[IGSREPORT-26429] Wk 2040 IGS Final Orbits
acc
acc at igs.org
Sun Mar 3 16:23:20 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2040 (Feb 10, 2019 - Feb 16, 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:
igs2040[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2040[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2040[0-6].cls IGS GPS clock combination summary report.
igs20407.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20407.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 | 21 22 21 22 BJNM LAUT OHI3 TIXI OHI3 TIXI
0 | EMR | DAEJ NIST
0 | ESA | DAV1
0 | GFZ | 18 GODE REUN AREQ DAV1 GODE REUN
0 | GRG | 21 21 CRO1 GLSV GLSV
0 | JPL | POLV LAUT MAR6 POLV
0 | MIT | PALM PALM
1 | COD | ANKR MAR6 TLSE TSKB ANKR
1 | EMR | GRAZ TLSE GRAZ MAR6
1 | ESA | 16 19 20 21 22 18 ALIC ASPA BRAZ CHTI DARW FAA1 FLRS
1 | ESA | GLSV GRAS GRAZ GUUG HOB2 INEG KERG KOUC LAUT MAG0
1 | ESA | MATE MKEA NANO NIUM NYA1 OHI2 ONSA POVE RIOP SALU
1 | ESA | SAVO SOFI THTI TUVA WTZR FLRS ONSA TLSE
1 | GFZ | FLRS GODE CCJ2 FLRS GODE TLSE TSKB
1 | GRG | CCJ2 CHTI GLSV GODE TLSE CHTI DAV1 GLSV GODE STK2
1 | JPL | LAUT
2 | COD | 10 10 18 BJNM NAUR TIXI BJNM CHTI NAUR TIXI
2 | EMR | 3 3 BOR1 TLSE
2 | ESA | 19 20 21 22 CHTI NRIL PDEL TRO1 CHTI
2 | GFZ | 27 DAV1 GODE NYA1 REUN DAV1 GODE NYA1 REUN TRO1
2 | GRG | ABMF GLSV MANA NRIL TRO1 GLSV NNOR NRIL PDEL TRO1
2 | JPL | DAV1 DAV1 NRIL
2 | MIT | 18 PALM PALM
3 | COD | 18
3 | EMR | GRAZ
3 | ESA | 3 18 22 3 18 ABPO ALIC ASPA BAKE BJCO BOGT BRMU BRST
3 | ESA | CEDU CHUR CUSV DARW DGAR FLIN HOB2 IRKJ KARR KERG
3 | ESA | KOUC KOUR LMMF MBAR MDVJ MGUE MKEA MOBS NANO NKLG
3 | ESA | NRIL NTUS OHI2 OHI3 ONSA PERT PETS PIMO PTBB SALU
3 | ESA | SCOR STK2 THTI TOW2 TWTF WTZR ABPO ALIC ASPA BAKE
3 | ESA | BJCO BOGT BRMU BRST CEDU CHUR CUSV DGAR DRAO FLIN
3 | ESA | HOB2 IRKJ KARR KERG KOUC KOUR MATE MBAR MDVJ MGUE
3 | ESA | MKEA MOBS NANO NKLG NOVM NRIL NTUS OHI2 OHI3 ONSA
3 | ESA | PERT PETS PIMO PTBB SALU SEYG STK2 TOW2 TWTF WTZR
3 | GFZ | 18 BJNM GODE REUN CHTI GODE REUN
3 | GRG | 18 18 ABMF GLSV NRMD PIMO ABMF CHTI GLSV NRMD PIMO
3 | JPL | YELL
3 | MIT | PIMO
4 | COD | ANKR BOR1 TIXI ABMF ANKR TIXI
4 | ESA | 22 LMMF LMMF
4 | GFZ | 18 18 BJNM CHTI GODE BJNM GODE
4 | GRG | ABMF GLSV NRMD GLSV NRMD
5 | COD | 18 18 ANKR BJNM NAUR TIXI TLSE ANKR BJNM NAUR TIXI
5 | EMR | 18 BOR1 DAEJ GRAZ TLSE BJNM DAEJ
5 | ESA | 18 TLSE
5 | GFZ | GODE REUN GODE REUN TLSE
5 | GRG | 13 18 13 18 GLSV SCOR TLSE GLSV SCOR TLSE YELL
5 | JPL | CHTI CHTI
5 | MIT | 18 ANKR DAV1
6 | COD | DAV1 CHTI DAV1
6 | EMR | GRAZ TLSE TLSE
6 | ESA | 1 2 3 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
6 | ESA | 21 22 23 24 25 26 27 28 29 30 31 32 1 2 3 5 6 7 8
6 | ESA | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
6 | ESA | 26 27 28 29 30 31 32
6 | GFZ | ABMF BJNM CHTI GODE BJNM CHTI GODE
6 | GRG | 6 18 18 BAKE GLSV TLSE GLSV TLSE
6 | JPL | 18
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
----+--------+--------+-------------
3 | ESA | ~06:15 | ~ 0.70 ns
5 | ESA | ~10:30 | ~ 0.08 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 G03 | 4 | 4 | 4 | 4 | | 4 | 4 |
PRN G04 | 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 | .0 -.1 .2 -8 8 -8 -.02
EMR | 0 | -2.8 -2.9 16.9 -41 11 -4 .06
ESA | 0 | -.3 .1 1.3 13 22 10 -.19
GFZ | 0 | 1.3 -.4 -.1 -10 -36 16 -.03
GRG | 0 | -.5 -4.3 22.6 49 6 93 .07
JPL | 0 | -2.9 -3.8 3.2 3 -8 11 -.06
MIT | 0 | .8 -6.4 8.5 14 71 -21 .07
NGS | 0 | -8.5 -2.8 8.3 15 -23 -13 -.13
SIO | 0 | -3.9 .9 -8.4 5 18 9 .01
COD | 1 | .3 .2 .9 -3 13 -22 -.36
EMR | 1 | 2.5 2.6 6.9 -20 23 -12 -.10
ESA | 1 | .5 -.5 .4 26 9 47 -.30
GFZ | 1 | .7 -.1 .0 0 -26 8 -.11
GRG | 1 | 3.0 -3.2 22.4 93 -3 52 -.05
JPL | 1 | -5.3 -6.2 4.0 4 7 22 -.16
MIT | 1 | 2.5 -6.6 7.2 -10 26 3 -.08
NGS | 1 | 1.3 -.8 8.5 28 -70 48 -.06
SIO | 1 | 1.0 .1 -10.8 -25 -2 -3 -.01
COD | 2 | .0 .4 -.0 0 8 -28 -.15
EMR | 2 | -4.7 -5.3 18.2 -15 63 -69 -.03
ESA | 2 | .2 -.5 1.2 14 14 14 -.10
GFZ | 2 | .8 -.5 -.0 4 -13 7 -.01
GRG | 2 | 2.5 -5.5 21.5 92 -14 47 .15
JPL | 2 | -.5 -3.3 9.3 4 1 17 -.13
MIT | 2 | 4.3 -3.2 9.2 -10 75 -7 .10
NGS | 2 | -4.7 -4.7 20.2 37 -77 -17 .08
SIO | 2 | .3 -.5 -7.7 -6 10 3 .24
COD | 3 | .1 .3 .1 4 11 -19 -.27
EMR | 3 | -.1 -3.4 7.1 -14 85 -104 .06
ESA | 3 | .4 .5 1.2 9 24 7 -.05
GFZ | 3 | .1 -1.3 .0 -26 -10 28 .08
GRG | 3 | -.2 -4.4 2.8 92 5 39 .20
JPL | 3 | -1.5 -4.7 19.2 -10 8 2 -.27
MIT | 3 | 2.2 -4.1 7.1 11 49 -18 .09
NGS | 3 | 3.1 -2.0 15.2 13 -77 -13 -.22
SIO | 3 | -1.0 .3 -7.1 -4 -6 25 .08
COD | 4 | -.2 -.2 .1 -8 25 -12 -.08
EMR | 4 | .6 -5.9 9.8 -19 39 -77 -.10
ESA | 4 | 1.2 -.1 1.2 -7 15 23 -.07
GFZ | 4 | -.1 .0 .5 -15 5 0 .07
GRG | 4 | 3.1 -6.4 16.3 76 2 28 .07
JPL | 4 | 2.6 -8.4 13.0 -7 11 -2 -.32
MIT | 4 | -1.8 -7.6 11.1 -15 42 -8 .18
NGS | 4 | -4.3 -9.9 19.3 -10 -81 -51 .18
SIO | 4 | .9 -3.9 -1.0 -6 16 -13 .29
COD | 5 | .4 -.3 .2 -1 11 -5 -.23
EMR | 5 | 1.5 -2.4 5.0 -16 60 -110 -.13
ESA | 5 | .9 .4 .5 16 4 19 -.18
GFZ | 5 | .3 -.4 -.4 -21 -8 10 -.09
GRG | 5 | 6.6 -3.4 13.5 76 -5 32 -.0
JPL | 5 | 4.4 -4.9 2.1 6 -1 -1 -.43
MIT | 5 | 4.3 -5.8 7.4 -12 30 2 .15
NGS | 5 | -6.3 -4.8 14.8 -9 -45 -40 -.01
SIO | 5 | 4.5 -5.1 .9 -5 2 3 .03
COD | 6 | -.2 .1 -.1 8 9 -6 -.10
EMR | 6 | 8.2 -1.3 2.9 -35 57 -80 .17
ESA | 6 | .7 .2 1.2 1 6 15 .01
GFZ | 6 | .4 -.2 -.5 -13 -27 -9 .11
GRG | 6 | 11.0 -4.5 2.9 75 14 30 .04
JPL | 6 | 3.4 -2.7 7.4 -3 -2 20 -.15
MIT | 6 | 3.1 -3.0 9.9 -19 29 7 .09
NGS | 6 | -2.4 -6.5 14.2 -24 -51 -59 .11
SIO | 6 | 3.1 3.9 3.7 -29 8 14 .06
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 1.2040.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2040.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 2.2040.[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 3.2040.[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 5.2040.0-6). 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 2040 summary. (Feb 10, 2019 - Feb 16, 2019)
Table 1.2040.a GPS week: 2040 MJD: 58524.000-58530.000
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 250| -1 0 1 2 13 9 -.03 9 8 | -523 40 8 102
| 0 0 1 13 16 7 .01 | 120 134
emr 79| 0 -1 1 -3 -32 13 .27 13 13 | 179219 -525 16 129
| 1 2 3 21 14 15 .04 | 2006 1293
esa 150| 0 0 0 -7 -1 14 -.06 10 10 | -608 -977 16 225
| 0 0 0 17 9 10 .02 | 503 1018
gfz 182| 0 1 2 0 3 -12 .12 12 12 | -231 102 12 116
| 0 0 2 15 16 11 .02 | 399 449
grg 101| 0 0 -2 9 15 -6 -.16 12 10 | -48 107 11 170
| 1 0 4 16 15 27 .02 | 272 270
igr n/a| 0 0 -1 -2 -1 -9 -.05 5 5 | 4101 -353 11 67
| 0 0 0 17 3 11 .01 | 1485 999
jpl 80| 0 0 2 5 0 9 .20 9 9 | 214887 -425 8 87
| 1 1 2 14 12 9 .03 | 1736 1071
mit 348| 1 -1 -4 2 -7 -23 -.18 15 13 | -204 -76 82 1629
| 0 0 1 21 38 9 .03 | 232 152
ngs 205| 0 0 2 8 -18 0 -.09 12 12 | -511 16 1121 2313
| 0 0 2 21 33 12 .03 | 92 147
sio 325| 1 0 -8 -45 56 -22 -.02 18 17 | --- --- --- ---
| 0 1 2 98 95 41 .05 | --- ---
Table 1.2040.b GPS week : 2040 MJD: 58524.000-58530.000
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 | 5 5 5 5 5 5 5 |
3 | 5 7 7 7 5 6 7 |
4 | 17 22 31 12 28 20 23 |
5 | 4 5 5 6 5 4 4 |
6 | 3 4 4 4 3 3 4 |
7 | 3 4 4 4 4 3 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 4 3 3 3 4 |
10 | 5 7 7 6 5 6 7 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 6 6 |
13 | 4 4 4 4 4 4 4 |
14 | 5 4 5 5 5 5 5 |
15 | 4 4 4 4 4 4 5 |
16 | 4 5 5 5 5 4 5 |
17 | 3 4 4 4 4 4 4 |
18 | 3 4 4 3 4 4 3 |
19 | 5 5 5 5 4 5 5 |
20 | 4 5 5 4 4 5 5 |
21 | 4 5 5 4 5 4 5 |
22 | 4 5 5 4 4 4 4 |
23 | 6 6 5 6 6 6 6 |
24 | 3 4 3 4 4 4 3 |
25 | 5 4 4 4 4 3 4 |
26 | 5 4 4 4 0 7 5 |
27 | 3 3 4 3 3 3 4 |
28 | 3 4 4 4 3 3 4 |
29 | 5 5 5 5 4 4 5 |
30 | 3 3 4 3 3 3 3 |
31 | 4 4 4 4 4 4 5 |
32 | 3 3 4 4 3 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 2.2040.0 GPS week: 2040 Day: 0 MJD: 58524.000
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 0 3 11 12 15 -.03 9 8 | -457 -3 9 113
emr 80| 0 0 2 1 -28 23 .27 13 13 | 180643 339 14 112
esa 150| 0 0 0 -7 -2 18 -.08 10 10 | -780 -277 9 221
gfz 176| 1 2 0 0 -3 -27 .13 10 10 | -456 105 11 200
grg 100| 0 0 1 -22 3 20 -.19 11 9 | -78 -23 12 186
igr n/a| 0 0 -2 9 -1 0 -.05 5 4 | 5037 295 12 72
jpl 80| -1 -2 2 0 3 0 .19 8 8 | 215970 417 8 105
mit 348| 1 0 -4 27 23 -30 -.15 15 13 | -64 -259 98 1531
ngs 206| 0 1 -1 37 -29 -2 -.07 11 11 | -487 6 953 2314
sio 317| 1 0 -11 -60 46 -4 .04 15 13 | --- --- --- ---
Table 2.2040.1 GPS week: 2040 Day: 1 MJD: 58525.000
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 0 1 -11 24 6 -.01 9 9 | -362 39 8 98
emr 80| 0 1 -1 15 -24 27 .27 13 13 | 181127 -986 15 118
esa 150| 0 0 -1 17 8 31 -.07 10 10 | -754 -1118 9 224
gfz 181| 0 2 2 9 -13 -25 .13 9 10 | -462 416 11 89
grg 102| 1 0 3 16 9 -26 -.17 12 10 | 60 -31 11 157
igr n/a| 0 0 -2 7 -3 -32 -.05 5 5 | 5345 -367 12 60
jpl 80| -3 -1 -1 16 -4 7 .15 10 10 | 216529 -454 9 94
mit 348| 1 -1 -3 -29 -30 -25 -.17 15 13 | -484 -285 143 1643
ngs 195| 0 0 1 -14 -8 8 -.06 12 12 | -400 114 1293 2472
sio 325| 2 0 -11 -85 65 10 .01 19 18 | --- --- --- ---
Table 2.2040.2 GPS week: 2040 Day: 2 MJD: 58526.000
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| -1 0 0 6 28 7 -.05 8 8 | -696 157 8 96
emr 80| -2 -6 8 16 -56 -15 .32 17 16 | 180563 -388 16 133
esa 150| 0 0 -1 0 -2 -3 -.06 10 10 | -209 -2214 8 205
gfz 181| 0 2 1 4 16 -11 .13 12 11 | 48 -130 13 102
grg 97| 0 0 -1 0 -5 29 -.12 10 9 | 210 -228 13 165
igr n/a| 0 0 -2 9 1 -4 -.04 5 5 | 5206 -135 10 56
jpl 80| 0 -1 0 15 -20 29 .19 8 8 | 216169 -226 9 89
mit 348| 1 0 -6 13 36 -21 -.19 15 14 | -192 -20 66 1588
ngs 211| 0 0 4 -16 -34 -28 -.07 11 11 | -564 -34 1072 2090
sio 325| 2 0 -11 -73 84 6 -.02 18 18 | --- --- --- ---
Table 2.2040.3 GPS week: 2040 Day: 3 MJD: 58527.000
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 0 -2 33 22 -.04 8 8 | -604 230 7 91
emr 80| 0 0 1 7 -14 5 .25 13 13 | 180693 -2743 18 159
esa 150| 1 1 0 -7 13 10 -.05 10 10 | 153 -1269 19 328
gfz 183| 0 1 6 -11 22 1 .07 14 15 | 444 -572 15 93
grg 104| 0 0 -8 25 38 -41 -.14 15 11 | 248 85 12 185
igr n/a| 0 0 0 -3 -7 -14 -.08 5 5 | 5314 -2118 17 85
jpl 80| -1 -1 5 1 12 7 .20 9 9 | 216179 -2388 8 79
mit 348| 1 0 -6 -7 -78 -28 -.16 14 13 | -203 60 52 1560
ngs 213| 0 0 3 3 -24 5 -.08 13 12 | -608 218 1150 2491
sio 327| 0 1 -6 -11 -79 -24 .00 17 17 | --- --- --- ---
Table 2.2040.4 GPS week: 2040 Day: 4 MJD: 58528.000
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 0 -14 0 3 -.03 8 8 | -628 106 9 102
emr 80| 3 -2 -1 -5 -46 26 .20 12 12 | 176884 1131 17 170
esa 150| 0 0 0 -38 -5 17 -.10 10 10 | -976 653 11 242
gfz 185| 0 1 5 7 20 -7 .14 13 12 | -494 523 12 116
grg 104| 0 0 0 27 13 -28 -.16 11 10 | -266 181 10 161
igr n/a| -1 1 -2 -5 1 -8 -.05 5 4 | 2484 690 10 64
jpl 80| -1 0 1 8 15 8 .20 8 8 | 213111 638 9 83
mit 348| 1 -2 -4 24 4 -34 -.23 16 14 | -471 -147 54 1904
ngs 207| 0 0 2 -3 -42 4 -.10 12 12 | -630 95 1178 2360
sio 328| 0 2 -6 24 63 -10 -.09 16 16 | --- --- --- ---
Table 2.2040.5 GPS week: 2040 Day: 5 MJD: 58529.000
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 0 6 0 2 -.03 8 8 | -486 -123 6 99
emr 80| 0 0 0 -42 -26 17 .31 12 12 | 178255 -1350 17 135
esa 150| 0 1 -1 -16 -10 11 -.04 9 9 | -353 -2090 8 237
gfz 185| 1 1 -1 -29 -16 0 .10 13 12 | -16 -268 13 89
grg 101| 0 0 -1 11 17 -13 -.18 11 10 | 13 128 10 174
igr n/a| -1 0 -1 -39 2 1 -.05 5 5 | 3490 -1228 10 59
jpl 80| 0 0 2 -24 -11 13 .24 8 9 | 214008 -1241 9 99
mit 349| 0 -1 -2 5 8 -10 -.19 15 13 | 191 49 69 1577
ngs 203| -1 0 5 32 51 0 -.12 13 13 | -402 -248 1068 2149
sio 327| 0 0 -4 99 -12 -23 -.09 15 15 | --- --- --- ---
Table 2.2040.6 GPS week: 2040 Day: 6 MJD: 58530.000
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 2 25 -7 10 -.06 11 11 | -433 -123 11 115
emr 79| 2 -2 1 -20 -29 9 .24 13 13 | 176369 322 18 76
esa 150| -1 0 0 -4 -11 16 -.04 9 9 | -1339 -524 48 121
gfz 184| 0 0 2 18 -3 -17 .12 13 12 | -683 644 12 123
grg 99| 0 0 -7 10 30 11 -.16 11 10 | -525 641 11 167
igr n/a| -1 0 -2 2 -1 -9 -.03 5 5 | 1834 391 12 73
jpl 80| 0 1 3 16 0 1 .26 9 9 | 212243 274 8 63
mit 349| 0 -1 -3 -14 -16 -12 -.18 16 14 | -208 65 95 1603
ngs 203| -2 0 4 20 -43 4 -.13 12 12 | -489 -33 1139 2317
sio 327| 1 2 -6 -213 230 -112 -.03 24 23 | --- --- --- ---
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 3.2040.0 GPS week: 2040 Day: 0 MJD: 58524.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 7 8 11 8 2 7 7 7 14 3 | 18 25 23 19 21 20 24 21 20 30 20
2 | 6 12 9 14 10 5 6 25 14 16 4 | 18 20 21 29 17 21 19 25 25 25 18
3E | 10 9 15 19 11 6 10 11 14 13 4 | 246 226 249 245 246 247 206 245 243 241 245
X4 | 15 --- --- --- 18 41 --- --- --- --- 16 | 446 --- --- --- 448 448 --- --- --- --- 446
5E | 8 9 8 9 13 3 9 14 9 14 3 | 126 127 124 125 126 125 127 128 128 129 126
6 | 7 9 9 8 7 1 6 13 9 11 3 | 29 31 32 31 25 28 30 25 29 31 28
7 | 7 11 9 5 5 4 8 13 11 16 3 | 25 29 23 29 21 22 27 22 23 23 24
8 | 7 9 5 9 5 4 7 8 6 11 2 | 20 25 21 21 20 21 24 21 21 24 20
9 | 9 7 12 6 8 3 8 7 7 9 3 | 30 37 31 36 32 32 36 31 32 36 32
10E | 13 10 15 24 17 5 10 10 9 7 5 | 38 36 36 43 36 38 37 37 37 39 37
11 | 7 10 15 10 11 5 9 3 5 13 3 | 19 29 17 22 24 20 29 19 23 19 21
12E | 7 26 9 8 16 7 9 16 18 15 5 | 46 50 44 47 46 44 49 41 42 46 45
13 | 4 10 8 9 8 4 10 19 13 21 4 | 31 36 28 26 30 31 36 38 33 38 30
14 | 10 7 7 9 9 4 7 28 14 22 4 | 21 24 21 23 23 26 23 39 32 36 23
15 | 9 11 10 7 11 4 6 17 14 19 4 | 53 54 49 52 46 48 51 43 47 52 49
16E | 10 18 8 9 10 3 8 15 12 15 4 | 34 34 33 39 37 33 32 30 31 32 33
17 | 6 12 9 8 8 3 7 13 11 10 3 | 25 28 20 26 22 22 26 25 25 25 23
18 | 6 9 10 8 6 4 7 6 7 14 3 | 23 26 25 26 24 22 26 22 23 30 24
19 | 8 20 8 12 9 5 8 18 15 18 4 | 21 20 19 23 18 21 23 26 29 29 20
20E | 6 14 5 8 8 4 11 11 12 13 3 | 39 44 39 41 39 38 43 39 40 43 39
21 | 13 11 7 6 9 5 9 15 15 19 4 | 18 23 18 20 16 16 21 22 23 25 17
22E | 9 9 8 11 10 6 9 12 11 12 3 | 47 50 50 50 49 47 49 51 49 55 48
23 | 10 23 10 9 12 7 7 35 14 21 5 | 27 24 23 26 23 25 24 36 26 33 22
24 | 6 8 12 9 8 4 6 11 11 9 3 | 19 26 20 24 16 17 26 17 16 28 19
25E | 13 12 7 8 19 10 10 16 13 16 4 | 67 71 73 67 67 69 70 65 66 73 68
26 | 10 20 10 10 20 3 10 11 7 10 4 | 22 25 20 22 24 22 22 20 21 24 22
27 | 8 8 6 10 8 4 7 11 7 13 3 | 22 27 23 21 22 21 24 22 21 21 21
28E | 6 9 6 6 12 4 7 18 9 12 3 | 31 31 35 35 31 35 31 40 37 43 33
29 | 11 17 9 10 10 4 7 18 18 17 4 | 27 25 23 30 24 25 25 26 30 29 24
30 | 7 7 12 5 9 2 8 9 3 11 3 | 23 32 26 26 24 24 33 26 23 32 26
31 | 7 11 11 10 6 4 8 16 11 15 3 | 31 32 28 27 29 27 35 26 28 29 28
32 | 10 9 9 8 6 3 7 12 7 12 3 | 35 40 35 35 34 34 38 31 34 34 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 10 11 5 8 15 11 15 |T 52 42 39 41 51 52 40 40 40 43 52
WRMS | 8 13 10 10 9 4 8 13 11 13 |NE 43 29 24 27 42 43 28 26 26 29 43
MEDI | 8 10 9 9 9 4 8 13 11 14 |MD 27 31 26 29 24 26 30 26 29 32 26
Table 3.2040.1 GPS week: 2040 Day: 1 MJD: 58525.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 8 6 7 6 5 8 7 7 16 2 | 29 32 26 28 25 25 29 27 22 35 27
2 | 8 9 10 8 10 5 8 24 16 24 4 | 29 29 29 29 26 28 28 35 34 40 28
X3E | 8 15 19 22 19 4 --- 12 18 18 6 | 299 261 297 300 295 298 --- 297 291 296 297
X4 | 18 --- --- --- 25 32 --- --- --- --- 21 | 316 --- --- --- 306 318 --- --- --- --- 311
5E | 17 11 10 10 25 5 13 11 10 19 5 | 101 105 100 100 105 100 102 103 102 102 101
6 | 8 8 10 8 8 3 10 14 10 25 3 | 31 38 34 35 32 32 35 34 35 39 33
7 | 9 11 8 4 7 4 10 14 12 19 3 | 26 30 25 29 24 25 29 24 23 31 26
8 | 6 9 7 8 9 5 5 7 5 16 2 | 35 33 31 31 31 29 32 31 30 34 31
9 | 7 8 11 8 10 5 7 9 8 17 3 | 35 43 38 37 39 37 41 37 36 45 38
10E | 14 17 19 18 29 8 20 15 16 16 6 | 48 47 46 55 58 46 48 49 41 49 48
11 | 9 11 15 8 10 8 10 6 10 18 3 | 30 34 26 28 24 23 29 24 21 29 26
12E | 9 20 6 9 16 5 9 14 19 25 4 | 54 58 51 55 53 51 56 50 51 54 53
13 | 7 13 11 8 6 5 12 18 14 20 4 | 25 35 26 25 25 26 35 28 30 30 27
14 | 8 10 9 10 9 4 7 25 12 19 4 | 33 32 27 31 28 32 33 39 35 42 31
15 | 8 10 11 5 10 5 8 19 13 20 4 | 47 43 44 45 45 42 46 37 43 48 44
16E | 9 21 7 10 14 5 9 15 13 19 4 | 49 44 43 48 43 42 44 40 40 44 44
17 | 10 14 10 8 10 5 9 16 11 18 4 | 32 35 28 32 30 29 32 33 30 34 30
18 | 9 9 11 8 9 5 7 8 8 23 3 | 31 32 28 29 24 26 28 27 24 39 28
19 | 11 16 9 12 12 7 9 19 15 23 4 | 30 31 30 36 30 31 32 36 34 40 31
20E | 9 19 7 8 14 4 19 12 12 17 4 | 23 30 21 21 27 20 24 22 23 30 21
21 | 12 11 11 7 9 5 20 14 12 21 4 | 24 27 23 26 23 21 27 27 25 31 23
22E | 10 7 13 19 10 8 7 15 16 20 4 | 21 25 25 22 25 22 24 24 30 31 22
23 | 10 20 8 8 11 7 6 35 16 25 5 | 30 27 27 27 27 29 27 39 29 42 27
24 | 8 10 13 6 9 4 9 8 13 14 3 | 28 31 28 31 28 28 33 28 29 41 29
25 | 10 13 7 11 17 4 9 7 9 19 4 | 51 53 51 54 51 52 54 49 53 56 52
26 | 9 19 11 11 15 4 9 11 8 16 4 | 36 30 30 31 32 31 29 29 28 34 33
27 | 7 7 7 9 8 7 8 7 7 14 3 | 36 33 32 34 32 30 36 33 33 36 34
28E | 6 10 8 9 7 4 6 13 7 22 3 | 41 43 41 38 37 42 39 46 42 49 41
29 | 12 20 9 9 11 4 8 16 16 26 4 | 30 29 28 32 32 27 29 30 29 38 29
30 | 4 8 10 5 10 4 8 7 6 16 2 | 33 40 35 36 32 33 39 33 33 44 35
31 | 7 13 10 7 6 4 6 15 10 17 3 | 29 33 24 29 29 27 31 29 31 38 29
32 | 10 9 10 6 6 3 7 11 7 9 3 | 44 44 41 43 42 42 47 41 40 45 43
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 9 12 5 10 15 12 19 |T 53 45 43 45 51 51 37 44 43 49 52
WRMS | 9 13 10 10 10 5 10 13 12 18 |NE 44 33 30 32 42 42 33 31 30 37 43
MEDI | 9 11 10 8 10 5 8 14 12 19 |MD 32 33 30 32 31 30 32 33 33 40 31
Table 3.2040.2 GPS week: 2040 Day: 2 MJD: 58526.000
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 13 8 8 8 4 7 7 7 16 3 | 22 32 24 22 22 21 26 24 24 31 23
2 | 7 15 11 12 14 5 8 24 15 19 4 | 16 23 21 25 16 18 18 19 24 27 16
X3E | 19 27 14 28 14 8 --- 10 20 16 7 | 173 146 177 173 179 175 --- 174 177 171 174
X4 | 27 --- --- --- 34 33 --- --- --- --- 30 | 514 --- --- --- 505 511 --- --- --- --- 510
5E | 10 15 8 13 18 6 9 14 13 14 4 | 81 85 82 81 78 80 84 84 83 83 82
6 | 7 17 16 15 9 4 8 13 10 15 4 | 22 27 30 27 22 23 26 21 22 29 22
7 | 7 14 7 7 5 5 7 13 11 19 3 | 22 31 20 29 19 22 24 21 27 31 23
8 | 5 15 7 10 8 5 8 9 7 15 3 | 24 33 27 24 25 25 26 25 27 31 25
9 | 9 12 11 7 6 4 9 8 8 16 3 | 22 31 22 24 22 20 28 22 22 30 22
X10E | 15 27 10 19 14 8 --- 12 22 18 6 | 56 51 47 65 56 48 --- 49 52 50 52
11 | 7 13 15 10 13 5 10 6 8 17 4 | 22 35 21 26 25 22 28 24 26 24 23
12E | 9 20 8 13 15 7 8 18 16 23 4 | 39 42 35 40 43 35 39 33 35 40 37
13 | 9 13 11 10 7 4 11 19 13 20 4 | 28 41 32 33 32 31 39 36 40 41 33
14 | 9 17 8 10 6 6 9 26 13 22 4 | 21 25 19 25 21 24 20 31 26 33 20
15 | 9 12 11 8 13 5 8 18 14 22 4 | 39 48 37 36 30 34 37 29 36 38 35
16E | 8 23 8 15 9 6 8 16 13 19 4 | 30 32 28 31 31 27 27 25 27 33 28
17 | 7 10 13 9 9 3 10 13 12 15 3 | 23 28 20 26 21 20 25 22 23 24 21
18 | 7 19 11 9 7 4 8 7 9 17 3 | 19 31 21 19 20 19 22 19 23 30 20
19 | 8 20 10 9 18 5 10 16 15 18 4 | 21 21 20 25 29 20 23 22 25 29 21
X20E | 12 --- 7 18 12 5 10 12 10 16 4 | 33 --- 32 34 32 30 31 31 34 38 31
21 | 13 20 10 11 10 5 10 18 14 21 4 | 26 30 21 23 21 19 25 22 21 28 21
22E | 8 22 9 25 8 6 6 12 12 15 4 | 38 45 41 40 36 38 38 39 42 42 38
23 | 7 26 9 8 10 7 8 32 14 25 5 | 24 25 20 24 19 23 23 32 26 35 20
24 | 8 10 12 7 8 5 8 11 8 14 3 | 23 33 26 27 20 23 32 20 23 36 24
25 | 5 14 7 11 13 3 10 8 6 16 3 | 29 32 29 30 32 27 31 26 27 38 28
26 | 12 16 10 10 13 5 8 11 7 19 4 | 24 28 25 25 29 21 25 23 24 32 23
27 | 6 15 9 20 7 5 8 10 9 18 4 | 23 31 25 29 23 22 25 24 24 27 23
28E | 9 17 9 10 8 5 8 17 12 18 4 | 32 39 33 27 29 32 32 38 35 38 31
29 | 9 23 10 13 11 7 9 16 17 22 4 | 28 33 24 30 29 25 27 28 28 40 26
30 | 7 11 10 6 9 3 6 8 8 24 3 | 19 30 19 25 20 19 27 20 22 34 21
31 | 8 13 10 9 6 3 9 15 12 19 3 | 30 37 29 28 28 28 35 23 31 33 29
32 | 9 22 10 9 6 4 9 12 4 13 3 | 21 38 23 22 21 20 26 17 22 20 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 17 10 12 10 5 8 15 11 18 |T 48 38 33 35 47 46 29 33 34 39 47
WRMS | 8 16 10 11 9 5 8 14 11 18 |NE 44 31 23 26 44 43 26 23 25 31 44
MEDI | 8 15 10 10 9 5 8 13 12 18 |MD 24 32 25 27 25 23 27 24 26 33 23
Table 3.2040.3 GPS week: 2040 Day: 3 MJD: 58527.000
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 8 7 9 4 8 8 9 15 3 | 23 28 23 21 22 20 26 24 18 32 22
2 | 5 10 13 10 15 6 8 22 17 22 4 | 20 24 24 29 20 23 23 24 26 32 21
3E | 11 9 15 38 40 6 10 11 18 15 7 | 173 161 172 177 176 171 95 173 170 173 172
X4 | 7 --- --- --- 18 30 --- --- --- --- 12 | 252 --- --- --- 256 262 --- --- --- --- 255
5E | 8 11 10 13 42 8 9 18 13 19 6 | 50 54 55 52 57 52 52 55 52 57 52
6 | 7 9 12 10 8 3 7 11 12 17 3 | 22 28 25 22 25 22 27 23 25 31 23
7 | 4 13 9 9 11 4 9 14 13 18 3 | 25 30 26 30 22 25 31 25 26 28 26
8 | 7 8 6 8 7 4 9 8 10 14 3 | 22 27 24 23 25 21 26 24 21 27 22
9 | 7 8 9 7 13 2 8 8 9 16 3 | 20 30 22 22 25 20 28 23 25 28 23
10E | 11 12 13 38 13 6 15 9 12 13 6 | 41 41 45 69 49 45 46 42 46 43 44
11 | 8 11 12 8 14 4 10 5 12 15 3 | 21 31 20 24 22 21 28 21 23 21 21
12E | 10 24 7 13 17 6 11 14 18 22 5 | 47 50 43 47 47 46 48 44 48 50 45
13 | 6 13 12 10 10 5 12 18 13 19 4 | 23 33 19 22 31 24 30 29 27 29 24
14 | 8 7 7 10 7 5 9 25 16 19 4 | 25 24 22 22 26 25 21 35 29 32 22
15 | 7 11 12 8 12 4 8 18 11 17 4 | 34 41 37 39 31 33 42 28 34 36 35
16E | 7 19 8 18 11 6 9 16 13 18 4 | 29 28 28 33 33 27 27 27 26 29 27
17 | 13 9 8 16 11 5 8 14 13 18 4 | 27 26 19 26 20 21 25 25 25 27 22
18 | 7 10 9 7 7 4 9 5 7 15 3 | 20 24 21 23 19 20 23 20 21 28 20
19 | 8 19 8 10 11 6 7 15 16 21 4 | 20 21 20 23 21 21 23 24 24 29 20
20E | 9 10 5 10 10 4 8 12 12 12 3 | 27 34 27 29 29 27 26 30 35 33 27
21 | 10 9 7 9 13 4 7 16 12 18 4 | 18 22 17 24 21 18 22 23 21 23 18
22E | 6 11 9 11 20 6 8 12 15 13 4 | 22 24 25 24 27 22 25 24 26 28 23
23 | 6 24 8 9 15 7 9 31 18 26 5 | 25 23 23 22 30 25 24 35 31 34 23
24 | 7 9 13 8 11 4 9 10 8 14 3 | 19 30 24 25 19 21 29 18 19 26 21
25 | 10 12 8 15 10 5 10 9 9 15 3 | 27 30 27 30 31 27 27 24 27 32 26
26 | 6 14 10 17 13 2 9 10 11 11 4 | 24 27 27 27 33 22 27 26 29 28 24
27 | 5 10 5 8 8 4 9 8 9 14 3 | 19 26 23 21 22 20 24 24 20 25 21
28E | 8 12 6 9 13 5 10 11 11 16 3 | 32 37 34 37 38 35 31 40 35 46 34
29 | 11 20 8 8 14 8 9 19 14 19 4 | 23 23 17 21 23 17 22 21 17 26 19
30 | 7 9 11 6 11 3 7 8 8 17 3 | 18 31 23 23 20 21 28 21 18 26 21
31 | 6 11 9 8 7 4 8 16 10 17 3 | 29 32 27 29 26 26 35 19 28 25 27
32 | 9 8 9 10 8 3 8 12 11 11 3 | 22 28 22 23 19 21 26 23 19 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 14 15 5 9 14 13 17 |T 37 34 31 33 39 37 31 32 31 35 37
WRMS | 8 13 10 15 11 5 9 13 12 17 |NE 32 27 22 24 33 32 26 24 23 27 32
MEDI | 7 11 9 10 11 4 9 12 12 17 |MD 23 28 24 24 25 22 27 24 26 29 23
Table 3.2040.4 GPS week: 2040 Day: 4 MJD: 58528.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 7 11 8 8 5 7 7 7 13 3 | 21 27 21 21 20 20 26 22 20 30 22
2 | 5 9 9 9 15 3 7 21 17 22 4 | 19 25 19 25 19 21 22 25 24 33 20
3E | 9 9 14 30 19 7 7 12 9 12 5 | 133 146 135 131 131 133 74 134 132 135 132
X4 | 22 --- --- --- 34 35 --- --- --- --- 28 | 562 --- --- --- 555 562 --- --- --- --- 559
5E | 12 12 11 14 18 6 7 16 16 23 5 | 67 68 67 63 65 63 69 68 67 66 66
6 | 7 9 9 11 7 3 8 11 9 13 3 | 27 30 25 26 27 25 30 25 25 31 26
7 | 7 8 9 7 6 4 9 13 13 15 3 | 28 28 24 28 23 24 27 24 23 26 25
8 | 7 9 9 9 7 5 7 10 6 13 3 | 25 27 26 23 25 24 28 22 24 25 24
9 | 7 7 12 11 7 4 7 9 10 11 3 | 29 34 31 32 30 28 33 29 30 31 30
10E | 7 8 14 34 12 4 8 11 12 12 5 | 35 34 34 44 37 36 34 34 34 35 34
11 | 9 10 16 10 14 6 9 7 9 13 4 | 19 30 19 25 20 21 29 20 22 20 21
12E | 8 19 10 13 13 6 10 16 15 18 4 | 46 47 42 47 42 43 45 41 41 44 43
13 | 6 14 10 12 7 4 11 19 12 19 4 | 28 38 25 22 28 26 35 30 30 31 28
14 | 8 7 8 11 9 5 8 26 17 22 4 | 19 22 17 24 21 22 22 31 25 27 19
15 | 9 11 11 10 10 5 6 20 13 19 4 | 43 44 42 45 40 40 42 35 37 41 40
16E | 8 18 8 15 13 6 7 20 16 17 4 | 32 31 29 34 34 29 29 28 27 28 29
17 | 9 12 9 12 8 3 8 15 13 15 3 | 28 26 23 31 26 25 29 27 26 27 26
18 | 6 9 13 11 10 4 8 6 8 13 3 | 22 25 24 27 21 22 25 22 23 29 23
19 | 7 17 9 12 11 4 8 17 14 17 4 | 24 22 23 28 21 24 25 24 25 26 22
20E | 8 10 6 9 13 4 7 16 14 14 3 | 20 23 20 20 26 19 19 21 23 25 20
21 | 15 9 7 12 11 5 7 20 14 19 4 | 23 22 19 24 18 17 20 22 19 20 18
22E | 8 8 8 9 15 5 6 12 13 11 3 | 25 25 26 31 23 25 25 24 27 29 24
23 | 8 22 9 11 10 6 7 32 16 26 5 | 22 21 18 19 21 22 21 33 25 33 18
24 | 7 10 10 9 10 3 8 11 11 16 3 | 23 34 25 31 21 24 30 23 20 34 25
25 | 8 11 8 11 9 5 8 10 9 17 3 | 33 36 33 32 33 31 34 29 29 37 32
X26 | 1 --- --- --- --- 23 --- --- --- --- 0 | 44 --- --- --- --- 13 --- --- --- --- 47
27 | 7 8 8 8 9 4 8 9 7 12 3 | 23 26 23 23 24 22 26 21 21 18 22
28E | 7 9 5 10 12 5 7 13 10 11 3 | 34 33 33 32 29 35 33 37 34 38 33
29 | 9 15 7 8 11 5 6 19 14 17 4 | 28 26 21 26 25 23 23 23 23 23 23
30 | 9 7 12 7 7 3 9 10 6 17 3 | 25 33 25 26 24 25 32 24 23 31 26
31 | 7 11 9 6 7 3 6 17 12 17 3 | 30 29 26 27 30 27 31 20 29 31 27
32 | 5 7 10 7 8 3 7 11 8 11 2 | 31 37 34 33 32 32 37 30 29 27 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 10 13 11 5 8 16 12 16 |T 49 34 30 33 48 46 31 31 31 34 48
WRMS | 8 12 10 12 10 4 8 14 12 16 |NE 49 28 24 26 48 47 28 25 24 28 48
MEDI | 7 9 9 10 10 5 7 13 12 15 |MD 28 29 25 27 26 25 29 25 25 30 26
Table 3.2040.5 GPS week: 2040 Day: 5 MJD: 58529.000
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 9 8 12 5 7 7 9 10 3 | 20 28 21 22 19 20 26 22 22 28 21
2 | 8 12 8 10 13 5 5 24 16 18 4 | 18 25 20 21 18 18 22 22 21 29 18
3E | 9 9 15 33 20 6 8 11 13 13 5 | 158 208 157 154 156 155 61 155 159 158 156
X4 | 16 --- --- --- 23 54 --- --- --- --- 20 | 557 --- --- --- 548 563 --- --- --- --- 553
5E | 14 10 7 8 12 5 9 15 13 13 4 | 85 86 83 84 85 83 87 83 85 84 84
6 | 8 8 6 12 6 3 6 12 9 13 3 | 22 29 22 23 21 20 27 22 22 33 23
7 | 5 9 8 7 5 4 8 13 12 15 3 | 18 23 17 21 17 18 24 20 22 24 19
8 | 8 9 7 10 7 4 8 9 12 11 3 | 28 30 29 27 27 27 28 27 28 25 26
9 | 6 8 10 9 8 4 9 6 9 16 3 | 39 42 37 39 41 39 44 39 38 42 39
10E | 10 9 13 36 10 5 10 13 11 14 5 | 31 32 29 38 31 32 30 31 34 33 30
11 | 7 9 16 9 14 5 12 5 11 12 4 | 19 29 17 22 20 20 29 19 25 19 20
12 | 13 25 8 7 21 8 11 16 17 16 5 | 64 73 65 64 66 65 71 62 62 64 65
13 | 6 12 9 12 7 6 12 20 15 16 4 | 24 36 24 24 29 27 35 31 30 32 27
14 | 10 7 8 14 6 5 7 25 18 21 4 | 14 21 15 19 19 19 19 28 28 29 17
15 | 10 10 10 9 9 5 8 18 12 15 4 | 34 36 29 32 31 32 38 27 35 34 32
16E | 9 16 8 17 8 5 8 17 13 15 4 | 31 31 28 32 28 27 26 27 27 26 27
17 | 6 11 9 9 9 3 8 14 16 14 3 | 23 26 19 25 21 19 26 22 22 22 21
18 | 5 11 12 10 11 6 10 4 12 9 3 | 20 24 23 24 18 20 21 19 23 26 20
19 | 8 24 8 10 12 5 7 17 18 19 4 | 20 24 22 24 18 20 22 24 24 27 20
20E | 11 11 6 12 11 5 11 18 15 20 4 | 50 50 48 47 47 48 50 48 46 50 47
21 | 12 9 7 10 11 5 9 17 15 19 4 | 20 24 18 22 16 17 22 19 19 23 17
22E | 7 11 7 14 13 6 8 13 15 12 4 | 42 45 46 44 42 45 46 47 46 46 43
23 | 8 22 7 10 11 5 8 32 20 24 5 | 19 22 15 17 18 17 19 28 25 26 14
24 | 10 8 9 8 9 5 9 9 9 14 3 | 20 27 21 24 15 18 28 16 19 31 21
25 | 9 12 6 9 8 3 8 10 9 12 3 | 29 34 30 31 32 30 32 27 32 30 30
X26 | 10 22 9 14 --- 6 --- 9 --- --- 6 | 17 25 18 17 --- 16 --- 16 --- --- 17
27 | 8 9 7 10 7 4 9 8 10 13 3 | 26 28 25 26 25 24 27 25 23 25 24
28E | 7 11 4 10 12 5 7 11 10 11 3 | 31 32 29 29 27 31 28 34 33 34 29
29 | 7 20 7 7 10 4 8 18 13 15 4 | 25 25 22 23 22 22 24 23 24 24 22
30 | 6 7 11 8 9 3 8 8 7 15 3 | 19 30 21 25 18 20 28 19 19 29 22
31 | 5 11 9 10 6 4 8 18 13 16 3 | 21 27 20 23 20 20 26 17 19 23 20
32 | 8 8 9 11 6 4 7 13 11 10 3 | 30 36 33 33 30 31 33 26 33 31 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 9 13 11 5 8 15 13 15 |T 49 38 32 34 49 48 33 33 34 36 48
WRMS | 8 12 9 12 10 5 9 13 13 15 |NE 45 28 22 24 45 45 27 23 24 27 45
MEDI | 8 10 8 10 10 5 8 13 12 14 |MD 24 29 23 25 25 22 28 26 25 29 23
Table 3.2040.6 GPS week: 2040 Day: 6 MJD: 58530.000
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 7 8 7 10 4 8 7 8 22 3 | 19 25 21 23 20 20 25 20 21 37 21
2 | 7 11 10 12 11 5 7 24 16 24 4 | 16 20 19 23 19 18 22 23 25 28 17
X3 | 11 --- 15 34 17 6 8 14 11 22 6 | 202 --- 206 208 208 207 95 206 204 208 205
X4 | 23 --- --- --- 23 38 --- --- --- --- 23 | 625 --- --- --- 624 624 --- --- --- --- 625
5 | 7 14 8 9 10 5 10 14 11 19 3 | 123 128 124 123 124 123 127 127 127 130 125
6 | 10 11 10 10 5 3 10 11 10 22 3 | 22 27 27 27 24 23 28 22 21 41 23
7 | 6 11 8 8 6 3 9 15 12 25 3 | 26 31 26 30 23 25 31 24 25 35 26
8 | 9 10 8 9 7 4 7 11 5 24 3 | 27 28 28 26 26 26 28 25 25 38 26
9 | 9 9 10 8 9 4 8 6 11 21 3 | 42 46 38 41 44 40 47 41 39 51 41
10 | 14 11 15 46 13 6 9 15 10 21 7 | 36 36 33 53 36 36 34 35 40 49 35
11 | 9 9 16 10 14 7 10 6 7 22 4 | 22 30 21 28 24 25 32 22 26 34 24
12 | 10 22 7 10 24 6 12 14 14 26 5 | 54 63 55 57 56 55 61 53 55 57 55
13 | 9 11 10 9 7 3 12 15 11 29 4 | 32 40 31 31 34 33 37 37 38 44 33
14 | 12 9 9 15 10 6 9 26 16 28 5 | 19 24 17 25 24 24 22 35 25 43 20
15 | 16 13 9 9 9 5 10 17 12 26 4 | 52 52 48 50 46 47 52 45 49 53 48
16 | 18 18 9 16 14 6 10 16 15 25 5 | 40 37 34 37 35 34 35 33 32 44 34
17 | 9 10 9 10 7 3 9 15 12 22 3 | 22 25 18 27 20 20 27 26 22 34 21
18 | 7 10 11 9 7 4 8 5 8 20 3 | 25 26 26 28 26 25 28 25 29 36 25
19 | 7 23 7 11 9 4 9 16 15 24 4 | 18 22 20 26 18 22 26 28 26 40 21
20 | 16 10 7 16 12 6 9 18 12 26 4 | 62 57 59 61 63 58 58 56 59 69 59
21 | 15 11 7 11 9 4 9 19 12 29 4 | 19 23 18 21 19 19 23 26 24 39 19
22 | 12 9 6 13 12 5 9 14 13 21 4 | 57 57 59 56 58 58 57 59 66 68 58
23 | 12 24 8 8 12 6 8 32 18 29 6 | 27 24 22 25 26 23 24 33 29 43 22
24 | 8 7 9 9 7 4 8 9 10 22 3 | 19 28 21 26 17 18 28 17 17 39 20
25 | 7 12 4 12 8 3 9 11 10 24 3 | 33 37 33 33 32 33 35 31 32 42 32
26 | 17 13 9 12 13 2 11 10 11 21 4 | 19 19 18 17 16 16 19 16 15 19 17
27 | 12 10 10 10 8 5 8 12 8 24 3 | 25 27 26 25 22 23 26 23 24 33 23
28 | 14 10 7 9 13 9 8 16 10 23 4 | 46 44 46 48 44 47 48 49 46 66 46
29 | 15 15 6 8 11 5 8 18 16 27 4 | 29 28 26 28 25 26 26 26 24 40 25
30 | 7 8 11 7 7 3 7 10 7 20 3 | 18 30 22 23 22 20 29 23 20 36 22
31 | 9 10 11 11 9 6 10 17 20 23 4 | 33 35 32 32 28 28 35 22 28 40 29
32 | 14 8 9 11 10 4 9 12 10 23 4 | 35 39 37 37 34 35 38 30 34 35 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 9 13 11 5 9 16 12 24 |T 57 36 39 41 57 57 38 39 40 50 57
WRMS | 11 13 9 12 10 5 9 14 12 23 |NE 51 29 25 28 51 51 29 26 26 38 51
MEDI | 10 10 9 10 10 5 9 14 11 23 |MD 27 30 27 28 26 26 31 28 28 40 26
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2040 GPS week: 2040 MJD: 58524.0-58530.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 |U 9 11 22 |U 10 13 45 |U 11 14 23 |
emr | emr 2934 |U 17 16 46 |U 14 20 61 |U 13 22 38 |
esa | esa 2962 | 9 11 25 |U 9 13 47 | 11 14 29 |
gfz | gfz 2962 |U 9 10 22 |U 12 13 54 |U 12 14 32 |
grg | grg 3044 |U 10 11 29 |U 12 17 58 | 10 14 26 |
igr | igr 2953 | 9 9 22 | 10 12 47 | 10 13 27 |
igs | igs 1737 | 9 9 27 | 10 14 51 | 10 14 26 |
jpl | jpl 2907 |U 13 13 41 |U 11 16 58 |U 12 18 34 |
mit | mit 2962 |U 19 20 32 |U 20 26 74 |U 15 14 34 |
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 5.2040.0 GPS week: 2040 Day: 0 MJD: 58524.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 11 26 | 6 11 46 | 11 15 20 |
emr | emr 2976 | 15 14 46 | 11 16 45 | 13 22 49 |
esa | esa 2976 | 11 14 28 | 7 13 48 | 12 19 42 |
gfz | gfz 2976 | 11 14 23 | 8 9 53 | 14 18 43 |
grg | grg 3072 | 12 14 24 | 7 15 48 | 11 18 29 |
igr | igr 2976 | 11 11 26 | 7 11 45 | 12 19 43 |
igs | igs 3071 | 11 12 26 | 6 11 43 | 12 19 40 |
jpl | jpl 2976 | 15 14 37 | 8 11 46 | 15 20 45 |
mit | mit 2976 | 14 16 40 | 20 31 85 | 16 25 47 |
Table 5.2040.1 GPS week: 2040 Day: 1 MJD: 58525.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 11 22 | 9 10 46 | 11 13 27 |
emr | emr 2976 | 17 16 50 | 10 19 55 | 14 20 36 |
esa | esa 2976 | 8 12 27 | 7 9 50 | 11 11 27 |
gfz | gfz 2976 | 9 11 22 | 9 8 52 | 11 11 29 |
grg | grg 3072 | 7 9 25 | 10 10 56 | 9 13 27 |
igr | igr 2976 | 8 10 23 | 8 9 48 | 10 9 24 |
igs | igs 0 | 8 9 28 | 8 8 49 | 10 10 24 |
jpl | jpl 2880 | 13 15 45 | 10 10 51 | 10 15 31 |
mit | mit 2976 | 62 72 71 | 33 40 94 | 30 26 48 |
Table 5.2040.2 GPS week: 2040 Day: 2 MJD: 58526.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 9 13 22 | 9 13 38 | 13 20 33 |
emr | emr 2880 | 23 16 44 | 16 28 70 | 19 32 29 |
esa | esa 2976 | 8 11 24 | 10 18 46 | 12 18 31 |
gfz | gfz 2976 | 9 11 21 | 10 11 40 | 13 17 34 |
grg | grg 3072 | 10 19 33 | 12 22 54 | 12 17 30 |
igr | igr 2970 | 8 10 23 | 9 12 39 | 12 16 29 |
igs | igs 0 | 8 10 24 | 10 18 47 | 12 19 29 |
jpl | jpl 2784 | 13 10 36 | 11 21 56 | 11 21 36 |
mit | mit 2976 | 8 11 26 | 15 32 64 | 12 8 27 |
Table 5.2040.3 GPS week: 2040 Day: 3 MJD: 58527.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 8 11 15 | 11 15 55 | 9 12 17 |
emr | emr 2975 | 16 19 46 | 18 27 90 | 14 28 36 |
esa | esa 2976 | 8 11 20 | 10 11 42 | 9 10 20 |
gfz | gfz 2975 | 8 11 17 | 15 17 82 | 11 13 23 |
grg | grg 3071 | 8 9 23 | 14 17 80 | 9 9 18 |
igr | igr 2955 | 10 11 15 | 13 14 60 | 10 13 22 |
igs | igs 0 | 8 10 19 | 15 17 79 | 9 12 20 |
jpl | jpl 2976 | 12 15 34 | 17 18 79 | 11 18 28 |
mit | mit 2976 | 9 12 17 | 17 20 86 | 10 8 21 |
Table 5.2040.4 GPS week: 2040 Day: 4 MJD: 58528.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 10 10 25 | 18 14 54 | 12 11 21 |
emr | emr 2880 | 17 14 43 | 14 17 56 | 13 17 32 |
esa | esa 2880 | 9 11 25 | 10 17 57 | 12 12 23 |
gfz | gfz 2880 | 9 10 24 | 24 16 70 | 13 14 30 |
grg | grg 2976 | 10 8 29 | 19 25 67 | 10 12 16 |
igr | igr 2880 | 9 9 22 | 13 15 53 | 11 11 23 |
igs | igs 2962 | 10 14 37 | 15 17 57 | 11 13 19 |
jpl | jpl 2880 | 12 12 42 | 13 16 64 | 12 20 26 |
mit | mit 2880 | 10 9 22 | 25 29 82 | 12 5 20 |
Table 5.2040.5 GPS week: 2040 Day: 5 MJD: 58529.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 10 21 | 9 11 31 | 9 12 20 |
emr | emr 2976 | 16 19 53 | 12 14 58 | 12 19 41 |
esa | esa 2976 | 9 8 28 | 9 11 38 | 10 11 26 |
gfz | gfz 2976 | 8 8 26 | 9 12 37 | 11 11 34 |
grg | grg 2976 | 8 10 39 | 11 15 49 | 11 13 27 |
igr | igr 2938 | 9 6 21 | 9 11 36 | 9 11 23 |
igs | igs 3056 | 9 7 28 | 9 11 37 | 9 12 26 |
jpl | jpl 2880 | 15 13 47 | 10 14 47 | 13 18 37 |
mit | mit 2976 | 14 13 23 | 11 10 44 | 17 13 39 |
Table 5.2040.6 GPS week: 2040 Day: 6 MJD: 58530.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 8 20 | 10 15 43 | 10 12 23 |
emr | emr 2880 | 17 11 42 | 15 21 57 | 10 17 43 |
esa | esa 2976 | 10 7 26 | 10 14 45 | 10 15 33 |
gfz | gfz 2976 | 10 7 23 | 12 15 44 | 10 10 34 |
grg | grg 3072 | 13 7 29 | 11 19 54 | 11 15 32 |
igr | igr 2976 | 10 5 24 | 10 15 47 | 9 11 25 |
igs | igs 3071 | 10 5 27 | 10 16 48 | 9 13 28 |
jpl | jpl 2976 | 13 12 43 | 11 19 61 | 10 16 33 |
mit | mit 2976 | 14 11 26 | 20 23 62 | 12 14 39 |
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 6.2040 GPS week: 2040 MJD: 58524.500-58530.500
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 -19 41 62 3 | 8 18
| 11 13 32 64 6 | 5
emr uuxxx | 43 -3 -63 18 24 | 46 52
| 42 70 244 217 21 | 13
esa uuuuu | 0 0 32 26 2 | 20 25
| 8 10 78 51 4 | 5
gfz uuuuu | 2 11 -86 97 -1 | 29 33
| 21 16 141 91 3 | 3
grg uuuuu | -8 0 -43 27 -3 | -3 15
| 25 24 29 56 2 | 3
igr xxxxx | -4 -5 27 14 2 | 4 15
| 12 14 75 79 2 | 5
irf xxxxx | 1 -7 -24 -23 -4 | 2 15
| 9 14 22 37 4 | 3
jpl uuuuu | 4 -9 30 -55 12 | 23 28
| 17 23 58 73 13 | 6
mit uuuuu | 21 7 -46 -58 -3 | 17 22
| 26 29 83 56 4 | 3
ngs uuuuu | -7 -3 36 24 -2 | 13 20
| 74 70 125 183 3 | 4
sio uuuux | -9 40 -50 -254 10 | 54 57
| 41 28 56 116 6 | 7
Table 7.2040.0 GPS week: 2040 Day: 0 MJD: 58524.500
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 | -16 -23 69 80 10 | -1 18
emr uuxxx | -4 20 -168 -79 36 | 28 33
esa uuuuu | -2 0 16 67 4 | 12 23
gfz uuuuu | 9 9 -73 26 1 | 23 30
grg uuuuu | 18 39 -40 74 -2 | -7 19
igr xxxxx | -12 -14 -84 -40 3 | -3 17
irf xxxxx | -8 -15 -4 -37 1 | -3 19
jpl uuuuu | -18 -10 69 -124 -5 | 15 22
mit uuuuu | -5 -41 43 -9 -6 | 13 21
ngs uuuuu | 57 7 -9 27 -4 | 7 19
sio uuuux | -50 0 -160 -217 11 | 43 47
Table 7.2040.1 GPS week: 2040 Day: 1 MJD: 58525.500
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 1 29 141 7 | 3 12
emr uuxxx | -17 6 -291 -258 24 | 34 37
esa uuuuu | -12 -5 -81 4 1 | 16 21
gfz uuuuu | 32 -16 127 117 0 | 27 30
grg uuuuu | 17 5 -1 107 -7 | -5 15
igr xxxxx | -11 -11 -25 -121 -2 | 0 12
irf xxxxx | -5 -20 -3 -78 -1 | 0 13
jpl uuuuu | 0 -40 28 -141 -6 | 17 21
mit uuuuu | 6 -16 47 -89 -1 | 15 20
ngs uuuuu | 10 77 -146 -32 0 | 9 16
sio uuuux | -33 9 -76 -397 14 | 48 49
Table 7.2040.2 GPS week: 2040 Day: 2 MJD: 58526.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -38 -26 24 120 5 | 7 17
emr uuxxx | 92 -149 452 445 52 | 39 45
esa uuuuu | -2 4 10 85 1 | 19 25
gfz uuuuu | -18 5 46 100 -6 | 29 33
grg uuuuu | 8 23 -27 22 -4 | -3 16
igr xxxxx | -16 -13 50 27 5 | 3 15
irf xxxxx | 8 0 -15 -13 -10 | 3 16
jpl uuuuu | -7 -20 65 -62 19 | 19 24
mit uuuuu | 4 9 -38 -115 -10 | 17 23
ngs uuuuu | 28 83 -94 -118 -4 | 12 20
sio uuuux | -3 31 -60 -211 15 | 51 54
Table 7.2040.3 GPS week: 2040 Day: 3 MJD: 58527.500
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 | -45 -16 46 -55 5 | 10 20
emr uuxxx | 41 -14 -102 18 31 | 48 57
esa uuuuu | -5 2 -39 25 -3 | 23 28
gfz uuuuu | 3 25 -67 89 1 | 31 35
grg uuuuu | 5 0 -62 43 -4 | -1 16
igr xxxxx | 19 -10 -22 8 2 | 6 17
irf xxxxx | 9 -4 -25 -41 -5 | 5 16
jpl uuuuu | 11 -11 9 77 8 | 25 31
mit uuuuu | 4 5 -17 -123 -1 | 19 25
ngs uuuuu | 62 4 103 166 0 | 15 22
sio uuuux | -59 43 -27 -383 9 | 56 59
Table 7.2040.4 GPS week: 2040 Day: 4 MJD: 58528.500
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 -5 24 34 1 | 14 20
emr uuxxx | 66 4 -32 -12 7 | 56 63
esa uuuuu | 15 17 74 15 -1 | 26 29
gfz uuuuu | -32 9 -273 72 1 | 34 37
grg uuuuu | -41 -17 -65 -17 -3 | 1 15
igr xxxxx | -5 3 40 105 3 | 10 17
irf xxxxx | -12 4 -45 -31 -7 | 7 16
jpl uuuuu | -4 -16 75 -47 20 | 28 33
mit uuuuu | 28 37 -117 -77 -2 | 21 26
ngs uuuuu | 13 -33 149 201 -2 | 18 23
sio uuuux | 1 55 -10 -325 15 | 60 63
Table 7.2040.5 GPS week: 2040 Day: 5 MJD: 58529.500
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 | -16 -38 1 53 -1 | 11 19
emr uuxxx | 33 48 -79 -75 27 | 55 62
esa uuuuu | 5 -15 128 -70 2 | 23 26
gfz uuuuu | 3 33 -221 -5 -2 | 31 33
grg uuuuu | -31 -17 -85 -61 -1 | -3 12
igr xxxxx | -2 25 127 15 2 | 7 15
irf xxxxx | 4 14 -63 0 -3 | 3 13
jpl uuuuu | 37 36 51 -12 24 | 26 31
mit uuuuu | 62 44 -184 -5 -1 | 18 22
ngs uuuuu | -130 -119 190 207 -6 | 15 20
sio uuuux | 53 68 -1 -101 2 | 60 62
Table 7.2040.6 GPS week: 2040 Day: 6 MJD: 58530.500
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 -23 96 65 -8 | 12 19
emr uuxxx | 88 66 -221 91 -11 | 61 66
esa uuuuu | 3 -4 114 55 9 | 23 26
gfz uuuuu | 17 15 -144 280 -3 | 30 33
grg uuuuu | -31 -29 -18 20 -3 | -4 13
igr xxxxx | 0 -11 102 104 2 | 8 14
irf xxxxx | 10 -27 -15 40 -2 | 3 13
jpl uuuuu | 9 2 -90 -78 25 | 29 33
mit uuuuu | 49 11 -59 11 2 | 17 21
ngs uuuuu | -88 -41 62 -281 3 | 15 20
sio uuuux | 28 74 -17 -146 2 | 61 63
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