[IGSREPORT-28519] Wk 2197 IGS Final Orbits
acc
acc at igs.org
Fri Mar 4 22:36:36 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2197 (Feb 13, 2022 - Feb 19, 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:
igs2197[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2197[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2197[0-6].cls IGS GPS clock combination summary report.
igs21977.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21977.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 | CHTI MAYG TLSE CHTI GRAS HYDE JFNG MAYG
0 | EMR | DAEJ
0 | ESA | 22 22 BAKE BOGT CPVG MCIL SYOG TLSE BAKE BOGT CPVG
0 | ESA | CZTG MCIL TLSE
0 | GFZ | CHTI POHN TLSE CHTI POHN
0 | GRG | 22 22 CHTI DAEJ LPGS STK2 SYOG XMIS CHTI LPGS
1 | COD | ALIC ASCG BOGT CCJ2 CRO1 FAA1 IRKJ KARR KOUR MAL2
1 | COD | MAYG MGUE NLIB NNOR NYA1 ONSA OUS2 PRDS SALU SAVO
1 | COD | SCRZ TLSE TOW2 TRO1 ULAB VILL VOIM WARK WIND WUHN
1 | COD | YELL MAYG
1 | EMR | ALGO YELL
1 | ESA | 22 22 ALGO WES2 YEL2 ALGO CZTG WES2 YEL2
1 | GFZ | CUSV POHN CUSV POHN
1 | GRG | 22 14 22 LHAZ STK2 SYOG CPVG LHAZ
1 | JPL | CPVG
2 | COD | GRAS HYDE MAYG MAYG
2 | ESA | 22 22 ASCG BAKE CPVG DAV1 SCH2 BAKE CZTG DAV1
2 | GFZ | POHN POHN
2 | GRG | 22 22 BRUX CPVG SVTL WARK BRUX CPVG LHAZ SVTL
3 | COD | BRAZ MAYG BRAZ MAYG
3 | EMR | HRAO MDVJ
3 | ESA | 22 22 POVE PTBB SAVO WES2 POVE PTBB SAVO WES2
3 | GFZ | NVSK HERS KIT3 NVSK SALU SAVO UFPR
3 | GRG | 22 22 LHAZ OUS2 STK2 SVTL SYOG LHAZ OUS2 SVTL
3 | JPL | 28 PTGG
3 | MIT | YEL2
3 | NGS | 11
4 | COD | 19 19 MAYG NRC1 MAYG NIST
4 | EMR | MDVJ NLIB
4 | ESA | 22 22 26
4 | GFZ | BOR1 KOKB BOR1 GRAZ NRC1
4 | GRG | 22 22 BAKE SYOG BAKE
4 | JPL | TOW2
4 | NGS | 11
5 | ESA | 22 22 CPVG
5 | GFZ | HERS NIST PRDS HERS NIST PRDS SUWN SYOG
5 | GRG | 22 22 SGOC SYOG SGOC
5 | JPL | BADG
5 | NGS | 11
6 | COD | PRDS PRDS
6 | ESA | 22 22 ASCG CPVG MAYG MCIL SYOG WUHN
6 | GFZ | POHN POHN
6 | GRG | 17 22 17 22 ASCG CPVG DAEJ KRGG MAYG SGOC SVTL SYOG
6 | GRG | LHAZ SGOC SVTL
6 | JPL | POHN
6 | NGS | 11
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
----+--------+--------+-------------
0 | COD | ~06:00 | ~ -0.18 ns
5 | JPL | ~13:45 | ~ -0.03 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 G14 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
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 | .1 .1 .2 4 5 -5 -.02
EMR | 0 | -5.7 -4.5 14.8 -13 -38 -15 .11
ESA | 0 | .7 -.5 .7 -10 31 0 -.17
GFZ | 0 | .6 -.3 .1 -2 -4 -15 -.15
GRG | 0 | .0 -3.0 -13.4 6 -41 -22 .12
JPL | 0 | 2.1 1.9 18.1 4 22 -1 -.19
MIT | 0 | -1.4 -3.4 17.8 73 86 45 .11
NGS | 0 | -4.4 -4.3 12.3 4 19 -25 .18
SIO | 0 | 1.2 -5.3 15.2 -118 -43 -74 -.16
COD | 1 | .2 -.0 .2 2 1 -1 -.15
EMR | 1 | -3.3 -5.1 19.0 -15 -34 -13 .09
ESA | 1 | -.1 -.5 .2 0 27 -5 -.26
GFZ | 1 | .6 -.2 .2 4 -2 -1 -.22
GRG | 1 | -1.2 -4.5 -12.9 8 -29 -24 .13
JPL | 1 | 7.4 3.5 15.7 -8 2 15 -.28
MIT | 1 | -.4 -2.3 17.3 139 98 148 .01
NGS | 1 | -1.4 -2.2 16.5 14 -15 -7 -.08
SIO | 1 | -3.0 -3.8 19.3 -79 17 -57 -.14
COD | 2 | .2 -.0 .1 1 -1 0 -.16
EMR | 2 | -1.2 1.8 12.0 -14 -27 -37 .14
ESA | 2 | -.2 .0 .1 -16 1 12 -.11
GFZ | 2 | .1 -.4 .4 0 6 -10 -.17
GRG | 2 | 6.0 -1.7 -3.3 -12 -27 -29 .11
JPL | 2 | 5.0 5.0 11.8 3 7 7 -.19
MIT | 2 | 3.5 .6 23.0 69 72 51 .0
NGS | 2 | 4.1 -3.4 10.5 11 -28 -16 -.12
SIO | 2 | 6.2 1.5 21.6 2 -141 -33 -.08
COD | 3 | .2 -.0 .2 1 0 -2 -.25
EMR | 3 | -1.7 -1.1 13.2 -12 -34 -37 .20
ESA | 3 | -.6 -.3 -.4 -19 16 16 -.18
GFZ | 3 | -.0 -.3 .1 13 9 4 -.19
GRG | 3 | 3.1 -4.8 5.3 -10 -36 -18 .08
JPL | 3 | 3.8 4.5 12.2 4 16 10 .11
MIT | 3 | 2.7 -3.4 18.7 62 75 46 .19
NGS | 3 | -2.0 -5.0 5.8 -7 14 -24 .07
SIO | 3 | 1.2 -7.7 15.5 -152 -67 -39 -.05
COD | 4 | .4 -.2 .1 0 -7 1 -.27
EMR | 4 | -5.9 -.2 14.8 -25 -62 -19 .12
ESA | 4 | -.7 -.8 -.9 -50 1 7 -.38
GFZ | 4 | -.0 -.3 .1 -3 5 -1 -.24
GRG | 4 | 1.3 -5.9 7.6 -7 -32 -15 .07
JPL | 4 | 1.7 2.9 15.4 -4 15 -8 -.06
MIT | 4 | 2.2 -3.2 21.9 97 86 150 -.10
NGS | 4 | -2.0 -8.1 11.9 -19 14 -46 -.17
SIO | 4 | 2.5 -2.8 18.7 -73 -67 -34 -.38
COD | 5 | .5 -.2 .4 -2 -1 2 -.37
EMR | 5 | -5.9 4.7 12.8 -20 -32 -5 .06
ESA | 5 | -.9 -.0 -.8 -39 8 14 -.29
GFZ | 5 | .3 -.2 -.2 -3 -13 5 -.20
GRG | 5 | -.3 -2.7 -1.7 -5 -35 -11 .04
JPL | 5 | -5.4 10.2 21.8 -9 7 14 -.16
MIT | 5 | -1.2 .1 23.1 178 58 203 -.06
NGS | 5 | -.3 -2.2 14.2 -1 -26 1 -.06
SIO | 5 | -3.6 -.6 23.3 -60 30 -46 -.17
COD | 6 | .2 -.2 .4 4 0 1 -.33
EMR | 6 | -2.7 2.3 13.0 -22 -26 -4 -.0
ESA | 6 | .0 -.4 -.1 -38 4 7 -.32
GFZ | 6 | .7 -.4 .0 -9 -16 4 -.25
GRG | 6 | 1.3 .6 2.8 -7 -18 -22 .08
JPL | 6 | 1.9 4.1 12.3 1 2 9 -.20
MIT | 6 | 1.6 2.1 19.9 55 78 65 -.04
NGS | 6 | 8.4 1.7 13.3 24 -70 -14 .05
SIO | 6 | -.7 -.6 14.5 -23 -42 -15 -.09
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 1.2197.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2197.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 2.2197.[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 3.2197.[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 5.2197.0-6). 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 2197 summary. (Feb 13, 2022 - Feb 19, 2022)
Table 1.2197.a GPS week: 2197 MJD: 59623.000-59629.000
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 655| -1 0 1 -2 -5 6 .02 7 6 | -308 -205 6 102
| 0 0 0 19 16 18 .02 | 333 416
emr 80| -3 0 2 -9 -15 -1 .04 13 13 | 207292 31 14 102
| 0 1 2 9 13 15 .01 | 9865 740
esa 150| 0 0 0 -24 -16 -1 -.06 7 7 | -552 -391 7 103
| 0 0 1 13 11 19 .02 | 268 322
gfz 228| 0 0 -1 -4 0 -18 .09 10 10 | -111 -57 11 96
| 0 0 1 20 11 17 .02 | 121 316
grg 109| 1 -1 -11 -17 -2 -3 -.15 11 10 | -69 42 9 144
| 0 0 7 13 21 14 .02 | 108 279
igr n/a| 0 0 -3 -6 -12 -1 .02 5 5 | 5479 -717 12 125
| 0 0 1 8 14 16 .02 | 2346 833
jpl 80| 0 -1 2 -4 -14 -8 .14 9 9 | -385 118 7 89
| 0 0 0 15 14 16 .01 | 616 738
mit 387| 0 1 2 43 13 69 -.04 7 6 | 3788 -771 26 1639
| 0 0 0 44 12 63 .01 | 2409 856
ngs 205| 0 0 0 -1 23 -41 -.04 10 9 | -984 -363 807 2208
| 0 0 2 25 13 23 .03 | 762 411
sio 382| 0 1 -1 1 16 -52 -.06 10 9 | --- --- --- ---
| 0 0 1 34 51 25 .02 | --- ---
Table 1.2197.b GPS week : 2197 MJD: 59623.000-59629.000
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 | 3 3 3 3 2 3 3 |
4 | 4 4 4 5 5 4 5 |
5 | 3 3 3 3 3 3 3 |
6 | 3 2 3 3 3 3 3 |
7 | 3 3 3 3 3 3 3 |
8 | 4 4 4 4 4 4 3 |
9 | 3 3 3 4 3 3 3 |
10 | 3 3 3 2 2 2 3 |
11 | 4 4 5 4 4 4 4 |
12 | 3 3 3 3 3 3 3 |
13 | 3 3 4 3 3 4 4 |
14 | 3 5 10 3 3 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 3 4 3 4 3 3 3 |
17 | 5 5 4 4 4 4 4 |
18 | 4 4 4 4 4 4 3 |
19 | 4 4 4 6 5 4 4 |
20 | 3 3 3 3 3 3 3 |
21 | 3 3 3 3 3 3 3 |
22 | 3 3 3 3 3 3 3 |
23 | 4 4 4 3 3 3 3 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 4 3 3 |
27 | 3 4 3 3 3 3 3 |
28 | 3 4 4 3 3 3 3 |
29 | 5 6 5 5 4 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 3 3 3 4 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 2.2197.0 GPS week: 2197 Day: 0 MJD: 59623.000
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 658| 0 0 3 33 9 -10 .03 8 7 | -556 -194 8 129
emr 80| -2 -1 6 -23 -25 16 .04 13 13 | 204401 305 15 122
esa 150| 0 0 0 -12 -10 8 -.07 7 7 | -1012 66 7 95
gfz 231| 1 0 0 10 2 -11 .10 10 9 | -77 -546 11 86
grg 109| 0 -1 -20 -10 -30 15 -.15 12 11 | -109 -156 10 156
igr n/a| 0 0 -3 -10 -29 0 .00 5 5 | 7533 588 12 117
jpl 80| 0 -1 3 -23 -16 -6 .14 8 8 | -10 715 7 99
mit 387| 0 1 2 34 -6 61 -.04 7 6 | 5998 534 25 1777
ngs 205| 0 0 0 -3 20 -13 -.03 8 8 | -586 28 973 2109
sio 381| 0 1 -2 -7 39 -62 -.07 9 8 | --- --- --- ---
Table 2.2197.1 GPS week: 2197 Day: 1 MJD: 59624.000
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 658| -1 0 2 3 -15 -1 .01 8 7 | -295 -101 8 124
emr 80| -2 0 3 -10 -18 -21 .05 14 14 | 204879 -237 15 91
esa 150| 1 0 -1 -9 -26 -42 -.09 8 7 | -434 -413 8 103
gfz 232| 0 0 -3 -17 12 -48 .06 11 10 | -9 -332 13 77
grg 109| 1 -1 -20 8 5 -23 -.17 19 11 | 119 -310 12 152
igr n/a| 0 0 -4 -3 -18 -32 .02 5 5 | 8303 -631 12 126
jpl 80| 0 -1 2 -24 0 -30 .14 8 8 | 479 -283 9 82
mit 387| 0 1 2 61 20 177 -.04 7 6 | 5644 -645 26 1660
ngs 205| 0 -1 0 -12 18 -63 -.03 10 10 | -33 -497 854 2698
sio 390| 0 1 1 -39 -1 -81 -.07 9 9 | --- --- --- ---
Table 2.2197.2 GPS week: 2197 Day: 2 MJD: 59625.000
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 655| -1 0 2 -18 5 -11 .02 7 6 | -613 -87 7 90
emr 80| -2 2 1 5 -21 13 .06 13 13 | 229569 -699 14 85
esa 150| 0 0 0 -22 -31 9 -.05 8 8 | -834 -264 9 104
gfz 232| 0 0 0 -29 4 -17 .07 10 9 | -323 121 11 81
grg 109| 0 -1 -13 -26 18 -21 -.17 10 10 | -243 140 9 137
igr n/a| 0 0 -3 -11 -1 -1 .01 4 4 | 7261 -1545 12 145
jpl 80| 0 0 3 7 -21 3 .14 8 8 | -124 -712 9 88
mit 387| 0 0 2 17 19 68 -.05 7 6 | 6252 -1698 32 1674
ngs 210| 1 0 0 -5 36 -48 -.07 10 9 | -625 -29 1093 3915
sio 376| 1 2 0 65 -29 -33 -.08 10 9 | --- --- --- ---
Table 2.2197.3 GPS week: 2197 Day: 3 MJD: 59626.000
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 655| -1 0 1 2 -21 6 .03 7 6 | -1 94 6 94
emr 80| -2 1 0 -8 -5 -5 .03 12 12 | 203662 -1026 14 119
esa 150| 0 0 0 -12 -8 9 -.03 7 7 | -369 -560 7 94
gfz 229| 0 -1 0 8 -22 -36 .09 11 10 | -61 224 12 85
grg 115| 2 -1 -6 -20 -9 5 -.15 10 9 | -14 81 8 130
igr n/a| 0 0 -3 0 -10 7 .03 4 4 | 5920 -1755 12 133
jpl 80| 0 0 3 5 -13 11 .14 9 9 | -369 -814 7 98
mit 387| 0 0 3 16 11 29 -.05 7 6 | 4412 -1779 27 1835
ngs 208| 0 0 -5 10 25 -36 -.05 9 9 | -764 -169 738 1589
sio 395| 0 1 0 -33 47 -29 -.07 11 9 | --- --- --- ---
Table 2.2197.4 GPS week: 2197 Day: 4 MJD: 59627.000
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 653| -1 0 0 -10 -25 1 .04 7 6 | 285 -1122 6 91
emr 80| -3 2 0 -6 -3 -17 .02 13 13 | 202317 173 14 87
esa 150| 1 -1 -1 -40 -10 4 -.08 9 9 | -296 -855 9 112
gfz 229| 0 0 0 16 0 -12 .09 10 10 | -113 -166 11 76
grg 108| 0 -2 -3 -18 4 9 -.15 9 9 | -79 -66 8 118
igr n/a| 0 0 -3 -15 0 -6 .05 4 4 | 3793 -1129 13 122
jpl 80| 0 -2 1 1 -10 -26 .15 9 9 | -1402 192 7 85
mit 387| 0 1 2 39 12 100 -.03 7 6 | 2812 -1195 24 1286
ngs 206| 0 -1 0 0 4 -72 -.00 11 10 | -849 -1173 615 1503
sio 384| 0 1 -3 0 26 -64 -.04 10 9 | --- --- --- ---
Table 2.2197.5 GPS week: 2197 Day: 5 MJD: 59628.000
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 652| 0 0 1 -23 16 21 -.03 7 6 | -502 -101 7 93
emr 80| -4 0 2 -17 -36 -5 .04 14 14 | 202548 1102 13 108
esa 150| 1 -1 0 -43 -26 -9 -.05 7 7 | -379 -633 8 102
gfz 225| 0 -1 -2 -27 -2 -9 .12 11 11 | 23 -54 12 136
grg 106| 1 -2 -9 -36 -29 -8 -.12 9 9 | -82 32 8 158
igr n/a| 0 0 -1 -13 -33 0 .00 5 5 | 2750 -15 13 121
jpl 80| -1 0 2 -14 -39 -19 .16 8 8 | -926 1053 9 96
mit 387| 1 2 4 133 2 79 -.05 7 6 | 799 11 23 1634
ngs 204| 0 0 0 -39 43 -46 -.01 11 10 | -1794 -489 690 1388
sio 360| 1 1 0 17 95 -77 -.06 10 10 | --- --- --- ---
Table 2.2197.6 GPS week: 2197 Day: 6 MJD: 59629.000
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 656| 0 -1 0 -2 -10 38 .02 7 6 | -477 73 6 99
emr 80| -2 1 0 -2 2 9 .05 13 13 | 203669 602 13 103
esa 150| 0 0 1 -26 -2 8 -.06 7 7 | -542 -81 7 111
gfz 223| 0 0 -1 10 7 4 .13 10 9 | -219 350 12 131
grg 107| 1 -2 -7 -21 21 -1 -.14 9 9 | -76 574 8 162
igr n/a| 0 0 -2 7 3 20 .04 4 4 | 2797 -538 12 114
jpl 80| -1 -1 2 12 1 7 .14 9 9 | -349 680 7 76
mit 387| 1 2 2 0 32 -29 -.04 7 6 | 602 -629 25 1610
ngs 202| 0 0 0 43 18 -11 -.07 9 9 | -2240 -213 689 2260
sio 393| 1 1 -2 8 -60 -15 -.02 10 9 | --- --- --- ---
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 3.2197.0 GPS week: 2197 Day: 0 MJD: 59623.000
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 12 7 11 7 5 7 5 7 5 2 | 17 18 19 16 17 17 22 17 18 17 17
2 | 9 12 4 10 8 4 8 5 8 8 2 | 20 20 17 19 18 17 18 18 17 21 17
3 | 6 12 8 10 9 4 9 4 9 7 3 | 22 21 23 22 23 22 23 19 22 20 21
4E | 10 20 7 9 15 5 10 9 9 10 3 | 49 51 52 52 55 50 53 51 48 46 49
5 | 6 11 6 8 10 5 8 6 6 11 2 | 31 32 30 30 35 31 33 28 29 29 29
6 | 6 8 7 8 7 5 7 6 7 7 2 | 23 24 22 24 21 21 25 20 22 23 21
7 | 7 12 5 5 9 4 8 6 7 7 2 | 63 65 62 63 59 62 66 63 62 65 63
8E | 8 11 9 24 10 5 10 8 7 7 4 | 30 29 33 34 35 30 31 27 30 35 30
9E | 8 10 6 6 9 6 8 4 10 7 2 | 28 31 29 29 30 28 29 30 28 30 28
10 | 5 8 6 10 10 4 8 4 7 9 2 | 29 29 30 30 33 30 32 29 28 27 29
X11 | 11 16 11 11 13 7 10 7 7 --- 4 | 44 40 42 41 46 43 42 42 41 --- 41
12 | 7 17 6 7 10 4 10 7 5 8 3 | 44 52 42 43 39 43 47 41 42 41 43
13 | 9 17 4 8 10 5 6 6 10 6 3 | 46 46 44 47 48 46 45 45 44 46 45
14 | 8 13 7 7 12 5 7 10 10 9 3 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
15E | 7 20 8 10 12 7 9 6 9 13 3 | 36 36 36 41 39 38 35 37 39 37 36
16 | 7 17 4 10 11 4 10 5 9 9 3 | 16 20 15 20 19 16 19 18 20 21 16
17E | 15 12 11 8 15 8 10 13 11 15 4 | 43 44 44 41 48 43 42 45 45 47 43
X18 | 12 9 9 6 10 5 8 10 10 --- 3 | 35 39 37 36 39 37 40 37 40 --- 36
19E | 8 15 7 9 21 4 8 9 12 9 3 | 75 69 70 73 78 71 71 70 68 67 70
20 | 7 16 7 9 8 5 8 5 10 11 3 | 26 25 23 25 23 23 26 26 27 30 25
21 | 7 14 4 14 8 6 6 8 7 8 3 | 12 18 14 22 14 14 18 16 16 17 14
22 | 8 11 5 10 12 6 7 6 6 7 2 | 30 31 29 32 29 29 30 30 29 32 29
23 | 8 13 10 7 11 5 9 7 14 11 3 | 80 80 77 78 78 78 80 79 79 82 79
24 | 9 10 6 6 6 4 8 4 6 6 2 | 23 28 23 22 21 22 28 23 23 22 22
25 | 7 9 6 6 11 4 9 7 6 7 2 | 21 27 21 22 22 21 27 22 20 21 21
26 | 9 8 7 7 9 3 8 7 6 6 2 | 26 28 26 28 22 24 29 25 27 24 25
27E | 7 11 8 12 10 4 10 9 6 9 3 | 30 32 31 30 32 30 31 26 30 35 29
X28 | 9 14 7 9 9 6 7 7 8 --- 3 | 21 24 15 21 19 17 23 18 21 --- 18
29E | 9 18 14 10 31 4 8 4 12 10 4 | 60 63 61 61 69 60 62 63 64 57 60
30 | 7 9 6 7 7 3 9 5 8 6 2 | 17 24 18 17 16 17 26 18 16 19 17
31 | 5 12 6 7 11 3 9 7 5 8 2 | 64 65 62 65 55 62 67 61 62 63 63
32E | 7 13 4 9 9 5 9 6 7 9 2 | 24 24 22 23 23 23 24 25 23 19 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 7 10 12 5 8 7 8 9 |T 35 36 34 35 35 34 36 34 34 35 34
WRMS | 7 13 7 9 11 5 8 6 8 8 |NE 31 33 30 32 30 30 34 31 31 31 30
MEDI | 7 12 7 9 10 5 8 6 7 8 |MD 30 31 30 30 32 30 31 28 29 30 29
Table 3.2197.1 GPS week: 2197 Day: 1 MJD: 59624.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 4 11 8 10 6 4 7 4 10 6 2 | 16 18 19 16 17 18 20 18 19 15 16
2 | 7 14 7 8 8 4 7 4 7 6 2 | 18 20 16 20 16 16 18 17 20 16 16
3 | 5 11 9 7 8 4 7 5 7 6 2 | 20 22 25 21 23 21 21 18 20 17 19
4E | 10 20 9 12 19 5 11 8 11 9 4 | 43 48 49 48 52 48 47 44 45 48 45
5 | 6 10 8 12 10 5 6 8 6 12 3 | 25 26 24 30 28 25 27 23 27 24 24
6 | 6 9 6 9 5 4 6 4 9 5 2 | 21 21 20 21 20 19 22 18 22 17 19
7 | 7 10 6 10 10 4 6 5 8 3 2 | 40 42 35 37 35 37 39 41 40 39 39
8E | 8 22 8 11 11 6 10 8 9 8 3 | 32 37 36 35 38 35 35 32 38 35 33
9E | 8 8 7 7 8 7 9 6 17 8 3 | 26 26 25 26 22 27 25 26 25 26 24
10 | 6 10 8 10 9 3 7 4 8 7 2 | 28 27 30 30 30 28 30 27 29 26 27
X11 | 10 13 12 14 13 5 8 7 14 --- 4 | 26 29 29 30 30 25 27 29 27 --- 27
12 | 5 20 6 5 9 3 7 6 3 8 2 | 23 29 21 23 20 22 27 22 24 23 22
13 | 9 13 6 8 12 4 8 9 9 4 3 | 39 44 40 40 43 41 42 40 44 40 40
14 | 9 11 8 10 52 6 7 10 10 9 5 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
15E | 7 15 7 21 12 6 11 8 8 9 3 | 35 36 37 41 36 38 34 34 39 37 35
16 | 5 19 7 14 10 4 7 7 15 9 3 | 13 18 13 17 15 12 15 14 22 13 12
17E | 15 15 11 10 41 8 8 11 6 14 5 | 26 26 24 26 43 25 25 26 26 26 24
X18 | 9 11 11 10 10 4 8 8 9 --- 3 | 19 26 23 24 26 23 26 26 25 --- 23
19E | 11 20 6 10 21 4 10 10 11 15 4 | 41 39 38 38 44 37 39 36 36 37 38
20 | 6 12 8 9 9 4 7 7 6 11 3 | 26 26 25 27 25 25 28 25 28 26 24
21 | 4 15 6 13 7 4 7 6 12 10 3 | 14 18 14 21 15 15 18 16 18 15 14
22 | 7 10 6 11 20 7 8 5 7 9 3 | 28 27 28 30 34 26 27 31 27 29 27
23 | 9 12 11 12 11 6 9 8 9 12 3 | 51 55 53 54 54 52 57 54 52 56 53
24 | 7 10 8 9 8 4 7 4 8 7 2 | 23 30 25 24 22 24 29 23 27 25 24
25 | 7 10 7 8 10 3 7 5 9 6 2 | 16 23 19 18 18 17 22 17 17 18 17
26 | 7 9 8 12 7 3 8 6 9 7 2 | 18 24 18 20 16 17 25 16 18 17 17
27E | 6 13 9 20 21 4 10 8 11 8 4 | 27 28 28 28 31 27 26 25 30 27 25
X28 | 6 15 6 15 11 5 8 6 9 --- 3 | 15 23 12 19 17 13 23 15 16 --- 15
29E | 10 20 6 12 46 11 8 11 18 17 5 | 46 44 45 52 63 48 47 45 49 47 46
30 | 6 10 7 9 10 3 8 4 9 5 2 | 18 24 18 16 19 17 25 18 16 17 17
31 | 7 12 6 7 10 3 9 5 8 14 3 | 44 47 43 47 39 43 48 42 45 41 44
32E | 7 9 6 9 11 5 9 6 10 7 2 | 22 23 23 26 20 24 24 22 25 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 8 11 19 5 8 7 10 9 |T 27 29 27 29 29 27 29 27 28 27 26
WRMS | 7 14 7 10 11 5 8 6 10 9 |NE 23 27 24 25 24 23 27 23 25 23 23
MEDI | 7 12 7 10 10 4 8 6 9 8 |MD 26 26 25 26 26 25 27 25 27 26 24
Table 3.2197.2 GPS week: 2197 Day: 2 MJD: 59625.000
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 8 8 10 6 2 8 4 10 7 2 | 23 25 24 22 21 23 26 24 22 22 22
2 | 4 14 7 8 9 3 7 5 10 9 2 | 20 18 19 24 19 20 19 22 21 22 19
3 | 5 8 8 7 7 3 8 6 5 7 2 | 25 27 28 27 24 25 28 23 23 23 24
4E | 11 18 9 12 18 3 11 8 9 7 4 | 34 38 40 41 43 37 38 38 32 39 36
5 | 6 9 9 11 8 5 6 11 7 10 3 | 30 30 29 32 28 30 30 27 28 28 28
6 | 6 9 6 8 8 4 5 4 7 7 2 | 26 23 25 27 22 23 24 24 23 24 23
7 | 5 11 5 8 10 4 7 6 7 7 2 | 53 55 53 52 50 52 56 56 51 53 53
8E | 5 15 10 14 12 3 10 7 11 9 3 | 18 22 21 20 23 19 20 21 21 23 18
9E | 8 8 6 7 9 3 8 6 11 4 2 | 29 30 27 27 26 27 28 30 27 27 27
10 | 6 10 9 8 9 3 7 5 8 6 2 | 29 28 32 29 27 29 31 27 29 27 28
X11 | 7 14 13 14 13 6 9 8 16 --- 4 | 25 27 26 27 27 27 27 30 28 --- 26
12 | 4 18 8 6 9 4 7 8 9 7 3 | 31 38 29 31 29 30 34 31 30 31 30
13 | 10 15 6 7 12 5 9 7 17 9 3 | 34 34 33 31 38 34 34 33 43 35 33
X14 | 10 --- --- 11 40 10 --- 16 11 --- 9 | 9999 --- --- 9999 9999 9999 --- 9999 9999 --- 9999
15E | 7 19 7 15 13 7 11 7 13 10 4 | 25 25 27 32 28 27 25 26 33 27 26
16 | 6 17 6 12 12 4 8 5 7 7 3 | 22 25 22 24 22 21 24 22 22 24 21
17E | 8 10 8 9 14 4 5 12 7 15 3 | 36 37 40 34 38 37 37 40 38 36 36
X18 | 10 11 10 9 10 4 7 8 8 --- 3 | 24 30 27 29 28 26 29 27 28 --- 26
19E | 11 16 6 9 11 3 9 12 16 15 4 | 36 35 33 36 33 32 34 32 28 27 32
20 | 5 11 9 6 8 4 7 8 8 9 2 | 20 19 19 20 17 20 20 23 22 25 19
21 | 5 13 6 11 8 5 7 6 9 12 3 | 19 24 19 24 18 22 24 21 20 23 19
22E | 6 10 7 9 8 7 8 7 10 8 2 | 32 31 31 34 28 30 32 33 34 32 31
23 | 8 12 13 11 12 5 8 8 10 9 3 | 59 61 57 60 60 58 60 62 62 65 60
24 | 7 15 9 9 11 4 8 6 8 8 3 | 19 24 18 20 16 18 24 20 17 22 18
25 | 7 7 9 7 10 4 9 6 8 8 2 | 23 29 26 26 25 25 31 26 27 24 25
26 | 6 7 8 10 9 2 7 7 7 6 2 | 30 35 32 32 28 30 35 29 33 30 30
27E | 7 13 7 14 8 5 9 7 9 10 3 | 17 20 18 18 20 18 19 19 22 21 17
X28 | 6 12 6 8 8 5 13 7 11 --- 3 | 23 26 19 22 21 21 29 24 22 --- 21
29E | 10 18 6 14 16 8 10 15 13 28 5 | 31 29 30 32 29 28 29 32 30 33 28
30 | 6 9 6 9 7 4 9 5 5 7 2 | 20 25 21 18 18 19 27 21 18 22 20
31 | 4 11 6 8 10 3 8 6 7 11 2 | 54 58 54 58 50 54 58 52 55 55 54
32E | 6 10 5 7 9 4 9 5 10 8 2 | 24 27 25 25 22 25 27 24 26 25 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 10 10 4 8 7 10 10 |T 28 30 29 30 28 28 30 29 29 30 28
WRMS | 6 13 8 9 10 4 8 6 9 9 |NE 28 31 28 30 27 28 31 29 29 30 28
MEDI | 6 11 7 9 9 4 8 7 9 8 |MD 25 28 27 27 27 27 29 27 28 27 26
Table 3.2197.3 GPS week: 2197 Day: 3 MJD: 59626.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 4 10 7 11 7 3 7 6 11 8 2 | 19 18 21 18 19 18 21 18 19 21 18
2 | 5 10 6 10 7 5 9 6 8 8 2 | 22 18 20 24 20 20 21 21 18 21 20
3 | 5 10 8 11 6 4 8 4 6 7 2 | 21 21 22 23 20 20 21 18 19 20 19
4E | 12 18 9 23 12 5 10 7 13 8 4 | 32 35 36 35 35 34 35 34 36 36 33
5 | 6 11 8 8 7 5 8 10 6 13 3 | 28 29 27 27 25 28 29 25 28 27 26
6 | 6 8 7 8 7 5 8 5 6 10 2 | 22 23 22 24 22 21 23 19 19 22 21
7 | 6 12 6 8 7 5 7 6 9 6 2 | 41 42 42 43 38 41 44 44 38 41 41
8E | 7 20 6 10 13 3 10 7 14 8 3 | 20 25 21 23 23 19 20 20 22 23 20
9E | 7 8 6 17 11 3 10 6 12 8 3 | 24 23 22 29 21 23 23 24 26 24 22
10 | 5 8 7 8 7 3 5 5 8 7 2 | 25 25 28 27 23 26 27 23 27 24 25
X11 | 8 11 11 13 14 12 10 6 13 --- 4 | 22 22 21 26 26 21 21 24 21 --- 22
12 | 5 15 6 8 8 4 6 6 8 8 2 | 39 44 39 40 37 38 42 37 35 38 38
13 | 7 9 6 7 15 3 9 6 8 14 3 | 50 51 49 49 51 49 50 49 50 53 49
X14 | 5 10 8 7 12 5 7 9 11 --- 3 | 807 668 670 807 799 804 671 801 800 --- 804
15E | 8 14 7 18 13 6 9 5 12 9 3 | 30 30 30 39 28 32 30 29 39 35 31
16 | 7 17 7 11 11 3 9 10 9 6 3 | 18 20 17 25 17 18 20 20 22 20 18
17E | 7 12 10 7 10 4 6 11 6 16 3 | 31 34 33 34 35 32 32 32 33 35 32
X18 | 10 13 10 8 11 5 8 7 9 --- 3 | 23 28 23 24 26 22 25 24 23 --- 23
19E | 18 18 6 20 19 4 12 12 14 19 5 | 48 37 38 37 45 36 38 35 36 36 38
20 | 6 11 5 8 7 5 9 7 7 12 2 | 20 21 18 22 19 19 20 22 17 24 19
21 | 5 12 6 10 8 5 7 7 10 12 3 | 18 20 17 21 18 17 21 18 16 23 17
22E | 6 8 6 11 8 5 9 6 10 8 3 | 28 29 30 35 31 30 30 29 27 29 29
23 | 7 12 11 9 11 5 7 9 10 7 3 | 47 45 45 48 50 44 47 50 44 49 47
24 | 8 8 9 8 8 3 8 4 7 7 2 | 22 26 24 21 20 22 26 22 21 23 22
25 | 6 9 6 8 11 4 9 5 8 8 2 | 22 28 22 26 20 22 28 22 22 24 22
26 | 4 6 8 7 7 3 9 9 9 9 2 | 25 26 25 29 22 24 28 23 26 24 24
27E | 6 14 7 9 11 3 10 8 12 8 3 | 20 21 23 25 23 21 21 21 21 22 20
X28 | 5 12 7 8 9 5 11 7 9 --- 3 | 20 22 17 21 16 19 25 18 22 --- 19
29E | 10 18 8 11 13 6 11 12 7 26 4 | 26 25 25 22 24 23 26 30 25 31 24
30 | 5 8 6 8 7 4 7 5 8 10 2 | 20 24 20 21 17 19 24 20 18 24 20
31 | 6 11 6 7 8 3 9 5 5 10 2 | 41 44 43 46 38 42 46 40 38 39 41
32E | 7 10 5 8 9 5 10 6 9 8 2 | 24 23 23 24 18 24 24 21 25 23 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 7 11 10 4 9 7 9 11 |T 51 48 47 53 50 50 48 51 51 28 50
WRMS | 6 12 7 10 9 4 9 6 9 9 |NE 62 57 56 64 61 62 58 62 61 27 62
MEDI | 6 11 7 8 9 4 9 6 9 8 |MD 24 25 23 26 23 23 26 23 25 24 22
Table 3.2197.4 GPS week: 2197 Day: 4 MJD: 59627.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 4 10 8 10 7 4 7 6 11 6 2 | 21 23 23 18 21 21 24 21 22 21 20
2 | 6 11 7 10 8 3 8 5 11 7 2 | 21 23 20 25 21 20 21 20 21 25 20
3 | 5 9 8 6 5 3 7 8 4 5 2 | 21 21 21 19 20 20 21 19 21 20 19
4E | 12 22 11 15 14 6 13 7 16 6 4 | 30 36 35 30 33 33 35 32 35 32 31
5 | 7 10 8 8 7 5 10 10 9 15 3 | 26 29 23 26 22 26 29 26 23 34 25
6 | 5 10 7 8 6 4 8 4 9 11 2 | 24 27 24 25 23 23 24 22 22 25 23
7 | 7 12 5 8 6 3 8 6 9 7 2 | 50 53 50 49 51 49 52 52 51 50 50
8E | 7 19 7 15 11 4 14 9 15 10 4 | 18 23 19 20 22 18 20 20 23 24 18
9E | 9 9 7 7 14 4 8 6 13 5 3 | 25 22 22 23 22 23 22 24 25 22 21
10 | 4 8 8 9 7 3 6 4 6 8 2 | 21 21 23 22 18 21 23 20 20 19 19
X11 | 9 12 13 11 12 6 9 8 13 --- 4 | 24 28 25 26 28 26 24 28 25 --- 24
12 | 5 15 8 8 8 4 6 6 5 10 2 | 33 36 31 31 31 31 35 31 32 30 31
13 | 6 9 4 15 10 4 9 6 11 9 3 | 48 50 49 50 44 49 51 50 47 53 48
14 | 8 11 8 4 11 4 6 9 10 9 3 | 9999 992 992 9999 9999 9999 990 9999 9999 9999 9999
15E | 8 19 9 23 10 7 10 6 11 9 4 | 29 29 29 38 23 29 28 27 26 27 27
16 | 6 18 8 7 9 3 8 5 7 7 3 | 20 24 20 21 22 21 24 23 22 23 20
17E | 6 12 13 7 8 7 7 9 8 14 3 | 38 39 40 35 42 37 36 35 38 38 36
X18 | 10 13 12 9 10 4 9 7 9 --- 3 | 23 30 24 25 28 24 30 26 27 --- 25
19E | 8 23 7 13 15 5 16 11 18 20 5 | 43 44 44 47 48 45 46 46 41 46 44
20 | 7 9 6 9 7 4 11 8 12 10 3 | 21 23 21 26 21 22 23 26 22 25 22
21 | 5 15 6 10 8 5 8 8 13 8 3 | 17 23 17 22 20 19 20 21 20 19 17
22E | 5 10 8 13 8 4 8 6 12 7 3 | 32 34 34 37 35 32 33 33 33 31 33
23 | 8 11 12 9 10 5 8 6 9 8 3 | 58 57 54 57 60 55 58 60 58 60 57
24 | 7 8 8 8 8 4 8 3 7 6 2 | 22 23 21 19 18 21 25 21 19 18 20
25 | 8 9 8 5 8 4 10 5 11 11 3 | 23 27 24 24 23 24 28 21 24 23 22
26 | 6 8 21 7 7 5 9 5 8 9 3 | 25 30 34 26 26 28 30 26 27 25 26
27E | 7 11 6 12 11 4 9 5 11 8 3 | 19 20 18 24 18 19 18 17 19 21 17
X28 | 6 12 7 8 7 4 8 6 9 --- 3 | 23 27 20 24 21 22 27 22 21 --- 22
29E | 7 16 7 9 13 5 10 8 9 20 4 | 27 27 28 29 27 28 30 27 34 31 27
30 | 5 11 8 8 6 3 7 5 11 9 2 | 21 26 21 21 19 21 26 22 23 22 21
31 | 3 11 6 7 7 3 9 5 11 7 2 | 49 52 49 52 48 49 54 50 52 49 50
32E | 6 12 6 10 9 4 8 5 9 9 3 | 22 25 21 20 17 21 23 21 22 22 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 9 10 9 4 9 7 11 10 |T 28 60 58 29 28 28 60 28 28 29 27
WRMS | 6 13 9 10 9 4 9 6 10 9 |NE 27 75 73 27 27 27 75 27 27 28 26
MEDI | 6 11 8 9 8 4 8 6 10 9 |MD 24 27 24 25 23 24 27 26 24 25 23
Table 3.2197.5 GPS week: 2197 Day: 5 MJD: 59628.000
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 9 6 5 7 7 8 9 2 | 17 19 20 15 17 16 22 19 19 18 17
2 | 7 20 5 10 9 6 9 6 10 11 3 | 17 23 15 20 16 16 17 16 18 19 15
3 | 5 8 8 18 8 5 7 6 8 7 3 | 20 21 22 25 19 19 23 15 20 19 19
4E | 9 20 9 16 14 5 12 6 17 9 4 | 30 35 37 38 37 33 35 32 34 32 32
5 | 7 13 11 10 7 7 7 10 9 13 3 | 24 27 26 28 22 25 26 21 24 25 23
6 | 5 10 7 7 5 4 7 6 14 10 2 | 19 21 20 20 18 18 21 17 22 18 18
7 | 5 11 7 9 8 4 8 5 8 7 2 | 35 36 36 37 35 34 37 38 35 36 35
8E | 7 18 5 12 14 9 12 6 11 12 3 | 24 24 23 22 23 22 21 17 24 23 21
9E | 9 8 6 11 13 7 8 8 8 8 3 | 22 22 20 25 18 23 21 24 21 21 19
10 | 4 7 6 10 6 4 6 4 7 6 2 | 23 24 25 26 23 25 27 21 25 22 23
X11 | 8 15 12 13 10 4 12 8 15 --- 4 | 25 31 31 30 29 30 30 29 30 --- 28
12 | 8 18 7 6 7 5 6 6 10 8 3 | 28 31 26 26 23 26 29 24 28 25 26
13E | 12 17 6 24 10 8 9 6 10 9 4 | 97 95 95 102 96 97 96 94 95 100 97
14 | 6 10 8 8 11 3 8 11 12 11 3 | 926 743 743 924 925 926 743 929 927 742 925
15E | 7 22 9 16 12 7 8 6 11 9 3 | 26 26 28 35 31 29 27 24 30 30 27
16 | 7 18 4 9 8 4 7 5 8 6 3 | 12 16 13 18 14 13 15 13 18 13 12
17E | 5 13 10 10 9 6 8 10 11 13 3 | 35 37 37 34 35 36 36 37 39 36 34
X18 | 10 11 10 9 8 6 11 6 12 --- 3 | 19 26 24 26 24 24 25 24 26 --- 22
19E | 5 22 7 12 9 6 13 8 12 13 3 | 53 54 52 50 51 51 54 51 54 51 51
20 | 7 14 9 6 6 5 9 7 7 13 3 | 23 29 24 23 22 23 24 24 23 30 24
21 | 5 13 6 10 8 6 9 7 13 13 3 | 14 17 15 17 15 15 19 15 20 20 14
22E | 8 9 6 11 9 5 7 5 6 7 2 | 29 26 26 27 28 26 28 28 27 25 26
23 | 8 12 10 10 9 7 7 8 10 10 3 | 56 56 56 60 58 56 57 59 60 57 57
24 | 9 10 9 6 7 4 8 4 9 10 2 | 24 25 22 22 21 21 27 21 24 20 22
25 | 7 10 7 7 10 3 8 5 10 8 2 | 16 22 17 14 14 15 23 15 18 17 16
26 | 5 9 6 8 6 4 8 6 8 8 2 | 15 21 14 16 13 13 21 13 16 13 14
27E | 8 17 4 11 10 4 8 6 12 10 3 | 22 23 21 26 22 22 21 16 27 19 20
X28 | 7 12 6 12 7 4 8 6 12 --- 3 | 15 20 11 18 16 14 22 15 18 --- 14
29E | 9 15 7 9 12 5 9 7 18 12 3 | 23 25 25 22 24 23 27 28 27 29 24
30 | 4 8 7 7 7 4 7 4 10 9 2 | 17 23 19 20 16 17 24 18 18 21 18
31 | 4 11 7 6 8 3 9 5 13 9 2 | 36 40 37 36 34 36 42 35 35 34 36
32E | 7 12 5 13 13 5 9 9 5 11 3 | 21 25 20 27 17 21 25 20 21 18 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 7 11 9 5 8 7 11 10 |T 55 51 50 57 54 55 52 54 56 52 54
WRMS | 6 14 7 11 9 5 8 6 10 10 |NE 65 60 57 67 65 65 60 65 67 63 65
MEDI | 7 12 7 10 8 5 8 6 10 9 |MD 23 25 24 26 22 23 25 21 24 23 22
Table 3.2197.6 GPS week: 2197 Day: 6 MJD: 59629.000
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 8 9 7 4 9 6 7 7 2 | 18 21 22 19 20 20 24 20 21 20 19
2 | 5 13 5 9 7 3 8 7 6 11 2 | 19 19 17 22 18 18 18 18 20 20 17
3 | 6 8 9 11 7 3 9 6 8 7 2 | 24 22 25 22 21 22 24 18 19 23 21
4E | 11 24 9 18 16 5 12 6 14 8 4 | 32 40 39 41 41 38 37 35 36 37 35
5 | 8 8 6 7 8 4 6 8 11 12 3 | 28 26 27 29 26 28 29 22 31 25 25
6 | 6 9 6 8 5 4 8 6 11 8 2 | 20 22 19 19 18 19 21 18 22 18 18
7 | 5 10 8 9 9 3 8 6 9 7 2 | 55 58 55 56 51 55 59 58 54 55 55
8E | 6 11 5 11 9 5 12 9 11 8 3 | 32 31 33 35 32 35 34 30 40 32 32
9E | 7 7 5 12 13 4 9 9 7 8 3 | 25 23 21 30 17 23 24 23 21 22 21
10 | 5 7 7 8 7 3 8 5 8 8 2 | 28 28 31 30 28 29 30 25 28 27 28
X11 | 8 13 11 11 10 4 11 8 13 --- 4 | 35 36 33 34 39 34 34 37 37 --- 34
12 | 5 16 6 7 6 3 7 7 7 12 2 | 46 51 44 45 43 44 49 43 43 42 44
13E | 12 11 5 14 11 4 7 6 9 20 4 | 88 90 88 92 90 89 89 87 88 87 88
14 | 8 10 6 6 13 3 9 10 7 16 3 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 985 9999
15E | 9 14 10 13 13 6 10 7 13 11 3 | 40 36 39 44 40 38 37 35 42 36 38
16 | 7 19 5 8 9 5 8 6 8 6 3 | 16 19 16 18 16 16 18 17 17 18 15
17E | 7 12 8 9 9 6 10 8 10 14 3 | 43 45 44 42 44 45 44 47 46 47 44
X18 | 9 11 8 6 9 4 8 8 7 --- 3 | 30 33 30 31 32 30 33 31 35 --- 30
19E | 6 19 6 10 13 5 10 10 10 10 3 | 56 55 56 55 56 58 59 62 57 58 57
20 | 5 11 5 9 7 4 8 7 15 10 3 | 29 29 27 31 28 27 26 30 33 29 28
21 | 7 13 6 8 7 4 9 7 8 9 2 | 16 22 17 21 18 18 21 19 22 19 17
22E | 7 11 5 10 9 5 8 7 8 8 2 | 35 34 32 34 35 32 34 34 32 33 33
23 | 7 11 9 8 10 5 7 7 10 9 3 | 83 83 83 87 85 83 83 86 88 86 84
24 | 9 9 8 7 7 3 7 5 7 9 2 | 30 29 26 26 25 26 30 25 25 23 25
25 | 5 11 5 9 8 3 9 5 8 7 2 | 21 29 25 24 22 24 28 23 23 24 23
26 | 5 9 8 8 7 4 8 7 7 6 2 | 25 29 24 25 24 24 29 25 24 25 24
27E | 7 11 6 9 11 3 10 5 9 11 3 | 31 33 32 35 30 33 33 28 39 31 31
X28 | 7 12 6 6 9 4 7 8 10 --- 3 | 20 22 16 19 19 18 23 18 19 --- 17
29E | 8 19 6 10 11 5 7 11 9 15 3 | 29 27 28 28 24 26 28 32 28 30 27
30 | 5 11 7 7 8 3 9 5 7 7 2 | 22 26 21 21 18 21 27 22 19 22 21
31 | 4 10 6 6 7 2 8 5 8 9 2 | 57 59 56 58 51 55 59 53 57 52 55
32E | 8 10 4 10 11 5 9 8 7 10 3 | 25 23 23 25 17 22 24 22 23 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 7 10 9 4 9 7 9 10 |T 34 35 33 35 33 33 35 33 35 67 33
WRMS | 6 13 7 9 9 4 9 6 9 9 |NE 31 33 30 31 30 30 33 30 31 84 30
MEDI | 7 11 6 9 9 4 8 7 8 9 |MD 29 29 28 30 28 28 30 28 31 29 28
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 4.2197 GPS week: 2197 MJD: 59623.0-59629.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 |U 10 10 27 |U 13 17 49 |U 9 11 21 |
emr | emr 3058 |U 17 18 34 |U 16 19 72 |U 18 17 39 |
esa | esa 3058 | 16 17 34 | 13 15 60 | 12 10 29 |
gfz | gfz 3069 |U 9 11 24 |U 13 14 46 |U 10 10 23 |
grg | grg 3069 |U 9 16 27 |U 15 17 49 | 10 12 26 |
igr | igr 3056 | 11 11 26 | 12 14 51 | 10 9 24 |
igs | igs 3067 | 11 11 27 | 12 15 51 | 10 10 24 |
jpl | jpl 3058 | 16 17 33 |U 14 17 66 | 14 18 34 |
mit | mit 3072 |U 10 14 26 |U 13 16 47 |U 10 10 24 |
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 5.2197.0 GPS week: 2197 Day: 0 MJD: 59623.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 6 22 | 11 18 46 | 8 6 18 |
emr | emr 3072 | 17 11 27 | 15 19 73 | 17 14 33 |
esa | esa 3072 | 16 15 31 | 12 15 58 | 12 7 26 |
gfz | gfz 3072 | 8 5 20 | 11 14 45 | 11 8 22 |
grg | grg 3072 | 9 8 25 | 11 18 43 | 9 11 21 |
igr | igr 3062 | 10 6 22 | 11 14 48 | 10 7 22 |
igs | igs 3072 | 9 7 22 | 11 14 50 | 9 7 24 |
jpl | jpl 3072 | 15 15 30 | 13 16 67 | 15 13 35 |
mit | mit 3072 | 9 8 22 | 11 16 48 | 12 11 27 |
Table 5.2197.1 GPS week: 2197 Day: 1 MJD: 59624.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 9 22 | 10 17 50 | 8 11 18 |
emr | emr 3072 | 19 9 26 | 12 15 78 | 16 16 36 |
esa | esa 3072 | 18 16 33 | 10 11 63 | 11 11 24 |
gfz | gfz 3072 | 10 8 18 | 11 13 52 | 10 10 20 |
grg | grg 3069 | 10 12 28 | 8 12 49 | 9 15 29 |
igr | igr 3072 | 12 8 20 | 9 12 57 | 9 8 19 |
igs | igs 3072 | 12 9 20 | 9 13 56 | 8 11 22 |
jpl | jpl 3072 | 17 15 29 | 10 15 70 | 14 21 34 |
mit | mit 3072 | 11 9 19 | 10 14 54 | 9 8 18 |
Table 5.2197.2 GPS week: 2197 Day: 2 MJD: 59625.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 | 15 23 40 | 23 18 52 | 9 13 19 |
emr | emr 2976 | 20 23 52 | 25 28 76 | 16 16 44 |
esa | esa 2976 | 17 28 45 | 20 25 59 | 13 13 29 |
gfz | gfz 3055 | 10 24 35 | 20 20 39 | 10 12 21 |
grg | grg 3055 | 9 30 31 | 17 18 36 | 11 13 23 |
igr | igr 2972 | 15 25 36 | 20 19 43 | 11 13 23 |
igs | igs 3043 | 12 22 38 | 19 21 43 | 10 12 23 |
jpl | jpl 2976 | 18 26 46 | 21 25 61 | 16 20 31 |
mit | mit 3072 | 9 41 29 | 21 21 37 | 9 10 21 |
Table 5.2197.3 GPS week: 2197 Day: 3 MJD: 59626.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 9 31 | 11 20 54 | 9 10 20 |
emr | emr 3072 | 14 12 34 | 12 19 68 | 16 17 37 |
esa | esa 3072 | 16 15 36 | 11 16 64 | 12 9 24 |
gfz | gfz 3072 | 9 9 29 | 11 16 49 | 9 9 20 |
grg | grg 3072 | 10 17 31 | 10 21 54 | 9 12 24 |
igr | igr 3072 | 10 8 30 | 10 16 56 | 10 8 21 |
igs | igs 3072 | 10 9 31 | 10 17 56 | 9 9 21 |
jpl | jpl 3072 | 17 15 41 | 12 16 69 | 14 21 33 |
mit | mit 3072 | 11 11 33 | 11 18 53 | 9 9 21 |
Table 5.2197.4 GPS week: 2197 Day: 4 MJD: 59627.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 7 25 | 13 13 41 | 11 13 26 |
emr | emr 3072 | 19 22 43 | 17 19 64 | 20 17 44 |
esa | esa 3072 | 19 17 37 | 13 11 50 | 14 11 36 |
gfz | gfz 3072 | 12 9 28 | 12 12 38 | 10 12 28 |
grg | grg 3072 | 10 13 30 | 13 12 36 | 11 12 30 |
igr | igr 3072 | 14 12 30 | 12 11 43 | 12 11 30 |
igs | igs 3072 | 14 11 32 | 13 11 40 | 11 11 29 |
jpl | jpl 3072 | 21 19 34 | 13 14 54 | 15 15 37 |
mit | mit 3072 | 12 8 26 | 13 12 41 | 11 10 28 |
Table 5.2197.5 GPS week: 2197 Day: 5 MJD: 59628.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 10 26 | 11 16 38 | 11 12 23 |
emr | emr 3072 | 15 23 30 | 13 17 73 | 20 19 40 |
esa | esa 3072 | 16 17 32 | 10 13 57 | 13 11 33 |
gfz | gfz 3072 | 9 11 23 | 9 11 37 | 11 12 27 |
grg | grg 3072 | 9 14 23 | 9 13 34 | 12 12 28 |
igr | igr 3072 | 10 10 24 | 9 13 42 | 12 10 28 |
igs | igs 3072 | 9 11 25 | 9 14 44 | 11 11 27 |
jpl | jpl 3072 | 14 15 25 | 13 16 63 | 13 17 34 |
mit | mit 3072 | 9 12 28 | 9 14 36 | 13 11 29 |
Table 5.2197.6 GPS week: 2197 Day: 6 MJD: 59629.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 10 23 | 16 21 59 | 9 10 22 |
emr | emr 3072 | 15 24 27 | 16 16 75 | 17 19 37 |
esa | esa 3072 | 12 12 26 | 15 17 72 | 12 9 30 |
gfz | gfz 3072 | 8 8 16 | 14 15 64 | 10 10 24 |
grg | grg 3072 | 8 18 19 | 36 24 92 | 9 10 29 |
igr | igr 3072 | 8 7 19 | 15 16 66 | 9 9 25 |
igs | igs 3072 | 7 9 19 | 14 17 67 | 9 9 24 |
jpl | jpl 3072 | 12 11 24 | 16 15 81 | 13 17 31 |
mit | mit 3072 | 9 9 22 | 15 17 63 | 11 10 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 6.2197 GPS week: 2197 MJD: 59623.500-59629.500
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 | 2 -5 47 -22 -2 | 7 17
| 19 13 53 41 3 | 4
emr uuuuu | 14 10 -65 255 2 | -11 25
| 15 23 161 70 10 | 4
esa uuuuu | 1 19 -39 -69 -4 | 16 23
| 9 17 45 38 3 | 5
gfz uuuuu | -15 -2 81 -55 6 | 14 20
| 8 23 75 51 7 | 2
grg uuuuu | 14 14 51 21 3 | 4 17
| 10 9 41 67 3 | 4
igr xxxxx | 6 3 0 -43 -2 | -3 17
| 10 7 45 39 8 | 5
irf xxxxx | 2 13 11 26 -4 | 0 16
| 11 10 21 7 7 | 5
jpl uuuuu | 37 8 19 8 -3 | 22 29
| 9 16 60 36 5 | 4
mit uuuuu | -10 -25 -29 23 -7 | 23 28
| 28 52 63 41 5 | 4
ngs uuuuu | -41 -3 -70 -48 -1 | 7 17
| 24 33 83 114 4 | 4
sio xxxxx | 51 64 -19 20 12 | 40 45
| 70 54 111 134 8 | 4
Table 7.2197.0 GPS week: 2197 Day: 0 MJD: 59623.500
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 | -11 -31 -66 33 -5 | 13 22
emr uuuuu | 26 7 162 236 6 | -5 27
esa uuuuu | -11 4 -1 -60 -3 | 24 30
gfz uuuuu | -12 -32 166 -26 5 | 16 23
grg uuuuu | 6 15 38 -57 0 | 10 22
igr xxxxx | 20 6 58 -37 -11 | 6 21
irf xxxxx | 22 9 4 20 -12 | 7 19
jpl uuuuu | 50 14 137 23 0 | 29 40
mit uuuuu | 36 6 -101 71 1 | 28 33
ngs uuuuu | -76 21 -167 -140 -1 | 12 21
sio xxxxx | 103 103 129 -43 15 | 37 42
Table 7.2197.1 GPS week: 2197 Day: 1 MJD: 59624.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 21 -3 85 -24 -4 | 9 17
emr uuuuu | 28 15 30 386 -7 | -9 25
esa uuuuu | 11 6 -100 -64 -9 | 20 25
gfz uuuuu | -16 1 126 -44 11 | 13 19
grg uuuuu | 4 -2 -23 20 4 | 7 18
igr xxxxx | 14 9 -40 -49 -9 | 0 15
irf xxxxx | 8 25 -5 22 -5 | 3 16
jpl uuuuu | 41 41 1 69 -8 | 23 31
mit uuuuu | -35 -41 3 -8 -2 | 25 29
ngs uuuuu | -42 -1 -104 -158 1 | 9 18
sio xxxxx | -20 78 12 -126 10 | 36 41
Table 7.2197.2 GPS week: 2197 Day: 2 MJD: 59625.500
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 | 2 -4 41 -21 -2 | 6 18
emr uuuuu | 8 -4 -43 195 7 | -13 28
esa uuuuu | 10 12 -25 -139 -6 | 17 25
gfz uuuuu | -20 1 170 -133 10 | 13 19
grg uuuuu | 0 12 58 81 0 | 4 18
igr xxxxx | 1 0 -29 -8 -2 | -5 18
irf xxxxx | 2 17 -7 17 -4 | 1 18
jpl uuuuu | 43 -1 38 9 -5 | 20 30
mit uuuuu | -11 4 -78 11 -5 | 24 29
ngs uuuuu | -42 -21 -143 119 -2 | 7 18
sio xxxxx | 173 10 -228 -160 28 | 37 41
Table 7.2197.3 GPS week: 2197 Day: 3 MJD: 59626.500
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 -15 75 -76 3 | 9 18
emr uuuuu | 7 18 -174 264 -12 | -7 23
esa uuuuu | -11 7 -13 -47 1 | 19 26
gfz uuuuu | -3 -15 76 0 15 | 17 22
grg uuuuu | 21 8 79 -7 1 | 7 19
igr xxxxx | 6 -3 -23 -5 10 | -2 16
irf xxxxx | 1 10 3 32 -12 | 4 17
jpl uuuuu | 27 1 26 -10 -6 | 25 30
mit uuuuu | -16 23 -53 -34 -8 | 27 31
ngs uuuuu | -24 -35 -48 71 -2 | 10 19
sio xxxxx | 52 149 13 155 7 | 44 48
Table 7.2197.4 GPS week: 2197 Day: 4 MJD: 59627.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 13 4 86 -19 2 | 6 14
emr uuuuu | -6 -9 -87 302 -4 | -14 21
esa uuuuu | -2 38 -97 -98 -1 | 15 20
gfz uuuuu | -18 -12 29 -9 -5 | 16 20
grg uuuuu | 19 15 87 50 4 | 3 14
igr xxxxx | -1 11 -21 -19 5 | -5 14
irf xxxxx | -14 19 1 28 -5 | -1 14
jpl uuuuu | 33 4 15 -10 -5 | 21 26
mit uuuuu | -24 -32 -71 -3 -11 | 23 26
ngs uuuuu | -14 -1 33 -94 4 | 6 14
sio xxxxx | 40 73 -66 49 12 | 43 47
Table 7.2197.5 GPS week: 2197 Day: 5 MJD: 59628.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -35 7 53 21 -5 | 2 13
emr uuuuu | 33 56 -345 191 16 | -17 24
esa uuuuu | 6 49 -49 -43 -6 | 11 18
gfz uuuuu | -27 44 1 -115 -1 | 12 18
grg uuuuu | 19 21 91 -58 5 | -1 14
igr xxxxx | 9 7 72 -64 -7 | -8 16
irf xxxxx | -4 16 50 25 3 | -6 16
jpl uuuuu | 42 0 -38 -47 8 | 17 23
mit uuuuu | 20 -133 72 70 -13 | 18 24
ngs uuuuu | -69 55 43 12 1 | 3 13
sio xxxxx | -31 43 42 189 9 | 42 46
Table 7.2197.6 GPS week: 2197 Day: 6 MJD: 59629.500
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 4 52 -70 0 | 2 14
emr uuuuu | 3 -12 2 215 8 | -15 22
esa uuuuu | 5 17 12 -28 -2 | 10 18
gfz uuuuu | -6 0 -4 -59 4 | 11 18
grg uuuuu | 28 25 25 119 9 | -1 13
igr xxxxx | -9 -8 -14 -116 -2 | -9 17
irf xxxxx | 2 -5 31 37 6 | -6 16
jpl uuuuu | 26 -2 -43 22 -4 | 17 24
mit uuuuu | -36 -6 23 52 -12 | 17 24
ngs uuuuu | -18 -41 -102 -143 -8 | 3 13
sio xxxxx | 39 -9 -33 74 5 | 44 47
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