[IGSREPORT-27111] Wk 2092 IGS Final Orbits
acc
acc at igs.org
Fri Feb 28 03:30:43 PST 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2092 (Feb 09, 2020 - Feb 15, 2020)
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:
igs2092[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2092[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2092[0-6].cls IGS GPS clock combination summary report.
igs20927.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20927.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 | TIXI TIXI
0 | ESA | PTBB PTBB
0 | GFZ | 4 4 ABPO BJNM GODE POHN ABPO BJNM GODE POHN
0 | GRG | CCJ2 NYA2 CCJ2 NYA2
0 | MIT | 18 BJNM MAW1
1 | COD | CPVG TIXI CPVG TIXI
1 | EMR | 18 NNOR
1 | ESA | 18 18 CPVG DJIG OHI3 PTBB UNSA CPVG DJIG OHI3 PTBB
1 | ESA | UNSA
1 | GFZ | 4 4 FLRS GODE POHN REUN FLRS GODE POHN
1 | GRG | OHI3 OHI3
1 | JPL | 18 REUN
1 | MIT | 18
2 | COD | BARH CPVG GOLD KOUR TIXI TLSE WIND CPVG TIXI TLSE
2 | EMR | 18
2 | ESA | 18 18 CHUR DAV1 LPGS PTBB REUN WIND CHUR DAV1 PTBB
2 | ESA | REUN WIND
2 | GFZ | 4 4 BJNM DAV1 KOUR LPGS POHN REUN DAV1 GOLD KOKV
2 | GFZ | KOUR POHN REUN TLSE
2 | GRG | CCJ2 JOG2 TLSE CCJ2 DARW JOG2 LPGS PDEL TLSE
2 | JPL | KOUR
2 | MIT | KOUR
3 | COD | TIXI TIXI
3 | EMR | 18
3 | ESA | 18 18 ANKR DJIG PTBB ANKR DJIG PTBB
3 | GFZ | 4 18 4 18 POHN GODE POHN
3 | GRG | ULAB ULAB
3 | MIT | 18 CRO1 GOPE
4 | COD | LPGS SAVO TIXI TWTF LPGS SAVO TIXI TWTF
4 | EMR | TLSE TLSE
4 | ESA | 18 18 AREG GLPS NKLG PTBB REUN AREG GLPS NKLG PTBB
4 | ESA | REUN
4 | GFZ | 4 4 GODE POHN TWTF GODE POHN TLSE TWTF
4 | GRG | 5 27 5 27 TLSE TLSE
4 | JPL | ASCG
5 | COD | BRFT REUN TIXI BJNM BRFT REUN TIXI
5 | ESA | 18 18 IQAL LPGS PTBB SCH2 IQAL PTBB SCH2
5 | GFZ | 4 4 GODE LPGS POHN GODE POHN
5 | GRG | HOFN HOFN
5 | JPL | 13 13
6 | COD | TIXI BJNM TIXI ZAMB
6 | ESA | 18 18 PTBB PTBB
6 | GFZ | 4 18 4 13 18 GODE POHN GODE POHN
6 | GRG | 13 13 NYA2 NYA2
6 | JPL | POLV POLV
6 | MIT | BJNM
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
----+--------+---------------
2 | ESA | 18
4 | GRG | 27
6 | MIT | ALL (high Transformation - See Table 2)
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G27 | 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 -.2 .5 8 22 27 -.24
EMR | 0 | 3.3 -8.1 5.2 -30 -2 22 -.05
ESA | 0 | .7 -.3 .2 13 37 84 -.52
GFZ | 0 | .4 .2 -.1 29 3 65 -.32
GRG | 0 | 3.0 -5.6 -3.1 47 -17 122 .11
JPL | 0 | -5.4 -8.4 8.7 12 24 17 -.16
MIT | 0 | 1.3 -.4 .3 -37 -15 44 .12
NGS | 0 | -.9 -11.7 3.6 -71 33 -14 .16
SIO | 0 | 3.3 -1.8 26.6 13 -11 -12 -.37
COD | 1 | 1.0 -.2 1.3 0 11 15 -.67
EMR | 1 | 13.1 -5.5 2.8 -28 -16 29 -.28
ESA | 1 | .7 -.2 .2 13 27 68 -.55
GFZ | 1 | 1.0 .3 .1 27 -6 65 -.42
GRG | 1 | 4.7 -6.2 -4.0 52 3 60 -.0
JPL | 1 | 10.6 -1.7 6.0 8 3 26 -.46
MIT | 1 | 6.3 -1.7 1.3 -12 -2 26 -.19
NGS | 1 | 6.5 -5.6 -3.7 -49 -4 -32 -.40
SIO | 1 | 2.1 -.2 22.6 15 -52 -16 -.48
COD | 2 | .1 -.2 1.3 5 28 27 -.44
EMR | 2 | 5.1 -4.7 3.2 -16 45 -9 -.01
ESA | 2 | .6 -.1 .6 7 38 102 -.29
GFZ | 2 | .0 .5 -.4 41 -5 65 -.16
GRG | 2 | 3.3 -3.5 6.5 5 -2 91 .21
JPL | 2 | 9.4 -3.4 .9 7 -1 4 -.21
MIT | 2 | 3.4 2.0 1.2 -49 -5 29 -.08
NGS | 2 | 4.4 -2.2 3.1 -40 11 38 -.05
SIO | 2 | -.2 1.6 17.0 3 -26 6 -.49
COD | 3 | .1 -.3 .6 6 20 17 -.15
EMR | 3 | 4.5 -7.6 11.1 -26 31 18 .26
ESA | 3 | .8 -.6 -.7 -10 32 78 -.17
GFZ | 3 | .9 .1 -.7 23 -7 63 -.04
GRG | 3 | 3.9 -1.2 11.6 13 3 98 .20
JPL | 3 | 9.4 -3.2 8.9 7 -4 4 -.22
MIT | 3 | 1.2 3.7 4.4 -18 5 -3 .13
NGS | 3 | 1.8 -9.1 6.0 -55 39 22 .21
SIO | 3 | .3 .9 17.2 -19 -40 8 -.14
COD | 4 | .1 -.5 1.0 -9 16 15 -.27
EMR | 4 | 8.2 -4.7 11.6 -40 50 -27 .04
ESA | 4 | .8 -.5 -.2 -11 24 88 -.07
GFZ | 4 | .7 -.1 .0 23 -14 79 -.19
GRG | 4 | -1.0 .4 30.5 41 5 92 -.35
JPL | 4 | 10.7 1.9 18.3 3 2 8 -.08
MIT | 4 | -3.3 -.2 8.2 -27 -8 22 .02
NGS | 4 | 1.5 -.3 11.7 -2 54 2 -.02
SIO | 4 | -4.8 -1.1 26.7 -19 -5 34 -.35
COD | 5 | .4 .5 .5 19 1 -3 -.34
EMR | 5 | 1.7 -4.8 16.7 -28 9 -40 .06
ESA | 5 | .9 .0 -.3 12 18 79 -.34
GFZ | 5 | .7 -.0 -.2 24 -13 75 -.15
GRG | 5 | 5.2 -.4 21.7 60 -32 92 -.12
JPL | 5 | 7.9 -2.5 18.8 18 25 9 -.35
MIT | 5 | -1.9 -.2 8.2 -10 4 7 .06
NGS | 5 | 3.1 -1.9 24.3 32 41 18 .02
SIO | 5 | .3 -.1 19.7 17 -23 -1 -.12
COD | 6 | -.3 .3 .8 3 26 -10 -.16
EMR | 6 | 4.9 -1.3 8.7 -17 13 -2 .14
ESA | 6 | -.2 -.4 -.6 -6 25 80 -.10
GFZ | 6 | -.0 -.1 -.6 11 10 72 .03
GRG | 6 | 2.8 -.9 17.7 42 -20 97 .29
JPL | 6 | 11.4 -2.3 21.0 15 10 14 -.20
MIT | 6 | -2.1 2.8 5.7 12 -8 16 .04
NGS | 6 | -2.5 3.6 16.5 37 79 0 -.05
SIO | 6 | .6 1.7 20.8 1 6 10 -.15
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 1.2092.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2092.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 2.2092.[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 3.2092.[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 5.2092.0-6). 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 2092 summary. (Feb 09, 2020 - Feb 15, 2020)
Table 1.2092.a GPS week: 2092 MJD: 58888.000-58894.000
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 252| 0 0 0 -1 6 9 -.04 8 8 | -700 67 7 102
| 0 0 4 21 8 8 .04 | 164 254
emr 79| 1 -2 1 -18 7 12 .19 13 13 | 142645 461 16 132
| 0 0 1 15 11 20 .02 | 622 825
esa 149| 0 0 0 -7 -6 26 -.04 10 10 | -1646 1307 7 73
| 0 0 1 10 10 16 .03 | 390 145
gfz 180| 0 1 -1 -10 0 -13 .08 9 9 | -108 -54 12 110
| 0 0 4 21 17 8 .02 | 362 610
grg 95| 0 0 -1 -8 -8 10 -.15 17 13 | -66 229 10 136
| 0 0 6 16 25 66 .03 | 206 435
igr n/a| 0 0 -2 -15 -2 -43 .03 4 4 | 5100 663 10 65
| 0 0 3 12 9 9 .01 | 1113 764
jpl 80| 0 0 4 23 15 3 .19 8 8 | 213232 345 9 90
| 0 1 1 23 27 26 .01 | 441 782
mit 384| 0 0 -3 18 -3 -20 -.08 13 13 | -361 121 60 1726
| 0 0 2 28 26 156 .01 | 126 192
ngs 205| 0 0 1 9 -14 -29 -.05 9 8 | -692 49 1098 2148
| 0 0 4 39 33 22 .03 | 128 208
sio 451| 0 0 -5 1 -13 -14 -.18 17 16 | --- --- --- ---
| 0 1 4 30 19 16 .07 | --- ---
Table 1.2092.b GPS week : 2092 MJD: 58888.000-58894.000
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 4 4 3 |
2 | 4 3 3 4 4 4 4 |
3 | 4 4 4 4 4 4 5 |
4 | 7 7 7 7 8 9 10 |
5 | 5 4 4 4 5 4 5 |
6 | 3 3 3 3 4 4 4 |
7 | 3 3 3 3 3 4 3 |
8 | 4 4 4 4 4 4 4 |
9 | 3 3 3 3 4 4 4 |
10 | 4 4 4 4 5 5 4 |
11 | 4 4 4 4 5 4 4 |
12 | 4 4 4 4 4 5 5 |
13 | 4 4 4 4 4 5 4 |
14 | 4 3 4 3 4 4 4 |
15 | 4 4 4 3 4 5 4 |
16 | 5 5 5 4 4 4 4 |
17 | 3 3 3 3 4 4 4 |
18 | 5 10 5 5 5 6 5 |
19 | 4 4 3 4 4 5 4 |
20 | 4 3 3 4 4 4 4 |
21 | 4 3 3 4 4 4 4 |
22 | 3 3 3 3 4 4 4 |
23 | 5 5 4 4 5 5 5 |
24 | 3 4 3 3 4 4 4 |
25 | 4 3 4 3 4 4 4 |
26 | 3 4 4 4 0 5 4 |
27 | 4 4 4 4 9 5 4 |
28 | 3 3 3 3 3 4 4 |
29 | 4 4 4 3 4 4 4 |
30 | 3 3 3 3 3 4 3 |
31 | 3 3 3 3 4 4 4 |
32 | 3 3 4 3 4 4 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 2.2092.0 GPS week: 2092 Day: 0 MJD: 58888.000
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| 0 0 -2 -37 -6 12 -.07 8 8 | -592 -151 7 106
emr 80| 1 -3 0 -26 -6 -12 .19 13 13 | 141807 456 20 144
esa 149| 0 0 1 -26 -11 2 .00 10 11 | -2009 1563 7 67
gfz 183| 0 1 2 -37 0 -17 .06 9 8 | 484 -555 12 106
grg 100| 0 -1 -8 -3 -49 120 -.14 17 15 | 152 38 12 125
igr n/a| 0 0 0 -33 -16 -59 .02 4 4 | 3675 589 9 58
jpl 80| 0 0 4 7 52 -37 .20 9 9 | 212822 487 11 85
mit 384| 0 0 0 23 -42 43 -.08 7 7 | -451 18 26 1608
ngs 208| 0 0 -1 76 55 -56 -.04 10 9 | -603 -141 965 2130
sio 455| 0 0 -1 49 -11 -21 -.21 16 15 | --- --- --- ---
Table 2.2092.1 GPS week: 2092 Day: 1 MJD: 58889.000
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 253| 0 -1 2 16 6 14 -.12 8 8 | -634 -7 6 92
emr 78| 1 -2 -1 6 15 -4 .20 13 13 | 141907 2251 18 136
esa 149| 0 0 0 5 8 20 -.04 10 10 | -1051 1390 7 70
gfz 185| 0 2 4 -11 -27 -23 .09 9 9 | -556 1177 12 84
grg 101| 1 -2 -10 19 -15 67 -.15 13 13 | -330 1142 13 145
igr n/a| -1 0 0 -26 7 -55 .05 4 4 | 3815 2269 10 54
jpl 80| -1 1 4 -2 33 14 .21 8 8 | 212943 1986 7 66
mit 384| 0 0 -2 -19 9 -15 -.08 6 6 | -207 424 83 1648
ngs 209| 1 0 -3 24 -29 -13 -.00 9 8 | -647 -3 1412 2156
sio 458| 0 0 -1 -18 -28 -21 -.08 16 16 | --- --- --- ---
Table 2.2092.2 GPS week: 2092 Day: 2 MJD: 58890.000
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| 0 0 3 4 2 24 -.01 9 9 | -844 397 7 93
emr 80| 0 -3 1 -8 11 12 .22 14 13 | 143079 -75 16 123
esa 149| 0 0 0 -12 -5 49 -.03 10 10 | -1354 1157 8 73
gfz 177| 0 0 0 11 -18 -10 .08 9 10 | -35 22 13 100
grg 95| 0 0 -2 1 -24 39 -.16 11 11 | 191 -212 10 123
igr n/a| 0 0 0 -2 -9 -37 .04 4 4 | 5188 -13 10 74
jpl 80| 0 0 2 29 -4 -15 .19 8 8 | 213939 -452 8 66
mit 384| 0 0 -2 -7 24 -46 -.07 6 6 | -228 -80 76 1751
ngs 205| 0 0 0 -3 -23 4 -.02 9 8 | -800 333 907 2081
sio 445| 1 0 -4 -2 16 10 -.12 17 15 | --- --- --- ---
Table 2.2092.3 GPS week: 2092 Day: 3 MJD: 58891.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 0 -1 3 13 8 3 -.04 8 8 | -645 48 8 105
emr 80| 1 0 2 -40 12 41 .18 13 13 | 142288 495 17 126
esa 149| 0 0 -1 -11 -1 26 -.03 9 9 | -2137 1384 7 71
gfz 181| 0 1 -1 -42 11 -12 .07 9 8 | -112 -435 10 144
grg 94| 0 0 -1 -24 11 -22 -.12 10 10 | -329 262 8 137
igr n/a| 0 0 -2 -21 3 -36 .03 3 3 | 4536 913 10 69
jpl 80| 0 0 4 22 -18 -8 .18 8 8 | 212743 346 10 76
mit 384| -1 0 -3 29 13 49 -.09 8 8 | -299 -38 54 1745
ngs 206| 0 0 0 38 -12 -31 -.05 8 7 | -649 51 1322 2434
sio 451| 0 0 -3 -13 -26 -24 -.13 17 16 | --- --- --- ---
Table 2.2092.4 GPS week: 2092 Day: 4 MJD: 58892.000
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 -1 -2 17 1 0 -.04 9 8 | -559 -185 8 96
emr 80| 3 -1 2 -25 9 3 .17 13 13 | 143214 68 15 119
esa 149| 0 -1 -1 1 1 37 -.03 11 10 | -1607 1188 9 71
gfz 176| -2 0 -4 6 23 -21 .11 10 12 | 198 -584 14 100
grg 93| 0 0 9 -6 30 -46 -.20 39 14 | -69 248 9 115
igr n/a| -1 0 -5 -5 3 -43 .04 5 5 | 6006 286 12 69
jpl 80| 1 1 4 0 -7 32 .20 9 9 | 213577 15 11 125
mit 384| 0 1 -5 50 -17 135 -.07 20 20 | -408 74 74 1839
ngs 202| 1 0 0 -22 -22 -58 -.07 9 8 | -568 -174 951 1892
sio 449| 0 1 -10 -10 -32 -25 -.22 18 19 | --- --- --- ---
Table 2.2092.5 GPS week: 2092 Day: 5 MJD: 58893.000
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 -6 3 18 3 -.02 9 9 | -619 -73 6 111
emr 80| 0 -1 2 -11 21 11 .18 12 12 | 143155 179 14 146
esa 149| 0 -1 0 -1 -17 13 -.09 10 10 | -1906 1261 9 78
gfz 181| 0 1 -8 0 3 -4 .09 9 9 | -405 -130 13 100
grg 92| 1 0 3 -11 -12 -32 -.12 14 13 | -6 153 11 156
igr n/a| -1 0 -5 -16 6 -38 .03 4 4 | 6236 337 12 69
jpl 80| 0 -1 7 55 40 33 .18 8 8 | 213457 10 10 102
mit 384| 0 0 -5 -2 20 38 -.07 30 30 | -560 108 49 1747
ngs 204| 0 1 7 -34 -53 -20 -.09 9 9 | -645 -54 1207 2405
sio 450| -1 2 -7 -35 -22 -27 -.26 17 15 | --- --- --- ---
Table 2.2092.6 GPS week: 2092 Day: 6 MJD: 58894.000
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 249| 0 0 -3 -25 14 5 .00 8 8 | -1011 445 7 112
emr 80| 0 -3 0 -23 -10 37 .18 13 13 | 143068 -144 13 130
esa 149| 0 0 -2 -8 -19 38 -.08 10 10 | -1459 1211 8 82
gfz 181| 0 0 0 0 7 -2 .06 9 9 | -336 121 12 142
grg 93| 0 0 0 -31 -2 -51 -.15 13 13 | -74 -28 10 154
igr n/a| 0 0 -6 0 -11 -37 .02 4 4 | 6249 266 11 63
jpl 80| -1 0 4 49 9 5 .19 8 8 | 213147 25 12 111
mit 384| -1 0 -7 53 -31 -350 -.06 16 16 | -379 347 61 1746
ngs 203| 1 1 6 -13 -16 -32 -.06 9 8 | -934 334 924 1943
sio 451| 0 1 -11 38 7 6 -.27 17 15 | --- --- --- ---
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 3.2092.0 GPS week: 2092 Day: 0 MJD: 58888.000
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 9 10 8 11 4 9 7 9 10 3 | 33 39 35 37 35 35 39 37 32 34 35
2 | 9 11 9 10 17 4 7 5 7 18 3 | 27 26 25 30 26 24 26 24 26 26 25
3E | 8 13 17 9 13 5 8 6 17 11 4 | 27 25 23 28 29 25 28 27 32 23 25
X4 | 8 --- 15 11 --- 7 24 8 11 43 7 | 68 --- 60 72 --- 66 64 71 70 75 68
5E | 10 12 12 10 48 3 9 7 12 17 5 | 30 31 30 29 44 29 31 27 34 24 28
6 | 7 11 10 8 13 4 10 6 7 9 3 | 52 53 50 48 50 49 51 48 48 50 49
7 | 5 9 7 8 11 3 8 6 10 16 3 | 22 27 25 25 24 23 29 24 27 21 24
8 | 6 9 15 8 16 4 8 8 12 8 3 | 24 27 27 23 32 25 26 26 27 22 24
9 | 7 13 10 5 12 3 8 6 14 8 3 | 48 52 48 49 48 48 52 47 49 50 48
10E | 8 13 17 12 15 3 10 11 11 11 4 | 22 21 19 20 26 20 23 20 24 19 19
11 | 6 10 18 8 16 3 9 8 8 16 3 | 21 27 24 23 23 22 28 20 23 20 21
12 | 8 19 7 9 25 5 10 5 12 20 4 | 34 40 35 37 42 36 39 37 38 32 35
13 | 8 11 10 10 18 4 10 6 12 18 3 | 33 43 30 29 44 34 40 38 41 38 35
14 | 8 9 7 9 12 4 8 8 9 27 3 | 41 44 42 46 42 42 41 41 41 51 41
15 | 8 10 10 7 19 3 10 6 12 16 3 | 41 43 41 39 38 40 43 39 42 42 40
16 | 6 23 9 11 15 5 8 13 10 18 4 | 34 41 34 40 39 34 33 36 40 31 35
17 | 7 8 5 7 14 3 10 7 6 15 3 | 32 32 31 34 34 30 31 29 32 27 30
X18 | 16 16 15 10 --- 6 9 11 12 --- 5 | 34 36 29 40 --- 33 35 35 40 --- 33
19 | 7 13 7 11 13 3 9 7 6 18 3 | 32 33 35 34 36 31 32 33 32 35 32
20E | 12 13 8 7 19 4 9 9 10 14 3 | 105 105 106 105 110 106 104 105 107 103 105
21 | 8 11 7 8 17 3 8 9 8 17 3 | 24 27 22 23 25 23 25 26 23 30 23
22E | 6 14 8 9 13 4 6 5 11 12 3 | 33 36 35 34 34 32 32 31 30 35 32
23 | 10 20 9 8 13 4 10 8 14 36 5 | 23 25 19 27 23 21 22 25 23 33 20
24 | 8 8 6 8 12 4 9 8 9 16 3 | 33 36 34 33 33 31 36 29 34 42 33
25 | 10 12 16 12 14 4 6 5 13 10 3 | 32 34 36 34 40 31 35 31 32 33 33
26 | 6 14 10 7 14 3 8 5 10 12 3 | 22 26 23 22 26 23 24 22 24 26 24
27 | 8 11 15 6 15 3 9 10 10 8 3 | 580 576 578 580 575 577 577 575 577 577 577
28 | 7 8 7 10 12 3 8 8 8 15 3 | 34 32 30 34 36 32 32 33 34 34 32
29 | 6 17 7 7 15 4 10 7 10 18 3 | 34 31 31 32 39 30 30 32 30 31 31
30 | 9 10 6 9 11 3 10 9 8 9 3 | 37 44 41 38 37 38 44 38 38 39 39
31 | 7 11 6 7 14 3 9 5 7 15 3 | 24 28 25 26 27 26 29 25 28 28 25
32 | 8 10 8 7 13 3 9 5 6 14 3 | 27 29 29 27 31 27 31 25 28 30 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 10 9 17 4 9 7 10 16 |T 51 53 51 53 54 51 53 51 53 53 51
WRMS | 8 12 11 8 15 4 9 7 9 15 |NE 53 55 53 54 56 53 55 53 54 56 53
MEDI | 8 11 9 8 14 4 9 7 10 15 |MD 33 33 31 34 35 31 32 31 32 33 32
Table 3.2092.1 GPS week: 2092 Day: 1 MJD: 58889.000
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 11 8 12 4 6 5 10 10 3 | 20 29 24 28 27 26 29 26 22 28 24
2 | 10 10 10 7 14 4 7 5 7 19 3 | 18 21 22 25 15 19 22 20 21 21 19
3E | 9 10 19 13 15 6 9 6 6 8 3 | 29 26 23 32 35 24 27 23 28 25 25
X4 | 9 --- 14 11 --- 7 24 7 10 46 7 | 49 --- 46 52 --- 49 47 50 47 63 49
5E | 7 11 10 13 18 5 6 4 9 17 3 | 29 30 29 25 27 27 30 27 31 29 27
6 | 7 8 9 6 11 3 7 4 10 6 2 | 31 36 34 34 31 34 35 32 32 35 33
7 | 7 9 8 8 10 3 6 6 10 17 3 | 19 20 19 24 18 19 22 17 24 18 18
8 | 7 11 15 10 15 5 8 8 10 8 3 | 17 23 21 18 26 21 22 21 21 20 19
9 | 8 10 9 8 10 4 7 5 9 7 2 | 36 41 39 38 40 38 42 36 37 40 37
10E | 6 15 16 9 11 4 8 8 10 9 3 | 18 22 17 18 24 19 22 19 21 21 18
11 | 7 10 18 11 12 4 10 7 8 15 3 | 16 25 22 18 17 17 26 17 15 14 16
12 | 9 19 7 7 21 3 10 4 10 19 4 | 27 35 28 30 32 29 33 29 32 24 28
13 | 9 15 9 7 14 4 10 6 10 21 3 | 29 37 27 30 35 30 36 31 35 29 30
14 | 6 11 7 7 11 3 6 5 7 26 3 | 36 38 35 38 37 37 35 37 35 45 36
15 | 10 11 7 9 17 3 7 6 12 15 3 | 32 30 29 32 30 30 34 27 29 31 29
16 | 9 26 8 12 14 5 7 12 9 19 4 | 30 39 29 37 33 30 30 30 34 25 30
17 | 8 14 6 8 14 3 9 6 10 15 3 | 25 27 23 28 28 25 29 24 26 24 24
X18 | 32 19 15 13 --- 8 12 13 46 --- 9 | 37 33 29 39 --- 35 32 33 63 --- 34
19 | 6 16 6 10 13 3 8 6 10 18 3 | 24 24 25 24 27 24 26 23 23 25 23
20E | 9 13 7 8 14 6 6 6 8 14 3 | 73 77 77 76 83 77 77 75 81 74 76
21 | 7 12 7 5 12 4 8 6 8 19 3 | 17 23 17 19 16 17 22 17 17 21 17
22E | 8 14 6 9 14 5 6 5 7 10 3 | 28 32 28 30 28 29 28 26 30 29 28
23 | 9 20 7 7 12 4 9 5 11 35 4 | 19 21 18 21 22 17 19 17 19 29 16
24 | 8 8 6 10 11 3 8 8 13 16 3 | 22 35 26 30 26 26 34 21 30 37 27
25 | 6 10 16 8 13 3 6 4 9 8 3 | 22 26 28 25 29 23 27 21 23 24 23
26 | 8 19 11 8 13 4 7 6 8 8 3 | 19 25 21 19 23 21 23 19 20 21 20
27 | 11 11 16 8 14 3 8 9 8 10 3 | 445 440 443 444 440 441 441 441 444 445 442
28 | 7 10 7 9 11 3 7 8 11 16 3 | 26 27 24 28 28 25 28 25 23 28 24
29 | 9 17 5 8 15 4 6 6 9 16 3 | 24 22 21 24 30 23 23 23 25 24 22
30 | 8 10 5 8 14 3 8 6 15 6 3 | 23 35 30 28 25 28 36 28 34 31 29
31 | 5 12 8 8 11 3 7 5 6 16 3 | 18 24 20 20 21 21 24 18 21 22 19
32 | 7 8 11 7 11 2 7 5 7 9 2 | 19 26 23 21 27 21 27 20 21 25 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 9 13 4 8 6 9 16 |T 39 43 40 42 42 40 43 39 42 42 40
WRMS | 8 13 10 9 13 4 8 6 8 16 |NE 40 44 41 43 43 41 44 40 43 44 41
MEDI | 8 11 8 8 13 4 7 6 9 15 |MD 24 27 25 28 27 25 28 24 26 25 24
Table 3.2092.2 GPS week: 2092 Day: 2 MJD: 58890.000
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 7 12 4 8 5 6 10 2 | 45 45 42 39 41 40 42 44 41 39 41
2 | 6 12 12 9 10 4 6 4 10 19 3 | 21 22 24 26 17 22 21 21 22 22 20
3E | 8 15 16 9 9 5 10 6 9 10 3 | 20 24 17 22 19 18 20 15 19 18 17
X4 | 10 --- 13 11 --- 6 23 8 13 50 7 | 45 --- 46 54 --- 48 48 51 53 57 49
5E | 9 18 10 13 10 4 8 4 8 18 3 | 31 28 29 29 28 28 29 27 30 31 27
6 | 8 9 10 10 11 4 9 5 7 8 3 | 49 49 49 49 47 47 50 48 43 44 47
7 | 6 9 6 5 7 3 7 5 6 17 2 | 24 26 23 26 21 23 25 20 23 20 22
8 | 9 11 14 10 14 4 9 8 9 10 3 | 24 27 27 26 28 24 26 27 26 26 25
9 | 14 12 9 5 7 5 9 5 11 8 3 | 46 50 45 46 45 46 48 41 44 49 45
10E | 9 11 15 13 12 5 8 9 10 10 3 | 22 23 17 24 25 20 22 21 23 21 20
11 | 6 10 17 8 13 4 9 6 5 16 3 | 15 25 17 16 16 16 24 18 17 16 16
12 | 13 20 7 8 19 4 9 6 9 18 4 | 27 32 28 30 32 28 31 30 29 26 27
13 | 9 16 8 9 10 3 11 5 8 21 3 | 27 36 28 22 28 27 35 31 26 31 27
14 | 10 9 8 10 10 4 8 6 6 26 3 | 34 37 32 38 33 35 36 42 37 39 35
15 | 9 14 7 10 12 3 9 6 13 17 3 | 34 36 30 31 27 31 31 26 37 31 30
16 | 12 31 7 11 10 5 8 10 8 19 4 | 33 42 26 34 30 27 29 31 29 25 29
17 | 8 9 9 10 10 3 8 5 9 17 3 | 27 29 27 31 27 26 28 24 29 24 26
X18 | 18 15 71 10 --- 6 8 7 9 --- 5 | 29 27 63 25 --- 25 27 26 22 --- 24
19 | 7 13 9 10 11 3 8 6 8 17 3 | 26 25 27 30 22 24 25 22 22 27 24
20 | 10 15 6 9 10 4 7 7 8 15 3 | 86 89 88 90 85 89 89 87 89 89 88
21 | 6 10 5 9 10 3 7 6 7 16 3 | 21 23 19 23 19 20 24 22 20 24 20
22E | 6 11 6 12 9 3 8 5 8 13 3 | 30 33 31 31 30 31 32 29 31 33 30
23 | 10 20 7 6 10 5 8 6 12 36 4 | 17 19 14 19 17 16 17 16 16 32 14
24 | 9 10 7 8 8 5 8 7 9 18 3 | 35 43 38 40 34 37 43 32 37 47 38
25 | 11 12 18 11 8 4 9 5 9 10 3 | 23 31 30 27 26 25 26 21 25 27 24
26 | 14 23 10 5 13 5 9 5 14 12 4 | 24 27 20 20 21 19 21 19 19 21 20
27 | 10 13 16 9 12 5 9 10 9 11 3 | 630 630 631 631 626 630 631 626 629 630 629
28 | 5 8 6 11 8 4 8 7 12 14 3 | 25 27 24 28 26 26 28 26 24 28 25
29 | 7 19 6 13 14 5 7 6 7 17 3 | 24 23 19 29 24 22 21 21 24 23 22
30 | 6 9 7 6 9 3 10 6 8 12 2 | 40 44 40 39 35 38 42 35 38 41 39
31 | 7 11 8 7 7 2 8 4 7 18 3 | 19 24 17 19 17 19 27 23 20 21 19
32 | 8 9 10 14 9 3 10 5 9 14 3 | 27 31 28 34 29 26 29 22 26 35 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 10 9 11 4 8 6 9 17 |T 49 52 49 50 49 48 50 48 49 51 48
WRMS | 9 13 10 10 11 4 8 6 8 15 |NE 51 55 52 53 51 50 53 50 51 54 50
MEDI | 9 12 8 9 10 4 8 6 9 16 |MD 27 29 28 29 27 26 28 26 26 28 26
Table 3.2092.3 GPS week: 2092 Day: 3 MJD: 58891.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 8 9 9 8 3 7 8 7 11 3 | 39 42 39 39 36 38 43 40 38 40 39
2 | 9 9 10 9 9 3 6 7 8 23 3 | 25 25 25 29 22 24 26 23 26 26 24
3E | 11 11 14 10 17 5 12 9 8 9 4 | 27 25 23 24 32 24 28 20 26 22 23
X4 | 10 --- 14 13 --- 6 22 7 8 46 7 | 40 --- 37 51 --- 42 41 47 44 47 42
5E | 8 20 8 8 10 4 9 6 8 16 3 | 29 28 27 31 27 28 29 27 31 33 27
6 | 7 10 9 8 8 2 7 8 7 9 2 | 36 39 38 36 34 36 40 35 37 37 36
7 | 8 11 7 8 8 2 6 8 9 17 3 | 20 23 19 22 19 20 21 18 23 17 19
8 | 9 11 15 8 14 3 9 9 7 10 3 | 26 27 30 27 31 26 27 25 26 25 26
9 | 8 10 10 7 8 4 8 6 7 9 2 | 24 29 24 24 23 22 27 20 22 27 23
10E | 9 13 15 9 10 5 9 9 8 11 3 | 22 24 19 22 22 20 24 21 23 26 20
11 | 8 12 16 10 11 4 10 8 6 16 3 | 22 29 22 21 22 21 30 23 21 21 21
12 | 7 18 7 8 17 3 6 5 8 23 3 | 25 29 25 31 33 26 26 26 29 21 26
13 | 7 13 7 10 7 4 10 7 6 23 3 | 20 31 21 22 25 22 31 25 25 30 23
14 | 6 11 6 7 6 3 5 7 9 26 3 | 20 26 23 25 24 23 24 25 26 30 22
15 | 8 16 7 5 11 3 8 6 7 19 3 | 28 32 24 25 26 25 28 25 26 26 25
16 | 9 22 7 14 12 4 9 10 7 21 4 | 22 32 24 33 25 24 25 28 28 24 25
17 | 8 9 6 10 12 3 9 10 5 17 3 | 28 28 25 29 24 27 28 25 27 22 26
X18 | 12 11 14 15 --- 5 8 9 13 --- 5 | 28 27 26 34 --- 25 26 26 24 --- 24
19 | 10 13 7 11 9 3 9 10 7 20 3 | 27 27 26 30 25 26 26 25 25 25 25
20 | 11 13 7 5 14 3 7 7 9 16 3 | 45 41 44 45 46 45 43 41 45 42 43
21 | 8 13 4 8 11 3 7 9 11 21 3 | 25 28 24 26 26 23 26 26 24 31 24
22E | 9 13 6 12 8 4 6 6 7 12 3 | 28 28 26 26 26 26 27 27 27 28 25
23 | 7 22 7 9 9 3 8 7 9 36 4 | 17 20 17 20 18 17 17 17 19 30 15
24 | 9 9 7 10 11 2 9 7 7 17 3 | 23 32 28 25 25 25 33 23 25 37 26
25 | 7 11 14 8 12 3 8 4 6 10 3 | 22 27 23 24 24 22 25 22 23 24 22
26 | 8 16 10 7 13 4 9 8 8 12 3 | 19 25 22 22 27 20 23 20 21 26 20
27 | 10 14 14 8 10 3 9 11 7 10 3 | 332 331 330 328 327 329 332 330 332 328 330
28 | 8 8 8 8 10 3 6 11 9 16 3 | 24 26 22 27 23 24 24 26 25 24 23
29 | 8 16 5 6 10 4 6 7 8 16 3 | 25 24 22 28 27 23 23 24 25 22 23
30 | 9 10 6 7 10 2 7 10 7 7 3 | 30 39 35 33 33 32 36 32 29 33 32
31 | 5 13 5 7 5 3 6 6 6 18 2 | 17 23 18 24 19 19 24 19 19 18 19
32 | 8 10 11 8 5 3 8 6 8 11 3 | 21 25 22 20 21 20 25 19 20 25 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 9 9 10 3 8 8 8 17 |T 35 38 35 37 36 35 37 35 36 37 34
WRMS | 8 13 9 8 10 3 8 8 7 16 |NE 36 40 36 39 37 36 39 36 37 39 36
MEDI | 8 12 7 8 10 3 8 7 7 16 |MD 25 28 24 26 25 24 26 25 25 26 24
Table 3.2092.4 GPS week: 2092 Day: 4 MJD: 58892.000
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 10 9 14 4 6 21 9 10 3 | 45 48 45 41 41 42 45 56 44 43 43
2 | 10 10 8 9 11 5 7 19 6 18 3 | 20 23 21 24 21 20 21 30 20 19 19
3E | 8 10 14 10 13 6 10 20 8 11 4 | 22 24 20 22 28 21 24 31 20 25 21
X4 | 9 --- 17 14 --- 6 23 19 12 50 8 | 49 --- 43 57 --- 48 47 53 56 55 49
5E | 8 15 10 18 15 5 10 17 9 18 4 | 27 26 27 27 31 26 29 33 26 28 25
6 | 10 8 12 7 14 5 6 20 6 9 3 | 43 48 42 37 42 41 45 53 44 41 42
7 | 7 8 7 6 8 3 6 23 8 18 3 | 19 21 19 22 18 19 22 24 21 16 18
8 | 9 10 16 12 14 5 8 23 10 13 4 | 27 31 34 26 27 28 30 39 29 30 28
9 | 8 8 11 9 11 4 6 19 10 10 3 | 36 40 39 40 37 38 40 31 42 40 38
10E | 9 13 16 12 20 5 8 21 7 14 4 | 20 21 18 17 28 20 23 28 21 25 19
11 | 8 10 19 11 16 3 7 23 10 12 4 | 20 28 22 21 18 20 28 32 20 19 20
12 | 10 21 7 8 19 5 7 18 5 21 4 | 24 32 25 29 31 25 28 34 27 25 25
13 | 6 10 10 11 9 5 10 17 7 27 4 | 31 37 29 31 29 31 38 42 34 34 32
14 | 7 10 9 7 10 4 6 19 9 23 3 | 39 40 39 41 40 40 41 48 39 42 39
15 | 7 14 7 6 14 5 7 16 10 20 3 | 32 36 30 30 34 29 34 28 31 29 30
16 | 6 18 9 10 15 6 7 19 7 22 4 | 27 31 25 29 27 24 27 34 28 28 26
17 | 7 11 6 8 12 3 8 20 7 16 3 | 28 27 24 27 22 26 27 30 25 22 24
X18 | 13 10 14 13 --- 6 8 23 8 --- 5 | 28 27 24 27 --- 24 27 35 28 --- 24
19 | 8 14 6 11 15 4 7 21 9 17 4 | 25 24 23 27 25 24 23 32 24 22 23
20 | 11 12 9 8 15 4 7 17 7 15 3 | 72 71 75 71 71 71 70 66 71 72 71
21 | 9 12 7 7 11 4 7 19 9 21 3 | 25 25 21 23 23 21 24 31 22 23 21
22E | 7 8 7 17 14 6 6 19 6 12 3 | 34 34 31 35 33 32 33 32 32 31 32
23 | 8 24 8 10 10 3 8 20 10 34 5 | 18 18 16 21 15 16 16 26 18 28 13
24 | 10 10 6 8 10 3 10 18 11 19 3 | 22 32 25 26 25 25 32 22 24 34 24
25 | 9 9 15 8 12 6 6 14 7 14 3 | 21 23 21 22 19 19 20 23 16 23 19
X26 | 2 --- --- --- --- 45 --- --- --- --- 0 | 106 --- --- --- --- 31 --- --- --- --- 106
27 | 15 30 20 21 202 13 30 26 20 27 9 | 987 987 983 986 923 981 988 974 981 982 984
28 | 7 9 8 8 11 2 6 23 7 13 3 | 26 25 22 27 23 24 23 27 23 25 22
29 | 6 17 6 7 15 6 7 17 9 18 3 | 23 19 16 22 22 19 18 27 22 17 18
30 | 8 8 8 9 9 3 6 23 6 9 3 | 31 37 34 33 29 31 36 28 35 33 32
31 | 7 13 6 6 8 4 7 17 10 19 3 | 21 24 20 20 20 20 24 29 20 23 20
32 | 9 10 11 8 8 4 8 18 7 11 3 | 20 26 24 22 26 21 26 24 19 24 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 10 39 5 9 20 9 18 |T 61 62 59 60 59 58 61 64 60 61 60
WRMS | 8 13 10 12 14 5 9 20 8 19 |NE 66 68 64 65 64 62 66 69 65 67 65
MEDI | 8 10 9 9 13 5 7 19 8 17 |MD 27 27 25 27 27 25 28 31 26 28 24
Table 3.2092.5 GPS week: 2092 Day: 5 MJD: 58893.000
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 8 9 8 9 4 7 31 6 13 3 | 65 71 66 68 67 67 71 75 64 66 67
2 | 9 10 9 9 13 5 6 28 9 19 4 | 21 19 21 26 19 18 19 35 20 17 18
3E | 9 10 12 11 16 4 10 32 10 12 4 | 22 25 19 18 29 20 24 34 21 22 20
X4 | 13 --- 17 13 --- 6 23 29 9 52 9 | 50 --- 43 55 --- 47 44 61 44 62 47
5E | 9 13 10 8 18 5 8 26 11 17 4 | 34 34 32 33 33 33 35 39 36 34 32
6 | 8 8 9 8 11 4 7 31 11 10 3 | 81 83 83 83 83 81 83 88 81 83 82
7 | 8 11 8 7 13 3 7 35 10 17 4 | 23 26 24 26 23 23 27 39 25 19 23
8 | 12 9 16 10 13 4 8 31 10 9 4 | 35 39 36 36 39 37 38 46 38 33 35
9 | 8 10 10 7 14 3 7 31 7 11 3 | 55 58 55 56 53 56 57 62 54 57 56
10E | 9 14 16 12 16 5 10 29 9 9 4 | 24 23 17 21 30 21 24 32 23 24 21
11 | 7 10 16 9 11 4 8 31 7 15 4 | 20 29 19 22 23 21 29 38 21 17 21
12 | 6 17 6 15 17 5 8 28 9 17 4 | 26 31 26 31 33 26 29 38 31 21 26
13 | 10 11 9 9 20 4 10 26 13 25 4 | 29 31 25 29 28 27 32 36 28 31 26
14 | 10 10 7 7 11 4 7 28 9 25 4 | 28 31 26 31 31 29 28 40 29 38 27
15 | 9 17 10 12 16 4 10 26 9 18 4 | 35 37 32 34 31 31 37 44 33 36 33
16 | 9 16 8 8 12 6 7 28 8 20 4 | 24 28 24 29 26 23 27 35 28 23 24
17 | 9 7 7 5 13 4 7 34 11 17 3 | 29 25 22 26 21 24 26 33 21 16 22
X18 | 20 11 14 13 --- 6 8 30 9 --- 5 | 37 29 24 30 --- 25 29 40 24 --- 26
19 | 9 13 7 13 13 5 6 32 12 20 4 | 23 20 23 27 22 22 22 35 22 22 21
20 | 11 12 7 8 17 3 7 28 10 13 4 | 68 71 71 74 66 71 72 75 74 70 71
21 | 8 10 10 10 13 5 6 31 9 20 4 | 21 24 18 22 22 19 23 35 22 22 19
22 | 7 9 6 12 18 5 6 30 8 14 4 | 32 32 33 31 35 31 33 40 33 34 31
23 | 8 23 8 9 14 5 9 29 9 36 5 | 18 17 16 22 20 18 17 37 18 32 15
24 | 8 8 8 6 13 5 9 25 9 15 3 | 57 60 61 57 53 56 61 58 57 63 58
25 | 9 11 16 7 11 5 7 27 7 10 4 | 36 36 35 37 35 34 36 38 34 34 35
X26 | 6 13 12 10 --- 5 --- 26 --- 11 5 | 18 23 17 17 --- 17 --- 30 --- 20 20
27 | 11 14 17 10 11 4 8 33 9 10 4 | 568 562 566 565 570 565 561 578 568 569 565
28 | 6 10 9 8 12 3 7 36 11 17 4 | 29 29 25 31 27 27 25 36 24 28 25
29 | 8 19 6 7 17 6 9 29 11 15 4 | 24 21 20 24 27 21 18 35 22 21 20
30 | 9 10 7 7 10 5 6 35 10 8 3 | 65 69 66 65 66 64 68 70 65 64 66
31 | 7 12 5 7 10 4 7 26 9 18 3 | 20 20 13 17 18 16 20 30 20 21 16
32 | 10 10 10 10 11 3 9 28 7 9 3 | 32 34 33 32 35 32 37 37 31 31 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 10 9 14 4 8 30 9 17 |T 51 52 49 52 53 50 53 60 51 52 50
WRMS | 9 12 10 9 13 4 8 30 9 15 |NE 54 55 52 55 57 52 56 64 54 55 52
MEDI | 9 11 9 9 13 4 7 29 9 15 |MD 29 31 25 31 31 27 29 38 29 31 26
Table 3.2092.6 GPS week: 2092 Day: 6 MJD: 58894.000
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 | 9 8 9 8 11 3 6 17 6 10 3 | 68 71 66 68 69 68 71 70 67 67 69
2 | 8 11 11 9 12 6 6 15 7 18 3 | 25 25 25 28 24 23 25 33 27 26 24
3E | 6 9 15 16 14 5 12 17 7 13 4 | 27 28 23 23 32 24 27 34 28 26 25
X4 | 10 --- 16 14 --- 6 23 17 15 52 9 | 61 --- 56 70 --- 60 56 70 65 70 61
5 | 8 13 10 12 20 5 8 14 11 17 4 | 38 37 36 38 38 36 38 48 43 40 37
6 | 8 10 11 10 11 4 6 17 8 11 3 | 86 87 84 85 86 83 85 84 81 84 85
7 | 7 10 7 7 13 3 4 19 8 18 3 | 26 29 24 29 27 26 30 35 25 19 25
8 | 7 9 17 10 13 4 7 15 10 7 4 | 34 38 39 36 40 38 38 44 39 35 37
9 | 10 12 11 9 12 4 7 15 7 11 3 | 63 65 63 61 61 62 67 68 62 67 63
10E | 9 14 16 9 14 6 10 16 10 12 4 | 27 28 24 27 25 26 28 36 28 27 25
11 | 7 9 18 8 16 4 8 17 6 18 4 | 22 28 23 23 25 23 30 34 24 21 23
12 | 8 18 7 10 19 5 6 15 11 22 4 | 35 43 35 41 42 37 40 49 42 31 37
13 | 5 16 11 9 12 4 9 15 9 24 4 | 33 38 29 31 36 32 36 43 33 36 31
14 | 9 13 9 7 11 4 7 14 7 26 4 | 38 38 36 38 38 37 37 42 41 46 37
15 | 7 14 9 6 14 4 9 14 9 20 4 | 35 41 36 37 35 35 38 40 37 35 35
16 | 7 17 8 9 12 6 7 17 7 21 4 | 33 38 32 38 34 32 34 45 37 31 33
17 | 6 15 7 8 15 4 9 17 10 14 3 | 33 30 30 32 31 32 33 42 31 24 30
X18 | 14 10 12 10 --- 5 7 19 12 --- 5 | 29 34 29 37 --- 31 35 42 32 --- 31
19 | 6 17 10 10 12 4 6 15 11 16 4 | 34 31 34 35 36 33 35 48 33 36 33
20 | 10 11 6 5 14 4 8 13 9 13 3 | 78 81 81 81 76 80 80 82 81 78 79
21 | 7 10 8 7 14 4 7 18 10 18 3 | 27 29 24 28 28 25 28 33 28 31 26
22 | 7 10 6 14 15 5 6 15 6 13 3 | 31 31 33 31 35 32 34 40 32 33 31
23 | 8 22 6 7 11 5 9 16 11 32 5 | 16 18 14 18 18 16 16 26 19 29 13
24 | 9 9 7 13 12 4 8 14 9 16 4 | 61 65 61 62 58 59 64 66 61 65 62
25 | 9 11 14 8 13 3 7 12 8 9 3 | 41 45 44 46 47 42 43 52 41 37 42
26 | 8 12 11 7 10 4 7 14 7 12 3 | 20 21 17 16 15 17 16 26 14 21 19
27 | 9 13 17 8 10 4 10 20 9 9 4 | 558 553 555 556 545 555 554 550 554 553 554
28 | 6 8 8 7 14 3 7 22 12 14 3 | 34 35 33 36 37 34 34 48 36 34 33
29 | 7 17 6 6 19 4 7 15 8 16 4 | 32 30 26 31 35 30 29 44 30 27 29
30 | 7 11 6 8 11 3 6 20 8 7 3 | 73 76 72 75 74 72 76 78 69 68 73
31 | 8 13 6 8 9 3 7 13 7 21 3 | 22 24 18 22 21 21 25 31 19 22 20
32 | 8 15 11 7 11 4 8 12 9 9 3 | 39 41 41 39 42 39 41 47 36 34 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 9 13 4 8 16 9 17 |T 55 57 54 56 57 55 56 63 56 56 55
WRMS | 8 13 10 9 13 4 8 16 8 15 |NE 58 60 57 59 60 57 59 66 58 59 57
MEDI | 8 12 9 8 12 4 7 15 9 16 |MD 34 37 33 36 36 33 35 44 36 34 33
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 4.2092 GPS week: 2092 MJD: 58888.0-58894.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 |U 11 18 24 |U 0 0 0 |U 8 12 20 |
emr | emr 2962 |U 21 25 46 |U 0 0 0 |U 12 23 40 |
esa | esa 3058 | 12 20 24 |U 0 0 0 | 11 14 29 |
gfz | gfz 3058 |U 11 19 25 |U 0 0 0 |U 9 11 24 |
grg | grg 2852 |U 14 24 29 |U 0 0 0 | 10 14 21 |
igr | igr 3028 | 12 21 23 | 0 0 0 | 9 13 22 |
igs | igs 3056 | 13 22 26 | 0 0 0 | 9 14 23 |
jpl | jpl 3044 |U 22 37 43 |U 0 0 0 |U 13 21 36 |
mit | mit 3058 | 29 22 41 |U 0 0 0 |U 17 19 37 |
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 5.2092.0 GPS week: 2092 Day: 0 MJD: 58888.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 12 17 26 | ---- ---- ---- | 9 15 22 |
emr | emr 2976 | 19 26 43 | ---- ---- ---- | 12 23 37 |
esa | esa 3072 | 13 21 28 | ---- ---- ---- | 10 17 28 |
gfz | gfz 3072 | 12 21 27 | ---- ---- ---- | 10 16 21 |
grg | grg 2880 | 14 21 29 | ---- ---- ---- | 14 20 24 |
igr | igr 3072 | 13 20 27 | ---- ---- ---- | 9 16 21 |
igs | igs 3072 | 13 21 28 | ---- ---- ---- | 9 17 19 |
jpl | jpl 3072 | 17 27 42 | ---- ---- ---- | 12 22 29 |
mit | mit 3072 | 13 20 27 | ---- ---- ---- | 10 17 24 |
Table 5.2092.1 GPS week: 2092 Day: 1 MJD: 58889.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 14 23 | ---- ---- ---- | 7 11 20 |
emr | emr 2976 | 15 14 39 | ---- ---- ---- | 13 22 43 |
esa | esa 3072 | 13 16 24 | ---- ---- ---- | 9 10 25 |
gfz | gfz 3071 | 11 16 26 | ---- ---- ---- | 9 11 21 |
grg | grg 2880 | 13 20 32 | ---- ---- ---- | 11 15 20 |
igr | igr 3071 | 11 14 25 | ---- ---- ---- | 8 12 19 |
igs | igs 3069 | 12 15 27 | ---- ---- ---- | 8 13 19 |
jpl | jpl 3072 | 15 20 37 | ---- ---- ---- | 13 17 31 |
mit | mit 3072 | 14 22 47 | ---- ---- ---- | 11 14 27 |
Table 5.2092.2 GPS week: 2092 Day: 2 MJD: 58890.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 11 18 21 | ---- ---- ---- | 9 12 25 |
emr | emr 2976 | 16 18 43 | ---- ---- ---- | 11 23 39 |
esa | esa 3072 | 13 20 21 | ---- ---- ---- | 10 15 33 |
gfz | gfz 3072 | 11 19 22 | ---- ---- ---- | 10 11 28 |
grg | grg 2878 | 17 30 32 | ---- ---- ---- | 11 14 25 |
igr | igr 3071 | 12 20 22 | ---- ---- ---- | 10 14 27 |
igs | igs 3072 | 12 20 24 | ---- ---- ---- | 9 13 25 |
jpl | jpl 3072 | 18 27 32 | ---- ---- ---- | 13 22 34 |
mit | mit 3072 | 12 21 30 | ---- ---- ---- | 25 21 49 |
Table 5.2092.3 GPS week: 2092 Day: 3 MJD: 58891.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 19 22 | ---- ---- ---- | 7 11 20 |
emr | emr 2976 | 16 15 40 | ---- ---- ---- | 13 22 35 |
esa | esa 3072 | 12 20 19 | ---- ---- ---- | 11 13 30 |
gfz | gfz 3072 | 11 19 23 | ---- ---- ---- | 9 10 25 |
grg | grg 2880 | 14 28 26 | ---- ---- ---- | 9 10 22 |
igr | igr 3026 | 12 22 20 | ---- ---- ---- | 9 11 23 |
igs | igs 3064 | 11 20 22 | ---- ---- ---- | 9 13 22 |
jpl | jpl 3072 | 18 32 38 | ---- ---- ---- | 14 22 37 |
mit | mit 3072 | 15 18 28 | ---- ---- ---- | 18 21 41 |
Table 5.2092.4 GPS week: 2092 Day: 4 MJD: 58892.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 11 17 27 | ---- ---- ---- | 10 12 22 |
emr | emr 2880 | 49 66 75 | ---- ---- ---- | 14 27 52 |
esa | esa 2976 | 13 20 31 | ---- ---- ---- | 13 16 33 |
gfz | gfz 2976 | 11 15 28 | ---- ---- ---- | 10 12 26 |
grg | grg 2784 | 11 18 29 | ---- ---- ---- | 10 24 24 |
igr | igr 2975 | 13 24 28 | ---- ---- ---- | 11 14 26 |
igs | igs 2976 | 17 35 35 | ---- ---- ---- | 11 15 28 |
jpl | jpl 2976 | 46 89 73 | ---- ---- ---- | 15 26 49 |
mit | mit 2976 | 17 20 66 | ---- ---- ---- | 18 17 36 |
Table 5.2092.5 GPS week: 2092 Day: 5 MJD: 58893.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 | 10 19 21 | ---- ---- ---- | 8 10 16 |
emr | emr 2976 | 14 13 39 | ---- ---- ---- | 12 22 35 |
esa | esa 3072 | 10 16 19 | ---- ---- ---- | 10 12 26 |
gfz | gfz 3072 | 9 15 21 | ---- ---- ---- | 9 9 22 |
grg | grg 2784 | 11 23 24 | ---- ---- ---- | 7 8 16 |
igr | igr 3011 | 11 20 18 | ---- ---- ---- | 9 10 18 |
igs | igs 3072 | 10 16 20 | ---- ---- ---- | 9 12 20 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 3072 | 13 25 34 | ---- ---- ---- | 14 18 42 |
Table 5.2092.6 GPS week: 2092 Day: 6 MJD: 58894.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 10 22 25 | ---- ---- ---- | 9 11 18 |
emr | emr 2976 | 16 22 46 | ---- ---- ---- | 13 20 38 |
esa | esa 3072 | 12 25 27 | ---- ---- ---- | 11 14 32 |
gfz | gfz 3071 | 11 27 30 | ---- ---- ---- | 9 11 27 |
grg | grg 2879 | 16 31 29 | ---- ---- ---- | 8 8 18 |
igr | igr 2976 | 12 24 25 | ---- ---- ---- | 10 12 20 |
igs | igs 3072 | 12 24 27 | ---- ---- ---- | 9 12 24 |
jpl | jpl 3072 | 19 29 38 | ---- ---- ---- | 13 20 38 |
mit | mit 3072 | 122 27 55 | ---- ---- ---- | 24 28 38 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.2092 GPS week: 2092 MJD: 58888.500-58894.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 2 -11 29 189 1 | 18 24
| 16 24 67 55 10 | 2
emr uuuuu | -18 18 -63 -197 4 | 52 56
| 23 24 80 50 14 | 2
esa uuuuu | 12 -10 114 42 7 | 36 40
| 22 9 73 105 5 | 3
gfz uuuxu | -13 25 -62 -31 0 | 23 28
| 20 25 69 214 3 | 3
grg uuuuu | 15 -1 -62 -46 0 | 1 15
| 17 23 41 50 5 | 2
igr xxxxx | 9 12 5 40 -2 | 5 19
| 10 11 48 46 3 | 3
irf xxxxx | -6 -20 22 -4 -1 | -2 17
| 18 24 27 12 7 | 3
jpl uuuuu | -45 -14 -30 -109 0 | 44 50
| 25 29 59 57 8 | 4
mit uuuuu | -5 -17 85 56 -4 | 18 24
| 34 43 67 43 7 | 3
ngs uuuxu | 60 -14 -7 358 -1 | 16 23
| 39 52 159 249 4 | 3
sio uuuux | -14 18 -37 -113 -5 | 40 43
| 38 18 52 96 7 | 4
Table 7.2092.0 GPS week: 2092 Day: 0 MJD: 58888.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 20 32 0 205 2 | 18 24
emr uuuuu | 27 -19 60 -136 0 | 48 53
esa uuuuu | 0 -13 203 -96 16 | 31 36
gfz uuuxu | -40 8 93 -248 -4 | 25 30
grg uuuuu | 53 -24 -76 -114 -1 | 1 16
igr xxxxx | 29 22 5 95 -2 | 6 20
irf xxxxx | 4 8 -25 -6 -3 | 0 17
jpl uuuuu | -67 -28 50 -83 3 | 38 50
mit uuuuu | 26 44 -19 62 -6 | 20 26
ngs uuuxu | -2 -67 -337 681 0 | 17 24
sio uuuux | 24 12 -37 -62 -10 | 43 46
Table 7.2092.1 GPS week: 2092 Day: 1 MJD: 58889.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 2 -19 3 252 -20 | 20 25
emr uuuuu | -10 -6 -108 -173 21 | 50 54
esa uuuuu | -2 -25 216 21 6 | 35 39
gfz uuuxu | -16 41 -101 -276 1 | 25 30
grg uuuuu | 10 -26 -14 -63 6 | 2 16
igr xxxxx | 2 28 86 21 -4 | 7 20
irf xxxxx | -2 7 23 -4 -5 | 1 16
jpl uuuuu | -53 44 -48 -224 12 | 42 52
mit uuuuu | 0 -5 50 90 -9 | 21 26
ngs uuuxu | 103 -51 -38 694 1 | 18 25
sio uuuux | -17 38 -35 -104 -6 | 43 46
Table 7.2092.2 GPS week: 2092 Day: 2 MJD: 58890.500
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 -11 8 229 2 | 19 25
emr uuuuu | -41 38 -112 -292 20 | 54 57
esa uuuuu | -11 -11 87 -33 5 | 37 41
gfz uuuxu | -41 25 -83 -196 0 | 25 30
grg uuuuu | 9 -17 -20 -85 4 | 3 15
igr xxxxx | 11 -1 24 90 -5 | 8 20
irf xxxxx | 9 -14 12 -4 -9 | 1 16
jpl uuuuu | -25 -7 -22 -124 -10 | 50 53
mit uuuuu | 14 15 44 100 -14 | 21 26
ngs uuuxu | 56 -29 6 420 -5 | 19 25
sio uuuux | 3 6 18 -32 -16 | 43 46
Table 7.2092.3 GPS week: 2092 Day: 3 MJD: 58891.500
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 | -24 -14 -68 95 0 | 20 26
emr uuuuu | -16 44 -66 -219 7 | 55 59
esa uuuuu | 1 3 121 8 7 | 39 42
gfz uuuxu | -2 71 -77 93 -4 | 25 30
grg uuuuu | 8 15 -28 11 5 | 4 15
igr xxxxx | 8 8 22 79 -5 | 8 20
irf xxxxx | -18 -17 33 22 -6 | 1 16
jpl uuuuu | -8 -19 -40 -93 -1 | 48 51
mit uuuuu | -21 -7 116 96 -10 | 20 26
ngs uuuxu | 58 -69 22 166 -4 | 19 25
sio uuuux | 4 47 -82 9 2 | 41 45
Table 7.2092.4 GPS week: 2092 Day: 4 MJD: 58892.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 19 -48 115 203 3 | 17 23
emr uuuuu | -31 32 -153 -209 0 | 52 56
esa uuuuu | 16 -12 13 131 10 | 37 41
gfz uuuxu | 2 16 -96 155 2 | 21 27
grg uuuuu | 4 -5 -82 -50 -1 | 1 14
igr xxxxx | 1 10 -62 17 3 | 4 18
irf xxxxx | -27 -31 24 -11 2 | -3 17
jpl uuuuu | -35 -4 -33 -71 2 | 45 48
mit uuuuu | -44 -31 139 46 -3 | 16 24
ngs uuuxu | 66 36 74 66 -4 | 16 23
sio uuuux | -92 14 27 -273 -7 | 38 41
Table 7.2092.5 GPS week: 2092 Day: 5 MJD: 58893.500
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 -20 119 205 7 | 16 23
emr uuuuu | -40 31 -99 -190 -4 | 52 56
esa uuuuu | 34 -14 95 45 2 | 38 41
gfz uuuxu | 11 19 -96 269 5 | 20 26
grg uuuuu | 17 24 -99 25 -6 | 0 14
igr xxxxx | 0 16 -42 -11 1 | 3 18
irf xxxxx | -26 -60 67 -15 8 | -4 17
jpl uuuuu | -83 -41 -136 -50 6 | 44 47
mit uuuuu | -50 -86 180 4 5 | 15 22
ngs uuuxu | 110 52 165 229 -1 | 14 22
sio uuuux | -25 -6 -30 -179 2 | 36 40
Table 7.2092.6 GPS week: 2092 Day: 6 MJD: 58894.500
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 2 22 133 11 | 15 22
emr uuuuu | -16 3 37 -162 -18 | 51 55
esa uuuuu | 49 -1 64 220 2 | 38 41
gfz uuuxu | -4 -7 -73 -17 0 | 19 25
grg uuuuu | 7 28 -113 -46 -5 | -1 14
igr xxxxx | 14 2 4 -10 -1 | 2 17
irf xxxxx | 19 -35 20 -12 9 | -5 17
jpl uuuuu | -43 -41 21 -117 -9 | 44 47
mit xxxxx | 37 -48 86 -5 5 | 14 21
ngs uuuxu | 31 31 55 249 6 | 12 21
sio uuuux | 4 13 -119 -150 1 | 34 37
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