[IGSREPORT-27858] Wk 2150 IGS Final Orbits
acc
acc at igs.org
Fri Apr 9 00:47:01 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2150 (Mar 21, 2021 - Mar 27, 2021)
Contacts: acc at igs.org
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:
igs2150[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2150[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2150[0-6].cls IGS GPS clock combination summary report.
igs21507.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21507.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 | 11 DGAR FAIR MDVJ SAVO TIXI TIXI
0 | EMR | HOB2
0 | ESA | CHUR CPVG DGAR MAW1 NRIL PTBB CHUR CPVG MAW1 NRIL
0 | ESA | PTBB
0 | GFZ | DGAR MDVJ
0 | GRG | CPVG HOB2 JOG2 NYA2 SVTL SYOG BRST JOG2 NYA2 SVTL
0 | GRG | SYOG
0 | JPL | MCM4 CPVG FAIR MCM4 TRO1
0 | MIT | YEL2
1 | COD | ANKR OPMT TIXI ANKR TIXI
1 | EMR | YELL MDVJ OPMT YELL
1 | ESA | PTBB SCOR PTBB SCOR
1 | GRG | BAKE FAA1 HOB2 SVTL SYOG TIXI WIND SVTL
1 | JPL | CHUR MCM4 TIXI
1 | MIT | YEL2
2 | COD | SCUB SEYG SFER ULAB UNSA WIND SCUB SFER TIXI ULAB
2 | COD | UNSA
2 | EMR | MDVJ
2 | ESA | CHUR PTBB SFER ULAB CHUR PTBB SCUB SFER
2 | GFZ | SFER ULAB SCUB SFER
2 | GRG | HOB2 JOG2 KIT3 LPGS SCUB SFER SUTM SVTL TASH WIND
2 | GRG | WUH2 HOB2 JOG2 KIT3 LPGS SFER SUTM SVTL TASH ULAB
2 | GRG | WIND WUH2
2 | JPL | WIND KIT3 SEYG ULAB WIND
3 | COD | TIXI TIXI
3 | EMR | MAS1 MDVJ
3 | ESA | BAKE PTBB BAKE PTBB
3 | GRG | MAS1 NYA2 SVTL VOIM MAS1 NYA2 VOIM
3 | JPL | 11 BADG ZECK BADG OHI2 ZECK
4 | COD | KIT3 TIDB YELL TIXI
4 | EMR | CHUR HOB2 TIDB YELL
4 | ESA | BAKE CHUR LHAZ PTBB VILL BAKE CHUR PTBB
4 | GFZ | VILL ANKR KIT3 NYA1
4 | GRG | HOB2 JOG2 KIT3 SVTL HOB2 SVTL VILL
4 | JPL | NRMD NRMD
5 | COD | FAA1 KIT3 POVE TIXI TIXI
5 | EMR | 25 25 HOB2 HOB2 KERG
5 | ESA | HOB2 PTBB ANKR HOB2 PTBB
5 | GFZ | KIT3
5 | GRG | BAKE SVTL SVTL
5 | JPL | SYOG CHUR DAV1 MAC1 MCM4 SYOG
6 | COD | TIXI TIXI
6 | EMR | HOB2 HOB2 KERG
6 | ESA | HOB2 PTBB HOB2 PTBB
6 | GRG | MOBS JOG2
6 | JPL | WTZR
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 | SIO | 14
1 | SIO | 14
2 | SIO | 14
3 | SIO | 14
4 | SIO | 14
5 | SIO | 14
6 | SIO | 14
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .2 .1 .7 5 2 -1 -.20
EMR | 0 | 3.6 7.4 -7.7 -18 -11 1 .03
ESA | 0 | -.1 -1.8 -.1 -16 1 30 -.20
GFZ | 0 | -.3 .0 .4 19 -11 35 -.06
GRG | 0 | 3.4 -2.6 -18.1 -6 5 -5 -.19
JPL | 0 | 2.9 -.8 -.8 -15 -13 -25 .07
MIT | 0 | 6.4 .8 .1 -10 17 9 .03
NGS | 0 | 1.5 -5.9 -7.2 -3 32 35 .05
SIO | 0 | 3.5 -4.4 3.3 -68 -80 -16 -.13
COD | 1 | .2 -.1 .8 4 5 5 -.24
EMR | 1 | -.0 8.2 -13.7 -18 -8 -14 .11
ESA | 1 | -.2 -1.7 -.7 -13 25 16 -.19
GFZ | 1 | -.3 -.3 .5 13 2 31 -.20
GRG | 1 | 4.0 1.9 -14.9 -6 -7 -13 -.01
JPL | 1 | 3.0 -.4 -5.6 -8 19 2 .35
MIT | 1 | 3.4 4.6 -2.8 -10 12 14 .03
NGS | 1 | 4.7 -4.5 6.2 2 15 13 .09
SIO | 1 | 3.8 -1.0 3.4 5 -75 37 -.04
COD | 2 | .0 -.2 .8 2 11 4 -.19
EMR | 2 | 4.3 3.2 -13.4 -2 -13 -2 .26
ESA | 2 | -.2 -1.7 -.6 -15 13 -3 -.27
GFZ | 2 | -.1 .1 .5 10 -9 20 -.18
GRG | 2 | 6.6 -.1 -12.5 -13 -17 -14 -.11
JPL | 2 | -7.8 -3.0 -8.1 -7 3 -2 -.10
MIT | 2 | 4.2 3.9 -3.9 -1 25 -3 .11
NGS | 2 | -.1 -3.1 8.3 -22 -26 -3 .04
SIO | 2 | 5.0 2.0 3.7 46 -127 20 -.14
COD | 3 | .1 -.2 .8 2 8 2 -.16
EMR | 3 | 5.2 -1.6 -9.9 -7 -5 -8 .28
ESA | 3 | .1 -1.8 .4 -12 20 15 -.18
GFZ | 3 | .0 -.7 .7 -9 -3 19 -.12
GRG | 3 | 7.1 -4.7 -16.8 -4 -5 0 -.09
JPL | 3 | 9.6 -1.6 2.6 -18 -1 9 -.09
MIT | 3 | 6.1 1.0 -1.2 2 24 11 .07
NGS | 3 | 4.2 -1.6 .4 0 10 11 -.0
SIO | 3 | 5.0 -3.4 4.2 -66 -125 -30 -.18
COD | 4 | .0 -.1 .8 4 9 1 -.18
EMR | 4 | 1.6 3.5 -14.4 -15 1 -10 .17
ESA | 4 | .0 -.8 .1 -23 6 21 -.05
GFZ | 4 | -.4 -.7 .8 -4 0 26 -.12
GRG | 4 | 5.2 -1.3 -20.2 -11 -9 -29 -.02
JPL | 4 | 5.6 2.1 1.9 -1 -2 4 -.12
MIT | 4 | 7.2 -1.0 -5.2 6 11 1 .17
NGS | 4 | 1.8 .3 -5.3 3 17 11 .10
SIO | 4 | 6.3 -.6 -4.5 -3 -119 -22 -.21
COD | 5 | -.0 -.1 .4 1 5 2 -.09
EMR | 5 | -.5 8.5 -11.0 -11 3 -14 .11
ESA | 5 | .1 -1.1 .1 -21 6 19 -.21
GFZ | 5 | -.7 -.6 .5 -8 1 16 -.11
GRG | 5 | 4.4 1.3 -14.6 -14 -23 -8 -.10
JPL | 5 | -1.1 2.7 2.8 1 -5 16 -.04
MIT | 5 | 4.3 2.8 -2.9 6 4 4 .08
NGS | 5 | -5.9 1.7 8.3 30 -14 29 .06
SIO | 5 | 2.7 1.5 -.9 25 -68 -21 -.26
COD | 6 | -.2 -.3 .5 -5 8 2 -.05
EMR | 6 | 2.7 7.4 -7.2 -39 -13 -24 .11
ESA | 6 | .3 -1.2 .3 -30 7 12 -.05
GFZ | 6 | -.6 -.6 .9 -12 8 15 -.04
GRG | 6 | 5.6 -1.0 -8.1 -14 -14 -23 .14
JPL | 6 | 7.2 -3.3 -1.6 -17 -13 -4 .06
MIT | 6 | 6.8 1.8 -6.3 -1 13 -10 .22
NGS | 6 | 4.1 2.0 3.8 -6 -10 -32 .15
SIO | 6 | 5.1 2.7 -2.0 50 -99 -23 -.13
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
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 1.2150.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2150.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 2.2150.[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 3.2150.[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 5.2150.0-6). 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 2150 summary. (Mar 21, 2021 - Mar 27, 2021)
Table 1.2150.a GPS week: 2150 MJD: 59294.000-59300.000
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 735| 0 0 6 5 -5 -7 -.11 7 7 | -725 196 7 83
| 0 0 1 10 17 16 .02 | 194 253
emr 80| -4 4 -3 -10 17 -8 .19 13 13 | 205192 -522 14 89
| 1 1 1 20 10 9 .03 | 1669 924
esa 150| 0 0 0 8 0 15 -.01 7 7 | -1125 718 6 81
| 0 0 1 18 11 7 .02 | 739 884
gfz 236| 0 -1 3 11 -7 11 .11 10 10 | -430 -95 12 68
| 0 0 1 15 15 13 .03 | 333 594
grg 113| 2 -2 -8 5 5 -11 -.13 10 9 | -149 20 8 125
| 0 0 2 15 13 9 .03 | 112 254
igr n/a| 0 0 0 5 0 -5 .04 4 4 | 3283 -453 10 85
| 0 0 0 11 8 7 .01 | 1474 755
jpl 80| 0 0 0 -8 -2 0 .19 8 8 | 3213 -363 8 83
| 1 1 1 15 13 22 .02 | 1450 773
mit 357| 1 0 -2 -7 2 14 -.05 6 6 | 2557 -455 25 1646
| 0 0 1 24 25 14 .01 | 1563 777
ngs 216| 0 0 5 -2 21 -17 -.03 9 9 | -788 267 877 2036
| 0 0 3 18 12 13 .02 | 198 355
sio 410| 0 0 -5 -5 -20 -24 -.07 21 11 | --- --- --- ---
| 0 0 1 59 47 29 .01 | --- ---
Table 1.2150.b GPS week : 2150 MJD: 59294.000-59300.000
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 | 2 3 3 3 3 3 3 |
2 | 3 3 3 3 3 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 5 5 5 4 5 4 4 |
5 | 3 3 3 3 3 3 3 |
6 | 3 3 3 3 3 3 3 |
7 | 4 3 3 4 3 3 4 |
8 | 4 4 4 4 4 3 3 |
9 | 3 3 4 3 3 3 3 |
10 | 3 3 3 3 3 3 2 |
11 | 5 5 6 5 5 5 5 |
12 | 3 3 3 3 3 3 3 |
13 | 3 4 4 3 3 3 3 |
14 | 3 3 3 3 3 3 3 |
15 | 4 4 4 4 4 4 3 |
16 | 3 3 3 3 3 3 3 |
17 | 3 4 4 3 4 3 3 |
18 | 4 4 4 4 4 4 4 |
19 | 3 3 4 4 3 3 4 |
20 | 3 3 3 3 3 3 3 |
21 | 3 3 3 3 3 3 3 |
22 | 3 2 3 3 3 3 3 |
23 | 3 3 3 3 3 3 3 |
24 | 3 3 4 3 3 4 3 |
25 | 3 3 3 3 3 5 2 |
26 | 3 3 3 3 3 3 3 |
27 | 3 4 4 3 4 3 3 |
28 | 3 3 3 3 3 2 2 |
29 | 5 5 4 4 4 4 4 |
30 | 3 4 3 3 3 3 4 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 4 3 3 3 3 |
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 2.2150.0 GPS week: 2150 Day: 0 MJD: 59294.000
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 734| 0 0 7 0 -14 23 -.10 8 7 | -802 199 7 82
emr 80| -4 5 -2 -11 30 -7 .22 13 13 | 205243 592 15 103
esa 150| 0 0 0 6 -1 22 -.05 6 6 | -1426 888 7 81
gfz 212| 0 0 3 23 16 31 .15 11 9 | -547 -157 12 62
grg 112| 0 -2 -8 7 27 1 -.12 9 9 | -144 -235 8 122
igr n/a| 0 0 0 15 8 -9 .04 4 4 | 3398 405 9 87
jpl 80| -2 0 0 6 -4 -29 .18 8 8 | 3251 566 8 97
mit 357| 0 0 0 -16 -13 6 -.06 6 6 | 2634 458 23 1636
ngs 215| 0 0 1 11 32 -10 -.02 9 8 | -944 425 714 2202
sio 412| 0 0 -3 -29 -57 -62 -.08 21 11 | --- --- --- ---
Table 2.2150.1 GPS week: 2150 Day: 1 MJD: 59295.000
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 734| 0 -1 8 9 -13 -6 -.12 8 7 | -866 358 6 76
emr 80| -5 4 -5 1 32 -4 .18 13 13 | 206557 -43 14 102
esa 150| 0 0 0 30 19 12 -.01 7 7 | -56 -284 8 85
gfz 241| 0 -1 2 22 -6 13 .13 11 11 | 143 -969 12 72
grg 111| 2 -1 -6 25 15 -20 -.15 11 9 | -148 30 8 123
igr n/a| 0 0 0 8 6 -4 .04 4 4 | 4675 -227 10 87
jpl 80| -1 0 -1 -1 22 -6 .21 9 9 | 4533 -37 8 81
mit 357| 1 0 -1 -27 -12 -7 -.05 6 6 | 4083 -276 22 1809
ngs 221| 1 0 6 -1 1 -8 -.03 11 10 | -542 -351 877 2012
sio 411| 0 0 -4 -50 -60 14 -.08 21 11 | --- --- --- ---
Table 2.2150.2 GPS week: 2150 Day: 2 MJD: 59296.000
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 734| 0 -1 9 20 32 -18 -.14 8 7 | -949 560 7 87
emr 80| -4 4 -4 -20 6 -17 .19 12 12 | 206260 92 15 76
esa 150| 0 0 0 -1 -13 0 -.02 7 7 | -1004 527 7 103
gfz 238| 1 -1 0 -6 -9 5 .12 11 11 | -703 314 13 70
grg 114| 2 -2 -4 -10 -6 -23 -.14 11 9 | -352 215 8 123
igr n/a| 0 0 1 -7 0 -9 .03 4 4 | 4222 33 11 86
jpl 80| -2 0 0 -34 -14 31 .18 8 8 | 4235 147 9 88
mit 357| 0 0 -2 19 41 18 -.04 7 7 | 3682 32 29 1857
ngs 214| 0 1 7 1 16 -40 -.07 11 11 | -1144 847 744 2256
sio 409| 0 0 -7 31 -55 15 -.07 20 10 | --- --- --- ---
Table 2.2150.3 GPS week: 2150 Day: 3 MJD: 59297.000
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 739| 0 0 7 -3 -16 -21 -.10 7 7 | -652 25 9 90
emr 80| -4 2 -3 22 17 -12 .22 13 13 | 206652 -991 14 94
esa 150| -1 0 0 27 2 21 -.01 7 8 | -740 472 6 75
gfz 242| 0 -1 2 16 -3 15 .09 10 10 | -179 -121 13 70
grg 115| 2 -2 -12 24 10 -16 -.17 10 9 | -105 292 10 120
igr n/a| 0 0 0 12 4 -9 .03 4 4 | 4523 -849 10 97
jpl 80| 0 0 2 -6 7 27 .21 9 8 | 4559 -1074 8 61
mit 357| 0 0 -2 -18 -31 7 -.03 6 6 | 3776 -846 29 1598
ngs 216| 1 1 5 5 33 -6 -.06 9 8 | -719 152 703 1633
sio 411| 0 1 -7 -97 41 -39 -.06 24 11 | --- --- --- ---
Table 2.2150.4 GPS week: 2150 Day: 4 MJD: 59298.000
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 736| 0 -1 6 15 0 -24 -.13 6 6 | -804 331 6 77
emr 80| -4 2 -2 -27 14 -22 .22 13 13 | 205640 -1804 17 91
esa 150| 0 0 1 -1 6 13 .02 7 7 | -1569 1372 7 80
gfz 243| 0 0 2 -8 -5 20 .08 9 10 | -324 -743 12 71
grg 113| 2 -2 -10 0 1 -12 -.11 10 8 | 8 -413 10 128
igr n/a| -1 0 0 -3 0 -8 .03 4 4 | 3455 -1528 10 80
jpl 80| 0 3 2 -14 -15 -5 .18 8 8 | 3223 -1209 9 80
mit 357| 1 0 -2 11 -5 36 -.05 6 6 | 2677 -1624 30 1383
ngs 216| 0 1 1 -26 33 -18 -.01 9 8 | -783 290 1041 2101
sio 411| 0 0 -5 36 -36 -23 -.08 21 10 | --- --- --- ---
Table 2.2150.5 GPS week: 2150 Day: 5 MJD: 59299.000
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 736| 0 0 5 -10 -4 -2 -.11 7 6 | -648 125 7 89
emr 80| -2 5 -3 0 5 2 .18 14 12 | 203933 -1560 15 79
esa 150| 0 0 -1 20 -13 21 .01 7 7 | -2360 2239 7 70
gfz 241| 0 -1 2 30 -35 -8 .09 9 9 | -820 660 11 72
grg 114| 2 -3 -9 1 -1 -3 -.13 10 9 | -90 158 9 137
igr n/a| 0 -1 0 22 -14 -5 .05 4 4 | 2133 -1242 10 78
jpl 80| 0 1 1 10 -11 3 .20 8 8 | 2070 -1214 7 75
mit 357| 0 0 -2 -41 10 23 -.06 6 6 | 1335 -1173 24 1558
ngs 213| 0 1 10 19 17 -32 -.01 9 9 | -708 240 1283 2199
sio 409| -1 0 -6 -3 49 -37 -.07 22 10 | --- --- --- ---
Table 2.2150.6 GPS week: 2150 Day: 6 MJD: 59300.000
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 732| 0 0 5 7 -18 -5 -.09 7 7 | -360 -221 7 86
emr 80| -2 5 -2 -40 18 0 .14 13 13 | 202062 57 13 83
esa 150| -1 0 0 -21 -3 16 .00 8 8 | -723 -187 6 76
gfz 239| 0 0 6 2 -8 0 .09 8 8 | -585 350 11 65
grg 116| 1 -3 -5 -11 -10 -2 -.08 9 8 | -217 93 9 128
igr n/a| 0 0 0 -5 -8 12 .04 4 4 | 577 232 10 84
jpl 80| 0 0 0 -17 0 -18 .20 8 8 | 622 278 10 99
mit 357| 1 0 -4 20 27 19 -.05 6 5 | -284 244 22 1683
ngs 219| 0 1 6 -28 12 -5 -.02 9 8 | -676 267 782 1849
sio 409| 0 0 -6 77 -26 -35 -.10 19 11 | --- --- --- ---
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 3.2150.0 GPS week: 2150 Day: 0 MJD: 59294.000
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 8 7 7 6 3 6 4 5 10 2 | 22 28 24 26 23 24 27 20 22 21 23
2 | 8 8 6 9 8 3 8 5 9 11 2 | 20 24 21 23 22 22 21 22 25 22 21
3 | 8 9 6 8 5 3 8 5 6 10 2 | 21 31 24 25 22 24 28 22 22 24 23
4E | 12 20 10 18 12 5 10 11 19 17 5 | 59 62 60 61 60 59 61 60 63 59 59
5 | 5 11 6 9 4 6 9 5 7 11 2 | 39 45 43 42 40 43 45 40 38 39 41
6 | 6 9 6 9 7 4 7 4 7 13 2 | 30 33 32 33 33 31 35 31 28 29 31
7 | 10 13 7 11 11 4 8 6 6 19 3 | 37 37 33 35 35 34 36 35 37 32 34
8E | 9 19 4 8 11 3 12 6 10 12 3 | 36 40 37 39 39 37 39 36 36 38 37
9E | 10 16 6 13 9 3 9 5 11 10 3 | 76 73 75 74 75 75 71 75 78 73 75
10 | 6 8 7 11 5 3 6 4 7 10 2 | 30 37 35 37 33 34 37 34 35 33 34
X11E | 11 15 --- 15 10 8 12 13 10 --- 5 | 33 35 --- 35 32 35 36 25 33 --- 30
12 | 6 16 3 8 10 2 7 3 7 6 2 | 21 25 20 22 19 21 26 22 23 19 21
13E | 7 19 8 9 7 4 7 6 7 11 3 | 40 43 42 44 41 42 44 44 43 46 42
14 | 7 10 7 8 9 4 8 7 7 97 3 | 14 18 15 19 20 15 15 18 15 76 16
15 | 7 17 10 9 11 3 8 9 10 11 3 | 44 47 41 45 43 43 44 46 45 47 44
16 | 6 18 4 8 6 4 7 6 10 10 2 | 17 20 20 22 19 19 23 19 23 20 19
17E | 8 14 8 8 11 5 9 6 10 14 3 | 33 35 40 35 38 38 36 36 39 35 36
X18 | 11 13 10 9 11 6 9 7 9 --- 3 | 71 67 65 65 68 66 69 65 67 --- 67
19E | 8 14 7 9 14 4 7 6 9 10 3 | 50 49 45 51 50 47 48 47 47 46 48
20 | 7 12 6 10 6 3 7 7 9 12 2 | 24 31 27 28 25 26 28 23 24 25 25
21 | 6 13 5 10 9 3 8 6 6 11 2 | 15 19 15 21 18 16 19 17 15 18 16
22 | 8 10 5 12 8 4 7 5 4 11 2 | 17 24 18 21 19 20 23 20 20 23 19
23 | 7 11 6 13 8 4 10 7 8 10 3 | 73 70 71 73 71 70 70 71 75 73 71
24 | 7 12 6 15 8 4 7 4 6 8 2 | 49 54 51 49 50 51 52 50 51 48 50
25 | 6 11 7 8 10 3 7 4 10 7 2 | 18 24 24 20 19 20 26 21 21 21 21
26 | 7 8 7 7 5 4 9 7 6 9 2 | 15 21 19 18 16 18 23 15 20 16 17
27E | 7 16 5 8 8 4 10 6 9 12 3 | 39 43 40 41 41 40 44 39 40 41 40
28 | 7 12 3 7 5 3 8 6 6 10 2 | 15 24 17 21 21 19 24 19 18 20 19
29E | 15 19 7 26 18 6 9 9 12 11 5 | 59 60 55 60 57 56 57 60 60 59 57
30 | 10 12 7 9 7 3 6 7 7 19 3 | 20 26 23 22 21 21 24 18 21 22 20
31 | 5 10 6 8 7 4 7 6 5 9 2 | 42 42 41 46 40 42 45 40 43 40 41
32E | 6 11 6 10 12 4 10 7 9 8 3 | 33 34 31 33 35 32 35 30 32 32 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 6 11 9 4 8 6 9 21 |T 34 38 35 37 35 35 37 35 36 36 35
WRMS | 7 13 6 9 9 4 8 6 8 11 |NE 29 33 30 32 30 30 33 30 31 31 30
MEDI | 7 12 6 9 8 4 8 6 7 11 |MD 33 35 33 35 33 34 36 31 33 32 32
Table 3.2150.1 GPS week: 2150 Day: 1 MJD: 59295.000
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 | 5 9 7 9 8 4 6 5 6 9 2 | 28 33 28 29 27 28 31 26 27 28 28
2 | 8 11 8 9 10 4 8 6 7 12 3 | 24 29 26 26 25 26 25 25 27 26 25
3 | 7 7 7 9 5 4 8 6 8 8 2 | 18 28 23 21 18 21 27 16 19 18 20
4E | 11 18 11 13 16 6 11 10 17 15 4 | 38 38 40 37 35 37 41 40 42 41 38
5 | 4 8 8 9 6 5 11 7 11 13 3 | 24 31 27 29 25 28 31 24 30 22 26
6 | 6 8 7 8 8 5 6 5 10 11 2 | 33 38 35 35 34 35 35 32 35 34 34
7 | 8 15 6 9 10 4 9 8 9 13 3 | 35 37 34 35 35 35 36 36 36 34 35
8E | 12 23 5 12 10 4 13 7 11 14 4 | 51 54 53 51 54 52 52 52 55 54 52
9E | 9 8 7 11 6 4 7 7 15 10 3 | 68 68 68 70 68 68 66 66 67 67 67
10 | 7 7 7 9 5 3 10 4 12 12 2 | 24 29 28 29 24 27 28 25 25 24 25
X11E | 9 16 --- 11 12 8 8 12 10 --- 4 | 37 39 --- 37 36 32 38 27 34 --- 33
12 | 6 15 5 9 10 4 6 5 7 7 2 | 22 29 23 28 21 24 27 23 25 23 23
13E | 8 19 9 13 12 6 13 7 13 12 4 | 20 27 19 22 18 20 25 23 21 23 19
14 | 8 10 7 8 8 6 8 8 10 102 3 | 13 17 16 18 18 14 13 17 15 82 15
15 | 8 15 11 11 19 3 8 10 9 15 4 | 44 49 42 47 50 45 47 46 47 48 45
16 | 7 17 4 11 9 4 9 7 12 11 3 | 18 20 20 20 21 20 21 19 24 20 19
17E | 7 14 9 10 12 4 9 5 12 13 3 | 32 37 38 37 33 38 33 34 39 37 35
X18 | 13 12 9 8 14 5 8 7 11 --- 4 | 50 55 50 48 52 50 53 49 48 --- 50
19E | 9 11 8 10 16 5 7 5 9 12 3 | 48 47 45 47 48 47 44 46 49 47 46
20 | 8 11 6 10 7 3 7 5 13 13 3 | 21 23 21 22 19 20 22 22 19 23 20
21 | 6 18 6 10 9 3 6 6 7 10 3 | 20 26 21 25 23 22 22 22 21 24 21
22 | 7 7 5 7 8 4 7 6 6 7 2 | 14 21 16 17 14 17 21 14 15 16 15
23 | 8 8 7 11 8 3 11 7 11 11 3 | 53 54 54 55 54 53 53 52 56 54 53
24 | 9 9 7 9 11 3 7 4 9 11 3 | 46 52 48 48 47 47 49 47 49 49 48
25 | 7 10 8 16 11 5 7 3 10 6 3 | 18 25 24 30 20 23 26 21 21 21 21
26 | 6 9 7 12 7 4 7 7 12 7 3 | 17 24 21 20 19 20 25 16 22 18 19
27E | 11 18 6 10 20 5 13 5 14 11 4 | 42 48 44 44 49 45 45 43 50 46 44
28 | 7 10 3 9 5 5 8 6 8 6 2 | 17 26 20 23 19 21 25 20 22 20 20
29E | 12 17 10 21 19 7 10 7 11 9 4 | 55 55 55 56 55 53 56 53 53 55 54
30 | 10 12 6 9 11 4 8 6 10 17 3 | 24 30 26 25 25 25 29 25 28 30 26
31 | 6 11 5 11 10 3 8 5 9 7 2 | 40 42 39 43 40 40 43 38 38 39 39
32E | 7 7 7 14 12 4 10 6 12 9 3 | 39 43 42 45 40 42 42 40 45 41 41
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 7 11 11 4 9 6 11 21 |T 32 36 33 34 33 33 35 32 34 35 33
WRMS | 7 13 7 11 9 4 9 6 10 11 |NE 27 32 29 30 28 29 31 27 29 31 28
MEDI | 8 11 7 10 10 4 8 6 10 11 |MD 28 33 28 30 27 28 31 26 30 30 28
Table 3.2150.2 GPS week: 2150 Day: 2 MJD: 59296.000
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 | 5 7 7 13 6 5 8 6 8 6 2 | 18 26 22 24 18 20 26 19 22 21 20
2 | 9 11 9 11 9 3 8 5 10 14 3 | 19 22 21 25 22 21 23 22 20 26 20
3 | 5 9 7 11 5 4 8 6 9 10 2 | 17 28 23 22 17 19 27 16 16 17 19
4E | 9 19 9 18 16 6 11 12 16 14 4 | 54 54 54 50 53 52 53 53 58 51 52
5 | 5 9 8 8 7 5 8 6 11 8 2 | 30 35 34 33 29 34 36 31 34 33 32
6 | 7 7 7 9 9 5 6 4 13 10 2 | 22 27 25 24 22 24 26 22 21 23 23
7 | 7 11 6 11 10 4 9 6 8 11 3 | 28 31 26 30 28 29 33 31 32 29 29
8 | 11 21 6 10 10 5 11 7 11 13 4 | 48 51 51 52 47 50 54 49 50 50 49
9 | 7 10 7 15 14 4 8 7 12 9 3 | 35 37 35 35 37 35 38 36 37 36 35
10 | 7 6 6 12 6 3 6 6 13 10 2 | 28 33 30 34 29 32 36 28 33 26 30
X11E | 10 14 --- 19 11 8 13 11 22 --- 5 | 28 34 --- 28 32 27 36 24 28 --- 28
12 | 7 15 5 9 10 3 7 5 10 9 3 | 17 23 18 21 17 19 24 19 21 18 18
13E | 7 17 8 10 8 6 8 7 12 11 3 | 24 30 27 24 29 28 30 31 29 31 27
14 | 6 9 9 10 8 5 8 7 10 93 3 | 11 17 14 14 17 12 14 15 12 74 13
15 | 9 12 8 9 18 5 8 9 12 13 3 | 35 37 33 33 36 34 38 38 35 40 35
16 | 7 17 4 7 10 4 6 8 12 7 3 | 14 18 17 19 18 18 19 15 16 15 16
17E | 6 15 9 10 12 6 7 6 12 14 3 | 26 33 33 31 26 31 30 28 34 30 29
18 | 12 12 12 7 15 5 9 6 16 9 3 | 39 39 36 34 41 35 40 35 42 43 36
19E | 6 13 7 11 17 5 8 5 9 15 3 | 36 35 33 33 38 33 34 35 41 35 34
20 | 7 11 7 10 8 3 8 5 10 8 2 | 21 22 20 24 22 21 21 21 21 21 20
21 | 6 11 7 12 10 4 8 8 8 10 3 | 15 21 18 21 18 17 21 19 19 24 17
22 | 6 8 7 10 8 4 10 7 9 9 3 | 16 24 20 20 17 18 26 17 19 18 18
23 | 8 9 7 11 8 4 10 7 10 6 3 | 51 49 51 48 50 47 49 51 48 50 49
24 | 9 8 10 14 8 4 9 6 10 24 4 | 42 46 44 41 41 41 47 43 47 43 42
25 | 6 9 8 8 9 4 7 3 14 4 2 | 14 21 22 18 17 18 25 18 19 16 18
26 | 7 6 8 8 8 3 7 7 11 7 2 | 14 22 19 18 17 18 23 13 16 13 16
27E | 8 16 6 13 20 5 11 6 13 10 4 | 37 40 38 39 45 39 39 41 41 40 39
28 | 5 10 6 12 6 5 7 6 9 6 2 | 17 25 18 19 18 18 26 18 19 20 18
29E | 13 16 9 10 17 6 9 7 11 7 4 | 33 31 34 35 33 32 35 35 33 34 33
30 | 9 9 7 9 8 4 7 6 8 12 3 | 22 25 24 23 22 23 27 22 24 21 22
31 | 6 10 5 9 8 3 7 5 11 5 2 | 30 33 29 33 29 30 35 28 30 27 29
32 | 7 8 7 12 16 4 10 8 13 6 3 | 24 28 27 26 27 25 27 23 25 23 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 7 11 11 4 8 7 11 20 |T 27 31 28 29 28 28 31 28 29 30 27
WRMS | 7 12 7 11 9 4 8 7 11 10 |NE 23 28 25 26 24 24 29 24 25 28 24
MEDI | 7 10 7 10 9 4 8 6 11 10 |MD 24 30 27 26 27 27 30 24 28 27 27
Table 3.2150.3 GPS week: 2150 Day: 3 MJD: 59297.000
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 8 8 10 6 3 6 6 8 10 2 | 17 24 21 22 19 19 23 18 19 20 19
2 | 9 11 8 10 9 4 10 5 10 16 3 | 19 23 20 24 20 20 20 20 20 22 19
3 | 7 10 8 7 6 4 7 6 9 7 2 | 16 29 24 21 19 21 28 18 18 18 20
4 | 10 21 10 13 13 6 12 9 10 16 4 | 50 54 51 56 48 50 51 48 53 52 50
5 | 6 10 9 7 5 4 7 7 10 10 2 | 35 39 38 36 36 37 39 34 31 34 35
6 | 5 8 7 8 6 4 6 3 9 19 2 | 19 23 21 20 19 19 23 18 17 23 19
7 | 9 13 7 9 10 5 10 6 12 17 3 | 18 23 19 20 18 19 22 21 24 20 19
8 | 9 18 8 12 23 4 13 6 11 13 4 | 23 30 25 28 31 27 29 24 27 26 25
9 | 6 10 7 13 10 3 8 6 11 12 3 | 25 26 26 26 26 25 27 25 24 25 24
10 | 6 8 7 7 6 3 8 5 5 9 2 | 22 29 26 28 23 25 30 23 24 20 24
X11E | 11 14 --- 17 8 7 14 10 14 --- 5 | 31 35 --- 28 30 28 38 26 33 --- 29
12 | 5 13 5 8 7 4 8 4 7 9 2 | 17 21 15 17 15 17 23 18 18 17 17
13E | 7 18 8 8 9 5 11 6 8 11 3 | 24 30 25 23 23 24 30 25 25 24 24
14 | 5 9 9 8 9 5 8 7 6 114 2 | 16 19 16 18 19 16 16 18 13 95 16
15 | 7 19 8 10 18 4 8 9 10 17 4 | 22 28 22 22 25 21 24 23 23 25 21
16 | 8 19 6 8 8 5 6 6 8 9 3 | 15 21 15 17 14 15 17 15 17 15 15
17E | 7 14 7 9 10 4 8 5 10 17 3 | 26 30 30 31 30 30 28 27 32 32 28
X18 | 10 13 11 8 13 5 9 8 15 --- 4 | 43 43 38 41 40 40 44 40 47 --- 41
19E | 9 13 6 8 13 2 7 5 13 16 3 | 30 32 31 34 32 31 30 32 29 31 30
20 | 5 8 6 9 7 3 7 5 8 11 2 | 16 17 16 21 14 15 19 18 17 15 16
21 | 7 11 6 9 8 3 6 7 7 9 2 | 15 22 18 21 19 18 20 18 19 20 17
22 | 7 8 7 9 8 3 6 6 7 8 2 | 14 22 17 19 15 17 20 14 16 15 15
23 | 6 9 7 14 8 3 11 5 8 9 3 | 35 33 31 35 33 31 32 32 40 36 33
24 | 8 14 8 13 9 5 9 6 6 14 3 | 26 33 26 24 22 24 30 25 20 23 24
25 | 5 8 6 8 8 3 7 5 8 7 2 | 15 23 20 20 17 18 24 20 15 18 18
26 | 8 9 9 9 8 4 9 6 7 11 3 | 14 24 19 20 16 18 23 15 17 15 16
27 | 9 14 7 8 9 6 11 5 8 12 3 | 66 68 65 64 65 66 66 69 67 68 66
28 | 6 11 6 9 6 3 8 5 6 9 2 | 15 24 17 19 17 19 24 17 17 19 17
29E | 12 20 8 18 16 6 10 7 9 8 4 | 24 25 25 28 23 24 24 26 26 25 23
30 | 7 10 7 8 9 4 6 7 10 12 3 | 18 26 22 19 21 21 24 18 23 18 19
31 | 7 11 8 8 8 4 9 5 9 10 2 | 23 27 21 26 18 21 26 19 23 23 21
32 | 5 7 7 8 13 3 11 5 8 10 3 | 19 21 21 21 22 19 20 18 20 18 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 7 10 10 4 9 6 9 24 |T 24 28 25 26 24 24 27 24 25 27 24
WRMS | 7 13 8 10 9 4 8 6 8 11 |NE 20 26 21 23 20 21 25 21 21 24 20
MEDI | 7 11 7 9 8 4 8 6 8 11 |MD 19 26 22 22 21 21 24 20 23 22 20
Table 3.2150.4 GPS week: 2150 Day: 4 MJD: 59298.000
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 | 5 9 8 10 6 4 6 6 6 11 2 | 22 29 23 22 22 22 26 20 22 22 22
2 | 7 10 6 11 8 4 9 7 7 13 3 | 23 26 24 26 24 24 24 24 22 26 23
3 | 5 10 6 8 7 5 7 6 5 8 2 | 15 26 19 17 16 19 24 14 17 17 17
4 | 8 24 11 13 16 6 12 10 12 14 4 | 47 47 45 51 46 44 45 47 48 46 45
5 | 7 8 7 9 6 4 8 7 8 10 2 | 32 37 34 35 33 35 37 32 32 33 33
6 | 5 8 6 10 6 4 6 5 7 14 2 | 24 30 27 29 25 27 30 23 24 26 25
7 | 6 12 6 6 8 2 8 7 5 14 2 | 29 33 29 27 31 28 31 30 30 31 29
8 | 5 17 5 12 15 3 11 6 10 14 3 | 31 34 31 31 33 30 34 31 29 32 30
9 | 6 16 7 9 8 3 7 6 9 11 3 | 38 42 39 37 40 38 41 37 39 39 38
10 | 5 6 8 8 7 2 7 6 8 13 2 | 22 29 27 25 25 24 29 23 24 21 24
X11E | 10 11 --- 16 9 7 13 8 15 --- 4 | 30 34 --- 32 31 30 36 28 36 --- 31
12 | 5 14 6 7 9 3 6 4 7 9 2 | 20 25 22 24 18 22 26 21 22 20 21
13E | 7 11 7 11 7 4 8 6 8 14 3 | 20 23 21 23 20 21 25 24 23 23 21
14 | 5 9 9 10 9 5 9 7 9 96 3 | 14 24 19 20 20 18 20 20 18 80 18
15 | 9 11 8 11 16 4 8 9 13 20 4 | 38 42 36 40 39 39 41 39 40 45 38
16 | 7 19 4 7 9 4 7 7 10 9 3 | 18 22 19 22 19 20 21 19 20 19 18
17E | 6 16 5 10 19 5 10 6 10 11 3 | 32 32 33 35 27 33 30 30 36 34 31
X18 | 13 14 10 7 14 5 8 8 10 --- 4 | 49 47 44 46 45 44 48 46 44 --- 45
19E | 6 14 5 8 13 4 8 5 9 12 3 | 38 41 37 37 38 37 38 36 37 39 37
20 | 6 10 8 7 8 3 5 6 7 13 2 | 16 18 19 19 14 16 18 17 15 17 16
21 | 5 13 7 10 8 3 6 7 7 10 2 | 17 23 17 17 20 19 21 20 18 23 18
22 | 4 9 5 7 9 4 7 7 9 8 2 | 13 22 14 14 13 15 20 13 15 15 14
23 | 6 11 8 10 8 3 10 6 7 12 3 | 54 55 54 56 53 54 56 53 57 55 54
24 | 9 12 7 10 8 4 8 8 7 13 3 | 39 46 42 41 39 41 44 40 42 40 40
25 | 5 9 8 9 6 5 7 3 9 6 2 | 18 25 25 23 20 22 27 20 21 20 21
26 | 6 9 8 7 6 3 7 7 10 7 2 | 17 24 20 19 18 19 24 14 20 17 18
27 | 7 14 6 8 21 5 11 7 10 11 3 | 40 45 44 45 49 45 45 44 46 45 43
28 | 6 11 4 8 8 3 9 5 9 7 2 | 15 27 18 21 20 20 25 19 21 22 19
29E | 10 18 7 15 14 6 10 7 12 7 4 | 36 36 34 36 39 34 36 37 37 36 35
30 | 6 10 6 9 8 3 7 7 6 15 3 | 20 27 23 20 22 21 24 20 21 24 21
31 | 5 11 6 8 7 4 7 5 11 6 2 | 35 39 32 35 31 35 36 31 33 35 33
32 | 4 9 7 7 8 3 8 6 9 9 2 | 24 28 28 25 28 27 26 22 28 24 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 13 7 9 10 4 8 6 9 21 |T 27 32 29 29 28 28 31 27 29 30 28
WRMS | 6 13 7 10 8 4 8 6 8 10 |NE 25 30 26 27 25 26 29 25 26 28 25
MEDI | 6 11 7 9 8 4 8 6 9 11 |MD 24 29 27 26 25 27 29 24 24 26 25
Table 3.2150.5 GPS week: 2150 Day: 5 MJD: 59299.000
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 | 4 10 7 8 8 4 7 4 6 9 2 | 19 24 22 21 21 21 25 19 22 24 20
2 | 6 8 6 10 8 5 9 6 5 11 2 | 20 24 20 25 21 22 21 22 21 24 20
3 | 7 10 6 8 8 3 6 6 8 11 2 | 14 27 20 21 14 19 23 13 16 16 16
4 | 8 20 10 11 13 6 11 8 11 14 4 | 44 46 43 48 45 43 45 46 44 48 44
5 | 6 9 7 12 7 5 7 7 7 7 2 | 30 34 32 36 28 33 34 32 29 34 31
6 | 8 8 7 7 6 3 9 5 6 10 2 | 26 27 28 27 27 27 29 26 26 27 26
7 | 6 11 4 9 13 3 11 6 8 13 3 | 29 34 30 34 31 31 34 34 38 31 32
8 | 7 10 5 8 13 4 13 5 9 15 3 | 27 29 28 31 28 28 32 26 30 31 27
9 | 5 11 8 11 12 2 8 5 10 9 3 | 31 34 35 32 32 32 33 31 33 31 31
10 | 5 8 8 8 5 3 9 6 10 11 2 | 23 29 29 26 23 26 31 25 23 24 25
X11E | 10 15 --- 11 13 9 12 10 14 --- 5 | 27 34 --- 30 33 27 35 26 34 --- 29
12 | 7 14 4 9 9 4 6 3 7 7 2 | 19 24 18 20 16 20 22 18 22 18 18
13E | 7 9 7 8 5 4 8 5 9 10 2 | 24 27 26 26 26 26 28 28 23 29 25
14 | 7 9 8 7 9 4 7 7 6 109 3 | 12 16 13 17 16 10 12 14 10 88 12
15 | 6 12 5 11 14 4 8 8 15 8 3 | 29 30 29 27 36 30 34 33 34 33 30
16 | 7 19 5 6 9 5 6 6 9 12 3 | 15 18 17 18 15 17 18 16 19 15 15
17E | 7 14 8 7 13 5 9 5 9 15 3 | 35 34 39 33 34 37 34 35 38 38 35
X18 | 11 15 11 8 14 4 9 8 12 --- 4 | 45 46 44 43 46 44 47 45 47 --- 44
19E | 8 11 6 7 14 5 7 10 9 11 3 | 37 36 36 37 40 35 36 37 40 37 36
20 | 7 11 7 6 7 4 6 6 9 14 2 | 24 28 26 25 23 25 26 25 22 24 24
21 | 5 11 5 10 11 3 6 7 7 9 2 | 14 18 15 18 19 16 19 20 18 21 16
22 | 5 9 5 9 11 3 6 5 8 10 2 | 15 23 19 19 18 19 22 16 19 21 17
23 | 6 12 8 8 8 4 12 6 10 10 3 | 41 41 45 43 45 41 40 43 45 43 42
24 | 9 9 8 12 10 5 7 10 9 13 3 | 42 47 44 41 44 43 45 46 47 45 43
25 | 5 43 8 10 8 4 9 5 7 9 4 | 15 41 21 19 16 18 22 17 17 17 17
26 | 7 7 9 9 6 3 8 6 9 8 2 | 15 22 19 17 14 17 20 14 16 15 15
27 | 6 11 7 10 14 4 11 5 11 10 3 | 27 29 30 30 27 28 31 26 31 28 27
28 | 8 10 4 8 7 3 6 5 6 8 2 | 13 22 16 18 17 16 22 15 17 18 16
29E | 8 17 9 10 13 5 10 7 11 10 3 | 47 46 45 47 46 46 48 47 52 47 46
30 | 8 11 6 12 10 5 7 8 7 13 3 | 19 23 21 21 19 19 22 19 20 20 19
31 | 6 11 6 11 9 3 8 5 10 7 2 | 30 36 31 37 31 32 36 32 36 33 32
32 | 6 8 7 9 11 5 9 6 9 11 3 | 19 22 23 22 24 21 24 20 21 25 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 7 9 10 4 8 6 9 22 |T 25 30 27 28 27 27 29 27 28 30 26
WRMS | 6 12 7 9 9 4 8 6 9 10 |NE 23 28 25 26 24 24 27 24 25 28 24
MEDI | 7 11 7 9 9 4 8 6 9 10 |MD 24 29 28 26 26 26 29 26 23 27 25
Table 3.2150.6 GPS week: 2150 Day: 6 MJD: 59300.000
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 | 5 10 7 8 6 3 7 4 10 10 2 | 24 26 26 23 25 23 28 22 25 25 24
2 | 5 13 7 8 9 4 8 4 9 9 2 | 25 27 23 27 24 24 25 23 26 26 24
3 | 3 9 7 7 8 3 8 5 9 9 2 | 18 28 23 20 17 21 27 17 19 19 20
4 | 7 23 12 13 11 6 12 8 9 13 4 | 60 60 59 65 63 59 58 60 63 60 60
5 | 8 6 7 7 7 4 7 7 10 10 2 | 43 46 45 45 42 46 46 42 42 43 43
6 | 5 9 7 7 8 5 8 5 7 12 2 | 34 36 36 34 33 35 37 33 34 36 34
7 | 11 13 6 8 10 3 9 5 8 20 3 | 40 43 42 43 39 40 42 41 40 37 40
8 | 5 14 6 8 10 4 10 5 8 14 3 | 33 38 35 35 34 34 37 34 34 36 34
9 | 5 13 8 11 8 4 8 6 9 12 3 | 39 40 41 41 39 39 39 38 38 39 38
10 | 4 9 6 7 5 2 9 4 7 10 2 | 26 32 29 28 27 28 35 28 26 27 28
X11E | 10 17 --- 14 10 6 14 9 13 --- 5 | 30 39 --- 32 35 30 39 28 30 --- 31
12 | 6 17 5 6 7 3 7 5 7 8 2 | 22 26 21 25 23 24 28 25 26 23 23
13E | 7 13 7 8 7 5 8 6 9 9 2 | 37 39 36 38 39 38 38 39 36 41 37
14 | 6 8 8 6 8 5 9 7 8 90 2 | 20 23 19 21 23 18 19 22 15 67 20
15 | 7 15 7 8 13 4 10 8 10 10 3 | 40 42 38 39 44 39 42 43 41 43 40
16 | 8 22 6 5 9 4 7 6 8 10 3 | 18 21 22 22 19 21 22 21 19 22 20
17E | 7 12 8 7 10 4 7 6 10 11 3 | 37 38 42 38 36 40 38 37 40 39 38
18 | 9 17 15 13 13 4 10 7 9 12 4 | 79 76 72 77 76 75 79 76 78 45 76
19E | 11 12 7 7 14 2 7 7 10 15 3 | 50 49 49 54 52 49 49 48 52 50 50
20 | 6 10 8 7 6 4 6 5 7 11 2 | 24 27 25 27 23 25 25 23 22 23 23
21 | 6 13 6 7 9 3 7 5 10 8 2 | 17 18 17 17 19 17 20 20 21 22 18
22 | 5 7 7 7 9 3 8 4 9 8 2 | 16 22 18 17 17 17 21 17 19 18 17
23 | 5 11 7 8 7 4 11 5 7 8 2 | 66 64 65 66 68 65 66 67 70 66 66
24 | 7 11 7 11 8 3 8 11 7 12 3 | 56 58 57 54 57 56 60 60 60 56 57
25 | 5 9 6 7 6 3 6 5 9 6 2 | 20 30 24 22 22 23 26 23 21 23 22
26 | 5 7 9 5 6 4 7 6 9 8 2 | 16 23 20 20 17 19 23 16 20 19 17
27 | 6 16 7 9 10 3 9 5 8 11 3 | 38 44 42 41 42 40 42 40 39 40 40
28 | 6 9 5 6 5 3 8 4 6 11 2 | 17 25 18 20 18 19 24 20 18 23 19
29E | 6 17 10 10 11 6 10 7 11 7 3 | 66 64 63 66 66 63 65 64 61 66 64
30 | 11 11 7 9 8 5 8 7 7 19 3 | 24 28 25 26 24 24 28 24 23 27 24
31 | 5 11 6 8 9 4 6 4 9 6 2 | 40 42 39 41 40 40 44 39 43 41 40
32 | 5 9 6 8 10 3 8 4 8 8 2 | 21 25 26 24 26 23 23 23 22 24 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 8 9 4 8 6 9 19 |T 34 37 35 35 35 34 37 34 35 36 34
WRMS | 7 13 8 8 8 4 8 5 8 11 |NE 31 34 32 32 31 31 34 31 32 33 31
MEDI | 6 11 7 8 8 4 8 5 9 10 |MD 30 36 35 32 33 30 37 28 30 36 31
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2150 GPS week: 2150 MJD: 59294.0-59300.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 8 7 20 |U 11 15 43 |U 8 9 31 |
emr | emr 3072 |U 14 17 33 |U 15 24 58 |U 12 14 46 |
esa | esa 2976 | 12 14 33 |U 12 16 52 | 12 12 35 |
gfz | gfz 3071 |U 8 7 20 |U 11 14 42 |U 10 10 34 |
grg | grg 3072 |U 9 9 22 |U 11 15 43 | 9 11 34 |
igr | igr 3072 | 8 8 21 | 11 15 44 | 9 10 32 |
igs | igs 3071 | 8 7 22 | 11 15 44 | 9 10 31 |
jpl | jpl 3072 |U 11 13 29 |U 13 19 52 | 12 14 40 |
mit | mit 3072 |U 8 7 22 |U 11 15 44 |U 9 10 35 |
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 5.2150.0 GPS week: 2150 Day: 0 MJD: 59294.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 9 6 20 | 12 19 54 | 8 8 30 |
emr | emr 3072 | 17 16 29 | 17 36 71 | 17 11 35 |
esa | esa 2976 | 13 17 35 | 13 18 54 | 13 12 33 |
gfz | gfz 3072 | 9 7 20 | 12 18 51 | 9 7 33 |
grg | grg 3072 | 10 7 25 | 13 17 48 | 9 11 29 |
igr | igr 3072 | 9 10 24 | 12 19 51 | 10 8 28 |
igs | igs 3072 | 9 9 23 | 12 18 52 | 9 8 28 |
jpl | jpl 3072 | 12 20 31 | 13 24 57 | 12 7 29 |
mit | mit 3072 | 9 9 28 | 12 18 54 | 9 10 34 |
Table 5.2150.1 GPS week: 2150 Day: 1 MJD: 59295.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 5 17 | 7 15 29 | 10 10 34 |
emr | emr 3072 | 14 19 31 | 12 27 40 | 16 11 48 |
esa | esa 2976 | 13 14 36 | 8 15 41 | 13 14 41 |
gfz | gfz 3072 | 8 5 17 | 9 11 31 | 11 7 35 |
grg | grg 3072 | 9 7 22 | 6 16 38 | 10 12 32 |
igr | igr 3072 | 8 7 21 | 6 15 30 | 10 9 33 |
igs | igs 3072 | 8 6 21 | 6 15 31 | 10 9 34 |
jpl | jpl 3072 | 11 15 30 | 9 18 40 | 13 13 46 |
mit | mit 3072 | 8 6 19 | 7 15 32 | 10 10 36 |
Table 5.2150.2 GPS week: 2150 Day: 2 MJD: 59296.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 6 20 | 8 16 37 | 9 9 34 |
emr | emr 3072 | 13 19 32 | 13 29 50 | 12 12 47 |
esa | esa 2976 | 12 16 33 | 11 14 43 | 11 11 34 |
gfz | gfz 3072 | 8 6 20 | 10 12 38 | 11 11 40 |
grg | grg 3072 | 9 6 23 | 9 16 25 | 8 11 38 |
igr | igr 3072 | 8 8 20 | 9 14 38 | 10 9 35 |
igs | igs 3072 | 8 8 23 | 8 15 35 | 9 9 34 |
jpl | jpl 3072 | 11 15 30 | 10 18 40 | 11 11 39 |
mit | mit 3072 | 8 7 26 | 8 16 38 | 9 12 39 |
Table 5.2150.3 GPS week: 2150 Day: 3 MJD: 59297.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 7 16 | 16 15 51 | 6 9 28 |
emr | emr 3072 | 12 22 39 | 19 18 62 | 10 13 37 |
esa | esa 2976 | 12 12 27 | 15 17 62 | 10 10 31 |
gfz | gfz 3072 | 8 7 18 | 14 15 46 | 9 10 33 |
grg | grg 3072 | 9 12 18 | 15 15 48 | 7 9 27 |
igr | igr 3072 | 8 6 16 | 16 14 55 | 7 9 29 |
igs | igs 3072 | 8 7 16 | 15 15 50 | 7 8 27 |
jpl | jpl 3072 | 11 14 22 | 18 17 57 | 10 13 36 |
mit | mit 3072 | 8 6 17 | 17 16 51 | 7 10 30 |
Table 5.2150.4 GPS week: 2150 Day: 4 MJD: 59298.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 8 15 | 13 13 44 | 7 10 33 |
emr | emr 3072 | 15 17 31 | 15 21 58 | 11 15 52 |
esa | esa 2976 | 12 11 33 | 12 13 43 | 11 14 38 |
gfz | gfz 3072 | 6 10 16 | 13 12 44 | 9 11 35 |
grg | grg 3072 | 8 13 16 | 12 12 48 | 8 12 39 |
igr | igr 3072 | 7 7 19 | 13 13 42 | 8 12 34 |
igs | igs 3066 | 7 7 19 | 13 13 44 | 8 12 34 |
jpl | jpl 3072 | 10 8 27 | 13 17 48 | 11 22 48 |
mit | mit 3072 | 7 9 15 | 13 13 42 | 8 11 37 |
Table 5.2150.5 GPS week: 2150 Day: 5 MJD: 59299.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 9 9 29 | 11 19 32 | 11 13 33 |
emr | emr 3072 | 14 12 34 | 11 20 56 | 11 20 56 |
esa | esa 2976 | 9 14 38 | 10 21 51 | 12 13 35 |
gfz | gfz 3070 | 8 9 29 | 10 19 33 | 12 15 34 |
grg | grg 3072 | 7 9 25 | 11 18 38 | 11 13 38 |
igr | igr 3072 | 8 9 28 | 9 19 38 | 11 13 32 |
igs | igs 3072 | 8 8 28 | 10 19 38 | 10 12 31 |
jpl | jpl 3072 | 9 12 34 | 9 25 51 | 13 17 39 |
mit | mit 3072 | 9 9 29 | 10 19 34 | 11 12 35 |
Table 5.2150.6 GPS week: 2150 Day: 6 MJD: 59300.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 8 22 | 12 12 55 | 8 8 27 |
emr | emr 3072 | 16 12 34 | 17 16 72 | 9 15 47 |
esa | esa 2976 | 14 13 31 | 14 12 69 | 12 13 34 |
gfz | gfz 3072 | 11 6 22 | 12 11 54 | 9 9 30 |
grg | grg 3072 | 10 11 25 | 12 11 56 | 9 10 34 |
igr | igr 3072 | 11 6 22 | 12 11 57 | 10 9 30 |
igs | igs 3072 | 11 6 22 | 12 10 57 | 9 9 29 |
jpl | jpl 3072 | 13 11 30 | 15 14 67 | 12 14 40 |
mit | mit 3072 | 11 6 23 | 12 11 56 | 9 8 30 |
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 6.2150 GPS week: 2150 MJD: 59294.500-59300.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 -15 93 41 2 | 5 15
| 20 16 59 55 7 | 1
emr uuuuu | -27 -1 -91 81 -8 | 58 60
| 18 8 109 70 11 | 3
esa uuuuu | 8 -8 -5 -14 2 | 32 35
| 11 10 58 30 4 | 2
gfz uuuuu | 16 -29 73 72 -2 | 25 28
| 15 9 53 148 3 | 1
grg uuuuu | 12 4 80 87 0 | 5 12
| 11 11 34 40 3 | 1
igr xxxxx | 0 -2 20 -33 0 | 2 14
| 6 7 20 37 3 | 1
irf xxxxx | 14 1 -3 7 0 | 1 14
| 7 12 28 14 10 | 3
jpl uuuuu | 13 5 45 -46 -8 | 42 44
| 11 16 43 14 6 | 2
mit uuuuu | 2 5 -102 -38 2 | 17 23
| 12 18 62 16 11 | 4
ngs uuuuu | -51 46 -85 -109 -5 | 15 19
| 18 23 98 81 4 | 1
sio xxxxx | 75 -12 -12 -290 -17 | 60 63
| 24 54 86 34 14 | 3
Table 7.2150.0 GPS week: 2150 Day: 0 MJD: 59294.500
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 | 25 -8 33 18 -8 | 7 15
emr uuuuu | -42 -10 -25 46 -6 | 62 65
esa uuuuu | 25 -9 92 44 -4 | 30 33
gfz uuuuu | 7 -38 79 34 2 | 24 27
grg uuuuu | 10 -1 31 80 2 | 6 12
igr xxxxx | 11 -14 46 -18 0 | 2 14
irf xxxxx | 3 9 -17 -7 8 | -4 14
jpl uuuuu | 26 2 -14 -63 -9 | 45 46
mit uuuuu | -11 26 -119 -52 8 | 13 19
ngs uuuuu | -67 9 -33 -62 2 | 16 20
sio xxxxx | 48 70 -99 -230 -6 | 65 67
Table 7.2150.1 GPS week: 2150 Day: 1 MJD: 59295.500
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 | 22 -14 89 2 -3 | 4 15
emr uuuuu | -53 1 -39 -8 -14 | 59 63
esa uuuuu | -6 -19 31 -3 6 | 29 32
gfz uuuuu | 18 -33 56 63 -2 | 24 27
grg uuuuu | 25 -6 65 165 -4 | 4 12
igr xxxxx | -1 1 16 -28 0 | 0 14
irf xxxxx | 16 -7 -3 -17 14 | -4 14
jpl uuuuu | -6 8 45 -54 0 | 42 44
mit uuuuu | 5 8 -99 -52 16 | 12 18
ngs uuuuu | -27 65 -114 -27 -3 | 15 19
sio xxxxx | 71 -12 94 -307 1 | 61 64
Table 7.2150.2 GPS week: 2150 Day: 2 MJD: 59296.500
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 -33 55 109 0 | 6 16
emr uuuuu | 0 -8 60 30 -9 | 60 63
esa uuuuu | 17 -17 31 -22 3 | 32 35
gfz uuuuu | 2 -32 72 73 -2 | 27 29
grg uuuuu | 18 5 120 67 -1 | 6 13
igr xxxxx | -2 6 20 2 0 | 2 14
irf xxxxx | 22 20 -51 13 5 | 1 14
jpl uuuuu | 25 15 102 -29 -2 | 43 46
mit uuuuu | 8 30 -215 -47 9 | 17 22
ngs uuuuu | -57 38 -97 -192 -3 | 17 21
sio xxxxx | 107 -69 -48 -293 -19 | 64 66
Table 7.2150.3 GPS week: 2150 Day: 3 MJD: 59297.500
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 2 81 -28 6 | 5 15
emr uuuuu | -37 -6 -79 97 1 | 57 59
esa uuuuu | 9 -9 -69 -19 6 | 32 35
gfz uuuuu | 24 -24 59 191 1 | 26 27
grg uuuuu | 23 -1 70 99 -2 | 4 11
igr xxxxx | -1 5 23 -70 6 | 1 13
irf xxxxx | 8 3 -1 16 1 | 2 14
jpl uuuuu | 7 29 80 -36 -8 | 42 44
mit uuuuu | -16 -11 -70 -18 6 | 18 24
ngs uuuuu | -34 28 -29 -176 -9 | 16 19
sio xxxxx | 90 40 86 -264 -10 | 60 62
Table 7.2150.4 GPS week: 2150 Day: 4 MJD: 59298.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 4 -33 78 8 2 | 7 16
emr uuuuu | -17 5 -139 100 12 | 58 60
esa uuuuu | -3 -1 -37 -36 0 | 33 36
gfz uuuuu | 28 -12 104 271 -5 | 27 29
grg uuuuu | 12 10 59 79 4 | 5 11
igr xxxxx | 0 1 -17 17 -2 | 3 14
irf xxxxx | 20 3 -12 21 -8 | 5 14
jpl uuuuu | 20 -20 73 -61 -15 | 43 45
mit uuuuu | 5 6 -133 -30 -5 | 21 26
ngs uuuuu | -58 65 11 -215 -8 | 17 20
sio xxxxx | 97 -4 15 -299 -22 | 61 63
Table 7.2150.5 GPS week: 2150 Day: 5 MJD: 59299.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 8 216 69 10 | 5 16
emr uuuuu | -14 14 -284 91 -14 | 55 58
esa uuuuu | 8 -8 -59 -53 4 | 32 35
gfz uuuuu | 35 -27 -19 75 -3 | 25 28
grg uuuuu | -8 24 90 33 1 | 4 11
igr xxxxx | -1 -9 37 -78 -2 | 2 15
irf xxxxx | 10 -19 32 2 -11 | 3 15
jpl uuuuu | 13 -12 22 -45 -17 | 41 43
mit uuuuu | 21 -19 -53 -51 -11 | 20 25
ngs uuuuu | -75 43 -48 -41 -5 | 14 19
sio xxxxx | 42 -37 -131 -304 -22 | 57 60
Table 7.2150.6 GPS week: 2150 Day: 6 MJD: 59300.500
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 | 22 -26 97 109 11 | 6 16
emr uuuuu | -23 0 -133 211 -22 | 52 54
esa uuuuu | 4 9 -24 -12 -2 | 33 36
gfz uuuuu | -4 -38 158 -203 -6 | 24 27
grg uuuuu | 7 -6 124 87 3 | 4 11
igr xxxxx | -8 -6 14 -60 0 | 2 14
irf xxxxx | 17 -2 29 19 -12 | 3 15
jpl uuuuu | 9 12 4 -33 -5 | 38 41
mit uuuuu | 1 -5 -26 -19 -12 | 20 25
ngs uuuuu | -39 71 -285 -55 -7 | 14 18
sio xxxxx | 71 -75 -2 -333 -40 | 55 58
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