[IGSREPORT-27165] Wk 2096 IGS Final Orbits
acc
acc at igs.org
Sat Mar 28 13:06:50 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2096 (Mar 08, 2020 - Mar 14, 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:
igs2096[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2096[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2096[0-6].cls IGS GPS clock combination summary report.
igs20967.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20967.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 | OHI3 TIXI TIXI
0 | EMR | TLSE
0 | ESA | 18 18 PTBB SCRZ TLSE PTBB SCRZ
0 | GFZ | 4 4 BJNM GODE POHN BJNM GODE POHN
0 | GRG | 13 BAKE CCJ2 COCO HOB2 COCO OHI3
1 | COD | 18 OHI3 TIXI OHI3 RAMO TIXI
1 | EMR | AREQ CHUR
1 | ESA | 5 5 DJIG PTBB SAVO SFER DJIG PTBB SAVO SFER
1 | GFZ | 4 4 16 COCO GODE MAL2 POHN COCO GODE MAL2 POHN
1 | GRG | 5 5 OHI3 SFER BRST DARW OHI3 SFER
1 | JPL | MONP MONP
2 | COD | TIXI TIXI
2 | EMR | NRC1 NRC1
2 | ESA | GLPS MONP PTBB GLPS PTBB
2 | GFZ | 4 4 BJNM GODE POHN BJNM GODE POHN
2 | GRG | 13 BRST TLSE BRST KARR TLSE
2 | JPL | 13 MAG0 MONP
3 | COD | TIXI TIXI
3 | EMR | TLSE TLSE
3 | ESA | DJIG PTBB TLSE DJIG PTBB TLSE
3 | GFZ | 4 4 BJNM GODE KOUR POHN GODE KOUR POHN
3 | GRG | 13 AREG
3 | JPL | BJNM POLV
4 | COD | TIXI TIXI
4 | EMR | TLSE TLSE
4 | ESA | GLPS PTBB SCOR GLPS PTBB SCOR
4 | GFZ | 4 4 BRUX FLRS GODE POHN BRUX FLRS GODE POHN
4 | GRG | WIND KARR WIND
4 | MIT | BJCO BJCO
5 | COD | TIXI TIXI
5 | EMR | 10 HOB2
5 | ESA | DGAR PTBB DGAR PTBB
5 | GFZ | 4 4 17 BJNM BOR1 DGAR GODE POHN USN7 BJNM BOR1 DGAR
5 | GFZ | FLRS GODE GOLD POHN USN7
5 | GRG | BRUX BRUX DARW KARR
5 | MIT | BJNM FLRS
6 | COD | TIXI TIXI
6 | ESA | GLPS PTBB WIND GLPS PTBB WIND
6 | GFZ | 4 4 BJNM GODE POHN BJNM GODE POHN
6 | GRG | TLSE
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
----+--------+---------------
1 | COD | 18
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 | -.5 .0 .9 8 29 9 -.16
EMR | 0 | 5.2 -5.2 9.6 -49 -11 91 .26
ESA | 0 | 1.5 -1.1 .2 -32 58 40 -.26
GFZ | 0 | .2 .1 -.3 19 -1 49 -.07
GRG | 0 | 3.9 1.2 3.6 159 40 142 .05
JPL | 0 | 11.8 -3.0 12.7 5 15 24 -.29
MIT | 0 | 2.9 1.6 9.6 13 -8 -5 .08
NGS | 0 | .1 -2.5 2.9 -30 36 8 .05
SIO | 0 | -4.2 -4.0 -9.1 17 -6 11 -.20
COD | 1 | -.3 .1 .4 3 9 4 -.12
EMR | 1 | -2.1 -4.7 5.0 -36 -26 75 .31
ESA | 1 | -.5 -.2 -.5 -21 44 64 -.02
GFZ | 1 | -.0 .6 -.6 25 2 52 .07
GRG | 1 | 2.4 -3.6 1.2 152 20 142 .02
JPL | 1 | 11.2 -7.7 10.9 1 0 2 -.24
MIT | 1 | 4.5 2.2 9.1 -26 -21 -5 .23
NGS | 1 | -1.9 -2.4 -1.3 -36 40 2 .16
SIO | 1 | -.8 -6.0 -8.0 15 -25 -7 .03
COD | 2 | -.1 .2 1.1 15 20 9 -.31
EMR | 2 | 1.5 -7.7 4.2 -21 6 15 -.05
ESA | 2 | .9 -1.6 .2 -13 51 65 -.29
GFZ | 2 | .4 .3 -.3 42 2 54 -.19
GRG | 2 | 4.6 -1.9 -4.4 95 11 130 -.14
JPL | 2 | 10.2 -1.7 5.8 21 14 11 -.35
MIT | 2 | 4.6 -2.3 7.3 -10 -14 -19 .01
NGS | 2 | .3 -1.9 -2.7 -30 17 -13 -.07
SIO | 2 | -.4 -8.9 -5.5 3 -15 16 -.47
COD | 3 | .1 -.1 1.2 22 9 17 -.27
EMR | 3 | -2.9 .6 13.8 -35 11 84 -.13
ESA | 3 | 1.2 -1.2 .4 -39 45 67 -.41
GFZ | 3 | .8 .0 -.1 32 -20 63 -.30
GRG | 3 | 2.1 -3.7 4.4 47 16 69 .02
JPL | 3 | 11.5 -4.4 10.6 -5 1 11 -.43
MIT | 3 | 1.3 .7 9.9 5 -1 0 .01
NGS | 3 | 1.2 -4.1 -8.6 -68 31 41 -.02
SIO | 3 | -2.0 -7.3 -10.7 -16 8 12 -.19
COD | 4 | -.2 -.3 .8 7 22 15 -.22
EMR | 4 | 3.6 -.4 10.1 -29 -15 54 .22
ESA | 4 | .3 -1.1 -.1 -29 63 81 -.13
GFZ | 4 | .7 -.1 .0 33 -14 60 -.09
GRG | 4 | 4.2 -2.4 2.1 37 -9 67 .0
JPL | 4 | 10.2 -4.0 9.1 7 16 1 -.07
MIT | 4 | 3.0 -.9 7.2 -4 -14 20 .10
NGS | 4 | 1.1 1.3 -.5 1 38 60 .18
SIO | 4 | -4.0 -6.2 -7.4 -13 -40 3 -.30
COD | 5 | -.8 .5 .4 27 27 8 .04
EMR | 5 | 6.5 -6.3 14.5 -26 23 30 .37
ESA | 5 | .7 -.9 -.7 -23 47 81 .11
GFZ | 5 | .1 -.4 -.6 39 -7 69 .03
GRG | 5 | 7.3 .3 4.7 73 -1 66 .07
JPL | 5 | 16.4 -2.8 11.7 1 0 2 -.26
MIT | 5 | 5.5 .5 8.4 4 12 23 .14
NGS | 5 | 4.1 -2.5 3.5 -12 3 27 .22
SIO | 5 | .0 -6.6 -3.3 -1 -3 32 -.06
COD | 6 | -.6 -.3 -.3 -8 0 22 .03
EMR | 6 | 2.9 -.1 14.3 -10 13 3 .47
ESA | 6 | .4 -1.1 -.5 -24 64 72 .18
GFZ | 6 | -.3 -.2 .0 26 6 63 .06
GRG | 6 | 1.4 .1 5.5 55 -13 92 .06
JPL | 6 | 15.7 -7.3 12.9 1 0 1 -.16
MIT | 6 | 1.9 -3.3 12.2 -15 -12 6 .33
NGS | 6 | 4.3 -5.4 5.6 -13 -8 -6 .28
SIO | 6 | -.8 -6.2 -8.5 7 3 22 .20
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 1.2096.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2096.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 2.2096.[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 3.2096.[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 5.2096.0-6). 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 2096 summary. (Mar 08, 2020 - Mar 14, 2020)
Table 1.2096.a GPS week: 2096 MJD: 58916.000-58922.000
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 9 -19 4 -.03 9 8 | -832 470 6 102
| 0 0 1 13 22 8 .04 | 254 549
emr 80| 0 -1 2 2 20 1 .01 13 13 | 212110 254 15 110
| 0 2 0 13 15 14 .07 | 1334 1012
esa 149| 0 0 2 -22 -4 11 -.05 10 10 | -1135 903 8 92
| 0 0 1 9 15 23 .03 | 661 576
gfz 181| 0 0 1 -24 -19 1 .07 11 10 | -176 88 12 114
| 0 0 3 14 11 16 .02 | 343 650
grg 95| 1 0 -6 -15 -10 17 -.11 11 9 | -36 176 11 134
| 0 0 3 18 10 33 .03 | 115 313
igr n/a| 0 0 0 -6 -20 -19 .03 4 4 | 5338 264 10 71
| 0 0 0 11 9 18 .01 | 1692 1512
jpl 80| 0 -1 4 21 13 9 .25 8 8 | 202245 264 8 88
| 0 0 0 12 11 19 .01 | 26990 1022
mit 383| 0 0 1 23 3 -9 -.05 9 9 | 4975 442 62 1831
| 0 0 0 28 14 63 .02 | 1788 1499
ngs 204| 0 0 -3 8 15 -25 -.01 9 8 | -816 445 960 2067
| 0 0 2 14 15 33 .01 | 325 689
sio 421| -1 -1 -5 -11 5 -4 -.14 17 16 | --- --- --- ---
| 0 1 1 34 15 24 .05 | --- ---
Table 1.2096.b GPS week : 2096 MJD: 58916.000-58922.000
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 4 4 4 3 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 7 8 7 8 8 8 8 |
5 | 4 4 3 3 3 3 4 |
6 | 3 3 3 3 3 3 3 |
7 | 3 4 3 4 4 4 4 |
8 | 4 5 4 5 5 7 7 |
9 | 4 4 4 4 4 4 4 |
10 | 3 3 3 3 3 4 3 |
11 | 4 5 4 4 4 4 4 |
12 | 4 4 4 4 4 4 4 |
13 | 4 4 4 5 4 4 4 |
14 | 3 4 4 3 3 4 4 |
15 | 4 4 4 4 4 5 4 |
16 | 3 4 4 4 4 4 4 |
17 | 3 4 4 4 4 4 3 |
18 | 5 12 --- --- --- --- 0 |
19 | 3 4 4 4 4 4 4 |
20 | 3 3 4 3 3 3 3 |
21 | 3 3 3 3 3 3 3 |
22 | 4 4 3 4 4 4 3 |
23 | 4 5 4 5 5 5 5 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 3 3 3 |
27 | 4 4 4 4 5 5 7 |
28 | 3 3 3 4 4 4 3 |
29 | 4 4 5 4 4 4 4 |
30 | 3 3 2 3 3 3 3 |
31 | 3 4 4 3 3 3 4 |
32 | 3 4 3 4 4 4 4 |
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 2.2096.0 GPS week: 2096 Day: 0 MJD: 58916.000
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 251| 0 0 -2 12 5 -13 -.05 8 7 | -579 -269 6 102
emr 81| 0 -3 2 -13 42 -16 .03 13 13 | 214036 -1514 16 122
esa 149| 0 0 1 -32 3 -18 -.03 10 10 | -984 893 9 83
gfz 182| 0 0 3 -32 -21 -20 .06 9 9 | 279 -470 11 96
grg 96| 1 0 -9 -3 -7 -16 -.07 12 10 | 123 -169 14 142
igr n/a| 0 0 -1 -15 -31 -38 .03 4 4 | 7708 -2231 10 64
jpl 80| 0 0 3 20 22 4 .25 9 9 | 214054 -1505 8 88
mit 383| 0 0 1 20 -10 76 -.04 7 6 | 7585 -2211 26 1846
ngs 205| 0 0 0 5 -19 -59 -.02 8 8 | -276 -835 821 1896
sio 451| -2 -2 -8 -17 13 19 -.16 17 15 | --- --- --- ---
Table 2.2096.1 GPS week: 2096 Day: 1 MJD: 58917.000
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 249| 0 0 -2 -6 -9 4 -.06 8 7 | -528 124 5 91
emr 80| 0 -3 1 -1 0 -1 .06 13 13 | 212599 162 14 112
esa 149| 0 0 3 -19 -19 -13 -.09 10 10 | 266 -179 8 87
gfz 180| 0 0 4 -35 -31 -9 .05 9 9 | -434 1165 12 102
grg 95| 1 0 -8 -22 -18 60 -.08 10 10 | -81 786 13 147
igr n/a| 0 0 0 -20 -3 -19 .03 4 4 | 5670 -487 10 61
jpl 80| 0 -1 5 17 16 24 .26 8 8 | 212656 138 8 83
mit 383| 0 0 1 32 19 1 -.06 10 10 | 5200 -437 53 1854
ngs 204| 0 1 -4 15 18 -67 -.02 9 9 | -660 290 1321 2185
sio 421| -1 0 -3 47 16 29 -.11 17 15 | --- --- --- ---
Table 2.2096.2 GPS week: 2096 Day: 2 MJD: 58918.000
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 -3 -1 -29 -2 -.04 9 8 | -1306 1533 6 111
emr 81| 1 -3 1 0 0 -1 .08 12 12 | 211790 -597 15 89
esa 149| 0 0 1 -32 2 5 -.07 10 10 | -1114 951 9 100
gfz 181| 0 0 4 -13 -2 8 .08 10 9 | -322 49 13 88
grg 95| 2 0 -9 2 0 34 -.14 12 10 | 81 -85 12 121
igr n/a| 0 0 0 -12 -24 -14 .05 4 4 | 4222 -838 10 64
jpl 80| 0 0 4 40 28 34 .24 8 8 | 211826 -585 8 101
mit 383| 0 0 0 14 -11 -39 -.05 6 6 | 3362 -129 79 1949
ngs 206| -1 0 0 -2 21 -20 .00 9 8 | -1295 1439 1153 2299
sio 422| 0 0 -5 -36 -8 10 -.13 18 17 | --- --- --- ---
Table 2.2096.3 GPS week: 2096 Day: 3 MJD: 58919.000
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 256| -1 0 0 28 -22 10 -.08 8 8 | -827 440 6 110
emr 79| 0 0 3 -8 29 -2 .08 13 13 | 211252 549 16 125
esa 149| 0 0 1 -29 -25 18 -.05 9 9 | -1422 855 8 104
gfz 181| 0 0 0 -7 -30 -6 .06 9 9 | -290 -30 12 132
grg 95| 1 0 0 -19 -4 -25 -.12 12 10 | -89 171 11 133
igr n/a| 0 0 -1 3 -29 -40 .03 4 4 | 3323 968 11 100
jpl 80| 2 -1 4 22 -1 8 .25 8 8 | 211283 537 9 75
mit 383| 0 0 1 3 16 41 -.06 8 8 | 3097 1145 134 1821
ngs 205| 0 0 -7 20 25 -44 -.00 9 8 | -947 612 793 2072
sio 419| -1 -2 -5 -64 15 -27 -.07 17 17 | --- --- --- ---
Table 2.2096.4 GPS week: 2096 Day: 4 MJD: 58920.000
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 257| 0 0 -2 14 -33 6 -.04 8 7 | -815 465 6 96
emr 81| 0 0 4 5 17 18 -.05 12 12 | 211251 1233 15 94
esa 149| 0 0 2 -20 7 24 -.06 10 10 | -1510 1631 10 98
gfz 183| 0 0 -2 -46 -22 10 .08 9 10 | -672 728 12 138
grg 96| 1 0 -3 -52 -28 10 -.13 10 9 | -138 168 10 137
igr n/a| 0 0 -1 -15 -20 -23 .03 4 4 | 3783 1794 11 76
jpl 80| 0 -1 5 20 21 -16 .25 7 7 | 211280 1253 8 91
mit 383| 0 -1 2 55 17 -21 -.05 13 12 | 3331 2091 64 1865
ngs 205| 0 0 -3 29 21 -15 -.02 9 8 | -819 466 1133 2102
sio 419| -2 -1 -6 -1 3 -30 -.16 18 17 | --- --- --- ---
Table 2.2096.5 GPS week: 2096 Day: 5 MJD: 58921.000
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| -1 0 -1 21 7 11 .03 9 8 | -885 412 6 104
emr 81| 0 -2 3 12 28 -7 -.05 13 13 | 210325 1295 20 113
esa 149| -1 0 2 -16 -15 13 -.03 9 9 | -1570 1422 9 91
gfz 182| -1 0 2 -17 -24 -4 .09 12 11 | 122 -143 12 135
grg 95| 1 0 -5 -13 -10 5 -.14 9 8 | -182 307 11 141
igr n/a| 0 0 0 8 -18 -13 .02 4 4 | 5398 1891 10 65
jpl 80| 1 0 4 0 -2 -11 .23 8 8 | 141085 1365 9 85
mit 383| 1 0 0 58 0 -1 -.06 12 12 | 5475 1870 45 1800
ngs 205| 0 0 -4 -12 18 0 .00 8 7 | -1045 835 747 2047
sio 407| -2 -2 -5 2 -22 -11 -.15 18 18 | --- --- --- ---
Table 2.2096.6 GPS week: 2096 Day: 6 MJD: 58922.000
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 -3 0 -55 10 -.00 11 10 | -886 589 7 104
emr 81| 1 3 3 25 23 25 -.07 14 14 | 213517 653 15 117
esa 149| 0 0 4 -6 16 48 -.02 10 10 | -1613 753 9 82
gfz 183| -1 1 -2 -15 -6 30 .04 17 13 | 79 -682 12 108
grg 99| 0 0 -5 -1 -2 52 -.11 8 8 | 32 59 10 122
igr n/a| 0 0 -1 4 -18 16 .04 4 4 | 7268 752 12 73
jpl 80| 0 -1 5 29 12 22 .25 8 8 | 213537 647 9 93
mit 383| 0 0 0 -22 -8 -123 -.00 7 7 | 6779 766 36 1687
ngs 201| 0 0 -2 3 18 27 .01 9 7 | -671 311 754 1868
sio 414| -2 0 -4 -11 18 -23 -.22 16 16 | --- --- --- ---
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 3.2096.0 GPS week: 2096 Day: 0 MJD: 58916.000
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 7 7 9 6 4 8 8 6 11 2 | 28 31 29 29 27 29 32 30 29 30 28
2 | 6 8 10 13 8 3 7 6 6 18 3 | 23 23 25 31 24 25 25 28 25 21 24
3 | 9 10 12 7 10 3 9 7 8 11 3 | 27 28 30 26 27 26 32 32 26 32 28
X4E | 13 --- 13 15 --- 7 26 7 15 44 7 | 54 --- 51 53 --- 51 54 57 55 58 52
5 | 8 18 9 9 14 4 8 7 9 16 3 | 36 40 38 37 38 36 39 37 38 33 37
6 | 5 7 9 10 5 3 6 6 7 10 2 | 30 29 30 33 32 31 34 32 31 32 30
7 | 5 10 8 8 12 3 7 6 6 26 3 | 52 53 54 58 49 54 56 56 54 50 53
8E | 7 15 14 12 16 4 11 12 8 19 4 | 40 39 38 36 40 38 39 44 38 45 38
9E | 8 13 14 11 13 4 10 5 10 12 3 | 53 48 51 51 48 50 52 57 49 54 51
10 | 5 10 12 6 9 3 8 6 10 12 3 | 26 27 28 26 27 27 30 29 29 29 26
11 | 8 16 15 10 10 4 9 10 8 13 3 | 33 42 29 39 33 35 40 35 36 35 34
12 | 7 15 8 8 28 6 7 6 9 21 4 | 49 56 53 51 65 50 54 53 50 48 52
13 | 9 17 8 7 12 5 10 7 6 16 3 | 38 40 39 41 37 35 42 42 38 37 39
14 | 6 11 8 10 14 5 8 5 9 18 3 | 56 53 52 55 48 53 53 54 55 51 53
15E | 13 19 8 10 11 3 13 4 7 20 4 | 34 31 30 29 35 31 33 31 33 39 31
16 | 6 15 5 8 11 3 8 5 7 23 3 | 37 39 39 36 37 37 38 39 42 39 38
17E | 9 11 8 7 10 4 9 5 9 17 3 | 75 71 68 73 73 72 75 74 73 68 73
X18 | 17 9 14 12 --- 6 9 11 7 --- 5 | --- --- --- --- --- --- --- --- --- --- 0
19E | 11 13 8 7 8 4 9 7 9 15 3 | 44 52 51 49 46 51 54 53 56 59 51
20 | 6 7 7 6 8 4 9 4 6 19 2 | 28 27 28 28 26 27 29 31 28 32 27
21 | 8 13 6 8 8 4 9 6 8 22 3 | 28 28 27 30 30 27 31 29 30 37 28
22 | 11 12 8 6 10 4 9 6 9 17 3 | 40 45 41 42 41 41 47 46 42 45 42
23E | 7 19 10 16 13 4 10 7 10 24 4 | 33 34 30 37 26 31 31 31 32 12 30
24 | 6 13 7 9 8 4 9 6 8 9 3 | 32 36 33 36 33 32 36 35 31 32 33
25 | 6 10 10 8 12 3 7 5 8 8 2 | 33 35 36 35 33 33 36 34 31 34 33
26 | 5 11 8 5 10 3 6 6 8 12 2 | 36 39 38 35 38 36 40 37 37 40 37
27E | 10 12 13 10 15 3 11 11 9 13 4 | 44 39 39 36 40 41 41 46 41 46 40
28 | 6 10 8 9 9 2 8 6 8 24 3 | 31 33 30 30 34 32 34 35 35 39 32
29E | 8 15 8 10 16 4 9 6 8 19 3 | 78 77 79 80 77 78 77 82 78 83 78
30 | 7 10 8 7 13 2 7 6 8 14 3 | 32 34 34 32 33 31 35 36 32 35 32
31 | 5 14 7 8 8 3 8 7 7 24 3 | 41 43 42 47 40 42 49 39 42 35 41
32E | 7 12 13 8 9 3 10 4 11 13 3 | 48 48 46 47 47 47 46 50 49 53 47
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 9 12 4 9 7 8 17 |T 39 40 39 40 39 39 42 42 40 41 39
WRMS | 7 13 10 9 10 4 9 6 8 15 |NE 33 36 34 35 35 34 37 36 35 35 34
MEDI | 7 12 8 8 10 4 9 6 8 17 |MD 36 39 38 36 37 36 39 37 38 39 37
Table 3.2096.1 GPS week: 2096 Day: 1 MJD: 58917.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 9 11 9 6 3 7 12 9 13 3 | 21 25 23 25 24 22 26 25 21 22 22
2 | 7 8 10 10 9 4 10 11 8 19 3 | 17 17 19 23 22 18 21 22 16 19 17
3 | 6 10 12 7 8 4 8 9 9 12 3 | 24 26 24 25 26 24 29 26 26 26 24
X4E | 11 --- 17 15 --- 8 24 9 17 45 7 | 44 --- 44 48 --- 43 47 48 45 60 45
5 | 7 11 8 9 14 4 8 9 8 16 3 | 27 30 27 27 30 27 31 28 25 28 26
6 | 9 10 9 8 6 3 7 9 7 9 3 | 23 25 23 28 26 24 28 21 19 25 22
7 | 8 11 7 7 11 3 9 11 6 30 3 | 36 35 34 37 35 34 38 34 34 35 34
8E | 7 18 14 11 10 4 11 17 10 14 4 | 30 29 30 32 33 28 29 30 26 28 28
9E | 7 12 12 13 11 4 8 9 9 19 3 | 40 40 36 38 38 37 40 40 39 39 38
10 | 5 9 12 6 9 4 8 11 11 11 3 | 26 25 28 25 26 25 31 29 24 31 25
11 | 8 18 18 13 13 4 8 13 10 14 4 | 27 36 22 35 29 29 34 31 29 26 28
12 | 6 18 8 7 15 5 8 12 10 21 4 | 40 43 37 39 43 40 44 41 40 40 39
13 | 8 14 6 8 11 5 7 8 12 15 3 | 32 34 31 34 35 31 36 34 35 36 33
14 | 6 12 9 10 11 4 9 7 9 16 3 | 45 44 44 48 47 44 46 44 42 44 44
15E | 15 14 6 11 12 3 9 6 9 18 4 | 30 22 23 24 27 22 22 22 24 29 23
16 | 5 18 5 8 9 4 6 9 7 25 3 | 25 28 26 27 25 23 28 24 26 27 24
17E | 10 13 9 6 13 3 8 10 8 16 3 | 56 55 49 57 62 54 55 55 53 50 54
X18 | 74 29 --- 14 --- 21 --- 15 23 --- 11 | --- --- --- --- --- --- --- --- --- --- 0
19E | 11 14 10 6 14 4 9 7 10 17 3 | 32 38 36 37 37 38 41 39 36 45 36
20 | 7 11 8 7 9 4 7 8 6 19 3 | 25 23 23 27 24 24 27 27 21 28 24
21 | 4 10 7 6 7 4 7 8 7 19 3 | 25 26 26 29 28 26 30 26 26 31 26
22 | 7 15 8 9 10 4 7 9 11 15 3 | 35 39 33 36 37 34 38 35 34 35 34
X23E | 7 24 9 12 11 5 9 9 14 --- 4 | 26 29 24 29 30 24 24 26 25 --- 24
24 | 10 7 8 7 12 3 9 8 11 12 3 | 28 29 29 29 27 27 32 28 28 28 27
25 | 6 11 11 9 11 4 8 8 9 8 3 | 24 29 24 26 30 25 31 26 25 28 25
26 | 4 11 8 6 6 4 5 7 8 11 2 | 24 25 24 25 26 23 30 23 23 27 24
27E | 9 14 15 6 11 3 13 12 8 12 4 | 28 27 27 32 32 28 34 31 29 30 28
28 | 6 12 9 7 7 3 6 11 9 23 3 | 27 31 22 27 27 27 30 26 30 32 26
29E | 10 18 10 13 15 5 8 10 12 19 4 | 54 52 54 56 52 56 56 53 55 60 53
30 | 7 8 9 6 9 3 7 12 6 14 3 | 26 30 28 28 29 26 31 30 25 26 27
31 | 5 13 9 7 8 3 8 7 8 27 3 | 28 32 30 34 28 29 35 29 31 27 29
32E | 7 13 13 9 7 3 9 9 7 10 3 | 36 36 34 33 37 36 39 38 37 40 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 10 9 10 4 8 10 9 17 |T 31 32 30 32 32 30 34 31 30 33 30
WRMS | 7 13 10 9 10 4 8 10 9 15 |NE 26 29 26 29 28 26 31 27 26 28 26
MEDI | 7 12 9 8 10 4 8 9 9 16 |MD 28 29 28 29 29 27 31 29 28 29 27
Table 3.2096.2 GPS week: 2096 Day: 2 MJD: 58918.000
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 | 10 7 11 10 7 3 6 7 10 15 3 | 28 28 30 28 26 27 31 27 26 28 27
2 | 10 9 9 11 9 4 7 7 8 21 3 | 24 20 23 26 20 21 21 21 22 21 20
3 | 9 9 11 7 9 4 8 6 8 16 3 | 21 22 22 20 20 20 24 22 18 25 20
X4E | 13 --- 13 16 --- 7 23 5 12 39 6 | 36 --- 33 38 --- 30 34 33 30 47 33
5 | 10 13 8 7 12 4 7 8 8 18 3 | 30 32 27 26 30 26 30 27 27 28 27
6 | 9 9 10 8 8 4 8 5 9 11 3 | 24 23 21 23 20 21 25 21 21 24 21
7 | 7 9 8 6 10 3 5 3 6 27 3 | 37 33 36 37 31 35 38 34 35 33 35
8E | 8 17 13 18 10 4 10 7 10 12 4 | 21 26 21 20 19 20 22 23 21 25 19
9E | 10 11 15 9 18 6 8 5 7 14 3 | 24 24 20 23 20 23 24 22 24 22 20
10 | 7 8 11 8 12 4 7 6 8 14 3 | 26 27 27 25 22 26 29 24 28 27 24
11 | 8 13 15 13 13 3 8 5 9 16 3 | 32 36 29 39 31 32 38 33 30 30 33
12 | 8 16 7 10 11 4 8 6 8 22 3 | 29 33 29 34 32 31 33 29 35 28 30
13 | 9 14 6 12 13 4 7 6 11 13 3 | 32 32 33 35 34 30 32 30 30 31 30
14E | 13 9 7 13 9 6 9 5 10 18 3 | 78 78 75 77 75 75 78 79 79 75 78
15E | 11 11 6 14 11 4 9 6 9 17 3 | 32 29 30 25 29 28 27 28 31 36 28
16 | 4 17 5 10 11 5 8 6 14 27 3 | 32 32 30 35 29 30 32 32 33 32 31
17E | 14 11 10 11 9 5 8 8 8 21 3 | 59 53 50 59 56 54 55 55 54 52 54
19E | 13 14 10 14 12 5 11 7 7 20 4 | 28 30 31 30 29 30 31 31 29 38 29
20 | 11 11 7 8 12 3 7 6 10 22 3 | 23 21 21 25 24 22 25 23 19 26 21
21 | 8 11 5 7 10 3 7 6 14 22 3 | 25 24 23 26 23 23 26 22 25 25 22
22 | 11 14 7 8 10 4 8 4 10 20 3 | 34 38 37 38 34 36 40 38 37 36 36
X23E | 9 23 9 10 15 6 10 5 8 --- 4 | 31 30 28 34 27 30 29 30 30 --- 29
24 | 7 11 7 8 10 3 8 7 8 9 3 | 37 39 37 33 38 36 40 36 33 39 36
25 | 6 10 10 4 9 4 6 5 6 9 2 | 21 26 21 22 19 20 24 19 20 21 20
26 | 7 9 7 5 6 3 6 5 8 13 2 | 27 29 29 30 27 30 31 28 28 28 28
27E | 8 17 15 9 12 5 11 7 11 10 4 | 24 25 23 28 24 25 25 23 26 26 23
28 | 6 11 9 7 9 4 5 4 6 20 2 | 30 30 25 28 27 29 31 28 29 33 28
29E | 7 17 11 7 37 4 9 8 9 21 5 | 34 33 33 33 51 32 32 31 36 35 32
30 | 6 8 7 7 9 3 7 3 7 10 2 | 29 30 29 29 28 28 31 29 27 29 28
31 | 7 12 5 10 8 5 9 7 8 26 3 | 36 35 32 40 32 34 39 33 37 28 34
32E | 7 13 12 8 10 3 9 6 9 14 3 | 23 30 24 24 22 25 29 25 28 27 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 10 10 12 4 8 6 9 18 |T 31 31 29 31 29 29 32 30 30 31 29
WRMS | 8 12 10 9 10 4 8 6 8 17 |NE 28 29 27 29 27 27 30 27 27 28 27
MEDI | 8 11 9 9 10 4 8 6 8 17 |MD 29 30 29 29 27 29 31 28 29 28 28
Table 3.2096.3 GPS week: 2096 Day: 3 MJD: 58919.000
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 7 10 7 9 2 6 11 7 12 3 | 29 29 29 28 28 28 32 28 26 27 28
2 | 11 13 7 7 9 4 7 7 9 20 3 | 23 22 21 24 19 19 20 23 19 20 19
3 | 7 11 9 10 10 3 9 9 8 11 3 | 21 28 24 23 23 22 27 24 25 26 23
X4E | 11 --- 14 17 --- 8 26 7 22 44 8 | 34 --- 36 38 --- 33 39 38 40 47 35
5 | 9 13 7 7 13 6 7 5 9 16 3 | 26 30 27 30 25 27 30 26 31 24 26
6 | 10 10 10 9 7 3 7 7 8 9 3 | 27 25 24 28 22 24 26 23 21 25 23
7 | 7 11 7 8 10 3 8 8 10 28 3 | 44 46 44 43 41 43 47 44 42 37 43
X8E | 9 --- 13 19 12 5 12 14 9 15 5 | 22 --- 23 26 23 20 25 23 23 23 21
9E | 11 16 12 9 9 3 7 9 13 21 4 | 25 26 22 26 24 24 26 27 25 27 23
10 | 9 11 12 6 12 3 5 8 8 14 3 | 21 23 25 22 24 21 27 25 22 31 22
11 | 10 13 15 7 13 3 9 11 9 12 4 | 29 33 28 33 30 30 37 32 32 27 30
12 | 6 17 6 6 11 3 7 8 10 22 3 | 29 34 27 26 28 27 30 27 27 23 27
13 | 11 15 7 15 30 5 7 8 8 16 4 | 32 36 34 39 39 32 37 32 33 36 33
14E | 6 14 6 9 10 6 8 7 9 13 3 | 33 30 32 33 36 31 34 36 30 32 32
15E | 8 12 7 17 22 4 8 5 12 18 4 | 23 22 27 19 27 23 26 26 34 30 23
16 | 8 15 7 7 10 5 8 7 9 26 3 | 24 26 24 26 26 24 26 27 26 27 24
17E | 10 14 10 14 11 4 8 8 8 20 3 | 56 50 49 58 55 52 53 52 55 51 53
19E | 9 13 10 16 8 4 10 7 9 19 4 | 38 38 40 38 38 37 40 40 36 43 38
20 | 11 13 8 8 9 3 8 7 6 18 3 | 24 24 21 24 24 23 25 25 22 27 22
21 | 6 8 5 10 7 3 7 8 6 18 3 | 22 24 21 24 22 22 26 24 22 26 22
22 | 10 12 6 8 12 3 8 8 9 18 3 | 28 33 28 28 31 28 33 31 29 32 29
X23E | 6 25 9 10 11 5 11 6 15 --- 4 | 19 23 22 24 17 20 18 18 25 --- 18
24 | 6 11 7 9 8 2 7 5 7 10 2 | 22 29 27 30 23 25 31 27 28 30 26
25 | 5 8 9 8 11 4 7 6 10 9 2 | 20 25 23 25 21 22 27 23 23 21 22
26 | 6 8 7 8 8 4 8 7 11 13 3 | 22 27 26 23 26 25 30 27 24 29 25
27E | 8 13 14 10 10 3 11 12 9 13 4 | 30 25 28 29 25 26 30 29 31 32 28
28 | 8 12 8 5 11 3 7 9 9 25 3 | 28 29 24 27 24 26 30 28 29 29 26
29E | 7 21 10 6 10 4 7 8 8 18 3 | 27 30 29 29 30 28 29 32 29 30 28
30 | 7 8 9 7 12 4 8 8 10 11 3 | 22 27 24 21 20 21 29 25 21 24 22
31 | 7 12 6 8 9 3 8 8 7 24 3 | 37 38 35 38 36 35 43 36 33 27 36
32E | 6 12 13 7 11 4 11 8 8 7 3 | 25 28 27 25 25 24 29 29 25 26 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 9 9 12 4 8 8 9 17 |T 27 29 28 29 27 27 31 29 28 29 27
WRMS | 8 13 9 9 10 4 8 8 8 17 |NE 26 29 26 27 25 25 30 27 26 26 26
MEDI | 8 12 9 8 10 4 8 8 9 16 |MD 26 28 27 27 25 25 30 27 27 27 26
Table 3.2096.4 GPS week: 2096 Day: 4 MJD: 58920.000
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 12 7 6 3 7 15 7 14 3 | 20 22 24 24 21 21 26 24 19 19 21
2 | 6 10 7 7 8 3 7 12 6 22 3 | 19 18 18 24 17 19 20 23 18 21 17
3 | 8 10 11 8 9 3 7 14 7 13 3 | 20 22 21 18 18 19 24 24 21 26 19
X4E | 12 --- 16 19 --- 8 23 12 18 45 8 | 33 --- 31 38 --- 29 35 35 34 46 32
5 | 6 10 10 5 11 3 7 9 7 18 3 | 29 26 28 29 24 28 29 29 31 28 27
6 | 6 9 9 8 6 5 6 11 8 8 2 | 19 22 20 21 18 20 24 20 20 21 19
7 | 5 11 10 10 7 5 6 13 10 28 3 | 38 38 39 39 35 38 41 40 38 36 37
8E | 9 20 14 20 13 4 8 19 11 13 5 | 20 24 20 28 24 20 21 23 20 21 19
9E | 10 11 15 6 9 5 8 13 11 22 4 | 27 24 22 23 23 24 26 27 25 27 22
10 | 5 11 11 8 10 4 5 13 7 14 3 | 27 25 29 26 26 26 30 30 28 30 26
11 | 7 14 16 11 12 5 6 15 7 20 4 | 23 28 22 29 24 24 30 28 22 25 24
12 | 6 15 8 8 12 3 6 12 8 23 3 | 30 33 30 34 31 32 34 34 34 29 30
13E | 7 15 9 8 13 6 7 9 11 16 3 | 35 36 34 30 31 34 37 38 36 38 33
14E | 5 10 9 8 11 7 7 10 8 16 3 | 28 25 28 30 31 27 24 25 27 24 26
15E | 10 14 7 19 11 3 7 9 14 17 4 | 26 22 25 19 26 22 23 24 29 31 22
16 | 6 16 6 5 10 6 8 12 7 28 3 | 27 29 26 26 27 26 31 29 26 30 27
17E | 12 13 10 10 8 6 7 13 11 16 3 | 59 50 47 54 52 51 55 53 49 48 52
19E | 13 13 9 13 9 5 9 12 11 17 4 | 31 37 34 32 30 32 37 33 36 41 33
20 | 8 9 7 6 11 2 5 12 9 20 3 | 22 21 24 25 21 22 27 28 24 27 22
21 | 6 11 5 8 7 4 5 11 11 21 3 | 23 23 23 25 23 22 26 25 24 29 22
22 | 8 12 7 7 10 4 7 12 9 18 3 | 25 30 28 26 25 26 31 33 29 28 27
X23E | 8 26 9 9 10 6 11 13 11 --- 4 | 29 33 27 28 19 26 24 35 28 --- 26
24 | 6 12 9 5 9 3 6 10 10 8 3 | 32 36 33 34 32 32 36 33 28 34 32
25 | 7 11 12 7 10 2 7 11 5 8 3 | 18 22 21 26 20 21 23 22 22 20 20
26 | 10 9 8 7 8 6 7 9 9 15 3 | 22 24 21 20 23 20 26 22 20 26 21
27E | 8 16 14 13 12 4 12 17 10 11 4 | 27 32 26 27 26 25 28 29 28 27 25
28 | 8 10 8 7 9 4 6 13 10 26 3 | 24 28 21 26 23 25 28 25 24 29 23
29E | 7 16 10 8 11 5 7 15 9 17 3 | 34 37 35 34 34 36 35 37 39 38 34
30 | 6 8 9 8 7 5 5 13 12 19 3 | 27 31 32 31 29 29 34 32 30 33 29
31 | 8 12 7 5 7 5 8 11 7 25 3 | 32 34 32 34 28 33 39 36 32 25 32
32E | 7 9 14 8 10 4 8 15 7 9 3 | 23 24 23 22 21 23 26 26 25 27 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 10 9 10 4 7 13 9 18 |T 27 28 27 28 26 26 30 29 27 29 26
WRMS | 7 12 10 10 9 4 7 12 8 17 |NE 25 26 25 27 24 25 29 28 25 27 25
MEDI | 7 11 9 8 10 4 7 12 9 17 |MD 27 26 26 27 24 26 28 29 28 28 26
Table 3.2096.5 GPS week: 2096 Day: 5 MJD: 58921.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 9 8 12 6 3 7 14 9 14 3 | 22 23 23 19 21 21 27 23 20 23 21
2 | 8 10 7 9 8 4 8 10 8 20 3 | 19 19 18 24 17 18 18 22 20 18 17
3 | 8 9 9 10 7 3 7 15 6 17 3 | 25 27 27 26 22 24 27 28 24 31 24
X4E | 13 --- 15 20 --- 6 22 12 19 45 8 | 37 --- 42 49 --- 40 43 43 43 53 41
5 | 7 11 7 8 10 4 7 8 9 19 3 | 32 32 32 34 28 31 31 32 32 33 31
6 | 8 9 9 7 6 3 7 8 7 8 2 | 25 23 23 26 21 23 26 22 23 26 23
7 | 7 11 7 8 6 3 8 12 8 29 3 | 32 33 30 33 30 30 34 32 30 33 30
8E | 13 23 11 41 10 4 10 23 11 16 6 | 23 28 21 33 24 21 23 27 22 23 20
9E | 9 17 15 13 11 6 7 12 9 17 4 | 39 40 38 39 36 38 37 40 40 37 37
10 | 11 11 10 6 9 4 6 15 7 16 3 | 30 31 32 31 26 30 34 35 27 40 29
11 | 8 15 14 14 10 4 7 15 8 16 4 | 26 33 23 34 26 27 34 31 27 29 28
12 | 7 14 6 9 13 3 7 10 6 21 3 | 29 33 32 30 31 29 33 33 29 28 30
13E | 11 13 5 9 13 4 10 9 10 15 3 | 32 32 32 34 32 32 36 38 37 37 33
14E | 11 10 8 8 11 4 8 13 7 14 3 | 27 27 25 28 24 25 25 34 26 26 25
15E | 13 17 8 17 14 5 10 12 11 19 4 | 25 22 22 20 26 22 21 24 25 27 21
16 | 9 16 5 7 8 5 9 12 7 27 3 | 28 29 29 28 25 27 28 28 26 27 26
17E | 8 13 10 7 10 4 9 10 6 18 3 | 66 60 57 64 66 61 63 62 64 58 62
19E | 11 14 9 13 13 3 9 11 8 16 4 | 47 52 53 53 46 50 54 52 53 58 51
20 | 8 9 6 7 10 3 7 11 6 18 3 | 23 23 24 28 23 25 26 29 21 28 23
21 | 6 12 5 8 8 4 6 11 10 19 3 | 20 24 20 25 22 21 26 25 19 27 20
22 | 10 12 7 8 7 3 6 13 9 20 3 | 32 30 28 30 27 31 35 36 28 33 30
X23E | 11 25 7 14 11 6 9 11 10 --- 4 | 28 27 24 29 23 24 23 25 28 --- 23
24 | 6 9 6 9 7 3 8 8 6 8 2 | 32 29 33 35 31 30 32 29 28 30 30
25 | 7 10 9 10 10 2 9 9 5 11 3 | 21 24 24 25 22 22 26 24 19 24 22
26 | 10 10 7 6 9 4 7 10 6 13 3 | 20 23 22 22 23 21 27 22 21 25 21
X27E | 10 --- 14 10 8 4 13 15 11 16 4 | 30 --- 28 34 30 31 34 34 31 34 29
28 | 9 11 8 7 10 4 9 12 6 26 3 | 30 29 24 27 24 26 29 26 28 31 26
29E | 9 15 9 10 12 4 9 13 11 16 4 | 49 50 52 50 51 49 50 51 50 55 49
30 | 5 8 7 7 4 3 7 11 9 15 2 | 26 28 27 27 24 24 29 26 26 27 25
31 | 9 11 6 6 7 4 9 11 7 23 3 | 29 29 27 31 22 27 35 29 28 25 27
32E | 11 12 12 9 7 3 8 12 10 10 3 | 37 39 36 38 36 37 40 41 37 40 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 12 9 4 8 12 8 18 |T 30 31 29 32 28 29 32 32 30 32 29
WRMS | 8 13 9 11 8 4 8 12 7 18 |NE 26 27 26 28 24 25 29 28 25 28 25
MEDI | 9 11 8 9 9 4 8 12 8 16 |MD 29 29 27 30 25 27 31 29 28 29 27
Table 3.2096.6 GPS week: 2096 Day: 6 MJD: 58922.000
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 8 4 3 6 7 7 8 2 | 29 31 28 27 28 28 33 30 29 27 29
2 | 11 11 10 6 8 3 7 5 9 18 3 | 26 23 24 24 21 22 23 25 23 20 22
3 | 10 8 9 9 7 5 6 8 6 12 2 | 27 27 29 23 25 26 32 32 26 32 28
X4E | 10 --- 13 22 --- 7 21 9 15 39 7 | 53 --- 51 58 --- 49 53 56 46 62 52
5 | 10 14 11 7 12 3 7 6 9 16 3 | 39 37 40 39 36 39 40 39 39 40 38
6 | 9 10 10 6 6 3 7 6 7 13 2 | 34 32 31 30 31 31 34 33 32 39 32
7 | 11 10 6 11 7 5 8 10 10 26 3 | 60 55 56 57 52 56 58 60 52 55 55
8E | 9 27 12 49 7 5 10 12 14 16 6 | 35 38 31 47 34 32 33 39 32 35 33
9E | 13 10 15 15 10 5 6 9 11 15 4 | 55 49 51 57 49 51 53 59 47 53 52
10 | 10 14 11 5 6 3 8 7 7 13 3 | 36 36 35 35 32 34 37 38 30 36 34
11 | 10 17 14 13 10 3 7 8 7 14 3 | 38 40 29 40 34 35 40 36 37 34 35
12 | 8 13 8 8 11 4 7 7 8 19 3 | 45 45 43 43 42 40 46 46 39 41 43
13E | 9 11 7 16 9 3 8 4 12 19 3 | 26 26 27 30 25 26 29 28 27 30 26
14E | 14 12 8 8 11 5 9 6 14 13 3 | 27 24 22 26 22 21 22 21 21 24 21
15E | 14 15 7 9 10 4 8 5 8 15 3 | 33 30 32 27 30 31 30 28 33 34 29
16 | 11 15 6 10 8 4 9 8 8 27 3 | 39 40 38 39 37 37 39 40 40 41 38
17E | 11 14 9 7 8 3 7 6 7 16 3 | 84 74 72 81 83 77 79 83 75 72 79
X18 | 3 --- --- --- --- 171 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
19E | 23 15 9 11 11 4 8 6 9 16 4 | 56 64 64 59 59 61 64 67 59 71 61
20 | 10 11 9 7 8 2 7 6 10 17 3 | 28 31 25 31 29 28 32 34 23 35 29
21 | 9 12 8 7 7 4 7 8 11 19 3 | 27 27 24 28 28 25 29 28 25 31 26
22 | 11 11 6 8 7 6 7 7 8 19 3 | 43 45 42 42 41 42 47 48 42 47 43
X23E | 9 26 6 16 7 5 10 11 7 --- 4 | 27 26 22 30 19 24 22 24 28 --- 22
24 | 13 11 8 10 6 2 7 6 7 7 3 | 36 33 36 36 34 33 35 34 31 33 33
25 | 10 11 11 7 9 3 7 5 5 9 3 | 31 31 31 31 29 30 34 34 32 31 31
26 | 9 13 7 9 9 5 7 6 7 13 3 | 35 36 34 34 36 32 37 37 33 37 35
27E | 11 14 15 56 9 5 11 10 10 11 6 | 45 43 39 56 43 41 46 48 43 45 43
28 | 8 14 9 7 7 3 8 8 5 19 3 | 33 35 27 35 33 33 35 35 34 38 33
29E | 9 17 8 16 10 5 8 8 8 16 3 | 74 72 75 75 75 73 75 79 75 76 75
30 | 8 12 8 8 7 3 7 9 8 15 3 | 33 33 32 31 28 30 35 35 28 32 31
31 | 11 16 8 8 6 5 8 6 7 24 3 | 44 48 48 50 44 48 55 48 49 38 47
32E | 20 14 14 9 9 4 10 8 8 8 4 | 50 55 51 51 49 51 56 58 52 54 53
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 10 17 8 4 8 7 9 16 |T 40 39 38 41 37 38 41 42 38 41 38
WRMS | 10 14 10 13 8 4 8 7 7 16 |NE 35 36 34 35 33 34 37 37 33 36 34
MEDI | 10 13 9 9 8 4 7 7 8 16 |MD 36 36 34 36 34 33 37 37 33 37 34
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2096 GPS week: 2096 MJD: 58916.0-58922.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2577 |U 0 0 0 |U 0 0 0 |U 10 15 30 |
emr | emr 2877 | 0 0 0 |U 0 0 0 |U 18 20 35 |
esa | esa 2989 | 0 0 0 |U 0 0 0 | 13 13 26 |
gfz | gfz 2564 |U 0 0 0 |U 0 0 0 |U 9 13 26 |
grg | grg 2877 |U 0 0 0 |U 0 0 0 | 9 11 30 |
igr | igr 2996 | 0 0 0 | 0 0 0 | 10 14 27 |
igs | igs 2997 | 0 0 0 | 0 0 0 | 10 14 27 |
jpl | jpl 2989 |U 0 0 0 |U 0 0 0 |U 20 23 39 |
mit | mit 3003 | 0 0 0 |U 0 0 0 |U 14 18 40 |
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 5.2096.0 GPS week: 2096 Day: 0 MJD: 58916.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | ---- ---- ---- | ---- ---- ---- | 9 15 27 |
emr | emr 2976 | ---- ---- ---- | ---- ---- ---- | 19 16 32 |
esa | esa 3072 | ---- ---- ---- | ---- ---- ---- | 11 12 19 |
gfz | gfz 3072 | ---- ---- ---- | ---- ---- ---- | 8 11 19 |
grg | grg 2875 | ---- ---- ---- | ---- ---- ---- | 10 11 20 |
igr | igr 3064 | ---- ---- ---- | ---- ---- ---- | 10 13 20 |
igs | igs 3072 | ---- ---- ---- | ---- ---- ---- | 10 13 21 |
jpl | jpl 3072 | ---- ---- ---- | ---- ---- ---- | 19 22 38 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 10 11 25 |
Table 5.2096.1 GPS week: 2096 Day: 1 MJD: 58917.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 0 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
emr | emr 2957 | ---- ---- ---- | ---- ---- ---- | 19 19 30 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 12 13 20 |
gfz | gfz 0 | ---- ---- ---- | ---- ---- ---- | 9 11 21 |
grg | grg 2876 | ---- ---- ---- | ---- ---- ---- | 10 8 26 |
igr | igr 3030 | ---- ---- ---- | ---- ---- ---- | 9 12 22 |
igs | igs 3030 | ---- ---- ---- | ---- ---- ---- | 10 12 22 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 20 22 32 |
mit | mit 3072 | ---- ---- ---- | ---- ---- ---- | 16 13 45 |
Table 5.2096.2 GPS week: 2096 Day: 2 MJD: 58918.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | ---- ---- ---- | ---- ---- ---- | 10 17 28 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 17 24 37 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 14 18 29 |
gfz | gfz 2976 | ---- ---- ---- | ---- ---- ---- | 11 17 30 |
grg | grg 2878 | ---- ---- ---- | ---- ---- ---- | 9 13 38 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 12 17 29 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 11 17 29 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 21 25 38 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | 16 22 45 |
Table 5.2096.3 GPS week: 2096 Day: 3 MJD: 58919.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | ---- ---- ---- | ---- ---- ---- | 11 18 33 |
emr | emr 2784 | ---- ---- ---- | ---- ---- ---- | 23 22 25 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 13 13 26 |
gfz | gfz 2976 | ---- ---- ---- | ---- ---- ---- | 10 15 27 |
grg | grg 2878 | ---- ---- ---- | ---- ---- ---- | 9 13 32 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 11 16 30 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 12 16 27 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 22 26 39 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | 19 27 46 |
Table 5.2096.4 GPS week: 2096 Day: 4 MJD: 58920.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | ---- ---- ---- | ---- ---- ---- | 9 13 28 |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | 15 18 42 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 14 14 33 |
gfz | gfz 2976 | ---- ---- ---- | ---- ---- ---- | 9 12 24 |
grg | grg 2876 | ---- ---- ---- | ---- ---- ---- | 9 10 28 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 11 12 30 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 11 13 27 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 20 23 45 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | 10 15 39 |
Table 5.2096.5 GPS week: 2096 Day: 5 MJD: 58921.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | ---- ---- ---- | ---- ---- ---- | 9 14 35 |
emr | emr 2784 | ---- ---- ---- | ---- ---- ---- | 14 19 44 |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | 12 10 30 |
gfz | gfz 2975 | ---- ---- ---- | ---- ---- ---- | 9 11 32 |
grg | grg 2879 | ---- ---- ---- | ---- ---- ---- | 9 12 37 |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | 10 12 34 |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | 10 12 33 |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | 19 18 43 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | 11 22 43 |
Table 5.2096.6 GPS week: 2096 Day: 6 MJD: 58922.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
emr | emr 2880 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
esa | esa 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
gfz | gfz 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
grg | grg 2880 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igr | igr 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igs | igs 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
jpl | jpl 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
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 6.2096 GPS week: 2096 MJD: 58916.500-58922.500
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 -15 116 -82 -1 | 10 18
| 25 16 80 57 9 | 2
emr uuuux | 2 31 -228 122 -37 | 18 34
| 16 19 111 56 17 | 10
esa uuuuu | -4 16 43 -43 1 | 33 36
| 18 10 56 27 5 | 2
gfz uuuuu | 3 23 21 -126 8 | 18 24
| 17 17 142 113 6 | 4
grg uuuuu | 16 3 -26 -84 -2 | 1 11
| 11 12 51 65 5 | 3
igr xxxxx | 23 6 25 -2 4 | 0 14
| 11 16 54 32 5 | 3
irf xxxxx | 5 -21 2 10 0 | -1 16
| 10 8 15 19 8 | 2
jpl uuuuu | -1 -19 -75 58 3 | 44 48
| 17 19 55 70 11 | 4
mit uuuuu | 10 -19 20 16 -2 | 19 25
| 14 14 33 32 10 | 2
ngs uuuuu | -13 -3 77 164 1 | 12 18
| 48 50 183 178 4 | 2
sio uuuux | 2 23 -44 -52 10 | 50 53
| 28 37 99 79 14 | 3
Table 7.2096.0 GPS week: 2096 Day: 0 MJD: 58916.500
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 -24 183 -77 -8 | 8 19
emr uuuux | -19 32 -396 90 -40 | 29 39
esa uuuuu | -17 29 -11 -42 6 | 29 33
gfz uuuuu | 9 11 234 -87 3 | 12 20
grg uuuuu | 24 -2 -40 -64 2 | -4 13
igr xxxxx | 38 33 -88 10 4 | -5 17
irf xxxxx | 2 -11 -14 -25 5 | -3 19
jpl uuuuu | -17 -35 -75 -37 -3 | 37 42
mit uuuuu | -2 -28 -5 -33 3 | 17 25
ngs uuuuu | 64 68 -132 304 -1 | 8 17
sio uuuux | -11 -35 144 -79 7 | 44 48
Table 7.2096.1 GPS week: 2096 Day: 1 MJD: 58917.500
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 | -34 2 61 -159 -7 | 11 17
emr uuuux | 26 1 -199 63 -30 | 27 40
esa uuuuu | 10 0 25 -28 -2 | 33 35
gfz uuuuu | -10 7 152 -331 9 | 15 20
grg uuuuu | 27 8 40 -66 2 | -1 9
igr xxxxx | 5 20 10 36 2 | -1 11
irf xxxxx | -9 -26 12 14 -10 | 1 15
jpl uuuuu | -14 -31 18 121 22 | 41 44
mit uuuuu | 13 -10 27 24 -15 | 21 26
ngs uuuuu | 18 31 -207 412 -4 | 11 16
sio uuuux | -3 -12 -37 55 -1 | 49 50
Table 7.2096.2 GPS week: 2096 Day: 2 MJD: 58918.500
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 11 107 -43 -7 | 13 19
emr uuuux | 21 36 -333 63 -15 | 25 38
esa uuuuu | -16 21 152 -94 -5 | 36 38
gfz uuuuu | -19 12 -13 -138 3 | 19 25
grg uuuuu | 9 -4 46 -128 4 | 3 10
igr xxxxx | 23 5 62 0 -3 | 2 13
irf xxxxx | 2 -15 7 -3 -13 | 4 15
jpl uuuuu | -14 -38 -142 -38 -12 | 47 51
mit uuuuu | 18 -13 -8 22 -14 | 23 27
ngs uuuuu | 8 -11 172 291 -1 | 14 19
sio uuuux | -3 64 -97 39 -15 | 52 54
Table 7.2096.3 GPS week: 2096 Day: 3 MJD: 58919.500
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 -37 204 18 -10 | 10 18
emr uuuux | -3 62 -195 117 -18 | 19 34
esa uuuuu | 18 20 51 -64 -4 | 33 35
gfz uuuuu | 9 30 -151 -149 6 | 17 23
grg uuuuu | -5 20 -66 -199 1 | 1 11
igr xxxxx | 33 -9 42 -51 2 | -1 13
irf xxxxx | 2 -12 -22 13 -2 | -1 16
jpl uuuuu | 21 13 -142 100 4 | 43 48
mit uuuuu | 8 -31 -6 55 -7 | 19 25
ngs uuuuu | -59 -53 274 100 6 | 12 18
sio uuuux | -28 39 -174 -129 15 | 48 50
Table 7.2096.4 GPS week: 2096 Day: 4 MJD: 58920.500
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 -13 73 -125 -1 | 8 17
emr uuuux | 3 13 -112 130 -55 | 16 31
esa uuuuu | -21 6 61 -27 5 | 33 35
gfz uuuuu | 14 58 -144 -80 13 | 17 23
grg uuuuu | 15 14 -40 -88 -4 | 2 11
igr xxxxx | 19 3 73 16 11 | -1 14
irf xxxxx | 14 -23 -1 25 4 | -2 15
jpl uuuuu | 10 -10 -71 97 0 | 46 50
mit uuuuu | 31 3 30 -6 3 | 18 23
ngs uuuuu | -74 -77 229 130 2 | 12 19
sio uuuux | 57 58 -81 -28 11 | 49 52
Table 7.2096.5 GPS week: 2096 Day: 5 MJD: 58921.500
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 | -38 -24 -7 -101 10 | 9 17
emr uuuux | -2 37 -96 193 -43 | 9 31
esa uuuuu | 16 12 -16 -28 7 | 35 38
gfz uuuuu | 28 23 56 46 17 | 22 26
grg uuuuu | 21 -13 -32 -51 -7 | 3 11
igr xxxxx | 24 -16 41 14 8 | 2 14
irf xxxxx | 21 -30 21 32 3 | -1 16
jpl uuuuu | 20 -4 -48 46 7 | 47 51
mit uuuuu | -14 -38 86 52 2 | 19 25
ngs uuuuu | -38 -1 57 -28 -4 | 14 20
sio uuuux | 15 36 3 -153 27 | 52 55
Table 7.2096.6 GPS week: 2096 Day: 6 MJD: 58922.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 26 -19 192 -90 13 | 9 17
emr uuuux | -10 33 -263 198 -59 | 0 22
esa uuuuu | -17 21 37 -17 1 | 35 38
gfz uuuuu | -12 22 10 -147 1 | 23 29
grg uuuuu | 22 -3 -88 9 -10 | 3 10
igr xxxxx | 19 3 34 -43 5 | 3 15
irf xxxxx | 5 -27 8 10 10 | -2 14
jpl uuuuu | -13 -31 -66 118 0 | 47 52
mit uuuuu | 13 -17 15 -1 12 | 17 22
ngs uuuuu | -8 20 148 -62 6 | 12 17
sio uuuux | -14 13 -70 -71 24 | 54 58
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