[IGSREPORT-21566] Wk 1724 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Feb 8 10:42:20 PST 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1724 (Jan 20, 2013 - Jan 26, 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:
igs1724[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1724[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1724[0-6].cls IGS GPS clock combination summary report.
igs17247.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17247.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 | 6 6 KOUC YELL KOUC YELL
0 | ESA | 6 6 UNSA
0 | GFZ | BOGT KIRU MATE QAQ1
0 | GRG | 3 3 MATE MCM4 SYOG USNO FAA1 MATE MCM4 SYOG USNO
0 | JPL | 3 6
0 | MIT | 3 15 16 18 21 3 15 16 18 19 21 JOZ2 JOZ2 TLSE
1 | COD | 6 6 KOUC NTUS FLRS KOUC MCM4 NTUS
1 | ESA | 6 6 NTUS NTUS UNSA
1 | GFZ | BOGT NTUS
1 | GRG | 3 3 MAW1 USNO ABMF LHAZ MAW1 SPT0 USNO
1 | JPL | 3 6
1 | MIT | 3 15 3 15 JOZ2 CONZ JOZ2 MAW1
2 | COD | 4 4 6 KOUC WUHN KOUC WUHN
2 | EMR | 6
2 | ESA | 6 NICO NICO
2 | GFZ | ABMF BOGT GRAS HARB METS TIDB WUHN
2 | GRG | 6 6 HARB HARB NYAL
2 | JPL | 3 6 30 PALM
2 | MIT | 3 4 6 26 3 4 19 26 JOZ2 USNO JOZ2 MDVJ USNO
3 | COD | 6 6 30 FLRS KOUC
3 | EMR | HERS
3 | ESA | 6 6 MATE MATE
3 | GFZ | BOGT BRFT MATE NOVM SEY1 TWTF
3 | GRG | 1 1 IRKT IRKT NKLG
3 | JPL | 6
3 | MIT | 1 3 28 30 1 3 28 30
4 | COD | 6 30 6 30 HERT JOZ2 KOUC PDEL SOFI WROC HERT JOZ2
4 | COD | KOUC SOFI WROC
4 | EMR | HOB2 SFER
4 | ESA | 6 6 HOB2
4 | GFZ | BOGT FLRS WTZR
4 | GRG | 1 1 HOB2 LPGS NKLG SFER LPGS NKLG
4 | JPL | 6
4 | MIT | 3 30 3 30 PDEL SFER PDEL SFER
5 | COD | NTUS NTUS REUN
5 | EMR | 6 6
5 | ESA | NTUS ASPA NTUS
5 | GFZ | BOGT BOR1 NTUS RIOP SUTM
5 | GRG | REUN SOFI MANA REUN SOFI WTZR
5 | JPL | 3
5 | MIT | 6 7 6 7 WTZR
6 | COD | BRMU MAC1 BAKO BRMU
6 | ESA | UNSA
6 | GFZ | 10 30 BOGT FAIR KOUC MANA NRMD WES2
6 | GRG | BRMU MAC1 NYAL WES2
6 | JPL | 6 24 TIXI
6 | MIT | 6 6 19 YELL NTUS NYAL YELL
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
----+------------+----------
G31 | 2013_01_23 | 2013008
7. 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.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | 1.2 .4 .6 -15 -19 -35 -.04
EMR | 0 | -1.8 5.2 19.3 12 6 0 -.08
ESA | 0 | .7 -2.9 -1.4 4 -134 113 -.02
GFZ | 0 | .5 .2 -.2 -35 -34 -12 -.02
GRG | 0 | -3.0 -7.6 5.6 -39 39 -39 .22
JPL | 0 | -7.5 -1.6 21.6 -121 -48 -38 .03
MIT | 0 | .6 .0 9.5 -14 12 -29 .25
NGS | 0 | -3.8 -6.2 1.1 -43 20 -19 .56
SIO | 0 | 8.1 -3.6 -29.3 38 -280 21 .16
COD | 1 | .4 .4 -.7 -32 -7 -16 -.02
EMR | 1 | 1.4 .7 20.2 15 9 1 -.03
ESA | 1 | -1.3 3.0 -1.1 92 -117 95 .11
GFZ | 1 | -.4 .7 -1.0 -17 -27 -20 -.09
GRG | 1 | .0 -.3 9.9 -33 35 -39 .33
JPL | 1 | -1.7 1.4 21.7 -95 -21 -29 -.19
MIT | 1 | -.3 3.3 11.6 -18 4 -36 .20
NGS | 1 | 2.0 1.1 4.3 -15 -26 40 .44
SIO | 1 | 10.5 1.4 -14.6 94 -276 49 .07
COD | 2 | -.4 -.3 -1.4 -37 3 -27 .16
EMR | 2 | 3.5 7.2 21.4 4 16 8 -.01
ESA | 2 | 1.2 3.8 -2.8 90 -144 104 .47
GFZ | 2 | -.9 -.3 -1.9 -24 -19 -19 .15
GRG | 2 | 6.4 .7 4.0 -40 30 -20 .56
JPL | 2 | 2.0 .6 23.4 -98 -39 -11 -.05
MIT | 2 | 4.8 5.2 7.8 -6 -2 -21 .32
NGS | 2 | .0 -2.7 5.7 -41 -15 17 .79
SIO | 2 | 9.2 1.0 -16.3 141 -246 126 .16
COD | 3 | -.9 .4 -1.1 -28 8 -24 -.01
EMR | 3 | 1.5 4.7 20.2 8 14 2 .03
ESA | 3 | -.9 -.6 -6.8 44 -123 133 .25
GFZ | 3 | -.2 .9 -1.8 -18 -23 -8 -.05
GRG | 3 | -.5 -5.3 -1.8 -19 19 -38 .22
JPL | 3 | 2.9 .0 21.1 -85 35 -71 .08
MIT | 3 | 2.1 -2.4 6.4 -12 4 -19 .05
NGS | 3 | .1 -.6 7.2 -35 -11 13 .47
SIO | 3 | 7.4 2.6 -15.7 130 -198 186 -.14
COD | 4 | -.2 .3 -.6 -37 -12 -19 -.15
EMR | 4 | .7 5.2 18.9 12 16 3 -.09
ESA | 4 | -1.5 -2.4 -3.6 15 -114 94 .20
GFZ | 4 | -.7 .8 -1.2 -26 -40 -19 -.35
GRG | 4 | -2.7 -3.2 -5.0 -4 8 -14 -.05
JPL | 4 | .5 -3.0 24.9 -64 27 -23 -.25
MIT | 4 | 1.9 -.9 6.7 -13 8 -33 -.18
NGS | 4 | -4.6 1.9 10.4 -55 2 -28 .19
SIO | 4 | 5.3 -2.2 -8.5 71 -165 266 -.28
COD | 5 | -.3 .4 -.4 -41 2 -6 -.16
EMR | 5 | .1 -.1 21.3 11 9 1 .07
ESA | 5 | .8 1.7 -3.3 71 -130 90 .22
GFZ | 5 | -.1 .6 -1.1 -33 -35 -9 -.22
GRG | 5 | 3.5 -3.2 -.6 -7 20 -18 .33
JPL | 5 | -5.1 -.3 27.3 -167 -3 59 .13
MIT | 5 | -2.5 1.7 1.7 -10 9 -31 -.01
NGS | 5 | -4.6 -1.8 4.4 -35 22 -31 .32
SIO | 5 | 5.1 -1.0 -28.3 103 -217 226 -.18
COD | 6 | -.2 .0 -.5 -45 14 2 -.22
EMR | 6 | 2.2 8.8 25.2 23 12 -9 -.10
ESA | 6 | -1.3 4.1 -7.3 94 -123 86 .17
GFZ | 6 | -.2 .7 -.6 -22 -18 -5 -.18
GRG | 6 | 3.2 1.4 .0 -13 -30 9 .13
JPL | 6 | -8.0 5.7 29.0 -96 -22 -50 .06
MIT | 6 | -2.6 3.7 8.6 -9 7 -29 -.14
NGS | 6 | -7.2 .5 13.6 -79 30 -50 .48
SIO | 6 | .8 1.6 -10.3 112 -92 357 -.11
9. 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.
10. 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 1.1724.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1724.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 2.1724.[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 3.1724.[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 5.1724.0-6). 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 1724 summary. (Jan 20, 2013 - Jan 26, 2013)
Table 1.1724.a GPS week: 1724 MJD: 56312.000-56318.000
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| -1 0 -4 -6 13 -8 -.47 12 11 | -859 53 18 87
| 0 0 1 37 17 12 .06 | 515 1056
emr 80| 1 -1 14 -31 -4 -23 .12 16 16 | 2187 641 14 103
| 0 1 2 23 16 6 .04 | 1641 767
esa 174| 0 0 0 63 -40 23 .08 5 5 | -661 678 10 99
| 0 0 1 26 10 14 .03 | 1506 2416
gfz 190| 0 -1 -3 -62 -16 6 -.43 10 10 | -23 94 19 124
| 0 0 1 32 31 17 .04 | 383 677
grg 140| 1 1 -6 -1 44 -8 .61 15 14 | -93 9 16 140
| 1 0 1 12 15 10 .03 | 273 410
igr n/a| 0 0 -2 -11 65 -24 -.16 4 4 | 4031 329 16 84
| 0 0 0 22 15 16 .02 | 1240 813
jpl 80| 1 -1 4 -33 3 -30 .28 13 13 | 3491 609 17 109
| 1 1 1 25 31 26 .03 | 1606 767
mit 239| 0 0 -1 3 6 7 -.19 6 6 | -255 313 20 176
| 0 0 0 19 17 8 .02 | 243 566
ngs 243| 0 0 2 -31 51 -27 .31 10 9 | -858 -12 1822 3280
| 0 1 3 38 52 16 .04 | 464 916
sio 258| -1 -1 1 67 -160 146 -.54 21 18 | --- --- --- ---
| 1 0 1 42 52 121 .07 | --- ---
Table 1.1724.b GPS week : 1724 MJD: 56312.000-56318.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 6 6 6 6 6 6 5 |
4 | 3 3 3 3 3 3 3 |
5 | 4 3 3 3 3 4 4 |
6 | 4 4 4 4 5 5 5 |
7 | 5 4 4 4 4 4 5 |
8 | 4 3 3 3 3 4 4 |
9 | 5 4 3 3 4 4 4 |
10 | 4 3 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 4 4 4 4 4 4 4 |
13 | 4 4 4 4 4 4 5 |
14 | 3 3 3 3 4 4 4 |
15 | 5 4 4 4 4 5 4 |
16 | 4 4 4 4 4 4 4 |
17 | 4 4 4 4 5 4 5 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 3 3 4 4 |
20 | 3 3 3 3 4 3 4 |
21 | 4 4 5 4 4 4 4 |
22 | 3 3 3 3 3 4 3 |
23 | 4 4 4 4 4 4 4 |
24 | 5 4 4 4 5 5 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 3 3 3 3 3 3 |
27 | 0 0 0 0 0 0 0 |
28 | 4 3 4 3 4 4 3 |
29 | 4 4 5 4 5 4 5 |
30 | 3 3 3 4 3 3 4 |
31 | 4 4 4 0 5 4 4 |
32 | 3 3 3 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
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 2.1724.0 GPS week: 1724 Day: 0 MJD: 56312.000
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 57 4 -13 -.51 12 11 | -786 -209 19 84
emr 80| 1 -1 13 -27 6 -27 .12 15 15 | -200 1053 13 90
esa 174| 1 0 1 30 -34 26 .06 5 5 | 1400 -1707 9 96
gfz 192| -1 0 -2 -98 24 4 -.41 10 10 | -502 575 19 120
grg 139| 2 1 -4 -8 66 -18 .59 15 14 | -154 57 19 150
igr n/a| 0 0 -2 21 64 -29 -.18 4 4 | 2234 807 17 84
jpl 80| 1 -1 2 -38 -25 -26 .30 14 13 | 1224 963 16 109
mit 240| 0 0 -1 -6 23 18 -.19 9 9 | -312 245 22 180
ngs 245| -1 -1 -2 28 12 -52 .24 11 9 | -852 -168 1711 3347
sio 255| -3 -2 1 -12 -198 -12 -.47 21 18 | --- --- --- ---
Table 2.1724.1 GPS week: 1724 Day: 1 MJD: 56313.000
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 266| -1 0 -2 -30 -8 0 -.43 11 10 | -464 -532 18 93
emr 80| 2 -1 11 -42 -17 -19 .16 16 16 | 887 702 13 103
esa 174| 0 0 1 59 -37 4 .10 5 5 | -461 20 9 91
gfz 190| 0 -1 -3 -12 26 10 -.38 10 9 | 273 -691 17 121
grg 140| 1 1 -4 5 47 -11 .65 16 15 | 18 -11 14 128
igr n/a| 0 0 -1 -20 47 -47 -.15 4 4 | 2936 410 14 90
jpl 80| 0 -1 3 -47 -14 1 .31 13 13 | 2015 603 17 119
mit 238| 0 0 -1 8 37 0 -.19 5 5 | 49 -121 21 210
ngs 245| 0 2 0 -60 -24 -13 .31 11 9 | -502 -518 1792 2817
sio 256| -3 0 0 53 -213 23 -.44 19 16 | --- --- --- ---
Table 2.1724.2 GPS week: 1724 Day: 2 MJD: 56314.000
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 -4 -22 15 -17 -.46 13 12 | -2005 2054 20 89
emr 80| 1 0 12 -59 21 -24 .14 15 15 | 1631 606 13 100
esa 174| 0 0 0 55 -24 24 .08 5 5 | 512 -2192 10 104
gfz 188| 0 -1 -3 -27 -34 7 -.45 10 10 | 38 492 20 135
grg 141| 2 0 -5 -19 61 -6 .58 16 14 | -305 335 17 170
igr n/a| 0 0 -1 -45 86 -33 -.11 4 4 | 3696 532 17 80
jpl 80| 0 0 3 -19 34 -11 .24 14 13 | 2923 821 16 113
mit 240| 0 0 -1 21 -3 6 -.14 6 5 | -493 991 19 161
ngs 242| 0 0 2 -68 25 -47 .31 11 9 | -1878 1708 1827 3239
sio 261| -1 -1 0 118 -210 96 -.52 19 18 | --- --- --- ---
Table 2.1724.3 GPS week: 1724 Day: 3 MJD: 56315.000
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 1 -2 20 6 -15 -.40 11 10 | -730 -301 15 86
emr 80| 1 -1 12 0 -6 -24 .12 15 15 | 1951 1770 14 103
esa 174| 0 1 0 56 -41 43 .12 5 5 | 276 764 8 99
gfz 193| 0 -1 -3 -93 -19 -2 -.37 10 9 | 447 633 18 123
grg 144| 0 1 -5 1 43 -18 .57 14 13 | 80 112 16 128
igr n/a| 0 0 -2 8 57 -28 -.17 4 4 | 4066 1368 15 82
jpl 80| 0 0 6 7 45 -62 .26 14 13 | 3527 1674 15 114
mit 240| 0 0 -1 -20 -9 0 -.20 5 5 | -357 776 20 179
ngs 245| 0 0 1 -12 63 -12 .34 10 8 | -781 -110 1807 4021
sio 262| -1 0 2 89 -156 138 -.58 19 18 | --- --- --- ---
Table 2.1724.4 GPS week: 1724 Day: 4 MJD: 56316.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| -2 0 -4 7 15 -22 -.45 12 11 | -661 205 23 93
emr 80| 2 0 13 -7 4 -22 .16 16 16 | 2690 1036 14 108
esa 174| 0 0 0 41 -40 22 .10 6 6 | -1791 3514 11 97
gfz 186| 0 -2 -5 -74 -54 -13 -.43 10 10 | -465 -60 20 132
grg 143| 1 2 -6 10 35 -10 .61 15 13 | -543 572 18 139
igr n/a| 0 0 -2 -12 48 -23 -.18 4 4 | 4358 719 18 86
jpl 80| 1 0 4 -20 5 -10 .32 14 13 | 3911 1002 19 116
mit 239| 0 0 -2 28 10 17 -.20 6 6 | -562 735 17 157
ngs 241| 0 0 6 -49 54 -27 .32 10 9 | -587 -7 1716 3261
sio 255| -1 0 1 68 -117 249 -.62 21 19 | --- --- --- ---
Table 2.1724.5 GPS week: 1724 Day: 5 MJD: 56317.000
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 1 -3 -24 47 2 -.56 12 12 | -713 493 17 84
emr 80| 2 -2 18 -21 -10 -31 .12 16 16 | 4523 -276 17 113
esa 174| 0 1 -1 96 -59 34 .05 6 5 | -2798 4193 11 107
gfz 192| 0 -1 -4 -71 -40 -1 -.46 11 11 | -243 669 19 112
grg 140| 0 1 -7 13 30 -10 .61 14 14 | 297 -326 17 122
igr n/a| 0 0 -1 -4 80 0 -.18 5 5 | 5948 -594 17 84
jpl 80| 1 -2 5 -71 15 -68 .28 13 12 | 5760 -246 21 101
mit 240| 0 1 -1 9 -7 13 -.20 7 7 | 40 189 22 187
ngs 244| 0 -1 2 -64 102 -21 .35 10 8 | -722 317 1707 3071
sio 258| 0 -1 3 95 -156 203 -.61 21 18 | --- --- --- ---
Table 2.1724.6 GPS week: 1724 Day: 6 MJD: 56318.000
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 0 -7 -53 11 10 -.53 12 12 | -655 -1339 17 82
emr 80| 1 1 17 -58 -27 -12 .04 16 16 | 3830 -401 17 104
esa 174| 0 1 -3 102 -46 5 .04 6 6 | -1767 158 12 102
gfz 191| 0 -1 -2 -62 -17 43 -.49 12 12 | 287 -957 20 126
grg 139| 0 2 -6 -14 27 13 .66 14 13 | -46 -672 17 145
igr n/a| 0 0 -1 -24 75 -7 -.16 4 4 | 4984 -939 15 82
jpl 80| 2 -2 6 -48 -41 -34 .27 13 12 | 5080 -552 17 97
mit 239| 0 0 -2 -18 -3 -1 -.19 6 6 | -150 -618 19 159
ngs 243| -1 0 6 6 126 -18 .30 10 8 | -684 -1308 2197 3208
sio 259| 0 -1 1 59 -70 325 -.56 24 19 | --- --- --- ---
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 3.1724.0 GPS week: 1724 Day: 0 MJD: 56312.000
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 21 3 9 11 4 18 6 12 16 4 | 25 30 24 20 34 25 38 26 32 26 25
2 | 15 18 4 10 11 3 15 9 7 22 4 | 25 31 20 23 22 21 27 25 25 30 22
3E | 21 19 7 13 14 6 19 11 31 30 6 | 72 75 68 72 70 71 73 70 87 83 71
4 | 11 10 4 9 13 4 10 9 7 12 3 | 29 27 28 32 32 29 29 29 29 25 29
5 | 10 13 4 11 13 3 11 11 8 32 3 | 34 36 36 40 42 36 39 37 38 36 37
6E | 12 17 4 10 13 5 18 9 15 19 4 | 34 31 27 28 31 29 32 32 31 24 28
7 | 12 18 5 9 21 5 17 9 11 11 4 | 17 27 19 14 37 17 29 21 29 15 20
8 | 10 12 4 10 14 3 11 9 8 14 3 | 18 22 16 16 21 14 20 16 24 13 17
9 | 10 18 6 12 23 5 14 11 6 32 4 | 55 61 52 50 57 52 59 48 55 51 52
10 | 18 8 5 8 11 4 10 10 12 26 3 | 34 29 30 34 37 32 36 32 31 29 32
11 | 10 18 5 9 20 3 12 6 12 21 4 | 20 32 21 17 43 21 30 22 28 19 23
12 | 11 16 5 10 19 4 16 10 10 19 4 | 24 26 21 21 35 19 29 23 26 16 23
13 | 12 14 4 11 22 4 10 8 9 13 4 | 26 32 19 17 40 19 29 19 30 22 23
14 | 8 13 4 7 13 3 9 9 7 21 3 | 16 23 15 13 23 13 22 15 20 23 16
15 | 20 15 5 10 16 6 14 10 10 17 4 | 26 29 20 20 31 15 24 17 28 16 21
16 | 10 12 5 12 15 4 16 8 10 22 3 | 19 23 18 20 30 17 27 21 23 21 20
17E | 11 14 4 7 12 4 15 9 9 12 3 | 24 28 22 24 30 21 26 24 27 27 24
18 | 7 13 5 16 17 4 15 8 10 28 4 | 34 33 35 40 37 33 34 35 37 38 35
19E | 14 15 5 11 9 5 13 7 15 23 4 | 43 34 36 33 33 34 37 35 37 34 34
20 | 10 10 5 10 9 2 9 7 11 20 3 | 35 38 38 34 40 36 41 35 38 35 36
21 | 9 16 6 10 13 4 15 10 11 27 4 | 28 33 26 30 33 25 34 24 31 34 28
22 | 8 11 4 7 10 2 11 7 8 29 2 | 39 35 37 38 41 37 37 37 36 46 37
23 | 8 16 4 9 16 5 13 8 8 17 3 | 18 29 18 13 31 15 27 18 26 17 19
24 | 14 27 5 9 14 5 13 12 8 18 4 | 47 39 40 43 52 44 46 49 51 36 45
25 | 10 17 4 10 17 3 14 10 10 14 4 | 21 21 19 16 29 16 30 20 25 15 20
26 | 9 14 7 8 13 4 12 9 7 15 3 | 17 22 13 16 18 11 19 17 17 11 15
X27 | 8 --- --- --- --- 73 --- --- --- --- 0 | 41 --- --- --- --- 31 --- --- --- --- 44
28 | 9 12 4 7 17 4 12 7 12 16 3 | 20 28 20 16 28 16 26 19 27 18 20
29E | 9 18 5 9 11 4 18 10 12 16 4 | 25 21 19 23 20 19 20 19 27 19 19
30 | 11 9 4 8 13 4 11 7 7 24 3 | 14 17 16 15 23 14 22 15 23 24 16
31 | 10 15 4 8 22 3 20 9 11 11 4 | 11 21 12 10 37 11 24 14 22 7 16
32 | 8 11 4 7 13 2 8 7 12 33 3 | 19 24 21 20 30 21 28 22 20 27 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 5 10 15 4 14 9 11 21 |T 28 30 26 26 34 25 32 26 31 27 27
WRMS | 11 15 5 10 14 4 13 9 9 18 |NE 26 29 24 24 33 23 31 25 29 25 26
MEDI | 10 15 4 9 13 4 13 9 10 19 |MD 25 29 21 21 33 21 29 23 28 24 23
Table 3.1724.1 GPS week: 1724 Day: 1 MJD: 56313.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 22 3 7 12 3 16 4 9 14 3 | 18 25 15 13 28 16 28 17 20 21 17
2 | 11 19 5 10 10 2 16 4 8 21 3 | 22 27 15 17 17 17 23 18 20 28 18
3E | 18 18 9 11 15 6 17 9 24 22 5 | 69 70 68 64 71 65 72 65 76 67 67
4 | 10 9 5 7 14 2 8 5 7 11 2 | 25 22 21 23 20 21 21 20 21 20 21
5 | 10 13 5 8 11 3 14 5 9 28 3 | 20 27 21 21 27 21 26 21 26 22 22
6E | 12 17 5 10 16 4 16 6 12 18 4 | 28 27 22 29 17 25 24 28 28 20 24
7 | 11 17 5 9 21 4 18 5 14 10 4 | 17 27 17 13 36 16 25 18 29 14 18
8 | 10 14 6 7 12 4 11 3 11 15 3 | 19 26 16 15 22 16 24 16 24 14 18
9 | 11 15 5 13 12 5 10 5 11 24 3 | 38 52 43 39 47 42 49 41 46 50 43
10 | 12 9 3 10 13 2 7 5 10 24 3 | 19 22 18 22 26 20 21 18 23 20 20
11 | 9 16 4 10 22 4 10 5 12 20 3 | 15 24 16 16 39 14 26 15 24 19 18
12 | 8 15 5 8 19 5 14 5 9 14 3 | 19 25 17 17 31 15 24 15 23 15 18
13 | 10 20 4 12 21 4 11 4 10 12 3 | 20 32 18 14 38 16 23 18 27 20 20
14 | 7 15 4 7 15 3 10 5 6 19 3 | 16 23 14 14 25 14 19 14 20 25 15
15 | 10 19 5 10 17 5 13 5 7 15 3 | 21 31 19 19 31 15 23 16 24 15 20
16 | 11 13 4 11 16 5 18 6 10 21 3 | 16 20 14 15 26 11 22 10 17 15 13
17E | 15 15 5 8 13 3 14 7 11 13 3 | 29 29 24 25 30 23 27 26 26 24 25
18 | 9 15 5 18 19 4 15 6 11 26 4 | 26 26 24 31 25 23 23 23 24 25 24
19E | 7 18 5 7 16 4 15 4 10 17 3 | 37 37 33 30 29 32 33 31 35 36 32
20 | 10 10 5 15 11 4 9 6 6 19 3 | 19 24 22 23 26 21 25 22 23 21 21
21 | 8 15 5 8 15 4 15 4 10 25 3 | 19 26 21 20 28 20 26 21 25 30 21
22 | 5 11 4 10 14 2 11 4 9 26 3 | 25 25 24 25 29 24 26 23 23 33 24
23 | 10 18 5 10 15 3 13 4 10 15 3 | 17 27 18 10 31 14 23 17 26 17 18
24 | 13 25 7 9 16 5 12 7 13 20 4 | 32 31 31 31 37 32 33 30 33 25 30
25 | 14 16 4 8 19 5 14 6 10 13 3 | 22 22 20 16 29 18 29 17 26 18 20
26 | 8 12 6 8 12 4 11 3 8 12 3 | 18 22 11 16 17 12 19 13 17 11 14
X27 | 7 --- --- --- --- 73 --- --- --- --- 0 | 30 --- --- --- --- 42 --- --- --- --- 31
28 | 9 12 5 8 16 4 11 5 11 15 3 | 21 30 19 18 31 18 26 18 28 19 21
29E | 10 16 5 8 24 5 14 6 13 11 4 | 24 24 17 19 21 19 19 19 26 19 19
30 | 11 11 3 8 15 6 12 5 9 24 3 | 13 20 13 13 20 10 16 10 20 21 13
31 | 12 15 5 9 23 4 17 6 13 14 4 | 13 19 11 13 22 11 18 11 18 12 14
32 | 8 12 2 6 14 3 7 3 7 32 2 | 17 22 18 15 26 18 21 17 20 25 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 5 10 16 4 13 5 11 19 |T 23 27 21 21 29 21 26 20 26 23 22
WRMS | 10 16 5 9 15 4 13 5 9 16 |NE 20 26 19 18 28 19 24 18 24 21 20
MEDI | 10 15 5 9 15 4 13 5 10 18 |MD 20 26 18 18 28 18 24 18 24 20 20
Table 3.1724.2 GPS week: 1724 Day: 2 MJD: 56314.000
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 21 3 6 12 3 15 9 7 14 3 | 21 23 18 15 30 17 28 20 21 20 18
2 | 11 19 5 12 13 3 15 5 9 19 4 | 20 26 16 18 16 15 20 18 16 25 16
3E | 18 20 10 11 15 6 17 7 24 25 5 | 60 65 58 57 62 58 64 56 68 56 59
4 | 9 11 5 8 14 3 8 3 9 13 2 | 27 19 22 21 21 19 18 20 20 20 20
5 | 12 13 5 9 11 3 11 7 8 26 3 | 31 28 28 27 30 27 27 25 28 24 27
6E | 12 17 6 8 15 3 16 5 17 19 4 | 26 27 23 29 21 23 24 26 24 24 22
7 | 11 16 5 10 20 2 21 6 8 10 4 | 17 26 19 13 34 16 28 18 24 15 18
8 | 13 11 6 7 14 4 11 4 7 12 3 | 18 22 15 14 19 12 20 14 18 14 15
9 | 10 13 5 10 12 5 10 6 8 25 3 | 54 60 57 54 59 55 60 54 57 61 56
10 | 14 7 4 10 11 3 7 5 9 23 3 | 21 24 23 26 29 25 25 24 19 23 23
11 | 12 14 5 9 23 3 9 7 12 17 4 | 16 24 16 14 37 15 21 16 24 16 16
12 | 15 15 5 11 20 6 15 6 10 15 4 | 20 23 17 17 29 16 21 15 23 14 17
13 | 10 19 3 10 22 4 10 6 10 11 4 | 15 28 16 12 37 15 20 16 20 16 16
14 | 8 15 6 8 15 2 12 5 9 16 3 | 12 22 12 11 23 10 17 12 16 20 11
15 | 20 16 6 11 17 4 13 7 9 15 4 | 22 25 14 16 28 12 18 13 20 13 15
16 | 12 16 5 11 15 5 19 6 11 20 4 | 15 23 15 14 21 14 24 13 15 16 12
17E | 15 15 4 10 15 4 16 7 15 18 4 | 18 20 14 16 19 14 17 18 18 23 15
18 | 15 14 6 15 17 3 14 5 11 27 4 | 21 24 27 28 25 24 22 23 27 28 23
19E | 12 18 6 6 23 4 15 6 11 10 4 | 23 25 23 21 31 21 21 21 25 20 20
20 | 10 9 8 10 8 4 10 6 7 21 3 | 21 27 29 24 27 25 29 28 27 27 26
21 | 18 16 7 12 15 3 17 7 9 24 4 | 23 26 21 16 30 19 26 17 22 20 18
22 | 9 10 4 12 9 2 11 3 11 23 3 | 23 27 28 29 30 26 25 24 24 34 25
23 | 7 18 6 9 14 5 15 5 10 13 3 | 10 23 14 8 27 12 21 12 19 13 13
24 | 18 24 5 9 16 6 12 5 8 16 4 | 26 27 29 29 32 29 31 28 31 25 26
25 | 14 17 5 11 18 4 14 6 8 12 4 | 12 19 17 15 28 13 26 15 20 12 15
X26 | 7 10 5 --- 11 4 11 5 9 --- 3 | 14 17 9 --- 12 10 16 13 13 --- 11
X27 | 7 --- --- --- --- 69 --- --- --- --- 0 | 43 --- --- --- --- 48 --- --- --- --- 44
28 | 10 12 5 9 17 4 12 5 14 16 3 | 16 25 14 18 27 14 20 16 23 15 16
29E | 18 16 6 11 19 4 16 5 13 15 4 | 24 19 15 15 19 17 15 14 24 15 14
30 | 10 10 4 8 12 4 11 4 6 24 2 | 10 17 13 11 16 10 15 10 15 20 9
31 | 13 14 4 9 21 6 19 6 10 13 4 | 13 23 15 13 35 13 19 13 20 8 14
32 | 10 10 3 7 10 3 9 3 7 32 2 | 12 19 16 16 21 15 21 17 15 27 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 15 5 10 16 4 14 6 11 19 |T 22 25 21 20 28 20 24 20 23 22 20
WRMS | 12 15 5 10 14 4 13 5 9 18 |NE 20 24 20 19 27 19 23 19 22 21 19
MEDI | 12 15 5 10 15 4 13 6 9 16 |MD 20 24 17 16 28 16 21 17 21 20 16
Table 3.1724.3 GPS week: 1724 Day: 3 MJD: 56315.000
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 20 3 9 11 3 14 7 8 14 3 | 19 22 18 11 27 17 28 17 24 16 17
2 | 10 20 5 10 10 3 15 4 8 17 3 | 21 26 14 18 16 16 23 19 17 27 16
3E | 24 20 11 13 19 6 19 8 18 19 5 | 73 76 73 73 75 70 77 70 79 73 72
4 | 10 10 4 6 11 2 9 4 6 14 2 | 23 20 20 23 24 22 21 22 17 20 20
5 | 9 13 4 8 13 2 12 4 8 25 3 | 29 30 30 32 35 30 30 31 29 27 30
6E | 13 17 8 11 14 4 17 6 12 21 4 | 30 26 25 27 24 26 26 26 26 21 24
7 | 8 21 5 9 17 4 18 4 11 12 4 | 19 28 20 16 37 19 27 18 30 17 20
8 | 8 10 4 8 11 3 11 3 8 11 2 | 17 20 13 15 19 13 22 14 20 13 15
9 | 8 13 5 7 11 5 14 6 9 28 3 | 42 51 43 43 47 42 53 43 45 55 44
10 | 11 8 3 8 10 3 6 5 8 23 2 | 26 23 25 28 29 27 27 27 23 24 25
11 | 9 19 5 7 21 2 10 4 8 15 3 | 14 24 18 13 40 15 24 15 25 14 17
12 | 10 15 5 9 18 5 14 6 10 15 3 | 18 22 17 18 29 14 25 15 22 13 17
13 | 14 17 4 11 22 3 13 5 7 12 4 | 20 29 17 15 38 15 27 16 20 18 18
14 | 8 13 5 10 15 3 10 5 11 15 3 | 14 19 14 16 24 11 19 12 18 19 12
15 | 10 16 5 8 16 3 13 5 9 15 3 | 23 26 14 12 28 12 22 14 18 15 15
16 | 11 17 6 15 11 3 17 5 9 21 4 | 15 18 16 16 23 12 23 11 16 15 13
17E | 11 15 6 8 13 3 18 8 11 15 4 | 21 22 17 18 21 16 24 18 22 17 18
18 | 9 15 4 19 18 3 16 6 10 27 4 | 29 26 30 37 33 29 28 30 30 31 29
19E | 8 14 6 7 11 4 13 4 11 12 3 | 24 22 23 20 24 20 24 21 23 22 20
20 | 11 11 6 11 10 4 10 4 7 20 3 | 29 32 35 29 33 30 33 31 30 31 31
21 | 7 16 6 10 16 3 15 4 12 23 3 | 18 24 19 20 28 16 26 18 21 22 18
22 | 7 10 4 11 11 3 10 4 10 22 3 | 32 31 32 35 36 32 33 34 29 36 32
23 | 12 17 6 9 14 4 17 5 9 13 3 | 18 25 18 13 28 14 27 14 23 17 16
24 | 12 23 5 7 15 6 11 6 10 16 3 | 27 27 27 29 34 28 31 29 28 26 27
25 | 11 17 4 10 16 4 13 5 7 12 3 | 16 18 18 15 27 14 28 14 19 12 16
26 | 9 12 6 8 11 3 10 4 9 11 3 | 17 16 10 17 14 10 18 13 13 13 11
X27 | 6 --- --- --- --- 67 --- --- --- --- 0 | 53 --- --- --- --- 51 --- --- --- --- 52
28 | 9 13 6 8 14 2 13 4 8 13 3 | 22 27 19 19 28 17 27 17 24 14 19
29E | 12 18 4 10 12 5 19 7 8 15 4 | 30 23 18 22 19 19 25 20 22 19 19
30 | 11 10 6 9 12 5 10 6 14 25 3 | 11 15 15 13 17 10 20 11 21 21 12
X31 | 6 --- --- --- --- 19 --- --- --- --- 0 | 76 --- --- --- --- 62 --- --- --- --- 80
32 | 10 12 4 10 9 4 9 3 8 32 2 | 18 22 23 20 27 19 25 21 23 27 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 5 10 14 4 14 5 10 19 |T 26 26 22 22 29 23 28 22 25 23 24
WRMS | 10 15 5 9 13 4 13 5 8 18 |NE 24 24 21 20 28 22 26 20 23 21 23
MEDI | 10 15 5 9 13 3 13 5 9 15 |MD 21 24 18 18 28 17 26 18 23 19 19
Table 3.1724.4 GPS week: 1724 Day: 4 MJD: 56316.000
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 26 7 10 11 2 13 5 7 19 4 | 16 22 15 12 28 14 25 15 17 18 14
2 | 13 20 7 11 14 3 14 7 9 19 4 | 20 28 14 16 19 14 22 20 18 27 16
3E | 25 19 10 12 20 7 19 6 14 24 5 | 54 56 51 48 59 49 55 50 60 45 51
4 | 11 11 5 9 12 3 9 3 10 13 3 | 22 17 19 24 22 20 19 20 20 19 19
5 | 8 13 5 8 10 4 13 4 9 25 3 | 25 29 26 29 29 26 29 26 22 23 26
6E | 14 19 6 13 18 4 17 7 12 23 4 | 28 23 22 27 18 22 26 25 24 22 21
7 | 10 17 5 7 14 4 20 5 8 12 3 | 13 23 15 11 32 13 25 14 22 13 15
8 | 9 14 6 9 12 4 11 5 10 15 3 | 20 28 20 23 23 17 28 19 20 19 20
9 | 12 14 5 12 11 6 11 9 7 38 3 | 64 72 66 63 68 64 72 61 69 66 66
10 | 11 9 4 12 10 2 8 3 10 25 3 | 25 21 21 29 26 23 25 24 23 23 23
11 | 9 15 5 12 22 3 9 5 12 18 4 | 13 24 16 15 41 13 25 16 22 15 17
12 | 14 16 6 12 18 4 13 6 7 15 4 | 17 20 16 17 28 12 22 13 20 10 15
13 | 8 19 5 10 24 3 13 6 9 14 4 | 17 28 16 15 40 13 25 18 23 20 18
14 | 9 14 8 10 16 3 11 6 13 16 3 | 14 20 12 17 24 11 17 15 14 24 12
15 | 14 19 5 10 16 4 14 7 11 16 4 | 24 29 16 16 29 13 24 16 20 17 18
16 | 12 14 7 11 12 4 15 7 10 21 3 | 14 20 14 12 23 9 21 10 18 15 12
17E | 10 18 5 11 18 4 20 8 10 18 4 | 18 22 13 15 21 14 23 16 18 18 15
18 | 9 13 4 10 17 4 14 6 13 --- 3 | 24 26 26 30 28 24 25 26 27 --- 25
19E | 11 13 5 9 12 5 12 5 9 17 3 | 20 25 19 20 22 17 23 19 19 30 17
20 | 10 12 8 10 9 3 9 7 9 24 3 | 27 29 34 28 31 28 32 29 30 31 29
21 | 10 16 7 9 14 3 15 3 11 25 3 | 18 27 18 18 29 18 23 18 24 27 19
22 | 6 11 8 10 7 3 11 5 9 21 3 | 29 28 31 33 32 29 27 29 24 35 29
23 | 9 19 7 8 17 3 16 6 8 15 4 | 11 28 16 10 30 11 23 14 20 15 14
24 | 19 24 6 8 19 6 12 6 9 19 4 | 39 32 27 31 36 29 34 31 32 24 30
25 | 11 18 6 9 16 6 14 7 6 11 3 | 14 18 18 13 25 11 27 13 18 11 15
26 | 11 13 5 8 12 4 13 4 7 12 3 | 16 17 6 16 15 8 19 9 9 12 9
X27 | 7 --- --- --- --- 59 --- --- --- --- 0 | 63 --- --- --- --- 27 --- --- --- --- 65
28 | 10 14 5 11 14 3 14 6 11 15 3 | 17 24 16 16 27 13 27 16 22 14 17
29E | 13 20 4 10 18 5 19 6 14 18 4 | 23 25 19 20 19 19 24 18 28 25 19
30 | 11 8 6 11 10 5 11 6 9 26 3 | 8 14 13 13 15 9 16 10 18 22 10
X31 | 10 14 --- 9 17 7 --- 6 7 --- 4 | 10 17 --- 11 25 8 --- 7 13 --- 9
32 | 11 14 5 6 11 2 7 7 10 35 3 | 16 21 20 18 24 16 23 19 17 29 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 10 15 4 14 6 10 21 |T 23 26 21 21 28 19 26 20 23 23 21
WRMS | 11 16 6 10 13 4 13 6 9 19 |NE 22 25 20 20 28 18 26 19 22 22 21
MEDI | 11 14 5 10 14 4 13 6 9 18 |MD 18 24 18 17 27 14 25 18 20 22 18
Table 3.1724.5 GPS week: 1724 Day: 5 MJD: 56317.000
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 22 5 10 12 3 15 7 8 25 4 | 20 23 22 14 31 19 36 19 27 28 20
2 | 10 19 5 13 13 5 14 9 10 17 4 | 21 29 16 19 15 16 22 22 18 27 17
3E | 25 19 10 13 14 9 17 8 19 31 5 | 67 72 67 65 71 65 75 65 75 64 67
4 | 9 12 5 12 11 4 9 5 7 14 3 | 18 17 15 22 18 14 19 17 11 15 14
5 | 9 12 5 11 11 4 12 8 7 27 3 | 24 26 24 28 27 24 27 26 24 24 24
6E | 15 19 5 13 14 5 19 7 16 23 4 | 28 27 22 30 18 23 24 24 24 23 21
7 | 9 22 5 8 16 3 18 5 9 12 4 | 16 28 17 13 32 15 26 17 26 13 17
8 | 10 15 7 8 12 4 11 7 9 14 3 | 17 25 16 15 19 13 25 15 19 16 16
9 | 11 16 4 10 16 7 12 9 11 29 4 | 59 69 61 61 59 60 65 63 64 68 62
10 | 7 9 4 11 10 3 8 5 9 26 2 | 22 22 20 26 22 20 25 21 19 22 21
11 | 9 16 4 10 23 5 10 6 8 18 4 | 13 25 18 13 40 12 26 17 22 14 18
12 | 13 16 4 9 18 5 16 7 8 15 4 | 16 25 16 18 30 14 26 21 25 15 19
13 | 8 19 5 12 23 4 12 6 7 14 4 | 18 31 19 15 39 14 28 17 21 18 19
14 | 12 16 5 9 14 3 9 7 12 17 3 | 15 22 13 15 25 12 19 16 18 22 14
15 | 26 15 5 12 17 4 12 8 9 19 4 | 23 28 15 21 32 16 23 20 22 22 19
16 | 8 15 5 12 12 5 14 6 8 23 3 | 13 21 15 17 24 11 23 17 15 15 15
17E | 11 15 6 12 15 4 16 11 9 18 4 | 18 26 16 21 27 16 26 22 19 22 19
18 | 11 14 5 15 18 4 14 5 9 26 4 | 20 21 25 28 25 22 23 25 27 22 24
19E | 12 12 7 10 17 4 12 8 16 16 4 | 22 22 21 21 25 18 24 20 24 28 19
20 | 7 11 8 11 9 5 10 5 7 22 3 | 22 28 29 23 28 21 30 25 26 19 25
21 | 9 17 5 9 11 4 13 7 10 25 3 | 15 28 17 18 32 17 27 19 24 23 19
22 | 7 12 6 12 11 3 9 5 15 23 3 | 21 22 25 27 29 22 24 24 25 27 23
23 | 10 18 5 10 17 5 16 7 5 15 4 | 18 28 19 16 29 14 25 17 19 17 17
24 | 19 26 7 10 14 4 11 7 14 21 4 | 27 26 21 25 34 23 29 26 35 26 24
25 | 11 19 5 9 15 4 13 8 9 11 4 | 13 21 19 20 27 16 28 25 22 15 20
26 | 12 13 6 9 11 4 8 7 8 14 3 | 19 21 16 23 17 16 21 22 16 21 17
X27 | 9 --- --- --- --- 81 --- --- --- --- 0 | 46 --- --- --- --- 57 --- --- --- --- 46
28 | 11 14 6 8 15 3 11 6 8 17 3 | 20 30 17 17 30 16 26 20 22 15 19
29E | 11 15 6 9 11 6 18 7 12 13 4 | 21 23 18 20 21 18 25 20 24 20 19
30 | 11 11 5 11 11 5 8 6 8 26 3 | 10 14 12 14 16 11 16 15 17 20 12
31 | 10 16 5 9 16 6 18 7 9 --- 4 | 11 18 7 11 18 7 19 12 11 --- 9
32 | 9 12 5 8 11 5 6 5 5 37 2 | 14 21 19 18 23 13 22 17 18 26 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 11 14 5 13 7 10 21 |T 22 27 21 22 28 20 27 22 24 23 22
WRMS | 12 16 5 11 14 5 12 7 8 18 |NE 20 25 19 20 27 19 26 21 22 22 21
MEDI | 10 15 5 10 14 4 12 7 9 18 |MD 19 25 18 20 27 16 25 20 22 22 19
Table 3.1724.6 GPS week: 1724 Day: 6 MJD: 56318.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 14 21 6 13 13 4 15 8 7 26 4 | 23 26 19 21 33 18 32 18 19 24 19
2 | 14 20 7 10 14 4 14 7 8 18 4 | 23 32 16 22 22 17 24 20 17 30 18
3E | 21 17 9 12 15 8 15 7 16 53 5 | 88 88 85 84 92 82 91 82 89 88 86
4 | 9 10 4 8 10 2 8 5 9 14 3 | 25 20 20 24 24 20 24 21 20 20 20
5 | 15 13 5 12 7 4 12 7 7 31 3 | 37 36 36 42 40 36 38 37 35 35 36
6E | 15 17 6 13 17 5 18 8 15 22 4 | 34 31 28 32 25 30 30 32 31 32 28
7 | 11 23 6 12 14 4 20 6 12 15 4 | 15 27 19 17 34 17 29 19 30 14 20
8 | 10 13 4 13 11 3 11 5 10 16 3 | 24 34 19 27 26 19 33 21 24 23 24
9 | 10 14 4 10 14 6 11 7 8 27 3 | 58 62 59 52 63 53 60 55 58 60 57
10 | 11 8 5 9 7 3 8 4 8 29 2 | 30 25 29 33 31 29 31 29 29 30 29
11 | 12 16 6 11 23 5 9 5 12 23 4 | 15 26 19 13 44 15 27 19 24 18 20
12 | 17 17 5 12 13 5 13 5 8 16 4 | 20 23 16 15 27 14 24 16 22 13 17
13 | 10 19 8 11 23 5 11 6 10 15 4 | 19 34 22 16 43 17 29 19 26 21 22
14 | 10 15 4 12 15 3 11 6 7 21 3 | 14 23 13 17 27 10 18 14 17 25 13
15 | 16 18 6 11 16 5 13 5 9 25 4 | 20 34 18 20 31 15 27 20 24 24 21
16 | 12 14 6 13 12 3 13 6 13 23 4 | 16 21 14 17 23 13 21 13 19 18 14
17E | 14 15 6 11 13 5 17 10 13 17 4 | 22 28 23 23 30 20 30 23 25 24 23
18 | 9 12 7 17 16 4 13 5 8 28 4 | 31 31 35 40 36 32 31 34 31 33 33
19E | 11 13 5 12 11 4 12 6 12 21 3 | 30 30 26 26 31 25 29 27 31 35 26
20 | 9 12 8 16 8 4 12 5 10 27 3 | 38 38 44 36 44 38 42 39 39 36 39
21 | 10 17 7 13 16 4 15 5 11 27 4 | 16 26 18 21 35 16 26 17 23 23 18
22 | 6 12 5 12 9 4 10 5 8 28 3 | 38 35 41 43 42 39 38 39 37 45 39
23 | 10 17 7 9 16 5 14 5 8 18 3 | 15 30 18 14 31 13 26 15 24 17 18
24 | 16 24 6 10 15 5 12 6 7 28 4 | 34 32 31 32 39 32 36 33 36 40 32
25 | 8 16 5 11 13 5 13 7 9 14 3 | 16 21 16 13 24 13 29 15 19 12 16
26 | 10 13 6 9 11 4 11 5 8 16 3 | 16 19 11 19 14 10 18 11 12 20 11
X27 | 9 --- --- --- --- 53 --- --- --- --- 0 | 37 --- --- --- --- 27 --- --- --- --- 38
28 | 11 11 5 11 12 3 11 5 7 18 3 | 24 33 24 22 30 19 33 22 25 19 24
29E | 13 16 5 11 12 5 20 9 11 14 4 | 24 24 16 19 19 16 23 19 24 20 18
30 | 12 11 5 11 12 4 12 5 7 24 3 | 8 15 14 13 18 10 16 12 20 21 12
31 | 12 14 6 11 15 3 17 6 8 17 4 | 10 19 7 11 28 9 19 8 13 7 11
32 | 10 13 5 10 8 4 8 5 10 40 3 | 21 22 25 25 31 23 27 24 23 36 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 6 12 14 4 13 6 10 24 |T 26 30 25 26 33 23 31 24 27 27 25
WRMS | 12 16 6 12 13 4 12 6 8 19 |NE 23 28 23 24 32 21 29 22 25 25 23
MEDI | 11 15 6 11 13 4 12 6 9 22 |MD 23 28 19 22 31 18 29 20 24 24 21
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 4.1724 GPS week: 1724 MJD: 56312.0-56318.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 |U 4 5 13 |U 12 14 37 |U 6 7 12 |
emr | emr 2954 | 8 6 20 | 15 14 52 | 10 8 16 |
esa | esa 2947 | 7 4 12 |U 15 17 44 | 8 8 15 |
gfz | gfz 2937 |U 9 6 19 |U 15 17 43 |U 7 7 14 |
grg | grg 2956 |U 9 8 19 |U 16 14 36 | 8 7 20 |
igr | igr 2961 | 6 5 15 | 10 13 38 | 6 6 13 |
igs | igs 2958 | 7 5 16 | 13 14 44 | 7 6 12 |
jpl | jpl 2939 | 9 8 22 |U 14 15 51 |U 9 8 17 |
mit | mit 2962 | 8 7 16 |U 12 14 38 |U 10 12 28 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1724.0 GPS week: 1724 Day: 0 MJD: 56312.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 4 4 14 | ---- ---- ---- | 7 8 13 |
emr | emr 2968 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
esa | esa 2976 | 16 5 15 | ---- ---- ---- | 7 7 13 |
gfz | gfz 2967 | 15 6 18 | ---- ---- ---- | 6 4 11 |
grg | grg 2973 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igr | igr 2975 | 16 5 14 | ---- ---- ---- | 7 7 12 |
igs | igs 2975 | 17 5 15 | ---- ---- ---- | 6 5 10 |
jpl | jpl 2967 | 17 6 17 | ---- ---- ---- | 7 5 15 |
mit | mit 2976 | 17 8 13 | ---- ---- ---- | 7 5 14 |
Table 5.1724.1 GPS week: 1724 Day: 1 MJD: 56313.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 5 7 16 | ---- ---- ---- | 5 3 10 |
emr | emr 2968 | 11 7 22 | ---- ---- ---- | 7 5 17 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
gfz | gfz 2968 | 12 7 26 | ---- ---- ---- | 6 4 14 |
grg | grg 2976 | 9 8 21 | ---- ---- ---- | 9 10 24 |
igr | igr 2975 | 5 6 14 | ---- ---- ---- | 6 5 12 |
igs | igs 2973 | 5 4 14 | ---- ---- ---- | 6 4 14 |
jpl | jpl 2967 | 9 10 21 | ---- ---- ---- | 11 9 23 |
mit | mit 2976 | 7 7 13 | ---- ---- ---- | 8 9 18 |
Table 5.1724.2 GPS week: 1724 Day: 2 MJD: 56314.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 3 3 9 | ---- ---- ---- | 6 6 16 |
emr | emr 2968 | 6 4 16 | ---- ---- ---- | 9 7 14 |
esa | esa 2976 | 4 4 12 | ---- ---- ---- | 7 6 15 |
gfz | gfz 2872 | 8 8 20 | ---- ---- ---- | 7 5 12 |
grg | grg 2975 | 9 8 20 | ---- ---- ---- | 9 6 20 |
igr | igr 2972 | 5 7 15 | ---- ---- ---- | 7 6 14 |
igs | igs 2971 | 6 5 14 | ---- ---- ---- | 7 5 12 |
jpl | jpl 2968 | 9 8 29 | ---- ---- ---- | 9 5 14 |
mit | mit 2976 | 8 9 18 | ---- ---- ---- | 23 33 91 |
Table 5.1724.3 GPS week: 1724 Day: 3 MJD: 56315.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2926 | 4 4 13 | 16 17 40 | 8 15 16 |
emr | emr 2872 | 8 6 23 | 17 16 48 | 15 17 28 |
esa | esa 2880 | 4 4 11 | 15 16 45 | 11 16 21 |
gfz | gfz 2870 | 7 7 20 | 16 17 43 | 10 17 20 |
grg | grg 2876 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igr | igr 2879 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igs | igs 2876 | 6 7 18 | 18 16 65 | 11 16 21 |
jpl | jpl 2872 | 10 14 24 | 17 16 41 | 13 19 23 |
mit | mit 2880 | 8 9 24 | 16 16 43 | 13 16 32 |
Table 5.1724.4 GPS week: 1724 Day: 4 MJD: 56316.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 | 4 8 16 | 8 10 27 | 7 5 10 |
emr | emr 2968 | 6 5 20 | 15 11 78 | 9 4 10 |
esa | esa 2880 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
gfz | gfz 2966 | 5 8 19 | ---- ---- ---- | ---- ---- ---- |
grg | grg 2970 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igr | igr 2976 | 3 4 17 | 8 10 29 | ---- ---- ---- |
igs | igs 2973 | 4 4 17 | 9 10 30 | 7 4 9 |
jpl | jpl 2871 | 9 7 25 | 18 13 82 | 7 5 13 |
mit | mit 2976 | 5 7 15 | 10 13 31 | 8 7 16 |
Table 5.1724.5 GPS week: 1724 Day: 5 MJD: 56317.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 2 3 7 | 15 18 44 | 6 4 12 |
emr | emr 2968 | 6 4 17 | 16 16 46 | 9 5 16 |
esa | esa 2976 | 3 3 13 | 14 17 42 | 6 5 13 |
gfz | gfz 2951 | 3 3 10 | 14 17 42 | 6 4 13 |
grg | grg 2954 | 7 7 15 | 16 14 36 | 7 7 16 |
igr | igr 2976 | 3 2 11 | 14 16 46 | 6 5 14 |
igs | igs 2969 | 4 4 16 | 15 17 43 | 7 4 12 |
jpl | jpl 2963 | 5 6 18 | 14 18 45 | 8 7 17 |
mit | mit 2976 | 3 4 10 | 14 15 43 | 7 6 15 |
Table 5.1724.6 GPS week: 1724 Day: 6 MJD: 56318.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3049 | 5 7 19 | 9 13 39 | 7 5 10 |
emr | emr 2968 | 9 8 20 | 11 14 35 | 10 7 12 |
esa | esa 2971 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
gfz | gfz 2967 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
grg | grg 2969 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igr | igr 2976 | 5 7 21 | 9 13 40 | 7 6 12 |
igs | igs 2974 | 6 6 19 | 9 13 39 | 7 5 10 |
jpl | jpl 2968 | 7 7 20 | 9 13 34 | 8 6 15 |
mit | mit 2976 | 6 5 19 | 9 14 33 | 8 7 14 |
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 6.1724 GPS week: 1724 MJD: 56312.500-56318.500
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 | -24 -14 14 -107 -7 | 4 15
| 16 34 55 123 6 | 3
emr uuuuu | 44 -22 299 179 7 | -8 21
| 27 27 99 142 12 | 1
esa uuuuu | -11 -21 59 -73 3 | 4 16
| 12 32 40 107 2 | 2
gfz uuuuu | 32 31 -71 -46 -5 | 6 15
| 7 13 38 33 3 | 2
grg uuuux | -9 -3 -1 -148 191 | 2 15
| 18 16 68 52 460 | 3
igr xxxxx | -59 8 -4 -47 1 | 0 16
| 13 16 27 36 4 | 2
irf xxxxx | -4 -10 -25 -10 5 | 2 13
| 8 15 23 25 12 | 2
jpl uuuuu | 40 11 19 107 19 | -8 25
| 29 28 110 74 8 | 4
mit uuuux | 7 -19 -99 82 13 | 5 23
| 27 12 40 70 26 | 5
ngs uuuuu | -61 67 -78 5 1 | -2 11
| 35 36 65 83 5 | 2
sio xxxxx | 190 -91 -34 7 -1 | 5 14
| 49 30 82 119 5 | 2
Table 7.1724.0 GPS week: 1724 Day: 0 MJD: 56312.500
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 -72 48 -85 -7 | 5 17
emr uuuuu | 49 -15 178 194 2 | -9 23
esa uuuuu | 2 30 46 -48 4 | 1 18
gfz uuuuu | 29 22 -31 12 -8 | 6 18
grg uuuux | -14 -4 70 -90 4 | 2 13
igr xxxxx | -56 -19 -12 -44 -2 | 0 19
irf xxxxx | -15 -24 9 7 25 | -2 12
jpl uuuuu | 67 -3 -140 133 22 | -14 30
mit uuuux | -52 -30 -79 39 62 | -3 14
ngs uuuuu | -23 12 -86 -40 1 | -2 14
sio xxxxx | 235 -62 94 141 5 | 4 16
Table 7.1724.1 GPS week: 1724 Day: 1 MJD: 56313.500
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 | -11 11 -47 -32 -3 | 5 17
emr uuuuu | 24 -17 285 85 -9 | -8 23
esa uuuuu | -17 -42 78 -60 6 | 2 18
gfz uuuuu | 36 41 -36 -32 -2 | 6 18
grg uuuux | -27 4 66 -111 -1 | 1 12
igr xxxxx | -66 4 19 -53 2 | 0 19
irf xxxxx | -6 4 -9 -18 3 | 1 15
jpl uuuuu | 37 35 -71 -23 14 | -11 29
mit uuuux | 9 -18 -58 52 3 | 2 24
ngs uuuuu | -36 73 -129 115 0 | -2 14
sio xxxxx | 249 -59 20 41 2 | 5 16
Table 7.1724.2 GPS week: 1724 Day: 2 MJD: 56314.500
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 -7 -12 -74 -7 | 7 17
emr uuuuu | 12 -19 330 1 5 | -8 23
esa uuuuu | -5 -52 98 -28 1 | 5 18
gfz uuuuu | 19 48 -72 -55 -6 | 8 18
grg uuuux | -28 20 -103 -163 1 | 1 12
igr xxxxx | -64 31 14 -34 0 | 2 18
irf xxxxx | -11 5 -18 6 9 | 2 14
jpl uuuuu | 14 -11 0 129 5 | -6 25
mit uuuux | 17 4 -80 75 18 | 3 24
ngs uuuuu | -29 72 -113 3 4 | 0 13
sio xxxxx | 207 -112 -67 -134 2 | 7 16
Table 7.1724.3 GPS week: 1724 Day: 3 MJD: 56315.500
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 | -1 -31 33 -140 -6 | 8 17
emr uuuuu | 34 -19 198 82 18 | -7 23
esa uuuuu | 2 -13 114 25 5 | 6 17
gfz uuuuu | 37 15 -101 -31 -2 | 8 18
grg uuuux | -16 10 -23 -205 7 | 0 12
igr xxxxx | -48 17 -4 -34 -2 | 3 18
irf xxxxx | 0 -11 -29 -45 -1 | 4 14
jpl uuuuu | -3 -3 -31 117 14 | -6 25
mit uuuux | 7 -25 -131 31 1 | 5 25
ngs uuuuu | -60 99 28 16 -7 | 1 12
sio xxxxx | 175 -143 -52 -79 -9 | 8 16
Table 7.1724.4 GPS week: 1724 Day: 4 MJD: 56316.500
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 | -16 -38 111 18 0 | 3 9
emr uuuuu | 31 -81 427 173 19 | -11 18
esa uuuuu | -25 13 52 -36 2 | 3 12
gfz uuuuu | 27 31 -124 -81 -6 | 3 9
grg uuuux | -1 -23 -42 -210 50 | 0 12
igr xxxxx | -37 11 -59 -110 -5 | -1 13
irf xxxxx | 10 -29 -53 -39 -7 | 2 13
jpl uuuuu | 37 -25 130 37 26 | -10 22
mit uuuux | 31 -20 -122 59 -10 | 6 25
ngs uuuuu | -68 88 -130 0 -4 | -3 9
sio xxxxx | 150 -77 -172 -82 -5 | 3 11
Table 7.1724.5 GPS week: 1724 Day: 5 MJD: 56317.500
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 | -44 12 6 -72 -19 | 3 10
emr uuuuu | 73 -16 252 301 19 | -9 19
esa uuuuu | -5 -43 4 -59 1 | 5 13
gfz uuuuu | 36 17 -96 -85 0 | 5 10
grg uuuux | 6 -21 28 -108 45 | 5 23
igr xxxxx | -63 0 3 11 4 | -1 13
irf xxxxx | -6 -19 -17 1 13 | 4 13
jpl uuuuu | 47 49 162 188 24 | -6 24
mit uuuux | 15 -34 -59 85 27 | 9 24
ngs uuuuu | -92 102 -118 -141 6 | -4 8
sio xxxxx | 204 -101 -47 -15 0 | 5 12
Table 7.1724.6 GPS week: 1724 Day: 6 MJD: 56318.500
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 | -40 25 -41 -364 -7 | 0 15
emr uuuuu | 88 9 421 414 -5 | -7 17
esa uuuuu | -26 -38 25 -308 -1 | 5 14
gfz uuuuu | 41 41 -36 -51 -10 | 3 11
grg uu--x | 20 -8 -- -- 1233 | 8 24
igr xxxxx | -77 10 13 -64 6 | -1 13
irf xxxxx | 3 5 -54 21 -9 | 6 11
jpl uuuuu | 82 36 83 167 24 | -2 19
mit uuuux | 23 -14 -163 234 -11 | 13 24
ngs uuuuu | -117 23 0 83 6 | -4 9
sio xxxxx | 110 -83 -14 180 -3 | 5 12
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