[IGSREPORT-26372] Wk 2036 IGS Final Orbits
acc
acc at igs.org
Thu Jan 31 21:00:29 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2036 (Jan 13, 2019 - Jan 19, 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:
igs2036[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2036[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2036[0-6].cls IGS GPS clock combination summary report.
igs20367.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20367.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 | GLSV OHI3 REUN SEYG TIXI ABMF FAA1 GLSV GUAM LHAZ
0 | COD | OHI3 TIXI
0 | EMR | GRAZ TLSE FAIR GRAZ TLSE
0 | ESA | 3 19 20 21 22 22 BRST FAA1 FAIR LAUT LHAZ PIMO SEYG
0 | ESA | LHAZ
0 | GFZ | DAV1 GODE NRC1 PIMO POHN BOR1 DAV1 FAA1 GODE NRC1
0 | GFZ | POHN
0 | GRG | 21 21 FAA1 FAIR GLSV REUN FAIR GLSV TLSE
0 | MIT | FAA1 GUAM
1 | COD | ABMF FAIR TIXI GLSV INEG TIXI
1 | EMR | MCM4 CHUR MCM4 OPMT
1 | ESA | 3 19 22 22 FAA1 GUAM LAUT FAIR
1 | GFZ | GODE POHN USN7 ABMF FAA1 FAIR GODE PIMO POHN USN7
1 | GFZ | YAR2
1 | GRG | GLSV MCM4 GLSV MCM4 REUN
1 | JPL | LAUT
2 | COD | GLSV OHI3 TIXI FAIR GLSV GUAM MCM4 OHI3 TIXI
2 | EMR | MCM4
2 | ESA | 3 22 22 PIMO PIMO TOW2
2 | GFZ | BOR1 GODE PIMO POHN RBAY BOR1 GODE PIMO POHN RBAY
2 | GRG | FAIR GLSV NRMD PIMO FAIR GLSV NRMD PIMO
2 | JPL | LMMF LAUT LMMF MCM4
3 | COD | RBAY TIXI FAA1 TIXI
3 | EMR | GRAZ YELL
3 | ESA | LMMF LMMF
3 | GFZ | BOR1 GODE GUAT POHN YAR2 BOR1 GODE GUAT POHN RBAY
3 | GFZ | YAR2
3 | GRG | GLSV LHAZ NRMD SCOR GLSV LHAZ NRMD SCOR
3 | JPL | LAUT
3 | MIT | PALM PALM
4 | ALL | 4 4
4 | COD | GLSV NAUR RAMO TIXI GLSV NAUR TIXI
4 | ESA | 22 SOFI FAA1
4 | GFZ | BOR1 GODE POHN REUN BOR1 GODE POHN REUN
4 | GRG | ABMF ALRT FAA1 GLSV ABMF ALRT FAA1 GLSV NRMD
4 | JPL | LAUT NRMD RAMO
5 | COD | FAA1 GLSV NAUR RBAY TIXI FAA1 GLSV NAUR RBAY TIXI
5 | EMR | 14 26 31 GRAZ ALBH AREQ BADG BOR1 CEDU CRO1 DAEJ
5 | EMR | FAIR GODE GOL2 GRAZ HARB HERS IENG JPLM KERG KIRU
5 | EMR | KOKB LPGS MAR6 MATE MCM4 MDO1 NIST NNOR NRC1 ONSA
5 | EMR | OPMT PIE1 PRDS PTBB SCH2 STJO SUWN THU3 TLSE TWTF
5 | EMR | USN7 VILL WILL WSRT
5 | ESA | 19 20 21 22 21 22 LAUT
5 | GFZ | 25 26 FAA1 GODE POHN YAR2 FAA1 GODE POHN
5 | GRG | GLSV LHAZ GLSV LHAZ
5 | JPL | LAUT
5 | MIT | PALM
6 | COD | FAA1 FAA1 POHN
6 | EMR | 26 26 YAR2 HOB2 PERT YAR2
6 | ESA | 22 22 LAUT MDVJ MDVJ
6 | GFZ | GODE POHN RBAY REUN GODE POHN RBAY REUN
6 | GRG | ADIS GLSV LPGS NRMD ADIS GLSV LPGS NRMD REUN
6 | JPL | CUSV LAUT
6 | MIT | PALM FAA1 PALM
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | GRG | 4
1 | GRG | 4
3 | GRG | 4
4 | GRG | 4
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G04 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .5 .2 1.1 6 20 -4 -.35
EMR | 0 | .1 -5.6 16.8 -13 57 -17 .09
ESA | 0 | -1.0 .8 .9 20 0 21 -.47
GFZ | 0 | .7 -.2 .7 2 -25 16 -.23
GRG | 0 | 11.3 -5.9 8.9 56 -4 54 .13
JPL | 0 | 6.2 -3.0 11.9 -12 6 -7 -.39
MIT | 0 | -1.8 .2 9.0 -36 37 3 .01
NGS | 0 | -2.5 -4.7 9.4 -10 -23 6 -.11
SIO | 0 | .4 -1.0 18.1 -21 25 -16 -.19
COD | 1 | .3 .2 .9 8 18 -8 -.40
EMR | 1 | -3.7 -2.8 13.0 -10 49 0 .11
ESA | 1 | -1.0 .1 .7 4 8 34 -.47
GFZ | 1 | .5 -.3 .5 -11 -27 15 -.25
GRG | 1 | 6.0 -1.2 9.0 35 -6 55 .09
JPL | 1 | 9.3 .7 10.1 0 0 2 -.13
MIT | 1 | -2.3 1.0 10.9 -50 68 28 -.22
NGS | 1 | -.2 -1.8 13.6 -17 -49 31 -.27
SIO | 1 | -3.7 -2.0 10.2 -30 12 -3 .02
COD | 2 | .3 .3 1.1 7 26 -10 -.43
EMR | 2 | -2.0 -6.7 18.8 30 55 -24 -.20
ESA | 2 | -.3 1.6 1.3 26 -13 32 -.57
GFZ | 2 | 1.0 -.3 .5 -10 -36 22 -.25
GRG | 2 | 9.4 -.7 13.3 56 -5 35 -.02
JPL | 2 | 13.5 .0 12.7 -8 2 1 -.16
MIT | 2 | -1.7 1.6 9.5 -30 43 -7 -.15
NGS | 2 | -2.9 3.2 14.7 29 -43 50 -.12
SIO | 2 | -.6 -1.6 6.4 -14 33 -32 -.06
COD | 3 | .7 -.2 1.2 9 8 7 -.48
EMR | 3 | .8 -4.5 11.1 -20 14 55 -.03
ESA | 3 | .8 1.7 .1 36 -26 33 -.39
GFZ | 3 | .7 .4 .1 -5 -34 4 -.04
GRG | 3 | 6.6 -2.8 16.3 61 -6 46 -.09
JPL | 3 | 9.2 -.9 6.7 -8 9 -10 -.46
MIT | 3 | 2.1 -1.8 7.2 -45 49 5 -.09
NGS | 3 | -1.1 -1.5 4.0 -5 -31 36 .01
SIO | 3 | 1.5 -4.8 4.9 -20 10 -20 .0
COD | 4 | .6 .0 .6 6 18 3 -.38
EMR | 4 | 3.0 -6.0 14.6 2 37 -26 -.07
ESA | 4 | -.3 1.4 -.1 19 -14 53 -.50
GFZ | 4 | .5 .2 .2 1 -31 6 -.13
GRG | 4 | 3.5 -2.7 15.3 58 7 43 -.22
JPL | 4 | 9.2 -4.1 10.7 5 -12 -24 -.04
MIT | 4 | 1.4 -4.5 9.1 -25 49 10 -.15
NGS | 4 | .1 -3.0 12.1 -23 -41 27 -.05
SIO | 4 | .4 -5.5 3.3 -10 -6 -31 .12
COD | 5 | -.2 .7 1.0 4 20 2 -.25
EMR | 5 | -3.8 4.2 15.8 -39 33 37 -.05
ESA | 5 | 2.1 .5 1.8 29 -29 28 -.38
GFZ | 5 | .6 .3 -.1 -1 -40 5 -.09
GRG | 5 | 5.4 -4.1 20.7 50 -10 49 -.23
JPL | 5 | 6.5 -3.7 2.0 2 -9 1 -.34
MIT | 5 | -3.3 -1.8 10.0 -22 24 -14 -.01
NGS | 5 | -8.1 -3.3 12.0 -48 41 17 .01
SIO | 5 | -1.6 -2.1 6.6 -8 15 -5 -.06
COD | 6 | .6 .5 .9 0 7 -6 -.34
EMR | 6 | 2.4 9.7 11.5 -63 38 11 -.18
ESA | 6 | 1.0 .4 1.0 29 -8 30 -.41
GFZ | 6 | .3 .1 .5 7 -14 12 -.12
GRG | 6 | 6.5 -4.0 10.4 68 15 61 -.17
JPL | 6 | 4.3 -3.7 1.0 8 -3 2 -.49
MIT | 6 | -1.4 -4.0 6.9 -25 49 7 -.10
NGS | 6 | -1.3 -2.1 10.4 -23 -19 10 -.10
SIO | 6 | 2.2 -4.3 6.0 -3 20 -16 -.07
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 1.2036.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2036.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 2.2036.[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 3.2036.[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 5.2036.0-6). 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 2036 summary. (Jan 13, 2019 - Jan 19, 2019)
Table 1.2036.a GPS week: 2036 MJD: 58496.000-58502.000
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 253| -1 0 -2 2 4 18 .03 9 9 | -475 -134 8 76
| 0 0 1 17 14 16 .03 | 131 249
emr 80| 0 1 5 -17 4 5 .11 13 12 | 177407 -225 18 115
| 0 4 2 10 3 11 .03 | 1105 729
esa 149| 0 0 0 -7 -22 7 -.04 9 9 | -818 -633 11 204
| 0 0 1 6 16 9 .02 | 562 1280
gfz 170| 0 1 -1 1 5 26 .12 13 13 | -296 30 11 98
| 0 0 2 13 18 15 .06 | 551 825
grg 103| 0 0 -1 -17 0 -19 -.13 10 9 | 0 -16 12 144
| 0 0 3 8 8 28 .02 | 175 335
igr n/a| 0 0 -2 -13 -15 -4 -.03 4 4 | -5168 -116 10 77
| 0 0 0 8 6 8 .01 | 1168 737
jpl 80| 0 0 3 18 13 -8 .18 9 9 | 203071 -136 10 96
| 1 1 1 13 7 13 .01 | 26827 637
mit 347| 0 0 -4 26 -1 -9 -.16 20 15 | -192 -160 77 1605
| 0 0 1 30 23 15 .02 | 240 210
ngs 200| 0 0 2 -14 -5 -12 -.06 10 10 | -464 -112 944 2134
| 0 0 2 9 21 12 .02 | 205 341
sio 315| 0 -1 -4 1 1 3 -.14 14 14 | --- --- --- ---
| 0 0 2 30 19 25 .02 | --- ---
Table 1.2036.b GPS week : 2036 MJD: 58496.000-58502.000
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 3 3 3 3 |
2 | 4 4 4 4 4 4 5 |
3 | 3 3 4 4 3 4 4 |
4 | 0 0 50 0 0 38 55 |
5 | 4 4 4 4 4 4 4 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 4 4 5 |
8 | 3 3 3 3 3 3 4 |
9 | 3 3 3 4 3 3 4 |
10 | 3 3 4 3 4 4 4 |
11 | 4 4 4 4 3 4 4 |
12 | 5 4 5 5 5 5 5 |
13 | 3 3 3 3 3 3 3 |
14 | 3 3 3 4 4 4 4 |
15 | 4 3 4 4 4 4 4 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 4 4 4 5 4 |
19 | 5 5 5 5 5 5 5 |
20 | 4 4 4 5 5 5 5 |
21 | 6 4 4 4 4 5 5 |
22 | 4 4 4 4 4 4 5 |
23 | 4 4 4 4 4 4 5 |
24 | 3 3 3 4 4 4 4 |
25 | 4 4 5 6 7 7 7 |
26 | 4 5 7 6 7 7 9 |
27 | 3 3 3 3 3 3 4 |
28 | 4 4 4 3 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 3 3 3 3 3 3 4 |
31 | 4 4 5 4 4 5 5 |
32 | 4 4 4 4 4 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2036.0 GPS week: 2036 Day: 0 MJD: 58496.000
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 -2 -12 9 5 .00 9 9 | -265 -622 7 82
emr 80| 1 -1 5 -11 8 -7 .14 12 12 | 179519 -809 17 95
esa 150| 0 0 2 -12 -11 -10 -.04 8 8 | -993 252 10 210
gfz 169| 0 1 0 -1 23 11 .17 11 12 | -410 553 10 88
grg 103| 0 0 -6 -19 3 11 -.14 11 10 | -17 230 9 131
igr n/a| 0 0 -2 -13 -9 -10 -.02 4 4 | -2972 -719 9 63
jpl 80| 0 0 4 12 8 -1 .17 10 10 | 215152 -778 9 96
mit 348| 0 0 -2 62 -26 -15 -.17 16 14 | 221 33 72 1666
ngs 209| 0 0 4 -14 -7 -12 -.05 10 10 | -354 -478 1034 2120
sio 316| 0 -2 -6 18 -5 26 -.15 13 13 | --- --- --- ---
Table 2.2036.1 GPS week: 2036 Day: 1 MJD: 58497.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| -1 0 -3 29 -17 -10 .08 8 8 | -652 -177 7 72
emr 80| 0 0 4 -12 3 3 .09 12 12 | 178204 -1089 15 111
esa 150| 0 0 0 -12 -5 11 -.03 8 8 | -1052 323 9 200
gfz 169| 0 0 -3 16 2 16 .14 12 12 | -174 -362 9 86
grg 104| 1 0 -5 -20 -2 12 -.16 10 10 | 61 -148 10 121
igr n/a| 0 0 -2 -3 -21 -11 -.01 4 4 | -4301 -1037 9 164
jpl 80| 0 0 3 35 22 -17 .15 9 9 | 213724 -661 9 98
mit 348| 0 0 -2 -25 20 3 -.16 15 14 | -361 -240 53 1639
ngs 199| 0 0 4 -14 -14 -8 -.07 10 10 | -718 -76 868 2164
sio 305| -1 -1 0 -33 9 12 -.16 13 13 | --- --- --- ---
Table 2.2036.2 GPS week: 2036 Day: 2 MJD: 58498.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 257| -2 0 -3 0 15 16 .07 10 9 | -483 122 6 71
emr 80| 0 -3 6 -2 8 2 .14 12 12 | 177106 83 15 136
esa 150| 0 0 0 -15 -19 0 -.04 9 9 | -1257 -1230 9 222
gfz 170| 0 2 -4 -10 1 46 .14 14 11 | -417 720 9 130
grg 105| 1 0 -1 -27 -10 -20 -.16 10 10 | -206 369 11 163
igr n/a| -1 0 -3 -20 -23 -12 -.03 5 5 | -5438 228 11 62
jpl 80| 2 1 3 31 21 -9 .18 9 9 | 142274 82 9 85
mit 347| 0 0 -3 33 -3 -4 -.17 17 14 | -251 -62 55 1780
ngs 192| -1 0 2 -5 -36 -14 -.09 10 10 | -494 153 1208 2492
sio 313| 0 0 -6 0 19 7 -.15 13 12 | --- --- --- ---
Table 2.2036.3 GPS week: 2036 Day: 3 MJD: 58499.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 256| -1 0 -2 -13 -11 26 .00 9 9 | -599 114 6 76
emr 80| 0 0 1 -21 6 17 .13 12 12 | 177193 -337 15 102
esa 150| 0 0 1 -1 -17 8 -.02 9 9 | -1052 424 8 205
gfz 170| 0 0 -2 -12 8 24 .06 14 15 | 831 -1565 11 125
grg 103| 0 0 1 -6 5 -60 -.11 10 9 | 325 -562 11 160
igr n/a| -1 0 -3 -20 -13 -7 -.03 4 4 | -5337 -336 10 61
jpl 80| 1 0 3 30 16 -25 .19 8 8 | 213069 -431 7 94
mit 348| 0 -1 -3 28 -9 15 -.16 19 15 | -67 -492 86 1570
ngs 204| 0 0 0 -12 9 8 -.04 10 10 | -110 -596 808 1803
sio 317| -1 -1 -5 6 -19 15 -.16 15 14 | --- --- --- ---
Table 2.2036.4 GPS week: 2036 Day: 4 MJD: 58500.000
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| -2 0 -3 22 8 29 .04 9 8 | -372 -176 6 73
emr 80| 1 0 3 -21 0 0 .13 12 12 | 176935 -348 18 122
esa 149| 2 -1 -1 0 -31 13 -.03 9 9 | -1220 297 11 224
gfz 170| 0 1 1 -1 17 33 .04 14 15 | -428 -252 10 90
grg 103| 0 0 0 -6 2 -33 -.11 10 9 | 60 -318 11 154
igr n/a| 0 0 -3 -20 -20 2 -.03 4 4 | -5679 -274 10 62
jpl 80| 0 1 3 14 14 4 .17 8 8 | 212706 -239 10 87
mit 348| 1 0 -6 -2 13 -19 -.19 22 16 | -172 -370 115 1645
ngs 197| 0 0 3 -11 -1 -26 -.07 10 10 | -368 -183 983 2111
sio 319| 0 0 -6 -36 -16 -1 -.16 16 14 | --- --- --- ---
Table 2.2036.5 GPS week: 2036 Day: 5 MJD: 58501.000
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 -2 6 21 28 .03 9 9 | -447 -140 21 77
emr 80| 0 5 7 -35 0 -1 .12 13 13 | 176603 -258 29 129
esa 150| 1 0 0 -1 -54 14 -.07 9 9 | 313 -2783 25 187
gfz 174| 1 0 0 23 -33 7 .08 12 14 | -968 614 24 88
grg 104| 0 0 0 -24 -7 -44 -.12 10 9 | -160 170 27 135
igr n/a| -1 0 -2 0 -9 5 -.04 4 4 | -6183 88 12 71
jpl 80| 0 0 0 7 1 10 .19 8 8 | 212368 -54 23 104
mit 348| 0 0 -4 52 27 -28 -.15 24 16 | -167 -37 80 1429
ngs 199| -1 0 1 -35 30 -7 -.07 11 11 | -582 16 930 2113
sio 315| 0 -1 -6 6 31 15 -.10 15 14 | --- --- --- ---
Table 2.2036.6 GPS week: 2036 Day: 6 MJD: 58502.000
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 -12 5 34 -.00 9 9 | -511 -60 7 83
emr 80| 0 10 6 -20 1 23 .05 14 13 | 176295 1182 18 116
esa 150| 2 -1 0 -6 -14 14 -.06 9 9 | -468 -1717 7 184
gfz 170| 0 1 0 -5 18 44 .20 11 12 | -511 505 10 83
grg 103| 0 0 -2 -19 13 0 -.14 10 9 | -62 146 11 144
igr n/a| 0 0 -1 -14 -8 5 -.03 4 4 | -6272 1233 10 60
jpl 80| -1 -3 3 0 12 -18 .17 10 10 | 212208 1128 8 109
mit 348| 0 1 -4 32 -32 -18 -.12 25 17 | -550 46 78 1510
ngs 200| -2 0 -1 -7 -17 -26 -.05 11 11 | -626 377 777 2140
sio 321| 1 -1 -4 51 -12 -52 -.13 15 14 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.2036.0 GPS week: 2036 Day: 0 MJD: 58496.000
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 9 8 11 9 4 9 22 6 11 3 | 22 24 22 22 20 22 25 36 21 26 22
2 | 13 8 6 8 12 4 11 17 15 11 4 | 31 26 30 33 30 27 26 32 26 28 27
3 | 9 12 4 9 9 3 8 15 8 8 3 | 26 28 23 26 24 23 25 34 23 28 24
X4 | 1 --- --- --- 140 110 --- --- --- --- 0 | 9999 --- --- --- 9999 9999 --- --- --- --- 9999
5 | 10 7 9 9 14 3 11 17 10 13 4 | 59 60 56 62 59 58 59 63 59 57 59
6 | 10 11 9 18 15 3 10 12 6 7 4 | 27 26 26 32 29 26 26 27 25 27 26
7 | 7 10 8 10 9 4 7 22 13 16 4 | 41 45 41 41 39 39 44 40 43 41 40
8 | 7 8 5 12 10 3 8 8 5 12 3 | 22 24 22 22 25 20 24 22 22 23 22
9 | 7 10 8 10 11 3 10 12 8 8 3 | 32 40 30 42 30 33 40 31 31 35 33
10 | 9 9 4 14 8 4 7 13 7 11 3 | 27 29 23 26 27 24 27 21 25 27 25
11 | 8 12 12 8 10 3 9 18 8 15 4 | 22 29 27 21 23 22 25 29 24 20 22
12E | 13 19 8 8 13 5 11 16 13 14 4 | 65 65 72 67 67 70 66 73 76 76 69
13 | 8 6 8 13 10 4 7 8 7 12 3 | 20 22 20 17 18 18 21 17 17 21 17
14 | 6 7 5 7 7 3 8 13 7 16 3 | 16 16 15 17 16 16 15 24 21 24 16
15 | 7 9 9 6 9 5 9 11 10 15 3 | 34 40 39 38 32 35 40 38 38 37 36
16E | 11 21 8 12 14 4 8 17 15 16 4 | 26 29 33 31 25 31 29 38 37 35 29
17 | 9 10 10 7 9 4 7 22 11 14 4 | 21 25 20 24 21 20 25 22 22 20 19
18 | 8 13 8 13 15 4 12 18 9 17 4 | 30 39 35 25 25 31 36 43 32 44 32
19 | 11 18 9 12 11 5 8 29 16 17 5 | 23 26 24 27 24 22 23 27 24 24 21
20 | 10 12 7 13 11 4 8 20 11 15 4 | 23 19 21 24 20 21 20 19 24 21 19
21 | 13 15 7 11 10 6 32 13 11 12 5 | 26 18 22 23 21 21 32 22 21 21 19
22 | 9 12 8 9 11 4 8 20 12 16 4 | 24 24 20 24 21 22 22 28 23 22 20
23 | 7 20 8 12 10 4 8 14 8 14 4 | 42 37 41 46 42 42 41 47 41 41 41
24 | 10 8 9 10 5 3 6 11 7 11 3 | 18 27 23 24 20 19 27 21 21 25 21
25E | 15 14 11 10 13 4 11 14 6 11 4 | 41 43 44 44 43 39 42 39 40 39 40
26E | 8 13 15 13 15 4 9 9 7 12 4 | 71 73 73 79 78 69 31 70 73 72 73
27 | 7 9 5 9 9 3 8 8 8 12 3 | 23 27 23 24 25 23 26 22 25 25 23
28E | 7 7 8 24 9 3 6 20 10 12 4 | 28 29 28 31 28 26 27 28 26 29 26
29 | 15 18 5 12 12 5 10 20 16 19 5 | 30 24 23 27 26 24 26 22 26 29 25
30 | 7 7 8 11 10 3 7 10 7 7 3 | 25 28 27 27 26 23 26 23 22 25 24
31 | 5 12 7 9 15 5 10 16 13 19 4 | 35 46 41 43 38 37 48 34 35 31 38
32 | 9 13 9 8 8 3 11 12 4 11 3 | 32 44 28 36 35 33 41 32 33 35 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 8 11 11 4 10 16 10 13 |T 31 33 31 33 30 30 31 33 31 32 30
WRMS | 9 12 8 12 10 4 10 14 10 13 |NE 28 30 27 29 27 26 30 29 27 29 27
MEDI | 8 11 8 10 10 4 8 15 8 12 |MD 27 28 27 27 26 24 27 29 25 28 25
Table 3.2036.1 GPS week: 2036 Day: 1 MJD: 58497.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 9 8 12 11 4 13 21 6 11 4 | 22 21 20 20 20 18 22 30 21 26 20
2 | 11 9 4 13 12 5 8 16 11 13 3 | 26 20 23 29 25 22 23 26 23 23 22
3 | 7 10 4 9 8 3 9 17 6 7 3 | 21 25 22 21 22 20 25 30 23 23 22
X4 | 3 --- --- --- 109 84 --- --- --- --- 0 | 9999 --- --- --- 9999 9999 --- --- --- --- 9999
5 | 7 6 9 8 16 3 10 14 10 11 3 | 47 48 44 48 50 45 47 48 47 46 46
6 | 9 13 8 22 15 3 10 11 9 7 4 | 23 24 22 26 26 21 25 22 21 22 22
7 | 5 13 9 8 10 3 8 22 11 15 4 | 29 32 25 28 25 27 29 29 30 29 26
8 | 8 8 4 8 7 2 8 8 6 7 2 | 19 21 19 18 18 16 21 18 18 19 18
9 | 6 9 7 10 10 4 9 11 7 8 3 | 25 34 27 34 23 25 35 26 26 28 28
10 | 11 9 5 15 10 2 8 7 9 8 3 | 22 26 21 22 23 20 24 20 24 23 22
11 | 8 11 12 7 11 4 12 14 9 14 3 | 23 24 22 20 18 20 25 22 21 18 19
12E | 7 22 5 10 12 3 11 16 15 14 4 | 50 49 52 51 50 52 49 54 55 56 51
13 | 5 8 9 8 8 2 6 9 9 12 3 | 20 21 20 14 17 16 20 15 13 18 16
14 | 7 7 6 7 7 3 8 15 8 14 3 | 19 16 16 16 17 17 16 23 21 22 16
15 | 7 9 8 6 6 4 7 12 13 16 3 | 25 27 24 23 21 22 26 24 23 30 23
16E | 11 20 6 12 11 4 7 15 15 15 4 | 32 32 34 35 32 33 31 37 39 35 33
17 | 8 10 9 9 10 5 9 22 10 13 4 | 21 22 18 21 17 18 23 18 22 15 17
18 | 7 9 7 10 12 4 11 14 8 16 3 | 31 32 32 28 23 28 31 38 31 39 30
19 | 6 18 8 13 11 5 7 29 13 17 4 | 19 22 21 23 17 18 22 21 19 18 16
20 | 9 11 7 10 11 4 7 15 11 14 3 | 19 16 17 23 18 17 16 15 22 14 16
21 | 10 13 6 8 10 3 10 15 12 11 3 | 20 17 18 21 17 17 22 18 19 13 15
22 | 9 10 6 8 8 3 10 19 10 15 3 | 20 19 15 17 17 16 19 17 18 15 15
23 | 7 19 6 11 8 4 7 11 9 17 3 | 34 32 35 37 36 35 35 35 34 36 34
24 | 6 7 9 5 8 4 8 10 8 11 3 | 21 25 21 21 17 18 26 21 20 24 21
25E | 8 13 10 12 10 3 10 17 8 7 3 | 31 39 32 32 32 29 29 30 29 29 30
26E | 9 9 15 34 12 4 8 12 8 12 5 | 53 51 50 60 57 50 23 52 48 51 51
27 | 8 9 4 5 8 3 8 7 6 9 2 | 22 22 20 20 18 20 21 18 19 20 19
28E | 5 10 6 15 8 3 8 16 8 11 3 | 22 23 22 24 20 20 25 25 21 22 21
29 | 14 19 5 15 9 6 8 19 16 18 4 | 25 20 18 25 18 19 20 18 20 24 19
30 | 7 9 6 9 10 3 6 8 6 6 2 | 19 25 21 22 22 19 26 21 21 21 21
31 | 8 13 8 5 10 4 10 16 14 19 4 | 24 33 28 27 27 26 34 26 28 22 26
32 | 8 13 9 5 8 3 13 16 5 7 3 | 27 37 22 29 27 25 35 24 23 26 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 8 12 10 4 9 15 10 13 |T 26 27 25 26 24 24 26 26 25 26 24
WRMS | 8 12 8 12 10 4 9 14 10 13 |NE 23 25 22 24 22 21 25 23 23 23 22
MEDI | 8 10 7 9 10 3 8 15 9 12 |MD 23 25 22 23 22 20 25 24 22 23 22
Table 3.2036.2 GPS week: 2036 Day: 2 MJD: 58498.000
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 11 7 4 12 19 6 11 3 | 21 25 20 19 19 18 22 28 18 24 19
2 | 7 11 5 13 11 5 9 15 11 12 3 | 26 22 24 29 22 22 22 23 21 22 21
3 | 8 10 6 9 7 5 9 20 8 11 3 | 23 26 21 19 22 20 22 29 23 25 21
X4 | 47 --- --- --- 53 48 --- --- --- --- 50 | 9999 --- --- --- 9999 9999 --- --- --- --- 9999
5 | 7 9 9 9 13 5 10 16 12 14 3 | 51 57 53 52 54 53 54 52 53 52 52
6 | 6 11 9 25 14 4 9 12 9 9 4 | 26 26 25 31 26 25 28 23 25 23 24
7 | 6 9 10 9 9 4 8 26 12 15 4 | 31 34 28 32 30 28 35 31 31 27 29
8 | 10 9 5 9 7 3 7 12 6 11 3 | 21 23 19 19 19 18 21 19 20 22 19
9 | 8 10 8 8 11 4 9 10 7 10 3 | 21 32 20 29 18 21 32 24 20 27 23
10 | 9 7 6 16 10 4 9 10 9 12 3 | 27 30 25 29 26 26 27 26 28 27 26
11 | 9 10 16 7 10 3 10 13 7 13 4 | 20 25 23 19 18 18 22 20 16 17 18
12E | 14 16 10 9 22 8 9 22 15 15 5 | 41 50 50 43 47 47 46 50 51 51 46
13 | 7 7 9 8 8 2 7 13 7 10 3 | 19 18 20 14 16 16 19 15 15 20 16
14 | 7 9 6 8 7 4 7 16 9 13 3 | 17 16 15 14 14 15 16 22 15 19 14
15 | 7 9 10 6 7 4 9 14 12 19 3 | 27 30 26 28 23 24 29 24 25 29 26
16E | 8 21 6 14 11 6 8 15 15 15 4 | 32 33 33 32 31 32 26 35 35 34 30
17 | 7 10 10 9 11 5 8 25 13 11 4 | 25 24 20 23 18 20 24 25 25 18 20
18 | 9 11 9 15 12 4 11 13 7 16 4 | 27 35 31 26 20 27 29 34 28 38 28
19 | 7 19 9 10 9 7 7 30 14 15 4 | 20 22 21 21 19 19 20 24 21 19 17
20 | 10 9 6 14 11 5 9 20 11 14 4 | 17 17 17 20 17 16 16 21 18 19 15
21 | 17 12 6 13 10 5 8 15 12 14 4 | 28 19 20 25 17 19 20 20 18 17 17
22 | 8 9 6 8 8 5 10 20 10 15 3 | 20 20 17 18 18 17 19 19 21 18 16
23 | 8 21 7 10 9 5 6 11 10 13 3 | 34 34 32 35 32 32 30 36 31 34 31
24 | 8 11 10 8 8 3 6 18 5 12 3 | 19 28 22 20 18 18 25 22 18 19 19
X25E | 13 --- 15 17 14 4 10 17 7 8 4 | 24 --- 29 26 30 26 29 31 28 25 26
26E | 12 13 17 47 12 4 9 15 10 9 6 | 53 54 51 65 56 52 34 55 52 53 53
27 | 10 10 6 7 8 4 8 9 7 10 3 | 21 23 19 19 18 18 21 17 19 20 18
28E | 10 11 6 9 7 4 8 16 10 11 3 | 22 23 21 23 20 20 22 25 21 23 20
29 | 11 19 6 15 10 6 8 19 18 16 4 | 26 22 19 24 19 20 19 18 22 24 19
30 | 8 7 8 10 9 3 6 9 6 5 2 | 19 25 21 23 22 19 25 22 20 21 20
31 | 18 12 10 6 10 5 9 15 15 18 4 | 36 37 34 32 33 29 39 29 28 24 31
32 | 10 14 9 8 9 5 12 17 9 7 3 | 24 34 20 26 20 23 33 28 22 25 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 9 14 10 5 9 17 10 13 |T 26 28 25 26 24 24 26 27 25 26 24
WRMS | 9 12 9 11 10 5 9 14 10 12 |NE 24 27 23 24 22 22 25 25 23 24 22
MEDI | 8 10 8 9 10 4 9 15 10 12 |MD 24 25 21 25 20 20 25 24 22 24 21
Table 3.2036.3 GPS week: 2036 Day: 3 MJD: 58499.000
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 | 5 8 8 9 8 4 9 18 8 13 3 | 20 23 22 20 22 20 23 30 22 27 21
2 | 8 8 8 11 11 4 10 17 12 11 3 | 24 19 26 26 20 23 21 20 22 23 21
3 | 10 13 9 9 8 4 9 23 5 8 3 | 21 26 21 18 20 17 20 28 20 21 19
X4 | 2 --- --- --- 515 216 --- --- --- --- 0 | 9999 --- --- --- 9999 9999 --- --- --- --- 9999
5 | 10 7 9 10 14 4 12 14 8 12 3 | 33 28 29 32 28 29 31 28 27 29 28
6 | 7 10 8 17 13 4 8 8 7 8 3 | 24 22 23 25 23 22 23 22 20 22 21
7 | 6 11 9 12 10 4 9 27 13 17 4 | 30 33 31 34 31 27 35 23 27 24 28
8 | 7 9 6 14 9 4 7 13 6 11 3 | 18 22 19 23 20 19 23 20 19 20 19
9 | 7 10 8 9 10 5 11 11 9 14 3 | 24 35 22 27 20 23 34 28 24 31 25
10 | 9 7 6 15 8 4 6 19 7 11 3 | 22 24 23 27 23 21 25 24 22 24 22
11 | 6 9 13 9 12 4 8 10 9 14 3 | 21 24 20 23 21 20 23 19 22 15 19
12E | 14 19 8 10 11 5 9 25 13 14 4 | 32 34 37 38 37 37 36 47 39 37 36
13 | 7 7 9 10 8 4 9 15 6 16 3 | 17 19 17 13 13 15 20 16 14 19 15
14 | 9 7 7 11 5 5 7 19 12 17 3 | 19 17 18 18 15 17 16 22 22 19 16
15 | 8 8 10 7 7 4 8 16 10 18 3 | 25 30 30 28 27 26 32 30 26 30 27
16E | 12 20 7 16 8 5 8 15 15 15 4 | 34 34 38 36 38 36 34 38 41 37 36
17 | 9 13 7 8 10 5 9 27 9 11 4 | 22 24 20 21 20 20 25 26 22 18 20
18 | 8 11 8 12 14 5 9 12 9 19 4 | 25 30 30 23 21 26 30 33 25 38 26
19 | 7 15 9 10 10 5 7 30 12 14 4 | 18 22 23 24 18 20 22 26 21 18 18
20 | 10 9 7 19 11 4 8 29 12 15 4 | 17 16 19 25 20 18 19 27 20 19 17
21 | 17 13 7 10 11 4 7 21 10 12 4 | 25 17 20 22 16 19 20 24 18 17 17
22 | 9 11 7 9 10 4 7 26 10 17 4 | 21 21 18 18 20 19 18 26 19 20 17
23 | 6 19 6 12 10 4 5 13 11 17 3 | 20 18 20 25 18 21 18 25 22 20 19
24 | 9 8 8 6 11 3 5 27 6 13 3 | 20 26 23 21 17 17 25 25 20 23 20
25E | 10 13 15 30 12 4 9 10 9 38 6 | 20 27 23 27 23 18 22 23 20 39 20
26E | 11 9 15 41 13 5 8 21 11 7 5 | 37 42 42 47 44 40 37 41 40 41 40
27 | 7 11 5 10 8 3 7 12 7 11 3 | 19 21 19 20 19 18 22 19 18 19 18
28E | 7 9 6 10 8 3 7 19 9 10 3 | 21 22 22 19 25 19 23 29 20 22 20
29 | 13 17 6 12 10 5 8 19 15 20 4 | 24 19 19 23 19 19 22 20 22 22 19
30 | 7 8 8 9 10 4 7 10 6 7 2 | 18 25 21 21 21 17 25 20 19 21 20
31 | 7 13 8 9 9 5 9 16 12 21 4 | 36 40 35 36 35 32 41 28 32 27 34
32 | 8 12 10 11 7 5 10 19 8 9 3 | 23 37 23 25 21 25 35 31 27 26 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 9 14 10 4 8 19 10 15 |T 23 25 24 25 23 22 25 26 23 24 22
WRMS | 9 12 9 15 9 4 8 15 10 14 |NE 22 24 22 23 21 21 24 24 22 22 21
MEDI | 8 10 8 10 10 4 8 18 9 14 |MD 22 24 22 24 21 20 23 26 22 22 20
Table 3.2036.4 GPS week: 2036 Day: 4 MJD: 58500.000
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 7 7 3 9 13 5 12 3 | 22 24 22 21 23 21 25 28 23 26 22
2 | 8 10 6 10 10 4 8 27 11 13 3 | 20 20 21 21 20 19 18 21 21 19 18
3 | 7 9 6 12 8 4 8 26 5 9 3 | 24 26 25 24 26 23 25 33 25 26 24
X4 | 3 --- --- --- 1567 265 --- --- --- --- 0 | 9999 --- --- --- 9999 9999 --- --- --- --- 9999
5 | 8 9 8 11 12 3 10 14 9 13 3 | 70 72 73 73 70 72 73 74 70 71 71
6 | 6 12 9 17 13 4 8 10 6 9 3 | 26 24 26 26 26 25 27 25 25 25 24
7 | 6 10 9 10 11 4 7 34 13 17 4 | 31 35 30 36 30 30 36 35 33 31 31
8 | 8 10 5 10 7 4 9 16 5 13 3 | 21 24 20 23 22 19 24 22 21 21 20
9 | 10 10 8 10 8 4 9 7 8 12 3 | 25 35 28 36 28 27 37 28 29 34 30
10 | 11 11 8 17 8 4 7 28 7 12 4 | 28 32 25 30 28 26 29 29 28 29 27
11 | 5 8 14 10 11 3 8 8 4 13 3 | 26 27 28 26 24 24 29 24 24 21 24
12E | 8 17 7 8 12 3 10 29 13 12 4 | 46 45 49 47 48 48 44 59 52 49 47
13 | 7 8 7 9 5 2 6 13 10 14 3 | 17 20 18 17 14 14 19 15 14 20 15
14 | 9 7 7 12 6 5 8 20 11 15 3 | 21 15 16 15 15 16 14 24 20 20 15
15 | 5 8 8 8 6 4 8 16 12 17 3 | 27 29 26 30 27 24 27 25 24 26 26
16E | 13 18 9 13 20 6 11 18 17 14 5 | 30 36 36 35 42 35 32 38 40 37 34
17 | 6 12 9 7 10 4 7 30 10 13 3 | 22 26 19 23 21 20 24 25 21 21 20
18 | 7 9 9 12 11 4 7 14 5 15 3 | 27 30 33 25 24 28 30 34 28 36 28
19 | 6 19 9 10 12 5 7 31 13 17 4 | 19 22 23 25 19 19 20 24 20 23 18
20 | 8 8 6 13 11 3 9 40 9 15 4 | 18 18 16 22 20 17 16 29 19 16 15
21 | 14 12 8 10 8 5 8 24 10 16 4 | 23 16 18 21 17 17 18 22 16 13 15
22 | 7 9 8 11 8 4 8 28 9 17 4 | 23 22 22 24 23 21 20 26 23 20 20
23 | 5 21 7 9 8 3 7 15 10 21 4 | 37 33 39 38 38 36 34 36 33 41 36
24 | 7 6 10 7 11 2 7 33 7 12 3 | 19 25 22 24 19 19 26 29 23 21 20
25E | 10 15 14 33 9 5 8 16 7 42 6 | 26 30 29 33 28 27 30 34 28 49 28
26E | 18 13 20 39 13 6 11 25 15 11 6 | 60 55 53 64 57 53 48 59 55 54 55
27 | 8 11 6 8 8 3 8 16 8 15 3 | 22 24 22 21 21 20 23 19 22 23 20
28E | 9 15 6 14 12 4 7 21 10 11 4 | 23 25 20 22 28 20 25 27 23 21 22
29 | 12 18 7 12 9 4 7 19 15 18 4 | 22 18 19 22 19 19 19 19 19 21 18
30 | 8 8 8 8 10 3 7 12 6 9 3 | 20 25 22 23 21 21 26 24 24 23 22
31 | 9 13 9 9 9 4 10 19 14 20 4 | 35 40 34 35 35 31 40 27 32 27 33
32 | 8 14 11 11 7 4 10 15 8 8 3 | 30 39 26 27 27 28 36 33 29 32 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 9 14 10 4 8 22 10 16 |T 27 29 27 29 27 26 28 30 27 28 26
WRMS | 8 12 9 15 9 4 8 16 10 14 |NE 25 27 25 27 25 24 27 28 25 26 24
MEDI | 8 10 8 10 9 4 8 19 9 13 |MD 24 26 25 25 24 23 26 27 24 25 24
Table 3.2036.5 GPS week: 2036 Day: 5 MJD: 58501.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 11 6 9 9 3 10 12 8 12 3 | 20 23 20 21 22 19 24 26 20 26 20
2 | 8 12 4 10 11 4 9 37 12 12 4 | 21 18 20 21 19 19 19 32 23 23 19
3 | 10 10 6 9 10 3 9 30 7 6 3 | 27 26 22 23 24 21 25 40 23 25 23
X4 | 34 --- --- --- 42 61 --- --- --- --- 38 | 9999 --- --- --- 9999 9999 --- --- --- --- 9999
5 | 6 10 6 11 14 2 10 16 10 12 3 | 64 62 59 65 66 61 61 60 60 64 62
6 | 9 15 9 18 14 4 9 10 10 9 4 | 23 25 22 25 26 21 24 23 24 27 22
7 | 6 13 10 6 8 4 8 35 13 16 4 | 30 36 28 32 31 30 35 42 32 31 30
8 | 7 12 8 7 7 4 7 18 7 9 3 | 20 21 19 24 21 19 22 21 20 20 19
9 | 9 10 9 9 10 4 9 7 9 9 3 | 24 34 24 30 21 23 36 23 25 32 26
10 | 10 8 6 13 7 4 7 26 6 12 3 | 26 31 26 30 30 26 29 33 28 29 27
11 | 10 11 16 10 11 5 9 11 7 17 4 | 21 23 22 21 19 20 25 19 19 18 19
12E | 8 16 6 11 13 2 10 31 14 13 4 | 61 63 61 60 59 61 59 67 67 65 61
13 | 5 7 8 5 6 3 6 11 10 12 2 | 15 19 17 16 13 15 18 15 15 18 15
14 | 10 7 6 9 6 3 7 19 15 17 3 | 16 16 14 14 17 15 14 24 23 25 15
15 | 7 11 8 9 6 4 7 15 15 17 3 | 18 25 20 26 17 17 20 21 17 23 18
16E | 7 25 10 23 8 5 7 16 14 12 4 | 31 36 33 26 27 32 30 34 37 35 30
17 | 11 14 8 9 11 6 9 33 10 12 4 | 25 29 19 25 19 20 24 33 23 23 21
18 | 8 10 13 17 14 6 9 20 7 18 4 | 27 32 34 27 22 29 32 36 30 40 29
19 | 8 17 8 8 11 7 8 34 14 15 4 | 22 27 24 27 20 21 24 32 24 24 22
20 | 9 12 7 14 10 5 8 41 13 15 4 | 16 19 18 22 19 16 16 34 19 16 15
21 | 9 11 10 15 10 5 10 23 13 17 4 | 17 18 17 20 14 15 16 19 18 13 13
22 | 10 11 6 9 11 4 9 28 11 15 4 | 25 21 18 22 19 19 20 30 20 20 18
23 | 7 21 6 7 9 4 8 24 12 13 4 | 28 26 24 28 27 27 28 36 26 28 26
24 | 9 10 11 8 9 3 7 37 11 11 4 | 17 27 19 23 16 16 23 33 18 21 18
25E | 10 11 15 34 14 4 12 14 8 39 6 | 35 36 36 35 36 33 35 38 34 46 34
X26E | 11 16 17 37 14 6 --- 18 14 14 7 | 45 46 43 53 48 42 --- 46 40 46 44
27 | 8 11 7 7 7 5 6 20 10 10 3 | 23 23 19 22 19 20 23 20 21 20 20
28E | 8 12 6 8 9 4 7 22 11 10 3 | 23 23 18 21 22 19 22 29 21 22 20
29 | 12 19 8 12 10 6 7 20 19 17 4 | 24 21 18 23 19 19 21 19 22 21 19
30 | 7 8 9 7 8 4 6 17 6 7 2 | 19 26 20 23 21 18 24 22 18 21 20
31 | 10 14 9 8 9 5 8 19 17 22 4 | 35 39 33 34 33 31 37 32 29 31 32
32 | 8 13 9 7 8 3 10 13 8 11 3 | 24 38 24 29 27 28 36 28 29 30 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 12 10 4 8 24 11 15 |T 26 29 25 28 25 24 27 31 26 28 25
WRMS | 9 13 9 14 9 4 8 16 11 14 |NE 24 27 23 25 23 22 26 28 24 25 22
MEDI | 8 11 8 9 10 4 8 20 11 12 |MD 24 26 22 25 21 20 24 32 23 25 21
Table 3.2036.6 GPS week: 2036 Day: 6 MJD: 58502.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 12 5 7 8 3 10 13 5 10 3 | 23 25 22 24 23 21 26 31 26 26 23
2 | 9 15 8 9 10 3 8 39 10 13 4 | 25 23 28 27 24 25 26 27 27 26 24
3 | 7 15 6 7 8 4 11 30 11 12 4 | 29 27 24 28 26 24 28 44 25 32 26
X4 | 52 --- --- --- 58 64 --- --- --- --- 55 | 9999 --- --- --- 9999 9999 --- --- --- --- 9999
5 | 8 10 7 9 16 3 11 21 12 13 4 | 62 60 59 62 62 60 60 60 60 60 60
6 | 9 17 8 11 12 3 9 10 8 8 3 | 25 27 27 31 30 26 29 27 26 28 26
7 | 7 12 10 9 8 4 9 37 16 16 4 | 42 47 43 43 37 41 47 52 42 41 41
8 | 8 14 9 9 9 4 9 18 9 9 3 | 20 24 20 24 23 20 25 24 23 22 21
9 | 9 13 11 7 10 4 11 11 9 12 3 | 26 37 22 29 25 26 34 29 27 33 27
10 | 10 9 6 13 6 4 8 22 8 11 3 | 32 35 29 36 31 31 33 36 35 31 31
11 | 8 14 17 7 12 5 9 11 6 15 4 | 26 30 26 26 25 23 29 24 26 21 24
12E | 13 14 7 10 13 5 7 30 16 13 4 | 71 74 77 71 73 75 76 79 79 82 74
13 | 8 9 8 6 8 2 7 11 12 13 3 | 20 26 19 21 18 19 23 18 20 25 19
14 | 10 8 8 7 7 4 10 18 10 17 3 | 19 19 16 19 20 17 15 29 25 29 18
15 | 6 12 10 9 5 3 9 18 11 15 3 | 33 41 35 40 32 33 40 39 34 36 35
16E | 13 33 9 11 12 5 7 18 17 13 5 | 31 48 34 31 30 34 33 38 40 37 32
17 | 7 12 10 7 11 5 9 38 9 12 4 | 24 27 22 28 22 22 27 42 24 25 23
18 | 9 10 11 13 11 5 9 20 7 13 4 | 37 38 39 34 29 35 37 39 39 41 35
19 | 8 19 9 9 14 5 9 37 11 15 4 | 25 30 28 31 23 25 27 41 26 27 25
20 | 8 12 4 13 11 4 9 37 11 15 4 | 22 23 21 28 21 22 21 39 25 23 21
21 | 13 16 6 11 11 5 13 27 13 17 4 | 24 20 19 23 18 19 22 28 20 17 17
22 | 10 11 9 8 9 4 13 31 13 16 4 | 29 24 20 27 23 21 22 34 23 24 22
23 | 6 21 7 9 10 3 9 32 13 15 4 | 34 32 31 39 36 34 32 48 35 36 33
24 | 7 8 10 6 10 3 8 37 8 11 4 | 19 26 22 23 17 18 26 39 18 21 19
25E | 10 12 17 32 10 6 11 15 8 38 6 | 42 39 42 40 43 39 41 40 39 45 39
X26E | 16 30 24 35 19 12 --- 20 24 17 9 | 73 83 75 89 77 72 --- 72 74 75 75
27 | 8 14 9 11 7 5 9 19 8 10 3 | 17 23 19 22 21 18 22 23 19 17 18
28E | 10 14 6 9 10 3 9 23 12 13 4 | 26 29 23 23 24 22 25 30 22 25 22
29 | 14 18 7 16 8 6 8 21 17 17 4 | 28 23 23 28 25 24 25 29 23 26 24
30 | 7 10 9 7 9 4 9 22 9 8 3 | 20 27 23 23 21 20 24 26 22 23 21
31 | 9 15 9 12 10 4 11 24 15 16 4 | 40 46 42 43 39 38 48 43 38 34 40
32 | 7 14 11 7 7 4 11 12 5 11 3 | 35 44 29 41 36 35 43 37 36 39 36
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 9 11 10 4 10 25 11 15 |T 31 34 30 34 30 30 32 37 32 33 30
WRMS | 9 13 9 12 9 4 10 17 11 14 |NE 28 30 27 30 27 26 30 34 28 29 27
MEDI | 8 14 9 9 10 4 9 21 11 13 |MD 26 29 26 28 25 25 27 37 26 28 25
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2036 GPS week: 2036 MJD: 58496.0-58502.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 10 11 22 |U 11 13 52 |U 10 9 29 |
emr | emr 2962 |U 18 16 36 |U 14 18 58 |U 17 15 43 |
esa | esa 2976 | 10 10 23 |U 11 15 54 |U 11 9 34 |
gfz | gfz 2974 |U 10 11 20 |U 12 15 50 |U 10 9 29 |
grg | grg 3070 |U 9 11 22 |U 12 15 49 | 12 12 33 |
igr | igr 2970 | 9 10 21 | 11 14 52 | 11 9 30 |
igs | igs 3023 | 10 12 21 | 11 14 53 | 11 9 31 |
jpl | jpl 2948 |U 15 13 31 |U 13 18 57 |U 14 11 42 |
mit | mit 2976 | 15 16 32 |U 17 24 71 |U 16 18 48 |
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 5.2036.0 GPS week: 2036 Day: 0 MJD: 58496.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 12 19 | 12 12 55 | 11 8 29 |
emr | emr 2976 | 27 19 57 | 12 16 67 | 13 10 40 |
esa | esa 2976 | 12 11 21 | 11 11 59 | 11 7 35 |
gfz | gfz 2976 | 11 11 19 | 12 10 62 | 10 8 30 |
grg | grg 3072 | 10 11 20 | 12 12 56 | 15 17 43 |
igr | igr 2948 | 12 11 21 | 11 11 56 | 11 8 31 |
igs | igs 3005 | 12 11 23 | 11 11 59 | 11 7 31 |
jpl | jpl 2976 | 17 15 33 | 13 15 68 | 13 16 46 |
mit | mit 2976 | 17 20 31 | 13 19 67 | 24 26 76 |
Table 5.2036.1 GPS week: 2036 Day: 1 MJD: 58497.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 12 20 | 11 15 58 | 9 8 28 |
emr | emr 2975 | 17 14 36 | 15 22 70 | 16 14 37 |
esa | esa 2976 | 11 12 24 | 12 19 61 | 11 7 31 |
gfz | gfz 2970 | 11 12 18 | 10 16 61 | 9 8 28 |
grg | grg 3068 | 8 11 17 | 12 18 51 | 10 9 27 |
igr | igr 2973 | 10 11 17 | 11 16 60 | 10 8 29 |
igs | igs 3032 | 10 12 20 | 12 18 58 | 10 8 28 |
jpl | jpl 2976 | 14 13 28 | 14 25 63 | 12 8 38 |
mit | mit 2976 | 13 17 45 | 16 24 67 | 13 10 37 |
Table 5.2036.2 GPS week: 2036 Day: 2 MJD: 58498.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 10 21 | 10 11 58 | 11 8 29 |
emr | emr 2880 | 18 9 37 | 13 19 44 | 16 17 42 |
esa | esa 2976 | 10 9 22 | 11 14 64 | 11 8 33 |
gfz | gfz 2976 | 10 10 20 | 10 12 59 | 10 8 29 |
grg | grg 3072 | 9 8 18 | 11 14 54 | 11 10 28 |
igr | igr 2972 | 10 9 20 | 9 11 60 | 10 8 28 |
igs | igs 3065 | 10 9 21 | 10 12 59 | 11 8 30 |
jpl | jpl 2976 | 13 13 30 | 12 17 64 | 13 12 39 |
mit | mit 2976 | 10 11 22 | 17 29 69 | 12 11 30 |
Table 5.2036.3 GPS week: 2036 Day: 3 MJD: 58499.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 7 20 | 13 13 47 | 10 8 22 |
emr | emr 2976 | 17 11 30 | 16 18 50 | 14 9 36 |
esa | esa 2976 | 9 9 22 | 14 15 51 | 11 7 27 |
gfz | gfz 2976 | 9 8 18 | 13 15 45 | 10 8 23 |
grg | grg 3072 | 8 9 19 | 14 15 43 | 11 9 25 |
igr | igr 2976 | 9 8 18 | 12 15 46 | 10 7 25 |
igs | igs 3002 | 10 9 19 | 14 14 46 | 11 7 26 |
jpl | jpl 2976 | 16 12 30 | 16 19 48 | 14 7 38 |
mit | mit 2976 | 11 13 32 | 20 29 67 | 11 8 35 |
Table 5.2036.4 GPS week: 2036 Day: 4 MJD: 58500.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 9 14 27 | 11 11 52 | 11 11 33 |
emr | emr 2976 | 15 16 34 | 14 18 59 | 14 17 42 |
esa | esa 2976 | 9 14 29 | 12 14 51 | 11 9 33 |
gfz | gfz 2971 | 9 14 24 | 13 14 46 | 11 10 34 |
grg | grg 3069 | 9 15 27 | 12 14 46 | 12 14 37 |
igr | igr 2973 | 9 15 26 | 11 13 48 | 12 10 34 |
igs | igs 2976 | 9 15 26 | 11 12 49 | 12 11 34 |
jpl | jpl 2976 | 15 18 37 | 14 17 53 | 15 13 44 |
mit | mit 2976 | 25 20 36 | 17 21 73 | 16 20 50 |
Table 5.2036.5 GPS week: 2036 Day: 5 MJD: 58501.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 9 30 | 9 16 45 | 11 8 29 |
emr | emr 2976 | 15 22 29 | 15 18 63 | 23 20 54 |
esa | esa 2976 | 9 8 21 | 10 16 46 | 13 17 45 |
gfz | gfz 2976 | 9 9 19 | 11 18 35 | 11 7 28 |
grg | grg 3070 | 11 9 32 | 9 14 45 | 12 9 34 |
igr | igr 2976 | 9 8 27 | 8 15 44 | 11 8 29 |
igs | igs 3051 | 11 16 19 | 8 17 52 | 13 12 32 |
jpl | jpl 2880 | 12 11 27 | 10 19 51 | 14 9 35 |
mit | mit 2976 | 18 17 32 | 20 20 68 | 16 29 61 |
Table 5.2036.6 GPS week: 2036 Day: 6 MJD: 58502.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 7 11 19 | 12 16 50 | 11 12 31 |
emr | emr 2975 | 17 17 28 | 13 14 54 | 22 16 51 |
esa | esa 2976 | 7 10 24 | 12 18 48 | 12 11 35 |
gfz | gfz 2975 | 8 13 21 | 11 18 42 | 12 12 33 |
grg | grg 3070 | 9 11 20 | 12 15 50 | 13 13 37 |
igr | igr 2975 | 7 11 19 | 12 17 50 | 12 12 35 |
igs | igs 3034 | 8 12 20 | 11 15 50 | 13 12 37 |
jpl | jpl 2880 | 15 12 30 | 11 14 56 | 15 14 52 |
mit | mit 2976 | 13 18 30 | 14 24 86 | 19 19 50 |
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 6.2036 GPS week: 2036 MJD: 58496.500-58502.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 2 -62 50 3 | 16 26
| 18 17 64 46 10 | 4
emr uuuxx | 42 -20 201 232 -16 | 38 44
| 34 31 140 257 14 | 2
esa uuuuu | 25 6 -56 79 -5 | 26 31
| 16 6 54 46 3 | 1
gfz uuuuu | -13 -17 -88 80 2 | 20 26
| 21 28 148 91 4 | 2
grg uuuuu | 12 24 -8 -21 1 | -3 16
| 12 6 45 40 5 | 2
igr xxxxx | 12 5 2 68 -2 | 4 18
| 11 9 24 38 4 | 1
irf xxxxx | -23 -20 -10 -47 -12 | 5 19
| 6 11 36 20 4 | 2
jpl uuuuu | -12 -31 94 2 2 | 30 35
| 15 16 41 51 12 | 2
mit uuuuu | -17 15 10 -175 -10 | 21 28
| 21 21 70 59 5 | 1
ngs uuuuu | -14 20 -7 -44 1 | 9 18
| 52 21 192 132 3 | 2
sio uuuux | -36 6 -68 -140 -1 | 37 42
| 20 17 62 35 5 | 2
Table 7.2036.0 GPS week: 2036 Day: 0 MJD: 58496.500
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 | 4 13 -2 88 2 | 11 24
emr uuuxx | 12 -45 286 18 -17 | 40 47
esa uuuuu | 15 10 -57 51 -4 | 26 31
gfz uuuuu | -18 -42 50 127 3 | 17 25
grg uuuuu | 13 16 -83 -51 1 | -6 19
igr xxxxx | 15 1 -23 147 3 | 3 19
irf xxxxx | -25 -11 -34 -78 -16 | 9 20
jpl uuuuu | -1 -3 61 -50 -10 | 32 38
mit uuuuu | -23 45 -24 -241 -14 | 21 29
ngs uuuuu | 3 18 -158 43 5 | 6 18
sio uuuux | -31 -18 16 -133 -2 | 37 43
Table 7.2036.1 GPS week: 2036 Day: 1 MJD: 58497.500
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 | 25 -16 -111 96 18 | 12 24
emr uuuxx | 23 -27 241 63 -10 | 39 46
esa uuuuu | 7 11 -34 51 -5 | 26 32
gfz uuuuu | -1 -38 -33 112 3 | 18 26
grg uuuuu | 1 30 50 -58 -7 | -4 18
igr xxxxx | 17 -3 26 34 1 | 4 19
irf xxxxx | -27 -28 5 -65 -17 | 8 20
jpl uuuuu | -27 -32 45 -69 -10 | 32 38
mit uuuuu | -38 24 22 -201 -14 | 21 29
ngs uuuuu | 21 23 40 37 4 | 8 18
sio uuuux | -40 32 -141 -113 1 | 37 43
Table 7.2036.2 GPS week: 2036 Day: 2 MJD: 58498.500
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 | -32 13 -94 -5 14 | 14 26
emr uuuxx | 19 -36 288 108 -9 | 38 45
esa uuuuu | 26 6 -119 129 -3 | 26 31
gfz uuuuu | -4 7 -121 21 2 | 18 26
grg uuuuu | 34 30 20 50 -2 | -5 18
igr xxxxx | 28 10 12 47 -2 | 4 18
irf xxxxx | -32 -17 -34 -37 -10 | 6 19
jpl uuuuu | -23 -48 91 24 -9 | 28 34
mit uuuuu | -4 29 -64 -173 -8 | 20 28
ngs uuuuu | 35 -3 69 -13 1 | 7 18
sio uuuux | -68 22 -53 -197 6 | 36 41
Table 7.2036.3 GPS week: 2036 Day: 3 MJD: 58499.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 10 14 -166 -18 -7 | 16 27
emr uuuxx | 24 -15 278 70 -6 | 37 44
esa uuuuu | 24 1 -117 131 -3 | 25 31
gfz uuuuu | -31 17 -270 -81 0 | 18 26
grg uuuuu | 23 21 -32 -27 4 | -5 18
igr xxxxx | 13 4 -15 59 -7 | 3 18
irf xxxxx | -27 -4 -58 -57 -9 | 5 19
jpl uuuuu | -28 -50 135 10 9 | 27 33
mit uuuuu | -45 23 -53 -159 -7 | 21 28
ngs uuuuu | 19 6 210 89 0 | 8 18
sio uuuux | -45 10 -61 -173 4 | 36 41
Table 7.2036.4 GPS week: 2036 Day: 4 MJD: 58500.500
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 -20 6 41 -1 | 19 27
emr uuuxx | 45 13 -67 260 -11 | 39 45
esa uuuuu | 33 15 -77 47 -7 | 28 32
gfz uuuuu | -43 6 -303 56 0 | 22 26
grg uuuuu | 3 27 -17 -28 7 | -2 15
igr xxxxx | 8 20 -27 44 -3 | 6 17
irf xxxxx | -17 -20 -19 -22 -15 | 6 19
jpl uuuuu | -14 -32 154 -14 0 | 30 35
mit uuuuu | -14 -5 -5 -61 -16 | 22 29
ngs uuuuu | -4 1 226 -1 -2 | 10 18
sio uuuux | -2 8 -126 -121 -10 | 39 43
Table 7.2036.5 GPS week: 2036 Day: 5 MJD: 58501.500
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 | -6 -12 -14 60 3 | 18 27
emr uuuxx | 63 28 85 363 -15 | 36 42
esa uuuuu | 56 2 -19 121 -11 | 27 31
gfz uuuuu | 21 -53 40 127 -5 | 21 26
grg uuuuu | 2 27 -21 -50 3 | -2 15
igr xxxxx | -6 -7 33 67 -6 | 5 17
irf xxxxx | -15 -36 27 -31 -9 | 2 18
jpl uuuuu | 2 -24 114 40 15 | 29 34
mit uuuuu | 17 -15 60 -161 -7 | 19 27
ngs uuuuu | -109 46 -194 -212 -2 | 10 17
sio uuuux | -34 0 3 -99 1 | 37 42
Table 7.2036.6 GPS week: 2036 Day: 6 MJD: 58502.500
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 | -7 19 -51 87 -7 | 22 26
emr uuuxx | 110 -56 299 745 -46 | 36 42
esa uuuuu | 13 0 31 25 -4 | 27 31
gfz uuuuu | -13 -18 23 201 8 | 23 26
grg uuuuu | 11 15 30 19 -1 | 1 9
igr xxxxx | 10 8 5 78 -4 | 6 16
irf xxxxx | -16 -27 41 -41 -7 | 3 18
jpl uuuuu | 10 -27 60 76 18 | 31 35
mit uuuuu | -14 2 137 -225 -4 | 20 27
ngs uuuuu | -60 51 -239 -249 2 | 11 17
sio uuuux | -30 -10 -115 -146 -4 | 40 43
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