[IGSREPORT-21963] Wk 1746 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Jul 11 04:40:37 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1746 (Jun 23, 2013 - Jun 29, 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:
igs1746[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1746[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1746[0-6].cls IGS GPS clock combination summary report.
igs17467.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17467.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 | CONZ
0 | EMR | 26 26 HERS MCM4 HERS MCM4 MDO1 USNO
0 | ESA | 26 IRKJ IRKJ UNSA
0 | GFZ | MATE
0 | GRG | 6 26 6 26 IRKJ IRKT IRKJ IRKT MATE NRIL
0 | JPL | 4 8
0 | MIT | 26 26 DAV1 MATE MAW1 NTUS DAV1 HNPT MATE MAW1 MDVJ
0 | MIT | NTUS TWTF
1 | COD | 26 26 KOUC FAA1 KOUC
1 | ESA | 26 26 BRST KOUC MOBS BRST KOUC MOBS UNSA
1 | GFZ | 26 AUCK BOR1 ABMF AUCK BOR1 REUN
1 | GRG | FAA1 NOVM USNO FAA1 NOVM
1 | MIT | 3 13 16 3 13 16 MAW1 MAW1 MDVJ USNO
2 | COD | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
2 | COD | 21 22 23 24 25 26 28 29 31 32 1 2 3 4 5 6 7 8 9 10
2 | COD | 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 28
2 | COD | 29 31 32
2 | ESA | 26 IRKJ ABMF IRKJ UNSA
2 | GRG | 26 26 IRKJ KOUC IRKJ KOUC
2 | JPL | 3
2 | MIT | 3 21 26 3 21 26 MDVJ
3 | EMR | 3 3 HERS HERS
3 | ESA | UNSA
3 | GFZ | ABMF BRAZ ABMF BRAZ PIE1
3 | GRG | 26 26 IRKJ NYAL POLV IRKJ NYAL POLV
3 | JPL | 3 26
3 | MIT | 3 26 3 26 MDVJ USNO MDVJ USNO
4 | COD | FLRS KOUC FLRS KOUC TSKB
4 | EMR | 3
4 | ESA | IRKJ IRKJ UNSA
4 | GFZ | NRC1 NTUS
4 | GRG | 26 3 26 ABMF IRKJ KOUC LPGS REYK SPT0 ABMF HOFN IRKJ
4 | GRG | KOUC LPGS REYK SPT0
4 | JPL | 3 26
4 | MIT | 8 13 26 3 8 13 26 MDVJ NTUS TSKB MDVJ NTUS TSKB
5 | COD | 3 CONZ KOUC CONZ KOUC REYK
5 | EMR | YELL TLSE YAKT YELL
5 | ESA | 32 3 32 IRKJ KOUC MATE IRKJ KOUC MATE SCH2 UNSA
5 | GFZ | REYK REYK SCH2
5 | GRG | 26 26 32 HOFN IRKJ USNO HOFN IRKJ USNO
5 | JPL | 3 9 26 32
5 | MIT | 26 32 26 32 MAC1 NYA1 USNO NYA1 USNO
6 | COD | 3 FLRS HOFN KOUC WHIT FLRS HOFN KOUC WHIT
6 | EMR | HERS QAQ1 TLSE WHIT CHUR FAIR HERS QAQ1 TLSE WHIT
6 | ESA | 3 3 KOUC KOUC
6 | GFZ | SYOG SYOG
6 | GRG | 26 26 DUBO REYK TLSE DUBO REYK TLSE
6 | JPL | 3 6 WHIT
6 | MIT | 3 6 13 26 3 6 26 BOR1 MAC1 MDVJ QAQ1 SCH2 BOR1 MAC1
6 | MIT | MDVJ QAQ1 SCH2
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. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G27 | 4 | | | 4 | 4 | 4 | 4 |
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 -.7 -.5 -40 18 -15 .20
EMR | 0 | 4.8 -10.8 11.9 8 -3 -16 .25
ESA | 0 | 4.3 -9.0 .3 26 0 -54 .08
GFZ | 0 | .0 -.5 -1.0 -16 -24 -18 .03
GRG | 0 | -4.0 -8.3 26.0 -4 35 -17 .52
JPL | 0 | 3.4 -5.8 25.0 -18 11 -32 .47
MIT | 0 | 4.3 -6.3 20.5 -15 0 -47 .38
NGS | 0 | 3.8 -12.3 19.5 -125 -39 6 .28
SIO | 0 | 3.8 -7.6 12.2 -31 -37 145 .22
COD | 1 | .1 -.8 -.8 -32 35 -39 .27
EMR | 1 | .7 -2.5 6.8 -18 0 -34 .30
ESA | 1 | 2.6 -5.6 -7.1 33 65 -60 .09
GFZ | 1 | .0 -.7 -.9 -25 -21 -15 .17
GRG | 1 | 9.3 -5.3 23.4 -11 19 -62 .60
JPL | 1 | -7.1 1.3 9.0 -53 14 -3 .32
MIT | 1 | 5.7 -8.9 18.1 -40 -19 -53 .33
NGS | 1 | -2.1 -5.5 19.9 -107 -37 -9 .47
SIO | 1 | 4.6 -5.7 19.8 -18 -6 117 .12
COD | 2 | -.9 .0 -.7 -36 46 -29 .31
EMR | 2 | -4.6 2.3 8.5 -55 -16 -28 .31
ESA | 2 | 4.4 -6.8 1.3 44 7 -33 .20
GFZ | 2 | -.1 -.4 -1.0 -24 -22 -10 -.04
GRG | 2 | 3.1 -5.5 20.6 -1 46 3 .29
JPL | 2 | 3.7 -2.0 9.4 -53 0 8 .04
MIT | 2 | -.7 -9.2 18.5 -23 -16 -50 .28
NGS | 2 | 2.6 -3.3 27.2 -128 -69 24 .45
SIO | 2 | 1.5 -3.0 27.5 31 17 130 .05
COD | 3 | -.5 -.1 -1.0 -32 43 -45 .08
EMR | 3 | 8.2 -6.3 14.3 -39 -22 -34 .28
ESA | 3 | 6.0 -9.8 6.1 25 -23 -47 -.04
GFZ | 3 | .0 -.5 -.8 -14 -11 -5 -.37
GRG | 3 | 1.5 -7.1 17.2 -4 43 -100 .13
JPL | 3 | 8.7 -1.3 21.5 -63 1 -21 -.15
MIT | 3 | 4.2 -4.7 18.8 -35 -10 -46 -.01
NGS | 3 | 1.6 -10.9 23.7 -163 -56 -25 .32
SIO | 3 | 4.9 -6.8 19.0 -94 -44 -98 -.29
COD | 4 | -.6 .3 -.6 -43 40 -61 .10
EMR | 4 | 2.9 -3.5 4.6 -37 -24 -28 .25
ESA | 4 | 2.3 -6.7 7.7 42 -16 -34 -.04
GFZ | 4 | -.1 .1 .1 -18 -11 -13 -.60
GRG | 4 | 1.7 -10.1 17.9 -11 41 -35 .08
JPL | 4 | -1.0 -4.8 12.2 -44 46 -15 -.30
MIT | 4 | 7.1 -5.9 18.5 -30 -10 -48 .0
NGS | 4 | 3.1 -3.9 15.1 -107 -32 5 .19
SIO | 4 | 6.4 -5.9 -1.0 -103 -100 -132 -.12
COD | 5 | .1 -.2 -1.0 -42 29 -49 .16
EMR | 5 | 2.4 -7.8 10.4 -41 -27 -34 .33
ESA | 5 | .7 -10.6 8.2 75 -6 -52 .07
GFZ | 5 | -.4 -.1 -.4 -21 -12 -12 -.39
GRG | 5 | 6.0 -11.9 22.2 -5 18 -34 .38
JPL | 5 | 3.4 -.7 16.0 -49 30 -9 .06
MIT | 5 | 2.9 -7.7 21.1 -36 -9 -55 .22
NGS | 5 | .3 -9.2 18.5 -119 -28 -12 .46
SIO | 5 | 3.9 -5.5 14.5 -50 -47 -73 .12
COD | 6 | .0 .6 -.5 -34 36 -46 .03
EMR | 6 | 6.6 -2.8 13.6 -36 -34 -53 .40
ESA | 6 | 3.5 -7.2 12.4 74 -20 -23 -.03
GFZ | 6 | .0 .2 -.3 -17 -26 -14 -.55
GRG | 6 | 1.0 -7.4 15.5 -13 32 -5 .24
JPL | 6 | 2.5 -6.6 11.1 -72 6 -9 .04
MIT | 6 | 10.3 -4.8 20.0 -29 -7 -50 .33
NGS | 6 | 5.6 -3.1 20.3 -130 -47 15 .41
SIO | 6 | 6.5 -7.4 34.2 -71 9 -78 -.14
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 1.1746.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1746.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 2.1746.[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 3.1746.[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 5.1746.0-6). 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 1746 summary. (Jun 23, 2013 - Jun 29, 2013)
Table 1.1746.a GPS week: 1746 MJD: 56466.000-56472.000
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 268| 0 0 -8 13 15 3 -.50 12 11 | -1020 -100 245 304
| 0 0 1 18 28 7 .02 | 279 343
emr 79| 1 -2 0 -6 -39 13 .27 15 15 | 2434 506 17 106
| 1 2 1 20 18 9 .03 | 1617 985
esa 150| 1 0 0 6 2 -13 .00 5 5 | -78 -1287 14 114
| 0 0 1 14 30 8 .02 | 648 1260
gfz 199| -2 0 0 -30 -16 -9 -.58 10 9 | 90 55 13 70
| 1 0 2 36 62 7 .02 | 544 890
grg 138| 1 2 11 6 30 21 .56 14 13 | 26 -69 23 137
| 0 0 1 11 17 30 .03 | 247 288
igr n/a| 0 0 -1 -1 4 5 -.20 4 4 | -428 565 15 75
| 0 0 0 17 17 13 .01 | 1389 972
jpl 80| -1 1 -7 0 -47 -22 .26 14 13 | 1979 496 17 106
| 1 0 1 37 34 20 .02 | 1169 935
mit 237| 0 0 1 -13 -5 9 .10 12 11 | 62 -29 26 220
| 1 0 1 20 16 6 .02 | 248 308
ngs 237| -1 0 4 15 47 18 .27 12 9 | -1065 -67 1730 3584
| 1 0 2 25 59 25 .05 | 269 375
sio 426| -1 1 -11 -69 -34 5 -.50 19 19 | --- --- --- ---
| 1 1 2 56 31 116 .02 | --- ---
Table 1.1746.b GPS week : 1746 MJD: 56466.000-56472.000
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 3 4 4 4 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 5 5 5 6 5 5 5 |
4 | 3 3 3 4 3 3 4 |
5 | 4 4 4 5 5 5 5 |
6 | 4 4 4 4 5 5 5 |
7 | 4 4 4 4 4 4 5 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 4 4 4 3 |
10 | 3 3 3 4 3 4 3 |
11 | 4 3 3 4 4 4 4 |
12 | 6 6 5 5 5 5 6 |
13 | 3 3 4 4 4 4 4 |
14 | 3 3 4 4 4 4 4 |
15 | 5 5 5 5 5 6 7 |
16 | 5 5 5 5 5 5 5 |
17 | 4 5 4 5 5 5 5 |
18 | 4 4 4 4 4 4 5 |
19 | 5 4 4 4 4 4 4 |
20 | 3 3 4 4 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 4 4 4 3 4 |
23 | 4 4 4 4 5 4 4 |
24 | 4 5 4 4 4 4 5 |
25 | 4 3 4 4 4 5 4 |
26 | 6 6 6 6 6 7 7 |
27 | 0 0 0 8 7 6 6 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 6 6 6 6 |
30 | 0 0 0 0 0 0 0 |
31 | 4 4 4 4 4 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
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1746.0 GPS week: 1746 Day: 0 MJD: 56466.000
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 268| 0 1 -5 23 17 4 -.51 11 11 | -1235 344 16 77
emr 80| 3 -5 1 -13 -14 -3 .31 15 15 | 1185 -163 18 98
esa 150| 1 0 0 -3 32 5 .02 5 5 | 90 -1159 13 107
gfz 199| -1 0 -2 -29 -46 -3 -.57 8 7 | -15 259 12 65
grg 140| 1 2 12 27 24 26 .57 14 13 | 149 4 26 140
igr n/a| 0 0 -1 0 22 -2 -.19 4 4 | -1333 -377 15 58
jpl 80| -2 1 -6 10 -47 -42 .29 15 14 | 1258 -180 17 122
mit 238| 0 0 2 11 5 13 .07 11 10 | 185 -17 25 212
ngs 245| -1 0 1 -4 -7 -19 .34 12 9 | -1283 345 1892 3903
sio 430| -2 1 -8 -48 -36 137 -.50 18 18 | --- --- --- ---
Table 2.1746.1 GPS week: 1746 Day: 1 MJD: 56467.000
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 271| 0 0 -7 9 -6 12 -.51 10 10 | -1124 12 18 88
emr 80| 0 -1 1 -5 -46 5 .30 14 14 | 185 1069 19 121
esa 150| 1 0 0 33 38 -18 .01 5 5 | -545 -1154 13 126
gfz 201| 0 0 -2 -70 -3 -7 -.56 10 9 | -443 543 13 62
grg 140| 1 1 12 9 34 22 .56 14 13 | -66 -114 26 164
igr n/a| 0 0 -1 18 0 -6 -.20 4 4 | -2571 1344 14 78
jpl 80| 0 1 -5 25 -71 -3 .24 14 13 | 247 1094 16 87
mit 236| -1 -1 3 -31 -5 6 .11 10 10 | -27 -216 28 246
ngs 233| -2 0 4 -17 -11 28 .33 11 8 | -1072 -127 1681 3371
sio 426| -2 1 -8 -35 -6 124 -.49 19 19 | --- --- --- ---
Table 2.1746.2 GPS week: 1746 Day: 2 MJD: 56468.000
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 268| 1 0 -9 0 53 2 -.52 12 12 | -1278 185 1612 1642
emr 80| 0 0 -1 -46 -38 14 .23 14 14 | 958 1597 17 117
esa 150| 1 0 0 0 20 -16 -.02 5 5 | 312 -2112 16 119
gfz 197| -1 1 -1 -28 -54 -1 -.61 10 9 | -48 612 11 66
grg 139| 1 2 11 4 28 63 .55 14 12 | -220 207 22 124
igr n/a| 0 0 -2 -22 16 -7 -.18 4 4 | -1546 1620 15 74
jpl 80| -1 0 -6 15 -89 -54 .26 14 13 | 961 1612 16 100
mit 237| 0 -1 1 16 -17 0 .07 10 9 | -205 238 24 215
ngs 234| 0 0 6 20 57 36 .28 11 9 | -1439 508 1794 3392
sio 412| -1 0 -12 24 -6 120 -.49 18 19 | --- --- --- ---
Table 2.1746.3 GPS week: 1746 Day: 3 MJD: 56469.000
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 269| 0 1 -9 43 25 -3 -.49 11 11 | -655 -453 16 81
emr 80| 2 -2 0 9 -38 19 .29 15 15 | 4143 -1349 19 99
esa 150| 2 0 -1 -12 -15 -11 -.02 6 6 | 1152 -3452 15 117
gfz 200| -1 1 0 -37 -40 -2 -.59 10 10 | 1176 -1710 15 71
grg 139| 2 1 10 12 22 -36 .56 15 13 | 510 -671 22 134
igr n/a| 0 0 -3 4 13 16 -.20 4 4 | 879 -1099 15 72
jpl 80| -1 1 -7 48 -78 -32 .28 15 14 | 3465 -1223 18 121
mit 237| 0 0 1 -31 -10 4 .13 11 10 | 521 -528 23 196
ngs 236| -4 0 7 2 110 53 .28 11 9 | -681 -510 1922 3871
sio 428| -2 2 -12 -124 -66 -88 -.50 19 19 | --- --- --- ---
Table 2.1746.4 GPS week: 1746 Day: 4 MJD: 56470.000
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 271| 0 1 -9 17 -15 6 -.47 12 12 | -588 -631 19 77
emr 78| 3 0 1 17 -69 22 .28 14 14 | 3101 620 17 103
esa 150| 0 0 0 15 -49 -17 -.01 5 5 | -553 672 12 109
gfz 198| -3 0 0 -67 96 -14 -.61 10 10 | -351 1005 14 86
grg 138| 1 3 9 0 67 14 .54 14 13 | 64 -98 25 143
igr n/a| 0 0 -1 18 -25 1 -.20 5 5 | 18 888 15 84
jpl 80| 0 1 -5 -1 -34 -3 .25 13 12 | 2364 581 18 97
mit 240| 1 -1 1 -18 20 19 .10 14 13 | 148 -160 26 221
ngs 237| 0 0 3 17 47 -3 .25 11 9 | -756 -435 1483 3511
sio 429| 0 1 -12 -129 -79 -130 -.52 20 18 | --- --- --- ---
Table 2.1746.5 GPS week: 1746 Day: 5 MJD: 56471.000
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 268| 0 1 -11 -15 -13 10 -.50 12 12 | -1162 -15 20 78
emr 79| 1 -3 0 -8 -51 16 .27 15 15 | 3461 1144 17 114
esa 150| 1 -1 2 1 -5 -19 -.00 6 5 | -381 -884 15 106
gfz 201| -2 0 3 39 26 -13 -.57 11 10 | 361 -336 13 64
grg 137| 0 3 9 -4 25 21 .52 14 12 | -154 127 27 134
igr n/a| 0 0 -1 -21 -8 28 -.19 4 4 | 542 1007 15 70
jpl 80| 0 0 -9 -56 6 -12 .23 14 13 | 2691 956 16 111
mit 235| 1 0 1 -8 0 7 .10 15 13 | -18 69 25 208
ngs 236| 0 -1 0 30 0 4 .20 12 10 | -1126 -78 1602 3748
sio 428| -1 1 -13 -63 -44 -63 -.52 20 18 | --- --- --- ---
Table 2.1746.6 GPS week: 1746 Day: 6 MJD: 56472.000
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 0 -10 12 46 -9 -.47 13 11 | -1100 -142 19 91
emr 80| 1 -3 0 1 -20 16 .23 16 16 | 4010 628 17 90
esa 150| 1 -1 0 7 -2 -16 .03 5 5 | -622 -921 16 117
gfz 199| -3 0 2 -19 -94 -20 -.56 9 9 | -47 17 16 77
grg 138| 1 2 11 -7 13 38 .61 14 13 | -95 56 19 124
igr n/a| -1 0 -1 -11 16 8 -.22 5 5 | 1011 574 16 89
jpl 80| -1 2 -7 -41 -17 -9 .26 14 14 | 2868 634 21 104
mit 238| 3 0 0 -30 -31 11 .12 15 14 | -168 405 36 243
ngs 239| -1 0 4 58 138 27 .21 13 9 | -1103 -173 1739 3293
sio 429| 0 3 -14 -112 0 -61 -.48 20 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 3.1746.0 GPS week: 1746 Day: 0 MJD: 56466.000
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 7 4 8 11 3 15 12 10 12 3 | 28 34 29 32 44 28 41 28 33 18 30
2 | 8 12 6 10 9 5 12 10 5 36 3 | 23 27 26 33 28 25 26 29 28 29 25
3E | 14 15 7 10 13 5 13 20 20 19 5 | 80 83 79 80 80 77 82 73 83 73 78
4 | 10 7 4 8 10 4 12 6 8 20 3 | 36 37 37 37 41 35 40 39 42 33 37
5 | 11 16 7 10 11 6 16 10 12 24 4 | 42 45 39 40 38 39 44 38 41 41 39
6 | 10 12 4 8 11 5 12 9 13 23 3 | 116 119 118 118 123 117 121 118 110 122 118
7 | 8 13 6 7 19 4 17 7 10 17 3 | 37 39 35 34 51 36 41 39 40 34 36
8 | 10 9 3 5 14 3 10 11 7 16 3 | 16 22 19 17 24 17 25 20 22 17 17
9 | 8 10 5 6 13 3 11 6 8 25 3 | 20 22 21 16 22 19 25 20 24 27 19
10 | 10 7 3 9 13 4 10 7 7 25 3 | 20 29 25 28 36 25 28 31 32 30 27
11 | 8 12 4 7 15 2 11 15 11 17 3 | 49 59 50 53 65 52 56 59 59 52 54
12 | 16 27 6 16 21 5 22 8 11 12 5 | 19 33 16 23 30 14 26 19 24 17 17
13E | 6 11 3 6 12 5 11 9 8 8 3 | 23 24 23 22 31 23 28 29 26 24 23
14E | 9 12 4 5 10 3 17 6 11 11 3 | 14 19 15 13 18 13 21 14 18 15 13
15E | 12 24 5 9 12 4 23 10 9 12 4 | 16 27 20 20 29 18 28 24 24 22 19
16 | 15 20 6 11 15 7 16 11 14 17 4 | 17 28 20 16 27 16 25 21 25 14 18
17 | 8 15 5 8 20 3 17 6 10 14 4 | 14 23 14 15 34 15 25 21 28 16 17
18 | 9 18 6 11 13 4 16 13 11 22 4 | 19 32 26 22 35 23 29 28 26 19 23
19 | 8 15 5 8 16 3 13 17 15 14 4 | 13 24 16 11 30 14 22 17 25 11 15
20 | 9 12 4 8 10 3 12 9 8 21 3 | 24 28 25 29 30 27 29 27 30 20 25
21 | 11 13 6 7 12 3 16 16 11 24 4 | 26 35 31 26 41 28 34 36 34 25 31
22 | 14 15 6 5 14 4 14 11 10 16 4 | 32 35 33 32 43 33 33 36 36 27 33
23E | 7 12 4 8 14 5 14 10 7 13 3 | 18 21 17 13 24 16 23 21 23 21 16
24 | 11 13 5 6 13 4 15 7 9 12 3 | 20 31 27 21 33 22 30 22 26 17 23
25 | 8 18 5 7 15 5 15 9 8 11 3 | 9 28 18 13 27 14 24 17 19 16 16
26E | 22 19 6 8 20 6 17 13 31 12 6 | 32 35 31 31 36 30 36 35 45 35 30
X27 | 8 --- --- --- --- 19 --- --- --- --- 0 | 185 --- --- --- --- 186 --- --- --- --- 188
28 | 11 13 3 8 22 3 10 12 9 15 4 | 19 27 19 16 38 17 27 21 26 16 19
29 | 8 22 7 11 15 3 23 12 10 13 4 | 19 24 16 19 25 14 25 21 23 15 16
X30 | 8 --- --- --- --- 68 --- --- --- --- 0 | 51 --- --- --- --- 30 --- --- --- --- 51
31 | 10 14 6 7 16 4 14 9 10 15 3 | 18 24 18 17 33 17 22 22 23 16 18
32 | 7 10 5 6 10 3 9 12 12 11 3 | 16 23 19 17 28 18 24 25 28 10 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 5 8 14 4 15 11 12 18 |T 33 34 29 28 38 33 34 31 34 27 34
WRMS | 11 15 5 7 13 4 14 10 9 18 |NE 24 30 25 24 34 24 30 27 30 22 26
MEDI | 9 13 5 8 13 4 14 10 10 15 |MD 20 28 23 22 33 23 28 25 26 20 23
Table 3.1746.1 GPS week: 1746 Day: 1 MJD: 56467.000
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 7 4 8 9 4 15 9 12 12 3 | 22 28 23 18 32 21 35 20 31 17 22
2 | 11 11 5 13 9 4 11 8 8 35 3 | 24 26 23 29 27 21 27 22 25 28 22
3E | 14 13 5 11 14 5 16 11 21 17 4 | 61 67 62 62 66 61 64 66 67 64 63
4 | 9 7 4 6 9 3 7 6 9 20 2 | 26 29 28 26 30 26 29 27 29 25 26
5 | 14 15 7 9 11 4 15 8 11 22 4 | 32 37 30 30 33 29 38 30 33 33 30
6 | 10 17 5 10 13 5 13 8 9 22 3 | 127 128 126 126 128 126 129 122 125 126 125
7 | 8 12 5 7 16 6 12 10 11 18 3 | 44 44 44 42 52 42 46 46 47 42 43
8 | 10 7 4 8 11 5 9 14 8 17 3 | 20 23 20 17 20 19 26 23 21 20 18
9 | 8 10 5 8 13 3 9 10 9 25 3 | 21 24 22 16 22 19 25 22 23 26 19
10 | 8 7 3 9 14 4 6 10 7 26 3 | 19 26 21 17 28 21 26 23 27 26 21
11 | 7 12 4 7 14 2 11 9 11 14 3 | 36 46 38 35 47 38 47 43 45 40 39
12 | 10 25 6 17 23 5 19 10 10 16 5 | 20 33 22 25 28 18 33 21 28 17 19
13E | 7 13 3 7 12 4 9 10 10 14 3 | 24 26 23 21 25 20 25 27 24 21 22
14E | 8 10 4 5 13 3 9 8 8 15 2 | 15 20 16 13 22 13 22 17 21 17 15
15E | 6 23 5 10 11 6 24 19 12 23 5 | 15 25 16 16 24 15 30 24 21 22 15
16 | 15 20 7 13 15 6 14 11 10 19 4 | 22 28 21 17 30 19 27 20 28 17 20
17 | 9 17 6 8 19 4 22 10 9 20 4 | 15 24 18 13 37 15 27 20 26 15 17
18 | 8 13 5 13 13 4 16 11 7 22 3 | 18 28 19 20 30 18 28 21 22 15 18
19 | 8 16 4 9 16 3 13 11 12 11 4 | 11 28 16 11 31 13 24 17 25 11 16
20 | 8 11 3 11 11 3 12 6 9 22 3 | 18 23 20 23 23 21 25 22 27 17 20
21 | 10 13 5 6 11 4 15 12 10 25 3 | 22 33 26 20 34 23 32 26 32 18 25
22 | 10 14 5 6 14 3 15 12 7 16 3 | 29 35 29 29 38 29 35 30 31 26 29
23E | 7 12 4 10 20 4 13 13 6 14 3 | 13 19 14 11 23 12 21 19 19 16 13
24 | 12 13 4 21 16 4 11 8 15 8 4 | 21 29 23 22 33 21 32 24 31 21 22
25 | 7 14 5 7 16 3 11 7 7 14 3 | 22 28 22 19 27 19 29 20 23 16 20
26E | 17 18 8 9 13 6 17 14 28 14 5 | 35 33 29 31 27 31 36 30 48 34 29
X27 | 9 --- --- --- --- 18 --- --- --- --- 0 | 140 --- --- --- --- 138 --- --- --- --- 142
28 | 8 14 4 7 19 3 12 14 7 18 3 | 27 32 28 23 39 26 32 28 33 23 27
29 | 10 20 5 11 17 4 21 9 14 15 4 | 22 26 16 19 26 16 27 19 21 15 17
X30 | 9 --- --- --- --- 41 --- --- --- --- 0 | 33 --- --- --- --- 31 --- --- --- --- 36
31 | 10 13 5 6 17 4 14 7 11 14 3 | 17 25 16 15 34 15 24 21 24 14 17
32 | 7 9 3 9 10 2 7 7 8 13 2 | 18 21 17 15 26 16 24 22 24 9 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 10 14 4 14 10 11 19 |T 30 33 27 26 34 29 34 29 32 26 30
WRMS | 10 14 5 9 13 4 13 10 8 19 |NE 23 29 23 21 31 22 30 24 28 21 23
MEDI | 9 13 5 9 13 4 13 10 9 17 |MD 22 28 22 20 30 21 28 22 27 20 21
Table 3.1746.2 GPS week: 1746 Day: 2 MJD: 56468.000
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 7 3 12 11 5 13 9 13 13 3 | 20 26 24 28 32 22 33 23 30 17 23
2 | 10 12 6 12 8 3 10 10 8 33 3 | 20 26 24 24 28 22 26 26 26 32 23
3E | 15 17 5 9 14 7 15 11 20 17 4 | 29 41 32 32 43 33 38 34 41 36 33
4 | 9 8 3 7 9 3 9 8 7 19 2 | 22 28 27 31 27 26 30 32 27 29 26
5 | 12 14 4 11 10 5 14 8 8 19 3 | 31 35 29 28 35 28 36 29 33 30 29
6E | 13 17 5 8 15 7 16 6 9 23 4 | 83 84 80 85 74 79 80 81 79 74 80
7 | 10 14 4 7 16 2 13 7 9 16 3 | 37 35 32 31 37 31 35 35 34 37 32
8 | 9 8 5 8 11 3 9 10 8 15 3 | 18 20 18 17 20 18 23 24 19 22 17
9 | 9 9 4 8 14 4 9 12 7 23 3 | 18 22 19 19 20 20 23 26 19 27 18
10 | 10 7 4 10 12 4 7 11 6 24 3 | 18 26 23 25 29 22 23 28 29 28 24
11 | 8 12 3 8 14 5 11 9 8 12 3 | 36 47 41 42 50 41 49 44 47 40 42
12 | 15 21 6 14 22 5 18 10 13 12 5 | 20 28 15 19 28 14 26 19 23 15 15
13E | 9 14 5 9 11 4 10 12 11 20 3 | 24 26 20 20 24 19 21 23 21 26 19
14E | 15 9 4 7 11 3 13 7 12 14 3 | 20 18 17 16 16 15 20 18 25 15 15
15E | 12 19 5 11 12 4 22 15 10 16 4 | 15 24 17 18 23 15 26 22 27 19 17
16 | 19 21 5 13 15 6 17 9 12 18 5 | 18 27 17 13 24 15 26 19 27 18 16
17 | 12 15 5 6 17 4 19 8 9 18 4 | 18 23 16 12 33 14 24 21 27 17 17
18 | 13 13 6 12 11 4 14 9 10 22 4 | 18 27 21 21 29 21 28 24 26 15 21
19 | 8 17 4 9 13 4 13 11 11 11 3 | 11 27 17 12 30 17 24 18 27 12 17
20 | 11 12 4 10 12 6 12 6 10 22 3 | 19 24 18 20 23 19 26 23 27 16 19
21 | 12 13 6 7 12 4 14 12 10 26 3 | 24 36 30 28 41 30 36 35 39 23 32
22 | 12 13 5 8 12 4 13 11 11 17 3 | 30 36 33 28 41 30 37 32 36 24 32
23E | 6 10 5 12 17 4 11 13 12 14 4 | 13 21 18 14 21 15 20 19 26 16 16
24 | 16 12 4 6 14 3 12 10 10 8 3 | 28 24 21 24 27 20 28 22 22 25 21
25 | 15 14 5 7 15 5 12 8 9 12 3 | 20 26 17 12 27 16 25 18 24 14 17
26E | 17 18 7 10 15 4 16 12 26 14 5 | 32 29 25 29 27 25 28 28 39 34 26
X27 | 10 --- --- --- --- 26 --- --- --- --- 0 | 146 --- --- --- --- 153 --- --- --- --- 149
28 | 8 13 4 7 19 3 12 14 8 19 4 | 27 27 23 22 31 22 28 30 31 29 23
29 | 18 21 6 12 14 4 21 12 9 14 5 | 24 25 18 21 25 17 25 21 28 16 18
X30 | 10 --- --- --- --- 50 --- --- --- --- 0 | 55 --- --- --- --- 26 --- --- --- --- 55
31 | 12 13 6 10 19 4 14 7 12 15 4 | 19 24 18 19 33 17 22 21 28 17 18
32 | 13 9 5 7 10 4 7 9 8 12 3 | 16 19 18 14 23 16 20 21 25 9 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 5 10 14 4 14 10 11 18 |T 29 29 24 24 30 27 29 27 30 24 28
WRMS | 12 14 5 9 12 4 13 9 9 19 |NE 23 27 22 22 30 21 28 25 28 22 23
MEDI | 12 13 5 9 13 4 13 10 10 16 |MD 20 26 20 21 28 20 26 23 27 22 21
Table 3.1746.3 GPS week: 1746 Day: 3 MJD: 56469.000
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 7 6 10 9 4 16 11 10 15 3 | 30 34 27 29 40 28 40 30 38 22 29
2 | 9 15 7 14 10 4 12 12 10 34 4 | 23 30 24 31 26 23 32 34 34 32 25
3E | 15 14 7 9 17 6 17 13 24 15 5 | 59 67 62 62 63 61 68 62 71 61 62
4 | 8 10 5 11 9 3 11 12 11 22 3 | 26 29 25 31 32 25 29 31 36 26 27
5 | 20 14 6 10 8 5 16 16 9 22 4 | 41 44 39 38 38 39 45 40 44 42 38
6E | 12 13 7 10 19 4 13 9 10 25 4 | 141 135 135 142 134 137 135 136 135 134 136
7 | 9 12 5 9 15 5 17 6 8 17 3 | 46 45 44 43 53 44 46 46 48 43 44
8 | 8 10 5 8 13 3 10 9 9 14 3 | 19 22 18 16 24 17 22 20 23 16 17
9 | 10 12 6 8 12 3 11 16 9 24 4 | 19 24 19 15 23 17 23 22 25 26 17
10 | 7 10 5 11 11 4 11 11 9 24 3 | 21 28 22 28 30 23 27 30 36 26 25
11 | 8 12 5 7 13 3 12 9 9 14 3 | 45 55 47 52 62 50 55 50 57 45 50
12 | 14 22 8 13 17 4 19 12 10 14 5 | 19 30 19 21 30 14 27 21 26 17 17
13E | 8 10 6 11 15 3 11 10 10 13 3 | 28 28 26 23 28 25 30 30 34 27 26
14E | 10 10 5 5 15 5 17 9 9 14 3 | 15 17 14 12 18 12 20 15 28 14 12
15E | 14 19 6 10 10 4 25 14 9 13 5 | 17 24 14 15 21 11 27 20 26 18 14
16 | 12 24 6 13 15 4 15 10 12 21 5 | 25 34 21 19 30 20 29 23 29 17 21
17 | 10 18 5 8 16 3 22 11 10 16 4 | 14 25 16 16 32 14 30 24 29 18 17
18 | 8 14 7 15 12 4 13 8 7 22 4 | 18 29 21 23 30 19 27 25 27 17 20
19 | 7 14 7 7 16 3 13 10 12 13 4 | 14 21 15 12 28 13 22 19 28 12 15
20 | 10 12 7 16 11 4 13 7 11 24 4 | 24 29 27 34 31 27 30 28 37 21 27
21 | 10 16 6 8 12 3 15 11 11 25 4 | 24 34 28 26 37 27 32 35 39 22 29
22 | 7 12 7 6 13 4 13 12 8 19 3 | 33 37 35 35 43 33 33 38 40 30 34
23E | 7 12 6 16 18 2 13 10 10 13 4 | 18 21 19 15 23 16 23 21 24 21 16
24 | 14 12 5 8 14 5 16 9 8 11 4 | 32 32 27 25 37 23 37 28 30 28 28
25 | 10 16 6 8 19 3 15 10 7 11 4 | 15 29 17 18 29 15 27 20 25 18 17
26E | 17 20 10 11 20 5 16 13 26 16 6 | 36 35 33 33 33 31 36 36 47 40 33
X27 | 10 23 --- --- --- 13 --- 12 11 --- 8 | 224 149 --- --- --- 226 --- 152 154 --- 225
28 | 6 13 5 10 18 4 14 15 11 20 4 | 25 31 25 22 39 23 30 25 34 23 25
29 | 19 25 7 10 18 4 22 12 10 15 5 | 24 29 17 22 22 18 31 23 34 20 19
X30 | 9 --- --- --- --- 56 --- --- --- --- 0 | 51 --- --- --- --- 31 --- --- --- --- 51
31 | 10 16 6 9 18 4 12 6 13 17 4 | 20 24 19 21 33 18 25 21 27 17 19
32 | 8 9 5 10 10 3 9 7 9 14 3 | 15 23 19 21 24 17 25 21 31 10 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 10 15 4 15 11 11 19 |T 36 38 29 30 36 34 35 36 41 28 36
WRMS | 11 15 6 10 13 4 14 10 9 19 |NE 25 31 24 26 33 24 31 28 33 23 26
MEDI | 10 13 6 10 14 4 13 11 10 16 |MD 24 29 22 23 30 23 30 28 34 22 25
Table 3.1746.4 GPS week: 1746 Day: 4 MJD: 56470.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 8 5 7 10 3 15 14 8 19 3 | 28 31 27 22 35 26 35 24 27 19 25
2 | 8 15 6 10 13 7 12 18 7 35 4 | 27 30 24 24 25 23 26 30 30 30 23
3E | 15 12 6 11 16 7 14 17 23 16 5 | 48 51 47 47 51 46 50 50 58 47 47
4 | 5 7 5 5 10 5 10 12 9 22 3 | 31 29 27 27 31 26 29 30 31 25 27
5 | 15 17 6 10 10 5 15 18 8 23 4 | 35 41 35 31 36 33 40 35 35 37 34
6E | 16 14 6 12 16 6 15 10 11 23 4 | 74 70 76 72 69 74 74 72 70 71 72
7 | 12 13 5 9 15 5 12 10 10 17 3 | 29 27 19 19 36 19 27 22 30 15 21
8 | 10 10 5 9 12 5 7 12 8 11 3 | 20 21 14 12 19 14 21 20 19 16 14
9 | 7 10 5 9 11 5 11 14 6 22 3 | 23 25 20 14 22 20 24 24 26 27 18
10 | 8 11 6 9 11 5 8 11 5 24 3 | 24 33 27 22 31 26 30 31 30 25 26
11 | 10 11 5 8 14 3 10 11 11 14 3 | 39 51 45 41 54 45 50 42 47 36 44
12 | 9 20 6 15 21 6 15 15 10 15 5 | 25 32 21 20 29 18 28 24 25 18 19
13E | 12 10 4 10 15 4 11 12 9 26 3 | 24 23 18 16 27 19 24 22 23 28 18
14E | 13 12 4 7 13 4 9 11 11 14 3 | 16 22 15 11 20 14 22 18 18 14 14
15E | 19 21 5 13 9 4 22 18 10 13 5 | 17 26 19 21 23 17 28 25 25 24 17
16 | 13 22 6 15 16 5 14 16 12 22 5 | 22 31 20 14 27 17 25 18 25 17 18
17 | 9 16 4 8 17 5 21 14 13 15 4 | 19 30 18 17 35 22 28 26 30 16 20
18 | 7 12 6 11 9 6 10 12 9 23 3 | 18 27 22 19 26 16 26 23 26 15 20
19 | 7 12 6 9 13 3 11 14 12 16 3 | 13 24 15 13 27 15 24 18 23 13 15
20 | 13 12 4 12 11 5 12 12 12 27 4 | 25 28 24 27 26 25 28 25 26 17 24
21 | 10 13 4 7 10 5 12 14 8 24 3 | 25 34 27 25 35 26 35 33 34 23 28
22 | 10 11 6 7 10 4 11 11 10 20 3 | 25 30 29 24 33 24 29 28 29 18 26
23E | 9 16 5 13 15 3 13 20 10 20 4 | 26 30 21 18 30 22 29 32 28 27 22
24 | 10 13 5 8 16 6 12 15 8 12 4 | 18 24 20 13 30 16 24 21 26 18 17
25 | 9 14 4 7 15 5 13 17 8 13 3 | 15 27 18 13 26 15 27 21 22 15 17
26E | 19 18 9 12 17 5 18 18 24 18 6 | 35 41 36 37 41 36 41 41 50 39 37
X27 | 10 --- --- --- --- 12 --- 13 7 --- 7 | 233 --- --- --- --- 232 --- 146 143 --- 231
28 | 7 13 4 10 19 4 13 14 7 17 4 | 20 29 19 13 32 18 24 21 27 16 18
29 | 19 21 5 10 18 4 22 17 10 16 5 | 22 27 18 18 22 17 28 24 22 20 17
X30 | 9 --- --- --- --- 61 --- --- --- --- 0 | 42 --- --- --- --- 52 --- --- --- --- 41
31 | 13 16 7 10 17 6 10 11 10 19 4 | 24 29 23 24 36 21 27 23 28 19 22
32 | 13 9 5 7 10 3 7 12 11 18 3 | 20 25 21 17 25 19 26 22 23 10 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 5 10 14 5 13 14 11 20 |T 33 31 25 23 31 31 30 31 34 23 31
WRMS | 12 14 5 10 13 5 12 13 9 18 |NE 24 29 23 20 30 23 28 25 27 20 23
MEDI | 10 13 5 9 13 5 12 14 10 18 |MD 24 29 21 19 30 21 28 24 27 19 21
Table 3.1746.5 GPS week: 1746 Day: 5 MJD: 56471.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 9 5 7 9 6 15 12 10 15 3 | 19 24 21 19 29 17 30 20 20 17 18
2 | 9 13 6 10 8 3 12 18 9 34 4 | 15 24 21 21 21 16 22 27 21 29 18
3E | 11 16 7 10 14 5 15 17 21 19 5 | 56 63 58 57 64 56 64 60 66 60 59
4 | 10 9 5 8 8 4 10 11 11 21 3 | 16 20 19 22 20 16 18 23 21 21 17
5 | 20 14 6 14 11 4 16 20 14 27 5 | 38 36 33 29 36 31 38 32 32 37 32
6E | 15 19 8 14 13 4 14 12 17 31 5 | 131 124 126 132 121 128 124 127 125 124 126
7 | 11 12 6 8 15 5 12 12 10 16 4 | 40 40 37 36 46 37 39 41 41 39 37
8 | 10 8 4 8 11 3 7 12 11 13 3 | 20 21 19 15 20 19 21 23 27 20 18
9 | 10 10 6 10 10 3 9 14 14 24 3 | 18 21 19 11 20 17 21 23 26 27 17
10 | 13 8 6 10 10 4 8 13 10 25 3 | 12 22 20 20 22 17 19 26 24 27 18
11 | 8 14 4 7 13 6 13 14 8 12 3 | 27 41 33 32 44 31 38 34 29 30 32
12 | 12 20 6 14 22 6 15 16 12 19 5 | 18 30 21 22 28 20 25 26 26 24 19
13E | 9 10 4 10 15 5 11 11 11 11 3 | 25 26 27 25 25 27 28 28 27 31 25
14E | 12 13 6 8 10 4 11 9 9 16 3 | 13 20 16 13 18 13 18 17 19 16 13
15E | 12 23 6 15 15 4 20 27 10 24 5 | 23 30 26 27 25 24 31 31 29 30 23
16 | 16 18 5 14 15 5 13 16 8 21 4 | 21 24 20 17 24 16 21 24 20 20 17
17 | 14 15 5 8 19 4 23 11 11 15 5 | 17 23 17 11 35 14 28 22 22 14 15
18 | 7 13 6 12 11 4 12 13 10 23 3 | 14 25 19 20 22 18 25 23 21 16 17
19 | 8 12 7 10 12 4 14 17 7 16 4 | 9 22 16 11 27 13 22 21 20 16 14
20 | 13 12 4 11 11 4 13 10 9 27 3 | 19 22 19 21 20 17 21 18 21 15 17
21 | 10 14 5 9 7 3 13 14 9 25 3 | 23 31 27 23 31 26 30 30 30 23 26
22 | 7 14 4 6 10 4 12 10 8 19 3 | 27 33 31 25 31 28 32 29 32 20 28
23E | 12 15 5 12 12 4 12 16 9 15 4 | 19 23 22 18 20 19 22 24 21 26 18
24 | 13 14 5 8 17 4 12 13 13 12 4 | 26 29 26 23 33 25 29 28 31 26 25
25 | 14 16 6 7 17 4 13 14 14 13 4 | 16 27 20 17 27 18 26 21 25 18 18
26E | 19 19 10 14 21 8 18 16 29 17 7 | 41 48 38 40 44 36 44 43 52 40 39
X27E | 12 14 8 --- --- 14 --- 13 9 --- 5 | 249 177 97 --- --- 252 --- 169 162 --- 249
28 | 7 12 5 8 19 2 11 12 10 18 3 | 20 27 22 16 33 20 25 25 26 24 20
29 | 18 25 8 13 14 4 26 16 11 16 6 | 18 26 16 20 22 15 28 24 25 23 16
X30 | 10 --- --- --- --- 76 --- --- --- --- 0 | 64 --- --- --- --- 56 --- --- --- --- 66
31 | 10 16 5 11 18 5 11 11 10 19 4 | 17 27 21 22 35 21 24 24 26 22 20
32 | 9 10 6 9 11 3 6 14 7 17 3 | 13 20 21 14 20 15 18 21 21 13 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 6 11 14 4 14 14 12 20 |T 33 36 29 25 32 33 31 34 35 28 34
WRMS | 12 15 5 10 12 4 13 13 10 18 |NE 21 26 22 20 28 21 26 25 25 22 22
MEDI | 11 14 6 10 12 4 12 13 10 18 |MD 19 26 21 21 27 19 25 25 26 23 18
Table 3.1746.6 GPS week: 1746 Day: 6 MJD: 56472.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 11 4 6 8 6 17 13 10 16 3 | 28 35 31 30 39 29 35 27 39 20 30
2 | 11 13 7 11 13 4 14 18 8 33 4 | 27 30 28 30 28 26 27 36 38 33 27
3E | 13 16 6 8 13 7 13 16 19 21 4 | 65 72 70 68 75 69 70 68 83 69 70
4 | 18 11 5 6 10 8 10 10 8 21 3 | 32 30 31 32 37 28 28 35 35 25 30
5 | 17 17 5 9 12 3 15 14 12 27 4 | 50 52 47 44 50 45 53 44 47 50 46
6E | 14 17 6 10 14 7 17 14 19 30 5 | 105 101 99 103 96 101 100 100 103 99 100
7 | 11 13 6 7 18 4 15 18 12 17 4 | 32 34 32 33 36 29 34 32 31 35 30
8 | 9 9 3 6 13 4 8 18 9 18 3 | 21 17 16 15 22 15 19 26 28 23 16
9 | 8 10 4 5 11 3 9 11 7 24 3 | 25 22 21 16 25 19 25 25 30 27 20
10 | 9 11 6 6 7 4 7 12 8 25 3 | 22 35 28 30 34 27 28 37 37 34 29
11 | 7 11 4 8 11 5 10 13 10 13 3 | 51 64 58 56 68 56 57 57 64 50 57
12 | 14 22 6 12 25 6 15 18 13 15 5 | 22 33 21 20 38 19 26 18 34 18 20
13E | 12 12 5 7 10 3 11 15 9 13 3 | 21 23 16 16 24 16 23 20 30 17 17
14E | 9 12 5 8 13 4 12 11 9 15 3 | 17 21 20 15 19 15 19 16 27 17 16
15 | 16 36 5 12 19 3 20 22 17 14 6 | 26 38 23 25 31 22 28 27 35 21 22
16 | 18 20 5 13 13 7 16 14 12 23 5 | 26 30 19 14 26 17 25 18 31 18 18
17 | 14 18 5 5 13 4 21 13 11 15 4 | 23 28 20 16 32 17 26 23 30 14 19
18 | 7 14 6 14 14 4 16 15 13 22 4 | 15 27 24 24 28 20 23 28 32 18 21
19 | 6 10 5 9 11 5 14 16 8 18 3 | 12 23 20 20 29 17 23 20 29 15 18
20 | 11 12 4 12 11 5 13 8 9 26 3 | 23 29 27 31 31 28 27 25 35 20 26
21 | 7 14 5 8 10 4 15 15 14 24 4 | 33 38 34 34 43 34 37 41 44 30 35
22 | 8 14 4 8 13 3 14 11 16 20 4 | 27 36 32 30 41 29 29 33 41 23 31
23E | 8 12 6 12 16 4 12 18 8 16 4 | 25 26 24 18 29 23 30 28 33 26 23
24 | 12 17 6 8 13 5 10 20 14 12 4 | 20 33 29 31 31 28 32 36 28 34 27
25 | 11 15 5 8 20 4 13 17 9 12 4 | 17 26 20 15 32 16 24 18 27 15 17
26E | 26 20 5 12 24 8 18 16 31 17 7 | 104 98 104 105 96 99 99 99 105 109 101
X27E | 15 14 7 --- --- 13 --- 16 9 --- 5 | 333 128 105 --- --- 334 --- 139 137 --- 334
28 | 8 13 5 10 16 5 13 17 9 18 4 | 17 25 16 15 28 16 23 18 29 16 16
29 | 20 28 6 11 14 4 27 22 10 21 6 | 31 31 22 25 26 21 30 27 33 24 22
X30 | 9 --- --- --- --- 118 --- --- --- --- 0 | 71 --- --- --- --- 40 --- --- --- --- 71
31 | 14 14 6 8 17 4 13 12 12 22 4 | 27 28 25 27 38 26 28 28 29 33 25
32 | 6 9 5 7 12 3 8 11 6 16 3 | 17 24 22 18 27 18 22 24 30 14 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 16 5 9 14 5 14 15 13 20 |T 42 39 34 31 38 40 35 37 43 31 42
WRMS | 11 16 5 9 13 5 14 14 9 19 |NE 27 31 27 26 34 25 29 29 34 25 27
MEDI | 11 14 5 8 13 4 13 15 10 18 |MD 26 30 25 25 31 26 28 28 33 23 25
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 4.1746 GPS week: 1746 MJD: 56466.0-56472.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 |U 5 6 13 |U 6 7 21 |U 23 20 97 |
emr | emr 2911 | 9 6 19 |U 9 10 26 | 23 22 83 |
esa | esa 2907 | 6 6 16 |U 6 7 23 | 15 19 78 |
gfz | gfz 2869 |U 6 5 15 |U 6 7 21 |U 24 17 89 |
grg | grg 2880 |U 11 13 35 |U 12 23 43 | 24 19 93 |
igr | igr 2925 | 6 6 16 | 6 7 21 | 21 21 89 |
igs | igs 2925 | 6 5 15 | 6 9 22 | 21 19 87 |
jpl | jpl 2869 | 8 7 19 |U 8 20 33 | 26 13 100 |
mit | mit 2934 | 6 6 15 |U 7 21 32 |U 28 15 126 |
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 5.1746.0 GPS week: 1746 Day: 0 MJD: 56466.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3061 | 5 6 12 | 5 7 19 | ---- ---- ---- |
emr | emr 2872 | 8 6 18 | 8 14 25 | ---- ---- ---- |
esa | esa 2880 | 5 6 16 | 6 6 20 | ---- ---- ---- |
gfz | gfz 2872 | 5 5 15 | 6 6 19 | ---- ---- ---- |
grg | grg 2880 | 11 10 31 | 11 21 33 | ---- ---- ---- |
igr | igr 2880 | 5 7 16 | 6 6 20 | ---- ---- ---- |
igs | igs 2867 | 5 6 15 | 5 6 19 | ---- ---- ---- |
jpl | jpl 2872 | 6 6 15 | 9 26 39 | ---- ---- ---- |
mit | mit 2880 | 5 6 15 | 6 21 27 | ---- ---- ---- |
Table 5.1746.1 GPS week: 1746 Day: 1 MJD: 56467.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 5 4 8 | 5 7 16 | ---- ---- ---- |
emr | emr 2872 | 9 7 13 | 10 18 26 | ---- ---- ---- |
esa | esa 2880 | 7 4 9 | 6 6 19 | ---- ---- ---- |
gfz | gfz 2872 | 6 4 10 | 6 7 18 | ---- ---- ---- |
grg | grg 2880 | 11 22 41 | 17 19 60 | ---- ---- ---- |
igr | igr 2880 | 6 5 10 | 5 7 19 | ---- ---- ---- |
igs | igs 2877 | 6 4 9 | 7 19 24 | ---- ---- ---- |
jpl | jpl 2872 | 8 5 14 | 7 20 24 | ---- ---- ---- |
mit | mit 2880 | 8 6 11 | 7 17 24 | ---- ---- ---- |
Table 5.1746.2 GPS week: 1746 Day: 2 MJD: 56468.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 5 7 17 | 6 8 25 | ---- ---- ---- |
emr | emr 2871 | 10 7 21 | 10 6 29 | ---- ---- ---- |
esa | esa 2880 | 6 6 19 | 7 7 36 | ---- ---- ---- |
gfz | gfz 2871 | 7 5 19 | 6 7 28 | ---- ---- ---- |
grg | grg 2880 | 11 13 31 | 10 22 46 | ---- ---- ---- |
igr | igr 2879 | 6 6 19 | 6 7 32 | ---- ---- ---- |
igs | igs 2850 | 7 6 18 | 7 9 33 | ---- ---- ---- |
jpl | jpl 2871 | 8 6 19 | 9 22 44 | ---- ---- ---- |
mit | mit 2880 | 5 5 17 | 9 23 46 | ---- ---- ---- |
Table 5.1746.3 GPS week: 1746 Day: 3 MJD: 56469.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 4 4 12 | 6 7 25 | ---- ---- ---- |
emr | emr 2966 | 10 6 18 | 10 12 32 | ---- ---- ---- |
esa | esa 2880 | 6 4 17 | 7 9 25 | ---- ---- ---- |
gfz | gfz 2867 | 6 4 15 | 7 10 26 | ---- ---- ---- |
grg | grg 2880 | 11 8 44 | 11 25 43 | ---- ---- ---- |
igr | igr 2973 | 6 4 17 | 7 9 25 | ---- ---- ---- |
igs | igs 2966 | 6 4 15 | 6 9 24 | ---- ---- ---- |
jpl | jpl 2870 | 8 6 18 | 10 25 38 | ---- ---- ---- |
mit | mit 2976 | 6 3 14 | 7 22 34 | ---- ---- ---- |
Table 5.1746.4 GPS week: 1746 Day: 4 MJD: 56470.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 5 6 13 | 6 5 17 | 53 45 253 |
emr | emr 2868 | 9 7 18 | 6 8 23 | 54 53 213 |
esa | esa 2880 | 6 7 13 | 6 6 16 | 31 43 194 |
gfz | gfz 2868 | 6 6 13 | 7 7 15 | 56 37 227 |
grg | grg 2880 | 12 14 36 | 9 19 35 | 44 27 220 |
igr | igr 2957 | 6 7 15 | 6 7 16 | 48 46 228 |
igs | igs 2974 | 6 6 14 | 6 6 16 | 49 42 225 |
jpl | jpl 2868 | 8 8 20 | 6 21 32 | 58 21 249 |
mit | mit 2976 | 5 7 14 | 6 23 30 | 63 25 319 |
Table 5.1746.5 GPS week: 1746 Day: 5 MJD: 56471.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 4 5 15 | 7 7 18 | 8 6 15 |
emr | emr 2964 | 8 5 22 | 9 8 18 | 7 7 20 |
esa | esa 2976 | 5 6 20 | 6 6 18 | 8 7 16 |
gfz | gfz 2868 | 5 6 18 | 7 7 19 | 8 7 16 |
grg | grg 2880 | 10 10 31 | 14 26 33 | 13 15 27 |
igr | igr 2948 | 5 5 21 | 6 6 16 | 7 7 15 |
igs | igs 2973 | 5 5 19 | 7 6 19 | 8 7 15 |
jpl | jpl 2868 | 11 11 22 | 8 23 33 | 10 10 25 |
mit | mit 2976 | 5 5 18 | 7 21 26 | 11 10 23 |
Table 5.1746.6 GPS week: 1746 Day: 6 MJD: 56472.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 6 8 16 | 5 6 24 | 8 9 22 |
emr | emr 2964 | 7 8 23 | 8 7 25 | 7 5 18 |
esa | esa 2976 | 5 9 18 | 6 7 25 | 8 8 24 |
gfz | gfz 2867 | 5 8 17 | 5 8 24 | 9 8 26 |
grg | grg 2880 | 14 15 29 | 12 28 55 | 14 15 33 |
igr | igr 2960 | 5 8 17 | 5 7 23 | 8 9 24 |
igs | igs 2972 | 5 8 17 | 6 6 23 | 7 8 22 |
jpl | jpl 2868 | 7 8 22 | 6 6 21 | 10 9 26 |
mit | mit 2976 | 6 10 16 | 7 24 40 | 10 11 36 |
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 6.1746 GPS week: 1746 MJD: 56466.500-56472.500
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 | -37 10 -111 104 2 | 4 20
| 17 21 79 105 4 | 4
emr uuuuu | 85 1 -50 2 -4 | 36 41
| 13 20 42 68 5 | 5
esa uuuuu | -2 -13 41 42 1 | 8 20
| 18 13 37 35 3 | 3
gfz uuuuu | 10 31 16 -23 -1 | -5 20
| 14 14 83 45 3 | 2
grg uuuux | -4 -32 88 -192 -47 | 35 64
| 15 22 58 84 9 | 4
igr xxxxx | -7 18 64 7 4 | -5 21
| 13 9 54 45 2 | 4
irf xxxxx | 0 5 -25 -55 2 | -1 19
| 8 7 36 19 4 | 4
jpl uuuuu | 57 -6 16 59 -2 | 10 20
| 37 41 53 48 8 | 1
mit uuuuu | -7 22 -73 -82 3 | 17 26
| 20 20 121 41 4 | 3
ngs uuuuu | -64 -6 -3 -15 0 | 7 18
| 51 49 123 56 3 | 3
sio xxxxx | 20 67 149 154 -1 | 32 37
| 46 43 86 71 3 | 2
Table 7.1746.0 GPS week: 1746 Day: 0 MJD: 56466.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -28 -7 -180 91 3 | -3 16
emr uuuuu | 84 10 -61 63 6 | 30 34
esa uuuuu | -25 -9 8 9 -1 | 3 15
gfz uuuuu | -5 29 -137 44 -4 | -7 19
grg uuuux | 13 -50 178 -301 -44 | 29 67
igr xxxxx | -29 26 -23 -11 4 | -9 20
irf xxxxx | -8 -3 33 -62 3 | -5 17
jpl uuuuu | 68 -35 -12 85 0 | 9 18
mit uuuuu | -28 22 102 -101 0 | 14 22
ngs uuuuu | 11 16 177 30 -2 | 4 15
sio xxxxx | 5 65 287 64 -1 | 30 34
Table 7.1746.1 GPS week: 1746 Day: 1 MJD: 56467.500
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 | -43 17 -38 74 6 | -1 17
emr uuuuu | 85 11 -36 78 -7 | 32 37
esa uuuuu | -15 -32 29 -10 2 | 4 17
gfz uuuuu | 20 15 72 -1 1 | -7 19
grg uuuux | -2 -52 120 -234 -50 | 30 67
igr xxxxx | -16 17 77 -5 3 | -9 20
irf xxxxx | -2 -1 -14 -27 5 | -5 17
jpl uuuuu | 66 -20 -3 65 -9 | 9 19
mit uuuuu | -13 13 -36 -14 2 | 13 21
ngs uuuuu | -32 73 -123 -3 -1 | 4 15
sio xxxxx | -17 45 143 175 -4 | 30 34
Table 7.1746.2 GPS week: 1746 Day: 2 MJD: 56468.500
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 | -59 6 0 302 0 | 3 21
emr uuuuu | 75 34 -54 23 -4 | 36 41
esa uuuuu | -12 -20 21 59 2 | 7 20
gfz uuuuu | 30 55 -1 -8 4 | -6 20
grg uuuux | 4 -42 114 -225 -58 | 36 65
igr xxxxx | -4 29 33 21 8 | -6 22
irf xxxxx | -12 8 -30 -44 5 | -2 20
jpl uuuuu | 98 -34 -3 -33 -6 | 10 20
mit uuuuu | -27 24 -53 -99 5 | 16 25
ngs uuuuu | -57 -11 -28 -105 -1 | 7 19
sio xxxxx | -34 -4 138 200 -2 | 32 37
Table 7.1746.3 GPS week: 1746 Day: 3 MJD: 56469.500
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 | -12 -14 -116 184 -2 | 5 21
emr uuuuu | 75 1 -102 -87 -10 | 38 42
esa uuuuu | 13 8 52 53 -4 | 9 21
gfz uuuuu | -10 43 -32 -11 2 | -5 21
grg uuuux | 8 -34 103 -257 -51 | 41 63
igr xxxxx | -4 10 66 -5 6 | -4 22
irf xxxxx | 11 4 3 -77 7 | 0 20
jpl uuuuu | 106 -53 -46 113 -5 | 10 20
mit uuuuu | -14 -2 20 -61 12 | 17 26
ngs uuuuu | -121 13 62 -63 4 | 8 19
sio xxxxx | 38 81 228 218 3 | 33 38
Table 7.1746.4 GPS week: 1746 Day: 4 MJD: 56470.500
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 21 -147 33 7 | 5 21
emr uuuuu | 106 1 -87 -97 -5 | 38 42
esa uuuuu | 25 -15 41 89 -1 | 9 21
gfz uuuuu | 13 28 53 -89 -1 | -5 21
grg uuuux | -31 -31 8 -150 -52 | 40 63
igr xxxxx | -11 3 113 -68 4 | -3 21
irf xxxxx | -2 6 -48 -73 2 | 1 20
jpl uuuuu | 32 1 25 27 -8 | 10 20
mit uuuuu | -2 16 -131 -78 3 | 18 27
ngs uuuuu | -129 -2 90 52 2 | 8 20
sio xxxxx | 103 105 111 191 -4 | 33 38
Table 7.1746.5 GPS week: 1746 Day: 5 MJD: 56471.500
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 | -38 49 -224 -5 -1 | 6 21
emr uuuuu | 98 -27 25 21 -4 | 40 43
esa uuuuu | -5 -1 21 68 0 | 8 21
gfz uuuuu | 4 20 116 -71 -3 | -5 21
grg uuuux | -14 -28 36 -79 -42 | 35 63
igr xxxxx | 11 15 139 70 1 | -2 21
irf xxxxx | 5 3 -43 -39 -1 | 1 20
jpl uuuuu | 11 51 122 74 3 | 9 20
mit uuuuu | 6 21 -149 -73 1 | 19 27
ngs uuuuu | -36 -74 -19 -40 1 | 8 19
sio xxxxx | 42 49 117 191 0 | 33 37
Table 7.1746.6 GPS week: 1746 Day: 6 MJD: 56472.500
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 | -55 1 -73 47 -1 | 10 22
emr uuuuu | 71 -20 -32 11 -1 | 43 46
esa uuuuu | 7 -21 118 26 5 | 13 23
gfz uuuuu | 20 25 38 -28 -6 | -1 19
grg uuuux | -6 12 58 -98 -31 | 36 63
igr xxxxx | 3 24 40 49 1 | 2 20
irf xxxxx | 8 17 -77 -65 -4 | 5 20
jpl uuuuu | 20 47 27 84 13 | 12 22
mit uuuuu | 29 63 -267 -146 -1 | 23 30
ngs uuuuu | -85 -58 -178 20 -6 | 12 21
sio xxxxx | 5 127 20 41 -2 | 36 40
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