[IGSREPORT-22664] Wk 1786 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Apr 18 10:47:42 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1786 (Mar 30, 2014 - Apr 05, 2014)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1786[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1786[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1786[0-6].cls IGS GPS clock combination summary report.
igs17867.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17867.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 | MAL2 MAL2
0 | EMR | MCM4
0 | GFZ | 1 2 1
0 | GRG | 10 MAL2 NYA1 THTI MAL2 NYA1 THTI
0 | MIT | 1 20 27 31 1 3 15 18 20 24 27 NTUS MDVJ NTUS
1 | COD | ASPA
1 | EMR | 10 MCM4 MCM4
1 | ESA | FAA1 HYDE FAA1
1 | GFZ | 1 2 1 HYDE NKLG
1 | GRG | 21 10 21 DGAR MAC1 NYAL THTI WUHN DGAR FAA1 MAC1
1 | GRG | NKLG NYAL THTI
1 | JPL | 10 GUAM NAMA PIMO RESO
1 | MIT | 23 31 10 15 21 23 MDVJ
2 | COD | REUN MAC1 REUN
2 | EMR | MCM4
2 | ESA | PIMO PIMO UNSA
2 | GFZ | 1 1 BAKO GUAM REUN
2 | GRG | HYDE KELY NTUS QAQ1
2 | MIT | 21 NTUS TLSE GOPE MDVJ NTUS TLSE
3 | COD | 10
3 | EMR | 10 21 MCM4
3 | ESA | 10 TSKB TSKB UNSA
3 | GFZ | 1 2 1 10 REUN WES2 WES2
3 | GRG | 10 32 32 FAA1 RBAY THTI FAA1 RBAY THTI
3 | MIT | 10 23 31 23 31 DARW
4 | COD | 10 KARR KARR
4 | EMR | 10 21 21 32 HERS
4 | ESA | 10 FAA1 FAA1 MBAR SYOG UNSA
4 | GFZ | 1 2 1 10 CAS1 CAS1 HNLC
4 | GRG | 10 32 DGAR FAA1 KARR RBAY THTI DARW DGAR FAA1 KARR
4 | GRG | NTUS RBAY THTI
4 | JPL | 10 THTI
4 | MIT | 10 14 27 28 14 25 27 28 32 AUCK IRKJ KIRU KOKB MAW1
4 | MIT | MDVJ MOBS NNOR TNML YEBE IRKJ MDVJ YEBE
5 | COD | 10 KARR KARR
5 | EMR | 10 32 MCM4 MCM4
5 | ESA | 10 PIMO PIMO SEY1 UNSA
5 | GFZ | 1 2 1 10 ARTU BJFS ARTU BJFS
5 | GRG | 10 32 BJFS DAV1 FAA1 BJFS DAV1 FAA1 MAL2 PIMO
5 | JPL | 8 22
5 | MIT | 10 32 MDVJ
6 | COD | 10 32 ARTU
6 | EMR | 12 26 MCM4 MCM4
6 | ESA | 1 2 3 4 5 7 8 9 10 11 12 13 14 15 16 17 18 19 20
6 | ESA | 21 22 23 24 25 26 27 28 29 31 32 1 2 3 4 5 7 8 9
6 | ESA | 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26
6 | ESA | 27 28 29 31 32 DGAV
6 | GFZ | 1 2 1 10 32
6 | GRG | SPT0 ARTU MAL2 SPT0
6 | JPL | 32
6 | MIT | 21 DAV1 DAV1
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G32 | 2014_04_01 | 2014033
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
6 | GRG | 6
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G06 | | | | | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.9 .4 -2.6 -20 14 -46 .71
EMR | 0 | 2.2 -2.9 4.7 -27 8 -60 .87
ESA | 0 | 4.7 5.3 25.1 -75 -63 45 .43
GFZ | 0 | -.4 .5 -.6 -8 -22 1 -.14
GRG | 0 | -2.7 1.5 4.9 2 4 12 .86
JPL | 0 | 7.2 2.2 15.2 -61 20 -11 .80
MIT | 0 | 2.3 -.5 7.0 -18 2 -36 .53
NGS | 0 | 10.4 3.4 15.4 -32 -66 46 .56
SIO | 0 | -.7 5.6 -37.7 -12 10 575 .38
COD | 1 | -.7 -.3 -2.5 -27 5 -52 .88
EMR | 1 | 10.4 -9.3 9.9 -32 18 -79 .84
ESA | 1 | 6.1 4.5 18.1 -49 -56 51 .34
GFZ | 1 | .3 .8 -1.2 -5 -34 -6 .01
GRG | 1 | 1.4 -4.9 9.5 -15 -1 3 1.07
JPL | 1 | 6.9 -.1 13.8 -20 60 12 1.12
MIT | 1 | 3.6 -5.1 9.5 -28 14 -52 .67
NGS | 1 | 11.6 -2.5 11.2 -44 -63 41 .82
SIO | 1 | 2.0 4.9 -37.4 -62 -31 1136 .47
COD | 2 | -1.4 .3 -1.9 -30 4 -20 .55
EMR | 2 | 3.1 -11.5 6.4 -27 16 -73 .89
ESA | 2 | 1.7 -4.1 23.1 -31 -35 12 .38
GFZ | 2 | .0 .6 -1.2 -15 -41 11 .10
GRG | 2 | -1.3 -5.9 3.9 -11 -11 2 1.01
JPL | 2 | 6.5 5.0 18.6 6 4 36 .73
MIT | 2 | 6.3 -5.7 11.2 -10 14 -59 .75
NGS | 2 | 5.7 -12.8 3.5 -74 -25 -14 .79
SIO | 2 | .7 -.7 -25.0 -4 21 -46 .46
COD | 3 | -.1 .7 -1.1 -15 -8 -17 .61
EMR | 3 | -1.3 -9.7 8.6 -2 7 -45 .49
ESA | 3 | -1.7 2.7 34.0 32 -43 5 .40
GFZ | 3 | .0 .9 -.8 -17 -50 13 -.08
GRG | 3 | 1.3 -.2 11.6 -15 -18 0 .88
JPL | 3 | -6.5 -1.5 10.7 33 80 73 .87
MIT | 3 | 1.0 -5.0 11.8 -11 -6 -66 .56
NGS | 3 | 3.2 -9.9 13.7 -93 -28 -10 .65
SIO | 3 | -5.2 -.4 -40.8 36 -3 -231 .42
COD | 4 | -.1 .8 -.7 -13 6 -59 .48
EMR | 4 | -.3 -2.6 16.2 0 9 -45 .67
ESA | 4 | -3.8 3.5 32.7 -62 -17 15 .27
GFZ | 4 | -.1 .6 -1.2 -7 -33 16 .10
GRG | 4 | -2.9 .1 4.7 -12 1 -13 .88
JPL | 4 | -1.4 6.9 13.4 -43 10 -38 .57
MIT | 4 | 1.3 -2.9 13.9 10 -4 -8 .84
NGS | 4 | 1.5 -5.4 15.5 -83 -30 -2 .63
SIO | 4 | -2.8 2.0 -31.3 53 -14 113 .27
COD | 5 | -.3 .7 -1.0 -5 -2 -35 .44
EMR | 5 | -.4 1.2 8.1 -3 16 -56 .58
ESA | 5 | .0 4.5 27.4 0 -66 48 .30
GFZ | 5 | .4 .8 -.9 -6 -37 19 -.07
GRG | 5 | -2.5 -2.1 6.0 -10 7 -3 .92
JPL | 5 | 5.3 4.1 16.4 -57 -88 85 .75
MIT | 5 | 4.8 -.6 13.3 20 -18 -14 .78
NGS | 5 | -2.6 -5.2 14.2 -73 -1 -32 .78
SIO | 5 | -.2 2.9 -26.2 5 -9 81 .36
COD | 6 | -1.8 .1 -1.8 -30 21 -14 .66
EMR | 6 | 1.6 -1.6 5.7 4 17 -53 .54
ESA | 6 | -1.4 2.4 24.6 -57 -68 33 .11
GFZ | 6 | .4 .6 -1.3 -22 -36 -2 .24
GRG | 6 | -1.3 .2 12.3 -19 -11 1 .87
JPL | 6 | 4.6 3.8 15.7 -25 -9 -68 .65
MIT | 6 | 5.5 .5 8.7 21 -2 -20 .88
NGS | 6 | -3.6 -6.7 17.8 -100 1 -45 .99
SIO | 6 | .3 .3 -23.1 38 -17 100 .68
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1786.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1786.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 2.1786.[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 3.1786.[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 5.1786.0-6). 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 1786 summary. (Mar 30, 2014 - Apr 05, 2014)
Table 1.1786.a GPS week: 1786 MJD: 56746.000-56752.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 0 4 13 29 -15 .02 9 8 | -1095 287 17 110
| 0 0 1 20 16 12 .03 | 443 698
emr 80| 0 -2 1 2 -24 19 .17 14 14 | 3465 4 15 121
| 1 1 1 16 11 20 .04 | 541 867
esa 150| 0 1 -2 -12 -29 10 -.25 6 6 | -2137 1587 18 189
| 0 0 1 32 24 12 .01 | 1117 1107
gfz 199| 0 0 -4 30 6 21 .12 10 9 | 195 18 12 130
| 1 0 0 20 13 12 .02 | 224 675
grg 182| 0 -2 12 -29 -17 10 .42 20 18 | -91 84 18 157
| 3 2 2 22 19 18 .18 | 249 346
igr n/a| 0 1 -1 8 14 -15 -.24 5 5 | 1579 492 18 96
| 0 0 0 19 7 11 .03 | 949 876
jpl 80| 0 3 -6 8 3 -26 .01 16 16 | 2264 116 19 138
| 1 1 1 35 35 20 .04 | 664 913
mit 299| 0 -2 3 27 0 -9 .03 11 10 | -43 -158 24 218
| 0 0 1 23 21 19 .01 | 277 511
ngs 227| 0 0 -2 -74 19 -12 .04 13 12 | -1028 199 1759 3430
| 1 1 2 51 68 6 .05 | 453 674
sio 479| 0 0 -8 -6 -12 226 -.52 21 20 | --- --- --- ---
| 0 0 1 16 18 449 .06 | --- ---
Table 1.1786.b GPS week : 1786 MJD: 56746.000-56752.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 5 5 5 5 5 5 5 |
3 | 4 4 3 4 4 4 4 |
4 | 4 4 4 4 4 4 5 |
5 | 5 4 5 4 5 5 4 |
6 | --- --- --- --- 0 0 0 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 4 4 4 4 4 |
9 | 3 4 4 4 4 4 4 |
10 | 6 6 5 5 4 4 4 |
11 | 4 4 4 3 4 4 4 |
12 | 5 5 5 5 5 6 5 |
13 | 5 5 4 4 4 5 4 |
14 | 4 4 5 4 5 5 5 |
15 | 5 5 4 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 6 5 5 5 5 5 5 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 5 4 5 4 5 4 4 |
21 | 4 4 4 4 4 4 5 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 4 5 5 4 |
24 | 4 4 4 4 4 4 5 |
25 | 4 4 4 4 4 4 5 |
26 | 4 4 4 4 4 4 5 |
27 | 4 4 4 4 4 5 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 0 0 0 0 0 0 0 |
31 | 5 4 4 4 5 5 5 |
32 | 4 5 0 6 5 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 2.1786.0 GPS week: 1786 Day: 0 MJD: 56746.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 249| 0 0 2 35 40 -11 -.04 9 9 | -639 -215 17 117
emr 79| 0 0 1 0 -11 13 .16 14 14 | 4138 303 13 128
esa 150| 1 1 -2 -44 -64 9 -.27 7 7 | -1182 1274 11 171
gfz 196| -2 0 -4 59 19 22 .14 10 10 | 45 1334 11 129
grg 189| 0 0 10 7 -11 -1 .25 14 14 | 260 -98 16 163
igr n/a| 0 1 -2 0 13 -25 -.23 5 5 | 1194 436 16 95
jpl 80| 0 1 -6 -4 65 -54 -.02 15 15 | 3061 488 19 137
mit 300| 0 -2 4 36 -19 11 .03 12 12 | 381 -405 24 229
ngs 233| 1 1 -2 -74 24 -11 .11 12 10 | -639 -222 2067 4019
sio 486| 0 0 -7 8 14 547 -.51 21 23 | --- --- --- ---
Table 2.1786.1 GPS week: 1786 Day: 1 MJD: 56747.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 0 -1 5 -5 36 -22 .02 8 8 | -1475 632 17 112
emr 80| 1 -4 2 -5 -24 39 .11 15 15 | 3678 -302 14 126
esa 150| 0 2 -2 -13 -42 24 -.23 7 7 | -3275 1096 11 162
gfz 202| -1 1 -5 33 -14 6 .13 10 9 | 395 -644 16 148
grg 187| 5 2 9 -20 0 9 .23 16 15 | -239 137 16 140
igr n/a| 0 0 -1 0 26 -20 -.27 5 4 | 885 39 17 102
jpl 80| 0 4 -8 4 19 -26 -.00 17 17 | 2746 -308 21 129
mit 299| 0 -2 3 31 36 -29 .05 11 10 | -72 -559 29 239
ngs 229| -1 -1 -2 -17 19 -9 .03 14 13 | -1589 959 1707 3703
sio 488| 0 0 -8 -24 -9 1098 -.48 21 20 | --- --- --- ---
Table 2.1786.2 GPS week: 1786 Day: 2 MJD: 56748.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 251| 0 0 5 38 42 0 .01 9 9 | -1775 1299 17 111
emr 80| 1 -3 3 -3 -14 36 .18 15 15 | 3436 -295 15 128
esa 150| 0 1 -4 -21 -18 1 -.25 7 7 | -2262 2893 12 167
gfz 202| -1 1 -6 46 12 25 .13 9 9 | -149 -427 12 125
grg 181| 4 -1 10 -17 6 50 .29 15 15 | -471 476 18 152
igr n/a| 0 0 -1 15 18 -2 -.24 5 4 | 924 155 18 98
jpl 80| 0 6 -7 39 10 -44 -.03 16 16 | 2325 -435 21 141
mit 297| 0 -2 4 1 20 -31 .02 9 9 | -542 425 26 216
ngs 225| 0 0 -4 -124 -91 -13 -.03 13 12 | -1746 1252 1903 3245
sio 485| 0 1 -6 -6 5 -45 -.41 20 18 | --- --- --- ---
Table 2.1786.3 GPS week: 1786 Day: 3 MJD: 56749.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| 0 0 2 -1 29 -8 .02 9 9 | -694 -336 16 102
emr 80| 0 -3 2 -11 -16 30 .21 14 14 | 3654 -1484 15 111
esa 150| 0 1 -2 49 -4 -4 -.26 6 6 | -160 -218 11 154
gfz 201| 0 0 -5 7 7 32 .12 10 9 | 73 196 12 121
grg 184| -1 -3 15 -61 -52 12 .43 19 18 | 77 -138 21 143
igr n/a| 0 1 -1 -23 13 3 -.27 5 5 | 1585 -839 16 87
jpl 80| 3 5 -4 -7 -41 0 -.00 17 17 | 2333 -1273 18 123
mit 300| 0 -3 3 -3 6 -26 .06 10 9 | -145 4 26 234
ngs 221| 0 -1 -1 -94 -15 -10 .08 13 12 | -653 -356 2001 3424
sio 480| -1 1 -7 -18 -11 -218 -.54 21 19 | --- --- --- ---
Table 2.1786.4 GPS week: 1786 Day: 4 MJD: 56750.000
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| 0 -1 3 22 37 -34 .04 9 9 | -743 -537 18 113
emr 81| 0 -1 2 15 -46 15 .22 14 14 | 2696 -72 22 119
esa 150| 0 1 0 -27 1 -1 -.25 6 6 | -2817 1073 9 135
gfz 201| 1 0 -4 42 -8 37 .10 10 10 | 504 -545 13 134
grg 185| -2 -3 13 -25 -25 2 .45 20 18 | 91 -487 19 177
igr n/a| 0 1 -2 39 15 -27 -.26 6 6 | 1008 456 25 104
jpl 80| 2 3 -5 51 -1 0 .03 15 15 | 1200 -77 19 140
mit 300| 0 -2 3 27 -11 13 .03 11 11 | 98 -997 24 212
ngs 230| 0 1 -5 -149 -7 -26 .01 14 12 | -762 -517 1813 3110
sio 481| 0 0 -10 11 -41 89 -.60 21 20 | --- --- --- ---
Table 2.1786.5 GPS week: 1786 Day: 5 MJD: 56751.000
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 243| 1 0 2 -13 27 -24 .04 8 8 | -1355 963 19 114
emr 81| -2 0 1 -13 -28 -20 .15 15 15 | 2783 1310 14 115
esa 150| 0 1 -2 11 -32 28 -.25 6 6 | -3087 2239 12 169
gfz 197| 0 0 -3 15 12 23 .09 10 9 | 304 62 12 126
grg 176| -3 -4 15 -45 -11 7 .54 24 20 | -117 276 19 147
igr n/a| 0 0 -1 19 7 -15 -.22 5 5 | 1904 1781 17 97
jpl 80| 1 2 -5 -54 -35 -34 .05 15 16 | 1556 1313 19 168
mit 300| 0 -1 3 68 -19 0 .03 11 10 | -15 266 22 211
ngs 229| 0 -1 -2 -46 94 -7 .06 13 12 | -986 273 1444 3287
sio 469| -1 0 -9 -23 -25 72 -.58 20 18 | --- --- --- ---
Table 2.1786.6 GPS week: 1786 Day: 6 MJD: 56752.000
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 5 18 -4 -5 .04 8 8 | -990 205 21 102
emr 80| -1 0 -1 33 -25 18 .16 14 14 | 3876 570 17 120
esa 150| 1 0 -1 -38 -48 12 -.24 6 6 | -2180 2756 60 365
gfz 196| 1 0 -3 8 19 2 .13 10 9 | 193 150 12 129
grg 175| -3 -4 13 -44 -26 -4 .73 29 24 | -242 427 19 181
igr n/a| 0 0 0 8 4 -19 -.19 5 5 | 3558 1418 22 95
jpl 80| -1 3 -6 30 4 -21 .06 16 16 | 2633 1108 20 132
mit 300| 1 0 0 28 -8 0 .03 13 11 | -8 156 23 189
ngs 225| 0 0 2 -13 111 -5 -.00 12 11 | -824 5 1380 3222
sio 467| 0 0 -9 8 -19 43 -.50 21 20 | --- --- --- ---
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 3.1786.0 GPS week: 1786 Day: 0 MJD: 56746.000
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 6 13 10 4 16 9 16 14 4 | 40 43 36 39 38 38 45 35 49 44 38
2 | 6 17 9 11 12 4 18 10 12 22 4 | 23 30 24 23 28 20 29 23 31 19 23
3 | 8 9 6 8 19 3 10 14 12 16 4 | 25 30 23 30 33 24 27 29 30 19 26
4 | 6 12 6 10 12 5 15 10 7 24 3 | 24 25 18 21 21 20 25 21 24 34 20
5E | 8 22 7 10 13 5 17 13 16 8 5 | 55 56 50 58 50 52 54 56 57 48 53
7 | 9 12 8 9 15 4 10 10 11 17 3 | 33 36 26 32 34 28 33 31 32 27 30
8 | 7 10 6 7 14 4 11 12 8 21 3 | 35 39 28 32 30 31 38 33 34 36 32
9 | 7 9 6 6 11 4 10 14 8 24 3 | 28 31 25 29 27 26 33 29 27 34 27
10E | 9 17 9 14 17 10 19 19 14 22 5 | 94 89 88 89 96 91 92 100 92 97 91
11 | 10 12 7 7 16 5 12 9 12 10 4 | 28 38 29 33 45 29 33 32 27 27 30
12M | 7 18 8 11 13 6 23 12 9 16 4 | 36 38 32 43 40 32 37 38 40 30 35
13 | 12 15 8 11 15 6 16 9 12 22 4 | 33 41 39 47 45 37 44 40 39 41 38
14 | 7 15 8 8 13 7 13 10 9 24 3 | 37 38 41 48 40 42 43 43 36 42 40
15 | 11 17 10 10 12 5 15 12 13 26 4 | 28 30 24 32 28 23 29 27 26 25 25
16 | 6 14 7 8 17 4 22 15 10 23 4 | 29 31 25 32 37 28 30 32 35 25 29
17 | 14 23 7 12 11 4 20 13 16 28 5 | 29 35 32 34 35 29 30 40 34 26 31
18E | 7 13 4 10 21 4 14 11 8 11 4 | 37 37 36 44 39 35 36 41 37 33 36
19M | 8 11 6 9 17 4 14 11 13 40 4 | 27 36 27 36 35 26 29 34 32 33 30
20E | 11 12 8 7 19 4 12 9 21 10 4 | 40 41 38 45 40 40 41 47 58 41 42
21M | 7 13 8 8 15 5 16 9 13 29 4 | 26 27 22 27 33 21 32 22 26 31 23
22E | 6 11 6 10 15 4 13 9 8 13 3 | 25 24 28 34 31 24 26 29 25 27 26
23 | 10 16 7 11 12 6 13 9 16 34 4 | 30 38 35 45 39 35 40 35 43 42 36
24 | 8 11 5 6 17 6 13 13 9 15 3 | 31 34 25 33 32 27 32 30 31 31 29
25 | 6 13 8 7 10 5 13 9 8 8 3 | 41 47 38 43 47 41 44 45 43 39 42
26 | 10 11 8 10 10 4 10 12 10 11 4 | 31 35 40 42 36 35 37 38 35 37 36
X27 | 8 10 6 8 --- 5 10 13 10 13 3 | 39 44 41 42 --- 41 44 47 41 38 41
28M | 11 13 6 9 14 3 12 9 8 10 3 | 36 34 32 36 39 31 29 36 31 28 32
29M | 11 15 8 12 14 4 18 12 11 34 4 | 37 38 33 41 39 33 37 38 33 43 35
X30 | 3 --- --- --- --- 29 --- --- --- --- 0 | 71 --- --- --- --- 74 --- --- --- --- 70
31M | 8 14 8 8 16 5 13 16 15 15 4 | 32 39 26 34 43 28 35 31 33 26 31
32 | 10 13 9 9 14 6 14 15 11 19 4 | 12 11 11 8 6 8 10 14 11 10 9
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 7 10 14 5 15 12 12 21 |T 35 37 32 37 37 33 36 36 36 34 35
WRMS | 9 14 7 10 14 5 15 12 10 23 |NE 30 35 30 35 35 30 34 33 34 32 31
MEDI | 8 13 7 9 14 5 13 11 11 17 |MD 32 36 29 34 37 31 33 34 33 33 32
Table 3.1786.1 GPS week: 1786 Day: 1 MJD: 56747.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 11 6 5 14 3 13 10 11 13 3 | 29 33 28 32 32 30 37 27 36 32 30
2 | 7 20 7 12 14 4 21 10 13 27 4 | 18 28 16 20 25 15 26 19 23 20 18
3 | 6 9 5 9 18 4 11 10 18 13 4 | 25 24 22 23 26 20 25 26 25 20 23
4 | 5 14 6 8 11 4 16 8 13 22 3 | 19 22 15 18 19 14 20 18 23 27 17
5E | 7 17 7 10 13 7 21 10 11 9 4 | 43 47 38 44 45 38 41 47 45 39 42
7M | 7 14 7 9 20 4 16 8 14 14 4 | 27 31 21 27 33 22 27 23 25 21 24
8M | 9 12 7 10 13 4 12 13 14 24 4 | 30 34 25 27 26 25 30 26 34 35 27
9M | 8 10 7 9 12 4 9 10 15 24 3 | 28 32 27 29 29 26 29 29 32 35 27
10E | 12 22 11 14 17 5 26 21 13 18 6 | 98 101 97 96 102 95 96 105 96 102 98
11 | 10 10 6 8 21 4 12 9 17 9 4 | 23 31 22 25 37 21 30 23 20 18 23
12 | 9 21 7 10 22 4 27 11 12 13 5 | 28 32 24 31 37 23 32 30 31 25 27
13 | 10 17 7 11 13 5 15 8 18 19 4 | 27 33 27 30 35 25 34 27 26 26 27
14 | 6 15 5 10 15 7 12 12 14 20 4 | 23 27 28 34 28 27 31 30 22 27 27
15 | 9 17 8 9 13 5 19 10 14 29 4 | 26 29 19 28 28 19 26 24 27 22 22
16 | 5 17 6 10 16 5 21 14 13 23 4 | 28 27 20 24 29 21 26 26 24 18 22
17 | 9 23 9 11 11 4 23 13 11 24 5 | 27 32 30 29 30 25 29 31 28 21 27
18E | 5 16 4 8 16 3 16 9 8 10 3 | 43 43 40 45 47 40 40 44 41 39 42
19M | 6 12 6 7 14 5 17 10 15 37 4 | 25 28 23 24 26 19 26 27 24 28 23
20E | 8 12 7 11 17 4 13 12 15 9 4 | 34 34 33 36 35 33 33 38 38 31 34
21 | 6 14 7 8 15 4 17 9 14 32 4 | 16 22 14 20 25 13 24 16 23 30 16
22E | 6 13 5 7 12 4 12 10 13 11 3 | 18 20 19 24 26 16 21 20 21 18 19
23 | 11 15 8 15 15 5 14 7 20 36 4 | 27 33 27 32 29 24 29 25 21 35 26
24 | 6 13 5 9 18 3 16 8 9 11 3 | 26 29 21 30 32 22 29 25 27 26 25
25 | 8 18 6 10 13 4 12 9 11 9 4 | 33 36 29 34 38 30 34 33 30 30 31
26 | 9 11 6 8 12 5 11 8 9 18 3 | 25 28 28 28 28 27 28 30 30 32 26
X27 | 10 8 6 9 --- 5 11 11 17 13 4 | 31 29 28 25 --- 25 33 32 27 25 28
28M | 8 10 6 11 18 4 13 9 16 9 4 | 26 29 24 29 34 23 24 28 28 21 26
29 | 11 15 7 11 15 4 21 11 10 32 4 | 27 29 20 27 25 19 27 25 25 35 23
X30M | 4 --- --- --- --- 24 --- --- --- --- 0 | 67 --- --- --- --- 63 --- --- --- --- 67
31 | 7 13 7 10 17 5 12 11 16 20 4 | 27 33 20 29 36 21 31 29 29 16 26
32 | 10 13 5 11 18 4 18 17 10 18 4 | 10 12 8 6 7 7 12 12 9 9 8
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 15 7 10 16 5 17 11 14 21 |T 30 32 26 30 32 26 31 29 29 28 29
WRMS | 8 15 7 9 15 4 17 10 13 20 |NE 25 28 23 27 29 22 28 25 25 24 24
MEDI | 8 14 6 10 15 4 15 10 13 18 |MD 27 29 24 28 29 23 29 27 27 26 26
Table 3.1786.2 GPS week: 1786 Day: 2 MJD: 56748.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 14 13 6 8 12 5 15 9 13 13 4 | 35 40 32 34 32 32 42 33 40 38 33
2 | 8 17 7 13 13 3 21 10 10 25 4 | 23 27 20 25 22 19 29 19 24 22 21
3 | 7 10 5 7 14 3 11 8 14 20 3 | 25 27 21 26 30 22 25 26 25 29 24
4 | 9 11 7 9 11 6 11 9 12 18 3 | 26 26 24 23 21 22 24 20 28 28 23
5E | 6 17 6 12 21 6 17 9 10 10 4 | 45 46 43 48 38 43 44 43 48 38 43
7 | 8 13 9 9 16 4 14 8 13 13 4 | 33 35 25 31 33 26 33 26 29 26 29
8 | 10 10 7 7 13 3 11 7 14 21 3 | 33 33 26 30 26 26 33 27 23 33 27
9 | 9 11 7 7 12 3 12 8 11 26 3 | 32 30 27 31 25 26 30 26 23 35 27
10E | 12 16 10 11 15 8 19 13 10 15 5 | 73 70 70 71 73 71 70 75 75 74 72
11 | 8 12 4 6 16 4 15 7 11 9 3 | 28 34 23 26 38 24 29 25 27 23 26
12 | 6 22 7 8 17 3 23 9 11 15 4 | 34 34 27 35 35 30 34 33 34 26 30
13 | 9 17 7 10 12 4 20 9 13 15 4 | 31 40 33 37 38 31 42 32 30 33 33
14 | 9 19 8 9 14 6 16 8 18 21 4 | 29 31 32 36 30 30 34 33 27 34 30
15 | 8 18 8 9 12 4 16 9 9 30 4 | 26 31 21 30 27 20 28 25 25 24 24
16 | 6 18 6 9 15 5 25 10 15 24 4 | 27 32 22 27 31 23 30 29 25 24 25
17 | 10 21 6 8 9 5 21 12 16 33 4 | 28 33 29 29 29 26 31 31 31 30 28
18E | 8 14 6 7 17 4 13 10 18 9 4 | 26 29 28 30 29 26 31 29 25 26 27
19 | 7 15 6 4 11 3 15 8 8 26 3 | 21 29 21 26 29 21 25 26 22 21 23
20E | 7 14 7 11 17 6 12 16 12 9 4 | 30 37 31 35 34 32 34 34 41 33 32
21 | 10 14 5 8 14 3 18 9 14 24 4 | 20 21 16 18 22 13 23 15 16 23 15
22E | 7 13 6 6 17 5 16 8 18 11 4 | 21 21 22 24 17 18 22 20 19 20 19
23 | 12 17 7 12 13 6 15 9 12 31 4 | 28 37 32 37 31 29 34 29 32 34 30
24 | 9 14 7 9 19 3 14 5 7 15 4 | 32 33 25 32 31 26 29 28 27 27 27
25 | 6 12 6 9 11 4 13 7 13 8 3 | 38 39 33 37 41 35 40 37 37 32 36
26 | 8 11 7 10 13 4 14 7 12 15 3 | 36 36 39 41 37 36 40 36 39 38 37
X27 | 10 10 6 8 --- 5 13 9 16 12 4 | 30 36 32 31 --- 32 37 36 32 31 32
28 | 8 13 6 7 18 6 15 10 14 11 4 | 28 27 22 27 34 24 24 28 26 23 24
29 | 10 16 6 11 15 5 22 13 12 33 4 | 29 30 24 31 30 25 31 32 27 41 27
X30 | 4 --- --- --- --- 39 --- --- --- --- 0 | 55 --- --- --- --- 53 --- --- --- --- 54
31 | 8 15 7 9 17 4 14 9 17 19 4 | 29 37 25 31 38 25 33 29 33 21 28
X32 | 4 --- --- --- --- 29 --- --- --- --- 0 | 44 --- --- --- --- 44 --- --- --- --- 45
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 7 9 15 5 16 9 13 20 |T 32 33 28 32 32 29 33 30 30 30 30
WRMS | 9 15 7 9 15 4 16 9 12 18 |NE 28 33 27 31 30 26 32 28 29 29 28
MEDI | 8 14 7 9 14 4 15 9 13 15 |MD 29 33 26 31 31 26 31 29 27 29 28
Table 3.1786.3 GPS week: 1786 Day: 3 MJD: 56749.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 10 7 8 17 4 13 9 21 13 4 | 36 39 34 35 34 32 42 34 44 38 34
2 | 8 19 7 12 19 4 18 11 11 31 4 | 22 30 22 25 33 19 31 26 28 30 23
3 | 10 9 5 6 19 3 14 9 14 19 3 | 26 28 24 26 34 22 29 28 26 25 25
4 | 6 11 5 10 26 5 14 7 10 28 3 | 25 26 20 22 36 19 26 22 22 36 22
5E | 6 14 5 10 13 5 18 12 15 11 4 | 46 48 40 48 46 40 45 47 44 38 44
7 | 6 11 5 10 19 5 13 7 12 14 3 | 32 34 27 32 37 27 32 30 32 29 29
8 | 6 11 4 9 26 6 11 7 11 27 3 | 27 34 26 28 33 25 32 29 30 36 27
9 | 5 10 5 8 23 5 11 8 10 26 3 | 28 31 27 30 35 26 32 30 29 35 28
10E | 9 13 7 15 18 5 18 12 10 14 4 | 96 93 92 94 102 91 96 99 94 97 94
11 | 9 10 5 7 18 5 10 7 12 12 3 | 30 37 29 33 46 31 35 30 28 28 31
12 | 6 18 7 10 20 5 29 11 11 11 5 | 36 37 31 38 42 31 39 36 33 28 33
13 | 10 15 7 12 17 4 14 8 11 18 4 | 35 39 36 42 43 34 41 37 34 37 36
14 | 7 17 7 10 17 4 19 9 10 20 4 | 37 35 36 41 37 36 37 38 37 36 36
15 | 8 17 7 11 16 4 18 11 13 26 4 | 28 32 25 31 31 22 28 26 27 25 25
16 | 15 16 5 8 17 4 21 13 16 23 4 | 31 31 24 29 38 23 28 30 25 22 26
17 | 11 21 5 9 16 5 21 12 13 34 4 | 31 36 33 32 41 29 36 36 32 36 31
18E | 9 12 5 10 19 5 17 9 13 12 4 | 36 34 34 36 38 31 34 35 35 31 33
19 | 6 13 5 6 15 4 15 7 19 31 3 | 27 33 26 29 33 23 33 29 29 24 27
20E | 8 14 6 11 22 5 14 10 11 11 4 | 31 30 29 33 34 28 33 32 38 32 30
21 | 9 16 5 11 20 5 20 8 12 26 4 | 21 25 20 22 35 16 27 20 20 26 19
22E | 7 12 5 7 21 4 15 9 13 13 3 | 24 26 26 25 28 22 26 25 20 25 23
23 | 9 14 7 12 15 4 16 10 13 36 4 | 34 35 33 41 36 32 35 33 40 42 34
24 | 7 10 6 8 19 7 18 9 12 13 3 | 32 32 27 33 37 28 36 30 31 28 29
25 | 7 15 5 9 18 4 13 12 10 9 3 | 44 43 38 43 48 38 37 40 42 37 40
26 | 10 12 5 11 24 5 12 7 14 17 4 | 33 35 35 40 41 32 36 33 33 36 34
X27 | 11 8 7 9 --- 4 15 8 8 14 3 | 36 38 40 38 --- 35 43 42 37 28 38
28 | 7 13 5 7 19 4 12 9 10 9 3 | 29 32 30 33 40 27 30 34 31 28 30
29 | 10 16 6 11 16 4 22 14 9 33 4 | 34 37 31 38 45 29 35 37 33 40 33
X30 | 2 --- --- --- --- 19 --- --- --- --- 0 | 67 --- --- --- --- 68 --- --- --- --- 67
31 | 8 16 5 7 16 4 14 10 16 17 4 | 30 38 28 34 42 28 36 32 32 25 31
32E | 14 21 7 11 22 9 21 14 16 17 5 | 44 56 46 47 50 41 45 53 50 49 48
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 6 10 19 5 17 10 13 21 |T 35 36 32 35 40 31 36 35 34 34 34
WRMS | 9 14 6 9 18 5 17 9 12 19 |NE 31 33 29 33 37 28 34 31 31 31 30
MEDI | 8 13 5 10 19 5 15 9 12 17 |MD 32 34 29 33 37 29 35 32 32 31 31
Table 3.1786.4 GPS week: 1786 Day: 4 MJD: 56750.000
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 7 8 16 7 13 8 19 14 4 | 28 32 28 28 29 27 37 28 38 35 28
2 | 10 16 6 13 23 6 17 14 12 23 5 | 16 26 17 21 28 14 24 22 24 20 17
3 | 5 10 4 9 21 4 10 6 17 16 3 | 22 24 18 20 31 17 23 23 22 21 20
4 | 8 10 5 8 27 5 10 10 10 32 3 | 20 22 15 16 33 14 19 16 21 35 16
5E | 7 15 5 10 18 8 19 17 22 8 5 | 39 41 32 40 40 37 34 42 43 35 36
X6 | 4 --- --- --- --- --- --- --- --- --- 0 | 9999 --- --- --- --- --- --- --- --- --- 9999
7 | 6 13 8 9 18 5 12 8 11 14 3 | 26 30 22 25 33 22 27 25 23 21 23
8 | 8 9 5 8 27 6 10 6 12 25 3 | 23 29 22 24 30 21 27 23 24 30 22
9 | 7 9 5 10 24 5 9 7 9 28 3 | 19 26 20 23 31 20 26 21 23 31 20
10E | 10 11 6 11 19 8 15 11 11 12 4 | 60 60 54 57 61 59 62 63 61 56 58
11 | 11 10 5 10 18 8 11 8 20 10 4 | 28 34 29 31 45 27 35 30 24 21 29
12 | 10 17 7 12 21 5 27 10 14 14 5 | 30 31 25 33 36 25 34 29 25 21 26
13 | 9 15 6 13 17 5 14 10 11 20 4 | 26 37 29 36 39 29 37 29 30 31 30
14 | 6 20 6 9 20 8 16 12 12 17 4 | 28 31 30 35 36 31 31 33 36 29 30
15 | 13 16 8 12 17 6 16 10 11 34 4 | 24 30 19 29 30 18 23 22 22 26 21
16 | 6 16 6 8 20 5 19 15 16 25 4 | 26 25 21 22 36 21 22 27 28 23 22
17 | 10 19 6 10 15 5 18 14 14 25 4 | 21 32 25 29 32 23 26 33 24 25 24
18E | 7 13 6 12 19 7 14 12 13 11 4 | 31 27 30 35 36 27 26 24 29 23 27
19 | 7 13 6 8 14 5 13 5 18 37 3 | 24 28 21 24 30 19 25 25 24 27 22
20E | 9 12 6 12 19 8 14 14 22 11 4 | 18 23 19 23 25 20 22 25 36 24 20
21 | 7 14 6 11 19 7 17 12 12 24 4 | 19 23 17 23 34 16 23 15 19 23 16
22E | 8 14 6 10 21 7 13 9 9 10 4 | 25 27 23 28 35 24 23 21 26 22 22
23 | 9 14 7 12 15 6 14 13 15 37 4 | 26 33 28 35 31 27 31 26 29 39 27
24 | 7 9 6 10 23 7 14 9 14 10 4 | 26 31 24 31 32 22 30 26 25 25 25
25 | 11 13 6 11 19 5 10 13 14 11 4 | 45 48 46 45 52 43 47 45 40 39 44
26 | 8 8 5 9 28 7 8 9 16 16 4 | 28 32 30 34 41 32 30 29 39 31 31
X27 | 10 6 7 11 --- 6 12 8 14 12 4 | 37 35 35 35 --- 31 38 37 32 27 35
28 | 4 12 4 8 18 6 10 9 15 9 3 | 25 29 27 29 33 24 27 31 28 23 26
29 | 15 16 8 11 17 7 20 17 12 33 5 | 33 32 28 33 35 27 27 30 30 33 28
X30 | 4 --- --- --- --- 24 --- --- --- --- 0 | 54 --- --- --- --- 48 --- --- --- --- 53
31 | 11 24 7 10 19 7 16 9 11 15 5 | 27 35 20 26 38 20 29 26 29 18 23
32E | 12 13 7 10 16 10 15 17 14 14 4 | 35 32 31 29 32 31 29 35 28 35 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 6 10 20 6 15 11 14 21 |T 28 31 26 29 35 26 29 28 29 28 27
WRMS | 9 14 6 10 18 6 15 11 12 20 |NE 25 30 24 28 34 23 29 27 28 27 25
MEDI | 8 13 6 10 19 6 14 10 14 15 |MD 26 31 25 29 33 24 27 26 28 26 26
Table 3.1786.5 GPS week: 1786 Day: 5 MJD: 56751.000
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 11 7 9 21 4 12 7 12 15 3 | 26 33 24 22 29 25 33 27 33 32 26
2 | 8 16 6 13 20 4 16 14 16 30 4 | 14 23 14 20 29 13 20 18 20 28 15
3 | 5 10 5 8 32 4 14 6 20 20 4 | 22 22 20 22 39 17 20 22 24 23 21
4 | 6 12 5 9 35 5 11 9 8 21 4 | 17 21 15 19 40 15 18 16 18 24 16
5E | 7 14 6 8 18 6 18 19 13 10 4 | 36 38 30 35 41 31 30 40 35 28 33
X6 | 3 --- --- --- --- 482 --- --- --- --- 0 | 9999 --- --- --- --- 268 --- --- --- --- 9999
7 | 8 11 8 9 24 4 12 7 12 15 3 | 27 29 22 26 35 23 25 24 29 25 24
8 | 8 11 5 9 37 6 8 9 10 23 4 | 23 28 20 22 39 21 25 23 26 29 22
9 | 7 11 6 8 34 6 8 8 12 24 3 | 20 26 20 22 39 20 23 23 26 28 21
10E | 9 13 7 9 24 5 14 10 14 13 4 | 70 74 70 70 76 72 70 72 79 72 71
11 | 7 13 7 10 18 4 11 7 16 11 3 | 24 35 25 27 43 23 30 24 22 21 25
12 | 7 20 7 12 19 3 31 12 12 17 5 | 26 29 22 31 37 22 29 27 26 24 24
13 | 11 16 6 11 19 5 14 12 13 19 4 | 22 34 22 28 38 23 31 28 25 27 24
14 | 9 21 6 10 24 6 15 6 12 17 4 | 29 27 29 33 37 28 27 28 26 23 27
15 | 7 17 8 9 19 3 16 13 13 32 4 | 22 27 19 24 32 17 23 21 25 27 20
16 | 7 16 6 9 23 4 19 11 15 19 4 | 24 27 21 24 40 19 22 24 26 19 22
17 | 8 20 7 9 21 7 20 14 9 27 4 | 19 31 22 23 28 17 25 25 21 28 20
18E | 5 13 3 9 22 5 13 10 10 11 3 | 22 25 20 23 29 21 21 23 20 23 21
19 | 6 16 8 8 15 4 15 7 14 33 4 | 25 30 24 24 31 19 24 24 22 23 23
20E | 8 12 5 12 22 5 15 12 12 10 4 | 26 30 26 29 25 27 24 31 35 31 27
21 | 5 12 8 12 22 5 18 11 13 25 4 | 13 19 11 17 33 12 22 15 11 27 11
22E | 6 15 5 6 24 4 15 10 10 13 3 | 18 24 20 22 29 19 24 21 20 22 19
23 | 9 15 8 13 19 5 15 15 11 34 4 | 21 31 24 30 31 24 26 26 24 35 24
24 | 6 9 6 8 26 4 14 13 9 12 3 | 22 24 18 26 33 19 28 23 22 22 21
25 | 8 13 5 8 21 4 12 11 14 11 4 | 44 49 44 46 52 43 47 48 47 44 45
26 | 9 8 6 8 34 5 8 11 13 15 4 | 22 24 24 22 38 20 23 22 26 23 22
X27 | 7 9 9 10 --- 4 13 5 20 15 4 | 29 31 35 30 --- 28 35 30 32 24 31
28 | 9 14 4 7 20 3 13 10 11 12 3 | 20 24 17 23 30 19 24 26 23 20 20
29 | 10 17 6 12 19 4 20 14 14 27 5 | 28 30 23 28 37 23 27 30 28 31 25
X30 | 3 --- --- --- --- 21 --- --- --- --- 0 | 44 --- --- --- --- 39 --- --- --- --- 44
31 | 9 24 7 8 24 5 14 8 13 17 4 | 26 34 17 25 40 19 25 22 25 19 22
32E | 11 11 6 11 21 8 15 14 11 15 4 | 39 39 38 40 44 39 39 41 39 36 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 15 6 10 24 5 15 11 13 20 |T 26 30 24 27 37 32 28 27 27 27 26
WRMS | 8 15 6 9 20 5 16 10 12 18 |NE 22 27 22 25 35 37 25 23 24 25 22
MEDI | 7 13 6 9 22 5 14 10 12 17 |MD 24 29 22 24 37 21 25 24 25 25 23
Table 3.1786.6 GPS week: 1786 Day: 6 MJD: 56752.000
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 4 8 25 5 13 7 12 16 3 | 31 33 26 27 33 28 38 31 38 38 29
2 | 8 16 7 15 25 5 16 14 9 29 4 | 20 28 20 28 38 20 27 23 22 32 20
3 | 7 8 5 7 40 5 12 6 11 19 3 | 24 26 23 26 50 20 27 25 23 26 23
4 | 6 13 5 8 46 4 12 11 14 22 4 | 22 24 16 18 56 17 23 23 22 27 19
5E | 6 15 5 8 18 4 19 15 10 14 4 | 42 46 37 44 46 40 40 45 42 37 41
X6 | 3 --- --- --- 686 146 --- --- --- --- 0 | 9999 --- --- --- 15 139 --- --- --- --- 9999
7 | 7 13 7 8 29 3 12 11 14 16 4 | 33 35 26 31 42 26 33 30 26 29 28
8 | 7 11 5 6 48 5 10 9 10 25 4 | 27 32 23 24 51 24 30 29 25 32 25
9 | 7 12 6 7 44 4 10 11 9 28 4 | 28 33 26 27 53 27 32 33 27 35 27
10E | 11 13 5 8 24 6 15 13 14 14 4 | 86 85 84 85 101 83 84 90 80 89 85
11 | 9 12 6 9 19 5 12 9 15 9 4 | 38 45 37 40 56 37 41 39 34 34 38
12 | 9 20 6 10 25 2 28 14 8 17 5 | 35 38 31 40 47 33 40 39 37 31 34
13 | 9 15 5 10 25 5 14 13 10 18 4 | 35 41 36 43 50 34 41 39 31 39 36
14 | 7 19 6 11 27 8 18 10 11 17 4 | 36 33 36 42 41 39 35 38 35 33 35
15 | 10 18 8 10 23 5 19 20 17 28 5 | 27 31 23 29 38 21 28 26 29 26 23
16 | 9 14 6 12 25 4 21 16 13 24 5 | 29 29 24 31 44 25 27 29 30 25 26
17 | 8 22 7 8 26 6 19 18 15 30 5 | 35 39 33 36 44 31 33 41 32 36 33
18E | 7 11 5 9 20 5 15 11 10 10 3 | 24 23 21 26 31 21 20 27 26 24 22
19 | 8 14 9 8 16 6 18 6 14 25 4 | 25 32 27 29 36 23 30 28 29 25 26
20E | 6 12 4 9 21 2 13 9 12 9 3 | 31 28 31 30 38 31 32 35 38 35 31
21 | 8 15 8 11 31 6 16 13 15 24 4 | 19 24 22 26 45 20 23 22 21 26 20
22E | 5 11 5 7 28 4 13 12 8 14 3 | 23 23 15 23 37 18 20 21 22 22 19
23 | 8 14 6 12 20 5 15 16 10 34 4 | 30 35 33 40 39 31 35 33 32 43 32
24 | 9 11 7 8 30 3 17 14 14 16 4 | 30 32 25 31 41 26 32 30 31 28 27
25E | 14 13 6 11 35 5 10 13 7 11 4 | 119 121 115 114 129 116 117 118 111 116 117
26 | 9 11 7 6 46 5 11 13 9 13 4 | 33 35 39 41 58 35 37 35 33 37 36
X27 | 10 6 5 6 --- 4 12 8 14 10 3 | 44 43 44 43 --- 40 45 44 38 35 42
28 | 9 15 4 8 22 3 12 9 8 13 3 | 28 30 26 29 37 25 26 32 28 25 26
29 | 10 16 8 15 23 4 21 13 12 34 5 | 36 36 31 40 47 33 33 38 35 40 33
X30 | 3 --- --- --- --- 19 --- --- --- --- 0 | 73 --- --- --- --- 66 --- --- --- --- 72
31 | 12 18 6 11 29 6 13 9 14 16 4 | 31 35 24 33 44 25 33 29 30 23 27
32E | 8 11 5 10 20 10 15 19 12 14 4 | 36 35 34 35 42 35 36 37 39 32 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 6 10 29 5 16 13 12 21 |T 36 37 32 37 47 37 36 36 34 36 35
WRMS | 8 14 6 9 24 5 16 11 11 20 |NE 31 33 29 33 43 36 33 32 30 32 29
MEDI | 8 13 6 8 25 5 14 12 12 16 |MD 31 33 26 31 44 28 33 32 31 32 29
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 4.1786 GPS week: 1786 MJD: 56746.0-56752.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2967 |U 5 6 14 |U 8 9 28 |U 6 8 13 |
emr | emr 2860 | 7 7 14 |U 11 16 36 | 8 7 17 |
esa | esa 2866 | 5 5 12 |U 8 9 28 | 6 7 14 |
gfz | gfz 2859 |U 5 5 13 |U 8 10 29 |U 7 7 14 |
grg | grg 2770 |U 8 6 21 |U 12 18 40 |U 9 8 17 |
igr | igr 2866 | 5 5 12 | 7 9 28 | 6 7 13 |
igs | igs 2855 | 5 5 12 | 9 14 32 | 7 7 13 |
jpl | jpl 2860 | 7 6 15 |U 10 15 33 | 8 8 21 |
mit | mit 2866 | 5 5 14 |U 11 18 40 |U 17 16 48 |
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 5.1786.0 GPS week: 1786 Day: 0 MJD: 56746.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 10 | 8 7 26 | 5 6 12 |
emr | emr 2878 | 6 6 13 | 7 6 27 | 7 6 18 |
esa | esa 2880 | 5 4 11 | 7 7 25 | 6 6 14 |
gfz | gfz 2876 | 5 4 11 | 7 8 25 | 6 7 15 |
grg | grg 2784 | 8 6 19 | 9 14 37 | 9 9 22 |
igr | igr 2880 | 5 4 11 | 6 6 25 | 6 5 14 |
igs | igs 2880 | 5 4 11 | 7 6 25 | 6 6 14 |
jpl | jpl 2878 | 6 5 14 | 9 8 33 | 7 5 19 |
mit | mit 2880 | 5 5 11 | 7 7 33 | 6 7 16 |
Table 5.1786.1 GPS week: 1786 Day: 1 MJD: 56747.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 5 5 13 | 8 9 26 | 6 5 14 |
emr | emr 2875 | 6 7 13 | 9 18 31 | 7 7 14 |
esa | esa 2880 | 5 6 14 | 7 7 25 | 5 3 14 |
gfz | gfz 2874 | 5 5 14 | 8 9 25 | 6 5 15 |
grg | grg 2782 | 7 6 21 | 10 18 39 | 8 7 17 |
igr | igr 2879 | 5 6 14 | 7 7 25 | 6 4 13 |
igs | igs 2853 | 5 6 13 | 7 8 24 | 6 4 14 |
jpl | jpl 2875 | 5 8 14 | 10 20 33 | 6 4 16 |
mit | mit 2880 | 5 5 12 | 12 18 34 | 6 5 13 |
Table 5.1786.2 GPS week: 1786 Day: 2 MJD: 56748.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2871 | 4 7 16 | 8 8 33 | 5 8 13 |
emr | emr 2780 | 7 12 21 | 12 21 37 | 9 9 14 |
esa | esa 2784 | 5 7 17 | 8 9 29 | 5 8 12 |
gfz | gfz 2780 | 5 8 19 | 7 8 29 | 6 8 12 |
grg | grg 2688 | 7 6 24 | 11 17 42 | 7 9 16 |
igr | igr 2784 | 5 7 18 | 7 8 29 | 5 7 10 |
igs | igs 2776 | 5 7 17 | 11 17 37 | 5 7 11 |
jpl | jpl 2780 | 7 8 20 | 11 16 35 | 7 7 13 |
mit | mit 2784 | 5 7 17 | 14 17 45 | 6 7 13 |
Table 5.1786.3 GPS week: 1786 Day: 3 MJD: 56749.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 5 11 | 8 9 27 | 7 8 14 |
emr | emr 2876 | 7 6 13 | 10 19 28 | 8 6 17 |
esa | esa 2880 | 5 5 10 | 7 9 25 | 7 9 15 |
gfz | gfz 2872 | 5 7 11 | 8 10 27 | 8 9 14 |
grg | grg 2784 | 8 6 16 | 11 22 38 | 9 8 16 |
igr | igr 2880 | 5 5 10 | 8 9 24 | 8 9 14 |
igs | igs 2878 | 5 6 12 | 9 17 26 | 7 7 13 |
jpl | jpl 2876 | 7 7 15 | 11 15 28 | 7 5 17 |
mit | mit 2880 | 5 6 13 | 9 21 25 | 7 7 14 |
Table 5.1786.4 GPS week: 1786 Day: 4 MJD: 56750.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 4 2 10 | 8 10 29 | 6 7 12 |
emr | emr 2872 | 7 6 13 | 13 15 34 | 8 6 22 |
esa | esa 2880 | 5 3 11 | 7 11 26 | 6 7 16 |
gfz | gfz 2872 | 6 3 12 | 7 11 26 | 6 7 15 |
grg | grg 2784 | 7 3 19 | 14 21 42 | 7 8 15 |
igr | igr 2880 | 6 3 12 | 7 10 28 | 6 6 14 |
igs | igs 2877 | 6 3 12 | 11 14 34 | 6 7 14 |
jpl | jpl 2872 | 7 4 13 | 9 13 30 | 7 7 19 |
mit | mit 2880 | 5 3 11 | 12 17 42 | 5 8 18 |
Table 5.1786.5 GPS week: 1786 Day: 5 MJD: 56751.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2999 | 6 9 19 | 11 15 34 | 8 11 14 |
emr | emr 2872 | 7 6 11 | 13 16 45 | 9 7 18 |
esa | esa 2880 | 4 4 7 | 10 16 37 | 7 7 13 |
gfz | gfz 2873 | 5 4 9 | 12 17 42 | 7 7 15 |
grg | grg 2784 | 7 6 17 | 17 15 43 | 8 7 12 |
igr | igr 2880 | 5 5 8 | 10 15 37 | 7 7 14 |
igs | igs 2850 | 5 5 8 | 11 15 36 | 9 9 13 |
jpl | jpl 2872 | 7 6 12 | 13 15 42 | 15 19 43 |
mit | mit 2880 | 4 4 8 | 13 22 52 | 16 49 58 |
Table 5.1786.6 GPS week: 1786 Day: 6 MJD: 56752.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3009 | 9 8 16 | 7 9 25 | 7 9 14 |
emr | emr 2870 | 8 7 16 | 12 21 52 | 9 6 18 |
esa | esa 2880 | 6 5 14 | 8 8 30 | 7 10 16 |
gfz | gfz 2872 | 7 6 15 | 8 9 29 | 7 9 16 |
grg | grg 2784 | 14 10 32 | 12 22 39 | 13 12 21 |
igr | igr 2880 | 7 5 14 | 7 8 29 | 7 8 14 |
igs | igs 2872 | 6 5 15 | 10 20 41 | 8 9 15 |
jpl | jpl 2872 | 8 7 19 | 10 17 28 | 8 6 19 |
mit | mit 2880 | 7 7 24 | 10 23 46 | 74 27 202 |
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 6.1786 GPS week: 1786 MJD: 56746.500-56752.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -24 1 39 29 -1 | 11 18
| 15 10 50 48 5 | 2
emr uuuuu | 27 14 -116 30 -4 | 25 29
| 15 19 81 59 18 | 1
esa uuuuu | 1 1 -21 86 -4 | 19 25
| 16 12 29 53 4 | 2
gfz uuuuu | -1 -41 135 -128 -5 | 26 29
| 21 12 76 78 7 | 2
grg uuuuu | 41 11 -40 177 10 | 26 31
| 22 17 73 24 8 | 5
igr xxxxx | 6 18 7 -54 -6 | -1 13
| 17 14 30 84 9 | 2
irf xxxxx | 2 -8 4 -36 2 | 4 16
| 12 6 20 32 4 | 3
jpl uuuuu | -16 -17 -107 -69 5 | 22 27
| 44 32 103 36 10 | 2
mit uuuuu | 1 -33 -25 -67 5 | 25 30
| 40 17 56 74 4 | 3
ngs uuuuu | 15 99 32 -69 -2 | 10 15
| 83 66 78 138 7 | 3
sio xxxxx | 11 1 71 -70 9 | 59 61
| 33 22 29 79 6 | 3
Table 7.1786.0 GPS week: 1786 Day: 0 MJD: 56746.500
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 | -34 -1 -33 -63 -5 | 10 16
emr uuuuu | 17 10 -83 -20 4 | 26 30
esa uuuuu | 33 -3 16 122 -6 | 21 25
gfz uuuuu | -19 -54 42 -111 4 | 27 29
grg uuuuu | 37 20 -80 154 -5 | 21 23
igr xxxxx | 34 29 5 73 -14 | 2 12
irf xxxxx | -3 -7 -16 -71 6 | 2 12
jpl uuuuu | -91 -2 85 -60 -5 | 21 25
mit uuuuu | -25 -23 -27 -148 6 | 22 25
ngs uuuuu | 65 76 66 99 5 | 8 14
sio xxxxx | -5 25 93 9 12 | 56 58
Table 7.1786.1 GPS week: 1786 Day: 1 MJD: 56747.500
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 | -30 14 95 51 4 | 6 10
emr uuuuu | 17 34 -136 -62 -34 | 24 27
esa uuuuu | 0 -7 -25 70 2 | 17 21
gfz uuuuu | 39 -43 58 -35 -7 | 24 25
grg uuuuu | 10 38 -155 186 11 | 19 21
igr xxxxx | 6 18 11 -21 -14 | -1 11
irf xxxxx | -7 -8 4 -41 7 | 0 10
jpl uuuuu | -46 -17 -87 -132 -7 | 19 22
mit uuuuu | -14 -12 0 -57 9 | 20 23
ngs uuuuu | 34 15 109 -128 -1 | 6 11
sio xxxxx | -16 8 35 -106 2 | 55 56
Table 7.1786.2 GPS week: 1786 Day: 2 MJD: 56748.500
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 | -29 -18 28 95 6 | 9 14
emr uuuuu | 13 15 -177 117 2 | 23 26
esa uuuuu | 5 26 -61 29 -1 | 20 24
gfz uuuuu | -4 -55 92 -43 1 | 26 27
grg uuuuu | 30 -16 49 212 19 | 23 26
igr xxxxx | 2 8 15 -57 -3 | 0 11
irf xxxxx | -9 -9 19 -27 7 | 3 13
jpl uuuuu | -27 -68 -40 -55 -2 | 21 24
mit uuuuu | -37 -21 59 -67 10 | 23 27
ngs uuuuu | 90 146 5 -313 -13 | 9 13
sio xxxxx | -26 30 85 -73 5 | 57 58
Table 7.1786.3 GPS week: 1786 Day: 3 MJD: 56749.500
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 | -26 0 39 20 -8 | 13 22
emr uuuuu | 33 39 -235 54 2 | 27 32
esa uuuuu | -17 -10 -14 145 -9 | 22 28
gfz uuuuu | -11 -37 180 -220 -8 | 29 33
grg uuuuu | 65 11 44 150 15 | 28 35
igr xxxxx | 1 33 -10 -122 -13 | 2 15
irf xxxxx | -3 -16 36 -82 1 | 7 20
jpl uuuuu | 23 -21 -136 -47 3 | 24 29
mit uuuuu | -29 -27 11 -161 6 | 27 34
ngs uuuuu | 80 103 -10 49 4 | 12 17
sio xxxxx | -9 -26 102 -186 10 | 61 63
Table 7.1786.4 GPS week: 1786 Day: 4 MJD: 56750.500
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 1 66 15 -3 | 11 20
emr uuuuu | 56 -6 -58 56 22 | 24 29
esa uuuuu | -6 -7 2 100 -6 | 19 24
gfz uuuuu | -6 -38 227 -103 -12 | 27 31
grg uuuuu | 32 0 -59 171 6 | 28 36
igr xxxxx | -23 8 -32 -193 -8 | -2 14
irf xxxxx | 0 -14 8 -29 -2 | 5 19
jpl uuuuu | -10 -37 -200 -105 22 | 23 28
mit uuuuu | -3 -58 -49 -85 2 | 26 32
ngs uuuuu | 38 218 -112 -83 -8 | 11 16
sio xxxxx | 32 -20 44 -136 14 | 60 63
Table 7.1786.5 GPS week: 1786 Day: 5 MJD: 56751.500
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 | -11 4 91 52 2 | 12 20
emr uuuuu | 25 19 -136 13 -20 | 26 31
esa uuuuu | -11 2 -59 132 -5 | 18 24
gfz uuuuu | -19 -43 221 -233 -11 | 27 30
grg uuuuu | 37 5 -67 165 9 | 30 37
igr xxxxx | 5 -3 -7 -26 -3 | -2 14
irf xxxxx | 11 -8 -25 -3 -4 | 6 19
jpl uuuuu | 40 37 -178 -59 11 | 24 30
mit uuuuu | 54 -53 -118 8 0 | 27 33
ngs uuuuu | -71 76 107 -122 4 | 11 16
sio xxxxx | 46 -8 44 -26 4 | 62 65
Table 7.1786.6 GPS week: 1786 Day: 6 MJD: 56752.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 4 8 -15 32 1 | 13 20
emr uuuuu | 27 -14 14 56 -2 | 24 30
esa uuuuu | 1 5 -6 7 -1 | 19 24
gfz uuuuu | 13 -19 126 -148 1 | 26 30
grg uuuuu | 74 18 -9 202 18 | 33 38
igr xxxxx | 15 32 65 -30 10 | -3 14
irf xxxxx | 24 3 4 3 1 | 6 18
jpl uuuuu | -4 -12 -192 -27 10 | 25 30
mit uuuuu | 61 -37 -52 40 4 | 28 34
ngs uuuuu | -128 60 59 14 -7 | 12 16
sio xxxxx | 56 -5 95 30 17 | 63 66
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