[IGSREPORT-26956] Wk 2080 IGS Final Orbits
acc
acc at igs.org
Sun Dec 8 16:21:30 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2080 (Nov 17, 2019 - Nov 23, 2019)
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:
igs2080[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2080[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2080[0-6].cls IGS GPS clock combination summary report.
igs20807.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20807.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 | 18 7 18 ASPA TIXI TLSE ASCG ASPA TIXI TLSE
0 | EMR | PTBB HARB HOB2 PTBB TLSE
0 | ESA | 18 18 COCO NRMD PTBB SEYG TLSE COCO NRMD PTBB SEYG
0 | ESA | TLSE
0 | GRG | COCO LPGS COCO DARW LPGS VOIM
1 | COD | 18 SEYG TIXI NAUR SEYG TIXI
1 | EMR | 18 18 30 PTBB HARB HOB2 PTBB USUD
1 | ESA | KOUR NNOR PTBB SEYG KOUR NNOR PTBB SEYG
1 | GFZ | 18 13 18 BJNM KOUR BJNM KOUR
1 | GRG | 13 18 13 18 NNOR
1 | JPL | 30
1 | MIT | BJNM
2 | COD | HRAO MAS1 NAUR NOVM TIXI HRAO MAS1 NAUR NOVM SEYG
2 | COD | TIXI
2 | EMR | 18 PTBB NLIB PTBB
2 | ESA | 18 18 MAS1 PTBB WIND MAS1 PTBB WIND
2 | GFZ | BJNM DGAR BJNM DGAR
2 | GRG | 13
2 | JPL | ASCG ASCG
2 | MIT | DGAR
3 | COD | MAS1 TIXI MAS1 TIXI
3 | EMR | 18 BJNM PTBB BJNM PTBB
3 | ESA | ANKR NOVM PTBB ANKR LPGS NOVM PTBB
3 | GFZ | 18 PIE1
3 | GRG | 13 13 LHAZ LPGS ULAB FAA1 LHAZ PIE1 ULAB
3 | MIT | BJNM
4 | COD | ASCG GUAT NOVM TLSE GUAT NOVM
4 | EMR | 18 PTBB TLSE PTBB
4 | ESA | 18 18 FAA1 GOLD KOUR NOVM PTBB TLSE FAA1 GOLD KOUR
4 | ESA | LPGS NOVM PTBB
4 | GFZ | KOUR PIE1 KOUR PIE1
4 | GRG | 13 13 21 FAA1 KIRU FAA1 KIRU
4 | JPL | ASCG
5 | COD | 18 18 ASCG BRAZ SAVO ASCG BRAZ POVE SAVO
5 | EMR | PTBB HARB PTBB
5 | ESA | 18 18 BAKE POVE PTBB BAKE LPGS PTBB
5 | GFZ | BJNM MAL2 UFPR BJNM GODE MAL2 UFPR
5 | GRG | 13 13 18 SCOR
5 | JPL | IQAL IQAL
5 | MIT | BJNM
6 | COD | 18 18 ASCG ASCG
6 | EMR | BJNM NLIB VILL
6 | ESA | 18 18 PTBB TLSE
6 | GFZ | 13 KOKV
6 | GRG | 13 18 13 18
6 | JPL | MCM4 MCM4
6 | MIT | BJNM BJNM
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
----+--------+---------------
4 | SIO | 4
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 -.1 .5 3 10 10 -.46
EMR | 0 | -3.8 4.0 13.6 -28 64 -148 -.36
ESA | 0 | 1.2 -.9 1.1 26 18 69 -.38
GFZ | 0 | -.3 .6 .1 23 23 44 -.15
GRG | 0 | 5.4 1.0 16.9 58 15 97 .06
JPL | 0 | 7.0 8.2 13.7 1 0 1 -.48
MIT | 0 | 4.8 6.1 8.0 12 42 -26 -.11
NGS | 0 | -3.8 .8 10.8 22 57 -48 -.13
SIO | 0 | -1.0 5.2 3.2 9 3 -4 -.04
COD | 1 | .7 -.1 1.1 7 14 -1 -.57
EMR | 1 | 3.5 -7.9 15.4 -51 25 -55 -.10
ESA | 1 | .9 -.5 1.3 6 29 54 -.47
GFZ | 1 | -.1 .6 .2 27 17 34 -.09
GRG | 1 | 8.9 -.8 17.5 76 14 130 .13
JPL | 1 | 13.8 5.0 14.8 12 9 4 -.63
MIT | 1 | 9.5 5.0 9.3 2 46 -30 -.16
NGS | 1 | 10.5 3.9 14.0 20 -18 -6 -.26
SIO | 1 | 8.6 3.2 5.3 -1 -11 2 -.07
COD | 2 | .6 .2 .5 5 5 6 -.37
EMR | 2 | 3.3 4.5 10.8 -54 48 -69 -.15
ESA | 2 | 1.9 -.8 1.3 5 8 71 -.09
GFZ | 2 | .1 .5 -.1 28 23 33 .03
GRG | 2 | 8.8 .0 6.1 95 9 131 .26
JPL | 2 | 11.9 9.6 10.4 1 0 1 -.53
MIT | 2 | 11.1 5.7 9.2 5 37 -32 -.05
NGS | 2 | 1.8 2.4 10.2 27 7 -21 -.21
SIO | 2 | 8.0 -.5 .8 14 -8 14 -.02
COD | 3 | .3 .4 .3 3 3 -19 -.47
EMR | 3 | 2.6 7.1 19.3 -30 67 -141 -.19
ESA | 3 | 1.1 -.9 2.3 -26 50 50 -.17
GFZ | 3 | -.3 .4 .5 23 36 7 -.08
GRG | 3 | 8.1 -2.1 16.4 107 20 100 .17
JPL | 3 | 10.5 .9 13.3 -2 23 0 -.35
MIT | 3 | 8.2 7.6 9.1 2 38 -31 .06
NGS | 3 | 4.0 6.3 11.3 36 2 -4 -.14
SIO | 3 | 6.2 3.0 .2 28 -3 -4 .07
COD | 4 | .9 .1 1.2 10 14 -9 -.48
EMR | 4 | 7.2 3.9 13.9 -26 82 -133 -.23
ESA | 4 | 1.5 -.2 1.7 -7 49 33 -.15
GFZ | 4 | .2 .7 .2 32 18 20 -.29
GRG | 4 | 3.1 -2.7 6.2 128 -2 113 .23
JPL | 4 | 13.6 5.9 10.4 9 -5 5 -.55
MIT | 4 | 5.0 6.3 3.6 25 58 -59 -.09
NGS | 4 | 5.2 3.3 8.4 24 -1 -14 -.23
SIO | 4 | 3.4 2.1 7.6 22 -23 -20 .09
COD | 5 | .5 .5 .3 17 11 -16 -.36
EMR | 5 | 9.7 9.1 9.1 -8 68 -117 -.38
ESA | 5 | .1 -1.2 1.3 9 36 39 -.16
GFZ | 5 | -.4 .9 -.5 32 25 28 -.22
GRG | 5 | 7.6 .1 -.2 132 -10 128 .10
JPL | 5 | 7.3 5.9 9.2 10 8 5 -.33
MIT | 5 | 7.3 9.5 4.5 42 47 -41 -.08
NGS | 5 | .8 10.5 3.4 68 0 6 -.31
SIO | 5 | 4.3 5.9 -4.5 26 -2 -4 -.14
COD | 6 | 1.1 -.2 1.1 6 4 13 -.54
EMR | 6 | 7.4 11.9 13.7 -21 58 -94 -.40
ESA | 6 | .6 -.1 .7 12 26 45 -.35
GFZ | 6 | .3 .6 -.1 30 1 33 -.19
GRG | 6 | 3.3 4.4 6.7 126 -30 151 .02
JPL | 6 | 8.5 6.5 11.2 10 8 5 -.54
MIT | 6 | 5.3 10.4 6.3 25 46 -39 -.26
NGS | 6 | 1.2 8.5 .7 52 14 -7 -.51
SIO | 6 | 2.9 3.7 -8.8 26 -24 -5 -.18
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 1.2080.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2080.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 2.2080.[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 3.2080.[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 5.2080.0-6). 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 2080 summary. (Nov 17, 2019 - Nov 23, 2019)
Table 1.2080.a GPS week: 2080 MJD: 58804.000-58810.000
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 250| -1 0 0 13 3 0 -.02 9 9 | -314 -165 6 100
| 1 1 1 14 5 19 .02 | 240 247
emr 80| 0 -2 4 -32 -5 -3 .17 13 13 | 141658 -177 16 113
| 2 4 1 7 18 11 .02 | 446 407
esa 150| 0 0 1 -18 4 10 -.10 9 9 | -145 -1548 7 79
| 0 0 1 12 11 6 .01 | 452 936
gfz 180| 0 -1 1 6 -6 -27 .06 9 10 | -301 -35 11 117
| 0 0 1 16 14 14 .04 | 280 521
grg 92| 1 0 -3 0 -10 91 -.16 12 11 | 184 -176 9 133
| 1 0 3 14 6 29 .01 | 212 466
igr n/a| 0 0 0 -21 -8 -22 .02 4 4 | 5373 -299 10 67
| 0 0 1 8 11 13 .02 | 581 369
jpl 80| 0 0 2 4 9 -11 .19 8 8 | 213121 -206 8 88
| 0 1 1 20 11 13 .03 | 451 403
mit 349| 0 0 -5 -6 -5 -10 -.09 14 12 | 898 38 80 1683
| 1 0 1 25 25 10 .02 | 669 278
ngs 205| 1 0 0 8 -4 -30 -.06 8 7 | -370 -70 1096 2383
| 0 1 3 17 15 20 .01 | 187 381
sio 311| 0 -1 -4 -7 -9 -2 -.00 16 16 | --- --- --- ---
| 0 0 1 23 40 31 .03 | --- ---
Table 1.2080.b GPS week : 2080 MJD: 58804.000-58810.000
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 | 4 4 4 4 4 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 3 3 3 3 3 3 3 |
4 | 11 10 11 10 11 10 10 |
5 | 4 4 4 4 4 4 4 |
6 | 4 4 4 4 4 4 4 |
7 | 6 4 4 4 4 4 4 |
8 | 4 4 3 4 4 4 4 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 3 4 4 5 4 4 4 |
12 | 4 4 4 5 4 4 4 |
13 | 4 4 5 4 4 4 4 |
14 | 3 4 4 4 0 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 4 4 4 4 4 4 4 |
17 | 4 4 4 4 4 4 4 |
18 | 6 5 6 6 5 8 6 |
19 | 4 4 4 4 4 5 5 |
20 | 3 4 4 4 4 4 4 |
21 | 4 4 5 5 5 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 4 4 4 |
24 | 4 5 4 4 4 4 4 |
25 | 3 4 4 4 4 4 4 |
26 | 3 3 4 4 4 4 3 |
27 | 3 4 4 4 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 4 5 5 5 |
30 | 7 7 6 5 5 5 4 |
31 | 5 5 4 4 3 4 4 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2080.0 GPS week: 2080 Day: 0 MJD: 58804.000
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 -1 14 3 23 -.04 9 9 | -222 -85 6 102
emr 80| -2 -3 3 -29 -21 -5 .18 12 12 | 142327 -478 18 120
esa 150| 0 0 3 -15 -6 13 -.08 9 9 | -158 -1671 7 75
gfz 178| 1 0 0 24 1 -17 .10 9 10 | -286 73 11 99
grg 96| 0 0 0 -21 -10 63 -.15 12 10 | 137 -247 9 126
igr n/a| 0 0 -1 -19 -27 -24 .05 4 4 | 6331 -489 10 64
jpl 80| -1 2 1 -16 20 -26 .20 8 8 | 213818 -626 9 101
mit 350| 3 0 -5 20 6 -7 -.10 14 11 | -93 -52 98 1682
ngs 207| 0 0 0 0 -6 -26 -.07 8 6 | -190 -243 835 1842
sio 314| 0 -1 -3 26 11 1 -.02 15 15 | --- --- --- ---
Table 2.2080.1 GPS week: 2080 Day: 1 MJD: 58805.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| 0 2 1 35 7 -18 -.02 10 10 | -170 253 8 115
emr 80| -4 -11 5 -32 -34 -10 .14 16 15 | 141744 -132 20 127
esa 150| 0 1 0 0 11 12 -.10 9 9 | 240 -2193 8 90
gfz 181| 0 0 2 20 0 -12 .03 9 9 | -452 236 11 149
grg 93| 2 0 0 -8 2 87 -.16 11 10 | -163 635 10 131
igr n/a| 0 1 -1 -11 7 -39 .00 4 3 | 5703 -233 10 80
jpl 80| -1 -1 1 -18 0 -12 .22 8 8 | 213019 -99 10 109
mit 349| 1 2 -7 -19 -9 -16 -.10 14 12 | 354 395 76 1649
ngs 202| 1 1 0 24 12 -26 -.06 10 7 | -238 385 1278 2696
sio 319| 0 0 -5 -35 -10 10 .01 16 17 | --- --- --- ---
Table 2.2080.2 GPS week: 2080 Day: 2 MJD: 58806.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| -2 0 -1 27 3 28 -.01 9 9 | 97 -252 6 96
emr 80| -1 0 3 -25 -5 -13 .17 13 12 | 141179 153 15 117
esa 150| 0 0 3 -10 4 18 -.10 9 8 | -471 -2244 7 80
gfz 182| 0 -2 2 -6 -5 -32 .01 9 8 | -320 -916 10 96
grg 93| 2 -1 -7 -12 -7 124 -.17 15 13 | 282 -740 11 123
igr n/a| 0 0 -1 -26 2 -25 .02 4 4 | 5013 144 9 57
jpl 80| 0 3 0 24 21 -26 .14 8 8 | 212466 219 9 84
mit 350| 2 0 -5 -15 -2 -7 -.08 15 13 | 432 -142 62 1612
ngs 200| 1 0 3 -11 -28 -52 -.07 9 8 | -240 396 1225 2997
sio 318| 0 -2 -7 -23 -7 15 .01 17 17 | --- --- --- ---
Table 2.2080.3 GPS week: 2080 Day: 3 MJD: 58807.000
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| -1 0 0 5 -5 -7 -.02 9 9 | -334 -502 7 93
emr 80| -1 0 4 -30 -4 5 .18 13 13 | 141911 -768 17 94
esa 150| 0 0 1 -35 14 1 -.10 9 8 | -98 -1419 7 77
gfz 183| 0 -2 1 21 7 -49 .00 10 10 | -43 -491 12 108
grg 91| 2 -1 -4 0 -18 109 -.15 15 13 | 437 -591 11 127
igr n/a| 0 0 0 -8 -11 -36 .03 4 4 | 5807 -906 11 68
jpl 80| 0 1 2 0 0 -9 .20 8 8 | 213372 -708 8 61
mit 349| 0 1 -5 -19 -20 8 -.07 14 12 | 1394 -451 68 1637
ngs 207| 1 1 0 30 6 -16 -.06 8 7 | -273 -580 978 2182
sio 316| 0 -2 -5 -16 -38 23 .04 16 15 | --- --- --- ---
Table 2.2080.4 GPS week: 2080 Day: 4 MJD: 58808.000
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| -2 0 0 2 6 -21 -.03 8 8 | -440 -346 6 84
emr 80| 1 -1 4 -49 4 -6 .17 13 13 | 140996 434 17 108
esa 150| 0 0 2 -23 14 2 -.08 11 11 | 477 -2467 9 89
gfz 181| 0 -1 0 -18 3 -36 .11 9 10 | -836 695 10 125
grg 92| 0 -1 -4 7 -14 117 -.17 12 11 | -23 -11 10 154
igr n/a| 0 0 -1 -30 -14 -5 .03 4 4 | 4793 76 10 75
jpl 80| 0 0 2 35 0 -14 .18 9 9 | 212680 322 9 71
mit 350| 0 0 -7 -19 29 -9 -.07 13 13 | 1206 136 74 1649
ngs 207| 1 1 0 21 -20 4 -.07 8 7 | -449 -336 1011 2057
sio 291| 0 -1 -4 -22 -30 -14 -.03 17 16 | --- --- --- ---
Table 2.2080.5 GPS week: 2080 Day: 5 MJD: 58809.000
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| -2 0 1 -3 9 -8 .01 10 10 | -614 4 7 103
emr 80| 0 0 5 -32 22 -13 .18 12 12 | 141745 -412 15 112
esa 150| 0 0 1 -31 8 7 -.09 9 9 | -907 267 7 75
gfz 180| 0 -1 1 4 -28 -34 .09 11 11 | -120 29 12 129
grg 91| 1 0 -9 20 -16 93 -.16 11 9 | 298 107 10 141
igr n/a| 0 0 1 -27 -12 -5 .01 4 4 | 5130 -533 11 63
jpl 80| -1 0 3 -2 24 13 .18 8 9 | 213320 -463 9 85
mit 349| 0 0 -4 38 -50 -26 -.09 15 13 | 1758 162 113 1795
ngs 206| 1 0 0 7 11 -43 -.05 8 7 | -702 153 1054 2639
sio 312| 1 -1 -4 1 -58 13 .00 18 16 | --- --- --- ---
Table 2.2080.6 GPS week: 2080 Day: 6 MJD: 58810.000
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 248| -1 0 0 12 0 7 -.04 10 10 | -517 -230 7 109
emr 80| 1 0 6 -28 3 17 .21 13 13 | 141706 -39 16 117
esa 150| 0 0 0 -12 -17 18 -.11 9 9 | -103 -1111 6 70
gfz 179| 0 -2 4 1 -24 -10 .07 9 9 | -51 126 13 119
grg 93| 0 0 0 11 -11 44 -.14 9 8 | 320 -390 8 129
igr n/a| 0 0 0 -28 -2 -16 .02 4 4 | 4834 -158 10 62
jpl 80| 0 1 2 8 3 -3 .19 8 8 | 213173 -91 8 108
mit 349| -1 0 -3 -29 11 -12 -.11 15 13 | 1236 222 73 1757
ngs 206| 1 0 -6 -13 -9 -50 -.04 9 8 | -504 -268 1296 2270
sio 311| 0 -2 -3 18 67 -69 -.04 16 15 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.2080.0 GPS week: 2080 Day: 0 MJD: 58804.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 12 16 7 10 4 10 8 7 11 3 | 63 61 61 62 60 60 62 64 58 67 62
2 | 10 9 5 9 13 2 9 15 8 16 3 | 27 25 24 27 23 23 25 24 25 23 24
3 | 10 9 6 7 7 3 7 8 9 9 2 | 28 35 26 32 23 28 34 25 28 34 28
X4 | 14 --- 10 --- --- 11 --- 22 --- --- 10 | 71 --- 65 --- --- 71 --- 71 --- --- 68
5 | 14 8 7 8 10 4 6 17 6 20 3 | 38 33 34 33 30 32 37 30 34 33 32
6 | 7 10 14 8 11 3 9 9 8 10 3 | 22 27 23 23 21 21 22 20 20 27 21
7E | 6 15 12 9 37 5 6 18 14 17 5 | 56 57 58 57 60 56 57 61 53 61 55
8 | 8 13 13 7 10 4 9 11 6 14 3 | 29 36 30 27 27 28 27 22 28 31 26
9 | 6 8 7 8 6 3 6 9 6 9 2 | 25 30 25 24 23 25 29 24 25 23 24
10 | 7 8 5 7 7 5 8 11 6 7 2 | 26 34 25 26 27 26 35 27 26 30 27
11E | 9 11 8 8 10 4 10 6 9 8 3 | 94 97 95 92 98 96 97 96 95 96 95
12 | 10 17 7 7 9 4 7 19 7 19 4 | 40 44 39 39 38 41 42 38 41 40 39
13 | 7 12 9 7 10 3 8 18 7 16 3 | 35 46 32 37 35 37 42 40 37 45 37
14 | 5 6 7 9 6 4 5 19 7 19 3 | 18 21 18 21 21 20 22 24 21 25 19
15 | 15 10 8 10 8 3 8 21 6 22 4 | 51 58 50 50 46 48 52 42 47 40 48
16 | 9 19 6 9 8 4 8 15 9 19 4 | 19 21 17 18 22 18 20 25 23 22 18
17 | 7 11 6 10 11 3 9 15 7 13 3 | 24 25 21 30 22 24 25 24 25 27 23
X18 | 19 15 12 15 14 6 9 16 14 --- 5 | 34 33 31 34 29 30 34 33 30 --- 30
19 | 6 16 7 9 13 3 8 16 6 16 3 | 23 21 20 22 22 20 21 20 21 22 20
20 | 6 8 8 8 8 4 5 15 4 16 3 | 35 36 34 33 34 33 34 38 35 37 33
21 | 7 10 6 11 11 5 7 17 11 16 3 | 26 28 28 27 24 27 27 29 28 27 26
22 | 8 8 10 6 7 3 8 15 9 19 3 | 25 28 21 25 20 24 24 29 22 30 22
23 | 8 19 8 6 7 3 8 16 4 20 3 | 29 22 22 27 25 26 29 34 27 29 25
24E | 9 10 15 16 17 3 8 9 8 15 4 | 25 24 21 23 22 21 25 23 25 27 21
25 | 10 11 11 8 10 3 6 9 6 14 3 | 24 29 26 26 25 26 29 22 26 26 24
26 | 8 8 11 10 8 5 8 10 7 10 3 | 24 28 28 24 27 26 26 24 27 25 24
27 | 8 10 14 7 8 5 8 8 5 17 3 | 23 27 25 22 22 22 25 22 23 28 22
28 | 8 13 9 10 11 3 8 14 8 15 3 | 19 27 23 23 20 22 25 19 24 18 20
29 | 14 20 7 8 13 4 7 18 8 22 4 | 32 25 26 31 27 27 26 31 28 31 27
X30E | 15 21 13 22 14 4 --- 19 15 15 6 | 82 79 77 83 81 80 --- 79 84 79 80
31E | 8 13 6 16 10 5 9 7 22 11 4 | 67 67 68 68 64 67 67 68 75 68 67
32 | 8 7 7 9 6 4 5 8 6 15 2 | 34 39 33 34 33 34 35 33 35 40 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 9 9 12 4 8 14 8 15 |T 36 37 35 35 33 35 35 36 35 37 35
WRMS | 9 12 9 10 10 4 8 11 6 15 |NE 31 32 30 30 28 30 31 31 29 31 30
MEDI | 8 11 8 8 10 4 8 15 7 15 |MD 28 30 26 27 27 27 29 29 28 30 26
Table 3.2080.1 GPS week: 2080 Day: 1 MJD: 58805.000
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 13 15 9 16 3 11 6 7 8 4 | 48 55 50 52 49 51 53 50 51 55 51
2 | 12 10 7 8 12 2 9 15 6 18 3 | 31 27 22 26 26 23 24 20 24 18 23
3 | 11 11 6 6 12 2 6 8 11 7 3 | 25 31 19 23 17 21 29 17 23 25 21
X4 | 14 --- 9 --- --- 11 --- 19 --- --- 10 | 57 --- 54 --- --- 54 --- 56 --- --- 54
5 | 9 10 10 7 11 3 7 14 7 16 3 | 26 32 25 24 23 24 29 26 24 31 25
6 | 9 12 13 12 12 4 10 11 6 13 4 | 26 31 26 22 24 23 26 22 23 29 23
7E | 14 15 7 10 9 3 8 16 7 15 4 | 28 31 32 32 31 33 33 36 32 36 31
8 | 8 12 12 8 10 4 9 10 9 15 3 | 21 27 21 20 21 20 23 19 20 25 20
9 | 7 8 7 8 7 3 7 9 7 7 2 | 21 31 21 22 21 22 30 22 23 22 22
10 | 6 11 4 5 7 3 6 10 6 7 2 | 17 28 17 17 19 16 25 19 16 20 18
11E | 9 12 6 10 15 3 10 10 10 9 3 | 80 87 78 76 80 79 83 79 80 79 79
12 | 12 15 7 7 11 2 8 18 6 18 4 | 34 36 33 32 34 34 35 35 33 34 32
13 | 8 18 9 8 11 3 9 17 6 16 4 | 21 36 17 21 20 22 31 24 22 27 22
14 | 7 6 5 10 8 2 6 20 7 21 3 | 12 17 12 18 15 15 17 17 14 20 13
15 | 8 13 8 12 8 4 7 23 6 24 4 | 43 49 42 48 41 41 43 38 40 36 41
16 | 11 19 6 8 9 3 7 15 9 23 4 | 19 20 16 15 20 16 19 20 17 19 15
17 | 5 15 7 11 11 3 6 12 9 15 3 | 22 22 17 26 22 21 23 23 26 28 21
X18 | 14 16 10 10 16 8 9 19 9 --- 4 | 26 28 22 22 21 22 27 31 23 --- 21
19 | 9 19 5 11 12 3 6 15 8 16 3 | 24 26 19 25 24 21 23 20 26 21 21
20 | 18 9 8 8 9 2 6 16 5 20 4 | 33 29 27 28 29 27 27 30 27 29 26
21 | 13 13 6 11 11 3 4 16 9 20 4 | 28 22 21 23 21 20 22 20 22 18 20
22 | 8 11 6 8 9 2 5 14 8 21 3 | 26 28 20 23 19 21 23 23 21 24 20
23 | 11 25 7 6 8 3 7 15 11 19 4 | 22 23 18 20 15 19 21 24 18 21 18
X24E | 13 --- 13 18 16 3 12 14 12 14 5 | 26 --- 21 22 25 23 27 24 26 25 22
25 | 12 11 12 7 13 3 9 11 6 11 3 | 22 27 23 22 23 22 25 20 22 21 21
26 | 10 12 10 9 9 3 7 8 10 12 3 | 20 26 24 17 22 21 25 21 22 26 20
27 | 7 12 14 6 10 3 8 9 8 17 3 | 18 23 20 17 20 18 22 18 18 23 18
28 | 10 18 9 7 10 3 8 12 7 11 3 | 18 29 20 19 18 19 22 17 23 17 19
29 | 13 21 7 8 12 3 9 18 8 19 4 | 26 28 25 25 26 24 26 25 23 23 23
30E | 14 41 20 11 22 8 17 14 23 15 7 | 65 81 62 59 62 62 55 62 67 64 62
31E | 11 12 6 11 12 8 9 9 22 12 4 | 32 31 34 32 33 33 33 32 39 37 32
32 | 7 12 7 5 9 2 6 9 6 13 2 | 31 39 29 31 31 30 33 29 28 34 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 9 9 11 4 8 14 10 16 |T 29 33 27 27 27 28 30 28 28 29 27
WRMS | 10 15 9 9 10 3 8 12 7 17 |NE 26 30 24 24 23 24 27 25 24 26 24
MEDI | 10 12 7 8 11 3 8 14 8 15 |MD 26 28 22 23 23 22 26 23 23 25 22
Table 3.2080.2 GPS week: 2080 Day: 2 MJD: 58806.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 12 15 10 13 3 11 8 8 15 4 | 27 29 25 27 24 25 26 25 24 31 24
2 | 8 9 6 10 12 3 8 17 11 17 3 | 33 30 29 33 28 30 31 29 35 27 30
3 | 10 9 5 7 11 3 8 7 7 11 3 | 20 28 18 20 19 21 26 18 21 26 20
X4 | 14 --- 10 --- --- 9 --- 23 --- --- 10 | 56 --- 53 --- --- 58 --- 67 --- --- 56
5 | 6 10 8 5 12 3 7 18 9 20 3 | 30 25 24 25 24 26 29 24 31 28 26
6 | 9 11 14 14 12 5 10 13 10 16 4 | 23 27 25 24 21 22 26 19 23 31 22
7E | 5 13 6 8 17 2 9 13 12 12 3 | 39 38 41 39 47 41 41 45 40 44 40
8 | 6 10 11 6 11 3 8 11 7 13 3 | 22 28 23 21 24 22 24 21 22 27 21
9 | 6 6 6 6 7 3 7 9 8 12 2 | 23 29 23 22 23 22 27 26 19 25 22
10 | 7 9 3 6 10 4 9 9 8 8 2 | 20 30 22 19 25 21 29 21 24 24 22
11E | 9 11 5 14 24 5 8 14 8 10 4 | 72 78 73 74 86 73 75 76 73 77 74
12 | 10 14 7 7 13 3 6 20 10 20 4 | 36 36 29 34 33 33 35 33 36 35 33
13 | 10 12 9 7 33 3 10 17 7 20 4 | 25 31 20 22 43 24 30 30 23 32 25
14 | 7 7 6 9 10 3 6 18 8 21 3 | 20 19 14 18 18 17 16 19 19 25 17
15 | 9 7 7 6 11 4 7 24 12 24 4 | 44 49 44 46 41 44 48 37 50 38 44
16 | 11 18 6 6 11 3 7 16 8 22 4 | 21 19 15 18 19 15 16 17 17 14 14
17 | 5 11 7 13 13 3 7 15 10 14 3 | 22 24 20 27 21 21 22 23 24 25 21
X18 | 19 12 9 17 16 7 10 17 16 --- 5 | 36 28 26 30 21 26 32 31 27 --- 26
19 | 7 13 7 10 14 3 8 16 12 16 3 | 19 20 20 26 19 20 20 19 22 19 19
20 | 9 9 7 9 11 4 5 16 6 21 3 | 26 28 25 25 26 24 27 27 28 31 25
21 | 7 13 5 16 18 5 5 18 13 19 4 | 26 21 23 27 22 24 23 22 28 21 22
22 | 10 7 7 5 11 3 6 15 5 22 3 | 18 22 17 19 20 18 20 24 18 27 18
23 | 8 20 7 9 8 3 7 16 8 23 4 | 21 21 17 24 18 19 20 25 15 22 18
24E | 8 11 14 9 19 4 9 11 8 12 4 | 24 26 19 21 20 22 26 23 24 27 21
25 | 10 12 9 7 14 3 8 11 8 16 3 | 24 27 25 25 23 23 26 22 25 27 23
26 | 9 12 9 9 12 3 8 9 8 14 3 | 21 25 23 20 26 21 24 20 23 24 21
27 | 9 10 12 6 12 4 8 10 8 15 3 | 23 26 20 19 24 19 22 20 21 24 20
28 | 9 14 9 7 13 3 8 16 13 17 4 | 18 29 23 22 20 22 26 18 28 22 21
29 | 15 17 6 8 15 5 7 19 9 25 4 | 24 22 19 21 21 20 21 22 26 19 20
30E | 14 32 19 11 25 6 13 17 15 14 6 | 39 51 44 43 39 40 42 41 40 40 38
31E | 7 14 6 9 25 3 12 11 9 16 4 | 42 39 40 43 44 42 43 43 42 45 41
32 | 7 11 6 8 9 4 7 8 7 17 3 | 29 36 31 28 33 30 35 30 32 41 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 9 15 4 8 15 9 17 |T 28 30 27 27 28 27 29 28 28 29 27
WRMS | 9 12 8 8 13 4 8 13 8 17 |NE 25 27 24 24 24 24 26 25 24 26 24
MEDI | 9 11 7 8 12 3 8 15 8 16 |MD 24 28 23 25 24 22 26 24 24 27 22
Table 3.2080.3 GPS week: 2080 Day: 3 MJD: 58807.000
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 10 15 10 12 4 11 8 7 12 3 | 28 26 27 28 26 26 29 25 26 31 26
2 | 8 10 6 11 13 3 8 16 7 17 3 | 28 30 28 31 28 27 28 24 29 23 26
3 | 9 12 7 8 10 3 8 9 8 7 3 | 21 32 18 19 21 21 29 19 25 25 22
X4 | 13 --- 9 --- --- 15 --- 22 --- --- 10 | 51 --- 45 --- --- 42 --- 54 --- --- 48
5 | 7 8 9 6 12 4 7 17 8 19 3 | 29 29 29 27 27 26 33 27 28 31 28
6 | 7 10 14 13 12 4 8 13 7 14 3 | 22 24 23 23 21 21 22 19 18 28 20
7E | 9 14 6 12 14 3 11 15 8 11 4 | 35 38 37 38 30 35 35 39 34 37 35
8 | 9 10 11 8 12 4 9 11 9 14 3 | 22 24 21 19 22 21 24 20 22 26 20
9 | 9 5 6 8 10 4 6 6 6 7 2 | 23 28 20 22 23 20 27 22 21 24 22
10 | 7 10 4 9 10 4 8 8 6 9 2 | 18 29 17 17 22 18 26 19 17 24 19
11E | 9 10 9 11 33 5 7 7 9 10 4 | 56 54 55 55 70 55 57 54 54 55 55
12 | 11 16 8 10 13 3 9 21 10 21 4 | 28 30 25 27 27 25 27 22 28 27 25
13 | 8 14 8 8 11 3 8 16 4 18 3 | 25 33 19 20 24 23 29 29 22 29 23
14 | 6 8 6 7 9 3 7 20 5 18 3 | 16 18 14 13 17 13 16 18 14 20 13
15 | 9 10 7 10 9 3 7 20 5 23 4 | 41 47 41 45 39 41 45 35 41 37 41
16 | 9 19 4 11 12 4 10 15 9 24 4 | 19 19 16 21 21 16 20 17 16 15 15
17 | 8 9 7 13 11 2 8 16 7 16 3 | 19 20 17 25 21 19 20 22 20 21 19
X18 | 14 18 11 13 11 6 --- 15 13 --- 5 | 33 35 27 26 28 28 --- 33 29 --- 27
19 | 10 13 8 13 13 4 8 17 7 18 4 | 20 16 17 22 20 17 17 18 20 18 17
20 | 8 11 5 10 12 4 6 17 5 19 3 | 20 23 16 18 25 17 20 25 21 26 19
21 | 10 12 8 12 30 5 7 17 7 19 4 | 26 26 24 30 45 27 27 30 29 23 26
22 | 8 9 7 9 9 2 6 16 7 22 3 | 15 21 13 15 16 15 17 24 17 26 15
23 | 11 22 7 8 8 4 7 15 10 20 4 | 24 17 16 21 18 20 19 26 23 23 19
24E | 9 11 16 14 20 4 10 9 7 11 4 | 25 22 17 27 23 23 25 21 22 28 21
25 | 9 15 11 9 11 2 9 11 7 13 3 | 19 22 21 22 20 19 22 16 19 21 18
26 | 10 12 9 11 13 3 7 10 6 12 3 | 21 26 23 21 26 22 24 19 20 24 21
27 | 8 10 12 8 13 2 8 12 11 16 3 | 20 23 20 20 20 19 21 19 21 22 18
28 | 9 13 9 10 12 3 7 18 6 16 3 | 17 26 21 26 19 19 24 18 19 20 19
29 | 13 19 5 7 15 4 8 17 8 22 4 | 19 18 17 18 21 18 18 20 22 19 17
30E | 12 14 18 14 22 5 9 13 10 10 5 | 35 37 33 33 35 33 32 34 35 37 33
31E | 7 14 7 12 16 4 12 9 9 16 4 | 34 36 34 40 38 36 37 39 38 39 36
32 | 8 15 6 7 8 3 8 8 7 13 3 | 22 28 19 17 23 19 24 17 20 30 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 10 15 4 8 14 8 16 |T 25 27 24 25 26 24 26 25 24 26 24
WRMS | 9 13 8 10 13 4 8 12 7 15 |NE 23 25 21 22 22 21 24 23 22 24 22
MEDI | 9 12 8 10 12 4 8 15 7 16 |MD 22 26 21 22 23 21 24 22 22 25 21
Table 3.2080.4 GPS week: 2080 Day: 4 MJD: 58808.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 9 17 8 11 3 10 8 7 10 3 | 30 30 29 32 29 30 32 29 30 32 29
2 | 9 11 6 12 12 3 11 16 9 16 4 | 35 36 33 39 35 34 36 32 35 32 34
3 | 6 8 7 6 9 2 8 8 7 11 2 | 17 27 18 27 18 20 25 20 19 24 20
X4 | 14 --- 11 --- --- 8 --- 21 --- 1647 10 | 51 --- 52 --- --- 52 --- 60 --- 89 53
5 | 7 9 10 5 8 4 10 18 7 21 3 | 28 31 29 28 26 28 35 28 28 31 28
6 | 9 9 15 12 11 4 10 11 8 14 4 | 21 23 21 22 21 20 22 18 20 27 19
7E | 10 15 7 8 8 3 10 13 8 13 3 | 37 40 39 37 37 38 39 44 35 42 38
8 | 5 13 14 6 12 4 9 11 6 14 3 | 22 28 22 21 23 21 26 20 22 25 21
9 | 8 8 7 8 6 3 6 5 6 10 2 | 17 27 19 19 20 18 24 19 21 22 19
10 | 7 12 6 8 8 5 10 9 7 14 3 | 18 27 17 18 19 18 27 18 16 24 18
11E | 11 13 11 15 18 4 8 7 9 12 4 | 67 70 66 64 73 67 70 66 70 71 67
12 | 9 16 7 8 11 3 9 21 9 18 4 | 36 34 29 38 35 34 34 32 33 33 32
13 | 9 11 9 9 11 3 11 16 5 17 3 | 25 31 23 23 32 23 31 27 24 29 25
X14 | 2 --- --- --- --- 17 --- --- --- --- 0 | 27 --- --- --- --- 16 --- --- --- --- 25
15 | 7 10 8 8 9 3 9 21 6 23 4 | 42 46 44 46 38 41 46 37 43 36 41
16 | 9 21 4 6 11 3 9 14 7 23 4 | 17 19 15 18 21 15 16 17 15 14 13
17 | 6 15 8 11 10 2 7 13 7 14 3 | 19 22 18 25 22 20 21 22 21 21 19
X18 | 10 14 11 13 13 5 --- 15 13 11 4 | 30 29 24 23 32 27 --- 29 27 17 25
19 | 6 19 7 9 12 2 7 16 8 17 3 | 18 20 18 23 20 17 19 17 19 13 16
20 | 9 9 8 9 10 5 7 16 7 22 3 | 23 22 19 24 22 22 22 26 20 27 20
21 | 7 13 7 8 27 5 7 18 12 20 4 | 30 31 30 33 38 31 32 31 33 29 30
22 | 7 6 13 4 10 3 5 14 9 22 3 | 18 23 16 22 19 18 19 27 22 26 18
23 | 9 21 8 8 7 3 7 14 6 20 3 | 20 17 15 21 19 18 18 23 20 21 17
24E | 9 11 16 10 14 6 9 9 10 10 4 | 22 23 18 22 19 21 25 21 24 27 20
25 | 9 11 13 7 10 3 8 10 8 14 3 | 22 24 20 24 21 20 23 17 18 22 19
26 | 9 14 11 6 12 3 9 8 6 14 3 | 19 27 24 21 27 22 25 20 20 25 21
27 | 6 11 14 6 12 4 10 10 5 15 3 | 21 24 21 21 21 20 22 19 19 22 19
28 | 7 16 13 10 10 5 8 16 7 16 4 | 15 25 22 23 18 17 22 17 18 14 17
29 | 12 23 7 6 14 4 8 17 10 24 4 | 21 22 18 21 24 20 23 22 20 20 19
30E | 10 13 21 13 20 4 8 11 7 11 4 | 38 42 40 40 37 39 30 42 41 40 38
31E | 7 14 6 7 13 3 10 9 6 15 3 | 40 40 38 41 41 39 38 44 37 46 39
32 | 8 11 7 9 8 3 7 6 6 11 2 | 29 34 28 28 32 29 33 29 28 33 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 11 9 12 4 9 13 8 17 |T 27 29 26 28 27 26 28 28 26 30 26
WRMS | 8 13 11 10 11 4 9 13 7 16 |NE 24 26 23 24 24 23 25 24 22 26 23
MEDI | 8 12 8 8 11 3 9 13 7 15 |MD 22 27 22 23 23 21 25 26 22 27 21
Table 3.2080.5 GPS week: 2080 Day: 5 MJD: 58809.000
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 10 15 13 12 3 11 9 6 15 4 | 23 25 22 24 22 22 24 24 22 30 22
2 | 10 11 5 10 14 4 11 15 11 15 4 | 30 30 27 32 28 27 29 30 26 30 27
3 | 7 9 6 9 9 3 8 6 6 10 2 | 18 27 18 20 18 17 25 18 19 21 18
X4 | 12 --- 8 --- --- 7 --- 21 --- --- 9 | 53 --- 51 --- --- 55 --- 55 --- --- 51
5 | 8 7 8 6 7 4 8 19 7 24 3 | 23 23 17 20 19 19 24 23 18 28 19
6 | 8 10 13 17 11 4 10 12 8 15 4 | 20 23 21 25 21 20 22 20 18 31 20
7E | 6 16 8 13 8 5 11 17 10 16 4 | 47 48 49 49 52 45 44 49 46 47 46
8 | 9 10 13 8 9 4 10 12 8 15 3 | 26 25 24 24 25 23 24 22 23 27 22
9 | 9 8 6 12 6 4 8 9 6 9 3 | 18 24 18 22 18 19 25 19 17 24 18
10 | 8 10 3 11 7 4 9 11 6 14 3 | 24 33 26 24 30 26 32 27 26 32 26
11E | 7 9 7 12 16 4 7 10 12 18 4 | 108 105 107 104 108 106 108 104 103 107 106
12 | 10 15 6 8 10 3 8 22 7 23 4 | 31 31 27 29 31 29 33 30 30 33 29
13 | 12 12 7 7 9 3 11 16 7 18 3 | 24 33 22 24 28 23 33 26 24 30 25
14 | 6 7 6 9 9 5 6 19 9 21 3 | 14 16 12 13 15 13 15 14 13 20 12
15 | 11 9 6 7 6 3 8 20 7 23 3 | 43 45 40 41 37 40 43 39 44 38 40
16 | 14 17 5 10 9 3 8 17 8 22 4 | 21 19 19 21 21 19 17 23 18 21 16
17 | 7 16 8 17 10 3 8 16 8 16 4 | 19 21 20 30 20 20 21 24 22 27 20
X18 | 11 17 11 17 36 8 16 22 24 --- 7 | 38 44 38 32 30 38 40 40 44 --- 34
19 | 9 16 8 19 11 4 8 20 9 19 4 | 22 22 20 33 20 20 20 20 23 20 20
20 | 10 8 8 9 9 5 7 16 5 22 3 | 22 27 25 25 29 24 25 29 28 32 24
21 | 12 12 7 8 17 5 8 16 11 18 4 | 26 25 24 27 30 25 24 24 28 22 23
22 | 7 7 7 8 10 5 7 15 6 23 3 | 19 22 17 22 20 20 22 23 21 26 18
23 | 8 19 7 10 6 5 6 16 8 21 4 | 20 18 17 20 20 18 20 24 20 21 17
24E | 7 11 16 9 13 4 6 10 8 13 3 | 23 23 18 25 25 22 23 22 21 26 21
25 | 12 13 11 9 6 4 9 12 6 13 3 | 29 32 32 30 31 30 34 28 30 30 29
26 | 12 11 11 8 8 3 8 9 8 14 3 | 24 25 26 24 24 22 22 23 20 24 21
27 | 10 11 13 8 10 3 8 12 7 15 3 | 26 24 22 24 23 22 23 23 22 24 21
28 | 7 10 8 10 8 3 7 17 8 15 3 | 16 23 19 21 18 18 22 17 18 16 18
29 | 18 20 9 9 11 4 9 19 7 26 4 | 24 20 19 24 22 21 20 21 22 21 19
30E | 11 11 20 13 18 5 9 13 11 15 5 | 49 48 52 51 46 49 37 50 50 49 48
31E | 9 11 6 8 14 4 9 10 7 11 3 | 36 32 33 37 36 34 33 36 32 35 33
32 | 7 9 7 12 9 3 9 8 8 10 3 | 29 35 32 29 31 30 35 32 31 34 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 9 11 11 4 8 15 8 18 |T 29 30 28 29 28 28 29 29 28 30 27
WRMS | 10 12 9 11 9 4 9 13 7 16 |NE 25 26 24 25 23 24 25 25 23 26 23
MEDI | 9 11 8 9 9 4 8 15 8 15 |MD 24 25 22 25 25 22 24 24 23 27 22
Table 3.2080.6 GPS week: 2080 Day: 6 MJD: 58810.000
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 13 16 9 8 6 11 9 6 16 3 | 33 36 32 30 33 31 33 33 30 39 31
2E | 9 11 6 10 13 3 10 22 8 18 4 | 31 29 28 32 36 30 30 33 29 33 30
3 | 11 10 7 8 8 4 8 5 11 11 3 | 24 33 23 23 25 25 32 25 28 32 25
X4 | 14 --- 9 --- --- 12 --- 21 --- --- 10 | 68 --- 63 --- --- 66 --- 68 --- --- 65
5 | 7 7 8 7 6 4 9 20 7 20 3 | 34 33 33 34 31 32 38 29 34 31 32
6 | 7 10 14 9 7 3 8 13 11 14 3 | 22 27 23 22 21 22 25 23 22 31 22
7E | 8 11 6 11 7 4 11 13 10 14 3 | 54 57 57 58 57 55 55 60 57 63 56
8 | 9 15 12 9 9 5 9 9 8 13 3 | 23 29 25 24 26 23 26 23 24 28 23
9 | 8 5 7 6 6 4 6 6 8 10 2 | 21 26 20 22 23 22 26 21 22 28 21
10 | 9 11 4 10 5 5 7 12 6 12 3 | 30 37 28 28 33 28 34 32 32 36 29
11E | 10 13 10 8 12 4 6 15 9 17 3 | 130 134 132 132 134 133 133 135 131 131 132
12 | 8 15 5 7 9 4 7 21 9 17 3 | 42 40 36 37 39 38 40 38 39 41 38
13 | 9 11 7 8 8 3 9 15 8 16 3 | 29 39 27 34 38 31 36 36 30 39 32
14 | 8 5 7 11 5 4 6 22 8 19 3 | 15 16 13 16 15 15 16 14 14 19 13
15 | 9 10 7 8 5 3 8 19 8 21 3 | 56 61 57 53 51 53 58 46 53 46 53
16 | 11 21 6 9 10 3 9 15 7 22 4 | 21 20 19 23 23 20 20 25 21 24 19
17 | 8 14 6 9 10 3 8 15 8 14 3 | 19 22 20 25 21 21 23 25 23 23 20
X18 | 18 14 11 11 15 12 16 34 13 --- 6 | 95 93 86 84 81 83 92 95 81 --- 87
19 | 19 18 8 9 12 3 7 17 7 15 4 | 27 26 23 26 22 22 23 21 25 18 22
20 | 6 9 7 13 9 6 6 16 8 21 3 | 32 34 32 33 39 32 33 39 38 40 33
21E | 11 12 8 17 7 6 7 16 10 16 4 | 37 33 33 38 34 35 35 34 34 36 34
22 | 8 9 10 8 8 3 7 15 9 20 3 | 24 27 20 23 24 22 24 30 25 31 22
23 | 8 20 8 9 6 4 5 17 6 21 4 | 27 17 19 27 27 23 23 30 25 30 23
24E | 9 9 13 9 8 4 8 8 9 11 3 | 23 22 18 23 23 23 25 23 25 26 22
25 | 10 13 12 8 7 2 8 10 8 11 3 | 29 32 30 31 31 30 32 28 27 30 29
26 | 10 12 13 7 7 5 8 10 7 11 3 | 25 28 30 25 30 28 27 24 28 25 26
27 | 10 12 14 8 10 6 7 10 7 13 3 | 22 24 21 22 24 21 22 21 20 24 20
28 | 9 9 8 10 9 4 8 14 12 17 3 | 18 25 21 24 20 19 23 20 24 21 19
29 | 13 22 7 8 10 4 9 17 10 22 4 | 25 23 20 26 23 21 21 24 23 21 21
30E | 12 11 16 10 11 4 7 13 8 12 4 | 64 64 65 63 59 63 40 66 61 62 62
31E | 10 12 5 9 11 6 8 13 7 14 3 | 60 57 56 59 58 59 58 58 60 61 58
32 | 10 9 6 11 6 4 8 10 11 10 3 | 33 41 33 33 35 34 38 35 33 38 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 9 9 9 4 8 15 9 16 |T 37 38 35 36 36 36 36 37 36 36 36
WRMS | 10 13 9 9 8 4 8 13 8 15 |NE 31 32 30 30 30 30 31 32 30 30 30
MEDI | 9 11 8 9 8 4 8 15 8 15 |MD 29 32 28 28 31 28 32 30 28 31 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 4.2080 GPS week: 2080 MJD: 58804.0-58810.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 |U 9 10 20 |U 0 0 0 |U 13 10 28 |
emr | emr 2948 |U 14 17 38 |U 0 0 0 |U 21 17 49 |
esa | esa 3058 | 11 13 28 |U 0 0 0 | 15 11 32 |
gfz | gfz 2962 |U 9 10 23 |U 0 0 0 |U 13 10 30 |
grg | grg 2959 |U 12 15 28 |U 0 0 0 | 15 10 31 |
igr | igr 3038 | 9 10 23 | 0 0 0 | 14 10 30 |
igs | igs 3048 | 8 11 24 | 0 0 0 | 15 10 31 |
jpl | jpl 2921 |U 13 17 34 |U 0 0 0 |U 21 15 42 |
mit | mit 3058 |U 19 13 32 |U 0 0 0 |U 18 13 42 |
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 5.2080.0 GPS week: 2080 Day: 0 MJD: 58804.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 8 15 | ---- ---- ---- | 13 11 28 |
emr | emr 2976 | 10 15 37 | ---- ---- ---- | 19 17 49 |
esa | esa 3072 | 9 11 18 | ---- ---- ---- | 16 12 32 |
gfz | gfz 2976 | 7 8 14 | ---- ---- ---- | 11 10 30 |
grg | grg 2974 | 6 8 19 | ---- ---- ---- | 14 11 30 |
igr | igr 3063 | 7 10 15 | ---- ---- ---- | 14 11 31 |
igs | igs 3063 | 6 9 16 | ---- ---- ---- | 15 11 31 |
jpl | jpl 2880 | 13 18 28 | ---- ---- ---- | 20 19 38 |
mit | mit 3072 | 52 12 73 | ---- ---- ---- | 26 25 54 |
Table 5.2080.1 GPS week: 2080 Day: 1 MJD: 58805.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 12 16 | ---- ---- ---- | 13 9 27 |
emr | emr 2879 | 28 18 57 | ---- ---- ---- | 28 24 51 |
esa | esa 3072 | 11 11 43 | ---- ---- ---- | 15 10 28 |
gfz | gfz 2975 | 11 11 39 | ---- ---- ---- | 14 10 30 |
grg | grg 2974 | 20 19 39 | ---- ---- ---- | 18 10 29 |
igr | igr 3014 | 11 11 37 | ---- ---- ---- | 13 8 26 |
igs | igs 3056 | 10 11 38 | ---- ---- ---- | 15 9 29 |
jpl | jpl 2976 | 15 16 45 | ---- ---- ---- | 22 13 42 |
mit | mit 3072 | 14 13 38 | ---- ---- ---- | 21 15 40 |
Table 5.2080.2 GPS week: 2080 Day: 2 MJD: 58806.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 11 10 22 | ---- ---- ---- | 11 7 24 |
emr | emr 2976 | 15 14 34 | ---- ---- ---- | 20 16 49 |
esa | esa 3072 | 11 10 28 | ---- ---- ---- | 14 8 28 |
gfz | gfz 2976 | 10 10 20 | ---- ---- ---- | 12 8 27 |
grg | grg 2975 | 10 9 24 | ---- ---- ---- | 13 9 28 |
igr | igr 3071 | 10 10 20 | ---- ---- ---- | 13 7 25 |
igs | igs 3054 | 10 10 22 | ---- ---- ---- | 14 8 26 |
jpl | jpl 2976 | 10 17 31 | ---- ---- ---- | 20 13 35 |
mit | mit 3072 | 12 9 20 | ---- ---- ---- | 14 7 28 |
Table 5.2080.3 GPS week: 2080 Day: 3 MJD: 58807.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 9 9 20 | ---- ---- ---- | 15 10 30 |
emr | emr 2975 | 12 17 30 | ---- ---- ---- | 22 17 53 |
esa | esa 3072 | 11 13 26 | ---- ---- ---- | 16 10 33 |
gfz | gfz 2975 | 9 7 19 | ---- ---- ---- | 15 10 31 |
grg | grg 2974 | 7 9 22 | ---- ---- ---- | 16 11 34 |
igr | igr 3015 | 9 10 20 | ---- ---- ---- | 15 10 31 |
igs | igs 3071 | 8 10 20 | ---- ---- ---- | 16 11 34 |
jpl | jpl 2880 | 13 19 29 | ---- ---- ---- | 20 18 43 |
mit | mit 3072 | 13 11 22 | ---- ---- ---- | 16 10 34 |
Table 5.2080.4 GPS week: 2080 Day: 4 MJD: 58808.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 8 26 | ---- ---- ---- | 14 10 28 |
emr | emr 2880 | 12 18 40 | ---- ---- ---- | 21 12 50 |
esa | esa 2976 | 10 13 32 | ---- ---- ---- | 16 10 36 |
gfz | gfz 2880 | 8 9 24 | ---- ---- ---- | 14 11 30 |
grg | grg 2877 | 8 9 20 | ---- ---- ---- | 13 9 30 |
igr | igr 2975 | 8 9 27 | ---- ---- ---- | 14 11 30 |
igs | igs 2972 | 8 9 27 | ---- ---- ---- | 15 10 32 |
jpl | jpl 2784 | 11 15 43 | ---- ---- ---- | 23 11 43 |
mit | mit 2976 | 21 21 31 | ---- ---- ---- | 17 11 33 |
Table 5.2080.5 GPS week: 2080 Day: 5 MJD: 58809.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 9 10 20 | ---- ---- ---- | 13 12 36 |
emr | emr 2976 | 10 17 35 | ---- ---- ---- | 18 17 49 |
esa | esa 3072 | 12 15 26 | ---- ---- ---- | 15 13 35 |
gfz | gfz 2976 | 9 8 21 | ---- ---- ---- | 14 11 31 |
grg | grg 2971 | 17 26 36 | ---- ---- ---- | 15 14 33 |
igr | igr 3064 | 9 11 19 | ---- ---- ---- | 14 11 34 |
igs | igs 3052 | 9 13 21 | ---- ---- ---- | 15 12 34 |
jpl | jpl 2976 | 15 18 30 | ---- ---- ---- | 21 16 45 |
mit | mit 3072 | 13 12 25 | ---- ---- ---- | 18 13 60 |
Table 5.2080.6 GPS week: 2080 Day: 6 MJD: 58810.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 9 19 | ---- ---- ---- | 13 9 26 |
emr | emr 2976 | 11 18 31 | ---- ---- ---- | 21 20 45 |
esa | esa 3072 | 9 16 26 | ---- ---- ---- | 15 13 36 |
gfz | gfz 2976 | 10 16 24 | ---- ---- ---- | 15 11 31 |
grg | grg 2974 | 15 26 37 | ---- ---- ---- | 14 10 30 |
igr | igr 3067 | 7 11 21 | ---- ---- ---- | 15 10 32 |
igs | igs 3072 | 8 13 22 | ---- ---- ---- | 15 12 31 |
jpl | jpl 2976 | 13 20 33 | ---- ---- ---- | 19 16 45 |
mit | mit 3072 | 10 12 19 | ---- ---- ---- | 16 13 44 |
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 6.2080 GPS week: 2080 MJD: 58804.500-58810.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -7 35 32 6 | 4 15
| 9 12 63 69 3 | 2
emr uuuuu | 10 41 -7 70 -2 | 34 38
| 41 21 79 108 8 | 2
esa uuuuu | -22 22 -49 -145 -3 | 18 23
| 12 17 69 45 4 | 3
gfz uuuuu | 6 -10 -45 22 -3 | 17 23
| 15 26 108 77 6 | 2
grg uuuuu | 18 6 14 89 -1 | -4 11
| 21 20 42 33 2 | 1
igr xxxxx | 10 24 24 -3 0 | -4 14
| 13 9 57 47 5 | 2
irf xxxxx | -5 -3 22 24 -1 | -2 14
| 8 16 41 21 4 | 1
jpl uuuuu | -19 -18 103 -74 -5 | 36 41
| 17 19 57 71 12 | 3
mit uuuuu | 13 9 31 64 -4 | 15 20
| 19 12 73 36 8 | 1
ngs uuxuu | 13 -25 118 36 2 | 9 15
| 25 41 253 78 4 | 2
sio uuuux | -12 31 -199 -24 5 | 44 46
| 16 8 83 108 8 | 2
Table 7.2080.0 GPS week: 2080 Day: 0 MJD: 58804.500
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 -5 20 39 3 | 5 15
emr uuuuu | 12 53 -110 33 -9 | 36 40
esa uuuuu | -3 9 -91 -134 1 | 21 25
gfz uuuuu | -3 -34 -60 -141 0 | 18 23
grg uuuuu | 5 7 47 34 -3 | -4 8
igr xxxxx | 34 17 46 -69 10 | -5 11
irf xxxxx | 9 -23 63 26 7 | -2 11
jpl uuuuu | -43 -4 140 61 1 | 37 41
mit uuuuu | 33 1 110 30 9 | 14 17
ngs uuxuu | 11 -18 75 24 1 | 9 14
sio uuuux | 0 31 -157 129 12 | 40 41
Table 7.2080.1 GPS week: 2080 Day: 1 MJD: 58805.500
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 -19 -15 33 3 | 7 17
emr uuuuu | 98 66 -115 192 -8 | 37 41
esa uuuuu | -41 11 -179 -134 -9 | 22 27
gfz uuuuu | 7 -6 15 14 -9 | 20 25
grg uuuuu | -4 14 29 97 1 | -2 9
igr xxxxx | 1 10 77 -27 -2 | -2 14
irf xxxxx | -4 -22 62 59 1 | 0 14
jpl uuuuu | 4 -4 157 -70 15 | 39 44
mit uuuuu | 20 6 130 57 4 | 17 22
ngs uuxuu | -17 -42 139 -49 -1 | 11 17
sio uuuux | 4 26 -112 71 17 | 43 45
Table 7.2080.2 GPS week: 2080 Day: 2 MJD: 58806.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -13 25 45 10 | 5 16
emr uuuuu | -28 37 33 -80 9 | 33 38
esa uuuuu | -21 9 14 -86 -7 | 20 25
gfz uuuuu | 20 17 -157 59 -4 | 19 25
grg uuuuu | 0 34 52 71 -3 | -3 10
igr xxxxx | 2 34 74 58 -3 | -2 14
irf xxxxx | -10 -1 30 9 0 | 0 15
jpl uuuuu | -39 -46 108 -171 -9 | 41 45
mit uuuuu | 33 19 5 48 0 | 17 22
ngs uuxuu | 56 -19 238 165 1 | 10 16
sio uuuux | -6 20 -139 52 11 | 45 47
Table 7.2080.3 GPS week: 2080 Day: 3 MJD: 58807.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 5 -23 174 -6 3 | 3 14
emr uuuuu | 5 57 -17 38 9 | 32 37
esa uuuuu | -25 45 11 -147 -3 | 16 23
gfz uuuuu | -11 -13 -160 26 -6 | 16 22
grg uuuuu | 14 22 4 113 0 | -5 12
igr xxxxx | 10 23 16 35 -8 | -4 15
irf xxxxx | -7 1 5 25 -1 | -2 15
jpl uuuuu | -10 2 27 -96 -9 | 36 40
mit uuuuu | 13 27 -21 97 -6 | 15 21
ngs uuxuu | 25 -71 170 123 3 | 7 15
sio uuuux | -24 36 -125 -112 3 | 44 46
Table 7.2080.4 GPS week: 2080 Day: 4 MJD: 58808.500
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 | 7 12 1 159 9 | 2 14
emr uuuuu | -3 44 59 -30 -3 | 33 38
esa uuuuu | -32 39 -5 -216 -1 | 15 22
gfz uuuuu | -8 28 -83 28 7 | 14 21
grg uuuuu | 21 8 19 68 -2 | -5 12
igr xxxxx | 6 36 59 -43 -2 | -5 16
irf xxxxx | -16 -7 53 -6 -5 | -3 15
jpl uuuuu | -10 -40 116 -47 -19 | 35 39
mit uuuuu | -10 3 74 55 -11 | 15 20
ngs uuxuu | 24 -67 523 -14 -2 | 7 14
sio uuuux | 4 42 -304 -51 -4 | 45 47
Table 7.2080.5 GPS week: 2080 Day: 5 MJD: 58809.500
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 3 34 -71 10 | 3 14
emr uuuuu | -9 16 82 142 -10 | 34 38
esa uuuuu | -20 37 -50 -109 -3 | 14 21
gfz uuuuu | 31 -18 -21 93 -9 | 14 21
grg uuuuu | 56 -20 -75 131 -3 | -5 12
igr xxxxx | 19 25 -76 34 1 | -6 16
irf xxxxx | -11 22 -37 18 -5 | -3 15
jpl uuuuu | -21 -26 151 -83 -17 | 33 38
mit uuuuu | -15 12 -28 33 -12 | 14 20
ngs uuxuu | 6 -12 -4 6 10 | 7 14
sio uuuux | -37 37 -258 -110 -5 | 45 47
Table 7.2080.6 GPS week: 2080 Day: 6 MJD: 58810.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 5 -5 8 27 6 | 5 15
emr uuuuu | -6 12 19 191 -2 | 33 37
esa uuuuu | -14 7 -42 -188 2 | 15 22
gfz uuuuu | 9 -43 151 71 -3 | 15 21
grg uuuuu | 33 -21 20 108 1 | -4 11
igr xxxxx | -3 22 -28 -7 0 | -4 16
irf xxxxx | 1 6 -22 38 -4 | -2 15
jpl uuuuu | -16 -8 20 -116 4 | 32 38
mit uuuuu | 19 -8 -52 129 -9 | 14 20
ngs uuxuu | -11 51 -312 -3 -2 | 9 16
sio uuuux | -23 26 -294 -150 2 | 46 48
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