[IGSREPORT-23008] Wk 1807 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Sep 12 22:08:07 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1807 (Aug 24, 2014 - Aug 30, 2014)
Contacts: igs.acc 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:
igs1807[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1807[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1807[0-6].cls IGS GPS clock combination summary report.
igs18077.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18077.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 | 4 4
0 | EMR | 8
0 | ESA | 4 4
0 | GFZ | 1 2 6 21 30 1 6 8 21 30 DAEJ DAEJ
0 | GRG | 6 6 FAA1 KELY BOGT FAA1
0 | JPL | 8
0 | MIT | CRO1 FLIN MDVJ MONP
1 | COD | KARR KOUC KARR KOUC
1 | EMR | 4 4
1 | GFZ | 1 2 6 30 1 6 30
1 | GRG | 4 6 4 6 CAS1 GLSV GRAZ IRKJ KARR USNO CAS1 GLSV GRAZ
1 | GRG | IRKJ KARR NKLG USNO
1 | JPL | 4 8
1 | MIT | 9 4 9
2 | COD | 4
2 | EMR | 8
2 | ESA | 4 SFER SFER
2 | GFZ | 1 2 6 30 1 6 30 BOR1 KELY NKLG KELY NKLG
2 | GRG | 6 6 DRAG KOUC MONP DRAG KOUC UNSA
2 | JPL | 8 BOGT
2 | MIT | 9 4 9 11 USNO MDVJ MONP USNO
3 | COD | 4 FLIN REUN
3 | EMR | 8 11 20 HOB2 HOB2
3 | ESA | 4 HOB2 HOB2 SFER UNSA
3 | GFZ | 1 6 30 1 6 30 MCM4
3 | GRG | 6 6 BOR1 HYDE MAC1 SFER BOR1 FLIN HYDE MAC1 SFER
3 | JPL | 8 TIXI
3 | MIT | SFER MDVJ SFER
4 | COD | 4 KARR TRO1
4 | ESA | 4 SFER FAA1 HOFN SFER
4 | GFZ | 1 2 4 6 30 1 4 6 30 FAIR FLIN IRKJ NYA1 SFER TRO1
4 | GFZ | WHIT FAIR NYA1 WHIT
4 | GRG | 6 6 CAS1 FAA1 MAR6 NYA1 CAS1 CHUM FAA1 IRKJ MAL2
4 | GRG | MAR6 NYA1 SFER TRO1
4 | JPL | 8 RESO
4 | MIT | HNLC MONP
5 | COD | 4 HOB2 HOB2
5 | EMR | 8 WHIT WHIT
5 | ESA | 4 FLIN HOB2 HOB2 UNSA
5 | GFZ | 1 2 4 6 30 1 4 6 30 CHUR FAIR GLSV INVK YELL CHUR
5 | GFZ | FAIR FLIN GLSV YELL
5 | GRG | 6 6 KOUC KOUC
5 | JPL | WHIT
5 | MIT | 11
6 | COD | 9 MAL2
6 | EMR | 4 WHIT
6 | ESA | UNSA
6 | GFZ | 1 2 6 30 1 6 30 MAL2 QAQ1 QAQ1
6 | GRG | 6 4 6 PDEL SFER PDEL SFER
6 | JPL | 4 WHIT
6 | MIT | 9 4 9 BRMU FLIN HNPT MONP
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | GRG | 6
3 | GFZ | 9
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G04 | 4 | 4 | 4 | 4 | | 4 | 4 |
PRN G08 | | | | 4 | | | |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.4 1.6 .1 -10 11 -9 .26
EMR | 0 | 3.6 3.7 10.1 -21 8 -14 .37
ESA | 0 | -.6 .1 -1.8 -5 -5 15 -.20
GFZ | 0 | .2 .6 -1.5 -21 -39 -14 -.09
GRG | 0 | 10.6 1.3 .4 -36 8 4 .65
JPL | 0 | 6.3 1.2 16.6 -108 36 -20 -.72
MIT | 0 | 3.5 -.4 2.3 0 10 -41 .34
NGS | 0 | -.8 2.8 19.9 -34 -43 8 .48
SIO | 0 | 1.1 1.6 -14.4 -4 14 -17 .24
COD | 1 | -1.0 -.5 -.9 -53 33 -55 .43
EMR | 1 | -2.3 5.8 1.2 -20 13 -30 .57
ESA | 1 | .6 .5 -1.9 5 -15 48 .06
GFZ | 1 | .3 -.1 -1.9 -17 -37 15 -.01
GRG | 1 | 9.8 -5.1 -6.2 -19 26 20 .79
JPL | 1 | -2.3 6.1 4.8 -58 38 -14 .01
MIT | 1 | .0 1.2 3.7 -1 4 -39 .43
NGS | 1 | -3.3 -9.8 11.5 -56 0 -46 .53
SIO | 1 | 2.7 5.1 -9.1 -1 0 9 .12
COD | 2 | -.4 .1 .6 -65 37 -37 .30
EMR | 2 | -2.4 7.2 2.5 -24 8 -19 .40
ESA | 2 | .0 .9 -1.9 9 -14 50 -.04
GFZ | 2 | .9 .6 -1.7 -23 -53 14 -.03
GRG | 2 | 7.2 -6.1 5.3 -21 37 -5 1.05
JPL | 2 | 1.6 7.8 11.4 -31 12 35 -.17
MIT | 2 | 3.5 .0 5.1 6 8 -35 .47
NGS | 2 | 3.6 -2.2 18.2 -61 -40 20 .60
SIO | 2 | 3.3 3.6 -15.6 -9 20 -3 .34
COD | 3 | -.1 .0 .1 -41 3 -2 .17
EMR | 3 | -5.0 2.8 8.7 -19 4 1 .21
ESA | 3 | -.2 .8 -1.5 9 -15 27 -.09
GFZ | 3 | .7 .3 -1.5 -51 -62 4 -.02
GRG | 3 | 9.9 -3.6 1.7 -26 31 -27 .40
JPL | 3 | -3.5 6.9 8.3 -26 0 -30 .38
MIT | 3 | -4.7 1.4 .3 4 7 -37 .46
NGS | 3 | -.2 -2.9 13.6 -39 -17 -14 .36
SIO | 3 | -2.0 7.7 -6.1 5 1 7 .29
COD | 4 | .1 -.1 .0 -34 -6 8 .26
EMR | 4 | 2.8 2.6 5.7 -25 11 -17 .28
ESA | 4 | .1 .9 -1.8 9 -12 24 -.10
GFZ | 4 | .7 .3 -1.6 -30 -46 9 .06
GRG | 4 | 17.8 -.6 -3.3 -25 31 13 .78
JPL | 4 | -2.5 3.3 5.8 -85 49 0 -.27
MIT | 4 | -1.2 4.4 .9 -6 10 -43 .40
NGS | 4 | -2.5 -5.8 15.9 -44 -18 -21 .60
SIO | 4 | 3.7 3.8 -5.9 3 8 -22 .31
COD | 5 | -1.0 .1 -.3 -20 24 -2 .07
EMR | 5 | -1.9 5.0 5.9 -16 7 -7 .07
ESA | 5 | -.2 .5 -1.9 -9 5 31 -.14
GFZ | 5 | .0 .0 -1.3 -36 -37 24 -.20
GRG | 5 | 19.0 .0 1.5 -8 18 -22 .63
JPL | 5 | 5.2 5.1 13.9 -93 35 18 -.35
MIT | 5 | 1.6 5.0 .7 -4 8 -35 .32
NGS | 5 | 2.6 -2.8 14.3 -36 -30 3 .38
SIO | 5 | 3.2 3.9 -6.2 -10 15 -4 .11
COD | 6 | -.1 -.4 .3 -32 6 18 .18
EMR | 6 | .0 6.8 10.4 -25 27 -37 .04
ESA | 6 | -.2 1.3 -1.8 1 -1 39 -.12
GFZ | 6 | -.1 .6 -1.5 -14 -33 15 -.25
GRG | 6 | 12.0 -2.3 2.5 -18 36 -38 .42
JPL | 6 | 5.7 10.8 15.7 -102 19 -19 -.32
MIT | 6 | 4.9 4.4 1.5 -4 9 -30 .33
NGS | 6 | 5.9 -9.5 19.1 -71 -44 2 .27
SIO | 6 | 1.9 6.5 -11.7 -8 27 -11 .16
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1807.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1807.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 2.1807.[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 3.1807.[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 5.1807.0-6). 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 1807 summary. (Aug 24, 2014 - Aug 30, 2014)
Table 1.1807.a GPS week: 1807 MJD: 56893.000-56899.000
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 250| 0 0 0 27 15 -2 .08 10 10 | -1109 -53 17 111
| 1 0 1 11 7 22 .02 | 190 591
emr 80| -2 0 0 19 -31 45 .30 13 13 | 2095 68 15 142
| 1 1 0 10 15 17 .03 | 628 640
esa 149| 0 0 -5 0 -1 6 -.31 12 12 | -254 -1209 10 173
| 0 0 0 13 8 9 .02 | 2018 4614
gfz 194| 0 0 4 4 -27 0 .15 14 13 | -288 163 15 147
| 0 0 1 25 14 18 .03 | 510 701
grg 175| 3 0 -2 14 23 -1 .28 21 18 | -182 -40 17 148
| 1 0 2 18 25 9 .02 | 60 121
igr n/a| 0 0 0 1 2 -14 -.19 6 6 | 5993 -202 17 115
| 0 0 0 17 10 13 .02 | 784 686
jpl 80| 0 0 -1 -24 32 -11 .03 13 12 | 1289 198 17 133
| 1 1 0 21 17 21 .03 | 777 710
mit 350| 1 -4 0 -11 -28 2 .07 16 14 | -107 -103 24 199
| 0 1 0 8 21 15 .01 | 171 194
ngs 228| 0 1 2 -26 31 -43 .03 12 11 | -1095 -10 1235 2762
| 0 0 0 35 21 25 .07 | 190 670
sio 630| 0 0 -1 -10 -19 6 -.60 15 15 | --- --- --- ---
| 1 0 1 19 29 11 .04 | --- ---
Table 1.1807.b GPS week : 1807 MJD: 56893.000-56899.000
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 | 5 6 4 4 5 4 5 |
2 | 4 4 4 5 4 4 4 |
4 | 6 7 8 7 7 6 6 |
5 | 5 4 5 5 4 5 5 |
6 | 5 6 6 6 6 6 6 |
7 | 5 5 5 5 5 4 4 |
8 | 6 6 6 6 6 6 5 |
9 | 10 8 7 0 0 0 7 |
10 | 4 4 4 5 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 5 5 5 4 4 |
14 | 5 5 5 5 5 5 4 |
15 | 5 5 5 5 5 5 5 |
16 | 6 5 5 6 5 5 5 |
17 | 6 5 5 5 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 5 5 5 |
20 | 5 5 5 5 5 5 5 |
21 | 4 5 4 4 4 5 4 |
22 | 5 5 5 5 5 5 5 |
23 | 5 5 4 5 4 4 4 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 3 4 4 4 |
27 | 5 5 5 5 5 5 5 |
28 | 5 5 5 5 5 5 4 |
29 | 5 5 5 5 5 5 5 |
30 | 5 4 4 4 4 4 4 |
31 | 6 6 6 5 5 5 5 |
32 | 5 4 4 4 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 2.1807.0 GPS week: 1807 Day: 0 MJD: 56893.000
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 248| -2 -1 0 45 25 14 .05 14 14 | -1387 409 22 118
emr 80| 0 1 0 21 -11 51 .23 13 13 | 2629 -1034 14 148
esa 150| 0 1 -5 -1 10 2 -.32 13 13 | -788 279 11 164
gfz 198| 0 0 4 15 -7 -9 .11 15 13 | -216 184 14 141
grg 177| 2 0 0 23 -4 8 .29 23 17 | -172 73 16 148
igr n/a| -1 0 -1 3 14 7 -.21 6 5 | 7627 -1388 16 101
jpl 80| -1 1 -1 -51 30 -10 .05 13 12 | 1514 -1055 17 133
mit 350| 1 -5 -1 -8 -40 0 .04 15 13 | 85 -144 25 218
ngs 233| 0 1 3 -27 5 -48 .08 11 10 | -1368 386 1264 2923
sio 655| 0 -1 -3 -11 -28 11 -.65 15 14 | --- --- --- ---
Table 2.1807.1 GPS week: 1807 Day: 1 MJD: 56894.000
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 255| 0 1 0 20 9 -30 .04 9 9 | -1268 324 20 131
emr 80| 0 0 0 30 -35 56 .31 13 13 | 1618 -408 18 149
esa 150| 0 1 -4 -1 2 20 -.29 12 12 | -246 -239 12 178
gfz 197| 0 0 5 3 -47 -1 .13 14 13 | -60 172 17 138
grg 176| 1 0 -1 7 -4 -8 .30 22 19 | -155 -16 18 145
igr n/a| 0 0 0 -21 1 0 -.19 6 5 | 6161 -663 18 98
jpl 80| 0 0 0 -15 59 12 .04 13 12 | 1676 -317 18 134
mit 350| 0 -5 0 -17 -33 -4 .08 18 15 | 83 -308 27 205
ngs 232| 0 2 1 -41 65 -38 .10 12 11 | -1151 441 1192 3021
sio 659| 0 -1 0 -11 -42 0 -.65 15 15 | --- --- --- ---
Table 2.1807.2 GPS week: 1807 Day: 2 MJD: 56895.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| 0 0 3 11 24 -34 .09 10 9 | -1095 102 16 103
emr 80| -1 0 -1 12 -34 55 .28 13 13 | 1349 295 14 133
esa 149| -1 0 -7 14 -5 21 -.31 13 13 | -877 -196 11 174
gfz 197| 0 0 5 24 -25 -11 .17 14 13 | -525 71 14 146
grg 177| 3 0 -1 52 24 6 .26 21 19 | -152 -70 18 188
igr n/a| 0 0 0 -9 10 -27 -.21 6 6 | 5507 -106 16 109
jpl 80| -1 0 -2 -6 27 22 .00 13 12 | 219 325 17 141
mit 350| 2 -5 0 -13 -14 -9 .07 15 13 | -17 -151 24 200
ngs 230| 0 1 2 -23 13 -59 .05 12 10 | -1122 179 1126 2904
sio 656| 2 0 -1 -43 -17 28 -.62 15 16 | --- --- --- ---
Table 2.1807.3 GPS week: 1807 Day: 3 MJD: 56896.000
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 250| -1 0 0 34 10 4 .11 10 10 | -931 -14 16 111
emr 80| -2 1 0 19 -20 58 .32 14 14 | 1669 767 19 153
esa 150| -1 0 -6 18 -10 -1 -.29 12 12 | -211 -931 10 164
gfz 182| 0 -1 3 40 -37 -18 .19 14 13 | -123 0 16 146
grg 173| 4 0 0 1 51 -9 .27 21 19 | -296 92 17 148
igr n/a| 0 0 1 32 9 -29 -.20 6 6 | 5466 520 18 130
jpl 80| 0 1 0 1 3 -32 .02 14 13 | 612 840 19 138
mit 350| 1 -4 0 -18 -9 -13 .07 14 13 | -290 114 21 192
ngs 233| 1 1 2 -73 53 -14 -.03 11 11 | -910 -48 1299 2714
sio 652| 0 0 -1 -25 -35 6 -.55 15 15 | --- --- --- ---
Table 2.1807.4 GPS week: 1807 Day: 4 MJD: 56897.000
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 246| 0 0 0 20 12 27 .08 9 9 | -1228 366 19 117
emr 80| -3 1 0 6 -46 46 .30 14 14 | 1789 758 16 150
esa 150| -1 1 -4 2 -9 0 -.34 13 13 | -1166 551 12 212
gfz 192| 0 0 3 -1 -37 11 .16 13 13 | -1012 1082 12 150
grg 175| 2 -2 -4 1 60 10 .26 21 19 | -209 -257 17 137
igr n/a| 1 0 1 0 6 -14 -.19 6 6 | 5316 620 18 126
jpl 80| 0 0 0 -47 41 -28 -.02 13 13 | 736 1024 17 135
mit 350| 1 -3 0 -4 -12 6 .05 15 14 | -83 -316 23 183
ngs 226| 0 0 2 0 27 -74 .06 12 10 | -1202 339 1414 2481
sio 636| 1 0 0 4 -27 6 -.57 14 16 | --- --- --- ---
Table 2.1807.5 GPS week: 1807 Day: 5 MJD: 56898.000
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 250| 0 0 0 30 8 3 .09 9 9 | -888 -1272 17 98
emr 80| -3 0 0 35 -53 45 .31 13 13 | 2721 99 12 144
esa 150| 0 0 -5 -10 -5 2 -.32 12 12 | 3987 -11219 10 182
gfz 196| 0 0 4 -37 -30 38 .15 14 13 | 581 -1140 16 163
grg 177| 3 -1 -3 12 11 -10 .26 21 18 | -191 -119 17 142
igr n/a| 0 0 1 14 -10 -18 -.19 6 5 | 6027 -152 16 130
jpl 80| -1 2 -1 -8 38 -23 .04 13 12 | 1918 466 17 126
mit 350| 2 -3 0 1 -17 2 .07 16 14 | -193 -112 28 201
ngs 226| 1 2 3 -55 25 -64 .05 12 11 | -789 -1480 1136 2435
sio 634| 0 0 -1 14 44 1 -.58 14 14 | --- --- --- ---
Table 2.1807.6 GPS week: 1807 Day: 6 MJD: 56899.000
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 251| 1 0 1 28 14 -4 .09 9 8 | -968 -287 14 100
emr 80| -3 3 0 8 -16 6 .34 14 14 | 2892 1 15 121
esa 150| 0 0 -4 -20 7 0 -.31 12 12 | -2479 3286 9 140
gfz 196| -1 0 4 -13 -9 -2 .16 13 12 | -664 773 16 150
grg 174| 4 0 -7 1 24 -8 .30 20 18 | -101 16 17 134
igr n/a| 0 0 0 -7 -12 -20 -.16 6 5 | 5853 -245 17 111
jpl 80| -2 -1 -2 -41 22 -21 .07 13 12 | 2350 107 16 127
mit 350| 3 -3 -1 -21 -70 32 .07 16 14 | -340 194 26 197
ngs 222| 0 0 3 32 32 -5 -.09 12 11 | -1124 113 1220 2859
sio 524| -1 0 -1 -1 -29 -7 -.60 14 15 | --- --- --- ---
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 3.1807.0 GPS week: 1807 Day: 0 MJD: 56893.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 13 9 14 18 12 5 11 17 15 9 4 | 29 29 31 29 24 30 31 35 32 32 29
2E | 7 12 9 13 19 7 11 12 7 11 4 | 22 22 17 24 21 16 20 26 21 17 18
4E | 17 17 11 15 15 8 15 31 14 16 6 | 211 211 210 209 206 208 210 208 208 209 208
5 | 18 13 16 19 16 5 13 15 10 11 5 | 27 36 32 25 30 22 31 21 28 24 26
6E | 12 12 16 13 86 6 12 12 13 14 5 | 33 28 33 29 47 28 29 28 33 28 29
7 | 18 18 9 11 19 5 17 11 8 13 5 | 30 33 22 32 37 23 28 26 26 20 24
8E | 17 15 14 12 15 7 15 21 18 20 6 | 106 105 105 103 106 104 107 109 106 110 105
X9 | 28 14 14 --- --- 12 --- 12 26 --- 10 | 40 24 25 --- --- 33 --- 20 23 --- 31
10 | 8 8 13 9 15 2 7 11 7 12 3 | 20 23 20 24 25 18 21 21 24 16 20
11 | 8 8 11 8 21 4 9 16 11 7 4 | 19 21 15 20 34 15 18 21 22 17 18
12 | 10 12 12 14 21 7 13 18 9 16 5 | 20 24 15 23 31 15 19 25 21 13 17
13 | 15 13 14 13 14 4 10 11 10 14 4 | 33 33 23 34 37 25 31 23 28 23 27
14 | 13 11 14 18 16 5 12 12 9 18 4 | 28 28 22 30 29 22 26 32 28 26 25
15 | 14 12 16 15 15 5 14 17 12 20 5 | 26 29 22 35 30 20 26 29 28 26 25
16 | 23 16 13 18 17 5 17 22 13 17 6 | 24 22 14 24 23 11 20 20 17 14 13
17 | 18 11 14 20 17 7 11 13 10 27 5 | 30 28 21 36 34 23 25 27 24 23 22
18 | 12 12 15 19 15 6 14 18 11 12 5 | 22 27 17 32 28 20 25 30 23 17 21
19 | 15 15 14 12 16 4 13 13 9 19 5 | 19 24 15 19 28 14 20 19 17 19 15
20 | 12 15 12 16 19 6 13 12 10 16 5 | 32 29 30 39 35 31 30 33 31 31 30
21E | 10 10 10 13 16 4 11 14 15 9 4 | 22 23 18 23 24 18 20 27 22 17 19
22 | 13 17 15 20 13 5 16 16 12 11 5 | 28 35 24 42 38 28 32 39 36 25 31
23 | 17 11 14 12 15 4 10 12 11 15 4 | 27 24 19 24 24 15 20 19 20 13 18
24 | 9 10 14 10 13 5 10 11 10 10 3 | 23 21 24 23 26 17 22 19 20 14 20
25 | 9 11 15 10 13 5 14 13 12 11 4 | 17 25 21 17 24 14 25 22 22 15 18
26 | 9 7 11 12 14 6 7 17 9 12 4 | 24 26 21 33 29 22 22 27 23 22 23
X27 | 13 12 13 9 --- 4 11 17 10 10 4 | 23 23 22 23 --- 17 28 19 22 16 20
28 | 14 10 13 16 17 6 12 12 9 16 4 | 24 24 19 32 33 20 24 24 19 17 20
29 | 10 14 14 18 19 7 16 10 13 18 5 | 26 33 29 26 28 23 32 28 30 26 25
X30E | 21 10 13 13 --- 5 10 13 10 7 5 | 67 64 66 67 --- 62 66 62 65 62 64
31 | 20 14 10 14 21 10 22 15 12 15 5 | 22 27 16 24 30 23 26 25 27 17 20
32 | 13 12 10 14 15 5 12 12 10 14 4 | 19 22 19 20 20 16 22 20 18 18 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 13 13 15 23 6 13 15 11 15 |T 35 36 31 37 38 30 35 34 34 30 32
WRMS | 14 13 13 13 17 5 12 13 10 14 |NE 25 27 21 27 29 20 25 24 24 19 21
MEDI | 13 12 14 13 16 5 12 13 10 14 |MD 26 27 22 26 29 22 25 26 24 19 22
Table 3.1807.1 GPS week: 1807 Day: 1 MJD: 56894.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 9 12 13 17 36 6 12 37 13 11 6 | 74 71 73 74 64 72 73 68 75 73 71
2E | 8 12 7 11 23 6 12 15 13 12 4 | 23 25 19 22 24 17 18 27 23 19 20
4E | 12 23 10 15 19 8 14 34 16 19 6 | 226 226 226 226 228 228 226 233 230 227 227
5 | 8 13 15 11 19 6 10 17 11 10 4 | 20 31 22 20 26 17 24 19 24 14 20
6E | 9 11 14 13 47 8 10 14 13 12 5 | 24 24 27 22 24 20 22 23 24 20 21
7 | 8 15 7 9 19 5 20 13 11 13 4 | 23 28 16 24 31 17 24 21 24 13 19
8E | 10 16 11 13 20 7 19 22 19 16 5 | 95 96 96 93 96 95 97 96 96 100 95
X9 | 18 13 17 20 --- 12 --- 9 14 --- 7 | 34 27 28 25 --- 34 --- 23 25 --- 31
10 | 4 8 11 10 18 6 7 12 10 13 3 | 21 23 19 20 21 17 21 21 19 19 18
11M | 8 10 12 7 23 5 10 13 8 11 4 | 23 22 16 19 31 18 20 20 24 18 18
12 | 9 10 10 16 20 6 13 19 16 12 4 | 20 27 15 20 26 13 21 22 21 16 16
13 | 10 11 13 13 21 5 11 11 10 16 4 | 19 29 20 22 30 18 26 16 24 18 19
14 | 9 11 12 16 13 5 11 15 13 19 4 | 22 28 24 24 21 22 27 26 27 20 22
15 | 11 11 15 14 13 3 12 18 11 17 4 | 18 27 18 27 20 15 22 20 25 19 18
16 | 11 17 12 19 20 4 15 20 11 15 5 | 19 23 16 23 22 13 19 20 16 15 14
17 | 10 11 14 17 20 7 13 15 12 24 5 | 22 28 16 27 29 16 23 25 21 20 17
18 | 8 16 13 17 15 6 15 19 11 14 5 | 17 26 20 24 22 17 24 22 24 15 17
19 | 10 15 12 18 22 6 16 13 11 18 5 | 19 27 17 20 26 14 22 16 18 17 14
20M | 10 17 12 13 20 6 13 27 9 13 5 | 45 39 44 42 42 41 43 44 46 48 42
21E | 7 11 8 14 31 6 10 12 13 10 4 | 23 26 21 27 31 20 22 20 26 22 20
22 | 9 19 12 20 16 6 15 16 12 10 5 | 23 31 22 34 30 25 29 30 32 20 24
23 | 10 10 14 13 20 5 11 11 10 17 4 | 18 23 17 18 19 13 19 16 20 11 15
24 | 9 12 14 11 14 5 12 15 13 10 4 | 23 23 24 21 24 17 23 19 21 16 19
25 | 10 12 11 9 12 5 12 17 14 11 4 | 18 27 22 19 24 16 25 20 20 19 18
26 | 7 10 10 9 17 4 7 15 10 12 3 | 16 22 13 22 21 14 18 18 22 16 15
X27 | 10 13 10 11 --- 6 14 19 10 14 4 | 19 21 18 21 --- 15 25 19 20 16 18
28 | 7 10 14 13 18 6 13 15 11 14 4 | 16 23 14 25 28 13 19 19 15 13 15
29 | 8 12 11 17 19 5 12 9 14 17 4 | 23 29 21 23 23 18 25 21 23 21 20
X30E | 7 9 13 7 --- 4 12 14 8 6 3 | 40 41 43 39 --- 38 38 33 41 36 38
31 | 10 13 9 18 32 5 22 15 15 16 5 | 21 26 13 24 36 16 25 22 23 15 17
32M | 7 8 10 12 20 7 11 8 9 17 4 | 20 23 24 22 22 20 24 25 24 28 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 12 14 22 6 13 18 12 15 |T 33 36 31 34 37 29 34 33 34 30 30
WRMS | 9 13 12 13 19 5 12 15 11 15 |NE 20 26 18 23 25 17 23 20 22 16 18
MEDI | 9 12 12 13 20 6 12 15 11 13 |MD 22 27 20 23 26 17 24 21 24 19 19
Table 3.1807.2 GPS week: 1807 Day: 2 MJD: 56895.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 12 13 13 16 5 9 13 13 7 4 | 31 32 35 35 35 32 35 30 35 35 33
2E | 7 11 10 12 16 6 12 14 9 10 4 | 24 27 24 26 23 20 21 25 22 16 21
4E | 18 22 14 23 21 11 16 31 22 25 7 | 165 169 166 168 172 169 169 178 172 173 170
5 | 9 12 15 12 18 5 12 15 8 13 4 | 22 33 27 22 30 20 29 22 24 20 23
6E | 11 11 15 13 49 7 11 14 8 11 5 | 26 23 28 24 22 19 24 24 24 19 21
7 | 9 16 7 11 18 4 18 14 10 15 4 | 22 25 13 24 30 18 25 19 24 17 18
8E | 10 18 13 13 17 7 17 21 17 17 5 | 82 83 79 78 82 76 81 87 79 78 79
X9 | 22 14 14 12 --- 10 --- 13 15 --- 7 | 29 25 23 22 --- 23 --- 20 20 --- 23
10 | 12 8 14 9 15 5 8 12 9 12 4 | 21 21 18 19 20 14 17 19 20 17 16
11 | 8 7 13 9 23 4 9 15 13 6 4 | 19 20 12 20 32 12 17 17 22 14 16
12 | 9 13 10 16 21 5 14 13 10 17 4 | 22 28 17 24 28 14 20 22 20 19 17
13 | 9 12 13 15 19 6 11 9 11 16 4 | 23 28 18 26 31 19 26 19 19 21 20
14 | 13 12 13 18 17 5 13 15 17 18 5 | 23 24 19 21 22 16 23 25 26 17 19
15 | 10 13 15 13 16 4 12 14 11 14 4 | 23 24 19 29 26 16 21 22 23 20 19
16 | 10 15 9 18 24 4 12 19 16 16 5 | 15 23 14 19 26 11 19 20 19 13 13
17 | 11 12 16 13 18 7 14 14 10 26 5 | 25 30 19 27 32 18 24 26 23 23 19
18 | 12 17 14 17 19 4 12 16 13 14 5 | 24 24 18 25 24 16 22 25 17 15 18
19 | 10 14 12 14 19 8 12 15 10 21 5 | 17 24 16 19 26 14 20 17 14 19 13
20 | 10 13 14 15 24 5 13 12 11 15 5 | 28 27 23 31 32 24 25 26 25 23 24
21E | 8 13 9 12 18 4 10 8 14 9 4 | 25 24 23 29 30 20 21 21 27 22 21
22 | 10 15 13 17 16 3 15 15 11 11 4 | 26 30 21 32 32 23 26 31 24 19 24
23 | 9 10 13 15 15 6 12 11 9 16 4 | 19 22 16 21 22 14 21 17 16 10 15
24 | 5 10 14 8 17 5 13 11 12 12 4 | 20 21 26 21 24 17 21 20 17 18 18
25 | 10 10 13 12 15 5 12 10 10 12 4 | 24 28 23 20 25 16 27 19 20 20 21
26 | 6 9 13 7 15 4 7 10 13 13 3 | 20 20 15 23 24 17 17 19 23 18 17
X27 | 11 11 11 9 --- 7 14 21 10 13 4 | 20 21 20 21 --- 16 27 21 20 17 18
28 | 7 11 14 13 19 7 12 15 13 17 4 | 21 25 17 27 29 16 22 22 22 14 17
29 | 9 14 14 16 21 6 13 9 10 16 4 | 27 30 23 23 25 19 26 25 25 20 22
X30E | 10 14 14 6 --- 3 11 16 8 7 4 | 49 50 48 46 --- 46 50 45 49 46 46
31 | 7 14 6 17 30 5 23 16 14 16 5 | 20 25 13 25 37 18 27 24 30 17 19
32 | 10 9 10 14 22 8 7 14 10 16 4 | 19 23 21 23 26 17 22 20 21 26 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 13 14 21 6 13 15 12 15 |T 30 32 27 31 34 25 30 29 29 26 27
WRMS | 9 13 13 13 19 6 12 13 10 16 |NE 22 25 18 23 27 16 23 21 21 17 18
MEDI | 10 12 13 13 18 5 12 14 11 14 |MD 23 25 20 24 26 18 23 22 23 19 19
Table 3.1807.3 GPS week: 1807 Day: 3 MJD: 56896.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 12 11 10 17 4 12 16 13 7 4 | 43 44 45 45 40 43 46 46 44 43 43
2E | 9 13 8 11 20 7 19 13 10 11 4 | 26 28 23 27 26 21 23 28 29 20 23
4E | 17 20 10 17 22 9 16 27 13 24 6 | 221 219 219 216 213 216 219 222 218 218 218
5 | 8 14 13 14 19 4 14 12 13 14 4 | 26 33 28 24 30 22 29 22 29 24 24
6E | 7 11 13 12 47 8 10 10 15 12 5 | 25 28 28 25 23 22 26 25 27 23 23
7 | 9 16 8 10 18 4 18 12 11 14 4 | 25 27 16 26 31 18 24 22 23 16 19
8E | 15 18 12 17 21 7 17 20 11 18 5 | 153 151 154 148 153 150 153 152 152 152 151
X9 | 2 --- --- >>>> --- 362 --- --- --- --- 0 | 1 --- --- 1 --- 1 --- --- --- --- 1
10 | 15 12 10 11 19 4 14 11 10 15 4 | 23 18 17 20 19 16 18 20 21 18 16
11 | 6 7 9 9 23 5 9 12 12 7 3 | 24 25 18 21 34 16 22 21 25 18 20
12 | 8 17 12 14 20 6 15 10 12 13 4 | 22 29 18 23 27 15 22 21 22 15 18
13 | 10 14 13 14 19 4 12 9 10 16 4 | 23 31 20 29 31 20 26 21 18 20 21
14 | 14 11 13 19 11 4 11 16 9 16 4 | 25 29 21 25 26 22 26 31 23 21 23
15 | 11 13 14 12 17 6 13 13 9 15 4 | 25 30 20 28 29 17 23 27 21 20 21
16 | 13 16 11 18 21 3 15 16 13 17 5 | 19 27 20 24 23 13 21 22 17 20 16
17 | 10 12 14 15 20 5 14 14 13 25 5 | 26 31 21 34 33 20 24 28 24 22 22
18 | 11 19 14 17 18 4 12 16 12 12 5 | 23 31 20 31 29 21 26 28 19 18 21
19 | 9 15 11 13 20 4 14 13 12 17 4 | 19 28 17 21 27 13 23 21 18 19 17
20 | 12 14 13 15 22 4 15 13 10 12 4 | 38 34 34 39 34 33 35 34 34 35 33
21E | 11 12 8 10 12 6 10 7 11 9 3 | 19 21 16 21 22 16 17 17 18 20 17
22 | 10 14 15 17 17 3 12 17 12 9 4 | 26 33 23 35 34 26 29 35 24 22 26
23 | 10 12 12 13 18 4 12 10 12 17 4 | 20 25 17 24 20 14 20 18 18 12 15
24 | 14 9 13 10 17 8 14 10 12 11 4 | 24 23 26 22 26 19 22 20 23 20 20
25 | 9 10 12 10 16 5 12 11 9 10 3 | 22 26 23 22 25 16 27 21 21 21 21
26 | 6 9 12 6 16 6 6 9 7 11 3 | 20 23 18 25 26 19 16 20 21 16 18
X27 | 11 11 13 10 --- 5 12 20 10 11 4 | 21 25 21 21 --- 19 27 25 21 21 21
28 | 7 14 14 13 20 5 16 13 11 15 4 | 19 24 17 28 30 15 20 23 20 16 17
29 | 9 16 12 15 21 7 15 12 14 15 5 | 29 34 27 27 27 22 30 30 26 27 25
X30 | 6 10 13 8 --- 3 12 11 7 9 3 | 79 80 79 81 --- 76 79 75 77 76 78
31 | 7 14 10 18 26 5 20 15 9 14 5 | 17 28 14 25 36 15 26 24 25 17 19
32 | 10 12 9 11 20 8 8 14 8 14 4 | 26 29 27 27 25 25 26 26 25 27 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 12 14 21 6 14 14 11 15 |T 35 40 34 37 39 31 37 37 36 33 33
WRMS | 10 14 12 13 19 6 13 13 11 15 |NE 21 27 20 24 27 17 23 23 21 19 19
MEDI | 10 13 12 13 19 5 13 13 11 14 |MD 24 28 21 25 27 19 26 24 23 20 21
Table 3.1807.4 GPS week: 1807 Day: 4 MJD: 56897.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 14 13 11 17 6 11 18 16 7 4 | 23 25 22 20 18 18 23 28 18 21 19
2E | 9 13 7 11 21 7 12 13 10 9 4 | 25 24 19 23 20 18 17 24 22 17 20
4E | 12 28 17 15 22 11 16 29 19 23 7 | 107 112 105 104 103 101 108 114 105 109 105
5 | 8 13 14 8 19 5 11 13 9 13 4 | 23 30 26 21 29 19 25 21 22 18 21
6E | 9 10 13 11 47 10 10 14 14 12 5 | 25 26 27 24 22 23 23 23 24 24 23
7 | 8 17 11 11 19 5 18 11 11 12 4 | 24 30 19 24 30 18 25 22 25 16 20
8E | 13 19 13 17 18 8 16 20 19 21 6 | 97 105 102 100 102 101 103 103 99 104 101
X9 | 2 --- --- --- --- 52 --- --- --- --- 0 | 1 --- --- --- --- 1 --- --- --- --- 1
10 | 6 11 13 10 18 4 10 12 7 12 3 | 23 24 21 20 22 17 18 22 18 18 19
11 | 8 9 12 8 24 5 9 15 11 7 4 | 21 23 18 21 32 14 18 21 18 17 18
12 | 9 12 12 14 23 6 14 14 8 16 4 | 23 31 22 28 29 21 24 25 23 24 22
13 | 8 12 13 14 19 6 12 10 9 17 4 | 18 31 21 25 28 21 27 23 21 23 22
14 | 9 11 15 12 13 5 12 16 14 19 4 | 23 29 24 26 23 22 26 32 28 23 24
15 | 9 14 16 12 14 5 14 15 15 18 5 | 24 30 21 32 26 22 25 28 26 26 24
16 | 11 13 12 17 21 6 13 14 15 16 5 | 23 27 21 23 24 18 24 23 21 20 19
17 | 10 13 13 15 18 7 13 13 12 23 5 | 24 31 21 32 31 21 24 28 22 21 21
18 | 9 15 17 18 17 5 14 15 9 11 5 | 22 30 21 29 24 21 23 24 23 16 21
19 | 9 14 14 13 22 6 13 17 10 16 4 | 21 29 21 21 26 15 24 25 16 21 19
20 | 8 14 14 14 22 7 14 15 10 14 4 | 20 22 25 26 21 22 22 25 20 28 20
21E | 9 10 8 11 17 4 12 9 14 9 4 | 23 24 20 24 28 20 22 22 22 22 21
22 | 10 13 17 12 15 4 14 19 11 9 4 | 27 33 21 34 31 25 28 36 29 20 26
23 | 9 11 12 13 18 5 11 11 10 16 4 | 17 26 19 18 19 16 22 20 19 14 17
24 | 7 9 14 11 15 6 13 13 11 10 4 | 22 25 26 26 25 20 21 22 23 22 21
25 | 9 11 14 10 17 4 11 12 8 9 3 | 23 33 29 25 27 23 26 28 24 28 26
26 | 6 11 12 9 18 4 8 12 8 10 3 | 22 27 20 28 22 19 20 23 22 21 21
X27 | 11 10 15 10 --- 8 13 20 12 11 5 | 23 27 21 20 --- 20 30 26 24 18 22
28 | 8 16 13 13 18 5 13 14 9 14 4 | 23 26 19 26 30 18 23 24 20 17 20
29 | 8 15 16 12 22 6 16 14 11 15 5 | 30 35 29 29 29 26 31 31 31 28 28
X30 | 8 12 13 12 --- 5 11 17 9 9 4 | 46 49 50 47 --- 47 50 40 48 47 47
31 | 9 13 10 15 30 6 17 14 13 13 5 | 19 29 18 26 35 19 25 23 25 20 20
32 | 9 10 10 11 20 7 9 14 9 14 4 | 18 21 19 17 17 14 19 20 19 21 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 13 13 21 6 13 15 12 14 |T 27 33 28 30 31 25 29 30 28 27 26
WRMS | 9 14 13 13 19 6 13 14 10 16 |NE 21 29 22 25 26 19 24 25 23 20 20
MEDI | 9 13 13 12 18 6 13 14 11 13 |MD 23 29 21 25 26 20 24 24 22 21 21
Table 3.1807.5 GPS week: 1807 Day: 5 MJD: 56898.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 5 10 12 10 14 4 12 17 14 8 4 | 38 39 39 39 35 37 41 43 39 37 38
2E | 6 11 8 11 20 7 13 14 12 7 4 | 27 27 25 28 26 24 22 27 31 20 25
4E | 13 16 12 15 17 10 16 31 15 21 6 | 207 212 206 207 211 207 212 216 210 210 209
5 | 9 14 13 15 20 6 14 15 10 10 4 | 26 33 25 25 33 22 28 25 28 21 25
6E | 7 14 13 16 48 6 12 15 14 10 5 | 25 26 27 25 24 21 24 23 28 25 24
7 | 8 13 8 11 19 4 17 11 9 13 4 | 21 27 16 24 30 18 22 20 22 15 19
8E | 11 20 13 15 18 7 16 21 15 19 5 | 131 133 134 130 133 131 134 137 133 135 133
X9 | 2 --- --- --- --- 71 --- --- --- --- 0 | 1 --- --- --- --- 1 --- --- --- --- 1
10 | 6 9 13 10 17 4 9 11 11 12 3 | 23 24 22 20 23 18 19 23 24 21 21
11 | 7 7 11 7 25 5 12 14 10 8 4 | 21 23 15 22 35 16 21 18 24 16 19
12 | 8 13 12 16 18 6 13 16 11 17 4 | 20 27 15 23 27 14 18 21 21 18 16
13 | 6 11 13 13 18 4 9 8 11 16 4 | 20 30 20 22 28 17 25 22 20 22 21
14 | 10 10 14 18 12 3 11 19 10 17 4 | 17 24 20 23 19 15 23 25 19 13 17
15 | 9 12 14 13 12 5 13 15 14 16 4 | 25 28 20 28 23 18 21 23 19 20 21
16 | 10 14 11 17 22 8 13 15 13 16 5 | 16 24 16 21 25 15 20 19 22 14 15
17 | 10 14 12 17 18 5 12 13 12 24 5 | 24 29 18 28 29 17 23 24 19 18 18
18 | 8 14 16 19 18 6 12 16 9 12 5 | 22 31 21 28 26 22 27 21 25 15 21
19 | 9 15 12 15 22 5 12 15 11 18 5 | 19 28 17 19 25 13 22 21 15 17 16
20 | 11 20 13 13 20 5 14 15 11 11 5 | 30 35 29 33 32 29 32 32 32 31 29
21E | 8 13 10 9 36 4 11 10 11 9 4 | 20 27 19 23 27 16 22 16 18 18 18
22 | 8 13 16 18 17 6 13 21 9 10 5 | 21 31 19 26 30 21 28 31 22 15 21
23 | 9 11 12 11 16 5 11 10 14 17 4 | 19 25 18 17 17 14 20 18 21 13 16
24 | 6 13 12 14 12 4 11 13 11 11 4 | 22 24 27 27 25 19 21 20 21 21 21
25 | 9 13 14 10 14 6 12 12 10 8 4 | 24 33 25 25 26 19 24 23 23 21 23
26 | 6 11 11 10 14 5 7 15 13 10 3 | 20 22 19 23 21 18 16 19 21 16 18
X27 | 8 13 15 10 --- 6 13 16 11 12 4 | 22 23 19 18 --- 17 28 20 23 19 20
28 | 7 12 11 14 20 5 14 15 12 15 4 | 15 23 15 24 28 13 20 19 16 14 14
29 | 10 14 14 12 17 6 11 18 10 14 4 | 26 31 25 25 26 21 27 27 25 21 23
X30 | 6 14 13 8 --- 4 13 15 8 9 4 | 38 42 42 41 --- 38 42 37 44 37 39
31 | 9 11 10 15 27 5 18 18 11 11 5 | 15 26 14 23 34 14 25 24 23 14 17
32 | 8 9 10 11 19 6 10 12 13 16 4 | 22 26 25 26 26 22 27 26 26 30 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 12 14 21 6 13 16 12 14 |T 31 37 31 34 37 28 34 34 33 30 30
WRMS | 9 13 12 13 18 5 12 14 11 14 |NE 19 27 19 23 26 16 22 22 21 17 18
MEDI | 8 13 12 13 18 5 12 15 11 12 |MD 22 27 20 25 26 18 23 23 23 19 21
Table 3.1807.6 GPS week: 1807 Day: 6 MJD: 56899.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 14 13 8 14 5 12 18 15 11 4 | 36 35 43 40 39 36 38 40 40 41 38
2E | 10 13 7 9 17 6 11 14 13 8 4 | 30 33 25 30 26 25 25 29 28 21 26
4E | 9 21 10 17 16 8 15 31 11 21 6 | 211 211 210 207 215 208 211 223 205 213 211
5 | 9 13 14 8 20 4 13 16 13 14 4 | 30 38 31 28 36 27 33 28 30 24 29
6E | 9 15 11 14 49 7 12 15 10 10 6 | 29 31 30 28 24 23 29 30 29 25 27
7 | 7 14 7 13 16 6 17 12 12 13 4 | 25 28 17 27 29 18 22 22 23 15 20
8E | 11 16 11 14 16 10 15 20 12 16 5 | 142 141 142 138 142 139 141 145 138 141 140
X9 | 12 15 14 19 --- 10 --- 13 13 --- 6 | 1 8 10 1 --- 1 --- 3 4 --- 1
10 | 8 10 12 11 14 6 10 18 8 10 4 | 27 26 21 25 23 21 25 29 22 22 23
11 | 6 9 11 9 24 5 10 14 9 10 4 | 23 26 17 24 39 17 22 20 23 18 20
12 | 9 14 9 15 19 7 14 18 14 19 5 | 23 29 17 27 31 16 23 22 18 19 18
13 | 10 13 13 10 18 4 11 8 12 15 4 | 30 33 23 31 33 24 29 25 25 24 26
14 | 10 10 13 11 12 6 12 17 10 15 4 | 25 31 26 30 29 25 30 33 29 25 26
15 | 9 12 13 11 11 5 15 17 16 15 4 | 28 31 23 33 31 22 27 30 29 26 26
16 | 9 15 13 19 23 5 13 15 11 14 5 | 21 29 17 28 29 17 24 22 19 16 18
17 | 9 17 12 16 18 6 12 12 11 24 5 | 25 32 20 35 33 21 25 28 18 22 21
18 | 6 14 15 17 17 5 11 16 11 16 4 | 27 32 23 37 31 27 28 29 30 18 26
19 | 9 16 13 13 22 6 13 12 10 18 4 | 21 33 19 24 34 16 26 22 20 19 20
20 | 10 19 13 13 17 5 14 15 12 10 4 | 30 33 27 37 35 29 28 32 30 28 29
21E | 9 16 9 11 22 4 11 10 12 9 4 | 24 27 18 27 24 19 25 21 25 21 21
22 | 11 14 14 17 16 5 13 20 12 10 5 | 32 38 27 44 39 32 32 42 35 24 32
23 | 9 12 13 10 18 4 10 8 12 15 4 | 22 28 19 23 21 17 23 21 21 14 19
24 | 9 10 11 9 11 5 14 17 12 13 4 | 25 26 28 27 26 21 23 21 21 23 23
25 | 8 13 14 8 14 6 12 12 13 11 4 | 23 33 25 26 30 18 25 21 16 20 22
26 | 8 11 9 10 14 4 8 19 14 12 4 | 25 26 22 28 29 22 21 25 22 23 23
X27 | 6 11 16 11 --- 5 12 14 11 12 4 | 28 31 23 25 --- 22 32 26 26 22 25
28 | 6 15 12 14 18 5 12 11 12 13 4 | 20 24 18 28 31 18 21 25 20 16 18
29 | 9 14 15 13 16 8 12 24 9 18 5 | 33 39 32 31 34 29 35 35 35 30 31
X30 | 5 17 11 13 --- 5 11 12 9 9 4 | 61 61 61 63 --- 58 60 56 59 58 59
31 | 7 12 11 16 27 4 16 16 15 10 5 | 21 29 17 29 38 19 25 26 24 18 21
32 | 8 12 11 13 17 3 8 12 9 15 4 | 22 27 23 22 26 19 23 23 24 27 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 12 13 20 6 13 16 12 14 |T 36 40 34 38 41 32 37 37 35 33 34
WRMS | 8 14 12 12 18 5 12 14 11 15 |NE 24 29 21 27 30 20 26 25 23 21 22
MEDI | 9 14 12 13 17 5 12 15 12 13 |MD 25 31 23 28 31 22 25 26 25 22 23
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 4.1807 GPS week: 1807 MJD: 56893.0-56899.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2946 |U 8 8 18 |U 5 6 21 |U 9 9 22 |
emr | emr 2926 | 9 9 21 |U 6 7 26 | 9 10 23 |
esa | esa 2934 | 9 9 19 |U 6 6 26 | 10 10 23 |
gfz | gfz 2923 |U 9 9 19 |U 6 8 25 |U 9 9 22 |
grg | grg 2688 | 10 10 27 |U 13 16 70 |U 10 11 22 |
igr | igr 2941 | 8 8 18 | 5 5 22 | 9 9 22 |
igs | igs 2931 | 8 8 18 | 5 6 25 | 9 9 22 |
jpl | jpl 2873 | 9 9 20 |U 6 7 26 |U 10 10 23 |
mit | mit 2934 | 8 8 20 |U 7 8 33 |U 9 9 21 |
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 5.1807.0 GPS week: 1807 Day: 0 MJD: 56893.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2972 | 6 6 13 | 5 5 19 | 7 9 18 |
emr | emr 2968 | 8 6 17 | 9 7 28 | 7 7 20 |
esa | esa 2976 | 8 7 16 | 7 6 26 | 8 6 22 |
gfz | gfz 2872 | 9 8 16 | 9 16 30 | 7 7 18 |
grg | grg 2688 | 10 8 25 | 15 24 75 | 7 8 21 |
igr | igr 2958 | 7 6 13 | 6 5 23 | 7 6 18 |
igs | igs 2972 | 7 6 14 | 6 6 25 | 6 6 18 |
jpl | jpl 2872 | 9 7 14 | 7 6 26 | 8 7 18 |
mit | mit 2976 | 9 7 16 | 8 8 41 | 7 8 19 |
Table 5.1807.1 GPS week: 1807 Day: 1 MJD: 56894.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 5 12 | 4 6 20 | 7 7 19 |
emr | emr 2968 | 8 6 17 | 6 6 23 | 7 9 21 |
esa | esa 2976 | 9 7 12 | 6 6 29 | 8 9 21 |
gfz | gfz 2968 | 10 9 15 | 6 6 25 | 7 7 18 |
grg | grg 2688 | 7 6 22 | 15 25 71 | 7 12 21 |
igr | igr 2976 | 8 8 12 | 5 5 22 | 7 8 19 |
igs | igs 2915 | 7 6 12 | 5 5 22 | 7 9 19 |
jpl | jpl 2872 | 9 8 16 | 7 5 23 | 7 8 22 |
mit | mit 2976 | 8 5 13 | 7 8 39 | 7 9 16 |
Table 5.1807.2 GPS week: 1807 Day: 2 MJD: 56895.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 11 19 | 4 5 23 | 8 12 19 |
emr | emr 2968 | 9 11 25 | 7 7 31 | 9 12 20 |
esa | esa 2976 | 8 12 20 | 6 5 28 | 10 13 21 |
gfz | gfz 2968 | 8 11 20 | 6 6 28 | 9 11 22 |
grg | grg 2688 | 13 13 28 | 12 13 75 | 9 12 21 |
igr | igr 2976 | 8 10 18 | 5 4 21 | 9 12 22 |
igs | igs 2972 | 8 10 19 | 6 5 31 | 9 11 20 |
jpl | jpl 2872 | 9 9 20 | 7 7 28 | 9 11 21 |
mit | mit 2976 | 9 9 20 | 9 6 39 | 8 11 21 |
Table 5.1807.3 GPS week: 1807 Day: 3 MJD: 56896.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 6 6 17 | 5 8 23 | 13 8 26 |
emr | emr 2864 | 7 9 20 | 7 8 29 | 14 9 28 |
esa | esa 2880 | 6 10 19 | 6 7 28 | 15 9 28 |
gfz | gfz 2945 | 6 7 15 | 5 8 27 | 14 9 26 |
grg | grg 2688 | 8 7 23 | 10 16 66 | 13 8 22 |
igr | igr 2941 | 6 8 16 | 5 7 25 | 14 9 26 |
igs | igs 2953 | 6 8 17 | 6 8 30 | 13 8 25 |
jpl | jpl 2872 | 7 9 21 | 7 8 30 | 15 10 27 |
mit | mit 2880 | 7 8 16 | 7 11 36 | 12 7 24 |
Table 5.1807.4 GPS week: 1807 Day: 4 MJD: 56897.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 8 10 21 | 5 5 19 | 8 9 26 |
emr | emr 2872 | 8 12 22 | 5 7 22 | 8 9 26 |
esa | esa 2880 | 9 10 25 | 5 5 22 | 9 10 26 |
gfz | gfz 2873 | 9 10 24 | 5 6 17 | 8 7 26 |
grg | grg 2688 | 11 14 31 | 11 11 69 | 10 11 26 |
igr | igr 2880 | 9 11 22 | 4 4 17 | 9 9 25 |
igs | igs 2877 | 8 11 23 | 5 5 19 | 8 9 26 |
jpl | jpl 2872 | 9 12 22 | 5 6 18 | 9 10 27 |
mit | mit 2880 | 8 10 22 | 6 8 26 | 8 8 25 |
Table 5.1807.5 GPS week: 1807 Day: 5 MJD: 56898.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 10 8 26 | 7 7 22 | 10 13 19 |
emr | emr 2876 | 10 10 27 | 6 7 27 | 11 14 23 |
esa | esa 2880 | 9 8 23 | 7 7 28 | 11 13 21 |
gfz | gfz 2873 | 10 8 24 | 7 8 23 | 11 12 20 |
grg | grg 2688 | 11 9 30 | 14 14 64 | 12 13 18 |
igr | igr 2880 | 10 7 23 | 6 6 24 | 11 12 21 |
igs | igs 2877 | 9 8 25 | 6 8 25 | 11 12 21 |
jpl | jpl 2876 | 9 8 27 | 7 8 30 | 11 13 24 |
mit | mit 2880 | 9 8 28 | 8 9 27 | 9 11 17 |
Table 5.1807.6 GPS week: 1807 Day: 6 MJD: 56899.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 10 8 21 | 4 6 20 | 9 8 24 |
emr | emr 2972 | 11 8 20 | 4 8 20 | 10 10 24 |
esa | esa 2976 | 11 9 22 | 5 8 23 | 10 9 22 |
gfz | gfz 2968 | 11 8 21 | 5 8 21 | 10 8 23 |
grg | grg 2688 | 11 13 32 | 14 13 70 | 12 11 29 |
igr | igr 2976 | 10 9 22 | 4 7 21 | 10 8 22 |
igs | igs 2954 | 10 8 20 | 4 7 20 | 10 8 23 |
jpl | jpl 2876 | 12 8 21 | 5 8 25 | 10 9 24 |
mit | mit 2976 | 10 8 23 | 6 9 24 | 10 9 28 |
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 6.1807 GPS week: 1807 MJD: 56893.500-56899.500
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 | -42 -31 103 -89 -1 | 23 29
| 12 14 76 76 6 | 4
emr uuuuu | 63 -30 26 218 10 | 56 60
| 19 8 51 87 18 | 4
esa uuuuu | 7 -1 -35 103 -1 | 16 23
| 8 12 50 79 4 | 3
gfz uuuuu | 8 -10 43 -118 -3 | 15 23
| 17 26 81 179 5 | 3
grg uuuuu | -10 1 -67 -140 -3 | 59 62
| 15 18 149 30 8 | 1
igr xxxxx | 5 -10 -10 109 0 | -1 19
| 14 15 78 43 5 | 3
irf xxxxx | 19 -2 -23 138 4 | -1 17
| 9 13 36 62 3 | 4
jpl uuuuu | -11 20 66 174 -4 | 37 47
| 16 28 80 86 12 | 3
mit uuuuu | 2 18 -234 -242 7 | 22 28
| 22 27 59 84 3 | 4
ngs uuuuu | -32 34 -19 -91 0 | 9 20
| 31 50 85 185 12 | 3
sio uuuux | 44 15 -13 160 -4 | 48 51
| 22 17 38 68 4 | 2
Table 7.1807.0 GPS week: 1807 Day: 0 MJD: 56893.500
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 -45 -60 -52 -4 | 20 27
emr uuuuu | 28 -28 58 57 -21 | 56 59
esa uuuuu | 11 2 -9 180 -1 | 13 22
gfz uuuuu | 23 -25 78 204 -6 | 13 22
grg uuuuu | -2 -11 125 -172 -9 | 58 61
igr xxxxx | -1 -9 29 136 1 | -5 19
irf xxxxx | 15 -26 41 101 6 | -5 17
jpl uuuuu | -24 66 177 70 15 | 32 44
mit uuuuu | 0 -21 -220 -165 6 | 19 25
ngs uuuuu | -24 46 -140 -199 4 | 9 21
sio uuuux | 48 -6 54 117 -4 | 49 52
Table 7.1807.1 GPS week: 1807 Day: 1 MJD: 56894.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -18 -24 138 28 -6 | 20 27
emr uuuuu | 72 -25 -21 212 6 | 52 56
esa uuuuu | 21 4 3 154 -2 | 13 22
gfz uuuuu | 36 -28 88 12 -4 | 12 22
grg uuuuu | 18 5 -165 -151 11 | 57 60
igr xxxxx | 13 -4 104 118 1 | -5 19
irf xxxxx | 14 -10 -26 75 6 | -5 17
jpl uuuuu | -38 6 41 161 -2 | 35 45
mit uuuuu | -39 -3 -249 -238 4 | 19 25
ngs uuuuu | -81 87 -65 -419 4 | 6 18
sio uuuux | 44 -7 -14 90 -12 | 48 51
Table 7.1807.2 GPS week: 1807 Day: 2 MJD: 56895.500
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 -5 157 -68 2 | 21 28
emr uuuuu | 79 -35 13 205 6 | 52 57
esa uuuuu | 6 -9 -18 182 -1 | 15 23
gfz uuuuu | -3 -27 136 -68 -1 | 14 23
grg uuuuu | -20 -25 39 -152 -11 | 60 63
igr xxxxx | -24 12 21 58 4 | -3 20
irf xxxxx | 6 -8 -39 49 4 | -3 19
jpl uuuuu | -2 3 -38 134 -11 | 36 47
mit uuuuu | -10 -3 -322 -311 7 | 20 27
ngs uuuuu | -7 67 -26 -54 -1 | 8 20
sio uuuux | 16 15 -28 63 -5 | 47 50
Table 7.1807.3 GPS week: 1807 Day: 3 MJD: 56896.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -41 -34 95 -134 11 | 21 28
emr uuuuu | 62 -37 -4 248 34 | 54 58
esa uuuuu | 5 -17 8 31 3 | 15 24
gfz uuuuu | 9 -38 103 -274 1 | 15 23
grg uuuuu | -22 -1 100 -166 0 | 59 62
igr xxxxx | 3 -37 -1 52 1 | -2 20
irf xxxxx | 19 4 -24 182 4 | -2 18
jpl uuuuu | 7 -8 49 109 -6 | 35 47
mit uuuuu | 24 28 -213 -126 8 | 20 27
ngs uuuuu | -59 79 -79 89 -16 | 8 20
sio uuuux | 42 27 -16 207 0 | 46 49
Table 7.1807.4 GPS week: 1807 Day: 4 MJD: 56897.500
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 | -56 -25 154 -189 -6 | 25 31
emr uuuuu | 80 -38 64 350 7 | 58 63
esa uuuuu | 8 -10 -17 -12 -8 | 17 25
gfz uuuuu | -14 -2 28 -286 -10 | 18 24
grg uuuuu | -25 30 -232 -113 -11 | 60 63
igr xxxxx | 16 -15 -34 122 -12 | 0 19
irf xxxxx | 34 11 -58 212 0 | 1 17
jpl uuuuu | -15 47 63 166 -25 | 38 48
mit uuuuu | 9 51 -292 -191 3 | 23 29
ngs uuuuu | -28 -43 9 107 17 | 8 20
sio uuuux | 80 40 -50 240 -7 | 48 51
Table 7.1807.5 GPS week: 1807 Day: 5 MJD: 56898.500
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 | -47 -44 140 -162 -3 | 25 31
emr uuuuu | 69 -29 -30 243 9 | 57 62
esa uuuuu | -2 13 -122 46 0 | 17 24
gfz uuuuu | 3 30 -54 -178 -7 | 17 24
grg uuuuu | -11 16 -166 -135 -3 | 58 60
igr xxxxx | 10 -12 -37 103 1 | 0 19
irf xxxxx | 27 9 -58 177 1 | 2 18
jpl uuuuu | -7 0 166 304 -3 | 37 47
mit uuuuu | 23 33 -196 -327 7 | 24 30
ngs uuuuu | -40 18 76 -2 5 | 10 23
sio uuuux | 55 12 -53 203 -2 | 48 50
Table 7.1807.6 GPS week: 1807 Day: 6 MJD: 56899.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -44 -40 95 -47 2 | 29 32
emr uuuuu | 47 -17 106 213 27 | 63 66
esa uuuuu | -1 12 -90 137 -1 | 21 25
gfz uuuuu | -2 19 -75 -234 3 | 20 24
grg uuuuu | -6 -6 -166 -88 4 | 61 63
igr xxxxx | 14 -7 -149 176 0 | 5 14
irf xxxxx | 18 5 5 170 7 | 6 14
jpl uuuuu | 4 24 2 276 1 | 43 49
mit uuuuu | 6 42 -148 -335 13 | 30 32
ngs uuuuu | 11 -19 94 -157 -14 | 15 23
sio uuuux | 19 22 16 197 0 | 51 53
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