[IGSREPORT-26325] Wk 2032 IGS Final Orbits
acc
acc at igs.org
Thu Jan 3 18:42:39 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2032 (Dec 16, 2018 - Dec 22, 2018)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs2032[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2032[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2032[0-6].cls IGS GPS clock combination summary report.
igs20327.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20327.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 KRGG NNOR TIXI DAV1 GLSV KRGG LHAZ NNOR
0 | COD | TIXI
0 | EMR | GRAZ
0 | ESA | 18 19 22 18 DAV1 LAUT LHAZ DAV1 LHAZ
0 | GFZ | 18 18 GODE POHN GODE POHN
0 | GRG | DAV1 GLSV LHAZ MCM4 TRO1 DAV1 GLSV TRO1
0 | JPL | LAUT
1 | COD | NOVM TIXI LHAZ NAUR NOVM TIXI
1 | EMR | GRAZ MCM4
1 | ESA | 18 20 21 22 18 ABPO ALIC ALRT ANKR ARTU AUCK BAKE
1 | ESA | BJFS BOGT BRAZ BRST CAS1 CEDU CHPI CHTI CHUM CHUR
1 | ESA | COCO CRO1 CUSV DAEJ DARW DAV1 DRAO DUBO FAA1 FAIR
1 | ESA | FLIN FLRS GLPS GLSV GRAS GRAZ GUAT HARB HOB2 IISC
1 | ESA | INEG IQAL IRKJ KARR KIRU KOKV KOUC KOUR LMMF MAC1
1 | ESA | MAG0 MAR6 MAS1 MATE MAW1 MBAR MCM4 MDO1 MDVJ MGUE
1 | ESA | MKEA MOBS NAUR NICO NIUM NKLG NNOR NRIL NYA1 OHI2
1 | ESA | OHI3 ONSA PDEL PERT PETS PIE1 PIMO PTBB QAQ1 RAMO
1 | ESA | REUN REYK RIOP SCH2 SCOR SCRZ SEYG SFER SOFI STHL
1 | ESA | STK2 SUTH SYOG THU2 TIXI TLSE TONG TOW2 TRO1 TUVA
1 | ESA | TWTF USN7 VILL WHIT WTZR XMIS ZAMB ZECK
1 | GFZ | 18 18 GODE POHN GODE POHN
1 | GRG | 21 21 GLSV MCM4 TLSE GLSV TLSE
1 | JPL | NRMD STJO LAUT NOVM NRMD
1 | MIT | PALM PALM
2 | COD | ALGO ANKR LAUT NAUR TIXI ALGO ANKR NAUR NICO SYOG
2 | COD | TIXI
2 | EMR | GRAZ
2 | ESA | 3 19 20 21 22 18 22 NOVM NOVM REUN
2 | GFZ | 18 18 21 BRMU GODE POHN BRMU GODE POHN
2 | GRG | GLSV KRGG LHAZ MCM4 NICO NRMD SYOG CRO1 GLSV KRGG
2 | GRG | LHAZ MCM4 NICO NRMD SYOG TUVA
2 | JPL | NOVM NRMD LAUT NOVM NRMD
3 | COD | 21 NAUR SUTH TIXI NAUR TIXI
3 | EMR | MATE
3 | ESA | 3 18 19 20 21 22 18 22 FAA1 PTBB FAA1 PTBB
3 | GFZ | 18 18 BJNM GODE POHN SUTH BJNM GODE POHN SUTH
3 | GRG | GLSV FAA1 GLSV KRGG
3 | JPL | LAUT SUTH
3 | MIT | PALM PALM
4 | COD | ANKR FAA1 NAUR TIXI YELL ANKR FAA1 NAUR TIXI YELL
4 | EMR | 18 CHUR MATE CHUR MATE
4 | ESA | 18 19 22 18 25 CHUR LAUT
4 | GFZ | 18 18 BOR1 GODE POHN BOR1 GODE POHN
4 | GRG | ADIS GLSV PDEL REUN TUVA ADIS GLSV PDEL REUN TUVA
4 | JPL | 18 25 LAUT
4 | MIT | YELL
5 | COD | 18 18 NAUR TIXI
5 | EMR | 16 GRAZ MATE MATE
5 | ESA | 18 19 20 21 22 18 22 ABPO ALIC ANKR ASPA AUCK BOGT
5 | ESA | BRAZ BRMU BRST CEDU CHPI CHTI CHUM CHUR COCO CRO1
5 | ESA | DARW DRAO FAA1 FLRS GLPS GLSV GRAS GRAZ GUAT GUUG
5 | ESA | HARB HOB2 IISC INEG KARR KERG KOKV KOUC KOUR LHAZ
5 | ESA | MAC1 MAG0 MAR6 MAS1 MBAR MCM4 MDO1 MDVJ MKEA NIUM
5 | ESA | NKLG NOVM NYA1 OHI2 ONSA PBRI PERT PETS PIMO PRDS
5 | ESA | PTBB REUN RIOP SCH2 SEYG SOFI STHL SUTH SUWN THTI
5 | ESA | THU2 TLSE TOW2 TWTF USN7 VILL WHIT WTZR XMIS YAKT
5 | ESA | ZAMB ZECK
5 | GFZ | 16 18 16 18 FLRS GODE POHN SYOG BRMU FLRS GODE POHN
5 | GFZ | POVE SYOG
5 | GRG | 18 18 LHAZ NRMD LHAZ NRMD SYOG
5 | JPL | STJO CUSV FLRS
6 | COD | GLSV NAUR TIXI GLSV NAUR TIXI
6 | ESA | 18 19 22 18
6 | GFZ | 18 18 GODE POHN GODE HRAO POHN
6 | GRG | ADIS HRAO MCM4 ADIS MCM4
6 | JPL | 18 18 ADIS ADIS
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
----+--------+--------+-------------
1 | ESA | ~02:24 | ~ -0.16 ns
2 | ESA | ~21:05 | ~ -0.06 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. 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 G18 | 4 | 4 | | 4 | 4 | 4 | 4 |
PRN G26 | 4 | 4 | 4 | 4 | 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 | .1 .2 .6 2 6 -7 -.28
EMR | 0 | 1.3 4.0 12.6 -45 22 2 -.17
ESA | 0 | -.3 .9 1.0 13 4 4 -.34
GFZ | 0 | .3 .3 .2 2 -20 15 -.09
GRG | 0 | 10.9 1.1 22.6 40 -10 44 .04
JPL | 0 | 6.4 4.6 10.3 6 -3 -1 -.34
MIT | 0 | 7.3 3.4 2.7 -16 27 -7 .0
NGS | 0 | 2.9 6.5 -4.9 52 -20 37 -.22
SIO | 0 | 4.5 2.1 2.6 32 -14 -22 -.10
COD | 1 | -.2 .4 .7 8 13 2 -.35
EMR | 1 | -2.6 8.8 13.2 -33 14 -11 -.37
ESA | 1 | .0 1.4 2.1 23 18 -9 -.40
GFZ | 1 | .4 .0 .5 -7 -25 27 -.24
GRG | 1 | 5.7 3.9 15.5 63 19 32 -.03
JPL | 1 | 1.7 -1.3 8.8 -3 8 2 -.55
MIT | 1 | 4.6 7.1 5.3 -14 15 -7 -.06
NGS | 1 | 3.6 6.2 -.5 31 -39 39 -.27
SIO | 1 | 6.0 8.7 2.8 21 -11 -21 -.37
COD | 2 | .2 .3 .7 -7 15 -3 -.24
EMR | 2 | 4.5 8.9 12.0 -22 48 -56 -.13
ESA | 2 | .2 1.8 1.6 21 21 -12 -.26
GFZ | 2 | .4 .1 .2 -9 -26 10 -.04
GRG | 2 | 8.1 3.0 14.5 73 24 29 .03
JPL | 2 | 5.1 4.0 5.9 6 -3 11 -.54
MIT | 2 | 5.4 9.3 4.3 -8 18 -21 .11
NGS | 2 | 1.7 7.4 -4.3 51 -34 40 -.13
SIO | 2 | .4 8.4 4.4 17 -1 -33 -.19
COD | 3 | .3 -.1 .3 7 14 -8 -.24
EMR | 3 | 3.4 9.3 13.1 -22 49 -50 -.24
ESA | 3 | .3 1.3 2.0 24 4 -9 -.23
GFZ | 3 | -.0 .5 .2 -1 -27 -1 -.07
GRG | 3 | 3.7 4.5 9.6 74 14 34 -.05
JPL | 3 | 8.5 5.2 3.2 4 -2 -1 -.44
MIT | 3 | 4.8 8.4 7.5 -4 22 -16 .06
NGS | 3 | 2.0 8.6 -7.1 63 -24 18 -.05
SIO | 3 | 6.2 6.5 6.4 31 -5 -27 -.23
COD | 4 | .3 .3 .0 8 -9 -12 -.15
EMR | 4 | 3.5 4.3 14.1 -17 39 -18 -.04
ESA | 4 | 1.4 .9 2.1 29 -1 -7 -.15
GFZ | 4 | .5 .3 .5 15 -28 1 -.10
GRG | 4 | 2.7 5.5 19.7 68 9 45 .09
JPL | 4 | 5.2 9.4 10.1 -9 10 6 -.49
MIT | 4 | 6.1 6.9 7.5 -8 9 -16 .04
NGS | 4 | 3.8 7.5 8.6 43 -75 52 .11
SIO | 4 | 6.6 2.5 9.0 25 7 -32 -.27
COD | 5 | .0 .6 .6 12 15 -17 -.23
EMR | 5 | 4.5 5.5 14.2 -34 31 41 -.23
ESA | 5 | .5 1.4 1.3 26 3 -15 -.28
GFZ | 5 | .3 .3 .2 -3 -26 -1 -.04
GRG | 5 | 1.6 6.9 13.1 73 31 61 -.0
JPL | 5 | 5.1 .4 6.6 6 4 -10 -.26
MIT | 5 | 4.4 5.6 10.4 8 14 -7 .03
NGS | 5 | 4.6 6.2 -2.3 42 -35 38 .06
SIO | 5 | 5.7 5.7 6.5 39 -25 -23 -.10
COD | 6 | .3 .0 .5 4 10 -11 -.28
EMR | 6 | -.6 .7 10.5 -43 29 55 -.13
ESA | 6 | .7 1.3 1.7 15 15 1 -.36
GFZ | 6 | .4 .2 .4 -7 -29 2 -.09
GRG | 6 | 1.6 4.6 17.5 88 26 64 -.03
JPL | 6 | 3.1 -.4 14.0 0 0 1 -.09
MIT | 6 | 1.5 3.2 10.3 -8 21 10 -.09
NGS | 6 | -1.6 3.6 5.8 27 -38 25 -.25
SIO | 6 | 3.0 5.6 16.5 19 5 -9 -.19
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 1.2032.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2032.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 2.2032.[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 3.2032.[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 5.2032.0-6). 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 2032 summary. (Dec 16, 2018 - Dec 22, 2018)
Table 1.2032.a GPS week: 2032 MJD: 58468.000-58474.000
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 256| -1 0 3 19 0 2 -.04 9 9 | -516 -99 7 99
| 0 0 2 11 14 8 .04 | 116 207
emr 80| 0 0 4 -28 -6 -9 .13 13 13 | 167432 -68 16 128
| 0 0 0 9 7 15 .02 | 17137 804
esa 150| 0 0 0 0 6 3 -.06 8 8 | -686 -241 6 198
| 0 0 1 11 10 17 .01 | 430 1046
gfz 182| 0 -1 2 18 -3 -1 .13 10 10 | -158 -24 11 108
| 0 0 1 9 9 7 .02 | 252 458
grg 102| 1 0 2 -23 -4 -29 -.15 11 10 | 95 -101 8 156
| 0 0 2 7 5 36 .01 | 166 319
igr n/a| 0 0 -1 -8 -11 8 -.04 4 4 | 2205 89 9 67
| 0 0 1 7 9 9 .01 | 771 824
jpl 80| 0 0 3 8 15 13 .17 9 9 | 213464 39 8 103
| 0 0 1 14 12 10 .01 | 902 873
mit 349| 2 0 -6 -15 -14 5 -.01 13 13 | -49 -91 75 1596
| 0 0 1 20 20 11 .02 | 266 279
ngs 206| -1 0 -6 -18 -3 13 -.06 11 11 | -554 -58 910 2041
| 0 0 1 19 11 18 .03 | 198 362
sio 244| 1 0 -9 20 -6 -7 -.06 14 13 | --- --- --- ---
| 0 0 2 19 20 26 .04 | --- ---
Table 1.2032.b GPS week : 2032 MJD: 58468.000-58474.000
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 | 4 4 4 4 4 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 3 3 3 3 3 3 4 |
4 | 12 7 8 10 10 10 11 |
5 | 4 4 4 4 5 4 5 |
6 | 4 3 3 3 3 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 4 3 4 4 |
10 | 3 4 3 3 3 3 3 |
11 | 3 3 3 4 4 4 3 |
12 | 4 4 4 4 5 5 4 |
13 | 4 4 4 4 4 4 4 |
14 | 4 3 3 3 3 3 3 |
15 | 4 4 4 4 4 4 4 |
16 | 4 5 5 5 4 6 5 |
17 | 4 4 4 4 4 4 3 |
18 | 5 5 6 6 6 6 6 |
19 | 4 4 4 4 5 4 4 |
20 | 5 5 4 4 4 4 4 |
21 | 4 6 5 4 5 5 3 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 4 4 4 |
24 | 4 3 3 3 3 3 3 |
25 | 4 4 3 4 5 3 3 |
26 | 3 3 7 3 3 4 3 |
27 | 4 3 3 3 3 4 3 |
28 | 4 3 4 4 4 4 4 |
29 | 5 5 4 4 5 5 5 |
30 | 4 3 4 4 4 4 3 |
31 | 4 4 4 4 5 4 4 |
32 | 3 3 3 4 4 4 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 2.2032.0 GPS week: 2032 Day: 0 MJD: 58468.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 257| -1 0 3 31 29 -3 -.06 9 9 | -649 129 8 97
emr 80| 0 0 4 -33 -2 -13 .14 13 13 | 178548 175 15 131
esa 150| 0 0 0 -8 -2 -10 -.06 8 8 | -1239 1286 6 192
gfz 182| 0 -2 1 22 6 -10 .13 10 10 | -62 221 12 92
grg 103| 0 0 5 -27 -7 32 -.14 10 9 | -77 285 8 139
igr n/a| 0 0 -2 -10 -16 -5 -.04 4 4 | 2842 731 9 66
jpl 80| 0 0 3 26 8 9 .17 9 9 | 214363 684 9 102
mit 349| 2 0 -8 6 -38 17 .01 14 13 | -155 15 120 1744
ngs 209| 0 0 -6 -42 8 -7 -.02 11 11 | -964 639 639 1711
sio 253| 1 0 -13 35 -26 18 -.08 15 14 | --- --- --- ---
Table 2.2032.1 GPS week: 2032 Day: 1 MJD: 58469.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 257| -1 0 3 27 2 10 -.02 9 8 | -445 -189 7 90
emr 80| 0 0 4 -35 -17 -30 .10 13 13 | 178692 -1327 15 123
esa 150| 0 0 2 7 5 -15 -.04 8 8 | -778 480 6 208
gfz 186| 0 -1 0 19 6 6 .14 10 9 | 188 -483 10 93
grg 105| 0 0 2 -16 -1 1 -.13 11 9 | 282 -146 8 157
igr n/a| 0 0 -1 6 -6 -3 -.04 4 4 | 3467 -1215 9 62
jpl 80| -1 0 4 20 27 2 .17 9 9 | 214920 -1256 8 98
mit 349| 3 0 -8 -26 -17 3 -.00 14 13 | -47 -34 78 1497
ngs 210| 0 0 -6 -38 -11 34 -.08 11 11 | -448 -181 1127 1884
sio 277| 2 0 -12 -5 -8 -7 -.09 14 12 | --- --- --- ---
Table 2.2032.2 GPS week: 2032 Day: 2 MJD: 58470.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 257| -1 0 6 26 -3 8 .04 9 8 | -422 -143 8 105
emr 80| 0 1 3 -33 -15 2 .15 13 13 | 177058 -693 16 119
esa 150| 0 0 0 -7 15 -9 -.08 8 8 | -132 -85 6 208
gfz 183| 0 -1 2 27 -17 0 .11 10 10 | -145 256 10 100
grg 105| 1 1 1 -22 5 -29 -.15 10 9 | 289 -392 9 163
igr n/a| -1 0 0 -11 -23 12 -.03 4 4 | 1899 -531 9 65
jpl 80| 0 2 2 19 -5 16 .18 9 9 | 213305 -731 7 84
mit 349| 2 0 -7 -14 -14 2 .02 14 13 | 189 -413 57 1700
ngs 206| -1 0 -8 -11 3 18 -.07 11 11 | -411 -152 865 2165
sio 251| 0 -2 -9 -2 10 -10 -.13 13 12 | --- --- --- ---
Table 2.2032.3 GPS week: 2032 Day: 3 MJD: 58471.000
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 261| -1 0 5 15 -7 13 -.05 10 9 | -361 -266 10 128
emr 80| 0 0 5 -38 -5 15 .13 13 13 | 176541 -276 16 142
esa 150| 0 0 1 7 11 5 -.07 8 8 | -353 -364 6 179
gfz 183| -1 0 1 8 -13 -1 .13 10 10 | 83 -584 12 114
grg 103| 1 0 0 -29 -3 -74 -.14 11 11 | 177 -242 8 150
igr n/a| -1 0 0 -10 -17 10 -.04 4 4 | 1490 -267 9 63
jpl 80| 0 0 2 7 10 29 .16 9 9 | 212741 -430 9 106
mit 349| 2 -1 -5 0 5 3 -.03 13 12 | -183 -538 52 1530
ngs 208| 0 -1 -7 -10 -18 -10 -.04 10 10 | -401 -235 916 2270
sio 234| 1 0 -8 25 6 -2 -.03 14 13 | --- --- --- ---
Table 2.2032.4 GPS week: 2032 Day: 4 MJD: 58472.000
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 255| -1 0 1 -4 -18 0 -.07 9 9 | -554 -7 8 95
emr 80| 0 0 5 -22 -2 -1 .12 13 13 | 176425 206 17 129
esa 150| 0 0 0 14 21 18 -.07 8 8 | -689 -2131 6 201
gfz 176| 0 -1 2 9 -3 2 .15 11 10 | -347 -191 12 119
grg 98| 2 0 5 -19 -7 -64 -.17 14 12 | 71 -358 10 170
igr n/a| 0 0 -2 -7 3 15 -.04 4 4 | 1334 307 9 78
jpl 80| 0 1 2 -8 30 5 .17 10 10 | 212414 309 8 127
mit 349| 2 0 -6 -18 -38 -14 -.01 13 13 | -196 -19 66 1645
ngs 202| -1 0 -2 13 13 36 -.10 10 10 | -491 -154 899 2136
sio 233| 3 0 -8 9 -39 -21 .00 15 15 | --- --- --- ---
Table 2.2032.5 GPS week: 2032 Day: 5 MJD: 58473.000
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| -2 0 4 17 -3 -7 -.08 9 9 | -671 170 6 84
emr 80| 1 1 5 -17 4 -20 .15 13 13 | 142030 1215 17 121
esa 150| 0 0 0 8 0 7 -.07 8 8 | -1227 -317 7 198
gfz 182| 0 -1 5 10 -7 -12 .16 11 10 | -532 727 11 116
grg 94| 1 0 0 -34 -10 -42 -.16 13 12 | -141 410 10 154
igr n/a| -1 0 -1 -9 -3 10 -.04 4 4 | 1878 1242 9 76
jpl 80| 1 0 3 -12 17 22 .19 9 9 | 212924 1228 9 99
mit 349| 2 -1 -5 -1 15 10 -.04 13 12 | 416 224 97 1601
ngs 202| -1 -1 -8 -18 -6 4 -.09 10 10 | -640 166 953 1987
sio 234| 0 0 -8 38 -8 24 -.02 13 13 | --- --- --- ---
Table 2.2032.6 GPS week: 2032 Day: 6 MJD: 58474.000
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 0 21 -1 -6 -.01 8 8 | -510 -393 7 94
emr 80| 0 1 3 -16 -4 -19 .13 13 13 | 142734 224 19 135
esa 150| 0 0 0 -16 -8 32 -.05 8 8 | -387 -560 7 202
gfz 182| -1 0 3 34 1 6 .13 10 11 | -295 -117 12 126
grg 106| 1 0 1 -11 -8 -32 -.16 10 9 | 70 -268 9 162
igr n/a| 0 0 -3 -19 -15 17 -.03 4 4 | 2530 362 9 62
jpl 80| 0 0 5 7 19 7 .15 9 9 | 213583 475 9 110
mit 349| 1 0 -5 -52 -15 18 -.03 13 12 | -371 128 61 1455
ngs 208| -1 0 -5 -23 -12 16 -.02 11 11 | -524 -492 971 2138
sio 229| 1 -1 -8 39 18 -55 -.04 12 12 | --- --- --- ---
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 3.2032.0 GPS week: 2032 Day: 0 MJD: 58468.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 15 9 9 13 4 8 8 7 13 3 | 29 36 32 34 28 30 34 33 32 33 30
2E | 6 14 7 12 12 5 10 16 13 15 4 | 27 30 24 30 28 25 27 25 25 25 25
3 | 7 9 9 7 8 3 7 9 10 11 3 | 51 54 53 53 53 52 54 53 51 54 52
X4 | 10 --- --- --- --- 12 13 --- --- --- 11 | 37 --- --- --- --- 33 33 --- --- --- 33
5 | 10 8 11 8 7 5 11 20 15 19 4 | 47 46 47 47 45 42 54 36 38 36 44
6E | 8 9 9 10 14 3 7 9 10 7 3 | 33 32 36 36 33 32 33 34 32 36 33
7 | 9 13 6 9 12 6 12 12 10 14 3 | 29 23 26 30 32 27 24 30 31 25 26
8 | 5 10 6 11 8 3 9 12 8 14 3 | 23 28 24 25 23 22 27 21 25 27 23
9 | 9 9 11 8 8 4 7 7 7 15 3 | 24 31 20 22 24 23 31 28 27 33 25
10 | 8 8 10 11 6 4 8 14 8 11 3 | 25 30 26 25 29 26 31 31 28 31 26
11E | 9 8 7 9 12 3 8 8 8 12 3 | 33 36 37 35 37 36 37 36 36 38 35
12 | 10 19 7 9 8 5 10 16 13 14 4 | 31 31 29 32 29 30 31 32 33 31 30
13 | 9 10 9 7 7 3 11 17 13 14 3 | 28 31 25 28 27 27 30 35 32 35 28
14 | 7 6 7 11 7 3 5 15 12 18 3 | 26 27 24 23 26 26 27 33 32 34 26
15 | 8 9 6 9 6 4 8 15 11 18 3 | 32 36 31 34 29 27 34 24 26 27 29
16 | 11 23 7 8 9 4 9 16 11 16 4 | 24 23 23 28 27 24 22 27 31 26 24
17 | 7 18 5 11 9 4 5 15 11 15 3 | 21 24 21 26 21 22 25 26 26 26 21
18E | 18 14 12 20 12 7 12 16 12 15 5 | 183 95 187 188 188 186 187 184 188 184 186
19 | 8 19 6 9 10 5 7 17 12 15 4 | 26 29 24 28 24 24 25 22 26 23 24
20 | 11 7 6 15 10 5 9 20 16 21 4 | 26 29 26 24 30 30 28 40 38 42 29
21E | 7 8 7 7 13 5 10 15 10 12 3 | 21 22 24 24 21 20 22 23 21 25 20
22 | 6 8 8 10 10 4 8 20 12 19 4 | 32 33 30 33 30 34 32 40 40 40 32
23 | 11 21 9 7 6 6 7 11 11 15 4 | 21 16 18 23 19 21 19 24 27 20 19
24 | 7 9 6 10 11 4 9 13 7 14 3 | 33 34 32 30 35 30 33 36 29 38 32
25 | 9 16 5 12 7 5 9 11 8 15 3 | 21 24 20 22 18 17 21 17 17 17 18
26 | 7 8 8 8 11 3 10 12 9 10 3 | 389 389 387 387 276 388 389 392 388 388 388
27 | 8 11 7 7 8 2 10 15 6 15 3 | 21 23 21 22 22 20 23 21 22 24 20
28 | 8 16 9 9 11 4 8 12 12 12 3 | 20 25 19 23 18 19 23 19 22 17 18
29 | 13 21 6 10 8 6 11 18 15 24 5 | 33 30 25 33 26 27 27 29 26 36 27
30 | 9 8 9 9 18 4 10 10 9 11 3 | 25 24 26 24 31 23 26 28 27 24 24
31 | 8 14 5 15 14 4 7 16 11 19 4 | 27 30 28 33 35 29 30 33 31 27 29
32 | 7 10 10 10 5 4 10 10 7 14 3 | 27 36 24 26 28 28 34 32 29 32 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 10 10 4 9 14 11 15 |T 44 43 44 46 41 43 46 46 46 46 43
WRMS | 9 13 8 10 9 4 9 13 11 14 |NE 42 44 41 43 38 41 43 44 44 44 41
MEDI | 8 10 7 9 9 4 9 15 11 15 |MD 27 30 26 28 28 27 30 31 29 31 27
Table 3.2032.1 GPS week: 2032 Day: 1 MJD: 58469.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 11 10 7 11 3 9 8 9 11 3 | 18 26 23 23 20 20 22 21 23 23 20
2E | 10 11 5 9 9 4 9 15 13 16 3 | 24 29 24 24 25 22 26 25 22 24 23
3 | 8 8 11 6 7 3 9 9 6 11 3 | 48 51 50 49 48 47 51 51 47 52 49
X4 | 5 --- --- --- --- 14 8 --- --- --- 7 | 29 --- --- --- --- 27 27 --- --- --- 27
5 | 7 7 11 8 9 6 9 18 15 20 4 | 36 36 34 34 32 31 38 29 27 34 32
6E | 11 7 8 6 12 4 8 9 7 7 3 | 23 21 24 24 25 21 23 22 24 21 22
7 | 9 13 6 7 12 4 13 13 11 14 3 | 26 19 19 24 24 21 20 24 23 17 20
8 | 6 10 5 8 5 2 9 11 8 12 3 | 21 24 22 21 21 20 25 22 20 28 21
9 | 7 8 11 9 9 3 8 7 6 14 3 | 20 30 21 24 20 21 31 26 23 32 23
10 | 6 12 10 13 5 3 8 13 6 16 3 | 24 32 25 25 25 24 30 28 23 31 25
11E | 6 11 9 9 8 3 9 9 7 10 3 | 32 33 36 33 36 34 34 34 34 33 33
12 | 12 19 6 8 8 4 7 17 15 14 4 | 31 30 26 30 28 27 28 31 31 29 28
13 | 7 10 8 6 6 3 10 17 12 14 3 | 24 30 23 27 23 24 29 28 26 28 24
14 | 5 7 8 10 6 3 5 14 12 15 3 | 20 19 18 15 20 18 21 25 25 24 19
15 | 7 10 6 8 5 4 10 16 11 16 3 | 22 26 22 24 19 19 25 19 19 20 20
16 | 10 24 5 10 9 4 11 15 13 16 4 | 25 21 22 26 24 22 21 25 28 22 21
17 | 5 16 5 11 9 4 6 16 12 11 3 | 19 23 18 24 21 21 23 25 25 23 20
18E | 18 15 13 18 10 8 12 16 12 16 5 | 177 93 178 182 178 178 179 179 177 181 178
19 | 7 21 6 9 10 4 7 17 12 13 4 | 23 28 21 26 24 22 24 23 25 24 22
20 | 10 9 8 13 11 3 9 19 15 22 4 | 21 25 22 23 24 24 24 31 27 35 23
21E | 9 8 7 11 40 6 8 15 11 12 5 | 20 22 20 21 44 19 21 24 24 22 20
22 | 6 9 9 7 6 5 9 19 10 20 3 | 28 31 29 30 29 29 30 31 30 32 28
23 | 7 19 8 9 7 4 8 11 9 17 3 | 16 15 14 20 12 15 16 19 18 18 15
24 | 7 9 7 8 9 3 8 11 7 8 3 | 29 31 28 30 30 27 29 33 28 30 28
25 | 9 13 5 13 8 2 10 12 7 7 3 | 20 22 20 23 18 17 22 17 16 19 18
26 | 8 10 7 8 9 3 10 13 7 10 3 | 428 427 427 428 330 427 428 426 428 424 427
27 | 7 11 5 12 7 3 10 13 7 10 3 | 24 24 21 23 22 21 23 23 22 22 21
28 | 5 10 6 8 9 3 8 11 10 10 3 | 16 22 18 21 17 17 22 20 19 18 17
29 | 13 23 6 9 9 5 13 17 15 18 4 | 28 23 21 27 22 22 23 23 22 25 22
30 | 6 10 8 6 15 3 10 10 9 9 3 | 26 25 26 24 28 23 27 27 25 22 24
31 | 8 15 5 12 10 4 7 13 11 11 3 | 21 25 22 30 26 23 25 27 25 21 23
32 | 5 11 9 11 6 3 9 10 6 13 3 | 27 35 26 27 28 27 35 30 27 31 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 10 11 4 9 14 11 14 |T 42 41 41 43 40 40 43 44 43 44 41
WRMS | 8 13 8 9 9 4 9 13 11 12 |NE 40 42 39 42 36 39 42 42 41 42 39
MEDI | 7 11 7 9 9 3 9 13 10 13 |MD 24 26 22 24 24 22 25 25 25 24 23
Table 3.2032.2 GPS week: 2032 Day: 2 MJD: 58470.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 12 12 14 12 4 8 10 11 10 4 | 21 27 27 22 23 23 25 25 25 26 22
2E | 11 10 7 10 7 4 8 16 14 15 3 | 22 25 22 22 25 20 21 23 25 19 21
3 | 9 8 10 8 6 3 7 10 9 8 3 | 44 44 40 43 42 42 45 43 43 45 42
X4 | 8 --- --- --- --- 12 7 --- --- --- 7 | 29 --- --- --- --- 24 24 --- --- --- 26
5 | 9 8 11 10 7 3 10 18 13 20 4 | 35 38 36 37 37 34 40 28 28 35 34
6E | 12 8 9 8 9 3 8 8 9 10 3 | 28 27 29 26 30 27 28 26 28 29 26
7 | 8 15 6 9 11 4 12 13 10 14 3 | 25 21 20 25 23 22 20 24 24 18 20
8 | 5 9 6 9 7 4 9 13 8 9 3 | 20 24 21 20 21 19 22 20 22 22 20
9 | 9 7 11 7 7 4 7 8 8 12 3 | 20 31 21 21 21 20 30 27 24 31 23
10 | 8 10 10 10 5 2 8 12 6 11 3 | 14 25 15 12 18 14 22 17 17 18 15
11E | 8 11 10 8 11 4 7 12 6 10 3 | 27 30 30 27 28 27 29 27 28 27 27
12 | 12 17 5 9 9 4 6 14 12 11 3 | 26 25 23 26 25 25 25 27 25 25 23
13 | 8 9 8 7 7 3 9 17 13 10 3 | 18 26 17 22 19 20 26 24 22 24 20
14 | 8 6 7 9 6 3 6 13 12 15 3 | 27 29 27 29 29 27 27 32 33 33 28
15 | 6 8 4 10 6 4 8 15 12 16 3 | 27 27 23 28 23 21 25 19 18 25 23
16 | 8 25 8 12 10 4 12 14 13 14 4 | 21 19 18 21 20 19 17 23 24 18 17
17 | 6 14 5 9 11 3 7 15 13 12 3 | 27 27 24 29 25 27 27 29 31 26 26
18E | 17 16 11 24 11 9 14 16 18 15 5 | 118 74 126 123 122 120 120 123 119 124 121
19 | 8 19 5 10 11 4 6 14 13 13 4 | 19 22 19 22 21 18 19 18 17 17 17
20 | 12 8 7 11 8 4 7 17 15 18 4 | 20 26 21 19 24 23 24 30 31 29 22
21E | 9 13 7 8 22 5 10 15 11 13 4 | 17 17 17 16 29 15 17 19 19 16 15
22 | 5 10 8 8 9 5 10 19 12 16 3 | 25 28 23 24 22 25 26 32 32 31 24
23 | 7 20 8 9 7 4 6 12 13 14 3 | 18 16 16 19 16 17 15 22 23 19 16
24 | 10 10 6 8 9 4 8 11 9 7 3 | 32 28 26 27 29 25 29 31 30 29 27
25 | 9 16 6 9 7 3 8 9 6 8 3 | 20 26 20 20 18 19 23 16 18 17 18
X26 | 12 26 10 15 --- 9 28 15 15 17 6 | 9999 9999 9999 9999 --- 9999 9999 9999 9999 9999 9999
27 | 6 10 7 8 7 4 9 11 7 15 3 | 22 24 20 20 20 19 22 21 22 23 20
28 | 7 14 7 10 11 4 7 13 11 10 3 | 19 23 19 25 18 19 21 20 21 17 18
29 | 11 22 7 6 9 4 11 16 11 15 4 | 26 23 20 25 22 22 23 23 22 25 22
30 | 9 8 9 10 13 3 9 11 7 7 3 | 23 24 24 24 29 21 23 25 24 22 22
31 | 6 10 6 13 11 2 8 12 10 11 3 | 21 23 20 27 25 21 22 26 25 21 21
32 | 8 11 9 6 6 3 10 9 9 12 3 | 24 33 22 23 24 23 31 25 28 26 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 10 10 4 9 14 11 13 |T 26 27 26 27 27 25 28 28 28 27 25
WRMS | 8 13 8 10 9 4 9 13 11 12 |NE 24 26 22 24 23 22 25 25 25 24 22
MEDI | 8 10 7 9 9 4 8 13 11 12 |MD 23 26 21 24 23 22 24 25 24 25 22
Table 3.2032.3 GPS week: 2032 Day: 3 MJD: 58471.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 11 11 13 12 2 7 10 8 15 3 | 21 25 29 27 23 24 27 24 28 27 24
2E | 8 13 7 13 8 4 11 16 12 15 4 | 23 27 23 28 25 24 25 25 30 26 24
3 | 7 10 10 10 8 3 8 8 5 10 3 | 22 30 24 29 25 23 31 28 25 32 26
X4 | 10 --- --- --- --- 22 9 --- --- --- 9 | 28 --- --- --- --- 23 24 --- --- --- 23
5 | 8 9 10 8 8 4 12 20 14 21 4 | 39 39 37 40 37 34 43 27 30 32 35
6E | 10 9 8 8 12 3 8 11 9 11 3 | 22 23 24 23 25 20 22 20 23 23 21
7 | 10 12 5 9 13 3 11 13 12 14 4 | 26 22 23 29 24 24 21 26 28 23 23
8 | 4 10 6 8 10 3 7 11 7 10 2 | 22 26 24 24 23 22 25 24 23 29 23
9 | 11 8 11 8 10 4 8 8 10 12 3 | 26 32 21 25 24 23 33 27 28 33 26
10 | 9 11 9 9 7 2 8 11 5 15 3 | 17 27 16 15 21 16 24 18 19 23 17
11E | 10 13 8 11 10 2 7 8 9 16 3 | 28 32 33 32 35 32 32 31 32 35 31
12 | 13 20 5 10 13 5 8 15 10 14 4 | 25 22 17 22 22 20 22 21 21 22 19
13 | 7 9 8 7 8 2 9 15 12 11 3 | 20 28 21 27 24 22 27 29 28 28 23
14 | 9 7 7 7 7 3 6 12 11 16 3 | 20 22 17 20 23 19 19 28 28 30 21
15 | 9 8 6 11 7 3 10 14 11 17 3 | 30 30 30 35 29 27 29 23 24 29 28
16 | 13 24 6 11 13 4 11 14 13 15 4 | 23 20 18 23 20 18 18 21 21 19 17
17 | 7 15 6 8 11 4 6 16 14 12 3 | 19 22 18 24 19 19 23 22 25 20 19
18E | 20 20 12 16 11 8 14 16 18 17 5 | 228 112 230 232 228 231 230 232 228 231 229
19 | 9 17 6 10 13 4 7 15 13 13 4 | 18 20 19 21 19 18 20 16 19 16 17
20 | 9 9 7 11 11 4 8 17 12 23 4 | 22 24 20 20 28 23 24 31 33 34 24
21E | 8 10 6 9 14 7 8 17 8 11 3 | 16 20 18 19 30 15 19 23 22 23 19
22 | 6 10 9 8 9 4 8 18 11 16 3 | 24 28 23 28 26 27 28 33 34 33 27
23 | 8 21 8 10 8 4 7 11 11 16 4 | 24 17 20 27 22 22 20 25 29 23 21
24 | 13 10 8 11 8 4 10 9 7 9 3 | 23 26 22 24 26 22 25 29 25 27 23
25 | 11 18 8 13 8 4 9 8 6 9 3 | 20 25 19 19 17 16 23 16 17 18 17
26 | 8 9 7 7 15 4 8 9 10 8 3 | 899 898 897 897 9999 897 897 896 896 896 897
27 | 5 11 4 8 9 3 8 10 7 12 3 | 21 24 20 21 20 20 23 23 22 24 20
28 | 9 9 8 10 11 3 7 13 11 12 3 | 18 22 20 24 18 18 22 18 19 20 18
29 | 12 20 4 8 11 4 10 15 12 16 4 | 23 21 17 20 17 17 20 18 22 21 18
30 | 10 11 7 9 13 2 10 11 7 8 3 | 24 23 25 27 27 22 21 25 24 24 22
31 | 7 14 5 17 10 2 6 13 9 12 3 | 23 25 22 28 27 22 25 26 25 23 23
32 | 8 13 9 9 9 3 10 8 8 16 3 | 17 33 18 20 25 20 31 23 24 26 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 8 10 11 4 9 13 10 14 |T 56 56 56 59 30 55 58 58 59 60 56
WRMS | 9 13 8 10 11 4 9 12 10 13 |NE 56 60 56 59 23 55 58 58 59 60 55
MEDI | 9 11 7 9 10 4 8 13 10 14 |MD 23 25 21 24 24 22 24 25 25 26 23
Table 3.2032.4 GPS week: 2032 Day: 4 MJD: 58472.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 10 11 10 16 3 8 13 8 12 3 | 21 22 26 22 23 22 25 21 25 23 21
2E | 9 14 6 8 15 3 13 15 12 18 4 | 25 29 25 26 26 24 27 25 24 29 24
3 | 6 9 11 5 9 4 7 9 7 13 3 | 47 54 48 51 48 48 53 48 53 53 50
X4 | 9 --- --- --- --- 26 10 --- --- --- 9 | 26 --- --- --- --- 34 28 --- --- --- 25
5 | 9 8 9 8 10 4 10 20 15 22 4 | 35 37 30 36 36 30 39 25 29 35 32
6E | 9 8 8 8 14 4 8 11 8 11 3 | 25 26 24 22 22 21 22 22 20 24 21
7 | 8 13 6 9 16 4 11 14 10 15 4 | 24 22 20 26 24 22 21 24 27 20 21
8 | 5 11 5 10 11 4 8 12 6 11 3 | 26 29 25 27 25 24 28 27 27 29 25
9 | 9 9 11 7 11 4 7 9 7 14 3 | 26 34 26 26 24 25 33 31 26 37 27
10 | 8 12 11 10 7 4 8 11 5 9 3 | 21 29 21 20 24 20 25 20 20 23 20
11E | 8 12 9 15 15 4 7 8 7 16 4 | 35 36 37 38 39 36 37 35 41 38 36
12 | 10 23 6 8 12 4 10 17 11 14 4 | 28 27 25 26 26 25 26 28 27 30 25
13 | 9 9 8 8 12 3 10 16 12 15 3 | 21 28 22 29 20 25 28 29 25 31 24
14 | 9 7 8 6 10 4 7 11 9 14 3 | 25 25 23 24 22 22 25 27 24 32 24
15 | 9 10 4 10 10 4 9 12 12 15 3 | 30 34 31 37 31 29 32 25 26 30 30
16 | 9 21 6 11 13 4 8 14 11 16 4 | 22 21 21 27 24 21 20 23 26 24 21
17 | 9 17 6 10 12 2 7 16 13 14 4 | 23 28 23 30 22 24 27 26 26 26 24
18E | 20 18 17 23 14 12 15 15 17 16 6 | 146 132 155 150 159 155 154 153 156 152 152
19 | 10 20 5 10 14 4 8 16 15 16 4 | 22 25 23 25 22 22 25 22 23 25 22
20 | 11 8 7 10 12 4 6 17 13 18 4 | 24 24 24 25 28 26 24 30 30 31 24
21E | 7 11 8 8 36 4 11 12 9 14 5 | 17 19 19 21 39 18 20 18 19 24 18
22 | 8 9 9 8 10 4 9 18 13 19 4 | 31 35 29 34 30 33 34 35 38 36 32
23 | 8 19 9 8 11 5 6 12 9 15 3 | 22 14 21 25 19 21 18 24 24 20 20
24 | 8 9 6 8 10 3 10 11 6 11 3 | 30 30 28 30 30 28 30 34 27 31 29
25 | 11 15 15 14 13 4 21 8 9 15 5 | 20 22 25 19 17 18 32 16 16 22 18
26 | 7 8 7 9 12 3 8 10 10 11 3 | 881 883 880 882 596 880 878 882 877 884 881
27 | 5 12 6 6 11 4 11 11 6 16 3 | 22 26 22 24 24 22 24 24 23 28 22
28 | 9 13 5 10 9 4 7 14 11 13 3 | 17 22 19 24 17 18 22 18 20 22 18
29 | 16 21 5 8 12 5 12 18 13 19 5 | 27 24 20 24 19 21 22 20 22 25 20
30 | 9 10 8 16 18 3 9 9 5 8 3 | 24 24 26 26 29 23 25 27 25 27 24
31 | 8 10 6 21 14 4 10 13 11 17 4 | 24 25 22 31 25 22 25 27 25 25 23
32 | 9 11 10 7 10 4 10 9 7 12 3 | 27 36 27 29 30 27 33 28 26 30 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 11 14 4 10 13 10 15 |T 56 58 57 59 49 55 58 57 57 60 55
WRMS | 9 13 8 10 12 4 10 13 10 15 |NE 58 62 59 62 48 58 60 60 60 63 58
MEDI | 9 11 8 9 12 4 9 12 10 15 |MD 25 27 25 26 25 24 26 26 26 29 24
Table 3.2032.5 GPS week: 2032 Day: 5 MJD: 58473.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 10 10 9 18 3 8 11 7 9 3 | 21 25 24 24 23 23 27 23 26 22 22
2E | 9 11 6 10 11 4 11 15 9 13 3 | 25 26 24 25 25 23 26 24 26 25 23
3 | 7 8 9 8 10 2 6 10 8 9 3 | 43 44 45 46 46 44 48 46 40 48 44
X4 | 9 --- --- --- --- 15 10 --- --- --- 10 | 31 --- --- --- --- 29 30 --- --- --- 29
5 | 7 9 10 8 9 4 10 20 14 17 4 | 29 32 25 28 29 25 32 23 25 30 27
X6E | 7 --- 7 14 14 3 8 11 8 9 3 | 25 --- 26 31 27 24 26 25 23 26 25
7 | 11 11 8 13 14 4 10 11 10 18 4 | 27 24 22 30 26 24 22 27 27 24 23
8 | 7 13 5 10 9 3 8 12 8 12 3 | 20 23 22 25 23 20 23 24 20 28 21
9 | 8 9 12 11 10 4 8 6 9 12 3 | 20 33 22 22 23 21 33 28 24 33 24
10 | 8 13 10 8 7 3 8 11 9 9 3 | 19 27 18 19 22 17 26 20 19 22 19
11E | 8 11 10 10 17 4 6 7 11 10 3 | 32 29 34 34 39 32 34 31 30 33 32
12 | 10 22 6 10 14 5 9 15 13 14 4 | 27 23 21 24 25 22 23 26 28 26 23
13 | 8 9 8 8 10 3 9 14 11 13 3 | 18 25 19 26 19 20 24 22 20 24 20
14 | 7 7 8 8 8 3 7 11 10 14 3 | 28 28 28 26 30 27 25 27 29 28 26
15 | 7 9 5 8 8 4 11 12 12 14 3 | 31 31 31 34 31 29 33 30 30 32 30
X16 | 9 21 --- 11 16 5 9 13 14 --- 5 | 23 22 --- 23 22 23 20 23 28 --- 21
17 | 9 14 7 11 12 4 6 16 13 11 4 | 24 30 22 31 24 26 30 28 31 30 26
18E | 15 19 14 17 11 6 14 17 12 16 5 | 256 165 261 258 258 260 257 259 263 259 258
19 | 8 16 5 12 14 3 7 19 15 10 4 | 22 24 22 29 22 23 24 19 24 22 22
20 | 9 9 8 11 11 3 8 15 13 20 4 | 22 24 23 24 26 23 26 28 28 30 23
21E | 11 8 8 10 33 5 9 14 12 14 5 | 19 19 18 20 39 17 21 19 19 20 18
22 | 8 10 7 8 11 4 8 16 14 18 4 | 27 31 29 29 35 30 34 35 33 36 30
23 | 9 21 9 10 11 3 8 11 11 15 4 | 18 12 17 22 21 18 17 21 24 18 17
24 | 9 8 6 7 10 4 8 10 8 10 3 | 28 26 24 25 27 23 26 29 25 27 25
25 | 10 13 8 8 8 5 9 8 7 9 3 | 18 22 19 17 19 16 21 16 17 20 17
26 | 8 9 8 10 13 3 10 13 8 12 3 | 822 821 822 824 700 823 825 820 826 824 823
27 | 8 14 6 10 8 4 9 9 8 16 3 | 22 23 20 24 21 19 22 21 21 26 20
28 | 8 17 7 8 11 2 7 12 10 11 3 | 18 23 18 23 18 18 21 19 19 22 18
29 | 14 21 6 8 10 5 11 15 12 16 4 | 29 25 24 27 26 24 24 25 25 29 24
30 | 12 10 7 12 17 4 10 8 5 8 3 | 26 24 24 22 29 21 23 26 22 24 22
31 | 8 12 6 21 11 3 7 14 9 14 4 | 25 26 22 29 27 23 26 26 27 21 23
32 | 7 12 9 10 8 3 11 9 7 13 3 | 22 30 20 18 25 19 32 21 22 22 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 8 11 13 4 9 13 10 13 |T 56 57 58 59 55 55 58 58 58 61 56
WRMS | 9 13 8 10 12 4 9 12 10 13 |NE 55 58 56 57 52 54 57 57 57 60 54
MEDI | 8 11 8 10 11 4 8 12 10 13 |MD 25 25 22 25 26 23 26 25 25 26 23
Table 3.2032.6 GPS week: 2032 Day: 6 MJD: 58474.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 9 9 11 9 16 3 8 11 7 7 3 | 33 34 35 33 27 32 35 34 34 34 32
2E | 10 10 6 14 9 6 12 15 9 13 3 | 29 29 28 32 28 27 30 28 26 26 27
3 | 7 10 12 9 12 4 9 15 8 8 3 | 69 68 75 67 68 69 69 71 68 70 69
X4 | 9 --- --- --- --- 14 11 --- --- --- 10 | 30 --- --- --- --- 26 30 --- --- --- 28
5 | 7 8 11 10 7 5 12 21 15 18 4 | 44 49 45 47 46 42 54 35 40 42 44
6E | 6 8 9 20 17 3 8 9 8 8 4 | 40 44 40 44 38 39 41 39 38 43 39
7 | 9 11 6 10 13 3 11 12 11 17 4 | 30 23 23 28 25 26 23 31 31 28 25
8 | 8 11 4 8 7 3 7 12 8 6 2 | 23 25 22 24 23 22 26 24 26 25 23
9 | 10 9 11 9 11 4 8 6 8 12 3 | 31 38 26 30 30 30 37 35 35 38 31
10 | 10 9 10 8 6 4 9 10 7 10 3 | 23 29 22 25 25 24 29 25 25 28 23
11E | 9 10 10 9 11 3 7 8 10 10 3 | 38 38 43 43 43 41 40 40 42 39 40
12 | 10 19 6 11 9 4 10 14 12 10 4 | 31 28 25 30 27 26 26 29 29 29 26
13 | 7 10 9 6 8 3 10 18 11 15 3 | 25 31 26 27 26 28 28 33 31 36 27
14 | 7 7 8 9 5 3 7 10 11 12 3 | 36 35 36 34 36 35 34 37 42 37 35
15 | 5 13 6 7 7 3 8 13 12 16 3 | 34 41 37 37 37 33 38 34 32 31 34
16 | 13 22 7 10 11 5 8 15 14 15 4 | 27 26 27 29 24 26 23 29 28 27 24
17 | 6 12 8 8 9 3 7 14 11 10 3 | 28 32 26 33 28 29 32 34 32 33 29
X18E | 15 --- 15 20 11 6 14 20 12 16 5 | 249 --- 257 249 253 253 251 255 254 260 253
19 | 6 19 5 10 10 3 8 14 14 10 3 | 25 29 25 27 24 24 25 22 23 25 23
20 | 9 11 6 13 10 4 8 19 14 20 4 | 26 31 28 28 32 31 29 40 37 41 30
21E | 8 7 6 8 10 3 6 12 10 11 3 | 18 19 20 18 23 17 19 18 20 20 17
22 | 6 11 9 9 9 3 10 17 13 19 4 | 37 37 38 37 39 39 38 45 45 42 38
23 | 6 23 9 10 9 4 7 11 13 13 4 | 25 14 21 27 22 24 20 28 32 24 22
24 | 8 10 5 8 9 3 9 13 7 10 3 | 29 31 28 27 30 27 29 34 32 34 29
25 | 7 14 7 9 7 2 10 10 9 9 3 | 22 26 24 23 21 22 24 22 21 26 21
26 | 8 9 8 10 11 3 7 13 8 10 3 | 867 867 867 871 681 869 870 865 870 868 869
27 | 7 13 6 6 8 4 9 12 7 10 3 | 20 25 22 21 22 20 23 23 21 23 20
28 | 11 20 7 12 11 3 8 12 10 11 4 | 27 27 23 27 20 21 23 24 22 25 21
29 | 13 22 4 8 8 4 11 18 16 13 4 | 36 32 30 33 30 31 32 36 29 35 31
30 | 6 11 6 8 13 3 8 11 7 7 3 | 28 27 28 26 30 25 26 30 27 28 26
31 | 10 15 7 18 11 4 6 14 10 16 4 | 27 32 27 32 30 27 30 33 30 28 27
32 | 7 12 8 12 6 3 12 7 9 8 3 | 28 36 27 25 30 28 35 31 32 31 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 8 10 10 4 9 13 11 12 |T 63 60 64 65 58 62 64 66 66 66 62
WRMS | 8 13 8 11 9 4 9 12 11 12 |NE 62 65 63 64 56 61 63 66 65 66 61
MEDI | 8 11 7 9 9 3 8 13 10 11 |MD 29 31 27 30 30 27 30 33 32 31 28
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 4.2032 GPS week: 2032 MJD: 58468.0-58474.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 |U 8 8 22 |U 13 19 48 |U 12 11 34 |
emr | emr 2943 |U 18 17 41 |U 17 18 54 |U 20 15 48 |
esa | esa 2962 | 12 12 22 |U 13 20 46 | 13 10 32 |
gfz | gfz 2969 |U 12 13 28 |U 13 20 44 |U 12 11 32 |
grg | grg 2957 |U 12 13 23 |U 12 20 48 | 12 10 35 |
igr | igr 2960 | 11 12 22 | 12 19 46 | 12 11 32 |
igs | igs 3056 | 9 9 23 | 13 18 48 | 13 10 33 |
jpl | jpl 3072 |U 0 0 0 |U 0 0 0 |U 0 0 0 |
mit | mit 2976 | 18 17 37 |U 23 30 80 |U 16 14 41 |
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 5.2032.0 GPS week: 2032 Day: 0 MJD: 58468.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 10 22 | 13 21 49 | 14 11 36 |
emr | emr 2972 | 13 15 25 | 16 13 58 | 21 18 55 |
esa | esa 2976 | 13 13 19 | 14 22 47 | 14 13 36 |
gfz | gfz 2972 | 15 10 22 | 12 22 46 | 13 12 38 |
grg | grg 2973 | 18 16 25 | 14 21 45 | 12 11 35 |
igr | igr 2967 | 18 13 24 | 13 21 46 | 13 12 37 |
igs | igs 3064 | 14 11 21 | 13 20 49 | 14 13 37 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 2976 | 12 24 49 | 42 41 90 | 26 17 50 |
Table 5.2032.1 GPS week: 2032 Day: 1 MJD: 58469.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 11 21 | 12 21 47 | 14 12 37 |
emr | emr 2972 | 15 17 29 | 14 15 64 | 21 17 51 |
esa | esa 2976 | 12 12 20 | 12 21 48 | 15 12 35 |
gfz | gfz 2972 | 11 12 21 | 11 23 42 | 13 11 36 |
grg | grg 2976 | 12 16 19 | 10 21 46 | 13 11 38 |
igr | igr 2959 | 11 13 19 | 11 19 45 | 14 11 34 |
igs | igs 3072 | 8 10 19 | 11 19 49 | 14 11 35 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 2976 | 17 17 42 | 17 22 71 | 20 24 43 |
Table 5.2032.2 GPS week: 2032 Day: 2 MJD: 58470.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 8 25 | 11 17 46 | 13 11 33 |
emr | emr 2972 | 30 20 100 | 15 18 44 | 26 20 59 |
esa | esa 2976 | 12 9 23 | 11 17 45 | 13 10 29 |
gfz | gfz 2972 | 12 10 31 | 12 17 40 | 13 11 37 |
grg | grg 2874 | 11 13 27 | 12 18 54 | 12 9 33 |
igr | igr 2966 | 11 10 30 | 11 17 45 | 12 11 29 |
igs | igs 3072 | 9 8 34 | 11 16 44 | 14 12 34 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 2976 | 24 9 32 | 14 20 48 | 12 12 33 |
Table 5.2032.3 GPS week: 2032 Day: 3 MJD: 58471.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 8 8 20 | 10 16 46 | 12 10 31 |
emr | emr 2972 | 29 15 51 | 15 16 49 | 18 12 42 |
esa | esa 2976 | 11 15 23 | 9 17 41 | 13 10 27 |
gfz | gfz 2972 | 14 21 46 | 9 18 42 | 12 10 23 |
grg | grg 2974 | 12 14 22 | 10 19 48 | 13 9 29 |
igr | igr 2964 | 11 15 24 | 9 16 43 | 13 10 29 |
igs | igs 3064 | 14 9 25 | 10 16 46 | 13 9 28 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 2976 | 18 10 25 | 18 34 75 | 12 8 30 |
Table 5.2032.4 GPS week: 2032 Day: 4 MJD: 58472.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 6 6 25 | 7 17 47 | 12 9 33 |
emr | emr 2972 | 14 11 27 | 17 20 54 | 20 14 49 |
esa | esa 2976 | 8 8 19 | 8 18 45 | 13 9 31 |
gfz | gfz 2971 | 8 9 21 | 7 18 45 | 12 9 31 |
grg | grg 2967 | 8 8 25 | 7 19 51 | 15 12 38 |
igr | igr 2964 | 7 8 17 | 7 17 47 | 12 10 32 |
igs | igs 3060 | 7 7 23 | 8 18 48 | 14 11 34 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 2976 | 14 18 31 | 14 27 73 | 15 10 34 |
Table 5.2032.5 GPS week: 2032 Day: 5 MJD: 58473.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 | 7 9 25 | 15 20 43 | 10 12 40 |
emr | emr 2861 | 11 25 33 | 14 24 47 | 17 12 46 |
esa | esa 2880 | 13 12 29 | 13 22 37 | 12 11 39 |
gfz | gfz 2957 | 9 13 27 | 14 21 39 | 10 11 34 |
grg | grg 2960 | 9 10 24 | 13 21 40 | 9 12 43 |
igr | igr 2941 | 9 12 23 | 13 21 41 | 11 11 38 |
igs | igs 3006 | 7 10 22 | 14 20 42 | 12 10 37 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 2976 | 25 26 47 | 29 25 129 | 13 19 61 |
Table 5.2032.6 GPS week: 2032 Day: 6 MJD: 58474.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 8 7 19 | 24 21 56 | 11 10 29 |
emr | emr 2880 | 16 13 22 | 27 22 61 | 18 11 33 |
esa | esa 2976 | 13 14 21 | 24 21 58 | 12 8 26 |
gfz | gfz 2971 | 12 14 30 | 25 22 55 | 9 9 26 |
grg | grg 2975 | 12 13 16 | 20 20 56 | 10 8 28 |
igr | igr 2963 | 11 12 20 | 23 21 57 | 10 9 29 |
igs | igs 3054 | 8 8 16 | 24 20 57 | 11 7 25 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 2976 | 13 16 31 | 30 39 77 | 15 11 37 |
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 6.2032 GPS week: 2032 MJD: 58468.500-58474.500
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 | 11 -29 120 80 5 | 7 15
| 14 18 66 84 8 | 3
emr uuuuu | 6 38 -30 59 0 | 27 30
| 17 22 85 64 6 | 2
esa uuuuu | -2 -10 68 61 2 | 14 18
| 11 16 75 46 3 | 1
gfz uuuuu | 7 -27 43 40 4 | 19 22
| 11 28 169 48 5 | 2
grg uuuuu | 20 26 -64 28 -3 | 2 9
| 12 8 43 59 2 | 1
igr xxxxx | 8 8 -50 -3 0 | 2 11
| 10 8 53 22 4 | 1
irf xxxxx | -15 5 -38 -35 3 | -1 10
| 6 9 22 22 5 | 2
jpl uuuuu | -31 -8 -30 -50 1 | 26 30
| 16 28 66 57 13 | 4
mit uuuuu | -2 9 -80 -116 -2 | 18 21
| 17 15 52 50 4 | 2
ngs uuuuu | 7 9 61 -60 -2 | 14 16
| 16 31 176 57 5 | 5
sio uuuux | -15 24 -254 -142 6 | 47 49
| 18 11 55 57 10 | 2
Table 7.2032.0 GPS week: 2032 Day: 0 MJD: 58468.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -18 -51 128 -17 2 | 6 16
emr uuuuu | 2 59 113 97 -6 | 27 30
esa uuuuu | 15 11 -33 35 4 | 15 19
gfz uuuuu | 15 -33 -102 39 8 | 18 22
grg uuuuu | 31 38 3 89 -1 | 4 10
igr xxxxx | 17 9 -51 -18 -4 | 3 12
irf xxxxx | -23 -10 -25 -54 -3 | 2 12
jpl uuuuu | -26 -42 50 25 -16 | 32 37
mit uuuuu | -35 -8 -61 -162 -3 | 21 24
ngs uuuuu | 10 38 45 -59 -2 | 20 22
sio uuuux | -6 21 -271 -152 -2 | 48 50
Table 7.2032.1 GPS week: 2032 Day: 1 MJD: 58469.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 -43 167 74 9 | 4 15
emr uuuuu | 28 64 -108 94 -6 | 27 31
esa uuuuu | -11 -13 28 18 1 | 15 19
gfz uuuuu | -7 -16 -12 53 10 | 18 23
grg uuuuu | 33 34 -86 72 -1 | 4 10
igr xxxxx | 7 -4 -55 -4 -3 | 3 12
irf xxxxx | -14 7 -60 -65 -4 | 1 11
jpl uuuuu | -56 -24 -48 -36 -15 | 30 35
mit uuuuu | 7 13 -127 -193 -7 | 21 23
ngs uuuuu | 18 20 248 -45 -11 | 21 23
sio uuuux | 0 13 -289 -161 5 | 47 49
Table 7.2032.2 GPS week: 2032 Day: 2 MJD: 58470.500
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 | 11 -44 201 87 18 | 3 14
emr uuuuu | 10 30 8 -10 9 | 24 27
esa uuuuu | -9 9 29 125 -2 | 13 17
gfz uuuuu | 22 2 -85 35 1 | 16 20
grg uuuuu | 4 25 -118 62 -5 | 1 8
igr xxxxx | 15 15 -49 -36 -4 | 0 10
irf xxxxx | -19 14 -63 -17 0 | -3 9
jpl uuuuu | -9 -32 33 -100 -4 | 24 29
mit uuuuu | 13 20 -138 -59 -4 | 18 20
ngs uuuuu | -24 -19 132 -178 -4 | 12 14
sio uuuux | -17 42 -178 -56 -8 | 46 47
Table 7.2032.3 GPS week: 2032 Day: 3 MJD: 58471.500
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 -11 60 14 9 | 6 16
emr uuuuu | 9 39 -42 149 5 | 27 29
esa uuuuu | -12 -13 52 0 0 | 14 18
gfz uuuuu | 9 -4 -102 35 0 | 18 22
grg uuuuu | 7 27 -30 5 -5 | 2 8
igr xxxxx | 7 4 33 21 -2 | 1 10
irf xxxxx | -5 14 -58 -4 3 | -2 9
jpl uuuuu | -17 -20 2 27 10 | 22 26
mit uuuuu | 6 35 -136 -58 1 | 17 20
ngs uuuuu | 3 -23 252 -62 2 | 14 16
sio uuuux | -7 13 -224 -130 12 | 45 47
Table 7.2032.4 GPS week: 2032 Day: 4 MJD: 58472.500
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 -2 41 108 -1 | 7 16
emr uuuuu | 20 54 -129 69 -4 | 27 29
esa uuuuu | -6 -30 85 107 4 | 13 18
gfz uuuuu | -7 -10 44 -55 9 | 18 22
grg uuuuu | 29 16 -48 26 -3 | 0 10
igr xxxxx | 1 0 -6 -14 2 | 0 11
irf xxxxx | -12 0 -10 -25 9 | -4 10
jpl uuuuu | -29 24 -30 -104 17 | 22 26
mit uuuuu | 11 -9 -35 -106 4 | 16 19
ngs uuuuu | 1 -29 87 3 -5 | 11 14
sio uuuux | -47 21 -213 -164 19 | 45 47
Table 7.2032.5 GPS week: 2032 Day: 5 MJD: 58473.500
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 | 20 -31 184 243 -4 | 10 15
emr uuuuu | -21 17 -77 -34 5 | 27 29
esa uuuuu | -2 -28 119 61 5 | 16 18
gfz uuuuu | 0 -51 275 78 1 | 21 23
grg uuuuu | 13 23 -66 -90 -2 | 1 9
igr xxxxx | -11 12 -101 4 5 | 1 11
irf xxxxx | -17 3 -19 -53 10 | -1 9
jpl uuuuu | -34 25 -73 -63 8 | 25 28
mit uuuuu | -1 4 -21 -115 0 | 18 20
ngs uuuuu | 23 40 -197 -27 2 | 10 13
sio uuuux | 1 28 -346 -238 18 | 48 50
Table 7.2032.6 GPS week: 2032 Day: 6 MJD: 58474.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 14 -22 60 49 0 | 11 15
emr uuuuu | -8 4 27 48 -4 | 29 31
esa uuuuu | 13 -3 198 78 5 | 17 19
gfz uuuuu | 14 -76 281 95 -1 | 23 25
grg uuuuu | 25 16 -103 29 -2 | 0 8
igr xxxxx | 19 18 -122 24 4 | 2 11
irf xxxxx | -16 10 -34 -29 5 | 0 10
jpl uuuuu | -46 13 -143 -99 9 | 26 29
mit uuuuu | -15 11 -40 -118 -3 | 18 20
ngs uuuuu | 20 34 -144 -53 3 | 10 13
sio uuuux | -29 31 -260 -96 0 | 52 53
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