[IGSREPORT-21894] Wk 1742 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jun 14 07:58:39 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1742 (May 26, 2013 - Jun 01, 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:
igs1742[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1742[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1742[0-6].cls IGS GPS clock combination summary report.
igs17427.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17427.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 | KOUC
0 | EMR | FAIR
0 | ESA | KOUC UNSA
0 | GFZ | ABPO MAW1
0 | GRG | KOUC DAV1 KOUC MAW1 NRMD TRO1 URUM
0 | JPL | ABPO
0 | MIT | 19 31 16 19 31 DAV1 KOUC MAC1 DAV1 MAC1 MAW1
1 | COD | DAV1 JOZ2 DAV1 JOZ2 MOBS
1 | ESA | ONSA NTUS ONSA UNSA
1 | GFZ | 23
1 | GRG | ADIS LHAZ MAW1 NTUS
1 | JPL | 23
1 | MIT | 23 4 23 DAV1 MDVJ
2 | COD | KOUC REYK XMIS
2 | EMR | MCM4 MCM4
2 | ESA | WES2 KOUC UNSA WES2
2 | GRG | 6 6 DAV1 DAV1 IRKT
2 | MIT | 31 31 DAV1 MAC1 MDVJ REYK
3 | COD | ALRT KOUC WHIT ALRT KOUC
3 | ESA | KOUC WHIT KOUC UNSA WES2
3 | GFZ | IRKJ
3 | GRG | FAA1 FAA1 LHAZ WHIT
3 | MIT | MDVJ MDVJ
4 | COD | KOUC KOUC XMIS
4 | ESA | KOUC KOUC MATE UNSA
4 | GFZ | IRKJ LHAZ
4 | GRG | PDEL USN3 PDEL TRO1 USN3
4 | JPL | 21
4 | MIT | 3 8 16 3 8 16 MDVJ MDVJ
5 | COD | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
5 | COD | 21 22 23 24 25 26 28 29 31 32 1 2 3 4 5 6 7 8 9 10
5 | COD | 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 28
5 | COD | 29 31 32
5 | EMR | ONSA
5 | ESA | ONSA UNSA
5 | GFZ | IRKJ MATE
5 | GRG | 21 21 MATE LHAZ
5 | MIT | 3 5 18 3 5 IRKJ KOUC MDVJ IRKJ MDVJ NRC1
6 | COD | KOUC KOUC
6 | EMR | SCH2 WES2 MCM4 QAQ1 SCH2 WES2
6 | ESA | HOFN KOUC UNSA
6 | GFZ | 21 23 BRFT FAIR HOFN IRKJ NTUS
6 | GRG | REYK KARR KOUC NRMD REYK
6 | JPL | 23 SCH2 YELL
6 | MIT | 10 21 23 10 21 23 CAS1 DAV1 NTUS CAS1 DAV1 GLSV HOFN
6 | MIT | KOSG MDVJ NTUS
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 |
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 -1.1 -36 6 2 .21
EMR | 0 | 1.2 -2.1 10.6 -8 15 -28 .32
ESA | 0 | 3.2 -5.9 5.5 23 -2 -48 -.04
GFZ | 0 | -1.0 .2 -.2 -25 -13 -32 -.21
GRG | 0 | .0 -.6 24.2 -49 58 -30 .35
JPL | 0 | -2.8 -5.8 13.0 3 49 13 .47
MIT | 0 | .2 -1.8 13.8 -7 7 -50 .13
NGS | 0 | 5.1 -1.8 19.6 -123 -82 41 .40
SIO | 0 | .4 -5.4 -48.0 -147 -281 -237 .21
COD | 1 | .1 .8 -.2 -40 19 -48 .13
EMR | 1 | -2.6 -.2 13.1 10 16 -14 .26
ESA | 1 | -5.3 -2.5 8.6 15 14 -45 .13
GFZ | 1 | -1.1 .2 -1.0 -14 -11 -25 .20
GRG | 1 | 3.9 .5 29.1 -50 33 -54 .33
JPL | 1 | -10.1 -7.5 16.1 -31 16 37 .39
MIT | 1 | .5 2.0 17.8 -5 -5 -42 .05
NGS | 1 | -1.3 -2.2 11.3 -87 -33 -8 .73
SIO | 1 | -3.2 -3.6 -52.1 -126 -260 -186 .25
COD | 2 | -.3 -.7 -.7 -45 9 -25 .03
EMR | 2 | -.7 -5.8 6.4 6 7 -19 .11
ESA | 2 | -4.2 -.6 4.6 27 9 -50 .28
GFZ | 2 | -.8 -.1 -1.1 -13 -20 -25 -.26
GRG | 2 | .0 -2.2 29.4 -25 26 -16 .44
JPL | 2 | .0 -3.8 9.2 -90 8 -4 .34
MIT | 2 | .6 .4 15.5 -32 -18 -57 .0
NGS | 2 | .3 -.5 18.4 -116 -73 8 .44
SIO | 2 | -4.6 -4.6 -54.6 -126 -178 -134 .30
COD | 3 | -.3 .0 -.4 -41 7 -18 .19
EMR | 3 | 1.3 -4.3 1.2 -2 16 -27 .25
ESA | 3 | -.1 -3.1 2.4 36 4 -50 .21
GFZ | 3 | -1.1 -.3 -1.1 -16 -14 -23 .12
GRG | 3 | 5.7 .7 24.2 -12 57 -80 .19
JPL | 3 | 8.8 -1.6 4.2 -53 1 -2 .33
MIT | 3 | .9 .9 15.5 -29 -17 -33 .15
NGS | 3 | -1.3 -2.6 10.6 -88 -26 -6 .48
SIO | 3 | -3.5 -5.3 -62.3 -74 -191 -46 .33
COD | 4 | .5 .5 -.1 -37 -1 -21 -.0
EMR | 4 | 4.1 -4.2 11.1 1 18 -28 .11
ESA | 4 | .2 -5.6 5.8 36 16 -46 .01
GFZ | 4 | -.7 .3 -.8 -7 -11 -25 -.31
GRG | 4 | 6.6 -5.4 39.1 -16 39 -17 .03
JPL | 4 | 5.7 -5.5 9.3 -44 1 10 .53
MIT | 4 | 1.5 1.5 17.5 -7 -2 -36 .02
NGS | 4 | 4.3 -3.2 22.0 -130 -71 17 .37
SIO | 4 | -1.1 -2.0 -81.0 -62 -249 42 .10
COD | 5 | .5 1.2 -.7 -28 -17 -27 .22
EMR | 5 | 3.8 -3.9 6.7 14 16 0 .19
ESA | 5 | .2 .2 8.1 55 2 -40 .05
GFZ | 5 | -.4 .2 -.5 -10 -26 -27 -.24
GRG | 5 | 4.4 .2 33.8 -2 25 -10 .25
JPL | 5 | -2.3 -1.8 8.3 -13 -3 12 .50
MIT | 5 | 1.1 1.4 16.6 -35 -16 -43 .21
NGS | 5 | -4.4 -8.9 24.6 -182 -15 -55 .61
SIO | 5 | -1.2 -6.0 -85.9 -123 -317 161 .03
COD | 6 | .1 1.0 -.5 -36 -5 -35 .24
EMR | 6 | .5 -9.1 2.2 -3 17 -22 .46
ESA | 6 | 1.4 1.9 5.6 68 -9 -49 .20
GFZ | 6 | -.6 .2 -.6 -29 -22 -23 .08
GRG | 6 | 3.2 .9 30.0 -37 56 -43 .33
JPL | 6 | 2.5 -3.4 6.9 -34 -13 -44 .38
MIT | 6 | 4.7 -2.5 19.0 -4 -5 -39 .17
NGS | 6 | 3.8 -3.9 6.5 -62 -42 23 .57
SIO | 6 | -2.6 -3.8 -68.4 -113 -265 78 .19
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 1.1742.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1742.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 2.1742.[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 3.1742.[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 5.1742.0-6). 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 1742 summary. (May 26, 2013 - Jun 01, 2013)
Table 1.1742.a GPS week: 1742 MJD: 56438.000-56444.000
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 270| 0 0 -6 7 11 4 -.47 10 10 | -961 -156 449 507
| 0 0 1 12 27 17 .05 | 270 367
emr 80| 0 -1 -3 -7 -21 5 .35 13 13 | 2223 -762 15 95
| 0 1 1 18 16 12 .01 | 1057 1256
esa 150| 0 0 2 7 11 -12 .11 6 6 | -246 -874 14 109
| 0 0 0 14 17 11 .03 | 754 1186
gfz 197| -1 0 -1 -11 0 5 -.40 9 9 | 139 -349 17 108
| 0 0 0 17 67 4 .04 | 660 774
grg 139| 2 2 14 -3 35 -20 .53 16 14 | 65 -348 17 145
| 0 1 3 19 19 20 .08 | 305 597
igr n/a| 0 0 -2 14 32 -19 -.14 4 4 | 3028 -575 16 83
| 0 0 0 10 10 6 .04 | 921 1193
jpl 80| 1 1 -7 19 -29 4 .39 14 14 | 2545 -823 17 114
| 2 1 0 27 40 30 .02 | 1169 1202
mit 233| 0 0 2 5 -22 8 -.55 12 11 | 760 -456 23 207
| 1 0 1 19 15 13 .03 | 2008 691
ngs 240| 0 0 0 -23 18 3 .32 9 8 | -1016 -193 1791 3498
| 0 0 3 24 26 24 .06 | 284 437
sio 385| -2 1 -6 -131 -254 -58 -.37 21 21 | --- --- --- ---
| 1 0 1 26 39 154 .04 | --- ---
Table 1.1742.b GPS week : 1742 MJD: 56438.000-56444.000
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 3 |
3 | 3 4 3 4 3 3 3 |
4 | 3 3 4 4 4 4 3 |
5 | 4 4 4 4 4 5 4 |
6 | 3 4 3 4 4 3 3 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 4 3 4 3 3 |
9 | 3 3 4 4 4 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 3 4 4 4 4 3 4 |
12 | 5 5 5 6 5 5 6 |
13 | 4 4 4 4 4 4 5 |
14 | 4 4 4 4 4 4 3 |
15 | 5 5 5 6 5 5 5 |
16 | 4 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 5 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 3 3 4 3 4 4 4 |
22 | 4 4 4 3 4 4 4 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 4 5 4 |
26 | 4 4 4 5 5 5 5 |
27 | --- --- --- --- --- 0 0 |
28 | 4 4 4 3 3 3 3 |
29 | 5 5 5 5 5 5 4 |
30 | 0 0 0 0 0 0 0 |
31 | 4 4 4 4 5 5 5 |
32 | 3 3 4 3 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1742.0 GPS week: 1742 Day: 0 MJD: 56438.000
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 -5 8 27 27 -.45 10 10 | -622 -690 19 76
emr 80| 0 0 -1 17 -17 13 .37 13 13 | 2902 -1829 16 92
esa 150| 1 -1 1 16 33 -13 .11 6 6 | 488 -162 16 110
gfz 192| 0 0 0 -31 -46 9 -.42 8 8 | 1064 -1013 17 121
grg 139| 2 4 8 20 44 -28 .60 16 13 | 434 -1106 16 132
igr n/a| 0 0 -3 23 41 -19 -.10 4 4 | 3128 -1432 17 85
jpl 80| 1 0 -7 38 33 11 .41 15 14 | 3556 -1895 18 123
mit 237| 1 0 2 -8 -4 0 -.53 10 9 | 300 -883 24 192
ngs 236| 0 0 2 -48 -32 -13 .39 10 8 | -597 -826 1695 3793
sio 368| -1 1 -8 -164 -284 -254 -.34 21 18 | --- --- --- ---
Table 2.1742.1 GPS week: 1742 Day: 1 MJD: 56439.000
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 0 -4 16 9 9 -.41 11 10 | -962 -148 18 76
emr 80| 1 0 -1 -31 -29 0 .35 13 13 | 1913 456 18 86
esa 150| 0 0 1 -13 19 4 .15 6 6 | 703 -2150 15 114
gfz 197| -2 0 -1 5 -30 6 -.34 9 9 | 250 431 17 100
grg 138| 1 1 13 -11 20 -20 .55 16 14 | -350 214 18 174
igr n/a| 0 0 -2 21 21 -15 -.10 4 4 | 2556 736 17 84
jpl 80| 5 0 -7 11 -11 27 .38 14 14 | 2487 428 18 109
mit 237| 0 0 4 23 -28 -9 -.53 9 8 | -350 386 24 215
ngs 239| 0 0 -2 -13 40 -23 .35 10 9 | -825 -443 1796 3698
sio 371| -4 1 -5 -138 -288 -202 -.34 20 18 | --- --- --- ---
Table 2.1742.2 GPS week: 1742 Day: 2 MJD: 56440.000
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 275| 0 0 -7 0 32 26 -.50 10 10 | -1313 341 19 85
emr 80| 0 -1 -3 -12 3 -5 .36 13 13 | 2570 -256 13 91
esa 150| 1 0 2 19 19 -34 .13 6 6 | -495 -1178 18 103
gfz 192| 0 0 -2 -3 -37 -2 -.37 8 9 | 617 -961 17 114
grg 141| 2 3 14 -20 12 21 .59 17 15 | -122 146 17 141
igr n/a| 0 0 -1 16 43 -27 -.10 4 4 | 3526 -267 16 84
jpl 80| 0 0 -8 -25 6 41 .37 15 15 | 3197 -540 17 103
mit 239| 0 0 2 13 -38 14 -.51 10 9 | -13 74 23 165
ngs 239| 0 0 2 -19 5 -4 .37 9 8 | -1351 326 2032 3971
sio 389| -3 2 -5 -146 -196 -148 -.34 20 20 | --- --- --- ---
Table 2.1742.3 GPS week: 1742 Day: 3 MJD: 56441.000
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 274| 0 0 -5 23 -23 -1 -.50 10 9 | -887 -289 20 97
emr 80| 0 -3 -4 14 -21 22 .35 14 14 | 2084 486 16 99
esa 150| 1 0 3 6 -9 -10 .06 5 5 | 97 -1825 13 114
gfz 199| 0 0 -1 -35 68 1 -.39 9 9 | -59 -41 18 106
grg 141| 2 2 11 0 65 -47 .58 13 12 | 298 -620 17 149
igr n/a| 0 0 -2 23 32 -9 -.19 4 4 | 2959 533 16 85
jpl 80| 0 1 -7 3 -33 28 .38 13 13 | 2355 468 17 115
mit 238| 1 1 3 -13 -44 12 -.57 12 11 | 289 -721 24 233
ngs 242| 0 0 -2 -5 32 -7 .29 10 9 | -926 -296 1854 2886
sio 386| -4 1 -6 -108 -213 -65 -.40 21 24 | --- --- --- ---
Table 2.1742.4 GPS week: 1742 Day: 4 MJD: 56442.000
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 274| 0 0 -8 -13 -28 -3 -.53 9 9 | -1130 -18 18 93
emr 80| 0 -2 -4 -8 -46 18 .35 13 13 | 2991 -904 18 101
esa 150| 0 0 2 -4 -13 -10 .10 6 6 | -1051 -524 12 109
gfz 200| 0 0 -1 -5 112 8 -.47 11 11 | -352 -695 17 109
grg 141| 2 1 16 -31 50 -21 .54 15 13 | 216 -1125 22 153
igr n/a| 0 0 -3 -1 15 -19 -.17 4 4 | 3658 -584 16 74
jpl 80| 0 0 -6 55 -77 -5 .38 12 12 | 3085 -895 17 99
mit 234| 0 0 1 17 -11 -1 -.56 15 14 | 9 -333 24 202
ngs 239| 0 0 3 6 34 -1 .23 9 9 | -1236 54 1583 3335
sio 384| -3 2 -6 -93 -251 27 -.42 22 23 | --- --- --- ---
Table 2.1742.5 GPS week: 1742 Day: 5 MJD: 56443.000
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 272| 0 1 -7 14 21 -9 -.47 9 9 | -624 -495 3033 3043
emr 80| 0 -2 -6 -7 -31 -6 .33 13 13 | 3054 -2959 14 98
esa 150| 0 0 1 26 8 -9 .11 6 6 | -150 -1576 12 102
gfz 203| -2 0 -1 -13 13 5 -.40 9 9 | 403 -1037 18 117
grg 138| 3 3 18 20 17 -22 .44 16 14 | 245 -125 16 132
igr n/a| 0 0 -3 15 37 -26 -.18 3 3 | 4097 -2739 16 81
jpl 80| 1 1 -7 43 -56 -36 .36 14 14 | 3072 -2847 19 129
mit 220| 0 0 0 -22 -19 30 -.58 15 14 | 5284 -1661 23 234
ngs 244| -1 0 5 -63 9 29 .29 8 8 | -871 -484 1633 3307
sio 395| -3 1 -9 -155 -300 179 -.44 23 23 | --- --- --- ---
Table 2.1742.6 GPS week: 1742 Day: 6 MJD: 56444.000
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 -5 2 41 -18 -.40 10 9 | -1192 202 20 80
emr 80| 0 -3 -4 -25 -9 -5 .33 14 14 | 47 -330 15 99
esa 150| 0 0 3 1 21 -9 .12 5 5 | -1314 1295 13 111
gfz 201| -1 0 0 6 -75 6 -.41 8 8 | -945 870 18 89
grg 139| 3 0 19 -2 36 -28 .38 17 16 | -264 179 16 136
igr n/a| 0 0 -1 2 37 -18 -.14 4 4 | 1277 -277 16 88
jpl 80| 0 4 -6 9 -64 -32 .41 14 14 | 66 -483 19 120
mit 231| 3 0 3 26 -8 14 -.59 14 13 | -198 -56 22 210
ngs 243| 0 -1 -4 -17 40 46 .30 10 9 | -1306 316 1948 3501
sio 407| 0 1 -3 -114 -244 50 -.35 22 20 | --- --- --- ---
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 3.1742.0 GPS week: 1742 Day: 0 MJD: 56438.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 8 5 13 10 4 17 6 11 24 4 | 44 56 53 52 62 49 60 52 52 36 51
2 | 9 10 6 7 12 4 12 15 7 31 3 | 25 26 29 30 35 26 26 32 31 24 28
3 | 7 8 5 6 11 3 10 14 9 22 3 | 26 27 27 27 27 26 28 26 33 30 25
4 | 9 8 5 8 13 3 9 9 7 30 3 | 35 33 36 39 44 34 31 41 37 34 36
5 | 10 16 6 11 15 3 16 11 7 17 4 | 18 28 19 26 31 17 25 21 23 18 20
6 | 9 9 4 9 9 4 12 11 8 22 3 | 15 19 13 17 20 13 19 16 21 21 13
7 | 7 11 6 8 22 4 11 12 11 34 4 | 28 30 27 26 39 26 28 27 33 34 26
8 | 10 9 5 6 19 3 9 12 10 16 3 | 16 20 19 20 25 18 22 21 21 16 17
9 | 9 10 6 6 14 3 11 9 7 22 3 | 25 28 27 28 26 25 29 22 30 27 25
10 | 10 8 4 7 13 4 10 8 12 20 3 | 18 23 21 20 28 18 22 21 27 24 20
11 | 7 10 5 8 10 4 11 7 8 16 3 | 31 39 32 32 47 31 36 35 32 27 33
12E | 12 17 6 13 20 6 22 15 9 19 5 | 31 31 26 32 29 27 30 20 31 21 26
13 | 11 12 7 9 24 2 11 7 10 14 4 | 26 31 28 25 43 24 30 25 26 26 26
14 | 9 15 5 5 16 5 13 8 12 19 3 | 24 29 22 19 34 21 24 18 29 23 22
15E | 12 21 7 12 13 5 21 9 12 13 5 | 20 31 24 24 30 17 27 20 25 22 21
16E | 9 14 5 8 20 4 16 12 8 14 4 | 17 22 22 27 24 20 23 23 28 21 21
17 | 12 15 8 9 17 5 16 9 7 26 4 | 21 26 22 24 32 21 25 18 26 19 20
18 | 9 13 5 5 16 3 20 10 8 20 3 | 23 28 25 22 36 23 28 27 31 24 23
19 | 7 16 7 9 14 4 18 16 9 25 4 | 13 25 14 15 31 13 26 20 25 24 16
20 | 12 11 6 9 15 5 13 10 10 13 3 | 23 28 23 25 36 21 25 24 27 18 23
21 | 9 11 5 6 11 3 15 9 7 36 3 | 23 31 26 25 34 25 30 29 27 36 25
22 | 8 12 6 6 13 3 16 8 9 17 3 | 22 29 27 24 40 26 28 28 33 26 25
23 | 10 13 6 9 25 3 12 8 13 18 4 | 30 33 28 25 36 26 31 31 29 36 27
24 | 12 12 5 9 14 4 15 5 13 12 4 | 24 26 22 20 30 21 29 20 23 22 20
25E | 11 12 6 6 14 5 15 9 10 14 3 | 23 27 24 23 28 20 28 19 26 16 22
26 | 11 12 7 5 13 4 12 8 10 23 3 | 18 27 24 25 24 19 23 24 27 27 22
28E | 8 10 7 6 29 3 9 7 9 11 4 | 22 22 24 22 23 21 23 19 24 19 20
29 | 14 18 7 10 11 3 24 8 13 19 4 | 27 41 30 31 33 29 44 28 35 34 31
X30E | 8 --- --- --- --- 48 --- --- --- --- 0 | 44 --- --- --- --- 40 --- --- --- --- 43
31 | 11 13 5 7 19 6 19 9 7 22 4 | 21 29 24 27 39 22 31 22 29 23 24
32 | 8 10 5 10 8 5 9 9 9 17 3 | 20 26 18 20 27 18 26 18 23 20 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 6 8 16 4 15 10 10 21 |T 24 29 25 25 33 23 28 24 28 24 24
WRMS | 10 13 6 8 13 4 14 9 8 18 |NE 23 29 25 26 34 23 29 26 29 25 24
MEDI | 9 12 6 8 14 4 13 9 9 19 |MD 23 28 24 25 31 22 28 22 27 24 23
Table 3.1742.1 GPS week: 1742 Day: 1 MJD: 56439.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 4 10 11 3 16 5 18 20 3 | 30 35 31 31 42 30 43 33 31 24 31
2 | 11 9 5 8 15 4 11 9 8 29 3 | 19 22 21 23 26 20 24 25 19 23 21
3 | 9 11 6 6 11 4 12 7 13 21 3 | 32 35 34 33 34 34 35 36 35 36 33
4 | 9 8 5 9 16 3 8 6 8 27 3 | 28 26 24 30 31 24 26 35 21 33 26
5 | 9 15 6 9 18 2 13 8 8 16 4 | 18 25 19 23 30 17 25 21 21 23 18
6 | 9 13 6 8 9 4 12 8 10 19 3 | 18 20 17 18 20 17 19 19 23 21 15
7 | 10 12 4 8 22 5 15 10 9 34 4 | 27 28 25 24 34 22 25 26 29 34 23
8 | 9 9 4 6 15 4 12 13 8 17 3 | 23 26 22 24 21 21 24 30 25 27 22
9 | 9 10 6 9 11 3 12 8 8 21 3 | 20 23 22 19 21 19 26 22 20 26 19
10 | 10 9 4 10 15 4 9 7 9 17 3 | 21 25 17 23 22 17 25 24 18 26 18
11 | 7 10 6 10 12 4 9 9 13 15 3 | 20 28 20 19 33 20 29 25 25 22 21
12E | 15 19 6 11 28 5 24 8 10 14 5 | 19 27 20 22 26 19 27 20 22 18 18
13 | 11 13 4 7 24 2 10 9 7 15 3 | 22 27 19 16 36 17 26 17 22 20 18
14 | 10 13 5 10 14 4 13 6 8 15 3 | 18 21 18 18 27 16 18 16 20 19 16
15E | 14 24 8 12 20 4 19 7 13 13 5 | 22 29 20 21 22 14 22 19 19 21 16
16E | 12 15 6 12 17 4 17 14 9 11 4 | 14 21 19 21 21 14 19 19 24 20 17
17 | 9 15 5 11 16 4 15 7 8 26 3 | 20 26 17 20 30 16 25 18 22 22 17
18 | 8 14 5 7 16 4 17 8 9 20 3 | 17 26 19 18 30 18 24 20 24 20 18
19 | 7 16 6 9 15 6 16 10 11 23 4 | 14 25 15 14 28 14 24 18 24 22 15
20 | 10 12 7 11 15 4 12 10 8 13 3 | 16 21 17 16 28 15 21 17 20 15 15
21 | 8 10 7 5 12 3 12 7 11 34 3 | 19 24 23 18 25 19 24 18 22 30 19
22 | 6 12 6 7 15 4 15 7 9 16 3 | 22 26 22 20 30 22 26 25 25 24 21
23E | 11 15 7 10 17 4 11 13 8 15 4 | 24 27 24 22 24 20 25 21 24 22 20
24 | 11 13 6 10 15 2 12 6 9 11 3 | 17 23 20 14 26 16 25 16 19 16 16
25E | 14 14 6 9 20 5 17 8 10 13 4 | 13 23 18 16 25 15 28 18 22 15 16
26 | 12 12 9 9 12 4 14 9 10 20 4 | 19 26 20 22 20 18 23 22 19 27 18
28E | 7 12 6 9 25 4 13 8 10 20 4 | 23 21 22 24 20 18 21 21 25 29 19
29 | 18 18 7 9 12 5 22 8 9 19 4 | 17 28 19 24 26 19 31 19 23 23 19
X30E | 7 --- --- --- --- 55 --- --- --- --- 0 | 30 --- --- --- --- 48 --- --- --- --- 28
31 | 14 15 7 8 18 3 13 7 11 20 4 | 19 24 20 19 34 16 23 16 21 17 17
32 | 9 10 5 9 10 2 9 9 7 15 3 | 15 20 17 15 20 14 24 16 21 16 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 6 9 16 4 14 9 10 20 |T 20 25 20 20 27 19 25 21 22 23 19
WRMS | 10 13 6 9 14 4 14 8 9 18 |NE 20 25 20 20 28 19 26 22 23 23 19
MEDI | 9 12 6 9 15 4 13 8 9 17 |MD 19 25 20 20 26 18 25 20 22 22 18
Table 3.1742.2 GPS week: 1742 Day: 2 MJD: 56440.000
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 | 15 9 4 6 15 3 19 7 11 19 3 | 35 43 40 38 53 38 49 40 39 31 39
2 | 11 10 6 10 15 3 11 10 7 26 3 | 18 18 19 21 28 18 18 23 21 18 18
3 | 8 10 5 6 14 4 13 6 9 21 3 | 26 32 23 27 29 23 30 24 28 31 25
4 | 9 7 7 8 16 3 10 16 10 27 4 | 26 22 23 27 34 24 24 31 23 30 24
5 | 8 12 6 8 17 3 13 11 8 15 3 | 18 21 17 20 31 14 22 18 24 17 17
6 | 8 12 4 7 11 4 15 10 7 21 3 | 13 20 10 15 19 11 19 13 18 15 11
7 | 7 12 5 7 18 3 14 10 9 33 3 | 23 25 22 22 33 21 25 24 25 34 21
8 | 10 10 5 6 14 3 10 15 9 18 3 | 17 19 17 20 22 17 20 27 19 21 17
9 | 9 10 5 7 14 3 12 14 7 20 3 | 20 22 20 20 22 18 25 24 22 25 18
10 | 10 7 4 8 14 3 9 11 8 17 3 | 15 19 18 18 24 15 22 19 24 22 17
11 | 10 11 5 7 17 3 13 8 9 16 3 | 24 34 27 27 42 27 33 29 31 25 27
12E | 14 20 6 8 17 4 24 8 13 12 5 | 29 27 20 23 23 19 26 20 26 18 20
13 | 8 16 4 9 22 4 13 9 6 13 4 | 22 26 25 21 42 22 26 25 28 25 23
14 | 7 10 5 10 14 4 15 8 11 14 3 | 21 26 24 24 31 23 25 22 32 25 23
15E | 10 22 6 12 23 6 18 7 10 13 4 | 20 29 20 20 25 14 23 21 24 25 19
16E | 16 15 7 15 22 4 18 17 11 18 5 | 25 25 25 30 25 23 29 29 28 28 24
17 | 8 15 6 7 17 3 18 10 6 24 4 | 16 23 14 15 32 14 26 15 23 18 14
18 | 8 16 4 8 16 4 20 8 11 19 4 | 18 28 23 21 35 21 26 21 30 22 21
19 | 6 14 6 8 15 5 18 8 9 23 3 | 13 25 16 15 31 16 26 16 25 20 16
20 | 10 14 5 8 17 3 15 7 7 14 3 | 16 22 18 19 31 19 22 20 26 15 18
21 | 8 13 7 7 13 3 12 6 9 35 3 | 20 29 26 25 33 24 25 22 26 34 23
22 | 7 14 5 8 16 4 18 8 8 16 3 | 22 29 25 26 38 22 29 22 29 20 23
23E | 10 13 6 11 20 4 13 8 8 15 4 | 27 29 26 21 36 23 30 26 32 29 25
24 | 13 16 6 6 15 2 13 8 8 11 3 | 16 23 19 17 26 15 27 17 21 20 16
25E | 12 13 6 7 17 4 16 12 11 12 4 | 18 24 18 15 23 15 27 16 23 14 16
26 | 13 13 9 8 16 3 15 11 9 18 4 | 18 25 19 20 22 15 25 20 22 25 18
28E | 8 10 4 6 23 3 12 9 7 20 3 | 20 22 20 22 21 17 25 21 23 24 18
29 | 16 19 6 10 12 3 23 8 10 19 4 | 24 33 21 23 28 21 34 23 26 27 22
X30E | 9 --- --- --- --- 66 --- --- --- --- 0 | 43 --- --- --- --- 28 --- --- --- --- 44
31 | 11 15 5 8 19 3 17 8 8 19 4 | 20 25 21 21 34 21 27 16 28 17 20
32 | 11 12 5 11 12 4 11 9 7 15 3 | 15 20 11 16 22 14 20 14 22 14 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 6 8 17 4 15 10 9 20 |T 21 25 20 21 29 19 26 21 25 22 20
WRMS | 10 13 6 9 15 4 15 9 8 20 |NE 19 25 20 21 31 19 26 21 25 22 20
MEDI | 10 13 5 8 16 3 14 8 9 18 |MD 20 25 20 21 29 19 25 21 25 22 20
Table 3.1742.3 GPS week: 1742 Day: 3 MJD: 56441.000
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 8 10 5 16 8 13 21 3 | 40 48 48 40 57 43 54 46 38 37 45
2 | 7 11 5 9 13 4 10 14 11 23 3 | 23 22 24 20 27 21 23 31 25 22 22
3 | 7 12 4 10 10 3 10 13 11 25 3 | 56 60 57 56 59 57 61 54 58 59 56
4 | 8 9 5 6 11 5 8 18 9 30 3 | 27 27 31 28 38 29 29 40 30 36 29
5 | 10 18 4 10 15 4 14 14 9 16 4 | 19 26 19 17 30 17 24 20 24 20 18
6 | 8 12 4 11 9 4 10 12 11 20 3 | 25 30 26 25 29 25 29 23 27 27 25
7 | 9 12 5 8 18 5 11 14 8 38 3 | 29 30 26 24 35 23 28 27 28 38 25
8 | 8 10 4 8 10 3 10 15 9 21 3 | 25 27 23 23 26 23 25 29 25 26 23
9 | 8 10 5 8 8 3 9 19 8 22 3 | 21 27 23 21 23 22 27 31 22 29 21
10 | 7 8 3 7 11 4 8 13 7 20 3 | 22 28 22 19 28 20 28 27 25 29 22
11 | 8 10 5 9 13 2 11 11 12 18 3 | 28 35 32 27 41 28 35 34 26 26 29
12E | 14 19 5 11 23 5 24 14 11 14 5 | 29 30 26 23 26 24 31 26 30 24 25
13 | 5 13 5 9 16 5 12 12 10 17 3 | 23 31 23 20 39 20 29 24 29 19 23
14 | 8 12 8 7 13 4 11 11 9 17 3 | 19 20 22 16 26 15 21 17 19 17 17
15E | 16 26 6 13 13 6 21 9 15 15 5 | 25 28 19 18 21 17 23 22 28 24 18
16E | 14 16 4 20 14 4 15 12 9 18 4 | 30 29 27 31 30 27 30 33 34 30 27
17 | 7 14 5 8 15 4 16 10 7 26 3 | 22 27 19 18 33 20 27 21 26 25 20
18 | 8 15 5 7 12 3 17 9 12 20 3 | 19 26 22 20 33 20 26 24 28 18 21
19 | 7 15 5 10 15 3 15 10 12 24 4 | 15 26 15 16 30 15 25 18 23 20 16
20 | 12 14 4 9 13 4 13 9 8 15 3 | 22 25 19 21 28 20 25 23 21 18 19
21 | 5 11 5 8 10 4 10 8 14 35 3 | 19 25 23 23 26 22 25 24 25 31 22
22 | 7 12 5 8 12 4 12 10 7 18 3 | 29 31 30 29 39 26 30 29 27 23 28
23E | 8 14 5 9 14 4 12 9 10 18 3 | 25 31 26 21 31 23 29 26 28 30 24
24 | 10 12 5 9 15 3 11 11 10 17 3 | 19 22 20 14 28 17 27 20 21 21 18
25E | 9 14 6 8 15 4 15 14 12 15 4 | 22 26 23 15 25 18 30 23 25 21 20
26 | 12 19 6 11 12 4 12 16 13 21 4 | 23 31 21 22 20 19 26 28 26 30 21
28E | 7 10 4 8 13 3 9 10 8 19 3 | 24 24 21 21 23 19 25 22 23 25 20
29 | 17 21 6 10 14 6 19 13 9 19 5 | 25 38 30 25 32 26 37 30 33 35 28
X30E | 8 --- --- --- --- 60 --- --- --- --- 0 | 57 --- --- --- --- 33 --- --- --- --- 56
31 | 10 15 5 8 17 4 10 10 12 20 3 | 18 26 20 18 35 19 26 20 28 20 20
32 | 12 11 4 8 10 3 8 12 6 16 3 | 20 24 14 12 22 12 22 19 21 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 9 13 4 13 12 10 21 |T 25 29 25 22 31 23 29 27 27 26 24
WRMS | 9 14 5 9 12 4 13 11 9 24 |NE 24 30 25 23 33 23 30 27 27 27 24
MEDI | 8 12 5 8 13 4 11 12 10 19 |MD 23 27 23 21 29 21 27 24 26 25 22
Table 3.1742.4 GPS week: 1742 Day: 4 MJD: 56442.000
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 4 10 8 3 17 14 11 24 3 | 37 46 44 36 54 38 50 39 43 32 41
2 | 7 8 6 12 14 4 9 17 10 22 3 | 20 23 21 20 25 19 23 30 23 23 20
3 | 9 9 6 7 11 3 9 14 9 22 3 | 35 34 34 35 33 34 37 43 39 38 33
4 | 11 7 7 10 13 4 8 19 11 30 4 | 27 24 21 28 28 22 26 37 28 36 23
5 | 9 14 5 10 15 5 14 18 8 16 4 | 21 30 22 18 30 21 29 28 26 27 22
6 | 9 10 5 8 9 3 9 17 9 21 3 | 22 22 20 21 24 19 23 30 26 26 19
7 | 7 12 5 9 20 5 10 14 9 36 4 | 24 32 24 22 34 22 27 29 26 38 23
8 | 9 10 5 8 13 4 8 22 9 19 3 | 49 50 49 47 47 48 48 50 47 44 47
9 | 7 10 6 11 10 3 8 18 6 24 3 | 29 32 29 23 23 25 31 36 23 36 26
10 | 9 7 5 10 13 3 7 14 7 21 3 | 19 24 21 17 23 18 24 26 21 32 19
11 | 7 11 4 10 11 3 10 13 11 17 3 | 23 36 30 24 42 25 36 30 31 25 28
12E | 14 16 5 13 22 5 20 20 8 20 5 | 25 30 24 25 28 23 31 30 29 25 23
13 | 8 12 4 10 19 4 9 17 9 21 4 | 30 34 30 25 41 29 32 33 31 32 29
14E | 7 11 6 10 15 4 9 15 10 14 3 | 37 39 38 34 40 35 37 36 34 33 35
15E | 9 18 6 13 19 4 19 13 10 17 5 | 23 27 21 19 24 17 24 26 23 24 19
16E | 10 19 6 14 17 3 12 15 9 15 4 | 24 30 26 24 29 23 26 24 32 27 24
17 | 6 15 6 13 16 4 12 9 11 28 4 | 21 30 23 22 33 20 29 23 28 27 22
18 | 7 13 7 9 13 4 15 11 10 19 4 | 22 29 25 20 32 22 30 24 26 20 23
19 | 6 14 5 9 14 3 14 12 9 24 3 | 19 31 22 16 33 18 29 21 24 23 21
20 | 10 15 4 8 12 3 12 14 9 19 3 | 17 28 21 18 32 19 26 24 28 20 20
21 | 7 11 5 10 10 3 10 11 12 36 3 | 24 28 29 24 32 25 30 29 34 38 26
22 | 7 10 6 9 12 3 13 12 11 18 3 | 24 28 31 23 35 25 27 26 32 22 26
23E | 9 12 4 12 14 5 13 15 9 21 4 | 18 25 21 17 26 17 25 25 20 26 18
24 | 10 12 5 11 16 4 11 13 11 14 4 | 22 26 22 18 26 19 28 25 25 23 20
25E | 10 13 6 11 15 3 14 17 7 19 4 | 18 27 22 19 24 17 29 26 24 22 19
26 | 11 19 8 12 14 5 18 17 10 22 5 | 21 31 21 20 23 20 30 31 17 32 19
28E | 6 11 5 11 13 3 7 11 7 25 3 | 28 32 30 26 32 27 30 31 27 33 27
29 | 15 16 8 10 13 6 19 13 8 22 4 | 21 30 23 21 28 19 30 27 25 28 22
X30E | 9 --- --- --- --- 82 --- --- --- --- 0 | 68 --- --- --- --- 46 --- --- --- --- 66
31 | 11 17 6 10 21 4 11 12 10 18 4 | 18 26 21 19 34 18 25 19 26 20 19
32 | 12 11 6 9 13 4 7 18 9 19 4 | 20 27 20 14 24 16 24 24 25 24 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 6 11 15 4 12 15 9 22 |T 26 30 26 23 31 24 29 29 28 28 25
WRMS | 9 13 6 11 13 4 12 14 9 23 |NE 24 30 26 23 32 23 30 29 28 28 24
MEDI | 9 12 5 10 13 4 11 14 9 21 |MD 23 30 23 21 30 22 29 28 26 27 23
Table 3.1742.5 GPS week: 1742 Day: 5 MJD: 56443.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 11 5 7 10 3 17 12 12 26 3 | 31 40 38 33 46 33 45 31 38 26 35
2 | 10 11 7 12 14 4 16 16 10 22 4 | 16 18 20 20 21 15 15 19 22 15 16
3 | 10 9 4 6 12 2 13 14 5 23 3 | 40 48 42 44 43 43 49 43 43 46 42
4 | 8 10 10 8 15 3 10 15 9 31 3 | 19 18 24 23 30 19 17 24 23 29 19
5 | 10 18 6 9 15 3 18 21 8 17 4 | 18 30 18 16 30 15 27 17 25 17 17
6 | 7 9 3 7 10 3 12 16 5 20 3 | 17 24 16 19 21 17 25 20 20 19 17
7 | 9 13 7 8 21 4 12 14 6 38 4 | 31 28 25 24 38 23 26 24 29 36 24
8 | 7 9 5 6 14 3 11 13 6 19 3 | 33 33 30 32 30 30 35 36 32 38 30
9 | 7 9 6 7 12 3 12 14 7 24 3 | 17 21 18 16 23 16 21 18 22 23 16
10 | 7 10 4 7 11 3 11 14 5 22 3 | 15 24 19 17 24 16 22 18 23 23 18
11 | 8 12 4 8 12 3 11 11 7 19 3 | 27 33 29 26 37 25 31 24 29 20 27
12E | 11 18 6 11 20 4 22 20 8 21 5 | 23 26 23 22 25 19 25 23 25 20 21
13 | 7 11 5 6 23 3 14 18 8 19 4 | 36 41 40 36 51 36 39 43 35 42 37
14E | 7 11 6 10 17 5 10 12 12 19 3 | 23 25 27 26 26 25 24 22 33 28 24
15E | 10 19 7 11 21 5 21 16 9 20 5 | 22 25 23 20 26 18 28 23 30 27 20
16E | 9 18 6 13 19 4 10 15 8 17 4 | 32 35 34 34 31 32 32 35 40 33 32
17 | 8 16 6 9 17 4 15 8 9 28 4 | 16 24 19 17 34 15 25 15 26 20 18
18 | 10 14 6 7 16 3 16 14 9 18 4 | 17 28 23 20 34 21 28 23 27 22 21
19 | 7 15 4 9 15 4 17 13 8 26 4 | 19 26 18 19 28 15 26 12 25 16 18
20 | 10 13 5 6 13 3 14 13 9 20 3 | 21 27 23 24 32 20 27 23 26 20 22
21 | 9 9 7 8 11 3 11 14 11 37 3 | 14 22 17 15 24 16 24 23 22 31 16
22 | 10 14 6 7 15 3 14 12 10 17 3 | 21 28 25 22 37 23 29 23 31 21 24
23E | 9 12 5 11 21 3 13 14 7 20 4 | 18 21 18 15 28 15 22 20 22 19 16
24 | 12 11 7 8 19 3 11 14 8 19 4 | 19 24 24 18 33 18 29 18 26 22 20
25E | 11 17 5 9 20 2 14 17 7 21 4 | 20 29 22 16 23 17 25 18 22 22 19
26 | 11 18 11 9 16 3 19 15 9 23 4 | 30 38 31 29 35 28 36 34 31 37 29
X27 | 8 --- --- --- --- 548 --- --- --- --- 0 | 284 --- --- --- --- 84 --- --- --- --- 282
28E | 7 9 5 8 15 2 9 11 7 16 3 | 17 24 20 19 23 18 24 21 25 19 18
29 | 14 16 5 10 13 4 19 16 9 22 4 | 25 30 22 22 26 21 29 25 27 28 22
X30E | 8 --- --- --- --- 66 --- --- --- --- 0 | 49 --- --- --- --- 31 --- --- --- --- 49
31 | 13 18 7 7 23 4 14 13 9 21 4 | 22 27 22 20 36 18 25 19 25 20 20
32 | 11 9 5 7 12 5 10 18 9 20 3 | 17 22 17 16 23 14 24 18 24 19 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 6 9 16 3 14 15 8 23 |T 31 27 24 22 30 23 27 23 27 25 31
WRMS | 9 13 6 9 14 3 14 14 8 23 |NE 33 28 24 22 31 24 28 23 27 25 33
MEDI | 9 12 6 8 15 3 13 14 8 20 |MD 21 26 23 20 30 19 26 23 26 22 20
Table 3.1742.6 GPS week: 1742 Day: 6 MJD: 56444.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 8 5 9 10 3 17 12 17 29 4 | 43 52 55 50 63 48 59 49 46 42 50
2 | 5 9 4 5 13 3 10 14 6 23 3 | 19 20 23 24 31 21 19 29 21 21 21
3 | 10 10 5 4 11 3 12 11 11 20 3 | 32 37 33 30 34 31 33 27 32 39 31
4 | 7 10 4 7 12 3 10 9 6 36 2 | 28 25 30 34 42 29 27 36 32 38 30
5 | 11 14 4 8 16 4 17 15 9 19 4 | 18 30 22 24 33 19 30 21 22 21 21
6 | 9 10 5 5 11 3 15 13 9 16 3 | 11 21 16 13 20 12 21 14 19 19 13
7 | 6 12 5 7 23 4 15 15 13 38 4 | 26 29 25 31 32 25 25 27 27 49 25
8 | 8 8 5 8 14 4 10 10 8 14 3 | 35 35 36 33 36 34 38 34 36 29 34
9 | 7 8 5 7 13 4 10 7 6 21 3 | 22 22 23 19 24 21 25 18 21 23 20
10 | 5 9 4 6 11 4 10 12 9 22 3 | 15 20 18 18 28 16 22 20 20 23 17
11 | 11 11 5 9 14 3 13 11 14 19 4 | 27 35 34 31 47 29 36 32 28 26 31
12E | 16 21 7 11 23 4 22 15 12 13 5 | 24 24 19 22 30 17 24 18 25 16 18
13 | 16 14 5 10 15 8 13 23 8 18 4 | 98 88 90 90 94 87 91 88 91 83 90
14E | 9 11 4 10 13 4 9 10 7 18 3 | 24 27 26 27 28 26 29 22 26 24 24
15E | 10 16 5 10 19 4 20 14 12 18 4 | 26 35 30 33 31 28 28 32 31 28 28
16E | 10 24 4 11 18 3 15 18 9 11 4 | 20 32 22 25 23 21 25 24 27 22 21
17 | 8 15 4 9 22 5 16 7 7 27 4 | 21 26 23 23 36 22 26 24 28 26 22
18 | 12 13 6 8 16 4 18 19 8 22 4 | 19 27 22 20 31 20 27 26 21 18 20
19 | 10 16 4 7 17 4 15 10 12 23 4 | 17 25 20 19 33 17 25 17 22 18 18
20 | 9 13 5 8 17 3 15 15 11 18 4 | 19 23 19 21 31 18 24 21 19 20 18
21 | 9 10 7 7 12 5 12 17 10 39 3 | 22 23 25 23 31 22 25 30 25 35 23
22 | 11 11 5 7 17 3 15 16 7 19 3 | 16 27 22 21 36 20 26 26 23 21 21
23E | 8 13 4 11 18 3 15 18 7 18 4 | 20 23 19 19 27 18 24 21 23 26 18
24 | 12 16 5 9 21 5 12 11 11 14 4 | 18 25 19 19 27 18 28 20 19 21 17
25E | 10 15 5 7 19 3 17 13 10 22 4 | 13 22 20 11 24 14 29 12 23 20 16
26E | 18 19 10 11 18 8 16 13 13 22 5 | 49 50 54 48 43 44 46 52 43 51 47
X27 | 7 --- --- --- --- 55 --- --- --- --- 0 | 192 --- --- --- --- 84 --- --- --- --- 190
28E | 6 11 5 7 17 4 12 7 6 13 3 | 19 19 21 16 22 17 22 15 20 16 17
29 | 11 19 5 10 15 6 17 13 9 22 4 | 26 34 23 24 26 23 36 27 30 31 25
X30E | 7 --- --- --- --- 34 --- --- --- --- 0 | 40 --- --- --- --- 26 --- --- --- --- 42
31 | 11 19 5 9 27 4 16 11 9 21 4 | 18 25 19 20 38 19 23 18 26 14 18
32 | 8 12 6 7 13 5 9 17 10 18 3 | 17 21 16 16 19 14 22 20 20 22 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 8 17 4 14 14 10 22 |T 31 30 27 26 34 26 30 27 28 28 31
WRMS | 9 14 5 8 16 4 14 13 9 20 |NE 33 30 27 27 36 28 31 28 28 29 33
MEDI | 9 12 5 8 16 4 15 13 9 19 |MD 21 25 22 23 31 21 26 24 25 23 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 4.1742 GPS week: 1742 MJD: 56438.0-56444.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2951 |U 6 6 14 |U 13 38 79 |U 7 7 18 |
emr | emr 2880 | 7 7 20 |U 15 37 79 | 8 7 22 |
esa | esa 2880 | 5 5 16 |U 16 37 82 | 7 7 18 |
gfz | gfz 2879 |U 5 6 16 |U 12 39 75 |U 7 6 17 |
grg | grg 2879 |U 11 13 35 |U 20 42 90 | 12 15 40 |
igr | igr 2880 | 5 6 16 | 12 37 80 | 7 6 17 |
igs | igs 2880 | 5 5 16 | 13 37 77 | 8 6 18 |
jpl | jpl 2880 | 7 7 21 |U 13 38 85 |U 8 7 23 |
mit | mit 2880 | 5 7 16 |U 18 39 92 |U 8 8 20 |
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 5.1742.0 GPS week: 1742 Day: 0 MJD: 56438.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2931 | 4 3 12 | 5 9 21 | 9 10 20 |
emr | emr 2880 | 9 7 23 | 7 6 21 | 10 10 20 |
esa | esa 2880 | 5 3 14 | 5 8 20 | 10 10 21 |
gfz | gfz 2880 | 5 3 13 | 5 8 20 | 9 9 18 |
grg | grg 2880 | 10 13 30 | 6 9 30 | 10 13 33 |
igr | igr 2880 | 5 3 14 | 5 8 20 | 9 10 20 |
igs | igs 2880 | 5 4 15 | 4 7 20 | 9 9 19 |
jpl | jpl 2880 | 6 5 20 | 5 8 20 | 10 8 18 |
mit | mit 2880 | 7 12 15 | 5 8 24 | 8 12 25 |
Table 5.1742.1 GPS week: 1742 Day: 1 MJD: 56439.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2933 | 12 8 17 | 9 11 34 | 8 7 18 |
emr | emr 2880 | 8 6 20 | 11 12 36 | 10 8 23 |
esa | esa 2880 | 4 5 16 | 9 11 36 | 8 6 20 |
gfz | gfz 2880 | 5 5 17 | 9 13 38 | 8 5 18 |
grg | grg 2880 | 12 14 36 | 12 10 39 | 10 18 35 |
igr | igr 2880 | 4 6 17 | 9 11 36 | 8 5 18 |
igs | igs 2880 | 4 5 17 | 9 12 36 | 8 6 18 |
jpl | jpl 2880 | 5 7 16 | 9 12 40 | 9 8 24 |
mit | mit 2880 | 4 7 18 | 10 13 38 | 10 9 21 |
Table 5.1742.2 GPS week: 1742 Day: 2 MJD: 56440.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2933 | 5 4 14 | 56 214 408 | 6 5 13 |
emr | emr 2880 | 8 7 21 | 52 211 400 | 8 7 20 |
esa | esa 2880 | 5 5 18 | 78 209 427 | 7 6 13 |
gfz | gfz 2880 | 5 4 17 | 50 220 363 | 7 5 12 |
grg | grg 2880 | 9 8 26 | 76 221 424 | 11 16 35 |
igr | igr 2880 | 5 5 18 | 53 209 407 | 7 5 13 |
igs | igs 2880 | 5 4 17 | 52 210 397 | 7 6 13 |
jpl | jpl 2880 | 6 6 21 | 53 211 438 | 8 6 21 |
mit | mit 2880 | 5 4 17 | 86 208 480 | 8 5 15 |
Table 5.1742.3 GPS week: 1742 Day: 3 MJD: 56441.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2940 | 7 9 18 | 8 13 26 | 9 9 24 |
emr | emr 2880 | 11 9 24 | 10 9 27 | 10 9 26 |
esa | esa 2880 | 10 8 20 | 7 9 24 | 10 8 25 |
gfz | gfz 2880 | 9 8 20 | 8 10 29 | 10 8 22 |
grg | grg 2880 | 13 14 40 | 14 11 37 | 14 15 45 |
igr | igr 2880 | 10 8 22 | 7 9 26 | 9 8 22 |
igs | igs 2880 | 9 8 21 | 8 9 24 | 10 8 23 |
jpl | jpl 2880 | 10 9 24 | 9 9 27 | 10 9 27 |
mit | mit 2880 | 9 8 19 | 7 9 26 | 10 10 22 |
Table 5.1742.4 GPS week: 1742 Day: 4 MJD: 56442.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2934 | 4 5 11 | 5 8 24 | 6 6 17 |
emr | emr 2880 | 6 7 15 | 9 8 23 | 7 6 22 |
esa | esa 2880 | 4 5 11 | 5 10 24 | 6 5 18 |
gfz | gfz 2880 | 5 5 11 | 6 8 29 | 6 7 16 |
grg | grg 2879 | 9 10 29 | 11 15 29 | 11 12 34 |
igr | igr 2880 | 4 4 10 | 5 9 25 | 6 5 18 |
igs | igs 2880 | 4 5 10 | 5 8 23 | 6 5 18 |
jpl | jpl 2880 | 6 6 12 | 6 8 25 | 7 7 24 |
mit | mit 2880 | 4 7 10 | 5 11 22 | 7 6 20 |
Table 5.1742.5 GPS week: 1742 Day: 5 MJD: 56443.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2978 | 5 4 14 | 5 7 24 | 7 6 19 |
emr | emr 2880 | 6 5 17 | 7 8 23 | 7 6 24 |
esa | esa 2880 | 4 6 18 | 5 7 27 | 7 6 18 |
gfz | gfz 2880 | 5 8 18 | 6 7 30 | 7 6 18 |
grg | grg 2880 | 16 24 57 | 12 15 39 | 18 21 80 |
igr | igr 2880 | 4 6 18 | 5 7 27 | 7 6 18 |
igs | igs 2880 | 4 6 17 | 5 7 25 | 7 6 19 |
jpl | jpl 2880 | 8 8 27 | 6 8 27 | 7 7 24 |
mit | mit 2880 | 4 7 18 | 6 8 31 | 8 6 22 |
Table 5.1742.6 GPS week: 1742 Day: 6 MJD: 56444.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3013 | 7 8 14 | 4 9 16 | 5 5 13 |
emr | emr 2880 | 5 6 18 | 7 7 21 | 7 6 19 |
esa | esa 2880 | 4 7 17 | 5 7 15 | 6 6 14 |
gfz | gfz 2876 | 5 8 16 | 5 7 18 | 6 5 13 |
grg | grg 2880 | 9 10 27 | 9 12 31 | 9 10 18 |
igr | igr 2880 | 4 7 17 | 4 7 15 | 5 5 14 |
igs | igs 2880 | 4 6 16 | 5 7 16 | 6 5 14 |
jpl | jpl 2880 | 6 7 28 | 6 9 20 | 7 7 25 |
mit | mit 2880 | 5 6 17 | 7 14 25 | 7 5 15 |
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 6.1742 GPS week: 1742 MJD: 56438.500-56444.500
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 | -51 -23 3 -200 -4 | 6 20
| 20 18 51 66 6 | 4
emr uuuuu | 37 26 -19 238 0 | 35 40
| 29 15 69 68 13 | 3
esa uuuuu | -4 -6 18 -53 0 | 18 26
| 13 13 66 47 4 | 2
gfz uuuuu | 16 9 -23 25 -1 | 11 22
| 15 13 70 35 3 | 3
grg uuuux | 3 -17 5 -55 -30 | 10 25
| 16 12 80 133 34 | 6
igr xxxxx | -38 -4 13 67 -5 | 1 19
| 17 9 56 32 4 | 5
irf xxxxx | 22 0 -19 2 0 | 3 19
| 10 3 18 29 2 | 2
jpl uuuuu | 39 -17 27 156 6 | 28 34
| 35 13 76 77 7 | 3
mit uuuuu | 42 -10 -88 23 4 | 13 24
| 27 20 85 53 4 | 2
ngs uuuuu | -42 31 42 16 0 | 8 17
| 54 24 100 61 4 | 2
sio xxxxx | 301 146 -61 229 7 | 32 38
| 55 30 25 59 7 | 2
Table 7.1742.0 GPS week: 1742 Day: 0 MJD: 56438.500
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 | -64 -12 18 -150 -7 | 8 20
emr uuuuu | 35 -3 11 222 -9 | 38 42
esa uuuuu | -20 -7 -1 -61 -2 | 17 25
gfz uuuuu | 35 24 -174 72 0 | 13 22
grg uuuux | 3 -23 -48 -125 -36 | 17 25
igr xxxxx | -39 0 -33 57 -8 | 5 19
irf xxxxx | 23 -1 -4 -26 4 | 3 18
jpl uuuuu | -16 -24 -27 72 2 | 27 34
mit uuuuu | 0 -27 43 -30 11 | 12 22
ngs uuuuu | 35 51 178 41 1 | 7 16
sio xxxxx | 332 163 -58 140 20 | 28 34
Table 7.1742.1 GPS week: 1742 Day: 1 MJD: 56439.500
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 | -48 -48 98 -217 0 | 9 20
emr uuuuu | 40 34 47 254 -3 | 37 41
esa uuuuu | 16 22 -103 1 4 | 18 26
gfz uuuuu | -10 16 7 3 2 | 13 23
grg uuuux | 16 -21 -64 -171 -32 | 16 25
igr xxxxx | -43 -7 -59 44 -5 | 5 19
irf xxxxx | 9 1 -5 -46 0 | 5 20
jpl uuuuu | 16 -27 48 61 -5 | 30 37
mit uuuuu | 24 -21 -11 -23 5 | 13 24
ngs uuuuu | -54 16 85 85 -4 | 9 18
sio xxxxx | 317 150 -105 163 9 | 33 39
Table 7.1742.2 GPS week: 1742 Day: 2 MJD: 56440.500
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 | -66 -22 -26 -118 -11 | 12 21
emr uuuuu | 1 15 35 210 -3 | 39 43
esa uuuuu | 6 -8 -13 -3 5 | 22 28
gfz uuuuu | 11 11 -10 -12 -2 | 16 24
grg uuuux | 8 -9 -10 -198 -4 | 14 25
igr xxxxx | -53 2 -3 58 -3 | 7 18
irf xxxxx | 13 -5 -35 -5 0 | 7 19
jpl uuuuu | 14 -3 19 177 12 | 32 38
mit uuuuu | 25 -18 -92 67 7 | 17 26
ngs uuuuu | -1 29 112 -99 2 | 11 18
sio xxxxx | 211 153 -58 255 8 | 35 41
Table 7.1742.3 GPS week: 1742 Day: 3 MJD: 56441.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -14 -31 31 -137 -6 | 7 20
emr uuuuu | 50 28 -115 290 9 | 34 38
esa uuuuu | -8 -6 53 -138 -3 | 18 25
gfz uuuuu | 12 4 5 74 1 | 11 22
grg uuuux | -29 -4 -57 -104 19 | 7 20
igr xxxxx | -62 8 15 42 -9 | 2 18
irf xxxxx | 24 0 -5 27 1 | 3 19
jpl uuuuu | 57 6 -101 201 7 | 27 32
mit uuuuu | 53 -24 -76 104 4 | 13 23
ngs uuuuu | -79 40 84 33 -1 | 8 17
sio xxxxx | 255 101 -30 235 4 | 33 39
Table 7.1742.4 GPS week: 1742 Day: 4 MJD: 56442.500
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 9 -18 -290 -6 | 4 18
emr uuuuu | 77 35 -121 277 18 | 32 36
esa uuuuu | 4 -5 68 -78 2 | 17 24
gfz uuuuu | 12 -10 40 25 0 | 10 20
grg uuuux | 5 -1 60 22 -19 | 9 21
igr xxxxx | -24 -2 104 89 -6 | -1 17
irf xxxxx | 37 6 -6 13 0 | 2 18
jpl uuuuu | 67 -18 78 265 17 | 25 30
mit uuuuu | 82 -3 -107 9 1 | 12 23
ngs uuuuu | -130 1 -96 8 -5 | 7 16
sio xxxxx | 322 108 -53 275 2 | 32 38
Table 7.1742.5 GPS week: 1742 Day: 5 MJD: 56443.500
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 | -63 -25 -28 -222 -6 | 5 19
emr uuuuu | 60 26 -1 309 9 | 35 40
esa uuuuu | -11 -22 98 -43 -5 | 19 26
gfz uuuuu | 18 -4 -3 1 -8 | 11 21
grg uuuux | 17 -26 -4 15 -59 | 8 21
igr xxxxx | -36 -11 63 49 -7 | -1 17
irf xxxxx | 28 -2 -34 32 -1 | 3 19
jpl uuuuu | 53 -27 34 111 3 | 28 34
mit uuuuu | 58 -9 -171 56 2 | 14 24
ngs uuuuu | -45 69 -68 -22 8 | 7 16
sio xxxxx | 378 164 -79 236 2 | 34 40
Table 7.1742.6 GPS week: 1742 Day: 6 MJD: 56444.500
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 | -68 -29 -56 -263 7 | 0 23
emr uuuuu | -2 44 10 106 -20 | 32 38
esa uuuuu | -14 -13 23 -47 -2 | 15 26
gfz uuuuu | 32 22 -29 10 -2 | 7 24
grg uuuux | -2 -32 158 178 -81 | -1 35
igr xxxxx | -11 -19 1 130 3 | -6 22
irf xxxxx | 18 2 -46 16 -2 | 0 22
jpl uuuuu | 79 -26 139 206 7 | 24 33
mit uuuuu | 51 30 -200 -21 0 | 11 25
ngs uuuuu | -21 9 -1 63 0 | 4 18
sio xxxxx | 294 180 -42 302 2 | 31 39
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