[IGSREPORT-22318] Wk 1767 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Dec 6 05:03:25 PST 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1767 (Nov 17, 2013 - Nov 23, 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:
igs1767[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1767[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1767[0-6].cls IGS GPS clock combination summary report.
igs17677.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17677.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 | MCM4 BRFT MCM4
0 | EMR | HERS
0 | ESA | TWTF CHPI TWTF
0 | GRG | IRKJ POLV USNO POLV
0 | JPL | CUSV
0 | MIT | 9 28 9 28 SCH2 ALIC MDVJ SCH2
1 | COD | DUBO HOLM
1 | EMR | HERS
1 | GFZ | HOLM
1 | GRG | DRAG FLIN KELY MONP POLV DRAG FLIN GUAM IRKJ KELY
1 | GRG | MONP POLV
1 | JPL | CUSV
1 | MIT | 1 2 6 7 9 19 31 1 2 6 7 9 19 26 27 31 BAKO MDVJ USNO
1 | MIT | BAKO MDVJ NRC1
2 | COD | ALIC POL2 TSKB ALIC
2 | EMR | HERS TSKB
2 | ESA | ALIC MATE ALIC MATE
2 | GFZ | CHUM NOVM RESO CHUM NOVM POL2 RESO
2 | GRG | DRAG FAA1 HYDE IRKJ KELY LPGS USNO DRAG FAA1 HYDE
2 | GRG | IRKJ KELY LPGS MCM4 USNO
2 | MIT | 3 9 17 22 27 28 3 9 17 22 27 28 BAKO DRAG HOB2 MDVJ
2 | MIT | TOW2 BAKO DRAG HOB2 MDVJ
3 | COD | BOR1 GRAZ HOB2 MCM4 BOR1
3 | EMR | HERS MATE HERS MATE MCM4
3 | ESA | BRAZ NTUS BRAZ LPGS NTUS TIXI
3 | GFZ | MATE NTUS MATE NTUS
3 | GRG | DRAG MCM4 POLV DRAG MCM4 POLV
3 | JPL | 17 CUSV MCM4 NKLG
3 | MIT | 1 2 7 9 21 22 23 28 31 1 2 3 6 7 9 21 22 23 28 31
3 | MIT | ALIC KOUR MDVJ NTUS PTBB ALIC BAKO KOUR MDVJ NTUS
3 | MIT | PTBB
4 | COD | FAA1 GUAT HOB2
4 | EMR | HERS
4 | GRG | BOGT FAA1 IRKJ JPLM KELY KOUR LPGS MONP BOGT FAA1
4 | GRG | IRKJ JPLM KELY KOUR MONP
4 | MIT | 6 7 9 18 26 31 9 18 22 JPLM MDVJ TIDB DRAG
5 | COD | ALIC HOB2 NKLG PTBB TOW2 YKRO NKLG
5 | EMR | HERS HERS
5 | ESA | ARTU DRAG ARTU DRAG
5 | GRG | 6 6 ALIC DRAG IRKJ MATE SPT0 USNO ZAMB ZIMM ALIC
5 | GRG | BUCU DRAG IRKJ MATE MONP SPT0 USNO ZAMB ZIMM
5 | MIT | 5 9 5 9 ALIC HOB2 PDEL PTBB SFER ALIC MDVJ MONP PDEL
5 | MIT | PTBB SFER TIDB
6 | COD | HOB2 NKLG
6 | EMR | 32 12 15 32 HERS MCM4 HERS MCM4
6 | ESA | 10 10 NKLG
6 | GFZ | HNLC NTUS
6 | GRG | 10 3 6 10 32 CRO1 DRAG IRKJ MONP NTUS CRO1 DRAG IRKJ
6 | GRG | MONP NKLG NTUS
6 | JPL | 12 15 25 CAS1
6 | MIT | 1 6 7 9 10 12 14 15 23 31 32 1 6 7 9 10 12 14 15
6 | MIT | 17 23 31 32 NTUS MDVJ NTUS
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | GRG | ~03:21 | ~ 0.15 ns
1 | GRG | ~23:58 | ~ 0.15 ns
1 | MIT | ~02:00 | ~ 0.05 ns
4 | MIT | ~22:30 | ~ 0.02 ns
6. 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.
7. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G29 | 2013_11_19 | 2013066
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 | -1.3 -.1 -1.2 -59 19 10 .10
EMR | 0 | 3.2 8.3 16.3 -29 14 -16 -.07
ESA | 0 | 3.7 5.1 .7 18 -26 46 -.08
GFZ | 0 | .0 .6 -1.8 -22 -64 24 .35
GRG | 0 | 2.0 8.8 -17.8 -2 29 -9 .46
JPL | 0 | -3.3 2.5 12.2 -94 -55 89 .10
MIT | 0 | 3.0 4.3 6.4 -35 22 -23 -.0
NGS | 0 | -2.1 1.4 14.9 -64 3 -21 .25
SIO | 0 | 2.3 5.0 47.5 147 167 241 .10
COD | 1 | -1.5 -.5 -1.0 -61 19 7 .15
EMR | 1 | -.4 4.6 13.0 -28 10 -16 -.16
ESA | 1 | 3.4 10.0 6.1 7 -50 65 -.25
GFZ | 1 | .3 .5 -.6 -34 -47 27 .06
GRG | 1 | -1.7 3.7 -21.0 -8 28 1 .26
JPL | 1 | -4.9 4.2 13.1 -38 10 86 -.03
MIT | 1 | .1 5.4 8.8 -22 23 -5 .04
NGS | 1 | 1.9 4.0 8.9 -40 -6 18 .45
SIO | 1 | 3.1 6.7 57.4 188 162 177 .19
COD | 2 | -1.2 -.7 -1.2 -64 3 18 -.10
EMR | 2 | -1.0 5.1 16.2 -20 21 -21 -.25
ESA | 2 | 3.0 7.0 2.5 15 -36 33 -.23
GFZ | 2 | .1 -.1 -.9 -33 -38 10 .14
GRG | 2 | -3.8 3.9 -18.0 -27 23 -22 .08
JPL | 2 | -.5 .1 13.9 -56 -6 -18 .09
MIT | 2 | -1.8 7.4 8.5 -26 17 -15 -.14
NGS | 2 | -.5 9.0 2.3 2 3 9 .25
SIO | 2 | 1.7 2.8 43.8 85 104 127 -.22
COD | 3 | .0 -.3 -1.1 -42 0 -22 .17
EMR | 3 | -.2 8.9 14.1 -19 20 -18 -.09
ESA | 3 | 7.3 12.1 1.1 10 -48 75 -.05
GFZ | 3 | .9 1.0 -1.2 -22 -51 5 .12
GRG | 3 | 2.4 4.5 -23.0 -10 -5 6 .10
JPL | 3 | 7.1 -3.6 15.3 -76 -34 -19 .31
MIT | 3 | 1.4 4.6 8.5 -34 13 -2 .13
NGS | 3 | .9 3.8 11.8 -48 -4 4 .48
SIO | 3 | 2.7 4.1 55.2 74 48 57 .10
COD | 4 | -.5 .2 -1.0 -28 -1 3 .10
EMR | 4 | 1.6 3.3 11.2 -40 17 -23 .31
ESA | 4 | 6.5 7.7 3.8 6 -51 60 -.09
GFZ | 4 | .5 .5 -1.2 -30 -44 16 .29
GRG | 4 | 1.8 8.7 -25.5 -23 17 -17 .25
JPL | 4 | 3.4 .5 17.0 -102 -25 -52 .29
MIT | 4 | 2.8 3.2 8.4 -16 -9 -19 .20
NGS | 4 | 3.0 3.1 4.0 -11 -2 16 .52
SIO | 4 | 2.3 -.3 58.5 107 106 26 -.07
COD | 5 | .2 .9 -1.2 -34 -13 13 .39
EMR | 5 | -2.3 9.3 16.3 -19 6 4 .20
ESA | 5 | 1.4 8.9 8.2 -19 -45 67 .20
GFZ | 5 | .3 .4 -1.2 -36 -53 36 .31
GRG | 5 | 2.0 7.0 -27.7 -16 34 -2 .42
JPL | 5 | 3.8 4.2 14.9 -87 -15 -52 .41
MIT | 5 | -2.9 4.4 3.5 -29 3 5 .43
NGS | 5 | -3.4 -.2 13.3 -70 18 -24 .64
SIO | 5 | 2.2 .5 60.5 51 108 -17 .27
COD | 6 | -.7 .5 -.8 -46 -10 -8 .25
EMR | 6 | 5.2 5.6 14.0 -9 16 -1 .23
ESA | 6 | 3.1 5.2 11.2 -10 -64 66 .21
GFZ | 6 | .3 .3 -1.1 -14 -54 27 .10
GRG | 6 | 2.2 10.3 -29.7 -14 14 -3 .26
JPL | 6 | 8.8 1.9 11.8 -84 22 -12 .17
MIT | 6 | .4 2.7 5.7 -17 -6 -14 .38
NGS | 6 | 6.8 .6 2.4 -18 -14 43 .60
SIO | 6 | 3.1 .3 72.1 75 116 -92 .20
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 1.1767.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1767.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 2.1767.[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 3.1767.[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 5.1767.0-6). 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 1767 summary. (Nov 17, 2013 - Nov 23, 2013)
Table 1.1767.a GPS week: 1767 MJD: 56613.000-56619.000
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 265| 1 0 4 0 14 -4 .10 9 9 | -792 -316 17 121
| 0 1 1 19 14 12 .03 | 416 588
emr 80| -1 0 7 -24 21 3 .14 14 14 | 1754 287 19 121
| 1 2 1 21 11 7 .05 | 697 1263
esa 150| 0 0 0 31 -13 9 -.19 5 5 | -1745 1626 9 114
| 0 0 0 14 19 13 .02 | 1297 1940
gfz 203| -1 0 -4 2 -10 3 -.01 10 10 | -195 151 12 72
| 0 1 0 14 10 11 .01 | 478 583
grg 193| 2 1 -13 -8 7 -6 .41 18 17 | -28 -125 19 134
| 0 2 4 21 80 17 .08 | 266 205
igr n/a| 0 0 0 6 18 -4 -.20 4 4 | 8403 159 14 76
| 0 0 0 6 13 12 .02 | 816 1335
jpl 80| -2 -1 1 -4 14 -18 .14 13 12 | 1060 406 16 146
| 1 1 1 13 23 31 .02 | 781 1480
mit 291| 0 0 -1 -2 -6 30 -.13 11 10 | -138 136 27 238
| 0 0 1 29 19 14 .03 | 225 178
ngs 245| 0 1 3 -72 -21 -44 .11 13 11 | -21367 30359 1757 3386
| 0 1 3 48 58 13 .05 | 54194 80836
sio 465| 1 0 3 70 154 52 -.59 18 18 | --- --- --- ---
| 0 0 1 41 41 121 .01 | --- ---
Table 1.1767.b GPS week : 1767 MJD: 56613.000-56619.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 4 4 4 4 4 5 5 |
4 | 4 3 3 3 4 4 4 |
5 | 5 4 5 4 5 4 4 |
6 | 4 4 4 3 4 4 5 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 3 3 4 4 |
9 | 3 3 3 3 3 4 3 |
10 | 4 4 4 4 4 4 7 |
11 | 5 4 4 4 4 4 4 |
12 | 5 5 5 5 5 6 6 |
13 | 4 4 4 4 4 3 4 |
14 | 4 4 4 4 4 4 4 |
15 | 5 5 5 5 5 6 5 |
16 | 5 5 5 5 4 5 5 |
17 | 4 5 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 5 5 5 5 4 5 6 |
20 | 5 4 4 4 4 5 4 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 3 4 4 4 4 |
23 | 5 4 4 4 4 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 3 4 4 3 4 4 |
27 | 4 5 6 4 4 4 4 |
28 | 4 4 4 5 4 4 4 |
29 | 4 4 0 5 5 5 5 |
31 | 5 5 5 4 4 4 4 |
32 | 4 3 3 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 2.1767.0 GPS week: 1767 Day: 0 MJD: 56613.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 266| 1 0 4 -14 6 10 .08 9 10 | -1249 440 18 117
emr 80| 0 -2 5 -26 0 1 .09 13 13 | 2296 -1071 15 122
esa 150| 0 0 0 51 4 -14 -.18 5 5 | -2592 2909 9 122
gfz 204| -1 0 -3 -4 -9 10 -.01 9 9 | -113 -21 10 65
grg 193| 2 1 -10 14 57 -12 .37 15 15 | -48 -166 17 112
igr n/a| 0 0 0 6 -2 -3 -.25 4 4 | 9465 -1312 13 73
jpl 80| 0 0 1 -9 -6 31 .17 13 13 | 1195 -1195 13 155
mit 299| 0 -1 -3 -10 26 19 -.13 11 10 | -253 349 22 250
ngs 250| -1 0 6 -154 -100 -51 .14 16 15 | -1178 353 1749 3523
sio 474| 2 0 4 107 206 228 -.59 18 17 | --- --- --- ---
Table 2.1767.1 GPS week: 1767 Day: 1 MJD: 56614.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 266| 1 3 6 -1 21 -14 .08 10 10 | -1067 249 21 126
emr 80| -3 -2 7 -26 14 2 .11 15 15 | 1511 -227 17 136
esa 150| 0 0 0 19 -7 9 -.16 5 5 | -1053 1197 9 136
gfz 203| -1 -2 -4 -1 -17 -6 -.00 10 10 | -78 -244 11 72
grg 194| 2 0 -10 -7 20 -18 .37 15 15 | 4 -141 15 138
igr n/a| 0 0 -1 0 15 -22 -.19 4 4 | 8501 -318 16 85
jpl 80| -1 -2 2 5 33 4 .15 13 13 | 430 -174 14 154
mit 299| 0 0 -2 -2 16 51 -.10 10 10 | 19 141 26 214
ngs 246| 0 1 0 -36 -39 -39 .19 11 9 | -1068 270 1754 3497
sio 477| 1 0 4 144 198 152 -.60 17 17 | --- --- --- ---
Table 2.1767.2 GPS week: 1767 Day: 2 MJD: 56615.000
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 267| 1 0 2 16 16 -7 .08 9 9 | -125 -1109 16 109
emr 80| -2 0 5 -52 20 -4 .23 14 14 | 1640 -380 17 110
esa 150| 1 0 0 34 12 7 -.22 5 5 | -2383 3033 8 88
gfz 205| 0 0 -2 13 -19 -9 -.02 10 9 | -158 605 15 84
grg 195| 1 -1 -8 -25 19 11 .33 14 15 | 359 -357 17 134
igr n/a| 0 0 0 11 13 14 -.19 4 4 | 8581 -403 14 73
jpl 80| -3 -1 -1 -4 14 -24 .12 13 13 | 940 -82 15 133
mit 299| 0 0 0 -8 -9 47 -.11 9 9 | 60 6 30 250
ngs 247| 0 2 2 -64 -77 -52 .11 13 12 | -144267 213677 1742 3062
sio 456| 1 -1 4 38 125 120 -.57 18 16 | --- --- --- ---
Table 2.1767.3 GPS week: 1767 Day: 3 MJD: 56616.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 266| 2 0 4 -29 35 -22 .13 9 9 | -397 -554 14 114
emr 80| -2 0 9 -46 30 -5 .17 15 15 | 968 1207 17 110
esa 150| 1 0 -1 25 -7 22 -.21 5 5 | -1396 595 9 123
gfz 203| 0 0 -4 -16 -10 17 -.02 11 10 | 324 -471 12 68
grg 193| 2 0 -14 -2 29 21 .32 15 15 | 49 -97 16 127
igr n/a| 0 0 0 4 37 0 -.20 4 4 | 7750 1035 15 68
jpl 80| -4 0 0 18 -20 -19 .15 13 12 | 565 1229 15 135
mit 299| 0 0 -1 8 -17 26 -.09 10 10 | -199 280 25 215
ngs 249| 0 0 6 -13 -14 -65 .09 13 12 | -411 -523 1934 3506
sio 456| 1 0 3 46 87 25 -.58 17 17 | --- --- --- ---
Table 2.1767.4 GPS week: 1767 Day: 4 MJD: 56617.000
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 264| 1 0 5 28 -6 6 .08 10 10 | -828 -241 17 127
emr 80| -1 -2 7 -18 20 14 .18 14 14 | 2456 -1044 15 121
esa 150| 1 0 -1 47 -26 15 -.19 5 5 | -1189 -267 9 117
gfz 204| -1 1 -5 25 -21 -2 -.00 10 10 | 61 -231 10 68
grg 192| 0 2 -13 -18 49 -15 .44 16 16 | 134 -300 17 140
igr n/a| 0 0 0 5 13 7 -.19 4 4 | 9013 -1350 14 75
jpl 80| -2 -2 1 -12 8 -37 .14 13 12 | 2172 -1314 15 150
mit 299| 0 0 0 -39 -14 33 -.12 11 10 | 141 -83 27 238
ngs 243| 0 0 3 -109 45 -45 .10 11 10 | -813 -253 1578 3216
sio 469| 0 0 5 54 164 18 -.58 18 18 | --- --- --- ---
Table 2.1767.5 GPS week: 1767 Day: 5 MJD: 56618.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 265| 1 1 4 -1 2 -7 .12 9 8 | -1174 -37 16 127
emr 80| 0 0 8 -10 35 12 .13 15 15 | 859 1916 16 123
esa 150| 0 0 -2 13 -25 23 -.18 6 5 | -3809 4596 8 115
gfz 203| -1 -1 -5 -8 1 17 -.03 9 9 | -1204 1207 10 69
grg 193| 3 2 -14 21 45 -8 .52 20 19 | -481 281 16 136
igr n/a| 0 0 0 0 21 -9 -.20 4 4 | 6982 1768 14 78
jpl 80| -2 0 3 -6 25 -67 .12 13 12 | 122 2110 14 143
mit 299| 2 0 -2 55 -21 12 -.18 13 12 | -512 302 29 241
ngs 244| 0 2 7 -83 -25 -30 .07 13 12 | -1161 -44 1547 3508
sio 462| 1 0 1 73 149 -72 -.60 18 19 | --- --- --- ---
Table 2.1767.6 GPS week: 1767 Day: 6 MJD: 56619.000
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 264| 0 0 4 5 24 5 .16 9 9 | -705 -961 22 132
emr 80| 0 2 10 10 28 0 .10 14 14 | 2553 1609 40 130
esa 150| 1 0 -1 29 -43 1 -.19 7 6 | 205 -680 12 102
gfz 200| 0 1 -4 10 7 -3 -.02 10 11 | -199 218 20 83
grg 191| 3 7 -23 -38 -171 -25 .54 31 28 | -219 -96 36 156
igr n/a| 0 0 -1 16 33 -15 -.19 5 5 | 8534 1698 16 86
jpl 80| -4 0 2 -21 47 -19 .12 13 13 | 1996 2269 28 152
mit 249| 1 0 -2 -22 -24 23 -.14 11 10 | -222 -43 33 264
ngs 242| 0 -1 0 -42 58 -24 .05 11 10 | -674 -965 1996 3391
sio 463| 0 1 2 32 152 -109 -.59 20 19 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1767.0 GPS week: 1767 Day: 0 MJD: 56613.000
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 10 4 11 11 3 17 12 20 13 4 | 52 57 58 61 69 56 64 59 56 52 58
2 | 10 12 6 10 17 6 13 10 13 31 4 | 22 23 25 29 33 26 24 30 28 24 25
3 | 6 13 4 9 18 3 9 8 19 17 3 | 18 24 14 17 25 14 20 16 25 21 17
4 | 11 8 4 9 14 4 7 10 13 30 3 | 35 36 39 44 48 39 38 40 35 36 39
5 | 16 14 7 9 18 5 11 10 17 13 4 | 25 21 15 21 31 17 18 17 32 16 18
6 | 7 10 3 9 13 4 7 8 20 18 3 | 17 15 13 17 24 13 16 16 23 20 15
7 | 11 15 5 8 14 3 13 12 16 21 4 | 27 24 20 21 30 18 22 23 26 21 21
8 | 7 9 5 6 14 3 9 9 13 22 3 | 20 20 19 19 22 17 20 20 24 29 19
9 | 5 8 5 7 14 3 8 10 11 17 3 | 22 19 18 19 22 18 17 22 24 22 19
10 | 8 10 7 9 16 5 11 9 19 25 4 | 19 22 18 24 22 17 23 18 27 24 20
11 | 8 15 5 12 15 3 10 12 25 13 4 | 39 45 43 47 59 43 48 43 37 38 43
12E | 9 19 5 10 17 4 19 15 9 13 4 | 37 37 34 40 35 36 34 39 42 37 36
13 | 7 11 4 7 19 3 11 12 15 8 3 | 26 29 25 25 36 23 30 22 34 18 25
14 | 14 10 6 10 12 4 12 13 11 15 4 | 24 23 19 24 27 19 25 19 23 21 20
15 | 8 17 5 8 16 5 24 10 17 10 4 | 36 39 32 33 39 32 37 37 44 34 34
16E | 7 18 5 12 22 4 16 15 25 16 5 | 22 27 22 25 22 20 22 25 35 20 22
17 | 10 14 6 9 14 4 16 12 11 14 4 | 25 26 22 30 35 24 26 31 28 21 25
18 | 9 13 4 10 14 3 15 9 10 20 3 | 21 22 23 27 32 19 23 22 21 18 21
19 | 9 16 9 9 14 6 15 20 21 24 5 | 21 24 19 24 31 21 23 23 22 23 20
20 | 11 20 6 14 17 4 14 16 16 15 5 | 30 32 34 41 39 31 31 31 38 24 32
21 | 8 12 6 9 10 2 12 7 20 25 3 | 26 28 29 33 35 27 28 30 32 20 28
22 | 8 11 4 7 16 2 8 10 13 23 3 | 26 28 28 30 40 26 28 26 26 22 27
23 | 10 18 5 11 16 4 17 13 16 9 4 | 32 34 31 33 32 28 34 28 35 28 29
24 | 10 13 5 9 13 4 11 12 13 15 3 | 21 22 18 18 25 16 26 19 25 11 19
25E | 8 12 4 9 12 3 15 11 6 13 3 | 23 26 24 26 28 24 31 25 28 26 25
26 | 8 12 5 7 10 5 9 8 19 21 3 | 18 19 17 20 19 18 19 20 31 24 18
X27 | 7 9 3 10 --- 4 12 7 21 11 3 | 39 37 33 29 --- 33 38 34 37 28 34
28E | 6 12 5 11 15 4 12 10 14 10 3 | 28 27 26 28 25 25 26 26 27 26 25
29 | 9 15 6 7 13 5 16 9 13 18 4 | 16 18 8 6 6 8 16 8 13 11 10
31 | 10 14 5 10 16 6 13 17 17 18 4 | 31 29 27 28 34 23 26 33 28 29 27
32 | 12 12 6 7 15 3 9 6 13 18 3 | 19 23 19 23 24 15 25 17 22 20 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 5 9 15 4 13 11 16 18 |T 26 27 24 27 31 24 27 26 29 24 25
WRMS | 10 13 5 9 15 4 13 10 15 17 |NE 25 26 24 27 32 23 26 25 28 23 24
MEDI | 9 12 5 9 14 4 12 10 16 17 |MD 25 26 23 26 31 23 26 25 28 23 25
Table 3.1767.1 GPS week: 1767 Day: 1 MJD: 56614.000
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 12 4 11 11 5 18 9 10 10 4 | 37 38 36 36 46 34 47 35 42 31 37
2 | 10 13 6 9 16 5 12 11 7 28 3 | 12 17 16 19 17 16 16 22 18 19 16
3 | 7 10 4 10 19 3 8 10 15 18 3 | 20 20 16 20 25 15 21 17 22 22 17
4 | 11 11 4 8 12 3 6 10 8 26 3 | 22 23 23 28 28 23 23 26 25 24 24
5 | 9 16 6 9 17 3 11 9 9 14 3 | 16 22 11 15 27 11 16 14 19 14 13
6 | 8 11 3 9 12 4 8 9 15 19 3 | 19 17 14 18 23 15 17 14 17 19 15
7 | 11 14 4 9 12 3 12 11 9 17 3 | 26 23 17 17 28 16 22 22 22 16 19
8 | 10 9 5 7 11 3 11 9 8 22 3 | 25 23 21 22 25 22 25 24 23 30 22
9 | 8 9 4 8 11 3 10 10 8 17 3 | 17 17 15 13 18 12 16 18 18 19 15
10 | 10 12 5 8 13 3 11 9 11 25 3 | 15 22 14 19 18 14 19 14 21 21 15
11 | 10 15 3 10 15 3 11 8 10 11 3 | 28 32 29 30 43 28 34 27 31 24 29
12E | 13 23 5 11 13 4 20 14 12 14 5 | 24 26 20 29 25 20 26 27 25 21 22
13 | 8 10 4 7 19 3 12 8 11 8 3 | 21 23 17 20 35 16 24 17 22 12 19
14 | 14 14 5 10 13 5 11 8 10 15 3 | 21 21 15 20 26 15 18 17 19 18 16
15 | 8 20 6 8 18 4 22 10 13 14 4 | 27 28 21 24 31 20 28 20 20 19 21
16E | 9 20 5 14 26 5 15 13 12 17 5 | 20 20 18 21 25 16 17 18 24 18 17
17 | 15 17 5 8 16 5 19 11 9 13 4 | 27 25 19 22 29 19 22 25 22 16 20
18 | 11 13 4 8 15 3 11 10 11 18 3 | 19 22 20 20 28 17 22 20 18 19 19
19 | 9 18 6 11 14 5 15 13 15 24 4 | 22 24 18 20 30 18 23 20 19 20 18
20 | 7 17 5 12 15 3 15 10 11 15 4 | 25 29 25 32 33 23 26 24 28 19 25
21 | 10 15 5 9 13 4 12 8 8 23 3 | 23 23 24 24 25 21 23 26 23 15 22
22 | 10 11 4 9 17 3 10 9 16 18 3 | 23 25 22 23 32 20 24 20 23 18 21
23 | 10 14 5 9 15 5 16 9 9 9 3 | 32 32 27 29 34 26 30 28 30 26 28
24 | 8 14 6 10 13 5 11 11 12 14 3 | 17 19 16 16 23 13 22 18 20 10 15
25E | 13 15 4 11 12 3 16 9 7 11 4 | 17 20 16 18 22 14 25 18 19 13 17
26 | 7 11 4 9 11 3 10 8 11 20 3 | 16 20 13 17 17 14 18 19 26 22 16
X27 | 11 13 4 --- --- 7 --- 12 16 --- 5 | 25 26 22 --- --- 23 --- 24 28 --- 23
28E | 9 14 3 12 14 3 13 11 13 11 4 | 22 20 17 18 21 16 21 17 21 20 17
29 | 10 19 5 9 12 4 16 8 9 18 4 | 15 18 8 11 9 12 17 9 8 12 14
31 | 11 17 5 11 15 4 14 16 14 15 4 | 25 29 23 26 29 22 27 24 28 22 23
32 | 7 12 4 7 15 3 9 6 8 17 3 | 18 22 15 19 20 14 21 17 19 19 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 5 10 15 4 13 10 11 17 |T 21 23 18 21 26 18 23 20 22 19 19
WRMS | 10 15 5 10 14 4 13 10 9 17 |NE 21 23 18 21 26 18 22 20 22 19 19
MEDI | 10 14 5 9 14 3 12 10 11 17 |MD 22 23 18 20 25 16 22 20 22 19 19
Table 3.1767.2 GPS week: 1767 Day: 2 MJD: 56615.000
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 11 3 11 9 4 19 8 11 10 3 | 48 46 43 40 54 45 57 45 46 40 45
2 | 11 12 7 8 16 3 13 9 11 28 4 | 16 20 19 22 23 18 23 23 19 22 19
3 | 5 12 6 9 16 3 9 10 15 18 3 | 19 20 16 16 20 15 20 18 21 23 16
4 | 9 8 5 9 14 4 8 9 12 24 3 | 29 31 30 33 35 30 34 33 27 29 30
5 | 19 16 6 10 16 5 11 11 14 13 4 | 22 23 13 18 27 12 19 17 21 13 15
6 | 7 10 3 10 13 3 10 9 16 20 3 | 18 18 13 15 17 13 18 15 18 21 13
7 | 10 13 5 11 14 4 15 10 13 17 4 | 26 26 18 22 30 19 24 22 23 16 20
8 | 8 10 6 7 9 4 11 9 10 22 3 | 19 23 15 16 19 15 20 19 22 28 17
9 | 6 10 5 7 9 3 9 8 12 16 3 | 19 19 14 13 18 14 18 17 21 18 14
10 | 11 9 5 9 12 4 11 9 12 23 3 | 21 23 18 20 22 17 25 18 24 25 19
11 | 8 13 5 12 10 3 12 8 18 10 3 | 35 40 34 34 45 34 45 34 36 30 35
12E | 8 24 5 9 14 4 20 15 10 16 5 | 31 37 29 35 31 30 32 33 36 29 30
13 | 8 10 4 7 21 3 10 7 8 9 3 | 27 27 23 23 37 21 26 20 24 16 23
14 | 12 11 5 10 13 4 11 7 11 15 3 | 22 22 17 23 25 17 22 17 22 18 18
15 | 8 20 5 10 14 5 23 11 19 16 5 | 69 69 66 68 66 64 66 66 68 65 66
16E | 7 19 6 12 18 3 14 11 19 17 4 | 24 21 24 26 27 20 20 25 27 21 21
17 | 8 14 6 11 12 4 14 8 10 13 3 | 25 26 21 26 31 22 25 27 26 19 23
18 | 8 12 4 9 16 3 15 13 10 20 4 | 21 24 19 24 28 17 23 20 22 16 19
19 | 11 19 6 8 13 5 14 11 17 25 4 | 19 26 15 18 25 17 24 20 22 21 16
20 | 9 18 6 13 16 3 11 8 14 16 4 | 29 33 28 33 36 27 30 27 32 20 28
21 | 6 13 7 7 11 5 11 12 12 21 3 | 22 23 24 26 25 22 24 24 23 13 22
22 | 6 10 4 8 16 3 13 7 10 17 3 | 26 28 23 29 34 22 26 23 21 18 23
23 | 8 12 5 10 17 3 13 8 9 11 3 | 32 33 29 29 33 27 32 27 30 27 28
24 | 7 14 6 8 13 5 12 10 11 15 3 | 20 25 19 19 25 17 27 19 23 12 19
25E | 7 14 4 9 17 5 16 9 12 13 4 | 25 27 25 27 31 22 29 21 23 20 23
26 | 7 11 6 11 12 3 10 10 17 21 3 | 18 23 17 21 19 17 22 20 27 24 17
X27 | 11 19 7 10 --- 8 --- 17 19 --- 6 | 24 26 21 21 --- 19 --- 25 26 --- 20
28E | 6 14 5 11 14 3 15 8 9 8 3 | 23 22 17 21 20 17 19 20 24 18 18
X29 | 2 --- --- --- --- 27 --- --- --- --- 0 | 49 --- --- --- --- 41 --- --- --- --- 49
31 | 11 19 6 9 18 4 14 10 13 17 4 | 24 29 23 27 31 21 25 21 26 21 22
32 | 9 12 4 6 14 3 10 7 10 17 3 | 22 25 18 21 21 16 24 17 19 19 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 5 10 14 4 13 9 13 18 |T 26 27 23 25 29 22 27 24 26 22 24
WRMS | 9 14 5 9 15 4 13 9 12 16 |NE 24 26 20 23 28 21 26 22 24 20 22
MEDI | 8 12 5 9 14 4 12 9 12 17 |MD 24 25 19 23 27 19 24 21 23 21 20
Table 3.1767.3 GPS week: 1767 Day: 3 MJD: 56616.000
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 9 11 6 17 8 17 9 4 | 44 46 49 49 58 45 55 48 45 44 48
2 | 8 11 5 13 13 5 12 10 8 29 3 | 19 18 20 25 26 20 21 25 16 22 20
3 | 7 13 5 13 18 3 7 11 15 15 4 | 20 25 18 21 26 17 21 20 25 22 19
4 | 8 8 4 9 12 4 8 11 13 24 3 | 31 29 32 36 39 30 32 35 23 30 32
5 | 15 16 4 9 16 5 11 9 14 13 4 | 20 21 13 16 26 12 19 16 21 13 15
6 | 7 12 5 10 12 3 7 9 12 18 3 | 18 23 17 21 23 16 19 17 17 21 17
7 | 10 13 4 11 12 3 12 9 14 18 3 | 24 26 19 24 29 19 23 24 25 16 21
8 | 8 10 4 8 10 3 9 9 12 22 3 | 23 26 21 22 23 21 25 25 26 31 22
9 | 6 11 4 8 9 4 8 9 10 15 3 | 21 25 21 19 20 20 22 23 26 22 21
10 | 6 12 6 9 11 4 11 10 12 21 3 | 16 23 16 19 21 13 20 18 17 23 16
11 | 8 15 4 12 17 3 12 9 22 11 4 | 33 40 38 39 51 35 43 38 32 33 37
12E | 9 25 5 10 13 4 23 14 11 14 5 | 22 25 18 26 21 17 23 23 27 22 20
13 | 6 9 4 10 19 3 10 8 9 10 3 | 20 25 20 23 37 18 24 20 20 16 21
14 | 12 11 4 11 14 6 12 10 13 15 3 | 20 19 14 19 26 14 19 15 21 17 15
15E | 10 19 7 13 17 5 23 9 18 13 5 | 50 52 50 48 54 47 53 48 50 47 49
16E | 7 24 7 12 23 3 12 11 12 14 5 | 20 27 19 23 27 18 19 17 25 15 19
17 | 15 15 6 10 13 3 14 10 12 14 4 | 25 25 22 26 36 21 25 28 23 19 23
18 | 9 14 5 10 15 2 12 14 12 21 4 | 19 24 18 23 30 17 22 20 22 18 19
19 | 10 17 6 13 16 4 14 13 14 25 4 | 17 26 17 22 30 19 25 21 19 23 18
20 | 9 18 6 13 17 4 13 10 12 15 4 | 21 30 28 34 35 24 28 29 29 20 26
21 | 9 12 5 9 12 2 10 8 17 23 3 | 24 25 27 30 34 26 27 27 30 19 27
22 | 6 11 4 9 17 3 10 11 11 18 3 | 20 26 24 28 37 21 26 23 23 20 23
23 | 8 13 5 12 14 3 13 11 8 10 3 | 27 30 23 30 32 24 28 26 26 21 25
24 | 8 11 5 11 17 5 11 12 9 15 3 | 18 21 16 17 25 15 24 20 19 11 17
25E | 10 16 4 10 13 3 13 9 12 13 4 | 21 26 18 21 26 18 26 19 21 18 20
26 | 8 11 5 8 11 3 11 9 16 21 3 | 18 19 14 17 19 14 19 20 21 22 16
X27 | 7 12 5 10 --- 4 14 11 12 13 4 | 25 27 23 23 --- 22 31 22 28 21 24
28E | 8 17 6 12 18 4 14 15 14 11 4 | 19 23 16 20 18 17 22 21 29 18 17
29 | 9 23 4 10 12 6 18 12 13 --- 4 | 20 24 12 16 20 13 21 18 13 --- 15
31 | 11 16 5 13 15 4 13 10 13 16 4 | 35 30 26 31 34 26 31 29 29 27 28
32 | 9 13 4 8 16 3 9 8 12 15 3 | 17 22 15 19 21 13 23 16 19 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 5 11 15 4 13 10 13 17 |T 23 26 22 25 30 21 26 24 24 22 22
WRMS | 9 15 5 10 15 4 12 10 12 17 |NE 22 25 21 24 30 20 25 23 23 22 22
MEDI | 8 13 5 10 14 4 12 10 12 15 |MD 20 25 19 23 26 19 24 22 23 21 20
Table 3.1767.4 GPS week: 1767 Day: 4 MJD: 56617.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 5 13 12 6 19 8 10 8 4 | 47 50 48 53 58 47 59 45 49 41 49
2 | 8 13 8 10 17 4 10 10 10 27 3 | 21 20 23 23 25 19 23 24 16 20 21
3 | 6 14 5 11 20 3 8 8 9 13 3 | 21 27 15 19 26 15 21 16 20 17 17
4 | 10 11 7 8 14 3 7 13 10 23 3 | 32 31 37 36 35 31 34 37 31 29 34
5 | 17 18 8 10 17 4 12 9 9 13 4 | 26 24 15 17 28 14 20 17 23 16 17
6 | 7 13 4 11 16 3 9 9 13 16 3 | 18 23 12 16 24 12 18 12 20 15 14
7 | 10 14 5 9 12 4 12 8 9 19 3 | 30 26 23 24 28 20 24 22 25 17 23
8 | 8 9 4 8 16 4 9 9 8 23 3 | 29 28 27 28 28 27 28 29 32 34 27
9 | 7 10 4 11 15 4 8 9 8 18 3 | 25 23 22 24 21 22 20 24 24 24 22
10 | 8 12 6 8 19 3 12 13 11 20 4 | 22 25 22 24 23 19 24 21 26 24 21
11 | 7 14 3 12 15 4 11 9 12 12 3 | 35 41 36 41 51 35 42 35 35 31 37
12E | 10 23 4 10 14 4 22 15 10 17 5 | 23 26 20 25 24 21 27 26 28 21 21
13 | 8 10 5 9 17 3 9 8 12 10 3 | 24 27 22 23 34 20 24 22 22 18 22
14 | 14 11 6 11 12 5 11 9 13 14 4 | 20 21 17 23 24 16 22 17 20 18 17
15E | 8 20 6 10 15 5 20 14 15 20 5 | 29 32 27 30 33 26 35 25 28 31 26
16E | 8 17 6 13 20 3 13 10 11 17 4 | 19 19 17 22 24 15 17 19 25 18 17
17 | 12 14 6 10 17 3 12 10 8 13 4 | 24 29 26 32 35 24 29 30 26 21 26
18 | 11 15 5 10 18 4 14 12 8 21 4 | 22 23 18 24 32 15 23 19 19 19 19
19 | 10 17 5 12 15 5 13 9 9 25 4 | 24 28 23 26 34 22 27 25 24 25 23
20 | 10 15 6 10 20 5 12 9 10 15 4 | 26 33 30 35 37 27 32 29 28 21 29
21 | 10 11 4 10 15 4 10 10 10 22 3 | 24 24 26 31 32 23 25 24 25 17 25
22 | 9 10 6 10 19 3 11 12 15 19 4 | 26 27 25 31 37 22 29 25 21 22 25
23 | 10 16 7 12 20 4 14 9 11 11 4 | 52 52 52 57 55 51 54 52 55 48 52
24 | 9 13 4 8 14 4 11 11 9 16 3 | 22 22 19 19 24 17 28 24 22 14 20
25E | 11 17 4 10 13 4 14 10 12 12 4 | 23 22 19 20 28 17 29 22 24 18 20
26 | 6 10 5 10 11 6 9 11 8 21 3 | 22 24 18 20 20 18 22 20 22 23 19
X27 | 9 9 5 12 --- 4 12 11 9 14 3 | 26 24 21 22 --- 19 29 22 25 21 22
28E | 12 15 6 11 16 5 14 14 10 12 4 | 22 24 25 26 25 21 25 26 23 22 22
29 | 9 20 5 10 18 4 16 15 14 --- 4 | 24 23 15 19 20 18 22 19 20 --- 19
31 | 13 15 4 12 14 5 12 10 10 17 4 | 27 26 23 25 33 23 28 25 28 25 24
32 | 12 13 5 9 20 4 9 7 12 17 4 | 20 28 21 25 23 17 28 19 21 20 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 5 10 16 4 13 11 11 18 |T 25 27 24 27 30 22 28 24 26 23 24
WRMS | 10 14 5 10 16 4 12 10 10 18 |NE 25 27 23 26 30 21 27 24 24 22 23
MEDI | 9 14 5 10 16 4 12 10 10 17 |MD 24 26 22 24 28 20 27 24 24 21 22
Table 3.1767.5 GPS week: 1767 Day: 5 MJD: 56618.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 4 12 17 5 18 10 14 9 4 | 30 35 30 34 45 29 43 32 30 29 32
2 | 6 12 7 9 16 4 12 11 10 30 3 | 21 22 23 25 22 21 23 22 19 21 21
3 | 8 13 6 9 29 3 8 17 15 16 4 | 28 29 25 28 35 25 29 26 30 24 26
4 | 7 10 6 8 20 3 8 12 14 26 3 | 28 25 30 31 30 26 27 31 23 25 27
5 | 7 19 5 10 18 3 13 10 13 12 4 | 22 25 15 20 29 17 20 14 28 12 18
6 | 7 10 4 8 25 4 9 12 16 17 4 | 20 22 16 19 30 16 20 20 21 22 17
7 | 9 14 5 11 15 3 13 11 10 21 4 | 29 26 21 26 32 21 23 20 30 15 23
8 | 6 10 5 8 26 3 10 11 11 22 3 | 50 51 47 51 48 48 51 47 52 51 48
9 | 5 10 5 8 20 3 9 12 9 20 3 | 21 20 20 18 26 18 18 19 20 20 19
10 | 7 14 7 10 25 5 10 13 14 23 4 | 18 24 18 24 22 18 21 19 20 28 18
11 | 8 14 5 11 20 2 12 13 13 14 4 | 20 32 21 24 39 21 31 27 21 24 23
12E | 10 23 5 10 18 5 23 18 11 14 5 | 22 24 16 21 30 17 24 25 23 18 19
13 | 6 9 4 8 18 3 9 11 9 15 3 | 21 24 19 23 36 17 22 18 27 15 21
14 | 11 11 5 9 14 4 10 12 10 13 3 | 25 22 19 23 27 19 22 18 17 18 20
15E | 14 22 8 11 15 6 25 9 14 9 5 | 24 32 20 20 31 20 31 22 21 22 22
16E | 8 21 5 13 21 4 11 14 15 14 4 | 20 26 17 24 28 17 20 19 28 16 19
17 | 10 14 5 10 20 5 14 14 12 13 4 | 23 26 19 25 33 19 23 26 23 18 21
18 | 9 16 4 10 19 3 13 13 9 23 4 | 26 26 23 27 35 20 26 19 22 19 23
19 | 9 16 6 9 25 5 14 13 16 27 4 | 20 25 18 19 32 16 24 18 21 23 18
20 | 10 16 6 10 23 4 13 12 13 14 4 | 22 26 22 26 33 20 23 21 30 16 22
21 | 8 12 6 10 19 3 10 12 19 25 4 | 24 22 26 25 32 21 23 23 23 17 23
22 | 9 13 4 6 20 3 9 11 7 22 3 | 25 28 24 28 42 23 28 22 25 22 25
23E | 16 21 6 12 20 7 12 18 12 15 5 | 83 76 76 79 76 71 76 67 77 69 76
24 | 8 11 6 9 15 5 11 11 14 17 3 | 21 20 19 16 27 17 26 17 20 13 19
25E | 9 16 5 6 19 3 13 12 12 11 4 | 23 25 19 20 29 20 26 17 22 19 21
26 | 6 13 6 9 15 4 10 15 17 20 4 | 19 26 16 21 25 17 23 17 28 23 19
X27 | 8 12 4 9 --- 4 13 14 16 16 4 | 27 27 24 25 --- 24 31 22 34 21 25
28E | 8 14 5 10 21 5 14 17 11 13 4 | 22 23 18 19 25 17 20 18 27 14 19
29 | 8 19 5 8 23 4 17 18 12 18 4 | 21 23 13 14 21 17 21 18 18 12 17
31 | 11 16 6 9 17 4 12 13 12 14 4 | 24 27 16 20 29 18 22 17 25 17 19
32 | 11 14 5 7 29 3 10 9 16 16 4 | 21 23 13 18 28 13 19 15 23 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 6 9 20 4 13 13 13 18 |T 25 27 22 25 32 22 26 23 26 22 23
WRMS | 8 15 5 9 19 4 12 12 12 19 |NE 24 26 21 24 31 20 25 21 25 20 22
MEDI | 8 14 5 9 20 4 12 12 13 16 |MD 22 25 19 24 30 19 23 20 23 19 21
Table 3.1767.6 GPS week: 1767 Day: 6 MJD: 56619.000
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 11 6 11 28 5 19 6 13 10 4 | 57 58 60 63 80 57 68 59 58 54 60
2 | 7 12 6 12 28 3 11 11 8 32 4 | 19 18 24 29 43 22 20 27 17 25 22
3 | 7 12 5 10 56 5 9 6 12 13 4 | 24 25 21 24 47 20 24 20 25 23 22
4 | 10 9 7 11 29 4 11 10 10 31 4 | 38 34 42 46 59 39 36 43 35 38 39
5 | 6 18 6 9 20 4 13 5 8 12 3 | 15 20 14 18 34 11 16 11 14 10 12
6 | 8 13 5 11 58 4 10 11 13 16 5 | 18 21 17 22 48 16 20 17 20 21 18
7 | 9 12 4 12 29 3 13 10 11 22 4 | 28 25 21 27 38 21 24 22 25 16 22
8 | 7 10 4 8 33 4 8 9 8 28 3 | 30 28 26 28 43 26 29 27 28 38 27
9 | 6 10 4 9 28 4 7 9 7 22 3 | 23 23 20 20 38 20 22 23 23 19 21
10 | 12 13 25 10 32 14 13 15 11 28 6 | 18 19 35 21 36 18 21 23 20 29 20
11 | 7 15 3 9 28 3 11 10 15 17 4 | 40 44 45 49 67 42 48 47 40 42 44
12E | 9 24 5 11 26 4 24 17 10 16 5 | 27 31 23 31 34 26 30 30 32 27 25
13 | 8 10 5 10 30 2 11 13 8 13 4 | 25 27 24 27 41 22 27 19 25 18 23
14 | 14 9 5 10 27 6 10 11 14 12 4 | 24 23 20 25 30 20 24 20 24 22 20
15E | 9 17 5 11 17 5 22 10 11 10 4 | 27 30 25 26 38 25 32 28 27 30 26
16E | 10 24 5 16 28 4 13 12 13 16 5 | 19 25 20 26 28 18 21 22 26 20 19
17 | 7 16 5 11 27 4 14 10 9 13 4 | 28 23 25 31 50 26 25 31 23 24 25
18 | 8 15 4 11 24 4 14 10 8 23 4 | 23 26 22 30 41 21 26 22 26 23 23
19 | 11 17 9 11 58 5 15 13 16 28 6 | 20 22 22 26 46 20 24 25 17 29 20
20 | 11 14 7 11 23 4 12 8 10 16 4 | 28 32 33 38 47 31 32 31 29 24 30
21 | 9 11 5 9 19 3 10 8 10 26 3 | 29 26 29 33 35 26 27 28 27 20 28
22 | 7 11 3 10 29 5 11 12 8 22 3 | 27 30 29 34 46 27 31 29 29 28 29
23E | 12 19 6 13 37 5 15 13 9 13 5 | 38 41 37 43 54 36 37 40 41 40 37
24 | 8 12 5 9 20 4 11 8 11 18 3 | 21 22 19 18 29 17 27 17 21 17 19
25E | 8 17 4 9 23 4 16 8 9 12 4 | 26 27 23 26 34 22 34 24 26 22 24
26 | 6 13 6 9 21 5 10 11 11 21 3 | 17 20 16 19 35 14 20 20 18 22 16
X27 | 12 12 4 12 --- 4 11 8 12 12 4 | 35 32 26 27 --- 26 35 26 34 25 29
28E | 6 14 5 11 29 4 13 13 14 16 4 | 21 22 18 20 33 17 22 19 23 17 18
29 | 8 17 6 9 24 5 15 17 11 19 4 | 24 24 16 26 34 19 23 24 20 11 21
31 | 10 14 5 11 24 4 13 12 9 13 4 | 26 26 20 26 35 21 27 26 26 24 22
32 | 10 11 5 9 33 4 8 10 12 16 4 | 19 24 18 23 35 17 24 18 20 21 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 7 10 31 5 13 11 11 20 |T 26 27 25 29 41 23 28 26 26 25 25
WRMS | 9 14 6 11 28 5 13 10 10 19 |NE 26 26 25 29 43 23 28 26 25 24 25
MEDI | 8 13 5 11 28 4 12 10 11 16 |MD 25 25 23 26 38 21 26 24 25 23 22
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 4.1767 GPS week: 1767 MJD: 56613.0-56619.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2960 |U 5 6 12 |U 10 10 31 |U 7 7 13 |
emr | emr 2960 | 8 9 17 |U 11 9 33 | 10 9 17 |
esa | esa 2962 | 6 7 12 |U 9 10 32 | 9 7 14 |
gfz | gfz 2945 |U 6 7 14 |U 9 9 32 |U 9 8 14 |
grg | grg 2865 |U 43 53 133 |U 39 43 111 |U 53 52 112 |
igr | igr 2955 | 5 7 12 | 9 9 31 | 8 7 14 |
igs | igs 2960 | 6 7 13 | 9 9 32 | 9 7 13 |
jpl | jpl 2934 | 7 8 17 |U 9 10 33 |U 10 9 18 |
mit | mit 2962 | 9 8 15 |U 10 11 33 |U 17 13 33 |
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 5.1767.0 GPS week: 1767 Day: 0 MJD: 56613.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 16 | 8 9 44 | 8 6 9 |
emr | emr 2976 | 8 9 22 | 11 9 48 | 10 8 13 |
esa | esa 2976 | 6 7 15 | 8 10 44 | 9 7 8 |
gfz | gfz 2976 | 7 8 15 | 8 9 46 | 9 6 9 |
grg | grg 2880 | 10 7 21 | 10 9 44 | 9 10 16 |
igr | igr 2976 | 6 7 16 | 8 9 43 | 9 6 9 |
igs | igs 2976 | 6 8 15 | 9 9 45 | 9 6 8 |
jpl | jpl 2976 | 8 8 21 | 8 9 46 | 10 9 14 |
mit | mit 2976 | 7 8 17 | 9 12 45 | 10 9 10 |
Table 5.1767.1 GPS week: 1767 Day: 1 MJD: 56614.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2969 | 6 6 12 | 8 8 25 | 9 9 16 |
emr | emr 2970 | 11 9 18 | 11 8 27 | 12 11 21 |
esa | esa 2976 | 8 8 13 | 8 8 27 | 11 9 17 |
gfz | gfz 2880 | 8 9 14 | 7 8 28 | 10 9 16 |
grg | grg 2880 | 11 9 18 | 11 11 27 | 14 12 21 |
igr | igr 2969 | 7 8 13 | 8 7 26 | 10 9 15 |
igs | igs 2969 | 8 8 13 | 8 7 27 | 11 9 15 |
jpl | jpl 2880 | 11 10 25 | 8 8 27 | 12 10 19 |
mit | mit 2976 | 8 8 14 | 9 8 30 | 11 12 15 |
Table 5.1767.2 GPS week: 1767 Day: 2 MJD: 56615.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2877 | 4 8 12 | 10 9 30 | 8 8 10 |
emr | emr 2877 | 6 7 14 | 12 9 31 | 12 11 15 |
esa | esa 2880 | 5 8 13 | 10 9 31 | 9 9 11 |
gfz | gfz 2862 | 5 8 14 | 10 9 29 | 10 11 13 |
grg | grg 2783 | 63 60 126 | 56 81 159 | 73 90 169 |
igr | igr 2869 | 4 7 13 | 10 9 30 | 9 10 12 |
igs | igs 2877 | 4 7 13 | 10 9 30 | 10 10 12 |
jpl | jpl 2782 | 6 6 14 | 10 9 34 | 10 10 17 |
mit | mit 2880 | 4 6 14 | 10 10 31 | 46 14 96 |
Table 5.1767.3 GPS week: 1767 Day: 3 MJD: 56616.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 17 | 11 8 23 | 8 8 15 |
emr | emr 2976 | 12 9 23 | 13 9 25 | 10 10 17 |
esa | esa 2976 | 8 8 17 | 11 8 26 | 9 8 15 |
gfz | gfz 2976 | 9 9 26 | 11 8 27 | 9 8 16 |
grg | grg 2880 | 29 44 86 | 29 27 82 | 28 22 54 |
igr | igr 2976 | 8 8 16 | 10 8 25 | 9 8 16 |
igs | igs 2976 | 8 8 17 | 11 8 25 | 9 8 14 |
jpl | jpl 2976 | 9 10 20 | 10 11 27 | 10 8 16 |
mit | mit 2976 | 27 17 27 | 11 11 28 | 12 12 30 |
Table 5.1767.4 GPS week: 1767 Day: 4 MJD: 56617.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 6 10 | 9 12 33 | 7 6 13 |
emr | emr 2976 | 7 9 12 | 9 14 37 | 10 9 19 |
esa | esa 2976 | 5 6 10 | 9 12 33 | 9 7 17 |
gfz | gfz 2976 | 5 7 10 | 9 12 33 | 9 7 17 |
grg | grg 2880 | 64 58 133 | 39 43 99 | 59 53 128 |
igr | igr 2976 | 4 6 9 | 9 12 34 | 9 7 16 |
igs | igs 2976 | 4 7 8 | 8 12 33 | 9 7 16 |
jpl | jpl 2976 | 6 7 12 | 8 13 32 | 10 8 20 |
mit | mit 2976 | 5 8 12 | 11 14 35 | 10 10 19 |
Table 5.1767.5 GPS week: 1767 Day: 5 MJD: 56618.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 4 9 | 9 10 29 | 5 5 12 |
emr | emr 2976 | 7 8 18 | 9 9 29 | 7 7 21 |
esa | esa 2976 | 4 4 9 | 9 10 30 | 6 5 14 |
gfz | gfz 2976 | 4 4 10 | 9 10 30 | 7 6 13 |
grg | grg 2879 | 88 114 368 | 82 85 225 | 125 100 251 |
igr | igr 2976 | 3 4 9 | 9 9 28 | 6 5 14 |
igs | igs 2976 | 4 5 9 | 9 10 28 | 6 5 14 |
jpl | jpl 2976 | 5 6 15 | 9 10 30 | 7 7 19 |
mit | mit 2976 | 5 6 9 | 11 12 30 | 8 8 17 |
Table 5.1767.6 GPS week: 1767 Day: 6 MJD: 56619.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 | 5 6 10 | 13 11 31 | 6 6 13 |
emr | emr 2974 | 8 9 14 | 12 9 32 | 7 7 17 |
esa | esa 2976 | 6 5 10 | 11 10 33 | 7 5 14 |
gfz | gfz 2974 | 5 6 10 | 11 10 33 | 7 6 14 |
grg | grg 2877 | 37 78 176 | 44 45 145 | 64 76 144 |
igr | igr 2944 | 5 5 9 | 12 11 34 | 7 7 15 |
igs | igs 2974 | 6 10 14 | 11 9 35 | 9 7 14 |
jpl | jpl 2973 | 7 8 15 | 12 10 37 | 9 9 20 |
mit | mit 2976 | 6 6 10 | 13 12 33 | 20 28 47 |
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 6.1767 GPS week: 1767 MJD: 56613.500-56619.500
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 | 5 0 6 14 -2 | 8 22
| 17 16 67 111 6 | 3
emr uuuuu | -25 -6 275 84 8 | 33 39
| 21 35 120 109 13 | 4
esa uuuuu | 3 -13 8 83 -1 | 9 20
| 7 15 43 80 3 | 3
gfz uuuuu | 0 -13 22 -110 -2 | 10 20
| 13 15 67 52 4 | 3
grg uuxux | 7 -2 10 -11 7 | 8 16
| 46 17 213 47 19 | 2
igr xxxxx | 0 -4 7 10 3 | 1 16
| 15 7 55 28 6 | 2
irf xxxxx | -2 -3 -62 -58 0 | -3 17
| 7 8 46 23 3 | 3
jpl uuuuu | 9 -6 -25 58 10 | 13 23
| 26 25 64 49 6 | 3
mit uuuuu | -9 8 -224 -175 0 | 12 20
| 33 15 70 56 4 | 3
ngs uuuuu | 18 63 19 -12 -2 | 5 12
| 56 47 103 89 5 | 2
sio xxxxx | -158 -73 -212 -202 -1 | 23 29
| 44 45 31 87 5 | 3
Table 7.1767.0 GPS week: 1767 Day: 0 MJD: 56613.500
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 | 6 7 -8 -104 -7 | 11 23
emr uuuuu | -2 19 32 16 -4 | 30 36
esa uuuuu | -3 -45 84 128 0 | 11 22
gfz uuuuu | -3 -19 68 -95 -7 | 14 24
grg uuxux | -23 -16 -74 23 -1 | 8 17
igr xxxxx | 18 -13 39 38 -7 | 2 18
irf xxxxx | -9 7 -71 -28 -5 | 0 18
jpl uuuuu | 26 21 -133 56 22 | 9 22
mit uuuuu | -44 20 -141 -121 -3 | 15 24
ngs uuuuu | 79 130 -55 -33 -2 | 6 14
sio xxxxx | -208 -105 -195 -66 -9 | 27 34
Table 7.1767.1 GPS week: 1767 Day: 1 MJD: 56614.500
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 | 7 13 -93 -81 -6 | 9 23
emr uuuuu | -12 3 249 78 -2 | 28 34
esa uuuuu | 4 -7 -18 97 0 | 9 21
gfz uuuuu | 16 -6 -25 -142 -8 | 10 22
grg uuxux | -2 0 -29 6 1 | 6 16
igr xxxxx | 8 8 78 18 2 | -1 17
irf xxxxx | -5 5 -56 -49 0 | -4 18
jpl uuuuu | -7 -5 -15 38 6 | 10 22
mit uuuuu | -40 1 -138 -147 1 | 12 21
ngs uuuuu | 25 17 174 57 3 | 5 14
sio xxxxx | -199 -154 -173 -136 -1 | 23 30
Table 7.1767.2 GPS week: 1767 Day: 2 MJD: 56615.500
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 | -6 -18 73 -36 2 | 9 23
emr uuuuu | -62 44 288 -98 35 | 29 35
esa uuuuu | -2 -17 12 208 -1 | 11 21
gfz uuuuu | 19 -14 -98 -5 -2 | 11 22
grg uuxux | -4 10 -44 -44 5 | 8 16
igr xxxxx | 20 1 -66 8 8 | 1 16
irf xxxxx | -6 -3 -96 -64 5 | -3 18
jpl uuuuu | 26 -5 -37 72 7 | 12 23
mit uuuuu | -26 1 -254 -220 7 | 12 21
ngs uuuuu | 76 58 142 -160 -10 | 7 13
sio xxxxx | -147 -44 -258 -223 6 | 23 30
Table 7.1767.3 GPS week: 1767 Day: 3 MJD: 56616.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -11 13 66 58 -2 | 10 23
emr uuuuu | -24 7 391 91 14 | 34 40
esa uuuuu | 3 1 -39 124 -2 | 11 21
gfz uuuuu | -6 2 -2 -102 5 | 11 21
grg uuxux | -3 -14 -79 -73 1 | 10 17
igr xxxxx | -9 -9 -68 45 9 | 2 16
irf xxxxx | -7 -3 -72 -100 0 | -2 18
jpl uuuuu | 45 -54 -24 -11 11 | 14 24
mit uuuuu | -8 16 -219 -264 0 | 13 22
ngs uuuuu | -1 17 20 -6 -5 | 7 13
sio xxxxx | -85 -41 -193 -287 2 | 23 30
Table 7.1767.4 GPS week: 1767 Day: 4 MJD: 56617.500
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 -26 53 193 -9 | 11 23
emr uuuuu | -23 -20 311 104 10 | 37 43
esa uuuuu | 11 -12 30 41 -6 | 12 21
gfz uuuuu | -10 -42 52 -165 -2 | 12 22
grg uuxux | -13 -2 -66 -13 -2 | 11 17
igr xxxxx | -8 -2 29 1 -2 | 4 17
irf xxxxx | 2 -6 -66 -66 -1 | -1 17
jpl uuuuu | 13 6 0 91 8 | 17 25
mit uuuuu | 49 -9 -327 -198 0 | 14 22
ngs uuuuu | -75 128 -33 -83 3 | 7 13
sio xxxxx | -120 -93 -250 -260 0 | 24 31
Table 7.1767.5 GPS week: 1767 Day: 5 MJD: 56618.500
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 | 36 5 -74 118 5 | 4 19
emr uuuuu | -43 -41 382 145 3 | 34 40
esa uuuuu | -4 -6 -33 -29 0 | 6 16
gfz uuuuu | -15 -5 65 -142 -3 | 6 17
grg uuxux | -14 -22 -123 -42 -5 | 7 15
igr xxxxx | -15 -6 29 5 4 | -1 15
irf xxxxx | 0 -16 -104 -57 -1 | -6 16
jpl uuuuu | -9 -16 82 20 6 | 14 22
mit uuuuu | -11 31 -279 -108 -5 | 9 17
ngs uuuuu | 47 47 -7 99 0 | 4 11
sio xxxxx | -184 -35 -197 -147 -3 | 19 24
Table 7.1767.6 GPS week: 1767 Day: 6 MJD: 56619.500
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 | -13 4 24 -52 6 | 3 18
emr uuuuu | -11 -55 272 255 2 | 37 42
esa uuuuu | 12 -8 19 12 2 | 5 15
gfz uuuuu | -1 -4 95 -121 0 | 4 15
grg uuxux | 111 27 489 64 50 | 6 13
igr xxxxx | -15 -6 9 -41 5 | -1 15
irf xxxxx | 10 -5 35 -40 1 | -7 16
jpl uuuuu | -30 14 -45 139 9 | 14 21
mit uuuuu | 19 -7 -210 -169 -1 | 7 16
ngs uuuuu | -21 46 -108 40 -4 | 2 9
sio xxxxx | -163 -41 -214 -294 -1 | 18 23
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