[IGSREPORT-27507] Wk 2122 IGS Final Orbits
acc
acc at igs.org
Thu Sep 24 21:34:54 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2122 (Sep 06, 2020 - Sep 12, 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:
igs2122[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2122[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2122[0-6].cls IGS GPS clock combination summary report.
igs21227.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21227.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 | ESA | PTBB PTBB
0 | GRG | CCJ2 COCO CCJ2 COCO
1 | COD | CPVG NRIL TIXI TIXI
1 | ESA | JOG2 PTBB COCO PTBB
1 | GFZ | JOG2
1 | GRG | 13 COCO NRIL SVTL COCO NRIL SVTL
2 | COD | TIXI TIXI
2 | ESA | AREG COCO CPVG PTBB CPVG PTBB
2 | GRG | 29 13 29 CCJ2 CPVG DAV1 IRKJ SVTL CCJ2 COCO CPVG
2 | GRG | DAV1 IRKJ SVTL
2 | JPL | MATE MATE
2 | MIT | SPT0 SPT0
3 | COD | TIXI TIXI
3 | EMR | KERG
3 | ESA | PTBB COCO PTBB
3 | GRG | 13 13 CCJ2 COCO SVTL CCJ2 COCO SVTL
4 | COD | CHTI IRKJ
4 | EMR | 8 IRKJ TLSE
4 | ESA | SGOC SGOC
4 | GFZ | IRKJ IRKJ
4 | GRG | IRKJ COCO IRKJ
4 | JPL | 8
5 | COD | COCO SCUB TIXI TIXI
5 | EMR | 27 27 QAQ1 HLFX QAQ1
5 | ESA | PTBB PTBB
5 | GRG | 21 21 COCO SVTL SVTL
6 | COD | 27 COCO TIXI TIXI
6 | ESA | ARTU PTBB ARTU COCO PTBB
6 | GRG | ADIS CCJ2 COCO LPGS SVTL ADIS COCO LPGS SVTL
6 | MIT | SPT0 SPT0
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 | GFZ | 8
6 | GFZ | 4 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.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
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 | .2 -.1 1.1 4 0 1 -.54
EMR | 0 | -3.3 1.1 -3.6 -27 7 16 -.30
ESA | 0 | -.9 -1.4 1.2 -47 -12 -7 -.77
GFZ | 0 | .1 -.4 1.2 -9 -10 1 -.45
GRG | 0 | -1.8 -2.4 6.7 -17 -6 -23 -.24
JPL | 0 | 5.8 -10.7 -.2 -2 -15 12 -.45
MIT | 0 | -2.5 -2.3 5.5 0 0 7 -.20
NGS | 0 | -2.1 -7.3 1.5 -21 -17 -15 -.15
SIO | 0 | -6.6 1.6 6.5 71 61 66 -.45
COD | 1 | .3 -.3 1.2 -1 -2 -2 -.54
EMR | 1 | -12.2 1.2 -7.1 -32 1 10 -.36
ESA | 1 | -1.0 -1.6 .4 -17 -5 -13 -.69
GFZ | 1 | .3 -.4 1.1 2 -11 8 -.50
GRG | 1 | -7.4 4.6 17.6 -14 -25 -19 -.34
JPL | 1 | 1.4 .1 1.2 16 -4 -7 -.29
MIT | 1 | -2.2 2.7 5.7 14 14 -15 -.20
NGS | 1 | -3.2 -1.9 5.8 -15 3 -16 -.18
SIO | 1 | -5.8 6.0 3.0 132 54 97 -.54
COD | 2 | .3 -.2 1.1 2 2 1 -.54
EMR | 2 | -.1 2.6 -4.8 -16 3 30 -.47
ESA | 2 | -.3 -1.4 .4 -14 -8 -4 -.57
GFZ | 2 | .1 -.5 1.1 -3 -8 3 -.39
GRG | 2 | -4.1 3.2 13.9 -16 -22 -12 -.21
JPL | 2 | 5.3 -.3 -3.7 4 2 0 -.37
MIT | 2 | 4.2 2.8 2.4 8 6 -18 -.23
NGS | 2 | -2.3 .0 2.7 1 -10 -4 -.41
SIO | 2 | -.3 8.5 3.8 200 -39 109 -.72
COD | 3 | .4 -.1 1.2 3 0 3 -.55
EMR | 3 | 3.8 -1.3 -4.2 -28 7 10 -.43
ESA | 3 | -.8 -1.3 .1 -20 -9 -2 -.71
GFZ | 3 | .2 -.2 .5 9 -3 7 -.41
GRG | 3 | 3.2 1.3 22.8 -10 -11 -17 -.40
JPL | 3 | 9.9 -8.3 .1 -2 8 0 -.40
MIT | 3 | 6.0 -.2 .4 0 -13 1 -.23
NGS | 3 | 3.1 -4.7 .9 -25 -13 -2 -.29
SIO | 3 | 1.7 3.1 6.1 94 -77 79 -.51
COD | 4 | .5 .0 1.1 4 -2 1 -.64
EMR | 4 | .5 10.5 -2.7 -26 5 17 -.40
ESA | 4 | -1.2 -1.7 .1 -21 -2 -10 -.65
GFZ | 4 | .4 -.1 .6 9 -14 8 -.48
GRG | 4 | 1.9 .1 10.6 -30 -8 -29 -.28
JPL | 4 | -3.8 2.0 4.9 2 -9 10 -.35
MIT | 4 | 3.5 -2.7 5.7 6 -4 -10 -.21
NGS | 4 | 2.1 -2.7 4.7 -31 -17 13 -.43
SIO | 4 | -4.9 1.0 14.6 70 8 92 -.50
COD | 5 | .3 -.1 1.0 2 4 -7 -.65
EMR | 5 | -16.1 11.8 -3.7 -11 3 0 -.40
ESA | 5 | -1.5 -1.5 -.6 -10 5 -22 -.82
GFZ | 5 | .5 -.1 .9 2 -15 10 -.59
GRG | 5 | -4.0 2.7 5.0 -23 -1 -27 -.37
JPL | 5 | -5.4 4.1 5.5 1 -13 3 -.28
MIT | 5 | -4.6 1.1 3.4 7 0 0 -.37
NGS | 5 | -6.4 -3.4 5.3 -37 -2 -41 -.37
SIO | 5 | -12.7 4.2 9.0 116 154 134 -.38
COD | 6 | .3 -.1 1.1 2 2 -4 -.56
EMR | 6 | -9.4 6.2 -5.0 -22 3 12 -.36
ESA | 6 | -1.0 -1.2 -.0 -16 3 -14 -.66
GFZ | 6 | .1 -.2 1.0 -2 -9 2 -.52
GRG | 6 | -2.7 3.0 4.6 -33 -7 -35 -.17
JPL | 6 | -.4 .5 -2.8 0 -11 3 -.48
MIT | 6 | -2.1 1.0 3.2 18 18 -6 -.21
NGS | 6 | -4.7 1.7 6.7 -15 1 -5 -.40
SIO | 6 | -6.7 3.6 7.4 108 61 100 -.40
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 1.2122.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2122.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 2.2122.[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 3.2122.[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 5.2122.0-6). 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 2122 summary. (Sep 06, 2020 - Sep 12, 2020)
Table 1.2122.a GPS week: 2122 MJD: 59098.000-59104.000
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 758| 0 0 0 -4 -11 21 -.08 7 7 | -844 303 5 100
| 0 0 1 12 13 19 .03 | 108 312
emr 80| -2 3 -2 -6 10 -3 -.01 12 12 | 201488 -4 12 94
| 1 3 1 27 17 8 .07 | 654 662
esa 150| 0 0 -3 -2 -7 -25 -.07 9 9 | -1252 235 7 86
| 0 0 1 21 8 11 .01 | 922 1549
gfz 177| 0 0 0 -4 5 -5 .09 12 10 | -159 86 88 531
| 0 1 1 26 17 7 .02 | 349 373
grg 108| 2 0 8 -4 0 1 -.04 11 9 | 68 -52 9 126
| 0 0 6 15 14 14 .02 | 181 253
igr n/a| 0 0 -2 0 -11 -6 .03 4 4 | 3822 -301 11 85
| 0 0 0 18 15 7 .01 | 465 505
jpl 80| 0 0 -2 0 -10 -12 .26 8 8 | 1165 -318 7 80
| 1 2 1 18 15 9 .01 | 611 786
mit 373| 0 0 1 -8 1 -19 -.03 6 6 | 3584 -276 24 1309
| 0 0 1 30 26 30 .01 | 647 492
ngs 186| 0 0 3 14 15 -20 -.04 9 8 | -853 283 833 2142
| 0 0 1 16 7 24 .02 | 110 281
sio 388| 0 0 -2 33 0 73 -.04 9 8 | --- --- --- ---
| 0 0 1 67 32 31 .02 | --- ---
Table 1.2122.b GPS week : 2122 MJD: 59098.000-59104.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 3 3 3 3 3 |
2 | 3 3 3 4 3 3 3 |
3 | 3 3 3 3 3 3 3 |
4 | 6 6 6 7 7 8 7 |
5 | 3 3 3 3 3 3 3 |
6 | 3 2 3 3 3 2 2 |
7 | 3 2 2 3 3 3 3 |
8 | 5 6 6 7 7 5 4 |
9 | 4 3 4 4 4 4 6 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 3 3 4 4 4 3 3 |
13 | 3 3 4 4 3 3 3 |
15 | 3 3 4 4 4 4 4 |
16 | 3 4 3 4 4 3 4 |
17 | 3 3 3 3 4 3 3 |
18 | 3 3 3 3 3 3 3 |
19 | 3 3 3 3 3 3 3 |
20 | 3 3 3 3 3 3 2 |
21 | 3 3 3 3 3 3 3 |
22 | 3 3 3 3 3 3 3 |
23 | 12 17 9 12 10 14 9 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 3 2 3 |
27 | 5 4 5 5 6 8 5 |
28 | 3 3 3 3 3 3 3 |
29 | 4 3 4 4 4 3 4 |
30 | 3 3 2 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 3 3 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 2.2122.0 GPS week: 2122 Day: 0 MJD: 59098.000
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 766| 0 0 0 -7 3 41 -.08 6 6 | -671 57 6 101
emr 80| 0 2 0 19 13 5 .09 12 12 | 201468 -684 11 100
esa 150| -1 0 -4 20 -10 -17 -.08 10 9 | -987 -130 9 72
gfz 181| 0 0 -1 20 13 -9 .08 11 9 | -45 75 82 523
grg 109| 2 0 7 19 -1 12 -.01 11 9 | 127 -122 10 124
igr n/a| 0 0 -2 30 -3 -3 .04 4 4 | 4682 -774 10 75
jpl 80| 0 0 -3 25 -2 -19 .26 8 8 | 2152 -1272 8 81
mit 373| 0 0 3 -8 -21 -37 -.05 6 6 | 4879 -755 23 1524
ngs 189| 0 0 2 30 29 -20 -.05 10 8 | -676 50 897 2191
sio 397| 0 0 -3 -72 -12 35 -.08 8 8 | --- --- --- ---
Table 2.2122.1 GPS week: 2122 Day: 1 MJD: 59099.000
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 764| 0 0 0 4 -26 -9 -.07 7 6 | -725 18 6 94
emr 80| -3 1 -2 -6 9 3 .07 11 11 | 200913 -804 12 120
esa 150| 0 0 -4 10 -11 -15 -.06 10 10 | 107 -1968 8 82
gfz 181| 0 0 -1 25 4 -12 .07 12 9 | 343 -371 84 530
grg 110| 2 0 14 0 -9 -2 -.05 12 11 | 253 -451 10 130
igr n/a| 0 0 -3 5 -10 -10 .04 4 4 | 4148 -1094 11 81
jpl 80| 0 -1 -3 2 -18 -3 .26 8 8 | 1074 -1198 6 73
mit 373| 0 0 0 -3 6 -19 -.04 6 5 | 3546 -990 22 1534
ngs 186| 0 0 4 10 21 -12 -.06 9 7 | -730 12 786 1973
sio 399| 0 0 -3 -21 18 78 -.04 8 7 | --- --- --- ---
Table 2.2122.2 GPS week: 2122 Day: 2 MJD: 59100.000
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 760| 0 0 1 -21 -13 10 -.08 6 6 | -829 95 5 84
emr 80| 0 1 -3 -33 12 -4 -.07 12 12 | 200569 516 12 82
esa 150| 0 0 -4 -23 -5 -35 -.08 9 9 | -2784 3059 7 75
gfz 178| 0 0 0 -28 9 -15 .11 12 10 | 29 -270 85 543
grg 109| 3 0 14 -21 0 2 -.06 12 10 | 60 -140 10 139
igr n/a| 0 0 -1 -27 -9 -18 .04 4 4 | 3494 -208 12 84
jpl 80| 0 0 -3 -10 -22 -21 .25 8 8 | 363 215 7 83
mit 373| 0 0 1 8 14 -1 -.01 7 6 | 3022 -189 23 877
ngs 182| 0 0 2 40 9 -27 -.03 8 7 | -857 99 844 2167
sio 388| -1 0 -4 85 -8 90 -.02 9 8 | --- --- --- ---
Table 2.2122.3 GPS week: 2122 Day: 3 MJD: 59101.000
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 757| 0 0 1 -4 -22 43 -.08 7 7 | -914 227 6 99
emr 80| -1 0 -1 10 34 -11 -.08 12 12 | 201099 1070 12 94
esa 150| -1 0 -4 9 -3 -12 -.07 10 9 | -2021 1162 7 105
gfz 172| 0 0 3 10 23 0 .09 12 11 | -410 400 84 533
grg 108| 1 0 16 1 17 26 -.07 14 11 | -13 185 10 107
igr n/a| 0 0 -2 2 6 4 .03 4 4 | 3368 406 12 81
jpl 80| 2 -5 -2 15 5 -6 .28 10 10 | 529 875 8 70
mit 373| 0 0 0 -24 1 -45 -.03 6 5 | 2971 414 34 1313
ngs 186| 0 0 0 8 11 -4 -.01 10 8 | -923 205 704 2005
sio 378| -1 0 -4 -1 -34 51 -.02 8 7 | --- --- --- ---
Table 2.2122.4 GPS week: 2122 Day: 4 MJD: 59102.000
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 752| 1 -1 -1 10 8 30 -.06 7 7 | -892 433 6 104
emr 80| -3 6 -3 -40 16 -17 -.06 13 13 | 202214 53 13 92
esa 150| 0 -1 -2 -33 -9 -36 -.07 9 9 | -874 45 7 80
gfz 177| 0 0 0 -44 -4 -9 .11 12 11 | 7 284 86 536
grg 108| 3 -1 3 -16 1 2 -.04 9 8 | 269 -133 9 117
igr n/a| 0 0 -1 -12 -11 -9 .02 4 4 | 3858 -6 11 95
jpl 80| -3 4 0 -25 -10 -22 .24 9 9 | 1536 -26 7 74
mit 373| 0 -1 0 39 11 37 -.02 7 7 | 3259 105 22 1391
ngs 186| 0 0 4 10 10 -67 -.05 9 8 | -894 470 886 2115
sio 389| 0 -1 -1 69 -35 48 -.03 11 9 | --- --- --- ---
Table 2.2122.5 GPS week: 2122 Day: 5 MJD: 59103.000
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 752| 1 0 0 -18 -21 9 -.14 8 7 | -950 913 6 113
emr 80| -6 8 0 30 12 -4 -.02 12 12 | 202174 121 15 87
esa 150| 0 0 -2 17 8 -38 -.08 9 9 | -933 -91 8 112
gfz 175| 1 0 0 7 22 6 .09 9 8 | -320 -155 97 535
grg 107| 2 0 0 4 13 -16 -.05 9 8 | 49 -45 8 126
igr n/a| 0 0 -2 10 -8 -6 .01 4 4 | 3756 -27 12 81
jpl 80| -1 2 0 10 7 -12 .25 7 7 | 1430 -78 8 101
mit 373| 0 -1 0 -59 -39 -22 -.04 6 5 | 3658 -54 22 1546
ngs 189| 0 0 2 11 13 -23 -.05 9 8 | -986 803 903 2130
sio 379| 0 -1 0 58 24 128 -.03 9 8 | --- --- --- ---
Table 2.2122.6 GPS week: 2122 Day: 6 MJD: 59104.000
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 756| 1 0 -1 6 -7 24 -.08 7 7 | -932 381 6 106
emr 80| -3 4 -2 -22 -23 4 .02 11 11 | 201980 -302 14 85
esa 150| 0 0 0 -17 -20 -22 -.08 9 9 | -1278 -431 6 79
gfz 177| 0 -2 -1 -20 -27 -1 .07 17 12 | -723 639 100 522
grg 111| 1 0 2 -22 -25 -12 -.03 9 8 | -269 338 8 144
igr n/a| 0 0 -1 -8 -44 0 .01 4 4 | 3453 -407 11 104
jpl 80| 0 1 -1 -18 -35 0 .26 8 8 | 1071 -743 7 80
mit 373| 0 0 0 -12 40 -50 -.03 6 6 | 3759 -468 22 982
ngs 187| -1 0 5 -10 8 11 -.06 9 8 | -909 345 814 2415
sio 388| -1 0 -2 117 50 78 -.06 9 8 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.2122.0 GPS week: 2122 Day: 0 MJD: 59098.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 4 9 7 7 10 3 6 5 12 8 2 | 26 30 29 27 30 27 32 24 28 27 27
2 | 8 12 5 9 9 4 6 9 8 7 3 | 14 19 18 21 21 17 19 20 17 19 17
3 | 4 11 11 8 16 3 8 6 8 5 3 | 22 28 25 21 24 23 27 21 23 23 22
X4E | 10 25 16 20 --- 3 10 9 19 12 5 | 68 71 71 78 --- 69 69 69 72 70 70
5 | 6 16 5 9 8 5 7 5 7 6 2 | 49 48 49 50 52 49 50 49 53 51 49
6 | 5 9 6 9 7 2 7 6 7 7 2 | 25 28 27 26 29 26 29 26 27 27 26
7 | 6 8 6 9 9 5 8 3 6 9 2 | 52 52 54 52 45 53 54 51 51 49 51
8E | 7 13 20 29 19 5 11 8 16 7 5 | 96 98 98 106 98 96 76 95 97 97 97
9E | 6 8 16 11 11 4 8 7 9 10 3 | 45 46 43 44 49 43 45 42 44 45 44
10 | 6 12 10 8 8 3 9 6 10 7 3 | 22 24 25 25 25 23 26 23 23 24 23
11 | 5 15 15 10 15 2 8 10 18 10 4 | 23 29 20 28 28 25 30 26 32 29 24
12 | 7 17 6 9 10 5 7 7 7 12 3 | 35 40 35 35 33 35 38 35 36 37 36
13 | 7 15 5 10 11 4 10 7 7 6 3 | 49 49 49 51 53 49 49 46 48 49 48
15E | 7 12 9 9 11 5 11 6 7 9 3 | 117 116 120 119 117 118 116 118 118 121 118
16 | 4 19 9 10 8 4 7 8 8 12 3 | 23 22 21 24 23 22 25 25 26 30 23
17E | 5 15 7 10 12 4 10 6 7 8 3 | 24 30 19 25 27 22 26 23 22 27 23
18 | 9 13 11 10 5 5 7 5 13 9 3 | 15 22 22 22 21 16 22 17 18 23 18
19E | 4 13 9 9 9 3 6 7 8 7 2 | 24 26 26 26 24 25 28 24 23 31 25
20 | 6 13 8 10 8 3 8 6 10 8 3 | 22 26 24 30 23 25 26 24 26 25 24
21 | 6 10 6 9 8 4 8 5 12 6 2 | 19 22 20 22 23 20 25 22 18 23 20
22 | 4 11 5 8 17 3 6 5 9 5 2 | 42 47 42 44 44 43 46 44 43 44 43
X23 | 6 --- --- --- 19 15 --- --- --- --- 11 | 51 --- --- --- 56 58 --- --- --- --- 53
24 | 7 9 8 9 6 3 7 4 7 6 2 | 28 28 28 25 25 28 31 26 26 30 27
25 | 9 8 9 7 8 4 7 4 6 7 2 | 21 25 24 26 23 23 27 20 22 23 22
26 | 6 6 9 9 5 4 7 8 5 10 2 | 22 27 24 27 23 24 28 23 23 28 23
27E | 7 12 19 24 12 4 9 7 14 8 4 | 38 39 42 49 43 39 18 37 42 39 39
28 | 6 10 4 6 7 3 8 6 8 9 2 | 20 25 20 24 25 21 26 20 23 21 21
29E | 6 15 11 8 20 3 9 6 10 9 3 | 43 43 46 45 49 44 44 45 45 44 44
30 | 5 8 5 8 7 2 8 7 6 6 2 | 25 30 26 26 24 26 31 26 25 26 26
31 | 5 11 9 11 7 3 7 7 9 7 2 | 60 57 61 59 52 58 60 54 55 56 57
32E | 7 10 12 7 6 4 9 7 12 9 3 | 51 50 49 50 53 51 51 49 52 51 50
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 12 10 11 11 4 8 6 10 8 |T 37 39 38 40 38 38 39 37 38 39 38
WRMS | 6 12 9 9 9 4 8 6 8 8 |NE 29 31 29 30 30 30 32 28 29 30 30
MEDI | 6 12 9 9 9 4 8 6 8 8 |MD 26 30 27 27 28 27 30 26 27 30 27
Table 3.2122.1 GPS week: 2122 Day: 1 MJD: 59099.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 10 7 9 11 2 6 4 7 7 2 | 28 31 29 31 31 28 32 25 28 29 28
2 | 8 10 8 11 10 4 8 6 9 9 3 | 17 23 25 26 22 21 22 24 22 23 21
3 | 5 8 12 10 16 4 7 5 8 6 3 | 22 26 25 23 28 23 28 22 23 25 23
X4E | 12 25 16 25 --- 5 12 9 22 12 6 | 51 56 56 65 --- 54 58 56 57 58 55
5 | 7 13 7 8 11 5 9 5 9 7 3 | 38 42 42 43 43 41 43 42 44 45 41
6 | 6 8 8 8 8 4 5 3 6 6 2 | 22 29 28 27 27 26 30 27 26 25 26
7 | 5 8 6 8 9 4 6 4 7 8 2 | 31 33 31 31 26 31 33 30 28 32 30
8E | 10 12 18 37 22 5 11 6 16 6 5 | 66 67 68 76 65 66 54 67 63 67 66
9E | 5 7 16 13 14 5 10 5 10 5 3 | 34 39 37 38 41 37 42 38 41 41 38
10 | 6 9 10 9 8 4 7 5 5 8 2 | 22 25 25 26 25 24 27 23 24 26 23
11 | 7 13 13 12 14 3 8 5 10 10 3 | 24 27 22 30 28 26 30 26 29 29 26
12 | 7 16 8 8 12 4 7 5 7 12 3 | 21 25 24 26 22 24 28 26 27 27 24
13 | 7 13 7 10 19 3 8 6 9 6 3 | 40 44 42 44 48 41 43 42 40 42 41
15E | 7 12 10 12 11 4 11 5 10 6 3 | 98 98 102 100 101 101 100 100 105 102 100
16 | 6 20 8 9 9 5 8 9 8 9 3 | 19 21 21 24 18 21 23 23 20 25 20
17E | 6 19 7 9 16 3 8 6 8 7 3 | 18 26 14 17 25 17 19 16 21 20 17
18 | 9 10 11 8 8 6 8 5 8 10 3 | 15 21 23 21 19 17 23 19 17 26 18
19E | 6 13 8 9 10 3 7 5 9 9 3 | 16 18 19 14 18 16 18 17 17 20 16
20 | 6 9 7 10 9 4 9 5 6 8 2 | 17 21 21 27 19 21 23 21 19 26 20
21 | 6 10 5 8 7 6 8 6 8 6 2 | 19 23 20 23 23 22 27 21 24 23 21
22 | 4 9 9 9 17 4 8 6 6 7 3 | 37 42 39 39 43 39 44 39 40 42 40
X23 | 8 --- --- --- 27 20 --- --- --- --- 16 | 32 --- --- --- 44 40 --- --- --- --- 35
24 | 7 7 8 11 8 3 7 6 8 7 2 | 21 24 24 21 23 23 28 23 21 25 22
25 | 7 8 9 10 9 5 5 3 9 6 2 | 18 25 21 24 22 21 26 21 21 23 21
26 | 5 7 8 10 5 5 6 7 5 7 2 | 19 25 22 23 20 21 27 20 20 23 21
27E | 8 12 16 23 13 6 10 9 10 9 4 | 38 38 42 42 40 38 23 38 39 40 38
28 | 7 9 6 6 8 3 7 4 11 6 2 | 17 25 22 20 19 19 24 21 22 20 20
29E | 9 15 11 9 14 3 9 5 8 8 3 | 28 25 23 28 25 25 23 27 24 29 24
30 | 5 8 7 9 7 3 8 7 8 7 2 | 22 29 23 26 23 23 30 25 23 25 24
31 | 7 8 8 11 8 4 6 6 8 7 2 | 39 40 39 41 34 39 42 38 34 43 38
32E | 7 11 12 8 7 4 9 7 10 6 3 | 40 43 42 40 44 41 44 42 40 42 41
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 11 10 12 12 4 8 6 9 8 |T 29 33 32 33 32 31 33 31 31 34 31
WRMS | 6 11 10 9 11 4 8 5 7 7 |NE 23 27 26 27 26 26 29 25 25 28 25
MEDI | 7 10 8 9 10 4 8 5 8 7 |MD 22 26 25 27 25 25 28 25 24 26 24
Table 3.2122.2 GPS week: 2122 Day: 2 MJD: 59100.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 4 11 7 8 9 3 6 5 7 10 2 | 23 25 25 28 24 25 29 23 22 25 24
2 | 8 11 6 10 9 4 6 8 8 9 3 | 15 18 18 18 19 18 19 21 19 20 17
3 | 7 12 11 9 13 4 7 6 10 8 3 | 19 20 20 19 26 20 24 19 21 20 19
X4E | 12 24 14 26 --- 5 10 11 15 13 5 | 29 30 36 48 --- 34 33 33 33 34 32
5 | 6 13 5 7 9 4 9 6 9 7 2 | 42 45 45 45 47 45 47 47 48 47 45
6 | 5 11 8 10 9 4 6 6 7 6 2 | 21 22 22 23 23 23 27 21 23 21 22
7 | 3 11 5 10 8 3 5 5 5 6 2 | 37 41 39 41 34 39 43 37 40 40 39
8E | 9 12 20 35 20 5 11 6 16 8 5 | 54 55 58 68 54 55 45 56 51 56 55
9E | 7 8 16 10 14 5 9 7 7 9 3 | 23 22 22 20 23 22 23 21 24 21 21
10 | 4 10 8 7 8 2 8 5 7 8 2 | 17 19 20 22 22 19 22 19 18 23 19
11 | 7 15 11 13 11 2 8 5 10 9 3 | 20 24 19 27 22 21 28 24 22 25 21
12 | 7 16 8 8 11 4 9 9 6 13 3 | 29 33 31 32 29 31 34 34 31 33 31
13E | 7 10 6 10 23 4 9 7 8 6 3 | 47 47 46 50 51 47 48 46 47 48 46
15E | 5 11 9 12 13 5 13 11 10 10 3 | 57 58 58 57 57 56 57 60 60 57 57
16 | 5 17 6 10 8 5 8 10 8 10 3 | 22 21 22 25 24 22 24 22 24 25 22
17E | 6 15 7 9 13 4 8 8 5 9 3 | 19 22 16 18 26 17 20 21 23 20 19
18 | 10 10 11 6 8 4 8 5 10 12 3 | 12 16 17 17 17 12 18 16 16 22 14
19E | 6 14 9 12 11 4 7 7 6 8 3 | 17 16 18 17 18 16 19 17 19 20 16
20 | 6 12 6 8 8 3 7 5 7 8 2 | 13 19 17 22 17 18 20 17 19 18 16
21 | 6 10 6 9 10 3 9 6 8 8 2 | 20 20 22 25 24 20 25 23 20 23 21
22 | 3 10 6 8 16 4 8 6 8 6 2 | 33 36 35 37 33 35 38 36 33 34 34
X23 | 5 --- --- --- 13 14 --- --- --- --- 8 | 40 --- --- --- 37 41 --- --- --- --- 40
24 | 5 10 7 10 7 5 9 7 9 7 2 | 23 24 25 21 20 23 29 21 20 24 22
25 | 8 7 9 7 7 5 7 5 9 7 2 | 18 22 23 23 20 21 26 20 20 19 20
26 | 6 7 7 10 6 5 5 11 6 10 3 | 18 22 21 24 18 20 25 20 21 22 20
27E | 9 10 17 25 18 5 11 12 11 10 4 | 24 25 28 31 29 25 18 28 25 29 25
28 | 5 11 4 8 9 3 7 6 7 8 2 | 17 23 18 22 20 19 24 20 21 19 19
29E | 6 15 13 8 16 5 8 7 8 9 3 | 43 45 46 47 43 46 46 44 43 42 43
30 | 4 8 6 10 7 4 6 6 5 6 2 | 17 21 20 18 17 19 25 19 17 17 18
31 | 7 8 6 10 8 3 7 6 8 10 2 | 42 43 41 44 34 41 45 38 36 42 40
32E | 6 12 13 11 7 3 8 7 11 8 3 | 27 30 27 29 30 28 30 31 29 31 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 12 9 12 12 4 8 7 8 9 |T 27 28 28 30 28 28 30 28 28 29 27
WRMS | 6 12 9 10 10 4 8 6 7 8 |NE 23 25 25 26 25 25 28 24 24 25 24
MEDI | 6 11 7 10 9 4 8 6 8 8 |MD 23 23 22 25 24 23 26 22 23 24 22
Table 3.2122.3 GPS week: 2122 Day: 3 MJD: 59101.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 4 9 8 10 11 3 7 4 7 6 2 | 18 22 20 24 21 19 26 19 19 20 19
2 | 9 12 7 12 10 4 9 9 11 10 3 | 15 18 19 18 19 18 21 22 18 20 17
3 | 7 14 10 12 16 4 6 3 9 6 3 | 17 21 19 16 25 17 23 17 18 18 17
X4E | 13 25 15 33 --- 6 12 10 17 12 6 | 24 28 31 54 --- 28 26 27 28 29 27
5 | 8 11 7 9 10 3 10 5 9 8 3 | 31 24 26 29 34 26 28 27 29 27 27
6 | 8 6 8 8 10 3 7 4 8 6 2 | 18 19 20 18 23 19 25 19 19 18 19
7 | 6 9 7 9 9 4 7 5 9 7 2 | 41 41 42 42 34 41 43 41 41 43 41
8E | 11 14 19 33 42 7 19 9 22 12 7 | 72 70 68 70 80 66 54 68 66 69 68
9E | 7 9 17 8 17 6 9 6 10 6 3 | 18 22 20 22 24 19 19 19 23 18 18
10 | 5 9 8 10 9 3 9 4 7 8 2 | 19 20 22 26 23 21 25 21 19 24 20
11 | 8 13 13 10 14 4 9 8 10 9 3 | 17 22 17 24 21 19 28 23 20 22 20
12 | 8 17 7 7 10 4 10 7 10 13 3 | 29 31 28 25 24 27 32 30 29 31 28
13E | 9 11 6 15 17 5 11 7 11 6 3 | 44 44 45 50 45 45 47 43 47 46 44
15E | 7 12 8 17 16 6 12 7 9 12 3 | 49 49 50 56 48 50 50 49 47 50 49
16 | 6 17 8 11 10 4 10 7 9 10 3 | 16 17 17 24 22 18 21 18 18 22 17
17E | 8 19 6 9 15 4 9 6 10 7 3 | 18 24 15 16 24 17 21 17 20 19 17
18 | 7 10 12 10 8 6 7 4 11 8 3 | 14 17 20 21 19 13 19 17 13 18 16
19E | 7 14 8 10 10 4 9 6 14 7 3 | 24 25 25 25 24 25 27 30 29 26 25
20 | 5 13 7 10 8 3 9 5 8 5 2 | 17 20 18 24 15 19 22 19 17 18 17
21 | 8 13 5 9 12 3 10 5 9 6 3 | 16 20 17 23 21 18 25 19 20 18 18
22 | 7 12 5 10 16 4 8 4 8 6 2 | 24 30 24 25 23 25 29 26 27 25 25
X23 | 5 --- --- --- 21 12 --- --- --- --- 12 | 43 --- --- --- 49 48 --- --- --- --- 45
24 | 6 10 9 9 8 4 8 4 7 11 2 | 22 24 25 20 19 22 28 22 22 25 22
25 | 10 10 11 6 8 2 8 5 6 7 2 | 15 21 21 20 18 18 25 17 17 19 18
26 | 6 7 8 9 6 4 7 8 5 7 2 | 20 24 23 20 19 21 25 20 21 21 20
27E | 10 15 16 16 27 6 14 7 11 8 4 | 27 28 31 28 38 28 23 31 30 31 29
28 | 7 11 4 5 9 4 8 4 10 6 2 | 17 22 17 20 22 18 25 20 22 19 19
29E | 6 16 13 9 17 5 10 6 11 10 3 | 27 30 28 27 34 25 27 29 29 29 27
30 | 7 8 8 8 8 3 8 6 7 6 2 | 19 24 20 19 18 20 26 22 20 22 20
31 | 6 11 7 10 9 4 9 4 7 8 2 | 41 43 45 40 34 42 45 41 40 43 41
32E | 7 9 14 11 9 4 10 5 9 9 3 | 24 26 23 27 28 24 29 26 25 28 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 10 12 14 4 10 6 10 8 |T 25 27 26 28 28 26 28 26 26 27 26
WRMS | 7 12 9 11 11 4 10 5 8 7 |NE 22 24 23 23 23 23 27 23 22 23 23
MEDI | 7 11 8 10 10 4 9 5 9 7 |MD 20 24 22 24 23 21 26 22 22 22 20
Table 3.2122.4 GPS week: 2122 Day: 4 MJD: 59102.000
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 11 8 9 8 4 7 7 9 10 3 | 19 24 22 24 20 21 27 17 19 19 20
2 | 8 13 6 10 8 4 9 12 9 8 3 | 14 17 17 16 18 16 19 22 23 20 16
3 | 6 9 10 10 12 5 7 6 11 9 3 | 21 23 24 22 25 22 26 20 23 19 21
X4E | 12 24 14 34 --- 7 11 10 21 13 6 | 31 38 39 57 --- 37 38 31 39 34 35
5 | 8 11 7 8 6 3 11 6 9 8 3 | 39 37 38 40 39 38 40 37 42 42 38
6 | 6 10 7 9 8 3 6 6 7 7 2 | 19 22 21 17 22 20 25 19 23 19 20
7 | 7 9 8 10 8 4 6 6 7 10 2 | 36 41 41 41 37 38 41 39 35 37 38
8E | 10 22 20 42 16 4 14 7 18 12 6 | 74 81 72 80 74 72 110 67 67 71 71
9E | 7 11 16 8 14 3 7 7 11 11 3 | 22 27 23 23 25 22 27 21 30 26 23
10 | 6 10 7 9 6 2 10 7 7 9 2 | 17 21 20 23 19 19 24 19 20 22 19
11 | 6 14 13 11 12 4 9 7 11 10 3 | 20 24 18 27 22 21 24 22 24 22 20
12 | 9 18 6 9 8 4 11 9 10 17 3 | 30 32 27 27 28 27 31 29 29 31 28
13E | 7 11 6 11 9 4 10 8 7 13 3 | 35 39 38 42 38 38 40 38 37 38 37
15E | 7 11 7 12 10 6 11 10 9 13 3 | 47 50 50 50 52 50 51 52 54 54 50
16 | 6 20 10 11 9 5 9 10 8 12 3 | 19 19 20 21 19 20 22 24 23 24 20
17E | 6 15 7 9 11 3 11 8 9 11 3 | 17 23 15 18 21 17 21 19 20 18 17
18 | 9 11 11 9 6 5 8 5 11 12 3 | 8 17 16 15 15 10 20 14 14 17 13
19E | 6 14 8 8 8 3 8 7 9 7 3 | 18 18 21 17 21 19 21 23 25 22 19
20 | 5 10 4 7 6 3 11 5 7 8 2 | 16 20 18 22 17 19 23 16 19 17 17
21 | 6 16 7 11 7 5 10 6 9 10 3 | 15 24 18 23 19 18 24 17 20 19 18
22 | 4 10 5 9 11 4 9 5 8 9 2 | 26 33 29 28 29 29 34 29 27 32 28
X23 | 7 --- --- --- 12 14 --- --- --- --- 9 | 47 --- --- --- 46 45 --- --- --- --- 46
24 | 5 10 8 11 6 4 8 8 9 8 2 | 20 24 23 18 21 20 27 20 22 20 20
25 | 10 10 8 5 5 4 8 6 8 12 3 | 15 21 19 21 17 17 23 18 17 20 17
26 | 8 9 6 10 6 5 6 9 8 10 3 | 25 28 25 27 23 23 29 24 27 22 24
X27E | 12 16 18 15 20 7 --- 8 13 9 5 | 27 31 31 31 32 27 --- 26 34 28 28
28 | 7 12 5 9 7 4 7 7 12 11 3 | 16 22 15 18 17 17 23 19 17 16 17
29E | 6 16 10 8 12 3 10 8 10 15 3 | 36 38 37 38 35 37 38 40 34 38 36
30 | 6 9 7 9 6 4 7 7 7 9 2 | 20 27 22 22 21 21 27 22 21 19 21
31 | 6 10 8 10 8 5 8 6 7 10 2 | 39 41 39 40 37 39 42 37 32 34 37
32E | 9 10 14 12 6 3 9 8 11 11 3 | 26 28 28 30 25 26 29 29 31 29 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 9 12 9 4 9 7 9 11 |T 26 29 27 29 27 27 31 27 28 27 27
WRMS | 7 13 9 11 8 4 9 7 8 9 |NE 22 25 23 24 24 23 27 23 23 23 23
MEDI | 7 11 8 9 8 4 9 7 9 10 |MD 21 24 23 23 22 22 27 22 24 22 21
Table 3.2122.5 GPS week: 2122 Day: 5 MJD: 59103.000
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 12 10 2 5 5 8 11 3 | 23 27 28 33 27 26 29 25 25 23 26
2 | 7 11 6 8 9 5 8 7 12 9 3 | 14 20 16 17 20 16 19 19 22 19 17
3 | 8 7 10 8 11 3 6 5 7 6 2 | 18 23 20 20 20 18 25 18 18 19 19
X4E | 19 28 16 40 --- 5 12 10 23 11 7 | 46 47 51 71 --- 49 50 47 51 49 49
5 | 9 11 6 8 6 4 8 5 8 8 2 | 53 55 53 54 54 54 57 53 55 53 54
6 | 7 9 8 7 7 3 6 4 7 5 2 | 23 27 24 23 26 24 29 23 23 23 24
7 | 7 12 7 10 7 3 7 5 9 8 2 | 31 32 31 34 29 30 32 31 31 29 30
X8E | 10 14 19 66 16 7 --- 7 15 9 5 | 131 129 137 141 132 130 --- 135 123 133 131
9E | 6 10 17 9 11 3 8 5 12 7 3 | 30 33 31 34 31 31 32 30 32 32 30
10 | 4 9 8 7 9 3 7 6 5 7 2 | 16 20 19 21 20 17 21 16 17 18 17
11 | 10 11 13 12 15 3 8 6 12 9 3 | 18 21 16 27 22 19 23 22 19 24 19
12 | 9 17 5 7 8 3 8 5 9 12 3 | 24 26 23 25 28 25 29 25 26 25 25
13E | 8 11 8 8 6 4 7 5 9 8 2 | 37 38 38 38 37 38 40 37 39 39 37
15E | 14 18 9 16 11 7 9 8 9 13 4 | 84 85 87 90 86 87 84 84 87 84 85
16 | 6 17 7 9 8 4 6 7 8 10 3 | 21 26 22 23 18 21 24 24 21 24 21
17E | 6 17 7 7 12 4 10 6 8 7 3 | 16 22 13 14 22 14 18 16 18 15 15
18 | 8 12 13 7 8 6 7 5 10 11 3 | 9 21 16 14 17 11 18 17 15 20 14
19E | 9 15 9 7 7 4 7 5 10 7 3 | 31 33 36 32 33 32 34 32 34 33 32
20 | 7 9 5 6 8 3 7 6 7 7 2 | 17 24 21 22 22 20 24 20 21 24 20
21 | 6 16 8 7 7 4 7 7 12 12 3 | 18 27 20 23 21 20 24 21 19 22 20
22 | 8 10 7 8 12 4 7 6 8 6 2 | 31 34 32 34 34 32 33 32 30 29 31
X23 | 12 --- --- --- 15 16 --- --- --- --- 14 | 43 --- --- --- 51 40 --- --- --- --- 46
24 | 6 8 9 8 5 4 7 4 7 14 2 | 19 24 22 23 24 21 27 21 20 27 21
25 | 9 9 7 7 6 4 6 3 9 6 2 | 17 23 21 23 21 21 24 21 21 20 20
26 | 7 9 6 7 5 4 6 6 8 7 2 | 24 28 26 27 24 25 28 27 24 28 25
X27E | 14 25 24 21 26 10 --- 18 19 26 8 | 34 42 36 40 43 34 --- 39 37 39 34
28 | 8 11 6 10 7 4 6 4 9 8 2 | 18 23 19 23 19 19 24 18 19 18 19
29E | 7 19 10 9 8 3 7 5 9 8 3 | 34 37 36 40 35 36 37 34 37 38 35
30 | 7 8 6 11 5 3 6 6 7 7 2 | 20 23 22 21 22 20 27 21 20 21 21
31 | 6 9 7 9 7 4 6 5 10 8 2 | 31 34 31 34 33 32 35 32 34 33 32
32E | 11 9 16 9 8 7 8 9 9 9 3 | 37 37 39 40 39 38 38 39 38 37 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 9 9 9 4 7 6 9 9 |T 31 34 32 35 33 32 31 32 32 33 32
WRMS | 7 12 9 8 8 4 7 5 8 8 |NE 23 26 24 26 26 24 27 24 24 24 24
MEDI | 8 11 8 8 8 4 7 5 9 8 |MD 24 27 24 27 26 25 28 25 24 25 25
Table 3.2122.6 GPS week: 2122 Day: 6 MJD: 59104.000
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 8 8 10 9 3 6 6 8 10 2 | 26 27 27 30 27 26 30 24 26 23 26
2 | 8 13 6 9 9 3 8 9 8 9 3 | 15 19 18 18 19 16 18 21 17 20 17
3 | 7 7 9 7 10 5 6 7 7 9 2 | 19 20 23 22 23 20 24 21 18 19 20
X4E | 15 26 17 50 --- 11 10 12 22 12 6 | 63 65 69 86 --- 67 69 68 68 62 65
5 | 8 13 7 8 4 4 7 8 7 9 2 | 61 59 62 63 63 62 64 64 65 63 63
6 | 5 10 6 6 7 2 5 5 6 6 2 | 29 29 30 30 31 28 32 29 27 27 29
7 | 6 11 7 10 8 4 6 5 10 8 2 | 51 51 53 55 47 50 50 50 48 51 50
8E | 10 13 20 63 10 5 10 4 10 6 4 | 138 136 143 148 138 137 118 140 135 137 138
9E | 9 10 16 40 15 5 8 6 13 12 5 | 40 41 38 52 42 40 43 40 40 39 40
10 | 7 8 7 7 5 3 7 6 5 8 2 | 20 22 21 21 21 20 22 19 20 20 20
11 | 8 9 15 12 13 5 8 7 10 10 3 | 20 23 19 25 22 20 25 25 27 27 22
12 | 6 15 6 9 8 5 8 7 9 14 3 | 34 38 35 34 35 34 37 35 35 36 35
13E | 7 11 8 8 6 5 9 6 10 7 2 | 38 41 42 41 41 39 40 41 40 41 40
15E | 6 14 6 22 13 4 12 7 11 10 4 | 120 120 121 124 120 120 120 124 120 124 121
16 | 7 19 6 7 9 5 9 9 11 10 3 | 20 22 24 24 19 22 25 26 26 26 23
17E | 6 11 8 9 14 3 8 5 8 8 3 | 23 25 18 23 29 21 23 21 25 20 22
18 | 9 10 13 7 6 5 9 4 7 11 3 | 11 17 17 12 17 9 17 16 11 18 13
19E | 7 11 8 8 7 3 7 5 8 8 2 | 39 43 44 41 39 42 43 40 38 41 40
20 | 5 9 4 7 4 3 7 6 7 7 2 | 21 28 22 23 22 25 27 22 23 23 23
21 | 8 15 6 9 7 4 10 6 10 10 3 | 19 27 20 21 22 19 25 20 22 24 21
22 | 7 8 7 8 11 4 6 8 8 7 2 | 38 41 39 39 40 38 41 40 36 38 39
X23 | 6 --- --- --- 11 9 --- --- --- --- 9 | 59 --- --- --- 55 58 --- --- --- --- 56
24 | 5 8 8 8 6 3 7 6 5 8 2 | 27 27 29 30 28 28 31 30 25 29 28
25 | 9 9 8 8 5 4 7 4 7 7 2 | 18 23 22 23 20 20 25 21 21 21 20
26 | 6 9 6 8 7 5 6 6 8 5 2 | 25 29 27 27 26 26 30 25 26 24 25
X27E | 13 17 15 15 8 4 --- 7 15 12 4 | 42 41 45 45 47 43 --- 44 35 49 42
28 | 6 10 7 8 7 2 5 3 9 9 2 | 19 23 19 23 21 20 25 21 21 19 20
29E | 8 17 9 13 7 3 7 6 10 11 3 | 53 49 51 56 52 53 52 51 51 49 51
30 | 4 8 9 9 7 3 6 8 8 7 2 | 24 27 26 26 25 25 29 26 24 23 25
31 | 7 8 8 10 5 4 7 6 11 8 2 | 51 54 55 52 51 51 53 51 49 49 51
32E | 10 9 15 8 7 5 8 7 9 8 3 | 49 51 48 51 49 49 48 50 52 48 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 11 9 17 9 4 8 6 9 9 |T 39 40 40 42 39 39 40 40 39 39 39
WRMS | 7 11 9 12 8 4 8 6 8 8 |NE 28 30 29 29 30 29 31 29 28 29 29
MEDI | 7 10 8 8 7 4 7 6 8 8 |MD 29 29 29 30 29 28 31 29 27 27 29
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 4.2122 GPS week: 2122 MJD: 59098.0-59104.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 |U 10 9 33 |U 9 9 39 |U 9 8 26 |
emr | emr 2880 |U 13 12 41 |U 12 14 56 | 16 18 32 |
esa | esa 2880 | 10 8 38 |U 8 14 48 | 11 11 33 |
gfz | gfz 2879 |U 12 9 32 |U 7 10 39 |U 9 10 33 |
grg | grg 2878 |U 16 19 45 |U 9 12 46 | 10 9 29 |
igr | igr 2878 | 10 10 34 | 8 10 43 | 9 10 31 |
igs | igs 2879 | 10 10 33 | 8 10 43 | 9 10 29 |
jpl | jpl 2825 |U 14 16 43 |U 10 12 54 | 12 12 33 |
mit | mit 2880 |U 11 11 34 |U 10 10 44 |U 10 10 31 |
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 5.2122.0 GPS week: 2122 Day: 0 MJD: 59098.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 9 8 31 | 8 7 37 | 10 10 31 |
emr | emr 2880 | 15 10 35 | 10 10 52 | 13 17 40 |
esa | esa 2880 | 9 6 38 | 7 10 48 | 10 9 36 |
gfz | gfz 2878 | 11 7 29 | 7 6 38 | 10 12 33 |
grg | grg 2878 | 14 10 39 | 9 9 51 | 10 12 34 |
igr | igr 2880 | 9 8 33 | 7 8 43 | 9 11 36 |
igs | igs 2880 | 9 9 32 | 7 7 43 | 9 10 34 |
jpl | jpl 2880 | 14 15 41 | 8 9 52 | 10 10 39 |
mit | mit 2880 | 10 10 33 | 8 8 45 | 11 11 35 |
Table 5.2122.1 GPS week: 2122 Day: 1 MJD: 59099.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 10 15 32 | 8 9 43 | 11 8 29 |
emr | emr 2880 | 15 17 53 | 11 14 49 | 12 18 38 |
esa | esa 2880 | 10 13 42 | 8 15 52 | 12 10 37 |
gfz | gfz 2879 | 12 12 30 | 7 10 45 | 12 10 36 |
grg | grg 2878 | 25 31 43 | 8 14 47 | 12 10 30 |
igr | igr 2880 | 11 15 34 | 8 10 50 | 11 10 35 |
igs | igs 2880 | 10 16 33 | 8 11 49 | 11 10 34 |
jpl | jpl 2880 | 15 18 41 | 9 11 61 | 14 11 38 |
mit | mit 2880 | 11 18 36 | 10 11 52 | 13 10 36 |
Table 5.2122.2 GPS week: 2122 Day: 2 MJD: 59100.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 9 7 33 | 8 10 34 | 9 8 23 |
emr | emr 2880 | 13 10 41 | 11 15 43 | 13 19 27 |
esa | esa 2880 | 8 6 40 | 9 16 40 | 11 10 28 |
gfz | gfz 2878 | 12 9 31 | 7 12 34 | 8 11 30 |
grg | grg 2879 | 12 13 35 | 8 12 37 | 9 9 27 |
igr | igr 2880 | 10 8 34 | 7 12 39 | 8 10 28 |
igs | igs 2880 | 10 8 34 | 8 13 38 | 8 10 26 |
jpl | jpl 2880 | 13 13 44 | 9 14 49 | 14 10 34 |
mit | mit 2880 | 11 10 36 | 10 13 37 | 9 10 26 |
Table 5.2122.3 GPS week: 2122 Day: 3 MJD: 59101.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 13 7 36 | 9 10 44 | 7 8 27 |
emr | emr 2880 | 14 9 38 | 15 15 88 | 43 20 33 |
esa | esa 2880 | 10 9 38 | 9 15 52 | 11 12 36 |
gfz | gfz 2880 | 13 8 35 | 9 12 40 | 9 11 37 |
grg | grg 2878 | 19 25 67 | 11 13 55 | 10 8 28 |
igr | igr 2880 | 11 7 36 | 8 12 47 | 10 11 34 |
igs | igs 2880 | 12 8 36 | 9 12 48 | 8 10 30 |
jpl | jpl 2880 | 14 12 43 | 11 14 61 | 13 13 35 |
mit | mit 2880 | 12 9 37 | 11 11 47 | 10 11 31 |
Table 5.2122.4 GPS week: 2122 Day: 4 MJD: 59102.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 9 10 32 | 8 6 38 | 9 8 24 |
emr | emr 2880 | 12 14 41 | 13 13 53 | 13 17 27 |
esa | esa 2880 | 10 7 35 | 8 13 45 | 9 12 32 |
gfz | gfz 2880 | 9 10 31 | 7 8 37 | 10 11 34 |
grg | grg 2880 | 11 15 33 | 8 10 40 | 12 9 28 |
igr | igr 2880 | 9 11 32 | 7 8 40 | 8 12 29 |
igs | igs 2877 | 8 10 33 | 8 8 40 | 9 12 28 |
jpl | jpl 2784 | 14 17 47 | 10 10 47 | 10 14 25 |
mit | mit 2880 | 8 12 32 | 9 9 44 | 11 11 29 |
Table 5.2122.5 GPS week: 2122 Day: 5 MJD: 59103.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 9 5 31 | 8 9 39 | 10 7 26 |
emr | emr 2880 | 11 12 40 | 12 14 47 | 12 14 29 |
esa | esa 2880 | 12 5 35 | 8 14 50 | 14 11 34 |
gfz | gfz 2880 | 14 8 30 | 7 11 39 | 9 8 30 |
grg | grg 2879 | 22 28 57 | 8 12 41 | 11 8 30 |
igr | igr 2880 | 12 7 31 | 8 9 43 | 10 10 28 |
igs | igs 2880 | 12 6 30 | 9 10 43 | 10 9 28 |
jpl | jpl 2688 | 18 15 37 | 11 11 55 | 15 12 33 |
mit | mit 2880 | 14 9 30 | 10 9 44 | 10 9 30 |
Table 5.2122.6 GPS week: 2122 Day: 6 MJD: 59104.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 11 9 37 | 10 10 39 | 8 6 23 |
emr | emr 2880 | 12 14 43 | 12 16 61 | 9 18 28 |
esa | esa 2880 | 9 8 40 | 9 14 47 | 11 10 29 |
gfz | gfz 2880 | 13 12 38 | 8 9 43 | 8 7 29 |
grg | grg 2879 | 12 13 41 | 11 18 48 | 9 8 28 |
igr | igr 2872 | 11 10 38 | 8 9 41 | 7 9 25 |
igs | igs 2879 | 11 10 37 | 9 11 43 | 7 9 26 |
jpl | jpl 2784 | 14 19 47 | 11 13 53 | 11 12 26 |
mit | mit 2880 | 12 11 38 | 9 9 43 | 9 8 28 |
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 6.2122 GPS week: 2122 MJD: 59098.500-59104.500
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 -3 22 -13 3 | 13 22
| 21 18 78 91 4 | 1
emr uuuux | -39 3 60 2 -21 | -6 25
| 35 22 43 57 22 | 8
esa uuuuu | 10 -5 -26 67 -2 | 22 28
| 8 10 13 80 3 | 2
gfz uuuuu | 0 -1 101 11 -1 | 28 33
| 10 15 125 105 4 | 2
grg uuuuu | 4 -4 24 -30 2 | 1 14
| 11 11 35 57 3 | 1
igr xxxxx | 12 -2 21 15 3 | -1 18
| 6 9 48 33 5 | 3
irf xxxxx | -5 11 -36 12 -2 | 0 17
| 10 13 13 10 3 | 1
jpl uuuuu | -2 1 42 12 -3 | 71 73
| 17 14 93 28 11 | 2
mit uuuuu | -1 18 -131 -16 -2 | 27 32
| 13 19 16 45 5 | 1
ngs uuuuu | -4 -19 36 -26 -5 | 14 23
| 28 32 100 108 2 | 2
sio xxxxx | -53 -73 -245 -38 7 | 41 47
| 75 38 116 61 11 | 5
Table 7.2122.0 GPS week: 2122 Day: 0 MJD: 59098.500
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 | 16 8 25 -36 7 | 11 20
emr uuuux | -54 13 88 13 -1 | 1 19
esa uuuuu | 17 -12 -2 115 0 | 20 26
gfz uuuuu | 1 11 -10 163 0 | 24 30
grg uuuuu | 24 -5 8 -42 1 | -1 14
igr xxxxx | 13 -16 -2 -19 4 | -6 19
irf xxxxx | -3 -5 -26 16 -4 | -1 18
jpl uuuuu | -1 10 -27 25 0 | 69 71
mit uuuuu | -7 0 -125 -40 -9 | 27 32
ngs uuuuu | -18 -32 167 -137 -6 | 15 23
sio xxxxx | -73 -56 -319 -101 -2 | 34 42
Table 7.2122.1 GPS week: 2122 Day: 1 MJD: 59099.500
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 | 41 -8 66 46 2 | 12 21
emr uuuux | -40 -15 129 -7 7 | -1 19
esa uuuuu | 15 -10 -35 177 3 | 21 27
gfz uuuuu | 8 -15 47 50 6 | 25 31
grg uuuuu | 1 2 5 -51 -1 | -1 14
igr xxxxx | 9 -10 32 13 9 | -5 18
irf xxxxx | -2 10 -40 18 0 | -1 17
jpl uuuuu | 5 11 20 23 -2 | 71 72
mit uuuuu | -10 30 -137 -73 -2 | 26 31
ngs uuuuu | -39 -33 46 -116 -4 | 14 23
sio xxxxx | -66 -82 -481 -16 3 | 36 43
Table 7.2122.2 GPS week: 2122 Day: 2 MJD: 59100.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 12 2 -40 71 1 | 14 22
emr uuuux | -58 38 45 -52 -37 | 1 19
esa uuuuu | 8 -3 -41 70 0 | 23 29
gfz uuuuu | 3 8 197 -17 1 | 28 33
grg uuuuu | 0 -16 31 -66 1 | 1 14
igr xxxxx | 4 6 96 40 8 | -2 18
irf xxxxx | 1 25 -27 -5 -2 | 1 17
jpl uuuuu | 8 -3 119 -24 3 | 72 73
mit uuuuu | 16 40 -156 -39 -1 | 28 33
ngs uuuuu | -25 -76 5 -13 -3 | 16 24
sio xxxxx | 0 -136 -187 -18 27 | 39 45
Table 7.2122.3 GPS week: 2122 Day: 3 MJD: 59101.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 35 -2 100 -89 9 | 14 22
emr uuuux | -91 16 21 -75 -54 | -2 22
esa uuuuu | 19 -2 -36 112 -2 | 25 29
gfz uuuuu | -10 -23 267 66 0 | 30 34
grg uuuuu | 0 -17 25 12 -3 | 2 14
igr xxxxx | 7 6 47 58 7 | 0 18
irf xxxxx | -15 4 -19 3 -2 | 2 17
jpl uuuuu | -34 12 -62 -33 13 | 73 74
mit uuuuu | 15 -1 -118 -34 1 | 29 33
ngs uuuuu | 7 13 -53 112 -3 | 17 24
sio xxxxx | 62 -42 -168 32 13 | 44 50
Table 7.2122.4 GPS week: 2122 Day: 4 MJD: 59102.500
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 -34 -82 4 1 | 14 22
emr uuuux | -35 12 78 3 -36 | -9 29
esa uuuuu | 12 14 -22 65 -4 | 24 29
gfz uuuuu | -3 4 177 -173 -5 | 30 34
grg uuuuu | -1 -7 100 -47 5 | 1 14
igr xxxxx | 13 4 37 40 -2 | 0 18
irf xxxxx | -16 28 -41 9 -5 | 1 17
jpl uuuuu | 12 -28 165 25 -21 | 74 75
mit uuuuu | -12 39 -145 -12 -6 | 28 32
ngs uuuuu | 38 9 -111 94 -5 | 15 23
sio xxxxx | -57 -22 -179 -143 4 | 44 50
Table 7.2122.5 GPS week: 2122 Day: 5 MJD: 59103.500
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 | 20 25 122 -166 -2 | 13 22
emr uuuux | 12 -19 -1 103 -18 | -16 31
esa uuuuu | -7 -18 -23 -19 -7 | 23 28
gfz uuuuu | -14 -7 120 -46 -4 | 29 34
grg uuuuu | 13 2 -4 79 7 | 1 14
igr xxxxx | 14 3 -53 -30 -2 | 0 18
irf xxxxx | -10 0 -40 24 0 | -1 16
jpl uuuuu | -16 4 -47 34 -11 | 71 72
mit uuuuu | -14 -2 -110 26 0 | 26 30
ngs uuuuu | 25 7 52 18 -7 | 13 21
sio xxxxx | -183 -98 -185 -5 -4 | 45 50
Table 7.2122.6 GPS week: 2122 Day: 6 MJD: 59104.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -13 -13 -36 81 3 | 14 22
emr uuuux | -4 -22 59 26 -6 | -18 33
esa uuuuu | 9 -5 -26 -53 -5 | 22 28
gfz uuuuu | 13 17 -89 33 -6 | 29 34
grg uuuuu | -8 13 6 -93 4 | 1 14
igr xxxxx | 23 -8 -13 2 -3 | 1 17
irf xxxxx | 11 17 -58 22 2 | 0 16
jpl uuuuu | 13 1 128 31 -6 | 70 72
mit uuuuu | 4 16 -124 58 5 | 26 30
ngs uuuuu | -18 -20 143 -142 -8 | 12 21
sio xxxxx | -53 -77 -197 -14 11 | 45 50
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