[IGSREPORT-22357] Wk 1769 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Dec 20 13:30:28 PST 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1769 (Dec 01, 2013 - Dec 07, 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:
igs1769[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1769[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1769[0-6].cls IGS GPS clock combination summary report.
igs17697.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17697.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 | HOB2 HOLM INVK INVK NRIL
0 | EMR | HERS SFER
0 | ESA | UNSA
0 | GRG | 26 26 KELY QAQ1 SFER KELY QAQ1 SFER
0 | MIT | 2 21 26 2 21 26 BRAZ BUCU DRAG KOUR OPMT BRAZ BUCU
0 | MIT | DRAG KOUR OPMT
1 | COD | 2 2 HOFN MAS1 HOFN
1 | EMR | 2 HERS
1 | ESA | DRAG HOB2 KOUR HOB2 KOUR MAS1
1 | GFZ | DRAG TIDB DRAG TIDB
1 | GRG | 26 2 26 HOFN IRKJ ISPA MOBS NRMD REUN THU3 HOB2 HOFN
1 | GRG | HYDE IRKJ ISPA MAL2 REUN THU3 USNO
1 | JPL | 2
1 | MIT | 2 9 16 26 2 6 9 16 26 OPMT OPMT
2 | COD | 2 2 ALIC ASPA HOB2 ALIC
2 | EMR | 2 2 HERS MCM4 HERS MCM4
2 | ESA | MATE
2 | GFZ | HRAO
2 | GRG | 2 26 26 DAV1 IRKJ KELY KOUC MATE DAV1 IRKJ KELY KOUC
2 | JPL | 2
2 | MIT | 2 9 26 2 9 26
3 | COD | 2 DAV1 DAV1
3 | GFZ | GOLD GOLD
3 | GRG | 1 26 1 26 IRKJ ISPA KELY KOUC MCM4 DRAG IRKJ ISPA
3 | GRG | KELY KOUC MAL2 MCM4
3 | MIT | 1 2 8 9 19 23 26 1 2 8 9 19 20 23 26 CAS1 CRO1 KOUR
3 | MIT | MOBS TIDB CRO1 KOUR MOBS TIDB
4 | COD | 2 BOGT BOR1 DARW KARR MONP BOGT KARR MONP
4 | EMR | 2 HERS
4 | ESA | 23 ARTU CAS1 ARTU BOGT CAS1 CHPI UNSA
4 | GFZ | WSRT
4 | GRG | 26 26 ARTU DARW DRAG IRKJ KARR KELY MOBS ARTU DARW
4 | GRG | DRAG IRKJ KARR KELY MAC1 MCIL MOBS
4 | JPL | 2
4 | MIT | 2 5 8 9 19 23 26 2 5 16 23 25 KELY NTUS OPMT REYK
4 | MIT | SCH2 OPMT SCH2
5 | COD | ASPA BOR1 BOR1
5 | GFZ | 1 SFER ABPO IISC SFER
5 | GRG | 1 26 1 26 DARW HOB2 HYDE IRKJ ISPA MCIL MOBS NOVM
5 | GRG | NRMD DARW FAA1 HOB2 HYDE IRKJ ISPA MCIL MOBS NOVM
5 | GRG | NRMD
5 | JPL | 26
5 | MIT | 2 9 11 13 21 22 26 2 3 9 11 13 21 22 26 PTBB GOPE
5 | MIT | HERS PTBB WSRT
6 | COD | 2 ASPA BRFT CHTI COCO DARW DGAR HOB2 HRAO KOUR MAL2
6 | COD | MONP NICO NRIL USNO
6 | ESA | KOUR NRIL
6 | GFZ | 1 1 BRAZ MCM4 RIOP BRAZ MCM4 NRIL RIOP
6 | GRG | 26 26 BUCU IRKJ KELY KOUR MDO1 NRIL NTUS POLV BUCU
6 | GRG | IRKJ IRKT KELY MDO1 NTUS POLV
6 | JPL | 2 26 CHPI
6 | MIT | 2 7 9 15 2 6 7 9 15 26 KOUR KOUR NTUS
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 | ~23:43 | ~ 0.15 ns
1 | GRG | ~04:20 | ~ -0.16 ns
1 | MIT | ~00:00 | ~ -0.69 ns
2 | GRG | ~13:30 | ~ -0.14 ns
3 | GRG | ~16:25 | ~ -0.14 ns
4 | GRG | ~13:49 | ~ 0.15 ns
4 | MIT | ~07:00 | ~ -0.19 ns
5 | GRG | ~00:50 | ~ 0.18 ns
6 | GRG | ~17:52 | ~ -0.17 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
----+--------+---------------
2 | GFZ | 24
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 G26 | | | | | | 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 | -1.0 .5 -1.7 -41 14 -23 .16
EMR | 0 | -3.0 5.6 3.0 5 22 10 -.06
ESA | 0 | 4.6 7.7 .2 14 -39 36 -.03
GFZ | 0 | .2 .0 -.7 -17 -21 11 -.01
GRG | 0 | -.6 6.6 -39.0 -12 0 3 .23
JPL | 0 | -3.3 5.8 7.4 -78 -24 10 .36
MIT | 0 | 3.7 6.9 -2.4 12 -6 -25 .20
NGS | 0 | -2.1 -3.8 -3.3 -8 15 -5 .60
SIO | 0 | 1.6 5.6 63.4 199 184 292 .19
COD | 1 | -1.6 .0 -1.8 -33 21 -3 .09
EMR | 1 | 3.7 1.7 11.9 12 25 -3 .18
ESA | 1 | 6.2 6.0 1.3 11 -41 37 .22
GFZ | 1 | .6 -.4 -1.1 -19 -34 -14 .24
GRG | 1 | 6.2 10.1 -33.4 -13 5 -13 .63
JPL | 1 | 7.6 2.7 11.0 -104 16 -44 .56
MIT | 1 | 4.1 3.6 2.3 -8 1 -29 .38
NGS | 1 | 2.5 2.5 -.7 4 -3 13 .42
SIO | 1 | 3.0 6.1 80.3 248 203 481 .14
COD | 2 | -1.3 -.2 -1.7 -46 27 -14 .12
EMR | 2 | 1.9 4.9 14.7 11 27 1 .07
ESA | 2 | 7.2 9.8 3.9 7 -50 68 -.07
GFZ | 2 | .3 .4 -1.3 -12 -26 -17 -.11
GRG | 2 | 4.4 10.9 -26.8 -27 16 -24 .23
JPL | 2 | 7.7 3.2 11.7 -80 -23 5 .35
MIT | 2 | 6.7 3.6 5.7 -11 4 -40 .29
NGS | 2 | 2.7 6.8 .6 9 -2 18 .53
SIO | 2 | 2.8 6.2 70.4 101 416 382 .23
COD | 3 | -.9 .3 -1.7 -41 23 -15 .03
EMR | 3 | 10.0 5.8 13.5 -13 25 -14 -.08
ESA | 3 | 10.5 8.9 11.1 30 -92 38 -.17
GFZ | 3 | .3 .1 -1.0 -14 -27 -13 -.35
GRG | 3 | 5.5 8.3 -20.5 -27 6 2 .35
JPL | 3 | 9.5 2.6 8.7 -66 -13 -1 .18
MIT | 3 | 6.7 3.0 4.1 -14 -8 -46 -.12
NGS | 3 | 6.4 -2.8 -.1 -13 -20 34 .27
SIO | 3 | 6.1 4.2 65.3 141 132 259 .01
COD | 4 | -1.4 .3 -2.6 -50 15 8 .40
EMR | 4 | 5.0 6.1 9.2 -7 23 -16 .05
ESA | 4 | 7.1 6.7 7.7 5 -63 30 -.23
GFZ | 4 | .8 -.1 -1.2 -27 -43 0 .14
GRG | 4 | 6.1 13.8 -25.8 -31 5 22 .59
JPL | 4 | 5.0 .8 16.7 -89 3 -27 .67
MIT | 4 | 1.8 2.6 .0 -16 -9 -16 .32
NGS | 4 | 2.9 -1.1 -2.5 -4 1 19 .43
SIO | 4 | 2.5 6.1 54.7 120 70 152 .24
COD | 5 | -.5 .2 -1.3 -41 5 -19 .32
EMR | 5 | 9.4 5.7 7.8 -11 16 -11 -.04
ESA | 5 | 8.5 2.3 11.4 -10 -76 30 -.16
GFZ | 5 | .9 .3 -1.4 -23 -47 11 .15
GRG | 5 | 9.5 6.0 -18.4 -25 13 -13 .57
JPL | 5 | 2.6 3.8 11.1 -90 -12 18 .19
MIT | 5 | 6.8 6.7 2.8 -9 16 -41 .23
NGS | 5 | 1.4 2.3 9.5 -39 4 10 .66
SIO | 5 | 3.3 6.6 44.5 92 65 -117 .30
COD | 6 | -.8 .4 -1.7 -53 13 4 .11
EMR | 6 | 7.9 8.8 4.8 -6 25 -5 -.07
ESA | 6 | 6.7 11.6 6.0 -5 -55 60 -.07
GFZ | 6 | 1.1 .4 -.9 -34 -42 16 -.0
GRG | 6 | 5.2 8.1 -24.0 -31 28 -2 .44
JPL | 6 | 8.7 4.0 6.9 -108 -35 -36 .35
MIT | 6 | 7.3 6.5 6.3 -28 39 -37 .15
NGS | 6 | -.7 7.0 2.4 13 1 -1 .52
SIO | 6 | 2.1 7.1 39.1 57 72 -170 .07
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 1.1769.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1769.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 2.1769.[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 3.1769.[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 5.1769.0-6). 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 1769 summary. (Dec 01, 2013 - Dec 07, 2013)
Table 1.1769.a GPS week: 1769 MJD: 56627.000-56633.000
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 262| 1 0 3 6 26 9 .13 10 10 | -756 -305 17 128
| 0 0 2 15 20 11 .01 | 317 556
emr 79| 0 0 10 -25 18 -20 .04 15 15 | 2567 -540 17 134
| 1 0 2 13 15 12 .03 | 232 657
esa 150| 0 0 0 27 -32 18 -.21 5 5 | -1060 1473 9 140
| 0 0 0 14 19 19 .02 | 1349 1493
gfz 200| -2 0 -4 -24 -8 13 .08 10 10 | 157 -437 11 84
| 0 0 1 17 13 9 .04 | 398 979
grg 190| 1 0 -16 -8 14 3 .24 16 16 | 178 -448 17 151
| 1 1 5 27 32 15 .04 | 129 409
igr n/a| 0 0 0 5 29 0 -.18 5 4 | 3339 -969 15 80
| 0 0 0 14 7 9 .02 | 1268 629
jpl 80| 0 -1 3 -8 12 -38 .09 14 14 | 2524 -465 16 128
| 0 1 1 17 25 27 .03 | 303 619
mit 289| 1 -1 -3 1 0 -1 -.13 14 12 | -237 145 26 244
| 1 1 1 47 42 26 .04 | 623 952
ngs 240| 0 0 2 -15 34 -27 .13 12 9 | 301018 -185419 1767 3476
| 1 0 2 63 58 28 .02 | 709705 375780
sio 455| 0 1 6 126 199 180 -.59 19 19 | --- --- --- ---
| 1 1 0 60 145 246 .05 | --- ---
Table 1.1769.b GPS week : 1769 MJD: 56627.000-56633.000
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 5 4 5 5 5 5 |
2 | 4 5 4 4 4 4 5 |
3 | 4 4 5 5 6 4 4 |
4 | 3 3 3 4 3 3 3 |
5 | 4 4 5 5 5 4 5 |
6 | 4 4 4 4 5 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 3 4 4 4 |
9 | 3 3 3 3 4 3 3 |
10 | 3 3 3 4 4 4 3 |
11 | 4 5 4 4 4 4 4 |
12 | 5 5 5 5 6 5 6 |
13 | 4 3 4 4 4 4 4 |
14 | 4 4 3 4 4 3 4 |
15 | 4 4 4 5 6 5 5 |
16 | 6 6 6 5 5 5 4 |
17 | 4 4 4 4 4 5 4 |
18 | 4 4 4 4 4 4 4 |
19 | 5 5 4 5 5 5 4 |
20 | 5 5 5 5 5 5 5 |
21 | 4 4 4 4 4 3 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 4 4 4 4 4 |
24 | 4 6 8 4 5 4 4 |
25 | 5 4 4 4 13 4 4 |
26 | 7 8 7 8 8 7 7 |
27 | 5 5 5 5 5 4 4 |
28 | 4 4 4 5 5 4 5 |
29 | 4 4 4 4 4 4 4 |
30 | --- --- --- --- 0 0 0 |
31 | 4 4 5 4 4 4 5 |
32 | 4 3 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1769.0 GPS week: 1769 Day: 0 MJD: 56627.000
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 1 6 3 6 0 .14 10 10 | -606 -740 19 128
emr 80| -3 0 12 -22 10 -31 .01 15 15 | 2824 224 18 135
esa 150| 1 0 -1 32 -9 4 -.18 5 5 | -1770 2591 9 135
gfz 197| -2 0 -5 -50 1 21 .01 10 9 | 41 445 12 87
grg 193| 0 2 -26 12 -24 9 .30 17 16 | 224 -509 18 160
igr n/a| 0 0 0 -3 22 8 -.20 4 4 | 5223 -437 15 83
jpl 80| 0 0 6 -43 -2 -17 .11 13 13 | 2648 27 15 121
mit 232| 2 0 -1 31 -50 -1 -.16 15 12 | 178 -379 22 200
ngs 241| -2 0 1 -5 45 -5 .14 10 8 | -592 -740 2370 3790
sio 426| 0 2 8 183 176 289 -.64 18 16 | --- --- --- ---
Table 2.1769.1 GPS week: 1769 Day: 1 MJD: 56628.000
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 264| 1 1 3 7 11 10 .14 9 9 | -946 227 16 115
emr 80| 0 -1 12 -18 14 -13 .04 16 15 | 2686 -694 17 105
esa 150| 0 0 0 41 -18 -5 -.21 5 5 | 1111 -1166 7 119
gfz 203| -2 0 -1 -2 -29 -4 .07 10 9 | 427 -1188 10 69
grg 193| 1 1 -22 1 -16 5 .22 17 16 | -16 -184 17 150
igr n/a| 0 0 0 -3 18 5 -.22 4 4 | 4427 -945 14 70
jpl 80| 0 0 4 -8 2 -5 .12 13 13 | 2371 -552 16 146
mit 299| 2 -1 -3 -39 -51 5 -.18 15 12 | 270 -863 26 231
ngs 235| -1 0 0 -68 100 21 .14 13 11 | -969 232 1736 3219
sio 459| 0 1 7 196 206 483 -.62 18 15 | --- --- --- ---
Table 2.1769.2 GPS week: 1769 Day: 2 MJD: 56629.000
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 5 -13 -1 -8 .13 11 11 | -831 -305 17 119
emr 79| -1 0 12 -13 32 -16 .02 15 15 | 2249 -776 18 106
esa 150| 0 0 0 21 -26 26 -.23 6 6 | -2176 2011 9 128
gfz 203| -3 0 -6 -26 -7 9 .07 11 10 | -242 8 13 76
grg 192| 0 0 -16 7 74 -3 .25 16 15 | 269 -878 17 161
igr n/a| 0 0 0 3 38 -11 -.17 5 4 | 3866 -1298 15 73
jpl 80| 0 -2 3 6 51 -16 .10 14 13 | 2144 -644 16 120
mit 299| 2 -2 -3 40 64 -4 -.16 14 11 | -1400 2023 23 242
ngs 240| 0 0 1 -34 -81 -25 .14 11 8 | 210429 -296530 1378 3402
sio 460| 2 2 6 123 515 377 -.61 17 15 | --- --- --- ---
Table 2.1769.3 GPS week: 1769 Day: 3 MJD: 56630.000
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 265| 2 0 1 14 40 13 .11 11 10 | -285 -1277 17 136
emr 79| 1 0 11 -41 37 -14 .03 15 15 | 2378 -1224 20 156
esa 150| 0 0 0 49 -63 19 -.21 6 5 | -1610 1768 13 163
gfz 201| -3 0 -3 -38 6 9 .10 10 10 | 585 -2001 12 87
grg 191| 0 0 -11 -24 0 21 .23 16 15 | 359 -1123 17 151
igr n/a| 0 0 0 4 36 4 -.19 5 5 | 3244 -1873 16 83
jpl 80| 0 -3 3 -11 37 -57 .05 14 14 | 2257 -1264 17 126
mit 299| 1 -3 -3 -52 5 -33 -.12 14 13 | 99 -583 30 254
ngs 244| 0 0 1 9 47 -30 .12 13 9 | -383 -1083 1618 3895
sio 461| 1 2 6 99 178 273 -.59 18 20 | --- --- --- ---
Table 2.1769.4 GPS week: 1769 Day: 4 MJD: 56631.000
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 264| 1 0 1 30 51 27 .14 11 10 | -817 -10 18 130
emr 79| 0 0 10 -42 27 -34 .02 14 14 | 2789 -659 16 131
esa 150| 0 0 0 19 -24 16 -.20 6 5 | -2033 3110 12 145
gfz 201| -1 0 -4 -6 -21 23 .12 11 11 | -487 620 12 99
grg 188| 1 -1 -13 26 20 4 .17 18 17 | 38 -28 18 141
igr n/a| 0 0 1 2 35 6 -.18 5 5 | 2920 -1226 17 85
jpl 80| -1 0 3 -10 14 -64 .06 14 14 | 2643 -467 15 122
mit 299| 0 -2 -4 64 -8 33 -.11 14 11 | -792 392 34 282
ngs 241| 1 -1 0 -114 5 -34 .14 14 12 | 1900551 -999999 1658 3017
sio 450| -2 0 6 172 110 117 -.60 18 20 | --- --- --- ---
Table 2.1769.5 GPS week: 1769 Day: 5 MJD: 56632.000
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 259| 1 0 2 -13 42 12 .14 10 9 | -535 -324 15 134
emr 80| 1 1 7 -35 20 -1 .06 15 15 | 2360 498 16 141
esa 150| 1 1 0 10 -51 15 -.21 5 5 | 650 87 9 142
gfz 201| -3 1 -5 -28 0 19 .09 11 11 | 353 95 13 90
grg 187| 2 -1 -14 -41 16 14 .26 16 17 | 183 -217 18 153
igr n/a| -1 0 0 -5 27 7 -.16 5 5 | 1853 75 16 91
jpl 80| 0 -1 3 -5 2 -30 .10 14 14 | 2552 601 17 139
mit 300| 0 0 -3 12 4 24 -.07 11 10 | -118 325 29 269
ngs 238| -1 0 8 76 57 -66 .13 12 9 | -659 -93 1717 3569
sio 465| -2 0 6 84 107 -99 -.51 19 22 | --- --- --- ---
Table 2.1769.6 GPS week: 1769 Day: 6 MJD: 56633.000
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 259| 1 0 2 13 35 11 .13 11 10 | -1273 289 17 140
emr 80| 0 0 7 -7 -9 -29 .09 15 15 | 2686 -1150 16 165
esa 150| 1 0 0 18 -36 56 -.20 6 5 | -1596 1914 10 149
gfz 199| -1 0 -2 -17 -11 17 .12 11 11 | 423 -1044 10 83
grg 190| 3 0 -12 -41 28 -26 .26 15 15 | 190 -201 16 146
igr n/a| 0 0 1 36 28 -15 -.15 4 4 | 1841 -1079 13 80
jpl 80| 0 -1 2 12 -21 -77 .08 15 14 | 3056 -961 16 122
mit 299| 1 0 -2 -45 34 -35 -.14 12 12 | 98 104 24 231
ngs 244| -2 0 2 28 65 -49 .09 12 10 | -1250 277 1898 3443
sio 464| -2 1 7 28 99 -180 -.53 21 22 | --- --- --- ---
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 3.1769.0 GPS week: 1769 Day: 0 MJD: 56627.000
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 | 13 13 4 13 12 5 19 23 8 26 4 | 60 63 63 63 77 60 73 61 61 56 63
2 | 9 10 5 8 15 5 11 15 5 29 3 | 26 27 30 36 36 27 29 37 29 23 30
3 | 9 13 6 9 18 4 9 19 10 16 4 | 22 20 18 16 23 17 23 29 23 24 18
4 | 8 11 4 8 14 4 9 15 6 15 3 | 30 27 33 37 42 31 29 38 31 25 32
5 | 11 17 4 11 18 6 14 12 10 15 4 | 37 46 31 33 39 33 41 28 33 34 33
6 | 9 11 6 9 16 4 10 20 11 25 4 | 33 26 29 26 33 28 31 40 31 35 29
7 | 12 12 5 8 14 3 11 17 7 23 3 | 29 28 25 28 31 23 27 29 29 30 26
8 | 7 9 6 8 12 3 9 9 9 18 3 | 19 19 17 19 19 16 21 15 17 19 17
9 | 5 10 5 7 11 3 10 12 7 12 3 | 17 18 14 16 16 14 21 13 16 13 14
10 | 7 12 4 6 15 3 8 12 9 32 3 | 24 24 25 31 32 24 26 27 23 34 25
11 | 10 18 3 10 14 3 13 20 9 20 4 | 52 54 53 54 66 51 55 53 50 48 52
12E | 11 20 5 15 19 5 21 16 8 16 5 | 45 50 45 55 47 47 52 51 47 45 47
13E | 8 11 3 9 21 3 13 11 9 12 3 | 72 70 70 71 73 69 72 73 69 74 70
14E | 9 13 5 10 15 4 10 8 7 10 3 | 29 27 25 29 30 26 29 26 26 26 26
15E | 8 15 5 11 19 5 15 9 11 12 4 | 41 33 36 40 39 34 35 37 39 31 36
16E | 11 26 5 15 27 5 15 21 9 14 5 | 34 40 32 36 44 32 35 37 34 31 33
17 | 10 16 6 8 18 3 14 13 8 10 4 | 19 22 16 22 33 17 21 24 24 11 19
18 | 13 15 4 9 18 4 16 12 7 20 4 | 27 27 26 34 41 24 28 26 27 19 27
19 | 13 18 6 11 18 6 16 22 8 18 5 | 84 76 85 81 81 82 79 75 85 78 81
20 | 12 17 7 9 14 4 17 17 9 23 4 | 39 41 43 42 52 42 43 39 42 31 41
21 | 11 11 4 7 17 4 12 10 11 25 3 | 26 26 28 31 38 27 26 26 35 25 28
22 | 8 14 4 8 16 3 13 10 9 14 3 | 37 38 39 43 55 39 38 39 41 35 39
23E | 11 17 5 9 26 4 14 16 10 16 4 | 48 47 46 47 48 46 47 52 48 54 46
24 | 10 16 5 8 14 4 14 13 11 10 4 | 20 22 18 28 24 18 25 17 24 14 19
25E | 13 22 5 10 15 5 14 14 8 12 4 | 80 84 81 81 82 79 82 76 81 79 81
26E | 19 20 12 13 16 9 18 15 31 20 7 | 96 95 98 95 96 94 96 95 102 95 95
X27 | 9 14 7 10 --- 5 13 24 11 19 5 | 48 45 44 40 --- 44 48 57 49 47 45
28E | 7 11 6 10 18 4 11 13 12 14 4 | 30 32 27 32 30 28 28 28 31 28 28
29 | 8 17 4 9 17 3 14 13 7 17 4 | 28 28 21 26 32 23 27 21 28 19 23
31 | 11 15 5 10 19 4 13 12 10 18 4 | 32 29 26 33 36 26 29 28 28 26 28
32 | 11 14 4 9 15 3 8 8 10 11 3 | 26 27 21 26 31 22 25 18 25 18 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 5 10 17 4 13 15 10 18 |T 39 39 37 40 44 36 40 39 39 36 37
WRMS | 10 15 5 9 16 4 13 12 8 16 |NE 33 34 32 35 40 31 36 32 34 29 32
MEDI | 10 14 5 9 16 4 13 13 9 16 |MD 32 29 30 34 38 28 29 37 31 31 30
Table 3.1769.1 GPS week: 1769 Day: 1 MJD: 56628.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 13 5 13 11 5 22 21 11 22 4 | 42 47 41 37 55 39 59 43 41 42 42
2 | 11 12 6 14 16 3 13 16 14 29 4 | 22 17 20 30 21 20 22 29 32 21 22
3M | 8 13 5 11 16 4 10 22 8 15 4 | 18 25 16 21 20 17 23 23 23 22 17
4 | 7 10 4 6 13 4 10 15 10 12 3 | 21 17 19 21 24 17 21 27 24 20 20
5 | 6 12 4 9 15 4 13 13 10 12 3 | 33 35 29 30 34 30 39 31 35 31 31
6M | 8 13 5 10 15 5 9 21 10 23 4 | 37 43 37 43 39 38 35 39 43 44 38
7 | 9 14 5 8 16 2 13 19 13 22 4 | 33 30 26 29 35 26 31 32 31 28 28
8 | 5 10 5 5 9 3 10 12 10 18 3 | 19 18 16 18 17 15 21 16 20 21 16
9 | 4 10 5 7 8 3 8 11 11 11 3 | 17 17 14 17 15 13 21 16 18 14 15
10 | 5 10 4 6 11 3 8 14 9 29 3 | 21 19 17 20 24 16 21 22 21 29 19
11 | 10 17 5 9 17 3 14 17 12 15 4 | 38 48 39 40 54 39 45 45 34 42 39
12E | 11 18 5 13 14 6 18 19 13 17 5 | 34 31 27 35 33 29 32 28 36 30 29
13E | 6 12 3 6 17 3 9 12 10 14 3 | 74 73 73 75 75 71 73 71 73 74 73
14E | 13 13 6 8 13 5 10 9 14 10 4 | 30 26 25 31 30 25 29 26 34 27 27
15E | 9 14 4 10 17 5 13 12 9 12 3 | 36 31 31 36 36 30 34 31 34 29 32
16E | 9 20 6 16 34 5 17 24 12 14 6 | 33 32 30 29 46 29 32 42 36 26 30
17 | 11 15 6 8 17 4 14 13 15 8 4 | 22 21 16 22 32 15 24 24 23 12 18
18 | 10 17 5 9 15 4 14 10 13 20 4 | 21 22 18 24 30 16 24 17 23 9 19
19 | 9 17 5 11 22 4 15 12 9 19 4 | 107 113 106 110 96 108 107 108 108 115 107
20 | 10 18 6 11 12 2 16 19 10 24 4 | 33 34 32 30 39 31 40 34 35 25 32
21M | 11 11 6 9 18 4 11 10 10 24 3 | 19 17 18 21 23 14 20 16 21 18 17
22M | 11 15 4 10 19 3 12 11 17 14 4 | 30 31 29 33 44 28 34 27 38 24 30
23E | 7 17 6 10 26 4 12 18 12 20 4 | 43 38 40 43 41 38 41 36 41 35 39
X24 | 12 16 6 --- 16 5 --- 20 12 --- 5 | 24 23 22 --- 27 19 --- 23 24 --- 22
25 | 9 19 6 11 14 6 15 12 14 8 4 | 39 45 38 43 43 40 42 40 40 38 39
26E | 19 39 10 14 17 9 16 17 35 18 7 | 99 110 100 99 99 98 96 101 100 98 99
X27M | 14 13 5 11 --- 6 14 22 10 18 5 | 56 62 56 62 --- 58 53 56 61 59 57
28E | 6 10 5 7 19 3 16 15 8 12 3 | 38 35 33 33 38 32 37 33 37 32 34
29 | 10 15 5 8 16 4 13 11 8 13 3 | 27 27 21 26 27 19 25 22 25 17 22
31 | 9 16 5 10 20 5 15 14 10 18 4 | 30 30 23 32 37 23 29 28 28 25 26
32 | 7 13 4 6 12 3 7 7 7 11 2 | 21 26 19 23 24 18 26 19 23 16 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 5 10 17 4 13 15 13 18 |T 36 36 33 37 38 32 37 35 37 34 34
WRMS | 9 15 5 9 16 4 13 12 11 15 |NE 32 33 29 32 35 28 36 32 32 30 30
MEDI | 9 14 5 9 16 4 13 14 10 15 |MD 33 31 27 30 34 28 32 29 34 27 29
Table 3.1769.2 GPS week: 1769 Day: 2 MJD: 56629.000
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 12 12 6 19 14 11 18 4 | 43 49 44 49 57 48 59 46 50 43 48
2 | 10 13 6 15 16 5 11 14 7 28 4 | 33 30 32 34 29 32 29 35 31 27 31
3 | 7 12 4 12 16 5 12 26 6 16 4 | 40 43 40 42 41 40 43 41 40 39 40
4M | 9 9 5 7 11 3 7 14 9 14 3 | 30 27 29 28 30 27 27 31 26 25 28
5 | 8 16 7 10 17 4 15 13 11 12 4 | 36 37 32 25 28 29 34 30 36 27 31
6M | 10 12 5 9 13 5 12 20 8 24 4 | 31 27 25 26 30 25 30 36 28 34 26
7 | 11 13 5 9 14 2 13 16 6 22 4 | 45 42 37 39 41 36 36 36 39 32 39
8 | 9 9 3 7 9 4 7 13 7 19 3 | 25 22 17 20 18 19 21 18 21 23 20
9 | 10 9 4 7 9 4 7 12 7 11 3 | 27 23 19 22 17 20 21 21 22 18 21
10 | 8 10 6 10 12 3 9 12 7 28 3 | 27 24 23 28 25 23 24 27 27 30 25
11 | 11 16 5 10 17 4 13 11 7 13 4 | 37 42 36 43 48 39 42 38 39 35 39
12E | 12 21 5 13 11 5 20 22 8 16 5 | 52 52 48 53 49 44 50 49 49 44 49
13E | 7 12 5 9 22 4 11 14 9 18 4 | 83 85 82 83 82 80 86 84 84 84 83
14E | 9 12 4 9 13 3 10 7 7 9 3 | 35 30 32 36 38 31 32 31 33 29 33
15E | 11 13 6 9 18 4 13 9 15 10 4 | 36 33 29 35 37 32 31 31 44 26 34
16E | 11 23 6 13 24 4 18 24 10 13 5 | 29 27 22 26 36 22 26 37 29 20 24
17 | 16 14 6 10 16 4 16 11 8 9 4 | 25 26 20 22 30 19 23 22 24 14 22
18 | 11 16 6 9 15 5 13 10 10 20 4 | 22 25 22 31 32 21 27 23 26 17 24
19 | 9 18 6 11 20 7 13 11 6 21 4 | 92 86 93 89 91 89 91 98 89 91 90
20 | 14 17 8 19 18 3 16 13 6 24 5 | 31 35 33 39 39 33 37 34 33 30 33
21 | 10 10 7 8 14 6 10 8 10 23 3 | 28 25 29 31 29 26 25 24 32 21 28
22M | 12 13 4 9 16 4 13 8 8 13 3 | 27 30 28 34 40 27 34 29 26 25 29
23E | 10 13 4 10 21 3 14 13 6 16 4 | 52 52 50 54 49 51 54 55 53 54 51
X24 | 15 19 --- 110 16 7 --- 21 10 --- 8 | 27 24 --- 94 27 20 --- 23 25 --- 23
25 | 10 20 5 10 14 5 15 9 7 11 4 | 32 35 29 29 33 29 40 29 28 33 30
26E | 22 18 11 13 13 9 18 18 33 17 7 | 53 57 53 54 52 54 53 45 69 54 54
X27 | 12 12 5 11 --- 6 15 25 8 22 5 | 38 35 35 28 --- 32 40 51 34 44 35
28E | 12 12 6 11 15 3 18 15 7 13 4 | 47 46 43 44 46 44 45 44 47 49 44
29 | 9 19 5 8 14 2 15 12 9 16 4 | 27 29 23 24 26 21 22 22 25 22 23
31M | 15 18 6 10 16 5 15 11 11 20 4 | 39 33 30 37 44 29 35 34 33 29 34
32 | 12 13 5 7 17 4 9 9 10 9 3 | 21 24 21 23 23 20 23 20 25 18 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 11 16 5 14 14 10 17 |T 37 37 35 39 38 34 38 36 37 34 35
WRMS | 11 15 6 10 15 4 13 11 8 15 |NE 34 34 32 38 35 31 34 32 34 30 32
MEDI | 10 13 5 10 15 4 13 13 8 16 |MD 33 33 30 34 36 29 34 34 33 29 31
Table 3.1769.3 GPS week: 1769 Day: 3 MJD: 56630.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 13 3 16 16 8 22 13 11 17 4 | 48 52 52 51 61 50 65 52 52 52 52
2 | 9 12 6 13 15 4 11 13 5 29 3 | 17 17 20 30 21 18 23 25 21 17 20
3 | 7 12 5 11 20 3 10 23 13 18 4 | 33 27 29 27 30 28 32 41 33 34 29
4 | 10 9 7 7 15 4 9 14 9 13 3 | 24 21 23 27 28 20 23 28 20 22 23
5 | 16 16 7 10 15 5 15 13 8 14 4 | 37 41 34 33 34 32 40 29 34 35 33
6 | 9 12 5 10 14 4 11 17 12 24 4 | 28 28 26 31 27 25 27 29 25 32 26
7 | 12 13 4 8 17 4 13 19 11 24 4 | 34 34 32 32 40 31 31 36 36 34 32
8 | 9 8 4 5 11 4 10 13 10 18 3 | 23 22 18 19 20 19 21 18 23 26 20
9 | 7 9 5 4 11 4 8 14 9 12 3 | 22 20 18 19 18 16 20 18 21 18 19
10 | 8 12 6 6 12 3 9 15 8 27 3 | 19 19 21 24 25 19 21 24 20 29 20
11 | 9 17 4 11 16 7 14 9 14 16 4 | 45 49 44 47 57 42 49 46 40 46 45
12 | 10 23 5 9 19 4 19 18 11 17 5 | 45 49 42 50 56 44 47 46 44 43 45
13E | 8 11 3 8 15 5 11 13 9 13 3 | 32 29 26 31 31 26 30 25 32 21 27
14E | 10 12 6 8 16 5 12 10 9 13 3 | 27 25 23 27 26 23 28 20 31 26 24
15E | 10 13 4 7 17 4 18 25 15 13 5 | 41 39 38 42 39 38 42 45 46 42 40
16E | 7 15 5 13 18 3 15 16 10 15 4 | 50 49 48 53 52 47 48 56 49 50 49
17 | 10 16 5 10 17 4 14 13 12 11 4 | 25 25 17 22 30 19 24 22 28 15 21
18 | 10 14 5 9 14 3 13 8 8 21 3 | 24 27 23 31 34 21 28 25 25 17 25
19 | 9 21 7 9 22 5 18 12 10 22 4 | 63 64 64 66 60 64 62 66 62 70 62
20 | 12 18 6 12 15 6 20 15 11 24 4 | 36 36 34 38 41 36 39 34 37 30 34
21 | 11 19 8 8 12 5 11 9 7 24 4 | 24 24 25 24 28 22 25 23 24 21 22
22 | 9 13 5 6 13 3 12 8 12 13 3 | 37 37 37 40 46 37 38 39 35 34 37
23E | 6 11 4 10 19 4 14 13 9 12 3 | 34 32 29 33 27 29 32 28 36 24 30
24 | 10 13 6 8 13 6 14 19 9 11 4 | 19 24 19 26 25 19 29 24 24 17 20
X25 | 8 19 5 7 13 3 --- 11 9 --- 4 | 31 35 26 28 39 28 --- 31 27 --- 30
26E | 23 18 13 14 14 8 19 20 41 17 8 | 112 115 113 113 113 112 109 113 118 115 112
X27 | 11 13 6 11 --- 5 14 13 13 22 4 | 48 49 47 50 --- 46 47 48 49 50 47
28 | 20 14 5 11 12 11 18 13 14 27 5 | 105 98 102 104 100 95 106 98 104 88 101
29 | 9 18 5 5 13 4 16 10 11 12 4 | 28 28 21 25 28 22 28 22 26 20 23
31 | 10 16 6 9 17 5 13 10 12 20 4 | 31 34 28 35 37 29 33 28 33 31 30
32 | 9 13 4 9 17 5 10 10 12 10 3 | 21 25 19 21 24 18 23 17 23 14 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 10 16 5 14 14 13 18 |T 37 37 35 38 39 34 39 37 38 35 36
WRMS | 10 15 5 10 15 5 14 13 9 20 |NE 30 32 29 32 34 28 33 30 31 29 29
MEDI | 9 13 5 9 15 4 13 13 11 17 |MD 32 32 28 31 31 28 31 29 33 30 30
Table 3.1769.4 GPS week: 1769 Day: 4 MJD: 56631.000
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 12 4 20 16 6 21 7 11 21 4 | 43 49 44 44 57 43 61 45 50 43 46
2 | 10 10 6 12 15 4 13 9 11 29 4 | 20 19 21 27 21 18 19 24 25 17 20
3 | 9 11 7 13 26 6 13 26 13 16 5 | 78 82 80 82 74 79 83 87 81 80 80
4 | 7 9 5 10 14 4 10 8 12 17 3 | 23 22 23 28 28 20 25 27 24 19 23
5 | 10 16 7 13 16 5 16 11 15 15 4 | 27 35 24 20 27 24 33 22 37 28 26
6 | 9 20 4 13 19 4 15 16 13 24 5 | 19 31 21 25 19 21 25 19 28 25 21
7 | 11 13 5 8 17 3 12 12 10 23 4 | 26 26 20 24 30 19 23 22 28 21 22
8 | 9 10 4 6 11 5 8 15 12 21 3 | 21 20 16 19 15 16 18 20 19 21 17
9 | 7 9 5 7 13 4 7 14 13 14 3 | 17 19 15 17 14 13 16 15 20 13 15
10 | 12 11 6 8 12 4 9 10 13 28 3 | 22 19 20 25 25 19 18 23 24 29 20
11 | 8 17 5 14 18 5 13 7 12 15 4 | 37 43 37 41 48 35 45 41 40 37 39
12 | 10 21 6 12 21 5 22 18 13 15 5 | 34 37 29 37 40 31 34 31 39 25 31
13E | 9 10 5 8 18 3 9 11 10 13 3 | 33 36 26 33 38 27 33 26 34 20 29
14E | 9 11 7 8 17 5 11 8 13 11 3 | 23 22 21 26 26 21 21 18 27 21 21
15E | 11 13 5 9 16 6 16 29 15 14 5 | 54 44 48 50 53 45 46 46 51 46 47
16 | 8 18 4 15 19 3 15 20 15 22 5 | 41 47 42 44 48 41 45 41 40 36 41
17 | 15 11 5 9 15 4 12 11 9 10 4 | 24 24 16 19 30 18 21 23 25 14 19
18 | 9 13 6 11 16 4 15 9 12 20 4 | 24 27 23 32 31 22 28 24 27 15 25
19 | 8 13 6 14 20 5 13 13 12 23 4 | 36 41 36 44 29 38 41 37 40 48 37
20 | 12 18 8 11 13 5 13 10 11 24 4 | 27 32 30 31 35 27 35 30 34 23 29
21 | 10 10 5 7 15 3 11 8 14 22 3 | 18 19 18 20 22 18 18 19 27 19 18
22 | 8 12 5 9 17 4 11 9 12 14 3 | 30 31 28 33 38 27 30 30 30 25 29
23E | 8 14 5 9 29 4 10 10 8 11 4 | 34 31 28 35 32 28 31 27 33 21 29
24 | 10 14 4 7 16 6 13 20 16 13 4 | 26 27 21 24 31 23 27 24 32 14 23
X25 | 15 18 --- --- 45 12 --- 19 27 --- 12 | 31 32 --- --- 65 32 --- 28 41 --- 31
26E | 27 18 11 14 16 8 20 20 41 21 8 | 115 110 111 111 113 111 115 110 112 111 110
X27 | 13 14 6 11 --- 4 16 13 13 23 4 | 36 40 35 34 --- 34 36 27 38 31 34
28 | 9 14 5 15 22 5 19 16 13 15 5 | 60 62 56 62 64 61 59 58 66 51 59
29 | 9 16 5 7 12 5 17 11 11 13 4 | 27 28 23 24 25 21 25 21 32 17 23
X30 | 4 --- --- --- --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
31 | 10 14 5 12 22 6 13 11 11 21 4 | 28 28 20 29 37 20 25 21 28 22 23
32 | 11 11 5 8 17 5 10 6 10 9 3 | 21 22 16 21 20 18 22 16 24 13 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 6 11 18 5 14 14 14 18 |T 34 35 31 35 37 31 35 32 37 30 32
WRMS | 10 14 5 11 17 5 14 11 12 20 |NE 26 28 24 27 29 23 28 25 30 23 25
MEDI | 9 13 5 10 16 5 13 11 12 16 |MD 27 31 23 29 31 24 28 26 32 22 26
Table 3.1769.5 GPS week: 1769 Day: 5 MJD: 56632.000
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 12 6 23 16 8 20 9 9 21 5 | 45 49 44 43 54 41 59 45 44 45 45
2 | 12 11 5 15 17 4 16 8 11 28 4 | 17 14 16 25 16 14 22 17 22 11 16
3 | 8 11 4 12 17 5 11 13 8 16 3 | 50 52 49 52 50 51 53 51 54 51 50
4 | 8 10 4 7 16 5 9 9 6 21 3 | 20 16 20 23 25 17 20 23 24 15 20
5 | 7 18 7 11 15 4 16 8 10 16 4 | 22 30 21 19 26 20 28 20 25 24 21
6 | 11 13 4 12 16 5 14 10 12 21 4 | 21 23 18 23 20 19 25 17 25 25 19
7 | 12 17 5 10 16 4 13 12 8 24 4 | 31 27 23 27 34 22 25 21 30 21 24
8 | 10 11 4 10 13 5 9 10 9 22 3 | 23 21 19 22 21 19 21 20 22 25 19
9 | 7 9 4 6 12 4 9 10 8 16 3 | 18 18 16 17 18 14 19 18 20 17 16
10 | 7 11 4 8 15 5 10 10 13 29 3 | 19 18 18 24 25 16 23 21 23 31 19
11 | 9 16 3 15 15 5 14 9 15 15 4 | 32 37 28 29 39 25 36 30 29 29 30
12 | 9 27 6 12 19 4 22 14 7 16 5 | 27 32 22 31 36 23 31 26 29 21 25
13E | 5 11 3 8 20 3 13 8 8 22 3 | 36 37 31 37 43 32 36 31 38 31 33
14E | 8 12 4 7 13 6 13 9 9 14 3 | 24 18 17 23 20 16 22 15 24 15 18
15E | 9 19 6 9 21 4 15 20 13 15 5 | 51 46 48 50 49 47 48 52 53 49 49
16 | 9 14 6 12 18 4 15 16 11 19 4 | 30 28 27 29 31 26 31 34 32 30 28
17 | 16 16 5 8 16 5 15 10 15 12 4 | 23 20 15 21 31 18 23 21 30 13 19
18 | 7 15 4 13 12 3 14 9 9 18 3 | 21 25 18 31 26 19 25 21 22 11 21
19 | 8 17 4 15 19 5 16 10 11 23 4 | 39 42 40 45 39 40 44 44 42 50 40
20 | 12 19 6 11 15 4 15 12 14 26 4 | 28 33 26 25 35 25 33 28 34 22 26
21 | 7 10 5 8 13 3 11 9 9 23 3 | 19 16 15 19 16 13 14 15 18 17 15
22 | 6 12 4 10 14 5 13 9 13 17 3 | 26 28 24 29 34 24 30 26 25 25 25
23E | 9 15 5 10 25 5 14 8 9 12 4 | 34 28 27 32 28 26 31 27 36 19 28
24 | 9 14 6 8 15 7 14 13 11 14 4 | 21 22 16 23 28 17 29 23 20 15 19
25 | 7 17 5 9 20 4 16 12 8 11 4 | 26 28 28 30 37 25 32 25 32 25 25
26E | 23 19 8 10 15 8 20 13 35 17 7 | 175 172 174 172 171 173 175 169 179 171 173
X27 | 11 13 5 13 --- 4 17 8 11 21 4 | 42 36 36 37 --- 36 39 32 41 38 36
28 | 10 13 6 10 17 3 15 12 12 14 4 | 32 28 27 30 38 26 30 29 36 23 29
29 | 10 17 5 8 13 4 15 11 11 14 4 | 22 21 17 19 23 16 19 20 26 13 18
X30 | 4 --- --- --- --- 96 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
31 | 7 15 5 10 20 4 15 11 11 22 4 | 27 26 19 27 36 21 28 22 26 19 23
32 | 12 10 5 10 14 4 8 9 12 10 3 | 20 21 14 18 21 14 19 16 23 10 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 5 11 16 5 14 11 12 19 |T 32 32 29 33 35 28 34 30 34 29 30
WRMS | 9 15 5 11 17 5 14 10 9 22 |NE 25 26 22 25 29 21 28 24 27 22 23
MEDI | 9 14 5 10 16 4 14 10 11 17 |MD 26 28 22 27 31 22 29 23 29 23 24
Table 3.1769.6 GPS week: 1769 Day: 6 MJD: 56633.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 11 4 18 11 6 22 10 11 26 4 | 59 61 57 57 72 56 72 64 54 57 59
2 | 13 13 8 18 15 4 12 7 10 29 4 | 22 21 29 36 26 23 26 28 26 15 25
3 | 9 13 5 11 18 4 12 11 10 18 4 | 54 53 48 48 52 48 53 55 49 56 49
4 | 9 8 5 10 13 4 10 11 8 21 3 | 31 29 33 36 37 29 32 35 31 25 31
5 | 16 19 7 9 15 5 15 8 8 17 4 | 40 45 35 30 31 33 43 32 38 37 35
6 | 9 12 6 12 14 5 11 13 11 25 4 | 26 28 21 25 23 20 27 23 21 31 21
7 | 11 14 5 8 16 3 15 11 13 25 4 | 32 27 23 26 32 22 29 25 23 22 24
8 | 8 9 5 6 13 4 11 11 12 21 3 | 25 25 20 24 22 20 25 26 21 29 21
9 | 7 10 5 7 12 3 10 11 11 16 3 | 23 23 17 21 19 18 22 23 18 21 18
10 | 6 10 5 7 15 4 9 12 9 30 3 | 27 22 24 30 33 23 23 27 23 34 24
11 | 10 16 5 14 15 5 13 9 9 21 4 | 44 50 47 48 60 44 52 51 41 46 47
12 | 11 26 6 13 18 5 22 14 10 17 5 | 46 44 40 49 50 41 46 42 43 36 42
13E | 7 13 4 9 13 4 12 10 9 23 3 | 37 36 30 36 41 31 38 34 33 35 33
14E | 12 14 6 7 11 4 15 15 8 12 4 | 23 18 19 24 21 18 23 27 22 16 19
15E | 11 17 6 8 17 5 17 13 15 17 4 | 54 45 48 52 52 46 47 46 52 46 48
16 | 10 20 4 12 17 4 16 11 8 22 4 | 42 44 43 46 46 43 45 45 42 38 42
17 | 14 13 5 7 15 4 18 12 10 12 4 | 27 28 20 26 36 23 27 27 27 16 23
18 | 8 16 5 11 13 4 15 11 9 22 4 | 25 25 25 34 35 21 29 26 21 15 25
19 | 11 13 4 13 19 5 16 12 10 23 4 | 47 44 46 47 47 44 45 52 45 51 44
20 | 12 15 5 13 14 4 17 11 15 25 4 | 35 37 35 40 41 36 40 38 35 31 35
21 | 10 11 7 7 11 5 11 15 8 25 3 | 20 19 20 23 25 18 20 22 19 22 19
22 | 7 12 5 8 13 4 12 10 13 23 3 | 31 33 33 37 43 30 35 34 29 33 32
23E | 8 13 4 10 19 5 15 17 10 17 4 | 37 31 29 37 32 30 33 34 36 24 31
24 | 10 13 4 9 13 5 11 14 13 17 4 | 25 23 19 20 30 20 29 19 26 15 21
25 | 14 15 6 6 13 5 16 12 7 11 4 | 23 27 23 24 31 22 31 23 22 19 23
26E | 20 19 12 11 16 6 14 14 39 20 7 | 157 162 159 163 165 161 164 161 168 162 161
X27 | 13 13 4 12 --- 5 12 10 12 29 4 | 49 42 39 38 --- 37 43 39 38 49 39
28 | 6 15 6 12 17 4 21 14 13 17 4 | 49 48 47 53 54 48 47 50 51 43 48
29 | 10 16 4 7 11 5 17 12 7 15 4 | 29 26 21 23 26 21 25 23 24 19 22
X30 | 3 --- --- --- --- 131 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
31 | 11 17 5 12 20 4 16 10 9 22 4 | 26 25 19 29 38 20 30 24 25 19 23
32 | 8 10 4 12 15 4 12 11 8 13 3 | 21 22 16 22 23 16 25 19 21 13 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 6 11 15 4 15 12 12 21 |T 38 37 35 38 41 34 39 37 36 34 35
WRMS | 10 14 5 11 15 4 14 12 10 22 |NE 32 31 28 32 35 28 34 32 29 28 29
MEDI | 10 13 5 10 15 4 15 11 10 21 |MD 31 29 29 36 35 29 32 32 29 31 31
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 4.1769 GPS week: 1769 MJD: 56627.0-56633.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2990 |U 5 5 11 |U 8 9 30 |U 7 7 13 |
emr | emr 2968 | 9 7 18 |U 10 9 28 | 9 7 17 |
esa | esa 2948 | 6 6 16 |U 8 10 30 | 8 7 16 |
gfz | gfz 2934 |U 6 6 16 |U 8 10 31 |U 9 7 16 |
grg | grg 2862 |U 11 10 38 |U 10 17 39 |U 12 13 24 |
igr | igr 2958 | 6 5 15 | 7 9 30 | 7 6 14 |
igs | igs 2970 | 6 5 14 | 8 9 29 | 7 6 15 |
jpl | jpl 2916 | 9 8 21 |U 8 10 31 | 9 8 16 |
mit | mit 2976 | 12 9 25 |U 8 10 33 |U 15 15 26 |
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 5.1769.0 GPS week: 1769 Day: 0 MJD: 56627.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 5 11 | 11 14 37 | 9 8 16 |
emr | emr 2972 | 10 7 19 | 12 12 37 | 12 9 19 |
esa | esa 2976 | 6 5 13 | 10 14 36 | 9 9 16 |
gfz | gfz 2972 | 7 6 13 | 10 13 38 | 9 7 16 |
grg | grg 2880 | 10 10 41 | 14 25 49 | 13 11 33 |
igr | igr 2976 | 6 5 14 | 10 13 35 | 9 8 16 |
igs | igs 2975 | 7 5 13 | 10 13 35 | 9 8 15 |
jpl | jpl 2972 | 9 12 17 | 11 14 39 | 10 9 17 |
mit | mit 2976 | 12 6 14 | 9 14 34 | 11 13 18 |
Table 5.1769.1 GPS week: 1769 Day: 1 MJD: 56628.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 5 8 | 6 7 32 | 8 9 12 |
emr | emr 2972 | 8 8 17 | 9 7 25 | 10 8 14 |
esa | esa 2976 | 5 5 14 | 6 8 31 | 8 8 13 |
gfz | gfz 2876 | 7 6 22 | 7 9 31 | 9 9 15 |
grg | grg 2880 | 10 11 53 | 9 19 39 | 14 15 24 |
igr | igr 2976 | 6 5 14 | 6 7 30 | 8 7 12 |
igs | igs 2975 | 5 4 14 | 6 7 30 | 8 8 12 |
jpl | jpl 2876 | 10 8 39 | 7 8 31 | 10 8 16 |
mit | mit 2976 | 14 5 21 | 7 10 34 | 10 14 15 |
Table 5.1769.2 GPS week: 1769 Day: 2 MJD: 56629.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2970 | 4 3 8 | 8 11 21 | 6 5 11 |
emr | emr 2960 | 10 6 26 | 9 11 18 | 8 5 18 |
esa | esa 2880 | 6 4 22 | 9 11 22 | 8 7 17 |
gfz | gfz 2946 | 5 5 21 | 9 10 23 | 7 7 17 |
grg | grg 2871 | 9 9 33 | 9 19 31 | 10 11 23 |
igr | igr 2952 | 6 4 18 | 8 10 21 | 5 5 14 |
igs | igs 2959 | 6 3 21 | 8 10 21 | 6 5 16 |
jpl | jpl 2876 | 9 9 22 | 9 11 20 | 8 6 18 |
mit | mit 2976 | 16 10 60 | 7 11 22 | 8 10 17 |
Table 5.1769.3 GPS week: 1769 Day: 3 MJD: 56630.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 2 10 | 5 7 24 | 7 6 12 |
emr | emr 2972 | 9 5 14 | 8 8 23 | 10 9 19 |
esa | esa 2976 | 6 5 16 | 6 8 22 | 8 6 16 |
gfz | gfz 2958 | 6 3 12 | 6 7 22 | 9 8 14 |
grg | grg 2851 | 20 11 41 | 7 14 34 | 12 14 24 |
igr | igr 2970 | 6 4 14 | 6 7 23 | 7 6 15 |
igs | igs 2973 | 6 3 11 | 5 7 22 | 8 6 15 |
jpl | jpl 2874 | 9 7 14 | 5 8 26 | 10 8 15 |
mit | mit 2976 | 12 11 26 | 9 9 33 | 12 14 21 |
Table 5.1769.4 GPS week: 1769 Day: 4 MJD: 56631.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2969 | 8 6 17 | 7 8 33 | 6 7 16 |
emr | emr 2962 | 9 7 16 | 10 7 34 | 8 6 15 |
esa | esa 2880 | 6 6 16 | 7 8 34 | 6 6 18 |
gfz | gfz 2876 | 6 6 13 | 8 8 37 | 6 7 18 |
grg | grg 2852 | 11 10 50 | 10 17 42 | 12 13 20 |
igr | igr 2880 | 6 6 17 | 7 8 35 | 6 6 16 |
igs | igs 2960 | 6 5 13 | 7 7 31 | 6 5 16 |
jpl | jpl 2876 | 9 9 17 | 8 9 37 | 8 7 15 |
mit | mit 2976 | ---- ---- ---- | 8 8 33 | 42 29 76 |
Table 5.1769.5 GPS week: 1769 Day: 5 MJD: 56632.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 4 7 11 | 8 11 25 | 8 7 13 |
emr | emr 2972 | 10 8 19 | 12 10 24 | 7 6 15 |
esa | esa 2976 | 6 9 14 | 8 10 27 | 7 6 14 |
gfz | gfz 2950 | 7 9 14 | 8 11 30 | 14 8 17 |
grg | grg 2846 | 8 10 20 | 11 14 32 | 12 10 22 |
igr | igr 2976 | 5 8 14 | 8 9 27 | 7 6 13 |
igs | igs 2975 | 6 8 14 | 9 10 26 | 7 6 12 |
jpl | jpl 2972 | 8 8 18 | 9 9 27 | 8 7 16 |
mit | mit 2976 | 10 13 16 | 9 10 30 | 9 10 18 |
Table 5.1769.6 GPS week: 1769 Day: 6 MJD: 56633.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 | 5 5 13 | 9 10 38 | 7 7 12 |
emr | emr 2972 | 9 6 18 | 11 8 32 | 8 6 19 |
esa | esa 2976 | 6 5 15 | 9 9 38 | 7 6 17 |
gfz | gfz 2961 | 6 5 14 | 9 9 39 | 8 7 18 |
grg | grg 2859 | 8 9 29 | 12 12 45 | 11 13 23 |
igr | igr 2976 | 6 4 15 | 8 9 37 | 6 6 15 |
igs | igs 2975 | 7 4 16 | 9 9 38 | 7 5 16 |
jpl | jpl 2972 | 7 4 21 | 9 9 38 | 10 10 18 |
mit | mit 2976 | 9 9 14 | 9 10 43 | 12 12 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 6.1769 GPS week: 1769 MJD: 56627.500-56633.500
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 0 19 -17 -4 | 21 27
| 24 18 90 100 5 | 2
emr uuuuu | 8 30 -4 216 -19 | 31 38
| 12 24 142 92 10 | 6
esa uuuuu | 6 -7 11 10 -3 | 9 18
| 7 13 77 37 1 | 1
gfz uuuuu | -3 -4 154 -193 8 | 12 20
| 14 25 82 90 4 | 4
grg uuuux | 10 7 -86 -11 0 | 4 20
| 18 15 44 89 7 | 3
igr xxxxx | -15 -2 -4 12 -1 | 1 15
| 8 11 43 59 3 | 1
irf xxxxx | 11 -4 -47 -23 4 | -1 16
| 10 13 29 44 2 | 3
jpl uuuuu | 28 -11 -26 167 -4 | 26 30
| 11 24 83 66 11 | 2
mit uuuuu | 1 0 -154 -123 2 | 8 18
| 16 11 112 65 6 | 2
ngs uuuuu | -39 4 -19 12 0 | 5 13
| 32 63 152 111 3 | 2
sio xxxxx | -202 -110 -234 -316 8 | 11 21
| 115 56 92 80 2 | 3
Table 7.1769.0 GPS week: 1769 Day: 0 MJD: 56627.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 15 -8 35 162 3 | 17 25
emr uuuuu | 17 13 17 254 -30 | 40 43
esa uuuuu | 0 -6 -16 53 -2 | 8 17
gfz uuuuu | -30 22 97 -295 6 | 7 16
grg uuuux | 20 -7 -43 -151 -2 | 6 27
igr xxxxx | -17 -1 -12 5 0 | 0 15
irf xxxxx | -6 4 -66 -94 -1 | -3 15
jpl uuuuu | 20 25 -36 163 8 | 23 28
mit uuuuu | -16 -4 -264 -215 -6 | 7 16
ngs uuuuu | -10 -20 109 -26 1 | 4 11
sio xxxxx | -229 -160 -219 -407 5 | 9 19
Table 7.1769.1 GPS week: 1769 Day: 1 MJD: 56628.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 21 4 -48 52 -2 | 20 25
emr uuuuu | 19 62 -264 249 -20 | 37 42
esa uuuuu | 4 -32 123 35 -4 | 9 16
gfz uuuuu | 12 -47 257 -262 12 | 9 15
grg uuuux | 23 -1 -10 -54 -6 | 6 27
igr xxxxx | -1 13 8 -49 -2 | 1 14
irf xxxxx | 3 -1 -31 -67 2 | -3 14
jpl uuuuu | 16 2 -104 95 4 | 25 28
mit uuuuu | -12 5 -150 -201 -2 | 7 16
ngs uuuuu | -90 97 -201 71 -2 | 4 11
sio xxxxx | -245 -208 -244 -411 9 | 9 19
Table 7.1769.2 GPS week: 1769 Day: 2 MJD: 56629.500
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 23 -65 -10 0 | 24 28
emr uuuuu | 14 -11 34 287 -29 | 37 42
esa uuuuu | 8 -11 115 -13 -1 | 11 19
gfz uuuuu | -2 -20 287 -287 7 | 13 21
grg uuuux | -22 14 -87 -46 -4 | 9 28
igr xxxxx | -21 0 77 80 1 | 3 16
irf xxxxx | 11 8 -82 -17 2 | 0 16
jpl uuuuu | 17 -38 82 131 9 | 28 33
mit uuuuu | 25 11 -315 -52 -1 | 10 19
ngs uuuuu | -58 41 -245 88 0 | 6 14
sio xxxxx | -427 -63 -344 -236 7 | 12 23
Table 7.1769.3 GPS week: 1769 Day: 3 MJD: 56630.500
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 -3 37 -14 -11 | 21 27
emr uuuuu | -3 45 40 273 -24 | 30 38
esa uuuuu | 10 -6 -32 -14 -4 | 8 17
gfz uuuuu | -11 9 101 -121 12 | 10 20
grg uuuux | 31 14 -101 30 -7 | 0 13
igr xxxxx | -13 -11 -18 -11 -2 | 0 14
irf xxxxx | 8 5 -83 5 5 | -3 16
jpl uuuuu | 34 -24 71 268 -18 | 26 30
mit uuuuu | -8 16 -201 -84 2 | 6 16
ngs uuuuu | -29 -38 45 -179 4 | 3 13
sio xxxxx | -180 -106 -308 -226 9 | 9 19
Table 7.1769.4 GPS week: 1769 Day: 4 MJD: 56631.500
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 -23 53 -124 -8 | 21 26
emr uuuuu | 2 41 43 286 -15 | 26 35
esa uuuuu | -5 -8 3 -46 -3 | 7 17
gfz uuuuu | 10 -13 122 -156 11 | 12 20
grg uuuux | -5 -13 -118 140 1 | -1 14
igr xxxxx | -10 -7 -20 108 -6 | -1 14
irf xxxxx | 15 -22 -31 23 6 | -2 15
jpl uuuuu | 30 11 -96 225 -3 | 24 29
mit uuuuu | 2 -11 -55 -90 8 | 6 16
ngs uuuuu | 6 42 -56 -23 -3 | 4 13
sio xxxxx | -105 -99 -230 -262 12 | 10 19
Table 7.1769.5 GPS week: 1769 Day: 5 MJD: 56632.500
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 | -27 23 -67 -75 -3 | 24 29
emr uuuuu | -12 28 196 79 -16 | 28 36
esa uuuuu | 7 9 -51 13 -2 | 10 19
gfz uuuuu | 3 17 114 -62 4 | 17 25
grg uuuux | 11 27 -113 5 12 | 3 15
igr xxxxx | -16 11 2 -18 3 | 2 15
irf xxxxx | 25 0 -22 20 5 | 3 17
jpl uuuuu | 33 -17 16 196 -13 | 28 33
mit uuuuu | 21 -3 -75 -70 6 | 11 21
ngs uuuuu | -38 -97 101 -12 3 | 7 15
sio xxxxx | -89 -53 -242 -297 7 | 15 24
Table 7.1769.6 GPS week: 1769 Day: 6 MJD: 56633.500
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 -16 186 -111 -6 | 22 28
emr uuuuu | 15 32 -90 87 0 | 23 33
esa uuuuu | 17 4 -65 46 -2 | 9 19
gfz uuuuu | -6 6 99 -164 4 | 18 26
grg uuuux | 13 18 -131 -1 8 | 4 16
igr xxxxx | -26 -17 -67 -32 0 | 2 15
irf xxxxx | 20 -21 -13 -28 6 | 3 17
jpl uuuuu | 47 -37 -111 92 -13 | 27 32
mit uuuuu | -5 -12 -18 -147 9 | 10 21
ngs uuuuu | -55 5 115 169 -1 | 6 15
sio xxxxx | -142 -77 -53 -372 8 | 15 25
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