[IGSREPORT-26731] Wk 2063 IGS Final Orbits
acc
acc at igs.org
Thu Aug 8 22:17:34 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2063 (Jul 21, 2019 - Jul 27, 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:
igs2063[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2063[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2063[0-6].cls IGS GPS clock combination summary report.
igs20637.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20637.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 16 18 TIXI ULAB WES2 TIXI ULAB WES2
0 | EMR | 18
0 | ESA | AREG CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB
0 | ESA | HERS HOB2 IISC KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS
0 | ESA | NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL AREG CEDU
0 | ESA | COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2
0 | ESA | IISC KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR
0 | ESA | ONSA POHN PTBB TONG TOW2 VILL
0 | GFZ | 18 POHN REYK POHN REYK
0 | JPL | SUWN SUWN
1 | COD | LHAZ TIXI GMSD LHAZ NYAL TIXI TSKB
1 | EMR | NLIB PTBB
1 | ESA | 18 18 AREG CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ
1 | ESA | HARB HERS HOB2 KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS
1 | ESA | NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL AREG CEDU
1 | ESA | COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2
1 | ESA | KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR ONSA
1 | ESA | POHN PTBB TONG TOW2 VILL
1 | GFZ | POHN POHN
1 | GRG | ALIC
1 | JPL | ALIC NTUS ALIC NTUS
1 | MIT | 18
2 | COD | 18 18 LHAZ LHAZ
2 | EMR | 18 18
2 | ESA | 18 18 AREG CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ
2 | ESA | HARB HERS HOB2 KIRU KOUR LAUT MAJU MAR6 MAS1 MAW1
2 | ESA | MGUE MOBS NAUR NNOR ONSA POHN TOW2 VILL AREG CEDU
2 | ESA | COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2
2 | ESA | KIRU KOUR LAUT MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR
2 | ESA | NNOR ONSA POHN TOW2 VILL
2 | GFZ | POHN FLRS POHN
2 | GRG | 3 10 3 10 LHAZ LHAZ
2 | MIT | 18 SUTH SUTH
3 | COD | 18 18 NRMD TIXI NRMD TIXI
3 | EMR | 8 6 8 18 ALGO
3 | ESA | CEDU COCO DARW DAV1 DGAR FAA1 FALK HARB HERS HOB2
3 | ESA | KIRU KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR
3 | ESA | ONSA POHN PTBB TOW2 VILL CEDU COCO DARW DAV1 DGAR
3 | ESA | FAA1 FALK HARB HERS HOB2 KIRU KOUR MAJU MAR6 MAS1
3 | ESA | MAW1 MGUE MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL
3 | GFZ | 18 18 ALGO GODE IISC POHN BARH GODE IISC POHN
3 | GRG | DAV1 DAV1 OHI3
3 | JPL | 18 DAV1 DAV1
3 | MIT | IISC IISC
4 | COD | ANKR ANKR REUN
4 | EMR | 18
4 | ESA | 18 18 CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB
4 | ESA | HERS HOB2 KIRU KOUR MAJU MAR6 MAS1 MAW1 MGUE MOBS
4 | ESA | NAUR NNOR NRIL ONSA POHN TOW2 VILL CEDU COCO DARW
4 | ESA | DAV1 DGAR FAA1 FALK GRAZ HARB HERS HOB2 KIRU KOUR
4 | ESA | MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR ONSA POHN
4 | ESA | TOW2 VILL
4 | GFZ | IRKJ POHN IRKJ POHN
4 | GRG | 21 21 IRKJ NRMD IRKJ NRIL NRMD
4 | MIT | ANKR
5 | COD | 21 21 TIXI TIXI
5 | EMR | PTBB
5 | ESA | 18 18 ANKR CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB
5 | ESA | HERS HOB2 KIRU KOUR LAUT MAJU MAR6 MAS1 MAW1 MGUE
5 | ESA | MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL ANKR CEDU
5 | ESA | COCO DARW DAV1 DGAR FAA1 GRAZ HARB HERS HOB2 KIRU
5 | ESA | KOUR LAUT MAJU MAR6 MAS1 MAW1 MGUE MOBS NAUR NNOR
5 | ESA | ONSA POHN PTBB TOW2 VILL
5 | GFZ | 21 21 DGAR KRGG POHN DGAR KRGG POHN
5 | GRG | 18 ALIC SAMO
5 | JPL | 18 21
6 | COD | 18 18 ANKR TIXI ANKR TIXI
6 | EMR | KOKB TWTF
6 | ESA | 18 18 CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB
6 | ESA | HERS HOB2 KIRU KOUR LAUT LPGS MAJU MAR6 MAS1 MAW1
6 | ESA | MDVJ MGUE MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL
6 | ESA | WTZR CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB
6 | ESA | HERS HOB2 KIRU KOUR LAUT LPGS MAJU MAR6 MAS1 MAW1
6 | ESA | MDVJ MGUE MOBS NAUR NNOR ONSA POHN PTBB TOW2 VILL
6 | GFZ | POHN GOLD POHN WTZR
6 | GRG | 18 18 SAMO
6 | JPL | 18
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
----+--------+--------+-------------
1 | GFZ | ~00:30 | ~ 0.26 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
----+--------+---------------
0 | COD | 4
0 | GFZ | 26
1 | COD | 4
2 | ESA | 4
2 | GRG | 3 10
2 | JPL | 3
3 | ESA | 4
4 | ESA | 4
5 | ESA | 4
6 | ESA | 4 18
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 G03 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G04 | 4 | 4 | | | | | |
PRN G10 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G20 | | | | 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 | .2 .0 .9 23 11 3 -.60
EMR | 0 | -1.3 -4.7 -1.6 -15 52 17 -.34
ESA | 0 | .3 -1.2 -.6 6 40 61 -.59
GFZ | 0 | -.1 .5 .6 45 21 10 -.55
GRG | 0 | .0 -2.9 -.5 127 26 145 -.24
JPL | 0 | 1.1 -6.8 3.9 4 10 -2 -.42
MIT | 0 | 2.4 -9.2 6.0 8 89 -4 -.09
NGS | 0 | -7.5 -5.8 -1.4 -34 103 -47 -.37
SIO | 0 | -3.2 -7.2 5.5 -9 19 -17 -.29
COD | 1 | .5 -.2 1.2 8 22 12 -.43
EMR | 1 | 2.3 -5.8 3.3 -46 52 2 -.21
ESA | 1 | 1.1 -1.0 -.7 -3 37 36 -.48
GFZ | 1 | -.4 .6 .8 50 19 16 -.39
GRG | 1 | -2.5 -3.4 -5.0 109 -9 122 -.36
JPL | 1 | 3.6 -15.3 8.3 26 -2 -8 -.74
MIT | 1 | .0 -8.4 5.8 -26 84 -7 -.13
NGS | 1 | -5.7 -11.6 6.4 -72 82 -28 -.28
SIO | 1 | -1.4 -8.0 .7 -39 9 4 -.11
COD | 2 | .3 .3 1.1 14 17 -7 -.41
EMR | 2 | -.2 -6.6 7.2 -24 78 7 -.16
ESA | 2 | .9 -1.6 .0 10 59 27 -.65
GFZ | 2 | -.4 .9 .4 53 19 14 -.45
GRG | 2 | -4.8 -15.9 -6.7 153 35 128 -.53
JPL | 2 | -.8 -14.0 5.4 -7 17 9 -.34
MIT | 2 | -5.8 -5.2 5.9 -26 109 6 -.29
NGS | 2 | -5.3 -16.9 14.2 -122 78 -35 -.33
SIO | 2 | -16.7 -.9 7.7 -15 9 -8 -.28
COD | 3 | .6 -.5 1.4 22 10 23 -.43
EMR | 3 | -.4 .2 3.7 -15 74 -18 -.20
ESA | 3 | 1.1 -1.5 -.6 3 27 24 -.65
GFZ | 3 | -.1 .7 1.1 54 28 29 -.48
GRG | 3 | .5 -3.7 -6.9 136 -8 146 -.46
JPL | 3 | 3.8 -4.9 5.4 10 11 -31 -.63
MIT | 3 | -4.7 -3.1 4.9 -21 53 -26 -.22
NGS | 3 | -7.0 -5.1 -1.7 -32 63 -16 -.36
SIO | 3 | -4.5 -2.3 4.0 -29 -11 4 -.21
COD | 4 | .3 .5 1.3 29 23 -6 -.59
EMR | 4 | -.8 7.1 1.8 -12 76 -24 -.25
ESA | 4 | .2 -.7 -.7 18 33 50 -.67
GFZ | 4 | .2 1.1 1.0 56 17 12 -.51
GRG | 4 | 2.1 -1.8 -3.3 135 21 131 -.43
JPL | 4 | 1.2 -4.9 .6 11 2 -12 -.83
MIT | 4 | -2.6 -1.2 5.2 -11 67 -25 -.33
NGS | 4 | 1.2 -1.9 7.0 -1 44 -9 -.40
SIO | 4 | -6.8 -2.1 8.9 -18 0 -18 -.48
COD | 5 | .2 .1 1.6 20 22 -12 -.56
EMR | 5 | 7.3 -3.8 1.4 -21 73 -13 -.23
ESA | 5 | -.1 -.9 -1.0 7 48 38 -.80
GFZ | 5 | -.1 .9 1.0 44 19 12 -.54
GRG | 5 | 3.5 -3.6 -4.9 118 1 142 -.44
JPL | 5 | 4.2 -6.8 -3.5 8 10 -8 -.65
MIT | 5 | 1.2 -4.9 4.7 -24 79 -26 -.32
NGS | 5 | 1.5 -4.4 -1.8 -15 36 -28 -.41
SIO | 5 | .1 -6.6 8.1 -23 13 -4 -.33
COD | 6 | .4 .2 1.4 19 19 -8 -.68
EMR | 6 | 2.4 -2.7 1.9 -21 61 -28 -.29
ESA | 6 | -.5 -1.2 -.6 13 55 26 -.81
GFZ | 6 | -.1 .8 1.3 46 25 25 -.55
GRG | 6 | 1.3 -3.4 -10.7 109 19 132 -.43
JPL | 6 | .6 -9.5 -2.7 0 0 1 -.59
MIT | 6 | -1.1 -5.7 4.5 -14 56 -35 -.43
NGS | 6 | -.4 -13.6 5.1 -64 53 7 -.33
SIO | 6 | -4.4 -6.8 7.9 -19 16 -7 -.31
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 1.2063.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2063.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 2.2063.[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 3.2063.[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 5.2063.0-6). 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 2063 summary. (Jul 21, 2019 - Jul 27, 2019)
Table 1.2063.a GPS week: 2063 MJD: 58685.000-58691.000
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 247| 0 0 -2 18 12 -9 -.01 9 9 | -709 120 7 94
| 0 0 2 16 19 15 .03 | 213 273
emr 80| -1 -1 3 -11 4 36 .14 12 11 | 171999 109 14 98
| 1 1 1 9 14 13 .01 | 14917 696
esa 150| -1 0 -1 -6 0 -6 -.14 15 10 | 1896 196 8 124
| 0 0 1 5 8 18 .04 | 2633 1245
gfz 183| 0 0 1 -9 0 -11 .05 12 10 | 27 -150 12 203
| 0 0 3 19 9 24 .03 | 415 681
grg 101| 3 0 -6 -13 5 25 -.08 18 11 | -10 -7 11 141
| 0 0 3 6 17 14 .02 | 268 381
igr n/a| 0 1 0 -23 -39 -7 -.05 4 4 | -15361 214 12 77
| 0 0 0 7 8 11 .01 | 1215 771
jpl 80| 0 0 1 7 -17 20 .12 7 7 | 213179 101 9 88
| 0 0 1 14 12 28 .02 | 758 761
mit 348| 0 -1 4 -9 0 10 -.06 15 13 | -420 52 72 1635
| 0 0 0 16 22 14 .01 | 193 256
ngs 212| 0 0 0 19 7 -29 -.08 8 7 | 17863 -98785 1075 2138
| 0 0 2 22 14 20 .02 | 48979 261317
sio 319| 0 -1 1 -28 -13 -9 -.06 17 16 | --- --- --- ---
| 0 1 3 23 22 60 .06 | --- ---
Table 1.2063.b GPS week : 2063 MJD: 58685.000-58691.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 4 4 4 3 3 3 |
2 | 4 4 4 4 3 3 4 |
3 | 3 4 14 4 4 4 4 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 4 4 4 3 4 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 4 4 13 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 4 4 13 4 5 4 4 |
11 | 3 4 4 4 4 4 3 |
12 | 5 4 4 5 4 4 4 |
13 | 3 3 3 3 3 3 3 |
14 | 3 4 4 3 4 4 4 |
15 | 3 4 4 4 3 3 3 |
16 | 6 5 5 5 4 4 4 |
17 | 3 4 4 4 4 4 3 |
18 | 3 4 4 4 3 3 3 |
19 | 4 4 5 5 4 4 4 |
20 | 4 4 7 0 5 4 3 |
21 | 4 4 4 4 4 3 4 |
22 | 4 3 5 3 4 3 3 |
23 | 4 4 4 4 4 4 4 |
24 | 3 3 4 4 4 3 3 |
25 | 6 4 4 5 4 4 4 |
26 | 5 7 6 5 5 11 7 |
27 | 3 9 4 3 4 3 3 |
28 | 3 4 4 4 4 3 4 |
29 | 4 4 4 4 4 4 4 |
30 | 2 3 3 3 3 3 3 |
31 | 3 4 4 3 3 3 3 |
32 | 3 3 4 4 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 2.2063.0 GPS week: 2063 Day: 0 MJD: 58685.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 251| 1 0 0 26 -1 -13 .00 9 8 | -613 -95 7 79
emr 80| -4 -3 0 4 8 27 .12 12 12 | 176990 167 15 78
esa 150| 0 0 -3 -1 -4 3 -.14 9 9 | 3338 603 9 132
gfz 183| 0 0 4 22 -1 -40 .03 15 12 | 425 -609 12 260
grg 101| 3 0 -1 -5 11 24 -.09 13 11 | 267 -240 13 156
igr n/a| 0 0 0 -16 -41 -19 -.05 4 3 | -16852 239 12 89
jpl 80| 0 0 0 -5 -13 45 .16 7 7 | 212480 165 9 105
mit 349| 1 0 4 1 -8 34 -.06 14 13 | -358 176 73 1772
ngs 211| 0 0 -2 -23 23 -57 -.05 7 6 | -602 -133 988 2234
sio 315| 0 -2 2 -11 -39 5 -.06 15 15 | --- --- --- ---
Table 2.2063.1 GPS week: 2063 Day: 1 MJD: 58686.000
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 227| 1 0 -4 -4 -12 -14 -.02 10 10 | -618 15 7 109
emr 80| -3 -3 1 -19 -3 10 .13 11 11 | 138209 -1295 16 93
esa 150| -1 0 -2 -14 -6 -27 -.15 10 10 | 4185 -1911 8 120
gfz 185| 0 2 3 -23 -5 -12 .06 12 11 | 623 -1272 12 195
grg 101| 3 0 -4 -14 -18 36 -.08 13 11 | 349 -650 10 136
igr n/a| 0 2 0 -28 -32 -20 -.03 4 4 | -16264 -993 13 76
jpl 80| 0 0 1 36 -11 31 .12 7 7 | 212892 -1255 10 71
mit 348| 0 0 3 -12 33 6 -.07 15 14 | -185 -386 79 1693
ngs 210| 0 1 2 14 10 -32 -.11 8 7 | -596 -27 1241 1941
sio 320| 0 -3 0 -1 15 76 -.08 18 18 | --- --- --- ---
Table 2.2063.2 GPS week: 2063 Day: 2 MJD: 58687.000
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 -5 38 26 -24 -.07 11 10 | -613 91 9 102
emr 80| 0 -2 1 -4 -1 41 .15 15 12 | 176392 827 16 119
esa 150| -2 0 1 -8 12 -16 -.20 12 11 | -1789 372 10 133
gfz 184| 1 1 5 -18 6 -48 -.01 14 12 | -368 19 13 187
grg 101| 1 0 -11 -12 31 24 -.10 55 12 | -291 33 13 143
igr n/a| 0 1 0 -23 -50 -17 -.06 6 5 | -16661 1341 14 84
jpl 80| 0 0 2 -3 -23 56 .14 10 10 | 212125 1082 11 87
mit 348| 0 0 3 -16 7 17 -.05 15 13 | -409 -166 68 1564
ngs 212| 0 0 2 35 -22 -46 -.05 10 8 | -383 -240 1185 2065
sio 322| 0 0 -4 -40 -15 10 .05 23 21 | --- --- --- ---
Table 2.2063.3 GPS week: 2063 Day: 3 MJD: 58688.000
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 35 42 -25 .00 9 9 | -455 -106 7 90
emr 80| -1 -1 3 -22 31 36 .16 11 11 | 177925 598 14 102
esa 150| -1 0 -1 -9 10 -30 -.17 11 10 | -2020 1953 11 133
gfz 183| 0 0 0 -2 16 -1 .04 10 11 | -115 334 11 183
grg 102| 3 0 -10 -24 -5 23 -.09 12 10 | -65 268 12 130
igr n/a| 0 0 0 -36 -31 -3 -.06 4 4 | -14822 908 11 66
jpl 80| 0 0 3 12 -37 26 .13 7 7 | 213577 705 9 92
mit 349| 0 -1 4 -38 -30 13 -.06 16 15 | -287 183 76 1552
ngs 211| 0 0 -2 24 2 -4 -.11 9 8 | 128937 -691397 953 2026
sio 319| 0 -1 2 -67 -30 -56 -.05 18 18 | --- --- --- ---
Table 2.2063.4 GPS week: 2063 Day: 4 MJD: 58689.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 256| 0 0 -2 15 -1 0 .01 8 8 | -693 130 6 93
emr 80| -2 0 2 -7 8 43 .15 12 12 | 178451 -83 13 95
esa 150| 0 0 -1 -1 -3 12 -.12 9 9 | 3364 -89 8 118
gfz 184| 0 0 2 -33 -11 5 .05 10 9 | 238 -133 14 200
grg 103| 3 1 -3 -10 16 -3 -.06 11 10 | 148 -4 10 151
igr n/a| 0 0 0 -23 -30 11 -.04 4 4 | -13870 -300 11 69
jpl 80| -1 0 0 -3 -22 -15 .11 7 7 | 214262 -341 9 80
mit 349| 0 0 3 1 22 14 -.05 14 13 | -450 213 62 1721
ngs 214| 0 -1 1 41 16 -4 -.08 9 7 | -704 40 1020 2106
sio 321| 0 -1 2 -27 18 -7 -.04 16 15 | --- --- --- ---
Table 2.2063.5 GPS week: 2063 Day: 5 MJD: 58690.000
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 1 -1 17 11 -7 .00 8 7 | -1104 703 8 101
emr 80| 0 -2 4 -17 4 43 .13 11 11 | 178274 59 14 98
esa 150| -1 0 -1 -1 3 7 -.10 9 9 | 2694 1091 7 115
gfz 185| -1 0 -4 -16 -6 0 .09 9 9 | -506 872 13 208
grg 101| 2 0 -4 -8 -11 33 -.08 10 10 | -322 566 9 135
igr n/a| -1 1 0 -12 -45 0 -.04 4 4 | -14183 -59 12 75
jpl 80| 1 0 2 12 0 -17 .11 7 7 | 213834 -43 11 103
mit 349| 0 -1 4 -12 -3 -5 -.06 14 13 | -800 359 93 1433
ngs 212| 0 0 0 10 14 -25 -.07 7 7 | -907 421 1082 2270
sio 318| 1 -2 4 -10 -29 17 -.11 16 16 | --- --- --- ---
Table 2.2063.6 GPS week: 2063 Day: 6 MJD: 58691.000
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 258| 0 1 -2 1 25 20 .01 8 8 | -868 104 6 90
emr 80| 0 0 6 -12 -17 50 .13 11 11 | 177753 490 14 105
esa 150| -1 -1 0 -6 -10 5 -.07 48 11 | 3504 -646 8 118
gfz 183| 0 0 0 6 0 15 .07 13 10 | -105 -265 13 189
grg 101| 2 0 -10 -20 13 39 -.04 12 11 | -157 -27 10 140
igr n/a| 0 0 -1 -20 -46 -3 -.03 4 4 | -14878 367 11 80
jpl 80| 0 0 0 2 -9 14 .10 7 7 | 213087 399 9 82
mit 348| 1 -1 5 12 -18 -8 -.05 14 13 | -457 -11 55 1716
ngs 214| 0 0 1 34 7 -39 -.09 7 6 | -700 -165 1062 2329
sio 324| 0 0 5 -42 -10 -115 -.12 13 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 3.2063.0 GPS week: 2063 Day: 0 MJD: 58685.000
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 14 10 8 3 8 12 5 11 3 | 19 22 18 19 22 17 19 20 19 22 18
2 | 10 10 6 7 10 4 6 17 7 19 3 | 23 26 23 25 21 23 24 30 21 25 22
3 | 7 11 12 6 15 2 8 7 6 9 3 | 477 328 478 478 508 478 475 477 479 480 478
X4 | 350 --- 2 --- --- 340 --- --- --- --- 0 | 34 --- 207 --- --- 112 --- --- --- --- 198
5 | 9 10 7 7 11 4 7 13 9 20 3 | 51 49 47 50 51 48 51 50 48 48 49
6 | 14 14 9 11 13 3 7 12 8 10 3 | 24 25 21 22 23 19 23 22 19 22 20
7 | 5 12 6 7 8 4 8 24 8 18 3 | 48 46 44 45 47 42 46 44 43 44 44
8 | 9 11 11 10 10 2 7 8 6 10 3 | 27 29 28 27 31 27 28 27 33 25 29
9 | 11 9 6 8 6 3 10 7 4 12 3 | 32 36 29 30 28 30 38 32 30 36 32
10 | 9 12 18 16 15 2 7 12 5 9 4 | 424 429 425 425 426 425 427 426 425 422 426
11 | 5 11 12 11 11 3 6 13 5 12 3 | 30 35 31 34 33 30 32 32 30 29 30
12E | 10 14 8 27 23 5 6 15 12 17 5 | 57 59 60 67 59 60 59 59 60 61 59
13 | 9 8 7 9 6 4 5 12 8 17 3 | 25 31 23 22 23 24 30 30 28 33 25
14 | 9 9 7 8 5 3 5 18 5 16 3 | 28 28 27 26 29 27 29 36 28 35 27
15 | 8 8 8 7 6 4 7 14 6 20 3 | 66 65 62 61 64 63 62 60 59 60 62
16E | 15 22 8 8 30 4 10 26 13 12 5 | 82 84 82 79 77 81 82 78 81 77 79
17 | 7 10 6 8 11 3 6 15 7 17 3 | 23 26 18 23 23 19 24 24 21 21 21
18 | 8 8 10 9 13 4 6 10 6 15 3 | 19 24 45 19 24 19 22 23 23 29 20
19 | 10 14 6 7 12 4 5 18 8 23 3 | 26 30 26 30 25 25 28 29 24 27 26
20E | 12 12 7 15 17 5 7 12 9 14 4 | 24 20 23 21 16 24 19 25 26 15 24
21 | 7 13 9 7 13 4 7 15 10 18 3 | 18 24 16 15 20 15 19 21 18 20 16
22 | 6 11 6 8 18 4 5 12 6 17 3 | 76 77 75 77 74 74 77 74 75 71 75
23 | 7 18 5 8 7 3 6 15 4 16 3 | 19 18 18 21 21 19 21 22 20 22 18
24 | 9 9 6 7 9 3 6 11 6 16 3 | 22 26 22 24 20 21 27 23 23 31 23
X25E | 9 --- 18 31 10 4 11 13 15 16 6 | 24 --- 21 38 24 21 26 23 26 24 22
26E | 11 11 14 64 17 4 6 14 10 13 4 | 22 26 20 63 35 24 24 24 26 21 24
27 | 9 13 10 11 9 2 7 8 6 9 3 | 29 29 30 32 33 29 28 27 27 26 30
28E | 6 11 9 9 14 3 7 9 6 14 3 | 69 70 73 72 68 70 69 72 69 69 69
29 | 8 16 9 9 9 4 6 15 8 19 3 | 29 29 25 30 27 25 29 26 26 30 26
30 | 5 8 6 7 8 2 5 6 6 10 2 | 27 30 24 27 27 25 30 25 25 29 27
31 | 5 8 8 7 10 4 5 17 6 21 3 | 36 37 34 35 38 32 37 26 32 31 33
32 | 6 9 5 11 7 3 9 12 8 13 3 | 35 39 34 36 33 34 41 36 36 39 36
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 9 15 13 4 7 14 7 15 |T 60 59 65 63 62 61 62 62 61 62 65
WRMS | 8 12 9 12 11 3 7 13 6 15 |NE 29 31 36 28 29 30 30 29 27 30 35
MEDI | 9 11 8 8 10 4 7 13 6 16 |MD 28 30 28 30 29 27 29 29 28 30 27
Table 3.2063.1 GPS week: 2063 Day: 1 MJD: 58686.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 8 16 11 8 4 7 12 8 16 3 | 22 23 21 19 24 21 22 20 22 29 21
2 | 9 12 7 17 10 4 8 19 8 20 4 | 23 28 25 28 20 24 24 29 26 27 23
3 | 7 10 15 7 19 3 9 8 9 13 4 | 473 390 476 475 487 476 474 476 474 474 474
X4 | 370 --- 3 --- --- 361 --- --- --- --- 0 | 34 --- 239 --- --- 101 --- --- --- --- 257
5 | 11 10 6 8 11 4 8 13 9 19 3 | 44 45 43 42 45 43 47 46 46 42 44
6 | 12 14 10 9 13 3 6 12 8 19 3 | 21 26 20 21 21 19 22 22 21 25 20
7 | 8 9 7 9 9 4 6 25 8 20 3 | 28 26 22 26 24 23 25 30 26 28 24
8 | 11 10 12 8 10 4 7 9 6 18 3 | 23 23 23 22 23 20 22 21 22 28 22
9 | 8 8 6 6 10 3 7 7 7 13 2 | 22 30 23 23 24 23 31 23 24 29 24
10 | 9 10 16 9 18 4 8 12 5 14 4 | 480 475 474 477 488 476 475 474 471 477 476
11 | 8 9 15 8 10 4 6 13 6 17 3 | 22 26 23 20 21 21 25 20 23 23 21
12E | 10 16 10 7 10 5 6 17 14 17 4 | 47 48 47 47 44 46 45 45 48 44 45
13 | 8 9 8 8 6 4 7 14 8 17 3 | 18 22 17 17 17 18 22 23 17 26 18
14 | 9 8 7 8 6 3 6 18 6 21 3 | 19 15 16 21 20 16 16 23 17 27 16
15 | 8 8 5 6 6 6 9 16 9 22 3 | 43 43 38 42 41 40 41 37 38 41 40
16E | 11 19 8 7 25 6 8 21 10 15 5 | 68 68 70 68 71 67 68 68 66 64 67
17 | 8 9 7 8 10 5 6 16 9 20 3 | 20 24 17 21 20 19 23 25 21 22 19
18 | 14 8 10 10 15 3 6 13 5 19 3 | 26 26 38 20 24 22 24 22 26 30 23
19 | 13 14 7 9 12 5 5 19 12 25 4 | 22 22 18 20 17 18 20 23 22 24 18
20E | 10 9 8 9 17 5 6 14 7 19 3 | 21 22 20 20 16 18 19 20 19 14 17
21 | 10 11 8 7 15 5 8 13 10 18 3 | 20 25 18 18 18 17 22 21 17 21 17
22 | 9 8 6 8 15 3 5 14 7 17 3 | 69 68 67 66 71 66 68 66 69 62 67
23 | 8 18 7 7 9 4 7 18 6 19 3 | 15 14 12 16 15 14 14 18 15 20 12
24 | 10 8 7 8 8 5 7 11 9 20 3 | 20 26 21 18 20 19 25 22 21 28 21
25E | 11 12 14 12 8 4 7 11 9 15 4 | 19 25 22 21 18 18 19 17 21 18 17
26E | 16 9 19 45 22 7 7 14 6 15 7 | 26 27 23 51 30 25 24 25 25 22 26
X27 | 7 --- --- --- 9 11 --- --- --- --- 8 | 31 --- --- --- 30 28 --- --- --- --- 30
28E | 8 10 9 10 19 6 5 12 9 19 3 | 59 62 61 60 59 61 60 64 57 63 59
29 | 10 17 6 9 11 6 7 14 11 19 4 | 27 23 18 25 19 19 20 21 22 23 20
30 | 9 6 6 9 8 3 6 3 6 17 2 | 21 24 20 20 19 19 25 19 22 31 21
31 | 11 8 8 5 10 4 6 19 11 22 3 | 25 27 20 22 23 21 26 19 25 24 22
32 | 12 10 6 8 8 3 8 11 9 15 3 | 33 35 28 29 29 29 35 29 28 32 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 10 12 13 4 7 15 8 18 |T 57 57 63 59 58 57 59 58 58 60 62
WRMS | 10 11 10 10 11 4 7 14 7 18 |NE 24 25 32 22 22 25 24 23 22 26 32
MEDI | 9 9 8 8 10 4 7 13 8 18 |MD 23 26 23 22 23 21 24 23 23 28 22
Table 3.2063.2 GPS week: 2063 Day: 2 MJD: 58687.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 12 19 12 9 4 7 11 8 16 4 | 31 33 27 26 33 26 30 26 29 35 28
2 | 8 7 6 11 12 5 7 16 7 26 3 | 20 24 24 28 23 24 23 30 26 36 23
X3 | 34 --- 19 26 359 20 113 27 36 38 13 | 9999 --- 9999 9999 9999 9999 9999 9999 9999 9999 9999
X4 | 4 --- 365 --- --- 358 --- --- --- --- 0 | 29 --- 226 --- --- 283 --- --- --- --- 113
5 | 8 10 8 7 13 4 7 12 10 26 3 | 41 43 43 43 45 41 44 45 45 48 43
6 | 9 13 11 13 13 3 7 12 8 24 4 | 25 32 27 27 31 26 30 28 32 35 27
7 | 8 11 10 8 9 6 6 26 9 22 4 | 45 45 39 41 47 39 43 45 45 48 42
8 | 10 10 15 13 10 4 8 9 9 17 3 | 37 39 38 34 38 33 39 36 40 37 37
9 | 14 9 8 7 10 3 9 9 6 14 3 | 23 32 25 21 27 23 33 24 27 31 25
10 | 30 54 29 27 293 20 40 26 27 32 13 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
11 | 11 10 18 13 11 4 6 12 7 18 4 | 34 34 28 32 33 28 33 30 30 32 30
12E | 7 16 6 9 17 4 9 14 14 24 4 | 30 31 30 31 30 29 31 29 35 41 29
13 | 6 9 7 11 6 5 4 13 9 23 3 | 32 36 34 34 34 34 36 39 35 42 34
14 | 9 9 9 9 10 4 6 19 8 24 3 | 42 42 42 40 45 41 43 42 39 48 41
15 | 8 8 5 7 9 4 5 15 11 26 3 | 48 47 43 45 50 46 46 43 46 50 45
16E | 10 19 8 11 13 5 7 19 11 24 4 | 34 30 31 33 31 30 29 33 35 40 30
17 | 11 13 6 14 11 4 6 17 8 28 4 | 28 29 23 29 26 24 28 28 29 35 26
18 | 14 9 14 13 14 6 6 10 8 19 4 | 29 28 39 22 31 20 26 23 25 34 23
19 | 10 18 8 9 11 5 6 20 9 32 4 | 32 35 32 31 32 31 33 36 35 41 32
X20E | 16 --- 8 --- --- 7 --- 10 8 --- 6 | 28 --- 22 --- --- 22 --- 27 31 --- 26
21 | 9 9 8 12 12 4 7 13 9 23 3 | 31 29 27 29 27 27 30 26 29 31 27
22 | 12 10 8 22 17 7 7 15 9 21 4 | 94 95 94 92 97 93 98 94 98 96 95
23 | 14 16 10 6 12 5 6 19 10 20 4 | 27 31 28 26 30 26 28 30 32 32 27
24 | 14 10 6 9 10 5 5 10 11 29 4 | 28 29 28 27 24 27 32 27 28 44 27
25E | 7 14 17 13 8 4 6 10 11 25 4 | 28 28 25 30 25 28 30 29 36 40 28
26E | 15 11 19 39 21 5 8 15 6 23 6 | 26 28 27 46 38 27 28 29 28 30 27
27 | 11 9 14 15 9 3 7 10 7 16 3 | 29 31 32 32 31 27 31 30 33 36 29
28E | 10 9 10 15 20 5 6 15 9 22 4 | 23 28 26 27 29 24 24 24 30 35 24
29 | 6 17 8 12 9 6 8 16 7 29 4 | 30 32 32 35 30 31 32 32 34 42 31
30 | 8 8 10 7 10 3 4 10 8 18 3 | 34 38 33 32 34 33 38 34 39 41 35
31 | 11 9 8 7 9 5 8 17 9 25 3 | 41 39 35 36 40 34 39 31 35 39 36
32 | 9 11 8 11 11 3 9 10 8 20 3 | 24 30 27 28 28 25 32 25 25 35 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 12 14 55 6 10 15 10 23 |T 33 35 39 34 35 40 35 33 35 40 35
WRMS | 10 12 11 12 12 5 10 13 8 21 |NE 31 34 40 31 33 41 33 31 33 38 34
MEDI | 10 10 8 11 11 5 7 14 9 23 |MD 30 32 30 31 31 28 32 30 33 37 29
Table 3.2063.3 GPS week: 2063 Day: 3 MJD: 58688.000
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 9 10 3 7 13 5 13 3 | 23 24 22 19 26 20 20 21 20 27 21
2 | 9 7 6 8 10 5 6 18 8 20 3 | 21 22 21 26 21 23 21 27 24 31 21
3 | 12 11 14 5 18 5 12 13 8 9 4 | 672 9999 674 670 676 670 669 666 668 673 671
X4 | 3 --- 349 --- --- 367 --- --- --- --- 0 | 24 --- 203 --- --- 281 --- --- --- --- 81
5 | 8 9 9 8 17 4 8 15 9 19 3 | 46 44 44 44 41 42 45 44 43 45 43
6 | 9 15 10 9 12 2 7 15 12 17 4 | 21 26 21 18 23 19 24 23 23 25 20
7 | 8 8 9 8 8 4 7 26 8 21 3 | 35 34 37 42 39 33 34 35 40 32 36
X8 | 15 16 --- --- 18 21 --- 15 42 --- 13 | 29 30 --- --- 27 25 --- 26 61 --- 32
9 | 9 8 5 7 8 3 8 10 9 13 3 | 21 29 22 25 21 20 28 21 23 27 23
10 | 7 11 16 10 21 4 9 13 8 12 4 | 650 649 650 649 637 648 647 647 651 647 648
11 | 9 7 16 9 12 3 6 14 7 17 3 | 29 32 24 27 30 27 29 28 27 29 27
12E | 10 15 12 13 30 7 6 19 8 20 5 | 41 37 37 43 44 39 37 38 39 46 38
13 | 8 8 8 7 9 5 5 15 6 20 3 | 19 21 16 17 16 16 21 22 15 27 17
14 | 6 10 8 5 9 4 4 20 5 21 3 | 18 17 16 17 17 15 14 22 16 23 15
15 | 8 8 7 8 11 4 7 16 7 20 3 | 47 48 45 47 52 45 47 40 43 43 45
16E | 7 22 8 14 12 3 9 16 11 14 4 | 29 32 31 30 34 29 30 31 29 37 30
17 | 8 13 7 5 10 4 5 18 9 22 3 | 21 22 16 20 21 18 23 21 23 23 19
18 | 6 7 13 13 14 4 5 11 8 19 3 | 21 23 40 17 28 18 21 21 18 33 19
19 | 13 16 9 8 11 5 5 21 12 26 4 | 22 24 20 22 20 19 22 22 22 23 19
X20E | 3 --- --- --- --- 63 --- --- --- --- 0 | 33 --- --- --- --- 32 --- --- --- --- 34
21 | 11 8 8 7 12 5 7 14 10 16 3 | 26 22 17 21 20 19 20 22 21 22 19
22E | 9 9 8 6 12 10 5 18 9 15 3 | 72 73 71 73 73 71 75 73 75 70 72
23 | 8 16 6 7 6 3 6 19 9 19 3 | 18 18 18 19 19 16 18 22 20 26 17
24 | 9 8 7 10 9 4 7 11 9 20 3 | 23 28 23 22 22 21 27 23 22 34 23
25E | 10 13 18 17 8 4 6 14 9 20 4 | 24 24 23 32 24 22 25 24 23 34 23
26E | 9 12 17 26 15 3 7 16 9 14 5 | 29 26 21 41 35 29 23 27 22 28 28
27 | 7 7 13 7 7 4 7 11 9 14 3 | 26 29 29 29 30 25 27 25 25 33 26
28E | 9 7 8 11 14 4 6 14 10 17 3 | 32 31 29 28 29 28 28 28 30 34 28
29 | 10 17 7 9 10 4 7 15 9 19 4 | 28 25 20 27 24 21 23 22 23 28 22
30 | 8 7 8 7 9 3 7 7 7 17 3 | 25 26 23 22 23 21 24 20 25 29 23
31 | 5 8 7 5 8 5 6 19 6 22 3 | 32 34 30 34 37 31 34 26 35 34 32
32 | 14 8 5 7 7 4 9 13 7 15 3 | 17 26 17 18 20 19 28 21 17 30 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 11 10 12 4 7 16 9 18 |T 67 50 75 72 70 73 71 69 70 75 68
WRMS | 9 11 10 11 10 4 7 15 8 18 |NE 24 26 32 24 25 34 25 24 25 28 26
MEDI | 8 9 8 8 10 4 7 15 9 19 |MD 26 26 23 27 26 23 27 24 23 31 23
Table 3.2063.4 GPS week: 2063 Day: 4 MJD: 58689.000
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 12 8 8 2 6 11 7 13 3 | 21 23 23 21 25 20 22 19 21 28 21
2 | 8 9 6 10 10 4 7 16 7 18 3 | 20 25 21 24 22 23 22 28 23 27 21
3 | 8 10 14 7 14 5 9 12 8 12 3 | 9999 661 9999 9999 9999 9999 9999 9999 9999 9999 9999
X4 | 1 --- 345 --- --- 23 --- --- --- --- 0 | 20 --- 204 --- --- 93 --- --- --- --- 52
5 | 11 11 6 9 9 2 9 12 8 15 3 | 59 57 57 59 60 58 57 60 64 58 58
6 | 10 14 10 10 12 4 7 13 8 13 3 | 19 27 19 18 23 18 23 20 19 23 19
7 | 8 9 9 10 6 3 6 25 6 17 3 | 36 38 35 38 35 34 38 37 35 34 35
8 | 5 8 11 11 10 2 8 10 7 14 3 | 24 24 26 27 27 22 28 23 19 31 22
9 | 9 8 6 7 7 2 6 10 9 10 2 | 20 29 22 24 22 21 29 20 20 24 22
10 | 8 13 17 14 23 3 8 11 8 9 4 | 802 803 808 806 802 805 807 803 804 804 805
11 | 9 7 13 6 11 3 6 11 9 17 3 | 25 29 24 26 26 25 27 24 29 26 25
12E | 6 18 8 9 11 3 8 13 12 17 4 | 42 42 41 44 43 41 41 42 45 48 42
13 | 9 8 7 9 9 4 6 11 8 12 3 | 21 24 19 22 21 20 25 26 22 24 21
14 | 8 10 7 8 8 3 7 18 5 19 3 | 27 28 27 32 28 27 30 32 27 31 27
15 | 9 12 7 9 9 4 7 14 7 14 3 | 42 46 38 38 42 39 43 37 37 38 40
16E | 7 18 8 7 10 5 7 14 7 15 3 | 40 43 40 42 43 40 38 38 43 41 40
17 | 9 9 6 7 10 4 5 17 8 22 3 | 23 24 18 22 21 20 23 23 24 26 21
18 | 6 8 9 9 12 5 7 10 8 15 3 | 18 24 39 18 27 18 21 20 20 30 20
19 | 9 14 6 7 12 5 5 19 8 26 4 | 22 24 22 24 20 20 22 25 24 26 21
20E | 11 14 8 20 12 6 6 17 12 15 4 | 29 34 32 29 37 29 30 31 35 35 28
21 | 11 13 7 8 10 5 6 16 14 19 4 | 22 21 13 18 19 15 17 19 18 18 15
22E | 6 8 6 8 17 4 5 13 9 16 3 | 68 68 66 68 65 66 66 65 67 65 66
23 | 7 19 8 7 9 3 3 16 7 19 3 | 15 17 13 18 19 15 17 18 17 20 15
24 | 8 16 7 10 8 4 6 8 8 18 3 | 16 28 18 16 17 18 25 21 19 32 19
25E | 6 12 17 11 6 2 7 10 12 12 3 | 19 18 18 24 22 18 21 19 22 23 18
26E | 10 14 14 17 17 5 7 17 8 13 4 | 24 21 18 31 32 24 22 24 25 25 25
27 | 9 10 9 15 7 2 6 10 6 11 3 | 31 29 28 35 31 30 31 28 28 34 31
28E | 8 12 8 11 10 4 5 15 11 17 3 | 32 33 33 35 33 33 31 35 33 35 31
29 | 7 19 7 9 7 3 8 17 9 15 3 | 22 20 16 23 23 18 18 19 21 20 19
30 | 9 6 8 6 8 3 6 9 7 13 2 | 22 27 22 23 21 22 28 19 26 28 23
31 | 5 7 7 4 9 3 8 17 5 22 3 | 31 35 30 31 33 29 37 25 29 30 31
32 | 6 8 6 5 7 3 8 8 9 13 2 | 24 29 22 25 24 23 30 24 23 31 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 9 10 11 4 7 14 9 16 |T 52 75 58 55 55 54 55 54 54 57 53
WRMS | 8 12 9 9 10 4 7 13 7 15 |NE 23 27 31 24 25 25 26 24 23 27 24
MEDI | 8 10 8 9 10 3 7 13 8 15 |MD 24 28 24 25 26 23 28 24 24 30 24
Table 3.2063.5 GPS week: 2063 Day: 5 MJD: 58690.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 8 14 10 9 3 7 10 6 15 3 | 21 23 21 21 25 20 24 20 21 29 22
2 | 6 6 6 8 9 4 5 15 9 23 3 | 21 24 22 25 21 23 23 29 24 27 22
3 | 9 11 13 7 14 4 9 11 6 10 3 | 766 625 771 766 775 769 767 768 769 769 768
X4 | 1 --- 331 --- --- 66 --- --- --- --- 0 | 25 --- 194 --- --- 71 --- --- --- --- 48
5E | 6 10 7 7 10 3 8 11 9 17 3 | 70 69 69 72 71 70 70 70 74 74 71
6 | 7 13 11 9 12 3 7 12 6 14 3 | 20 27 21 20 22 19 24 21 20 23 20
7 | 5 8 9 9 8 3 6 27 8 19 3 | 29 32 29 35 31 29 32 32 32 29 30
8 | 9 9 12 8 10 4 9 12 6 9 3 | 25 25 24 23 27 21 26 23 23 26 23
9 | 8 9 5 8 9 3 6 11 5 12 2 | 27 34 28 31 26 28 33 27 29 32 29
10 | 14 10 16 12 12 4 11 11 10 10 4 | 639 634 633 639 632 635 635 633 634 636 635
11 | 9 8 16 9 10 3 6 11 9 15 3 | 23 28 22 24 22 22 27 21 23 22 22
12E | 6 16 9 7 12 4 7 16 11 16 3 | 48 48 46 49 49 48 49 45 52 48 47
13 | 7 9 7 8 8 4 6 13 6 17 3 | 19 27 21 23 21 21 26 25 19 27 21
14 | 8 11 7 7 9 4 5 19 5 19 3 | 29 28 25 26 28 26 26 31 26 33 26
15 | 7 10 5 7 10 4 5 15 8 19 3 | 38 36 32 37 34 34 34 33 33 37 34
16E | 8 21 7 10 9 4 7 15 8 15 3 | 42 46 45 45 46 44 43 42 45 44 43
17 | 7 10 7 7 10 4 6 17 6 22 3 | 20 26 17 21 21 18 24 22 21 24 19
18 | 6 9 10 11 13 10 6 11 6 15 3 | 15 21 89 16 23 18 21 19 17 28 18
19 | 6 16 6 9 10 5 6 19 9 24 4 | 27 33 29 32 24 28 31 32 26 34 28
20E | 12 10 8 9 15 5 8 13 10 15 3 | 29 27 26 24 22 30 25 25 25 22 28
21 | 6 9 5 7 11 5 8 13 9 18 3 | 19 20 16 20 18 18 20 20 17 20 17
22E | 9 7 8 6 12 5 4 15 5 16 3 | 64 62 61 63 60 62 63 61 62 56 62
23 | 8 18 6 7 7 5 6 19 5 20 3 | 16 18 16 19 16 15 16 15 15 21 15
24 | 7 10 5 8 9 4 5 8 6 19 3 | 22 27 18 22 22 20 26 23 23 33 22
25E | 5 10 16 13 8 4 7 12 9 13 3 | 17 17 18 22 17 16 18 19 18 21 16
X26E | 8 --- --- --- 13 10 --- --- --- --- 10 | 37 --- --- --- 46 36 --- --- --- --- 40
27 | 8 8 12 9 8 4 8 9 7 10 3 | 23 26 28 27 25 25 24 24 24 25 24
28E | 8 8 7 10 14 3 6 12 7 17 3 | 33 34 33 32 34 32 32 35 35 38 32
29 | 7 16 6 8 7 4 7 19 10 18 3 | 23 22 18 24 20 19 21 24 23 25 20
30 | 6 7 6 8 10 2 6 9 6 13 2 | 22 26 22 24 19 23 27 19 24 28 23
31 | 6 7 9 6 9 5 9 15 8 19 3 | 26 29 25 28 28 24 29 24 25 29 25
32 | 7 7 5 7 8 4 7 10 6 10 2 | 29 32 29 31 26 27 32 28 27 31 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 11 9 9 10 4 7 14 7 16 |T 70 70 78 74 72 71 74 73 73 76 71
WRMS | 7 11 9 9 10 4 7 13 7 16 |NE 23 26 33 25 23 24 26 24 23 27 24
MEDI | 7 9 7 8 10 4 6 12 7 16 |MD 25 27 26 25 25 25 26 25 24 29 25
Table 3.2063.6 GPS week: 2063 Day: 6 MJD: 58691.000
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 7 8 2 6 11 6 7 3 | 21 23 24 23 26 21 24 21 22 23 22
2 | 10 5 6 9 12 4 8 17 7 14 3 | 25 26 25 26 22 26 26 33 27 29 24
3E | 11 10 13 10 22 3 11 12 8 8 4 | 842 604 843 840 858 843 840 843 841 843 841
X4 | 2 --- 369 --- --- 28 --- --- --- --- 0 | 19 --- 224 --- --- 60 --- --- --- --- 71
5E | 7 12 7 15 12 4 10 12 8 13 3 | 92 90 90 89 86 90 91 92 97 90 91
6 | 9 11 11 11 15 4 8 9 5 10 3 | 21 26 25 23 25 20 25 22 25 21 22
7 | 5 8 8 10 8 4 5 26 6 15 3 | 46 47 49 50 49 45 48 44 46 43 46
8 | 10 10 12 8 10 3 7 13 5 8 3 | 26 29 31 29 30 27 29 26 31 25 28
9 | 8 7 5 6 7 2 7 11 6 10 2 | 31 36 30 31 31 32 37 33 35 38 33
10E | 11 13 14 23 12 3 8 12 8 7 4 | 661 661 666 664 668 662 659 660 660 659 661
11 | 7 9 14 8 11 2 6 11 7 10 3 | 32 36 30 34 35 32 36 32 32 28 32
12E | 6 14 8 6 13 4 8 16 9 13 3 | 64 64 64 65 62 62 63 62 60 61 62
13 | 8 8 6 8 6 4 8 15 10 12 3 | 23 31 25 24 25 25 31 32 28 33 26
14 | 8 7 8 9 9 3 7 19 5 16 3 | 33 34 31 34 35 33 33 40 32 39 32
15 | 8 10 6 10 8 4 6 16 7 16 3 | 62 61 60 65 63 61 62 58 63 63 61
16E | 7 23 7 8 12 4 9 17 12 9 4 | 62 64 61 62 63 60 62 61 63 60 61
17 | 7 9 7 7 9 5 6 16 8 17 3 | 21 27 22 22 23 21 25 24 24 21 22
18 | 6 8 264 7 16 5 6 11 6 11 3 | 21 23 117 20 27 18 22 22 22 27 20
19 | 8 15 7 8 11 5 7 20 8 19 4 | 28 31 31 31 27 28 30 33 30 31 29
20E | 8 7 7 15 12 3 6 12 7 12 3 | 42 30 32 28 34 42 32 31 30 38 41
21 | 6 11 6 9 12 4 8 12 9 16 3 | 19 23 15 17 21 16 21 21 19 22 17
22E | 12 6 7 7 12 3 5 15 4 14 3 | 64 63 63 61 69 62 64 58 62 61 63
23 | 8 18 7 6 9 3 4 20 7 20 4 | 21 21 19 18 21 18 21 23 24 24 19
24 | 9 9 7 9 12 4 8 7 5 12 3 | 21 27 22 24 23 21 26 22 24 31 23
25E | 6 15 15 8 10 4 7 6 10 9 3 | 23 25 22 26 20 21 24 23 26 25 21
26E | 9 10 18 46 23 6 6 17 6 10 6 | 35 34 33 55 43 34 33 31 31 26 33
27 | 10 8 12 13 8 2 7 10 6 6 3 | 25 28 30 34 29 28 26 26 29 28 28
28E | 8 11 9 12 14 5 5 14 7 15 3 | 41 43 43 43 40 42 40 45 39 41 40
29 | 6 17 6 9 8 4 9 16 6 15 3 | 28 31 24 29 27 25 27 28 28 30 26
30 | 6 8 6 7 10 3 6 8 6 11 2 | 26 30 27 27 26 25 30 24 29 30 27
31 | 6 8 7 7 8 3 6 15 5 17 3 | 38 39 40 37 42 36 40 30 35 36 37
32 | 7 7 5 6 7 3 7 10 8 11 2 | 36 36 34 35 34 34 38 34 32 40 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 11 48 13 12 4 7 14 7 13 |T 79 75 89 82 83 80 82 81 82 82 81
WRMS | 8 11 11 10 11 4 7 13 6 13 |NE 28 31 42 30 30 29 31 29 30 31 30
MEDI | 8 9 7 8 11 4 7 13 7 12 |MD 28 31 31 31 31 32 32 32 31 31 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 4.2063 GPS week: 2063 MJD: 58685.0-58691.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3052 |U 15 15 40 |U 6 12 23 |U 14 13 35 |
emr | emr 2892 |U 20 16 63 |U 11 16 44 |U 21 19 49 |
esa | esa 3017 | 17 20 43 |U 6 15 29 | 14 11 31 |
gfz | gfz 2906 |U 17 14 43 |U 7 12 25 |U 15 12 34 |
grg | grg 2929 |U 18 19 50 |U 8 16 31 | 15 13 39 |
igr | igr 2919 | 14 13 44 | 6 12 24 | 14 12 33 |
igs | igs 2958 | 16 16 45 | 7 12 24 | 15 13 35 |
jpl | jpl 2907 |U 14 17 30 |U 10 17 36 |U 19 16 42 |
mit | mit 2934 | 19 18 42 |U 12 20 41 |U 51 38 112 |
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 5.2063.0 GPS week: 2063 Day: 0 MJD: 58685.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 9 10 21 | 8 9 24 | 14 15 38 |
emr | emr 2879 | 16 15 37 | 10 10 46 | 18 16 45 |
esa | esa 3072 | 12 11 25 | 8 9 25 | 15 15 32 |
gfz | gfz 2975 | 11 10 24 | 8 8 20 | 16 15 38 |
grg | grg 2975 | 10 11 31 | 9 11 34 | 15 17 40 |
igr | igr 2975 | 10 10 22 | 8 8 23 | 15 15 36 |
igs | igs 2975 | 10 10 23 | 8 9 20 | 16 16 38 |
jpl | jpl 2976 | 12 15 26 | 9 10 27 | 20 19 43 |
mit | mit 2976 | 17 19 33 | 10 18 43 | 22 20 57 |
Table 5.2063.1 GPS week: 2063 Day: 1 MJD: 58686.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3061 | 10 8 23 | 6 12 15 | 14 13 29 |
emr | emr 2880 | 12 13 33 | 8 19 39 | 18 15 48 |
esa | esa 2976 | 11 10 24 | 7 16 26 | 13 11 26 |
gfz | gfz 2880 | 10 8 23 | 7 13 21 | 13 10 25 |
grg | grg 2963 | 11 12 32 | 8 15 27 | 13 12 37 |
igr | igr 2880 | 9 8 21 | 6 13 18 | 13 11 27 |
igs | igs 2966 | 10 8 24 | 6 13 19 | 13 11 28 |
jpl | jpl 2880 | 10 11 27 | 8 17 27 | 17 12 40 |
mit | mit 2880 | 17 18 57 | 14 13 39 | 240 137 469 |
Table 5.2063.2 GPS week: 2063 Day: 2 MJD: 58687.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 10 10 30 | 7 11 20 | 18 17 45 |
emr | emr 2783 | 17 19 38 | 17 21 71 | 26 27 67 |
esa | esa 3072 | 11 13 26 | 6 17 35 | 17 17 45 |
gfz | gfz 2879 | 13 10 21 | 8 12 27 | 21 21 48 |
grg | grg 2879 | 18 15 30 | 9 22 43 | 18 18 45 |
igr | igr 2975 | 11 10 25 | 6 11 24 | 18 16 43 |
igs | igs 2975 | 11 13 29 | 8 10 32 | 19 17 47 |
jpl | jpl 2880 | 17 25 31 | 17 19 76 | 28 21 60 |
mit | mit 2976 | 14 13 36 | 11 20 41 | 21 20 53 |
Table 5.2063.3 GPS week: 2063 Day: 3 MJD: 58688.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2964 | 11 13 25 | 6 11 22 | 14 12 35 |
emr | emr 2872 | 15 14 37 | 8 18 39 | 20 17 48 |
esa | esa 2880 | 14 18 26 | 6 16 26 | 13 11 26 |
gfz | gfz 2784 | 12 18 30 | 6 13 24 | 15 10 35 |
grg | grg 2871 | 15 18 32 | 7 13 24 | 15 11 41 |
igr | igr 2830 | 12 15 26 | 5 13 23 | 14 11 30 |
igs | igs 2871 | 12 14 26 | 6 14 21 | 15 11 33 |
jpl | jpl 2784 | 13 17 32 | 8 18 30 | 18 13 34 |
mit | mit 2880 | 11 14 29 | 8 13 32 | 15 10 39 |
Table 5.2063.4 GPS week: 2063 Day: 4 MJD: 58689.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 13 13 36 | 6 12 28 | 12 10 32 |
emr | emr 2976 | 16 15 40 | 11 14 38 | 23 19 48 |
esa | esa 3072 | 14 15 32 | 5 16 33 | 11 9 30 |
gfz | gfz 2974 | 16 16 35 | 7 13 31 | 12 10 32 |
grg | grg 2878 | 19 14 54 | 6 16 31 | 16 11 37 |
igr | igr 2976 | 12 13 33 | 6 13 29 | 11 10 31 |
igs | igs 2976 | 12 14 34 | 6 13 28 | 12 11 33 |
jpl | jpl 2976 | 14 16 35 | 9 18 30 | 15 14 36 |
mit | mit 2976 | 12 14 37 | 14 28 49 | 13 14 39 |
Table 5.2063.5 GPS week: 2063 Day: 5 MJD: 58690.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 39 35 116 | 6 15 27 | 11 10 32 |
emr | emr 2879 | 44 21 224 | 11 14 48 | 20 18 37 |
esa | esa 2976 | 37 52 141 | 6 15 33 | 15 7 26 |
gfz | gfz 2879 | 38 20 141 | 8 12 29 | 15 7 33 |
grg | grg 2967 | 33 42 120 | 8 14 22 | 14 12 32 |
igr | igr 2879 | 32 17 150 | 7 13 27 | 14 7 29 |
igs | igs 2967 | 40 37 151 | 6 13 24 | 13 11 31 |
jpl | jpl 2880 | ---- ---- ---- | 10 16 31 | ---- ---- ---- |
mit | mit 2880 | 43 28 74 | 16 26 54 | 32 49 88 |
Table 5.2063.6 GPS week: 2063 Day: 6 MJD: 58691.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 15 17 32 | 6 13 23 | 14 11 33 |
emr | emr 2976 | 17 19 32 | 11 14 27 | 20 23 49 |
esa | esa 3072 | 17 17 28 | 6 18 26 | 14 11 34 |
gfz | gfz 2976 | 18 17 29 | 5 14 26 | 14 10 29 |
grg | grg 2976 | 18 18 53 | 7 19 36 | 16 12 39 |
igr | igr 2924 | 15 16 29 | 6 15 24 | 14 11 33 |
igs | igs 2976 | 15 17 28 | 6 15 23 | 15 12 35 |
jpl | jpl 2976 | 15 19 28 | 8 20 28 | 18 16 38 |
mit | mit 2976 | 17 18 31 | 8 19 33 | 16 14 37 |
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 6.2063 GPS week: 2063 MJD: 58685.500-58691.500
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 -23 -21 51 0 | 13 19
| 18 20 50 107 4 | 2
emr uuuuu | 26 9 125 118 4 | 32 38
| 18 24 45 45 5 | 2
esa uuuuu | 9 12 39 78 -1 | 12 21
| 7 6 52 43 6 | 3
gfz uuuuu | -20 -5 117 -159 -1 | 27 31
| 14 14 99 106 2 | 2
grg uuuuu | -13 -17 -22 -176 3 | 2 18
| 18 10 39 84 2 | 2
igr xxxxx | 33 19 66 -43 0 | -1 15
| 11 7 23 41 4 | 2
irf xxxxx | 5 3 -54 -57 -3 | 0 18
| 10 13 25 22 2 | 2
jpl uuuuu | 36 9 79 76 -6 | 38 41
| 17 16 49 46 9 | 3
mit uuuuu | -30 20 -102 -150 -3 | 29 34
| 8 17 52 68 4 | 2
ngs uuuuu | -32 -12 -184 2 -2 | 14 22
| 33 26 135 105 3 | 3
sio uuuux | 44 28 -117 45 8 | 66 69
| 20 23 44 73 15 | 4
Table 7.2063.0 GPS week: 2063 Day: 0 MJD: 58685.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -13 -35 9 -147 1 | 16 20
emr uuuuu | 17 2 95 105 3 | 31 36
esa uuuuu | 11 10 -5 89 -10 | 17 23
gfz uuuuu | -5 -6 -80 -98 0 | 29 33
grg uuuuu | 0 -26 -22 -45 3 | 5 18
igr xxxxx | 40 10 56 -1 -1 | 1 14
irf xxxxx | 7 -19 -28 -27 -1 | 3 16
jpl uuuuu | 37 31 25 71 11 | 41 43
mit uuuuu | -34 -4 -15 -107 3 | 32 36
ngs uuuuu | -45 4 48 8 -3 | 18 23
sio uuuux | 41 -7 -159 106 13 | 63 64
Table 7.2063.1 GPS week: 2063 Day: 1 MJD: 58686.500
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 -17 -41 92 7 | 15 20
emr uuuuu | 25 27 141 41 7 | 32 37
esa uuuuu | 11 24 -50 89 -9 | 16 22
gfz uuuuu | 0 16 93 20 0 | 30 33
grg uuuuu | -1 -30 -43 -146 3 | 5 18
igr xxxxx | 22 15 72 -48 7 | 1 14
irf xxxxx | 0 1 -52 -71 -5 | 3 16
jpl uuuuu | 39 -2 53 99 -5 | 41 43
mit uuuuu | -27 15 -93 -233 -3 | 33 36
ngs uuuuu | -84 -32 -45 -129 -5 | 18 23
sio uuuux | 39 19 -148 38 8 | 65 66
Table 7.2063.2 GPS week: 2063 Day: 2 MJD: 58687.500
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 | -30 -44 -84 117 -3 | 12 18
emr uuuuu | 57 5 185 129 11 | 30 35
esa uuuuu | 9 15 48 119 -1 | 10 21
gfz uuuuu | -20 -4 141 -174 1 | 26 30
grg uuuuu | -34 -8 38 -152 0 | 1 18
igr xxxxx | 42 11 103 -25 0 | -3 15
irf xxxxx | 18 -8 -27 -73 0 | -1 18
jpl uuuuu | 56 28 81 84 -7 | 38 42
mit uuuuu | -42 10 -86 -212 1 | 28 33
ngs uuuuu | -49 -17 -244 -116 3 | 13 22
sio uuuux | 39 10 -139 158 32 | 62 64
Table 7.2063.3 GPS week: 2063 Day: 3 MJD: 58688.500
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 -42 -66 174 -5 | 13 20
emr uuuuu | 0 31 57 112 7 | 33 40
esa uuuuu | 1 7 32 11 0 | 10 22
gfz uuuuu | -18 -24 125 -119 -6 | 27 32
grg uuuuu | 0 -4 2 -124 6 | 2 19
igr xxxxx | 23 28 69 -65 3 | -1 17
irf xxxxx | 9 12 -40 -82 -4 | 0 19
jpl uuuuu | 59 -15 143 34 -2 | 39 42
mit uuuuu | -34 17 -77 -217 -5 | 30 35
ngs uuuuu | -35 29 -258 -37 1 | 15 24
sio uuuux | 60 64 -99 45 15 | 67 71
Table 7.2063.4 GPS week: 2063 Day: 4 MJD: 58689.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -13 39 -21 3 | 11 18
emr uuuuu | 29 -36 176 145 5 | 33 40
esa uuuuu | 10 9 68 97 2 | 10 21
gfz uuuuu | -32 9 161 -278 -3 | 25 31
grg uuuuu | -42 -21 -59 -208 2 | 1 19
igr xxxxx | 21 22 59 -106 0 | -2 17
irf xxxxx | -5 11 -82 -31 -3 | -2 19
jpl uuuuu | 30 7 125 135 -19 | 38 41
mit uuuuu | -21 21 -157 -72 -5 | 28 34
ngs uuuuu | -32 -3 -326 59 -2 | 13 22
sio uuuux | 74 36 -154 53 7 | 68 72
Table 7.2063.5 GPS week: 2063 Day: 5 MJD: 58690.500
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 -25 39 111 -1 | 12 18
emr uuuuu | 17 31 108 110 -3 | 36 41
esa uuuuu | -2 5 92 26 6 | 10 21
gfz uuuuu | -31 -9 244 -285 1 | 26 31
grg uuuuu | 2 -17 -72 -287 3 | 3 18
igr xxxxx | 33 17 26 -63 1 | -1 16
irf xxxxx | 12 15 -90 -64 -3 | 0 18
jpl uuuuu | 17 2 17 110 -9 | 36 40
mit uuuuu | -18 45 -168 -112 -3 | 29 34
ngs uuuuu | 7 -15 -268 160 -6 | 14 22
sio uuuux | 42 34 -50 -52 -2 | 71 74
Table 7.2063.6 GPS week: 2063 Day: 6 MJD: 58691.500
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 12 -43 34 -2 | 11 17
emr uuuuu | 35 0 116 188 -2 | 32 36
esa uuuuu | 21 11 88 116 6 | 8 19
gfz uuuuu | -36 -14 133 -181 0 | 24 29
grg uuuuu | -16 -10 0 -266 4 | 1 16
igr xxxxx | 49 27 78 11 -7 | -3 15
irf xxxxx | -9 10 -57 -48 -5 | -3 17
jpl uuuuu | 15 13 107 2 -14 | 31 35
mit uuuuu | -31 37 -120 -94 -11 | 27 31
ngs uuuuu | 12 -51 -198 71 -1 | 11 19
sio uuuux | 12 43 -69 -30 -16 | 70 73
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