[IGSREPORT-27152] Wk 2095 IGS Final Orbits
acc
acc at igs.org
Sun Mar 22 03:48:26 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2095 (Mar 01, 2020 - Mar 07, 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:
igs2095[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2095[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2095[0-6].cls IGS GPS clock combination summary report.
igs20957.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20957.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 | SEYG TIXI SEYG TIXI
0 | EMR | MCM4
0 | ESA | 18 18 DJIG PTBB DJIG PTBB
0 | GFZ | 4 4 18 BJNM GODE POHN BJNM GODE POHN
0 | GRG | NYA2 NYA2
0 | JPL | SEYG SEYG
0 | MIT | BJNM
1 | COD | BJNM BJNM HOFN
1 | EMR | DAEJ DAEJ
1 | ESA | DUBO MOBS POHN TLSE DUBO MOBS POHN TLSE
1 | GFZ | 4 4 FLRS REUN REYK FLRS GODE HOFN REUN REYK
1 | GRG | 13 13 NYA2 TLSE NYA2 TLSE
1 | JPL | 32
1 | MIT | BJNM HOFN MOBS
2 | COD | TIXI TIXI
2 | EMR | TLSE TLSE
2 | ESA | 18 18 PDEL PTBB SCOR BJCO PDEL PTBB SCOR
2 | GFZ | 4 4 BJNM FALK FLRS GODE PDEL POHN FALK FLRS GODE
2 | GFZ | KOKB PDEL POHN
2 | GRG | BRST TLSE BRST TLSE
2 | JPL | HRAO HRAO
3 | COD | BRMU TIXI BRMU
3 | ESA | 18 18 PTBB YSSK PTBB YSSK
3 | GFZ | 4 18 4 18 BJNM BOR1 DGAR GODE POHN WTZR BJCO BOR1
3 | GFZ | DGAR GODE POHN WTZR
3 | GRG | 13 13 BRST XMIS BRST
3 | MIT | 18
4 | COD | BARH BJCO SAVO TIXI COCO SAVO TIXI
4 | EMR | 13 13
4 | ESA | 18 18 DAV1 DJIG PTBB ULAB DJIG GLPS IQAL PTBB
4 | GFZ | 4 4 BJNM GLPS GODE POHN PTBB BARH BJNM GLPS GODE
4 | GFZ | MAL2 NRC1 POHN PTBB ULAB
4 | GRG | 13 29 13 29 ABMF CHTI COCO DAV1 ULAB WUH2 COCO DAV1
4 | MIT | BJNM CPVG MAL2 MCM4 PTBB
5 | COD | BRST DAV1 IISC TIXI BRST TIXI
5 | ESA | 18 DAV1 PDEL PTBB DAV1 PDEL PTBB
5 | GFZ | 4 4 BJNM DAV1 GODE IISC PDEL POHN DAV1 GODE IISC
5 | GFZ | PDEL POHN
5 | GRG | COCO KARR COCO
5 | MIT | PALM
6 | COD | 18 TIXI TIXI
6 | EMR | MCM4 MCM4 PRDS
6 | ESA | 18 18 GLPS PTBB GLPS PTBB SGOC TLSE
6 | GFZ | 4 4 BJNM GODE POHN BJNM GODE MCM4 POHN SGOC TLSE
6 | GRG | 13 KARR
6 | JPL | POLV
6 | MIT | 18 BJNM MCM4
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 | SIO | 4
1 | JPL | 32
3 | ESA | 18
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 G32 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .1 .3 1.6 10 29 9 -.38
EMR | 0 | 2.7 -1.8 13.5 -36 -21 15 -.08
ESA | 0 | .3 -1.2 -1.3 18 52 68 -.32
GFZ | 0 | .5 -.1 -.4 33 -3 70 -.28
GRG | 0 | -.2 2.5 5.8 111 2 110 -.27
JPL | 0 | 5.6 -.2 8.9 17 10 9 -.41
MIT | 0 | -.2 .9 10.4 2 -4 4 -.0
NGS | 0 | -2.3 1.6 1.4 -18 54 38 -.27
SIO | 0 | -1.1 -1.5 -4.7 7 -7 18 -.26
COD | 1 | -.1 .3 1.4 12 16 2 -.42
EMR | 1 | 4.6 -3.3 .6 -47 -35 16 -.25
ESA | 1 | -.3 -.5 -1.2 12 45 35 -.42
GFZ | 1 | .7 -.4 -.7 31 -13 69 -.34
GRG | 1 | 5.4 5.7 2.9 95 -2 99 -.33
JPL | 1 | 7.8 -5.5 11.2 4 7 31 -.40
MIT | 1 | 3.0 1.5 6.7 15 -10 -4 -.13
NGS | 1 | -3.3 -6.7 -6.8 -81 44 -3 -.23
SIO | 1 | -.8 -3.3 -3.4 32 -38 6 -.46
COD | 2 | .3 .3 1.3 8 13 -2 -.46
EMR | 2 | 7.1 1.6 1.0 -43 -10 44 -.22
ESA | 2 | .6 -.3 -.6 5 22 66 -.56
GFZ | 2 | .0 1.0 -.0 44 11 38 -.27
GRG | 2 | 1.9 8.4 -3.5 65 15 105 -.49
JPL | 2 | 13.0 -3.9 9.7 -3 -3 -8 -.46
MIT | 2 | 5.4 5.3 8.3 -16 -4 -23 -.18
NGS | 2 | 3.2 2.8 -4.4 -14 14 -70 -.17
SIO | 2 | -.4 3.0 -12.9 38 -19 6 -.45
COD | 3 | .1 .5 1.1 20 12 10 -.38
EMR | 3 | 5.8 -2.0 5.1 -67 -11 48 -.18
ESA | 3 | .6 .3 -1.0 14 40 59 -.29
GFZ | 3 | -1.1 1.1 -1.1 42 17 52 .02
GRG | 3 | 3.3 2.4 -5.6 82 -8 114 -.38
JPL | 3 | 13.0 -4.6 11.6 15 13 -3 -.33
MIT | 3 | 2.7 2.1 11.0 15 -16 2 -.03
NGS | 3 | 6.0 -.2 .7 -13 -13 -3 -.25
SIO | 3 | .9 -2.5 -15.4 30 2 5 -.30
COD | 4 | -.1 -.1 1.1 10 23 9 -.21
EMR | 4 | 4.7 -9.6 5.7 -36 -19 39 -.44
ESA | 4 | -.1 -.8 -1.0 9 46 61 -.29
GFZ | 4 | -.7 .6 -.4 43 15 50 -.03
GRG | 4 | 4.0 -3.4 -5.0 92 23 113 -.15
JPL | 4 | 11.9 -10.4 11.1 13 8 28 -.10
MIT | 4 | 2.0 .6 8.5 -6 -5 -16 .13
NGS | 4 | 2.3 -6.3 1.8 -35 23 13 -.02
SIO | 4 | -3.1 -3.2 -15.9 29 -23 17 -.14
COD | 5 | -.2 -.2 1.0 12 19 24 -.21
EMR | 5 | 7.4 -3.4 8.4 -31 -6 34 .28
ESA | 5 | -.3 .0 -1.3 11 54 66 -.02
GFZ | 5 | -.4 .0 .5 37 20 62 .01
GRG | 5 | 2.9 .3 .9 120 42 120 .20
JPL | 5 | 14.5 -6.8 9.4 14 6 13 -.21
MIT | 5 | 3.7 2.6 10.6 -21 23 30 .17
NGS | 5 | 4.8 -3.4 8.6 -7 11 34 .09
SIO | 5 | -3.8 -3.1 -20.8 36 3 37 -.10
COD | 6 | -.1 .1 .6 1 16 5 -.15
EMR | 6 | 5.6 -4.1 6.4 -34 -11 5 .29
ESA | 6 | .9 -.5 -.7 -17 41 57 -.14
GFZ | 6 | .1 .3 -.1 34 14 57 -.07
GRG | 6 | 4.3 -1.2 -.2 103 35 116 .11
JPL | 6 | 6.4 -.4 6.3 22 6 10 -.21
MIT | 6 | .1 1.4 7.8 2 1 -4 .16
NGS | 6 | 2.5 -3.7 .5 -44 4 -4 .12
SIO | 6 | -3.1 -2.1 -17.3 30 -17 18 -.13
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 1.2095.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2095.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 2.2095.[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 3.2095.[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 5.2095.0-6). 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 2095 summary. (Mar 01, 2020 - Mar 07, 2020)
Table 1.2095.a GPS week: 2095 MJD: 58909.000-58915.000
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 251| 0 0 -1 0 -11 6 -.04 8 8 | -615 142 6 112
| 0 0 1 13 14 25 .03 | 191 432
emr 81| 0 -3 1 -9 -1 0 .16 13 13 | 214348 244 16 111
| 1 0 1 17 7 19 .06 | 1417 1043
esa 148| 0 0 1 -13 -8 3 -.05 10 10 | -1110 914 8 95
| 0 0 0 13 19 26 .01 | 372 557
gfz 179| 0 0 0 -5 -3 7 .04 10 10 | -64 31 12 118
| 0 0 3 25 8 15 .02 | 360 505
grg 94| 0 0 -5 -29 0 32 -.07 10 9 | -14 212 9 136
| 0 0 3 16 9 43 .03 | 288 414
igr n/a| 0 0 0 -20 -21 -20 .02 4 4 | 15767 2339 10 71
| 0 0 0 19 6 17 .01 | 7537 4048
jpl 80| 0 0 5 23 15 0 .22 8 8 | 214362 239 9 91
| 1 0 0 15 11 20 .02 | 1403 1036
mit 368| 0 0 0 21 -2 -11 -.05 9 9 | 15579 2344 64 1679
| 0 0 0 35 15 93 .02 | 7397 4059
ngs 201| 0 0 0 -9 1 -21 -.03 8 7 | -552 77 976 2139
| 0 1 2 26 17 20 .03 | 171 371
sio 440| -2 -1 -5 12 6 -1 -.29 17 16 | --- --- --- ---
| 1 1 1 35 15 25 .05 | --- ---
Table 1.2095.b GPS week : 2095 MJD: 58909.000-58915.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 3 3 3 3 3 |
2 | 4 4 4 3 3 4 3 |
3 | 4 3 3 3 3 3 3 |
4 | 7 8 8 7 8 8 9 |
5 | 4 4 4 3 4 4 3 |
6 | 3 3 3 3 3 4 3 |
7 | 3 3 3 3 3 4 3 |
8 | 4 4 4 4 4 4 4 |
9 | 3 3 4 3 4 4 4 |
10 | 4 3 3 3 3 4 3 |
11 | 4 4 4 4 4 4 4 |
12 | 4 4 4 4 4 4 4 |
13 | 4 4 4 4 3 4 4 |
14 | 3 4 3 3 4 3 3 |
15 | 5 4 4 4 4 4 5 |
16 | 4 4 3 4 4 4 4 |
17 | 4 3 4 3 4 4 4 |
18 | 5 5 5 5 5 6 5 |
19 | 4 4 4 3 4 5 4 |
20 | 4 4 3 3 4 4 3 |
21 | 4 3 3 3 3 3 4 |
22 | 3 3 4 3 3 4 4 |
23 | 4 4 4 4 5 5 5 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 4 3 4 |
26 | 3 3 3 3 3 3 3 |
27 | 4 4 4 4 4 4 4 |
28 | 3 3 3 3 3 3 4 |
29 | 4 5 4 4 4 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 4 3 3 4 4 3 |
32 | 4 16 4 4 4 5 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 2.2095.0 GPS week: 2095 Day: 0 MJD: 58909.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 251| 0 0 -2 11 13 -14 -.07 8 7 | -674 364 7 121
emr 81| -1 -3 3 13 -1 -20 .22 13 13 | 212966 -560 16 122
esa 149| 0 0 1 -17 0 -15 -.06 10 10 | -1210 893 10 117
gfz 179| 0 0 -3 -37 -20 -1 .06 10 9 | -134 -401 13 110
grg 98| 0 0 -1 -10 -11 48 -.07 10 9 | 337 -441 10 131
igr n/a| 0 0 -1 -24 -15 -32 .02 4 4 | 17632 4355 11 77
jpl 80| -1 0 5 38 4 -16 .21 9 9 | 212996 -545 8 103
mit 368| 0 1 0 1 -15 42 -.02 8 8 | 17084 4386 28 1687
ngs 200| 0 -1 0 1 16 -3 -.03 10 8 | -667 332 1057 2291
sio 439| -1 0 -4 -11 -3 -37 -.28 16 16 | --- --- --- ---
Table 2.2095.1 GPS week: 2095 Day: 1 MJD: 58910.000
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| -1 0 -1 -17 -9 -5 -.05 7 7 | -739 272 7 114
emr 81| 0 -2 0 -22 7 0 .18 14 14 | 211973 2156 16 103
esa 149| -1 0 2 -30 10 -3 -.05 12 11 | -1762 1147 9 93
gfz 174| 0 0 -3 6 -6 3 -.00 11 11 | -563 806 16 101
grg 95| 1 1 0 -16 14 33 -.08 11 9 | -548 758 11 124
igr n/a| 0 0 0 -45 -9 -21 .01 4 4 | 21549 7829 11 73
jpl 80| 0 -1 5 -5 30 34 .22 8 8 | 212010 2135 8 97
mit 368| 0 0 0 67 -19 -20 -.06 7 7 | 21397 7848 84 1459
ngs 202| 1 0 -3 -29 -32 -42 .01 9 8 | -753 285 1368 2318
sio 443| 0 0 -4 43 -11 0 -.31 17 18 | --- --- --- ---
Table 2.2095.2 GPS week: 2095 Day: 2 MJD: 58911.000
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 -1 18 -18 7 -.06 8 8 | -491 76 7 118
emr 81| 0 -2 0 8 -6 18 .22 12 12 | 214090 946 14 107
esa 149| 0 0 0 -7 -48 40 -.06 10 10 | -813 553 8 100
gfz 182| 0 0 3 40 -3 -14 .04 9 9 | 544 -772 11 98
grg 95| 0 0 -6 -16 6 73 -.10 11 9 | 243 -122 8 108
igr n/a| 0 0 0 -2 -29 -3 .01 4 4 | 29478 7283 10 70
jpl 80| 0 0 4 32 24 3 .19 8 8 | 214113 947 10 86
mit 368| 0 1 0 -23 14 -47 -.06 8 8 | 29084 7282 112 1362
ngs 201| 0 1 -1 -37 10 -35 -.03 9 8 | -504 137 902 2161
sio 444| -1 -1 -6 -45 10 16 -.37 18 17 | --- --- --- ---
Table 2.2095.3 GPS week: 2095 Day: 3 MJD: 58912.000
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 -2 -7 -28 30 -.06 8 8 | -603 37 8 113
emr 81| 0 -3 1 -34 7 3 .17 14 14 | 215091 289 17 127
esa 148| 0 0 1 -26 3 26 -.04 9 9 | -927 578 8 96
gfz 182| 0 0 3 5 -6 25 .06 10 9 | -335 127 12 149
grg 93| 0 0 -8 -24 -3 75 -.09 11 10 | -68 93 9 150
igr n/a| 0 0 0 -36 -27 -4 .02 4 4 | 11041 -229 10 69
jpl 80| 0 -1 4 27 15 -4 .24 8 8 | 215083 312 12 76
mit 368| 0 0 0 51 1 -72 -.03 6 6 | 10672 -205 37 1763
ngs 204| 0 0 0 -41 -7 1 -.01 8 7 | -632 104 924 1979
sio 439| -4 -2 -7 46 29 1 -.28 17 17 | --- --- --- ---
Table 2.2095.4 GPS week: 2095 Day: 4 MJD: 58913.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| -1 0 -4 -3 -1 44 .03 10 10 | -806 628 7 113
emr 81| -2 -3 2 -24 -9 25 .17 13 13 | 215619 163 16 112
esa 149| 0 0 1 -8 -5 19 -.05 9 9 | -693 246 7 88
gfz 180| 2 0 1 -27 0 22 .06 10 9 | -136 100 11 121
grg 94| 1 0 -8 -53 3 36 -.09 10 9 | -44 219 9 167
igr n/a| 0 0 0 -32 -21 -6 .01 4 4 | 10869 -425 9 87
jpl 80| 0 0 6 22 6 17 .23 8 8 | 215626 129 11 80
mit 368| 0 0 0 42 -18 -86 -.06 9 8 | 10989 -459 29 1649
ngs 201| 0 1 0 18 16 -27 -.06 7 6 | -628 194 625 1817
sio 443| -3 -1 -4 18 -10 21 -.33 17 15 | --- --- --- ---
Table 2.2095.5 GPS week: 2095 Day: 5 MJD: 58914.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 251| 0 0 0 13 -19 12 -.03 8 7 | -746 349 6 108
emr 81| 0 -4 0 -2 -11 1 .11 14 14 | 215717 -364 17 107
esa 149| 0 0 0 8 -8 -4 -.05 10 10 | -1398 1969 7 77
gfz 180| 0 0 -1 -10 6 20 .03 11 11 | -40 36 13 109
grg 94| 0 0 -7 -44 0 10 -.07 9 8 | 94 374 10 133
igr n/a| 0 1 -1 -3 -20 -22 .01 4 4 | 10556 -922 10 61
jpl 80| 0 -1 4 35 3 -4 .23 8 8 | 215727 -399 9 87
mit 368| 0 0 0 -17 13 -73 -.04 15 15 | 10403 -836 96 1946
ngs 203| 0 0 3 2 11 1 -.06 8 7 | -436 234 897 2234
sio 437| -4 -1 -5 -10 16 21 -.23 18 16 | --- --- --- ---
Table 2.2095.6 GPS week: 2095 Day: 6 MJD: 58915.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 251| 0 0 0 -10 -16 -26 -.05 8 8 | -251 -732 5 101
emr 81| 1 -4 1 -2 1 -27 .06 13 13 | 214983 -922 17 101
esa 149| 0 0 0 -14 -12 -37 -.03 10 9 | -971 1015 8 95
gfz 182| 0 0 1 -11 4 -6 .06 9 9 | 214 326 10 141
grg 95| 0 0 -5 -40 -12 -50 -.01 10 9 | -115 607 11 145
igr n/a| 0 0 0 3 -24 -52 .04 4 4 | 9250 -1512 9 61
jpl 80| -2 0 4 15 26 -28 .25 10 10 | 214982 -904 10 110
mit 368| 1 0 0 24 7 175 -.04 8 8 | 9425 -1603 63 1888
ngs 202| 1 1 0 19 -1 -42 -.03 9 7 | -244 -746 1064 2173
sio 439| -2 -2 -8 42 12 -34 -.21 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 3.2095.0 GPS week: 2095 Day: 0 MJD: 58909.000
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 8 8 8 5 3 7 9 12 12 3 | 22 28 23 28 24 22 26 22 21 24 23
2 | 8 9 11 9 7 3 7 9 7 21 3 | 17 20 21 20 19 18 20 21 17 18 17
3 | 7 10 13 13 8 4 10 7 8 11 3 | 26 27 29 28 27 25 26 22 23 26 24
X4 | 11 --- 20 16 --- 5 22 7 13 55 7 | 61 --- 56 69 --- 59 58 59 67 63 60
5 | 7 11 10 11 17 4 8 9 9 14 3 | 23 29 27 28 26 25 27 23 27 23 24
6 | 7 5 10 8 5 2 7 7 6 9 2 | 25 31 27 28 27 26 30 27 22 26 26
7 | 4 11 7 9 7 4 8 7 8 23 3 | 61 61 61 61 60 61 65 64 62 59 61
8E | 6 15 14 10 7 4 10 10 11 13 3 | 29 32 28 30 34 31 31 34 30 30 30
9 | 8 14 13 8 7 5 9 5 11 11 3 | 37 47 35 35 36 37 41 38 41 39 38
10 | 6 13 15 7 7 3 8 11 8 11 3 | 27 26 31 26 30 26 27 23 26 28 25
11 | 9 11 16 9 10 3 8 9 9 15 3 | 26 36 22 31 30 28 33 29 26 26 27
12 | 7 17 9 9 17 4 8 8 10 20 4 | 28 39 32 31 35 29 34 31 31 23 30
13 | 7 18 9 11 9 4 8 6 12 18 3 | 20 29 24 28 20 22 28 22 23 21 21
14 | 5 12 5 6 6 4 6 7 9 20 3 | 35 36 34 34 35 35 36 37 35 30 34
15 | 13 21 9 24 13 9 14 10 12 16 5 | 60 62 64 70 61 59 62 62 61 62 61
16 | 5 18 5 7 9 6 9 8 8 24 3 | 31 35 33 32 36 32 33 34 32 35 32
17E | 11 11 10 8 11 5 7 6 9 17 3 | 51 47 40 46 49 43 46 45 44 41 45
X18 | 12 11 11 14 --- 5 7 14 11 --- 5 | 82 81 69 85 --- 78 79 77 78 --- 79
19 | 9 11 9 11 16 5 13 6 8 18 4 | 40 45 44 41 41 45 49 46 45 51 43
20 | 7 10 10 10 9 3 9 7 11 16 3 | 33 30 29 35 34 32 30 29 33 30 30
21 | 10 12 7 11 7 4 11 8 8 19 3 | 22 22 20 24 20 21 23 19 21 16 19
22 | 7 14 7 8 9 3 8 7 11 15 3 | 36 38 34 38 36 34 37 35 37 35 35
23 | 8 24 5 8 11 4 11 6 14 23 4 | 55 61 56 55 54 56 59 58 56 52 56
24 | 7 9 9 8 9 3 10 7 10 10 3 | 17 25 19 18 16 18 27 17 20 20 18
25 | 7 10 12 5 14 3 8 5 8 9 3 | 31 34 32 31 38 29 34 31 31 30 31
26 | 7 10 9 11 9 4 6 8 9 13 3 | 30 35 33 31 36 32 35 31 31 34 31
27E | 8 13 15 11 11 3 12 8 8 9 3 | 28 33 22 30 32 28 31 31 27 29 28
28 | 9 10 8 6 7 3 6 7 10 19 3 | 27 29 24 27 29 27 30 28 26 29 26
29E | 12 16 9 11 13 8 10 7 12 14 4 | 88 87 84 87 87 85 87 85 84 86 86
30 | 8 9 9 6 7 4 7 7 5 10 2 | 22 30 25 25 23 24 31 27 23 22 24
31 | 7 13 6 8 6 3 11 8 5 21 3 | 67 71 68 68 67 69 73 68 68 64 68
32 | 6 16 13 9 7 3 10 11 13 11 3 | 9999 709 9999 9999 709 9999 9999 9999 9999 9999 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 10 10 4 9 8 10 16 |T 37 61 36 39 59 37 40 37 37 35 37
WRMS | 7 13 10 9 9 4 9 8 8 16 |NE 33 36 33 35 31 33 36 33 33 31 33
MEDI | 7 11 9 9 9 4 8 7 9 15 |MD 30 35 32 31 34 31 33 31 31 30 30
Table 3.2095.1 GPS week: 2095 Day: 1 MJD: 58910.000
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 10 10 6 3 6 8 7 8 2 | 23 27 24 24 24 23 27 21 21 21 22
2 | 9 12 12 8 8 3 7 7 9 22 3 | 19 21 23 20 18 20 21 20 25 20 19
3 | 6 9 14 13 7 4 8 8 6 12 3 | 24 27 25 25 25 22 25 22 24 27 23
X4 | 11 --- 18 22 --- 6 23 11 13 53 8 | 43 --- 41 51 --- 41 40 46 45 52 43
5 | 8 11 15 10 15 4 6 8 9 17 3 | 24 29 28 27 23 24 26 21 25 23 23
6 | 8 10 14 8 6 3 6 7 7 12 3 | 22 29 26 24 22 22 25 22 22 23 22
7 | 6 10 9 7 8 4 6 7 11 23 3 | 47 48 48 46 47 47 50 48 50 45 48
8E | 6 15 13 15 11 3 9 9 14 15 4 | 23 29 25 27 27 25 26 25 25 26 24
9 | 7 12 14 8 6 3 7 8 9 12 3 | 36 38 35 34 35 36 38 37 36 36 35
10 | 8 11 16 8 8 4 7 8 7 17 3 | 22 24 26 23 26 23 24 22 24 27 22
11 | 8 15 17 11 13 4 7 9 9 15 3 | 24 32 21 28 30 25 31 25 24 25 25
12 | 4 19 18 12 12 3 7 7 11 22 4 | 23 30 32 26 31 25 29 25 24 20 25
13 | 8 19 11 13 10 4 9 6 10 18 4 | 17 24 20 19 18 17 25 21 22 16 17
14 | 6 19 7 13 6 6 7 7 7 21 3 | 32 34 30 36 31 31 32 34 33 26 31
15E | 10 21 7 13 9 6 12 5 11 19 4 | 59 58 59 59 60 57 56 57 58 59 57
16 | 5 15 6 8 10 3 7 7 10 23 3 | 28 29 26 23 31 27 29 26 28 29 26
17E | 7 10 11 13 13 4 7 5 6 15 3 | 40 39 36 43 45 39 41 38 41 35 39
X18 | 13 15 13 11 --- 5 8 11 16 --- 5 | 76 82 70 77 --- 77 77 77 81 --- 77
19 | 7 13 9 11 14 2 8 6 9 14 3 | 35 35 37 36 34 36 37 36 36 41 35
20 | 8 14 10 10 9 4 7 6 9 22 3 | 30 30 28 33 30 28 27 27 30 32 28
21 | 8 11 7 10 6 5 5 5 12 22 3 | 23 24 23 26 21 23 24 20 26 19 21
22 | 6 13 10 11 8 3 7 7 9 15 3 | 30 32 29 31 32 28 32 28 30 31 29
23 | 5 22 8 10 11 4 9 9 6 21 3 | 56 60 56 55 53 56 57 58 53 52 55
24 | 5 9 9 12 6 4 9 6 15 11 3 | 18 24 18 18 16 18 25 15 20 20 17
25 | 7 12 14 12 11 4 7 6 10 9 3 | 25 30 28 23 32 25 32 26 25 24 26
26 | 6 13 9 11 9 4 6 7 9 12 3 | 24 28 24 24 30 24 30 23 23 28 24
27E | 8 13 18 8 12 3 11 9 7 10 3 | 23 27 21 25 26 23 28 24 24 24 23
28 | 5 11 8 9 8 2 7 5 10 23 3 | 25 28 23 29 25 24 27 23 24 28 24
29E | 9 18 11 12 26 10 10 9 12 19 5 | 58 60 61 62 64 60 59 58 61 62 59
30 | 5 8 8 8 6 3 7 5 6 12 2 | 21 28 25 22 24 23 28 23 23 26 23
31 | 8 15 7 11 7 4 9 7 8 25 3 | 51 54 52 52 53 52 57 50 49 49 51
X32 | 33 --- 25 36 --- 22 107 29 40 53 15 | 9999 --- 9999 9999 --- 9999 9999 9999 9999 9999 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 12 11 11 4 8 7 9 17 |T 32 35 32 33 32 32 35 32 33 31 32
WRMS | 7 14 11 11 9 4 8 7 8 18 |NE 29 32 30 30 28 29 32 28 30 27 28
MEDI | 7 13 11 11 9 4 7 7 9 17 |MD 25 29 28 27 30 25 29 25 25 27 25
Table 3.2095.2 GPS week: 2095 Day: 2 MJD: 58911.000
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 6 8 8 8 4 7 8 9 11 2 | 20 25 24 20 24 21 26 21 22 23 21
2 | 8 11 11 9 9 3 7 9 10 20 3 | 22 19 24 25 21 22 20 25 23 24 20
3 | 9 9 14 8 9 4 7 8 4 12 3 | 23 28 28 23 26 25 26 22 27 23 24
X4 | 12 --- 18 17 --- 6 24 10 14 49 8 | 49 --- 47 52 --- 46 47 49 54 56 48
5 | 7 11 7 6 17 4 7 11 10 20 3 | 24 31 25 27 33 25 28 28 26 29 25
6 | 5 6 9 9 6 2 6 7 8 12 2 | 28 31 29 25 28 28 31 28 30 28 27
7 | 7 10 8 6 8 2 8 8 6 25 3 | 56 57 59 55 54 56 58 57 58 53 55
8E | 6 13 14 10 10 3 9 12 12 16 4 | 29 31 30 28 33 30 30 30 33 31 28
9 | 11 13 16 9 8 4 8 8 8 14 3 | 28 30 28 28 30 27 29 26 30 28 27
10 | 7 9 14 7 7 3 8 8 9 13 3 | 25 26 31 25 28 25 27 23 25 29 25
11 | 10 12 17 11 14 3 7 9 7 16 4 | 21 30 23 27 26 24 29 25 27 26 24
12 | 5 19 8 7 16 4 5 7 9 20 3 | 33 38 33 36 31 34 36 34 36 34 33
13 | 10 12 6 13 10 3 9 8 10 21 3 | 25 29 27 29 24 24 31 29 25 25 24
14 | 7 13 6 10 7 5 6 7 9 20 3 | 41 37 39 42 41 38 40 41 39 37 38
15E | 11 14 6 9 8 5 11 6 7 21 3 | 34 33 32 29 35 32 34 29 32 38 31
16 | 8 15 4 8 8 4 6 9 6 23 3 | 32 35 35 34 38 34 35 35 37 39 33
17E | 9 9 10 8 17 5 8 7 11 17 3 | 40 38 35 38 48 36 39 37 37 31 37
X18 | 15 12 14 11 --- 5 9 10 13 --- 5 | 78 72 57 78 --- 73 76 73 71 --- 73
19 | 7 11 8 7 18 4 6 7 11 17 3 | 54 52 52 56 47 53 55 52 54 55 53
20 | 8 10 8 9 10 3 7 7 8 21 3 | 28 28 28 29 29 28 28 25 29 29 27
21 | 8 9 6 8 7 4 5 8 7 20 3 | 22 25 23 23 21 21 26 21 21 22 21
22 | 10 11 9 10 11 5 10 11 10 17 3 | 43 43 41 43 42 43 43 44 41 39 42
23 | 10 21 8 9 11 4 9 10 9 24 4 | 55 59 56 56 53 54 56 54 55 55 54
24 | 10 8 6 11 9 4 8 8 10 12 3 | 27 29 24 24 22 23 30 23 27 24 24
25 | 8 10 12 7 12 4 6 6 8 10 3 | 37 41 37 40 38 38 40 38 40 40 37
26 | 7 11 9 7 9 3 5 9 7 14 3 | 36 39 39 37 40 37 40 37 39 40 37
27E | 7 12 16 6 10 2 11 10 8 10 3 | 29 31 25 28 30 27 31 27 29 31 27
28 | 7 10 7 7 8 3 5 8 8 21 3 | 29 33 28 28 27 28 30 27 30 29 27
29E | 9 19 9 11 13 6 10 8 10 17 4 | 49 47 48 48 51 49 47 46 48 52 47
30 | 5 7 7 6 7 3 8 9 5 14 2 | 24 32 28 24 24 25 31 25 27 25 25
31 | 5 13 7 9 6 4 7 8 6 23 3 | 65 66 66 69 66 67 70 66 65 67 66
32 | 8 14 15 8 8 3 8 10 9 10 3 | 974 9999 974 975 9999 975 978 976 982 978 977
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 10 9 11 4 8 8 9 18 |T 65 37 64 65 34 64 67 64 66 65 64
WRMS | 8 12 10 9 9 4 8 8 8 17 |NE 34 36 34 35 32 34 36 34 35 33 33
MEDI | 8 11 8 8 9 4 7 8 9 17 |MD 29 32 31 29 31 30 31 29 32 31 28
Table 3.2095.3 GPS week: 2095 Day: 3 MJD: 58912.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 7 7 10 6 3 6 6 6 11 2 | 19 25 23 23 19 21 25 22 20 19 20
2 | 9 9 9 11 10 3 9 5 8 20 3 | 28 22 26 25 22 23 22 25 25 24 23
3 | 8 11 11 8 9 4 9 5 6 12 3 | 22 26 25 21 24 23 24 22 22 24 22
X4 | 10 --- 17 18 --- 6 23 6 12 48 7 | 44 --- 39 47 --- 41 43 43 48 43 43
5 | 7 13 5 9 14 4 9 7 9 16 3 | 26 29 24 26 32 28 30 27 31 26 27
6 | 7 8 8 9 6 4 7 5 7 8 2 | 21 25 22 20 20 20 24 21 19 20 20
7 | 5 10 5 7 10 3 7 4 5 26 3 | 44 46 43 43 38 43 45 44 44 37 42
8E | 8 13 12 7 8 3 10 10 10 16 3 | 21 25 21 23 22 22 23 24 23 22 21
9 | 7 13 11 10 9 4 9 4 8 13 3 | 43 49 44 42 48 44 48 45 45 47 44
10 | 8 11 12 8 10 3 7 7 8 11 3 | 27 25 31 28 27 26 28 25 23 30 26
11 | 9 13 15 12 11 3 8 7 8 18 3 | 22 30 23 30 26 25 31 28 25 23 25
12 | 7 18 6 8 22 3 6 5 7 22 3 | 34 40 36 33 31 34 37 35 34 30 33
13 | 10 21 8 13 12 2 9 8 11 16 4 | 20 28 22 26 19 20 26 22 22 17 19
14 | 8 13 6 8 10 4 7 5 9 19 3 | 27 23 23 24 25 24 24 26 26 18 23
15E | 13 21 8 19 12 5 10 6 8 18 4 | 78 78 76 78 80 76 75 78 76 79 76
16 | 6 16 6 13 9 3 11 7 6 24 3 | 23 25 23 26 24 24 25 25 24 29 23
17E | 7 12 9 11 13 4 7 4 5 15 3 | 35 36 35 41 44 36 37 37 39 31 36
X18 | 18 11 73 10 --- 8 9 10 7 --- 5 | 76 72 68 76 --- 74 73 71 76 --- 74
19E | 8 13 8 9 14 6 10 5 9 16 3 | 50 47 51 51 46 50 49 50 47 50 48
20 | 9 11 6 8 10 3 7 6 6 22 3 | 25 25 24 26 22 23 26 23 22 21 22
21 | 7 11 6 7 6 3 6 6 7 21 2 | 23 24 23 26 24 22 26 21 24 19 22
22 | 8 15 5 10 10 4 8 4 7 17 3 | 27 32 31 31 28 29 31 30 28 26 28
23 | 8 22 9 8 13 4 9 5 9 24 4 | 63 64 61 62 67 62 64 62 63 62 62
24 | 6 9 7 7 9 3 7 4 6 8 2 | 19 26 23 20 21 21 27 20 19 21 20
25 | 7 11 10 7 13 3 7 5 7 7 3 | 24 26 26 24 21 23 27 26 21 22 23
26 | 7 10 8 9 10 3 8 6 9 13 3 | 23 24 23 24 21 23 27 22 22 22 22
27E | 6 15 12 9 9 3 11 7 9 11 3 | 20 27 20 25 24 22 24 24 22 24 22
28 | 8 9 7 8 7 3 5 5 9 21 3 | 27 31 25 28 23 25 28 26 28 28 25
29E | 11 19 8 8 11 5 9 6 6 16 3 | 44 43 43 45 44 43 43 43 45 43 43
30 | 7 10 7 9 5 3 7 5 9 19 2 | 24 32 25 23 22 24 30 25 23 28 24
31 | 9 14 6 9 10 3 8 6 8 22 3 | 43 47 46 50 43 46 48 42 46 40 44
32 | 12 14 13 12 11 3 11 6 9 11 3 | 849 532 853 854 530 852 849 850 848 850 851
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 9 10 11 4 8 6 8 17 |T 58 51 58 60 47 58 60 58 58 57 57
WRMS | 8 14 9 9 10 4 8 6 7 17 |NE 29 31 29 30 25 28 31 29 29 25 28
MEDI | 8 13 8 9 10 3 8 6 8 16 |MD 27 29 25 26 24 25 28 26 25 26 25
Table 3.2095.4 GPS week: 2095 Day: 4 MJD: 58913.000
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 8 8 9 4 4 7 7 5 10 2 | 20 24 22 23 22 20 24 21 18 17 20
2 | 11 7 7 8 8 4 6 6 7 19 3 | 20 21 21 20 21 18 21 23 19 19 19
3 | 9 11 11 9 7 5 9 8 7 9 3 | 24 25 25 24 25 23 24 21 22 19 22
X4 | 12 --- 16 14 --- 6 24 11 13 50 8 | 40 --- 41 43 --- 42 43 44 44 46 41
5 | 17 11 8 7 14 4 7 9 8 14 3 | 32 30 25 25 26 26 28 28 27 23 25
6 | 11 5 7 8 6 4 6 7 6 7 2 | 26 29 26 24 27 24 31 28 25 23 25
7 | 6 11 5 6 8 3 6 7 4 27 3 | 62 65 65 63 63 62 67 62 64 56 63
8E | 8 15 12 13 13 4 12 8 9 16 4 | 23 27 23 22 29 23 26 27 22 25 23
9 | 11 11 12 9 7 5 10 8 8 15 3 | 49 50 48 46 46 48 50 48 49 47 48
10 | 11 12 13 6 7 3 9 9 7 10 3 | 26 21 26 22 27 21 23 22 19 23 21
11 | 9 13 17 18 9 5 8 8 8 19 4 | 26 31 19 35 26 25 28 25 24 26 24
12 | 9 20 6 8 10 3 8 9 7 23 3 | 41 44 37 40 43 38 40 38 41 34 38
13 | 9 15 7 7 7 4 9 9 7 18 3 | 22 25 20 23 22 20 26 24 23 18 20
14 | 9 13 5 13 11 4 9 9 8 17 3 | 39 37 37 42 40 36 36 41 34 31 36
15E | 15 11 8 12 8 4 10 9 10 22 4 | 52 50 49 46 46 49 48 48 52 52 48
16 | 9 15 4 9 8 3 7 9 6 27 3 | 32 35 34 33 37 34 36 36 32 36 33
17E | 9 12 8 11 13 4 9 8 8 14 3 | 43 41 39 44 48 40 42 43 40 35 41
X18 | 12 10 14 16 --- 5 8 12 8 --- 4 | 118 118 125 121 --- 115 109 122 111 --- 116
19E | 10 12 8 14 17 6 9 9 10 16 4 | 50 51 51 48 48 52 50 49 51 53 49
20 | 15 10 7 6 8 3 7 9 6 21 3 | 35 30 27 31 30 29 30 29 29 32 28
21 | 6 10 5 11 6 4 5 11 8 21 3 | 24 23 22 26 22 21 24 23 23 21 21
22 | 9 13 7 11 8 4 8 8 6 19 3 | 43 44 39 43 42 41 43 42 41 41 41
23 | 12 25 10 9 11 5 9 11 6 22 4 | 88 90 85 85 82 85 85 85 85 82 85
24 | 10 10 5 8 7 3 7 9 6 12 3 | 27 30 24 26 23 23 31 24 27 28 25
25 | 14 12 9 8 12 3 7 10 6 7 3 | 51 49 45 47 46 45 48 48 48 46 47
26 | 8 11 8 8 7 3 6 9 7 13 3 | 30 35 35 32 36 32 37 36 31 36 33
27E | 11 17 14 8 13 3 12 8 8 10 4 | 27 28 20 25 26 24 28 27 23 22 23
28 | 7 9 6 8 7 3 7 7 7 20 3 | 31 35 30 33 32 31 34 32 34 30 31
29E | 11 16 9 13 14 4 9 7 8 17 4 | 52 51 52 50 54 51 51 52 51 52 51
30 | 8 7 5 8 6 3 7 6 5 12 2 | 25 33 28 26 27 26 34 28 29 27 28
31 | 8 13 6 10 8 4 8 8 8 24 3 | 63 63 61 66 62 63 66 65 61 61 62
32 | 11 16 14 11 9 3 10 9 7 10 3 | 995 810 995 994 810 996 995 994 995 997 995
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 9 10 10 4 8 9 7 17 |T 69 65 68 69 62 68 70 69 68 66 68
WRMS | 10 13 9 9 9 4 8 8 6 15 |NE 37 38 36 37 33 35 38 37 35 31 35
MEDI | 9 12 8 9 8 4 8 9 7 17 |MD 32 35 34 33 32 32 36 36 32 32 33
Table 3.2095.5 GPS week: 2095 Day: 5 MJD: 58914.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 7 9 11 4 4 6 12 7 10 2 | 15 21 18 20 20 17 23 23 17 16 17
2 | 8 13 12 8 8 4 5 12 8 20 3 | 20 21 21 20 19 17 19 24 19 21 17
3 | 4 10 13 9 7 5 7 13 7 10 3 | 19 20 23 18 23 19 23 25 19 20 19
X4 | 11 --- 15 16 --- 6 22 16 14 51 8 | 31 --- 36 35 --- 34 36 39 40 50 35
5 | 8 10 7 6 14 3 6 16 6 17 3 | 29 34 27 28 32 28 32 35 29 24 28
6 | 5 27 11 9 6 4 6 13 8 6 3 | 22 34 24 22 23 22 25 24 20 20 21
7 | 5 11 7 8 9 4 6 11 5 29 3 | 30 32 31 33 31 31 32 33 30 32 30
8E | 8 12 17 13 9 4 10 11 10 20 4 | 21 24 26 23 29 23 26 31 24 29 23
9E | 10 11 12 12 9 5 8 14 8 14 3 | 60 62 59 59 63 60 62 58 62 65 61
10 | 8 14 15 8 8 3 9 17 5 7 3 | 19 19 22 20 23 18 21 22 18 17 18
11 | 8 12 18 14 9 4 8 12 6 13 4 | 17 25 17 26 21 19 26 26 19 20 19
12 | 7 17 8 8 13 3 5 16 8 22 3 | 26 32 27 26 26 26 31 29 30 19 26
13 | 7 20 9 10 12 3 9 15 9 18 4 | 25 31 25 25 25 24 29 32 27 23 24
14 | 4 11 6 10 8 4 7 16 8 16 3 | 25 26 24 27 25 23 26 31 27 18 24
15E | 9 14 8 13 10 4 10 18 6 19 4 | 64 62 61 61 61 62 62 62 64 65 62
16 | 7 13 5 11 8 3 8 15 8 25 3 | 19 21 19 20 25 19 21 26 21 23 18
17E | 6 10 9 14 13 4 8 13 10 15 3 | 42 41 38 46 42 40 43 48 39 37 41
X18 | 17 12 15 13 --- 5 --- 17 7 --- 6 | 55 51 44 52 --- 49 --- 59 50 --- 50
19E | 6 12 9 24 11 4 8 13 13 16 4 | 36 40 39 34 37 38 41 41 41 43 38
20 | 8 10 11 8 9 5 7 16 5 21 3 | 22 22 21 23 27 22 22 27 22 26 21
21 | 7 10 7 9 8 4 6 17 5 21 3 | 19 18 17 20 18 16 20 22 17 19 16
22 | 7 16 10 9 9 5 6 14 8 17 3 | 21 24 22 27 24 21 25 26 23 20 22
23E | 12 24 9 9 11 5 7 16 10 24 4 | 59 60 57 55 60 57 57 57 61 56 58
24 | 8 10 7 12 8 3 7 17 8 10 3 | 23 27 21 23 20 21 28 23 19 21 21
25 | 5 11 10 10 10 4 6 16 6 6 3 | 19 25 24 23 24 20 26 22 19 17 20
26 | 6 10 7 8 7 4 6 15 8 14 3 | 28 32 28 28 33 28 30 32 31 31 28
27E | 8 13 15 15 10 3 12 12 6 17 4 | 21 25 19 16 23 20 27 29 24 28 20
28 | 6 10 9 8 7 3 5 12 8 20 3 | 20 27 17 23 24 21 24 25 23 25 21
29E | 9 14 9 11 9 4 8 15 8 16 3 | 54 55 56 58 55 56 56 61 57 58 55
30 | 6 6 7 8 9 3 7 9 8 17 3 | 20 25 23 20 21 20 27 24 20 23 20
31 | 7 14 7 9 6 3 7 16 8 27 3 | 50 53 49 49 46 50 54 50 54 46 49
32E | 17 16 15 11 9 7 10 18 8 9 4 | 583 490 582 587 492 583 581 586 580 581 583
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 10 11 9 4 8 15 8 18 |T 47 47 47 48 46 47 50 51 48 48 47
WRMS | 7 14 10 11 8 4 8 15 7 16 |NE 24 28 25 26 25 24 27 29 25 24 24
MEDI | 7 12 9 10 9 4 7 15 8 17 |MD 23 27 24 26 25 23 27 29 24 24 23
Table 3.2095.6 GPS week: 2095 Day: 6 MJD: 58915.000
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 8 9 10 6 4 6 7 9 10 2 | 19 21 20 17 22 17 23 20 20 18 18
2 | 10 8 10 9 8 3 9 7 8 18 3 | 25 19 22 23 20 19 20 21 18 21 19
3 | 9 12 11 7 8 3 9 9 6 8 3 | 22 22 26 22 25 22 23 24 22 19 21
X4 | 13 --- 16 13 --- 6 28 10 20 47 8 | 54 --- 52 57 --- 53 52 59 62 58 54
5 | 9 14 7 6 13 4 9 8 5 15 3 | 30 35 30 31 36 31 32 32 33 31 30
6 | 6 8 8 8 5 2 7 10 7 9 2 | 24 25 24 26 25 23 28 25 25 26 24
7 | 7 11 5 6 12 3 7 6 7 26 3 | 53 53 54 50 51 52 56 54 53 50 52
8E | 7 16 14 10 15 4 11 6 11 16 4 | 26 24 26 23 33 25 26 22 28 26 24
9E | 11 16 12 9 9 3 10 9 8 13 3 | 56 62 57 57 65 58 59 66 61 58 59
10 | 5 10 13 6 10 3 9 10 7 9 3 | 23 21 28 23 24 22 24 23 22 23 21
11 | 5 13 17 13 7 4 8 10 7 15 3 | 23 28 20 26 25 23 29 23 24 23 22
12 | 7 18 6 7 13 3 11 7 7 22 3 | 27 36 29 27 27 26 33 30 29 21 27
13 | 8 14 7 10 11 3 9 8 12 16 3 | 33 34 30 29 27 31 35 37 37 33 31
14 | 6 11 7 8 12 5 9 8 8 17 3 | 30 30 29 31 32 29 30 35 30 26 29
15E | 11 16 7 10 10 4 15 11 16 20 4 | 45 44 45 47 46 45 45 51 47 48 45
16 | 8 14 6 11 13 2 7 8 7 26 3 | 23 24 23 24 27 22 24 26 24 27 21
17E | 8 13 8 11 9 5 11 11 8 16 3 | 40 36 35 45 44 38 40 36 36 34 37
X18 | 17 12 11 11 --- 6 10 9 11 --- 5 | 56 46 44 47 --- 47 61 41 45 --- 46
19E | 8 16 8 20 8 4 12 9 7 15 4 | 40 45 43 36 43 41 45 43 43 49 42
20 | 7 9 7 4 9 3 10 9 8 18 3 | 26 26 25 27 30 27 27 29 25 28 25
21 | 8 10 8 7 7 4 11 11 10 20 3 | 17 20 20 20 19 19 23 19 23 21 18
22 | 10 15 8 8 9 4 8 8 6 18 3 | 30 33 30 32 30 29 32 32 30 30 30
23E | 9 26 10 10 10 5 11 10 10 22 4 | 48 55 47 51 53 48 50 54 47 45 49
24 | 7 10 11 9 10 1 9 7 11 9 3 | 20 24 21 23 20 20 25 22 21 20 19
25 | 7 12 10 8 12 3 9 9 10 9 3 | 23 27 25 28 23 23 27 28 24 21 22
26 | 9 9 8 7 9 2 6 9 7 13 3 | 32 35 33 34 36 32 37 33 33 37 32
27E | 8 13 15 10 10 3 12 6 8 11 3 | 25 25 18 19 25 22 26 21 26 24 21
28 | 7 10 8 7 8 3 11 7 8 25 3 | 21 26 20 20 20 20 23 24 26 29 20
29E | 9 20 11 11 13 5 9 8 13 18 4 | 65 64 65 61 68 63 62 57 63 67 62
30 | 7 10 6 8 10 3 7 5 6 13 2 | 22 28 25 19 23 22 28 26 25 22 22
31 | 7 12 7 7 8 4 8 7 7 24 3 | 70 73 72 72 67 72 75 72 72 66 70
32E | 8 9 11 8 7 5 11 9 10 11 3 | 824 664 822 828 662 826 825 823 823 827 825
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 9 10 4 10 8 9 17 |T 58 55 58 58 54 57 60 59 59 58 57
WRMS | 8 13 9 9 9 4 10 8 7 15 |NE 30 31 30 30 29 29 33 31 31 29 29
MEDI | 8 12 8 8 9 3 9 8 8 16 |MD 27 30 29 28 27 27 30 30 29 28 27
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2095 GPS week: 2095 MJD: 58909.0-58915.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 |U 0 0 0 |U 0 0 0 |U 9 15 23 |
emr | emr 2962 | 0 0 0 |U 0 0 0 |U 19 19 30 |
esa | esa 3072 | 0 0 0 |U 0 0 0 | 12 15 20 |
gfz | gfz 3071 |U 0 0 0 |U 0 0 0 |U 9 13 20 |
grg | grg 2863 |U 0 0 0 |U 0 0 0 | 11 14 26 |
igr | igr 3061 | 0 0 0 | 0 0 0 | 10 15 21 |
igs | igs 3058 | 0 0 0 | 0 0 0 | 11 15 20 |
jpl | jpl 3058 |U 0 0 0 | 0 0 0 |U 19 26 36 |
mit | mit 3072 | 0 0 0 |U 0 0 0 |U 34 21 46 |
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 5.2095.0 GPS week: 2095 Day: 0 MJD: 58909.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | ---- ---- ---- | 7 12 14 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 19 23 22 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 12 16 18 |
gfz | gfz 3070 | ---- ---- ---- | ---- ---- ---- | 8 15 13 |
grg | grg 2877 | ---- ---- ---- | ---- ---- ---- | 10 19 20 |
igr | igr 3072 | ---- ---- ---- | ---- ---- ---- | 10 15 15 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 10 16 14 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | 17 27 33 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 9 13 15 |
Table 5.2095.1 GPS week: 2095 Day: 1 MJD: 58910.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | ---- ---- ---- | ---- ---- ---- | 11 12 19 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 24 18 22 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 14 15 19 |
gfz | gfz 3071 | ---- ---- ---- | ---- ---- ---- | 11 11 20 |
grg | grg 2780 | ---- ---- ---- | ---- ---- ---- | 13 13 25 |
igr | igr 3069 | ---- ---- ---- | ---- ---- ---- | 13 14 18 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 13 14 15 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | 19 23 30 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 30 26 74 |
Table 5.2095.2 GPS week: 2095 Day: 2 MJD: 58911.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 | ---- ---- ---- | ---- ---- ---- | 10 16 20 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 20 21 24 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 14 19 20 |
gfz | gfz 3070 | ---- ---- ---- | ---- ---- ---- | 9 15 14 |
grg | grg 2878 | ---- ---- ---- | ---- ---- ---- | 10 16 26 |
igr | igr 3066 | ---- ---- ---- | ---- ---- ---- | 11 19 20 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 12 18 18 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | 20 29 38 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 25 39 65 |
Table 5.2095.3 GPS week: 2095 Day: 3 MJD: 58912.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | ---- ---- ---- | 9 17 30 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 19 20 40 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 11 13 19 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 9 15 26 |
grg | grg 2876 | ---- ---- ---- | ---- ---- ---- | 10 15 32 |
igr | igr 3011 | ---- ---- ---- | ---- ---- ---- | 9 17 26 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 10 16 26 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | 18 27 35 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 17 12 33 |
Table 5.2095.4 GPS week: 2095 Day: 4 MJD: 58913.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | ---- ---- ---- | 10 15 22 |
emr | emr 2975 | ---- ---- ---- | ---- ---- ---- | 20 17 31 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 14 16 20 |
gfz | gfz 3071 | ---- ---- ---- | ---- ---- ---- | 8 10 16 |
grg | grg 2878 | ---- ---- ---- | ---- ---- ---- | 10 11 23 |
igr | igr 3069 | ---- ---- ---- | ---- ---- ---- | 11 14 20 |
igs | igs 3071 | ---- ---- ---- | ---- ---- ---- | 11 15 19 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | 21 27 41 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 11 15 24 |
Table 5.2095.5 GPS week: 2095 Day: 5 MJD: 58914.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | ---- ---- ---- | 9 16 25 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 15 18 30 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 11 13 22 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 7 10 24 |
grg | grg 2878 | ---- ---- ---- | ---- ---- ---- | 10 13 25 |
igr | igr 3072 | ---- ---- ---- | ---- ---- ---- | 9 13 23 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 10 14 24 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 18 24 42 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 140 28 80 |
Table 5.2095.6 GPS week: 2095 Day: 6 MJD: 58915.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 | ---- ---- ---- | ---- ---- ---- | 9 15 29 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 18 18 40 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 11 14 20 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 8 12 24 |
grg | grg 2880 | ---- ---- ---- | ---- ---- ---- | 11 12 30 |
igr | igr 3072 | ---- ---- ---- | ---- ---- ---- | 9 14 24 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 10 14 26 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | 18 24 31 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 10 16 30 |
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 6.2095 GPS week: 2095 MJD: 58909.500-58915.500
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 | -5 -14 86 -82 1 | 11 22
| 13 10 47 39 7 | 4
emr uuuux | 9 24 -125 83 -14 | 42 46
| 15 20 26 61 20 | 4
esa uuuuu | -10 4 70 -165 -3 | 36 41
| 19 12 58 43 5 | 3
gfz uuuuu | 12 -7 70 26 -3 | 19 29
| 19 26 115 163 7 | 3
grg uuuuu | 14 30 -2 -5 1 | 0 17
| 24 15 38 47 5 | 2
igr xxxxx | 24 22 -16 10 -1 | -1 20
| 5 14 34 40 4 | 3
irf xxxxx | 4 -21 -6 0 -2 | 3 21
| 12 7 16 27 7 | 4
jpl uuuuu | -8 -11 -83 81 2 | 40 45
| 14 8 52 48 13 | 3
mit uuuuu | 18 -19 -27 14 1 | 21 29
| 24 12 44 62 8 | 4
ngs uuuuu | -21 26 -27 86 -3 | 15 24
| 27 37 95 171 5 | 3
sio uuuux | -8 -26 41 -7 6 | 42 47
| 25 37 46 55 6 | 6
Table 7.2095.0 GPS week: 2095 Day: 0 MJD: 58909.500
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 | -22 -22 82 -120 6 | 6 23
emr uuuux | 0 17 -157 -10 -7 | 40 47
esa uuuuu | -26 7 77 -172 -7 | 35 42
gfz uuuuu | 33 37 50 39 4 | 17 28
grg uuuuu | 27 18 -49 41 -2 | -3 19
igr xxxxx | 18 28 -58 37 1 | -3 22
irf xxxxx | -2 -26 11 -38 5 | -1 23
jpl uuuuu | -7 -22 -150 135 -16 | 39 45
mit uuuuu | 9 -22 37 -62 6 | 16 27
ngs uuuuu | -4 4 12 221 -3 | 12 25
sio uuuux | -10 25 63 -69 8 | 34 41
Table 7.2095.1 GPS week: 2095 Day: 1 MJD: 58910.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 8 -14 132 -46 5 | 5 22
emr uuuux | -10 29 -118 67 2 | 39 45
esa uuuuu | -23 18 49 -128 -9 | 33 40
gfz uuuuu | 30 -16 -13 -39 -16 | 17 28
grg uuuuu | -7 5 -48 42 -2 | -2 19
igr xxxxx | 17 36 4 62 -7 | -4 22
irf xxxxx | -6 -11 -8 -35 6 | -2 23
jpl uuuuu | -29 1 -49 12 10 | 36 41
mit uuuuu | 8 -23 -12 -81 8 | 16 27
ngs uuuuu | 21 39 -50 214 2 | 11 24
sio uuuux | 5 -20 57 30 10 | 35 42
Table 7.2095.2 GPS week: 2095 Day: 2 MJD: 58911.500
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 -28 69 -91 4 | 8 20
emr uuuux | 10 -12 -116 122 2 | 42 46
esa uuuuu | 15 0 94 -247 -2 | 34 40
gfz uuuuu | -17 -35 -37 -185 -3 | 17 28
grg uuuuu | -14 41 16 -19 -7 | -1 17
igr xxxxx | 23 13 22 -52 -1 | -3 20
irf xxxxx | 5 -22 -32 13 3 | 2 20
jpl uuuuu | -1 -7 -22 120 6 | 38 43
mit uuuuu | 34 -2 -92 59 7 | 19 27
ngs uuuuu | -27 80 38 199 3 | 13 23
sio uuuux | 11 -79 85 15 11 | 39 43
Table 7.2095.3 GPS week: 2095 Day: 3 MJD: 58912.500
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 -4 90 -131 -5 | 15 22
emr uuuux | -3 37 -107 55 -12 | 48 52
esa uuuuu | -32 11 86 -122 4 | 39 44
gfz uuuuu | -8 -29 40 -165 1 | 22 31
grg uuuuu | 6 29 -27 -95 0 | 3 17
igr xxxxx | 25 34 9 6 2 | 3 19
irf xxxxx | 1 -17 -18 -5 -3 | 8 21
jpl uuuuu | 1 -15 -79 124 10 | 43 48
mit uuuuu | 28 -24 -61 15 6 | 25 32
ngs uuuuu | -5 27 67 238 -2 | 19 27
sio uuuux | -32 4 -50 34 13 | 47 50
Table 7.2095.4 GPS week: 2095 Day: 4 MJD: 58913.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -23 -16 157 -102 10 | 14 22
emr uuuux | 24 52 -101 58 -1 | 45 48
esa uuuuu | -9 -9 157 -146 -5 | 39 44
gfz uuuuu | 16 21 21 117 -4 | 22 31
grg uuuuu | 6 50 33 0 1 | 2 16
igr xxxxx | 30 31 1 19 -2 | 2 19
irf xxxxx | 25 -15 8 25 -11 | 7 20
jpl uuuuu | 4 -5 -41 37 0 | 44 48
mit uuuuu | 59 -7 -39 41 -6 | 26 32
ngs uuuuu | -61 -39 -146 -1 -9 | 18 26
sio uuuux | 25 -14 18 64 0 | 48 52
Table 7.2095.5 GPS week: 2095 Day: 5 MJD: 58914.500
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 | 5 -14 18 -38 -3 | 15 22
emr uuuux | 30 23 -109 110 -33 | 42 45
esa uuuuu | -6 -15 60 -151 -5 | 37 42
gfz uuuuu | 21 -14 125 229 -7 | 19 29
grg uuuuu | 21 39 16 -22 8 | 1 16
igr xxxxx | 27 4 -34 33 -3 | 1 19
irf xxxxx | -8 -24 9 30 -12 | 5 20
jpl uuuuu | 3 -18 -153 84 19 | 42 47
mit uuuuu | -14 -16 14 79 -10 | 25 31
ngs uuuuu | -40 28 51 -131 -8 | 17 26
sio uuuux | -7 -33 41 -56 2 | 48 51
Table 7.2095.6 GPS week: 2095 Day: 6 MJD: 58915.500
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 | -5 1 55 -43 -9 | 12 20
emr uuuux | 15 19 -166 182 -49 | 36 40
esa uuuuu | 12 14 -35 -188 1 | 33 38
gfz uuuuu | 11 -14 303 185 2 | 16 25
grg uuuuu | 58 25 43 17 7 | -2 14
igr xxxxx | 27 5 -59 -33 4 | -3 17
irf xxxxx | 13 -31 -14 8 -5 | 0 18
jpl uuuuu | -26 -11 -88 53 -15 | 41 46
mit uuuuu | 0 -37 -33 45 -7 | 21 28
ngs uuuuu | -31 41 -162 -138 -1 | 12 20
sio uuuux | -46 -65 75 -67 -4 | 46 50
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