[IGSREPORT-21443] Wk 1717 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Dec 21 09:38:44 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1717 (Dec 02, 2012 - Dec 08, 2012)
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:
igs1717[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1717[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1717[0-6].cls IGS GPS clock combination summary report.
igs17177.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17177.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.
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 | SPT0
0 | EMR | HERS
0 | GFZ | ASPA BOGT MKEA RAMO TIDB
0 | GRG | MCM4 NICO THU3 GUAT LHAZ MCM4 NICO THU3
0 | MIT | 30 30
1 | COD | WROC FLRS WROC
1 | EMR | HARB HARB
1 | ESA | UNSA
1 | GFZ | HARB HOLM NYAL
1 | GRG | GUAT SCH2 YELL GUAT SCH2 SOFI YELL
1 | JPL | 25 PALM
1 | MIT | 2 30 2 30 YEBE YEBE
2 | COD | HNPT HERT HNPT
2 | ESA | IRKJ UNSA
2 | GFZ | 30 CONZ GRAZ IRKJ LHAZ NYAL QAQ1 SCOR SUTM SYOG
2 | GRG | 26 26 HYDE MCM4 HYDE MCM4
2 | JPL | 30 YARR
2 | MIT | 5 21 26 30 32 5 21 26 30 32 GMAS
3 | COD | HNPT HOLM KOUC ALRT FLRS HNPT KOUC
3 | EMR | DRAO
3 | ESA | NICO NICO UNSA
3 | GFZ | 28 LHAZ MATE METS NRMD STHL SUTM
3 | GRG | 21 21 MCM4 MCM4
3 | MIT | DRAO BAKO DRAO
4 | COD | HNPT KOUC HNPT KOUC
4 | EMR | HARB HARB
4 | ESA | LHAZ UNSA
4 | GFZ | BOGT HARB NRMD SEY1 STHL
4 | GRG | CONZ LPGS RAMO
4 | JPL | RAMO
4 | MIT | 5 5 KERG NNOR STR1 JPLM KERG MAC1 STR1
5 | EMR | CHUR
5 | ESA | UNSA
5 | GFZ | ALRT BOGT LHAZ MATE WIND
5 | GRG | MCM4 SCH2 USNO CHUR MCM4 SCH2 USNO WIND
5 | JPL | BRAZ
6 | COD | FLRS
6 | EMR | HARB HARB
6 | ESA | AREQ
6 | GFZ | BOGT HOLM POLV
6 | GRG | ADIS CHPI LHAZ
6 | JPL | 24
6 | MIT | 8 8 NNOR NNOR
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G16 | 2012_12_06 | 2012079
G16 | 2012_12_07 | 2012079
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | SIO | ALL (high Transformation - See Table 2)
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 | -.6 .3 -.9 -54 4 -13 -.09
EMR | 0 | -6.0 7.5 7.6 10 24 -5 .08
ESA | 0 | 6.4 4.0 -3.0 87 -203 84 -.04
GFZ | 0 | .2 -.1 -.4 -74 -39 -27 -.06
GRG | 0 | -2.0 3.0 -8.7 -27 51 -62 .22
JPL | 0 | -5.4 5.6 19.5 -7 -33 -13 .23
MIT | 0 | 1.8 3.7 -1.3 -2 5 -35 .14
NGS | 0 | 9.1 .2 .1 3 -36 81 .48
SIO | 0 | -.3 9.7 19.3 107 72 -148 .07
COD | 1 | -.5 .4 -1.2 -48 -10 -23 -.19
EMR | 1 | -5.3 7.9 17.5 14 28 -10 .07
ESA | 1 | 4.6 5.9 -1.6 135 -173 86 .17
GFZ | 1 | .3 .3 .0 -52 -49 -45 -.20
GRG | 1 | .2 5.0 -14.1 -16 49 -49 .20
JPL | 1 | -10.1 7.2 17.0 -38 6 22 .30
MIT | 1 | 2.5 9.8 5.1 -2 3 -29 .05
NGS | 1 | 1.5 4.3 .1 13 -9 27 .48
SIO | 1 | -2.8 6.6 21.9 40 104 -108 -.02
COD | 2 | .1 .3 -.3 -45 -17 -8 -.08
EMR | 2 | -5.5 -.6 16.2 12 26 -7 .17
ESA | 2 | 1.0 2.0 -.1 80 -119 76 .13
GFZ | 2 | .0 -.4 -.5 -53 -43 -46 -.03
GRG | 2 | -4.9 .5 -11.4 -23 49 -43 .12
JPL | 2 | -5.3 4.6 12.0 -54 -6 -3 .09
MIT | 2 | .6 1.9 3.5 -4 -2 -27 .23
NGS | 2 | 6.5 3.9 10.5 -52 -33 58 .49
SIO | 2 | -5.7 4.5 23.3 8 144 -19 -.01
COD | 3 | -.7 .4 -.7 -59 -3 -23 -.20
EMR | 3 | -6.3 1.4 20.3 3 16 -6 .13
ESA | 3 | -4.5 -1.8 .7 14 -40 94 .12
GFZ | 3 | -.1 -.1 -.2 -69 -41 -50 -.08
GRG | 3 | -3.3 .9 -12.2 -40 55 -47 .14
JPL | 3 | -8.2 6.1 8.4 -71 8 -8 .04
MIT | 3 | -4.5 7.3 7.2 -4 5 -30 -.03
NGS | 3 | -3.0 -1.7 3.0 -38 19 -24 .44
SIO | 3 | -9.7 3.9 26.7 4 265 15 -.10
COD | 4 | -.3 .7 -.7 -47 -15 -13 -.13
EMR | 4 | -7.0 6.7 25.0 14 17 5 .23
ESA | 4 | -3.4 4.7 9.7 95 -4 81 .04
GFZ | 4 | -.3 .4 -.9 -69 -51 -37 .0
GRG | 4 | -6.0 6.8 -17.6 -30 39 -42 .45
JPL | 4 | -9.9 20.6 12.5 -39 -30 13 .14
MIT | 4 | -4.5 5.4 5.6 1 -1 -33 .34
NGS | 4 | -2.2 3.5 16.0 -100 19 -25 .59
SIO | 4 | -7.4 7.3 30.4 12 246 -38 .27
COD | 5 | -.6 .9 -.5 -55 0 -19 -.05
EMR | 5 | 1.5 5.3 20.2 21 30 -1 .19
ESA | 5 | 2.8 2.4 3.3 77 -107 92 .0
GFZ | 5 | -.3 .8 -1.2 -61 -40 -18 -.13
GRG | 5 | -.5 1.4 -13.2 -1 60 -48 .24
JPL | 5 | -1.3 13.9 14.8 -120 -21 -29 -.07
MIT | 5 | 2.3 7.1 1.8 11 1 -15 .25
NGS | 5 | .0 1.7 2.4 -5 -1 10 .60
SIO | 5 | .6 6.1 29.0 66 75 40 -.02
COD | 6 | -1.2 .7 -.8 -54 -12 -5 -.09
EMR | 6 | -1.0 4.1 18.9 20 18 11 .24
ESA | 6 | -.2 5.1 3.7 103 -73 71 .09
GFZ | 6 | -.7 .2 -1.3 -63 -46 -24 -.17
GRG | 6 | -4.6 9.5 -5.9 -5 50 -17 .10
JPL | 6 | .8 8.3 18.4 -93 -8 -34 -.14
MIT | 6 | 3.6 8.7 7.5 11 -1 -14 .13
NGS | 6 | 1.9 5.7 6.9 -17 -11 28 .40
SIO | 6 | .9 7.6 41.4 53 134 73 .22
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 1.1717.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1717.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 2.1717.[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 3.1717.[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 5.1717.0-6). 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 1717 summary. (Dec 02, 2012 - Dec 08, 2012)
Table 1.1717.a GPS week: 1717 MJD: 56263.000-56269.000
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 261| 1 0 2 4 0 5 -.39 12 11 | -1160 788 20 82
| 0 0 1 35 41 16 .05 | 552 756
emr 80| -3 0 11 -43 10 -17 .35 15 15 | 66769 382 13 94
| 1 1 2 32 31 9 .03 | 170054 675
esa 172| 1 0 0 86 -26 3 .09 5 5 | -2143 2371 11 118
| 0 0 1 15 66 12 .02 | 1144 2084
gfz 189| 0 0 -4 -107 -76 5 -.44 9 9 | -332 523 20 124
| 0 1 1 57 83 13 .03 | 587 474
grg 129| 1 1 -13 5 29 -15 .43 16 15 | -366 456 16 151
| 0 0 1 12 31 19 .06 | 372 515
igr n/a| 0 0 -2 -11 56 -4 -.13 4 4 | 6087 309 16 84
| 0 0 1 33 30 7 .02 | 738 709
jpl 80| 0 -1 5 0 11 12 .44 14 13 | 2097 516 16 105
| 1 1 1 30 28 9 .02 | 1303 832
mit 239| 0 0 -2 -7 18 7 -.16 6 6 | -497 678 22 175
| 0 0 0 25 29 6 .03 | 332 534
ngs 243| 0 1 2 -43 34 -8 .37 10 9 | -1121 655 1895 3555
| 1 0 2 29 33 19 .03 | 419 614
sio 281| 0 0 2 25 189 -40 -.42 19 18 | --- --- --- ---
| 0 1 0 22 74 64 .03 | --- ---
Table 1.1717.b GPS week : 1717 MJD: 56263.000-56269.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 5 4 4 4 |
2 | 4 4 4 4 3 4 4 |
3 | 3 3 3 3 3 4 3 |
4 | 4 4 4 3 3 4 4 |
5 | 4 3 4 3 3 3 3 |
6 | 3 3 3 4 4 3 3 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 4 4 4 3 3 3 3 |
11 | 3 3 3 3 3 4 3 |
12 | 5 4 4 5 5 5 5 |
13 | 4 4 4 4 3 4 3 |
14 | 3 3 3 3 3 3 3 |
15 | 5 4 4 5 4 4 5 |
16 | 4 4 4 5 6 0 4 |
17 | 4 4 4 4 3 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 3 4 4 4 |
22 | 4 3 3 3 3 3 3 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 4 4 4 5 |
25 | 4 4 4 4 4 4 4 |
26 | 3 3 4 3 4 4 4 |
27 | 0 0 0 0 0 0 0 |
28 | 4 3 3 4 3 4 4 |
29 | 4 4 4 4 4 4 4 |
30 | 6 6 6 6 5 5 5 |
31 | 4 4 4 5 4 4 4 |
32 | 3 3 3 4 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
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1717.0 GPS week: 1717 Day: 0 MJD: 56263.000
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 256| 1 0 2 12 67 0 -.43 12 11 | -1540 1385 20 83
emr 80| -3 0 8 -50 52 -28 .30 14 14 | 2539 617 17 89
esa 172| 1 0 0 94 -83 28 .06 6 6 | -2363 2411 13 112
gfz 187| 0 0 -3 -133 -86 30 -.46 11 10 | -295 133 21 112
grg 131| 0 1 -12 9 66 -39 .49 16 15 | -469 650 16 143
igr n/a| 0 0 -1 -28 108 -7 -.15 4 4 | 6285 372 16 80
jpl 80| 0 0 4 11 63 4 .42 14 13 | 1575 380 15 94
mit 239| 0 0 -2 -25 0 5 -.17 7 7 | -851 1283 21 168
ngs 243| 1 0 4 -4 58 -7 .41 11 9 | -1359 1094 2040 3595
sio 283| 0 -1 2 54 113 -119 -.47 20 18 | --- --- --- ---
Table 2.1717.1 GPS week: 1717 Day: 1 MJD: 56264.000
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| 0 0 2 -46 4 17 -.37 11 11 | -2224 2174 19 92
emr 80| -2 0 11 -91 -20 -10 .36 14 14 | 2024 1331 15 101
esa 172| 0 0 1 88 -109 6 .12 5 5 | -2423 3763 11 125
gfz 191| 0 -1 -3 -15 1 1 -.41 8 8 | -1128 1116 22 131
grg 131| 0 1 -12 -19 41 -6 .50 16 15 | -764 1203 16 141
igr n/a| 0 0 -1 -58 47 9 -.11 4 4 | 5499 1150 16 81
jpl 80| -2 -1 3 -33 7 17 .46 13 13 | 682 1563 16 114
mit 239| 0 0 -3 18 64 14 -.16 7 7 | -841 1438 21 191
ngs 244| 0 1 0 -73 58 -21 .35 10 9 | -1938 1676 1953 3477
sio 285| 0 0 2 17 155 -120 -.43 19 17 | --- --- --- ---
Table 2.1717.2 GPS week: 1717 Day: 2 MJD: 56265.000
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| 0 -1 4 -21 2 -8 -.36 11 11 | -970 670 27 89
emr 80| -4 -1 9 -57 35 -26 .33 15 15 | 1825 882 15 103
esa 172| 1 0 0 70 -28 -4 .09 6 5 | -1646 1687 14 142
gfz 190| 0 0 -4 -58 -123 -8 -.47 9 9 | -635 807 20 120
grg 127| 1 2 -12 4 23 -15 .46 16 14 | -459 569 16 146
igr n/a| 0 0 0 -26 68 -7 -.09 4 4 | 5202 1034 18 80
jpl 80| -1 0 5 0 7 3 .46 15 14 | 854 1335 19 108
mit 240| 0 0 -2 16 12 8 -.12 6 6 | -654 720 23 162
ngs 243| 0 2 2 -75 80 31 .33 10 9 | -1091 787 1933 3893
sio 283| 0 0 3 3 151 -37 -.41 19 17 | --- --- --- ---
Table 2.1717.3 GPS week: 1717 Day: 3 MJD: 56266.000
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| 1 0 2 64 16 -12 -.49 13 13 | -695 327 23 83
emr 80| -5 -2 10 6 30 -3 .35 15 15 | 2038 328 13 101
esa 172| 0 0 -1 82 46 -1 .08 5 5 | -1239 -129 13 128
gfz 187| 1 0 -3 -163 -159 -4 -.45 9 8 | -767 586 22 125
grg 129| 1 2 -14 10 1 -22 .44 17 16 | -690 691 18 140
igr n/a| 0 0 -1 48 64 -6 -.14 4 4 | 5513 487 18 90
jpl 80| 0 -1 7 54 24 25 .44 14 13 | 1480 788 16 105
mit 238| 0 0 -1 -34 38 18 -.16 6 6 | -480 442 22 161
ngs 243| -2 1 2 -12 -14 -30 .35 10 8 | -866 510 1690 3706
sio 278| 0 0 2 -7 321 8 -.42 19 18 | --- --- --- ---
Table 2.1717.4 GPS week: 1717 Day: 4 MJD: 56267.000
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 -9 -40 34 -.38 11 11 | -1111 648 21 78
emr 80| -2 1 12 -62 9 -17 .38 15 15 | 2602 494 11 77
esa 172| 0 0 1 66 78 -7 .11 5 5 | -3722 4991 10 109
gfz 192| 0 -2 -6 -78 -184 2 -.38 8 7 | -28 837 18 126
grg 130| 2 0 -13 1 -23 1 .42 17 16 | -463 524 16 192
igr n/a| 0 0 -2 -16 39 -2 -.13 4 3 | 6087 347 15 84
jpl 80| 1 0 4 -36 11 24 .42 15 14 | 2513 646 16 109
mit 239| 0 0 -3 17 -28 0 -.16 6 5 | -536 694 21 189
ngs 246| -1 1 5 -59 34 -7 .40 11 9 | -1064 446 1538 3101
sio 278| -1 0 2 30 260 -62 -.39 18 20 | --- --- --- ---
Table 2.1717.5 GPS week: 1717 Day: 5 MJD: 56268.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 263| 1 0 3 23 11 0 -.33 11 11 | -663 396 18 79
emr 80| -1 -1 14 -13 3 -26 .39 16 16 | 3944 -452 10 95
esa 172| 0 1 0 111 -41 -1 .10 5 5 | -401 -317 12 99
gfz 189| 0 -1 -3 -164 -18 15 -.45 8 8 | 683 -290 19 129
grg 128| 1 1 -14 21 53 -38 .43 17 16 | 255 -257 16 142
igr n/a| 0 0 -2 1 58 -15 -.14 4 4 | 7186 -437 18 96
jpl 80| -1 -2 9 10 -6 9 .48 14 14 | 3999 -460 16 108
mit 240| 0 0 -2 -36 9 5 -.16 6 6 | 11 19 22 171
ngs 246| -1 1 0 -22 11 -10 .38 11 10 | -681 338 2157 3516
sio 281| -1 1 3 39 137 -5 -.38 19 17 | --- --- --- ---
Table 2.1717.6 GPS week: 1717 Day: 6 MJD: 56269.000
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| 1 0 1 8 -60 8 -.38 12 12 | -923 -81 18 71
emr 80| 0 -2 13 -34 -36 -11 .34 15 15 | 452414 -526 11 92
esa 172| 1 0 0 94 -45 0 .09 6 6 | -3208 4197 10 112
gfz 188| 0 -1 -3 -139 33 1 -.46 10 10 | -158 478 20 129
grg 129| 1 2 -16 11 41 10 .31 16 15 | 27 -188 14 158
igr n/a| 0 0 -4 2 6 -4 -.16 4 4 | 6839 -785 14 78
jpl 80| 0 -2 4 -3 -28 3 .45 13 12 | 3580 -636 15 101
mit 239| 0 0 -4 -8 31 0 -.21 7 7 | -130 153 25 184
ngs 242| -1 1 4 -55 9 -15 .34 9 8 | -854 -266 1955 3600
sio 282| 0 0 1 42 188 52 -.45 21 17 | --- --- --- ---
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 3.1717.0 GPS week: 1717 Day: 0 MJD: 56263.000
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 | 7 12 6 12 10 4 18 7 11 12 3 | 66 64 69 66 75 68 73 66 67 65 66
2 | 8 10 7 9 15 4 11 6 7 26 3 | 34 39 39 38 42 37 38 36 40 35 37
3 | 8 10 4 12 14 3 9 6 11 13 3 | 12 19 10 13 14 8 16 10 19 8 9
4 | 11 10 4 9 14 6 9 7 10 37 4 | 43 46 48 48 57 46 46 46 48 41 46
5 | 10 15 8 8 18 4 11 6 9 12 3 | 14 26 15 17 30 13 21 13 21 16 16
6 | 9 11 4 11 13 4 6 7 12 14 3 | 13 21 14 15 21 12 18 14 21 15 13
7 | 12 14 5 12 17 4 13 7 8 28 4 | 28 25 23 24 28 20 25 20 24 32 21
8 | 10 12 5 8 15 4 10 5 9 16 3 | 21 24 23 21 22 20 25 23 26 26 23
9 | 12 12 5 9 12 4 12 5 10 15 3 | 17 26 23 20 23 20 23 22 24 17 21
10 | 10 12 9 8 14 4 9 10 7 27 4 | 26 32 31 27 33 26 31 27 31 40 29
11 | 8 13 6 8 10 3 11 5 9 13 3 | 48 47 51 50 58 49 48 48 46 44 47
12E | 11 14 6 10 23 4 24 9 15 18 4 | 21 21 14 19 16 13 24 16 21 18 14
13 | 10 11 3 10 22 3 15 6 10 12 3 | 31 31 29 28 43 27 33 28 30 29 29
14 | 9 10 4 9 17 4 10 6 10 13 3 | 26 29 29 26 35 27 31 27 28 26 26
15E | 19 15 8 12 13 4 21 8 11 14 4 | 34 35 37 32 36 34 39 35 39 41 34
16E | 10 17 5 14 17 4 14 8 11 13 4 | 22 20 21 18 18 18 19 15 21 16 17
17 | 17 17 6 10 14 3 16 7 11 20 4 | 33 37 31 27 37 29 35 28 35 26 29
18 | 14 14 6 13 17 4 12 6 11 18 4 | 23 30 20 16 30 18 26 17 23 20 19
19 | 12 17 7 11 13 4 15 5 13 23 4 | 24 29 26 21 27 21 30 20 27 27 22
20 | 14 13 7 12 18 4 15 7 10 18 4 | 23 24 20 22 25 17 24 17 20 24 17
21 | 10 9 6 11 13 3 10 8 10 34 4 | 52 53 53 48 53 51 53 46 52 54 50
22 | 6 11 5 11 17 2 9 5 11 22 3 | 20 32 26 21 42 23 33 22 28 22 24
23 | 11 13 4 14 21 5 17 6 10 14 4 | 49 45 46 39 49 44 49 41 46 46 43
24 | 12 19 6 9 17 4 12 6 12 13 4 | 25 24 23 25 25 22 25 22 22 20 20
25E | 14 20 5 10 13 5 17 7 11 17 4 | 23 21 21 16 28 19 31 21 21 25 20
26 | 9 16 6 8 10 4 9 5 11 18 3 | 26 28 24 25 27 22 25 24 29 29 24
X27E | 8 --- --- --- --- 60 --- --- --- --- 0 | 42 --- --- --- --- 41 --- --- --- --- 41
28E | 10 13 5 10 20 3 13 7 13 14 3 | 23 28 25 24 24 22 24 23 26 23 23
29 | 17 17 7 12 14 6 15 5 11 19 4 | 35 35 31 27 37 30 35 28 30 29 28
30E | 19 18 11 16 14 6 20 11 21 35 6 | 48 57 48 52 56 51 59 53 62 56 51
31 | 19 18 5 10 19 4 12 7 9 19 4 | 45 46 36 35 39 37 39 34 41 35 35
32 | 10 9 5 9 16 2 8 5 8 12 3 | 19 19 21 22 24 20 23 19 17 18 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 6 11 16 4 14 7 11 20 |T 30 32 29 28 34 28 32 27 31 29 28
WRMS | 11 14 6 10 15 4 13 7 9 18 |NE 29 33 30 28 35 27 32 27 31 29 28
MEDI | 10 13 6 10 15 4 12 6 11 17 |MD 26 29 26 25 30 22 31 23 28 26 24
Table 3.1717.1 GPS week: 1717 Day: 1 MJD: 56264.000
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 6 9 9 5 18 5 13 10 3 | 40 45 41 37 47 40 51 39 43 41 41
2 | 10 10 5 8 15 4 14 5 11 25 3 | 25 30 29 22 26 27 26 24 29 25 26
3 | 7 12 7 9 18 3 8 6 8 14 3 | 14 28 16 16 19 15 20 14 19 11 15
4 | 9 8 4 7 13 4 11 6 10 32 3 | 29 35 34 31 35 34 35 33 36 28 33
5 | 10 14 6 6 13 4 11 5 11 15 3 | 22 30 21 16 29 21 25 20 25 20 21
6 | 8 11 5 10 14 4 8 7 11 15 3 | 16 29 17 18 22 16 23 17 23 17 17
7 | 15 12 7 9 19 3 10 9 14 29 4 | 26 33 26 24 32 25 29 21 26 34 24
8 | 13 14 6 6 13 2 11 5 8 16 3 | 23 29 22 19 23 21 27 22 24 25 23
9 | 9 13 5 6 9 3 13 5 10 14 3 | 17 27 21 18 21 19 25 18 21 19 20
10 | 17 10 5 6 14 3 12 9 7 26 3 | 28 36 27 23 28 25 33 24 33 37 27
11 | 6 14 4 6 13 3 11 5 9 13 3 | 34 40 30 32 41 32 39 34 32 31 33
12E | 11 15 4 8 24 4 22 8 13 16 4 | 21 28 18 19 25 20 25 16 25 17 19
13 | 11 12 6 7 25 2 10 9 14 15 3 | 23 27 21 18 40 20 26 21 30 18 23
14 | 9 10 4 9 19 5 11 7 10 15 3 | 19 25 22 16 36 18 23 18 26 21 20
15E | 16 15 6 9 12 4 20 7 13 12 4 | 38 43 36 36 40 38 43 35 43 38 37
16E | 11 17 6 12 20 4 15 9 8 14 4 | 23 33 21 23 28 21 25 17 23 21 22
17 | 11 16 7 6 13 4 15 9 11 20 3 | 25 34 23 20 31 24 31 23 29 21 24
18 | 10 14 3 8 15 4 12 7 8 23 3 | 18 32 21 19 28 19 26 19 23 19 20
19 | 14 16 6 9 18 4 14 5 11 24 4 | 28 33 21 23 29 22 28 20 20 22 22
20 | 12 15 7 8 14 3 14 7 9 15 3 | 26 30 22 23 28 21 29 23 27 24 24
21 | 6 25 6 7 13 4 9 7 8 34 4 | 39 52 41 37 40 40 39 37 43 42 39
22 | 7 10 4 6 16 3 11 6 9 26 3 | 26 38 28 25 41 27 34 29 34 23 29
23E | 11 13 7 13 20 3 13 11 10 21 4 | 32 36 34 32 33 30 35 30 34 31 31
24 | 12 21 3 9 20 4 15 6 11 16 4 | 37 39 33 34 37 34 37 33 36 32 33
25E | 10 21 5 6 13 5 17 6 8 13 3 | 19 29 22 20 26 21 31 17 26 24 21
26 | 10 12 5 7 12 4 11 6 12 14 3 | 27 35 26 28 31 27 32 24 36 31 28
X27E | 6 --- --- --- --- 45 --- --- --- --- 0 | 70 --- --- --- --- 64 --- --- --- --- 70
28E | 10 13 4 8 17 5 11 7 10 13 3 | 19 26 18 13 21 19 23 17 25 16 18
29 | 10 18 6 8 12 5 15 6 10 19 3 | 35 42 34 34 32 35 35 35 38 33 34
X30E | 23 --- 9 11 18 6 21 12 17 27 5 | 39 --- 41 37 49 41 50 40 51 45 42
31 | 14 13 4 8 20 4 13 8 8 18 3 | 42 44 37 37 49 36 43 34 38 39 37
32 | 12 12 6 6 17 2 10 6 9 14 3 | 16 19 11 18 20 12 17 15 13 14 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 5 8 16 4 13 7 10 19 |T 28 33 26 24 31 27 31 24 30 26 27
WRMS | 11 14 5 8 15 4 13 7 9 17 |NE 26 34 26 25 31 25 31 25 29 26 26
MEDI | 10 13 6 8 15 4 12 7 10 16 |MD 26 33 23 23 31 24 29 23 29 24 24
Table 3.1717.2 GPS week: 1717 Day: 2 MJD: 56265.000
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 | 12 13 8 9 11 5 20 7 9 13 3 | 37 42 45 48 49 45 50 46 45 44 43
2 | 10 10 5 11 14 3 13 7 12 23 3 | 23 24 24 29 29 23 24 23 29 24 24
3 | 8 15 4 8 18 4 10 5 10 14 3 | 12 29 16 17 17 14 21 15 21 15 15
4 | 13 8 4 11 12 5 10 9 7 25 3 | 27 31 33 35 39 29 32 30 31 23 30
5 | 12 15 7 9 15 4 15 6 10 13 3 | 15 20 17 18 24 13 20 17 17 15 14
6 | 8 13 4 8 13 4 9 5 10 15 3 | 14 27 16 18 22 15 23 18 20 17 17
7 | 15 12 6 7 18 4 13 6 9 28 4 | 27 28 24 27 31 21 25 21 26 31 23
8 | 13 12 6 6 14 4 11 5 8 15 3 | 16 21 18 13 18 16 21 16 21 21 16
9 | 7 12 4 8 9 3 11 4 7 14 2 | 14 20 17 20 18 15 23 16 18 16 16
10 | 10 12 6 8 12 4 14 8 7 25 3 | 16 30 25 23 25 21 28 21 25 36 22
11 | 8 15 4 8 14 3 13 4 11 13 3 | 33 35 32 38 42 32 37 34 27 32 32
12E | 8 20 5 10 20 5 23 6 13 16 4 | 17 22 12 18 16 11 23 13 21 13 12
13 | 9 11 5 9 23 2 12 7 7 12 3 | 23 26 24 23 39 23 28 23 29 25 24
14 | 10 10 6 8 16 3 10 5 9 14 3 | 24 30 24 25 36 25 30 26 30 24 25
15E | 9 18 5 10 13 4 21 6 13 19 4 | 25 35 25 25 29 26 33 26 31 38 26
16E | 9 15 6 14 19 4 15 6 8 16 3 | 15 17 13 20 17 11 15 10 18 15 12
17 | 12 15 7 6 14 3 16 6 13 19 3 | 21 27 22 19 29 18 28 19 26 21 20
18 | 11 14 5 8 16 3 17 4 7 20 3 | 14 25 14 13 25 12 23 12 16 16 12
19 | 10 24 6 8 15 4 18 7 10 21 4 | 23 34 17 22 21 18 27 17 22 20 18
20 | 13 15 5 13 17 3 16 7 8 13 3 | 21 22 13 24 19 15 23 19 17 18 15
21 | 7 14 3 8 11 4 10 5 11 36 3 | 36 39 35 40 37 35 35 35 35 35 35
22 | 7 13 5 8 17 3 11 6 8 20 3 | 18 28 18 19 34 18 27 19 22 12 18
23E | 9 20 5 15 18 3 12 8 10 15 4 | 29 37 32 31 37 31 34 33 34 32 31
24 | 15 20 4 9 18 5 13 6 10 14 3 | 30 28 23 29 30 23 30 23 23 28 24
25E | 9 22 6 8 11 5 19 6 10 12 3 | 17 23 19 15 21 16 27 15 23 17 15
26 | 10 15 7 8 12 5 11 7 9 14 3 | 14 28 20 23 22 16 22 19 23 25 19
X27E | 6 --- --- --- --- 60 --- --- --- --- 0 | 50 --- --- --- --- 49 --- --- --- --- 48
28E | 11 12 4 7 18 3 13 5 10 11 3 | 18 22 18 16 18 15 22 17 23 15 17
29 | 13 17 5 11 13 6 16 7 15 18 4 | 27 31 27 30 24 28 29 28 25 24 26
30E | 20 20 9 14 15 7 23 9 19 28 5 | 39 49 37 41 47 40 52 39 50 41 40
31 | 17 13 7 11 22 5 13 7 10 19 4 | 31 32 28 34 47 28 34 26 34 28 29
X32 | 11 10 6 10 18 4 10 5 8 --- 3 | 14 18 16 20 22 15 19 17 16 --- 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 9 16 4 15 6 10 19 |T 23 28 22 24 28 22 27 22 25 24 22
WRMS | 11 15 5 9 14 4 14 6 9 17 |NE 22 28 22 25 28 21 27 22 24 23 22
MEDI | 10 14 5 8 15 4 13 6 10 15 |MD 21 28 22 23 25 18 27 19 23 23 20
Table 3.1717.3 GPS week: 1717 Day: 3 MJD: 56266.000
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 | 16 14 7 13 16 4 19 7 9 14 4 | 52 57 59 59 66 58 61 53 59 59 56
2 | 16 8 7 8 13 3 12 6 9 25 3 | 36 34 36 36 37 33 34 31 33 30 33
3 | 10 11 4 8 19 3 9 7 10 25 3 | 19 26 18 24 21 16 22 16 21 22 17
4 | 14 10 5 7 14 6 9 6 9 26 3 | 36 38 41 42 47 37 39 37 38 31 38
5 | 8 16 6 6 14 2 15 5 6 10 3 | 18 25 14 15 24 13 22 10 19 13 13
6 | 9 11 4 10 15 4 11 6 13 18 3 | 26 26 22 24 25 20 25 20 25 25 20
7 | 13 12 6 6 17 3 13 4 11 29 3 | 30 30 30 27 32 27 29 26 28 34 26
8 | 9 12 5 5 13 4 11 3 7 17 2 | 22 24 22 23 24 20 27 18 25 23 20
9 | 18 10 4 5 14 4 10 6 5 14 3 | 22 23 19 20 22 18 26 15 23 18 18
10 | 9 10 6 3 12 4 12 7 5 24 3 | 25 27 29 23 30 24 30 22 28 36 24
11 | 6 15 6 7 17 2 11 4 9 14 3 | 44 45 47 48 56 45 44 43 45 43 44
12E | 15 21 6 9 23 4 26 6 11 15 5 | 24 24 12 20 13 11 26 13 15 13 12
13 | 10 10 5 7 24 3 12 6 10 12 3 | 28 26 26 23 40 25 28 22 25 27 23
14 | 12 11 3 8 19 4 11 5 10 14 3 | 25 28 27 21 33 24 30 22 24 24 22
15E | 17 18 6 11 18 5 22 7 11 15 4 | 49 45 45 42 42 42 49 44 48 49 44
16E | 9 16 6 16 22 3 16 8 10 20 4 | 17 18 17 22 15 15 19 13 15 19 12
17 | 9 16 5 7 14 4 16 4 11 20 3 | 32 36 29 26 35 29 36 26 37 30 28
18 | 18 15 5 8 17 3 15 7 11 19 4 | 17 24 19 16 27 15 27 12 22 16 15
19 | 12 19 6 10 14 3 18 6 10 24 4 | 31 32 32 30 32 31 34 28 30 38 28
20 | 16 16 6 14 17 3 14 6 11 11 4 | 26 25 20 24 22 20 24 15 22 18 16
21 | 9 12 4 6 9 3 9 6 9 39 2 | 48 45 48 44 47 46 47 43 47 51 45
22 | 12 14 5 7 16 3 9 5 10 22 3 | 28 34 32 27 42 30 36 26 33 28 29
23E | 10 11 5 13 20 3 14 8 12 16 4 | 40 39 38 37 44 38 42 35 37 39 35
24 | 8 21 5 10 19 4 12 6 7 13 3 | 55 55 53 53 56 53 58 51 53 53 51
25E | 10 25 6 8 13 3 18 5 8 8 4 | 20 25 18 25 24 17 30 20 22 20 18
26 | 12 12 5 7 14 4 10 4 9 14 3 | 27 29 26 30 31 24 32 24 31 31 26
X27E | 8 --- --- --- --- 105 --- --- --- --- 0 | 104 --- --- --- --- 64 --- --- --- --- 107
28E | 9 14 5 9 26 3 14 4 10 18 3 | 21 25 19 22 34 19 25 19 28 17 20
29 | 12 23 6 8 13 5 16 6 11 16 4 | 38 44 36 38 37 37 40 35 41 39 36
30E | 22 25 9 9 15 7 21 10 19 22 5 | 46 59 46 47 50 47 57 49 60 42 48
31 | 19 15 4 10 24 3 13 6 17 16 4 | 47 44 43 39 44 42 45 40 46 41 40
32 | 16 9 6 8 19 2 10 6 12 16 3 | 20 19 17 19 21 15 24 12 18 14 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 15 5 9 17 4 14 6 10 19 |T 33 33 30 30 34 29 34 27 32 30 30
WRMS | 13 15 5 8 16 4 13 6 8 18 |NE 32 33 31 31 35 29 34 27 33 31 29
MEDI | 12 14 5 8 16 3 13 6 10 16 |MD 28 29 29 26 33 25 30 24 28 30 26
Table 3.1717.4 GPS week: 1717 Day: 4 MJD: 56267.000
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 11 4 8 13 2 21 3 12 11 3 | 40 47 47 52 55 48 55 48 45 46 47
2 | 7 10 4 7 14 3 14 7 9 23 3 | 29 29 29 31 29 28 29 28 24 30 27
3 | 9 12 5 9 17 2 12 3 11 14 3 | 14 23 17 16 14 14 20 13 23 14 14
4 | 8 8 4 6 13 2 11 6 12 26 3 | 32 35 36 38 42 36 38 36 33 27 34
5 | 9 15 5 6 13 3 15 6 11 11 3 | 17 22 15 19 23 13 20 13 18 11 13
6 | 10 12 4 10 14 3 13 4 18 16 3 | 15 22 17 17 17 14 21 13 27 17 14
7 | 10 13 4 8 21 3 13 6 10 29 3 | 26 27 24 26 31 23 25 22 27 31 22
8 | 9 13 5 5 15 2 11 3 9 15 3 | 16 20 18 21 23 16 18 15 21 20 16
9 | 8 11 4 4 11 3 14 4 6 12 2 | 16 19 19 16 19 15 21 14 19 15 15
10 | 11 9 5 5 12 2 11 6 8 26 3 | 16 28 27 23 29 23 29 23 27 39 24
11 | 5 15 5 6 14 3 12 5 10 16 3 | 36 33 36 40 43 35 36 34 28 33 33
12E | 17 24 4 8 25 4 23 7 10 14 4 | 21 27 16 20 17 15 23 15 21 17 15
13 | 8 10 5 6 27 3 10 6 9 13 3 | 16 23 20 18 39 19 23 19 22 20 18
14 | 8 11 4 8 16 4 12 6 11 14 3 | 41 44 40 40 45 38 47 38 41 39 40
15E | 15 17 6 9 14 3 21 6 15 16 4 | 29 31 29 28 32 27 34 28 33 37 27
X16E | 6 --- 5 --- --- 6 --- --- --- --- 5 | 12 --- 14 --- --- 12 --- --- --- --- 12
17 | 9 15 5 7 12 2 17 4 10 18 3 | 16 29 18 18 27 17 26 18 27 19 17
18 | 13 15 4 10 16 3 15 5 10 18 3 | 13 28 18 15 25 14 26 11 16 13 14
19 | 9 17 4 11 17 4 15 7 11 20 3 | 23 28 22 23 21 20 26 19 24 23 19
20 | 13 14 5 10 18 3 13 4 11 12 3 | 19 22 13 18 16 10 18 9 14 11 9
21 | 9 12 5 10 11 4 12 5 13 31 3 | 28 30 31 30 31 29 29 29 31 31 28
22 | 10 13 4 10 16 2 11 4 11 20 3 | 14 29 22 22 33 19 28 17 23 15 19
23E | 9 13 4 12 20 4 14 6 8 15 3 | 28 28 28 28 36 27 29 28 31 29 27
24 | 11 21 4 6 18 4 16 5 6 15 3 | 22 26 25 22 25 24 25 22 22 27 21
25E | 11 22 6 7 15 5 18 6 10 9 3 | 11 22 21 19 20 14 27 14 20 18 15
26 | 11 17 5 10 19 5 11 6 11 18 3 | 23 30 22 23 33 20 25 22 27 25 21
X27E | 6 --- --- --- --- 65 --- --- --- --- 0 | 64 --- --- --- --- 49 --- --- --- --- 64
28E | 10 14 3 9 14 3 11 4 8 13 3 | 17 27 19 21 22 17 22 17 26 16 18
29 | 19 21 5 9 12 5 17 8 9 13 4 | 21 30 20 19 20 18 26 17 22 20 16
30E | 17 18 10 11 22 7 20 9 16 18 5 | 36 50 42 39 47 41 49 44 48 37 41
31 | 14 13 5 8 23 3 12 6 8 15 3 | 30 33 29 22 35 27 31 26 28 26 26
32 | 10 14 6 7 15 3 10 5 9 19 3 | 13 16 15 17 18 11 14 12 12 12 10
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 5 8 17 4 15 6 11 18 |T 23 28 24 24 28 22 28 22 26 23 23
WRMS | 11 15 5 7 16 3 14 5 9 20 |NE 21 27 23 24 27 21 26 20 24 22 20
MEDI | 10 13 5 8 15 3 13 6 10 15 |MD 21 28 22 22 27 19 26 19 24 20 19
Table 3.1717.5 GPS week: 1717 Day: 5 MJD: 56268.000
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 4 8 12 5 20 7 18 13 3 | 38 40 40 45 41 40 43 42 42 38 40
2 | 10 8 5 6 14 3 11 6 13 25 3 | 20 19 21 24 26 20 22 19 21 19 20
3 | 8 15 6 8 17 4 8 7 12 15 3 | 13 21 11 13 14 9 18 9 16 9 10
4 | 9 8 4 6 14 4 9 8 12 26 3 | 31 35 36 32 40 33 36 34 37 25 33
5 | 8 15 5 7 16 4 14 8 10 12 3 | 17 23 15 14 25 14 23 16 21 14 15
6 | 9 11 4 9 15 4 7 6 10 17 3 | 14 18 12 14 18 11 20 12 18 14 12
7 | 13 13 7 8 22 3 13 6 9 28 4 | 26 27 23 22 31 20 26 21 24 26 21
8 | 10 12 6 4 17 4 11 4 11 16 3 | 24 26 22 21 27 22 27 23 25 23 23
9 | 9 10 4 7 12 3 12 5 6 11 2 | 17 20 16 17 20 15 24 18 17 16 16
10 | 11 10 6 4 15 4 11 8 6 25 3 | 22 28 25 22 29 24 29 24 30 38 25
11 | 5 17 6 6 14 2 12 6 12 18 3 | 34 30 31 37 34 33 30 34 31 31 31
12E | 9 22 5 10 18 5 26 8 10 16 4 | 20 25 14 21 19 16 28 19 18 20 16
13 | 8 11 4 7 37 3 10 7 6 12 3 | 25 29 25 25 49 24 30 25 29 27 26
14E | 8 9 5 8 12 3 10 6 9 13 2 | 31 34 30 29 34 28 33 31 31 24 30
15E | 11 17 5 9 17 7 22 7 12 24 4 | 58 61 57 60 56 56 58 61 62 67 58
X16E | 5 --- --- --- --- 27 --- --- --- --- 0 | 19 --- --- --- --- 19 --- --- --- --- 17
17 | 14 16 5 5 14 4 16 4 9 17 3 | 27 34 28 21 32 26 33 25 29 27 26
18 | 13 14 5 9 15 4 15 6 8 16 3 | 21 28 18 16 26 16 28 15 21 17 17
19 | 13 24 7 9 15 4 17 9 12 21 4 | 23 28 17 21 20 16 25 16 16 24 16
20 | 14 16 6 10 17 3 15 6 10 16 4 | 25 25 17 23 17 16 26 17 19 17 17
21 | 8 11 4 12 11 5 11 8 11 30 3 | 31 31 30 31 32 29 33 26 32 28 29
22 | 7 13 5 8 16 2 11 3 10 17 3 | 19 29 21 19 33 18 30 19 22 17 20
23E | 11 16 5 13 23 3 16 6 11 16 4 | 26 28 22 23 33 23 29 24 25 20 22
24 | 14 21 5 8 19 4 15 5 8 11 3 | 41 37 34 39 40 33 40 33 35 35 34
25E | 11 23 4 7 13 4 16 5 9 7 3 | 26 22 22 22 29 20 32 22 22 19 22
26 | 10 22 4 9 16 5 17 6 11 20 4 | 59 62 56 57 60 56 61 56 55 59 56
X27E | 5 --- --- --- --- 42 --- --- --- --- 0 | 51 --- --- --- --- 48 --- --- --- --- 50
28E | 8 14 4 9 17 5 12 4 11 23 3 | 20 26 19 20 21 20 26 20 25 19 20
29 | 21 22 4 9 12 5 16 6 12 14 4 | 32 29 23 26 25 23 28 22 25 24 23
30E | 19 21 9 12 18 6 21 10 15 23 5 | 35 46 34 35 40 33 48 34 44 29 35
31 | 13 12 5 8 21 3 11 7 11 16 3 | 24 32 26 26 40 24 34 23 33 27 26
32 | 12 10 5 8 15 3 8 5 9 17 3 | 19 18 17 19 23 18 24 20 19 14 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 5 8 17 4 14 6 11 19 |T 27 30 25 26 31 25 31 25 28 25 25
WRMS | 11 16 5 8 16 4 14 6 10 17 |NE 24 27 23 23 28 21 28 22 25 23 22
MEDI | 10 14 5 8 15 4 12 6 10 16 |MD 25 28 22 22 29 22 29 22 25 24 22
Table 3.1717.6 GPS week: 1717 Day: 6 MJD: 56269.000
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 14 5 14 10 5 18 6 10 15 3 | 68 68 69 74 75 70 72 70 66 67 69
2 | 14 9 4 14 14 2 11 6 7 26 3 | 39 38 39 42 45 40 40 40 40 36 39
3 | 8 13 4 11 14 3 8 7 8 19 3 | 21 29 17 19 18 17 25 15 22 12 18
4 | 10 8 5 12 16 3 8 7 10 31 3 | 40 42 45 49 55 46 47 46 43 33 44
5 | 9 13 5 8 12 3 12 6 7 14 3 | 12 25 14 15 26 14 24 16 23 16 16
6 | 10 12 4 9 11 4 7 5 8 19 3 | 20 27 18 20 21 16 25 18 21 18 19
7 | 13 13 6 7 24 2 12 8 7 28 4 | 27 32 27 25 33 24 30 24 28 29 24
8 | 12 12 7 5 14 3 10 4 6 15 3 | 22 25 22 18 22 20 23 21 23 20 20
9 | 13 13 4 7 12 4 10 4 8 14 3 | 29 31 27 25 28 26 32 27 28 25 27
10 | 11 9 4 7 13 3 9 6 6 28 3 | 28 31 29 28 33 28 31 28 31 41 29
11 | 6 14 4 9 13 4 10 6 12 20 3 | 49 45 47 54 55 50 47 49 41 45 47
12E | 13 24 6 10 24 5 24 9 12 16 5 | 27 36 20 20 29 21 32 19 25 23 21
13E | 8 12 5 7 15 4 10 9 7 12 3 | 32 33 29 24 31 27 32 27 29 26 28
14E | 8 11 6 10 17 4 12 8 7 12 3 | 34 34 32 31 33 30 39 28 32 27 31
15E | 18 13 7 11 21 3 20 6 11 23 4 | 34 36 35 30 36 34 40 34 39 37 34
X16E | 7 19 6 14 23 4 15 7 8 --- 4 | 22 20 10 12 16 21 18 8 10 --- 23
17 | 9 14 6 10 16 3 11 7 11 17 3 | 31 35 30 27 36 29 33 30 33 29 29
18 | 15 14 6 9 12 3 12 6 11 18 3 | 27 29 22 22 26 21 28 22 19 19 21
19 | 15 20 7 10 14 4 18 8 9 22 4 | 32 34 24 23 26 23 32 23 24 32 24
20 | 10 14 7 12 13 3 13 7 11 21 3 | 27 28 20 23 21 19 27 19 22 23 20
21 | 11 14 5 9 11 4 11 7 6 30 3 | 48 43 47 47 46 45 43 42 42 39 44
22 | 9 14 6 9 12 4 9 4 10 19 3 | 25 31 26 27 36 24 32 25 25 18 25
23E | 11 13 6 13 16 5 12 9 10 15 3 | 44 46 41 40 44 41 43 42 40 42 41
24 | 18 23 6 18 21 4 12 6 9 13 4 | 43 36 34 37 40 35 40 36 35 31 35
25E | 14 19 6 7 15 5 16 6 6 14 3 | 22 26 20 20 25 19 31 19 24 25 20
26E | 13 21 6 10 16 6 17 5 7 28 4 | 37 50 39 37 46 37 48 38 40 50 39
X27E | 7 --- --- --- --- 61 --- --- --- --- 0 | 61 --- --- --- --- 60 --- --- --- --- 59
28E | 11 13 5 6 21 4 13 5 12 15 3 | 25 28 23 18 24 23 29 21 28 15 22
29 | 17 16 7 8 14 4 15 5 11 13 4 | 35 41 35 35 31 34 37 34 34 38 33
30E | 15 21 8 12 17 7 20 10 10 36 5 | 58 66 55 56 61 56 68 56 62 53 57
31 | 12 15 6 10 24 4 10 8 11 18 4 | 33 38 31 30 45 29 38 27 40 28 31
32 | 7 10 6 9 14 3 8 6 9 20 3 | 17 21 14 18 23 15 21 17 17 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 6 10 16 4 13 7 9 21 |T 33 35 30 30 35 31 35 29 31 30 31
WRMS | 12 15 6 10 15 4 12 7 8 17 |NE 32 34 30 31 35 29 34 29 31 29 29
MEDI | 11 14 6 10 14 4 12 6 9 18 |MD 31 34 29 27 33 27 32 27 29 28 28
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 4.1717 GPS week: 1717 MJD: 56263.0-56269.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3010 |U 7 7 16 |U 8 11 26 |U 7 6 15 |
emr | emr 2930 | 10 9 20 |U 9 10 26 | 9 9 17 |
esa | esa 2948 | 8 8 17 |U 8 10 26 | 8 8 16 |
gfz | gfz 2942 |U 11 10 19 |U 9 11 27 |U 8 7 15 |
grg | grg 2947 |U 11 13 30 |U 9 12 34 | 10 9 21 |
igr | igr 2948 | 8 8 16 | 8 10 26 | 8 7 15 |
igs | igs 2948 | 8 8 17 | 8 10 25 | 8 8 15 |
jpl | jpl 2942 | 10 11 24 |U 8 10 27 |U 8 9 18 |
mit | mit 2948 | 8 8 18 |U 9 11 25 |U 9 11 25 |
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 5.1717.0 GPS week: 1717 Day: 0 MJD: 56263.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3009 | 21 17 35 | 6 8 29 | 8 7 14 |
emr | emr 2972 | 22 21 34 | 9 6 26 | 10 11 16 |
esa | esa 2976 | 22 19 35 | 7 7 26 | 8 8 14 |
gfz | gfz 2972 | 21 20 31 | 6 8 25 | 8 7 14 |
grg | grg 2976 | 19 18 34 | 6 10 27 | 11 9 25 |
igr | igr 2976 | 22 19 34 | 6 6 24 | 8 8 14 |
igs | igs 2976 | 22 19 35 | 6 6 24 | 8 8 14 |
jpl | jpl 2968 | 23 20 36 | 6 7 25 | 9 9 16 |
mit | mit 2976 | 21 20 35 | 8 8 25 | 10 16 30 |
Table 5.1717.1 GPS week: 1717 Day: 1 MJD: 56264.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 6 7 17 | 7 11 24 | 8 7 13 |
emr | emr 2880 | 9 6 23 | 9 10 24 | 8 7 18 |
esa | esa 2976 | 6 7 17 | 7 12 26 | 9 8 15 |
gfz | gfz 2970 | 7 6 16 | 8 11 27 | 9 8 14 |
grg | grg 2976 | 7 11 21 | 8 11 32 | 9 8 19 |
igr | igr 2976 | 7 6 19 | 7 12 25 | 8 8 14 |
igs | igs 2976 | 6 6 17 | 7 11 24 | 8 8 15 |
jpl | jpl 2969 | 13 11 36 | 6 9 23 | 9 8 15 |
mit | mit 2976 | 7 7 18 | 8 12 28 | 9 11 32 |
Table 5.1717.2 GPS week: 1717 Day: 2 MJD: 56265.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 4 3 14 | 11 11 26 | 7 7 19 |
emr | emr 2968 | 8 6 15 | 10 11 28 | 10 10 20 |
esa | esa 2976 | 5 4 13 | 10 10 27 | 9 9 21 |
gfz | gfz 2965 | 29 17 33 | 10 10 25 | 8 8 18 |
grg | grg 2971 | 8 11 23 | 11 14 28 | 10 8 26 |
igr | igr 2972 | 5 4 13 | 10 9 24 | 8 8 20 |
igs | igs 2972 | 5 4 13 | 10 10 25 | 7 8 20 |
jpl | jpl 2966 | 7 6 16 | 10 11 29 | 8 11 27 |
mit | mit 2976 | 5 5 13 | 10 10 20 | 10 13 33 |
Table 5.1717.3 GPS week: 1717 Day: 3 MJD: 56266.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3027 | 5 5 11 | 12 10 24 | 8 7 16 |
emr | emr 2972 | 9 7 18 | 12 8 30 | 10 11 20 |
esa | esa 2976 | 6 6 13 | 11 9 27 | 10 11 18 |
gfz | gfz 2971 | 6 7 13 | 12 10 27 | 9 10 16 |
grg | grg 2976 | 8 12 21 | 12 11 34 | 9 7 18 |
igr | igr 2976 | 6 6 12 | 11 9 25 | 10 10 18 |
igs | igs 2976 | 6 6 13 | 11 9 26 | 9 10 17 |
jpl | jpl 2972 | 8 9 15 | 10 8 27 | 9 10 16 |
mit | mit 2976 | 6 7 13 | 12 9 24 | 11 12 33 |
Table 5.1717.4 GPS week: 1717 Day: 4 MJD: 56267.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2924 | 4 5 13 | 7 14 18 | 7 6 13 |
emr | emr 2876 | 7 8 19 | 7 13 21 | 10 9 16 |
esa | esa 2880 | 5 7 12 | 7 14 19 | 8 7 12 |
gfz | gfz 2876 | 6 8 12 | 9 16 25 | 8 7 13 |
grg | grg 2880 | 21 21 53 | 10 14 40 | 11 17 22 |
igr | igr 2880 | 5 6 12 | 7 13 20 | 7 6 11 |
igs | igs 2880 | 5 7 13 | 7 13 19 | 8 6 12 |
jpl | jpl 2876 | 8 10 23 | 8 15 22 | 9 12 22 |
mit | mit 2880 | 7 7 14 | 7 14 17 | 8 7 12 |
Table 5.1717.5 GPS week: 1717 Day: 5 MJD: 56268.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 3 5 11 | 9 12 35 | 8 8 17 |
emr | emr 2876 | 6 8 13 | 9 14 29 | 7 9 13 |
esa | esa 2880 | 4 7 14 | 8 13 33 | 8 8 16 |
gfz | gfz 2874 | 5 9 14 | 11 13 33 | 8 7 15 |
grg | grg 2880 | 6 8 28 | 8 12 42 | 8 7 20 |
igr | igr 2880 | 4 7 12 | 8 13 32 | 7 7 15 |
igs | igs 2880 | 5 7 13 | 8 13 32 | 8 8 16 |
jpl | jpl 2873 | 8 12 26 | 9 13 30 | 8 6 12 |
mit | mit 2880 | 4 7 14 | 10 11 33 | 8 9 16 |
Table 5.1717.6 GPS week: 1717 Day: 6 MJD: 56269.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 5 5 10 | 8 9 24 | 5 4 15 |
emr | emr 2972 | 7 7 15 | 8 9 27 | 6 5 13 |
esa | esa 2976 | 5 5 17 | 8 9 24 | 7 4 15 |
gfz | gfz 2972 | 6 6 17 | 8 10 26 | 7 4 16 |
grg | grg 2974 | 9 13 33 | 9 16 38 | 10 8 20 |
igr | igr 2976 | 5 5 13 | 8 9 30 | 6 4 15 |
igs | igs 2976 | 5 5 14 | 8 9 24 | 6 4 15 |
jpl | jpl 2971 | 7 7 14 | 8 10 32 | 8 6 18 |
mit | mit 2976 | 6 5 17 | 8 10 27 | 9 8 18 |
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 6.1717 GPS week: 1717 MJD: 56263.500-56269.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -10 -13 102 -101 3 | -1 17
| 34 18 65 126 6 | 2
emr uuuxu | 2 -3 96 343 12 | 4 20
| 19 29 128 62 7 | 4
esa uuuuu | -19 -32 17 -14 4 | -4 16
| 57 23 61 28 6 | 2
gfz uuuuu | 88 84 -40 118 0 | 2 16
| 20 16 73 72 5 | 2
grg uuuux | -24 -8 -7 34 -32 | 6 27
| 32 9 69 91 28 | 4
igr xxxxx | -57 15 5 16 3 | -1 16
| 27 19 69 55 6 | 3
irf xxxxx | -8 -14 -15 7 0 | -4 13
| 16 14 7 41 4 | 1
jpl uuuuu | -5 -19 -67 70 7 | 10 22
| 36 16 79 55 9 | 5
mit uuuuu | -2 -8 -75 -52 -6 | -6 13
| 28 24 76 81 12 | 2
ngs uuuuu | -30 40 33 52 0 | 6 14
| 65 29 118 95 5 | 2
sio xuuuu | -192 -70 83 -94 -11 | -2 17
| 74 40 121 109 4 | 3
Table 7.1717.0 GPS week: 1717 Day: 0 MJD: 56263.500
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 | -54 -23 116 -32 2 | -1 20
emr uuuxu | -22 32 110 274 1 | 1 21
esa uuuuu | 61 -37 80 -45 1 | -5 18
gfz uuuuu | 59 92 50 83 4 | 0 19
grg uuuux | -36 -3 87 -5 9 | 4 28
igr xxxxx | -86 36 25 -23 7 | -4 18
irf xxxxx | -31 1 -3 24 -1 | -3 14
jpl uuuuu | -45 -21 -120 34 6 | 5 23
mit uuuuu | -34 22 -161 7 -3 | -3 12
ngs uuuuu | -11 14 -59 29 7 | 5 17
sio xuuuu | -145 -118 35 -62 -13 | 0 19
Table 7.1717.1 GPS week: 1717 Day: 1 MJD: 56264.500
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 | -41 10 110 33 5 | -4 19
emr uuuxu | -6 38 180 324 15 | -1 20
esa uuuuu | 44 -57 -19 29 12 | -7 18
gfz uuuuu | 78 78 47 29 6 | -1 18
grg uuuux | -49 7 44 20 -19 | 7 27
igr xxxxx | -78 32 44 99 11 | -5 18
irf xxxxx | -30 -1 -15 -62 -2 | -5 14
jpl uuuuu | -63 -1 -25 -27 22 | 4 23
mit uuuuu | -1 -7 -128 -182 -17 | -4 13
ngs uuuuu | -96 18 -35 194 -4 | 4 16
sio xuuuu | -129 -52 56 32 -12 | -2 20
Table 7.1717.2 GPS week: 1717 Day: 2 MJD: 56265.500
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 | -17 11 210 -96 12 | -3 19
emr uuuxu | -11 9 -53 375 8 | 1 22
esa uuuuu | -7 -27 -77 -51 6 | -6 19
gfz uuuuu | 87 95 -91 230 3 | 0 19
grg uuuux | -39 -20 -18 66 -20 | 9 26
igr xxxxx | -71 18 27 28 6 | -3 19
irf xxxxx | -4 -11 -14 26 -2 | -4 14
jpl uuuuu | 9 -39 86 75 13 | 7 26
mit uuuuu | 6 -24 29 14 -11 | -5 13
ngs uuuuu | -64 31 41 -108 -5 | 4 16
sio xuuuu | -195 -8 -82 -157 -5 | -2 20
Table 7.1717.3 GPS week: 1717 Day: 3 MJD: 56266.500
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 | 20 -38 45 32 -9 | 2 17
emr uuuxu | -8 -19 -103 305 16 | 5 20
esa uuuuu | -61 15 -8 -1 5 | -3 16
gfz uuuuu | 83 98 -92 40 -5 | 4 16
grg uuuux | 2 -10 -121 81 -22 | 11 25
igr xxxxx | -38 -17 -82 1 -2 | 1 15
irf xxxxx | -7 -43 -20 -35 -2 | -3 13
jpl uuuuu | -3 -41 -130 86 6 | 14 22
mit uuuuu | -30 -50 20 -116 -6 | -6 14
ngs uuuuu | 77 19 269 63 3 | 7 14
sio xxxxx | -300 -98 206 -77 -17 | 1 16
Table 7.1717.4 GPS week: 1717 Day: 4 MJD: 56267.500
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 | 33 -23 111 -307 1 | 2 17
emr uuuxu | 30 -27 176 464 10 | 9 20
esa uuuuu | -98 -37 40 3 3 | -1 15
gfz uuuuu | 124 95 -124 147 5 | 5 15
grg uuuux | 38 -14 -57 197 -47 | 10 25
igr xxxxx | -10 7 -102 71 2 | 2 14
irf xxxxx | 7 -11 -22 38 0 | -2 13
jpl uuuuu | 37 -20 -96 150 -6 | 16 23
mit uuuuu | -11 3 -47 -98 -6 | -6 14
ngs uuuuu | 20 35 65 122 5 | 9 14
sio xuuuu | -293 -30 -33 -57 -13 | 0 17
Table 7.1717.5 GPS week: 1717 Day: 5 MJD: 56268.500
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 | -30 -14 4 -125 3 | 0 15
emr uuuxu | 9 -25 118 343 9 | 7 19
esa uuuuu | -22 -40 100 -13 -7 | -2 14
gfz uuuuu | 86 52 -77 163 -8 | 3 14
grg uuuux | -48 -15 -11 -66 -52 | 4 27
igr xxxxx | -69 27 40 -60 -8 | 2 14
irf xxxxx | 1 -20 -20 49 9 | -4 10
jpl uuuuu | 6 -8 -135 93 -1 | 14 21
mit uuuuu | 7 14 -125 -26 18 | -10 12
ngs uuuuu | -34 77 31 67 -3 | 7 12
sio xuuuu | -135 -94 235 -306 -13 | -3 14
Table 7.1717.6 GPS week: 1717 Day: 6 MJD: 56269.500
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 | 17 -16 117 -213 6 | -2 14
emr uuuxu | 22 -31 247 314 23 | 6 17
esa uuuuu | -49 -37 7 -22 9 | -5 15
gfz uuuuu | 99 77 7 135 -1 | 0 13
grg uuuux | -36 -1 31 -55 -75 | -1 32
igr xxxxx | -46 3 82 -6 3 | -2 13
irf xxxxx | 10 -11 -7 9 -2 | -5 10
jpl uuuuu | 27 -1 -50 79 12 | 12 19
mit uuuuu | 50 -16 -114 37 -15 | -9 12
ngs uuuuu | -102 85 -82 -2 -4 | 5 10
sio xuuuu | -148 -86 162 -34 -6 | -8 15
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