[IGSREPORT-26289] Wk 2029 IGS Final Orbits
acc
acc at igs.org
Thu Dec 13 18:38:24 PST 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2029 (Nov 25, 2018 - Dec 01, 2018)
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:
igs2029[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2029[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2029[0-6].cls IGS GPS clock combination summary report.
igs20297.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20297.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 | ALL | 4
0 | COD | 24 24 NAUR NYA1 TIXI NAUR NYA1 TIXI
0 | EMR | JOZE
0 | ESA | LHAZ REUN URUM LHAZ REUN URUM
0 | GFZ | BJNM GODE REUN BJNM GODE NYAL REUN
0 | GRG | GLSV DARW GLSV
0 | JPL | 24 24 LAUT
1 | COD | GLSV NAUR NICO NYA1 RBAY TIXI TRO1 WIND GLSV NAUR
1 | COD | NICO NYA1 RBAY TIXI WIND
1 | EMR | NYAL TLSE NYAL TLSE
1 | ESA | WIND TLSE WIND WTZR
1 | GFZ | 8 BJNM GODE NOVM NYA1 BJNM GODE NOVM NYA1
1 | GRG | DARW GLSV KRGG NICO RABT SHAO DARW GLSV KRGG SHAO
1 | JPL | POLV SHAO CUSV NICO POLV SHAO
2 | COD | NAUR TIXI BRMU NAUR REUN TIXI
2 | EMR | JOZE
2 | ESA | REUN PTBB
2 | GFZ | BJNM GODE POHN BJNM GODE POHN REUN
2 | GRG | REUN DARW
2 | JPL | 27 MAG0 MAG0
2 | MIT | BJNM
3 | COD | 7 7 NAUR POVE RBAY TIXI NAUR POVE RBAY TIXI
3 | EMR | TLSE YAR2 PERT TLSE YAR2
3 | ESA | 22 FAA1 NICO OUS2 FAA1 OUS2
3 | GFZ | GODE MAL2 POHN GODE MAL2 POHN
3 | GRG | FAA1 KRGG MCM4 TLSE DARW FAA1 KRGG LHAZ MAL2 MCM4
3 | GRG | TLSE
3 | JPL | MCM4 MCM4
4 | COD | 31 30 31 GLSV MAL2 TIXI GLSV MAL2 TIXI
4 | EMR | 30 30
4 | ESA | 22 TRO1 TRO1
4 | GFZ | 8 8 BJNM GODE MAL2 POHN BJNM GODE MAL2 POHN TSKB
4 | GRG | 7 7 GLSV GLSV
4 | JPL | 30 30 NOVM
4 | MIT | BJNM
5 | COD | ANKR TIXI ANKR BRMU TIXI
5 | EMR | 10 24 GRAZ ALBH ALGO AREQ BADG BOR1 CEDU CHUR CRO1
5 | EMR | DAEJ DRAO FAIR GODE GRAZ HARB HERS HOB2 IENG KERG
5 | EMR | KIRU MAR6 MAS1 MATE MCM4 MDO1 NIST NRC1 NYAL ONSA
5 | EMR | PIE1 PRDS PTBB QAQ1 SCH2 SFER STJO SYOG TIDB TSKB
5 | EMR | TWTF USN7 USUD WHIT WILL YAKT YAR2 YELL
5 | ESA | 19 22 BRMU CORD LAUT MAL2 REUN MAL2
5 | GFZ | GODE POHN YELL GODE POHN YELL
5 | GRG | 24 31 GLSV MCM4 YELL GLSV MCM4 REUN
5 | JPL | LAUT
5 | MIT | ALBH CHUR SCH2 SUTH
6 | COD | MAG0 MCM4 TIXI NAUR TIXI
6 | EMR | MCM4 TLSE TLSE
6 | ESA | 22 MCM4
6 | GFZ | 29 29 GODE MCM4 POHN BRMU GODE POHN
6 | GRG | GLSV LHAZ TLSE YELL GLSV LHAZ MCM4 TLSE YELL
6 | JPL | MCM4
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G07 | 4 | | | | | | 4 |
PRN G18 | | | | 4 | 4 | 4 | 4 |
PRN G31 | 4 | | | | | 4 | 4 |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .3 .0 .7 0 18 -10 -.31
EMR | 0 | 8.3 -.5 24.4 19 1 24 .15
ESA | 0 | -1.3 .5 1.7 6 15 33 -.14
GFZ | 0 | -1.0 .4 .4 12 -4 -5 -.02
GRG | 0 | 4.8 .5 11.5 47 -11 31 .09
JPL | 0 | 2.9 -2.8 11.0 4 4 12 -.27
MIT | 0 | 5.9 3.2 13.9 -6 32 -27 -.36
NGS | 0 | 3.8 -.5 22.2 25 -104 12 -.21
SIO | 0 | 3.8 -2.9 25.9 2 24 -3 .06
COD | 1 | .7 .0 .8 -5 14 -18 -.47
EMR | 1 | 7.4 1.7 14.7 -6 1 7 -.05
ESA | 1 | -1.0 .5 .7 -12 -2 19 -.45
GFZ | 1 | -.2 -.3 .5 -10 -22 -9 -.25
GRG | 1 | 3.4 -2.6 7.6 30 -24 41 -.09
JPL | 1 | 12.2 -7.5 12.2 1 0 1 -.50
MIT | 1 | 5.8 -1.1 13.1 -15 27 -30 -.28
NGS | 1 | -2.3 2.3 12.4 -5 -57 -10 -.18
SIO | 1 | 3.9 -2.9 19.5 15 -8 -27 -.09
COD | 2 | -.2 .4 .7 13 16 -14 -.36
EMR | 2 | 8.7 6.0 12.0 21 30 -48 -.02
ESA | 2 | -1.1 1.4 1.5 -2 -7 10 -.25
GFZ | 2 | -.0 -.0 .4 -4 -34 -13 -.07
GRG | 2 | 5.9 .1 13.2 31 -24 43 -.03
JPL | 2 | 10.1 -1.2 11.4 0 0 1 -.37
MIT | 2 | 5.8 2.4 14.0 9 18 -32 -.31
NGS | 2 | -1.9 6.6 14.3 13 -38 34 -.29
SIO | 2 | 3.0 2.0 21.2 28 18 -8 -.16
COD | 3 | .5 .0 .6 9 5 -9 -.36
EMR | 3 | 9.3 2.0 11.5 -4 46 -45 -.04
ESA | 3 | -.5 1.1 2.3 8 -2 7 -.35
GFZ | 3 | -.3 .2 .7 -17 -23 0 -.14
GRG | 3 | 2.4 -.5 23.4 42 -16 47 .08
JPL | 3 | 5.6 -1.8 9.2 1 0 1 -.49
MIT | 3 | 7.3 .4 15.1 21 31 -25 -.20
NGS | 3 | 3.4 6.3 8.6 34 -65 30 -.16
SIO | 3 | 10.2 .8 14.6 53 -4 -37 -.08
COD | 4 | -.0 -.1 .4 4 18 0 -.30
EMR | 4 | 5.9 -3.5 21.5 -6 47 -49 -.12
ESA | 4 | -.7 1.1 2.0 5 10 10 -.19
GFZ | 4 | .1 -.2 .1 -11 -34 2 -.23
GRG | 4 | 1.3 .5 20.0 40 -24 45 .02
JPL | 4 | 11.5 3.7 12.5 0 -7 -9 -.16
MIT | 4 | 4.8 -.2 19.8 35 29 -29 .0
NGS | 4 | 4.5 1.6 17.2 14 -73 33 .11
SIO | 4 | 1.2 1.0 25.2 43 -10 -35 -.16
COD | 5 | -.2 .2 .8 10 20 -10 -.36
EMR | 5 | 8.4 10.3 19.3 -7 49 -66 -.03
ESA | 5 | -.8 .5 1.7 2 23 3 -.10
GFZ | 5 | -.9 .4 .1 1 -8 -16 -.03
GRG | 5 | 3.5 3.8 15.6 29 -26 43 .04
JPL | 5 | 2.3 5.2 10.3 9 24 -5 -.46
MIT | 5 | 4.0 2.0 15.3 -1 25 -25 -.10
NGS | 5 | -.4 3.8 9.7 24 -40 35 -.14
SIO | 5 | 1.9 -1.9 16.1 29 19 -26 -.22
COD | 6 | .6 .1 1.0 13 9 2 -.38
EMR | 6 | 10.3 3.2 19.6 -8 12 38 -.17
ESA | 6 | -.7 .5 1.4 12 -9 9 -.09
GFZ | 6 | -.2 .4 .3 -2 -13 -10 -.10
GRG | 6 | 6.2 .1 17.1 55 -17 36 .11
JPL | 6 | 12.4 2.4 12.4 0 -1 1 -.23
MIT | 6 | 10.8 1.0 15.9 -5 11 -27 -.04
NGS | 6 | 8.1 3.6 6.2 22 -74 45 -.03
SIO | 6 | 7.2 .2 8.2 31 10 -16 -.12
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.2029.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2029.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 2.2029.[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 3.2029.[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 5.2029.0-6). 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 2029 summary. (Nov 25, 2018 - Dec 01, 2018)
Table 1.2029.a GPS week: 2029 MJD: 58447.000-58453.000
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 255| -1 1 0 14 7 1 -.01 10 9 | -499 -111 8 83
| 1 0 1 9 33 12 .02 | 76 222
emr 79| 1 -2 5 -37 -1 6 .19 13 13 | 146720 -283 21 139
| 0 2 2 11 6 15 .03 | 14179 1044
esa 150| 0 1 1 -10 11 -3 -.06 9 9 | -1181 543 10 204
| 0 0 2 12 8 7 .02 | 344 547
gfz 178| 0 0 0 9 5 -7 .08 10 10 | -104 36 12 114
| 0 1 1 10 9 10 .04 | 259 371
grg 105| 0 0 -1 -26 0 5 -.15 11 9 | 184 -192 10 158
| 0 0 3 6 8 23 .03 | 267 439
igr n/a| 0 0 -1 9 2 1 -.04 5 4 | 1663 0 10 69
| 0 0 1 11 14 5 .02 | 515 947
jpl 80| 0 0 4 23 11 9 .19 10 10 | 215228 -144 11 94
| 2 1 1 17 10 14 .02 | 643 1090
mit 349| 0 0 -3 23 -21 -16 -.06 13 12 | -286 -267 85 1687
| 0 0 1 23 26 5 .02 | 232 242
ngs 194| 0 0 1 -14 -27 9 -.06 11 11 | 174154 -142909 978 2156
| 0 0 3 25 21 11 .03 | 462155 377941
sio 255| 0 0 -8 13 3 -5 -.03 14 13 | --- --- --- ---
| 1 0 2 15 28 21 .02 | --- ---
Table 1.2029.b GPS week : 2029 MJD: 58447.000-58453.000
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 4 3 3 3 3 |
2 | 4 4 5 4 4 4 4 |
3 | 3 3 3 3 3 3 3 |
4 | 8 11 11 13 14 11 12 |
5 | 3 4 3 3 4 4 4 |
6 | 4 3 3 3 3 3 3 |
7 | 4 6 4 5 4 4 4 |
8 | 4 4 4 4 5 4 4 |
9 | 4 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 3 4 4 4 3 3 4 |
12 | 4 4 4 4 5 4 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 5 4 4 4 4 |
16 | 5 5 5 5 5 4 4 |
17 | 4 4 4 4 4 4 4 |
18 | --- --- --- 0 6 5 5 |
19 | 5 5 4 4 4 4 4 |
20 | 3 4 4 3 4 4 4 |
21 | 4 4 4 5 4 4 4 |
22 | 3 4 4 4 4 4 4 |
23 | 5 4 5 5 5 5 5 |
24 | 6 6 5 5 5 4 4 |
25 | 3 3 4 3 4 3 4 |
26 | 3 3 3 3 4 3 3 |
27 | 4 4 4 4 4 4 4 |
28 | 5 5 4 4 5 5 5 |
29 | 5 5 5 5 5 5 5 |
30 | 5 5 5 6 8 6 7 |
31 | 3 4 4 5 4 5 4 |
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 2.2029.0 GPS week: 2029 Day: 0 MJD: 58447.000
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 254| 0 2 0 3 38 7 -.04 10 10 | -479 -211 6 82
emr 79| 1 -4 7 -43 -3 12 .14 14 13 | 140630 1861 19 151
esa 150| 0 1 -1 -27 6 6 -.03 8 8 | -1245 1149 7 199
gfz 178| 1 0 0 8 11 -10 .11 9 9 | -117 531 11 121
grg 106| 0 0 -5 -30 -10 -34 -.18 10 9 | -99 380 9 159
igr n/a| 0 0 -4 9 -11 5 -.04 5 5 | 827 1934 12 70
jpl 80| -3 0 6 25 15 26 .21 10 10 | 214312 2003 11 106
mit 349| 1 0 -5 47 -10 -11 -.07 13 11 | -422 -60 115 1687
ngs 194| 0 0 6 2 -57 3 -.04 11 11 | -530 4 1022 1938
sio 291| 0 0 -6 39 12 -3 -.02 14 14 | --- --- --- ---
Table 2.2029.1 GPS week: 2029 Day: 1 MJD: 58448.000
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 257| -3 2 0 16 26 -7 -.02 10 9 | -380 -255 7 82
emr 80| 2 -3 3 -44 -6 8 .19 12 12 | 142184 -920 19 130
esa 150| 0 0 2 -8 10 -2 -.06 9 9 | -1695 -353 9 207
gfz 179| 0 0 0 -3 10 -19 .09 11 10 | -52 -332 10 136
grg 106| 0 0 -3 -17 -4 9 -.13 12 9 | 265 -441 9 183
igr n/a| -1 0 -1 7 11 -6 -.03 6 5 | 2343 -864 13 74
jpl 80| 3 0 1 32 13 29 .15 10 10 | 215891 -838 8 81
mit 349| 1 0 -3 -15 -39 -16 -.06 14 12 | 59 -479 71 1746
ngs 187| 0 0 4 14 1 -3 -.02 10 10 | -152 -730 806 2013
sio 294| 0 0 -7 11 -47 -4 -.07 13 13 | --- --- --- ---
Table 2.2029.2 GPS week: 2029 Day: 2 MJD: 58449.000
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 257| -2 0 0 20 58 4 -.05 11 10 | -608 66 8 99
emr 80| 1 -3 1 -27 6 6 .21 13 13 | 141183 247 20 126
esa 150| 0 1 3 1 0 3 -.03 9 8 | -1461 1063 9 196
gfz 178| 0 0 0 13 5 3 .14 10 10 | -563 493 11 100
grg 105| 1 0 -3 -35 -4 6 -.12 11 9 | -185 268 8 158
igr n/a| 0 0 0 23 22 0 -.01 4 4 | 1436 461 9 79
jpl 80| 0 0 2 41 -9 1 .20 10 10 | 215084 547 11 96
mit 349| 0 0 -4 3 -47 -25 -.05 14 12 | -303 -184 79 1547
ngs 194| -1 0 3 -30 -34 7 -.10 12 12 | -755 248 882 2243
sio 297| 0 0 -7 0 5 0 -.02 14 13 | --- --- --- ---
Table 2.2029.3 GPS week: 2029 Day: 3 MJD: 58450.000
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 256| -1 0 -2 15 -4 1 -.00 9 9 | -457 -416 6 79
emr 80| 0 -4 3 -53 1 -10 .18 13 13 | 141460 -479 18 131
esa 150| 0 1 2 -8 9 -10 -.08 9 8 | -814 421 8 210
gfz 181| 0 0 0 14 -9 -5 .06 10 12 | 85 -42 11 137
grg 107| 0 0 4 -25 -1 29 -.19 15 11 | 573 -840 10 161
igr n/a| 0 0 -1 1 -14 -1 -.05 4 4 | 1831 -128 10 63
jpl 80| 0 -2 2 19 9 -3 .20 9 9 | 215558 -144 8 88
mit 349| 1 0 -3 18 28 -10 -.09 13 12 | -126 -545 56 1863
ngs 194| 0 0 0 -21 -51 13 -.04 11 11 | -622 -160 1016 2407
sio 214| 0 0 -7 23 39 -9 -.03 14 13 | --- --- --- ---
Table 2.2029.4 GPS week: 2029 Day: 4 MJD: 58451.000
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 256| -1 0 -2 25 -12 -19 .00 9 9 | -490 -241 6 67
emr 80| 0 -4 5 -45 6 -12 .21 14 14 | 141361 -675 18 136
esa 150| 0 1 4 -26 25 -8 -.05 13 10 | -850 37 12 207
gfz 179| 0 0 0 23 1 9 .04 11 11 | 152 -430 12 112
grg 102| 0 -1 0 -30 15 34 -.12 11 10 | 389 -491 9 144
igr n/a| 0 0 -3 -5 0 1 -.03 4 4 | 1979 -444 12 66
jpl 80| 0 0 4 -12 7 -7 .19 10 10 | 215775 -702 10 89
mit 349| 1 0 -3 49 -24 -11 -.06 13 11 | -303 -530 162 1952
ngs 191| 0 1 2 14 -23 23 -.09 12 11 | 1222225 -999999 834 2378
sio 235| 0 0 -14 -3 -9 4 -.03 15 14 | --- --- --- ---
Table 2.2029.5 GPS week: 2029 Day: 5 MJD: 58452.000
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 253| -1 1 0 20 -22 5 .00 8 8 | -502 107 21 91
emr 80| 0 0 8 -27 -3 6 .20 13 13 | 141365 -1098 38 152
esa 150| 0 0 2 2 16 -13 -.07 8 8 | -871 807 21 201
gfz 176| 0 -3 -1 -5 1 -13 .04 10 9 | 93 -73 25 103
grg 104| 1 0 -1 -22 -6 7 -.13 10 9 | 254 20 20 150
igr n/a| -1 0 -1 25 -6 11 -.05 4 4 | 1969 -400 11 71
jpl 80| 0 0 4 35 18 2 .19 9 9 | 215567 -900 24 103
mit 349| 0 0 -3 35 -11 -18 -.06 13 12 | -225 15 50 1191
ngs 201| 0 0 -2 -48 -6 -2 -.04 11 11 | -520 162 1176 2139
sio 231| 1 0 -10 0 -4 21 -.04 15 14 | --- --- --- ---
Table 2.2029.6 GPS week: 2029 Day: 6 MJD: 58453.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| -2 0 -1 -1 -29 19 .01 10 10 | -582 169 6 81
emr 80| 1 0 8 -21 -9 33 .21 13 13 | 178859 -923 15 148
esa 150| -1 0 -1 -5 13 -2 -.07 10 9 | -1335 677 8 209
gfz 176| 0 -2 3 14 19 -16 .08 10 10 | -327 105 10 94
grg 105| 0 0 -1 -22 5 -11 -.16 9 8 | 94 -246 9 152
igr n/a| -1 0 -1 4 14 -2 -.06 4 4 | 1260 -563 9 65
jpl 80| 0 0 5 23 24 14 .17 10 10 | 214414 -974 9 96
mit 349| 0 1 -2 24 -43 -20 -.02 13 12 | -682 -87 67 1826
ngs 199| 0 1 -3 -34 -22 22 -.07 11 11 | -568 110 1114 1979
sio 229| 2 -1 -7 22 28 -48 .01 15 14 | --- --- --- ---
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 3.2029.0 GPS week: 2029 Day: 0 MJD: 58447.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 12 6 7 10 5 10 8 5 19 3 | 28 28 26 25 24 23 29 29 26 36 26
2 | 13 9 7 14 9 6 9 14 15 17 4 | 22 21 18 25 19 18 21 20 20 17 18
3 | 8 9 9 5 9 6 9 8 7 12 3 | 30 37 26 29 23 27 37 29 30 34 29
X4 | 7 --- --- --- --- 10 8 --- --- --- 7 | 32 --- --- --- --- 29 29 --- --- --- 29
5 | 6 8 9 5 7 4 11 12 11 11 3 | 30 29 25 30 27 24 34 26 26 28 27
6 | 9 9 7 19 13 4 8 9 10 14 4 | 23 28 22 29 23 20 27 22 24 32 23
7E | 13 12 6 10 13 5 10 14 9 11 3 | 167 165 165 165 165 163 166 164 162 164 165
8 | 5 15 7 10 8 3 10 10 10 13 3 | 22 26 21 24 21 19 25 23 21 27 21
9 | 14 8 11 8 10 4 8 9 4 10 3 | 23 27 22 20 21 20 29 21 20 24 21
10 | 8 11 10 5 8 4 11 9 6 7 3 | 23 34 20 26 24 24 33 27 23 30 25
11E | 9 10 8 10 11 5 9 10 9 9 3 | 16 25 17 22 19 17 22 17 20 18 17
12 | 13 20 6 7 10 5 10 15 12 13 4 | 29 29 24 28 24 24 29 23 25 23 24
13 | 7 13 12 7 9 7 14 12 12 14 4 | 30 38 27 35 31 34 37 34 35 36 32
14 | 5 7 8 10 8 6 8 18 12 18 3 | 26 29 26 30 31 30 29 36 32 29 27
15 | 9 12 9 7 9 7 13 16 15 18 4 | 52 57 53 51 47 44 56 40 41 41 48
16 | 10 24 8 9 11 9 10 13 12 20 4 | 22 19 17 21 21 20 19 22 22 19 17
17 | 10 15 5 9 14 6 13 17 11 13 4 | 29 28 25 29 27 25 31 27 29 24 26
19 | 13 16 7 6 16 8 10 19 12 15 4 | 35 32 29 30 33 28 29 27 26 27 28
20 | 7 9 8 7 4 5 6 13 10 13 3 | 35 39 38 38 37 38 32 39 35 40 36
21 | 9 12 5 9 10 6 12 15 11 16 3 | 15 18 17 17 18 14 20 19 20 16 14
22 | 5 8 8 6 7 5 10 11 10 17 3 | 21 22 19 21 18 20 21 22 20 24 19
23 | 9 25 10 7 10 8 9 16 13 23 4 | 30 22 25 30 25 32 27 37 33 30 27
X24E | 16 --- 16 11 21 6 18 11 19 13 6 | 49 --- 50 44 44 45 45 44 51 45 45
25 | 11 10 5 7 7 4 11 10 8 12 3 | 24 24 24 26 22 22 25 20 20 21 22
26 | 8 10 5 8 8 3 9 7 11 9 3 | 19 24 21 21 22 20 25 21 22 21 20
27 | 6 15 7 7 10 3 10 9 10 12 3 | 26 26 26 27 24 24 25 28 24 29 24
28 | 6 13 13 10 11 7 11 30 13 13 5 | 15 21 21 24 16 19 22 16 24 15 16
29 | 19 21 8 10 11 7 8 15 16 15 4 | 23 23 23 23 25 22 25 23 26 22 21
30E | 9 31 13 10 15 3 9 8 7 10 4 | 79 87 79 84 79 80 60 81 79 78 79
31E | 7 9 6 10 7 4 10 10 12 11 3 | 187 183 185 187 185 187 185 188 188 189 186
32 | 7 8 8 9 7 3 10 9 6 9 3 | 29 33 30 31 28 28 32 28 30 32 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 8 9 10 5 10 13 11 14 |T 38 40 37 39 37 36 39 38 38 39 36
WRMS | 10 13 8 9 9 5 10 11 11 14 |NE 26 28 25 27 25 24 28 26 26 27 24
MEDI | 9 12 8 8 10 5 10 11 11 13 |MD 28 28 25 28 24 24 29 27 26 28 26
Table 3.2029.1 GPS week: 2029 Day: 1 MJD: 58448.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 12 6 10 9 5 9 8 7 10 3 | 23 28 23 22 22 21 27 24 24 29 23
2 | 10 10 6 11 8 6 10 12 11 14 3 | 23 23 20 24 20 18 22 20 17 13 18
3 | 8 10 9 7 9 5 8 10 8 8 3 | 21 33 21 26 18 22 31 23 25 26 24
X4 | 10 --- --- --- --- 16 10 --- --- --- 10 | 30 --- --- --- --- 34 29 --- --- --- 28
5 | 7 6 7 5 7 5 11 13 14 14 3 | 21 24 21 23 20 22 26 26 24 27 22
6 | 7 8 7 10 7 5 10 7 6 10 3 | 25 29 25 22 25 23 29 26 25 32 25
7E | 20 10 7 12 34 9 9 16 13 13 6 | 123 118 118 120 117 117 121 118 118 117 118
8 | 8 14 7 12 8 5 10 10 6 8 3 | 21 27 20 21 19 20 20 20 20 23 19
9 | 9 8 12 10 8 3 8 8 4 8 3 | 24 28 22 22 23 21 28 23 22 23 23
10 | 7 10 10 6 6 4 9 11 5 9 3 | 24 36 24 27 24 25 31 29 22 31 26
11E | 9 11 11 14 11 6 8 11 7 8 3 | 20 21 17 24 15 18 20 18 18 16 16
12 | 9 17 5 8 9 5 8 18 11 13 3 | 23 27 22 27 23 23 27 26 24 20 23
13 | 8 13 11 8 9 7 12 12 13 13 4 | 21 29 14 22 18 22 28 22 21 23 19
14 | 8 8 8 11 8 6 6 17 11 17 3 | 16 22 15 20 21 21 21 25 22 22 18
15 | 9 10 9 8 8 6 11 16 13 18 4 | 38 45 44 43 39 38 46 38 38 37 40
16 | 11 22 10 10 9 7 9 16 12 20 4 | 19 19 20 23 19 19 18 20 22 19 17
17 | 11 14 7 9 11 5 10 18 11 14 4 | 35 35 29 33 33 30 33 34 34 31 32
19 | 14 16 5 11 15 8 8 20 15 14 4 | 33 30 27 31 31 25 28 24 24 26 27
20 | 9 9 7 9 6 5 9 15 9 15 3 | 38 41 39 41 36 41 37 42 37 41 38
21 | 11 9 6 11 11 6 11 16 12 15 4 | 19 22 18 22 17 18 19 20 18 16 16
22 | 6 9 10 9 7 5 6 13 11 17 3 | 20 23 19 24 16 19 21 20 21 20 18
23 | 10 20 10 7 8 8 7 15 12 16 4 | 24 20 17 25 19 26 23 26 29 22 21
24E | 13 13 18 13 28 7 21 13 13 15 6 | 35 45 42 38 36 37 45 37 35 37 36
25 | 8 8 6 8 8 2 9 11 6 11 3 | 32 35 30 34 31 31 34 32 28 29 31
26 | 7 9 7 8 8 3 9 11 10 9 3 | 21 24 24 21 23 20 23 21 23 21 21
27 | 10 14 8 8 10 4 12 10 5 11 3 | 24 25 23 23 20 21 22 22 21 23 21
28 | 7 13 13 12 8 5 8 28 13 10 4 | 17 23 21 25 18 18 23 20 20 15 17
29 | 13 20 8 11 11 7 10 16 13 15 4 | 27 27 25 31 24 25 25 25 27 25 25
30E | 17 11 13 27 15 5 11 10 10 8 5 | 61 61 57 65 58 59 45 63 58 60 59
31E | 7 9 8 10 10 7 7 12 10 12 3 | 117 117 116 115 118 118 119 119 122 122 118
32 | 9 8 10 9 7 3 6 11 6 12 3 | 31 36 34 35 31 33 34 33 33 36 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 9 11 12 6 10 14 10 13 |T 32 35 31 34 31 31 34 33 32 32 31
WRMS | 9 12 9 10 9 5 10 12 10 13 |NE 25 28 23 26 23 24 27 25 24 25 24
MEDI | 9 10 8 10 8 5 9 12 11 13 |MD 24 28 23 25 23 23 28 25 24 25 23
Table 3.2029.2 GPS week: 2029 Day: 2 MJD: 58449.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 13 5 8 10 4 10 7 9 16 3 | 27 32 27 27 25 25 28 26 26 32 26
2 | 22 9 6 10 8 4 11 14 16 14 4 | 27 20 20 22 20 19 19 20 21 17 18
3 | 9 9 9 7 9 3 9 9 9 7 3 | 27 36 27 34 25 27 35 28 27 30 28
X4 | 10 --- --- --- --- 10 11 --- --- --- 10 | 25 --- --- --- --- 25 24 --- --- --- 23
5 | 10 8 8 8 6 4 10 11 11 12 3 | 26 25 25 26 22 24 27 27 22 27 24
6 | 10 8 7 12 6 3 8 7 7 8 3 | 22 26 22 23 20 21 26 20 21 28 22
7E | 12 16 8 8 18 5 8 15 13 11 4 | 107 109 107 102 111 106 107 104 105 104 106
8 | 11 14 8 14 8 4 11 12 10 12 4 | 25 27 23 23 21 21 23 21 23 24 21
9 | 8 10 12 8 10 3 7 8 8 5 3 | 21 29 24 20 22 20 27 21 22 24 22
10 | 9 12 9 7 6 3 11 9 12 7 3 | 17 31 16 18 21 18 28 22 18 24 19
11E | 9 11 8 8 24 5 9 10 10 9 4 | 16 21 18 20 26 17 17 16 19 16 15
12 | 13 21 5 8 9 5 8 15 14 15 4 | 26 25 19 25 20 21 25 21 21 20 20
13 | 10 12 10 7 9 5 10 14 13 15 4 | 28 37 25 30 28 30 34 34 31 34 29
14 | 11 7 8 10 6 3 9 16 11 17 3 | 20 30 23 31 28 28 28 34 28 32 26
15 | 9 12 9 9 8 5 11 18 15 21 4 | 37 42 37 41 36 34 41 29 31 33 35
16 | 9 22 8 9 10 4 10 14 14 19 4 | 21 22 19 26 20 18 18 19 17 17 17
17 | 9 12 7 8 10 3 12 17 13 12 4 | 20 26 22 27 23 22 27 24 24 22 22
19 | 10 15 8 6 11 4 12 18 13 14 4 | 31 29 27 31 29 25 28 23 27 27 26
20 | 10 10 7 8 6 5 7 13 13 15 3 | 30 31 31 27 30 30 29 32 31 34 29
21 | 11 12 7 10 10 5 14 13 11 19 4 | 20 20 17 23 19 18 23 22 19 21 17
22 | 7 9 7 8 6 4 7 12 14 20 3 | 22 25 21 26 21 20 23 23 23 26 21
23 | 7 20 12 6 8 5 10 16 11 19 4 | 27 26 28 30 27 29 28 32 31 29 27
24E | 14 11 16 11 17 4 13 18 12 15 5 | 35 29 37 27 30 32 35 33 34 39 32
25 | 9 10 6 9 9 4 12 12 12 12 3 | 24 28 25 27 20 24 29 19 25 26 23
26 | 5 8 4 7 9 4 7 9 12 10 2 | 18 24 20 19 22 17 21 19 19 21 18
27 | 10 13 7 11 8 3 19 12 9 13 4 | 27 29 27 28 27 24 27 25 27 25 25
28 | 5 13 12 8 7 4 10 26 12 13 4 | 18 23 20 21 15 18 22 17 19 15 16
29 | 16 22 8 9 11 6 12 14 16 15 4 | 21 18 18 23 20 19 17 21 24 19 17
30E | 15 13 12 20 16 3 10 10 8 8 4 | 48 49 43 50 48 48 47 52 46 50 48
31E | 13 10 6 14 12 3 8 13 11 12 4 | 112 114 113 111 110 112 113 114 112 113 112
32 | 9 10 10 6 5 3 7 9 8 10 3 | 25 30 22 24 24 22 26 21 26 29 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 9 10 11 4 10 14 12 14 |T 30 33 30 32 30 29 32 30 30 31 29
WRMS | 10 13 8 10 9 4 10 12 12 13 |NE 24 27 23 26 23 23 26 24 24 25 22
MEDI | 10 12 8 8 9 4 10 13 12 13 |MD 25 28 23 26 23 24 27 23 24 26 23
Table 3.2029.3 GPS week: 2029 Day: 3 MJD: 58450.000
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 15 6 7 10 3 11 8 7 15 3 | 33 35 32 31 32 30 33 32 30 35 31
2 | 9 8 5 13 11 4 11 13 12 16 4 | 28 26 24 30 28 24 26 25 25 22 25
3 | 8 9 9 5 10 3 9 9 7 9 3 | 31 41 31 32 29 32 38 33 34 37 33
X4 | 12 --- --- --- --- 14 12 --- --- --- 12 | 37 --- --- --- --- 36 31 --- --- --- 32
5 | 6 7 9 6 9 4 8 12 12 13 3 | 30 32 31 31 33 29 35 31 30 32 31
6 | 8 11 6 11 7 3 8 5 7 9 3 | 30 32 30 31 30 28 34 29 30 32 30
7E | 10 9 6 7 35 6 7 13 14 14 5 | 74 71 71 75 86 70 71 70 68 71 72
8 | 13 12 9 11 10 2 12 9 8 15 4 | 30 32 28 26 30 27 30 28 28 33 27
9 | 5 8 11 8 8 3 7 7 6 8 2 | 30 32 27 28 28 28 33 26 30 31 29
10 | 5 10 8 6 6 3 8 13 8 6 2 | 34 39 29 34 30 30 37 32 33 34 32
11E | 8 9 13 8 13 5 9 9 5 11 3 | 28 26 26 26 31 24 29 24 26 26 25
12 | 9 18 5 10 11 4 10 15 12 15 4 | 31 33 28 33 29 30 33 28 28 30 29
13 | 8 10 10 9 12 4 11 15 12 16 4 | 32 36 28 30 28 32 36 36 37 38 32
14 | 7 7 8 8 8 4 7 16 14 17 3 | 26 31 22 26 26 28 29 33 36 30 27
15 | 8 8 9 9 8 4 9 17 13 20 4 | 48 52 50 50 49 43 52 39 39 44 47
16 | 12 23 6 11 11 5 8 15 13 17 4 | 27 28 26 28 29 26 27 26 27 25 25
17 | 8 16 6 9 11 3 10 16 14 14 4 | 31 34 31 33 34 32 36 37 40 35 33
X18 | 2 --- --- --- --- >>>> --- --- --- --- 0 | 9999 --- --- --- --- 847 --- --- --- --- 9999
19 | 11 18 7 7 12 6 9 17 13 16 4 | 31 32 27 32 32 28 28 31 29 31 29
20 | 6 8 7 7 9 2 7 15 10 15 3 | 27 27 28 29 28 27 25 27 30 27 26
21 | 12 10 6 7 30 4 14 15 11 17 5 | 29 29 30 28 39 27 31 28 28 26 27
22 | 8 9 8 9 9 3 5 15 10 17 3 | 28 32 28 32 27 28 27 32 27 33 28
23 | 6 21 10 10 8 4 7 16 16 18 4 | 35 31 31 36 31 36 36 37 42 35 34
24E | 9 9 15 13 25 5 10 10 7 9 4 | 32 27 35 28 34 31 34 30 30 37 31
25 | 9 9 5 8 12 3 9 10 7 12 3 | 33 35 32 34 32 33 35 31 31 32 32
26 | 10 11 4 9 9 3 9 8 8 11 3 | 29 33 27 26 27 26 29 26 28 30 27
27 | 12 12 8 8 10 3 10 11 8 12 3 | 29 32 29 26 32 27 30 28 28 29 28
28 | 6 15 11 8 9 4 8 26 8 12 4 | 23 30 28 29 27 25 31 26 27 26 25
29 | 13 21 6 10 14 6 8 16 15 18 4 | 35 31 32 35 33 31 32 33 33 31 32
30E | 14 9 15 29 15 4 9 10 15 12 5 | 71 72 66 78 72 71 52 72 70 72 70
31E | 9 11 8 13 33 7 7 12 15 16 5 | 95 90 90 93 103 91 90 94 92 91 92
32 | 5 9 10 10 6 2 6 9 7 10 3 | 27 33 26 23 29 25 30 25 28 33 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 10 15 4 9 13 11 14 |T 35 37 34 35 36 59 36 34 35 36 34
WRMS | 9 13 8 11 11 4 9 12 11 13 |NE 30 33 29 30 30 59 32 30 31 31 29
MEDI | 8 10 8 9 10 4 9 13 10 14 |MD 31 32 29 31 30 29 33 31 30 32 30
Table 3.2029.4 GPS week: 2029 Day: 4 MJD: 58451.000
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 6 8 9 5 11 9 12 7 3 | 26 30 27 25 25 25 30 26 26 25 25
2 | 9 13 5 12 8 3 11 12 13 17 4 | 24 21 21 23 20 19 20 20 19 16 18
3 | 8 10 8 7 8 3 11 8 9 9 3 | 27 36 27 24 23 24 34 25 21 28 26
X4 | 11 --- --- --- --- 9 15 --- --- --- 13 | 30 --- --- --- --- 28 29 --- --- --- 27
5 | 8 7 9 7 8 4 8 14 12 16 3 | 23 27 22 21 23 21 30 27 24 29 23
6 | 7 8 5 15 8 4 8 6 8 10 3 | 22 23 22 23 20 19 23 19 21 21 20
7E | 7 22 6 11 11 4 12 11 11 11 4 | 105 109 108 107 104 107 109 107 104 106 106
8 | 9 13 10 20 11 2 12 10 7 17 4 | 24 27 24 24 23 21 25 23 24 29 22
9 | 10 7 12 8 9 4 8 6 7 10 3 | 34 38 34 33 30 33 38 32 34 36 33
10 | 8 10 10 7 7 3 9 11 8 11 3 | 19 30 18 21 19 19 29 23 17 29 20
11E | 5 9 8 7 11 4 11 7 9 12 3 | 15 16 16 17 20 15 18 12 14 17 13
12 | 11 19 8 10 10 5 7 16 13 17 4 | 23 25 19 25 20 19 24 19 21 20 19
13 | 9 11 11 6 11 4 12 14 14 16 4 | 28 37 26 29 29 31 36 34 35 39 30
14 | 7 6 8 10 8 3 9 16 13 18 3 | 25 29 23 29 27 28 28 33 30 31 26
15 | 9 12 12 6 9 3 10 16 14 20 4 | 38 43 41 34 37 33 40 29 29 29 35
16 | 12 26 9 8 12 5 11 13 13 21 5 | 24 24 22 24 25 20 21 21 22 22 20
17 | 6 13 9 12 10 3 11 14 12 12 4 | 20 21 18 26 21 18 24 21 20 23 19
X18 | 13 12 --- 14 --- 11 12 20 12 --- 6 | 9999 30 --- 23 --- 451 30 23 24 --- 9999
19 | 8 17 8 9 12 6 7 15 12 15 4 | 30 31 28 31 31 28 29 23 28 29 27
20 | 7 11 9 8 9 3 6 13 10 15 3 | 24 29 27 25 28 26 27 29 29 31 26
21 | 9 14 9 9 10 5 16 13 8 16 4 | 21 23 21 20 20 18 25 21 18 17 18
22 | 6 7 8 11 9 4 8 14 13 21 4 | 21 23 21 18 19 17 21 21 15 25 18
23 | 9 24 11 8 6 6 10 14 12 23 4 | 29 26 23 26 25 28 28 28 28 32 25
24E | 8 8 16 15 21 5 10 9 7 10 4 | 24 23 29 20 24 24 27 24 26 30 24
25 | 11 12 6 9 10 4 10 10 7 13 3 | 19 21 19 22 17 17 22 17 17 20 17
26 | 11 11 6 9 9 3 12 7 9 12 3 | 22 26 21 18 23 20 26 20 18 23 20
27 | 10 11 8 14 9 3 12 9 11 15 4 | 33 33 31 30 29 29 29 30 33 30 29
28 | 9 16 15 10 8 5 11 25 11 10 4 | 15 23 21 20 16 18 23 17 20 19 15
29 | 13 22 8 8 11 6 11 18 15 17 4 | 22 18 19 23 20 18 21 23 26 17 19
30E | 9 12 51 16 20 5 12 11 23 11 8 | 58 62 85 62 59 57 82 59 49 64 58
31E | 9 11 7 14 14 7 11 14 14 16 4 | 137 134 132 134 137 132 130 133 136 132 134
32 | 8 10 11 9 6 3 8 9 9 11 3 | 23 28 25 21 22 22 26 19 24 27 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 13 11 11 4 10 13 12 15 |T 31 34 32 31 31 43 34 30 30 33 30
WRMS | 9 14 10 11 10 4 10 11 11 14 |NE 24 27 24 24 23 38 27 23 23 25 23
MEDI | 9 12 8 9 9 4 11 13 12 15 |MD 24 27 23 24 23 22 27 23 24 28 23
Table 3.2029.5 GPS week: 2029 Day: 5 MJD: 58452.000
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 9 11 4 10 7 8 13 3 | 31 32 34 34 31 29 30 34 34 34 31
2 | 9 14 5 11 8 4 9 13 11 14 3 | 26 25 21 26 24 23 23 24 26 20 22
3 | 7 10 9 8 7 4 9 7 7 10 3 | 33 39 32 32 30 31 39 34 37 37 34
X4 | 9 --- --- --- --- 14 11 --- --- --- 10 | 26 --- --- --- --- 26 28 --- --- --- 25
5 | 6 9 9 8 7 4 8 14 12 16 3 | 23 23 20 22 21 20 26 26 22 26 22
6 | 7 9 8 8 8 4 9 8 9 10 3 | 25 26 24 24 22 23 26 22 25 26 23
7E | 8 14 7 8 9 3 10 10 12 10 3 | 108 107 109 108 109 108 111 107 106 108 108
8 | 5 14 8 15 8 5 10 9 10 14 3 | 26 27 25 29 24 23 28 25 27 29 25
9 | 8 7 10 6 7 3 6 6 9 9 2 | 23 30 25 23 23 24 27 23 25 28 24
10 | 9 12 11 9 5 3 10 8 7 9 3 | 20 31 17 19 21 20 32 21 22 26 22
11E | 7 9 9 6 10 4 7 8 10 11 3 | 18 19 21 22 19 17 20 18 20 17 18
12 | 10 20 8 8 10 4 8 17 11 18 4 | 23 24 20 25 21 21 25 22 24 23 21
13 | 5 12 9 9 9 3 10 15 13 13 3 | 37 43 35 38 37 37 42 40 40 39 38
14 | 9 7 8 11 8 4 7 16 14 17 3 | 26 28 25 29 30 29 32 35 37 33 29
15 | 7 9 8 10 7 4 8 18 12 24 4 | 39 42 34 36 33 32 39 28 31 33 34
16 | 7 18 6 9 8 5 10 13 13 18 4 | 24 23 23 26 27 24 25 25 27 18 23
17 | 8 12 6 10 11 4 7 14 11 12 3 | 21 22 23 29 21 23 25 25 30 24 23
X18 | 17 13 13 17 11 5 8 10 13 --- 5 | 9999 22 20 21 15 372 20 24 21 --- 9999
19 | 11 13 6 9 11 6 7 15 10 13 3 | 33 29 28 33 30 29 29 26 30 30 29
20 | 9 10 8 9 7 3 6 12 12 15 3 | 26 29 27 30 26 26 28 28 28 27 26
21 | 10 13 6 9 11 4 8 12 12 16 3 | 24 26 25 26 27 24 24 25 27 19 23
22 | 6 8 7 8 8 4 6 15 10 24 3 | 25 23 24 24 21 22 23 28 28 34 23
23 | 9 20 9 11 7 7 9 15 13 20 4 | 37 34 36 37 34 36 35 38 39 37 35
24E | 10 11 13 8 19 6 9 11 6 13 4 | 21 19 26 20 18 20 22 22 20 25 20
25 | 9 10 6 7 7 4 8 11 6 10 3 | 23 27 25 27 25 24 27 24 26 22 24
26 | 9 10 4 10 8 3 8 7 8 10 3 | 21 25 22 22 22 19 24 20 21 23 21
27 | 7 13 7 12 7 4 10 10 12 15 3 | 27 29 28 30 27 26 29 27 27 28 27
28 | 8 13 10 11 10 6 8 27 12 10 4 | 21 24 20 26 20 23 24 23 28 21 21
29 | 15 21 7 15 9 5 9 19 16 19 5 | 30 26 28 31 30 28 27 28 29 24 27
X30E | 17 23 9 14 13 7 --- 10 23 15 6 | 109 111 108 104 104 105 --- 107 107 107 105
31E | 10 13 8 11 19 4 12 14 8 15 4 | 160 159 159 161 165 160 161 161 161 160 160
32 | 8 9 10 9 6 3 7 8 8 13 3 | 24 27 21 22 22 21 26 22 25 27 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 8 10 10 4 9 13 11 15 |T 35 37 35 36 34 45 34 35 37 36 35
WRMS | 8 13 8 9 9 4 9 12 11 13 |NE 26 28 25 27 25 38 28 26 28 27 25
MEDI | 8 12 8 9 8 4 8 12 11 13 |MD 26 27 25 27 25 24 27 25 27 27 24
Table 3.2029.6 GPS week: 2029 Day: 6 MJD: 58453.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 12 6 7 9 4 9 8 7 17 3 | 30 33 30 29 28 28 31 33 29 41 30
2 | 12 11 7 13 10 4 11 15 14 15 4 | 26 23 19 26 21 19 21 20 22 18 19
3 | 8 9 10 4 6 3 10 7 7 9 2 | 32 40 30 34 29 32 40 34 33 38 33
X4 | 11 --- --- --- --- 13 12 --- --- --- 11 | 34 --- --- --- --- 30 31 --- --- --- 30
5 | 7 11 10 9 5 5 10 13 13 16 3 | 26 29 28 28 25 23 32 27 24 28 26
6 | 8 8 8 15 6 4 7 9 9 10 3 | 22 25 22 28 19 20 24 19 19 29 21
7E | 9 14 7 9 8 3 9 14 8 11 3 | 153 154 151 151 152 152 151 152 153 153 152
8 | 9 12 7 13 6 2 9 11 10 16 3 | 23 27 24 24 23 21 25 22 27 27 22
9 | 7 7 10 6 5 3 6 5 5 8 2 | 22 25 20 20 19 19 25 22 19 23 20
10 | 10 9 9 7 5 2 11 8 5 8 3 | 23 31 20 25 22 23 32 27 26 30 24
11E | 10 10 8 11 8 4 11 11 10 11 3 | 19 19 19 21 21 17 18 17 23 18 17
12 | 18 17 7 9 7 4 8 19 15 19 4 | 31 27 24 28 23 23 27 20 23 24 23
13 | 10 11 9 10 8 4 12 15 13 14 4 | 35 42 32 39 37 37 38 41 42 44 37
14 | 7 8 8 10 7 4 6 15 13 18 3 | 30 31 29 30 31 31 32 38 38 37 31
15 | 7 10 9 8 6 4 11 16 11 21 4 | 48 54 48 46 44 42 54 37 38 35 45
16 | 10 23 7 8 9 3 10 11 10 16 4 | 24 22 22 23 25 22 21 26 26 22 21
17 | 7 10 6 10 10 4 10 14 13 12 3 | 21 21 20 25 18 21 22 26 29 24 21
X18 | 11 10 10 11 10 7 15 12 12 --- 4 | 9999 25 20 24 14 318 24 24 26 --- 9999
19 | 11 14 6 8 10 4 8 16 11 14 3 | 34 31 28 30 30 29 29 26 29 26 29
20 | 9 8 9 9 7 3 6 12 11 18 3 | 35 38 37 36 35 37 35 42 38 42 36
21 | 7 13 8 8 12 3 13 12 11 16 4 | 18 24 19 19 21 18 24 21 21 17 18
22 | 9 9 10 6 5 4 5 15 9 21 3 | 21 23 20 22 19 20 23 27 21 32 20
23 | 7 21 9 11 6 6 8 14 13 23 4 | 32 29 31 37 33 34 33 36 38 41 33
24E | 12 9 15 11 13 4 9 12 10 12 4 | 40 29 44 39 33 38 41 38 40 39 38
25 | 16 12 7 10 6 3 8 14 8 11 3 | 28 22 25 28 20 22 23 24 20 24 23
26 | 9 11 4 6 5 2 8 6 10 12 2 | 20 23 21 19 23 20 23 19 24 22 20
27 | 11 14 7 11 6 3 10 11 8 17 3 | 26 29 28 25 27 24 27 26 27 27 25
28 | 10 14 11 8 8 5 10 25 11 11 4 | 16 23 21 22 17 18 22 19 22 16 16
29 | 16 21 7 10 9 5 12 20 16 19 5 | 33 26 30 33 29 30 26 33 31 28 29
30E | 14 26 31 19 22 7 15 17 10 16 7 | 111 112 122 110 103 108 98 107 111 103 109
31E | 8 12 7 12 15 3 11 10 6 13 3 | 204 202 202 202 206 202 203 203 201 207 203
32 | 7 8 10 8 5 3 8 7 6 11 2 | 23 29 23 22 21 22 26 20 22 26 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 10 10 9 4 10 13 11 15 |T 40 40 39 40 37 46 40 39 40 41 38
WRMS | 10 13 9 10 8 4 10 12 11 14 |NE 27 28 25 27 25 36 28 27 27 28 25
MEDI | 9 11 8 9 7 4 10 12 10 14 |MD 28 29 25 28 25 23 27 26 27 28 25
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 4.2029 GPS week: 2029 MJD: 58447.0-58453.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3019 |U 11 13 19 |U 12 15 48 |U 12 13 35 |
emr | emr 2907 |U 17 22 40 |U 17 23 60 |U 22 21 48 |
esa | esa 2907 | 11 14 26 |U 12 17 48 | 13 14 34 |
gfz | gfz 2921 |U 12 15 23 |U 11 15 48 |U 12 15 42 |
grg | grg 2906 |U 11 15 23 |U 12 17 51 | 13 12 35 |
igr | igr 2918 | 11 16 20 | 12 16 48 | 12 13 36 |
igs | igs 2989 | 11 16 23 | 12 16 47 | 13 13 35 |
jpl | jpl 3003 |U 17 25 34 |U 14 15 52 |U 20 20 48 |
mit | mit 2921 | 27 25 50 |U 21 27 78 |U 23 21 68 |
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 5.2029.0 GPS week: 2029 Day: 0 MJD: 58447.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 16 14 20 | 17 15 49 | 13 10 39 |
emr | emr 2784 | 25 31 47 | 24 22 70 | 26 20 47 |
esa | esa 2880 | 17 14 32 | 16 16 45 | 15 13 38 |
gfz | gfz 2880 | 16 16 28 | 15 16 50 | 12 14 43 |
grg | grg 2880 | 10 17 26 | 17 18 53 | 16 18 40 |
igr | igr 2878 | 16 15 25 | 16 15 46 | 13 14 44 |
igs | igs 2878 | 17 15 29 | 17 16 45 | 16 16 44 |
jpl | jpl 2976 | 23 26 43 | 19 16 53 | 21 20 51 |
mit | mit 2880 | 18 19 31 | 27 24 78 | 28 28 69 |
Table 5.2029.1 GPS week: 2029 Day: 1 MJD: 58448.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 7 13 16 | 9 12 35 | 11 11 32 |
emr | emr 2880 | 13 18 33 | 15 17 47 | 28 20 44 |
esa | esa 2880 | 8 13 24 | 10 14 35 | 12 12 27 |
gfz | gfz 2880 | 9 14 22 | 9 13 41 | 10 16 37 |
grg | grg 2880 | 10 15 21 | 9 15 38 | 13 9 34 |
igr | igr 2880 | 8 14 17 | 9 13 36 | 9 11 28 |
igs | igs 2975 | 9 16 21 | 10 13 35 | 12 11 30 |
jpl | jpl 2976 | 15 25 34 | 11 13 46 | 18 19 42 |
mit | mit 2880 | 11 14 26 | 16 23 106 | 12 10 38 |
Table 5.2029.2 GPS week: 2029 Day: 2 MJD: 58449.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 11 14 | 12 11 46 | 13 18 35 |
emr | emr 2880 | 16 19 40 | 19 20 51 | 18 16 44 |
esa | esa 2880 | 9 12 24 | 12 14 44 | 13 17 35 |
gfz | gfz 2880 | 9 12 21 | 11 14 46 | 12 18 40 |
grg | grg 2880 | 9 13 20 | 13 15 47 | 11 16 33 |
igr | igr 2880 | 8 13 16 | 12 12 45 | 12 15 35 |
igs | igs 2976 | 9 14 19 | 13 12 43 | 12 16 35 |
jpl | jpl 2976 | 14 22 29 | 12 13 53 | 18 17 47 |
mit | mit 2880 | 34 21 35 | 21 22 65 | 16 23 44 |
Table 5.2029.3 GPS week: 2029 Day: 3 MJD: 58450.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2993 | 9 11 20 | 16 33 86 | 12 15 29 |
emr | emr 2880 | 16 15 43 | 18 34 92 | 26 17 38 |
esa | esa 2880 | 9 13 28 | 13 36 97 | 14 15 28 |
gfz | gfz 2880 | 10 12 23 | 14 30 86 | 11 13 32 |
grg | grg 2880 | 12 15 19 | 16 35 95 | 15 8 25 |
igr | igr 2880 | 9 13 21 | 14 35 98 | 12 12 28 |
igs | igs 2932 | 10 13 23 | 15 37 99 | 14 13 29 |
jpl | jpl 2976 | 15 21 31 | 17 18 87 | 20 17 38 |
mit | mit 2880 | 18 20 38 | 16 36 101 | 22 8 30 |
Table 5.2029.4 GPS week: 2029 Day: 4 MJD: 58451.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 11 22 | 10 10 39 | 13 10 31 |
emr | emr 2976 | 11 14 37 | 14 21 49 | 19 22 50 |
esa | esa 2880 | 11 13 27 | 11 13 37 | 14 12 32 |
gfz | gfz 2976 | 11 12 24 | 9 10 35 | 10 8 32 |
grg | grg 2878 | 10 13 26 | 12 10 39 | 14 10 34 |
igr | igr 2973 | 10 13 23 | 11 12 33 | 13 10 32 |
igs | igs 3055 | 9 13 24 | 11 10 35 | 15 12 34 |
jpl | jpl 3072 | 16 20 30 | 13 16 41 | 26 22 49 |
mit | mit 2976 | 80 61 179 | 33 41 93 | 55 50 209 |
Table 5.2029.5 GPS week: 2029 Day: 5 MJD: 58452.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 9 16 21 | 10 14 43 | 12 13 28 |
emr | emr 2976 | 13 33 43 | 17 24 63 | 19 27 46 |
esa | esa 2976 | 9 18 22 | 11 11 45 | 14 12 29 |
gfz | gfz 2976 | 9 18 20 | 9 10 43 | 11 10 31 |
grg | grg 2971 | 9 17 27 | 10 15 48 | 13 11 31 |
igr | igr 2967 | 9 19 18 | 10 11 43 | 12 12 29 |
igs | igs 3068 | 9 19 23 | 9 13 40 | 14 14 26 |
jpl | jpl 2976 | 13 26 29 | 12 12 44 | 19 19 38 |
mit | mit 2976 | 9 18 23 | 13 15 54 | 14 10 34 |
Table 5.2029.6 GPS week: 2029 Day: 6 MJD: 58453.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 17 18 21 | 10 13 35 | 12 15 50 |
emr | emr 2976 | 23 25 38 | 12 23 46 | 18 26 70 |
esa | esa 2976 | 13 16 26 | 11 14 34 | 13 17 51 |
gfz | gfz 2976 | 18 20 21 | 10 12 35 | 14 25 75 |
grg | grg 2976 | 16 19 26 | 11 12 36 | 10 16 45 |
igr | igr 2968 | 19 22 23 | 10 14 33 | 11 15 53 |
igs | igs 3044 | 16 21 23 | 11 13 34 | 12 14 50 |
jpl | jpl 3072 | 26 36 39 | 13 17 42 | 16 23 69 |
mit | mit 2976 | 24 20 19 | 23 31 52 | 16 17 53 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.2029 GPS week: 2029 MJD: 58447.500-58453.500
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 -10 -9 -44 -1 | 9 24
| 25 16 61 120 8 | 4
emr uuuuu | 0 43 95 -46 0 | 34 40
| 11 19 95 54 11 | 5
esa uuuuu | -21 21 -156 -59 -1 | 22 31
| 10 16 69 70 3 | 4
gfz uuuuu | -11 -9 9 -96 -1 | 19 29
| 12 22 76 94 4 | 4
grg uuuuu | 23 30 -1 157 3 | 0 19
| 27 16 30 39 6 | 1
igr xxxxx | -20 -13 -26 -38 -1 | -3 21
| 9 11 59 48 4 | 4
irf xxxxx | -1 -25 16 39 -2 | 2 21
| 10 13 29 26 3 | 3
jpl uuuuu | -29 -39 58 -48 -4 | 32 40
| 18 16 66 109 12 | 4
mit uuuuu | 19 -40 10 95 0 | 19 28
| 11 14 68 39 7 | 2
ngs uuuuu | 63 4 139 -5 -4 | 14 26
| 19 39 171 97 8 | 5
sio uuuux | -27 7 -125 142 5 | 41 45
| 18 25 58 83 7 | 3
Table 7.2029.0 GPS week: 2029 Day: 0 MJD: 58447.500
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 | -38 15 -62 -93 -14 | 17 25
emr uuuuu | -5 46 260 43 -20 | 42 45
esa uuuuu | -36 33 -103 -110 0 | 28 34
gfz uuuuu | -33 4 6 -128 5 | 25 32
grg uuuuu | 33 2 -29 108 6 | 1 18
igr xxxxx | -15 -7 64 -105 -5 | 3 19
irf xxxxx | 10 -22 10 70 -1 | 7 20
jpl uuuuu | 0 -55 6 166 14 | 37 43
mit uuuuu | 15 -24 37 146 10 | 22 28
ngs uuuuu | 90 -32 121 -73 -9 | 21 28
sio uuuux | -3 13 -127 102 1 | 47 50
Table 7.2029.1 GPS week: 2029 Day: 1 MJD: 58448.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -18 -9 -24 121 -6 | 14 23
emr uuuuu | -1 76 33 -106 -9 | 38 43
esa uuuuu | -17 13 -118 -138 -4 | 26 33
gfz uuuuu | -23 22 -98 -84 -6 | 24 31
grg uuuuu | 68 28 -54 214 10 | 1 18
igr xxxxx | -21 -8 -26 -15 -1 | 1 19
irf xxxxx | 8 -29 -2 15 -4 | 5 19
jpl uuuuu | -36 -41 -11 -129 -22 | 37 43
mit uuuuu | 18 -28 16 96 3 | 21 28
ngs uuuuu | 47 -53 376 -47 0 | 19 27
sio uuuux | -26 14 -138 186 -4 | 44 47
Table 7.2029.2 GPS week: 2029 Day: 2 MJD: 58449.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -40 -16 -89 113 -7 | 9 23
emr uuuuu | -20 49 -3 -108 3 | 34 40
esa uuuuu | -15 12 -159 -76 -1 | 22 31
gfz uuuuu | -1 0 -27 19 2 | 20 29
grg uuuuu | 41 41 3 149 7 | -1 18
igr xxxxx | -30 -18 -127 -71 1 | -3 20
irf xxxxx | 4 -36 49 3 3 | 2 21
jpl uuuuu | -21 -35 36 -94 -5 | 32 40
mit uuuuu | 8 -50 89 23 7 | 19 27
ngs uuuuu | 89 4 320 -152 -13 | 16 26
sio uuuux | -42 -17 -65 118 11 | 40 44
Table 7.2029.3 GPS week: 2029 Day: 3 MJD: 58450.500
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 -5 13 -116 2 | 7 24
emr uuuuu | 8 46 24 -69 10 | 32 39
esa uuuuu | -23 23 -236 -51 -5 | 20 31
gfz uuuuu | -9 6 -53 -283 -4 | 18 28
grg uuuuu | -6 32 12 203 1 | -1 19
igr xxxxx | -7 -8 9 -10 4 | -5 22
irf xxxxx | -3 -34 55 48 -1 | 1 22
jpl uuuuu | -15 -46 121 3 4 | 30 40
mit uuuuu | 43 -60 72 104 -2 | 19 27
ngs uuuuu | 52 29 209 143 -2 | 13 27
sio uuuux | -18 -17 -123 282 3 | 40 44
Table 7.2029.4 GPS week: 2029 Day: 4 MJD: 58451.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 17 -35 -2 -68 8 | 7 23
emr uuuuu | 14 46 49 -47 4 | 32 39
esa uuuuu | -33 50 -268 -52 4 | 19 29
gfz uuuuu | 0 -24 85 -80 -7 | 18 28
grg uuuuu | -10 45 10 153 5 | -1 19
igr xxxxx | -30 -4 -4 -71 2 | -5 22
irf xxxxx | -20 0 25 22 -2 | 1 22
jpl uuuuu | -31 -5 117 -106 -4 | 30 40
mit uuuuu | 14 -52 10 72 -3 | 19 28
ngs uuuuu | 51 -9 52 53 -13 | 12 26
sio uuuux | -24 -12 -41 157 -2 | 40 44
Table 7.2029.5 GPS week: 2029 Day: 5 MJD: 58452.500
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 -23 100 -65 1 | 8 24
emr uuuuu | -1 23 154 -22 1 | 30 37
esa uuuuu | -21 7 -107 -73 0 | 20 30
gfz uuuuu | -5 -30 115 -80 -1 | 16 27
grg uuuuu | 25 45 15 130 1 | 1 20
igr xxxxx | -13 -35 -42 -35 -7 | -4 22
irf xxxxx | -5 -22 -23 58 -5 | 1 22
jpl uuuuu | -49 -46 -5 -27 1 | 29 39
mit uuuuu | 21 -36 -108 121 -8 | 19 28
ngs uuuuu | 61 59 -33 -14 3 | 11 25
sio uuuux | -19 16 -173 139 10 | 40 44
Table 7.2029.6 GPS week: 2029 Day: 6 MJD: 58453.500
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 | 23 1 1 -203 9 | 4 24
emr uuuuu | 1 16 146 -12 8 | 27 35
esa uuuuu | -6 9 -99 83 2 | 17 29
gfz uuuuu | -7 -38 37 -38 0 | 13 26
grg uuuuu | 12 19 35 138 -7 | -1 21
igr xxxxx | -22 -9 -53 40 -2 | -8 24
irf xxxxx | 1 -35 -3 58 -3 | -2 24
jpl uuuuu | -51 -45 139 -147 -15 | 26 38
mit uuuuu | 13 -31 -46 103 -4 | 16 27
ngs uuuuu | 50 27 -70 52 5 | 7 24
sio uuuux | -58 54 -210 9 14 | 38 42
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