[IGSREPORT-22797] Wk 1794 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jun 13 05:57:33 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1794 (May 25, 2014 - May 31, 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:
igs1794[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1794[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1794[0-6].cls IGS GPS clock combination summary report.
igs17947.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17947.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 | AREQ AREQ
0 | EMR | 26 26
0 | ESA | IRKJ IRKJ MONP UNSA
0 | GFZ | 1 2 30 1 30 DRAG MCM4 WUHN DRAG MCM4 WUHN
0 | GRG | 26 26 FAA1 IRKJ KOUC NKLG ADIS FAA1 IRKJ KOUC NKLG
0 | JPL | 8 17
0 | MIT | 6 9 26 30 6 9 18 26 30 NRC1 GMSD MDVJ NRC1
1 | COD | 26 26
1 | EMR | AREQ AREQ TNML
1 | ESA | 26 26 BRAZ REUN BRAZ REUN
1 | GFZ | 1 2 26 30 1 26 30 ASPA DGAR GOPE MDVJ NRMD ONSA PIMO
1 | GFZ | SSIA TSKB WUHN
1 | GRG | IRKJ KELY KOUC NRC1 SOFI KELY NRC1 SOFI
1 | JPL | POVE
1 | MIT | 6 9 16 26 30 6 9 16 30 MDVJ
2 | EMR | 26 9 26
2 | ESA | UNSA
2 | GFZ | 1 2 30 1 30 ALBH BRFT CONZ CRO1 FAIR GODE HNPT MDVJ
2 | GFZ | THU3 TIDB WES2 XMIS WUHN
2 | GRG | 26 26 BOR1 BRAZ DARW GODE GUAT LAMA LAMA NRMD
2 | MIT | 6 26 30 6 26 30 MDVJ MDVJ XMIS
3 | COD | NTUS NTUS
3 | EMR | 21 21 TSKB
3 | ESA | UNSA
3 | GFZ | 1 2 30 1 30 ALBH CAS1 TSKB WUHN CAS1
3 | GRG | BOR1 BRAZ DRAG NRMD NTUS ONSA BRAZ DRAG NRMD ONSA
3 | JPL | 21
3 | MIT | 6 30 6 21 30 MDVJ
4 | COD | 26 KARR BOR1 KARR
4 | EMR | 26 YEBE CHUR YEBE
4 | ESA | 26 UNSA
4 | GFZ | 1 2 26 30 1 26 30 CHUR GUUG INVK KARR NTUS STJO CHUR
4 | GFZ | INVK KARR KELY NTUS STJO
4 | GRG | 26 CONZ FAA1 KOUC REUN KELY
4 | JPL | 3 17
4 | MIT | 6 26 30 6 30 MDVJ
5 | EMR | 26 30 26 HERS YAKT YEBE YEBE
5 | GFZ | 1 2 30 1 26 30 IRKJ INVK IRKJ NRMD
5 | GRG | 26 26
5 | JPL | 8 NOVM
5 | MIT | 26 30 26 30 IRKJ IRKJ MDVJ
6 | COD | BOR1
6 | EMR | 26 26 WUHN WUHN
6 | ESA | NTUS NTUS UNSA
6 | GFZ | 1 2 30 1 26 30 NTUS NTUS
6 | GRG | 26 26 BOR1 KELY WUHN KELY KOUC WUHN
6 | MIT | 26 30 26 30 MDVJ MDVJ
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
----+--------+--------+-------------
5 | GFZ | ~04:00 | ~ -0.16 ns
6 | GFZ | ~14:30 | ~ -0.21 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 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 | MIT | 6 30
1 | MIT | 6 30
1 | NGS | 6
2 | MIT | 6 30
2 | NGS | 6
3 | MIT | 6 30
3 | NGS | 6
4 | MIT | 6 30
4 | NGS | 6
5 | MIT | 30
6 | MIT | 30
8. 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 G06 | 4 | 4 | 4 | 4 | | 8 | |
9. 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.
10. 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 | -1.0 -.3 -3.1 -39 25 -21 .51
EMR | 0 | -1.4 -2.3 .0 -14 18 -83 .57
ESA | 0 | 1.0 .1 -.7 -33 -7 23 .23
GFZ | 0 | -.3 -.2 -3.0 -19 -18 -34 -.20
GRG | 0 | 10.8 -5.3 14.9 3 22 -49 .25
JPL | 0 | 2.7 -.7 12.6 -70 -24 7 -.71
MIT | 0 | 2.5 -4.6 9.8 5 9 -34 .58
NGS | 0 | -7.3 -8.5 17.5 -53 -3 -47 .42
SIO | 0 | .7 -2.3 -30.3 75 90 330 .40
COD | 1 | -.9 .6 -2.1 -25 16 -44 .48
EMR | 1 | 4.0 -3.0 -7.6 -26 16 -90 .42
ESA | 1 | .5 -.4 -1.2 -8 -21 28 .28
GFZ | 1 | .2 -.7 -2.3 -22 -29 -37 .31
GRG | 1 | 14.3 -5.0 7.0 -21 18 -16 .22
JPL | 1 | 4.7 -8.9 8.1 -84 -20 -45 -.55
MIT | 1 | 6.3 -6.0 6.3 11 11 -51 .66
NGS | 1 | 5.5 -7.7 3.7 -11 -23 15 .61
SIO | 1 | 7.8 .4 -33.4 71 -16 863 .65
COD | 2 | -.9 .8 -1.9 -23 15 -47 .43
EMR | 2 | 1.5 -.9 -2.5 -21 9 -73 .74
ESA | 2 | .4 .0 -.7 -11 -10 26 .17
GFZ | 2 | -.1 -.2 -2.3 -16 -8 -42 .11
GRG | 2 | 6.0 -8.8 29.6 -10 24 -13 .72
JPL | 2 | 2.9 -5.1 14.5 -65 -23 -46 -.80
MIT | 2 | 5.1 -6.3 16.8 23 22 -35 .53
NGS | 2 | 5.2 -14.8 26.7 -106 -57 -16 .61
SIO | 2 | 1.5 -1.3 -32.2 8 28 -209 .43
COD | 3 | -.6 1.2 -1.5 -13 -13 -6 .51
EMR | 3 | 1.1 -1.4 4.2 -20 8 -82 .76
ESA | 3 | .3 -.3 -1.0 -3 -11 16 .14
GFZ | 3 | .3 -.6 -2.2 -46 -38 -35 .46
GRG | 3 | 4.8 -9.5 22.6 -16 26 -43 .64
JPL | 3 | -3.3 -5.8 8.6 -27 -5 -40 -.58
MIT | 3 | 1.3 -4.9 16.5 20 -1 -95 .59
NGS | 3 | -2.2 -6.2 13.7 -50 -14 -35 .65
SIO | 3 | -2.0 -.7 -35.1 -63 -6 115 .39
COD | 4 | -1.2 .6 -1.8 -22 10 -29 .36
EMR | 4 | 6.6 -.5 .7 0 7 -36 .22
ESA | 4 | .1 -.4 -1.4 -2 -8 26 .06
GFZ | 4 | .0 -.8 -2.9 -28 -25 -21 .26
GRG | 4 | 14.9 -13.6 22.7 -13 36 -29 .28
JPL | 4 | -.4 -7.4 6.7 -35 -3 -19 -.45
MIT | 4 | 2.9 -3.0 13.9 42 -11 -28 .49
NGS | 4 | -1.8 -2.2 17.0 -62 -25 -18 .20
SIO | 4 | .7 .5 -18.6 20 -23 -32 .37
COD | 5 | -.9 1.5 -2.0 -24 22 -40 .58
EMR | 5 | 6.6 -5.0 8.8 2 5 -32 .49
ESA | 5 | .3 .4 -1.8 -3 -6 17 .13
GFZ | 5 | .1 -.5 -3.0 -20 -18 -25 .25
GRG | 5 | 11.7 -3.2 16.8 -6 3 -19 .64
JPL | 5 | 4.4 -7.4 13.3 -11 -24 -29 -.54
MIT | 5 | 7.0 -4.8 12.7 12 25 -68 .66
NGS | 5 | 4.2 -3.3 13.2 -26 -39 8 .53
SIO | 5 | 4.8 -2.0 -15.8 4 42 1 .53
COD | 6 | -1.3 1.0 -1.6 -32 31 -45 .37
EMR | 6 | 9.6 4.0 5.6 0 5 -22 .43
ESA | 6 | .5 .0 -1.3 -20 -6 6 .12
GFZ | 6 | .1 -.7 -1.8 -24 -18 -37 -.19
GRG | 6 | 14.5 -6.2 26.5 5 41 -16 .63
JPL | 6 | 5.2 -4.1 11.2 -42 -11 -1 -.40
MIT | 6 | 5.0 -3.4 12.3 12 2 -25 .44
NGS | 6 | 2.1 -5.0 17.0 -38 -40 4 .46
SIO | 6 | 7.0 -1.5 -5.0 -13 -17 -6 .25
11. 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.
12. 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 1.1794.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1794.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 2.1794.[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 3.1794.[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 5.1794.0-6). 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 1794 summary. (May 25, 2014 - May 31, 2014)
Table 1.1794.a GPS week: 1794 MJD: 56802.000-56808.000
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| -1 1 -2 5 27 5 -.01 9 9 | -792 -423 16 108
| 0 0 2 17 11 14 .01 | 307 424
emr 80| 0 -1 -2 6 -22 17 .22 12 12 | 1964 -217 15 129
| 1 0 1 16 14 11 .03 | 625 821
esa 150| 0 0 -6 15 15 -4 -.36 11 11 | 91 -1429 12 149
| 0 0 0 33 15 7 .04 | 538 1371
gfz 191| 0 0 0 -2 2 -4 -.00 12 11 | -216 232 13 144
| 1 0 0 22 9 17 .05 | 191 826
grg 183| 4 0 14 -5 9 0 .25 16 15 | 55 -81 17 163
| 0 1 3 16 24 16 .03 | 173 381
igr n/a| 0 0 0 17 11 -7 -.21 5 5 | 9702 -64 16 86
| 0 0 0 12 14 11 .01 | 417 761
jpl 80| 0 1 -4 3 -40 5 .04 13 12 | 1749 -156 17 140
| 1 1 1 14 14 23 .01 | 594 717
mit 299| 0 -1 6 21 -14 -22 -.06 14 12 | -13 1 22 195
| 0 1 0 47 29 19 .04 | 237 557
ngs 231| 0 0 2 -47 3 -9 .03 11 10 | -724 -507 1745 3199
| 0 0 3 47 50 18 .02 | 325 453
sio 467| 0 0 -2 1 -7 158 -.44 20 19 | --- --- --- ---
| 0 1 2 29 42 344 .12 | --- ---
Table 1.1794.b GPS week : 1794 MJD: 56802.000-56808.000
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 5 5 5 5 5 5 |
2 | 4 4 4 4 4 4 5 |
3 | 4 4 4 5 4 4 4 |
4 | 4 4 4 4 4 4 6 |
5 | 5 5 5 5 5 5 5 |
6 | 25 14 19 21 13 0 13 |
7 | 4 4 4 4 4 4 5 |
8 | 3 4 4 4 4 4 4 |
9 | 5 5 11 --- --- --- --- |
10 | 4 4 4 4 4 4 4 |
11 | 5 4 4 4 5 4 5 |
12 | 6 6 6 6 6 6 6 |
13 | 5 4 4 4 4 4 4 |
14 | 5 5 4 4 4 4 4 |
15 | 5 5 6 6 5 5 5 |
16 | 6 5 5 5 5 6 5 |
17 | 5 4 5 5 5 4 5 |
18 | 5 5 5 5 5 5 5 |
19 | 6 6 6 6 6 6 6 |
20 | 5 4 4 5 5 5 5 |
21 | 4 4 4 4 4 4 3 |
22 | 5 5 5 4 5 5 5 |
23 | 4 5 4 4 4 5 5 |
24 | 4 4 4 5 4 4 5 |
25 | 5 5 5 5 4 4 5 |
26 | 6 6 7 6 6 5 7 |
27 | 5 5 5 7 5 5 5 |
28 | 5 4 4 5 5 5 5 |
29 | 5 5 5 6 5 5 6 |
30 | 5 5 5 6 5 5 5 |
31 | 4 4 5 5 5 5 6 |
32 | 4 4 4 4 3 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 2.1794.0 GPS week: 1794 Day: 0 MJD: 56802.000
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| -1 1 0 33 35 4 .00 9 9 | -796 -197 15 112
emr 80| -1 -1 -2 10 -22 6 .17 12 12 | 2744 425 16 141
esa 150| 1 0 -6 -17 13 -14 -.29 11 12 | 500 -1661 13 159
gfz 193| 0 0 0 -2 10 -5 .07 10 11 | -570 1878 11 141
grg 185| 3 0 16 21 0 -14 .23 16 15 | 4 561 15 167
igr n/a| 0 0 -1 5 26 -12 -.22 5 5 | 9854 816 16 82
jpl 80| 0 0 -6 -24 -60 44 .04 13 13 | 2543 661 17 118
mit 300| 0 0 6 53 -17 -32 -.13 14 12 | -331 1168 24 209
ngs 234| 0 0 2 -81 8 10 .01 12 10 | -680 -341 1680 3541
sio 509| 0 0 -5 23 20 342 -.44 19 17 | --- --- --- ---
Table 2.1794.1 GPS week: 1794 Day: 1 MJD: 56803.000
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 -6 23 17 .01 9 8 | -997 -207 16 104
emr 80| -1 0 -3 -3 -22 5 .19 13 13 | 2288 -659 16 140
esa 150| 1 0 -6 76 24 -9 -.37 11 11 | -333 -2252 13 150
gfz 194| 0 0 1 10 -4 4 -.02 10 10 | 1 -635 12 144
grg 188| 5 -1 17 6 7 -8 .32 16 15 | -88 -176 17 169
igr n/a| 0 0 0 24 15 -10 -.22 5 5 | 9755 -459 16 82
jpl 80| 0 1 -5 3 -36 -17 .03 13 12 | 2316 -780 17 137
mit 299| 0 0 6 28 -43 -26 -.08 14 11 | -69 -196 20 197
ngs 234| 0 0 -1 -90 11 18 .02 10 9 | -1000 -219 1990 3163
sio 430| 0 2 0 23 -71 845 -.35 20 18 | --- --- --- ---
Table 2.1794.2 GPS week: 1794 Day: 2 MJD: 56804.000
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 1 -6 -15 6 -14 -.02 9 9 | -1061 7 15 112
emr 80| 0 -1 -2 -8 -38 33 .23 12 12 | 1285 880 15 119
esa 150| 0 0 -8 4 -1 7 -.33 11 11 | 426 -1860 15 168
gfz 191| 0 0 0 7 13 21 .04 11 11 | -342 296 13 144
grg 182| 3 0 15 -10 29 26 .23 17 17 | -56 -283 17 168
igr n/a| 0 0 -1 -3 7 10 -.19 5 5 | 9051 634 18 81
jpl 80| 0 1 -4 -2 -36 -17 .05 12 12 | 1212 447 16 140
mit 299| 0 -1 6 36 43 -10 -.07 13 10 | -76 -99 24 188
ngs 228| 0 -1 7 -11 -27 -26 -.00 11 10 | -1006 -119 1939 3078
sio 484| 0 3 -3 -2 56 -195 -.30 19 19 | --- --- --- ---
Table 2.1794.3 GPS week: 1794 Day: 3 MJD: 56805.000
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| 0 2 -5 -13 19 -1 -.02 11 11 | -489 -877 18 113
emr 80| 0 -2 -1 -6 -18 6 .20 12 12 | 2032 489 17 132
esa 150| 0 0 -6 -8 -3 0 -.41 11 11 | -519 -119 12 157
gfz 191| 0 0 0 -32 -13 2 .02 11 11 | -240 557 15 140
grg 184| 3 1 16 -24 12 9 .24 16 15 | -6 239 19 151
igr n/a| 0 0 0 15 4 0 -.22 6 6 | 9788 616 17 84
jpl 80| 0 2 -3 0 -37 -7 .05 13 12 | 1680 568 20 147
mit 300| 0 -2 7 34 -40 -35 -.07 14 12 | 72 66 20 189
ngs 226| -1 0 0 38 64 -7 .06 10 9 | -475 -926 1759 3190
sio 493| 0 1 -2 -12 -42 119 -.40 21 21 | --- --- --- ---
Table 2.1794.4 GPS week: 1794 Day: 4 MJD: 56806.000
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 249| -2 0 -2 16 41 24 -.00 9 9 | -832 -660 15 113
emr 80| 0 -1 -3 26 -2 19 .26 12 12 | 2570 -1387 16 126
esa 150| 0 0 -6 28 13 -9 -.40 11 12 | 742 -2053 13 151
gfz 192| 1 0 0 30 4 -23 -.04 12 11 | -169 -291 13 149
grg 188| 3 1 12 -22 29 -13 .27 16 16 | 291 -586 18 172
igr n/a| 0 0 -1 20 -13 -7 -.19 5 5 | 10400 -1137 16 96
jpl 80| 1 3 -2 10 -40 1 .03 12 11 | 2124 -1073 18 150
mit 300| 0 -2 5 -17 -3 5 -.03 13 11 | -162 -234 22 201
ngs 232| 0 0 3 -89 -34 -29 .02 11 10 | -563 -966 1372 2933
sio 479| -1 0 -4 -35 -9 -46 -.41 20 18 | --- --- --- ---
Table 2.1794.5 GPS week: 1794 Day: 5 MJD: 56807.000
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 247| -1 0 -2 9 28 15 -.01 9 9 | -276 -1025 16 95
emr 80| 0 0 0 -4 -45 26 .23 12 12 | 1727 -521 16 128
esa 150| 0 0 -5 -9 26 2 -.36 12 12 | -547 963 11 123
gfz 193| 0 0 0 -32 1 -4 -.05 12 11 | -110 66 12 137
grg 177| 3 0 8 -2 -39 14 .24 16 15 | 316 -303 17 153
igr n/a| 0 0 -1 29 8 -9 -.21 5 5 | 9685 -194 15 84
jpl 80| 0 1 -5 17 -54 11 .03 13 12 | 1407 -217 18 136
mit 300| 1 -1 5 80 -33 -51 -.03 15 12 | 433 -624 23 193
ngs 235| -1 0 3 -41 69 -21 .04 11 10 | -237 -1032 2062 3258
sio 449| 0 -1 -1 43 -11 38 -.53 19 19 | --- --- --- ---
Table 2.1794.6 GPS week: 1794 Day: 6 MJD: 56808.000
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 245| -2 1 -3 14 35 -7 -.02 11 10 | -1095 -8 18 113
emr 80| 1 0 -1 31 -10 21 .25 11 11 | 1102 -747 14 119
esa 150| 1 -1 -6 32 37 -3 -.33 11 11 | 368 -3023 11 137
gfz 187| 2 -2 0 0 8 -28 -.03 14 14 | -83 -247 15 155
grg 177| 3 1 12 -4 26 -14 .23 16 15 | -75 -21 17 165
igr n/a| 0 0 -1 32 28 -25 -.22 6 6 | 9384 -724 18 97
jpl 80| -2 1 -4 17 -14 26 .02 13 12 | 963 -704 19 153
mit 300| 1 -2 5 -63 -9 -5 -.01 16 14 | 37 -70 22 193
ngs 232| -1 1 1 -58 -64 -10 .03 13 10 | -1113 53 1417 3231
sio 431| 1 -1 0 -27 9 5 -.66 21 21 | --- --- --- ---
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 3.1794.0 GPS week: 1794 Day: 0 MJD: 56802.000
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 8 18 9 12 5 16 10 14 11 4 | 41 45 41 48 55 42 46 46 42 43 43
2 | 9 8 11 10 12 4 11 12 8 15 3 | 20 24 22 26 24 19 20 27 23 22 22
3 | 7 11 10 8 12 5 12 13 13 16 4 | 38 39 39 37 36 37 36 35 35 38 35
4 | 7 9 9 10 13 4 10 12 9 29 3 | 25 26 24 31 31 23 23 32 29 42 26
5 | 12 13 14 12 16 3 15 11 10 18 5 | 42 45 42 34 34 38 44 32 36 37 37
X6 | 20 --- 33 --- --- 32 --- 2256 49 --- 24 | 405 --- 320 --- --- 406 --- 9999 320 --- 405
7 | 7 11 12 10 15 6 12 10 11 32 4 | 26 29 23 28 30 22 26 26 24 34 25
8 | 6 9 11 10 11 4 10 7 7 12 3 | 23 25 26 28 22 22 26 25 22 28 24
X9 | 10 12 11 12 --- 16 13 13 13 --- 5 | 13 16 11 15 --- 9 6 10 17 --- 11
10 | 7 8 11 8 14 5 8 10 6 20 3 | 24 25 24 26 28 23 24 25 25 32 23
11 | 8 10 16 9 14 4 14 12 15 25 4 | 37 43 35 41 51 37 42 43 40 47 38
12 | 8 22 6 15 17 7 22 10 12 17 5 | 32 36 24 33 29 27 32 29 28 24 27
13E | 7 13 9 11 15 5 13 15 14 8 4 | 27 30 28 29 32 26 28 25 31 26 27
14E | 10 11 7 8 17 7 11 21 11 14 4 | 23 22 19 21 17 20 18 24 23 23 19
15E | 8 14 6 15 23 6 18 11 14 15 5 | 28 29 31 30 25 30 32 27 29 29 27
16E | 11 18 8 14 17 5 11 15 17 13 5 | 34 39 35 40 38 34 32 40 38 33 35
17 | 7 10 11 10 17 4 16 11 10 19 4 | 20 25 18 26 29 19 24 24 23 20 20
18 | 12 14 12 12 21 5 13 11 12 28 5 | 30 32 28 34 35 29 27 30 28 31 28
19 | 7 13 12 11 17 4 13 31 9 27 5 | 33 35 32 34 37 31 33 37 32 31 30
20 | 7 11 16 8 14 5 10 15 13 16 4 | 34 37 37 40 44 34 35 34 38 34 35
21 | 10 8 10 8 11 5 11 10 10 28 3 | 24 27 26 27 32 24 24 29 25 29 25
22 | 11 11 12 9 19 4 12 13 15 25 4 | 30 32 32 34 39 32 29 36 30 33 30
23E | 8 10 9 10 14 6 12 14 11 9 4 | 29 31 28 31 28 28 29 27 32 33 28
24 | 10 11 11 8 11 6 12 8 9 9 4 | 24 24 24 25 24 21 27 22 21 21 22
25 | 8 11 13 6 22 5 14 8 10 12 4 | 27 27 29 25 30 24 28 26 23 25 25
26E | 14 17 10 8 15 6 13 30 19 19 6 | 77 78 74 76 74 74 76 87 68 69 75
X27 | 8 12 14 9 --- 4 12 13 15 12 5 | 69 69 72 70 --- 69 71 68 72 71 69
28E | 9 9 7 14 13 4 13 15 14 14 4 | 49 50 47 52 51 45 48 47 44 46 47
29 | 9 14 10 13 17 6 16 13 9 17 4 | 23 26 19 21 24 17 22 21 19 18 18
X30 | 8 10 11 8 --- 7 --- 1581 10 --- 4 | 22 26 25 20 --- 21 --- 9999 20 --- 21
31 | 7 13 15 8 15 7 11 11 12 16 4 | 28 30 23 29 34 22 28 26 26 20 25
32 | 7 8 13 7 14 4 9 10 10 17 3 | 26 27 28 26 25 26 27 25 25 31 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 11 10 16 5 13 14 12 19 |T 43 33 40 33 34 41 32 32 40 33 42
WRMS | 9 12 12 11 15 5 13 12 10 17 |NE 25 28 24 26 29 23 25 25 24 26 23
MEDI | 8 11 11 10 15 5 12 12 11 16 |MD 28 30 28 30 31 26 28 27 28 31 27
Table 3.1794.1 GPS week: 1794 Day: 1 MJD: 56803.000
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 12 17 5 14 6 18 9 8 12 4 | 32 39 27 31 40 29 39 33 31 32 31
2 | 6 8 12 12 10 5 8 14 10 17 4 | 12 16 15 14 16 12 15 15 19 16 13
3 | 7 9 10 8 11 4 9 8 9 15 3 | 37 40 37 40 38 38 38 38 42 42 38
4 | 7 8 8 11 12 4 9 12 11 27 3 | 17 17 14 19 22 16 16 20 21 30 16
5 | 11 16 13 13 17 5 13 12 7 22 4 | 34 40 31 27 39 28 36 26 31 25 31
X6 | 13 --- 15 --- --- 23 --- 2129 95 --- 14 | 197 --- 193 --- --- 204 --- 9999 198 --- 198
7 | 8 12 12 9 15 5 9 10 13 27 4 | 25 27 19 22 28 18 23 22 23 22 21
8 | 6 10 10 9 15 4 8 6 10 12 3 | 18 21 17 17 15 15 19 17 18 20 16
X9 | 9 11 10 13 --- 8 --- 11 10 --- 4 | 14 18 11 20 --- 13 --- 14 17 --- 13
10 | 7 12 12 7 17 4 8 11 7 20 3 | 19 22 21 19 22 17 19 16 22 26 18
11 | 8 11 14 8 16 3 12 9 7 38 4 | 31 39 31 31 42 30 37 34 28 52 31
12 | 7 20 7 15 19 5 24 11 8 17 5 | 23 27 19 27 30 18 26 25 24 17 21
13E | 9 12 6 11 16 3 11 10 7 7 4 | 30 29 21 25 27 22 29 21 26 23 24
14E | 12 10 6 6 21 5 11 16 15 14 4 | 21 18 13 17 21 14 16 14 22 22 15
15E | 8 20 5 10 22 5 16 15 13 16 5 | 24 24 22 23 18 21 23 17 28 21 20
16 | 11 20 9 13 19 6 13 13 8 17 5 | 35 41 33 37 38 34 37 39 36 33 35
17 | 5 12 11 11 16 5 14 8 12 19 4 | 18 23 16 24 30 17 21 19 24 14 18
18 | 13 16 12 12 22 6 14 12 11 24 5 | 17 27 19 21 34 19 22 18 23 20 18
19 | 8 12 11 12 18 4 14 30 9 25 5 | 33 37 32 36 38 31 35 37 34 29 32
20 | 10 12 13 11 13 6 11 10 8 16 4 | 34 38 32 39 40 35 36 36 34 33 34
21 | 8 9 9 8 15 6 9 12 9 28 3 | 19 23 20 20 26 20 22 21 20 23 19
22 | 11 11 12 11 16 5 12 9 13 24 4 | 19 25 21 25 33 22 24 19 25 21 21
23E | 10 12 7 14 12 6 15 21 8 12 5 | 16 21 16 22 16 15 18 26 17 18 15
24 | 9 8 11 7 10 5 9 11 10 10 3 | 19 21 21 18 25 17 23 20 23 17 19
25 | 7 11 14 7 20 5 14 12 10 14 4 | 18 21 26 21 31 18 23 18 24 20 20
26E | 12 15 10 8 15 6 14 31 10 20 5 | 76 75 73 73 74 74 75 75 74 74 74
X27 | 7 16 14 8 --- 4 13 7 9 13 4 | 73 72 75 73 --- 72 76 72 76 79 73
28E | 10 9 7 10 16 8 11 15 8 17 4 | 64 59 60 65 58 57 62 55 63 57 60
29 | 8 16 11 12 22 6 18 16 12 19 5 | 20 26 20 16 29 14 25 16 20 12 16
X30 | 10 11 10 11 --- 7 18 1597 7 --- 5 | 18 25 19 17 --- 15 32 9999 20 --- 19
31 | 8 12 14 8 16 7 11 9 10 23 4 | 23 28 18 26 34 18 24 23 26 19 23
32 | 6 8 13 8 15 4 6 12 8 15 3 | 20 24 20 19 22 18 22 18 21 18 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 10 16 5 13 14 10 20 |T 33 31 31 28 31 30 30 27 34 28 31
WRMS | 8 13 11 10 15 5 12 11 9 18 |NE 19 24 19 20 28 17 23 19 22 19 19
MEDI | 8 12 11 10 16 5 12 12 9 17 |MD 21 26 21 23 30 18 24 21 24 22 20
Table 3.1794.2 GPS week: 1794 Day: 2 MJD: 56804.000
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 | 6 10 15 10 15 7 17 8 11 19 4 | 30 41 32 36 47 33 43 35 37 40 35
2 | 8 9 13 10 11 4 12 11 9 13 4 | 23 26 22 23 22 20 22 25 25 20 22
3 | 7 9 10 8 13 7 9 8 10 12 3 | 31 37 33 33 37 32 36 35 35 38 34
4 | 5 8 9 8 14 5 7 12 10 22 3 | 24 29 23 26 28 23 26 29 26 30 25
5 | 10 16 15 15 16 4 14 12 14 18 5 | 38 49 36 35 37 33 41 30 31 31 35
X6 | 16 --- 23 --- --- 31 --- 2001 101 --- 19 | 310 --- 242 --- --- 294 --- 9999 249 --- 303
7 | 7 10 11 12 17 4 12 7 10 35 4 | 29 33 25 31 33 25 27 26 27 31 27
8 | 7 8 10 11 11 3 10 6 11 9 3 | 25 31 26 27 25 24 28 25 26 24 26
X9 | 9 37 --- 14 --- 15 --- 15 29 --- 11 | 14 37 --- 16 --- 18 --- 16 24 --- 13
10 | 5 9 13 10 14 4 8 9 11 17 3 | 25 28 24 24 27 24 23 25 25 31 24
11 | 8 9 14 10 14 4 9 7 11 21 4 | 28 39 32 36 43 31 37 35 36 40 33
12 | 8 21 9 16 22 5 20 10 12 18 5 | 29 34 26 32 28 25 33 27 26 22 26
13E | 8 12 8 10 18 4 12 8 8 9 4 | 35 36 32 33 38 31 32 31 33 31 33
14E | 10 11 6 8 13 5 13 10 10 15 4 | 26 23 20 21 22 18 22 20 24 24 21
15E | 12 16 6 14 28 4 17 11 16 21 5 | 35 37 36 39 29 34 34 31 31 34 33
16 | 10 16 9 12 20 8 10 17 14 13 5 | 28 33 27 33 34 28 29 32 32 27 28
17 | 8 9 13 13 16 5 13 10 12 16 4 | 24 28 19 25 30 20 25 23 26 17 22
18 | 12 12 13 11 21 6 14 11 11 32 5 | 28 31 26 30 30 24 27 27 25 27 26
19 | 9 11 12 12 18 5 11 29 9 26 5 | 32 39 32 35 41 32 33 36 37 28 32
20 | 9 11 13 10 11 4 11 11 10 15 4 | 36 37 32 39 41 32 35 35 33 33 34
21 | 8 9 10 9 12 4 7 11 13 26 3 | 19 24 21 24 26 20 21 25 24 20 21
22 | 12 10 13 9 18 3 13 9 10 26 4 | 28 28 28 27 32 24 27 26 29 26 26
23E | 9 10 7 10 13 5 13 10 7 11 3 | 29 29 25 27 26 24 25 27 25 25 25
24 | 11 8 12 12 15 4 10 6 9 10 4 | 29 29 29 30 25 25 28 23 23 24 26
25 | 7 15 14 6 21 4 13 9 14 11 4 | 26 30 31 28 27 24 30 23 20 22 25
26E | 12 19 8 13 15 7 14 36 16 14 7 | 60 63 59 62 54 60 61 52 63 59 58
X27 | 6 15 14 9 --- 4 9 9 11 12 4 | 72 72 73 71 --- 72 74 74 77 79 73
28 | 7 10 9 12 18 9 11 12 13 13 4 | 55 57 54 55 59 52 55 54 50 51 53
29 | 10 15 11 12 20 6 16 12 14 18 5 | 27 28 24 26 25 19 25 20 19 19 21
X30 | 10 9 12 15 --- 7 16 1606 9 --- 5 | 28 32 26 24 --- 24 35 9999 25 --- 26
31 | 12 13 14 11 17 6 11 9 10 24 4 | 31 32 24 31 36 24 27 25 25 22 27
32 | 8 7 11 8 15 5 6 10 8 16 3 | 26 28 27 25 25 24 23 25 26 28 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 11 11 17 5 12 13 11 19 |T 40 35 37 32 33 37 32 30 37 31 38
WRMS | 9 12 11 11 17 5 12 10 10 19 |NE 26 31 26 27 29 23 28 24 25 24 24
MEDI | 8 10 12 11 15 5 12 10 11 16 |MD 28 32 27 30 30 24 28 27 26 28 26
Table 3.1794.3 GPS week: 1794 Day: 3 MJD: 56805.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1M | 8 10 16 10 16 8 16 10 8 23 4 | 38 44 36 44 50 37 44 41 37 44 39
2 | 6 6 11 11 11 3 11 15 10 22 4 | 13 18 17 15 20 14 15 24 18 19 15
3M | 13 12 10 10 19 8 12 11 9 16 4 | 49 49 48 48 46 45 49 50 50 51 47
4M | 13 9 10 10 10 6 9 16 9 29 4 | 18 21 17 21 24 16 17 29 19 32 18
5 | 14 14 13 17 17 7 12 14 11 22 5 | 42 45 37 33 33 34 41 31 41 33 36
X6M | 19 --- 22 --- --- 38 --- 1914 102 --- 21 | 265 --- 179 --- --- 268 --- 9999 171 --- 263
7 | 12 8 11 12 16 5 13 11 9 33 4 | 24 24 17 24 30 18 21 24 23 29 20
8 | 7 10 11 11 9 4 10 9 7 17 3 | 18 22 20 21 20 16 20 22 19 27 18
10 | 6 10 13 10 12 5 8 14 6 19 3 | 17 22 18 20 22 16 18 24 20 27 18
11M | 10 11 14 9 16 4 10 10 11 29 4 | 38 45 37 39 49 39 42 41 35 48 38
12 | 10 23 7 18 19 5 21 11 12 14 6 | 24 28 17 33 28 19 28 22 21 18 20
13E | 11 12 7 13 14 6 13 7 9 10 4 | 40 35 35 39 38 32 33 37 33 35 35
14E | 9 15 6 10 12 5 15 12 8 15 4 | 20 21 16 19 18 16 21 19 19 20 17
15E | 13 15 8 11 20 5 18 17 12 18 5 | 33 30 30 30 26 28 28 30 32 32 28
16 | 11 17 6 11 17 6 14 15 7 16 4 | 23 25 18 23 28 21 21 24 27 17 21
17 | 12 10 14 11 16 4 12 13 9 21 4 | 22 23 18 24 29 16 21 24 21 20 19
18 | 13 14 13 10 18 5 17 12 12 29 5 | 23 30 22 26 33 23 29 27 24 25 23
19M | 12 12 13 13 17 8 13 30 10 26 6 | 41 42 39 44 47 39 41 45 41 35 39
20M | 11 13 12 12 15 4 10 9 10 19 4 | 43 50 44 50 51 45 47 49 49 47 46
21M | 9 8 10 9 15 4 12 11 6 23 3 | 24 27 24 20 30 23 29 31 22 29 24
22 | 10 12 12 9 14 5 15 11 10 24 4 | 28 33 28 31 36 31 31 31 28 29 28
23E | 10 11 7 11 19 5 13 11 7 14 4 | 34 33 32 33 32 33 33 33 36 35 32
24 | 12 10 14 9 11 5 12 8 13 14 4 | 18 20 20 19 22 14 21 19 17 19 17
25 | 11 13 14 6 20 6 13 13 9 12 4 | 21 22 24 22 29 18 25 20 17 19 19
26E | 13 15 9 14 12 4 14 27 12 15 5 | 73 74 70 71 72 71 72 68 71 69 70
X27M | 15 21 16 14 --- 17 17 12 13 28 6 | 98 95 101 96 --- 94 98 101 97 106 97
28 | 8 10 8 11 18 6 8 19 12 23 4 | 42 40 40 42 44 38 40 35 38 35 38
29 | 10 17 11 15 18 6 18 16 10 18 5 | 19 24 17 19 23 14 22 19 17 17 15
X30 | 15 9 11 11 --- 7 18 1623 8 --- 5 | 20 24 20 16 --- 15 33 9999 17 --- 19
31 | 19 14 11 11 17 7 13 9 9 22 5 | 24 27 16 29 32 18 21 21 26 14 21
32M | 7 8 12 8 18 5 8 11 11 17 4 | 19 22 21 19 25 18 18 23 24 24 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 11 11 16 6 13 14 10 21 |T 39 33 34 32 33 36 32 33 35 32 37
WRMS | 11 12 11 11 15 6 12 12 9 21 |NE 22 25 20 23 27 19 24 23 22 22 20
MEDI | 11 12 11 11 16 5 13 12 10 19 |MD 24 27 24 26 30 23 28 29 26 29 23
Table 3.1794.4 GPS week: 1794 Day: 4 MJD: 56806.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 16 10 16 6 18 9 12 15 4 | 33 38 30 34 43 32 42 32 35 32 33
2 | 9 8 12 14 10 6 6 13 9 19 4 | 15 18 17 20 20 12 17 22 19 21 16
3 | 6 10 10 8 13 4 12 11 12 15 4 | 26 28 26 24 26 22 24 25 23 29 23
4 | 10 8 10 10 16 8 7 15 10 27 4 | 25 21 20 24 26 20 21 29 30 31 22
5 | 12 15 14 14 15 7 11 11 13 25 5 | 32 39 29 26 32 29 31 26 28 27 28
X6 | 12 --- 14 --- --- 14 --- 1875 102 --- 13 | 135 --- 273 --- --- 141 --- 9999 278 --- 137
7 | 8 9 13 11 17 5 12 10 9 31 4 | 25 27 20 28 31 21 24 24 27 26 23
8 | 7 8 12 9 11 5 10 11 11 16 3 | 19 22 21 22 19 19 22 20 22 24 19
10 | 8 8 12 10 13 5 9 13 9 17 4 | 19 22 18 22 24 18 24 21 21 23 19
11 | 8 9 16 11 16 5 11 10 12 18 4 | 29 36 27 32 40 29 35 30 35 33 31
12 | 10 21 7 20 20 5 21 14 13 21 6 | 22 29 20 30 30 19 30 22 26 19 22
13E | 7 14 7 8 12 5 9 10 7 11 3 | 31 31 25 29 34 26 31 29 30 28 28
14E | 7 11 7 11 21 3 14 12 9 17 4 | 18 18 15 16 19 14 19 17 16 21 14
15E | 11 15 9 11 17 6 16 11 19 10 5 | 32 30 28 29 27 30 28 29 33 33 28
16 | 8 18 8 16 17 4 13 15 14 21 5 | 25 26 19 27 28 20 21 24 22 19 21
17 | 11 11 14 9 19 5 12 14 12 19 4 | 20 22 16 21 30 14 19 22 22 17 17
18 | 11 14 13 15 17 4 13 13 14 21 5 | 22 28 22 25 26 19 25 22 27 20 21
19 | 7 12 13 16 18 7 12 30 12 28 6 | 30 34 29 31 38 28 29 32 29 25 27
20 | 11 12 13 13 13 5 9 12 11 17 4 | 31 32 27 36 35 28 28 33 35 29 30
21 | 8 9 11 12 17 5 12 11 12 22 4 | 19 23 18 21 22 15 26 24 19 22 19
22 | 10 12 13 12 23 4 10 9 12 23 4 | 25 28 25 30 35 23 27 25 31 23 25
23E | 7 11 8 10 15 6 13 11 10 14 4 | 24 26 24 27 23 21 23 22 25 28 23
24 | 12 8 13 9 12 4 11 9 10 15 4 | 15 22 20 16 26 15 24 20 20 18 18
25 | 9 11 14 7 18 4 12 12 9 11 4 | 18 21 24 21 28 17 23 17 20 16 19
26E | 14 18 10 21 14 11 14 19 11 17 6 | 40 48 39 38 37 43 44 34 37 33 37
X27 | 8 13 15 10 --- 12 11 8 12 14 4 | 69 71 73 69 --- 71 72 70 74 74 70
28 | 6 9 8 12 17 5 11 18 13 17 4 | 34 34 28 34 40 30 28 28 38 26 31
29 | 11 16 9 13 17 3 13 12 10 21 4 | 18 21 16 20 21 14 20 17 20 19 15
X30 | 10 10 13 9 --- 6 15 1636 13 --- 5 | 22 23 20 17 --- 17 31 9999 24 --- 20
31 | 14 14 12 12 18 5 10 7 12 25 4 | 23 28 19 26 32 19 23 22 23 20 21
32 | 7 8 11 5 14 5 6 9 7 21 3 | 22 24 21 22 25 19 24 21 22 27 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 11 12 16 5 12 13 11 20 |T 29 29 32 27 29 27 27 26 35 26 28
WRMS | 9 12 12 11 16 5 11 11 10 18 |NE 21 25 20 23 27 18 24 21 23 21 20
MEDI | 9 11 12 11 16 5 12 12 12 18 |MD 25 27 22 26 28 20 24 24 26 25 22
Table 3.1794.5 GPS week: 1794 Day: 5 MJD: 56807.000
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 | 6 9 16 15 10 7 17 13 10 15 4 | 29 39 24 34 37 25 38 27 37 28 31
2 | 7 7 13 14 12 6 9 14 13 18 4 | 15 22 20 20 17 15 16 21 28 20 17
3 | 8 9 9 11 15 5 11 14 10 19 4 | 31 36 34 33 37 32 33 33 38 36 33
4 | 6 7 10 8 14 6 7 17 10 34 3 | 20 22 20 22 23 17 20 28 22 36 20
5 | 12 12 15 13 13 5 12 12 12 18 4 | 30 38 29 32 32 27 31 28 28 25 29
X6 | 2 --- --- --- --- 1063 --- --- --- --- 0 | 177 --- --- --- --- 9999 --- --- --- --- 179
7 | 8 10 13 8 16 6 10 13 10 29 4 | 22 26 17 23 29 18 21 23 28 22 21
8 | 8 10 12 11 13 4 6 12 7 19 3 | 23 24 23 24 21 22 21 21 27 27 22
10 | 7 7 13 10 15 7 8 12 9 16 3 | 16 22 16 20 20 15 19 21 20 23 17
11 | 7 9 16 13 12 5 12 11 7 17 4 | 26 34 26 31 34 23 32 26 29 31 27
12 | 9 20 8 19 23 7 21 16 13 16 6 | 22 31 19 30 31 17 26 20 23 14 21
13E | 8 11 9 9 16 4 13 13 10 10 4 | 23 27 20 26 31 21 23 25 27 21 23
14E | 9 11 6 10 17 4 13 13 10 19 4 | 20 21 17 21 14 17 19 17 25 20 18
15E | 8 13 10 10 21 4 17 12 15 15 5 | 25 22 25 26 21 24 23 24 31 33 23
16 | 11 19 8 17 18 6 13 14 11 15 5 | 21 25 21 26 27 19 21 22 28 18 20
17 | 9 10 12 10 13 4 13 14 9 13 4 | 22 27 17 22 29 16 22 22 24 15 20
18 | 12 12 12 13 19 5 13 12 9 28 4 | 21 26 22 23 23 18 23 20 25 25 19
19 | 8 11 10 14 18 5 13 32 9 26 5 | 33 39 33 36 41 33 33 34 41 22 33
20 | 8 11 13 11 11 5 11 18 11 19 4 | 41 44 38 46 44 39 42 46 43 40 42
21 | 9 7 9 12 12 6 12 12 11 24 4 | 18 23 22 21 19 19 20 21 27 16 20
22 | 12 11 12 12 18 5 10 10 10 24 4 | 21 27 25 24 28 22 23 22 26 26 22
23E | 8 11 10 12 18 5 14 12 9 13 4 | 28 26 28 31 27 27 26 26 31 31 26
24 | 10 9 14 8 16 5 11 13 9 11 4 | 20 23 22 21 28 18 24 21 26 19 21
25 | 7 10 13 10 18 4 11 10 9 12 4 | 19 21 24 22 28 16 22 15 21 17 19
26E | 9 17 14 12 13 8 11 20 11 16 5 | 73 73 70 67 71 71 70 60 71 69 69
X27 | 8 15 15 11 --- 8 11 9 10 16 4 | 76 75 79 75 --- 77 78 77 83 80 77
28 | 6 9 9 11 22 5 8 17 11 14 4 | 33 36 30 33 46 31 33 26 34 26 32
29 | 8 15 9 12 19 5 21 12 11 17 5 | 20 22 17 20 25 13 23 18 22 18 17
X30 | 8 9 13 7 --- 6 15 1645 8 15 4 | 18 24 21 18 --- 16 29 9999 22 11 20
31 | 8 17 11 14 18 4 12 8 14 21 5 | 23 27 19 30 32 19 22 19 24 18 21
32 | 7 10 11 7 14 4 7 13 9 23 3 | 23 28 25 21 24 21 24 25 28 32 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 12 12 16 5 13 15 11 19 |T 31 31 26 29 29 24 28 27 31 27 31
WRMS | 9 12 12 11 15 5 12 12 10 19 |NE 20 25 20 23 26 18 23 20 24 20 20
MEDI | 8 10 12 11 16 5 12 13 10 17 |MD 23 26 22 24 28 19 23 23 27 23 22
Table 3.1794.6 GPS week: 1794 Day: 6 MJD: 56808.000
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 16 13 11 6 17 12 10 9 4 | 44 53 41 50 56 43 52 45 42 43 45
2 | 10 8 11 14 15 4 11 17 12 23 4 | 20 23 23 26 20 20 20 32 28 23 21
3 | 6 10 10 10 16 6 12 18 9 16 4 | 30 33 32 27 32 27 30 30 27 31 28
4 | 24 10 11 13 16 9 9 18 13 32 5 | 32 27 25 32 29 24 24 37 30 37 26
5 | 13 10 12 12 15 5 15 14 12 21 5 | 45 46 41 41 41 39 48 37 42 36 41
X6 | 13 --- 12 --- --- 35 --- --- --- --- 13 | 69 --- 10 --- --- 377 --- --- --- --- 71
7 | 9 8 13 11 16 8 14 12 11 29 4 | 27 30 24 33 32 22 29 27 26 29 25
8 | 6 8 11 10 12 5 9 13 9 22 3 | 22 25 24 27 20 21 26 26 23 29 22
10 | 8 7 12 10 12 5 8 15 14 23 4 | 24 26 23 27 28 23 25 30 27 34 24
11 | 9 10 17 11 14 5 16 12 12 23 4 | 38 47 39 43 48 40 43 42 39 46 40
12 | 12 19 6 23 22 7 19 14 13 18 6 | 30 33 24 38 31 26 33 27 27 23 26
13E | 9 10 7 9 18 6 10 13 6 10 4 | 26 27 23 28 29 23 27 29 24 24 25
14E | 8 11 6 13 20 4 10 13 9 20 4 | 26 25 22 23 26 21 23 23 18 27 21
15E | 8 12 7 14 16 4 15 9 17 11 4 | 31 35 31 35 30 32 33 32 36 38 32
16 | 9 18 9 15 17 8 13 16 12 16 5 | 24 26 23 28 30 22 25 26 26 19 22
17 | 10 11 11 8 18 4 13 15 12 15 4 | 28 29 26 29 30 23 30 32 26 23 25
18 | 10 10 11 12 17 6 14 11 17 26 5 | 27 31 27 29 32 26 30 29 37 29 28
19 | 8 10 11 14 19 5 12 34 10 23 5 | 33 36 30 36 40 31 33 33 32 24 30
20 | 9 10 13 23 11 7 11 16 17 24 5 | 45 45 37 54 49 41 43 46 45 41 43
21 | 8 7 9 10 9 5 9 10 8 29 3 | 23 28 24 26 28 24 28 30 27 27 25
22 | 11 9 11 15 16 5 12 11 11 26 4 | 30 33 31 36 40 31 30 32 34 33 31
23E | 12 13 8 16 13 5 18 16 8 11 5 | 39 36 35 37 32 35 30 33 32 32 32
24 | 12 10 13 11 14 5 11 19 12 14 5 | 21 25 25 25 29 20 26 27 25 20 22
25 | 11 13 12 9 19 5 14 11 13 16 4 | 24 26 28 25 29 22 29 22 21 21 23
26E | 13 18 13 16 18 12 15 28 21 12 6 | 73 78 71 78 70 72 76 80 76 79 74
X27 | 10 16 15 8 --- 5 14 11 11 15 5 | 74 75 77 72 --- 75 77 75 77 78 75
28 | 5 9 7 12 19 4 9 19 13 21 4 | 38 38 36 41 43 37 37 40 38 40 37
29 | 10 15 10 15 20 4 16 12 16 19 5 | 25 27 23 26 23 19 26 23 21 22 20
X30 | 9 9 13 11 --- 8 17 1659 11 15 5 | 25 27 28 23 --- 23 38 9999 28 20 26
31 | 22 11 13 12 18 7 12 12 13 20 5 | 30 30 23 29 36 23 29 27 28 21 25
32 | 5 8 14 18 13 4 5 12 8 23 4 | 29 31 30 30 31 27 30 29 28 35 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 11 14 16 6 13 16 12 21 |T 33 35 30 35 34 41 34 34 33 32 32
WRMS | 10 11 11 14 15 6 12 14 10 21 |NE 27 29 26 29 30 24 29 28 28 25 25
MEDI | 9 10 11 12 16 5 12 13 12 20 |MD 30 30 27 29 31 26 30 30 28 29 26
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 4.1794 GPS week: 1794 MJD: 56802.0-56808.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 |U 6 6 13 |U 6 8 25 |U 7 9 18 |
emr | emr 2914 | 8 9 18 |U 11 17 36 | 10 9 24 |
esa | esa 2989 | 7 7 16 |U 6 8 27 | 8 9 20 |
gfz | gfz 2914 |U 6 6 13 |U 7 13 33 |U 8 9 19 |
grg | grg 2688 |U 7 8 17 |U 12 22 43 |U 9 10 23 |
igr | igr 2969 | 6 7 15 | 6 8 24 | 8 10 21 |
igs | igs 2954 | 6 7 14 | 7 13 28 | 8 10 21 |
jpl | jpl 2875 | 8 11 19 | 10 22 38 |U 9 10 24 |
mit | mit 2989 | 15 14 29 |U 9 21 36 |U 8 10 22 |
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 5.1794.0 GPS week: 1794 Day: 0 MJD: 56802.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 | 5 6 12 | 6 10 25 | 8 8 14 |
emr | emr 2970 | 7 9 19 | 10 15 42 | 10 9 20 |
esa | esa 3072 | 6 9 18 | 6 9 25 | 8 7 17 |
gfz | gfz 2972 | 5 7 13 | 6 10 24 | 8 8 16 |
grg | grg 2688 | 5 6 17 | 10 15 41 | 9 10 22 |
igr | igr 3010 | 5 7 14 | 6 9 24 | 8 8 16 |
igs | igs 3000 | 5 7 14 | 6 9 26 | 9 9 20 |
jpl | jpl 2875 | 6 10 19 | 10 23 48 | 10 10 21 |
mit | mit 3072 | 5 7 22 | 10 20 33 | 9 8 19 |
Table 5.1794.1 GPS week: 1794 Day: 1 MJD: 56803.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 6 7 14 | 7 8 28 | 7 6 17 |
emr | emr 2972 | 9 9 16 | 10 20 38 | 10 8 28 |
esa | esa 3072 | 7 9 15 | 7 9 27 | 8 7 20 |
gfz | gfz 2972 | 6 8 13 | 7 8 28 | 8 7 18 |
grg | grg 2688 | 9 11 17 | 9 22 54 | 9 9 20 |
igr | igr 3033 | 6 10 14 | 6 9 27 | 8 7 21 |
igs | igs 3032 | 7 9 13 | 8 22 38 | 8 7 20 |
jpl | jpl 2876 | 9 13 18 | 8 22 45 | 11 9 26 |
mit | mit 3072 | 8 10 20 | 10 26 33 | 11 14 35 |
Table 5.1794.2 GPS week: 1794 Day: 2 MJD: 56804.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3035 | 6 7 20 | 5 8 21 | 5 8 14 |
emr | emr 2953 | 7 9 18 | 10 17 38 | 8 9 23 |
esa | esa 2976 | 7 8 18 | 6 10 26 | 7 8 17 |
gfz | gfz 2954 | 6 8 20 | 6 14 27 | 6 8 15 |
grg | grg 2688 | 7 9 18 | 10 18 42 | 8 8 14 |
igr | igr 3021 | 7 9 19 | 5 8 21 | 6 9 16 |
igs | igs 2984 | 6 7 18 | 6 9 22 | 6 7 16 |
jpl | jpl 2876 | 8 12 20 | 7 19 41 | 9 9 22 |
mit | mit 3072 | 9 10 20 | 7 16 41 | 7 9 19 |
Table 5.1794.3 GPS week: 1794 Day: 3 MJD: 56805.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 5 5 13 | 5 7 26 | 11 16 24 |
emr | emr 2876 | 6 6 17 | 10 16 31 | 9 9 18 |
esa | esa 2976 | 7 6 16 | 6 7 27 | 11 16 24 |
gfz | gfz 2876 | 5 5 10 | 5 8 24 | 12 17 25 |
grg | grg 2688 | 6 6 13 | 9 18 39 | 12 14 28 |
igr | igr 2939 | 6 6 14 | 5 7 24 | 12 16 27 |
igs | igs 2963 | 5 5 13 | 7 18 27 | 11 16 24 |
jpl | jpl 2876 | 7 9 22 | 11 26 33 | 9 9 17 |
mit | mit 2976 | 6 6 17 | 7 21 38 | 9 10 17 |
Table 5.1794.4 GPS week: 1794 Day: 4 MJD: 56806.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 7 8 12 | 7 7 21 | 7 8 20 |
emr | emr 2876 | 8 13 19 | 11 16 27 | 9 8 24 |
esa | esa 2976 | 8 10 18 | 6 7 26 | 7 8 19 |
gfz | gfz 2876 | 7 9 13 | 8 16 41 | 7 7 19 |
grg | grg 2688 | 8 12 19 | 12 18 30 | 10 10 25 |
igr | igr 2962 | 7 9 14 | 6 7 22 | 7 8 19 |
igs | igs 2954 | 7 10 14 | 8 17 32 | 7 8 21 |
jpl | jpl 2876 | 9 13 18 | 10 25 35 | 9 8 23 |
mit | mit 2976 | 61 50 96 | 8 21 34 | 8 8 26 |
Table 5.1794.5 GPS week: 1794 Day: 5 MJD: 56807.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2878 | 6 5 13 | 6 8 25 | 6 7 19 |
emr | emr 2876 | 10 8 22 | 10 19 35 | 9 10 27 |
esa | esa 2880 | 7 6 15 | 6 9 26 | 8 10 25 |
gfz | gfz 2877 | 6 5 12 | 8 16 38 | 7 9 23 |
grg | grg 2688 | 9 6 19 | 17 31 56 | 9 11 27 |
igr | igr 2879 | 7 6 13 | 5 9 23 | 8 10 25 |
igs | igs 2834 | 7 5 13 | 6 8 23 | 6 10 25 |
jpl | jpl 2876 | 9 10 19 | 7 16 29 | 9 10 29 |
mit | mit 2880 | 6 6 13 | 8 23 34 | 8 10 19 |
Table 5.1794.6 GPS week: 1794 Day: 6 MJD: 56808.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 4 3 12 | 7 9 29 | 7 9 19 |
emr | emr 2876 | 7 6 18 | 15 16 39 | 10 10 28 |
esa | esa 2976 | 6 4 14 | 8 8 33 | 9 11 21 |
gfz | gfz 2876 | 4 3 13 | 8 19 48 | 8 10 21 |
grg | grg 2688 | 7 5 18 | 20 33 37 | 10 10 26 |
igr | igr 2945 | 5 4 13 | 7 7 28 | 8 10 22 |
igs | igs 2917 | 5 4 12 | 8 7 29 | 8 12 24 |
jpl | jpl 2876 | 6 7 15 | 15 25 38 | 9 13 31 |
mit | mit 2880 | 7 7 17 | 11 20 39 | 8 11 22 |
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 6.1794 GPS week: 1794 MJD: 56802.500-56808.500
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 -13 85 -112 -4 | 21 32
| 15 21 52 78 5 | 1
emr uuuuu | 20 20 -150 59 -16 | 37 46
| 23 14 80 77 9 | 7
esa uuuuu | -22 -8 59 -23 -3 | 20 29
| 11 18 35 76 7 | 2
gfz uuuuu | -15 6 22 -75 0 | 14 27
| 15 22 71 36 5 | 3
grg uuuuu | 16 -7 -104 45 10 | 31 36
| 27 17 87 106 4 | 3
igr xxxxx | 3 -29 14 1 -1 | 1 22
| 20 12 50 48 4 | 3
irf xxxxx | -3 -14 -39 -40 2 | 6 21
| 10 14 45 22 3 | 2
jpl uuuuu | 61 -18 -38 93 -17 | 38 47
| 23 17 72 64 10 | 7
mit uuuuu | 8 -37 -81 -14 2 | 26 33
| 25 27 100 60 5 | 2
ngs uuuuu | 12 52 119 78 5 | 11 21
| 59 63 74 87 5 | 2
sio xxxxx | 19 -1 56 35 2 | 50 53
| 27 37 78 46 8 | 2
Table 7.1794.0 GPS week: 1794 Day: 0 MJD: 56802.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -66 -42 95 -125 1 | 22 30
emr uuuuu | 27 4 12 162 -21 | 47 51
esa uuuuu | -33 10 19 -95 9 | 23 28
gfz uuuuu | -20 -6 -23 -105 -1 | 18 26
grg uuuuu | 34 -31 -227 153 13 | 28 33
igr xxxxx | 4 -33 9 47 -4 | 4 18
irf xxxxx | -11 -20 -22 -69 -2 | 8 19
jpl uuuuu | 95 0 -6 147 -17 | 48 52
mit uuuuu | -23 -30 7 -85 -4 | 28 33
ngs uuuuu | 39 98 12 76 -3 | 14 21
sio xxxxx | -4 -14 108 99 5 | 49 52
Table 7.1794.1 GPS week: 1794 Day: 1 MJD: 56803.500
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 -10 62 -107 -5 | 23 30
emr uuuuu | 45 28 -138 127 -19 | 44 49
esa uuuuu | -26 -25 41 -82 -6 | 24 29
gfz uuuuu | -6 -3 -84 -120 -8 | 18 26
grg uuuuu | 17 -11 -82 102 12 | 30 34
igr xxxxx | -4 -45 13 -7 -7 | 4 19
irf xxxxx | 2 -33 17 -52 1 | 8 19
jpl uuuuu | 66 -25 -115 81 -21 | 47 52
mit uuuuu | 3 -76 39 -35 2 | 28 33
ngs uuuuu | -12 96 191 135 12 | 13 21
sio xxxxx | 47 -59 120 78 16 | 50 52
Table 7.1794.2 GPS week: 1794 Day: 2 MJD: 56804.500
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 18 161 -138 1 | 20 32
emr uuuuu | 50 16 -168 106 -23 | 38 48
esa uuuuu | -17 -1 76 -37 1 | 20 30
gfz uuuuu | -37 -6 -24 -97 7 | 13 28
grg uuuuu | 21 7 -93 177 8 | 28 33
igr xxxxx | 3 -28 94 -32 3 | -1 25
irf xxxxx | 7 -4 -77 -14 5 | 4 23
jpl uuuuu | 53 -8 -122 -4 -35 | 42 51
mit uuuuu | 36 -16 -178 63 4 | 24 33
ngs uuuuu | -28 -16 232 70 1 | 9 22
sio xxxxx | 46 32 -45 32 7 | 48 51
Table 7.1794.3 GPS week: 1794 Day: 3 MJD: 56805.500
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 | -49 4 73 -221 0 | 21 33
emr uuuuu | 12 31 -189 -24 -27 | 36 46
esa uuuuu | 0 15 20 -69 -11 | 20 31
gfz uuuuu | 5 25 120 -27 6 | 13 28
grg uuuuu | 37 15 -70 40 16 | 29 36
igr xxxxx | 34 -17 57 62 -2 | -1 24
irf xxxxx | 10 2 -62 -38 -1 | 5 24
jpl uuuuu | 71 -21 46 131 -16 | 37 47
mit uuuuu | 40 -28 -173 15 -4 | 25 34
ngs uuuuu | -65 -39 82 178 6 | 9 21
sio xxxxx | 42 35 25 45 -2 | 50 54
Table 7.1794.4 GPS week: 1794 Day: 4 MJD: 56806.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -66 -17 41 -166 -1 | 19 31
emr uuuuu | -9 17 -243 57 -15 | 31 43
esa uuuuu | -28 -30 117 -10 -8 | 18 29
gfz uuuuu | -26 -28 92 -49 -2 | 11 27
grg uuuuu | -3 -14 -61 -6 12 | 29 36
igr xxxxx | 4 -45 -2 -69 4 | -3 24
irf xxxxx | -11 -22 -17 -7 5 | 3 22
jpl uuuuu | 74 4 -74 37 -16 | 32 42
mit uuuuu | 19 -65 -51 61 9 | 23 31
ngs uuuuu | 56 125 123 135 4 | 8 20
sio xxxxx | 18 -31 -7 31 -2 | 49 53
Table 7.1794.5 GPS week: 1794 Day: 5 MJD: 56807.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -24 -35 144 10 -10 | 21 32
emr uuuuu | 21 39 -135 -42 -8 | 31 43
esa uuuuu | -25 -3 61 10 -5 | 19 29
gfz uuuuu | 0 22 40 -41 -4 | 13 26
grg uuuuu | 41 6 -212 -25 7 | 32 37
igr xxxxx | 12 -21 -62 35 -2 | -1 23
irf xxxxx | -7 1 -108 -50 0 | 5 21
jpl uuuuu | 45 -42 54 82 -3 | 30 41
mit uuuuu | -18 0 -200 -58 1 | 25 32
ngs uuuuu | -15 22 70 41 8 | 10 19
sio xxxxx | -22 34 18 -11 -4 | 51 54
Table 7.1794.6 GPS week: 1794 Day: 6 MJD: 56808.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -38 -10 18 -36 -11 | 22 32
emr uuuuu | -9 1 -187 26 -2 | 31 44
esa uuuuu | -28 -20 78 125 0 | 20 30
gfz uuuuu | -20 35 31 -83 0 | 15 27
grg uuuuu | -36 -19 18 -123 3 | 36 41
igr xxxxx | -32 -18 -9 -31 -1 | 1 23
irf xxxxx | -15 -23 -2 -53 3 | 7 22
jpl uuuuu | 25 -33 -52 179 -12 | 31 42
mit uuuuu | 0 -44 -8 -58 8 | 27 34
ngs uuuuu | 110 78 124 -87 5 | 13 22
sio xxxxx | 3 -3 172 -31 -6 | 53 56
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