[IGSREPORT-28431] Wk 2191 IGS Final Orbits
acc
acc at igs.org
Fri Jan 21 04:49:56 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2191 (Jan 02, 2022 - Jan 08, 2022)
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:
igs2191[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2191[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2191[0-6].cls IGS GPS clock combination summary report.
igs21917.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21917.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 | BRFT DAV1 KIRU KIRU
0 | EMR | NLIB PERT
0 | ESA | DAV1 BAKE DAV1
0 | GFZ | 23 5 13 23 KIT3
0 | GRG | 22 DAV1 SVTL DAV1 KIT3 MAS1 SVTL
0 | JPL | MAW1
1 | COD | ABMF ASCG BOGT DARW INVK KIT3 MAYG MCM4 STJO SUTM
1 | COD | STJO
1 | EMR | BADG
1 | ESA | SGOC KIT3
1 | GFZ | 23 23 KIT3 SGOC STJO AREQ BAKO KIT3 MDVJ SGOC STJO
1 | GFZ | UNSA
1 | GRG | STJO SVTL SGOC STJO SVTL
1 | JPL | MCM4 BADG INVK MAC1 MAW1 MCM4 NYA1
2 | COD | INVK MAYG MCM4 SAMO SGOC
2 | ESA | DAV1 PTBB
2 | GFZ | 3 CKSV DAV1 GODE GOLD CKSV GODE GOLD KIT3
2 | GRG | 5 5 21 FLIN INVK SVTL
2 | JPL | DAV1 SVTL INVK MCM4 ZECK
3 | COD | 22 22 BRFT CRO1 DGAR NTUS REUN BRFT CRO1 DGAR
3 | EMR | CRO1 CRO1 NLIB
3 | ESA | CRO1 SAVO SVTL CRO1 SAVO SVTL
3 | GFZ | 23 23 GODE POHN REUN BRFT GODE POHN REUN
3 | GRG | CZTG DGAR MCM4 CZTG DGAR MCM4
3 | JPL | BADG MCM4 BADG MCM4
4 | COD | PIE1 PIE1
4 | EMR | BADG NLIB
4 | ESA | DAV1 DAV1
4 | GFZ | 5 23 5 23 DAV1 GODE LHAZ DAV1 GODE LHAZ
4 | GRG | GODE LHAZ MCM4 GODE
4 | JPL | BADG CPVG DAEJ
5 | COD | 5 5 CKIS MAYG
5 | EMR | 23 23 NLIB
5 | ESA | CZTG
5 | GFZ | 23 23 GODE POHN POHN ZAMB
5 | GRG | CKIS BRFT
5 | JPL | BADG BADG
6 | COD | ABMF AREG ASCG AUCK BOGT BRFT CPVG CRO1 GRAS HOFN
6 | COD | KARR MANA MAYG MCIL MCM4 NLIB POHN REUN SAMO SCUB
6 | COD | SGOC USUD WTZR WUHN
6 | EMR | 10 NLIB
6 | GFZ | 5 10 POHN POHN
6 | GRG | 3 10 SVTL BRFT SVTL
6 | JPL | 3 10 REUN BADG MCM4 REUN WTZR
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
1 | GFZ | ~04:30 | ~ -0.08 ns
4 | COD | ~11:30 | ~ -0.22 ns
5 | COD | ~07:30 | ~ 0.24 ns
6. 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.
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G09 | | | 4 | 4 | 4 | 4 | 4 |
PRN G14 | | | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
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.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .2 -.0 .0 0 2 -3 -.19
EMR | 0 | .6 -4.0 11.2 -28 -41 -29 .25
ESA | 0 | -.0 -.3 -.1 -35 -7 17 -.17
GFZ | 0 | .2 .0 .1 -2 -2 -2 -.02
GRG | 0 | 5.9 -4.5 5.8 -32 -8 -9 -.10
JPL | 0 | 9.3 .4 15.1 -3 -2 0 .02
MIT | 0 | 8.9 .3 20.3 18 2 -7 -.03
NGS | 0 | 3.5 .5 14.8 5 -32 14 -.12
SIO | 0 | 7.9 .1 25.9 27 -139 64 -.23
COD | 1 | .0 .1 .2 -3 0 -2 -.17
EMR | 1 | 5.6 -5.6 8.8 -30 -35 -22 .31
ESA | 1 | -.0 -.0 -.0 -27 -13 12 -.31
GFZ | 1 | .3 -.3 .2 1 -4 4 -.13
GRG | 1 | 11.2 -5.3 11.5 -17 7 -39 .11
JPL | 1 | 6.1 -1.1 9.6 -2 -3 1 .14
MIT | 1 | 7.9 -2.7 16.8 27 -7 -10 -.06
NGS | 1 | 3.2 -2.0 1.4 -22 -15 -7 -.18
SIO | 1 | 6.1 -2.1 22.3 -1 -145 67 -.25
COD | 2 | .1 .2 .4 0 -1 -2 -.13
EMR | 2 | 3.3 -3.4 6.4 -33 -24 -18 .23
ESA | 2 | -.6 .1 -.3 -33 -11 32 -.18
GFZ | 2 | .6 -.1 .5 4 -2 13 -.26
GRG | 2 | 6.4 -3.3 .1 -14 -15 -31 .03
JPL | 2 | 2.8 -4.3 8.2 1 0 0 .09
MIT | 2 | 5.2 -1.6 16.4 4 -17 -4 -.08
NGS | 2 | .8 2.0 6.5 -4 4 11 -.15
SIO | 2 | 3.0 -.9 20.3 -2 -103 44 -.40
COD | 3 | .2 .1 .3 -3 -1 0 -.13
EMR | 3 | 1.6 -6.7 8.1 -33 -14 -45 .37
ESA | 3 | -.5 -.0 -.4 -24 -16 16 -.10
GFZ | 3 | .5 -.3 .4 -1 -10 13 -.18
GRG | 3 | 1.3 -4.0 -1.4 6 -13 -32 -.06
JPL | 3 | 1.7 .2 5.4 0 0 0 .04
MIT | 3 | 3.2 -1.3 15.4 7 -4 -38 -.16
NGS | 3 | 1.3 -.1 -3.7 -29 14 24 -.23
SIO | 3 | -.9 .1 17.4 21 -27 -3 -.31
COD | 4 | .2 .2 .3 -3 -1 -1 -.17
EMR | 4 | 2.1 .7 10.7 -40 -10 -14 .08
ESA | 4 | -.8 -.4 -.5 -10 -17 26 -.26
GFZ | 4 | .4 -.6 .2 -3 -12 7 -.18
GRG | 4 | 1.6 -4.8 -1.9 7 -13 -29 -.07
JPL | 4 | 2.7 -2.5 12.1 -10 1 -2 -.24
MIT | 4 | 5.6 -.1 17.5 29 -17 -32 -.17
NGS | 4 | 1.6 -.8 10.2 18 -9 1 .0
SIO | 4 | -.8 2.1 27.4 73 -45 11 -.39
COD | 5 | .1 -.0 .3 -3 2 -4 -.21
EMR | 5 | 4.8 -3.2 11.2 -36 -24 -44 .14
ESA | 5 | -.6 -.3 -.3 -19 -3 12 -.34
GFZ | 5 | .4 -.2 .3 -5 -7 15 -.14
GRG | 5 | 4.8 -3.5 3.1 1 -9 -45 -.10
JPL | 5 | 6.1 -6.2 3.0 3 -3 2 .07
MIT | 5 | 8.7 -2.1 18.2 3 -7 -12 -.16
NGS | 5 | .1 1.2 7.2 -21 19 2 -.10
SIO | 5 | 3.4 2.0 24.0 59 -98 18 -.36
COD | 6 | .4 .2 -.0 -2 3 6 -.18
EMR | 6 | 5.7 -4.4 19.4 -62 -13 -35 .32
ESA | 6 | -.8 .2 -.3 -30 5 16 -.24
GFZ | 6 | .3 -.4 -.2 -16 -11 6 -.02
GRG | 6 | 1.0 .1 -1.2 9 -9 -42 -.06
JPL | 6 | .5 -1.7 11.7 -6 7 -12 .11
MIT | 6 | 7.2 -.9 15.1 12 3 -8 -.10
NGS | 6 | 1.1 1.3 11.5 3 -8 7 .03
SIO | 6 | .7 2.9 16.8 74 -37 31 -.35
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 1.2191.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2191.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 2.2191.[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 3.2191.[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 5.2191.0-6). 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 2191 summary. (Jan 02, 2022 - Jan 08, 2022)
Table 1.2191.a GPS week: 2191 MJD: 59581.000-59587.000
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 675| 0 0 1 8 0 6 .05 7 7 | -431 -243 5 116
| 0 0 1 13 11 15 .03 | 181 308
emr 80| -1 0 5 -3 -19 -9 .18 14 14 | 202912 562 16 94
| 2 1 1 20 9 11 .03 | 774 711
esa 149| 0 0 0 -12 -8 4 -.00 8 7 | -452 -221 7 100
| 0 0 0 12 13 14 .01 | 323 406
gfz 233| 0 1 0 -11 -14 3 .20 11 10 | 42 -47 12 201
| 1 0 1 12 12 14 .02 | 200 256
grg 112| 0 -4 -5 -5 1 0 -.12 11 10 | -75 63 9 144
| 0 0 4 12 14 12 .04 | 273 452
igr n/a| 0 0 -2 0 5 -9 .08 5 4 | -685 710 11 108
| 0 0 0 8 11 12 .02 | 1183 726
jpl 80| 0 0 4 -17 -7 -12 .16 10 10 | 464 559 8 98
| 1 1 2 12 12 17 .04 | 682 940
mit 371| 0 0 0 15 1 -6 -.19 8 7 | -2079 701 29 1699
| 0 0 1 15 15 27 .02 | 1284 750
ngs 208| 0 0 -2 -21 12 -8 .02 10 9 | -401 -222 743 1632
| 0 0 3 12 20 11 .02 | 204 264
sio 403| 0 0 -4 47 51 26 -.19 11 10 | --- --- --- ---
| 0 0 1 52 28 31 .02 | --- ---
Table 1.2191.b GPS week : 2191 MJD: 59581.000-59587.000
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 | 3 3 3 3 3 3 3 |
2 | 3 3 3 3 3 3 3 |
3 | 4 4 4 4 4 6 6 |
4 | 3 3 3 3 3 3 3 |
5 | 3 4 4 4 4 4 4 |
6 | 3 3 3 3 3 3 3 |
7 | 3 3 3 3 3 2 3 |
8 | 4 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 4 4 4 4 5 5 6 |
11 | 5 5 5 5 5 5 5 |
12 | 4 5 5 5 4 4 4 |
13 | 4 3 3 3 3 3 3 |
14 | 4 5 5 5 4 4 4 |
15 | 3 3 3 3 3 3 3 |
16 | 7 5 4 4 4 5 4 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 4 4 4 4 5 |
19 | 3 3 3 4 3 3 3 |
20 | 4 5 4 3 3 3 3 |
21 | 3 3 3 3 3 3 3 |
22 | 5 4 5 4 3 3 4 |
23 | 6 5 6 6 6 7 7 |
24 | 3 3 3 3 3 3 3 |
25 | 4 3 3 3 3 3 3 |
26 | 4 4 4 3 3 3 3 |
27 | 4 3 3 4 3 3 3 |
28 | 4 4 4 4 4 4 4 |
29 | 4 4 3 4 3 3 3 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 2 |
32 | 3 3 3 3 2 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 2.2191.0 GPS week: 2191 Day: 0 MJD: 59581.000
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 684| 0 0 0 -1 -10 -13 .01 8 8 | -727 69 6 95
emr 80| -3 0 3 17 -33 0 .13 14 14 | 201945 -128 19 79
esa 150| 1 0 0 -2 -18 0 -.02 7 7 | -605 -386 8 81
gfz 229| 0 0 0 -15 -24 8 .16 11 10 | -214 -135 13 170
grg 113| 1 -3 -1 6 4 -15 -.10 12 11 | -141 -393 8 129
igr n/a| 0 0 -1 7 -1 -3 .10 5 5 | -2246 131 12 89
jpl 80| 0 0 4 3 -19 -12 .17 10 10 | 31 -58 10 88
mit 371| 0 0 0 13 3 -1 -.18 10 8 | -3031 144 29 1391
ngs 204| -1 0 -2 -6 45 -1 -.00 9 9 | -745 107 956 2034
sio 375| 1 0 -7 -7 78 70 -.14 13 12 | --- --- --- ---
Table 2.2191.1 GPS week: 2191 Day: 1 MJD: 59582.000
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 682| 0 0 2 27 7 5 .02 8 7 | -302 -439 6 129
emr 80| 0 -1 4 0 -28 -28 .18 14 14 | 202199 963 19 112
esa 147| 0 0 -1 -29 -28 -23 .00 7 7 | -504 -89 7 123
gfz 238| -1 1 0 -32 -12 -27 .20 10 9 | 43 -73 12 595
grg 111| 0 -4 1 3 24 -8 -.13 12 12 | -225 543 12 158
igr n/a| -1 1 -2 -8 -1 -32 .08 4 4 | -1846 1126 11 138
jpl 80| 2 0 5 -25 -13 -7 .16 9 10 | 385 291 9 94
mit 371| 0 0 0 39 -6 35 -.20 8 9 | -3759 1198 27 1700
ngs 208| 0 1 -5 -18 27 -19 .02 10 9 | -374 -226 649 1410
sio 412| 0 0 -5 46 55 53 -.19 10 9 | --- --- --- ---
Table 2.2191.2 GPS week: 2191 Day: 2 MJD: 59583.000
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 677| 0 0 2 14 -5 -4 .03 6 6 | -224 -734 6 93
emr 80| -2 -2 4 13 -10 -17 .16 14 14 | 202902 318 18 82
esa 150| 1 0 0 -5 14 7 .01 7 7 | -388 -33 7 74
gfz 235| 0 2 0 0 -6 12 .20 12 10 | 161 -143 13 101
grg 115| 0 -4 -6 -7 11 -1 -.08 13 11 | 257 -154 10 143
igr n/a| 0 0 -2 4 16 -19 .11 4 4 | -941 556 12 94
jpl 80| 1 -2 4 -11 4 -46 .16 10 10 | 296 200 9 96
mit 371| 0 1 0 8 2 21 -.19 8 8 | -2780 600 26 1564
ngs 209| -1 1 -2 -15 16 10 .03 10 9 | -104 -635 523 1512
sio 411| 0 0 -4 7 0 21 -.21 10 9 | --- --- --- ---
Table 2.2191.3 GPS week: 2191 Day: 3 MJD: 59584.000
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 674| 0 1 3 18 -15 16 .06 7 7 | -416 -302 6 100
emr 80| -2 0 5 13 -7 8 .21 14 14 | 203262 -591 17 91
esa 150| 0 0 0 5 -5 13 -.00 8 8 | 203 -1021 7 76
gfz 234| 0 2 -2 -13 -19 17 .24 12 11 | 389 -425 14 95
grg 114| 1 -4 -6 6 -8 -5 -.19 11 10 | 252 -449 9 128
igr n/a| 0 0 -1 11 13 2 .07 4 4 | -272 -547 12 103
jpl 80| 0 0 5 -18 7 -10 .15 9 9 | 485 -807 8 117
mit 371| 0 0 2 5 34 -9 -.19 9 7 | -2123 -666 30 1777
ngs 209| 0 0 -8 -27 -17 -2 .04 12 10 | -296 -381 743 1591
sio 419| 0 0 -3 -1 51 -27 -.17 12 11 | --- --- --- ---
Table 2.2191.4 GPS week: 2191 Day: 4 MJD: 59585.000
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 670| 0 0 2 12 4 -3 .09 7 7 | -361 -239 5 128
emr 80| -2 0 3 -25 -16 -6 .19 13 13 | 202505 1271 15 119
esa 150| 0 0 0 -20 -7 22 .00 8 8 | -690 105 8 120
gfz 234| 0 1 0 -5 9 2 .19 11 11 | -161 387 12 121
grg 110| 1 -3 -8 -18 -8 8 -.13 11 9 | -517 751 10 148
igr n/a| -1 1 -2 -8 19 -8 .07 4 4 | -933 1623 12 117
jpl 80| -1 0 4 -35 0 12 .15 10 10 | -539 1998 8 102
mit 371| 0 0 1 35 -10 -19 -.20 8 7 | -2071 1517 28 1872
ngs 202| 0 0 -1 -43 13 -23 -.00 9 9 | -357 -237 886 1847
sio 399| 0 0 -3 93 41 12 -.19 11 9 | --- --- --- ---
Table 2.2191.5 GPS week: 2191 Day: 5 MJD: 59586.000
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 672| 0 0 1 -9 6 18 .10 7 6 | -630 194 5 128
emr 80| 0 0 5 -11 -16 -5 .22 13 13 | 203374 928 13 90
esa 150| 0 0 0 -13 -6 0 .00 9 8 | -782 176 8 111
gfz 231| -2 2 1 4 -15 3 .22 12 11 | 61 -108 13 139
grg 111| 1 -4 -6 -1 4 5 -.12 10 9 | -12 13 9 158
igr n/a| -1 1 -1 -6 0 -4 .08 5 4 | 286 1033 11 120
jpl 80| -1 0 1 -11 -5 -4 .09 11 11 | 993 921 9 86
mit 371| 1 0 0 0 0 -28 -.17 8 6 | -348 1158 32 1925
ngs 216| 0 0 0 -12 -5 -6 .03 11 9 | -573 110 604 1470
sio 402| 1 0 -4 63 46 18 -.21 11 10 | --- --- --- ---
Table 2.2191.6 GPS week: 2191 Day: 6 MJD: 59587.000
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 671| 0 0 0 -1 19 28 .04 8 6 | -361 -255 6 141
emr 80| 3 -1 9 -31 -24 -15 .19 14 14 | 204198 1176 12 88
esa 150| 0 0 1 -21 -8 12 .01 8 7 | -404 -304 8 115
gfz 230| -1 1 0 -15 -30 5 .19 10 10 | 16 162 11 192
grg 116| 0 -3 -11 -24 -16 22 -.09 11 9 | -142 136 9 144
igr n/a| -1 0 -1 -3 -9 2 .08 5 4 | 1154 1054 12 98
jpl 80| -1 -1 8 -24 -26 -17 .22 10 10 | 1597 1368 9 107
mit 371| 0 0 -1 3 -12 -44 -.22 8 6 | -443 957 34 1670
ngs 209| 0 0 0 -24 10 -15 .00 10 9 | -360 -297 846 1566
sio 409| 1 0 -4 131 88 35 -.21 10 8 | --- --- --- ---
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 3.2191.0 GPS week: 2191 Day: 0 MJD: 59581.000
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 7 11 10 3 10 5 10 10 3 | 32 35 34 34 29 34 33 31 33 37 32
2 | 6 11 4 10 10 4 7 6 5 13 2 | 33 33 37 42 35 36 34 32 37 39 35
3E | 11 12 9 10 14 4 10 8 13 10 3 | 53 38 55 54 54 53 53 55 53 58 53
4M | 7 11 5 8 9 6 11 7 12 11 3 | 80 81 80 80 82 83 78 81 84 92 81
5E | 8 11 8 10 14 7 10 8 8 10 3 | 39 45 44 45 44 44 45 42 47 44 43
6 | 6 13 7 8 7 3 8 7 6 8 2 | 36 38 36 39 33 36 38 33 36 37 35
7M | 5 10 7 11 8 4 7 5 7 10 2 | 46 50 46 52 42 48 52 46 48 49 47
8 | 7 14 8 10 8 5 12 10 10 13 3 | 31 35 33 33 31 33 34 31 33 34 31
9M | 9 10 8 8 8 6 8 10 9 9 3 | 49 52 47 51 46 48 52 48 50 52 48
10E | 9 12 7 15 10 5 10 8 8 14 3 | 71 73 71 70 70 72 71 69 73 72 71
X11 | 9 18 15 12 13 10 9 9 16 --- 4 | 60 58 55 60 63 57 60 56 62 --- 58
12 | 10 21 8 10 22 7 10 9 9 9 4 | 47 52 44 49 51 45 48 46 49 49 47
13 | 6 13 5 9 4 5 14 15 9 13 3 | 39 49 43 43 40 44 49 45 42 46 42
14M | 9 16 7 12 13 5 13 13 12 16 4 | 77 75 76 81 79 78 76 75 81 83 77
15 | 7 11 6 7 7 4 8 10 7 12 3 | 56 57 52 54 53 51 58 49 54 48 52
16M | 11 26 12 16 27 10 10 27 11 27 6 | 46 55 43 43 54 43 44 48 49 48 45
17 | 8 10 4 11 10 3 8 8 9 12 3 | 36 36 35 44 35 36 36 35 36 41 36
X18 | 9 17 12 12 10 5 9 8 10 --- 4 | 60 63 58 65 64 58 60 59 57 --- 59
19 | 7 17 5 11 10 3 7 7 8 13 3 | 36 36 40 43 35 39 38 36 39 41 37
20E | 11 9 7 10 13 9 8 12 6 12 3 | 68 68 69 67 69 68 68 63 68 66 66
21 | 6 13 6 11 11 4 9 5 7 13 3 | 31 32 30 35 28 32 32 29 33 38 30
X22E | 8 12 7 13 25 7 10 10 10 --- 4 | 69 70 71 74 67 69 68 66 71 --- 69
23E | 8 21 9 23 18 7 11 11 19 21 5 | 72 73 71 70 70 70 76 71 72 73 71
24 | 7 14 8 9 10 4 9 8 8 9 3 | 32 43 38 39 31 36 41 31 34 39 35
25 | 8 14 7 9 13 3 11 10 7 9 3 | 34 37 40 38 39 37 36 37 34 38 36
26M | 10 13 9 10 14 6 10 11 8 13 4 | 47 47 49 46 49 47 46 53 45 56 48
27 | 6 14 8 10 9 4 10 11 10 19 3 | 34 36 34 34 32 34 36 31 34 33 33
X28 | 9 11 5 12 12 6 7 6 10 --- 3 | 47 46 48 48 43 48 47 45 46 --- 45
29 | 10 21 7 7 14 4 7 9 13 9 3 | 39 42 39 39 38 40 41 38 43 39 39
30 | 6 10 4 9 7 3 9 6 6 14 2 | 31 40 34 35 29 35 38 31 33 39 33
31M | 7 9 6 8 4 4 8 8 9 12 3 | 42 47 45 43 43 43 48 43 39 43 43
32M | 4 10 7 8 7 4 10 8 5 9 2 | 36 43 40 39 35 41 43 38 38 43 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 7 11 12 5 10 10 9 13 |T 47 49 48 49 47 48 49 46 48 49 47
WRMS | 8 14 7 10 11 5 10 8 9 12 |NE 39 42 40 43 39 40 42 38 40 39 39
MEDI | 8 12 7 10 10 4 9 8 9 12 |MD 42 46 44 44 43 44 46 45 45 43 43
Table 3.2191.1 GPS week: 2191 Day: 1 MJD: 59582.000
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 7 8 9 3 10 7 7 7 2 | 27 29 29 28 24 28 29 22 27 26 26
2 | 7 15 5 12 10 3 7 6 6 7 3 | 27 26 27 31 24 27 25 26 26 26 25
3E | 13 9 8 10 14 4 9 10 9 12 3 | 35 24 32 34 29 31 32 28 31 34 30
4 | 6 10 5 7 10 5 11 6 8 11 2 | 54 54 55 55 53 55 54 55 56 59 54
5E | 9 12 9 10 14 6 9 9 8 10 3 | 32 29 31 31 33 29 28 28 29 32 28
6 | 5 11 8 8 7 4 7 5 7 7 2 | 33 35 34 33 29 33 35 30 31 32 31
7 | 5 10 5 6 8 4 6 6 9 5 2 | 22 25 24 28 22 24 26 23 23 26 23
8 | 6 9 7 9 11 4 9 9 8 9 3 | 28 31 33 31 30 32 31 27 27 31 29
9 | 5 9 9 6 9 4 10 7 8 6 2 | 90 88 88 88 90 89 88 87 89 86 88
10E | 11 10 8 9 14 5 9 8 9 12 3 | 35 36 31 34 30 32 32 32 33 34 31
X11 | 10 16 15 14 15 6 11 9 14 --- 4 | 42 47 44 42 44 43 43 41 42 --- 42
12 | 9 25 8 11 22 5 12 6 8 13 4 | 27 31 24 29 27 25 28 24 26 27 24
13 | 5 13 6 10 6 4 13 8 7 10 3 | 33 40 35 34 33 35 39 33 34 35 33
14 | 10 17 10 16 12 6 11 15 16 12 4 | 96 96 94 101 91 96 95 91 98 96 94
15 | 6 9 6 8 9 4 9 7 7 8 2 | 39 42 36 38 38 38 39 36 37 39 37
16 | 8 25 11 11 16 6 10 12 9 15 4 | 29 36 27 37 33 29 28 31 34 34 30
17 | 8 9 5 7 11 3 8 8 8 7 2 | 27 25 21 29 24 24 28 23 24 27 24
X18 | 10 16 12 9 14 6 12 8 11 --- 4 | 37 41 37 37 37 36 39 38 34 --- 36
19 | 8 15 5 10 10 4 8 6 9 8 3 | 30 32 29 33 27 31 31 27 30 31 28
20E | 6 12 9 10 20 5 8 5 27 13 4 | 67 71 72 71 71 71 68 66 73 67 68
21 | 10 13 6 7 13 3 8 6 9 6 3 | 29 29 28 32 22 29 30 24 30 28 27
X22E | 10 10 7 7 24 5 9 11 12 --- 4 | 66 69 67 68 72 68 68 66 67 --- 67
23E | 10 22 9 20 17 6 13 12 18 17 5 | 30 35 34 35 35 32 34 32 35 35 31
24 | 7 10 6 8 8 3 10 6 10 13 3 | 25 35 31 32 25 29 34 24 27 28 27
25 | 7 11 6 9 12 3 9 7 11 9 3 | 27 30 30 30 30 28 30 25 28 27 27
26 | 12 13 9 10 11 7 9 13 9 16 4 | 29 33 34 31 33 30 31 30 29 36 30
27 | 6 9 8 7 13 3 9 7 7 9 3 | 31 34 34 35 31 33 31 27 28 28 30
X28 | 8 12 6 16 9 5 11 6 10 --- 3 | 46 50 50 51 47 49 50 46 49 --- 48
29 | 9 19 6 7 16 5 9 7 9 8 3 | 28 32 29 29 31 30 31 29 30 28 28
30 | 5 10 5 6 6 3 9 7 7 6 2 | 25 34 29 28 25 28 33 26 28 33 27
31 | 6 10 6 7 6 4 7 10 8 7 2 | 40 45 42 40 38 41 43 38 40 41 40
32 | 5 10 7 9 9 2 9 5 11 7 2 | 18 25 18 19 16 19 24 15 18 20 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 7 10 12 4 9 8 10 10 |T 37 40 38 39 37 38 39 35 37 37 36
WRMS | 7 14 7 9 12 4 10 9 9 9 |NE 31 34 32 33 30 32 33 29 31 29 30
MEDI | 7 11 7 9 11 4 9 7 9 9 |MD 30 34 32 33 31 31 32 29 30 32 30
Table 3.2191.2 GPS week: 2191 Day: 2 MJD: 59583.000
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 8 7 8 5 8 5 11 9 2 | 35 37 38 34 35 36 38 33 32 36 34
2 | 6 15 6 14 9 4 7 5 8 9 3 | 37 34 38 42 35 36 36 34 38 35 35
3E | 9 11 8 22 14 5 10 9 12 11 4 | 26 29 28 27 25 26 27 26 25 28 25
4 | 5 10 4 9 10 5 11 7 11 7 2 | 49 48 49 50 52 49 50 50 51 52 50
5E | 5 11 9 12 32 5 10 8 11 7 4 | 40 39 40 42 43 39 41 38 42 39 39
6 | 4 12 7 8 6 4 7 8 7 9 2 | 36 38 39 41 35 37 39 35 37 37 36
7 | 5 11 7 7 8 3 5 8 10 5 2 | 45 45 44 46 42 44 45 42 44 43 43
8 | 6 9 8 10 8 4 10 10 11 7 3 | 34 38 36 32 35 35 36 34 35 34 34
9 | 6 10 8 8 7 5 6 6 8 8 2 | 187 187 186 188 185 184 187 185 184 184 186
X10E | 7 --- 8 9 19 5 11 7 9 9 3 | 33 --- 34 38 30 33 35 33 35 34 33
X11 | 10 16 16 15 12 10 11 9 15 --- 4 | 45 46 41 45 45 43 46 44 49 --- 44
12 | 9 27 7 17 20 7 11 6 11 11 4 | 47 47 41 44 44 41 46 43 44 48 43
13 | 4 15 7 12 8 3 12 10 8 11 3 | 45 51 47 45 46 46 53 45 47 48 46
14 | 8 17 11 16 12 4 13 12 16 8 4 | 189 190 190 196 190 191 190 190 191 191 190
15 | 5 7 6 7 8 4 10 8 6 10 2 | 51 52 49 52 49 49 55 49 52 49 50
16 | 6 27 9 11 14 6 10 12 8 12 4 | 42 49 40 44 43 41 46 45 43 45 42
17 | 6 11 5 8 9 6 9 7 8 9 2 | 31 32 31 34 31 33 32 30 30 34 30
X18 | 8 14 13 8 12 5 12 8 8 --- 4 | 46 47 43 44 47 43 46 47 42 --- 44
19 | 7 17 6 11 9 5 10 7 11 7 3 | 37 35 38 42 36 39 37 36 38 38 36
20E | 4 13 9 13 21 3 9 8 12 15 4 | 60 60 60 62 63 59 60 59 59 61 59
21 | 6 12 5 7 23 4 9 5 11 8 3 | 35 39 37 36 43 37 39 36 35 37 36
X22E | 7 11 7 15 18 8 10 12 18 --- 4 | 90 91 90 89 88 88 91 89 87 --- 89
23E | 9 22 10 25 20 7 12 13 16 17 5 | 31 33 35 40 34 31 34 29 31 30 31
24 | 5 13 7 7 9 3 13 5 9 10 3 | 34 42 35 35 32 35 45 34 36 37 35
25 | 6 10 7 7 11 4 10 7 6 7 2 | 35 35 36 34 34 33 37 33 30 34 33
26 | 5 17 8 11 9 5 11 10 6 13 3 | 45 47 44 42 43 44 48 45 40 46 43
27 | 7 9 7 7 8 3 9 9 7 9 3 | 41 43 43 38 42 41 44 41 40 41 40
X28 | 8 11 5 18 10 5 12 8 8 --- 3 | 48 48 47 53 47 47 51 48 48 --- 47
29 | 5 18 7 7 12 4 9 8 8 11 3 | 35 35 32 34 34 35 36 33 34 34 33
30 | 5 11 5 8 9 2 9 8 7 8 2 | 31 38 33 30 31 33 38 30 31 34 32
31 | 4 13 6 8 5 4 10 6 8 7 2 | 62 67 61 60 61 62 68 61 62 63 62
32 | 5 9 6 10 7 3 9 7 5 9 2 | 29 33 28 30 26 29 32 25 28 25 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 14 7 12 13 4 10 8 10 10 |T 50 53 51 52 50 50 53 50 50 50 50
WRMS | 6 14 7 10 11 4 10 8 9 9 |NE 39 40 39 39 38 38 41 38 38 38 38
MEDI | 6 12 7 9 9 4 10 8 8 9 |MD 40 43 40 42 42 39 44 38 40 37 39
Table 3.2191.3 GPS week: 2191 Day: 3 MJD: 59584.000
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 8 8 7 3 7 5 17 11 3 | 42 44 45 43 41 43 44 42 40 40 41
2 | 6 15 6 12 9 2 7 7 10 8 3 | 43 43 45 48 42 44 41 43 47 41 42
3E | 9 13 8 18 11 5 9 11 9 12 4 | 46 36 46 50 44 45 45 46 46 43 45
4 | 5 11 5 9 10 3 10 7 10 10 3 | 55 56 55 58 58 55 55 55 60 53 55
5E | 10 13 9 7 13 6 7 13 19 14 4 | 48 50 47 47 45 47 47 47 53 47 46
6 | 6 11 8 9 7 3 6 6 8 11 2 | 47 52 50 51 46 49 48 47 49 47 47
7 | 4 13 6 9 7 3 7 7 8 10 2 | 46 48 46 46 41 44 46 44 43 40 44
8 | 7 8 8 10 8 5 9 9 13 11 3 | 42 46 43 43 43 43 42 42 43 42 42
9 | 9 9 8 7 9 3 8 8 9 11 3 | 339 341 339 342 343 341 340 338 339 333 339
10E | 10 11 10 21 19 6 10 7 10 9 4 | 55 59 54 54 53 54 56 55 54 55 54
X11 | 10 18 17 14 14 7 10 11 12 --- 5 | 48 50 46 49 50 46 47 51 49 --- 47
12 | 10 22 8 14 20 6 8 7 13 12 4 | 41 44 38 41 44 40 41 39 40 40 39
13 | 7 13 6 12 6 5 12 7 9 14 3 | 41 48 43 40 43 42 47 40 44 40 41
14 | 8 16 11 16 13 6 12 9 17 14 4 | 210 211 210 217 212 212 212 208 212 212 211
15 | 7 8 5 9 8 4 6 8 6 12 2 | 53 54 51 50 48 50 55 50 48 49 50
16 | 7 24 9 8 15 7 9 12 11 15 4 | 42 48 41 44 40 42 44 48 44 47 43
17 | 8 13 7 12 11 4 7 5 9 11 3 | 46 49 46 50 46 46 46 46 48 43 45
X18 | 9 15 13 10 14 6 9 9 7 --- 4 | 53 58 49 56 56 53 55 55 55 --- 53
19 | 8 17 5 14 12 3 9 6 12 8 3 | 43 46 47 51 45 46 44 45 47 44 44
20E | 6 13 8 10 10 3 7 6 12 12 3 | 42 46 44 44 43 43 40 40 43 40 41
21 | 6 10 7 9 9 4 7 6 13 8 3 | 42 46 44 45 44 42 45 42 40 42 42
X22E | 10 12 8 16 13 7 8 10 17 --- 4 | 40 38 39 46 39 38 39 36 39 --- 37
23E | 8 21 11 22 16 7 12 17 23 20 5 | 57 56 56 57 56 55 54 57 54 55 54
24 | 6 11 8 9 10 4 11 8 9 13 3 | 41 50 42 47 38 45 50 42 43 40 42
25 | 8 11 8 6 9 3 8 9 10 5 3 | 43 46 43 44 44 43 46 41 41 40 42
26 | 7 12 8 8 9 5 8 12 7 14 3 | 44 45 42 43 41 43 45 46 40 47 43
27 | 8 10 7 19 10 5 9 8 8 13 3 | 43 45 44 45 42 43 43 42 42 43 42
X28 | 7 15 7 16 10 6 9 10 16 --- 4 | 53 54 57 56 54 53 54 55 54 --- 53
29 | 7 20 8 10 12 5 8 8 10 13 3 | 43 47 42 46 45 44 44 44 46 43 43
30 | 6 11 5 7 8 2 9 8 8 12 3 | 45 51 48 47 45 47 49 45 45 44 46
31 | 4 10 7 8 6 3 8 7 9 8 2 | 46 49 46 46 42 45 48 45 44 45 45
32 | 5 9 6 7 7 3 7 6 9 9 2 | 50 52 48 49 45 48 51 48 46 47 48
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 12 11 4 9 9 12 12 |T 60 62 60 62 59 60 61 60 60 60 59
WRMS | 7 14 8 11 10 4 9 7 10 11 |NE 44 48 45 47 45 45 46 45 45 42 44
MEDI | 7 12 8 10 10 4 8 8 10 11 |MD 45 48 46 47 44 45 46 45 46 43 44
Table 3.2191.4 GPS week: 2191 Day: 4 MJD: 59585.000
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 6 6 3 10 5 9 9 2 | 24 26 25 22 21 23 26 20 21 21 22
2 | 8 12 6 10 8 3 8 5 9 8 2 | 22 22 23 27 20 22 19 19 23 22 20
3E | 7 12 9 20 9 6 12 7 11 13 4 | 44 42 43 41 42 41 40 41 44 38 41
4 | 5 10 7 8 8 4 11 7 6 6 2 | 54 53 52 53 55 52 51 50 54 52 52
5E | 7 11 8 8 20 5 11 10 10 13 3 | 34 34 34 34 39 35 34 35 36 36 33
6 | 6 11 8 10 6 3 7 6 6 10 2 | 27 28 29 29 25 28 29 24 25 25 26
7 | 6 12 6 8 7 4 7 6 10 8 2 | 29 32 28 31 26 28 33 27 30 28 28
8 | 6 8 8 9 8 4 8 9 9 10 3 | 21 22 23 20 20 20 21 19 22 18 19
9 | 6 13 8 6 6 3 8 7 7 7 2 | 418 418 419 421 420 419 422 417 418 414 419
10E | 10 11 10 23 19 6 12 8 14 10 4 | 29 30 27 25 27 27 30 27 30 26 26
X11 | 10 16 16 13 13 7 11 7 16 --- 5 | 29 34 28 29 33 29 31 29 34 --- 29
12 | 8 22 8 7 20 5 11 7 8 10 4 | 28 29 21 27 30 22 28 22 24 23 23
13 | 5 12 7 8 7 3 12 6 12 10 3 | 25 33 24 24 26 26 33 25 28 26 25
14 | 8 18 11 11 12 6 11 10 15 14 4 | 294 298 297 299 294 297 295 294 295 292 295
15 | 6 7 6 5 10 4 9 7 8 9 2 | 35 38 33 34 32 32 37 32 36 33 34
16 | 7 25 9 9 14 6 10 11 9 13 4 | 28 35 26 28 26 26 29 34 34 33 29
17 | 8 13 8 9 9 4 7 7 9 7 3 | 32 32 29 32 29 29 31 27 32 29 29
X18 | 9 15 13 9 11 6 11 10 9 --- 4 | 37 41 36 39 39 36 40 41 38 --- 38
19 | 8 17 6 11 8 2 8 5 9 9 3 | 20 21 20 25 17 20 21 18 22 22 19
20E | 5 15 9 10 10 6 10 8 5 14 3 | 33 34 34 34 32 33 35 35 34 37 33
21 | 7 10 6 8 9 5 6 7 10 8 2 | 19 21 20 22 22 21 22 19 24 21 20
X22E | 6 7 9 13 9 6 8 6 8 --- 3 | 47 49 48 52 46 48 50 46 51 --- 48
23E | 11 17 13 22 12 6 14 15 19 24 5 | 42 42 42 38 41 39 42 45 39 46 40
24 | 4 10 6 9 9 3 12 6 7 14 3 | 17 29 18 25 14 20 30 13 16 19 17
25 | 8 10 10 7 10 3 8 6 6 7 2 | 20 22 22 20 21 20 23 19 18 18 19
26 | 7 11 9 7 8 5 9 11 8 13 3 | 26 29 28 27 26 26 30 30 26 29 27
27 | 7 10 8 7 8 4 10 9 7 11 3 | 25 26 25 26 22 25 24 22 25 21 23
X28 | 8 12 7 16 10 4 9 11 8 --- 4 | 33 35 33 36 31 33 35 34 33 --- 32
29 | 7 18 7 9 10 6 7 6 5 10 3 | 22 19 17 23 21 21 19 18 22 17 19
30 | 4 10 4 11 7 3 10 8 6 11 2 | 16 27 18 20 14 18 26 13 16 16 16
31 | 6 8 6 7 6 4 8 6 7 9 2 | 46 45 44 47 41 44 47 44 42 46 44
32 | 6 8 6 7 7 3 7 4 6 8 2 | 21 26 21 22 20 20 23 15 20 17 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 11 11 4 10 8 9 11 |T 49 52 49 51 49 49 51 48 50 50 48
WRMS | 7 13 8 11 9 4 10 7 9 9 |NE 25 28 24 26 24 24 27 23 25 22 23
MEDI | 7 11 8 9 9 4 9 7 8 10 |MD 28 32 28 28 26 27 30 27 30 26 27
Table 3.2191.5 GPS week: 2191 Day: 5 MJD: 59586.000
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 8 7 5 7 4 7 8 2 | 22 24 25 23 21 24 25 18 20 18 21
2 | 6 11 6 7 10 2 6 4 9 7 2 | 23 23 25 28 20 24 22 23 25 23 22
3E | 8 13 9 33 12 6 20 8 19 11 5 | 45 38 46 53 46 46 49 46 47 47 45
4 | 5 11 6 6 9 5 10 6 8 9 2 | 54 52 55 59 57 55 57 57 56 60 56
5E | 6 11 11 15 13 5 7 10 18 14 4 | 33 33 34 29 30 30 32 39 40 39 33
6 | 5 9 7 11 7 4 7 5 8 11 2 | 25 30 27 27 24 27 29 22 24 24 24
7 | 5 11 6 8 7 4 7 5 8 5 2 | 26 30 26 30 24 27 28 24 27 25 25
8 | 7 8 7 11 7 4 10 9 9 11 3 | 21 21 23 20 22 20 18 18 22 18 19
9 | 4 7 8 7 6 3 7 6 7 7 2 | 502 504 501 504 502 503 503 499 501 493 501
10E | 11 13 10 20 22 6 15 11 12 11 5 | 55 57 56 58 50 55 54 53 56 50 53
X11 | 7 18 17 11 12 7 10 6 16 --- 4 | 42 45 43 42 43 40 43 40 40 --- 41
12 | 8 22 7 9 17 3 9 7 9 8 3 | 32 37 26 30 31 28 30 27 30 29 28
13 | 5 12 8 11 6 3 11 5 8 16 3 | 20 31 18 19 19 21 29 20 22 22 20
14 | 9 18 12 15 12 6 13 8 13 11 4 | 379 382 383 390 381 382 382 381 380 379 382
15 | 5 7 12 9 10 3 9 6 9 13 3 | 32 34 37 30 30 31 34 29 34 30 31
16 | 7 29 7 11 12 7 10 11 10 12 4 | 29 41 27 30 29 27 30 34 35 31 30
17 | 7 12 6 8 9 3 9 6 6 7 2 | 32 33 29 37 32 32 32 31 34 33 31
X18 | 9 13 16 11 10 7 10 8 10 --- 4 | 47 51 49 49 51 47 48 49 47 --- 48
19 | 7 16 5 6 9 4 8 5 8 7 2 | 25 28 26 28 23 26 26 25 27 28 25
20E | 5 14 7 9 9 4 9 6 11 11 3 | 43 42 41 42 41 42 42 40 45 43 41
21 | 7 9 7 9 9 5 8 7 9 6 2 | 19 20 20 24 21 21 21 16 19 18 18
X22E | 8 10 9 10 7 6 9 6 10 --- 3 | 60 63 61 61 60 61 61 58 60 --- 60
23E | 12 18 20 17 13 8 21 20 26 26 6 | 69 69 68 69 70 68 66 70 78 75 68
24 | 4 13 6 7 6 3 14 5 5 12 2 | 18 32 21 22 16 23 32 18 20 20 20
25 | 6 10 9 5 9 2 6 4 9 6 2 | 23 25 27 27 25 25 26 24 24 24 24
26 | 8 15 10 9 7 7 10 10 7 10 3 | 26 29 27 32 26 26 28 29 26 27 26
27 | 8 8 9 10 7 5 9 9 6 14 3 | 21 22 22 26 19 20 20 18 22 18 19
X28 | 7 13 6 15 9 6 8 8 8 --- 3 | 25 30 29 32 24 29 29 28 31 --- 27
29 | 7 16 8 7 11 6 10 6 9 13 3 | 28 27 26 29 26 26 22 25 27 29 26
30 | 5 11 5 8 5 3 11 7 7 8 2 | 23 32 24 26 22 24 31 22 22 23 23
31 | 5 10 7 12 4 5 10 5 6 9 2 | 63 64 61 64 61 62 63 63 64 62 62
32 | 4 8 7 10 7 3 8 5 9 9 2 | 21 26 23 26 20 22 24 18 23 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 9 12 10 5 11 8 11 11 |T 58 61 59 61 58 59 60 58 60 61 58
WRMS | 6 13 8 11 9 4 11 6 9 10 |NE 26 30 27 28 26 27 28 25 27 23 25
MEDI | 7 11 7 9 9 5 9 6 9 10 |MD 28 32 27 30 26 27 30 28 30 28 27
Table 3.2191.6 GPS week: 2191 Day: 6 MJD: 59587.000
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 8 8 7 4 9 4 9 7 2 | 28 30 30 27 29 28 30 26 28 29 27
2 | 7 13 6 11 8 3 9 6 9 8 3 | 27 29 31 34 28 30 27 29 30 27 28
X3E | 15 --- 9 25 15 8 14 13 18 14 6 | 44 --- 42 43 44 40 48 45 39 45 41
4 | 6 12 5 6 10 6 10 5 6 14 3 | 79 76 79 80 82 81 80 80 80 86 80
5E | 9 12 9 11 13 4 9 8 10 9 3 | 54 52 52 53 55 53 56 55 53 56 53
6 | 6 12 8 9 6 3 8 6 5 9 2 | 37 36 36 35 34 35 35 33 35 33 34
7 | 4 9 6 8 8 4 7 6 8 7 2 | 39 43 38 42 34 37 43 37 38 37 38
8 | 8 11 7 10 7 3 11 7 10 5 3 | 23 25 25 23 24 23 25 21 25 24 22
9 | 7 9 9 8 7 3 8 7 5 8 2 | 617 617 617 619 619 617 616 614 615 606 616
10E | 19 20 12 13 23 6 19 13 19 16 6 | 92 94 90 91 91 91 93 94 93 94 91
X11 | 10 16 16 12 11 6 11 7 15 --- 4 | 61 64 61 61 64 59 63 62 64 --- 61
12 | 8 24 8 8 18 5 8 8 7 11 4 | 35 42 30 33 34 30 36 31 33 32 32
13 | 5 13 6 9 5 5 12 6 10 10 3 | 26 36 26 27 28 28 38 29 32 29 28
14 | 8 18 11 13 11 5 12 9 18 11 4 | 485 489 487 499 488 489 489 487 483 487 488
15 | 6 9 7 9 10 4 9 6 7 11 2 | 44 49 46 45 41 45 50 41 45 44 44
16 | 4 26 7 9 12 7 10 9 12 6 3 | 30 41 27 32 32 27 31 34 36 33 31
17 | 8 11 8 8 8 3 11 5 12 8 3 | 30 30 30 36 31 32 32 30 35 31 30
X18 | 10 16 15 10 8 6 11 13 9 --- 4 | 64 68 64 68 67 64 67 65 65 --- 64
19 | 8 13 6 11 9 3 9 5 9 6 3 | 25 24 29 31 24 27 27 24 26 27 25
20E | 6 12 9 10 11 5 8 8 10 11 3 | 73 72 74 75 74 74 74 71 77 75 73
21 | 8 9 5 8 9 5 7 9 8 8 2 | 23 25 23 26 24 23 24 22 25 25 22
X22E | 4 14 9 8 11 7 8 5 15 --- 3 | 88 91 89 89 88 89 88 85 90 --- 88
23E | 12 22 15 21 24 10 19 24 16 30 7 | 72 69 68 69 74 67 69 72 70 69 68
24 | 6 15 6 7 8 3 12 7 9 10 3 | 18 34 22 25 16 22 34 15 22 18 20
25 | 6 10 8 6 10 3 7 7 6 8 2 | 23 25 27 27 26 24 25 22 23 22 23
26 | 7 14 9 8 7 6 8 8 6 7 3 | 30 33 31 31 30 29 33 35 29 33 31
27 | 6 10 6 8 6 4 12 7 7 8 2 | 23 27 25 27 26 25 27 23 25 26 24
X28 | 10 12 5 12 8 5 8 9 16 --- 3 | 33 34 33 36 32 35 35 33 37 --- 33
29 | 6 17 8 6 11 3 9 6 6 9 3 | 30 31 29 31 31 30 31 29 31 28 29
30 | 4 10 5 7 6 3 10 7 6 8 2 | 21 32 22 26 21 23 31 22 20 21 22
31 | 4 10 5 6 5 4 7 4 5 4 2 | 85 88 87 87 85 86 88 85 86 87 86
32 | 5 11 7 8 8 3 8 6 5 7 2 | 38 41 37 39 34 36 39 35 38 37 36
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 8 10 11 5 10 8 10 10 |T 74 78 75 77 75 74 77 74 75 77 74
WRMS | 6 14 7 10 9 4 10 6 9 8 |NE 31 35 32 34 32 32 35 30 33 27 31
MEDI | 6 12 8 8 8 4 9 7 9 8 |MD 35 41 33 36 34 35 36 34 36 33 33
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 4.2191 GPS week: 2191 MJD: 59581.0-59587.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 |U 9 7 27 |U 15 19 57 |U 21 14 43 |
emr | emr 3044 |U 17 14 55 |U 22 29 74 |U 20 22 47 |
esa | esa 3072 | 12 10 43 | 16 19 69 | 25 20 57 |
gfz | gfz 3072 |U 9 9 33 |U 14 18 59 |U 20 15 47 |
grg | grg 3070 |U 10 15 34 |U 14 17 60 |U 20 17 55 |
igr | igr 3071 | 9 7 27 | 15 18 57 | 22 13 44 |
igs | igs 3066 | 9 10 26 | 16 18 63 | 20 17 44 |
jpl | jpl 3072 | 16 12 48 |U 17 21 66 | 22 23 63 |
mit | mit 3072 |U 7 7 20 |U 16 17 59 |U 18 17 37 |
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 5.2191.0 GPS week: 2191 Day: 0 MJD: 59581.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | ---- ---- ---- | 10 6 24 |
emr | emr 3072 | ---- ---- ---- | ---- ---- ---- | 15 17 41 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 15 14 45 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 9 8 32 |
grg | grg 3071 | ---- ---- ---- | ---- ---- ---- | 6 11 26 |
igr | igr 3072 | ---- ---- ---- | ---- ---- ---- | 10 9 32 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 9 8 29 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | 13 12 46 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 8 8 25 |
Table 5.2191.1 GPS week: 2191 Day: 1 MJD: 59582.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 7 24 | 16 24 71 | 76 34 145 |
emr | emr 3072 | 17 16 52 | 21 31 78 | 51 38 107 |
esa | esa 3072 | 13 11 43 | 16 22 79 | 74 57 122 |
gfz | gfz 3072 | 10 10 38 | 16 24 65 | 58 39 137 |
grg | grg 3072 | 9 18 37 | 15 22 62 | 75 58 140 |
igr | igr 3072 | 9 6 27 | 15 23 66 | 81 32 125 |
igs | igs 3072 | 9 6 28 | 15 22 61 | 71 56 127 |
jpl | jpl 3072 | 17 12 44 | 18 21 74 | 63 74 192 |
mit | mit 3072 | 8 7 22 | 15 20 48 | 69 60 110 |
Table 5.2191.2 GPS week: 2191 Day: 2 MJD: 59583.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | 15 16 56 | 11 8 24 |
emr | emr 2976 | ---- ---- ---- | 22 25 78 | 14 20 38 |
esa | esa 3072 | ---- ---- ---- | 16 16 67 | 17 13 55 |
gfz | gfz 3072 | ---- ---- ---- | 14 13 59 | 12 9 37 |
grg | grg 3072 | ---- ---- ---- | 15 11 55 | 11 8 49 |
igr | igr 3072 | ---- ---- ---- | 14 14 58 | 11 9 28 |
igs | igs 3072 | ---- ---- ---- | 14 14 54 | 10 9 29 |
jpl | jpl 3072 | ---- ---- ---- | 17 17 54 | 12 15 39 |
mit | mit 3072 | ---- ---- ---- | 13 10 44 | 8 7 21 |
Table 5.2191.3 GPS week: 2191 Day: 3 MJD: 59584.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | 23 17 51 | 11 14 28 |
emr | emr 3072 | ---- ---- ---- | 31 25 72 | 12 20 32 |
esa | esa 3072 | ---- ---- ---- | 26 18 67 | 13 11 41 |
gfz | gfz 3072 | ---- ---- ---- | 22 19 58 | 13 10 27 |
grg | grg 3071 | ---- ---- ---- | 23 16 58 | 10 13 47 |
igr | igr 3072 | ---- ---- ---- | 25 16 54 | 9 11 30 |
igs | igs 3072 | ---- ---- ---- | 24 16 56 | 9 11 31 |
jpl | jpl 3072 | ---- ---- ---- | 26 20 63 | 12 11 40 |
mit | mit 3072 | ---- ---- ---- | 22 14 48 | 10 13 27 |
Table 5.2191.4 GPS week: 2191 Day: 4 MJD: 59585.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | 15 27 64 | 14 10 22 |
emr | emr 3072 | ---- ---- ---- | 23 31 64 | 16 22 34 |
esa | esa 3072 | ---- ---- ---- | 17 25 73 | 19 16 44 |
gfz | gfz 3072 | ---- ---- ---- | 14 23 62 | 15 11 24 |
grg | grg 3072 | ---- ---- ---- | 12 21 66 | 11 9 39 |
igr | igr 3072 | ---- ---- ---- | 15 23 63 | 13 11 27 |
igs | igs 3072 | ---- ---- ---- | 15 23 64 | 13 11 26 |
jpl | jpl 3072 | ---- ---- ---- | 17 23 69 | 15 15 37 |
mit | mit 3072 | ---- ---- ---- | 15 20 61 | 12 12 22 |
Table 5.2191.5 GPS week: 2191 Day: 5 MJD: 59586.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | 10 16 43 | 13 10 25 |
emr | emr 3072 | ---- ---- ---- | 18 29 66 | 16 16 39 |
esa | esa 3072 | ---- ---- ---- | 11 16 56 | 19 13 45 |
gfz | gfz 3072 | ---- ---- ---- | 7 12 47 | 18 10 27 |
grg | grg 3072 | ---- ---- ---- | 8 14 54 | 13 11 43 |
igr | igr 3072 | ---- ---- ---- | 10 15 44 | 14 8 28 |
igs | igs 3072 | ---- ---- ---- | 10 15 44 | 13 9 29 |
jpl | jpl 3072 | ---- ---- ---- | 14 21 54 | 18 15 39 |
mit | mit 3072 | ---- ---- ---- | 15 21 50 | 11 9 25 |
Table 5.2191.6 GPS week: 2191 Day: 6 MJD: 59587.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 8 30 | 10 15 55 | 15 14 31 |
emr | emr 2976 | 17 12 57 | 19 31 85 | 17 19 41 |
esa | esa 3072 | 11 10 43 | 10 18 73 | 19 19 50 |
gfz | gfz 3072 | 8 7 27 | 11 15 61 | 15 18 48 |
grg | grg 3066 | 11 12 32 | 10 18 65 | 12 10 41 |
igr | igr 3071 | 9 7 27 | 9 16 57 | 15 13 36 |
igs | igs 3032 | 9 13 24 | 17 18 98 | 13 13 37 |
jpl | jpl 3072 | 16 11 52 | 12 23 85 | 19 22 50 |
mit | mit 3072 | 7 8 19 | 18 18 104 | 9 8 31 |
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 6.2191 GPS week: 2191 MJD: 59581.500-59587.500
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 -4 -17 -15 2 | 5 26
| 14 17 70 47 7 | 4
emr uuuuu | -3 15 -78 43 2 | 15 32
| 42 23 111 71 13 | 5
esa uuuuu | -1 2 -27 -71 2 | 17 30
| 12 10 112 41 2 | 4
gfz uuxuu | 2 20 -9 -92 1 | 26 36
| 22 17 230 138 6 | 4
grg uuuuu | 10 -13 -91 19 -2 | 10 25
| 36 14 36 70 4 | 4
igr xxxxx | -11 -7 21 -10 0 | 4 26
| 11 6 107 35 6 | 4
irf xxxxx | -1 -6 49 -6 -5 | 4 27
| 12 13 32 30 7 | 4
jpl uuuuu | -1 27 -40 -14 -2 | 13 31
| 33 16 65 80 21 | 4
mit uuuuu | -8 -33 159 41 -3 | 29 39
| 30 16 77 50 10 | 4
ngs uuxuu | 6 6 13 133 -2 | 12 27
| 62 37 207 86 4 | 4
sio xxxxx | 60 -44 76 17 -8 | 49 56
| 68 47 118 92 11 | 5
Table 7.2191.0 GPS week: 2191 Day: 0 MJD: 59581.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 19 23 68 51 2 | 2 18
emr uuuuu | 70 45 -291 156 -19 | 16 27
esa uuuuu | 11 -10 73 -44 3 | 13 21
gfz uuxuu | -15 -6 154 -357 -6 | 23 30
grg uuuuu | -32 -4 -75 -66 -10 | 8 17
igr xxxxx | -9 -15 184 -44 0 | -1 20
irf xxxxx | 17 -3 70 38 6 | 3 17
jpl uuuuu | 38 9 -124 49 22 | 5 20
mit uuuuu | 23 -25 130 137 16 | 25 30
ngs uuxuu | -98 -10 -209 53 -7 | 10 20
sio xxxxx | 158 -50 242 -28 6 | 50 53
Table 7.2191.1 GPS week: 2191 Day: 1 MJD: 59582.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -1 -21 -136 -7 5 | 8 23
emr uuuuu | 36 -9 56 82 -3 | 20 30
esa uuuuu | 7 5 117 -92 0 | 20 29
gfz uuxuu | -29 31 109 -145 2 | 29 36
grg uuuuu | -43 -38 -61 -76 -3 | 13 22
igr xxxxx | -3 -4 155 39 7 | 7 24
irf xxxxx | 8 14 42 25 -14 | 9 24
jpl uuuuu | 7 53 -54 -88 10 | 15 30
mit uuuuu | 41 -13 55 74 -8 | 33 41
ngs uuxuu | -40 -17 -69 309 -7 | 16 26
sio xxxxx | 126 17 189 -84 -18 | 57 61
Table 7.2191.2 GPS week: 2191 Day: 2 MJD: 59583.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 14 2 -63 -62 -2 | 12 24
emr uuuuu | -23 10 -7 43 -10 | 21 31
esa uuuuu | -19 -3 57 -24 2 | 23 30
gfz uuxuu | -2 3 142 -52 -3 | 32 38
grg uuuuu | 30 -27 -117 33 1 | 16 23
igr xxxxx | -18 -13 -20 30 0 | 11 24
irf xxxxx | -8 -10 67 14 -7 | 10 24
jpl uuuuu | -10 39 -72 -33 9 | 20 32
mit uuuuu | -15 -32 142 38 5 | 35 42
ngs uuxuu | 30 13 -108 140 0 | 18 26
sio xxxxx | 68 14 59 189 3 | 56 61
Table 7.2191.3 GPS week: 2191 Day: 3 MJD: 59584.500
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 0 -9 -74 -1 | 1 29
emr uuuuu | -26 -2 -125 6 21 | 8 32
esa uuuuu | -16 -12 -25 -16 1 | 13 31
gfz uuxuu | 5 9 234 -40 4 | 21 36
grg uuuuu | 49 -15 -100 61 -1 | 6 27
igr xxxxx | -21 2 -51 -2 -5 | 1 29
irf xxxxx | -18 -30 93 -34 -2 | -1 31
jpl uuuuu | -22 33 -106 5 -19 | 11 33
mit uuuuu | -49 -46 247 7 -5 | 25 39
ngs uuxuu | 82 56 -139 121 -1 | 8 28
sio xxxxx | -40 -33 117 72 -18 | 46 54
Table 7.2191.4 GPS week: 2191 Day: 4 MJD: 59585.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 6 -29 -27 30 12 | 2 30
emr uuuuu | -27 19 -96 15 4 | 11 35
esa uuuuu | -5 8 -171 -111 0 | 15 33
gfz uuxuu | -6 29 -66 -38 5 | 22 38
grg uuuuu | 46 -3 -128 80 1 | 7 28
igr xxxxx | -27 -2 -103 -35 -2 | 2 30
irf xxxxx | -10 -6 48 -32 -2 | 0 32
jpl uuuuu | -34 26 32 -66 -15 | 12 33
mit uuuuu | -23 -59 275 31 -5 | 27 41
ngs uuxuu | 48 56 22 69 -3 | 9 29
sio xxxxx | -1 -100 45 39 -20 | 45 54
Table 7.2191.5 GPS week: 2191 Day: 5 MJD: 59586.500
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 | 0 4 58 1 8 | 7 30
emr uuuuu | -52 -6 -23 -72 5 | 14 36
esa uuuuu | 4 10 -120 -96 5 | 18 33
gfz uuxuu | 30 36 -314 93 11 | 26 39
grg uuuuu | 21 -3 -125 103 4 | 9 28
igr xxxxx | -4 -9 -23 -49 7 | 5 29
irf xxxxx | -5 0 -3 -32 -5 | 3 31
jpl uuuuu | -33 7 8 -89 -34 | 14 33
mit uuuuu | -15 -18 113 -3 -6 | 30 42
ngs uuxuu | 41 -25 334 86 5 | 11 29
sio xxxxx | 62 -72 -99 -42 -8 | 45 54
Table 7.2191.6 GPS week: 2191 Day: 6 MJD: 59587.500
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 -11 -8 -41 -8 | 7 30
emr uuuuu | 4 46 -63 71 12 | 12 35
esa uuuuu | 8 12 -120 -112 3 | 17 33
gfz uuxuu | 28 35 -323 -103 -3 | 26 39
grg uuuuu | 2 -1 -33 1 -5 | 8 28
igr xxxxx | 4 -11 3 -7 -10 | 4 28
irf xxxxx | 7 -5 23 -17 -11 | 2 31
jpl uuuuu | 46 21 33 126 15 | 11 34
mit uuuuu | -19 -36 148 5 -16 | 29 41
ngs uuxuu | -21 -31 259 154 0 | 10 29
sio xxxxx | 47 -88 -24 -23 -1 | 45 53
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