[IGSREPORT-26720] Wk 2062 IGS Final Orbits
acc
acc at igs.org
Fri Aug 2 04:23:35 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2062 (Jul 14, 2019 - Jul 20, 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:
igs2062[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2062[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2062[0-6].cls IGS GPS clock combination summary report.
igs20627.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20627.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 18 NRMD PTBB TIXI WES2 KIT3 NRMD TIXI WES2
0 | EMR | GOL2 PTBB
0 | ESA | AREG CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB
0 | ESA | HERS HOB2 IISC KIRU KOUR MAL2 MAR6 MAS1 MAW1 MGUE
0 | ESA | MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL AREG CEDU
0 | ESA | COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2
0 | ESA | IISC KIRU KOUR MAL2 MAR6 MAS1 MAW1 MGUE MOBS NAUR
0 | ESA | NNOR ONSA POHN PTBB TOW2 VILL
0 | GFZ | 18 18 22 POHN POHN
0 | GRG | 16 LPGS LPGS
0 | MIT | HRAO
1 | COD | 18 PDEL TIXI PDEL TIXI
1 | EMR | 25 25 HOB2 NLIB PTBB
1 | ESA | AREG CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB
1 | ESA | HERS HOB2 IISC KIRU MAJU MAL2 MAR6 MAS1 MAW1 MGUE
1 | ESA | MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL AREG CEDU
1 | ESA | COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2
1 | ESA | IISC IRKJ KIRU MAJU MAL2 MAR6 MAS1 MAW1 MGUE MOBS
1 | ESA | NAUR NNOR ONSA POHN PTBB TOW2 VILL
1 | GFZ | GODE PDEL POHN GODE PDEL POHN
1 | GRG | BAKE KIT3 BAKE KIT3
1 | JPL | REUN
2 | COD | 18 18 INEG KIT3 LHAZ NRIL TIXI KIT3 TIXI WES2
2 | EMR | PTBB
2 | ESA | 18 18 AREG CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB
2 | ESA | HERS HOB2 IISC INEG KIRU LAUT MAJU MAL2 MAR6 MAS1
2 | ESA | MAW1 MGUE MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL
2 | ESA | AREG CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB HERS
2 | ESA | HOB2 IISC INEG KIRU LAUT MAJU MAL2 MAR6 MAS1 MAW1
2 | ESA | MGUE MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL
2 | GFZ | 22 19 20 21 22 BARH FLRS POHN BARH CEDU DGAR FLRS
2 | GFZ | GODE POHN
2 | GRG | NKLG NKLG
3 | COD | BJFS QAQ1 TIXI TIXI
3 | EMR | PTBB PTBB QAQ1
3 | ESA | 18 18 AREG BAKE CEDU COCO DARW DAV1 DGAR FAA1 GRAZ
3 | ESA | HARB HERS HOB2 IISC KIRU MAJU MAR6 MAS1 MAW1 MGUE
3 | ESA | MOBS NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL WIND
3 | ESA | AREG BAKE CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB
3 | ESA | HERS HOB2 IISC KIRU MAJU MAR6 MAS1 MAW1 MGUE MOBS
3 | ESA | NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL WIND
3 | GFZ | 18 22 18 19 22 GODE POHN RBAY SUTH GLSV GODE LHAZ
3 | GFZ | POHN RBAY SUTH
3 | GRG | BJFS
4 | COD | 18 18 BRST GLPS TIXI WES2 BRST TIXI WES2
4 | EMR | TSKB
4 | ESA | 18 18 CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB
4 | ESA | HERS HOB2 IISC KIRU MAJU MAR6 MAS1 MAW1 MGUE MOBS
4 | ESA | NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL CEDU COCO
4 | ESA | DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2 IISC
4 | ESA | KIRU MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR ONSA
4 | ESA | POHN PTBB TONG TOW2 VILL
4 | GFZ | 6 19 20 21 22 DAV1 GLPS POHN DAV1 GLPS GODE POHN
4 | GFZ | STJO
4 | GRG | DAV1 GLPS GLSV NRMD DAV1 GLPS GLSV NRMD
4 | JPL | GLPS
5 | COD | 6 TIXI TIXI
5 | EMR | 18 CEDU CEDU STJO
5 | ESA | CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS
5 | ESA | HOB2 IISC KIRU KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS
5 | ESA | NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL CEDU COCO
5 | ESA | DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2 IISC
5 | ESA | KIRU KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR
5 | ESA | ONSA POHN PTBB TONG TOW2 VILL
5 | GFZ | GODE POHN GODE POHN
5 | JPL | NYAL NYAL
6 | COD | 12 12 IRKJ TIXI TIXI
6 | ESA | 18 18 ANKR AREG CEDU COCO DARW DAV1 DGAR FAA1 FALK
6 | ESA | GRAZ HARB HERS HOB2 IISC KIRU KOUR MAJU MAR6 MAS1
6 | ESA | MAW1 MGUE MOBS NAUR NNOR ONSA POHN PTBB REUN TOW2
6 | ESA | VILL AREG CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ
6 | ESA | HARB HERS HOB2 KIRU KOUR MAJU MAR6 MAS1 MAW1 MGUE
6 | ESA | MOBS NAUR NNOR ONSA POHN PTBB REUN TOW2 VILL
6 | GFZ | 18 IISC POHN POHN
6 | MIT | 18
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | GFZ | ~08:30 | ~ -0.11 ns
1 | GFZ | ~04:00 | ~ 0.10 ns
6. 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.
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
1 | GFZ | 26
2 | GFZ | 25 26
3 | GFZ | 26
3 | NGS | 30
4 | GFZ | 26
5 | GFZ | 26
5 | NGS | 6
6 | COD | 4
6 | GFZ | 26
8. 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 G04 | | | | | 4 | 4 | 4 |
9. 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.
10. 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 .2 1.2 16 15 -20 -.51
EMR | 0 | 1.3 3.8 -9.6 -31 56 -28 -.03
ESA | 0 | .5 -.6 -.3 10 22 31 -.52
GFZ | 0 | .1 1.1 1.2 47 11 13 -.66
GRG | 0 | .5 -2.2 5.2 83 -15 136 -.17
JPL | 0 | 1.3 -4.1 -6.0 2 5 -1 -.66
MIT | 0 | -3.6 -8.7 .4 -5 66 -13 -.10
NGS | 0 | -7.4 -4.9 1.9 8 86 -38 -.16
SIO | 0 | -6.2 -8.1 -3.5 -12 2 -2 -.24
COD | 1 | .2 -.3 .6 10 14 -14 -.54
EMR | 1 | .4 -1.3 -6.5 -22 57 -57 -.17
ESA | 1 | .5 -.7 -.2 13 15 50 -.55
GFZ | 1 | -.0 .9 .9 45 12 12 -.70
GRG | 1 | -.7 -3.5 .9 66 -9 127 -.45
JPL | 1 | -3.9 -3.7 -1.8 6 12 -9 -.39
MIT | 1 | -6.0 -7.2 -1.4 -12 53 -21 -.14
NGS | 1 | -4.1 -1.8 4.5 5 67 -34 -.44
SIO | 1 | -4.0 -8.9 -6.7 -17 -5 -2 -.26
COD | 2 | .4 -.4 .4 8 8 -10 -.55
EMR | 2 | 6.4 -1.9 -8.3 -33 49 -56 -.33
ESA | 2 | .9 -1.2 -.3 8 33 72 -.57
GFZ | 2 | .1 .9 1.0 51 20 15 -.54
GRG | 2 | .7 -6.7 -9.0 76 -56 146 -.61
JPL | 2 | 7.4 -8.2 -7.8 8 -3 -2 -.25
MIT | 2 | -2.1 -6.3 -5.6 -2 84 4 -.19
NGS | 2 | 2.1 -.7 .3 18 61 3 -.47
SIO | 2 | -.3 -2.8 -9.3 -17 4 11 -.31
COD | 3 | .1 -.0 1.3 15 26 -2 -.65
EMR | 3 | 6.3 -.6 -5.9 -51 10 -20 -.32
ESA | 3 | 1.0 -.5 -.0 11 24 53 -.60
GFZ | 3 | .0 .6 .8 45 25 24 -.52
GRG | 3 | .1 -4.5 3.6 73 -54 152 -.47
JPL | 3 | -2.2 -5.5 -5.7 7 3 -10 -.69
MIT | 3 | -.9 -5.3 -1.7 -7 59 -18 -.21
NGS | 3 | -.5 -3.8 2.2 10 63 -21 -.43
SIO | 3 | .5 -6.1 -1.5 -13 4 16 -.29
COD | 4 | -.0 -.4 1.2 12 26 5 -.68
EMR | 4 | -.7 .9 -7.0 -27 59 -25 -.50
ESA | 4 | .4 -.5 -.2 17 46 39 -.70
GFZ | 4 | -.1 1.1 1.1 57 23 22 -.58
GRG | 4 | -1.3 -2.1 3.0 83 -33 134 -.53
JPL | 4 | 1.7 -7.1 -3.2 7 5 -19 -.67
MIT | 4 | -2.1 -8.5 .8 -11 83 -2 -.36
NGS | 4 | -2.3 -2.6 -5.2 48 57 -1 -.38
SIO | 4 | -4.3 -6.7 -1.7 -5 9 -4 -.44
COD | 5 | -.0 .2 1.7 16 26 -6 -.61
EMR | 5 | 2.0 -2.6 -2.0 -33 42 -15 -.25
ESA | 5 | .4 -.9 -.3 15 48 40 -.58
GFZ | 5 | -.2 1.3 .9 64 24 16 -.53
GRG | 5 | -.5 -6.6 .2 67 -34 179 -.51
JPL | 5 | .5 -9.3 1.2 24 11 -33 -.48
MIT | 5 | -1.8 -6.0 3.4 -14 74 -13 -.25
NGS | 5 | -10.4 -7.1 6.9 -14 77 -45 -.38
SIO | 5 | -3.8 -6.3 8.6 -26 9 21 -.37
COD | 6 | .3 .4 1.3 14 14 -11 -.67
EMR | 6 | .1 -2.5 -1.2 -32 49 -37 -.25
ESA | 6 | .6 -1.0 -.7 7 28 27 -.72
GFZ | 6 | .3 .7 .7 37 8 13 -.56
GRG | 6 | .4 .9 1.0 69 -14 135 -.48
JPL | 6 | -.6 -8.6 1.0 16 -6 -2 -.41
MIT | 6 | -2.0 -2.4 3.5 -5 76 -31 -.33
NGS | 6 | -7.7 -6.1 6.4 -19 73 -50 -.32
SIO | 6 | -2.5 -2.4 .9 0 -1 10 -.32
11. 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.
12. 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 1.2062.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2062.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 2.2062.[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 3.2062.[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 5.2062.0-6). 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 2062 summary. (Jul 14, 2019 - Jul 20, 2019)
Table 1.2062.a GPS week: 2062 MJD: 58678.000-58684.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 1 0 2 20 16 -19 -.03 9 9 | -473 -191 6 85
| 0 1 2 14 19 10 .04 | 126 219
emr 79| -1 0 0 -11 -3 12 .10 11 11 | 136643 -1 16 86
| 1 0 1 5 6 12 .03 | 523 559
esa 149| 0 0 -3 -4 -2 -6 -.10 10 10 | 2321 -131 8 114
| 0 0 1 13 10 7 .03 | 2619 1066
gfz 182| 0 0 2 -14 2 -12 .02 17 11 | -303 101 16 211
| 0 0 1 10 9 9 .03 | 339 502
grg 98| 3 0 0 -12 -1 24 -.09 13 12 | 28 -132 10 137
| 0 0 4 8 13 40 .02 | 176 322
igr n/a| 0 0 0 -20 -32 -8 -.06 4 4 | -18288 28 11 75
| 0 0 0 9 10 15 .01 | 522 569
jpl 80| 0 0 -1 12 -9 18 .12 7 7 | 201072 -132 9 87
| 0 1 1 19 12 18 .02 | 28442 609
mit 348| 0 -1 0 -8 0 12 -.02 13 11 | -598 -36 112 1792
| 0 1 0 31 30 23 .02 | 489 339
ngs 211| 0 0 0 8 4 -6 -.07 8 7 | -19317 112231 1021 2200
| 0 0 1 16 11 13 .02 | 55586 302387
sio 319| 0 -2 0 -4 -18 -1 -.02 14 14 | --- --- --- ---
| 0 1 1 27 32 24 .03 | --- ---
Table 1.2062.b GPS week : 2062 MJD: 58678.000-58684.000
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 3 3 4 3 |
2 | 4 4 4 4 4 3 4 |
3 | 3 3 4 3 4 4 4 |
4 | --- --- --- --- 0 0 0 |
5 | 3 3 3 3 4 4 4 |
6 | 4 4 4 4 4 9 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 4 4 4 4 4 4 4 |
11 | 3 4 3 3 4 4 4 |
12 | 5 5 4 4 4 5 4 |
13 | 3 3 3 3 3 3 3 |
14 | 3 3 3 3 3 3 4 |
15 | 3 3 3 3 3 3 4 |
16 | 5 5 4 5 5 5 6 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 3 3 4 4 4 |
19 | 4 5 5 4 4 5 5 |
20 | 4 4 4 4 4 4 5 |
21 | 4 4 3 4 4 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 3 4 0 4 |
24 | 3 3 3 3 3 3 3 |
25 | 10 14 6 5 5 5 6 |
26 | 8 5 5 5 5 5 5 |
27 | 3 3 3 3 3 3 3 |
28 | 4 4 3 4 3 4 4 |
29 | 5 4 4 4 4 4 4 |
30 | 3 3 3 7 4 3 3 |
31 | 4 4 4 5 4 4 4 |
32 | 4 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 2.2062.0 GPS week: 2062 Day: 0 MJD: 58678.000
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| 0 0 2 10 0 -25 .01 8 8 | -328 -463 6 79
emr 80| -2 1 0 -17 -4 35 .12 12 12 | 136573 -655 18 94
esa 150| 0 0 -4 -19 -17 -8 -.13 10 10 | -1057 156 8 115
gfz 182| 0 1 0 -18 -8 -7 -.01 12 10 | -264 -54 13 213
grg 100| 4 0 5 4 11 -55 -.10 14 13 | -249 306 9 152
igr n/a| 0 0 0 -15 -32 -28 -.08 4 4 | -18360 -659 11 72
jpl 80| 0 2 -1 27 -13 10 .11 8 8 | 212269 -757 9 77
mit 349| 0 -2 0 -31 20 43 .00 13 12 | -825 -239 146 1885
ngs 210| 0 0 1 34 25 9 -.04 8 7 | -436 -276 686 2364
sio 322| -1 -4 -2 -37 -5 23 -.09 15 15 | --- --- --- ---
Table 2.2062.1 GPS week: 2062 Day: 1 MJD: 58679.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| 1 2 4 25 22 0 -.03 9 8 | -536 7 6 82
emr 80| -3 0 0 -7 5 4 .07 12 12 | 136073 -635 16 81
esa 150| 0 0 -4 -15 -15 -6 -.09 9 9 | 4104 -1271 8 104
gfz 184| 0 0 0 -20 15 -8 .08 16 10 | 192 -852 13 221
grg 100| 4 0 4 -12 18 2 -.11 13 12 | 207 -720 8 121
igr n/a| 0 1 0 -34 -24 13 -.06 4 4 | -18883 -653 11 70
jpl 80| -1 0 -3 19 -14 32 .12 8 8 | 211656 -905 10 98
mit 349| 0 -1 0 14 -42 -18 -.00 13 12 | -158 -578 52 1687
ngs 211| 0 0 1 -8 10 1 -.09 8 7 | -543 -18 1072 2018
sio 321| 0 -2 0 20 -37 3 -.01 15 15 | --- --- --- ---
Table 2.2062.2 GPS week: 2062 Day: 2 MJD: 58680.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| 0 0 6 15 20 -24 -.11 8 8 | -426 -302 6 81
emr 79| -3 0 -2 -9 -12 20 .17 12 12 | 136006 744 15 83
esa 150| 0 0 0 -12 13 7 -.04 9 9 | 4255 -1085 6 94
gfz 185| -1 1 2 0 8 -12 -.00 20 10 | -347 18 14 180
grg 99| 2 0 -7 -22 -18 30 -.08 11 11 | -57 -51 11 122
igr n/a| 0 0 0 -19 -36 -8 -.05 4 4 | -18905 731 11 76
jpl 80| 0 1 -1 13 -9 -9 .14 8 8 | 211298 533 9 101
mit 349| 0 -2 -1 2 -7 37 -.01 12 11 | -1177 246 84 1806
ngs 215| 1 0 0 7 6 -7 -.06 7 6 | -432 -306 980 2229
sio 320| 0 -2 3 -2 -47 5 -.02 14 14 | --- --- --- ---
Table 2.2062.3 GPS week: 2062 Day: 3 MJD: 58681.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 1 0 0 15 3 -18 -.00 10 10 | -298 -481 8 98
emr 80| 0 0 -1 -5 -6 4 .08 11 11 | 136527 227 16 81
esa 150| 0 0 -2 -2 -3 -10 -.09 10 10 | 4079 -961 8 122
gfz 180| 0 0 3 -11 3 -13 .02 22 11 | -548 132 15 189
grg 100| 2 -1 1 -9 -14 61 -.11 13 13 | 114 -244 11 134
igr n/a| 0 1 0 -30 -19 9 -.05 4 4 | -18436 360 12 71
jpl 80| 0 0 -2 6 4 22 .11 7 7 | 136575 275 10 79
mit 349| 0 -1 0 -54 15 0 .01 12 11 | -786 -173 158 1876
ngs 209| 0 0 1 24 -6 -29 -.05 7 6 | -4420 12481 1535 2269
sio 323| 0 -2 2 2 6 23 -.03 14 13 | --- --- --- ---
Table 2.2062.4 GPS week: 2062 Day: 4 MJD: 58682.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 254| 1 -1 0 48 24 -27 -.02 9 9 | -517 -35 6 80
emr 80| -1 1 0 -19 -8 -2 .09 11 11 | 136735 388 16 88
esa 150| 0 0 -3 -3 2 -3 -.10 10 10 | 3460 203 6 109
gfz 184| 0 0 4 -28 9 0 .05 22 11 | -688 452 16 219
grg 96| 3 -1 0 -21 2 29 -.08 13 12 | 4 -30 9 130
igr n/a| 0 1 0 -22 -44 -8 -.05 4 4 | -18162 209 11 89
jpl 80| 0 0 0 -28 11 7 .11 7 7 | 211647 270 10 91
mit 348| 0 -1 0 34 -34 25 -.03 13 12 | -598 252 132 1767
ngs 212| 0 0 -2 13 6 -4 -.07 8 7 | 15779 -23826 984 2062
sio 323| 0 -2 0 38 -65 -4 -.00 14 14 | --- --- --- ---
Table 2.2062.5 GPS week: 2062 Day: 5 MJD: 58683.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 257| 0 0 1 24 51 -28 -.01 10 9 | -569 -74 8 79
emr 80| -1 0 -1 -6 -1 12 .09 11 11 | 137435 -417 15 98
esa 150| 0 0 -4 2 4 -6 -.14 10 10 | -1868 1757 12 122
gfz 182| 0 0 4 -2 -2 -30 .01 10 11 | 100 262 32 229
grg 96| 4 -1 -2 -11 -8 57 -.12 13 12 | 254 -260 12 136
igr n/a| 0 0 0 -8 -45 -21 -.07 4 4 | -17561 -320 12 77
jpl 80| 0 0 0 28 -23 21 .16 7 7 | 212270 -658 10 77
mit 348| 0 0 0 -31 11 11 -.05 12 11 | 256 -132 141 1720
ngs 211| 0 0 3 -6 -4 -15 -.06 9 7 | -144506 797544 924 2132
sio 313| -1 -1 0 -35 -6 -9 -.03 14 14 | --- --- --- ---
Table 2.2062.6 GPS week: 2062 Day: 6 MJD: 58684.000
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 0 4 -8 -12 -.04 11 10 | -638 10 8 100
emr 80| -3 0 1 -13 3 8 .11 11 11 | 137155 338 16 82
esa 149| 0 0 -3 20 -4 -15 -.10 10 10 | 3278 278 8 133
gfz 182| 0 2 3 -18 -8 -14 .02 17 13 | -572 754 12 229
grg 98| 3 0 -1 -13 0 45 -.05 14 12 | -76 73 13 165
igr n/a| 0 1 0 -12 -24 -12 -.07 4 4 | -17710 528 12 75
jpl 80| 0 0 0 21 -20 47 .11 7 7 | 211793 312 10 91
mit 349| -1 0 0 6 41 -9 -.04 13 11 | -900 370 72 1807
ngs 210| 0 0 0 -5 -6 1 -.08 8 7 | -664 24 971 2326
sio 316| 0 0 0 -16 27 -49 .01 13 14 | --- --- --- ---
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 3.2062.0 GPS week: 2062 Day: 0 MJD: 58678.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 9 15 12 11 2 9 7 7 9 3 | 22 24 23 22 26 20 23 22 23 22 22
2 | 9 11 6 9 12 5 7 21 10 18 4 | 27 26 27 27 23 25 25 32 26 27 25
3 | 8 9 12 8 12 3 8 6 7 11 3 | 36 37 33 35 28 34 38 33 34 35 34
5 | 9 11 6 8 11 4 5 11 9 15 3 | 23 23 19 24 22 20 24 24 23 19 21
6 | 7 13 11 9 14 3 8 10 7 8 3 | 26 27 24 21 27 23 24 24 24 22 24
7 | 7 9 9 9 10 5 6 22 7 18 4 | 39 45 42 45 45 40 45 40 40 38 41
8 | 6 8 9 9 10 2 6 6 6 11 2 | 25 24 24 25 24 20 24 24 23 25 23
9 | 7 12 8 8 9 4 9 5 6 16 3 | 31 40 28 31 30 30 39 34 31 38 33
10 | 7 11 16 13 17 3 9 7 5 6 3 | 20 23 26 22 25 19 24 20 21 23 20
11 | 9 7 12 9 10 2 6 7 7 14 3 | 27 30 27 27 24 24 28 27 27 24 26
12E | 8 19 9 7 13 4 7 16 14 20 4 | 27 30 29 25 26 26 29 28 33 29 26
13 | 10 9 8 8 11 4 6 10 8 9 3 | 26 27 22 26 20 21 25 30 26 25 24
14 | 8 8 8 7 8 3 5 11 6 10 2 | 38 35 37 37 36 36 36 40 37 38 36
15 | 8 9 6 8 12 2 8 11 6 13 3 | 42 47 43 43 43 42 45 45 42 45 43
16E | 7 19 11 9 30 6 9 19 7 19 5 | 17 17 17 20 21 16 15 23 19 23 16
17 | 8 8 7 8 14 4 8 18 7 19 3 | 23 27 20 22 23 21 26 28 24 22 22
18 | 9 9 9 9 11 3 8 9 8 16 3 | 18 25 23 18 25 17 24 21 19 31 20
19 | 8 9 6 7 12 5 7 20 8 23 4 | 22 25 20 22 21 20 24 26 22 24 21
20 | 10 13 8 12 18 4 9 13 9 12 4 | 22 21 23 25 25 20 21 23 23 23 20
21 | 5 11 6 9 15 3 8 13 12 15 3 | 22 23 20 24 24 19 20 24 23 21 20
22 | 8 8 6 6 15 3 6 14 9 18 3 | 22 24 20 23 27 20 24 22 24 19 21
23 | 10 21 7 6 6 3 7 10 7 13 3 | 19 17 14 17 14 15 14 18 18 18 15
24 | 9 8 7 9 11 3 6 7 8 12 3 | 20 28 22 22 20 22 28 22 21 29 22
X25E | 23 25 25 28 29 8 --- 29 28 17 10 | 122 117 114 114 121 111 --- 118 106 112 114
26E | 9 15 24 46 35 6 14 11 13 13 8 | 36 41 37 59 53 37 39 36 35 34 37
27 | 7 9 11 8 10 3 5 6 9 9 3 | 25 26 25 26 26 22 25 24 24 26 24
28E | 11 10 9 8 14 4 6 12 7 15 3 | 21 23 22 25 28 21 23 25 24 26 22
29 | 8 19 6 9 12 5 9 18 8 22 4 | 26 21 21 27 26 22 23 26 25 28 23
30 | 8 7 8 7 12 2 6 8 7 9 2 | 80 79 70 73 81 79 47 81 84 45 80
31 | 6 10 8 5 10 5 8 20 6 19 3 | 36 41 36 36 38 34 41 34 38 32 36
32 | 9 10 7 11 8 4 11 10 8 9 3 | 36 43 37 36 33 35 42 39 38 40 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 10 12 14 4 8 13 8 15 |T 31 33 30 32 32 29 28 32 31 31 30
WRMS | 8 12 10 10 13 4 8 12 7 15 |NE 28 31 27 29 29 26 29 30 29 28 28
MEDI | 8 10 8 9 12 4 7 11 7 14 |MD 26 27 24 25 26 22 25 26 24 26 24
Table 3.2062.1 GPS week: 2062 Day: 1 MJD: 58679.000
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 10 15 9 10 3 11 10 7 13 3 | 23 24 24 26 27 21 22 22 21 26 23
2 | 8 10 6 7 14 4 8 18 6 18 3 | 21 24 25 22 20 22 22 30 23 24 22
3 | 8 13 11 9 14 4 7 7 6 11 3 | 37 40 38 37 45 38 39 40 37 42 38
5 | 7 10 5 6 11 3 6 9 10 19 3 | 22 24 18 22 24 20 22 23 22 20 20
6 | 9 14 13 12 15 4 8 12 8 10 4 | 21 25 23 20 25 20 24 22 23 22 22
7 | 8 11 9 8 9 3 6 21 9 19 3 | 27 29 26 30 29 25 30 31 26 29 27
8 | 6 11 11 8 10 3 7 9 7 12 3 | 21 22 21 23 24 19 22 20 19 22 21
9 | 9 12 5 8 7 4 10 8 5 12 3 | 26 36 26 26 27 25 35 28 26 33 28
10 | 7 10 15 17 17 3 7 7 6 7 4 | 19 23 21 24 25 18 21 19 18 23 20
11 | 8 11 12 8 12 2 8 11 6 15 3 | 22 26 23 22 20 20 24 20 22 21 21
12E | 6 23 11 12 16 2 6 16 11 18 4 | 27 32 30 24 27 27 29 31 28 31 27
13 | 8 8 8 7 7 4 6 11 9 12 3 | 23 21 21 25 16 18 20 26 18 20 19
14 | 7 7 8 9 6 3 9 12 6 14 3 | 33 30 29 34 32 31 32 36 33 33 31
15 | 8 7 6 8 10 3 7 12 10 14 3 | 28 31 30 32 25 26 32 28 23 28 28
16E | 10 21 11 5 20 5 7 21 8 18 4 | 20 19 19 18 21 17 17 23 17 20 16
17 | 9 9 7 8 13 3 9 19 10 23 4 | 21 26 19 23 21 20 25 27 22 21 21
18 | 10 9 9 10 14 3 8 9 6 13 3 | 18 22 23 16 24 16 20 19 16 25 18
19 | 9 12 7 12 14 4 7 19 11 27 4 | 21 26 21 25 19 21 23 25 23 22 21
20 | 11 11 7 10 17 4 7 14 7 11 3 | 19 20 19 25 25 18 20 20 20 19 19
21 | 7 12 7 10 18 5 7 14 6 17 3 | 20 21 19 22 22 18 19 24 17 20 17
22 | 10 11 5 8 16 4 6 13 5 17 3 | 18 19 15 18 30 16 18 19 16 17 16
23 | 8 19 7 7 8 4 9 12 7 13 3 | 16 16 18 22 18 16 16 20 17 23 17
24 | 10 11 6 6 10 3 7 9 6 11 3 | 20 25 22 24 19 21 29 24 23 29 22
X25E | 19 29 --- --- 42 35 --- 33 17 --- 13 | 57 55 --- --- 74 51 --- 47 48 --- 49
26E | 12 13 17 73 19 4 10 11 11 11 5 | 28 30 27 58 33 24 26 32 27 27 27
27 | 7 9 9 6 10 3 7 7 6 11 2 | 20 21 20 24 21 19 20 19 19 20 20
28E | 14 10 8 10 12 3 7 12 7 18 3 | 29 28 28 30 32 26 28 32 27 32 28
29 | 8 17 6 10 12 3 10 17 10 19 4 | 24 24 20 25 21 20 20 24 24 22 21
30 | 7 9 8 7 8 3 6 6 7 14 2 | 82 79 71 73 82 80 50 82 84 56 81
31 | 8 13 8 8 8 4 9 24 6 20 4 | 27 30 23 25 25 24 30 32 25 25 25
32 | 7 12 7 7 6 4 11 9 6 10 3 | 27 35 29 33 29 28 34 29 28 33 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 9 16 13 4 8 13 8 15 |T 26 28 24 27 28 24 25 28 25 26 25
WRMS | 8 12 9 10 12 4 8 12 7 15 |NE 25 27 24 26 26 23 25 27 24 25 24
MEDI | 8 11 8 8 12 3 7 12 7 14 |MD 22 25 23 24 25 21 23 25 23 23 22
Table 3.2062.2 GPS week: 2062 Day: 2 MJD: 58680.000
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 9 10 2 11 9 7 10 3 | 23 23 24 23 28 21 22 20 22 26 22
2 | 8 12 6 10 11 3 7 19 8 16 3 | 21 27 24 24 19 21 22 29 22 22 21
3 | 8 11 12 9 16 3 9 8 8 9 3 | 25 28 24 25 35 25 27 25 24 26 25
5 | 8 10 5 6 10 4 7 11 10 17 3 | 26 25 21 21 25 21 25 23 25 20 23
6 | 9 18 12 8 15 4 9 12 8 13 4 | 34 35 31 28 36 30 31 32 31 30 32
7 | 6 10 7 7 11 5 7 21 6 18 3 | 31 38 33 34 42 32 35 37 31 35 33
8 | 10 10 10 8 9 2 8 8 6 11 3 | 25 25 23 24 27 22 24 23 21 21 23
9 | 10 11 5 10 7 4 11 8 8 12 3 | 20 31 21 19 17 20 31 20 17 27 21
10 | 11 14 16 12 16 3 7 7 6 6 4 | 19 24 20 20 26 19 20 19 18 19 18
11 | 11 8 12 6 11 2 8 8 5 14 3 | 22 25 20 22 24 19 23 19 20 19 20
12E | 6 18 9 16 7 4 6 14 10 14 4 | 30 29 26 28 29 27 29 27 35 28 28
13 | 5 10 7 8 6 4 8 11 8 10 2 | 25 30 24 25 23 24 28 29 28 26 26
14 | 6 7 8 8 6 2 8 11 6 15 3 | 40 41 38 41 42 39 37 41 38 38 39
15 | 5 8 5 10 6 5 9 11 7 13 3 | 28 34 28 31 31 29 30 27 28 28 29
16E | 9 20 7 8 15 3 8 14 7 15 4 | 13 16 11 12 16 11 12 16 17 16 12
17 | 10 10 6 8 12 3 8 19 8 20 4 | 20 25 18 23 21 19 24 25 22 24 21
18 | 10 10 8 11 14 4 7 7 7 12 3 | 17 21 19 17 25 13 19 14 17 24 17
19 | 9 11 6 13 14 3 7 20 10 27 4 | 18 23 19 25 18 17 21 22 18 21 18
20 | 10 11 6 13 18 4 8 13 6 13 3 | 15 17 14 20 24 14 16 16 15 16 13
21 | 5 11 5 11 14 3 7 13 6 17 3 | 17 20 17 21 22 16 18 20 17 17 16
22 | 10 9 6 9 17 3 7 11 7 15 3 | 24 28 25 25 35 25 26 27 23 24 24
23 | 10 19 5 9 7 4 7 12 7 15 3 | 18 18 16 19 19 17 17 18 15 20 17
24 | 7 6 5 10 7 5 7 7 6 11 2 | 19 28 21 26 23 23 27 23 25 26 23
X25E | 14 11 16 79 16 6 --- 11 15 13 6 | 39 37 42 69 41 38 --- 38 39 35 36
26E | 9 12 16 99 16 3 6 14 10 13 4 | 25 31 29 73 35 26 27 30 26 24 27
27 | 10 10 10 10 7 2 6 6 8 10 3 | 21 22 21 24 25 19 21 21 18 19 20
28E | 9 13 6 7 9 4 7 9 5 13 3 | 20 23 17 17 20 16 19 21 16 25 18
29 | 8 17 6 10 8 4 9 14 7 16 3 | 21 20 16 23 22 18 20 21 19 24 19
30 | 5 8 6 5 9 3 8 6 5 9 2 | 73 75 59 58 71 73 44 71 80 46 73
31 | 8 10 10 6 9 4 8 20 5 21 3 | 34 38 30 33 36 31 36 32 32 29 32
32 | 8 9 6 9 6 3 11 5 5 11 2 | 23 31 23 22 20 22 32 24 23 32 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 9 20 11 4 8 12 7 14 |T 25 28 24 28 28 24 25 26 25 25 24
WRMS | 8 12 9 10 11 4 8 11 6 14 |NE 25 28 24 25 28 24 26 26 24 25 24
MEDI | 9 10 7 9 10 3 8 11 7 13 |MD 23 27 23 24 25 21 24 23 22 24 23
Table 3.2062.3 GPS week: 2062 Day: 3 MJD: 58681.000
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 14 9 10 3 8 10 5 9 3 | 24 25 26 24 27 22 23 23 23 25 23
2 | 12 10 5 8 14 4 7 16 7 15 3 | 28 27 25 27 22 23 26 29 25 28 25
3 | 7 10 12 11 14 3 8 7 6 8 3 | 24 26 24 24 27 22 27 20 22 22 23
5 | 10 9 7 8 11 5 7 10 9 17 3 | 26 25 21 23 26 21 26 25 24 21 23
6 | 9 16 11 8 16 3 8 10 7 10 3 | 28 29 24 21 27 23 25 24 26 25 25
7 | 5 10 9 9 10 4 8 21 6 16 3 | 37 41 37 38 37 34 40 37 38 36 37
8 | 7 8 10 11 12 2 8 5 5 10 3 | 22 21 22 23 21 20 22 22 21 20 20
9 | 10 10 5 7 11 2 9 6 7 12 3 | 25 36 25 28 20 25 34 27 26 33 27
10 | 8 10 17 17 16 4 8 7 6 7 4 | 21 26 25 26 26 21 23 21 22 22 22
11 | 8 8 12 9 11 2 6 9 5 12 3 | 25 27 24 25 22 22 25 24 21 21 22
12E | 7 15 11 15 19 3 6 14 9 15 4 | 24 28 28 28 29 24 26 25 28 25 25
13 | 9 8 8 7 6 5 6 10 9 11 3 | 23 26 20 23 20 20 24 25 21 22 21
14 | 9 9 10 5 8 3 8 12 5 14 3 | 21 23 23 23 23 22 21 24 25 22 22
15 | 9 9 8 7 6 4 6 13 5 14 3 | 34 41 34 33 35 32 38 33 32 30 34
16E | 9 19 9 9 23 5 8 20 10 15 4 | 21 18 19 21 24 17 16 25 19 20 17
17 | 7 8 7 7 15 3 7 17 8 17 3 | 23 27 21 26 22 22 24 26 25 24 23
18 | 10 10 8 11 14 3 8 7 6 12 3 | 21 24 25 22 26 18 23 19 20 27 21
19 | 10 13 6 9 13 4 7 18 10 22 4 | 23 27 21 24 20 19 22 24 22 21 20
20 | 8 10 8 15 18 5 7 12 8 13 3 | 24 26 27 29 29 24 25 25 25 23 24
21 | 17 10 5 13 17 5 6 13 5 17 4 | 28 21 19 26 21 20 21 22 22 17 19
22 | 9 7 5 8 17 4 7 12 9 14 3 | 21 22 19 21 26 19 21 20 18 15 18
23 | 6 18 7 10 8 4 5 12 4 13 3 | 16 14 14 17 14 14 13 15 13 18 14
24 | 10 11 7 8 8 3 8 7 9 10 3 | 21 27 23 24 23 23 31 23 25 27 24
25E | 9 9 17 27 9 4 7 6 11 9 4 | 42 45 46 49 44 45 22 45 49 40 45
26E | 12 9 17 104 16 4 8 11 9 12 4 | 31 29 34 76 37 31 31 32 31 29 30
27 | 11 9 9 9 13 2 6 4 6 9 3 | 24 23 24 24 22 21 24 23 23 20 22
28E | 14 9 7 16 16 3 5 11 7 14 3 | 22 19 19 20 24 18 20 21 21 22 19
29 | 9 15 10 9 11 3 7 14 7 18 3 | 26 24 21 24 22 22 25 24 27 25 23
X30 | 6 13 --- --- 19 9 --- 10 80 --- 7 | 82 90 --- --- 73 88 --- 88 144 --- 84
31 | 14 13 10 7 9 5 8 20 8 24 4 | 36 38 33 34 35 32 39 33 35 33 34
32 | 11 11 6 9 8 4 10 6 7 11 3 | 28 34 29 30 27 28 35 29 32 32 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 10 22 13 4 7 12 7 14 |T 27 29 25 27 27 25 25 27 29 24 26
WRMS | 10 11 10 11 13 4 7 11 6 13 |NE 27 29 24 25 26 25 26 27 29 24 26
MEDI | 9 10 8 9 13 4 7 11 7 13 |MD 24 26 24 24 26 22 24 24 25 23 23
Table 3.2062.4 GPS week: 2062 Day: 4 MJD: 58682.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 15 8 9 2 7 12 6 10 3 | 22 21 21 23 25 19 22 17 20 23 20
2 | 8 9 6 9 13 4 8 15 8 18 3 | 20 22 22 24 20 20 20 27 22 24 20
3 | 8 9 14 11 16 3 6 10 6 9 3 | 18 22 20 20 27 18 22 18 20 19 19
X4 | 3 --- --- --- --- 2856 --- --- --- --- 0 | 9999 --- --- --- --- 81 --- --- --- --- 9999
5 | 7 8 8 10 12 3 6 11 10 18 3 | 23 21 19 18 24 18 21 21 22 15 19
6 | 10 16 10 14 17 4 7 12 7 11 4 | 28 30 31 30 26 25 33 31 21 31 25
7 | 7 8 9 9 8 5 6 22 7 19 3 | 35 34 32 34 34 32 35 34 34 32 33
8 | 8 7 9 11 12 2 7 8 8 9 3 | 21 23 19 26 23 20 23 21 21 18 20
9 | 10 9 5 7 10 5 7 9 6 13 3 | 21 31 22 25 21 23 31 24 20 27 24
10 | 8 8 18 10 17 2 7 8 5 7 3 | 20 21 21 19 26 18 20 19 17 23 18
11 | 11 8 13 6 12 2 7 11 7 12 3 | 22 25 20 25 22 20 24 20 21 17 20
12E | 6 13 9 8 15 3 5 17 14 14 4 | 20 21 21 17 18 18 20 23 21 24 18
13 | 7 7 9 10 5 3 5 10 5 12 2 | 24 25 22 20 22 21 24 26 22 25 22
14 | 7 7 10 8 7 3 7 12 6 14 3 | 34 34 32 37 36 34 34 37 33 35 34
15 | 8 8 6 6 9 4 6 13 9 15 3 | 32 32 29 28 28 29 33 26 26 29 28
16E | 11 17 9 9 18 5 8 20 12 16 4 | 20 20 20 20 18 18 16 21 22 21 16
17 | 10 9 6 7 15 5 6 16 9 19 3 | 24 25 20 25 22 23 26 28 24 23 22
18 | 10 8 9 11 13 4 7 12 8 13 3 | 17 22 21 21 23 15 21 18 16 25 17
19 | 8 17 6 8 14 5 6 19 10 24 4 | 20 24 17 22 18 18 21 21 20 19 18
20 | 10 10 9 10 17 4 8 13 6 10 3 | 20 15 19 21 28 16 16 16 19 18 16
21 | 10 10 7 7 15 4 6 15 12 17 3 | 19 20 17 18 20 17 20 23 20 18 16
22 | 7 9 8 9 19 3 5 14 7 15 3 | 21 23 20 22 29 21 23 21 23 18 20
23 | 8 17 6 9 9 4 6 14 6 15 3 | 14 13 13 18 16 13 11 15 15 18 13
24 | 8 8 6 8 8 3 7 8 8 10 2 | 22 24 21 22 18 19 23 21 20 28 20
25E | 10 9 20 28 12 3 8 12 11 7 5 | 23 22 27 31 20 22 17 24 25 22 21
26E | 13 13 17 110 22 4 6 13 9 15 5 | 28 27 28 75 35 24 22 25 26 19 24
27 | 8 10 9 9 11 3 6 8 7 12 3 | 19 20 18 21 21 17 20 18 19 20 18
28E | 11 8 6 13 12 3 6 9 6 12 3 | 18 18 18 21 23 16 18 17 19 19 17
29 | 7 15 6 8 13 2 7 15 6 18 3 | 23 21 17 22 21 19 21 22 21 22 19
X30 | 7 8 8 8 11 3 --- 8 8 --- 3 | 92 90 107 112 93 90 --- 91 85 --- 92
31 | 8 10 11 5 12 4 7 20 5 21 3 | 34 37 34 32 31 30 35 31 33 30 32
32 | 11 9 7 6 8 4 7 7 7 9 2 | 26 34 26 29 27 25 33 28 26 32 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 10 22 13 4 7 13 8 14 |T 25 26 24 28 26 24 23 25 24 23 23
WRMS | 9 11 10 11 12 4 7 12 7 14 |NE 25 27 25 27 26 25 24 25 24 23 24
MEDI | 8 9 9 9 12 3 7 12 7 13 |MD 22 23 21 22 23 20 22 22 21 22 20
Table 3.2062.5 GPS week: 2062 Day: 5 MJD: 58683.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 9 15 11 9 3 9 9 6 10 3 | 20 23 20 21 23 18 21 19 19 21 20
2 | 12 7 6 8 11 4 7 13 7 13 3 | 22 21 22 22 19 20 21 27 22 24 20
3 | 8 10 14 7 18 2 6 8 7 10 3 | 20 22 18 19 26 17 21 18 20 19 19
X4 | 4 --- --- --- --- 43 --- --- --- --- 0 | 506 --- --- --- --- 52 --- --- --- --- 487
5 | 10 9 7 8 13 3 8 10 8 16 3 | 24 20 16 16 22 16 20 19 21 10 17
X6 | 11 14 --- --- 20 10 --- 15 87 --- 8 | 49 49 --- --- 46 49 --- 46 99 --- 47
7 | 7 10 7 10 11 5 7 23 6 19 4 | 29 34 29 29 31 28 31 35 27 32 29
8 | 6 7 10 10 11 3 7 7 7 13 3 | 18 18 17 18 19 16 18 18 17 16 16
9 | 14 10 7 7 8 3 7 7 7 11 3 | 26 32 23 26 21 24 32 24 27 29 26
10 | 7 10 17 13 17 4 7 7 8 6 4 | 19 21 20 19 22 17 21 18 19 18 18
11 | 8 7 13 11 12 3 6 9 7 14 3 | 24 26 24 25 21 21 25 21 22 17 22
12E | 18 13 14 8 14 8 5 18 17 18 5 | 22 19 20 19 18 19 19 20 22 20 17
13 | 8 8 7 9 5 2 6 9 7 10 2 | 21 21 17 17 15 16 21 20 20 20 18
14 | 7 7 10 8 6 2 5 13 7 14 3 | 23 26 23 26 27 25 24 31 27 27 24
15 | 7 8 6 5 9 3 6 12 10 16 3 | 20 24 20 19 23 20 24 20 21 23 21
16E | 10 25 10 9 14 5 8 19 14 18 5 | 20 21 20 20 17 18 18 23 23 18 16
17 | 6 10 7 6 21 5 9 16 10 16 4 | 18 22 17 20 23 18 23 22 20 17 18
18 | 9 7 10 12 13 4 8 9 6 16 3 | 18 20 21 20 19 16 21 18 19 25 17
19 | 13 15 8 7 12 5 7 18 12 20 4 | 24 24 20 22 21 19 22 21 23 19 20
20 | 10 11 9 10 25 5 6 13 8 13 4 | 35 35 36 37 38 35 38 37 37 37 35
21 | 15 9 6 10 18 5 6 15 11 19 4 | 22 22 18 19 17 17 20 24 20 21 17
22 | 7 7 7 8 20 4 5 12 11 16 3 | 16 16 14 18 27 13 15 17 15 13 14
X23 | 4 --- --- --- --- 26 --- --- --- --- 0 | 12 --- --- --- --- 10 --- --- --- --- 14
24 | 10 8 7 9 8 3 6 7 8 13 3 | 19 25 19 20 19 18 25 20 20 28 20
25E | 12 8 18 24 11 4 8 8 9 9 4 | 35 35 33 40 35 34 18 36 36 32 33
X26E | 13 --- 17 85 14 5 6 12 14 14 5 | 29 --- 30 58 32 28 27 30 30 23 27
27 | 7 11 10 8 10 3 6 6 9 10 3 | 18 17 18 20 19 17 20 18 18 18 17
28E | 11 8 6 17 10 4 8 8 6 12 3 | 18 16 18 22 24 18 19 18 21 20 18
29 | 13 16 8 6 13 4 7 12 12 15 4 | 23 22 20 21 23 20 21 25 24 24 20
30 | 7 8 6 6 8 3 6 8 6 9 2 | 33 36 27 26 33 34 45 34 39 44 33
31 | 7 10 9 5 10 4 6 19 6 18 3 | 29 34 27 29 29 26 33 30 24 27 28
32 | 12 10 5 11 8 3 9 6 8 10 3 | 31 37 32 32 27 30 37 31 33 35 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 10 10 13 4 7 12 9 14 |T 38 25 22 24 24 22 24 24 26 23 36
WRMS | 9 11 10 11 12 4 7 11 7 14 |NE 41 25 21 22 24 22 24 24 26 23 39
MEDI | 8 9 8 9 11 4 7 10 8 14 |MD 22 22 20 21 23 19 21 21 22 21 20
Table 3.2062.6 GPS week: 2062 Day: 6 MJD: 58684.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 7 14 12 9 2 7 10 6 8 3 | 18 20 21 21 20 17 19 19 18 21 18
2 | 12 7 6 10 10 4 5 13 9 16 3 | 23 23 25 27 22 24 23 27 27 25 23
3 | 8 10 14 8 15 3 9 8 6 6 3 | 18 22 22 20 26 18 22 20 19 19 19
X4 | 337 --- 3 --- --- 334 --- --- --- --- 0 | 490 --- 35 --- --- 37 --- --- --- --- 658
5 | 10 11 5 7 12 3 6 10 8 18 3 | 22 23 18 20 24 19 22 23 20 20 20
6 | 10 14 10 8 15 4 7 12 6 10 3 | 38 42 29 34 44 38 32 39 58 31 39
7 | 8 10 7 8 10 4 8 23 7 19 4 | 45 46 45 45 48 43 45 46 43 43 44
8 | 6 10 11 8 10 3 7 7 7 9 3 | 22 22 21 21 23 19 20 21 21 19 20
9 | 13 9 4 8 8 4 9 8 5 9 3 | 28 33 26 27 25 27 34 30 26 33 28
10 | 10 8 15 10 17 3 8 9 8 7 3 | 22 23 24 23 25 19 22 22 19 22 20
11 | 6 8 12 13 11 3 6 11 7 11 3 | 29 32 30 29 24 27 30 29 29 26 27
12E | 13 16 8 12 8 4 7 11 11 12 4 | 31 34 33 38 32 32 34 35 30 36 32
13 | 11 10 7 8 7 3 7 9 6 10 3 | 26 30 24 26 24 24 27 28 23 28 25
14 | 14 8 9 9 8 4 8 14 6 13 3 | 38 33 32 35 35 34 33 39 32 37 33
15 | 9 10 7 6 7 5 11 13 7 15 3 | 36 41 36 33 37 35 43 34 34 37 36
16E | 20 23 8 8 24 5 9 22 13 14 5 | 30 22 22 23 24 21 21 29 24 25 20
17 | 8 8 7 9 22 4 5 17 8 20 4 | 22 23 20 26 26 21 23 24 25 19 21
18 | 9 8 11 14 16 3 7 11 7 12 3 | 19 21 21 18 21 16 20 20 19 26 18
19 | 12 14 7 10 12 5 4 18 9 25 4 | 26 25 23 27 22 23 24 27 27 26 23
20 | 14 11 8 15 38 4 9 11 8 11 5 | 34 37 37 35 37 33 37 38 33 36 34
21 | 11 11 8 9 15 4 8 15 9 14 4 | 22 24 17 18 19 17 19 24 19 20 17
22 | 7 7 6 8 20 4 6 12 7 13 3 | 17 18 16 20 29 16 17 19 18 14 16
23 | 10 17 6 9 9 5 6 17 6 14 3 | 13 12 8 9 9 11 12 11 8 14 13
24 | 11 9 5 7 8 3 6 8 6 12 2 | 21 24 22 21 20 20 25 22 19 28 21
25E | 12 13 19 34 12 4 11 10 15 10 6 | 33 35 32 40 34 32 20 35 35 30 31
26E | 10 12 16 69 13 4 6 12 11 15 4 | 40 43 41 61 45 39 39 41 40 35 39
27 | 9 10 10 9 8 3 7 6 7 7 3 | 25 23 22 22 24 21 25 22 21 27 23
28E | 17 12 8 15 11 5 6 10 8 10 3 | 27 26 24 24 25 21 23 24 26 23 23
29 | 13 19 7 7 11 4 9 12 8 16 4 | 29 28 23 27 27 24 25 28 28 30 25
30 | 9 7 7 6 10 2 7 8 6 7 2 | 35 39 37 37 38 35 31 36 39 31 36
31 | 6 8 10 8 10 4 7 21 7 17 3 | 39 43 41 39 40 37 42 35 37 35 38
32 | 14 9 7 10 8 4 9 8 7 9 3 | 36 42 36 38 35 36 40 40 35 41 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 10 17 14 4 7 13 8 13 |T 42 29 26 28 28 26 27 28 27 27 46
WRMS | 10 11 10 13 12 4 7 11 7 14 |NE 44 28 26 26 27 25 27 27 26 27 49
MEDI | 10 10 8 9 11 4 7 11 7 12 |MD 27 26 24 27 25 24 25 28 26 27 23
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 4.2062 GPS week: 2062 MJD: 58678.0-58684.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2988 |U 10 11 25 |U 7 10 20 |U 12 12 31 |
emr | emr 2942 |U 15 16 35 |U 10 15 35 |U 19 16 39 |
esa | esa 2934 | 12 14 29 |U 7 13 23 | 12 12 29 |
gfz | gfz 2920 |U 12 13 29 |U 7 11 22 |U 13 13 35 |
grg | grg 2954 |U 11 14 30 |U 9 13 26 | 14 12 36 |
igr | igr 2920 | 10 12 24 | 6 10 19 | 12 11 31 |
igs | igs 2950 | 11 12 26 | 7 11 20 | 13 12 33 |
jpl | jpl 2880 |U 12 15 36 |U 7 15 23 |U 15 15 39 |
mit | mit 2962 | 22 25 50 |U 18 24 73 |U 24 27 72 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.2062.0 GPS week: 2062 Day: 0 MJD: 58678.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 10 25 | 7 11 19 | 14 10 28 |
emr | emr 2976 | 14 18 37 | 12 20 37 | 25 18 48 |
esa | esa 2976 | 14 12 23 | 6 14 25 | 13 13 28 |
gfz | gfz 2976 | 11 10 26 | 8 13 19 | 15 12 31 |
grg | grg 2975 | 11 11 21 | 9 15 26 | 14 12 30 |
igr | igr 2976 | 11 10 22 | 6 12 17 | 14 11 27 |
igs | igs 2976 | 11 11 25 | 7 13 20 | 15 13 30 |
jpl | jpl 2880 | 11 11 29 | 7 18 20 | 16 15 37 |
mit | mit 2976 | 15 12 44 | 43 58 122 | 25 24 64 |
Table 5.2062.1 GPS week: 2062 Day: 1 MJD: 58679.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 | 10 13 24 | 7 9 22 | 10 9 24 |
emr | emr 2962 | 16 18 40 | 11 14 37 | 15 17 38 |
esa | esa 2880 | 12 14 27 | 6 12 17 | 12 12 28 |
gfz | gfz 2880 | 11 14 22 | 7 11 21 | 11 9 28 |
grg | grg 2961 | 12 17 33 | 9 13 28 | 12 10 34 |
igr | igr 2880 | 10 13 21 | 7 10 18 | 11 10 28 |
igs | igs 2951 | 11 13 27 | 7 10 24 | 12 10 31 |
jpl | jpl 2880 | 14 16 34 | 8 14 21 | 13 15 44 |
mit | mit 2976 | 13 11 34 | 8 11 39 | ---- ---- ---- |
Table 5.2062.2 GPS week: 2062 Day: 2 MJD: 58680.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 12 19 | 6 11 19 | 13 17 37 |
emr | emr 2976 | 16 16 33 | 9 12 30 | 16 20 37 |
esa | esa 2976 | 13 12 25 | 6 14 21 | 12 15 32 |
gfz | gfz 2976 | 13 18 26 | 6 13 17 | 16 17 44 |
grg | grg 2972 | 12 15 24 | 7 13 22 | 16 16 45 |
igr | igr 2976 | 10 10 19 | 6 11 18 | 13 14 35 |
igs | igs 2976 | 10 11 20 | 6 11 18 | 13 14 36 |
jpl | jpl 2880 | 13 14 33 | 7 14 24 | 14 19 41 |
mit | mit 2976 | 14 24 42 | 10 16 57 | 16 20 54 |
Table 5.2062.3 GPS week: 2062 Day: 3 MJD: 58681.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2957 | 9 12 25 | 9 8 19 | 13 11 29 |
emr | emr 2957 | 14 16 30 | 10 15 28 | 19 15 35 |
esa | esa 2880 | 13 17 32 | 9 13 18 | 14 12 26 |
gfz | gfz 2879 | 11 14 25 | 8 11 22 | 14 11 28 |
grg | grg 2957 | 11 16 30 | 10 11 25 | 16 12 33 |
igr | igr 2879 | 10 13 25 | 8 10 17 | 14 11 26 |
igs | igs 2951 | 11 14 25 | 8 11 17 | 14 11 32 |
jpl | jpl 2880 | 11 16 31 | 9 15 21 | 16 14 33 |
mit | mit 2976 | 36 52 58 | 22 24 148 | 32 42 76 |
Table 5.2062.4 GPS week: 2062 Day: 4 MJD: 58682.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3008 | 11 12 31 | 6 9 22 | 11 15 30 |
emr | emr 2975 | 15 19 34 | 8 14 37 | 17 17 30 |
esa | esa 2976 | 14 16 36 | 7 12 26 | 12 12 27 |
gfz | gfz 2976 | 12 13 37 | 6 9 25 | 12 12 26 |
grg | grg 2975 | 13 15 39 | 8 13 28 | 14 11 37 |
igr | igr 2975 | 11 13 32 | 6 10 20 | 12 12 31 |
igs | igs 2975 | 12 14 33 | 6 10 21 | 13 12 30 |
jpl | jpl 2880 | 14 17 48 | 6 14 27 | 16 15 30 |
mit | mit 2976 | 42 36 78 | 15 20 53 | 32 34 130 |
Table 5.2062.5 GPS week: 2062 Day: 5 MJD: 58683.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2965 | 9 11 22 | 7 8 20 | 11 14 39 |
emr | emr 2775 | 17 16 31 | 10 13 34 | 22 16 52 |
esa | esa 2784 | 10 14 27 | 7 12 23 | 11 11 41 |
gfz | gfz 2783 | 12 13 25 | 6 8 25 | 13 13 43 |
grg | grg 2869 | 11 13 28 | 8 10 27 | 12 13 42 |
igr | igr 2783 | 9 12 23 | 7 9 21 | 13 12 43 |
igs | igs 2845 | 10 11 25 | 7 10 20 | 14 14 48 |
jpl | jpl 2784 | 10 14 33 | 8 16 27 | 15 14 49 |
mit | mit 2880 | ---- ---- ---- | 11 15 42 | ---- ---- ---- |
Table 5.2062.6 GPS week: 2062 Day: 6 MJD: 58684.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 10 31 | 8 10 21 | 9 7 26 |
emr | emr 2976 | 16 13 41 | 10 17 45 | 16 11 31 |
esa | esa 3072 | 12 14 33 | 8 13 29 | 10 7 23 |
gfz | gfz 2974 | 14 12 39 | 8 9 27 | 11 20 46 |
grg | grg 2974 | 11 12 36 | 11 12 25 | 12 9 34 |
igr | igr 2976 | 10 11 29 | 7 10 21 | 10 7 25 |
igs | igs 2976 | 10 11 31 | 7 11 22 | 11 8 26 |
jpl | jpl 2976 | 12 14 47 | 7 15 22 | ---- ---- ---- |
mit | mit 2976 | 13 17 43 | 19 23 50 | 14 16 36 |
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 6.2062 GPS week: 2062 MJD: 58678.500-58684.500
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 | -21 -30 81 95 -5 | 19 22
| 29 16 90 88 6 | 4
emr uuuuu | 34 31 18 93 1 | 32 34
| 11 24 117 68 8 | 2
esa uuuuu | -6 12 111 -13 -4 | 18 22
| 11 10 53 51 4 | 2
gfz uuuuu | -17 17 22 -97 5 | 24 28
| 13 13 115 94 4 | 1
grg uuuuu | 16 -11 -38 -52 1 | 1 16
| 21 11 39 81 3 | 2
igr xxxxx | 25 25 27 -55 0 | 0 12
| 12 9 34 27 3 | 2
irf xxxxx | -1 -6 -44 -57 1 | 1 14
| 3 8 16 12 4 | 3
jpl uuuuu | 16 -9 42 26 2 | 38 41
| 17 18 29 58 13 | 2
mit uuuuu | -31 5 -83 -148 3 | 28 32
| 9 10 50 52 4 | 2
ngs uuuuu | -14 -5 -90 -26 0 | 17 22
| 16 44 124 60 4 | 2
sio uuuux | 45 9 -182 117 7 | 56 58
| 14 29 84 46 5 | 1
Table 7.2062.0 GPS week: 2062 Day: 0 MJD: 58678.500
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 | 23 -19 90 200 -1 | 25 28
emr uuuuu | 36 47 -90 53 -6 | 36 38
esa uuuuu | 15 23 144 48 -11 | 22 27
gfz uuuuu | 2 26 2 5 4 | 25 30
grg uuuuu | -19 -23 -98 -199 3 | 4 20
igr xxxxx | 27 19 47 -85 -1 | 4 17
irf xxxxx | 1 -13 -20 -66 -4 | 6 20
jpl uuuuu | -6 5 -1 -51 -2 | 38 42
mit uuuuu | -26 -7 -10 -107 3 | 32 37
ngs uuuuu | -46 -60 3 -90 6 | 21 28
sio uuuux | 47 42 -229 80 5 | 56 58
Table 7.2062.1 GPS week: 2062 Day: 1 MJD: 58679.500
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 -25 44 224 -8 | 24 27
emr uuuuu | 35 36 -10 133 -2 | 34 36
esa uuuuu | 1 15 132 -88 2 | 20 25
gfz uuuuu | -20 34 -93 -140 9 | 23 29
grg uuuuu | 6 -29 -77 -20 -3 | 3 19
igr xxxxx | 26 27 40 -13 2 | 2 16
irf xxxxx | 2 4 -47 -44 -5 | 4 18
jpl uuuuu | 10 -13 66 25 22 | 36 40
mit uuuuu | -16 15 -61 -118 -4 | 30 35
ngs uuuuu | -20 -38 18 -87 -3 | 19 26
sio uuuux | 52 50 -240 176 6 | 55 57
Table 7.2062.2 GPS week: 2062 Day: 2 MJD: 58680.500
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 | -29 -10 -46 27 -17 | 21 25
emr uuuuu | 53 57 -30 167 17 | 32 34
esa uuuuu | -11 11 111 56 -2 | 18 24
gfz uuuuu | -10 9 -111 9 3 | 23 28
grg uuuuu | 38 -6 -33 -29 1 | 1 18
igr xxxxx | 37 24 46 -29 -4 | 0 14
irf xxxxx | -4 -3 -34 -48 1 | 0 16
jpl uuuuu | 7 10 79 -35 10 | 37 40
mit uuuuu | -31 16 -69 -126 2 | 27 32
ngs uuuuu | -13 -44 51 -72 1 | 16 23
sio uuuux | 40 -16 -96 51 7 | 55 57
Table 7.2062.3 GPS week: 2062 Day: 3 MJD: 58681.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -16 -50 251 112 -5 | 17 19
emr uuuuu | 32 48 -141 8 -8 | 32 34
esa uuuuu | -5 4 193 -23 -4 | 16 21
gfz uuuuu | -30 17 -22 -72 11 | 22 27
grg uuuuu | 24 -10 -41 -4 3 | -1 16
igr xxxxx | 6 33 42 -73 5 | -2 11
irf xxxxx | -2 -6 -59 -45 3 | -2 14
jpl uuuuu | 0 8 40 3 4 | 37 40
mit uuuuu | -30 -6 -96 -99 3 | 26 30
ngs uuuuu | -2 -3 -87 -27 -1 | 14 20
sio uuuux | 58 -3 -281 132 2 | 55 57
Table 7.2062.4 GPS week: 2062 Day: 4 MJD: 58682.500
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 | -40 -46 46 -7 2 | 17 19
emr uuuuu | 16 27 107 57 3 | 32 34
esa uuuuu | -18 22 63 -50 -1 | 17 20
gfz uuuuu | -20 27 202 -80 -1 | 25 27
grg uuuuu | 36 -2 -14 34 -2 | 1 12
igr xxxxx | 30 36 -30 -72 2 | 0 8
irf xxxxx | -4 -7 -65 -77 2 | 0 10
jpl uuuuu | 30 -35 65 86 6 | 40 41
mit uuuuu | -41 12 -176 -247 3 | 28 30
ngs uuuuu | -6 29 -264 -7 1 | 16 20
sio uuuux | 57 -21 -81 166 14 | 57 58
Table 7.2062.5 GPS week: 2062 Day: 5 MJD: 58683.500
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 | -69 -43 72 61 0 | 15 17
emr uuuuu | 29 3 111 45 0 | 30 32
esa uuuuu | -17 11 101 -22 -8 | 16 20
gfz uuuuu | -4 -5 45 -144 5 | 24 27
grg uuuuu | 27 1 -21 -25 -1 | 0 13
igr xxxxx | 36 11 -14 -73 -3 | -2 9
irf xxxxx | 0 -2 -51 -61 7 | -1 11
jpl uuuuu | 38 -27 22 55 -3 | 39 41
mit uuuuu | -41 3 -85 -164 9 | 27 29
ngs uuuuu | -1 54 -117 56 3 | 15 19
sio uuuux | 39 19 -242 122 14 | 57 58
Table 7.2062.6 GPS week: 2062 Day: 6 MJD: 58684.500
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 | -8 -19 112 45 -5 | 14 17
emr uuuuu | 37 -5 178 186 4 | 29 31
esa uuuuu | -4 -6 33 -10 -4 | 15 20
gfz uuuuu | -34 13 134 -258 2 | 26 27
grg uuuuu | 0 -6 18 -125 7 | 1 12
igr xxxxx | 10 23 56 -41 -1 | -2 9
irf xxxxx | 1 -19 -30 -57 3 | 0 10
jpl uuuuu | 30 -9 24 99 -21 | 40 41
mit uuuuu | -33 0 -81 -173 5 | 28 30
ngs uuuuu | -12 29 -234 45 -8 | 16 19
sio uuuux | 19 -11 -107 88 3 | 58 59
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