[IGSREPORT-21677] Wk 1730 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Mar 22 09:59:19 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1730 (Mar 03, 2013 - Mar 09, 2013)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi 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:
igs1730[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1730[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1730[0-6].cls IGS GPS clock combination summary report.
igs17307.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17307.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 | CHUR CHUR
0 | EMR | 4 8 9 4 8 9
0 | ESA | UNSA
0 | GFZ | 4 8 9 LHAZ SYOG
0 | GRG | 4 9 4 9 NICO NICO USNO
0 | JPL | 4 8 9 BOR1
0 | MIT | 4 9 14 22 4 9 14 22 USNO WROC BOR1 WROC
1 | COD | 4 8 4 8
1 | EMR | 8 9 8 9 MATE
1 | ESA | 4 4 UNSA
1 | GFZ | 4 8 9 MATE POTS
1 | GRG | 9 21 21 AREQ TIXI
1 | JPL | 8 9 BAKE
1 | MIT | 4 9 4 8
2 | COD | 2 4 2 4 WROC WROC
2 | EMR | 8 9 8 9 HERS
2 | ESA | 4 4
2 | GFZ | 4 9 ZAMB
2 | GRG | 8 9 13 9 13 NKLG ABMF HOFN NKLG
2 | JPL | 8 9
2 | MIT | 2 8 9 2 9 VILL
3 | COD | 4 1 4
3 | EMR | 1 8 1 8 9 HARB WROC HARB WROC
3 | ESA | 4 4 MAS1 UNSA
3 | GFZ | 9 GOPE MAS1 MIZU NRIL SYOG
3 | GRG | 9 LPGS MAS1 NICO ADIS AREQ ASPA LHAZ LPGS
3 | JPL | 1 8 9 NKLG
3 | MIT | 21 1 9 21 NICO WROC GRAZ NICO TWTF WROC
4 | COD | 4 4 9 JOZ2 JOZ2 KOSG
4 | EMR | 8 8 MCM4 TNML MCM4 TNML
4 | ESA | 4 4 9
4 | GFZ | 9
4 | GRG | 8 8 NICO ARTU BARH GOPE
4 | JPL | 8 9
4 | MIT | 8 8 NICO
5 | COD | 4 9 4 9
5 | EMR | 8 8 HARB HARB HERS
5 | ESA | 4 9 4 9 DGAV
5 | GFZ | 30 IRKT KOSG LHAZ NRIL RIOP YAR2
5 | GRG | 8 8 HARB LPGS NICO WROC HARB LPGS NICO TRO1 WROC
5 | JPL | 8 9
5 | MIT | 8 12 23 8 9 12 19 23 NYAL WROC NYAL WROC
6 | COD | 4 9 4 9
6 | EMR | 8 8 HERS HERS
6 | ESA | 4 9 4 9 UNSA
6 | GFZ | 9 LHAZ MATE
6 | GRG | 8 8 ADIS
6 | JPL | 8 9
6 | MIT | 8 11 13 14 18 21 22 8 11 13 14 18 21 22 DARW MDVJ
6 | MIT | WROC
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 table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G13 | 2013_03_06 | 2013020
G13 | 2013_03_07 | 2013020
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | GRG | 4
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G01 | | | 2 | | | | |
PRN G13 | | | | 4 | 1 | | |
9. 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.
10. 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 | .7 1.4 -1.0 -35 8 -2 -.09
EMR | 0 | 12.0 -7.7 19.2 2 13 -6 -.10
ESA | 0 | 1.5 -.1 -5.4 31 -184 189 .02
GFZ | 0 | .6 .7 -.3 -5 -19 -6 -.07
GRG | 0 | 4.1 -5.6 13.7 -31 31 3 .33
JPL | 0 | 1.9 -.7 18.8 -76 -16 39 .09
MIT | 0 | 3.8 -.5 10.9 1 -3 -19 -.05
NGS | 0 | -.7 -2.9 1.7 -38 6 4 .56
SIO | 0 | 5.1 -1.1 2.3 13 -99 73 .07
COD | 1 | .7 .7 -.7 -23 -11 -18 .10
EMR | 1 | 13.3 -13.6 12.9 -3 6 5 .32
ESA | 1 | .5 -5.6 -3.2 -33 -119 174 .21
GFZ | 1 | .4 .4 -.1 -16 -24 -9 .16
GRG | 1 | 3.2 -7.3 14.8 -14 52 -54 .59
JPL | 1 | 1.2 -2.4 13.9 -96 28 -21 .26
MIT | 1 | -.1 -2.5 7.4 -5 1 -18 .21
NGS | 1 | 4.8 -10.0 -1.4 -37 -34 54 .56
SIO | 1 | 2.4 -1.6 -3.4 11 -100 94 .34
COD | 2 | .8 1.1 -1.0 -35 -3 -10 .16
EMR | 2 | 8.6 -10.8 15.2 0 10 3 .31
ESA | 2 | 2.5 -2.6 -3.6 34 -206 179 .26
GFZ | 2 | -.2 .2 -.2 -9 -27 -25 -.02
GRG | 2 | 4.8 -3.1 15.7 -21 17 -27 .62
JPL | 2 | 5.4 -6.0 17.6 -96 -1 -23 .32
MIT | 2 | .3 -.5 10.2 8 -11 -24 .23
NGS | 2 | 4.7 -2.6 7.1 -61 -21 33 .57
SIO | 2 | 4.7 -1.7 19.0 -46 4 117 .35
COD | 3 | 1.0 1.5 -.2 -53 -12 -11 .06
EMR | 3 | 7.4 -7.6 10.5 -3 3 8 .28
ESA | 3 | 3.5 -.3 -4.2 46 -198 154 .27
GFZ | 3 | .1 .5 .2 -29 -16 -18 -.22
GRG | 3 | 3.0 -4.7 2.7 -41 42 -16 .46
JPL | 3 | .0 3.6 11.4 -60 20 6 .20
MIT | 3 | 1.1 2.8 9.0 0 -6 -4 .21
NGS | 3 | -2.6 2.0 2.6 -14 24 -7 .50
SIO | 3 | 3.0 3.5 2.4 35 -46 -7 .24
COD | 4 | .6 .7 -.4 -40 -7 -6 .03
EMR | 4 | 3.7 -8.5 .1 -4 6 1 .23
ESA | 4 | 2.4 -2.7 -5.2 25 -215 171 .15
GFZ | 4 | .3 .4 -.1 -29 -25 -10 -.17
GRG | 4 | 1.6 -7.3 5.1 -13 26 -20 .47
JPL | 4 | -4.2 4.2 6.1 -50 -17 4 .28
MIT | 4 | -.1 -.8 7.7 0 -3 -13 .07
NGS | 4 | 6.1 3.6 1.5 6 -37 61 .53
SIO | 4 | 1.5 -1.0 -7.1 36 -129 201 .08
COD | 5 | 1.2 1.2 -.7 -29 3 -23 .12
EMR | 5 | 3.9 -2.2 1.9 -1 -3 16 .15
ESA | 5 | 4.7 -3.4 -3.2 10 -210 180 .01
GFZ | 5 | -.1 .3 -.1 -28 -15 -14 .07
GRG | 5 | 1.7 -3.5 7.8 -15 24 11 .33
JPL | 5 | 2.4 6.2 7.9 -80 29 -29 .19
MIT | 5 | -.2 1.7 9.4 7 -8 -15 -.10
NGS | 5 | .4 -1.9 8.5 -63 -5 5 .64
SIO | 5 | 4.3 -.2 -12.0 67 -182 150 .24
COD | 6 | .6 1.2 -1.1 -35 -13 5 .19
EMR | 6 | 4.7 -11.8 6.8 1 2 10 .47
ESA | 6 | 1.7 -4.9 -.3 11 -161 179 .22
GFZ | 6 | -.5 .4 -.4 -36 -18 -18 .25
GRG | 6 | -.9 -8.0 5.0 -21 17 3 .42
JPL | 6 | 3.8 -.7 9.0 -40 0 -1 .40
MIT | 6 | 2.5 .6 12.5 -1 -3 -18 .01
NGS | 6 | 6.4 -6.0 3.7 -64 -30 42 .56
SIO | 6 | 1.5 -1.8 -.9 25 -104 262 .02
11. 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.
12. 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 1.1730.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1730.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 2.1730.[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 3.1730.[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 5.1730.0-6). 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 1730 summary. (Mar 03, 2013 - Mar 09, 2013)
Table 1.1730.a GPS week: 1730 MJD: 56354.000-56360.000
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 268| 0 0 1 2 -3 7 -.37 11 11 | -775 -268 22 93
| 0 0 0 16 14 13 .03 | 716 1400
emr 80| 0 -4 2 -29 -21 9 .27 18 18 | 3899 401 14 97
| 1 1 2 20 8 24 .02 | 1670 1081
esa 150| 1 0 0 11 -11 -4 .08 7 6 | -939 380 12 114
| 0 0 0 11 15 10 .02 | 1324 2022
gfz 202| 0 0 -5 -20 -12 -12 -.39 11 11 | 108 -39 19 103
| 0 1 1 42 48 9 .03 | 312 412
grg 137| 2 0 0 -3 8 -10 .66 17 15 | -59 -102 19 146
| 1 0 2 10 16 9 .02 | 367 780
igr n/a| 0 0 0 -1 52 -24 -.13 5 4 | 191 442 17 82
| 0 0 1 18 20 11 .02 | 1720 1193
jpl 80| -1 -1 1 -13 1 -7 .36 17 16 | 3885 407 17 105
| 1 1 1 24 9 7 .03 | 1618 1241
mit 239| 0 0 0 19 -5 15 -.58 14 11 | -196 169 25 186
| 1 1 0 18 10 16 .02 | 299 603
ngs 238| 0 0 0 -1 42 0 .32 11 9 | -653 -528 1797 3426
| 0 1 2 28 59 25 .04 | 558 1169
sio 268| 0 -2 -2 -48 -88 91 -.23 19 18 | --- --- --- ---
| 0 0 0 33 53 95 .04 | --- ---
Table 1.1730.b GPS week : 1730 MJD: 56354.000-56360.000
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 | 6 5 7 6 6 5 5 |
2 | 5 5 5 5 4 4 4 |
3 | 4 4 4 4 3 4 4 |
4 | 12 6 6 6 7 5 6 |
5 | 5 5 5 5 5 5 5 |
6 | 4 4 4 4 3 3 3 |
7 | 4 4 4 4 4 4 5 |
8 | 7 8 7 6 6 6 7 |
9 | 6 6 6 6 6 6 6 |
10 | 4 4 4 4 4 4 4 |
11 | 4 3 4 4 4 5 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 4 4 6 0 4 5 |
14 | 4 4 4 5 5 5 5 |
15 | 5 6 5 6 6 5 5 |
16 | 5 5 4 5 5 5 5 |
17 | 6 5 5 5 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 4 5 5 4 5 4 5 |
20 | 4 5 5 5 5 6 4 |
21 | 4 4 4 4 4 4 6 |
22 | 5 4 5 5 5 5 5 |
23 | 4 4 4 4 4 5 4 |
24 | 5 6 5 5 5 5 5 |
25 | 4 4 4 4 4 4 5 |
26 | 4 4 4 4 5 4 4 |
27 | 0 0 0 0 0 0 0 |
28 | 5 5 5 4 5 5 5 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 3 4 4 4 4 |
31 | 4 5 5 4 4 5 5 |
32 | 3 3 4 4 4 4 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1730.0 GPS week: 1730 Day: 0 MJD: 56354.000
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 266| 0 2 2 -20 -18 -14 -.37 11 11 | 187 -2530 21 87
emr 80| 1 -5 4 -5 -31 -31 .26 18 18 | 2011 1246 16 110
esa 150| 0 1 1 1 -3 5 .09 10 7 | -936 411 14 124
gfz 199| 0 -2 -3 -38 -12 -15 -.43 12 11 | 451 328 20 101
grg 138| 4 0 -2 -8 10 -4 .68 25 14 | -199 852 19 134
igr n/a| 0 0 -1 0 40 -45 -.16 5 5 | -2034 1475 17 92
jpl 80| -1 -2 1 12 0 -12 .35 16 16 | 1814 1452 16 93
mit 240| 0 0 0 13 6 -10 -.56 14 11 | -11 363 24 185
ngs 243| 1 0 -4 29 42 29 .36 12 9 | 83 -2355 1764 3721
sio 252| 0 -1 -3 -48 -92 24 -.23 19 16 | --- --- --- ---
Table 2.1730.1 GPS week: 1730 Day: 1 MJD: 56355.000
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 270| -1 1 3 19 15 0 -.38 11 11 | -1544 1576 21 91
emr 80| 1 -4 3 -8 -4 -3 .27 18 18 | 2584 1562 15 104
esa 150| 1 0 0 17 7 13 .09 6 6 | -2090 3199 14 143
gfz 205| 0 0 -4 -64 0 0 -.39 10 9 | -115 618 19 98
grg 138| 2 1 -3 2 34 -7 .64 16 16 | -492 600 21 158
igr n/a| 0 1 -1 13 68 -19 -.12 4 4 | -1509 1556 18 85
jpl 80| 0 -1 3 -23 9 -9 .30 16 15 | 2278 1608 18 104
mit 240| -2 -1 0 32 -14 2 -.57 15 12 | -503 891 24 195
ngs 244| 0 0 -3 -19 -40 -22 .26 11 9 | -1440 1468 2099 3642
sio 250| 0 -2 -1 -27 -105 81 -.22 19 17 | --- --- --- ---
Table 2.1730.2 GPS week: 1730 Day: 2 MJD: 56356.000
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 270| -1 0 0 26 5 20 -.37 11 10 | -52 -1104 20 102
emr 80| 0 -3 3 -9 -23 24 .29 18 18 | 3081 -276 15 89
esa 150| 1 0 0 16 -14 -8 .08 7 6 | 1468 -3070 12 114
gfz 202| 0 -1 -7 -62 13 -5 -.40 11 10 | 72 -405 18 96
grg 139| 3 0 3 -5 2 -19 .63 16 15 | 526 -1015 17 147
igr n/a| 0 1 -1 -12 59 -8 -.14 5 4 | -260 -446 17 86
jpl 80| 1 -3 3 -36 17 -4 .34 17 16 | 3540 -544 17 111
mit 240| -1 -1 0 53 -21 4 -.56 15 12 | 175 -482 23 167
ngs 242| 0 2 0 -15 14 -11 .28 10 9 | -99 -1144 1853 3478
sio 277| 0 -2 -2 -105 -12 86 -.19 19 17 | --- --- --- ---
Table 2.1730.3 GPS week: 1730 Day: 3 MJD: 56357.000
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 268| -1 0 1 7 -7 25 -.34 11 10 | -1383 970 24 94
emr 80| 0 -6 3 -45 -24 40 .24 19 19 | 2671 1067 13 86
esa 150| 2 0 0 28 -40 -11 .12 6 6 | -1596 1061 13 116
gfz 201| 0 -1 -7 -46 47 -27 -.36 11 10 | -438 18 22 93
grg 138| 1 1 0 -1 17 4 .65 16 16 | -355 -172 20 124
igr n/a| 0 1 -1 31 11 -21 -.10 5 4 | -620 1285 17 85
jpl 80| -2 0 2 9 -7 -18 .38 19 18 | 3067 1363 19 120
mit 240| 0 0 0 17 0 31 -.56 13 11 | -665 710 22 164
ngs 238| -1 1 1 -12 57 -18 .31 12 9 | -739 -93 1676 2970
sio 270| 0 -2 -2 -22 -44 -58 -.20 19 20 | --- --- --- ---
Table 2.1730.4 GPS week: 1730 Day: 4 MJD: 56358.000
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 269| 0 0 1 -6 6 10 -.34 11 11 | -544 -431 21 90
emr 80| 0 -5 0 -38 -28 32 .24 18 18 | 5519 -236 14 100
esa 150| 2 0 0 9 -13 -5 .10 7 7 | -2419 1969 12 98
gfz 204| 0 0 -5 20 20 -8 -.39 12 12 | 186 -222 20 99
grg 139| 0 0 0 15 14 -25 .66 17 15 | 46 -203 23 158
igr n/a| 0 1 0 -9 57 -19 -.12 5 5 | 1908 -168 18 76
jpl 80| -2 0 0 -26 1 2 .38 16 15 | 5608 -242 17 96
mit 240| 0 -1 1 12 3 31 -.58 12 11 | -81 48 29 198
ngs 224| -1 1 0 -29 -8 -26 .34 12 11 | -502 -644 1663 3044
sio 282| -1 -1 -1 -36 -115 184 -.24 19 21 | --- --- --- ---
Table 2.1730.5 GPS week: 1730 Day: 5 MJD: 56359.000
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 269| -1 0 1 -11 0 3 -.41 12 12 | -1532 517 23 92
emr 80| -1 -2 -1 -49 -18 -1 .27 17 17 | 5864 -1445 15 105
esa 150| 2 0 0 -5 -10 -7 .05 6 6 | -51 -61 10 100
gfz 203| 0 -1 -4 19 -62 -9 -.41 12 11 | 164 -572 21 119
grg 137| 0 0 0 -9 -1 -13 .64 15 14 | 302 -1177 17 146
igr n/a| 0 0 1 -19 63 -30 -.14 5 5 | 2135 -1578 19 71
jpl 80| -3 -1 0 -42 -6 -2 .37 15 15 | 5772 -1658 17 103
mit 240| 0 0 1 16 -12 24 -.63 13 12 | -13 -746 30 197
ngs 238| 0 1 1 48 115 32 .30 11 10 | -1262 -78 1612 3392
sio 283| 0 -1 -2 -15 -177 92 -.32 20 20 | --- --- --- ---
Table 2.1730.6 GPS week: 1730 Day: 6 MJD: 56360.000
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 270| 0 0 1 3 -23 10 -.39 11 10 | -561 -878 24 96
emr 80| -1 -3 2 -47 -19 3 .29 18 18 | 5566 895 13 89
esa 150| 1 0 1 9 -1 -14 .06 7 7 | -955 -846 9 105
gfz 202| 0 1 -4 31 -90 -18 -.33 12 12 | 437 -42 19 116
grg 134| 1 -1 -1 -19 -16 -9 .69 18 16 | -242 399 20 155
igr n/a| 0 0 0 -12 64 -23 -.13 4 4 | 1717 976 17 83
jpl 80| -2 0 0 16 -6 -3 .40 17 17 | 5119 871 16 110
mit 239| 1 0 1 -5 -2 23 -.59 13 10 | -276 403 26 196
ngs 241| 0 0 0 -7 114 18 .38 11 9 | -613 -853 1916 3740
sio 268| 0 -2 -2 -85 -75 227 -.25 20 18 | --- --- --- ---
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 3.1730.0 GPS week: 1730 Day: 0 MJD: 56354.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 27 8 12 12 5 14 21 12 15 5 | 67 61 70 64 73 67 74 68 75 65 68
2E | 8 19 7 11 15 3 18 11 9 10 4 | 37 36 37 35 35 34 37 39 32 33 34
3 | 12 12 4 10 15 3 9 14 15 14 4 | 23 21 18 15 24 15 22 23 19 20 17
4E | 19 27 40 25 111 12 25 26 17 17 11 | 110 120 125 113 182 111 122 118 116 111 116
5 | 10 17 6 14 16 6 18 9 8 21 4 | 30 32 30 27 32 25 33 29 29 29 27
6 | 6 12 4 9 14 2 12 10 12 13 3 | 18 21 22 18 26 18 23 23 20 22 19
7E | 9 18 6 10 14 4 16 7 12 12 4 | 17 22 18 14 26 15 23 16 25 13 16
8E | 18 27 9 19 23 7 20 21 21 24 7 | 32 40 31 36 36 30 35 36 36 37 30
9E | 13 20 9 14 17 5 20 20 13 16 5 | 30 37 31 30 32 26 37 27 30 26 28
10 | 11 16 5 13 17 4 13 9 7 14 4 | 24 19 26 32 34 25 20 24 25 25 23
11E | 9 13 6 10 17 4 10 13 11 18 4 | 22 29 24 22 33 23 29 25 32 24 23
12 | 12 16 7 12 17 4 18 14 11 20 4 | 26 29 25 21 36 21 28 26 25 19 23
13 | 9 16 6 10 17 4 16 9 15 19 4 | 18 20 17 11 20 13 19 14 16 15 16
14 | 6 17 5 14 16 5 13 8 14 20 4 | 26 28 30 36 38 27 29 28 32 28 28
15 | 19 19 5 12 18 6 18 13 9 22 5 | 31 32 29 33 42 27 31 26 27 27 27
16 | 7 20 7 12 14 4 22 7 9 22 4 | 18 27 23 21 30 18 28 19 21 20 19
17 | 8 18 11 16 16 7 20 19 12 29 5 | 17 25 22 25 23 18 25 16 22 30 16
18 | 13 21 6 15 17 4 20 10 12 27 5 | 26 32 25 23 28 20 33 20 23 23 22
19 | 10 16 5 9 13 5 16 12 12 23 4 | 16 23 12 13 19 9 23 15 19 19 11
20 | 11 17 8 10 9 6 18 10 13 26 4 | 22 30 22 21 30 21 31 22 28 20 21
21E | 6 14 8 11 11 4 15 6 10 11 3 | 23 26 27 24 25 21 26 24 26 20 23
22 | 6 18 6 11 16 3 17 15 11 23 4 | 22 26 24 25 30 21 25 23 21 23 20
23 | 10 16 6 11 13 4 15 9 13 23 4 | 24 31 27 28 35 24 31 23 29 20 25
24E | 11 19 8 12 14 5 12 24 9 14 5 | 23 24 24 22 32 21 27 19 23 19 20
25 | 9 15 5 10 16 3 14 11 8 13 4 | 18 25 23 16 36 20 33 21 23 16 20
26 | 6 9 5 11 15 4 10 12 9 14 3 | 22 19 22 23 29 18 19 22 18 17 19
X27 | 6 --- --- --- --- 74 --- --- --- --- 0 | 41 --- --- --- --- 30 --- --- --- --- 42
28 | 11 20 6 11 16 5 18 11 11 20 4 | 28 36 36 35 39 31 35 34 32 31 30
29 | 17 18 6 10 15 4 19 9 9 24 4 | 28 27 25 22 26 22 27 24 23 22 21
30 | 8 13 6 7 16 4 12 15 10 13 4 | 17 22 20 17 22 16 24 19 23 22 16
31E | 10 17 6 7 13 6 18 15 6 13 4 | 19 22 22 21 26 19 24 20 25 19 19
32 | 10 11 4 9 12 4 9 6 10 20 3 | 21 22 23 23 31 21 27 24 29 22 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 10 12 25 5 16 14 12 19 |T 28 31 29 27 36 25 32 27 29 27 26
WRMS | 11 18 7 11 14 5 16 11 9 16 |NE 23 26 23 23 30 20 26 22 24 22 22
MEDI | 10 17 6 11 16 4 16 11 11 19 |MD 23 27 24 23 31 21 28 23 25 22 22
Table 3.1730.1 GPS week: 1730 Day: 1 MJD: 56355.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 26 6 9 11 4 13 17 11 17 4 | 49 50 54 47 54 51 55 58 58 58 52
2E | 9 16 5 10 18 4 19 19 10 12 4 | 27 28 24 30 27 26 29 28 23 27 25
3 | 10 12 5 9 16 3 11 12 9 15 3 | 17 18 14 12 19 12 18 18 18 18 12
4E | 22 22 7 13 20 5 17 16 15 14 6 | 106 113 112 105 102 108 114 108 108 111 109
5 | 13 19 6 13 15 4 17 11 10 17 4 | 25 29 27 29 33 23 30 26 25 27 25
6 | 6 12 4 9 16 4 12 12 14 14 3 | 13 20 14 16 21 14 20 19 23 19 14
7E | 10 14 8 9 14 5 14 7 8 10 3 | 21 26 19 15 35 17 26 19 26 21 19
8E | 19 22 11 11 20 6 22 38 23 32 7 | 27 32 26 20 30 22 32 40 32 37 23
9E | 13 22 7 11 18 7 20 22 12 13 5 | 30 34 29 28 28 26 34 37 26 29 26
10 | 11 13 3 10 16 3 11 9 8 13 3 | 22 19 22 22 28 21 19 20 20 26 20
11E | 7 9 4 7 13 4 9 15 8 17 3 | 18 24 23 17 29 20 26 22 24 23 19
12 | 12 17 8 8 18 4 17 22 10 21 5 | 23 27 23 18 34 19 27 22 26 17 21
13 | 8 19 4 9 16 4 15 12 11 20 4 | 17 25 18 12 19 15 24 21 20 18 19
14 | 8 16 5 12 16 4 13 10 12 20 4 | 20 25 23 24 31 21 26 20 20 21 21
15 | 22 21 7 11 17 5 19 19 15 23 6 | 31 31 29 27 39 26 33 32 25 27 27
16 | 6 22 6 11 16 3 21 9 13 22 4 | 13 24 16 14 26 12 26 16 19 15 13
17 | 11 16 6 16 18 4 20 10 13 28 5 | 24 26 20 22 27 18 28 19 27 23 19
18 | 11 19 6 16 17 4 17 10 8 22 4 | 22 25 21 25 27 17 26 15 18 17 19
19 | 12 19 5 12 15 3 19 11 10 22 4 | 16 25 15 16 21 13 25 16 15 18 13
20 | 8 20 6 12 12 3 19 12 11 26 4 | 22 31 23 22 31 21 33 24 25 23 22
21E | 7 16 3 8 16 5 13 6 10 13 3 | 22 25 22 24 30 21 24 20 26 20 22
22 | 6 17 5 10 17 5 15 12 9 23 4 | 17 23 19 18 28 17 23 17 17 19 16
23 | 7 17 4 9 15 3 15 8 9 23 3 | 25 30 25 24 35 24 32 27 23 24 24
24E | 6 20 9 8 16 4 14 28 14 15 5 | 22 24 24 19 32 20 28 32 23 23 21
25 | 13 16 5 8 17 5 14 17 6 14 4 | 17 23 21 14 33 18 33 19 20 16 19
26 | 10 10 5 9 15 4 11 12 9 15 3 | 19 14 18 17 26 13 16 22 15 14 15
X27 | 6 --- --- --- --- 55 --- --- --- --- 0 | 27 --- --- --- --- 20 --- --- --- --- 28
28 | 9 20 5 13 15 4 17 8 10 21 4 | 25 37 29 31 38 28 34 28 33 28 28
29 | 19 16 6 8 18 4 18 11 12 22 5 | 31 27 22 20 31 21 29 25 29 26 23
30 | 7 14 4 9 16 3 12 15 13 12 4 | 16 25 20 20 22 16 23 23 25 22 19
31E | 10 18 6 7 20 6 17 13 12 12 4 | 19 23 20 16 28 18 25 14 25 21 18
32 | 7 11 4 6 14 3 10 7 7 17 3 | 21 23 23 22 27 19 26 24 20 27 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 6 10 16 4 16 15 11 19 |T 25 29 25 24 31 23 30 26 26 26 24
WRMS | 11 18 6 9 16 4 15 12 9 17 |NE 21 25 21 20 28 18 26 21 22 21 19
MEDI | 10 17 5 9 16 4 15 12 10 17 |MD 22 25 22 20 29 20 26 22 24 23 21
Table 3.1730.2 GPS week: 1730 Day: 2 MJD: 56356.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 14 26 11 13 15 4 15 34 15 37 6 | 148 133 134 134 141 138 140 142 148 133 140
2E | 8 18 6 9 17 4 23 20 9 15 5 | 32 30 29 31 34 29 30 35 30 27 30
3 | 7 13 6 8 18 4 9 9 7 13 3 | 12 18 16 9 24 11 19 17 15 16 12
4E | 19 24 7 16 15 7 18 20 13 18 6 | 49 61 50 59 58 54 58 51 55 51 53
5 | 13 17 6 14 15 6 17 8 11 19 4 | 25 28 22 30 27 22 27 27 24 23 23
6 | 7 13 5 7 16 3 9 8 10 12 3 | 15 22 17 14 27 12 22 19 16 19 16
7E | 10 16 4 10 13 3 17 7 10 13 4 | 20 27 15 14 23 15 24 21 26 20 18
8E | 17 22 10 13 20 8 21 31 19 22 7 | 25 33 21 23 32 24 31 34 30 30 22
9E | 13 22 7 12 20 5 20 20 10 14 5 | 25 28 21 24 22 18 26 31 24 23 20
10 | 11 14 6 9 14 3 13 13 8 15 4 | 28 23 23 28 28 24 21 25 25 27 24
11E | 8 13 4 8 17 4 13 12 8 16 3 | 24 27 23 18 31 20 27 28 27 22 22
12 | 14 18 7 8 20 4 18 18 8 20 5 | 24 30 21 21 38 18 27 17 25 17 22
13 | 8 18 6 10 14 3 16 7 8 20 4 | 22 19 18 9 22 16 17 15 13 15 21
14 | 7 15 6 13 12 3 14 9 9 19 4 | 23 27 25 33 32 24 26 26 23 27 25
15 | 17 21 6 14 17 6 19 15 11 23 5 | 26 28 21 28 31 23 26 29 19 24 22
16 | 6 20 7 9 16 3 19 11 9 24 4 | 14 27 19 18 28 15 24 18 19 19 17
17 | 11 17 7 14 16 3 18 8 9 25 4 | 19 28 17 18 28 15 26 17 21 20 17
18 | 12 18 8 17 14 6 16 10 11 20 4 | 23 28 23 26 26 20 28 18 22 17 20
19 | 15 19 5 10 14 6 20 11 12 20 4 | 20 26 12 12 24 10 26 19 19 16 14
20 | 11 21 9 10 13 4 19 19 8 26 5 | 22 32 22 23 28 18 29 20 21 26 20
21E | 9 14 6 10 14 4 14 6 10 11 3 | 20 25 22 24 26 19 21 23 19 25 20
22 | 5 17 9 10 17 6 15 15 10 23 4 | 19 24 24 23 26 19 23 23 17 24 18
23 | 8 18 6 11 13 3 16 6 8 22 4 | 27 32 25 28 27 23 32 27 26 26 26
24E | 9 22 7 11 13 3 15 24 11 14 5 | 21 22 16 14 22 14 22 27 22 16 16
25 | 9 15 5 8 17 4 14 16 9 13 4 | 19 22 20 17 36 17 34 17 20 17 20
26 | 9 9 5 12 16 5 9 11 10 13 3 | 21 19 19 19 25 16 15 22 14 14 17
X27 | 6 --- --- --- --- 62 --- --- --- --- 0 | 58 --- --- --- --- 30 --- --- --- --- 59
28 | 9 22 5 13 18 3 18 10 11 20 4 | 22 37 28 29 41 26 33 29 35 31 29
29 | 10 17 6 10 19 3 20 13 10 20 4 | 21 28 18 20 31 18 29 20 22 22 21
30 | 7 12 5 5 16 4 13 9 6 12 3 | 28 33 28 27 31 26 33 30 33 31 29
31E | 9 19 6 7 16 5 19 19 13 12 4 | 18 24 18 18 24 17 23 22 26 22 17
32 | 9 13 5 8 12 4 12 12 8 19 3 | 22 27 25 26 25 23 26 26 25 34 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 7 11 16 5 17 15 10 19 |T 27 31 25 26 32 24 30 28 27 26 26
WRMS | 10 18 6 10 15 4 16 12 9 17 |NE 23 26 21 21 28 19 25 21 21 22 22
MEDI | 9 18 6 10 16 4 16 12 10 19 |MD 22 27 21 23 28 19 26 23 23 23 21
Table 3.1730.3 GPS week: 1730 Day: 3 MJD: 56357.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 26 7 13 26 6 20 16 15 21 5 | 74 84 80 80 77 77 77 80 79 85 78
2E | 10 18 4 9 19 4 24 9 9 19 4 | 23 24 19 21 25 20 27 24 17 19 20
3 | 13 15 6 9 17 3 13 7 11 13 4 | 20 21 17 15 25 14 17 15 17 16 16
4E | 16 28 9 12 14 5 30 15 14 16 6 | 122 125 122 120 125 123 134 120 122 121 123
5 | 9 19 5 16 13 5 21 16 12 22 5 | 32 35 33 33 35 30 38 37 28 34 31
6 | 8 15 6 12 13 3 12 8 13 13 3 | 17 22 19 23 26 17 20 19 20 18 19
7E | 10 18 7 8 12 4 19 6 14 12 4 | 21 26 18 18 28 20 30 18 28 24 20
8E | 14 22 10 13 18 5 21 22 17 18 6 | 21 28 17 19 27 16 31 29 25 26 18
9E | 13 23 8 10 16 7 21 20 9 14 5 | 24 32 21 26 27 22 30 31 21 27 22
10 | 6 15 5 9 14 3 15 7 6 13 3 | 24 21 26 28 30 23 20 24 23 27 23
11E | 6 12 6 10 17 4 13 11 10 20 3 | 28 38 32 33 39 32 38 31 34 34 31
12 | 12 17 6 9 22 4 20 14 15 19 5 | 26 31 23 22 37 22 30 22 26 23 23
X13 | 7 --- 3 --- --- 1038 --- --- --- --- 5 | 9999 --- 19 --- --- 91 --- --- --- --- 9999
14 | 8 18 7 12 16 6 15 9 16 22 4 | 25 29 28 30 33 27 31 28 32 27 28
15 | 19 21 6 12 16 7 23 15 12 24 5 | 33 38 33 35 41 32 39 34 31 36 32
16 | 7 23 6 11 17 3 20 8 10 24 4 | 21 26 22 23 33 19 26 19 22 20 21
17 | 10 18 7 13 14 3 21 10 7 25 4 | 18 26 13 18 27 15 25 16 18 20 15
18 | 12 22 7 14 16 6 20 10 17 21 5 | 23 32 21 23 27 19 29 19 26 17 20
19 | 12 19 6 8 13 5 18 9 11 20 4 | 17 27 17 17 21 16 25 18 20 19 16
20 | 10 23 7 11 15 7 22 20 10 27 5 | 25 32 29 26 32 23 30 29 23 22 24
21E | 8 16 4 9 13 5 14 10 12 17 3 | 27 27 26 25 29 23 30 30 23 28 25
22 | 9 21 6 13 17 6 19 14 19 23 5 | 19 26 19 25 30 19 25 22 17 22 17
23 | 6 20 5 13 12 3 21 11 8 23 4 | 27 33 28 33 34 28 33 28 28 26 28
24E | 11 21 6 9 15 2 14 18 11 14 4 | 21 25 19 19 30 18 27 23 19 25 19
25 | 11 16 4 7 17 3 16 12 10 13 4 | 16 21 20 14 33 16 31 20 19 18 17
26 | 9 13 4 11 14 6 12 10 8 14 3 | 18 22 17 18 25 18 19 22 18 19 18
X27 | 5 --- --- --- --- 51 --- --- --- --- 0 | 40 --- --- --- --- 25 --- --- --- --- 42
28 | 8 22 4 8 16 3 19 10 8 21 4 | 29 38 34 30 43 30 36 32 36 32 32
29 | 14 18 6 10 17 3 20 11 8 19 4 | 23 28 21 21 30 20 27 23 24 24 21
30 | 6 14 4 9 17 4 11 9 13 12 3 | 16 21 18 15 21 16 21 20 23 19 16
31E | 9 17 6 9 17 6 20 10 11 14 4 | 20 25 21 20 24 18 28 19 27 22 21
32 | 7 13 5 9 14 5 13 12 9 22 3 | 22 22 23 27 29 22 25 25 24 26 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 6 11 16 5 19 13 12 19 |T 28 32 27 28 34 28 33 29 29 29 27
WRMS | 10 19 6 10 16 4 18 11 9 20 |NE 23 27 22 23 30 24 27 23 23 23 22
MEDI | 9 18 6 10 16 5 19 10 11 19 |MD 23 27 21 23 30 20 29 23 23 24 21
Table 3.1730.4 GPS week: 1730 Day: 4 MJD: 56358.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 25 8 20 22 6 11 11 12 14 5 | 52 54 52 52 53 49 53 51 52 51 51
2E | 7 15 6 8 22 4 16 10 11 20 4 | 25 27 23 22 30 24 26 26 28 23 25
3 | 7 11 4 8 14 3 11 6 10 11 3 | 12 20 16 14 19 10 16 13 16 15 12
4E | 15 26 9 9 17 7 19 22 22 20 6 | 85 95 87 87 84 84 86 91 87 86 86
5 | 12 16 9 14 17 5 17 13 8 24 4 | 23 27 26 23 24 20 25 25 18 28 20
6 | 7 13 4 9 13 4 10 8 8 9 3 | 11 21 17 15 21 13 17 16 15 17 14
7E | 10 14 4 8 18 4 17 8 11 10 4 | 15 24 16 13 28 13 20 16 25 19 16
8E | 14 20 11 12 21 4 22 18 19 16 6 | 18 30 18 22 28 16 29 28 24 28 18
9E | 14 20 11 11 16 5 19 20 11 14 5 | 20 32 22 18 22 19 27 27 27 26 20
10 | 13 11 6 8 20 4 12 9 11 14 4 | 25 25 25 26 29 24 25 26 26 32 24
11E | 8 11 6 8 17 5 9 11 13 13 3 | 33 38 35 29 43 32 37 33 39 33 34
12 | 14 20 8 10 20 5 17 13 15 19 5 | 23 29 23 18 36 20 28 23 28 22 22
X13 | 5 --- --- --- --- 17 --- --- --- --- 0 | 91 --- --- --- --- 14 --- --- --- --- 93
14 | 10 15 6 12 15 5 15 11 14 22 4 | 22 29 26 28 30 25 30 28 30 27 26
15 | 20 20 7 17 15 5 17 13 11 23 5 | 26 32 26 29 33 24 28 25 25 28 24
16 | 6 22 8 13 13 4 20 7 14 24 4 | 12 24 16 18 26 13 22 16 16 16 13
17 | 10 20 7 16 14 5 15 12 12 24 4 | 14 27 12 16 26 11 23 17 21 19 14
18 | 14 17 6 15 15 5 17 10 9 25 4 | 22 29 21 23 28 19 29 20 22 21 21
19 | 19 17 7 8 14 4 19 10 12 19 5 | 20 28 17 12 21 14 26 14 20 18 15
20 | 9 23 8 12 14 6 19 20 9 26 5 | 22 30 22 19 29 19 25 28 28 24 21
21E | 8 12 5 11 14 4 13 15 11 14 4 | 16 18 20 20 20 14 20 22 21 16 16
22 | 8 18 6 10 17 5 16 12 12 23 4 | 19 25 21 20 28 18 23 24 19 27 19
23 | 8 19 7 10 13 5 16 11 12 24 4 | 21 28 24 21 31 22 26 23 27 23 22
24E | 9 21 8 11 16 5 14 19 10 15 5 | 18 27 20 19 33 20 25 21 24 25 19
25 | 10 15 5 7 16 5 14 11 10 13 4 | 20 25 21 16 34 20 33 20 24 21 21
26 | 13 14 8 18 16 5 12 10 7 19 4 | 17 20 16 21 21 14 18 20 19 22 16
X27 | 5 --- --- --- --- 132 --- --- --- --- 0 | 138 --- --- --- --- 25 --- --- --- --- 139
28 | 12 25 7 10 16 3 17 12 12 19 5 | 15 32 24 18 36 18 28 23 27 26 20
29 | 14 17 6 12 15 6 16 10 10 19 4 | 20 24 18 13 25 16 22 14 23 19 15
30 | 6 13 5 8 19 4 13 7 12 12 3 | 20 28 20 19 30 19 29 22 27 24 22
31E | 7 17 6 11 16 4 18 9 11 17 4 | 20 26 18 21 28 16 24 21 24 23 20
32 | 7 12 7 9 16 4 11 9 9 19 3 | 24 24 26 24 28 22 20 28 23 29 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 7 12 17 5 16 12 12 19 |T 28 29 24 23 30 21 28 25 26 26 28
WRMS | 11 18 7 12 15 5 15 11 11 21 |NE 28 26 20 19 27 18 24 21 22 22 28
MEDI | 10 17 7 10 16 5 16 11 11 19 |MD 20 27 21 20 28 19 25 23 24 23 20
Table 3.1730.5 GPS week: 1730 Day: 5 MJD: 56359.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 12 24 8 14 17 6 11 14 11 15 5 | 33 36 43 35 38 39 40 40 43 37 37
2E | 7 15 7 12 18 3 17 9 9 17 4 | 19 20 15 20 21 17 20 20 17 16 17
3 | 14 10 3 10 15 4 9 7 9 12 3 | 16 20 20 10 20 14 17 12 21 14 13
4E | 11 21 10 10 12 5 14 13 20 16 5 | 106 105 107 107 105 105 106 106 107 103 105
5 | 10 15 6 13 14 4 15 12 12 26 4 | 24 23 23 26 20 20 24 25 22 27 20
6 | 5 10 3 11 14 4 8 7 10 11 3 | 14 21 20 15 23 15 18 17 21 17 16
7E | 10 16 5 9 12 5 18 9 10 12 4 | 17 25 18 17 26 15 25 18 25 21 17
8E | 18 19 10 15 17 7 19 17 17 18 6 | 16 28 23 21 29 17 28 28 30 30 18
9E | 15 19 9 12 18 7 22 18 10 15 5 | 24 28 21 24 27 19 30 26 24 21 20
10 | 14 11 5 8 14 4 11 13 10 16 4 | 22 22 20 20 23 17 21 19 22 24 19
11E | 10 12 9 13 18 5 11 11 11 12 4 | 46 50 48 46 51 46 50 46 51 45 46
12 | 14 18 6 11 20 5 17 11 11 19 4 | 22 28 24 22 36 20 28 22 25 21 22
13 | 7 17 6 10 14 4 17 15 8 --- 4 | 48 17 10 10 10 8 15 16 10 --- 45
14 | 13 15 5 16 14 6 14 11 9 22 4 | 19 26 22 29 28 19 25 23 24 24 22
15 | 24 18 5 11 16 5 18 10 10 24 5 | 28 29 27 24 30 23 28 27 26 27 23
16 | 9 18 6 13 12 2 20 10 10 26 4 | 16 24 21 19 28 17 22 13 25 17 17
17 | 11 17 7 17 14 4 17 13 9 23 4 | 14 27 17 19 27 13 24 14 21 17 14
18 | 13 19 7 16 14 5 18 12 14 30 5 | 18 28 20 20 26 18 27 17 22 22 18
19 | 11 17 6 10 14 4 18 9 8 20 4 | 16 24 17 12 20 11 21 14 16 17 13
20 | 10 18 8 14 15 5 20 29 15 24 6 | 20 26 22 19 30 15 27 29 20 17 18
21E | 12 12 3 10 13 4 14 7 9 20 3 | 21 22 25 23 22 22 19 21 21 30 19
22 | 6 18 6 15 14 5 16 15 10 25 4 | 14 23 16 18 24 14 21 18 18 25 13
23 | 9 16 7 13 10 4 15 15 10 26 4 | 21 27 24 21 28 19 27 24 23 21 20
24E | 10 20 8 11 16 3 12 16 10 19 4 | 12 21 16 14 25 13 22 23 19 26 14
25 | 16 18 3 12 12 5 14 12 9 14 4 | 17 24 20 14 30 18 32 21 22 20 19
26 | 11 10 6 9 14 5 8 12 9 22 3 | 14 19 18 14 20 12 18 16 19 19 13
X27 | 6 --- --- --- --- 67 --- --- --- --- 0 | 44 --- --- --- --- 31 --- --- --- --- 46
28 | 13 22 6 11 15 5 18 10 10 21 4 | 20 36 27 25 40 24 33 28 33 34 27
29 | 20 17 5 9 14 6 16 11 10 17 4 | 23 26 19 16 27 16 24 17 22 19 17
30 | 9 12 6 8 15 2 12 10 8 --- 3 | 14 25 20 20 20 17 25 19 25 --- 18
31E | 7 18 7 11 11 6 17 11 13 19 4 | 14 24 18 17 24 15 19 14 20 21 14
32 | 8 10 5 11 12 3 11 11 10 19 3 | 20 21 21 21 21 14 19 18 15 25 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 6 12 15 5 15 13 11 20 |T 24 28 24 23 29 21 27 24 26 26 23
WRMS | 12 17 6 11 14 5 15 12 10 20 |NE 21 24 20 18 25 17 23 19 21 21 20
MEDI | 11 17 6 11 14 5 16 11 10 19 |MD 19 25 20 20 26 17 24 20 22 21 18
Table 3.1730.6 GPS week: 1730 Day: 6 MJD: 56360.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 22 8 13 15 5 15 8 13 12 4 | 40 44 50 44 55 46 50 43 55 48 46
2E | 7 17 7 12 17 3 20 10 9 15 4 | 25 22 20 27 27 21 24 27 21 20 22
3 | 7 11 4 11 15 2 9 7 13 14 3 | 10 17 15 15 21 12 15 13 20 16 10
4E | 14 26 8 11 11 5 17 11 21 23 5 | 106 112 111 108 108 110 108 108 114 104 109
5 | 10 17 8 16 15 3 23 12 9 26 5 | 25 25 24 29 25 21 29 25 19 29 21
6 | 6 12 4 10 15 3 8 8 8 14 3 | 18 23 19 27 28 19 23 22 19 19 20
7E | 11 16 6 10 17 6 17 11 12 10 4 | 19 19 17 15 29 14 22 15 24 15 15
8E | 19 20 11 14 21 6 24 15 22 22 6 | 17 28 21 25 22 16 30 30 29 32 17
9E | 12 23 10 12 17 4 22 22 11 16 5 | 21 28 18 23 21 16 26 30 22 21 17
10 | 8 13 5 8 15 3 14 9 7 14 3 | 24 25 31 28 33 24 24 25 31 29 26
11 | 9 11 7 10 25 5 9 12 11 13 4 | 25 34 29 24 45 27 30 27 34 30 27
12 | 15 18 7 11 18 5 22 12 10 19 5 | 29 29 22 24 37 19 29 24 28 21 23
13 | 7 17 6 13 16 4 15 16 11 20 4 | 42 15 8 11 9 8 15 17 11 6 40
14 | 7 20 6 15 18 4 14 16 10 22 4 | 25 33 31 41 40 29 35 33 31 32 30
15 | 17 20 6 13 12 5 24 11 9 23 5 | 34 32 29 36 37 28 29 29 25 29 28
16 | 7 20 7 13 15 4 20 8 11 26 4 | 16 24 19 24 31 17 24 16 19 17 16
17 | 10 22 6 17 12 4 20 13 12 23 5 | 16 30 17 24 29 14 28 15 24 18 16
18 | 11 17 7 16 17 5 17 13 11 31 5 | 23 30 20 25 30 19 30 21 24 26 20
19 | 12 16 7 12 16 5 16 8 12 22 4 | 16 28 17 18 20 12 26 15 21 22 14
20 | 7 18 6 13 14 3 16 15 8 28 4 | 20 31 25 25 32 21 28 26 23 29 22
21E | 9 12 4 12 43 5 14 16 9 20 5 | 24 26 21 28 37 22 28 30 26 27 21
22 | 6 17 5 12 18 4 15 16 8 24 4 | 21 26 20 26 32 20 26 25 20 27 19
23 | 9 16 7 15 13 4 15 10 12 24 4 | 26 31 27 34 34 27 32 28 27 29 28
24E | 7 23 8 14 15 6 14 18 11 17 5 | 14 22 16 19 25 14 24 26 20 26 15
25 | 14 17 5 11 14 4 16 14 7 13 4 | 18 23 21 19 35 18 32 23 21 19 19
26 | 8 11 6 10 13 7 15 20 9 19 4 | 19 23 22 24 27 17 17 21 17 22 18
X27 | 6 --- --- --- --- 116 --- --- --- --- 0 | 75 --- --- --- --- 27 --- --- --- --- 74
28 | 13 21 7 11 18 4 20 12 10 22 5 | 17 38 29 31 42 25 32 31 31 33 27
29 | 14 16 6 11 16 5 23 14 8 18 4 | 19 27 18 23 30 16 30 21 24 21 19
30 | 8 14 5 9 18 4 12 8 8 12 3 | 15 20 18 18 20 16 21 21 22 20 15
31E | 10 21 5 12 15 5 19 8 12 16 4 | 15 26 15 20 28 10 20 17 20 21 14
32 | 9 10 4 13 12 3 9 8 8 17 3 | 20 24 23 28 29 21 23 24 24 26 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 7 12 18 4 17 13 11 20 |T 26 29 24 27 32 22 29 26 27 26 25
WRMS | 10 18 7 12 16 4 17 10 9 18 |NE 24 26 21 25 29 19 26 22 22 23 23
MEDI | 9 17 6 12 15 4 16 12 10 19 |MD 20 26 21 25 30 19 28 25 24 26 20
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 4.1730 GPS week: 1730 MJD: 56354.0-56360.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3016 |U 5 5 15 |U 8 9 28 |U 6 6 16 |
emr | emr 2936 | 7 7 19 |U 9 9 30 | 10 10 19 |
esa | esa 2948 | 5 4 13 |U 8 9 29 | 6 6 17 |
gfz | gfz 2936 |U 5 4 13 |U 8 9 30 |U 8 7 21 |
grg | grg 2948 |U 7 6 17 |U 9 10 32 | 10 9 23 |
igr | igr 2953 | 5 5 13 | 7 8 28 | 6 6 16 |
igs | igs 2933 | 5 5 13 | 8 8 28 | 8 8 18 |
jpl | jpl 2935 | 6 7 18 |U 7 10 31 | 10 10 20 |
mit | mit 2948 | 6 5 13 |U 8 9 31 |U 11 11 23 |
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 5.1730.0 GPS week: 1730 Day: 0 MJD: 56354.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3019 | 3 3 11 | 6 7 28 | 7 6 17 |
emr | emr 2964 | 8 8 17 | 8 7 30 | 11 13 26 |
esa | esa 2976 | 4 4 13 | 8 8 35 | 8 8 19 |
gfz | gfz 2965 | 5 4 12 | 8 9 35 | 7 8 21 |
grg | grg 2976 | 7 7 21 | 10 8 35 | 10 9 31 |
igr | igr 2961 | 4 4 11 | 7 8 34 | 9 7 18 |
igs | igs 2935 | 5 5 14 | 7 7 32 | 10 9 20 |
jpl | jpl 2964 | 6 6 16 | 7 6 34 | 11 12 24 |
mit | mit 2976 | 4 5 12 | 8 8 35 | 12 12 26 |
Table 5.1730.1 GPS week: 1730 Day: 1 MJD: 56355.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 | 4 3 10 | 8 8 21 | 6 6 15 |
emr | emr 2964 | 8 5 17 | 10 9 26 | 11 12 20 |
esa | esa 2976 | 5 5 15 | 8 8 21 | 6 6 18 |
gfz | gfz 2965 | 4 4 13 | 8 9 23 | 9 5 20 |
grg | grg 2976 | 7 7 12 | 10 9 32 | 9 10 24 |
igr | igr 2961 | 5 5 16 | 8 8 23 | 5 4 17 |
igs | igs 2927 | 5 4 13 | 8 8 23 | 6 8 21 |
jpl | jpl 2962 | 6 8 19 | 8 10 28 | 11 14 22 |
mit | mit 2976 | 9 4 11 | 8 9 25 | 12 12 24 |
Table 5.1730.2 GPS week: 1730 Day: 2 MJD: 56356.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 5 4 14 | 7 7 28 | 5 3 15 |
emr | emr 2964 | 7 6 17 | 8 6 31 | 14 12 19 |
esa | esa 2976 | 4 3 13 | 7 7 27 | 5 4 17 |
gfz | gfz 2963 | 4 3 13 | 7 8 30 | 6 5 18 |
grg | grg 2976 | 8 7 15 | 8 12 28 | 10 10 27 |
igr | igr 2973 | 5 5 14 | 7 7 24 | 5 4 17 |
igs | igs 2946 | 4 3 11 | 7 8 27 | 6 6 15 |
jpl | jpl 2964 | 6 5 18 | 7 7 31 | 13 12 22 |
mit | mit 2976 | 6 8 14 | 7 8 29 | 10 9 21 |
Table 5.1730.3 GPS week: 1730 Day: 3 MJD: 56357.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2944 | 7 8 20 | 9 11 34 | 7 6 21 |
emr | emr 2868 | 8 7 21 | 8 11 34 | 10 8 16 |
esa | esa 2880 | 5 4 15 | 8 10 35 | 6 4 18 |
gfz | gfz 2867 | 5 4 13 | 6 7 31 | 9 7 21 |
grg | grg 2880 | 6 6 20 | 8 10 42 | 11 11 17 |
igr | igr 2950 | 5 5 14 | 6 8 30 | 6 4 16 |
igs | igs 2958 | 6 5 17 | 6 6 30 | 7 4 19 |
jpl | jpl 2866 | 7 7 21 | 6 11 33 | 9 7 16 |
mit | mit 2880 | 8 6 18 | 7 8 35 | 11 9 26 |
Table 5.1730.4 GPS week: 1730 Day: 4 MJD: 56358.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 | 5 4 13 | 5 7 23 | 6 5 14 |
emr | emr 2868 | 6 7 18 | 8 9 27 | 8 8 15 |
esa | esa 2880 | 4 4 12 | 6 7 24 | 6 5 16 |
gfz | gfz 2869 | 5 4 13 | 6 7 25 | 9 6 27 |
grg | grg 2880 | 5 6 18 | 8 9 26 | 9 7 19 |
igr | igr 2877 | 5 4 12 | 5 7 24 | 6 4 14 |
igs | igs 2870 | 5 5 12 | 6 7 24 | 8 7 14 |
jpl | jpl 2867 | 5 5 14 | 6 11 26 | 11 10 18 |
mit | mit 2880 | 6 4 13 | 6 9 31 | 10 10 17 |
Table 5.1730.5 GPS week: 1730 Day: 5 MJD: 56359.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 5 6 20 | 8 9 33 | 5 5 13 |
emr | emr 2964 | 6 8 21 | 9 10 31 | 9 8 19 |
esa | esa 2976 | 5 5 13 | 8 7 31 | 5 6 15 |
gfz | gfz 2962 | 6 5 15 | 9 8 33 | 6 7 21 |
grg | grg 2976 | 7 7 16 | 9 8 32 | 10 8 20 |
igr | igr 2975 | 5 5 13 | 7 8 31 | 6 5 15 |
igs | igs 2934 | 5 5 15 | 8 8 31 | 7 7 20 |
jpl | jpl 2963 | 7 8 21 | 8 11 34 | 8 8 21 |
mit | mit 2976 | 5 5 15 | 8 10 31 | 8 9 23 |
Table 5.1730.6 GPS week: 1730 Day: 6 MJD: 56360.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3018 | 8 8 20 | 11 15 29 | 7 13 19 |
emr | emr 2964 | 8 7 21 | 10 14 34 | 9 10 17 |
esa | esa 2976 | 7 4 12 | 10 12 30 | 8 12 17 |
gfz | gfz 2964 | 7 5 13 | 11 13 31 | 9 12 19 |
grg | grg 2976 | 7 6 15 | 10 13 32 | 11 12 26 |
igr | igr 2974 | 7 5 12 | 10 12 30 | 7 12 18 |
igs | igs 2966 | 6 5 13 | 10 13 29 | 9 12 18 |
jpl | jpl 2964 | 8 7 18 | 10 12 33 | 8 9 15 |
mit | mit 2976 | 6 4 11 | 11 12 32 | 11 17 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 6.1730 GPS week: 1730 MJD: 56354.500-56360.500
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 | -16 19 -17 -104 6 | 10 17
| 13 19 66 75 4 | 4
emr uuuuu | 10 57 -157 -5 10 | 40 44
| 8 30 81 48 11 | 7
esa uuuuu | -2 -13 9 -41 0 | 17 22
| 14 12 50 38 5 | 3
gfz uuuuu | 14 -17 75 -3 -3 | 10 15
| 25 9 36 80 2 | 1
grg uuuux | 7 -5 38 93 16 | -2 27
| 25 14 66 54 23 | 7
igr xxxxx | -44 -11 35 44 0 | -1 11
| 12 20 45 56 5 | 1
irf xxxxx | 11 -11 -25 20 -7 | 7 16
| 7 7 19 33 2 | 1
jpl uuuuu | -5 -5 140 56 -2 | 45 47
| 16 29 61 41 10 | 1
mit uuuuu | 46 -23 -161 100 -3 | 17 23
| 24 22 55 107 5 | 3
ngs uuuuu | -44 17 53 12 -2 | 8 14
| 53 43 89 125 6 | 1
sio xxxxx | 101 26 -522 -42 11 | 76 77
| 62 28 63 55 7 | 6
Table 7.1730.0 GPS week: 1730 Day: 0 MJD: 56354.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 5 45 -61 -146 6 | 5 16
emr uuuuu | 11 27 -174 28 15 | 29 37
esa uuuuu | -24 10 53 -109 0 | 14 21
gfz uuuuu | 4 -18 85 43 -7 | 11 17
grg uuuux | 15 -17 30 168 -2 | 10 41
igr xxxxx | -37 -5 10 31 -9 | 1 12
irf xxxxx | 13 -12 -6 50 -9 | 7 17
jpl uuuuu | -1 -43 173 26 -8 | 47 49
mit uuuuu | 48 -32 -114 250 -1 | 14 22
ngs uuuuu | -24 -1 -32 -42 -1 | 9 16
sio xxxxx | 101 -2 -501 58 17 | 68 70
Table 7.1730.1 GPS week: 1730 Day: 1 MJD: 56355.500
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 | -29 4 -76 -185 12 | 5 16
emr uuuuu | 5 31 -138 -10 18 | 31 39
esa uuuuu | -14 -15 30 -24 3 | 13 21
gfz uuuuu | 24 -22 79 75 -4 | 8 15
grg uuuux | -20 -20 6 119 5 | 6 38
igr xxxxx | -55 -8 -10 3 -4 | -1 12
irf xxxxx | 0 -20 -35 37 -4 | 6 17
jpl uuuuu | -7 -6 106 -3 -14 | 44 47
mit uuuuu | 1 -21 -107 128 4 | 13 22
ngs uuuuu | 44 64 22 5 -12 | 8 16
sio xxxxx | 75 23 -492 -38 19 | 69 71
Table 7.1730.2 GPS week: 1730 Day: 2 MJD: 56356.500
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 | -17 -4 84 -159 8 | 9 17
emr uuuuu | 16 28 -75 -38 22 | 38 42
esa uuuuu | 6 -19 65 -16 2 | 16 22
gfz uuuuu | 45 -7 23 56 -2 | 9 15
grg uuuux | 6 14 -64 139 -18 | 1 32
igr xxxxx | -51 15 28 -2 -1 | -1 11
irf xxxxx | 14 -15 -63 40 -6 | 7 16
jpl uuuuu | -27 31 112 100 -3 | 43 46
mit uuuuu | 47 -47 -246 133 1 | 16 23
ngs uuuuu | -62 41 -22 -73 -8 | 9 15
sio xxxxx | -10 66 -619 -38 15 | 73 75
Table 7.1730.3 GPS week: 1730 Day: 3 MJD: 56357.500
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 -6 -14 8 | 12 19
emr uuuuu | -3 90 -120 -87 -4 | 44 47
esa uuuuu | 16 -28 41 -23 6 | 18 23
gfz uuuuu | 45 -32 66 -17 -2 | 11 16
grg uuuux | -15 -9 123 52 13 | -8 19
igr xxxxx | -21 -48 63 -16 5 | 0 12
irf xxxxx | 20 -16 -8 55 -7 | 9 17
jpl uuuuu | 26 2 83 74 -11 | 44 46
mit uuuuu | 79 -47 -181 199 -3 | 19 24
ngs uuuuu | -132 66 -19 -132 -4 | 10 15
sio xxxxx | 93 2 -594 -18 14 | 77 79
Table 7.1730.4 GPS week: 1730 Day: 4 MJD: 56358.500
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 | -27 40 -100 12 8 | 13 19
emr uuuuu | 13 51 -72 57 11 | 45 48
esa uuuuu | -5 -18 -65 -82 0 | 20 24
gfz uuuuu | 12 -15 142 35 -4 | 11 16
grg uuuux | -9 -17 122 99 45 | -9 19
igr xxxxx | -54 -20 123 60 1 | 0 11
irf xxxxx | 2 -8 -26 -4 -6 | 8 17
jpl uuuuu | -3 -12 255 97 9 | 44 46
mit uuuuu | 47 -10 -205 -19 -6 | 20 24
ngs uuuuu | -26 11 98 -28 -1 | 9 16
sio xxxxx | 134 13 -514 -53 9 | 79 81
Table 7.1730.5 GPS week: 1730 Day: 5 MJD: 56359.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -19 23 40 -106 3 | 12 18
emr uuuuu | 5 78 -230 -12 -6 | 45 48
esa uuuuu | 11 -7 -34 -16 -6 | 18 22
gfz uuuuu | -18 -4 78 -66 -3 | 8 14
grg uuuux | 23 10 33 14 28 | -7 21
igr xxxxx | -42 -1 18 109 3 | -2 10
irf xxxxx | 16 -11 -20 -17 -4 | 6 15
jpl uuuuu | -16 29 156 21 2 | 44 46
mit uuuuu | 61 -20 -171 43 -5 | 18 23
ngs uuuuu | -52 -54 128 120 4 | 6 12
sio xxxxx | 194 14 -499 -96 9 | 80 81
Table 7.1730.6 GPS week: 1730 Day: 6 MJD: 56360.500
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 | 0 3 -2 -131 -2 | 15 17
emr uuuuu | 23 96 -290 25 14 | 47 49
esa uuuuu | -5 -15 -23 -17 -8 | 20 22
gfz uuuuu | -11 -17 54 -148 -1 | 9 14
grg uuuux | 51 3 14 58 41 | -4 21
igr xxxxx | -50 -6 11 125 7 | -1 8
irf xxxxx | 11 3 -19 -23 -10 | 7 15
jpl uuuuu | -7 -36 93 77 12 | 45 47
mit uuuuu | 41 16 -102 -31 -13 | 19 23
ngs uuuuu | -54 -8 198 235 5 | 7 11
sio xxxxx | 122 66 -435 -108 -3 | 84 84
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