[IGSREPORT-26454] Wk 2042 IGS Final Orbits
acc
acc at igs.org
Thu Mar 14 22:52:36 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2042 (Feb 24, 2019 - Mar 02, 2019)
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:
igs2042[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2042[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2042[0-6].cls IGS GPS clock combination summary report.
igs20427.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20427.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 | BRMU LMMF MAR6 NAUR TIXI BRMU LMMF MAR6 NAUR TIXI
0 | EMR | BJNM TLSE BJNM TLSE
0 | GFZ | ALRT GODE POHN ALRT GODE POHN
0 | GRG | 18 18 DARW GLSV KRGG LHAZ NRMD GLSV KRGG LHAZ STJO
0 | MIT | HARB MAJU MBAR MDO1 PADO PIE1 HARB MAJU MBAR MDO1
0 | MIT | PADO PIE1
1 | COD | 18 18 MAR6 SEYG SOFI TIXI TLSE LHAZ MAR6 SOFI TIXI
1 | COD | TLSE
1 | EMR | BJNM
1 | ESA | 18 18 MGUE REUN SEYG MGUE REUN SEYG TLSE
1 | GFZ | ABMF BJNM GODE POHN ABMF GLPS GODE GUAT MAL2 POHN
1 | GRG | GLSV LHAZ MAL2 RABT GLSV LHAZ RABT TLSE
1 | JPL | SEYG
1 | MIT | PALM BJNM PALM WAB2
2 | COD | 18 18 BOR1 BRMU MAR6 MDO1 TASH TIXI TLSE BRMU MAR6
2 | COD | MDO1 TIXI TLSE
2 | EMR | AREQ CEDU GOL2 HARB HOB2 IENG JOZE KERG KIRU KOKB
2 | EMR | MAS1 MATE NIST NNOR NYAL ONSA OPMT PERT PIE1 PTBB
2 | EMR | SUWN THTI TIDB TLSE TSKB TWTF VILL
2 | ESA | 18 18 BRMU MAL2 TLSE ANKR BRMU MAL2
2 | GFZ | ABMF BJNM GODE POHN USN7 ABMF BJNM BOR1 GODE POHN
2 | GFZ | TASH USN7
2 | GRG | GLSV TLSE
2 | JPL | 21 LAUT
3 | COD | BOR1 PBRI TIXI YAR2 BOR1 PBRI TIXI
3 | EMR | PIE1
3 | ESA | 18 18
3 | GFZ | BJNM GODE PIE1 POHN BJNM GODE PIE1 POHN
3 | GRG | ABMF ADIS GLSV ADIS GLSV
3 | JPL | BRMU
3 | MIT | PALM PALM
4 | COD | BRMU NIST TIXI WES2 BRMU NIST TIXI WES2
4 | EMR | YELL FAIR YELL
4 | ESA | TRO1 TRO1
4 | GFZ | GODE POHN ANKR AUCK CHTI GODE MDVJ NYA1 POHN
4 | GRG | CHTI GLSV KRGG GLSV
4 | MIT | PALM ANKR NNOR PALM REYK SYOG
5 | COD | KRGG NAUR TLSE CRO1 KRGG LHAZ NAUR
5 | EMR | KERG
5 | ESA | BRMU TLSE BRMU
5 | GFZ | GODE POHN GODE POHN
5 | GRG | ABMF ADIS GLSV LHAZ ABMF ADIS GLSV LHAZ
5 | JPL | INVK MCM4
6 | COD | 18 ANKR NAUR NRMD TIXI ANKR NAUR NRMD TIXI
6 | EMR | PRDS
6 | GFZ | GODE POHN STJO GODE POHN STJO
6 | GRG | ABMF BAKE GLSV KRGG NNOR ABMF GLSV NNOR
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
2 | EMR | ~14:35 | ~ 1.56 ns
2 | GRG | ~01:30 | ~ 0.10 ns
6. 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.
7. 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 | ESA | 18
2 | GRG | 4
3 | ESA | 18
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.
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 | -.5 -.6 -.8 -11 5 1 .15
EMR | 0 | 3.8 -7.0 7.5 1 33 -46 .47
ESA | 0 | 1.0 .4 1.6 -16 14 50 .11
GFZ | 0 | .2 -.5 -.4 -19 -16 1 .27
GRG | 0 | 8.1 -3.4 21.8 27 7 89 .17
JPL | 0 | 10.7 -1.7 8.8 1 -1 2 .10
MIT | 0 | 5.3 -.9 2.7 -20 24 -14 .39
NGS | 0 | .5 -6.3 8.3 -31 -14 -8 .39
SIO | 0 | 3.5 -1.9 -4.0 -26 2 -2 .38
COD | 1 | -.7 -.4 .0 -10 17 -4 .05
EMR | 1 | 7.7 -9.9 6.3 10 13 21 .31
ESA | 1 | .5 -.6 1.1 -6 16 23 -.01
GFZ | 1 | .3 -.3 -.0 -19 -12 -9 .11
GRG | 1 | 10.4 -5.5 16.8 14 2 99 .05
JPL | 1 | 13.1 -7.9 11.2 0 -1 2 .02
MIT | 1 | 2.0 -4.8 4.1 -26 44 -2 .33
NGS | 1 | 2.3 -2.3 7.6 -49 -24 47 .16
SIO | 1 | 5.3 -4.0 -8.1 -29 -4 0 .30
COD | 2 | .2 -.8 .1 -11 23 -5 -.06
EMR | 2 | 4.0 -8.7 5.3 2 38 -25 .12
ESA | 2 | .7 -.9 1.1 -17 19 30 -.06
GFZ | 2 | .5 -.2 -.1 -9 -22 -12 .14
GRG | 2 | 6.2 -7.1 15.5 33 2 94 -.25
JPL | 2 | 1.8 -2.9 5.0 5 -2 -11 -.0
MIT | 2 | 2.1 -7.1 7.9 -61 48 -2 .17
NGS | 2 | -.9 -9.9 8.5 -63 3 -25 .18
SIO | 2 | 4.2 -4.8 -3.4 -51 17 0 .14
COD | 3 | -.3 -.6 .3 -10 14 2 -.14
EMR | 3 | 3.8 -9.9 5.8 -45 -9 27 .24
ESA | 3 | .1 -.5 2.4 -21 19 53 -.35
GFZ | 3 | -.1 -.1 -.1 -12 -10 -2 -.0
GRG | 3 | 2.3 -10.8 21.3 23 -1 116 -.17
JPL | 3 | 1.8 -9.5 8.9 11 -9 -8 -.25
MIT | 3 | -1.9 -9.2 4.4 -42 37 10 -.01
NGS | 3 | -1.1 -8.3 18.9 -136 -20 24 -.08
SIO | 3 | 2.7 -6.9 -5.8 -49 16 -4 .04
COD | 4 | -.2 -.1 .7 -3 24 1 -.18
EMR | 4 | -.3 -13.4 7.2 -32 -10 7 .36
ESA | 4 | -.6 .3 2.2 -24 14 46 -.23
GFZ | 4 | .0 -.2 .3 -17 -22 -6 .06
GRG | 4 | 4.3 -13.2 14.6 21 0 95 -.15
JPL | 4 | 6.6 -14.4 9.1 12 -4 -16 -.36
MIT | 4 | -.1 -9.9 3.5 -55 34 23 -.08
NGS | 4 | 3.0 -18.5 19.0 -200 -45 7 -.04
SIO | 4 | 4.2 -9.5 -3.2 -42 23 0 .07
COD | 5 | -.3 -.3 -.1 -7 14 -9 .09
EMR | 5 | .4 -5.6 3.9 -9 7 -43 .34
ESA | 5 | -.3 -.2 .6 -22 17 31 -.13
GFZ | 5 | -.1 -.0 -.3 -13 -22 -8 .18
GRG | 5 | 4.9 -6.5 14.0 18 -8 100 .11
JPL | 5 | -1.8 -8.4 1.4 1 0 2 -.17
MIT | 5 | 1.0 -4.5 -.1 -47 40 19 .12
NGS | 5 | -5.9 -12.6 11.6 -139 30 -17 .17
SIO | 5 | 2.1 -6.1 -8.6 -41 -4 5 .23
COD | 6 | -.3 -.3 -.0 -12 18 -8 .06
EMR | 6 | -.6 -8.8 1.0 -33 14 -46 .45
ESA | 6 | -.5 -.5 .5 -15 12 22 -.14
GFZ | 6 | -.1 -.3 -.1 -11 -23 3 .09
GRG | 6 | 7.6 -6.9 7.2 14 -17 101 -.04
JPL | 6 | 4.6 -11.3 8.5 1 0 1 -.01
MIT | 6 | -.0 -5.2 .1 -25 27 -13 .17
NGS | 6 | -1.8 -11.7 12.1 -145 -13 -3 .16
SIO | 6 | 3.7 -4.5 -9.9 -36 12 3 .34
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
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 1.2042.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2042.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 2.2042.[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 3.2042.[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 5.2042.0-6). 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 2042 summary. (Feb 24, 2019 - Mar 02, 2019)
Table 1.2042.a GPS week: 2042 MJD: 58538.000-58544.000
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 254| 0 0 0 0 5 11 -.03 8 8 | -367 -273 9 138
| 0 0 0 11 7 14 .02 | 235 323
emr 79| 1 -2 0 0 -18 3 .25 13 13 | 173714 -123 15 155
| 1 0 0 12 9 10 .03 | 15133 719
esa 150| 0 0 -1 -14 -1 10 -.03 22 8 | -144 -1338 7 229
| 0 0 1 8 7 18 .02 | 613 1043
gfz 185| 0 1 -1 -9 4 -8 .07 10 10 | -47 -80 12 162
| 0 0 2 13 8 9 .02 | 269 602
grg 106| 0 -1 3 11 27 -20 -.10 13 13 | 61 -127 10 168
| 1 0 2 21 14 48 .03 | 157 259
igr n/a| -1 1 -2 13 -12 -2 -.03 4 4 | 5001 -255 10 69
| 0 0 0 9 7 8 .01 | 688 731
jpl 80| 0 0 3 29 -5 2 .22 8 8 | 215346 -109 9 140
| 0 0 0 11 14 13 .02 | 712 728
mit 348| 0 -1 -7 -4 -10 -5 -.22 16 14 | 90 -135 86 1380
| 0 0 1 41 26 8 .02 | 644 345
ngs 207| -1 0 2 -2 1 5 -.08 11 11 | -402 -232 1012 2278
| 1 0 2 18 18 18 .02 | 175 242
sio 328| 0 1 -3 -22 -10 -8 -.13 13 13 | --- --- --- ---
| 0 0 1 40 19 22 .06 | --- ---
Table 1.2042.b GPS week : 2042 MJD: 58538.000-58544.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 3 3 3 3 3 |
2 | 4 4 4 4 5 4 4 |
3 | 4 4 4 4 4 4 3 |
4 | 36 17 0 30 18 32 22 |
5 | 4 4 5 5 4 5 4 |
6 | 3 4 3 3 4 0 3 |
7 | 4 4 4 3 4 4 4 |
8 | 3 3 3 3 3 4 3 |
9 | 3 3 3 3 3 4 3 |
10 | 4 4 4 4 4 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 5 5 4 4 4 |
14 | 5 5 5 5 5 5 5 |
15 | 4 4 4 4 4 4 4 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 3 |
18 | 3 3 3 3 3 3 3 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 5 4 4 4 4 4 4 |
22 | 5 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 4 3 4 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 4 4 4 4 4 3 4 |
27 | 3 3 3 3 3 3 3 |
28 | 3 4 4 4 4 4 3 |
29 | 4 4 5 4 4 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 4 4 4 4 4 4 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 2.2042.0 GPS week: 2042 Day: 0 MJD: 58538.000
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 -1 0 10 3 15 -.06 9 9 | -488 -90 11 129
emr 80| 2 -3 1 13 -19 6 .28 13 13 | 179154 -189 14 159
esa 150| 0 0 -1 -10 10 26 -.04 8 8 | -791 -356 8 214
gfz 183| 0 0 2 -22 19 -3 .04 11 12 | -7 -461 11 154
grg 105| 0 -1 4 5 29 -84 -.12 14 14 | 123 -332 13 191
igr n/a| -2 0 -3 0 -7 4 -.05 5 5 | 5055 -530 10 77
jpl 80| 0 2 3 17 -18 25 .22 9 8 | 215123 -383 9 139
mit 348| 0 -1 -6 -35 -32 8 -.21 16 14 | -115 89 53 224
ngs 212| 0 0 0 28 25 -4 -.11 10 10 | -505 -80 980 2570
sio 325| 0 1 -4 -44 -37 -13 -.04 13 14 | --- --- --- ---
Table 2.2042.1 GPS week: 2042 Day: 1 MJD: 58539.000
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 258| 0 0 0 1 13 6 -.03 7 7 | -134 -633 10 132
emr 80| 0 -1 0 -8 -2 18 .25 13 13 | 139423 -381 14 140
esa 150| 0 1 -1 -10 -11 5 -.04 76 10 | -456 -1424 8 223
gfz 188| 0 1 0 -6 10 -17 .05 11 12 | 82 -374 14 196
grg 105| -2 0 1 -12 45 -58 -.03 14 14 | 283 -431 11 147
igr n/a| -1 0 -2 10 -2 9 -.03 5 5 | 4589 -75 11 74
jpl 80| 0 0 4 10 -7 7 .21 8 8 | 214764 63 10 147
mit 348| 0 -1 -7 47 -27 -19 -.23 16 15 | 195 -599 78 1572
ngs 213| -1 0 1 -12 -4 20 -.04 10 10 | -364 -329 1150 2265
sio 332| 0 0 -1 12 -27 0 -.13 13 14 | --- --- --- ---
Table 2.2042.2 GPS week: 2042 Day: 2 MJD: 58540.000
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 259| 1 0 0 14 18 -18 -.01 8 7 | -537 11 10 140
emr 80| 1 -2 -1 0 -29 15 .26 14 14 | 178472 969 19 162
esa 150| 0 0 0 -2 2 29 -.07 8 8 | -364 -570 7 216
gfz 189| 0 1 0 14 -3 -24 .06 10 10 | -381 482 10 134
grg 109| 0 -1 3 33 41 -56 -.12 14 14 | 43 -228 12 169
igr n/a| -1 1 -2 30 -14 -6 -.01 4 4 | 4343 737 9 67
jpl 80| 0 1 2 35 -26 -3 .22 8 8 | 214612 801 7 142
mit 348| 0 -1 -6 -71 1 -6 -.19 16 14 | 455 -433 132 1610
ngs 206| -2 0 0 -3 11 35 -.08 10 10 | -571 80 984 2053
sio 333| 0 0 -3 -99 -7 19 -.08 15 14 | --- --- --- ---
Table 2.2042.3 GPS week: 2042 Day: 3 MJD: 58541.000
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 0 -1 -18 -1 15 -.05 8 8 | -695 173 9 137
emr 80| 3 -3 -1 -8 -26 -1 .25 13 13 | 179426 616 14 137
esa 150| 0 0 -2 -22 -3 28 -.00 36 10 | 186 -1143 9 236
gfz 189| 0 2 -1 -7 -3 -9 .07 10 11 | 333 -601 11 167
grg 109| -1 -1 5 30 23 6 -.12 13 13 | -163 192 10 155
igr n/a| -1 1 -4 21 -10 -3 -.02 4 4 | 5386 483 10 61
jpl 80| 0 1 1 34 -6 -9 .22 8 8 | 215655 666 9 138
mit 349| 0 -1 -8 34 12 -9 -.24 16 14 | -130 371 79 1456
ngs 206| -1 0 7 -5 5 -12 -.08 10 10 | -556 -52 830 2318
sio 326| 2 1 -4 -13 21 -15 -.16 12 12 | --- --- --- ---
Table 2.2042.4 GPS week: 2042 Day: 4 MJD: 58542.000
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 239| 0 0 0 -10 -1 26 -.01 9 9 | -239 -440 9 167
emr 80| 0 -2 0 7 -10 -3 .26 13 13 | 180230 -809 15 157
esa 150| 0 0 0 -25 3 9 -.02 8 8 | -610 -1834 9 269
gfz 184| 0 1 -4 -25 3 -4 .09 9 10 | 192 -771 15 176
grg 108| -1 -1 6 34 31 -20 -.07 13 13 | 71 -198 9 167
igr n/a| -1 2 -3 12 -15 -16 -.03 4 4 | 6090 -1185 10 66
jpl 80| 0 0 3 43 15 -13 .21 8 8 | 216397 -864 11 131
mit 348| 0 -2 -7 12 -11 -1 -.20 16 14 | 758 -219 50 1560
ngs 205| 0 0 3 -30 -27 4 -.09 11 11 | -328 -347 980 2357
sio 328| 0 1 -4 15 -12 -27 -.20 13 13 | --- --- --- ---
Table 2.2042.5 GPS week: 2042 Day: 5 MJD: 58543.000
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| 0 0 0 8 1 16 -.03 8 8 | -42 -671 8 123
emr 78| 0 -2 -1 15 -25 0 .20 13 13 | 180182 -1030 17 170
esa 150| 0 0 0 -20 -6 -10 -.02 8 8 | 1017 -3391 8 243
gfz 185| 1 1 -3 -10 5 -1 .11 10 9 | -288 656 13 163
grg 103| 0 0 2 1 14 33 -.12 12 12 | 183 -159 10 169
igr n/a| 0 1 -2 5 -24 -5 -.01 5 5 | 5404 -1089 10 62
jpl 80| 0 0 2 38 1 0 .22 8 8 | 216109 -1129 9 139
mit 348| 0 -1 -8 -17 29 -8 -.22 16 15 | 617 -296 149 1516
ngs 207| -1 0 4 -5 -15 -16 -.06 10 10 | -63 -653 1155 2172
sio 328| 0 1 -3 -34 -8 15 -.18 13 13 | --- --- --- ---
Table 2.2042.6 GPS week: 2042 Day: 6 MJD: 58544.000
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 258| 0 0 0 -1 2 16 -.04 8 8 | -435 -265 8 138
emr 80| 0 -1 0 -18 -17 -11 .22 13 13 | 179117 -41 15 160
esa 150| 0 0 -1 -14 -5 -13 -.02 7 7 | 6 -648 6 202
gfz 183| 0 1 0 -8 1 1 .06 9 9 | -266 503 11 147
grg 108| 0 0 -2 -15 3 36 -.09 12 11 | -113 261 11 184
igr n/a| -1 1 -1 12 -13 -1 -.03 4 4 | 4141 -126 10 82
jpl 80| 1 1 3 28 4 12 .26 8 8 | 214763 83 9 146
mit 348| 0 -1 -5 -4 -46 -2 -.22 16 13 | -1148 136 64 1727
ngs 204| -2 0 3 14 14 9 -.10 11 11 | -431 -248 1009 2216
sio 328| 0 0 0 4 0 -41 -.10 13 13 | --- --- --- ---
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 3.2042.0 GPS week: 2042 Day: 0 MJD: 58538.000
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 6 7 8 10 5 7 10 7 12 2 | 20 26 21 19 20 19 25 19 19 25 20
2 | 9 15 10 7 11 4 8 19 13 17 4 | 30 31 30 31 28 26 30 28 27 26 27
3E | 9 8 10 23 16 6 9 9 8 9 4 | 26 29 28 24 30 25 27 25 26 27 25
X4 | 24 --- --- --- 52 36 --- --- --- --- 36 | 48 --- --- --- 99 48 --- --- --- --- 64
5E | 9 15 8 8 25 3 9 12 10 8 4 | 41 40 39 42 48 39 40 39 41 44 40
6 | 9 11 9 5 10 3 8 13 6 10 3 | 20 26 21 19 16 18 25 19 17 24 20
7 | 6 11 7 6 10 3 8 16 12 13 3 | 26 30 27 29 23 25 30 26 24 27 26
8 | 6 6 7 11 13 4 8 10 7 8 3 | 23 28 24 23 21 21 24 23 22 22 22
9 | 8 9 5 8 12 5 10 8 5 8 3 | 35 39 34 37 35 32 38 33 35 39 35
10E | 7 13 9 12 18 3 9 12 7 12 3 | 26 29 30 22 32 25 29 28 28 30 27
11 | 8 10 15 9 15 6 9 9 8 9 3 | 41 46 33 43 43 39 44 39 42 36 39
12 | 9 25 5 10 22 5 10 19 14 15 5 | 28 45 31 35 33 29 36 25 29 26 30
13 | 8 11 10 11 9 4 13 18 12 22 4 | 24 31 19 22 23 24 30 33 27 25 22
14 | 11 8 7 10 11 7 8 36 14 19 5 | 32 37 35 35 35 36 36 46 39 37 34
15 | 8 11 9 6 15 5 9 16 10 13 3 | 47 50 44 45 45 45 50 43 47 47 46
16 | 10 25 8 15 14 7 7 17 14 18 5 | 41 46 37 44 36 34 37 32 35 32 36
17 | 7 11 7 9 12 3 10 14 11 11 3 | 35 39 33 35 33 33 37 32 33 31 33
18 | 5 9 9 7 11 3 8 7 7 12 3 | 27 30 122 30 29 28 31 28 28 35 29
19 | 8 15 7 9 12 5 9 17 15 16 4 | 21 25 23 23 24 24 23 32 30 29 23
20 | 12 12 5 8 17 3 9 16 10 14 4 | 27 22 23 25 26 24 25 25 24 24 23
21 | 12 9 10 10 13 5 9 20 15 17 4 | 29 28 29 30 25 26 31 23 23 23 26
22E | 14 11 5 24 20 7 6 12 12 12 4 | 86 87 89 84 84 85 88 87 93 90 87
23 | 8 23 8 10 11 6 9 27 13 22 5 | 38 35 40 39 39 37 39 43 40 42 37
24 | 5 9 10 12 16 3 7 15 9 13 3 | 20 26 21 23 15 18 28 18 21 29 21
25 | 10 11 4 12 15 5 7 9 8 8 3 | 24 29 27 29 25 25 28 28 26 28 26
26 | 10 16 9 12 16 4 9 11 8 8 3 | 31 30 31 29 32 26 31 28 27 26 28
27 | 10 7 6 7 11 4 7 11 6 8 2 | 28 30 26 24 26 23 26 23 23 21 24
28 | 7 9 5 6 15 5 8 13 9 12 3 | 34 37 33 36 32 37 34 40 37 37 34
29 | 8 21 8 6 15 5 8 16 13 14 4 | 64 66 67 67 63 67 66 69 70 66 66
30 | 6 10 10 7 11 3 8 11 7 11 3 | 26 39 32 29 28 29 36 28 27 35 30
31 | 8 12 7 9 11 4 8 21 12 16 4 | 54 54 52 54 55 53 55 53 56 55 53
32 | 10 10 4 7 11 4 9 10 7 10 3 | 35 38 36 37 38 35 39 29 36 35 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 11 14 5 9 16 10 13 |T 33 37 36 34 35 32 36 33 33 34 34
WRMS | 9 13 8 12 14 5 8 14 10 14 |NE 32 35 35 33 33 31 34 32 32 32 32
MEDI | 8 11 8 9 13 4 8 13 10 12 |MD 29 31 31 30 32 28 31 28 28 30 29
Table 3.2042.1 GPS week: 2042 Day: 1 MJD: 58539.000
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 6 9 8 13 5 6 8 5 9 2 | 23 30 25 23 24 24 27 26 26 29 24
2 | 7 8 12 6 11 4 9 19 14 17 4 | 24 26 28 26 22 21 26 22 25 22 23
3E | 10 11 10 16 17 6 10 10 14 12 4 | 30 32 30 26 35 29 31 29 33 30 29
X4 | 10 --- --- --- 27 38 --- --- --- --- 17 | 48 --- --- --- 48 37 --- --- --- --- 47
5E | 8 11 7 17 17 5 10 18 12 11 4 | 30 29 30 32 35 30 30 28 29 31 29
6 | 7 9 12 7 11 4 8 13 10 9 3 | 17 25 23 18 17 17 25 19 22 24 19
7 | 6 12 6 5 10 4 11 16 13 15 3 | 21 26 22 26 23 22 27 23 23 22 22
8 | 7 8 7 9 13 5 8 9 6 6 2 | 19 22 23 19 21 18 21 20 19 18 19
9 | 6 11 6 10 11 4 8 8 7 7 2 | 28 32 27 35 31 29 32 28 28 31 29
10E | 10 13 9 9 17 4 8 12 7 12 3 | 28 27 28 25 33 25 26 27 27 28 26
11 | 7 9 15 13 16 6 10 7 4 9 3 | 37 44 31 42 42 38 42 38 42 35 38
12 | 8 26 5 11 20 6 8 22 13 15 5 | 26 37 26 32 31 25 31 19 24 22 26
13 | 7 12 11 13 8 3 11 22 14 19 4 | 22 33 22 25 23 24 31 27 27 23 23
14 | 10 8 8 9 12 6 8 33 13 17 4 | 25 28 25 31 29 29 28 36 31 25 25
15 | 7 10 9 8 15 4 7 19 11 13 3 | 37 38 32 35 35 34 37 36 36 37 35
16 | 7 20 10 25 16 6 8 16 13 17 5 | 25 32 24 37 25 24 26 18 26 21 24
17 | 7 15 8 11 13 4 9 14 8 12 3 | 32 35 32 31 31 29 33 31 33 29 30
18 | 6 11 421 9 12 6 7 9 8 9 3 | 21 23 274 23 20 21 22 19 22 25 21
19 | 8 20 9 11 13 5 9 16 12 15 4 | 24 22 22 27 23 23 23 26 28 22 22
20 | 10 14 6 11 19 3 8 16 10 14 4 | 29 24 24 27 30 24 25 25 25 24 25
21 | 9 8 9 9 12 5 6 19 13 17 4 | 28 28 27 30 24 24 30 20 23 22 25
22 | 7 12 6 18 19 6 8 12 16 11 4 | 48 52 53 49 47 50 51 49 53 53 50
23 | 7 26 10 10 13 7 8 27 13 19 5 | 31 29 33 34 33 32 30 34 29 33 29
24 | 5 9 11 10 15 3 7 18 7 10 3 | 21 29 23 24 16 20 28 17 21 28 22
25 | 7 12 6 13 13 4 7 10 7 7 3 | 24 25 25 28 22 22 26 24 22 25 23
26 | 8 18 7 13 17 3 8 10 9 7 3 | 19 24 20 22 26 18 22 22 22 21 19
27 | 7 9 6 8 11 4 7 11 6 9 3 | 21 23 22 21 22 19 23 21 21 18 20
28 | 6 8 6 8 18 6 9 13 11 13 3 | 26 26 25 27 27 25 24 29 26 27 24
29 | 6 17 8 9 14 6 8 18 12 13 4 | 52 55 55 56 51 56 56 56 59 56 54
30 | 6 9 10 5 10 4 7 12 7 11 3 | 25 32 28 27 25 24 32 20 25 30 27
31 | 7 13 9 8 10 3 9 22 11 14 4 | 43 44 38 42 44 41 43 38 43 42 41
32 | 7 8 5 8 11 3 7 10 6 7 2 | 27 30 26 26 30 27 31 22 30 26 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 76 11 14 5 8 16 10 13 |T 28 31 36 29 29 27 30 27 29 28 28
WRMS | 7 13 10 12 14 5 8 15 10 14 |NE 27 30 36 29 28 26 29 26 28 27 27
MEDI | 7 11 9 9 13 4 8 14 11 12 |MD 26 29 26 27 27 24 28 26 26 26 25
Table 3.2042.2 GPS week: 2042 Day: 2 MJD: 58540.000
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 7 9 8 11 5 7 5 6 8 2 | 23 33 28 23 22 25 31 26 28 31 26
2 | 7 11 9 8 12 4 7 20 12 19 4 | 21 24 24 27 22 21 24 24 23 28 22
3E | 10 8 11 17 13 4 11 11 7 10 4 | 33 37 39 31 33 36 38 33 39 37 34
X4 | 2 --- --- --- 81 63 --- --- --- --- 0 | 78 --- --- --- 69 46 --- --- --- --- 77
5 | 9 19 6 15 25 6 10 16 11 25 5 | 22 28 23 27 26 23 24 24 26 35 23
6 | 9 7 10 6 10 4 7 12 10 11 3 | 22 31 26 23 20 22 28 24 28 29 24
7 | 6 11 6 5 12 3 9 16 13 16 3 | 37 41 37 39 35 35 38 35 41 35 36
8 | 6 7 6 8 16 4 9 8 7 9 3 | 23 30 29 25 29 27 29 27 30 27 26
9 | 6 9 6 7 12 3 8 7 5 13 2 | 38 41 38 40 38 37 39 36 39 44 38
10E | 10 13 9 8 15 6 10 13 9 11 3 | 32 38 35 36 32 35 37 36 38 39 34
11 | 7 9 15 10 17 5 9 7 5 11 3 | 32 37 27 33 32 30 38 31 30 29 31
12 | 10 22 6 10 24 5 10 20 15 18 5 | 28 33 25 32 35 26 30 23 29 28 26
13 | 7 13 11 10 8 4 10 21 15 21 4 | 23 33 21 23 23 22 30 31 27 28 23
14 | 8 12 9 12 11 6 5 34 14 17 4 | 41 44 42 41 39 40 42 49 42 41 39
15 | 8 9 7 9 13 5 10 21 12 18 4 | 51 55 49 52 47 49 51 51 53 53 50
16 | 6 20 9 17 15 4 8 17 13 16 4 | 35 40 39 37 35 36 36 35 39 35 35
17 | 7 15 7 8 12 3 11 15 10 14 3 | 29 31 27 26 27 27 33 26 26 25 27
18 | 6 10 10 9 13 4 8 7 6 11 3 | 32 38 160 30 35 34 36 34 37 40 34
19 | 9 21 8 9 12 5 8 16 12 17 4 | 19 25 24 24 24 22 23 26 28 27 22
20 | 11 13 5 8 15 4 7 14 10 13 3 | 22 21 20 23 21 20 20 20 21 21 19
21 | 9 9 10 7 11 5 7 19 12 19 4 | 23 25 21 24 21 21 26 17 19 20 20
22 | 8 9 6 11 17 3 7 14 10 10 3 | 31 34 31 33 30 30 32 32 35 33 31
23 | 9 26 9 10 12 5 7 27 13 23 5 | 46 46 48 50 47 47 47 48 50 49 45
24 | 5 8 10 10 12 3 9 17 12 13 3 | 26 35 27 34 22 25 33 27 26 37 28
25 | 8 12 6 8 13 3 7 9 10 9 3 | 23 25 25 24 24 22 24 24 22 25 23
26 | 7 25 7 11 17 3 7 11 8 10 4 | 27 38 30 28 31 27 31 29 29 31 28
27 | 6 8 6 9 12 3 9 11 6 11 3 | 23 30 27 24 24 24 29 23 26 25 24
28 | 7 10 7 8 16 4 8 14 9 13 3 | 34 35 32 35 34 32 31 34 34 33 32
29 | 8 22 7 8 18 6 10 19 12 16 4 | 54 50 49 55 53 52 49 54 52 53 51
30 | 6 7 9 6 12 3 9 10 9 12 3 | 31 40 35 34 34 31 37 33 36 37 34
31 | 4 13 9 7 11 4 8 23 13 16 4 | 59 63 59 60 59 60 64 59 64 61 60
32 | 5 10 6 9 11 4 7 12 6 8 2 | 38 42 40 40 39 39 42 36 41 40 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 8 10 14 4 8 16 10 15 |T 33 36 36 33 33 31 34 32 34 34 33
WRMS | 7 14 8 10 14 4 8 14 10 14 |NE 33 36 37 33 33 32 34 32 34 34 33
MEDI | 7 11 8 9 12 4 8 14 10 13 |MD 31 35 30 32 32 30 33 31 30 33 31
Table 3.2042.3 GPS week: 2042 Day: 3 MJD: 58541.000
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 8 13 8 12 3 6 7 8 8 3 | 18 29 25 21 18 20 26 21 23 24 21
2 | 8 9 11 8 10 4 9 18 11 14 3 | 37 38 37 36 32 33 34 35 34 35 34
3 | 8 11 10 13 22 5 8 9 7 6 3 | 25 30 25 22 26 24 27 25 30 25 24
X4 | 21 --- --- --- 42 33 --- --- --- --- 30 | 63 --- --- --- 80 54 --- --- --- --- 65
5 | 11 20 8 12 19 4 11 18 12 11 4 | 39 41 38 39 39 38 36 41 43 37 37
6 | 8 9 10 8 9 3 6 12 8 9 3 | 24 29 25 22 20 23 29 24 27 28 24
7 | 5 11 8 5 8 4 9 14 10 13 3 | 24 26 25 24 21 24 25 25 25 22 23
8 | 9 7 10 10 14 4 5 10 8 6 3 | 18 26 24 20 21 19 23 21 25 18 20
9 | 6 12 7 10 7 6 8 9 9 10 3 | 22 27 20 24 19 21 24 24 24 27 22
10 | 7 13 10 11 12 5 8 12 6 7 3 | 19 25 25 21 26 21 25 24 24 23 22
11 | 9 11 16 11 18 3 8 8 7 8 4 | 26 38 29 32 30 28 35 29 32 26 29
12 | 9 24 7 14 23 6 9 22 15 17 5 | 25 35 21 32 32 21 27 17 26 21 23
13 | 9 11 12 11 10 3 10 20 12 19 4 | 24 32 18 20 17 22 27 31 23 27 22
14 | 8 7 9 11 8 6 6 34 14 16 4 | 21 24 23 22 21 24 24 39 21 28 21
15 | 9 9 10 7 12 4 8 19 10 14 3 | 29 31 24 28 25 25 28 24 28 27 26
16 | 10 22 8 15 17 6 6 18 15 19 5 | 26 32 23 32 28 22 24 20 27 21 23
17 | 8 11 7 7 12 3 9 14 10 11 3 | 34 35 30 32 32 30 33 30 31 28 31
18 | 7 9 198 9 10 4 8 11 6 7 3 | 22 26 159 22 23 21 24 23 26 24 22
19 | 7 17 7 8 13 4 8 15 10 14 3 | 26 26 24 26 26 24 24 25 28 25 24
20 | 10 15 6 10 12 4 6 18 11 13 3 | 25 24 21 24 21 22 23 25 23 24 21
21 | 9 9 10 9 9 5 7 18 13 14 4 | 27 30 27 29 24 24 31 24 24 24 25
22 | 9 10 7 16 15 5 8 15 12 12 4 | 36 44 43 41 40 41 43 38 43 42 40
23 | 9 24 7 10 10 6 7 29 14 20 5 | 28 26 29 34 27 30 28 36 29 31 27
24 | 7 8 10 10 8 4 7 15 9 13 3 | 21 28 22 22 16 20 27 20 20 31 21
25 | 8 11 6 14 9 4 7 10 7 7 3 | 26 30 26 33 26 25 29 24 25 27 26
26 | 9 14 7 9 18 3 6 12 9 6 3 | 24 30 27 28 32 23 27 24 27 23 25
27 | 6 6 8 12 12 4 7 10 5 5 2 | 22 25 25 23 22 21 24 20 25 17 21
28 | 7 10 9 10 13 4 8 13 10 13 3 | 30 33 28 31 29 29 28 30 34 26 28
29 | 6 16 9 10 15 5 9 19 13 15 4 | 40 43 38 42 48 38 40 33 40 45 40
30 | 4 9 10 6 8 3 6 11 7 9 2 | 22 32 26 23 22 22 27 21 24 26 23
31 | 7 11 10 8 9 5 8 25 13 17 4 | 28 31 26 29 24 27 31 31 28 31 27
32 | 5 9 6 9 7 3 6 12 6 10 2 | 24 27 24 26 23 23 26 18 24 26 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 36 10 13 4 8 16 10 12 |T 27 30 30 27 27 26 28 26 27 27 26
WRMS | 8 13 10 11 13 4 8 14 10 12 |NE 27 30 30 27 27 25 27 25 26 26 26
MEDI | 8 11 9 10 12 4 8 14 10 12 |MD 25 30 25 26 25 24 27 24 26 26 24
Table 3.2042.4 GPS week: 2042 Day: 4 MJD: 58542.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 7 10 6 12 4 6 7 9 14 3 | 21 27 22 19 18 21 26 21 22 29 21
2 | 18 11 8 6 9 4 8 20 15 17 4 | 41 43 43 39 36 38 40 40 36 40 38
3 | 7 9 8 11 20 5 10 7 12 10 3 | 21 26 25 21 24 21 24 21 29 21 22
X4 | 13 --- --- --- 25 30 --- --- --- --- 18 | 46 --- --- --- 66 57 --- --- --- --- 50
5 | 9 8 8 16 17 3 10 16 13 10 4 | 34 36 32 32 41 32 34 41 42 35 33
X6 | 9 7 9 8 --- 5 7 13 12 8 3 | 20 27 22 19 --- 19 28 24 23 26 21
7 | 6 10 6 6 12 3 8 15 12 18 3 | 43 44 45 43 36 41 44 41 41 43 41
8 | 7 6 7 9 16 4 9 8 9 5 3 | 20 24 23 20 20 20 22 21 21 20 19
9 | 6 8 6 9 9 4 7 10 10 13 3 | 31 34 33 32 30 28 33 32 31 35 31
10 | 7 15 9 14 7 3 10 12 9 11 3 | 21 24 23 24 25 20 25 22 23 25 21
11 | 6 9 16 7 16 5 9 7 10 9 3 | 44 47 35 44 45 41 48 43 45 39 42
12 | 9 24 8 9 23 4 8 19 15 15 5 | 26 35 24 29 30 25 29 21 28 25 24
13 | 8 10 8 12 10 3 10 21 12 17 4 | 22 27 20 24 19 21 29 28 26 24 21
14 | 11 12 8 8 10 8 7 33 13 16 4 | 43 43 39 43 43 42 44 54 45 45 42
15 | 8 10 8 9 13 3 7 20 11 15 4 | 44 47 45 46 43 45 45 46 45 48 44
16 | 10 22 6 12 19 5 6 16 12 17 4 | 33 39 35 35 34 34 34 36 39 38 33
17 | 9 12 8 6 12 4 8 16 11 13 3 | 43 43 41 42 41 40 43 40 39 38 41
18 | 5 8 9 7 10 3 5 6 8 10 2 | 21 28 49 25 25 24 28 25 27 29 24
19 | 10 19 7 8 11 4 8 16 12 14 4 | 25 24 25 26 26 24 25 30 30 26 24
20 | 10 10 6 10 13 3 8 15 12 14 3 | 26 22 22 30 25 24 23 24 23 19 22
21 | 7 10 9 10 9 4 8 18 16 16 4 | 32 34 32 35 30 30 34 23 21 24 29
22 | 6 11 6 12 12 4 6 14 12 12 3 | 29 31 30 32 30 29 29 29 33 30 28
23 | 8 25 7 9 9 6 7 27 13 20 5 | 44 45 45 48 45 45 46 53 44 49 44
24 | 11 11 11 9 11 3 7 13 7 12 3 | 26 31 23 22 19 21 28 21 24 26 23
25 | 11 11 6 7 11 4 6 9 11 8 3 | 26 28 26 28 26 25 26 26 24 25 25
26 | 9 14 5 10 19 5 5 12 10 8 3 | 22 30 26 26 28 24 27 27 29 28 24
27 | 5 9 5 8 10 4 9 9 8 8 2 | 21 25 22 24 22 21 24 22 25 20 20
28 | 5 9 6 8 15 5 7 14 15 14 3 | 35 39 35 38 35 36 37 39 39 37 35
29 | 9 16 5 11 14 4 6 19 14 13 4 | 75 71 72 73 74 72 72 72 70 71 72
30 | 7 8 9 7 10 3 8 8 8 9 3 | 33 38 35 32 29 32 38 32 30 35 33
31 | 8 10 7 7 11 5 8 22 13 16 4 | 66 67 65 67 66 67 69 70 70 72 67
32 | 9 9 5 6 6 6 9 14 5 10 2 | 33 34 33 34 36 33 37 34 35 37 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 9 13 4 8 16 11 13 |T 33 35 33 33 34 32 35 34 34 34 32
WRMS | 9 13 8 10 13 4 8 14 11 13 |NE 34 36 34 34 35 33 36 35 34 35 33
MEDI | 8 10 8 9 12 4 8 14 12 13 |MD 31 34 32 32 30 29 33 30 30 30 29
Table 3.2042.5 GPS week: 2042 Day: 5 MJD: 58543.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 8 9 8 10 5 6 7 6 12 3 | 18 24 18 19 17 17 24 17 21 24 18
2 | 8 7 8 9 10 4 8 19 13 19 4 | 39 43 43 44 41 39 43 33 37 34 39
3 | 8 11 7 12 13 5 12 8 4 8 3 | 22 26 26 21 23 22 25 22 24 24 22
X4 | 26 --- --- --- 39 29 --- --- --- --- 31 | 45 --- --- --- 53 45 --- --- --- --- 42
5 | 7 11 8 21 20 6 9 18 16 17 5 | 28 28 25 32 30 27 28 26 29 27 26
X6 | 1 --- --- --- --- 40 --- --- --- --- 0 | 20 --- --- --- --- 16 --- --- --- --- 20
7 | 7 12 8 6 8 2 9 15 11 15 3 | 36 38 39 41 36 37 41 39 35 38 38
8 | 8 9 6 14 15 5 7 10 9 10 3 | 17 20 19 20 19 17 21 18 20 16 17
9 | 9 11 7 8 8 4 7 11 13 11 3 | 35 37 36 36 36 35 40 34 43 39 36
10 | 8 10 9 11 8 4 8 12 7 9 3 | 19 22 22 21 23 19 24 22 22 22 20
11 | 7 9 15 8 17 7 8 7 6 10 3 | 35 42 30 35 39 35 41 34 40 34 36
12 | 9 22 7 10 21 6 9 21 13 17 5 | 28 35 24 31 31 24 30 17 27 22 25
13 | 6 13 8 11 10 3 11 21 11 19 4 | 19 31 17 22 20 21 27 27 22 25 20
14 | 13 11 8 9 8 8 6 32 13 16 4 | 34 34 34 35 32 31 34 36 34 29 31
15 | 9 11 8 9 12 5 9 18 10 13 3 | 43 45 42 42 44 42 45 41 48 45 43
16 | 9 24 6 10 15 5 7 18 13 18 4 | 28 36 29 29 32 28 28 26 30 28 28
17 | 11 10 6 8 11 4 10 16 10 12 3 | 43 46 40 39 39 41 46 39 42 39 40
18 | 7 9 10 7 10 4 7 9 5 9 2 | 26 26 28 26 25 25 26 27 24 27 25
19 | 8 17 6 10 11 5 8 17 14 15 4 | 25 24 24 25 22 25 25 28 32 26 24
20 | 10 12 6 9 12 3 7 14 13 14 3 | 27 22 22 28 26 24 22 24 28 25 23
21 | 11 9 9 8 8 5 10 19 14 15 4 | 33 30 29 32 27 27 30 24 28 26 28
22 | 8 12 7 9 14 5 8 15 10 13 3 | 18 23 20 21 22 20 21 19 24 20 19
23 | 11 22 9 8 12 6 9 27 14 21 5 | 47 46 49 48 47 46 47 46 52 48 46
24 | 8 7 10 7 9 3 8 13 8 10 3 | 21 28 24 27 17 21 29 21 19 28 23
25 | 6 12 6 8 9 4 8 9 6 10 2 | 24 27 24 28 22 23 25 25 26 24 23
26 | 9 14 5 7 17 4 7 11 5 8 3 | 18 23 20 19 26 18 23 21 20 22 20
27 | 6 10 5 12 11 5 7 9 5 8 3 | 17 21 21 22 18 18 21 18 21 16 18
28 | 8 12 7 7 12 5 8 15 9 14 3 | 26 27 23 28 25 25 24 27 29 24 24
29 | 9 20 6 9 17 5 8 18 12 11 4 | 70 68 68 69 64 70 68 70 77 70 69
30 | 6 11 10 7 8 5 7 11 4 11 3 | 26 30 29 28 23 24 31 25 27 33 28
31 | 8 11 8 9 9 5 8 23 12 15 4 | 57 60 56 59 57 57 60 54 59 56 57
32 | 7 10 6 7 8 4 6 10 6 7 2 | 33 34 33 31 33 31 35 26 33 32 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 8 10 12 5 8 16 10 13 |T 30 33 30 31 31 29 32 29 32 30 30
WRMS | 8 13 8 9 12 5 8 14 10 13 |NE 31 34 31 33 32 30 34 30 33 31 31
MEDI | 8 11 7 9 11 5 8 15 10 12 |MD 27 30 26 28 27 25 28 26 28 27 25
Table 3.2042.6 GPS week: 2042 Day: 6 MJD: 58544.000
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 7 9 7 10 4 7 7 6 9 2 | 20 25 21 18 17 19 25 20 20 24 20
2 | 6 10 9 10 12 4 9 17 16 16 4 | 35 38 38 38 37 34 38 32 32 32 34
3 | 7 10 7 9 14 5 9 8 10 9 3 | 25 27 26 24 22 23 27 23 31 29 24
X4 | 15 --- --- --- 29 34 --- --- --- --- 21 | 71 --- --- --- 68 51 --- --- --- --- 65
5 | 7 11 6 7 19 5 8 15 15 12 4 | 24 26 23 26 29 22 26 25 29 22 23
6 | 8 11 11 8 10 4 7 12 9 9 3 | 17 23 16 13 13 16 22 15 16 21 19
7 | 7 12 8 7 8 3 8 15 12 15 3 | 32 34 33 32 29 31 35 32 35 32 31
8 | 8 8 6 10 12 4 8 10 7 7 3 | 24 26 25 22 23 22 24 21 23 24 23
9 | 8 9 6 10 10 3 8 10 8 12 3 | 42 45 43 47 47 43 47 42 46 51 44
10 | 8 11 6 12 7 4 7 13 7 8 3 | 20 24 23 22 24 20 26 23 23 21 21
11 | 6 9 15 9 14 5 10 7 6 8 3 | 35 40 29 37 37 34 41 34 37 34 35
12 | 9 21 6 9 22 5 8 19 12 14 4 | 30 39 29 32 29 29 34 26 32 24 28
13 | 6 13 9 10 10 3 10 23 12 17 4 | 19 30 18 20 21 21 26 34 26 23 20
14 | 11 11 9 12 7 6 7 34 15 16 4 | 33 35 34 35 33 36 36 45 39 36 33
15 | 12 16 8 10 15 4 10 20 9 13 4 | 48 49 47 49 46 47 47 44 50 49 46
16 | 9 24 6 13 13 5 6 18 14 20 4 | 37 45 38 41 37 36 39 32 36 34 36
17 | 7 11 5 6 9 3 9 14 11 14 3 | 39 42 38 37 38 37 42 36 40 36 38
18 | 6 8 11 8 7 3 7 10 5 8 2 | 33 35 28 36 35 35 35 39 35 36 35
19 | 7 18 5 8 11 5 8 16 13 16 4 | 23 22 24 24 25 26 25 29 35 29 24
20 | 10 12 6 12 11 4 7 18 12 15 4 | 25 24 23 30 26 24 23 24 25 24 23
21 | 9 8 7 11 8 6 7 18 14 17 4 | 30 31 28 30 26 26 30 25 24 25 26
22 | 9 11 6 9 12 4 7 16 11 14 3 | 28 28 28 33 26 28 27 28 31 28 26
23 | 8 22 7 11 13 5 9 29 16 18 5 | 47 44 48 48 49 47 47 47 50 47 46
24 | 7 9 7 8 9 4 7 13 6 9 3 | 24 26 26 25 17 22 28 21 24 26 23
25 | 7 10 4 8 8 3 7 10 8 7 2 | 24 29 26 27 23 24 27 27 26 25 25
26 | 11 15 5 10 14 4 8 14 8 7 3 | 25 29 24 23 26 22 29 24 27 25 24
27 | 8 9 7 7 8 4 8 8 7 6 2 | 24 27 25 25 23 22 26 21 24 24 23
28 | 5 11 5 10 12 4 7 12 9 14 3 | 35 36 35 36 37 34 35 36 41 35 34
29 | 8 21 5 8 15 4 8 20 13 14 4 | 72 71 72 73 69 73 71 73 79 73 72
30 | 7 11 9 7 9 2 7 10 7 14 3 | 25 31 27 25 24 25 31 27 26 31 26
31 | 6 11 6 8 7 4 8 23 13 17 3 | 56 60 58 59 57 58 60 56 61 59 58
32 | 7 9 4 8 6 3 8 10 6 7 2 | 37 39 38 38 37 37 41 32 41 39 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 7 9 12 4 8 16 11 13 |T 33 34 31 33 32 32 34 32 34 32 32
WRMS | 8 13 7 9 11 4 8 13 11 13 |NE 34 36 33 34 33 33 35 33 35 34 33
MEDI | 7 11 6 9 10 4 8 14 10 14 |MD 30 31 28 32 29 28 31 29 32 29 26
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 4.2042 GPS week: 2042 MJD: 58538.0-58544.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 |U 8 10 22 |U 10 13 33 |U 8 10 15 |
emr | emr 2962 |U 16 15 46 |U 15 18 43 |U 16 19 38 |
esa | esa 2962 | 8 14 23 |U 9 13 31 | 9 10 20 |
gfz | gfz 2961 |U 9 11 21 |U 10 13 32 |U 8 9 20 |
grg | grg 3043 |U 9 14 24 |U 10 15 33 | 8 11 19 |
igr | igr 2954 | 8 10 22 | 9 12 31 | 8 9 16 |
igs | igs 3037 | 9 10 23 | 10 13 33 | 8 10 19 |
jpl | jpl 2962 |U 14 14 37 |U 11 15 42 |U 12 15 32 |
mit | mit 2962 |U 17 16 39 |U 22 35 79 |U 28 29 54 |
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 5.2042.0 GPS week: 2042 Day: 0 MJD: 58538.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 9 19 | 11 15 36 | 8 10 13 |
emr | emr 2975 | 18 12 44 | 15 17 41 | 15 20 34 |
esa | esa 2976 | 10 13 24 | 11 15 36 | 10 9 17 |
gfz | gfz 2975 | 10 8 20 | 11 16 37 | 10 9 17 |
grg | grg 3070 | 11 14 23 | 10 15 36 | 11 14 21 |
igr | igr 2975 | 10 8 21 | 11 14 34 | 9 9 15 |
igs | igs 3031 | 11 9 24 | 11 14 36 | 10 11 17 |
jpl | jpl 2976 | 15 13 37 | 13 14 43 | 12 14 26 |
mit | mit 2976 | 12 9 28 | 15 18 75 | 10 6 21 |
Table 5.2042.1 GPS week: 2042 Day: 1 MJD: 58539.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 8 11 22 | 15 18 44 | 9 8 14 |
emr | emr 2976 | 15 15 45 | 18 26 56 | 16 19 35 |
esa | esa 2976 | 8 15 30 | 10 16 33 | 12 8 22 |
gfz | gfz 2975 | 9 9 20 | 15 16 43 | 10 7 22 |
grg | grg 3070 | 9 13 24 | 14 22 40 | 11 8 17 |
igr | igr 2946 | 8 10 23 | 8 15 34 | 9 8 15 |
igs | igs 3060 | 9 10 25 | 14 18 43 | 10 9 17 |
jpl | jpl 2976 | 13 16 36 | 12 16 43 | 12 15 31 |
mit | mit 2976 | 19 10 34 | 27 83 117 | 14 15 33 |
Table 5.2042.2 GPS week: 2042 Day: 2 MJD: 58540.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 8 23 | 10 12 29 | 7 10 14 |
emr | emr 2976 | 14 21 57 | 11 13 41 | 19 20 38 |
esa | esa 2976 | 8 15 26 | 9 13 30 | 8 11 17 |
gfz | gfz 2976 | 10 12 24 | 9 9 28 | 7 9 17 |
grg | grg 3072 | 8 9 26 | 10 13 29 | 7 11 18 |
igr | igr 2976 | 8 8 24 | 9 12 30 | 8 8 13 |
igs | igs 3044 | 9 10 28 | 9 12 29 | 8 10 16 |
jpl | jpl 2976 | 16 14 47 | 9 16 35 | ---- ---- ---- |
mit | mit 2976 | 23 20 57 | 34 32 136 | 56 89 83 |
Table 5.2042.3 GPS week: 2042 Day: 3 MJD: 58541.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 7 8 20 | 10 11 32 | 8 8 16 |
emr | emr 2976 | 15 11 44 | 14 18 42 | 16 17 42 |
esa | esa 2976 | 8 12 19 | 8 12 31 | 12 10 23 |
gfz | gfz 2975 | 8 9 17 | 10 10 34 | 9 8 23 |
grg | grg 3071 | 8 14 23 | 10 12 33 | 8 9 20 |
igr | igr 2958 | 8 10 20 | 9 11 32 | 9 8 19 |
igs | igs 3060 | 8 8 21 | 9 11 34 | 9 8 21 |
jpl | jpl 2976 | 12 11 35 | 10 14 42 | 12 14 35 |
mit | mit 2976 | 9 9 28 | 14 16 53 | 18 13 43 |
Table 5.2042.4 GPS week: 2042 Day: 4 MJD: 58542.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 8 13 25 | 8 11 32 | 7 10 13 |
emr | emr 2975 | 16 15 47 | 14 14 44 | 15 17 35 |
esa | esa 2976 | 8 15 20 | 8 12 34 | 8 8 19 |
gfz | gfz 2975 | 9 13 24 | 10 12 29 | 7 9 17 |
grg | grg 2975 | 9 15 23 | 8 13 35 | 7 13 16 |
igr | igr 2975 | 9 10 23 | 8 11 33 | 7 8 16 |
igs | igs 3070 | 10 13 22 | 8 11 34 | 7 9 18 |
jpl | jpl 2976 | 14 14 31 | 11 14 44 | 10 15 32 |
mit | mit 2976 | 10 9 24 | 11 15 42 | 10 10 22 |
Table 5.2042.5 GPS week: 2042 Day: 5 MJD: 58543.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 11 22 | 8 10 23 | 7 11 19 |
emr | emr 2880 | 17 14 43 | 15 21 44 | 16 21 44 |
esa | esa 2880 | 9 15 22 | 8 12 21 | 8 10 21 |
gfz | gfz 2880 | 8 13 21 | 9 12 19 | 7 10 22 |
grg | grg 2976 | 9 16 25 | 8 14 25 | 7 11 20 |
igr | igr 2880 | 9 12 23 | 8 11 22 | 7 9 19 |
igs | igs 2956 | 10 11 23 | 8 12 24 | 7 10 20 |
jpl | jpl 2880 | 15 13 37 | 10 12 35 | 12 14 36 |
mit | mit 2880 | 41 40 75 | 36 65 85 | 62 35 141 |
Table 5.2042.6 GPS week: 2042 Day: 6 MJD: 58544.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 6 11 21 | 11 14 32 | 7 12 20 |
emr | emr 2976 | 16 19 41 | 16 17 35 | 15 20 42 |
esa | esa 2976 | 7 13 21 | 10 15 32 | 8 11 22 |
gfz | gfz 2976 | 6 12 22 | 10 18 33 | 8 14 24 |
grg | grg 3072 | 6 14 23 | 12 17 32 | 7 14 23 |
igr | igr 2968 | 6 12 21 | 10 14 31 | 7 10 19 |
igs | igs 3041 | 7 12 22 | 11 14 34 | 8 12 22 |
jpl | jpl 2976 | 12 19 34 | 13 15 50 | 13 16 33 |
mit | mit 2976 | 9 14 28 | 14 19 44 | 25 33 38 |
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 6.2042 GPS week: 2042 MJD: 58538.500-58544.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -10 -13 17 70 -1 | 9 22
| 16 11 63 93 3 | 3
emr uuuuu | 26 -10 23 -77 -9 | 58 61
| 20 9 78 44 10 | 1
esa uuuuu | 11 -1 161 142 -2 | 31 37
| 8 10 59 83 4 | 3
gfz uuuuu | 1 1 34 90 -2 | 17 25
| 27 20 42 165 4 | 2
grg uuuuu | -18 -26 -80 9 -3 | -6 18
| 17 18 41 54 3 | 2
igr xxxxx | 19 -13 51 50 -2 | 0 19
| 8 8 48 42 4 | 2
irf xxxxx | -5 -16 -6 -30 8 | -3 23
| 11 7 15 23 5 | 5
jpl uuuuu | 14 -15 -52 -60 -7 | 42 47
| 21 13 60 43 5 | 1
mit uuuuu | 9 16 -11 -102 11 | 8 24
| 16 14 31 50 4 | 4
ngs uuuuu | -36 20 -129 -44 0 | 6 19
| 28 23 60 110 3 | 2
sio uuuux | 11 45 -23 -180 -3 | 52 56
| 12 17 48 77 6 | 1
Table 7.2042.0 GPS week: 2042 Day: 0 MJD: 58538.500
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 -28 52 37 -1 | 5 20
emr uuuuu | 41 -13 27 -62 6 | 57 59
esa uuuuu | 2 -5 248 144 6 | 27 33
gfz uuuuu | -28 36 -45 -94 -5 | 17 25
grg uuuuu | -30 0 -60 -57 -4 | -8 19
igr xxxxx | 13 4 144 -38 -3 | -1 19
irf xxxxx | -15 -7 17 -15 16 | -10 21
jpl uuuuu | 44 4 -161 -34 -7 | 42 46
mit uuuuu | 36 12 3 -15 11 | 3 20
ngs uuuuu | -55 -25 -87 119 -4 | 4 18
sio uuuux | 22 40 -78 -215 -2 | 53 56
Table 7.2042.1 GPS week: 2042 Day: 1 MJD: 58539.500
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 -22 0 81 -1 | 5 21
emr uuuuu | 6 -13 125 -127 -10 | 58 61
esa uuuuu | 15 -18 209 35 -3 | 29 35
gfz uuuuu | 26 6 66 211 -3 | 16 24
grg uuuuu | -30 -19 -138 84 0 | -8 19
igr xxxxx | 3 -18 33 43 -6 | -1 19
irf xxxxx | -7 -14 -30 -20 11 | -8 22
jpl uuuuu | 16 3 -25 -63 -18 | 42 46
mit uuuuu | -4 18 -46 -95 6 | 4 21
ngs uuuuu | -40 12 -196 -73 3 | 4 18
sio uuuux | 31 61 -83 -127 -9 | 52 54
Table 7.2042.2 GPS week: 2042 Day: 2 MJD: 58540.500
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 | -39 -12 -6 -67 4 | 6 21
emr uuuuu | 45 -24 34 -63 -6 | 56 59
esa uuuuu | 10 0 150 195 -8 | 30 36
gfz uuuuu | 44 -25 41 360 -5 | 15 24
grg uuuuu | -32 -33 -67 -10 -6 | -7 18
igr xxxxx | 22 -20 5 63 -7 | -2 19
irf xxxxx | 12 -14 -10 -21 13 | -6 21
jpl uuuuu | 40 -23 30 -40 -4 | 41 46
mit uuuuu | 24 42 -43 -123 15 | 5 21
ngs uuuuu | -76 38 -209 -163 -2 | 5 18
sio uuuux | 5 71 5 -286 6 | 51 54
Table 7.2042.3 GPS week: 2042 Day: 3 MJD: 58541.500
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 | -15 4 -30 21 -3 | 9 24
emr uuuuu | 30 -10 21 -74 -6 | 59 62
esa uuuuu | 25 11 201 283 0 | 32 38
gfz uuuuu | 7 -8 74 107 -2 | 16 25
grg uuuuu | -21 -36 -87 22 -4 | -5 19
igr xxxxx | 20 -17 47 79 0 | -1 20
irf xxxxx | 2 -26 -15 -8 9 | -3 24
jpl uuuuu | 13 -18 -55 -32 -6 | 42 47
mit uuuuu | 13 21 -38 -68 11 | 8 25
ngs uuuuu | -54 12 -127 -179 2 | 6 20
sio uuuux | 12 29 31 -162 -1 | 53 56
Table 7.2042.4 GPS week: 2042 Day: 4 MJD: 58542.500
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 -4 -76 51 -2 | 13 24
emr uuuuu | 10 -10 69 -95 -12 | 60 63
esa uuuuu | 0 10 108 89 -4 | 35 40
gfz uuuuu | -4 13 17 68 3 | 19 27
grg uuuuu | -5 -57 -122 75 -3 | -2 17
igr xxxxx | 23 -17 7 90 -2 | 2 19
irf xxxxx | -17 -10 -6 -25 6 | 2 23
jpl uuuuu | -1 -15 -23 -12 -9 | 44 48
mit uuuuu | 1 -5 7 -100 15 | 12 27
ngs uuuuu | -9 35 -38 -56 0 | 9 20
sio uuuux | 2 23 23 -167 -11 | 55 59
Table 7.2042.5 GPS week: 2042 Day: 5 MJD: 58543.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 8 -16 103 225 1 | 10 23
emr uuuuu | 48 -6 -132 2 -26 | 58 62
esa uuuuu | 12 1 99 165 -1 | 33 38
gfz uuuuu | -28 -2 63 -111 4 | 17 25
grg uuuuu | -24 -20 -71 -28 -7 | -5 18
igr xxxxx | 27 -10 43 61 5 | 0 19
irf xxxxx | -13 -14 -1 -60 6 | 0 23
jpl uuuuu | -7 -30 -46 -127 -1 | 41 46
mit uuuuu | -1 14 13 -156 13 | 11 26
ngs uuuuu | -10 36 -108 63 2 | 7 19
sio uuuux | 10 39 -5 -250 0 | 51 55
Table 7.2042.6 GPS week: 2042 Day: 6 MJD: 58544.500
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 -15 77 142 -4 | 13 24
emr uuuuu | -1 4 14 -122 -12 | 57 61
esa uuuuu | 12 -4 109 79 -2 | 34 39
gfz uuuuu | -8 -11 17 88 -4 | 20 27
grg uuuuu | 15 -16 -15 -25 3 | -4 18
igr xxxxx | 21 -14 74 49 2 | 2 19
irf xxxxx | 2 -24 4 -65 -1 | 4 23
jpl uuuuu | -9 -25 -85 -110 -4 | 42 47
mit uuuuu | -7 11 28 -156 5 | 15 28
ngs uuuuu | -8 34 -139 -18 2 | 8 20
sio uuuux | -3 51 -55 -57 -3 | 53 57
More information about the IGSREPORT
mailing list