[IGSREPORT-21909] Wk 1743 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jun 21 04:58:48 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1743 (Jun 02, 2013 - Jun 08, 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:
igs1743[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1743[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1743[0-6].cls IGS GPS clock combination summary report.
igs17437.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17437.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 | JOZ2 JOZ2
0 | EMR | 26 26 TLSE WUHN TLSE WUHN
0 | ESA | IRKJ KOUC MATE WES2 KOUC MATE
0 | GFZ | MATE WES2 IRKJ MATE
0 | GRG | CONZ IRKJ NYAL THU3 CONZ NYAL THU3
0 | JPL | 26
0 | MIT | 23 26 23 26 DAV1 MDVJ POLV DAV1 IRKJ MDVJ POLV
1 | COD | 24 JOZ2 KOUC JOZ2 KOUC
1 | EMR | 21 26 21 26 HERS IRKT
1 | ESA | IRKJ KOUC NTUS KOUC MATE NTUS UNSA
1 | GFZ | MATE IRKJ MATE PIMO
1 | GRG | 26 26 IRKJ NTUS NTUS
1 | JPL | 21
1 | MIT | 3 26 3 26 MDVJ DAV1 IRKJ MDVJ
2 | COD | CONZ HERT KOUC TLSE CONZ HERT KOUC TLSE
2 | EMR | 21 26 21 26 TLSE
2 | ESA | IRKJ KOUC KOUC
2 | GFZ | ARTU DAEJ MANA YKRO ARTU DAEJ DAV1 GLPS IRKJ MANA
2 | GFZ | YKRO
2 | GRG | 3 21 26 3 21 26 DAV1 IRKJ NTUS DAV1 NTUS
2 | JPL | 21 26
2 | MIT | 21 26 21 26 MDVJ DAV1 IRKJ MDVJ PRDS
3 | COD | 21 21 FLRS KOUC CONZ FLRS KOUC
3 | EMR | 21 26 21 26 HERS HERS
3 | ESA | KOUC KOUC UNSA
3 | GFZ | ARTU CHTI DAEJ IRKJ IRKT CHTI DAEJ IRKJ IRKT
3 | GRG | 3 26 3 26 ISPA ISPA
3 | JPL | 3
3 | MIT | 26 3 26 IRKT MDVJ CAS1 IRKT MDVJ NTUS
4 | COD | 26 26 HERT JOZ2 MOBS HERT JOZ2 MOBS XMIS
4 | EMR | MCM4 MCM4
4 | ESA | 26 26 UNSA
4 | GFZ | 26 13 26 AUCK NRMD AUCK COCO NRMD
4 | GRG | DAV1 IRKT KOUC NTUS WROC DAV1 KOUC WROC
4 | MIT | 23 23 QAQ1 REUN MDVJ QAQ1 REUN
5 | COD | HERT MAC1 HERT MAC1
5 | EMR | 26 HERS WHIT WUHN YAKT YELL WHIT WUHN YELL
5 | ESA | 21 21 HOFN IRKJ HOFN UNSA
5 | GFZ | KOUC AUCK IRKJ KOUC
5 | GRG | 26 26 AUCK DARW IRKJ REUN IRKJ REUN REYK
5 | JPL | WHIT
5 | MIT | 3 6 16 23 26 28 31 3 6 10 23 28 MAC1 MDVJ NTUS PALM
5 | MIT | RIOP IRKJ MAC1 MDVJ NTUS PALM RIOP
6 | COD | 26 26 KOUC
6 | EMR | HERS THTI WUHN HERS THTI WUHN
6 | ESA | 26 26 CHUR IRKJ CHUR IRKJ KOUC
6 | GFZ | 26 26 CHTI HOB2 KOUC AREQ CHTI HOB2
6 | GRG | ALRT IRKJ KOUC NKLG NRMD PIMO THTI ALRT IRKJ KOUC
6 | GRG | NKLG NRMD PIMO THTI URUM
6 | MIT | 16 31 16 26 31 KOUC MDVJ MDVJ
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. 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 G27 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.1 1.3 -.4 -41 -6 -13 .22
EMR | 0 | -.9 -8.2 4.6 -12 7 -24 .35
ESA | 0 | -.8 -.7 5.2 44 4 -42 .28
GFZ | 0 | -.1 .0 -.7 -32 -23 -15 .12
GRG | 0 | 3.2 -.3 39.1 -32 49 -19 .06
JPL | 0 | -.5 -2.5 5.6 -46 -20 -70 .38
MIT | 0 | 3.5 -2.4 13.0 -33 -13 -38 .39
NGS | 0 | .9 -5.0 18.4 -118 -45 -10 .70
SIO | 0 | 1.5 -5.7 -73.5 -136 -321 48 .21
COD | 1 | -1.3 1.3 -1.2 -39 9 -6 .32
EMR | 1 | -3.9 -9.5 4.7 -10 12 -26 .18
ESA | 1 | -3.5 -3.4 2.8 43 15 -41 .17
GFZ | 1 | -.5 .3 -.2 -22 -21 1 .13
GRG | 1 | 1.8 -1.9 38.8 -26 34 -49 .20
JPL | 1 | -2.1 -3.5 1.4 -69 0 -22 .53
MIT | 1 | 2.2 -3.5 13.0 -6 7 -37 .31
NGS | 1 | -2.0 -8.8 13.1 -103 -2 -35 .56
SIO | 1 | -.9 -7.1 -64.8 -144 -334 5 .32
COD | 2 | -.2 1.1 -.9 -36 1 -19 .14
EMR | 2 | -2.1 -10.5 1.8 -2 4 -21 .23
ESA | 2 | -4.3 -4.1 1.5 39 37 -52 .18
GFZ | 2 | -.9 .4 -.9 -11 -27 -4 .06
GRG | 2 | .7 -3.4 23.1 -28 25 -52 .08
JPL | 2 | .1 -4.8 3.8 -39 29 -39 .28
MIT | 2 | 4.3 .0 10.5 -1 15 -43 .06
NGS | 2 | -2.4 -6.4 18.9 -151 -32 -34 .55
SIO | 2 | -.5 -7.9 -57.2 -128 -242 18 .06
COD | 3 | -.7 .4 -1.2 -56 26 -43 .30
EMR | 3 | -1.5 -.4 6.0 -18 13 -21 .30
ESA | 3 | -.4 -2.3 3.2 48 -6 -41 .12
GFZ | 3 | -.1 .1 -.2 -18 -24 0 .02
GRG | 3 | 3.9 1.3 36.2 -26 41 -57 .23
JPL | 3 | 5.2 -.8 10.1 -32 24 -57 .24
MIT | 3 | 2.3 -2.0 17.0 -2 7 -44 .22
NGS | 3 | 2.7 -5.8 20.4 -129 -44 17 .54
SIO | 3 | -.6 -2.8 -63.1 -58 -267 154 .20
COD | 4 | -1.0 1.1 -1.1 -39 23 -1 .20
EMR | 4 | -.2 .7 2.9 -15 4 -22 .25
ESA | 4 | -3.0 .3 3.7 45 19 -18 .02
GFZ | 4 | -1.5 .9 -1.1 -12 -21 -11 .22
GRG | 4 | 5.4 4.1 35.3 -19 36 -41 .24
JPL | 4 | -.7 -3.7 7.6 -34 -9 -28 .29
MIT | 4 | 2.4 -4.8 14.4 -34 -16 -33 .23
NGS | 4 | 1.1 -10.0 13.5 -109 -27 -19 .64
SIO | 4 | .0 -3.5 -48.9 -98 -239 70 .04
COD | 5 | -.1 .8 -.8 -46 4 -13 .12
EMR | 5 | 5.0 -1.1 7.4 -7 7 -23 .13
ESA | 5 | 3.7 -1.8 8.8 66 -53 21 .03
GFZ | 5 | -.4 .3 .1 -26 -24 -2 -.23
GRG | 5 | 2.2 .6 41.7 -37 26 -12 .35
JPL | 5 | 4.5 -6.6 10.9 -33 14 -45 .06
MIT | 5 | 6.4 -1.6 17.0 -36 -27 -40 .31
NGS | 5 | 4.2 -4.9 12.6 -102 -52 26 .62
SIO | 5 | -.2 -4.0 -50.8 -173 -274 -63 .12
COD | 6 | .5 .9 .0 -42 -6 -28 .12
EMR | 6 | -4.0 -4.5 5.9 -12 12 -36 .11
ESA | 6 | 2.5 -2.6 2.3 45 0 -42 .06
GFZ | 6 | -.6 .5 -.2 -24 -23 -14 -.18
GRG | 6 | -2.1 1.5 29.5 -45 28 -15 .42
JPL | 6 | -.8 -7.3 12.7 -15 34 -46 .23
MIT | 6 | .2 -3.1 18.5 -36 -21 -50 .15
NGS | 6 | -4.0 -4.1 14.1 -101 14 -27 .48
SIO | 6 | 2.3 -3.7 -42.3 -89 -243 58 .09
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1743.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1743.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 2.1743.[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 3.1743.[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 5.1743.0-6). 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 1743 summary. (Jun 02, 2013 - Jun 08, 2013)
Table 1.1743.a GPS week: 1743 MJD: 56445.000-56451.000
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 267| -1 1 -6 21 28 -4 -.44 10 9 | -879 -419 18 84
| 0 0 1 20 22 16 .03 | 245 499
emr 80| 0 -2 -3 -4 -17 8 .34 13 13 | -5 229 15 97
| 1 0 1 18 12 13 .05 | 1017 1342
esa 150| 0 0 1 13 11 -4 .11 5 5 | -505 -998 15 119
| 0 0 1 9 19 6 .03 | 1132 694
gfz 202| 0 0 -1 -46 -65 15 -.42 9 9 | 174 -88 13 79
| 0 1 1 24 66 12 .03 | 339 583
grg 137| 2 1 21 -8 19 1 .59 16 15 | 44 -177 17 170
| 0 0 4 5 19 19 .06 | 152 507
igr n/a| 0 0 -1 20 42 -36 -.12 4 4 | 1543 264 15 80
| 0 0 0 8 15 12 .04 | 1259 1381
jpl 80| 0 0 -5 12 -35 -34 .42 13 13 | -445 181 15 108
| 0 0 1 12 26 12 .05 | 1158 1445
mit 236| 0 0 1 7 -12 3 -.57 10 9 | 17 -75 22 212
| 0 0 1 15 21 16 .02 | 132 506
ngs 243| 0 -1 -1 -19 52 0 .35 10 8 | -889 -449 1695 3566
| 0 0 2 34 38 15 .05 | 222 465
sio 419| 0 1 -6 -146 -284 21 -.33 20 18 | --- --- --- ---
| 1 0 0 47 33 70 .02 | --- ---
Table 1.1743.b GPS week : 1743 MJD: 56445.000-56451.000
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 5 4 |
2 | 3 3 3 3 3 4 3 |
3 | 3 3 3 3 3 4 3 |
4 | 3 3 4 3 3 3 3 |
5 | 4 4 4 4 4 5 4 |
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 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 3 4 4 4 3 |
12 | 5 5 5 6 6 6 6 |
13 | 4 4 3 3 4 4 4 |
14 | 4 4 3 4 4 3 4 |
15 | 4 5 5 5 4 5 4 |
16 | 4 4 4 4 5 5 4 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 3 4 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 3 4 3 4 4 |
21 | 3 5 4 4 3 3 4 |
22 | 4 4 3 4 4 4 4 |
23 | 4 4 4 4 4 4 5 |
24 | 4 4 3 4 4 4 4 |
25 | 4 4 4 4 4 4 5 |
26 | 6 5 5 5 6 5 5 |
27 | 0 0 0 0 0 0 0 |
28 | 4 3 3 3 3 3 4 |
29 | 4 4 4 4 4 5 5 |
30 | 0 0 0 0 0 0 0 |
31 | 4 4 4 4 3 4 4 |
32 | 3 3 3 3 3 3 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1743.0 GPS week: 1743 Day: 0 MJD: 56445.000
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| 0 1 -9 37 41 -10 -.43 10 10 | -604 -1107 17 83
emr 80| 0 -1 -4 16 -27 9 .34 13 13 | 178 -1647 15 99
esa 150| 0 0 2 27 21 -3 .07 5 5 | -3046 -386 14 116
gfz 202| -1 -1 0 -68 -96 1 -.38 9 10 | 223 -1043 16 94
grg 138| 1 0 24 -11 30 25 .60 16 14 | 144 -1022 15 161
igr n/a| 0 0 -2 33 59 -40 -.11 4 4 | 1309 -1607 15 81
jpl 80| 0 1 -5 29 -38 -26 .43 13 13 | -29 -1953 15 100
mit 234| 0 0 0 -6 7 26 -.60 11 10 | 47 -896 24 202
ngs 245| 0 -1 0 -48 48 -3 .28 10 9 | -641 -1111 1861 3576
sio 405| 1 0 -6 -171 -306 62 -.36 19 16 | --- --- --- ---
Table 2.1743.1 GPS week: 1743 Day: 1 MJD: 56446.000
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| -3 2 -6 28 31 -18 -.43 10 9 | -795 -513 20 82
emr 80| 1 -1 -5 15 -25 27 .41 14 14 | -521 -598 16 97
esa 150| 0 0 1 7 36 4 .09 5 5 | -429 -1203 17 119
gfz 206| 0 -1 0 -78 -107 22 -.39 8 8 | 123 112 13 67
grg 140| 1 2 26 -8 6 -3 .62 16 15 | 74 -310 20 152
igr n/a| 0 0 -1 14 16 -32 -.17 4 4 | 562 -537 15 68
jpl 80| 0 1 -3 23 -43 -43 .43 14 13 | -1051 -778 17 104
mit 236| 0 0 0 30 8 -19 -.57 10 9 | 131 -371 24 208
ngs 248| 0 -1 -3 -13 47 -1 .30 10 8 | -774 -588 1773 3725
sio 420| 1 2 -4 -146 -340 -14 -.32 18 17 | --- --- --- ---
Table 2.1743.2 GPS week: 1743 Day: 2 MJD: 56447.000
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 2 -5 24 44 26 -.43 9 9 | -618 -1006 19 93
emr 80| 1 -2 -5 -6 -5 10 .40 13 13 | -541 -570 14 99
esa 150| 0 0 1 5 28 -11 .14 4 4 | 60 -643 15 112
gfz 206| 0 -1 0 -58 -170 34 -.42 9 9 | 413 115 17 102
grg 138| 1 1 17 -6 -20 -30 .55 16 14 | 47 -295 17 177
igr n/a| 0 0 -1 17 51 -33 -.11 3 3 | 728 -225 16 99
jpl 80| 0 0 -5 0 -6 -27 .49 13 12 | -1143 -573 15 112
mit 236| 0 0 1 2 -21 -10 -.56 8 7 | 11 -327 22 233
ngs 242| 0 0 1 34 86 -3 .37 10 8 | -654 -993 1716 3760
sio 424| 0 2 -7 -151 -276 8 -.33 18 17 | --- --- --- ---
Table 2.1743.3 GPS week: 1743 Day: 3 MJD: 56448.000
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| 0 2 -6 52 60 -21 -.38 10 10 | -839 -290 18 78
emr 80| 0 -2 -2 -14 0 15 .34 14 14 | -1087 1827 15 86
esa 150| 0 0 0 9 11 0 .15 5 5 | -138 -441 19 119
gfz 202| 0 -1 -2 -49 -83 22 -.41 9 9 | 137 635 11 62
grg 139| 2 1 20 -14 33 -8 .48 17 15 | -281 661 17 145
igr n/a| 0 0 -2 29 59 -58 -.04 4 4 | 452 1937 16 92
jpl 80| 1 0 -3 23 4 -20 .44 13 12 | -1819 1792 14 105
mit 236| -1 0 4 28 4 19 -.54 9 8 | -213 582 20 178
ngs 243| 1 -1 1 -75 -27 -25 .36 11 10 | -889 -208 1877 3624
sio 420| -1 1 -5 -75 -257 137 -.31 19 18 | --- --- --- ---
Table 2.1743.4 GPS week: 1743 Day: 4 MJD: 56449.000
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| 0 1 -5 -4 1 -5 -.45 10 10 | -898 -263 19 90
emr 80| 1 -1 -2 -31 -32 -4 .29 14 14 | -301 1442 16 106
esa 150| 0 0 2 24 -5 -2 .11 5 4 | 30 -1403 14 117
gfz 203| 0 0 -1 -26 5 8 -.43 9 8 | 283 -87 10 72
grg 139| 3 1 16 -2 30 21 .62 15 14 | 32 129 17 148
igr n/a| 0 0 -2 11 33 -29 -.11 4 4 | 1398 1710 15 66
jpl 80| 0 1 -4 8 -74 -47 .37 14 13 | -819 1539 17 116
mit 236| 0 -1 1 3 -6 -5 -.58 10 9 | -43 327 21 191
ngs 244| 0 -1 -3 -16 71 4 .38 9 8 | -917 -294 1782 3493
sio 420| -1 0 -6 -126 -240 28 -.34 19 19 | --- --- --- ---
Table 2.1743.5 GPS week: 1743 Day: 5 MJD: 56450.000
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 264| -1 1 -6 17 15 2 -.46 10 10 | -1181 -31 17 90
emr 80| -1 -2 -2 -19 -11 -13 .32 13 13 | 154 1502 17 111
esa 150| 0 0 3 15 -17 -9 .09 5 5 | -6 -2310 15 129
gfz 202| 0 0 -2 -36 -4 16 -.46 9 10 | -512 331 12 84
grg 134| 2 1 27 0 26 0 .65 16 15 | 147 -187 19 286
igr n/a| 0 0 -2 19 35 -42 -.15 4 4 | 2370 1330 14 94
jpl 80| 0 0 -8 2 -38 -52 .43 14 14 | -3 1537 18 117
mit 237| 0 0 2 -4 -38 10 -.58 11 10 | -14 271 23 263
ngs 244| 1 0 -5 -15 72 24 .39 10 8 | -1208 -61 1643 3504
sio 417| 0 2 -5 -230 -302 -94 -.32 19 18 | --- --- --- ---
Table 2.1743.6 GPS week: 1743 Day: 6 MJD: 56451.000
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 -4 -2 3 -3 -.49 9 8 | -1220 273 16 72
emr 80| 0 -3 -1 5 -23 16 .28 13 13 | 2080 -349 16 82
esa 150| 0 0 1 3 2 -11 .08 5 5 | -7 -604 16 121
gfz 199| 1 1 0 -9 -2 1 -.43 9 9 | 557 -680 15 75
grg 135| 1 1 19 -14 26 8 .64 16 16 | 151 -219 18 126
igr n/a| 0 0 -1 16 44 -19 -.13 4 4 | 3982 -758 15 64
jpl 80| 1 0 -7 1 -51 -26 .35 13 12 | 1746 -292 15 104
mit 237| 0 -1 2 0 -42 1 -.58 13 11 | 203 -116 26 212
ngs 236| 0 -1 -3 0 70 8 .40 9 7 | -1145 110 1213 3281
sio 427| -1 1 -6 -121 -268 26 -.34 24 19 | --- --- --- ---
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 3.1743.0 GPS week: 1743 Day: 0 MJD: 56445.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 5 8 13 5 17 7 14 20 3 | 39 49 50 49 64 46 56 47 43 36 47
2 | 9 9 5 7 12 4 10 10 10 18 3 | 17 19 23 24 30 20 19 25 20 20 20
3 | 9 10 5 8 11 3 11 8 10 18 3 | 24 26 22 23 20 22 25 24 29 28 23
4 | 10 8 6 9 12 3 10 10 9 27 3 | 38 40 46 47 53 42 41 44 40 38 42
5 | 11 16 4 7 15 5 14 13 8 19 4 | 23 30 19 21 28 19 30 21 21 27 19
6 | 7 9 5 10 11 4 11 9 11 13 3 | 19 23 18 18 22 18 24 19 27 23 19
7 | 11 12 5 8 17 2 12 11 12 31 4 | 34 30 27 24 38 28 32 28 32 35 27
8 | 10 8 4 9 13 2 8 11 9 10 3 | 14 17 17 19 19 16 21 19 23 14 15
9 | 8 8 5 6 11 2 10 10 6 25 2 | 18 20 20 18 21 18 23 20 23 27 18
10 | 11 8 4 8 11 3 9 9 6 12 3 | 16 24 21 23 31 19 25 22 21 21 20
11 | 12 12 4 9 13 3 9 10 11 17 3 | 25 38 34 34 51 31 41 34 29 27 33
12E | 15 20 5 12 20 5 24 13 11 17 5 | 32 29 24 28 31 25 34 26 29 26 25
13E | 8 13 4 10 20 5 10 13 9 10 3 | 24 25 22 19 40 21 28 24 26 21 22
14E | 7 11 4 12 11 5 9 14 10 16 3 | 19 24 22 21 31 19 27 26 26 25 21
15E | 11 18 4 10 16 4 17 12 12 11 4 | 26 26 23 28 29 20 28 25 26 26 23
16E | 10 18 5 13 19 3 13 12 8 16 4 | 26 28 24 27 29 25 27 29 29 27 24
17 | 11 15 6 9 17 6 16 7 6 13 4 | 20 25 19 20 32 18 27 18 22 17 18
18 | 11 13 6 9 18 4 17 12 9 19 4 | 22 23 24 25 36 22 25 27 24 19 21
19 | 8 15 3 12 16 2 14 14 10 35 4 | 16 26 20 23 31 17 27 19 26 30 19
20 | 11 15 5 9 13 4 13 10 9 14 3 | 25 27 25 26 39 25 29 26 23 19 24
21 | 9 8 6 6 10 3 10 10 12 36 3 | 20 20 23 18 24 18 20 24 22 30 19
22 | 8 14 5 7 14 3 12 10 8 16 3 | 23 25 26 26 40 25 28 29 26 23 24
23E | 8 12 4 12 19 5 13 9 10 10 3 | 31 33 31 26 38 30 38 28 38 31 30
24 | 14 12 5 9 16 4 13 9 9 14 4 | 23 29 25 21 36 24 35 24 28 25 24
25E | 10 16 5 11 17 4 14 12 13 13 4 | 22 31 23 18 31 20 32 20 25 22 22
26E | 20 19 9 10 24 10 21 12 9 26 5 | 87 90 82 78 95 88 92 81 89 88 84
X27 | 9 --- --- --- --- 53 --- --- --- --- 0 | 405 --- --- --- --- 411 --- --- --- --- 402
28E | 8 11 5 8 22 3 10 10 9 14 3 | 18 23 18 20 28 18 25 18 26 17 18
29 | 10 17 5 9 16 4 18 9 12 21 4 | 32 41 33 31 35 32 43 34 36 38 33
X30E | 9 --- --- --- --- 43 --- --- --- --- 0 | 32 --- --- --- --- 31 --- --- --- --- 33
31 | 8 14 5 9 20 5 11 6 11 17 3 | 19 26 22 21 36 21 27 18 26 19 21
32 | 11 13 4 7 14 5 9 10 7 18 3 | 24 26 19 19 28 19 28 19 24 24 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 5 9 16 4 13 11 10 19 |T 37 29 26 26 35 37 31 27 29 27 37
WRMS | 10 13 5 10 14 4 13 10 9 16 |NE 22 26 23 23 31 22 27 24 26 25 22
MEDI | 10 12 5 9 15 4 12 10 9 17 |MD 23 26 23 23 31 21 28 24 26 25 22
Table 3.1743.1 GPS week: 1743 Day: 1 MJD: 56446.000
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 9 4 8 13 5 17 8 13 18 3 | 25 32 29 29 41 27 41 28 25 20 28
2 | 9 9 4 7 11 5 9 11 6 16 3 | 14 16 16 20 19 12 20 17 14 14 14
3 | 8 12 5 7 12 5 10 8 5 16 3 | 15 23 14 14 17 11 21 15 17 18 14
4 | 9 8 4 7 12 4 9 7 7 23 2 | 32 36 35 37 43 32 40 34 33 33 34
5 | 11 18 5 7 17 3 17 12 10 17 4 | 18 27 17 22 27 16 27 20 21 22 16
6 | 7 11 4 6 11 5 10 8 7 11 2 | 12 18 12 11 18 9 21 13 17 14 11
7 | 9 11 5 7 17 5 14 9 10 32 3 | 23 28 23 26 28 23 28 25 29 37 22
8 | 8 8 4 5 11 2 9 10 6 7 2 | 12 15 12 15 12 12 20 17 20 10 12
9 | 8 8 4 6 12 2 10 8 6 22 2 | 15 18 14 17 15 13 22 16 21 21 14
10 | 9 9 4 6 12 3 8 10 8 12 3 | 14 18 15 20 23 13 22 17 16 16 14
11 | 9 11 3 8 16 3 11 7 13 14 3 | 19 33 24 21 41 21 35 23 25 20 23
12E | 14 20 6 12 24 3 20 12 13 13 5 | 19 25 20 21 32 17 28 17 24 17 18
13E | 9 12 5 10 16 4 13 10 14 7 4 | 13 21 16 20 28 16 23 18 20 15 15
14E | 7 10 5 9 15 3 9 11 10 17 3 | 15 16 16 14 22 12 18 17 22 17 14
15E | 13 17 5 10 19 4 19 10 15 10 4 | 20 19 13 22 17 12 18 16 20 16 13
16E | 11 17 4 13 20 4 12 11 8 15 4 | 19 23 19 20 27 16 23 19 20 18 17
17 | 9 16 5 10 16 3 14 6 10 13 4 | 13 20 16 15 31 11 22 12 20 10 13
18 | 7 17 6 6 15 4 17 11 8 19 3 | 19 24 16 15 28 16 24 21 20 14 15
19 | 7 17 4 10 16 4 16 13 7 30 4 | 10 25 13 15 27 11 24 14 18 23 13
20 | 11 14 4 10 14 3 13 9 9 15 3 | 18 20 13 20 27 15 22 19 16 16 14
21 | 11 12 15 9 26 8 13 10 13 35 5 | 15 21 25 16 19 12 21 18 17 27 15
22 | 7 14 5 7 15 5 13 10 10 17 3 | 18 23 17 15 31 15 26 23 20 19 16
23E | 10 17 4 11 18 4 15 10 11 12 4 | 23 34 29 27 30 26 31 27 32 29 27
24 | 13 11 6 8 14 4 12 9 10 10 3 | 20 20 18 17 24 16 25 16 22 18 16
25E | 9 14 5 6 19 4 14 12 13 12 4 | 18 27 23 14 27 18 29 17 28 21 20
26E | 15 19 8 11 16 6 20 13 12 23 5 | 72 71 74 75 76 73 71 71 74 80 72
X27 | 8 --- --- --- --- 107 --- --- --- --- 0 | 779 --- --- --- --- 819 --- --- --- --- 777
28E | 8 11 4 7 17 3 10 7 8 11 3 | 12 18 14 13 22 10 21 12 21 10 12
29 | 13 20 5 9 12 4 19 11 9 19 4 | 21 29 18 19 24 17 30 18 22 24 18
X30E | 8 --- --- --- --- 44 --- --- --- --- 0 | 36 --- --- --- --- 23 --- --- --- --- 37
31 | 6 13 4 7 16 4 12 6 12 17 3 | 10 23 13 12 32 12 22 10 22 10 13
32 | 12 10 4 10 14 4 7 7 9 17 3 | 15 20 14 17 22 12 21 14 21 18 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 8 16 4 14 10 10 18 |T 43 24 19 20 27 42 26 20 23 20 42
WRMS | 9 14 5 8 15 4 13 9 8 17 |NE 17 22 18 18 25 15 24 18 21 20 16
MEDI | 9 12 4 8 15 4 13 10 10 16 |MD 18 23 16 17 27 15 23 17 21 18 15
Table 3.1743.2 GPS week: 1743 Day: 2 MJD: 56447.000
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 8 3 9 12 3 16 6 18 16 3 | 28 36 36 32 44 32 44 32 37 25 33
2 | 10 9 4 7 12 4 9 9 11 18 3 | 17 17 19 21 18 16 16 21 21 15 17
3 | 8 11 5 8 11 4 9 6 12 14 3 | 19 22 18 19 15 17 21 17 30 21 17
4 | 11 9 3 8 16 4 9 17 8 28 4 | 48 52 51 47 55 49 51 50 55 41 49
5 | 8 14 4 12 16 3 17 10 9 17 4 | 17 22 13 16 22 13 24 17 24 20 13
6 | 6 10 5 9 11 4 10 7 11 12 3 | 14 21 14 17 16 14 21 14 25 18 13
7 | 8 13 5 8 22 4 13 9 8 33 3 | 25 26 23 24 30 21 23 24 29 38 21
8 | 10 8 4 9 16 2 8 7 4 10 3 | 10 12 10 14 16 11 14 14 21 8 9
9 | 7 8 4 7 14 2 8 6 7 21 2 | 13 15 13 13 17 12 15 15 23 21 12
10 | 8 9 3 10 12 3 11 9 7 15 3 | 17 25 23 23 28 21 25 21 29 20 21
11 | 9 11 3 6 14 3 9 8 11 14 3 | 22 32 26 23 40 24 34 25 33 21 25
12E | 15 23 6 12 24 5 22 8 11 13 5 | 27 25 19 22 29 18 26 19 30 21 19
13E | 6 12 3 7 15 4 13 8 9 9 3 | 15 23 17 17 28 16 21 18 27 18 16
14E | 8 12 3 10 12 2 9 5 7 18 3 | 22 21 20 20 25 20 22 21 29 23 20
15E | 14 18 5 9 16 3 21 7 10 12 4 | 21 21 20 23 22 18 25 22 26 21 18
16E | 6 13 6 13 19 4 10 11 10 12 4 | 20 24 20 21 31 22 23 20 32 19 20
17 | 8 15 4 10 17 3 13 7 8 13 3 | 15 22 13 15 27 13 23 12 26 12 13
18 | 6 15 5 7 14 2 14 6 9 17 3 | 20 23 18 20 27 19 22 20 27 16 18
19 | 5 15 4 11 18 3 15 10 7 29 3 | 13 24 14 14 25 13 23 14 26 22 14
20 | 7 14 4 8 11 4 12 6 10 15 3 | 20 23 19 21 26 21 23 21 29 16 19
21 | 6 10 5 8 18 3 14 7 9 33 3 | 19 17 16 15 24 19 22 17 23 30 15
22 | 7 10 5 8 15 2 14 6 11 15 3 | 23 22 21 21 31 22 23 23 28 20 20
23E | 9 12 4 11 14 3 14 8 11 11 3 | 14 19 16 18 20 15 19 17 26 19 14
24 | 10 13 4 6 18 4 12 5 8 13 3 | 26 22 20 24 26 18 26 20 25 24 19
25E | 8 16 6 9 19 3 15 8 11 15 4 | 23 33 25 23 31 23 34 21 29 24 23
26E | 15 18 7 12 21 6 20 15 11 23 5 | 47 52 50 54 53 50 50 52 48 57 49
X27 | 8 --- --- --- --- 79 --- --- --- --- 0 | 439 --- --- --- --- 451 --- --- --- --- 441
28E | 10 9 4 9 14 3 13 9 6 11 3 | 12 18 14 17 22 14 19 15 26 14 12
29 | 11 17 5 9 12 3 17 7 8 18 3 | 24 30 23 24 28 24 31 23 31 27 23
X30E | 8 --- --- --- --- 29 --- --- --- --- 0 | 30 --- --- --- --- 25 --- --- --- --- 31
31 | 13 13 4 9 22 3 14 7 11 18 4 | 19 22 18 18 36 17 23 13 31 14 16
32 | 9 10 4 9 10 3 8 7 12 17 3 | 14 19 12 14 18 11 20 12 23 18 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 4 9 16 3 13 8 10 18 |T 34 24 20 21 27 33 25 21 28 22 33
WRMS | 9 13 4 9 14 3 12 7 8 17 |NE 20 23 19 20 27 19 24 20 28 22 18
MEDI | 8 12 4 9 15 3 13 7 9 15 |MD 20 22 19 20 26 18 23 20 27 20 18
Table 3.1743.3 GPS week: 1743 Day: 3 MJD: 56448.000
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 10 4 7 12 5 17 8 16 15 4 | 29 42 38 36 51 34 45 39 38 30 37
2 | 11 7 5 12 12 5 8 10 9 17 3 | 17 18 18 24 22 17 16 23 21 17 17
3 | 9 12 3 8 13 6 11 9 10 16 3 | 25 27 22 24 18 22 23 20 32 23 22
4 | 10 7 4 9 15 6 9 7 10 25 3 | 21 30 29 27 36 27 28 29 31 26 27
5 | 12 16 5 10 15 3 18 9 10 17 4 | 22 27 19 20 24 19 29 19 24 25 19
6 | 7 10 5 7 12 4 10 9 10 14 3 | 21 23 19 20 17 19 22 18 28 19 18
7 | 9 12 4 8 23 5 11 7 12 35 3 | 24 22 19 23 30 19 22 19 27 35 19
8 | 9 8 4 6 15 3 7 7 9 15 2 | 13 17 16 20 18 14 16 19 18 18 15
9 | 7 9 5 7 15 3 9 7 8 22 3 | 18 21 19 20 21 17 21 19 25 26 18
10 | 9 7 3 8 12 3 9 7 8 11 2 | 13 20 17 16 23 15 20 18 23 17 16
11 | 11 12 3 8 15 5 13 9 13 15 3 | 25 37 27 24 43 28 35 30 31 23 27
12E | 11 26 6 13 24 5 19 11 13 15 5 | 21 28 21 21 29 17 27 21 19 22 19
13E | 8 10 5 10 14 4 12 7 6 11 3 | 19 24 21 17 30 19 25 22 25 22 19
14E | 8 12 4 8 17 4 10 11 13 15 3 | 26 25 25 25 31 26 26 25 27 22 24
15E | 11 19 5 12 26 5 19 9 13 19 5 | 23 26 20 25 24 19 25 24 26 20 20
16E | 9 13 4 11 18 4 10 12 11 13 3 | 24 28 27 28 29 25 28 26 32 25 25
17 | 9 13 5 10 17 5 15 6 7 13 3 | 17 22 16 19 29 18 22 17 24 17 16
18 | 7 14 6 8 15 4 18 6 12 17 3 | 20 23 19 21 27 20 24 20 19 13 17
19 | 7 12 3 9 17 4 14 11 12 29 3 | 16 24 18 19 25 17 24 17 26 20 17
20 | 9 14 6 12 18 3 11 7 10 16 3 | 19 25 20 23 30 21 24 22 25 16 20
21 | 9 24 7 7 19 7 10 5 13 33 4 | 19 31 23 18 24 17 17 18 17 28 17
22 | 6 12 6 9 15 3 13 6 11 16 3 | 23 24 23 24 32 22 23 24 22 18 21
23E | 10 12 5 12 19 4 12 8 10 15 3 | 26 31 30 29 31 29 31 28 37 30 29
24 | 11 13 5 7 18 4 10 10 9 12 3 | 24 27 25 24 33 25 30 26 28 24 24
25E | 9 14 5 6 17 3 12 8 11 20 3 | 23 27 22 20 26 21 29 19 26 20 21
26E | 17 20 8 11 14 7 16 17 11 24 5 | 70 74 71 69 76 71 69 71 77 75 71
X27 | 8 --- --- --- --- 50 --- --- --- --- 0 | 602 --- --- --- --- 616 --- --- --- --- 601
28E | 9 10 4 9 18 3 8 6 8 10 3 | 16 19 16 17 27 16 21 15 24 18 16
29 | 12 18 5 10 12 4 18 8 13 17 4 | 23 31 26 24 27 26 32 23 33 29 25
X30E | 8 --- --- --- --- 61 --- --- --- --- 0 | 46 --- --- --- --- 25 --- --- --- --- 47
31 | 10 14 6 8 22 5 13 8 18 15 4 | 20 22 19 20 36 19 23 15 26 14 17
32 | 6 9 4 10 14 4 8 7 10 15 3 | 18 21 15 18 20 16 21 14 23 20 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 9 17 4 13 9 11 19 |T 41 27 23 23 29 41 26 23 27 23 41
WRMS | 10 14 5 9 15 4 12 8 10 18 |NE 19 24 20 21 27 19 22 20 24 22 19
MEDI | 9 12 5 9 15 4 11 8 10 15 |MD 21 25 20 21 27 19 24 20 26 22 19
Table 3.1743.4 GPS week: 1743 Day: 4 MJD: 56449.000
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 8 4 7 12 3 15 7 14 17 3 | 35 41 39 37 46 35 49 37 31 30 37
2 | 5 8 5 8 10 4 12 12 9 17 3 | 20 20 24 23 23 18 23 24 19 20 20
3 | 11 14 3 9 11 4 13 7 8 16 3 | 18 27 21 23 20 19 26 22 25 23 20
4 | 7 9 4 8 15 4 10 8 7 26 3 | 29 34 34 28 38 28 35 29 30 28 31
5 | 12 17 4 10 16 3 17 11 9 16 4 | 27 36 24 25 31 24 33 24 26 32 24
6 | 9 10 4 7 10 4 12 8 7 12 3 | 18 25 20 19 21 16 23 19 23 20 18
7 | 9 11 4 7 17 5 15 10 9 38 3 | 24 25 21 18 31 18 25 19 24 34 19
8 | 10 8 3 7 12 3 9 9 6 16 3 | 15 19 17 15 21 15 22 19 20 19 16
9 | 7 8 4 7 12 3 10 6 7 23 2 | 16 21 20 17 21 16 25 17 20 25 17
10 | 10 7 4 7 11 4 9 8 10 12 3 | 15 21 20 15 23 15 21 18 18 21 17
11 | 10 13 4 9 13 3 12 12 11 17 3 | 30 42 34 31 43 30 45 34 29 30 33
12E | 12 29 7 13 25 4 22 11 10 12 5 | 26 34 21 22 35 20 34 23 22 22 21
13E | 9 14 4 10 12 3 13 10 8 13 3 | 18 24 20 19 27 17 24 21 23 19 18
14E | 8 12 4 9 16 4 12 9 11 18 3 | 24 23 22 22 28 19 23 21 27 25 20
15E | 7 17 5 8 18 3 21 10 9 18 4 | 22 25 20 21 23 18 24 22 23 26 19
16E | 12 18 5 14 16 3 11 14 10 13 4 | 18 24 19 20 26 17 22 19 26 18 17
17 | 11 13 4 8 17 3 12 5 10 15 3 | 23 23 20 19 32 17 26 19 23 17 19
18 | 11 18 6 9 15 4 17 9 6 18 4 | 20 24 17 22 27 16 25 17 16 17 16
19 | 10 15 5 12 15 3 15 12 5 29 4 | 14 27 20 19 28 16 26 19 21 25 18
20 | 10 15 4 10 14 3 10 4 7 15 3 | 18 24 18 19 26 17 25 19 21 15 18
21 | 9 10 4 6 11 3 11 10 10 35 3 | 18 24 21 20 26 17 23 17 19 34 19
22 | 8 16 5 7 13 4 15 7 6 15 3 | 20 24 21 21 30 18 24 20 20 18 19
23E | 9 13 4 11 17 3 13 8 8 15 3 | 20 24 24 20 25 22 29 18 29 23 21
24 | 13 13 4 6 17 4 12 8 8 13 3 | 21 24 19 19 29 16 27 21 23 22 19
25E | 11 14 5 4 12 3 12 10 10 21 3 | 33 39 36 33 40 34 44 37 36 45 35
26E | 14 18 6 15 21 4 19 20 13 23 5 | 35 43 37 36 45 34 44 37 37 42 36
X27 | 7 --- --- --- --- 59 --- --- --- --- 0 | 325 --- --- --- --- 352 --- --- --- --- 323
28E | 8 10 3 8 17 3 8 10 8 20 3 | 17 25 21 18 25 19 25 22 24 25 19
29 | 10 18 6 8 15 4 17 13 10 18 4 | 26 33 29 24 31 27 34 26 28 32 26
X30E | 7 --- --- --- --- 43 --- --- --- --- 0 | 46 --- --- --- --- 32 --- --- --- --- 46
31 | 9 14 5 5 15 3 12 8 9 15 3 | 18 24 20 18 34 17 25 19 26 15 19
32 | 10 8 4 8 12 3 9 7 10 15 3 | 17 19 17 15 20 13 23 13 19 20 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 9 15 4 14 10 9 19 |T 32 27 23 21 29 31 28 22 24 24 31
WRMS | 10 14 4 8 14 4 13 9 8 19 |NE 20 25 21 19 28 18 26 20 22 24 19
MEDI | 10 13 4 8 15 3 12 9 9 16 |MD 20 24 21 20 27 18 25 20 23 23 19
Table 3.1743.5 GPS week: 1743 Day: 5 MJD: 56450.000
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 | 17 10 5 7 12 4 18 6 17 20 4 | 17 35 30 26 41 24 37 28 24 22 26
2 | 6 9 6 9 12 2 11 11 11 17 3 | 17 14 14 17 18 11 13 20 14 19 12
3 | 9 11 5 9 12 4 12 10 9 16 3 | 17 19 14 20 18 14 21 19 23 19 15
4 | 8 7 4 8 13 4 10 10 9 27 3 | 20 26 26 20 34 19 25 21 23 23 22
5 | 11 15 6 12 17 4 19 8 13 17 4 | 21 30 22 21 26 20 32 23 25 30 22
6 | 8 9 4 8 11 4 11 11 11 14 3 | 16 17 13 17 20 11 20 18 21 16 13
7 | 10 11 5 12 19 6 15 10 10 39 4 | 21 28 23 28 29 23 28 29 27 45 24
8 | 11 9 5 11 13 4 9 14 6 18 3 | 11 18 14 15 17 13 18 18 17 14 12
9 | 10 8 6 9 11 3 10 11 7 24 3 | 16 19 17 16 16 14 20 18 17 22 15
10 | 7 7 4 10 14 3 13 9 7 12 3 | 11 17 14 13 22 11 16 16 15 18 13
11 | 11 12 4 8 13 4 10 7 11 15 3 | 21 33 25 23 39 23 31 24 25 21 24
12E | 10 29 7 13 23 5 24 9 12 11 5 | 17 28 18 18 29 13 27 17 20 18 16
13E | 12 13 4 9 13 3 14 8 8 11 3 | 20 19 15 17 25 13 20 15 19 17 15
14E | 9 11 4 8 14 4 10 9 9 20 3 | 23 23 24 22 28 22 27 24 25 25 23
15E | 10 16 4 11 24 5 20 10 10 18 4 | 24 21 21 24 23 19 23 23 23 25 20
16E | 11 16 5 14 22 5 12 15 9 12 4 | 19 25 19 18 35 17 21 20 25 18 18
17 | 9 17 5 10 19 3 19 7 9 16 4 | 18 21 14 18 29 14 24 18 21 19 15
18 | 7 15 6 9 19 4 18 7 6 18 4 | 18 22 16 22 32 17 22 17 16 15 15
19 | 8 14 4 10 15 5 18 13 10 29 4 | 10 20 13 14 29 11 24 12 22 21 13
20 | 8 12 5 9 12 5 13 9 12 16 3 | 16 21 16 14 27 15 21 18 21 16 15
21 | 7 10 5 7 17 5 12 7 8 35 3 | 13 15 17 14 23 11 15 14 15 29 13
22 | 7 13 5 7 18 3 13 8 6 17 3 | 19 22 18 21 35 19 21 18 20 18 18
23E | 11 14 4 10 17 4 12 10 8 15 3 | 26 27 24 25 29 24 25 26 28 27 24
24 | 14 11 6 7 12 5 14 14 8 12 4 | 31 28 27 26 30 26 32 29 27 30 26
25E | 14 17 7 6 18 5 14 10 11 11 4 | 37 41 40 34 41 36 40 32 44 39 37
26E | 12 16 7 12 16 5 15 17 8 23 4 | 70 67 67 66 66 67 69 73 69 73 68
X27 | 8 --- --- --- --- 48 --- --- --- --- 0 | 463 --- --- --- --- 471 --- --- --- --- 463
28E | 10 9 4 8 17 3 11 5 8 10 3 | 24 26 22 23 31 22 27 24 27 23 22
29 | 9 18 6 11 15 4 19 18 8 20 4 | 28 30 23 26 25 22 30 32 26 32 24
X30E | 8 --- --- --- --- 54 --- --- --- --- 0 | 31 --- --- --- --- 21 --- --- --- --- 31
31 | 8 13 4 6 15 4 12 10 10 14 3 | 16 20 14 14 29 14 21 13 21 14 14
32 | 9 9 4 8 14 3 9 10 10 16 3 | 12 19 14 12 21 11 19 10 21 18 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 5 9 16 4 14 11 10 19 |T 35 25 21 21 28 33 25 22 24 24 34
WRMS | 10 13 5 10 15 4 14 10 8 18 |NE 17 21 18 18 25 16 22 19 20 23 17
MEDI | 9 12 5 9 15 4 13 10 9 16 |MD 19 22 18 20 29 17 23 19 22 21 18
Table 3.1743.6 GPS week: 1743 Day: 6 MJD: 56451.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1M | 11 8 3 9 13 4 16 9 12 25 3 | 36 48 48 46 61 43 55 48 40 40 45
2M | 7 7 4 10 10 2 9 11 8 19 3 | 22 20 23 27 26 20 21 28 22 26 21
3 | 7 9 4 7 13 4 11 11 8 18 3 | 18 24 18 21 18 18 25 25 27 24 18
4 | 7 8 4 8 13 2 8 10 6 31 2 | 27 32 35 33 44 30 34 34 32 37 32
5 | 8 12 4 8 14 3 13 10 7 18 3 | 28 34 25 26 28 25 37 26 28 35 26
6M | 7 9 5 6 13 4 9 10 7 15 3 | 20 28 24 23 25 22 26 21 28 25 22
7 | 8 10 4 8 18 5 12 10 10 41 3 | 23 23 19 21 29 19 24 21 25 39 19
8 | 8 8 4 5 12 3 10 14 7 19 3 | 14 19 18 17 17 16 22 24 21 21 16
9 | 7 8 5 5 12 2 9 12 6 25 2 | 17 20 21 18 18 17 23 21 24 27 18
10 | 7 6 4 10 12 2 6 10 5 16 2 | 17 21 20 19 28 17 25 22 22 22 19
11M | 8 11 3 8 15 3 11 6 8 15 3 | 27 36 31 29 48 28 37 32 26 25 30
12E | 10 26 6 15 21 5 20 12 10 12 5 | 19 28 17 20 27 15 25 18 18 17 16
13E | 8 11 5 9 12 2 12 19 8 12 3 | 21 26 20 19 31 19 26 26 26 21 20
14E | 8 10 4 6 19 4 10 10 9 16 3 | 18 23 19 16 27 18 25 20 25 23 18
15E | 12 17 5 6 13 2 18 12 12 23 4 | 25 22 22 21 24 19 23 25 26 26 20
16E | 10 17 6 13 19 4 13 12 8 13 4 | 16 25 21 19 30 17 25 18 22 19 18
17 | 6 13 5 9 16 4 15 10 9 19 3 | 19 20 18 21 33 18 23 22 24 22 18
18M | 9 17 7 8 16 4 15 13 6 24 4 | 24 27 24 25 32 22 24 25 22 23 21
19M | 6 14 5 10 19 5 16 20 7 37 4 | 16 27 21 18 34 18 27 25 27 26 20
20M | 8 13 4 10 13 3 11 13 10 16 3 | 20 25 22 24 36 21 25 25 23 18 21
21 | 7 10 8 7 16 5 14 11 12 35 3 | 18 22 22 18 32 17 21 20 21 33 18
22 | 8 13 6 8 15 3 12 10 9 17 3 | 21 26 24 25 37 22 26 24 19 19 22
23E | 11 12 4 11 32 3 14 15 7 18 4 | 25 26 26 25 29 22 28 22 26 28 23
24 | 10 12 5 8 16 3 13 9 9 11 3 | 20 23 19 17 24 17 24 20 19 19 17
25 | 9 17 6 7 15 6 15 18 13 57 4 | 98 100 98 95 99 92 100 102 90 116 96
26E | 11 17 5 11 15 4 16 20 8 21 4 | 76 75 76 72 74 74 73 76 74 78 74
X27M | 8 --- --- --- --- 55 --- --- --- --- 0 | 464 --- --- --- --- 481 --- --- --- --- 466
28E | 7 9 4 5 14 3 14 21 8 29 3 | 16 24 20 19 29 18 25 28 26 30 19
29M | 10 13 5 8 12 4 16 23 12 20 4 | 57 59 54 51 54 53 58 56 57 67 54
X30 | 8 --- --- --- --- 60 --- --- --- --- 0 | 34 --- --- --- --- 21 --- --- --- --- 35
31 | 11 13 5 6 18 5 11 9 8 16 3 | 18 22 18 18 34 18 23 18 26 15 18
32M | 10 9 5 7 14 4 9 14 10 18 3 | 17 22 18 15 27 14 23 17 23 23 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 5 9 16 4 13 13 9 24 |T 40 30 28 27 35 39 31 29 29 31 40
WRMS | 8 13 5 9 16 4 12 11 7 19 |NE 20 23 21 21 28 19 25 23 24 26 20
MEDI | 8 11 5 8 14 4 12 11 8 18 |MD 20 25 21 21 29 19 25 24 25 25 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 4.1743 GPS week: 1743 MJD: 56445.0-56451.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 |U 7 5 15 |U 9 11 38 |U 8 7 20 |
emr | emr 2876 | 8 6 20 |U 12 25 40 | 9 9 26 |
esa | esa 2880 | 6 5 16 |U 8 13 39 | 8 7 21 |
gfz | gfz 2876 |U 6 5 16 |U 9 10 38 |U 8 6 20 |
grg | grg 2879 |U 14 13 35 |U 13 20 58 | 14 13 34 |
igr | igr 2877 | 6 5 16 | 8 10 29 | 8 7 20 |
igs | igs 2860 | 6 5 16 | 8 14 40 | 8 7 22 |
jpl | jpl 2876 | 7 6 19 | 10 24 39 | 9 9 27 |
mit | mit 2880 | 6 5 17 |U 9 23 42 |U 9 8 24 |
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 5.1743.0 GPS week: 1743 Day: 0 MJD: 56445.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 | 5 5 12 | 4 7 17 | 6 7 18 |
emr | emr 2878 | 6 7 17 | 7 21 23 | 6 8 27 |
esa | esa 2880 | 4 4 13 | 4 6 17 | 7 8 18 |
gfz | gfz 2876 | 5 5 14 | 6 7 24 | 7 8 18 |
grg | grg 2880 | 13 11 31 | 10 16 44 | 15 8 38 |
igr | igr 2880 | 5 5 14 | 4 6 17 | 6 7 19 |
igs | igs 2880 | 5 5 13 | 5 6 16 | 6 7 19 |
jpl | jpl 2877 | 6 6 16 | 6 11 21 | 7 9 26 |
mit | mit 2880 | 5 6 16 | 5 25 29 | 7 8 27 |
Table 5.1743.1 GPS week: 1743 Day: 1 MJD: 56446.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 5 4 11 | 6 11 23 | 7 8 17 |
emr | emr 2876 | 6 6 15 | 8 22 27 | 9 10 23 |
esa | esa 2880 | 4 5 11 | 6 10 19 | 7 9 18 |
gfz | gfz 2876 | 5 4 13 | 6 10 22 | 7 7 17 |
grg | grg 2880 | 9 9 29 | 11 24 54 | 12 18 40 |
igr | igr 2880 | 4 4 12 | 5 8 19 | 6 7 18 |
igs | igs 2842 | 4 4 11 | 6 10 22 | 7 8 18 |
jpl | jpl 2876 | 6 7 11 | 8 23 27 | 8 8 23 |
mit | mit 2880 | 4 4 12 | 6 24 27 | 9 10 25 |
Table 5.1743.2 GPS week: 1743 Day: 2 MJD: 56447.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 4 4 14 | 7 6 29 | 7 8 21 |
emr | emr 2876 | 7 5 18 | 9 25 25 | 9 9 27 |
esa | esa 2880 | 4 5 12 | 7 8 23 | 8 7 20 |
gfz | gfz 2877 | 4 3 13 | 6 7 25 | 8 7 19 |
grg | grg 2875 | 10 10 16 | 11 19 47 | 11 10 21 |
igr | igr 2879 | 5 4 12 | 6 8 21 | 8 7 20 |
igs | igs 2835 | 5 3 12 | 7 6 26 | 8 8 26 |
jpl | jpl 2876 | 7 5 15 | 9 31 29 | 9 10 30 |
mit | mit 2880 | 5 4 12 | 8 25 25 | 9 7 24 |
Table 5.1743.3 GPS week: 1743 Day: 3 MJD: 56448.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 5 4 14 | 7 7 32 | 9 8 26 |
emr | emr 2876 | 8 5 18 | 11 21 34 | 11 10 32 |
esa | esa 2880 | 6 4 15 | 6 7 28 | 9 7 28 |
gfz | gfz 2876 | 6 4 15 | 6 7 27 | 9 7 28 |
grg | grg 2880 | 11 12 30 | 14 20 59 | 16 9 33 |
igr | igr 2860 | 6 4 15 | 6 7 26 | 9 7 28 |
igs | igs 2835 | 6 3 14 | 7 6 28 | 8 7 29 |
jpl | jpl 2875 | 7 4 16 | 8 26 37 | 10 8 33 |
mit | mit 2880 | 6 4 14 | 8 23 36 | 8 8 26 |
Table 5.1743.4 GPS week: 1743 Day: 4 MJD: 56449.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 13 10 21 | 8 8 27 | 8 4 15 |
emr | emr 2876 | 10 8 24 | 10 24 35 | 11 8 20 |
esa | esa 2880 | 8 7 20 | 8 8 23 | 8 4 14 |
gfz | gfz 2876 | 8 7 21 | 8 10 27 | 8 4 13 |
grg | grg 2880 | 14 12 26 | 13 18 57 | 11 9 33 |
igr | igr 2880 | 8 6 19 | 7 8 23 | 7 4 14 |
igs | igs 2878 | 8 6 20 | 8 23 36 | 8 4 14 |
jpl | jpl 2876 | 9 7 26 | 8 22 36 | 11 11 25 |
mit | mit 2880 | 8 7 20 | 7 22 34 | 8 6 17 |
Table 5.1743.5 GPS week: 1743 Day: 5 MJD: 56450.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3011 | 8 7 18 | 26 29 105 | 10 8 24 |
emr | emr 2876 | 9 7 29 | 31 42 109 | 12 11 29 |
esa | esa 2880 | 7 6 20 | 21 45 144 | 11 9 25 |
gfz | gfz 2876 | 8 6 20 | 22 17 119 | 10 8 25 |
grg | grg 2880 | 35 34 98 | 22 22 96 | 22 27 43 |
igr | igr 2880 | 7 6 19 | 21 28 75 | 10 9 26 |
igs | igs 2879 | 7 6 20 | 16 27 118 | 10 10 25 |
jpl | jpl 2876 | 7 7 25 | 17 26 88 | 11 10 31 |
mit | mit 2880 | 8 7 20 | 20 24 110 | 11 11 21 |
Table 5.1743.6 GPS week: 1743 Day: 6 MJD: 56451.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 7 4 16 | 7 9 31 | 8 6 21 |
emr | emr 2876 | 11 7 22 | 11 19 29 | 9 9 25 |
esa | esa 2880 | 8 6 21 | 6 8 23 | 7 6 21 |
gfz | gfz 2876 | 7 6 18 | 6 11 26 | 7 5 21 |
grg | grg 2880 | 8 5 18 | 10 18 48 | 12 9 29 |
igr | igr 2880 | 8 6 20 | 6 8 23 | 7 6 20 |
igs | igs 2876 | 8 6 20 | 7 21 31 | 8 7 22 |
jpl | jpl 2876 | 9 8 23 | 11 32 37 | 9 9 22 |
mit | mit 2880 | 8 5 21 | 7 21 33 | 11 9 26 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1743 GPS week: 1743 MJD: 56445.500-56451.500
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 | -51 -20 -40 -165 2 | 3 22
| 15 15 41 90 3 | 2
emr uuuuu | 26 17 52 178 -8 | 34 39
| 18 21 35 76 9 | 2
esa uuuuu | -4 -12 52 -39 0 | 17 26
| 11 9 26 42 4 | 2
gfz uuuuu | 15 27 -70 -32 -2 | 9 22
| 17 14 39 49 2 | 3
grg uuuux | 19 -3 22 -15 16 | -10 41
| 14 5 37 56 34 | 5
igr xxxxx | -33 -11 9 53 3 | -3 20
| 14 9 37 33 5 | 1
irf xxxxx | 13 6 -39 0 -2 | 3 20
| 5 8 28 16 3 | 2
jpl uuuuu | 50 -25 17 94 -1 | 34 40
| 25 15 76 59 11 | 3
mit uuuuu | 12 2 -105 50 -3 | 16 25
| 14 16 72 66 5 | 3
ngs uuuuu | -28 26 30 48 3 | 8 18
| 62 40 100 72 5 | 1
sio xxxxx | 274 165 76 158 -6 | 34 39
| 60 37 105 51 4 | 4
Table 7.1743.0 GPS week: 1743 Day: 0 MJD: 56445.500
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 | -65 -22 -46 -195 4 | 2 24
emr uuuuu | 25 -8 75 161 -10 | 34 40
esa uuuuu | -14 -10 66 -38 -6 | 17 28
gfz uuuuu | 31 19 -65 52 -1 | 9 26
grg uuuux | 11 -7 37 42 16 | -7 40
igr xxxxx | -49 -18 -9 19 -2 | -4 23
irf xxxxx | 14 -5 -22 -29 2 | 2 23
jpl uuuuu | 64 -44 115 187 9 | 29 37
mit uuuuu | 10 -15 -95 -58 4 | 14 27
ngs uuuuu | -17 72 -118 -14 -1 | 7 20
sio xxxxx | 343 172 123 117 -3 | 34 42
Table 7.1743.1 GPS week: 1743 Day: 1 MJD: 56446.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -48 -26 -36 -150 1 | 6 24
emr uuuuu | 61 1 78 318 8 | 36 41
esa uuuuu | -25 -10 19 -25 -3 | 20 29
gfz uuuuu | 2 41 -8 -43 -2 | 13 26
grg uuuux | 34 -11 -29 0 33 | -4 41
igr xxxxx | -10 -5 28 9 -1 | -1 22
irf xxxxx | 21 -2 -12 -12 -4 | 6 22
jpl uuuuu | 46 -45 45 102 7 | 34 40
mit uuuuu | 31 -8 -85 -33 -6 | 19 28
ngs uuuuu | -20 44 17 -10 1 | 10 20
sio xxxxx | 377 179 54 106 -10 | 38 44
Table 7.1743.2 GPS week: 1743 Day: 2 MJD: 56447.500
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 | -41 -14 15 -43 0 | 4 22
emr uuuuu | 16 43 70 192 -4 | 35 40
esa uuuuu | 0 -2 18 -85 4 | 17 26
gfz uuuuu | 8 7 -58 -48 -1 | 11 23
grg uuuux | 36 5 49 58 -16 | -5 40
igr xxxxx | -38 -9 -49 66 4 | -3 20
irf xxxxx | 15 1 -17 11 1 | 4 20
jpl uuuuu | 32 -6 66 88 8 | 34 40
mit uuuuu | 10 -17 -41 74 0 | 17 26
ngs uuuuu | -34 1 -70 -19 -1 | 9 18
sio xxxxx | 262 156 159 197 -8 | 36 42
Table 7.1743.3 GPS week: 1743 Day: 3 MJD: 56448.500
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 | -77 -49 -118 -93 7 | 5 22
emr uuuuu | 3 11 71 201 -6 | 36 41
esa uuuuu | 3 -13 49 -96 6 | 19 26
gfz uuuuu | -3 19 -56 -79 -5 | 11 23
grg uuuux | 2 -1 -30 -23 -38 | -11 39
igr xxxxx | -50 -21 -8 91 11 | -2 19
irf xxxxx | 15 7 -37 2 -3 | 5 19
jpl uuuuu | 5 -32 -101 22 -2 | 37 42
mit uuuuu | -12 7 -28 101 -2 | 19 26
ngs uuuuu | 99 79 167 143 -2 | 9 19
sio xxxxx | 229 106 183 222 -7 | 37 42
Table 7.1743.4 GPS week: 1743 Day: 4 MJD: 56449.500
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 | -39 -3 -28 -192 1 | 4 21
emr uuuuu | 30 45 44 172 -15 | 35 39
esa uuuuu | 2 -29 77 -35 -1 | 18 25
gfz uuuuu | 0 28 -98 -92 -1 | 9 21
grg uuuux | 18 -1 26 -94 26 | -16 42
igr xxxxx | -27 6 4 29 9 | -2 19
irf xxxxx | 14 9 -28 -4 -8 | 3 17
jpl uuuuu | 78 -19 -70 112 -16 | 36 41
mit uuuuu | 22 19 -94 79 -11 | 16 23
ngs uuuuu | -69 10 35 129 11 | 8 16
sio xxxxx | 234 164 126 179 -12 | 34 38
Table 7.1743.5 GPS week: 1743 Day: 5 MJD: 56450.500
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 -19 -52 -328 1 | 1 21
emr uuuuu | 26 21 -21 134 -10 | 30 36
esa uuuuu | 1 -14 53 -22 -1 | 15 23
gfz uuuuu | 31 49 -69 -11 -4 | 5 20
grg uuuux | 29 -3 58 -14 65 | -16 42
igr xxxxx | -23 -16 65 79 1 | -4 19
irf xxxxx | 9 15 -65 19 0 | -1 18
jpl uuuuu | 61 -20 24 124 4 | 33 39
mit uuuuu | 5 9 -155 95 -2 | 12 22
ngs uuuuu | -67 -7 116 99 5 | 6 16
sio xxxxx | 239 230 9 187 -4 | 29 34
Table 7.1743.6 GPS week: 1743 Day: 6 MJD: 56451.500
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 | -38 -5 -13 -158 0 | 3 19
emr uuuuu | 21 3 45 69 -18 | 31 37
esa uuuuu | 5 -6 79 29 -1 | 16 24
gfz uuuuu | 37 28 -134 -4 1 | 6 19
grg uuuux | 4 -6 45 -73 29 | -10 43
igr xxxxx | -34 -17 33 74 2 | -3 18
irf xxxxx | 6 14 -90 8 -2 | 0 17
jpl uuuuu | 65 -11 37 19 -17 | 34 40
mit uuuuu | 21 22 -240 89 -3 | 13 22
ngs uuuuu | -87 -20 66 8 7 | 8 15
sio xxxxx | 236 147 -119 93 1 | 29 34
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