[IGSREPORT-22946] Wk 1803 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Mon Aug 18 07:17:00 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1803 (Jul 27, 2014 - Aug 02, 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:
igs1803[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1803[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1803[0-6].cls IGS GPS clock combination summary report.
igs18037.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18037.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 | 8
0 | ESA | 8 DRAG
0 | GFZ | 1 2 6 8 12 30 1 6 8 12 30 WUHN
0 | GRG | 6 6 FAA1 IRKJ FAA1 IRKJ
0 | MIT | 24 MATE GOPE MATE MDVJ
1 | COD | GRAZ
1 | EMR | 1 1 8
1 | ESA | UNSA
1 | GFZ | 1 2 6 30 1 6 30 BAKE CHUR GRAS BAKE CHUR GRAS
1 | GRG | 6 6 8 FAA1 GLPS GRAZ IRKJ FAA1 GLPS IRKJ NRMD
1 | JPL | 3 8 29
1 | MIT | 22 24 8 22 24 26 MDVJ SUWN
2 | COD | 8 NRMD NRMD
2 | ESA | 8 UNSA
2 | GFZ | 1 6 8 30 1 6 8 30 INVK KELY INVK KELY
2 | GRG | 6 6 ASPA KELY KOKB KOUC
2 | JPL | 22 TIXI
2 | MIT | 26
3 | COD | 8
3 | ESA | 8 DUBO DUBO TLSE
3 | GFZ | 1 2 6 30 1 6 8 30 TLSE GODE TLSE
3 | GRG | 6 6 KOUC MAL2 ADIS KOUC MAL2
3 | JPL | 8
3 | MIT | 31
4 | COD | 8
4 | ESA | 8 KARR KARR UNSA
4 | GFZ | 1 2 6 8 30 1 6 8 30 NRMD REUN REUN
4 | GRG | 6 6 FAA1 IRKJ KARR KOUC REUN FAA1 KARR KELY KOUC
4 | GRG | REUN
4 | JPL | 7 IRKJ
4 | MIT | FLIN MDVJ MONP WTZR
5 | COD | 31 31 HOB2 NRMD HOB2 NKLG NRMD
5 | EMR | 8
5 | GFZ | 1 2 6 30 1 6 30 BAKE MATE BAKE MATE
5 | GRG | 6 6 8 BRST IRKJ KOUC MONP BRST IRKJ KOUC MATE
5 | JPL | 8 27
5 | MIT | 8 MATE MATE MONP
6 | COD | 8
6 | ESA | 8
6 | GFZ | 1 2 6 8 30 1 6 8 30
6 | GRG | 6 6
6 | JPL | 8 27 TIXI
6 | MIT | GRAZ MATE
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | GRG | 6
6 | ESA | 30
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G08 | | | | | | 4 | 4 |
PRN G30 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.3 -.7 -1.4 -49 16 -53 .18
EMR | 0 | 10.0 .7 6.1 -28 6 -38 -.32
ESA | 0 | -.3 -.5 -1.4 -1 -20 21 -.04
GFZ | 0 | .3 .1 -.9 -9 -41 -20 -.42
GRG | 0 | 11.9 -11.7 23.4 -14 34 -22 .39
JPL | 0 | 8.2 -2.0 4.2 -107 29 -9 -.89
MIT | 0 | .7 -7.7 5.4 6 9 -57 .28
NGS | 0 | -.6 -.4 -3.9 33 9 1 .32
SIO | 0 | 2.9 -7.8 8.7 7 9 -21 .17
COD | 1 | -.2 .2 -.7 -27 4 -24 .17
EMR | 1 | 13.8 -2.1 2.7 -29 4 -42 -.06
ESA | 1 | -.2 -.4 -1.5 2 -21 32 -.10
GFZ | 1 | .4 .2 -.9 -19 -48 -11 -.22
GRG | 1 | 13.8 -9.0 24.4 -38 -1 -17 .78
JPL | 1 | 1.7 -1.7 2.7 -83 11 -56 -.96
MIT | 1 | 2.5 -8.2 4.5 1 16 -54 .27
NGS | 1 | -.2 -5.5 -.1 0 8 -13 .44
SIO | 1 | .3 -5.8 13.3 -11 -6 -12 .09
COD | 2 | -.6 .4 -.3 -4 4 -2 .08
EMR | 2 | .8 -4.0 .1 -34 2 -24 -.09
ESA | 2 | .1 -.8 -1.0 -6 -10 28 -.21
GFZ | 2 | .3 .4 -.5 -15 -44 -10 -.32
GRG | 2 | 14.6 -16.0 21.5 -44 18 -9 .33
JPL | 2 | .2 -4.9 11.2 -52 28 -56 -.30
MIT | 2 | -4.0 -9.1 6.6 4 12 -57 .31
NGS | 2 | -1.4 -10.9 2.0 -31 10 -31 .33
SIO | 2 | -2.4 -8.0 15.2 -5 -7 -4 .21
COD | 3 | -.2 .1 -.1 -27 12 -18 .02
EMR | 3 | -1.2 .8 -.4 -42 -12 -27 .01
ESA | 3 | -.9 .1 -1.4 -5 7 15 -.34
GFZ | 3 | .4 .5 .4 -7 -60 -11 -.59
GRG | 3 | 13.7 -7.3 5.8 -45 13 -6 .24
JPL | 3 | -2.1 .6 10.9 -106 11 9 -.94
MIT | 3 | -1.2 -10.9 3.8 5 19 -54 .26
NGS | 3 | -7.0 -9.6 6.6 -47 29 -66 .45
SIO | 3 | -3.0 -8.7 10.2 -1 -16 -9 .09
COD | 4 | -.4 .2 .0 -20 5 -26 .31
EMR | 4 | 2.4 3.4 3.8 -32 1 -35 -.02
ESA | 4 | .0 -.1 -1.6 4 -5 25 -.17
GFZ | 4 | .4 -.1 -.8 -14 -59 -7 -.24
GRG | 4 | 13.8 -9.3 14.6 -33 25 -30 .67
JPL | 4 | -11.5 -6.6 15.2 -81 15 -39 -.69
MIT | 4 | -3.9 -10.8 5.2 0 23 -58 .44
NGS | 4 | .6 -4.7 12.9 -47 -18 -9 .27
SIO | 4 | -1.8 -4.5 8.4 1 22 -5 .10
COD | 5 | -.6 .3 .5 -39 11 -37 .24
EMR | 5 | -1.7 3.8 9.7 -21 -1 -29 -.02
ESA | 5 | -.3 -.1 -.9 -30 -18 14 -.11
GFZ | 5 | .4 .3 -.3 -29 -69 -8 -.25
GRG | 5 | 8.9 -13.5 18.2 -49 24 -12 .67
JPL | 5 | -7.3 -3.0 19.9 -89 12 -6 -.66
MIT | 5 | -2.7 -7.9 6.2 0 14 -51 .34
NGS | 5 | -5.5 -7.4 11.0 -54 15 -48 .53
SIO | 5 | -2.7 -3.8 3.1 -28 6 -38 .29
COD | 6 | -.3 .0 .0 -20 17 -41 .20
EMR | 6 | .8 -2.5 9.8 -19 -1 -16 -.27
ESA | 6 | .0 .1 -1.8 8 -13 28 -.33
GFZ | 6 | .0 .6 -.7 -14 -46 -7 -.56
GRG | 6 | 9.1 -7.0 20.6 -44 8 -35 .26
JPL | 6 | -4.3 .0 18.9 -93 70 -7 -.69
MIT | 6 | -.2 -7.8 10.8 4 10 -40 .25
NGS | 6 | -3.3 -.8 18.0 -65 -14 -24 .29
SIO | 6 | .9 -3.1 4.4 -22 -5 -10 .10
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1803.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1803.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 2.1803.[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 3.1803.[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 5.1803.0-6). 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 1803 summary. (Jul 27, 2014 - Aug 02, 2014)
Table 1.1803.a GPS week: 1803 MJD: 56865.000-56871.000
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 239| 0 0 2 6 -14 6 .02 10 10 | -1434 81 16 111
| 0 1 1 22 17 10 .03 | 349 588
emr 80| 1 0 1 10 -17 47 .15 13 13 | 2544 27 14 133
| 3 1 1 10 10 13 .04 | 530 439
esa 150| 0 0 -7 7 8 -2 -.39 12 11 | -617 -302 11 177
| 1 0 1 10 10 7 .02 | 536 573
gfz 189| -1 2 -1 8 -27 -26 .07 13 11 | -360 -11 14 129
| 1 0 0 15 11 13 .04 | 524 930
grg 180| 2 0 18 15 -7 -27 .19 21 17 | -421 166 17 148
| 1 0 3 21 26 20 .04 | 243 464
igr n/a| 0 0 -1 -3 -8 -5 -.20 5 5 | 3518 517 16 94
| 0 0 0 14 8 10 .02 | 1080 567
jpl 80| 0 1 -2 -33 19 -22 -.02 12 12 | 1690 -28 17 139
| 1 1 1 12 10 8 .05 | 694 603
mit 300| 0 -1 4 -1 -21 -6 .03 14 13 | -242 18 23 193
| 1 1 1 31 26 11 .03 | 221 420
ngs 227| -1 0 -3 -10 34 8 .02 11 10 | -1448 145 1501 3099
| 0 0 3 23 17 18 .05 | 362 597
sio 451| 0 0 2 -21 -24 12 -.50 15 15 | --- --- --- ---
| 0 0 2 29 25 26 .08 | --- ---
Table 1.1803.b GPS week : 1803 MJD: 56865.000-56871.000
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 | 5 4 5 5 6 5 5 |
2 | 4 4 5 4 5 4 5 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 4 4 4 4 5 4 5 |
6 | 9 9 8 7 8 8 8 |
7 | 5 5 5 5 5 5 5 |
8 | 5 7 7 8 9 8 6 |
10 | 4 3 4 3 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 5 6 5 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 6 5 5 5 6 |
16 | 5 5 5 5 5 5 5 |
17 | 4 5 5 5 5 5 5 |
18 | 5 5 5 5 4 5 5 |
19 | 5 4 4 5 4 5 5 |
20 | 5 4 4 5 4 5 5 |
21 | 5 5 5 5 5 5 5 |
22 | 4 4 4 5 5 5 5 |
23 | 5 4 5 5 5 5 5 |
24 | 7 7 5 5 6 6 5 |
25 | 4 4 5 4 4 4 4 |
26 | 4 4 4 4 4 4 5 |
27 | 5 4 5 5 5 5 4 |
28 | 5 4 5 5 5 5 5 |
29 | 6 6 6 5 5 5 5 |
30 | 5 6 6 6 6 11 41 |
31 | 5 5 5 5 5 5 5 |
32 | 4 4 4 4 4 4 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
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 2.1803.0 GPS week: 1803 Day: 0 MJD: 56865.000
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 238| 0 0 2 -15 -37 11 .03 9 9 | -1075 -453 17 110
emr 80| 3 -1 3 22 -8 56 .13 13 13 | 3588 -670 15 142
esa 150| 0 0 -6 -2 4 -17 -.39 11 10 | -193 -1002 14 194
gfz 189| -2 3 -2 -2 -10 -7 .04 11 10 | 285 -580 13 128
grg 184| 2 0 22 35 4 4 .16 21 17 | -221 528 18 157
igr n/a| -1 0 0 0 -12 10 -.21 5 4 | 3263 -480 17 92
jpl 80| 2 0 0 -38 28 -13 .06 13 13 | 3068 -1103 17 130
mit 300| 0 -3 6 31 -24 -8 .00 17 16 | 118 -41 24 200
ngs 225| -2 0 -8 -3 42 -25 .08 11 9 | -1020 -488 1482 3281
sio 463| 1 0 3 -5 -17 65 -.45 17 15 | --- --- --- ---
Table 2.1803.1 GPS week: 1803 Day: 1 MJD: 56866.000
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 238| 0 0 3 18 -31 25 -.01 10 9 | -1569 -153 14 111
emr 80| 7 0 1 18 -20 34 .10 14 14 | 2197 634 16 119
esa 150| 0 0 -8 13 14 -2 -.38 12 11 | -1580 655 12 162
gfz 189| -2 2 -1 7 -27 -43 .09 11 9 | -786 549 12 117
grg 181| 1 0 22 16 -23 -34 .18 21 18 | -107 -343 18 151
igr n/a| -1 0 0 5 -17 -17 -.18 5 5 | 2040 1169 16 88
jpl 80| 0 1 -3 -39 32 -22 -.03 12 11 | 1106 637 17 157
mit 300| 0 -2 4 -41 5 -11 .06 16 14 | -356 97 25 195
ngs 227| -1 0 -4 -2 30 29 .08 11 9 | -1758 303 1360 3204
sio 467| 0 -1 5 -36 -16 10 -.42 16 14 | --- --- --- ---
Table 2.1803.2 GPS week: 1803 Day: 2 MJD: 56867.000
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 238| 2 0 3 9 -3 -2 -.02 10 10 | -1959 1150 17 114
emr 80| -1 -1 1 9 -7 59 .16 13 13 | 2057 352 13 129
esa 150| 2 0 -5 5 28 -2 -.40 11 11 | -749 -126 11 161
gfz 190| -2 2 -2 30 -17 -22 .11 12 10 | -849 311 13 123
grg 180| 0 -1 20 45 -55 -23 .14 22 19 | -547 184 17 153
igr n/a| 0 0 0 0 3 -11 -.21 5 5 | 2427 1129 16 91
jpl 80| -1 3 -3 -45 15 -22 -.08 12 11 | 1054 624 18 117
mit 300| 0 -1 4 22 -49 -17 .05 14 13 | -335 32 22 200
ngs 228| -1 0 -6 -55 32 0 .05 12 10 | -1942 1192 1163 3056
sio 473| 0 0 3 17 -35 6 -.40 15 15 | --- --- --- ---
Table 2.1803.3 GPS week: 1803 Day: 3 MJD: 56868.000
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 241| 0 0 0 -1 -23 -6 .05 12 11 | -1692 360 16 109
emr 80| -1 0 1 0 -25 66 .13 13 13 | 2131 -191 14 123
esa 150| 2 0 -9 19 10 -3 -.41 13 13 | -855 -685 13 180
gfz 192| 0 2 -1 24 -36 -25 .11 12 11 | -421 206 15 132
grg 179| 3 1 13 4 -15 -6 .18 23 17 | -672 89 17 138
igr n/a| 0 0 -1 18 -7 -13 -.21 5 5 | 3241 333 16 90
jpl 80| 0 1 -2 -16 21 -20 -.06 11 11 | 1550 -306 16 135
mit 300| 0 0 4 -48 -21 -1 .03 14 13 | -385 -317 24 168
ngs 228| -1 0 0 13 62 13 -.01 11 9 | -1658 317 1654 3076
sio 475| 0 0 4 -56 -34 13 -.55 15 14 | --- --- --- ---
Table 2.1803.4 GPS week: 1803 Day: 4 MJD: 56869.000
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 240| 0 -1 2 5 -12 2 .02 9 9 | -1251 -276 16 111
emr 80| 0 0 0 2 -31 36 .15 12 12 | 2573 -199 14 144
esa 150| 0 0 -7 15 4 8 -.42 12 11 | 99 -642 11 172
gfz 192| -1 2 -1 12 -44 -29 .05 14 14 | 445 -1879 15 133
grg 182| 4 0 17 20 5 -39 .22 21 17 | -299 -431 16 155
igr n/a| 0 0 -2 -10 -5 1 -.20 5 5 | 4126 233 14 99
jpl 80| 1 2 -4 -40 10 -39 -.01 12 12 | 1901 -249 17 139
mit 300| -2 -1 3 13 9 -20 .04 13 12 | -56 -566 22 207
ngs 229| 0 0 -1 -20 26 26 .00 12 10 | -1233 -339 1868 3015
sio 374| 0 0 1 8 22 19 -.52 16 17 | --- --- --- ---
Table 2.1803.5 GPS week: 1803 Day: 5 MJD: 56870.000
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 239| 0 -1 1 -20 11 12 .04 10 9 | -1514 397 16 115
emr 80| -1 2 2 21 -5 45 .21 13 13 | 2792 332 15 135
esa 150| 0 0 -7 -8 3 -5 -.38 11 11 | -606 183 11 182
gfz 187| -1 3 -1 1 -29 -43 .02 15 14 | -759 765 15 133
grg 179| 4 0 14 7 5 -45 .24 19 16 | -763 899 17 158
igr n/a| 0 0 -2 -8 0 -12 -.23 5 5 | 4754 624 17 107
jpl 80| 0 0 -2 -15 1 -19 -.00 12 11 | 1862 130 18 157
mit 300| -1 0 2 15 -59 6 -.00 13 12 | -527 779 23 198
ngs 228| -1 -2 -2 10 44 17 -.01 12 11 | -1496 418 1725 3198
sio 441| 0 1 1 -23 -61 -14 -.57 15 14 | --- --- --- ---
Table 2.1803.6 GPS week: 1803 Day: 6 MJD: 56871.000
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 239| 0 2 0 47 -3 5 .01 11 11 | -984 -455 16 109
emr 80| 0 -2 2 0 -25 34 .18 12 12 | 2473 -66 13 142
esa 150| 0 0 -7 10 -3 3 -.35 12 11 | -436 -503 11 192
gfz 187| 0 2 -2 -11 -25 -14 .08 14 12 | -438 548 16 143
grg 179| 2 0 16 -18 24 -51 .23 19 16 | -343 238 17 128
igr n/a| 0 0 -1 -29 -21 0 -.18 5 5 | 4781 615 18 94
jpl 80| -1 0 -4 -41 22 -15 -.01 12 12 | 1294 71 17 141
mit 300| -2 -2 2 -3 -10 10 .01 12 12 | -157 147 23 183
ngs 228| 0 0 0 -13 5 0 -.03 11 9 | -1033 -388 1257 2867
sio 466| 0 0 -2 -53 -29 -10 -.59 14 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 3.1803.0 GPS week: 1803 Day: 0 MJD: 56865.000
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 19 15 9 14 6 12 12 10 11 4 | 29 25 35 25 24 26 27 26 31 23 27
2 | 8 11 8 9 18 4 14 11 7 17 4 | 24 27 25 23 21 21 27 20 24 24 22
3 | 9 9 11 10 12 5 11 18 10 20 4 | 22 26 24 23 21 20 26 26 24 24 22
4 | 6 10 9 11 15 5 10 10 9 12 3 | 75 76 79 77 69 75 76 76 79 76 75
5 | 9 9 10 8 18 4 12 15 9 14 4 | 38 42 44 40 38 40 44 34 45 42 40
6 | 13 19 11 20 61 6 18 27 15 31 8 | 41 53 40 42 27 37 48 51 36 52 39
7E | 7 12 8 8 18 5 11 25 10 9 4 | 50 49 46 50 50 46 46 59 46 45 48
8E | 8 14 13 11 15 6 15 25 15 14 5 | 98 100 96 98 101 98 102 95 98 99 98
10 | 7 6 8 6 19 4 8 15 11 12 3 | 51 51 52 52 57 50 48 55 49 56 50
11E | 7 14 7 7 17 3 12 10 9 10 3 | 27 26 27 27 29 23 25 27 29 21 25
12 | 8 12 10 12 20 4 15 17 10 17 4 | 27 29 22 30 32 22 28 28 29 22 25
13 | 8 13 13 10 20 4 13 11 9 14 4 | 28 33 26 31 42 27 32 27 27 28 28
14 | 9 13 12 14 20 4 13 15 11 21 5 | 34 34 31 39 42 32 33 40 34 35 33
15 | 9 15 14 11 20 6 16 19 12 21 5 | 32 39 32 33 34 30 36 30 33 35 31
16 | 11 15 11 15 21 6 13 18 9 23 5 | 25 27 23 28 22 21 27 25 25 24 22
17 | 7 14 8 11 20 3 12 12 10 15 4 | 24 28 18 26 33 20 25 28 25 18 23
18 | 10 9 10 12 10 5 11 21 10 18 4 | 22 25 23 21 25 20 24 32 26 25 22
19 | 10 14 7 11 21 3 11 17 11 16 4 | 24 26 20 23 26 18 23 23 24 18 21
20 | 9 9 11 16 15 4 10 14 9 23 4 | 25 23 23 35 27 23 23 25 27 27 24
21 | 11 11 9 13 19 4 11 18 11 18 4 | 22 24 24 27 24 22 26 20 25 25 22
22 | 8 9 11 10 12 5 13 16 7 13 4 | 24 27 23 26 33 21 25 33 25 22 24
23 | 8 15 13 11 18 3 15 14 13 18 5 | 25 30 25 27 32 23 29 24 24 23 24
24E | 11 13 17 10 22 9 23 21 23 16 6 | 110 108 110 112 112 108 107 109 102 106 108
25 | 9 9 12 7 16 4 14 16 7 15 4 | 30 25 26 27 28 24 31 26 30 24 27
26 | 5 10 10 6 17 3 7 17 7 12 3 | 28 28 27 27 37 26 24 35 29 32 27
X27 | 9 16 14 8 --- 7 14 17 12 13 5 | 23 25 27 24 --- 22 28 24 26 24 23
28 | 9 13 13 14 17 4 11 13 10 16 4 | 24 28 23 31 31 22 26 29 27 21 24
29 | 9 19 7 16 20 6 19 14 12 13 5 | 26 27 23 35 25 25 29 28 29 23 25
X30E | 9 13 17 9 --- 7 13 15 10 16 5 | 170 107 183 178 --- 167 88 110 109 111 173
31E | 7 12 8 10 19 4 13 19 13 11 4 | 44 42 37 42 49 41 43 43 46 44 42
32 | 9 9 7 7 17 4 8 13 9 12 3 | 22 22 22 22 19 20 20 19 25 17 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 11 21 5 13 17 11 17 |T 40 39 39 41 38 37 38 39 38 37 39
WRMS | 9 13 10 10 17 4 13 16 9 15 |NE 29 32 29 31 32 27 31 31 31 29 28
MEDI | 9 13 11 10 18 4 13 16 10 15 |MD 27 28 26 30 32 24 28 28 29 25 25
Table 3.1803.1 GPS week: 1803 Day: 1 MJD: 56866.000
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 14 15 10 13 5 9 11 9 9 4 | 20 18 26 18 25 18 20 18 21 15 18
2 | 7 13 8 7 17 4 13 12 11 18 4 | 18 20 15 20 20 13 18 14 20 19 15
3 | 10 12 9 6 13 5 10 14 8 18 3 | 22 27 23 24 25 22 26 21 27 20 23
4 | 8 13 11 8 13 5 10 8 10 14 3 | 53 49 54 54 53 55 50 56 57 50 53
5 | 8 14 10 8 17 5 11 14 9 15 4 | 19 28 23 24 21 20 24 21 26 22 21
6 | 10 20 11 21 64 9 18 23 12 28 8 | 41 49 41 44 30 39 45 48 38 52 40
7E | 7 15 8 8 18 4 13 28 10 9 5 | 49 47 46 46 47 46 45 63 52 48 48
8E | 13 18 15 11 18 6 16 27 19 18 6 | 93 96 93 96 96 95 97 96 95 94 94
10 | 9 8 8 6 17 4 7 10 7 11 3 | 46 48 49 45 52 47 46 45 46 50 46
11E | 5 14 7 7 14 3 9 10 8 9 3 | 23 21 23 23 31 21 20 24 24 16 22
12 | 10 13 10 12 21 6 10 13 9 16 4 | 20 27 18 23 28 16 21 23 21 14 19
13 | 8 15 13 9 20 4 11 11 9 15 4 | 19 25 17 20 34 17 25 17 19 14 18
14 | 7 12 11 14 21 3 12 14 13 19 4 | 19 24 22 20 28 20 22 27 23 22 20
15 | 9 14 14 11 19 6 14 14 15 18 5 | 23 31 23 25 25 18 26 18 23 18 21
16 | 10 15 9 16 19 5 12 13 8 26 4 | 19 21 14 24 24 13 20 15 16 19 15
17 | 9 17 11 11 17 3 15 11 10 10 4 | 25 26 17 27 29 18 24 25 26 13 22
18 | 10 12 11 10 9 4 11 22 11 15 4 | 14 21 17 10 15 12 18 25 17 18 14
19 | 9 12 5 10 21 4 11 15 8 15 4 | 20 22 15 22 27 15 18 17 19 11 17
20 | 8 10 12 14 15 4 8 12 10 23 4 | 18 19 19 29 23 18 21 20 21 23 18
21 | 11 15 9 12 20 4 11 17 10 15 4 | 20 22 17 20 25 16 19 14 19 16 16
22 | 11 12 11 8 10 4 11 17 10 12 4 | 15 23 18 14 20 14 19 21 17 12 15
23 | 8 14 12 11 17 3 11 11 10 17 4 | 18 22 17 20 29 16 21 16 19 14 16
24E | 18 15 33 9 15 4 17 21 13 19 7 | 83 81 95 79 77 81 78 78 81 78 81
25 | 9 10 11 8 17 5 12 13 10 13 4 | 18 22 21 19 24 17 24 19 22 20 18
26 | 5 12 11 8 16 5 8 17 9 10 4 | 20 24 18 21 24 18 16 23 17 21 18
X27 | 9 14 12 7 --- 6 10 14 8 9 4 | 19 16 23 22 --- 17 22 16 19 17 18
28 | 9 13 12 12 16 4 11 9 8 13 4 | 22 25 21 30 29 20 26 24 24 17 22
29 | 12 17 11 16 22 6 16 14 15 12 5 | 19 23 20 27 22 18 18 23 31 16 19
X30E | 11 14 18 10 --- 7 17 14 11 12 5 | 177 87 189 183 --- 172 71 82 78 81 179
31E | 12 11 6 12 29 4 12 15 10 14 5 | 42 40 36 34 43 36 40 40 40 40 38
32 | 11 9 6 8 14 5 9 11 8 12 3 | 18 17 14 15 19 15 16 18 19 15 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 12 11 21 5 12 16 11 16 |T 33 32 33 34 32 31 30 31 31 28 32
WRMS | 9 14 11 9 18 5 11 14 9 14 |NE 22 25 22 24 27 20 24 23 24 21 21
MEDI | 9 14 11 10 17 4 11 14 10 15 |MD 20 24 21 24 27 18 22 23 23 19 19
Table 3.1803.2 GPS week: 1803 Day: 2 MJD: 56867.000
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 14 14 9 16 3 11 10 12 9 4 | 24 24 29 24 22 22 25 23 27 18 23
2 | 12 12 7 9 23 5 14 13 12 14 4 | 22 23 18 21 24 16 24 21 21 17 18
3 | 6 11 11 7 16 7 11 13 11 19 4 | 23 24 26 23 22 21 24 16 27 24 22
4 | 8 11 8 10 17 5 11 10 8 13 3 | 34 36 35 36 32 33 36 34 37 33 35
5 | 10 11 10 10 19 6 10 14 9 13 4 | 28 33 32 29 29 26 31 26 31 30 29
6 | 13 18 12 22 60 7 17 21 11 27 8 | 41 51 43 46 35 37 47 47 38 54 41
7E | 8 13 8 9 15 4 13 28 10 7 5 | 32 28 27 28 29 27 28 46 29 31 29
8E | 12 18 21 14 16 8 14 25 24 17 7 | 49 49 50 45 43 43 43 52 45 46 44
10 | 6 8 9 7 17 4 9 12 9 11 3 | 57 55 60 54 59 56 55 52 52 59 55
11E | 8 12 6 7 19 3 11 10 10 8 4 | 24 28 23 26 27 21 23 25 27 18 24
12 | 13 12 9 14 28 6 12 11 11 16 5 | 19 26 18 22 29 17 20 23 22 15 18
13 | 10 13 14 10 20 5 12 10 9 17 4 | 24 29 21 25 36 21 27 22 22 20 23
14 | 8 10 13 15 26 3 13 14 16 20 5 | 27 30 28 33 36 27 31 31 34 26 29
15 | 12 14 15 15 21 8 15 14 12 18 5 | 27 33 26 31 26 24 29 25 26 23 25
16 | 11 14 10 16 20 6 12 11 15 21 5 | 22 25 20 28 23 18 25 21 27 18 21
17 | 10 16 7 11 18 3 14 9 9 12 4 | 21 29 16 27 31 18 22 24 25 13 21
18 | 8 14 12 14 17 6 8 20 10 15 5 | 17 24 20 20 22 17 24 27 23 20 19
19 | 8 13 6 10 22 5 8 12 9 13 4 | 20 25 18 24 28 17 20 18 22 12 20
20 | 9 10 11 16 13 3 8 12 11 20 4 | 23 23 22 33 21 20 21 22 22 25 21
21 | 9 17 10 14 24 5 11 16 12 15 5 | 20 28 20 24 29 20 27 19 26 21 21
22 | 9 10 12 10 15 5 9 14 10 10 4 | 18 23 21 22 25 17 23 24 20 18 20
23 | 9 13 12 9 17 4 14 11 11 18 4 | 20 28 20 22 28 18 25 20 18 16 20
24E | 12 14 16 15 21 7 12 10 13 8 5 | 58 60 62 57 53 58 54 56 60 56 57
25 | 11 12 12 10 23 6 14 9 11 11 4 | 20 21 21 20 26 18 27 22 24 19 20
26 | 5 7 11 8 17 6 8 14 10 8 3 | 19 21 19 23 26 20 20 25 20 20 20
X27 | 8 13 13 10 --- 6 11 15 11 10 4 | 20 18 25 23 --- 19 26 20 24 18 21
28 | 9 13 13 15 16 6 10 9 7 18 4 | 19 23 19 31 29 18 23 24 24 16 21
29 | 11 21 7 17 26 8 15 13 12 13 5 | 20 26 16 28 23 21 25 22 26 18 19
X30E | 12 14 19 17 --- 7 13 12 10 16 5 | 173 115 180 180 --- 170 101 112 113 111 175
31E | 11 10 8 11 21 5 11 17 9 10 4 | 36 42 35 39 39 37 41 44 40 40 38
32 | 11 9 7 7 15 4 11 9 12 10 3 | 19 22 17 19 19 15 19 18 17 12 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 11 12 22 5 12 14 12 15 |T 31 32 31 34 30 29 31 31 31 27 31
WRMS | 10 13 11 10 19 5 11 13 10 15 |NE 24 28 24 27 28 22 27 25 26 22 23
MEDI | 9 13 11 10 19 5 11 12 11 13 |MD 23 28 22 27 28 21 25 24 26 20 21
Table 3.1803.3 GPS week: 1803 Day: 3 MJD: 56868.000
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 24 14 11 13 6 11 14 13 10 5 | 23 31 30 24 28 23 27 24 26 21 23
2 | 9 11 10 10 14 4 12 11 10 13 4 | 23 25 23 24 24 20 26 20 23 19 20
3 | 7 10 10 7 11 3 11 14 6 19 3 | 25 32 28 28 28 26 27 30 30 22 26
4 | 7 10 11 9 11 5 10 12 7 15 3 | 29 36 36 32 36 31 34 36 36 35 32
5 | 9 10 13 10 13 5 8 15 11 14 4 | 31 35 34 30 32 30 31 28 34 29 29
6 | 12 13 12 19 90 7 19 18 15 26 6 | 49 54 46 44 61 44 53 53 44 57 48
7E | 10 15 9 8 16 6 13 25 8 7 5 | 55 52 48 52 53 50 51 63 53 48 52
8E | 20 19 21 15 18 10 14 24 26 18 7 | 94 97 95 93 94 92 95 94 94 95 93
10 | 8 6 8 7 14 5 6 11 8 11 3 | 52 55 57 53 58 56 58 58 55 57 55
11E | 7 9 7 7 15 4 9 12 8 10 3 | 29 28 29 29 32 25 29 29 31 22 28
12 | 14 13 11 16 20 8 10 13 13 19 5 | 30 31 23 31 33 19 25 26 22 22 24
13 | 24 13 14 10 17 6 13 9 10 16 5 | 32 34 26 30 38 27 32 25 29 25 27
14 | 8 11 14 13 19 5 11 17 9 19 4 | 24 29 25 32 34 26 28 34 28 25 26
15 | 11 11 16 14 16 6 13 12 15 18 5 | 32 36 32 36 33 26 33 30 32 28 30
16 | 13 13 10 14 21 5 13 11 9 20 5 | 31 30 25 30 30 25 32 28 26 27 26
17 | 9 17 10 14 20 4 14 11 10 13 5 | 27 30 22 32 34 22 26 27 32 19 24
18 | 14 10 17 13 11 7 10 22 12 18 5 | 20 22 20 16 17 15 22 27 24 16 17
19 | 8 15 8 11 21 5 12 13 8 14 4 | 23 29 23 26 31 21 25 24 26 19 22
20 | 10 9 12 17 15 3 8 13 9 21 4 | 22 21 21 31 25 19 21 21 19 23 19
21 | 13 14 12 14 20 4 12 17 12 15 5 | 28 30 29 28 29 26 31 24 34 24 26
22 | 12 11 17 11 12 5 12 16 10 12 4 | 21 22 21 21 24 16 24 25 27 16 19
23 | 9 13 13 12 16 4 11 10 10 17 4 | 27 30 24 28 31 24 29 24 28 21 24
24E | 14 10 16 15 18 6 9 12 14 6 5 | 60 55 60 57 60 55 61 57 50 56 56
25 | 11 8 14 9 17 6 11 11 10 11 4 | 28 27 25 27 32 20 29 28 21 26 25
26 | 8 12 14 10 14 4 7 11 7 8 4 | 29 29 23 28 29 23 25 29 29 26 25
X27 | 11 14 13 10 --- 5 12 12 9 15 5 | 27 25 29 27 --- 22 27 24 26 25 24
28 | 12 13 13 13 16 5 12 11 7 13 4 | 27 31 23 30 33 23 27 28 31 20 25
29 | 13 12 10 13 21 6 13 13 14 13 5 | 28 29 26 32 28 25 28 29 34 23 26
X30E | 13 11 19 14 --- 7 14 10 12 13 5 | 225 105 231 226 --- 219 77 104 103 105 224
31E | 11 11 10 12 25 5 8 15 8 9 4 | 48 48 43 48 54 45 50 50 49 49 48
32 | 11 9 8 8 18 4 7 8 8 12 3 | 24 23 20 21 21 20 21 21 22 20 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 13 13 12 23 5 11 14 11 15 |T 39 37 38 40 36 35 35 36 36 32 37
WRMS | 11 13 12 11 17 5 11 13 9 14 |NE 28 31 27 29 32 25 29 28 29 25 26
MEDI | 11 11 12 12 16 5 11 12 10 14 |MD 28 30 26 30 32 25 29 28 30 25 26
Table 3.1803.4 GPS week: 1803 Day: 4 MJD: 56869.000
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 23 17 10 15 5 11 14 13 10 5 | 23 24 28 20 24 20 22 21 24 15 20
2 | 9 11 11 9 17 4 14 11 11 15 4 | 22 21 22 18 20 17 22 17 19 15 17
3 | 5 8 9 9 13 6 9 14 11 20 3 | 18 22 19 17 21 15 21 23 16 22 18
4 | 9 11 9 11 13 8 13 9 11 13 4 | 22 23 24 20 19 20 23 23 26 22 20
5 | 11 9 14 9 15 6 11 12 11 14 4 | 28 33 33 26 27 26 33 26 27 25 27
6 | 11 13 12 19 60 7 16 13 11 27 7 | 41 47 40 42 37 35 43 44 37 50 39
7E | 7 14 9 11 18 5 15 15 12 9 4 | 43 45 40 46 44 39 42 49 46 38 43
8E | 17 21 28 17 21 11 18 24 32 20 8 | 96 98 101 95 95 95 98 98 97 96 96
10 | 6 9 9 9 13 4 7 12 9 9 3 | 52 55 56 56 56 57 55 54 50 57 53
11E | 8 12 5 10 15 4 12 11 10 12 4 | 24 22 20 26 29 21 21 20 22 17 22
12 | 9 11 11 14 21 6 12 11 8 20 4 | 22 27 19 25 27 20 23 24 21 17 21
13 | 9 13 11 14 20 5 13 9 8 15 4 | 23 30 21 26 35 21 29 21 20 20 23
14 | 9 11 14 13 19 5 10 16 14 17 5 | 27 29 25 30 36 26 26 33 27 25 26
15 | 11 10 15 13 22 5 17 13 12 18 5 | 29 33 27 32 32 24 30 26 29 23 27
16 | 12 12 10 18 18 6 13 8 12 21 5 | 24 24 19 26 24 16 23 19 17 19 19
17 | 8 15 9 18 16 4 14 9 12 10 4 | 22 24 16 30 30 18 23 24 23 16 21
18 | 8 9 13 12 11 4 11 16 10 17 4 | 20 23 19 17 25 16 23 29 16 19 19
19 | 9 13 6 11 17 4 12 11 8 13 4 | 20 24 15 20 25 15 20 19 17 16 18
20 | 10 8 11 17 12 3 10 11 11 22 4 | 22 20 20 29 22 18 22 20 19 24 19
21 | 8 12 9 12 22 4 13 13 12 16 4 | 19 25 17 23 28 16 22 21 21 22 18
22 | 9 12 13 12 11 3 10 13 12 11 4 | 25 28 24 28 31 22 26 31 21 20 24
23 | 8 12 11 14 18 5 14 11 11 18 4 | 23 29 21 26 28 19 26 21 21 19 21
24E | 11 9 16 28 20 5 15 11 10 11 5 | 31 29 32 30 34 29 33 33 24 31 29
25 | 8 7 12 8 18 5 14 10 12 13 4 | 19 24 23 22 24 19 26 24 23 21 21
26 | 6 8 16 10 21 4 7 10 9 9 4 | 25 25 22 25 33 21 20 25 23 20 23
X27 | 6 12 13 11 --- 4 11 12 9 12 4 | 21 21 23 21 --- 18 23 22 19 22 20
28 | 11 12 12 15 16 4 12 10 10 17 4 | 23 26 20 30 29 20 24 24 19 15 21
29 | 8 14 9 13 20 5 13 12 11 13 4 | 21 24 14 24 22 18 23 25 21 18 19
X30E | 12 14 19 16 --- 6 17 13 17 11 6 | 228 55 246 235 --- 226 89 50 50 51 231
31E | 7 13 8 13 22 8 10 20 12 10 5 | 54 54 51 52 59 52 51 58 53 49 52
32 | 9 10 6 9 17 3 9 8 8 12 3 | 19 19 15 16 18 14 18 19 15 16 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 12 14 20 5 12 13 12 16 |T 35 31 34 36 32 32 31 30 27 27 33
WRMS | 9 12 11 14 17 5 12 12 10 17 |NE 24 27 23 25 28 21 25 25 22 22 22
MEDI | 9 12 11 12 18 5 12 12 11 13 |MD 23 25 22 26 28 20 23 24 22 21 21
Table 3.1803.5 GPS week: 1803 Day: 5 MJD: 56870.000
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 17 13 13 14 6 9 16 11 11 4 | 20 21 24 21 25 18 20 18 19 15 18
2 | 9 13 7 10 15 5 10 10 10 15 4 | 19 20 14 19 21 14 16 15 16 12 15
3 | 7 10 9 10 10 4 10 13 13 22 4 | 26 29 25 25 27 23 29 24 27 31 25
4 | 8 12 9 14 10 5 8 7 12 13 3 | 34 33 33 38 31 33 31 32 30 30 32
5 | 7 11 11 14 15 4 11 11 10 14 4 | 19 25 22 19 20 17 24 19 20 15 19
6 | 12 14 12 24 58 10 16 15 15 25 8 | 46 55 48 44 39 42 53 49 40 55 46
7E | 9 14 7 8 18 4 15 9 12 11 4 | 60 56 54 55 58 52 57 59 57 51 56
8E | 16 21 18 19 17 8 14 25 23 18 7 | 149 152 151 149 152 153 150 154 152 150 151
10 | 10 6 8 17 12 6 8 11 11 9 4 | 45 46 51 49 50 47 47 47 46 49 47
11E | 9 16 5 9 14 3 11 13 8 7 4 | 23 30 17 23 28 17 21 19 22 12 21
12 | 11 14 11 14 21 6 12 11 12 17 5 | 22 23 16 22 26 14 19 21 18 13 17
13 | 11 15 12 14 17 5 12 9 13 15 4 | 22 29 21 25 32 20 27 19 19 15 21
14 | 10 10 13 14 16 5 11 16 14 16 5 | 23 25 21 25 28 21 24 25 22 19 21
15 | 9 13 14 17 19 4 13 13 9 18 5 | 24 30 24 33 28 20 26 24 24 24 23
16 | 11 14 9 18 16 4 13 7 15 21 5 | 22 24 18 25 25 16 23 20 23 19 19
17 | 7 17 9 23 19 5 13 9 14 13 5 | 21 26 13 30 30 16 22 22 23 14 19
18 | 11 8 13 16 10 5 10 16 10 19 4 | 14 19 17 17 15 11 20 23 14 17 14
19 | 9 16 6 14 17 3 13 11 11 12 4 | 22 28 16 22 28 16 21 17 22 11 19
20 | 9 12 11 15 13 5 8 15 9 22 4 | 18 19 18 24 16 14 17 19 15 19 15
21 | 9 11 9 15 22 2 12 14 11 16 4 | 14 21 17 19 29 14 20 18 22 17 16
22 | 12 10 13 14 13 3 11 15 11 11 4 | 19 22 18 18 23 14 20 20 16 12 16
23 | 9 14 12 14 15 5 12 10 14 17 4 | 21 27 21 24 25 18 24 19 21 17 19
24E | 10 14 15 20 19 5 11 13 13 10 5 | 45 47 46 51 46 46 44 47 45 45 46
25 | 7 9 14 6 16 7 10 12 12 11 4 | 20 24 21 21 25 18 24 21 21 18 20
26 | 6 10 13 10 18 4 8 12 10 10 4 | 20 21 16 23 25 17 21 24 20 17 19
X27 | 11 13 12 13 --- 5 10 10 14 11 5 | 24 21 24 20 --- 18 23 19 24 18 21
28 | 10 11 13 22 18 6 15 11 12 13 5 | 20 24 16 32 27 17 23 19 23 14 18
29 | 8 12 9 12 18 5 15 15 13 13 4 | 18 21 14 21 21 16 19 23 22 16 16
X30E | 15 30 22 20 --- 10 --- 14 35 14 10 | 311 116 314 303 --- 302 --- 106 105 103 306
31E | 9 12 8 12 16 7 13 11 14 10 4 | 73 74 68 67 78 71 70 74 74 67 71
32 | 9 10 7 10 14 3 7 8 9 13 3 | 16 22 16 19 18 15 16 17 18 14 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 11 15 19 5 12 13 12 15 |T 39 36 38 41 34 36 31 33 32 29 38
WRMS | 9 13 11 14 16 5 11 12 11 14 |NE 22 26 21 25 26 19 24 22 22 20 21
MEDI | 9 13 11 14 16 5 11 12 12 13 |MD 22 25 21 24 27 18 23 21 22 17 19
Table 3.1803.6 GPS week: 1803 Day: 6 MJD: 56871.000
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 13 12 12 15 6 12 14 11 10 4 | 28 25 33 25 29 26 26 25 29 23 25
2 | 9 11 7 12 18 5 13 14 11 14 4 | 26 26 23 27 27 21 27 24 24 22 23
3 | 6 10 12 12 9 5 9 8 7 --- 3 | 27 30 30 26 28 26 28 25 28 --- 27
4 | 7 9 10 8 11 6 10 9 9 10 3 | 30 33 33 31 29 33 32 33 31 32 31
5 | 14 12 12 12 18 4 13 12 14 11 5 | 38 44 43 40 37 37 42 36 44 36 38
6 | 17 14 11 24 58 10 17 16 11 21 8 | 51 60 53 54 37 47 56 58 46 60 51
7E | 14 16 9 12 12 5 13 13 9 9 4 | 57 56 55 58 55 56 54 58 57 53 56
8E | 15 18 16 16 17 6 11 17 20 15 6 | 168 172 169 169 171 168 171 173 170 171 169
10 | 6 7 10 17 14 4 5 12 9 7 4 | 48 48 49 46 52 47 47 49 48 52 47
11E | 9 16 8 8 17 5 11 10 9 8 4 | 29 33 28 25 35 24 27 27 30 22 27
12 | 10 14 10 16 19 5 17 14 10 18 5 | 26 30 20 29 30 20 28 26 24 21 23
13 | 11 13 14 13 17 6 12 9 10 14 4 | 28 37 26 31 40 28 35 29 31 27 29
14 | 9 11 13 16 17 5 10 13 16 17 5 | 32 31 29 36 41 30 31 36 32 28 30
15 | 13 12 16 13 22 6 15 13 15 17 5 | 34 40 34 36 35 28 37 31 34 32 32
16 | 14 14 12 16 16 5 13 12 12 17 5 | 28 27 21 28 26 21 27 23 23 20 22
17 | 11 15 10 15 15 6 14 11 10 13 4 | 26 29 18 35 32 22 28 29 27 19 25
18 | 12 11 12 16 13 3 9 15 10 18 4 | 25 25 21 21 27 18 26 31 20 22 21
19 | 12 16 8 15 15 4 12 11 9 11 4 | 26 30 21 26 31 21 24 25 24 20 22
20 | 10 9 13 16 14 5 8 16 11 21 4 | 24 24 24 31 28 21 26 26 24 26 22
21 | 12 13 10 14 24 4 12 13 14 16 5 | 26 29 26 29 33 23 31 25 34 26 26
22 | 11 11 12 12 13 2 11 13 9 10 4 | 30 29 25 27 34 22 29 32 22 21 26
23 | 9 12 12 13 15 5 12 10 11 18 4 | 25 31 23 29 30 23 28 25 27 24 24
24E | 8 11 15 15 16 4 11 13 8 11 4 | 50 50 52 53 49 51 51 49 46 50 49
25 | 8 12 14 7 13 6 11 11 7 15 4 | 25 33 24 25 28 22 31 26 24 25 25
26 | 11 9 12 10 18 6 12 14 13 8 4 | 30 31 24 28 36 26 27 34 29 26 27
X27 | 8 11 14 10 --- 4 12 7 9 15 4 | 30 24 29 24 --- 25 28 25 26 29 25
28 | 10 12 13 19 15 6 9 12 12 16 4 | 28 32 23 36 30 24 30 30 29 22 27
29 | 9 14 10 15 22 5 13 13 9 11 5 | 29 29 24 33 29 24 25 29 29 23 25
X30E | 33 --- 144 51 --- 67 --- --- --- --- 41 | 421 --- 500 453 --- 403 --- --- --- --- 432
31E | 10 13 8 12 21 6 13 9 9 10 4 | 69 68 63 67 67 66 71 67 67 64 67
32 | 8 8 7 10 13 4 8 7 7 15 3 | 25 26 23 21 24 22 24 27 23 27 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 12 14 19 5 12 12 11 14 |T 49 39 50 51 39 45 38 37 36 35 48
WRMS | 11 12 11 12 16 5 12 12 9 14 |NE 29 32 27 30 32 26 30 30 29 27 27
MEDI | 10 12 12 13 16 5 12 12 10 14 |MD 29 31 26 31 32 25 28 29 29 26 27
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 4.1803 GPS week: 1803 MJD: 56865.0-56871.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 |U 8 8 19 |U 6 7 22 |U 9 11 22 |
emr | emr 2958 | 11 10 24 |U 7 7 25 | 9 10 24 |
esa | esa 2976 | 10 10 21 |U 6 7 24 | 10 11 24 |
gfz | gfz 2972 |U 10 10 21 |U 7 7 24 |U 9 12 24 |
grg | grg 2783 |U 11 12 24 |U 8 9 28 |U 11 12 31 |
igr | igr 2974 | 10 9 20 | 7 7 22 | 9 11 24 |
igs | igs 2962 | 10 9 20 | 7 6 23 | 9 11 24 |
jpl | jpl 2944 | 11 13 30 |U 7 8 27 |U 11 12 28 |
mit | mit 2962 | 10 10 23 |U 9 8 30 |U 10 13 27 |
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 5.1803.0 GPS week: 1803 Day: 0 MJD: 56865.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 11 10 27 | 6 5 20 | 12 15 24 |
emr | emr 2971 | 10 10 30 | 7 6 23 | 12 12 21 |
esa | esa 2976 | 10 9 28 | 5 5 21 | 13 14 25 |
gfz | gfz 2971 | 11 9 26 | 6 6 22 | 12 13 23 |
grg | grg 2783 | 11 14 34 | 9 6 27 | 13 12 31 |
igr | igr 2975 | 11 9 26 | 6 5 22 | 12 13 24 |
igs | igs 2971 | 10 9 26 | 6 5 23 | 12 13 24 |
jpl | jpl 2971 | 11 8 23 | 6 7 25 | 12 11 26 |
mit | mit 2976 | 13 12 36 | 17 10 52 | 13 21 38 |
Table 5.1803.1 GPS week: 1803 Day: 1 MJD: 56866.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 4 19 | 7 5 23 | 7 7 19 |
emr | emr 2972 | 9 6 26 | 10 7 25 | 9 11 29 |
esa | esa 2976 | 9 6 23 | 6 5 19 | 8 9 23 |
gfz | gfz 2972 | 10 7 23 | 9 6 22 | 8 11 29 |
grg | grg 2784 | 10 7 24 | 10 8 31 | 10 11 37 |
igr | igr 2976 | 8 5 21 | 8 5 22 | 8 9 27 |
igs | igs 2975 | 9 4 20 | 8 5 22 | 8 10 27 |
jpl | jpl 2972 | 8 20 60 | 8 10 23 | 10 12 28 |
mit | mit 2976 | 8 4 17 | 7 6 30 | 8 10 28 |
Table 5.1803.2 GPS week: 1803 Day: 2 MJD: 56867.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 13 12 23 | 6 9 18 | 7 13 19 |
emr | emr 2971 | 17 16 32 | 5 9 17 | 7 13 27 |
esa | esa 2976 | 15 14 25 | 5 8 23 | 8 13 26 |
gfz | gfz 2973 | 13 12 21 | 7 10 21 | 7 15 25 |
grg | grg 2784 | 14 14 22 | 8 15 27 | 9 18 32 |
igr | igr 2976 | 14 12 22 | 5 9 17 | 7 16 27 |
igs | igs 2973 | 14 13 26 | 5 8 17 | 7 14 26 |
jpl | jpl 2972 | 15 15 31 | 5 7 18 | 10 14 34 |
mit | mit 2976 | 13 13 24 | 9 10 20 | 9 17 27 |
Table 5.1803.3 GPS week: 1803 Day: 3 MJD: 56868.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 18 | 8 7 27 | 8 9 25 |
emr | emr 2972 | 8 7 21 | 8 9 29 | 9 10 28 |
esa | esa 2976 | 7 7 19 | 8 8 31 | 9 10 23 |
gfz | gfz 2973 | 7 7 23 | 9 9 30 | 9 12 24 |
grg | grg 2784 | 7 8 20 | 8 11 29 | 9 10 23 |
igr | igr 2976 | 6 7 19 | 9 8 27 | 9 10 24 |
igs | igs 2962 | 7 7 19 | 8 9 27 | 9 11 24 |
jpl | jpl 2971 | 8 8 19 | 8 9 28 | 10 12 26 |
mit | mit 2976 | 7 8 22 | 8 9 26 | 12 14 23 |
Table 5.1803.4 GPS week: 1803 Day: 4 MJD: 56869.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 13 | 6 6 20 | 10 12 23 |
emr | emr 2972 | 8 9 18 | 6 7 23 | 10 10 27 |
esa | esa 2976 | 7 8 14 | 6 6 21 | 11 13 26 |
gfz | gfz 2972 | 6 7 15 | 7 7 22 | 10 12 25 |
grg | grg 2784 | 6 12 23 | 8 8 26 | 12 15 33 |
igr | igr 2976 | 6 7 13 | 7 7 20 | 10 12 26 |
igs | igs 2971 | 6 7 13 | 6 6 19 | 10 12 25 |
jpl | jpl 2972 | 8 9 16 | 6 6 19 | 12 13 29 |
mit | mit 2976 | 6 9 14 | 8 7 24 | 10 13 27 |
Table 5.1803.5 GPS week: 1803 Day: 5 MJD: 56870.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 9 18 | 5 8 20 | 8 8 21 |
emr | emr 2972 | 16 15 21 | 6 6 22 | 8 8 17 |
esa | esa 2976 | 17 18 18 | 5 7 24 | 9 8 22 |
gfz | gfz 2972 | 15 17 17 | 5 7 20 | 9 9 20 |
grg | grg 2784 | 16 17 30 | 6 7 21 | 11 9 31 |
igr | igr 2976 | 16 17 18 | 5 5 21 | 9 9 21 |
igs | igs 2965 | 14 13 19 | 5 6 21 | 9 8 22 |
jpl | jpl 2876 | 13 18 19 | 7 11 47 | 11 10 29 |
mit | mit 2976 | 12 13 20 | 6 6 24 | 10 9 25 |
Table 5.1803.6 GPS week: 1803 Day: 6 MJD: 56871.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 10 19 | 7 7 27 | 11 10 22 |
emr | emr 2876 | 9 9 22 | 9 8 34 | 10 9 19 |
esa | esa 2976 | 9 10 17 | 9 7 32 | 12 9 22 |
gfz | gfz 2972 | 7 9 21 | 8 7 33 | 9 11 24 |
grg | grg 2784 | 10 12 20 | 9 10 36 | 11 9 26 |
igr | igr 2969 | 8 9 19 | 8 7 29 | 11 10 22 |
igs | igs 2918 | 8 9 19 | 8 7 30 | 9 9 21 |
jpl | jpl 2875 | 14 17 46 | 9 8 31 | 9 10 22 |
mit | mit 2880 | 8 10 25 | 8 7 35 | 12 10 24 |
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 6.1803 GPS week: 1803 MJD: 56865.500-56871.500
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 | 7 -18 -10 -9 3 | 20 29
| 33 25 50 186 8 | 4
emr uuuuu | 43 -10 -31 51 -6 | 28 38
| 32 24 122 114 11 | 4
esa uuuuu | -16 -12 50 57 -6 | 18 28
| 8 12 67 55 6 | 4
gfz uuuuu | 13 13 -32 -51 2 | 17 27
| 19 21 133 119 6 | 3
grg uuuxu | 33 -34 17 340 -1 | 32 38
| 22 26 56 98 4 | 3
igr xxxxx | 2 -5 3 38 2 | -1 21
| 11 16 43 45 6 | 3
irf xxxxx | 8 -11 -63 -72 2 | 3 21
| 9 8 30 50 2 | 3
jpl uuuuu | -14 40 -32 93 -14 | 47 56
| 26 12 65 87 18 | 4
mit uuuuu | -6 -6 -99 -188 8 | 25 33
| 19 22 71 95 3 | 4
ngs uuuuu | -40 14 107 -2 1 | 17 23
| 26 27 119 32 8 | 3
sio xxxxx | 32 22 65 93 6 | 67 71
| 14 17 39 54 7 | 4
Table 7.1803.0 GPS week: 1803 Day: 0 MJD: 56865.500
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 | 56 5 -64 207 -4 | 22 30
emr uuuuu | -3 -38 148 -62 -16 | 36 43
esa uuuuu | -14 -7 -8 40 -8 | 24 33
gfz uuuuu | 39 -9 37 10 6 | 15 27
grg uuuxu | 34 -55 100 183 -7 | 31 38
igr xxxxx | 7 -5 46 18 4 | -1 21
irf xxxxx | 4 -7 -75 -164 -1 | 4 22
jpl uuuuu | -31 50 -41 -40 19 | 51 58
mit uuuuu | -16 25 -144 -362 3 | 24 34
ngs uuuuu | -75 12 5 -43 4 | 15 22
sio xxxxx | 37 1 74 -9 10 | 65 69
Table 7.1803.1 GPS week: 1803 Day: 1 MJD: 56866.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 38 -18 20 178 -8 | 21 29
emr uuuuu | 5 -7 -105 -104 -24 | 33 40
esa uuuuu | -12 -21 125 87 -10 | 22 31
gfz uuuuu | 14 -11 177 -142 11 | 16 28
grg uuuxu | 55 -40 -69 250 -4 | 32 38
igr xxxxx | 10 -17 24 -15 2 | -1 21
irf xxxxx | 5 -9 -67 -107 1 | 3 22
jpl uuuuu | -36 54 -19 62 -28 | 54 61
mit uuuuu | -5 -10 -175 -202 8 | 24 33
ngs uuuuu | -41 29 -96 -3 13 | 16 23
sio xxxxx | 30 25 13 64 5 | 67 71
Table 7.1803.2 GPS week: 1803 Day: 2 MJD: 56867.500
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 | 6 -29 79 31 -2 | 15 26
emr uuuuu | 53 7 -191 3 -5 | 25 36
esa uuuuu | -26 -20 17 110 -10 | 16 27
gfz uuuuu | -11 -7 -10 -29 4 | 13 26
grg uuuxu | 50 -70 65 376 1 | 27 36
igr xxxxx | -7 -28 -33 -1 8 | -6 22
irf xxxxx | -5 -20 -85 -58 2 | -1 22
jpl uuuuu | -10 51 -66 69 -34 | 46 56
mit uuuuu | -32 -6 -141 -201 5 | 20 30
ngs uuuuu | 2 41 206 -32 9 | 14 22
sio xxxxx | 22 11 57 80 -2 | 63 67
Table 7.1803.3 GPS week: 1803 Day: 3 MJD: 56868.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 5 -18 -27 -57 15 | 15 26
emr uuuuu | 67 8 -69 166 -8 | 23 35
esa uuuuu | -20 -29 133 67 -11 | 14 26
gfz uuuuu | 7 27 -116 -154 4 | 14 27
grg uuuxu | 58 -18 -13 424 4 | 28 37
igr xxxxx | -9 -11 -3 20 2 | -5 23
irf xxxxx | 16 -5 -47 -52 2 | -1 22
jpl uuuuu | -23 29 -13 100 -27 | 42 54
mit uuuuu | 9 -4 -59 -140 7 | 20 30
ngs uuuuu | -66 -6 137 -5 -3 | 15 23
sio xxxxx | 43 16 108 150 -2 | 64 68
Table 7.1803.4 GPS week: 1803 Day: 4 MJD: 56869.500
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 | 7 -19 3 59 3 | 19 28
emr uuuuu | 54 -13 4 87 2 | 26 35
esa uuuuu | -27 1 -22 -16 -7 | 16 26
gfz uuuuu | 4 20 -218 -83 -3 | 18 27
grg uuuxu | 17 -43 34 415 3 | 33 38
igr xxxxx | -11 0 -6 83 8 | -1 20
irf xxxxx | 8 1 -107 -63 4 | 3 19
jpl uuuuu | -21 25 85 78 -5 | 45 54
mit uuuuu | 5 9 -154 -168 12 | 25 32
ngs uuuuu | -31 12 235 -2 -2 | 18 24
sio xxxxx | 26 16 50 135 9 | 68 71
Table 7.1803.5 GPS week: 1803 Day: 5 MJD: 56870.500
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 16 -27 -173 10 | 23 30
emr uuuuu | 37 -46 102 57 2 | 28 37
esa uuuuu | -8 1 101 -11 4 | 17 27
gfz uuuuu | 38 40 -135 181 -6 | 20 28
grg uuuxu | 9 -12 20 435 -5 | 36 41
igr xxxxx | 19 7 -66 53 -8 | 2 20
irf xxxxx | 5 -19 -44 -55 5 | 6 20
jpl uuuuu | 43 31 -131 247 -10 | 46 55
mit uuuuu | -24 -8 -17 -201 12 | 29 35
ngs uuuuu | -46 -33 83 16 -8 | 20 25
sio xxxxx | 13 37 33 110 16 | 71 74
Table 7.1803.6 GPS week: 1803 Day: 6 MJD: 56871.500
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 | -42 -60 -58 -311 6 | 24 32
emr uuuuu | 85 17 -108 207 4 | 29 37
esa uuuuu | -8 -6 1 120 1 | 18 27
gfz uuuuu | -3 31 42 -138 -2 | 21 29
grg uuuxu | 5 3 -20 296 -1 | 36 41
igr xxxxx | 5 20 57 108 -4 | 3 20
irf xxxxx | 23 -19 -14 -5 1 | 8 21
jpl uuuuu | -22 40 -43 137 -14 | 46 55
mit uuuuu | 21 -46 -3 -43 6 | 32 38
ngs uuuuu | -24 42 178 56 -4 | 21 26
sio xxxxx | 55 50 122 123 3 | 74 77
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