[IGSREPORT-22831] Wk 1796 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat Jun 28 19:42:30 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1796 (Jun 08, 2014 - Jun 14, 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:
igs1796[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1796[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1796[0-6].cls IGS GPS clock combination summary report.
igs17967.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17967.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 | ESA | GUAT IRKJ GUAT IRKJ UNSA
0 | GFZ | 1 2 18 30 1 18 30 BAKE FAIR FLIN KOUC NTUS QAQ1 SCOR
0 | GFZ | YELL YIBL BAKE FAIR FLIN NTUS NYAL QAQ1 SCOR YIBL
0 | GRG | 26 26 FAA1 HYDE IRKJ MAL2 NTUS FAA1 HYDE KOUC MAL2
0 | GRG | NTUS WUHN
0 | JPL | 26
0 | MIT | 6 26 6 26 NRC1 REYK
1 | EMR | WUHN
1 | ESA | UNSA
1 | GFZ | 1 2 30 1 30 CAS1 CHUR IRKJ MDVJ NTUS WSRT WUHN CAS1
1 | GFZ | IRKJ NTUS
1 | GRG | 26 26 KOUC NRIL NRMD NTUS KOUC NRIL NRMD NTUS
1 | JPL | 26 TIXI
1 | MIT | 26 26 IRKJ IRKJ MDVJ
2 | COD | GRAZ
2 | ESA | IRKJ WUHN UNSA
2 | GFZ | 1 2 30 1 30 GRAZ INVK MAL2 MATE WUHN INVK IRKJ MAL2
2 | GFZ | MATE
2 | GRG | 3 26 3 26 FAA1 IRKJ KOUC NRMD SOFI FAA1 KOUC NRMD
2 | GRG | SOFI
2 | JPL | 26
2 | MIT | 6 26 6 26 IRKJ MDVJ
3 | EMR | WUHN WUHN
3 | ESA | MBAR UNSA WUHN
3 | GFZ | 1 6 30 1 6 30 INVK WUHN INVK
3 | GRG | 3 6 26 3 6 26 BOR1 MAC1 MAS1 MAC1 MAS1 SUTH
3 | JPL | 3 26
3 | MIT | 26 10 26 MDVJ
4 | COD | FLIN REUN
4 | ESA | CHUR FLIN HARB IRKJ KERG MAG0 CHUR HARB IRKJ KERG
4 | ESA | MAG0 UNSA
4 | GFZ | 1 2 6 18 30 1 6 18 30 DUBO KERG DUBO KERG
4 | GRG | 3 6 3 6 BOR1 IRKJ ISPA KELY KERG NRMD CHUR DUBO IRKJ
4 | GRG | ISPA KELY KERG NRMD
4 | JPL | 3 26
4 | MIT | 7 10 26 7 10 26 MDVJ PARC TLSE
5 | COD | 3
5 | ESA | 3 NNOR WUHN NNOR UNSA WHIT
5 | GFZ | 1 2 6 30 1 6 30 IRKJ
5 | GRG | 6 3 6 GRAZ KELY KOUC NRMD WUHN GRAZ KELY KOUC NRMD
5 | JPL | 26
5 | MIT | 26 26 IRKJ SPT0 IRKJ MDVJ SPT0
6 | COD | 3 MAW1 MAW1
6 | EMR | WUHN SYOG WUHN
6 | ESA | 3 IRKJ IRKJ UNSA
6 | GFZ | 1 2 6 30 1 6 30 KELY MCM4 WUHN KELY MCM4 WUHN
6 | GRG | 6 6 IRKJ QAQ1 REUN FAA1 IRKJ QAQ1 REUN
6 | JPL | 26
6 | MIT | 12 26 12 26 MDVJ
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following 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
----+------------+----------
G04 | 2014_06_12 | 2014051
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
----+--------+---------------
3 | GRG | 6
4 | GRG | 6
5 | GRG | 6
6 | GRG | 6
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 G09 | | | | | | 4 | 4 |
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 | -.9 1.0 -.8 -28 16 -41 .35
EMR | 0 | 3.5 -1.5 15.3 -2 7 -34 .04
ESA | 0 | .6 .3 -1.5 -10 -7 15 .21
GFZ | 0 | -.1 .3 -1.7 -22 -27 -11 -.11
GRG | 0 | 8.5 -5.8 24.9 -5 18 -35 .20
JPL | 0 | -5.2 4.3 5.4 -69 -9 -4 -.16
MIT | 0 | 8.1 -4.2 14.4 -7 -1 -68 .25
NGS | 0 | -2.5 -5.0 23.7 -71 -44 -31 .30
SIO | 0 | 3.8 -.7 10.8 -9 14 -12 -.02
COD | 1 | -1.0 .0 -1.1 -48 16 -42 .27
EMR | 1 | 5.9 -4.7 12.7 -14 14 -62 .06
ESA | 1 | .6 .7 -1.5 -21 -25 8 .12
GFZ | 1 | .3 -.6 -2.0 -22 -29 -21 -.21
GRG | 1 | 7.9 -13.9 17.2 12 6 -13 .51
JPL | 1 | 1.4 -1.6 13.4 -58 48 -43 -.21
MIT | 1 | 8.7 -5.4 15.5 7 -4 -48 .50
NGS | 1 | -2.4 -3.5 32.7 -64 -82 -12 .41
SIO | 1 | 6.0 -2.8 27.5 13 -9 1 .10
COD | 2 | -.6 .1 -1.2 -51 15 -54 .24
EMR | 2 | 2.0 -4.8 18.8 -12 4 -68 .04
ESA | 2 | .0 .5 -1.3 -18 -22 16 .05
GFZ | 2 | .0 .6 -1.6 -22 -24 -16 -.40
GRG | 2 | 14.6 -5.9 26.0 -6 21 -49 .34
JPL | 2 | .1 5.4 16.8 -2 29 -31 -.15
MIT | 2 | 12.4 -4.6 19.2 7 5 -49 .40
NGS | 2 | -8.2 -8.9 28.3 -106 -22 -63 .37
SIO | 2 | 9.1 .6 18.4 6 40 -21 .10
COD | 3 | -.8 .3 -1.8 -57 21 -31 .34
EMR | 3 | 4.5 -.7 17.9 3 20 -69 .15
ESA | 3 | .0 .7 -1.7 -11 -15 28 .11
GFZ | 3 | .0 .8 -1.9 -23 -23 -8 -.23
GRG | 3 | 13.4 -8.0 25.2 -24 13 -20 .45
JPL | 3 | 2.7 3.9 16.6 -15 -15 -35 -.22
MIT | 3 | 5.0 -4.5 19.4 10 5 -33 .22
NGS | 3 | 1.3 -2.2 39.7 -135 -94 -5 .43
SIO | 3 | 8.3 1.8 20.6 21 42 21 .06
COD | 4 | -.5 .5 -.9 -33 13 -48 .39
EMR | 4 | 4.3 -1.0 13.4 7 24 -73 .21
ESA | 4 | .5 .1 -2.0 -13 -9 20 .22
GFZ | 4 | .1 .1 -1.9 -27 -33 -15 -.0
GRG | 4 | 8.8 -14.4 34.7 -12 17 -28 .78
JPL | 4 | 1.8 4.8 13.5 1 14 -38 -.0
MIT | 4 | -1.1 -5.1 20.2 -8 2 -47 .40
NGS | 4 | -.4 -13.8 30.5 -130 -48 -50 .53
SIO | 4 | 5.6 2.1 21.1 9 18 14 .26
COD | 5 | .1 .1 -.6 -30 8 -46 .60
EMR | 5 | 3.1 -7.9 22.0 -6 10 -71 .27
ESA | 5 | .6 .5 -1.8 -12 -9 2 .26
GFZ | 5 | -.2 .0 -2.1 -24 -38 -18 .20
GRG | 5 | 16.7 -12.6 20.1 -20 18 -30 .81
JPL | 5 | 3.4 -1.5 14.8 -11 8 -50 -.22
MIT | 5 | -2.1 -6.8 16.6 -3 0 -53 .37
NGS | 5 | -3.5 -4.5 24.3 -88 -11 -31 .57
SIO | 5 | 2.5 -.6 32.8 -8 -20 3 .35
COD | 6 | -.3 .4 -.4 -38 20 -64 .37
EMR | 6 | 2.8 -1.8 12.7 4 19 -70 .21
ESA | 6 | .0 .9 -1.3 -17 -3 6 -.07
GFZ | 6 | -.2 1.1 -2.1 -6 -32 -16 .01
GRG | 6 | 11.5 -6.0 22.4 -12 20 -18 .68
JPL | 6 | 1.6 3.0 12.7 -23 26 -34 -.16
MIT | 6 | -3.8 -5.6 18.9 1 -1 -55 .21
NGS | 6 | -2.7 -6.2 21.7 -62 -9 -25 .49
SIO | 6 | 1.8 -.3 34.5 22 -2 2 .03
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 1.1796.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1796.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 2.1796.[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 3.1796.[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 5.1796.0-6). 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 1796 summary. (Jun 08, 2014 - Jun 14, 2014)
Table 1.1796.a GPS week: 1796 MJD: 56816.000-56822.000
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 247| -1 1 -5 4 3 3 -.00 9 9 | -1654 280 15 105
| 0 0 1 11 14 9 .02 | 857 389
emr 80| 1 -3 2 -11 -16 21 .25 13 13 | 4285 -728 17 132
| 1 2 4 18 16 12 .03 | 1567 600
esa 150| 1 0 -9 1 10 -5 -.38 12 12 | 24 -711 11 159
| 0 0 1 12 16 13 .03 | 657 1515
gfz 196| 0 0 0 -5 9 -20 -.05 12 11 | -82 -32 12 131
| 0 1 0 18 20 29 .02 | 286 571
grg 180| 6 -2 12 17 -17 1 .39 15 15 | -8 -118 17 149
| 3 2 2 12 28 14 .08 | 288 594
igr n/a| 0 0 -4 7 -8 13 -.22 5 5 | 8055 -845 16 83
| 0 0 0 15 11 8 .03 | 1716 650
jpl 80| -1 1 -6 39 2 -3 .00 14 14 | 3581 -667 16 108
| 1 1 2 39 17 15 .03 | 1446 602
mit 300| 0 0 3 8 -1 11 -.10 13 12 | 176 -313 22 214
| 2 0 1 30 28 13 .07 | 497 585
ngs 230| -1 0 7 -36 6 -9 .04 12 9 | -13637 2667 1561 3261
| 0 0 3 41 27 15 .03 | 31301 6009
sio 467| 0 2 -4 -15 -2 20 -.91 20 18 | --- --- --- ---
| 1 1 1 20 18 17 .07 | --- ---
Table 1.1796.b GPS week : 1796 MJD: 56816.000-56822.000
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 4 5 4 4 4 5 |
2 | 4 4 4 4 5 4 4 |
3 | 6 6 7 7 6 10 6 |
4 | 4 4 4 4 0 5 5 |
5 | 6 6 6 6 6 6 6 |
6 | 7 7 6 7 6 6 7 |
7 | 5 4 5 4 4 4 4 |
8 | 4 3 4 4 4 4 4 |
9 | --- --- --- --- --- 0 14 |
10 | 4 3 4 4 4 4 5 |
11 | 4 5 4 4 4 4 4 |
12 | 5 5 6 6 6 6 6 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 4 4 4 5 |
15 | 6 5 6 6 6 6 6 |
16 | 5 5 6 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 5 4 5 4 5 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 5 4 4 5 5 |
22 | 4 5 4 4 4 4 4 |
23 | 4 4 4 5 4 4 4 |
24 | 4 4 4 4 5 6 6 |
25 | 4 4 4 5 5 5 5 |
26 | 10 8 7 7 7 8 8 |
27 | 4 5 5 5 5 5 5 |
28 | 5 5 5 5 5 5 5 |
29 | 5 6 6 6 6 5 6 |
30 | 4 4 4 4 4 5 4 |
31 | 4 5 5 4 4 5 5 |
32 | 4 4 4 3 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1796.0 GPS week: 1796 Day: 0 MJD: 56816.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 0 -6 13 16 -5 .01 10 9 | -1096 -339 15 106
emr 80| 0 -1 0 3 -15 38 .23 12 12 | 6333 177 15 137
esa 150| 2 0 -8 -8 40 -18 -.34 12 12 | 522 -1149 11 154
gfz 188| 0 0 1 -5 -2 -5 -.03 11 11 | 273 -118 12 137
grg 187| 5 -1 14 4 -9 -7 .34 13 12 | -2 366 15 164
igr n/a| -1 0 -4 1 -11 0 -.23 6 5 | 10516 -95 17 86
jpl 80| -3 0 -5 -8 -23 -27 .01 12 12 | 5590 139 16 116
mit 300| 2 0 5 47 11 36 -.21 15 12 | -10 330 23 215
ngs 234| -2 0 3 -48 -3 -9 -.01 14 10 | -1097 -339 2006 3682
sio 449| 2 2 -3 -15 10 46 -1.03 20 19 | --- --- --- ---
Table 2.1796.1 GPS week: 1796 Day: 1 MJD: 56817.000
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 1 -3 -14 -4 19 -.01 10 9 | -3378 713 16 108
emr 80| 0 -2 -2 13 -5 14 .29 13 13 | 5554 -833 17 129
esa 150| 1 0 -8 0 15 -7 -.35 12 12 | 648 -2701 12 156
gfz 200| 0 0 0 -14 4 7 -.04 12 11 | 113 -577 13 140
grg 187| 3 -1 10 37 -24 -7 .33 13 13 | -53 19 15 142
igr n/a| 0 0 -3 18 0 4 -.23 5 5 | 9712 -1391 18 98
jpl 80| -1 3 -8 -8 -3 -9 .06 14 12 | 5026 -1163 19 120
mit 300| 1 0 1 -21 -3 3 -.17 13 12 | 242 -633 24 211
ngs 236| -1 0 9 26 19 -34 .00 12 9 | -3369 718 1633 3205
sio 476| -1 1 -5 -22 -35 21 -.94 19 19 | --- --- --- ---
Table 2.1796.2 GPS week: 1796 Day: 2 MJD: 56818.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 1 -4 11 -9 11 .01 10 10 | -2015 337 16 101
emr 80| 1 -4 0 -34 -34 4 .23 12 12 | 4911 -324 13 115
esa 150| 2 0 -9 -14 -3 -3 -.39 12 13 | -74 425 12 170
gfz 200| 0 0 0 -31 12 -10 -.07 12 11 | 155 276 13 143
grg 186| 3 0 10 20 21 18 .29 13 13 | -193 135 16 143
igr n/a| 0 1 -3 -16 -9 14 -.21 5 5 | 8278 -364 17 89
jpl 80| -3 0 -6 44 -2 4 -.02 13 12 | 3810 -212 15 111
mit 300| 2 0 3 42 49 1 -.15 14 13 | -18 -51 20 193
ngs 234| 0 0 6 -15 -12 -17 .05 13 9 | -2114 544 1456 3152
sio 479| 0 1 -5 9 17 -7 -.91 18 19 | --- --- --- ---
Table 2.1796.3 GPS week: 1796 Day: 3 MJD: 56819.000
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 242| 0 0 -6 0 0 7 -.03 9 9 | -1388 544 15 113
emr 80| 2 -2 2 -32 -25 22 .24 13 13 | 4975 -1209 17 126
esa 150| 1 0 -9 15 -7 14 -.39 11 11 | 862 -2422 10 152
gfz 194| -2 -1 0 22 54 -82 -.04 13 11 | -14 303 13 116
grg 180| 3 0 10 0 -57 16 .33 13 12 | -183 303 16 144
igr n/a| 0 1 -4 25 0 24 -.28 5 5 | 8458 -923 16 75
jpl 80| -2 2 -7 98 20 10 .02 16 16 | 3918 -874 16 101
mit 300| 0 0 1 -32 -5 12 -.10 13 12 | 8 202 22 224
ngs 228| 0 1 10 -31 21 -8 .05 12 9 | -1384 536 1189 2955
sio 471| 0 2 -4 -39 -8 29 -.92 20 18 | --- --- --- ---
Table 2.1796.4 GPS week: 1796 Day: 4 MJD: 56820.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| -1 1 -6 10 30 -1 -.01 10 10 | -1708 366 14 110
emr 80| 2 -3 2 -12 -11 10 .29 12 12 | 3294 -421 18 137
esa 150| 2 0 -12 18 4 -9 -.42 11 11 | -836 1308 12 178
gfz 198| 0 0 0 8 -4 -11 -.07 11 10 | -310 769 13 130
grg 183| 8 -2 15 24 -37 -4 .47 16 16 | -354 293 19 146
igr n/a| 0 0 -5 16 2 23 -.22 5 5 | 7054 -276 17 91
jpl 80| 0 2 -6 65 18 13 -.01 14 14 | 2654 -108 17 106
mit 300| -2 0 2 19 -25 5 -.04 13 12 | -315 17 26 228
ngs 230| -2 0 12 -108 1 13 .04 12 10 | -1697 391 1521 3330
sio 468| 0 3 -5 8 -12 30 -.81 19 19 | --- --- --- ---
Table 2.1796.5 GPS week: 1796 Day: 5 MJD: 56821.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 246| -1 2 -5 -4 -8 -1 -.00 8 8 | -1183 514 15 100
emr 80| 5 -9 11 -19 -34 33 .23 20 15 | 2950 -849 19 134
esa 150| 1 1 -10 -6 3 -22 -.40 12 12 | -416 432 11 153
gfz 198| 0 1 1 -19 4 -12 -.05 11 10 | -487 46 14 135
grg 182| 8 -5 12 11 -31 -19 .49 18 18 | 494 -938 20 153
igr n/a| 0 1 -5 -6 -15 14 -.21 5 5 | 6770 -978 17 70
jpl 80| -1 0 -4 61 -12 -15 -.00 15 15 | 2597 -1012 16 105
mit 300| -3 1 1 0 3 22 -.03 13 12 | 1240 -843 22 213
ngs 227| -1 0 6 -21 54 5 .08 11 10 | -1203 551 1778 3625
sio 500| 0 5 -2 -43 3 18 -.83 20 18 | --- --- --- ---
Table 2.1796.6 GPS week: 1796 Day: 6 MJD: 56822.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 248| 0 1 -4 14 2 -8 .03 9 10 | -816 -171 16 98
emr 80| 2 -1 2 -1 11 27 .22 11 11 | 1981 -1639 20 148
esa 150| 0 0 -9 5 19 9 -.39 11 11 | -535 -876 10 151
gfz 198| 0 1 0 1 0 -26 -.06 11 10 | -306 -928 11 122
grg 161| 12 -6 14 24 14 12 .45 21 21 | 235 -1004 20 157
igr n/a| 0 0 -3 11 -28 9 -.20 5 5 | 5602 -1893 16 75
jpl 80| -1 0 -1 23 21 -2 -.03 14 14 | 1475 -1441 18 97
mit 300| -2 0 4 1 -38 1 -.03 14 13 | 88 -1218 22 218
ngs 227| -1 0 3 -56 -32 -16 .05 11 9 | -84601 16273 1344 2884
sio 432| 0 3 -2 -8 11 3 -.92 20 18 | --- --- --- ---
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 3.1796.0 GPS week: 1796 Day: 0 MJD: 56816.000
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 10 15 12 13 6 13 7 16 11 4 | 35 44 35 39 45 35 42 37 38 30 38
2 | 7 9 13 17 11 6 8 10 13 21 4 | 27 33 28 29 32 25 28 28 29 28 27
3E | 15 15 12 11 14 8 15 25 13 16 5 | 112 111 112 113 115 109 115 110 109 111 111
4 | 8 9 11 9 9 5 7 10 11 24 3 | 16 18 16 20 16 19 15 15 16 31 17
5 | 11 13 14 11 11 7 14 27 13 25 5 | 35 40 37 33 35 30 38 30 26 35 32
X6 | 9 --- 12 --- --- 22 --- 13 14 --- 6 | 139 --- 141 --- --- 139 --- 133 135 --- 137
7 | 9 10 12 13 14 8 14 19 10 20 4 | 31 33 30 31 36 28 31 31 31 30 30
8 | 9 8 10 10 14 4 8 8 9 23 3 | 29 30 31 30 32 30 28 27 29 30 29
10 | 8 8 13 8 14 5 5 10 10 15 3 | 35 38 31 36 44 33 34 39 36 37 36
11 | 8 9 16 7 15 5 10 8 11 11 4 | 40 49 37 44 54 39 45 42 43 35 43
12 | 9 19 8 18 13 7 15 11 14 14 5 | 31 34 29 39 34 29 31 30 31 29 30
13E | 8 8 7 9 10 4 11 11 7 10 3 | 31 31 31 33 37 31 31 28 31 33 31
14E | 9 9 6 10 13 4 10 13 9 11 3 | 26 29 28 30 34 26 27 27 32 36 28
15E | 8 14 9 14 14 4 20 18 15 22 5 | 36 40 34 41 42 37 39 38 43 44 38
16 | 9 16 11 16 12 5 12 16 13 16 5 | 28 31 27 34 32 28 30 31 28 27 28
17 | 10 12 9 9 14 4 14 15 10 18 4 | 32 34 27 27 35 28 31 22 24 30 27
18 | 8 11 13 12 13 4 12 15 9 26 4 | 36 39 34 37 42 36 36 41 41 42 36
19 | 8 13 11 12 17 4 10 12 10 16 4 | 34 35 35 31 39 32 34 35 31 34 32
20 | 8 9 15 10 11 6 9 8 11 29 4 | 34 36 30 39 42 36 33 35 40 36 35
21 | 7 11 12 9 9 4 11 11 10 40 3 | 29 34 28 28 34 28 31 31 28 36 29
22 | 11 11 13 9 12 4 9 9 9 21 4 | 42 45 41 46 51 45 42 45 50 44 44
23E | 8 12 10 14 13 4 10 11 9 15 4 | 26 27 26 32 31 25 26 26 26 33 26
24 | 8 10 14 10 8 5 11 11 8 14 3 | 30 33 36 32 34 29 32 29 33 33 32
25 | 7 8 14 6 10 5 11 8 11 16 3 | 30 30 35 31 32 28 32 28 25 25 29
26E | 23 22 20 12 20 13 24 28 49 28 10 | 29 38 32 35 30 33 42 30 55 51 31
X27 | 7 12 15 9 --- 5 12 7 9 14 4 | 38 33 40 36 --- 36 37 33 37 39 36
28 | 8 11 10 12 16 5 10 26 11 12 5 | 32 34 29 37 35 30 32 34 28 32 29
29 | 10 15 9 12 18 4 19 12 11 20 5 | 27 30 25 25 33 22 30 24 26 31 25
X30 | 8 9 12 8 --- 4 14 11 8 12 4 | 34 37 40 34 --- 34 40 32 39 33 36
31 | 8 10 14 11 13 5 9 12 9 13 4 | 28 33 28 33 39 27 28 27 28 26 29
32 | 9 7 14 5 12 4 7 11 10 16 3 | 28 31 26 30 35 27 28 33 32 27 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 12 11 13 6 12 15 14 20 |T 37 37 37 36 39 36 35 37 38 36 37
WRMS | 9 12 12 11 12 5 12 12 10 19 |NE 35 34 35 33 36 34 32 35 36 32 35
MEDI | 8 10 12 10 13 5 11 11 10 16 |MD 31 34 31 33 35 30 32 31 31 33 31
Table 3.1796.1 GPS week: 1796 Day: 1 MJD: 56817.000
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 8 14 10 13 6 16 10 12 11 4 | 24 30 20 21 33 21 32 25 22 21 24
2 | 8 12 12 14 10 3 9 11 9 22 4 | 19 27 22 15 20 18 23 19 22 17 18
3E | 15 16 13 12 16 8 17 21 15 17 6 | 106 105 107 104 108 105 108 110 107 106 106
4 | 14 11 10 12 8 4 8 9 5 20 3 | 16 18 17 20 14 14 15 15 15 25 15
5 | 12 14 14 12 11 8 18 24 12 24 5 | 27 33 24 25 28 20 32 24 23 22 24
X6 | 10 --- 11 --- --- 11 --- 11 15 --- 7 | 94 --- 96 --- --- 90 --- 89 91 --- 92
7 | 8 10 12 11 12 7 12 13 9 14 4 | 26 27 22 26 31 20 25 27 26 20 24
8 | 9 8 11 8 10 4 8 7 8 29 3 | 25 27 28 25 23 23 26 25 25 34 24
10 | 7 9 11 7 9 3 7 9 7 23 3 | 25 26 22 25 26 21 23 25 24 27 24
11 | 9 8 17 10 15 4 9 10 13 12 4 | 28 35 24 27 40 24 34 30 26 24 28
12 | 10 18 7 17 16 6 17 10 14 14 5 | 25 30 20 31 28 20 26 22 27 21 23
13E | 9 12 7 9 11 3 11 9 7 12 3 | 23 25 20 22 25 21 25 22 25 22 22
14E | 8 9 7 7 11 5 11 10 9 15 3 | 24 23 22 23 25 19 20 23 24 28 21
15E | 7 16 8 17 15 5 21 12 11 20 5 | 27 31 23 31 28 23 27 27 31 29 26
16 | 13 18 11 16 13 5 14 15 11 17 5 | 25 29 21 27 30 21 25 26 27 23 23
17 | 9 13 7 10 14 4 18 13 9 14 4 | 23 26 19 24 29 19 27 16 22 21 19
18 | 7 11 13 14 15 3 13 11 9 27 4 | 24 27 24 26 30 21 26 26 22 30 23
19 | 8 11 12 10 17 4 12 12 9 16 4 | 25 29 28 26 36 24 26 28 28 27 26
20 | 8 9 13 12 12 3 12 9 10 31 4 | 25 26 21 29 28 21 25 24 27 25 23
21 | 9 12 13 6 10 5 14 11 9 34 4 | 21 26 20 20 23 16 25 21 24 17 20
22 | 11 9 13 13 13 4 12 8 12 20 4 | 26 29 27 30 34 25 27 28 31 26 27
23E | 8 11 8 15 15 3 13 9 11 16 4 | 22 22 16 24 21 15 19 18 22 24 18
24 | 7 11 14 8 8 6 13 9 9 12 3 | 23 28 30 24 29 21 29 21 25 23 25
25 | 8 10 14 8 14 4 13 9 10 16 4 | 22 25 27 27 28 20 24 20 23 21 22
26E | 19 17 15 10 17 10 18 16 34 15 7 | 25 29 17 21 14 14 23 18 41 28 20
X27 | 7 13 14 9 --- 6 12 10 11 19 4 | 28 27 34 28 --- 28 30 28 31 33 28
28 | 10 12 9 13 16 5 12 20 13 13 5 | 21 24 19 27 28 18 22 22 23 22 19
29 | 10 22 8 14 19 6 22 12 9 21 5 | 22 28 18 23 25 17 29 17 22 24 18
X30 | 8 9 12 8 --- 6 14 8 11 13 4 | 28 30 32 28 --- 27 36 28 29 27 29
31 | 7 12 15 11 14 6 11 13 10 16 4 | 24 30 22 28 35 19 24 22 27 21 23
32 | 10 6 13 8 12 6 6 8 7 12 3 | 26 25 21 24 32 20 23 25 25 19 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 12 12 13 5 14 13 12 19 |T 29 29 27 27 30 25 28 28 30 26 27
WRMS | 9 13 12 11 13 5 12 12 9 19 |NE 26 27 26 25 28 23 26 26 27 23 25
MEDI | 9 11 12 10 13 5 12 10 10 16 |MD 25 27 22 25 28 21 25 24 25 24 23
Table 3.1796.2 GPS week: 1796 Day: 2 MJD: 56818.000
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 8 14 12 12 6 16 6 17 15 4 | 33 36 25 31 37 28 39 29 33 29 31
2 | 6 11 13 13 10 4 9 9 10 19 4 | 19 27 22 18 23 19 22 20 21 17 19
3E | 13 18 15 9 16 9 18 28 19 15 6 | 63 61 60 58 61 58 60 66 59 59 60
4 | 13 9 11 10 8 4 7 6 9 17 3 | 29 20 19 18 18 22 21 18 20 30 22
5 | 12 12 14 12 11 6 13 25 12 23 5 | 29 34 30 25 26 25 32 22 25 26 26
X6 | 7 --- 11 --- --- 8 --- 12 13 --- 6 | 101 --- 102 --- --- 100 --- 95 97 --- 98
7 | 9 10 13 9 16 7 13 13 10 15 4 | 29 29 24 27 36 23 25 27 28 22 26
8 | 10 7 12 11 11 4 8 9 10 27 3 | 28 26 27 25 28 24 24 24 28 34 25
10 | 7 7 13 9 9 5 7 9 10 21 3 | 31 31 26 32 34 29 28 31 30 33 30
11 | 8 8 17 9 15 5 10 8 8 12 4 | 32 40 29 33 43 31 38 33 34 30 34
12 | 9 19 10 20 17 6 17 10 12 14 5 | 25 33 26 35 31 24 26 26 28 27 25
13E | 5 7 9 7 10 4 11 14 8 12 3 | 28 29 24 30 36 27 29 31 31 26 28
14E | 8 8 7 7 14 3 12 13 9 12 3 | 27 29 26 29 31 28 24 29 32 35 28
15E | 9 16 8 19 11 6 22 19 17 23 6 | 33 37 31 38 35 32 37 36 35 37 33
16 | 10 20 11 14 15 6 13 16 13 16 5 | 25 31 21 29 31 23 28 29 28 24 25
17 | 10 10 10 11 14 4 17 16 11 16 4 | 28 28 22 25 33 23 27 20 24 23 23
18 | 8 13 13 15 14 4 13 11 12 24 4 | 29 37 28 34 36 30 33 33 37 32 31
19 | 7 12 11 12 17 3 9 18 9 17 4 | 29 33 30 29 39 27 32 33 29 28 30
20 | 8 9 15 13 10 4 10 8 8 31 4 | 30 33 23 34 34 29 31 32 33 32 29
21 | 8 10 14 7 16 6 13 13 13 29 4 | 23 28 24 22 29 23 26 24 25 20 23
22 | 10 9 14 9 14 4 9 12 10 19 4 | 35 38 32 39 41 36 35 36 37 34 35
23E | 9 10 10 15 10 5 14 10 7 18 4 | 27 24 21 30 27 21 24 25 27 28 23
24 | 9 10 14 11 7 5 12 8 9 12 4 | 27 32 32 29 32 26 29 28 28 29 29
25 | 11 9 14 8 12 6 11 11 9 14 4 | 22 27 30 25 32 23 26 23 25 22 24
26E | 17 16 15 12 14 7 17 14 34 18 7 | 21 29 22 27 17 23 28 23 45 33 23
X27 | 8 13 15 6 --- 6 12 14 15 17 5 | 33 29 34 30 --- 31 33 31 33 33 30
28 | 9 12 9 14 18 5 8 23 7 13 5 | 27 29 24 35 35 27 29 28 29 25 26
29 | 11 21 9 15 19 8 21 15 11 18 6 | 23 28 20 22 30 20 28 21 23 25 20
X30 | 9 10 13 9 --- 5 12 7 9 12 4 | 34 34 37 30 --- 31 39 31 32 31 33
31 | 14 13 14 11 16 6 11 14 12 12 5 | 29 34 22 29 37 22 25 24 27 19 26
32 | 9 9 14 7 12 5 9 7 7 15 3 | 28 32 23 29 35 25 29 31 29 27 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 12 12 13 5 13 14 13 18 |T 31 31 29 29 33 29 30 30 32 29 30
WRMS | 10 12 13 11 13 5 12 13 9 19 |NE 31 31 29 28 32 28 29 29 31 26 29
MEDI | 9 10 13 11 14 5 12 12 10 16 |MD 29 31 26 29 33 26 28 29 29 28 28
Table 3.1796.3 GPS week: 1796 Day: 3 MJD: 56819.000
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 12 10 8 4 15 6 7 13 3 | 31 40 34 35 44 33 43 34 39 29 35
2 | 8 13 12 15 11 5 12 11 9 18 4 | 21 31 23 24 25 21 26 25 28 22 23
3E | 10 20 14 13 12 9 20 25 20 21 6 | 91 92 93 97 94 92 100 97 91 94 93
4 | 9 10 11 13 8 4 7 5 11 29 3 | 15 21 21 21 16 15 19 16 20 39 15
5 | 11 13 14 13 11 6 16 24 11 24 5 | 28 32 25 25 27 22 33 25 24 23 24
X6 | 14 --- 10 20 83 9 --- 9 12 35 6 | 118 --- 121 66 83 114 --- 115 114 67 116
7 | 10 11 11 13 14 6 13 8 10 13 4 | 29 34 31 32 40 28 32 29 36 24 31
8 | 8 7 11 11 9 3 9 9 9 29 3 | 28 31 31 28 31 26 28 28 29 37 28
10 | 6 8 12 13 12 3 9 8 11 23 3 | 31 38 30 35 41 32 35 39 41 40 35
11 | 8 10 15 10 12 4 15 6 11 17 4 | 32 45 34 39 49 35 42 37 47 33 38
12 | 9 20 7 20 16 6 22 10 10 18 5 | 31 34 27 40 34 29 33 30 28 29 29
13E | 5 11 7 10 12 5 15 9 8 12 3 | 28 34 30 33 37 29 33 30 30 31 30
14E | 9 10 7 8 13 6 15 8 8 13 3 | 33 29 28 27 34 26 30 29 37 34 29
15E | 10 17 6 17 14 5 24 14 13 23 5 | 36 43 35 43 43 37 39 40 42 42 38
16 | 8 20 10 15 12 5 10 12 11 19 4 | 28 35 28 39 33 28 35 32 29 29 29
17 | 10 11 9 12 16 4 20 13 12 16 5 | 33 29 29 28 36 28 37 25 29 29 28
18 | 6 12 13 14 14 5 15 12 11 25 4 | 33 39 33 38 41 35 35 35 44 35 35
19 | 8 12 10 10 14 4 13 13 9 16 4 | 37 37 37 33 39 32 41 36 38 33 35
20 | 9 10 14 16 10 4 12 8 10 29 4 | 38 40 32 42 39 34 38 35 43 35 36
21 | 8 12 12 7 10 5 15 13 13 32 4 | 25 30 24 25 29 22 29 27 34 25 25
22 | 9 11 12 9 13 5 17 9 12 19 4 | 37 43 37 42 45 39 39 41 49 40 40
23E | 8 12 8 17 11 5 17 15 7 15 4 | 30 32 27 37 33 27 30 32 32 30 29
24 | 7 11 13 10 11 4 17 10 8 13 4 | 30 33 36 32 36 29 36 32 35 32 32
25 | 11 12 14 9 15 5 15 11 9 13 4 | 28 29 32 33 34 28 31 28 27 23 28
26E | 14 16 14 10 17 5 17 16 28 18 6 | 21 33 27 28 17 26 31 28 47 38 27
X27 | 6 12 15 7 --- 4 12 9 11 18 4 | 39 33 42 40 --- 36 41 34 36 40 36
28 | 7 14 8 16 17 4 10 21 8 15 5 | 31 34 28 36 40 28 33 30 30 32 29
29 | 13 20 7 14 18 5 25 14 10 13 5 | 30 31 22 28 32 24 33 28 26 26 25
X30 | 7 8 12 10 --- 4 13 6 10 14 4 | 32 38 39 31 --- 33 40 33 38 35 35
31 | 7 12 13 11 14 6 10 11 12 13 4 | 31 35 26 34 40 26 30 28 35 23 30
32 | 8 9 11 9 7 7 8 7 7 13 3 | 32 35 29 36 39 30 35 34 41 28 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 13 13 5 16 13 12 20 |T 35 36 35 36 39 33 36 35 39 34 35
WRMS | 9 13 11 11 12 5 16 12 9 18 |NE 33 34 33 34 37 32 34 34 37 32 33
MEDI | 8 12 12 12 12 5 15 10 10 18 |MD 31 34 30 34 37 29 33 32 36 32 30
Table 3.1796.4 GPS week: 1796 Day: 4 MJD: 56820.000
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 7 14 10 10 6 15 7 11 15 4 | 28 34 27 29 41 25 37 27 28 28 28
2 | 11 12 14 15 15 4 11 11 13 12 5 | 24 29 22 21 26 20 24 25 25 21 21
3E | 12 15 12 12 16 9 19 19 22 16 6 | 68 76 68 68 73 66 71 72 68 68 68
X4 | 4 --- --- --- --- 39 --- --- --- --- 0 | 56 --- --- --- --- 7 --- --- --- --- 55
5 | 12 11 13 10 15 6 15 25 16 30 5 | 28 32 26 24 31 22 31 23 27 22 25
X6 | 11 --- 13 13 81 6 --- 9 12 33 5 | 118 --- 118 57 69 113 --- 109 107 60 111
7 | 8 10 10 12 13 6 13 8 11 15 4 | 26 30 21 27 35 22 24 24 30 20 24
8 | 9 8 11 9 18 4 9 7 10 32 3 | 25 29 26 23 31 22 23 25 24 37 24
10 | 9 8 11 8 23 5 7 6 8 16 4 | 23 31 23 31 45 25 25 30 34 27 28
11 | 9 8 16 9 14 4 13 9 8 12 4 | 28 38 27 30 47 27 36 30 35 23 31
12 | 11 20 8 16 17 5 18 11 13 13 5 | 23 29 19 29 29 20 25 23 25 19 22
13E | 8 10 10 7 14 3 13 7 9 11 3 | 26 25 23 26 34 24 23 25 33 25 25
14E | 10 11 8 8 15 4 11 11 9 15 4 | 30 30 29 31 32 26 29 28 32 34 28
15E | 9 17 7 15 17 5 24 16 12 23 5 | 29 38 27 36 39 30 36 33 40 34 32
16 | 12 18 10 12 13 6 15 14 14 16 5 | 24 28 23 28 26 22 25 23 26 20 22
17 | 11 10 9 11 18 6 20 16 11 17 5 | 29 28 23 25 36 23 29 21 21 25 23
18 | 11 11 13 14 15 5 14 11 11 27 4 | 25 33 25 31 35 26 31 27 33 28 27
19 | 8 11 9 11 19 4 14 13 12 16 4 | 30 34 31 29 40 28 33 35 28 27 30
20 | 8 9 13 10 14 4 9 7 9 28 3 | 29 33 24 33 35 26 26 28 34 31 28
21 | 10 11 12 7 11 4 12 11 11 31 4 | 19 28 19 21 28 20 26 24 27 21 22
22 | 12 10 12 9 14 5 11 10 9 25 4 | 32 36 31 36 38 33 33 33 41 36 33
23E | 9 9 11 12 15 4 12 10 7 14 4 | 23 24 17 25 25 21 19 23 25 22 20
24 | 12 11 13 10 13 3 14 13 10 14 4 | 25 30 28 25 30 23 26 27 25 27 25
25 | 11 10 14 9 16 5 13 10 9 13 4 | 25 24 27 24 29 23 25 20 25 16 23
X26E | 14 18 13 11 --- 7 15 21 28 17 7 | 18 29 22 27 --- 19 26 24 40 31 22
X27 | 8 10 15 9 --- 4 11 9 13 15 4 | 29 27 37 30 --- 29 30 29 30 31 29
28 | 7 12 7 11 17 4 12 21 11 13 4 | 28 31 24 28 34 23 26 24 24 26 24
29 | 9 20 8 12 24 6 20 12 12 18 5 | 24 26 19 23 31 19 28 22 24 23 20
X30 | 5 9 11 9 --- 5 13 8 13 14 4 | 29 35 32 28 --- 28 35 29 36 30 31
31 | 8 12 11 9 12 6 13 12 13 12 4 | 27 31 21 29 36 20 25 24 27 21 25
32 | 11 7 12 8 14 5 7 8 7 12 3 | 30 31 23 27 37 24 28 28 33 19 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 11 11 16 5 14 13 12 19 |T 31 32 29 30 36 27 29 30 33 28 30
WRMS | 10 12 11 10 16 5 14 12 10 19 |NE 31 30 28 28 35 26 28 29 32 26 30
MEDI | 9 11 11 10 15 5 13 11 11 15 |MD 28 30 24 28 35 23 26 25 28 26 25
Table 3.1796.5 GPS week: 1796 Day: 5 MJD: 56821.000
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 13 9 13 6 14 6 8 13 3 | 27 39 23 27 41 25 39 26 29 23 28
2 | 7 11 13 12 17 5 12 10 10 15 4 | 19 29 19 18 23 17 22 21 24 17 19
3E | 13 67 15 16 16 12 19 21 20 21 9 | 80 81 80 82 85 79 82 86 84 82 79
X4 | 8 10 --- 8 16 9 --- 10 --- --- 5 | 19 16 --- 11 19 12 --- 14 --- --- 16
5 | 8 12 14 11 18 7 17 24 15 31 5 | 24 31 25 26 31 22 29 24 25 22 23
X6 | 10 --- 12 9 80 5 --- 13 14 35 6 | 94 --- 97 53 68 90 --- 91 85 55 91
7 | 7 13 12 11 12 5 15 8 10 14 4 | 27 32 22 28 35 23 25 24 30 17 25
8 | 8 11 11 9 22 4 8 11 11 33 4 | 25 29 25 20 33 21 22 19 27 38 22
X9 | 3 --- --- --- --- 5797 --- --- --- --- 0 | 892 --- --- --- --- 28 --- --- --- --- 895
10 | 6 9 12 7 26 6 10 9 8 23 4 | 27 36 25 28 43 25 30 26 34 31 28
11 | 5 13 16 9 18 3 13 7 9 13 4 | 26 45 24 27 47 25 35 26 31 19 28
12 | 11 25 8 17 20 5 20 17 14 14 6 | 22 33 18 29 31 19 24 25 22 21 20
13E | 7 11 9 9 14 4 11 6 9 9 3 | 25 25 20 24 34 21 22 20 22 19 22
14E | 7 13 8 8 18 5 14 9 8 16 4 | 21 26 19 19 24 17 21 21 21 26 19
15E | 9 20 9 16 19 5 23 13 13 26 5 | 29 38 26 32 44 30 36 33 35 37 31
16 | 8 26 10 14 12 6 14 13 15 18 5 | 25 33 21 28 26 21 25 21 30 19 22
17 | 11 13 10 10 19 4 21 17 9 13 5 | 29 26 26 24 39 22 28 22 27 19 23
18 | 7 13 13 13 18 3 15 12 11 34 4 | 20 31 21 24 34 18 26 19 25 31 20
19 | 6 12 10 9 23 4 15 8 8 14 4 | 28 29 28 27 41 26 32 29 28 22 27
20 | 8 13 14 10 14 4 11 9 10 27 4 | 32 37 25 32 34 26 29 29 31 29 29
21 | 7 15 13 7 16 2 16 9 12 33 4 | 20 29 19 20 30 16 25 20 24 14 19
22 | 7 15 13 10 16 3 12 9 11 26 4 | 26 35 26 32 33 24 28 26 32 33 26
23E | 7 13 10 14 15 4 12 9 10 17 4 | 21 25 16 25 26 17 18 19 23 25 19
24 | 11 17 15 9 18 3 15 21 11 16 5 | 23 28 27 24 30 20 26 28 22 25 23
25 | 9 17 14 11 21 5 14 14 10 15 5 | 24 26 28 31 32 22 23 21 26 19 23
X26E | 15 18 13 17 --- 6 16 24 27 15 7 | 21 31 23 27 --- 21 28 28 41 26 23
X27 | 7 22 15 10 --- 5 11 7 12 15 5 | 28 27 32 29 --- 26 28 24 29 28 26
28 | 8 15 9 15 18 5 8 21 8 13 5 | 27 32 24 31 36 23 29 23 26 23 24
29 | 8 16 10 11 27 4 22 12 11 14 5 | 22 22 17 24 34 16 25 23 22 18 19
X30 | 9 12 12 9 --- 5 14 11 12 14 4 | 29 37 33 27 --- 30 37 25 35 30 30
31 | 8 15 14 9 15 5 16 12 16 13 4 | 28 33 20 29 38 20 27 23 26 19 24
32 | 7 11 13 7 19 6 7 8 11 15 4 | 29 34 23 27 38 24 28 30 33 21 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 20 12 11 18 5 15 13 11 20 |T 55 32 27 28 36 25 29 27 31 26 54
WRMS | 8 15 12 10 18 5 15 12 10 18 |NE 62 31 26 26 35 24 27 26 30 24 61
MEDI | 8 13 12 10 18 5 14 11 11 15 |MD 26 31 24 27 34 22 28 24 27 23 23
Table 3.1796.6 GPS week: 1796 Day: 6 MJD: 56822.000
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 9 13 10 16 5 14 9 14 14 4 | 38 44 31 34 49 35 46 40 39 33 37
2 | 9 10 13 13 20 4 10 10 9 17 4 | 24 31 24 25 32 22 26 30 25 26 24
3E | 9 16 11 11 15 8 18 21 21 14 6 | 98 99 101 101 99 100 101 100 101 101 100
4 | 13 8 13 9 20 8 10 15 9 44 4 | 17 11 8 9 19 9 7 15 4 4 12
5 | 13 10 14 12 22 6 16 25 14 24 6 | 36 35 35 36 38 31 35 32 34 31 33
X6 | 9 --- 14 15 83 8 --- 17 10 35 6 | 148 --- 149 53 77 142 --- 139 139 62 142
7 | 9 9 10 12 17 4 17 10 10 14 4 | 30 32 25 33 38 28 30 28 33 21 29
8 | 7 8 12 7 23 4 9 9 7 29 3 | 27 29 27 27 37 25 23 25 28 35 26
X9 | 21 18 --- --- --- 18 --- 24 32 --- 14 | 816 11 --- --- --- 35 --- 7 5 --- 822
10 | 8 8 12 6 32 6 9 10 12 19 4 | 35 41 28 37 57 33 31 40 38 40 36
11 | 7 9 16 9 20 4 11 7 13 10 4 | 35 48 32 37 55 37 44 40 42 31 39
12 | 8 17 11 17 22 4 16 15 12 13 5 | 32 33 24 39 37 28 30 33 32 26 30
13E | 6 11 9 8 18 4 13 9 9 10 3 | 31 35 28 33 40 30 31 31 34 28 31
14E | 8 9 7 11 22 4 17 12 12 15 4 | 29 31 23 29 42 24 28 28 28 33 27
15E | 8 19 9 15 21 6 22 12 13 21 5 | 39 48 36 47 52 41 42 43 45 43 41
16 | 9 15 8 14 13 5 14 11 14 16 4 | 26 31 26 33 33 27 29 29 33 27 27
17 | 10 11 10 10 21 5 21 17 9 14 5 | 30 29 26 27 41 26 29 24 24 25 25
18 | 11 11 13 11 19 5 14 14 10 30 4 | 33 41 31 36 49 35 39 39 45 41 36
19 | 7 11 8 10 25 5 12 9 10 16 4 | 35 35 35 31 46 32 34 32 34 29 33
20 | 8 10 12 11 15 4 12 10 10 21 4 | 39 40 30 45 44 37 35 42 40 33 38
21 | 12 12 13 9 16 5 14 10 11 33 4 | 27 33 24 25 37 26 31 30 32 25 27
22 | 10 10 11 9 21 5 14 11 9 28 4 | 43 47 38 45 53 44 45 44 48 47 43
23E | 7 8 9 15 20 3 12 12 9 14 4 | 29 32 25 35 36 27 30 30 30 27 28
24 | 12 9 15 12 22 5 13 24 9 17 5 | 32 34 34 32 37 28 34 36 32 36 31
25 | 10 10 15 10 24 3 14 9 9 15 4 | 27 27 31 31 38 27 30 27 28 24 28
X26E | 18 18 14 13 --- 7 18 25 28 14 8 | 19 35 25 30 --- 25 31 34 45 32 27
X27E | 7 18 15 8 --- 6 11 9 10 17 4 | 36 30 40 33 --- 35 35 32 36 36 33
28 | 9 11 10 13 22 6 11 21 8 13 5 | 33 34 28 38 39 31 30 28 30 30 29
29 | 14 17 7 13 31 4 21 8 9 15 5 | 29 26 20 25 41 21 29 24 23 23 23
X30 | 7 8 13 8 --- 4 13 11 8 15 4 | 33 38 37 33 --- 34 39 31 38 34 35
31 | 9 14 10 11 17 5 15 13 11 12 4 | 28 36 23 29 39 24 27 26 29 22 27
32 | 8 7 11 10 22 5 8 9 5 14 3 | 35 39 30 37 46 32 34 38 39 29 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 11 11 21 5 14 14 11 20 |T 61 35 34 35 44 35 34 36 37 33 61
WRMS | 10 11 11 10 21 5 14 13 9 18 |NE 67 33 33 33 42 33 32 35 35 30 66
MEDI | 9 10 12 11 21 5 14 11 10 15 |MD 32 34 28 33 40 30 31 31 33 31 31
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 4.1796 GPS week: 1796 MJD: 56816.0-56822.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2974 |U 9 11 29 |U 9 10 28 |U 8 10 21 |
emr | emr 2871 | 12 13 35 |U 9 9 30 | 10 11 21 |
esa | esa 2948 | 10 11 31 |U 9 10 31 | 9 12 22 |
gfz | gfz 2913 |U 10 11 31 |U 9 10 30 |U 10 11 28 |
grg | grg 2687 |U 12 13 32 |U 12 16 40 |U 11 14 26 |
igr | igr 2951 | 10 11 30 | 9 9 30 | 9 12 23 |
igs | igs 2964 | 10 11 30 | 9 9 30 | 9 11 21 |
jpl | jpl 2844 |U 11 13 34 | 11 23 43 | 10 11 24 |
mit | mit 2976 | 10 12 33 |U 9 18 39 |U 8 10 23 |
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 5.1796.0 GPS week: 1796 Day: 0 MJD: 56816.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 8 9 24 | 7 9 26 | 5 8 16 |
emr | emr 2874 | 11 10 32 | 6 8 32 | 7 7 17 |
esa | esa 2976 | 10 8 24 | 7 10 36 | 6 9 18 |
gfz | gfz 2872 | 10 10 34 | 6 8 33 | 8 9 41 |
grg | grg 2688 | 10 8 29 | 9 20 47 | 6 9 19 |
igr | igr 2965 | 9 8 24 | 7 9 32 | 6 10 19 |
igs | igs 2970 | 9 9 25 | 6 9 33 | 6 9 17 |
jpl | jpl 2874 | 11 9 26 | 7 17 38 | 7 9 17 |
mit | mit 2976 | 8 9 25 | 7 20 43 | 6 8 16 |
Table 5.1796.1 GPS week: 1796 Day: 1 MJD: 56817.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 12 20 60 | 15 17 41 | 10 12 22 |
emr | emr 2872 | 14 21 57 | 17 20 44 | 10 11 21 |
esa | esa 2976 | 14 20 58 | 15 17 42 | 11 14 23 |
gfz | gfz 2872 | 13 21 59 | 15 18 41 | 10 12 21 |
grg | grg 2687 | 15 23 59 | 19 27 42 | 11 13 27 |
igr | igr 2970 | 13 22 59 | 15 17 41 | 10 13 23 |
igs | igs 2948 | 13 21 58 | 15 17 41 | 10 12 20 |
jpl | jpl 2872 | 13 22 61 | 20 33 39 | 10 12 22 |
mit | mit 2976 | 14 21 58 | 16 24 40 | 9 11 21 |
Table 5.1796.2 GPS week: 1796 Day: 2 MJD: 56818.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 8 8 32 | 12 8 40 | 8 9 20 |
emr | emr 2872 | 13 10 37 | 9 6 39 | 9 9 20 |
esa | esa 2976 | 9 8 37 | 11 9 42 | 9 11 21 |
gfz | gfz 2873 | 8 8 32 | 12 8 40 | 8 9 20 |
grg | grg 2688 | 11 11 36 | 14 19 56 | 10 12 25 |
igr | igr 2947 | 8 8 36 | 12 8 43 | 8 10 21 |
igs | igs 2955 | 9 8 36 | 11 7 41 | 8 10 20 |
jpl | jpl 2872 | 10 12 36 | 12 26 50 | 9 11 23 |
mit | mit 2976 | 9 9 33 | 11 19 42 | 7 9 22 |
Table 5.1796.3 GPS week: 1796 Day: 3 MJD: 56819.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 15 17 37 | 6 8 21 | 9 14 21 |
emr | emr 2872 | 17 19 43 | 7 7 21 | 12 15 20 |
esa | esa 2976 | 16 18 42 | 6 9 23 | 10 16 23 |
gfz | gfz 2968 | 16 17 41 | 6 8 20 | 9 14 23 |
grg | grg 2784 | 16 16 37 | 10 16 42 | 13 19 29 |
igr | igr 2880 | 15 16 40 | 6 7 19 | 10 16 25 |
igs | igs 2974 | 15 17 38 | 5 8 19 | 10 15 23 |
jpl | jpl 2872 | 17 18 44 | 7 18 42 | 10 15 24 |
mit | mit 2976 | 15 16 37 | 5 16 30 | 9 14 25 |
Table 5.1796.4 GPS week: 1796 Day: 4 MJD: 56820.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 7 8 18 | 5 9 16 | 11 11 25 |
emr | emr 2776 | 10 10 24 | 8 8 22 | 14 14 26 |
esa | esa 2880 | 8 8 17 | 5 8 18 | 12 13 29 |
gfz | gfz 2872 | 7 8 17 | 4 8 17 | 16 14 48 |
grg | grg 2592 | 9 9 17 | 8 10 24 | 16 18 27 |
igr | igr 2880 | 8 9 18 | 5 7 19 | 12 14 28 |
igs | igs 2880 | 7 8 17 | 4 8 20 | 12 13 26 |
jpl | jpl 2776 | 11 11 24 | 10 19 36 | 13 14 31 |
mit | mit 2880 | 7 8 18 | 6 13 28 | 9 11 26 |
Table 5.1796.5 GPS week: 1796 Day: 5 MJD: 56821.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2986 | 9 11 20 | 10 7 23 | 6 6 23 |
emr | emr 2872 | 13 17 36 | 11 7 24 | 7 6 26 |
esa | esa 2880 | 10 13 26 | 10 8 27 | 8 7 19 |
gfz | gfz 2966 | 9 10 21 | 9 8 27 | 7 6 23 |
grg | grg 2688 | 13 18 32 | 12 9 29 | 8 12 33 |
igr | igr 2969 | 9 10 22 | 10 7 28 | 7 8 23 |
igs | igs 2972 | 10 12 23 | 9 8 25 | 7 7 23 |
jpl | jpl 2776 | 11 13 31 | 11 24 51 | 8 6 24 |
mit | mit 2976 | 9 11 23 | 9 18 35 | 6 7 24 |
Table 5.1796.6 GPS week: 1796 Day: 6 MJD: 56822.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 5 3 15 | 10 9 27 | 10 10 19 |
emr | emr 2965 | 8 6 17 | 8 9 30 | 12 11 19 |
esa | esa 2976 | 5 5 13 | 9 10 26 | 11 12 20 |
gfz | gfz 2968 | 5 3 13 | 9 10 33 | 10 10 19 |
grg | grg 2688 | 8 7 16 | 11 11 38 | 10 13 19 |
igr | igr 3050 | 5 4 11 | 9 9 25 | 10 12 21 |
igs | igs 3052 | 5 4 13 | 9 11 34 | 10 11 19 |
jpl | jpl 2872 | 6 6 15 | 10 22 45 | 11 11 23 |
mit | mit 3072 | ---- ---- ---- | 11 16 57 | 9 8 24 |
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 6.1796 GPS week: 1796 MJD: 56816.500-56822.500
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 | -10 8 -27 87 0 | 9 23
| 20 21 95 78 4 | 4
emr uuuuu | 52 15 -139 112 5 | 32 41
| 15 26 95 53 9 | 3
esa uuuuu | -26 -15 53 -79 2 | 8 22
| 9 12 49 61 3 | 4
gfz uuuuu | -18 11 -51 -8 -1 | 0 22
| 17 20 150 94 4 | 6
grg uuuuu | 27 -32 66 -16 1 | 38 42
| 26 24 108 111 4 | 4
igr xxxxx | -5 -22 -20 -86 2 | -8 21
| 13 13 39 60 4 | 4
irf xxxxx | -3 -9 11 -43 -2 | -1 22
| 8 16 44 31 4 | 5
jpl uuuuu | -10 -56 13 -44 -7 | 17 30
| 26 43 44 92 7 | 6
mit uuuuu | -17 -3 33 -75 -5 | 26 34
| 19 31 80 56 4 | 5
ngs uuuuu | 3 42 92 -22 3 | 9 19
| 46 35 160 195 4 | 4
sio xxxxx | -23 11 38 -125 -3 | 56 60
| 17 28 79 36 8 | 2
Table 7.1796.0 GPS week: 1796 Day: 0 MJD: 56816.500
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 -21 46 -40 0 | 17 23
emr uuuuu | 46 -32 3 139 11 | 33 40
esa uuuuu | -39 -8 68 -34 4 | 15 23
gfz uuuuu | -19 -4 -14 0 -9 | 10 19
grg uuuuu | 22 9 -119 -120 5 | 45 47
igr xxxxx | -6 -37 -64 3 -2 | 0 15
irf xxxxx | -5 14 -24 -34 -7 | 9 17
jpl uuuuu | 32 -20 23 73 -5 | 26 33
mit uuuuu | -31 43 -11 -91 -9 | 35 38
ngs uuuuu | 34 51 -27 49 9 | 16 20
sio xxxxx | -3 49 -26 -77 4 | 61 62
Table 7.1796.1 GPS week: 1796 Day: 1 MJD: 56817.500
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 | -9 38 1 54 -1 | 12 24
emr uuuuu | 56 4 -265 167 21 | 31 40
esa uuuuu | -26 -15 21 -57 4 | 11 24
gfz uuuuu | -32 -4 86 -140 -4 | 5 24
grg uuuuu | 27 -44 55 -187 -3 | 40 45
igr xxxxx | -17 -13 -57 -57 2 | -5 22
irf xxxxx | -15 -23 28 -91 -5 | 3 23
jpl uuuuu | 10 8 -27 2 5 | 22 33
mit uuuuu | -28 -8 49 -143 -8 | 29 37
ngs uuuuu | 9 0 80 232 -3 | 13 21
sio xxxxx | -24 -13 26 -146 10 | 58 61
Table 7.1796.2 GPS week: 1796 Day: 2 MJD: 56818.500
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 | -16 -5 -69 22 0 | 9 23
emr uuuuu | 77 37 -178 95 6 | 32 40
esa uuuuu | -26 -10 135 -67 4 | 8 23
gfz uuuuu | -38 -3 138 -94 0 | 1 23
grg uuuuu | -5 -19 -34 -38 -4 | 38 42
igr xxxxx | -3 -9 13 -59 7 | -8 23
irf xxxxx | -12 3 65 -57 -2 | 0 23
jpl uuuuu | -30 -77 78 -29 -16 | 19 31
mit uuuuu | -36 24 112 -94 -5 | 26 35
ngs uuuuu | 59 43 -105 164 4 | 9 20
sio xxxxx | -58 18 113 -121 -2 | 57 60
Table 7.1796.3 GPS week: 1796 Day: 3 MJD: 56819.500
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 25 -55 129 -5 | 6 23
emr uuuuu | 56 46 -138 37 1 | 29 39
esa uuuuu | -14 -28 19 10 -1 | 4 21
gfz uuuuu | -15 6 -85 121 0 | -3 23
grg uuuuu | 52 -21 167 72 5 | 34 40
igr xxxxx | -28 -18 34 -68 -1 | -11 23
irf xxxxx | 1 -10 47 -7 -2 | -4 23
jpl uuuuu | -24 -128 68 54 -4 | 14 31
mit uuuuu | -17 -2 110 -60 -7 | 22 33
ngs uuuuu | -31 50 -30 -355 6 | 6 18
sio xxxxx | -28 -11 2 -150 -14 | 55 59
Table 7.1796.4 GPS week: 1796 Day: 4 MJD: 56820.500
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 | -23 -6 56 179 -1 | 6 23
emr uuuuu | 57 28 -232 69 -3 | 31 41
esa uuuuu | -23 -34 -15 -150 5 | 4 21
gfz uuuuu | 15 15 -272 95 0 | -4 22
grg uuuuu | 53 -51 124 141 4 | 34 40
igr xxxxx | 10 -31 -54 -116 2 | -11 23
irf xxxxx | 1 -18 -5 -54 2 | -5 23
jpl uuuuu | -27 -66 -13 -150 -17 | 13 29
mit uuuuu | -25 -18 66 -94 0 | 22 32
ngs uuuuu | -11 93 348 -125 3 | 5 17
sio xxxxx | -14 -9 90 -156 -2 | 54 58
Table 7.1796.5 GPS week: 1796 Day: 5 MJD: 56821.500
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 | 27 4 44 155 -3 | 5 22
emr uuuuu | 30 15 -108 183 6 | 32 41
esa uuuuu | -17 1 76 -158 0 | 4 21
gfz uuuuu | -17 52 -211 4 5 | -5 22
grg uuuuu | 47 -36 106 1 -1 | 34 40
igr xxxxx | 4 -8 -21 -185 0 | -12 23
irf xxxxx | 10 0 -61 -51 0 | -6 23
jpl uuuuu | 8 -56 -32 -122 -7 | 10 26
mit uuuuu | 16 -6 -118 -80 -3 | 20 30
ngs uuuuu | -75 -6 211 -57 2 | 5 17
sio xxxxx | -14 48 -79 -149 -7 | 54 57
Table 7.1796.6 GPS week: 1796 Day: 6 MJD: 56822.500
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 | -3 24 -211 109 8 | 9 23
emr uuuuu | 42 9 -53 95 -5 | 38 45
esa uuuuu | -36 -10 69 -94 -1 | 9 22
gfz uuuuu | -17 12 2 -43 1 | -1 22
grg uuuuu | -7 -65 167 21 5 | 38 43
igr xxxxx | 7 -39 8 -121 7 | -7 21
irf xxxxx | 0 -32 30 -4 3 | -1 22
jpl uuuuu | -36 -52 -2 -134 -4 | 14 27
mit uuuuu | 4 -55 23 40 0 | 24 32
ngs uuuuu | 33 65 165 -61 -3 | 9 19
sio xxxxx | -18 -8 140 -73 -6 | 57 60
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