[IGSREPORT-27178] Wk 2097 IGS Final Orbits
acc
acc at igs.org
Sun Apr 5 15:41:48 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2097 (Mar 15, 2020 - Mar 21, 2020)
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:
igs2097[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2097[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2097[0-6].cls IGS GPS clock combination summary report.
igs20977.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20977.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 | TIXI TIXI
0 | EMR | SYOG HERS SYOG
0 | ESA | PTBB AREG PTBB
0 | GFZ | 4 4 BJNM POHN BJNM POHN
0 | GRG | CCJ2 CCJ2 DARW
1 | COD | TIXI IISC PETS TIXI
1 | EMR | 24 24 SYOG SYOG
1 | ESA | BAKE PTBB SGOC WIND BAKE PTBB SGOC WIND
1 | GFZ | 4 4 BAKE GLPS GODE POHN SUTH GLPS GODE POHN SUTH
1 | JPL | MONP POLV MONP POLV
1 | MIT | PETS
2 | EMR | SYOG YELL SYOG YELL
2 | ESA | DJIG PDEL WIND DJIG PDEL WIND
2 | GFZ | 4 18 4 18 BJNM MAL2 PIE1 POHN BJNM PIE1 POHN
2 | GRG | PIE1 VILL PIE1 VILL
2 | MIT | 18
3 | COD | TIXI ZECK TIXI
3 | EMR | SYOG SYOG
3 | ESA | DAV1 LPGS PTBB DAV1 LPGS PTBB WIND
3 | GFZ | 4 4 BAKE BJNM FLRS GODE POHN SPT0 BAKE BJNM FLRS
3 | GFZ | GODE MAL2 POHN SAVO SPT0
3 | GRG | BAKE NRMD BAKE NRMD
3 | JPL | MOBS
3 | MIT | BJNM
4 | COD | 8 23 8 23 SGOC WIND BJNM SGOC WIND
4 | EMR | 8 9 32 8 9 32 SYOG NLIB SYOG
4 | ESA | AUCK KIRU SCOR SGOC AUCK KIRU SCOR SGOC
4 | GFZ | 4 4 13 18 BJNM POHN POHN
4 | GRG | BAKE WIND ULAB WIND
5 | COD | 27 32 27 32 NOVM TIXI ZAMB NOVM TIXI ZAMB
5 | EMR | 27 8 27 SYOG SYOG
5 | ESA | NRIL PTBB WIND NRIL PTBB
5 | GFZ | 4 18 4 18 FAA1 POHN WIND ZAMB FAA1 POHN ZAMB
5 | GRG | 29 29 ULAB ULAB
5 | JPL | 32 32 BRFT POLV
6 | COD | TIXI TIXI
6 | EMR | 27 27 SYOG HARB SYOG
6 | ESA | PTBB PTBB
6 | GFZ | 4 18 4 18 BJNM GODE POHN BJNM GODE POHN
6 | GRG | 13
6 | JPL | POLV
6 | MIT | BJNM MAW1 RBAY
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
5 | GRG | 8
6 | GRG | 8
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.8 .0 .3 1 14 21 .11
EMR | 0 | -.3 -5.4 11.6 -37 32 -7 .53
ESA | 0 | 1.3 -1.4 -.7 -19 43 83 .14
GFZ | 0 | -.2 -.1 .0 29 11 53 .24
GRG | 0 | -1.4 -1.5 1.6 75 25 87 .36
JPL | 0 | 3.4 -8.8 10.3 0 -1 1 .06
MIT | 0 | -1.2 -.3 9.6 4 1 1 .38
NGS | 0 | -1.2 -8.6 7.1 -39 68 -17 .46
SIO | 0 | -3.0 -8.3 -13.1 -10 3 -4 .17
COD | 1 | -1.0 .3 .6 2 21 24 -.05
EMR | 1 | -2.5 -8.1 9.8 -36 16 22 .25
ESA | 1 | 1.2 -.8 -.2 -14 46 91 -.12
GFZ | 1 | -.0 -.4 .5 12 3 59 -.04
GRG | 1 | 3.4 -.4 8.4 87 13 95 .17
JPL | 1 | 6.4 -9.7 13.2 21 12 10 -.29
MIT | 1 | 3.6 -2.6 11.1 -3 1 14 .13
NGS | 1 | -1.3 -9.5 .7 -69 71 -24 .14
SIO | 1 | -1.3 -7.8 -9.8 14 5 21 .0
COD | 2 | -.8 .1 .4 4 9 23 -.20
EMR | 2 | .2 4.4 11.1 -41 -2 -29 .23
ESA | 2 | 1.6 -.7 -.3 -28 41 89 -.05
GFZ | 2 | -.1 -.2 .7 21 2 63 .01
GRG | 2 | 5.3 -.8 9.3 107 15 94 -.10
JPL | 2 | 10.8 -2.7 7.8 6 -3 3 -.01
MIT | 2 | 2.1 -.3 7.5 3 -7 -3 .06
NGS | 2 | 5.9 -2.5 13.6 20 -17 -26 .05
SIO | 2 | 3.0 -10.1 -5.6 1 -9 12 -.08
COD | 3 | -.7 -.3 -.1 -4 -4 13 -.06
EMR | 3 | 5.6 2.9 15.4 -33 18 -15 .34
ESA | 3 | 2.0 -1.9 -.3 -55 43 101 .17
GFZ | 3 | -.4 -.4 .3 25 6 53 .16
GRG | 3 | 3.5 -6.1 12.0 53 -9 104 .33
JPL | 3 | 7.0 -2.8 9.1 5 -5 -1 -.10
MIT | 3 | 2.1 1.7 7.2 -7 25 16 .24
NGS | 3 | 6.6 -2.0 5.9 7 20 -4 .42
SIO | 3 | 5.0 -5.8 -9.5 11 -15 -2 .23
COD | 4 | -.8 -.3 -.2 2 11 16 .03
EMR | 4 | 1.8 7.1 23.6 -34 2 -20 .32
ESA | 4 | 1.0 -1.9 -1.3 -38 39 81 .01
GFZ | 4 | -.0 -.0 .5 35 7 50 -.01
GRG | 4 | 4.8 -6.5 8.0 63 36 98 .32
JPL | 4 | 9.3 -1.9 15.3 -5 6 5 -.27
MIT | 4 | 1.8 -5.3 7.8 -8 4 -13 .28
NGS | 4 | 5.7 -3.8 8.8 3 -16 -1 .30
SIO | 4 | 2.9 -7.3 -7.0 6 7 7 .26
COD | 5 | -1.0 .6 -.4 35 22 20 .20
EMR | 5 | .5 3.8 17.4 -51 11 -44 .30
ESA | 5 | 1.3 -1.5 -.9 -41 24 100 .02
GFZ | 5 | -.6 -.1 -.2 42 12 61 .16
GRG | 5 | 1.1 -4.7 9.2 107 15 128 .11
JPL | 5 | 2.6 -12.5 16.8 -14 -12 -1 -.09
MIT | 5 | 1.5 -2.4 8.3 -6 6 9 .29
NGS | 5 | -1.5 -4.7 11.2 0 29 11 .31
SIO | 5 | .8 -7.4 -2.6 26 9 14 .32
COD | 6 | -.5 .1 .8 11 30 -7 -.15
EMR | 6 | -3.9 .3 14.2 -56 44 -69 .25
ESA | 6 | 1.1 -1.8 -.4 -35 47 70 .04
GFZ | 6 | -.2 -.1 .4 23 18 47 .05
GRG | 6 | -.8 .4 14.6 109 5 120 .13
JPL | 6 | 9.7 -14.5 10.3 -17 -13 5 -.18
MIT | 6 | -1.2 .2 8.2 4 14 -7 .29
NGS | 6 | 1.0 -1.1 13.1 50 31 -15 .18
SIO | 6 | .3 -4.8 1.6 42 -18 -1 .27
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.2097.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2097.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 2.2097.[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 3.2097.[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 5.2097.0-6). 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 2097 summary. (Mar 15, 2020 - Mar 21, 2020)
Table 1.2097.a GPS week: 2097 MJD: 58923.000-58929.000
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 254| 0 0 -2 4 -9 -3 -.03 10 9 | -780 202 6 105
| 0 1 1 11 16 18 .05 | 186 380
emr 81| 0 3 4 -4 17 4 -.01 12 12 | 213308 -425 15 114
| 1 3 2 15 22 31 .08 | 796 729
esa 149| 0 0 1 -25 -1 18 -.06 10 10 | -1419 1159 9 93
| 0 0 2 24 19 15 .03 | 380 543
gfz 182| 0 0 0 -20 -1 -1 .04 14 12 | -57 -199 12 113
| 1 0 1 15 20 14 .03 | 294 373
grg 94| 1 0 -2 -11 -8 0 -.13 11 9 | 46 25 9 127
| 0 1 3 15 17 22 .03 | 192 303
igr n/a| 0 0 -1 0 -16 -24 .02 4 4 | 6903 -715 11 69
| 0 0 1 13 11 14 .01 | 1234 873
jpl 80| 0 0 3 10 -7 9 .25 8 8 | 213333 -416 8 80
| 1 2 2 10 25 20 .05 | 800 738
mit 374| 0 0 -2 19 10 6 -.03 9 8 | 5669 -177 69 1688
| 0 0 1 34 27 32 .03 | 2129 1434
ngs 206| 0 0 0 21 4 -26 -.01 9 8 | -768 131 929 2068
| 0 1 1 16 18 31 .03 | 219 375
sio 420| 0 -1 -3 -15 -4 -2 -.05 17 16 | --- --- --- ---
| 0 1 1 23 21 20 .06 | --- ---
Table 1.2097.b GPS week : 2097 MJD: 58923.000-58929.000
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 | 4 3 4 4 4 4 4 |
3 | 3 3 3 4 3 3 3 |
4 | 7 8 8 8 8 8 10 |
5 | 4 3 4 4 3 4 4 |
6 | 3 3 3 3 4 3 3 |
7 | 4 4 4 4 4 4 3 |
8 | 5 6 5 6 7 9 6 |
9 | 4 5 5 5 9 6 5 |
10 | 3 3 3 3 4 4 3 |
11 | 4 4 4 4 4 5 4 |
12 | 3 4 4 4 4 4 4 |
13 | 4 4 4 4 4 4 4 |
14 | 3 4 4 3 4 5 4 |
15 | 4 4 5 4 4 4 4 |
16 | 3 4 4 4 4 4 4 |
17 | 3 4 4 4 4 4 4 |
18 | 0 0 6 7 7 6 5 |
19 | 4 4 4 3 4 3 3 |
20 | 3 3 4 4 4 4 3 |
21 | 3 3 4 3 3 4 3 |
22 | 3 3 3 4 4 4 3 |
23 | 4 6 6 7 6 5 4 |
24 | 3 3 3 3 3 3 4 |
25 | 3 3 3 3 3 4 3 |
26 | 3 3 5 3 3 3 3 |
27 | 6 6 6 5 6 7 9 |
28 | 3 3 3 4 4 4 3 |
29 | 4 5 5 4 5 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 4 3 4 4 0 4 4 |
32 | 4 5 5 5 12 7 5 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2097.0 GPS week: 2097 Day: 0 MJD: 58923.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| 0 0 -1 -9 -10 -18 -.01 10 8 | -389 -490 6 102
emr 81| 1 0 3 -7 19 -27 -.12 13 13 | 214607 -1261 16 121
esa 149| 0 0 2 -17 1 -6 -.01 11 11 | -798 144 9 89
gfz 183| -1 0 -1 -31 19 -21 .08 13 11 | -217 -424 11 123
grg 97| 0 0 -6 -29 -7 23 -.10 9 9 | 97 -92 9 136
igr n/a| -1 0 0 -5 -18 -41 .03 4 4 | 8462 -1223 10 65
jpl 80| 0 0 6 5 -14 4 .22 8 8 | 214637 -1249 8 90
mit 374| 0 0 0 42 -8 47 -.02 6 6 | 1475 2413 181 1408
ngs 208| 0 0 0 -2 14 -28 .02 8 7 | -307 -608 1104 2278
sio 423| 0 -1 -4 -29 -9 -18 -.13 17 17 | --- --- --- ---
Table 2.2097.1 GPS week: 2097 Day: 1 MJD: 58924.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| -1 -2 0 -8 11 -18 .04 12 10 | -967 617 7 97
emr 81| 0 0 1 -10 13 2 -.09 12 12 | 213391 581 15 117
esa 149| 0 0 4 -29 10 27 -.06 10 11 | -1281 820 10 79
gfz 183| 0 0 -2 -32 -13 -6 .04 13 10 | -438 381 14 95
grg 97| 1 0 -6 -9 -13 11 -.13 10 9 | -211 347 10 142
igr n/a| 0 0 0 -27 -21 -27 .04 4 4 | 7323 839 10 66
jpl 80| -1 0 5 14 9 5 .26 9 9 | 213414 605 9 83
mit 374| 0 0 -1 23 -1 21 -.01 6 6 | 7139 805 34 1784
ngs 203| 0 0 0 20 -15 -35 .00 9 8 | -965 612 1075 2061
sio 416| -1 0 -3 -1 -1 3 -.09 18 16 | --- --- --- ---
Table 2.2097.2 GPS week: 2097 Day: 2 MJD: 58925.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| 0 -1 -3 5 3 -2 -.01 11 10 | -823 582 7 110
emr 81| 0 4 2 9 -12 -21 -.00 12 12 | 213833 -544 16 112
esa 149| 0 -1 2 -34 21 29 -.11 12 11 | -1858 1769 11 98
gfz 183| -1 -1 0 -40 -14 3 .05 15 15 | -161 -206 14 96
grg 94| 1 0 -1 9 23 -12 -.11 9 8 | -43 93 8 117
igr n/a| 0 0 -2 13 3 -29 .02 5 5 | 7900 -737 11 70
jpl 80| -1 1 2 15 -12 17 .24 7 7 | 213866 -543 9 70
mit 374| 0 0 -2 -2 -3 6 -.01 9 8 | 7397 -511 44 1714
ngs 207| 0 0 2 42 -13 -47 -.00 11 10 | -743 64 840 2060
sio 422| 0 -1 -6 -50 -10 31 -.12 17 16 | --- --- --- ---
Table 2.2097.3 GPS week: 2097 Day: 3 MJD: 58926.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| 0 -1 -5 -3 -33 -13 -.02 10 9 | -902 376 5 101
emr 81| 1 6 4 9 4 -3 -.01 12 12 | 213462 -452 14 126
esa 149| 0 -1 1 -61 0 40 -.04 9 9 | -1271 1229 9 82
gfz 180| 0 -1 -1 -10 -22 -7 .06 14 16 | 1 -113 14 132
grg 95| 2 0 2 -26 -22 -21 -.11 10 9 | 84 119 8 127
igr n/a| 0 0 -1 1 -24 -16 .02 4 4 | 7334 -678 11 67
jpl 80| -1 1 3 20 -35 -30 .18 9 9 | 213499 -457 9 77
mit 374| 0 0 -1 71 65 26 -.01 10 9 | 7297 -660 81 1931
ngs 206| 0 -2 -2 12 28 21 .02 9 7 | -936 346 592 1929
sio 421| 0 -2 -3 10 -1 -20 -.03 17 16 | --- --- --- ---
Table 2.2097.4 GPS week: 2097 Day: 4 MJD: 58927.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| -1 -1 -2 15 -25 0 -.12 10 9 | -845 58 7 115
emr 81| 0 8 8 6 4 -6 .00 13 13 | 213103 -1071 18 108
esa 149| 0 -1 -2 -25 -38 5 -.04 9 9 | -1351 1137 10 119
gfz 183| 0 0 -2 -23 -17 9 .05 12 11 | 430 -732 13 91
grg 95| 1 -1 -1 -13 1 -33 -.14 9 9 | 369 -546 10 108
igr n/a| 0 -1 -4 6 -28 -31 .02 4 4 | 6739 -1420 12 78
jpl 80| -1 3 5 21 41 16 .26 7 7 | 213113 -1083 9 83
mit 374| 0 -1 -4 -14 -3 20 -.02 12 11 | 6518 -1494 62 1753
ngs 211| 1 -2 0 39 22 -17 -.04 10 9 | -836 99 1097 1934
sio 420| 0 -1 -3 -31 -16 6 -.02 18 16 | --- --- --- ---
Table 2.2097.5 GPS week: 2097 Day: 5 MJD: 58928.000
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 252| 0 0 -2 17 -11 -7 -.03 10 9 | -776 50 8 108
emr 81| 1 4 7 -33 33 27 .06 13 12 | 212215 538 14 107
esa 149| 0 -1 1 -29 -11 10 -.08 10 8 | -1910 1475 10 87
gfz 182| -2 0 1 3 6 -12 .03 14 12 | 207 -430 12 103
grg 92| 0 0 -4 -20 -26 7 -.16 10 10 | -123 320 11 133
igr n/a| 0 0 -2 0 -23 -27 .01 4 4 | 5497 -77 13 67
jpl 80| 1 0 4 0 -16 11 .31 9 9 | 212246 565 9 85
mit 374| 0 -1 -4 40 31 -30 -.09 11 10 | 5032 -18 49 1547
ngs 206| 0 -1 0 28 -10 0 -.01 8 8 | -837 157 743 1926
sio 419| 0 0 -4 10 39 6 -.00 18 17 | --- --- --- ---
Table 2.2097.6 GPS week: 2097 Day: 6 MJD: 58929.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| 0 0 -2 14 1 35 -.04 8 8 | -761 222 8 102
emr 81| -1 3 4 -6 56 64 .09 12 12 | 212551 -771 15 112
esa 149| 0 0 0 19 7 22 -.07 9 8 | -1466 1543 8 97
gfz 183| 0 0 0 -10 30 22 -.01 13 11 | -227 127 11 152
grg 94| 2 1 -1 9 -15 21 -.17 17 10 | 151 -61 10 129
igr n/a| 0 0 -1 10 -6 3 .02 4 4 | 5070 -1714 11 72
jpl 80| 2 -3 0 -4 -24 38 .31 9 9 | 212559 -753 9 76
mit 374| 0 0 -2 -22 -8 -43 -.06 8 7 | 4830 -1778 35 1679
ngs 205| 0 0 3 9 1 -75 -.04 8 6 | -756 250 1056 2289
sio 420| 0 0 -1 -14 -31 -25 .02 17 15 | --- --- --- ---
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 3.2097.0 GPS week: 2097 Day: 0 MJD: 58923.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 7 8 11 6 3 7 7 6 12 2 | 20 22 21 19 21 20 26 20 22 23 21
2 | 12 8 12 8 9 3 9 5 12 21 3 | 22 15 17 19 18 16 18 18 20 24 16
3 | 9 9 10 9 8 4 7 6 8 9 3 | 26 28 29 25 27 27 28 24 26 27 25
X4E | 10 --- 13 19 --- 5 21 5 13 39 6 | 40 --- 43 48 --- 41 44 44 41 49 42
5 | 7 15 11 7 12 4 8 7 8 17 3 | 35 35 40 41 39 38 38 34 40 32 36
6 | 6 10 10 8 6 4 7 4 6 9 2 | 23 24 24 23 21 23 26 21 23 26 22
7 | 8 10 8 7 10 3 9 5 6 28 3 | 109 109 111 106 105 108 111 107 112 107 108
8E | 10 20 15 24 9 3 9 9 10 13 4 | 80 80 76 81 76 78 42 80 76 79 78
9E | 9 15 18 11 14 6 7 7 8 18 4 | 69 70 72 71 71 68 68 71 68 69 69
10 | 11 8 11 7 6 5 8 5 8 15 3 | 20 21 26 24 22 23 24 20 23 29 21
11 | 7 11 14 19 12 4 7 7 6 16 3 | 20 28 17 35 23 24 30 23 26 20 24
12 | 7 18 9 6 11 3 8 5 8 18 3 | 27 32 28 28 29 26 32 27 27 24 27
13E | 9 18 8 8 12 5 7 5 9 20 3 | 33 37 34 35 31 33 32 30 35 37 32
14E | 15 10 9 8 12 4 9 5 7 12 3 | 41 42 36 41 37 38 37 37 39 37 38
15E | 8 13 10 14 12 4 8 5 10 19 3 | 91 94 91 94 89 93 92 90 93 92 91
16 | 6 13 7 7 9 3 7 5 5 26 3 | 16 16 17 16 19 16 18 15 16 24 15
17E | 10 13 10 8 9 3 8 4 9 17 3 | 44 36 36 41 40 38 38 38 42 38 38
X18 | 1 --- --- --- --- 175 --- --- --- --- 0 | 40 --- --- --- --- 101 --- --- --- --- 41
19E | 19 12 9 13 8 3 9 5 8 15 3 | 55 58 58 55 57 57 61 57 58 61 57
20 | 10 7 9 7 8 4 7 3 8 19 3 | 29 27 24 28 27 27 30 25 26 29 26
21 | 7 10 7 8 8 5 7 4 7 20 2 | 16 18 16 19 18 17 20 15 18 26 16
22 | 7 10 8 8 8 4 7 5 7 20 3 | 17 27 21 24 21 22 29 22 22 29 22
X23E | 8 24 6 15 8 6 10 7 11 --- 4 | 62 62 59 63 58 59 60 58 64 --- 60
24 | 10 9 11 12 7 4 7 4 9 8 3 | 24 28 28 32 22 26 30 23 25 27 25
25 | 6 8 12 10 9 4 7 4 9 10 3 | 16 18 18 21 16 17 21 16 16 19 16
26 | 10 10 9 7 8 3 6 4 7 11 2 | 23 19 23 20 19 19 22 19 21 21 19
27E | 12 18 17 44 8 6 9 10 9 11 6 | 47 48 50 53 54 50 26 49 50 50 49
28 | 7 12 6 6 7 3 7 5 7 24 3 | 23 25 21 21 19 21 25 20 23 28 20
29E | 6 15 9 10 9 3 9 8 6 19 3 | 77 77 78 77 82 77 79 77 79 80 77
30 | 8 12 9 8 8 3 7 7 5 18 3 | 31 34 35 30 28 30 34 29 33 28 30
31 | 10 15 8 7 8 4 9 6 9 24 3 | 29 26 24 27 19 29 29 23 24 26 28
32E | 23 13 16 10 10 4 10 7 9 11 4 | 53 50 49 53 49 48 32 49 46 48 48
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 11 13 9 4 8 6 8 17 |T 39 40 39 40 38 40 38 38 39 40 38
WRMS | 8 13 11 11 9 4 8 6 7 17 |NE 28 29 28 29 27 31 31 26 28 29 27
MEDI | 8 12 9 8 8 4 8 5 8 17 |MD 29 28 29 32 27 29 30 27 27 29 28
Table 3.2097.1 GPS week: 2097 Day: 1 MJD: 58924.000
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 9 8 9 4 3 7 6 5 12 2 | 20 20 20 18 20 19 25 18 21 22 19
2 | 10 10 6 8 10 3 8 5 7 23 3 | 18 15 16 17 16 16 17 18 21 22 15
3 | 7 7 10 10 7 4 9 6 7 12 2 | 19 20 21 17 19 20 25 17 20 24 19
X4E | 14 --- 12 26 --- 6 21 6 16 40 7 | 31 --- 32 43 --- 32 32 33 32 41 32
5 | 9 11 8 8 13 5 7 6 7 20 3 | 29 26 25 30 28 27 30 25 30 29 26
6 | 8 7 7 9 5 3 7 5 9 12 2 | 21 22 22 21 20 21 26 20 20 25 21
7 | 7 11 7 8 18 4 10 5 9 28 4 | 139 138 137 136 129 136 138 136 143 135 136
8E | 12 22 15 32 9 4 12 13 11 11 5 | 51 55 54 56 53 52 24 55 49 52 52
9E | 9 11 16 25 11 5 7 8 12 19 4 | 52 51 56 58 50 53 50 54 52 53 52
10 | 12 9 12 8 6 5 9 4 9 15 3 | 21 18 19 18 19 18 21 16 20 26 17
11 | 9 13 14 13 10 4 8 6 8 11 3 | 20 26 18 29 20 22 28 22 27 19 22
12 | 10 18 9 7 12 4 7 5 8 20 3 | 21 19 19 23 23 20 24 20 21 20 19
13E | 9 12 7 11 14 4 9 5 13 16 3 | 28 30 29 31 26 28 30 29 34 34 28
14E | 15 9 9 8 10 4 9 7 9 15 3 | 31 27 25 28 28 26 28 23 26 25 25
15E | 14 15 10 9 12 4 8 7 15 18 4 | 68 70 69 68 65 67 69 69 70 69 67
16 | 10 16 6 7 7 4 7 5 8 28 3 | 18 13 15 17 18 16 18 14 17 22 14
17E | 17 10 9 11 9 3 9 7 12 15 3 | 44 35 36 40 42 38 39 38 42 34 38
X18 | 2 --- --- --- --- 13 --- --- --- --- 0 | 25 --- --- --- --- 66 --- --- --- --- 26
19E | 25 13 9 12 9 4 9 6 7 15 4 | 44 52 54 51 48 53 52 50 52 53 50
20 | 11 8 9 8 7 4 9 5 7 19 3 | 25 22 20 23 22 22 27 21 18 25 21
21 | 15 9 8 8 8 4 6 5 7 22 3 | 23 15 13 19 16 15 19 14 16 25 15
22 | 9 9 7 8 9 5 7 5 7 18 3 | 14 19 17 14 17 15 24 17 17 22 16
X23E | 11 30 8 28 9 5 12 7 16 --- 6 | 42 42 40 54 42 41 40 41 44 --- 41
24 | 10 11 12 11 7 4 8 5 10 11 3 | 22 21 23 23 19 22 25 18 21 25 19
25 | 9 7 13 7 9 3 6 5 7 11 3 | 18 16 19 19 17 16 21 16 15 16 15
26 | 12 10 9 6 6 3 6 5 10 13 3 | 20 17 18 18 18 16 22 15 21 22 17
27E | 14 12 16 39 6 3 10 9 9 9 5 | 48 47 49 48 48 46 26 47 46 47 47
28 | 9 9 7 7 7 3 9 8 8 21 3 | 17 20 15 17 18 18 23 18 19 21 17
29E | 12 20 11 12 15 4 10 8 7 21 4 | 58 60 61 60 62 61 60 58 63 65 59
30 | 7 11 6 9 9 2 6 8 10 19 3 | 27 28 27 25 23 26 29 25 28 28 25
31 | 7 13 9 7 6 2 7 5 9 25 3 | 26 23 21 20 17 22 27 20 20 22 21
32E | 26 12 15 10 10 4 16 8 11 12 4 | 43 38 39 40 37 39 34 38 35 35 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 10 13 10 4 9 6 9 18 |T 33 33 33 34 32 34 33 32 34 35 32
WRMS | 10 12 11 10 9 4 9 6 8 16 |NE 27 26 25 26 25 27 29 24 27 28 25
MEDI | 10 11 9 9 9 4 8 6 9 16 |MD 25 23 23 25 22 22 27 22 26 25 22
Table 3.2097.2 GPS week: 2097 Day: 2 MJD: 58925.000
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 8 8 9 5 5 6 8 13 10 3 | 30 30 29 28 27 28 33 28 31 30 29
2 | 10 9 10 7 8 5 7 7 11 23 3 | 25 22 23 24 20 22 23 23 24 25 21
3 | 7 9 9 11 8 5 6 8 17 10 3 | 30 29 30 26 28 29 33 28 35 31 29
X4E | 12 --- 11 24 --- 7 21 11 20 36 7 | 38 --- 38 40 --- 36 41 37 42 47 38
5 | 20 12 10 9 10 6 6 10 11 20 4 | 36 33 35 35 30 34 35 32 34 33 32
6 | 8 7 10 9 5 3 6 7 7 12 2 | 26 27 28 25 23 25 29 24 26 31 25
7 | 8 9 6 9 8 6 8 7 11 28 3 | 71 69 68 67 69 69 71 70 68 64 69
8E | 9 20 14 29 12 5 9 17 13 9 5 | 37 41 38 38 38 37 25 36 40 36 36
9E | 10 10 16 23 17 7 7 12 12 18 4 | 44 45 48 48 39 45 45 44 46 45 43
10 | 9 11 10 8 6 3 5 7 11 11 3 | 22 20 23 25 22 21 25 21 20 25 21
11 | 9 16 13 13 11 4 8 9 11 12 4 | 23 31 23 32 27 26 31 25 28 26 25
12 | 11 15 6 7 9 3 6 6 8 24 3 | 26 31 26 27 30 26 32 27 26 26 26
13E | 11 13 10 14 12 6 10 6 15 15 4 | 25 21 22 29 18 20 23 24 29 27 21
14E | 8 11 10 11 8 4 7 7 15 13 3 | 24 21 19 24 22 20 21 21 27 21 20
15E | 17 11 9 20 9 5 7 12 10 20 4 | 34 32 32 37 29 31 32 29 31 35 30
16 | 8 14 6 10 9 3 6 8 11 26 3 | 25 21 22 27 26 21 23 20 22 28 21
17E | 13 10 9 11 9 4 7 6 12 15 3 | 42 33 35 37 36 37 36 36 40 34 36
X18 | 15 --- 16 13 --- 9 --- 8 9 --- 6 | 35 --- 41 40 --- 29 --- 40 39 --- 31
19E | 13 12 10 12 7 4 6 7 8 14 3 | 49 51 54 50 49 50 52 50 55 56 51
20 | 10 11 11 12 8 4 7 9 9 18 3 | 21 22 21 28 22 21 23 24 26 28 21
21 | 8 14 7 11 8 6 6 8 9 20 3 | 24 23 20 25 21 21 26 22 19 30 21
22 | 7 11 6 10 10 5 7 7 8 19 3 | 17 24 18 19 20 18 25 20 20 25 19
X23E | 13 23 8 15 14 5 10 18 15 --- 5 | 25 23 23 26 23 21 19 30 26 --- 21
24 | 10 10 12 14 7 4 7 6 6 9 3 | 29 30 33 33 28 29 34 27 27 30 29
25 | 13 9 10 7 9 3 5 7 9 8 3 | 24 24 23 23 25 22 27 23 20 25 22
26 | 11 11 33 10 8 5 7 8 12 14 5 | 24 23 41 26 24 21 25 20 21 28 23
27E | 11 13 16 37 9 5 9 13 14 10 5 | 43 41 39 42 43 40 21 36 40 38 40
28 | 8 8 6 9 8 4 7 8 9 21 3 | 27 29 26 28 24 26 31 28 28 29 26
29E | 16 16 11 14 11 4 8 10 11 20 4 | 57 50 49 50 52 48 52 50 46 54 50
30 | 7 8 7 13 8 4 7 8 10 15 3 | 28 27 25 25 26 24 29 24 30 27 25
31 | 9 14 8 5 8 4 6 6 7 25 3 | 28 27 20 25 19 27 29 22 25 22 27
32E | 11 14 12 31 11 4 10 11 14 12 5 | 40 41 41 51 42 41 31 44 45 40 41
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 12 15 9 5 7 9 11 17 |T 32 31 31 33 30 30 31 30 32 33 30
WRMS | 10 12 11 15 8 5 7 8 10 16 |NE 28 28 28 29 26 26 30 27 28 29 27
MEDI | 10 11 10 11 8 4 7 8 11 15 |MD 28 29 28 28 26 26 29 27 28 30 26
Table 3.2097.3 GPS week: 2097 Day: 3 MJD: 58926.000
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 8 11 6 4 8 8 5 9 3 | 17 23 19 21 17 17 24 17 18 18 18
2 | 8 10 8 11 10 5 8 9 8 22 3 | 21 17 19 21 19 18 19 21 21 24 18
3 | 12 10 8 13 9 5 8 9 10 11 3 | 22 22 21 19 18 19 23 18 20 19 18
X4E | 11 --- 11 25 --- 7 19 13 18 34 7 | 29 --- 27 31 --- 25 30 25 29 33 25
5 | 8 12 8 10 12 6 8 8 9 18 3 | 39 35 38 36 32 35 36 35 40 37 35
6 | 5 9 9 10 5 4 8 7 6 11 2 | 24 23 23 23 21 22 26 21 23 27 22
7 | 8 7 6 9 8 4 8 6 8 31 3 | 70 72 70 68 68 69 71 70 70 66 69
8E | 18 14 14 30 14 5 15 21 17 12 6 | 82 74 75 85 85 76 44 83 73 74 76
9E | 12 12 16 20 15 5 13 15 13 21 5 | 44 48 50 46 49 48 58 48 45 45 45
10 | 9 11 9 9 8 3 9 8 9 12 3 | 20 20 22 23 18 19 23 20 20 24 19
11 | 9 16 14 13 11 4 10 11 7 10 4 | 23 31 19 28 23 22 30 24 21 21 23
12 | 5 13 6 7 11 4 8 8 6 22 3 | 22 26 22 24 24 22 26 24 23 20 22
13E | 10 12 8 10 11 4 9 9 8 16 3 | 29 26 28 29 27 27 25 30 29 34 27
14E | 7 10 6 12 9 3 7 9 9 9 3 | 27 32 27 29 29 26 29 29 26 30 27
15E | 9 13 7 15 11 5 7 8 6 11 3 | 38 35 33 38 34 34 34 35 37 35 34
16 | 6 16 6 9 8 3 8 11 9 25 4 | 15 15 15 19 17 15 16 17 17 19 14
17E | 15 10 8 10 8 4 8 7 5 15 3 | 37 30 32 33 35 33 33 34 36 34 33
X18 | 8 --- --- 12 --- 9 --- 14 12 --- 7 | 20 --- --- 22 --- 14 --- 18 17 --- 22
19E | 11 11 8 9 8 4 8 6 7 14 3 | 29 30 31 31 26 30 31 30 31 33 29
20 | 10 9 7 11 10 2 9 9 9 19 3 | 23 21 20 27 22 21 25 24 19 27 20
21 | 9 12 5 8 8 4 8 7 7 22 3 | 16 20 14 19 17 16 21 16 17 25 16
22 | 12 12 7 11 9 4 9 9 9 22 3 | 17 26 21 23 21 21 27 25 19 27 20
X23E | 18 22 6 14 30 4 8 17 16 --- 6 | 61 55 54 57 56 54 55 57 58 --- 55
24 | 7 9 10 11 10 3 8 8 8 9 3 | 19 23 22 22 19 20 25 18 18 20 19
25 | 7 8 8 8 11 4 7 7 6 12 3 | 14 19 19 21 16 16 21 17 16 24 16
26 | 9 10 8 6 7 3 7 9 7 11 3 | 16 21 20 18 22 18 23 20 18 23 18
27E | 9 15 16 31 11 5 11 14 13 10 5 | 39 43 37 41 36 38 32 35 36 35 37
28 | 11 11 6 10 7 3 7 9 9 21 3 | 20 25 17 22 17 18 23 19 23 21 18
29E | 9 13 10 8 11 4 9 13 10 18 4 | 29 26 27 25 28 28 29 27 33 27 26
30 | 7 7 7 10 7 4 9 9 7 17 3 | 21 26 22 20 21 20 28 23 19 26 21
X31 | 7 14 7 7 --- 3 8 7 7 25 3 | 19 26 23 27 --- 20 30 24 25 23 19
32E | 9 16 13 27 11 4 12 10 13 13 5 | 54 52 53 57 54 51 37 59 49 53 53
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 9 14 10 4 9 10 9 17 |T 29 31 29 31 30 28 30 30 29 30 28
WRMS | 9 12 9 16 9 4 9 9 7 16 |NE 22 25 23 25 22 22 27 23 23 25 22
MEDI | 9 11 8 10 10 4 8 9 8 15 |MD 23 26 23 25 23 22 28 24 23 27 22
Table 3.2097.4 GPS week: 2097 Day: 4 MJD: 58927.000
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 12 9 10 5 4 6 12 9 10 3 | 18 25 20 17 20 19 25 18 21 18 18
2 | 12 11 8 9 8 3 7 12 7 20 3 | 21 15 17 18 16 16 20 19 15 20 15
3 | 10 14 9 11 9 5 7 10 8 9 3 | 20 25 22 17 20 20 24 17 22 19 19
X4E | 12 --- 12 25 --- 6 22 16 18 34 8 | 25 --- 27 29 --- 25 26 25 28 35 23
5 | 8 12 8 8 10 5 6 10 9 19 3 | 29 27 31 32 29 31 32 31 31 31 29
6 | 13 12 9 9 5 5 8 12 7 12 3 | 22 24 23 21 20 21 25 22 21 25 21
7 | 8 13 7 9 9 3 8 10 12 29 4 | 68 66 66 65 65 64 69 64 65 65 65
X8E | 22 22 14 26 11 7 --- 22 19 16 7 | 69 68 65 66 75 64 --- 78 58 70 65
X9E | 28 24 14 25 22 16 --- 24 21 25 8 | 75 71 64 64 79 60 --- 59 66 65 65
10 | 9 14 11 8 7 4 6 13 10 14 3 | 17 20 23 23 17 20 20 22 19 24 18
11 | 9 18 15 9 11 5 8 13 8 11 4 | 22 33 17 26 24 20 31 24 22 21 22
12 | 8 13 6 7 11 4 6 9 10 25 3 | 24 30 22 24 23 23 29 24 27 26 23
13E | 9 17 8 16 12 5 8 14 11 18 4 | 23 25 24 32 25 24 23 24 25 30 22
14E | 8 13 7 9 10 4 9 15 9 17 3 | 23 27 23 27 25 24 24 27 26 29 23
15E | 6 13 6 15 11 4 8 11 10 12 3 | 33 30 30 37 32 32 34 31 36 30 31
16 | 8 19 6 10 8 4 8 11 9 26 4 | 16 20 17 18 16 16 18 13 17 21 14
17E | 15 13 8 8 7 4 7 11 10 16 3 | 36 30 29 33 29 31 31 30 35 27 30
X18 | 8 --- 17 10 --- 7 --- 16 13 --- 6 | 22 --- 21 17 --- 26 --- 24 15 --- 23
19E | 11 12 10 15 6 3 7 11 9 15 3 | 36 43 42 37 40 40 44 38 42 41 40
20 | 8 9 8 11 9 4 7 14 8 19 3 | 22 25 24 30 26 25 28 30 23 32 25
21 | 8 9 7 8 8 5 6 13 9 20 3 | 14 21 15 17 18 16 22 19 19 24 16
22 | 9 15 6 9 9 4 7 10 8 22 3 | 21 31 21 23 22 22 30 24 21 25 22
X23E | 17 21 10 15 16 5 10 19 16 --- 5 | 54 49 49 47 41 49 53 58 52 --- 49
24 | 8 9 11 12 8 4 7 9 8 9 3 | 18 24 23 22 19 20 24 17 20 26 20
25 | 11 13 8 8 12 2 5 10 8 9 3 | 20 23 18 21 16 18 23 17 17 21 17
26 | 8 9 7 7 7 3 6 11 9 13 3 | 15 24 19 19 18 17 24 17 17 24 17
27E | 14 15 16 32 10 5 14 17 19 12 6 | 59 57 56 59 59 56 33 57 58 60 57
28 | 8 12 6 8 7 3 6 12 8 27 3 | 19 26 20 22 18 22 25 19 23 23 19
29E | 10 13 9 15 13 5 9 16 13 16 4 | 48 52 49 50 51 50 51 49 53 51 50
30 | 8 10 8 8 8 3 5 11 9 17 3 | 26 32 27 26 25 25 32 26 27 30 26
X31 | 3 --- --- --- --- 17 --- --- --- --- 0 | 18 --- --- --- --- 20 --- --- --- --- 20
X32E | 19 34 15 42 21 12 --- 48 28 27 11 | 108 99 97 117 105 100 --- 112 99 97 102
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 9 12 9 4 7 12 10 18 |T 32 35 32 34 33 31 30 33 32 34 31
WRMS | 9 13 9 11 9 4 7 11 9 16 |NE 22 27 23 24 22 23 27 23 23 26 22
MEDI | 9 13 8 10 9 4 7 12 9 17 |MD 22 27 23 26 25 24 26 24 25 27 23
Table 3.2097.5 GPS week: 2097 Day: 5 MJD: 58928.000
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 12 11 8 7 3 6 11 6 12 3 | 31 33 30 30 30 29 34 31 30 30 30
2 | 8 9 9 8 8 5 8 13 8 20 3 | 20 17 18 21 17 17 20 23 17 21 17
3 | 11 10 9 9 8 3 6 10 6 12 3 | 25 27 26 20 22 23 29 23 27 22 23
X4E | 10 --- 13 25 --- 6 24 18 15 32 8 | 37 --- 38 41 --- 36 40 41 41 46 37
5 | 7 7 8 8 10 5 8 10 11 20 3 | 29 28 29 29 28 30 35 32 28 30 29
6 | 8 8 12 10 9 4 7 9 5 13 3 | 25 28 25 25 23 24 30 24 24 27 24
7 | 10 10 8 9 8 3 7 13 6 31 4 | 42 43 43 44 44 41 47 37 40 39 41
X8E | 14 22 14 37 111 7 --- 23 22 23 9 | 144 142 138 149 189 140 --- 145 146 141 143
9E | 9 10 16 43 14 4 9 15 10 18 6 | 113 110 114 116 107 112 105 115 114 109 110
10 | 13 10 10 8 10 5 7 10 10 12 3 | 19 19 20 20 17 18 22 19 22 23 17
11 | 9 18 17 17 10 3 8 12 7 12 4 | 27 36 22 39 25 27 32 28 28 26 27
12 | 6 14 7 9 12 5 11 11 11 23 4 | 27 30 24 30 28 26 33 32 26 25 26
13E | 11 12 6 13 12 7 10 8 9 20 4 | 23 22 20 24 23 20 21 23 22 30 20
14E | 11 30 9 10 11 6 16 11 10 16 5 | 32 50 29 30 32 28 33 28 32 31 31
15E | 8 14 6 11 12 4 11 9 8 14 3 | 38 39 36 38 37 36 38 37 37 34 36
16 | 6 14 6 8 11 4 9 8 8 28 3 | 22 23 22 21 26 22 27 20 24 24 21
17E | 9 10 7 11 12 4 8 10 6 16 3 | 34 30 30 38 32 31 32 34 35 30 31
X18 | 10 --- 14 9 --- 7 --- 12 9 --- 5 | 31 --- 24 25 --- 33 --- 24 25 --- 32
19E | 6 10 8 9 9 4 7 9 6 13 3 | 46 48 50 49 48 48 46 47 48 51 47
20 | 10 9 7 8 10 4 6 10 10 18 3 | 25 27 25 27 27 26 28 28 25 29 25
21 | 11 16 6 10 9 5 7 9 7 21 3 | 19 24 17 20 19 17 23 19 19 25 17
22 | 11 12 7 9 9 4 7 9 7 22 3 | 17 26 20 21 18 21 26 22 22 25 20
X23E | 10 16 11 14 9 4 10 18 12 --- 4 | 81 81 82 82 79 79 78 80 77 --- 80
24 | 8 8 11 13 10 3 9 8 8 11 3 | 25 27 26 30 26 25 33 27 25 32 25
25 | 7 11 9 10 14 4 9 9 9 10 3 | 20 23 22 23 23 19 27 23 21 25 20
26 | 10 10 6 9 10 3 7 9 6 13 3 | 19 23 18 20 21 18 27 16 18 23 18
X27E | 11 19 9 18 34 7 --- 23 16 16 7 | 56 56 55 57 66 58 --- 62 59 60 56
28 | 8 8 7 10 9 4 9 13 6 24 3 | 22 27 20 26 22 22 27 28 25 27 22
29E | 16 12 10 10 13 5 8 13 10 15 4 | 70 66 68 66 72 66 68 67 70 66 67
30 | 7 7 9 10 7 3 6 11 7 23 3 | 27 27 27 27 26 25 31 24 25 29 25
31 | 8 15 6 10 9 4 9 10 6 27 3 | 19 25 14 22 18 18 26 18 19 15 18
32E | 17 16 22 32 9 6 15 17 16 12 6 | 56 51 51 65 53 48 58 45 47 49 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 10 14 10 4 9 11 8 18 |T 38 40 36 39 39 36 37 38 38 38 37
WRMS | 9 12 8 12 10 4 9 10 8 17 |NE 24 27 23 26 24 24 29 24 24 26 23
MEDI | 9 11 9 10 10 4 8 10 8 16 |MD 27 28 26 29 26 26 32 28 26 29 26
Table 3.2097.6 GPS week: 2097 Day: 6 MJD: 58929.000
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 12 8 8 8 5 8 7 9 9 3 | 27 31 27 26 28 26 33 28 31 29 28
2 | 8 10 9 11 10 3 11 7 6 21 3 | 21 27 25 22 19 22 29 22 22 21 22
3 | 9 9 7 6 10 3 5 6 6 11 2 | 28 29 28 25 23 25 28 22 26 25 25
X4E | 17 --- 14 26 --- 6 32 14 34 35 10 | 40 --- 44 54 --- 47 44 50 64 58 47
5 | 6 12 10 6 11 5 9 6 9 20 3 | 47 46 50 49 44 48 49 48 50 45 48
6 | 7 9 9 7 9 3 7 9 6 11 3 | 31 35 35 32 30 33 40 32 32 31 33
7 | 8 10 9 8 10 3 8 6 6 24 3 | 63 62 65 62 61 63 69 62 60 60 63
8E | 12 13 11 31 70 5 17 11 15 15 6 | 131 134 128 133 139 132 117 130 135 127 131
9E | 10 13 14 33 10 3 10 10 14 17 5 | 108 106 113 110 106 108 102 109 108 108 108
10 | 8 11 7 10 10 3 7 5 8 12 3 | 19 24 23 23 22 21 25 19 20 29 21
11 | 8 16 13 11 10 5 10 9 7 10 3 | 30 40 26 38 32 33 37 29 31 31 31
12 | 9 13 6 9 11 3 8 8 6 22 3 | 35 43 34 40 36 36 44 40 40 38 38
13E | 10 18 9 13 16 5 6 7 7 19 4 | 26 27 25 27 27 23 21 21 21 30 21
14E | 6 18 7 11 9 4 9 9 8 14 3 | 35 42 34 38 36 34 34 31 36 32 33
15E | 6 19 7 9 9 4 9 9 8 14 3 | 50 52 49 50 53 51 52 49 50 48 49
16 | 9 17 5 10 8 5 8 6 5 27 3 | 27 29 27 27 30 28 30 28 27 34 28
17E | 14 8 7 7 14 3 10 8 7 16 3 | 44 34 32 38 31 36 37 38 39 35 36
X18 | 9 --- 13 9 --- 6 --- 8 10 --- 5 | 46 --- 33 32 --- 45 --- 32 30 --- 48
19E | 10 13 8 8 12 4 8 6 9 15 3 | 51 52 55 51 55 53 53 55 53 60 54
20 | 8 9 5 7 10 3 7 7 7 19 3 | 32 39 32 34 37 34 36 34 32 36 34
21 | 6 13 3 7 8 4 7 6 6 21 3 | 19 24 18 20 18 18 24 20 21 27 19
22 | 11 10 5 8 12 4 6 5 5 22 3 | 25 32 26 30 28 27 32 27 27 36 28
X23E | 8 18 11 8 9 6 9 12 10 --- 4 | 90 91 89 88 90 87 90 88 87 --- 87
24 | 9 9 10 13 9 4 7 10 9 10 3 | 28 39 31 30 30 31 39 35 32 37 32
25 | 9 11 6 9 10 3 7 5 6 11 3 | 22 25 21 23 22 21 29 23 22 28 22
26 | 8 10 5 9 6 4 9 6 7 11 2 | 22 26 21 24 23 21 27 22 21 29 23
X27E | 34 34 18 27 18 6 --- 13 18 17 8 | 110 108 100 105 96 100 --- 102 96 93 100
28 | 8 7 6 6 8 4 8 11 5 22 3 | 23 26 20 22 22 22 29 26 23 28 23
29E | 4 15 10 9 13 4 9 10 9 15 3 | 78 76 80 79 83 78 81 79 80 83 80
30 | 7 8 8 7 9 3 6 7 4 12 2 | 28 30 29 25 27 27 34 27 28 27 27
31 | 6 15 5 9 12 4 7 6 9 23 3 | 21 23 15 22 15 21 26 19 21 17 22
32E | 7 10 17 25 10 3 9 7 11 12 4 | 58 56 57 60 54 55 46 58 58 52 56
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 9 13 17 4 9 8 8 17 |T 44 46 43 44 43 43 44 43 44 44 44
WRMS | 8 12 8 11 10 4 9 7 6 15 |NE 29 33 29 30 28 30 34 29 29 32 30
MEDI | 8 12 8 9 10 4 8 7 7 15 |MD 31 35 32 32 30 33 36 32 32 34 33
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2097 GPS week: 2097 MJD: 58923.0-58929.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 |U 0 0 0 |U 0 0 0 |U 8 14 37 |
emr | emr 2866 | 0 0 0 |U 0 0 0 |U 18 20 54 |
esa | esa 3017 | 0 0 0 |U 0 0 0 | 14 15 37 |
gfz | gfz 3026 |U 0 0 0 |U 0 0 0 |U 10 14 34 |
grg | grg 2849 |U 0 0 0 |U 0 0 0 | 11 16 39 |
igr | igr 3003 | 0 0 0 | 0 0 0 | 10 14 39 |
igs | igs 3008 | 0 0 0 | 0 0 0 | 11 15 39 |
jpl | jpl 2880 |U 0 0 0 |U 0 0 0 |U 18 19 49 |
mit | mit 3030 | 0 0 0 |U 0 0 0 |U 23 32 72 |
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 5.2097.0 GPS week: 2097 Day: 0 MJD: 58923.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | ---- ---- ---- | 7 15 39 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 15 21 48 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 11 12 38 |
gfz | gfz 2976 | ---- ---- ---- | ---- ---- ---- | 9 15 40 |
grg | grg 2880 | ---- ---- ---- | ---- ---- ---- | 9 16 40 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 8 15 38 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 9 15 41 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 18 16 46 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | 84 108 187 |
Table 5.2097.1 GPS week: 2097 Day: 1 MJD: 58924.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | ---- ---- ---- | 7 15 37 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 16 25 55 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 12 14 36 |
gfz | gfz 2976 | ---- ---- ---- | ---- ---- ---- | 8 15 34 |
grg | grg 2880 | ---- ---- ---- | ---- ---- ---- | 8 13 34 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 9 15 36 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 9 15 38 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 18 21 45 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | 7 19 41 |
Table 5.2097.2 GPS week: 2097 Day: 2 MJD: 58925.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | ---- ---- ---- | ---- ---- ---- | 7 15 31 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 14 18 57 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 13 13 31 |
gfz | gfz 3064 | ---- ---- ---- | ---- ---- ---- | 9 14 31 |
grg | grg 2880 | ---- ---- ---- | ---- ---- ---- | 9 12 31 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 9 14 33 |
igs | igs 3021 | ---- ---- ---- | ---- ---- ---- | 9 13 33 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 16 18 42 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 11 14 45 |
Table 5.2097.3 GPS week: 2097 Day: 3 MJD: 58926.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | ---- ---- ---- | ---- ---- ---- | 10 14 44 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 17 21 55 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 17 19 42 |
gfz | gfz 3062 | ---- ---- ---- | ---- ---- ---- | 12 16 42 |
grg | grg 2780 | ---- ---- ---- | ---- ---- ---- | 14 20 48 |
igr | igr 3029 | ---- ---- ---- | ---- ---- ---- | 12 17 48 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 13 17 48 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 17 20 56 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 18 20 59 |
Table 5.2097.4 GPS week: 2097 Day: 4 MJD: 58927.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | ---- ---- ---- | ---- ---- ---- | 11 15 33 |
emr | emr 2784 | ---- ---- ---- | ---- ---- ---- | 22 21 48 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 17 19 37 |
gfz | gfz 2972 | ---- ---- ---- | ---- ---- ---- | 11 14 31 |
grg | grg 2780 | ---- ---- ---- | ---- ---- ---- | 15 22 40 |
igr | igr 2934 | ---- ---- ---- | ---- ---- ---- | 12 15 35 |
igs | igs 2970 | ---- ---- ---- | ---- ---- ---- | 13 18 37 |
jpl | jpl 2592 | ---- ---- ---- | ---- ---- ---- | 21 25 56 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | 18 23 72 |
Table 5.2097.5 GPS week: 2097 Day: 5 MJD: 58928.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | ---- ---- ---- | 8 11 38 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 18 18 61 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 15 13 36 |
gfz | gfz 3061 | ---- ---- ---- | ---- ---- ---- | 10 13 29 |
grg | grg 2864 | ---- ---- ---- | ---- ---- ---- | 11 12 40 |
igr | igr 3060 | ---- ---- ---- | ---- ---- ---- | 9 11 41 |
igs | igs 3070 | ---- ---- ---- | ---- ---- ---- | 11 12 41 |
jpl | jpl 2784 | ---- ---- ---- | ---- ---- ---- | 17 22 52 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 13 20 54 |
Table 5.2097.6 GPS week: 2097 Day: 6 MJD: 58929.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | ---- ---- ---- | 10 14 40 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 21 17 53 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 15 14 38 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 10 12 30 |
grg | grg 2879 | ---- ---- ---- | ---- ---- ---- | 12 15 44 |
igr | igr 3072 | ---- ---- ---- | ---- ---- ---- | 11 13 41 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 12 14 40 |
jpl | jpl 2880 | ---- ---- ---- | ---- ---- ---- | 16 14 45 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 12 18 46 |
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 6.2097 GPS week: 2097 MJD: 58923.500-58929.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -14 -12 82 -109 1 | 15 22
| 20 13 52 95 8 | 3
emr uuxux | 18 8 -11 190 -4 | -22 35
| 42 36 281 136 35 | 8
esa uuuuu | 2 30 8 36 -6 | 37 39
| 17 16 100 36 6 | 1
gfz uuuuu | -6 14 61 -32 1 | 30 34
| 16 22 74 61 6 | 3
grg uuuuu | 8 3 -72 -53 -2 | 3 11
| 24 16 34 86 5 | 1
igr xxxxx | 22 3 11 -6 -4 | 7 17
| 15 14 36 73 3 | 1
irf xxxxx | 13 -28 -35 6 -1 | 5 16
| 12 13 15 20 9 | 3
jpl uuuuu | 11 -17 -8 80 9 | 51 55
| 30 29 23 74 14 | 3
mit uuuuu | -11 -17 -43 -18 6 | 25 30
| 12 20 45 34 10 | 5
ngs uuuuu | -12 8 6 -23 0 | 18 22
| 52 13 56 133 7 | 3
sio uuuux | 9 7 -17 -127 24 | 74 78
| 28 14 54 67 12 | 11
Table 7.2097.0 GPS week: 2097 Day: 0 MJD: 58923.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -13 146 30 6 | 12 21
emr uuxux | -21 42 -239 115 -48 | -7 24
esa uuuuu | 12 18 -56 66 4 | 37 40
gfz uuuuu | 5 35 -58 37 10 | 25 31
grg uuuuu | 23 19 -36 48 -9 | 4 11
igr xxxxx | 23 11 -54 -80 1 | 5 17
irf xxxxx | 6 -28 -2 16 13 | 0 17
jpl uuuuu | 6 -22 -7 59 3 | 48 53
mit uuuuu | -11 -46 48 6 18 | 19 25
ngs uuuuu | -4 32 -48 -223 10 | 14 20
sio uuuux | -19 10 -70 -149 42 | 58 63
Table 7.2097.1 GPS week: 2097 Day: 1 MJD: 58924.500
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 -13 17 -27 11 | 12 21
emr uuxux | 6 23 -131 99 -50 | -17 29
esa uuuuu | -13 27 137 38 -8 | 37 40
gfz uuuuu | 17 42 55 -6 -4 | 27 32
grg uuuuu | 21 6 -77 -63 -4 | 3 12
igr xxxxx | 17 28 12 -86 -8 | 6 17
irf xxxxx | 23 -19 -33 34 6 | 2 16
jpl uuuuu | -10 -30 4 80 5 | 49 54
mit uuuuu | 0 -22 -65 44 12 | 21 27
ngs uuuuu | -2 13 19 -157 -3 | 16 21
sio uuuux | 8 -12 -33 -94 28 | 63 69
Table 7.2097.2 GPS week: 2097 Day: 2 MJD: 58925.500
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 | -42 12 90 -243 9 | 12 21
emr uuxux | 43 -2 -193 142 -4 | -25 38
esa uuuuu | -22 49 -29 50 -15 | 36 40
gfz uuuuu | -2 13 110 6 4 | 27 32
grg uuuuu | -29 15 -73 -44 -5 | 1 12
igr xxxxx | -5 -7 46 -51 -3 | 5 18
irf xxxxx | 5 -44 -34 18 5 | 3 16
jpl uuuuu | 42 -20 -18 116 1 | 48 53
mit uuuuu | -2 -34 -62 -30 11 | 22 27
ngs uuuuu | -18 -9 102 31 3 | 15 21
sio uuuux | 19 23 -50 -122 27 | 67 72
Table 7.2097.3 GPS week: 2097 Day: 3 MJD: 58926.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 4 -4 31 -146 -5 | 17 23
emr uuxux | 28 -1 -18 97 -3 | -23 37
esa uuuuu | -4 54 160 13 -6 | 38 41
gfz uuuuu | -16 -24 2 -115 4 | 32 35
grg uuuuu | -14 9 -123 -47 -1 | 3 12
igr xxxxx | 24 -12 33 105 -4 | 8 18
irf xxxxx | 35 -41 -42 9 -1 | 7 16
jpl uuuuu | 63 -42 28 97 -7 | 53 56
mit uuuuu | 3 -1 -96 -37 9 | 27 31
ngs uuuuu | -81 6 -19 159 5 | 19 23
sio uuuux | 48 -7 11 -176 28 | 75 79
Table 7.2097.4 GPS week: 2097 Day: 4 MJD: 58927.500
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 -27 80 -198 -8 | 18 24
emr uuxux | 95 61 -255 458 3 | -25 38
esa uuuuu | 29 26 -9 -34 -5 | 37 40
gfz uuuuu | -7 12 157 -121 1 | 33 37
grg uuuuu | 4 10 -106 -90 1 | 4 12
igr xxxxx | 44 0 46 -23 -2 | 9 18
irf xxxxx | 10 -35 -47 -29 -3 | 7 16
jpl uuuuu | -13 -39 8 139 6 | 54 57
mit uuuuu | -24 -20 -23 -38 6 | 28 32
ngs uuuuu | -69 8 -51 44 4 | 21 24
sio uuuux | 35 2 -64 -239 19 | 80 84
Table 7.2097.5 GPS week: 2097 Day: 5 MJD: 58928.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -20 60 -97 3 | 17 22
emr uuxux | 0 -37 315 290 42 | -29 38
esa uuuuu | 11 29 -46 71 -4 | 36 38
gfz uuuuu | -9 -1 117 -3 3 | 32 35
grg uuuuu | 11 -12 -35 -210 -1 | 2 10
igr xxxxx | 32 -6 2 50 -4 | 7 16
irf xxxxx | 4 -11 -45 -6 -8 | 6 16
jpl uuuuu | 7 -4 -30 141 33 | 51 53
mit uuuuu | -27 12 -45 -60 -3 | 29 33
ngs uuuuu | 14 13 -14 -67 -4 | 20 24
sio uuuux | -32 27 79 -69 15 | 83 87
Table 7.2097.6 GPS week: 2097 Day: 6 MJD: 58929.500
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 | -36 -18 154 -84 -7 | 18 22
emr uuxux | -28 -30 446 130 31 | -29 38
esa uuuuu | 2 8 -97 46 -9 | 36 38
gfz uuuuu | -33 24 48 -24 -8 | 34 36
grg uuuuu | 41 -26 -50 34 6 | 1 11
igr xxxxx | 22 7 -9 46 -8 | 7 16
irf xxxxx | 6 -17 -40 -2 -15 | 7 15
jpl uuuuu | -18 42 -39 -73 22 | 56 57
mit uuuuu | -17 -6 -54 -14 -11 | 31 33
ngs uuuuu | 73 -5 55 49 -10 | 20 23
sio uuuux | 4 8 12 -42 5 | 89 90
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