[IGSREPORT-22228] Wk 1762 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Nov 1 13:29:01 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1762 (Oct 13, 2013 - Oct 19, 2013)
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:
igs1762[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1762[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1762[0-6].cls IGS GPS clock combination summary report.
igs17627.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17627.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 | 10 BRAZ BRFT CHTI GLSV HERT HOB2 HRAO INVK MAC1 MAW1
0 | COD | NNOR REYK TOW2 TWTF BRAZ HERT NNOR REYK
0 | ESA | CHPI
0 | GFZ | HNLC ISPA
0 | GRG | HYDE IRKJ KELY HYDE IRKJ
0 | JPL | 10 32 CUSV
0 | MIT | 2 9 12 17 2 9 12 MDVJ TNML USNO BAKO MDVJ TNML
1 | COD | DGAR FAA1 KOUC MAW1 MOBS NNOR REYK SYDN WROC XMIS
1 | COD | KOUC MOBS NNOR WROC XMIS
1 | EMR | MCM4 OPMT
1 | GFZ | REUN
1 | GRG | KELY WILL BRFT FAA1 KELY KOUC MAW1 POLV WILL
1 | JPL | 24 26 32 MCM4
1 | MIT | 7 23 26 28 7 14 23 26 28 CAS1 DAV1 MDVJ
2 | COD | KOUC KOUC MAW1
2 | EMR | 32 5 10 12 25 32 HERS
2 | ESA | MBAR
2 | GFZ | 32 HNLC
2 | GRG | IRKJ LPGS POLV HYDE IRKJ KOUC LPGS NTUS PDEL
2 | JPL | 5 12 25 32
2 | MIT | 1 2 3 6 9 19 21 22 23 27 2 21 PDEL ALIC BAKO BRMU
2 | MIT | CRO1 HOB2 IRKT KOUR MAW1 MONP NNOR OPMT PDEL PRDS
2 | MIT | TIDB
3 | COD | 10 32 KOUC MOBS NNOR REYK WROC XMIS KOUC MOBS NNOR
3 | COD | REYK WROC XMIS
3 | EMR | OPMT
3 | ESA | 32 MATE NTUS MATE NTUS
3 | GFZ | IRKT MATE IRKT MATE
3 | GRG | 25 CRO1 IRKJ IRKT KELY KOUC ZAMB IRKJ KELY
3 | JPL | 10 32
3 | MIT | 4 19 22 25 2 4 18 19 22 25 IRKJ IRKJ USNO
4 | COD | 32 32 ALIC BAKO CAS1 CONZ HOB2 HRAO HYDE INVK KOUC
4 | COD | MAC1 MDVJ NNOR REUN SSIA TIDB WAB2 WILL XMIS INVK
4 | COD | KOUC XMIS
4 | ESA | 32 32
4 | GFZ | ALIC KOUC ALIC
4 | GRG | IRKJ IRKJ KOUC NRMD POL2 POLV
4 | JPL | 10 32 KOUC MCM4
4 | MIT | 4 12 TWTF TWTF
5 | COD | 32 32 ABPO ALIC CAS1 DARW DGAR HERT HOLB JOZ2 KARR
5 | COD | KOUC MAC1 MIZU MOBS NICO NNOR NRIL REYK SHAO TSKB
5 | COD | USN3 WAB2 WROC WSRT HERT JOZ2 KOUC MOBS REYK WROC
5 | EMR | USNO HERS MATE TSKB USNO
5 | ESA | 32 32
5 | GRG | IRKJ MATE NOVM IRKJ MATE NOVM NTUS PENC
5 | JPL | 10 32
5 | MIT | 20 NTUS
6 | COD | 32 32 CHTI HOB2 KOUC MAG0 BRAZ KOUC REYK
6 | EMR | 12 HERS
6 | ESA | 32 32
6 | GFZ | SYOG WILL SYOG
6 | GRG | BRAZ HYDE IRKJ KELY ABMF ALBH ALGO ALIC ARTU AUCK
6 | GRG | BAKE BARH BJFS BOGT BOR1 BRAZ BREW BRFT BRMU BRUX
6 | GRG | CAS1 CHTI CHUM CHUR COCO CONZ CRO1 DAEJ DARW DAV1
6 | GRG | DRAO DUBO DUM1 FAIR GLPS GLSV GODE GOLD GOPE GRAZ
6 | GRG | GUAT GUUG HARB HERT HLFX HNPT HOB2 HOFN HOLB HRAO
6 | GRG | HYDE IISC INVK IRKJ IRKT ISPA JOZ2 JPLM KARR KELY
6 | GRG | KERG KIRU KOKB KOUC KOUR LAMA LPGS MAC1 MAL2 MAR6
6 | GRG | MAS1 MATE MAW1 MBAR MCIL MCM4 MDO1 MDVJ MKEA MOBS
6 | GRG | MONP NANO NICO NKLG NNOR NOVM NRC1 NRIL NRMD NTUS
6 | GRG | NYA1 NYAL OHI2 ONSA PDEL PERT PIMO POL2 POLV QAQ1
6 | GRG | RABT REUN REYK SCH2 SCOR SFER SHAO SPT0 SSIA STJO
6 | GRG | SUTH SUWN SYOG THTI THU3 TIDB TIXI TLSE TNML TOW2
6 | GRG | TRO1 TWTF URUM USN3 VILL WHIT WILL WROC WSRT WTZR
6 | GRG | XMIS YEBE YELL ZAMB ZECK ZIMM
6 | JPL | 12 KOUC
6 | MIT | 2 4 9 10 22 26 2 4 9 10 18 22 26 HYDE POLV HYDE MDVJ
6 | MIT | WILL
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | GRG | ~02:53 | ~ -0.16 ns
0 | MIT | ~00:00 | ~ 0.07 ns
2 | MIT | ~23:55 | ~ 0.10 ns
3 | GRG | ~07:17 | ~ -0.15 ns
4 | GRG | ~19:08 | ~ 0.15 ns
4 | MIT | ~10:45 | ~ 0.12 ns
5 | GRG | ~13:58 | ~ 0.16 ns
5 | MIT | ~02:10 | ~ 0.02 ns
6 | GRG | ~10:55 | ~ -0.51 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 orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | EMR | 25
3 | GRG | 25
3 | JPL | 25
3 | MIT | 25
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G25 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.3 .1 -1.0 -63 27 18 .09
EMR | 0 | 3.2 9.9 8.1 -19 5 -22 .09
ESA | 0 | 5.6 5.9 -7.5 -13 -16 32 .02
GFZ | 0 | .0 .5 -.7 -22 -1 12 -.14
GRG | 0 | 6.4 1.8 -3.9 -8 -3 9 .41
JPL | 0 | 7.0 7.7 19.6 -56 3 1 .19
MIT | 0 | 4.3 3.3 4.7 -21 8 -29 .10
NGS | 0 | 4.2 .6 3.4 -10 -1 31 .41
SIO | 0 | 3.2 1.9 1.4 -6 -37 -83 -.05
COD | 1 | -.7 -.3 -.4 -57 32 -10 -.07
EMR | 1 | 1.5 11.7 6.4 -14 10 -21 -.05
ESA | 1 | -.3 8.8 -8.5 -2 -1 61 -.24
GFZ | 1 | .1 .4 -.6 -23 -6 5 -.24
GRG | 1 | -.3 -1.3 -6.5 -14 29 8 .23
JPL | 1 | 6.4 9.6 12.8 -71 12 -9 .20
MIT | 1 | -3.1 3.9 .7 -30 29 -6 -.02
NGS | 1 | -1.0 -8.6 8.6 -78 12 -9 .41
SIO | 1 | 4.7 2.0 -5.8 -19 -93 -126 -.16
COD | 2 | -.5 -.4 -1.1 -41 34 -27 .06
EMR | 2 | 1.1 11.1 1.7 -24 8 -29 -.25
ESA | 2 | 1.5 5.6 -12.2 -9 -2 46 -.26
GFZ | 2 | .1 .5 -1.3 -19 -12 9 -.07
GRG | 2 | 6.0 -2.6 -5.7 -13 18 -28 .36
JPL | 2 | 5.3 7.2 14.0 -80 -19 22 .21
MIT | 2 | 1.5 4.0 1.3 -25 25 9 .06
NGS | 2 | -2.5 -3.7 7.3 -47 18 -11 .24
SIO | 2 | .6 -.1 -15.1 -72 -88 -236 -.30
COD | 3 | -.4 .1 -.8 -43 31 14 -.04
EMR | 3 | 1.3 8.2 7.9 -18 3 -23 -.15
ESA | 3 | -.6 4.1 -16.0 -19 5 25 -.12
GFZ | 3 | .3 .9 -1.7 -14 -12 33 .20
GRG | 3 | 1.1 3.3 -11.0 -6 18 -22 .24
JPL | 3 | -.1 3.6 9.6 -72 84 -36 .05
MIT | 3 | 5.4 1.4 -1.1 -10 24 -29 .13
NGS | 3 | 3.1 -4.8 12.7 -83 0 18 .56
SIO | 3 | -1.9 5.3 -19.9 -9 -73 -153 -.19
COD | 4 | -.2 .3 -1.0 -38 47 0 -.03
EMR | 4 | -3.5 9.6 4.3 -20 16 -24 -.06
ESA | 4 | -1.4 -.1 -13.1 -1 5 18 -.02
GFZ | 4 | .2 1.1 -1.2 -20 -17 26 .22
GRG | 4 | 1.2 2.8 -12.3 -19 27 4 .16
JPL | 4 | 1.7 5.6 11.6 -79 -14 -2 .35
MIT | 4 | -2.4 5.2 -2.5 -28 9 -4 .16
NGS | 4 | -6.3 -6.9 8.5 -72 31 -45 .50
SIO | 4 | -3.4 4.9 -15.7 -63 -50 -392 .01
COD | 5 | .1 -.7 -.1 -53 11 25 .08
EMR | 5 | -2.1 10.6 4.6 -18 9 -21 .03
ESA | 5 | 3.9 6.3 -9.4 -12 2 34 -.08
GFZ | 5 | .0 1.1 -1.4 -9 -23 15 .24
GRG | 5 | 1.8 1.3 -6.4 -15 19 0 .49
JPL | 5 | .7 4.2 18.4 -84 37 -4 .47
MIT | 5 | -2.0 6.2 -1.8 -15 1 -3 .27
NGS | 5 | .3 -4.0 8.9 -48 5 -2 .35
SIO | 5 | -.9 4.0 -10.0 -42 -60 -293 .20
COD | 6 | .4 -.2 .5 -50 16 25 .12
EMR | 6 | 7.2 8.1 -.4 -17 15 -31 -.15
ESA | 6 | 5.2 6.4 -10.5 11 1 56 -.02
GFZ | 6 | .0 .6 -1.0 -22 -11 9 .17
GRG | 6 | 5.1 5.5 -9.5 -23 27 -14 .41
JPL | 6 | 11.6 7.5 8.2 -107 32 23 .58
MIT | 6 | 2.0 5.9 -3.1 -36 3 -16 .20
NGS | 6 | -.8 -6.4 9.7 -78 8 -21 .60
SIO | 6 | -.2 3.5 -17.9 -69 -77 -401 .04
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1762.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1762.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 2.1762.[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 3.1762.[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 5.1762.0-6). 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 1762 summary. (Oct 13, 2013 - Oct 19, 2013)
Table 1.1762.a GPS week: 1762 MJD: 56578.000-56584.000
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 259| 1 0 1 -13 26 8 .10 11 11 | -741 -149 20 126
| 0 0 1 14 17 17 .02 | 134 323
emr 79| 0 4 6 -6 -11 1 .03 16 15 | 1960 -335 22 147
| 0 1 0 13 8 14 .03 | 1098 727
esa 150| 1 0 0 11 5 0 -.21 6 5 | -1272 1274 10 121
| 0 0 0 10 15 17 .02 | 649 1152
gfz 196| -1 0 -3 1 -16 19 .08 10 9 | -31 -94 13 102
| 0 0 1 19 9 22 .03 | 400 762
grg 191| 1 0 -2 18 0 -13 .32 13 13 | -238 365 16 192
| 0 1 2 19 21 13 .05 | 613 1185
igr n/a| 0 0 0 -11 29 -12 -.37 5 4 | -5924 -252 16 92
| 0 0 0 16 14 5 .05 | 945 701
jpl 80| -2 0 1 -10 16 0 .15 15 14 | 1318 -309 19 134
| 0 1 1 15 26 11 .03 | 1212 661
mit 298| 0 -3 -4 -14 -10 -7 -.15 14 11 | -173 68 29 300
| 0 0 1 20 15 30 .03 | 218 322
ngs 241| 0 0 5 -18 -9 -21 .06 12 10 | -233908 726556 1661 3242
| 1 0 1 53 42 15 .06 | 398233 1241142
sio 456| -1 -1 4 -66 -63 -261 -.49 19 19 | --- --- --- ---
| 2 2 0 27 25 122 .06 | --- ---
Table 1.1762.b GPS week : 1762 MJD: 56578.000-56584.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 5 4 5 4 5 4 4 |
3 | 4 4 4 4 4 3 3 |
4 | 3 3 4 4 3 3 3 |
5 | 5 5 4 4 4 4 4 |
6 | 3 3 4 3 3 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 4 3 4 3 3 |
9 | 3 4 3 3 3 3 3 |
10 | 6 6 6 6 6 6 5 |
11 | 4 4 4 4 4 5 5 |
12 | 5 5 5 5 5 5 6 |
13 | 4 4 4 4 4 4 4 |
14 | 5 4 4 6 5 5 5 |
15 | 4 4 4 4 4 4 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 4 4 5 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 5 4 |
20 | 4 4 4 4 4 4 5 |
21 | 4 4 4 4 4 4 5 |
22 | 4 4 4 4 4 5 5 |
23 | 5 5 4 5 5 5 5 |
24 | 4 4 3 4 4 4 4 |
25 | 5 5 5 10 5 6 4 |
26 | 3 3 4 3 4 4 4 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 4 4 |
31 | 5 5 5 5 5 5 5 |
32 | 6 5 6 6 5 5 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 2.1762.0 GPS week: 1762 Day: 0 MJD: 56578.000
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| 1 -1 -1 -12 49 40 .11 13 13 | -682 -434 19 129
emr 80| -2 6 7 16 -27 16 .04 16 16 | 2862 -553 13 127
esa 150| 1 0 0 12 -19 -15 -.22 6 6 | -423 -720 10 140
gfz 195| -1 0 -5 13 -12 21 .02 10 10 | 308 -1621 14 105
grg 191| 1 0 1 36 16 -6 .35 11 11 | 19 -238 13 118
igr n/a| 0 0 0 -16 11 -8 -.34 4 4 | -5035 -589 15 89
jpl 80| -1 0 -1 12 0 0 .16 14 14 | 2598 -613 15 145
mit 300| 0 -4 -2 -3 -6 -18 -.18 13 11 | 9 -338 26 324
ngs 239| 0 0 3 -85 29 -8 -.02 11 9 | -705 -438 1699 3201
sio 454| 0 -4 5 -26 -8 -111 -.59 18 19 | --- --- --- ---
Table 2.1762.1 GPS week: 1762 Day: 1 MJD: 56579.000
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 260| 1 0 0 -21 15 -7 .11 11 10 | -687 -199 20 136
emr 80| 0 5 5 -8 -14 -7 .02 16 16 | 3347 -698 13 164
esa 150| 1 0 0 22 7 11 -.20 5 5 | -1977 2384 8 153
gfz 197| -2 1 -2 -20 -30 57 .09 10 9 | -609 314 12 103
grg 192| 2 2 -3 15 31 -10 .39 12 12 | 105 -206 16 365
igr n/a| 0 0 0 -4 10 -16 -.35 4 4 | -4691 -816 16 105
jpl 80| -2 0 2 -2 -26 -4 .12 14 13 | 2841 -893 16 154
mit 300| 0 -3 -4 -32 -12 -50 -.18 13 12 | 83 -193 25 334
ngs 243| -1 -1 5 4 14 -34 .04 12 10 | -694 -166 1713 3081
sio 461| 1 -4 4 -49 -79 -149 -.54 18 18 | --- --- --- ---
Table 2.1762.2 GPS week: 1762 Day: 2 MJD: 56580.000
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 262| 2 0 2 12 25 -1 .13 10 10 | -726 -387 22 143
emr 80| 0 4 4 -7 -5 8 .08 15 15 | 2677 475 41 154
esa 150| 1 0 0 -5 16 7 -.23 5 5 | -1765 2530 14 114
gfz 196| -2 2 -3 -14 -4 3 .08 10 9 | -411 692 16 119
grg 192| 2 1 -2 48 -3 -18 .38 11 11 | -144 511 25 362
igr n/a| -1 0 -1 -40 27 -18 -.45 5 4 | -5498 490 17 130
jpl 80| -2 -2 0 -34 17 -15 .17 15 14 | 1992 69 28 147
mit 300| 0 -3 -5 8 -31 -14 -.16 13 12 | -487 650 41 372
ngs 242| -2 0 4 -16 -28 -8 .02 12 9 | -826400 2572733 1991 3362
sio 464| 0 -3 4 -71 -89 -256 -.53 18 19 | --- --- --- ---
Table 2.1762.3 GPS week: 1762 Day: 3 MJD: 56581.000
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 262| 0 0 0 -35 22 10 .11 12 12 | -1025 242 19 117
emr 80| 0 4 7 -9 0 20 .01 21 16 | 2278 -1376 15 142
esa 150| 0 0 0 3 15 -2 -.21 6 6 | -1165 1323 10 123
gfz 199| -1 0 -5 -20 -26 43 .09 11 9 | 28 281 12 103
grg 191| 1 1 -6 22 -19 -19 .31 19 19 | 100 -220 15 124
igr n/a| 0 0 0 -3 35 -15 -.41 5 4 | -5781 -1126 17 81
jpl 80| -3 1 2 -8 58 19 .12 21 18 | 1183 -1099 16 117
mit 300| 0 -3 -4 -40 5 -34 -.18 22 10 | -11 -39 23 238
ngs 245| 0 0 6 59 -41 -31 .05 11 8 | -1080 518 1732 3389
sio 462| -1 -2 5 -50 -65 -177 -.48 18 19 | --- --- --- ---
Table 2.1762.4 GPS week: 1762 Day: 4 MJD: 56582.000
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 263| 1 0 3 -13 22 24 .08 11 11 | -699 145 18 117
emr 77| 0 4 6 -27 -13 1 .04 16 16 | 1019 -853 13 147
esa 150| 0 0 0 7 -8 -28 -.22 5 5 | -902 386 8 105
gfz 197| -2 0 -2 15 -9 9 .08 9 8 | 486 -432 11 94
grg 192| 0 0 -5 7 -31 11 .31 13 13 | 71 -274 13 126
igr n/a| 0 0 -1 12 51 -13 -.35 5 4 | -6846 -651 16 76
jpl 80| -1 0 3 -27 29 -3 .19 14 13 | 100 -556 14 123
mit 299| 0 -3 -5 8 -13 27 -.12 12 10 | -417 24 32 287
ngs 241| 0 0 3 -7 40 -2 .04 12 10 | -807214 2513731 1816 3295
sio 457| 0 0 4 -77 -64 -400 -.43 19 19 | --- --- --- ---
Table 2.1762.5 GPS week: 1762 Day: 5 MJD: 56583.000
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 260| 1 0 2 -8 48 -5 .09 10 9 | -766 142 19 123
emr 80| -1 3 6 4 -7 -15 .04 15 15 | 477 561 14 141
esa 150| 1 0 0 21 23 6 -.19 5 5 | -2014 1886 8 105
gfz 197| -1 0 -5 28 -11 1 .06 10 10 | -232 241 12 95
grg 191| 0 0 -1 7 -5 -25 .27 13 13 | -220 1 13 115
igr n/a| 0 0 0 -9 36 -2 -.37 4 4 | -7275 570 15 73
jpl 80| 0 1 0 -7 10 -8 .15 14 13 | -314 759 14 120
mit 295| -1 -3 -5 -12 -24 29 -.13 12 9 | -230 125 24 289
ngs 242| -1 1 5 -91 -80 -23 .12 13 10 | -737 141 1297 2975
sio 457| -3 0 3 -77 -68 -311 -.43 19 20 | --- --- --- ---
Table 2.1762.6 GPS week: 1762 Day: 6 MJD: 56584.000
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 263| 2 0 0 -13 0 0 .09 10 11 | -603 -552 25 118
emr 80| 0 1 6 -13 -12 -11 -.00 15 15 | 1062 94 48 154
esa 150| 1 0 0 17 4 21 -.20 5 5 | -660 1134 13 110
gfz 196| -2 1 -2 9 -17 1 .12 11 10 | 211 -135 20 95
grg 188| 0 -1 -2 -9 10 -24 .26 14 14 | -1600 2981 19 136
igr n/a| 0 0 0 -16 37 -11 -.32 5 5 | -6343 355 17 93
jpl 80| -2 0 1 -2 28 9 .16 14 14 | 829 165 31 132
mit 294| -1 -2 -5 -30 10 10 -.11 13 10 | -161 252 34 259
ngs 239| 0 0 6 8 -2 -42 .16 12 10 | -531 -625 1382 3395
sio 442| -4 1 3 -113 -67 -421 -.42 20 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 3.1762.0 GPS week: 1762 Day: 0 MJD: 56578.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 14 11 6 7 10 5 9 12 11 15 3 | 24 25 18 18 26 14 26 21 20 16 19
2 | 14 23 8 13 10 4 15 13 14 27 5 | 30 32 33 41 37 31 30 35 28 32 31
3 | 13 10 5 12 9 4 9 9 9 15 3 | 21 23 23 32 29 22 25 27 24 19 24
4 | 9 10 5 6 8 3 7 9 12 20 3 | 33 28 28 31 30 28 26 32 24 29 28
5E | 12 19 7 12 13 4 23 10 11 10 5 | 30 28 25 34 27 22 27 29 31 19 26
6 | 11 9 4 12 9 3 8 9 8 13 3 | 26 25 27 34 32 26 27 32 29 21 28
7 | 9 14 4 14 9 6 16 9 11 17 4 | 27 26 23 31 30 18 23 22 24 17 23
8 | 11 9 5 8 8 4 8 16 8 23 3 | 19 24 17 19 21 15 22 24 21 23 18
9 | 9 10 4 9 7 3 8 16 7 18 3 | 20 25 17 20 21 16 23 22 21 21 18
10E | 15 24 11 12 11 8 14 14 20 15 5 | 36 46 33 34 37 32 40 34 37 33 33
11 | 15 15 5 8 12 4 10 13 12 18 4 | 54 63 63 65 69 60 63 70 59 59 62
12 | 14 23 7 8 13 3 22 18 9 16 5 | 28 25 16 22 28 16 22 24 27 15 20
13 | 9 16 6 10 11 4 14 11 13 18 4 | 30 37 26 33 38 24 34 25 27 24 28
14 | 21 14 8 6 11 6 14 10 11 18 4 | 34 33 29 29 33 24 32 30 29 24 28
15 | 9 15 6 8 9 5 17 15 9 17 4 | 29 29 25 26 30 22 31 24 29 20 25
16 | 19 15 6 14 17 3 14 15 8 13 5 | 26 22 16 23 25 14 18 19 21 16 18
17 | 15 17 8 10 7 5 19 12 10 24 4 | 31 35 35 39 37 32 35 42 33 32 34
18E | 9 9 6 11 12 3 17 15 9 12 4 | 29 24 23 29 30 21 28 25 27 20 24
19 | 13 14 6 10 7 4 12 10 10 24 3 | 24 29 30 35 31 28 30 34 27 25 29
20E | 12 12 5 10 12 4 12 8 10 15 3 | 40 45 37 42 42 37 41 39 42 34 39
21 | 8 17 5 10 15 3 13 11 7 22 4 | 37 32 37 45 44 35 34 37 32 37 36
22E | 10 16 7 8 10 3 13 13 9 18 4 | 32 33 28 32 36 27 35 30 31 25 30
23 | 12 16 8 10 11 4 15 14 12 22 4 | 25 30 21 27 28 19 29 22 23 20 22
24 | 12 12 4 9 8 5 12 12 9 17 3 | 22 21 16 17 24 14 26 16 22 16 18
25 | 13 23 6 13 12 5 17 21 11 12 5 | 387 382 383 385 380 387 381 382 389 325 384
26 | 9 12 5 10 8 3 9 10 11 18 3 | 22 23 20 27 26 19 22 23 19 24 21
X27 | 11 7 5 13 --- 4 13 10 9 22 4 | 39 45 44 52 --- 45 53 49 46 38 46
28 | 8 16 4 11 14 4 10 13 11 13 4 | 20 23 19 22 32 15 20 25 22 17 20
29 | 11 16 7 10 9 3 19 22 10 27 4 | 37 34 35 41 35 34 38 37 30 28 34
31 | 15 15 6 12 14 4 17 11 13 21 4 | 23 23 20 25 34 18 25 22 30 26 22
32E | 20 15 8 11 16 6 12 20 18 15 5 | 61 70 61 64 66 60 66 71 67 66 63
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 16 6 10 11 4 14 13 11 18 |T 41 43 39 44 45 37 42 42 41 36 40
WRMS | 13 16 6 10 11 4 14 11 9 19 |NE 28 29 26 31 32 24 29 29 27 24 27
MEDI | 12 15 6 10 10 4 13 12 10 18 |MD 29 29 26 32 31 24 29 29 28 24 28
Table 3.1762.1 GPS week: 1762 Day: 1 MJD: 56579.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 11 4 7 11 3 11 13 15 15 3 | 23 23 17 17 25 15 26 20 19 17 17
2 | 6 15 4 11 10 4 14 12 14 28 4 | 30 24 24 30 30 23 27 29 23 29 25
3 | 9 12 5 9 15 3 9 11 10 15 3 | 21 21 18 25 25 17 21 24 22 17 20
4 | 9 9 3 8 11 4 7 10 11 20 3 | 29 22 23 26 24 23 24 28 25 27 24
5E | 11 19 6 13 16 5 19 12 10 11 4 | 31 29 23 30 25 22 27 27 31 19 25
6 | 9 10 5 10 12 2 7 9 8 11 3 | 23 22 22 23 26 21 24 26 20 20 21
7 | 10 16 4 10 10 5 16 9 9 15 3 | 28 23 20 27 30 17 24 21 22 16 21
8 | 10 11 6 10 9 3 10 18 10 23 4 | 24 24 21 23 24 18 25 27 22 28 20
9 | 8 9 5 9 8 3 10 14 12 17 3 | 23 23 19 23 23 17 24 24 21 24 19
10E | 18 21 10 11 11 5 16 14 18 14 5 | 32 41 30 33 34 30 34 33 38 32 31
11 | 9 17 5 8 13 3 13 10 12 20 4 | 42 45 43 44 51 42 45 48 40 40 43
12 | 11 23 6 10 14 4 24 15 8 14 5 | 28 27 17 23 29 16 26 27 27 17 21
13 | 9 16 6 7 14 3 14 11 11 16 4 | 26 33 22 27 35 19 29 23 22 21 24
14 | 10 17 7 10 11 6 14 11 12 18 4 | 23 30 25 26 30 22 29 25 27 21 24
15 | 13 17 4 10 13 4 17 12 12 16 4 | 25 29 21 27 34 21 30 26 25 17 24
16 | 15 21 6 14 18 3 17 16 12 13 5 | 27 29 19 24 25 17 25 23 26 20 21
17 | 15 18 4 9 8 5 17 16 16 24 4 | 25 29 24 31 29 23 30 31 25 23 25
18E | 10 10 6 11 12 3 13 13 9 12 3 | 29 25 23 28 28 22 27 24 26 22 23
19 | 11 14 5 9 9 3 12 12 8 22 3 | 22 21 20 23 25 18 23 24 18 19 19
20E | 9 14 5 11 17 3 15 10 9 13 4 | 35 35 34 40 36 33 34 35 32 33 34
21 | 9 15 5 12 15 4 15 8 9 20 4 | 29 28 24 31 33 23 28 24 25 26 25
22E | 10 12 6 7 11 4 11 12 8 19 3 | 27 27 23 27 30 23 28 27 30 22 25
23 | 9 18 7 8 12 5 17 14 13 21 4 | 25 29 21 26 28 18 28 23 20 20 22
24 | 9 14 5 7 8 4 13 11 12 17 3 | 22 23 20 20 27 15 28 20 25 20 20
25 | 9 23 6 10 13 4 15 18 13 11 4 | 393 390 391 395 389 392 391 386 393 205 392
26 | 9 10 4 10 8 3 9 9 12 18 3 | 19 18 17 24 20 16 19 21 17 21 17
X27 | 8 11 5 10 --- 4 14 11 7 20 3 | 31 31 33 32 --- 29 40 33 30 28 32
28 | 10 16 4 11 12 4 13 11 13 11 4 | 25 23 19 26 31 17 23 26 21 19 21
29 | 11 19 5 12 13 6 21 15 7 24 4 | 30 26 25 31 30 25 29 28 27 23 26
31 | 13 18 5 14 15 5 15 11 11 22 4 | 27 25 22 22 35 18 27 24 28 26 23
32E | 16 14 7 6 16 6 15 16 20 15 5 | 65 64 56 59 63 57 63 63 65 59 60
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 5 10 12 4 14 13 12 18 |T 39 39 36 40 42 34 40 39 38 30 36
WRMS | 10 16 5 9 12 4 13 12 10 18 |NE 26 26 22 26 29 20 27 26 24 22 23
MEDI | 10 15 5 10 12 4 14 12 11 17 |MD 27 27 22 27 29 21 27 26 25 22 24
Table 3.1762.2 GPS week: 1762 Day: 2 MJD: 56580.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 8 4 5 11 6 12 12 11 12 3 | 23 25 19 21 29 17 28 21 22 19 21
2 | 7 17 6 17 11 7 16 12 13 29 4 | 29 30 28 42 34 29 30 35 25 30 29
3 | 10 11 4 10 11 3 10 14 7 15 3 | 21 22 20 23 24 18 22 22 23 17 20
4 | 7 8 4 11 11 4 8 13 13 15 3 | 28 24 25 32 25 24 24 27 23 23 25
5E | 9 18 5 9 12 3 18 10 13 9 4 | 31 29 23 28 29 22 27 28 35 22 27
6 | 9 11 4 11 10 4 9 12 10 12 3 | 22 22 23 24 27 23 22 24 28 19 23
7 | 11 16 4 12 9 5 16 9 8 17 3 | 30 23 21 29 31 18 23 19 21 17 23
8 | 8 10 5 8 9 5 10 17 6 23 3 | 22 21 17 21 20 15 21 19 17 26 17
9 | 6 11 4 8 8 5 9 14 5 18 3 | 23 23 18 23 20 18 21 17 21 21 19
10E | 16 25 12 13 10 6 14 13 28 17 6 | 21 37 22 24 26 21 29 25 37 22 23
11 | 12 15 4 7 12 4 13 12 9 18 3 | 45 52 48 51 57 49 52 53 47 50 49
12 | 8 23 7 8 12 4 21 15 7 15 4 | 24 22 15 20 28 14 21 22 22 16 18
13 | 10 15 5 10 11 4 16 10 7 17 3 | 32 32 27 34 38 24 31 22 28 22 29
14 | 12 15 5 10 12 5 16 11 8 15 4 | 27 26 24 27 30 22 28 26 27 20 25
15 | 9 16 5 10 8 5 17 11 13 15 4 | 26 30 24 28 33 24 31 25 31 21 26
16 | 12 19 5 11 18 4 18 16 14 16 5 | 26 27 21 22 27 19 22 20 29 20 21
17 | 11 17 5 10 8 4 17 13 11 23 4 | 30 30 26 35 30 27 30 33 25 25 27
18E | 8 12 6 10 12 4 12 11 10 13 3 | 29 26 26 31 30 26 28 26 31 24 27
19 | 12 14 5 10 8 4 13 17 10 23 4 | 21 24 23 24 24 22 24 26 19 21 21
20E | 8 13 6 8 9 2 17 10 12 10 3 | 37 38 36 40 38 33 37 35 37 34 36
21 | 6 16 5 11 17 4 15 13 12 23 4 | 35 32 31 39 37 31 32 33 34 30 32
22E | 10 12 5 9 14 5 11 12 9 20 3 | 33 32 30 32 32 29 31 31 33 23 30
23 | 11 16 7 9 11 3 19 14 8 22 4 | 27 27 21 26 29 18 27 20 23 20 22
24 | 7 11 4 9 8 4 12 9 13 17 3 | 18 21 16 20 27 13 26 18 19 17 18
25 | 12 24 5 12 11 6 21 17 11 12 5 | 355 353 350 351 352 351 358 344 351 338 352
26 | 8 11 4 11 7 4 9 11 14 16 3 | 22 22 18 25 20 19 19 20 17 22 19
X27 | 9 10 4 13 --- 5 14 14 8 21 4 | 36 37 37 40 --- 37 43 38 39 33 37
28 | 9 14 4 12 15 4 13 10 8 9 3 | 21 18 17 25 30 14 19 20 22 14 19
29 | 11 17 5 10 10 6 19 16 11 22 4 | 45 40 38 47 41 38 39 41 40 34 40
31 | 10 15 5 16 14 3 17 11 12 22 4 | 30 27 24 26 37 22 27 25 29 25 26
32E | 16 15 8 9 15 8 15 18 26 19 5 | 63 59 54 57 61 49 61 59 57 55 57
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 5 10 11 5 15 13 12 18 |T 39 39 36 40 42 35 39 37 39 34 37
WRMS | 10 15 5 9 11 4 14 12 9 19 |NE 27 27 24 29 30 23 27 26 26 23 25
MEDI | 10 15 5 10 11 4 15 12 11 17 |MD 28 27 24 28 30 22 28 25 28 22 25
Table 3.1762.3 GPS week: 1762 Day: 3 MJD: 56581.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 11 7 12 11 4 10 13 9 12 3 | 23 25 20 25 30 18 28 23 26 17 22
2 | 14 17 7 12 13 5 14 9 9 30 4 | 31 31 35 45 39 34 36 38 30 34 34
3 | 8 13 6 10 9 4 9 12 9 15 3 | 21 22 23 31 28 21 26 27 25 22 24
4 | 8 11 5 6 11 4 8 13 10 15 3 | 33 28 31 35 32 29 30 35 28 28 30
5E | 11 16 5 10 9 4 16 11 11 9 4 | 30 27 25 30 32 22 29 33 35 25 27
6 | 10 12 5 9 7 4 8 12 7 12 3 | 24 23 26 30 31 25 28 32 25 25 26
7 | 8 13 6 8 10 4 14 7 8 17 3 | 28 26 25 28 31 22 24 23 27 20 24
8 | 10 9 5 8 7 5 10 15 4 21 3 | 24 26 22 21 23 20 30 25 25 27 22
9 | 8 10 5 7 5 4 8 9 4 16 2 | 23 26 20 21 23 20 27 23 25 23 21
10E | 15 21 10 8 11 6 14 12 25 15 5 | 33 44 31 36 36 30 39 34 42 32 33
11 | 11 18 5 8 11 4 12 12 10 17 4 | 57 57 59 64 68 58 60 64 57 57 59
12 | 12 24 7 12 14 5 24 9 11 16 5 | 27 26 19 25 30 16 29 26 24 18 21
13 | 12 14 6 7 12 4 13 10 9 15 3 | 28 35 26 28 37 25 33 25 26 21 27
14 | 25 18 7 14 12 7 17 15 9 15 5 | 36 29 30 32 30 24 30 35 33 26 29
15 | 8 16 5 8 9 3 15 10 8 17 3 | 28 30 26 30 33 24 32 29 30 23 27
16 | 13 24 6 13 16 3 17 14 12 17 5 | 25 27 19 25 28 17 24 24 26 25 21
17 | 10 17 5 8 11 5 16 13 10 28 4 | 34 35 33 40 40 31 36 41 39 31 35
18E | 9 14 8 10 11 4 11 14 10 14 4 | 35 29 28 34 32 28 30 30 31 29 29
19 | 11 16 7 10 7 5 11 18 8 21 4 | 25 25 26 35 30 27 28 34 28 25 27
20E | 12 12 6 11 12 3 12 9 9 11 3 | 44 42 40 43 43 38 39 41 45 39 41
21 | 9 16 5 10 12 3 13 8 12 23 4 | 40 35 37 45 45 36 39 38 36 37 38
22E | 10 15 6 9 14 4 12 13 10 19 4 | 34 31 31 35 34 29 36 33 33 28 31
23 | 15 19 7 7 11 3 16 15 9 20 4 | 26 30 23 27 30 21 29 26 24 20 24
24 | 10 12 6 8 9 5 16 8 13 15 3 | 23 24 23 24 27 18 31 22 23 22 22
25 | 16 78 12 17 82 15 86 104 22 26 9 | 978 974 970 971 942 977 978 984 978 507 973
26 | 10 10 5 7 9 3 11 10 7 17 3 | 20 20 18 23 21 17 23 22 21 24 19
X27 | 9 11 5 9 --- 7 13 14 8 17 4 | 35 37 39 45 --- 40 46 45 39 38 40
28 | 11 13 5 10 14 5 12 9 9 9 3 | 22 21 18 23 31 15 22 21 24 15 19
29 | 14 16 5 11 10 5 16 17 12 20 4 | 40 35 36 41 38 35 37 44 35 32 36
31 | 13 16 5 15 15 5 15 11 8 21 4 | 27 30 25 29 38 23 29 29 29 29 27
32E | 20 16 8 22 15 6 16 15 22 15 6 | 60 61 57 57 59 53 63 60 64 56 57
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 21 6 11 19 5 21 22 11 18 |T 61 61 59 63 64 57 63 63 62 43 60
WRMS | 12 16 6 9 19 4 18 10 8 19 |NE 29 29 27 32 33 25 31 31 29 26 28
MEDI | 11 16 6 10 11 4 13 12 9 17 |MD 28 29 26 31 32 25 30 32 29 26 27
Table 3.1762.4 GPS week: 1762 Day: 4 MJD: 56582.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 11 5 7 11 6 8 15 12 13 3 | 16 22 14 17 25 12 25 21 19 15 17
2 | 14 16 7 11 15 5 14 9 12 31 4 | 32 31 29 39 37 31 32 35 34 30 31
3 | 9 13 4 9 10 6 7 9 13 14 3 | 21 24 23 27 26 21 26 25 26 21 23
4 | 6 10 4 5 13 4 7 11 9 11 3 | 25 22 23 28 27 24 22 29 27 22 24
5E | 8 15 6 13 13 4 17 8 11 8 4 | 30 27 23 29 28 21 28 27 28 23 26
6 | 10 13 4 11 11 5 8 9 8 13 3 | 21 24 23 27 26 22 26 28 27 21 24
7 | 8 17 5 8 13 4 14 7 10 16 3 | 26 22 20 25 28 16 23 18 22 15 21
8 | 10 9 5 7 9 4 12 14 9 23 3 | 19 20 15 18 16 14 22 20 18 26 16
9 | 8 9 5 7 9 4 10 8 9 16 3 | 18 21 17 18 18 16 22 18 20 22 17
10E | 11 21 9 10 10 8 15 14 26 14 5 | 25 35 21 23 26 21 31 31 33 24 23
11 | 10 19 4 7 13 5 12 17 11 18 4 | 45 50 50 52 58 49 50 57 50 50 50
12 | 14 23 5 8 13 5 22 10 11 19 5 | 31 27 20 23 31 19 24 24 29 19 23
13 | 9 15 6 6 15 3 16 9 8 16 3 | 25 31 23 28 36 23 33 23 27 18 25
14 | 22 18 6 8 12 7 17 16 9 22 5 | 35 28 27 31 30 24 31 35 29 29 28
15 | 9 15 4 8 14 3 14 11 11 20 4 | 25 28 24 24 30 21 29 22 28 18 24
16 | 12 21 4 12 14 3 14 14 5 15 4 | 25 27 19 24 23 17 24 23 21 23 20
17 | 15 16 5 12 11 5 16 12 12 26 4 | 22 29 26 35 32 26 28 33 27 26 27
18E | 10 14 6 11 14 4 14 11 11 14 4 | 31 24 25 32 29 25 29 28 30 24 26
19 | 11 17 4 8 10 5 13 21 9 24 4 | 22 26 25 29 24 24 27 34 28 25 25
20E | 10 11 6 8 9 3 15 9 12 11 3 | 38 37 33 37 38 31 36 35 36 32 34
21 | 7 15 4 14 14 3 17 8 8 26 4 | 33 32 34 42 44 33 34 34 29 34 34
22E | 11 13 6 8 13 3 12 13 12 23 4 | 33 31 29 34 32 29 33 32 33 22 30
23 | 12 18 7 8 12 4 15 14 11 20 4 | 23 27 19 25 27 19 28 25 22 17 21
24 | 14 12 5 9 11 5 15 7 10 15 3 | 22 21 16 18 24 15 25 15 22 15 18
25 | 11 20 6 10 13 3 17 12 16 --- 4 | 556 552 555 555 554 557 553 562 562 --- 556
26 | 11 11 5 9 13 4 11 12 10 16 3 | 20 20 18 21 22 15 20 22 21 22 18
X27 | 9 13 7 10 --- 4 14 12 9 17 4 | 36 40 37 40 --- 36 46 42 41 34 39
28 | 10 17 4 10 14 3 12 9 10 8 3 | 20 23 17 23 30 15 19 19 19 14 18
29 | 9 18 5 12 18 6 19 18 13 26 5 | 64 63 64 70 66 63 66 70 65 64 65
31 | 13 16 6 12 19 7 16 9 13 21 4 | 23 26 21 25 36 19 27 24 31 23 23
32E | 12 13 5 7 13 4 14 15 23 16 4 | 47 49 44 49 47 42 50 53 53 49 47
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 5 9 13 5 14 12 12 19 |T 45 46 43 47 49 41 47 47 47 25 44
WRMS | 11 16 5 8 13 4 13 10 10 19 |NE 27 28 25 29 31 23 29 29 28 25 26
MEDI | 10 15 5 9 13 4 14 11 11 16 |MD 25 27 23 28 29 22 28 28 28 23 24
Table 3.1762.5 GPS week: 1762 Day: 5 MJD: 56583.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 9 5 7 10 3 10 14 11 12 3 | 22 23 20 25 29 18 29 22 26 21 21
2 | 9 16 6 10 14 4 14 8 13 30 4 | 32 28 27 34 34 26 31 32 25 24 28
3 | 8 12 4 9 9 4 8 8 11 15 3 | 21 22 23 26 24 18 25 22 24 19 22
4 | 7 7 4 9 13 3 7 12 12 11 3 | 22 24 22 27 26 20 24 26 19 18 22
5E | 9 16 6 11 9 4 14 9 17 9 4 | 31 27 24 30 31 22 29 28 35 22 27
6 | 8 11 4 11 10 4 8 9 13 16 3 | 26 24 26 27 27 21 26 25 26 22 24
7 | 8 17 6 9 13 4 13 7 11 17 3 | 25 21 20 23 29 15 22 17 23 16 20
8 | 8 8 4 8 9 4 11 11 7 24 3 | 22 19 14 16 18 12 23 15 20 26 15
9 | 7 10 4 8 10 3 10 6 9 17 3 | 21 19 16 17 21 14 22 17 20 22 17
10E | 15 20 8 10 12 6 14 13 27 19 5 | 33 40 28 30 31 26 38 33 38 28 29
11 | 12 18 6 8 11 6 12 19 12 20 4 | 43 48 47 49 50 45 47 51 45 47 46
12 | 10 24 5 10 15 3 24 11 11 20 5 | 28 27 15 22 30 15 25 20 24 15 19
13 | 10 16 5 9 17 3 14 8 7 15 4 | 25 30 21 25 36 19 29 20 25 16 23
14 | 10 17 6 10 12 5 16 17 8 23 4 | 25 27 25 27 30 21 26 34 24 27 25
15 | 8 13 5 10 14 4 17 9 12 20 4 | 27 27 23 27 32 20 30 23 26 19 24
16 | 8 20 5 12 19 4 14 14 13 16 4 | 22 21 16 22 25 14 19 22 23 17 17
17 | 7 16 6 10 11 4 15 12 15 29 4 | 27 27 26 32 29 21 30 28 25 20 25
18E | 7 12 6 10 11 3 12 13 12 14 3 | 31 26 24 32 32 23 28 28 28 22 26
19 | 12 17 6 10 8 4 13 22 10 24 4 | 23 24 25 29 23 21 27 29 21 20 23
20E | 10 13 4 9 10 4 14 9 15 12 3 | 49 44 44 47 48 43 43 46 52 45 45
21 | 6 14 5 12 14 4 17 8 12 26 4 | 34 36 34 40 41 30 35 33 31 31 34
22E | 9 16 5 11 13 4 12 22 8 23 4 | 33 30 26 30 33 24 31 37 30 24 28
23 | 13 17 5 11 14 3 18 16 8 18 4 | 26 26 19 23 28 16 26 21 24 15 20
24 | 9 14 5 9 10 3 12 7 16 12 3 | 18 20 15 18 24 11 25 16 20 11 16
25E | 15 19 8 17 20 7 17 11 14 --- 5 | 569 562 563 565 560 564 563 564 559 --- 563
26 | 6 10 3 8 14 3 10 6 17 17 3 | 20 18 17 22 25 16 19 20 22 22 18
X27 | 11 11 6 13 --- 4 13 11 12 19 4 | 35 35 35 41 --- 34 42 35 34 30 35
28 | 7 15 4 10 13 4 12 7 8 8 3 | 20 18 16 23 29 13 22 16 21 13 18
29 | 13 17 5 12 11 5 17 9 9 30 4 | 45 41 44 48 44 42 43 43 41 34 43
31 | 9 15 4 17 19 6 17 13 7 21 4 | 24 26 20 24 35 16 27 29 27 18 22
32E | 11 14 6 8 23 5 14 16 16 17 4 | 65 65 58 63 59 57 66 65 65 61 61
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 5 10 13 4 14 12 13 19 |T 46 45 43 47 49 40 47 45 45 24 43
WRMS | 9 15 5 10 13 4 13 9 10 20 |NE 26 26 23 27 29 20 28 25 25 21 24
MEDI | 9 15 5 10 12 4 14 11 12 17 |MD 26 27 24 27 30 21 28 28 25 22 24
Table 3.1762.6 GPS week: 1762 Day: 6 MJD: 56584.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 10 5 8 12 6 9 13 12 11 3 | 26 23 21 25 31 19 30 23 23 20 22
2 | 13 14 5 13 12 5 14 9 9 33 4 | 36 33 34 46 41 35 37 41 35 37 36
3 | 9 12 4 12 11 4 9 8 9 17 3 | 25 24 27 34 31 24 29 27 28 22 27
4 | 5 7 4 10 13 3 6 9 12 10 3 | 32 27 29 37 37 29 30 34 28 25 30
5E | 8 14 6 13 11 5 12 16 11 8 4 | 36 33 30 35 38 29 33 40 36 32 33
6 | 7 12 6 12 13 3 10 10 9 19 3 | 28 26 32 33 35 28 31 34 33 25 31
7 | 10 17 5 12 15 3 16 7 12 23 4 | 33 25 24 32 33 22 25 24 31 28 25
8 | 10 10 5 9 10 5 9 9 8 23 3 | 22 22 18 19 22 15 26 21 23 30 19
9 | 8 9 4 9 11 4 9 10 9 17 3 | 20 23 17 17 23 16 24 21 26 24 19
10E | 10 19 6 11 13 5 16 13 24 18 5 | 34 41 33 39 38 32 39 37 46 40 36
11 | 9 18 5 8 13 5 13 21 15 22 4 | 65 64 69 71 77 68 69 76 70 67 69
12 | 11 27 6 10 14 5 26 11 12 18 5 | 25 29 18 24 30 16 29 22 24 16 20
13 | 10 15 5 8 18 4 14 9 10 15 4 | 29 34 26 31 42 26 34 25 29 22 28
14 | 19 19 7 9 16 5 19 16 11 24 5 | 32 26 28 31 31 24 27 36 34 30 27
15 | 10 15 4 11 14 4 17 12 15 20 4 | 35 36 28 32 37 29 35 33 35 28 31
16 | 12 21 6 14 18 4 13 10 12 14 4 | 26 26 19 25 24 16 18 20 26 19 20
17 | 11 16 5 9 9 5 16 12 13 29 4 | 31 33 34 41 37 33 37 43 32 33 34
18E | 10 13 5 9 10 4 13 13 11 15 3 | 34 28 26 32 31 25 29 32 35 23 29
19 | 11 14 5 12 8 4 12 19 12 26 4 | 29 30 32 37 32 31 33 37 35 27 31
20E | 9 12 6 9 23 4 16 14 11 11 4 | 58 53 51 55 63 49 51 50 55 48 53
21 | 9 16 5 12 13 4 16 11 15 33 4 | 45 39 43 52 50 41 41 45 43 43 43
22E | 9 16 6 10 16 5 16 19 9 20 4 | 34 30 28 34 39 26 32 37 35 22 30
23 | 12 16 6 10 15 4 15 15 11 18 4 | 27 27 21 25 31 19 28 23 24 19 22
24 | 13 12 5 6 12 4 12 10 10 15 3 | 17 24 16 20 28 14 29 20 23 14 19
25E | 9 16 7 11 16 7 14 11 12 13 4 | 412 411 413 413 409 413 410 414 414 520 412
26 | 10 10 5 11 15 3 10 6 12 16 3 | 26 27 24 28 31 23 27 27 27 28 25
X27 | 6 10 4 16 --- 3 12 11 13 25 4 | 46 46 50 50 --- 47 54 51 51 41 49
28 | 9 14 4 10 14 4 12 8 10 10 3 | 24 23 21 24 29 17 24 22 23 20 21
29 | 11 18 6 13 10 4 17 11 8 36 4 | 52 50 51 55 52 49 46 55 47 55 50
31 | 10 16 6 19 22 7 18 11 8 24 5 | 28 30 24 30 39 20 28 29 33 23 26
32E | 12 12 5 9 23 6 14 17 18 17 5 | 65 62 58 61 60 56 65 64 63 61 60
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 5 11 14 5 14 13 12 20 |T 46 45 43 48 50 41 46 47 47 46 44
WRMS | 11 15 5 10 14 5 14 10 10 21 |NE 31 31 29 34 35 27 32 32 32 29 30
MEDI | 10 14 5 10 13 4 14 11 11 18 |MD 32 30 28 33 35 26 31 34 33 28 30
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 4.1762 GPS week: 1762 MJD: 56578.0-56584.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 |U 6 6 16 |U 8 10 28 |U 7 8 19 |
emr | emr 2967 | 9 8 22 |U 8 9 27 | 8 8 18 |
esa | esa 2976 | 6 7 18 |U 8 11 28 | 7 7 17 |
gfz | gfz 2967 |U 7 7 18 |U 8 10 27 |U 7 7 17 |
igr | igr 2975 | 7 6 18 | 8 10 28 | 7 7 17 |
igs | igs 2974 | 7 7 20 | 8 9 27 | 7 8 19 |
jpl | jpl 2967 | 9 7 21 |U 8 10 29 |U 8 8 18 |
mit | mit 2976 | 8 7 20 |U 11 13 31 |U 14 14 28 |
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 5.1762.0 GPS week: 1762 Day: 0 MJD: 56578.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 4 14 | 8 11 24 | 6 7 18 |
emr | emr 2968 | 8 5 18 | 9 9 24 | 7 6 19 |
esa | esa 2976 | 6 5 15 | 7 10 24 | 6 6 17 |
gfz | gfz 2968 | 7 5 15 | 8 10 22 | 6 6 17 |
igr | igr 2976 | 6 5 16 | 7 10 23 | 6 6 17 |
igs | igs 2976 | 6 4 14 | 7 10 23 | 6 6 18 |
jpl | jpl 2968 | 8 5 17 | 8 11 27 | 7 6 19 |
mit | mit 2976 | 6 4 14 | 8 13 24 | 6 7 16 |
Table 5.1762.1 GPS week: 1762 Day: 1 MJD: 56579.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 17 | 7 11 27 | 8 9 25 |
emr | emr 2968 | 7 4 23 | 7 9 32 | 8 9 23 |
esa | esa 2976 | 5 5 19 | 7 11 30 | 8 6 22 |
gfz | gfz 2969 | 6 6 19 | 7 10 28 | 7 7 23 |
igr | igr 2976 | 5 5 20 | 7 10 29 | 8 7 23 |
igs | igs 2976 | 5 5 20 | 7 10 30 | 7 6 23 |
jpl | jpl 2966 | 7 4 24 | 7 10 29 | 8 8 23 |
mit | mit 2976 | 6 4 20 | 12 11 37 | 10 7 26 |
Table 5.1762.2 GPS week: 1762 Day: 2 MJD: 56580.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 4 11 | 8 12 28 | 6 7 20 |
emr | emr 2968 | 8 7 19 | 8 9 27 | 7 9 19 |
esa | esa 2976 | 5 5 13 | 8 12 26 | 7 8 16 |
gfz | gfz 2968 | 6 5 13 | 8 11 25 | 7 8 17 |
igr | igr 2976 | 5 4 14 | 8 11 25 | 7 8 16 |
igs | igs 2975 | 6 6 19 | 9 9 25 | 7 9 19 |
jpl | jpl 2968 | 8 6 20 | 7 11 27 | 7 8 17 |
mit | mit 2976 | 14 11 30 | 20 22 32 | 37 43 67 |
Table 5.1762.3 GPS week: 1762 Day: 3 MJD: 56581.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 6 10 20 | 9 9 27 | 8 12 19 |
emr | emr 2967 | 8 12 26 | 9 9 26 | 8 8 17 |
esa | esa 2976 | 7 11 23 | 9 10 27 | 8 10 18 |
gfz | gfz 2967 | 8 11 23 | 10 10 24 | 8 10 18 |
igr | igr 2975 | 7 11 23 | 10 9 28 | 7 11 18 |
igs | igs 2974 | 7 11 23 | 10 9 25 | 7 11 19 |
jpl | jpl 2967 | 8 9 25 | 10 11 27 | 9 10 18 |
mit | mit 2976 | 8 8 23 | 10 9 33 | 10 13 24 |
Table 5.1762.4 GPS week: 1762 Day: 4 MJD: 56582.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 5 16 | 8 11 34 | 6 6 19 |
emr | emr 2968 | 12 8 22 | 8 11 33 | 8 6 15 |
esa | esa 2976 | 10 7 18 | 8 12 34 | 8 5 17 |
gfz | gfz 2968 | 11 8 17 | 8 11 34 | 6 6 17 |
igr | igr 2975 | 10 7 18 | 8 11 34 | 6 5 18 |
igs | igs 2974 | 10 7 18 | 8 11 33 | 6 5 17 |
jpl | jpl 2968 | 12 8 23 | 9 11 37 | 7 6 17 |
mit | mit 2976 | 9 8 19 | 9 14 32 | 14 9 24 |
Table 5.1762.5 GPS week: 1762 Day: 5 MJD: 56583.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 12 | 6 8 28 | 7 9 19 |
emr | emr 2968 | 9 8 17 | 8 9 23 | 8 10 16 |
esa | esa 2976 | 6 6 14 | 8 10 25 | 8 8 16 |
gfz | gfz 2968 | 8 8 13 | 7 9 27 | 8 8 15 |
igr | igr 2976 | 6 5 13 | 7 9 28 | 7 8 15 |
igs | igs 2973 | 6 7 12 | 7 8 26 | 8 9 15 |
jpl | jpl 2968 | 9 8 14 | 7 9 27 | 9 10 16 |
mit | mit 2976 | 6 8 11 | 6 8 28 | 10 10 15 |
Table 5.1762.6 GPS week: 1762 Day: 6 MJD: 56584.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 6 9 21 | 8 10 30 | 7 8 16 |
emr | emr 2967 | 9 8 26 | 9 10 25 | 8 9 18 |
esa | esa 2976 | 7 9 25 | 7 10 27 | 6 8 15 |
gfz | gfz 2967 | 7 9 23 | 8 9 29 | 6 7 14 |
igr | igr 2972 | 7 8 24 | 7 10 26 | 6 7 14 |
igs | igs 2971 | 9 12 33 | 8 8 30 | 7 8 20 |
jpl | jpl 2968 | 8 10 25 | 8 11 29 | 8 10 19 |
mit | mit 2976 | 7 10 22 | 11 10 33 | 8 10 22 |
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 6.1762 GPS week: 1762 MJD: 56578.500-56584.500
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 18 73 211 -2 | 19 21
| 16 20 68 68 6 | 3
emr uuxxu | 30 -40 200 268 -7 | 37 40
| 12 27 122 52 6 | 4
esa uuuuu | -4 5 -33 -99 0 | 12 16
| 17 7 32 48 4 | 2
gfz uuuuu | 1 -22 88 -46 0 | 17 19
| 14 25 50 159 3 | 1
grg uuuux | 1 -9 -53 -54 -2 | 11 14
| 15 12 47 53 3 | 3
igr xxxxx | -24 14 2 24 -6 | 3 13
| 11 6 49 48 3 | 4
irf xxxxx | 9 1 -26 4 -6 | 3 12
| 10 12 47 27 4 | 4
jpl uuuuu | 24 0 23 199 8 | 34 37
| 48 18 121 55 10 | 1
mit uuuuu | -9 10 -59 23 -8 | 23 26
| 27 27 100 69 4 | 4
ngs uuuuu | 0 22 -3 -71 2 | 8 12
| 59 62 124 85 4 | 2
sio xxxxx | 46 51 -159 -39 6 | 29 30
| 27 37 57 83 3 | 1
Table 7.1762.0 GPS week: 1762 Day: 0 MJD: 56578.500
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 | -50 14 121 132 1 | 23 25
emr uuxxu | 46 -86 280 177 -5 | 42 44
esa uuuuu | 11 12 -66 -105 2 | 16 19
gfz uuuuu | 7 -15 25 -79 0 | 19 21
grg uuuux | -2 -26 -58 -81 0 | 15 16
igr xxxxx | -12 18 47 -17 -5 | 9 14
irf xxxxx | 18 -13 -24 34 -7 | 9 13
jpl uuuuu | 65 -14 29 190 15 | 34 35
mit uuuuu | 11 -34 -31 142 -7 | 28 30
ngs uuuuu | -80 100 72 15 -2 | 11 14
sio xxxxx | 49 -8 -96 -7 13 | 29 30
Table 7.1762.1 GPS week: 1762 Day: 1 MJD: 56579.500
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 31 74 202 5 | 21 22
emr uuxxu | 40 -35 296 247 -16 | 41 44
esa uuuuu | 1 -3 -1 -62 -5 | 14 16
gfz uuuuu | 11 0 42 -18 3 | 18 19
grg uuuux | -27 -16 -85 -92 -2 | 14 15
igr xxxxx | -17 3 44 -7 -8 | 7 11
irf xxxxx | 1 -4 -37 -3 -11 | 7 10
jpl uuuuu | 97 15 135 214 -10 | 34 36
mit uuuuu | -28 11 -82 16 -14 | 27 28
ngs uuuuu | -42 -12 -81 -142 6 | 10 13
sio xxxxx | 45 26 -103 -178 2 | 29 30
Table 7.1762.2 GPS week: 1762 Day: 2 MJD: 56580.500
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 | -13 4 -62 262 3 | 21 22
emr uuxxu | 26 -69 369 327 -4 | 39 43
esa uuuuu | -1 9 -13 -122 1 | 12 14
gfz uuuuu | 12 7 63 164 2 | 18 19
grg uuuux | -5 -19 -119 -138 -4 | 12 14
igr xxxxx | -31 23 19 17 -10 | 5 12
irf xxxxx | 3 -9 -76 -34 -8 | 5 11
jpl uuuuu | 21 24 178 114 9 | 33 35
mit uuuuu | -33 20 -160 -47 -11 | 25 27
ngs uuuuu | 9 -5 166 -59 -1 | 10 13
sio xxxxx | 30 82 -187 -101 5 | 29 30
Table 7.1762.3 GPS week: 1762 Day: 3 MJD: 56581.500
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 57 124 313 -5 | 18 20
emr uuxxu | 14 -21 149 319 -8 | 37 41
esa uuuuu | -18 1 -8 -194 6 | 10 14
gfz uuuuu | 14 -2 82 101 4 | 16 18
grg uuuux | 16 -3 -64 -4 -8 | 9 13
igr xxxxx | -26 14 -46 -13 -3 | 2 14
irf xxxxx | 6 6 -78 26 -6 | 1 13
jpl uuuuu | -51 6 54 246 8 | 32 35
mit uuuuu | -2 11 -198 48 -11 | 22 26
ngs uuuuu | 57 -43 32 -199 -3 | 8 13
sio xxxxx | 56 35 -211 13 5 | 27 28
Table 7.1762.4 GPS week: 1762 Day: 4 MJD: 56582.500
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 | -8 9 32 176 -3 | 17 20
emr uuxxu | 22 -18 185 291 -1 | 35 39
esa uuuuu | 21 6 -35 -57 2 | 10 15
gfz uuuuu | -7 -44 103 8 -1 | 16 19
grg uuuux | 15 2 -55 -1 1 | 8 12
igr xxxxx | -34 10 -84 114 -6 | 2 14
irf xxxxx | 0 12 -39 -8 -1 | 0 13
jpl uuuuu | 3 8 31 155 21 | 34 36
mit uuuuu | -44 19 -62 -52 -4 | 21 25
ngs uuuuu | -18 17 18 -121 -1 | 7 12
sio xxxxx | -2 83 -244 -26 5 | 28 30
Table 7.1762.5 GPS week: 1762 Day: 5 MJD: 56583.500
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 17 116 254 -4 | 18 20
emr uuxxu | 26 -41 23 242 -3 | 35 38
esa uuuuu | -26 -4 -87 -68 1 | 11 16
gfz uuuuu | -24 -51 153 -264 -5 | 17 21
grg uuuux | 7 -8 -22 -56 -1 | 9 14
igr xxxxx | -8 12 10 11 -4 | 1 13
irf xxxxx | 11 -5 28 -19 -5 | 0 13
jpl uuuuu | 31 -20 -162 198 7 | 36 40
mit uuuuu | 3 -12 58 -12 -9 | 20 24
ngs uuuuu | 94 116 0 18 5 | 7 12
sio xxxxx | 59 47 -118 -50 4 | 30 32
Table 7.1762.6 GPS week: 1762 Day: 6 MJD: 56584.500
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 -3 106 139 -13 | 15 18
emr uuxxu | 40 -13 98 272 -13 | 30 33
esa uuuuu | -13 14 -21 -86 -4 | 9 15
gfz uuuuu | -8 -47 148 -230 -3 | 15 18
grg uuuux | 3 7 30 -7 -1 | 7 12
igr xxxxx | -37 18 26 61 -3 | -2 12
irf xxxxx | 25 21 42 35 -1 | -3 12
jpl uuuuu | 1 -19 -102 278 7 | 36 39
mit uuuuu | 32 53 66 64 -2 | 16 21
ngs uuuuu | -20 -19 -229 -10 8 | 6 10
sio xxxxx | 84 94 -154 79 7 | 28 31
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