[IGSREPORT-23052] Wk 1810 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Oct 3 12:23:15 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1810 (Sep 14, 2014 - Sep 20, 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:
igs1810[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1810[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1810[0-6].cls IGS GPS clock combination summary report.
igs18107.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18107.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 | 3 HOB2 HOB2
0 | ESA | ALRT ALRT
0 | GFZ | 1 6 30 1 6 30
0 | GRG | 6 6 KOUC USNO KOUC MONP USNO
0 | MIT | 1 3 12 18 26 1 3 9 10 12 14 18 26 MDVJ MONP
1 | COD | ALRT
1 | EMR | 21 TSKB TSKB
1 | ESA | 21 ALRT
1 | GFZ | 1 6 30 1 6 30 MCM4
1 | GRG | 6 6 ZIMM MAL2 ONSA ZIMM
1 | JPL | KARR
1 | MIT | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
1 | MIT | 21 22 23 24 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7
1 | MIT | 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24
1 | MIT | 25 26 27 28 29 30 31 32
2 | COD | BRAZ BRAZ
2 | EMR | YELL
2 | ESA | HOB2 UNSA
2 | GFZ | 1 6 21 30 1 6 21 30 BRAZ YELL HYDE
2 | GRG | 6 21 25 6 21 25 BOR1 HOB2 IRKJ MAL2 NKLG BOR1 IRKJ
2 | GRG | MAL2 RBAY
2 | JPL | 21 IRKJ
2 | MIT | 3 19 21 27 3 19 21 24 27 HOB2 TLSE MDVJ TLSE
3 | COD | FAA1 HOB2
3 | EMR | 3
3 | ESA | BRAZ PIMO BRAZ PIMO
3 | GFZ | 1 2 6 9 30 1 3 6 30 BRAZ DRAG HOB2 XMIS BRAZ DGAR
3 | GFZ | DRAG HOB2
3 | GRG | 6 6 GRAZ HYDE TLSE GRAZ HYDE TLSE
3 | MIT | 3 4 9 11 1 3 4 5 9 11 19 TLSE MDVJ TLSE
4 | COD | 3
4 | EMR | TLSE
4 | ESA | PIMO UNSA
4 | GFZ | 1 2 6 9 30 1 6 9 30 FAA1 NOVM TLSE NOVM
4 | GRG | 6 9 6 9 FAA1 HOB2 HYDE IRKJ KELY MAL2 SOFI TLSE FAA1
4 | GRG | HOB2 HYDE IRKJ KELY SOFI TLSE
4 | JPL | IRKJ
4 | MIT | 1 3 4 16 19 22 26 27 1 3 4 7 16 19 22 26 27 HOB2
4 | MIT | HOB2 MDVJ MONP
5 | COD | FLIN
5 | ESA | DUBO IRKJ DUBO IRKJ
5 | GFZ | 1 2 6 9 30 1 6 30 FLIN YELL FLIN SCH2
5 | GRG | 6 9 6 9 ALRT GRAZ IRKJ MAL2 ALRT GRAZ IRKJ MAL2
5 | JPL | IRKJ
5 | MIT | 31 FLIN MONP PDEL
6 | COD | FAA1 FAA1 TSKB
6 | ESA | UNSA
6 | GFZ | 1 2 6 9 30 1 6 9 30 WSRT XMIS XMIS
6 | GRG | 6 9 6 9 GRAZ HYDE MAL2 BOGT DRAG FAA1 GRAZ HYDE MAL2
6 | MIT | 1 3 5 6 11 12 18 22 1 3 5 6 11 12 15 18 22 HYDE HYDE
6 | MIT | KOUR
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G13 | 2014_09_19 | 2014072
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
2 | GRG | 25
2 | JPL | 25
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G25 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.4 -1.2 -.8 -76 36 -37 .13
EMR | 0 | 3.5 2.6 1.7 -14 13 -30 .15
ESA | 0 | .0 .4 -1.7 1 -4 33 .01
GFZ | 0 | .4 -1.3 -1.0 -52 -41 -16 .39
GRG | 0 | 10.2 -4.5 -7.7 -27 31 -33 .67
JPL | 0 | .4 8.0 4.0 -12 -38 -17 .57
MIT | 0 | 3.3 .8 -1.6 -2 8 -41 .35
NGS | 0 | -1.4 -2.6 9.0 -21 -8 -14 .50
SIO | 0 | 6.6 4.0 -5.1 -26 17 -13 .18
COD | 1 | -.7 -.6 -1.0 -47 38 -23 .27
EMR | 1 | 9.0 -.5 2.0 -14 7 -36 .28
ESA | 1 | .1 1.2 -1.7 2 0 38 .02
GFZ | 1 | .1 -.3 -1.9 -51 -61 -29 .40
GRG | 1 | 17.2 -2.9 -24.3 -24 29 -6 1.03
JPL | 1 | 9.8 6.0 9.5 -43 19 -15 .18
MIT | 1 | 4.2 2.1 2.3 3 9 -33 .45
NGS | 1 | 10.3 -1.5 14.5 -34 -68 67 .62
SIO | 1 | 6.4 1.9 -7.9 -22 13 -10 .42
COD | 2 | -.5 -1.0 -.1 -25 37 -22 .36
EMR | 2 | -1.3 2.4 -.5 -4 13 -38 .35
ESA | 2 | -.1 .7 -1.5 -7 -6 38 .0
GFZ | 2 | .4 .0 -2.4 -52 -52 -17 .31
GRG | 2 | 9.7 -7.6 -15.8 -15 53 -39 1.12
JPL | 2 | -2.6 2.8 8.5 -67 12 5 .35
MIT | 2 | -1.9 .7 -1.9 -4 13 -43 .38
NGS | 2 | 4.6 -5.8 2.8 -2 -19 16 .63
SIO | 2 | 2.5 1.4 -6.9 -13 20 -4 .34
COD | 3 | -1.0 -.8 .0 -47 35 -25 .20
EMR | 3 | 3.7 -.4 1.2 -13 -5 -30 .45
ESA | 3 | .3 .6 -1.3 -7 1 34 -.06
GFZ | 3 | .0 -.6 -2.7 -24 -45 -17 .20
GRG | 3 | 12.6 -4.0 -14.3 -13 32 -12 .84
JPL | 3 | .8 8.2 12.8 -74 7 -22 -.37
MIT | 3 | .7 2.2 -.8 -3 16 -37 .30
NGS | 3 | 1.9 1.1 -4.3 50 -2 23 .55
SIO | 3 | 4.1 2.3 -3.6 0 21 2 .38
COD | 4 | -.7 -1.1 -.6 -66 32 -11 .04
EMR | 4 | 1.7 .8 1.9 -17 -1 -20 .17
ESA | 4 | .2 .5 -1.6 5 -6 51 -.29
GFZ | 4 | .4 -.8 -2.1 -43 -47 -17 .04
GRG | 4 | 15.4 -1.1 -5.9 -17 32 -9 .63
JPL | 4 | 3.4 9.4 10.7 -46 -9 -13 .19
MIT | 4 | .1 4.1 -2.2 -1 5 -28 .16
NGS | 4 | -2.8 -.9 9.2 -13 1 -15 .65
SIO | 4 | 8.3 4.1 -7.8 2 8 7 -.02
COD | 5 | -1.3 -.7 -.8 -56 45 -18 .10
EMR | 5 | 11.6 2.5 6.1 -18 14 -40 .17
ESA | 5 | .9 .7 -1.8 4 -2 43 -.16
GFZ | 5 | .1 -.3 -2.1 -27 -47 -22 -.07
GRG | 5 | 16.5 2.9 -15.8 -18 23 -8 .73
JPL | 5 | 2.6 14.5 7.5 -66 -41 8 .41
MIT | 5 | 1.0 3.3 -4.1 2 10 -36 .25
NGS | 5 | 8.0 -.1 3.7 19 -34 38 .36
SIO | 5 | 7.6 4.0 -3.0 -8 13 -11 -.0
COD | 6 | -.8 -1.1 -.9 -45 20 2 .27
EMR | 6 | -.8 .3 4.3 -19 1 -48 .40
ESA | 6 | .4 .4 -2.2 1 3 44 .08
GFZ | 6 | -.2 -.3 -2.2 -38 -66 -19 .13
GRG | 6 | 8.5 -1.3 -12.3 -22 39 -16 1.21
JPL | 6 | -3.7 11.8 4.4 -46 73 -11 .03
MIT | 6 | .3 2.3 -6.4 -2 15 -39 .43
NGS | 6 | .0 -1.8 10.9 -11 -17 -2 .44
SIO | 6 | 4.3 1.9 -3.9 7 15 5 .31
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1810.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1810.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 2.1810.[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 3.1810.[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 5.1810.0-6). 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 1810 summary. (Sep 14, 2014 - Sep 20, 2014)
Table 1.1810.a GPS week: 1810 MJD: 56914.000-56920.000
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 255| 1 0 2 15 22 -2 .10 8 8 | -916 -400 17 107
| 0 0 2 10 15 7 .02 | 568 649
emr 80| 0 -1 2 17 -14 29 .23 13 13 | 2939 -191 14 157
| 1 1 1 25 17 17 .02 | 750 749
esa 150| 0 0 0 3 -16 12 -.23 11 12 | -591 -587 10 166
| 0 0 1 18 10 11 .03 | 1810 2621
gfz 196| -1 2 5 12 -6 3 .18 13 13 | -5 -400 16 150
| 0 0 1 9 10 16 .03 | 288 544
grg 177| 3 0 -10 -11 14 8 .34 21 19 | -199 -150 18 139
| 1 1 3 29 24 17 .04 | 119 351
igr n/a| 0 0 1 -13 3 1 -.13 5 5 | 5083 -244 17 102
| 0 0 1 15 11 12 .02 | 582 806
jpl 80| -2 -1 -2 -9 8 -5 .07 13 13 | 2880 -138 16 149
| 2 1 1 20 21 18 .02 | 710 973
mit 350| 0 -2 0 -26 -28 -4 -.08 14 13 | -91 -260 36 256
| 0 0 1 22 36 25 .02 | 1121 1286
ngs 232| 0 0 0 -22 22 -28 .01 11 10 | -959 -259 1407 2951
| 1 0 3 54 39 26 .06 | 367 543
sio 482| -1 0 -2 -1 -27 1 -.66 14 15 | --- --- --- ---
| 0 0 0 32 27 18 .03 | --- ---
Table 1.1810.b GPS week : 1810 MJD: 56914.000-56920.000
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 4 4 4 |
2 | 5 5 5 5 5 5 5 |
3 | 14 13 12 10 17 26 17 |
4 | 4 4 4 4 4 4 4 |
5 | 4 5 5 4 4 4 5 |
6 | 6 6 6 7 6 5 5 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 4 4 4 5 4 |
9 | 5 6 6 6 7 6 7 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 4 4 0 4 |
14 | 4 4 4 4 4 4 4 |
15 | 5 5 5 6 5 5 5 |
16 | 6 5 6 5 6 6 6 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 5 4 5 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 5 4 4 5 5 |
22 | 4 4 4 5 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 5 5 4 4 4 |
25 | 4 4 17 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 4 5 4 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 4 5 |
31 | 5 5 5 5 5 5 5 |
32 | 4 4 4 4 4 5 5 |
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 2.1810.0 GPS week: 1810 Day: 0 MJD: 56914.000
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 256| 1 1 2 -2 44 -10 .09 8 8 | -837 60 15 104
emr 80| 1 0 0 -8 -10 25 .20 13 13 | 1572 551 14 155
esa 150| 0 0 -1 -22 -5 31 -.26 12 12 | -1417 2504 10 170
gfz 195| -2 2 6 14 5 11 .19 13 12 | -36 179 16 143
grg 177| 3 0 -9 -26 15 9 .34 20 17 | -22 3 18 151
igr n/a| 0 0 1 1 -7 -3 -.15 5 5 | 4102 565 16 116
jpl 80| -1 -3 -1 20 -25 23 .10 12 12 | 1673 965 18 229
mit 350| 0 -1 0 -31 -63 28 -.04 14 12 | -219 70 29 257
ngs 235| 1 0 0 44 22 -71 -.02 11 9 | -1025 215 1834 3672
sio 481| -1 0 -1 -20 -43 5 -.67 15 15 | --- --- --- ---
Table 2.1810.1 GPS week: 1810 Day: 1 MJD: 56915.000
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 256| 1 0 2 18 14 -5 .10 8 8 | -1196 -219 22 127
emr 80| 2 0 3 66 3 34 .27 13 13 | 2325 660 17 179
esa 150| 0 0 -1 -20 -4 10 -.24 12 12 | -2161 -271 10 151
gfz 198| 0 2 4 13 -1 -9 .16 13 13 | 136 -138 17 142
grg 177| 3 0 -15 -35 -8 28 .34 20 18 | -208 123 18 130
igr n/a| -1 0 0 -22 5 -7 -.13 5 5 | 4744 533 19 91
jpl 80| -3 -1 -3 -9 3 -25 .11 14 14 | 2458 -62 17 164
mit 350| 0 -2 -1 -54 3 16 -.06 12 12 | -518 295 85 480
ngs 235| 1 0 6 43 -12 -26 -.04 11 11 | -756 -226 1361 3241
sio 480| -1 0 -2 -55 -15 12 -.65 14 15 | --- --- --- ---
Table 2.1810.2 GPS week: 1810 Day: 2 MJD: 56916.000
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 257| 0 0 4 8 29 -2 .13 8 8 | -1065 -548 20 118
emr 80| 1 -1 2 14 -8 34 .25 12 12 | 2953 -192 16 175
esa 150| 0 0 0 -1 -11 22 -.24 12 12 | -335 -314 10 144
gfz 198| -1 2 6 17 -5 10 .16 15 14 | -185 -591 17 154
grg 177| 3 0 -13 -53 -11 14 .29 21 19 | -277 -292 20 150
igr n/a| 0 0 2 -26 3 5 -.16 6 6 | 5077 63 18 93
jpl 80| 1 0 0 -11 15 -10 .08 12 12 | 2504 292 18 123
mit 350| 0 -2 0 -11 -63 9 -.09 14 13 | -147 -876 33 262
ngs 236| 1 -1 -3 -16 56 -54 -.07 12 11 | -1490 481 1169 2392
sio 485| -2 0 -3 9 -70 18 -.66 15 15 | --- --- --- ---
Table 2.1810.3 GPS week: 1810 Day: 3 MJD: 56917.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| 0 0 1 21 -1 -9 .09 8 8 | -1865 557 18 99
emr 80| 1 -1 4 4 -36 14 .22 12 12 | 3182 336 14 140
esa 150| 2 0 0 25 -33 0 -.24 11 11 | -1269 1569 11 167
gfz 197| 0 2 5 5 -17 10 .21 13 14 | -456 98 17 160
grg 178| 2 0 -8 16 31 21 .35 21 19 | -392 410 18 128
igr n/a| 0 0 3 -36 -12 28 -.11 5 5 | 5616 373 16 100
jpl 80| -2 -1 -1 -20 0 -18 .06 12 12 | 3221 943 17 174
mit 350| 0 -2 1 -7 23 -3 -.10 13 12 | -1741 1603 25 189
ngs 232| 0 0 -3 -48 29 1 -.00 10 9 | -668 -537 1103 2812
sio 482| -1 -1 -1 20 8 8 -.62 16 16 | --- --- --- ---
Table 2.1810.4 GPS week: 1810 Day: 4 MJD: 56918.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| 0 0 0 28 16 3 .07 8 8 | -600 -1187 16 101
emr 80| 0 -1 3 19 -36 48 .20 13 13 | 3501 -803 13 149
esa 150| 0 1 1 12 -20 7 -.23 11 11 | -2271 -436 10 143
gfz 194| 0 1 5 -4 -12 -9 .20 14 14 | -137 -1153 18 139
grg 178| 5 2 -11 -3 20 -27 .39 20 18 | -192 -497 18 145
igr n/a| 0 0 2 -6 16 -8 -.13 5 5 | 5737 -1223 18 110
jpl 80| -2 -1 -2 -40 18 -7 .06 13 13 | 3812 -1518 16 121
mit 350| 0 -1 0 -36 -40 -14 -.10 13 12 | -41 -453 31 207
ngs 231| 0 0 0 -24 81 -21 .07 12 10 | -617 -1192 1851 3045
sio 486| 0 0 -2 11 -45 -20 -.64 14 13 | --- --- --- ---
Table 2.1810.5 GPS week: 1810 Day: 5 MJD: 56919.000
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| 2 0 5 19 33 12 .11 8 8 | -844 -230 16 111
emr 80| 0 -4 3 26 -20 50 .22 14 14 | 3721 -557 15 152
esa 150| 2 1 -1 16 -26 -1 -.18 11 11 | 2895 -5690 11 235
gfz 196| -1 2 4 11 -20 -19 .21 14 13 | 236 -128 18 188
grg 176| 2 2 -6 -7 -2 11 .38 22 20 | -96 -216 18 143
igr n/a| 0 0 0 -8 17 -5 -.09 5 5 | 5496 -880 18 108
jpl 80| -6 -2 -4 11 1 -13 .04 14 14 | 3285 -379 17 124
mit 350| 0 -1 -1 -48 0 -20 -.08 13 12 | -31 139 23 179
ngs 230| 0 0 -3 -41 13 -20 .04 10 9 | -725 -440 1225 2503
sio 481| 0 1 -1 -19 -8 -29 -.69 14 14 | --- --- --- ---
Table 2.1810.6 GPS week: 1810 Day: 6 MJD: 56920.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| 2 1 0 13 19 -3 .13 9 9 | -8 -1236 15 95
emr 80| -1 -3 3 -3 9 2 .23 13 13 | 3325 -1337 14 149
esa 150| 0 0 0 15 -12 16 -.25 11 11 | 421 -1471 10 153
gfz 195| 0 3 4 26 5 27 .14 13 12 | 406 -1070 14 128
grg 178| 4 0 -8 30 56 6 .32 22 20 | -208 -581 17 131
igr n/a| 0 0 0 3 0 2 -.13 5 5 | 4810 -1143 16 97
jpl 80| -2 -1 0 -12 43 15 .07 13 13 | 3207 -1208 15 108
mit 350| 1 -1 -1 4 -56 -47 -.07 15 15 | 2058 -2599 30 224
ngs 228| -3 0 2 -113 -34 -3 .10 12 10 | -1436 -114 1312 2998
sio 482| 0 0 -3 41 -15 13 -.70 14 14 | --- --- --- ---
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 3.1810.0 GPS week: 1810 Day: 0 MJD: 56914.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 9 12 9 16 6 11 12 9 12 3 | 19 19 23 22 25 16 22 16 20 14 17
2 | 8 13 12 17 19 7 13 12 8 16 4 | 16 20 15 21 22 11 17 17 16 21 11
X3 | 36 22 22 24 --- 12 --- 21 41 --- 13 | 45 38 21 38 --- 42 --- 41 41 --- 34
4 | 6 10 11 11 15 7 10 12 9 19 4 | 16 21 17 19 22 13 20 15 20 20 16
5 | 8 12 10 11 18 4 13 11 11 15 4 | 20 20 13 24 27 14 18 21 20 15 16
6 | 8 8 10 14 55 7 11 11 9 12 5 | 43 46 48 42 56 41 45 41 39 47 43
7 | 6 12 10 9 16 4 12 9 9 14 3 | 23 24 16 27 30 16 21 20 21 14 19
8 | 7 9 11 11 15 4 13 18 7 20 4 | 17 19 19 18 19 15 23 22 17 24 17
X9 | 10 10 11 11 --- 7 --- 17 7 --- 5 | 51 53 53 53 --- 48 --- 52 53 --- 51
10 | 8 11 13 11 14 5 11 10 12 14 4 | 44 49 48 44 50 47 48 53 47 51 47
11 | 7 8 15 8 25 6 10 13 8 11 4 | 33 37 30 32 55 30 37 34 31 31 33
12 | 7 16 12 16 18 4 17 18 10 16 5 | 20 23 16 25 27 13 22 21 19 15 15
13 | 7 11 13 11 15 4 11 11 10 14 4 | 23 28 19 26 27 19 27 18 21 19 21
14 | 5 9 13 13 12 3 11 16 9 19 4 | 27 30 25 32 25 25 28 30 25 23 25
15 | 11 13 15 15 12 4 16 13 18 15 5 | 35 34 34 36 30 28 34 32 30 31 30
16 | 9 15 12 17 26 7 13 22 14 15 5 | 17 23 16 21 26 12 19 19 17 17 13
17 | 8 13 14 13 13 6 14 13 12 18 4 | 24 28 22 30 36 22 27 30 24 22 23
18 | 9 14 11 16 17 6 13 17 12 15 4 | 17 21 17 18 24 12 20 16 20 15 13
19 | 11 13 14 14 16 6 10 12 9 17 4 | 20 29 21 25 34 18 26 22 23 20 21
20 | 9 16 10 12 16 6 13 9 8 14 4 | 20 20 13 21 27 12 17 17 18 11 14
21 | 7 13 10 10 24 3 10 15 12 13 4 | 21 26 16 20 32 15 21 20 20 15 17
22 | 6 11 10 16 16 4 10 14 10 13 4 | 14 21 14 22 26 13 19 16 17 11 13
23 | 9 13 14 12 15 5 14 12 10 16 4 | 22 27 19 26 21 16 25 21 18 15 18
24 | 6 11 13 11 12 4 15 10 15 11 4 | 20 25 26 21 23 19 27 19 24 19 21
25 | 5 17 14 14 16 4 15 13 7 8 4 | 9999 719 9999 9999 993 9999 9999 9999 9999 9999 9999
26 | 8 11 11 8 12 4 8 12 14 9 3 | 23 23 19 26 22 20 21 25 19 22 20
X27 | 10 12 14 11 --- 3 12 10 13 13 4 | 31 33 30 33 --- 31 40 34 37 29 32
28 | 7 14 13 14 19 5 10 9 6 10 4 | 18 19 15 28 32 14 19 22 18 17 16
29 | 9 18 14 12 17 4 13 15 13 16 5 | 30 39 32 31 35 28 37 31 30 29 29
X30 | 6 10 11 9 --- 6 13 9 7 11 3 | 24 27 27 23 --- 23 29 22 25 21 24
31 | 6 14 12 16 22 5 13 19 13 18 5 | 18 25 14 23 33 15 23 26 21 16 18
32 | 6 11 10 14 16 6 11 13 9 13 4 | 37 42 38 41 36 35 41 43 38 39 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 12 13 20 5 12 14 11 15 |T 25 50 23 28 64 22 26 26 25 22 23
WRMS | 8 13 12 12 17 5 12 12 9 15 |NE 24 50 23 27 64 21 26 25 24 22 23
MEDI | 7 12 12 12 16 5 12 12 10 14 |MD 22 26 19 26 27 18 23 22 21 20 20
Table 3.1810.1 GPS week: 1810 Day: 1 MJD: 56915.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 10 12 8 14 4 13 8 13 12 3 | 19 17 22 22 23 14 21 18 20 17 17
2 | 9 14 12 18 18 6 16 11 12 18 5 | 19 22 18 25 20 13 19 21 18 26 15
X3 | 29 33 19 18 --- 26 --- 18 41 --- 12 | 47 40 20 42 --- 46 --- 38 49 --- 35
4 | 7 10 10 11 17 6 9 10 10 20 4 | 17 20 19 18 20 14 19 17 24 23 17
5 | 9 14 10 12 20 5 19 13 11 15 4 | 19 24 15 27 29 15 22 27 16 22 18
6 | 8 9 9 14 53 6 12 11 11 12 5 | 31 34 35 31 40 30 35 32 32 34 31
7 | 8 15 9 10 18 4 12 10 11 16 4 | 24 25 16 26 31 16 23 22 22 19 19
8 | 7 11 10 11 16 4 11 11 9 20 4 | 20 23 20 22 22 18 25 21 20 27 20
X9 | 11 10 13 14 --- 6 --- 13 13 --- 5 | 42 41 40 39 --- 38 --- 41 36 --- 37
10 | 8 10 12 13 12 5 12 9 10 11 3 | 56 55 53 56 55 53 56 55 54 56 54
11 | 8 8 15 8 23 6 12 8 14 12 4 | 24 26 24 25 42 23 30 24 24 25 23
12 | 9 15 10 18 18 7 18 16 12 14 5 | 23 26 16 30 27 16 24 24 25 18 19
13 | 6 11 13 11 17 4 12 8 12 12 3 | 20 25 17 19 25 16 25 15 18 15 18
14 | 7 10 13 16 15 5 12 13 9 13 4 | 17 27 22 22 20 18 20 22 26 18 19
15 | 10 14 15 13 14 4 17 16 9 14 4 | 24 29 26 29 24 21 29 28 24 23 23
16 | 9 16 11 16 24 7 12 21 13 14 5 | 18 25 17 17 27 14 21 19 23 21 14
17 | 9 15 12 13 14 6 14 15 13 18 4 | 23 27 24 26 29 21 26 25 21 20 20
18 | 9 15 10 15 21 6 17 16 12 14 4 | 13 24 11 18 23 10 22 19 19 16 12
19 | 11 15 14 11 19 6 13 14 15 17 5 | 16 28 21 20 27 14 24 21 20 17 16
20 | 8 13 10 13 17 6 11 9 11 16 4 | 19 18 15 20 25 13 19 18 21 17 14
21 | 7 8 10 8 20 5 14 13 11 14 4 | 20 20 14 20 27 14 22 21 22 17 16
22 | 9 12 10 16 19 5 14 12 10 12 4 | 12 21 11 21 26 12 19 16 19 13 12
23 | 8 12 13 13 18 4 15 10 14 17 4 | 21 28 21 25 24 16 26 20 20 19 19
24 | 7 14 11 15 16 5 19 9 11 10 4 | 23 29 25 26 28 23 32 23 30 21 24
25 | 7 14 12 12 15 6 14 9 8 8 4 | 9999 684 9999 9999 9999 9999 9999 9999 9999 9999 9999
26 | 7 9 12 11 13 7 12 12 10 12 3 | 22 21 19 30 18 19 19 23 20 20 19
X27 | 7 10 13 10 --- 5 15 10 11 15 4 | 25 26 25 24 --- 21 34 24 25 25 24
28 | 6 15 11 10 18 4 12 12 10 8 4 | 21 21 19 25 32 17 23 24 22 18 19
29 | 10 16 13 14 20 5 17 12 13 17 5 | 22 26 23 26 26 19 26 24 27 22 20
X30 | 6 12 9 7 --- 4 12 8 9 12 3 | 21 24 26 22 --- 21 30 23 24 21 22
31 | 7 16 13 22 23 5 16 18 12 13 5 | 16 24 13 23 33 14 22 24 25 14 16
32 | 8 9 10 12 15 6 14 13 11 14 4 | 41 44 44 38 44 39 45 48 39 45 42
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 12 13 20 5 14 12 11 14 |T 23 47 22 26 28 20 26 25 25 22 21
WRMS | 8 13 12 13 18 5 14 12 11 15 |NE 22 47 22 25 28 19 26 24 24 22 21
MEDI | 8 12 12 13 18 5 13 12 11 14 |MD 21 25 20 25 27 17 24 23 23 20 19
Table 3.1810.2 GPS week: 1810 Day: 2 MJD: 56916.000
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 9 18 4 12 13 11 14 4 | 22 22 24 19 26 17 24 20 19 19 19
2 | 7 12 11 18 21 6 13 12 12 15 4 | 20 21 18 27 23 13 17 22 20 20 16
X3 | 34 29 16 21 --- 25 --- 17 31 --- 12 | 47 43 18 40 --- 50 --- 40 43 --- 37
4 | 7 8 11 13 17 6 9 13 8 18 4 | 19 23 22 18 23 17 19 19 21 23 19
5 | 7 13 9 12 21 6 16 13 12 14 4 | 23 26 16 28 29 16 20 24 22 19 19
6 | 7 9 9 17 51 7 10 17 12 12 5 | 39 43 43 38 47 37 43 39 40 42 40
7 | 8 11 10 14 19 4 12 12 11 15 4 | 23 27 20 31 32 19 24 23 22 19 21
8 | 9 8 12 12 17 5 9 16 10 18 4 | 22 26 26 25 25 22 26 23 24 28 23
X9 | 13 14 13 11 --- 8 --- 14 11 --- 6 | 47 44 44 39 --- 35 --- 42 40 --- 41
10 | 5 9 12 11 17 6 10 10 11 17 4 | 64 62 62 67 56 64 66 61 68 58 62
11 | 8 9 15 9 27 6 10 11 9 7 4 | 31 34 29 30 49 29 32 31 30 31 30
12 | 9 15 9 19 18 4 19 19 14 15 5 | 24 26 16 33 29 17 22 24 29 17 20
13 | 7 10 13 11 19 4 11 10 11 12 4 | 21 28 22 24 26 22 26 20 19 16 22
14 | 9 8 13 12 12 4 11 13 12 16 4 | 25 29 27 26 28 24 24 27 30 24 24
15 | 10 12 14 14 14 5 16 15 17 16 5 | 36 34 33 38 31 28 33 32 29 32 31
16 | 11 12 13 23 24 6 13 22 13 13 5 | 20 20 17 25 27 17 19 20 23 19 16
17 | 9 13 13 14 19 6 14 17 12 20 5 | 25 30 24 32 36 24 28 29 24 23 24
18 | 9 17 13 18 19 6 14 17 12 17 5 | 21 26 20 22 27 18 22 18 23 19 17
19 | 11 12 14 17 19 5 11 13 10 17 4 | 20 29 22 29 34 18 25 22 25 21 21
20 | 9 13 9 14 16 5 12 9 10 10 4 | 25 24 21 25 27 18 21 21 26 16 20
21 | 7 8 12 15 25 6 9 17 11 17 4 | 22 23 17 24 31 15 20 23 19 19 17
22 | 7 11 10 14 16 5 11 14 12 12 4 | 20 27 20 25 30 20 22 20 28 13 20
23 | 10 11 15 14 18 4 13 11 12 18 4 | 26 31 26 30 26 22 27 22 23 19 22
24 | 9 13 12 16 15 9 14 13 15 15 4 | 21 25 22 21 24 21 25 23 27 22 20
X25 | 29 --- 21 55 201 78 159 54 40 26 17 | 9999 --- 9999 9999 9999 9999 9999 9999 9999 9999 9999
26 | 7 10 11 13 13 8 7 14 13 11 3 | 26 24 23 33 25 21 22 27 18 25 22
X27 | 11 8 13 15 --- 6 15 7 13 13 4 | 25 31 26 28 --- 27 35 28 35 26 28
28 | 7 10 13 14 21 6 10 13 9 10 4 | 20 22 19 28 34 18 23 25 21 21 20
29 | 9 16 13 20 17 5 14 13 10 17 5 | 25 28 26 34 32 22 27 27 23 25 24
X30 | 7 13 10 9 --- 5 13 9 7 12 4 | 26 28 30 27 --- 26 32 26 28 29 27
31 | 8 13 13 16 20 5 11 18 13 16 4 | 20 27 18 30 35 20 22 24 24 21 21
32 | 8 10 10 14 17 6 10 15 9 17 4 | 40 41 41 36 41 36 39 48 38 43 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 12 15 21 6 12 14 12 15 |T 27 29 25 30 31 24 27 27 27 24 25
WRMS | 8 12 12 14 19 6 12 13 11 15 |NE 26 29 25 29 31 23 27 27 27 24 24
MEDI | 8 11 12 14 18 6 12 13 12 15 |MD 24 27 22 28 29 21 24 24 24 21 22
Table 3.1810.3 GPS week: 1810 Day: 3 MJD: 56917.000
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 10 11 14 13 4 11 9 10 15 4 | 25 22 23 20 22 17 22 18 19 17 19
2 | 6 16 11 18 16 6 10 13 11 20 4 | 20 24 19 23 23 14 18 21 20 22 16
X3 | 21 30 22 25 --- 23 --- 16 21 --- 10 | 44 46 18 41 --- 55 --- 39 47 --- 39
4 | 6 9 10 11 14 4 9 10 6 20 3 | 20 22 19 17 23 15 22 18 17 23 17
5 | 9 12 11 11 21 5 13 13 9 13 4 | 20 24 15 22 28 16 19 21 21 13 16
6 | 6 14 9 17 61 8 11 16 8 11 6 | 39 45 43 39 47 37 43 38 36 41 39
7 | 8 11 10 12 18 4 13 12 8 16 4 | 23 26 17 25 31 17 22 21 22 15 19
8 | 8 10 10 11 15 5 10 12 8 18 4 | 21 24 20 18 21 16 22 22 23 22 19
X9 | 15 12 10 11 --- 5 --- 10 16 --- 5 | 51 45 46 43 --- 43 --- 44 54 --- 46
10 | 5 13 12 11 12 5 9 9 10 12 3 | 48 49 50 44 52 47 50 52 50 50 49
11 | 8 8 13 10 22 5 10 8 7 12 3 | 38 38 34 35 51 33 41 34 37 30 35
12 | 9 16 8 13 18 4 18 18 8 14 4 | 24 27 18 26 29 18 23 23 21 16 19
13 | 7 10 13 13 18 4 10 10 10 18 4 | 22 29 20 20 28 17 24 18 19 24 20
14 | 8 10 14 15 12 5 10 12 9 16 4 | 25 33 25 28 24 25 25 27 23 23 24
15 | 12 14 15 13 16 5 17 16 16 19 5 | 30 33 28 29 29 25 30 27 27 27 25
16 | 10 16 11 16 23 6 12 20 11 15 5 | 22 26 22 25 23 21 24 24 23 22 19
17 | 8 15 12 12 15 4 14 17 10 20 4 | 26 31 25 33 34 24 30 32 30 22 26
18 | 12 12 8 15 20 6 15 16 12 18 5 | 25 25 19 21 23 17 26 14 19 15 16
19 | 10 14 11 11 18 7 12 11 10 19 4 | 24 31 24 23 30 20 27 20 25 19 22
20 | 7 15 7 13 15 4 11 10 9 14 3 | 24 22 17 21 24 15 19 18 20 14 17
21 | 8 9 11 10 21 7 8 14 9 11 3 | 28 25 20 25 27 20 27 21 19 18 21
22 | 9 11 10 14 19 5 12 12 13 13 4 | 21 23 20 23 26 18 21 17 21 18 17
23 | 8 12 12 14 19 4 13 10 9 19 4 | 21 27 20 25 26 17 25 18 17 16 18
24 | 8 12 11 16 19 5 17 12 11 12 4 | 39 37 39 38 36 36 36 37 39 39 36
25 | 8 13 12 10 16 5 12 12 11 11 4 | 749 9999 751 753 760 742 752 745 748 749 748
26 | 8 11 11 10 15 5 10 12 6 12 3 | 22 29 24 31 30 24 27 29 24 27 24
X27 | 10 9 13 12 --- 7 14 9 10 13 4 | 36 41 38 41 --- 38 44 41 39 37 38
28 | 7 14 13 10 18 4 9 13 11 10 4 | 19 22 16 21 31 16 19 23 23 17 17
29 | 8 14 13 12 18 5 15 13 11 19 4 | 30 33 29 30 31 26 33 28 26 26 27
X30 | 6 11 10 9 --- 4 14 8 12 13 4 | 25 28 25 21 --- 23 30 22 32 20 24
31 | 9 13 11 15 21 5 14 14 11 15 4 | 19 29 18 27 35 22 25 22 26 19 20
32 | 8 10 9 12 16 6 9 15 10 15 4 | 51 54 52 56 51 51 56 58 52 53 53
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 11 13 21 5 12 13 10 16 |T 50 31 48 51 56 47 52 49 50 48 48
WRMS | 8 12 11 14 19 5 12 12 9 16 |NE 51 30 49 51 56 47 52 50 50 48 48
MEDI | 8 12 11 12 18 5 12 12 10 15 |MD 25 29 22 25 29 21 25 23 23 22 21
Table 3.1810.4 GPS week: 1810 Day: 4 MJD: 56918.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 11 13 12 15 6 12 9 11 10 3 | 20 20 22 20 23 16 21 16 17 15 16
2 | 8 15 13 19 18 5 12 15 10 19 5 | 16 22 15 25 21 13 16 21 17 21 12
X3 | 28 47 --- 20 --- 17 --- 18 48 --- 17 | 59 67 --- 54 --- 50 --- 54 63 --- 53
4 | 5 9 11 11 18 6 11 13 9 16 4 | 18 21 20 19 24 16 18 17 18 21 16
5 | 7 13 9 11 19 4 16 11 12 11 4 | 23 26 17 25 30 17 21 21 19 14 18
6 | 7 10 8 14 53 7 15 15 8 11 5 | 41 43 42 36 51 38 42 37 40 40 40
7 | 8 12 11 15 16 3 13 12 8 15 4 | 23 24 16 27 30 16 22 20 19 17 18
8 | 7 11 11 11 18 4 9 14 11 20 4 | 20 22 20 19 22 16 21 19 17 25 18
X9 | 9 11 10 14 58 6 --- 12 9 17 6 | 41 44 37 37 32 38 --- 40 44 35 41
10 | 8 10 10 10 16 5 10 12 13 12 4 | 30 31 30 26 32 31 32 32 34 33 30
11 | 6 8 13 11 22 4 10 9 11 8 3 | 28 33 24 27 46 25 31 28 32 27 28
12 | 8 16 7 14 18 6 19 14 15 13 4 | 21 23 13 25 28 15 21 23 21 15 16
13 | 7 10 13 12 18 4 10 10 10 15 4 | 23 29 22 26 32 18 26 20 19 20 20
14 | 9 10 15 14 11 5 14 11 11 12 4 | 23 26 23 19 23 19 24 25 28 18 21
15 | 9 12 13 11 15 6 16 16 14 14 4 | 26 31 28 31 29 24 28 29 28 25 25
16 | 13 19 11 21 25 6 15 20 14 15 5 | 17 22 13 21 25 11 18 19 15 18 10
17 | 10 16 14 13 18 6 12 17 13 18 5 | 21 28 23 29 32 19 26 29 23 22 21
18 | 7 17 10 17 19 5 14 16 11 13 4 | 19 24 18 24 28 18 26 16 23 16 16
19 | 10 15 12 16 16 5 11 10 12 16 4 | 16 26 18 22 29 14 22 20 23 17 17
20 | 9 13 7 12 18 4 12 8 8 12 3 | 23 21 15 23 28 17 20 19 21 14 17
21 | 6 10 12 9 22 4 12 13 8 14 4 | 21 22 15 23 30 14 20 19 19 18 16
22 | 5 12 9 14 18 5 11 12 13 12 4 | 15 23 15 23 30 16 21 17 23 13 16
23 | 9 13 13 14 19 4 12 12 14 16 4 | 23 26 20 26 22 16 23 16 16 13 17
24 | 6 13 12 12 12 7 12 12 13 12 4 | 30 34 32 30 33 33 34 28 38 30 31
25 | 7 16 10 11 15 4 13 13 14 9 4 | 561 388 563 559 548 562 557 561 559 562 561
26 | 7 10 8 10 14 5 10 11 13 12 3 | 20 27 23 31 22 19 21 28 20 25 21
X27 | 6 9 15 12 --- 4 12 11 13 12 4 | 30 27 28 25 --- 26 34 26 33 21 27
28 | 6 12 10 14 21 5 11 12 12 10 4 | 17 20 15 24 32 14 17 22 23 15 16
29 | 9 14 12 14 18 3 14 14 12 14 4 | 25 28 26 30 31 23 29 30 25 27 24
X30 | 5 13 9 8 --- 5 13 8 10 11 3 | 23 24 24 18 --- 19 27 20 23 21 21
31 | 6 15 10 21 20 5 18 12 15 14 5 | 16 26 13 23 32 15 23 17 21 13 14
32 | 6 11 8 12 17 6 10 15 9 14 4 | 43 46 42 44 40 40 44 48 41 46 43
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 11 14 20 5 13 13 12 14 |T 41 39 39 43 47 38 42 41 42 39 39
WRMS | 8 13 11 14 18 5 13 12 10 13 |NE 41 38 39 43 47 38 42 41 41 39 38
MEDI | 7 12 11 12 18 5 12 12 12 13 |MD 23 26 22 25 30 18 23 21 23 21 18
Table 3.1810.5 GPS week: 1810 Day: 5 MJD: 56919.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 11 11 11 15 5 12 11 10 12 3 | 20 20 21 19 22 15 23 14 15 14 16
2 | 7 18 11 18 18 5 13 12 11 18 4 | 19 27 15 25 21 14 20 21 13 20 14
X3E | 16 --- --- 38 --- 129 --- --- --- --- 26 | 43 --- --- 55 --- 112 --- --- --- --- 39
4 | 9 10 11 13 16 6 12 14 8 18 4 | 19 20 18 15 19 13 20 16 14 19 15
5 | 7 13 10 12 26 4 18 9 11 11 4 | 16 22 12 22 31 12 21 19 21 16 15
6 | 6 10 8 13 47 8 12 15 12 10 5 | 39 39 38 37 46 31 40 33 33 35 36
7 | 8 11 11 10 21 3 12 13 8 15 4 | 23 24 16 24 32 15 23 19 17 12 17
8 | 8 11 12 13 22 3 11 14 9 17 4 | 23 24 22 21 22 18 26 21 16 20 19
X9 | 9 12 11 11 52 7 --- 11 9 21 6 | 37 39 34 33 31 33 --- 33 39 29 36
10 | 5 13 8 13 21 6 12 10 7 15 4 | 33 36 32 36 32 31 31 35 32 32 32
11 | 7 10 14 7 26 3 10 10 9 8 4 | 24 30 24 25 44 23 30 24 29 21 24
12 | 9 17 10 14 15 7 20 17 9 12 4 | 25 29 21 24 28 19 23 25 23 15 20
X13 | 4 --- --- --- --- 25 --- --- --- --- 0 | 14 --- --- --- --- 5 --- --- --- --- 13
14 | 7 10 13 14 17 6 16 13 8 12 4 | 26 25 24 26 27 20 25 27 20 18 21
15 | 9 15 14 15 17 5 18 16 13 17 5 | 22 30 25 28 27 20 30 24 22 19 20
16 | 12 21 11 14 25 6 17 23 12 12 5 | 19 27 14 20 20 11 19 22 17 16 13
17 | 10 16 12 13 18 7 15 17 8 16 4 | 21 28 23 26 29 19 27 31 24 23 21
18 | 7 16 8 13 24 5 17 15 11 12 4 | 21 25 19 25 24 19 32 22 23 22 19
19 | 8 13 12 9 19 4 12 12 11 16 4 | 16 25 20 18 25 15 23 19 17 17 15
20 | 9 13 10 12 19 5 12 9 9 10 4 | 23 23 15 18 27 16 22 18 18 16 17
21 | 6 17 10 12 22 5 17 11 14 17 4 | 22 27 16 26 24 15 29 17 20 23 17
22 | 6 15 9 14 22 5 13 10 10 13 4 | 18 23 16 26 27 17 23 15 20 19 16
23 | 11 14 14 11 24 5 14 11 14 18 5 | 23 28 21 21 25 16 26 16 16 11 16
24 | 7 11 12 11 15 6 14 10 7 10 3 | 32 32 36 35 34 32 37 30 36 31 32
25 | 8 15 11 9 12 5 14 14 8 9 4 | 391 420 393 393 393 389 391 394 389 386 391
26 | 5 12 10 23 19 5 10 11 8 12 4 | 26 32 25 42 30 25 30 29 26 27 27
X27 | 4 6 12 9 --- 3 13 12 9 13 3 | 25 26 24 29 --- 24 29 26 26 24 25
28 | 7 13 11 20 17 5 15 10 8 10 4 | 20 22 17 28 31 15 20 22 20 19 18
29 | 9 15 13 14 19 4 14 11 13 15 4 | 26 32 27 28 25 22 25 26 24 22 22
X30 | 4 15 10 16 --- 5 15 8 9 12 4 | 22 26 24 26 --- 21 27 20 24 21 21
31 | 12 17 10 13 22 4 17 10 13 12 4 | 23 29 17 22 33 17 23 21 24 12 18
32 | 9 18 8 15 21 8 14 16 8 15 4 | 79 81 81 77 74 74 79 92 80 79 80
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 11 14 22 5 14 13 10 14 |T 37 42 36 40 42 35 40 37 36 34 34
WRMS | 8 14 11 13 20 5 14 12 9 14 |NE 37 42 36 39 42 32 40 37 36 34 34
MEDI | 7 13 11 13 19 5 14 11 9 12 |MD 23 27 21 26 27 19 26 22 22 20 19
Table 3.1810.6 GPS week: 1810 Day: 6 MJD: 56920.000
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 10 12 10 18 4 11 14 14 10 4 | 21 21 21 21 24 16 20 15 20 11 17
2 | 8 15 11 18 22 6 13 14 12 20 5 | 16 24 13 27 25 12 16 19 19 23 13
X3E | 35 34 --- 27 --- 20 --- 27 37 --- 16 | 62 79 --- 62 --- 71 --- 72 61 --- 58
4 | 8 8 10 9 17 4 9 16 12 16 4 | 13 17 15 14 20 11 16 16 18 17 13
5 | 7 12 9 12 25 4 18 10 13 10 4 | 18 23 13 26 30 15 19 22 25 16 18
6 | 6 11 9 14 50 6 12 13 10 10 5 | 48 50 50 43 61 46 49 41 48 47 47
7 | 9 9 11 13 21 4 13 16 8 13 4 | 22 23 17 27 29 15 19 20 21 12 17
8 | 8 11 12 7 18 4 9 15 11 19 4 | 16 20 20 19 18 15 18 18 22 23 17
X9 | 11 9 9 14 58 7 --- 22 10 18 7 | 82 85 78 76 54 77 --- 88 80 62 81
10 | 5 12 13 12 20 5 12 11 11 17 4 | 22 25 22 25 26 23 25 28 27 24 23
11 | 7 8 14 8 23 3 9 16 9 7 4 | 31 36 30 33 52 32 38 36 37 33 33
12 | 11 15 11 13 19 5 22 21 10 14 5 | 24 27 18 25 30 17 25 25 22 12 18
X13 | 10 11 13 11 --- 5 10 12 9 14 4 | 8 14 15 3 --- 6 11 4 5 4 7
14 | 10 10 12 13 13 4 12 16 10 12 4 | 28 32 27 29 26 25 27 32 32 25 27
15 | 9 14 14 11 17 4 18 19 14 14 5 | 33 36 33 36 34 30 33 32 36 29 31
16 | 12 17 11 17 26 6 15 23 13 15 5 | 21 24 16 21 21 15 20 20 24 18 15
17 | 8 14 12 11 21 6 13 16 12 18 4 | 26 31 24 30 38 23 27 33 27 23 25
18 | 8 15 7 14 18 5 11 19 10 12 4 | 16 22 16 18 23 13 19 14 18 15 13
19 | 12 15 12 16 19 5 10 15 14 16 5 | 20 30 21 26 30 19 23 26 29 20 21
20 | 10 12 10 10 18 4 9 11 8 11 3 | 21 19 14 22 20 16 18 18 21 18 16
21 | 8 12 9 12 25 3 13 11 12 15 4 | 17 23 15 22 30 12 20 15 17 18 14
22 | 7 14 7 13 17 4 12 13 11 10 4 | 15 23 14 20 23 12 19 13 17 14 13
23 | 12 13 13 12 24 7 12 14 11 17 5 | 25 29 19 27 28 17 23 22 21 12 19
24 | 9 9 10 10 16 4 12 17 7 11 4 | 29 32 32 30 30 28 31 36 35 28 30
25 | 9 11 13 11 14 3 13 17 9 7 4 | 315 306 317 316 315 313 311 319 313 312 314
26 | 7 11 10 12 20 6 10 12 12 8 4 | 22 27 25 30 29 22 21 29 27 25 23
X27 | 8 9 13 11 --- 5 10 16 10 14 4 | 28 31 26 32 --- 29 34 35 36 29 30
28 | 8 14 9 12 24 5 12 12 8 8 4 | 17 20 14 23 35 13 17 21 20 14 16
29 | 10 18 12 15 20 5 17 13 15 17 5 | 31 40 31 35 36 30 36 34 36 32 31
X30 | 8 14 10 17 --- 6 14 11 12 11 4 | 24 29 26 26 --- 22 30 21 28 22 24
31 | 10 17 11 17 21 4 13 18 16 13 5 | 17 31 18 26 32 20 26 21 29 18 19
32 | 10 12 10 12 21 6 12 19 15 16 4 | 42 48 45 48 42 41 47 54 51 48 46
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 13 22 5 13 15 12 14 |T 35 39 33 38 41 33 34 37 38 32 34
WRMS | 9 13 11 12 20 5 13 15 10 14 |NE 34 38 33 37 41 31 34 36 37 32 33
MEDI | 8 12 11 12 20 5 12 15 11 14 |MD 22 27 21 26 30 19 23 22 27 22 19
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 4.1810 GPS week: 1810 MJD: 56914.0-56920.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 |U 6 6 12 |U 6 7 20 |U 7 8 17 |
emr | emr 3022 | 9 9 18 |U 6 7 21 | 8 9 18 |
esa | esa 3017 | 6 6 15 |U 6 7 22 | 8 8 17 |
gfz | gfz 3057 |U 6 6 13 |U 6 7 22 |U 7 7 17 |
grg | grg 2701 | 9 10 18 |U 7 8 29 |U 9 10 21 |
igr | igr 3050 | 6 6 13 | 5 6 20 | 8 8 16 |
igs | igs 3041 | 6 7 13 | 5 6 20 | 7 8 16 |
jpl | jpl 2865 | 8 8 17 |U 7 8 23 | 9 8 19 |
mit | mit 3044 |U 11 8 27 |U 7 9 25 |U 9 9 19 |
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 5.1810.0 GPS week: 1810 Day: 0 MJD: 56914.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 4 4 11 | 5 7 19 | 6 7 14 |
emr | emr 3062 | 7 7 19 | 6 6 18 | 9 8 16 |
esa | esa 3072 | 4 5 14 | 6 6 22 | 8 7 14 |
gfz | gfz 3072 | 4 4 13 | 6 6 20 | 6 5 15 |
grg | grg 2688 | 6 5 18 | 6 8 34 | 8 10 19 |
igr | igr 3072 | 4 4 11 | 5 6 20 | 7 6 12 |
igs | igs 3072 | 4 4 13 | 5 6 19 | 7 6 13 |
jpl | jpl 2876 | 6 5 16 | 8 8 28 | 9 6 15 |
mit | mit 3072 | 5 6 13 | 7 8 19 | 7 6 15 |
Table 5.1810.1 GPS week: 1810 Day: 1 MJD: 56915.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 5 5 13 | 4 5 18 | 8 6 12 |
emr | emr 3062 | 7 9 14 | 4 5 23 | 8 9 15 |
esa | esa 3072 | 5 4 10 | 5 5 23 | 8 6 13 |
gfz | gfz 3071 | 5 5 13 | 4 5 19 | 7 6 12 |
grg | grg 2688 | 7 8 16 | 5 5 30 | 9 9 16 |
igr | igr 3048 | 5 5 11 | 4 4 19 | 8 7 11 |
igs | igs 3072 | 5 5 12 | 4 4 19 | 7 6 11 |
jpl | jpl 2880 | 7 7 14 | 5 5 19 | 9 8 14 |
mit | mit 3072 | 34 16 105 | 8 14 31 | 10 9 23 |
Table 5.1810.2 GPS week: 1810 Day: 2 MJD: 56916.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 7 7 11 | 5 7 21 | 7 7 18 |
emr | emr 2969 | 14 12 13 | 6 7 22 | 8 8 13 |
esa | esa 3072 | 8 8 13 | 6 7 24 | 8 7 16 |
gfz | gfz 3072 | 8 7 12 | 5 7 21 | 8 7 17 |
grg | grg 2687 | 12 11 16 | 7 9 31 | 10 11 25 |
igr | igr 3071 | 8 9 11 | 5 6 19 | 10 7 14 |
igs | igs 3072 | 9 9 12 | 5 6 20 | 7 7 15 |
jpl | jpl 2880 | 11 10 14 | 6 9 16 | 9 9 19 |
mit | mit 3072 | 8 7 11 | 8 7 26 | 7 7 16 |
Table 5.1810.3 GPS week: 1810 Day: 3 MJD: 56917.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 7 6 9 | 6 7 20 | 8 10 22 |
emr | emr 3063 | 8 8 14 | 6 6 19 | 8 9 22 |
esa | esa 3072 | 6 6 12 | 6 6 21 | 8 9 21 |
gfz | gfz 3070 | 7 6 9 | 6 9 24 | 8 9 21 |
grg | grg 2688 | 10 10 13 | 8 7 26 | 11 11 26 |
igr | igr 3047 | 6 5 11 | 5 6 19 | 9 9 22 |
igs | igs 3040 | 7 7 10 | 5 6 18 | 8 9 21 |
jpl | jpl 2878 | 9 9 17 | 5 7 16 | 8 8 24 |
mit | mit 3072 | 8 6 12 | 6 10 22 | 11 11 24 |
Table 5.1810.4 GPS week: 1810 Day: 4 MJD: 56918.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 8 7 16 | 6 7 23 | 7 7 16 |
emr | emr 3060 | 12 10 26 | 7 10 22 | 7 6 14 |
esa | esa 2976 | 8 7 21 | 6 8 24 | 8 8 16 |
gfz | gfz 3072 | 8 7 18 | 6 8 24 | 7 6 14 |
grg | grg 2784 | 10 11 28 | 8 9 30 | 8 8 17 |
igr | igr 3072 | 8 7 18 | 6 8 23 | 7 8 14 |
igs | igs 3045 | 8 7 19 | 6 8 22 | 7 6 15 |
jpl | jpl 2879 | 11 7 25 | 7 10 24 | 8 7 18 |
mit | mit 3072 | 9 7 17 | 7 9 28 | 9 9 14 |
Table 5.1810.5 GPS week: 1810 Day: 5 MJD: 56919.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2944 | 5 10 16 | 5 6 17 | 8 15 21 |
emr | emr 2880 | 8 12 20 | 6 8 18 | 11 16 27 |
esa | esa 2880 | 7 9 18 | 7 7 19 | 9 15 22 |
gfz | gfz 2976 | 6 10 18 | 6 8 19 | 8 13 23 |
grg | grg 2688 | 9 14 21 | 7 10 29 | 9 16 22 |
igr | igr 2976 | 6 10 17 | 6 6 20 | 9 14 20 |
igs | igs 2932 | 6 10 16 | 6 6 19 | 8 14 21 |
jpl | jpl 2784 | 9 10 22 | 11 10 30 | 11 14 22 |
mit | mit 2880 | 6 9 16 | 6 6 23 | 10 14 22 |
Table 5.1810.6 GPS week: 1810 Day: 6 MJD: 56920.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3029 | 5 6 11 | 7 8 21 | 7 6 16 |
emr | emr 3060 | 8 8 17 | 7 10 25 | 8 6 18 |
esa | esa 2976 | 5 5 13 | 8 8 24 | 7 5 17 |
gfz | gfz 3067 | 5 6 10 | 8 8 24 | 7 5 17 |
grg | grg 2688 | 7 8 18 | 7 11 27 | 8 7 20 |
igr | igr 3066 | 5 5 12 | 7 8 21 | 7 6 17 |
igs | igs 3057 | 5 6 12 | 7 8 23 | 7 5 16 |
jpl | jpl 2880 | 7 7 16 | 8 9 24 | 9 6 21 |
mit | mit 3072 | 9 8 14 | 10 11 26 | 10 10 20 |
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 6.1810 GPS week: 1810 MJD: 56914.500-56920.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -31 -5 8 1 -2 | 24 28
| 18 10 57 83 4 | 4
emr uuuuu | 26 -22 87 125 -13 | 27 37
| 19 23 97 87 10 | 10
esa uuuuu | 27 -13 24 28 2 | 25 29
| 6 20 37 50 6 | 3
gfz uuuuu | 7 -3 -108 -41 4 | 18 24
| 15 14 86 73 4 | 3
grg uuuuu | 9 9 -65 -118 6 | 34 36
| 15 32 94 104 3 | 2
igr xxxxx | 24 6 -50 99 -1 | -3 15
| 10 19 53 43 5 | 3
irf xxxxx | 24 3 -25 169 -2 | -3 14
| 9 18 56 43 5 | 4
jpl uuuuu | 12 11 3 166 -1 | 19 25
| 31 18 81 76 11 | 2
mit uuuuu | -8 18 -98 -150 -4 | 24 28
| 12 20 30 70 8 | 3
ngs uuuuu | -13 13 73 -69 1 | 8 16
| 35 65 60 51 9 | 4
sio xxxxx | 38 -3 -21 189 0 | 34 37
| 12 34 60 46 6 | 3
Table 7.1810.0 GPS week: 1810 Day: 0 MJD: 56914.500
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 | -62 7 54 -72 -1 | 27 30
emr uuuuu | 20 -8 136 152 -30 | 41 47
esa uuuuu | 19 21 -17 5 1 | 28 31
gfz uuuuu | 7 14 -126 -23 1 | 21 25
grg uuuuu | 8 36 -176 -182 6 | 36 38
igr xxxxx | 36 2 -114 142 -6 | 1 12
irf xxxxx | 35 32 -87 213 3 | 0 12
jpl uuuuu | 76 -8 6 290 19 | 20 24
mit uuuuu | -2 49 -91 -132 7 | 26 29
ngs uuuuu | -6 -73 49 -63 -8 | 13 16
sio xxxxx | 54 40 -87 238 5 | 37 39
Table 7.1810.1 GPS week: 1810 Day: 1 MJD: 56915.500
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 -14 143 -2 | 29 31
emr uuuuu | 2 21 103 -25 -14 | 37 45
esa uuuuu | 27 4 2 135 -7 | 30 32
gfz uuuuu | -12 -8 -194 -131 -5 | 23 26
grg uuuuu | 1 10 -82 -215 7 | 37 39
igr xxxxx | 10 17 -72 79 2 | 2 12
irf xxxxx | 12 14 32 109 -4 | 2 10
jpl uuuuu | -1 16 142 72 4 | 24 27
mit uuuuu | -16 35 -38 -153 -3 | 29 31
ngs uuuuu | 46 -65 48 -41 4 | 13 16
sio xxxxx | 30 26 41 125 1 | 39 40
Table 7.1810.2 GPS week: 1810 Day: 2 MJD: 56916.500
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 | -17 1 -7 82 2 | 25 29
emr uuuuu | 14 -41 197 60 -4 | 31 41
esa uuuuu | 33 -10 21 23 15 | 25 29
gfz uuuuu | -6 -13 -196 -114 9 | 18 24
grg uuuuu | 20 66 -193 -204 7 | 33 35
igr xxxxx | 22 25 -112 127 3 | -2 15
irf xxxxx | 29 9 -54 182 6 | -2 15
jpl uuuuu | 5 10 56 150 3 | 19 24
mit uuuuu | -15 24 -99 -215 6 | 26 29
ngs uuuuu | -13 1 40 -9 -12 | 9 16
sio xxxxx | 39 24 -52 202 9 | 35 38
Table 7.1810.3 GPS week: 1810 Day: 3 MJD: 56917.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -23 -21 115 -78 0 | 23 28
emr uuuuu | 47 -26 -37 133 -14 | 27 39
esa uuuuu | 28 -33 68 36 1 | 25 29
gfz uuuuu | -5 -11 11 -76 4 | 17 24
grg uuuuu | -5 -8 -48 -88 12 | 32 34
igr xxxxx | 32 7 8 87 5 | -3 16
irf xxxxx | 17 4 -86 143 -6 | -3 15
jpl uuuuu | 12 39 -107 188 -1 | 18 24
mit uuuuu | -18 17 -129 -70 -12 | 25 29
ngs uuuuu | -21 42 13 -40 1 | 6 17
sio xxxxx | 27 -10 -86 161 1 | 33 36
Table 7.1810.4 GPS week: 1810 Day: 4 MJD: 56918.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -23 -12 -32 -25 -9 | 23 28
emr uuuuu | 39 -47 155 121 -20 | 23 33
esa uuuuu | 30 -10 9 3 2 | 24 28
gfz uuuuu | 23 18 -18 -18 5 | 17 24
grg uuuuu | 26 1 -25 -19 3 | 33 36
igr xxxxx | 22 20 -60 104 -6 | -3 16
irf xxxxx | 29 -1 -36 233 -8 | -4 15
jpl uuuuu | 4 23 5 219 -6 | 19 25
mit uuuuu | 7 12 -126 -79 -13 | 24 28
ngs uuuuu | -68 28 52 -157 12 | 6 17
sio xxxxx | 50 -40 -33 255 -4 | 33 36
Table 7.1810.5 GPS week: 1810 Day: 5 MJD: 56919.500
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 1 -10 1 -4 | 20 26
emr uuuuu | 49 -32 -58 226 -2 | 15 28
esa uuuuu | 33 -25 84 11 3 | 22 27
gfz uuuuu | 28 -7 -61 -3 5 | 15 22
grg uuuuu | 25 -11 3 57 7 | 31 35
igr xxxxx | 14 6 4 20 1 | -6 18
irf xxxxx | 28 -12 1 151 -2 | -7 17
jpl uuuuu | 14 9 -62 81 -9 | 17 24
mit uuuuu | 10 -8 -95 -135 -8 | 21 27
ngs uuuuu | -35 53 123 -119 4 | 4 17
sio xxxxx | 44 -13 5 167 -9 | 30 34
Table 7.1810.6 GPS week: 1810 Day: 6 MJD: 56920.500
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 | -12 -11 -49 -45 4 | 19 26
emr uuuuu | 13 -21 110 211 -3 | 13 27
esa uuuuu | 19 -34 4 -17 0 | 22 27
gfz uuuuu | 14 -15 -172 82 5 | 15 22
grg uuuuu | -11 -30 68 -173 3 | 32 35
igr xxxxx | 33 -31 -6 138 -4 | -6 18
irf xxxxx | 17 -23 54 151 1 | -7 18
jpl uuuuu | -23 -14 -22 164 -16 | 17 24
mit uuuuu | -19 -2 -106 -265 -7 | 20 26
ngs uuuuu | 9 107 187 -53 6 | 5 17
sio xxxxx | 24 -46 65 176 -5 | 30 34
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