[IGSREPORT-23107] Wk 1814 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Oct 30 08:52:12 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1814 (Oct 12, 2014 - Oct 18, 2014)
Contacts: igs.acc at noaa.gov
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:
igs1814[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1814[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1814[0-6].cls IGS GPS clock combination summary report.
igs18147.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18147.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 | 32 32
0 | EMR | 10
0 | ESA | 32 32
0 | GFZ | 1 2 6 30 1 6 30 IISC IISC
0 | GRG | 10 BOR1 SOFI BOR1 GRAZ SOFI
0 | JPL | 32
0 | MIT | 4 11 21 25 4 10 11 21 25 27 FLIN MDVJ MONP
1 | COD | 32 32
1 | EMR | 10
1 | ESA | 32 32
1 | GFZ | 1 6 30 32 1 6 30 32 IISC RESO THU3 CUSV IISC RESO
1 | GFZ | THU3
1 | GRG | 10 TLSE KOUR TLSE
1 | JPL | 8 18 32
1 | MIT | 26 10 18 26 BAKO TLSE BAKO KOUR MDVJ TLSE
2 | COD | 3 3 32 HOB2 HOB2
2 | EMR | 10
2 | ESA | 3 32 3 32 HOB2 KOUR NRIL HOB2 KOUR NRIL TIXI
2 | GFZ | 1 2 6 30 1 6 30 32 FAIR MAC1 SCOR FAIR MAC1 SCOR
2 | GRG | 10 DAV1 GRAZ HOB2 HYDE DAV1 GRAZ HOB2 HYDE KELY
2 | JPL | 10 18 32 PIMO
2 | MIT | 3 32 3 10 32 KOUR BAKO KOUR MDVJ
3 | COD | 32 3 32 TLSE
3 | EMR | 10 TLSE
3 | ESA | 32 3 32 UNSA
3 | GFZ | 1 3 6 30 32 1 6 13 30 32 CAS1 CAS1 IRKJ NYA1
3 | GRG | 3 10 13 GRAZ GRAZ ONSA
3 | MIT | 3 3 10 11 28 32
4 | COD | 3 KARR TRO1 GUAM KARR TRO1
4 | EMR | 10 32 10 32
4 | ESA | 3 3 TRO1 UNSA
4 | GFZ | 1 6 30 1 6 30 MCM4 NYA1 MCM4 NYA1
4 | GRG | 3 32 3 10 32 GRAZ KARR SOFI USNO GRAZ KARR SOFI USNO
4 | JPL | 10 32 HOFN
4 | MIT | 1 2 3 4 6 8 12 18 19 22 23 27 30 32 1 2 3 4 6 8 10
4 | MIT | 12 18 19 22 23 27 30 32 KOUR ALGO HNPT KOUR
5 | COD | 10 KARR HOB2 KARR
5 | EMR | 32 32 HOB2
5 | ESA | 3 10 CHUR PIMO CHUR HOB2 PIMO
5 | GFZ | 1 2 6 30 32 1 6 10 30 32 REUN BAKE REUN
5 | GRG | 32 32 GRAZ MOBS REUN GRAZ MAL2 MOBS
5 | JPL | 32
5 | MIT | 3 32 32 TLSE KOUR MDVJ TLSE
6 | COD | 32 3 10 32
6 | ESA | 3 32 3 10 32
6 | GFZ | 1 2 6 9 30 32 1 2 6 10 30 32 AREQ NRIL ALRT AREQ
6 | GFZ | MAW1 NRIL
6 | GRG | 3 3 GOPE GRAZ GOPE GRAZ
6 | JPL | 32
6 | MIT | 3 21 3 21
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
----+--------+---------------
1 | COD | 3
2 | GRG | 3
3 | GRG | 3
4 | GRG | 3
5 | GRG | 3
6 | GRG | 3
7. 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.
8. 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 | -.8 .0 -.2 -52 7 2 .05
EMR | 0 | -1.0 5.0 2.6 -12 26 -14 -.18
ESA | 0 | .1 .5 -1.9 0 8 64 -.21
GFZ | 0 | -.2 .6 -2.2 -2 -69 18 .19
GRG | 0 | 5.1 13.4 -1.6 -18 36 -20 .34
JPL | 0 | -.2 9.2 14.5 -63 15 35 -.55
MIT | 0 | -.6 7.3 -6.6 -5 9 -27 .01
NGS | 0 | .5 1.5 3.1 16 -10 10 .72
SIO | 0 | 1.5 6.1 -5.9 -7 16 6 .13
COD | 1 | .2 .0 -.2 -55 -7 -22 -.03
EMR | 1 | 1.5 6.9 1.3 -17 25 -1 -.17
ESA | 1 | .0 .4 -1.9 5 11 58 -.09
GFZ | 1 | .5 .6 -1.3 2 -69 28 .06
GRG | 1 | 4.3 .7 -.6 -23 63 -12 .40
JPL | 1 | 1.0 9.5 9.7 -81 13 -6 -.08
MIT | 1 | -4.0 5.9 -5.1 -2 10 -26 .10
NGS | 1 | 8.3 2.3 3.9 21 -41 56 .67
SIO | 1 | -1.9 .7 -10.6 -2 3 21 -.03
COD | 2 | .0 .0 -.4 -54 10 12 -.02
EMR | 2 | -.9 8.5 2.5 -16 24 5 .01
ESA | 2 | -.2 -.6 -1.6 33 -42 70 .08
GFZ | 2 | .0 .3 -1.8 0 -12 24 .13
GRG | 2 | 3.1 14.7 6.9 -24 61 -13 .23
JPL | 2 | -3.3 1.2 1.7 -73 15 -20 -.16
MIT | 2 | -.2 7.1 -3.2 2 5 -27 .09
NGS | 2 | -7.6 -4.3 -3.8 12 44 -53 .59
SIO | 2 | 1.2 .8 -17.1 -19 1 8 -.04
COD | 3 | -.5 .2 -.5 -42 0 17 .17
EMR | 3 | -.3 .3 -.8 -26 25 -5 .20
ESA | 3 | .1 .2 -2.1 -10 -24 50 .07
GFZ | 3 | .2 .7 -2.0 -14 -83 14 .03
GRG | 3 | 1.7 4.1 .8 -30 57 4 .67
JPL | 3 | -.7 1.6 5.2 -82 -18 -18 .25
MIT | 3 | -2.1 5.1 -5.5 -4 9 -34 .19
NGS | 3 | .8 -8.9 4.8 -14 -7 -12 .79
SIO | 3 | 4.9 -.2 -17.3 -14 -14 24 .15
COD | 4 | -.6 .1 -.2 -29 5 3 .29
EMR | 4 | 3.9 6.8 6.6 -28 27 -2 -.01
ESA | 4 | .5 .5 -2.2 5 -12 57 .17
GFZ | 4 | -.1 .5 -2.1 -3 -81 22 .31
GRG | 4 | 5.2 7.5 -6.0 -25 33 4 .65
JPL | 4 | 6.6 7.1 10.1 -69 14 9 .08
MIT | 4 | -.1 2.4 -.6 -7 5 -26 .29
NGS | 4 | -3.2 -4.1 3.3 -4 9 -29 .72
SIO | 4 | 2.6 1.6 -11.9 -3 1 4 .21
COD | 5 | -.5 -.9 -.8 -56 3 -7 .18
EMR | 5 | 1.5 3.1 -1.3 -17 30 -13 .04
ESA | 5 | .0 -.2 -2.1 -4 -9 38 .03
GFZ | 5 | -.7 .4 -2.4 -15 -67 14 .30
GRG | 5 | 4.0 7.7 2.9 -37 42 7 .40
JPL | 5 | 8.4 3.4 8.9 -77 -56 33 .18
MIT | 5 | -1.9 4.5 -3.9 -1 7 -25 .30
NGS | 5 | -.7 -8.0 -9.4 26 29 -28 .85
SIO | 5 | 1.4 .1 -14.4 -1 2 1 .28
COD | 6 | -1.6 -.5 -1.4 -53 13 14 .24
EMR | 6 | 5.0 2.9 -1.2 -11 26 -6 .01
ESA | 6 | .7 .0 -1.9 8 -9 52 .12
GFZ | 6 | -.4 .6 -2.2 -16 -83 -6 .33
GRG | 6 | 3.1 11.9 -1.3 -36 32 -30 .63
JPL | 6 | 1.8 10.8 6.8 -90 2 64 .19
MIT | 6 | -2.1 5.7 -3.7 1 9 -32 .30
NGS | 6 | -3.0 -4.6 2.0 -2 11 -32 .63
SIO | 6 | -1.0 -.1 -12.4 -10 17 3 .39
9. 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.
10. 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.
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 1.1814.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1814.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 2.1814.[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 3.1814.[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 5.1814.0-6). 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 1814 summary. (Oct 12, 2014 - Oct 18, 2014)
Table 1.1814.a GPS week: 1814 MJD: 56942.000-56948.000
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 248| 1 0 0 22 9 13 .11 10 10 | -692 -417 15 107
| 0 0 1 16 12 8 .02 | 824 1262
emr 80| 0 0 2 -4 -18 27 .30 13 13 | 1681 -249 17 136
| 1 1 1 11 12 13 .03 | 1281 998
esa 150| 0 0 2 -4 -9 -6 -.29 12 12 | -995 -311 14 156
| 0 0 1 15 14 14 .02 | 198 1751
gfz 199| 0 1 4 9 -33 7 -.07 15 14 | 195 -299 16 155
| 1 0 1 15 8 14 .03 | 176 538
grg 173| 0 0 2 -4 16 -32 .27 16 15 | 88 -146 18 133
| 0 0 2 10 13 21 .04 | 225 405
igr n/a| 0 0 1 4 1 -1 -.18 6 5 | 2262 -430 16 103
| 0 0 1 9 15 10 .02 | 1221 914
jpl 80| 0 0 1 -42 -3 -11 .12 13 12 | 1471 -224 17 126
| 1 1 0 19 15 18 .02 | 1388 1060
mit 350| 0 -1 -3 -24 -23 -13 -.10 15 12 | 36 8 25 216
| 0 0 1 22 24 11 .03 | 1001 2490
ngs 228| 0 0 -4 30 66 1 -.01 13 11 | -423 -1214 1394 2969
| 1 1 3 48 43 23 .05 | 475 1340
sio 476| 0 0 -4 -3 -9 0 -.43 14 13 | --- --- --- ---
| 0 0 1 18 31 34 .04 | --- ---
Table 1.1814.b GPS week : 1814 MJD: 56942.000-56948.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 3 4 4 3 |
2 | 7 6 6 6 6 6 6 |
3 | 14 13 16 14 11 12 13 |
4 | 4 4 3 4 4 4 4 |
5 | 4 5 5 5 5 5 5 |
6 | 4 4 4 4 4 4 4 |
7 | 5 5 5 4 5 4 5 |
8 | 4 4 5 5 5 5 5 |
9 | 8 8 8 8 7 8 7 |
10 | 5 5 6 6 5 5 6 |
11 | 4 4 4 4 4 4 4 |
12 | 5 6 6 6 6 5 5 |
13 | 5 5 5 5 5 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 5 5 6 5 |
18 | 4 4 5 4 4 4 4 |
19 | 5 5 5 5 5 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 5 5 5 5 4 5 4 |
22 | 3 4 4 4 4 4 4 |
23 | 5 6 5 5 6 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 4 5 4 5 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 5 5 5 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 4 5 |
31 | 5 5 5 5 5 5 5 |
32 | 6 6 7 6 6 6 6 |
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 2.1814.0 GPS week: 1814 Day: 0 MJD: 56942.000
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| 2 -1 0 35 13 7 .09 9 9 | -828 442 15 101
emr 80| -1 0 2 10 -4 28 .26 12 12 | 2319 -1489 14 136
esa 150| 0 0 1 11 -32 -9 -.28 12 12 | -864 -2138 12 163
gfz 201| -2 1 4 -4 -34 21 -.02 14 13 | 343 -160 14 152
grg 174| 0 0 1 5 39 -57 .24 16 15 | -77 388 16 121
igr n/a| 0 0 0 4 -6 -13 -.16 6 5 | 3265 -1316 15 94
jpl 80| 0 -2 2 -14 -5 -4 .12 12 12 | 2124 -1255 16 132
mit 350| 0 0 -4 -21 -40 3 -.11 16 12 | -518 3718 27 227
ngs 229| 1 1 -2 -56 87 22 -.02 13 11 | -550 -2939 1485 3038
sio 473| -1 1 -3 2 -1 -19 -.44 15 11 | --- --- --- ---
Table 2.1814.1 GPS week: 1814 Day: 1 MJD: 56943.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 2 -1 0 0 4 4 .08 11 11 | 489 -2065 14 108
emr 80| -2 1 3 -3 -20 40 .28 13 13 | 1152 -460 14 125
esa 150| 0 0 3 -9 -12 -15 -.27 12 12 | -1202 1439 11 153
gfz 203| 0 1 6 1 -37 13 -.10 15 14 | -109 -37 14 159
grg 172| 0 0 0 2 26 -30 .26 15 14 | 10 59 15 130
igr n/a| 0 0 2 -10 12 0 -.21 6 6 | 2194 -949 17 95
jpl 80| -1 0 1 -61 -16 -1 .10 13 12 | 1150 -750 17 137
mit 350| 0 -2 -3 -2 -33 -4 -.07 15 13 | 1681 -3216 29 241
ngs 230| 3 2 -4 67 112 -24 -.04 13 12 | 329 -1516 1121 2815
sio 477| 0 0 -4 18 -19 33 -.40 15 15 | --- --- --- ---
Table 2.1814.2 GPS week: 1814 Day: 2 MJD: 56944.000
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| 2 -1 -1 18 8 8 .12 10 9 | -1958 1394 14 109
emr 80| -1 3 1 0 -24 21 .30 14 14 | 755 -1636 15 142
esa 150| 1 0 2 -19 0 10 -.28 12 12 | -1252 919 11 167
gfz 196| 0 0 5 9 -42 -22 -.04 15 14 | 66 -559 17 163
grg 172| 0 0 5 -11 22 -22 .30 18 16 | 163 -526 19 129
igr n/a| 0 0 2 -4 -5 16 -.17 6 5 | 1318 -1656 17 105
jpl 80| 0 0 1 -56 4 -17 .10 13 12 | 420 -1576 17 143
mit 350| 1 0 -4 -13 -9 -10 -.06 16 14 | -1020 1736 21 200
ngs 228| 0 0 -4 71 29 -31 -.01 13 11 | -155 -2469 1459 2772
sio 475| 0 0 -4 -17 7 47 -.43 15 13 | --- --- --- ---
Table 2.1814.3 GPS week: 1814 Day: 3 MJD: 56945.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 247| 1 0 -1 18 6 18 .10 9 9 | -405 -1330 12 107
emr 80| 0 0 0 0 -13 16 .34 13 13 | -234 856 13 142
esa 150| 0 0 2 -1 12 -8 -.29 12 13 | -1009 147 10 156
gfz 202| 2 1 4 29 -28 7 -.08 15 13 | 182 -1224 14 157
grg 174| 1 1 6 -2 6 -46 .34 17 16 | 131 -646 16 133
igr n/a| 0 0 0 17 31 -13 -.17 6 6 | 297 622 16 107
jpl 80| -2 1 0 -59 26 -41 .10 13 12 | -678 1151 17 131
mit 350| 0 -1 -3 -26 -42 -26 -.09 15 12 | 275 -2341 21 214
ngs 230| 0 -1 0 22 56 2 -.05 12 11 | -1190 1179 1206 3045
sio 475| 0 0 -6 -10 -56 28 -.42 14 14 | --- --- --- ---
Table 2.1814.4 GPS week: 1814 Day: 4 MJD: 56946.000
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 0 21 -13 7 .13 9 9 | -1393 580 20 106
emr 80| 0 1 3 -12 -42 29 .32 13 13 | 1397 732 40 138
esa 150| 0 0 2 -10 -16 15 -.32 12 13 | -950 1378 35 161
gfz 205| 2 2 3 8 -21 14 -.09 15 14 | 181 377 30 159
grg 178| 1 0 -1 -19 8 -36 .24 16 15 | -265 288 34 159
igr n/a| 0 0 1 8 -14 0 -.21 6 5 | 1802 671 17 102
jpl 80| -1 0 1 -37 -9 -11 .13 12 12 | 1119 1029 26 117
mit 350| 0 -1 -1 -30 15 -9 -.12 15 11 | -982 1599 37 242
ngs 231| 0 0 -4 60 65 14 -.02 13 12 | -588 -1231 1484 3124
sio 489| 0 0 -7 -7 24 -35 -.39 15 14 | --- --- --- ---
Table 2.1814.5 GPS week: 1814 Day: 5 MJD: 56947.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 1 0 2 11 23 26 .15 12 12 | 3 -1409 16 109
emr 80| 0 0 1 -24 -14 7 .31 12 12 | 3110 219 13 134
esa 150| 0 0 3 -22 -3 -24 -.30 12 13 | -666 -2956 10 145
gfz 200| 1 1 2 -8 -27 9 -.10 14 13 | 399 120 14 167
grg 173| 0 0 3 7 11 8 .24 17 17 | 438 -173 15 145
igr n/a| 0 0 0 1 2 0 -.18 6 6 | 3570 -70 16 118
jpl 80| 0 -1 1 -48 -17 -20 .16 13 12 | 3111 110 16 114
mit 350| 0 -2 -3 -8 -48 -20 -.11 14 11 | 921 -1412 20 203
ngs 228| 0 0 -11 61 118 30 .09 13 11 | -197 -775 1707 3351
sio 475| 0 1 -3 19 -40 -22 -.47 13 13 | --- --- --- ---
Table 2.1814.6 GPS week: 1814 Day: 6 MJD: 56948.000
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 0 1 52 21 19 .12 10 9 | -752 -537 16 110
emr 80| 0 -1 1 0 -11 48 .29 13 13 | 3268 30 14 138
esa 150| 0 1 0 19 -11 -14 -.27 13 13 | -1024 -969 11 147
gfz 186| 0 2 2 33 -43 7 -.05 16 15 | 309 -611 14 129
grg 173| 0 0 4 -13 2 -44 .26 16 15 | 216 -418 15 117
igr n/a| 0 0 0 10 -7 4 -.16 5 5 | 3389 -317 17 100
jpl 80| 0 -2 1 -16 -3 19 .10 12 12 | 3051 -279 16 109
mit 350| 0 -1 -2 -70 -3 -25 -.11 15 12 | -99 -22 20 187
ngs 224| 0 0 -2 -10 -2 0 -.01 11 9 | -614 -753 1298 2643
sio 468| 0 0 -5 -30 23 -30 -.48 14 12 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1814.0 GPS week: 1814 Day: 0 MJD: 56942.000
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 13 11 10 4 8 8 12 9 3 | 31 35 27 31 35 26 33 29 29 29 30
2 | 11 14 16 19 12 6 10 39 15 19 6 | 34 35 30 37 34 31 31 43 36 29 29
X3E | 23 46 26 26 --- 22 --- 20 29 --- 13 | 105 101 101 94 --- 96 --- 101 115 --- 103
4 | 7 8 12 11 12 4 9 9 11 10 3 | 36 38 33 38 39 33 34 38 36 34 35
5E | 7 13 8 15 14 5 14 14 10 6 4 | 40 38 35 41 39 36 36 43 40 34 37
6 | 9 10 12 12 10 5 10 15 11 8 3 | 32 38 32 32 35 30 38 31 33 32 32
7 | 12 11 12 18 17 4 13 12 9 16 4 | 34 34 28 37 36 27 30 31 30 23 29
8 | 8 7 12 11 16 6 9 9 8 23 4 | 43 42 40 39 41 39 39 41 38 49 40
9 | 20 13 13 24 20 15 15 37 21 37 8 | 61 70 60 51 59 55 70 83 58 83 63
10E | 9 19 12 16 13 6 13 19 16 11 5 | 88 96 89 82 88 84 89 100 88 84 89
11 | 8 9 16 14 15 3 10 9 14 8 4 | 52 55 47 55 61 50 54 56 52 51 52
12E | 11 20 7 15 14 5 20 18 13 13 5 | 25 30 21 26 26 20 27 21 28 20 21
13 | 9 11 14 13 21 5 10 10 13 11 4 | 34 38 28 38 45 32 34 33 30 25 32
14 | 10 12 14 14 14 5 9 11 15 17 4 | 32 36 28 36 39 30 33 30 32 21 30
15 | 8 11 13 15 23 4 12 16 13 14 5 | 30 33 27 30 34 26 29 30 34 26 28
16E | 9 13 8 17 22 6 10 15 21 14 5 | 25 27 23 29 28 23 23 30 31 22 23
17 | 7 13 13 13 12 5 15 12 14 17 4 | 34 38 31 41 40 33 35 38 34 34 34
18E | 9 10 6 12 13 4 8 12 7 9 3 | 35 36 32 38 37 32 33 39 36 30 34
19 | 13 15 12 20 16 4 10 12 14 15 5 | 33 37 30 37 39 32 35 36 32 31 32
20E | 9 9 9 11 14 6 9 12 15 8 3 | 32 32 27 30 29 26 27 29 32 22 28
21 | 7 9 16 15 13 4 10 19 9 14 4 | 37 41 33 41 43 36 38 41 39 32 37
22E | 8 10 7 12 11 4 7 8 11 8 3 | 40 38 33 38 40 35 38 34 39 31 36
23 | 11 13 12 14 19 6 13 17 16 14 5 | 30 34 24 29 34 24 28 27 24 17 24
24 | 7 7 13 11 18 6 12 10 11 16 4 | 24 30 26 23 32 23 30 25 24 18 24
25E | 9 11 15 11 14 4 11 10 12 14 4 | 24 27 31 26 26 24 28 25 31 21 24
26 | 6 7 13 10 17 4 9 12 8 11 3 | 30 32 29 33 34 27 28 36 29 29 29
27 | 7 8 14 16 11 4 10 17 12 13 4 | 41 41 33 40 42 36 45 41 38 36 38
28E | 7 12 9 10 16 4 12 6 9 8 3 | 28 27 24 26 26 22 27 27 25 19 24
29 | 10 13 15 18 14 6 15 16 17 15 5 | 33 34 31 35 33 30 32 31 34 27 29
30 | 7 10 11 9 11 5 13 10 10 9 3 | 30 30 30 26 30 26 36 29 27 27 29
31 | 11 14 14 15 16 6 9 16 12 14 4 | 29 37 23 33 39 25 30 31 28 22 27
32E | 11 20 14 10 23 6 19 20 23 17 6 | 56 56 55 55 58 55 58 67 57 65 56
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 12 14 16 6 12 16 13 15 |T 38 41 35 38 39 35 37 40 38 33 36
WRMS | 9 12 12 13 14 5 12 12 11 11 |NE 35 38 31 36 39 31 36 37 34 32 33
MEDI | 9 11 13 14 14 5 10 12 12 14 |MD 33 36 30 37 37 30 33 33 33 29 30
Table 3.1814.1 GPS week: 1814 Day: 1 MJD: 56943.000
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 14 10 9 3 10 7 9 13 3 | 21 29 20 20 28 18 29 21 23 26 22
2 | 10 12 14 21 12 7 11 37 14 20 6 | 17 23 21 23 21 16 21 36 21 20 16
X3E | 117 25 21 32 --- 15 --- 19 29 --- 12 | 136 90 80 73 --- 88 --- 86 76 --- 83
4 | 9 8 13 9 12 4 7 8 12 11 3 | 21 26 23 22 28 22 26 26 27 23 23
5E | 9 14 7 19 11 4 17 15 12 8 4 | 27 29 22 28 27 23 27 26 27 24 24
6 | 6 8 13 12 9 4 11 13 9 10 3 | 22 27 21 21 26 19 30 20 21 21 22
7 | 11 12 13 16 16 6 13 10 10 15 4 | 26 29 21 26 30 20 22 22 22 15 21
8 | 7 7 10 13 15 5 10 10 9 24 4 | 37 39 38 39 38 37 36 36 38 44 37
9 | 20 14 13 21 18 15 15 34 17 34 7 | 68 75 68 63 66 64 77 90 66 86 71
10E | 10 19 12 16 12 7 16 19 9 10 5 | 66 76 69 65 69 65 74 81 66 66 69
11 | 10 10 16 11 14 5 10 9 12 13 4 | 29 40 31 30 44 30 39 35 37 33 34
12E | 11 21 7 19 13 7 23 18 16 17 6 | 18 26 14 24 22 13 25 15 21 18 14
13 | 11 12 13 12 22 5 12 10 13 13 4 | 25 33 21 28 38 22 28 24 21 19 24
14 | 13 12 11 16 15 6 10 13 18 16 5 | 24 29 23 27 29 20 26 20 21 14 21
15 | 8 11 14 17 16 6 12 15 11 12 4 | 22 26 21 20 26 17 22 23 20 19 19
16E | 11 15 9 19 18 7 10 16 13 13 5 | 23 24 18 26 25 17 19 29 27 20 20
17 | 9 14 13 16 13 4 15 12 14 18 4 | 19 28 21 26 29 19 26 25 24 21 21
18E | 8 11 7 11 23 5 10 12 9 8 4 | 30 28 26 28 29 25 29 28 26 25 26
19 | 13 12 14 17 15 5 10 13 9 16 4 | 21 30 21 19 28 19 26 23 24 19 20
20E | 9 7 9 12 14 7 9 10 12 11 3 | 23 24 19 22 23 17 21 20 22 15 19
21 | 8 12 16 15 11 5 12 16 11 18 4 | 27 29 24 29 29 23 29 26 26 26 25
22E | 11 16 5 13 13 5 8 9 13 7 4 | 32 29 27 29 30 26 29 29 36 24 28
23 | 14 15 13 16 19 7 14 17 13 18 5 | 23 32 19 25 29 19 26 21 17 13 19
24 | 8 8 13 12 11 4 13 12 10 16 4 | 15 23 18 16 22 14 24 19 17 14 16
25E | 10 11 15 9 18 6 14 11 16 12 4 | 18 21 26 19 24 17 25 19 21 14 18
26 | 8 6 12 15 12 5 9 14 14 10 4 | 20 23 21 23 21 18 20 22 20 19 18
27 | 12 9 13 20 15 5 13 13 16 15 5 | 23 29 22 23 34 22 34 25 32 27 26
28E | 7 12 10 16 13 6 9 7 11 10 3 | 19 22 18 21 23 15 19 21 22 12 17
29 | 10 13 14 15 15 8 14 15 19 15 5 | 24 24 22 23 21 19 22 20 24 16 19
30 | 7 13 11 10 10 6 11 7 6 11 3 | 21 25 24 21 27 19 26 21 22 23 22
31 | 12 12 12 14 18 4 11 12 20 14 5 | 21 32 19 22 32 17 25 20 24 15 20
32E | 16 23 13 11 18 8 22 17 18 15 6 | 42 45 39 38 42 41 47 38 50 43 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 12 15 15 6 13 15 13 15 |T 30 33 27 28 30 25 29 30 29 24 27
WRMS | 11 13 12 14 14 6 12 13 12 15 |NE 25 31 24 26 30 22 29 27 26 24 24
MEDI | 10 12 13 15 14 5 11 13 12 13 |MD 23 29 21 24 28 19 26 23 24 20 21
Table 3.1814.2 GPS week: 1814 Day: 2 MJD: 56944.000
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 10 13 12 12 5 11 7 9 9 3 | 28 31 25 25 27 21 30 22 27 21 25
2 | 12 13 14 19 15 8 10 37 11 20 6 | 29 33 27 30 26 25 28 45 29 28 26
X3E | 43 31 24 --- 1530 20 --- 25 26 --- 16 | 95 72 54 --- 57 62 --- 57 53 --- 59
4 | 5 7 12 11 10 5 7 10 7 11 3 | 32 31 28 33 31 27 30 33 33 30 30
5E | 7 16 8 17 15 5 19 14 12 8 4 | 26 26 21 26 23 21 25 24 26 21 22
6 | 6 10 13 13 10 6 11 16 12 10 4 | 30 34 28 29 32 27 35 28 30 27 29
7 | 10 13 13 17 20 4 12 12 8 15 4 | 30 32 25 32 34 24 28 26 25 23 26
8 | 7 8 11 13 19 4 11 12 9 23 4 | 21 25 25 24 25 20 23 21 21 28 22
9 | 21 18 11 25 19 13 16 34 22 33 8 | 63 77 63 54 60 60 72 87 60 81 66
10E | 11 26 11 17 15 6 16 17 14 10 5 | 65 78 68 63 70 65 73 77 68 66 68
11 | 6 9 15 12 11 3 10 11 11 12 4 | 41 44 38 41 46 37 43 43 37 40 40
12E | 9 20 7 18 23 5 26 15 13 13 5 | 25 29 19 26 24 18 29 22 22 21 19
13 | 9 11 13 16 22 5 14 12 12 12 4 | 29 37 26 35 44 25 30 28 23 23 27
14 | 10 11 14 13 18 5 11 14 15 14 4 | 27 32 28 30 35 25 30 26 25 21 25
15 | 7 12 11 14 21 7 14 15 17 12 5 | 24 28 23 27 27 19 25 28 30 24 23
16E | 8 14 10 18 21 5 12 13 10 11 4 | 34 38 34 36 33 32 33 35 33 31 33
17 | 8 14 12 13 13 7 15 11 12 21 4 | 30 34 29 34 32 29 35 32 33 27 29
18E | 9 12 7 14 34 4 10 12 14 7 5 | 31 31 29 31 38 26 30 29 27 27 28
19 | 12 14 14 18 18 5 11 13 12 18 5 | 24 31 27 30 31 23 28 28 24 24 24
20E | 8 9 7 11 19 5 10 13 11 10 3 | 26 27 22 27 23 21 23 24 27 22 23
21 | 9 11 15 18 13 6 13 15 16 16 5 | 28 34 29 33 31 27 31 31 25 27 27
22E | 9 23 6 12 16 6 8 8 12 8 4 | 31 31 29 29 33 28 30 31 30 25 28
23 | 11 13 13 16 21 7 15 18 13 15 5 | 23 29 23 25 29 18 26 23 18 17 20
24 | 7 10 12 12 16 4 11 10 11 14 4 | 22 27 25 25 29 19 28 23 20 18 21
25E | 8 11 15 10 17 4 12 11 8 14 4 | 24 27 29 25 24 21 27 23 21 23 23
26 | 6 8 11 13 13 4 10 14 18 12 4 | 24 25 24 29 27 22 23 28 19 23 22
27 | 12 12 13 19 18 5 10 13 9 14 4 | 29 35 27 32 36 27 36 32 29 31 30
28E | 7 11 7 11 14 5 10 9 9 9 3 | 26 26 19 24 23 19 21 24 23 19 21
29 | 10 15 15 17 16 7 14 15 16 16 5 | 28 32 28 32 28 26 28 29 26 25 25
X30 | 5 10 11 15 --- 4 10 11 12 11 4 | 24 27 26 25 --- 22 29 22 24 22 24
31 | 9 16 13 14 19 5 10 12 15 13 4 | 25 36 23 26 36 23 28 25 27 21 24
32E | 16 26 15 12 18 8 20 25 15 14 6 | 40 45 40 44 40 39 40 40 42 44 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 12 15 18 6 13 16 13 15 |T 32 35 30 31 34 28 32 32 29 28 29
WRMS | 9 14 12 14 16 5 12 14 11 13 |NE 29 34 28 31 33 26 31 31 27 27 27
MEDI | 9 12 12 14 18 5 11 13 12 13 |MD 28 31 27 30 31 25 29 28 27 24 25
Table 3.1814.3 GPS week: 1814 Day: 3 MJD: 56945.000
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 14 9 12 4 10 8 8 10 3 | 20 27 19 22 25 18 27 20 18 22 20
2 | 9 14 13 21 13 7 11 36 13 18 6 | 27 29 26 32 28 27 23 41 27 27 24
X3E | 28 27 34 19 1450 34 --- 22 46 --- 14 | 80 79 87 94 166 87 --- 80 91 --- 77
4 | 8 8 12 9 12 6 8 11 12 12 3 | 25 25 22 24 25 22 26 28 19 29 23
5E | 7 14 6 20 16 6 20 12 13 11 4 | 25 26 19 29 26 22 26 25 25 22 22
6 | 6 8 14 10 10 6 11 14 7 11 3 | 22 29 24 24 28 21 30 26 21 26 23
7 | 9 12 12 15 15 5 12 10 11 14 4 | 26 28 20 27 31 20 25 22 23 19 21
8 | 9 8 12 12 19 6 10 13 8 26 4 | 33 35 32 35 39 33 37 33 32 40 33
9 | 19 16 12 26 18 15 21 33 18 30 7 | 79 84 76 67 75 74 92 94 78 93 80
10E | 9 24 11 17 16 7 14 19 17 13 5 | 68 77 68 62 71 66 75 80 71 67 70
11 | 7 9 16 12 14 4 10 10 13 10 4 | 41 44 37 44 46 39 44 44 34 43 40
12E | 10 19 7 15 25 5 21 11 13 15 5 | 18 21 12 20 19 13 19 17 21 20 14
13 | 8 12 14 21 28 5 12 9 11 13 5 | 26 31 21 33 38 21 26 23 20 19 22
14 | 9 12 15 11 18 5 13 10 13 13 4 | 22 26 21 25 32 18 23 21 25 14 20
15 | 7 14 11 16 19 5 15 12 15 11 4 | 23 28 22 23 26 18 27 22 21 24 20
16E | 9 12 10 18 22 6 12 15 10 11 4 | 36 40 34 39 44 34 35 41 37 37 36
17 | 8 13 14 12 13 4 13 13 13 16 4 | 28 30 25 31 31 25 28 33 20 29 26
18E | 7 9 8 11 18 4 9 10 9 9 3 | 22 21 17 24 25 19 22 24 24 20 20
19 | 10 15 15 17 16 5 10 16 11 16 5 | 22 30 22 29 25 21 25 25 19 26 21
20E | 7 10 9 10 16 6 9 9 11 9 3 | 23 24 16 22 23 18 23 22 23 17 19
21 | 8 10 15 12 14 6 13 14 15 16 4 | 30 32 27 31 29 29 32 31 31 28 28
22E | 7 12 9 12 16 5 9 9 9 7 3 | 42 44 37 38 42 40 44 43 43 39 41
23 | 11 12 14 15 18 8 13 16 14 15 5 | 25 29 19 24 30 18 24 20 19 13 18
24 | 5 9 12 12 17 4 10 8 11 13 3 | 16 23 19 15 28 13 24 19 16 14 16
25E | 8 13 15 10 19 4 13 8 13 13 4 | 20 23 25 21 23 17 21 19 20 15 18
26 | 6 7 11 14 16 5 9 12 11 13 3 | 17 21 18 22 24 18 18 23 21 20 18
27 | 12 13 14 18 15 8 9 11 8 13 4 | 29 31 23 29 32 26 33 28 25 28 27
28E | 6 11 8 9 16 4 9 7 9 11 3 | 19 20 14 16 22 15 19 20 21 14 16
29 | 9 14 15 16 14 7 17 13 21 16 5 | 26 27 24 30 25 22 26 26 27 23 22
X30 | 5 10 11 10 --- 3 12 10 9 13 3 | 18 21 19 16 --- 15 25 17 18 20 17
31 | 9 12 16 18 16 4 9 10 12 12 4 | 24 32 20 29 36 20 26 20 27 20 23
32E | 13 17 12 13 16 8 18 20 13 14 5 | 36 34 32 36 30 32 32 29 39 33 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 12 15 17 6 13 15 12 14 |T 30 33 28 31 36 27 30 31 29 27 28
WRMS | 9 13 13 13 16 6 12 12 11 14 |NE 27 31 25 29 32 24 30 29 25 27 25
MEDI | 8 12 12 13 16 5 12 11 12 13 |MD 25 29 22 29 29 21 26 25 23 23 22
Table 3.1814.4 GPS week: 1814 Day: 4 MJD: 56946.000
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 14 11 12 4 10 6 8 9 3 | 20 27 18 19 25 18 26 19 20 17 19
2 | 11 13 14 20 12 8 9 37 11 19 6 | 27 31 25 31 31 27 28 44 25 28 25
X3E | 30 19 17 18 1894 29 --- 19 32 --- 11 | 76 66 54 56 232 57 --- 55 61 --- 58
4 | 5 7 12 13 14 4 8 8 11 12 3 | 23 25 23 26 28 23 25 25 26 25 23
5E | 9 14 7 18 17 5 18 13 13 6 4 | 23 25 18 26 27 19 22 24 24 23 21
6 | 6 9 13 11 10 5 10 12 12 9 3 | 23 32 22 20 28 21 29 25 23 22 23
7 | 10 11 14 15 17 5 12 10 11 16 4 | 23 27 18 25 27 16 21 18 21 13 18
8 | 7 8 12 13 14 5 9 10 7 28 4 | 34 33 30 31 29 30 31 30 32 45 31
9 | 18 14 12 25 16 12 16 32 20 27 7 | 67 75 66 61 66 61 78 79 70 78 69
10E | 11 22 12 16 14 5 15 20 10 9 5 | 66 79 69 64 68 66 74 80 68 68 70
11 | 7 9 16 14 16 4 10 9 13 12 4 | 37 40 37 41 44 37 41 40 40 42 38
12E | 9 19 6 14 22 5 24 13 12 14 5 | 20 26 14 21 19 15 24 17 20 17 16
13 | 7 11 15 15 20 5 13 10 15 16 4 | 22 29 17 25 33 17 24 18 17 14 18
14 | 11 14 13 13 18 6 10 13 15 15 4 | 22 29 20 23 27 17 23 22 22 15 19
15 | 8 13 14 19 19 5 15 14 18 14 5 | 23 29 23 23 26 18 24 21 28 24 21
16E | 7 16 7 19 16 5 11 14 13 12 4 | 23 23 18 26 25 19 21 22 22 18 19
17 | 11 15 14 11 13 4 14 11 15 18 4 | 30 32 25 29 34 25 27 31 28 31 27
18E | 8 10 7 13 18 6 10 12 13 10 4 | 26 25 23 27 19 20 25 28 23 25 23
19 | 11 14 12 16 16 4 9 15 13 17 4 | 19 27 21 21 25 17 21 21 18 22 18
20E | 7 8 8 11 14 5 9 8 12 12 3 | 23 22 16 23 23 18 19 21 20 20 19
21 | 8 11 14 12 13 6 11 12 11 17 4 | 28 29 24 28 30 22 26 25 27 24 24
22E | 9 12 6 10 20 5 6 8 15 9 4 | 40 39 34 36 37 36 39 33 35 33 35
23 | 11 13 14 18 20 6 13 18 18 17 5 | 22 27 16 20 24 13 22 18 18 9 14
24 | 6 8 15 10 15 4 11 7 13 15 4 | 18 24 18 16 24 13 24 17 19 14 17
25E | 7 12 15 11 16 6 12 9 10 12 4 | 20 21 26 18 16 18 20 18 18 14 18
26 | 6 8 12 15 16 6 9 13 14 13 4 | 17 22 17 20 22 15 15 21 18 18 16
27 | 9 12 14 18 14 4 10 10 11 11 4 | 25 26 23 25 28 21 28 23 24 23 23
28E | 8 13 10 10 17 5 10 8 10 12 3 | 22 23 17 18 22 16 18 19 25 17 18
29 | 10 15 14 16 14 7 15 14 19 16 5 | 28 31 28 30 26 25 29 26 27 23 24
30 | 7 9 11 9 11 3 13 11 11 10 3 | 18 22 19 18 27 16 28 15 20 17 18
31 | 9 12 14 15 17 7 9 9 14 13 4 | 24 30 19 25 33 19 24 19 23 17 21
32E | 14 19 11 18 17 7 19 17 16 15 5 | 32 36 33 41 34 32 34 31 36 32 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 12 15 16 6 12 15 13 15 |T 28 32 25 28 36 24 28 28 28 25 26
WRMS | 9 13 13 14 15 5 12 11 12 14 |NE 26 30 24 26 30 22 28 26 26 24 24
MEDI | 8 12 13 14 16 5 11 12 13 13 |MD 23 27 22 25 27 19 25 22 23 22 21
Table 3.1814.5 GPS week: 1814 Day: 5 MJD: 56947.000
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 13 10 12 4 10 5 13 5 3 | 21 26 18 18 25 16 27 20 25 15 19
2 | 11 11 15 18 12 9 11 36 12 19 6 | 23 26 23 25 23 22 22 41 29 22 21
X3E | 25 17 16 24 1884 18 --- 16 48 --- 11 | 80 64 70 72 188 59 --- 63 67 --- 65
4 | 10 7 12 8 15 6 7 7 9 11 3 | 25 20 19 21 25 19 20 20 26 21 20
5E | 8 14 7 18 17 4 18 12 12 14 4 | 22 27 22 27 23 22 24 26 27 23 22
6 | 12 7 14 14 12 6 15 12 12 8 4 | 22 28 21 20 28 19 34 23 21 20 21
7 | 12 11 12 14 18 4 11 10 9 12 4 | 26 27 20 24 31 17 24 20 18 15 20
8 | 8 7 9 12 16 7 10 10 11 24 4 | 50 48 46 47 50 46 46 47 45 54 47
9 | 21 14 12 26 24 15 18 29 21 27 7 | 103 114 105 101 99 99 117 125 105 119 109
10E | 14 20 12 13 15 5 15 21 8 10 5 | 63 74 68 64 69 64 74 81 66 65 68
11 | 10 9 15 11 14 6 10 8 15 12 4 | 36 34 32 33 38 31 35 32 38 32 32
12E | 10 18 7 12 22 6 21 12 13 10 5 | 20 21 13 19 16 12 18 18 23 16 14
13 | 11 12 14 17 27 6 13 10 14 12 5 | 27 30 20 28 41 20 26 23 22 16 22
14 | 10 12 12 14 19 7 10 15 13 14 4 | 19 26 19 21 28 14 23 22 18 14 17
15 | 7 12 11 13 21 6 14 12 11 11 4 | 24 28 22 24 26 18 23 24 22 22 21
16E | 8 13 7 14 19 5 15 15 15 13 4 | 31 29 27 33 31 27 30 29 32 27 28
17 | 23 15 16 14 13 6 14 13 12 15 5 | 29 28 22 28 28 21 25 29 27 22 22
18E | 10 11 8 12 17 5 13 12 9 10 4 | 22 20 15 20 18 15 23 20 21 16 17
19 | 10 15 13 14 18 4 10 13 11 16 4 | 18 25 20 21 21 17 22 19 22 19 17
20E | 9 10 8 13 17 6 9 9 13 9 3 | 24 19 17 21 24 18 20 22 29 18 19
21 | 10 11 15 14 14 5 12 12 15 15 4 | 27 29 25 26 26 21 27 22 28 21 23
22E | 10 11 7 9 15 5 10 12 8 8 3 | 47 46 43 44 43 42 48 48 49 42 45
23 | 11 13 13 17 21 6 13 15 17 15 5 | 22 26 16 18 25 12 21 16 17 10 14
24 | 6 8 14 11 14 6 11 5 9 13 3 | 18 22 20 17 24 14 22 17 17 11 16
25E | 9 10 15 11 15 4 10 8 12 12 4 | 19 21 26 20 16 16 19 20 21 16 18
26 | 6 9 11 11 19 5 8 13 13 13 4 | 16 21 17 20 27 14 16 22 17 16 16
27 | 11 9 14 14 12 4 10 10 10 13 4 | 24 25 21 20 24 19 28 22 29 22 22
28E | 12 13 10 10 15 4 10 7 12 7 3 | 24 19 16 18 23 15 19 19 23 13 17
29 | 12 14 14 17 14 6 17 12 14 16 5 | 25 27 24 30 27 22 24 26 30 22 23
30 | 18 13 10 12 12 5 13 8 11 7 4 | 28 23 21 20 27 17 31 17 17 17 20
31 | 10 12 15 16 20 6 10 9 14 12 4 | 24 30 18 21 32 16 24 19 23 18 20
32E | 16 17 12 16 21 8 16 17 20 15 6 | 32 30 30 35 33 32 32 27 36 31 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 12 14 17 6 13 14 13 13 |T 30 32 28 29 36 25 30 30 30 25 27
WRMS | 12 12 13 13 17 6 12 11 11 13 |NE 28 31 26 27 32 23 30 28 28 25 25
MEDI | 10 12 12 14 16 6 11 12 12 12 |MD 24 27 21 21 27 19 24 22 25 20 21
Table 3.1814.6 GPS week: 1814 Day: 6 MJD: 56948.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 9 13 12 11 4 10 8 7 8 3 | 25 28 20 22 26 21 30 22 25 19 22
2 | 11 13 13 17 14 7 12 37 13 17 6 | 28 32 28 34 33 30 32 45 32 28 28
X3E | 34 18 22 15 2044 16 --- 19 44 --- 13 | 82 65 66 70 65 69 --- 70 79 --- 68
4 | 7 9 11 12 12 3 7 11 9 11 3 | 31 29 27 31 30 30 31 33 32 30 29
5E | 10 13 7 19 14 4 15 14 11 10 4 | 32 32 27 37 28 27 33 31 31 28 28
6 | 5 10 13 12 10 5 12 11 10 9 3 | 27 30 24 23 30 22 33 24 21 26 24
7 | 8 14 14 19 15 3 11 8 9 14 4 | 30 29 21 32 31 21 27 22 20 19 22
8 | 8 10 12 16 13 4 8 15 8 22 4 | 65 66 66 71 65 67 67 69 67 63 66
9 | 20 17 12 24 12 13 18 33 17 26 7 | 73 80 72 58 66 67 84 83 74 82 73
10E | 20 20 11 14 13 6 16 22 9 10 5 | 73 80 74 67 71 71 80 87 73 72 74
11 | 8 10 14 12 14 4 10 9 10 10 3 | 49 50 46 53 53 49 53 53 50 50 49
12E | 9 17 8 13 26 4 18 13 14 11 5 | 23 25 16 23 19 15 21 18 21 17 16
13 | 9 13 15 17 20 4 12 11 11 13 4 | 29 32 20 33 39 23 29 23 19 17 23
14 | 9 12 11 11 16 5 10 15 13 14 4 | 25 29 20 26 30 18 25 25 20 15 21
15 | 9 13 12 16 20 5 15 14 8 11 4 | 24 30 24 27 26 21 27 22 26 24 21
16E | 7 21 8 20 20 5 14 13 13 14 5 | 21 29 21 30 27 22 23 25 24 27 22
17 | 10 13 16 12 11 6 14 15 9 16 4 | 27 30 24 32 34 27 30 36 32 32 28
18E | 10 11 9 15 16 5 11 11 9 10 4 | 25 24 21 26 23 19 24 25 22 20 21
19 | 12 17 14 17 16 4 11 16 10 14 5 | 24 31 22 31 28 24 27 31 25 27 24
20E | 9 9 8 12 14 4 7 9 9 12 3 | 28 27 25 32 30 26 29 25 27 27 25
21 | 7 11 15 16 13 5 10 10 8 14 4 | 32 36 28 38 33 30 33 33 32 30 31
22E | 7 12 9 11 15 6 9 10 13 7 3 | 37 34 30 35 38 32 36 36 35 26 33
23 | 10 15 14 17 21 6 12 17 14 15 5 | 25 28 18 26 27 17 24 23 21 19 18
24 | 7 11 14 7 15 4 13 7 9 14 4 | 17 26 19 18 27 14 28 17 19 15 17
25E | 8 11 15 13 15 4 11 10 7 13 4 | 24 24 29 21 20 18 22 20 20 12 19
26 | 6 9 13 16 18 5 11 11 5 10 4 | 16 21 14 20 23 14 19 21 12 15 14
27 | 7 10 19 17 10 4 10 9 11 14 4 | 31 31 26 35 33 29 37 32 31 30 30
28E | 7 14 10 10 13 4 12 8 7 10 3 | 23 23 14 19 20 15 20 17 20 13 16
29 | 11 16 15 18 14 8 17 14 14 16 5 | 31 32 29 33 29 27 31 29 30 25 27
30 | 8 10 12 27 13 6 13 9 9 11 4 | 24 24 21 28 25 18 32 18 20 18 21
31 | 13 16 14 16 19 3 10 14 9 13 4 | 28 31 19 28 36 21 27 23 24 21 23
32E | 16 15 12 10 19 6 18 17 14 15 5 | 44 41 41 47 47 43 43 39 46 43 41
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 13 16 16 5 12 15 11 14 |T 33 35 29 34 34 29 34 33 32 28 30
WRMS | 9 13 13 15 15 5 12 12 9 12 |NE 31 34 28 33 34 28 34 32 30 28 29
MEDI | 9 13 13 15 14 5 12 11 9 13 |MD 28 30 24 31 30 23 30 25 25 26 24
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 4.1814 GPS week: 1814 MJD: 56942.0-56948.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 |U 6 6 17 |U 7 9 26 |U 8 9 17 |
emr | emr 3057 | 9 8 19 |U 9 11 31 | 10 13 21 |
esa | esa 3072 | 7 7 18 |U 7 8 28 | 10 12 21 |
gfz | gfz 3045 |U 7 7 18 |U 8 8 29 |U 9 11 20 |
grg | grg 3010 | 12 9 27 |U 10 11 34 |U 9 12 20 |
igr | igr 3007 | 6 6 18 | 7 8 27 | 9 11 18 |
igs | igs 2993 | 7 6 18 | 8 11 29 | 9 11 19 |
jpl | jpl 2968 | 8 8 20 | 10 15 38 |U 10 11 20 |
mit | mit 3072 | 10 8 23 |U 9 13 34 |U 9 11 20 |
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 5.1814.0 GPS week: 1814 Day: 0 MJD: 56942.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 | 6 5 18 | 5 9 28 | 8 7 15 |
emr | emr 3056 | 10 7 25 | 9 11 37 | 10 13 21 |
esa | esa 3072 | 7 5 21 | 6 10 32 | 10 11 19 |
gfz | gfz 3060 | 6 5 21 | 6 10 30 | 8 8 15 |
grg | grg 2976 | 11 9 24 | 10 9 35 | 11 15 16 |
igr | igr 3043 | 7 5 20 | 5 8 32 | 9 9 15 |
igs | igs 2931 | 7 5 21 | 6 9 33 | 8 10 16 |
jpl | jpl 2968 | 8 6 24 | 7 11 37 | 10 11 18 |
mit | mit 3072 | 10 7 21 | 7 10 37 | 9 12 15 |
Table 5.1814.1 GPS week: 1814 Day: 1 MJD: 56943.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 5 7 21 | 9 11 37 | 8 10 18 |
emr | emr 3057 | 9 8 25 | 11 15 49 | 10 12 18 |
esa | esa 3072 | 6 8 20 | 9 11 39 | 8 11 17 |
gfz | gfz 3060 | 6 8 20 | 9 11 39 | 7 10 18 |
grg | grg 2976 | 10 8 25 | 12 16 46 | 8 13 18 |
igr | igr 2880 | 6 6 22 | 9 11 36 | 8 11 18 |
igs | igs 2927 | 6 7 21 | 9 12 40 | 7 10 16 |
jpl | jpl 2968 | 7 8 26 | 19 28 72 | 12 9 22 |
mit | mit 3072 | 9 9 24 | 11 25 48 | 7 8 18 |
Table 5.1814.2 GPS week: 1814 Day: 2 MJD: 56944.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 4 3 11 | 7 9 31 | 9 12 18 |
emr | emr 3060 | 9 6 13 | 11 12 36 | 10 14 23 |
esa | esa 3072 | 5 5 13 | 7 8 29 | 10 13 22 |
gfz | gfz 2967 | 7 6 15 | 8 8 26 | 8 11 20 |
grg | grg 2974 | 15 8 38 | 11 15 44 | 9 13 22 |
igr | igr 3010 | 4 4 13 | 7 8 26 | 9 12 19 |
igs | igs 3012 | 5 5 13 | 9 15 38 | 8 12 19 |
jpl | jpl 2968 | 7 8 16 | 11 18 37 | 10 11 20 |
mit | mit 3072 | 10 6 21 | 9 14 33 | 9 12 21 |
Table 5.1814.3 GPS week: 1814 Day: 3 MJD: 56945.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 7 5 15 | 5 9 18 | 9 8 17 |
emr | emr 3057 | 9 7 17 | 7 8 19 | 11 13 22 |
esa | esa 3072 | 8 6 15 | 7 7 24 | 10 12 22 |
gfz | gfz 3057 | 9 6 14 | 7 8 27 | 10 10 21 |
grg | grg 2934 | 16 7 38 | 9 8 26 | 10 11 21 |
igr | igr 3050 | 7 6 16 | 7 8 26 | 9 11 18 |
igs | igs 2991 | 8 6 15 | 6 7 18 | 9 10 19 |
jpl | jpl 2968 | 9 9 17 | 8 8 34 | 12 12 20 |
mit | mit 3072 | 10 6 20 | 7 7 26 | 10 9 19 |
Table 5.1814.4 GPS week: 1814 Day: 4 MJD: 56946.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 | 8 10 25 | 6 8 19 | 7 9 12 |
emr | emr 3060 | 9 13 25 | 7 8 25 | 8 12 16 |
esa | esa 3072 | 9 11 26 | 5 7 23 | 9 11 17 |
gfz | gfz 3060 | 9 11 25 | 7 7 22 | 7 11 14 |
grg | grg 3072 | 10 10 25 | 8 7 26 | 8 9 14 |
igr | igr 3050 | 8 11 25 | 5 7 22 | 8 10 13 |
igs | igs 3062 | 8 10 21 | 6 8 24 | 9 14 17 |
jpl | jpl 2968 | 8 13 24 | 7 10 26 | 8 10 15 |
mit | mit 3072 | 9 10 26 | 10 11 42 | 11 13 24 |
Table 5.1814.5 GPS week: 1814 Day: 5 MJD: 56947.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 5 6 17 | 6 9 22 | 7 9 16 |
emr | emr 3055 | 7 9 16 | 9 14 24 | 8 11 20 |
esa | esa 3072 | 6 7 18 | 6 8 21 | 11 12 22 |
gfz | gfz 3055 | 6 7 16 | 8 8 30 | 9 11 22 |
grg | grg 3069 | 12 8 23 | 10 15 27 | 8 11 18 |
igr | igr 2976 | 5 7 18 | 6 9 18 | 10 12 17 |
igs | igs 2967 | 6 8 18 | 8 15 26 | 9 11 19 |
jpl | jpl 2968 | 8 10 18 | 10 18 31 | 9 10 19 |
mit | mit 3072 | 6 6 17 | 10 17 25 | 8 11 19 |
Table 5.1814.6 GPS week: 1814 Day: 6 MJD: 56948.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3061 | 5 4 14 | 8 10 29 | 11 12 22 |
emr | emr 3059 | 8 6 15 | 9 9 27 | 12 13 26 |
esa | esa 3072 | 7 4 14 | 9 8 28 | 13 14 26 |
gfz | gfz 3060 | 7 5 14 | 9 9 29 | 13 14 28 |
grg | grg 3072 | 8 14 19 | 10 9 31 | 11 13 27 |
igr | igr 3045 | 5 4 14 | 8 8 30 | 12 13 23 |
igs | igs 3062 | 6 4 15 | 9 9 26 | 12 13 26 |
jpl | jpl 2968 | 8 5 15 | 10 11 27 | 11 13 23 |
mit | mit 3072 | 14 15 28 | 9 9 27 | 12 12 26 |
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 6.1814 GPS week: 1814 MJD: 56942.500-56948.500
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 | -37 -11 11 -70 -8 | 20 28
| 12 21 111 68 5 | 7
emr uuuuu | 9 1 -2 -42 18 | 12 24
| 9 17 111 46 3 | 4
esa uuuuu | 7 8 47 38 -5 | 21 27
| 14 15 58 62 6 | 6
gfz uuuuu | 11 -18 51 -180 -10 | -54 62
| 22 18 70 77 12 | 13
grg uuuuu | 13 9 -5 113 6 | 31 35
| 17 18 55 100 8 | 3
igr xxxxx | 13 13 6 111 -4 | 0 17
| 16 11 60 25 6 | 5
irf xxxxx | 27 12 -17 50 -2 | 0 14
| 11 11 19 24 3 | 4
jpl uuuuu | 11 33 20 75 1 | 16 25
| 17 17 63 37 5 | 4
mit uuuuu | 30 12 -65 83 -3 | 21 25
| 25 14 52 49 4 | 4
ngs uuuxu | -49 -38 -72 346 -4 | 11 16
| 55 59 77 154 5 | 3
sio uuxxx | 33 10 -64 236 5 | 42 44
| 14 12 69 48 10 | 2
Table 7.1814.0 GPS week: 1814 Day: 0 MJD: 56942.500
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 | -40 -31 82 -102 -11 | 25 34
emr uuuuu | -4 -14 95 45 18 | 4 20
esa uuuuu | 27 -8 45 -26 -3 | 24 31
gfz uuuuu | 25 -16 81 -190 -27 | -36 56
grg uuuuu | -6 -1 -15 118 2 | 28 33
igr xxxxx | 15 12 81 110 -3 | 2 19
irf xxxxx | 40 10 -31 62 -3 | 0 16
jpl uuuuu | 35 15 -68 84 8 | 17 27
mit uuuuu | 60 9 -94 123 -1 | 19 25
ngs uuuxu | -102 67 -193 450 -10 | 11 17
sio uuxxx | 34 0 -66 289 -7 | 41 45
Table 7.1814.1 GPS week: 1814 Day: 1 MJD: 56943.500
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 | -28 15 -121 -72 -16 | 29 36
emr uuuuu | 3 -10 -7 -46 14 | 11 23
esa uuuuu | 8 -4 17 -25 -7 | 29 34
gfz uuuuu | -9 -26 146 -218 -21 | -39 57
grg uuuuu | 12 -1 29 168 13 | 33 37
igr xxxxx | 23 5 96 141 -13 | 7 18
irf xxxxx | 45 17 -7 52 3 | 5 14
jpl uuuuu | 25 52 105 93 -4 | 21 31
mit uuuuu | 63 22 -41 107 5 | 25 28
ngs uuuxu | -103 -79 -57 384 -5 | 15 19
sio uuxxx | 51 25 11 271 6 | 45 48
Table 7.1814.2 GPS week: 1814 Day: 2 MJD: 56944.500
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 | -48 -24 60 -11 -8 | 26 33
emr uuuuu | 20 6 -41 -78 18 | 13 24
esa uuuuu | -15 18 113 34 -9 | 26 31
gfz uuuuu | -18 -21 -16 -306 -11 | -48 59
grg uuuuu | 7 21 -20 53 18 | 34 37
igr xxxxx | -1 24 -22 133 -11 | 4 17
irf xxxxx | 20 25 -46 92 -3 | 4 14
jpl uuuuu | 6 58 11 130 -3 | 18 28
mit uuuuu | 36 23 -148 140 -4 | 25 28
ngs uuuxu | 4 -83 -40 581 -5 | 13 17
sio uuxxx | 44 21 -138 262 0 | 44 46
Table 7.1814.3 GPS week: 1814 Day: 3 MJD: 56945.500
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 -4 -11 -20 -9 | 22 29
emr uuuuu | 21 0 -77 -41 20 | 14 25
esa uuuuu | -4 13 -65 101 -11 | 22 27
gfz uuuuu | 5 -27 7 -166 -8 | -59 60
grg uuuuu | 5 -14 96 89 -2 | 34 37
igr xxxxx | -15 6 -55 66 -6 | 1 15
irf xxxxx | 18 0 0 14 -5 | 2 13
jpl uuuuu | -10 39 50 48 6 | 15 24
mit uuuuu | -2 4 1 -9 -4 | 24 27
ngs uuuxu | 17 -19 42 319 -2 | 12 16
sio uuxxx | 10 3 38 166 25 | 42 44
Table 7.1814.4 GPS week: 1814 Day: 4 MJD: 56946.500
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 -10 48 -18 1 | 17 24
emr uuuuu | 14 1 82 -21 21 | 15 25
esa uuuuu | 16 25 52 117 -3 | 17 23
gfz uuuuu | 2 -3 54 -157 3 | -63 65
grg uuuuu | 4 30 -3 -64 11 | 30 34
igr xxxxx | 12 -4 -17 99 -1 | -3 16
irf xxxxx | 24 19 -28 51 -3 | -1 13
jpl uuuuu | 3 21 -13 12 3 | 13 23
mit uuuuu | 26 21 -107 80 -6 | 20 24
ngs uuuxu | -54 -76 -147 378 -8 | 9 15
sio uuxxx | 30 -8 -140 186 12 | 40 42
Table 7.1814.5 GPS week: 1814 Day: 5 MJD: 56947.500
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 | -47 14 -145 -204 -6 | 16 23
emr uuuuu | 5 -12 121 -58 13 | 16 26
esa uuuuu | 12 21 93 80 -9 | 16 22
gfz uuuuu | 35 10 -37 -49 -11 | -63 65
grg uuuuu | 47 -3 -50 192 -5 | 32 36
igr xxxxx | 26 22 -44 124 5 | -3 16
irf xxxxx | 19 17 6 38 -4 | -2 14
jpl uuuuu | 22 23 85 73 3 | 15 24
mit uuuuu | 19 17 -23 68 -7 | 20 24
ngs uuuxu | -104 -86 -45 143 6 | 9 15
sio uuxxx | 42 11 -56 208 1 | 42 44
Table 7.1814.6 GPS week: 1814 Day: 6 MJD: 56948.500
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 | -52 -39 163 -64 -3 | 9 17
emr uuuuu | 7 35 -190 -99 19 | 14 26
esa uuuuu | 8 -11 71 -18 5 | 10 19
gfz uuuuu | 39 -45 124 -174 5 | -69 71
grg uuuuu | 24 31 -73 235 7 | 28 33
igr xxxxx | 29 24 0 106 -2 | -8 15
irf xxxxx | 22 -4 -11 37 -1 | -7 15
jpl uuuuu | -4 25 -30 85 -4 | 10 20
mit uuuuu | 8 -14 -47 70 -6 | 14 20
ngs uuuxu | -3 12 -66 166 -3 | 5 13
sio uuxxx | 23 19 -101 269 1 | 38 41
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