[IGSREPORT-23192] Wk 1819 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Dec 5 08:27:33 PST 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1819 (Nov 16, 2014 - Nov 22, 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:
igs1819[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1819[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1819[0-6].cls IGS GPS clock combination summary report.
igs18197.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18197.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 | PIE1
0 | ESA | TIXI
0 | GFZ | 1 2 6 9 30 1 6 30
0 | GRG | BOGT BRFT DAV1 BRFT DARW DAV1
0 | JPL | YELL
0 | MIT | BAKO MDVJ PERT
1 | COD | BRAZ BRST BRAZ BRST PRDS
1 | ESA | BJFS BRMU BJFS BRAZ BRMU
1 | GFZ | 1 2 6 9 30 1 6 30 BRAZ HOB2 HOB2 ISPA
1 | GRG | BOGT BOR1 BRMU GRAZ ISPA BOGT BOR1 BRMU GRAZ ISPA
1 | GRG | SOFI
1 | JPL | 26
1 | MIT | 8 21 29 1 8 21 29 MDVJ PDEL
2 | ESA | ISPA KELY ISPA KELY
2 | GFZ | 1 2 6 9 30 1 6 30 NOVM FAIR NOVM
2 | GRG | CRO1 ISPA ISPA
2 | JPL | 26
3 | COD | ZECK BOR1 ZECK
3 | ESA | BJFS BJFS
3 | GFZ | 1 2 6 9 30 1 6 30
3 | GRG | 26 26 BOR1 GRAZ KELY WSRT GRAZ KELY WSRT
4 | COD | HOB2 HOB2
4 | ESA | BOGT TLSE BOGT TLSE
4 | GFZ | 1 2 6 30 1 6 30 BOR1 CRO1 GRAZ KIRU KOUC MAL2 MAS1
4 | GFZ | PARC SUTH VILL ZECK MAL2 MAS1 ZECK
4 | GRG | 26 26 MAS1 MCM4 VILL WES2 GRAZ MAS1 MCM4 SUTH VILL
4 | GRG | WES2
4 | JPL | INVK SCOR
4 | MIT | 8 8
5 | GFZ | 1 2 6 9 30 1 6 30 HOB2 ONSA HOB2 ONSA
5 | GRG | 26 26 BRST GRAZ KELY KOUC MCM4 ONSA BRST GRAZ KELY
5 | GRG | KOUC MCM4 ONSA
5 | JPL | 26 SCOR
5 | MIT | 8 8 28 HOB2 HOB2
6 | ESA | KOUR KOUR
6 | GFZ | 1 2 3 6 9 30 1 3 6 30 WSRT WSRT
6 | GRG | 13 13 26 BRFT BRST CHUR KOUC MCM4 BRFT BRST KELY
6 | GRG | KOUC
6 | MIT | 8 8 26
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | GRG | ~05:40 | ~ 0.22 ns
4 | MIT | ~00:00 | ~ -0.81 ns
6. 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.
7. 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
----+------------+----------
G04 | 2014_11_21 | 2014085
G04 | 2014_11_22 | 2014085
8. 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 | SIO | ALL (high Transformation - See Table 2)
5 | GRG | 9
6 | ESA | 3
6 | GFZ | 3
6 | GRG | 9
6 | NGS | 9
9. 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 G03 | | | | | | 4 | 4 |
PRN G09 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
10. 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.
11. 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 | -1.4 .1 -1.9 -23 -9 33 .69
EMR | 0 | -1.6 4.1 31.7 11 38 13 .69
ESA | 0 | .5 -.6 -1.1 3 -25 29 .59
GFZ | 0 | -.6 .3 -1.8 -12 -83 10 .59
GRG | 0 | 2.6 2.1 -20.8 -27 27 -2 .97
JPL | 0 | .8 -6.8 15.7 11 4 28 .76
MIT | 0 | 8.1 -3.2 4.7 -18 -2 -47 .96
NGS | 0 | -1.8 -2.6 10.8 -35 3 -32 .97
SIO | 0 | 13.3 -1.0 51.2 -48 -22 621 .69
COD | 1 | -1.6 .1 -1.7 -34 -5 13 .52
EMR | 1 | -6.3 5.5 28.1 13 29 4 .50
ESA | 1 | .6 -.3 -.6 -7 -26 39 .43
GFZ | 1 | .3 .3 -1.3 -13 -97 29 .42
GRG | 1 | -1.1 .5 -10.6 -35 -9 -9 .81
JPL | 1 | -3.8 -7.9 16.7 -43 -5 31 .71
MIT | 1 | 6.4 -.2 8.6 -13 2 -47 .61
NGS | 1 | -5.4 -4.8 6.5 -37 17 -43 1.08
SIO | 1 | 11.8 -3.1 46.3 2 -29 56 .59
COD | 2 | -1.3 -1.0 -1.4 -59 6 29 .34
EMR | 2 | -.8 4.4 32.1 25 37 32 .33
ESA | 2 | .4 -.8 -1.1 -1 -10 42 .32
GFZ | 2 | .5 1.0 -1.9 -5 -78 10 .15
GRG | 2 | 3.4 1.3 -13.3 -22 5 -4 .85
JPL | 2 | -2.4 -.8 20.4 -64 13 -9 .56
MIT | 2 | 10.3 2.0 4.9 -8 -2 -41 .54
NGS | 2 | 3.7 1.8 9.6 -10 -30 14 .76
SIO | 2 | 9.7 1.0 37.3 1 3 -11 .57
COD | 3 | -3.0 -1.0 -2.7 -51 31 14 .31
EMR | 3 | 2.7 1.4 32.0 27 27 22 .08
ESA | 3 | -.1 -.2 -1.1 -11 -22 37 .37
GFZ | 3 | .2 .6 -2.1 -11 -74 11 .10
GRG | 3 | 7.2 1.1 -10.6 -11 28 15 .57
JPL | 3 | 6.6 -1.6 19.3 -26 27 -22 .48
MIT | 3 | 11.9 -.1 7.7 9 6 -14 .48
NGS | 3 | -2.6 -5.4 16.8 -74 -8 -39 .92
SIO | 3 | 10.8 .1 46.0 66 34 176 .63
COD | 4 | -3.1 -2.3 -3.4 -60 49 34 .62
EMR | 4 | 2.1 -.5 27.8 23 21 34 .39
ESA | 4 | -.2 -.7 -.1 -14 -29 54 .16
GFZ | 4 | .3 -.9 -2.0 -31 -74 9 .34
GRG | 4 | 11.9 2.7 -18.5 -13 1 1 .80
JPL | 4 | -.1 -2.8 12.9 -36 26 20 .71
MIT | 4 | 13.5 -2.0 6.7 7 5 -14 .69
NGS | 4 | 5.6 -8.3 6.9 -33 -27 0 .57
SIO | 4 | 9.5 .7 38.6 -4 19 -1 .72
COD | 5 | -3.3 -3.0 -3.4 -76 52 43 .70
EMR | 5 | 3.0 -4.2 20.0 28 24 26 .20
ESA | 5 | -.9 -.4 -.8 -14 -10 37 .26
GFZ | 5 | -.4 .5 -1.7 -38 -63 18 .22
GRG | 5 | 11.2 -1.4 -12.3 -6 20 -2 1.06
JPL | 5 | 3.5 .3 14.7 -56 22 14 .47
MIT | 5 | 11.9 -2.5 .5 4 3 -27 .82
NGS | 5 | 5.9 -3.2 11.2 -29 -24 13 .82
SIO | 5 | 12.7 -3.3 44.7 38 8 194 .91
COD | 6 | -2.4 -1.2 -2.0 -43 23 33 .31
EMR | 6 | -4.2 -5.3 19.4 25 37 20 .37
ESA | 6 | -.3 -.7 .2 21 -52 69 .33
GFZ | 6 | .7 .6 -1.7 -31 -67 2 .04
GRG | 6 | 4.7 10.7 -10.4 -1 0 22 .62
JPL | 6 | 7.4 2.1 7.4 -26 18 24 .49
MIT | 6 | 12.1 .6 -3.0 3 3 -21 .57
NGS | 6 | 3.5 5.2 3.0 21 -18 16 .84
SIO | 6 | 11.0 -6.6 52.5 20 33 2 .51
12. 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.
13. 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 1.1819.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1819.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 2.1819.[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 3.1819.[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 5.1819.0-6). 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 1819 summary. (Nov 16, 2014 - Nov 22, 2014)
Table 1.1819.a GPS week: 1819 MJD: 56977.000-56983.000
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 242| 1 0 -2 4 7 -1 .04 9 9 | -858 -127 17 115
| 0 0 1 9 12 19 .03 | 103 170
emr 80| -2 -2 9 -31 -18 0 .31 13 13 | 2935 248 15 146
| 1 4 2 17 12 17 .06 | 1351 1151
esa 150| 1 0 1 -1 -14 -10 -.35 12 12 | -202 -38 9 149
| 0 0 1 16 9 22 .04 | 743 860
gfz 195| -1 0 1 12 -18 39 -.15 12 11 | 58 -266 13 159
| 0 1 1 26 13 15 .05 | 192 415
grg 171| 1 0 -18 5 13 -40 .23 17 16 | 95 -122 15 144
| 1 0 2 20 22 20 .08 | 246 404
igr n/a| -1 0 -4 -10 13 -21 -.21 5 5 | -96 28 15 82
| 0 0 0 7 14 10 .02 | 1144 1354
jpl 80| 0 1 8 5 33 -32 .28 12 12 | 2938 266 16 120
| 1 2 2 16 24 23 .05 | 1362 1144
mit 349| 2 0 -6 11 -2 -7 -.16 13 11 | -219 6 21 177
| 0 0 1 28 29 10 .04 | 185 250
ngs 219| -1 0 0 -10 -4 -16 -.04 12 10 | -810 -203 1338 2737
| 1 1 2 22 30 29 .04 | 90 64
sio 324| 0 0 1 6 0 137 -.09 13 12 | --- --- --- ---
| 0 0 3 32 29 216 .24 | --- ---
Table 1.1819.b GPS week : 1819 MJD: 56977.000-56983.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 4 4 5 4 4 4 4 |
3 | --- --- --- --- --- 0 0 |
4 | 4 4 4 4 4 0 5 |
5 | 5 5 4 5 4 5 5 |
6 | 4 4 4 4 4 4 4 |
7 | 5 5 5 5 5 4 5 |
8 | 5 5 5 5 4 4 6 |
9 | 5 5 7 7 8 10 19 |
10 | 4 3 4 4 4 4 4 |
11 | 5 4 4 4 4 4 5 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 3 3 4 4 3 4 |
15 | 5 5 4 5 4 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 5 4 5 5 5 5 5 |
19 | 5 5 5 5 5 5 5 |
20 | 5 5 4 5 4 5 5 |
21 | 5 4 4 4 4 4 4 |
22 | 5 4 5 5 5 4 5 |
23 | 5 5 5 5 4 5 7 |
24 | 5 4 4 4 4 5 4 |
25 | 5 4 4 4 4 4 4 |
26 | 6 6 7 7 8 7 8 |
27 | 5 4 4 4 5 5 4 |
28 | 4 3 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 5 3 4 4 4 4 4 |
31 | 6 5 5 5 5 5 6 |
32 | 4 3 3 4 3 4 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 2.1819.0 GPS week: 1819 Day: 0 MJD: 56977.000
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| 0 0 -3 0 -9 11 .08 8 8 | -768 -128 15 121
emr 80| 0 1 12 -49 -33 -4 .29 13 13 | 2383 -492 14 129
esa 150| 1 0 0 -3 -24 -8 -.32 11 12 | -1544 1502 9 152
gfz 197| -1 1 3 29 -18 34 -.24 13 12 | -129 -370 11 146
grg 175| 2 -1 -19 -17 42 -33 .21 18 17 | 214 -355 14 162
igr n/a| -1 0 -4 -18 31 -8 -.20 5 5 | 760 -965 15 87
jpl 80| 0 -1 9 36 12 -7 .31 11 11 | 2369 -456 16 122
mit 350| 3 -1 -6 -11 44 1 -.24 15 12 | -466 68 21 197
ngs 227| -2 0 -2 6 8 -5 -.10 11 10 | -748 -141 1732 3363
sio 342| 0 -1 -2 -17 40 583 -.59 14 13 | --- --- --- ---
Table 2.1819.1 GPS week: 1819 Day: 1 MJD: 56978.000
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 248| 1 -1 -2 -8 20 -23 .02 9 8 | -884 77 16 104
emr 80| -4 2 10 -40 2 -20 .36 13 13 | 2285 -941 13 126
esa 150| 1 0 2 -20 -17 -16 -.32 12 12 | -189 -312 10 146
gfz 201| 0 0 2 -1 -23 52 -.18 11 10 | 242 -244 13 170
grg 171| 1 0 -15 4 2 -57 .29 16 14 | 366 -486 14 135
igr n/a| 0 0 -5 -7 12 -26 -.19 5 5 | 188 -1432 16 71
jpl 80| -2 -1 9 1 29 -30 .32 11 11 | 2281 -944 17 96
mit 350| 1 0 -7 33 -23 -6 -.17 13 10 | 97 -301 21 175
ngs 227| -2 0 -1 9 17 5 -.06 12 10 | -655 -232 1109 2260
sio 327| 1 0 -2 41 -30 88 -.12 12 11 | --- --- --- ---
Table 2.1819.2 GPS week: 1819 Day: 2 MJD: 56979.000
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 245| 1 -1 -4 5 24 28 .01 9 8 | -818 -191 15 109
emr 80| -3 1 10 3 -18 8 .38 13 13 | 1785 -815 16 148
esa 150| 0 0 0 24 -9 -4 -.34 12 12 | -137 -562 9 157
gfz 201| -1 -2 1 65 -13 52 -.12 12 11 | -46 -139 14 169
grg 173| 1 -1 -17 44 -11 -15 .32 17 15 | 52 -239 15 142
igr n/a| 0 0 -4 -10 16 -16 -.20 5 5 | -1033 -1290 16 80
jpl 80| -1 1 10 -1 31 -59 .30 12 12 | 1784 -777 16 113
mit 350| 2 0 -5 -31 -14 -8 -.17 12 9 | -309 -50 19 164
ngs 227| 0 1 0 -29 6 -1 -.02 12 10 | -858 -157 1121 2324
sio 329| 1 -1 1 -47 -15 -29 -.10 11 11 | --- --- --- ---
Table 2.1819.3 GPS week: 1819 Day: 3 MJD: 56980.000
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| 1 0 -4 8 -5 -12 .04 10 10 | -834 -158 20 121
emr 80| -2 -1 11 -39 -28 3 .35 13 13 | 1963 1148 14 128
esa 150| 0 1 1 -2 -28 -43 -.32 11 12 | -487 451 11 154
gfz 197| -1 -1 0 6 -42 16 -.10 12 11 | -18 -558 13 161
grg 173| 1 0 -20 -5 36 -64 .30 17 16 | -99 98 16 140
igr n/a| -2 0 -4 -21 12 -36 -.21 5 5 | -1462 785 17 76
jpl 80| 0 1 10 -9 0 -33 .31 13 13 | 1950 1193 16 121
mit 350| 2 0 -6 -4 17 -29 -.15 12 10 | -156 -311 22 164
ngs 214| -3 0 4 -14 25 -9 -.03 13 11 | -830 -156 1534 3061
sio 321| 0 0 -1 42 41 132 -.07 11 12 | --- --- --- ---
Table 2.1819.4 GPS week: 1819 Day: 4 MJD: 56981.000
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 236| 0 0 -3 10 8 3 .06 9 8 | -1077 124 18 114
emr 80| -2 -3 9 -29 -29 15 .35 13 13 | 3008 965 16 174
esa 150| 0 0 2 9 -13 4 -.36 11 11 | -188 171 8 151
gfz 192| -1 0 1 -1 -6 40 -.14 13 12 | -155 378 12 152
grg 171| 3 -1 -21 6 26 -53 .22 18 17 | 176 -280 16 144
igr n/a| -1 0 -2 -10 0 -19 -.19 6 5 | -530 370 16 89
jpl 80| 1 2 9 -1 53 -53 .30 12 12 | 3016 977 16 126
mit 349| 2 0 -4 46 3 1 -.13 12 10 | -98 55 22 172
ngs 219| -1 0 0 -44 -35 -7 -.04 13 10 | -925 -194 1140 2760
sio 323| 0 0 1 -3 4 26 .02 12 11 | --- --- --- ---
Table 2.1819.5 GPS week: 1819 Day: 5 MJD: 56982.000
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 246| 0 0 0 18 0 -24 .01 9 9 | -839 -294 21 128
emr 80| 0 -5 6 -28 -8 -25 .24 13 13 | 3409 2077 16 168
esa 150| 1 0 1 7 -4 -30 -.40 13 13 | 204 -317 9 129
gfz 195| -2 0 0 -1 -23 24 -.09 12 12 | 183 -3 13 158
grg 169| 2 0 -14 -6 -12 -47 .13 17 16 | -339 701 16 125
igr n/a| -1 0 -5 -6 -7 -30 -.22 5 5 | -490 2336 15 86
jpl 80| 0 2 5 -9 32 -45 .24 12 12 | 3434 2060 18 126
mit 350| 1 0 -6 22 0 -9 -.15 14 11 | -352 361 22 193
ngs 215| 0 0 1 -21 5 -11 -.01 12 9 | -878 -218 1250 2745
sio 320| 1 0 4 22 -26 205 .09 13 12 | --- --- --- ---
Table 2.1819.6 GPS week: 1819 Day: 6 MJD: 56983.000
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 232| 2 0 -1 -5 12 9 .07 10 10 | -791 -320 20 114
emr 80| -4 -9 7 -39 -15 20 .23 14 14 | 5717 -200 17 152
esa 150| 1 0 2 -21 -4 26 -.40 12 12 | 921 -1205 13 154
gfz 182| -3 1 0 -9 0 54 -.15 13 12 | 332 -928 15 163
grg 169| 0 -1 -16 14 8 -11 .12 18 18 | 298 -297 17 161
igr n/a| -1 1 -4 2 27 -11 -.24 6 6 | 1893 396 16 87
jpl 80| 2 4 5 20 72 4 .20 13 13 | 5735 -185 18 142
mit 350| 1 1 -7 27 -46 -4 -.11 15 12 | -249 223 23 175
ngs 207| 0 3 -3 17 -57 -81 .01 14 12 | -776 -327 1480 2651
sio 306| 0 -1 8 9 -11 -46 .12 14 13 | --- --- --- ---
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 3.1819.0 GPS week: 1819 Day: 0 MJD: 56977.000
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 12 13 12 15 4 11 11 11 12 4 | 54 56 47 52 67 53 58 58 50 54 53
2 | 8 13 9 10 14 5 9 11 9 15 4 | 27 27 26 25 33 24 25 28 24 27 25
4 | 7 6 11 17 12 4 7 11 11 11 4 | 27 23 21 28 24 28 21 22 23 22 27
5 | 7 12 13 15 19 4 11 12 10 15 4 | 37 47 41 38 41 38 49 33 39 33 39
6 | 8 11 13 15 16 6 11 10 9 10 4 | 55 61 52 54 70 54 58 57 54 54 56
7 | 8 9 12 12 20 4 8 27 11 11 5 | 23 31 19 26 30 20 27 26 22 16 21
X8 | 10 12 12 13 --- 9 10 10 18 --- 5 | 28 34 31 31 --- 29 31 27 29 --- 29
9E | 10 14 14 12 18 5 12 19 10 19 5 | 301 295 302 298 304 300 25 304 297 305 299
10 | 6 10 12 13 14 5 9 10 8 14 3 | 18 24 20 14 22 16 23 17 15 18 17
11 | 8 11 16 10 18 4 9 11 11 15 4 | 48 52 46 50 66 49 52 54 47 51 49
12E | 11 19 8 13 17 6 14 16 8 16 5 | 62 63 59 64 66 60 63 65 61 59 62
13E | 7 9 9 14 19 4 8 8 6 10 3 | 25 29 24 23 31 22 27 22 23 23 24
14E | 6 9 6 12 20 4 10 14 9 14 4 | 26 26 21 25 33 22 23 21 23 16 23
15E | 7 14 8 14 21 5 14 17 17 18 5 | 31 31 28 34 26 28 32 30 33 22 29
16E | 8 17 7 18 19 5 13 14 14 13 5 | 27 36 27 35 33 27 30 25 29 24 28
17 | 7 11 12 9 17 5 11 13 9 16 4 | 32 33 26 28 43 30 30 30 31 24 29
18 | 9 12 10 14 16 5 13 18 12 17 5 | 24 26 22 26 32 21 26 23 19 15 21
19 | 9 16 12 12 23 4 12 12 16 15 5 | 26 35 26 31 40 28 30 30 31 28 28
20 | 11 11 11 11 20 5 11 14 10 14 4 | 23 31 24 26 33 24 30 30 24 22 24
21 | 9 11 10 12 13 7 11 18 11 17 4 | 26 23 25 23 32 23 21 29 19 24 23
22 | 7 11 11 15 16 4 12 13 14 16 4 | 29 29 28 33 40 27 28 30 25 24 27
23E | 6 13 7 16 23 6 10 13 12 13 4 | 25 33 23 30 33 25 30 28 29 23 27
24 | 9 13 14 10 21 7 10 12 13 19 4 | 23 27 27 23 27 24 28 20 23 13 23
25 | 10 13 14 11 20 5 11 13 10 10 4 | 28 29 31 22 34 24 29 19 22 18 25
26E | 12 18 13 16 17 6 15 21 14 12 5 | 68 68 69 70 63 69 66 58 69 64 66
27 | 10 10 16 15 20 5 11 11 12 10 5 | 26 32 31 28 28 25 29 27 24 22 26
28E | 9 10 7 10 17 5 7 13 7 9 3 | 37 37 30 34 38 31 36 35 30 29 33
29 | 9 15 11 16 20 8 15 15 13 14 5 | 24 35 24 19 29 21 32 16 23 18 23
30 | 8 12 12 9 15 5 19 9 10 10 4 | 22 31 25 19 30 21 33 19 22 14 23
31 | 8 16 11 13 19 7 13 23 13 14 5 | 29 38 23 28 36 22 36 21 29 18 26
32 | 6 8 13 9 18 6 8 9 11 9 3 | 22 29 25 21 19 21 28 19 24 18 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 11 13 18 5 11 15 11 14 |T 40 44 39 40 46 38 34 39 39 36 39
WRMS | 8 12 12 12 17 5 11 12 10 13 |NE 26 31 26 25 33 24 30 23 24 19 25
MEDI | 8 12 12 13 18 5 11 13 11 14 |MD 27 32 26 28 33 25 30 28 25 23 27
Table 3.1819.1 GPS week: 1819 Day: 1 MJD: 56978.000
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 9 11 10 13 5 10 11 8 10 3 | 36 42 30 30 45 32 41 36 34 37 35
2 | 6 12 10 11 10 5 9 8 10 14 3 | 18 21 20 24 20 19 21 19 17 21 18
4 | 8 7 11 16 10 5 8 16 15 11 4 | 22 23 20 19 18 20 21 18 26 17 19
5 | 7 14 16 11 18 6 12 9 17 12 4 | 28 41 33 30 37 31 39 27 36 29 31
6 | 5 11 13 8 12 5 11 8 9 9 3 | 34 42 31 34 46 33 40 34 29 33 34
7 | 10 8 12 9 16 5 10 24 9 13 4 | 24 29 19 24 27 18 25 22 23 15 19
X8 | 10 12 13 13 --- 6 10 10 13 --- 4 | 37 41 37 38 --- 40 39 37 41 --- 37
9E | 9 12 16 11 20 6 11 16 11 8 4 | 274 273 278 273 276 275 19 275 275 275 274
10 | 5 10 12 11 11 5 8 8 6 10 3 | 14 21 18 17 18 14 18 14 13 18 15
11 | 7 8 17 8 13 6 7 11 10 16 4 | 30 37 29 29 42 30 36 33 34 38 32
12E | 12 17 9 11 15 7 14 17 11 14 4 | 82 82 76 79 78 76 84 77 81 82 79
13E | 6 13 10 12 16 4 10 8 8 9 3 | 32 40 31 32 38 30 33 29 34 29 32
14E | 8 11 7 8 13 5 10 10 9 8 3 | 23 24 19 24 25 21 22 22 23 23 22
15E | 7 17 10 13 18 5 13 10 14 14 4 | 30 33 27 34 27 27 32 32 34 31 30
16E | 12 17 10 17 24 6 12 12 18 11 5 | 38 41 35 41 43 35 39 38 39 36 37
17 | 7 12 12 10 15 4 12 8 11 11 3 | 23 25 19 22 30 20 24 23 24 19 21
18 | 8 14 14 12 14 4 13 11 8 14 4 | 22 28 20 24 25 20 28 18 18 17 20
19 | 9 14 13 10 16 6 13 12 14 14 4 | 19 30 20 21 26 19 24 22 22 16 19
20 | 11 13 11 10 19 4 13 12 12 16 4 | 24 28 25 22 34 21 29 28 21 19 22
21 | 8 12 10 7 12 4 10 13 12 12 3 | 18 21 19 17 23 17 20 20 16 18 17
22 | 7 12 12 11 13 3 11 10 14 15 4 | 22 28 22 26 30 21 27 23 20 21 21
23E | 7 11 10 17 22 4 9 12 13 12 4 | 20 27 17 26 25 18 26 25 24 28 21
24 | 10 10 18 8 12 6 10 8 11 13 4 | 20 29 29 22 26 21 27 21 26 20 22
25 | 8 13 16 10 12 6 12 10 9 9 4 | 23 28 32 23 26 23 26 20 25 21 23
26E | 15 20 10 14 15 9 15 19 21 14 5 | 56 57 52 60 49 54 53 41 56 45 51
27 | 10 10 16 13 15 5 11 8 17 8 4 | 27 31 29 26 27 23 29 27 26 29 26
28E | 6 10 8 9 13 5 10 12 8 7 3 | 41 45 39 41 42 39 40 38 39 39 40
29 | 9 16 13 12 13 7 15 13 12 10 4 | 23 27 20 21 24 18 27 17 21 19 19
30 | 5 12 12 7 10 4 9 7 8 6 3 | 19 26 20 17 24 17 24 16 19 16 18
31 | 11 14 12 16 20 8 11 24 13 12 5 | 27 35 23 28 32 22 31 24 26 24 24
32 | 9 6 12 7 19 4 6 7 8 7 3 | 19 23 19 15 19 15 22 14 16 13 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 12 11 16 5 11 13 12 12 |T 36 41 35 36 40 34 31 35 36 34 35
WRMS | 8 13 12 10 14 5 11 10 10 11 |NE 23 29 24 24 26 21 27 21 23 20 22
MEDI | 8 12 12 11 14 5 11 11 11 11 |MD 24 29 25 26 27 21 27 24 26 21 22
Table 3.1819.2 GPS week: 1819 Day: 2 MJD: 56979.000
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 10 10 11 13 5 12 10 11 12 3 | 43 46 40 40 54 42 45 43 41 41 41
X2 | 11 13 13 13 13 5 --- 8 10 11 4 | 16 19 22 28 25 19 --- 24 23 22 19
4 | 7 7 9 14 11 4 7 13 12 11 3 | 23 19 18 20 23 20 18 19 17 19 21
5 | 8 11 15 11 17 3 12 8 13 9 4 | 31 34 29 26 32 24 37 24 33 26 27
6 | 6 11 12 9 12 5 13 7 10 9 3 | 42 46 41 44 54 40 45 43 43 41 42
7 | 8 9 14 12 14 5 11 21 12 10 4 | 24 25 19 22 26 16 26 17 23 13 17
X8 | 11 12 12 14 --- 12 9 9 11 --- 4 | 27 25 22 23 --- 27 25 23 26 --- 22
X9E | 11 21 17 15 31 8 --- 13 24 11 6 | 329 325 331 327 327 325 --- 328 319 328 327
10 | 8 10 13 12 14 5 9 8 6 12 3 | 18 21 19 22 21 13 19 15 15 21 16
11 | 10 8 15 10 16 4 10 11 10 14 4 | 38 43 38 37 51 37 40 39 31 41 37
12 | 9 18 9 13 27 5 17 12 12 13 5 | 55 59 52 61 64 56 57 58 62 54 56
13E | 6 11 9 12 16 5 13 7 9 10 3 | 27 30 23 26 36 23 30 23 24 25 24
14E | 7 12 7 10 13 5 10 8 9 7 3 | 33 27 29 33 33 27 32 29 30 26 28
15E | 8 15 9 11 19 5 13 12 12 11 4 | 30 29 28 33 29 27 30 31 32 29 29
16E | 12 18 11 16 21 9 11 11 14 11 5 | 59 56 55 56 55 49 55 59 53 59 55
17 | 6 12 11 8 16 5 14 10 11 12 3 | 24 26 22 26 34 21 27 24 23 19 22
18 | 8 15 13 15 18 5 14 12 12 13 4 | 20 24 19 24 30 16 25 18 19 15 17
19 | 9 19 11 12 21 5 13 12 12 14 4 | 25 30 23 25 32 20 26 23 23 20 21
20 | 10 11 12 9 17 4 13 11 12 12 4 | 28 31 26 27 35 25 30 26 27 18 25
21 | 8 14 12 12 11 6 10 10 13 11 4 | 20 19 23 19 24 17 23 24 19 21 18
22 | 9 13 13 17 17 4 13 10 11 13 4 | 27 26 23 32 38 22 27 23 18 20 22
23E | 6 15 8 16 27 5 11 15 14 9 4 | 28 30 21 29 29 21 27 31 30 30 25
24 | 10 11 15 6 13 4 10 10 10 12 3 | 20 27 25 21 26 18 25 19 23 15 19
25 | 6 11 14 11 11 4 11 9 9 6 3 | 22 23 28 19 23 17 23 18 20 19 19
26E | 21 22 13 12 17 8 18 20 23 13 6 | 56 54 50 55 49 52 53 39 55 43 49
27 | 11 10 12 12 20 4 11 9 10 9 4 | 27 31 28 24 29 23 29 26 27 30 26
28E | 9 9 9 9 14 8 10 12 8 8 3 | 57 57 56 57 56 54 58 57 61 57 56
29 | 8 15 12 13 14 8 15 13 13 13 4 | 23 25 18 21 26 17 27 14 25 22 18
30 | 7 12 13 7 10 3 10 7 13 6 3 | 19 24 23 19 23 17 26 15 22 15 18
31 | 8 15 14 14 20 5 12 22 15 9 5 | 25 32 23 29 34 20 30 20 23 21 21
32 | 9 7 10 9 16 4 8 6 9 8 3 | 23 25 23 21 22 19 26 17 23 18 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 12 12 17 5 12 12 12 11 |T 39 41 38 40 44 36 32 37 39 37 37
WRMS | 8 13 12 11 15 5 12 9 10 11 |NE 22 25 22 24 28 19 26 19 22 19 19
MEDI | 8 12 12 12 16 5 11 10 12 11 |MD 27 29 23 26 32 22 27 24 25 22 22
Table 3.1819.3 GPS week: 1819 Day: 3 MJD: 56980.000
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 12 10 16 14 4 13 11 9 12 4 | 48 48 44 43 58 44 49 47 42 47 45
2 | 10 10 10 13 14 5 9 9 13 13 4 | 25 24 23 28 31 24 25 27 25 25 24
4 | 9 8 10 18 14 5 10 10 13 13 4 | 22 21 18 21 19 19 19 17 20 18 20
5 | 9 11 16 11 19 5 13 8 14 11 4 | 34 40 32 28 31 28 39 26 29 29 30
6 | 7 10 13 9 12 5 11 8 13 11 3 | 47 51 42 45 58 45 49 50 44 51 47
7 | 9 10 13 8 17 4 12 21 11 10 4 | 26 29 20 22 28 18 28 20 25 17 20
X8 | 10 13 11 16 --- 11 14 8 14 --- 5 | 42 39 37 41 --- 41 39 37 45 --- 38
X9E | 12 21 19 9 27 12 --- 12 31 15 7 | 373 373 377 373 372 366 --- 375 361 377 373
10 | 8 8 12 10 15 5 8 8 8 10 3 | 21 24 20 18 25 17 21 18 16 20 18
11 | 8 9 14 13 17 4 10 11 9 12 4 | 40 44 40 39 55 39 43 42 35 44 40
12 | 10 18 8 12 21 5 16 15 15 15 5 | 38 44 35 44 45 37 43 41 40 36 38
13E | 6 11 9 10 16 5 12 8 13 6 3 | 25 29 20 20 32 20 28 21 23 24 22
14E | 8 11 6 11 13 5 11 12 8 7 3 | 27 25 23 27 27 25 25 28 23 28 24
15E | 7 14 9 11 24 6 14 11 13 10 4 | 30 29 24 29 23 26 29 28 31 29 26
16 | 13 16 7 12 22 5 13 13 11 12 4 | 55 60 56 58 57 55 57 57 61 58 56
17 | 8 10 12 10 17 6 13 10 16 10 4 | 26 26 19 20 34 18 24 24 29 22 21
18 | 9 13 12 14 17 7 16 12 13 17 4 | 25 26 21 30 31 22 25 23 25 18 21
19 | 8 16 11 10 18 4 17 10 13 12 4 | 23 32 22 22 32 21 28 26 21 27 22
20 | 14 14 12 12 16 4 14 11 12 14 4 | 29 32 26 27 37 25 32 29 28 25 26
21 | 8 12 12 7 16 6 9 15 12 13 4 | 25 20 23 21 31 21 21 25 18 23 20
22 | 8 14 12 14 16 4 14 12 16 14 4 | 30 30 27 32 38 26 30 29 30 25 27
23E | 10 14 8 14 27 5 12 15 12 10 4 | 28 30 23 30 28 23 28 34 28 33 27
24 | 10 11 14 7 13 5 10 11 13 14 4 | 22 26 23 18 24 17 23 17 21 13 18
25 | 9 17 13 8 14 4 12 9 10 8 4 | 22 27 27 19 23 20 25 18 22 19 20
26E | 19 23 11 16 18 9 17 20 26 14 6 | 49 49 44 46 41 45 47 32 50 39 41
27 | 12 14 12 12 18 5 13 9 15 6 4 | 33 36 33 28 26 26 28 27 32 28 28
28 | 11 10 10 9 14 9 10 11 6 10 3 | 67 68 60 66 63 60 68 64 66 65 65
29 | 11 15 11 10 18 7 16 15 14 13 4 | 27 32 25 20 25 19 30 18 25 23 21
30 | 6 11 13 8 13 5 14 9 10 6 3 | 22 25 22 18 25 17 26 16 21 19 19
31 | 9 14 12 13 22 5 12 21 10 9 4 | 26 34 22 26 36 23 31 23 29 24 23
32 | 18 9 11 10 18 4 9 6 9 9 4 | 23 28 24 20 19 17 27 18 28 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 11 12 17 5 13 12 13 11 |T 42 45 40 41 45 38 32 40 41 40 40
WRMS | 10 13 12 11 16 5 13 10 11 12 |NE 26 29 24 24 29 22 28 22 26 21 23
MEDI | 9 12 12 11 17 5 12 11 13 11 |MD 27 30 24 28 31 24 28 27 28 25 24
Table 3.1819.4 GPS week: 1819 Day: 4 MJD: 56981.000
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 | 5 13 9 16 14 5 12 12 12 13 4 | 41 44 38 39 53 38 44 41 42 41 40
2 | 7 13 11 14 15 6 9 9 12 14 4 | 20 21 18 25 23 21 19 22 26 21 20
4 | 8 9 10 21 16 4 8 10 16 11 4 | 23 20 20 24 26 20 22 20 23 16 19
5 | 7 10 16 12 19 6 11 10 8 11 4 | 32 37 31 26 32 27 35 25 33 27 29
6 | 7 11 14 8 14 6 10 9 15 7 3 | 39 45 36 39 54 37 42 42 45 39 40
7 | 11 10 13 10 19 4 12 23 10 11 4 | 25 28 19 18 27 18 24 21 21 17 18
X8 | 9 12 10 12 --- 6 11 6 13 --- 4 | 21 22 19 14 --- 17 20 17 20 --- 18
X9E | 11 21 18 13 45 8 --- 22 11 13 7 | 592 592 593 593 589 595 --- 598 594 595 592
10 | 10 10 12 11 17 5 8 9 7 9 3 | 24 22 16 13 26 15 19 19 19 21 18
11 | 7 10 14 14 17 5 10 11 15 13 4 | 40 42 37 37 49 35 39 38 37 41 38
12 | 10 16 10 11 22 6 14 11 11 13 4 | 35 38 30 38 39 33 37 34 35 33 33
13E | 7 10 8 16 20 4 12 11 9 8 4 | 23 28 18 17 31 19 25 20 23 25 20
14E | 8 12 7 13 16 6 10 8 9 7 3 | 21 22 17 24 28 18 19 20 22 23 19
15E | 8 15 7 12 23 6 13 10 9 11 4 | 31 30 23 30 25 25 29 29 33 31 28
16 | 8 24 9 13 20 4 16 15 12 15 5 | 37 44 36 39 42 36 42 41 39 35 37
17 | 8 10 10 11 20 6 13 9 13 9 4 | 21 25 17 20 31 16 22 19 21 18 18
18 | 8 14 12 16 14 6 13 12 9 21 4 | 22 29 20 24 29 19 24 21 19 23 20
19 | 10 16 10 12 20 5 17 11 11 11 4 | 23 34 22 22 34 20 27 26 23 21 22
20 | 11 13 12 10 16 4 15 11 11 12 4 | 28 33 27 25 38 26 31 28 29 27 26
21 | 8 13 12 8 13 5 9 11 11 18 4 | 21 21 20 17 27 17 18 22 14 26 18
22 | 9 17 12 14 16 7 13 10 10 21 4 | 28 31 27 29 38 23 29 28 24 30 26
23E | 8 12 7 11 22 5 12 15 11 10 4 | 27 32 19 23 25 20 25 34 25 30 25
24 | 7 10 13 8 15 7 12 7 8 16 3 | 21 27 23 18 25 17 23 19 21 14 19
25 | 6 13 14 8 14 5 11 9 9 7 3 | 19 27 26 21 25 19 22 17 21 19 20
26E | 25 19 15 17 19 12 17 20 33 14 7 | 52 53 48 50 48 48 48 37 55 42 45
27 | 14 15 11 11 14 7 10 15 9 14 4 | 27 33 31 25 29 25 32 30 23 32 27
28 | 7 10 8 9 22 6 11 10 9 8 3 | 40 42 35 38 45 36 37 37 39 35 37
29 | 8 16 12 13 14 5 16 15 10 9 4 | 24 31 24 21 24 20 29 20 24 22 21
30 | 8 10 12 18 13 4 11 10 9 7 4 | 24 27 24 19 27 19 23 17 18 22 20
31 | 8 14 11 14 23 4 11 21 20 13 5 | 23 31 19 26 34 19 28 18 25 20 20
32 | 7 9 10 8 19 4 7 6 9 10 3 | 17 25 19 15 23 15 22 15 20 17 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 13 18 6 12 12 13 12 |T 45 49 43 44 51 42 28 44 45 45 43
WRMS | 8 13 11 12 17 5 12 10 10 11 |NE 23 27 21 21 28 19 24 20 22 21 20
MEDI | 8 13 11 12 17 5 11 11 11 11 |MD 24 31 23 24 29 20 25 22 24 25 21
Table 3.1819.5 GPS week: 1819 Day: 5 MJD: 56982.000
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 12 13 16 14 6 10 11 13 11 4 | 32 40 25 32 40 32 42 34 35 33 33
2 | 8 10 13 15 13 5 8 12 10 17 4 | 16 20 15 25 14 16 16 19 15 18 15
X3 | 1 --- --- --- --- --- --- --- --- --- 0 | 9999 --- --- --- --- --- --- --- --- --- 9999
X4 | 1 --- --- --- --- 50 --- --- --- --- 0 | 79 --- --- --- --- 13 --- --- --- --- 76
5 | 8 11 17 14 17 5 12 10 10 17 4 | 28 35 30 27 29 24 32 22 30 32 27
6 | 6 14 13 9 11 5 10 11 15 12 4 | 33 43 28 34 40 31 37 36 25 32 32
7 | 8 14 13 8 16 3 9 17 9 9 4 | 27 29 21 24 27 19 25 19 23 25 22
X8 | 10 11 11 14 --- 6 9 8 9 --- 4 | 39 37 35 35 --- 37 36 37 39 --- 35
X9E | 18 29 27 22 95 8 --- 20 34 22 10 | 672 671 671 672 666 671 --- 671 664 673 670
10 | 9 10 12 11 16 4 6 10 8 13 3 | 19 26 19 18 21 14 20 16 16 25 17
11 | 9 10 16 15 17 5 9 9 13 11 4 | 28 37 29 28 39 28 38 30 33 33 30
12 | 9 16 10 12 20 5 14 13 9 14 4 | 37 39 31 40 44 36 40 37 39 39 36
13E | 7 10 9 9 13 4 13 14 8 11 3 | 25 30 21 23 29 19 25 21 20 31 22
14E | 6 11 7 11 13 6 10 9 8 8 3 | 21 22 18 23 21 17 23 18 20 19 19
15E | 8 13 11 12 22 5 14 13 13 16 4 | 27 27 21 28 23 22 26 26 27 34 25
16 | 10 22 9 15 21 4 14 15 12 17 5 | 26 27 20 26 29 22 27 29 27 29 23
17 | 8 12 12 9 16 4 14 12 15 11 4 | 23 26 15 21 26 15 22 18 26 18 18
18 | 9 11 13 13 12 4 13 13 9 19 4 | 23 28 21 29 26 20 28 21 24 24 22
19 | 9 17 12 14 20 4 13 13 9 14 4 | 20 29 19 23 27 18 25 26 21 20 20
20 | 11 13 13 13 17 5 15 14 12 16 4 | 27 34 27 27 34 26 36 30 27 24 26
21 | 8 8 10 11 12 5 9 10 8 11 3 | 21 23 19 21 21 17 19 20 17 22 18
22 | 8 12 13 14 14 5 11 11 11 16 4 | 28 32 26 33 36 25 33 28 29 27 27
23E | 8 15 10 11 21 7 12 26 14 14 5 | 29 29 19 28 21 22 27 47 28 38 27
24 | 10 10 15 6 15 5 10 16 16 19 4 | 19 26 24 19 24 18 23 22 27 21 19
25 | 8 16 16 10 14 6 11 8 8 6 4 | 22 26 29 23 25 21 25 17 24 20 21
26E | 20 20 16 16 21 8 15 21 30 16 7 | 51 49 45 51 48 46 46 33 52 37 43
27 | 9 11 17 16 15 3 12 21 11 13 5 | 28 28 34 22 27 23 27 37 28 34 26
28 | 7 11 9 9 20 4 10 11 10 11 3 | 28 31 22 28 35 25 30 26 27 26 26
29 | 10 16 13 12 14 6 16 14 11 15 4 | 24 28 22 23 25 20 28 16 25 23 21
30 | 5 9 14 9 12 4 8 12 7 9 3 | 22 24 24 15 23 16 23 17 19 22 19
31 | 9 13 11 14 20 5 10 23 7 13 4 | 23 30 20 30 34 20 28 19 24 21 21
32 | 9 9 13 11 16 3 7 9 7 8 3 | 22 26 24 19 21 17 26 18 20 17 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 13 12 17 5 12 14 12 13 |T 49 51 45 48 50 43 28 47 47 48 46
WRMS | 9 13 13 12 16 5 12 11 9 12 |NE 24 28 23 24 25 20 26 20 24 23 21
MEDI | 8 12 13 12 16 5 11 12 10 13 |MD 27 29 22 26 27 21 27 22 26 25 23
Table 3.1819.6 GPS week: 1819 Day: 6 MJD: 56983.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1M | 6 14 11 15 13 4 10 12 15 12 4 | 55 55 47 48 65 50 56 56 48 52 52
2 | 9 11 12 11 13 6 9 8 12 14 4 | 26 23 22 27 27 20 20 26 21 22 22
X3 | 2 --- 258 193 --- 79 --- --- --- --- 0 | 9999 --- 9999 9999 --- 9999 --- --- --- --- 9999
X4M | 7 11 12 18 --- 5 8 13 --- 11 5 | 23 12 8 7 --- 7 10 4 --- 4 23
5 | 10 13 16 15 15 5 14 11 12 15 4 | 34 42 35 30 31 29 39 30 36 35 32
6M | 10 14 11 7 11 7 10 10 13 13 4 | 56 60 50 51 65 49 54 57 48 52 53
7 | 11 16 12 8 19 6 13 19 10 14 4 | 28 30 21 22 29 20 26 22 26 28 22
X8 | 16 13 14 18 --- 14 11 9 18 --- 6 | 32 28 29 27 --- 31 30 26 34 --- 28
X9E | 29 55 35 52 118 14 --- 46 79 42 19 | 863 865 875 873 870 870 --- 881 877 883 871
10 | 10 13 13 10 13 6 9 10 10 13 4 | 20 33 24 21 26 18 22 22 21 31 21
11M | 9 16 15 15 17 5 10 13 17 13 5 | 46 51 47 45 62 47 50 53 44 48 47
12 | 10 15 9 11 16 6 14 13 11 14 4 | 43 45 39 47 47 41 47 43 44 43 43
13E | 10 9 7 10 14 5 14 14 10 16 4 | 25 32 24 24 31 22 28 23 25 39 25
14E | 5 11 7 15 15 6 12 9 10 6 3 | 23 21 20 26 24 21 25 19 25 23 21
15E | 8 17 9 12 20 6 15 10 16 14 4 | 32 29 26 31 23 25 28 27 32 33 27
16 | 9 21 9 16 22 6 14 12 11 17 5 | 41 46 38 44 40 38 41 42 42 40 39
17 | 10 12 10 10 19 5 13 10 10 11 4 | 26 29 20 23 33 18 24 22 22 21 21
18 | 9 15 14 19 16 7 14 14 13 20 5 | 24 27 23 37 34 23 28 26 27 28 24
19M | 11 15 10 12 22 6 13 19 14 14 5 | 33 43 37 37 44 33 36 41 36 31 35
20M | 13 15 13 13 17 6 14 19 16 17 5 | 38 45 39 39 52 39 43 44 36 44 39
21M | 7 11 12 14 14 3 11 10 11 11 4 | 23 22 27 28 31 22 24 25 22 25 22
22 | 9 13 13 13 20 5 13 14 12 15 4 | 33 34 30 38 47 32 35 35 34 34 33
23E | 14 14 12 14 33 8 17 31 17 22 7 | 50 47 51 50 38 44 49 67 47 67 49
24 | 9 12 14 10 15 7 10 11 13 14 4 | 21 25 24 18 24 17 23 19 22 17 19
25 | 10 12 14 8 13 4 12 9 11 9 4 | 19 26 25 19 24 16 23 18 19 26 20
26E | 21 22 13 20 18 11 17 19 36 19 7 | 49 49 44 53 46 48 48 34 59 41 44
27M | 10 13 12 9 18 5 9 11 13 17 4 | 51 56 57 51 54 49 50 51 47 53 51
28 | 9 13 8 9 18 5 10 12 12 10 4 | 42 41 34 40 45 36 39 39 41 40 38
29 | 12 18 14 15 17 7 16 15 11 11 5 | 25 34 26 27 30 23 34 17 26 20 23
30 | 9 13 14 10 12 6 11 14 12 11 4 | 24 24 26 20 25 19 24 21 21 25 21
31 | 9 12 13 14 24 5 12 25 16 14 5 | 26 30 22 31 36 23 31 23 30 23 23
32M | 10 11 12 10 16 3 9 18 12 11 4 | 21 23 21 19 22 18 25 23 23 20 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 12 13 18 6 13 15 14 14 |T 59 62 58 59 66 56 33 59 61 61 58
WRMS | 10 14 12 12 18 6 13 12 12 13 |NE 26 29 25 26 30 22 27 23 26 25 23
MEDI | 10 13 12 13 17 6 12 13 12 14 |MD 32 33 27 31 34 25 30 26 32 31 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 4.1819 GPS week: 1819 MJD: 56977.0-56983.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 |U 4 4 11 |U 8 9 34 |U 6 6 14 |
emr | emr 2958 | 7 6 15 |U 8 9 31 | 6 6 19 |
esa | esa 2976 | 6 5 17 |U 8 10 33 | 7 7 18 |
gfz | gfz 2972 |U 5 5 11 |U 8 9 34 |U 7 6 17 |
grg | grg 2852 | 9 8 20 |U 10 10 38 |U 8 9 20 |
igr | igr 2962 | 5 5 12 | 7 9 33 | 6 6 15 |
igs | igs 2967 | 5 4 12 | 8 9 33 | 6 6 15 |
jpl | jpl 2875 | 7 6 17 |U 9 10 35 |U 8 7 17 |
mit | mit 2962 | 6 5 14 |U 8 9 36 |U 7 7 19 |
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 5.1819.0 GPS week: 1819 Day: 0 MJD: 56977.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 3 4 13 | 9 8 32 | 5 4 11 |
emr | emr 2976 | 5 5 17 | 8 8 28 | 6 5 18 |
esa | esa 2976 | 4 5 17 | 9 9 32 | 7 6 19 |
gfz | gfz 2976 | 4 4 13 | 9 8 29 | 7 6 16 |
grg | grg 2880 | 7 8 21 | 9 9 36 | 7 7 21 |
igr | igr 2976 | 4 5 14 | 9 8 30 | 6 5 14 |
igs | igs 2976 | 4 4 14 | 9 8 29 | 6 5 14 |
jpl | jpl 2976 | 5 4 17 | 9 10 31 | 6 4 17 |
mit | mit 2976 | 4 5 14 | 9 8 30 | 6 6 15 |
Table 5.1819.1 GPS week: 1819 Day: 1 MJD: 56978.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 4 3 9 | 9 10 41 | 5 5 16 |
emr | emr 2972 | 5 4 16 | 9 11 43 | 5 6 20 |
esa | esa 2976 | 4 4 16 | 8 12 40 | 6 6 19 |
gfz | gfz 2972 | 4 3 14 | 9 11 41 | 6 4 17 |
grg | grg 2880 | 7 8 14 | 11 13 46 | 9 10 21 |
igr | igr 2976 | 4 4 14 | 8 11 41 | 5 5 17 |
igs | igs 2976 | 4 4 11 | 9 10 41 | 5 5 17 |
jpl | jpl 2970 | 6 6 18 | 9 12 41 | 8 7 21 |
mit | mit 2976 | 5 4 10 | 10 12 38 | 5 6 19 |
Table 5.1819.2 GPS week: 1819 Day: 2 MJD: 56979.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 13 | 8 10 42 | 7 8 17 |
emr | emr 2972 | 8 6 16 | 9 11 40 | 8 8 23 |
esa | esa 2976 | 7 6 16 | 8 13 43 | 8 8 21 |
gfz | gfz 2972 | 6 6 11 | 10 13 45 | 9 9 23 |
grg | grg 2879 | 7 6 18 | 9 12 47 | 8 10 20 |
igr | igr 2976 | 6 6 12 | 8 10 42 | 7 8 17 |
igs | igs 2976 | 6 5 14 | 8 11 41 | 7 8 19 |
jpl | jpl 2778 | 10 8 16 | 12 15 54 | 11 11 17 |
mit | mit 2976 | 6 6 13 | 8 9 46 | 7 9 23 |
Table 5.1819.3 GPS week: 1819 Day: 3 MJD: 56980.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 3 4 9 | 9 9 26 | 5 6 12 |
emr | emr 2972 | 8 6 16 | 9 9 26 | 5 5 16 |
esa | esa 2976 | 6 5 14 | 9 10 26 | 6 7 16 |
gfz | gfz 2972 | 5 5 10 | 9 10 29 | 6 6 15 |
grg | grg 2880 | 13 9 29 | 11 9 33 | 8 8 15 |
igr | igr 2976 | 4 5 11 | 9 9 27 | 6 7 14 |
igs | igs 2976 | 5 5 12 | 9 9 27 | 6 6 13 |
jpl | jpl 2876 | 7 6 14 | 10 11 30 | 7 7 16 |
mit | mit 2976 | 4 5 11 | 9 9 28 | 5 6 14 |
Table 5.1819.4 GPS week: 1819 Day: 4 MJD: 56981.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 5 8 | 7 7 37 | 6 7 12 |
emr | emr 2972 | 9 6 13 | 8 6 32 | 7 8 20 |
esa | esa 2976 | 6 4 15 | 7 8 34 | 7 8 17 |
gfz | gfz 2972 | 6 5 9 | 9 7 38 | 7 8 17 |
grg | grg 2880 | 9 11 14 | 10 7 37 | 7 9 18 |
igr | igr 2976 | 5 5 9 | 7 7 36 | 6 7 15 |
igs | igs 2976 | 5 5 10 | 8 7 36 | 6 7 16 |
jpl | jpl 2874 | 7 5 18 | 8 8 38 | 7 6 17 |
mit | mit 2976 | 5 7 15 | 8 8 39 | 9 12 28 |
Table 5.1819.5 GPS week: 1819 Day: 5 MJD: 56982.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 5 4 12 | 5 8 30 | 6 6 13 |
emr | emr 2876 | 9 6 15 | 6 7 26 | 7 6 15 |
esa | esa 2880 | 6 5 19 | 5 9 26 | 7 7 15 |
gfz | gfz 2876 | 7 5 12 | 6 7 26 | 7 6 15 |
grg | grg 2784 | 11 7 20 | 8 8 31 | 9 9 19 |
igr | igr 2880 | 5 5 14 | 5 7 28 | 6 5 13 |
igs | igs 2880 | 7 5 14 | 5 7 27 | 6 6 13 |
jpl | jpl 2780 | 8 7 16 | 6 8 28 | 6 6 16 |
mit | mit 2880 | 10 6 17 | 6 8 33 | 6 5 16 |
Table 5.1819.6 GPS week: 1819 Day: 6 MJD: 56983.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 | 4 4 12 | 7 7 31 | 7 5 15 |
emr | emr 2972 | 9 7 16 | 9 9 26 | 8 7 22 |
esa | esa 3072 | 5 5 20 | 8 9 28 | 9 7 19 |
gfz | gfz 3068 | 6 5 10 | 7 8 29 | 9 6 16 |
grg | grg 2784 | 9 7 26 | 11 9 38 | 10 9 30 |
igr | igr 2976 | 5 4 14 | 6 7 26 | 7 5 15 |
igs | igs 3015 | 6 4 11 | 7 7 27 | 7 6 16 |
jpl | jpl 2876 | 9 9 18 | 8 8 25 | 8 6 18 |
mit | mit 2976 | 6 4 17 | 7 8 34 | 9 7 18 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1819 GPS week: 1819 MJD: 56977.500-56983.500
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 13 -64 47 7 | 13 21
| 17 16 78 127 4 | 5
emr uuuuu | 25 16 165 20 4 | 42 46
| 17 13 71 32 7 | 2
esa uuuuu | 13 9 31 -9 0 | 18 24
| 7 19 50 62 3 | 3
gfz uuuux | 3 -21 -6 23 1 | -63 65
| 18 18 103 118 5 | 2
grg uuuuu | -16 3 -93 -127 -6 | 20 25
| 14 29 132 103 8 | 2
igr xxxxx | -27 -2 38 -60 1 | 0 17
| 15 16 56 61 4 | 2
irf xxxxx | 6 7 -53 5 2 | -2 15
| 4 9 44 12 3 | 3
jpl uuuuu | -25 -21 22 29 -5 | 33 38
| 30 24 108 72 10 | 1
mit uuuuu | 4 8 -143 -6 -1 | 10 17
| 11 21 71 27 4 | 1
ngs uuuuu | -2 6 87 -48 -2 | 4 14
| 38 35 109 63 6 | 1
sio uuxxx | -18 -13 -11 -80 8 | 33 36
| 20 20 64 38 11 | 4
Table 7.1819.0 GPS week: 1819 Day: 0 MJD: 56977.500
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 13 -96 -65 15 | 6 13
emr uuuuu | 35 20 134 24 0 | 40 44
esa uuuuu | 21 11 66 15 2 | 15 20
gfz uuuux | 11 -32 -36 165 -4 | -66 67
grg uuuuu | -32 41 -172 -231 -6 | 21 26
igr xxxxx | -50 -5 68 6 2 | -2 17
irf xxxxx | 8 18 -30 12 -1 | -5 14
jpl uuuuu | -20 -31 64 -13 6 | 32 36
mit uuuuu | -2 28 -91 30 -6 | 9 16
ngs uuuuu | -14 -36 82 36 -15 | 4 15
sio xxxxx | -51 26 -22 -51 -9 | 28 32
Table 7.1819.1 GPS week: 1819 Day: 1 MJD: 56978.500
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 15 1 9 1 | 10 22
emr uuuuu | -3 11 174 31 7 | 41 46
esa uuuuu | 22 19 -25 -56 -1 | 18 25
gfz uuuux | 3 4 -61 55 -1 | -64 66
grg uuuuu | -12 22 -197 -202 -15 | 22 28
igr xxxxx | -30 -17 -13 12 2 | 0 20
irf xxxxx | 2 23 -101 -15 3 | -3 17
jpl uuuuu | -14 -33 139 117 4 | 34 41
mit uuuuu | 4 35 -224 -49 0 | 10 19
ngs uuuuu | 2 -40 119 -2 3 | 5 17
sio uuxxx | 3 -24 -67 -88 8 | 29 34
Table 7.1819.2 GPS week: 1819 Day: 2 MJD: 56979.500
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 19 66 65 3 | 9 21
emr uuuuu | 6 4 75 -29 9 | 39 43
esa uuuuu | 3 -4 102 -90 2 | 16 22
gfz uuuux | 24 -53 -61 128 8 | -65 67
grg uuuuu | 0 -43 -26 -173 -4 | 19 25
igr xxxxx | -24 31 -46 -153 2 | -3 17
irf xxxxx | 3 2 -96 -3 3 | -4 16
jpl uuuuu | -18 7 -172 96 -7 | 32 37
mit uuuuu | 10 6 -219 -14 -2 | 9 17
ngs uuuuu | 0 53 218 -95 0 | 3 14
sio uuxxx | -11 -13 -86 -124 8 | 29 34
Table 7.1819.3 GPS week: 1819 Day: 3 MJD: 56980.500
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 | 15 -7 -34 38 10 | 12 20
emr uuuuu | 43 8 255 45 11 | 40 44
esa uuuuu | 17 0 56 79 6 | 18 23
gfz uuuux | 20 -15 -43 -1 -1 | -63 64
grg uuuuu | -32 21 -197 -67 -12 | 20 25
igr xxxxx | -5 3 63 -37 7 | -1 16
irf xxxxx | 7 6 -38 7 3 | -2 14
jpl uuuuu | 20 10 -36 -8 1 | 33 37
mit uuuuu | 11 11 -101 -27 0 | 10 16
ngs uuuuu | -67 0 52 -114 -5 | 4 14
sio uuxxx | -41 -9 3 -47 -2 | 32 35
Table 7.1819.4 GPS week: 1819 Day: 4 MJD: 56981.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -10 -1 -104 -123 7 | 16 23
emr uuuuu | 28 5 208 39 8 | 44 47
esa uuuuu | 6 -12 29 -41 -3 | 21 25
gfz uuuux | 1 -11 -92 75 0 | -61 63
grg uuuuu | -7 9 -113 33 -5 | 20 25
igr xxxxx | -22 -7 71 -60 1 | 2 16
irf xxxxx | 8 5 -84 22 6 | 0 14
jpl uuuuu | -33 -21 125 97 -10 | 35 39
mit uuuuu | 10 14 -197 0 6 | 11 18
ngs uuuuu | 29 31 181 21 -4 | 5 14
sio uuxxx | -15 -11 -48 -31 12 | 36 37
Table 7.1819.5 GPS week: 1819 Day: 5 MJD: 56982.500
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 | 19 11 -148 161 9 | 17 24
emr uuuuu | 25 21 229 50 1 | 45 48
esa uuuuu | 11 6 27 -28 -4 | 20 25
gfz uuuux | -11 -24 50 -148 7 | -62 63
grg uuuuu | -3 -1 -121 -38 -7 | 18 22
igr xxxxx | -14 -16 112 -69 3 | 1 16
irf xxxxx | 11 0 -39 6 2 | 0 14
jpl uuuuu | -30 -19 50 -22 -10 | 34 38
mit uuuuu | 15 -20 -127 19 0 | 11 17
ngs uuuuu | -19 33 75 -89 1 | 3 11
sio uuxxx | -12 -18 53 -95 21 | 36 38
Table 7.1819.6 GPS week: 1819 Day: 6 MJD: 56983.500
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 | 33 42 -133 246 5 | 20 25
emr uuuuu | 39 42 81 -20 -10 | 45 49
esa uuuuu | 14 45 -38 58 1 | 21 25
gfz uuuux | -28 -16 204 -116 -2 | -61 62
grg uuuuu | -28 -25 174 -214 10 | 17 21
igr xxxxx | -43 0 9 -118 -6 | 2 16
irf xxxxx | 1 -2 20 5 -2 | 2 13
jpl uuuuu | -82 -58 -19 -63 -22 | 32 37
mit uuuuu | -18 -17 -42 0 -7 | 12 17
ngs uuuuu | 53 -1 -119 -91 1 | 3 11
sio uuxxx | -2 -40 90 -126 19 | 39 41
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