[IGSREPORT-22592] Wk 1782 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Mar 21 09:03:08 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1782 (Mar 02, 2014 - Mar 08, 2014)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1782[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1782[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1782[0-6].cls IGS GPS clock combination summary report.
igs17827.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17827.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 4 1 4
0 | EMR | 6 8 1 6 8 HERS HERS
0 | ESA | 4 4 DGAV PIMO SEY1
0 | GFZ | 2 2 CHUR CHUR
0 | GRG | 1
0 | JPL | 8 CUSV GUUG
1 | ALL | 1
1 | COD | 4 4 KOUR KOUR
1 | EMR | 8 8 HERS HERS
1 | ESA | 4 4
1 | GFZ | 2 2 PIMO
1 | JPL | 4 8 CAS1 CUSV
1 | MIT | 4 4 NYAL NYAL
2 | COD | 4 KARR
2 | EMR | 8 8 HERS THU3 HERS THU3
2 | ESA | 4 4 RESO WHIT PIMO RESO WHIT
2 | GFZ | 2 2
2 | JPL | 4 8 CUSV KARR
3 | ALL | 1
3 | COD | ALIC ALIC
3 | EMR | 8 8 HERS HERS
3 | ESA | 1 HOB2
3 | GFZ | 2 1 2 CHUR HOB2 CHUR HOB2 NRIL
3 | GRG | ALRT ALRT
3 | JPL | 4 8
4 | COD | DARW DARW ZAMB
4 | EMR | 8 8 HERS MCM4 CHUR HERS MCM4
4 | ESA | NICO ARTU DGAV FLIN NICO
4 | GFZ | 2 2 ARTU
4 | GRG | KELY
4 | JPL | 2 4 8 CUSV
5 | ALL | 1
5 | COD | 25 25 MDVJ
5 | EMR | HERS HERS
5 | ESA | 25 1 25 ALIC
5 | GFZ | 2 1 2
5 | JPL | 2 9
5 | MIT | 1
6 | ALL | 1 1
6 | COD | GUAT GUAT HYDE
6 | EMR | 24 24 HERS THU3 HERS
6 | GFZ | 2 2
6 | JPL | 10 CUSV GLPS
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
----+------------+----------
G05 | 2014_03_05 | 2014023
G17 | 2014_03_07 | 2014024
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
----+--------+---------------
1 | EMR | 6
1 | MIT | 6
1 | NGS | 6
5 | ESA | 25
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 G04 | | | | | | | 4 |
PRN G30 | 4 | 4 | 4 | 4 | 4 | 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 .7 -.7 -22 -7 7 .53
EMR | 0 | 2.1 2.2 1.3 9 5 -66 .75
ESA | 0 | 5.9 -1.1 4.5 -17 -28 58 .22
GFZ | 0 | .7 .1 -1.5 -21 -52 -1 .38
GRG | 0 | 3.9 2.1 -14.5 -22 -8 -27 1.03
JPL | 0 | 2.3 -4.1 13.2 58 -42 31 .93
MIT | 0 | .8 -3.8 -.1 5 2 -7 .50
NGS | 0 | -1.3 -2.4 4.8 -36 6 -20 .87
SIO | 0 | -.8 5.2 22.7 11 -19 53 .51
COD | 1 | -.4 .5 -.5 -30 -5 -35 .65
EMR | 1 | 4.0 4.7 5.8 3 14 -59 .71
ESA | 1 | 2.4 -5.0 .3 -40 2 32 .31
GFZ | 1 | -.2 -.5 -2.2 -37 -38 -24 .65
GRG | 1 | .8 4.1 -21.1 -18 -15 -5 .88
JPL | 1 | 2.3 -2.1 23.6 -43 18 27 -.70
MIT | 1 | -1.8 -2.7 1.3 12 0 -14 .54
NGS | 1 | -.8 -.6 2.9 -14 6 -11 .67
SIO | 1 | -4.5 4.8 20.1 6 -28 -7 .56
COD | 2 | .2 -.4 .0 -37 3 -41 .86
EMR | 2 | 6.5 .5 9.1 0 22 -64 .90
ESA | 2 | 2.2 -3.0 3.0 -31 -16 42 .52
GFZ | 2 | -.3 -.4 -1.9 -45 -27 -29 .79
GRG | 2 | -.3 -.5 -3.9 -24 -25 -11 1.33
JPL | 2 | -2.6 -2.2 13.8 1 41 51 .38
MIT | 2 | 2.3 -1.3 3.7 -2 7 -16 .81
NGS | 2 | -2.8 -8.6 14.7 -89 1 -46 .73
SIO | 2 | -1.1 3.6 6.6 7 -53 54 .94
COD | 3 | -1.1 .5 -1.7 -22 10 -40 .67
EMR | 3 | 8.3 7.5 11.7 14 9 -47 .45
ESA | 3 | 2.7 -2.0 3.9 -26 -8 62 .21
GFZ | 3 | .0 -.1 -1.4 -46 -26 -18 .42
GRG | 3 | 6.2 -1.6 -6.4 -4 -12 19 1.04
JPL | 3 | 6.8 .4 18.7 -23 -16 39 .29
MIT | 3 | 4.1 -.1 8.0 -2 -7 -21 .24
NGS | 3 | -1.1 -3.9 8.4 -47 9 -18 .95
SIO | 3 | 4.9 6.0 29.7 28 -68 170 .53
COD | 4 | -1.6 .3 -2.7 -19 -3 -34 .69
EMR | 4 | 8.4 6.1 5.2 21 13 -65 .58
ESA | 4 | 7.1 4.1 7.1 -1 -65 75 .10
GFZ | 4 | -.2 .0 -.8 -37 -21 -21 .35
GRG | 4 | 1.3 -4.0 -8.4 -11 -39 6 .93
JPL | 4 | 5.3 1.4 11.8 25 -183 -58 .87
MIT | 4 | 2.3 .8 7.8 8 -1 4 .63
NGS | 4 | 1.1 -1.8 11.5 -44 -6 -4 1.02
SIO | 4 | 3.7 7.4 15.4 -14 -31 18 .44
COD | 5 | -1.7 .6 -2.8 -40 -12 20 .61
EMR | 5 | 7.1 5.3 8.1 10 21 -62 .47
ESA | 5 | 12.0 6.2 1.3 8 -21 86 .04
GFZ | 5 | .5 1.5 -.3 -31 -40 5 .02
GRG | 5 | -4.1 2.2 -27.3 -11 -34 10 1.01
JPL | 5 | -1.1 8.8 20.6 4 -89 41 -.25
MIT | 5 | 1.7 3.5 8.5 4 -7 4 .49
NGS | 5 | 4.1 -.9 7.6 -36 -32 16 .76
SIO | 5 | 2.8 7.4 6.6 19 -63 47 .47
COD | 6 | -1.2 .0 -2.3 -55 8 -24 .80
EMR | 6 | 6.5 2.0 15.7 20 22 -70 .39
ESA | 6 | 4.1 1.8 9.6 2 -33 57 .34
GFZ | 6 | -.4 -.7 -1.3 -51 5 -25 .14
GRG | 6 | 7.0 1.0 1.1 -7 -18 25 1.16
JPL | 6 | 2.4 3.9 28.3 -4 -22 -14 -.30
MIT | 6 | 3.7 1.9 15.8 -9 4 8 .34
NGS | 6 | 10.2 -5.2 4.7 -45 -72 43 .86
SIO | 6 | 4.0 7.6 21.6 24 23 4676 .67
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 1.1782.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1782.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 2.1782.[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 3.1782.[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 5.1782.0-6). 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 1782 summary. (Mar 02, 2014 - Mar 08, 2014)
Table 1.1782.a GPS week: 1782 MJD: 56718.000-56724.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 0 0 4 8 24 7 .10 11 10 | -760 -428 20 117
| 0 1 0 28 18 15 .03 | 225 418
emr 79| 1 1 4 -6 3 2 .07 18 18 | 4371 -485 15 93
| 0 1 1 10 24 12 .03 | 651 511
esa 150| 1 0 0 1 -29 13 -.21 8 8 | -787 638 9 111
| 1 0 1 18 19 13 .01 | 1091 1783
gfz 191| -1 0 -2 41 -7 -16 .18 10 10 | 330 -801 12 72
| 0 0 0 17 18 9 .03 | 501 928
grg 184| 1 0 -1 -40 1 -31 .31 16 16 | 80 -189 46 216
| 0 1 4 14 17 20 .04 | 150 401
igr n/a| 0 0 -1 -18 22 -6 -.16 5 5 | 11440 -583 16 72
| 0 0 1 10 15 19 .01 | 364 620
jpl 80| 0 0 0 34 -33 6 .03 17 17 | 3749 -538 18 122
| 1 1 1 35 70 24 .03 | 456 638
mit 299| 0 -2 -2 -13 6 -11 -.15 13 11 | 135 -358 269 501
| 0 0 1 15 22 19 .02 | 165 318
ngs 230| -1 0 -1 -45 70 -16 .02 13 12 | -735 -477 1747 3549
| 1 0 2 28 51 28 .05 | 219 402
sio 476| -1 0 -1 -6 -9 684 -.57 22 20 | --- --- --- ---
| 0 1 4 21 19 1757 .06 | --- ---
Table 1.1782.b GPS week : 1782 MJD: 56718.000-56724.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 5 6 5 6 |
2 | 6 5 5 6 5 5 6 |
3 | 5 4 4 3 4 4 4 |
4 | 7 7 6 7 8 8 5 |
5 | 5 5 5 0 5 6 5 |
6 | 5 0 --- --- --- --- --- |
7 | 5 5 5 5 6 5 5 |
8 | 5 5 5 5 5 5 5 |
9 | 5 4 4 4 4 4 4 |
10 | 4 4 4 5 4 4 4 |
11 | 5 5 4 4 4 4 4 |
12 | 5 5 4 4 5 5 5 |
13 | 4 4 4 4 5 4 5 |
14 | 5 5 5 4 4 6 4 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 4 5 5 5 |
17 | 5 5 5 5 6 0 6 |
18 | 5 5 4 4 5 5 4 |
19 | 5 5 4 4 5 4 5 |
20 | 5 4 5 5 5 5 5 |
21 | 5 4 5 4 4 5 5 |
22 | 5 5 4 4 4 5 4 |
23 | 4 4 4 3 4 4 5 |
24 | 4 4 4 4 4 5 4 |
25 | 5 4 4 4 4 6 5 |
26 | 4 4 4 4 3 4 4 |
27 | 5 4 4 4 4 4 4 |
28 | 4 4 5 4 4 5 5 |
29 | 5 4 5 5 5 5 5 |
30 | 0 0 0 0 0 0 0 |
31 | 6 5 5 4 5 5 5 |
32 | 4 4 3 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1782.0 GPS week: 1782 Day: 0 MJD: 56718.000
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| 0 2 6 -8 27 5 .09 11 10 | -364 -672 21 108
emr 78| 0 3 4 5 -3 -13 .06 18 18 | 4726 -809 15 85
esa 150| 0 -1 0 -15 -15 4 -.21 6 6 | -738 -636 9 103
gfz 194| 0 1 -2 25 -40 -17 .21 11 10 | 785 -1898 14 67
grg 188| 1 0 -4 -45 -20 -61 .24 16 15 | 176 -449 45 201
igr n/a| 0 0 0 -32 41 12 -.15 5 5 | 11082 -278 15 75
jpl 80| 0 1 2 78 -42 2 -.00 17 17 | 3482 -744 18 127
mit 300| 0 -3 -5 8 44 7 -.17 14 12 | 124 -473 269 528
ngs 229| -2 -1 -2 -13 106 33 .06 15 13 | -350 -713 1703 3511
sio 472| -1 0 -1 9 -9 -28 -.57 22 18 | --- --- --- ---
Table 2.1782.1 GPS week: 1782 Day: 1 MJD: 56719.000
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| 0 0 4 53 25 21 .07 10 10 | -748 -76 20 117
emr 80| 1 3 6 -3 -19 4 .06 19 19 | 4226 -318 14 80
esa 150| 0 0 1 -15 -11 -1 -.22 6 6 | -958 1846 8 100
gfz 193| -1 0 -2 65 -2 -1 .18 10 10 | 456 -209 12 80
grg 185| 2 0 -4 -29 11 -17 .31 15 14 | 47 -39 41 230
igr n/a| 0 0 -1 -24 4 6 -.17 5 5 | 11494 -145 16 80
jpl 80| 0 1 1 -17 36 16 .04 17 17 | 3555 1 19 121
mit 300| 0 -2 -4 -17 -27 10 -.14 12 10 | 360 -819 187 465
ngs 227| -1 0 -1 -81 38 -53 .09 14 12 | -655 -272 1823 3846
sio 471| 0 0 5 0 -17 -1 -.59 21 21 | --- --- --- ---
Table 2.1782.2 GPS week: 1782 Day: 2 MJD: 56720.000
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 3 43 3 20 .10 12 11 | -913 -132 17 116
emr 80| 1 0 5 5 -9 11 .10 19 19 | 4030 -559 14 91
esa 150| 1 -1 0 -9 -15 9 -.22 6 6 | -555 71 8 116
gfz 194| -1 1 -2 47 18 -9 .18 10 10 | 263 -453 13 78
grg 187| 1 1 2 -25 12 -40 .30 16 14 | -64 438 48 217
igr n/a| 0 1 -2 -22 33 -3 -.16 5 5 | 11532 -704 17 87
jpl 80| 0 1 0 -2 54 29 .05 17 17 | 3834 -689 17 117
mit 300| 0 -1 -4 -12 12 -25 -.12 10 9 | 144 -49 296 473
ngs 233| -2 0 1 -36 -33 -24 .06 14 12 | -970 3 1932 3733
sio 473| 0 0 0 -21 0 27 -.49 22 22 | --- --- --- ---
Table 2.1782.3 GPS week: 1782 Day: 3 MJD: 56721.000
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| 1 -1 4 5 21 20 .13 10 9 | -692 -405 22 114
emr 80| 3 2 3 -13 -23 11 .04 18 18 | 3439 141 14 96
esa 150| 2 0 0 -5 -24 2 -.19 6 6 | -276 644 11 125
gfz 194| -1 1 -2 25 -5 -14 .18 11 9 | -103 -222 15 72
grg 186| 1 0 0 -31 -2 -13 .30 15 16 | 262 -533 40 221
igr n/a| 1 0 -2 -9 23 1 -.16 5 5 | 10862 -17 18 74
jpl 80| -2 0 0 34 -16 43 .08 17 17 | 2950 437 19 122
mit 300| -1 -1 -2 -1 -8 -41 -.14 10 8 | 279 -581 408 511
ngs 234| -2 0 -2 -15 86 -14 -.01 14 12 | -684 -399 1933 3441
sio 476| 0 0 -1 21 -9 134 -.54 22 19 | --- --- --- ---
Table 2.1782.4 GPS week: 1782 Day: 4 MJD: 56722.000
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 0 3 -10 36 10 .13 11 10 | -1078 -19 19 123
emr 80| 2 3 4 -17 44 17 .12 18 18 | 4370 -1053 16 94
esa 150| 2 0 0 11 -39 22 -.21 7 7 | -303 99 9 112
gfz 192| -1 2 -1 61 6 -28 .15 10 10 | 488 -1718 12 69
grg 184| 0 -2 0 -31 26 -13 .36 18 18 | 242 -734 50 198
igr n/a| 0 0 -3 -21 35 -17 -.15 5 5 | 11599 -1131 16 63
jpl 80| -1 2 1 27 -156 0 .05 16 16 | 4133 -1090 18 113
mit 300| -1 -2 -2 -14 3 -4 -.16 12 9 | 191 -495 416 601
ngs 234| 0 -1 0 -65 87 -41 .00 12 11 | -938 -264 1643 3345
sio 507| -1 0 -9 -45 22 4 -.58 21 18 | --- --- --- ---
Table 2.1782.5 GPS week: 1782 Day: 5 MJD: 56723.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| 0 0 5 -13 55 -17 .10 10 10 | -670 -1209 22 112
emr 80| 2 0 3 -18 8 -9 .06 17 17 | 4257 194 17 98
esa 150| 1 1 -1 14 -66 35 -.21 22 20 | -3067 3933 12 120
gfz 189| -1 0 0 31 -10 -21 .13 10 10 | -509 494 12 69
grg 180| 0 0 -8 -62 1 -53 .33 18 19 | -126 -4 55 239
igr n/a| 0 0 0 -21 11 -45 -.16 6 6 | 11541 -138 19 69
jpl 80| 2 -3 0 72 -66 -23 -.02 16 16 | 4026 -270 18 121
mit 300| 0 -2 0 -15 15 -4 -.17 16 12 | -93 69 204 459
ngs 230| 0 1 -1 -31 99 -4 -.01 12 11 | -649 -1247 1530 3570
sio 464| -2 -3 -1 -6 -44 -14 -.57 23 21 | --- --- --- ---
Table 2.1782.6 GPS week: 1782 Day: 6 MJD: 56724.000
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 0 4 -10 2 -7 .07 11 10 | -860 -483 21 129
emr 80| 1 -1 2 -5 26 -8 .06 18 18 | 5554 -991 19 107
esa 150| 0 0 -1 33 -30 24 -.19 6 6 | 385 -1490 8 101
gfz 186| -1 0 -1 31 -16 -26 .20 11 10 | 934 -1604 10 74
grg 181| 2 0 3 -58 -18 -20 .34 16 15 | 28 -7 44 208
igr n/a| 0 0 0 0 5 0 -.19 6 5 | 11975 -1674 16 61
jpl 80| 1 0 0 46 -42 -18 .03 16 16 | 4268 -1412 19 134
mit 299| 0 -1 -1 -42 4 -24 -.16 17 15 | -57 -164 107 470
ngs 223| 0 -1 -5 -74 108 -9 -.04 12 11 | -904 -451 1667 3400
sio 470| -2 -1 -3 0 -5 4667 -.68 21 23 | --- --- --- ---
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 3.1782.0 GPS week: 1782 Day: 0 MJD: 56718.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 9 15 5 8 11 7 19 11 18 12 4 | 37 34 32 36 38 32 37 31 38 27 34
2E | 15 19 7 10 25 5 18 16 13 15 5 | 20 18 16 21 26 15 17 16 23 15 16
3 | 7 9 5 13 16 3 14 13 20 20 4 | 26 26 25 31 31 25 25 29 30 30 26
4E | 13 19 8 8 18 8 18 36 21 19 6 | 97 97 95 96 98 94 94 105 94 95 96
5 | 13 17 7 10 16 8 20 11 9 17 4 | 16 15 8 12 6 8 16 12 13 12 11
6 | 13 13 7 14 16 8 14 9 20 --- 4 | 50 17 3 4 4 13 5 6 51 --- 48
7 | 10 22 7 6 17 4 16 19 11 11 4 | 33 30 23 29 34 26 29 29 33 22 27
8E | 14 17 5 11 16 6 20 20 11 20 5 | 52 61 52 52 60 52 62 59 52 53 54
9 | 9 16 6 12 19 5 15 16 11 28 4 | 20 27 16 20 23 17 27 24 21 30 18
10 | 10 16 6 8 18 4 12 12 14 24 4 | 15 16 18 18 25 16 15 23 21 22 16
X11 | 9 15 5 11 19 4 --- 11 16 20 4 | 27 26 25 29 37 23 --- 20 29 25 25
12 | 8 22 6 8 18 5 20 10 12 17 4 | 26 28 21 25 31 22 27 23 27 18 23
13 | 8 16 7 8 15 3 16 10 13 38 4 | 36 38 36 41 44 36 38 34 38 46 36
14 | 11 19 5 12 15 4 15 12 21 19 5 | 35 34 37 46 44 37 36 39 35 28 37
15 | 12 24 7 10 12 3 23 11 9 31 5 | 28 30 29 38 38 29 30 32 30 28 29
16 | 12 17 6 12 16 5 20 12 21 28 5 | 25 24 17 25 25 17 24 21 26 21 19
17 | 14 20 7 11 14 6 16 12 19 31 5 | 20 28 21 26 26 22 27 21 32 30 24
18 | 11 23 4 17 16 4 20 9 16 24 5 | 21 26 18 35 30 18 23 20 20 19 20
19 | 10 16 6 11 11 5 16 12 16 26 4 | 30 32 32 37 36 30 32 29 28 30 31
20 | 10 18 5 9 16 5 19 15 11 20 4 | 22 28 19 26 30 19 23 26 23 17 21
21E | 9 15 4 14 20 5 19 8 12 16 4 | 25 23 24 24 30 21 25 18 24 22 22
22 | 9 19 4 14 13 4 16 10 13 19 4 | 26 22 23 35 35 24 23 26 24 17 25
23 | 7 14 7 8 13 3 13 9 11 25 3 | 30 29 29 35 35 28 29 26 27 25 29
24 | 10 16 7 9 9 5 15 7 14 13 4 | 22 22 18 25 23 17 23 19 21 21 19
25 | 9 21 5 8 16 5 14 10 16 12 4 | 23 31 23 29 29 24 33 20 29 21 24
26 | 10 15 6 7 12 5 13 12 9 20 3 | 21 23 27 30 32 23 25 31 23 29 25
X27 | 8 16 6 14 --- 5 16 12 20 13 5 | 20 27 22 26 --- 19 29 21 25 15 21
28 | 11 17 6 9 15 5 17 15 7 16 4 | 19 26 19 23 31 18 26 22 22 14 20
29 | 13 21 7 14 15 7 20 13 17 41 5 | 27 33 24 29 31 24 31 26 34 40 26
X30E | 4 --- --- --- --- 147 --- --- --- --- 0 | 537 --- --- --- --- 542 --- --- --- --- 537
31 | 11 22 7 10 21 4 17 21 13 12 5 | 30 36 32 41 45 32 34 33 37 29 33
32 | 7 10 4 8 14 7 11 13 16 13 3 | 16 17 13 17 18 15 15 15 20 13 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 6 11 16 5 17 14 15 22 |T 44 29 25 31 33 41 29 27 30 27 43
WRMS | 10 18 6 10 15 5 17 12 13 18 |NE 25 26 22 28 29 22 25 24 27 24 24
MEDI | 10 17 6 10 16 5 16 12 14 19 |MD 26 27 23 29 31 23 27 24 27 22 25
Table 3.1782.1 GPS week: 1782 Day: 1 MJD: 56719.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 19 7 10 14 6 16 7 15 9 4 | 29 25 23 30 33 23 29 22 27 20 24
2E | 15 18 6 9 23 4 21 13 13 15 5 | 16 20 15 18 26 12 20 15 24 17 15
3 | 9 10 7 12 16 5 11 10 16 19 4 | 25 24 22 31 24 21 20 24 26 22 22
4E | 13 24 8 11 16 6 17 32 21 22 6 | 78 81 81 80 80 81 82 82 90 76 81
5 | 15 19 8 9 17 6 18 12 14 15 5 | 16 16 13 16 7 10 16 14 15 15 12
X6 | 4 285 --- --- --- 284 --- 221 452 --- 0 | 103 36 --- --- --- 23 --- 10 116 --- 99
7 | 6 22 8 7 21 5 16 11 14 14 4 | 29 27 20 29 32 22 28 22 28 19 22
8E | 10 18 7 12 13 5 19 17 10 18 4 | 53 51 50 49 51 48 49 51 48 55 49
9 | 8 15 7 10 16 6 15 15 8 23 4 | 25 22 20 23 19 16 25 22 18 27 18
10 | 9 16 5 8 17 3 15 10 12 22 4 | 21 18 22 23 20 19 16 23 24 19 19
11 | 9 17 6 10 22 7 15 7 15 17 4 | 24 26 22 27 33 17 28 16 23 21 20
12 | 11 21 5 8 14 3 20 9 10 18 4 | 28 26 19 28 29 18 24 19 24 15 21
13 | 9 17 5 9 13 3 17 7 13 33 4 | 26 32 24 30 34 24 32 25 25 38 25
14 | 17 20 6 13 15 5 17 14 14 19 5 | 32 23 26 33 31 26 25 26 28 20 26
15 | 12 23 7 10 12 4 21 7 17 31 5 | 28 28 25 34 32 23 31 24 25 24 25
16 | 12 20 6 10 14 3 20 11 16 25 5 | 21 23 13 21 22 14 23 17 20 20 15
17 | 10 22 8 14 11 5 16 10 13 28 4 | 18 24 16 23 20 14 20 16 22 22 17
18 | 10 22 5 15 16 4 19 9 9 26 4 | 22 24 15 29 26 16 21 18 19 20 18
19 | 11 16 7 11 12 8 20 9 18 25 4 | 26 25 20 29 25 20 24 21 24 24 21
20 | 9 14 5 7 14 4 20 13 13 23 4 | 23 23 18 25 29 18 24 24 23 17 20
21E | 9 18 5 11 19 5 13 8 15 14 4 | 27 29 21 26 29 21 27 20 24 23 22
22 | 10 19 5 12 18 4 17 9 11 19 4 | 23 21 17 25 30 18 20 19 17 12 18
23 | 6 17 5 9 11 4 14 11 14 21 4 | 23 25 20 27 25 19 23 22 19 17 20
24 | 8 14 6 9 12 4 14 13 13 12 4 | 25 23 24 30 29 22 26 18 28 20 23
25 | 12 20 4 11 9 5 15 6 11 16 4 | 22 29 23 26 24 17 28 16 20 20 19
26 | 8 17 8 8 9 5 14 9 10 13 3 | 22 19 26 28 25 20 24 24 22 21 22
X27 | 7 12 6 9 --- 5 13 8 15 13 3 | 25 23 22 27 --- 18 26 18 22 17 21
28 | 7 21 6 9 13 7 16 13 11 17 4 | 20 25 19 24 27 15 22 17 23 15 18
29 | 7 18 5 10 13 7 19 8 11 30 4 | 27 28 22 29 25 20 25 22 26 25 23
X30E | 4 --- --- --- --- 124 --- --- --- --- 0 | 344 --- --- --- --- 379 --- --- --- --- 344
31 | 8 23 7 9 19 5 17 14 16 9 5 | 28 31 22 31 38 24 27 26 30 19 25
32 | 8 23 6 8 17 5 12 8 13 17 4 | 15 24 15 14 17 10 14 15 14 18 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 6 10 15 5 17 12 14 21 |T 38 27 23 28 29 32 26 22 28 23 35
WRMS | 10 19 6 10 14 5 17 10 12 21 |NE 26 24 20 26 25 18 23 19 26 20 23
MEDI | 9 19 6 10 14 5 16 10 13 18 |MD 25 25 21 27 27 19 24 21 24 20 21
Table 3.1782.2 GPS week: 1782 Day: 2 MJD: 56720.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 14 14 3 8 13 7 14 7 11 11 3 | 31 33 30 38 37 27 30 30 32 27 30
2E | 19 19 6 8 21 4 20 10 11 13 5 | 21 20 22 23 26 18 19 17 26 18 18
3 | 12 13 4 8 18 3 8 6 15 26 3 | 28 24 23 31 30 25 25 27 36 39 26
4E | 15 19 9 9 17 7 18 26 17 24 6 | 47 48 48 50 46 44 47 44 49 48 45
X5 | 12 20 6 9 --- 7 --- 10 13 14 4 | 17 18 14 18 --- 9 --- 16 16 14 14
7 | 12 23 8 11 19 5 18 10 14 12 5 | 38 31 26 36 32 28 28 27 33 20 27
8E | 15 21 7 11 17 6 22 14 11 25 5 | 47 45 43 45 46 41 44 48 48 50 43
9 | 11 15 7 11 17 4 15 11 9 29 4 | 28 26 20 25 19 18 25 21 24 33 19
10 | 10 18 8 10 19 3 15 8 13 16 4 | 18 14 18 18 19 12 14 17 21 18 14
11 | 10 20 4 8 21 9 11 8 15 17 4 | 28 36 22 28 36 20 21 21 25 24 24
12 | 9 22 5 9 14 3 21 8 6 19 4 | 28 27 23 29 31 20 26 22 27 16 23
13 | 8 16 5 8 13 3 17 11 16 37 4 | 32 34 29 33 33 27 34 30 24 46 28
14 | 13 17 4 13 9 6 15 15 13 24 4 | 40 32 33 42 36 34 34 34 30 26 34
15 | 14 23 7 10 11 5 22 8 15 37 5 | 36 29 29 36 32 30 30 28 26 30 28
16 | 14 19 5 10 16 3 19 11 17 24 5 | 25 24 16 23 25 17 26 20 29 20 18
17 | 14 23 7 13 13 4 17 9 14 35 5 | 28 26 24 28 26 24 24 20 27 28 25
18 | 10 18 5 13 13 4 19 7 10 20 4 | 24 23 20 31 27 19 23 21 24 13 21
19 | 13 19 5 9 17 4 16 7 15 23 4 | 28 30 24 33 35 26 29 27 32 30 26
20 | 13 17 6 10 16 5 18 13 11 25 4 | 22 23 17 23 25 15 21 21 23 19 18
21E | 11 16 5 11 20 4 16 7 16 12 4 | 25 21 20 23 30 19 25 20 23 16 20
22 | 8 18 5 10 15 5 16 7 11 15 4 | 24 24 21 29 31 24 23 23 25 14 22
23 | 7 14 5 9 11 4 13 11 17 19 4 | 28 28 25 30 24 23 28 26 26 20 24
24 | 11 16 6 9 14 5 14 10 12 13 4 | 29 25 25 29 31 23 28 22 26 20 24
25 | 8 20 3 9 10 4 14 7 10 15 3 | 22 28 21 25 25 19 29 19 25 20 21
26 | 13 14 5 8 11 5 12 9 14 16 3 | 24 22 25 29 26 22 22 27 24 21 23
X27 | 14 14 6 9 --- 6 12 6 12 11 4 | 26 27 22 28 --- 22 30 23 29 21 23
28 | 13 27 7 13 16 5 15 9 12 16 5 | 23 33 21 31 31 19 24 20 25 18 21
29 | 8 22 6 13 15 5 20 8 15 25 4 | 30 29 24 29 27 22 28 23 28 22 24
X30E | 3 --- --- --- --- 125 --- --- --- --- 0 | 278 --- --- --- --- 293 --- --- --- --- 279
31 | 12 21 7 13 18 4 19 10 21 10 5 | 37 39 32 38 43 33 38 35 40 31 34
32 | 7 13 5 7 13 3 9 8 11 16 3 | 20 20 14 21 19 14 17 16 23 16 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 19 6 10 16 5 17 10 14 22 |T 36 27 24 30 30 31 27 24 28 24 32
WRMS | 11 19 6 10 14 5 17 9 12 22 |NE 27 26 22 28 28 21 26 23 26 23 23
MEDI | 12 18 5 9 15 5 16 9 13 17 |MD 28 27 23 29 30 22 26 22 26 20 24
Table 3.1782.3 GPS week: 1782 Day: 3 MJD: 56721.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 17 19 5 12 13 6 20 8 17 12 5 | 39 32 26 34 33 31 34 27 32 28 29
2E | 21 17 9 10 20 5 27 10 11 15 5 | 24 20 17 22 22 17 23 17 20 19 17
3 | 8 8 5 8 15 4 11 6 13 21 3 | 27 26 23 29 27 23 26 25 25 30 24
4E | 17 22 11 24 20 8 16 25 19 29 7 | 82 80 77 85 74 80 83 75 78 80 78
X5 | 3 --- --- --- --- 46 --- --- --- --- 0 | 24 --- --- --- --- 23 --- --- --- --- 21
7 | 8 27 6 7 17 4 22 13 10 12 5 | 28 31 22 29 31 24 33 25 28 24 24
8E | 11 18 6 12 14 8 23 11 11 30 4 | 56 57 51 52 57 52 56 54 55 57 53
9 | 7 15 5 9 20 6 14 8 10 29 4 | 22 25 18 23 21 18 25 22 24 33 19
10 | 10 18 6 11 22 6 14 6 14 16 4 | 20 19 18 23 21 20 15 21 15 18 17
11 | 10 13 5 8 18 4 15 5 15 18 4 | 27 30 22 27 33 22 30 20 25 25 23
12 | 6 18 5 7 15 5 19 8 8 19 3 | 23 26 17 26 30 20 25 21 24 18 20
13 | 9 16 5 8 13 5 16 13 13 25 4 | 27 34 29 32 35 31 35 31 30 35 29
14 | 7 17 6 11 11 5 14 14 16 22 4 | 37 37 39 46 42 38 37 40 38 32 38
15 | 9 21 6 9 14 5 23 9 14 33 4 | 29 32 27 33 35 30 30 29 29 31 28
16 | 8 16 4 10 16 6 19 8 12 24 4 | 23 23 17 20 23 17 25 17 19 18 18
17 | 12 18 10 16 14 4 19 12 16 40 5 | 20 24 19 25 22 19 23 20 18 39 19
18 | 8 18 4 12 15 3 18 7 10 23 4 | 21 24 19 27 27 17 22 19 18 16 19
19 | 10 15 5 11 11 6 15 8 15 24 4 | 28 29 26 32 32 25 29 26 22 27 26
20 | 12 16 4 9 14 7 17 13 14 26 4 | 22 21 18 23 27 16 20 22 18 20 18
21E | 10 18 5 12 15 5 15 7 15 10 4 | 29 30 22 27 29 22 26 21 25 20 23
22 | 8 13 5 9 14 4 15 6 11 15 3 | 23 21 21 29 33 22 22 23 22 15 22
23 | 8 15 4 7 10 4 12 7 13 21 3 | 25 27 26 29 29 26 28 25 24 22 25
24 | 8 15 7 7 10 3 14 9 13 13 3 | 20 24 20 24 25 19 26 19 24 22 20
25 | 7 24 4 9 11 6 13 7 16 13 4 | 20 32 27 23 25 20 28 16 23 20 19
26 | 10 13 7 7 14 6 10 8 20 19 4 | 22 21 23 27 27 23 25 26 31 23 23
X27 | 10 11 5 8 --- 6 14 8 16 12 4 | 21 25 22 25 --- 19 30 22 23 15 22
28 | 9 21 4 15 14 4 14 6 11 17 4 | 20 25 17 30 29 17 22 19 20 15 19
29 | 8 20 6 14 12 5 22 6 15 24 4 | 27 29 22 27 27 20 29 23 27 22 23
X30 | 3 --- --- --- --- 83 --- --- --- --- 0 | 615 --- --- --- --- 576 --- --- --- --- 615
31 | 6 21 5 6 14 4 17 7 13 13 4 | 30 32 26 34 40 28 32 27 34 25 29
32 | 8 11 4 9 11 3 12 8 15 14 3 | 17 17 13 16 18 14 15 16 19 17 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 11 15 5 17 10 14 22 |T 46 29 24 30 31 42 29 25 27 26 44
WRMS | 9 18 6 9 16 5 17 8 12 19 |NE 24 26 22 27 28 22 26 23 24 23 22
MEDI | 8 17 5 9 14 5 15 8 14 19 |MD 24 26 22 27 29 22 26 22 24 22 23
Table 3.1782.4 GPS week: 1782 Day: 4 MJD: 56722.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 13 21 8 8 38 6 16 11 16 15 6 | 32 35 34 35 49 33 35 34 39 32 33
2E | 16 17 8 11 21 6 20 8 13 14 5 | 30 31 24 26 27 22 30 26 25 30 26
3 | 12 13 4 9 16 5 11 11 13 19 4 | 29 31 27 28 29 27 25 28 32 31 27
4E | 15 21 13 10 21 6 18 36 19 33 7 | 97 95 93 90 95 92 97 101 91 97 93
5 | 14 18 9 13 13 7 14 15 15 13 5 | 22 16 7 14 13 13 13 15 13 14 15
7 | 11 28 8 8 17 4 22 19 9 13 5 | 29 31 24 29 34 26 30 28 25 27 25
8E | 11 24 8 15 20 9 19 10 12 31 5 | 45 54 44 46 54 45 49 44 50 46 45
9 | 6 12 7 8 17 6 14 9 9 30 3 | 21 25 17 22 27 19 23 20 22 35 19
10 | 7 15 6 9 19 4 12 5 13 16 3 | 16 18 16 21 23 17 13 23 17 22 17
11 | 9 17 6 8 16 6 13 9 13 18 4 | 24 29 23 27 34 20 25 22 27 22 23
12 | 10 18 6 11 18 4 21 10 11 16 4 | 27 26 21 31 35 21 24 24 27 17 23
13 | 11 16 5 9 12 5 17 16 13 27 4 | 25 34 29 34 37 32 32 32 33 38 30
14 | 9 16 5 10 19 7 15 8 11 25 4 | 40 39 36 45 43 40 35 37 38 34 38
15 | 9 20 8 12 12 5 22 10 11 34 4 | 34 31 31 34 36 29 32 32 34 31 31
16 | 9 17 5 13 13 5 16 10 15 20 4 | 25 27 18 24 27 20 23 21 27 19 20
17 | 12 18 8 12 31 6 23 16 13 41 6 | 19 27 22 29 36 18 26 26 22 43 20
18 | 13 19 5 10 17 6 17 8 12 22 4 | 23 27 22 27 30 21 24 24 20 23 22
19 | 13 14 7 7 11 6 18 11 14 24 4 | 30 32 27 28 32 25 28 28 30 24 27
20 | 11 16 7 9 17 5 15 15 11 24 4 | 25 26 23 27 33 24 20 29 25 26 24
21E | 13 15 6 11 18 4 14 9 9 8 4 | 28 26 22 25 28 23 22 23 27 22 23
22 | 12 15 5 10 16 5 15 8 10 14 4 | 23 26 23 28 33 24 23 26 23 23 24
23 | 10 16 5 7 11 5 13 8 11 23 3 | 27 31 29 32 30 30 26 29 32 29 29
24 | 7 15 5 6 13 6 14 10 9 13 3 | 23 25 24 25 30 21 25 23 23 23 22
25 | 10 23 5 9 18 5 13 8 9 16 4 | 22 32 32 26 27 20 27 22 24 24 21
26 | 6 12 5 8 13 5 11 6 7 16 3 | 24 23 26 30 31 24 25 30 27 26 26
X27 | 12 13 6 7 --- 4 11 9 14 14 4 | 25 32 27 26 --- 25 31 27 29 21 26
28 | 9 16 4 11 15 5 11 8 11 15 3 | 21 29 22 32 30 21 24 24 23 19 23
29 | 13 18 6 15 16 6 19 6 10 18 4 | 35 34 27 33 33 26 31 29 33 26 30
X30 | 3 --- --- --- --- 90 --- --- --- --- 0 | 631 --- --- --- --- 603 --- --- --- --- 631
31 | 9 21 7 9 20 4 21 7 16 13 4 | 29 33 27 34 41 29 28 28 33 27 28
32 | 9 18 5 9 16 5 10 11 9 12 4 | 21 25 19 23 23 20 15 23 22 21 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 7 10 18 5 16 12 12 21 |T 48 31 27 31 34 45 28 29 29 29 47
WRMS | 10 18 7 10 18 5 16 9 11 18 |NE 25 28 23 28 31 23 25 26 26 25 24
MEDI | 11 17 6 9 17 5 15 9 11 16 |MD 25 29 24 28 32 24 25 26 27 26 25
Table 3.1782.5 GPS week: 1782 Day: 5 MJD: 56723.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 19 7 9 18 4 19 11 11 16 4 | 26 27 21 26 30 21 23 27 26 23 22
2E | 16 16 8 10 22 7 14 11 12 13 5 | 35 32 35 32 38 30 29 28 41 32 33
3 | 8 11 7 9 15 6 15 9 11 25 3 | 26 25 21 23 25 21 23 24 23 26 21
4E | 14 23 12 10 24 7 21 46 16 32 8 | 119 117 116 118 122 120 118 136 116 128 118
5 | 15 19 7 11 17 7 15 17 17 15 5 | 17 17 8 12 8 11 15 14 16 12 11
7 | 9 21 9 8 16 4 17 16 13 18 5 | 28 27 22 25 33 22 25 22 27 19 22
8E | 11 19 8 11 14 7 19 18 14 33 5 | 66 66 65 65 64 65 66 72 71 73 66
9 | 4 16 6 6 18 5 10 14 14 28 4 | 20 24 16 19 22 17 20 21 22 29 16
10 | 6 15 8 7 23 5 11 15 11 16 4 | 13 14 17 14 23 13 14 15 11 17 12
11 | 7 15 8 8 17 7 17 10 11 19 4 | 21 27 14 22 33 16 21 19 24 22 18
12 | 10 17 10 12 19 5 15 12 17 21 5 | 25 27 18 26 30 19 24 18 29 17 20
13 | 9 16 6 8 12 5 19 15 8 28 4 | 20 30 23 25 33 22 32 21 22 33 22
14 | 21 15 7 11 23 8 13 12 13 29 5 | 39 35 33 41 41 36 35 34 34 28 34
15 | 8 20 8 12 19 8 22 13 11 36 5 | 27 28 22 29 34 26 30 25 29 24 24
16 | 12 16 5 9 16 4 18 10 13 28 4 | 20 22 13 19 25 15 23 17 21 18 16
X17 | 5 --- --- --- --- 31 --- --- --- --- 0 | 14 --- --- --- --- 10 --- --- --- --- 14
18 | 12 19 5 13 19 6 18 10 9 25 4 | 20 25 19 25 32 19 22 19 20 19 19
19 | 10 14 6 8 12 6 16 11 10 28 4 | 29 28 21 27 26 20 28 24 25 21 23
20 | 8 16 10 10 14 4 18 19 12 27 4 | 18 19 19 23 29 17 21 27 22 25 18
21E | 11 12 4 12 23 6 20 9 12 12 4 | 31 28 26 25 41 26 34 26 31 24 26
22 | 10 17 6 8 21 5 16 11 10 18 4 | 21 26 21 23 36 20 23 20 21 17 20
23 | 10 16 6 8 11 4 13 9 10 25 3 | 20 28 21 24 26 19 24 23 22 19 21
24 | 4 15 8 11 15 7 16 13 16 14 4 | 20 26 19 24 26 19 25 18 23 18 19
25 | 8 26 114 8 18 10 14 13 17 15 6 | 18 33 93 17 26 18 24 17 26 18 17
26 | 7 11 7 11 16 6 9 15 9 18 3 | 17 18 19 20 25 19 19 17 20 16 17
X27 | 11 11 8 9 --- 7 13 8 10 16 4 | 24 25 18 18 --- 16 29 20 21 17 19
28 | 10 19 6 11 14 5 16 19 12 22 4 | 19 25 18 26 27 15 24 20 19 20 18
29 | 8 17 5 13 18 8 20 8 9 16 4 | 26 29 21 27 28 21 27 21 22 19 22
X30 | 5 --- --- --- --- 138 --- --- --- --- 0 | 270 --- --- --- --- 303 --- --- --- --- 269
31 | 8 18 7 8 18 5 16 11 13 19 4 | 24 28 20 26 38 24 28 25 28 22 24
32 | 8 17 9 8 12 4 12 13 7 20 4 | 15 17 17 16 19 13 15 19 17 19 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 22 10 18 6 16 16 12 23 |T 35 30 27 28 33 33 29 27 28 26 32
WRMS | 10 17 20 10 19 6 16 12 11 21 |NE 21 25 22 22 28 18 23 20 22 20 19
MEDI | 9 16 7 9 17 6 16 12 12 20 |MD 21 27 21 25 29 19 24 21 23 20 20
Table 3.1782.6 GPS week: 1782 Day: 6 MJD: 56724.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 17 22 8 12 15 6 16 23 15 13 5 | 31 38 32 31 32 28 32 36 32 30 30
2 | 16 20 7 9 29 5 19 15 12 8 5 | 42 39 39 40 40 36 38 33 40 43 37
3 | 12 11 4 8 16 4 12 12 17 22 4 | 30 26 26 29 27 26 26 29 35 31 26
4E | 11 17 7 12 21 11 13 18 15 28 5 | 168 167 165 164 166 164 171 166 166 165 166
5 | 12 17 7 10 15 4 16 18 9 13 4 | 14 13 9 16 12 10 14 16 17 12 11
7 | 8 21 6 6 17 5 16 18 15 15 4 | 31 32 24 29 33 25 31 30 31 30 26
8E | 11 19 7 11 14 11 21 17 14 25 5 | 94 97 95 96 97 92 97 96 99 92 95
9 | 5 14 5 9 14 5 10 18 8 31 3 | 21 22 17 24 19 17 23 24 21 33 18
10 | 8 13 4 9 19 4 11 15 9 19 4 | 17 13 19 23 28 18 11 24 15 21 17
11 | 8 14 7 9 19 4 12 16 10 17 4 | 24 25 21 25 34 20 23 23 25 24 21
12 | 11 18 5 12 15 6 19 10 9 20 4 | 23 23 18 27 29 16 23 19 23 20 19
13 | 11 18 5 12 13 3 17 10 14 28 4 | 32 37 34 42 42 35 37 33 35 41 34
14 | 11 16 6 12 12 5 14 12 12 25 4 | 36 38 38 47 41 36 38 40 35 39 38
15 | 11 19 6 12 16 8 21 12 7 28 4 | 28 29 30 39 41 31 32 34 32 32 30
16 | 15 16 5 11 12 7 20 13 13 24 4 | 22 24 15 18 24 17 25 20 24 16 17
17 | 10 25 7 15 12 4 18 35 16 32 6 | 11 22 5 9 2 7 17 4 6 5 7
18 | 10 19 6 11 13 5 15 12 8 30 4 | 21 21 20 29 30 18 20 22 21 27 19
19 | 14 16 7 13 12 6 18 14 17 23 5 | 35 30 29 35 31 29 30 29 29 25 29
20 | 9 18 6 13 16 7 17 24 12 21 5 | 25 24 23 30 33 22 24 34 24 28 23
21E | 10 14 7 13 12 4 14 18 12 13 4 | 26 26 25 22 30 22 27 25 31 24 23
22 | 8 16 7 10 14 3 14 13 13 16 4 | 24 23 24 31 36 24 23 28 25 21 24
23 | 10 16 6 13 11 4 15 16 11 23 4 | 29 30 32 39 32 31 30 31 30 30 30
24 | 7 15 5 11 13 7 13 13 11 12 4 | 22 23 18 25 26 18 23 20 24 20 19
25 | 9 27 6 8 13 6 14 10 11 14 4 | 17 32 27 22 24 16 26 17 23 20 17
26 | 10 12 5 7 16 5 10 14 12 16 3 | 23 23 28 30 35 26 23 31 31 25 26
X27 | 11 9 5 9 --- 4 12 8 12 12 3 | 26 27 25 26 --- 22 29 23 27 20 24
28 | 9 19 5 7 17 4 13 20 12 12 4 | 22 28 22 29 31 20 24 27 21 21 22
29 | 12 18 6 12 17 5 18 11 11 20 4 | 34 36 32 34 32 31 37 29 33 32 31
X30 | 2 --- --- --- --- 84 --- --- --- --- 0 | 825 --- --- --- --- 844 --- --- --- --- 825
31 | 11 18 8 13 16 6 17 13 17 15 5 | 26 28 23 38 39 26 33 30 27 24 27
32 | 7 14 4 7 10 5 8 17 10 13 3 | 19 16 15 20 22 15 19 24 17 16 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 6 11 16 6 16 17 12 21 |T 58 33 31 35 36 56 33 33 33 32 56
WRMS | 10 18 6 10 15 5 16 15 11 23 |NE 24 25 22 28 29 22 25 25 25 24 22
MEDI | 10 17 6 11 15 5 15 14 12 19 |MD 26 26 24 29 32 24 26 28 27 25 24
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 4.1782 GPS week: 1782 MJD: 56718.0-56724.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2961 |U 5 5 14 |U 11 12 36 |U 8 8 18 |
emr | emr 2868 | 7 6 19 |U 10 14 32 | 10 8 21 |
esa | esa 2866 | 5 5 14 |U 9 12 31 | 9 9 18 |
gfz | gfz 2858 |U 5 5 15 |U 9 11 31 |U 10 11 21 |
grg | grg 2756 |U 7 9 23 |U 11 13 40 |U 14 15 33 |
igr | igr 2806 | 5 5 14 | 9 12 34 | 9 8 18 |
igs | igs 2797 | 5 5 16 | 9 12 34 | 11 10 19 |
jpl | jpl 2832 | 7 6 18 | 10 13 32 |U 10 11 30 |
mit | mit 2880 | 53 25 52 |U 13 13 45 |U 14 16 36 |
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 5.1782.0 GPS week: 1782 Day: 0 MJD: 56718.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3046 | 4 5 12 | 8 7 31 | 10 7 28 |
emr | emr 2966 | 6 7 19 | 8 9 30 | 11 6 29 |
esa | esa 2976 | 4 4 12 | 7 7 30 | 9 9 24 |
gfz | gfz 2968 | 4 5 15 | 8 7 26 | 11 11 28 |
grg | grg 2880 | 6 10 20 | 9 9 37 | 15 16 41 |
igr | igr 2974 | 4 4 13 | 6 7 27 | 9 8 25 |
igs | igs 2875 | 4 5 14 | 7 7 32 | 14 11 25 |
jpl | jpl 2872 | 7 5 17 | 8 8 29 | 11 11 38 |
mit | mit 2976 | 5 6 16 | 9 9 29 | 8 12 20 |
Table 5.1782.1 GPS week: 1782 Day: 1 MJD: 56719.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 | 5 4 15 | 15 21 45 | 8 11 17 |
emr | emr 2935 | 7 6 24 | 16 20 35 | 12 11 22 |
esa | esa 2880 | 5 4 12 | 14 19 35 | 10 11 15 |
gfz | gfz 2873 | 5 4 15 | 14 16 35 | 13 15 21 |
grg | grg 2784 | 6 11 30 | 14 18 42 | 15 13 34 |
igr | igr 2927 | 6 5 13 | 14 18 34 | 9 11 16 |
igs | igs 2843 | 4 5 16 | 14 17 35 | 16 14 20 |
jpl | jpl 2872 | 7 5 18 | 16 18 35 | 13 10 30 |
mit | mit 2976 | 328 136 258 | 14 20 68 | 14 17 27 |
Table 5.1782.2 GPS week: 1782 Day: 2 MJD: 56720.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2963 | 5 4 10 | 10 9 37 | 8 9 21 |
emr | emr 2872 | 8 6 12 | 10 9 35 | 14 13 31 |
esa | esa 2880 | 6 4 13 | 9 8 34 | 10 11 21 |
gfz | gfz 2872 | 6 4 12 | 9 8 33 | 15 17 31 |
grg | grg 2688 | 7 5 26 | 9 12 37 | 18 23 43 |
igr | igr 2784 | 6 4 12 | 8 7 34 | 10 9 16 |
igs | igs 2767 | 7 5 16 | 9 8 36 | 16 15 25 |
jpl | jpl 2776 | 8 6 13 | 10 10 35 | 8 9 26 |
mit | mit 2880 | 5 4 17 | 10 11 37 | 12 11 27 |
Table 5.1782.3 GPS week: 1782 Day: 3 MJD: 56721.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2875 | 6 6 16 | 12 8 22 | 6 7 15 |
emr | emr 2776 | 8 7 21 | 9 14 25 | 8 8 15 |
esa | esa 2784 | 5 4 16 | 7 10 19 | 6 8 16 |
gfz | gfz 2777 | 5 3 17 | 8 10 21 | 7 10 17 |
grg | grg 2688 | 7 5 21 | 10 12 23 | 12 15 29 |
igr | igr 2679 | 6 4 17 | 8 9 24 | 9 8 17 |
igs | igs 2784 | 5 4 17 | 8 10 19 | 6 7 14 |
jpl | jpl 2776 | 8 9 22 | 9 13 22 | 13 21 46 |
mit | mit 2784 | 6 4 18 | 10 13 36 | 14 14 33 |
Table 5.1782.4 GPS week: 1782 Day: 4 MJD: 56722.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 7 11 | 7 12 28 | 8 7 16 |
emr | emr 2872 | 6 5 16 | 7 13 22 | 9 5 17 |
esa | esa 2880 | 4 7 11 | 5 11 20 | 11 9 20 |
gfz | gfz 2873 | 5 6 14 | 6 10 20 | 10 9 19 |
grg | grg 2784 | 7 8 23 | 6 14 33 | 13 13 26 |
igr | igr 2848 | 5 7 11 | 5 11 20 | 10 8 16 |
igs | igs 2783 | 4 5 12 | 5 12 20 | 10 7 17 |
jpl | jpl 2872 | 6 6 15 | 6 14 18 | 11 12 27 |
mit | mit 2880 | 7 7 18 | 22 13 38 | 25 27 62 |
Table 5.1782.5 GPS week: 1782 Day: 5 MJD: 56723.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2873 | 7 5 21 | 10 13 37 | 7 6 18 |
emr | emr 2779 | 9 5 24 | 8 13 28 | 9 5 22 |
esa | esa 2784 | 7 5 22 | 7 12 29 | 6 7 18 |
gfz | gfz 2773 | 7 5 21 | 8 10 28 | 7 7 16 |
grg | grg 2685 | 14 16 26 | 10 11 51 | 16 13 40 |
igr | igr 2650 | 7 4 21 | 7 12 33 | 8 7 24 |
igs | igs 2743 | 7 5 21 | 8 12 32 | 8 7 21 |
jpl | jpl 2779 | 8 5 24 | 9 14 34 | 6 7 21 |
mit | mit 2784 | 6 5 22 | 9 11 41 | 12 13 27 |
Table 5.1782.6 GPS week: 1782 Day: 6 MJD: 56724.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2973 | 3 5 11 | 12 17 51 | 6 6 12 |
emr | emr 2878 | 6 5 16 | 13 17 48 | 7 5 15 |
esa | esa 2880 | 4 5 14 | 12 16 53 | 7 7 14 |
gfz | gfz 2872 | 4 5 13 | 13 16 54 | 8 9 18 |
grg | grg 2784 | 5 6 14 | 15 15 56 | 10 10 19 |
igr | igr 2784 | 4 4 12 | 12 17 67 | 8 7 14 |
igs | igs 2784 | 4 4 12 | 13 17 65 | 7 7 13 |
jpl | jpl 2880 | 5 7 21 | 13 17 52 | 8 8 25 |
mit | mit 2880 | 11 15 20 | 15 17 64 | 16 21 53 |
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 6.1782 GPS week: 1782 MJD: 56718.500-56724.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 6 -7 -12 237 2 | 11 16
| 19 37 55 130 6 | 3
emr uuxuu | -23 -18 324 -73 -1 | 60 62
| 28 29 118 70 10 | 1
esa uuuuu | 14 2 -9 51 3 | 10 16
| 13 18 39 45 4 | 3
gfz uuuuu | 15 -37 47 -34 0 | 12 18
| 16 18 34 94 10 | 2
grg uuuuu | 4 53 -99 -225 -2 | 17 22
| 22 20 83 91 7 | 2
igr xxxxx | 4 30 32 -7 0 | 2 13
| 16 20 46 43 3 | 3
irf xxxxx | -3 8 -5 -83 3 | 0 14
| 11 8 35 57 3 | 3
jpl uuuuu | 26 -64 93 6 -11 | 25 27
| 77 32 49 91 8 | 2
mit uuuuu | -12 9 -34 -127 5 | 13 19
| 12 14 78 103 4 | 3
ngs uuuuu | -52 65 10 -44 -2 | 1 10
| 48 37 85 132 6 | 2
sio xxxxx | -8 35 38 -46 -8 | 60 61
| 25 14 67 68 11 | 2
Table 7.1782.0 GPS week: 1782 Day: 0 MJD: 56718.500
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 | -2 9 -54 166 -1 | 9 14
emr uuxuu | 14 -37 183 15 -13 | 61 63
esa uuuuu | -3 15 0 19 -4 | 9 15
gfz uuuuu | 32 -35 100 -73 13 | 8 14
grg uuuuu | 36 82 -120 -183 -3 | 15 21
igr xxxxx | -18 62 -31 66 3 | 0 12
irf xxxxx | 12 22 9 8 1 | -3 13
jpl uuuuu | 37 -94 76 103 -18 | 27 29
mit uuuuu | -13 18 8 65 -3 | 11 17
ngs uuuuu | -96 18 -34 -217 0 | -1 9
sio xxxxx | 10 43 -39 -24 -22 | 62 63
Table 7.1782.1 GPS week: 1782 Day: 1 MJD: 56719.500
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 | -1 -55 -109 93 -3 | 9 14
emr uuxuu | 1 -29 426 -51 7 | 60 61
esa uuuuu | 16 13 14 -1 1 | 8 14
gfz uuuuu | 19 -37 88 97 -1 | 11 18
grg uuuuu | 24 39 -106 -93 -8 | 16 22
igr xxxxx | 24 42 6 3 1 | 1 13
irf xxxxx | 6 -1 44 -40 4 | -3 13
jpl uuuuu | -49 -5 46 54 -17 | 27 30
mit uuuuu | -16 -21 59 -76 3 | 11 17
ngs uuuuu | -22 117 -10 -102 3 | -1 10
sio xxxxx | 5 40 -48 39 -21 | 62 63
Table 7.1782.2 GPS week: 1782 Day: 2 MJD: 56720.500
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 | 31 -60 48 338 -3 | 8 12
emr uuxuu | -22 -45 323 -76 8 | 59 60
esa uuuuu | 13 18 -82 -1 0 | 7 12
gfz uuuuu | -5 -28 36 74 -6 | 11 18
grg uuuuu | 3 30 63 -216 -7 | 15 20
igr xxxxx | -5 32 53 -33 -1 | -1 11
irf xxxxx | -13 3 23 -62 5 | -4 13
jpl uuuuu | -67 -42 106 -43 -6 | 24 25
mit uuuuu | -30 16 28 -101 6 | 9 15
ngs uuuuu | 40 75 -46 -91 3 | 0 10
sio xxxxx | -25 21 31 10 -9 | 60 61
Table 7.1782.3 GPS week: 1782 Day: 3 MJD: 56721.500
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 | 26 19 32 476 12 | 9 13
emr uuxuu | -7 0 243 -192 -11 | 60 61
esa uuuuu | 8 -10 -27 84 5 | 9 13
gfz uuuuu | 36 -14 22 -5 -3 | 12 18
grg uuuuu | -14 41 -130 -335 0 | 15 20
igr xxxxx | 15 0 69 6 1 | 1 11
irf xxxxx | -4 7 -4 -109 4 | -2 13
jpl uuuuu | -3 -69 92 -162 -5 | 24 26
mit uuuuu | -6 11 -21 -186 8 | 11 16
ngs uuuuu | -81 24 80 -96 -12 | 1 11
sio xxxxx | -7 29 52 -97 -8 | 60 61
Table 7.1782.4 GPS week: 1782 Day: 4 MJD: 56722.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -11 14 23 237 9 | 13 18
emr uuxuu | -67 40 213 -76 11 | 60 61
esa uuuuu | 22 -1 30 65 8 | 12 17
gfz uuuuu | -2 -72 8 -60 -9 | 15 20
grg uuuuu | -22 46 -140 -147 1 | 19 23
igr xxxxx | -14 31 16 -58 3 | 4 13
irf xxxxx | -21 2 -22 -81 2 | 2 14
jpl uuuuu | 165 -75 192 1 -18 | 27 29
mit uuuuu | -21 7 -54 -143 7 | 15 20
ngs uuuuu | -70 67 -94 -37 -3 | 3 10
sio xxxxx | -51 32 126 -43 4 | 60 61
Table 7.1782.5 GPS week: 1782 Day: 5 MJD: 56723.500
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 | -19 -10 -13 196 5 | 15 20
emr uuxuu | -43 -17 502 -127 2 | 63 64
esa uuuuu | 38 13 -22 89 2 | 14 19
gfz uuuuu | 7 -42 35 -142 -11 | 15 21
grg uuuuu | -14 78 -203 -315 -7 | 20 24
igr xxxxx | 15 33 106 15 -5 | 6 14
irf xxxxx | 1 18 -29 -146 -1 | 4 15
jpl uuuuu | 44 -96 53 -1 -16 | 26 27
mit uuuuu | 1 24 -81 -207 4 | 17 23
ngs uuuuu | -54 55 158 204 4 | 4 11
sio xxxxx | 24 61 110 -165 -5 | 60 61
Table 7.1782.6 GPS week: 1782 Day: 6 MJD: 56724.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 14 36 -15 156 -2 | 14 20
emr uuxuu | -36 -34 380 -7 -10 | 61 62
esa uuuuu | 6 -32 26 105 7 | 13 19
gfz uuuuu | 16 -32 41 -129 14 | 13 21
grg uuuuu | 14 53 -60 -288 12 | 17 23
igr xxxxx | 11 12 7 -48 0 | 4 15
irf xxxxx | -4 9 -60 -149 6 | 3 15
jpl uuuuu | 55 -69 86 91 0 | 22 26
mit uuuuu | 1 6 -175 -242 7 | 17 23
ngs uuuuu | -85 101 12 29 -9 | 4 11
sio xxxxx | -10 20 35 -41 8 | 56 58
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