[IGSREPORT-22612] Wk 1783 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Mar 28 19:48:57 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1783 (Mar 09, 2014 - Mar 15, 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:
igs1783[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1783[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1783[0-6].cls IGS GPS clock combination summary report.
igs17837.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17837.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 | NYA1
0 | ESA | 1 1 TNML TNML
0 | GFZ | 1 1 DRAO FAA1 MAL2 DRAO FAA1 MCIL
0 | GRG | DARW FAA1 HYDE MAL2 NYA1 NYAL TRO1 TWTF DARW FAA1
0 | GRG | HYDE MCIL NTUS NYA1 TRO1 TWTF
0 | MIT | 1
1 | COD | AUCK NYA1 TIDB
1 | EMR | 24 HERS MCM4 MCM4
1 | ESA | 1 1 KOUR MAL2 KOUR MAL2 SEY1
1 | GFZ | 1 2 1 2 DRAG DRAG
1 | GRG | KELY NYA1 RBAY KELY POL2 RBAY
1 | JPL | 2 10 CUSV INVK POL2
1 | MIT | 1 1
2 | COD | GRAZ KOUR
2 | EMR | 17 17 24 HERS THU3 NYAL THU3
2 | ESA | 1 1 PIMO PIMO
2 | GFZ | 1 2 1 2 NTUS NTUS
2 | GRG | BOGT FAA1 GLPS GRAZ HYDE KELY KERG KOUR MAL2 NYA1
2 | GRG | WUHN FAA1 KELY NYA1 PERT
2 | JPL | CUSV RESO
2 | MIT | 12
3 | COD | DGAR
3 | EMR | MIZU MIZU
3 | ESA | ARTU DGAV SEY1
3 | GFZ | 1 2 1
3 | GRG | ALRT HYDE KELY RBAY ALRT KELY NTUS
4 | EMR | 24 24
4 | ESA | QAQ1 WROC
4 | GFZ | 1 1
4 | GRG | DARW MDVJ NYA1 DARW MDVJ NYA1
5 | COD | 4 23 ARTU YAKT
5 | ESA | 4 ARTU SEY1 UNSA
5 | GFZ | 1 2 1 IRKJ NTUS HYDE IRKJ NTUS
5 | GRG | 4 4 DRAG HYDE ARTU BARH DRAG HYDE REUN
6 | COD | 5
6 | ESA | HOLM NTUS HOLM MBAR
6 | GFZ | 1 2 1 2 SEY1
6 | GRG | DRAG SPT0 SYOG DRAG SPT0
6 | JPL | 2 21
6 | MIT | NTUS
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. 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 G30 | | 4 | 4 | 4 | 4 | 4 | 4 |
7. 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.
8. 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 | -2.0 .3 -2.0 -43 3 -18 .63
EMR | 0 | 5.4 3.1 1.1 35 14 -44 .36
ESA | 0 | 4.6 4.3 15.4 -12 -37 48 .18
GFZ | 0 | .6 .1 -1.2 -45 -30 -23 .04
GRG | 0 | 7.5 4.1 6.3 -37 -36 -5 .95
JPL | 0 | 7.9 12.5 18.2 117 126 38 -.27
MIT | 0 | 1.5 2.1 10.1 -4 4 -17 .26
NGS | 0 | 4.7 1.6 26.3 -70 -36 14 .68
SIO | 0 | 2.9 7.9 24.0 39 -79 -4 .25
COD | 1 | -2.4 -.4 -1.4 -30 18 -31 .65
EMR | 1 | 5.1 -1.2 6.5 16 27 -49 .21
ESA | 1 | 1.4 1.2 9.7 -42 -7 45 .10
GFZ | 1 | -.2 .0 -1.9 -29 -26 -24 .26
GRG | 1 | 1.7 4.1 4.1 -38 -34 1 1.01
JPL | 1 | 5.3 5.5 14.8 -14 -95 27 .19
MIT | 1 | 3.8 1.3 5.3 6 -5 -14 .59
NGS | 1 | 6.4 .5 14.7 -44 -37 24 .75
SIO | 1 | .7 6.5 7.6 30 -48 7 .53
COD | 2 | -1.8 -.4 -2.3 -22 8 -37 .80
EMR | 2 | 6.8 1.4 7.9 25 19 -53 .50
ESA | 2 | 5.3 .4 10.2 -48 -37 62 .32
GFZ | 2 | .3 .1 -2.4 -22 -35 -28 .37
GRG | 2 | 5.3 .9 -3.9 -43 -45 4 1.28
JPL | 2 | 7.0 4.2 21.3 -46 106 -69 -.23
MIT | 2 | 5.7 -.7 8.8 -11 3 -28 .35
NGS | 2 | 1.7 .2 19.0 -69 -25 0 .73
SIO | 2 | 7.1 8.3 11.3 20 -62 42 .36
COD | 3 | -2.7 -.2 -1.7 -30 26 -30 .59
EMR | 3 | 11.4 -8.0 2.6 35 15 -33 .38
ESA | 3 | 4.3 -.3 8.5 -16 -33 27 .35
GFZ | 3 | .6 -.2 -1.3 -28 -37 -31 .19
GRG | 3 | 12.5 -.1 -8.0 -34 -47 -1 1.16
JPL | 3 | 7.8 5.4 17.2 -49 40 22 .20
MIT | 3 | 9.2 -1.7 6.7 6 -2 -46 .67
NGS | 3 | 2.4 -2.6 11.7 -64 -26 0 .92
SIO | 3 | 6.4 5.0 -1.3 22 -64 25 .74
COD | 4 | -2.8 -.8 -3.0 -25 49 -54 .65
EMR | 4 | 4.2 -3.3 .2 21 14 -52 .39
ESA | 4 | 7.3 -1.7 9.2 6 -148 59 .44
GFZ | 4 | 1.1 .2 -1.6 -15 -44 -30 -.03
GRG | 4 | 6.3 -11.2 .5 -56 -44 -27 .97
JPL | 4 | .2 1.7 20.2 -65 49 -1 .19
MIT | 4 | 9.5 -1.3 6.0 -8 15 -54 .14
NGS | 4 | 2.7 -8.0 22.1 -164 -30 -7 .54
SIO | 4 | 3.5 5.9 -12.8 -8 -53 -2 .19
COD | 5 | -2.0 .0 -1.9 -19 27 -49 .46
EMR | 5 | 1.4 3.9 .5 5 36 -66 .29
ESA | 5 | 1.0 1.5 4.6 30 -68 58 -.03
GFZ | 5 | .4 .1 -1.8 -13 -37 -25 -.08
GRG | 5 | 4.8 2.2 -2.8 -31 -51 11 .75
JPL | 5 | .4 .8 14.6 -67 86 -16 .39
MIT | 5 | 5.4 -1.1 5.7 -6 17 -40 .11
NGS | 5 | 8.2 -3.8 3.6 -35 -50 47 .55
SIO | 5 | 4.5 6.0 -3.3 19 -48 4 .0
COD | 6 | -1.0 .2 -1.7 -15 36 -66 .68
EMR | 6 | 3.0 -3.1 -2.9 11 33 -53 .29
ESA | 6 | 5.7 2.3 10.5 17 -72 72 .12
GFZ | 6 | .9 -.3 -1.2 -14 -38 -28 -.22
GRG | 6 | 1.7 -4.3 1.0 -17 12 9 .86
JPL | 6 | 4.2 3.1 7.9 -48 -55 24 .29
MIT | 6 | 4.6 -2.8 6.9 -13 19 -44 .19
NGS | 6 | 3.2 -3.9 9.8 -78 -21 8 .31
SIO | 6 | 3.3 3.6 -17.8 -10 -62 0 .34
9. 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.
10. 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 1.1783.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1783.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 2.1783.[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 3.1783.[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 5.1783.0-6). 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 1783 summary. (Mar 09, 2014 - Mar 15, 2014)
Table 1.1783.a GPS week: 1783 MJD: 56725.000-56731.000
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| 0 0 4 10 21 -3 .03 11 11 | -1171 364 23 133
| 1 0 2 25 17 18 .05 | 356 421
emr 80| 0 0 0 -14 3 5 .05 17 17 | 3493 -58 18 129
| 1 1 1 19 11 14 .04 | 1251 1255
esa 150| 0 0 0 -9 -34 18 -.23 7 7 | -1309 476 10 156
| 0 0 1 32 40 19 .01 | 1107 1002
gfz 187| 0 0 -4 26 -1 -10 .18 10 10 | 92 -59 12 115
| 0 0 1 7 8 17 .03 | 414 626
grg 182| 2 0 4 -39 0 -8 .31 15 14 | -38 -158 16 152
| 1 1 2 15 22 11 .03 | 241 452
igr n/a| 0 0 -1 -5 8 7 -.15 5 5 | 8563 -494 17 98
| 0 0 1 13 16 7 .03 | 1232 1180
jpl 80| -1 0 -2 70 -23 -48 .07 16 16 | 2449 4 20 136
| 2 1 1 68 63 35 .02 | 902 1253
mit 300| 0 -1 -2 -14 14 21 -.17 12 11 | -65 -107 136 583
| 1 0 1 23 32 17 .01 | 197 572
ngs 228| 0 0 2 -25 41 -19 .04 12 11 | -1171 372 1825 3290
| 2 0 3 32 35 27 .06 | 362 435
sio 464| 0 0 -3 -3 -17 37 -.76 21 19 | --- --- --- ---
| 0 0 3 21 22 27 .03 | --- ---
Table 1.1783.b GPS week : 1783 MJD: 56725.000-56731.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 5 5 5 5 5 5 5 |
2 | 5 5 5 5 6 6 5 |
3 | 4 4 4 4 4 4 4 |
4 | 5 5 4 4 5 4 4 |
5 | 5 5 5 5 5 5 5 |
7 | 5 4 5 4 5 5 5 |
8 | 4 4 4 4 4 4 4 |
9 | 4 4 4 4 4 4 3 |
10 | 4 4 4 4 5 4 5 |
11 | 4 4 5 4 4 4 4 |
12 | 5 5 5 5 6 5 5 |
13 | 5 5 4 4 5 4 5 |
14 | 5 5 5 5 6 4 5 |
15 | 5 5 5 5 5 5 5 |
16 | 6 5 5 5 6 5 6 |
17 | 5 5 5 5 6 5 5 |
18 | 5 5 5 4 5 5 5 |
19 | 5 5 5 5 4 4 5 |
20 | 5 5 5 5 5 5 5 |
21 | 5 4 4 4 5 5 4 |
22 | 4 5 5 4 5 4 4 |
23 | 5 5 4 5 5 4 4 |
24 | 4 5 4 4 4 4 4 |
25 | 4 4 5 4 5 5 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 4 4 4 4 3 4 |
28 | 5 5 5 4 5 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 0 0 0 0 0 0 0 |
31 | 5 5 5 5 5 5 5 |
32 | 4 4 5 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 2.1783.0 GPS week: 1783 Day: 0 MJD: 56725.000
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 34 -9 .06 11 11 | -894 416 23 123
emr 80| 1 -1 -1 -11 19 -10 .11 17 17 | 3941 -200 18 131
esa 150| 0 0 -1 -2 -28 22 -.24 7 7 | -1878 509 12 212
gfz 186| 0 1 -3 36 16 -21 .16 10 10 | -512 489 12 126
grg 186| 4 0 5 -58 -13 -11 .33 15 14 | -188 93 17 153
igr n/a| 0 0 0 -27 38 5 -.14 5 5 | 9782 -652 16 93
jpl 80| -3 0 -1 119 -84 23 .07 16 16 | 2197 -80 23 147
mit 300| -2 -1 -4 -16 41 40 -.16 13 12 | -62 -17 48 376
ngs 231| 0 -1 6 -57 16 -53 -.02 12 10 | -896 429 1811 3363
sio 471| -1 0 -7 4 -10 -2 -.69 20 16 | --- --- --- ---
Table 2.1783.1 GPS week: 1783 Day: 1 MJD: 56726.000
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| -2 0 5 1 11 -20 .08 10 10 | -1402 587 25 125
emr 80| 1 0 0 0 0 -1 .05 17 17 | 4325 -1299 21 131
esa 150| 0 0 -3 -35 24 15 -.22 6 6 | -1715 -588 9 104
gfz 192| 0 2 -2 19 -3 20 .15 10 10 | 2 -75 13 94
grg 186| 2 -1 5 -21 -4 -9 .34 15 15 | -148 -277 16 157
igr n/a| 0 0 0 -4 3 5 -.10 6 6 | 9937 -1728 18 119
jpl 80| 0 0 -1 85 -99 -65 .09 16 16 | 2975 -1464 20 130
mit 300| 0 -1 -3 16 -40 35 -.17 13 12 | -125 -123 64 336
ngs 231| 2 0 5 -14 32 -7 .02 14 12 | -1397 592 2149 3249
sio 470| 0 0 -1 27 -56 15 -.76 21 19 | --- --- --- ---
Table 2.1783.2 GPS week: 1783 Day: 2 MJD: 56727.000
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 254| 1 1 1 25 55 -1 .07 11 11 | -1192 175 21 114
emr 80| 0 0 4 1 6 29 .11 17 17 | 1498 1661 17 106
esa 150| 0 0 0 -51 -12 43 -.23 7 7 | -857 -19 11 106
gfz 191| -1 0 -5 23 -7 -31 .20 11 10 | -355 1055 12 90
grg 185| 3 1 7 -53 4 -23 .30 16 15 | -344 483 16 155
igr n/a| 0 0 -2 -6 0 -2 -.14 5 5 | 8294 1156 17 87
jpl 80| -3 0 -1 186 -64 -65 .08 15 15 | 1491 1660 24 147
mit 300| 1 -1 -1 -40 32 30 -.16 12 11 | -292 599 76 641
ngs 230| 0 -1 0 -29 -4 -56 -.00 12 10 | -1185 176 1603 2968
sio 471| 0 0 -7 -24 -14 45 -.76 21 20 | --- --- --- ---
Table 2.1783.3 GPS week: 1783 Day: 3 MJD: 56728.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 250| 0 1 6 -26 9 -7 .04 10 10 | -1647 859 22 137
emr 80| 0 -2 2 -1 12 -6 .05 18 18 | 4908 -2040 18 139
esa 150| 0 0 -1 -33 -16 28 -.23 6 6 | -1918 2380 10 131
gfz 188| 0 0 -5 19 -1 -3 .19 10 10 | 679 -407 12 132
grg 182| 2 0 4 -36 -8 -21 .33 14 14 | 9 227 16 146
igr n/a| 0 0 -2 -14 0 18 -.13 5 5 | 9607 -2273 17 101
jpl 80| -4 -2 -2 67 15 -57 .08 16 16 | 3443 -1844 18 128
mit 300| 0 -1 -1 19 -14 21 -.18 11 11 | -240 639 271 696
ngs 227| 0 0 1 36 39 -22 .04 10 9 | -1641 861 2138 3632
sio 462| 0 0 -1 5 -35 60 -.79 21 20 | --- --- --- ---
Table 2.1783.4 GPS week: 1783 Day: 4 MJD: 56729.000
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 4 4 16 27 .02 12 12 | -758 18 22 173
emr 80| 1 0 0 -19 -18 4 .03 18 18 | 2305 292 19 171
esa 150| 1 0 0 34 -97 -12 -.23 9 9 | 195 -21 14 287
gfz 185| 0 2 -4 23 -3 -5 .13 9 9 | 343 -752 15 148
grg 181| 1 -1 7 -43 30 -4 .32 15 14 | 373 -838 16 153
igr n/a| -1 1 -2 1 19 15 -.17 5 5 | 6837 108 18 122
jpl 80| 0 0 -4 -5 81 -28 .05 17 17 | 1192 766 20 145
mit 300| 2 -2 -3 -20 27 8 -.18 12 11 | 313 -900 42 628
ngs 228| -3 -1 5 -19 31 -12 .02 13 12 | -750 7 1906 2929
sio 455| -1 0 -3 -36 9 61 -.74 21 20 | --- --- --- ---
Table 2.1783.5 GPS week: 1783 Day: 5 MJD: 56730.000
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 235| 0 0 5 47 11 13 -.03 12 12 | -1496 791 30 137
emr 80| -1 2 2 -55 3 2 .01 17 17 | 3037 763 17 123
esa 150| 0 0 2 1 -36 -1 -.22 7 6 | -2904 1157 10 121
gfz 188| 0 0 -3 39 -9 -23 .22 10 9 | 229 -484 12 129
grg 181| 2 0 1 -45 -34 9 .30 14 13 | -134 -311 16 159
igr n/a| 0 1 0 -3 10 0 -.16 5 5 | 7390 231 18 88
jpl 80| 0 0 -2 42 -7 -67 .05 17 17 | 2375 652 19 133
mit 300| 1 -2 -1 -28 8 22 -.16 10 10 | -69 -451 412 672
ngs 225| -1 0 -4 -28 103 15 .11 12 11 | -1530 843 1799 3105
sio 463| 0 0 2 4 -17 17 -.76 21 20 | --- --- --- ---
Table 2.1783.6 GPS week: 1783 Day: 6 MJD: 56731.000
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 1 7 29 9 -25 -.04 11 11 | -809 -294 20 125
emr 80| -1 0 0 -14 -1 17 .02 18 18 | 4441 415 18 105
esa 150| 0 1 -1 23 -75 34 -.21 7 7 | -88 -84 10 131
gfz 185| 0 0 -3 23 1 -10 .20 10 10 | 264 -243 12 91
grg 178| 1 1 2 -19 21 -2 .26 14 14 | 164 -488 15 144
igr n/a| 0 1 -1 17 -12 8 -.19 5 5 | 8095 -301 15 82
jpl 80| 2 -1 0 -1 -7 -77 .05 17 17 | 3475 342 17 122
mit 300| 0 -2 -3 -28 48 -11 -.17 11 10 | 14 -501 42 737
ngs 224| -2 0 0 -63 72 0 .14 12 10 | -802 -300 1371 3784
sio 456| 1 -1 -2 -5 2 66 -.79 21 20 | --- --- --- ---
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 3.1783.0 GPS week: 1783 Day: 0 MJD: 56725.000
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 | 9 18 9 13 16 7 15 15 11 15 4 | 32 32 29 32 32 29 32 28 34 33 29
2 | 19 17 8 7 15 3 19 11 11 9 5 | 17 22 19 21 25 18 29 18 24 19 18
3 | 8 12 5 11 13 4 10 8 11 25 3 | 16 21 17 22 22 16 23 16 17 18 17
4 | 11 14 8 8 24 5 17 16 11 27 5 | 27 31 25 30 29 24 34 31 29 41 26
5 | 14 18 7 9 15 4 12 13 13 12 4 | 22 21 17 28 30 18 25 24 23 15 20
7 | 11 17 6 6 16 5 20 15 14 16 4 | 25 24 16 22 27 16 28 22 25 17 19
8 | 11 15 6 7 19 11 19 9 9 24 4 | 28 32 23 26 22 24 35 24 25 31 24
9 | 8 14 6 7 15 5 12 11 9 28 3 | 24 26 20 23 18 19 27 23 23 31 20
10 | 9 11 6 4 16 5 12 11 6 17 3 | 20 23 24 25 29 21 24 25 22 24 22
11 | 9 13 5 8 21 4 13 9 14 17 4 | 21 24 17 23 35 19 25 18 25 22 20
12 | 11 19 8 12 17 6 20 12 9 19 4 | 24 22 18 30 34 19 25 19 24 18 21
13 | 9 16 6 8 14 3 17 21 13 13 4 | 30 39 32 36 36 32 40 35 30 30 32
14 | 10 16 7 15 11 5 16 20 13 31 5 | 29 33 35 45 36 34 38 43 29 41 35
15 | 10 23 11 11 11 7 20 15 15 27 5 | 25 28 30 37 32 30 33 31 21 28 27
16 | 17 18 7 13 14 6 22 14 15 25 5 | 25 24 21 27 28 19 24 20 23 19 21
17 | 12 22 8 14 11 3 19 14 13 30 5 | 22 28 25 31 30 24 28 28 29 30 24
18 | 10 22 7 11 15 8 19 11 8 24 4 | 28 29 31 41 38 29 33 35 28 29 31
19 | 9 17 7 11 10 5 18 10 16 26 4 | 22 24 21 28 27 21 30 20 18 16 21
20 | 12 18 6 10 16 4 19 21 12 23 5 | 30 28 29 33 32 26 30 38 27 34 27
21 | 7 16 7 13 22 5 17 11 8 17 4 | 22 25 20 20 32 20 32 20 24 20 21
22 | 8 15 6 8 15 5 18 10 9 14 4 | 32 32 38 42 42 36 34 40 35 35 36
23 | 9 16 7 11 11 4 14 10 17 20 4 | 30 32 33 38 26 31 34 29 29 31 30
24 | 8 15 5 7 13 7 13 13 12 15 4 | 28 27 20 26 27 21 29 24 26 24 23
25 | 6 23 7 7 13 6 13 10 6 14 4 | 22 30 18 24 30 18 27 18 21 18 20
26 | 11 11 8 8 13 5 12 14 12 15 4 | 27 30 35 37 34 33 37 35 28 32 32
X27 | 9 12 9 7 --- 7 15 10 13 17 4 | 28 33 31 31 --- 29 38 28 30 30 29
28 | 11 26 7 8 16 4 12 10 9 14 4 | 24 34 25 27 38 23 31 27 26 23 25
29 | 9 18 7 13 15 6 19 8 11 18 4 | 40 43 35 40 38 37 44 34 39 38 37
X30 | 3 --- --- --- --- 67 --- --- --- --- 0 | 36 --- --- --- --- 35 --- --- --- --- 37
31 | 11 22 9 8 18 6 18 10 18 17 5 | 22 28 17 24 33 16 28 21 26 20 20
32 | 9 11 5 11 14 3 11 12 10 13 3 | 18 22 21 24 24 19 23 29 20 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 7 10 15 5 16 13 12 20 |T 25 28 24 29 30 24 30 26 26 26 25
WRMS | 11 17 7 10 14 5 16 12 10 16 |NE 25 28 24 29 30 24 30 26 26 26 25
MEDI | 9 16 7 8 15 5 17 11 11 17 |MD 25 28 23 28 30 23 30 25 25 24 24
Table 3.1783.1 GPS week: 1783 Day: 1 MJD: 56726.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 15 16 7 12 15 5 14 9 14 15 4 | 23 25 21 23 28 21 25 21 30 23 21
2 | 8 17 5 9 16 5 22 12 13 11 4 | 19 19 14 19 20 12 20 14 14 16 14
3 | 11 12 6 9 15 4 12 9 12 26 4 | 18 16 14 17 17 14 15 13 16 19 14
4 | 8 18 6 10 17 7 13 16 12 30 4 | 26 27 19 25 24 21 22 26 21 35 21
5 | 10 17 6 9 16 5 15 16 17 12 4 | 22 20 13 22 28 14 20 18 23 11 16
7 | 6 17 7 5 15 6 18 10 14 14 4 | 21 24 12 19 27 16 22 20 23 16 17
8 | 10 15 5 7 21 7 15 10 11 25 4 | 20 26 15 21 20 16 26 18 21 28 18
9 | 8 15 5 7 16 8 11 12 10 29 3 | 18 23 12 17 18 14 20 17 17 28 14
10 | 7 12 6 6 18 5 9 16 16 23 4 | 17 16 14 17 19 13 16 22 16 22 14
11 | 10 14 3 8 19 4 14 9 16 19 4 | 21 25 15 21 33 15 21 16 27 18 18
12 | 7 20 5 12 18 5 20 13 10 19 4 | 23 24 16 27 30 18 20 18 22 15 19
13 | 11 19 7 10 12 6 19 15 16 15 4 | 20 32 21 24 29 22 30 24 22 20 21
14 | 8 15 7 12 15 7 18 16 19 28 5 | 29 28 28 35 31 29 32 30 25 25 28
15 | 10 19 7 9 10 7 16 16 11 28 4 | 23 25 19 25 26 22 29 25 23 22 21
16 | 8 17 6 11 15 3 19 11 11 21 4 | 24 23 18 23 25 17 23 19 24 18 19
17 | 11 22 5 13 12 5 16 16 13 27 5 | 19 28 16 23 26 17 25 22 21 24 19
18 | 11 21 6 12 14 6 19 13 12 22 4 | 23 25 25 32 31 22 23 28 18 22 24
19 | 13 17 8 11 11 5 18 11 14 30 4 | 23 22 16 24 21 14 21 16 17 21 17
20 | 9 19 9 12 15 6 16 21 19 22 5 | 18 22 18 23 25 17 22 30 22 27 17
21 | 7 21 6 9 15 3 15 11 10 18 4 | 15 24 16 18 26 16 21 18 17 19 16
22 | 8 14 6 7 14 6 19 13 17 17 4 | 28 26 29 30 32 25 26 30 24 24 26
23 | 11 14 5 14 11 6 16 12 20 23 4 | 20 26 19 27 23 21 26 23 19 23 20
24 | 9 15 6 7 13 8 19 17 12 14 4 | 24 22 18 21 27 18 27 20 21 17 19
25 | 6 20 7 14 14 7 13 10 13 15 4 | 18 26 15 21 26 18 24 15 22 16 17
26 | 11 11 6 6 11 7 10 15 11 16 3 | 14 23 19 20 24 19 25 21 26 19 19
X27 | 10 12 8 8 --- 5 13 10 13 14 4 | 22 23 23 23 --- 19 29 19 22 21 21
28 | 9 22 5 7 16 6 19 12 9 17 4 | 20 26 16 22 33 15 28 20 21 19 19
29 | 10 21 6 15 16 5 19 8 13 25 5 | 27 32 24 31 29 26 30 23 28 29 26
X30 | 4 --- --- --- --- >>>> --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
31 | 9 17 6 10 17 5 16 12 17 18 4 | 24 24 18 25 33 18 25 20 27 18 21
32 | 8 13 6 11 11 4 11 13 14 13 4 | 15 17 15 19 18 15 17 22 20 18 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 6 10 15 6 16 13 14 21 |T 21 23 17 23 25 18 23 20 21 21 19
WRMS | 10 17 6 10 15 6 16 12 12 19 |NE 21 23 17 23 25 18 23 20 21 21 19
MEDI | 9 17 6 9 15 6 16 12 13 19 |MD 21 24 16 23 26 17 23 20 22 20 19
Table 3.1783.2 GPS week: 1783 Day: 2 MJD: 56727.000
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 | 14 16 9 10 13 9 15 8 14 16 4 | 31 28 24 26 30 26 37 26 30 29 26
2 | 18 21 7 11 15 4 17 10 10 12 5 | 16 23 18 20 19 17 33 14 20 20 16
3 | 13 12 5 10 17 5 9 8 12 32 4 | 22 21 15 22 22 16 25 15 20 23 17
4 | 12 15 7 11 13 7 14 13 7 28 4 | 30 28 24 28 26 27 35 26 29 38 26
5 | 19 18 10 10 18 6 15 13 11 14 5 | 26 22 18 27 31 19 32 20 25 16 21
7 | 10 18 7 6 16 4 19 10 11 16 4 | 25 29 15 23 30 18 34 21 22 15 20
8 | 10 16 6 8 20 5 14 9 13 25 4 | 21 31 17 21 23 17 35 19 19 26 19
9 | 7 14 7 8 16 4 13 10 12 27 4 | 17 26 14 17 18 14 30 15 18 24 15
10 | 8 15 7 11 17 3 9 10 8 25 4 | 21 19 22 26 24 22 31 22 26 30 22
11 | 12 13 4 8 21 5 13 11 16 18 4 | 20 29 15 22 35 16 33 17 19 15 19
12 | 7 21 6 11 19 5 18 13 10 17 4 | 22 23 16 26 31 17 31 20 22 15 19
13 | 9 16 6 11 13 4 14 10 10 20 4 | 27 33 25 32 32 27 43 27 28 29 27
14 | 19 14 4 13 13 6 15 16 16 24 5 | 29 30 28 41 32 30 37 33 26 29 29
15 | 11 21 9 9 12 9 21 12 12 27 5 | 27 28 24 32 27 26 39 26 27 24 25
16 | 12 16 6 13 15 4 18 11 15 24 4 | 23 24 17 29 27 18 30 17 25 11 20
17 | 13 18 8 13 12 5 21 14 12 27 5 | 17 27 17 23 28 16 35 21 20 23 19
18 | 12 23 5 14 15 5 15 11 10 22 4 | 24 26 25 38 32 28 35 30 28 28 27
19 | 12 16 6 11 16 7 18 12 14 28 4 | 22 24 18 24 24 18 32 18 18 13 18
20 | 8 13 8 10 16 4 17 21 14 20 5 | 24 24 22 26 30 21 34 32 26 27 23
21 | 7 23 6 11 14 4 13 9 11 21 4 | 17 24 14 22 23 16 29 16 22 21 16
22 | 8 22 5 10 16 5 14 12 10 14 4 | 28 32 27 34 34 27 36 35 25 28 28
23 | 11 14 7 13 11 4 13 8 12 22 4 | 24 26 23 31 25 25 35 24 24 25 24
24 | 7 13 6 7 15 6 13 14 7 15 3 | 22 29 22 24 28 20 36 23 21 21 22
25 | 5 26 6 8 16 6 14 9 9 16 4 | 21 34 18 24 31 19 32 17 20 18 20
26 | 11 9 9 6 14 6 14 11 9 19 4 | 24 28 29 32 27 26 42 27 26 30 27
X27 | 11 10 5 9 --- 5 13 8 12 14 4 | 28 30 23 28 --- 24 37 24 29 19 26
28 | 10 20 8 11 16 4 16 11 13 13 4 | 17 32 23 26 35 17 32 22 22 15 22
29 | 7 17 7 13 16 9 18 10 10 26 4 | 32 36 28 36 32 31 41 29 33 36 30
X30 | 4 --- --- --- --- --- --- --- --- --- 0 | 9999 --- --- --- --- --- --- --- --- --- 9999
31 | 11 14 7 10 16 4 16 11 14 14 4 | 23 25 16 25 34 15 31 21 25 16 20
32 | 12 15 6 10 15 4 12 12 18 14 4 | 23 22 17 18 22 15 30 23 17 17 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 7 11 16 5 15 12 12 21 |T 23 27 20 26 28 20 34 22 23 22 22
WRMS | 11 17 7 10 15 5 15 11 10 20 |NE 23 27 20 26 28 20 34 22 23 22 22
MEDI | 11 16 6 10 16 5 14 11 12 20 |MD 23 27 18 26 28 19 34 22 24 23 21
Table 3.1783.3 GPS week: 1783 Day: 3 MJD: 56728.000
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 | 12 18 9 13 13 6 16 12 9 13 4 | 28 29 23 24 29 24 29 25 28 25 24
2 | 20 21 9 11 13 5 21 11 5 12 5 | 16 21 19 21 21 15 25 14 19 17 16
3 | 10 9 4 9 15 5 11 7 11 28 3 | 16 16 12 18 18 13 17 12 17 18 13
4 | 11 16 7 9 12 4 14 12 9 25 4 | 24 25 21 24 24 21 28 22 24 32 22
5 | 13 20 8 10 15 5 16 12 10 13 4 | 24 22 15 26 28 16 23 20 22 13 18
7 | 8 18 6 8 14 4 18 11 7 14 4 | 22 25 16 22 27 17 26 20 23 16 18
8 | 10 15 5 6 19 5 14 9 10 26 4 | 22 28 17 21 22 17 28 18 23 28 19
9 | 8 17 6 6 16 6 12 11 9 29 3 | 18 26 14 18 18 15 27 17 21 27 16
10 | 10 16 7 11 19 3 11 9 9 20 4 | 17 20 19 25 27 17 20 19 20 20 19
11 | 10 16 4 7 18 3 14 11 10 20 4 | 19 26 14 19 33 14 23 15 20 20 17
12 | 8 21 5 8 15 2 21 13 9 19 4 | 24 24 16 23 30 17 24 21 20 20 19
13 | 11 19 6 10 12 3 19 9 8 11 4 | 24 36 30 34 35 28 39 28 27 28 29
14 | 9 18 5 13 13 6 14 11 17 27 4 | 29 29 32 42 37 33 33 33 30 32 31
15 | 10 21 7 12 11 3 20 12 13 35 4 | 27 29 27 36 30 26 31 29 26 28 27
16 | 13 19 6 12 14 7 23 11 12 22 4 | 23 23 19 25 26 16 22 17 20 14 19
17 | 11 21 6 12 13 7 18 11 9 23 4 | 26 31 25 28 29 21 28 26 29 22 25
18 | 9 21 6 12 15 5 16 10 8 21 4 | 27 25 22 34 32 22 25 29 23 19 25
19 | 10 17 7 10 15 4 19 13 9 33 4 | 23 24 17 24 24 16 25 21 15 24 18
20 | 11 14 8 11 13 6 18 21 11 20 5 | 21 22 22 27 29 20 27 30 26 25 22
21 | 8 22 6 9 14 5 16 9 11 20 4 | 19 25 15 20 26 15 24 15 19 20 16
22 | 7 17 4 9 16 5 14 10 10 13 3 | 28 29 28 37 37 28 26 30 31 24 29
23 | 11 18 7 14 10 2 15 10 12 24 4 | 25 30 30 36 28 26 33 27 26 31 27
24 | 9 14 5 7 14 5 15 15 12 14 4 | 26 25 17 22 25 18 24 21 20 20 19
25 | 6 24 4 6 12 4 12 9 6 14 3 | 17 28 13 18 24 14 27 15 17 14 16
26 | 11 12 7 8 13 4 11 11 10 22 3 | 21 25 25 28 29 23 27 27 24 27 24
X27 | 13 9 6 8 --- 4 14 10 12 16 4 | 27 27 24 28 --- 22 34 25 21 22 25
28 | 9 18 4 8 15 5 17 12 11 14 4 | 22 27 17 22 30 16 26 20 21 15 19
29 | 9 20 5 13 15 6 20 10 13 25 4 | 32 38 29 36 33 30 40 30 30 36 31
X30 | 4 --- --- --- --- 51 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
31 | 8 19 6 10 16 4 14 11 16 20 4 | 22 25 18 24 31 15 22 20 23 16 20
32 | 8 14 5 9 11 3 13 12 9 18 3 | 18 23 17 20 20 16 21 20 20 19 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 6 10 14 5 16 11 10 21 |T 22 26 20 26 27 19 26 22 22 22 21
WRMS | 10 18 6 10 14 5 16 11 9 20 |NE 22 26 20 26 27 19 26 22 22 22 21
MEDI | 10 18 6 9 14 5 15 11 10 20 |MD 23 25 19 24 28 17 26 21 22 20 19
Table 3.1783.4 GPS week: 1783 Day: 4 MJD: 56729.000
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 | 9 20 9 8 16 7 17 11 14 10 4 | 27 27 22 24 27 20 31 22 25 20 23
2 | 17 20 9 10 14 5 27 16 13 13 6 | 17 20 13 15 19 12 24 11 21 18 12
3 | 13 11 8 7 17 3 10 7 8 25 3 | 16 16 14 19 23 13 14 15 15 19 14
4 | 12 15 11 10 14 4 15 10 13 23 4 | 26 24 18 21 23 17 24 20 24 29 20
5 | 16 16 8 9 13 7 18 11 15 7 5 | 24 23 17 23 27 16 25 20 27 12 20
7 | 8 16 9 7 17 5 17 11 17 15 4 | 24 22 15 23 28 18 24 21 32 17 19
8 | 10 13 7 7 16 5 14 8 12 26 4 | 22 25 17 22 20 18 26 16 31 27 18
9 | 7 16 8 7 11 5 12 8 13 31 3 | 19 23 15 17 17 13 22 14 26 28 15
10 | 12 14 9 9 18 5 12 10 12 21 4 | 15 17 16 18 21 14 17 19 20 22 16
11 | 7 16 7 9 18 5 11 11 13 18 4 | 22 28 18 23 35 16 24 17 23 20 20
12 | 11 20 11 8 19 4 22 17 21 17 6 | 25 24 16 23 29 16 26 21 21 15 18
13 | 13 19 8 12 11 5 21 10 11 18 5 | 21 36 25 31 32 24 33 26 25 25 25
14 | 23 18 11 11 19 8 13 12 17 25 6 | 30 31 30 38 32 30 32 32 27 29 30
15 | 12 20 11 13 13 5 18 10 17 27 5 | 28 28 28 35 27 24 29 29 28 28 26
16 | 14 17 11 12 16 5 23 12 14 25 5 | 21 20 15 26 28 18 22 19 23 21 18
17 | 16 24 13 12 10 6 23 12 18 26 6 | 23 29 30 28 33 21 27 26 38 25 26
18 | 8 23 6 13 16 5 14 11 11 24 4 | 21 22 22 31 30 19 21 25 23 21 23
19 | 13 16 8 6 15 7 16 10 8 30 4 | 22 24 22 26 27 19 21 20 22 20 21
20 | 10 15 12 9 17 4 20 20 7 14 5 | 19 23 23 21 26 16 21 26 19 18 19
21 | 11 13 11 10 17 4 14 10 9 23 4 | 14 18 18 20 25 12 20 16 22 22 15
22 | 11 22 8 10 15 5 15 10 12 17 4 | 19 27 25 31 33 21 24 27 20 23 24
23 | 11 15 11 13 10 5 15 8 10 26 4 | 21 28 25 28 22 21 25 24 24 27 23
24 | 8 14 6 7 13 5 13 13 10 14 4 | 21 23 17 22 25 17 23 18 21 19 19
25 | 7 22 6 8 15 4 16 14 10 15 4 | 16 28 16 20 26 16 27 18 19 17 17
26 | 8 12 7 7 11 4 9 10 16 17 3 | 20 26 25 26 25 21 21 26 20 24 22
X27 | 9 10 6 7 --- 3 13 8 10 14 3 | 26 27 25 26 --- 24 30 25 29 25 26
28 | 9 18 9 9 15 6 14 11 11 16 4 | 22 25 22 26 33 17 25 21 31 17 22
29 | 10 20 8 10 19 4 16 10 20 29 5 | 30 34 30 34 30 28 31 28 40 38 29
X30 | 3 --- --- --- --- 102 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
31 | 9 23 9 7 16 7 19 11 15 17 5 | 20 29 18 26 32 18 24 22 22 20 20
32 | 11 10 9 10 13 3 13 14 9 17 4 | 17 19 18 18 16 13 16 18 18 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 18 9 9 15 5 17 12 13 21 |T 21 24 20 24 26 18 24 21 24 22 20
WRMS | 12 18 9 9 14 5 17 11 12 20 |NE 21 24 20 24 26 18 24 21 24 22 20
MEDI | 11 16 9 9 15 5 15 11 12 18 |MD 21 24 18 23 27 18 24 21 23 21 20
Table 3.1783.5 GPS week: 1783 Day: 5 MJD: 56730.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 9 19 10 13 10 6 15 8 --- 16 4 | 23 26 25 24 27 21 27 22 --- 20 22
2 | 24 20 8 8 14 4 28 12 10 14 5 | 19 21 14 16 19 11 23 12 20 18 12
3 | 11 9 4 8 19 3 10 7 15 23 3 | 16 16 13 18 18 12 15 14 23 15 13
4 | 11 13 7 10 12 5 17 10 12 28 4 | 24 22 16 22 22 19 24 19 24 32 18
5 | 17 18 7 7 14 4 21 10 7 10 4 | 22 20 13 19 28 14 20 17 23 12 16
7 | 9 14 7 8 19 4 16 9 15 14 4 | 22 23 15 21 30 16 21 20 27 15 18
8 | 9 13 5 8 14 4 14 10 13 25 4 | 19 27 15 21 22 17 24 17 24 27 17
9 | 7 12 6 6 12 4 11 7 13 29 3 | 14 22 12 15 19 12 21 14 19 26 13
10 | 9 13 9 13 14 7 12 9 9 25 4 | 15 18 18 16 19 12 16 20 20 25 15
11 | 6 16 4 11 18 4 10 9 14 21 4 | 20 30 20 26 36 19 24 16 31 22 21
12 | 12 20 7 10 17 6 25 13 11 18 5 | 26 21 15 22 28 14 25 21 26 14 18
13 | 9 16 5 9 11 3 17 7 9 15 3 | 18 31 22 26 33 21 33 23 27 17 23
14 | 10 15 5 10 12 6 15 12 11 27 4 | 28 26 21 31 27 25 29 26 27 26 25
15 | 8 21 11 10 11 5 22 10 15 28 5 | 24 27 29 31 27 25 30 26 27 27 25
16 | 19 16 5 12 15 6 22 12 16 22 5 | 21 23 18 24 24 15 20 19 28 17 18
17 | 10 22 8 11 11 4 20 11 10 27 4 | 20 28 23 24 25 18 26 22 23 23 21
18 | 9 26 5 13 15 5 20 9 11 24 4 | 19 25 20 29 28 18 25 23 27 21 21
19 | 10 16 5 11 14 5 16 8 11 31 4 | 20 23 19 28 21 16 22 19 22 24 18
20 | 14 18 8 12 13 6 17 14 11 16 4 | 19 24 20 24 24 16 22 25 24 19 19
21 | 8 22 5 10 16 6 15 10 14 20 4 | 15 23 14 19 27 13 21 15 22 21 15
22 | 8 18 4 9 16 6 17 11 13 16 4 | 21 22 19 29 32 20 25 25 30 20 23
23 | 11 15 7 10 8 4 15 9 12 20 4 | 19 26 21 24 24 18 26 21 25 18 20
24 | 12 14 6 9 10 6 14 12 11 17 4 | 22 24 16 22 26 17 26 17 23 20 18
25 | 9 23 9 8 11 8 16 10 11 15 4 | 18 28 17 17 24 15 27 15 21 16 16
26 | 10 13 7 8 8 4 14 9 10 15 3 | 18 21 23 25 26 21 26 22 24 21 22
X27 | 7 9 5 7 --- 5 12 8 10 12 3 | 23 26 23 24 --- 20 27 22 28 21 22
28 | 8 24 6 9 15 4 14 8 11 11 4 | 18 31 17 22 31 15 22 20 22 13 19
29 | 14 21 7 12 15 8 18 10 10 28 4 | 29 34 25 30 28 27 32 27 33 34 27
X30 | 4 --- --- --- --- 32 --- --- --- --- 0 | 9999 --- --- --- --- 1 --- --- --- --- 9999
31 | 11 16 6 7 18 4 15 12 13 16 4 | 21 24 16 24 36 18 28 21 26 17 20
32 | 10 11 6 9 11 6 13 10 12 14 3 | 12 18 17 17 17 11 16 17 23 13 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 7 10 14 5 17 10 12 21 |T 20 24 18 23 25 16 24 19 24 20 18
WRMS | 12 17 6 9 13 5 17 10 11 20 |NE 20 24 18 23 25 16 24 19 24 20 18
MEDI | 10 16 6 9 14 5 15 10 11 18 |MD 20 24 18 24 26 17 24 20 24 20 18
Table 3.1783.6 GPS week: 1783 Day: 6 MJD: 56731.000
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 | 9 20 12 13 11 8 22 8 15 12 5 | 21 23 22 25 30 21 27 21 30 20 21
2 | 19 20 7 9 14 5 27 11 8 14 5 | 13 20 12 14 20 13 25 11 16 18 12
3 | 12 12 5 9 19 3 13 9 13 23 4 | 16 14 12 19 24 12 15 14 16 15 14
4 | 11 16 9 9 10 5 15 11 10 25 4 | 22 22 13 19 21 16 24 21 22 29 17
5 | 21 15 8 9 17 5 17 9 9 11 5 | 25 21 14 21 30 15 20 19 24 15 18
7 | 11 14 7 7 17 5 18 13 15 17 4 | 25 21 16 20 27 17 22 21 20 21 18
8 | 8 13 6 7 15 5 13 7 11 20 3 | 18 25 12 18 21 14 24 16 18 25 16
9 | 6 11 6 6 12 4 10 7 9 23 3 | 15 21 12 16 18 13 21 14 16 24 14
10 | 8 13 9 11 13 4 13 17 9 22 4 | 18 17 16 19 22 13 19 25 16 21 15
11 | 9 13 6 8 19 3 16 9 12 19 4 | 26 29 25 28 39 24 32 20 28 25 25
12 | 9 19 6 12 20 4 24 13 13 17 5 | 21 22 15 25 30 14 22 22 19 16 17
13 | 8 19 6 10 11 5 23 9 11 19 4 | 26 37 32 39 38 31 38 32 28 33 31
14 | 12 15 5 13 14 5 16 12 14 27 4 | 30 34 33 47 38 34 37 40 33 36 35
15 | 9 21 7 12 10 5 21 9 16 24 4 | 26 30 29 40 34 29 34 33 29 30 29
16 | 17 21 7 11 16 7 20 12 15 20 5 | 30 26 21 27 28 19 25 22 25 21 23
17 | 13 26 8 14 10 6 22 10 11 24 5 | 29 31 30 37 32 26 28 31 30 29 28
18 | 10 22 5 15 16 6 20 10 9 22 4 | 25 24 22 35 29 21 25 27 23 22 24
19 | 11 19 7 8 15 6 16 9 13 36 4 | 25 26 25 29 27 20 25 23 22 34 23
20 | 12 18 9 11 14 4 18 16 9 15 4 | 14 19 19 24 25 17 18 27 21 27 18
21 | 9 18 6 10 14 3 15 11 12 24 4 | 17 21 15 20 26 13 22 17 19 23 16
22 | 10 18 4 10 16 5 16 11 9 11 4 | 23 24 27 37 37 25 27 32 31 21 28
23 | 11 16 8 11 10 4 17 10 12 23 4 | 21 30 29 34 29 27 30 28 28 30 27
24 | 9 15 5 9 12 5 10 14 11 18 4 | 22 26 15 24 23 16 23 18 20 23 18
25 | 8 22 6 8 12 6 15 10 12 18 4 | 16 28 14 18 25 14 26 15 20 17 16
26 | 13 13 6 6 12 4 13 10 11 16 4 | 23 29 29 33 34 27 29 32 28 28 29
X27 | 13 10 6 9 --- 4 12 8 16 12 4 | 31 34 33 34 --- 29 38 32 29 30 32
28 | 7 19 6 9 17 4 14 9 15 13 4 | 21 22 19 27 35 17 21 22 23 18 21
29 | 12 21 8 10 14 7 20 13 15 34 5 | 33 42 32 35 34 34 38 35 37 45 33
X30 | 5 --- --- --- --- 17 --- --- --- --- 0 | 9999 --- --- --- --- 1 --- --- --- --- 9999
31 | 9 20 7 9 16 6 14 10 20 18 4 | 25 32 20 30 35 21 25 26 27 23 24
32 | 11 16 8 10 10 5 16 12 7 16 4 | 14 18 18 18 17 11 12 20 18 17 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 7 10 14 5 17 11 12 21 |T 22 25 21 27 28 19 25 23 23 24 21
WRMS | 11 18 7 10 14 5 17 10 10 20 |NE 22 25 21 27 28 19 25 23 23 24 21
MEDI | 10 18 6 9 14 5 16 10 12 19 |MD 22 24 19 25 29 17 25 22 23 23 21
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 4.1783 GPS week: 1783 MJD: 56725.0-56731.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2909 |U 5 4 11 |U 9 12 25 |U 7 7 17 |
emr | emr 2877 | 7 5 13 |U 9 10 23 | 7 7 22 |
esa | esa 2880 | 5 4 11 |U 8 9 24 | 7 8 18 |
gfz | gfz 2879 |U 5 4 11 |U 7 10 23 |U 7 8 18 |
grg | grg 2782 |U 6 5 15 |U 8 10 26 |U 8 8 21 |
igr | igr 2851 | 5 4 11 | 7 9 23 | 7 8 17 |
igs | igs 2878 | 5 4 11 | 8 9 22 | 7 8 18 |
jpl | jpl 2878 | 5 5 13 | 9 10 25 |U 8 8 23 |
mit | mit 2880 | 13 7 23 |U 9 11 29 |U 8 10 21 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1783.0 GPS week: 1783 Day: 0 MJD: 56725.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2950 | 4 5 12 | 12 14 24 | 8 8 24 |
emr | emr 2878 | 5 5 12 | 9 12 23 | 9 8 27 |
esa | esa 2880 | 4 6 11 | 10 16 27 | 9 8 24 |
gfz | gfz 2880 | 4 5 10 | 8 16 26 | 9 8 24 |
grg | grg 2784 | 4 6 21 | 10 16 26 | 9 9 22 |
igr | igr 2784 | 3 4 11 | 9 14 28 | 8 8 21 |
igs | igs 2880 | 4 5 11 | 10 14 25 | 9 8 26 |
jpl | jpl 2880 | 4 5 12 | 12 14 27 | 9 7 27 |
mit | mit 2880 | 4 6 9 | 11 15 34 | 9 10 23 |
Table 5.1783.1 GPS week: 1783 Day: 1 MJD: 56726.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 6 4 11 | 8 12 24 | 7 11 18 |
emr | emr 2877 | 8 4 12 | 10 11 25 | 8 11 29 |
esa | esa 2880 | 5 4 11 | 9 10 25 | 7 11 20 |
gfz | gfz 2880 | 6 4 11 | 9 10 25 | 7 11 20 |
grg | grg 2784 | 7 5 16 | 10 10 25 | 7 9 22 |
igr | igr 2880 | 5 3 10 | 9 10 25 | 7 11 22 |
igs | igs 2880 | 6 3 10 | 9 10 24 | 7 11 21 |
jpl | jpl 2880 | 5 3 12 | 11 10 27 | 8 11 24 |
mit | mit 2880 | 6 5 10 | 11 12 28 | 10 14 25 |
Table 5.1783.2 GPS week: 1783 Day: 2 MJD: 56727.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 5 4 13 | 8 10 24 | 6 7 18 |
emr | emr 2880 | 7 5 15 | 9 11 21 | 7 6 22 |
esa | esa 2880 | 5 3 11 | 7 8 22 | 5 6 16 |
gfz | gfz 2880 | 6 4 13 | 7 8 23 | 5 7 17 |
grg | grg 2784 | 7 5 16 | 9 10 23 | 7 6 25 |
igr | igr 2784 | 5 5 14 | 7 9 23 | 6 7 17 |
igs | igs 2880 | 6 4 13 | 8 9 21 | 5 6 18 |
jpl | jpl 2880 | 6 4 16 | 9 9 23 | 6 7 21 |
mit | mit 2880 | 61 15 93 | 9 9 28 | 6 8 22 |
Table 5.1783.3 GPS week: 1783 Day: 3 MJD: 56728.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2953 | 3 2 7 | 6 10 20 | 7 8 13 |
emr | emr 2880 | 5 4 11 | 8 7 23 | 7 6 17 |
esa | esa 2880 | 3 3 8 | 6 11 20 | 7 9 12 |
gfz | gfz 2880 | 4 4 9 | 6 12 21 | 7 8 13 |
grg | grg 2784 | 6 6 15 | 6 7 29 | 9 9 20 |
igr | igr 2880 | 4 4 9 | 5 8 20 | 7 8 12 |
igs | igs 2880 | 4 3 9 | 6 9 21 | 7 8 12 |
jpl | jpl 2880 | 4 5 10 | 8 10 25 | 8 8 15 |
mit | mit 2880 | 4 5 10 | 9 15 30 | 10 14 19 |
Table 5.1783.4 GPS week: 1783 Day: 4 MJD: 56729.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 4 3 9 | 12 11 31 | 6 8 16 |
emr | emr 2875 | 6 5 12 | 13 10 24 | 6 7 21 |
esa | esa 2880 | 4 4 10 | 13 12 31 | 6 7 18 |
gfz | gfz 2880 | 4 4 8 | 12 10 29 | 7 8 19 |
grg | grg 2784 | 6 6 7 | 13 10 36 | 8 8 19 |
igr | igr 2880 | 4 4 9 | 12 10 27 | 7 8 18 |
igs | igs 2880 | 4 3 9 | 12 10 29 | 6 7 17 |
jpl | jpl 2880 | 5 5 11 | 13 10 29 | 7 9 24 |
mit | mit 2880 | 4 4 8 | 13 12 32 | 7 9 17 |
Table 5.1783.5 GPS week: 1783 Day: 5 MJD: 56730.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2849 | 6 4 12 | 12 23 34 | 8 5 18 |
emr | emr 2873 | 6 5 15 | 6 10 21 | 7 7 21 |
esa | esa 2880 | 5 4 12 | 5 6 22 | 6 7 18 |
gfz | gfz 2873 | 5 4 11 | 5 6 20 | 7 9 19 |
grg | grg 2776 | 7 4 16 | 7 8 21 | 9 8 23 |
igr | igr 2873 | 5 3 12 | 5 8 19 | 6 7 17 |
igs | igs 2872 | 6 4 13 | 6 7 19 | 6 7 18 |
jpl | jpl 2873 | 5 4 14 | 7 10 22 | 7 7 21 |
mit | mit 2880 | 5 5 14 | 7 8 31 | 7 9 22 |
Table 5.1783.6 GPS week: 1783 Day: 6 MJD: 56731.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 9 5 13 | 5 6 18 | 6 6 14 |
emr | emr 2880 | 9 7 15 | 6 9 21 | 7 5 15 |
esa | esa 2880 | 9 6 13 | 4 4 19 | 7 6 16 |
gfz | gfz 2880 | 9 5 13 | 4 6 18 | 7 7 16 |
grg | grg 2784 | 8 5 17 | 4 7 21 | 9 7 20 |
igr | igr 2880 | 9 6 14 | 4 5 18 | 7 6 16 |
igs | igs 2880 | 9 5 14 | 4 5 17 | 7 6 15 |
jpl | jpl 2879 | 9 6 15 | 5 8 21 | 15 10 27 |
mit | mit 2880 | 9 6 15 | 6 9 20 | 8 9 21 |
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 6.1783 GPS week: 1783 MJD: 56725.500-56731.500
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 | 4 -2 26 161 -8 | 17 20
| 33 27 83 111 11 | 1
emr uuxuu | -5 0 396 36 -17 | 60 62
| 20 19 107 86 12 | 5
esa uuuuu | 18 -16 42 98 -4 | 17 20
| 43 42 33 29 4 | 1
gfz uuuuu | -2 -40 103 -82 4 | 18 22
| 8 16 93 85 4 | 1
grg uuuuu | 17 54 -146 -67 -2 | 21 25
| 19 16 122 86 5 | 1
igr xxxxx | 15 19 92 15 -5 | 6 13
| 13 11 67 54 5 | 2
irf xxxxx | -8 18 -33 -106 -4 | 7 12
| 14 10 28 41 3 | 2
jpl uuuuu | 18 -71 136 32 2 | 22 25
| 75 72 72 68 9 | 1
mit uuuuu | -17 32 -108 -233 -4 | 22 24
| 30 7 41 82 5 | 1
ngs uuuuu | -35 53 -112 -46 3 | 4 9
| 32 32 51 81 5 | 1
sio xxxxx | 16 24 91 -36 -9 | 57 58
| 30 20 45 82 7 | 2
Table 7.1783.0 GPS week: 1783 Day: 0 MJD: 56725.500
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 27 92 179 -4 | 17 21
emr uuxuu | -24 -7 315 -118 -3 | 64 64
esa uuuuu | -20 -7 67 90 -7 | 18 21
gfz uuuuu | 9 -39 4 -36 -1 | 18 23
grg uuuuu | 26 79 -267 -35 5 | 23 25
igr xxxxx | 4 16 90 46 -1 | 8 13
irf xxxxx | -5 16 -41 -116 -1 | 8 13
jpl uuuuu | 85 -151 131 -62 -8 | 24 27
mit uuuuu | -24 25 -87 -270 2 | 22 24
ngs uuuuu | 24 61 -70 46 2 | 6 10
sio xxxxx | 6 31 51 -44 -3 | 59 60
Table 7.1783.1 GPS week: 1783 Day: 1 MJD: 56726.500
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 14 33 109 3 | 17 21
emr uuxuu | -16 -17 509 20 -7 | 63 64
esa uuuuu | -26 -3 15 80 3 | 17 20
gfz uuuuu | 10 -32 220 23 7 | 18 22
grg uuuuu | 29 58 -351 -49 3 | 23 26
igr xxxxx | 32 33 34 25 1 | 8 13
irf xxxxx | 8 23 -50 -103 -5 | 8 13
jpl uuuuu | 90 -90 150 97 12 | 23 25
mit uuuuu | 13 38 -157 -257 -3 | 23 25
ngs uuuuu | -33 30 -80 -211 -4 | 6 9
sio xxxxx | 40 8 104 14 -5 | 59 60
Table 7.1783.2 GPS week: 1783 Day: 2 MJD: 56727.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -49 -11 35 -52 -4 | 18 21
emr uuxuu | -17 -4 412 96 -3 | 63 64
esa uuuuu | -11 13 -8 101 -2 | 17 20
gfz uuuuu | -1 -53 209 -115 7 | 18 23
grg uuuuu | 35 61 -70 53 -3 | 22 25
igr xxxxx | 23 22 112 104 -9 | 7 13
irf xxxxx | -3 22 -13 -52 0 | 7 13
jpl uuuuu | 94 -169 5 131 5 | 22 24
mit uuuuu | 12 40 -132 -155 1 | 22 25
ngs uuuuu | -15 89 -68 -50 0 | 5 10
sio xxxxx | 56 11 95 87 2 | 57 59
Table 7.1783.3 GPS week: 1783 Day: 3 MJD: 56728.500
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 | 21 28 -153 196 0 | 18 21
emr uuxuu | 32 -17 494 126 -27 | 63 64
esa uuuuu | 2 9 22 73 -4 | 18 20
gfz uuuuu | -11 -53 164 -186 7 | 19 23
grg uuuuu | 30 42 -22 -15 -1 | 22 25
igr xxxxx | 18 18 181 14 -1 | 7 14
irf xxxxx | 9 18 6 -87 -1 | 8 13
jpl uuuuu | -15 -69 194 -16 13 | 22 24
mit uuuuu | 15 27 -66 -212 -1 | 23 25
ngs uuuuu | -55 0 -81 -12 -2 | 5 10
sio xxxxx | 36 20 140 -24 -9 | 58 59
Table 7.1783.4 GPS week: 1783 Day: 4 MJD: 56729.500
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 | 29 2 62 294 -8 | 17 20
emr uuxuu | 9 29 324 -19 -22 | 60 62
esa uuuuu | 85 -107 86 72 -9 | 16 19
gfz uuuuu | -5 -10 59 -83 0 | 17 21
grg uuuuu | -7 63 -164 -78 -7 | 20 24
igr xxxxx | -1 34 174 -17 -3 | 5 12
irf xxxxx | -26 36 -62 -124 -7 | 6 12
jpl uuuuu | -105 24 224 -14 -1 | 22 24
mit uuuuu | -44 40 -131 -224 -7 | 22 24
ngs uuuuu | -35 60 -202 -3 6 | 3 9
sio xxxxx | -31 66 105 -138 -12 | 56 58
Table 7.1783.5 GPS week: 1783 Day: 5 MJD: 56730.500
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 | 37 -36 30 243 -17 | 16 20
emr uuxuu | -19 23 487 33 -29 | 56 58
esa uuuuu | 34 4 65 120 -6 | 16 19
gfz uuuuu | -4 -57 1 -184 6 | 17 21
grg uuuuu | 15 50 -57 -213 -5 | 20 24
igr xxxxx | 4 5 25 -69 -10 | 4 12
irf xxxxx | -10 8 -5 -77 -6 | 5 12
jpl uuuuu | -4 -39 92 51 2 | 22 25
mit uuuuu | -36 23 -45 -133 -9 | 21 24
ngs uuuuu | -61 40 -133 -32 6 | 3 9
sio xxxxx | 0 17 131 -7 -14 | 56 57
Table 7.1783.6 GPS week: 1783 Day: 6 MJD: 56731.500
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 -36 83 158 -28 | 14 20
emr uuxuu | 3 -8 233 114 -26 | 51 54
esa uuuuu | 63 -23 46 151 -4 | 14 18
gfz uuuuu | -9 -38 66 7 -1 | 17 21
grg uuuuu | -11 28 -91 -129 -9 | 20 23
igr xxxxx | 24 7 31 1 -10 | 3 12
irf xxxxx | -26 4 -64 -181 -9 | 4 12
jpl uuuuu | -20 0 159 39 -9 | 21 24
mit uuuuu | -53 28 -135 -379 -11 | 20 23
ngs uuuuu | -72 89 -150 -62 10 | 3 8
sio xxxxx | 8 16 11 -141 -20 | 54 55
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