[IGSREPORT-22894] Wk 1800 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Jul 24 11:47:02 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1800 (Jul 06, 2014 - Jul 12, 2014)
Contacts: igs.acc at noaa.gov
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1800[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1800[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1800[0-6].cls IGS GPS clock combination summary report.
igs18007.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18007.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 | 3
0 | ESA | 3
0 | GFZ | 1 2 6 30 1 3 6 30 ASPA
0 | GRG | 6 6 9 KOUR MAL2 WUHN KOUR MAL2 WUHN
0 | MIT | 9 9 21 ASPA OPMT ASPA GUUG MDVJ OPMT
1 | COD | 3
1 | EMR | 9
1 | ESA | 3 WUHN CAS1 PTBB UNSA WUHN
1 | GFZ | 1 2 6 30 1 3 6 30 JPLM NTUS JPLM
1 | GRG | 6 6 DAEJ GRAZ KOUC ONSA SPT0 KELY KOUC NOVM ONSA
1 | GRG | SPT0
1 | JPL | 8
1 | MIT | 9 9 MDVJ
2 | COD | GOPE
2 | EMR | 3
2 | ESA | UNSA
2 | GFZ | 1 2 6 30 1 6 30 CAS1 GOPE IRKJ NRMD WUHN CAS1 IRKJ
2 | GFZ | NRMD WUHN
2 | GRG | 6 3 6 KOUC QAQ1 SOFI WUHN KOUC QAQ1 SOFI WUHN
2 | JPL | 28
2 | MIT | 9 3 9 GOPE IRKJ IRKJ MDVJ
3 | COD | REUN
3 | EMR | 3
3 | ESA | 9 WTZR GRAS UNSA WTZR
3 | GFZ | 1 2 6 30 1 3 6 30 WUHN
3 | GRG | 6 3 6 IRKJ QAQ1 SOFI TLSE WTZR IRKJ NTUS QAQ1 SOFI
3 | GRG | TLSE WTZR
3 | MIT | 9 3 9 MDVJ YIBL
4 | COD | BOR1
4 | EMR | 3 3
4 | ESA | 9 ONSA WTZR ARTU ONSA UNSA WTZR
4 | GFZ | 1 2 6 30 1 6 30 BAKE HOB2 ONSA WUHN YIBL HOB2 ONSA
4 | GFZ | YIBL
4 | GRG | 6 9 3 6 IRKJ ONSA WUHN IRKJ ONSA SOFI
4 | JPL | 3 ARTU
4 | MIT | 9 3 MDVJ
5 | COD | NKLG
5 | EMR | 3 3 HOB2
5 | ESA | 9 UNSA
5 | GFZ | 1 2 6 30 1 6 30 CAS1 NYA1 NYAL WUHN CAS1 NYA1 NYAL
5 | GFZ | WUHN
5 | GRG | 6 3 6 DAEJ NTUS DAEJ NTUS WUHN
5 | JPL | 3
5 | MIT | 9 9 20 DAEJ MDVJ
6 | COD | BOGT
6 | ESA | 9 UNSA
6 | GFZ | 1 2 6 30 1 6 30 BOGT FAIR INVK WUHN YELL FAIR INVK
6 | GFZ | WUHN YELL
6 | GRG | 3 6 3 6 IRKJ KELY KOUC WUHN GRAZ IRKJ KELY KOUC WUHN
6 | JPL | BOGT INVK
6 | MIT | 9 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. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G10 | 2014_07_10 | 2014056
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | GRG | 6
1 | GRG | 6 9
2 | GRG | 6
3 | GRG | 6
3 | MIT | 9
4 | GRG | 6 9
5 | GRG | 6
6 | GRG | 6 9
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G09 | | 4 | | 4 | | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.2 .6 .0 -26 14 -40 .17
EMR | 0 | 3.6 -8.5 1.3 -17 5 -39 .09
ESA | 0 | .2 .8 -1.4 -11 -5 28 -.04
GFZ | 0 | -.1 .1 -.2 -20 -18 3 -.15
GRG | 0 | 17.2 -20.3 19.0 -36 -10 -33 .62
JPL | 0 | 2.2 -4.7 11.3 -29 51 35 -.61
MIT | 0 | 6.6 -12.6 9.7 5 3 -42 .32
NGS | 0 | 8.5 -4.9 4.2 -3 -34 37 .49
SIO | 0 | 7.0 -10.3 8.9 5 18 -31 .31
COD | 1 | -1.0 -.3 .0 -28 13 -49 .20
EMR | 1 | 10.5 -10.6 .0 1 8 -49 -.17
ESA | 1 | .7 .6 -1.4 -5 -12 6 -.14
GFZ | 1 | .4 .2 -1.2 -26 -25 -29 -.07
GRG | 1 | 23.6 -23.8 20.9 -31 20 -30 .47
JPL | 1 | -1.3 -1.9 12.9 -75 -26 -22 .12
MIT | 1 | 11.9 -7.6 10.7 -1 1 -41 .32
NGS | 1 | 5.9 -5.0 11.2 -35 -36 20 .43
SIO | 1 | 6.5 -6.0 5.1 8 20 -44 .12
COD | 2 | -.6 .5 -.2 -22 22 -56 .15
EMR | 2 | 6.6 -8.4 .3 -30 9 -55 -.0
ESA | 2 | .1 1.0 -1.5 -17 -16 19 -.06
GFZ | 2 | .3 .1 -1.0 -22 -21 -23 -.17
GRG | 2 | 22.2 -25.7 24.5 -25 24 -21 .38
JPL | 2 | -3.4 -5.0 8.1 -107 -23 -18 -.88
MIT | 2 | 10.8 -14.2 10.5 3 8 -54 .31
NGS | 2 | 2.4 -13.1 12.5 -69 -22 -19 .54
SIO | 2 | 7.1 -12.1 3.5 5 16 -34 .14
COD | 3 | .2 .0 .2 -54 22 -68 .22
EMR | 3 | -.2 -10.0 -.9 -11 -5 -21 -.10
ESA | 3 | .1 .4 -1.4 -16 -6 10 .02
GFZ | 3 | .5 .2 -.7 -24 -23 -22 -.30
GRG | 3 | 22.3 -26.3 25.1 -3 38 -18 .69
JPL | 3 | -3.2 -3.2 12.1 -81 -9 10 -.74
MIT | 3 | 7.8 -14.6 7.6 11 7 -51 .23
NGS | 3 | 7.0 -13.2 10.9 -62 -36 6 .33
SIO | 3 | 5.2 -9.2 -2.9 9 31 -31 .02
COD | 4 | -.4 .3 .7 -37 10 -74 .23
EMR | 4 | -2.2 -6.5 .2 -11 -3 -20 -.15
ESA | 4 | .1 .4 -1.7 -8 -17 21 -.03
GFZ | 4 | .5 .4 -.3 -14 -29 -25 -.82
GRG | 4 | 17.7 -13.9 26.3 -16 31 -22 .40
JPL | 4 | 5.2 -10.1 10.8 -80 4 -37 -.83
MIT | 4 | 5.2 -15.5 5.1 -5 -1 -42 .40
NGS | 4 | -4.3 -8.6 10.2 -47 11 -42 .62
SIO | 4 | 5.5 -7.5 .7 10 14 -14 .27
COD | 5 | -1.0 1.2 -.8 -34 21 -49 .07
EMR | 5 | -1.5 -2.7 -.9 -3 -16 -24 -.14
ESA | 5 | .4 .2 -1.3 -6 -24 12 -.30
GFZ | 5 | .1 .7 -1.1 -24 -22 -20 -.57
GRG | 5 | 10.2 -13.7 23.5 5 28 -19 .15
JPL | 5 | -4.8 -5.3 5.2 -28 17 -37 -.79
MIT | 5 | 4.4 -9.1 2.1 -5 4 -42 .13
NGS | 5 | 1.9 -8.0 9.6 -47 -19 -8 .52
SIO | 5 | 1.3 -7.6 -5.5 5 32 -44 .10
COD | 6 | -.6 .9 -.7 -24 3 -45 .35
EMR | 6 | -1.1 -8.0 -1.3 -6 -13 -30 .08
ESA | 6 | .1 .3 -1.8 13 -2 24 .19
GFZ | 6 | .0 .6 -.4 -13 -25 -8 -.21
GRG | 6 | 13.7 -18.1 26.1 -32 8 -39 .25
JPL | 6 | 4.2 -5.3 7.6 -29 46 -4 -.09
MIT | 6 | 5.2 -9.3 3.5 0 13 -61 .28
NGS | 6 | -1.7 -6.6 15.0 -53 -7 -26 .65
SIO | 6 | 3.4 -6.2 3.9 12 38 -24 -.11
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1800.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1800.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 2.1800.[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 3.1800.[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 5.1800.0-6). 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 1800 summary. (Jul 06, 2014 - Jul 12, 2014)
Table 1.1800.a GPS week: 1800 MJD: 56844.000-56850.000
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 248| 0 0 2 15 0 -9 .05 9 9 | -1323 410 17 117
| 0 0 1 22 18 12 .03 | 388 470
emr 80| 0 -3 -3 -12 -14 30 .20 12 12 | 1448 660 16 138
| 1 0 1 12 13 16 .02 | 1629 1101
esa 150| 0 0 -6 -2 2 -12 -.28 11 10 | 28 -1023 10 163
| 0 0 0 16 20 12 .03 | 665 1354
gfz 197| 0 1 -1 9 -10 -16 .06 11 10 | -126 171 12 121
| 0 0 1 28 14 13 .03 | 187 519
grg 186| 4 -1 18 36 -33 -2 .23 21 16 | -61 -165 19 150
| 0 1 2 15 16 16 .03 | 196 544
igr n/a| 0 0 0 14 0 0 -.18 5 5 | 1866 1167 17 95
| 0 0 0 15 15 11 .04 | 2740 1119
jpl 80| -1 3 -6 -36 12 10 -.03 13 13 | 788 637 17 137
| 1 0 1 22 22 11 .02 | 1511 1139
mit 299| 0 -1 2 -17 -18 7 -.12 12 11 | 192 -699 21 184
| 0 0 1 18 29 4 .03 | 947 1828
ngs 234| 0 0 0 7 40 -6 .00 11 10 | -1282 531 1545 3474
| 1 0 4 50 41 20 .05 | 346 856
sio 478| 1 1 0 -28 -14 4 -.72 16 14 | --- --- --- ---
| 1 0 0 8 16 19 .04 | --- ---
Table 1.1800.b GPS week : 1800 MJD: 56844.000-56850.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 5 6 5 5 4 4 4 |
3 | 5 4 4 5 5 6 5 |
4 | 4 4 4 3 4 4 4 |
5 | 4 4 4 5 4 4 5 |
6 | 9 9 9 9 8 9 9 |
7 | 5 5 5 5 5 5 4 |
8 | 4 4 4 4 4 4 4 |
9 | 16 20 14 14 12 11 13 |
10 | 4 4 4 4 0 3 4 |
11 | 5 5 5 5 5 5 4 |
12 | 6 6 6 5 5 6 6 |
13 | 5 5 5 5 4 5 4 |
14 | 4 5 5 4 5 5 5 |
15 | 6 5 5 5 5 5 5 |
16 | 5 5 5 5 4 5 5 |
17 | 5 4 5 5 5 6 5 |
18 | 4 5 4 4 4 4 5 |
19 | 5 4 5 4 4 4 5 |
20 | 4 4 4 4 4 4 4 |
21 | 5 5 5 5 5 5 5 |
22 | 4 3 4 4 3 3 4 |
23 | 4 5 5 4 5 5 5 |
24 | 5 5 4 4 5 5 4 |
25 | 4 6 5 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 4 5 5 4 5 5 |
28 | 5 4 4 5 5 4 4 |
29 | 5 5 5 5 6 6 5 |
30 | 4 4 4 4 4 5 4 |
31 | 5 4 5 5 5 5 5 |
32 | 3 3 3 4 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 2.1800.0 GPS week: 1800 Day: 0 MJD: 56844.000
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 244| 0 1 3 6 20 -12 .06 9 9 | -674 -449 16 116
emr 80| 0 -2 -2 -33 -10 16 .18 11 11 | 452 -525 14 131
esa 150| 0 -1 -5 -21 19 7 -.33 10 11 | -435 -1216 11 174
gfz 194| -1 1 0 21 -19 -4 .12 12 11 | -87 -252 12 121
grg 191| 5 -1 16 17 -61 -15 .24 16 16 | 283 -883 17 134
igr n/a| -1 0 0 1 18 7 -.20 5 5 | -1042 120 17 90
jpl 80| -2 2 -6 -11 26 28 -.04 13 12 | -393 -269 18 134
mit 300| 0 0 3 -10 -41 9 -.11 12 11 | 1807 -4043 22 185
ngs 233| 0 0 -7 27 38 -32 -.02 11 10 | -1404 1030 1845 3590
sio 481| 1 1 0 -30 -30 15 -.77 14 11 | --- --- --- ---
Table 2.1800.1 GPS week: 1800 Day: 1 MJD: 56845.000
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 247| -1 -1 4 19 13 -4 .04 9 9 | -1968 821 15 112
emr 80| 1 -3 -5 -7 -23 1 .23 12 12 | -52 308 14 126
esa 150| 0 0 -4 5 4 -22 -.28 10 10 | -238 -1356 10 169
gfz 196| 0 1 1 58 -2 -7 .10 12 12 | -27 -606 12 128
grg 185| 6 -1 15 24 -37 7 .28 17 16 | -89 -313 18 153
igr n/a| -1 0 -1 21 -15 -9 -.18 5 5 | -624 732 16 85
jpl 80| -1 2 -7 -31 -10 -1 -.04 12 10 | -443 202 17 116
mit 300| 2 0 4 -15 16 11 -.09 12 11 | -1384 1946 19 165
ngs 233| -1 1 -2 -68 7 25 -.05 11 11 | -754 -948 1302 3085
sio 485| 0 1 0 -20 1 34 -.70 14 14 | --- --- --- ---
Table 2.1800.2 GPS week: 1800 Day: 2 MJD: 56846.000
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 1 10 -3 -17 .11 10 10 | -1202 245 19 121
emr 80| 0 -3 -2 -26 7 24 .19 13 12 | 500 -215 15 113
esa 150| 0 1 -6 -3 3 -8 -.26 11 10 | -331 -329 12 171
gfz 198| 0 1 0 -22 -30 -33 .07 12 10 | -212 26 13 123
grg 183| 5 -3 17 42 -32 13 .26 22 14 | -233 -55 20 153
igr n/a| -1 1 -1 13 -2 0 -.14 5 5 | 331 472 18 92
jpl 80| -1 4 -7 -47 33 2 .01 14 14 | 92 -307 19 133
mit 300| 1 -1 2 -7 -25 8 -.14 12 11 | 390 -581 21 185
ngs 235| 0 0 0 65 40 5 -.05 11 9 | -1038 185 1925 3671
sio 485| 1 0 0 -17 -33 0 -.72 16 15 | --- --- --- ---
Table 2.1800.3 GPS week: 1800 Day: 3 MJD: 56847.000
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 249| 0 1 0 58 13 -8 .06 11 11 | -1432 635 18 106
emr 80| 0 -3 -2 -6 -3 34 .19 12 11 | 254 1507 17 141
esa 150| 0 0 -7 3 -25 -25 -.24 11 10 | 1143 -3434 13 171
gfz 198| 0 1 -1 -4 -19 -19 .03 11 10 | -313 609 12 116
grg 188| 4 0 16 34 -42 3 .23 22 15 | -63 -467 19 154
igr n/a| -1 0 0 42 -21 1 -.22 6 6 | 775 2183 20 127
jpl 80| 0 2 -4 -44 -15 16 -.03 13 13 | -333 1576 18 151
mit 299| 0 -1 3 0 -15 8 -.15 12 11 | -228 -139 23 188
ngs 238| -1 0 0 -45 67 -10 .00 11 10 | -1259 308 1366 3463
sio 474| 0 0 0 -24 -21 -24 -.73 16 15 | --- --- --- ---
Table 2.1800.4 GPS week: 1800 Day: 4 MJD: 56848.000
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 252| -1 0 1 2 -28 -24 .04 8 8 | -1495 975 14 120
emr 80| 0 -2 -1 -5 -31 41 .23 12 12 | 1552 2699 19 141
esa 150| 0 0 -6 18 -10 -18 -.28 11 11 | 837 -1580 11 163
gfz 200| -1 0 -1 -1 -10 -30 .02 11 11 | -347 909 13 124
grg 188| 4 -1 19 65 -31 -4 .24 23 18 | -329 891 20 146
igr n/a| 0 1 0 22 -8 19 -.22 5 5 | 2652 3242 16 94
jpl 80| 0 3 -4 -59 -2 15 -.03 14 13 | 815 2797 18 151
mit 300| 0 -2 0 -56 13 2 -.15 12 11 | 48 -9 22 179
ngs 236| 1 0 -3 34 110 12 .01 12 10 | -1846 1725 1076 3400
sio 489| 1 0 0 -38 -2 19 -.76 17 16 | --- --- --- ---
Table 2.1800.5 GPS week: 1800 Day: 5 MJD: 56849.000
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 244| 0 0 4 20 11 14 .03 9 9 | -1218 382 17 122
emr 80| -3 -2 -5 -5 -13 46 .18 13 13 | 3897 412 18 167
esa 150| 0 0 -5 -28 -9 -16 -.30 11 10 | -402 783 9 145
gfz 199| 0 1 -3 -14 -4 -23 .05 11 9 | 204 82 11 120
grg 185| 5 0 21 42 -6 10 .20 23 16 | -44 -277 21 160
igr n/a| 0 0 0 1 12 -15 -.13 5 5 | 5513 745 19 102
jpl 80| 0 3 -5 -60 13 -3 -.03 13 13 | 3212 168 17 155
mit 300| 0 -1 0 -11 -67 0 -.14 13 12 | 347 -383 22 194
ngs 236| 0 -1 3 48 38 -22 .06 10 9 | -1192 322 1668 4117
sio 468| 1 1 0 -29 -20 -7 -.69 16 14 | --- --- --- ---
Table 2.1800.6 GPS week: 1800 Day: 6 MJD: 56850.000
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| 0 0 2 -14 -20 -14 .03 9 9 | -1278 262 24 122
emr 80| 0 -3 -4 -5 -25 46 .18 13 13 | 3533 435 19 150
esa 150| 0 0 -5 6 35 0 -.28 10 10 | -373 -30 10 154
gfz 195| 1 2 -3 27 13 0 .06 11 10 | -103 434 13 120
grg 186| 3 0 22 28 -25 -32 .18 22 17 | 44 -56 19 153
igr n/a| 0 0 0 1 11 3 -.17 5 5 | 5462 678 17 77
jpl 80| -4 2 -7 -3 42 13 -.04 14 14 | 2569 297 17 124
mit 300| 0 -1 0 -23 -10 10 -.10 13 12 | 367 -1684 23 195
ngs 229| 0 0 5 -10 -21 -20 .07 11 9 | -1486 1100 1635 2992
sio 468| 3 2 0 -37 6 -4 -.64 16 14 | --- --- --- ---
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 3.1800.0 GPS week: 1800 Day: 0 MJD: 56844.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 7 12 13 11 6 15 13 13 11 4 | 30 34 33 28 30 30 37 32 35 31 31
2 | 13 14 12 12 19 5 14 18 10 17 5 | 21 27 20 23 24 16 20 23 21 14 19
3E | 7 14 12 12 15 6 16 9 8 16 4 | 82 86 85 81 89 82 85 87 84 82 84
4 | 8 9 10 9 12 4 10 9 9 10 3 | 16 19 17 18 19 15 17 17 17 13 16
5 | 8 10 8 14 13 4 11 9 10 13 4 | 27 28 25 37 36 25 26 32 26 26 28
X6 | 14 --- 11 21 88 8 29 23 18 30 8 | 92 --- 91 90 118 88 104 84 91 88 91
7 | 9 19 8 12 18 4 18 11 14 12 5 | 31 36 24 34 34 26 32 32 27 20 29
8 | 9 8 9 10 10 4 11 6 8 18 3 | 45 41 43 42 44 42 41 43 43 45 42
X9 | 21 32 --- --- 44 19 --- 23 41 --- 16 | 116 119 --- --- 134 119 --- 111 120 --- 115
10 | 9 9 7 10 16 5 6 8 10 8 3 | 19 15 14 21 18 18 16 16 13 13 18
11 | 9 9 14 11 20 4 12 15 12 8 4 | 19 23 20 19 34 15 21 20 19 15 18
12 | 10 14 11 13 19 8 14 25 15 15 5 | 26 25 21 33 31 22 22 28 31 26 23
13 | 8 13 9 11 21 5 14 12 10 12 4 | 25 29 21 30 43 24 25 31 26 27 26
14 | 8 8 11 11 17 4 16 12 8 15 4 | 30 29 25 34 42 26 24 36 29 33 29
15 | 20 12 11 12 21 8 16 14 14 16 6 | 28 24 17 27 36 18 22 24 21 19 21
16 | 9 13 11 16 17 4 13 12 11 19 4 | 26 28 21 30 30 23 26 27 25 26 24
17E | 8 14 9 12 19 5 17 10 10 13 4 | 37 35 30 41 40 34 32 34 34 27 34
18 | 7 7 11 13 10 4 8 17 9 16 4 | 22 25 24 26 28 21 23 32 22 24 23
19E | 6 13 8 10 18 5 14 16 10 11 4 | 40 43 38 40 44 38 41 42 41 39 40
20 | 6 9 8 11 12 6 9 13 10 19 3 | 27 22 24 30 31 25 21 26 26 25 24
21 | 11 15 13 12 17 6 15 14 12 19 5 | 16 26 19 18 28 16 22 19 19 19 17
22 | 7 6 10 10 10 5 8 14 10 11 3 | 26 28 28 30 34 26 26 35 27 28 27
23 | 9 14 10 11 15 6 14 8 10 18 4 | 27 30 23 30 39 25 25 30 28 30 26
24E | 8 9 16 9 16 4 15 10 19 9 5 | 37 40 41 39 38 39 37 37 44 39 38
25 | 10 9 12 10 12 8 12 10 11 11 4 | 28 28 28 26 31 24 31 27 30 25 27
26 | 8 8 9 12 14 4 12 6 12 19 3 | 28 25 24 28 32 23 25 26 23 26 24
X27E | 8 11 14 17 --- 5 14 8 8 10 4 | 33 31 37 32 --- 31 35 33 32 30 32
28 | 6 14 9 16 15 4 14 8 11 19 4 | 29 32 30 40 34 29 30 31 28 30 29
29E | 9 12 9 10 15 5 20 9 15 10 4 | 43 36 39 43 41 38 35 38 46 35 39
X30 | 7 7 11 7 --- 5 12 8 10 11 3 | 31 29 32 28 --- 28 31 28 30 29 29
31 | 8 12 10 18 21 5 15 9 9 9 4 | 20 26 13 24 36 14 22 17 20 9 18
32 | 5 7 8 10 11 4 8 9 9 13 3 | 19 21 16 26 30 19 22 22 17 19 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 10 12 16 5 13 12 11 14 |T 34 33 29 33 41 31 31 35 34 29 33
WRMS | 9 11 11 11 16 5 12 11 10 11 |NE 28 26 26 31 36 25 28 30 28 27 27
MEDI | 8 11 10 12 16 5 14 10 10 13 |MD 28 28 24 30 34 25 26 31 27 26 27
Table 3.1800.1 GPS week: 1800 Day: 1 MJD: 56845.000
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 | 7 11 10 9 12 5 12 11 14 11 4 | 22 29 25 22 29 22 32 25 29 24 25
2 | 12 15 12 12 19 5 11 18 15 16 5 | 21 27 22 22 24 17 21 22 26 12 20
3E | 8 14 10 10 14 6 14 11 11 17 4 | 73 75 73 72 75 69 72 70 71 72 72
4 | 9 9 9 8 11 3 8 10 10 9 3 | 16 17 18 16 18 17 15 15 20 16 16
5 | 8 11 7 11 12 4 10 13 12 14 4 | 21 24 19 26 26 19 20 24 22 21 21
X6 | 17 --- 10 24 83 9 34 18 16 27 9 | 84 --- 82 80 101 80 98 81 88 80 84
7 | 8 16 8 8 20 4 12 14 9 14 4 | 25 34 19 26 39 23 26 29 27 22 25
8 | 8 9 10 14 19 4 10 11 10 16 4 | 85 84 86 87 82 85 82 82 82 84 83
X9 | 21 25 --- --- 173 30 --- 29 54 --- 19 | 155 160 --- --- 252 151 --- 151 187 --- 161
10 | 12 9 6 13 14 4 7 8 8 10 3 | 17 16 15 14 16 15 12 14 16 16 14
11 | 7 12 12 8 23 4 10 15 11 9 4 | 14 23 16 18 34 14 18 18 21 15 16
12 | 9 14 8 13 20 7 11 25 16 15 5 | 24 30 22 26 28 21 22 26 27 22 21
13 | 8 12 9 13 21 4 12 13 9 16 4 | 27 27 21 29 38 22 24 26 22 23 24
14 | 8 11 11 12 20 6 13 11 10 17 4 | 26 25 21 28 33 21 22 27 26 28 23
15 | 10 14 12 14 22 4 14 12 13 18 5 | 25 26 19 26 35 19 21 21 24 20 21
16 | 10 14 10 13 17 5 10 13 11 19 4 | 25 28 21 23 30 22 24 24 24 20 22
17E | 8 12 7 10 19 5 14 9 11 12 4 | 30 28 23 29 33 26 27 26 31 25 26
18 | 6 9 11 17 12 5 9 17 10 17 4 | 17 20 18 20 22 16 19 23 21 19 18
19E | 11 13 5 8 14 5 14 11 7 10 4 | 34 35 32 31 38 32 31 33 35 30 32
20 | 9 10 7 12 13 5 9 10 9 17 3 | 23 20 21 27 24 22 19 25 19 22 20
21 | 10 15 12 12 17 6 14 14 11 16 5 | 15 25 18 18 23 13 22 14 18 17 15
22 | 6 6 10 10 11 4 8 10 9 10 3 | 19 20 20 20 24 17 18 22 20 16 19
23 | 10 14 10 11 16 5 14 10 11 21 4 | 31 32 23 29 35 25 27 28 26 26 26
24E | 15 14 13 8 17 5 14 8 15 9 5 | 34 31 31 27 31 26 31 25 31 29 29
25 | 10 10 13 24 16 5 13 12 15 11 5 | 26 28 28 37 29 24 29 24 26 23 25
26 | 8 9 10 11 15 4 9 7 9 15 3 | 25 25 23 23 27 21 18 21 22 24 22
X27E | 7 11 12 12 --- 4 12 6 8 11 4 | 26 28 33 26 --- 26 27 29 28 28 27
28 | 8 10 10 14 17 4 8 12 12 16 4 | 25 28 24 28 33 24 25 25 24 24 24
29E | 9 14 7 12 15 5 18 12 12 10 4 | 33 28 28 36 28 28 24 31 31 26 28
X30 | 7 7 11 8 --- 3 11 11 8 13 3 | 36 38 39 34 --- 36 36 37 34 34 36
31 | 8 9 10 7 21 4 12 10 12 9 4 | 21 25 16 21 31 17 23 19 24 16 19
32 | 6 6 7 7 9 5 7 7 10 15 2 | 20 19 15 20 22 16 17 18 15 13 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 10 12 17 5 12 12 11 14 |T 33 34 28 30 42 30 29 32 34 27 32
WRMS | 9 12 10 12 16 5 10 11 11 14 |NE 27 27 26 29 33 25 27 27 28 25 26
MEDI | 8 11 10 12 17 5 12 11 11 15 |MD 25 28 22 26 30 22 24 25 26 23 23
Table 3.1800.2 GPS week: 1800 Day: 2 MJD: 56846.000
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 | 9 11 13 11 10 5 14 9 10 11 4 | 31 30 33 25 32 27 32 30 32 26 29
2 | 13 13 13 9 17 4 13 15 10 17 4 | 20 22 20 19 24 15 20 22 17 14 17
3E | 8 14 11 11 11 6 16 11 8 21 4 | 53 55 51 49 51 48 55 50 54 50 51
4 | 10 8 9 9 11 3 9 9 7 12 3 | 15 16 17 16 17 15 17 13 16 14 14
5 | 10 10 8 10 13 5 12 13 9 13 4 | 22 25 23 29 30 21 23 27 18 25 23
6 | 18 27 11 26 83 13 31 21 16 32 9 | 54 46 55 49 78 50 67 47 51 54 52
7 | 8 16 8 10 20 6 15 10 9 11 4 | 46 44 39 47 42 42 44 44 40 40 42
8 | 8 11 9 13 12 4 9 9 7 19 3 | 48 45 47 46 48 46 44 43 47 48 45
X9 | 12 22 --- --- 26 23 --- 25 45 --- 14 | 127 127 --- --- 118 132 --- 133 135 --- 126
10 | 8 8 6 14 16 4 8 9 9 12 3 | 18 14 14 15 16 17 15 14 15 16 16
11 | 9 12 14 6 24 5 10 15 11 13 4 | 15 22 20 19 34 15 20 21 21 15 17
12 | 8 12 11 11 18 6 11 25 16 13 5 | 24 28 23 30 32 21 23 26 29 24 22
13 | 11 14 12 11 20 5 11 11 12 15 4 | 30 28 21 31 40 25 25 27 28 24 25
14 | 12 11 11 14 17 4 13 10 9 14 4 | 33 30 26 34 41 27 25 31 32 30 29
15 | 10 13 15 11 20 5 18 13 11 17 5 | 24 28 23 26 36 22 23 24 20 22 22
16 | 16 13 11 14 13 5 17 12 7 20 5 | 32 28 22 29 30 23 27 26 26 21 25
17E | 11 14 8 10 23 6 14 9 11 13 4 | 34 30 25 32 31 28 30 29 31 24 28
18 | 8 9 10 16 11 4 8 13 12 17 4 | 17 22 19 23 26 18 18 25 18 21 19
19E | 7 18 7 10 12 5 16 13 9 15 4 | 40 44 39 39 43 39 36 42 41 35 39
20 | 11 8 8 11 14 5 9 10 9 18 3 | 30 21 21 29 25 23 19 24 23 21 22
21 | 11 15 13 9 20 5 15 10 12 17 5 | 17 22 18 13 23 13 20 13 20 18 13
22 | 9 9 10 8 11 2 10 8 7 9 3 | 21 25 21 25 29 22 23 26 21 21 22
23 | 11 14 11 11 13 5 14 11 13 20 4 | 32 28 22 32 37 27 25 27 33 25 27
24E | 9 13 13 6 15 5 11 8 12 10 4 | 35 34 37 30 39 31 35 34 34 37 34
25 | 10 12 14 9 12 4 14 15 10 13 4 | 29 29 28 32 33 26 32 26 26 26 27
26 | 10 8 10 8 16 3 9 8 12 20 4 | 29 27 25 26 32 24 25 26 22 30 25
X27E | 8 11 13 13 --- 6 16 10 10 14 4 | 34 29 37 34 --- 31 35 33 32 33 32
28 | 11 10 10 14 16 5 11 9 11 16 4 | 26 31 28 34 32 26 32 29 26 25 27
29E | 9 18 9 13 18 4 19 10 14 11 5 | 36 29 31 38 31 30 28 34 37 27 32
X30 | 5 8 12 6 --- 4 11 9 8 12 3 | 41 42 45 41 --- 41 41 38 39 39 40
31 | 9 10 11 8 16 6 16 11 10 10 4 | 23 23 17 25 30 17 25 22 25 19 20
32 | 5 6 9 7 10 4 10 8 10 14 3 | 24 22 18 25 26 18 22 21 22 15 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 11 12 22 5 14 12 11 16 |T 33 32 27 30 36 30 29 32 32 27 30
WRMS | 10 12 10 10 14 5 14 11 9 15 |NE 26 26 24 27 32 23 26 25 25 24 24
MEDI | 9 12 11 11 16 5 13 10 10 14 |MD 30 28 23 30 32 25 25 27 26 25 25
Table 3.1800.3 GPS week: 1800 Day: 3 MJD: 56847.000
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 11 13 9 12 5 12 11 13 12 4 | 39 36 41 35 36 36 38 39 38 34 36
2 | 12 13 12 8 18 4 11 15 10 16 4 | 23 26 23 21 24 18 23 21 22 18 20
3E | 11 15 11 9 16 9 15 10 9 22 4 | 78 81 77 75 79 75 81 77 79 78 77
4 | 9 8 11 5 11 5 7 9 8 9 3 | 22 19 20 19 19 18 18 18 20 17 18
5 | 17 9 9 9 12 5 10 14 16 13 4 | 34 28 25 30 32 23 23 32 27 26 27
6 | 15 25 14 23 85 13 33 21 14 29 9 | 87 42 86 87 104 82 91 83 89 86 86
7E | 11 13 9 12 15 6 14 15 11 10 4 | 39 40 34 35 42 36 38 39 36 36 36
8 | 11 8 11 13 12 4 9 9 11 17 4 | 58 56 55 59 60 56 55 55 57 57 56
X9E | 29 22 17 --- 20 16 --- 72 40 --- 14 | 216 227 43 --- 283 219 --- 219 227 --- 223
10 | 10 8 7 10 16 3 8 8 12 10 3 | 13 16 13 16 18 11 14 15 17 14 11
11 | 8 12 16 7 22 6 12 12 9 12 4 | 24 24 26 23 35 20 22 22 27 17 22
12 | 9 13 8 14 19 6 12 24 11 14 5 | 31 31 29 33 35 28 27 30 29 28 27
13 | 10 12 13 9 19 4 12 9 10 15 4 | 33 33 27 36 46 30 32 32 32 28 31
14 | 9 9 11 11 17 4 12 10 9 17 4 | 33 30 27 34 42 30 27 35 32 34 30
15 | 10 13 12 12 19 7 12 12 11 22 4 | 26 30 20 29 39 20 24 28 24 24 24
16 | 9 11 12 14 15 5 13 10 12 21 4 | 32 30 26 34 35 27 28 30 31 29 28
17E | 15 13 10 9 18 6 16 9 11 14 4 | 44 35 31 38 35 32 37 36 37 28 35
18 | 10 6 10 13 11 6 6 16 10 14 4 | 26 25 23 23 28 25 24 31 29 23 25
19E | 9 14 8 6 13 5 14 14 9 11 4 | 45 43 40 43 46 38 37 45 41 37 41
20 | 8 8 10 9 13 6 8 11 10 18 3 | 26 28 27 33 30 28 26 30 25 28 27
21 | 11 13 12 10 18 7 13 13 12 17 4 | 19 23 20 19 28 19 20 18 16 19 16
22 | 8 6 10 9 10 4 9 10 10 11 3 | 30 29 27 29 31 28 29 32 28 25 28
23 | 7 12 12 9 14 4 12 9 10 18 4 | 34 35 27 35 43 30 31 34 32 29 31
24E | 11 14 13 8 14 6 13 10 7 10 4 | 38 42 41 35 40 37 38 36 36 38 37
25 | 9 9 11 12 13 5 11 10 12 14 4 | 36 31 34 37 36 30 34 32 32 30 32
26 | 12 12 11 5 11 6 8 7 9 17 3 | 29 28 23 26 29 23 23 27 20 29 24
X27E | 9 13 13 9 --- 5 12 9 9 14 4 | 41 34 42 37 --- 35 34 36 38 36 36
28 | 17 10 11 13 16 7 11 11 9 21 4 | 31 36 30 39 38 30 35 35 32 34 32
29E | 8 17 6 16 17 6 17 11 9 9 5 | 40 35 36 43 37 34 37 37 39 33 36
X30 | 10 7 11 6 --- 5 10 10 10 11 4 | 35 36 38 32 --- 34 35 32 36 31 34
31E | 11 7 9 12 17 5 17 14 10 9 4 | 31 30 24 28 36 24 27 20 33 20 26
32 | 10 6 10 9 14 4 8 9 10 15 3 | 24 27 21 24 30 23 26 28 23 19 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 11 11 22 6 13 12 11 16 |T 41 39 33 35 47 37 33 40 40 31 38
WRMS | 11 11 10 10 15 6 13 11 10 15 |NE 32 30 29 32 37 28 30 32 31 29 29
MEDI | 10 12 11 9 15 5 12 10 10 14 |MD 33 31 27 34 36 30 29 32 32 29 30
Table 3.1800.4 GPS week: 1800 Day: 4 MJD: 56848.000
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 13 15 9 13 5 13 8 10 10 4 | 34 30 36 26 33 30 33 32 36 26 30
2 | 9 12 10 9 17 5 10 11 11 19 4 | 21 26 19 21 24 17 21 21 23 18 19
3E | 10 15 13 10 14 9 17 10 9 23 4 | 53 54 55 48 55 51 52 52 50 55 52
4 | 6 9 11 8 11 4 11 10 9 15 3 | 17 19 20 16 20 17 18 18 22 16 16
5 | 8 9 8 10 12 4 12 13 10 15 3 | 26 29 22 31 33 23 25 29 26 28 26
6 | 14 25 10 22 87 7 28 21 15 31 8 | 56 43 51 56 63 54 67 55 48 56 55
7E | 8 14 9 9 18 6 14 10 18 13 4 | 34 37 28 32 40 30 33 31 33 33 31
8 | 9 10 8 9 12 5 7 9 17 19 4 | 34 33 30 31 39 31 31 32 31 37 32
X9E | 29 19 21 --- 200 17 --- 20 29 --- 12 | 130 119 38 --- 170 114 --- 111 114 --- 118
X10 | 2 --- --- --- --- 28 --- --- --- --- 0 | 26 --- --- --- --- 16 --- --- --- --- 27
11 | 7 13 15 5 25 5 12 10 7 15 4 | 20 23 21 20 36 18 21 17 26 15 18
12 | 7 12 9 13 18 5 15 23 12 15 5 | 29 32 26 31 31 25 26 28 28 27 25
13 | 7 12 12 11 20 4 12 8 9 17 4 | 26 30 21 30 42 25 26 24 24 26 25
14 | 11 10 12 10 16 3 14 12 10 17 4 | 27 28 26 29 40 25 26 32 25 30 26
15 | 8 15 12 10 18 4 17 15 15 18 5 | 28 29 19 26 37 21 25 23 27 21 23
16 | 9 12 12 14 14 6 11 7 10 22 4 | 31 31 26 33 30 26 29 28 34 32 28
17E | 7 16 8 12 18 5 17 10 11 19 4 | 31 34 26 33 40 28 27 31 34 28 29
18 | 6 8 10 11 8 4 11 14 11 14 3 | 18 19 22 19 24 19 22 23 21 17 19
19E | 8 11 7 8 14 6 13 11 7 13 3 | 36 38 35 40 43 35 36 39 40 36 36
20 | 8 9 10 10 15 4 10 8 12 20 3 | 25 22 20 26 27 22 22 22 27 25 21
21 | 8 13 13 10 16 5 15 14 17 16 5 | 26 30 29 28 35 28 28 30 24 31 26
22 | 6 6 9 7 9 4 10 11 9 11 3 | 23 24 24 22 27 22 27 28 22 22 23
23 | 7 11 13 12 15 4 13 9 13 20 4 | 26 32 22 32 38 25 26 25 26 24 25
24E | 9 11 13 8 20 5 17 9 11 12 4 | 31 28 29 28 32 27 30 27 30 29 27
25 | 7 8 12 8 11 3 13 11 8 12 3 | 29 28 30 31 26 27 29 27 27 27 27
26 | 8 10 10 7 13 3 11 7 13 16 3 | 29 28 25 23 35 24 23 26 22 28 24
X27E | 9 13 13 8 --- 5 16 7 5 11 4 | 31 29 35 31 --- 30 36 29 34 30 31
28 | 11 10 12 14 18 6 12 10 13 18 4 | 29 34 25 36 36 26 27 31 31 29 28
29E | 9 18 7 14 22 3 19 12 13 10 5 | 35 33 31 39 31 31 34 32 37 31 32
X30 | 9 9 12 5 --- 5 13 8 15 11 4 | 63 64 66 64 --- 64 64 65 66 64 64
31E | 10 9 9 9 19 5 17 12 12 11 4 | 28 30 25 26 36 24 32 30 28 31 27
32 | 8 5 8 6 13 3 7 8 11 14 3 | 21 23 18 19 29 19 23 20 24 18 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 11 11 23 5 14 12 12 17 |T 33 34 29 30 39 30 30 32 33 29 31
WRMS | 8 12 11 11 18 5 13 11 10 16 |NE 27 28 25 27 33 24 27 27 27 26 25
MEDI | 8 11 11 9 16 5 13 10 11 15 |MD 29 30 26 30 35 25 27 29 28 28 27
Table 3.1800.5 GPS week: 1800 Day: 5 MJD: 56849.000
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 | 9 12 12 10 13 4 11 10 7 8 4 | 32 36 35 31 33 32 38 35 35 26 33
2 | 11 11 12 9 17 4 11 10 7 17 4 | 21 24 18 19 25 16 20 20 19 13 18
3E | 11 18 14 14 17 10 17 13 11 21 5 | 88 90 89 85 93 86 88 87 84 89 87
4 | 6 11 11 5 13 4 10 9 11 12 3 | 16 21 18 17 17 15 17 20 17 11 16
5 | 10 12 10 8 15 4 10 12 8 16 4 | 27 29 23 30 30 24 22 26 30 25 26
6 | 15 29 12 21 83 9 30 26 14 32 8 | 80 42 80 86 85 82 90 84 82 85 82
7E | 10 14 9 11 19 5 13 14 10 10 4 | 26 28 17 26 33 20 24 24 25 19 23
8 | 8 12 12 9 11 4 9 9 11 20 3 | 52 52 51 49 52 50 49 50 53 52 50
X9E | 29 22 16 --- 43 9 --- 15 18 --- 11 | 176 186 37 --- 126 176 --- 182 185 --- 180
10 | 5 7 7 8 15 4 7 9 8 10 3 | 19 16 17 12 14 18 14 17 15 15 18
11 | 9 9 14 10 21 4 10 11 9 11 4 | 21 24 22 26 35 21 23 16 26 16 21
12 | 9 13 9 16 18 3 12 25 10 17 5 | 24 29 21 30 30 22 24 24 26 20 22
13 | 8 12 12 9 21 5 13 13 9 12 4 | 23 27 19 23 38 21 25 23 23 22 22
14 | 8 12 10 10 16 4 13 11 13 19 4 | 24 27 23 26 34 23 25 28 25 29 23
15 | 9 15 12 9 18 6 15 17 12 17 5 | 25 31 20 25 35 21 24 28 24 16 23
16 | 9 15 12 11 15 6 12 12 13 23 4 | 25 29 21 27 27 22 25 24 28 23 23
17E | 6 15 9 9 41 5 16 11 8 13 5 | 29 33 22 32 37 28 28 30 31 21 27
18 | 8 9 10 13 10 3 8 14 9 16 4 | 21 21 22 19 24 18 20 23 22 15 19
19E | 9 12 8 8 13 4 12 15 10 11 4 | 36 39 35 40 38 35 33 38 38 32 36
20 | 7 9 8 10 16 6 8 9 10 17 3 | 27 23 21 29 23 24 22 26 29 26 24
21 | 11 16 12 9 18 4 14 14 10 14 4 | 23 27 27 24 22 22 27 21 29 23 22
22 | 6 8 11 9 9 4 7 12 8 9 3 | 18 19 21 18 24 18 20 25 23 17 19
23 | 10 13 11 8 15 6 13 15 12 19 4 | 27 30 21 25 34 22 25 25 28 22 24
24E | 8 10 13 10 19 3 14 10 11 15 4 | 24 24 28 24 27 23 26 24 26 22 23
25 | 10 8 11 8 13 4 12 11 10 16 4 | 26 26 27 28 27 23 28 24 25 23 25
26 | 8 14 11 7 16 4 10 6 11 14 4 | 25 25 21 21 28 22 24 22 21 23 21
X27E | 9 13 12 9 --- 6 15 10 13 11 4 | 32 24 34 32 --- 28 29 28 30 27 29
28 | 10 9 11 13 15 5 10 11 9 16 4 | 26 30 24 33 33 26 29 32 32 26 27
29E | 11 23 8 15 20 5 19 12 13 10 5 | 28 30 27 34 29 28 29 30 31 25 27
X30 | 14 12 13 8 --- 6 14 9 10 10 5 | 107 108 107 109 --- 104 110 108 109 106 107
31E | 12 9 8 9 17 6 21 14 13 10 5 | 22 21 14 19 28 16 24 20 24 15 17
32 | 5 7 9 8 9 3 7 11 7 12 3 | 20 25 19 17 24 19 22 23 26 17 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 11 23 5 13 13 10 16 |T 36 37 30 32 36 34 32 37 38 29 35
WRMS | 9 13 10 9 16 5 13 12 9 14 |NE 27 27 25 27 31 25 27 28 29 24 26
MEDI | 9 12 11 9 16 4 12 11 10 14 |MD 25 27 22 26 30 22 25 25 26 23 23
Table 3.1800.6 GPS week: 1800 Day: 6 MJD: 56850.000
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 13 13 10 14 4 11 10 10 10 4 | 40 39 42 36 38 37 43 42 39 31 39
2 | 9 12 11 7 20 5 10 10 7 15 4 | 23 27 22 23 28 19 23 23 23 15 21
3E | 8 21 13 14 15 9 14 10 15 24 5 | 73 75 71 74 70 71 71 72 72 71 71
4 | 6 10 11 7 15 4 11 11 9 10 3 | 19 20 19 18 22 16 18 19 23 14 17
5 | 14 12 8 10 17 7 11 9 13 16 4 | 31 32 31 41 43 34 26 36 35 33 32
6 | 12 26 7 22 74 11 35 25 13 29 8 | 71 45 73 79 80 69 78 78 73 73 73
7E | 8 14 7 10 18 5 16 11 8 11 4 | 32 33 26 31 38 26 28 29 30 30 29
8 | 6 9 9 10 13 5 12 10 10 21 3 | 52 51 53 49 51 49 52 50 55 54 51
X9E | 18 24 19 --- 205 15 --- 23 35 --- 12 | 165 177 36 --- 195 169 --- 176 175 --- 172
10 | 9 9 6 7 21 6 9 10 8 11 3 | 24 20 17 13 16 23 16 21 20 16 23
11 | 5 11 13 5 24 4 11 13 7 11 4 | 22 26 22 22 37 19 24 20 23 14 21
12 | 8 15 8 13 20 6 14 25 10 17 5 | 29 30 26 34 34 26 27 28 28 25 26
13 | 8 11 12 9 20 5 13 10 8 16 4 | 32 33 27 35 48 30 30 30 36 25 31
14 | 11 13 11 11 19 4 14 12 10 17 4 | 32 32 29 36 47 31 29 38 37 35 33
15 | 9 15 12 11 21 6 16 14 11 16 5 | 31 33 25 34 41 24 27 31 26 21 28
16 | 9 15 11 12 17 7 12 10 14 21 4 | 26 28 23 31 30 24 28 28 29 26 25
17E | 7 17 10 9 19 5 16 13 8 12 4 | 35 35 29 39 37 32 31 35 35 26 33
18 | 11 8 10 15 12 3 10 15 13 18 4 | 26 28 25 24 36 25 27 34 34 28 26
19E | 7 12 7 11 19 4 12 13 14 11 4 | 37 40 38 44 43 37 36 43 40 35 39
20 | 7 10 10 12 13 3 9 10 10 18 3 | 34 28 28 38 34 30 26 33 36 29 31
21 | 13 14 13 12 22 6 15 14 10 17 5 | 22 29 18 18 35 18 25 26 22 21 20
22 | 7 8 9 9 11 3 9 13 9 9 3 | 29 30 28 29 39 28 29 37 33 28 30
23 | 8 13 12 11 15 5 13 12 10 18 4 | 33 35 28 36 45 30 30 32 37 25 32
24E | 8 11 13 9 15 2 14 11 12 13 4 | 39 37 41 38 38 36 38 38 35 38 37
25 | 9 13 10 7 17 4 14 11 7 15 4 | 31 29 30 32 33 29 32 31 29 29 29
26 | 6 11 10 9 15 6 9 8 12 16 3 | 29 30 28 28 38 28 27 27 26 30 27
X27E | 10 15 14 6 --- 5 14 9 11 11 4 | 34 31 38 35 --- 33 35 34 36 32 33
28 | 8 11 11 14 18 6 11 10 11 16 4 | 30 37 32 44 38 33 34 37 34 29 33
29E | 9 16 9 13 24 4 20 13 11 11 5 | 45 40 39 45 40 41 42 40 44 35 40
X30E | 8 13 12 6 --- 6 14 9 8 9 4 | 57 61 60 60 --- 57 61 59 59 57 59
31E | 11 11 9 10 14 6 19 12 17 12 5 | 26 26 19 21 29 19 27 22 27 22 21
32 | 9 9 9 8 14 3 7 11 6 11 3 | 28 27 23 26 35 23 28 27 26 19 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 10 11 22 5 14 13 11 16 |T 38 38 32 35 44 36 33 39 39 31 37
WRMS | 9 13 10 10 17 5 14 12 9 14 |NE 31 31 29 33 38 29 30 33 32 28 30
MEDI | 8 12 10 10 17 5 13 11 10 15 |MD 31 32 28 35 38 30 29 33 34 29 31
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 4.1800 GPS week: 1800 MJD: 56844.0-56850.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3018 |U 6 9 17 |U 5 6 19 |U 10 10 19 |
emr | emr 3018 | 8 9 20 |U 6 6 18 | 11 10 21 |
esa | esa 3017 | 7 8 17 |U 5 6 18 | 12 11 21 |
gfz | gfz 2958 |U 6 9 17 |U 6 9 28 |U 11 10 20 |
grg | grg 2866 |U 11 14 26 |U 8 9 38 |U 13 12 24 |
igr | igr 3005 | 6 8 18 | 4 5 16 | 11 11 21 |
igs | igs 2999 | 6 8 17 | 4 5 18 | 11 10 20 |
jpl | jpl 2959 | 8 9 22 |U 5 6 21 |U 11 11 21 |
mit | mit 3058 | 6 7 18 |U 5 7 24 |U 11 11 23 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1800.0 GPS week: 1800 Day: 0 MJD: 56844.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 8 14 20 | 5 6 19 | 9 8 16 |
emr | emr 2961 | 11 13 21 | 5 7 21 | 9 7 18 |
esa | esa 2976 | 8 13 17 | 6 7 21 | 9 8 16 |
gfz | gfz 2973 | 8 13 19 | 6 7 24 | 10 9 18 |
grg | grg 2880 | 12 17 27 | 7 6 33 | 11 8 21 |
igr | igr 3028 | 8 12 18 | 5 6 18 | 8 9 17 |
igs | igs 3007 | 8 13 17 | 5 6 21 | 9 8 16 |
jpl | jpl 2972 | 9 11 22 | 6 6 22 | 9 9 19 |
mit | mit 3072 | 8 14 19 | 6 6 20 | 10 9 19 |
Table 5.1800.1 GPS week: 1800 Day: 1 MJD: 56845.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 6 6 19 | 4 5 19 | 9 9 21 |
emr | emr 2968 | 9 7 21 | 6 4 15 | 10 10 23 |
esa | esa 2976 | 6 5 18 | 5 6 22 | 11 11 22 |
gfz | gfz 2972 | 6 5 20 | 5 7 21 | 9 10 22 |
grg | grg 2880 | 14 14 29 | 7 6 28 | 11 13 26 |
igr | igr 3029 | 6 5 21 | 5 4 17 | 9 12 24 |
igs | igs 3013 | 7 4 19 | 4 4 20 | 10 10 23 |
jpl | jpl 2972 | 8 7 22 | 5 6 22 | 10 11 26 |
mit | mit 3072 | 6 5 18 | 5 6 27 | 11 14 25 |
Table 5.1800.2 GPS week: 1800 Day: 2 MJD: 56846.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 5 9 16 | 4 6 16 | 12 11 23 |
emr | emr 3065 | 7 9 22 | 5 5 14 | 13 11 22 |
esa | esa 2976 | 6 8 18 | 4 6 13 | 13 11 23 |
gfz | gfz 2972 | 5 8 15 | 4 5 16 | 11 10 22 |
grg | grg 2880 | 8 11 21 | 5 6 26 | 16 13 28 |
igr | igr 3053 | 5 7 15 | 4 5 13 | 12 10 23 |
igs | igs 3015 | 5 9 17 | 4 4 16 | 13 11 22 |
jpl | jpl 2972 | 6 8 19 | 5 5 17 | 13 12 23 |
mit | mit 3072 | 5 8 17 | 4 6 21 | 14 13 24 |
Table 5.1800.3 GPS week: 1800 Day: 3 MJD: 56847.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 5 6 16 | 5 6 18 | 12 11 21 |
emr | emr 3063 | 7 7 18 | 7 6 22 | 15 10 23 |
esa | esa 3072 | 6 5 15 | 6 7 18 | 14 11 24 |
gfz | gfz 2972 | 5 6 15 | 5 6 20 | 12 12 22 |
grg | grg 2880 | 8 5 19 | 9 8 39 | 13 11 24 |
igr | igr 3028 | 5 6 18 | 5 6 18 | 13 12 22 |
igs | igs 2989 | 5 5 15 | 5 5 19 | 13 11 23 |
jpl | jpl 2972 | 6 8 20 | 5 6 21 | 13 11 25 |
mit | mit 3072 | 5 5 15 | 6 7 25 | 12 11 26 |
Table 5.1800.4 GPS week: 1800 Day: 4 MJD: 56848.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2933 | 7 8 20 | 6 8 16 | 10 8 19 |
emr | emr 2962 | 10 11 18 | 7 6 15 | 11 11 19 |
esa | esa 2976 | 8 9 20 | 5 8 13 | 12 11 18 |
gfz | gfz 2876 | 7 8 22 | 5 8 18 | 11 10 20 |
grg | grg 2784 | 15 22 36 | 9 7 31 | 15 14 27 |
igr | igr 2880 | 8 8 21 | 4 7 13 | 12 10 20 |
igs | igs 2875 | 7 8 18 | 5 6 15 | 11 9 18 |
jpl | jpl 2876 | 11 11 24 | 6 8 20 | 12 10 19 |
mit | mit 2976 | 7 8 21 | 6 9 29 | 11 9 19 |
Table 5.1800.5 GPS week: 1800 Day: 5 MJD: 56849.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 7 9 15 | 5 6 19 | 10 14 20 |
emr | emr 3047 | 8 9 22 | 7 7 21 | 11 15 20 |
esa | esa 3072 | 7 8 16 | 4 7 16 | 11 14 20 |
gfz | gfz 2972 | 8 12 16 | 5 8 25 | 11 13 18 |
grg | grg 2880 | 9 10 20 | 7 9 31 | 14 15 20 |
igr | igr 3016 | 7 8 15 | 4 5 17 | 11 15 19 |
igs | igs 3040 | 7 8 16 | 4 5 17 | 11 14 19 |
jpl | jpl 2974 | 10 9 24 | 5 7 21 | 12 14 19 |
mit | mit 3072 | 7 7 17 | 6 7 20 | 10 14 19 |
Table 5.1800.6 GPS week: 1800 Day: 6 MJD: 56850.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 5 8 16 | 4 7 22 | 9 8 17 |
emr | emr 3062 | 7 7 20 | 7 6 19 | 11 10 21 |
esa | esa 3072 | 6 7 17 | 5 5 19 | 12 11 21 |
gfz | gfz 2972 | 5 9 16 | 14 26 77 | 10 9 19 |
grg | grg 2880 | 12 21 30 | 15 23 81 | 13 12 22 |
igr | igr 3002 | 5 9 17 | 4 5 16 | 10 9 21 |
igs | igs 3054 | 5 8 16 | 4 4 16 | 10 9 19 |
jpl | jpl 2976 | 7 9 20 | 4 6 24 | 10 9 19 |
mit | mit 3072 | 4 5 18 | 6 6 24 | 12 10 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 6.1800 GPS week: 1800 MJD: 56844.500-56850.500
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 -5 -13 -145 -1 | 19 24
| 23 19 48 106 4 | 3
emr uuuuu | 52 -16 94 126 -1 | 30 34
| 18 14 48 51 7 | 4
esa uuuuu | -6 1 -19 70 1 | 14 19
| 19 14 44 43 1 | 4
gfz uuuuu | -4 1 -35 -117 4 | 10 18
| 23 39 131 146 3 | 5
grg uuuxu | 67 -36 8 563 -16 | 31 34
| 9 16 73 93 4 | 3
igr xxxxx | -2 -10 -36 47 0 | 6 15
| 7 14 42 28 3 | 4
irf xxxxx | 10 -7 -11 -7 -3 | 1 13
| 9 13 39 30 2 | 2
jpl uuuuu | -16 29 17 44 8 | 12 21
| 24 30 80 47 8 | 6
mit uuuuu | 5 14 -31 -93 -5 | 17 21
| 17 25 96 78 4 | 2
ngs uuuuu | -31 0 -3 145 -2 | 6 14
| 55 59 137 182 3 | 2
sio xxxxx | 13 33 21 87 2 | 38 40
| 24 24 37 38 6 | 4
Table 7.1800.0 GPS week: 1800 Day: 0 MJD: 56844.500
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 | -55 10 3 -158 5 | 15 22
emr uuuuu | 55 -10 148 129 -3 | 27 32
esa uuuuu | -15 -1 51 62 0 | 11 17
gfz uuuuu | -15 -31 85 -279 4 | 5 15
grg uuuxu | 78 -18 -22 392 -10 | 33 36
igr xxxxx | -5 -1 -50 8 4 | 2 14
irf xxxxx | 10 16 -55 8 -2 | 1 13
jpl uuuuu | -45 -11 17 -23 0 | 6 19
mit uuuuu | 21 50 -176 -58 -6 | 18 22
ngs uuuuu | 17 -3 -129 361 -1 | 6 14
sio xxxxx | 63 26 -37 147 6 | 36 38
Table 7.1800.1 GPS week: 1800 Day: 1 MJD: 56845.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -52 1 -58 -307 -5 | 19 24
emr uuuuu | 77 -27 145 223 -4 | 30 34
esa uuuuu | -8 -2 11 57 2 | 13 19
gfz uuuuu | -49 -62 80 -314 11 | 8 16
grg uuuxu | 68 -17 -67 573 -16 | 34 37
igr xxxxx | -1 -32 4 54 3 | 5 14
irf xxxxx | 22 -17 19 19 -3 | 3 13
jpl uuuuu | -11 14 -106 83 -4 | 9 20
mit uuuuu | 27 3 24 -3 -6 | 19 23
ngs uuuuu | -1 78 -35 379 -1 | 7 14
sio xxxxx | 12 4 46 74 3 | 37 40
Table 7.1800.2 GPS week: 1800 Day: 2 MJD: 56846.500
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 1 20 -247 -2 | 19 24
emr uuuuu | 38 10 8 147 -2 | 30 34
esa uuuuu | -7 0 0 84 1 | 14 19
gfz uuuuu | 21 6 120 -214 4 | 10 18
grg uuuxu | 60 -38 93 560 -16 | 33 36
igr xxxxx | -4 -22 25 48 -3 | 6 15
irf xxxxx | 0 -6 5 4 -5 | 2 13
jpl uuuuu | -12 53 -57 99 17 | 9 20
mit uuuuu | -21 16 -6 -68 -7 | 18 22
ngs uuuuu | -25 -50 -151 255 -5 | 7 14
sio xxxxx | 11 20 -17 116 10 | 37 39
Table 7.1800.3 GPS week: 1800 Day: 3 MJD: 56847.500
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 | -44 -38 46 -133 5 | 15 21
emr uuuuu | 39 -24 90 104 -8 | 25 29
esa uuuuu | 17 12 -79 63 2 | 11 16
gfz uuuuu | 10 18 -61 -21 3 | 7 16
grg uuuxu | 74 -50 55 646 -17 | 28 31
igr xxxxx | 5 -19 -11 94 -1 | 2 14
irf xxxxx | 10 -16 5 3 -4 | -2 12
jpl uuuuu | 17 28 23 58 5 | 7 17
mit uuuuu | -10 -24 24 -53 -10 | 13 18
ngs uuuuu | -70 62 -73 -11 1 | 2 11
sio xxxxx | 3 7 67 77 -5 | 35 37
Table 7.1800.4 GPS week: 1800 Day: 4 MJD: 56848.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -12 1 -45 -55 0 | 17 22
emr uuuuu | 76 -11 80 117 11 | 26 30
esa uuuuu | 3 -23 -52 71 0 | 12 17
gfz uuuuu | 2 37 -216 21 4 | 9 17
grg uuuxu | 72 -62 93 684 -11 | 27 31
igr xxxxx | -6 3 -71 33 1 | 4 14
irf xxxxx | 21 -16 45 18 -2 | -1 12
jpl uuuuu | 2 68 115 -13 16 | 10 17
mit uuuuu | 14 0 109 -84 -4 | 14 18
ngs uuuuu | -137 -30 41 -50 -7 | 4 11
sio xxxxx | 6 58 28 98 -6 | 37 39
Table 7.1800.5 GPS week: 1800 Day: 5 MJD: 56849.500
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 -24 -82 -110 -5 | 23 28
emr uuuuu | 45 -20 72 102 5 | 33 37
esa uuuuu | 11 22 -47 150 2 | 18 23
gfz uuuuu | 7 49 -153 1 1 | 16 22
grg uuuxu | 51 -37 -13 528 -22 | 31 34
igr xxxxx | 7 0 -70 66 0 | 10 18
irf xxxxx | 4 5 -49 -49 -3 | 4 15
jpl uuuuu | -14 52 106 31 11 | 19 24
mit uuuuu | -3 41 -101 -243 -5 | 18 23
ngs uuuuu | -17 -82 238 61 1 | 7 15
sio xxxxx | 3 61 44 73 2 | 42 43
Table 7.1800.6 GPS week: 1800 Day: 6 MJD: 56850.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 15 24 -2 -2 | 24 29
emr uuuuu | 34 -30 113 58 -6 | 37 40
esa uuuuu | -42 1 -18 5 1 | 20 24
gfz uuuuu | -8 -13 -99 -12 3 | 18 24
grg uuuxu | 63 -33 -82 556 -17 | 28 32
igr xxxxx | -13 -2 -82 26 -2 | 11 19
irf xxxxx | 0 -14 -47 -50 1 | 4 15
jpl uuuuu | -50 -3 22 73 12 | 23 28
mit uuuuu | 6 12 -90 -141 4 | 18 23
ngs uuuuu | 14 28 91 20 -2 | 9 17
sio xxxxx | -11 53 16 27 5 | 45 46
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