[IGSREPORT-23097] Wk 1813 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Oct 24 10:42:00 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1813 (Oct 05, 2014 - Oct 11, 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:
igs1813[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1813[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1813[0-6].cls IGS GPS clock combination summary report.
igs18137.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18137.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 FAA1
0 | EMR | 32
0 | ESA | 32 DGAV SEY1 UNSA
0 | GFZ | 1 2 6 9 30 32 1 6 9 30 INVK INVK
0 | GRG | 32 FAA1 GRAZ XMIS GRAZ XMIS
0 | JPL | 32
0 | MIT | 1 4 7 24 1 4 7 11 24 26 32 HOB2 HYDE MDVJ
1 | COD | 20 32 20 32 FAA1 TLSE
1 | EMR | HOB2 TLSE
1 | ESA | 32 32 SFER DGAV FAA1 SEY1 SFER UNSA
1 | GFZ | 1 2 6 9 30 1 6 30 HYDE NYA1
1 | GRG | GRAZ HOB2 HYDE NYA1 TLSE WES2 GRAZ HOB2 MAL2 NYA1
1 | GRG | TLSE WES2
1 | JPL | 12 18
1 | MIT | 1 2 6 11 13 14 18 19 23 27 1 2 6 11 13 14 16 18 19
1 | MIT | 21 23 27 HYDE KOUR MONP
2 | ALL | 3 3
2 | COD | 32 32 FAA1 FAA1
2 | ESA | 32 21 32 ARTU SEY1 UNSA
2 | GFZ | 1 2 6 9 30 1 6 30 BRAZ MCM4 ONSA BRAZ MCM4 ONSA
2 | GRG | 21 FAA1 GRAZ KELY TOW2 FAA1 GRAZ KELY ONSA TOW2
2 | JPL | 21 32
2 | MIT | 8 ALRT IRKJ ALRT DUBO HYDE IRKJ
3 | COD | 32 32 HRAO PIMO TLSE GUAM HRAO TLSE
3 | EMR | 3 3 PRDS PRDS
3 | ESA | 32 32 PIMO TLSE BJFS PIMO TLSE UNSA
3 | GFZ | 1 2 3 6 30 1 2 3 6 9 30 CAS1 HOLB MCM4 TLSE CAS1
3 | GFZ | FAIR GUAM HOLB MAW1 MCM4 TLSE
3 | GRG | GRAZ GUAM GRAZ
3 | JPL | 20 32
3 | MIT | 3 4 3 4 MAW1 MDVJ
4 | COD | 32 5 32
4 | EMR | 3 3 CHUR CHUR
4 | ESA | 32 32
4 | GFZ | 1 3 6 30 1 3 6 30 BAKE FAIR FLIN MAC1 SCH2 SCOR BAKE
4 | GFZ | FAIR FLIN INVK RESO SCH2 SCOR TSKB WHIT
4 | GRG | KELY MAW1 KELY MAW1
4 | MIT | 3 10 3 10 MAC1 MDVJ
5 | COD | 10 32 BOR1
5 | ESA | 3 10 32 PIMO WUHN PIMO SEY1 TIXI TLSE WUHN
5 | GFZ | 1 3 6 30 1 6 10 30 THU3 WUHN THU3 TLSE WUHN
5 | GRG | BOR1 KELY ZIMM GUAM KELY
5 | JPL | 32
5 | MIT | 3 13 16 32 7 13 16 21 26 32 MAW1 PARC
6 | COD | 32 32 HOB2 IISC
6 | EMR | 3 3 10
6 | ESA | 32 32
6 | GFZ | 1 2 3 6 30 1 3 6 30 HOLM INVK YELL HOLM INVK KELY
6 | GFZ | YELL
6 | GRG | 10 BAKE DGAR DGAR IISC KELY
6 | JPL | 10 INVK
6 | MIT | 3 10 19 22 27 3 10 19 22 27 HYDE HYDE
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
----+--------+---------------
4 | COD | 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 -1.5 -.8 -73 -8 6 .24
EMR | 0 | 1.8 2.7 .8 -10 6 17 -.12
ESA | 0 | .5 .5 -1.5 10 9 52 -.16
GFZ | 0 | -.2 .1 -1.7 -10 -10 24 .31
GRG | 0 | 5.6 2.0 -8.5 -27 26 1 .47
JPL | 0 | 5.3 9.0 8.7 -83 -21 4 .22
MIT | 0 | -1.7 7.8 1.4 -9 1 -22 .09
NGS | 0 | 2.9 -.7 15.1 -23 -36 12 .62
SIO | 0 | 8.2 3.3 8.5 -2 14 2 -.14
COD | 1 | -.9 -.9 -.8 -70 -7 12 -.01
EMR | 1 | 5.2 6.3 4.9 -16 2 13 -.20
ESA | 1 | .0 .4 -1.9 8 5 55 -.14
GFZ | 1 | -.3 .5 -2.0 -7 -68 15 -.05
GRG | 1 | 5.4 6.6 6.8 -14 64 -16 .12
JPL | 1 | 5.8 9.6 10.6 -87 93 86 .33
MIT | 1 | .8 4.1 3.3 -16 -3 -11 .09
NGS | 1 | 7.2 -9.4 10.8 -40 -40 8 .54
SIO | 1 | 8.9 -1.5 17.0 -20 19 2 .01
COD | 2 | -.3 -.7 -.3 -70 -12 21 .11
EMR | 2 | -2.0 5.5 18.2 -14 6 24 -.11
ESA | 2 | .6 .2 -1.8 -4 6 57 -.06
GFZ | 2 | -.3 1.0 -1.7 -20 -72 26 .03
GRG | 2 | 2.3 1.5 8.0 -27 59 -14 .44
JPL | 2 | 4.6 4.0 15.9 -132 5 61 .21
MIT | 2 | .8 5.1 3.4 -13 0 -10 .19
NGS | 2 | -.6 -6.0 9.7 -35 -17 -18 .52
SIO | 2 | 4.7 -2.7 15.4 -13 7 16 .12
COD | 3 | -.5 -.8 .0 -53 3 7 -.11
EMR | 3 | -3.9 .6 10.2 -11 22 18 -.11
ESA | 3 | .8 .0 -1.6 6 1 49 -.01
GFZ | 3 | -.3 1.0 -3.0 0 -65 33 .06
GRG | 3 | -.4 11.1 -6.5 -38 61 -3 .28
JPL | 3 | -5.2 6.4 12.1 -87 43 35 -.24
MIT | 3 | -5.2 5.0 .8 -18 9 -35 -.05
NGS | 3 | 1.9 -4.3 5.6 -3 -16 -34 .45
SIO | 3 | .3 .8 6.5 -6 5 26 -.09
COD | 4 | -.1 -.7 -.2 -41 -2 -21 .07
EMR | 4 | -2.7 5.5 3.8 -11 16 0 -.04
ESA | 4 | .2 .0 -2.5 1 -9 47 -.24
GFZ | 4 | -.2 .5 -2.7 -27 -83 4 .10
GRG | 4 | 2.8 12.7 -1.8 -16 41 15 .27
JPL | 4 | -1.7 8.7 14.1 -40 3 24 .06
MIT | 4 | -1.2 6.4 -3.5 -13 1 -25 .10
NGS | 4 | -2.2 6.7 6.4 17 -11 16 .53
SIO | 4 | .5 5.9 4.6 -10 9 19 .0
COD | 5 | -1.3 -.3 -.7 -36 10 -10 .05
EMR | 5 | -1.8 8.3 -4.4 -14 6 6 -.16
ESA | 5 | -.3 .5 -1.9 8 -6 68 -.09
GFZ | 5 | -.5 .5 -2.6 -26 -71 9 .27
GRG | 5 | -1.3 13.3 -6.2 -21 26 -20 .50
JPL | 5 | 1.9 2.5 9.9 -138 -20 78 .43
MIT | 5 | -3.9 6.7 -4.9 -8 3 -26 .29
NGS | 5 | -.8 3.5 8.9 -16 -15 4 .57
SIO | 5 | 3.0 2.4 -2.6 -3 12 16 .21
COD | 6 | -.9 -.2 .0 -56 9 18 -.04
EMR | 6 | 2.1 6.9 .2 -8 17 -7 -.13
ESA | 6 | .4 .5 -2.4 6 4 66 -.13
GFZ | 6 | -.8 .3 -1.4 -29 -76 13 .21
GRG | 6 | -.2 6.8 -3.3 -53 55 -16 .28
JPL | 6 | 4.1 2.8 14.2 -89 8 10 -.46
MIT | 6 | -2.9 8.7 -5.7 6 13 -17 -.08
NGS | 6 | 3.7 2.3 10.7 6 -45 31 .53
SIO | 6 | 1.5 5.8 -6.5 -20 12 10 .07
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 1.1813.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1813.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 2.1813.[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 3.1813.[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 5.1813.0-6). 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 1813 summary. (Oct 05, 2014 - Oct 11, 2014)
Table 1.1813.a GPS week: 1813 MJD: 56935.000-56941.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 1 -1 -1 4 5 -14 .08 10 10 | -1452 412 16 106
| 0 0 0 22 11 12 .03 | 666 903
emr 79| 0 0 4 14 -12 16 .18 13 13 | 2406 -217 18 135
| 0 1 2 13 26 14 .04 | 587 1231
esa 150| 1 0 0 12 -5 0 -.28 13 13 | -823 182 14 154
| 0 0 1 18 15 4 .03 | 658 1240
gfz 199| -1 1 3 16 -13 26 -.04 14 12 | -69 136 16 145
| 1 0 1 18 10 17 .01 | 211 602
grg 174| 0 0 0 -2 35 -17 .27 16 15 | -70 206 18 140
| 0 0 2 15 9 24 .03 | 159 523
igr n/a| 0 0 -1 -7 9 -12 -.19 6 5 | 3662 -182 15 100
| 0 0 1 12 13 8 .02 | 514 1135
jpl 80| -1 0 0 -17 23 -4 .09 13 13 | 2022 -73 18 127
| 0 0 0 25 22 10 .03 | 615 1256
mit 350| -1 -1 -2 -25 -11 -1 -.06 15 12 | -854 1097 26 208
| 0 0 1 27 26 12 .03 | 3014 4869
ngs 228| 0 0 0 -28 0 -14 .05 13 11 | -1042 -210 1349 2795
| 0 0 2 43 40 23 .05 | 2090 3181
sio 479| 0 0 -3 2 -9 9 -.43 15 13 | --- --- --- ---
| 0 0 1 26 21 17 .02 | --- ---
Table 1.1813.b GPS week : 1813 MJD: 56935.000-56941.000
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 4 4 4 3 |
2 | 5 5 5 6 5 5 5 |
3 | 15 16 44 12 18 12 12 |
4 | 3 4 4 4 4 4 4 |
5 | 4 4 4 4 4 4 4 |
6 | 4 4 4 4 4 5 5 |
7 | 5 5 5 5 4 5 5 |
8 | 4 4 5 5 5 4 4 |
9 | 9 9 9 10 9 9 8 |
10 | 6 5 6 5 6 6 5 |
11 | 4 4 4 4 4 4 4 |
12 | 5 6 6 8 6 6 8 |
13 | 4 5 5 5 5 5 5 |
14 | 5 5 5 5 4 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 6 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 4 4 4 4 4 4 4 |
19 | 5 5 5 5 5 5 5 |
20 | 4 4 4 6 4 4 4 |
21 | 5 6 5 5 5 5 5 |
22 | 5 5 5 5 3 4 4 |
23 | 5 6 5 5 5 5 5 |
24 | 4 4 5 4 4 5 4 |
25 | 5 4 4 4 4 4 5 |
26 | 4 4 4 4 4 4 4 |
27 | 4 5 4 5 4 5 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 3 3 4 4 |
31 | 5 6 5 5 5 5 5 |
32 | 6 5 5 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 2.1813.0 GPS week: 1813 Day: 0 MJD: 56935.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 2 0 0 -13 21 -18 .10 10 9 | -1749 303 14 104
emr 80| 0 0 3 23 -16 37 .17 12 12 | 3268 -2601 13 135
esa 150| 1 0 -1 47 18 -2 -.23 13 13 | -787 -719 12 152
gfz 198| -1 0 1 46 1 25 -.04 13 12 | -40 -857 14 129
grg 178| 0 0 -2 -2 48 -14 .26 16 15 | 85 -655 15 129
igr n/a| 0 0 -3 -10 25 -23 -.16 6 5 | 4163 -2202 16 97
jpl 80| -2 0 -1 -37 40 -22 .11 13 13 | 2536 -2366 14 101
mit 350| 0 0 0 -28 -25 -17 -.09 15 12 | -1011 -660 28 201
ngs 233| 0 0 2 -88 -69 -31 -.02 14 11 | -618 -548 1692 2967
sio 480| 0 0 -2 27 -19 9 -.45 14 13 | --- --- --- ---
Table 2.1813.1 GPS week: 1813 Day: 1 MJD: 56936.000
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 -2 -2 20 -12 -31 .11 11 10 | -1323 346 25 106
emr 80| 0 2 4 4 -25 22 .22 13 13 | 1828 436 47 157
esa 150| 1 0 -1 19 -5 4 -.27 13 13 | -1420 138 35 159
gfz 200| -1 0 2 27 -8 34 -.03 13 12 | 100 -107 28 157
grg 176| 1 1 3 12 30 -15 .24 16 15 | -309 283 32 146
igr n/a| 0 -1 -2 4 26 -21 -.20 6 6 | 3048 646 17 107
jpl 80| -3 1 -1 -32 17 -14 .09 14 14 | 1241 667 29 121
mit 350| -1 -1 0 -34 6 7 -.08 15 12 | -2536 4221 34 255
ngs 229| 0 0 0 -40 18 -25 .00 12 10 | -102 -2059 1230 3046
sio 484| 0 0 -2 -3 1 17 -.43 16 12 | --- --- --- ---
Table 2.1813.2 GPS week: 1813 Day: 2 MJD: 56937.000
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 17 -4 -23 .09 9 9 | -1246 297 15 102
emr 80| -1 0 6 0 -10 13 .14 13 13 | 1854 859 13 142
esa 150| 1 0 -1 6 -25 -6 -.28 13 13 | -1119 1642 11 169
gfz 204| 0 2 3 16 -24 29 -.05 13 11 | -373 910 13 160
grg 175| 0 0 0 16 29 -42 .24 15 14 | -170 244 15 147
igr n/a| 0 0 -3 -19 0 -15 -.20 6 5 | 3298 939 15 87
jpl 80| 0 0 0 -17 16 -9 .08 13 13 | 1437 1046 19 134
mit 350| -1 0 -2 -32 -15 15 -.07 16 12 | -305 157 25 183
ngs 229| 0 0 3 -21 63 -12 .07 14 11 | -1227 271 1399 2728
sio 479| 0 1 -5 -17 -1 38 -.40 15 13 | --- --- --- ---
Table 2.1813.3 GPS week: 1813 Day: 3 MJD: 56938.000
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| 2 -1 0 -37 5 -2 .09 11 11 | -2816 2249 17 103
emr 79| -1 0 6 27 -51 -8 .13 12 12 | 2862 -1057 14 143
esa 150| 1 0 1 12 -11 3 -.31 13 13 | -1569 -1201 10 158
gfz 197| -1 1 3 3 -11 43 -.03 14 12 | 148 70 14 86
grg 176| 0 1 -1 -8 48 0 .28 18 14 | -28 182 15 131
igr n/a| 0 -1 0 -16 4 -12 -.16 6 6 | 4366 -1194 16 121
jpl 80| 0 0 0 6 66 1 .09 15 15 | 2491 -1121 18 138
mit 350| -1 -1 -2 22 10 5 -.08 15 12 | -2780 5904 23 208
ngs 230| 1 0 -2 -73 -26 -29 .12 13 11 | -277 -3337 1064 2387
sio 485| 0 1 -5 43 -4 18 -.42 15 13 | --- --- --- ---
Table 2.1813.4 GPS week: 1813 Day: 4 MJD: 56939.000
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 -1 -2 19 17 -14 .06 9 9 | -970 -261 15 115
emr 80| -1 0 5 -5 29 26 .16 13 13 | 1874 777 14 119
esa 150| 1 0 1 -4 1 0 -.28 13 13 | 386 -1156 11 139
gfz 200| -1 0 3 8 -6 27 -.06 14 13 | -15 -109 14 165
grg 175| 0 0 0 3 36 25 .32 14 14 | 165 -202 16 155
igr n/a| 0 0 0 -21 9 -5 -.20 6 5 | 3259 592 15 104
jpl 80| -2 -1 0 -30 20 7 .03 13 13 | 1457 1040 17 129
mit 350| 0 -1 -2 -24 -61 -8 -.04 14 12 | 5085 -7700 24 193
ngs 230| 1 1 1 16 3 -37 .09 12 11 | -5455 6332 1239 2411
sio 482| -1 0 -4 -5 -52 -13 -.44 15 13 | --- --- --- ---
Table 2.1813.5 GPS week: 1813 Day: 5 MJD: 56940.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 1 0 0 2 6 -13 .03 10 10 | -1226 552 14 112
emr 80| 0 0 2 23 -21 19 .22 13 13 | 2841 105 15 137
esa 150| 0 0 2 -8 -20 -2 -.31 14 14 | -455 1550 10 145
gfz 201| -2 2 5 21 -22 36 -.03 14 12 | 47 236 15 155
grg 171| 1 0 0 -30 23 -32 .23 15 15 | -102 921 17 147
igr n/a| 0 0 0 4 -9 2 -.21 6 5 | 4028 127 16 101
jpl 80| -1 0 0 27 5 1 .09 13 13 | 2675 193 18 130
mit 350| -1 -2 -3 -68 14 0 .00 16 13 | -4300 6175 28 235
ngs 225| 1 0 -2 32 8 8 .05 12 11 | 1196 -2273 1428 3194
sio 479| -1 0 -4 -33 15 4 -.42 14 13 | --- --- --- ---
Table 2.1813.6 GPS week: 1813 Day: 6 MJD: 56941.000
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 246| 0 -1 -1 21 2 6 .09 10 9 | -839 -599 13 106
emr 80| 0 0 0 25 12 9 .22 13 13 | 2321 -43 15 116
esa 150| 0 0 0 12 2 2 -.31 12 12 | -802 1026 12 158
gfz 199| -2 1 5 -10 -24 -9 -.04 15 14 | -356 813 15 165
grg 169| 0 1 2 -4 32 -41 .31 18 15 | -131 672 18 128
igr n/a| 0 0 1 6 12 -12 -.19 6 5 | 3474 -188 16 88
jpl 80| -1 0 0 -38 -1 3 .11 13 13 | 2320 30 17 141
mit 350| 0 -1 -5 -16 -8 -14 -.04 16 14 | -131 -413 22 186
ngs 223| 1 0 2 -23 7 27 .02 12 10 | -813 141 1393 2835
sio 470| 0 0 -2 7 -7 -8 -.43 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 3.1813.0 GPS week: 1813 Day: 0 MJD: 56935.000
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 13 10 11 5 12 8 8 11 3 | 26 29 27 26 29 21 32 24 22 26 25
2 | 8 10 15 14 16 5 11 17 12 20 5 | 33 36 29 38 38 32 35 38 29 31 31
X3E | 33 32 34 27 --- 22 --- 28 45 --- 15 | 106 79 73 88 --- 89 --- 79 89 --- 88
4 | 7 8 11 7 12 6 7 10 9 12 3 | 29 26 28 28 28 26 29 31 25 29 27
5E | 6 13 8 11 19 5 15 9 14 9 4 | 73 71 66 67 74 66 67 67 70 64 68
6 | 6 9 12 10 13 5 14 16 12 9 4 | 34 37 36 33 36 30 41 29 35 34 33
7 | 11 9 14 17 18 6 12 9 9 16 4 | 32 29 26 36 36 24 27 25 24 21 25
8 | 6 9 14 9 16 6 8 12 12 16 4 | 21 21 21 17 19 16 22 20 16 25 18
9 | 20 12 14 24 20 14 13 45 17 34 8 | 87 87 87 74 78 81 90 107 82 103 86
10E | 11 17 17 14 17 8 14 12 31 11 6 | 39 45 41 37 39 36 42 45 48 35 39
11 | 8 8 14 8 15 4 10 9 10 8 3 | 54 54 50 54 61 53 59 54 51 52 53
12E | 13 17 6 11 25 9 22 11 12 12 5 | 32 33 29 31 35 27 31 35 37 33 30
13 | 11 11 15 12 17 5 10 11 10 12 4 | 38 41 31 39 47 33 38 34 32 26 34
14 | 12 13 15 15 16 4 15 16 8 11 4 | 40 40 33 44 41 34 36 43 37 36 37
15 | 7 12 14 14 16 5 14 9 15 11 4 | 24 28 24 26 27 18 27 22 22 20 21
16E | 10 15 7 19 18 5 12 14 12 12 4 | 21 23 20 27 26 21 24 29 26 26 22
17 | 12 14 15 14 11 4 15 16 14 19 5 | 34 38 33 42 40 37 42 43 40 37 36
18E | 9 14 11 13 12 6 13 13 9 14 4 | 57 56 53 56 55 53 57 55 54 50 54
19 | 11 15 12 14 15 6 10 15 14 17 5 | 34 36 34 39 39 34 38 36 29 33 33
20E | 10 10 7 11 15 4 11 8 11 8 3 | 51 48 48 46 44 47 45 46 47 41 46
21 | 8 10 15 16 18 4 13 9 13 12 4 | 34 33 30 40 41 31 36 33 28 31 31
22E | 10 9 10 12 12 6 13 25 9 13 4 | 56 54 50 52 57 50 52 50 55 43 51
23 | 14 14 13 13 18 6 13 15 14 17 5 | 33 35 27 36 38 27 33 33 24 22 28
24 | 5 9 12 9 15 4 12 5 9 12 3 | 23 25 24 23 29 20 30 22 22 20 22
25E | 7 16 14 12 18 5 12 9 13 12 4 | 21 27 28 24 20 19 25 23 26 20 21
26 | 7 8 11 12 13 3 9 8 13 8 3 | 47 51 44 50 52 45 48 50 45 43 47
27 | 5 9 15 12 14 5 13 10 12 15 4 | 47 44 41 50 51 46 49 50 43 47 46
28E | 10 7 10 17 14 5 15 13 12 8 4 | 20 19 18 24 24 17 22 27 22 17 19
29 | 10 14 13 15 15 6 16 15 15 14 5 | 35 33 29 36 34 31 35 36 28 31 31
30 | 8 9 11 10 11 5 13 9 7 8 3 | 24 27 27 23 28 20 29 22 21 22 23
31 | 11 14 13 18 20 4 15 12 14 16 5 | 30 33 25 32 39 25 29 32 32 27 28
32E | 11 17 12 8 19 5 14 13 27 13 5 | 68 73 66 66 62 62 69 60 66 56 65
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 13 13 16 6 13 15 14 14 |T 40 40 37 40 40 36 39 40 38 35 38
WRMS | 9 12 13 12 15 5 13 12 11 13 |NE 36 37 33 37 39 32 38 37 32 34 34
MEDI | 10 11 13 12 16 5 13 12 12 12 |MD 34 36 30 37 39 31 36 35 32 31 31
Table 3.1813.1 GPS week: 1813 Day: 1 MJD: 56936.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 10 15 8 11 5 11 10 10 8 3 | 22 27 22 22 25 16 27 19 19 19 20
2 | 9 15 14 16 14 5 11 15 11 25 5 | 28 32 25 32 30 25 30 30 28 21 25
X3E | 38 38 30 23 --- 25 --- 37 38 --- 15 | 85 92 72 85 --- 71 --- 94 79 --- 86
4 | 7 8 15 9 13 3 10 13 6 11 3 | 20 21 22 21 23 18 19 21 17 21 19
5E | 8 14 7 11 15 4 15 10 12 11 4 | 47 50 46 51 50 45 47 48 50 43 47
6 | 8 10 12 8 10 5 13 13 10 12 3 | 23 32 26 24 30 23 34 20 25 29 25
7 | 12 11 14 14 17 5 12 9 11 15 4 | 26 25 19 26 34 17 22 20 24 15 21
8 | 10 11 14 10 15 4 8 12 8 19 4 | 21 23 18 16 20 14 20 16 18 29 17
9 | 24 13 15 24 20 15 13 45 15 42 9 | 56 58 55 46 46 51 60 83 53 79 56
10E | 11 17 14 11 16 6 15 12 21 13 5 | 38 45 40 38 37 35 39 41 41 35 37
11 | 8 10 15 12 16 5 10 9 10 8 4 | 33 36 32 34 41 31 35 33 29 32 32
12E | 11 21 7 13 16 8 26 13 13 12 5 | 31 36 29 30 32 29 38 28 31 28 28
13 | 12 12 15 12 20 5 10 9 9 14 4 | 28 34 24 29 40 24 29 25 25 22 26
14 | 11 13 14 12 16 5 18 18 12 19 5 | 28 31 26 30 36 26 30 34 28 30 27
15 | 8 11 16 12 15 5 15 10 11 13 4 | 21 27 21 25 27 16 23 21 20 18 19
16E | 15 16 9 17 23 6 14 15 14 15 5 | 24 20 19 24 26 14 20 22 14 21 17
17 | 9 13 14 11 10 4 13 15 11 16 4 | 25 29 24 29 29 26 30 31 25 25 25
18E | 8 11 9 12 12 6 14 13 10 15 4 | 46 48 47 46 47 46 46 45 45 43 45
19 | 11 14 13 15 15 8 11 17 11 18 5 | 20 26 21 20 25 19 23 22 14 20 18
20E | 12 10 8 11 15 4 14 9 6 9 3 | 33 36 31 34 32 30 35 33 33 30 31
21 | 9 25 14 17 14 6 17 13 14 18 5 | 26 33 22 30 30 21 25 19 23 20 21
22E | 9 10 9 13 12 6 12 24 9 12 4 | 58 54 54 57 57 54 55 51 52 48 53
23 | 15 14 14 14 20 6 13 16 14 18 5 | 26 32 20 25 33 19 26 23 18 16 20
24 | 7 8 12 10 16 5 11 6 13 13 4 | 22 25 21 21 29 18 31 20 21 20 21
25E | 6 14 13 9 16 7 13 6 12 13 4 | 19 25 27 18 20 19 28 19 20 18 19
26 | 7 10 11 10 16 7 9 8 14 11 3 | 55 57 55 55 57 55 57 55 62 55 55
27 | 13 12 12 16 11 8 12 16 13 16 4 | 45 41 41 42 44 41 45 41 39 42 40
28E | 10 10 9 12 11 7 15 11 8 7 3 | 24 22 19 24 22 16 23 20 20 14 18
29 | 11 14 15 17 14 8 19 15 12 16 5 | 29 26 25 28 24 24 26 25 22 23 22
30 | 7 12 11 8 13 5 11 7 8 10 3 | 23 24 24 19 29 17 27 18 21 20 21
31 | 10 16 14 13 21 6 17 15 17 13 5 | 25 31 23 25 36 22 29 29 29 21 24
32E | 10 16 14 10 18 6 15 12 17 16 5 | 58 64 57 57 53 54 61 53 56 55 56
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 13 13 16 6 14 15 12 16 |T 33 36 31 33 34 29 33 33 31 29 30
WRMS | 10 13 13 12 15 6 14 12 10 12 |NE 28 31 26 28 32 24 30 28 26 27 26
MEDI | 10 12 14 12 15 6 13 13 11 13 |MD 26 32 25 29 32 24 30 25 25 23 25
Table 3.1813.2 GPS week: 1813 Day: 2 MJD: 56937.000
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 14 9 8 3 11 12 10 8 3 | 21 25 21 19 25 17 26 22 19 20 20
2 | 10 13 15 15 14 6 10 12 13 21 5 | 28 30 26 33 33 26 29 32 25 26 26
X3E | 35 --- --- 54 --- 117 --- --- --- --- 43 | 96 --- --- 69 --- 81 --- --- --- --- 74
4 | 7 8 11 9 9 3 8 14 10 10 3 | 22 23 24 23 25 22 24 30 20 25 22
5E | 7 15 11 13 10 4 15 11 10 9 4 | 52 48 46 52 54 49 51 51 52 48 50
6 | 6 9 12 7 14 7 13 16 15 13 4 | 26 31 27 28 30 25 35 26 34 32 27
7 | 11 11 13 14 16 6 12 10 14 13 4 | 27 27 21 29 29 19 24 23 27 17 22
8 | 8 11 12 10 17 5 8 14 9 21 4 | 17 22 18 18 17 15 21 22 18 30 18
9 | 21 12 16 22 20 14 16 46 20 44 9 | 68 66 66 59 62 63 73 91 65 90 67
10E | 9 19 16 13 15 6 16 11 32 12 6 | 35 41 35 35 32 28 38 37 43 31 33
11 | 9 9 15 10 12 4 10 11 15 9 4 | 41 44 40 43 49 42 46 45 43 41 42
12E | 12 21 6 14 17 6 24 14 11 13 5 | 31 37 27 33 36 26 32 27 30 26 28
13 | 11 11 14 12 20 4 12 9 13 11 4 | 29 35 25 32 40 26 30 29 31 24 28
14 | 10 12 15 12 13 4 14 18 13 13 4 | 33 35 27 35 34 28 36 35 29 28 30
15 | 10 10 14 12 17 6 13 11 19 12 4 | 21 22 21 21 25 17 24 23 25 20 19
16E | 10 18 9 17 22 7 12 15 15 13 5 | 20 26 20 25 29 19 22 31 23 28 22
17 | 9 14 14 10 9 6 13 16 11 20 4 | 32 31 28 31 34 30 31 35 26 30 29
18E | 7 13 8 11 15 4 11 15 10 10 4 | 40 40 34 36 44 35 39 37 37 35 36
19 | 11 15 12 15 14 4 11 17 14 17 5 | 26 32 29 32 34 28 33 33 27 27 27
20E | 9 11 9 11 11 4 10 10 8 11 3 | 34 32 30 30 34 30 31 30 30 30 30
21 | 7 13 14 15 16 5 16 9 12 16 4 | 28 30 26 32 35 26 34 28 28 27 27
22E | 8 14 9 12 14 7 9 26 9 12 4 | 43 43 38 40 42 39 44 40 41 40 39
23 | 14 13 14 13 18 6 14 19 9 17 5 | 25 31 21 28 33 21 30 32 25 22 24
24 | 7 10 14 11 12 6 19 8 15 16 4 | 24 27 26 23 28 20 33 24 23 21 23
25E | 5 12 14 11 17 5 12 6 11 12 4 | 22 26 31 25 26 23 25 26 23 22 24
26 | 6 9 12 11 13 7 12 9 12 9 3 | 55 61 55 60 59 59 61 56 63 58 57
27 | 6 7 13 15 13 4 13 11 11 15 4 | 43 39 38 43 46 41 47 43 39 44 41
28E | 7 11 8 11 12 7 10 12 12 9 3 | 23 22 20 21 23 20 19 27 27 22 21
29 | 8 14 13 16 14 7 17 13 13 15 4 | 30 29 28 33 31 29 30 32 27 29 27
30 | 8 11 10 8 13 5 14 7 12 9 3 | 23 27 24 20 26 19 30 22 25 21 22
31 | 9 15 18 14 19 6 14 16 14 12 5 | 27 34 26 28 36 23 30 29 28 24 26
32E | 11 17 13 8 20 5 14 13 18 17 5 | 50 54 50 50 42 46 51 46 47 48 47
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 13 13 15 6 13 16 14 15 |T 34 34 30 33 35 31 34 34 32 31 32
WRMS | 9 13 13 11 14 5 13 12 11 13 |NE 30 33 29 31 34 28 34 33 30 31 29
MEDI | 9 12 13 12 14 6 13 12 12 13 |MD 28 31 27 32 34 26 31 31 28 28 27
Table 3.1813.3 GPS week: 1813 Day: 3 MJD: 56938.000
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 13 9 9 4 11 11 11 8 3 | 26 27 25 22 27 22 29 21 26 21 24
2 | 16 11 14 19 13 7 14 11 16 21 5 | 31 34 31 41 38 34 33 36 35 32 32
X3E | 20 28 20 20 --- 13 --- 24 42 --- 12 | 60 78 73 63 --- 77 --- 72 65 --- 56
4 | 9 8 12 12 11 4 10 14 8 11 3 | 29 24 28 30 28 26 25 29 32 28 27
5E | 11 13 8 10 15 3 16 11 12 11 4 | 58 58 54 61 59 56 57 61 61 54 58
6 | 7 9 14 12 8 6 13 15 11 10 4 | 30 34 31 28 30 29 35 27 34 32 30
7 | 10 11 12 16 15 5 13 11 10 13 4 | 29 29 25 34 35 25 29 28 32 22 27
8 | 8 9 14 14 14 6 10 13 8 23 4 | 22 24 23 24 21 21 24 23 26 33 23
9 | 22 13 17 26 19 17 11 46 23 46 9 | 74 77 75 65 68 70 78 97 73 99 75
10E | 11 19 14 10 13 6 15 8 25 10 5 | 40 43 40 37 40 38 38 40 47 33 38
11 | 9 10 16 13 12 5 11 13 7 9 4 | 46 45 44 47 54 44 47 48 50 45 46
12E | 14 21 8 13 56 8 22 15 16 12 8 | 33 33 27 33 59 30 33 29 38 29 30
13 | 10 10 14 14 18 6 12 9 11 12 4 | 34 39 31 38 44 33 35 35 35 28 34
14 | 10 10 14 13 16 6 12 15 14 11 4 | 35 38 32 39 40 35 35 42 36 33 35
15 | 8 10 14 13 18 6 16 11 9 14 4 | 28 29 27 29 31 23 28 26 26 24 25
16E | 10 13 10 18 18 6 14 14 11 10 4 | 22 21 18 26 23 20 19 25 25 22 20
17 | 12 13 15 14 10 7 15 15 12 18 5 | 36 35 34 42 38 39 36 40 37 36 35
18E | 10 10 8 11 11 5 12 14 14 12 4 | 58 56 56 56 60 55 55 56 50 54 55
19 | 13 14 13 19 15 4 12 16 14 15 5 | 33 34 30 35 34 29 32 34 34 28 30
20E | 10 11 9 8 12 5 40 14 12 9 5 | 32 31 29 30 27 28 41 31 30 26 28
21 | 9 11 15 13 13 5 14 11 12 16 4 | 33 33 28 38 38 32 32 33 34 32 31
22E | 11 10 11 12 15 6 9 24 13 12 4 | 40 41 40 42 38 41 40 40 39 39 39
23 | 12 12 14 14 19 6 14 17 16 16 5 | 31 35 30 37 36 29 33 35 27 27 30
24 | 8 10 14 11 15 6 15 6 11 13 4 | 24 29 26 26 30 23 31 25 32 19 25
25E | 11 10 14 10 14 4 14 10 16 10 4 | 27 25 31 27 24 26 28 26 35 20 26
26 | 8 7 11 11 10 7 9 8 7 15 3 | 47 48 48 50 49 47 46 50 46 45 48
27 | 16 10 14 19 13 6 12 13 14 14 5 | 39 41 40 46 48 43 46 47 48 42 42
28E | 10 10 10 12 10 6 16 10 10 7 3 | 25 22 24 27 28 23 24 24 26 24 24
29 | 9 12 14 12 13 6 17 11 16 16 4 | 35 33 31 38 34 34 34 35 39 35 33
30 | 8 9 11 8 8 5 11 10 8 10 3 | 21 25 25 22 29 21 29 23 25 22 23
31 | 14 13 16 15 20 5 12 15 10 13 5 | 33 35 28 30 39 28 30 32 34 22 29
32E | 15 13 15 9 26 6 12 14 15 14 5 | 52 55 51 51 42 49 52 45 50 47 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 13 14 18 6 15 15 13 15 |T 36 37 35 37 38 35 36 37 38 33 35
WRMS | 11 12 13 12 14 6 15 12 11 13 |NE 34 35 32 36 37 32 35 36 36 33 33
MEDI | 10 10 14 13 14 6 13 13 12 12 |MD 33 34 31 37 38 30 33 34 35 32 30
Table 3.1813.4 GPS week: 1813 Day: 4 MJD: 56939.000
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 9 12 12 9 4 10 13 12 7 3 | 21 24 20 23 24 17 25 19 20 17 20
2 | 8 13 16 16 14 5 11 12 9 18 4 | 27 30 23 29 31 26 27 31 27 21 25
X3E | 93 41 31 29 --- 19 --- 24 49 --- 18 | 95 74 51 46 --- 49 --- 51 73 --- 52
4 | 8 10 11 12 11 5 9 15 8 10 3 | 29 24 26 30 26 24 23 27 25 23 25
5E | 7 12 11 11 15 3 13 9 9 12 4 | 75 72 69 74 71 70 71 72 75 70 72
6 | 4 8 15 11 10 5 12 17 12 9 4 | 24 32 29 27 30 26 34 24 31 27 27
7 | 9 12 13 17 12 5 12 12 9 11 4 | 25 29 21 29 30 21 28 26 26 18 23
8 | 8 8 11 11 16 4 10 12 12 22 4 | 20 20 19 17 17 15 20 16 19 29 17
9 | 21 13 16 23 16 15 12 43 18 39 8 | 66 68 69 57 59 61 72 85 64 85 66
10E | 9 22 15 13 15 5 18 10 20 15 5 | 38 43 40 35 36 33 37 39 44 28 36
11 | 8 10 15 15 13 6 11 12 13 10 4 | 45 42 42 51 49 44 47 46 42 42 44
12E | 11 20 8 14 17 6 25 16 11 12 5 | 23 28 19 24 30 23 27 23 27 22 21
13 | 9 12 15 13 18 5 11 11 12 11 4 | 29 34 25 31 36 25 29 30 26 22 27
14 | 9 10 14 13 15 5 12 13 14 11 4 | 27 32 27 33 31 25 30 31 30 21 27
15 | 7 11 14 17 15 4 13 12 13 14 4 | 25 26 23 30 26 20 21 24 27 20 22
16E | 9 17 10 17 17 5 9 14 15 11 4 | 24 27 21 31 25 22 26 27 27 27 24
17 | 9 17 14 14 12 7 14 13 12 18 4 | 27 30 27 35 31 29 30 33 26 28 27
18E | 9 12 10 14 14 6 9 8 8 11 3 | 63 62 62 69 61 63 60 59 61 57 61
19 | 11 14 12 17 14 6 13 12 12 15 4 | 29 31 28 35 31 27 34 31 32 26 29
20E | 9 11 10 10 15 4 10 9 7 8 3 | 26 25 24 25 28 22 22 25 24 21 23
21 | 7 11 17 15 12 5 11 14 11 15 4 | 29 30 24 35 36 27 29 32 28 27 28
22E | 8 9 9 8 13 3 9 8 9 10 3 | 41 38 38 39 41 38 37 37 40 37 38
23 | 11 15 13 16 17 7 14 21 13 15 5 | 26 29 21 26 26 18 27 30 21 16 21
24 | 6 11 15 11 13 4 15 8 13 15 4 | 20 27 23 23 27 20 29 21 23 16 21
25E | 8 15 15 8 15 5 12 10 12 11 4 | 20 26 27 20 19 20 25 24 24 18 21
26 | 6 9 11 12 13 4 9 7 9 11 3 | 28 30 26 33 30 27 30 31 26 24 28
27 | 9 8 14 17 8 5 11 10 12 16 4 | 37 34 30 38 37 33 39 38 38 36 35
28E | 7 17 9 13 12 5 9 9 11 7 4 | 20 26 18 26 24 16 22 18 23 16 19
29 | 12 14 16 16 14 6 18 13 15 14 5 | 28 30 28 35 34 28 29 30 31 31 28
30 | 7 8 11 8 8 4 10 9 8 10 3 | 20 23 23 17 26 19 26 20 23 19 20
31 | 10 13 15 21 16 7 12 19 11 14 5 | 28 32 25 28 35 22 27 33 34 20 26
32E | 12 24 12 13 17 4 14 13 15 14 5 | 49 61 51 52 47 47 51 43 53 44 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 13 14 14 6 13 14 12 15 |T 33 35 31 34 34 29 33 33 34 29 31
WRMS | 9 13 13 13 14 5 13 12 11 13 |NE 29 31 27 31 32 26 31 31 29 27 27
MEDI | 9 12 13 13 14 5 12 12 12 12 |MD 27 30 26 31 31 25 29 30 27 24 27
Table 3.1813.5 GPS week: 1813 Day: 5 MJD: 56940.000
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 7 16 8 12 3 13 9 8 11 3 | 19 25 21 21 24 17 31 19 21 20 20
2 | 8 14 16 18 14 7 13 13 15 20 5 | 24 29 21 27 29 22 28 32 29 19 22
X3E | 22 31 29 18 --- 22 --- 25 35 --- 12 | 65 64 55 54 --- 54 --- 53 72 --- 57
4 | 7 9 14 10 10 3 9 13 10 10 3 | 23 23 22 25 22 20 28 25 25 20 22
5E | 7 15 11 13 16 5 14 14 11 8 4 | 51 49 48 51 53 47 48 55 48 49 50
6 | 9 9 14 13 12 6 14 22 9 8 4 | 21 30 25 23 26 19 32 27 19 23 22
7 | 12 14 13 17 18 5 14 13 11 14 5 | 25 28 21 29 28 19 28 24 23 20 21
8 | 7 9 11 13 14 4 9 9 8 22 4 | 18 19 16 17 16 13 22 14 17 30 16
9 | 21 14 15 26 17 15 16 43 17 38 8 | 60 66 59 49 55 55 69 79 59 77 60
10E | 9 20 17 12 16 7 16 12 21 12 5 | 48 50 46 44 43 42 49 48 46 38 44
11 | 7 10 17 8 13 4 10 11 8 9 3 | 37 37 33 37 43 35 45 40 39 35 36
12E | 11 19 8 15 20 6 26 19 11 13 5 | 23 28 17 23 26 18 30 19 26 18 19
13 | 8 13 17 15 21 5 12 12 11 10 4 | 25 32 22 29 36 21 30 29 22 22 24
14 | 12 11 14 13 15 5 12 13 11 13 4 | 27 29 23 29 33 23 31 30 30 17 25
15 | 9 13 15 14 18 4 11 14 18 13 4 | 26 27 24 25 27 17 25 25 26 19 22
16E | 10 11 8 17 20 6 14 17 15 10 4 | 23 22 19 22 24 18 28 28 23 20 20
17 | 9 14 14 13 16 6 13 13 14 15 4 | 21 31 23 29 29 23 31 32 31 24 25
18E | 8 11 8 10 11 4 12 12 13 9 3 | 55 56 56 56 59 55 57 63 56 56 56
19 | 12 15 12 17 17 5 10 12 13 15 4 | 24 31 25 28 30 22 32 27 26 20 24
20E | 10 10 9 10 14 4 14 8 9 7 3 | 26 28 22 25 24 22 32 25 26 22 23
21 | 9 9 17 14 15 5 12 20 12 15 4 | 25 30 22 25 33 22 34 29 27 26 25
22E | 9 14 8 11 10 4 11 20 7 9 4 | 44 41 41 45 48 42 43 56 43 42 43
23 | 10 15 16 17 19 5 15 19 13 14 5 | 25 29 20 26 26 18 29 26 21 14 20
24 | 7 10 14 10 16 4 14 11 14 15 4 | 19 25 21 17 27 15 28 21 20 14 18
25E | 9 9 15 8 14 7 15 15 12 12 4 | 17 21 23 17 21 15 26 21 24 12 17
26 | 7 8 14 10 12 5 11 10 13 9 3 | 28 29 28 31 30 29 29 32 38 29 29
27 | 13 9 13 17 16 7 11 17 11 16 4 | 38 38 37 40 46 36 48 44 37 36 38
28E | 9 12 10 11 16 6 11 8 10 4 3 | 22 24 15 26 23 16 26 18 22 16 18
29 | 11 13 17 19 16 7 17 12 16 14 5 | 21 29 23 28 29 20 26 29 30 24 23
30 | 6 8 11 10 11 4 14 11 12 8 3 | 19 24 21 19 26 17 33 19 19 20 20
31 | 10 12 15 18 17 7 12 22 9 13 5 | 24 32 21 25 35 20 30 36 29 18 24
32E | 13 22 18 16 16 5 14 19 11 14 5 | 47 59 49 50 45 45 55 35 49 39 46
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 14 14 15 6 13 16 12 14 |T 30 33 28 31 32 26 34 33 31 27 29
WRMS | 10 13 14 12 15 5 13 13 11 13 |NE 26 30 25 27 30 23 32 30 28 25 25
MEDI | 9 12 14 13 16 5 13 13 11 13 |MD 25 29 23 27 29 21 31 29 26 22 23
Table 3.1813.6 GPS week: 1813 Day: 6 MJD: 56941.000
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 12 10 12 4 10 11 8 8 3 | 21 24 21 21 26 18 26 21 23 20 21
2 | 8 14 15 16 15 5 12 15 11 22 5 | 30 33 27 32 35 27 35 35 29 27 28
X3E | 23 20 24 19 --- 18 --- 17 38 --- 11 | 58 65 62 57 --- 65 --- 65 74 --- 60
4 | 7 10 10 9 12 5 7 14 8 10 3 | 28 27 28 29 31 26 27 33 32 28 28
5E | 7 13 10 14 14 4 15 12 9 6 4 | 74 70 68 71 74 67 69 73 72 69 70
6 | 7 8 13 11 14 6 12 22 11 11 4 | 29 33 31 30 30 27 32 28 31 33 28
7 | 10 15 13 20 15 4 13 14 9 13 4 | 30 30 23 34 32 23 25 29 28 23 25
8 | 8 9 11 12 18 4 9 11 9 21 4 | 20 22 18 17 23 15 20 18 19 30 19
9 | 20 14 13 24 19 14 14 43 17 36 8 | 81 82 79 64 72 75 83 89 78 92 77
10E | 12 18 12 14 14 7 15 17 17 14 5 | 47 56 49 46 49 45 51 59 52 43 49
11 | 8 11 15 9 12 5 9 12 15 10 4 | 56 54 53 57 61 54 57 60 57 53 55
12E | 15 19 8 17 56 5 24 16 11 16 7 | 24 27 17 25 54 18 26 21 23 19 19
13 | 9 13 15 16 25 5 11 15 11 10 4 | 32 38 29 39 44 31 34 39 30 28 32
14 | 11 12 13 14 14 6 12 12 13 14 4 | 34 35 27 38 35 30 32 35 29 26 30
15 | 9 11 14 22 18 5 15 11 15 14 5 | 29 31 28 36 31 24 28 29 30 24 27
16E | 7 12 8 16 19 6 12 14 13 14 4 | 20 23 20 25 25 18 25 24 20 25 21
17 | 9 14 12 14 16 6 14 14 9 18 4 | 32 35 31 36 39 33 37 41 32 34 33
18E | 8 12 7 15 11 5 10 11 7 7 3 | 62 59 59 59 57 58 56 60 55 57 57
19 | 10 15 11 17 11 6 11 15 11 14 4 | 34 37 32 38 35 31 34 39 31 33 32
20E | 8 11 8 10 17 5 12 12 8 8 3 | 31 30 27 27 28 26 25 29 30 23 27
21 | 7 11 16 18 15 5 13 23 14 15 5 | 34 36 30 39 43 31 33 41 32 36 33
22E | 11 10 8 12 10 5 9 15 10 7 3 | 46 42 42 43 41 41 39 50 39 46 41
23 | 10 17 14 15 17 6 13 21 13 15 5 | 27 32 24 30 32 23 29 32 20 20 24
24 | 7 9 13 14 17 5 10 12 8 16 4 | 20 28 23 23 30 20 29 23 25 17 22
25E | 6 9 15 12 22 4 13 13 12 13 4 | 18 22 26 18 18 17 24 23 24 13 19
26 | 9 9 12 12 16 4 9 11 11 13 4 | 24 29 25 28 30 25 25 31 28 31 26
27 | 11 8 13 18 11 8 9 16 9 14 4 | 47 47 42 49 50 44 50 52 47 44 46
28E | 8 11 6 13 15 3 10 9 7 8 3 | 21 23 16 19 27 16 19 20 20 15 18
29 | 13 13 14 17 16 4 18 15 15 16 5 | 32 31 29 38 33 30 32 37 34 32 31
30 | 7 8 11 12 11 4 15 13 10 7 3 | 22 25 23 18 28 19 31 23 23 21 22
31 | 8 12 14 14 16 6 15 15 13 13 4 | 24 34 22 26 35 23 28 29 28 22 25
32E | 11 20 14 13 20 6 18 20 19 13 6 | 48 58 51 49 45 46 56 34 50 37 46
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 12 15 18 6 13 16 12 14 |T 35 38 33 36 38 32 36 38 35 32 34
WRMS | 9 13 12 14 15 5 13 14 10 12 |NE 32 35 30 34 36 29 34 36 32 32 31
MEDI | 8 12 13 14 15 5 12 14 11 13 |MD 30 33 28 34 35 27 32 33 30 28 28
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 4.1813 GPS week: 1813 MJD: 56935.0-56941.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 |U 7 8 22 |U 6 9 27 |U 7 7 16 |
emr | emr 3041 | 9 9 25 |U 9 11 29 | 9 9 21 |
esa | esa 3058 | 8 8 21 |U 7 10 30 | 8 7 18 |
gfz | gfz 3058 |U 8 8 22 |U 8 11 30 |U 8 7 20 |
grg | grg 2976 | 11 11 30 |U 9 11 36 |U 10 11 21 |
igr | igr 3014 | 7 8 23 | 6 8 28 | 8 7 18 |
igs | igs 2991 | 8 8 23 | 8 11 29 | 8 8 18 |
jpl | jpl 2967 | 9 9 28 | 10 15 34 |U 8 8 20 |
mit | mit 3058 | 10 11 26 |U 10 14 41 |U 9 9 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 5.1813.0 GPS week: 1813 Day: 0 MJD: 56935.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 8 8 26 | 7 7 26 | 6 7 20 |
emr | emr 3051 | 8 9 27 | 8 7 25 | 7 8 18 |
esa | esa 3072 | 7 7 20 | 7 7 28 | 7 6 17 |
gfz | gfz 3060 | 7 8 24 | 7 7 26 | 6 6 19 |
grg | grg 2976 | 10 8 28 | 8 8 34 | 9 9 22 |
igr | igr 3014 | 7 7 23 | 6 6 27 | 7 6 17 |
igs | igs 2964 | 8 8 25 | 6 7 26 | 6 7 18 |
jpl | jpl 2968 | 8 9 28 | 7 11 29 | 7 6 18 |
mit | mit 3072 | 7 10 24 | 7 7 31 | 7 5 18 |
Table 5.1813.1 GPS week: 1813 Day: 1 MJD: 56936.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 6 5 18 | 6 9 24 | 7 6 18 |
emr | emr 3050 | 9 6 26 | 7 7 27 | 15 11 39 |
esa | esa 3072 | 7 5 19 | 7 8 29 | 9 7 23 |
gfz | gfz 3059 | 7 5 20 | 7 8 24 | 9 6 22 |
grg | grg 2976 | 11 8 24 | 8 9 38 | 11 9 23 |
igr | igr 3030 | 6 5 19 | 6 7 24 | 8 5 21 |
igs | igs 2972 | 10 7 24 | 7 7 26 | 10 6 23 |
jpl | jpl 2968 | 10 8 30 | 10 15 39 | 9 6 24 |
mit | mit 3072 | 12 16 29 | 14 15 83 | 10 13 28 |
Table 5.1813.2 GPS week: 1813 Day: 2 MJD: 56937.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3049 | 9 8 26 | 5 10 29 | 7 8 14 |
emr | emr 2968 | 11 9 29 | 6 11 29 | 8 8 17 |
esa | esa 2976 | 9 8 24 | 5 8 28 | 7 8 15 |
gfz | gfz 3058 | 9 7 25 | 6 10 28 | 7 8 17 |
grg | grg 2976 | 11 11 31 | 7 10 32 | 9 11 18 |
igr | igr 2975 | 9 8 26 | 5 9 29 | 7 8 16 |
igs | igs 2974 | 9 8 26 | 6 10 28 | 7 8 15 |
jpl | jpl 2968 | 10 8 27 | 9 15 33 | 7 9 17 |
mit | mit 2976 | 10 9 27 | 6 11 26 | 8 8 20 |
Table 5.1813.3 GPS week: 1813 Day: 3 MJD: 56938.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 7 9 21 | 6 9 27 | 7 7 13 |
emr | emr 3055 | 8 11 27 | 8 13 28 | 7 6 14 |
esa | esa 3072 | 8 10 22 | 9 13 32 | 8 5 14 |
gfz | gfz 3051 | 7 9 20 | 9 13 35 | 6 4 16 |
grg | grg 2976 | 8 12 30 | 8 9 34 | 8 8 17 |
igr | igr 3009 | 7 9 22 | 6 10 32 | 8 6 18 |
igs | igs 3020 | 7 9 21 | 8 12 32 | 7 5 13 |
jpl | jpl 2968 | 11 12 32 | 8 13 32 | 8 6 15 |
mit | mit 3072 | 9 9 22 | 11 17 40 | 7 5 14 |
Table 5.1813.4 GPS week: 1813 Day: 4 MJD: 56939.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 9 10 30 | 6 7 30 | 8 8 15 |
emr | emr 3060 | 10 9 30 | 9 8 34 | 9 9 18 |
esa | esa 3072 | 10 11 29 | 7 7 33 | 8 8 17 |
gfz | gfz 3059 | 9 11 29 | 8 8 31 | 8 8 21 |
grg | grg 2976 | 13 15 39 | 10 7 44 | 13 14 23 |
igr | igr 3022 | 9 10 30 | 6 7 32 | 9 9 18 |
igs | igs 3015 | 10 10 30 | 7 8 34 | 8 9 17 |
jpl | jpl 2968 | 10 10 30 | 16 17 43 | 9 10 19 |
mit | mit 3072 | 9 9 29 | 7 10 33 | 9 9 18 |
Table 5.1813.5 GPS week: 1813 Day: 5 MJD: 56940.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 8 9 22 | 6 10 26 | 8 7 16 |
emr | emr 3052 | 8 10 21 | 12 22 30 | 9 10 17 |
esa | esa 3072 | 7 9 20 | 7 16 28 | 8 9 17 |
gfz | gfz 3060 | 9 10 22 | 7 15 32 | 9 7 18 |
grg | grg 2976 | 13 13 31 | 11 18 39 | 13 17 22 |
igr | igr 3021 | 8 9 23 | 5 8 27 | 8 8 17 |
igs | igs 2969 | 9 10 23 | 10 20 29 | 9 11 17 |
jpl | jpl 2967 | 8 11 27 | 10 18 30 | 9 9 20 |
mit | mit 3072 | 17 14 35 | 9 19 41 | 10 12 17 |
Table 5.1813.6 GPS week: 1813 Day: 6 MJD: 56941.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 5 6 13 | 9 13 29 | 9 7 21 |
emr | emr 3056 | 7 8 18 | 10 11 31 | 10 11 25 |
esa | esa 3072 | 7 6 14 | 9 11 30 | 11 9 22 |
gfz | gfz 3059 | 6 7 14 | 10 14 32 | 10 8 25 |
grg | grg 2976 | 10 9 26 | 11 13 34 | 10 12 23 |
igr | igr 3033 | 5 6 14 | 9 12 26 | 11 8 21 |
igs | igs 3028 | 6 6 13 | 9 13 30 | 9 8 21 |
jpl | jpl 2968 | 8 7 24 | 11 15 34 | 9 8 24 |
mit | mit 3072 | 6 6 16 | 14 17 34 | 10 10 23 |
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 6.1813 GPS week: 1813 MJD: 56935.500-56941.500
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 | -12 -5 -40 31 -5 | 27 34
| 17 17 67 123 11 | 2
emr uuuuu | 34 -18 44 87 0 | 5 21
| 26 22 132 83 20 | 5
esa uuuuu | 2 -11 4 -57 -5 | 25 32
| 10 20 68 43 8 | 1
gfz uuuux | 5 -29 87 -3 -55 | -6 36
| 25 18 106 118 12 | 17
grg uuuuu | -29 11 -25 -85 -2 | 29 34
| 19 21 70 129 5 | 2
igr xxxxx | 5 14 10 44 -1 | 1 19
| 22 17 55 35 6 | 2
irf xxxxx | 5 11 -22 -5 -2 | 1 16
| 11 11 26 32 4 | 2
jpl uuuuu | 12 6 27 149 -7 | 17 26
| 25 26 66 71 10 | 2
mit uuuuu | -7 21 -17 -63 0 | 21 26
| 30 20 44 68 3 | 2
ngs uuuuu | -9 27 -48 -89 4 | 7 16
| 52 49 69 180 13 | 2
sio uuxxx | 5 5 -7 89 -4 | 42 45
| 15 17 40 84 9 | 2
Table 7.1813.0 GPS week: 1813 Day: 0 MJD: 56935.500
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 | -9 12 -100 101 10 | 26 32
emr uuuuu | 58 -30 129 169 -19 | 13 29
esa uuuuu | -12 -49 -8 -43 11 | 25 31
gfz uuuux | 11 -62 38 137 -69 | 16 25
grg uuuuu | -48 -1 -110 -288 6 | 28 33
igr xxxxx | -18 20 -80 52 4 | -1 17
irf xxxxx | -5 -6 -26 -14 2 | 1 16
jpl uuuuu | -20 34 35 193 -3 | 16 24
mit uuuuu | -40 -11 17 -97 1 | 21 26
ngs uuuuu | 61 108 6 -332 0 | 6 15
sio uuxxx | -15 0 -64 43 12 | 38 42
Table 7.1813.1 GPS week: 1813 Day: 1 MJD: 56936.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 14 -7 -133 122 3 | 27 33
emr uuuuu | 52 -52 263 157 17 | 7 20
esa uuuuu | 8 -16 7 -37 -2 | 25 31
gfz uuuux | 12 -36 0 68 -68 | 8 26
grg uuuuu | -33 -5 -19 -242 -7 | 28 33
igr xxxxx | -26 22 17 40 -4 | 0 18
irf xxxxx | -7 10 -39 -6 0 | 1 16
jpl uuuuu | 26 26 41 196 -16 | 17 24
mit uuuuu | -30 28 -24 -88 1 | 20 25
ngs uuuuu | -45 65 -86 -248 -2 | 5 14
sio uuxxx | -12 -5 -1 34 -4 | 40 44
Table 7.1813.2 GPS week: 1813 Day: 2 MJD: 56937.500
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 | -1 1 -90 -6 5 | 27 33
emr uuuuu | 52 4 74 142 -11 | 8 21
esa uuuuu | 17 1 -97 -145 -6 | 25 31
gfz uuuux | -7 -9 -59 -122 -57 | 1 32
grg uuuuu | -17 -21 95 -33 0 | 28 33
igr xxxxx | -1 -3 35 -11 9 | 1 17
irf xxxxx | 4 1 -20 -64 -1 | 2 15
jpl uuuuu | 39 17 79 144 5 | 17 24
mit uuuuu | -32 8 32 -177 2 | 21 26
ngs uuuuu | -67 14 56 205 3 | 4 13
sio uuxxx | 4 -26 15 56 -8 | 42 45
Table 7.1813.3 GPS week: 1813 Day: 3 MJD: 56938.500
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 | -1 18 -32 213 -7 | 31 37
emr uuuuu | 54 -29 60 132 -26 | 9 22
esa uuuuu | -2 -16 -43 -34 -8 | 27 33
gfz uuuux | -41 -32 87 -202 -56 | -4 33
grg uuuuu | -59 17 -31 -72 -1 | 32 37
igr xxxxx | 15 -14 23 74 1 | 5 20
irf xxxxx | 12 22 -41 35 -2 | 4 17
jpl uuuuu | -26 -27 135 1 -14 | 21 28
mit uuuuu | 9 42 -60 -13 1 | 23 29
ngs uuuuu | 35 20 -111 -153 22 | 7 16
sio uuxxx | 5 12 27 47 1 | 45 48
Table 7.1813.4 GPS week: 1813 Day: 4 MJD: 56939.500
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 -25 30 -28 -11 | 28 34
emr uuuuu | 1 7 -45 52 -6 | 1 17
esa uuuuu | -2 0 10 -59 -6 | 25 32
gfz uuuux | 7 -33 142 45 -55 | -13 38
grg uuuuu | -26 24 -78 -15 -6 | 29 34
igr xxxxx | 23 32 -45 54 -5 | 3 19
irf xxxxx | -2 23 -28 0 -3 | 2 16
jpl uuuuu | 15 24 -26 172 -22 | 18 27
mit uuuuu | -16 44 -3 -60 0 | 21 26
ngs uuuuu | 40 -47 -29 -85 21 | 8 17
sio uuxxx | 10 26 23 110 -15 | 44 46
Table 7.1813.5 GPS week: 1813 Day: 5 MJD: 56940.500
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 | -30 -9 23 -25 -22 | 26 34
emr uuuuu | 22 1 -139 -31 19 | -1 18
esa uuuuu | 7 12 123 -67 -10 | 24 31
gfz uuuux | 17 -23 261 41 -47 | -22 46
grg uuuuu | -10 41 -66 6 -2 | 28 33
igr xxxxx | 33 27 86 10 -8 | 1 20
irf xxxxx | 14 8 34 -11 -3 | 0 16
jpl uuuuu | 15 -31 -20 209 -1 | 17 27
mit uuuuu | 25 12 12 -45 1 | 19 25
ngs uuuuu | -47 -2 -141 -63 -8 | 10 18
sio uuxxx | 23 8 15 65 -4 | 42 45
Table 7.1813.6 GPS week: 1813 Day: 6 MJD: 56941.500
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 | -34 -25 18 -159 -13 | 24 33
emr uuuuu | 1 -27 -37 -10 23 | 1 18
esa uuuuu | -3 -12 38 -14 -11 | 23 31
gfz uuuux | 40 -11 139 15 -33 | -31 52
grg uuuuu | -9 24 35 50 -7 | 27 32
igr xxxxx | 13 11 34 90 -5 | 0 20
irf xxxxx | 22 17 -36 25 -9 | -1 17
jpl uuuuu | 33 1 -53 129 1 | 16 27
mit uuuuu | 35 26 -91 36 -6 | 18 24
ngs uuuuu | -38 27 -31 52 -10 | 9 18
sio uuxxx | 21 16 -66 271 -13 | 41 45
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