[IGSREPORT-28400] Wk 2189 IGS Final Orbits
acc
acc at igs.org
Thu Jan 6 23:59:56 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2189 (Dec 19, 2021 - Dec 25, 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:
igs2189[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2189[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2189[0-6].cls IGS GPS clock combination summary report.
igs21897.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21897.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 | AREQ DAV1 MAYG DAV1
0 | EMR | KERG
0 | GFZ | 14 14 BOR1 BOR1 ZAMB
0 | GRG | CCJ2 DAV1 MCM4 SVTL DAV1 SVTL
0 | JPL | BADG THU2 AREQ BADG NYA1 THU2 ZAMB
1 | COD | NTUS
1 | EMR | ALGO
1 | ESA | CZTG LPGS QAQ1 CZTG IQAL LPGS QAQ1
1 | GFZ | 14 14 POHN ABMF ALGO POHN QAQ1
1 | GRG | MCM4 MCM4
1 | JPL | DAV1 MAC1
2 | COD | CPVG
2 | ESA | CHUR PTBB CHUR
2 | GFZ | LHAZ POHN LHAZ POHN VILL
2 | GRG | BAKE LHAZ SVTL BAKE LHAZ SVTL
2 | JPL | CZTG ZECK CZTG ZECK
3 | COD | HYDE MCM4 HYDE
3 | EMR | NLIB
3 | ESA | NRMD PTBB NRMD PTBB
3 | GFZ | NYA2 POHN NYA2 POHN
3 | GRG | GODE LHAZ MCM4 CPVG DAV1 LHAZ MCM4 ULAB
3 | JPL | NTUS MCM4 NTUS NYA1
4 | COD | ASCG FAA1 MAYG POHN SEYG
4 | ESA | PTBB
4 | GFZ | DAV1 POHN DAV1 POHN
4 | GRG | CKIS JFNG LHAZ SVTL DAV1 SEYG SVTL
4 | JPL | BADG BADG CZTG
5 | COD | ASCG BADG BOGT CAS1 CKIS HARB KARR MAYG MGUE MOBS
5 | COD | NOVM TONG TOW2 VOIM WUHN
5 | EMR | NOVM
5 | ESA | WES2 MCIL PTBB WES2
5 | GFZ | 13 13 POHN
5 | GRG | 13 13 HARB MCM4 SVTL HARB MCM4 SVTL
5 | JPL | BADG
6 | COD | IRKJ WIND WIND
6 | EMR | IRKJ SVTL
6 | ESA | CZTG CZTG NRMD PTBB
6 | GFZ | POHN POHN
6 | GRG | 13 21 13 21 IRKJ MCM4 XMIS MCM4
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. 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.
7. 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 | .3 .3 -.0 5 -2 1 -.17
EMR | 0 | 4.5 5.6 9.7 -4 -5 -7 .27
ESA | 0 | -.1 -.2 -.3 -20 5 16 -.12
GFZ | 0 | .5 .3 -.1 4 -6 3 -.20
GRG | 0 | 1.2 -2.1 7.2 -8 -24 -44 -.03
JPL | 0 | 1.9 5.3 10.9 -2 10 5 -.04
MIT | 0 | 6.9 .1 22.5 81 -43 51 .02
NGS | 0 | 5.0 -1.5 10.9 -11 -39 8 -.07
SIO | 0 | 5.3 -.1 24.5 66 -103 91 -.30
COD | 1 | .2 .1 -.0 4 0 -2 -.10
EMR | 1 | 4.8 6.9 14.2 -23 1 13 .02
ESA | 1 | .2 -.2 -.3 -13 -10 22 -.08
GFZ | 1 | .3 .1 -.9 -3 -17 2 -.08
GRG | 1 | 4.2 .3 18.7 -7 -30 -48 .02
JPL | 1 | 8.4 .2 12.4 -4 2 1 .21
MIT | 1 | 7.2 2.8 24.0 54 -33 37 -.12
NGS | 1 | 3.9 -1.3 16.4 0 -66 -6 -.13
SIO | 1 | 4.8 4.6 27.0 140 -178 107 -.15
COD | 2 | .1 .3 -.3 5 1 3 -.09
EMR | 2 | 5.1 2.3 9.2 -12 8 -17 .0
ESA | 2 | -.2 .3 .4 -18 -4 12 .03
GFZ | 2 | .1 -.0 -.7 -3 -6 8 -.13
GRG | 2 | 3.5 -2.0 15.2 -15 -9 -37 .10
JPL | 2 | 4.6 8.6 12.5 5 13 4 .24
MIT | 2 | 8.8 3.9 19.9 65 -17 60 -.03
NGS | 2 | 5.0 1.8 2.7 6 -21 24 -.08
SIO | 2 | 7.9 5.0 29.8 162 -215 78 -.12
COD | 3 | .1 .1 -.1 4 0 3 -.19
EMR | 3 | 5.7 1.6 15.2 -21 12 -7 .19
ESA | 3 | -.6 -.5 .2 -18 -11 10 -.02
GFZ | 3 | -.1 .0 .0 -6 -5 -4 -.08
GRG | 3 | 5.4 -1.7 18.0 -20 -21 -53 .08
JPL | 3 | 9.3 4.8 14.9 -4 15 -2 .07
MIT | 3 | 7.5 3.4 22.0 56 -47 -15 .05
NGS | 3 | 7.8 -6.7 12.3 -15 -76 -33 .10
SIO | 3 | 4.7 3.6 30.5 123 -138 59 -.22
COD | 4 | .1 -.1 -.1 0 0 -3 -.26
EMR | 4 | 8.5 5.6 14.2 -28 -2 -31 -.02
ESA | 4 | -.6 -.3 .0 -18 0 3 -.19
GFZ | 4 | .2 -.2 -.6 -12 -16 -3 -.19
GRG | 4 | 1.8 -.2 -1.1 -8 -24 -50 -.01
JPL | 4 | 8.4 8.4 18.0 0 -8 -1 -.07
MIT | 4 | 5.1 2.4 21.9 25 -50 -19 -.06
NGS | 4 | 6.0 -1.8 22.9 12 -115 -30 -.23
SIO | 4 | 6.2 -.2 28.2 27 -186 22 -.29
COD | 5 | .4 -.1 .0 2 -4 2 -.30
EMR | 5 | 5.9 8.1 18.0 -13 -5 -32 -.06
ESA | 5 | -.1 .1 -.7 -26 10 5 -.20
GFZ | 5 | .4 .0 -.3 -4 -18 -9 -.17
GRG | 5 | .5 3.0 2.6 -20 -15 -48 -.01
JPL | 5 | 2.7 3.2 18.2 3 0 1 -.04
MIT | 5 | 4.6 4.4 26.3 92 -27 25 -.16
NGS | 5 | 3.0 -.4 16.6 23 -50 -30 -.11
SIO | 5 | 5.3 3.9 35.4 117 -176 2 -.44
COD | 6 | .4 -.1 -.1 1 -7 3 -.29
EMR | 6 | 7.8 .2 11.0 -1 -7 -35 -.13
ESA | 6 | -.2 .0 .2 -12 -4 8 -.34
GFZ | 6 | .5 -.1 -.2 -9 -12 2 -.32
GRG | 6 | 2.9 -2.6 9.1 -12 -7 -27 .14
JPL | 6 | 5.9 2.6 14.3 6 -5 7 .05
MIT | 6 | 5.5 2.7 26.4 95 -38 7 -.13
NGS | 6 | 6.3 -.9 22.8 43 -71 -20 -.08
SIO | 6 | 3.9 5.7 29.6 126 -129 -14 -.38
8. 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.
9. 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 1.2189.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2189.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 2.2189.[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 3.2189.[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 5.2189.0-6). 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 2189 summary. (Dec 19, 2021 - Dec 25, 2021)
Table 1.2189.a GPS week: 2189 MJD: 59567.000-59573.000
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 678| -1 0 3 -3 -2 1 .03 7 7 | -343 -121 7 106
| 0 0 0 16 12 18 .01 | 191 303
emr 80| -1 0 1 -9 -1 -29 .19 15 15 | 202769 11 16 93
| 0 1 1 8 15 6 .03 | 437 451
esa 149| 0 0 0 -12 -2 4 -.03 7 7 | -357 -205 7 83
| 0 0 1 10 11 12 .02 | 233 541
gfz 240| 0 1 -1 -14 -7 1 .17 11 11 | 19 11 12 133
| 0 0 1 11 11 11 .01 | 209 265
grg 109| 0 -2 -2 -15 4 -24 -.10 11 10 | 30 33 8 137
| 0 0 5 9 12 33 .02 | 148 269
igr n/a| 0 0 -3 -4 -6 -9 .04 5 4 | -722 187 12 92
| 0 0 1 12 9 19 .01 | 562 519
jpl 80| 0 0 4 -26 -5 -47 .15 10 10 | 2087 89 9 81
| 0 1 0 10 19 24 .02 | 413 515
mit 381| 1 0 0 52 -14 21 -.12 9 8 | -2433 160 26 1698
| 0 0 0 20 19 39 .01 | 706 524
ngs 213| 0 0 -2 -1 26 -6 -.02 9 9 | -398 -111 837 1819
| 0 0 3 14 19 14 .02 | 135 234
sio 425| 1 1 -7 32 22 59 -.12 12 11 | --- --- --- ---
| 0 0 1 36 51 41 .02 | --- ---
Table 1.2189.b GPS week : 2189 MJD: 59567.000-59573.000
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 4 3 3 4 |
3 | 4 4 3 4 4 3 3 |
4 | 4 4 4 4 4 4 4 |
5 | 4 4 4 4 4 3 3 |
6 | 3 3 3 3 3 3 3 |
7 | 3 3 3 3 3 2 3 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 4 3 4 3 4 4 3 |
11 | 6 6 6 6 6 6 6 |
12 | 4 4 4 5 4 4 4 |
13 | 3 3 3 3 3 3 4 |
14 | 5 5 5 5 5 5 5 |
15 | 3 3 3 3 3 3 3 |
16 | 6 5 5 5 5 5 5 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 3 3 3 3 3 |
20 | 3 4 3 4 3 3 3 |
21 | 3 3 3 3 3 3 3 |
22 | 4 4 4 4 4 3 4 |
23 | 4 5 5 5 5 5 5 |
24 | 3 3 3 3 3 3 3 |
25 | 4 4 4 3 4 3 4 |
26 | 5 5 5 5 5 5 4 |
27 | 3 4 4 4 4 4 3 |
28 | 4 4 4 4 4 4 4 |
29 | 4 4 4 4 3 3 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 3 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 2.2189.0 GPS week: 2189 Day: 0 MJD: 59567.000
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 675| -1 0 3 3 -26 -11 .04 8 7 | -453 -270 7 111
emr 80| 0 1 2 -3 23 -37 .22 16 16 | 202393 352 17 124
esa 150| 0 -1 1 -19 8 -1 -.02 7 7 | -654 11 6 84
gfz 234| -1 1 -1 -8 -12 -14 .17 12 11 | 338 -299 13 88
grg 109| 0 -1 -2 -1 -13 -48 -.08 13 11 | 27 -219 9 142
igr n/a| 0 0 -1 -10 -1 -26 .03 4 4 | -1659 677 13 89
jpl 80| 0 0 5 -33 12 -52 .15 10 11 | 1483 618 9 83
mit 381| 0 0 0 84 -1 51 -.12 9 8 | -3588 464 28 1811
ngs 204| 1 0 -4 -12 21 -24 -.05 9 9 | -459 -240 709 1686
sio 527| 1 0 -4 -25 -2 110 -.10 10 10 | --- --- --- ---
Table 2.2189.1 GPS week: 2189 Day: 1 MJD: 59568.000
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 673| -1 0 2 20 -8 -20 .03 8 7 | -331 213 8 98
emr 80| -1 1 0 -8 0 -29 .20 16 16 | 202881 350 17 103
esa 150| 0 0 0 -28 -3 9 .02 8 8 | -606 -32 8 108
gfz 241| 0 2 -1 -10 -13 -5 .18 12 11 | -105 -67 12 212
grg 106| 1 -3 4 -10 13 -68 -.10 12 11 | -69 -42 10 145
igr n/a| 0 0 -3 -12 1 -27 .04 5 4 | -936 774 12 116
jpl 80| 0 0 3 -6 5 -32 .15 10 10 | 2061 429 9 65
mit 381| 0 0 0 44 -1 40 -.14 9 8 | -2505 1007 25 2083
ngs 216| 0 0 0 -27 31 -4 -.01 9 9 | -603 334 703 1751
sio 403| 1 0 -8 15 1 85 -.14 11 9 | --- --- --- ---
Table 2.2189.2 GPS week: 2189 Day: 2 MJD: 59569.000
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| -1 0 3 -9 -5 -13 .03 8 8 | 68 -634 8 106
emr 80| -1 0 1 -16 8 -33 .19 16 16 | 203576 -353 16 108
esa 150| -1 0 0 -17 2 -11 -.03 8 8 | -11 -536 7 76
gfz 242| -1 0 0 -10 -17 -6 .18 11 10 | -16 290 16 216
grg 99| 0 -2 4 -27 12 -51 -.08 11 10 | 231 -237 9 127
igr n/a| 0 0 -3 -18 -5 -29 .07 5 5 | 118 -300 13 89
jpl 80| 0 1 4 -32 12 -87 .17 11 11 | 2784 -413 10 110
mit 381| 0 0 0 55 -2 61 -.10 8 7 | -1960 -391 26 1650
ngs 216| 0 0 -5 -2 25 1 -.03 9 9 | -186 -405 757 1844
sio 399| 2 1 -6 40 -35 98 -.13 10 9 | --- --- --- ---
Table 2.2189.3 GPS week: 2189 Day: 3 MJD: 59570.000
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 675| -1 1 3 -29 5 24 .02 8 7 | -331 -152 8 112
emr 80| -1 0 1 -12 -15 -17 .21 15 15 | 202821 -452 17 79
esa 150| 0 0 1 2 -18 -9 -.02 7 7 | -170 -779 8 91
gfz 242| -1 1 -3 -9 10 3 .17 12 13 | 78 -328 14 89
grg 112| 0 -1 1 -25 8 -9 -.11 11 10 | 45 -28 8 143
igr n/a| 0 0 -3 0 -20 -15 .05 4 4 | -655 -139 12 88
jpl 80| 0 -1 5 -29 4 -73 .15 10 10 | 2048 -137 10 82
mit 381| 0 0 0 30 -5 29 -.12 8 7 | -2788 27 25 1284
ngs 216| 0 0 -5 15 -8 -3 -.01 9 8 | -344 -152 931 1808
sio 404| 2 1 -7 59 72 49 -.10 12 12 | --- --- --- ---
Table 2.2189.4 GPS week: 2189 Day: 4 MJD: 59571.000
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 681| -2 0 3 11 1 11 .03 7 7 | -411 -230 8 109
emr 80| -1 3 0 -23 5 -30 .17 15 15 | 202457 114 17 83
esa 150| -1 -1 0 -3 11 15 -.04 7 7 | -280 -13 7 76
gfz 238| 0 2 2 -4 6 5 .17 10 11 | -306 306 12 75
grg 112| 0 -2 -9 -9 15 9 -.14 11 9 | -143 155 8 131
igr n/a| 0 0 -3 16 4 6 .04 4 4 | -744 247 12 102
jpl 80| 1 -1 3 -31 -14 -34 .11 10 10 | 2027 140 10 78
mit 381| 1 1 0 27 -27 6 -.10 9 8 | -1376 365 28 1677
ngs 213| 0 0 2 4 23 -27 -.03 9 9 | -419 -239 848 1651
sio 409| 2 1 -7 39 -30 37 -.12 12 11 | --- --- --- ---
Table 2.2189.5 GPS week: 2189 Day: 5 MJD: 59572.000
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 679| -1 0 2 -8 5 -3 .03 7 6 | -480 245 6 102
emr 80| -1 2 3 -1 -17 -35 .18 14 14 | 202951 596 16 71
esa 150| 0 0 2 -6 -2 6 -.04 8 8 | -477 714 7 77
gfz 241| 0 1 0 -18 -16 9 .16 11 11 | 196 210 11 71
grg 113| 0 -3 -7 -19 -11 -22 -.09 12 10 | 221 557 8 139
igr n/a| -1 0 -3 5 -14 13 .03 4 4 | -253 590 12 73
jpl 80| 0 -1 4 -18 -26 -27 .15 10 10 | 2396 655 9 67
mit 381| 1 1 -1 58 -7 18 -.12 9 8 | -2101 179 28 1603
ngs 216| 0 0 -1 8 37 10 -.04 9 8 | -300 -38 854 2217
sio 418| 1 1 -7 7 53 39 -.12 13 12 | --- --- --- ---
Table 2.2189.6 GPS week: 2189 Day: 6 MJD: 59573.000
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 688| -1 0 5 -15 10 26 .02 6 6 | -467 -20 7 107
emr 80| -2 -1 2 -1 -15 -24 .14 15 15 | 202310 -529 15 89
esa 149| 0 0 0 -16 -14 20 -.05 7 7 | -302 -805 6 73
gfz 242| 0 2 -2 -38 -6 18 .17 10 11 | -46 -34 12 180
grg 115| 0 -3 -7 -13 4 21 -.07 12 10 | -97 49 9 136
igr n/a| -1 0 -6 -13 -12 10 .05 5 5 | -927 -537 14 87
jpl 80| 0 -1 5 -31 -33 -24 .15 10 10 | 1812 -667 9 84
mit 381| 2 0 0 69 -54 -56 -.12 9 8 | -2719 -529 28 1779
ngs 215| 0 1 0 3 54 1 -.01 9 9 | -481 -41 1063 1781
sio 415| 1 0 -8 87 95 -7 -.16 13 12 | --- --- --- ---
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 3.2189.0 GPS week: 2189 Day: 0 MJD: 59567.000
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 | 8 9 7 9 8 5 9 8 6 7 2 | 26 31 30 27 25 26 30 28 29 32 27
2 | 9 12 5 11 9 4 9 9 6 8 3 | 21 22 22 22 21 20 21 25 22 23 20
3 | 7 9 9 15 9 5 8 9 9 11 3 | 30 34 31 28 32 31 34 28 37 32 29
4 | 5 20 5 10 9 3 20 9 9 10 3 | 69 68 67 70 69 71 68 68 72 70 68
5 | 5 13 8 13 10 5 14 8 7 10 3 | 53 50 51 54 53 52 51 51 53 52 51
6 | 8 14 7 15 8 3 9 7 7 6 3 | 32 36 31 31 29 30 33 30 31 32 29
7 | 7 10 8 8 9 4 5 10 8 8 2 | 62 62 64 60 61 61 63 60 59 58 61
8 | 8 10 8 8 10 4 9 7 7 9 3 | 22 24 27 23 23 24 25 21 23 26 22
9 | 6 12 6 10 9 4 11 7 8 10 3 | 22 31 23 23 22 23 33 22 24 21 22
10 | 8 17 7 11 12 5 9 10 8 11 3 | 30 38 32 34 32 31 32 30 32 31 30
X11 | 15 22 15 18 18 9 14 16 17 --- 6 | 86 91 82 85 93 83 88 80 92 --- 85
12E | 8 18 7 13 17 5 13 9 12 11 4 | 42 41 38 37 44 40 42 40 42 39 40
13 | 6 9 8 8 6 4 10 10 8 9 3 | 23 27 25 25 21 26 26 27 25 26 23
14E | 10 21 8 25 16 5 9 7 20 12 5 | 41 39 45 52 48 44 44 41 42 40 41
15 | 5 9 5 7 6 4 9 7 7 10 2 | 66 68 63 66 65 63 69 62 67 58 64
16E | 10 28 10 17 40 8 9 15 13 17 6 | 37 40 33 38 53 33 34 37 35 38 35
17 | 8 11 5 9 11 5 8 7 9 9 3 | 23 29 20 29 20 22 24 25 26 29 22
18 | 9 19 11 13 11 5 11 10 14 11 4 | 73 77 74 75 78 74 77 73 79 73 75
19 | 7 19 6 13 9 5 9 8 10 10 3 | 23 29 21 27 22 21 25 23 24 26 22
20E | 9 9 7 9 12 3 10 7 9 14 3 | 62 63 62 64 62 63 62 60 66 64 61
21 | 8 12 4 9 10 4 9 6 8 7 2 | 16 24 18 22 18 17 20 19 22 23 18
X22 | 7 13 8 11 19 8 6 9 9 --- 4 | 44 47 43 41 45 44 46 44 51 --- 43
23 | 11 25 9 10 13 5 11 11 11 11 4 | 96 95 90 93 96 93 93 90 93 95 92
24 | 7 11 6 7 8 3 11 6 6 4 2 | 20 30 19 21 18 19 26 19 19 20 19
25E | 6 18 6 14 18 4 11 10 7 9 3 | 25 34 22 23 18 24 29 23 25 24 23
26E | 9 26 8 14 14 4 9 10 14 15 4 | 31 40 32 32 32 32 33 32 36 32 31
X27 | 6 11 7 11 9 3 7 8 9 --- 3 | 18 20 21 16 18 18 20 16 18 --- 17
X28E | 10 13 6 11 12 4 7 9 11 --- 3 | 29 28 28 27 34 29 30 30 31 --- 28
29 | 9 20 6 9 8 4 11 9 9 12 3 | 25 30 22 24 22 24 25 23 26 23 23
30 | 7 8 7 10 10 4 7 5 5 7 2 | 22 27 22 24 22 22 26 21 21 23 21
31 | 6 10 7 9 8 4 9 10 7 11 3 | 57 60 57 53 54 53 62 54 55 53 56
32 | 7 11 5 7 7 3 13 9 7 9 3 | 18 29 21 22 18 20 29 17 19 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 16 7 12 13 4 10 9 9 10 |T 38 42 38 39 39 38 41 38 40 38 38
WRMS | 7 16 7 11 11 4 11 8 9 10 |NE 36 40 36 37 35 35 39 35 37 35 35
MEDI | 8 12 7 10 10 4 9 9 8 10 |MD 30 34 31 29 32 30 33 30 31 32 29
Table 3.2189.1 GPS week: 2189 Day: 1 MJD: 59568.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 9 9 10 9 6 8 7 7 6 3 | 19 26 25 25 22 23 24 22 23 27 21
2 | 6 15 6 9 9 3 11 8 9 8 3 | 20 17 19 22 19 18 17 21 24 22 18
3 | 7 11 7 10 9 4 10 9 12 11 3 | 25 29 26 27 26 25 27 23 27 31 24
4 | 4 20 5 9 14 3 21 7 10 14 4 | 46 45 46 47 48 47 48 48 49 56 46
5 | 10 11 9 10 12 6 10 8 8 9 3 | 52 56 51 53 52 54 54 54 53 57 52
6 | 5 10 6 14 8 3 8 6 9 10 3 | 30 32 28 28 26 27 28 27 27 32 27
7 | 5 10 8 8 9 3 5 7 6 8 2 | 50 50 49 46 48 47 50 47 44 47 48
8 | 7 8 10 9 8 5 10 8 9 11 3 | 19 20 24 21 18 19 22 18 21 23 18
9 | 4 11 6 8 8 3 9 6 7 8 2 | 17 28 21 18 19 19 27 16 20 24 18
10 | 7 13 7 10 10 5 10 9 10 10 3 | 27 31 27 25 30 26 26 26 29 29 26
X11 | 14 24 17 15 19 7 13 13 17 --- 6 | 51 54 51 57 56 54 52 51 54 --- 51
12E | 9 20 8 14 16 7 11 10 9 14 4 | 39 36 38 36 38 37 40 37 37 32 37
13 | 7 9 6 9 9 3 7 10 8 13 3 | 20 25 21 19 19 21 23 19 20 21 18
14E | 9 20 7 28 13 7 10 8 21 10 5 | 34 35 37 52 39 39 37 34 35 38 35
15 | 8 9 6 9 8 4 7 8 5 8 2 | 40 42 38 42 45 39 41 36 41 40 39
16E | 11 25 9 11 16 7 9 14 8 22 5 | 29 29 25 27 31 25 27 30 27 35 27
17 | 7 11 6 13 12 4 6 8 6 9 3 | 22 25 19 28 18 21 21 21 23 29 20
18 | 9 20 12 13 14 6 11 9 9 10 4 | 40 46 43 44 48 41 41 41 43 42 41
19 | 8 21 5 14 10 3 7 9 7 10 3 | 24 28 22 28 20 22 22 21 25 29 21
20E | 7 13 6 20 15 5 8 9 11 12 4 | 59 62 59 58 60 60 58 57 60 61 58
21 | 10 12 6 10 12 3 8 7 9 7 3 | 13 20 15 22 15 15 16 15 22 20 14
X22E | 8 13 9 10 16 7 7 9 6 --- 3 | 32 33 29 32 37 33 30 32 32 --- 30
23 | 12 28 11 12 13 5 11 10 11 12 4 | 73 72 68 72 74 71 70 70 71 76 70
24 | 6 9 8 10 10 2 9 8 7 6 2 | 17 27 18 24 18 18 25 17 16 21 18
25E | 6 15 7 9 18 3 11 10 11 8 3 | 27 33 24 25 21 24 28 22 24 26 24
26E | 9 25 8 13 19 8 9 11 13 18 4 | 31 34 31 27 27 29 30 32 32 36 29
X27 | 7 9 9 10 9 4 12 11 8 --- 3 | 17 20 21 15 16 16 21 15 16 --- 16
X28E | 9 13 6 24 11 7 9 10 8 --- 4 | 25 23 26 40 24 27 26 28 26 --- 25
29 | 9 22 7 6 9 5 10 8 8 12 3 | 21 23 17 19 16 18 20 18 21 20 18
30 | 5 8 7 8 10 2 7 7 7 6 2 | 20 26 20 18 21 19 24 20 20 22 19
31 | 6 11 7 7 8 5 9 10 7 9 3 | 41 48 43 43 41 41 46 41 43 40 42
32 | 5 11 8 8 6 4 11 9 7 9 3 | 14 27 19 16 16 19 25 11 19 19 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 16 8 12 12 5 10 9 9 11 |T 31 34 31 33 31 31 32 30 32 34 30
WRMS | 7 16 8 11 11 4 10 8 9 9 |NE 27 31 27 29 27 27 29 26 28 29 26
MEDI | 7 12 7 10 10 4 9 9 8 10 |MD 27 29 26 27 26 25 27 26 27 29 25
Table 3.2189.2 GPS week: 2189 Day: 2 MJD: 59569.000
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 | 8 11 9 8 8 5 8 6 6 8 3 | 21 24 25 23 19 22 24 18 20 25 20
2 | 8 14 6 10 11 4 10 7 10 8 3 | 24 23 24 25 23 23 21 26 24 28 23
3 | 6 10 8 9 11 4 9 8 12 12 3 | 22 23 23 23 23 21 22 19 23 26 20
4 | 5 19 6 8 11 5 21 7 12 17 4 | 60 61 62 61 61 61 60 61 68 65 61
5 | 10 11 8 11 11 5 14 7 9 9 3 | 53 52 54 55 51 56 55 52 56 53 53
6 | 6 11 6 14 11 5 10 5 7 7 3 | 22 28 24 25 21 23 24 19 21 23 21
7 | 7 11 7 7 8 4 5 5 7 9 2 | 44 45 43 45 43 43 47 43 42 48 43
8 | 8 11 8 10 7 4 9 7 8 9 3 | 26 28 29 24 26 26 27 25 25 29 25
9 | 6 19 6 7 10 6 12 8 7 7 3 | 22 32 25 26 23 24 31 23 25 28 24
10 | 8 14 8 9 9 6 9 10 10 11 3 | 33 37 35 33 32 34 37 34 36 40 34
X11 | 13 23 18 16 18 9 12 11 11 --- 5 | 52 50 46 53 56 46 49 44 47 --- 48
12E | 9 22 7 9 12 5 11 9 11 13 4 | 29 31 27 29 29 30 30 31 32 31 29
13 | 7 10 5 10 6 6 10 10 8 10 3 | 19 26 17 17 17 19 23 21 21 22 18
14E | 8 17 8 21 15 5 12 6 17 9 4 | 30 31 35 40 33 34 36 31 32 34 32
15 | 8 10 7 8 5 4 9 9 10 11 3 | 46 49 41 44 45 43 47 42 40 43 43
16E | 11 23 12 14 17 7 11 11 7 19 4 | 37 38 35 33 41 35 35 39 36 42 36
17 | 9 15 6 13 12 4 10 7 5 8 3 | 24 27 21 29 21 23 25 23 22 29 22
18 | 10 21 13 16 12 6 10 7 11 6 4 | 47 53 48 53 53 47 50 47 47 49 49
19 | 11 19 5 10 10 4 9 7 8 7 3 | 23 26 22 28 18 22 22 21 19 27 21
20E | 7 11 6 9 11 5 9 9 9 11 3 | 35 32 34 32 34 36 34 34 37 41 34
21 | 8 12 6 9 8 4 8 6 10 12 3 | 19 24 23 25 20 21 21 22 25 28 21
X22E | 7 9 10 10 12 8 10 7 9 --- 3 | 28 29 27 28 30 26 29 29 30 --- 27
23 | 11 30 11 13 14 6 12 11 11 12 4 | 75 71 73 72 75 73 72 70 75 75 72
24 | 6 11 7 7 8 3 8 5 8 7 2 | 25 33 24 25 21 24 29 25 22 29 25
25E | 7 15 6 8 17 4 11 9 8 8 3 | 27 30 26 26 23 26 29 24 26 27 25
26E | 12 26 9 13 15 6 10 10 13 15 4 | 40 45 38 39 36 38 40 39 38 42 39
X27 | 8 10 9 13 9 4 9 10 9 --- 3 | 21 24 26 22 21 21 23 20 21 --- 21
X28E | 9 12 7 15 13 5 8 7 11 --- 3 | 30 27 31 35 28 30 30 30 34 --- 30
29 | 11 21 8 8 10 3 11 8 8 11 3 | 26 31 23 25 23 24 26 25 26 30 25
30 | 5 8 6 8 10 4 8 5 5 6 2 | 20 25 20 21 20 20 26 19 19 25 20
31 | 7 11 6 8 7 5 10 6 7 8 2 | 43 46 42 42 45 41 48 43 40 44 43
32 | 6 10 5 8 6 5 10 8 6 10 2 | 24 35 25 26 22 28 34 21 24 28 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 16 8 11 11 5 11 8 9 10 |T 32 35 32 33 32 32 34 31 32 36 32
WRMS | 8 16 8 10 10 5 11 7 9 9 |NE 30 34 30 31 29 30 32 29 29 33 29
MEDI | 8 12 7 9 11 5 10 7 9 9 |MD 27 31 27 28 26 26 30 26 26 29 25
Table 3.2189.3 GPS week: 2189 Day: 3 MJD: 59570.000
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 7 10 7 4 8 7 8 11 2 | 19 24 21 18 18 19 20 17 18 22 17
2 | 9 15 5 13 10 4 9 9 6 15 3 | 21 19 21 25 19 20 19 21 22 30 19
3 | 8 11 6 11 9 4 12 8 11 12 3 | 21 23 22 24 21 21 25 18 22 24 19
4 | 3 18 5 10 11 4 20 7 8 15 3 | 40 44 41 40 42 43 45 40 47 42 41
5 | 6 14 8 11 13 5 11 6 7 14 3 | 49 50 50 52 47 51 50 49 53 52 49
6 | 5 12 6 14 10 4 9 5 8 10 3 | 23 27 24 26 19 22 25 18 22 26 21
7 | 6 10 8 9 7 4 6 6 5 13 2 | 41 42 39 39 38 38 43 38 35 45 39
8 | 6 8 8 12 6 4 11 8 8 11 3 | 18 20 22 18 18 19 20 17 18 24 17
9 | 5 11 6 7 10 4 8 7 9 11 2 | 16 27 16 17 13 18 27 15 18 20 16
10 | 6 9 8 9 9 5 9 9 9 10 3 | 30 31 31 31 28 29 29 28 31 30 29
X11 | 12 23 15 17 18 6 12 9 15 --- 5 | 44 43 36 35 47 35 40 38 43 --- 39
12E | 10 21 7 22 16 8 11 8 9 15 4 | 33 32 32 37 36 33 33 33 36 36 32
13 | 6 8 6 9 6 4 7 7 8 13 2 | 18 24 19 21 18 21 24 19 26 27 19
14E | 8 18 9 24 13 5 9 7 18 12 4 | 29 31 33 42 35 33 33 30 33 35 31
15 | 7 10 4 8 7 3 8 6 7 12 2 | 43 47 43 44 44 42 48 41 43 39 43
16E | 15 25 11 17 11 6 9 15 11 18 5 | 32 30 26 33 28 27 26 30 30 28 27
17 | 6 10 5 11 10 3 7 8 7 12 3 | 22 23 18 24 17 19 22 20 20 28 19
18 | 12 18 11 13 12 6 11 6 10 11 4 | 42 45 42 45 48 41 45 45 48 48 44
19 | 7 19 5 10 9 3 7 7 9 11 3 | 20 21 18 21 15 17 19 18 20 26 17
20E | 7 12 6 11 15 6 9 8 10 17 3 | 34 34 34 35 37 34 32 36 34 40 33
21 | 8 8 9 8 9 4 10 7 6 8 3 | 15 20 18 20 17 15 19 16 17 25 15
X22E | 7 9 9 11 14 8 12 8 10 --- 3 | 32 31 31 33 35 31 33 30 29 --- 30
23 | 12 24 11 14 18 4 11 10 14 15 5 | 81 78 77 82 81 80 75 75 81 82 78
24 | 9 9 6 8 7 3 9 5 9 8 2 | 16 26 18 19 14 17 24 19 19 22 18
25E | 8 13 6 11 12 5 9 9 7 6 3 | 25 27 22 21 17 23 26 20 23 23 21
26E | 9 23 10 16 16 5 11 12 13 16 4 | 31 35 31 29 30 30 32 28 33 29 29
X27 | 6 8 8 13 8 4 9 11 10 --- 3 | 18 19 21 18 16 18 21 16 17 --- 17
X28E | 7 12 4 16 9 4 8 7 11 --- 3 | 24 26 25 30 25 25 25 24 30 --- 24
29 | 7 21 7 12 9 3 8 8 7 13 3 | 22 25 21 23 18 22 22 19 21 26 20
30 | 6 9 6 11 7 3 7 7 6 10 2 | 18 23 16 16 16 16 23 16 16 22 16
31 | 5 11 6 14 6 5 8 6 6 13 2 | 45 50 45 39 47 42 55 44 41 49 45
32 | 7 13 5 6 6 4 11 7 7 12 2 | 16 27 17 15 12 17 24 13 15 17 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 15 7 12 11 4 10 8 9 12 |T 29 32 29 30 28 28 31 27 30 32 28
WRMS | 7 15 7 13 10 4 10 7 8 12 |NE 25 29 25 26 24 25 29 24 26 29 24
MEDI | 7 12 6 11 9 4 9 7 8 12 |MD 24 27 24 26 21 23 26 21 26 28 21
Table 3.2189.4 GPS week: 2189 Day: 4 MJD: 59571.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 11 7 9 6 4 9 6 8 9 2 | 19 22 22 20 18 19 24 17 20 18 19
2 | 8 12 4 11 10 3 8 8 9 8 3 | 22 26 23 27 21 23 22 26 27 25 23
3 | 7 12 8 7 15 4 9 9 11 11 3 | 23 27 25 23 26 23 24 18 26 23 22
4 | 5 17 4 9 11 4 19 8 9 15 4 | 54 55 52 53 58 54 56 53 57 52 54
5E | 7 10 9 9 12 7 9 7 11 13 3 | 41 41 40 43 39 41 41 40 43 45 40
6 | 7 11 6 14 7 4 8 6 7 14 3 | 24 26 24 27 21 23 24 20 24 25 22
7 | 6 12 6 7 8 4 8 6 7 9 2 | 49 49 51 52 45 49 53 47 49 51 49
8 | 7 9 9 10 5 4 8 8 10 8 3 | 23 23 26 21 22 22 23 20 25 23 22
9 | 6 12 6 6 7 4 9 8 13 14 3 | 17 28 17 20 16 18 27 16 22 23 18
10 | 6 15 7 13 20 4 10 9 10 11 4 | 29 32 30 28 38 30 31 25 31 27 28
X11 | 13 23 18 17 16 8 12 10 19 --- 6 | 44 48 38 42 43 40 41 40 48 --- 41
12E | 8 20 9 8 11 8 11 9 9 17 3 | 30 30 26 32 28 29 30 28 34 29 28
13 | 8 11 6 10 6 4 10 8 9 12 3 | 14 25 15 11 18 17 21 17 18 21 15
14E | 10 18 9 21 19 3 10 8 17 14 4 | 28 29 32 35 40 31 32 28 31 33 29
15 | 7 9 6 5 7 3 9 8 9 12 2 | 41 43 39 43 33 39 43 38 45 37 40
16E | 11 26 10 15 11 6 9 13 12 17 4 | 41 43 38 40 42 37 37 43 42 43 40
17 | 6 10 5 9 9 4 6 8 7 15 3 | 23 23 19 24 17 19 20 18 25 27 19
18 | 9 17 12 12 11 6 10 8 9 10 3 | 44 47 44 49 44 43 47 46 47 47 45
19 | 7 18 3 8 9 5 8 8 7 14 3 | 19 20 17 22 14 17 17 16 22 22 16
20E | 6 10 6 8 11 5 8 9 9 13 3 | 26 27 25 26 29 25 23 24 26 29 24
21 | 7 10 5 7 10 4 8 6 8 8 2 | 16 19 19 18 19 17 18 17 22 20 17
X22E | 7 12 10 9 14 5 9 9 13 --- 4 | 27 26 25 29 31 26 27 26 28 --- 25
23E | 11 27 9 12 16 5 11 10 10 14 4 | 86 85 84 83 89 84 84 82 81 87 83
24 | 9 9 5 6 7 3 8 6 8 9 2 | 18 26 16 19 15 16 25 17 20 22 18
25E | 7 14 5 9 14 3 11 10 7 11 3 | 21 28 20 21 17 21 24 20 20 24 20
26E | 7 21 8 7 16 7 9 16 13 17 4 | 37 41 37 37 35 37 38 37 39 36 36
X27 | 6 9 10 11 6 4 8 11 10 --- 3 | 23 22 27 17 21 20 24 19 20 --- 21
X28E | 6 13 7 10 11 7 8 10 13 --- 3 | 28 27 31 31 29 29 27 27 31 --- 27
29 | 5 18 6 10 9 4 8 8 7 14 3 | 24 23 19 26 22 23 21 22 25 26 22
30 | 4 10 7 7 7 2 8 7 6 8 2 | 18 24 17 19 16 17 25 17 21 19 17
31 | 6 9 4 6 6 3 8 8 6 8 2 | 48 51 48 48 42 46 51 46 49 47 47
32 | 6 11 5 6 7 4 11 8 6 15 3 | 18 27 19 19 18 21 26 14 19 19 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 15 7 10 11 4 10 9 9 12 |T 30 33 30 31 30 29 32 28 32 32 29
WRMS | 7 15 7 11 9 4 10 8 9 11 |NE 27 31 27 28 26 27 30 26 30 29 27
MEDI | 7 12 6 9 10 4 9 8 9 12 |MD 24 27 25 27 26 23 26 24 26 26 23
Table 3.2189.5 GPS week: 2189 Day: 5 MJD: 59572.000
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 9 9 4 8 7 6 9 2 | 24 27 27 23 23 25 29 26 28 32 24
2 | 7 11 7 13 9 2 9 7 8 12 3 | 20 19 23 28 21 21 19 21 23 27 20
3 | 7 9 9 9 12 4 8 9 11 10 3 | 27 31 30 29 25 29 29 26 31 33 27
4 | 4 15 5 10 10 4 19 10 10 14 3 | 49 50 49 54 52 51 51 51 53 56 50
5E | 5 10 8 8 13 5 12 8 9 12 3 | 31 32 33 34 33 34 34 31 35 38 32
6 | 5 13 8 14 8 3 8 6 9 13 3 | 23 28 26 25 23 23 27 21 24 31 23
7 | 4 9 6 7 8 3 6 5 5 11 2 | 40 42 38 40 33 37 41 36 36 37 38
8 | 6 8 9 13 6 5 8 8 7 11 3 | 18 21 23 19 18 19 20 18 18 23 17
9 | 4 11 7 7 8 4 10 8 7 13 2 | 24 32 26 27 22 24 31 23 26 30 24
10E | 7 12 8 13 10 5 8 10 11 12 3 | 35 35 35 35 32 34 35 34 38 36 33
X11 | 12 19 18 15 14 7 13 11 16 --- 5 | 56 59 59 58 57 57 58 53 59 --- 56
12E | 11 23 8 11 13 6 11 9 9 15 4 | 35 37 34 37 36 36 37 32 36 36 34
13 | 5 11 7 13 7 4 10 9 9 11 3 | 21 27 19 20 16 21 27 21 21 28 19
14E | 8 18 11 20 14 4 11 9 20 10 4 | 31 35 36 42 41 36 37 34 38 37 34
15 | 7 9 7 7 8 4 8 8 8 12 3 | 38 42 40 39 38 38 40 35 41 39 38
16E | 8 25 11 14 11 6 9 18 6 23 5 | 30 32 25 26 28 26 30 36 29 36 28
17 | 6 10 6 8 11 4 7 10 5 12 3 | 23 25 21 25 18 22 24 22 25 33 21
18 | 10 19 14 13 9 5 10 9 8 9 4 | 48 55 50 52 49 49 52 49 53 51 50
19 | 5 20 5 8 10 4 8 8 6 13 3 | 20 22 21 23 18 19 21 19 24 30 19
20E | 6 9 8 9 10 7 7 10 9 14 3 | 38 41 43 44 41 43 41 41 42 46 40
21 | 8 10 5 7 16 4 8 6 7 7 3 | 12 17 15 17 19 14 16 15 18 21 14
X22E | 6 10 10 8 11 5 9 8 7 --- 3 | 36 36 35 37 40 36 35 35 39 --- 35
23E | 11 23 10 12 17 4 11 12 12 16 4 | 118 118 117 118 120 118 116 117 118 123 117
24 | 7 10 6 7 8 4 8 7 6 10 2 | 19 27 17 20 14 17 25 20 16 27 18
25E | 6 15 6 10 11 4 11 8 6 7 3 | 24 28 21 21 20 22 26 20 22 24 21
26 | 9 13 8 9 32 5 9 13 9 21 5 | 39 39 38 38 46 37 39 35 39 39 37
X27 | 5 8 12 15 9 4 7 8 10 --- 3 | 18 20 23 18 17 18 18 16 17 --- 16
X28E | 8 15 7 19 10 4 8 9 7 --- 4 | 24 23 26 35 26 27 25 27 30 --- 25
29 | 7 15 6 9 10 4 10 9 9 12 3 | 19 19 19 23 19 20 18 19 23 23 18
30 | 4 8 7 9 8 3 6 6 5 13 2 | 17 25 16 19 16 17 24 17 16 25 17
31 | 6 9 7 6 7 4 7 8 7 14 2 | 45 49 47 46 44 45 49 45 44 46 45
32 | 6 12 5 9 5 2 11 9 6 10 2 | 17 28 17 16 16 18 26 15 16 19 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 11 12 4 10 9 9 13 |T 31 35 32 34 31 32 34 31 33 36 31
WRMS | 6 14 8 11 10 4 10 8 8 12 |NE 27 31 28 29 26 27 30 27 29 32 27
MEDI | 6 11 7 9 10 4 8 8 8 12 |MD 24 31 26 28 25 26 29 26 29 33 25
Table 3.2189.6 GPS week: 2189 Day: 6 MJD: 59573.000
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 7 9 7 9 6 10 10 2 | 26 29 29 26 25 27 30 26 29 31 26
2 | 6 17 6 16 11 3 8 8 7 11 3 | 24 24 26 33 22 26 24 24 28 30 24
3E | 7 9 6 9 15 5 10 10 11 9 3 | 41 43 41 40 43 39 41 38 43 41 39
4 | 4 16 5 9 9 4 19 10 10 11 3 | 72 69 70 75 75 74 69 72 75 77 72
5E | 6 11 8 10 12 6 10 7 8 13 3 | 46 47 48 52 51 49 48 48 49 51 48
6 | 5 12 8 19 9 4 7 5 7 10 3 | 29 30 30 35 25 30 30 25 28 33 27
7 | 4 12 5 6 7 3 8 5 7 11 2 | 59 60 59 58 54 56 61 57 55 57 57
8 | 4 10 8 11 8 6 9 7 6 11 3 | 22 23 25 23 23 23 22 21 24 23 21
9 | 4 12 6 8 8 3 10 8 6 10 2 | 26 33 27 30 25 27 35 25 28 30 27
10E | 6 10 6 9 14 6 10 9 11 10 3 | 51 49 49 51 52 51 51 49 56 52 50
X11 | 11 23 17 17 15 8 12 10 14 --- 5 | 85 83 79 80 86 81 84 79 85 --- 82
12E | 9 21 7 9 11 8 10 8 7 16 3 | 36 35 31 32 38 33 34 35 36 36 34
13 | 5 13 7 9 20 5 12 8 10 13 3 | 24 32 24 24 25 26 30 26 28 28 24
14E | 8 18 9 17 16 5 12 10 19 12 4 | 36 39 38 46 46 41 41 36 40 40 37
15 | 6 10 5 5 8 4 11 9 8 11 2 | 64 67 60 63 62 61 66 58 66 60 62
16E | 9 29 9 16 13 4 9 13 7 20 4 | 39 47 38 42 42 37 39 43 38 43 39
17 | 6 13 5 9 10 5 7 7 7 12 2 | 25 31 22 26 19 23 26 21 28 34 23
18 | 9 19 14 10 11 7 12 9 12 10 4 | 76 80 77 80 81 76 77 79 82 78 78
19 | 6 17 6 10 9 5 7 8 7 11 3 | 24 26 23 24 18 22 24 21 26 30 21
20E | 5 10 6 8 9 8 8 10 9 17 3 | 42 45 45 42 43 46 46 40 47 49 43
21 | 7 12 6 7 10 6 9 6 10 8 3 | 17 20 21 21 22 20 21 19 19 23 18
X22E | 7 9 9 9 15 6 10 7 11 --- 3 | 43 41 39 42 50 40 41 41 44 --- 41
23E | 11 23 10 12 21 4 11 9 12 16 4 | 137 133 134 136 138 136 134 134 136 134 134
24 | 9 12 5 8 7 4 9 8 6 12 3 | 19 29 21 20 17 20 29 22 22 28 20
25E | 7 15 7 11 13 5 12 9 7 10 3 | 27 31 28 26 28 27 32 25 25 27 26
26 | 5 18 7 9 19 4 11 14 11 20 4 | 39 43 41 42 46 40 41 43 43 46 40
X27 | 4 12 9 9 9 5 8 10 8 --- 3 | 18 21 21 16 19 18 20 17 18 --- 17
X28E | 11 14 6 16 9 8 11 10 11 --- 4 | 36 36 38 38 37 38 41 41 41 --- 37
29 | 7 20 8 7 10 3 7 10 10 13 3 | 19 24 19 23 19 21 19 20 24 23 19
30 | 4 10 6 6 6 2 8 7 8 12 2 | 21 26 19 23 18 20 27 19 21 27 20
31 | 5 12 6 8 6 4 7 9 9 18 3 | 60 61 61 56 55 57 65 57 58 54 59
32 | 5 14 5 8 6 3 10 9 9 13 3 | 21 31 19 18 21 20 27 16 21 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 15 7 10 12 5 10 9 9 13 |T 40 43 40 41 41 40 42 39 42 43 40
WRMS | 6 15 7 11 10 5 10 8 9 12 |NE 36 39 36 37 35 36 39 35 38 38 35
MEDI | 6 12 6 9 10 5 10 9 9 11 |MD 36 35 31 35 37 33 35 35 36 34 34
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 4.2189 GPS week: 2189 MJD: 59567.0-59573.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 |U 11 13 20 |U 12 15 49 |U 14 15 34 |
emr | emr 3072 |U 25 22 54 |U 18 25 74 |U 17 19 53 |
esa | esa 3072 | 17 20 41 | 12 16 62 | 15 14 51 |
gfz | gfz 3071 |U 8 12 19 |U 13 16 49 |U 12 12 33 |
grg | grg 3069 |U 10 10 24 |U 14 20 57 |U 14 11 35 |
igr | igr 3072 | 12 14 23 | 11 13 50 | 12 12 33 |
igs | igs 3072 | 12 13 25 | 11 15 50 | 12 13 37 |
jpl | jpl 3072 |U 21 23 38 |U 13 19 71 | 19 17 56 |
mit | mit 3072 |U 12 10 21 |U 11 15 46 |U 13 14 30 |
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 5.2189.0 GPS week: 2189 Day: 0 MJD: 59567.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 8 14 | 12 10 45 | 10 11 28 |
emr | emr 3072 | 21 19 53 | 21 25 78 | 14 11 51 |
esa | esa 3072 | 14 14 37 | 11 13 59 | 13 11 45 |
gfz | gfz 3072 | 7 8 14 | 15 12 40 | 10 10 29 |
grg | grg 3072 | 7 9 15 | 12 11 42 | 8 9 33 |
igr | igr 3072 | 9 8 17 | 11 10 45 | 10 9 31 |
igs | igs 3072 | 9 9 18 | 11 10 45 | 10 10 33 |
jpl | jpl 3072 | 17 20 30 | 12 18 75 | 15 11 56 |
mit | mit 3072 | 9 6 14 | 11 10 37 | 9 12 27 |
Table 5.2189.1 GPS week: 2189 Day: 1 MJD: 59568.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 12 20 | 12 24 41 | 13 11 28 |
emr | emr 3072 | 25 17 52 | 18 29 69 | 21 9 45 |
esa | esa 3072 | 17 18 41 | 12 24 53 | 12 9 46 |
gfz | gfz 3072 | 8 10 18 | 12 16 39 | 10 10 26 |
grg | grg 3072 | 10 13 20 | 13 23 47 | 29 9 29 |
igr | igr 3072 | 11 12 21 | 11 20 41 | 10 8 30 |
igs | igs 3072 | 12 12 23 | 12 22 41 | 9 9 31 |
jpl | jpl 3072 | 20 21 37 | 14 27 64 | 31 13 59 |
mit | mit 3072 | 12 9 18 | 12 21 37 | 29 10 23 |
Table 5.2189.2 GPS week: 2189 Day: 2 MJD: 59569.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 14 21 | 13 16 54 | 12 14 29 |
emr | emr 3072 | 24 19 53 | 17 22 72 | 17 19 55 |
esa | esa 3072 | 16 20 42 | 13 17 65 | 13 12 46 |
gfz | gfz 3072 | 8 11 19 | 12 11 51 | 10 11 26 |
grg | grg 3072 | 10 12 24 | 13 17 61 | 10 10 29 |
igr | igr 3072 | 11 14 22 | 12 13 56 | 10 11 29 |
igs | igs 3072 | 12 14 25 | 12 14 54 | 10 12 31 |
jpl | jpl 3072 | 19 23 38 | 15 18 70 | 15 13 52 |
mit | mit 3072 | 11 11 22 | 12 17 50 | 8 12 25 |
Table 5.2189.3 GPS week: 2189 Day: 3 MJD: 59570.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 11 22 | 11 16 50 | 15 20 54 |
emr | emr 3072 | 23 21 58 | 17 22 73 | 19 33 72 |
esa | esa 3072 | 17 17 45 | 10 14 66 | 19 24 70 |
gfz | gfz 3072 | 9 8 23 | 8 14 44 | 15 19 54 |
grg | grg 3071 | 10 8 28 | 9 19 52 | 16 19 59 |
igr | igr 3072 | 11 9 27 | 9 13 52 | 17 19 43 |
igs | igs 3072 | 12 11 30 | 9 15 52 | 15 21 58 |
jpl | jpl 3072 | 20 18 45 | 11 15 70 | 19 23 59 |
mit | mit 3072 | 12 8 25 | 9 17 43 | 12 21 55 |
Table 5.2189.4 GPS week: 2189 Day: 4 MJD: 59571.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 14 13 22 | 13 14 52 | 14 15 35 |
emr | emr 3072 | 28 28 62 | 21 22 71 | 16 16 57 |
esa | esa 3072 | 19 21 41 | 12 13 60 | 15 12 49 |
gfz | gfz 3072 | 10 14 20 | 21 23 70 | 12 10 33 |
grg | grg 3068 | 11 9 29 | 16 18 70 | 9 8 35 |
igr | igr 3072 | 14 17 24 | 11 12 50 | 12 10 33 |
igs | igs 3072 | 15 15 27 | 11 12 50 | 12 12 37 |
jpl | jpl 3072 | 26 24 45 | 14 15 64 | 15 18 62 |
mit | mit 3072 | 12 13 22 | 11 15 48 | 11 12 30 |
Table 5.2189.5 GPS week: 2189 Day: 5 MJD: 59572.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 15 25 | 11 12 48 | 15 17 34 |
emr | emr 3072 | 25 22 52 | 18 27 75 | 14 19 45 |
esa | esa 3072 | 19 22 43 | 13 16 61 | 17 16 51 |
gfz | gfz 3069 | 9 13 22 | 14 19 47 | 14 11 35 |
grg | grg 3060 | 11 10 26 | 15 22 59 | 13 13 32 |
igr | igr 3072 | 13 14 25 | 11 11 48 | 14 12 32 |
igs | igs 3072 | 13 14 27 | 11 13 49 | 14 15 34 |
jpl | jpl 3072 | 21 25 38 | 13 19 72 | 17 21 53 |
mit | mit 3072 | 12 10 23 | 9 13 49 | 13 14 27 |
Table 5.2189.6 GPS week: 2189 Day: 6 MJD: 59573.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 20 19 | 13 16 55 | 16 18 31 |
emr | emr 3072 | 27 26 50 | 18 28 78 | 16 25 47 |
esa | esa 3072 | 18 27 36 | 14 15 69 | 18 15 50 |
gfz | gfz 3071 | 9 21 16 | 13 17 54 | 11 12 29 |
grg | grg 3071 | 14 14 28 | 21 31 67 | 12 11 27 |
igr | igr 3072 | 12 21 21 | 12 15 60 | 13 13 31 |
igs | igs 3072 | 13 20 24 | 13 15 59 | 13 14 32 |
jpl | jpl 3072 | 21 29 35 | 14 18 81 | 18 21 54 |
mit | mit 3072 | 13 16 23 | 14 16 56 | 12 14 24 |
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 6.2189 GPS week: 2189 MJD: 59567.500-59573.500
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 | 5 -3 15 -6 -3 | 6 23
| 16 18 84 65 5 | 5
emr uuuuu | -34 28 -129 -50 -5 | 32 38
| 31 23 100 51 3 | 5
esa uuuuu | -7 12 -25 -93 -4 | 16 26
| 7 18 78 54 2 | 6
gfz uuuuu | -8 10 102 -153 1 | 23 31
| 26 23 76 83 3 | 5
grg uuuuu | 1 18 -37 61 5 | 1 18
| 11 13 37 57 5 | 4
igr xxxxx | 5 1 6 1 -3 | -3 21
| 4 12 39 38 6 | 5
irf xxxxx | -8 8 40 33 5 | -1 20
| 14 7 14 14 4 | 3
jpl uuuuu | 9 35 -41 -26 -8 | 20 29
| 27 11 35 33 10 | 6
mit uuuuu | 18 -58 105 115 6 | 19 27
| 25 32 40 33 3 | 3
ngs uuuuu | -3 -12 -57 132 0 | 7 21
| 40 19 29 40 3 | 5
sio xxxxx | 122 -101 32 61 13 | 45 50
| 55 48 54 98 9 | 4
Table 7.2189.0 GPS week: 2189 Day: 0 MJD: 59567.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 26 -10 -95 -104 -8 | 16 34
emr uuuuu | -78 38 -112 -63 0 | 41 50
esa uuuuu | -13 27 12 -75 -7 | 27 40
gfz uuuuu | 40 -12 246 -27 0 | 32 44
grg uuuuu | 15 5 7 88 7 | 9 30
igr xxxxx | 7 6 46 39 -9 | 6 29
irf xxxxx | -15 3 38 17 -1 | 6 31
jpl uuuuu | -10 31 -88 6 -1 | 29 40
mit uuuuu | -10 -55 138 119 8 | 24 36
ngs uuuuu | 8 -5 -88 103 -1 | 16 32
sio xxxxx | 26 -66 55 -51 13 | 45 53
Table 7.2189.1 GPS week: 2189 Day: 1 MJD: 59568.500
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 -26 80 -14 -8 | 9 24
emr uuuuu | -39 36 -187 -15 -8 | 34 41
esa uuuuu | -13 42 -91 -104 -2 | 19 29
gfz uuuuu | -10 -4 133 -124 1 | 24 33
grg uuuuu | 9 21 -45 58 4 | 2 17
igr xxxxx | -5 15 -14 21 -3 | -1 20
irf xxxxx | -21 4 49 36 5 | -2 20
jpl uuuuu | -12 22 -14 -35 3 | 23 31
mit uuuuu | 17 -83 125 150 6 | 19 27
ngs uuuuu | 23 24 -88 81 -2 | 10 22
sio xxxxx | 103 -135 -52 -23 18 | 40 47
Table 7.2189.2 GPS week: 2189 Day: 2 MJD: 59569.500
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 76 64 -2 | 5 25
emr uuuuu | -49 45 -232 -55 -9 | 31 39
esa uuuuu | 1 1 -120 -49 -6 | 16 27
gfz uuuuu | -12 1 77 -293 1 | 21 32
grg uuuuu | 8 27 -6 67 2 | -1 18
igr xxxxx | 8 10 -49 -55 -2 | -3 22
irf xxxxx | -8 10 61 36 11 | -4 21
jpl uuuuu | -15 35 1 -16 1 | 20 30
mit uuuuu | -10 -57 160 72 12 | 16 26
ngs uuuuu | 24 -11 -84 129 -4 | 7 23
sio xxxxx | 168 -153 11 89 23 | 40 47
Table 7.2189.3 GPS week: 2189 Day: 3 MJD: 59570.500
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 | -5 15 69 -21 5 | 7 25
emr uuuuu | -27 26 -87 -147 -2 | 33 40
esa uuuuu | 0 -7 -46 -59 -3 | 17 27
gfz uuuuu | -45 17 84 -109 -4 | 24 33
grg uuuuu | -7 29 -3 -59 1 | 1 18
igr xxxxx | 7 -3 32 -12 3 | -1 21
irf xxxxx | -16 8 29 13 6 | -1 20
jpl uuuuu | -10 54 -83 -13 -9 | 22 31
mit uuuuu | 29 -50 58 82 7 | 19 28
ngs uuuuu | 22 -38 -30 201 -1 | 8 23
sio xxxxx | 78 -112 -16 -33 18 | 46 51
Table 7.2189.4 GPS week: 2189 Day: 4 MJD: 59571.500
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 | 10 -27 -34 -54 -9 | 2 18
emr uuuuu | -47 39 -82 17 -4 | 28 32
esa uuuuu | -6 1 -31 -88 -2 | 11 19
gfz uuuuu | -24 -9 118 -207 2 | 19 24
grg uuuuu | 5 -2 -62 114 14 | -3 14
igr xxxxx | 5 -21 -35 51 -7 | -5 17
irf xxxxx | -21 11 29 49 6 | -4 17
jpl uuuuu | 25 38 -13 -8 -25 | 17 24
mit uuuuu | 6 5 107 135 3 | 17 24
ngs uuuuu | 10 -18 -47 155 1 | 4 17
sio xxxxx | 167 -12 88 202 7 | 46 50
Table 7.2189.5 GPS week: 2189 Day: 5 MJD: 59572.500
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 | -15 4 95 6 0 | 0 18
emr uuuuu | -14 36 -243 -40 -6 | 27 31
esa uuuuu | -16 19 -16 -66 -4 | 10 19
gfz uuuuu | 0 28 36 -145 5 | 18 24
grg uuuuu | -6 31 -55 56 5 | -2 14
igr xxxxx | 8 -2 12 -32 -7 | -7 19
irf xxxxx | 11 -3 51 33 8 | -3 16
jpl uuuuu | 39 25 -52 -95 -17 | 13 24
mit uuuuu | 40 -89 100 96 5 | 17 24
ngs uuuuu | -21 -20 -37 144 2 | 3 17
sio xxxxx | 167 -132 45 139 18 | 46 50
Table 7.2189.6 GPS week: 2189 Day: 6 MJD: 59573.500
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 | -8 16 -88 84 1 | 2 17
emr uuuuu | 20 -22 39 -47 -6 | 28 32
esa uuuuu | -4 -1 119 -207 -1 | 11 19
gfz uuuuu | -7 50 17 -163 3 | 21 24
grg uuuuu | -15 17 -94 101 0 | 0 13
igr xxxxx | 4 5 49 -3 8 | -7 19
irf xxxxx | 13 20 24 50 1 | 0 13
jpl uuuuu | 49 39 -36 -23 -9 | 13 24
mit uuuuu | 56 -78 49 154 1 | 20 24
ngs uuuuu | -86 -19 -24 109 5 | 4 16
sio xxxxx | 146 -99 92 104 -3 | 51 54
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