[IGSREPORT-28026] Wk 2162 IGS Final Orbits
acc
acc at igs.org
Fri Jul 2 11:46:24 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2162 (Jun 13, 2021 - Jun 19, 2021)
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:
igs2162[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2162[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2162[0-6].cls IGS GPS clock combination summary report.
igs21627.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21627.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 | 26 26 TIXI TIXI
0 | EMR | 26 HOB2
0 | ESA | PTBB YEL2 PTBB YEL2
0 | GRG | CCJ2 CCJ2 LHAZ
0 | JPL | CZTG
1 | COD | LHAZ MDVJ NICO THU2 TIXI LHAZ NICO TIXI
1 | EMR | MDVJ
1 | ESA | PTBB LHAZ PTBB
1 | GRG | JFNG
1 | JPL | NYAL NYAL THU2
2 | COD | GLSV JFNG LHAZ NYAL TIXI ZECK GLSV JFNG TIXI
2 | EMR | ZECK
2 | ESA | ARTU CZTG LHAZ MAS1 PTBB ARTU MAS1 PTBB
2 | GRG | 10 25 10 25 SVTL SVTL
2 | JPL | FAIR MCM4 NYAL YEL2 ZECK
3 | COD | JFNG MDVJ PARC SYOG TIXI ZECK JFNG TIXI
3 | EMR | DRAO MDVJ
3 | ESA | PTBB SGOC PTBB
3 | GFZ | FLRS FLRS
3 | GRG | 10 13 10 13 FAIR SVTL FAIR MAS1 SVTL
3 | JPL | BAKE FAIR BAKE FAIR MCM4 PARC SCOR ZECK
3 | MIT | SYDN SYDN
4 | COD | FAIR IRKJ MCM4 NLIB SCUB THU2 TIXI TIXI
4 | EMR | 14 14
4 | ESA | CPVG CZTG PTBB CPVG CZTG MCIL PTBB
4 | GRG | CPVG HOB2 IRKJ STK2 CPVG
4 | JPL | SVTL CHUR FAIR MCM4 SVTL
5 | COD | 14 14 DAV1 TIXI WIND YELL TIXI WIND YELL
5 | EMR | CHUR FAIR SFER ZECK
5 | ESA | CPVG SCOR SCOR
5 | GFZ | FLRS FLRS
5 | GRG | CPVG SVTL SVTL
5 | JPL | CHUR DAV1
6 | COD | DAV1 LHAZ MDVJ SCUB STK2 TIXI YAKT LHAZ TIXI
6 | EMR | MDVJ YAKT
6 | ESA | DAV1 PTBB ULAB PTBB ULAB
6 | GRG | LHAZ LHAZ
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
----+--------+---------------
1 | GFZ | 26
2 | GFZ | 26
3 | GFZ | 26
4 | GFZ | 26
5 | GFZ | 26
6 | GFZ | 14 26
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G25 | 4 | 4 | | | | | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
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.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .2 -.2 .5 3 -2 9 -.33
EMR | 0 | .2 .1 -.4 -21 -6 7 -.15
ESA | 0 | -.2 -1.1 -.9 -40 -3 21 -.34
GFZ | 0 | -.1 .0 .4 10 -9 12 -.26
GRG | 0 | 5.1 -7.1 6.1 14 -12 -6 -.22
JPL | 0 | 7.7 -10.3 1.8 1 -11 21 -.17
MIT | 0 | 4.4 -6.1 1.3 -7 -19 15 .18
NGS | 0 | 8.0 -2.6 7.2 -28 -54 9 .01
SIO | 0 | .2 -.8 2.1 -5 -10 16 -.04
COD | 1 | .2 -.1 .4 4 -2 8 -.28
EMR | 1 | .5 -5.9 1.2 -23 -1 16 -.26
ESA | 1 | -.2 -.9 -.9 -16 17 24 -.34
GFZ | 1 | -.0 -.4 .5 24 1 31 -.27
GRG | 1 | 5.2 -8.2 7.8 6 1 -9 -.18
JPL | 1 | 7.4 -11.6 6.3 2 6 -21 -.19
MIT | 1 | 3.6 -5.7 .9 -8 -4 24 .07
NGS | 1 | 3.5 -7.8 8.0 -16 -39 -9 -.11
SIO | 1 | -1.9 -3.5 2.7 -46 22 16 -.09
COD | 2 | .2 -.0 .5 5 2 6 -.29
EMR | 2 | .3 -7.3 -5.4 -33 -2 15 .07
ESA | 2 | -.3 -.8 -.6 -15 11 36 -.29
GFZ | 2 | -.2 -.1 .5 15 1 16 -.21
GRG | 2 | 6.0 -8.1 1.5 9 -6 3 -.07
JPL | 2 | -.2 -14.0 -3.9 7 13 7 -.20
MIT | 2 | 1.3 -5.3 1.7 -12 -6 13 .12
NGS | 2 | 4.9 -4.9 9.4 -14 -34 3 -.05
SIO | 2 | -5.2 .0 -1.7 13 91 39 -.08
COD | 3 | .4 -.1 .6 8 -2 6 -.32
EMR | 3 | -5.7 -1.4 -5.6 -41 -8 26 .03
ESA | 3 | -.6 -1.0 -.7 -29 7 21 -.36
GFZ | 3 | -.1 .0 .4 19 4 12 -.29
GRG | 3 | 3.7 -5.4 -1.3 14 1 -9 -.14
JPL | 3 | 3.8 -11.5 -2.6 7 -4 -9 -.07
MIT | 3 | -.1 -1.7 .7 -6 -12 14 -.01
NGS | 3 | 2.4 -3.5 4.7 -17 -26 14 -.10
SIO | 3 | -3.1 -1.6 .8 -11 44 59 -.19
COD | 4 | .3 .1 .6 4 -2 3 -.32
EMR | 4 | -2.1 -3.5 .3 -41 -12 9 -.01
ESA | 4 | -.2 -.7 -.3 -34 16 14 -.20
GFZ | 4 | -.1 .1 .4 11 2 13 -.19
GRG | 4 | 1.2 -8.2 2.8 26 -3 -5 -.11
JPL | 4 | -.2 -10.8 1.7 0 -2 -11 -.17
MIT | 4 | 2.6 -5.7 2.8 4 -7 8 .12
NGS | 4 | 1.7 -6.2 10.1 -29 -38 2 -.02
SIO | 4 | -1.8 -2.3 -2.4 -27 36 49 -.16
COD | 5 | .3 .0 .5 4 -1 2 -.31
EMR | 5 | -1.9 -11.3 -.1 -29 10 15 -.18
ESA | 5 | -.9 -.5 -1.2 -29 17 19 -.41
GFZ | 5 | -.1 .0 .7 10 -5 21 -.42
GRG | 5 | 4.8 -2.3 -7.7 26 -10 -8 -.35
JPL | 5 | 1.2 -6.2 -.9 -3 7 0 -.29
MIT | 5 | 3.7 -4.2 -1.1 1 -8 5 -.04
NGS | 5 | 4.8 -3.4 8.6 -7 -32 -2 -.17
SIO | 5 | -.7 -1.5 -3.1 -18 18 52 -.30
COD | 6 | .4 -.1 .6 2 -4 5 -.34
EMR | 6 | 6.9 .7 -6.3 -26 3 16 -.14
ESA | 6 | -.3 -1.1 -1.5 -29 9 26 -.38
GFZ | 6 | .0 .0 .2 11 -7 13 -.27
GRG | 6 | .9 -2.2 -6.3 22 -1 -10 -.27
JPL | 6 | 2.8 -6.0 .7 7 -5 0 -.15
MIT | 6 | 3.5 -6.3 -5.2 1 2 17 -.09
NGS | 6 | 5.0 -2.0 4.7 -20 -36 14 -.14
SIO | 6 | 1.4 -6.6 -5.2 -108 -25 29 -.46
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
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 1.2162.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2162.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 2.2162.[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 3.2162.[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 5.2162.0-6). 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 2162 summary. (Jun 13, 2021 - Jun 19, 2021)
Table 1.2162.a GPS week: 2162 MJD: 59378.000-59384.000
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 738| 0 0 0 -3 7 -1 -.01 8 7 | -676 -27 6 91
| 0 0 0 15 12 12 .02 | 93 199
emr 80| -3 1 -2 2 -9 18 .07 13 13 | 177761 -332 15 136
| 0 1 1 14 16 6 .04 | 639 755
esa 150| 0 0 0 0 -1 1 -.00 9 8 | -957 406 7 82
| 0 0 1 16 15 7 .02 | 314 667
gfz 233| 0 0 4 17 -5 -13 .04 17 11 | 206 -239 265 392
| 0 0 2 24 16 18 .04 | 185 495
grg 120| 4 0 1 21 4 -26 -.09 11 10 | 106 -198 8 134
| 0 0 3 7 17 9 .01 | 247 469
igr n/a| 0 0 -1 9 -5 -13 .00 4 4 | -10811 -498 11 79
| 0 0 1 11 18 4 .01 | 698 1038
jpl 80| -1 0 -2 0 -9 0 .14 10 10 | 1426 -180 7 72
| 1 1 1 14 18 13 .01 | 822 934
mit 355| 0 0 0 0 -7 18 -.01 6 6 | -11894 -422 25 1569
| 0 0 0 20 30 15 .02 | 703 1045
ngs 205| 0 0 4 -1 12 -33 -.05 9 9 | -668 -50 812 1666
| 0 0 1 11 14 13 .02 | 119 238
sio 438| 0 0 -1 -16 0 26 -.02 9 8 | --- --- --- ---
| 0 0 1 40 32 22 .02 | --- ---
Table 1.2162.b GPS week : 2162 MJD: 59378.000-59384.000
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 | 3 3 3 3 3 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 4 4 3 4 4 4 4 |
5 | 3 3 3 3 3 3 3 |
6 | 3 3 4 3 3 3 3 |
7 | 3 3 3 2 3 3 3 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
12 | 4 4 4 3 4 4 4 |
13 | 3 3 3 3 2 3 3 |
14 | 5 5 5 5 7 10 7 |
15 | 3 3 3 3 3 3 3 |
16 | 4 4 4 4 4 4 4 |
17 | 3 3 3 3 3 3 3 |
18 | 5 5 5 5 5 6 5 |
19 | 3 3 3 3 3 3 3 |
20 | 3 3 3 3 3 3 3 |
21 | 3 3 3 3 3 4 3 |
22 | 3 3 3 3 3 3 3 |
23 | 4 4 4 4 4 4 4 |
24 | 3 3 3 3 3 3 2 |
25 | 6 6 6 6 5 5 4 |
26 | 7 5 4 4 4 4 4 |
27 | 3 3 3 3 3 3 3 |
28 | 4 3 4 4 4 4 4 |
29 | 3 3 3 3 3 3 3 |
30 | 3 2 2 2 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 4 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 2.2162.0 GPS week: 2162 Day: 0 MJD: 59378.000
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 738| 0 0 0 -21 32 8 -.03 7 7 | -852 359 6 96
emr 81| -3 4 0 -10 5 10 .01 13 13 | 176791 -121 17 171
esa 150| 0 0 -1 -17 18 -3 .02 8 8 | -1203 209 6 71
gfz 233| 0 0 4 -5 6 -28 .10 11 9 | 56 -287 248 369
grg 122| 3 0 2 18 22 -28 -.10 13 11 | -164 23 7 129
igr n/a| 0 0 -1 0 15 -3 .01 4 4 | -11524 259 12 77
jpl 80| 1 -1 -2 -5 12 -20 .14 10 10 | 345 243 8 72
mit 355| 0 0 -2 37 -44 45 -.02 7 7 | -11738 551 24 1643
ngs 206| 0 0 2 -17 2 -28 -.08 9 9 | -847 342 686 1778
sio 444| 0 0 0 22 -37 23 -.02 9 8 | --- --- --- ---
Table 2.2162.1 GPS week: 2162 Day: 1 MJD: 59379.000
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 743| 0 0 -2 -25 1 8 -.01 7 7 | -599 -53 7 93
emr 81| -3 0 -3 27 1 28 .08 13 13 | 177050 251 17 161
esa 150| 0 0 -2 26 9 4 .02 8 8 | -848 34 7 85
gfz 235| 0 2 3 20 11 15 -.00 13 9 | 75 27 251 369
grg 120| 4 0 3 25 14 -30 -.09 11 9 | -3 -156 8 121
igr n/a| 0 0 -3 17 5 -9 .01 4 4 | -11112 331 12 84
jpl 80| 0 1 -1 26 4 0 .12 9 9 | 643 472 9 76
mit 355| 0 -1 -1 -10 0 -1 -.01 6 6 | -11526 56 23 1484
ngs 205| 1 0 3 7 2 -16 -.00 9 9 | -721 100 688 1615
sio 442| 0 0 0 -45 -42 -9 -.04 8 7 | --- --- --- ---
Table 2.2162.2 GPS week: 2162 Day: 2 MJD: 59380.000
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 742| 0 0 0 3 3 5 -.01 7 7 | -611 -18 6 93
emr 79| -3 2 -4 -8 -27 22 .12 13 13 | 177707 453 17 151
esa 150| 0 0 0 6 -5 12 -.03 8 8 | -1189 1130 7 90
gfz 232| 2 0 4 -5 -15 -30 .01 18 14 | 181 -47 265 422
grg 118| 3 0 2 9 -7 -20 -.09 10 9 | -68 108 8 117
igr n/a| 0 0 -3 7 -2 -17 -.01 4 4 | -10498 309 12 73
jpl 80| 0 0 -2 0 -7 -12 .13 9 9 | 1227 817 9 80
mit 355| 0 0 0 -4 -3 4 .02 6 6 | -11394 335 22 1469
ngs 203| 0 0 3 -9 25 -27 -.04 9 9 | -614 -29 715 1450
sio 441| 0 0 0 17 15 40 -.03 8 7 | --- --- --- ---
Table 2.2162.3 GPS week: 2162 Day: 3 MJD: 59381.000
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 736| 0 0 -1 13 -7 -18 -.02 7 7 | -590 -187 6 88
emr 80| -5 1 -2 0 -17 21 .08 13 13 | 178212 234 15 129
esa 150| 0 0 0 7 5 3 .01 8 8 | -1090 964 7 85
gfz 229| 0 0 7 36 -4 -29 .06 22 11 | 221 179 284 406
grg 121| 4 0 2 24 11 -41 -.12 10 9 | 66 218 8 144
igr n/a| 0 0 -1 16 -6 -13 -.00 4 4 | -10118 165 12 85
jpl 80| -1 -1 -3 -9 5 16 .15 9 9 | 2103 609 7 74
mit 355| 0 0 0 -24 -5 16 -.02 6 5 | -11331 54 25 1101
ngs 210| 0 0 2 8 14 -37 -.07 9 8 | -600 -122 866 1607
sio 431| 0 0 -2 -31 5 63 -.02 9 8 | --- --- --- ---
Table 2.2162.4 GPS week: 2162 Day: 4 MJD: 59382.000
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 733| 0 0 -1 5 10 6 -.00 9 6 | -718 69 6 87
emr 80| -4 1 -2 2 -29 13 .10 13 13 | 178572 -1166 13 97
esa 150| -1 0 0 -4 -20 3 -.01 10 9 | -486 -235 7 83
gfz 234| 0 0 7 44 -32 -18 .01 22 10 | 442 -989 277 390
grg 120| 4 0 5 33 -25 -12 -.10 12 11 | 295 -649 10 145
igr n/a| 0 0 -1 20 -40 -17 .00 4 4 | -9730 -2115 11 84
jpl 80| -2 -1 -1 -7 -36 12 .12 10 10 | 2743 -1552 8 65
mit 355| 0 0 -1 -2 14 15 -.02 5 5 | -11462 -2068 29 1962
ngs 205| 2 1 5 -1 1 -50 -.05 9 9 | -611 -124 877 1633
sio 434| 1 0 -3 -38 51 20 .01 8 7 | --- --- --- ---
Table 2.2162.5 GPS week: 2162 Day: 5 MJD: 59383.000
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 736| -1 0 0 -10 7 -20 -.02 9 7 | -716 -240 6 93
emr 80| -4 -2 0 -6 10 18 .08 13 13 | 177867 -468 16 119
esa 150| 0 0 1 -20 1 -10 .01 10 8 | -1279 1163 8 81
gfz 232| 0 0 2 -8 10 4 .09 12 11 | 0 277 273 400
grg 121| 4 0 -3 15 19 -32 -.08 12 11 | 53 108 9 149
igr n/a| 0 0 -1 -10 4 -15 .01 5 4 | -11379 -739 12 80
jpl 80| -2 2 -2 -15 -12 3 .15 11 11 | 1606 -823 7 72
mit 355| 0 0 0 12 -46 27 -.04 7 7 | -12979 -128 25 1501
ngs 202| 1 0 6 -13 37 -50 -.07 12 10 | -781 -76 723 1868
sio 433| 1 0 -2 34 0 35 -.06 9 9 | --- --- --- ---
Table 2.2162.6 GPS week: 2162 Day: 6 MJD: 59384.000
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 742| -1 1 0 7 7 -4 .03 7 7 | -648 -120 6 93
emr 80| -2 1 -1 15 -10 14 .01 13 13 | 178128 -1510 12 126
esa 150| -1 0 0 7 -23 -1 -.03 8 8 | -606 -418 7 81
gfz 237| 0 0 1 43 -13 -6 .04 19 14 | 467 -839 262 392
grg 122| 4 0 -1 22 -6 -23 -.08 10 9 | 568 -1038 8 139
igr n/a| 0 0 0 12 -16 -15 .02 4 4 | -11319 -1701 11 74
jpl 80| -1 0 0 14 -31 -4 .14 9 9 | 1321 -1030 6 66
mit 355| 0 0 0 -13 37 23 -.02 7 6 | -12831 -1759 28 1825
ngs 207| 1 0 3 12 2 -20 -.04 9 8 | -504 -442 1131 1717
sio 441| 1 0 -1 -73 13 15 -.03 9 8 | --- --- --- ---
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 3.2162.0 GPS week: 2162 Day: 0 MJD: 59378.000
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 12 7 10 19 3 9 6 8 7 3 | 23 23 25 22 29 22 24 20 21 19 21
2 | 6 13 11 10 9 5 10 7 6 7 3 | 32 29 32 34 33 30 29 32 32 31 31
3 | 6 9 7 8 9 4 6 7 7 6 2 | 21 24 23 24 24 22 23 21 20 20 21
4 | 6 18 6 10 8 3 20 6 6 6 3 | 57 57 54 57 58 55 55 55 58 58 55
5 | 5 9 6 9 9 3 7 7 9 6 2 | 24 25 23 24 25 25 26 26 24 25 24
6 | 7 16 7 9 13 4 10 6 9 9 3 | 27 29 28 25 29 26 32 26 25 24 26
7 | 7 10 8 9 9 4 7 6 7 6 2 | 48 49 47 48 48 46 48 51 47 49 48
8 | 4 9 6 9 9 2 8 4 6 7 2 | 21 22 24 24 23 21 22 21 22 20 21
9 | 8 13 6 8 9 4 12 6 8 10 3 | 27 34 28 30 23 26 33 24 29 28 27
10 | 6 8 7 13 14 3 8 8 6 7 3 | 25 28 27 27 25 25 24 27 27 25 25
12E | 7 18 13 10 11 5 7 7 12 7 3 | 43 41 48 45 40 43 46 43 43 43 43
13 | 7 6 9 8 9 2 8 4 9 9 2 | 17 20 25 25 16 19 21 20 18 20 19
14E | 11 16 13 23 19 4 10 8 17 18 5 | 128 133 132 131 135 131 129 133 133 132 131
15 | 8 7 7 7 9 4 7 8 9 9 2 | 50 49 47 47 43 47 50 47 43 44 46
16E | 6 27 12 9 12 4 10 4 10 10 4 | 29 33 28 29 29 26 28 26 26 27 27
17 | 4 10 8 6 9 5 8 5 8 10 2 | 28 27 28 30 28 26 28 29 26 31 28
X18 | 13 20 9 16 10 8 13 12 13 --- 5 | 60 62 59 56 57 58 60 55 58 --- 57
19 | 6 16 7 7 10 5 10 4 8 8 3 | 25 28 30 31 26 28 29 27 26 27 27
20 | 6 9 5 9 10 3 6 9 11 8 3 | 21 21 19 19 21 19 20 20 19 19 18
21 | 8 11 8 10 17 5 7 6 8 6 3 | 30 25 28 34 35 26 27 26 26 29 27
22 | 7 10 8 9 15 4 8 10 9 6 3 | 21 21 20 24 25 20 20 22 21 20 20
23 | 8 14 13 12 16 6 9 8 12 8 3 | 87 83 80 89 88 84 83 88 91 88 86
24 | 8 9 8 8 9 4 6 7 9 6 2 | 27 28 27 29 22 26 30 28 22 27 26
25E | 12 12 11 20 29 8 12 13 15 14 5 | 178 173 181 180 182 179 141 179 170 185 179
X26E | 16 16 10 29 29 13 --- 6 18 10 6 | 49 50 45 69 56 45 --- 48 44 45 47
27 | 4 10 7 8 10 3 10 6 9 8 2 | 20 21 23 22 21 20 21 21 22 21 20
28E | 10 15 7 12 12 4 11 7 9 15 3 | 29 29 29 31 31 28 30 29 29 27 28
29 | 6 16 6 9 10 4 8 4 11 7 3 | 27 25 23 28 28 25 26 27 29 28 26
30 | 5 9 8 8 8 2 8 5 7 5 2 | 24 23 22 19 23 23 24 24 22 23 22
31 | 8 13 9 8 12 4 8 5 10 12 3 | 49 50 47 48 47 47 50 48 43 44 47
32 | 5 14 5 17 6 4 14 7 6 8 3 | 25 35 29 27 24 26 34 29 29 28 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 11 13 4 10 7 9 9 |T 41 41 41 42 41 40 40 41 40 40 40
WRMS | 7 13 8 9 11 4 10 7 9 8 |NE 32 33 32 33 32 31 33 32 32 31 31
MEDI | 7 12 8 9 10 4 8 6 9 8 |MD 27 29 28 30 29 26 29 27 27 27 27
Table 3.2162.1 GPS week: 2162 Day: 1 MJD: 59379.000
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 14 3 10 7 9 7 3 | 26 28 28 26 28 26 28 22 28 23 25
2 | 6 12 10 10 10 5 9 6 10 7 3 | 33 31 32 36 32 32 33 34 36 34 32
3 | 5 9 7 10 7 3 5 6 7 7 2 | 28 29 27 28 28 26 29 22 27 24 26
4 | 5 18 5 9 6 4 19 6 7 6 3 | 36 35 34 37 36 34 37 35 35 33 34
5 | 6 10 6 6 9 3 8 6 8 7 2 | 26 27 24 26 28 26 27 24 27 27 25
6 | 9 19 5 7 13 3 10 7 9 6 3 | 29 31 30 31 28 29 32 28 31 27 28
7 | 6 13 6 6 8 4 7 4 7 6 2 | 35 39 34 35 33 35 37 35 37 36 35
8 | 6 10 6 7 9 2 7 5 7 8 2 | 25 27 26 25 25 24 26 23 27 24 24
9 | 6 15 4 7 7 4 12 4 9 6 2 | 22 34 25 24 21 24 34 21 28 21 24
10 | 6 9 10 10 12 4 9 7 7 9 3 | 30 30 32 27 31 28 29 29 27 31 28
12E | 6 20 13 10 10 4 9 5 9 9 3 | 24 27 25 20 22 23 24 25 24 24 23
13 | 5 7 8 10 6 3 7 5 7 8 2 | 24 26 28 25 22 25 28 25 28 26 25
14E | 8 15 10 20 17 6 10 10 18 12 4 | 104 106 106 104 106 103 105 102 108 102 104
15 | 6 9 6 6 7 4 5 8 9 8 2 | 35 33 33 33 31 33 34 35 33 34 33
16E | 8 20 14 10 13 4 11 6 9 7 3 | 28 26 22 27 28 24 24 27 28 27 25
17 | 6 11 7 7 10 6 8 7 8 6 2 | 31 34 28 32 31 28 33 30 33 30 30
X18 | 16 21 12 12 9 7 13 9 11 --- 5 | 41 48 47 40 40 41 44 40 38 --- 41
19 | 7 18 8 8 11 5 9 5 7 6 3 | 25 33 29 31 25 27 30 25 30 26 26
20 | 7 10 6 6 8 3 7 7 10 7 2 | 27 27 26 25 27 26 28 24 28 25 25
21 | 7 8 7 9 15 4 7 7 7 7 3 | 30 29 28 31 35 28 29 28 30 29 29
22 | 6 9 6 8 14 4 8 8 7 7 3 | 28 27 25 26 31 25 28 26 29 25 26
23 | 9 14 12 9 12 5 9 7 12 8 3 | 68 67 63 65 69 63 65 68 68 67 66
24 | 6 8 8 6 6 4 7 5 9 6 2 | 31 35 32 33 31 31 36 30 29 30 31
X25E | 18 15 11 14 25 9 --- 7 13 16 5 | 193 216 194 195 193 191 --- 187 182 189 190
26E | 13 13 9 55 23 5 8 6 14 10 4 | 24 28 23 57 33 25 26 27 30 28 25
27 | 7 11 8 7 9 3 9 5 9 6 2 | 22 23 24 23 22 21 24 21 23 21 21
28E | 7 12 7 8 10 4 7 9 11 11 3 | 20 25 21 24 23 21 24 23 25 26 22
29 | 5 15 6 9 10 4 9 4 8 5 2 | 28 28 27 31 31 27 28 28 28 27 28
30 | 5 10 8 8 7 2 7 4 7 5 2 | 28 32 29 27 27 28 33 26 30 26 28
31 | 9 13 8 7 12 4 7 5 8 11 3 | 41 42 38 40 40 40 42 39 40 38 39
32 | 8 15 6 13 6 4 15 7 7 9 3 | 23 35 24 22 21 24 33 24 21 25 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 13 11 4 9 6 9 8 |T 37 40 37 38 38 36 34 36 38 36 36
WRMS | 7 13 8 9 9 4 9 6 9 7 |NE 30 33 30 31 30 30 33 29 31 29 30
MEDI | 6 12 7 8 10 4 8 6 9 7 |MD 28 31 28 31 31 27 29 27 29 27 28
Table 3.2162.2 GPS week: 2162 Day: 2 MJD: 59380.000
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 10 9 4 9 7 7 7 2 | 21 23 23 21 24 20 24 19 21 17 20
2 | 8 13 8 13 8 5 7 6 11 8 3 | 25 24 25 29 23 23 23 25 23 23 23
3 | 3 9 7 8 10 3 7 5 7 6 2 | 17 19 19 19 20 17 19 14 18 16 16
4 | 4 18 5 10 7 4 19 5 8 6 3 | 46 47 46 49 48 44 47 46 46 47 46
5 | 7 8 6 8 7 5 8 7 10 6 2 | 23 25 22 25 26 25 27 26 26 26 24
6 | 11 18 5 11 12 4 10 6 11 8 3 | 25 26 24 22 24 21 23 21 22 20 22
7 | 5 10 7 7 8 4 7 5 10 6 2 | 36 38 34 36 33 33 37 35 30 36 34
8 | 4 11 7 9 8 3 9 4 7 7 2 | 19 22 21 19 21 19 20 19 20 18 19
9 | 6 13 5 6 7 5 12 5 7 7 2 | 21 35 24 25 21 23 33 21 24 23 23
10 | 6 10 8 10 13 4 7 6 6 4 2 | 20 23 21 16 21 19 20 18 19 17 18
12E | 7 18 13 11 9 6 7 6 10 6 3 | 24 25 26 22 23 26 26 23 27 25 23
13 | 7 7 7 13 8 4 7 6 8 9 2 | 13 18 14 11 12 14 17 18 17 17 14
14E | 8 14 12 24 14 5 12 10 17 16 5 | 94 95 92 93 97 92 92 90 92 91 92
15 | 5 11 6 11 7 3 9 6 8 8 2 | 34 37 33 34 31 34 36 35 33 34 34
16E | 6 20 13 8 10 5 10 8 8 14 3 | 20 20 22 20 22 21 19 22 21 23 20
17 | 7 10 7 7 10 5 8 5 10 6 2 | 19 24 17 20 20 19 23 20 22 21 19
X18 | 13 20 13 18 10 6 13 8 18 --- 5 | 28 35 29 30 29 29 31 27 35 --- 28
19 | 7 12 6 10 10 5 7 3 9 5 2 | 18 21 19 20 19 19 21 19 22 18 19
20 | 8 10 6 9 8 4 8 7 13 7 3 | 16 19 17 16 18 15 16 17 18 16 16
21 | 6 11 9 13 12 6 6 6 8 7 3 | 24 22 22 29 28 21 21 22 21 24 22
22 | 5 9 7 9 16 5 8 11 8 5 3 | 17 19 14 18 24 16 16 16 17 16 15
23 | 10 14 10 11 14 5 10 5 11 8 3 | 60 55 54 58 61 53 56 58 55 58 57
24 | 6 7 8 8 9 3 6 6 9 7 2 | 21 28 23 21 20 22 28 23 22 26 23
X25E | 8 --- 9 16 23 9 --- 11 18 14 5 | 131 --- 132 136 132 132 --- 131 132 137 132
26E | 10 15 10 79 11 5 8 6 10 13 4 | 25 32 28 65 32 25 21 25 27 27 26
27 | 4 10 7 10 7 3 9 5 8 6 2 | 26 26 27 25 26 25 27 25 26 24 25
28E | 9 12 7 11 12 5 9 10 9 13 3 | 23 23 21 26 23 21 23 24 23 25 22
29 | 8 17 6 11 8 3 9 5 9 7 3 | 21 18 17 24 20 19 19 19 21 23 19
30 | 4 8 7 5 8 3 7 5 8 5 2 | 21 24 22 21 21 22 26 21 21 20 21
31 | 8 13 8 7 11 4 8 5 8 11 3 | 38 42 36 37 36 37 39 36 35 32 36
32 | 7 14 6 16 5 5 13 6 7 6 3 | 22 34 26 23 23 22 34 24 27 22 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 18 10 4 9 6 9 8 |T 30 29 30 32 31 29 28 30 31 30 30
WRMS | 7 13 8 14 9 4 9 6 9 7 |NE 25 28 25 25 25 24 27 24 25 24 24
MEDI | 7 11 7 10 9 5 8 6 9 7 |MD 23 24 23 24 23 22 23 23 23 23 23
Table 3.2162.3 GPS week: 2162 Day: 3 MJD: 59381.000
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 9 9 2 10 4 8 9 3 | 26 28 28 27 27 25 27 24 25 24 25
2 | 9 8 9 17 7 5 7 7 7 7 3 | 32 31 33 39 31 31 30 32 32 31 31
3 | 4 8 7 10 9 3 7 6 6 6 2 | 25 25 26 29 27 24 25 23 24 23 24
4 | 5 18 6 11 7 3 20 6 7 8 3 | 39 40 40 45 41 37 38 41 40 42 40
5 | 6 12 6 10 7 3 8 8 9 8 3 | 29 32 26 33 28 29 29 28 30 28 28
6 | 10 14 4 8 11 4 10 6 9 8 3 | 31 31 31 29 30 28 31 27 29 27 28
7 | 4 11 6 6 9 3 6 5 6 6 2 | 47 48 45 44 44 44 45 46 44 45 45
8 | 5 11 6 8 7 3 9 4 6 6 2 | 24 26 26 25 24 24 25 24 24 24 24
9 | 7 14 5 6 7 2 11 5 7 10 2 | 27 38 30 31 27 28 37 28 29 25 28
10 | 7 11 8 9 13 2 8 5 6 7 3 | 29 30 28 26 26 26 25 24 24 26 25
12E | 8 19 10 7 8 2 8 6 8 7 3 | 28 28 29 32 29 29 31 30 30 31 29
13 | 6 9 7 10 10 4 7 6 7 9 2 | 23 27 24 20 21 22 25 25 25 25 23
14E | 9 15 12 23 15 6 13 14 14 15 5 | 46 45 47 48 49 44 46 47 47 43 45
15 | 5 11 7 7 6 4 9 9 8 7 2 | 41 44 40 37 37 40 43 39 36 42 39
16E | 5 18 12 9 11 5 9 7 10 10 3 | 32 31 30 30 28 31 30 33 31 33 30
17 | 7 11 9 10 8 5 8 5 7 9 2 | 26 31 26 27 27 26 29 25 30 28 26
X18 | 15 20 13 14 10 6 12 7 13 --- 4 | 41 41 36 39 37 35 38 35 36 --- 36
19 | 8 15 8 9 8 5 7 5 11 8 3 | 23 27 25 25 23 23 24 23 27 24 23
20 | 6 13 6 9 8 4 7 8 11 9 3 | 23 25 22 26 24 23 22 21 24 23 22
21 | 8 8 6 11 12 5 7 4 9 8 3 | 29 26 27 33 31 26 26 26 24 27 26
22 | 5 11 6 9 15 6 6 5 8 8 3 | 21 21 20 24 25 20 19 19 22 20 19
23 | 10 17 11 9 14 4 10 8 13 7 3 | 57 55 50 58 62 54 53 55 58 53 55
24 | 5 7 8 9 6 3 6 5 10 6 2 | 28 32 28 31 27 27 33 29 25 30 28
X25E | 12 15 8 28 21 5 --- 12 16 10 5 | 104 86 105 104 100 103 --- 104 102 104 103
26E | 10 17 9 108 9 5 8 7 11 13 4 | 24 28 24 86 24 23 23 23 26 21 22
27 | 5 11 7 9 8 3 9 5 7 6 2 | 30 28 30 29 30 29 32 28 29 26 28
28E | 11 10 7 10 11 4 9 8 10 15 3 | 24 27 24 25 27 25 25 26 28 29 25
29 | 7 19 7 10 9 3 9 3 8 7 3 | 30 28 27 31 27 27 27 26 26 26 27
30 | 5 8 7 6 8 2 7 4 6 8 2 | 31 31 28 27 29 28 31 28 29 30 28
31 | 7 14 9 6 12 4 7 5 9 13 3 | 49 51 45 45 48 46 49 46 45 43 46
32 | 6 13 6 8 7 4 13 6 7 11 3 | 27 35 25 27 26 26 35 26 28 32 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 22 10 4 9 6 9 9 |T 33 34 33 36 33 32 31 32 33 32 32
WRMS | 7 13 8 11 9 4 9 5 8 8 |NE 31 33 30 32 31 29 31 29 30 30 30
MEDI | 7 12 7 9 9 4 8 6 8 8 |MD 29 31 28 31 28 28 30 28 29 28 28
Table 3.2162.4 GPS week: 2162 Day: 4 MJD: 59382.000
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 11 10 11 10 2 11 5 7 6 3 | 23 23 24 23 25 21 24 20 22 19 21
2 | 7 9 10 13 8 5 8 5 10 6 3 | 23 22 25 28 25 23 22 22 26 24 23
3 | 3 9 8 9 9 4 8 6 8 6 2 | 18 20 20 18 19 18 22 16 18 15 17
4 | 5 17 10 9 7 3 20 5 8 7 3 | 52 52 52 52 52 49 51 50 48 50 50
5 | 5 10 8 8 8 3 7 6 9 7 2 | 28 31 28 31 30 29 30 30 28 30 28
6 | 9 14 5 9 13 3 10 5 8 7 3 | 27 31 26 26 27 25 28 24 26 23 25
7 | 5 12 6 8 9 4 8 4 7 6 2 | 39 40 39 41 33 37 39 40 35 40 38
8 | 6 10 7 10 9 3 8 4 8 6 2 | 18 21 20 18 19 18 20 18 19 19 18
9 | 6 13 6 7 8 4 12 4 7 5 2 | 24 37 28 25 24 26 36 24 29 24 26
10 | 6 10 10 13 17 4 9 4 5 6 3 | 21 24 23 20 23 19 22 18 19 19 19
12E | 6 18 11 9 12 4 8 6 12 9 3 | 28 33 30 26 26 28 31 27 31 27 27
13 | 6 5 7 4 10 4 7 5 8 6 2 | 14 17 17 15 15 15 17 17 18 17 15
14E | 31 20 26 24 16 8 25 7 12 11 7 | 99 92 90 94 96 91 92 93 91 91 92
15 | 6 13 6 8 8 5 10 7 9 8 3 | 34 39 35 31 31 35 37 34 33 35 34
16E | 7 16 14 9 11 4 10 5 8 9 3 | 15 18 17 14 16 12 16 16 15 16 14
17 | 6 12 7 9 7 5 8 4 8 9 2 | 21 24 17 20 20 20 23 21 22 21 20
X18 | 13 19 14 15 12 5 12 8 13 --- 5 | 30 38 30 28 32 28 32 30 31 --- 29
19 | 6 14 8 10 9 5 8 3 8 9 2 | 18 22 19 18 19 19 21 18 20 19 18
20 | 5 10 7 8 10 3 7 6 10 9 2 | 17 18 18 19 19 16 16 17 19 17 16
21 | 8 11 9 10 14 5 7 5 7 7 3 | 21 20 20 24 25 19 20 19 21 23 20
22 | 6 10 9 7 18 5 6 4 10 5 3 | 15 17 16 16 19 15 17 16 19 14 14
23 | 9 15 13 10 16 6 10 6 14 9 4 | 64 59 60 63 65 60 63 61 62 61 61
24 | 5 8 7 9 9 4 6 4 11 5 2 | 21 26 23 23 18 21 25 20 21 21 20
25E | 6 12 7 26 23 6 8 7 13 13 4 | 108 92 109 109 109 108 42 105 110 109 108
26E | 11 15 10 107 13 4 6 7 9 14 4 | 32 38 29 82 32 28 19 30 27 29 28
27 | 4 10 8 8 9 3 7 4 10 7 2 | 29 29 31 32 30 28 30 30 30 30 29
28E | 11 11 6 12 15 3 7 8 9 11 3 | 22 21 22 22 25 21 22 22 23 24 21
29 | 6 18 5 9 8 4 8 4 11 6 3 | 19 18 16 23 19 17 17 17 21 17 17
30 | 6 8 10 6 8 2 8 3 7 8 2 | 25 28 26 25 23 25 28 23 24 26 24
31 | 6 12 10 9 11 3 10 4 12 8 3 | 37 43 37 35 35 37 42 37 33 33 36
32 | 6 12 7 13 9 4 13 7 9 6 3 | 25 35 27 25 25 26 36 27 29 28 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 22 12 4 10 5 9 8 |T 31 33 31 33 31 30 30 30 31 30 30
WRMS | 6 13 9 10 11 4 10 5 9 7 |NE 26 29 27 27 26 25 28 25 26 26 25
MEDI | 6 12 8 9 10 4 8 5 9 7 |MD 24 28 26 25 25 25 25 23 26 24 24
Table 3.2162.5 GPS week: 2162 Day: 5 MJD: 59383.000
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 13 7 8 10 4 11 7 9 10 3 | 21 25 24 20 23 21 24 19 22 20 20
2 | 6 8 6 9 9 4 7 6 7 5 2 | 20 20 22 21 20 20 21 19 22 16 19
3 | 7 9 7 7 11 3 9 8 10 8 3 | 20 22 20 17 21 18 24 16 17 18 17
4 | 7 19 6 9 8 5 20 7 6 6 3 | 43 46 44 48 44 44 47 48 46 47 45
5 | 5 9 7 9 8 4 8 8 7 5 2 | 22 20 19 24 22 21 22 23 21 23 21
6 | 8 10 7 15 14 4 10 6 9 7 3 | 21 24 24 22 22 21 27 21 20 19 21
7 | 6 10 7 8 7 5 7 6 10 9 2 | 34 38 34 40 36 33 36 37 31 38 35
8 | 8 9 7 11 9 4 10 7 12 7 3 | 22 23 22 21 22 19 21 19 18 18 19
9 | 8 13 7 7 7 5 10 8 8 9 3 | 22 31 25 24 18 22 32 20 24 23 22
10 | 7 9 8 12 18 4 7 5 8 9 3 | 23 28 25 22 25 21 24 22 22 22 22
X12E | 8 --- 10 13 14 4 6 7 6 8 3 | 23 --- 28 33 26 27 27 26 31 26 26
13 | 5 8 6 8 7 4 7 6 6 8 2 | 15 18 20 21 12 16 19 16 14 13 15
14E | 25 28 31 34 25 7 32 12 37 15 9 | 136 129 127 133 130 128 125 128 139 133 129
15 | 6 12 5 7 8 5 7 9 8 7 2 | 23 25 20 24 23 23 25 23 23 24 22
16E | 8 17 13 10 14 5 9 6 10 8 3 | 17 18 15 19 17 15 14 15 18 18 15
17 | 7 12 8 8 10 5 8 6 7 7 2 | 19 24 18 20 19 19 24 18 21 21 19
X18 | 13 22 14 17 14 7 12 9 16 --- 5 | 31 38 32 35 34 30 33 33 33 --- 31
19 | 8 17 6 9 10 5 8 7 9 8 3 | 18 26 20 22 18 20 24 17 19 19 18
20 | 6 10 8 8 8 4 7 8 7 6 2 | 17 16 17 18 18 16 18 16 17 16 15
21 | 9 12 8 10 17 6 10 6 6 9 3 | 24 22 22 27 27 20 20 21 23 23 21
22 | 7 10 5 6 14 4 8 5 7 7 2 | 20 21 17 17 24 17 21 18 17 18 17
23 | 9 16 14 10 17 5 9 6 17 10 4 | 60 60 57 61 60 58 57 61 64 61 59
24 | 9 9 7 7 7 3 6 7 11 8 2 | 20 26 21 24 18 20 25 18 20 20 20
25E | 9 12 9 29 16 4 8 6 13 16 4 | 109 92 112 107 109 109 45 106 110 112 108
X26E | 8 --- 9 97 12 5 10 7 9 11 3 | 33 --- 31 70 32 29 15 30 26 28 29
27 | 6 9 7 11 10 3 8 6 10 7 3 | 27 26 26 27 25 25 26 24 26 27 25
28E | 12 11 5 16 12 4 8 9 13 17 4 | 16 22 16 24 21 17 21 19 19 24 18
29 | 8 19 6 11 9 5 7 7 10 5 3 | 17 21 13 23 17 17 17 17 17 17 16
30 | 8 10 9 8 7 4 7 6 7 7 2 | 22 26 21 22 24 22 27 22 20 23 22
31 | 8 15 9 7 12 4 9 4 8 9 3 | 37 43 37 35 34 35 40 35 36 33 36
32 | 8 12 7 9 9 4 13 8 9 11 3 | 22 33 24 23 22 23 32 24 23 26 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 12 12 5 11 7 12 9 |T 30 33 30 33 31 29 30 30 30 30 29
WRMS | 7 13 8 11 11 4 11 7 10 9 |NE 24 28 24 26 25 24 27 24 24 24 24
MEDI | 8 12 7 9 10 4 8 7 9 8 |MD 22 25 22 24 23 21 24 21 22 23 21
Table 3.2162.6 GPS week: 2162 Day: 6 MJD: 59384.000
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 11 7 8 9 3 10 5 6 7 2 | 25 24 24 24 25 22 25 21 23 20 22
2 | 5 10 6 12 8 3 9 6 8 6 2 | 29 28 30 32 28 28 29 28 27 26 28
3 | 5 11 6 6 11 3 8 6 9 7 2 | 22 24 22 19 23 21 24 19 20 20 20
4 | 6 16 5 10 7 4 20 5 8 7 3 | 66 68 66 69 66 66 69 68 69 69 67
5 | 5 8 8 7 8 3 6 5 9 7 2 | 27 27 25 29 28 27 27 29 30 30 27
6 | 7 14 6 8 11 3 9 5 12 6 3 | 28 32 29 26 28 27 31 26 28 26 27
7 | 7 11 7 13 9 5 7 7 8 9 3 | 53 54 54 60 52 51 54 56 50 57 54
8 | 6 7 8 12 8 4 7 7 9 5 2 | 24 26 26 26 26 24 25 28 27 27 25
9 | 8 13 5 10 6 4 11 5 8 8 2 | 27 35 29 29 25 28 35 28 28 29 28
10 | 5 10 7 9 15 3 8 4 7 8 3 | 25 30 26 28 27 23 25 23 24 24 24
12E | 6 17 10 9 13 4 6 7 11 9 3 | 40 45 44 44 40 43 45 41 42 43 42
13 | 6 8 8 8 7 5 7 6 5 7 2 | 14 17 16 15 14 13 16 17 15 18 15
14E | 18 23 17 56 18 6 18 20 14 21 7 | 148 147 146 149 150 146 146 145 144 149 145
15 | 5 10 8 9 8 4 7 9 6 6 2 | 49 49 47 46 45 47 50 47 44 49 47
16E | 4 21 13 11 15 5 11 9 12 12 4 | 23 28 24 26 25 24 25 27 26 28 24
17 | 5 10 7 11 8 4 8 4 8 10 2 | 23 25 22 22 23 22 25 23 24 25 22
X18 | 10 21 15 13 12 5 12 9 13 --- 4 | 51 55 49 51 49 50 52 51 52 --- 50
19 | 6 14 6 11 8 6 8 6 10 9 3 | 24 26 24 25 24 24 25 24 24 25 24
20 | 5 8 7 6 9 3 6 5 9 7 2 | 18 16 17 17 17 16 17 17 19 19 16
21 | 8 11 9 17 11 5 9 6 4 8 3 | 30 28 26 36 31 26 27 27 27 29 27
22 | 7 9 6 8 15 3 8 4 9 7 2 | 24 23 21 22 28 22 25 23 23 23 22
23 | 9 17 11 12 17 5 9 6 11 11 4 | 87 84 83 87 88 84 85 88 87 84 85
24 | 7 7 6 7 6 3 7 5 6 8 2 | 26 27 24 26 22 24 28 23 22 24 24
25E | 7 10 9 27 9 3 7 5 7 11 3 | 157 134 159 156 154 156 60 154 155 156 156
26E | 8 20 8 66 12 5 9 6 11 12 4 | 46 54 44 65 47 43 22 44 44 42 44
27 | 5 12 6 12 8 3 8 6 11 6 2 | 29 28 29 30 27 28 29 26 30 27 27
28E | 14 11 7 21 9 3 9 10 8 12 4 | 31 33 32 38 31 30 31 33 30 34 32
29 | 7 18 7 11 8 4 9 6 8 6 3 | 22 22 19 25 21 20 21 20 24 21 20
30 | 7 10 10 11 7 5 6 5 10 13 3 | 25 28 26 30 25 25 28 25 25 30 25
31 | 7 12 8 7 9 4 8 5 7 8 2 | 50 54 47 45 46 48 52 48 47 45 48
32 | 7 11 5 7 7 4 11 8 8 11 3 | 33 40 35 35 32 34 39 38 35 36 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 19 10 4 9 7 9 9 |T 41 42 40 42 40 40 38 40 40 41 40
WRMS | 7 13 8 14 9 4 9 6 8 8 |NE 33 34 32 34 32 32 34 32 32 32 32
MEDI | 7 11 7 11 9 4 8 6 8 8 |MD 28 28 29 30 28 27 28 28 28 28 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 4.2162 GPS week: 2162 MJD: 59378.0-59384.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 |U 12 10 32 |U 11 15 33 |U 12 14 40 |
emr | emr 2934 |U 22 12 40 |U 15 25 47 |U 17 14 61 |
esa | esa 2976 | 14 12 35 |U 12 20 41 | 12 12 38 |
gfz | gfz 2973 |U 14 12 32 |U 10 13 34 |U 13 14 37 |
grg | grg 2972 |U 14 12 36 |U 13 20 36 | 13 15 39 |
igr | igr 2975 | 13 11 31 | 10 15 33 | 12 13 39 |
igs | igs 2974 | 13 10 31 | 10 15 33 | 12 13 39 |
jpl | jpl 2921 | 17 12 36 |U 12 24 40 | 14 14 49 |
mit | mit 2976 |U 13 11 32 |U 10 13 34 |U 13 13 36 |
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 5.2162.0 GPS week: 2162 Day: 0 MJD: 59378.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 12 9 38 | 12 18 46 | 15 19 52 |
emr | emr 2976 | 25 13 49 | 16 20 58 | 18 19 75 |
esa | esa 2976 | 16 10 41 | 12 18 43 | 14 18 45 |
gfz | gfz 2976 | 13 11 36 | 10 15 42 | 16 18 43 |
grg | grg 2976 | 12 11 30 | 13 18 32 | 14 22 55 |
igr | igr 2973 | 13 10 36 | 11 16 37 | 14 16 40 |
igs | igs 2971 | 14 10 38 | 10 15 34 | 15 17 49 |
jpl | jpl 2880 | 18 12 50 | 11 26 38 | 16 15 54 |
mit | mit 2976 | 12 9 36 | 10 15 34 | 15 16 50 |
Table 5.2162.1 GPS week: 2162 Day: 1 MJD: 59379.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 11 9 30 | 11 13 35 | 11 11 36 |
emr | emr 2976 | 22 9 50 | 15 25 42 | 18 13 64 |
esa | esa 2976 | 13 10 35 | 11 19 43 | 13 12 37 |
gfz | gfz 2976 | 12 9 34 | 9 11 38 | 11 11 38 |
grg | grg 2976 | 11 9 26 | 13 13 29 | 11 10 35 |
igr | igr 2976 | 10 8 31 | 10 14 34 | 11 10 39 |
igs | igs 2976 | 11 8 30 | 10 13 33 | 11 10 37 |
jpl | jpl 2880 | 14 11 32 | 10 20 43 | 13 14 45 |
mit | mit 2976 | 11 9 32 | 10 13 37 | 11 11 36 |
Table 5.2162.2 GPS week: 2162 Day: 2 MJD: 59380.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 10 6 29 | 16 16 42 | 14 12 38 |
emr | emr 2880 | 23 11 33 | 20 33 63 | 17 15 55 |
esa | esa 2976 | 15 11 34 | 19 25 56 | 14 14 32 |
gfz | gfz 2971 | 11 8 33 | 15 14 43 | 14 11 37 |
grg | grg 2972 | 15 12 43 | 18 17 48 | 16 11 34 |
igr | igr 2975 | 11 8 28 | 16 18 46 | 14 11 34 |
igs | igs 2972 | 11 7 28 | 17 18 47 | 14 11 34 |
jpl | jpl 2880 | 18 11 32 | 19 29 61 | 13 13 45 |
mit | mit 2976 | 11 7 28 | 17 16 46 | 15 9 32 |
Table 5.2162.3 GPS week: 2162 Day: 3 MJD: 59381.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 11 11 35 | 12 13 31 | 10 13 39 |
emr | emr 2976 | 21 9 34 | 14 26 38 | 16 13 54 |
esa | esa 2976 | 13 14 34 | 12 19 37 | 11 10 37 |
gfz | gfz 2964 | 14 19 27 | 10 12 29 | 12 15 36 |
grg | grg 2958 | 14 14 44 | 12 14 27 | 12 15 38 |
igr | igr 2976 | 12 12 31 | 11 14 27 | 10 11 38 |
igs | igs 2976 | 12 13 31 | 11 14 30 | 11 12 38 |
jpl | jpl 2880 | 17 11 37 | 13 24 32 | 12 16 45 |
mit | mit 2976 | 12 14 33 | 10 12 35 | 12 14 37 |
Table 5.2162.4 GPS week: 2162 Day: 4 MJD: 59382.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 14 12 29 | 12 14 30 | 11 15 40 |
emr | emr 2976 | 24 14 35 | 14 23 50 | 18 13 67 |
esa | esa 2976 | 16 13 33 | 13 21 33 | 11 12 41 |
gfz | gfz 2976 | 16 12 27 | 10 12 34 | 12 17 36 |
grg | grg 2976 | 16 13 35 | 23 48 52 | 12 17 36 |
igr | igr 2976 | 14 11 26 | 11 14 30 | 12 14 40 |
igs | igs 2976 | 15 11 27 | 12 13 33 | 12 14 39 |
jpl | jpl 2976 | 17 14 31 | 14 23 39 | 15 12 51 |
mit | mit 2976 | 14 12 28 | 11 12 34 | 12 15 35 |
Table 5.2162.5 GPS week: 2162 Day: 5 MJD: 59383.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 14 12 37 | 8 18 28 | 14 16 44 |
emr | emr 2784 | 22 17 41 | 12 25 47 | 18 14 66 |
esa | esa 2976 | 17 12 37 | 10 22 42 | 14 14 43 |
gfz | gfz 2976 | 16 13 39 | 9 15 28 | 13 18 39 |
grg | grg 2976 | 14 12 39 | 9 15 34 | 14 16 43 |
igr | igr 2976 | 15 12 35 | 8 18 30 | 14 16 46 |
igs | igs 2976 | 15 11 34 | 8 17 29 | 14 16 44 |
jpl | jpl 2976 | 20 13 38 | 10 26 38 | 17 15 54 |
mit | mit 2976 | 15 12 35 | 8 14 28 | 12 16 38 |
Table 5.2162.6 GPS week: 2162 Day: 6 MJD: 59384.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 13 13 30 | 5 12 21 | 10 13 31 |
emr | emr 2976 | 15 11 36 | 12 24 34 | 16 13 48 |
esa | esa 2976 | 12 13 29 | 7 18 34 | 11 7 34 |
gfz | gfz 2976 | 14 14 30 | 6 12 23 | 11 11 27 |
grg | grg 2976 | 14 14 33 | 6 12 29 | 11 13 29 |
igr | igr 2976 | 12 13 28 | 6 14 24 | 11 11 32 |
igs | igs 2976 | 12 12 28 | 6 13 22 | 11 11 30 |
jpl | jpl 2976 | 14 12 34 | 10 20 32 | 14 11 47 |
mit | mit 2976 | 13 15 29 | 6 12 21 | 10 9 24 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.2162 GPS week: 2162 MJD: 59378.500-59384.500
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 1 31 -55 1 | 6 21
| 9 14 57 56 3 | 2
emr uuuuu | 30 11 -78 48 5 | 18 28
| 11 10 120 97 10 | 2
esa uuuuu | 7 -10 179 127 -1 | 17 25
| 6 7 27 62 4 | 2
gfz uuuuu | 4 -19 29 -23 -2 | 24 31
| 16 25 139 134 7 | 2
grg uuuuu | 1 -26 -15 -9 0 | 3 19
| 8 11 26 31 3 | 2
igr xxxxx | -3 -8 63 -22 -3 | 1 18
| 6 9 43 45 3 | 2
irf xxxxx | 0 -2 -35 11 -2 | 1 19
| 6 12 18 12 3 | 1
jpl uuuuu | 19 6 78 -3 -4 | 32 37
| 20 18 53 54 8 | 2
mit uuuuu | 2 5 -119 6 -2 | 28 34
| 13 18 32 38 5 | 2
ngs uuuuu | -37 28 -105 -95 -1 | 19 28
| 37 14 116 103 5 | 2
sio xxxxx | -16 36 -256 51 12 | 22 29
| 42 47 123 70 5 | 5
Table 7.2162.0 GPS week: 2162 Day: 0 MJD: 59378.500
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 -3 2 -97 -1 | 7 19
emr uuuuu | 27 -1 163 -87 -8 | 18 25
esa uuuuu | -6 -7 196 131 3 | 18 25
gfz uuuuu | 7 -3 -97 130 11 | 21 29
grg uuuuu | 3 -33 -20 -41 -4 | 4 16
igr xxxxx | -5 -10 81 36 0 | 2 16
irf xxxxx | -8 6 -41 1 3 | 2 17
jpl uuuuu | -21 5 177 -105 9 | 28 34
mit uuuuu | 13 3 -136 33 5 | 27 32
ngs uuuuu | 11 31 -201 13 1 | 18 26
sio xxxxx | -9 31 -351 -17 14 | 17 24
Table 7.2162.1 GPS week: 2162 Day: 1 MJD: 59379.500
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 | -14 33 57 -94 -4 | 6 20
emr uuuuu | 27 21 -76 72 12 | 15 25
esa uuuuu | 12 -17 207 185 -5 | 18 25
gfz uuuuu | 0 -6 -60 -16 -9 | 23 29
grg uuuuu | 4 -15 -30 -12 -1 | 2 17
igr xxxxx | -8 5 74 -13 -1 | 1 16
irf xxxxx | -1 -15 -40 30 1 | 1 17
jpl uuuuu | 11 -6 12 -8 0 | 30 34
mit uuuuu | -8 -24 -162 42 4 | 27 32
ngs uuuuu | -14 22 49 -168 5 | 17 25
sio xxxxx | -22 74 -457 37 7 | 17 24
Table 7.2162.2 GPS week: 2162 Day: 2 MJD: 59380.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -12 -4 46 -64 0 | 6 20
emr uuuuu | 35 -3 -27 66 16 | 17 27
esa uuuuu | 8 -13 167 67 -8 | 19 25
gfz uuuuu | 30 22 -156 9 -4 | 24 30
grg uuuuu | 8 -17 -59 0 1 | 3 18
igr xxxxx | -9 -7 -7 -57 -6 | 2 17
irf xxxxx | 3 -11 -33 23 -2 | 2 18
jpl uuuuu | 19 -12 63 53 -14 | 34 38
mit uuuuu | -5 0 -91 25 -2 | 29 34
ngs uuuuu | -60 40 -19 -135 2 | 19 28
sio xxxxx | -79 -1 -303 -25 5 | 20 27
Table 7.2162.3 GPS week: 2162 Day: 3 MJD: 59381.500
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 -2 67 -59 2 | 8 21
emr uuuuu | 40 11 -166 -31 2 | 20 31
esa uuuuu | 8 -14 143 208 -4 | 20 26
gfz uuuuu | 13 -55 67 19 3 | 27 32
grg uuuuu | -10 -15 -1 27 1 | 6 19
igr xxxxx | -3 -18 35 -94 -6 | 4 18
irf xxxxx | 1 -14 -8 10 -3 | 4 19
jpl uuuuu | 21 27 83 -32 -2 | 36 39
mit uuuuu | 5 -1 -79 -6 -1 | 32 36
ngs uuuuu | -64 44 -187 -157 -4 | 22 30
sio xxxxx | -39 -19 -169 38 19 | 23 30
Table 7.2162.4 GPS week: 2162 Day: 4 MJD: 59382.500
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 -2 4 44 2 | 4 22
emr uuuuu | 44 8 -130 14 5 | 16 30
esa uuuuu | 6 0 174 155 -2 | 15 25
gfz uuuuu | 10 -33 66 73 -2 | 23 31
grg uuuuu | -12 -36 -20 -18 2 | 1 21
igr xxxxx | 9 -20 132 -37 0 | -1 21
irf xxxxx | 11 -4 -17 10 -2 | 0 21
jpl uuuuu | 38 33 65 14 -12 | 32 38
mit uuuuu | 22 3 -90 -38 -5 | 28 34
ngs uuuuu | -91 15 -17 -234 5 | 17 29
sio xxxxx | -1 10 -221 78 14 | 22 30
Table 7.2162.5 GPS week: 2162 Day: 5 MJD: 59383.500
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 | 0 -7 -68 -111 2 | 4 22
emr uuuuu | 27 22 -198 219 15 | 17 30
esa uuuuu | 7 -18 213 110 4 | 14 25
gfz uuuuu | -10 -24 224 -97 -2 | 24 32
grg uuuuu | 6 -42 8 29 -2 | 1 21
igr xxxxx | -3 -6 49 22 -4 | 0 21
irf xxxxx | -8 12 -55 -7 -4 | 0 21
jpl uuuuu | 39 4 39 9 -4 | 32 37
mit uuuuu | -17 37 -125 -49 -8 | 28 34
ngs uuuuu | -43 6 -91 -18 -9 | 18 30
sio xxxxx | -22 35 -202 64 14 | 25 33
Table 7.2162.6 GPS week: 2162 Day: 6 MJD: 59384.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -25 -8 106 -6 7 | 6 20
emr uuuuu | 9 16 -113 79 -5 | 21 31
esa uuuuu | 14 -4 154 35 3 | 17 25
gfz uuuuu | -20 -37 156 -282 -11 | 26 32
grg uuuuu | 7 -24 17 -51 3 | 3 19
igr xxxxx | 0 -2 78 -10 -1 | 1 20
irf xxxxx | -1 10 -53 11 -5 | 1 20
jpl uuuuu | 22 -10 106 50 -6 | 34 38
mit uuuuu | 0 14 -148 37 -7 | 29 35
ngs uuuuu | 0 35 -267 33 -4 | 19 29
sio xxxxx | 60 119 -89 183 14 | 30 34
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