[IGSREPORT-21424] Wk 1713 IGS Final Orbits [Resubmission]
IGS ACC
igs.acc at noaa.gov
Mon Dec 17 08:10:21 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1713 (Nov 04, 2012 - Nov 10, 2012)
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:
igs1713[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1713[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1713[0-6].cls IGS GPS clock combination summary report.
igs17137.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17137.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.
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 10 32 KOUC FLRS KOUC
0 | EMR | 30 30
0 | ESA | 32 10 32
0 | GFZ | 10 ALGO ASPA DGAR GUAT KIRU PIMO SANT STJO YAKT ZIMM
0 | GRG | 13 30 13 30 MCM4 SOFI ZECK ADIS KIT3 LHAZ MCM4 SOFI
0 | GRG | ZECK
0 | JPL | 10 30 32
0 | MIT | 30 30
1 | COD | 10 10 FLRS GUAT MCM4
1 | EMR | 30 32 32
1 | ESA | 10 32 10 32 BAN2
1 | GFZ | 10 30 32 ASPA LHAZ
1 | GRG | 30 MCM4 NICO ADIS KARR MCM4 THTI
1 | JPL | 10 30 32
1 | MIT | 3 6 13 18 21 26 30 32 3 6 11 13 18 21 26 30 32 GMAS
1 | MIT | MDVJ
2 | ALL | 13
2 | COD | 10 19 30 10 19 30 KOUC MCM4 NICO KOUC MCM4 NRMD
2 | EMR | 32 METS METS
2 | ESA | 10 30 10 30 MATE BAN2 NICO TLSE
2 | GFZ | 10 30 32 LHAZ PIMO SYOG
2 | GRG | 21 13 21 NICO
2 | JPL | 6
2 | MIT | 8 32 8 TLSE
3 | COD | 10 30 10 30 KOUC KOUC XMIS
3 | EMR | HERS HERS
3 | ESA | 10 30 10 30 NKLG WIND
3 | GFZ | 10 30 32 COCO GUUG NTUS YAKT
3 | GRG | 32 32 KOUC SPT0 ASPA KOUC SPT0
3 | JPL | 8 10 CHAN
3 | MIT | MAC1
4 | COD | 10 30 32 10 30 HERT KOUC SOFI HERT KOUC
4 | EMR | 32 32
4 | ESA | 10 30 32 10 30 MATE MATE NICO
4 | GFZ | 10 30 32 ADIS MATE NKLG YAKT
4 | GRG | MCM4 NICO NYAL WROC WSRT ASPA GUAT KIT3 MCM4 NYAL
4 | GRG | POTS RAMO SOFI WROC WSRT
4 | JPL | 32 RAMO
4 | MIT | 10 23 10 23 NICO SOFI NICO SOFI
5 | COD | 10 30 32 10 30 32 KOUC FLRS KOUC MCM4
5 | EMR | 32 32
5 | ESA | 10 30 32 10 30 32 TLSE TLSE
5 | GFZ | 10 30 32 OHI2 TLSE WILL YAKT
5 | GRG | IRKT WROC IRKT USNO WROC
5 | JPL | 17 32
6 | COD | 10 30 10 30 XMIS FLRS XMIS
6 | EMR | 32 32
6 | ESA | 10 30 10 30
6 | GFZ | 10 30 32 BOGT IRKT OHI2 YAKT
6 | GRG | 12 32 12
6 | JPL | 10 32
6 | MIT | 10 24 32 10 24
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
2 | SIO | ALL (high Transformation - See Table 2)
4 | SIO | ALL (high Transformation - See Table 2)
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G24 | | | 4 | 4 | | | |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .7 .4 .5 -62 -3 4 -.09
EMR | 0 | 9.6 6.3 -5.9 9 24 3 .22
ESA | 0 | 3.6 5.3 -20.1 122 -267 111 -.02
GFZ | 0 | .6 -.3 .7 -36 -44 -9 -.11
GRG | 0 | -1.7 .2 -5.7 -24 54 -32 .27
JPL | 0 | 5.2 6.7 5.9 -74 -25 36 -.01
MIT | 0 | 2.0 8.1 -4.9 -7 2 -24 .20
NGS | 0 | 5.6 5.3 -7.5 51 -18 59 .15
SIO | 0 | -.2 1.8 -42.6 77 -203 -5 .08
COD | 1 | .0 .2 .1 -42 -6 -12 -.32
EMR | 1 | 3.1 5.1 -5.6 16 30 1 -.04
ESA | 1 | 5.4 6.6 -20.7 189 -292 123 -.16
GFZ | 1 | .1 .2 1.1 -49 -38 -21 -.36
GRG | 1 | 3.4 -2.2 -5.2 -8 41 -27 .11
JPL | 1 | 7.0 -3.1 3.1 -49 38 13 .04
MIT | 1 | 4.0 7.2 -1.9 -3 -5 -23 -.11
NGS | 1 | 6.3 2.7 -14.4 87 -25 67 .05
SIO | 1 | 3.3 2.2 -45.5 141 -332 67 -.18
COD | 2 | -.1 .9 -1.0 -44 -7 -22 -.23
EMR | 2 | 10.3 .0 -4.5 10 33 -1 -.02
ESA | 2 | 5.9 4.8 -17.2 138 -305 106 -.03
GFZ | 2 | -.6 1.2 .2 -34 -26 -27 -.26
GRG | 2 | 3.2 -3.0 -6.5 -13 46 -31 .14
JPL | 2 | 7.3 -1.8 1.6 -43 -2 0 .09
MIT | 2 | 6.1 5.8 -2.4 -6 0 -24 -.06
NGS | 2 | 15.2 -3.7 -5.0 18 -50 110 .12
SIO | 2 | 7.2 .7 -56.4 157 -427 70 .04
COD | 3 | -.7 .4 -1.3 -39 1 -21 .0
EMR | 3 | 10.2 4.0 -4.7 1 29 9 .05
ESA | 3 | 2.3 5.6 -17.0 159 -233 102 .11
GFZ | 3 | -.1 .3 -.4 -46 -44 -20 .03
GRG | 3 | -.2 3.8 -2.8 -11 56 -47 .27
JPL | 3 | 9.6 -1.6 2.2 -23 13 10 .07
MIT | 3 | 5.6 7.1 1.8 -7 1 -22 .03
NGS | 3 | 8.4 6.9 -3.0 30 -27 84 .36
SIO | 3 | 8.1 .0 -44.4 168 -365 222 .11
COD | 4 | -.3 .4 -1.3 -30 -12 -20 .14
EMR | 4 | 4.4 3.8 -1.9 -4 20 8 .10
ESA | 4 | 2.7 5.3 -20.2 153 -281 135 .05
GFZ | 4 | .3 .4 -.2 -38 -67 -18 .08
GRG | 4 | -6.3 4.9 -11.7 -7 20 -33 .42
JPL | 4 | 1.2 5.0 7.2 -28 7 4 .38
MIT | 4 | 3.6 3.2 -1.3 -13 0 -24 .26
NGS | 4 | 3.6 3.3 -.3 10 -7 36 .24
SIO | 4 | 1.4 1.2 -63.7 74 -444 142 .24
COD | 5 | .1 1.4 -.9 -31 -8 2 -.03
EMR | 5 | -3.1 7.9 -3.1 0 15 1 .22
ESA | 5 | -4.1 5.0 -14.5 129 -155 97 .21
GFZ | 5 | .3 .7 -.7 -47 -74 -14 .03
GRG | 5 | -8.2 8.7 1.4 -5 31 -40 .41
JPL | 5 | -6.2 6.9 4.7 -72 21 -11 .29
MIT | 5 | -.1 7.1 -.8 -6 0 -21 .13
NGS | 5 | -.5 -2.2 -8.7 41 0 5 .38
SIO | 5 | -3.3 4.0 -51.7 137 -287 -21 .16
COD | 6 | .3 1.6 -.2 -38 -14 11 -.20
EMR | 6 | 1.3 10.9 -3.5 3 19 12 .29
ESA | 6 | 1.0 7.4 -11.9 151 -229 118 -.15
GFZ | 6 | .6 .6 -.1 -53 -61 -10 -.23
GRG | 6 | -5.3 5.4 4.8 -17 34 -46 .43
JPL | 6 | -1.5 6.7 7.9 -63 17 19 -.08
MIT | 6 | 2.9 9.5 -.5 -9 -1 -26 .10
NGS | 6 | 6.8 10.1 -3.6 48 -27 58 .31
SIO | 6 | 1.9 4.8 -55.4 172 -349 -97 .22
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
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 1.1713.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1713.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 2.1713.[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 3.1713.[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 5.1713.0-6). 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 1713 summary. (Nov 04, 2012 - Nov 10, 2012)
Table 1.1713.a GPS week: 1713 MJD: 56235.000-56241.000
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 258| 0 0 1 9 54 3 -.39 11 11 | -926 -215 19 84
| 0 0 1 19 24 17 .02 | 512 850
emr 79| -2 0 -1 -43 42 -5 .33 16 16 | 3510 155 12 90
| 1 0 0 11 20 17 .03 | 843 688
esa 175| 1 0 1 125 -112 0 .05 6 6 | -1664 1265 11 99
| 0 0 0 27 55 11 .02 | 356 927
gfz 190| 0 -1 0 -84 -36 8 -.42 12 11 | 232 180 19 123
| 0 0 1 71 105 10 .03 | 500 800
grg 129| 0 0 0 0 76 -31 .46 14 13 | -172 44 15 148
| 0 0 2 16 25 16 .04 | 271 580
igr n/a| 0 0 1 -37 106 -36 -.16 4 4 | 8731 893 17 89
| 0 0 0 15 21 11 .03 | 2257 742
jpl 80| -1 0 0 -16 77 4 .38 15 14 | 3061 141 15 94
| 1 1 0 18 24 13 .04 | 831 769
mit 239| 0 0 0 -44 35 -6 -.18 6 6 | -270 40 22 203
| 0 0 0 29 44 11 .03 | 262 429
ngs 240| 0 0 -3 -88 81 14 .33 10 9 | -824 -412 1940 3959
| 1 0 2 52 29 19 .02 | 429 719
sio 280| -1 -1 8 98 -287 28 -.28 18 16 | --- --- --- ---
| 2 2 1 38 90 97 .03 | --- ---
Table 1.1713.b GPS week : 1713 MJD: 56235.000-56241.000
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 4 |
2 | 4 4 4 4 4 4 4 |
3 | 3 3 3 3 3 4 3 |
4 | 3 3 3 4 3 4 3 |
5 | 4 4 4 4 4 4 5 |
6 | 3 3 3 3 3 3 3 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 3 3 4 3 |
9 | 3 3 3 3 3 4 4 |
10 | 5 5 5 4 5 5 5 |
11 | 3 3 4 4 4 4 4 |
12 | 5 4 5 5 5 4 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 3 4 4 4 4 4 |
15 | 4 4 4 4 4 5 4 |
16 | 4 4 4 4 4 5 4 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 5 4 3 5 4 |
20 | 3 3 3 3 4 3 3 |
21 | 4 4 5 4 4 5 4 |
22 | 4 3 3 3 3 3 3 |
23 | 4 4 4 4 4 5 4 |
24 | 7 0 13 0 0 0 6 |
25 | 4 5 4 4 5 4 4 |
26 | 3 3 3 3 4 4 3 |
27 | 0 0 0 0 0 0 0 |
28 | 3 3 3 3 4 4 3 |
29 | 4 4 4 4 4 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 4 4 4 4 5 4 5 |
32 | 5 6 5 5 5 5 5 |
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 2.1713.0 GPS week: 1713 Day: 0 MJD: 56235.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| -1 1 1 16 78 15 -.43 12 11 | -919 -215 19 81
emr 80| -1 0 0 -40 56 -25 .36 16 16 | 2568 -958 16 97
esa 175| 0 1 0 118 -110 2 .05 6 6 | -1843 790 12 93
gfz 179| 0 0 0 -106 -38 12 -.42 11 11 | 441 -655 21 123
grg 130| 1 0 0 -31 97 -34 .54 14 13 | 29 -385 15 138
igr n/a| 0 0 1 -22 144 -48 -.15 4 4 | 5697 -260 17 103
jpl 80| -1 -1 1 -25 73 17 .43 14 14 | 2275 -1161 14 86
mit 239| 0 0 -1 -19 2 0 -.17 5 4 | -28 -276 24 177
ngs 240| 0 0 -1 -72 87 6 .35 10 9 | -859 -359 1910 4221
sio 282| 2 -4 8 73 -136 0 -.29 19 17 | --- --- --- ---
Table 2.1713.1 GPS week: 1713 Day: 1 MJD: 56236.000
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 259| 0 0 0 20 17 -3 -.39 13 12 | -868 408 17 85
emr 79| -4 -1 0 -35 33 -23 .35 16 16 | 2419 266 15 99
esa 175| 0 0 1 161 -158 19 .07 5 5 | -1157 -329 11 101
gfz 192| 0 -1 0 -115 72 10 -.36 11 10 | 571 63 19 115
grg 129| 0 1 1 3 93 -38 .45 13 12 | -167 164 16 167
igr n/a| 0 0 1 -38 103 -44 -.16 4 4 | 6277 1013 17 101
jpl 80| -4 0 1 -15 92 -21 .39 17 16 | 1948 402 17 96
mit 240| 0 0 0 -57 82 -7 -.17 5 5 | -310 322 26 216
ngs 242| 1 0 -4 -136 34 -6 .32 10 8 | -696 70 1830 3776
sio 279| 0 -3 8 114 -235 46 -.28 18 16 | --- --- --- ---
Table 2.1713.2 GPS week: 1713 Day: 2 MJD: 56237.000
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 261| 0 0 1 -1 41 -10 -.40 12 12 | -1018 -1236 16 87
emr 80| -3 0 -1 -53 40 -5 .30 15 15 | 3162 137 14 91
esa 175| 0 0 0 107 -157 -3 .04 7 7 | -1959 2527 13 108
gfz 190| -1 -1 1 -17 27 9 -.42 10 10 | 939 -966 19 124
grg 129| 0 0 0 9 91 -26 .47 13 12 | 185 -787 15 141
igr n/a| 0 0 2 -56 110 -24 -.18 4 4 | 7668 731 18 104
jpl 80| -1 0 0 -24 95 0 .37 15 14 | 2692 190 17 91
mit 240| 0 0 0 -14 -1 -12 -.20 6 5 | -316 -306 24 229
ngs 241| 1 0 -2 -71 80 36 .31 9 8 | -936 -1424 2400 4234
sio 281| -2 -2 8 154 -409 47 -.25 19 16 | --- --- --- ---
Table 2.1713.3 GPS week: 1713 Day: 3 MJD: 56238.000
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 260| 0 0 0 28 66 -27 -.38 9 9 | -640 -456 17 81
emr 80| 0 0 -1 -23 16 -17 .37 16 16 | 4261 -18 13 70
esa 175| 1 0 1 153 -132 1 .09 6 6 | -1599 1719 12 96
gfz 191| 1 -1 0 -102 22 -2 -.39 12 11 | 239 186 17 125
grg 130| 1 0 -3 11 103 -62 .43 15 15 | 22 -172 15 154
igr n/a| 0 0 1 -25 87 -50 -.14 4 4 | 9232 877 17 83
jpl 80| -3 -2 0 19 41 7 .41 15 14 | 3712 59 16 91
mit 240| 0 0 0 -82 57 -26 -.16 6 6 | 141 -503 20 168
ngs 240| 1 0 -4 -131 92 18 .31 11 9 | -643 -436 1828 3906
sio 281| -2 -1 8 86 -291 175 -.24 17 17 | --- --- --- ---
Table 2.1713.4 GPS week: 1713 Day: 4 MJD: 56239.000
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 261| 0 -2 3 -16 77 7 -.36 12 12 | -1862 1328 24 88
emr 80| -1 1 -1 -59 66 7 .31 16 16 | 4474 -286 10 79
esa 175| 0 0 1 81 -125 0 .05 6 6 | -1884 1707 10 87
gfz 195| 0 0 -1 44 -120 -3 -.43 10 10 | -615 935 20 120
grg 130| 0 1 -4 0 51 -13 .44 14 13 | -433 686 15 148
igr n/a| 0 0 1 -59 113 -30 -.22 4 4 | 10454 372 17 93
jpl 80| 0 0 0 -28 104 17 .33 14 13 | 4141 -433 16 105
mit 240| 0 0 0 -8 64 1 -.23 6 6 | -576 725 23 254
ngs 243| -2 1 0 -151 64 -13 .34 10 9 | -1602 822 1577 4004
sio 254| -3 -1 7 75 -380 99 -.31 17 18 | --- --- --- ---
Table 2.1713.5 GPS week: 1713 Day: 5 MJD: 56240.000
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 256| 0 0 0 33 70 21 -.40 12 12 | -1023 -492 22 88
emr 80| -1 1 -2 -41 64 10 .33 16 16 | 3427 1090 11 99
esa 175| 1 0 2 136 4 -20 .04 6 6 | -1201 775 13 109
gfz 194| 0 0 0 -137 -230 3 -.46 16 16 | -120 1270 23 126
grg 126| 0 0 0 16 43 -20 .40 14 13 | -573 858 15 132
igr n/a| 1 0 0 -39 113 -34 -.17 5 4 | 9998 2043 17 61
jpl 80| 0 -1 0 -35 87 5 .32 14 13 | 2872 1167 15 79
mit 240| 0 0 -1 -74 -31 7 -.20 7 7 | -567 253 24 210
ngs 240| -1 0 -4 -48 131 24 .38 10 9 | -876 -614 1837 3771
sio 297| -3 1 8 46 -279 -44 -.29 18 15 | --- --- --- ---
Table 2.1713.6 GPS week: 1713 Day: 6 MJD: 56241.000
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 261| 0 -1 3 -12 31 18 -.38 10 10 | -154 -845 19 83
emr 80| -2 0 -1 -46 18 16 .32 16 16 | 4264 860 11 97
esa 175| 1 0 1 120 -106 -3 .06 6 6 | -2010 1668 12 102
gfz 193| 0 -2 -1 -158 9 26 -.45 11 11 | 175 428 19 128
grg 131| 2 0 3 -13 58 -25 .46 15 14 | -268 -55 16 158
igr n/a| 0 0 2 -20 75 -23 -.11 5 5 | 11796 1479 17 78
jpl 80| -1 0 0 -6 45 5 .41 15 15 | 3792 769 16 112
mit 240| 0 0 -1 -51 74 -9 -.14 7 6 | -236 65 17 167
ngs 239| 0 1 -6 -9 80 36 .33 11 9 | -162 -946 2204 3802
sio 289| -1 2 11 135 -278 -127 -.30 18 16 | --- --- --- ---
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 3.1713.0 GPS week: 1713 Day: 0 MJD: 56235.000
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 | 11 15 8 9 12 5 13 5 9 15 3 | 41 49 52 42 57 47 56 47 50 46 48
2 | 11 17 6 15 13 3 16 7 11 23 4 | 18 22 10 14 15 12 21 14 16 16 13
3 | 8 9 5 14 13 2 9 5 8 18 3 | 25 30 25 35 31 25 29 27 30 24 27
4 | 9 9 6 11 9 2 8 3 6 25 3 | 32 34 35 37 38 32 33 34 36 39 34
5E | 7 16 5 13 12 3 18 4 10 14 3 | 11 18 11 16 17 8 19 10 16 13 9
6 | 8 9 4 12 13 4 9 5 12 16 3 | 25 31 29 34 35 27 33 28 30 26 28
7 | 10 19 6 11 12 4 13 4 9 14 3 | 22 25 18 21 28 15 24 16 25 16 19
8 | 9 9 6 10 13 4 11 5 10 17 3 | 12 19 14 15 16 11 20 13 18 18 12
9 | 11 12 6 10 10 3 11 3 7 16 3 | 18 17 16 17 17 14 15 17 17 16 16
10E | 14 20 7 10 15 6 18 6 16 22 4 | 56 71 58 53 70 56 68 56 66 52 59
11 | 8 15 5 9 14 4 12 3 9 23 3 | 35 38 36 33 42 33 37 33 35 31 33
12 | 14 23 7 10 15 4 24 8 11 20 4 | 21 28 17 20 30 18 27 19 24 23 18
13 | 9 15 7 12 15 5 15 4 9 16 3 | 25 32 24 29 39 23 32 23 26 19 25
14 | 18 18 6 12 13 4 12 6 14 17 4 | 24 31 26 22 32 24 28 22 28 18 21
15 | 13 17 7 11 16 4 18 4 9 14 3 | 21 26 19 18 25 18 24 18 24 16 17
16 | 11 22 5 13 17 4 15 6 14 19 4 | 17 28 16 23 28 16 20 17 25 20 14
17 | 8 17 6 9 8 3 15 3 7 26 3 | 28 31 30 31 33 28 31 28 34 27 28
18E | 16 10 7 11 19 3 13 4 10 17 3 | 25 23 26 23 25 22 28 20 26 18 22
19 | 20 12 4 11 9 4 12 4 8 29 3 | 23 25 25 28 26 24 25 23 24 30 23
20E | 10 10 5 9 12 5 9 2 8 12 2 | 23 31 24 31 29 25 27 26 31 29 26
21 | 9 15 5 12 13 3 16 3 10 24 3 | 23 35 27 20 34 22 35 21 30 16 24
22E | 11 17 6 10 17 3 11 4 7 17 3 | 23 25 25 17 30 20 27 17 26 16 20
23 | 12 17 5 15 15 5 17 5 10 19 4 | 31 33 25 27 31 24 33 27 25 21 26
X24 | 19 --- 8 --- --- 13 --- 4 --- --- 6 | --- --- --- --- --- --- --- 5 --- --- 12
25 | 13 25 7 12 21 4 15 4 10 14 4 | 26 35 31 34 31 28 32 26 32 29 26
26 | 9 11 5 8 11 4 9 3 7 11 2 | 17 16 16 14 20 15 17 14 15 15 12
X27 | 8 --- --- --- --- 57 --- --- --- --- 0 | 64 --- --- --- --- 46 --- --- --- --- 66
28 | 6 11 4 9 15 3 11 3 8 15 2 | 19 26 25 25 38 21 25 23 31 26 23
29 | 10 16 6 11 13 6 16 6 11 27 4 | 24 25 27 27 24 28 24 25 32 24 22
30E | 14 16 6 13 16 4 14 6 11 17 4 | 32 30 31 27 30 29 29 26 29 28 26
31 | 12 15 5 16 16 3 13 5 11 14 3 | 20 27 22 25 32 22 27 18 26 19 18
32E | 20 22 5 11 16 6 21 6 8 15 4 | 54 45 48 49 43 47 44 49 44 44 46
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 11 14 4 14 5 10 19 |T 26 30 26 26 31 25 29 23 29 24 25
WRMS | 11 16 6 11 13 4 14 4 9 17 |NE 24 28 25 25 30 23 28 23 27 23 23
MEDI | 11 15 6 11 13 4 13 4 9 17 |MD 24 28 25 25 30 24 27 23 26 21 23
Table 3.1713.1 GPS week: 1713 Day: 1 MJD: 56236.000
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 | 14 19 7 10 9 5 13 4 11 16 3 | 27 35 34 29 39 31 42 31 38 35 33
2 | 14 17 6 14 11 2 16 7 11 22 4 | 25 24 16 17 17 15 24 16 23 19 20
3 | 7 12 4 11 11 3 8 6 7 16 3 | 30 30 26 26 29 26 30 26 30 25 30
4 | 12 10 4 8 10 4 10 4 10 25 3 | 28 31 26 26 29 25 27 27 32 36 27
5E | 9 16 5 9 14 3 24 4 10 13 3 | 23 24 15 15 17 13 24 13 22 17 17
6 | 8 11 3 13 13 3 7 5 10 14 3 | 28 29 23 27 28 24 29 25 28 25 28
7 | 10 16 4 12 16 3 16 5 9 13 3 | 20 27 17 19 29 16 24 17 27 18 19
8 | 11 12 4 8 13 4 12 3 6 14 2 | 20 26 17 15 21 16 24 19 27 21 20
9 | 10 11 5 8 13 4 12 4 9 13 3 | 19 21 15 16 17 16 20 17 24 17 18
10E | 23 23 7 12 13 5 18 6 16 21 5 | 55 68 54 49 64 52 67 52 65 46 54
11 | 6 16 4 9 12 4 13 4 12 19 3 | 30 33 23 26 27 26 30 25 29 23 28
12 | 10 22 7 8 13 7 26 7 10 20 4 | 22 30 21 21 31 20 30 20 32 24 20
13 | 10 15 7 15 20 3 16 5 8 16 4 | 27 34 26 27 40 25 32 25 29 21 25
14 | 10 15 5 9 15 3 15 6 8 14 3 | 18 30 19 16 32 17 26 19 27 14 20
15 | 11 15 5 7 18 4 18 5 10 14 3 | 23 26 19 17 31 17 23 18 25 17 20
16 | 12 18 5 16 13 3 14 5 12 20 4 | 24 30 22 22 30 20 25 21 27 27 23
17 | 9 17 6 11 8 3 16 3 10 25 3 | 26 34 26 26 29 25 32 25 31 23 26
18E | 17 11 6 10 18 2 14 4 5 17 3 | 31 28 28 26 29 25 27 26 32 27 26
19 | 27 16 4 9 8 4 14 6 8 27 4 | 32 24 16 21 19 17 24 16 18 18 21
20E | 8 11 4 12 15 5 9 4 7 12 2 | 37 39 34 37 36 34 36 36 38 39 35
21 | 10 15 6 9 9 4 15 5 10 27 3 | 21 35 23 21 32 21 33 22 31 13 23
22E | 8 12 4 7 12 3 10 4 9 8 2 | 18 25 20 14 25 17 22 16 26 16 18
23 | 10 15 6 13 16 4 18 5 9 16 3 | 28 30 24 24 29 22 30 22 24 22 23
X24 | 6 --- --- --- --- >>>> --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 1
25 | 15 29 7 13 12 6 17 5 10 20 4 | 47 48 44 43 48 42 52 44 46 52 46
26 | 7 13 3 7 10 3 9 3 7 12 2 | 20 24 12 13 20 13 19 15 21 15 18
X27 | 6 --- --- --- --- 50 --- --- --- --- 0 | 70 --- --- --- --- 39 --- --- --- --- 71
28 | 8 10 4 9 12 3 14 4 7 13 2 | 25 32 26 19 38 23 30 23 32 28 27
29 | 12 22 7 8 11 5 18 6 11 25 4 | 20 28 19 17 16 15 23 18 25 19 18
30E | 13 18 7 13 15 4 15 8 11 18 4 | 23 28 23 33 28 24 25 22 30 24 23
31 | 15 17 5 12 17 3 16 4 11 14 3 | 20 28 20 19 34 19 29 19 31 19 22
32E | 19 23 9 13 18 6 50 8 10 20 6 | 43 40 34 42 38 35 47 36 35 32 36
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 16 5 11 13 4 17 5 10 18 |T 28 31 24 24 30 23 30 23 30 24 26
WRMS | 12 16 5 10 12 4 16 5 8 16 |NE 24 28 21 21 27 20 27 21 27 21 23
MEDI | 10 15 5 10 13 4 15 5 10 16 |MD 25 30 23 21 29 22 27 22 29 22 23
Table 3.1713.2 GPS week: 1713 Day: 2 MJD: 56237.000
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 | 14 14 7 10 8 5 12 4 12 15 3 | 33 39 37 30 43 34 42 34 39 37 35
2 | 9 15 5 15 12 2 13 4 11 22 3 | 18 25 15 17 16 16 22 17 18 17 18
3 | 9 8 5 9 12 4 9 5 9 17 3 | 24 28 24 22 29 22 28 23 29 22 25
4 | 8 8 5 10 10 4 10 4 10 28 3 | 24 29 25 28 31 25 26 27 27 35 27
5E | 9 13 5 11 13 3 21 5 9 12 3 | 19 23 16 16 17 14 24 16 18 20 18
6 | 9 9 3 10 10 3 8 5 8 12 2 | 24 29 27 22 32 24 30 24 29 23 26
7 | 11 17 5 10 15 4 14 4 5 13 3 | 22 28 18 22 27 19 23 22 23 19 21
8 | 11 9 5 9 9 4 9 4 7 15 2 | 15 22 16 15 16 15 20 17 19 22 14
9 | 5 12 5 7 9 3 13 4 6 12 2 | 18 20 17 16 20 16 18 19 17 21 18
10E | 13 19 6 9 13 7 18 8 12 17 4 | 49 68 54 50 65 52 64 53 58 49 54
11 | 8 15 6 11 13 5 13 5 9 21 3 | 31 33 28 29 33 26 29 28 28 27 28
12 | 12 22 7 6 17 5 28 7 11 19 5 | 25 34 23 24 34 26 31 23 33 24 22
13 | 11 14 6 13 16 3 12 6 8 14 3 | 24 31 22 24 34 21 27 23 23 19 22
14 | 9 14 8 10 14 5 14 7 10 16 3 | 19 29 22 20 31 21 26 20 26 17 21
15 | 8 15 6 8 13 4 20 6 7 18 3 | 23 31 23 19 30 23 30 25 24 28 25
16 | 11 17 4 13 18 3 16 6 12 16 4 | 21 27 20 19 32 18 23 18 26 23 19
17 | 15 20 8 12 10 4 17 4 8 28 4 | 32 31 24 28 29 25 27 25 30 19 26
18E | 8 12 7 8 19 3 13 7 8 17 3 | 17 23 22 15 28 18 22 16 23 22 19
19 | 32 12 7 12 7 5 10 7 8 27 5 | 27 23 21 22 20 19 21 21 20 22 21
20E | 11 8 5 9 16 4 12 4 7 21 3 | 28 22 22 26 24 21 24 23 24 29 23
21 | 11 14 16 10 11 6 14 6 9 30 4 | 19 31 25 17 30 18 28 19 24 16 20
22E | 9 12 6 6 11 2 11 4 8 15 3 | 16 24 20 18 26 16 24 20 21 18 18
23 | 11 17 7 13 14 4 18 7 12 16 4 | 30 31 22 20 26 22 29 24 25 22 24
X24 | 15 --- 11 --- --- 19 --- --- --- --- 12 | --- --- --- --- --- --- --- --- --- --- 1
25E | 9 27 6 9 12 4 15 5 7 10 4 | 33 41 31 31 33 32 34 33 33 31 31
26 | 11 13 4 10 11 3 9 4 10 8 3 | 16 26 20 19 23 19 21 22 22 23 22
X27 | 6 --- --- --- --- 196 --- --- --- --- 0 | 107 --- --- --- --- 160 --- --- --- --- 110
28 | 10 14 5 9 16 2 10 4 7 13 3 | 21 31 24 22 40 23 26 24 31 27 24
29 | 10 19 9 10 10 4 16 5 10 25 4 | 17 27 22 19 21 21 21 22 23 21 19
30E | 13 13 6 11 15 3 13 6 11 20 4 | 27 24 23 29 22 23 23 22 24 23 21
31 | 12 16 5 12 14 2 16 4 7 14 3 | 19 26 17 20 30 17 25 17 25 16 19
32E | 17 26 7 10 17 6 19 8 9 21 5 | 35 32 30 36 26 30 33 31 25 26 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 7 10 13 4 15 6 9 19 |T 26 29 23 23 28 26 27 23 26 23 25
WRMS | 12 15 7 10 12 4 14 5 8 16 |NE 22 28 22 21 27 21 25 22 24 22 22
MEDI | 11 14 6 10 13 4 13 5 9 16 |MD 24 28 22 22 29 21 26 22 24 22 22
Table 3.1713.3 GPS week: 1713 Day: 3 MJD: 56238.000
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 | 12 16 10 12 13 3 14 5 12 14 4 | 35 46 43 35 50 42 50 41 38 39 40
2 | 9 17 5 16 11 4 15 7 15 21 4 | 21 26 19 23 21 16 23 18 27 18 22
3 | 6 10 4 11 17 3 11 4 10 18 3 | 32 36 29 32 35 28 37 31 31 28 36
4 | 8 9 7 13 11 5 9 6 8 26 3 | 35 38 37 36 37 33 33 35 39 41 36
5E | 5 17 7 11 11 3 20 6 11 11 3 | 20 27 19 19 23 16 24 19 22 18 22
6 | 6 10 4 11 13 3 9 6 9 14 3 | 31 34 31 32 35 27 35 31 32 28 35
7 | 8 19 5 14 17 4 15 7 9 12 3 | 22 26 18 21 26 15 23 16 21 15 18
8 | 8 13 5 7 12 5 10 4 8 12 2 | 18 24 17 15 18 16 23 18 20 21 16
9 | 6 10 7 7 9 5 12 5 9 13 2 | 18 23 19 16 19 16 20 17 23 18 19
10E | 12 21 6 14 15 6 15 6 11 14 4 | 55 72 59 51 69 57 69 56 64 52 60
11 | 7 16 6 10 18 3 14 4 14 19 3 | 33 38 32 31 38 30 36 31 28 26 32
12 | 10 21 6 10 14 4 26 9 12 17 4 | 52 54 47 56 52 49 53 50 54 48 48
13 | 9 16 5 12 21 4 14 6 11 14 4 | 23 32 21 24 37 20 30 20 24 16 21
14 | 9 15 7 10 16 3 15 8 10 14 3 | 26 30 23 21 33 21 31 24 28 18 26
15 | 6 14 6 8 15 6 18 7 11 16 3 | 27 34 29 26 35 25 32 26 29 26 31
16 | 8 19 7 14 18 4 13 6 8 19 4 | 21 28 19 24 30 18 23 23 23 17 23
17 | 9 16 8 15 8 4 17 6 11 25 4 | 32 37 32 35 36 31 35 31 38 25 34
18E | 8 14 7 10 20 5 14 4 7 12 3 | 33 35 32 31 31 27 37 28 34 31 35
19 | 7 15 5 10 11 4 14 6 10 26 3 | 28 29 23 29 27 21 29 23 19 21 26
20E | 9 11 6 10 16 4 9 5 8 13 3 | 22 28 21 26 26 22 27 25 23 27 21
21 | 10 14 6 16 9 4 15 7 12 26 4 | 24 34 26 27 31 22 34 24 31 15 24
22E | 8 11 6 8 13 5 11 4 7 11 3 | 20 24 22 20 23 19 25 18 24 20 20
23 | 10 16 6 14 17 3 16 6 11 17 4 | 25 31 20 20 26 18 29 19 24 17 20
X24 | 7 --- --- --- --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 1
25E | 10 26 6 16 12 4 16 7 13 11 4 | 32 38 32 32 34 35 39 37 34 33 32
26 | 7 13 7 10 11 4 11 4 8 9 3 | 22 26 21 19 25 18 23 19 21 19 24
X27E | 7 --- --- --- --- 64 --- --- --- --- 0 | 97 --- --- --- --- 115 --- --- --- --- 99
28 | 9 12 5 8 16 3 10 5 11 14 3 | 25 33 25 25 40 24 29 27 35 24 29
29 | 10 17 5 11 12 5 16 7 12 23 4 | 27 33 22 30 25 25 30 28 26 23 25
30E | 12 14 5 12 13 6 13 7 11 15 3 | 22 26 23 29 26 20 23 25 25 24 21
31 | 10 15 6 12 15 4 16 7 10 14 3 | 19 27 18 22 32 17 29 20 24 19 23
32E | 19 19 8 13 20 5 18 8 13 20 5 | 41 40 38 43 38 40 44 40 39 31 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 6 12 15 4 15 6 11 17 |T 30 33 27 28 32 28 32 27 30 25 29
WRMS | 9 16 6 11 15 4 14 6 9 17 |NE 26 31 25 26 30 23 30 24 27 22 26
MEDI | 8 15 6 11 13 4 14 6 11 14 |MD 26 32 23 26 31 22 30 25 27 23 25
Table 3.1713.4 GPS week: 1713 Day: 4 MJD: 56239.000
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 | 16 13 8 9 13 4 12 5 8 12 3 | 29 37 42 34 44 36 40 33 38 34 35
2 | 9 15 7 11 10 3 14 7 13 23 4 | 17 24 20 19 14 18 23 17 27 14 17
3 | 7 10 4 10 15 3 10 8 8 17 3 | 19 31 22 27 26 23 28 20 31 22 24
4 | 9 7 5 9 10 3 8 6 10 27 3 | 25 33 34 34 34 29 31 28 32 35 30
5E | 9 17 4 10 15 3 17 6 12 12 4 | 12 22 16 17 16 13 21 12 27 13 13
6 | 8 11 3 9 12 4 11 5 10 15 3 | 21 31 25 27 32 24 29 24 32 24 25
7 | 10 17 4 11 14 3 14 5 8 14 3 | 22 29 25 22 29 22 25 20 30 20 20
8 | 9 10 4 7 11 3 12 5 7 11 2 | 16 24 23 19 19 20 23 16 28 18 18
9 | 10 11 5 8 9 4 11 6 7 14 3 | 16 20 19 16 15 17 16 15 25 14 13
10E | 14 22 7 10 14 5 17 7 13 20 4 | 48 67 56 50 64 53 66 51 62 53 54
11 | 9 15 5 10 14 4 12 6 13 16 3 | 23 29 29 29 31 26 28 25 28 19 24
12E | 10 20 8 10 13 5 23 8 11 15 4 | 27 32 27 27 29 25 30 27 33 23 24
13 | 10 15 7 8 18 3 12 7 9 15 3 | 17 32 25 21 38 22 29 21 30 19 20
14 | 11 15 6 11 14 5 12 6 8 16 3 | 27 33 32 20 34 26 30 24 36 22 25
15 | 10 17 6 7 13 4 20 6 9 17 4 | 16 25 21 17 26 19 24 16 28 18 16
16 | 11 16 5 10 17 4 13 8 11 14 4 | 31 39 35 36 41 35 36 34 41 36 34
17 | 16 17 6 13 10 3 16 4 8 26 4 | 27 32 30 34 32 29 31 28 34 24 29
18E | 9 13 6 10 18 5 12 6 12 16 3 | 30 27 31 26 25 27 29 24 35 25 26
19 | 12 12 3 10 10 3 12 6 8 25 3 | 21 25 20 25 18 21 24 18 25 18 19
20E | 13 12 4 11 12 7 10 6 9 11 3 | 25 35 31 29 31 30 28 27 35 29 23
21 | 7 15 6 10 9 4 14 5 12 27 3 | 19 35 30 24 34 26 33 25 31 17 24
22E | 9 14 6 9 14 3 10 5 9 11 3 | 23 30 32 22 30 27 30 25 35 27 24
23 | 14 15 6 13 13 3 14 7 12 16 4 | 16 28 20 18 26 19 24 17 25 17 16
X24 | 7 --- --- --- --- 44 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 1
25E | 12 24 7 8 12 3 17 6 12 12 4 | 23 30 30 26 26 26 31 26 34 26 24
26 | 13 13 5 10 11 4 11 6 9 11 3 | 13 21 15 19 16 14 17 15 26 14 14
X27E | 7 --- --- --- --- 105 --- --- --- --- 0 | 50 --- --- --- --- 116 --- --- --- --- 51
28 | 9 17 5 9 26 3 12 6 10 11 4 | 24 35 33 31 51 30 32 28 34 29 30
29 | 16 18 6 9 13 5 17 6 12 24 4 | 28 31 26 23 27 26 27 25 31 20 22
30E | 15 12 6 9 15 7 15 5 14 17 4 | 21 23 23 23 22 20 22 20 22 19 18
31 | 17 18 6 12 19 6 17 7 12 14 4 | 21 30 24 17 35 22 31 21 30 22 19
32E | 21 21 7 11 20 6 16 10 11 16 5 | 38 40 41 40 39 39 37 39 43 35 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 10 14 4 14 6 10 17 |T 24 31 27 25 30 28 29 24 32 23 23
WRMS | 12 16 6 10 13 4 13 6 9 18 |NE 20 28 25 23 27 23 27 21 29 20 21
MEDI | 10 15 6 10 13 4 12 6 10 15 |MD 23 30 26 24 29 26 29 24 31 22 24
Table 3.1713.5 GPS week: 1713 Day: 5 MJD: 56240.000
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 | 14 14 5 15 12 3 13 5 11 16 3 | 38 41 41 34 44 40 45 40 42 31 37
2 | 7 15 6 18 10 3 15 7 7 24 4 | 21 24 22 17 21 19 24 17 22 19 19
3 | 6 11 5 19 15 4 8 7 12 15 3 | 29 30 29 23 28 30 30 29 35 23 29
4 | 10 8 5 14 11 4 8 6 6 24 3 | 29 31 30 29 33 30 31 29 33 37 30
5E | 10 18 8 16 14 3 23 6 10 9 4 | 19 21 22 15 20 17 27 11 19 13 15
6 | 8 11 4 18 14 5 7 6 13 11 3 | 30 29 32 25 32 31 32 29 36 25 30
7 | 14 17 5 20 19 5 14 5 8 14 4 | 22 27 24 22 30 22 26 20 24 19 17
8 | 12 10 6 13 17 7 10 6 10 12 3 | 23 26 25 20 26 24 28 22 29 22 18
9 | 7 14 6 15 10 3 12 7 9 17 3 | 20 20 22 14 19 20 20 19 23 17 15
10E | 14 25 6 16 13 5 15 7 8 21 4 | 50 67 54 50 59 53 63 51 58 51 55
11 | 8 15 6 16 15 4 12 5 14 16 4 | 33 30 30 31 31 30 29 29 31 21 26
12E | 9 18 6 13 16 4 20 8 10 13 4 | 23 31 28 27 28 26 30 27 34 24 23
13 | 11 14 6 16 19 5 13 7 9 16 4 | 26 32 28 25 36 26 31 25 29 22 22
14 | 11 15 7 15 15 4 14 7 12 14 4 | 20 28 24 18 31 20 26 19 26 16 20
15 | 16 17 7 9 12 9 18 9 10 20 4 | 20 23 24 17 27 21 24 18 22 19 19
16E | 13 20 6 19 16 3 14 5 9 32 4 | 37 36 34 21 34 31 33 25 37 18 28
17 | 11 17 8 18 8 4 15 6 12 24 4 | 32 30 29 27 30 28 33 26 36 22 29
18E | 12 10 7 16 17 3 12 5 9 9 3 | 21 25 26 21 27 21 25 20 29 21 23
19 | 18 15 5 19 10 6 10 8 13 24 4 | 24 24 25 26 20 24 23 22 26 20 20
20E | 11 10 4 12 11 3 9 6 11 12 3 | 26 26 27 28 29 25 26 23 27 25 22
21 | 7 17 8 16 13 4 16 7 14 26 4 | 23 36 28 17 33 22 33 20 29 15 23
22E | 10 9 7 13 15 4 10 4 9 11 3 | 18 24 24 21 23 19 24 18 26 20 18
23 | 13 16 6 20 17 6 17 6 10 19 4 | 29 31 28 22 27 25 31 24 27 20 20
X24E | 8 --- --- --- --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 1
25E | 14 24 6 11 11 4 19 6 7 11 4 | 21 23 23 16 23 20 28 17 24 18 15
26 | 7 14 6 11 10 3 12 8 11 12 3 | 25 25 27 17 23 23 25 18 22 19 20
X27E | 7 --- --- --- --- 68 --- --- --- --- 0 | 71 --- --- --- --- 47 --- --- --- --- 71
28E | 9 21 6 14 21 4 9 8 10 8 4 | 51 57 50 52 53 49 51 52 55 52 52
29 | 15 19 6 18 13 6 15 7 10 21 4 | 28 26 27 22 24 24 28 22 28 18 20
30E | 15 17 6 20 17 4 15 6 8 13 4 | 27 30 31 30 29 28 27 27 27 24 21
31 | 13 18 8 19 15 5 16 6 7 19 4 | 16 29 23 16 29 18 25 13 25 17 17
32E | 21 16 10 14 19 6 18 8 10 15 4 | 46 42 46 49 40 43 41 44 40 38 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 16 14 5 14 7 10 18 |T 28 30 29 25 30 27 30 25 30 23 25
WRMS | 12 16 6 16 13 4 13 7 9 15 |NE 25 28 27 22 28 25 28 23 28 21 22
MEDI | 11 15 6 16 14 4 14 6 10 15 |MD 26 29 27 22 29 25 28 22 28 20 21
Table 3.1713.6 GPS week: 1713 Day: 6 MJD: 56241.000
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 | 14 13 9 10 13 4 13 5 11 13 3 | 43 52 52 47 56 49 52 48 49 44 48
2 | 8 14 7 11 12 4 16 8 12 25 4 | 16 23 16 16 19 14 24 15 17 22 16
3 | 5 12 6 9 14 5 11 5 10 17 3 | 21 28 22 22 30 21 29 21 30 22 24
4 | 9 7 5 9 12 4 10 5 9 23 3 | 32 38 35 38 41 36 37 35 36 42 36
5E | 10 20 6 12 12 4 22 8 15 11 4 | 15 26 11 18 17 12 25 16 20 17 15
6 | 7 10 3 11 14 4 10 5 8 13 3 | 25 31 26 26 36 26 32 26 33 25 28
7 | 10 16 5 10 18 5 15 7 10 16 4 | 21 23 16 20 27 15 23 17 19 14 15
8 | 8 9 5 5 13 5 13 6 9 10 3 | 13 20 15 14 20 13 21 13 19 14 13
9 | 10 12 6 10 13 4 11 6 12 14 3 | 22 24 20 18 21 19 25 18 23 19 19
10E | 13 21 6 11 16 7 17 8 13 22 4 | 56 75 63 54 68 59 74 59 63 58 61
11 | 7 14 6 7 16 4 14 5 15 18 3 | 33 38 35 35 41 35 33 34 36 30 33
12E | 8 20 8 9 26 5 22 7 15 17 4 | 22 35 26 28 36 24 32 24 31 25 24
13 | 15 14 7 11 20 6 12 8 11 19 4 | 22 29 21 21 35 18 29 19 22 16 19
14 | 8 15 6 12 13 5 14 9 10 16 3 | 18 30 21 20 34 20 30 23 26 17 21
15 | 7 17 6 8 19 6 21 6 15 20 4 | 24 37 24 24 34 24 37 26 37 26 27
16E | 8 17 6 14 17 4 16 6 10 14 4 | 19 30 23 28 32 23 28 23 25 24 23
17 | 12 16 7 12 8 5 17 7 11 25 4 | 33 39 32 37 36 34 35 33 36 28 33
18E | 9 12 6 12 17 4 14 4 8 9 3 | 16 23 19 21 27 18 26 18 22 19 19
19 | 8 16 5 11 10 4 16 6 7 25 3 | 25 27 25 28 28 24 24 25 27 26 25
20E | 9 12 5 12 11 5 8 5 12 13 3 | 26 34 25 31 31 27 31 30 25 31 27
21 | 7 15 6 13 8 3 18 6 8 26 4 | 21 33 24 25 32 23 35 23 28 20 24
22E | 10 11 6 10 12 4 11 5 12 12 3 | 22 28 23 21 26 23 27 22 30 26 22
23 | 12 17 6 14 19 7 15 8 10 20 4 | 23 30 19 18 27 19 28 21 22 17 18
X24E | 12 --- 8 --- --- 12 --- 7 --- --- 6 | --- --- --- --- --- --- --- 6 --- --- 1
25E | 12 24 7 10 14 3 17 7 9 12 4 | 31 38 32 34 32 31 38 32 31 34 31
26 | 7 14 8 9 10 4 10 6 10 12 3 | 24 35 27 27 30 25 34 27 28 28 28
X27E | 6 --- --- --- --- 65 --- --- --- --- 0 | 69 --- --- --- --- 57 --- --- --- --- 72
28E | 6 18 5 7 16 6 11 5 5 15 3 | 45 53 48 52 55 47 48 50 49 48 49
29 | 12 20 8 12 14 4 17 5 10 25 4 | 36 37 29 36 31 32 30 33 35 29 30
30E | 15 17 6 14 15 6 14 8 7 18 4 | 24 31 21 28 25 21 29 23 19 27 21
31 | 10 18 7 15 18 5 18 8 13 16 4 | 19 31 22 20 35 19 28 19 25 18 20
32E | 20 19 9 12 24 4 14 8 13 13 5 | 49 46 45 52 47 48 46 48 45 45 45
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 6 11 15 5 15 7 11 18 |T 27 34 27 28 33 27 33 26 30 27 27
WRMS | 10 16 6 11 14 5 15 6 9 16 |NE 24 31 25 25 32 24 30 25 28 24 25
MEDI | 9 15 6 11 14 4 14 6 10 16 |MD 24 31 24 26 32 24 30 23 28 25 24
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1713 GPS week: 1713 MJD: 56235.0-56241.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 |U 5 5 14 |U 7 9 26 |U 8 7 16 |
emr | emr 2868 | 11 13 18 |U 8 9 27 | 9 9 21 |
esa | esa 2921 | 6 6 14 |U 7 10 27 | 8 8 19 |
gfz | gfz 2867 |U 7 5 14 |U 7 9 29 |U 10 10 21 |
grg | grg 2879 |U 13 14 21 |U 9 11 33 | 10 13 27 |
igr | igr 2906 | 6 5 14 | 7 9 27 | 8 8 19 |
igs | igs 2900 | 11 14 16 | 8 9 27 | 9 10 20 |
jpl | jpl 2867 | 11 14 19 |U 9 12 29 | 8 9 19 |
mit | mit 2907 | 15 16 23 |U 8 10 27 |U 9 10 21 |
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 5.1713.0 GPS week: 1713 Day: 0 MJD: 56235.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 5 4 16 | 8 9 31 | 8 8 21 |
emr | emr 2868 | 8 7 18 | 9 12 31 | 11 13 24 |
esa | esa 2976 | 5 4 18 | 8 11 33 | 9 9 24 |
gfz | gfz 2869 | 6 4 17 | 8 10 35 | 8 9 24 |
grg | grg 2880 | 7 7 18 | 9 13 42 | 14 21 43 |
igr | igr 2971 | 6 3 18 | 8 10 32 | 9 9 23 |
igs | igs 2967 | 7 7 17 | 8 10 32 | 10 12 23 |
jpl | jpl 2868 | 7 7 19 | 8 11 30 | 9 11 24 |
mit | mit 2976 | 10 8 20 | 9 12 31 | 10 12 21 |
Table 5.1713.1 GPS week: 1713 Day: 1 MJD: 56236.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2930 | 6 5 14 | 8 9 24 | 9 5 15 |
emr | emr 2868 | 9 8 17 | 10 10 27 | 8 8 20 |
esa | esa 2880 | 4 5 13 | 8 8 24 | 7 6 18 |
gfz | gfz 2867 | 5 6 10 | 8 7 24 | 7 7 21 |
grg | grg 2880 | 8 8 15 | 10 11 35 | 10 12 23 |
igr | igr 2852 | 5 5 12 | 8 8 25 | 6 5 16 |
igs | igs 2854 | 9 10 14 | 9 8 28 | 11 10 26 |
jpl | jpl 2867 | 8 9 17 | 12 14 33 | 8 7 18 |
mit | mit 2880 | 17 18 59 | 8 11 31 | 12 11 32 |
Table 5.1713.2 GPS week: 1713 Day: 2 MJD: 56237.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2914 | 5 5 14 | 6 10 19 | 8 7 18 |
emr | emr 2868 | 10 13 17 | 7 8 22 | 9 11 25 |
esa | esa 2976 | 5 6 12 | 6 9 22 | 8 10 21 |
gfz | gfz 2867 | 8 6 16 | 6 7 19 | 10 11 20 |
grg | grg 2879 | 12 16 19 | 7 9 30 | 9 13 20 |
igr | igr 2924 | 6 5 15 | 6 9 18 | 8 10 20 |
igs | igs 2960 | 10 14 13 | 6 8 20 | 9 12 20 |
jpl | jpl 2868 | 10 14 19 | 8 11 20 | 9 11 20 |
mit | mit 2880 | 15 16 16 | 6 8 20 | 9 13 21 |
Table 5.1713.3 GPS week: 1713 Day: 3 MJD: 56238.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2997 | 3 6 11 | 5 6 22 | 9 6 17 |
emr | emr 2868 | 14 18 17 | 5 7 21 | 12 8 24 |
esa | esa 2880 | 5 8 12 | 5 7 24 | 9 8 21 |
gfz | gfz 2867 | 6 4 13 | 6 7 29 | 12 9 20 |
grg | grg 2880 | 17 19 19 | 6 8 27 | 9 14 30 |
igr | igr 2880 | 5 6 11 | 5 7 24 | 8 7 22 |
igs | igs 2871 | 14 19 16 | 5 6 22 | 10 9 21 |
jpl | jpl 2868 | 14 20 20 | 8 9 29 | 11 8 24 |
mit | mit 2880 | 17 21 15 | 7 7 23 | 10 11 23 |
Table 5.1713.4 GPS week: 1713 Day: 4 MJD: 56239.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2943 | 7 3 11 | 10 9 37 | 8 6 15 |
emr | emr 2868 | 16 17 19 | 10 10 32 | 8 10 21 |
esa | esa 2880 | 8 4 12 | 10 10 33 | 8 9 17 |
gfz | gfz 2868 | 8 4 13 | 9 10 34 | 13 13 24 |
grg | grg 2880 | 15 16 23 | 11 10 34 | 9 11 20 |
igr | igr 2879 | 8 4 14 | 10 9 33 | 8 8 18 |
igs | igs 2857 | 15 17 14 | 12 9 35 | 8 9 14 |
jpl | jpl 2868 | 15 17 17 | 9 9 30 | 8 8 16 |
mit | mit 2880 | 16 14 15 | 10 10 33 | 9 12 16 |
Table 5.1713.5 GPS week: 1713 Day: 5 MJD: 56240.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2926 | 4 5 13 | 8 12 26 | 8 7 16 |
emr | emr 2868 | 10 13 17 | 9 10 26 | 7 7 17 |
esa | esa 2880 | 6 7 14 | 8 13 31 | 7 8 15 |
gfz | gfz 2869 | 6 6 13 | 8 10 36 | 10 12 21 |
grg | grg 2879 | 14 20 28 | 10 13 33 | 9 9 23 |
igr | igr 2878 | 5 6 13 | 8 12 31 | 6 7 17 |
igs | igs 2848 | 15 16 16 | 9 11 30 | 6 7 15 |
jpl | jpl 2868 | 10 15 19 | 13 17 42 | 7 8 17 |
mit | mit 2880 | 15 15 17 | 9 11 30 | 6 6 14 |
Table 5.1713.6 GPS week: 1713 Day: 6 MJD: 56241.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 5 5 17 | 7 11 21 | 8 6 14 |
emr | emr 2868 | 12 12 25 | 7 9 27 | 9 9 18 |
esa | esa 2976 | 7 7 18 | 7 10 21 | 9 8 14 |
gfz | gfz 2866 | 8 7 18 | 7 10 26 | 12 10 18 |
grg | grg 2880 | 14 11 25 | 7 12 33 | 11 15 29 |
igr | igr 2963 | 6 8 18 | 6 10 23 | 9 8 16 |
igs | igs 2944 | 12 14 22 | 6 11 23 | 10 10 19 |
jpl | jpl 2868 | 11 13 22 | 6 11 22 | 9 10 18 |
mit | mit 2976 | 16 16 22 | 7 11 23 | 9 8 18 |
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 6.1713 GPS week: 1713 MJD: 56235.500-56241.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -24 -43 47 -105 7 | -7 16
| 20 21 52 127 5 | 2
emr uuuuu | 14 5 32 -119 5 | 24 31
| 13 16 44 89 9 | 3
esa uuuuu | -54 -22 28 -125 1 | -5 16
| 36 25 76 64 6 | 1
gfz uuuuu | 73 54 -25 3 -2 | 2 13
| 37 30 77 65 5 | 2
grg uuuux | -8 -38 35 118 12 | -10 34
| 34 15 51 117 10 | 5
igr xxxxx | -26 8 -10 78 -2 | -2 14
| 25 9 57 64 6 | 2
irf xxxxx | 13 6 7 0 3 | -3 12
| 16 5 11 31 3 | 2
jpl uuuuu | -4 -13 -73 53 -13 | 35 39
| 28 23 118 89 13 | 4
mit uuuuu | 37 32 -62 43 1 | -4 11
| 14 19 93 66 11 | 2
ngs uuuuu | -4 52 26 174 -4 | 5 14
| 35 44 102 111 4 | 2
sio xuuuu | 373 -145 59 101 0 | 30 34
| 88 54 97 31 8 | 3
Table 7.1713.0 GPS week: 1713 Day: 0 MJD: 56235.500
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 -41 44 68 0 | -8 12
emr uuuuu | 7 16 37 -22 6 | 21 25
esa uuuuu | -48 24 -60 -105 -3 | -4 10
gfz uuuuu | 44 29 49 -47 -6 | 4 8
grg uuuux | -21 -40 26 -54 22 | -5 37
igr xxxxx | -54 -8 5 1 -7 | 0 8
irf xxxxx | -1 5 0 -11 1 | -1 7
jpl uuuuu | 15 -39 97 -57 -1 | 39 40
mit uuuuu | 20 1 -4 72 3 | -1 6
ngs uuuuu | 26 49 -84 41 2 | 7 10
sio xuuuu | 200 -130 81 109 8 | 25 29
Table 7.1713.1 GPS week: 1713 Day: 1 MJD: 56236.500
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 -53 63 25 10 | -8 12
emr uuuuu | 17 -15 104 -5 15 | 23 26
esa uuuuu | -27 -61 44 -60 7 | -4 11
gfz uuuuu | 52 81 -135 -1 3 | 3 9
grg uuuux | -36 -25 -15 32 5 | -4 37
igr xxxxx | -49 7 16 8 1 | -1 9
irf xxxxx | 8 6 -3 -11 1 | -2 7
jpl uuuuu | -43 10 -126 16 -5 | 39 39
mit uuuuu | 23 36 -57 -8 -6 | -1 6
ngs uuuuu | -2 105 46 45 -5 | 6 9
sio xuuuu | 352 -183 196 135 11 | 28 30
Table 7.1713.2 GPS week: 1713 Day: 2 MJD: 56237.500
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 | -13 -53 23 -187 6 | -6 13
emr uuuuu | -2 7 -17 -250 -8 | 25 29
esa uuuuu | -14 -15 -3 -104 -4 | -3 12
gfz uuuuu | 52 89 -55 60 -1 | 3 10
grg uuuux | -43 -47 4 47 22 | -7 35
igr xxxxx | -39 -1 -27 135 -1 | 0 10
irf xxxxx | 1 -3 9 13 3 | -1 8
jpl uuuuu | -17 -31 -120 3 -21 | 39 40
mit uuuuu | 34 27 16 88 4 | -1 6
ngs uuuuu | -43 -22 81 195 -6 | 6 10
sio xxxxx | 460 -188 -41 96 -3 | 32 34
Table 7.1713.3 GPS week: 1713 Day: 3 MJD: 56238.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -52 -53 30 -24 11 | -10 18
emr uuuuu | 37 11 18 -152 18 | 20 29
esa uuuuu | -59 -26 118 -131 11 | -8 19
gfz uuuuu | 61 84 -118 -42 6 | -1 15
grg uuuux | -15 -44 18 124 2 | -15 32
igr xxxxx | -16 12 96 61 4 | -4 17
irf xxxxx | 17 11 8 -31 0 | -5 15
jpl uuuuu | 28 -19 -23 -1 0 | 32 38
mit uuuuu | 60 39 -178 30 -17 | -6 14
ngs uuuuu | -30 95 163 261 -6 | 2 16
sio xuuuu | 409 -180 51 55 5 | 30 35
Table 7.1713.4 GPS week: 1713 Day: 4 MJD: 56239.500
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 | -49 -31 -20 -234 7 | -7 19
emr uuuuu | 3 -20 63 -129 6 | 24 33
esa uuuuu | -40 -26 -70 -71 -1 | -5 20
gfz uuuuu | 61 26 42 -49 -4 | 1 17
grg uuuux | -15 -54 -5 174 18 | -15 32
igr xxxxx | -15 14 -72 177 -8 | -3 17
irf xxxxx | 3 3 30 -26 2 | -4 15
jpl uuuuu | -38 -22 27 158 -21 | 33 39
mit uuuuu | 29 23 66 -58 3 | -7 14
ngs uuuuu | 43 67 -57 346 -2 | 3 16
sio xxxxx | 453 -33 -91 118 -9 | 32 37
Table 7.1713.5 GPS week: 1713 Day: 5 MJD: 56240.500
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 -69 150 -240 2 | -5 20
emr uuuuu | 17 21 -22 -191 0 | 27 36
esa uuuuu | -126 -31 112 -251 -5 | -5 20
gfz uuuuu | 151 19 21 122 -6 | 2 17
grg uuuux | 59 -46 113 242 -3 | -13 32
igr xxxxx | 18 19 -24 90 -8 | -3 17
irf xxxxx | 44 6 0 60 9 | -3 16
jpl uuuuu | 16 26 -106 185 -35 | 32 38
mit uuuuu | 47 66 -160 143 18 | -6 14
ngs uuuuu | 18 47 -86 143 -8 | 4 17
sio xuuuu | 350 -136 121 63 -10 | 33 37
Table 7.1713.6 GPS week: 1713 Day: 6 MJD: 56241.500
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 | -13 -3 41 -139 11 | -4 19
emr uuuuu | 15 12 42 -83 0 | 29 37
esa uuuuu | -66 -16 54 -152 2 | -4 20
gfz uuuuu | 89 51 21 -19 -6 | 1 17
grg uuuux | 12 -11 101 263 18 | -15 33
igr xxxxx | -29 14 -62 76 5 | -3 18
irf xxxxx | 17 11 4 9 3 | -2 15
jpl uuuuu | 7 -15 -264 66 -9 | 29 37
mit uuuuu | 43 30 -118 36 0 | -4 14
ngs uuuuu | -42 20 116 191 -2 | 4 17
sio xuuuu | 387 -163 94 131 -4 | 32 37
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