[IGSREPORT-22574] Wk 1781 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Mar 14 10:53:22 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1781 (Feb 23, 2014 - Mar 01, 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:
igs1781[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1781[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1781[0-6].cls IGS GPS clock combination summary report.
igs17817.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17817.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 | 1 4
0 | EMR | 4 8 9 1 8 9 HERS
0 | ESA | 4 SCOR SCOR SEY1
0 | GFZ | 2 4 NTUS NTUS
0 | GRG | 4 8 9 1 8 9 BRMU CHUR FAA1 HARB LPGS MATE NRMD NTUS
0 | GRG | LPGS NRMD NTUS
0 | JPL | 4 8 9 HYDE
0 | MIT | 2 4 6 8 9 11 31 1 2 4 6 8 9 11 BREW CONZ DAV1 DUBO
0 | MIT | GOPE HLFX MDVJ NTUS TNML DUBO GOPE MDVJ NTUS
1 | ALL | 1
1 | COD | 4 4 8
1 | EMR | 8 9 9 HERS
1 | ESA | 4 4 8
1 | GFZ | 2 2 DARW HOB2 DARW IRKJ
1 | GRG | 8 9 8 9 DARW DRAG GRAZ HOB2 HYDE KELY MAL2 NRMD NYA1
1 | GRG | GRAZ HYDE KELY MAL2 NYA1 POLV
1 | JPL | 2 8 9
1 | MIT | 2 3 4 6 8 9 14 22 23 31 2 3 4 6 8 9 14 22 31 ALIC
1 | MIT | BREW CRO1 DARW DAV1 DRAG GOPE HOB2 HYDE MAC1 MAS1
1 | MIT | MDVJ MOBS NTUS NYAL TIDB TNML TWTF VILL YELL DARW
1 | MIT | DAV1 DRAG GOPE HOB2 HYDE MDVJ NYAL
2 | COD | 1 4 BOGT BOGT
2 | EMR | 4 8 9 8 9 MCM4
2 | ESA | 1 1 4 21 CHUR DARW ARTU CHUR DARW
2 | GFZ | 1 2 4 1 DARW SFER DRAG NRMD SFER
2 | GRG | 4 8 9 8 9 ABMF ARTU BOGT BOR1 BRFT BRMU BRST BRUX
2 | GRG | CHTI CHUR COCO CRO1 FAA1 GRAZ GUUG HARB HOB2 HRAO
2 | GRG | HYDE INVK ISPA KARR KELY KOUC KOUR MAC1 MAL2 MAS1
2 | GRG | MAW1 MCM4 NICO NKLG NRMD NTUS PDEL REUN THTI TOW2
2 | GRG | WTZR ZAMB BOGT GRAZ HYDE ISPA KELY NTUS
2 | JPL | 2 8 9 BOGT KARR
2 | MIT | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
2 | MIT | 21 22 23 24 25 26 27 28 29 31 32 1 2 3 4 5 6 7 8
2 | MIT | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
2 | MIT | 26 27 28 29 31 32
3 | COD | 4 KARR KARR
3 | EMR | 8 6 8 12 31 HERS PRDS
3 | ESA | 1 1 4 PIMO DGAV HYDE PIMO SEY1
3 | GFZ | 1 2 1 REUN GRAZ REUN
3 | GRG | 9 BRAZ GLPS KELY NTUS REUN USNO BRAZ GLPS KELY NTUS
3 | JPL | 2 7 8 9 17 29 31 CAS1
3 | MIT | 1 2 4 6 8 14 17 19 20 21 22 23 1 2 4 6 8 11 14 17
3 | MIT | 19 20 21 22 23 28 BAKO CONZ USNO
4 | ALL | 1
4 | COD | 4 1 4 TRO1 TRO1
4 | EMR | HERS
4 | ESA | 4 1 4
4 | GFZ | 2 1 TSKB
4 | GRG | 28 28 ABMF ALIC BOGT BRMU DARW GUAT HOFN HYDE KOUR
4 | GRG | MAL2 MCM4 MONP NOVM NRMD SYOG TRO1 ALIC BOGT MAL2
4 | GRG | NRMD
4 | JPL | SCOR
4 | MIT | 2 3 4 5 6 7 9 10 11 12 13 14 15 16 17 18 19 20 21
4 | MIT | 22 23 24 25 26 27 28 29 31 32 1 2 3 4 5 6 7 9 10
4 | MIT | 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27
4 | MIT | 28 29 31 32 MAW1 MAW1
5 | ALL | 1
5 | COD | 4
5 | EMR | 8 8
5 | ESA | 1 4 ARTU SEY1 UNSA
5 | GFZ | 2 1
5 | GRG | 8 8 ARTU BRST CONZ DARW GOPE KELY MAL2 MAS1 MOBS
5 | GRG | NRIL NTUS POLV REYK TLSE TNML TWTF ZECK MOBS NTUS
5 | JPL | 8 21
5 | MIT | 2 4 6 8 11 1 2 4 6 8 MAC1 MDVJ USNO MAC1 USNO
6 | ALL | 1
6 | COD | 4 6
6 | EMR | 4 8 8 HERS MCM4 MCM4 YELL
6 | ESA | 1 4 SEY1
6 | GFZ | 2 4 1 CHUR
6 | GRG | 4 8 8 ABMF ARTU BOGT BRAZ BRFT BRMU BRST BRUX CHTI
6 | GRG | COCO DAEJ DARW DRAG GRAZ GUUG HOFN HYDE KARR KOUC
6 | GRG | MAC1 MAL2 MAW1 MCM4 NICO NTUS PDEL REUN SSIA TNML
6 | GRG | TOW2 TWTF WTZR ZAMB GRAZ MAL2
6 | JPL | 4 8 9
6 | MIT | 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
6 | MIT | 21 22 23 24 25 26 27 28 29 31 32 1 2 3 4 5 6 7 8
6 | MIT | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
6 | MIT | 26 27 28 29 31 32
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
----+------------+----------
G08 | 2014_02_27 | 2014020
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G09 | 4 | | | | | | |
PRN G30 | | | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -2.2 -.2 -2.0 -39 3 -14 .67
EMR | 0 | -4.1 -1.7 1.9 49 46 -40 .76
ESA | 0 | 7.3 2.3 1.2 -1 -25 62 .32
GFZ | 0 | -.5 -.3 -2.2 -52 -31 -18 .56
GRG | 0 | -.4 6.8 -4.3 -2 -29 29 .85
JPL | 0 | -4.1 -6.5 15.3 -59 45 27 .34
MIT | 0 | 3.8 1.3 8.9 7 0 -30 .57
NGS | 0 | -1.6 6.1 14.8 -12 -28 15 .67
SIO | 0 | -1.6 2.9 4.6 14 -42 31 .66
COD | 1 | -2.2 -.6 -1.9 -55 -5 7 .60
EMR | 1 | 3.6 -1.5 5.4 49 29 -20 .62
ESA | 1 | 6.2 5.5 -1.6 6 -9 84 .25
GFZ | 1 | -.4 -.1 -1.7 -49 -16 -31 .56
GRG | 1 | 4.5 3.8 -2.3 -19 -25 27 .79
JPL | 1 | 6.1 -1.7 11.2 -54 -22 -19 .62
MIT | 1 | 3.5 1.4 13.8 -23 4 -27 .33
NGS | 1 | -3.4 1.7 16.3 -48 -4 -17 .58
SIO | 1 | 1.5 2.7 9.8 1 -44 29 .60
COD | 2 | -1.9 -.5 -1.3 -36 6 -14 .57
EMR | 2 | 3.7 4.8 8.6 46 23 -33 .78
ESA | 2 | 3.9 4.4 5.7 -2 -56 79 .26
GFZ | 2 | .0 -.3 -.6 -55 -23 -20 .15
GRG | 2 | 8.2 2.6 3.4 -30 -34 16 .67
JPL | 2 | -2.0 3.0 22.7 62 -103 1 -.60
MIT | 2 | 3.4 3.7 9.4 -5 -3 -12 .27
NGS | 2 | 2.8 5.6 23.6 -35 -70 28 .61
SIO | 2 | 4.1 5.8 23.1 -25 -39 22 .30
COD | 3 | -1.0 -.7 -2.1 -26 -3 -24 .82
EMR | 3 | 5.9 1.3 7.9 12 13 -46 .80
ESA | 3 | 6.1 6.4 6.0 3 -76 81 .33
GFZ | 3 | -.4 .0 -1.6 -44 -12 -31 .31
GRG | 3 | 2.7 -3.0 1.6 -34 -29 24 1.24
JPL | 3 | 5.2 -7.4 27.6 134 0 52 -.32
MIT | 3 | 1.0 4.6 8.2 -1 -13 -2 .83
NGS | 3 | -6.4 4.2 17.9 -50 0 -26 .91
SIO | 3 | 4.6 5.2 14.0 7 -48 16 .86
COD | 4 | -1.8 -.8 -2.8 -43 7 13 .79
EMR | 4 | 5.1 6.8 2.1 4 22 -55 .70
ESA | 4 | 7.8 -.6 1.6 -7 -36 75 .31
GFZ | 4 | -.2 .0 -1.8 -47 -39 -14 .37
GRG | 4 | 15.1 -.3 -6.9 1 -15 40 1.01
JPL | 4 | -3.3 3.8 14.2 -43 -13 4 .82
MIT | 4 | .3 2.6 8.7 -6 5 0 .48
NGS | 4 | 4.7 -.3 21.2 -70 -81 16 .97
SIO | 4 | 6.4 6.2 11.9 14 -67 34 .46
COD | 5 | -.3 .3 -1.8 -22 -7 -8 .77
EMR | 5 | 4.1 -2.4 7.5 15 13 -47 .84
ESA | 5 | 5.9 -1.2 -.9 4 -4 69 .24
GFZ | 5 | -.5 -.3 -1.9 -49 -11 -22 .62
GRG | 5 | 1.3 6.7 -13.2 -7 -38 14 1.32
JPL | 5 | 8.1 -1.1 18.4 7 -4 28 .86
MIT | 5 | 1.1 1.2 7.0 -5 -23 -14 .67
NGS | 5 | -3.4 -1.2 8.5 -39 5 -22 .97
SIO | 5 | 3.7 4.9 26.1 11 -66 -19 .85
COD | 6 | -.7 .5 -1.6 -21 10 1 .80
EMR | 6 | 6.8 -2.7 7.2 10 24 -47 .77
ESA | 6 | .7 -3.4 2.5 -8 -3 38 .15
GFZ | 6 | .2 -.2 -1.1 -37 -36 -1 .25
GRG | 6 | -.9 -2.2 -2.3 -1 -28 18 1.10
JPL | 6 | -.8 -2.0 21.2 64 -56 71 .30
MIT | 6 | 3.0 -.4 6.6 8 -6 -12 .59
NGS | 6 | -1.6 -6.7 16.1 -100 -20 -43 .80
SIO | 6 | 2.2 5.6 22.3 39 -22 74 .69
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1781.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1781.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 2.1781.[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 3.1781.[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 5.1781.0-6). 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 1781 summary. (Feb 23, 2014 - Mar 01, 2014)
Table 1.1781.a GPS week: 1781 MJD: 56711.000-56717.000
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 1 3 21 39 3 .09 11 10 | -990 16 21 125
| 0 1 1 13 35 11 .03 | 259 534
emr 79| 0 -1 3 -10 20 5 .09 18 18 | 3206 123 21 114
| 2 1 1 20 27 15 .03 | 828 612
esa 150| 1 0 0 16 -44 16 -.23 7 6 | -653 423 10 106
| 0 0 1 18 76 22 .01 | 1354 1890
gfz 191| 0 0 -6 43 1 -34 .17 11 10 | -293 -6 14 115
| 0 1 1 15 31 19 .01 | 388 534
grg 183| 1 0 1 -36 -9 -32 .35 15 14 | -91 10 19 165
| 1 0 2 18 51 11 .04 | 202 305
igr n/a| 0 0 -1 -30 29 -10 -.18 5 5 | 7488 671 16 95
| 0 0 1 23 23 16 .04 | 2101 650
jpl 80| 0 0 -1 20 -7 -23 .04 18 17 | 1732 228 21 141
| 1 2 1 35 49 35 .03 | 1339 736
mit 295| 0 0 -2 -9 18 16 -.18 12 10 | -176 91 75 274
| 1 1 0 24 36 19 .05 | 236 435
ngs 228| -1 1 3 -83 46 1 .06 14 12 | -926 -87 1737 3288
| 1 1 2 33 64 30 .05 | 249 530
sio 470| 0 -1 -2 0 -16 15 -.61 20 20 | --- --- --- ---
| 0 1 2 24 25 19 .12 | --- ---
Table 1.1781.b GPS week : 1781 MJD: 56711.000-56717.000
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 | 6 5 5 4 5 4 6 |
2 | 5 5 5 5 5 5 5 |
3 | 4 4 3 4 4 4 4 |
4 | 8 6 6 6 6 6 5 |
5 | 5 5 5 5 5 5 5 |
6 | 5 5 5 5 5 5 5 |
7 | 5 5 5 5 5 6 4 |
8 | 8 7 6 5 0 5 5 |
9 | 6 6 5 5 5 5 5 |
10 | 4 4 4 4 5 5 5 |
11 | 4 4 4 4 5 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 5 4 4 5 4 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 6 5 6 5 5 6 6 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 4 5 4 4 5 |
20 | 5 5 5 5 5 5 5 |
21 | 4 4 6 4 4 5 4 |
22 | 5 5 4 5 4 5 4 |
23 | 4 4 4 4 4 4 4 |
24 | 5 4 5 4 5 4 4 |
25 | 4 4 4 4 5 4 4 |
26 | 4 4 3 3 4 5 4 |
27 | 4 4 4 4 5 5 4 |
28 | 6 6 5 5 5 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | --- --- 0 0 0 0 0 |
31 | 5 5 5 5 4 5 4 |
32 | 4 4 4 4 4 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 2.1781.0 GPS week: 1781 Day: 0 MJD: 56711.000
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 4 37 31 7 .10 11 11 | -1407 764 20 127
emr 80| -4 -1 1 0 14 -7 .14 19 19 | 3158 -425 16 106
esa 150| 1 0 -1 10 -9 7 -.24 7 6 | -1343 2097 9 105
gfz 191| 0 -1 -6 77 18 -25 .16 11 11 | 80 -683 12 116
grg 185| 1 0 3 -12 -74 -35 .35 14 13 | -452 484 17 144
igr n/a| 0 0 -2 -35 26 3 -.22 5 5 | 5609 119 16 87
jpl 80| -1 0 1 9 16 11 .04 17 17 | 1181 -440 19 153
mit 300| 1 -2 -1 -5 5 -2 -.20 16 12 | -293 491 27 224
ngs 225| -1 2 1 -151 3 33 .02 13 11 | -1282 639 1719 3770
sio 459| 0 -4 -2 8 -20 17 -.49 21 18 | --- --- --- ---
Table 2.1781.1 GPS week: 1781 Day: 1 MJD: 56712.000
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 5 2 28 1 .14 11 10 | -1007 -69 19 119
emr 80| -1 -1 2 -13 24 15 .07 18 18 | 2396 -315 17 111
esa 150| 2 -1 0 10 0 20 -.23 7 7 | 986 -1792 12 113
gfz 193| 0 -1 -6 36 2 -47 .17 11 11 | -573 865 13 73
grg 186| 4 0 -1 -25 -49 -16 .35 13 13 | -40 -70 16 140
igr n/a| -1 0 -1 -14 34 -10 -.18 5 5 | 5370 127 16 89
jpl 80| -1 0 -2 0 39 12 .09 17 16 | 420 -420 17 118
mit 295| 0 0 -2 8 -5 7 -.21 13 10 | -163 -13 31 219
ngs 233| -2 0 3 -45 -25 -21 .00 13 12 | -861 -384 1620 3128
sio 472| 0 -2 -4 23 -47 14 -.41 20 19 | --- --- --- ---
Table 2.1781.2 GPS week: 1781 Day: 2 MJD: 56713.000
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| 1 0 0 11 19 4 .12 11 10 | -839 -428 21 132
emr 79| 0 0 2 1 11 -8 .11 19 19 | 1942 1063 20 109
esa 150| 0 -1 0 33 -69 12 -.22 8 7 | -1217 2453 8 98
gfz 192| -1 -1 -6 41 -1 -54 .19 12 11 | 18 1 17 122
grg 182| 3 0 0 -46 4 -51 .33 15 14 | -129 269 19 162
igr n/a| 0 0 -2 -7 15 1 -.14 5 5 | 5623 1449 19 95
jpl 80| 1 -2 -2 -1 -12 -2 .02 17 16 | 142 1050 21 152
mit 298| 0 0 -2 -14 50 39 -.25 12 10 | -353 368 99 190
ngs 226| 0 1 6 -67 72 6 .06 13 11 | -810 -443 1680 3332
sio 471| 0 0 -4 -30 3 30 -.71 20 20 | --- --- --- ---
Table 2.1781.3 GPS week: 1781 Day: 3 MJD: 56714.000
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 1 22 16 4 .06 10 10 | -656 -786 24 127
emr 80| 2 -3 3 1 7 18 .10 18 18 | 3039 859 45 131
esa 150| 2 -1 0 13 -58 19 -.24 7 7 | -1022 1175 16 110
gfz 191| 0 0 -7 31 -33 -33 .17 10 10 | -89 -375 18 117
grg 184| 2 0 4 -59 32 -31 .31 15 14 | 72 144 30 183
igr n/a| 0 0 -2 -19 40 -10 -.13 5 5 | 7005 1506 19 123
jpl 80| -1 0 -1 3 -51 -79 .06 19 19 | 1138 1129 33 122
mit 294| -1 0 -2 21 48 45 -.21 11 10 | -472 183 36 228
ngs 227| -2 2 1 -78 96 -11 .05 13 11 | -615 -840 1722 3301
sio 475| 0 -1 -3 21 -6 3 -.73 21 20 | --- --- --- ---
Table 2.1781.4 GPS week: 1781 Day: 4 MJD: 56715.000
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| 0 2 1 26 119 -19 .05 11 11 | -1230 372 21 117
emr 80| 1 0 2 -53 77 -10 .07 18 18 | 3890 65 23 127
esa 150| 1 0 1 39 -200 62 -.22 6 6 | -1004 1063 9 102
gfz 189| 0 0 -5 38 53 -55 .18 10 10 | -982 138 12 126
grg 182| 1 0 0 -40 77 -32 .40 16 15 | -106 -294 18 188
igr n/a| 0 0 0 -80 69 -44 -.18 5 5 | 8705 1020 16 87
jpl 80| 0 -2 -2 -10 61 -38 .07 18 18 | 2587 595 22 141
mit 292| -1 0 -1 -25 66 0 -.15 11 10 | -219 456 119 421
ngs 231| 0 0 3 -87 101 -43 .10 18 17 | -1240 390 1493 3305
sio 471| 1 0 -5 12 12 5 -.68 20 20 | --- --- --- ---
Table 2.1781.5 GPS week: 1781 Day: 5 MJD: 56716.000
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 3 2 38 31 5 .06 11 11 | -999 408 23 132
emr 80| 0 -1 5 -16 -8 6 .06 18 18 | 3819 62 18 115
esa 150| 1 0 0 25 0 -8 -.23 7 7 | -2388 483 10 108
gfz 192| 0 0 -4 42 -38 -21 .17 11 10 | -65 -406 12 121
grg 184| 0 -1 0 -55 -34 -37 .40 16 15 | 188 -363 17 196
igr n/a| 0 0 0 -25 -5 -13 -.17 6 6 | 9807 498 15 86
jpl 80| -3 -3 -1 74 -28 -9 .00 19 19 | 3244 324 18 141
mit 291| 0 -2 -1 -52 -29 23 -.12 11 11 | 56 -87 27 266
ngs 229| 0 0 0 -88 112 42 .06 14 13 | -933 269 1795 2997
sio 471| 0 0 2 -37 -53 -11 -.60 20 19 | --- --- --- ---
Table 2.1781.6 GPS week: 1781 Day: 6 MJD: 56717.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 0 0 4 11 26 19 .09 10 10 | -794 -149 20 122
emr 80| 2 0 4 6 14 27 .08 18 18 | 4200 -448 14 105
esa 150| 0 0 0 -16 26 0 -.24 6 6 | 1411 -2515 9 107
gfz 190| 0 1 -4 32 6 -2 .19 11 10 | -441 418 16 132
grg 182| 0 -1 0 -17 -21 -23 .32 17 15 | -174 -97 17 143
igr n/a| 0 0 0 -32 23 2 -.22 5 5 | 10299 -22 17 102
jpl 80| 0 3 -2 69 -75 -56 .03 17 17 | 3417 -640 20 162
mit 296| 0 -1 -2 3 -9 0 -.14 11 10 | 209 -757 187 376
ngs 229| -1 0 4 -66 -36 7 .14 14 12 | -743 -246 2134 3189
sio 474| 1 0 0 6 -1 48 -.62 21 21 | --- --- --- ---
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 3.1781.0 GPS week: 1781 Day: 0 MJD: 56711.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 8 12 6 23 20 10 --- 9 15 19 5 | 33 33 32 36 32 30 --- 29 33 28 30
2E | 11 17 6 12 19 6 19 12 9 33 4 | 25 25 23 25 23 23 24 29 29 35 23
3 | 8 15 5 9 16 6 12 7 14 18 4 | 29 31 27 33 36 27 29 28 27 30 28
4E | 14 31 9 10 18 7 22 43 20 21 8 | 39 52 41 38 46 43 42 31 48 39 39
5 | 13 19 7 15 11 7 18 10 9 21 4 | 49 51 40 40 43 40 50 43 46 49 43
6 | 14 12 5 9 11 6 13 12 19 --- 4 | 28 29 29 29 17 26 22 29 30 --- 27
7E | 11 17 5 8 15 5 19 11 13 14 4 | 37 31 25 33 30 27 32 28 31 26 28
8E | 16 20 15 10 18 8 22 39 17 18 7 | 55 59 45 48 35 50 58 57 56 45 50
9E | 15 23 9 17 15 6 18 14 11 23 5 | 156 154 152 159 153 150 153 158 145 153 153
10 | 11 13 7 8 15 4 11 7 9 15 3 | 22 19 21 26 25 18 18 17 18 25 19
11E | 11 11 7 9 13 6 13 15 14 13 4 | 49 48 46 44 47 44 46 45 45 41 45
12 | 8 20 6 11 16 4 20 14 14 22 5 | 30 31 25 33 35 26 31 23 31 27 27
13 | 8 17 3 8 10 4 16 12 11 21 3 | 38 43 38 44 45 38 42 39 37 41 39
14 | 19 18 8 9 12 5 15 11 13 17 4 | 34 37 42 49 42 40 36 41 33 37 38
15 | 11 20 6 12 13 5 18 15 11 28 4 | 25 28 27 39 37 28 29 28 28 31 27
16 | 11 21 6 13 14 4 21 12 15 24 5 | 23 31 20 26 28 21 28 20 30 22 22
17 | 12 24 11 14 13 5 18 16 14 23 5 | 33 37 40 45 41 36 35 39 42 35 37
18 | 9 21 6 14 13 4 19 9 12 22 4 | 27 26 21 38 29 23 27 22 25 19 23
19 | 7 19 7 10 14 5 20 12 17 20 5 | 36 37 36 39 43 34 33 35 32 27 34
20 | 9 20 7 10 11 5 19 13 13 26 4 | 25 27 23 30 24 23 25 23 25 30 21
21E | 11 13 7 9 13 3 15 15 8 18 4 | 32 27 26 32 28 26 28 28 29 24 27
22 | 9 19 7 10 11 4 21 10 12 23 4 | 29 27 27 37 33 30 25 29 29 30 27
23 | 7 16 5 8 9 4 14 8 14 23 3 | 32 32 33 42 34 33 31 30 33 30 32
24E | 12 19 5 10 19 5 16 15 10 10 4 | 77 80 77 82 91 80 83 76 80 80 79
25 | 10 14 6 11 14 4 17 13 9 12 4 | 24 28 22 29 29 22 33 21 25 22 23
26 | 10 14 5 10 10 6 11 13 9 18 3 | 30 26 30 38 32 28 29 30 28 26 29
X27 | 8 12 7 9 --- 5 13 9 14 17 4 | 22 27 24 22 --- 21 29 23 23 25 22
28 | 11 23 6 7 17 4 18 27 15 14 5 | 33 37 30 36 38 30 36 35 31 31 31
29 | 14 18 6 17 13 5 20 13 8 30 5 | 26 26 19 28 27 21 23 23 26 26 21
31E | 11 18 7 9 13 5 20 9 12 12 4 | 36 34 31 36 35 31 33 30 41 31 32
32 | 6 11 4 8 9 4 10 10 14 12 3 | 27 25 23 30 29 25 27 26 28 21 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 7 11 14 5 17 16 13 21 |T 37 38 35 40 39 35 37 35 37 36 35
WRMS | 11 19 6 11 13 5 17 12 11 18 |NE 28 30 26 33 32 26 29 27 28 28 27
MEDI | 11 18 6 10 13 5 18 12 13 19 |MD 32 31 29 36 34 28 31 29 31 30 28
Table 3.1781.1 GPS week: 1781 Day: 1 MJD: 56712.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 7 12 7 16 18 6 --- 10 10 16 4 | 33 36 33 35 35 31 --- 33 31 32 33
2E | 8 17 6 11 13 3 20 13 12 22 4 | 18 16 13 20 10 13 17 16 19 23 13
3 | 6 11 6 8 15 4 10 6 16 18 3 | 29 30 27 32 30 28 30 27 29 31 28
4E | 16 25 9 9 14 8 18 15 18 16 5 | 31 36 27 29 28 27 29 30 34 29 27
5 | 14 21 5 14 12 7 18 14 13 17 5 | 32 34 24 26 30 23 32 25 30 28 26
X6 | 8 14 5 13 --- 6 13 9 17 --- 4 | 23 24 18 27 --- 22 20 21 30 --- 21
7E | 7 18 10 8 13 4 18 11 14 14 4 | 34 31 29 34 33 28 32 31 35 25 30
8E | 18 19 13 11 16 8 21 33 17 18 7 | 52 51 41 46 31 46 54 56 51 45 47
9E | 14 22 10 16 16 7 20 10 11 23 5 | 148 149 145 146 146 144 146 145 145 147 146
10 | 8 14 6 9 12 5 11 11 11 13 3 | 22 18 19 25 23 16 19 20 18 21 18
11E | 15 11 6 9 15 4 12 10 8 18 4 | 40 41 39 38 47 38 42 39 42 32 40
12 | 7 22 5 11 14 3 19 9 13 23 4 | 24 25 18 27 29 18 25 18 24 19 20
13 | 9 16 5 10 13 3 15 12 13 18 4 | 28 34 23 32 34 24 34 27 25 27 26
14 | 15 18 4 11 14 5 14 9 10 18 4 | 37 32 29 36 32 30 31 28 27 29 30
15 | 12 21 5 7 11 5 17 15 15 26 4 | 23 24 19 27 28 20 26 19 21 20 19
16 | 12 18 6 15 14 4 21 10 11 27 4 | 23 25 17 25 25 20 26 15 21 17 19
17 | 9 16 9 17 12 4 18 17 15 19 5 | 26 28 25 33 32 24 27 26 27 20 25
18 | 11 21 6 16 13 4 21 10 15 26 5 | 27 24 20 36 28 23 27 23 20 20 22
19 | 9 18 8 10 10 4 20 9 13 25 4 | 29 30 24 29 29 24 28 24 20 21 24
20 | 8 19 7 12 13 2 20 14 9 27 4 | 22 25 19 26 24 19 27 25 20 32 19
21E | 10 12 5 10 14 4 15 7 12 16 4 | 19 17 17 20 19 16 17 14 14 17 14
22 | 10 16 7 13 12 5 19 13 14 18 4 | 26 26 23 30 28 24 27 27 18 23 23
23 | 7 15 5 14 11 4 15 7 16 24 4 | 23 25 19 30 22 19 26 21 22 22 20
24E | 8 18 8 10 13 5 15 8 9 11 4 | 42 42 40 40 45 39 45 41 43 40 40
25 | 11 15 5 8 10 6 16 10 14 11 4 | 20 27 17 22 25 17 31 16 24 16 19
26 | 8 15 6 9 11 6 10 8 11 26 3 | 23 17 20 26 23 18 21 17 19 30 19
X27 | 8 12 8 10 --- 3 11 8 13 17 4 | 22 25 20 22 --- 19 29 18 20 16 20
28 | 12 25 9 12 14 5 16 22 12 17 5 | 33 39 30 32 35 29 35 29 33 30 29
29 | 5 17 7 13 13 3 19 10 13 28 4 | 22 24 18 26 24 17 25 19 22 21 19
31E | 9 19 7 9 17 5 19 7 13 8 4 | 27 27 21 25 34 24 26 22 26 22 23
32 | 6 9 6 9 16 5 10 11 13 18 3 | 22 20 17 22 27 18 22 22 20 27 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 7 11 13 5 17 13 13 20 |T 31 32 27 33 32 27 32 28 30 29 28
WRMS | 10 18 7 11 13 5 16 10 12 19 |NE 25 26 21 27 27 21 26 21 23 22 22
MEDI | 9 17 6 11 13 5 17 10 13 18 |MD 26 27 21 29 29 23 27 24 24 23 23
Table 3.1781.2 GPS week: 1781 Day: 2 MJD: 56713.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 9 13 7 17 16 6 --- 9 9 17 4 | 24 33 29 31 26 28 --- 23 28 24 26
2E | 13 16 7 12 14 5 15 15 12 14 4 | 24 24 24 22 20 22 22 25 22 21 21
3 | 7 12 4 7 13 6 11 7 12 22 3 | 27 24 24 31 27 25 25 22 32 26 25
4E | 14 27 9 10 14 7 18 16 24 14 6 | 23 34 25 22 23 22 26 22 28 23 21
5 | 14 19 7 12 11 5 17 11 10 15 4 | 39 42 36 35 38 33 41 34 41 35 36
X6 | 11 11 9 11 --- 9 10 9 17 --- 4 | 28 25 29 32 --- 25 20 22 33 --- 26
7E | 10 20 7 7 14 5 18 11 11 11 4 | 38 35 31 36 36 31 33 33 30 28 32
8E | 13 19 11 12 16 8 17 19 11 --- 5 | 56 50 45 52 38 48 53 53 48 --- 50
9E | 12 24 12 15 14 9 20 8 9 33 5 | 114 116 112 109 112 113 116 111 110 118 111
10 | 8 19 8 10 11 4 13 14 8 17 4 | 27 21 28 32 24 25 19 27 25 24 25
11 | 7 12 7 6 20 6 13 14 11 11 4 | 43 46 44 42 47 41 44 38 43 36 41
12 | 8 23 7 13 17 5 19 12 15 27 5 | 31 31 26 33 33 25 28 25 25 31 26
13 | 10 17 6 13 16 4 16 9 12 23 4 | 35 39 34 42 39 34 37 34 33 38 34
14 | 18 17 5 11 14 6 13 11 13 19 4 | 34 31 29 40 34 33 31 32 29 26 31
15 | 9 22 5 13 11 6 17 9 15 23 4 | 28 27 25 34 30 24 25 24 20 22 24
16 | 16 17 6 13 14 4 20 9 11 21 5 | 25 26 19 30 25 18 27 17 17 17 19
17 | 7 19 9 18 9 4 20 19 14 23 5 | 33 34 35 40 36 30 32 32 30 24 32
18 | 11 20 5 19 16 5 18 10 14 20 5 | 25 29 22 41 28 24 29 26 24 19 25
19 | 8 16 7 10 12 5 20 9 11 21 4 | 33 31 32 41 35 31 31 29 35 24 31
20 | 10 19 6 10 13 3 16 14 9 24 4 | 26 31 24 28 25 24 26 24 21 29 23
21E | 9 17 15 10 26 6 17 12 18 20 6 | 23 24 27 28 33 24 28 23 32 27 24
22 | 7 19 7 10 13 3 17 9 14 18 4 | 23 26 23 31 30 23 26 24 16 21 23
23 | 11 16 6 12 13 3 15 10 13 20 4 | 30 31 31 38 30 28 29 29 28 27 29
24E | 13 19 7 9 23 5 14 8 15 17 5 | 70 73 71 74 77 68 70 67 70 67 70
25 | 9 20 5 9 12 7 14 9 12 15 4 | 27 31 26 31 29 24 32 23 19 22 25
26 | 6 12 8 9 11 5 9 5 11 17 3 | 30 25 29 31 28 25 25 26 22 25 27
X27 | 10 12 8 12 --- 7 13 9 10 17 4 | 29 28 28 29 --- 24 29 21 27 18 25
28 | 11 19 6 11 14 4 19 13 10 20 4 | 30 39 32 35 41 30 35 29 31 30 32
29 | 9 19 7 16 16 5 22 10 9 34 5 | 26 25 24 33 27 22 27 21 20 30 23
X30E | 2 --- --- --- --- 175 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
31E | 9 22 8 9 16 5 17 8 13 8 4 | 29 33 27 31 34 25 29 24 29 23 26
32 | 9 13 7 10 15 5 9 9 9 13 3 | 21 25 21 22 22 20 19 18 17 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 8 12 15 5 17 12 13 20 |T 33 35 32 37 35 31 33 30 31 30 31
WRMS | 10 19 7 11 14 5 16 10 11 20 |NE 28 28 26 33 30 25 27 24 25 24 26
MEDI | 9 19 7 11 14 5 17 10 12 19 |MD 29 31 28 33 30 25 29 25 28 25 26
Table 3.1781.3 GPS week: 1781 Day: 3 MJD: 56714.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 6 15 5 13 14 7 --- 11 13 15 4 | 32 38 32 35 33 34 --- 33 33 33 33
2E | 15 19 8 10 21 5 20 11 11 13 5 | 27 25 20 21 25 19 27 24 20 20 22
3 | 9 10 5 7 20 3 12 5 12 23 3 | 30 30 30 32 38 27 32 29 33 30 30
4E | 11 22 10 8 13 7 21 21 16 16 5 | 21 30 25 26 23 21 25 25 25 24 22
5 | 14 22 6 9 11 6 20 10 9 17 4 | 37 43 33 30 35 31 43 30 31 34 33
X6 | 11 10 7 10 --- 5 17 7 16 --- 4 | 27 26 26 26 --- 19 21 23 27 --- 24
7E | 8 20 7 10 20 6 23 12 10 15 5 | 24 23 17 26 31 18 29 23 19 16 21
X8E | 14 19 10 8 --- 10 21 11 10 20 5 | 51 58 46 48 --- 45 62 47 48 49 48
9E | 9 22 11 10 16 8 25 8 11 29 5 | 145 142 137 143 138 134 144 141 138 138 140
10 | 8 16 7 9 15 4 14 11 12 19 4 | 23 20 22 28 22 20 29 24 22 25 22
11 | 10 14 7 8 19 5 16 9 10 14 4 | 36 37 36 34 43 32 42 32 34 32 34
12 | 8 22 7 13 17 5 20 13 14 23 5 | 30 30 23 31 31 24 34 24 26 27 25
13 | 8 17 8 10 12 5 21 10 9 24 4 | 29 36 28 36 35 29 38 34 29 36 30
14 | 8 16 7 12 17 6 14 11 17 17 4 | 37 37 39 46 37 38 38 39 37 34 38
15 | 11 22 6 10 10 5 25 9 12 28 4 | 30 29 28 37 34 31 33 28 30 25 29
16 | 15 18 7 12 16 4 22 8 16 23 5 | 30 28 22 30 31 23 28 23 31 22 26
17 | 9 21 8 18 13 5 23 13 14 27 5 | 29 36 33 37 39 29 36 30 31 30 32
18 | 9 22 5 13 15 6 22 10 9 19 4 | 25 29 24 38 31 25 34 26 24 23 26
19 | 8 20 8 10 15 3 19 8 14 23 4 | 33 35 32 36 42 31 34 33 33 27 33
20 | 11 18 7 12 12 3 17 15 17 19 5 | 18 25 20 28 24 19 24 25 24 24 19
21E | 8 16 7 13 10 5 12 8 14 17 4 | 26 23 24 29 25 22 26 22 21 27 24
22 | 8 17 6 9 14 5 23 10 11 17 4 | 26 28 25 30 33 28 31 28 24 29 26
23 | 10 17 8 10 11 4 18 9 11 23 4 | 25 30 25 33 28 24 32 27 24 25 25
24 | 6 15 8 9 15 9 15 9 17 14 4 | 128 129 128 131 132 128 127 127 127 129 128
25 | 8 16 5 10 14 4 15 13 9 13 4 | 23 29 23 29 27 22 37 23 22 23 24
26 | 6 13 5 8 9 7 12 5 12 22 3 | 26 24 27 36 28 27 29 27 25 27 27
X27 | 10 10 7 9 --- 4 17 10 9 14 4 | 26 27 22 27 --- 21 33 23 24 17 24
28 | 10 18 6 8 13 5 21 14 15 19 4 | 30 36 27 33 37 27 37 32 30 27 29
29 | 10 19 7 11 14 5 22 10 9 37 4 | 27 29 23 29 28 21 34 23 24 35 24
X30E | 2 --- --- --- --- 106 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
31E | 8 22 7 8 18 4 19 8 16 10 4 | 29 28 25 29 29 23 30 23 30 20 25
32 | 9 11 5 10 12 4 12 8 10 12 3 | 19 23 19 25 22 19 25 20 21 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 7 10 15 5 19 11 13 21 |T 35 37 33 38 38 32 39 34 34 34 34
WRMS | 10 18 7 10 14 5 19 10 11 20 |NE 28 29 26 32 31 25 32 26 27 27 27
MEDI | 9 18 7 10 14 5 19 10 12 19 |MD 29 29 25 31 31 25 33 27 27 27 26
Table 3.1781.4 GPS week: 1781 Day: 4 MJD: 56715.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 11 14 7 9 15 4 --- 8 21 17 4 | 34 36 35 28 34 32 --- 33 34 33 32
2E | 14 19 6 10 22 5 20 12 15 11 5 | 21 23 19 22 25 19 22 21 21 20 21
3 | 11 11 5 10 21 5 14 6 20 24 4 | 23 29 22 30 29 23 26 22 31 29 25
4E | 12 18 7 10 13 6 17 21 24 15 5 | 31 28 29 24 30 27 28 35 32 31 28
5 | 14 22 7 9 13 4 20 11 17 10 5 | 29 38 28 28 33 26 37 25 31 28 29
X6 | 11 12 6 11 --- 4 --- 8 18 --- 4 | 22 25 21 24 --- 19 --- 19 27 --- 20
7E | 12 20 6 9 21 5 20 12 20 15 5 | 46 50 43 49 56 44 48 44 53 45 47
X8E | 7 --- --- --- --- 32 --- --- --- --- 0 | 34 --- --- --- --- 36 --- --- --- --- 35
9 | 10 17 8 12 15 8 21 7 12 23 4 | 86 86 85 91 84 84 87 85 84 92 85
10 | 15 17 6 9 16 3 14 10 16 20 4 | 25 20 23 26 30 21 22 25 19 28 23
11 | 8 17 8 9 15 5 17 11 20 15 4 | 33 41 34 33 36 31 35 31 32 28 31
12 | 11 17 5 10 15 3 21 16 16 22 5 | 26 28 23 28 31 23 29 26 26 24 24
13 | 7 17 6 8 13 4 18 11 17 24 4 | 31 37 30 33 39 28 44 31 30 35 32
14 | 17 13 5 6 19 5 15 8 20 21 4 | 30 32 29 34 34 30 30 31 25 25 30
15 | 12 22 6 9 11 3 22 10 19 28 4 | 26 28 27 31 30 25 30 26 23 27 26
16 | 14 16 5 13 16 4 21 8 23 23 5 | 20 25 18 24 26 20 26 19 25 17 20
17 | 12 22 9 16 15 5 17 11 19 23 5 | 24 32 26 32 32 27 31 27 30 23 28
18 | 7 17 6 11 19 3 21 9 17 23 4 | 25 31 23 34 36 23 27 26 22 23 26
19 | 8 14 5 11 15 6 17 8 20 20 4 | 26 32 27 32 32 23 27 24 26 20 26
20 | 14 20 5 13 15 9 14 13 17 19 5 | 33 38 31 33 33 31 31 32 36 36 31
21E | 7 13 4 10 16 4 15 6 17 12 3 | 18 24 19 19 22 19 23 20 26 22 20
22 | 10 14 6 9 16 4 19 8 13 18 4 | 28 30 29 36 40 28 29 32 24 28 30
23 | 11 16 5 11 10 4 17 9 16 22 4 | 26 30 25 30 28 25 31 25 30 24 27
24 | 12 18 6 8 16 5 15 9 19 13 4 | 58 54 54 60 65 55 58 52 54 57 54
25 | 11 19 4 9 13 5 15 12 18 13 4 | 23 27 19 22 25 20 29 20 23 18 21
26 | 9 14 6 8 12 4 13 8 17 14 3 | 26 21 23 27 27 22 23 23 16 24 24
X27 | 10 14 8 11 --- 5 16 9 25 16 5 | 28 34 27 32 --- 27 35 27 36 28 28
28 | 10 27 5 10 12 4 16 10 13 17 4 | 24 32 22 27 33 23 29 23 26 21 24
29 | 8 16 5 12 13 7 20 11 23 39 4 | 27 29 25 28 29 27 32 25 36 41 26
X30E | 7 --- --- --- --- 458 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
31E | 7 17 4 9 15 7 16 10 18 10 4 | 24 26 20 24 30 20 23 20 24 20 22
32 | 11 12 5 10 12 5 14 6 20 15 4 | 22 20 20 20 21 20 23 19 25 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 6 10 16 5 18 11 18 20 |T 29 32 28 32 34 28 32 28 30 29 29
WRMS | 11 18 6 10 15 5 18 10 17 20 |NE 25 28 23 28 31 23 28 24 26 25 25
MEDI | 11 17 6 10 15 5 17 9 18 18 |MD 26 30 25 28 31 25 29 25 26 27 26
Table 3.1781.5 GPS week: 1781 Day: 5 MJD: 56716.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 10 15 5 9 11 8 --- 7 12 15 4 | 35 31 33 30 30 29 --- 31 32 32 30
2E | 14 20 7 10 21 4 23 13 10 11 5 | 20 24 19 21 21 18 24 19 21 20 18
3 | 10 10 4 8 20 4 12 6 14 24 3 | 25 24 21 28 28 21 24 20 24 28 22
4E | 12 18 9 9 19 5 17 19 16 16 5 | 23 28 22 24 26 22 26 32 30 24 23
5 | 14 21 7 12 15 6 21 11 12 15 5 | 26 32 20 24 28 20 32 22 28 24 23
X6 | 13 11 6 13 --- 7 --- 9 17 --- 5 | 27 24 24 25 --- 20 --- 20 29 --- 22
7E | 17 24 8 11 18 12 21 14 15 16 5 | 98 90 92 92 95 92 88 96 98 90 93
8E | 13 20 7 11 18 8 21 12 13 16 5 | 33 27 11 12 14 25 22 15 12 14 25
9 | 7 17 8 13 23 6 22 9 14 25 5 | 95 93 88 86 95 87 96 87 88 93 90
10 | 11 17 7 8 22 3 11 12 19 16 4 | 24 20 19 20 28 18 19 26 28 22 21
11 | 10 13 6 8 16 6 13 10 15 17 4 | 34 33 31 33 38 31 35 29 31 28 30
12 | 10 17 7 8 16 4 23 13 12 18 4 | 26 26 19 26 28 18 27 23 21 17 21
13 | 13 16 8 12 15 6 20 12 13 25 4 | 30 36 30 31 38 29 39 31 30 33 30
14 | 22 16 6 10 20 7 15 10 14 25 5 | 35 29 29 39 34 27 33 33 33 29 31
15 | 11 21 8 10 12 7 27 12 14 29 5 | 28 26 26 32 29 24 30 29 22 23 25
16 | 16 16 5 12 17 5 23 11 14 24 5 | 29 25 20 26 27 22 24 22 27 20 21
17 | 12 25 8 18 14 6 21 9 17 23 5 | 24 33 24 31 33 24 31 27 29 21 25
18 | 8 20 5 14 16 7 20 10 11 19 4 | 24 25 18 34 30 19 25 23 22 14 22
19 | 10 16 5 9 12 4 19 11 15 24 4 | 29 29 25 29 31 26 28 23 28 21 25
20 | 9 16 6 13 14 8 19 10 13 20 4 | 26 26 25 32 32 21 29 28 27 23 25
21E | 7 15 7 10 20 7 17 7 17 14 4 | 14 18 14 17 22 13 18 13 17 18 12
22 | 8 18 7 10 16 5 21 9 13 18 4 | 25 24 21 31 33 21 25 24 27 18 23
23 | 9 16 6 11 12 4 15 8 13 24 4 | 27 28 27 32 29 26 29 25 27 18 26
24 | 10 16 6 7 15 6 13 8 11 15 4 | 48 51 49 53 54 47 47 47 45 50 48
25 | 10 18 5 8 13 4 16 11 12 15 4 | 22 29 21 24 27 21 30 22 20 23 21
26 | 8 14 9 11 14 6 13 10 16 19 4 | 20 20 23 24 23 21 23 22 19 23 20
X27 | 13 12 8 12 --- 4 16 8 10 15 4 | 24 26 23 25 --- 21 31 19 27 21 22
28 | 8 21 6 9 13 4 14 10 16 16 4 | 29 34 31 35 39 29 34 30 32 26 31
29 | 10 18 6 8 11 6 20 14 14 29 4 | 26 30 22 25 26 20 29 24 23 28 23
X30E | 4 --- --- --- --- 419 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
31E | 9 21 6 7 17 6 18 13 19 9 5 | 29 34 30 32 34 28 33 30 35 28 29
32 | 10 11 4 11 14 7 12 8 11 14 3 | 21 17 15 23 21 15 19 15 23 16 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 7 11 16 6 19 11 14 20 |T 31 32 28 32 34 27 32 29 30 28 28
WRMS | 11 18 7 10 15 6 19 11 13 19 |NE 26 26 22 27 29 21 27 23 25 22 23
MEDI | 10 17 6 10 16 6 19 10 14 17 |MD 26 28 23 29 29 22 29 24 27 23 23
Table 3.1781.6 GPS week: 1781 Day: 6 MJD: 56717.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 8 17 8 9 24 15 --- 17 15 16 5 | 100 107 107 101 97 101 --- 108 105 107 104
2E | 12 18 7 9 23 5 19 11 13 15 5 | 20 22 20 26 27 20 22 20 25 23 20
3 | 8 11 4 10 15 4 12 7 12 20 3 | 25 24 22 29 30 23 24 23 25 26 23
4E | 11 21 9 10 18 6 18 14 16 17 5 | 31 31 34 31 29 30 32 31 32 33 30
5 | 9 21 6 11 16 6 21 11 10 15 4 | 31 39 23 25 31 24 38 24 30 28 26
6 | 12 11 5 14 12 7 13 7 24 --- 4 | 26 22 20 32 20 22 21 22 32 --- 23
7 | 8 24 6 5 20 8 16 9 10 12 4 | 55 59 54 56 60 53 58 54 61 56 55
8E | 16 16 6 9 16 6 22 15 14 17 5 | 29 22 13 16 15 26 22 15 13 17 28
9 | 9 16 6 10 22 5 14 11 12 28 4 | 91 94 88 89 97 89 97 90 85 99 90
10 | 10 20 5 8 22 5 15 12 14 23 4 | 25 22 27 30 37 23 23 32 26 33 26
11 | 7 15 5 7 23 8 14 12 15 21 4 | 50 53 54 52 50 50 53 50 52 55 51
12 | 8 19 5 8 16 5 18 13 12 14 4 | 26 25 16 26 28 17 24 21 26 12 20
13M | 10 18 5 8 15 3 17 6 12 24 4 | 32 39 31 36 43 32 41 37 30 40 33
14 | 17 17 6 12 16 6 14 10 13 21 4 | 34 32 32 44 37 34 33 37 34 32 34
15 | 11 22 7 8 14 5 23 8 12 30 4 | 28 29 31 39 36 31 31 33 30 30 31
16 | 11 21 5 13 14 4 21 11 14 27 4 | 23 24 16 26 27 17 24 21 24 21 20
17M | 13 21 10 16 14 4 17 15 14 29 5 | 23 35 27 36 33 27 32 35 34 30 29
18 | 10 20 5 18 16 5 19 7 11 22 4 | 33 29 27 47 40 30 29 31 30 26 31
19M | 8 18 7 11 13 5 19 10 15 25 4 | 30 29 28 37 34 27 30 27 27 27 28
20M | 14 19 8 11 18 4 18 11 13 19 5 | 37 29 34 38 38 31 29 38 33 37 33
21E | 7 13 3 12 14 6 16 7 11 21 3 | 20 20 17 27 23 15 25 18 20 24 19
22 | 8 17 5 11 15 3 18 10 12 19 4 | 36 30 36 46 45 36 33 39 38 32 37
23M | 7 16 6 12 12 3 14 11 13 21 4 | 24 28 25 36 32 25 30 29 25 24 26
24 | 9 17 6 10 16 5 14 12 11 12 4 | 78 74 74 80 82 76 78 73 76 73 76
25 | 9 20 5 10 12 6 16 11 12 17 4 | 21 30 17 25 25 17 31 18 21 19 20
26 | 10 15 6 9 16 3 13 11 15 19 4 | 22 21 27 32 31 23 25 28 20 27 25
X27 | 9 12 6 10 --- 5 16 9 14 16 4 | 28 28 23 29 --- 23 32 23 30 24 25
28 | 9 17 5 9 16 4 17 10 12 18 4 | 28 32 27 31 36 25 32 34 28 26 29
29 | 8 19 7 13 12 7 20 11 20 40 4 | 33 37 30 32 33 28 40 30 30 43 30
X30E | 3 --- --- --- --- 199 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
31E | 7 22 5 8 18 4 16 10 12 8 4 | 34 40 30 38 40 29 37 30 28 30 31
32M | 7 13 6 8 18 7 15 10 17 13 4 | 30 34 34 31 36 29 33 33 29 30 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 11 17 5 17 11 14 21 |T 35 36 33 39 39 33 35 35 35 36 34
WRMS | 10 18 6 10 15 5 17 10 12 21 |NE 27 28 24 32 32 24 29 27 28 27 26
MEDI | 9 18 6 10 16 5 16 11 13 19 |MD 30 30 27 32 34 27 31 31 30 30 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 4.1781 GPS week: 1781 MJD: 56711.0-56717.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3009 |U 5 4 14 |U 7 9 27 |U 7 7 18 |
emr | emr 2952 | 6 6 18 |U 9 12 29 | 11 8 20 |
esa | esa 2962 | 4 4 13 |U 8 9 28 | 9 7 19 |
gfz | gfz 2952 |U 5 4 17 |U 7 9 28 |U 9 10 18 |
grg | grg 2784 |U 7 7 19 |U 9 11 32 |U 12 11 24 |
igr | igr 2953 | 5 4 14 | 7 9 28 | 8 7 19 |
igs | igs 2922 | 5 4 16 | 8 10 29 | 11 10 19 |
jpl | jpl 2829 | 6 6 17 | 8 12 38 |U 13 10 24 |
mit | mit 2962 | 21 18 56 |U 11 13 45 |U 41 18 51 |
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 5.1781.0 GPS week: 1781 Day: 0 MJD: 56711.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 4 4 11 | 7 8 22 | 8 6 21 |
emr | emr 2963 | 5 6 16 | 9 7 26 | 10 6 22 |
esa | esa 2976 | 4 4 13 | 8 9 23 | 10 7 22 |
gfz | gfz 2964 | 4 4 16 | 7 8 25 | 9 9 18 |
grg | grg 2880 | 6 5 15 | 9 8 34 | 11 7 21 |
igr | igr 2976 | 4 4 13 | 8 10 23 | 8 7 20 |
igs | igs 2943 | 4 4 15 | 8 10 26 | 11 9 20 |
jpl | jpl 2866 | 6 9 19 | 7 7 32 | 11 7 23 |
mit | mit 2976 | 5 6 20 | 10 21 35 | 9 8 19 |
Table 5.1781.1 GPS week: 1781 Day: 1 MJD: 56712.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 4 2 14 | 7 10 35 | 7 6 15 |
emr | emr 2964 | 6 7 17 | 9 13 35 | 10 8 15 |
esa | esa 2976 | 4 3 13 | 7 11 36 | 9 6 15 |
gfz | gfz 2965 | 5 3 17 | 7 11 30 | 8 9 15 |
grg | grg 2784 | 6 7 16 | 9 11 29 | 9 8 19 |
igr | igr 2974 | 4 3 12 | 7 12 35 | 7 6 19 |
igs | igs 2818 | 4 4 16 | 7 11 35 | 17 7 15 |
jpl | jpl 2868 | 6 8 14 | 8 13 30 | 12 12 28 |
mit | mit 2976 | 5 3 17 | 8 10 33 | 13 11 20 |
Table 5.1781.2 GPS week: 1781 Day: 2 MJD: 56713.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3044 | 6 6 22 | 10 9 24 | 6 7 16 |
emr | emr 2966 | 7 5 27 | 11 9 31 | 10 11 22 |
esa | esa 2976 | 6 5 22 | 10 9 27 | 8 8 20 |
gfz | gfz 2963 | 6 5 28 | 9 8 28 | 9 12 18 |
grg | grg 2784 | 7 7 24 | 12 11 32 | 10 11 25 |
igr | igr 2976 | 5 6 21 | 9 7 27 | 8 9 22 |
igs | igs 2966 | 6 5 27 | 10 8 25 | 9 12 21 |
jpl | jpl 2870 | 6 5 23 | 9 10 32 | 11 12 25 |
mit | mit 2976 | 6 6 26 | 12 21 62 | 144 19 93 |
Table 5.1781.3 GPS week: 1781 Day: 3 MJD: 56714.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3049 | 5 6 13 | 7 10 29 | 6 6 18 |
emr | emr 2967 | 7 7 17 | 9 13 36 | 11 8 19 |
esa | esa 2976 | 6 5 13 | 8 10 31 | 9 7 22 |
gfz | gfz 2966 | 5 4 14 | 7 10 31 | 9 10 19 |
grg | grg 2688 | 6 7 18 | 9 11 34 | 10 9 21 |
igr | igr 2976 | 6 5 13 | 7 11 34 | 7 7 22 |
igs | igs 2971 | 5 5 15 | 8 12 35 | 9 8 20 |
jpl | jpl 2872 | 7 6 16 | 10 23 83 | 13 9 28 |
mit | mit 2976 | 59 37 68 | 18 15 80 | 19 13 53 |
Table 5.1781.4 GPS week: 1781 Day: 4 MJD: 56715.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2949 | 5 4 20 | 7 12 27 | 9 8 18 |
emr | emr 2874 | 6 5 20 | 10 14 29 | 12 10 18 |
esa | esa 2880 | 5 4 13 | 7 10 27 | 11 8 19 |
gfz | gfz 2873 | 5 4 15 | 6 10 25 | 12 10 17 |
grg | grg 2688 | 9 10 17 | 8 12 31 | 19 17 34 |
igr | igr 2880 | 5 4 14 | 7 11 26 | 9 9 19 |
igs | igs 2831 | 5 4 14 | 7 11 27 | 13 11 19 |
jpl | jpl 2684 | 6 5 20 | 8 13 30 | 11 10 20 |
mit | mit 2880 | 10 8 28 | 7 8 37 | 13 10 20 |
Table 5.1781.5 GPS week: 1781 Day: 5 MJD: 56716.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 5 4 11 | 8 8 29 | 7 8 19 |
emr | emr 2968 | 7 5 18 | 10 12 26 | 11 9 23 |
esa | esa 2976 | 4 3 10 | 8 8 28 | 10 8 19 |
gfz | gfz 2968 | 6 5 17 | 8 9 31 | 10 10 21 |
grg | grg 2784 | 7 6 16 | 11 15 36 | 13 9 25 |
igr | igr 2936 | 5 4 16 | 8 8 32 | 9 8 18 |
igs | igs 2956 | 5 4 14 | 8 8 29 | 10 10 22 |
jpl | jpl 2776 | 6 6 17 | 9 10 34 | 12 9 21 |
mit | mit 2976 | 8 12 19 | 8 10 32 | 76 60 136 |
Table 5.1781.6 GPS week: 1781 Day: 6 MJD: 56717.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 | 5 4 8 | 5 10 23 | 7 6 15 |
emr | emr 2968 | 5 5 13 | 7 13 25 | 11 7 19 |
esa | esa 2976 | 4 3 9 | 6 9 23 | 6 7 14 |
gfz | gfz 2968 | 4 3 10 | 6 8 23 | 10 13 21 |
grg | grg 2880 | 6 8 30 | 7 11 26 | 14 16 24 |
igr | igr 2957 | 5 3 10 | 5 8 22 | 8 6 17 |
igs | igs 2969 | 4 3 11 | 6 10 24 | 10 12 19 |
jpl | jpl 2872 | 6 6 13 | 7 10 27 | 19 12 25 |
mit | mit 2976 | 57 51 213 | 10 9 40 | 14 8 17 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1781 GPS week: 1781 MJD: 56711.500-56717.500
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 | -23 -15 -92 10 -2 | 10 17
| 20 15 77 117 4 | 2
emr uuuuu | 2 -10 159 103 -3 | 62 64
| 27 24 63 96 13 | 2
esa uuuuu | -6 -19 87 -93 0 | 8 17
| 16 16 24 60 2 | 1
gfz uuuuu | -13 -60 49 -222 4 | 7 15
| 11 21 76 136 4 | 1
grg uuuuu | 41 47 -111 55 1 | 15 21
| 20 22 65 130 7 | 2
igr xxxxx | 2 31 4 55 -1 | 1 14
| 19 16 46 66 3 | 2
irf xxxxx | 14 14 -48 15 -3 | -1 15
| 13 11 27 20 4 | 3
jpl uuuuu | 16 -42 61 72 3 | 26 30
| 49 27 82 69 6 | 1
mit uuuuu | 12 26 -130 71 -6 | 15 22
| 24 35 67 91 5 | 4
ngs uuuuu | 5 100 -49 217 -1 | 1 12
| 86 40 116 148 4 | 3
sio xxxxx | 33 8 -4 143 8 | 58 58
| 36 16 50 97 34 | 26
Table 7.1781.0 GPS week: 1781 Day: 0 MJD: 56711.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -38 -31 -94 37 0 | 12 18
emr uuuuu | -24 9 78 57 19 | 61 63
esa uuuuu | -6 -16 69 -49 2 | 9 18
gfz uuuuu | 3 -101 104 36 10 | 8 15
grg uuuuu | 61 13 6 82 -6 | 19 23
igr xxxxx | -3 41 -2 70 1 | 4 14
irf xxxxx | 13 11 -85 -10 -5 | 4 15
jpl uuuuu | -55 -42 153 87 -1 | 28 33
mit uuuuu | 12 31 -226 -79 -5 | 20 25
ngs uuuuu | 41 159 -118 -70 -6 | 6 12
sio xxxxx | -3 -8 53 25 82 | 0 0
Table 7.1781.1 GPS week: 1781 Day: 1 MJD: 56712.500
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 | -45 0 -122 -146 5 | 11 18
emr uuuuu | -22 -29 199 115 -9 | 62 64
esa uuuuu | -4 -6 87 -91 0 | 8 17
gfz uuuuu | -11 -75 139 -144 2 | 7 14
grg uuuuu | 45 46 -93 131 5 | 16 21
igr xxxxx | -7 17 -14 16 -3 | 2 14
irf xxxxx | 15 8 -54 15 -7 | 2 15
jpl uuuuu | -38 -42 78 154 8 | 25 30
mit uuuuu | 10 26 -201 42 -10 | 18 24
ngs uuuuu | 66 72 -54 174 -4 | 2 11
sio xxxxx | 21 -9 -15 125 9 | 69 69
Table 7.1781.2 GPS week: 1781 Day: 2 MJD: 56713.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -21 -4 -7 -68 0 | 11 18
emr uuuuu | -8 -45 172 8 11 | 61 63
esa uuuuu | 15 -30 89 -193 1 | 8 17
gfz uuuuu | -14 -40 22 -219 6 | 7 14
grg uuuuu | 50 55 -139 212 4 | 15 20
igr xxxxx | -7 22 22 -72 0 | 2 14
irf xxxxx | 24 0 -25 18 -6 | 0 15
jpl uuuuu | 33 -10 -109 15 3 | 25 30
mit uuuuu | 30 -33 -100 192 -12 | 16 23
ngs uuuuu | -81 134 17 273 -4 | 1 12
sio xxxxx | 47 0 79 261 3 | 70 70
Table 7.1781.3 GPS week: 1781 Day: 3 MJD: 56714.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 6 -17 -171 66 0 | 12 19
emr uuuuu | 31 -23 174 187 -11 | 64 66
esa uuuuu | -7 -18 134 -130 0 | 9 18
gfz uuuuu | 1 -46 -63 -321 -2 | 7 15
grg uuuuu | 13 67 -96 -24 -8 | 16 21
igr xxxxx | -15 5 88 62 -3 | 2 14
irf xxxxx | 27 4 -13 41 -7 | 0 15
jpl uuuuu | 72 -7 68 -1 11 | 25 30
mit uuuuu | 44 -3 -65 159 -10 | 16 23
ngs uuuuu | -123 89 40 247 5 | 0 11
sio xxxxx | 65 5 -31 247 -5 | 72 72
Table 7.1781.4 GPS week: 1781 Day: 4 MJD: 56715.500
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 -36 -201 65 -5 | 11 19
emr uuuuu | 17 -3 264 252 -11 | 63 66
esa uuuuu | 5 -6 65 -121 0 | 9 18
gfz uuuuu | -21 -60 -26 -370 5 | 6 16
grg uuuuu | 25 65 -107 113 -1 | 15 21
igr xxxxx | 19 45 12 115 -4 | 1 16
irf xxxxx | 15 25 -27 29 -1 | -2 18
jpl uuuuu | 6 -46 114 93 -3 | 27 31
mit uuuuu | -14 68 -51 103 -6 | 14 24
ngs uuuuu | 63 45 -10 416 2 | -1 12
sio xxxxx | 86 30 -54 193 -10 | 65 66
Table 7.1781.5 GPS week: 1781 Day: 5 MJD: 56716.500
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 | -35 -21 -40 -83 -9 | 9 15
emr uuuuu | 41 25 114 124 -14 | 61 63
esa uuuuu | -8 -49 70 -36 0 | 8 16
gfz uuuuu | -22 -48 49 -302 5 | 5 14
grg uuuuu | 65 63 -208 66 11 | 14 20
igr xxxxx | 37 39 -17 120 3 | 0 14
irf xxxxx | 15 20 -75 27 2 | -4 15
jpl uuuuu | 26 -62 60 155 5 | 26 29
mit uuuuu | 24 53 -159 67 -2 | 11 20
ngs uuuuu | -41 121 58 271 -2 | -1 12
sio xxxxx | 33 18 -22 127 -13 | 65 66
Table 7.1781.6 GPS week: 1781 Day: 6 MJD: 56717.500
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 | 3 1 -11 200 -3 | 7 14
emr uuuuu | -19 -5 112 -19 -10 | 60 62
esa uuuuu | -37 -7 96 -27 -6 | 7 15
gfz uuuuu | -26 -52 117 -234 5 | 6 15
grg uuuuu | 29 23 -142 -192 2 | 13 19
igr xxxxx | -11 48 -62 74 -4 | -2 13
irf xxxxx | -13 31 -56 -14 3 | -5 15
jpl uuuuu | 68 -85 62 -1 -5 | 25 28
mit uuuuu | -23 43 -107 12 1 | 9 17
ngs uuuuu | 107 81 -273 210 2 | -3 10
sio xxxxx | -15 23 -35 21 -12 | 64 65
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