[IGSREPORT-26757] Wk 2065 IGS Final Orbits
acc
acc at igs.org
Fri Aug 23 03:17:59 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2065 (Aug 04, 2019 - Aug 10, 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:
igs2065[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2065[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2065[0-6].cls IGS GPS clock combination summary report.
igs20657.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20657.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 ANKR TIXI WES2 ANKR TIXI WES2
0 | EMR | 18 PTBB
0 | ESA | CEDU COCO CPVG DARW DAV1 DGAR FAA1 GRAZ HARB HERS
0 | ESA | HOB2 KIRU KOUR LAUT MAJU MAS1 MAW1 MGUE MOBS NAUR
0 | ESA | NNOR ONSA POHN PTBB TOW2 VILL CEDU COCO CPVG DARW
0 | ESA | DAV1 DGAR FAA1 GRAZ HARB HERS HOB2 KIRU KOUR LAUT
0 | ESA | MAJU MAS1 MAW1 MGUE MOBS NAUR NNOR ONSA POHN PTBB
0 | ESA | TOW2 VILL
0 | GFZ | 5 5 HERS POHN HERS PIE1 POHN
0 | GRG | 5 PIE1
0 | JPL | 18 NRMD
0 | MIT | 18
1 | ALL | 3
1 | COD | ARTU TIXI ARTU TIXI
1 | EMR | 22 22 CHUR WHIT CHUR FAIR SCH2 WHIT YELL
1 | ESA | AREG CEDU COCO CPVG DARW DAV1 DGAR FAA1 FALK GRAZ
1 | ESA | HARB HERS HOB2 KIRU KOUR LAUT MAC1 MAJU MAS1 MAW1
1 | ESA | MGUE MOBS NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL
1 | ESA | AREG CEDU COCO CPVG DARW DAV1 DGAR FAA1 FALK GRAZ
1 | ESA | HARB HERS HOB2 KIRU KOUR LAUT MAC1 MAJU MAS1 MAW1
1 | ESA | MGUE MOBS NAUR NNOR ONSA POHN PTBB TONG TOW2 VILL
1 | GFZ | GODE POHN GODE POHN SOFI
1 | GRG | MAC1
1 | JPL | FLIN FLIN INVK NRIL
1 | MIT | NNOR
2 | COD | INEG INEG XMIS
2 | EMR | 18 QAQ1
2 | ESA | AREG ARTU CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB
2 | ESA | HERS HOB2 INEG KIRU KOUR LAUT LHAZ MAJU MAS1 MAW1
2 | ESA | MGUE MOBS NNOR ONSA POHN QAQ1 SCOR TOW2 VILL XMIS
2 | ESA | AREG ARTU CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB
2 | ESA | HERS HOB2 INEG KIRU KOUR LAUT LHAZ MAJU MAS1 MGUE
2 | ESA | MOBS NNOR ONSA POHN SCOR TOW2 VILL
2 | GFZ | FLRS GLSV LHAZ PDEL POHN WTZR FLRS LHAZ PDEL POHN
2 | GFZ | WTZR
2 | GRG | 5 OUS2 PDEL SCOR OUS2 PDEL SCOR XMIS
2 | JPL | XMIS XMIS
3 | COD | 18 18 MDVJ TIXI MDVJ TIXI
3 | EMR | 9 9
3 | ESA | 18 18 AREG BARH CEDU COCO DARW DAV1 DGAR FAA1 FALK
3 | ESA | GRAZ HARB HERS HOB2 KIRU KOUR LAUT MAJU MAS1 MAW1
3 | ESA | MGUE MOBS NNOR ONSA OUS2 POHN PTBB TONG TOW2 VILL
3 | ESA | AREG BARH CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ
3 | ESA | HARB HERS HOB2 KIRU KOUR LAUT MAJU MAS1 MAW1 MGUE
3 | ESA | MOBS NNOR ONSA OUS2 POHN PTBB TONG TOW2 VILL
3 | GFZ | 18 POHN ABMF GODE POHN SCOR
3 | GRG | CPVG NICO SCOR CPVG NICO SCOR WIND
4 | COD | NICO NICO ULAB
4 | ESA | 18 18 ABMF CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ
4 | ESA | HARB HERS HOB2 KIRU KOUR LAUT MAJU MAS1 MAW1 MOBS
4 | ESA | NNOR ONSA POHN TONG TOW2 VILL ZAMB ABMF CEDU COCO
4 | ESA | DARW DAV1 DGAR FAA1 GRAZ HARB HERS HOB2 KIRU KOUR
4 | ESA | LAUT MAJU MAS1 MAW1 MOBS NNOR ONSA POHN TONG TOW2
4 | ESA | VILL ZAMB
4 | GFZ | 28 GODE POHN REYK GODE POHN
4 | GRG | 12 21 28 12 21 28 GODE LPGS LPGS SCOR
4 | MIT | PALM ZAMB
5 | COD | DAV1 LHAZ LHAZ
5 | EMR | 18 18 YAR2 YELL QAQ1 YAR2 YELL
5 | ESA | 21 21 ABMF BJCO CEDU COCO DARW DAV1 DGAR FAA1 FALK
5 | ESA | GRAZ HARB HERS HOB2 KIRU KOUR LAUT MAJU MAS1 MAW1
5 | ESA | MGUE MOBS NAUR NNOR ONSA POHN TONG TOW2 VILL ABMF
5 | ESA | BJCO CEDU COCO DARW DAV1 DGAR FAA1 FALK GRAZ HARB
5 | ESA | HERS HOB2 KIRU KOUR LAUT MAJU MAS1 MAW1 MGUE MOBS
5 | ESA | NAUR NNOR ONSA POHN TONG TOW2 VILL
5 | GFZ | BJCO POHN TOW2 BJCO GODE POHN TOW2
5 | GRG | 18 18 SCOR LPGS NRMD SCOR
5 | JPL | CCJ2
5 | MIT | PALM BJCO PALM
6 | COD | 18 GLSV NRC1 TIXI TOW2 NRC1 TIXI TOW2
6 | EMR | 16 WES2
6 | ESA | AREG BAKE CEDU COCO DARW DAV1 DGAR FAA1 GRAZ HARB
6 | ESA | HERS HOB2 KIRU KOUR LAUT MAJU MAS1 MAW1 MGUE MOBS
6 | ESA | NAUR NNOR ONSA POHN PTBB TOW2 VILL AREG BAKE CEDU
6 | ESA | COCO DARW DAV1 DGAR FAA1 GRAZ HARB HERS HOB2 KIRU
6 | ESA | KOUR LAUT MAJU MAS1 MAW1 MGUE MOBS NAUR NNOR ONSA
6 | ESA | POHN PTBB RAMO TOW2 VILL
6 | GFZ | 18 18 GODE IISC POHN GLSV GODE IISC POHN
6 | GRG | 10 18 10 18 LPGS LPGS SEYG XMIS
6 | MIT | XMIS
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
----+--------+--------+-------------
4 | EMR | ~23:00 | ~ 0.07 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
1 | COD | 4
2 | COD | 4
3 | ESA | 4
3 | NGS | 9
4 | COD | 4
5 | ESA | 4
6 | COD | 4
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 | 4 | 4 | 4 | 4 |
PRN G05 | | | | | | | 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 | .7 .2 1.8 15 23 -10 -.73
EMR | 0 | 2.8 -5.4 1.5 -54 82 19 -.10
ESA | 0 | -.1 -1.0 -.6 6 34 24 -.83
GFZ | 0 | .4 .8 .8 44 7 22 -.71
GRG | 0 | -.0 -4.0 -1.9 94 -13 148 -.18
JPL | 0 | .6 -6.8 -3.1 7 10 -8 -.72
MIT | 0 | 2.0 -2.4 3.6 -29 77 2 -.39
NGS | 0 | 4.2 -5.9 2.1 -15 37 19 -.57
SIO | 0 | -4.3 .5 5.9 -35 12 -8 -.45
COD | 1 | 1.0 .1 1.4 23 3 12 -.65
EMR | 1 | 2.9 .1 6.3 -54 62 -6 -.23
ESA | 1 | .4 -1.2 -1.1 -1 6 80 -.60
GFZ | 1 | .4 .4 .8 42 2 30 -.62
GRG | 1 | -2.6 -.7 -11.3 79 13 68 -.31
JPL | 1 | -1.6 -7.3 3.6 7 1 7 -.80
MIT | 1 | .0 -3.7 .6 -20 61 -19 -.40
NGS | 1 | -5.2 -6.8 4.9 -33 59 -38 -.46
SIO | 1 | -2.9 -.6 10.3 -18 7 -14 -.44
COD | 2 | .6 .1 1.5 17 18 1 -.78
EMR | 2 | -5.6 -2.6 3.5 -52 35 27 -.11
ESA | 2 | .4 -.3 -.6 -1 31 26 -.84
GFZ | 2 | -.5 .7 .4 46 26 18 -.60
GRG | 2 | 1.7 2.0 -8.1 103 65 58 -.26
JPL | 2 | .5 -6.2 1.0 -11 15 5 -.79
MIT | 2 | 1.9 -1.1 2.0 -7 66 -26 -.51
NGS | 2 | -3.1 -5.0 -.8 -10 49 18 -.51
SIO | 2 | -4.4 .9 5.3 -4 12 -18 -.38
COD | 3 | .8 .1 .9 17 5 7 -.67
EMR | 3 | .7 -4.6 3.1 -39 75 2 -.08
ESA | 3 | -.1 -.6 -.8 7 24 28 -.78
GFZ | 3 | .1 .5 .6 49 16 23 -.61
GRG | 3 | 4.7 2.1 -9.4 122 34 82 -.40
JPL | 3 | .7 -8.0 -3.4 7 19 -6 -.56
MIT | 3 | 2.4 -3.0 -.9 -8 77 -29 -.47
NGS | 3 | -2.4 -1.2 3.1 -4 59 -41 -.56
SIO | 3 | -3.2 1.6 6.5 -25 19 -16 -.43
COD | 4 | .3 .2 .9 21 16 -4 -.62
EMR | 4 | 4.0 -7.6 12.8 -58 89 5 .0
ESA | 4 | .2 -.3 -.5 11 34 22 -.86
GFZ | 4 | .4 .6 .7 51 18 22 -.67
GRG | 4 | .2 2.1 1.2 120 24 97 -.31
JPL | 4 | -.6 -6.0 -4.7 -10 9 23 -.48
MIT | 4 | 3.8 -1.5 -1.3 -10 71 -50 -.46
NGS | 4 | 1.1 -6.0 8.6 -27 59 -25 -.43
SIO | 4 | -4.2 -.7 3.7 3 16 -20 -.30
COD | 5 | .3 .1 1.0 20 2 -4 -.71
EMR | 5 | -6.6 -6.5 .4 -41 56 19 -.10
ESA | 5 | .0 .1 -.6 12 19 39 -.69
GFZ | 5 | .4 .5 .7 44 14 32 -.64
GRG | 5 | -3.5 .5 -2.1 95 30 95 -.29
JPL | 5 | 5.2 -4.5 -2.8 6 5 5 -.75
MIT | 5 | .7 .3 -3.9 -6 42 -28 -.50
NGS | 5 | -5.0 -4.1 3.4 -44 53 -11 -.37
SIO | 5 | -2.2 -.1 5.5 -2 -1 0 -.41
COD | 6 | .7 .4 1.7 17 19 -13 -.79
EMR | 6 | 6.2 -16.2 1.2 -34 53 33 -.17
ESA | 6 | .4 -.5 .9 -22 -1 73 -.59
GFZ | 6 | .4 .7 1.4 29 22 19 -.68
GRG | 6 | -2.5 -1.8 .6 105 24 113 -.20
JPL | 6 | .1 1.0 -2.7 5 4 -5 -.88
MIT | 6 | .3 -2.7 -.9 -29 53 -39 -.47
NGS | 6 | -6.8 -4.6 4.8 -59 72 -33 -.43
SIO | 6 | -3.5 -2.3 3.1 12 7 -9 -.37
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 1.2065.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2065.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 2.2065.[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 3.2065.[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 5.2065.0-6). 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 2065 summary. (Aug 04, 2019 - Aug 10, 2019)
Table 1.2065.a GPS week: 2065 MJD: 58699.000-58705.000
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 261| 0 0 0 12 7 -1 .02 9 9 | -769 121 7 96
| 0 0 1 30 17 15 .03 | 194 298
emr 79| -1 -1 4 -7 3 49 .15 12 12 | 155313 -72 15 98
| 1 2 1 5 24 22 .02 | 19742 523
esa 150| -1 0 -2 -6 -9 4 -.13 9 9 | 2662 476 8 121
| 0 0 1 10 5 21 .01 | 2056 760
gfz 185| -1 0 -1 -18 -9 -12 .11 10 10 | -73 88 12 180
| 0 0 1 13 12 11 .02 | 397 509
grg 99| 4 0 -4 -11 22 -9 -.08 14 13 | -13 51 11 151
| 1 1 2 10 14 46 .03 | 198 287
igr n/a| 0 0 0 -14 -33 -7 -.05 4 4 | -9050 689 11 72
| 0 0 0 7 8 6 .01 | 2087 683
jpl 80| 0 0 0 10 10 9 .14 7 7 | 211753 -157 10 82
| 0 1 1 12 24 14 .03 | 395 767
mit 349| 0 -1 2 -17 4 12 -.19 17 15 | -769 115 150 1598
| 0 0 0 23 29 9 .01 | 888 344
ngs 217| 0 0 1 30 -5 -21 -.07 9 7 | -73848 527597 1066 2161
| 0 0 2 17 24 10 .01 | 193568 1395842
sio 328| 0 0 2 -20 -3 -20 -.01 15 15 | --- --- --- ---
| 0 0 2 24 25 33 .03 | --- ---
Table 1.2065.b GPS week : 2065 MJD: 58699.000-58705.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 3 3 3 3 3 |
2 | 5 4 5 4 5 4 4 |
3 | 4 8 4 5 6 7 7 |
4 | 0 0 0 0 0 0 0 |
5 | 5 4 4 5 4 5 5 |
6 | 3 4 4 3 3 3 3 |
7 | 3 3 3 3 3 3 3 |
8 | 3 4 4 4 4 4 4 |
9 | 4 3 3 6 3 3 3 |
10 | 5 4 4 4 4 5 6 |
11 | 5 5 5 4 5 4 5 |
12 | 4 4 4 4 5 4 4 |
13 | 4 4 4 3 3 4 4 |
14 | 4 3 4 3 3 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 5 6 6 5 5 6 6 |
17 | 4 4 4 4 0 4 4 |
18 | 3 4 4 3 4 3 4 |
19 | 4 4 5 4 5 4 4 |
20 | 4 4 6 4 4 4 4 |
21 | 5 4 4 6 5 4 4 |
22 | 4 4 4 5 4 4 4 |
23 | 4 4 4 4 4 4 4 |
24 | 3 3 3 3 3 3 3 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 4 4 3 3 3 4 |
28 | 4 4 4 4 4 4 5 |
29 | 4 4 4 4 4 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 4 3 4 3 3 4 3 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2065.0 GPS week: 2065 Day: 0 MJD: 58699.000
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 260| 0 0 -1 -26 -12 -18 -.02 10 9 | -922 444 7 83
emr 80| -1 0 5 -6 33 52 .19 11 11 | 176119 562 13 77
esa 150| -1 0 -1 -2 -3 -33 -.12 10 9 | -1960 2026 8 116
gfz 183| -2 0 -1 -35 13 -15 .13 10 10 | -233 325 12 151
grg 100| 2 -1 -2 8 5 81 -.09 13 12 | -317 471 13 145
igr n/a| 0 1 0 -7 -34 -12 -.04 4 4 | -12290 1568 11 63
jpl 80| 1 1 0 23 -8 0 .11 7 7 | 211166 772 10 82
mit 349| 0 0 3 -11 2 25 -.18 17 15 | -1118 460 67 1538
ngs 219| 0 0 0 26 -8 -15 -.07 9 8 | -700 127 1096 2204
sio 326| 1 0 5 -4 3 -26 .02 16 16 | --- --- --- ---
Table 2.2065.1 GPS week: 2065 Day: 1 MJD: 58700.000
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| 2 0 -1 21 22 17 .05 9 9 | -987 366 7 88
emr 80| -2 0 4 -13 19 16 .18 13 13 | 139129 244 15 71
esa 150| 0 0 -1 -10 -14 26 -.12 9 9 | 3312 213 7 105
gfz 183| -2 0 1 -26 -8 -9 .10 9 8 | -81 251 11 166
grg 101| 3 0 -8 -16 14 4 -.09 13 11 | -237 362 12 134
igr n/a| 0 0 -1 -24 -33 -20 -.04 4 4 | -10922 933 11 76
jpl 80| 1 0 0 24 -32 -11 .12 8 8 | 211656 52 12 85
mit 350| 0 -1 2 -26 7 18 -.20 18 16 | -939 344 76 1658
ngs 213| 0 0 4 38 15 -39 -.07 9 8 | -841 157 1214 2539
sio 330| 0 0 0 -18 22 -8 -.01 16 15 | --- --- --- ---
Table 2.2065.2 GPS week: 2065 Day: 2 MJD: 58701.000
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 261| 1 0 0 20 -15 14 .06 10 9 | -544 -320 8 104
emr 81| -1 0 5 -6 -37 48 .12 12 12 | 176513 63 14 87
esa 150| 0 0 0 -4 -2 -8 -.14 10 9 | 3750 -36 9 125
gfz 187| -1 0 -1 -24 -23 4 .11 9 8 | -203 367 11 168
grg 100| 4 1 -5 -18 37 -49 -.13 15 13 | 147 -53 10 167
igr n/a| 0 0 0 -25 -34 -7 -.04 4 4 | -9804 1225 12 69
jpl 80| 0 0 2 -4 30 11 .14 8 8 | 211868 511 9 75
mit 350| 1 -1 3 -12 -8 -3 -.20 17 16 | -2539 367 68 1533
ngs 216| 0 -1 -3 65 32 -26 -.08 11 9 | -590 -194 1116 2247
sio 332| 0 0 4 -20 -16 0 -.00 15 15 | --- --- --- ---
Table 2.2065.3 GPS week: 2065 Day: 3 MJD: 58702.000
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 262| 0 0 -3 32 0 8 -.01 9 8 | -817 160 7 97
emr 80| 0 0 4 -10 20 35 .14 12 12 | 176613 -887 14 85
esa 150| -1 0 -3 -17 -13 16 -.13 10 10 | 3776 -92 8 125
gfz 187| -1 0 -2 -24 -16 -4 .09 10 10 | 282 -93 13 215
grg 101| 5 2 -6 -7 11 -49 -.09 17 14 | 201 -77 11 138
igr n/a| 0 0 -1 -13 -37 0 -.02 5 5 | -8440 19 14 65
jpl 80| 0 0 2 11 17 2 .15 7 7 | 212471 -1068 10 100
mit 350| 1 -1 2 -17 8 15 -.19 18 14 | -175 -564 600 1677
ngs 216| 0 0 3 17 -8 -17 -.06 9 7 | -512820 3693071 1141 2043
sio 324| 0 0 2 -30 -13 0 .01 16 16 | --- --- --- ---
Table 2.2065.4 GPS week: 2065 Day: 4 MJD: 58703.000
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 264| 1 0 0 39 10 -3 .01 10 9 | -490 -138 7 97
emr 75| 0 0 4 -12 11 43 .14 13 12 | 139010 361 17 90
esa 150| -1 0 -4 -19 -9 3 -.14 9 10 | 3477 -22 7 122
gfz 187| -2 0 -1 -7 -17 -30 .10 10 10 | 481 -868 14 204
grg 97| 5 1 0 -17 14 -38 -.03 14 13 | 65 -231 10 135
igr n/a| 0 0 -1 -11 -47 -4 -.06 4 4 | -8298 815 12 91
jpl 80| 0 1 0 0 30 29 .19 8 8 | 211538 49 11 81
mit 350| 0 -2 1 -35 37 12 -.19 17 15 | -341 -3 80 1573
ngs 217| 0 0 1 32 -42 -18 -.09 7 6 | -468 -165 1024 2036
sio 331| 0 0 0 -21 19 -15 -.00 16 15 | --- --- --- ---
Table 2.2065.5 GPS week: 2065 Day: 5 MJD: 58704.000
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 263| 0 0 -1 -35 27 -9 .05 7 7 | -705 -60 7 99
emr 79| -5 -1 1 2 -6 57 .13 13 13 | 139995 -311 17 157
esa 150| 0 0 -1 -1 -7 1 -.15 10 10 | 3271 874 8 127
gfz 184| 0 0 -2 -17 -13 -13 .09 11 10 | -757 733 13 184
grg 97| 5 1 -1 -23 42 -20 -.06 15 13 | -61 162 10 159
igr n/a| 0 1 0 -10 -19 -3 -.06 4 4 | -7300 679 11 79
jpl 80| 0 -2 0 21 34 26 .13 7 7 | 211722 -116 11 83
mit 349| 0 0 1 27 -49 11 -.18 17 15 | -373 84 89 1483
ngs 220| 0 0 1 18 -15 -29 -.07 9 7 | -593 -209 1077 2052
sio 327| 0 0 2 17 -50 3 -.02 14 14 | --- --- --- ---
Table 2.2065.6 GPS week: 2065 Day: 6 MJD: 58705.000
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 263| 0 1 1 33 24 -18 .01 11 10 | -918 395 8 104
emr 80| 0 -7 2 -2 -16 88 .14 12 12 | 139814 -537 17 122
esa 150| -1 0 -3 10 -16 25 -.13 9 9 | 3008 375 10 131
gfz 188| 0 1 -4 5 -3 -21 .13 11 12 | -6 -96 11 176
grg 102| 4 1 -2 -6 30 5 -.05 14 12 | 109 -272 13 184
igr n/a| 0 1 0 -6 -30 -4 -.06 4 4 | -6297 -414 12 64
jpl 80| 0 0 -1 0 2 4 .16 7 7 | 211856 -1302 10 69
mit 349| 0 0 1 -45 36 4 -.21 17 15 | 100 122 70 1728
ngs 218| 0 0 4 17 -15 -7 -.05 8 7 | -927 394 796 2012
sio 327| 1 1 2 -62 13 -91 -.08 15 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 3.2065.0 GPS week: 2065 Day: 0 MJD: 58699.000
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 5 14 11 8 2 5 10 8 12 3 | 23 27 27 24 26 23 26 22 23 30 24
2 | 11 9 6 11 12 5 8 31 9 19 4 | 28 27 25 31 29 24 26 28 27 24 24
3E | 16 10 15 6 16 2 6 9 8 10 4 | 57 58 58 64 63 57 37 58 61 58 58
X4 | 345 --- 3 --- --- 333 --- --- --- --- 0 | 38 --- 235 --- --- 47 --- --- --- --- 226
5E | 10 10 9 12 29 4 9 15 9 18 4 | 127 125 127 125 124 127 127 127 123 128 126
6 | 8 9 9 10 14 3 6 9 6 11 3 | 35 35 36 33 38 32 35 29 32 37 34
7 | 7 10 6 9 9 4 6 15 6 19 3 | 36 36 38 40 39 36 38 34 36 39 36
8 | 9 10 12 7 12 3 6 8 6 11 3 | 21 19 21 19 23 17 18 16 19 19 18
9 | 8 10 5 19 9 3 5 10 9 10 3 | 52 58 43 53 53 54 47 54 83 46 55
10E | 10 12 17 13 11 3 7 17 13 14 4 | 55 59 53 53 62 53 42 57 53 56 55
11 | 12 9 16 7 12 3 6 29 8 16 4 | 22 26 21 22 18 18 23 23 19 17 17
12E | 16 17 10 8 11 6 7 17 10 16 4 | 36 32 29 33 30 29 29 27 31 32 29
13 | 7 11 8 11 10 4 9 18 7 17 3 | 37 42 32 33 38 34 39 42 34 45 36
14 | 13 7 8 10 8 3 7 19 8 20 3 | 48 49 44 47 49 46 45 51 47 52 46
15 | 10 8 6 7 11 3 5 21 7 18 3 | 57 57 56 56 63 56 55 51 53 54 55
16E | 8 26 6 19 25 5 8 14 8 16 5 | 19 25 18 27 29 18 17 19 21 20 17
17 | 16 10 6 7 11 4 7 16 11 20 4 | 29 23 18 21 19 21 22 20 21 20 22
18 | 7 7 11 9 12 3 7 13 9 10 3 | 18 23 25 18 20 19 20 27 21 22 19
19 | 12 13 6 8 11 4 5 20 11 21 4 | 37 33 35 38 31 33 33 37 30 36 33
20E | 12 10 6 8 14 3 9 15 10 12 3 | 65 61 61 61 69 60 62 60 59 61 61
21 | 7 11 9 5 15 5 8 31 8 20 4 | 22 26 20 21 26 20 23 29 20 22 19
22E | 11 7 9 9 11 3 3 14 13 16 3 | 94 96 93 95 95 94 96 92 96 91 94
23 | 8 18 5 4 10 3 5 19 9 21 4 | 47 45 43 46 50 45 47 47 44 48 45
24 | 8 8 7 10 6 4 7 12 9 13 3 | 18 28 20 22 24 20 27 17 21 30 22
25E | 12 12 15 8 9 3 10 12 8 13 4 | 33 37 29 38 36 32 36 36 35 31 33
26 | 8 12 15 10 17 4 8 15 8 15 4 | 28 26 26 31 30 26 25 28 25 25 25
27 | 8 13 12 11 8 3 6 11 10 13 3 | 27 29 29 31 30 26 28 26 26 34 27
28E | 8 11 9 10 12 4 6 15 9 14 3 | 17 15 16 13 18 13 14 20 15 18 13
29 | 7 16 8 8 18 5 8 16 7 15 4 | 42 40 37 43 43 40 40 41 39 44 40
30 | 7 7 7 6 10 3 6 5 8 11 2 | 25 31 28 26 28 27 30 25 25 32 27
31 | 7 7 8 5 9 4 8 18 8 21 3 | 40 43 40 39 42 39 45 32 39 41 40
32 | 11 8 7 9 10 3 6 14 9 14 3 | 41 44 38 40 45 40 42 41 42 46 41
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 10 10 13 4 7 17 9 16 |T 39 41 44 40 41 38 38 39 39 40 44
WRMS | 9 11 9 10 12 4 7 15 8 16 |NE 33 34 40 33 34 32 33 32 33 34 40
MEDI | 9 10 8 9 11 3 7 15 8 15 |MD 36 35 32 33 36 32 35 32 32 36 33
Table 3.2065.1 GPS week: 2065 Day: 1 MJD: 58700.000
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 7 11 11 7 3 7 10 7 14 3 | 22 24 21 21 23 20 22 20 22 30 21
2 | 6 11 6 10 13 5 5 31 11 19 4 | 22 24 22 30 23 22 21 26 27 21 21
X3E | 6 --- --- --- 10 10 --- --- --- --- 7 | 53 --- --- --- 54 49 --- --- --- --- 50
X4 | 382 --- 2 --- --- 379 --- --- --- --- 0 | 38 --- 248 --- --- 48 --- --- --- --- 241
5E | 6 12 5 10 10 2 10 14 9 14 3 | 88 86 88 88 93 87 84 88 85 89 87
6 | 10 16 8 8 13 3 7 12 7 9 3 | 30 31 29 28 32 26 29 24 28 30 28
7 | 7 11 6 4 7 4 6 14 9 17 3 | 27 25 21 25 27 23 26 23 25 28 24
8 | 8 10 12 8 15 3 7 10 11 13 3 | 22 22 22 19 26 19 22 19 23 20 20
9 | 9 9 6 6 8 3 6 11 6 9 2 | 54 56 39 38 53 53 39 55 86 42 53
10E | 10 14 15 8 12 2 10 17 10 14 4 | 44 50 46 44 50 44 40 49 47 47 46
11 | 11 7 14 7 13 3 8 31 9 16 4 | 22 24 20 22 19 19 24 24 21 15 18
12E | 8 17 9 11 16 3 7 18 9 16 4 | 31 33 29 32 30 28 28 26 30 31 28
13 | 9 14 7 8 10 3 10 18 9 16 3 | 30 37 30 31 30 29 34 33 32 34 31
14 | 8 8 7 6 8 2 5 20 7 20 3 | 37 37 33 36 40 35 35 39 39 39 36
15 | 9 9 6 6 11 5 8 21 9 18 3 | 39 39 37 38 42 38 40 33 36 40 37
16E | 9 25 8 20 35 6 10 19 10 17 6 | 19 24 18 27 29 17 15 19 21 22 17
17 | 9 12 6 11 12 4 8 18 8 20 3 | 28 23 20 26 22 24 22 26 24 23 25
18 | 6 8 10 10 12 3 8 15 9 13 3 | 21 24 24 21 25 20 24 28 22 30 22
19 | 10 15 6 8 13 5 6 20 7 24 4 | 40 35 37 41 35 35 34 40 36 40 36
20E | 11 13 6 9 15 4 10 16 8 12 3 | 46 52 49 49 48 48 51 56 50 52 49
21 | 7 10 5 6 12 4 8 31 11 22 4 | 20 25 17 20 23 18 22 26 22 22 17
22E | 10 9 9 7 9 3 5 16 12 17 3 | 65 65 61 65 65 63 62 62 64 61 63
23 | 9 20 7 5 11 4 5 20 7 21 4 | 41 44 38 41 43 39 41 39 40 42 40
24 | 12 9 6 6 8 3 7 13 9 15 3 | 19 29 22 24 21 21 28 18 22 32 22
25E | 12 12 14 10 13 4 10 14 8 10 4 | 41 48 41 48 38 44 44 43 46 48 43
26 | 9 17 11 6 20 4 8 15 9 14 4 | 26 29 23 25 33 24 23 26 26 27 24
27 | 10 8 11 7 7 3 7 14 11 19 3 | 26 29 27 27 31 25 27 28 27 37 27
28E | 7 8 6 13 13 3 7 12 11 12 3 | 20 19 16 17 23 16 17 20 23 22 17
29 | 8 18 8 7 11 6 9 17 10 16 3 | 42 39 38 44 39 39 39 40 42 43 40
30 | 7 9 4 6 10 3 5 4 8 10 2 | 29 30 28 28 26 27 31 26 32 32 29
31 | 5 8 7 5 8 4 6 18 4 21 3 | 29 33 26 28 31 27 31 24 31 30 28
32 | 9 10 5 9 10 3 7 13 8 10 3 | 33 40 34 35 38 34 38 37 35 39 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 9 13 4 8 18 9 16 |T 34 35 38 33 35 33 33 33 35 35 39
WRMS | 9 13 9 8 11 4 8 16 8 15 |NE 30 31 37 29 31 28 29 29 31 31 38
MEDI | 9 10 7 8 11 3 7 16 9 16 |MD 30 31 29 28 31 27 29 26 30 32 28
Table 3.2065.2 GPS week: 2065 Day: 2 MJD: 58701.000
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 11 10 8 3 5 10 9 9 3 | 25 25 26 25 27 23 27 23 25 27 25
2 | 13 10 7 10 17 5 7 33 12 20 5 | 25 22 20 26 26 20 24 24 23 19 19
3E | 11 7 15 10 13 6 7 10 8 14 3 | 34 41 43 48 37 36 37 45 46 49 36
X4 | 501 --- 2 --- --- 492 --- --- --- --- 0 | 23 --- 298 --- --- 57 --- --- --- --- 334
5E | 8 13 5 10 30 3 8 10 11 12 4 | 65 67 65 66 62 66 67 66 63 68 65
6 | 10 14 9 9 18 4 5 11 7 11 3 | 35 31 31 28 34 28 35 28 29 30 30
7 | 7 11 7 8 8 4 6 15 6 18 3 | 26 27 25 28 28 24 25 22 26 26 25
8 | 10 11 12 7 14 3 8 9 10 12 3 | 20 21 20 19 24 18 19 17 21 19 18
9 | 6 8 8 8 8 3 5 11 10 10 2 | 45 49 29 37 45 45 32 47 108 34 46
10E | 10 13 16 7 13 3 9 16 12 11 4 | 32 36 30 29 32 29 28 35 28 33 30
11 | 10 10 16 8 10 3 7 29 9 16 4 | 21 25 20 20 20 18 24 20 19 15 17
12E | 9 15 8 7 15 5 10 20 11 17 4 | 34 36 31 35 34 31 32 30 38 34 32
13 | 8 11 7 8 9 4 8 15 12 17 3 | 29 36 26 28 31 29 35 31 31 32 30
14 | 10 9 5 8 9 4 6 21 7 21 3 | 37 38 37 43 35 37 36 42 33 40 37
15 | 9 8 5 7 13 3 6 22 10 20 3 | 39 37 33 37 38 36 39 30 40 36 36
16E | 11 21 7 10 35 7 10 18 13 16 5 | 20 20 17 22 32 18 16 20 21 23 17
17 | 12 12 7 7 12 3 7 15 9 19 3 | 22 22 16 20 20 17 21 19 22 19 17
18 | 7 8 9 9 12 3 7 15 9 14 3 | 21 21 20 20 26 17 20 26 18 28 20
19 | 15 18 7 7 15 4 6 19 10 21 4 | 28 25 20 22 22 21 24 25 26 23 21
20E | 23 12 12 17 18 5 10 15 21 11 5 | 38 31 33 36 37 33 33 33 33 36 32
21 | 8 11 9 6 12 6 8 30 12 19 4 | 22 23 17 19 21 18 22 24 20 20 16
22E | 9 8 9 9 15 4 9 15 18 16 4 | 47 46 48 52 48 47 46 47 47 49 47
23 | 8 19 6 8 10 6 6 22 9 19 4 | 28 29 27 31 29 29 28 31 27 32 28
24 | 10 9 4 8 9 7 7 13 12 15 3 | 22 27 22 23 16 20 27 16 22 32 22
25 | 12 12 17 6 13 6 9 10 9 11 4 | 30 33 28 32 30 26 33 30 26 33 28
26 | 8 16 13 9 16 4 10 15 9 13 4 | 24 23 23 29 27 22 22 24 22 26 22
27 | 12 13 12 9 7 3 9 14 10 13 3 | 28 28 28 29 29 26 28 26 28 29 27
28E | 7 8 7 11 15 4 7 15 8 13 3 | 21 21 18 20 23 17 17 23 22 24 19
29 | 6 13 7 7 11 4 9 18 9 14 3 | 32 30 28 33 31 30 30 29 29 32 29
30 | 7 11 4 8 9 3 5 5 7 12 2 | 22 28 21 21 19 20 28 20 21 27 22
31 | 7 10 7 6 9 5 9 16 9 22 3 | 33 37 32 35 33 30 36 26 32 36 33
32 | 8 9 5 7 9 4 5 11 9 9 2 | 25 27 21 25 21 21 27 21 22 25 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 10 9 15 4 8 17 11 15 |T 29 31 36 30 30 28 29 29 31 30 37
WRMS | 9 12 9 8 13 4 8 16 9 15 |NE 27 28 36 27 27 26 27 25 29 27 39
MEDI | 9 11 7 8 12 4 7 15 9 14 |MD 28 28 26 28 29 26 28 26 26 30 27
Table 3.2065.3 GPS week: 2065 Day: 3 MJD: 58702.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 10 9 9 10 3 4 9 8 10 2 | 23 25 24 24 27 22 25 21 20 26 23
2 | 5 7 8 10 16 5 5 33 8 19 4 | 16 19 17 24 21 18 18 26 17 17 15
3E | 11 9 16 26 15 5 8 11 9 10 5 | 14 20 20 27 21 16 20 19 22 19 16
X4 | 2 --- 405 --- --- 384 --- --- --- --- 0 | 27 --- 240 --- --- 334 --- --- --- --- 227
5E | 11 10 7 9 42 5 8 14 10 15 5 | 61 59 59 61 68 61 60 57 60 58 59
6 | 6 13 9 8 17 2 6 11 8 13 3 | 24 28 26 23 24 22 25 21 24 26 23
7 | 8 10 8 6 9 3 8 15 7 16 3 | 30 31 30 33 33 29 32 25 31 28 30
8 | 7 13 12 9 17 3 7 7 7 11 3 | 18 20 21 20 25 18 20 16 19 20 18
X9 | 7 9 --- --- 15 14 --- 12 477 --- 6 | 90 94 --- --- 84 94 --- 94 472 --- 90
10E | 10 10 16 14 12 5 7 17 10 11 4 | 27 31 27 29 31 27 25 32 33 29 28
11 | 8 10 14 6 13 3 7 30 8 18 4 | 21 25 18 22 22 18 24 20 19 15 17
12E | 6 18 8 6 17 5 7 19 10 19 4 | 34 39 34 36 36 36 34 32 37 39 34
13 | 6 12 7 9 10 4 7 16 7 15 3 | 21 30 19 21 23 23 28 28 25 32 23
14 | 7 6 7 6 10 4 6 18 7 21 3 | 22 24 20 24 20 22 23 25 23 27 22
15 | 10 7 5 7 13 4 7 21 7 19 3 | 45 44 43 45 44 42 43 33 37 36 40
X16E | 11 25 6 10 15 5 --- 15 8 14 5 | 18 22 16 21 21 15 --- 16 17 21 15
17 | 10 12 7 7 14 5 5 17 8 22 3 | 22 22 18 22 23 20 24 23 21 23 20
18 | 7 7 9 9 15 3 7 14 9 12 3 | 22 26 24 26 29 23 25 30 23 29 24
19 | 12 18 8 6 16 5 5 20 8 23 4 | 22 23 18 20 21 18 19 19 20 19 17
20E | 11 10 5 13 17 3 8 17 6 11 3 | 34 35 34 39 41 34 34 41 37 38 35
21 | 7 13 7 6 41 6 8 33 8 21 5 | 20 24 15 20 42 16 20 25 17 19 16
22E | 15 9 13 8 17 11 5 19 22 17 5 | 45 41 39 40 45 39 42 39 48 40 41
23 | 10 21 6 5 11 5 6 21 7 19 4 | 19 20 15 17 18 17 20 21 17 21 17
24 | 7 8 8 8 12 4 6 14 8 15 3 | 19 27 20 20 18 20 25 17 21 31 20
25 | 8 12 17 7 15 4 9 8 10 11 4 | 21 29 20 24 26 22 27 23 25 28 22
26 | 8 11 12 8 15 4 10 13 9 12 3 | 30 27 30 30 33 29 28 31 29 30 28
27 | 9 9 12 8 10 2 7 12 5 13 3 | 19 21 21 23 23 20 22 20 20 22 20
28E | 8 10 7 18 17 5 8 17 8 15 4 | 19 21 18 21 27 17 19 23 21 19 17
29 | 7 18 7 7 12 5 9 17 8 16 3 | 23 20 20 23 24 20 21 21 20 23 19
30 | 7 10 5 6 10 3 6 5 6 14 2 | 20 26 19 20 18 20 27 19 23 27 21
31 | 7 7 7 6 9 4 7 14 7 18 3 | 29 30 30 28 31 27 30 22 26 29 27
32 | 11 7 7 5 10 4 5 8 7 10 2 | 18 23 18 19 20 17 23 17 16 22 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 10 10 17 5 7 18 9 16 |T 27 29 31 26 30 36 27 27 40 27 32
WRMS | 8 12 10 10 14 5 7 14 7 16 |NE 26 28 32 24 28 38 24 26 42 24 33
MEDI | 8 10 8 8 15 4 7 15 8 15 |MD 22 26 20 23 25 22 25 23 23 26 22
Table 3.2065.4 GPS week: 2065 Day: 4 MJD: 58703.000
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 8 9 8 9 3 5 10 8 18 3 | 25 26 24 26 30 23 28 25 23 35 25
2 | 11 8 6 11 14 5 8 33 9 22 4 | 26 23 23 29 28 22 24 28 26 22 21
3E | 11 32 18 23 13 5 7 9 7 11 5 | 36 42 28 35 39 35 35 29 29 30 35
X4 | 367 --- 3 --- --- 369 --- --- --- --- 0 | 19 --- 234 --- --- 50 --- --- --- --- 255
5E | 14 11 7 15 17 3 9 7 9 11 4 | 70 65 66 65 66 66 64 65 67 64 65
6 | 10 11 7 7 17 4 7 9 6 10 3 | 34 33 31 30 35 30 34 27 33 32 31
7 | 8 14 6 9 8 3 6 15 5 18 3 | 30 27 27 31 32 28 30 27 28 31 28
8 | 10 16 11 10 15 4 9 9 6 11 3 | 22 24 20 22 27 18 23 18 22 18 20
9 | 6 10 9 8 9 4 5 10 5 10 2 | 44 45 65 62 40 41 64 41 82 64 43
10E | 12 10 17 14 13 5 7 15 7 11 4 | 37 40 37 43 44 37 37 41 39 35 38
11 | 12 9 14 9 11 3 8 29 10 19 4 | 21 26 19 22 25 18 26 21 20 22 19
12E | 9 15 7 6 31 4 9 18 7 18 4 | 40 39 37 40 47 38 38 36 38 36 37
13 | 8 12 8 9 11 4 7 15 4 16 3 | 30 37 28 30 35 31 35 36 32 38 32
14 | 7 5 6 5 12 4 7 17 5 19 3 | 38 38 35 39 38 37 38 39 35 41 37
15 | 12 9 6 9 13 3 8 20 8 21 4 | 44 41 41 44 39 39 40 33 39 41 39
X16E | 11 29 8 14 13 6 --- 15 7 12 5 | 15 20 18 22 28 15 --- 17 18 21 16
X17 | 2 --- --- --- --- 38 --- --- --- --- 0 | 78 --- --- --- --- 20 --- --- --- --- 78
18 | 10 9 8 8 13 3 7 15 8 18 3 | 19 22 18 19 26 16 21 26 18 30 18
19 | 14 13 7 7 13 5 7 19 12 26 4 | 31 28 27 30 27 26 29 26 28 26 26
20E | 13 10 7 14 15 4 10 17 7 13 4 | 35 37 34 38 38 35 36 41 36 35 35
21 | 7 13 8 8 12 4 9 31 8 19 4 | 20 27 19 23 24 19 24 27 20 20 18
22E | 18 6 9 13 11 4 7 16 11 14 4 | 67 63 59 62 62 62 63 59 64 60 62
23 | 9 23 6 5 10 5 6 21 6 21 4 | 34 35 30 35 38 33 33 34 31 35 32
24 | 8 11 5 8 13 4 7 13 6 17 3 | 23 30 21 25 22 21 28 18 22 34 23
25 | 9 12 15 7 13 3 11 9 6 10 3 | 26 31 24 26 30 24 28 25 26 26 25
26 | 7 11 13 9 16 4 9 13 8 12 3 | 28 28 28 30 29 28 28 27 28 27 27
27 | 8 10 11 9 8 3 9 14 5 12 3 | 24 27 26 25 30 24 27 25 26 24 25
28E | 9 10 7 15 20 4 6 16 9 15 4 | 23 20 17 22 35 19 20 23 25 22 20
29 | 9 19 9 8 9 4 11 17 8 18 4 | 34 36 31 35 35 33 32 31 34 37 32
30 | 9 10 5 9 11 3 4 5 5 13 2 | 25 28 22 24 26 24 30 23 26 29 25
31 | 8 7 7 8 10 4 7 14 6 18 3 | 32 37 32 34 36 32 37 31 31 39 33
32 | 4 9 6 6 10 4 7 7 6 9 2 | 30 33 28 29 31 27 33 29 25 31 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 9 10 14 4 8 17 7 16 |T 33 33 37 33 34 30 33 30 32 33 39
WRMS | 9 12 10 10 13 4 8 15 6 15 |NE 30 31 37 30 31 27 31 28 29 32 39
MEDI | 9 10 7 9 13 4 7 15 7 15 |MD 30 31 28 30 32 28 32 27 28 31 28
Table 3.2065.5 GPS week: 2065 Day: 5 MJD: 58704.000
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 11 9 7 12 3 4 11 6 8 2 | 26 30 26 27 30 24 27 24 26 25 26
2 | 6 7 9 10 15 5 4 31 11 18 4 | 28 33 29 33 31 28 30 31 32 28 28
3E | 7 29 18 35 17 4 8 11 15 10 6 | 50 55 51 58 56 54 42 48 54 48 54
X4 | 3 --- 355 --- --- 21 --- --- --- --- 0 | 23 --- 256 --- --- 40 --- --- --- --- 174
5E | 11 9 8 12 18 4 7 12 20 11 4 | 147 147 146 147 150 147 148 147 148 145 147
6 | 6 11 10 8 14 4 7 10 10 8 3 | 33 39 36 36 36 33 38 35 35 38 35
7 | 6 13 7 9 10 3 5 15 5 17 3 | 35 34 32 37 34 33 33 34 35 36 33
8 | 9 12 12 8 13 3 8 8 6 11 3 | 26 26 26 25 29 24 26 23 26 24 25
9 | 7 8 8 7 9 3 5 12 6 8 2 | 57 60 45 48 60 59 48 60 101 45 59
10E | 9 12 18 23 14 4 7 13 11 10 4 | 49 56 54 57 57 53 46 55 53 53 53
11 | 8 11 14 7 13 4 7 30 8 15 4 | 25 28 21 23 23 20 26 23 21 16 20
12E | 6 16 8 8 14 6 8 17 10 16 3 | 47 50 49 49 50 50 49 48 52 49 48
13 | 7 11 10 8 10 4 8 15 7 16 3 | 39 44 39 37 43 41 45 41 41 44 40
14 | 8 7 7 10 10 4 5 16 7 21 3 | 53 52 52 56 53 51 52 52 51 52 52
15 | 8 9 6 9 12 3 5 21 5 18 3 | 42 41 40 44 40 40 43 37 38 40 40
16E | 7 23 8 16 45 5 8 19 7 15 5 | 16 21 18 23 34 17 18 20 19 17 17
X17 | 13 10 6 7 14 7 7 16 --- 18 4 | 25 20 15 22 22 18 21 17 --- 14 19
18 | 6 8 8 9 13 2 7 14 7 9 3 | 22 26 23 24 30 21 24 30 24 26 23
19 | 11 12 8 7 14 6 8 19 12 21 4 | 31 30 28 30 28 27 29 32 28 33 28
20E | 9 10 6 11 14 4 10 16 7 14 3 | 54 54 54 57 58 54 53 59 56 57 55
21 | 5 11 8 6 12 6 10 32 9 17 4 | 22 26 21 24 26 21 26 30 24 23 21
22E | 8 9 7 7 16 4 7 19 10 12 3 | 88 90 90 91 90 90 88 90 93 89 90
23 | 7 20 6 6 10 4 5 21 9 20 4 | 39 42 38 40 40 39 40 38 42 38 39
24 | 6 9 6 7 11 4 7 14 7 13 3 | 24 31 25 28 26 24 30 21 26 31 26
25 | 7 15 16 9 14 3 10 10 7 10 4 | 28 38 27 32 35 29 32 31 29 33 29
26 | 5 13 12 7 17 2 9 12 9 10 3 | 39 42 42 43 44 41 40 42 41 40 40
27 | 6 10 13 8 8 3 6 13 5 15 3 | 35 38 40 40 38 37 37 37 38 44 38
28E | 7 9 8 12 24 4 8 17 12 15 4 | 23 22 19 25 34 20 21 22 23 22 21
29 | 6 16 9 8 11 4 9 17 8 21 4 | 30 29 24 32 28 26 25 27 28 34 27
30 | 7 7 7 8 11 3 5 6 7 13 2 | 33 34 31 33 30 31 35 32 34 38 33
31 | 6 10 10 11 14 4 8 14 7 18 3 | 38 44 39 41 42 38 43 35 41 40 40
32 | 6 7 6 7 10 4 5 7 7 10 2 | 36 41 38 38 41 36 40 39 38 39 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 10 11 15 4 7 17 9 14 |T 39 42 46 41 43 39 40 40 43 40 44
WRMS | 7 13 10 10 13 4 7 15 7 14 |NE 33 35 42 34 35 32 34 33 36 34 39
MEDI | 7 11 8 8 13 4 7 15 7 15 |MD 33 38 36 37 36 33 37 35 35 38 35
Table 3.2065.6 GPS week: 2065 Day: 6 MJD: 58705.000
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 | 10 9 10 10 8 2 4 8 9 9 3 | 24 27 26 24 27 24 25 22 27 23 24
2 | 8 7 8 8 13 5 7 33 6 17 4 | 26 29 26 28 30 26 27 30 28 25 25
X3E | 14 14 19 30 18 6 --- 11 14 13 6 | 51 46 44 52 56 50 --- 43 47 49 51
X4 | 418 --- 3 --- --- 415 --- --- --- --- 0 | 31 --- 272 --- --- 50 --- --- --- --- 294
5E | 20 11 11 17 19 4 8 15 14 15 5 | 156 155 154 157 155 157 157 157 154 162 156
6 | 9 13 10 8 12 3 8 10 6 9 3 | 37 41 40 35 40 35 38 34 38 39 37
7 | 9 11 8 11 8 3 5 16 6 17 3 | 36 37 40 40 37 36 36 32 37 34 36
8 | 11 14 11 9 14 2 8 10 6 9 3 | 23 24 22 22 25 20 21 17 21 17 20
9 | 9 9 8 8 8 2 5 12 5 10 2 | 35 39 28 30 38 34 30 36 51 34 35
X10E | 12 17 16 16 12 5 --- 13 16 12 5 | 50 50 48 47 53 46 --- 49 49 51 49
11 | 15 13 15 13 10 4 7 29 10 16 5 | 25 30 24 26 25 23 28 28 27 17 22
12E | 10 17 9 12 12 4 7 18 7 14 4 | 54 51 49 56 52 50 50 44 50 46 49
13 | 8 12 9 9 9 4 9 16 6 12 3 | 36 43 34 35 37 36 41 40 38 41 37
14 | 10 10 7 7 9 4 5 16 7 21 3 | 51 50 49 52 51 49 50 54 49 56 50
15 | 11 10 7 7 11 4 6 19 7 18 3 | 50 50 48 48 45 47 48 38 47 44 46
16E | 12 21 8 15 43 7 9 19 6 17 6 | 24 28 20 25 42 21 21 22 26 24 23
17 | 12 11 7 8 10 4 5 15 7 18 3 | 24 20 15 19 21 18 21 15 17 17 19
18 | 8 8 8 10 13 3 7 15 9 12 3 | 18 22 21 20 28 19 21 26 21 24 20
19 | 11 13 8 8 10 6 5 19 8 20 3 | 33 32 31 32 30 30 31 35 32 32 30
20E | 19 12 7 13 11 4 7 16 10 13 4 | 55 51 53 55 60 52 55 54 49 57 53
21 | 10 9 6 7 9 5 8 32 9 17 4 | 25 29 21 25 24 22 24 31 26 22 21
22E | 13 13 6 14 11 3 8 15 11 11 4 | 97 92 91 94 96 93 93 92 91 96 93
23 | 10 19 6 8 11 4 6 20 6 19 4 | 36 37 34 36 40 36 37 38 35 38 35
24 | 10 12 6 9 13 4 5 13 7 13 3 | 19 25 19 26 18 19 25 14 19 27 20
25 | 7 13 16 7 13 3 8 9 7 10 3 | 25 32 26 27 28 24 28 26 27 26 25
26 | 8 12 14 10 16 4 8 11 6 12 3 | 32 29 29 32 35 29 28 31 31 33 29
27 | 10 9 10 15 7 4 7 13 6 11 3 | 40 42 40 40 43 39 41 39 40 45 40
28E | 8 11 7 19 28 4 6 15 6 15 4 | 22 22 19 20 39 18 19 25 21 24 19
29 | 8 19 6 8 9 5 8 18 6 14 3 | 38 37 32 38 34 34 32 33 35 36 34
30 | 9 8 6 11 11 3 5 8 6 14 3 | 24 28 25 25 22 23 29 23 26 30 25
31 | 7 8 8 8 10 3 7 12 7 19 3 | 42 44 41 43 45 40 45 36 42 44 41
32 | 12 8 7 6 9 3 7 7 6 10 2 | 28 32 30 31 32 29 32 30 28 34 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 9 11 14 4 7 17 8 15 |T 39 41 45 40 42 38 39 38 39 40 46
WRMS | 10 12 9 12 12 4 7 15 7 14 |NE 31 33 41 32 33 31 32 31 32 32 42
MEDI | 10 12 8 9 11 4 7 15 7 14 |MD 33 37 31 32 37 34 31 33 35 34 34
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 4.2065 GPS week: 2065 MJD: 58699.0-58705.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 |U 0 0 0 |U 40 110 195 |U 12 11 33 |
emr | emr 2946 |U 0 0 0 |U 37 97 179 |U 15 14 43 |
esa | esa 3030 | 0 0 0 |U 37 102 185 | 13 13 39 |
gfz | gfz 2934 |U 0 0 0 |U 37 83 138 |U 13 14 36 |
grg | grg 2959 |U 0 0 0 |U 41 102 196 | 13 16 38 |
igr | igr 2934 | 0 0 0 | 38 104 188 | 12 13 35 |
igs | igs 2947 | 0 0 0 | 38 102 185 | 12 13 36 |
jpl | jpl 2880 |U 0 0 0 |U 39 114 205 |U 17 18 47 |
mit | mit 2948 | 0 0 0 |U 36 41 132 |U 19 20 56 |
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 5.2065.0 GPS week: 2065 Day: 0 MJD: 58699.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | 6 12 32 | 11 12 33 |
emr | emr 2976 | ---- ---- ---- | 7 15 45 | 15 14 41 |
esa | esa 3072 | ---- ---- ---- | 5 15 40 | 13 11 34 |
gfz | gfz 2976 | ---- ---- ---- | 7 10 36 | 12 11 32 |
grg | grg 2976 | ---- ---- ---- | 6 13 33 | ---- ---- ---- |
igr | igr 2976 | ---- ---- ---- | 5 11 36 | 12 11 31 |
igs | igs 2976 | ---- ---- ---- | 5 12 36 | 13 12 32 |
jpl | jpl 2976 | ---- ---- ---- | 7 16 40 | 18 16 40 |
mit | mit 2976 | ---- ---- ---- | 10 17 61 | 15 19 41 |
Table 5.2065.1 GPS week: 2065 Day: 1 MJD: 58700.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | ---- ---- ---- | 4 13 28 | 13 12 26 |
emr | emr 2880 | ---- ---- ---- | 9 19 44 | 17 11 51 |
esa | esa 2976 | ---- ---- ---- | 5 16 34 | 14 13 39 |
gfz | gfz 2880 | ---- ---- ---- | 6 12 33 | 12 12 34 |
grg | grg 2969 | ---- ---- ---- | 6 15 35 | 13 17 38 |
igr | igr 2880 | ---- ---- ---- | 5 13 29 | 12 13 36 |
igs | igs 2880 | ---- ---- ---- | 5 13 29 | 13 13 36 |
jpl | jpl 2880 | ---- ---- ---- | 7 17 31 | 19 17 38 |
mit | mit 2880 | ---- ---- ---- | 20 29 75 | 38 43 92 |
Table 5.2065.2 GPS week: 2065 Day: 2 MJD: 58701.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | ---- ---- ---- | 7 12 36 | 11 9 43 |
emr | emr 2976 | ---- ---- ---- | 8 15 40 | 12 10 53 |
esa | esa 3072 | ---- ---- ---- | 6 14 47 | 12 10 49 |
gfz | gfz 2976 | ---- ---- ---- | 7 11 35 | 10 11 46 |
grg | grg 2976 | ---- ---- ---- | 8 10 41 | 13 12 46 |
igr | igr 2976 | ---- ---- ---- | 6 12 38 | 11 11 45 |
igs | igs 2976 | ---- ---- ---- | 6 12 39 | 11 11 46 |
jpl | jpl 2976 | ---- ---- ---- | 7 15 46 | 15 21 59 |
mit | mit 2976 | ---- ---- ---- | 20 27 72 | 14 22 67 |
Table 5.2065.3 GPS week: 2065 Day: 3 MJD: 58702.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 | ---- ---- ---- | 9 11 36 | 13 14 33 |
emr | emr 2968 | ---- ---- ---- | 8 15 40 | 18 16 46 |
esa | esa 2976 | ---- ---- ---- | 9 17 53 | 17 18 39 |
gfz | gfz 2880 | ---- ---- ---- | 10 14 42 | 14 14 37 |
grg | grg 2967 | ---- ---- ---- | 9 11 40 | 13 15 33 |
igr | igr 2879 | ---- ---- ---- | 9 14 49 | 14 15 35 |
igs | igs 2967 | ---- ---- ---- | 8 13 35 | 14 15 36 |
jpl | jpl 2784 | ---- ---- ---- | 11 22 62 | 19 17 49 |
mit | mit 2976 | ---- ---- ---- | 12 11 50 | 23 20 62 |
Table 5.2065.4 GPS week: 2065 Day: 4 MJD: 58703.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | ---- ---- ---- | 97 571 749 | 12 13 31 |
emr | emr 2880 | ---- ---- ---- | 89 472 613 | 17 15 39 |
esa | esa 2976 | ---- ---- ---- | 98 511 657 | 14 15 37 |
gfz | gfz 2880 | ---- ---- ---- | 89 393 520 | 23 26 35 |
grg | grg 2880 | ---- ---- ---- | 102 517 691 | 16 22 36 |
igr | igr 2880 | ---- ---- ---- | 96 534 701 | 11 15 31 |
igs | igs 2880 | ---- ---- ---- | 98 515 676 | 13 15 32 |
jpl | jpl 2784 | ---- ---- ---- | 97 583 791 | 18 18 46 |
mit | mit 2880 | ---- ---- ---- | 66 33 140 | 11 14 40 |
Table 5.2065.5 GPS week: 2065 Day: 5 MJD: 58704.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | ---- ---- ---- | 149 144 440 | 12 12 31 |
emr | emr 2974 | ---- ---- ---- | 129 130 426 | 13 16 36 |
esa | esa 3072 | ---- ---- ---- | 128 126 418 | 13 13 35 |
gfz | gfz 2976 | ---- ---- ---- | 132 132 261 | 11 12 35 |
grg | grg 2975 | ---- ---- ---- | 149 135 483 | 12 14 38 |
igr | igr 2975 | ---- ---- ---- | 136 131 422 | 12 12 32 |
igs | igs 2975 | ---- ---- ---- | 137 132 435 | 12 12 32 |
jpl | jpl 2976 | ---- ---- ---- | 134 129 428 | 16 17 43 |
mit | mit 2976 | ---- ---- ---- | 109 155 458 | 13 16 48 |
Table 5.2065.6 GPS week: 2065 Day: 6 MJD: 58705.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | ---- ---- ---- | 10 11 46 | 9 10 33 |
emr | emr 2974 | ---- ---- ---- | 10 14 44 | 13 15 34 |
esa | esa 3072 | ---- ---- ---- | 10 16 45 | 11 14 38 |
gfz | gfz 2975 | ---- ---- ---- | 10 12 42 | 10 11 31 |
grg | grg 2975 | ---- ---- ---- | 9 12 51 | 12 14 36 |
igr | igr 2975 | ---- ---- ---- | 9 15 43 | 10 12 33 |
igs | igs 2976 | ---- ---- ---- | 9 14 43 | 9 12 37 |
jpl | jpl 2784 | ---- ---- ---- | 9 19 35 | 15 19 53 |
mit | mit 2976 | ---- ---- ---- | 12 15 70 | 18 10 43 |
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 6.2065 GPS week: 2065 MJD: 58699.500-58705.500
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 | -10 -29 52 71 3 | 21 28
| 14 15 91 70 10 | 5
emr uuuuu | 28 16 52 132 7 | 28 34
| 42 10 66 79 12 | 5
esa uuuuu | 6 14 -19 12 2 | 14 20
| 7 13 39 68 4 | 3
gfz uuuuu | -21 8 20 -251 -4 | 32 35
| 20 15 52 64 6 | 3
grg uuuuu | -25 9 -23 -171 -3 | 1 12
| 20 21 49 66 4 | 2
igr xxxxx | 24 13 0 -41 1 | 1 16
| 11 6 26 36 5 | 4
irf xxxxx | 5 0 -22 -53 -1 | 3 16
| 6 11 24 34 8 | 4
jpl uuuuu | -11 -9 38 54 1 | 20 24
| 24 18 51 26 11 | 2
mit uuuuu | -11 12 -26 -165 6 | 30 34
| 14 7 46 58 7 | 5
ngs uuuuu | 18 -17 -57 95 -2 | 16 21
| 12 32 99 93 3 | 3
sio uuuux | 33 25 -121 126 -3 | 73 74
| 19 15 42 56 8 | 3
Table 7.2065.0 GPS week: 2065 Day: 0 MJD: 58699.500
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 -6 124 30 4 | 14 23
emr uuuuu | 5 27 91 255 19 | 22 29
esa uuuuu | 8 3 50 77 4 | 10 18
gfz uuuuu | -41 27 13 -344 6 | 28 32
grg uuuuu | 2 -30 -16 -212 -8 | 1 12
igr xxxxx | 35 3 -5 3 9 | -4 16
irf xxxxx | 8 5 -23 -11 12 | -2 16
jpl uuuuu | 12 -15 53 50 -17 | 20 23
mit uuuuu | -15 22 -27 -86 17 | 22 27
ngs uuuuu | 27 -31 -213 103 2 | 12 19
sio uuuux | -4 42 -154 68 11 | 69 70
Table 7.2065.1 GPS week: 2065 Day: 1 MJD: 58700.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -34 -23 73 -13 14 | 15 24
emr uuuuu | -5 18 119 114 11 | 23 30
esa uuuuu | 6 15 -39 28 2 | 11 19
gfz uuuuu | -16 15 82 -209 -8 | 30 34
grg uuuuu | -21 3 -32 -207 -4 | 1 12
igr xxxxx | 23 13 13 -16 0 | -2 16
irf xxxxx | 11 -1 -41 -52 3 | 0 16
jpl uuuuu | 31 -15 78 41 -7 | 19 23
mit uuuuu | -22 17 -65 -165 11 | 25 30
ngs uuuuu | 15 -33 -177 210 -3 | 14 20
sio uuuux | 32 45 -150 128 -9 | 70 72
Table 7.2065.2 GPS week: 2065 Day: 2 MJD: 58701.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 12 -28 81 63 16 | 19 27
emr uuuuu | 41 25 7 56 23 | 25 32
esa uuuuu | 8 16 -33 96 1 | 13 20
gfz uuuuu | 12 11 -13 -196 -12 | 32 35
grg uuuuu | -31 8 2 -132 -7 | 1 13
igr xxxxx | 24 19 30 -29 4 | 0 17
irf xxxxx | -3 3 -47 -58 2 | 2 16
jpl uuuuu | -33 15 15 82 1 | 20 23
mit uuuuu | -32 12 -87 -221 10 | 28 33
ngs uuuuu | -4 -75 29 38 -4 | 16 21
sio uuuux | 27 19 -67 110 2 | 71 73
Table 7.2065.3 GPS week: 2065 Day: 3 MJD: 58702.500
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 | -6 -49 -28 19 7 | 20 29
emr uuuuu | -17 16 17 104 5 | 26 34
esa uuuuu | 18 32 -27 8 5 | 12 19
gfz uuuuu | -13 23 -57 -161 -3 | 30 34
grg uuuuu | -1 19 -51 -49 -4 | 0 11
igr xxxxx | 34 16 -10 -20 5 | 0 17
irf xxxxx | 8 19 -17 -13 -1 | 3 17
jpl uuuuu | -17 -32 104 84 0 | 19 23
mit uuuuu | -11 12 3 -109 5 | 29 35
ngs uuuuu | 19 4 13 -64 0 | 16 21
sio uuuux | 42 20 -84 168 -6 | 72 74
Table 7.2065.4 GPS week: 2065 Day: 4 MJD: 58703.500
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 | -6 -49 107 115 -8 | 27 32
emr uuuuu | 4 21 23 34 5 | 31 37
esa uuuuu | 6 28 18 28 -6 | 17 21
gfz uuuuu | -25 -2 5 -288 -5 | 34 36
grg uuuuu | -30 30 -108 -166 3 | 3 10
igr xxxxx | 30 14 -14 -87 -4 | 6 14
irf xxxxx | 5 0 -37 -48 -10 | 8 14
jpl uuuuu | -33 -13 0 75 5 | 23 25
mit uuuuu | 9 15 -54 -160 -1 | 35 38
ngs uuuuu | 35 -14 30 65 -8 | 20 23
sio uuuux | 61 25 -184 200 1 | 76 77
Table 7.2065.5 GPS week: 2065 Day: 5 MJD: 58704.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -7 -19 125 92 2 | 28 32
emr uuuuu | 71 0 -35 165 -8 | 36 39
esa uuuuu | -2 9 -64 -49 1 | 18 22
gfz uuuuu | -19 -1 93 -275 -3 | 36 37
grg uuuuu | -42 32 -9 -177 -2 | 4 11
igr xxxxx | 8 18 -42 -49 -4 | 7 13
irf xxxxx | -3 -8 -8 -106 -10 | 8 14
jpl uuuuu | -21 -21 -44 26 16 | 23 26
mit uuuuu | -9 2 10 -253 0 | 37 39
ngs uuuuu | 14 17 -37 186 -2 | 21 23
sio uuuux | 34 20 -108 45 -8 | 78 79
Table 7.2065.6 GPS week: 2065 Day: 6 MJD: 58705.500
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 -32 -116 195 -11 | 23 30
emr uuuuu | 93 4 144 198 -9 | 31 38
esa uuuuu | -3 -3 -34 -101 3 | 13 21
gfz uuuuu | -48 -17 16 -285 1 | 31 34
grg uuuuu | -52 3 52 -252 -2 | -2 15
igr xxxxx | 10 9 28 -90 -5 | 2 16
irf xxxxx | 9 -18 24 -83 -4 | 2 18
jpl uuuuu | -14 16 62 24 11 | 19 23
mit uuuuu | 1 2 41 -163 0 | 32 36
ngs uuuuu | 19 10 -45 126 -1 | 15 21
sio uuuux | 38 1 -101 163 -12 | 73 75
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