[IGSREPORT-26416] Wk 2039 IGS Final Orbits
acc
acc at igs.org
Sun Feb 24 21:46:58 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2039 (Feb 03, 2019 - Feb 09, 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:
igs2039[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2039[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2039[0-6].cls IGS GPS clock combination summary report.
igs20397.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20397.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 | DAV1 GLSV OHI3 DAV1 GLSV OHI3
0 | EMR | BOR1 YELL YELL
0 | ESA | SCOR SCOR
0 | GFZ | BJNM DAV1 GODE BJNM DAV1 GODE
0 | GRG | 13 ALRT DARW FAA1 GLSV HOLB KRGG LHAZ RABT SCOR YELL
0 | GRG | GLSV TLSE
0 | JPL | ALRT
0 | MIT | BJNM
1 | COD | GLSV MAW1 OHI3 TIXI USUD BJNM GLSV KOKV MAW1 NRIL
1 | COD | TIXI TLSE USUD
1 | EMR | TLSE GOL2 MDO1 TLSE
1 | ESA | NOVM PDEL NOVM PDEL
1 | GFZ | ALRT DAV1 GODE MAW1 PDEL ALRT BJNM DAV1 GODE MAW1
1 | GFZ | PDEL YELL
1 | GRG | 13 13 DAV1 GLSV RABT DAV1 GLSV RABT
1 | JPL | CHTI POLV CHTI KOKB POLV
2 | COD | GLSV LHAZ NAUR NYAL TIXI GLSV LHAZ NAUR TIXI
2 | EMR | YELL
2 | ESA | AUCK CHTI HYDE AUCK CHTI
2 | GFZ | BJNM GODE REUN ABMF BJNM GODE NKLG PIE1 REUN
2 | GRG | 16 16 ABMF GLSV HOLB HRAO HYDE KRGG NKLG NRMD OHI3
2 | GRG | REYK SHAO YELL CHTI GLSV YELL
2 | JPL | NYAL
2 | MIT | PALM PALM
3 | COD | NAUR OHI3 TIXI NAUR OHI3 TIXI
3 | EMR | 8 GRAZ GRAZ MCM4 YAKT
3 | ESA | 22 CHTI CHTI
3 | GFZ | AUCK BJNM CUSV GODE ABMF CHTI CUSV GODE
3 | GRG | GLSV NRMD GLSV MCM4 NRMD
4 | COD | NAUR TIXI NAUR TIXI
4 | EMR | DAEJ DAEJ
4 | ESA | 22 LHAZ OHI3 OHI3
4 | GFZ | 18 ANKR ASPA BJNM CORD GLSV GODE REUN ASPA AUCK BJNM
4 | GFZ | CORD GODE IISC REUN SOFI
4 | GRG | 6 ADIS CHTI LHAZ ADIS CHTI METG
5 | COD | NAUR PTBB TIXI NAUR NRIL TIXI
5 | EMR | BJNM
5 | ESA | 22
5 | GFZ | ABMF GODE HRAO ABMF GODE HRAO PTBB SOFI
5 | GRG | 5 5 NRIL NRIL
5 | JPL | GLSV GLSV
5 | MIT | MBAR
6 | COD | TIXI TIXI
6 | GFZ | GODE STJO GODE STJO
6 | GRG | 18 21 18 21 ALRT GLSV TRO1 YELL ALRT GLSV STJO TRO1
6 | GRG | YELL
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
6 | SIO | ALL (high Transformation - See Table 2)
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G04 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G15 | | | | | | | 4 |
PRN G17 | | | | | | 4 | 4 |
PRN G26 | | | | | 4 | 4 | 4 |
PRN G30 | | | | | | 4 | 4 |
PRN G31 | | | | | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
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 .5 9 20 -23 -.24
EMR | 0 | -1.0 -3.3 13.7 34 18 -11 .07
ESA | 0 | .7 -.2 1.7 16 22 16 -.36
GFZ | 0 | -.3 -.3 .2 -8 -17 14 .0
GRG | 0 | 5.0 -2.7 14.0 17 -2 91 -.04
JPL | 0 | 5.4 -2.5 3.8 6 -1 -1 -.38
MIT | 0 | -1.3 -3.9 1.4 8 33 -5 .15
NGS | 0 | .1 1.0 -.6 62 -33 4 .0
SIO | 0 | 4.2 -1.7 -13.5 8 4 -3 .0
COD | 1 | -.1 .0 .1 1 16 -11 -.14
EMR | 1 | 5.9 -1.7 13.5 40 22 -29 .11
ESA | 1 | .9 .1 .8 15 20 0 -.06
GFZ | 1 | .2 -.2 .1 -10 -38 1 .12
GRG | 1 | 6.5 -.7 21.3 48 28 83 .12
JPL | 1 | 8.5 -9.0 5.5 -7 7 -3 -.26
MIT | 1 | .7 -3.1 3.8 -1 40 -21 .25
NGS | 1 | 1.9 .2 1.2 44 -49 16 -.01
SIO | 1 | 2.0 -1.9 -14.7 1 15 -17 .21
COD | 2 | .2 -.0 .2 6 5 -6 -.16
EMR | 2 | 5.8 .0 10.9 -8 -11 50 -.12
ESA | 2 | .7 -.4 .8 17 29 14 -.12
GFZ | 2 | .4 -.3 .1 -7 -23 17 -.01
GRG | 2 | 9.4 -3.2 16.0 58 14 83 -.05
JPL | 2 | 9.2 -3.1 10.2 5 1 -1 -.47
MIT | 2 | 3.9 -5.7 5.4 -19 19 -15 .20
NGS | 2 | 3.3 -.5 -.7 31 -15 -11 -.22
SIO | 2 | 6.6 -.4 -5.4 -2 -1 -6 .01
COD | 3 | .3 -.1 -.3 0 -11 -10 -.02
EMR | 3 | 4.7 -4.0 11.9 -42 33 -71 .10
ESA | 3 | 1.1 -.2 .8 6 28 14 .03
GFZ | 3 | .7 -.1 -.2 -4 -37 -1 .04
GRG | 3 | 7.6 -2.5 26.9 64 18 95 .02
JPL | 3 | 7.5 -2.3 13.6 3 7 17 -.31
MIT | 3 | 2.2 -2.9 6.4 -1 55 -18 .30
NGS | 3 | 8.9 -4.2 10.8 3 -63 -17 .10
SIO | 3 | 4.5 .6 -7.4 -7 23 -8 .14
COD | 4 | -.2 .0 -.1 1 6 -12 .02
EMR | 4 | 4.1 -.2 16.7 -32 18 15 .27
ESA | 4 | .5 .0 2.0 0 9 35 .08
GFZ | 4 | .1 -.2 -.2 -8 -21 10 .14
GRG | 4 | 3.9 -1.9 21.8 59 31 96 .04
JPL | 4 | .7 -6.9 10.6 1 0 1 -.07
MIT | 4 | -.8 -1.0 7.4 -14 63 -31 .35
NGS | 4 | -2.7 -3.5 11.2 19 -13 -32 .24
SIO | 4 | 1.7 -1.0 1.5 -6 35 -23 .35
COD | 5 | -.5 -.2 -.1 1 20 -9 .05
EMR | 5 | 4.2 .5 15.1 14 -1 21 .29
ESA | 5 | -.2 .1 .3 14 18 21 .16
GFZ | 5 | .2 -.0 -.8 -13 -36 6 .25
GRG | 5 | 7.1 -.5 17.7 49 21 93 -.01
JPL | 5 | 5.6 -2.4 9.6 1 0 1 -.03
MIT | 5 | 1.6 -3.0 5.8 -2 80 -11 .24
NGS | 5 | -5.4 -1.1 8.0 19 -10 -13 .14
SIO | 5 | 2.1 1.8 -7.6 -9 35 -10 .28
COD | 6 | -.2 .3 -.1 -3 9 -13 -.05
EMR | 6 | .1 -1.7 15.0 -34 -3 -8 .05
ESA | 6 | .4 -.1 1.3 31 10 33 -.21
GFZ | 6 | 1.0 -.3 -.2 -1 -32 7 -.05
GRG | 6 | -1.6 -3.2 32.8 52 14 97 .06
JPL | 6 | -3.5 1.2 4.2 7 9 3 -.13
MIT | 6 | .0 -2.6 6.7 21 41 -8 .24
NGS | 6 | -4.5 -1.2 11.8 15 -38 -23 -.10
SIO | 6 | -2.0 2.3 -4.2 -1 27 4 .03
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 1.2039.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2039.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 2.2039.[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 3.2039.[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 5.2039.0-6). 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 2039 summary. (Feb 03, 2019 - Feb 09, 2019)
Table 1.2039.a GPS week: 2039 MJD: 58517.000-58523.000
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 249| 0 0 1 1 8 12 -.08 8 8 | -470 4 10 109
| 0 0 0 18 16 2 .03 | 147 182
emr 80| 1 0 2 0 -11 -4 .17 13 13 | 166875 730 17 155
| 1 1 1 16 16 10 .02 | 18086 706
esa 150| 0 0 0 -13 1 12 -.08 10 10 | -343 -2082 7 219
| 0 0 1 20 18 12 .01 | 388 1068
gfz 178| 1 1 1 -19 -5 -4 .11 10 10 | -138 62 11 124
| 0 0 1 18 6 6 .02 | 221 356
grg 100| 0 0 0 -35 18 46 -.19 12 10 | -41 66 11 179
| 0 0 3 14 17 8 .03 | 116 289
igr n/a| 0 0 -1 0 -14 -5 -.04 4 4 | 2342 751 10 62
| 0 0 1 8 9 10 .01 | 1734 483
jpl 80| 0 0 4 14 1 -8 .16 9 9 | 213543 676 8 96
| 1 0 1 8 17 9 .02 | 1668 570
mit 348| 0 0 -5 9 0 -27 -.05 12 12 | -15 -219 90 1651
| 0 0 0 24 22 11 .01 | 203 206
ngs 204| 0 0 -2 25 -8 -31 -.05 11 11 | 526 217 1061 2222
| 0 0 2 15 29 14 .02 | 2669 523
sio 316250| 0 0 -8 -41 72 -3 .02 16 16 | --- --- --- ---
| 1 0 2 171 228 26 .03 | --- ---
Table 1.2039.b GPS week : 2039 MJD: 58517.000-58523.000
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 4 5 4 |
3 | 4 4 4 4 3 4 5 |
4 | 19 0 28 16 17 14 17 |
5 | 5 4 4 4 4 4 4 |
6 | 3 4 4 3 3 3 3 |
7 | 4 4 4 4 3 4 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 4 3 3 3 3 3 |
10 | 3 4 4 4 4 4 7 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 4 4 5 4 |
16 | 5 5 4 5 4 5 5 |
17 | 4 4 4 4 4 6 4 |
18 | 3 3 3 3 3 3 3 |
19 | 5 4 4 4 4 5 5 |
20 | 4 3 4 4 5 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 4 3 3 4 3 3 4 |
23 | 5 5 5 5 5 6 5 |
24 | 3 3 3 4 3 3 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 5 5 4 4 4 6 |
27 | 3 3 3 3 3 3 3 |
28 | 4 4 3 3 3 4 4 |
29 | 5 5 4 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 4 3 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2039.0 GPS week: 2039 Day: 0 MJD: 58517.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 0 1 25 8 13 -.08 8 8 | -427 -85 7 122
emr 80| 0 0 2 27 -40 -10 .16 12 12 | 176180 -271 18 160
esa 150| 1 0 -1 -13 -13 10 -.08 9 9 | -211 -3133 6 219
gfz 173| 0 2 0 17 -2 -3 .12 10 11 | -485 326 13 137
grg 103| 0 0 -1 -55 -12 54 -.15 12 10 | 4 -107 13 210
igr n/a| 0 0 0 0 -17 -2 -.03 4 4 | 96 425 11 62
jpl 80| 0 -1 3 14 -28 -15 .14 8 8 | 211634 -4 7 89
mit 348| 0 -1 -5 9 16 -27 -.07 12 13 | 147 -249 47 1765
ngs 203| -2 0 0 27 -32 -26 -.07 11 11 | -443 -73 808 1859
sio 311108| 1 0 -4 -116 169 24 -.05 13 13 | --- --- --- ---
Table 2.2039.1 GPS week: 2039 Day: 1 MJD: 58518.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| -1 0 1 6 15 13 -.09 9 8 | -399 58 7 85
emr 80| 0 1 1 5 -6 -13 .17 13 13 | 176163 457 19 172
esa 150| 0 0 0 -20 0 13 -.08 10 10 | -500 -2811 7 208
gfz 178| 1 2 1 -30 -6 -5 .13 9 9 | -267 -149 11 108
grg 103| 0 0 4 -35 24 49 -.16 12 11 | -16 -1 9 145
igr n/a| 0 0 0 4 -15 1 -.04 4 4 | 728 1056 9 63
jpl 80| 0 -1 4 17 -3 -2 .16 9 9 | 211791 1031 8 90
mit 348| 0 -1 -6 37 -10 -31 -.05 13 13 | -29 -141 70 1788
ngs 210| 0 0 -3 0 -25 -55 -.07 11 11 | -422 90 892 2040
sio 312106| 0 0 -7 31 16 17 .01 13 13 | --- --- --- ---
Table 2.2039.2 GPS week: 2039 Day: 2 MJD: 58519.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| -1 0 3 -4 -1 10 -.12 8 8 | -458 49 8 114
emr 80| 1 0 2 -1 7 9 .13 13 13 | 176830 487 18 168
esa 150| 0 0 0 14 14 -3 -.06 10 10 | -780 -138 6 207
gfz 181| 0 1 4 -21 -17 -8 .13 9 10 | 160 -504 14 147
grg 104| 0 -1 -1 -26 37 49 -.18 11 11 | 101 -379 12 175
igr n/a| -1 0 -2 5 1 4 -.04 4 4 | 1881 47 10 57
jpl 80| 0 0 5 11 5 -1 .18 9 9 | 212986 122 8 105
mit 348| 0 -1 -5 -8 -11 -20 -.05 12 12 | 182 -321 101 1520
ngs 204| 0 0 -7 47 -46 -37 -.04 11 11 | -248 -316 914 2235
sio 315111| 0 0 -7 -5 34 10 .03 12 13 | --- --- --- ---
Table 2.2039.3 GPS week: 2039 Day: 3 MJD: 58520.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 0 -1 1 -32 -21 12 -.10 8 7 | -619 84 7 109
emr 80| 1 0 1 6 0 -7 .20 13 13 | 177100 1750 19 223
esa 150| 0 0 -2 -4 30 -1 -.08 10 10 | 183 -2123 7 226
gfz 182| 1 1 3 -15 1 4 .09 8 8 | -209 514 10 108
grg 104| 0 0 1 -34 37 46 -.20 12 10 | 22 -50 12 169
igr n/a| -1 1 -2 2 -4 2 -.05 4 4 | 1963 936 10 64
jpl 80| 0 0 5 15 14 -9 .17 9 9 | 213142 971 8 96
mit 348| -1 0 -5 20 -9 -24 -.04 11 11 | -324 -187 145 1690
ngs 202| 0 0 -1 36 6 -8 -.04 11 11 | -624 90 1239 2433
sio 322110| 0 0 -7 16 -55 -9 .03 13 13 | --- --- --- ---
Table 2.2039.4 GPS week: 2039 Day: 4 MJD: 58521.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 251| 0 0 0 7 13 10 -.04 7 7 | -531 -137 7 95
emr 80| 2 -1 3 10 -6 -12 .18 13 13 | 140056 1161 17 129
esa 150| 0 0 2 -42 -23 20 -.09 9 9 | 147 -3076 7 217
gfz 178| 1 0 0 -24 -3 1 .15 10 10 | -54 0 10 102
grg 99| 0 0 -1 -23 19 41 -.18 10 10 | -145 255 11 201
igr n/a| 0 0 0 3 -28 -24 -.04 4 4 | 2843 1155 10 65
jpl 80| -1 0 5 28 -9 -14 .15 9 9 | 214100 1054 9 107
mit 348| 0 0 -5 -25 28 -31 -.05 13 13 | -50 -20 139 1613
ngs 203| 0 0 0 17 5 -33 -.01 11 11 | 6571 1319 1452 2373
sio 319107| 0 1 -9 49 -43 2 .02 13 13 | --- --- --- ---
Table 2.2039.5 GPS week: 2039 Day: 5 MJD: 58522.000
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 247| 0 -1 2 -2 32 15 -.11 9 9 | -212 -253 8 108
emr 80| 2 0 3 -19 -16 -5 .18 13 13 | 140957 1325 16 114
esa 150| 0 0 1 -34 7 20 -.07 10 10 | -659 -1462 9 219
gfz 177| 1 1 0 -42 -4 -4 .08 10 10 | -204 362 11 123
grg 101| 0 0 -2 -54 16 54 -.23 14 11 | -249 501 12 193
igr n/a| 0 0 -1 -18 -18 -11 -.05 4 4 | 3752 1320 10 56
jpl 80| -1 0 4 0 5 6 .18 9 9 | 214885 1416 9 93
mit 348| 0 0 -5 38 19 -46 -.05 13 12 | 188 -610 43 1826
ngs 210| -1 0 -1 31 42 -31 -.07 11 11 | -498 80 1105 2308
sio 317106| 0 1 -7 125 -155 -13 .03 14 15 | --- --- --- ---
Table 2.2039.6 GPS week: 2039 Day: 6 MJD: 58523.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 -1 2 12 14 8 -.05 9 8 | -644 312 30 133
emr 80| 1 -1 1 -21 -22 10 .15 13 13 | 180845 201 16 125
esa 150| 0 0 -1 5 -5 29 -.08 10 10 | -581 -1834 9 237
gfz 177| 2 1 0 -19 -9 -16 .10 11 10 | 92 -115 11 143
grg 92| 0 0 4 -18 6 30 -.23 12 10 | -7 247 10 162
igr n/a| 0 0 -3 -3 -15 -6 -.06 4 4 | 5137 321 11 70
jpl 80| -1 0 1 12 26 -20 .14 8 8 | 216265 145 7 94
mit 348| 0 0 -5 -7 -36 -8 -.06 13 12 | -225 -5 88 1356
ngs 196| -1 0 -3 14 -6 -29 -.04 11 11 | -654 329 1022 2307
sio 317105| 3 0 -14 -395 540 -55 .04 36 36 | --- --- --- ---
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 3.2039.0 GPS week: 2039 Day: 0 MJD: 58517.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 9 7 6 7 4 7 6 8 13 2 | 21 22 23 22 19 20 22 20 20 30 20
2 | 7 11 7 11 10 6 8 16 16 15 4 | 20 23 22 25 20 20 22 29 22 29 21
3E | 10 12 11 10 14 3 9 8 9 12 3 | 39 38 42 39 37 38 39 38 39 42 38
X4 | 13 --- --- --- 25 27 --- --- --- --- 18 | 520 --- --- --- 448 521 --- --- --- --- 516
5E | 8 8 6 17 28 5 11 14 10 15 4 | 37 35 33 33 41 34 34 39 38 43 35
6 | 5 10 7 8 8 3 9 8 8 11 3 | 23 27 27 23 25 23 28 23 23 28 24
7 | 7 12 9 9 6 4 9 15 12 18 3 | 34 37 34 35 31 32 40 28 29 31 33
8 | 7 8 6 6 7 5 7 7 9 7 2 | 19 24 21 22 21 21 24 21 26 26 21
9 | 4 8 11 9 7 4 7 6 8 13 3 | 25 33 28 26 25 25 31 26 26 34 27
10E | 7 7 11 10 12 5 7 8 8 12 3 | 36 37 38 37 37 35 35 37 34 35 35
11 | 8 12 16 10 8 4 10 7 7 13 3 | 23 32 21 25 26 23 30 24 26 26 24
12E | 6 21 6 13 16 6 11 10 14 11 4 | 45 47 42 46 43 42 45 39 40 44 42
13 | 7 11 9 8 27 3 12 15 10 14 4 | 22 30 20 22 24 23 29 31 25 34 23
14 | 9 7 10 11 8 4 6 13 10 19 3 | 28 27 23 24 25 26 25 36 32 38 26
15 | 8 12 10 8 9 4 8 21 13 15 4 | 82 85 85 84 80 81 85 76 78 83 81
16E | 11 20 8 12 17 4 6 15 14 16 4 | 25 27 27 32 29 25 24 29 28 34 25
17 | 8 12 10 8 11 4 8 12 13 16 3 | 84 87 82 88 86 86 84 88 90 84 85
18 | 7 11 12 7 8 5 11 7 9 13 3 | 30 31 31 29 27 30 32 29 30 36 29
19 | 9 17 9 11 10 7 7 15 18 17 4 | 24 32 29 32 27 25 26 28 29 30 26
20E | 8 10 6 17 15 5 10 8 9 8 3 | 42 42 44 47 45 43 43 44 44 52 43
21 | 11 8 8 9 11 5 7 15 15 17 4 | 20 20 17 20 18 16 19 18 20 25 16
22E | 10 8 8 9 12 3 9 10 9 12 3 | 36 38 36 40 40 36 40 38 36 47 37
23 | 8 19 8 9 12 4 7 19 14 18 4 | 24 23 23 23 23 23 25 30 30 32 22
24 | 7 8 10 12 9 5 6 9 10 11 3 | 22 28 26 31 21 24 28 22 24 37 24
25E | 6 12 11 13 15 5 7 14 10 8 4 | 21 27 28 22 18 21 25 23 21 25 21
26E | 13 16 13 16 12 4 8 8 9 12 4 | 23 27 26 23 21 22 23 23 23 29 21
27 | 7 9 6 9 7 3 7 6 5 11 2 | 18 26 21 23 22 21 23 23 21 23 20
28E | 4 10 6 13 10 4 7 15 8 12 3 | 28 25 26 21 29 26 24 31 29 35 26
29 | 12 18 7 9 10 5 6 18 18 17 4 | 24 23 19 23 19 20 21 21 23 27 20
30 | 5 9 11 7 7 4 7 10 8 9 3 | 19 27 22 21 19 19 26 23 20 26 21
31 | 9 10 10 6 7 5 8 12 10 15 3 | 40 40 37 37 35 35 41 33 34 38 36
32 | 8 8 12 9 8 4 7 9 6 8 3 | 18 26 20 20 18 18 25 18 16 23 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 9 10 12 4 8 12 11 13 |T 46 33 31 32 43 45 32 31 31 36 45
WRMS | 8 12 9 11 10 4 8 13 11 13 |NE 92 24 21 23 81 92 23 22 22 29 91
MEDI | 8 10 9 9 10 4 7 10 10 13 |MD 24 28 27 25 25 25 28 29 28 34 25
Table 3.2039.1 GPS week: 2039 Day: 1 MJD: 58518.000
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 | 12 10 6 7 8 4 9 6 7 12 3 | 23 24 22 23 22 22 26 21 22 28 22
2 | 8 11 9 8 12 4 9 16 13 17 4 | 21 25 22 26 22 21 23 27 22 26 21
3E | 9 12 12 12 14 4 8 8 14 7 4 | 35 36 36 37 35 36 38 37 38 38 36
X4 | 2 --- --- --- --- 108 --- --- --- --- 0 | 645 --- --- --- --- 598 --- --- --- --- 646
5E | 7 10 11 13 14 4 11 15 12 12 4 | 27 28 28 26 29 25 27 28 31 32 26
6 | 10 13 11 10 10 4 7 10 7 6 3 | 25 32 26 24 24 22 27 24 20 27 24
7 | 5 13 10 6 6 3 9 13 11 16 3 | 23 29 23 24 22 22 28 21 22 24 22
8M | 13 10 7 6 7 4 8 8 7 6 3 | 22 24 21 22 22 20 24 20 20 23 20
9M | 5 12 14 8 8 4 7 13 12 11 3 | 21 31 24 23 23 22 28 25 23 30 23
10E | 10 8 13 14 14 4 9 13 9 11 4 | 33 37 37 35 38 34 35 39 36 38 35
11M | 6 11 15 8 10 4 10 6 7 16 3 | 22 27 23 24 23 22 28 20 21 19 21
12E | 8 19 5 8 22 5 13 11 12 11 4 | 43 46 40 40 38 39 44 41 37 40 40
13 | 7 13 10 9 32 6 13 14 12 15 5 | 24 32 23 24 36 24 31 33 23 33 26
14 | 8 8 9 9 7 4 8 16 13 20 4 | 13 18 14 18 17 18 16 28 25 30 17
15 | 8 12 11 7 9 3 10 18 14 16 4 | 63 65 64 63 60 62 66 60 58 60 62
16E | 18 17 9 10 13 6 7 15 15 12 4 | 24 26 26 27 32 24 25 25 24 26 24
17M | 10 16 11 10 9 3 9 13 14 12 4 | 77 78 74 81 80 77 77 82 78 79 78
18M | 6 11 11 7 9 3 8 6 6 12 3 | 28 31 34 31 29 30 32 30 30 36 30
19M | 8 17 8 10 10 4 9 16 14 16 4 | 33 35 33 38 35 33 35 40 34 36 34
20E | 7 12 5 10 12 4 10 10 6 8 3 | 33 33 34 34 31 32 33 34 33 34 32
21 | 12 8 7 9 9 4 7 16 13 17 4 | 21 20 18 20 18 16 21 18 18 16 16
22E | 7 9 6 7 14 3 9 11 11 10 3 | 23 24 24 25 29 22 22 23 25 27 23
23M | 7 20 11 9 12 5 7 18 18 20 4 | 22 19 15 21 18 21 22 24 25 25 19
24 | 6 7 10 8 7 3 6 9 13 10 3 | 23 30 25 32 23 25 29 23 23 35 26
25E | 6 11 11 9 17 5 7 13 7 9 3 | 23 27 29 25 21 23 26 21 22 25 22
26E | 12 26 13 11 16 4 9 19 10 12 5 | 38 41 37 41 43 38 38 42 39 40 38
27 | 8 11 8 5 9 3 7 8 7 8 2 | 20 28 23 21 25 22 26 24 23 24 22
28E | 9 14 8 9 10 3 8 14 11 13 3 | 23 27 28 26 29 28 25 36 32 37 27
29M | 10 19 8 9 7 5 8 18 13 19 4 | 24 22 20 23 21 20 21 21 22 25 20
30 | 7 9 11 6 6 5 7 10 7 7 3 | 19 28 22 21 21 20 27 23 16 23 20
31M | 8 12 10 7 8 3 9 13 13 16 3 | 28 31 27 25 27 25 32 28 26 27 26
32 | 8 9 11 7 7 5 8 13 8 12 3 | 20 30 21 24 21 21 25 23 20 25 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 9 12 4 9 13 11 13 |T 47 31 28 29 29 45 30 30 28 31 47
WRMS | 8 13 10 9 11 4 9 13 11 13 |NE 109 25 20 23 21 103 23 22 21 26 110
MEDI | 8 12 10 9 10 4 8 13 12 12 |MD 23 29 25 25 25 23 27 25 24 28 24
Table 3.2039.2 GPS week: 2039 Day: 2 MJD: 58519.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 10 7 4 9 5 7 6 8 13 2 | 21 25 23 22 21 20 24 20 23 32 22
2M | 7 15 11 7 13 5 8 17 12 14 4 | 20 24 23 27 20 21 20 27 24 26 21
3E | 7 10 12 14 12 4 10 9 11 9 3 | 17 19 22 17 20 18 21 19 20 22 17
X4 | 23 --- --- --- 34 36 --- --- --- --- 28 | 318 --- --- --- 415 320 --- --- --- --- 314
5E | 9 10 7 9 12 4 12 12 11 11 3 | 35 34 33 34 34 31 33 31 35 34 33
6M | 9 11 11 9 11 6 7 10 6 12 3 | 24 25 24 22 20 22 25 21 21 27 22
7M | 6 13 10 9 6 3 8 15 12 15 3 | 26 28 27 29 24 24 32 23 21 25 25
8 | 8 8 6 7 8 3 7 7 8 8 2 | 20 24 21 22 21 20 22 20 21 21 20
9 | 5 10 13 8 8 3 8 9 8 8 3 | 28 37 32 35 29 30 35 30 33 38 32
10E | 7 9 12 12 13 3 10 9 8 8 3 | 21 22 24 19 24 20 23 24 24 25 21
11 | 8 13 15 9 12 4 11 7 8 12 3 | 24 32 19 28 26 22 28 21 23 21 23
12E | 8 22 6 6 19 6 13 10 14 11 4 | 24 27 24 27 26 25 26 25 28 28 24
13M | 6 11 9 9 12 4 11 11 11 13 3 | 21 30 21 19 29 22 29 28 28 27 23
14 | 10 7 9 10 8 4 9 16 17 20 4 | 21 22 20 25 22 23 20 28 27 33 21
15M | 7 13 10 10 11 4 10 18 14 13 4 | 70 73 71 73 68 69 76 67 65 67 70
16E | 9 17 7 12 9 5 9 17 11 12 4 | 25 23 28 30 27 25 23 28 26 25 24
17 | 7 16 11 7 13 3 7 12 11 13 3 | 88 93 87 91 93 91 93 95 92 95 91
18 | 7 11 10 6 6 3 8 6 8 11 2 | 23 24 25 23 23 21 24 21 21 29 22
19 | 8 16 10 7 14 6 7 15 13 15 4 | 24 30 27 32 31 28 28 29 29 28 27
20E | 10 10 6 12 18 4 12 7 12 7 4 | 28 29 31 31 36 29 30 29 34 32 29
21 | 11 8 5 5 10 4 8 15 13 15 3 | 26 27 22 23 22 21 25 21 21 21 21
22E | 7 8 7 8 11 4 9 11 9 10 3 | 31 33 32 33 31 31 34 32 35 35 32
23 | 5 19 11 8 11 4 8 18 14 19 4 | 20 19 18 22 21 19 22 24 22 24 19
24 | 6 7 12 7 8 4 7 11 10 12 3 | 17 25 22 25 16 18 25 15 16 27 19
25E | 12 12 12 9 16 4 8 12 9 9 4 | 23 29 30 26 23 23 26 22 24 24 23
26E | 10 16 13 19 12 4 10 10 11 9 4 | 55 58 60 56 55 54 55 58 57 57 55
27 | 9 9 7 7 9 4 7 9 8 10 3 | 21 24 21 21 22 19 21 20 22 19 20
28E | 7 11 6 6 10 4 8 11 10 8 3 | 22 24 23 24 25 24 24 29 28 31 24
29 | 9 22 6 9 8 4 7 17 16 14 4 | 26 27 21 25 25 23 23 23 25 23 23
30M | 5 10 12 7 10 3 7 12 7 8 3 | 39 45 40 41 43 41 46 46 43 45 42
31 | 6 10 10 8 7 3 10 12 13 14 3 | 70 73 71 69 67 68 73 69 71 70 70
32 | 8 10 11 6 8 4 8 11 11 10 3 | 17 27 19 23 18 18 25 19 16 20 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 9 11 4 9 12 11 12 |T 38 33 31 32 43 38 32 31 31 33 38
WRMS | 8 13 10 10 11 4 9 12 11 13 |NE 63 25 21 23 76 62 23 20 20 25 62
MEDI | 8 11 10 8 11 4 8 11 11 12 |MD 24 27 24 26 25 23 25 25 25 27 23
Table 3.2039.3 GPS week: 2039 Day: 3 MJD: 58520.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 10 7 6 9 4 9 5 6 15 3 | 18 22 19 20 19 19 23 22 20 35 20
2 | 5 13 9 10 11 4 7 16 14 15 4 | 17 21 19 24 18 18 20 22 22 21 18
3E | 8 10 12 10 14 5 9 7 7 7 3 | 21 25 28 17 19 20 24 21 23 20 20
X4 | 11 --- --- --- 22 30 --- --- --- --- 16 | 235 --- --- --- 137 238 --- --- --- --- 235
5E | 9 9 7 8 15 4 12 12 8 11 3 | 30 31 28 26 28 27 27 30 28 31 27
6 | 6 12 10 7 9 3 8 7 8 8 3 | 20 28 24 22 20 21 26 21 22 26 22
7 | 6 13 11 7 6 3 9 12 11 15 3 | 37 43 36 39 34 36 42 34 37 38 36
8 | 6 8 8 7 9 4 9 8 7 7 2 | 18 21 20 17 20 18 22 20 16 21 18
9 | 7 8 12 8 8 5 8 8 11 12 3 | 20 28 23 25 22 21 28 21 24 28 22
10E | 10 8 13 14 12 5 12 9 8 10 4 | 21 24 26 20 21 21 23 25 21 27 21
11 | 7 13 16 7 11 5 10 5 6 12 3 | 19 29 17 23 23 18 28 19 21 18 20
12E | 7 23 7 8 25 8 13 11 15 13 5 | 30 29 28 31 28 28 30 29 30 30 27
13 | 6 11 9 8 8 4 11 11 13 15 3 | 25 34 24 25 26 27 32 31 33 30 27
14 | 9 7 9 8 8 4 9 16 16 22 4 | 16 18 14 16 17 20 17 28 24 34 17
15 | 8 12 10 8 10 4 11 16 15 13 4 | 72 76 70 72 71 68 74 67 68 67 70
16E | 10 22 8 10 8 5 9 13 16 15 4 | 22 26 24 23 22 21 21 26 23 28 21
17 | 7 12 10 9 10 3 7 11 11 12 3 | 108 114 109 113 107 111 108 111 108 110 109
18 | 6 10 11 6 6 2 9 6 6 16 3 | 23 21 24 21 23 20 24 21 19 32 21
19 | 7 17 9 8 10 5 8 13 15 15 4 | 22 22 23 27 23 22 23 25 22 25 22
20E | 7 11 6 10 19 6 12 6 6 6 3 | 39 35 39 37 44 37 39 34 37 41 38
21 | 11 9 8 5 9 4 8 14 11 16 3 | 20 22 19 19 17 18 23 20 17 19 17
22E | 8 8 8 7 29 3 6 10 10 12 4 | 23 25 24 23 38 23 25 24 25 27 23
23 | 6 21 11 11 11 6 8 20 19 21 5 | 18 21 18 20 19 19 19 25 24 23 17
24 | 8 6 11 9 9 4 8 10 16 11 3 | 18 26 21 27 15 17 26 17 20 26 20
25E | 9 10 11 7 17 4 7 12 8 9 3 | 26 30 32 27 24 26 28 22 25 31 25
26E | 7 15 14 14 14 3 9 8 10 9 4 | 122 124 126 123 122 124 126 125 127 123 124
27 | 6 9 9 7 10 3 7 10 5 11 3 | 21 22 21 20 20 20 24 24 19 19 20
28E | 7 11 6 8 11 4 7 12 11 10 3 | 17 21 21 16 22 21 18 27 26 29 20
29 | 9 20 8 5 8 6 8 17 15 13 4 | 25 22 20 22 22 19 22 22 21 25 21
30 | 7 10 11 6 7 2 8 8 5 10 3 | 90 93 87 87 89 89 90 90 88 91 89
31 | 9 12 10 7 8 4 11 11 13 15 3 | 132 134 135 135 133 133 136 134 133 131 134
32 | 7 8 11 6 7 4 9 9 11 13 3 | 19 24 19 20 18 16 25 17 17 21 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 8 12 4 9 11 11 13 |T 42 39 36 36 39 41 38 37 36 39 41
WRMS | 7 13 10 8 10 4 9 11 11 13 |NE 49 22 18 20 34 49 23 21 19 25 49
MEDI | 7 11 10 8 10 4 9 11 11 12 |MD 22 26 24 23 22 21 25 25 24 28 21
Table 3.2039.4 GPS week: 2039 Day: 4 MJD: 58521.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 10 7 8 9 6 9 5 7 11 3 | 22 24 20 22 20 20 23 20 18 30 20
2 | 6 9 8 12 12 4 9 16 12 17 4 | 16 20 20 27 18 19 20 18 19 26 17
3E | 7 11 11 11 9 4 8 9 7 6 3 | 28 30 30 24 27 25 26 25 23 27 25
X4 | 14 --- --- --- 20 28 --- --- --- --- 17 | 309 --- --- --- 229 301 --- --- --- --- 308
5E | 8 11 6 12 12 2 10 12 10 14 3 | 28 27 23 24 28 25 27 31 30 35 26
6 | 5 11 9 7 9 5 8 9 8 8 3 | 18 25 23 22 20 21 24 21 22 28 21
7 | 4 13 10 6 6 3 9 12 9 15 3 | 37 39 36 38 34 36 38 35 38 38 36
8 | 10 12 6 8 7 4 9 9 7 8 3 | 23 28 21 22 22 21 24 21 21 22 21
9 | 5 11 13 8 8 4 9 10 10 11 3 | 23 30 26 26 23 23 28 25 26 29 24
10E | 9 10 12 11 18 4 9 11 7 9 4 | 25 27 26 23 23 25 25 28 23 28 23
11 | 8 13 14 7 11 5 9 5 9 10 3 | 18 27 15 21 19 17 26 17 20 15 18
12E | 8 22 5 16 16 6 13 10 14 12 4 | 28 29 27 33 30 26 29 27 27 29 27
13 | 6 11 8 11 9 5 12 12 13 15 3 | 36 42 35 36 40 36 41 40 37 41 37
14 | 8 9 11 8 9 4 8 18 13 23 4 | 14 17 14 20 18 18 17 27 22 33 17
15 | 8 12 10 9 11 5 9 19 14 16 4 | 50 57 52 53 49 49 55 47 51 47 51
16E | 7 20 8 11 8 4 8 13 10 9 3 | 23 25 24 27 25 23 22 27 21 25 22
17 | 7 17 10 6 9 4 8 12 11 11 3 | 71 73 70 73 72 70 71 70 70 71 71
18 | 6 11 10 7 7 3 9 6 8 11 3 | 26 24 27 25 23 24 27 22 23 31 24
19 | 5 22 8 8 10 6 6 16 14 14 4 | 17 22 19 22 18 19 20 21 21 22 17
20E | 10 15 7 17 11 4 13 18 7 9 4 | 43 43 43 50 42 46 46 50 45 52 44
21 | 10 10 5 9 10 4 8 17 12 17 4 | 22 20 19 23 19 18 24 18 19 21 18
22E | 7 11 7 5 8 3 9 8 9 10 3 | 20 21 20 22 20 18 21 22 19 25 19
23 | 7 20 8 12 10 5 7 20 15 20 4 | 21 21 17 23 18 19 17 24 21 23 17
24 | 8 7 12 9 10 3 7 10 10 12 3 | 17 26 20 27 17 19 26 16 19 29 20
25E | 6 11 10 11 13 5 7 12 10 11 3 | 25 27 26 28 19 22 25 20 22 25 22
26E | 7 17 12 12 14 4 8 8 12 9 4 | 251 253 248 250 251 251 249 248 246 249 250
27 | 7 11 8 8 9 3 7 12 10 10 3 | 20 25 21 19 21 20 23 22 23 20 19
28E | 5 11 6 11 12 5 9 14 7 8 3 | 27 28 27 24 28 27 27 31 31 32 27
29 | 7 18 5 12 8 7 7 16 15 13 4 | 25 21 19 26 23 20 21 20 21 25 21
30 | 8 10 13 7 8 3 8 9 6 8 3 | 133 134 134 136 135 132 133 136 134 134 134
31 | 7 10 9 9 9 4 11 11 13 15 3 | 195 193 193 193 193 195 194 192 191 194 193
32 | 6 12 13 7 8 3 7 11 12 10 3 | 17 29 20 22 18 18 24 19 17 23 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 9 10 10 4 9 13 11 13 |T 50 45 42 44 48 50 44 43 42 46 50
WRMS | 7 13 9 10 10 4 9 13 11 13 |NE 60 23 19 22 48 59 22 20 19 26 60
MEDI | 7 11 9 9 9 4 9 12 10 11 |MD 25 27 24 25 23 23 26 25 23 29 22
Table 3.2039.5 GPS week: 2039 Day: 5 MJD: 58522.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 10 7 9 11 3 8 9 5 15 3 | 17 21 19 20 21 18 23 19 19 34 19
2 | 7 10 10 14 15 5 7 17 15 15 4 | 17 23 23 30 19 19 23 22 17 31 19
3E | 9 9 13 14 10 3 7 10 10 10 3 | 25 26 28 25 25 26 26 29 27 32 25
X4 | 11 --- --- --- 18 31 --- --- --- --- 14 | 215 --- --- --- 169 205 --- --- --- --- 212
5E | 9 9 6 11 15 4 9 14 12 19 4 | 33 35 36 37 39 36 38 37 38 41 35
6 | 7 10 10 9 8 4 7 9 10 12 3 | 17 25 22 25 21 20 26 19 19 31 21
7 | 8 11 10 8 9 3 8 13 12 17 3 | 55 56 53 56 53 54 55 55 55 55 54
8 | 9 9 7 10 10 4 7 7 10 9 3 | 25 29 27 26 25 26 28 27 27 27 25
9 | 6 11 13 5 9 4 8 6 9 11 3 | 20 29 23 23 22 21 27 22 21 31 22
10E | 9 7 13 15 18 5 10 9 8 9 4 | 25 27 27 24 21 24 26 29 27 31 24
11 | 8 12 15 11 16 8 8 7 7 14 4 | 18 26 18 22 21 18 26 16 19 21 18
12E | 8 21 6 9 21 6 12 12 13 13 4 | 28 31 27 29 34 27 29 30 27 33 27
13 | 7 11 10 11 8 4 11 13 13 16 4 | 62 64 60 56 64 62 65 61 59 61 61
14 | 8 7 8 8 9 3 8 19 15 22 4 | 22 25 23 27 24 25 26 32 29 39 25
15 | 10 11 11 11 10 5 10 19 14 16 4 | 98 99 97 99 94 97 101 96 94 96 97
16E | 11 24 8 8 10 6 7 16 12 13 4 | 24 24 23 23 23 20 21 24 22 24 21
17 | 11 13 12 11 45 6 15 15 11 12 6 | 242 237 238 240 237 240 238 242 241 235 239
18 | 5 12 12 8 8 3 8 7 6 16 3 | 22 22 25 21 22 22 26 24 23 38 22
19 | 8 21 7 12 13 6 7 16 16 16 4 | 14 20 19 24 19 19 22 21 20 25 17
20E | 10 11 6 16 14 4 11 10 13 9 4 | 67 67 70 74 67 70 71 72 70 76 70
21 | 15 11 5 7 10 5 9 16 17 16 4 | 21 20 17 20 19 17 23 19 20 26 17
22E | 6 9 6 8 8 3 10 7 8 12 3 | 30 31 33 32 33 31 33 30 29 39 30
23 | 9 20 13 11 10 5 8 24 17 24 5 | 16 22 19 20 15 15 16 22 19 24 14
24 | 7 6 12 9 8 4 10 10 10 11 3 | 17 25 21 27 16 17 26 15 15 29 20
25E | 8 11 10 9 16 4 9 10 6 9 3 | 24 28 28 27 18 23 27 22 21 28 23
26 | 15 12 12 12 15 4 9 8 9 10 4 | 312 310 308 315 314 309 310 310 311 309 311
27 | 9 9 7 9 11 4 8 10 7 10 3 | 20 22 21 17 20 18 21 20 19 26 18
28E | 15 10 7 8 10 4 7 13 12 13 3 | 14 20 21 18 18 21 19 28 26 34 19
29 | 11 16 6 10 8 6 7 16 15 17 4 | 22 21 18 25 20 20 21 20 21 28 20
30 | 5 9 12 8 9 3 6 9 8 11 3 | 189 190 188 190 191 190 193 188 188 185 190
31 | 7 12 10 7 9 4 9 11 13 16 3 | 243 243 239 241 240 241 241 243 242 246 241
32 | 10 9 10 6 7 3 7 11 9 14 3 | 16 26 17 20 16 17 25 19 18 27 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 10 14 4 9 13 11 14 |T 61 59 57 59 60 61 59 58 57 63 61
WRMS | 9 13 10 10 11 4 9 12 11 15 |NE 46 23 19 21 40 45 24 20 20 30 47
MEDI | 8 11 10 9 10 4 8 11 11 13 |MD 24 26 25 26 22 23 26 27 26 32 23
Table 3.2039.6 GPS week: 2039 Day: 6 MJD: 58523.000
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 5 10 4 8 8 7 33 3 | 21 24 23 21 19 21 24 23 22 57 21
2 | 8 10 9 11 10 4 7 16 15 37 4 | 17 18 18 26 17 17 18 19 20 44 17
3E | 8 13 14 20 15 5 8 11 12 31 5 | 36 36 37 35 37 35 35 39 35 59 35
X4 | 15 --- --- --- 19 32 --- --- --- --- 16 | 297 --- --- --- 214 287 --- --- --- --- 292
5E | 10 12 7 9 15 4 7 16 12 35 4 | 40 42 41 42 41 40 40 43 46 63 41
6 | 10 10 10 7 7 3 7 9 7 39 3 | 23 26 29 27 24 24 27 24 21 58 24
7 | 6 13 8 7 8 4 8 12 12 37 3 | 67 71 68 67 64 65 70 62 63 82 66
8 | 8 10 5 11 8 5 6 8 10 31 3 | 23 25 23 22 24 22 27 24 23 54 23
9 | 8 10 11 7 9 4 8 7 7 36 3 | 21 29 26 26 22 23 28 26 23 59 24
10E | 13 8 17 35 16 5 8 11 8 36 6 | 33 36 35 43 36 33 36 36 34 53 33
11 | 9 10 15 7 14 4 8 6 7 31 3 | 21 29 21 22 24 20 29 22 22 47 22
12E | 6 24 7 9 18 6 12 13 14 36 5 | 35 36 31 36 34 32 37 32 30 64 33
13 | 7 10 8 9 9 6 10 14 13 43 3 | 57 60 55 58 58 56 58 63 60 75 57
14 | 7 7 7 7 9 3 8 18 13 42 3 | 28 27 25 29 28 29 28 41 32 68 28
15 | 8 9 9 7 10 4 9 17 15 42 4 | 177 183 179 176 176 176 180 175 178 184 178
16E | 11 19 9 7 14 5 9 18 12 38 4 | 27 27 26 29 30 24 24 28 23 62 24
17 | 9 16 11 14 10 5 8 11 10 35 4 | 212 209 209 216 212 213 209 217 211 218 211
18 | 5 11 10 7 7 4 8 9 8 33 3 | 26 27 29 27 25 26 28 30 30 52 27
19 | 10 22 9 14 9 5 7 15 15 34 4 | 19 21 19 27 21 19 21 22 23 62 19
20E | 9 12 5 11 13 5 12 9 9 37 4 | 71 70 72 75 72 71 69 72 74 105 71
21 | 13 11 7 7 8 4 8 15 14 41 4 | 23 22 19 23 19 18 22 22 20 57 19
22E | 13 10 5 5 9 4 10 6 9 33 3 | 43 41 41 43 39 40 42 41 41 75 41
23 | 6 21 9 7 11 5 6 22 12 34 4 | 22 23 20 27 24 22 23 31 24 59 21
24 | 5 7 14 8 9 3 9 8 8 32 3 | 19 26 21 25 15 19 26 17 18 57 20
25E | 9 10 10 10 12 3 8 11 5 36 3 | 30 31 31 30 24 29 31 27 29 66 28
26 | 12 23 15 13 30 5 10 11 10 38 6 | 369 369 371 368 370 369 370 370 368 375 369
27 | 8 9 5 7 8 4 7 6 9 33 3 | 20 22 19 17 21 18 21 21 19 48 19
28E | 8 10 7 13 11 4 7 14 11 40 4 | 23 24 24 19 21 23 22 29 31 66 22
29 | 9 15 7 9 10 4 7 17 14 39 4 | 25 22 21 26 22 21 21 21 23 58 22
30 | 6 8 11 7 10 2 7 7 6 36 3 | 236 236 234 234 235 236 234 237 236 240 235
31 | 7 11 9 7 6 4 8 13 14 34 3 | 321 321 322 322 323 321 323 321 322 325 322
32 | 9 10 10 6 5 3 9 12 7 40 3 | 18 26 21 21 18 18 25 19 17 53 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 11 12 4 8 13 11 36 |T 75 69 68 69 72 73 69 69 68 95 74
WRMS | 8 13 10 10 10 4 8 12 11 36 |NE 60 24 21 22 47 58 24 23 21 56 59
MEDI | 8 10 9 7 10 4 8 11 10 36 |MD 27 29 29 29 25 26 28 30 30 62 27
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2039 GPS week: 2039 MJD: 58517.0-58523.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 9 9 22 |U 15 16 57 |U 10 16 29 |
emr | emr 2975 |U 17 15 42 |U 19 24 61 |U 12 20 37 |
esa | esa 2976 | 10 12 28 |U 15 16 61 | 9 16 29 |
gfz | gfz 2975 |U 9 11 23 |U 15 17 60 |U 12 17 30 |
grg | grg 3055 |U 9 10 24 |U 15 18 59 | 12 20 31 |
igr | igr 2974 | 10 9 24 | 14 16 57 | 10 15 28 |
igs | igs 3042 | 10 10 26 | 14 16 58 | 9 16 26 |
jpl | jpl 2976 |U 14 14 40 |U 15 18 65 |U 10 20 33 |
mit | mit 2976 |U 15 15 39 |U 27 32 130 |U 17 18 43 |
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 5.2039.0 GPS week: 2039 Day: 0 MJD: 58517.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 8 9 20 | 12 16 60 | 10 16 34 |
emr | emr 2976 | 16 13 35 | 21 22 59 | 13 15 46 |
esa | esa 2976 | 8 9 27 | 12 15 62 | 9 16 34 |
gfz | gfz 2976 | 7 8 22 | 14 18 68 | 10 19 35 |
grg | grg 3072 | 8 7 21 | 13 19 59 | 11 22 37 |
igr | igr 2975 | 8 7 22 | 12 17 62 | 9 16 33 |
igs | igs 3063 | 8 7 24 | 12 16 61 | 9 17 34 |
jpl | jpl 2976 | 14 12 38 | 13 17 72 | 11 21 40 |
mit | mit 2976 | 8 7 23 | 13 21 81 | 11 16 37 |
Table 5.2039.1 GPS week: 2039 Day: 1 MJD: 58518.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 8 18 | 15 18 56 | 10 12 28 |
emr | emr 2976 | 18 12 35 | 21 23 62 | 15 12 40 |
esa | esa 2976 | 10 10 27 | 15 16 57 | 9 15 31 |
gfz | gfz 2975 | 9 8 21 | 15 20 58 | 10 14 30 |
grg | grg 2973 | 9 7 19 | 15 18 54 | 12 17 33 |
igr | igr 2975 | 9 7 21 | 15 18 52 | 9 13 28 |
igs | igs 2976 | 9 7 22 | 15 18 54 | 9 13 27 |
jpl | jpl 2976 | 13 12 38 | 17 18 58 | 9 19 32 |
mit | mit 2976 | 16 24 41 | 20 30 77 | 16 14 29 |
Table 5.2039.2 GPS week: 2039 Day: 2 MJD: 58519.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 8 18 | 14 12 45 | 10 15 30 |
emr | emr 2976 | 13 12 31 | 17 22 59 | 9 18 32 |
esa | esa 2976 | 8 9 22 | 13 13 53 | 9 16 26 |
gfz | gfz 2976 | 7 10 19 | 13 12 49 | 11 17 31 |
grg | grg 3072 | 6 6 18 | 14 16 55 | 12 17 28 |
igr | igr 2976 | 8 8 19 | 13 12 51 | 9 14 27 |
igs | igs 3072 | 8 8 19 | 13 13 50 | 9 15 25 |
jpl | jpl 2976 | 10 13 34 | 14 16 55 | 10 18 28 |
mit | mit 2976 | 13 10 32 | 24 41 86 | 20 35 65 |
Table 5.2039.3 GPS week: 2039 Day: 3 MJD: 58520.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 9 8 22 | 15 23 62 | 11 17 27 |
emr | emr 2976 | 17 15 40 | 17 29 62 | 11 19 36 |
esa | esa 2976 | 9 11 27 | 16 18 63 | 10 16 27 |
gfz | gfz 2976 | 9 10 23 | 15 21 63 | 13 18 26 |
grg | grg 3071 | 8 9 23 | 18 24 63 | 13 22 30 |
igr | igr 2972 | 9 8 24 | 15 22 62 | 11 15 27 |
igs | igs 3071 | 9 9 25 | 15 21 62 | 10 17 24 |
jpl | jpl 2976 | 15 13 39 | 16 20 77 | 10 21 31 |
mit | mit 2976 | 29 24 55 | 78 79 442 | 22 15 65 |
Table 5.2039.4 GPS week: 2039 Day: 4 MJD: 58521.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 12 13 25 | 32 24 76 | 11 17 30 |
emr | emr 2975 | 19 21 52 | 33 27 70 | 10 19 32 |
esa | esa 2976 | 12 16 33 | 30 23 81 | 9 16 28 |
gfz | gfz 2975 | 12 17 28 | 31 23 74 | 13 19 34 |
grg | grg 3070 | 11 16 27 | 28 25 77 | 12 19 36 |
igr | igr 2975 | 12 13 28 | 31 23 73 | 10 16 28 |
igs | igs 3071 | 12 15 29 | 32 23 78 | 10 17 27 |
jpl | jpl 2976 | 16 19 44 | 33 22 82 | 10 22 31 |
mit | mit 2976 | 20 20 51 | 34 23 91 | 20 18 44 |
Table 5.2039.5 GPS week: 2039 Day: 5 MJD: 58522.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 7 25 | 7 8 48 | 10 18 31 |
emr | emr 2976 | 18 16 48 | 11 20 51 | 12 26 36 |
esa | esa 2976 | 10 11 31 | 7 19 51 | 9 18 31 |
gfz | gfz 2975 | 10 10 25 | 7 13 51 | 12 17 31 |
grg | grg 3065 | 8 8 31 | 8 17 43 | 15 29 36 |
igr | igr 2975 | 10 8 28 | 6 15 46 | 10 17 29 |
igs | igs 3071 | 10 9 30 | 6 15 44 | 9 18 28 |
jpl | jpl 2976 | 14 15 43 | 7 22 52 | 11 27 36 |
mit | mit 2976 | 10 8 28 | 7 13 57 | 10 14 27 |
Table 5.2039.6 GPS week: 2039 Day: 6 MJD: 58523.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 12 12 24 | 9 10 52 | 10 16 24 |
emr | emr 2976 | 19 16 49 | 12 25 68 | 14 30 33 |
esa | esa 2976 | 12 16 31 | 10 9 60 | 10 14 24 |
gfz | gfz 2976 | 13 14 26 | 9 9 60 | 11 14 23 |
grg | grg 3067 | 13 15 29 | 10 11 63 | 11 15 21 |
igr | igr 2976 | 13 12 27 | 9 9 55 | 10 12 22 |
igs | igs 2976 | 14 13 32 | 9 9 57 | 10 15 21 |
jpl | jpl 2976 | 18 17 46 | 9 11 61 | 11 16 31 |
mit | mit 2976 | 11 14 42 | 15 15 74 | 21 15 36 |
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 6.2039 GPS week: 2039 MJD: 58517.500-58523.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -13 -8 40 28 -3 | 3 21
| 17 19 120 24 6 | 3
emr uuuuu | 10 9 -98 4 0 | 29 35
| 16 23 49 34 7 | 1
esa uuuuu | -15 -1 62 -70 3 | 12 24
| 23 18 66 42 3 | 1
gfz uuuuu | 9 22 -9 32 1 | 23 30
| 28 19 62 88 5 | 2
grg uuuuu | 1 41 -14 54 -3 | -3 20
| 19 20 38 42 4 | 2
igr xxxxx | 13 -1 20 37 1 | -3 19
| 20 12 28 41 3 | 1
irf xxxxx | 2 -8 18 -7 1 | -2 20
| 12 12 15 25 1 | 2
jpl uuuuu | -1 -11 -34 -75 1 | 17 25
| 24 13 47 43 7 | 2
mit uuuuu | 9 -23 50 18 -2 | 15 25
| 11 21 32 46 1 | 2
ngs uuuuu | 10 -24 -21 42 4 | 5 20
| 38 39 124 128 4 | 1
Table 7.2039.0 GPS week: 2039 Day: 0 MJD: 58517.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -27 -10 -26 37 -9 | 6 22
emr uuuuu | 31 3 -136 -25 -9 | 29 34
esa uuuuu | -24 11 -21 -99 -2 | 13 24
gfz uuuuu | -37 -13 96 25 4 | 22 29
grg uuuuu | 16 81 6 6 0 | -2 19
igr xxxxx | -10 10 -6 -50 -1 | -3 20
irf xxxxx | -8 -8 32 -9 2 | -1 21
jpl uuuuu | 20 -25 66 -83 9 | 15 24
mit uuuuu | 12 -55 97 41 0 | 17 26
ngs uuuuu | 26 34 -117 134 3 | 4 20
Table 7.2039.1 GPS week: 2039 Day: 1 MJD: 58518.500
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 | -21 -5 -80 10 -10 | 5 23
emr uuuuu | -6 -23 -6 -44 -2 | 27 33
esa uuuuu | -14 1 83 -107 1 | 11 24
gfz uuuuu | -19 29 19 -94 6 | 22 29
grg uuuuu | -21 38 -67 65 3 | -3 20
igr xxxxx | 19 -14 38 25 -1 | -3 20
irf xxxxx | 17 -6 34 -14 1 | -2 21
jpl uuuuu | 20 -23 -42 -37 3 | 16 24
mit uuuuu | 26 -28 71 23 -3 | 17 26
ngs uuuuu | 45 6 49 230 1 | 4 20
Table 7.2039.2 GPS week: 2039 Day: 2 MJD: 58519.500
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 0 -19 30 -6 | 7 24
emr uuuuu | -8 3 -116 24 -5 | 31 37
esa uuuuu | -43 -31 87 -121 3 | 14 26
gfz uuuuu | 10 40 -76 -67 6 | 26 33
grg uuuuu | -23 48 18 75 -1 | 0 21
igr xxxxx | -13 -11 22 53 -2 | 0 20
irf xxxxx | 0 -31 15 29 -1 | 1 22
jpl uuuuu | 11 10 -61 -74 5 | 20 28
mit uuuuu | 20 -18 55 86 -1 | 19 28
ngs uuuuu | 48 -63 126 115 1 | 7 22
Table 7.2039.3 GPS week: 2039 Day: 3 MJD: 58520.500
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 25 68 55 -3 | 4 22
emr uuuuu | -5 4 -66 52 0 | 30 36
esa uuuuu | -41 -14 43 -66 4 | 12 25
gfz uuuuu | 18 15 -68 30 -7 | 26 33
grg uuuuu | 1 39 -69 25 -2 | -2 20
igr xxxxx | 16 -12 -18 52 2 | -2 20
irf xxxxx | 1 -14 -5 -15 1 | -2 21
jpl uuuuu | -11 -4 -36 -67 -7 | 18 26
mit uuuuu | -5 -19 37 6 -2 | 15 25
ngs uuuuu | 7 -59 53 -40 11 | 6 21
Table 7.2039.4 GPS week: 2039 Day: 4 MJD: 58521.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -26 -10 -65 -8 -2 | 1 20
emr uuuuu | 17 12 -126 18 -3 | 29 34
esa uuuuu | 22 23 154 -45 7 | 10 23
gfz uuuuu | 23 23 3 128 4 | 23 30
grg uuuuu | -4 25 -11 28 -5 | -4 19
igr xxxxx | 29 -2 60 78 1 | -3 19
irf xxxxx | 16 1 22 23 3 | -4 20
jpl uuuuu | 6 -22 -41 -14 -5 | 16 25
mit uuuuu | 5 5 49 50 -3 | 14 23
ngs uuuuu | -30 -46 31 -135 7 | 5 20
Table 7.2039.5 GPS week: 2039 Day: 5 MJD: 58522.500
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 -21 220 60 0 | 1 20
emr uuuuu | 21 10 -146 23 14 | 28 34
esa uuuuu | -3 13 109 -2 7 | 12 23
gfz uuuuu | 43 43 -59 130 -5 | 24 30
grg uuuuu | 15 21 15 50 -9 | -5 20
igr xxxxx | 40 8 36 48 6 | -2 18
irf xxxxx | 7 3 28 -23 0 | -3 19
jpl uuuuu | 0 -9 -43 -139 7 | 16 25
mit uuuuu | -4 -1 47 -27 -3 | 14 23
ngs uuuuu | -53 -47 -240 -63 0 | 7 19
Table 7.2039.6 GPS week: 2039 Day: 6 MJD: 58523.500
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 -38 182 15 7 | -2 18
emr uuuuu | 22 53 -91 -17 2 | 28 34
esa uuuuu | -4 -9 -23 -49 5 | 11 21
gfz uuuuu | 28 17 18 71 -1 | 22 28
grg uuuuu | 24 32 12 131 -9 | -7 19
igr xxxxx | 8 16 4 52 2 | -3 17
irf xxxxx | -16 1 0 -41 3 | -5 18
jpl uuuuu | -50 -3 -80 -113 -6 | 16 24
mit uuuuu | 8 -42 -8 -49 -1 | 12 21
ngs uuuuu | 25 10 -49 55 2 | 6 18
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