[IGSREPORT-26695] Wk 2060 IGS Final Orbits
acc
acc at igs.org
Sun Jul 21 05:05:19 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2060 (Jun 30, 2019 - Jul 06, 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:
igs2060[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2060[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2060[0-6].cls IGS GPS clock combination summary report.
igs20607.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20607.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 | INEG TIXI INEG TIXI
0 | ESA | 18 CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB HERS HOB2
0 | ESA | KIRU KOUR MAJU MAS1 MAW1 MGUE MOBS NNOR ONSA POHN
0 | ESA | PTBB TOW2 USN7 VILL CEDU COCO DARW DAV1 DGAR FAA1
0 | ESA | GRAZ HARB HERS HOB2 KIRU KOUR MAJU MAS1 MAW1 MGUE
0 | ESA | MOBS NNOR ONSA POHN PTBB TOW2 USN7 VILL
0 | GFZ | 18 19 22 KRGG POHN GODE KRGG POHN
0 | GRG | IRKJ NNOR IRKJ NNOR
0 | MIT | NNOR
1 | COD | ANKR ANKR
1 | EMR | CHUR CHUR
1 | ESA | 18 18 ABMF CEDU COCO DARW DAV1 DGAR FAA1 GLPS GRAZ
1 | ESA | HARB HERS HOB2 KIRU KOUR MAJU MAR6 MAS1 MAW1 MGUE
1 | ESA | MOBS NNOR ONSA POHN TONG TOW2 VILL ABMF CEDU COCO
1 | ESA | DARW DAV1 DGAR FAA1 GLPS HARB HERS HOB2 KIRU KOUR
1 | ESA | MAJU MAR6 MAS1 MAW1 MGUE MOBS NNOR ONSA POHN TONG
1 | ESA | TOW2 VILL
1 | GFZ | 18 16 18 19 20 21 22 GODE POHN GODE POHN WTZR
1 | GRG | TRO1 TRO1
1 | JPL | RAMO
2 | COD | 21 18 KRGG SOFI TIXI KRGG SOFI TIXI
2 | EMR | 21 USN7 YAKT
2 | ESA | 18 21 18 CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB
2 | ESA | HERS HOB2 KIRU KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS
2 | ESA | NAUR NNOR ONSA POHN PTBB TOW2 VILL CEDU COCO DARW
2 | ESA | DAV1 DGAR FAA1 GRAZ HARB HERS HOB2 IRKJ KIRU KOUR
2 | ESA | MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR ONSA POHN
2 | ESA | PTBB TOW2 VILL
2 | GFZ | 18 18 19 22 POHN GLSV GODE POHN
2 | GRG | IRKJ KIT3 IRKJ KIT3
2 | JPL | MCIL MCIL
2 | MIT | SOFI
3 | COD | GLSV KIT3 TIXI GLSV KERG KIT3 TIXI
3 | EMR | QAQ1 QAQ1
3 | ESA | 18 CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS
3 | ESA | HOB2 KIRU KOUR LAUT LPGS MAJU MAR6 MAS1 MAW1 MGUE
3 | ESA | MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL CEDU COCO
3 | ESA | DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2 KIRU
3 | ESA | KOUR LAUT LPGS MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR
3 | ESA | NNOR ONSA POHN PTBB TOW2 VILL
3 | GFZ | 18 KERG POHN WES2 KERG POHN WES2
3 | GRG | PIE1 SCOR NRIL PIE1 SCOR
3 | MIT | GLSV KERG WAB2
4 | COD | TIXI HOB2 TIXI
4 | EMR | IENG PTBB
4 | ESA | 18 18 CEDU COCO DARW DAV1 DGAR FALK GRAZ HARB HERS
4 | ESA | IISC KIRU KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR
4 | ESA | NNOR ONSA POHN PTBB TONG TOW2 VILL CEDU COCO DARW
4 | ESA | DAV1 DGAR FALK GRAZ HARB HERS HOB2 IISC KIRU KOUR
4 | ESA | MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR ONSA POHN
4 | ESA | PTBB TONG TOW2 VILL
4 | GFZ | 18 18 19 20 21 22 IISC POHN GODE HOB2 IISC MCIL POHN
4 | GRG | CPVG
4 | JPL | MCIL NYAL HOB2 MCIL NYAL
5 | COD | TIXI SOFI TIXI
5 | EMR | PTBB PTBB TSKB
5 | ESA | AREG CEDU COCO DARW DAV1 DGAR GRAZ HARB HERS HOB2
5 | ESA | IISC KIRU KOUR LPGS MAJU MAR6 MAS1 MAW1 MGUE MOBS
5 | ESA | NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL AREG CEDU
5 | ESA | COCO DARW DAV1 DGAR GRAZ HARB HERS HOB2 IISC KIRU
5 | ESA | KOUR LPGS MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR
5 | ESA | ONSA POHN PTBB TONG TOW2 VILL
5 | GFZ | IISC KRGG IISC KRGG
5 | GRG | 17 11 17 21 BRST
6 | COD | BARH TIXI TIXI
6 | EMR | 21
6 | ESA | 6 AREG CEDU COCO DARW DAV1 DGAR GRAZ HARB HERS HOB2
6 | ESA | IISC KIRU KOUR LHAZ MAJU MAR6 MAS1 MAW1 MGUE MOBS
6 | ESA | NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL AREG CEDU
6 | ESA | COCO DARW DAV1 DGAR GRAZ HARB HERS HOB2 IISC KIRU
6 | ESA | KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR ONSA
6 | ESA | POHN PTBB TONG TOW2 VILL
6 | GFZ | 19 20 21 22 POHN BARH POHN
6 | GRG | LPGS LPGS
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. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G24 | | | | | 4 | 4 | 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 | -.1 .5 1.0 12 31 -11 -.45
EMR | 0 | -2.4 -17.3 -2.3 -38 68 -38 -.23
ESA | 0 | .2 -.0 1.3 -34 5 27 -.67
GFZ | 0 | -.8 1.1 1.3 38 32 -9 -.41
GRG | 0 | -7.8 -14.1 -3.8 130 27 85 -.48
JPL | 0 | -.6 -8.4 -2.9 4 19 -1 -.79
MIT | 0 | -6.2 -13.0 4.5 -41 38 12 -.16
NGS | 0 | -2.8 -17.0 -.9 -33 39 3 -.22
SIO | 0 | -6.0 -11.3 2.0 -10 -5 -21 -.24
COD | 1 | .2 .2 1.9 24 37 -3 -.69
EMR | 1 | -7.4 -10.3 -8.1 -21 75 -67 -.40
ESA | 1 | .3 .2 1.5 -11 5 29 -.80
GFZ | 1 | -.5 1.0 1.3 53 26 3 -.47
GRG | 1 | -4.6 -12.3 -3.2 109 23 84 -.46
JPL | 1 | -2.2 -7.6 -2.5 4 3 -22 -.82
MIT | 1 | -10.6 -14.0 6.6 -24 50 2 -.11
NGS | 1 | -1.1 -13.8 -5.6 8 33 5 -.46
SIO | 1 | -7.0 -9.9 -7.2 -24 9 -22 -.21
COD | 2 | .3 .0 2.0 18 36 -2 -.71
EMR | 2 | -7.3 -10.4 -10.8 -22 67 -87 -.48
ESA | 2 | .1 .5 1.8 -15 32 8 -.79
GFZ | 2 | .1 .7 1.2 40 12 -3 -.63
GRG | 2 | -4.9 -14.1 -4.8 102 -10 110 -.41
JPL | 2 | -7.1 -10.9 -7.4 3 5 -1 -.83
MIT | 2 | -9.5 -14.2 .8 -20 48 -13 -.29
NGS | 2 | -6.7 -10.3 -5.3 13 54 1 -.41
SIO | 2 | -9.9 -11.4 -7.3 -13 5 -39 -.42
COD | 3 | .7 -.1 1.3 19 20 -3 -.61
EMR | 3 | -3.8 -7.3 -15.4 -7 47 -92 -.58
ESA | 3 | .5 -.1 2.0 -29 20 -7 -.72
GFZ | 3 | -.3 .9 1.2 43 25 1 -.50
GRG | 3 | -4.7 -13.4 -.7 105 -12 135 -.44
JPL | 3 | -2.1 -11.9 -5.8 -8 7 1 -.69
MIT | 3 | -9.0 -9.0 -1.0 1 50 -27 -.22
NGS | 3 | -4.8 -11.2 -5.3 16 30 35 -.38
SIO | 3 | -7.9 -9.3 -4.5 -16 14 -17 -.28
COD | 4 | .2 .4 1.2 26 21 -4 -.52
EMR | 4 | -1.8 -3.4 -6.8 -6 65 -82 -.31
ESA | 4 | .2 .1 1.5 -7 3 18 -.71
GFZ | 4 | -.4 1.1 1.2 53 19 -4 -.53
GRG | 4 | -1.5 -6.7 -18.0 85 -4 88 -.34
JPL | 4 | 2.0 -6.0 -6.6 11 3 -1 -.44
MIT | 4 | -3.7 -9.8 .1 -10 47 -12 -.22
NGS | 4 | -1.5 -8.1 -5.7 16 43 4 -.18
SIO | 4 | -4.6 -9.0 -4.0 5 -8 -20 -.29
COD | 5 | -.5 .3 .5 17 26 -15 -.32
EMR | 5 | 5.6 -4.4 -10.4 -34 59 -78 -.01
ESA | 5 | -.4 -.9 .2 -40 10 3 -.33
GFZ | 5 | -.4 .7 .9 36 26 -4 -.43
GRG | 5 | -.9 -9.1 .8 78 2 86 -.11
JPL | 5 | -.6 -4.6 -7.0 13 6 -7 -.72
MIT | 5 | .2 -10.7 4.8 -27 48 -33 .04
NGS | 5 | -1.8 -5.1 -10.2 41 50 -15 -.22
SIO | 5 | -2.2 -9.1 -5.1 -31 13 -28 -.10
COD | 6 | .2 -.0 1.5 7 20 1 -.54
EMR | 6 | 3.9 -.2 -12.5 -62 64 -35 -.11
ESA | 6 | -.1 -.8 -.2 6 38 46 -.64
GFZ | 6 | .1 .7 .9 40 21 14 -.63
GRG | 6 | 2.1 -6.6 -4.1 77 1 109 -.34
JPL | 6 | 3.0 -6.3 -4.7 3 9 -4 -.72
MIT | 6 | -3.6 -10.3 1.7 -33 50 8 -.16
NGS | 6 | 2.6 -9.8 -6.5 -8 51 10 -.47
SIO | 6 | -4.1 -7.1 -6.4 -13 21 -10 -.31
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 1.2060.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2060.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 2.2060.[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 3.2060.[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 5.2060.0-6). 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 2060 summary. (Jun 30, 2019 - Jul 06, 2019)
Table 1.2060.a GPS week: 2060 MJD: 58664.000-58670.000
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 248| 1 0 3 7 16 0 -.03 9 9 | -607 -17 6 91
| 0 0 2 13 8 13 .03 | 198 366
emr 79| -1 0 -3 -9 -8 12 .09 12 12 | 138129 285 17 107
| 1 1 1 12 12 12 .02 | 1449 968
esa 150| 0 0 -2 -23 -1 -9 -.10 10 10 | 1547 411 7 106
| 0 0 1 7 7 10 .03 | 2864 750
gfz 178| 0 1 1 -20 9 -5 .10 10 10 | -93 32 12 207
| 0 0 1 11 9 9 .06 | 288 476
grg 98| 2 0 -3 0 5 21 -.10 13 12 | -30 -32 11 137
| 0 0 6 11 7 39 .04 | 137 250
igr n/a| 0 1 1 -23 -35 -11 -.02 4 4 | -15580 -161 11 70
| 0 0 0 11 5 16 .01 | 1000 1145
jpl 80| -1 1 0 32 8 17 .11 7 7 | 212948 427 9 77
| 0 1 0 8 12 13 .02 | 1815 1036
mit 349| 0 -1 4 -9 -14 -3 -.01 12 11 | -774 3 54 1738
| 0 0 1 26 23 18 .02 | 567 173
ngs 210| 0 0 -2 7 -4 -10 -.03 8 7 | -570 -47 939 2132
| 0 0 1 8 15 18 .02 | 86 237
sio 324| 0 -2 4 -2 -24 -15 -.11 14 14 | --- --- --- ---
| 0 1 1 16 33 15 .03 | --- ---
Table 1.2060.b GPS week : 2060 MJD: 58664.000-58670.000
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 | 3 4 3 3 4 4 4 |
3 | 3 3 3 3 3 3 3 |
4 | 0 0 0 0 0 0 0 |
5 | 3 4 3 4 4 3 4 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 4 4 3 |
8 | 3 3 3 3 3 3 3 |
9 | 4 3 4 3 3 3 3 |
10 | 3 3 3 3 4 4 4 |
11 | 4 3 4 3 4 4 4 |
12 | 4 4 4 4 4 5 4 |
13 | 3 3 3 3 3 3 3 |
14 | 3 3 3 3 3 3 4 |
15 | 4 4 3 3 3 3 3 |
16 | 5 4 4 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 5 5 4 5 8 6 5 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 5 5 4 5 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 3 4 3 3 3 3 3 |
24 | 3 3 3 4 3 3 3 |
25 | 4 4 4 5 5 4 5 |
26 | 4 4 4 4 4 4 5 |
27 | 3 3 3 3 3 3 3 |
28 | 3 4 3 4 4 4 4 |
29 | 4 4 4 4 4 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 4 4 4 4 4 4 4 |
32 | 4 3 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2060.0 GPS week: 2060 Day: 0 MJD: 58664.000
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 228| 0 0 2 8 20 6 -.02 11 10 | -704 270 8 99
emr 80| -3 -1 -1 -8 0 12 .08 12 12 | 136517 114 17 105
esa 150| 0 0 -1 -26 -6 -6 -.06 10 9 | -1588 1091 7 104
gfz 181| 0 1 -1 -15 23 -11 .13 10 10 | -44 253 12 205
grg 98| 2 0 -4 11 16 -18 -.14 12 11 | -62 204 11 135
igr n/a| 0 1 0 -4 -32 2 .00 4 4 | -16363 -354 11 77
jpl 80| -1 0 0 27 19 26 .08 7 7 | 210855 136 8 81
mit 350| 1 -1 5 -33 -41 -21 -.04 13 13 | -553 131 43 1856
ngs 214| 1 0 0 6 8 0 .00 8 7 | -535 197 733 1801
sio 330| 1 0 3 -14 -73 -15 -.16 14 13 | --- --- --- ---
Table 2.2060.1 GPS week: 2060 Day: 1 MJD: 58665.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 2 0 4 24 29 1 -.03 10 9 | -641 142 7 84
emr 80| -2 0 -2 -20 -4 37 .06 11 11 | 136242 1167 17 108
esa 150| 0 0 -1 -19 0 4 -.08 9 9 | -1619 1331 8 109
gfz 182| 0 0 0 -27 18 13 .15 10 10 | -31 237 11 204
grg 101| 2 -1 -4 -7 9 -30 -.11 13 11 | -6 54 10 136
igr n/a| 0 1 1 -36 -34 -5 -.02 4 4 | -16998 960 12 76
jpl 80| -1 2 0 29 -15 -3 .10 8 8 | 210652 1362 9 84
mit 350| 0 -2 5 8 16 0 -.02 12 11 | -261 86 59 1696
ngs 213| 0 0 -2 5 -6 5 -.03 7 7 | -647 149 945 2244
sio 328| 0 -1 4 -4 -29 -27 -.12 14 15 | --- --- --- ---
Table 2.2060.2 GPS week: 2060 Day: 2 MJD: 58666.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 2 0 3 8 12 7 -.06 9 8 | -558 -19 6 81
emr 80| -1 0 -4 -21 0 10 .10 12 12 | 137225 1221 18 123
esa 150| 0 0 0 -29 10 4 -.07 10 10 | 3661 541 8 105
gfz 180| 0 2 2 -22 0 -13 .13 9 10 | 114 9 14 220
grg 100| 2 0 -3 5 10 -3 -.09 13 11 | 8 -81 9 133
igr n/a| 0 1 2 -22 -35 3 -.01 4 4 | -16149 932 12 65
jpl 80| -1 0 0 42 2 25 .13 7 7 | 211804 1518 10 81
mit 350| 0 -1 2 -31 -27 3 .02 12 10 | -1642 131 41 1902
ngs 210| -1 0 -3 18 11 -2 -.06 7 7 | -583 -88 1108 1993
sio 327| 1 -2 4 -19 -49 -30 -.14 13 13 | --- --- --- ---
Table 2.2060.3 GPS week: 2060 Day: 3 MJD: 58667.000
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 7 -17 20 16 -.05 10 9 | -987 559 7 94
emr 80| -3 0 -4 -14 -36 12 .09 13 13 | 138570 1253 19 101
esa 150| 0 1 -4 -28 1 -23 -.14 10 10 | 3560 193 9 116
gfz 179| 0 0 0 0 12 -15 .14 9 10 | 389 -1004 11 211
grg 100| 1 0 -2 12 7 27 -.06 11 11 | -182 294 10 141
igr n/a| 0 1 0 -21 -29 -9 -.03 4 4 | -15049 947 11 67
jpl 80| 0 1 0 22 16 23 .10 8 8 | 213449 1426 9 76
mit 348| 0 -1 3 31 -12 -26 .00 12 10 | -382 67 49 1719
ngs 210| -1 0 -3 -6 -15 6 -.04 8 7 | -658 187 806 2036
sio 326| 0 -3 6 18 -18 -16 -.09 14 13 | --- --- --- ---
Table 2.2060.4 GPS week: 2060 Day: 4 MJD: 58668.000
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 3 15 5 -4 -.07 9 8 | -532 -262 6 82
emr 80| 0 0 -2 -13 -5 9 .10 12 12 | 139807 -258 18 108
esa 150| 0 0 -1 -18 -14 -11 -.12 14 11 | 3839 -101 7 102
gfz 179| 0 0 2 -19 6 -2 .06 9 9 | -357 311 14 197
grg 100| 1 -1 -16 5 0 48 -.12 15 13 | 240 -459 13 141
igr n/a| 0 1 2 -19 -32 -9 -.03 4 4 | -14015 -746 12 71
jpl 80| -2 1 -1 33 12 26 .11 7 7 | 214855 -127 9 67
mit 348| 0 -1 4 -29 -3 -5 -.02 12 11 | -309 6 79 1777
ngs 209| 0 0 -1 16 14 -29 -.02 9 8 | -524 -274 986 2467
sio 322| 0 -1 6 -19 -23 -28 -.08 14 13 | --- --- --- ---
Table 2.2060.5 GPS week: 2060 Day: 5 MJD: 58669.000
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 250| 1 0 0 15 10 -26 -.03 9 8 | -391 -442 7 106
emr 79| 0 0 -3 -2 -3 -5 .09 12 12 | 139233 -213 18 114
esa 150| -1 0 -3 -33 0 -17 -.11 10 9 | 4282 -877 8 107
gfz 175| 0 1 3 -34 0 -6 .00 9 9 | -325 42 9 222
grg 96| 2 0 4 -13 0 68 -.02 17 16 | -140 -184 13 138
igr n/a| 0 1 2 -41 -47 -17 -.04 4 4 | -15020 -902 10 70
jpl 80| 0 0 1 26 4 24 .13 7 7 | 214351 -104 11 81
mit 349| 0 0 4 12 9 -2 .01 13 12 | -1477 -32 50 1639
ngs 208| 0 0 -5 4 -15 -10 -.03 8 7 | -633 -97 852 2020
sio 317| 0 -3 2 18 -8 6 -.11 14 14 | --- --- --- ---
Table 2.2060.6 GPS week: 2060 Day: 6 MJD: 58670.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| 0 0 2 -2 21 5 .01 8 8 | -440 -369 7 96
emr 80| 1 3 -4 13 -12 12 .11 13 13 | 139311 -1284 18 96
esa 150| -1 0 -2 -11 1 -17 -.10 11 11 | -1302 701 8 99
gfz 174| 0 0 1 -27 0 -3 .06 10 10 | -401 377 13 190
grg 94| 3 0 1 -14 -3 57 -.11 14 14 | -72 -53 12 136
igr n/a| 0 1 1 -19 -36 -45 -.01 3 3 | -15470 -1967 11 70
jpl 80| 0 0 -1 47 20 0 .12 8 8 | 214671 -1221 9 73
mit 349| 0 -1 4 -21 -42 29 -.01 13 11 | -798 -366 60 1581
ngs 209| 0 -1 -3 5 -27 -42 -.06 8 7 | -415 -407 1146 2366
sio 319| 0 -1 4 1 34 4 -.10 14 13 | --- --- --- ---
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 3.2060.0 GPS week: 2060 Day: 0 MJD: 58664.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 11 17 14 12 3 7 13 6 7 3 | 25 27 23 27 27 23 26 27 25 22 24
2E | 9 10 8 5 11 3 6 16 7 11 3 | 34 34 31 28 29 31 29 33 36 32 31
3 | 10 9 9 8 11 5 5 8 8 9 3 | 28 26 27 24 25 24 27 21 25 25 25
X4 | 2 --- --- --- --- 23 --- --- --- --- 0 | 25 --- --- --- --- 30 --- --- --- --- 25
5 | 7 10 9 10 10 2 6 12 7 15 3 | 29 31 28 32 32 29 33 25 33 24 29
6E | 9 13 16 13 13 4 7 10 9 9 4 | 29 26 26 29 26 24 27 27 26 29 25
7 | 8 11 8 12 10 3 6 15 8 19 3 | 37 39 38 40 39 36 38 37 37 35 37
8 | 8 8 10 6 13 3 7 8 5 8 3 | 20 21 20 20 21 17 22 17 18 16 18
9 | 9 12 6 13 10 4 9 9 8 10 3 | 26 35 28 24 24 26 35 25 27 30 28
10 | 10 7 10 10 14 3 6 9 6 7 3 | 21 25 25 25 28 23 25 21 25 23 23
11 | 10 7 11 15 15 3 6 13 7 12 3 | 30 34 37 32 26 32 36 37 35 30 32
12E | 13 20 7 9 8 4 9 15 8 13 4 | 35 32 35 30 35 35 30 41 36 38 33
13 | 10 7 7 12 9 3 5 11 8 12 3 | 12 18 17 27 13 16 16 18 19 19 16
14 | 11 8 9 12 7 3 7 11 7 12 3 | 21 15 20 28 20 20 14 23 19 20 18
15 | 9 11 6 12 8 3 7 15 6 15 3 | 21 25 23 30 22 23 24 23 25 24 22
16E | 25 21 8 8 16 8 9 18 11 18 5 | 78 71 73 71 72 70 72 71 70 67 71
17 | 8 9 6 7 13 4 6 17 6 16 3 | 27 30 24 25 25 25 30 32 27 25 26
18E | 9 11 16 19 16 7 8 15 8 15 4 | 111 111 106 110 117 109 109 106 110 110 109
19 | 13 15 6 8 13 4 6 17 9 22 4 | 25 29 22 23 22 24 27 27 27 23 23
20 | 9 11 6 13 14 3 6 17 8 17 4 | 15 17 16 24 22 17 17 24 18 18 15
21E | 9 11 7 11 18 3 6 13 6 11 3 | 20 22 19 18 25 19 21 23 22 23 19
22 | 11 8 6 8 11 5 6 17 8 20 3 | 26 23 21 24 25 23 24 27 24 21 22
23 | 8 16 7 7 7 4 5 9 8 10 3 | 21 16 19 18 14 17 14 17 21 16 16
24 | 11 9 7 10 8 5 7 7 8 8 3 | 20 24 22 21 22 21 23 20 20 19 19
25E | 13 14 18 12 14 5 8 9 10 9 4 | 39 36 41 34 31 34 34 33 35 35 34
26E | 10 13 13 10 11 4 8 11 10 16 4 | 32 33 29 32 31 31 31 31 31 33 30
27 | 9 9 11 6 9 3 6 9 7 9 3 | 19 18 20 19 20 16 18 17 18 16 17
28E | 11 12 7 10 9 4 6 13 7 12 3 | 26 23 21 23 24 22 23 25 23 24 22
29 | 11 20 6 8 9 4 7 15 10 19 4 | 36 35 30 29 30 31 31 32 36 30 30
30 | 7 11 10 9 10 3 7 8 10 11 3 | 32 32 36 33 35 31 34 31 32 33 32
31 | 10 11 8 8 17 4 8 15 6 24 4 | 34 39 32 36 37 31 36 30 35 23 32
32 | 15 10 6 7 8 4 9 13 8 11 3 | 28 36 25 31 25 26 34 24 24 33 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 10 10 12 4 7 13 8 14 |T 30 31 30 31 30 29 30 30 30 29 29
WRMS | 10 12 9 10 11 4 7 13 7 13 |NE 23 26 23 25 23 23 25 23 24 22 23
MEDI | 9 11 8 10 11 4 7 13 8 12 |MD 26 29 25 28 25 24 27 27 26 24 25
Table 3.2060.1 GPS week: 2060 Day: 1 MJD: 58665.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 9 8 15 7 14 2 9 13 8 7 3 | 21 25 21 24 29 22 25 24 26 23 23
2E | 13 11 7 6 8 4 6 14 7 15 3 | 24 24 23 25 23 24 21 27 22 26 22
3 | 9 11 9 10 11 5 6 7 5 9 3 | 23 28 23 23 25 23 27 22 23 25 23
X4 | 3 --- --- --- --- 44 --- --- --- --- 0 | 34 --- --- --- --- 20 --- --- --- --- 34
5 | 7 9 9 8 11 3 7 10 10 16 3 | 25 29 24 28 27 25 29 26 27 21 25
6E | 14 12 14 12 12 4 7 13 6 7 4 | 26 28 22 30 26 24 27 31 27 26 25
7 | 7 9 9 11 13 3 7 14 7 18 3 | 31 34 31 36 32 31 32 33 32 31 31
8 | 10 9 11 8 11 3 7 8 5 8 3 | 21 22 21 22 22 18 22 18 19 17 20
9 | 11 11 5 12 7 4 10 7 6 11 3 | 19 33 23 17 18 21 34 22 23 29 24
10 | 7 8 11 10 12 3 6 9 5 11 3 | 22 25 26 24 27 23 25 23 25 27 23
11 | 10 7 10 7 13 2 6 10 7 11 3 | 27 30 33 28 28 28 31 29 27 25 28
12E | 10 16 8 10 12 3 9 16 8 15 4 | 26 22 23 19 27 24 22 30 23 28 22
13 | 9 7 7 11 9 4 6 11 7 14 3 | 18 21 19 31 16 20 20 22 17 19 19
14 | 9 7 9 7 6 3 7 8 6 12 2 | 22 17 20 24 17 19 15 20 20 18 18
15 | 11 8 6 8 9 2 9 11 9 15 3 | 20 21 20 25 20 19 23 23 22 21 20
16E | 7 21 9 7 12 6 8 20 9 16 4 | 26 28 26 27 26 26 24 34 28 27 25
17 | 9 10 8 9 14 3 7 14 6 14 3 | 23 27 20 25 22 21 27 27 24 21 22
18E | 11 11 13 26 12 5 8 15 9 20 5 | 104 109 103 112 104 106 108 107 107 106 106
19 | 9 14 6 8 12 3 7 16 8 20 3 | 20 26 21 23 20 21 26 23 25 17 21
20 | 8 11 9 8 15 2 7 15 7 18 3 | 18 19 18 22 24 18 18 23 18 21 17
21E | 9 13 6 14 35 4 8 12 5 12 4 | 15 18 18 25 41 17 18 23 20 25 18
22 | 11 7 7 8 11 4 6 17 6 19 3 | 29 28 25 28 27 26 28 29 27 23 25
23 | 10 18 9 7 6 5 8 10 7 11 3 | 20 16 21 22 15 18 15 18 19 20 17
24 | 9 9 8 11 10 4 8 7 7 9 3 | 17 25 22 21 22 20 25 20 20 23 20
25E | 12 13 17 18 13 4 7 9 8 9 4 | 36 32 39 34 31 32 31 32 36 31 32
26E | 8 11 13 13 13 4 8 15 10 9 4 | 32 35 34 30 33 31 32 36 32 32 32
27 | 9 10 9 8 9 4 7 9 8 8 3 | 23 20 20 24 21 18 20 19 21 16 20
28E | 15 13 8 10 10 4 8 12 9 13 3 | 23 22 21 24 25 19 22 24 24 24 21
29 | 10 18 5 9 9 3 8 17 9 18 4 | 32 27 25 26 27 26 25 27 31 28 26
30 | 8 8 9 8 11 3 7 7 8 10 3 | 31 31 32 31 29 29 31 28 30 28 30
31 | 8 10 8 7 18 4 7 15 8 22 4 | 32 37 33 36 35 31 36 32 32 29 32
32 | 8 10 6 5 9 4 9 11 8 13 3 | 20 32 21 25 18 20 32 16 18 30 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 9 10 13 4 8 12 7 14 |T 26 28 26 28 27 25 28 28 27 27 26
WRMS | 9 11 9 10 11 4 8 11 7 15 |NE 23 26 22 25 23 21 26 23 23 22 23
MEDI | 9 10 9 8 11 4 7 12 7 13 |MD 23 27 23 25 26 22 25 24 24 25 23
Table 3.2060.2 GPS week: 2060 Day: 2 MJD: 58666.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 10 14 10 13 3 8 11 7 8 3 | 24 25 22 27 28 22 25 23 22 24 23
2E | 9 12 7 12 10 4 6 14 5 12 3 | 19 23 22 15 20 18 21 26 22 23 19
3 | 7 7 9 6 10 4 5 6 6 9 2 | 19 22 19 20 22 18 23 17 19 20 19
X4 | 2 --- --- --- --- 57 --- --- --- --- 0 | 54 --- --- --- --- 33 --- --- --- --- 55
5M | 8 9 8 6 13 3 7 12 8 15 3 | 35 35 35 34 32 33 38 34 36 32 34
6E | 11 14 12 9 14 3 8 11 7 6 3 | 25 28 22 24 28 23 28 26 25 25 25
7M | 6 10 9 8 11 3 6 12 6 20 3 | 27 30 27 28 32 25 30 22 26 23 27
8 | 7 9 10 6 12 4 7 7 6 8 2 | 19 20 19 20 21 17 21 17 17 17 18
9 | 13 12 4 13 8 4 12 7 7 11 3 | 22 37 25 21 21 25 37 29 26 32 27
10 | 6 8 10 10 12 3 6 9 7 7 3 | 17 21 19 20 22 17 20 15 18 15 17
11M | 10 8 11 7 12 3 8 12 9 11 3 | 20 24 25 23 25 21 25 22 20 21 21
12E | 11 21 8 11 9 5 10 13 8 12 4 | 31 23 25 22 26 26 27 29 27 28 25
13 | 9 6 8 5 8 3 4 11 7 13 2 | 14 16 16 21 11 15 17 22 16 16 15
14 | 7 6 7 10 6 4 6 10 7 13 2 | 16 15 15 24 17 17 13 18 13 16 14
15 | 5 9 8 10 6 3 6 11 6 13 3 | 18 21 18 24 18 18 20 21 18 18 18
16E | 6 21 9 14 9 4 7 17 9 16 4 | 26 29 27 27 28 26 24 28 28 28 25
17 | 8 9 5 9 13 3 7 17 7 16 3 | 22 29 22 27 24 25 30 30 28 21 25
18E | 8 11 12 16 15 4 9 14 7 14 4 | 55 58 50 54 53 53 57 54 55 51 53
19 | 8 16 5 9 14 3 7 19 7 20 4 | 28 32 30 33 27 30 31 33 30 30 29
20M | 10 8 8 8 13 4 8 16 7 17 3 | 20 21 19 24 22 19 19 24 20 19 18
21E | 7 9 18 9 38 6 8 13 8 12 5 | 23 20 29 22 39 20 20 28 22 23 21
22 | 6 20 7 7 10 3 7 13 4 19 3 | 17 28 17 19 20 18 21 20 17 16 17
23M | 7 18 6 6 6 3 6 10 5 10 3 | 13 14 17 15 12 14 15 18 14 15 14
24 | 8 8 10 8 9 4 6 7 7 8 2 | 20 26 25 21 21 21 25 21 21 22 21
25E | 9 11 18 11 16 6 10 8 8 8 4 | 30 30 34 27 25 28 30 28 27 28 27
26E | 14 15 13 13 14 4 9 9 8 10 4 | 25 28 22 20 20 21 24 24 23 24 21
27 | 9 10 9 8 6 3 5 8 7 8 2 | 20 19 18 20 21 16 20 18 16 18 18
28E | 11 12 7 10 10 4 6 11 6 9 3 | 20 21 20 21 26 18 23 22 20 21 20
29 | 9 16 9 9 8 3 8 12 7 15 3 | 25 23 21 29 28 24 27 25 25 27 24
30M | 7 11 10 8 8 3 6 10 6 9 3 | 40 40 42 37 42 39 43 42 39 41 41
31 | 8 12 7 8 16 4 8 16 5 19 3 | 26 31 25 26 28 24 30 21 26 17 24
32 | 10 11 5 5 8 3 10 11 11 13 3 | 23 34 21 29 23 22 32 19 17 31 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 10 9 13 4 7 12 7 13 |T 24 26 24 24 25 23 26 25 23 23 24
WRMS | 8 12 10 10 11 4 7 10 7 13 |NE 23 25 20 22 21 21 24 22 21 20 23
MEDI | 8 11 9 9 10 3 7 11 7 12 |MD 22 25 22 24 24 21 25 23 22 23 21
Table 3.2060.3 GPS week: 2060 Day: 3 MJD: 58667.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 10 15 9 12 3 9 10 8 11 3 | 26 27 23 30 30 25 26 26 28 28 26
2E | 14 8 8 6 9 3 6 13 7 13 3 | 21 21 22 22 22 21 22 26 24 23 21
3 | 8 8 9 7 10 4 7 7 8 9 3 | 28 30 30 28 30 27 30 26 31 27 28
X4 | 4 --- --- --- --- 44 --- --- --- --- 0 | 33 --- --- --- --- 25 --- --- --- --- 34
5 | 10 9 8 7 8 4 7 11 12 16 3 | 36 37 33 38 40 36 38 34 40 27 35
6E | 12 13 13 13 12 4 9 10 10 10 4 | 24 28 22 29 25 24 28 27 26 27 24
7 | 10 11 9 8 10 3 7 17 9 19 3 | 50 53 53 53 54 51 53 52 54 49 52
8 | 6 9 11 8 11 3 5 7 6 13 3 | 22 24 22 25 26 22 24 23 23 23 22
9 | 11 12 6 8 7 4 12 7 8 11 3 | 29 43 32 31 29 32 41 34 30 35 32
10 | 7 7 13 8 15 2 5 9 5 10 3 | 26 30 30 28 33 27 29 28 29 33 28
11 | 10 8 11 7 13 3 7 9 7 13 3 | 24 29 27 29 27 26 29 28 28 26 26
12E | 10 20 9 8 9 3 10 17 11 15 4 | 28 27 26 29 32 27 27 30 28 31 27
13 | 7 6 8 5 6 3 7 9 9 12 2 | 22 20 22 25 21 22 23 25 24 22 22
14M | 10 6 8 8 6 3 7 9 7 12 3 | 25 19 21 27 21 21 21 22 18 22 20
15 | 10 10 8 7 8 3 7 11 6 15 3 | 26 28 26 34 30 27 30 29 28 25 27
16E | 9 25 11 16 10 4 7 19 9 15 4 | 38 40 40 39 39 39 37 40 41 38 38
17 | 9 12 7 8 11 3 8 15 8 16 3 | 26 30 27 31 30 28 31 31 31 27 28
18E | 9 12 14 12 15 5 11 14 11 18 4 | 129 130 125 132 130 130 130 131 131 132 129
19 | 10 15 6 8 9 4 8 17 9 21 4 | 22 27 25 29 26 25 28 28 26 26 24
20 | 8 14 11 11 17 4 4 14 7 17 4 | 26 29 27 30 33 27 29 32 29 29 27
21E | 9 9 9 8 18 5 7 14 5 16 3 | 19 23 21 21 29 21 20 26 24 24 20
22 | 7 10 6 6 12 4 7 15 7 16 3 | 27 29 26 28 28 26 28 27 29 24 26
23 | 10 21 7 6 7 3 6 9 6 11 3 | 25 24 26 27 23 25 23 25 27 24 24
24M | 9 9 8 9 12 5 11 10 10 7 3 | 109 113 109 111 107 114 118 113 114 113 112
25E | 11 10 18 15 12 4 10 12 11 11 4 | 32 33 39 36 31 32 33 36 34 34 32
26E | 11 11 12 13 11 3 7 12 10 10 4 | 28 33 29 27 31 27 29 30 30 27 28
27 | 8 12 10 10 5 3 6 8 7 12 3 | 25 25 23 27 27 23 24 23 23 26 24
28E | 14 14 9 14 11 4 8 11 7 12 4 | 25 22 23 29 30 22 24 25 24 28 24
29M | 9 19 7 7 11 4 8 13 9 14 3 | 26 23 20 25 25 22 25 24 22 25 22
30 | 9 11 9 6 8 2 8 6 6 10 3 | 35 38 40 37 40 37 41 39 39 39 38
31 | 8 10 7 6 15 4 8 17 8 20 4 | 33 39 34 36 35 33 37 32 35 30 33
32M | 8 13 5 9 8 3 11 11 7 13 3 | 25 37 22 24 25 25 35 24 25 34 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 10 9 11 4 8 12 8 14 |T 33 35 33 36 35 33 35 35 35 34 33
WRMS | 9 13 10 10 11 4 8 10 7 13 |NE 26 29 27 29 28 26 29 27 28 27 27
MEDI | 9 11 9 8 11 3 7 11 8 13 |MD 26 29 26 29 30 26 29 28 28 27 27
Table 3.2060.4 GPS week: 2060 Day: 4 MJD: 58668.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 7 11 15 7 13 3 8 9 7 10 3 | 31 35 31 32 36 30 33 31 31 32 32
2E | 13 10 8 10 13 5 6 12 12 14 3 | 26 27 27 27 34 26 26 28 31 27 26
3 | 8 9 10 7 14 3 6 5 5 7 2 | 25 31 28 26 35 26 30 24 26 24 27
X4 | 2 --- --- --- --- 62 --- --- --- --- 0 | 44 --- --- --- --- 76 --- --- --- --- 45
5 | 9 9 6 7 14 4 6 14 12 18 3 | 38 34 34 37 46 36 38 33 40 30 36
6E | 9 10 13 8 11 3 8 8 11 7 3 | 39 39 38 41 42 39 41 37 38 38 39
7 | 9 9 8 7 12 4 6 17 9 19 3 | 44 46 43 45 49 42 46 43 43 44 44
8 | 6 9 11 9 12 4 6 7 6 12 3 | 25 31 26 28 29 26 30 26 25 23 26
9 | 10 11 5 7 11 4 10 7 9 11 3 | 38 48 40 41 41 41 48 40 39 43 42
10 | 7 6 13 10 19 2 6 8 7 10 3 | 24 27 27 27 37 24 27 22 25 27 25
11 | 5 8 12 7 16 2 5 10 11 15 3 | 31 34 31 31 37 29 32 30 30 29 30
12E | 10 16 7 9 14 3 8 17 10 15 4 | 37 31 34 31 37 33 32 37 33 37 33
13 | 7 10 7 4 7 3 5 11 9 9 2 | 24 22 24 24 26 26 25 28 28 25 24
14 | 8 5 9 11 7 3 7 9 9 13 3 | 21 24 22 26 24 22 20 22 21 21 21
15 | 7 7 8 7 8 3 5 11 9 12 3 | 31 29 30 32 35 29 29 28 28 28 29
16E | 7 19 11 7 28 5 6 19 10 16 4 | 42 43 43 40 46 41 41 43 42 44 41
17 | 7 8 5 9 10 4 6 17 8 17 3 | 31 35 32 32 33 34 38 38 36 33 34
18E | 11 13 53 13 18 10 12 13 10 18 7 | 73 71 69 72 76 72 69 72 71 80 70
19 | 9 16 6 9 10 5 6 17 11 23 4 | 23 27 23 26 26 25 28 26 27 24 24
20 | 8 13 9 9 23 3 7 13 6 13 4 | 32 28 29 34 40 30 30 32 29 29 29
21E | 6 11 9 18 31 5 9 13 8 16 5 | 31 32 31 36 47 31 32 32 33 32 31
22 | 7 8 8 7 15 4 7 14 6 18 3 | 20 23 20 21 28 19 22 21 19 17 19
23 | 9 20 6 4 8 3 5 10 5 12 3 | 23 28 24 25 27 24 25 24 25 24 24
24 | 8 8 8 6 11 3 5 10 9 9 3 | 291 288 289 289 290 288 287 286 285 289 288
25E | 10 16 20 13 13 7 7 12 9 9 4 | 34 38 36 36 37 33 35 34 35 32 33
26E | 11 11 15 14 13 4 8 11 10 12 4 | 24 31 24 28 27 24 26 26 24 27 24
27 | 8 8 12 7 9 2 6 7 6 8 2 | 27 31 28 32 30 27 31 27 27 27 28
28E | 10 12 8 10 13 3 6 11 12 9 3 | 25 30 28 28 35 27 30 30 28 29 28
29 | 9 14 7 8 12 3 6 14 9 15 3 | 37 33 31 35 35 33 34 32 33 33 33
30 | 6 9 10 6 12 3 6 7 12 8 3 | 33 36 36 34 43 34 38 36 36 34 36
31 | 8 12 9 9 16 3 7 15 9 19 4 | 30 35 30 36 37 29 35 27 29 24 30
32 | 11 12 7 12 11 3 12 9 8 17 4 | 61 66 60 63 59 61 65 59 61 64 61
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 14 9 15 4 7 12 9 14 |T 41 43 40 42 45 41 42 41 41 40 41
WRMS | 8 12 11 9 13 4 7 11 8 13 |NE 28 30 28 29 32 31 31 27 28 26 29
MEDI | 8 10 9 8 13 3 6 11 9 13 |MD 31 32 31 32 37 30 32 31 31 29 30
Table 3.2060.5 GPS week: 2060 Day: 5 MJD: 58669.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 11 14 11 14 4 8 11 11 10 3 | 29 27 25 28 32 24 29 26 24 30 26
2E | 7 10 7 11 19 5 8 13 6 10 3 | 23 26 23 21 31 22 22 27 27 25 23
3 | 7 7 10 11 14 5 5 6 6 7 3 | 21 24 21 17 24 18 23 17 19 18 19
X4 | 2 --- --- --- --- 17 --- --- --- --- 0 | 30 --- --- --- --- 24 --- --- --- --- 31
5 | 8 8 7 6 13 4 7 12 10 16 3 | 27 27 25 23 26 24 30 25 28 22 25
6E | 8 15 11 8 15 4 7 12 6 10 3 | 33 36 36 33 41 33 37 36 35 37 34
7 | 7 10 9 7 12 4 6 18 9 19 3 | 55 58 56 57 59 56 58 59 55 59 57
8 | 5 10 10 7 14 4 7 7 7 9 3 | 17 21 20 17 22 16 20 18 18 18 18
9 | 8 11 4 11 12 4 10 7 7 12 3 | 26 36 28 21 22 25 36 26 26 33 27
10 | 8 8 13 8 20 4 7 11 10 11 3 | 21 24 26 21 28 21 23 20 26 26 22
11 | 7 8 12 8 30 3 6 11 10 10 4 | 23 24 26 21 39 21 25 21 20 22 22
12E | 10 17 8 12 16 4 9 18 9 17 4 | 35 29 30 26 38 31 29 36 28 35 29
13 | 8 9 8 5 10 3 6 10 8 10 3 | 18 18 20 17 19 19 19 24 18 17 17
14 | 9 7 9 6 7 2 4 13 5 15 3 | 18 14 13 16 18 15 14 19 16 14 13
15 | 10 9 7 7 11 4 7 13 7 16 3 | 18 20 17 21 20 18 21 21 17 23 18
16E | 12 23 9 11 17 4 6 16 10 14 4 | 25 28 26 27 26 27 24 30 32 27 24
17 | 8 10 5 10 16 3 7 17 7 18 3 | 23 28 25 28 27 25 28 30 30 26 25
18E | 11 13 17 18 23 8 14 14 10 23 5 | 140 142 152 147 147 143 145 142 147 147 144
19 | 10 15 7 10 14 5 7 17 10 23 4 | 22 26 22 21 23 20 24 23 25 20 21
20 | 8 12 10 10 24 5 6 14 10 14 4 | 21 27 24 26 30 24 26 27 29 29 24
21E | 9 9 7 6 34 7 7 12 9 10 4 | 27 26 27 25 45 25 26 28 25 29 26
22 | 9 7 6 5 17 4 6 14 7 21 3 | 18 17 13 17 25 15 17 17 14 15 13
23 | 6 18 8 6 9 4 6 9 6 12 3 | 15 15 18 18 16 16 12 16 17 18 14
24 | 10 8 8 8 11 4 6 9 8 8 3 | 446 451 449 448 450 449 449 451 452 450 449
25E | 9 11 19 13 14 6 8 15 8 8 4 | 28 29 32 28 29 28 29 29 26 28 26
26E | 9 10 15 10 16 4 7 8 7 8 3 | 22 24 20 20 18 18 20 21 21 22 19
27 | 8 8 11 7 14 3 6 7 7 7 3 | 18 19 19 19 20 16 20 18 17 16 17
28E | 8 14 7 6 18 4 7 12 6 12 3 | 21 22 23 22 34 21 25 24 24 25 22
29 | 9 17 6 6 17 4 7 14 9 15 3 | 28 27 23 25 26 23 25 23 22 25 23
30 | 8 8 8 5 15 3 7 6 10 8 3 | 27 29 31 26 31 26 30 28 26 29 28
31 | 10 13 9 7 17 4 6 16 8 19 4 | 26 28 21 27 20 21 25 21 23 17 22
32 | 11 14 6 11 9 4 11 12 7 15 3 | 74 79 76 75 78 75 81 74 75 78 75
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 10 9 17 4 7 13 8 14 |T 42 45 44 43 47 41 44 44 43 44 42
WRMS | 8 12 9 9 16 4 7 12 7 14 |NE 21 23 21 20 22 19 23 21 21 20 20
MEDI | 8 10 8 8 15 4 7 12 8 12 |MD 23 27 25 23 27 23 25 25 25 25 23
Table 3.2060.6 GPS week: 2060 Day: 6 MJD: 58670.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 14 18 10 13 2 9 9 5 8 3 | 32 35 31 34 39 31 32 30 31 31 32
2E | 11 10 7 9 15 4 6 13 9 10 3 | 45 42 43 44 42 44 43 42 44 45 43
3 | 7 8 11 9 14 3 6 6 7 6 3 | 33 36 37 32 37 34 35 32 36 33 33
X4 | 2 --- --- --- --- 71 --- --- --- --- 0 | 52 --- --- --- --- 37 --- --- --- --- 52
5 | 7 9 7 8 11 3 7 13 8 18 3 | 49 50 49 49 50 50 51 48 50 44 48
6E | 11 11 11 14 17 4 9 12 9 8 4 | 35 36 32 33 32 33 35 34 33 35 33
7 | 6 10 8 8 9 3 5 16 6 17 3 | 82 83 81 82 83 80 82 81 84 79 81
8 | 7 9 12 7 13 2 7 6 7 9 3 | 27 27 28 27 30 25 29 25 26 24 26
9 | 11 12 6 9 10 4 11 6 7 12 3 | 33 44 36 30 33 35 43 34 35 39 35
10 | 6 8 15 10 19 3 8 13 6 12 3 | 34 39 42 38 39 38 38 35 39 36 36
11 | 7 6 14 9 15 2 6 10 7 11 3 | 33 36 37 31 33 32 35 33 31 32 32
12E | 7 17 9 9 10 3 10 16 7 14 4 | 26 25 26 22 24 25 24 31 26 31 24
13 | 7 5 8 11 8 3 6 13 8 9 3 | 30 33 32 27 28 30 31 37 30 30 29
14 | 8 7 9 14 6 3 9 10 10 14 3 | 28 25 26 34 25 26 22 27 27 24 24
15 | 9 11 7 6 10 3 6 12 7 13 3 | 31 35 30 31 31 30 32 32 29 31 30
16E | 9 26 10 11 16 3 7 19 9 18 5 | 31 36 33 30 30 30 30 34 33 30 29
17 | 7 10 7 9 14 3 7 16 7 17 3 | 29 34 29 32 31 30 33 37 31 30 30
18E | 6 14 17 22 17 4 10 14 9 18 5 | 102 109 108 102 102 104 106 107 105 107 104
19 | 9 14 6 9 14 4 6 18 7 23 4 | 28 35 28 29 26 28 31 30 27 27 27
20 | 8 12 10 11 21 4 7 16 9 17 4 | 35 37 37 37 35 36 36 38 34 38 33
21E | 8 9 7 11 19 5 10 14 8 17 4 | 31 31 31 31 38 31 31 36 30 32 30
22 | 7 8 8 6 17 3 6 12 10 17 3 | 30 30 30 30 37 29 29 28 31 21 27
23 | 7 20 7 7 9 4 7 10 6 9 3 | 22 24 25 26 24 24 20 23 26 22 22
24 | 10 7 8 6 10 3 7 10 8 9 3 | 615 612 613 615 615 614 614 612 615 614 614
25E | 10 16 21 19 13 4 12 10 8 9 4 | 45 47 50 47 42 45 46 45 45 43 44
26E | 11 12 16 13 18 4 9 14 10 10 4 | 44 46 41 41 41 41 41 39 42 41 40
27 | 7 11 12 7 13 2 8 7 5 7 3 | 25 27 25 26 25 24 27 24 24 26 25
28E | 12 16 8 6 13 4 6 11 8 10 3 | 27 29 26 24 27 24 28 28 25 28 25
29 | 8 19 7 8 12 4 8 15 7 16 4 | 28 29 25 30 27 27 29 26 25 28 26
30 | 6 10 9 5 12 4 5 7 4 6 2 | 64 64 66 64 64 64 66 63 64 65 64
31 | 7 10 8 7 15 4 8 16 9 20 3 | 40 46 41 43 39 38 43 36 38 33 38
32 | 8 10 7 7 8 4 9 13 10 15 3 | 92 96 92 94 90 92 95 93 92 98 93
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 11 10 14 3 8 13 8 14 |T 58 60 59 58 58 57 59 58 58 57 57
WRMS | 8 13 11 10 14 3 8 11 7 13 |NE 32 35 32 31 32 31 33 31 31 30 32
MEDI | 7 10 8 9 13 3 7 13 8 12 |MD 33 36 33 32 35 32 35 34 33 32 32
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 4.2060 GPS week: 2060 MJD: 58664.0-58670.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 |U 13 14 31 |U 8 10 26 |U 12 12 31 |
emr | emr 2972 |U 21 13 50 |U 11 15 34 |U 14 12 43 |
esa | esa 2976 | 15 10 30 |U 7 11 24 | 13 12 26 |
gfz | gfz 2972 |U 13 14 34 |U 7 11 28 |U 12 12 31 |
grg | grg 2973 |U 15 17 33 |U 9 16 40 | 13 14 34 |
igr | igr 2934 | 14 12 32 | 7 10 22 | 12 12 30 |
igs | igs 2917 | 14 13 36 | 7 11 25 | 12 12 29 |
jpl | jpl 2976 |U 16 15 51 |U 8 13 36 |U 13 13 34 |
mit | mit 2976 | 15 15 37 |U 9 12 33 |U 15 17 36 |
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 5.2060.0 GPS week: 2060 Day: 0 MJD: 58664.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 12 11 34 | 8 9 28 | 13 14 36 |
emr | emr 2972 | 18 10 55 | 9 12 40 | 13 10 45 |
esa | esa 2976 | 13 10 35 | 7 11 27 | 12 13 29 |
gfz | gfz 2972 | 12 12 37 | 7 11 32 | 12 12 36 |
grg | grg 2976 | 14 14 38 | 7 15 51 | 12 13 37 |
igr | igr 2971 | 13 10 35 | 7 9 26 | 11 13 34 |
igs | igs 2880 | 14 11 38 | 6 9 30 | 11 12 35 |
jpl | jpl 2976 | 18 14 53 | 8 12 46 | 13 13 43 |
mit | mit 2976 | 12 11 35 | 8 10 35 | 12 14 36 |
Table 5.2060.1 GPS week: 2060 Day: 1 MJD: 58665.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 12 18 28 | 8 11 28 | 12 11 30 |
emr | emr 2972 | 20 15 44 | 12 14 36 | 13 11 29 |
esa | esa 2976 | 13 14 28 | 8 11 24 | 12 13 19 |
gfz | gfz 2973 | 12 19 29 | 7 13 29 | 12 11 28 |
grg | grg 2976 | 14 23 34 | 10 22 40 | 13 19 35 |
igr | igr 2930 | 12 16 29 | 8 10 26 | 12 13 27 |
igs | igs 2976 | 13 18 33 | 8 12 25 | 12 11 23 |
jpl | jpl 2976 | 16 21 46 | 8 12 37 | 13 13 23 |
mit | mit 2976 | 13 19 37 | 11 14 40 | 18 29 36 |
Table 5.2060.2 GPS week: 2060 Day: 2 MJD: 58666.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 11 14 24 | 7 11 26 | 10 11 27 |
emr | emr 2972 | 21 16 51 | 17 15 37 | 15 15 52 |
esa | esa 2976 | 12 10 28 | 6 11 30 | 11 11 26 |
gfz | gfz 2971 | 12 16 28 | 7 12 33 | 11 11 30 |
grg | grg 2976 | 12 18 23 | 9 13 41 | 12 14 33 |
igr | igr 2784 | 13 11 25 | 6 12 21 | 11 13 27 |
igs | igs 2865 | 12 15 30 | 6 12 28 | 11 12 27 |
jpl | jpl 2976 | 15 16 51 | 8 12 42 | 13 14 37 |
mit | mit 2976 | 11 16 29 | 8 12 32 | 10 13 32 |
Table 5.2060.3 GPS week: 2060 Day: 3 MJD: 58667.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 10 13 33 | 8 9 27 | 13 12 33 |
emr | emr 2972 | 17 14 49 | 13 17 31 | 16 13 50 |
esa | esa 2976 | 12 7 28 | 6 11 22 | 14 11 25 |
gfz | gfz 2972 | 12 13 35 | 7 10 25 | 14 13 34 |
grg | grg 2969 | 13 16 36 | 8 15 34 | 15 14 35 |
igr | igr 2956 | 11 11 34 | 7 9 20 | 13 11 31 |
igs | igs 2880 | 11 11 36 | 7 9 25 | 14 12 34 |
jpl | jpl 2976 | 13 11 55 | 7 11 31 | 15 11 36 |
mit | mit 2976 | 10 13 35 | 9 13 34 | 14 16 38 |
Table 5.2060.4 GPS week: 2060 Day: 4 MJD: 58668.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 12 12 29 | 9 11 27 | 13 9 29 |
emr | emr 2972 | 20 11 48 | 11 16 29 | 15 12 45 |
esa | esa 2976 | 15 7 26 | 8 12 22 | 14 11 28 |
gfz | gfz 2973 | 13 12 35 | 8 11 28 | 14 9 28 |
grg | grg 2976 | 15 15 32 | 10 19 46 | 14 9 31 |
igr | igr 2949 | 13 10 31 | 8 11 22 | 13 8 29 |
igs | igs 2966 | 14 10 35 | 8 12 23 | 13 9 29 |
jpl | jpl 2976 | 16 12 49 | 9 14 30 | 13 10 34 |
mit | mit 2976 | 21 18 43 | 10 15 36 | 17 12 37 |
Table 5.2060.5 GPS week: 2060 Day: 5 MJD: 58669.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 12 12 29 | 9 9 27 | 12 14 31 |
emr | emr 2975 | 21 13 45 | 9 12 35 | 13 15 41 |
esa | esa 2976 | 13 10 26 | 7 14 21 | 12 14 26 |
gfz | gfz 2972 | 11 11 32 | 8 9 28 | 12 14 30 |
grg | grg 2969 | 14 14 30 | 10 17 30 | 13 17 35 |
igr | igr 2975 | 13 10 30 | 7 9 22 | 12 14 30 |
igs | igs 2880 | 12 11 33 | 8 10 25 | 12 14 31 |
jpl | jpl 2976 | 13 11 46 | 7 15 33 | 12 18 38 |
mit | mit 2976 | 14 10 35 | 9 11 26 | 19 24 43 |
Table 5.2060.6 GPS week: 2060 Day: 6 MJD: 58670.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3060 | 22 17 41 | 8 10 19 | 13 12 31 |
emr | emr 2975 | 28 15 57 | 10 15 30 | 15 12 38 |
esa | esa 2976 | 24 12 42 | 6 11 24 | 13 13 24 |
gfz | gfz 2972 | 21 15 44 | 6 8 23 | 13 11 29 |
grg | grg 2973 | 22 16 39 | 9 12 40 | 13 14 35 |
igr | igr 2973 | 23 14 44 | 6 9 18 | 12 11 28 |
igs | igs 2976 | 24 15 47 | 6 10 22 | 13 12 27 |
jpl | jpl 2976 | 24 16 59 | 6 15 33 | 13 15 29 |
mit | mit 2976 | 23 22 47 | 9 9 30 | 14 13 31 |
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 6.2060 GPS week: 2060 MJD: 58664.500-58670.500
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 | -27 -11 20 11 -2 | 18 23
| 15 17 46 101 4 | 2
emr uuuuu | 19 38 -8 -39 -3 | 23 28
| 20 25 137 42 9 | 3
esa uuuuu | -8 33 56 -84 -1 | 16 22
| 14 11 66 86 8 | 2
gfz uuuuu | -6 32 -67 15 4 | 16 20
| 20 21 156 87 8 | 3
grg uuuuu | 1 -24 21 11 -4 | 0 14
| 21 19 62 38 5 | 2
igr xxxxx | 28 18 62 -33 -3 | 5 14
| 7 11 36 31 4 | 2
irf xxxxx | 11 -19 -9 -52 3 | 0 15
| 10 10 19 16 4 | 2
jpl uuuuu | 18 -30 87 89 2 | 28 31
| 21 13 48 39 5 | 2
mit uuuuu | 12 6 -49 -143 5 | 20 25
| 19 8 37 34 4 | 2
ngs uuuuu | -25 -25 -4 31 2 | 16 22
| 53 22 187 77 5 | 2
sio uuuux | 32 10 -198 9 3 | 37 40
| 28 21 83 56 5 | 2
Table 7.2060.0 GPS week: 2060 Day: 0 MJD: 58664.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -42 -33 -4 4 -1 | 19 22
emr uuuuu | -5 74 -139 -41 -9 | 27 30
esa uuuuu | 8 35 -36 -48 12 | 13 18
gfz uuuuu | -27 36 -263 -94 12 | 12 16
grg uuuuu | 33 -17 26 81 -15 | 3 12
igr xxxxx | 24 3 18 -36 4 | 4 11
irf xxxxx | -2 -38 -2 -66 -1 | 0 13
jpl uuuuu | -21 -44 104 56 -3 | 30 33
mit uuuuu | -9 0 22 -122 0 | 20 23
ngs uuuuu | 35 2 181 74 11 | 14 19
sio uuuux | 38 -27 -91 6 3 | 37 39
Table 7.2060.1 GPS week: 2060 Day: 1 MJD: 58665.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -42 -25 -31 -51 -4 | 18 22
emr uuuuu | -2 33 -28 -70 -17 | 26 29
esa uuuuu | 2 33 18 -67 6 | 14 19
gfz uuuuu | -36 65 -286 11 7 | 14 17
grg uuuuu | 3 2 -41 -38 -5 | 1 12
igr xxxxx | 27 35 26 -40 -6 | 5 11
irf xxxxx | 5 -24 -39 -64 4 | -1 13
jpl uuuuu | 22 -49 152 45 -3 | 27 30
mit uuuuu | -2 -8 -65 -82 5 | 19 22
ngs uuuuu | 30 -31 196 154 5 | 15 20
sio uuuux | 3 31 -208 -63 2 | 36 39
Table 7.2060.2 GPS week: 2060 Day: 2 MJD: 58666.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -25 -16 75 -25 -6 | 17 21
emr uuuuu | 11 71 -195 -40 -1 | 23 25
esa uuuuu | -37 47 5 -185 0 | 15 20
gfz uuuuu | 1 52 -82 -3 7 | 14 18
grg uuuuu | 6 -8 -38 10 -3 | 0 11
igr xxxxx | 24 14 81 -95 -1 | 4 10
irf xxxxx | 15 -7 -15 -59 3 | -2 11
jpl uuuuu | 26 -23 22 153 6 | 26 28
mit uuuuu | 4 4 -23 -143 2 | 18 21
ngs uuuuu | -13 -69 182 59 1 | 15 20
sio uuuux | 45 18 -196 59 -1 | 35 37
Table 7.2060.3 GPS week: 2060 Day: 3 MJD: 58667.500
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 14 -23 233 -4 | 20 23
emr uuuuu | 54 7 194 -82 -11 | 26 28
esa uuuuu | -11 31 71 -136 -12 | 19 22
gfz uuuuu | -13 3 10 57 14 | 18 21
grg uuuuu | -19 -43 -25 -11 0 | 3 11
igr xxxxx | 17 13 41 -26 -2 | 8 12
irf xxxxx | 25 -17 -27 -64 2 | 2 12
jpl uuuuu | 20 -15 143 56 7 | 28 31
mit uuuuu | 18 12 -70 -185 6 | 22 24
ngs uuuuu | -52 -18 -81 -66 -1 | 19 22
sio uuuux | 41 25 -360 92 7 | 39 40
Table 7.2060.4 GPS week: 2060 Day: 4 MJD: 58668.500
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 | -17 -17 68 -64 -6 | 16 23
emr uuuuu | 27 27 121 -76 0 | 20 27
esa uuuuu | -9 25 144 -179 -6 | 15 23
gfz uuuuu | 3 22 3 147 1 | 15 21
grg uuuuu | -14 -19 18 7 -5 | -2 15
igr xxxxx | 28 18 60 -6 -3 | 3 15
irf xxxxx | 13 -19 2 -53 10 | -3 16
jpl uuuuu | 36 -17 66 110 8 | 24 29
mit uuuuu | 28 9 -55 -136 12 | 18 23
ngs uuuuu | -104 -14 -221 57 5 | 14 22
sio uuuux | 72 -10 -197 -5 10 | 35 37
Table 7.2060.5 GPS week: 2060 Day: 5 MJD: 58669.500
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 | -32 -14 61 -16 0 | 16 23
emr uuuuu | 21 35 27 13 5 | 20 27
esa uuuuu | -7 45 56 -20 -6 | 16 24
gfz uuuuu | 16 22 138 75 -6 | 17 23
grg uuuuu | -23 -48 114 -8 1 | -2 15
igr xxxxx | 37 30 109 -28 -4 | 4 16
irf xxxxx | 15 -19 16 -28 4 | -1 17
jpl uuuuu | 40 -25 65 94 0 | 27 31
mit uuuuu | 45 9 -88 -155 6 | 20 26
ngs uuuuu | -76 -31 -213 -34 0 | 16 24
sio uuuux | 37 8 -194 -54 -2 | 36 40
Table 7.2060.6 GPS week: 2060 Day: 6 MJD: 58670.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -34 10 -5 -1 5 | 18 28
emr uuuuu | 25 18 -38 22 9 | 23 32
esa uuuuu | -4 15 131 45 -3 | 19 28
gfz uuuuu | 14 25 14 -87 -4 | 21 28
grg uuuuu | 21 -37 90 38 0 | 1 20
igr xxxxx | 39 11 102 -2 -9 | 7 20
irf xxxxx | 2 -13 1 -32 -3 | 3 22
jpl uuuuu | 5 -35 59 107 -3 | 30 37
mit uuuuu | 2 17 -65 -174 1 | 24 32
ngs uuuuu | 3 -18 -70 -26 -4 | 19 29
sio uuuux | -10 26 -137 30 2 | 40 45
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