[IGSREPORT-22556] Wk 1780 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Mar 7 07:21:34 PST 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1780 (Feb 16, 2014 - Feb 22, 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:
igs1780[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1780[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1780[0-6].cls IGS GPS clock combination summary report.
igs17807.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17807.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. 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 | PDEL PDEL
0 | EMR | 4 8 9 8 9 HERS
0 | ESA | 4 FLIN DRAG FLIN SEY1
0 | GFZ | 2 4 4 8 DAEJ DAEJ
0 | GRG | 4 8 9 4 8 9 DAEJ DRAG IRKJ KELY DAEJ IRKJ KELY
0 | JPL | 8 9 POL2
0 | MIT | 1 2 18 1 2 4 8 9 18 19 21 MAS1 MDVJ STR1 SYDN
1 | COD | 4 21 GUAT ISPA GUAT
1 | EMR | 4 8 9 21 25 8 9 21 25
1 | ESA | 4 DGAV KARR
1 | GFZ | 2 4 4 KARR
1 | GRG | 4 8 9 21 8 9 21 DARW FAA1 GUAT HYDE IRKJ ISPA KOUC
1 | GRG | KOUR MAL2 NOVM NRMD POL2 FAA1 GUAT HYDE IRKJ ISPA
1 | GRG | KOUC MAL2
1 | JPL | 4 8 9
1 | MIT | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
1 | MIT | 21 22 23 24 25 26 27 28 29 31 32 1 2 3 4 5 6 7 8
1 | MIT | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
1 | MIT | 26 27 28 29 31 32
2 | COD | 9 21 NTUS
2 | EMR | 1 4 8 9 1 4 8 31
2 | ESA | 9 HOFN NOVM DGAV HOFN NOVM UNSA
2 | GFZ | 2 4 4 8
2 | GRG | 4 8 9 21 4 8 21 HOFN IRKJ KELY NRMD POL2 HOFN IRKJ
2 | GRG | KELY NRMD POL2
2 | JPL | 2 4 8 9 21 29 31
2 | MIT | 1 2 4 8 9 12 14 18 21 26 29 32 1 2 3 4 8 9 12 14
2 | MIT | 18 21 25 26 28 29 32 HYDE NNOR NTUS HYDE NNOR NTUS
3 | COD | 1 4 WHIT WHIT
3 | EMR | 1 4 8 9 8 9 HERS WHIT USNO WHIT
3 | ESA | 4 21 KOUR NICO KOUR NICO SCOR
3 | GFZ | 2 4 4 21 QAQ1 SYOG QAQ1 SYOG
3 | GRG | 1 4 8 9 17 21 8 9 17 DARW FAA1 IRKJ KELY NICO NOVM
3 | GRG | NRMD NTUS NYAL SPT0 TIDB TLSE TRO1 FAA1 IRKJ KELY
3 | GRG | NICO NOVM NYAL OHI2 REYK SPT0 TRO1
3 | JPL | 8 9 TIXI WHIT
3 | MIT | 1 2 3 4 8 9 11 18 19 24 25 31 1 2 3 4 8 9 18 24 25
3 | MIT | HOFN MAC1 MDVJ NICO NYAL REYK TIDB HOFN MAC1 NICO
3 | MIT | NYAL TIDB
4 | COD | HOFN HOFN
4 | EMR | 8 9 8 9 HERS NYAL HERS NYAL SYOG
4 | ESA | 1 1 FLIN SCOR FLIN SCOR
4 | GFZ | 1 2 4 8 1 8
4 | GRG | 8 9 8 9 BRST DARW HOFN HRAO IRKJ NTUS HOFN HRAO IRKJ
4 | GRG | NTUS
4 | JPL | 8 9 ALRT
4 | MIT | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
4 | MIT | 21 22 23 24 25 26 27 28 29 31 32 1 2 3 4 5 6 7 8
4 | MIT | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
4 | MIT | 26 27 28 29 31 32 CONZ CONZ
5 | COD | 1
5 | EMR | 4 8 9 1 4 8 9 HERS HERS MCM4
5 | ESA | 1 1
5 | GFZ | 1 2 4 4 CHUR NOVM CHUR NOVM
5 | GRG | 4 8 9 4 8 9 BARH BOGT BOR1 BRST CHUR DARW GRAZ IRKJ
5 | GRG | ISPA KELY KOUC MCM4 NRMD SPT0 SYOG BARH CHUR GRAZ
5 | GRG | IRKJ KOUC SPT0
5 | JPL | 8 9 13 21 CUSV TIXI
5 | MIT | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
5 | MIT | 21 22 23 24 25 26 27 28 29 31 32 1 2 3 4 5 6 7 8
5 | MIT | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
5 | MIT | 26 27 28 29 31 32
6 | COD | SYOG SYOG
6 | EMR | 4 8 9 4 8 9 SYOG MCM4 SYOG
6 | ESA | 1 1 BAKE FLIN FLIN
6 | GFZ | 1 4 4 MATE MATE
6 | GRG | 4 8 9 4 8 9 CHUR DAV1 ISPA KELY KOUC MATE CHUR DAV1
6 | GRG | ISPA KELY KOUC MATE
6 | JPL | 8 9 YELL
6 | MIT | 1 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. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | MIT | ~23:15 | ~ 0.27 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G16 | 2014_02_18 | 2014013
8. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
6 | COD | 1
6 | NGS | 1
9. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G01 | | | | | | | 4 |
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
11. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.0 -.1 -.2 -29 12 -41 .20
EMR | 0 | 6.1 2.9 -.4 44 46 -32 .04
ESA | 0 | .4 6.1 -17.1 20 23 54 -.03
GFZ | 0 | -.5 .0 -1.6 -35 -7 -28 .47
GRG | 0 | 3.2 -.1 -9.0 1 0 -6 .60
JPL | 0 | -1.3 4.4 15.9 26 62 -58 .36
MIT | 0 | 4.2 -3.4 1.2 7 0 -38 .28
NGS | 0 | 4.3 -1.6 -3.4 6 -15 14 .41
COD | 1 | -2.2 .0 -.9 -11 18 -36 .11
EMR | 1 | .7 5.8 .2 44 62 -24 .07
ESA | 1 | 5.4 8.9 -16.6 29 9 94 -.17
GFZ | 1 | -.3 -.1 -1.5 -39 -6 -23 .29
GRG | 1 | 5.9 4.1 -10.4 2 -10 17 .65
JPL | 1 | 1.1 5.3 19.8 -1 -72 105 -.11
MIT | 1 | -1.2 2.9 3.7 -8 -3 -42 .27
NGS | 1 | 1.2 5.4 -1.3 2 0 -7 .32
COD | 2 | -1.3 -.5 -1.2 -17 3 -27 .40
EMR | 2 | 5.3 -2.5 2.4 41 46 -24 .52
ESA | 2 | 4.6 5.1 -14.0 19 -1 72 -.10
GFZ | 2 | .0 .5 -1.3 -40 -17 -18 .10
GRG | 2 | 2.9 -4.4 -11.6 18 9 11 .96
JPL | 2 | 2.8 4.2 10.5 -71 29 -71 .33
MIT | 2 | 1.6 -.5 2.0 9 -14 -39 .24
NGS | 2 | -4.0 -11.1 -7.3 -46 46 -54 .32
COD | 3 | -.6 .1 -1.1 -36 19 -45 .49
EMR | 3 | -.9 4.9 -3.0 41 37 -23 .19
ESA | 3 | 2.4 6.5 -9.1 54 -24 83 .07
GFZ | 3 | .1 .3 -1.6 -42 -11 -17 .16
GRG | 3 | 12.9 9.9 -13.4 4 -13 -8 .64
JPL | 3 | .4 -1.0 20.9 -2 -6 0 -.38
MIT | 3 | 1.4 -.4 2.2 -8 0 -47 .35
NGS | 3 | -5.4 -4.3 -8.0 -7 54 -50 .27
COD | 4 | -.9 -.2 -.6 -34 1 -38 .40
EMR | 4 | 7.6 -5.4 3.2 26 33 -47 .60
ESA | 4 | 3.7 .6 .0 1 -21 56 .08
GFZ | 4 | -.1 -.4 -1.2 -56 -12 -8 .20
GRG | 4 | 2.2 7.1 -1.4 -6 -1 16 .55
JPL | 4 | -1.9 -2.1 9.0 -29 -16 -67 .07
MIT | 4 | 3.9 -3.9 5.5 -9 11 -46 .49
NGS | 4 | -5.4 3.8 10.5 -15 14 -21 .61
COD | 5 | -1.0 -.1 -.6 -30 11 -33 .42
EMR | 5 | 5.6 -5.9 -6.7 34 36 -42 .66
ESA | 5 | 7.6 -.7 3.8 -6 -40 61 .21
GFZ | 5 | -.1 .0 -.7 -42 -9 -17 -.01
GRG | 5 | 5.7 -2.1 -1.5 -14 18 26 1.14
JPL | 5 | .9 -2.0 20.7 -31 -33 93 .49
MIT | 5 | 3.5 .9 9.5 -1 8 -41 .53
NGS | 5 | 2.9 -1.6 4.5 -25 -16 4 .64
COD | 6 | -1.1 -.1 -1.5 -24 -9 -13 .35
EMR | 6 | -6.2 7.1 -1.5 55 41 -30 .52
ESA | 6 | 5.5 5.6 .2 -1 -26 75 .19
GFZ | 6 | .6 -.3 -1.2 -32 -23 -13 -.12
GRG | 6 | 3.9 .2 6.7 -44 19 -2 .83
JPL | 6 | -8.7 -.8 8.9 -10 18 -9 .44
MIT | 6 | 5.0 .5 7.2 7 8 -31 .36
NGS | 6 | -3.8 5.7 8.1 0 9 -7 .56
12. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
13. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1780.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1780.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 2.1780.[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 3.1780.[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 5.1780.0-6). 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 1780 summary. (Feb 16, 2014 - Feb 22, 2014)
Table 1.1780.a GPS week: 1780 MJD: 56704.000-56710.000
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 249| 0 0 3 1 11 -9 .10 11 10 | -1032 75 19 144
| 0 0 1 24 20 13 .02 | 144 307
emr 79| -3 -1 2 -11 9 11 .09 18 18 | 5012 -328 24 134
| 2 2 1 16 7 17 .03 | 1503 1139
esa 150| 1 0 0 38 -4 12 -.22 6 6 | -1215 379 11 132
| 0 0 1 21 25 31 .02 | 1198 1808
gfz 192| 1 0 -5 30 -10 -27 .15 11 10 | -80 -126 14 133
| 1 0 1 12 15 15 .01 | 429 645
grg 183| 3 1 1 -40 -13 -14 .26 16 15 | -133 107 21 163
| 1 1 2 18 31 18 .03 | 194 529
igr n/a| 0 0 0 -17 16 0 -.19 5 5 | 5911 200 18 92
| 0 0 1 20 11 13 .02 | 1311 1247
jpl 80| 0 1 1 9 6 0 .05 17 17 | 3744 -421 22 156
| 1 1 2 35 23 11 .02 | 1639 1211
mit 299| -1 -2 -1 -20 -6 -5 -.12 12 11 | -126 82 45 280
| 1 0 1 15 12 22 .02 | 215 339
ngs 231| -2 0 -2 -90 14 15 .05 13 11 | -952 -3 1766 3509
| 1 1 3 43 44 20 .05 | 144 261
Table 1.1780.b GPS week : 1780 MJD: 56704.000-56710.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 5 6 5 5 5 5 16 |
2 | 5 5 5 5 5 6 5 |
3 | 3 4 5 3 4 4 4 |
4 | 6 6 7 5 6 6 6 |
5 | 5 5 5 5 5 4 5 |
6 | 4 4 5 3 4 5 5 |
7 | 4 5 5 4 4 4 5 |
8 | 6 6 6 5 5 7 7 |
9 | 6 5 6 5 5 5 5 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 5 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 5 |
14 | 4 4 5 5 4 4 6 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 0 6 5 4 5 |
17 | 5 5 5 6 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 4 5 4 4 4 4 5 |
20 | 4 5 5 4 5 5 5 |
21 | 4 4 4 6 5 5 4 |
22 | 4 5 5 4 4 5 5 |
23 | 4 4 4 4 4 4 4 |
24 | 5 5 4 5 5 5 5 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 5 5 4 4 4 6 |
28 | 4 5 5 5 5 5 5 |
29 | 4 5 5 4 5 5 5 |
31 | 5 5 5 5 5 5 6 |
32 | 4 4 4 4 3 4 5 |
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 2.1780.0 GPS week: 1780 Day: 0 MJD: 56704.000
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 3 3 13 -18 .08 10 9 | -1032 202 18 142
emr 80| -3 0 2 4 6 16 .09 17 17 | 3829 1565 18 147
esa 150| 1 0 0 59 43 23 -.26 6 6 | -1516 1895 11 141
gfz 191| 2 0 -4 33 -6 -37 .17 11 10 | 29 188 14 131
grg 183| 1 1 0 -14 -33 -2 .29 13 13 | -455 944 17 142
igr n/a| 0 0 0 -30 29 13 -.20 5 5 | 4216 2056 17 93
jpl 80| 2 2 3 12 2 -22 .03 17 17 | 3756 1553 20 159
mit 300| -1 -2 -1 -44 -21 13 -.09 12 11 | -535 609 29 235
ngs 230| -2 -1 -3 -139 -62 14 .11 13 11 | -830 -27 1899 3062
Table 2.1780.1 GPS week: 1780 Day: 1 MJD: 56705.000
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 1 3 -35 -7 -24 .08 11 10 | -1168 343 18 141
emr 80| -2 -1 5 -29 5 4 .09 17 17 | 4656 688 25 141
esa 150| 1 0 0 32 4 28 -.24 6 6 | -142 794 13 150
gfz 195| 1 0 -4 12 -40 -45 .16 11 10 | 128 -94 14 132
grg 183| 3 0 3 -24 -5 -41 .23 16 15 | -148 220 17 205
igr n/a| 0 0 1 -35 20 -10 -.21 5 5 | 5556 1489 18 88
jpl 80| 0 2 2 75 -31 7 .04 17 17 | 4599 710 20 169
mit 300| -2 -2 0 -9 0 6 -.11 12 11 | 0 -128 49 221
ngs 232| -1 0 -6 -69 88 11 .09 14 12 | -1111 278 1365 3282
Table 2.1780.2 GPS week: 1780 Day: 2 MJD: 56706.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| 1 0 3 -1 -7 16 .08 13 12 | -795 -441 23 150
emr 80| -2 -2 3 -38 9 35 .07 17 17 | 6640 -621 53 177
esa 150| 2 1 -1 75 -12 -53 -.22 7 7 | 325 -625 15 121
gfz 192| 2 0 -6 31 -18 -11 .13 12 11 | 301 -573 18 131
grg 182| 2 0 1 -47 27 1 .28 15 14 | 207 -615 32 159
igr n/a| 0 0 1 -45 1 22 -.18 5 5 | 6922 -19 20 81
jpl 80| 0 2 4 -16 2 -4 .04 16 16 | 5306 -977 34 137
mit 299| -1 -2 0 -3 12 29 -.11 12 12 | 77 -301 43 354
ngs 231| -2 -3 -2 -135 6 35 .08 13 12 | -767 -352 1877 3779
Table 2.1780.3 GPS week: 1780 Day: 3 MJD: 56707.000
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 253| 1 0 4 32 34 -16 .12 9 9 | -1057 134 20 167
emr 80| -3 -1 3 -3 24 33 .07 18 18 | 6896 -430 22 137
esa 150| 0 1 0 35 -3 41 -.23 6 6 | -2737 3590 11 138
gfz 190| 1 -1 -3 24 9 -38 .14 11 11 | -312 817 12 122
grg 178| 4 0 0 -73 -68 -5 .31 17 15 | -148 461 22 172
igr n/a| 1 0 0 -15 18 -17 -.21 5 5 | 7776 -35 20 93
jpl 80| 1 1 1 30 -6 -1 .05 17 17 | 5357 -561 23 175
mit 297| 0 -2 0 -30 -23 -32 -.11 10 9 | -36 299 30 292
ngs 231| -3 -2 -4 -129 19 -20 .08 14 12 | -1071 183 1688 3997
Table 2.1780.4 GPS week: 1780 Day: 4 MJD: 56708.000
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 2 1 -1 -4 -1 .11 10 10 | -1237 390 17 119
emr 80| -1 -4 2 2 2 -6 .06 18 18 | 5911 -1529 18 89
esa 150| 1 0 0 29 0 11 -.20 6 6 | -1974 -1248 10 86
gfz 191| -1 0 -5 21 -2 -9 .15 10 9 | -425 -88 14 116
grg 183| 3 1 2 -46 -22 -39 .23 16 14 | -178 192 21 148
igr n/a| 0 0 0 -2 0 -2 -.17 5 5 | 6799 -1239 18 76
jpl 80| 0 2 0 -34 9 0 .04 17 17 | 3969 -1640 21 142
mit 300| -1 -3 -1 -24 0 -28 -.14 13 12 | -306 370 44 181
ngs 231| -2 0 4 -30 24 43 .02 13 12 | -1117 177 1752 3159
Table 2.1780.5 GPS week: 1780 Day: 5 MJD: 56709.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 247| -1 1 2 30 41 -4 .10 11 10 | -980 151 19 136
emr 80| -1 -4 1 -9 2 -10 .08 17 17 | 4252 -1606 16 104
esa 150| 1 1 2 18 -34 5 -.20 6 6 | -2259 -729 9 92
gfz 194| 0 -2 -6 37 -11 -11 .15 10 10 | 459 -1246 15 128
grg 187| 4 3 1 -33 -5 2 .24 18 15 | -67 -10 19 152
igr n/a| 0 0 0 -1 19 1 -.17 5 5 | 5588 -1224 17 77
jpl 80| 0 -1 -1 4 41 10 .10 17 17 | 2387 -1759 19 149
mit 300| -1 -3 0 -27 -7 -18 -.13 13 11 | -31 -150 45 188
ngs 233| 0 0 -1 -79 11 17 -.03 12 10 | -908 86 1922 3353
Table 2.1780.6 GPS week: 1780 Day: 6 MJD: 56710.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 244| 0 1 6 -18 10 -15 .13 12 11 | -956 -250 19 154
emr 79| -8 2 0 -5 12 5 .15 20 20 | 2901 -366 19 144
esa 150| 1 0 0 15 -28 31 -.20 6 6 | -205 -1023 13 197
gfz 193| 1 -1 -7 51 -5 -37 .14 10 11 | -746 110 16 176
grg 185| 5 1 5 -45 12 -17 .24 18 17 | -144 -443 19 166
igr n/a| 0 0 -2 8 25 -5 -.18 5 5 | 4520 374 22 141
jpl 80| 1 -1 -1 -3 25 11 .07 19 18 | 834 -277 20 166
mit 300| 1 -1 -3 -2 -4 -10 -.13 14 13 | -52 -121 79 495
ngs 232| -1 0 0 -51 15 4 .03 13 11 | -861 -369 1864 3934
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 3.1780.0 GPS week: 1780 Day: 0 MJD: 56704.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs IGS | cod emr esa gfz grg igr jpl mit ngs IGS
------+---------------------------------------------------+----------------------------------------------------
X1E | 9 18 7 10 14 5 --- 15 8 4 | 101 108 108 107 109 105 --- 100 100 106
2E | 12 20 7 9 19 5 18 13 11 5 | 27 22 24 27 20 22 22 24 25 22
3 | 9 11 4 7 14 6 11 7 10 3 | 24 26 22 25 31 24 22 26 25 24
4E | 17 18 8 15 17 8 16 12 23 5 | 112 116 105 110 119 108 116 115 113 111
5 | 14 21 6 11 11 5 19 11 8 4 | 52 57 47 47 50 47 55 47 47 49
6 | 9 12 5 9 12 6 12 7 9 3 | 21 26 19 23 27 18 19 21 18 20
7E | 10 17 7 9 12 5 17 10 12 4 | 27 25 21 29 29 21 24 21 26 22
8E | 15 20 10 14 14 7 21 18 17 5 | 63 72 68 61 70 67 71 68 64 66
9E | 17 23 9 19 13 7 17 11 11 5 | 63 74 60 58 65 58 68 57 61 61
10 | 9 16 6 9 11 4 9 9 14 3 | 27 22 33 35 32 27 25 33 25 29
11E | 12 11 7 9 13 6 15 10 11 4 | 26 25 21 28 32 21 26 21 23 23
12 | 8 21 6 15 17 7 21 13 16 5 | 27 26 20 31 31 19 24 27 25 22
13 | 9 17 4 10 14 4 17 13 11 4 | 39 42 38 45 46 36 41 40 36 39
14 | 6 18 6 8 14 4 18 9 13 4 | 45 42 45 52 50 45 44 50 49 46
15 | 10 22 7 11 13 5 21 9 11 4 | 38 40 37 45 43 39 40 37 39 38
16 | 9 17 7 11 13 5 23 8 13 4 | 11 19 10 13 11 13 21 8 14 13
17 | 10 19 6 15 13 3 21 15 8 4 | 28 30 30 38 36 26 27 26 29 28
18 | 10 21 7 18 15 3 19 9 18 5 | 35 29 34 48 41 32 30 35 35 34
19 | 6 16 6 9 14 6 19 11 14 4 | 20 27 19 25 28 21 22 23 23 20
20 | 9 18 6 13 8 3 18 9 11 4 | 34 34 39 47 39 38 34 40 34 37
21E | 9 13 5 8 15 4 13 8 14 4 | 21 20 20 27 21 19 20 16 22 19
22 | 7 18 6 9 12 4 19 10 10 4 | 43 39 44 52 51 44 40 48 45 44
23 | 9 16 6 13 11 4 15 8 10 4 | 34 34 34 42 36 32 31 30 29 33
24E | 7 13 7 12 17 4 14 17 16 4 | 24 23 22 28 31 18 25 20 23 21
25 | 8 18 5 7 11 4 15 13 10 4 | 21 27 18 21 28 17 28 20 20 19
26 | 8 15 7 9 7 5 18 12 9 4 | 28 28 33 37 31 27 27 29 29 29
X27 | 10 15 7 12 --- 6 13 11 13 4 | 28 30 22 28 --- 22 32 23 32 25
28 | 12 17 6 9 11 5 16 12 13 4 | 25 33 27 27 33 24 27 28 25 26
29 | 8 16 5 8 12 4 17 16 14 4 | 24 26 21 27 26 21 27 22 31 22
31E | 11 16 6 8 14 4 21 15 18 5 | 32 30 31 34 33 30 28 28 43 30
32 | 9 10 4 10 11 5 11 12 12 3 | 18 20 20 30 26 19 22 23 25 20
------+---------------------------------------------------+----------------------------------------------------
RMS | 10 17 6 11 13 5 17 12 13 |T 36 37 35 40 40 34 34 35 36 35
WRMS | 9 17 6 10 13 5 17 11 11 |NE 29 31 29 35 34 28 30 30 30 29
MEDI | 9 17 6 10 13 5 17 11 12 |MD 28 29 30 34 32 26 27 28 29 28
Table 3.1780.1 GPS week: 1780 Day: 1 MJD: 56705.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs IGS | cod emr esa gfz grg igr jpl mit ngs IGS
------+---------------------------------------------------+----------------------------------------------------
X1E | 13 22 8 10 17 4 --- 12 16 5 | 80 86 84 84 84 83 --- 80 87 84
2E | 11 18 6 10 12 6 18 18 13 4 | 25 22 22 26 17 17 19 26 22 21
3 | 11 12 5 9 22 5 11 12 14 4 | 25 31 24 28 30 22 27 28 25 26
4E | 19 17 8 14 20 7 17 21 22 6 | 121 126 119 125 130 120 126 131 123 124
5 | 14 23 8 10 11 6 20 15 11 5 | 41 42 31 40 38 32 35 38 35 36
6 | 11 12 5 10 19 4 14 9 14 4 | 22 27 19 23 22 19 21 23 24 21
7E | 9 17 6 12 17 4 17 13 12 4 | 26 28 21 31 22 20 24 26 29 24
8E | 18 19 7 13 17 5 21 18 12 5 | 78 80 79 78 81 78 77 79 77 78
9E | 13 20 7 15 16 6 17 16 10 5 | 59 65 53 58 58 54 62 53 56 57
10 | 11 15 5 11 15 3 13 11 10 4 | 28 26 29 33 31 25 22 29 27 28
11E | 9 9 3 10 17 3 13 12 16 4 | 25 26 19 25 27 19 25 25 28 22
12 | 9 17 7 11 18 4 19 11 15 4 | 26 27 18 26 31 18 25 25 23 21
13 | 9 16 7 9 14 5 15 9 9 4 | 29 36 28 33 38 26 33 30 30 30
14 | 6 15 5 8 13 5 16 11 12 4 | 36 38 37 40 37 36 35 40 37 37
15 | 9 21 7 12 14 4 17 10 15 4 | 32 37 33 39 36 30 35 29 33 33
16 | 15 18 6 8 18 4 19 10 17 5 | 23 22 13 14 10 11 21 10 14 13
17 | 10 17 7 12 16 4 21 9 11 4 | 23 30 21 31 35 21 28 24 24 24
18 | 10 19 6 17 13 3 18 11 14 5 | 26 28 26 38 25 24 25 26 20 25
19 | 8 14 5 8 21 4 18 12 15 4 | 24 31 20 27 31 21 28 26 20 22
20 | 13 18 8 12 13 4 18 12 13 4 | 28 33 27 33 30 27 29 31 30 28
21E | 8 13 5 11 22 6 14 5 11 4 | 21 22 17 22 31 15 16 18 16 18
22 | 12 17 7 10 14 4 19 12 12 4 | 31 34 31 35 33 30 28 31 27 30
23 | 10 15 5 11 13 4 15 7 12 4 | 28 29 26 33 28 25 27 27 29 27
24E | 8 16 7 10 15 4 12 16 14 4 | 24 26 21 30 29 19 26 21 24 22
25 | 6 16 4 7 14 4 15 9 16 4 | 21 29 19 25 26 18 30 20 22 21
26 | 7 17 7 9 13 6 11 12 11 4 | 22 27 25 31 27 21 26 24 26 25
X27 | 10 16 7 12 --- 5 14 13 14 4 | 30 34 23 29 --- 23 33 25 31 26
28 | 13 20 5 10 18 6 12 11 9 4 | 29 33 26 27 36 26 33 27 26 26
29 | 9 17 6 12 14 7 23 11 15 4 | 28 34 27 33 31 26 35 28 32 28
31E | 7 20 6 9 17 3 21 12 18 5 | 32 37 29 31 33 28 28 30 41 30
32 | 11 8 4 7 18 6 9 9 15 3 | 22 23 19 20 20 17 21 20 25 19
------+---------------------------------------------------+----------------------------------------------------
RMS | 11 17 6 11 16 5 17 12 14 |T 34 37 31 37 36 30 33 33 34 33
WRMS | 10 17 6 10 15 5 17 11 12 |NE 27 31 24 30 29 23 28 26 26 26
MEDI | 10 17 6 10 16 4 17 12 14 |MD 28 31 26 31 31 24 28 27 27 26
Table 3.1780.2 GPS week: 1780 Day: 2 MJD: 56706.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs IGS | cod emr esa gfz grg igr jpl mit ngs IGS
------+---------------------------------------------------+----------------------------------------------------
X1E | 11 24 9 11 13 8 --- 15 12 5 | 89 94 86 86 88 90 --- 86 89 87
2E | 14 18 6 9 18 3 18 17 12 5 | 26 21 24 22 20 19 19 22 25 20
3 | 11 12 5 10 20 4 9 12 16 4 | 25 26 21 24 24 21 25 26 26 22
4E | 24 19 11 22 21 7 17 13 25 7 | 116 126 112 116 124 114 124 125 117 117
5 | 14 20 6 11 15 4 18 14 13 5 | 40 45 37 34 40 34 41 33 39 37
6 | 10 14 5 10 20 4 11 12 15 4 | 24 25 21 23 20 20 23 21 27 21
7E | 11 13 6 10 17 6 18 15 9 4 | 28 28 22 25 29 21 27 28 27 25
8E | 19 21 10 12 15 7 21 16 13 5 | 50 44 46 46 42 44 46 48 46 45
9E | 18 23 9 18 15 7 18 14 12 5 | 46 54 37 41 42 35 49 35 41 40
10 | 11 13 7 13 17 4 9 13 8 4 | 26 27 31 32 31 28 25 29 27 28
11E | 9 13 3 10 17 5 13 15 13 4 | 28 27 22 27 29 20 24 25 27 24
12 | 11 17 7 11 20 5 19 10 8 4 | 35 35 29 34 37 28 32 32 32 31
13 | 11 16 6 9 14 6 18 8 10 4 | 32 37 32 34 36 31 33 32 35 32
14 | 18 16 5 14 14 6 14 8 12 4 | 38 43 42 50 42 40 40 40 37 40
15 | 11 22 8 11 11 6 22 13 13 5 | 30 36 32 36 34 32 36 31 33 31
X16 | 2 --- --- --- --- 33 --- --- --- 0 | 45 --- --- --- --- 66 --- --- --- 40
17 | 13 17 11 13 16 4 16 12 11 5 | 23 29 25 29 38 24 29 26 30 26
18 | 11 20 7 16 13 3 16 10 10 4 | 28 34 32 40 33 28 27 32 29 31
19 | 8 15 5 10 16 5 17 13 12 4 | 25 31 25 28 30 23 29 25 25 25
20 | 18 19 7 14 11 7 19 13 15 5 | 36 40 40 44 37 38 34 36 34 36
21E | 7 15 7 11 11 3 13 6 10 3 | 22 23 21 27 21 19 20 18 27 21
22 | 11 18 7 11 13 5 19 13 13 4 | 36 39 42 47 43 38 36 40 41 40
23 | 9 16 7 11 9 6 15 7 12 4 | 31 35 33 36 33 31 30 30 30 31
24E | 11 16 7 8 16 6 14 12 10 4 | 27 28 25 30 34 26 28 27 30 26
25 | 11 15 4 10 13 6 16 9 14 4 | 26 34 24 29 29 24 34 26 26 26
26 | 10 14 8 9 12 5 16 10 11 4 | 26 28 29 30 28 26 25 26 27 27
X27 | 12 16 7 10 --- 6 14 13 17 5 | 36 37 31 33 --- 29 37 29 38 33
28 | 12 17 7 9 13 7 15 12 14 4 | 30 36 33 33 42 30 34 38 31 33
29 | 11 15 6 9 14 4 20 11 11 4 | 35 40 34 36 35 32 41 37 39 35
31E | 8 16 6 8 12 5 20 12 15 4 | 34 33 30 33 32 26 26 27 34 29
32 | 10 10 5 9 13 5 11 9 13 3 | 26 26 25 28 24 23 26 24 27 24
------+---------------------------------------------------+----------------------------------------------------
RMS | 13 17 7 12 15 5 16 12 13 |T 36 38 34 37 37 34 34 35 36 34
WRMS | 12 17 7 11 14 5 16 12 12 |NE 31 34 30 34 33 30 31 30 31 30
MEDI | 11 16 7 10 14 5 16 12 12 |MD 30 34 31 33 34 28 30 29 30 31
Table 3.1780.3 GPS week: 1780 Day: 3 MJD: 56707.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs IGS | cod emr esa gfz grg igr jpl mit ngs IGS
------+---------------------------------------------------+----------------------------------------------------
X1E | 10 13 5 11 12 4 --- 13 15 4 | 92 96 94 98 96 96 --- 95 98 96
2E | 9 19 5 11 23 3 17 12 15 4 | 26 21 21 28 24 20 22 22 32 22
3 | 6 14 4 7 12 6 12 7 14 3 | 23 24 19 22 24 19 24 21 24 20
4E | 15 20 7 11 16 7 16 15 19 5 | 109 118 106 111 116 109 113 114 117 111
5 | 7 22 5 11 11 4 21 10 12 4 | 42 46 35 41 36 37 43 39 41 38
6 | 5 17 4 7 10 4 11 8 14 3 | 22 23 16 20 23 15 19 18 22 17
7E | 7 16 6 8 15 5 21 6 13 4 | 25 27 19 23 24 19 24 20 26 20
8E | 10 22 8 14 13 4 18 14 16 5 | 96 93 95 98 88 96 93 97 94 94
9E | 8 20 6 13 14 7 19 11 11 4 | 56 62 53 57 56 52 59 53 56 54
10 | 6 18 5 13 14 5 10 10 15 4 | 25 20 28 32 32 26 22 31 32 27
11E | 7 12 5 8 10 5 15 10 16 3 | 25 27 23 27 28 22 23 25 32 23
12 | 11 20 5 12 18 4 16 9 11 4 | 31 30 24 33 34 24 27 26 30 27
13 | 8 16 4 7 15 2 17 7 14 3 | 29 35 32 34 38 31 38 31 35 31
14 | 16 15 6 11 18 5 15 9 12 4 | 45 45 45 50 46 43 45 46 45 44
15 | 12 24 6 10 15 7 18 14 16 5 | 42 43 40 46 45 41 41 41 44 40
X16 | 12 --- --- 9 13 9 --- 7 16 5 | 24 --- --- 19 22 16 --- 15 24 18
17 | 12 18 9 16 30 3 18 7 15 5 | 21 25 24 31 41 18 23 21 22 21
18 | 8 20 8 15 16 4 20 9 9 4 | 32 27 29 39 29 28 26 29 31 29
19 | 9 16 5 9 12 5 21 9 11 4 | 26 32 24 26 29 24 28 24 31 24
20 | 13 17 6 8 13 5 17 10 10 4 | 34 31 34 39 33 34 31 36 41 33
21E | 6 22 5 13 44 3 27 6 13 6 | 21 26 16 20 48 15 23 15 14 17
22 | 8 19 5 10 14 4 18 8 8 4 | 42 38 40 47 40 40 36 41 40 40
23 | 9 16 6 10 14 5 17 7 11 3 | 26 31 27 34 30 27 28 27 31 27
24E | 10 18 6 10 14 6 12 22 15 5 | 26 31 21 28 30 22 27 21 29 23
25 | 8 14 5 7 12 6 14 7 11 3 | 24 25 20 26 31 20 30 22 23 22
26 | 7 16 5 11 10 7 14 9 13 3 | 23 22 27 33 30 25 24 27 25 25
X27 | 5 16 7 7 --- 4 13 9 18 4 | 28 35 26 29 --- 27 33 26 40 28
28 | 10 24 7 9 16 5 16 9 11 4 | 36 41 32 33 36 32 34 32 30 32
29 | 10 18 5 12 12 5 19 9 11 4 | 29 32 24 29 31 26 30 25 35 26
31E | 8 18 6 10 15 6 20 11 17 4 | 32 34 30 33 35 28 32 32 39 31
32 | 7 8 4 9 12 4 11 6 18 3 | 17 19 17 24 21 16 20 18 22 17
------+---------------------------------------------------+----------------------------------------------------
RMS | 9 18 6 11 17 5 17 10 13 |T 36 38 34 39 39 33 35 35 38 34
WRMS | 9 18 6 11 15 5 17 9 12 |NE 29 31 28 32 32 27 30 28 31 27
MEDI | 8 18 5 10 14 5 17 9 14 |MD 28 31 27 33 32 26 28 27 32 27
Table 3.1780.4 GPS week: 1780 Day: 4 MJD: 56708.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs IGS | cod emr esa gfz grg igr jpl mit ngs IGS
------+---------------------------------------------------+----------------------------------------------------
X1E | 15 14 7 9 13 9 --- 13 13 4 | 103 105 105 103 105 103 --- 104 98 105
2E | 10 20 6 9 22 3 18 17 14 5 | 22 18 22 24 19 18 18 23 25 19
3 | 6 14 5 8 15 5 13 8 14 3 | 24 25 21 23 27 20 23 23 26 22
4E | 15 23 9 10 15 7 15 19 16 5 | 95 104 93 99 99 92 99 104 94 96
5 | 7 20 6 11 12 3 17 13 15 4 | 28 37 29 31 32 28 38 29 33 29
6 | 7 14 4 7 15 4 12 8 12 3 | 20 24 17 21 21 17 22 18 25 18
7E | 7 17 5 8 18 5 17 9 12 4 | 28 30 22 28 30 22 29 27 25 24
8E | 12 16 9 13 14 8 17 15 18 5 | 75 73 74 69 72 72 71 72 75 72
9E | 8 19 7 12 15 6 17 12 10 4 | 38 47 34 36 45 33 46 32 34 36
10 | 10 18 7 7 12 6 14 10 13 4 | 25 23 28 28 28 24 29 27 24 24
11E | 8 13 7 9 16 4 15 10 16 4 | 22 24 20 26 27 20 25 24 27 21
12 | 12 19 6 12 21 4 17 17 12 5 | 31 29 25 31 34 23 27 26 30 25
13 | 7 17 5 10 14 5 16 11 11 4 | 25 34 26 32 35 24 31 27 22 26
14 | 12 13 7 9 14 6 15 10 12 4 | 37 35 30 41 31 32 35 33 31 32
15 | 9 22 6 12 13 8 19 20 11 5 | 30 34 29 34 33 30 32 33 28 29
16 | 17 22 6 10 18 4 23 10 10 5 | 28 25 12 21 22 18 24 16 18 18
17 | 11 21 7 13 15 5 22 8 11 4 | 24 26 22 33 30 21 25 24 25 22
18 | 7 20 7 13 16 4 17 9 14 4 | 27 29 26 32 27 24 27 28 22 25
19 | 9 18 7 9 14 4 18 8 13 4 | 20 22 15 20 23 15 22 18 20 16
20 | 11 23 6 9 13 5 18 9 12 4 | 30 30 30 33 31 29 31 32 29 28
21E | 7 19 5 10 28 4 16 12 10 5 | 19 24 16 21 32 14 18 18 17 16
22 | 7 17 5 9 12 4 18 9 11 4 | 35 29 35 42 35 35 35 37 31 34
23 | 11 16 6 12 12 6 16 12 10 4 | 23 30 24 34 28 25 28 27 24 25
24E | 7 14 6 8 13 4 13 23 12 4 | 26 24 24 28 25 21 27 28 27 23
25 | 11 15 4 6 17 6 13 13 12 4 | 21 26 18 21 29 16 27 19 21 19
26 | 7 15 7 9 13 4 14 14 15 4 | 23 17 20 26 25 19 23 21 19 20
X27 | 10 14 6 7 --- 4 13 10 16 4 | 27 30 24 26 --- 22 32 21 28 25
28 | 9 28 6 10 17 4 19 11 13 5 | 22 32 24 25 29 22 28 26 23 22
29 | 9 16 6 11 16 7 18 11 16 4 | 29 28 21 26 26 21 26 23 27 23
31E | 10 20 6 10 16 4 23 10 13 4 | 27 31 19 27 32 19 25 23 27 22
32 | 5 11 3 7 15 3 11 7 12 3 | 20 21 19 24 21 19 23 24 25 20
------+---------------------------------------------------+----------------------------------------------------
RMS | 10 18 6 10 16 5 17 13 13 |T 32 34 29 34 35 28 31 31 31 30
WRMS | 10 18 6 9 14 5 17 12 12 |NE 26 27 23 28 28 23 28 25 25 23
MEDI | 9 17 6 9 15 4 17 11 12 |MD 27 29 24 28 29 22 27 26 26 24
Table 3.1780.5 GPS week: 1780 Day: 5 MJD: 56709.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs IGS | cod emr esa gfz grg igr jpl mit ngs IGS
------+---------------------------------------------------+----------------------------------------------------
X1E | 7 16 6 8 8 9 --- 17 19 4 | 142 142 144 144 147 141 --- 141 141 143
2E | 14 18 6 8 22 3 20 27 10 5 | 23 22 16 19 21 15 16 26 23 17
3 | 6 12 7 7 22 3 11 9 12 4 | 21 24 20 21 27 17 24 21 19 20
4E | 17 23 8 12 12 4 16 15 15 5 | 92 102 89 95 94 88 95 97 91 92
5 | 7 22 5 9 13 4 17 13 11 4 | 25 33 23 24 26 21 29 22 26 23
6 | 9 14 4 9 25 4 14 12 17 4 | 19 24 15 17 25 15 21 20 20 16
7E | 8 16 7 6 15 3 17 9 12 4 | 22 23 14 22 24 15 21 21 23 17
8E | 20 20 12 14 21 10 22 17 24 6 | 127 128 128 126 123 125 125 127 125 126
9E | 13 19 6 10 18 6 18 14 9 4 | 53 58 47 52 50 48 54 47 50 50
10 | 12 15 6 11 15 3 11 12 9 4 | 18 20 19 25 21 19 20 21 22 19
11E | 6 13 3 8 14 3 12 12 14 3 | 20 25 16 22 27 17 22 23 23 19
12 | 11 18 6 12 20 3 20 10 11 4 | 26 28 23 30 34 22 30 23 29 24
13 | 9 16 4 9 13 4 16 10 8 3 | 24 32 22 28 32 23 31 25 25 24
14 | 11 14 4 12 11 5 14 13 11 4 | 30 33 29 38 33 30 29 36 29 31
15 | 18 21 6 9 16 6 21 15 10 5 | 28 31 23 28 29 27 29 29 25 24
16 | 6 19 5 8 19 3 21 10 8 4 | 22 21 10 19 24 14 24 15 17 17
17 | 11 16 9 14 17 4 18 11 12 4 | 20 25 19 27 31 17 24 21 21 20
18 | 10 20 7 16 14 4 19 9 13 5 | 19 22 19 29 22 17 20 20 13 18
19 | 8 16 7 8 19 3 17 8 14 4 | 23 29 22 26 33 22 29 23 25 22
20 | 12 18 5 11 14 4 18 10 12 4 | 24 27 22 28 25 21 25 25 24 22
21E | 9 16 6 10 32 6 14 9 11 5 | 16 18 12 18 30 11 12 11 19 12
22 | 8 16 7 12 13 3 17 11 16 4 | 24 24 26 31 27 24 22 28 18 23
23 | 9 15 5 12 12 5 14 7 8 3 | 23 26 18 27 23 21 25 20 21 20
24E | 12 17 7 11 15 3 17 19 11 5 | 27 25 23 27 27 20 27 26 29 23
25 | 9 16 5 8 15 5 15 11 13 4 | 20 26 18 22 28 16 28 18 23 19
26 | 7 15 6 8 19 7 11 12 8 3 | 17 20 18 23 25 17 23 21 22 19
X27 | 7 13 5 10 --- 4 15 10 11 4 | 29 29 22 26 --- 23 34 22 25 24
28 | 12 19 6 7 18 8 17 13 14 4 | 24 30 24 26 36 22 32 32 27 25
29 | 10 18 5 12 18 5 19 11 9 4 | 26 29 22 29 30 23 30 26 27 24
31E | 9 18 6 10 16 4 19 12 12 4 | 23 28 16 28 30 18 24 23 28 21
32 | 7 14 5 8 20 7 9 10 11 3 | 21 24 18 21 23 19 23 24 21 19
------+---------------------------------------------------+----------------------------------------------------
RMS | 11 17 6 10 18 5 17 13 12 |T 33 36 30 35 37 29 31 33 33 31
WRMS | 10 17 6 10 15 5 17 11 10 |NE 23 26 20 25 27 20 26 23 22 21
MEDI | 9 16 6 10 16 4 17 11 11 |MD 23 26 22 27 27 21 25 23 24 22
Table 3.1780.6 GPS week: 1780 Day: 6 MJD: 56710.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs IGS | cod emr esa gfz grg igr jpl mit ngs IGS
------+---------------------------------------------------+----------------------------------------------------
X1E | 134 27 21 34 54 15 --- 33 201 15 | 398 446 445 435 438 441 --- 436 390 440
2E | 10 16 4 8 21 5 22 14 12 4 | 24 25 21 25 19 20 24 25 28 22
3 | 7 14 6 7 23 3 14 15 11 4 | 31 25 27 26 36 24 25 27 24 26
4E | 15 29 11 12 13 5 19 16 15 6 | 102 114 99 106 105 99 104 107 102 103
5 | 15 22 7 9 15 5 17 15 10 4 | 37 39 28 27 33 28 37 27 34 29
6 | 10 10 6 11 26 6 12 16 16 5 | 27 23 21 22 36 18 19 21 22 20
7E | 9 19 5 9 16 5 19 11 13 4 | 24 31 18 21 23 16 21 22 22 19
8E | 17 28 10 9 20 4 22 16 23 6 | 102 100 102 101 99 102 95 105 104 101
9E | 12 22 8 12 21 4 21 12 11 5 | 52 61 49 51 56 49 53 48 48 50
10 | 17 10 5 8 15 5 9 13 15 4 | 27 18 26 29 30 22 22 27 23 24
11E | 14 17 6 11 17 5 17 17 13 5 | 30 32 22 24 26 21 24 26 25 23
12 | 9 26 6 11 19 6 22 9 9 4 | 33 34 27 33 38 26 28 29 29 28
13 | 12 18 4 11 14 2 18 11 13 4 | 26 39 28 35 39 28 35 30 26 29
14 | 23 18 6 14 16 5 19 15 15 5 | 37 35 37 47 39 35 29 39 34 35
15 | 11 26 6 10 18 6 22 16 9 5 | 29 36 33 40 40 34 36 35 35 32
16 | 9 19 5 9 20 4 25 13 11 4 | 20 28 13 21 28 18 25 15 21 19
17 | 12 24 7 14 15 5 17 14 16 5 | 25 30 21 32 30 19 22 25 25 22
18 | 9 19 6 11 16 5 23 11 10 4 | 27 28 29 38 34 27 23 30 28 28
19 | 9 19 8 9 17 3 24 14 13 5 | 28 30 24 24 35 20 25 20 23 23
20 | 11 20 6 13 15 5 18 17 14 5 | 29 35 34 44 33 34 34 40 33 33
21E | 7 16 4 8 20 6 20 12 10 4 | 19 21 16 21 19 13 17 14 19 15
22 | 12 18 6 10 18 3 25 11 12 4 | 39 36 40 48 47 39 30 44 35 39
23 | 11 16 5 11 12 4 18 7 13 4 | 25 33 25 37 30 27 27 26 23 26
24E | 12 16 6 12 18 5 15 14 14 4 | 32 32 25 32 38 25 31 27 31 28
25 | 8 20 6 8 15 4 17 10 10 4 | 26 28 24 22 32 19 27 19 20 22
26 | 8 19 6 7 24 4 14 12 8 4 | 21 21 22 26 34 20 25 23 21 22
X27 | 19 13 9 12 --- 7 16 16 12 5 | 30 29 24 25 --- 22 31 23 29 24
28 | 12 19 7 9 20 10 17 15 8 4 | 28 29 26 28 38 23 31 34 26 26
29 | 8 20 5 10 18 4 22 9 6 4 | 27 33 22 26 30 23 32 24 29 25
31E | 9 23 8 10 18 5 22 18 15 5 | 22 30 19 26 28 18 22 26 27 20
32 | 14 14 6 14 24 5 12 19 15 5 | 27 30 22 32 34 23 24 33 25 24
------+---------------------------------------------------+----------------------------------------------------
RMS | 12 20 6 10 18 5 19 14 13 |T 45 49 44 48 51 43 32 46 43 44
WRMS | 11 20 6 11 17 5 18 13 11 |NE 28 30 26 31 34 25 27 28 26 26
MEDI | 11 19 6 10 18 5 18 14 13 |MD 28 31 25 29 34 23 27 27 27 26
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 4.1780 GPS week: 1780 MJD: 56704.0-56710.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 |U 5 4 14 |U 13 17 48 |U 8 7 16 |
emr | emr 2932 | 9 8 23 |U 18 23 53 | 14 10 28 |
esa | esa 2948 | 7 6 19 |U 16 22 54 | 11 8 20 |
gfz | gfz 2950 |U 7 6 19 |U 16 21 52 |U 13 9 19 |
grg | grg 2865 |U 9 8 23 |U 16 20 55 |U 16 9 29 |
igr | igr 2961 | 7 6 19 | 16 20 50 | 9 8 18 |
igs | igs 2906 | 8 7 23 | 18 22 58 | 9 8 18 |
jpl | jpl 2840 | 9 8 24 |U 18 23 59 |U 17 11 28 |
mit | mit 2962 | 8 7 25 |U 29 33 64 |U 19 16 29 |
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 5.1780.0 GPS week: 1780 Day: 0 MJD: 56704.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 4 14 | 12 13 44 | 8 8 15 |
emr | emr 2964 | 8 5 17 | 12 15 44 | 19 13 32 |
esa | esa 2976 | 7 6 16 | 12 12 46 | 14 9 24 |
gfz | gfz 2964 | 6 5 17 | 12 13 46 | 17 8 24 |
grg | grg 2880 | 6 4 14 | 12 14 47 | 22 10 30 |
igr | igr 2974 | 6 5 19 | 11 13 42 | 9 8 18 |
igs | igs 2927 | 6 5 17 | 12 13 48 | 10 12 18 |
jpl | jpl 2868 | 8 5 18 | 12 14 43 | 20 14 28 |
mit | mit 2976 | 6 5 17 | 12 12 48 | 13 9 25 |
Table 5.1780.1 GPS week: 1780 Day: 1 MJD: 56705.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 9 | 17 17 43 | 7 5 12 |
emr | emr 2937 | 8 7 18 | 19 22 49 | 11 10 31 |
esa | esa 2976 | 6 5 11 | 17 18 44 | 7 7 18 |
gfz | gfz 2964 | 6 4 12 | 17 18 45 | 11 7 16 |
grg | grg 2880 | 8 6 15 | 17 19 41 | 17 8 24 |
igr | igr 2976 | 7 5 12 | 17 18 43 | 8 7 14 |
igs | igs 2907 | 8 6 11 | 23 18 50 | 8 10 21 |
jpl | jpl 2868 | 9 7 17 | 18 25 61 | 15 12 30 |
mit | mit 2976 | 9 11 20 | 31 48 79 | 43 22 42 |
Table 5.1780.2 GPS week: 1780 Day: 2 MJD: 56706.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 3 4 12 | 18 30 61 | 9 10 15 |
emr | emr 2866 | 8 8 20 | 21 31 63 | 14 14 26 |
esa | esa 2880 | 4 4 12 | 19 31 65 | 13 12 21 |
gfz | gfz 2868 | 4 4 12 | 18 31 63 | 10 11 19 |
grg | grg 2781 | 8 9 19 | ---- ---- ---- | 14 11 40 |
igr | igr 2880 | 4 5 12 | 18 31 64 | 10 11 20 |
igs | igs 2824 | 7 8 23 | 18 31 67 | 9 11 18 |
jpl | jpl 2771 | 6 8 17 | 18 26 60 | 15 14 36 |
mit | mit 2880 | 4 4 12 | 20 24 59 | 20 14 26 |
Table 5.1780.3 GPS week: 1780 Day: 3 MJD: 56707.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 3 13 | 12 18 41 | 7 5 14 |
emr | emr 2868 | 7 9 20 | 17 22 52 | 18 9 45 |
esa | esa 2880 | 6 6 14 | 16 23 50 | 12 8 21 |
gfz | gfz 2964 | 5 6 11 | 14 22 45 | 12 9 18 |
grg | grg 2880 | 9 8 32 | 14 20 48 | 25 12 39 |
igr | igr 2975 | 6 5 14 | 15 19 38 | 8 6 16 |
igs | igs 2962 | 4 6 12 | 15 17 39 | 6 6 17 |
jpl | jpl 2772 | 12 9 28 | 18 31 75 | 16 8 42 |
mit | mit 2976 | 5 7 16 | 14 17 40 | 9 10 37 |
Table 5.1780.4 GPS week: 1780 Day: 4 MJD: 56708.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 5 18 | 13 7 57 | 8 5 22 |
emr | emr 2961 | 6 6 23 | 15 8 55 | 13 6 16 |
esa | esa 2976 | 5 5 18 | 14 7 60 | 12 7 18 |
gfz | gfz 2964 | 5 6 21 | 14 7 58 | 14 9 22 |
grg | grg 2880 | 6 6 16 | 14 8 69 | 13 8 24 |
igr | igr 2976 | 5 5 21 | 14 7 50 | 8 6 20 |
igs | igs 2950 | 10 9 38 | 17 7 71 | 14 7 21 |
jpl | jpl 2868 | 5 6 24 | 17 10 42 | 21 7 16 |
mit | mit 2976 | 11 7 39 | 85 69 124 | 20 30 24 |
Table 5.1780.5 GPS week: 1780 Day: 5 MJD: 56709.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 18 | 11 20 59 | 9 10 21 |
emr | emr 2964 | 8 8 21 | 11 22 56 | 9 10 21 |
esa | esa 2976 | 6 6 16 | 11 19 61 | 11 11 21 |
gfz | gfz 2965 | 6 6 19 | 11 18 61 | 15 10 22 |
grg | grg 2880 | 10 15 25 | 13 19 66 | 10 9 23 |
igr | igr 2976 | 6 6 16 | 11 16 63 | 10 10 20 |
igs | igs 2883 | 6 7 18 | 11 16 56 | 8 7 16 |
jpl | jpl 2868 | 9 10 22 | 15 18 73 | 13 13 27 |
mit | mit 2976 | 10 10 32 | 16 19 52 | 21 15 26 |
Table 5.1780.6 GPS week: 1780 Day: 6 MJD: 56710.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 4 14 | 11 13 34 | 7 5 16 |
emr | emr 2964 | 15 11 43 | 29 38 53 | 14 10 26 |
esa | esa 2976 | 15 9 43 | 26 42 54 | 9 6 17 |
gfz | gfz 2964 | 14 8 41 | 25 36 48 | 10 7 15 |
grg | grg 2880 | 15 11 42 | 27 39 58 | 13 7 22 |
igr | igr 2974 | 15 10 42 | 26 34 49 | 8 7 18 |
igs | igs 2889 | 15 9 45 | 31 51 79 | 8 6 16 |
jpl | jpl 2867 | 15 14 44 | 30 38 63 | 18 7 20 |
mit | mit 2976 | 14 9 40 | 26 45 47 | 11 9 24 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1780 GPS week: 1780 MJD: 56704.500-56710.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -7 6 -156 20 2 | 6 16
| 17 20 122 129 3 | 3
emr uuuuu | -11 3 87 60 15 | 44 49
| 20 21 75 64 5 | 7
esa uuuuu | 9 -12 47 -67 4 | 2 17
| 15 11 39 53 4 | 4
gfz uuuuu | -22 -43 -39 -199 -2 | 4 17
| 16 19 61 52 4 | 2
grg uuuuu | 29 37 -93 49 -2 | 14 21
| 36 21 79 154 4 | 3
igr xxxxx | 0 10 32 42 1 | -2 16
| 11 11 44 32 4 | 3
irf xxxxx | 18 8 1 -16 -2 | 0 16
| 7 10 25 36 2 | 2
jpl uuuuu | -13 -39 106 57 -1 | 21 29
| 42 36 144 80 9 | 3
mit uuuuu | 13 -6 -13 26 -1 | 16 23
| 20 33 51 133 3 | 2
ngs uuuuu | -8 85 63 198 -4 | 1 16
| 63 58 167 121 6 | 3
Table 7.1780.0 GPS week: 1780 Day: 0 MJD: 56704.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -7 -3 -78 72 2 | 5 13
emr uuuuu | -22 -25 208 -5 13 | 35 40
esa uuuuu | -14 -18 18 -124 -2 | 0 14
gfz uuuuu | -32 -44 18 -189 2 | 3 15
grg uuuuu | 13 18 1 -8 -1 | 12 17
igr xxxxx | -12 26 -30 -15 3 | -4 15
irf xxxxx | 5 -8 18 -37 -3 | 1 14
jpl uuuuu | -7 -37 -67 53 -10 | 18 26
mit uuuuu | -8 -54 19 65 -4 | 17 22
ngs uuuuu | 92 179 -75 296 1 | -1 15
Table 7.1780.1 GPS week: 1780 Day: 1 MJD: 56705.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 13 -30 93 6 | 3 12
emr uuuuu | -27 41 137 33 21 | 38 42
esa uuuuu | 20 -4 49 -88 2 | -2 14
gfz uuuuu | 2 -23 -63 -265 -2 | 1 14
grg uuuuu | 52 10 -32 166 -6 | 11 17
igr xxxxx | 0 22 4 46 0 | -5 15
irf xxxxx | 16 2 -1 -11 1 | -2 13
jpl uuuuu | 50 -107 29 94 -4 | 19 26
mit uuuuu | -14 -13 -21 59 3 | 14 19
ngs uuuuu | -116 86 -87 136 -10 | -2 15
Table 7.1780.2 GPS week: 1780 Day: 2 MJD: 56706.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -12 13 -378 -244 0 | 6 17
emr uuuuu | -7 -3 22 136 5 | 42 48
esa uuuuu | 25 -1 20 -123 5 | 0 17
gfz uuuuu | -29 -65 31 -221 -10 | 3 17
grg uuuuu | 3 27 -97 -14 1 | 14 21
igr xxxxx | -8 7 85 57 4 | -3 17
irf xxxxx | 23 10 -8 49 -3 | 0 16
jpl uuuuu | -4 -40 123 155 5 | 20 29
mit uuuuu | 34 -19 -23 203 1 | 16 23
ngs uuuuu | -46 95 318 325 1 | 1 17
Table 7.1780.3 GPS week: 1780 Day: 3 MJD: 56707.500
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 | -25 -19 -162 -53 1 | 7 18
emr uuuuu | -38 -8 122 -35 13 | 45 51
esa uuuuu | 15 -2 117 -93 4 | 1 18
gfz uuuuu | -38 -26 -155 -242 -3 | 4 17
grg uuuuu | 84 57 -180 324 -1 | 16 22
igr xxxxx | 5 1 75 17 3 | -1 18
irf xxxxx | 20 3 16 -4 -4 | 1 17
jpl uuuuu | 12 -48 81 90 -5 | 22 30
mit uuuuu | 2 -30 38 137 -4 | 17 24
ngs uuuuu | -4 131 67 161 2 | 3 17
Table 7.1780.4 GPS week: 1780 Day: 4 MJD: 56708.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 10 20 -122 50 6 | 5 18
emr uuuuu | -12 15 63 106 16 | 45 51
esa uuuuu | -10 -27 61 -34 10 | 0 19
gfz uuuuu | -20 -26 -27 -173 -2 | 2 18
grg uuuuu | 47 47 -111 4 -10 | 14 22
igr xxxxx | 18 4 40 73 0 | -3 19
irf xxxxx | 27 18 36 -8 0 | -1 18
jpl uuuuu | -20 9 99 75 -10 | 21 30
mit uuuuu | 27 4 49 10 1 | 15 23
ngs uuuuu | -8 12 -22 85 -6 | 1 18
Table 7.1780.5 GPS week: 1780 Day: 5 MJD: 56709.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -31 -14 -70 106 -2 | 6 19
emr uuuuu | 2 12 68 74 15 | 48 54
esa uuuuu | 12 -24 65 2 8 | 3 19
gfz uuuuu | -2 -43 -36 -106 -1 | 3 18
grg uuuuu | 24 35 -27 32 2 | 14 22
igr xxxxx | 5 14 -6 46 5 | -2 19
irf xxxxx | 18 20 -26 -39 -1 | -1 18
jpl uuuuu | -44 -11 75 33 15 | 20 30
mit uuuuu | 17 35 -66 -130 0 | 15 24
ngs uuuuu | 12 65 -33 42 -13 | 1 18
Table 7.1780.6 GPS week: 1780 Day: 6 MJD: 56710.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 7 35 -256 114 1 | 11 18
emr uuuuu | 23 -9 -12 112 19 | 57 60
esa uuuuu | 17 -10 1 -10 1 | 9 18
gfz uuuuu | -36 -72 -43 -195 -2 | 8 16
grg uuuuu | -23 66 -208 -160 -1 | 19 23
igr xxxxx | -11 -2 56 72 -7 | 4 14
irf xxxxx | 19 11 -31 -63 -4 | 4 15
jpl uuuuu | -82 -39 401 -103 -1 | 28 33
mit uuuuu | 34 36 -85 -164 -2 | 21 25
ngs uuuuu | 13 25 275 341 0 | 6 12
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