[IGSREPORT-21423] Wk 1712 IGS Final Orbits [Resubmission]
IGS ACC
igs.acc at noaa.gov
Mon Dec 17 08:05:40 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1712 (Oct 28, 2012 - Nov 03, 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:
igs1712[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1712[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1712[0-6].cls IGS GPS clock combination summary report.
igs17127.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17127.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 | KOUC KOUC
0 | EMR | 32 32
0 | ESA | AREQ
0 | GFZ | 32 ARTU BOGT LHAZ POLV RESO SOFI YELL
0 | GRG | MCM4 SOFI YEBE BARH MCM4 NTUS SOFI YEBE
0 | JPL | 21 32
0 | MIT | 16 21 22 32 16 21 22 24 32 AREQ NTUS SOFI GMAS NICO
0 | MIT | NTUS SOFI
1 | COD | HERT MATE HERT MATE
1 | EMR | 32 32 WUHN
1 | ESA | AREQ
1 | GFZ | BOGT BOR1 CHPI MCM4 PALM POLV SFER WSRT
1 | GRG | 13 13 NOVM
1 | JPL | 21 REUN
1 | MIT | 24 32 24 32 GMAS
2 | COD | 32 32 KOUC KOUC
2 | EMR | HERS HERS
2 | ESA | 32 32
2 | GFZ | ARTU BOGT LHAZ LPGS
2 | GRG | HYDE LPGS HYDE LPGS
2 | JPL | PIMO
2 | MIT | GMAS JPLM
3 | ALL | 13
3 | COD | 32 32 KOUC KOSG KOUC SUTM
3 | EMR | THTI
3 | ESA | 32 32 AREQ
3 | GFZ | BOGT METS POLV SFER
3 | GRG | 13 HYDE HYDE LHAZ RAMO
3 | JPL | 30
4 | COD | 18 22 30 32 18 22 32 KOUC MATE MOBS ALRT FLRS KOUC
4 | COD | MATE MOBS
4 | EMR | 30
4 | ESA | 30 32 32 FLIN TIXI
4 | GFZ | BOGT
4 | GRG | 30 ALRT MAC1 USNO XMIS MAL2 MATE USNO XMIS
4 | JPL | 30
4 | MIT | 5 24 5 24 30 MAC1 NTUS
5 | COD | 30 32 30 32 ALIC KOUC ALIC FLRS KOUC
5 | EMR | CHUR
5 | ESA | 30 32 30 32 CHUR AREQ
5 | GFZ | ASPA HOFN LHAZ POLV YAKT
5 | GRG | WSRT ADIS THTI WSRT
5 | JPL | 10
5 | MIT | 2 10 21 2 10 21 24 GMAS
6 | COD | 30 32 10 30 32 KOUC AREQ KOUC
6 | ESA | 10 30 32 10 30 32 MATE MATE
6 | GFZ | 10 30 ABPO KERG LHAZ MAC1 SUTM
6 | GRG | SOFI WSRT ADIS AREQ KOUC SOFI WSRT
6 | JPL | MAC1
6 | MIT | 19 22 19 22 MAC1 GMAS MAC1
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 G30 | | | | 1 | | | |
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 | .3 1.2 -.7 -44 -5 -9 -.08
EMR | 0 | 2.1 6.1 5.3 1 10 8 .22
ESA | 0 | 5.8 3.9 -9.2 108 -237 126 -.12
GFZ | 0 | -.4 .7 -.3 -40 -44 -18 .0
GRG | 0 | 1.8 1.3 -4.4 -23 47 -72 .14
JPL | 0 | .0 -.6 10.4 -38 1 24 .03
MIT | 0 | 6.1 7.2 4.5 -7 5 -34 .09
NGS | 0 | 5.8 -2.4 6.0 -41 -21 40 .26
SIO | 0 | 3.1 1.9 -15.8 38 -137 -109 .11
COD | 1 | .2 1.1 .5 -25 17 -22 -.40
EMR | 1 | 8.9 11.0 8.5 -3 7 -3 -.04
ESA | 1 | 9.1 8.4 -17.4 200 -352 106 -.22
GFZ | 1 | .2 .8 .0 -31 -52 -30 -.09
GRG | 1 | 5.5 7.0 4.7 -36 24 -49 -.02
JPL | 1 | 6.5 7.9 12.8 -42 22 -16 -.31
MIT | 1 | 12.5 6.3 5.6 -9 0 -22 -.02
NGS | 1 | 9.0 -.2 6.5 -38 -43 69 .05
SIO | 1 | 2.6 4.9 -13.4 34 -74 -243 -.08
COD | 2 | 1.1 1.8 .2 -42 -5 -24 -.24
EMR | 2 | 3.4 9.4 6.8 3 0 1 .09
ESA | 2 | 8.4 6.6 -14.2 171 -305 126 -.25
GFZ | 2 | .6 .8 -.5 -28 -50 -22 -.20
GRG | 2 | -1.4 -1.1 1.2 -32 27 -50 .34
JPL | 2 | 2.0 10.3 11.9 -38 6 -39 -.08
MIT | 2 | 6.2 8.3 2.4 -5 3 -28 .0
NGS | 2 | 11.4 1.0 6.3 -29 -41 82 .18
SIO | 2 | 4.7 2.3 -20.1 62 -177 -96 -.01
COD | 3 | 1.0 .9 -.4 -40 -16 -1 -.25
EMR | 3 | 5.7 10.7 4.3 -5 -2 0 .04
ESA | 3 | 11.7 6.8 -16.6 191 -388 128 -.24
GFZ | 3 | .4 1.0 -.8 4 -69 -19 -.18
GRG | 3 | .5 -1.6 -2.5 -16 52 -56 .24
JPL | 3 | 6.1 5.7 8.6 -77 42 -1 .02
MIT | 3 | 6.8 9.6 1.3 -7 2 -30 .01
NGS | 3 | 2.8 5.1 .4 5 -11 30 .23
SIO | 3 | 2.7 3.8 -23.0 41 -175 -192 -.15
COD | 4 | .7 1.3 -.8 -35 6 -14 -.18
EMR | 4 | 5.5 11.9 .4 10 15 5 .0
ESA | 4 | 10.5 7.9 -19.0 242 -369 121 .03
GFZ | 4 | 1.1 .8 .9 -21 -79 -29 -.12
GRG | 4 | 1.9 .2 -.4 -5 50 -31 .17
JPL | 4 | -1.5 8.0 7.4 -65 26 -13 .34
MIT | 4 | 7.0 11.1 -2.9 -6 2 -26 .06
NGS | 4 | 3.8 2.2 -.2 5 -17 29 .30
SIO | 4 | 4.7 4.5 -31.4 29 -261 -262 -.03
COD | 5 | .7 .5 .3 -51 12 -23 -.12
EMR | 5 | 3.9 12.9 -1.6 -1 14 4 .21
ESA | 5 | 7.6 4.1 -18.8 172 -314 128 .24
GFZ | 5 | 1.1 .0 .0 -28 -56 -12 .03
GRG | 5 | 3.5 1.5 6.5 -16 35 -34 .20
JPL | 5 | -1.6 4.9 4.5 -24 19 -41 .09
MIT | 5 | 7.8 7.5 .7 0 -2 -28 .18
NGS | 5 | 1.6 2.1 -.4 -2 -8 24 .32
SIO | 5 | 1.5 4.2 -45.9 92 -252 -183 .21
COD | 6 | .9 .8 .2 -41 1 -25 -.19
EMR | 6 | 7.3 5.6 -5.7 13 12 -11 .22
ESA | 6 | 7.8 5.4 -15.3 176 -343 103 .25
GFZ | 6 | 1.4 -.4 -.4 -22 -46 -26 .05
GRG | 6 | 2.1 1.8 -6.9 -15 46 -44 .35
JPL | 6 | 2.8 -2.2 2.7 0 -2 10 .32
MIT | 6 | 7.7 7.9 -2.9 -3 7 -31 .16
NGS | 6 | 3.2 3.2 7.3 -37 -11 27 .47
SIO | 6 | 3.2 2.5 -53.6 114 -361 -120 .12
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 1.1712.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1712.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 2.1712.[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 3.1712.[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 5.1712.0-6). 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 1712 summary. (Oct 28, 2012 - Nov 03, 2012)
Table 1.1712.a GPS week: 1712 MJD: 56228.000-56234.000
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 254| 1 0 0 18 73 17 -.43 12 12 | -641 -310 20 95
| 1 0 1 25 23 16 .01 | 827 1403
emr 80| -2 0 1 -8 61 11 .27 15 15 | 2423 333 15 100
| 1 1 1 27 30 17 .04 | 854 583
esa 175| 0 0 1 124 -168 16 .04 6 6 | -1326 1091 12 115
| 0 0 1 20 50 12 .03 | 743 814
gfz 184| -1 0 -1 -121 -39 14 -.42 12 12 | -139 216 21 142
| 1 0 1 36 71 17 .04 | 285 336
grg 126| 0 0 -1 -8 85 -21 .44 15 14 | -168 109 14 156
| 1 1 1 13 23 21 .05 | 327 467
igr n/a| 0 0 0 -53 131 -18 -.15 4 4 | 4350 496 16 100
| 0 0 0 27 41 8 .01 | 851 549
jpl 80| -1 0 1 -1 90 10 .42 14 13 | 3233 85 17 160
| 1 1 1 41 35 11 .03 | 979 524
mit 239| 0 0 -1 -26 45 5 -.16 6 6 | -122 -107 21 200
| 0 0 0 28 32 12 .02 | 394 567
ngs 239| 0 0 1 -99 118 9 .39 11 9 | -684 -239 1706 3441
| 0 1 3 48 20 29 .01 | 590 1025
sio 272| -1 -1 0 34 -134 -167 -.19 17 16 | --- --- --- ---
| 0 1 1 44 88 65 .03 | --- ---
Table 1.1712.b GPS week : 1712 MJD: 56228.000-56234.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 3 4 4 3 |
2 | 4 4 4 4 4 5 4 |
3 | 3 3 3 3 3 4 4 |
4 | 4 4 4 3 4 3 3 |
5 | 4 3 4 4 4 4 4 |
6 | 3 3 3 3 4 3 3 |
7 | 4 4 4 4 4 5 4 |
8 | 4 3 3 3 3 3 3 |
9 | 4 3 3 4 4 4 3 |
10 | 6 6 6 6 5 5 5 |
11 | 4 3 4 3 4 4 4 |
12 | 4 4 5 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 3 4 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 4 4 4 4 4 4 4 |
17 | 4 4 4 4 4 4 4 |
18 | 3 4 4 3 4 4 3 |
19 | 4 5 5 5 4 5 4 |
20 | 3 3 4 4 4 3 3 |
21 | 4 4 4 4 4 4 4 |
22 | 3 3 3 3 4 4 3 |
23 | 4 4 4 4 5 5 4 |
24 | 8 8 9 7 9 9 10 |
25 | 5 4 5 5 4 4 4 |
26 | 3 3 3 4 3 3 3 |
27 | 0 0 0 0 0 0 0 |
28 | 3 3 3 4 3 4 3 |
29 | 4 4 4 4 4 4 4 |
30 | 4 4 5 5 5 5 5 |
31 | 4 4 4 4 4 4 5 |
32 | 4 4 4 4 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 2.1712.0 GPS week: 1712 Day: 0 MJD: 56228.000
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| 1 0 0 57 81 17 -.43 11 11 | -1364 401 18 106
emr 80| -1 1 1 29 59 23 .24 14 14 | 1772 628 12 106
esa 175| 0 1 2 96 -78 28 .05 6 6 | -1317 788 11 161
gfz 187| -2 0 -2 -159 -131 -3 -.35 12 11 | 197 69 21 190
grg 128| -1 2 -3 16 59 -50 .46 17 15 | -463 398 16 152
igr n/a| 0 -1 0 -48 157 -21 -.15 4 4 | 3370 473 16 108
jpl 80| 0 0 0 48 110 7 .41 12 12 | 2878 613 16 154
mit 240| 0 0 -2 -35 -12 -11 -.15 6 6 | -371 291 20 241
ngs 242| 0 -1 5 -112 128 9 .41 13 10 | -1305 270 1737 3593
sio 285| 0 -3 -1 3 -90 -102 -.20 18 15 | --- --- --- ---
Table 2.1712.1 GPS week: 1712 Day: 1 MJD: 56229.000
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| 1 0 -2 17 31 19 -.42 12 12 | -1821 1601 22 96
emr 80| 0 2 2 -10 5 34 .25 15 15 | 1849 880 13 103
esa 175| 0 0 0 147 -235 30 .07 7 7 | -1681 1906 12 111
gfz 189| 0 0 0 -117 63 0 -.40 11 11 | -73 55 22 141
grg 128| -1 1 -2 -12 68 -11 .41 14 14 | -578 628 14 169
igr n/a| 1 0 0 -33 61 -16 -.16 4 4 | 3380 1006 17 107
jpl 80| -2 0 0 7 54 14 .44 13 13 | 3213 718 16 163
mit 240| 1 0 -1 -44 72 13 -.17 5 5 | -621 715 21 205
ngs 241| 0 0 2 -51 88 -24 .40 12 9 | -1453 1049 1544 3273
sio 214| 0 -3 0 4 4 -230 -.23 17 15 | --- --- --- ---
Table 2.1712.2 GPS week: 1712 Day: 2 MJD: 56230.000
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 258| 2 0 -3 -5 66 20 -.43 15 14 | -355 -443 19 79
emr 80| 0 2 2 -24 44 16 .26 14 14 | 2764 534 15 103
esa 175| 0 0 1 94 -156 10 -.00 7 6 | -1590 1398 11 102
gfz 188| -2 0 -2 -60 -22 12 -.43 12 11 | -89 -222 19 124
grg 127| -1 0 1 -21 58 -22 .49 15 14 | 177 -628 15 161
igr n/a| 0 0 0 -90 109 -32 -.15 4 4 | 4433 530 16 86
jpl 80| 0 -1 2 -26 90 9 .38 14 13 | 3960 163 17 152
mit 240| 0 0 -1 11 56 -5 -.17 6 6 | -22 -196 19 173
ngs 240| 0 1 0 -142 91 -19 .40 12 9 | -367 -489 1433 3190
sio 282| 0 -1 0 48 -115 -80 -.19 16 15 | --- --- --- ---
Table 2.1712.3 GPS week: 1712 Day: 3 MJD: 56231.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 2 -1 2 26 111 29 -.43 13 13 | 793 -3013 21 91
emr 80| 0 0 2 17 106 16 .23 15 15 | 4043 -558 15 107
esa 175| 1 0 2 135 -184 18 .07 6 6 | -204 307 12 126
gfz 186| -2 -2 -4 -122 -123 42 -.44 14 14 | 176 405 24 159
grg 126| 0 0 -1 0 116 -33 .48 16 15 | 340 -285 14 147
igr n/a| 0 0 0 -39 187 -5 -.17 4 4 | 5697 -391 16 119
jpl 80| -3 0 2 -16 154 10 .41 13 13 | 4726 -496 16 158
mit 240| 0 0 -1 -68 29 0 -.19 5 5 | 635 -1002 22 203
ngs 239| 2 0 -2 -36 127 26 .39 11 9 | 317 -2277 1771 3630
sio 280| -2 0 0 -12 -98 -189 -.20 16 16 | --- --- --- ---
Table 2.1712.4 GPS week: 1712 Day: 4 MJD: 56232.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 251| 0 0 0 -20 78 40 -.43 11 11 | -409 -661 23 98
emr 80| -3 0 2 -55 76 12 .30 16 16 | 2743 -340 18 79
esa 175| 0 1 0 126 -179 9 .03 6 6 | -522 -124 15 119
gfz 178| 0 0 1 -90 -53 33 -.47 12 12 | -206 196 22 127
grg 128| 1 -2 0 -20 109 10 .43 15 14 | -254 337 17 163
igr n/a| 1 0 0 -94 151 -14 -.13 4 4 | 4817 -58 18 100
jpl 80| -1 -2 0 -73 94 31 .41 14 13 | 3695 -694 22 155
mit 240| 1 0 -1 8 78 8 -.17 7 7 | -229 188 25 200
ngs 235| 0 -1 0 -115 138 -13 .40 11 9 | -572 -261 1795 3458
sio 284| 0 -1 1 15 -163 -250 -.18 17 15 | --- --- --- ---
Table 2.1712.5 GPS week: 1712 Day: 5 MJD: 56233.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 2 0 0 32 78 4 -.45 12 12 | -699 -192 21 106
emr 80| -5 0 0 0 72 -4 .30 16 16 | 1553 933 16 105
esa 175| 1 0 0 142 -140 22 .04 6 6 | -2403 2092 11 100
gfz 183| -1 0 -2 -146 -31 8 -.44 14 13 | -402 166 20 117
grg 124| 0 0 -2 -2 88 -38 .33 16 15 | -183 -159 14 154
igr n/a| 0 0 0 -25 146 -16 -.14 4 4 | 3927 1077 19 88
jpl 80| -4 0 2 34 74 6 .45 14 13 | 2106 224 18 173
mit 239| 0 0 0 -35 27 5 -.16 6 5 | -240 -548 21 189
ngs 240| 1 0 0 -167 136 49 .37 11 10 | -737 -123 1983 3512
sio 281| -1 0 0 68 -204 -191 -.20 17 17 | --- --- --- ---
Table 2.1712.6 GPS week: 1712 Day: 6 MJD: 56234.000
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| 0 0 0 24 63 -11 -.42 11 11 | -637 135 18 89
emr 80| -1 0 -2 -17 61 -16 .34 16 16 | 2242 255 17 102
esa 175| 0 0 0 126 -203 -5 .06 7 7 | -1570 1275 12 90
gfz 181| 0 -2 0 -154 25 6 -.41 10 9 | -582 848 19 140
grg 127| 0 0 -1 -15 95 -3 .45 16 15 | -218 476 13 147
igr n/a| 0 0 0 -40 104 -23 -.13 4 4 | 4829 839 15 96
jpl 80| -1 -1 0 15 52 -4 .45 14 14 | 2056 71 16 169
mit 239| 0 0 -2 -23 65 25 -.13 5 5 | -10 -202 21 189
ngs 240| 0 0 7 -72 117 37 .41 11 10 | -673 158 1682 3431
sio 278| -1 0 3 112 -271 -127 -.14 19 18 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1712.0 GPS week: 1712 Day: 0 MJD: 56228.000
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 16 8 12 16 4 11 5 12 13 3 | 32 36 38 36 48 35 51 37 41 41 37
2 | 8 17 6 15 15 4 14 6 10 22 4 | 21 28 22 20 28 18 30 18 26 17 19
3 | 10 8 4 11 17 3 7 7 11 16 3 | 19 24 24 22 33 20 30 19 27 25 20
4 | 7 8 6 11 14 4 8 4 14 34 4 | 32 30 30 38 35 31 28 34 25 32 30
5E | 8 14 4 12 15 6 16 7 10 10 3 | 35 43 40 39 47 38 42 39 42 36 38
6 | 9 7 5 13 14 2 7 4 9 11 2 | 26 29 29 24 34 26 33 24 28 28 25
7 | 9 13 7 10 15 5 14 4 12 18 3 | 21 22 18 18 25 15 21 15 22 17 14
8 | 13 11 6 10 12 5 10 6 12 23 3 | 19 20 15 16 19 14 22 15 18 18 12
9 | 8 10 5 12 13 4 8 7 16 15 3 | 15 20 15 18 21 15 24 17 23 20 14
10E | 18 24 8 15 18 7 16 7 30 25 5 | 23 36 23 28 27 20 30 25 40 23 23
11 | 14 15 5 8 15 4 12 4 10 10 3 | 28 40 30 33 44 31 40 33 30 31 31
12 | 11 18 6 11 18 5 19 7 9 15 4 | 22 24 21 22 30 19 27 21 27 20 20
13 | 10 13 6 13 20 4 12 6 12 14 3 | 22 29 22 24 35 20 29 20 21 20 20
X14 | 11 15 5 12 --- 4 11 5 12 12 3 | 21 21 18 23 --- 18 27 19 21 19 17
15 | 10 14 8 7 16 5 14 8 13 17 3 | 17 24 21 20 33 18 27 21 26 19 19
16 | 9 15 6 11 19 3 15 6 9 14 3 | 23 27 23 19 31 20 27 20 24 17 19
17 | 10 14 5 16 12 4 13 5 12 26 4 | 30 30 29 35 36 30 32 30 27 30 28
18E | 7 8 8 11 14 4 10 4 12 10 3 | 34 37 35 28 41 34 42 32 35 36 32
19 | 11 12 6 9 10 4 10 5 12 24 3 | 23 27 27 25 30 25 31 25 26 29 23
20E | 12 11 6 9 21 5 10 4 8 12 3 | 41 46 41 47 43 43 43 44 48 47 44
21 | 9 16 5 13 16 4 13 5 10 15 3 | 21 32 19 18 27 18 30 17 22 15 17
22E | 8 9 7 9 19 3 11 5 9 11 3 | 23 27 25 23 34 21 28 22 27 25 23
23 | 14 14 6 13 18 6 13 6 12 18 4 | 24 27 21 19 26 17 28 18 20 18 17
X24 | 23 --- 10 --- 23 14 --- 9 --- --- 8 | --- --- 110 --- 118 109 --- 111 --- --- 110
25 | 13 23 6 13 40 6 14 7 12 20 5 | 24 25 24 30 39 23 32 24 31 31 23
26 | 9 12 5 8 13 5 9 5 11 18 3 | 22 29 26 31 33 22 28 29 24 21 25
X27 | 9 --- --- --- --- 70 --- --- --- --- 0 | 46 --- --- --- --- 22 --- --- --- --- 49
28 | 9 14 5 10 16 4 11 5 6 10 3 | 19 22 18 17 31 15 25 16 21 19 16
29 | 14 16 5 11 15 4 13 5 12 27 4 | 27 28 27 29 29 26 29 27 25 23 24
30 | 8 14 5 16 16 3 12 7 10 24 4 | 44 47 44 42 42 43 47 40 44 41 41
31 | 13 17 5 15 15 2 15 5 11 13 4 | 23 29 22 23 32 19 31 20 29 22 20
32E | 16 16 6 10 15 5 14 7 18 11 4 | 42 48 43 38 49 42 50 42 51 42 43
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 6 12 17 4 12 6 12 18 |T 26 30 29 26 36 27 32 28 29 26 27
WRMS | 11 14 6 11 15 4 12 6 10 15 |NE 24 27 27 24 35 25 29 26 25 23 25
MEDI | 10 14 6 11 15 4 12 5 12 15 |MD 23 28 24 24 33 21 30 24 26 23 23
Table 3.1712.1 GPS week: 1712 Day: 1 MJD: 56229.000
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 | 13 16 10 9 12 3 11 6 8 10 3 | 26 33 37 29 44 34 49 34 38 36 34
2 | 7 19 9 15 11 4 16 5 10 23 4 | 20 34 26 23 28 21 31 21 23 16 22
3 | 10 9 3 12 12 4 8 4 14 16 3 | 18 27 20 22 25 19 26 19 23 18 20
4 | 4 12 5 9 10 4 8 4 14 30 3 | 39 35 33 39 34 38 35 38 33 39 36
5E | 7 17 5 9 12 3 15 4 9 15 3 | 33 42 33 30 40 33 38 33 37 32 34
6 | 10 10 4 11 10 3 7 4 15 11 3 | 21 30 22 25 27 22 29 20 27 20 22
7 | 13 13 7 13 14 4 14 5 11 15 3 | 23 29 22 23 27 24 28 21 24 25 21
8 | 9 12 5 7 10 4 11 5 9 13 3 | 17 24 14 15 16 16 22 15 16 22 14
9 | 12 11 6 10 13 5 9 6 9 17 3 | 16 28 20 18 25 18 25 18 18 23 18
10E | 16 20 11 12 22 5 16 5 27 19 5 | 27 42 31 26 36 29 39 30 40 29 28
11 | 9 15 7 8 14 6 12 4 10 10 3 | 23 36 28 23 36 25 36 25 25 27 26
12 | 17 20 7 9 14 4 20 6 8 16 4 | 26 32 24 21 31 23 30 21 28 22 22
13 | 10 14 6 12 19 3 14 4 11 12 3 | 22 31 21 21 36 22 32 21 24 25 21
14 | 11 15 8 11 13 3 12 4 12 15 3 | 23 30 19 23 26 20 28 19 23 23 19
15 | 14 15 5 8 21 4 15 5 10 20 4 | 15 25 19 16 36 18 27 18 23 19 18
16 | 10 13 6 11 16 4 13 4 9 17 3 | 19 28 21 22 31 20 25 21 23 15 20
17 | 10 16 7 14 8 4 14 4 10 24 4 | 20 30 23 24 26 25 27 24 21 24 22
18E | 20 12 8 12 12 3 9 4 11 12 3 | 30 29 23 26 31 24 29 27 26 28 25
19 | 29 12 6 10 11 6 14 7 17 22 4 | 32 28 21 18 24 20 28 18 20 19 20
20E | 10 12 6 8 10 4 13 5 10 16 3 | 43 46 43 41 47 43 47 42 40 45 42
21 | 10 16 7 12 13 5 13 5 13 16 3 | 14 30 15 14 27 16 28 15 23 15 16
22E | 8 11 8 11 16 2 10 4 6 10 3 | 18 26 23 18 27 21 31 20 24 23 20
23 | 10 18 5 11 16 3 17 5 9 16 3 | 23 29 21 18 31 22 30 22 25 21 20
X24 | 21 --- 12 --- 21 12 --- 10 --- --- 8 | --- --- 72 --- 82 76 --- 76 --- --- 73
25 | 10 24 9 12 15 4 18 5 10 17 4 | 22 31 23 24 34 24 32 22 24 30 22
26 | 9 10 5 9 13 3 8 2 6 15 2 | 25 33 27 25 33 27 30 29 30 26 27
X27 | 7 --- --- --- --- 130 --- --- --- --- 0 | 79 --- --- --- --- 62 --- --- --- --- 81
28 | 9 16 7 8 14 4 12 5 9 7 3 | 17 28 18 17 29 17 25 18 22 19 17
29 | 13 19 5 13 14 4 16 5 11 23 4 | 25 30 21 23 25 21 28 20 24 19 20
30 | 10 14 6 15 14 3 15 8 10 24 4 | 63 66 65 67 64 62 68 63 63 63 63
31 | 13 19 7 14 16 4 17 6 10 16 4 | 16 28 16 17 27 18 29 16 24 17 15
32E | 16 15 7 7 15 5 14 7 17 12 4 | 34 45 37 30 45 36 46 36 45 39 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 7 11 14 4 13 5 12 17 |T 26 32 27 24 33 28 32 26 27 25 27
WRMS | 12 15 7 11 14 4 13 5 9 15 |NE 24 29 24 21 31 25 29 23 24 22 25
MEDI | 10 15 7 11 14 4 13 5 10 16 |MD 23 30 23 23 31 22 29 21 24 23 22
Table 3.1712.2 GPS week: 1712 Day: 2 MJD: 56230.000
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 | 13 16 10 9 11 5 11 8 9 10 3 | 26 32 33 33 46 33 45 33 38 37 34
2 | 12 14 7 15 13 3 13 6 10 23 4 | 16 30 23 23 25 21 27 21 26 14 20
3 | 9 7 4 12 13 4 8 4 8 19 3 | 12 23 18 25 26 16 21 17 23 15 18
4 | 11 11 6 12 11 2 11 4 10 28 3 | 29 22 23 27 23 24 22 22 27 28 22
5E | 9 14 7 11 11 4 14 6 12 17 3 | 37 45 43 45 42 41 42 41 40 49 41
6 | 8 7 4 14 10 3 7 4 11 14 3 | 18 24 21 30 26 18 24 21 24 18 20
7 | 13 14 6 13 13 4 20 5 8 12 3 | 16 23 15 20 25 16 23 15 22 16 15
8 | 10 11 5 12 12 3 13 5 8 11 3 | 14 20 13 18 17 16 19 16 19 20 13
9 | 13 9 4 12 11 3 9 4 10 15 3 | 14 20 15 14 21 15 22 14 24 17 14
10E | 30 21 12 13 21 7 15 9 30 16 6 | 33 33 25 22 26 19 28 22 35 21 21
11 | 10 17 6 6 12 3 13 7 15 11 3 | 24 34 24 26 36 23 32 25 25 26 25
12 | 11 20 6 17 19 3 22 6 13 16 4 | 21 27 23 29 30 23 28 21 30 20 20
13 | 10 15 7 12 15 4 14 5 9 12 3 | 17 29 20 23 36 21 28 20 24 19 20
14 | 11 17 6 12 13 4 12 5 9 12 3 | 15 24 17 19 22 17 22 14 21 15 15
15 | 16 11 4 11 15 4 15 5 8 18 3 | 16 25 19 17 30 19 25 19 26 18 18
16 | 12 16 8 9 15 4 15 8 11 16 4 | 16 24 17 17 30 17 22 17 24 12 16
17 | 13 16 7 16 11 5 15 6 10 24 4 | 28 26 20 29 26 24 26 22 31 23 23
18E | 20 9 8 12 16 4 11 5 11 10 3 | 34 29 31 30 38 31 33 27 32 30 29
19 | 33 11 6 10 10 4 12 5 8 22 4 | 30 25 20 25 24 17 24 20 22 20 20
20E | 10 10 6 9 18 4 15 5 9 13 3 | 36 40 36 37 43 37 38 38 38 41 36
21 | 11 14 6 12 13 4 15 6 12 18 3 | 13 26 19 16 27 16 27 14 26 12 16
22E | 8 10 6 12 18 3 11 6 8 8 3 | 15 19 18 16 20 16 20 16 20 16 14
23 | 13 17 6 12 15 4 16 6 14 15 4 | 19 27 18 20 28 19 26 19 22 18 18
X24 | 26 --- 10 --- 20 12 --- 10 --- --- 8 | --- --- 88 --- 92 91 --- 91 --- --- 90
25 | 17 23 10 12 17 3 17 5 8 18 4 | 23 24 23 21 32 22 31 21 28 29 21
26 | 9 9 4 12 13 3 7 5 10 12 3 | 16 21 19 16 25 18 20 18 21 19 17
X27 | 8 --- --- --- --- 41 --- --- --- --- 0 | 35 --- --- --- --- 38 --- --- --- --- 36
28 | 9 14 4 13 17 6 9 7 8 8 3 | 13 23 17 17 30 16 20 18 21 16 15
29 | 13 15 6 13 14 4 16 7 10 25 4 | 21 27 24 28 26 26 26 28 31 21 23
30E | 16 17 9 15 22 5 15 10 11 24 5 | 69 73 64 64 68 64 73 61 65 67 64
31 | 16 15 9 13 17 4 16 7 10 12 4 | 20 25 18 17 27 17 25 13 23 13 13
32E | 15 18 7 10 15 4 14 7 19 10 4 | 31 43 35 29 41 33 43 33 42 34 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 14 7 12 15 4 14 6 12 16 |T 23 28 25 25 32 25 28 25 28 23 25
WRMS | 14 14 6 11 14 4 13 6 9 15 |NE 19 25 22 22 30 23 25 22 25 19 22
MEDI | 12 14 6 12 14 4 14 6 10 15 |MD 20 25 20 23 27 19 26 21 25 19 20
Table 3.1712.3 GPS week: 1712 Day: 3 MJD: 56231.000
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 | 13 17 4 13 13 4 10 3 7 11 3 | 25 30 32 34 45 31 45 32 39 36 33
2 | 7 17 8 16 13 4 14 6 11 21 4 | 19 29 21 22 25 17 28 19 25 16 20
3 | 10 9 5 12 12 3 8 5 9 19 3 | 15 21 18 24 22 18 22 16 24 17 17
4 | 7 9 6 11 11 4 10 3 9 25 3 | 29 24 25 34 27 27 24 29 30 29 27
5E | 11 13 5 12 17 3 14 5 10 10 3 | 51 49 50 50 45 47 46 46 51 46 48
6 | 9 10 5 14 11 4 8 5 11 16 3 | 20 24 22 29 26 22 25 21 23 24 21
7 | 14 15 5 12 17 4 14 5 10 13 3 | 23 24 16 22 26 15 23 17 23 16 18
8 | 10 10 3 13 18 4 11 4 7 13 3 | 15 17 12 18 16 10 18 13 16 16 13
9 | 16 11 5 15 10 3 11 5 8 17 3 | 17 21 17 18 20 16 23 16 21 18 17
10E | 16 20 10 13 27 6 16 7 24 15 5 | 32 35 29 30 33 26 34 28 38 27 28
11 | 8 15 6 11 15 4 12 4 9 12 3 | 22 34 25 27 38 24 33 24 28 25 25
12 | 16 20 7 13 17 4 22 7 14 15 4 | 20 27 21 22 29 18 26 20 28 16 19
13 | 11 14 6 17 20 4 12 5 8 11 3 | 23 28 22 28 36 21 28 21 20 20 22
14 | 12 15 4 13 11 3 13 4 10 12 3 | 21 25 23 20 24 19 25 17 20 17 17
15 | 11 14 6 11 16 4 14 4 15 17 3 | 18 23 19 22 30 14 25 16 21 17 17
16 | 14 16 7 13 18 6 13 5 7 15 3 | 20 23 22 19 27 17 22 14 23 15 16
17 | 10 16 7 20 11 4 16 5 11 23 4 | 21 26 26 34 27 23 26 24 23 23 23
18E | 10 10 7 11 17 4 12 4 9 7 3 | 30 35 35 29 37 32 37 30 34 33 31
19 | 29 12 7 13 11 4 10 5 9 22 4 | 27 25 25 29 27 24 26 22 27 23 23
20E | 10 10 9 12 22 3 15 3 11 11 3 | 37 36 38 40 47 35 39 36 32 35 36
21 | 11 16 5 12 15 4 14 4 8 19 3 | 17 29 17 17 25 15 26 14 19 13 16
22E | 9 11 7 13 18 3 10 5 9 8 3 | 24 24 23 21 18 21 25 18 22 18 19
23 | 14 16 5 18 14 4 15 4 11 14 4 | 21 26 19 25 27 17 24 18 21 17 18
X24 | 22 --- 11 --- 17 9 --- 7 --- --- 7 | --- --- 96 --- 107 98 --- 99 --- --- 99
25 | 18 24 6 12 15 3 17 4 15 12 4 | 22 23 25 30 32 22 29 22 27 25 22
26 | 13 12 6 11 14 5 8 8 10 11 3 | 19 25 20 23 27 19 26 24 21 20 21
X27 | 10 --- --- --- --- 52 --- --- --- --- 0 | 53 --- --- --- --- 44 --- --- --- --- 57
28 | 11 14 6 15 18 5 12 5 9 9 3 | 16 21 16 23 28 12 21 14 19 16 15
29 | 10 15 8 10 13 7 15 6 14 24 4 | 22 26 23 30 23 25 26 26 28 21 23
30E | 18 17 8 20 22 7 18 8 11 20 5 | 135 130 130 121 127 129 133 126 133 125 128
31 | 15 18 5 17 15 4 14 6 13 13 4 | 19 26 20 21 26 17 26 14 27 13 16
32E | 16 18 7 12 19 4 15 5 18 12 4 | 32 44 37 31 39 34 44 33 41 37 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 15 6 14 16 4 13 5 11 16 |T 27 31 29 29 35 28 31 28 30 25 29
WRMS | 13 15 6 14 15 4 13 5 9 16 |NE 21 25 24 24 30 23 25 23 24 19 24
MEDI | 11 15 6 13 15 4 13 5 10 13 |MD 22 26 23 25 27 21 26 21 24 20 21
Table 3.1712.4 GPS week: 1712 Day: 4 MJD: 56232.000
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 17 6 10 14 4 12 6 10 10 3 | 28 36 37 32 44 35 49 37 38 37 37
2 | 7 18 6 14 12 4 15 7 8 22 4 | 21 33 22 23 26 20 30 24 28 17 23
3 | 10 9 4 15 11 3 8 6 8 18 3 | 16 23 18 25 22 17 22 19 24 15 19
4 | 5 11 5 12 12 3 9 6 10 23 3 | 27 24 25 30 28 26 25 30 25 25 26
5E | 7 14 6 9 14 4 15 7 9 12 3 | 50 55 50 51 59 50 52 57 53 48 53
6 | 20 10 5 14 12 2 8 6 6 15 3 | 22 25 20 28 24 20 25 22 25 20 21
7 | 14 17 4 12 20 4 15 6 12 13 4 | 19 24 16 17 25 14 22 17 24 10 15
8 | 9 12 4 9 10 5 12 5 10 10 3 | 14 18 14 16 13 13 17 16 17 16 13
9 | 7 10 7 11 15 3 12 6 13 18 3 | 14 23 18 16 23 15 23 15 28 15 16
10E | 13 24 7 12 15 4 19 9 20 25 5 | 24 35 24 25 30 20 28 21 39 33 24
11 | 10 18 6 7 16 4 13 6 15 12 3 | 23 38 29 28 36 24 35 28 33 25 29
12 | 11 24 5 8 14 4 23 6 13 16 4 | 16 28 22 21 28 19 27 20 32 14 19
13 | 11 17 5 14 19 4 14 7 11 12 4 | 19 27 16 20 32 16 26 20 19 16 17
14 | 10 17 5 10 14 4 12 9 10 14 3 | 17 27 17 20 25 16 23 18 20 16 16
15 | 9 16 7 7 16 3 16 6 10 18 3 | 21 26 24 23 31 20 27 20 22 22 21
16 | 9 16 7 11 14 4 12 7 9 17 3 | 11 25 15 22 24 14 22 15 20 11 15
17 | 10 16 6 14 11 5 15 6 10 23 4 | 24 27 26 31 26 24 26 26 27 26 24
18E | 8 12 7 8 12 4 12 5 8 22 3 | 39 37 39 36 42 35 40 36 38 37 37
19 | 20 11 5 12 9 5 12 6 9 21 4 | 26 26 25 27 23 23 27 25 27 20 23
20E | 10 12 5 13 17 5 12 6 10 24 4 | 36 39 36 36 45 34 35 37 35 38 36
21 | 8 17 7 9 13 4 13 8 13 21 4 | 13 30 16 17 28 15 27 21 23 17 18
22E | 7 16 9 11 18 3 10 8 11 10 3 | 28 33 26 30 27 25 30 30 23 27 27
23 | 15 17 5 15 17 4 16 8 11 17 4 | 19 27 16 20 26 15 26 19 20 14 17
X24 | 19 --- 10 --- 34 13 --- 8 --- --- 9 | --- --- 93 --- 99 88 --- 91 --- --- 92
25 | 11 27 8 9 13 6 16 8 8 9 4 | 22 27 25 23 33 22 30 21 31 22 22
26 | 9 10 6 9 13 4 10 6 8 6 3 | 14 26 18 20 22 17 26 16 22 19 18
X27 | 8 --- --- --- --- 115 --- --- --- --- 0 | 58 --- --- --- --- 70 --- --- --- --- 59
28 | 7 13 4 12 15 4 12 6 8 7 3 | 11 20 17 15 29 12 20 16 21 14 15
29 | 9 18 6 11 12 5 16 8 11 24 4 | 18 27 23 22 22 22 24 24 27 19 21
30E | 16 22 9 18 17 4 19 9 10 18 5 | 98 106 100 109 104 100 105 96 96 104 99
31 | 11 15 6 14 17 3 13 8 10 14 4 | 16 26 19 22 30 17 25 18 25 16 17
32E | 14 18 6 15 16 4 17 8 17 9 4 | 29 43 34 32 38 31 43 31 38 31 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 6 12 15 4 14 7 11 17 |T 25 32 28 27 34 27 31 28 30 24 28
WRMS | 11 16 6 12 14 4 13 7 9 15 |NE 20 26 23 22 29 23 26 24 25 18 24
MEDI | 10 16 6 11 14 4 13 6 10 16 |MD 21 27 23 23 28 20 26 21 25 19 21
Table 3.1712.5 GPS week: 1712 Day: 5 MJD: 56233.000
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 14 4 15 14 3 11 4 12 12 3 | 27 36 35 31 45 34 49 35 41 37 35
2 | 7 18 8 20 12 4 17 6 10 22 4 | 19 32 21 26 26 19 31 23 25 18 21
3 | 12 10 4 15 14 2 10 4 9 20 3 | 20 20 20 17 22 16 22 17 22 16 16
4 | 6 11 5 11 13 4 9 4 7 25 3 | 21 19 17 22 22 19 19 21 19 21 18
5E | 7 13 5 12 12 3 16 5 11 20 3 | 38 40 38 39 40 37 40 37 42 42 37
6 | 11 10 5 16 12 3 9 4 9 15 3 | 24 22 24 21 22 21 24 20 27 21 20
7 | 13 18 9 14 23 5 13 7 12 16 4 | 19 26 18 21 30 16 23 20 22 16 16
8 | 11 10 5 14 16 4 10 5 8 11 3 | 15 19 11 18 20 11 21 16 15 19 14
9 | 10 11 7 10 12 5 11 5 12 15 3 | 15 20 14 12 20 12 24 14 22 14 14
10E | 12 24 6 15 13 4 21 8 19 21 5 | 32 43 31 33 31 30 40 33 40 41 32
11 | 8 16 5 12 14 4 11 4 12 14 3 | 20 36 23 23 34 22 35 24 31 24 24
12 | 11 21 8 14 16 6 24 6 11 15 4 | 15 25 18 21 28 13 26 16 25 13 16
13 | 10 16 6 15 23 4 13 6 7 13 4 | 21 30 23 24 36 20 29 23 22 18 21
14 | 9 15 10 11 16 2 12 8 12 12 4 | 17 22 22 17 24 14 23 14 22 14 16
15 | 10 15 5 10 17 5 16 7 10 17 3 | 18 23 17 16 30 14 25 15 22 16 15
16 | 13 19 6 11 16 4 14 7 10 16 4 | 18 25 17 15 26 15 24 15 20 13 15
17 | 9 15 6 14 11 3 16 6 8 26 4 | 16 23 17 24 21 15 24 18 21 16 17
18E | 16 12 7 12 16 3 11 5 11 6 3 | 27 31 31 29 31 28 31 26 31 28 27
19 | 25 13 6 12 12 4 12 5 13 22 4 | 20 24 23 20 23 18 26 19 23 16 18
20E | 9 11 5 10 12 6 12 4 11 10 3 | 22 28 22 18 28 21 26 24 26 24 23
21 | 11 16 7 12 15 3 12 5 12 23 4 | 16 29 17 17 27 15 26 16 20 17 16
22E | 8 20 7 14 14 2 12 4 13 9 3 | 25 37 28 30 32 25 28 25 25 24 26
23 | 13 18 7 16 20 5 16 6 11 16 4 | 22 26 20 21 29 18 27 20 20 16 19
X24 | 29 --- 10 --- 20 11 --- 9 --- --- 9 | --- --- 74 --- 81 69 --- 71 --- --- 72
25 | 15 22 7 13 16 6 16 6 6 9 4 | 17 19 16 21 28 16 25 16 22 17 15
26 | 9 11 4 11 12 4 8 4 11 9 2 | 22 29 22 25 26 21 27 26 28 25 24
X27 | 8 --- --- --- --- 103 --- --- --- --- 0 | 44 --- --- --- --- 55 --- --- --- --- 42
28 | 8 13 6 14 16 4 12 6 7 13 3 | 14 20 14 17 26 11 23 17 18 19 15
29 | 13 16 8 12 13 5 15 8 12 23 4 | 21 24 23 24 21 18 26 23 25 18 19
30E | 19 18 8 14 18 5 17 9 12 21 5 | 96 103 97 104 103 97 100 98 96 93 98
31 | 12 16 7 15 21 4 12 7 12 15 4 | 19 24 20 15 27 15 26 14 23 16 15
32E | 19 19 6 15 16 4 17 7 16 10 4 | 34 42 34 30 37 33 45 32 40 33 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 14 16 4 14 6 11 17 |T 24 29 26 25 32 24 30 25 27 23 25
WRMS | 12 16 6 13 15 4 13 5 10 17 |NE 20 24 21 20 28 20 26 21 23 18 21
MEDI | 11 15 6 14 15 4 12 6 11 15 |MD 20 25 22 21 28 18 26 20 23 18 19
Table 3.1712.6 GPS week: 1712 Day: 6 MJD: 56234.000
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 | 10 16 5 8 16 5 13 3 8 13 3 | 36 41 40 37 53 40 56 41 46 46 41
2 | 7 19 8 18 10 4 19 5 8 25 4 | 23 33 23 26 26 22 35 24 29 24 24
3 | 11 11 5 11 19 3 7 6 10 21 3 | 15 26 20 20 28 15 23 17 22 18 18
4 | 6 10 5 9 12 3 9 3 11 23 3 | 32 30 30 32 32 30 29 31 26 28 29
5E | 8 15 6 9 11 4 20 7 12 11 3 | 45 51 49 44 51 45 50 47 54 44 47
6 | 10 9 6 12 16 4 9 4 10 14 3 | 20 30 26 31 33 23 28 24 23 27 24
7 | 8 17 5 10 20 3 16 6 10 16 3 | 21 27 16 20 28 16 26 16 21 18 18
8 | 10 9 5 9 13 4 11 4 8 10 2 | 14 16 13 16 15 11 17 13 18 15 12
9 | 8 13 7 8 16 4 10 3 10 18 3 | 13 21 15 12 22 12 21 14 23 16 15
10E | 9 20 9 11 12 5 17 6 15 28 4 | 26 40 29 26 35 28 37 30 38 32 29
11 | 8 16 6 10 18 3 12 3 8 16 3 | 27 38 28 27 44 28 38 29 28 31 29
12 | 12 23 11 8 13 4 22 5 12 17 4 | 21 31 19 18 30 15 30 18 25 14 20
13 | 9 16 7 10 21 3 14 6 11 16 4 | 23 34 24 27 41 22 33 22 21 26 24
14 | 11 17 7 8 18 3 14 8 10 15 4 | 19 23 21 22 27 16 24 17 22 18 18
15 | 9 13 6 7 20 4 16 4 7 18 3 | 21 27 22 20 36 19 29 19 24 25 21
16 | 11 12 8 12 15 3 13 5 10 18 3 | 16 24 17 13 25 14 25 16 25 13 17
17 | 12 17 6 10 11 5 17 5 12 26 4 | 31 32 29 32 32 28 28 28 26 29 27
18E | 8 13 7 9 15 2 12 4 7 15 3 | 36 36 36 32 40 33 40 34 37 34 35
19 | 22 13 6 11 12 4 11 4 14 25 4 | 27 29 27 29 29 24 28 26 24 25 25
20E | 12 11 7 8 14 5 11 6 10 11 3 | 29 36 29 28 33 27 34 28 29 32 29
21 | 7 15 5 7 13 4 16 6 9 26 3 | 18 32 18 12 28 15 31 16 24 20 18
22E | 8 14 6 10 16 2 10 5 11 11 3 | 37 35 32 32 34 32 36 34 33 34 34
23 | 13 17 10 10 18 4 16 5 12 19 4 | 24 32 24 22 31 20 33 20 22 23 22
X24 | 17 --- 7 --- 46 9 --- 9 --- --- 10 | --- --- 105 --- 116 106 --- 107 --- --- 107
25 | 9 24 7 7 12 3 17 6 12 11 3 | 22 24 23 23 33 20 33 21 28 22 22
26 | 7 11 4 9 13 4 8 6 7 10 2 | 19 20 18 18 25 17 20 19 19 18 18
X27 | 7 --- --- --- --- 47 --- --- --- --- 0 | 50 --- --- --- --- 25 --- --- --- --- 51
28 | 6 11 5 10 13 3 11 5 8 9 2 | 15 21 14 19 27 14 20 17 21 18 17
29 | 13 17 12 8 14 6 14 6 13 23 4 | 29 29 30 30 29 26 27 28 25 23 26
30E | 18 20 9 13 17 4 18 9 11 33 5 | 110 111 106 106 110 105 112 102 110 115 107
31 | 17 17 5 11 22 4 14 7 12 22 4 | 20 26 17 18 29 14 25 14 23 21 15
32E | 17 21 9 9 19 4 18 7 16 11 4 | 37 50 37 32 47 35 48 34 41 35 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 7 10 16 4 14 5 11 19 |T 28 33 30 27 37 28 33 29 30 28 30
WRMS | 11 16 7 9 15 4 14 5 10 18 |NE 23 28 25 22 34 23 28 24 24 22 26
MEDI | 9 15 6 9 15 4 14 5 10 16 |MD 23 30 24 26 32 22 29 24 25 24 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 4.1712 GPS week: 1712 MJD: 56228.0-56234.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 |U 4 4 12 |U 7 9 23 |U 7 7 16 |
emr | emr 2870 | 8 7 18 |U 9 8 26 | 10 11 21 |
esa | esa 2976 | 5 4 14 |U 7 10 24 | 8 9 18 |
gfz | gfz 2868 |U 6 5 13 |U 7 8 23 |U 9 11 20 |
grg | grg 2933 |U 9 9 22 |U 8 11 30 | 10 11 23 |
igr | igr 2966 | 6 5 14 | 6 9 23 | 9 9 18 |
igs | igs 2968 | 6 5 15 | 7 9 24 | 8 8 17 |
jpl | jpl 2868 | 7 7 18 |U 7 10 26 | 10 11 24 |
mit | mit 2976 | 7 5 15 |U 8 9 27 |U 9 9 20 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1712.0 GPS week: 1712 Day: 0 MJD: 56228.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3038 | 4 4 9 | 7 9 27 | 5 4 11 |
emr | emr 2872 | 8 8 12 | 9 7 30 | 7 7 16 |
esa | esa 2976 | 6 6 12 | 7 7 27 | 6 6 14 |
gfz | gfz 2873 | 7 7 10 | 7 7 25 | 6 6 15 |
grg | grg 2880 | 7 9 16 | 8 9 33 | 8 8 21 |
igr | igr 2976 | 7 6 12 | 7 7 26 | 6 6 14 |
igs | igs 2974 | 6 6 11 | 7 7 27 | 7 6 14 |
jpl | jpl 2869 | 12 8 15 | 7 7 29 | 10 9 38 |
mit | mit 2976 | 7 6 12 | 8 7 27 | 8 9 20 |
Table 5.1712.1 GPS week: 1712 Day: 1 MJD: 56229.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 3 3 11 | ---- ---- ---- | 5 6 12 |
emr | emr 2872 | 7 5 18 | ---- ---- ---- | 8 8 21 |
esa | esa 2976 | 4 3 15 | ---- ---- ---- | 6 7 14 |
gfz | gfz 2870 | 6 3 13 | ---- ---- ---- | 7 7 15 |
grg | grg 2975 | 7 8 20 | ---- ---- ---- | 9 11 21 |
igr | igr 2948 | 5 3 12 | ---- ---- ---- | 8 8 16 |
igs | igs 2960 | 5 3 15 | ---- ---- ---- | 7 7 14 |
jpl | jpl 2871 | 7 6 18 | ---- ---- ---- | 7 9 17 |
mit | mit 2976 | 5 3 13 | ---- ---- ---- | 8 9 16 |
Table 5.1712.2 GPS week: 1712 Day: 2 MJD: 56230.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 4 4 11 | 6 11 20 | 6 6 16 |
emr | emr 2871 | 8 8 18 | 9 12 29 | 10 10 22 |
esa | esa 2976 | 6 5 14 | 7 12 25 | 7 7 18 |
gfz | gfz 2870 | 5 6 13 | 7 10 25 | 8 8 19 |
grg | grg 2975 | 7 9 23 | 8 12 25 | 10 9 26 |
igr | igr 2967 | 6 6 14 | 7 11 25 | 7 7 17 |
igs | igs 2973 | 6 5 16 | 7 12 24 | 7 6 17 |
jpl | jpl 2870 | 6 7 19 | 7 13 28 | 11 11 22 |
mit | mit 2976 | 5 6 14 | 8 12 25 | 9 7 18 |
Table 5.1712.3 GPS week: 1712 Day: 3 MJD: 56231.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 4 5 12 | 6 9 23 | 8 8 17 |
emr | emr 2872 | 7 6 14 | 8 7 27 | 11 10 17 |
esa | esa 2976 | 4 4 12 | 6 10 24 | 10 9 20 |
gfz | gfz 2868 | 5 5 11 | 6 7 26 | 10 25 29 |
grg | grg 2970 | 6 6 16 | 7 9 25 | 11 9 20 |
igr | igr 2953 | 5 4 13 | 6 10 24 | 9 8 19 |
igs | igs 2974 | 4 4 12 | 6 8 24 | 9 8 16 |
jpl | jpl 2868 | 6 6 16 | 7 9 28 | 11 11 21 |
mit | mit 2976 | 5 5 12 | 7 8 24 | 10 9 21 |
Table 5.1712.4 GPS week: 1712 Day: 4 MJD: 56232.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 | 4 5 14 | 5 8 18 | 8 9 20 |
emr | emr 2867 | 8 7 21 | 7 8 19 | 10 11 20 |
esa | esa 2976 | 5 5 19 | 5 11 19 | 9 10 19 |
gfz | gfz 2867 | 5 7 19 | 5 9 21 | 9 9 19 |
grg | grg 2879 | 7 9 21 | 6 12 27 | 10 8 21 |
igr | igr 2966 | 6 6 19 | 5 11 18 | 10 10 22 |
igs | igs 2952 | 5 5 19 | 5 10 19 | 10 10 21 |
jpl | jpl 2865 | 6 7 20 | 6 11 19 | 9 11 20 |
mit | mit 2976 | 6 6 19 | 7 11 22 | 10 9 21 |
Table 5.1712.5 GPS week: 1712 Day: 5 MJD: 56233.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3019 | 5 5 13 | 9 9 28 | 9 12 21 |
emr | emr 2868 | 8 7 20 | 12 8 28 | 14 19 28 |
esa | esa 2976 | 6 5 13 | 8 9 24 | 10 13 24 |
gfz | gfz 2866 | 6 6 13 | 9 7 21 | 12 16 25 |
grg | grg 2976 | 13 10 39 | 10 14 40 | 10 20 32 |
igr | igr 2976 | 6 5 14 | 8 8 23 | 10 14 23 |
igs | igs 2972 | 6 5 14 | 9 8 23 | 9 13 21 |
jpl | jpl 2867 | 7 9 18 | 10 10 28 | 12 17 27 |
mit | mit 2976 | 11 8 18 | 9 8 35 | 10 13 25 |
Table 5.1712.6 GPS week: 1712 Day: 6 MJD: 56234.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 7 4 16 | 6 9 20 | 9 8 17 |
emr | emr 2868 | 9 6 22 | 8 9 23 | 11 12 25 |
esa | esa 2976 | 7 4 15 | 7 10 25 | 10 9 18 |
gfz | gfz 2866 | 7 5 15 | 6 8 22 | 8 8 19 |
grg | grg 2880 | 15 10 20 | 7 10 31 | 10 11 22 |
igr | igr 2976 | 7 4 15 | 6 9 24 | 10 9 18 |
igs | igs 2972 | 7 5 18 | 6 10 25 | 8 7 18 |
jpl | jpl 2867 | 8 7 21 | 7 10 27 | 11 11 23 |
mit | mit 2976 | 10 6 15 | 7 11 27 | 9 8 17 |
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 6.1712 GPS week: 1712 MJD: 56228.500-56234.500
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 -37 5 22 -5 | -3 14
| 15 18 64 63 4 | 2
emr uuuuu | 27 -15 89 158 7 | 15 22
| 28 21 83 119 11 | 3
esa uuuuu | -42 -23 -18 -134 -4 | 0 13
| 35 31 79 61 4 | 2
gfz uuuuu | 67 41 -6 -65 -5 | 8 14
| 22 15 44 26 4 | 1
grg uuuux | -8 -22 28 -48 -19 | -2 36
| 30 15 67 24 37 | 10
igr xxxxx | -50 38 -12 8 -1 | 1 12
| 20 18 47 98 4 | 2
irf xxxxx | 9 8 19 7 0 | -2 9
| 15 9 12 12 3 | 1
jpl uuuuu | 12 -38 -9 161 -1 | 38 41
| 25 33 52 57 6 | 1
mit uuuuu | 25 11 -2 53 2 | -6 13
| 13 19 53 49 7 | 2
ngs uuuxu | -32 108 -22 85 2 | 5 10
| 42 49 99 278 5 | 2
sio xuuuu | 188 -58 -23 -42 17 | 16 23
| 104 41 63 89 3 | 4
Table 7.1712.0 GPS week: 1712 Day: 0 MJD: 56228.500
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 | -4 -65 30 17 -5 | 0 19
emr uuuuu | 63 -55 188 254 -3 | 15 24
esa uuuuu | -102 29 58 -174 -7 | 2 19
gfz uuuuu | 87 32 -77 -50 -4 | 10 19
grg uuuux | 48 -38 130 -61 22 | -19 55
igr xxxxx | -61 46 -1 -146 1 | 2 16
irf xxxxx | 32 -7 -3 22 1 | 0 13
jpl uuuuu | 10 -67 -91 149 -4 | 40 43
mit uuuuu | 31 1 -66 70 7 | -4 17
ngs uuuxu | -7 151 -81 -320 -3 | 6 16
sio xuuuu | 125 -82 33 -92 18 | 13 21
Table 7.1712.1 GPS week: 1712 Day: 1 MJD: 56229.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -22 -53 72 58 -5 | -4 16
emr uuuuu | 58 -2 16 288 -5 | 12 21
esa uuuuu | -19 -46 69 -166 1 | -2 16
gfz uuuuu | 70 29 -11 -92 -5 | 7 16
grg uuuux | -5 4 36 -56 6 | -14 53
igr xxxxx | -32 18 34 -61 -3 | -1 14
irf xxxxx | 12 16 26 -5 2 | -4 8
jpl uuuuu | -3 -48 -4 156 2 | 37 40
mit uuuuu | 27 35 -51 20 4 | -7 14
ngs uuuxu | -120 72 -87 -25 -3 | 3 9
sio xuuuu | 48 -35 10 50 20 | 11 18
Table 7.1712.2 GPS week: 1712 Day: 2 MJD: 56230.500
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 | -21 -35 -42 79 -9 | -2 13
emr uuuuu | 46 -22 81 255 2 | 14 22
esa uuuuu | -59 -23 6 -179 -10 | 1 14
gfz uuuuu | 94 50 6 -103 2 | 9 16
grg uuuux | -2 -26 -9 -28 16 | -4 42
igr xxxxx | -32 52 -37 -28 0 | 1 13
irf xxxxx | 13 5 29 1 -1 | -3 8
jpl uuuuu | 12 -31 -1 239 -10 | 40 42
mit uuuuu | 16 0 53 40 6 | -8 14
ngs uuuxu | -26 110 -86 -147 1 | 3 9
sio xuuuu | 156 -43 -149 -99 20 | 15 22
Table 7.1712.3 GPS week: 1712 Day: 3 MJD: 56231.500
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 -27 -50 -30 -11 | -2 14
emr uuuuu | -4 -19 35 167 -3 | 15 22
esa uuuuu | 3 -7 -39 -202 -2 | 0 15
gfz uuuuu | 58 25 6 -55 -7 | 10 15
grg uuuux | 4 -26 72 -55 -7 | 8 23
igr xxxxx | -73 43 -40 -17 -9 | 2 12
irf xxxxx | -5 3 25 25 0 | -3 9
jpl uuuuu | -28 7 11 211 -2 | 39 42
mit uuuuu | -1 -6 46 112 7 | -8 14
ngs uuuxu | 13 70 -69 14 4 | 4 9
sio xuuuu | 133 -18 -17 -119 16 | 16 23
Table 7.1712.4 GPS week: 1712 Day: 4 MJD: 56232.500
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 | -31 -11 -79 34 2 | -6 11
emr uuuuu | 2 5 183 124 19 | 11 17
esa uuuuu | -17 -70 -3 -99 -2 | -3 11
gfz uuuuu | 71 62 1 -64 -8 | 6 10
grg uuuux | -41 -37 66 -51 -47 | 8 23
igr xxxxx | -70 62 -29 117 4 | -1 10
irf xxxxx | -14 20 30 11 -8 | -4 9
jpl uuuuu | 7 6 60 172 -2 | 36 37
mit uuuuu | 26 39 -37 33 -13 | -5 11
ngs uuuxu | -26 66 -26 338 5 | 3 8
sio xuuuu | 251 -13 -29 20 18 | 16 22
Table 7.1712.5 GPS week: 1712 Day: 5 MJD: 56233.500
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 | -10 -31 19 -90 -4 | -4 12
emr uuuuu | 18 -16 136 -37 21 | 17 22
esa uuuuu | -62 -23 -164 -70 -2 | 0 9
gfz uuuuu | 61 31 -32 -24 -8 | 8 11
grg uuuux | -22 -17 -47 -79 -74 | 5 24
igr xxxxx | -57 13 -74 82 -4 | 3 9
irf xxxxx | 14 10 11 -3 3 | -2 7
jpl uuuuu | 39 -66 -66 142 6 | 39 40
mit uuuuu | 35 -7 57 117 7 | -4 10
ngs uuuxu | -24 195 186 309 0 | 7 10
sio xuuuu | 244 -102 33 -133 16 | 21 27
Table 7.1712.6 GPS week: 1712 Day: 6 MJD: 56234.500
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 | -31 -39 87 87 -2 | -5 12
emr uuuuu | 8 7 -19 59 15 | 20 24
esa uuuuu | -39 -22 -52 -46 -8 | -1 9
gfz uuuuu | 27 59 67 -64 -4 | 6 10
grg uuuux | -37 -14 -50 -6 -49 | -1 33
igr xxxxx | -24 35 61 111 -1 | 2 9
irf xxxxx | 9 9 16 -1 0 | -1 6
jpl uuuuu | 44 -65 27 59 6 | 39 40
mit uuuuu | 37 12 -16 -18 0 | -2 8
ngs uuuxu | -37 92 12 424 10 | 6 9
sio xuuuu | 361 -116 -42 82 12 | 23 28
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