAS1 SVTL
4 | COD | ASCG MAYG SYOG
4 | ESA | CZTG PTBB CZTG PTBB
4 | GFZ | NVSK POHN NVSK POHN
4 | GRG | CCJ2 MCM4 SVTL MCM4 SVTL SYOG
4 | JPL | ZECK BADG ZECK
5 | COD | CAS1 INVK IQAL MAYG SCRZ
5 | EMR | NIST
5 | GFZ | 23 17 23 SGOC BOR1 SGOC
5 | GRG | 13 13 SVTL XMIS SVTL
5 | JPL | BADG MCM4 BADG CAS1 INVK IQAL MCM4
6 | COD | HYDE
6 | EMR | PERT YAR2
6 | ESA | BAKE PTBB BAKE HYDE PTBB
6 | GFZ | 23 23 HYDE NVSK POHN HYDE NVSK POHN PTBB
6 | GRG | 21 21 LHAZ MCM4 LHAZ MCM4 SVTL
6 | JPL | NICO CZTG LHAZ NICO
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
----+--------+---------------
3 | NGS | 11
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.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
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 | .2 .1 .1 1 -2 -3 -.19
EMR | 0 | 8.4 3.9 14.9 -24 3 -34 .12
ESA | 0 | -.1 .1 .3 -28 3 4 -.12
GFZ | 0 | -.1 -.3 -.4 -11 -6 1 -.07
GRG | 0 | 7.8 -3.9 8.4 -6 -20 -21 .20
JPL | 0 | 7.9 1.8 12.8 0 0 0 .39
MIT | 0 | 4.1 4.6 22.8 28 -26 -85 .05
NGS | 0 | 4.4 9.2 22.7 37 -69 20 -.05
SIO | 0 | 1.9 4.8 32.2 84 -84 35 -.26
COD | 1 | .1 .2 -.1 -3 0 -3 -.16
EMR | 1 | 6.4 -2.2 14.9 -33 0 -39 .19
ESA | 1 | -.2 .1 .6 -25 -2 14 -.03
GFZ | 1 | .1 -.2 -.0 -13 -12 -1 -.06
GRG | 1 | 2.9 -.3 5.5 -8 -15 10 .15
JPL | 1 | 11.1 -.3 19.0 -13 -3 -6 .01
MIT | 1 | 4.9 4.2 23.7 32 -35 -33 .11
NGS | 1 | 5.3 .9 14.8 9 -52 -4 .12
SIO | 1 | 2.1 3.1 32.9 55 -96 4 -.14
COD | 2 | .1 .3 -.0 -3 -1 -3 -.15
EMR | 2 | 3.5 4.0 18.8 -20 1 -47 .18
ESA | 2 | -.3 -.1 .4 -17 -9 12 -.10
GFZ | 2 | .5 -.2 -.0 -6 -11 11 -.16
GRG | 2 | 1.8 1.7 8.0 -7 -3 0 .18
JPL | 2 | -.1 4.0 12.6 0 0 0 .12
MIT | 2 | 5.0 4.6 25.0 19 -28 -55 -.09
NGS | 2 | 6.4 3.6 16.4 23 -73 6 -.24
SIO | 2 | 5.2 2.6 33.6 40 -129 27 -.38
COD | 3 | .1 .0 -.0 -4 0 -1 -.16
EMR | 3 | 3.8 -3.5 17.8 -25 -9 -55 .21
ESA | 3 | -.3 -.5 .5 -22 14 26 .06
GFZ | 3 | .3 -.3 -.0 -9 -6 -1 -.08
GRG | 3 | 1.1 1.8 11.1 -21 -23 -3 .03
JPL | 3 | 3.3 .2 14.9 -23 -5 0 -.01
MIT | 3 | 4.4 4.1 28.4 42 -30 11 -.01
NGS | 3 | 3.6 .2 19.8 9 -72 -3 -.19
SIO | 3 | 3.1 4.2 37.1 68 -110 66 -.29
COD | 4 | .2 .4 -.0 3 -3 -3 -.19
EMR | 4 | 4.0 -3.5 12.4 -12 -19 -19 .17
ESA | 4 | -1.0 .2 .4 -23 -3 20 -.18
GFZ | 4 | .4 -.1 .0 -12 -9 -5 -.02
GRG | 4 | 3.7 .6 13.1 -30 4 -14 .21
JPL | 4 | 4.9 -.7 11.6 -2 0 4 -.19
MIT | 4 | 5.1 5.0 24.8 81 -20 56 .05
NGS | 4 | 1.4 -1.1 21.3 1 -63 -16 -.04
SIO | 4 | 6.7 4.8 30.8 93 -163 121 -.21
COD | 5 | .2 .3 .1 4 -3 0 -.18
EMR | 5 | 4.3 .3 15.5 -8 -30 -15 .34
ESA | 5 | -1.3 -.1 -.1 -21 0 12 -.11
GFZ | 5 | .4 -.3 .2 -10 -7 5 -.18
GRG | 5 | 3.2 .1 17.9 -27 9 -2 .07
JPL | 5 | 1.3 4.5 15.2 1 7 -5 .09
MIT | 5 | 5.2 4.2 24.5 -17 -43 -29 -.13
NGS | 5 | 3.6 -1.2 6.9 -5 3 -17 -.05
SIO | 5 | 6.4 4.7 29.7 92 -143 161 -.40
COD | 6 | .1 .2 -.0 1 -3 0 -.16
EMR | 6 | 3.8 -3.0 12.3 -17 -24 -15 .30
ESA | 6 | -1.2 -.5 .3 -20 -7 23 -.0
GFZ | 6 | .2 -.1 .2 -16 -3 -5 -.05
GRG | 6 | 4.0 -1.4 15.4 -29 14 -12 .08
JPL | 6 | -2.1 1.3 20.3 1 9 -6 -.10
MIT | 6 | 4.9 1.5 24.7 10 -30 -27 .06
NGS | 6 | -1.8 -2.3 10.6 6 -28 -14 -.07
SIO | 6 | 4.8 -1.2 31.5 38 20 171 -.46
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 1.2190.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2190.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 2.2190.[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 3.2190.[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 5.2190.0-6). 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 2190 summary. (Dec 26, 2021 - Jan 01, 2022)
Table 1.2190.a GPS week: 2190 MJD: 59574.000-59580.000
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 673| 0 0 4 0 -2 2 .03 7 7 | -479 -139 7 114
| 0 0 1 9 16 14 .02 | 137 434
emr 79| -1 -1 2 -1 -18 -17 .15 14 14 | 202174 22 14 83
| 1 1 1 11 16 8 .02 | 444 528
esa 149| 0 0 0 -16 -3 8 -.03 7 7 | -614 -58 7 88
| 0 0 1 13 10 10 .02 | 198 514
gfz 239| 0 1 -2 -5 6 8 .19 10 10 | 4 -141 12 158
| 1 0 1 12 9 15 .03 | 134 336
grg 112| 1 -3 -4 -2 4 -4 -.09 10 9 | -17 -45 8 139
| 0 0 3 6 17 15 .03 | 123 235
igr n/a| 0 0 -3 0 1 -1 .06 5 5 | -1567 -32 13 109
| 0 0 1 15 10 12 .02 | 166 397
jpl 80| 0 -1 4 -12 5 -22 .14 9 10 | 957 -56 9 100
| 0 0 0 19 13 18 .02 | 331 476
mit 373| 1 0 0 16 -16 -26 -.15 8 8 | -2465 -1223 27 2147
| 0 0 1 35 13 28 .01 | 1147 3389
ngs 213| 0 1 0 -12 5 -11 -.01 10 9 | -3856 4316 809 1691
| 0 0 4 23 17 8 .01 | 6598 8295
sio 406| 0 0 -7 51 49 69 -.16 11 11 | --- --- --- ---
| 0 0 1 61 45 58 .02 | --- ---
Table 1.2190.b GPS week : 2190 MJD: 59574.000-59580.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 3 3 3 3 3 |
2 | 4 3 3 3 3 3 3 |
3 | 4 3 3 3 3 3 3 |
4 | 3 4 3 3 3 3 3 |
5 | 4 4 4 4 4 4 4 |
6 | 3 3 3 3 3 3 3 |
7 | 3 3 3 3 3 3 3 |
8 | 3 3 3 3 4 3 4 |
9 | 3 3 3 3 3 3 4 |
10 | 4 3 4 3 4 3 4 |
11 | 6 6 5 7 5 5 5 |
12 | 4 4 4 4 5 4 5 |
13 | 3 3 3 3 3 3 4 |
14 | 5 5 5 5 4 4 5 |
15 | 3 3 3 3 3 3 4 |
16 | 5 5 4 4 5 5 5 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 4 4 5 4 4 |
19 | 3 3 4 3 4 3 4 |
20 | 4 4 4 4 4 3 4 |
21 | 3 3 3 3 3 3 3 |
22 | 5 4 5 5 4 3 4 |
23 | 5 5 5 5 6 6 6 |
24 | 3 3 3 3 3 3 3 |
25 | 4 3 4 3 3 3 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 4 3 4 3 3 4 |
28 | 4 4 4 4 4 4 4 |
29 | 4 3 3 3 4 4 4 |
30 | 3 3 3 2 3 3 3 |
31 | 3 3 4 3 3 3 3 |
32 | 3 3 3 3 3 3 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 2.2190.0 GPS week: 2190 Day: 0 MJD: 59574.000
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 684| 0 0 4 -5 -10 0 .03 7 7 | -266 -483 8 126
emr 80| -2 0 1 4 -23 -12 .18 15 15 | 201863 513 14 95
esa 149| 0 -1 1 2 3 14 -.06 8 8 | -847 289 8 80
gfz 235| -1 1 -2 -26 5 12 .14 9 10 | -35 58 12 268
grg 114| 0 -3 -8 -1 -6 12 -.05 11 10 | -51 110 10 133
igr n/a| 0 1 -5 17 -3 0 .06 5 5 | -1482 346 13 126
jpl 80| 0 -1 4 12 -6 -14 .13 10 10 | 1248 309 9 101
mit 373| 1 0 -1 36 -17 -18 -.14 8 8 | -2564 324 28 1802
ngs 215| 0 2 2 1 13 -17 -.01 10 10 | -233 -469 780 1688
sio 425| 1 0 -8 -29 82 34 -.14 11 11 | --- --- --- ---
Table 2.2190.1 GPS week: 2190 Day: 1 MJD: 59575.000
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 681| 0 0 5 6 -8 -8 .05 7 6 | -662 656 8 116
emr 80| -2 -2 1 -14 0 -17 .13 15 15 | 202183 -283 13 78
esa 149| 0 0 0 -21 -8 18 -.02 7 7 | -759 474 7 91
gfz 242| 0 3 -2 1 8 20 .19 10 9 | -34 84 13 303
grg 119| 0 -3 -6 -1 0 -7 -.06 10 9 | 25 64 8 135
igr n/a| 0 0 -3 14 -1 0 .06 4 4 | -1398 -129 14 126
jpl 80| 0 0 4 -28 5 8 .12 10 10 | 1221 -393 10 94
mit 373| 1 0 0 26 -3 -12 -.15 9 8 | -2757 -32 29 1711
ngs 216| 0 1 2 -2 -14 -3 -.01 10 9 | -649 564 829 1709
sio 422| 1 0 -8 20 60 -16 -.15 10 10 | --- --- --- ---
Table 2.2190.2 GPS week: 2190 Day: 2 MJD: 59576.000
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 678| 0 0 5 -1 -6 26 .02 7 6 | -628 222 8 103
emr 80| 0 0 3 8 -12 -32 .14 14 14 | 201626 -197 14 81
esa 150| 0 0 1 -10 -2 15 -.00 7 7 | -661 -210 7 75
gfz 246| 0 0 -1 0 9 28 .20 10 10 | 193 -540 13 139
grg 113| 0 -3 -4 7 17 14 -.09 12 10 | 32 -305 9 124
igr n/a| 0 0 -4 0 13 23 .05 5 5 | -1778 -197 12 88
jpl 80| -2 -1 5 2 11 -29 .12 9 9 | 365 123 9 116
mit 373| 1 0 -1 6 -13 -51 -.17 8 8 | -9 -8832 25 4515
ngs 219| 0 1 -1 4 -4 -5 -.02 9 8 | -6823 21147 712 1479
sio 419| 0 0 -10 -2 20 33 -.18 12 11 | --- --- --- ---
Table 2.2190.3 GPS week: 2190 Day: 3 MJD: 59577.000
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 671| 0 1 4 19 20 -3 .06 8 7 | -367 -585 8 118
emr 80| -2 -1 3 -1 -44 -27 .18 14 14 | 201867 541 13 103
esa 150| 1 0 0 -22 -22 3 -.00 7 7 | -389 -439 7 71
gfz 242| -1 0 -5 2 -3 10 .18 10 9 | -197 182 11 79
grg 113| 1 -2 -4 -5 -24 -10 -.13 9 9 | 102 -123 7 119
igr n/a| 0 0 -3 9 -13 -15 .06 4 4 | -1696 326 14 120
jpl 80| 0 -1 3 -41 -18 -27 .15 9 9 | 643 542 9 107
mit 373| 0 0 1 22 -5 -11 -.15 8 7 | -3173 747 27 1550
ngs 217| 0 0 3 0 22 -3 -.03 10 10 | -17822 9765 746 1671
sio 421| 0 0 -8 41 99 53 -.15 10 10 | --- --- --- ---
Table 2.2190.4 GPS week: 2190 Day: 4 MJD: 59578.000
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 662| 0 0 2 0 -19 -13 .02 7 6 | -481 -325 7 105
emr 79| -1 -2 3 -13 3 -8 .12 14 14 | 202189 345 14 74
esa 150| 0 0 0 -31 11 -10 -.04 8 8 | -782 553 9 98
gfz 243| -2 1 -3 6 25 -8 .17 10 8 | -86 170 14 77
grg 110| 1 -2 -3 -10 13 -22 -.09 10 9 | -279 329 7 138
igr n/a| 0 0 -4 -8 15 -6 .04 5 4 | -1677 188 13 112
jpl 80| 0 -1 3 -29 9 -13 .14 9 9 | 1067 114 9 94
mit 373| 1 1 1 71 -20 10 -.14 9 8 | -3577 93 29 2028
ngs 217| 0 0 4 -60 32 -18 -.02 10 10 | -516 -304 1040 1935
sio 420| 0 1 -8 92 -30 114 -.15 11 11 | --- --- --- ---
Table 2.2190.5 GPS week: 2190 Day: 5 MJD: 59579.000
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 667| 0 0 3 -8 20 18 .05 7 7 | -476 -202 7 111
emr 80| -1 0 4 16 -26 -15 .16 14 14 | 202612 167 16 79
esa 150| 1 0 0 -3 0 4 -.03 7 7 | -519 -837 8 96
gfz 226| 0 2 -2 0 -1 10 .21 10 9 | 53 -404 13 128
grg 110| 0 -3 1 4 1 3 -.12 10 9 | 42 -332 7 175
igr n/a| -1 0 0 3 1 -3 .07 5 5 | -1611 39 14 108
jpl 80| 0 -1 4 -6 20 -35 .17 9 9 | 1163 -211 9 85
mit 373| 0 0 2 -38 -9 -74 -.14 8 7 | -2665 0 27 1515
ngs 202| 0 0 -8 -5 -6 -8 -.00 9 9 | -428 -310 749 1696
sio 408| 0 0 -7 97 29 139 -.18 11 11 | --- --- --- ---
Table 2.2190.6 GPS week: 2190 Day: 6 MJD: 59580.000
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 672| 0 0 2 -4 -15 -2 .01 8 7 | -478 -257 8 120
emr 80| -3 0 2 -9 -22 -11 .15 14 14 | 202882 -926 18 71
esa 150| 1 0 -2 -29 -5 16 -.02 8 8 | -347 -242 9 109
gfz 239| 0 0 -2 -18 0 -14 .21 11 12 | 139 -542 12 115
grg 110| 1 -3 -2 -7 27 -21 -.09 12 11 | 6 -60 10 155
igr n/a| 0 1 -2 -28 -5 -5 .11 6 6 | -1330 -799 15 86
jpl 80| 0 -1 6 0 14 -47 .13 10 10 | 996 -877 12 109
mit 373| 0 0 3 -8 -44 -28 -.14 9 8 | -2515 -865 29 1909
ngs 209| 0 1 -2 -27 -5 -24 .01 9 9 | -527 -177 808 1664
sio 333| 0 0 -4 141 81 127 -.15 11 9 | --- --- --- ---
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 3.2190.0 GPS week: 2190 Day: 0 MJD: 59574.000
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 7 8 9 6 9 7 11 9 3 | 29 31 29 27 29 30 32 24 28 25 27
2 | 9 19 6 12 9 2 8 8 7 14 3 | 26 25 27 30 24 24 25 28 27 26 25
3E | 10 11 9 8 15 5 9 7 10 9 3 | 30 26 30 27 34 28 27 27 30 30 27
4 | 6 16 4 9 9 4 16 6 7 9 3 | 73 70 73 77 77 75 72 76 76 80 74
5E | 7 12 9 7 12 6 9 10 10 13 3 | 39 36 39 35 42 39 37 40 38 46 38
6 | 5 10 7 11 8 5 7 5 8 11 2 | 25 27 26 21 22 24 26 20 26 23 22
7 | 5 11 6 7 9 5 6 6 7 7 2 | 49 51 50 48 47 47 53 49 49 48 49
8 | 7 11 8 9 7 6 9 9 7 12 3 | 33 34 35 39 36 35 32 32 35 36 33
9 | 4 12 6 6 6 5 10 8 6 9 2 | 26 32 24 27 25 25 31 26 27 27 25
10E | 11 9 6 9 13 7 9 9 16 10 3 | 30 29 32 30 33 32 32 31 32 33 30
X11 | 11 23 18 17 13 7 12 11 15 --- 5 | 88 79 73 88 88 79 82 80 75 --- 84
12E | 9 26 9 10 13 8 10 8 8 13 4 | 58 59 53 52 61 53 57 55 53 55 55
13 | 5 11 7 6 7 6 10 5 8 14 2 | 25 32 26 28 24 25 31 25 25 26 25
14E | 8 17 10 14 17 6 11 15 17 11 4 | 91 92 90 95 95 92 92 93 91 95 91
15 | 7 7 5 5 8 4 7 6 8 9 2 | 70 69 67 68 63 65 70 65 70 64 67
16E | 7 25 11 14 20 7 11 11 11 14 4 | 38 45 37 44 46 39 40 44 41 46 40
17 | 6 10 8 9 8 3 8 9 6 9 3 | 38 43 36 42 38 39 39 40 39 46 38
18 | 10 18 14 12 10 6 11 8 13 9 4 | 82 80 78 82 78 76 82 80 82 45 80
19 | 7 18 5 9 9 4 8 7 10 10 3 | 33 42 35 36 32 35 33 36 39 43 34
20E | 7 14 7 13 6 4 7 10 10 17 3 | 34 37 33 40 35 34 32 32 38 42 34
21 | 8 10 5 6 7 5 8 6 9 7 2 | 26 27 25 29 27 27 27 25 30 30 26
X22E | 10 8 11 11 29 9 10 8 13 --- 5 | 44 40 36 40 47 38 39 39 38 --- 39
23E | 11 25 11 16 18 6 10 13 17 16 5 | 48 52 54 59 54 55 52 52 50 53 51
24 | 8 11 6 9 7 3 9 6 7 7 2 | 30 39 31 31 31 31 36 30 31 34 31
25E | 7 14 9 8 19 6 13 9 11 9 3 | 58 60 60 60 60 60 60 59 60 59 59
26 | 6 18 8 5 15 5 10 13 14 18 4 | 40 44 41 39 45 40 39 42 40 43 40
X27 | 6 10 8 13 7 4 9 10 9 --- 3 | 34 34 36 40 35 35 35 35 34 --- 34
X28E | 11 10 6 13 8 6 11 7 8 --- 3 | 33 36 36 37 37 37 32 36 34 --- 34
29 | 6 20 7 8 8 4 9 8 10 14 3 | 39 47 40 40 38 40 42 39 38 41 39
30 | 3 10 6 7 7 4 9 6 7 9 2 | 21 28 22 21 19 21 27 20 23 24 21
31 | 5 11 6 6 7 4 10 9 10 9 2 | 45 48 48 44 43 43 51 44 46 45 45
32 | 6 13 6 9 6 3 12 8 10 9 3 | 32 37 33 28 30 31 39 29 28 29 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 15 8 9 11 5 10 8 10 11 |T 42 44 42 43 43 42 43 42 42 42 42
WRMS | 7 15 8 10 10 5 10 8 10 11 |NE 41 43 40 42 40 40 43 40 41 38 40
MEDI | 7 11 7 9 9 5 9 8 10 9 |MD 34 39 36 39 37 37 37 36 38 42 34
Table 3.2190.1 GPS week: 2190 Day: 1 MJD: 59575.000
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 7 8 10 4 8 7 9 8 2 | 23 24 24 21 24 22 24 19 24 22 21
2 | 8 20 5 12 10 3 8 7 8 8 3 | 23 25 24 27 22 24 21 25 26 26 22
3E | 7 9 7 8 12 5 8 8 12 9 3 | 21 21 20 19 23 19 20 18 20 20 19
4 | 5 15 5 9 10 4 16 6 12 11 3 | 48 48 51 56 52 52 52 53 56 56 51
5E | 9 12 10 12 10 7 11 10 8 12 3 | 35 35 35 34 37 36 33 37 36 36 34
6 | 5 9 8 12 10 3 8 7 6 9 3 | 24 25 26 24 23 23 27 20 24 23 22
7 | 5 9 7 5 10 3 7 7 7 8 2 | 38 37 36 39 34 36 38 37 36 37 36
8 | 5 11 7 8 6 4 8 8 12 7 2 | 26 27 26 27 28 25 24 23 27 30 25
9 | 6 13 8 8 8 4 8 7 7 10 3 | 20 27 19 23 19 18 25 17 19 18 19
10E | 10 10 6 9 13 6 8 6 11 8 3 | 26 26 25 24 25 26 24 24 27 25 24
X11 | 11 25 16 16 14 6 16 11 12 --- 5 | 57 55 62 59 58 53 56 52 60 --- 55
12E | 11 23 7 10 10 8 9 8 10 12 3 | 40 41 34 35 35 34 38 35 36 35 35
13 | 4 11 8 6 5 4 12 6 6 13 2 | 21 28 22 20 20 21 27 19 18 20 20
14E | 9 19 8 16 13 5 12 12 17 13 4 | 70 73 72 76 76 73 74 72 74 72 72
15 | 6 8 5 7 7 3 8 6 9 13 2 | 49 49 45 45 43 46 48 46 50 44 46
16E | 7 26 11 12 10 4 9 17 13 14 4 | 22 27 22 25 23 23 22 26 28 23 21
17 | 7 15 7 7 8 3 6 8 7 8 2 | 28 31 26 30 27 29 30 27 31 32 28
X18 | 10 17 14 10 9 5 12 8 8 --- 4 | 46 47 44 45 44 44 46 43 45 --- 44
19 | 7 20 7 10 9 4 6 7 10 8 3 | 23 25 27 30 23 25 27 26 28 29 25
20E | 5 11 7 11 11 5 8 13 12 12 3 | 36 36 36 37 40 37 35 33 34 41 35
21 | 6 10 5 7 10 3 9 7 8 7 2 | 22 22 21 26 24 22 21 21 24 27 21
X22E | 8 8 10 9 10 6 8 10 12 --- 3 | 46 40 39 40 49 41 39 45 51 --- 43
23E | 11 22 10 15 14 7 11 10 15 15 4 | 28 35 35 40 36 35 33 30 32 34 32
24 | 8 16 5 6 8 3 9 6 9 10 3 | 30 41 30 33 31 30 35 28 31 31 31
25 | 6 12 8 7 17 4 11 8 7 5 3 | 31 31 32 31 33 30 32 29 27 29 29
26 | 6 19 7 11 11 4 11 13 8 14 4 | 35 39 35 33 39 36 36 36 36 36 35
X27 | 6 12 9 14 6 4 8 13 10 --- 3 | 26 25 28 30 27 25 25 23 26 --- 25
X28E | 10 15 8 13 7 5 8 11 11 --- 4 | 24 24 24 26 25 25 28 24 28 --- 23
29 | 7 19 7 7 7 4 9 9 9 11 3 | 28 32 26 29 29 29 27 28 28 28 27
30 | 5 11 7 5 6 3 8 7 8 9 2 | 26 31 26 26 23 25 30 25 23 27 25
31 | 4 11 6 8 4 4 9 7 7 9 2 | 33 34 32 28 31 30 38 31 34 33 32
32 | 4 10 5 9 6 3 11 6 7 9 2 | 19 26 17 15 16 17 26 16 17 18 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 15 7 10 10 4 10 9 10 10 |T 32 33 31 32 32 31 33 30 33 31 31
WRMS | 6 15 7 9 9 4 10 8 9 10 |NE 30 33 30 31 30 30 32 29 31 29 29
MEDI | 6 12 7 9 10 4 8 8 9 9 |MD 28 31 27 30 28 29 30 27 28 29 27
Table 3.2190.2 GPS week: 2190 Day: 2 MJD: 59576.000
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 10 7 7 10 6 9 7 8 11 3 | 26 28 29 26 27 27 31 27 28 28 26
2 | 7 14 5 12 10 3 8 8 5 8 3 | 20 22 23 29 20 21 23 23 24 22 21
3E | 9 8 6 11 9 5 7 8 10 10 3 | 22 21 21 21 21 20 20 19 22 22 19
4 | 5 13 4 7 10 4 13 6 8 8 3 | 59 57 58 58 60 61 56 58 60 63 58
5E | 9 11 8 9 13 7 10 9 7 16 3 | 28 31 29 29 33 29 28 32 31 37 30
6 | 5 8 8 14 6 3 9 7 7 8 3 | 24 25 27 22 22 25 28 23 25 25 23
7 | 5 11 6 8 9 4 9 6 8 10 2 | 37 40 35 38 32 34 43 37 36 39 36
8 | 5 11 8 8 7 3 8 8 7 8 2 | 25 27 29 31 26 28 25 25 30 30 26
9 | 5 10 7 6 7 4 9 8 9 8 2 | 21 28 19 20 19 19 28 20 20 17 20
10E | 12 11 6 12 13 6 9 8 11 9 3 | 22 21 22 22 24 23 21 20 23 22 20
X11 | 9 22 --- 10 12 7 14 10 7 --- 4 | 55 53 --- 55 57 56 53 55 99 --- 54
12E | 8 21 8 9 15 8 10 7 10 12 3 | 39 37 32 35 40 33 36 34 34 34 34
13 | 5 12 6 7 6 4 11 7 8 11 2 | 15 26 16 15 14 18 24 16 20 17 16
14E | 8 19 9 11 14 6 11 12 15 15 4 | 73 74 74 76 73 75 73 70 74 72 72
15 | 6 9 6 6 6 3 6 6 8 10 2 | 51 53 48 49 46 48 51 45 49 44 48
16E | 6 28 9 13 10 5 9 13 9 16 4 | 27 31 25 32 27 25 25 26 28 26 25
17 | 6 13 5 8 7 4 7 7 7 11 2 | 35 37 36 38 34 38 33 37 37 42 35
X18 | 9 18 13 11 9 5 12 10 9 --- 4 | 51 53 52 54 53 51 54 52 51 --- 51
19 | 10 19 6 14 8 5 8 9 8 10 3 | 27 32 31 38 26 31 28 30 30 36 29
20E | 8 13 6 8 26 6 7 9 8 16 4 | 17 18 16 18 31 18 17 19 19 23 17
21 | 8 12 5 7 9 5 8 6 8 7 2 | 20 21 22 25 21 22 23 19 22 21 20
X22E | 9 10 9 8 31 6 7 8 10 --- 4 | 30 25 24 24 37 24 28 26 26 --- 25
23E | 11 19 8 18 17 8 10 11 18 16 5 | 28 32 34 41 36 36 32 29 34 32 31
24 | 8 12 7 7 9 2 9 6 7 10 3 | 25 34 29 29 24 28 35 28 27 30 28
25 | 7 14 8 12 14 5 10 7 7 7 3 | 38 41 41 39 39 40 42 39 39 40 39
26 | 6 15 7 9 11 5 8 11 9 19 3 | 29 31 31 29 32 28 30 30 28 35 29
X27 | 5 10 8 10 9 2 8 12 6 --- 3 | 26 28 27 29 26 26 26 24 27 --- 25
X28E | 8 16 6 15 10 7 11 7 12 --- 4 | 25 27 27 29 27 29 28 25 31 --- 25
29 | 6 18 6 6 9 5 6 9 6 15 3 | 26 31 26 29 25 29 27 28 27 27 26
30 | 4 10 6 5 8 4 9 5 7 12 2 | 17 26 19 19 16 18 26 18 19 24 18
31 | 5 10 6 8 22 3 8 7 9 11 3 | 33 40 36 36 31 33 39 34 32 37 34
32 | 5 11 6 8 6 3 10 7 6 9 2 | 24 31 24 23 23 23 28 20 22 20 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 7 10 12 5 9 8 9 12 |T 31 33 31 33 31 31 33 30 33 32 30
WRMS | 6 14 7 10 10 5 9 8 8 11 |NE 30 34 30 32 30 31 33 30 33 30 30
MEDI | 7 12 6 8 9 5 9 8 8 10 |MD 26 31 29 29 27 28 28 27 28 30 26
Table 3.2190.3 GPS week: 2190 Day: 3 MJD: 59577.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 10 8 8 8 3 9 4 8 6 2 | 24 25 25 24 22 23 25 22 27 27 23
2 | 5 14 6 10 11 4 9 7 10 6 3 | 21 22 23 24 22 20 22 23 24 23 21
3E | 8 9 7 10 9 4 9 7 10 7 3 | 20 19 21 21 21 20 21 19 22 24 19
4 | 6 14 4 7 10 4 14 6 8 8 3 | 36 38 40 39 40 39 39 36 37 40 38
5E | 8 12 10 12 13 7 10 9 13 8 3 | 24 28 26 28 27 25 26 25 29 31 25
6 | 5 9 7 14 5 3 7 6 10 7 2 | 25 27 25 20 22 23 27 20 28 23 22
7 | 4 11 7 7 6 2 8 4 8 8 2 | 35 40 35 35 30 33 39 36 36 35 35
8 | 4 10 7 8 8 4 8 7 9 9 2 | 28 31 33 33 30 32 31 30 30 33 30
9 | 6 10 7 7 5 4 8 8 6 8 2 | 22 28 20 23 19 20 29 20 23 23 21
10E | 11 9 5 9 8 6 7 6 11 8 3 | 24 24 23 23 23 22 23 23 24 26 22
X11 | 12 21 --- 24 11 19 13 10 516 --- 6 | 52 50 --- 51 53 45 49 50 425 --- 49
12E | 15 23 8 10 14 6 9 7 10 10 4 | 51 46 45 44 49 46 46 44 49 45 46
13 | 6 10 6 9 5 4 12 8 7 14 3 | 18 26 18 15 17 19 27 17 22 23 18
14 | 9 18 9 16 13 8 14 11 14 12 4 | 58 57 55 64 59 57 58 54 57 59 57
15 | 7 7 5 6 6 4 7 9 7 12 2 | 55 58 51 52 51 50 55 52 53 46 52
16E | 5 22 11 8 11 5 7 10 10 13 3 | 29 30 29 30 28 28 28 27 31 29 27
17 | 10 11 5 11 9 4 8 7 10 9 3 | 32 33 29 34 29 30 32 31 32 38 30
X18 | 10 16 12 11 9 5 11 9 11 --- 4 | 58 59 56 60 58 56 59 61 61 --- 58
19 | 10 19 6 9 9 3 8 6 7 8 3 | 27 31 28 30 26 27 28 28 32 34 27
20E | 7 11 6 10 12 6 7 9 12 15 3 | 24 27 25 26 25 25 26 23 29 32 24
21 | 6 12 6 7 11 4 7 5 7 7 2 | 20 24 22 26 22 22 24 22 25 28 22
X22E | 7 10 10 12 30 7 11 8 9 --- 5 | 24 24 24 23 38 24 24 26 26 --- 24
23E | 11 18 9 20 16 6 11 12 18 18 5 | 25 27 31 41 31 31 30 23 29 30 27
24 | 8 12 6 7 7 3 10 4 11 7 2 | 20 32 21 26 19 22 31 21 21 25 22
25 | 8 15 7 10 9 3 11 7 10 8 3 | 34 37 36 36 36 36 38 32 35 36 34
26 | 6 16 8 10 10 5 8 9 8 15 3 | 25 27 29 26 27 25 27 27 25 30 25
27 | 6 13 9 7 7 4 9 9 12 13 3 | 27 30 32 31 27 29 30 29 28 17 28
X28E | 7 13 4 16 10 4 9 8 8 --- 3 | 25 25 25 32 27 25 26 24 29 --- 25
29 | 8 18 5 7 8 4 7 9 7 10 3 | 31 33 29 30 29 30 31 28 27 31 29
30 | 6 9 4 4 7 2 9 5 6 6 2 | 18 28 20 21 16 19 27 20 22 23 20
31 | 5 11 8 7 6 3 10 6 10 8 2 | 38 42 38 36 37 36 47 39 38 40 38
32 | 5 10 6 7 5 3 8 7 6 8 2 | 22 29 21 20 19 21 28 19 21 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 7 10 9 4 9 8 10 10 |T 30 33 30 32 30 30 32 29 43 31 29
WRMS | 7 14 7 9 9 4 9 7 10 10 |NE 30 33 29 31 29 29 33 30 49 29 29
MEDI | 7 12 7 9 9 4 9 7 10 8 |MD 25 29 28 30 27 25 28 26 29 30 25
Table 3.2190.4 GPS week: 2190 Day: 4 MJD: 59578.000
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 7 10 8 4 7 5 10 10 3 | 27 25 26 25 23 24 28 22 28 22 24
2 | 5 16 7 9 8 3 9 8 9 8 3 | 19 22 20 26 22 21 19 21 23 21 20
3E | 7 10 7 10 10 4 7 8 11 10 3 | 21 20 20 23 20 20 22 18 21 20 19
4 | 4 12 6 6 9 4 13 6 11 9 3 | 55 55 59 57 58 57 58 56 57 57 56
5E | 7 12 10 8 16 6 11 10 8 11 3 | 23 25 22 23 26 24 23 25 25 27 23
6 | 5 9 7 10 7 3 7 4 9 6 2 | 22 22 23 20 20 21 24 17 23 20 20
7 | 3 12 8 7 7 3 8 6 9 8 2 | 37 43 38 38 35 36 42 36 37 35 37
8 | 6 11 13 10 6 5 9 10 11 12 3 | 23 25 25 25 22 25 25 22 24 29 22
9 | 5 11 9 14 5 4 8 7 8 9 3 | 21 28 19 27 20 20 28 19 21 18 20
10E | 11 10 7 10 10 5 9 9 11 10 3 | 21 18 21 20 21 20 20 21 23 21 19
X11 | 8 23 17 13 14 6 12 10 14 --- 5 | 48 50 46 47 50 46 45 46 128 --- 46
12E | 16 23 9 11 15 8 9 9 10 11 4 | 82 82 80 84 79 80 82 83 84 84 81
13 | 4 11 6 9 6 4 12 9 7 11 3 | 19 28 19 18 21 20 29 20 22 22 20
14 | 10 20 11 15 9 6 11 11 11 12 4 | 63 65 62 69 65 64 64 63 62 64 63
15 | 4 10 7 7 6 3 9 8 10 11 2 | 46 52 44 45 46 44 49 43 51 40 46
16E | 8 22 12 8 9 7 9 14 13 19 4 | 27 27 22 29 27 25 24 30 34 30 26
17 | 9 12 5 9 9 4 8 8 12 10 3 | 31 30 27 36 30 30 29 29 31 33 29
X18 | 10 20 13 10 8 5 13 10 9 --- 4 | 51 49 47 52 49 47 50 54 54 --- 50
19 | 9 19 4 10 10 4 9 8 12 10 3 | 25 24 24 29 23 23 24 23 28 27 23
20E | 5 11 7 9 18 6 10 13 10 16 4 | 22 25 21 24 25 22 20 26 22 28 22
21 | 5 9 6 10 8 4 9 6 9 8 2 | 22 21 21 28 21 22 22 20 27 23 21
X22E | 6 8 9 12 10 6 9 9 12 --- 3 | 27 25 24 28 30 26 26 26 29 --- 26
23E | 10 21 9 24 16 7 11 14 19 17 5 | 25 29 31 43 28 32 31 26 28 29 28
24 | 7 11 5 7 7 3 11 6 8 10 2 | 23 34 24 25 24 26 34 24 28 25 25
25 | 7 11 5 6 10 3 12 9 5 8 3 | 34 35 37 33 38 34 36 32 36 32 34
26 | 7 14 9 8 10 4 9 14 10 19 4 | 27 29 30 27 30 28 27 29 28 30 27
27 | 6 10 9 9 6 4 9 11 11 11 3 | 24 25 28 26 22 25 24 21 23 17 23
X28E | 8 12 7 14 11 6 8 11 9 --- 3 | 36 39 37 41 37 38 36 38 39 --- 36
29 | 9 23 8 5 9 3 8 11 10 12 3 | 29 27 25 26 26 26 27 24 28 26 25
30 | 4 11 6 8 6 3 9 7 7 10 2 | 17 28 18 20 16 19 26 17 19 19 19
31 | 6 10 6 4 7 4 8 9 8 13 2 | 36 40 36 37 35 34 43 40 38 40 37
32 | 5 10 6 8 8 3 9 9 8 10 2 | 21 25 18 20 18 19 24 18 22 17 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 10 10 5 9 9 10 11 |T 31 33 31 33 31 31 33 30 35 30 30
WRMS | 6 14 8 8 9 4 9 8 10 11 |NE 29 32 29 31 29 29 32 28 35 27 28
MEDI | 7 11 7 9 9 4 9 9 10 10 |MD 25 28 25 27 26 25 27 25 28 27 25
Table 3.2190.5 GPS week: 2190 Day: 5 MJD: 59579.000
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 8 8 5 8 5 7 9 2 | 20 22 21 21 19 21 22 17 18 17 18
2 | 6 15 6 7 9 4 7 8 8 13 3 | 16 18 19 20 19 18 16 20 20 21 16
3E | 9 9 6 12 11 4 10 6 9 9 3 | 23 20 22 23 21 21 22 20 23 23 20
4 | 6 11 5 5 11 6 12 7 7 8 2 | 58 58 55 59 60 57 59 60 60 62 58
5E | 10 9 10 11 17 6 11 11 6 11 4 | 22 21 23 23 26 20 21 23 23 24 21
6 | 6 13 6 11 8 2 9 4 6 10 2 | 23 28 22 19 19 21 25 17 18 20 20
7 | 6 11 7 8 8 5 9 4 7 9 2 | 31 33 27 32 28 30 34 28 31 28 29
8 | 6 9 7 9 9 4 10 8 11 11 3 | 22 22 24 21 19 22 22 21 25 23 21
9 | 6 10 7 8 5 5 9 6 6 10 2 | 20 25 18 21 18 20 26 17 17 18 18
10E | 10 10 6 10 10 6 9 9 12 7 3 | 26 26 27 26 28 26 26 27 30 27 26
X11 | 9 22 15 15 15 10 10 9 14 --- 5 | 50 53 45 49 55 46 50 48 83 --- 49
12 | 10 26 9 10 13 6 10 7 8 12 4 | 94 97 94 97 96 94 95 93 96 96 94
13 | 6 13 6 8 7 4 11 9 12 13 3 | 15 26 15 15 15 18 25 15 20 16 15
14 | 10 19 9 15 10 7 12 9 11 11 4 | 56 59 57 66 58 57 59 58 58 60 58
15 | 6 10 6 9 7 4 8 8 6 12 2 | 37 41 38 34 38 37 39 35 36 35 36
16E | 6 23 12 8 13 7 10 12 13 15 4 | 38 43 35 40 41 38 39 44 43 42 39
17 | 8 12 5 14 8 7 8 7 8 9 3 | 27 26 26 32 25 26 25 25 28 28 25
X18 | 10 16 13 11 11 7 11 8 8 --- 4 | 46 50 48 47 50 46 50 49 45 --- 47
19 | 7 16 6 13 8 3 9 7 8 9 3 | 24 24 26 31 24 23 24 23 23 25 23
20E | 7 9 6 7 13 4 8 9 9 16 3 | 16 17 14 18 19 15 15 18 18 23 15
21 | 7 10 6 8 8 5 7 5 8 6 2 | 16 17 16 22 14 16 18 16 17 19 15
X22E | 6 9 8 7 10 5 7 8 13 --- 3 | 38 36 36 36 38 35 36 35 35 --- 36
23E | 12 21 8 24 13 7 11 14 19 16 5 | 35 38 40 50 36 38 39 38 39 40 37
24 | 7 12 5 8 6 2 11 7 10 9 3 | 21 29 20 27 18 22 30 18 21 21 21
25 | 8 15 5 7 11 4 11 9 9 7 3 | 36 36 38 35 36 36 35 34 36 36 35
26 | 6 14 8 8 10 4 9 12 9 12 3 | 24 24 25 25 26 23 25 25 22 28 23
27 | 6 9 7 8 8 3 9 11 11 13 3 | 22 23 23 21 18 21 23 21 24 17 21
X28E | 10 16 7 14 11 8 8 10 11 --- 4 | 64 71 68 70 63 70 67 65 70 --- 66
29 | 10 17 8 6 13 5 8 9 9 12 3 | 27 25 22 25 23 23 25 24 25 25 23
30 | 5 10 4 7 6 5 10 5 6 8 2 | 16 26 17 17 14 17 26 17 17 20 17
31 | 6 10 5 8 5 3 7 7 11 10 2 | 31 37 32 32 34 32 35 34 30 34 32
32 | 6 12 5 8 4 4 8 7 6 8 2 | 28 36 28 26 28 30 34 26 26 24 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 7 10 10 5 9 8 9 11 |T 31 34 31 33 32 31 33 31 33 30 31
WRMS | 7 14 7 9 9 5 9 7 9 11 |NE 27 30 27 28 26 27 30 26 28 25 26
MEDI | 7 12 6 8 9 5 9 8 9 10 |MD 26 26 26 26 26 23 26 25 25 24 23
Table 3.2190.6 GPS week: 2190 Day: 6 MJD: 59580.000
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 9 7 8 9 5 6 5 6 8 2 | 24 24 25 25 23 24 25 20 24 21 22
2 | 5 16 6 15 12 9 9 9 7 6 3 | 21 24 24 30 23 24 23 25 26 27 22
3E | 9 10 7 12 13 5 9 7 11 8 3 | 26 24 24 25 23 24 25 21 25 24 22
4 | 6 12 5 8 10 6 11 6 11 11 3 | 74 74 77 79 77 78 76 75 79 82 76
5E | 10 12 9 14 17 9 12 8 8 12 4 | 32 31 32 37 36 33 30 35 35 38 33
6 | 5 10 8 13 8 5 8 6 8 9 3 | 25 28 26 24 23 25 28 20 27 22 23
7 | 6 10 8 8 6 4 8 6 9 8 2 | 47 47 47 45 43 44 50 45 44 43 45
8 | 6 11 8 12 11 6 11 9 9 11 3 | 34 34 35 36 31 36 30 34 35 35 33
9 | 8 11 10 10 6 5 10 11 9 9 3 | 23 29 23 28 23 23 30 22 22 23 23
10E | 7 15 6 15 10 7 10 9 11 8 3 | 26 28 27 30 30 28 28 24 30 26 26
X11 | 9 17 16 14 18 11 10 9 15 --- 5 | 84 80 70 80 87 80 81 81 81 --- 81
12 | 8 22 9 14 23 7 12 9 7 9 4 | 64 66 61 63 69 61 66 62 65 62 63
13 | 5 12 7 8 5 6 14 10 9 17 3 | 21 30 20 20 22 22 31 19 22 27 21
14 | 9 20 12 18 10 5 14 11 14 9 4 | 68 67 67 75 68 70 70 67 72 71 68
15 | 8 9 8 9 8 4 9 9 8 19 3 | 67 69 64 66 63 63 66 63 68 60 64
16 | 10 22 12 9 28 9 11 13 11 14 5 | 34 38 31 37 34 32 33 37 38 39 33
17 | 7 11 5 10 9 6 7 8 6 11 3 | 36 35 34 39 33 35 34 34 39 38 35
18 | 8 18 14 10 8 8 12 9 10 8 3 | 84 79 79 84 83 80 83 87 84 44 82
19 | 7 19 6 14 10 7 8 9 8 10 3 | 33 33 33 38 30 33 32 31 35 36 32
20E | 7 14 6 9 14 6 10 10 11 12 3 | 29 31 28 32 27 29 29 29 30 33 28
21 | 7 11 6 9 12 5 9 6 9 9 3 | 24 24 23 29 25 24 26 23 26 26 24
X22E | 7 10 9 10 13 8 7 8 8 --- 3 | 50 45 46 42 52 44 46 47 47 --- 46
23E | 10 22 10 24 17 10 13 10 20 16 5 | 41 45 47 51 47 50 47 42 44 48 44
24 | 7 14 6 8 7 5 10 8 8 7 3 | 28 37 29 31 27 30 37 29 29 30 29
25 | 8 12 6 10 13 4 10 10 8 11 3 | 42 42 43 43 43 42 41 40 40 42 41
26 | 13 16 10 10 11 6 10 14 7 10 4 | 30 32 31 29 31 29 27 29 27 30 28
27 | 7 10 9 7 11 4 11 10 10 13 3 | 30 29 32 35 29 32 29 31 33 18 30
X28 | 6 13 7 12 15 8 14 12 12 --- 4 | 52 53 50 49 52 53 54 49 54 --- 51
29 | 9 23 7 8 13 4 9 9 6 11 3 | 36 40 34 35 33 34 37 33 34 34 34
30 | 5 9 6 9 7 3 8 7 6 8 2 | 18 29 21 19 18 21 27 19 23 21 20
31 | 7 10 6 8 6 5 9 7 7 7 2 | 45 50 46 43 45 44 52 47 48 45 46
32 | 6 10 7 7 7 4 10 7 6 9 2 | 30 38 33 32 30 33 37 28 32 28 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 8 11 12 6 10 9 9 11 |T 39 41 39 41 40 40 41 39 41 37 39
WRMS | 7 14 8 12 11 6 10 8 9 9 |NE 38 41 38 40 38 38 41 37 39 34 38
MEDI | 7 12 7 10 10 6 10 9 8 9 |MD 33 35 33 36 31 33 33 33 35 34 33
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 4.2190 GPS week: 2190 MJD: 59574.0-59580.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 10 14 25 |U 10 13 44 |U 15 13 30 |
emr | emr 3071 |U 20 17 50 |U 14 25 62 |U 14 22 45 |
esa | esa 3044 | 14 18 41 | 11 14 60 | 17 15 49 |
gfz | gfz 3062 |U 8 13 26 |U 10 11 46 |U 13 10 29 |
grg | grg 3069 |U 9 11 32 |U 10 12 48 |U 10 10 30 |
igr | igr 3061 | 10 13 27 | 10 12 48 | 13 10 31 |
igs | igs 3071 | 10 12 29 | 10 12 46 | 12 11 31 |
jpl | jpl 3072 | 17 18 43 |U 13 16 62 | 15 16 52 |
mit | mit 3072 |U 9 9 25 |U 9 11 41 |U 11 10 24 |
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 5.2190.0 GPS week: 2190 Day: 0 MJD: 59574.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 11 21 | 9 10 37 | 14 15 29 |
emr | emr 3072 | 25 13 56 | 16 24 64 | 12 20 42 |
esa | esa 3072 | 17 17 40 | 11 11 53 | 16 13 53 |
gfz | gfz 3072 | 9 10 18 | 9 9 41 | 11 10 26 |
grg | grg 3071 | 10 10 27 | 10 11 49 | 9 7 29 |
igr | igr 3072 | 12 11 28 | 10 10 43 | 13 11 30 |
igs | igs 3072 | 12 10 28 | 9 10 41 | 13 12 32 |
jpl | jpl 3072 | 20 19 47 | 12 15 55 | 16 19 52 |
mit | mit 3072 | 10 8 29 | 9 10 36 | 12 13 23 |
Table 5.2190.1 GPS week: 2190 Day: 1 MJD: 59575.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 14 27 | 13 17 51 | 17 16 25 |
emr | emr 3072 | 21 19 49 | 16 29 63 | 13 23 42 |
esa | esa 3072 | 17 22 43 | 16 15 68 | 18 15 49 |
gfz | gfz 3072 | 9 14 23 | 13 15 47 | 13 12 27 |
grg | grg 3068 | 12 12 35 | 13 13 49 | 9 9 27 |
igr | igr 3072 | 12 16 26 | 13 15 53 | 14 11 28 |
igs | igs 3072 | 12 14 31 | 13 15 52 | 13 12 28 |
jpl | jpl 3072 | 18 24 46 | 17 18 72 | 15 17 50 |
mit | mit 3072 | 10 10 28 | 13 14 47 | 12 12 19 |
Table 5.2190.2 GPS week: 2190 Day: 2 MJD: 59576.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 17 30 | 13 12 49 | 13 13 28 |
emr | emr 3071 | 23 19 54 | 14 20 69 | 15 23 49 |
esa | esa 2976 | 16 22 42 | 14 11 67 | 15 16 48 |
gfz | gfz 3058 | 9 15 26 | 13 11 53 | 11 12 27 |
grg | grg 3064 | 13 14 44 | 14 12 49 | 10 13 28 |
igr | igr 3058 | 11 15 29 | 13 11 56 | 11 10 30 |
igs | igs 3071 | 11 15 32 | 13 10 53 | 11 13 31 |
jpl | jpl 3072 | 20 19 43 | 15 16 72 | 15 17 53 |
mit | mit 3072 | ---- ---- ---- | 13 11 48 | ---- ---- ---- |
Table 5.2190.3 GPS week: 2190 Day: 3 MJD: 59577.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 16 29 | 6 7 39 | 18 16 36 |
emr | emr 3072 | 15 18 48 | 10 20 56 | 17 29 50 |
esa | esa 2976 | 12 20 40 | 8 14 56 | 18 17 47 |
gfz | gfz 3025 | 7 13 27 | 6 7 39 | 13 13 32 |
grg | grg 3072 | 7 14 31 | 8 9 38 | 9 7 30 |
igr | igr 3015 | 8 14 28 | 7 9 40 | 14 13 32 |
igs | igs 3072 | 8 14 29 | 7 8 40 | 14 15 34 |
jpl | jpl 3072 | 15 21 43 | 11 15 60 | 18 23 54 |
mit | mit 3072 | 8 12 26 | 6 8 35 | 13 13 28 |
Table 5.2190.4 GPS week: 2190 Day: 4 MJD: 59578.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 16 21 | 7 17 42 | 17 11 35 |
emr | emr 3072 | 20 13 44 | 11 27 57 | 14 23 46 |
esa | esa 3072 | 13 18 38 | 9 15 55 | 17 13 49 |
gfz | gfz 3065 | 6 11 21 | 9 14 49 | 13 9 31 |
grg | grg 3070 | 8 9 26 | 8 14 49 | 9 11 27 |
igr | igr 3072 | 9 12 21 | 7 14 44 | 13 7 33 |
igs | igs 3072 | 9 11 23 | 7 15 45 | 13 8 32 |
jpl | jpl 3072 | 16 16 35 | 10 17 66 | 14 13 54 |
mit | mit 3072 | 7 8 17 | 7 13 44 | 11 7 25 |
Table 5.2190.5 GPS week: 2190 Day: 5 MJD: 59579.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 14 23 | 9 14 49 | 12 8 30 |
emr | emr 3072 | 18 18 51 | 13 31 69 | 15 20 43 |
esa | esa 3072 | 14 17 42 | 10 15 66 | 19 16 45 |
gfz | gfz 3072 | 8 11 35 | 9 9 54 | 10 7 27 |
grg | grg 3071 | 8 9 28 | 8 9 44 | 13 12 27 |
igr | igr 3072 | 12 14 27 | 9 12 55 | 12 8 32 |
igs | igs 3072 | 10 11 27 | 8 12 51 | 12 7 28 |
jpl | jpl 3072 | 19 15 42 | 11 17 64 | 15 11 50 |
mit | mit 3072 | 9 9 24 | 7 10 42 | 11 6 20 |
Table 5.2190.6 GPS week: 2190 Day: 6 MJD: 59580.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 12 26 | 10 14 38 | 14 12 28 |
emr | emr 3072 | 18 16 48 | 17 25 54 | 15 21 42 |
esa | esa 3072 | 10 14 42 | 10 17 55 | 18 14 50 |
gfz | gfz 3072 | 9 18 35 | 8 13 39 | 17 12 31 |
grg | grg 3072 | 6 12 34 | 12 18 59 | 12 13 44 |
igr | igr 3072 | 9 11 29 | 9 14 42 | 14 11 35 |
igs | igs 3072 | 7 10 30 | 9 13 39 | 12 11 32 |
jpl | jpl 3072 | 14 13 42 | 12 16 46 | 16 13 48 |
mit | mit 3072 | 7 10 24 | 9 12 37 | 11 12 29 |
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 6.2190 GPS week: 2190 MJD: 59574.500-59580.500
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 | 3 0 -45 -6 -1 | 3 20
| 19 11 46 57 1 | 1
emr uuuuu | 9 -26 24 64 -12 | 25 32
| 24 17 138 124 9 | 4
esa uuuuu | -8 9 48 -78 1 | 13 22
| 8 14 45 65 3 | 1
gfz uuuuu | -8 0 7 8 -1 | 23 30
| 8 19 136 82 4 | 1
grg uuuuu | -6 10 -72 35 3 | 6 18
| 19 16 32 80 6 | 2
igr xxxxx | -10 -5 -22 -32 5 | -3 22
| 7 7 62 49 5 | 2
irf xxxxx | 2 3 27 54 -1 | 2 17
| 8 11 33 21 3 | 1
jpl uuuuu | 4 16 -38 33 -1 | 9 23
| 15 18 62 51 13 | 4
mit uuuuu | 29 -26 65 115 2 | 23 29
| 23 21 53 51 6 | 1
ngs uuxuu | -29 8 -112 -128 2 | 9 21
| 40 31 229 169 3 | 1
sio xxxxx | 80 -90 119 130 -6 | 53 56
| 55 15 95 79 9 | 1
Table 7.2190.0 GPS week: 2190 Day: 0 MJD: 59574.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 15 -59 -11 -2 | 4 20
emr uuuuu | -9 -23 25 -26 -7 | 30 36
esa uuuuu | -13 -10 105 -122 -2 | 13 22
gfz uuuuu | -9 24 37 -82 3 | 23 29
grg uuuuu | 3 21 -37 125 11 | 2 17
igr xxxxx | -14 -15 23 -57 7 | -6 23
irf xxxxx | -8 13 25 54 -3 | 2 16
jpl uuuuu | -7 13 -136 -3 -20 | 14 25
mit uuuuu | 30 -29 39 182 -3 | 23 28
ngs uuxuu | -18 -16 -131 -54 5 | 7 21
sio xxxxx | 65 -90 162 152 -5 | 53 55
Table 7.2190.1 GPS week: 2190 Day: 1 MJD: 59575.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 2 -1 -102 -28 -1 | 4 21
emr uuuuu | -32 -19 162 -113 -14 | 29 34
esa uuuuu | -3 8 110 -114 2 | 14 23
gfz uuuuu | -15 -15 68 -46 -5 | 25 31
grg uuuuu | 8 6 -95 84 12 | 5 20
igr xxxxx | -7 -9 -131 30 5 | -4 23
irf xxxxx | -6 11 -29 22 -4 | 4 17
jpl uuuuu | -25 24 -36 -43 -12 | 14 25
mit uuuuu | 11 -19 -22 106 -5 | 24 30
ngs uuxuu | 39 10 -351 166 5 | 9 23
sio xxxxx | 81 -98 217 87 1 | 55 58
Table 7.2190.2 GPS week: 2190 Day: 2 MJD: 59576.500
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 10 36 8 0 | 4 21
emr uuuuu | 4 -36 81 -12 -5 | 26 34
esa uuuuu | -20 7 48 -142 7 | 14 23
gfz uuuuu | -15 24 -195 -4 6 | 24 31
grg uuuuu | -9 18 -113 132 -1 | 7 18
igr xxxxx | -12 -1 -54 33 11 | -3 22
irf xxxxx | -1 1 -7 73 -3 | 3 18
jpl uuuuu | 6 -8 35 10 -12 | 11 26
mit uuuuu | 6 -11 44 138 0 | 24 30
ngs uuxuu | 6 -14 107 -53 4 | 10 22
sio xxxxx | 125 -73 62 286 -22 | 56 58
Table 7.2190.3 GPS week: 2190 Day: 3 MJD: 59577.500
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 | -28 -4 -76 74 -2 | 1 19
emr uuuuu | 27 -36 168 48 -3 | 24 31
esa uuuuu | -12 31 17 -138 1 | 12 21
gfz uuuuu | -8 13 -122 -6 -3 | 23 30
grg uuuuu | -8 26 -28 -50 -5 | 6 18
igr xxxxx | -9 -12 60 -71 9 | -4 22
irf xxxxx | 13 12 39 71 -2 | 1 17
jpl uuuuu | 18 27 45 38 9 | 6 21
mit uuuuu | 65 -39 59 168 0 | 22 28
ngs uuxuu | -59 -36 172 -150 2 | 8 21
sio xxxxx | 84 -81 108 123 -2 | 53 56
Table 7.2190.4 GPS week: 2190 Day: 4 MJD: 59578.500
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 | 26 -8 -66 -112 0 | 1 19
emr uuuuu | 15 -23 46 232 -25 | 22 29
esa uuuuu | -10 15 51 -21 2 | 12 21
gfz uuuuu | -10 -8 -41 176 -2 | 22 29
grg uuuuu | 16 18 -58 19 4 | 5 17
igr xxxxx | -23 -1 -10 -84 5 | -3 22
irf xxxxx | -1 6 59 74 -1 | 1 17
jpl uuuuu | 16 37 -53 41 8 | 6 21
mit uuuuu | 3 -66 137 98 0 | 22 28
ngs uuxuu | -65 35 31 -307 -2 | 8 20
sio xxxxx | 113 -103 127 28 -15 | 53 56
Table 7.2190.5 GPS week: 2190 Day: 5 MJD: 59579.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -16 7 -14 31 -1 | 3 19
emr uuuuu | 15 -47 -113 141 -7 | 21 29
esa uuuuu | -3 -7 -2 5 -2 | 13 22
gfz uuuuu | 8 -22 105 -3 -4 | 23 30
grg uuuuu | -6 2 -94 -3 -1 | 7 18
igr xxxxx | -5 -6 -44 -65 -1 | 0 21
irf xxxxx | 12 -17 57 58 1 | 3 17
jpl uuuuu | 12 24 -60 105 7 | 6 21
mit uuuuu | 40 -5 109 81 7 | 23 29
ngs uuxuu | -46 33 -180 -326 0 | 9 21
sio xxxxx | 122 -109 -57 107 -2 | 53 56
Table 7.2190.6 GPS week: 2190 Day: 6 MJD: 59580.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 7 -16 -32 -1 -4 | 3 19
emr uuuuu | 42 5 -203 176 -23 | 20 29
esa uuuuu | 3 17 6 -11 -2 | 14 22
gfz uuuuu | -8 -13 199 24 2 | 24 30
grg uuuuu | -45 -22 -76 -63 2 | 8 18
igr xxxxx | -4 6 4 -12 -4 | 1 21
irf xxxxx | 5 -2 42 29 5 | 3 17
jpl uuuuu | 9 -8 -61 86 9 | 6 21
mit uuuuu | 46 -15 92 36 13 | 24 30
ngs uuxuu | -59 43 -434 -171 0 | 11 21
sio xxxxx | -33 -73 211 129 2 | 52 55
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