[IGSREPORT-22926] Wk 1802 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Aug 7 14:16:49 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1802 (Jul 20, 2014 - Jul 26, 2014)
Contacts: igs.acc at noaa.gov
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1802[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1802[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1802[0-6].cls IGS GPS clock combination summary report.
igs18027.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18027.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 | KARR YAR2 KARR YAR2
0 | EMR | 8
0 | GFZ | 1 2 6 30 1 6 30 DRAG WUHN DRAG WUHN
0 | GRG | 6 6 8
0 | JPL | 8
0 | MIT | 9 8 9 PTBB PTBB
1 | EMR | 8
1 | ESA | 19 19
1 | GFZ | 1 2 6 30 1 6 30 WSRT WUHN WUHN
1 | GRG | 6 19 6 8 19 KOUC KOUC
1 | JPL | 8
1 | MIT | 19 8 19
2 | COD | BOR1
2 | EMR | 8 WUHN
2 | ESA | UNSA
2 | GFZ | 1 2 6 30 1 6 30 BOR1 REUN WUHN REUN WUHN
2 | GRG | 6 6 8 IRKJ KOUC IRKJ KOUC SOFI
2 | JPL | 8
2 | MIT | 8 BOR1 BOR1
3 | COD | KERG NRMD
3 | EMR | 8 KERG TLSE
3 | ESA | UNSA WUHN
3 | GFZ | 1 2 6 30 1 6 30 BRFT KERG NRMD TLSE WUHN BRFT
3 | GRG | 6 6 8 IRKJ KERG BARH FAA1 IRKJ
3 | JPL | 8
3 | MIT | 6 6 8
4 | EMR | 8
4 | ESA | TLSE UNSA
4 | GFZ | 1 6 30 1 6 30 GRAZ NRMD TSKB WUHN YIBL GRAZ NRMD
4 | GFZ | WUHN
4 | GRG | 1 6 1 6 8 IRKJ NYAL SOFI ADIS SOFI WUHN
4 | JPL | 8 HOB2
4 | MIT | 6 8 TSKB MDVJ
5 | EMR | 8
5 | ESA | UNSA
5 | GFZ | 1 2 6 30 1 6 30 BOR1 NTUS NTUS
5 | GRG | 6 6 8 KOUC NRMD KELY KOUC NRMD
5 | JPL | 8
5 | MIT | 8 TLSE
6 | COD | YAR2 YAR2
6 | EMR | 8 WUHN
6 | ESA | UNSA
6 | GFZ | 1 2 6 30 1 6 30 DAV1 FAIR HOB2 INVK NTUS YELL DAV1
6 | GFZ | FAIR INVK NTUS
6 | GRG | 6 6 8 HYDE HYDE NTUS WUHN
6 | JPL | 8
6 | MIT | 8 MDVJ PDEL
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 orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | GRG | 6
1 | GRG | 6
2 | GRG | 6
3 | GRG | 6
4 | GRG | 1
7. 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 G01 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.1 .2 .2 -47 27 -33 .34
EMR | 0 | 9.2 -.2 -3.8 -8 10 -42 .01
ESA | 0 | -.1 .4 -1.8 23 -6 46 .03
GFZ | 0 | -.6 .0 -1.1 -20 -44 -4 -.28
GRG | 0 | 23.6 -13.6 25.6 -34 22 -8 .48
JPL | 0 | 2.5 -1.8 -.2 -65 53 -2 -1.12
MIT | 0 | 6.5 -3.2 3.6 -5 10 -52 .19
NGS | 0 | 4.8 -4.5 -.3 13 -15 18 .37
SIO | 0 | 6.1 -6.0 -4.3 -8 14 -28 .40
COD | 1 | -.5 .6 .4 -21 17 8 .05
EMR | 1 | -1.8 -1.0 -3.1 -12 -5 -14 -.25
ESA | 1 | -.2 .6 -2.1 4 -20 40 -.18
GFZ | 1 | -.3 .2 -1.0 -18 -35 -2 -.37
GRG | 1 | 12.1 -11.2 23.8 -29 24 -25 .40
JPL | 1 | -1.5 -4.0 -.6 -63 22 -2 -.81
MIT | 1 | 4.5 -5.0 3.3 0 8 -43 .22
NGS | 1 | -1.1 -5.2 -1.6 9 11 -24 .33
SIO | 1 | 4.5 -7.9 -.6 5 4 -29 .13
COD | 2 | -1.3 -.4 -.1 -37 23 -45 .25
EMR | 2 | 2.9 -4.1 3.8 -29 3 -22 -.19
ESA | 2 | -.4 .7 -2.0 -1 -15 28 -.14
GFZ | 2 | -.3 .3 -.6 -11 -38 -4 -.31
GRG | 2 | 15.4 -9.1 26.1 -10 24 -6 .41
JPL | 2 | .1 -6.2 2.9 -82 23 -27 -.57
MIT | 2 | 5.6 -4.7 3.5 10 3 -51 .25
NGS | 2 | -.9 -7.8 5.2 -24 -1 -25 .29
SIO | 2 | 5.1 -5.5 1.7 7 -3 -30 .29
COD | 3 | -1.1 .1 -1.0 -8 28 -53 .23
EMR | 3 | 2.5 -2.4 -1.2 -23 -5 -27 -.03
ESA | 3 | .7 .2 -1.3 5 -1 40 -.10
GFZ | 3 | .3 .5 -.5 -1 -42 -5 -.27
GRG | 3 | 14.8 -11.5 27.7 -22 40 20 .65
JPL | 3 | .1 -6.3 -.4 -56 25 -8 -.59
MIT | 3 | 3.7 -7.5 2.7 6 10 -57 .17
NGS | 3 | -2.9 -13.1 .2 -22 18 -45 .36
SIO | 3 | 2.8 -10.3 6.8 -9 11 -41 .25
COD | 4 | -.5 .2 -.9 -20 10 -41 .23
EMR | 4 | .7 1.5 2.0 -19 -1 -33 -.07
ESA | 4 | -.4 .3 -1.5 -10 -19 29 -.09
GFZ | 4 | .7 -.5 -1.2 -35 -41 -6 -.06
GRG | 4 | 10.8 -10.2 15.4 1 41 -5 .52
JPL | 4 | -5.8 -7.5 -2.3 -94 24 -49 -.16
MIT | 4 | 1.1 -7.7 .9 4 17 -39 .20
NGS | 4 | -5.9 -1.7 -2.5 15 39 -30 .46
SIO | 4 | -1.2 -6.7 -2.7 -16 25 -39 .29
COD | 5 | -.6 -1.2 -.9 -49 34 -68 .17
EMR | 5 | -3.1 -2.5 .2 -16 15 -21 -.19
ESA | 5 | -.2 -.2 -1.8 3 -20 30 -.03
GFZ | 5 | .3 .1 -1.3 -16 -45 -2 -.33
GRG | 5 | 4.5 -18.7 23.7 -8 36 -11 .41
JPL | 5 | .8 -2.4 -5.7 -62 1 29 .16
MIT | 5 | -2.8 -9.9 -.1 5 13 -50 .30
NGS | 5 | -2.3 -10.4 -5.9 -5 31 -44 .59
SIO | 5 | .4 -10.2 1.9 6 14 -37 .10
COD | 6 | .2 -.7 -1.2 -41 16 -49 .31
EMR | 6 | 5.6 .7 .1 -21 9 -21 -.03
ESA | 6 | -.1 -.6 -1.3 -2 -15 34 -.05
GFZ | 6 | .6 -.1 -1.1 -17 -45 -14 -.51
GRG | 6 | 9.5 -7.8 26.1 -10 51 -23 .64
JPL | 6 | -1.3 -6.7 -.1 -131 39 -29 -.71
MIT | 6 | -.3 -7.5 7.4 1 10 -56 .32
NGS | 6 | 1.9 -1.5 7.6 -9 -22 6 .34
SIO | 6 | -.3 -8.0 6.7 2 22 -41 .20
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1802.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1802.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 2.1802.[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 3.1802.[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 5.1802.0-6). 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 1802 summary. (Jul 20, 2014 - Jul 26, 2014)
Table 1.1802.a GPS week: 1802 MJD: 56858.000-56864.000
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 244| 0 0 2 -8 -25 -5 .04 9 9 | -1276 127 16 113
| 0 0 1 10 23 13 .03 | 83 235
emr 80| 0 0 0 13 -11 49 .18 13 13 | 1341 412 16 132
| 1 1 1 9 12 13 .02 | 652 1133
esa 150| 0 0 -6 15 1 2 -.31 11 11 | -846 189 11 179
| 1 0 0 8 12 7 .03 | 963 975
gfz 194| 0 2 -2 9 -11 -2 .09 12 10 | -278 375 13 124
| 1 0 1 14 8 13 .03 | 559 1125
grg 182| 2 0 24 33 -24 -17 .17 26 18 | -258 143 19 157
| 2 1 2 8 45 17 .05 | 183 418
igr n/a| 0 0 0 -3 -16 5 -.15 5 5 | 586 433 15 84
| 0 0 0 9 9 12 .04 | 719 1321
jpl 80| 0 0 -2 -37 34 -36 .02 13 12 | 794 398 16 129
| 1 1 2 17 11 17 .02 | 725 1141
mit 300| 0 -2 3 -15 -15 1 -.17 16 14 | -70 119 22 176
| 0 1 1 33 23 14 .05 | 204 367
ngs 233| 0 0 -4 3 42 1 .03 11 9 | -1291 195 1359 3029
| 0 0 1 12 26 21 .04 | 109 236
sio 475| 0 0 3 -17 -28 -9 -.54 16 16 | --- --- --- ---
| 0 0 2 19 21 24 .09 | --- ---
Table 1.1802.b GPS week : 1802 MJD: 56858.000-56864.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 13 5 6 |
2 | 5 5 5 5 4 4 5 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 4 4 4 4 4 |
5 | 4 4 4 4 4 4 4 |
6 | 8 8 7 7 9 8 8 |
7 | 5 5 4 4 4 5 5 |
8 | 5 5 5 5 4 5 5 |
9 | 12 0 --- --- --- --- --- |
10 | 3 4 3 3 4 3 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 4 4 5 |
13 | 4 4 5 5 4 5 5 |
14 | 5 5 5 5 5 4 5 |
15 | 5 5 6 5 5 5 5 |
16 | 7 7 7 7 8 7 7 |
17 | 6 5 5 5 5 5 5 |
18 | 4 4 4 4 4 4 5 |
19 | 5 5 4 4 4 5 5 |
20 | 4 5 5 4 4 5 5 |
21 | 5 5 5 5 4 4 5 |
22 | 5 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 5 4 5 4 5 5 7 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 5 4 5 5 5 5 |
28 | 5 4 5 5 5 5 5 |
29 | 5 6 6 5 6 6 6 |
30 | 4 4 4 5 5 5 5 |
31 | 5 5 5 5 5 5 5 |
32 | 4 4 3 4 3 3 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 2.1802.0 GPS week: 1802 Day: 0 MJD: 56858.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 245| 0 0 5 -19 -22 -14 .07 10 10 | -1341 355 18 103
emr 80| 0 0 -1 8 -17 67 .17 12 12 | 1509 -60 17 127
esa 150| 1 0 -5 23 9 7 -.26 11 11 | -360 -690 14 198
gfz 194| -1 1 -2 8 -10 -18 .11 11 9 | -333 1089 13 120
grg 182| 4 0 27 35 -59 -3 .22 22 17 | -475 637 19 154
igr n/a| 0 0 0 -1 -11 2 -.15 5 5 | 1261 -268 16 84
jpl 80| -2 0 -4 -40 48 -3 -.02 12 11 | 1326 -355 16 122
mit 300| 1 -1 3 30 14 15 -.22 15 13 | -83 856 19 175
ngs 238| 0 0 -7 -12 12 -32 .00 12 11 | -1400 360 1252 3080
sio 473| 0 0 4 -17 -19 29 -.62 15 14 | --- --- --- ---
Table 2.1802.1 GPS week: 1802 Day: 1 MJD: 56859.000
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 243| 0 0 2 5 -8 0 -.01 10 9 | -1361 153 18 113
emr 80| -1 0 -1 12 -12 61 .19 12 12 | 333 1170 16 135
esa 150| 1 0 -6 6 6 4 -.30 10 11 | -203 -960 10 166
gfz 196| 0 1 -3 -10 -9 7 .13 12 10 | -135 -59 13 126
grg 186| 3 0 25 35 -95 -25 .22 22 16 | -165 -348 19 144
igr n/a| 0 0 0 -15 -9 -3 -.18 5 5 | -210 1017 16 85
jpl 80| 0 0 -4 -35 31 -46 .04 13 12 | -239 1239 15 130
mit 300| 0 -1 3 -24 -16 8 -.20 16 14 | -84 -100 20 179
ngs 234| -1 0 -1 20 44 -20 .02 10 9 | -1414 223 1127 2695
sio 476| 0 0 0 -25 -54 -21 -.61 16 16 | --- --- --- ---
Table 2.1802.2 GPS week: 1802 Day: 2 MJD: 56860.000
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 2 -9 0 -25 .07 9 9 | -1188 -144 16 120
emr 80| 0 -1 0 11 4 44 .18 14 14 | 2210 -331 17 134
esa 150| 1 0 -5 11 9 6 -.29 10 10 | 44 726 10 167
gfz 199| 0 2 -2 21 -28 20 .08 11 9 | 11 507 12 125
grg 189| 3 2 24 32 -47 -11 .17 22 17 | -148 514 20 167
igr n/a| 0 1 0 -4 -2 -5 -.15 5 5 | 1524 -655 14 81
jpl 80| 0 -1 -5 -57 30 -43 .04 13 12 | 1691 -502 16 118
mit 300| 0 0 2 -5 -17 9 -.19 15 13 | 218 -21 23 189
ngs 235| -1 0 -3 12 23 10 -.04 10 9 | -1216 104 1181 2924
sio 479| 0 0 0 -24 -46 -18 -.61 16 16 | --- --- --- ---
Table 2.1802.3 GPS week: 1802 Day: 3 MJD: 56861.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 246| 0 0 2 -17 -4 -13 .03 8 8 | -1337 127 17 110
emr 80| 1 -1 0 16 -18 50 .14 13 13 | 1923 -897 15 134
esa 150| 0 0 -7 23 8 11 -.34 11 11 | -209 -96 12 172
gfz 195| 0 4 -4 23 -6 -2 .06 11 9 | 293 -319 14 122
grg 185| 2 0 24 29 -17 -7 .17 21 17 | 56 -194 20 159
igr n/a| 0 0 1 5 -24 -4 -.19 5 5 | 956 -1080 16 89
jpl 80| -1 0 -3 -43 34 -59 .02 12 12 | 1250 -1036 17 122
mit 300| 0 -3 2 0 -13 -1 -.18 16 14 | 173 -18 23 159
ngs 235| 0 0 -2 -2 20 16 .08 10 10 | -1261 64 1429 3226
sio 480| 1 -1 3 2 -35 -10 -.59 16 16 | --- --- --- ---
Table 2.1802.4 GPS week: 1802 Day: 4 MJD: 56862.000
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 243| 0 0 5 -11 -52 0 .06 9 9 | -1153 -238 17 117
emr 80| 1 -1 0 5 -31 34 .21 15 13 | 895 303 17 127
esa 150| 0 0 -7 25 -14 -9 -.34 11 10 | -1035 -203 12 183
gfz 192| 0 2 -1 17 -8 -6 .06 14 12 | -49 -739 15 129
grg 177| 4 0 19 23 5 1 .19 51 17 | -341 -317 19 194
igr n/a| 0 0 0 0 -13 27 -.17 6 5 | -339 722 17 87
jpl 80| 0 0 -3 -21 15 -29 .01 14 12 | -66 698 15 131
mit 300| 0 -2 3 -55 -11 -25 -.16 16 14 | -166 -288 20 170
ngs 228| 0 0 -5 14 90 14 .05 11 9 | -1155 -217 1482 2897
sio 480| -1 0 5 -37 6 3 -.49 17 16 | --- --- --- ---
Table 2.1802.5 GPS week: 1802 Day: 5 MJD: 56863.000
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 241| 0 0 0 -13 -40 -1 .04 8 8 | -1320 330 15 113
emr 80| 0 -1 2 3 -1 31 .19 13 13 | 1578 153 18 133
esa 150| 0 0 -6 7 9 2 -.34 10 10 | -1518 670 11 184
gfz 195| 0 1 -3 -10 -2 0 .06 11 9 | -276 -370 12 118
grg 179| 1 0 27 26 3 -32 .16 22 18 | -414 429 21 130
igr n/a| 0 1 0 9 -26 18 -.06 5 5 | 695 396 14 76
jpl 80| 1 1 0 -8 30 -45 .02 13 12 | 973 455 18 138
mit 300| 1 -4 5 9 -62 -7 -.10 16 15 | -187 177 26 200
ngs 231| -1 0 -6 -3 50 25 .06 10 9 | -1396 502 1171 2942
sio 470| 0 0 6 14 -38 0 -.42 17 15 | --- --- --- ---
Table 2.1802.6 GPS week: 1802 Day: 6 MJD: 56864.000
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 241| 0 0 1 6 -54 17 .02 9 9 | -1236 307 15 118
emr 80| 3 -2 1 33 -6 60 .17 13 13 | 944 2549 18 140
esa 150| -1 0 -7 12 -17 -7 -.31 11 11 | -2644 1881 14 187
gfz 193| -1 1 -2 18 -18 -19 .10 12 11 | -1458 2522 13 131
grg 180| -1 1 24 50 37 -47 .07 24 21 | -321 281 20 151
igr n/a| -1 0 0 -17 -26 2 -.16 5 5 | 217 2901 17 87
jpl 80| 2 1 0 -56 48 -29 .05 13 12 | 628 2292 17 148
mit 300| 0 -5 6 -61 -4 14 -.11 18 16 | -361 231 23 166
ngs 231| -1 0 -4 -2 54 -6 .06 11 10 | -1199 332 1877 3442
sio 470| -1 0 3 -34 -14 -48 -.41 16 16 | --- --- --- ---
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 3.1802.0 GPS week: 1802 Day: 0 MJD: 56858.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 11 12 6 14 5 14 9 15 10 4 | 314 316 318 316 320 315 316 312 318 310 316
2 | 12 12 9 10 16 7 13 18 15 18 5 | 21 24 20 23 25 17 22 24 26 23 20
3 | 10 12 10 7 14 5 9 11 11 19 4 | 23 29 28 26 26 23 26 21 24 31 24
4 | 8 10 10 8 12 4 10 8 10 11 3 | 25 26 23 23 21 21 24 23 23 20 23
5 | 12 9 8 9 14 5 11 15 12 13 4 | 31 31 30 30 34 29 30 33 34 30 29
6 | 11 22 10 20 75 8 25 23 19 26 7 | 56 58 52 65 32 55 60 64 51 55 56
7E | 9 15 8 9 21 4 13 13 10 10 4 | 25 27 20 23 23 20 22 25 22 19 21
8E | 8 22 11 10 13 6 11 12 11 18 4 | 61 63 63 64 62 63 61 65 62 63 61
X9 | 23 25 13 --- --- 19 --- 31 25 --- 11 | --- --- --- --- --- --- --- --- --- --- 0
10 | 8 6 6 6 14 6 6 10 12 12 3 | 28 24 23 26 32 22 23 26 23 23 24
11 | 7 10 9 8 23 4 11 10 11 12 4 | 44 45 42 46 56 43 45 42 43 42 44
12 | 10 11 10 11 16 4 13 10 14 16 4 | 22 27 23 29 28 20 26 23 22 23 22
13 | 7 12 12 8 20 5 10 7 7 13 4 | 22 28 17 22 39 19 24 20 21 18 21
14 | 11 12 15 13 22 4 11 15 14 18 5 | 30 29 25 34 43 27 25 34 24 28 28
15 | 10 12 14 14 19 6 16 14 14 18 5 | 30 37 30 30 31 25 35 28 32 28 29
16 | 13 12 11 13 16 8 11 43 11 20 7 | 24 24 22 27 25 19 24 43 20 19 18
17E | 11 18 7 15 21 7 15 13 13 12 5 | 37 40 33 43 43 37 39 35 40 34 36
18 | 14 10 11 9 14 6 6 14 12 16 4 | 21 18 21 23 25 19 18 24 24 22 20
19E | 11 11 8 11 28 5 10 15 11 12 5 | 29 32 30 36 38 28 33 30 32 31 29
20 | 9 8 10 15 15 5 9 12 11 17 4 | 30 24 22 37 27 24 22 25 26 29 25
21 | 11 11 12 9 22 6 10 15 14 17 4 | 19 24 22 19 33 16 22 20 17 20 19
22 | 11 10 13 8 13 4 8 13 16 13 4 | 24 25 23 26 34 22 23 30 24 22 24
23 | 9 14 13 11 16 5 13 16 9 16 4 | 24 29 18 25 34 21 26 22 22 21 21
24E | 11 8 13 9 19 4 17 10 13 7 4 | 26 24 28 23 31 22 26 21 25 22 23
25 | 8 8 12 6 14 4 11 9 11 17 3 | 24 26 26 26 28 21 28 20 22 24 24
26 | 8 10 11 8 15 5 9 11 9 12 3 | 22 21 17 20 28 17 19 22 17 21 18
X27 | 12 12 12 8 --- 7 13 12 12 13 4 | 25 19 30 25 --- 22 25 22 26 22 23
28 | 9 11 11 14 14 5 14 11 8 15 4 | 25 31 24 34 28 24 27 29 27 24 26
29E | 9 15 8 16 17 6 17 11 12 11 5 | 47 45 45 55 50 47 48 50 46 46 46
X30E | 7 12 13 7 --- 6 10 13 8 12 4 | 62 64 65 63 --- 63 65 61 62 63 63
31E | 10 10 10 11 27 5 14 11 16 12 5 | 29 28 26 29 32 24 28 23 26 27 25
32 | 11 8 9 7 13 4 7 8 12 14 3 | 25 22 21 27 26 20 21 21 20 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 11 11 22 5 12 15 12 15 |T 39 40 38 41 43 36 39 39 38 38 38
WRMS | 10 12 11 9 17 5 11 13 11 14 |NE 39 40 37 41 43 36 39 40 38 37 37
MEDI | 10 11 11 9 16 5 11 12 12 13 |MD 25 28 25 27 32 22 26 25 25 24 24
Table 3.1802.1 GPS week: 1802 Day: 1 MJD: 56859.000
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 10 13 10 16 4 13 8 8 13 4 | 317 317 318 318 318 315 318 315 316 316 318
2 | 12 11 9 10 20 4 12 17 9 17 4 | 18 21 16 22 22 13 18 16 17 17 15
3 | 8 11 11 10 10 4 11 10 7 21 3 | 21 27 25 18 24 19 25 19 22 27 21
4 | 6 10 9 10 13 4 10 8 9 16 3 | 17 21 17 21 22 16 18 18 18 18 17
5 | 9 12 9 8 14 5 10 17 9 14 4 | 16 24 20 21 20 17 19 19 21 16 18
6 | 13 20 12 26 75 8 26 23 16 28 8 | 53 55 50 64 43 51 52 58 50 51 52
7E | 10 13 9 9 18 3 15 10 10 9 4 | 23 25 19 24 29 20 23 23 27 19 22
8E | 9 21 14 11 13 5 13 12 11 20 5 | 57 61 59 59 58 60 59 58 61 60 58
X9 | 1 --- --- --- --- 92 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
10 | 10 7 7 8 16 3 7 12 9 11 3 | 20 21 18 25 24 18 18 19 22 16 19
11 | 6 10 9 7 23 3 10 8 7 12 3 | 38 40 36 38 54 38 39 39 41 33 39
12 | 9 11 9 14 17 8 14 11 11 17 4 | 17 24 18 24 25 13 22 20 18 17 18
13 | 7 13 12 9 19 5 12 8 9 12 4 | 20 26 18 19 34 17 24 17 19 12 19
14 | 11 8 12 14 20 4 12 13 10 17 4 | 22 25 22 28 30 22 23 23 22 19 22
15 | 8 12 13 14 23 6 15 14 12 20 5 | 25 30 23 26 29 19 28 22 27 18 23
16 | 12 11 12 13 19 8 11 44 11 18 6 | 20 22 19 22 24 15 22 39 20 14 15
17 | 9 19 8 14 23 5 17 11 9 16 5 | 36 41 32 42 42 33 34 35 34 31 35
18 | 11 9 11 11 13 5 8 17 10 18 4 | 15 16 18 15 9 13 13 17 21 16 13
X19E | 10 13 7 10 19 4 --- 11 9 --- 4 | 23 28 22 25 32 22 --- 28 25 --- 24
20 | 8 9 11 20 14 3 12 13 14 19 5 | 24 21 20 39 18 22 23 22 30 25 23
21 | 12 12 10 14 20 7 12 15 12 15 5 | 18 25 18 22 23 16 23 18 21 14 17
22 | 10 7 9 9 12 3 7 14 10 14 3 | 15 22 20 17 20 16 21 18 18 14 16
23 | 8 15 12 10 15 4 12 16 11 16 4 | 23 27 21 22 28 18 24 17 20 14 20
24E | 10 12 12 7 15 4 13 14 8 11 4 | 21 21 26 23 24 18 21 21 22 16 20
25 | 13 12 11 6 16 5 11 12 9 14 4 | 14 25 20 21 23 15 24 16 16 17 17
26 | 5 10 11 8 17 5 8 12 9 15 3 | 20 22 20 20 24 18 20 18 22 19 19
X27 | 12 13 13 8 --- 5 12 9 10 12 4 | 24 19 27 20 --- 18 25 20 20 19 20
28 | 8 13 12 14 14 4 11 9 9 16 4 | 19 29 19 26 27 18 24 21 26 17 21
29 | 13 14 7 14 21 9 19 23 14 13 5 | 43 43 40 47 48 43 46 43 50 41 43
X30E | 8 12 13 7 --- 5 13 11 7 13 4 | 38 35 40 37 --- 36 40 34 39 36 37
31E | 11 9 8 11 22 4 15 11 9 10 4 | 27 27 21 24 25 20 22 23 24 25 22
32 | 8 10 8 6 12 2 9 9 9 17 3 | 20 21 20 21 20 16 20 15 18 18 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 10 12 22 5 13 16 10 16 |T 34 37 34 37 38 32 36 34 35 32 33
WRMS | 9 12 11 10 16 5 12 14 9 16 |NE 34 38 34 37 38 32 36 34 35 32 33
MEDI | 9 12 11 10 17 4 12 12 9 15 |MD 21 25 20 24 25 18 23 21 22 18 20
Table 3.1802.2 GPS week: 1802 Day: 2 MJD: 56860.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 13 11 7 13 4 10 10 12 15 4 | 379 381 383 381 391 378 383 380 380 375 381
2 | 9 12 8 10 18 8 12 16 11 16 4 | 18 19 15 19 18 13 18 15 14 19 13
3 | 6 10 10 8 13 4 10 10 8 20 3 | 19 25 21 16 18 17 23 17 20 22 18
4 | 7 9 9 9 15 3 10 9 9 15 3 | 14 17 15 16 17 11 17 16 13 15 13
5 | 8 12 9 8 16 5 10 16 10 12 4 | 22 23 21 20 23 18 21 24 18 23 19
6 | 13 24 10 18 71 7 23 23 14 30 7 | 48 50 42 50 38 44 49 54 42 50 46
7E | 7 14 8 8 16 4 14 12 10 10 4 | 20 21 14 21 24 15 20 23 21 18 18
8E | 8 29 14 11 12 5 12 11 8 19 5 | 27 42 27 28 29 29 31 25 31 30 28
10 | 9 8 7 9 16 7 8 9 7 9 3 | 17 17 14 17 24 13 15 18 13 18 15
11 | 5 11 10 7 27 5 10 9 9 14 4 | 24 26 21 23 35 23 21 24 24 22 22
12 | 10 15 11 12 19 7 15 14 11 19 4 | 18 23 14 21 24 12 21 18 19 15 15
13 | 11 12 13 11 19 5 16 8 9 13 4 | 21 25 17 23 36 18 25 19 18 15 19
14 | 9 11 12 14 19 3 10 13 10 16 4 | 20 25 22 28 32 21 21 25 22 22 21
15 | 12 14 13 13 23 7 17 14 13 22 5 | 28 33 24 26 27 19 29 23 24 20 23
16 | 10 12 11 15 18 7 13 45 12 16 7 | 21 22 18 23 23 14 22 41 19 16 14
17 | 9 21 9 14 19 6 18 12 10 15 5 | 28 32 21 34 32 23 31 30 25 22 26
18 | 8 9 12 7 13 6 10 13 5 15 3 | 16 15 16 14 18 11 15 19 13 17 13
19E | 8 12 6 11 23 4 13 12 8 11 4 | 43 48 43 42 47 42 46 44 47 45 44
20 | 9 9 11 20 16 6 11 13 13 20 5 | 20 21 16 35 20 17 18 19 17 22 18
21 | 8 15 10 11 22 4 13 14 9 14 4 | 15 24 15 14 24 11 20 15 16 15 14
22 | 8 8 10 8 15 5 9 13 8 15 3 | 15 21 19 17 25 14 20 21 16 15 17
23 | 9 15 13 13 15 4 13 16 9 18 4 | 20 26 18 22 28 16 22 18 15 15 17
24E | 6 13 13 9 22 4 12 12 12 12 4 | 19 23 25 20 25 17 19 18 20 18 19
25 | 11 9 11 7 17 8 12 12 7 11 4 | 15 18 18 19 21 13 22 14 13 13 15
26 | 5 10 10 9 20 5 9 12 7 13 3 | 17 18 14 16 23 14 17 19 12 18 14
X27 | 11 12 12 6 --- 5 13 10 7 11 4 | 25 18 27 19 --- 18 24 18 22 19 20
28 | 9 14 12 14 15 4 12 11 8 17 4 | 21 27 19 28 27 16 26 24 22 19 21
29 | 9 24 6 13 20 6 19 12 12 13 5 | 37 38 30 38 32 35 36 33 35 34 33
X30E | 7 15 13 7 --- 5 11 10 6 13 4 | 48 49 50 49 --- 49 49 47 50 47 48
31E | 6 8 10 8 24 4 15 12 15 12 4 | 21 26 16 22 29 19 20 17 26 18 19
32 | 9 8 7 7 17 4 7 10 7 13 3 | 21 21 18 18 20 16 18 17 16 16 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 10 11 22 5 13 15 10 16 |T 34 37 33 36 38 31 36 35 33 33 32
WRMS | 9 14 10 9 17 5 12 13 9 16 |NE 36 39 35 38 41 32 38 37 34 35 34
MEDI | 9 12 10 9 18 5 12 12 9 15 |MD 21 24 19 22 25 17 21 19 20 19 19
Table 3.1802.3 GPS week: 1802 Day: 3 MJD: 56861.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 15 13 12 13 5 10 13 10 15 4 | 455 456 457 452 463 455 456 455 457 452 455
2 | 9 11 10 10 17 5 15 16 11 19 4 | 15 18 15 21 20 10 19 16 17 19 13
3 | 5 10 10 10 12 5 9 9 10 19 3 | 17 22 20 20 19 15 20 17 23 25 18
4 | 5 8 10 7 16 4 8 13 8 15 3 | 16 19 17 18 20 17 19 17 20 16 16
5 | 8 9 11 6 15 5 9 17 10 12 4 | 25 28 25 24 29 23 24 28 27 24 24
6 | 12 20 10 18 69 7 23 26 17 28 7 | 54 59 53 58 39 56 58 63 55 60 55
7E | 7 11 7 8 17 2 14 12 12 12 4 | 24 26 21 25 28 22 24 28 26 26 23
8E | 7 20 14 11 13 5 13 12 11 20 5 | 54 56 53 53 55 54 57 55 53 55 53
10 | 4 6 7 5 18 5 7 13 9 12 3 | 18 18 16 17 28 16 18 23 19 18 17
11E | 6 10 10 8 17 4 11 16 6 15 3 | 35 37 35 37 44 34 39 41 40 34 37
12 | 12 12 9 12 19 7 13 14 11 15 4 | 23 22 17 23 25 14 22 21 21 18 18
13 | 9 13 14 8 21 5 13 9 10 14 4 | 22 29 20 23 39 21 26 23 21 18 22
14 | 7 10 14 12 19 3 13 12 9 18 4 | 22 25 20 27 37 20 23 25 18 25 21
15 | 8 14 16 10 23 5 16 15 9 22 5 | 26 36 29 31 30 23 31 27 26 24 27
16 | 12 12 11 14 19 7 11 46 14 19 7 | 22 21 17 25 22 13 20 41 23 17 15
17 | 8 19 9 12 20 6 15 14 11 20 5 | 25 31 17 27 31 21 27 26 23 19 22
18 | 9 13 11 8 12 5 7 14 10 17 4 | 15 19 18 14 18 14 15 20 19 18 15
19 | 7 14 7 9 19 8 11 11 10 12 4 | 63 60 60 66 61 58 53 65 65 55 61
20 | 7 7 11 15 16 4 9 13 11 19 4 | 22 22 20 33 25 21 20 21 22 23 21
21 | 10 15 9 10 21 5 12 16 12 15 4 | 15 22 16 17 22 11 21 15 19 15 14
22 | 7 8 12 9 11 3 8 12 7 13 3 | 19 21 20 18 27 18 20 23 20 18 19
23 | 9 14 14 11 16 3 12 16 10 16 4 | 22 27 19 25 34 19 23 21 19 17 20
24E | 7 8 15 11 15 3 15 13 8 12 4 | 20 20 27 22 26 18 21 20 21 19 20
25 | 8 8 11 8 17 7 15 12 8 12 4 | 17 18 19 20 22 13 27 17 18 17 17
26 | 5 10 12 7 20 4 9 12 11 11 4 | 18 18 16 16 25 16 18 20 17 20 16
X27 | 7 11 12 12 --- 5 12 9 13 11 4 | 21 20 26 19 --- 17 23 18 26 18 20
28 | 10 14 13 13 16 5 11 12 10 16 4 | 21 30 19 29 30 19 28 27 23 18 22
29 | 7 21 7 13 20 4 17 11 12 12 5 | 30 32 27 35 31 28 32 29 32 29 29
X30E | 9 13 14 6 --- 3 14 14 9 13 4 | 47 46 49 44 --- 46 51 46 46 47 46
31E | 7 9 8 9 23 4 16 16 11 11 4 | 29 30 24 27 26 24 28 28 28 26 26
32 | 7 8 8 7 19 3 7 8 11 14 3 | 19 22 18 16 25 16 19 19 21 17 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 11 11 21 5 12 16 10 16 |T 39 42 39 41 44 37 41 41 40 38 38
WRMS | 8 13 11 9 17 5 12 14 10 16 |NE 41 44 40 43 47 38 43 43 42 40 40
MEDI | 7 11 11 10 17 5 12 13 10 15 |MD 22 25 20 25 28 19 23 23 23 19 21
Table 3.1802.4 GPS week: 1802 Day: 4 MJD: 56862.000
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 | 18 48 15 26 254 18 46 25 27 30 12 | 894 904 898 899 806 896 905 898 895 899 898
2 | 8 11 10 11 17 6 10 13 11 16 4 | 16 19 16 19 20 12 17 15 13 14 13
3 | 6 13 10 9 11 6 8 11 8 18 3 | 17 25 20 20 20 16 19 15 20 24 17
4 | 8 11 11 12 15 5 8 13 8 15 4 | 16 20 17 15 18 13 17 17 17 15 14
5 | 8 11 11 15 16 4 12 14 8 13 4 | 24 28 23 27 25 21 26 23 24 22 22
6 | 11 20 8 23 64 7 20 29 12 27 8 | 67 71 63 77 53 68 69 81 66 70 66
7E | 8 12 10 10 14 5 11 12 12 10 4 | 29 31 27 27 30 24 29 28 29 26 27
8E | 9 15 13 11 12 4 13 11 9 20 4 | 43 42 42 43 39 40 42 40 43 43 41
10 | 15 9 9 12 16 6 7 10 10 14 4 | 23 20 15 22 23 15 18 20 17 17 16
11E | 7 10 8 10 18 4 10 10 6 13 3 | 26 26 27 30 33 26 27 26 34 25 27
12 | 10 11 10 12 20 5 11 11 8 18 4 | 23 26 19 23 29 18 24 24 23 17 20
13 | 9 12 15 10 20 5 11 6 9 13 4 | 21 28 19 22 35 17 24 20 18 17 19
14 | 8 11 12 14 19 4 13 11 13 18 4 | 26 26 22 27 32 22 24 25 28 24 23
15 | 10 13 13 14 21 7 17 15 11 20 5 | 30 34 27 30 30 21 31 26 26 22 26
16 | 12 14 11 18 19 7 12 45 14 18 7 | 22 24 19 25 24 17 23 43 22 18 16
17 | 8 20 8 15 19 4 15 12 10 16 5 | 28 29 19 30 32 21 28 26 26 20 24
18 | 7 11 13 9 11 5 7 14 10 18 4 | 18 17 18 16 16 14 17 21 20 16 15
19 | 7 14 7 10 19 4 11 12 8 20 4 | 30 34 30 36 36 31 31 34 35 34 31
20 | 7 10 10 16 15 5 8 12 13 21 4 | 22 22 19 33 21 21 21 21 28 26 21
21 | 9 12 9 11 20 4 12 12 10 13 4 | 15 21 13 17 24 12 18 16 19 14 13
22 | 8 7 10 11 12 4 9 12 10 13 3 | 23 22 20 20 25 18 21 24 19 17 19
23 | 9 12 13 12 17 5 13 17 12 16 4 | 24 28 21 23 30 18 25 19 23 18 20
24E | 12 16 14 19 18 4 11 14 10 12 5 | 26 26 27 21 29 21 22 22 20 20 21
25 | 7 8 12 7 15 4 12 10 9 14 3 | 20 21 22 21 26 17 27 20 21 17 20
26 | 8 11 10 11 14 5 9 12 9 12 3 | 20 22 17 21 23 14 19 20 16 19 16
X27 | 8 14 13 16 --- 6 13 11 12 13 5 | 20 21 26 26 --- 18 23 19 23 19 20
28 | 11 17 13 21 18 6 9 13 11 16 5 | 25 32 21 36 30 19 27 26 26 19 24
29 | 8 21 8 20 22 4 20 12 15 13 6 | 21 30 20 32 30 21 31 22 26 19 22
X30E | 11 11 16 11 --- 5 14 12 11 14 5 | 39 37 41 35 --- 35 37 33 36 33 36
31E | 7 9 7 14 23 5 12 14 13 13 4 | 27 28 20 22 26 22 24 29 29 27 23
32 | 6 8 7 11 16 5 7 8 7 11 3 | 20 21 15 14 21 16 19 18 21 14 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 11 14 51 6 14 16 11 17 |T 53 55 51 55 54 49 54 53 53 51 51
WRMS | 9 13 10 12 17 5 12 14 9 16 |NE 63 66 61 65 63 59 64 64 62 60 60
MEDI | 8 12 10 12 18 5 11 12 10 15 |MD 23 26 20 25 29 19 24 23 23 19 21
Table 3.1802.5 GPS week: 1802 Day: 5 MJD: 56863.000
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 13 12 19 6 13 11 9 11 4 | 623 622 624 625 623 625 619 620 626 620 623
2 | 7 13 9 7 18 4 12 14 12 15 4 | 19 21 18 21 19 16 15 19 20 16 16
3 | 8 13 10 7 17 4 8 16 10 20 4 | 17 23 20 16 18 17 19 20 20 27 17
4 | 8 9 8 9 16 4 8 13 8 17 3 | 19 19 16 15 18 16 14 19 17 20 15
5 | 7 11 13 7 17 5 9 15 8 15 4 | 19 25 21 20 24 18 22 23 20 21 19
6 | 11 20 11 19 61 7 21 21 14 31 8 | 48 60 50 55 46 49 62 58 49 59 51
7E | 10 13 8 11 19 5 12 13 11 9 4 | 32 31 29 32 32 30 27 33 34 30 30
8E | 9 22 13 11 18 5 12 11 12 21 5 | 59 63 60 61 62 61 59 61 63 62 60
10 | 8 7 7 6 19 6 8 11 8 13 3 | 17 18 15 17 23 16 16 18 20 17 16
11E | 7 14 6 6 21 4 10 13 14 10 4 | 41 42 41 42 48 42 40 40 53 42 43
12 | 8 13 9 13 20 4 13 11 7 19 4 | 24 26 19 26 26 19 24 24 23 17 21
13 | 8 13 13 11 20 4 14 10 11 15 4 | 18 29 17 21 35 18 25 21 21 19 19
14 | 7 12 12 10 18 5 15 12 9 20 4 | 24 24 25 26 29 23 22 25 24 23 22
15 | 12 13 14 11 24 6 18 16 8 21 5 | 31 33 27 28 29 23 29 25 26 22 26
16 | 8 13 11 16 23 6 14 46 12 21 7 | 20 22 18 25 23 17 23 43 22 21 16
17 | 6 17 9 11 19 3 15 11 9 16 4 | 22 26 16 26 29 19 23 25 23 17 20
18 | 8 9 10 8 12 5 10 15 9 16 3 | 17 17 18 15 15 14 15 22 15 16 14
19 | 7 15 6 10 22 3 12 14 12 17 4 | 24 27 25 28 32 22 24 25 28 24 24
20 | 9 9 11 18 18 3 10 13 9 24 4 | 20 22 20 35 23 22 20 20 25 28 21
21 | 7 14 9 13 20 4 11 13 8 16 4 | 14 22 15 22 22 15 18 19 18 20 16
22 | 6 9 11 8 12 3 13 12 7 11 3 | 20 22 21 19 22 19 20 23 22 16 19
23 | 8 12 14 11 20 4 13 17 11 16 4 | 21 27 20 22 31 19 24 21 21 21 19
24E | 12 15 14 13 18 5 12 22 7 15 5 | 28 29 29 21 26 24 20 27 24 21 23
25 | 9 9 11 6 16 5 12 11 10 15 3 | 25 24 24 25 25 20 23 22 25 22 23
26 | 8 12 11 8 19 5 10 13 8 13 4 | 18 23 17 16 23 16 18 22 19 20 17
X27 | 10 14 15 10 --- 5 11 14 11 13 5 | 21 19 25 19 --- 19 23 19 20 21 19
28 | 12 11 12 13 17 5 13 12 12 16 4 | 22 27 19 25 29 19 24 25 26 16 21
29 | 8 21 7 16 19 6 19 14 12 14 5 | 25 30 25 34 28 27 29 28 29 25 26
X30E | 10 11 14 8 --- 5 13 14 11 12 4 | 34 36 38 34 --- 35 35 33 35 32 34
31E | 9 11 9 11 25 6 14 16 15 13 5 | 21 23 13 21 20 18 21 21 24 21 18
32 | 7 8 7 6 19 2 9 11 7 12 3 | 17 22 16 19 23 17 20 20 21 18 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 11 22 5 13 16 10 17 |T 43 46 43 45 48 42 44 45 45 43 42
WRMS | 8 13 10 9 18 5 12 15 9 15 |NE 48 52 48 50 53 47 49 51 50 49 47
MEDI | 8 13 11 11 19 5 12 13 10 15 |MD 21 25 20 25 26 19 23 23 23 21 20
Table 3.1802.6 GPS week: 1802 Day: 6 MJD: 56864.000
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 16 14 18 19 6 14 15 14 9 5 | 541 543 542 531 534 538 543 537 542 535 539
2 | 9 11 10 12 22 4 13 15 11 15 4 | 31 30 27 29 27 25 26 27 24 22 25
3 | 8 11 10 10 18 6 11 15 9 21 4 | 24 28 25 24 22 23 24 23 27 34 23
4 | 8 11 9 10 20 6 8 13 12 14 4 | 26 29 26 22 26 24 25 25 25 27 23
5 | 7 12 12 8 21 4 11 17 6 12 4 | 39 42 38 38 43 37 40 41 38 36 38
6 | 13 19 12 22 61 7 19 20 15 32 8 | 72 79 72 81 52 74 80 86 74 87 74
7E | 8 12 7 11 23 3 12 19 10 8 4 | 30 31 24 29 25 27 26 30 32 28 27
8E | 9 13 15 10 18 5 14 13 12 17 4 | 66 68 66 64 67 65 70 65 66 67 66
10 | 8 7 9 6 23 4 7 11 9 13 3 | 28 30 26 28 37 26 28 29 29 27 27
11E | 9 12 8 9 19 3 10 12 11 9 4 | 48 53 48 48 44 46 50 49 50 44 47
12 | 8 11 11 12 24 6 13 12 10 17 4 | 36 34 29 36 36 29 32 31 32 26 31
13 | 8 13 14 12 21 4 12 15 10 14 4 | 31 36 27 30 46 28 34 31 29 29 30
14 | 7 13 13 14 24 5 15 15 10 19 5 | 32 34 30 37 46 32 31 38 30 31 31
15 | 8 12 14 13 23 4 16 17 10 20 5 | 35 40 35 39 36 32 41 34 35 32 34
16 | 12 12 11 14 22 7 11 48 12 17 7 | 31 28 26 33 28 26 28 46 30 24 25
17 | 9 15 7 13 22 4 13 13 12 14 4 | 33 36 28 35 41 29 33 33 34 27 31
18 | 8 12 11 13 16 4 9 18 9 17 4 | 30 29 30 31 34 30 27 36 30 29 28
19 | 7 13 7 12 24 5 13 15 11 14 4 | 38 38 35 45 43 37 34 41 42 33 38
20 | 9 9 12 16 19 5 9 12 14 22 4 | 33 33 29 44 33 32 31 31 39 39 32
21 | 6 15 9 11 23 3 12 14 12 13 4 | 25 28 26 30 31 24 26 26 28 24 25
22 | 7 9 12 10 15 4 12 13 8 13 4 | 32 34 31 34 37 32 32 37 33 28 32
23 | 8 12 13 11 20 5 12 21 11 18 4 | 30 33 27 30 38 26 30 29 27 27 27
24E | 11 14 17 12 25 5 14 39 15 12 7 | 43 37 44 34 44 34 37 50 32 37 36
25 | 8 10 12 8 21 3 13 11 9 14 4 | 33 28 31 31 34 28 32 29 32 28 30
26 | 5 11 12 9 21 3 9 15 9 10 4 | 30 30 25 27 32 26 27 30 24 29 25
X27 | 9 15 12 9 --- 3 15 16 11 13 5 | 30 28 31 30 --- 26 31 27 31 29 28
28 | 12 12 14 16 20 3 9 15 11 17 5 | 31 36 26 38 35 27 32 32 31 25 29
29 | 10 19 8 16 23 6 23 13 16 14 6 | 41 38 36 48 40 40 41 36 40 35 38
X30E | 12 12 16 10 --- 5 15 16 10 14 5 | 60 59 60 54 --- 57 58 53 59 57 57
31E | 10 14 9 9 24 5 13 17 12 12 4 | 27 29 21 27 30 23 23 27 27 28 24
32 | 8 10 9 7 24 4 11 13 8 13 4 | 33 32 28 29 32 27 30 31 33 27 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 12 24 5 13 18 11 16 |T 52 53 49 52 54 49 51 52 51 50 49
WRMS | 9 13 11 11 21 5 12 16 10 16 |NE 56 57 53 56 59 53 55 57 55 54 53
MEDI | 8 12 12 11 22 4 12 15 11 14 |MD 32 34 29 34 36 29 32 32 32 29 30
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 4.1802 GPS week: 1802 MJD: 56858.0-56864.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2991 |U 7 9 22 |U 6 7 22 |U 9 10 19 |
emr | emr 2983 | 9 10 26 |U 6 7 22 | 10 11 21 |
esa | esa 2989 | 8 10 23 |U 6 7 22 | 10 11 20 |
gfz | gfz 2971 |U 7 9 23 |U 7 7 23 |U 8 10 19 |
grg | grg 2783 |U 9 11 29 |U 9 10 31 |U 11 12 26 |
igr | igr 2984 | 8 9 24 | 7 7 22 | 9 10 19 |
igs | igs 2963 | 7 9 23 | 6 6 21 | 9 9 19 |
jpl | jpl 2958 | 10 10 26 |U 6 7 23 | 10 10 21 |
mit | mit 2989 | 8 9 23 |U 8 9 29 |U 10 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 5.1802.0 GPS week: 1802 Day: 0 MJD: 56858.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3046 | 9 10 23 | 5 5 18 | 11 10 18 |
emr | emr 3058 | 11 10 28 | 5 4 20 | 11 10 20 |
esa | esa 3072 | 11 11 26 | 5 5 20 | 10 11 18 |
gfz | gfz 2973 | 9 9 25 | 6 5 22 | 9 10 17 |
grg | grg 2784 | 8 11 32 | 8 8 35 | 12 12 25 |
igr | igr 3044 | 9 9 25 | 5 4 20 | 9 11 18 |
igs | igs 3023 | 9 10 25 | 5 4 20 | 9 9 17 |
jpl | jpl 2971 | 13 12 32 | 6 4 24 | 10 11 19 |
mit | mit 3072 | 9 10 24 | 6 6 22 | 10 8 16 |
Table 5.1802.1 GPS week: 1802 Day: 1 MJD: 56859.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3016 | 6 9 19 | 4 8 21 | 8 7 16 |
emr | emr 2965 | 7 10 23 | 6 5 20 | 9 8 21 |
esa | esa 2976 | 7 8 22 | 6 7 22 | 10 8 17 |
gfz | gfz 2965 | 5 7 19 | 6 6 21 | 8 8 18 |
grg | grg 2777 | 7 11 25 | 7 6 26 | 12 10 27 |
igr | igr 2969 | 7 8 21 | 6 6 21 | 8 7 16 |
igs | igs 2937 | 6 8 21 | 5 5 20 | 8 7 17 |
jpl | jpl 2876 | 8 10 23 | 5 6 22 | 10 8 18 |
mit | mit 2976 | 6 5 18 | 5 8 25 | 9 7 20 |
Table 5.1802.2 GPS week: 1802 Day: 2 MJD: 56860.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 15 32 | 8 9 26 | 8 12 20 |
emr | emr 2972 | 11 14 34 | 6 8 23 | 10 11 18 |
esa | esa 2976 | 9 17 34 | 6 8 20 | 10 14 21 |
gfz | gfz 2973 | 8 16 32 | 8 8 28 | 9 13 20 |
grg | grg 2784 | 12 18 40 | 11 13 37 | 12 13 26 |
igr | igr 2976 | 9 15 33 | 7 7 25 | 9 14 21 |
igs | igs 2944 | 9 15 33 | 7 8 23 | 9 12 19 |
jpl | jpl 2972 | 11 15 36 | 7 8 22 | 10 12 20 |
mit | mit 2976 | 9 17 32 | 8 7 29 | 9 12 21 |
Table 5.1802.3 GPS week: 1802 Day: 3 MJD: 56861.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2972 | 9 6 17 | 8 7 24 | 10 13 25 |
emr | emr 2972 | 12 8 22 | 6 7 22 | 11 11 23 |
esa | esa 2976 | 10 8 19 | 7 7 21 | 11 13 26 |
gfz | gfz 2972 | 9 7 18 | 7 7 24 | 10 11 25 |
grg | grg 2784 | 10 7 18 | 9 9 27 | 13 14 33 |
igr | igr 2976 | 9 7 20 | 7 7 23 | 10 12 22 |
igs | igs 2958 | 9 7 17 | 7 6 22 | 10 11 23 |
jpl | jpl 2971 | 11 7 22 | 7 7 22 | 11 12 26 |
mit | mit 2976 | 11 7 23 | 11 9 38 | 10 13 27 |
Table 5.1802.4 GPS week: 1802 Day: 4 MJD: 56862.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 8 19 | 9 11 23 | 7 11 16 |
emr | emr 2972 | 10 11 26 | 8 12 23 | 11 12 22 |
esa | esa 2976 | 8 9 19 | 8 10 27 | 9 13 20 |
gfz | gfz 2972 | 7 8 20 | 9 10 23 | 7 10 17 |
grg | grg 2784 | 8 11 30 | 11 15 28 | 8 12 26 |
igr | igr 2976 | 8 8 21 | 8 10 22 | 8 9 19 |
igs | igs 2959 | 7 8 20 | 8 10 22 | 8 10 17 |
jpl | jpl 2972 | 9 8 21 | 8 9 26 | 10 11 20 |
mit | mit 2976 | 8 9 19 | 11 15 33 | 9 11 21 |
Table 5.1802.5 GPS week: 1802 Day: 5 MJD: 56863.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 6 25 | 6 5 21 | 8 7 15 |
emr | emr 2972 | 7 9 28 | 8 5 24 | 10 8 16 |
esa | esa 2976 | 7 9 24 | 6 7 21 | 10 9 18 |
gfz | gfz 2972 | 6 7 25 | 7 6 22 | 8 7 16 |
grg | grg 2784 | 9 11 28 | 11 7 29 | 9 8 21 |
igr | igr 2976 | 5 8 25 | 6 5 21 | 9 7 17 |
igs | igs 2959 | 6 7 25 | 6 5 20 | 9 7 16 |
jpl | jpl 2972 | 7 8 27 | 6 6 22 | 10 7 18 |
mit | mit 2976 | 7 8 24 | 6 10 28 | 10 8 21 |
Table 5.1802.6 GPS week: 1802 Day: 6 MJD: 56864.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 18 | 6 7 23 | 10 12 21 |
emr | emr 2972 | 8 9 22 | 5 6 24 | 11 14 26 |
esa | esa 2976 | 7 10 20 | 5 6 24 | 12 13 21 |
gfz | gfz 2972 | 7 8 20 | 6 7 23 | 9 12 19 |
grg | grg 2784 | 8 10 30 | 10 13 32 | 14 12 26 |
igr | igr 2976 | 7 9 21 | 6 7 22 | 11 13 21 |
igs | igs 2962 | 6 8 21 | 5 7 23 | 10 11 20 |
jpl | jpl 2972 | 8 8 22 | 5 6 25 | 11 12 24 |
mit | mit 2976 | 8 9 21 | 8 9 26 | 11 11 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 6.1802 GPS week: 1802 MJD: 56858.500-56864.500
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 | 35 5 -13 169 -3 | 20 25
| 26 10 30 127 6 | 5
emr uuuuu | 19 -1 15 -59 -7 | 36 40
| 14 13 91 42 5 | 6
esa uuuuu | 3 -26 31 104 -5 | 23 28
| 11 14 26 45 2 | 5
gfz uuuuu | 20 9 -44 68 -1 | 14 21
| 12 20 101 98 7 | 7
grg uuuxu | 49 -43 20 345 7 | 24 27
| 28 12 31 144 5 | 3
igr xxxxx | 15 -2 -32 19 -7 | 2 18
| 4 14 42 42 5 | 8
irf xxxxx | 3 -8 -57 -71 -3 | 3 17
| 11 12 42 17 4 | 6
jpl uuuuu | -46 48 -27 -69 8 | 40 45
| 17 27 48 81 7 | 3
mit uuuuu | -16 1 -95 -227 -3 | 23 28
| 28 17 85 38 5 | 5
ngs uuuuu | -53 -11 94 -115 2 | 12 16
| 51 15 90 135 7 | 4
sio xxxxx | 9 24 8 7 7 | 57 59
| 23 15 45 47 3 | 2
Table 7.1802.0 GPS week: 1802 Day: 0 MJD: 56858.500
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 | 48 11 -8 397 0 | 30 33
emr uuuuu | 15 -12 139 -124 -13 | 48 50
esa uuuuu | -13 -48 29 94 -5 | 32 35
gfz uuuuu | 33 22 -215 216 -6 | 25 29
grg uuuxu | 72 -35 7 447 0 | 29 31
igr xxxxx | 20 -7 10 12 -10 | 15 20
irf xxxxx | 2 3 -91 -53 -8 | 13 17
jpl uuuuu | -72 50 40 -187 -8 | 46 49
mit uuuuu | -37 15 -132 -204 -9 | 32 34
ngs uuuuu | -40 -18 166 -377 12 | 19 21
sio xxxxx | -8 19 38 -53 8 | 61 62
Table 7.1802.1 GPS week: 1802 Day: 1 MJD: 56859.500
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 -6 8 248 -14 | 24 29
emr uuuuu | 16 -5 70 -68 -10 | 40 44
esa uuuuu | -6 -14 -12 83 -5 | 27 32
gfz uuuuu | 31 32 -81 15 1 | 19 26
grg uuuxu | 84 -32 78 590 13 | 23 27
igr xxxxx | 12 10 -67 66 -11 | 8 20
irf xxxxx | -12 -6 -44 -76 -3 | 7 18
jpl uuuuu | -57 60 13 29 7 | 40 45
mit uuuuu | -54 1 -36 -252 -1 | 26 31
ngs uuuuu | -19 -37 -9 -158 2 | 15 19
sio xxxxx | -10 44 21 29 10 | 57 59
Table 7.1802.2 GPS week: 1802 Day: 2 MJD: 56860.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 13 4 -54 116 3 | 21 27
emr uuuuu | -5 9 88 -39 -5 | 37 42
esa uuuuu | 2 -25 61 81 -4 | 24 30
gfz uuuuu | 12 -20 61 -63 1 | 16 24
grg uuuxu | 71 -39 18 338 9 | 23 27
igr xxxxx | 18 0 -76 -25 -3 | 4 19
irf xxxxx | -9 -17 -31 -64 -5 | 5 18
jpl uuuuu | -22 61 -27 26 11 | 39 44
mit uuuuu | -40 -13 -71 -201 -6 | 25 30
ngs uuuuu | -9 8 -53 -16 -3 | 13 18
sio xxxxx | 0 10 -17 -9 8 | 57 59
Table 7.1802.3 GPS week: 1802 Day: 3 MJD: 56861.500
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 18 -14 124 -1 | 18 23
emr uuuuu | 20 -2 -70 -50 -14 | 34 38
esa uuuuu | 3 -35 58 99 -6 | 21 27
gfz uuuuu | 0 -11 -60 -13 -6 | 13 19
grg uuuxu | 49 -38 -24 375 8 | 22 26
igr xxxxx | 14 -11 -49 0 -12 | 0 15
irf xxxxx | 1 -10 -45 -70 -5 | 1 15
jpl uuuuu | -48 37 -47 -93 6 | 38 43
mit uuuuu | -12 9 -74 -205 -7 | 21 27
ngs uuuuu | 5 2 188 -13 6 | 10 14
sio xxxxx | -2 9 -2 -3 1 | 55 57
Table 7.1802.4 GPS week: 1802 Day: 4 MJD: 56862.500
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 | 55 15 8 196 0 | 16 22
emr uuuuu | 43 23 -82 -100 2 | 31 37
esa uuuuu | 14 -35 16 47 -9 | 19 26
gfz uuuuu | 22 13 -57 137 -9 | 9 17
grg uuuxu | 24 -61 30 155 10 | 22 26
igr xxxxx | 17 -21 -60 -33 -10 | -4 17
irf xxxxx | 19 -29 0 -105 -3 | -1 16
jpl uuuuu | -38 47 -76 -124 11 | 37 42
mit uuuuu | 18 -29 9 -302 -5 | 19 26
ngs uuuuu | -118 -10 123 -3 5 | 9 13
sio xxxxx | 25 12 4 -40 4 | 55 57
Table 7.1802.5 GPS week: 1802 Day: 5 MJD: 56863.500
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 | 35 3 -52 3 -7 | 15 21
emr uuuuu | 25 -2 36 -26 -7 | 30 36
esa uuuuu | 1 -5 19 186 -7 | 17 25
gfz uuuuu | 14 28 -47 56 4 | 6 14
grg uuuxu | 28 -34 11 273 9 | 22 25
igr xxxxx | 18 -6 -20 35 -2 | -7 17
irf xxxxx | 10 5 -59 -77 3 | -3 15
jpl uuuuu | -29 -4 -1 -27 12 | 38 43
mit uuuuu | 13 18 -106 -224 3 | 17 24
ngs uuuuu | -72 -20 124 -66 -2 | 8 12
sio xxxxx | 55 34 79 64 9 | 55 57
Table 7.1802.6 GPS week: 1802 Day: 6 MJD: 56864.500
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 | 74 -8 22 96 -3 | 16 21
emr uuuuu | 18 -17 -77 -5 -4 | 31 37
esa uuuuu | 21 -22 44 134 -2 | 18 26
gfz uuuuu | 27 -4 93 130 10 | 8 16
grg uuuxu | 14 -59 21 236 3 | 25 29
igr xxxxx | 8 23 37 76 0 | -6 17
irf xxxxx | 11 -5 -127 -56 1 | -1 16
jpl uuuuu | -54 82 -91 -109 15 | 43 48
mit uuuuu | 1 9 -258 -200 2 | 19 26
ngs uuuuu | -117 -2 119 -175 -7 | 10 14
sio xxxxx | 2 38 -65 62 8 | 58 60
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