[IGSREPORT-22057] Wk 1752 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Aug 22 05:17:34 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1752 (Aug 04, 2013 - Aug 10, 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:
igs1752[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1752[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1752[0-6].cls IGS GPS clock combination summary report.
igs17527.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17527.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 | 9 KOUC NRMD KOUC MOBS NRMD
0 | EMR | FAIR HERS
0 | ESA | 9 IRKJ KOUC YELL IRKJ KOUC YELL
0 | GFZ | 9 9
0 | GRG | 7 7 ADIS IRKJ NKLG ADIS IRKJ NKLG
0 | JPL | 9
0 | MIT | GRAZ GRAZ YARR
1 | COD | HERT JOZ2 KOUC MOBS HERT JOZ2 KOUC MAR6 MOBS
1 | ESA | KOUC KOUC UNSA
1 | GFZ | 9 9 ALGO BRMU CONZ DAV1 GLSV GUAT HOB2 IRKJ NOVM
1 | GFZ | PDEL PRDS SCH2 STHL TSKB ALGO BRMU CONZ GLSV GUAT
1 | GFZ | HOB2 IRKJ NOVM PDEL PRDS SCH2 STHL TSKB
1 | GRG | SYOG MBAR SYOG
1 | JPL | 8
1 | MIT | 26 26 IRKJ PARC IRKJ PARC
2 | COD | KOUC MAC1 XMIS
2 | EMR | THU3 THU3
2 | ESA | FLRS IRKJ FLRS IRKJ KOUC UNSA
2 | GFZ | 9 9 KOUC PDEL WES2 MCM4 PDEL WES2
2 | GRG | GOPE IRKJ KOUC NRMD TLSE IRKJ NRMD TLSE
2 | MIT | 8 11 8 11
3 | COD | 9 31 USNO
3 | EMR | 8 TLSE HARB TLSE
3 | ESA | 9 IRKJ IRKJ
3 | GFZ | 9 9 KOUR NRMD HARB KOUC KOUR
3 | GRG | 8 IRKJ KOUC KOUR GOPE HARB IRKJ KOUC KOUR
3 | JPL | 8 KOUR
3 | MIT | 9 11 26 28 8 11 26 KOUR NICO KOUR MDVJ NICO
4 | COD | 8 9 JOZ2 JOZ2 NNOR REYK
4 | EMR | 9 9 MDO1
4 | ESA | 8 9 ARTU IRKJ KOUC ARTU KOUC
4 | GFZ | 9 8 9
4 | GRG | BARH IRKJ SPT0 ARTU BARH DGAR SPT0 USNO
4 | JPL | 8 9
4 | MIT | KOUC PTBB GMSD KOUC MDVJ PTBB SCH2
5 | COD | ADIS KOUC ADIS KOUC XMIS
5 | EMR | 9 8 9 MCM4 HERS MCM4
5 | ESA | IRKJ KOUC IRKJ ISPA KOUC
5 | GFZ | 9 9 AUCK AUCK
5 | GRG | 8 9 IRKJ MDO1 HARB IRKJ MDO1
5 | JPL | 8 9
5 | MIT | 9 18 22 28 32 6 28 NICO NICO
6 | COD | KOUC ADIS KOUC NYA1 TRO1
6 | EMR | 9 8
6 | ESA | KOUC TRO1 KOUC
6 | GFZ | 9 TLSE TRO1 TLSE
6 | GRG | 7 7 8 HARB HERT HYDE IRKJ IRKT LPGS POLV HARB HERT
6 | GRG | HYDE IRKJ LPGS NOVM POLV TRO1
6 | JPL | 8
6 | MIT | 9 11 26 8 10 11 26 NICO NYAL USNO MDVJ NICO NYAL
6 | MIT | USNO
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 | EMR | ~22:47 | ~ -0.05 ns
5 | MIT | ~00:00 | ~ -0.07 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. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G09 | | 4 | | 4 | | 4 | |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .2 .1 -.7 -30 21 -39 .05
EMR | 0 | .4 -1.0 -3.8 -12 -7 -3 .08
ESA | 0 | -2.2 -4.5 16.6 21 -23 -26 -.09
GFZ | 0 | -.4 .2 .0 -19 -18 -22 -.54
GRG | 0 | 3.2 -5.1 14.7 -13 16 -32 .01
JPL | 0 | -5.7 -1.9 -.6 -50 20 -30 -.17
MIT | 0 | 3.8 -.7 12.6 -11 15 -51 .03
NGS | 0 | .2 -4.2 7.9 -50 2 -4 .10
SIO | 0 | -3.3 3.7 -12.1 -25 -34 -59 -.02
COD | 1 | .6 .1 -.1 -33 27 -32 .15
EMR | 1 | -2.5 .4 -5.6 -9 -5 1 -.02
ESA | 1 | -3.0 -2.8 15.2 62 -31 -21 -.26
GFZ | 1 | -.3 .2 -.1 -23 -26 -19 -.40
GRG | 1 | .8 -11.1 6.4 -23 17 -16 .02
JPL | 1 | -3.8 -3.3 -1.5 -61 21 -5 -.05
MIT | 1 | -.7 -1.0 9.6 -5 13 -41 .03
NGS | 1 | -1.6 .3 6.1 -38 5 -7 .14
SIO | 1 | -4.3 -.3 -13.7 -47 -8 -187 -.02
COD | 2 | 1.0 -.1 .2 -26 22 -22 .15
EMR | 2 | -4.4 1.0 -6.9 -20 -8 -19 -.06
ESA | 2 | -.7 -3.0 15.3 44 -31 -19 -.06
GFZ | 2 | .2 .1 .0 -11 -24 -16 -.42
GRG | 2 | -1.5 -1.6 13.8 -31 7 8 -.03
JPL | 2 | -9.9 .6 1.6 -5 13 22 .08
MIT | 2 | .3 -1.8 10.5 -2 17 -49 .22
NGS | 2 | -3.0 -3.1 -1.5 -16 21 -21 .07
SIO | 2 | -1.7 -1.9 -3.2 -21 -3 -58 .06
COD | 3 | .8 .1 -.4 -47 24 -8 .20
EMR | 3 | -3.1 1.0 -4.2 -20 -15 -9 .07
ESA | 3 | -2.2 -1.2 21.1 114 -66 -3 -.03
GFZ | 3 | .1 .0 .3 -35 -10 -6 -.31
GRG | 3 | -1.3 -3.8 9.7 -38 25 3 .18
JPL | 3 | -.4 3.6 4.6 -19 6 7 .09
MIT | 3 | -2.1 -.8 11.7 -3 12 -31 .10
NGS | 3 | .8 .2 9.6 -39 -12 11 .13
SIO | 3 | -.9 1.0 -13.6 -11 -36 -108 .17
COD | 4 | 1.1 .3 -.7 -42 21 -16 .21
EMR | 4 | -1.9 2.5 -2.5 -10 -12 -13 .28
ESA | 4 | .0 -3.5 14.2 65 -51 -21 -.10
GFZ | 4 | .2 -.2 .4 -24 -16 -10 -.69
GRG | 4 | 1.1 1.4 6.4 -16 22 -26 .05
JPL | 4 | -6.3 -1.2 5.1 -60 9 -23 -.11
MIT | 4 | -1.6 -.8 13.7 -7 12 -42 .10
NGS | 4 | .7 3.0 3.3 -11 -2 19 .30
SIO | 4 | -2.2 1.4 -13.0 2 -44 -7 .24
COD | 5 | 1.0 -.4 -.4 -30 22 -47 .29
EMR | 5 | -4.5 2.8 -8.9 -17 -7 -26 .16
ESA | 5 | 1.7 -4.2 10.0 73 -37 -21 -.08
GFZ | 5 | .3 .0 -.1 -20 -37 -12 -.41
GRG | 5 | -3.4 -7.8 5.6 -15 11 -5 .15
JPL | 5 | 1.7 2.0 4.2 -85 6 -6 -.02
MIT | 5 | -1.0 -3.2 10.1 -2 6 -39 .20
NGS | 5 | .1 -1.9 -.8 -14 6 -4 .37
SIO | 5 | -.9 1.2 -23.6 3 -91 34 .03
COD | 6 | .5 .2 -.1 -26 26 -42 .12
EMR | 6 | -2.4 -4.2 -3.5 -15 -5 -26 .04
ESA | 6 | -.1 -6.1 14.0 77 -51 -38 .08
GFZ | 6 | .2 -.1 .2 -25 -28 -23 -.57
GRG | 6 | 3.6 -7.3 13.5 -24 54 9 -.04
JPL | 6 | -8.3 -.5 -2.6 -65 12 -28 .01
MIT | 6 | 2.3 -1.7 9.2 -5 13 -46 .12
NGS | 6 | 1.8 -3.6 8.0 -46 -18 -1 .05
SIO | 6 | -.2 1.4 -14.5 -17 -56 -110 .0
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1752.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1752.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 2.1752.[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 3.1752.[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 5.1752.0-6). 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 1752 summary. (Aug 04, 2013 - Aug 10, 2013)
Table 1.1752.a GPS week: 1752 MJD: 56508.000-56514.000
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 260| 0 -1 2 -3 13 15 .21 9 9 | -1323 134 23 99
| 0 0 0 22 21 6 .02 | 267 579
emr 79| -1 -2 -5 12 -5 30 .12 16 16 | 3353 -550 18 109
| 1 0 1 19 16 15 .02 | 1582 957
esa 150| 0 0 1 16 4 -22 -.09 6 6 | -127 -739 19 144
| 0 0 1 20 33 28 .01 | 448 639
gfz 194| 0 2 -2 7 -27 -9 -.57 10 9 | 145 33 18 91
| 0 0 1 34 47 11 .04 | 380 544
grg 137| 1 0 9 0 11 14 .38 14 13 | 41 -169 20 159
| 0 0 3 14 22 11 .02 | 217 482
igr n/a| 0 0 1 -10 1 15 -.34 5 4 | -4402 -1571 18 84
| 0 0 0 17 12 9 .04 | 3491 820
jpl 80| 0 1 -4 -14 6 -2 .17 14 14 | 2581 -557 17 100
| 1 1 1 23 15 10 .03 | 1372 792
mit 237| 0 -2 0 -8 10 0 -.04 12 11 | 101 -325 30 223
| 0 0 1 23 34 20 .03 | 221 526
ngs 236| 0 0 -2 -33 -24 1 .20 10 9 | -1270 124 1680 3455
| 0 0 2 16 25 18 .03 | 196 532
sio 437| 1 0 0 -39 -47 -89 -.55 21 21 | --- --- --- ---
| 1 1 1 22 26 82 .04 | --- ---
Table 1.1752.b GPS week : 1752 MJD: 56508.000-56514.000
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 | 3 4 4 4 4 4 4 |
2 | 5 4 4 4 5 5 5 |
3 | 3 3 4 3 4 4 4 |
4 | 3 4 3 4 5 3 4 |
5 | 4 4 4 4 4 4 4 |
6 | 3 4 4 3 4 4 4 |
7 | 6 5 6 5 5 4 5 |
8 | 4 4 4 5 5 4 4 |
9 | 5 5 5 6 7 4 6 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 5 4 5 4 4 5 4 |
13 | 4 3 4 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 5 5 4 4 |
16 | 4 5 5 5 5 5 5 |
17 | 5 5 5 5 5 4 4 |
18 | 3 4 4 4 4 4 5 |
19 | 4 4 4 4 5 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 5 4 4 4 5 5 5 |
22 | 3 3 4 4 4 4 4 |
23 | 4 4 4 4 4 4 4 |
24 | 4 3 4 4 5 4 4 |
25 | 3 4 4 4 4 4 3 |
26 | 4 3 4 4 4 3 4 |
27 | 4 4 4 4 4 5 4 |
28 | 4 3 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 0 0 0 0 --- --- --- |
31 | 5 5 5 5 5 5 4 |
32 | 3 3 4 3 3 3 3 |
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 2.1752.0 GPS week: 1752 Day: 0 MJD: 56508.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| 0 -1 1 10 16 7 .16 9 9 | -880 -310 20 96
emr 80| -2 -2 -6 13 -6 19 .13 15 15 | 4870 78 18 116
esa 150| 0 0 0 0 -4 -7 -.08 5 5 | -237 -74 15 136
gfz 190| 0 2 -4 15 -24 0 -.61 11 10 | 408 -85 12 86
grg 136| 2 0 13 15 -8 22 .34 15 14 | 248 -28 18 143
igr n/a| 0 0 1 -28 6 7 -.37 5 5 | 87 -1177 16 93
jpl 80| -1 1 -7 -3 18 -6 .16 15 14 | 4120 -219 17 119
mit 235| 0 -2 0 -29 41 -11 -.09 11 11 | 260 -151 26 212
ngs 239| 0 0 0 -11 -27 -3 .21 10 8 | -1002 -69 1724 3569
sio 434| 1 -1 -1 -48 -20 -66 -.52 22 19 | --- --- --- ---
Table 2.1752.1 GPS week: 1752 Day: 1 MJD: 56509.000
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 257| 1 -1 0 -19 11 12 .22 8 8 | -1552 484 29 82
emr 80| -2 -2 -6 -2 -16 17 .15 16 15 | 4728 -388 29 110
esa 150| 0 0 3 14 21 -15 -.10 5 5 | -634 -165 25 136
gfz 194| 0 2 -3 40 -40 -18 -.59 8 8 | 375 -142 28 102
grg 135| 2 0 9 0 2 12 .42 13 12 | 2 -67 29 135
igr n/a| 0 0 1 -9 8 12 -.29 4 4 | -1180 -1733 24 87
jpl 80| -2 2 -5 -46 26 -17 .19 15 14 | 3732 -828 24 110
mit 236| 0 -3 -1 3 -51 3 -.05 11 11 | 59 -170 34 223
ngs 238| 0 0 -2 -51 10 18 .26 11 10 | -1533 478 1541 3836
sio 438| 2 0 0 -61 -62 -222 -.52 21 20 | --- --- --- ---
Table 2.1752.2 GPS week: 1752 Day: 2 MJD: 56510.000
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 -1 3 3 -9 17 .22 9 9 | -1345 -114 33 113
emr 80| -2 -2 -5 15 -35 20 .13 16 16 | 4954 -1973 22 121
esa 150| 0 0 1 28 -19 -10 -.08 6 6 | 605 -1751 31 164
gfz 192| 0 2 -2 -20 62 -11 -.60 9 8 | 375 -635 38 132
grg 139| 1 0 13 -15 1 30 .39 14 12 | 348 -748 23 255
igr n/a| 0 0 2 1 -21 26 -.35 5 5 | -2136 -2724 28 99
jpl 80| 0 1 -6 3 -12 -6 .12 16 15 | 3640 -1561 22 98
mit 236| 0 -2 1 -28 45 -11 -.03 11 10 | 507 -1076 37 222
ngs 235| -1 0 -6 -13 -51 -20 .22 11 10 | -1296 -201 1703 3926
sio 434| 1 0 1 -65 -5 -87 -.53 21 21 | --- --- --- ---
Table 2.1752.3 GPS week: 1752 Day: 3 MJD: 56511.000
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| 0 0 2 -39 46 9 .20 9 9 | -1089 -689 25 100
emr 80| 0 0 -5 -21 -5 21 .08 15 15 | 2698 -508 14 115
esa 150| 0 0 1 23 -42 9 -.09 6 6 | -476 -1304 16 126
gfz 197| -1 1 -3 52 -2 -15 -.56 9 9 | -143 -478 11 73
grg 139| 1 0 6 -14 41 2 .37 13 12 | 142 -835 17 157
igr n/a| 0 0 1 -31 -8 8 -.32 4 4 | -4975 -1244 16 75
jpl 80| 1 0 -4 -42 3 -7 .15 14 14 | 1922 -61 17 104
mit 239| 0 -2 0 11 12 -25 -.03 11 10 | 44 -777 29 255
ngs 237| 0 0 -1 -24 -32 -23 .21 11 10 | -1027 -730 1842 2986
sio 431| 1 -2 1 -35 -55 -147 -.56 20 19 | --- --- --- ---
Table 2.1752.4 GPS week: 1752 Day: 4 MJD: 56512.000
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| 0 0 2 30 -13 23 .20 12 11 | -1428 641 19 103
emr 80| -1 -2 -3 34 4 58 .12 15 15 | 3211 -1539 15 98
esa 150| 0 0 1 -17 63 -80 -.07 6 6 | 259 -693 16 139
gfz 197| 0 2 -1 5 -87 11 -.58 9 8 | 125 504 15 82
grg 138| 2 0 6 21 -16 2 .37 15 14 | -171 549 15 124
igr n/a| 0 0 1 14 0 30 -.32 5 5 | -5279 -2478 16 87
jpl 80| 0 2 -2 -1 -6 16 .17 14 14 | 2708 -1417 15 102
mit 238| 0 -2 1 -13 -11 38 -.01 12 11 | -148 522 25 213
ngs 234| 0 1 -5 -37 -11 25 .20 11 10 | -1405 663 1911 3335
sio 437| 1 -2 2 -26 -75 6 -.54 21 23 | --- --- --- ---
Table 2.1752.5 GPS week: 1752 Day: 5 MJD: 56513.000
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 2 -4 10 19 .21 9 9 | -1305 -24 19 108
emr 80| -1 -2 -6 26 10 35 .12 15 15 | 800 885 14 91
esa 150| 0 0 0 46 0 -28 -.10 5 5 | -452 -210 16 141
gfz 197| 0 2 0 -48 -59 -9 -.55 10 10 | -575 923 11 72
grg 138| 1 0 8 1 28 7 .39 14 14 | -253 -161 20 133
igr n/a| 0 0 1 4 15 6 -.40 4 4 | -8745 -334 16 70
jpl 80| -1 0 -2 13 -7 6 .21 13 13 | 317 704 15 73
mit 237| 0 -2 0 -28 31 0 -.02 12 11 | -92 -561 34 238
ngs 236| 0 1 -2 -49 -3 1 .17 10 9 | -1252 -21 1843 3261
sio 446| 1 0 0 -41 -72 9 -.58 21 22 | --- --- --- ---
Table 2.1752.6 GPS week: 1752 Day: 6 MJD: 56514.000
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 261| 0 -1 1 -8 34 19 .23 9 9 | -1662 954 16 97
emr 79| 0 -2 -2 23 12 39 .10 19 17 | 2215 -406 15 117
esa 150| 0 0 0 18 8 -26 -.09 5 5 | 40 -982 16 171
gfz 195| 0 1 -1 4 -43 -22 -.51 10 9 | 452 146 13 94
grg 134| 2 0 7 -6 33 24 .38 16 16 | -26 102 19 172
igr n/a| 0 0 0 -22 10 16 -.32 5 5 | -8588 -1311 16 79
jpl 80| 1 0 -2 -22 21 -3 .16 15 15 | 1629 -518 15 96
mit 238| 0 -1 0 28 3 3 -.02 13 12 | 80 -66 31 202
ngs 235| 0 1 -1 -43 -59 10 .17 10 9 | -1379 748 1197 3274
sio 441| 0 1 1 0 -41 -116 -.62 23 23 | --- --- --- ---
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 3.1752.0 GPS week: 1752 Day: 0 MJD: 56508.000
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 | 4 13 4 9 11 6 12 6 13 15 3 | 28 32 26 25 32 27 33 32 36 28 28
2 | 12 14 6 11 16 4 15 18 7 14 4 | 22 30 20 21 25 18 27 16 22 24 20
3 | 6 11 4 9 10 5 10 9 5 21 2 | 19 24 17 17 19 14 22 19 22 21 17
4 | 9 12 4 7 11 5 12 10 8 22 3 | 20 22 22 25 18 21 19 19 20 20 19
5 | 9 15 6 8 11 4 14 13 10 24 3 | 34 37 32 34 36 33 35 33 34 33 33
6 | 6 11 4 9 10 6 12 8 8 17 3 | 20 22 17 20 19 17 24 18 24 22 18
7E | 14 23 4 10 33 3 20 14 8 10 5 | 29 30 27 27 30 25 28 27 28 24 25
8E | 10 16 6 11 13 6 14 11 7 24 4 | 69 66 65 65 68 62 67 68 65 73 65
9E | 7 19 9 22 12 5 15 8 8 20 4 | 148 149 146 154 149 149 148 146 147 145 148
10 | 7 8 4 10 10 3 13 10 12 17 3 | 21 21 20 19 25 17 20 19 22 19 19
11 | 8 19 4 8 24 4 12 7 9 13 4 | 35 40 34 34 44 34 37 35 40 31 35
12 | 11 15 5 15 17 5 15 14 11 28 4 | 19 23 15 20 27 14 22 20 22 21 16
13 | 6 14 5 9 20 4 14 8 10 16 3 | 26 29 25 22 44 22 26 23 23 20 24
14 | 10 15 6 11 15 4 17 9 9 25 4 | 25 26 27 25 38 25 23 26 26 29 25
15 | 8 17 6 11 13 5 20 13 9 27 4 | 24 29 19 20 29 17 29 22 23 18 20
16 | 9 16 8 13 15 6 17 12 10 47 4 | 23 22 17 21 24 16 24 20 23 41 18
17 | 14 16 5 10 16 6 18 18 11 23 4 | 24 26 20 18 31 18 24 25 28 16 20
18 | 9 11 4 9 9 4 10 12 9 25 3 | 24 26 24 19 27 20 26 25 24 18 22
19 | 8 13 3 11 22 4 11 11 8 19 3 | 22 21 17 20 32 16 21 22 23 14 18
20 | 7 10 5 14 12 4 14 11 15 24 4 | 28 26 26 28 29 24 26 26 32 32 26
21 | 10 18 3 13 15 5 15 15 12 17 4 | 19 29 15 19 27 13 26 17 22 15 17
22 | 7 11 3 10 8 3 11 11 7 21 3 | 23 24 24 19 29 21 24 26 24 18 23
23 | 7 16 4 9 17 3 17 8 9 21 3 | 23 24 22 20 36 19 24 19 22 22 21
24E | 9 11 3 7 16 5 15 12 8 10 3 | 27 26 22 19 33 22 25 20 23 22 22
25 | 8 10 3 12 14 5 12 8 6 13 3 | 20 24 19 21 27 17 28 20 23 14 20
26 | 7 9 6 11 12 5 12 11 13 18 3 | 20 21 22 24 26 20 19 22 24 23 21
X27 | 8 16 4 9 --- 9 13 12 8 17 3 | 39 41 33 30 --- 33 39 30 37 42 34
28 | 10 12 4 12 12 5 13 10 9 32 3 | 25 27 22 25 32 18 27 28 27 28 24
29 | 8 23 6 16 11 3 21 10 10 13 4 | 22 30 21 29 24 22 28 19 26 16 21
X30 | 3 --- --- --- --- 26 --- --- --- --- 0 | 29 --- --- --- --- 14 --- --- --- --- 27
31E | 9 18 6 11 21 5 22 9 7 11 4 | 38 36 29 27 42 27 33 30 33 30 30
32 | 7 8 4 8 14 3 8 8 12 21 3 | 19 19 16 15 21 14 16 16 21 20 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 5 11 15 5 15 11 10 22 |T 30 32 27 28 34 25 31 28 31 29 27
WRMS | 9 15 5 10 14 5 14 11 8 19 |NE 23 26 21 22 28 19 25 22 25 22 21
MEDI | 8 14 4 10 13 5 14 11 9 20 |MD 24 26 22 21 29 20 26 22 24 22 21
Table 3.1752.1 GPS week: 1752 Day: 1 MJD: 56509.000
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 16 6 10 9 7 13 11 11 17 3 | 25 27 23 26 26 22 27 29 32 26 24
2 | 8 16 5 7 14 3 16 11 9 16 3 | 23 24 17 16 23 15 23 17 17 19 17
3 | 6 12 6 8 9 4 11 9 12 14 3 | 20 22 18 16 20 14 24 17 23 20 17
4 | 9 11 6 12 7 4 15 9 11 22 3 | 25 23 24 30 21 26 22 25 28 25 23
5 | 7 14 5 7 12 3 12 14 9 23 3 | 26 26 22 21 24 19 23 21 25 22 21
6 | 5 11 6 8 12 4 13 12 13 12 3 | 21 24 22 16 25 17 24 17 19 19 19
7E | 12 18 6 9 13 4 20 14 12 9 4 | 33 35 26 27 32 26 36 30 31 27 28
8E | 9 22 6 10 13 7 15 9 10 23 4 | 68 65 66 63 67 64 62 64 71 70 65
9E | 9 18 7 10 14 7 17 16 11 19 4 | 152 155 152 155 152 152 156 153 150 151 152
10 | 5 8 4 6 10 2 8 9 8 17 2 | 20 18 18 14 20 16 19 18 22 16 17
11E | 8 16 5 10 12 3 12 8 15 26 4 | 40 43 41 36 44 38 43 39 44 36 40
12 | 9 15 5 8 18 5 14 16 11 26 4 | 20 21 13 16 26 13 21 18 20 23 14
13 | 7 13 3 5 16 3 12 8 10 16 3 | 19 25 18 15 36 16 25 17 18 14 18
14 | 9 17 8 7 14 3 15 9 10 26 4 | 18 25 24 18 30 19 24 22 20 25 20
15 | 7 17 5 7 14 5 20 13 11 23 4 | 22 26 17 14 27 14 26 18 21 14 17
16 | 8 18 7 10 14 3 19 12 14 44 4 | 21 21 19 16 23 14 23 17 21 36 16
17 | 16 16 5 9 17 5 16 15 12 21 4 | 28 24 19 16 32 15 25 24 22 18 19
18 | 13 14 5 7 10 3 14 11 7 25 3 | 27 24 22 12 23 16 27 20 25 14 20
19 | 8 17 5 9 14 4 13 11 13 17 4 | 17 18 13 13 27 10 18 17 21 13 14
20 | 9 11 5 12 12 5 13 9 15 26 3 | 26 26 25 27 25 24 27 25 33 31 25
21 | 8 20 3 9 12 3 15 15 7 16 4 | 19 24 15 18 24 13 24 14 20 14 16
22 | 7 12 3 7 9 3 13 12 8 21 3 | 20 22 19 10 24 14 23 18 20 14 17
23 | 6 17 6 7 12 3 18 8 10 22 3 | 21 24 20 17 29 16 25 17 19 16 18
24E | 6 14 4 8 10 3 12 9 7 11 3 | 26 25 20 16 28 19 27 22 26 21 21
25 | 8 10 4 6 13 3 14 11 11 13 3 | 22 20 16 11 27 14 28 17 20 15 17
26 | 5 8 5 5 11 4 9 9 6 16 2 | 18 18 17 15 19 14 17 19 19 20 16
X27 | 7 17 4 8 --- 8 15 15 12 12 4 | 27 31 26 19 --- 20 32 21 26 27 24
28 | 8 11 4 8 12 4 13 9 9 30 3 | 22 26 18 17 30 15 26 22 21 24 19
29 | 7 33 5 12 13 5 20 13 12 12 5 | 19 31 14 22 22 16 23 18 25 15 16
X30 | 4 --- --- --- --- 24 --- --- --- --- 0 | 27 --- --- --- --- 14 --- --- --- --- 25
31E | 8 20 5 8 19 5 17 14 11 17 4 | 25 29 23 20 28 21 28 20 26 27 22
32 | 8 8 4 5 13 3 10 9 14 23 3 | 18 19 17 14 18 14 20 18 19 17 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 16 5 8 13 4 15 11 11 21 |T 28 30 25 24 31 23 30 26 29 26 25
WRMS | 8 15 5 8 12 4 14 11 10 20 |NE 21 23 19 17 25 16 23 19 22 19 18
MEDI | 8 16 5 8 12 4 14 11 11 19 |MD 22 24 19 16 26 16 25 19 22 20 19
Table 3.1752.2 GPS week: 1752 Day: 2 MJD: 56510.000
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 16 5 9 12 9 15 12 16 21 4 | 35 42 38 39 37 38 38 42 44 43 37
2 | 10 18 9 8 16 4 15 10 7 14 4 | 24 32 21 20 30 19 26 21 25 19 22
3 | 6 14 5 9 10 5 13 10 12 14 3 | 23 24 19 18 21 18 24 21 27 21 20
4 | 7 12 6 5 9 4 14 7 6 21 3 | 26 29 29 28 28 28 27 28 28 26 27
5 | 11 14 6 10 11 5 13 10 10 24 3 | 30 33 27 28 29 27 31 27 33 30 28
6 | 7 13 4 8 9 6 15 9 10 12 3 | 22 23 17 14 19 14 22 17 21 17 17
7E | 10 21 8 11 37 4 21 13 10 9 6 | 30 32 22 26 51 23 30 28 30 23 25
8E | 8 17 6 10 13 6 16 12 13 20 4 | 49 48 44 40 48 45 48 45 50 48 45
9E | 8 21 11 13 11 7 17 18 12 22 5 | 89 92 90 89 93 89 90 86 84 91 88
10 | 9 9 7 8 11 3 8 10 9 17 3 | 25 24 19 17 24 19 19 20 23 17 20
11E | 6 19 5 8 11 4 13 8 15 12 4 | 30 33 28 24 36 26 29 27 39 23 29
12 | 11 13 8 9 18 3 13 15 9 26 4 | 26 28 22 22 30 20 26 22 27 26 22
13 | 7 15 5 7 18 3 16 7 9 16 3 | 24 31 24 21 40 21 27 22 22 18 23
14 | 8 18 7 8 13 5 17 9 7 27 4 | 27 27 23 23 34 24 25 26 26 28 23
15 | 13 17 7 7 13 4 19 10 9 21 4 | 27 28 18 16 30 18 28 20 26 16 20
16 | 13 20 7 11 11 4 19 10 11 45 4 | 28 26 20 19 25 16 24 20 23 36 20
17 | 14 16 5 10 15 5 18 11 10 17 4 | 31 29 23 21 32 20 26 26 30 16 24
18 | 9 15 5 9 6 4 15 12 7 27 3 | 26 27 21 15 25 20 26 24 27 17 21
19 | 6 18 6 10 11 5 15 8 14 17 4 | 25 23 20 20 29 18 22 22 28 17 21
20 | 9 9 6 9 11 4 12 10 13 22 3 | 28 27 25 23 28 23 26 25 28 29 25
21 | 7 20 4 8 15 4 15 15 9 17 4 | 21 29 20 18 30 18 27 19 27 16 20
22 | 7 16 5 7 7 3 15 11 8 23 3 | 26 26 21 16 28 20 25 22 24 18 21
23 | 6 17 5 7 13 3 18 9 10 21 3 | 27 28 24 22 34 22 27 21 23 20 23
24E | 9 11 7 9 17 5 15 10 10 12 4 | 26 26 21 15 31 19 27 21 27 21 21
25 | 7 12 5 5 12 3 13 10 11 15 3 | 24 25 20 16 26 18 28 20 25 16 20
26 | 8 13 6 7 11 4 10 10 13 16 3 | 19 23 16 18 23 19 19 21 23 24 18
X27 | 8 18 6 7 --- 11 16 12 11 13 4 | 32 35 27 21 --- 25 32 27 25 30 27
28 | 12 15 5 9 12 3 16 8 14 31 4 | 27 30 24 23 33 20 28 26 29 27 25
29 | 9 27 7 14 11 4 20 10 10 13 5 | 26 34 26 31 28 26 28 24 35 20 25
X30 | 4 --- --- --- --- 57 --- --- --- --- 0 | 62 --- --- --- --- 14 --- --- --- --- 60
31E | 9 19 7 8 20 5 21 10 11 12 4 | 28 28 22 18 32 21 27 23 29 23 22
32 | 9 7 5 8 10 4 10 9 15 21 3 | 22 22 18 12 20 16 21 18 24 19 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 6 9 14 5 16 11 11 21 |T 30 31 25 23 32 23 29 26 30 25 26
WRMS | 9 16 6 8 12 5 15 10 10 21 |NE 27 28 22 20 28 20 26 23 26 22 24
MEDI | 8 16 6 8 11 4 15 10 10 17 |MD 26 28 22 21 30 20 27 22 27 21 22
Table 3.1752.3 GPS week: 1752 Day: 3 MJD: 56511.000
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 14 6 9 10 4 11 11 8 15 3 | 31 33 32 32 34 30 34 31 33 28 31
2 | 11 15 7 7 13 3 15 13 8 14 4 | 24 27 23 18 26 20 28 23 23 21 22
3 | 7 12 6 7 10 5 11 9 9 16 3 | 24 24 22 23 21 20 25 23 28 24 22
4 | 7 12 6 9 10 4 12 9 10 21 3 | 37 40 43 36 38 42 41 34 41 36 39
5 | 9 14 5 8 9 5 13 10 8 24 3 | 33 34 34 31 32 30 34 30 31 34 31
6 | 6 12 5 5 10 5 11 11 9 13 3 | 22 21 22 20 22 17 25 20 20 19 20
7E | 9 18 8 10 10 4 17 13 8 8 4 | 22 24 22 16 26 17 23 23 24 19 20
8E | 11 19 9 10 11 6 14 13 10 19 4 | 57 57 57 57 58 56 58 58 59 61 56
9E | 11 23 11 11 19 7 18 23 14 23 6 | 176 180 176 176 180 174 180 175 177 173 177
10 | 7 8 4 8 12 3 10 9 7 17 3 | 23 20 24 17 22 18 21 21 25 18 21
11E | 8 18 7 7 13 3 11 7 11 12 3 | 36 38 37 33 39 32 34 35 37 29 35
12 | 8 13 6 11 18 5 12 8 13 25 4 | 23 24 22 20 27 18 24 21 23 23 20
13 | 7 15 5 9 16 4 14 8 10 16 3 | 22 29 22 19 38 20 27 21 22 18 22
14 | 8 16 5 9 11 4 16 9 11 26 3 | 23 29 30 28 34 26 26 27 30 28 27
15 | 9 15 6 13 13 5 18 10 16 21 4 | 29 28 23 24 30 20 28 24 27 19 23
16 | 15 20 8 9 14 4 19 11 10 44 5 | 30 25 24 23 26 20 25 21 23 39 22
17 | 16 16 4 11 17 6 17 9 12 16 4 | 30 26 22 18 33 18 25 23 26 17 22
18 | 10 12 7 7 8 3 12 16 12 26 4 | 26 26 24 14 22 20 27 26 25 17 21
19 | 9 16 7 8 16 3 14 10 9 17 4 | 24 22 21 21 30 18 20 22 24 16 21
20 | 8 10 4 12 9 4 10 9 11 22 3 | 30 26 26 26 26 24 25 27 28 31 26
21 | 10 16 6 9 14 4 16 14 9 16 4 | 22 29 19 22 29 17 27 20 22 19 21
22 | 9 14 5 6 8 4 12 12 8 22 3 | 25 25 24 19 25 21 26 26 26 20 23
23 | 7 15 5 8 13 3 16 8 10 20 3 | 24 26 22 20 32 20 26 20 25 19 22
24E | 8 14 8 9 11 5 11 12 15 13 4 | 27 29 26 19 31 22 26 25 30 24 23
25 | 6 10 7 6 16 5 12 9 14 14 3 | 26 24 25 18 27 20 31 24 23 19 23
26 | 6 11 6 10 11 3 12 11 11 16 3 | 23 24 22 18 22 18 22 22 19 24 20
X27 | 9 16 5 6 --- 6 12 12 10 14 4 | 31 35 31 26 --- 27 34 28 31 35 30
28 | 9 13 6 12 15 4 17 8 10 30 4 | 22 26 22 23 32 18 28 24 26 25 22
29 | 8 26 7 11 16 4 19 8 13 12 5 | 24 31 22 25 24 21 28 22 25 18 22
X30 | 5 --- --- --- --- 84 --- --- --- --- 0 | 73 --- --- --- --- 17 --- --- --- --- 72
31E | 11 20 5 12 19 4 17 9 13 13 4 | 26 27 23 21 28 21 25 24 30 23 23
32 | 8 7 6 10 9 4 8 5 11 21 3 | 21 20 20 19 21 17 18 18 22 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 6 9 13 4 14 11 11 20 |T 33 33 31 28 34 27 32 30 32 29 31
WRMS | 9 15 6 9 12 4 14 10 10 19 |NE 27 26 24 22 28 21 27 23 25 23 25
MEDI | 8 15 6 9 12 4 13 10 10 17 |MD 25 26 23 21 28 20 26 24 26 23 22
Table 3.1752.4 GPS week: 1752 Day: 4 MJD: 56512.000
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 14 6 8 10 7 10 13 10 14 3 | 24 25 24 24 23 23 26 27 26 19 23
2 | 12 14 6 9 18 3 17 12 12 16 4 | 26 28 22 19 25 19 27 26 21 24 21
3 | 7 11 6 7 15 4 10 14 12 15 3 | 21 22 19 12 21 14 22 19 20 20 18
4 | 13 13 6 6 15 5 15 19 13 22 4 | 74 72 72 72 67 71 70 75 69 74 70
5 | 11 15 6 9 10 4 12 11 14 24 4 | 29 31 25 25 28 25 29 26 34 29 26
6 | 7 11 6 7 13 4 11 13 9 14 3 | 21 21 18 15 23 14 22 21 19 19 18
7E | 16 19 5 11 14 4 18 14 10 10 5 | 27 25 20 18 25 17 23 23 25 21 20
8E | 15 17 7 11 13 6 14 12 9 19 4 | 40 43 41 36 43 36 43 42 38 43 39
9E | 30 20 15 10 17 8 15 18 15 21 6 | 126 119 114 115 124 118 117 121 120 119 117
10 | 7 8 3 9 14 3 7 8 10 16 3 | 26 23 22 22 23 19 21 21 26 16 22
11E | 10 14 6 7 8 4 11 7 12 12 3 | 29 29 30 24 35 24 28 28 29 25 28
12 | 12 13 6 11 19 5 14 8 9 26 4 | 25 24 17 18 28 15 24 19 22 22 18
13 | 10 15 6 6 18 5 13 10 11 15 4 | 25 31 21 18 38 19 28 20 19 16 22
14 | 10 17 6 11 14 3 17 7 10 28 4 | 21 26 24 23 29 22 24 24 28 25 22
15 | 12 16 5 13 13 5 20 10 9 22 4 | 28 29 21 24 28 20 30 24 26 16 23
16 | 18 18 7 9 17 6 18 13 13 43 5 | 26 24 18 20 25 14 25 19 20 37 18
17 | 15 14 5 8 19 6 16 9 9 16 4 | 33 24 19 17 34 14 22 22 24 15 21
18 | 13 13 6 9 9 3 10 18 8 27 4 | 25 27 23 16 24 20 28 28 27 17 23
19 | 10 15 8 8 19 3 12 14 13 16 4 | 23 20 18 14 28 12 19 16 19 14 16
20 | 9 10 6 12 14 5 12 10 14 20 4 | 29 27 28 28 26 24 28 26 33 31 27
21 | 14 21 6 11 15 3 14 13 9 19 4 | 23 30 21 19 32 20 26 22 25 19 21
22 | 11 15 4 9 10 4 12 9 7 24 3 | 23 26 23 19 25 20 26 25 25 19 22
23 | 6 16 7 7 13 5 16 12 10 19 4 | 27 28 24 20 30 20 26 19 22 18 22
24E | 11 17 6 10 16 5 13 15 10 15 4 | 24 24 20 14 30 15 24 25 22 21 19
25 | 8 9 4 8 19 3 13 9 9 16 3 | 23 25 24 16 31 19 30 23 24 17 22
26 | 10 9 4 10 14 4 8 10 14 16 3 | 19 21 16 14 21 14 17 20 21 23 16
X27 | 8 14 7 8 --- 9 12 16 11 13 4 | 35 34 31 26 --- 25 35 29 32 35 30
28 | 11 14 5 11 16 6 12 9 11 31 4 | 25 26 19 22 32 16 25 21 23 24 21
29 | 11 20 5 13 17 4 17 9 11 12 4 | 22 28 21 24 25 21 27 21 27 17 21
31E | 10 17 5 10 21 6 18 10 16 15 4 | 24 23 18 15 24 17 22 19 25 20 17
32 | 9 8 5 6 12 4 8 7 10 21 3 | 21 20 18 10 17 13 20 16 19 21 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 6 9 15 5 14 12 11 21 |T 30 30 26 24 32 23 30 27 29 26 26
WRMS | 11 15 6 8 14 5 14 11 10 23 |NE 26 27 23 21 28 20 27 24 26 23 23
MEDI | 11 14 6 9 14 4 13 11 10 16 |MD 25 26 21 19 28 19 26 23 25 21 22
Table 3.1752.5 GPS week: 1752 Day: 5 MJD: 56513.000
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 14 6 7 11 6 12 16 7 18 3 | 23 25 20 17 25 17 29 21 21 19 20
2 | 13 15 6 14 17 4 15 14 10 17 4 | 26 26 20 17 28 18 25 22 26 19 20
3 | 9 13 5 6 13 6 10 16 9 19 3 | 21 19 18 15 24 15 22 19 20 18 18
4 | 6 12 4 10 11 3 12 9 8 21 3 | 61 63 60 56 61 61 61 61 62 64 60
5 | 10 15 6 8 12 4 12 10 9 26 3 | 26 29 24 24 28 22 29 25 27 27 24
6 | 8 12 5 7 10 6 11 17 9 18 3 | 22 21 20 13 22 14 25 19 21 17 18
7E | 9 18 7 12 12 4 15 14 10 10 4 | 22 29 20 15 27 16 28 20 22 15 19
8E | 9 14 6 7 14 5 12 13 7 19 3 | 54 51 51 48 51 48 50 49 50 50 50
9E | 10 17 7 8 12 5 14 16 9 20 4 | 158 164 162 163 168 162 167 163 160 163 162
10 | 5 9 4 8 14 5 8 8 10 16 3 | 24 24 21 21 26 20 25 20 23 14 21
11E | 8 20 6 5 11 4 12 10 12 14 3 | 28 32 25 18 33 21 30 25 27 23 25
12 | 11 14 5 14 19 4 16 11 11 25 4 | 22 23 16 17 29 14 24 21 21 21 17
13 | 6 14 4 7 17 4 12 10 12 17 3 | 25 33 23 20 39 23 32 24 23 16 24
14 | 11 15 6 11 14 3 17 13 9 26 4 | 21 24 20 23 29 18 26 24 23 25 20
15 | 8 17 6 10 13 5 17 10 10 22 4 | 26 26 20 21 30 17 27 24 27 16 22
16 | 9 19 6 9 16 5 17 12 11 42 4 | 28 25 18 18 25 14 24 17 21 34 18
17 | 8 14 4 13 17 4 16 9 12 18 4 | 25 24 19 21 33 16 26 19 27 13 21
18 | 9 16 6 11 8 3 12 19 9 27 4 | 24 25 20 16 23 16 26 27 23 17 20
19 | 8 16 8 9 18 4 13 11 12 18 4 | 22 19 16 15 30 12 21 16 18 12 16
20 | 7 11 5 11 12 4 13 11 7 21 3 | 30 29 27 27 27 24 32 25 28 29 27
21 | 9 24 5 13 15 5 13 16 10 20 4 | 23 29 19 16 30 15 26 20 21 18 19
22 | 9 17 6 10 8 2 13 13 8 24 3 | 23 24 17 16 24 15 25 22 21 17 18
23 | 6 16 5 9 15 3 16 11 8 21 3 | 27 29 23 22 31 22 30 22 24 19 23
24E | 8 12 5 11 11 5 12 12 12 15 3 | 24 18 18 15 26 16 24 22 27 18 19
25 | 7 10 5 10 17 4 13 9 13 16 3 | 22 22 20 15 29 15 29 20 21 16 19
26 | 7 11 5 9 13 3 7 7 10 18 3 | 18 22 15 15 22 16 23 18 23 21 17
X27 | 8 17 6 9 --- 10 11 19 12 18 4 | 27 29 23 19 --- 20 30 25 24 29 23
28 | 8 14 6 12 15 4 13 8 12 30 4 | 22 28 21 23 33 18 30 22 24 24 22
29 | 8 23 6 13 17 4 18 12 9 14 4 | 23 27 19 21 25 17 25 21 21 14 19
31E | 10 16 6 11 22 4 16 13 10 15 4 | 29 27 22 20 31 20 27 25 29 25 23
32 | 10 8 3 8 12 4 7 9 9 22 3 | 24 23 18 17 19 16 24 18 17 21 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 5 10 14 4 13 12 10 21 |T 30 31 26 25 34 24 32 28 29 26 27
WRMS | 9 15 5 10 14 4 13 11 9 22 |NE 25 26 21 20 28 19 27 22 24 21 21
MEDI | 8 15 6 10 13 4 13 12 10 19 |MD 24 26 20 18 28 17 26 22 23 19 20
Table 3.1752.6 GPS week: 1752 Day: 6 MJD: 56514.000
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 16 7 7 15 7 11 13 11 23 3 | 27 28 25 26 30 26 29 27 31 23 25
2 | 11 15 5 8 19 3 18 13 11 18 4 | 25 25 21 16 27 17 26 21 24 22 20
3 | 8 14 4 9 14 6 11 15 8 18 3 | 22 25 18 20 21 17 23 30 26 26 21
4 | 7 14 5 16 11 4 16 10 12 23 4 | 50 51 50 48 50 48 52 44 48 50 48
5 | 11 17 6 8 15 4 13 11 11 26 4 | 36 37 33 34 37 33 38 35 39 37 34
6 | 8 13 5 6 13 7 11 16 6 20 3 | 17 20 14 13 20 9 18 20 19 20 15
7E | 8 27 7 10 14 5 18 19 10 28 5 | 24 30 18 15 22 15 20 22 23 31 17
8E | 9 17 6 10 18 5 15 12 9 19 4 | 66 68 65 61 66 63 66 64 63 70 64
9E | 8 50 7 12 16 6 16 15 10 24 6 | 139 152 138 141 144 139 141 137 141 136 140
10 | 8 10 3 7 17 3 9 10 11 18 3 | 22 20 20 17 25 18 19 21 21 18 19
11E | 6 23 7 7 14 4 13 11 11 20 4 | 32 35 31 27 38 26 30 28 31 24 29
12 | 9 14 6 10 18 6 15 11 10 25 4 | 23 23 19 20 28 17 22 23 21 22 18
13 | 7 15 4 9 21 5 14 13 10 23 4 | 24 26 23 22 39 22 27 22 24 21 22
14 | 9 17 5 10 16 2 16 12 11 27 4 | 27 27 27 29 35 26 26 31 25 30 26
15 | 10 17 5 10 17 4 19 10 11 24 4 | 27 31 22 20 29 19 29 23 27 20 22
16 | 11 21 7 11 18 5 20 13 9 42 4 | 25 23 19 21 24 15 24 19 23 36 18
17 | 8 18 4 10 18 5 17 10 8 15 4 | 26 26 16 19 32 14 23 21 24 18 19
18 | 10 17 7 11 12 4 16 18 7 28 4 | 24 25 23 20 26 18 24 32 21 17 21
19 | 7 19 6 8 16 5 14 14 9 21 4 | 19 22 15 16 26 11 19 21 20 22 16
20 | 9 13 5 12 15 4 12 10 8 21 3 | 30 24 24 26 26 22 26 25 23 28 24
21 | 11 21 3 12 18 6 17 15 11 19 4 | 24 28 20 20 30 17 27 23 23 25 20
22 | 9 14 5 7 11 4 16 14 7 23 3 | 23 24 22 21 29 19 24 31 22 19 22
23 | 7 18 5 7 18 4 16 13 6 23 4 | 26 25 24 21 33 21 28 21 23 21 22
24E | 9 14 6 13 14 5 12 13 11 18 4 | 28 24 26 16 30 22 26 26 25 28 23
25 | 6 11 4 6 18 5 12 10 8 18 3 | 24 23 23 16 30 21 29 24 25 18 22
26 | 7 13 5 9 16 4 12 10 7 19 3 | 17 21 16 17 25 14 16 19 17 20 15
X27 | 7 15 5 9 --- 9 12 17 9 15 4 | 36 40 33 28 --- 31 38 35 34 41 33
28 | 10 13 6 13 15 4 15 9 10 30 4 | 22 25 21 27 30 18 24 25 23 26 21
29 | 8 23 6 12 18 4 18 12 11 13 4 | 25 29 24 27 28 24 26 29 27 24 23
31E | 8 17 5 10 20 6 19 10 10 16 4 | 26 27 24 24 29 24 27 25 26 25 24
32 | 9 8 3 5 16 4 9 10 11 24 3 | 24 19 17 11 22 15 20 17 16 19 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 19 5 10 16 5 15 13 10 23 |T 30 32 28 27 34 25 31 30 30 30 27
WRMS | 9 17 5 9 16 5 15 12 9 23 |NE 25 26 22 22 29 20 26 25 25 24 22
MEDI | 8 16 5 10 16 5 15 12 10 21 |MD 25 25 23 21 29 19 26 25 24 24 22
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 4.1752 GPS week: 1752 MJD: 56508.0-56514.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3007 |U 6 6 17 |U 5 6 20 |U 10 10 24 |
emr | emr 2968 | 9 7 25 |U 9 13 33 | 12 10 28 |
esa | esa 2976 | 7 7 18 |U 5 6 21 | 10 10 26 |
gfz | gfz 2968 |U 7 6 18 |U 5 8 24 |U 10 10 25 |
grg | grg 2880 |U 13 13 38 |U 16 19 51 | 18 19 43 |
igr | igr 2975 | 6 6 18 | 5 6 20 | 10 10 26 |
igs | igs 2953 | 7 7 19 | 7 9 26 | 10 10 25 |
jpl | jpl 2968 | 8 8 23 |U 11 17 41 |U 11 10 27 |
mit | mit 2976 | 11 7 19 |U 15 19 37 |U 12 12 32 |
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 5.1752.0 GPS week: 1752 Day: 0 MJD: 56508.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 5 4 15 | 5 10 20 | 12 14 40 |
emr | emr 2972 | 9 5 24 | 6 7 25 | 16 12 36 |
esa | esa 2976 | 6 6 19 | 5 7 23 | 14 13 38 |
gfz | gfz 2968 | 6 6 17 | 5 10 23 | 14 14 39 |
grg | grg 2880 | 9 7 28 | 7 12 30 | 15 16 41 |
igr | igr 2976 | 5 5 18 | 5 7 21 | 14 13 39 |
igs | igs 2972 | 6 6 19 | 5 7 25 | 14 13 39 |
jpl | jpl 2972 | 9 9 30 | 5 9 28 | 16 13 37 |
mit | mit 2976 | 6 7 18 | 5 9 27 | 17 16 43 |
Table 5.1752.1 GPS week: 1752 Day: 1 MJD: 56509.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3033 | 7 8 19 | 4 6 19 | 11 15 24 |
emr | emr 2968 | 11 7 26 | 11 16 36 | 14 13 32 |
esa | esa 2976 | 9 9 21 | 5 6 20 | 11 14 25 |
gfz | gfz 2968 | 8 8 20 | 5 8 25 | 11 13 24 |
grg | grg 2880 | 9 9 30 | 8 7 30 | 16 20 35 |
igr | igr 2976 | 8 8 20 | 4 5 17 | 10 13 24 |
igs | igs 2976 | 8 8 20 | 9 11 27 | 11 13 25 |
jpl | jpl 2967 | 10 7 21 | 12 20 42 | 13 15 30 |
mit | mit 2976 | 8 10 20 | 16 26 37 | 11 16 32 |
Table 5.1752.2 GPS week: 1752 Day: 2 MJD: 56510.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 | 9 9 22 | 6 6 24 | 8 6 22 |
emr | emr 2968 | 11 9 30 | 12 22 44 | 10 9 30 |
esa | esa 2976 | 8 9 25 | 5 5 21 | 9 7 25 |
gfz | gfz 2968 | 8 8 24 | 5 6 23 | 9 7 24 |
grg | grg 2880 | 35 35 100 | 36 33 106 | 40 42 89 |
igr | igr 2975 | 8 8 24 | 5 5 24 | 9 7 26 |
igs | igs 2976 | 8 10 26 | 11 13 35 | 9 9 24 |
jpl | jpl 2968 | 10 8 27 | 11 21 46 | 10 8 28 |
mit | mit 2976 | 8 8 23 | 16 21 42 | 9 9 28 |
Table 5.1752.3 GPS week: 1752 Day: 3 MJD: 56511.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3038 | 4 5 13 | 5 7 18 | 11 10 17 |
emr | emr 2968 | 9 6 22 | 10 15 35 | 12 10 24 |
esa | esa 2976 | 4 6 14 | 5 5 18 | 10 9 19 |
gfz | gfz 2968 | 4 6 13 | 5 8 17 | 9 9 19 |
grg | grg 2880 | 6 7 18 | 16 23 47 | 11 9 24 |
igr | igr 2976 | 4 5 13 | 4 6 18 | 9 9 18 |
igs | igs 2960 | 4 6 15 | 5 5 20 | 10 9 19 |
jpl | jpl 2968 | 7 8 22 | 9 16 47 | 12 12 22 |
mit | mit 2976 | 5 5 14 | 18 22 51 | 11 11 25 |
Table 5.1752.4 GPS week: 1752 Day: 4 MJD: 56512.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 6 20 | 6 5 27 | 10 8 27 |
emr | emr 2968 | 11 8 30 | 7 10 37 | 10 9 28 |
esa | esa 2976 | 8 6 22 | 6 6 28 | 10 8 29 |
gfz | gfz 2968 | 8 6 20 | 7 9 34 | 9 8 29 |
grg | grg 2880 | 12 12 35 | 15 19 56 | 15 16 39 |
igr | igr 2976 | 8 6 22 | 6 5 26 | 9 8 29 |
igs | igs 2956 | 8 6 22 | 11 17 40 | 9 8 28 |
jpl | jpl 2968 | 10 7 24 | 16 17 46 | 11 9 28 |
mit | mit 2976 | 8 6 23 | 22 21 38 | 9 11 35 |
Table 5.1752.5 GPS week: 1752 Day: 5 MJD: 56513.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 8 17 | 5 5 20 | 8 6 15 |
emr | emr 2968 | 7 7 20 | 8 10 28 | 8 5 19 |
esa | esa 2976 | 7 8 16 | 6 7 21 | 8 8 19 |
gfz | gfz 2968 | 7 7 16 | 6 7 23 | 8 8 19 |
grg | grg 2880 | 10 14 33 | 13 18 39 | 9 12 29 |
igr | igr 2976 | 7 7 17 | 5 6 19 | 8 8 19 |
igs | igs 2953 | 6 7 17 | 6 7 22 | 8 8 18 |
jpl | jpl 2968 | 6 8 18 | 10 18 39 | 8 6 20 |
mit | mit 2976 | 32 10 18 | 17 22 42 | 14 8 31 |
Table 5.1752.6 GPS week: 1752 Day: 6 MJD: 56514.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 3 12 | 4 6 13 | ---- ---- ---- |
emr | emr 2968 | 7 8 21 | 13 11 29 | ---- ---- ---- |
esa | esa 2976 | 4 3 13 | 5 6 15 | ---- ---- ---- |
gfz | gfz 2968 | 6 4 14 | 5 7 20 | ---- ---- ---- |
grg | grg 2880 | 9 7 20 | 19 18 46 | ---- ---- ---- |
igr | igr 2976 | 5 3 12 | 5 6 16 | ---- ---- ---- |
igs | igs 2879 | 5 4 14 | 5 5 15 | ---- ---- ---- |
jpl | jpl 2966 | 6 6 17 | 11 20 40 | ---- ---- ---- |
mit | mit 2976 | 7 5 20 | 12 15 25 | ---- ---- ---- |
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 6.1752 GPS week: 1752 MJD: 56508.500-56514.500
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 | 0 -4 -9 146 5 | 15 20
| 21 13 87 73 5 | 5
emr uuuuu | -6 16 -195 -101 -10 | 37 40
| 10 14 115 40 7 | 3
esa uuuuu | 5 -33 64 89 -4 | 10 16
| 11 11 38 34 4 | 3
gfz uuuuu | 8 16 52 -21 0 | 1 13
| 17 17 55 76 3 | 4
grg uuuux | 0 -9 28 -99 -27 | 8 15
| 14 10 92 43 12 | 5
igr xxxxx | -14 25 32 1 1 | -3 14
| 15 15 52 46 6 | 4
irf xxxxx | -16 -6 -42 -93 -2 | 1 12
| 7 5 34 19 2 | 3
jpl uuuuu | -34 19 40 -16 -4 | 39 40
| 14 16 83 80 8 | 1
mit uuuuu | -18 1 -100 -185 -1 | 18 22
| 20 17 50 59 3 | 3
ngs uuuuu | 26 40 -21 -40 1 | 10 15
| 29 32 59 108 5 | 4
sio xxxxx | 36 40 40 -30 2 | 28 31
| 36 27 60 62 2 | 4
Table 7.1752.0 GPS week: 1752 Day: 0 MJD: 56508.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -25 1 -113 112 -4 | 9 14
emr uuuuu | -10 8 -65 -74 -15 | 44 48
esa uuuuu | 9 -21 58 100 -6 | 9 14
gfz uuuuu | 33 30 -23 -26 3 | -2 9
grg uuuux | 4 -18 135 -120 -33 | 16 22
igr xxxxx | -37 51 77 60 -11 | -4 12
irf xxxxx | -3 -5 12 -74 -6 | 0 9
jpl uuuuu | -59 16 29 -159 -11 | 38 39
mit uuuuu | -24 13 -3 -150 -7 | 17 19
ngs uuuuu | 37 8 -32 -8 4 | 6 9
sio xxxxx | 29 64 118 55 0 | 26 27
Table 7.1752.1 GPS week: 1752 Day: 1 MJD: 56509.500
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 | 18 8 -114 96 5 | 10 14
emr uuuuu | 4 39 -178 -179 -12 | 40 44
esa uuuuu | 2 -37 31 93 -10 | 9 13
gfz uuuuu | 31 -3 68 134 -1 | -2 10
grg uuuux | 21 -3 107 -38 -16 | 13 20
igr xxxxx | -10 24 27 16 0 | -5 11
irf xxxxx | -15 -10 -33 -107 -2 | -1 9
jpl uuuuu | -36 33 61 30 6 | 38 40
mit uuuuu | -44 -6 -93 -304 -2 | 16 18
ngs uuuuu | -27 47 87 -139 6 | 7 11
sio xxxxx | -14 74 6 -110 1 | 26 27
Table 7.1752.2 GPS week: 1752 Day: 2 MJD: 56510.500
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 | 5 6 -62 73 10 | 10 14
emr uuuuu | 5 29 -215 -124 -5 | 35 37
esa uuuuu | 5 -24 88 106 -4 | 7 13
gfz uuuuu | -7 4 79 -22 -3 | -2 10
grg uuuux | -7 4 114 -162 -19 | 9 16
igr xxxxx | -20 8 113 -13 0 | -6 11
irf xxxxx | -17 -13 -15 -77 -1 | -1 9
jpl uuuuu | -27 15 1 -30 -13 | 38 39
mit uuuuu | 2 -26 -81 -132 -2 | 16 18
ngs uuuuu | 10 32 -54 81 2 | 7 11
sio xxxxx | 22 25 80 45 0 | 25 27
Table 7.1752.3 GPS week: 1752 Day: 3 MJD: 56511.500
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 0 29 81 5 | 14 17
emr uuuuu | 2 7 -107 -96 -21 | 35 37
esa uuuuu | 25 -29 30 117 -4 | 9 13
gfz uuuuu | 1 40 37 -55 2 | -1 9
grg uuuux | -17 1 -14 -127 -29 | 5 11
igr xxxxx | 12 18 21 62 6 | -5 10
irf xxxxx | -23 1 -74 -97 2 | 0 9
jpl uuuuu | -13 11 215 -55 -11 | 37 39
mit uuuuu | -35 0 -144 -159 3 | 17 19
ngs uuuuu | 39 -8 -67 114 0 | 8 12
sio xxxxx | 39 49 -51 -29 6 | 26 28
Table 7.1752.4 GPS week: 1752 Day: 4 MJD: 56512.500
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 | 28 -24 36 261 3 | 17 23
emr uuuuu | -9 5 -218 -79 -10 | 35 36
esa uuuuu | -4 -35 122 117 1 | 11 16
gfz uuuuu | -1 18 17 -108 3 | 2 14
grg uuuux | 14 -22 11 -110 -49 | 5 12
igr xxxxx | -18 13 44 -45 6 | -2 15
irf xxxxx | -20 -5 -75 -102 -1 | 2 13
jpl uuuuu | -32 47 -30 -6 -5 | 38 40
mit uuuuu | -29 -2 -140 -150 3 | 19 23
ngs uuuuu | 39 52 -5 -97 -6 | 11 17
sio xxxxx | 16 9 7 -37 4 | 29 32
Table 7.1752.5 GPS week: 1752 Day: 5 MJD: 56513.500
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 5 55 211 4 | 21 28
emr uuuuu | -22 19 -160 -95 -9 | 37 39
esa uuuuu | 4 -53 95 19 1 | 14 22
gfz uuuuu | -6 22 39 -59 -6 | 6 19
grg uuuux | -1 -8 -110 -71 -15 | 5 12
igr xxxxx | -22 22 -29 -36 3 | 2 19
irf xxxxx | -13 -7 -39 -122 -2 | 5 17
jpl uuuuu | -33 -2 21 98 6 | 40 43
mit uuuuu | 8 1 -99 -217 1 | 22 29
ngs uuuuu | 18 82 -89 -55 6 | 15 22
sio xxxxx | 96 6 97 -49 0 | 33 38
Table 7.1752.6 GPS week: 1752 Day: 6 MJD: 56514.500
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 | -14 -21 105 189 9 | 22 28
emr uuuuu | -13 4 -424 -62 1 | 35 38
esa uuuuu | -9 -32 25 74 -4 | 15 22
gfz uuuuu | 7 -1 150 -10 2 | 7 18
grg uuuux | -12 -16 -45 -64 -29 | 2 13
igr xxxxx | -6 38 -31 -35 3 | 3 19
irf xxxxx | -19 -3 -73 -70 -3 | 6 17
jpl uuuuu | -41 14 -20 11 -3 | 41 43
mit uuuuu | -6 28 -138 -180 0 | 23 29
ngs uuuuu | 64 69 14 -173 -4 | 16 22
sio xxxxx | 64 57 22 -87 1 | 34 38
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