[IGSREPORT-26304] Wk 2030 IGS Final Orbits
acc
acc at igs.org
Thu Dec 20 20:39:35 PST 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2030 (Dec 02, 2018 - Dec 08, 2018)
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:
igs2030[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2030[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2030[0-6].cls IGS GPS clock combination summary report.
igs20307.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs20307.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 | GLSV NAUR GLSV NAUR
0 | ESA | 22 DAV1
0 | GFZ | 16 DAV1 GODE POHN GODE KOKV POHN
0 | GRG | DAV1 GLSV DAV1 GLSV LHAZ YELL
0 | MIT | SCH2 SCH2
1 | ALL | 4 4
1 | COD | GLSV NAUR NICO PDEL RABT GLSV NAUR NICO PDEL RABT
1 | EMR | YELL
1 | ESA | 22 18 22 LHAZ NRIL NRIL RIO2
1 | GFZ | GODE KOKB POHN REYK GODE KOKB POHN REYK USUD
1 | GRG | GLSV TUVA GLSV LPGS TUVA YELL
1 | JPL | LAUT
2 | COD | NAUR TIXI LHAZ NAUR STJO TIXI
2 | EMR | 13 13
2 | ESA | 22 22 NICO PTBB WIND PTBB WIND
2 | GFZ | GODE POHN STJO GODE POHN STJO
2 | GRG | GLSV NICO GLSV PIE1
3 | COD | BAKE NAUR TIXI NAUR TIXI
3 | EMR | CRO1 KERG
3 | ESA | 19 22 22 FLIN FLIN KOKV
3 | GFZ | 8 24 ALBH GODE POHN ALBH GODE POHN
3 | GRG | LHAZ TRO1 BAKE LHAZ MANA TRO1
3 | MIT | PALM PALM
4 | COD | 11 11 NAUR TIXI KERG NAUR TIXI
4 | EMR | MCM4 MCM4
4 | ESA | 19 21 22 MAG0 MCM4 ABMF
4 | GFZ | CORD GODE IISC POHN CORD GODE IISC MAG0 POHN REUN
4 | GRG | DAV1 GLSV HOFN MCM4 ABMF GLSV HOFN MCM4
4 | MIT | ALBH BAKE SUTH BAKE SUTH
5 | COD | GLSV NAUR NRIL RIO2 TIXI WIND YAKT GLSV NAUR NRIL
5 | COD | RIO2 TIXI WIND YAKT
5 | EMR | GRAZ GRAZ PERT YAKT
5 | ESA | 19 21 22 ABMF ABPO ALIC ANKR CHPI DARW GRAS GUAT
5 | ESA | GUUG IQAL KOKV KOUR MKEA PBRI PETS RBAY RIOP THTI
5 | ESA | YAKT
5 | GFZ | ALGO GODE NRC1 POHN ALGO GODE NRC1 POHN
5 | GRG | GLSV ABMF DARW GLSV
5 | JPL | NRIL HOFN NRIL SYOG
5 | MIT | NRC1
6 | COD | NAUR TIXI NAUR TIXI
6 | EMR | MCM4
6 | ESA | 18 22 18 LAUT
6 | GFZ | GODE POHN GODE POHN
6 | GRG | GLSV MCM4 WIND DARW GLSV LHAZ MCM4 WIND
6 | JPL | LAUT
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. 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.
7. 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 .1 1.4 5 29 -7 -.49
EMR | 0 | 7.5 6.6 18.2 -17 45 -48 -.19
ESA | 0 | -.1 .6 1.0 18 8 14 -.27
GFZ | 0 | .5 -.1 .8 -8 -24 0 -.23
GRG | 0 | 4.6 1.5 9.1 37 12 54 .03
JPL | 0 | 6.7 -.1 18.3 0 0 15 -.29
MIT | 0 | 8.5 .9 14.4 10 47 -26 -.16
NGS | 0 | 4.3 4.5 .7 48 -50 42 -.22
SIO | 0 | -2.1 1.1 6.5 27 21 -35 -.11
COD | 1 | .4 .0 .8 0 24 -8 -.46
EMR | 1 | 3.5 11.7 23.8 -13 44 -31 -.21
ESA | 1 | -.8 .3 .9 4 23 7 -.28
GFZ | 1 | .2 -.5 1.3 -18 -29 0 -.11
GRG | 1 | 4.2 3.1 7.5 31 17 67 -.03
JPL | 1 | 2.1 1.1 18.3 9 13 -1 -.54
MIT | 1 | 7.4 2.1 12.7 -6 54 -35 -.23
NGS | 1 | 3.1 1.7 13.4 2 -75 27 -.11
SIO | 1 | 6.2 .3 13.0 37 17 -45 -.32
COD | 2 | .2 .0 .7 6 12 -11 -.39
EMR | 2 | -6.3 2.2 23.3 -22 44 -68 .0
ESA | 2 | .1 .4 1.4 1 18 6 -.42
GFZ | 2 | .7 .4 .8 -10 -25 -1 -.22
GRG | 2 | .7 6.8 17.6 36 14 61 -.11
JPL | 2 | -1.6 4.5 16.5 15 -17 -20 -.18
MIT | 2 | 2.9 5.5 17.8 0 59 -41 -.15
NGS | 2 | -4.1 7.8 13.3 22 -56 30 -.13
SIO | 2 | -2.0 6.6 18.1 30 5 -68 -.03
COD | 3 | .8 -.1 1.1 12 16 -3 -.55
EMR | 3 | -3.0 4.9 19.2 -24 48 -103 .02
ESA | 3 | .1 .9 1.0 4 5 4 -.40
GFZ | 3 | .3 .2 .5 -4 -23 6 -.21
GRG | 3 | 2.6 5.5 10.1 39 -1 60 .0
JPL | 3 | 2.9 3.5 19.2 1 0 1 -.24
MIT | 3 | 5.2 3.2 15.1 -13 37 -15 -.04
NGS | 3 | -1.0 4.6 11.2 14 -50 0 -.12
SIO | 3 | 1.1 1.8 5.6 22 -8 -40 -.04
COD | 4 | .3 -.1 .5 6 6 1 -.23
EMR | 4 | -2.0 1.6 21.7 -29 14 22 -.15
ESA | 4 | .0 1.0 1.0 -2 24 16 -.25
GFZ | 4 | .1 .5 .3 0 -23 -3 .01
GRG | 4 | 3.4 3.3 6.9 35 5 58 -.19
JPL | 4 | 7.5 -2.7 12.1 -3 -1 12 -.13
MIT | 4 | 8.3 3.3 10.8 -4 33 -21 -.05
NGS | 4 | .4 1.6 10.0 4 -60 9 .15
SIO | 4 | 6.7 -.3 11.7 7 -4 -12 .19
COD | 5 | .1 .4 1.0 17 11 -12 -.34
EMR | 5 | 1.2 6.7 15.8 -25 -1 -34 .03
ESA | 5 | -.4 .9 1.4 -2 16 8 -.27
GFZ | 5 | .7 -.2 .5 -1 -38 6 -.22
GRG | 5 | 6.3 1.2 14.3 25 8 57 .06
JPL | 5 | 8.3 -2.0 3.5 -3 -6 -12 .05
MIT | 5 | 4.3 4.5 13.2 -17 46 -27 -.07
NGS | 5 | -3.3 1.5 1.2 -12 -28 8 -.08
SIO | 5 | 5.3 1.9 8.1 3 25 -28 -.04
COD | 6 | -.0 -.0 .6 12 27 6 -.26
EMR | 6 | -1.9 10.9 22.1 -26 14 23 .14
ESA | 6 | -1.2 .4 1.1 3 16 9 -.36
GFZ | 6 | .4 .1 .6 -4 -21 -3 -.07
GRG | 6 | 2.9 1.0 10.1 35 12 55 -.03
JPL | 6 | 4.3 .6 14.3 1 19 3 -.40
MIT | 6 | 3.4 3.8 8.1 -16 28 -38 -.11
NGS | 6 | -.8 2.9 2.2 1 -45 21 -.15
SIO | 6 | -1.4 3.1 6.5 17 15 -29 .23
8. 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.
9. 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 1.2030.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2030.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 2.2030.[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 3.2030.[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 5.2030.0-6). 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 2030 summary. (Dec 02, 2018 - Dec 08, 2018)
Table 1.2030.a GPS week: 2030 MJD: 58454.000-58460.000
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 253| -1 1 0 27 2 6 -.02 10 10 | -609 188 7 88
| 0 0 1 11 11 10 .04 | 168 206
emr 79| 0 0 9 -38 -1 17 .16 13 13 | 144452 5 16 155
| 0 1 1 12 12 11 .03 | 14554 469
esa 150| 0 0 0 4 7 2 -.06 8 8 | -1043 665 7 205
| 0 0 0 6 13 7 .01 | 287 524
gfz 179| 0 -2 1 0 -9 6 .06 10 10 | -218 -26 11 105
| 0 0 2 11 9 10 .03 | 200 487
grg 105| 1 0 -6 -30 -3 -52 -.15 11 11 | 97 22 10 159
| 0 0 3 8 6 14 .01 | 117 246
igr n/a| 0 0 -1 3 -10 15 -.05 4 4 | 1528 94 11 69
| 0 0 0 9 12 11 .01 | 530 434
jpl 80| 0 0 5 18 3 17 .20 9 9 | 213452 -31 9 94
| 1 0 1 9 16 17 .02 | 343 464
mit 348| 1 0 -3 6 8 -18 -.06 13 12 | -554 -91 77 1596
| 0 0 0 21 23 12 .02 | 315 180
ngs 204| 0 0 -2 -12 -19 8 -.05 10 10 | -615 221 773 1977
| 0 0 2 11 8 8 .02 | 147 235
sio 253| 1 0 -8 10 10 -5 .01 15 14 | --- --- --- ---
| 1 0 1 25 29 24 .04 | --- ---
Table 1.2030.b GPS week : 2030 MJD: 58454.000-58460.000
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 4 3 4 |
2 | 4 4 5 4 4 4 4 |
3 | 3 3 3 3 3 3 3 |
4 | 0 12 0 11 0 0 0 |
5 | 4 4 4 4 4 4 4 |
6 | 4 4 4 4 4 3 3 |
7 | 3 4 5 4 4 4 4 |
8 | 4 4 4 4 4 4 4 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 3 3 4 3 |
11 | 3 3 4 4 4 3 4 |
12 | 5 5 5 5 4 4 4 |
13 | 4 4 4 4 4 4 5 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 5 4 4 4 4 |
16 | 4 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 5 5 6 5 5 5 6 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 4 5 4 |
21 | 4 4 4 4 4 4 3 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 5 5 4 5 4 |
24 | 4 4 4 4 4 0 3 |
25 | 4 4 3 3 3 3 3 |
26 | 4 3 4 3 4 4 3 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 6 5 5 5 5 5 |
30 | 6 5 5 4 4 4 4 |
31 | 4 4 4 3 3 4 4 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2030.0 GPS week: 2030 Day: 0 MJD: 58454.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| -1 0 1 34 -19 4 .04 11 10 | -641 119 7 79
emr 80| 0 0 8 -33 -1 19 .16 13 13 | 139296 -781 13 144
esa 150| 0 0 1 9 14 -3 -.05 8 8 | -840 85 9 197
gfz 177| 0 -2 2 -5 -15 -7 .06 10 10 | 88 -828 13 92
grg 108| 0 0 -7 -24 0 -50 -.15 10 10 | 176 -96 10 154
igr n/a| -1 0 0 -14 -25 -1 -.06 4 4 | 1024 -237 10 69
jpl 80| -1 0 6 8 1 35 .19 8 8 | 213816 -753 9 106
mit 348| 2 0 -2 19 22 -30 -.05 13 12 | -216 -103 135 1336
ngs 207| 0 0 -4 -8 -25 12 -.07 9 9 | -760 346 828 2357
sio 236| 0 0 -6 0 37 14 -.04 14 13 | --- --- --- ---
Table 2.2030.1 GPS week: 2030 Day: 1 MJD: 58455.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| -1 1 0 20 5 6 .00 11 11 | -893 586 7 79
emr 80| 0 0 11 -24 2 0 .15 12 12 | 138702 -329 16 154
esa 150| 0 0 0 7 8 6 -.07 7 7 | -1432 1101 7 191
gfz 177| 0 -2 0 -1 -24 0 .07 11 11 | -161 -90 12 112
grg 108| 1 0 -10 -21 -12 -49 -.15 11 11 | -3 -17 11 153
igr n/a| 0 0 0 0 -22 20 -.05 4 4 | 888 39 11 67
jpl 80| -1 -1 6 17 0 25 .18 9 9 | 213251 -428 9 83
mit 349| 1 -1 -3 12 25 -29 -.07 14 12 | -636 -369 134 1787
ngs 209| 0 0 1 -28 -24 16 -.07 10 10 | -688 332 805 2013
sio 253| 0 -1 -9 14 14 -3 -.00 16 15 | --- --- --- ---
Table 2.2030.2 GPS week: 2030 Day: 2 MJD: 58456.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| -1 0 -1 20 14 10 -.05 11 10 | -673 78 8 93
emr 79| -1 -2 7 -44 -1 32 .19 14 14 | 138616 139 18 148
esa 150| 0 0 0 -1 29 2 -.06 9 9 | -1365 1147 9 195
gfz 178| 0 -2 0 -20 -11 18 .05 10 10 | -338 427 11 92
grg 105| 0 1 -2 -22 0 -77 -.16 12 12 | 24 5 11 153
igr n/a| 0 0 -2 4 0 30 -.06 4 4 | 1166 411 11 70
jpl 80| 0 0 5 17 3 43 .18 10 10 | 213039 71 10 89
mit 349| 1 1 -2 39 -21 -30 -.04 12 11 | -318 -134 53 1802
ngs 202| 0 1 0 -27 -17 6 -.04 11 11 | -675 93 746 1684
sio 230| 3 1 -9 53 -38 -44 .04 16 15 | --- --- --- ---
Table 2.2030.3 GPS week: 2030 Day: 3 MJD: 58457.000
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 1 0 44 1 -3 -.04 10 10 | -616 268 8 93
emr 80| 0 -2 8 -21 13 9 .19 13 13 | 138681 745 16 162
esa 150| 0 0 0 13 7 10 -.07 8 8 | -1189 912 7 197
gfz 179| 0 -2 0 7 4 18 .06 11 11 | -395 475 10 108
grg 104| 1 1 -7 -31 0 -59 -.16 11 11 | -62 533 9 147
igr n/a| 0 0 -1 17 6 26 -.04 4 4 | 1427 929 11 82
jpl 80| -1 0 7 15 4 11 .21 9 9 | 213018 715 9 87
mit 349| 2 1 -3 -20 0 -9 -.06 13 13 | -1171 200 55 1435
ngs 201| 0 0 0 -12 -10 13 -.05 10 10 | -736 523 707 1723
sio 250| 1 0 -10 -15 -1 -12 -.04 15 13 | --- --- --- ---
Table 2.2030.4 GPS week: 2030 Day: 4 MJD: 58458.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 255| -2 1 1 24 8 8 -.01 9 9 | -391 -79 7 83
emr 80| 0 -1 9 -41 6 31 .13 13 13 | 139222 112 17 159
esa 150| 0 0 0 -2 13 9 -.06 9 9 | -671 111 9 228
gfz 183| 0 0 2 5 -9 2 .07 10 9 | 1 -441 11 99
grg 107| 1 1 -9 -29 0 -58 -.17 11 11 | 278 -182 10 171
igr n/a| 0 0 -1 8 -2 5 -.05 4 4 | 2171 -49 14 72
jpl 80| 0 0 5 14 18 3 .19 9 9 | 213595 160 8 91
mit 349| 1 0 -4 1 -5 -7 -.08 13 12 | -400 46 55 1307
ngs 204| -1 0 -1 -5 -28 -8 -.05 10 10 | -341 -166 762 2136
sio 239| 1 0 -7 -4 -14 31 .01 14 13 | --- --- --- ---
Table 2.2030.5 GPS week: 2030 Day: 5 MJD: 58459.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 253| -1 1 1 35 12 -3 -.05 11 10 | -419 212 7 96
emr 80| 0 0 9 -43 -27 15 .20 13 13 | 139196 140 18 162
esa 150| 0 0 2 3 -8 -10 -.06 8 8 | -871 141 7 222
gfz 180| -1 -3 4 11 -6 12 .11 11 11 | -293 -87 10 102
grg 104| 0 0 -2 -38 -14 -38 -.16 10 10 | 117 -178 9 167
igr n/a| 0 0 0 5 -20 7 -.03 4 4 | 2052 -149 10 65
jpl 80| 1 0 3 39 -27 7 .23 10 10 | 213667 72 10 103
mit 349| 0 0 -5 -19 46 -2 -.05 14 13 | -482 -207 57 1824
ngs 202| -1 0 -6 -4 -5 14 -.04 11 11 | -516 365 643 1712
sio 283| 0 0 -7 -11 46 0 .01 14 14 | --- --- --- ---
Table 2.2030.6 GPS week: 2030 Day: 6 MJD: 58460.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 252| -1 0 3 11 -3 25 -.07 8 9 | -635 133 8 93
emr 80| 0 1 8 -57 -5 17 .11 13 13 | 177453 15 19 162
esa 150| 0 0 0 0 -8 1 -.07 8 8 | -934 1162 7 209
gfz 179| 1 -1 -2 8 -1 -2 .01 10 10 | -429 358 10 136
grg 105| 1 0 -5 -45 0 -32 -.13 11 10 | 150 93 10 172
igr n/a| 0 0 -1 2 -6 19 -.05 4 4 | 1968 -281 10 59
jpl 80| -1 0 6 16 24 -5 .18 9 9 | 213780 -57 10 105
mit 349| 0 0 -4 13 -5 -17 -.05 14 13 | -655 -73 54 1686
ngs 205| 0 0 -2 0 -25 6 -.03 10 10 | -591 59 925 2217
sio 280| 1 -1 -10 33 25 -21 .08 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 3.2030.0 GPS week: 2030 Day: 0 MJD: 58454.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 12 6 8 10 3 7 6 7 17 3 | 23 24 24 24 22 21 26 23 22 32 23
2 | 13 12 5 13 13 4 11 15 10 14 4 | 42 42 43 45 43 42 42 43 42 42 41
3 | 8 9 11 3 6 5 8 5 8 9 2 | 24 32 25 25 23 25 31 25 25 28 25
X4 | 2 --- --- --- --- 19 --- --- --- --- 0 | 38 --- --- --- --- 35 --- --- --- --- 38
5 | 10 10 11 6 6 3 7 15 10 16 3 | 41 40 43 43 38 39 46 39 38 41 40
6 | 10 9 7 15 12 4 8 8 7 12 3 | 33 36 32 37 33 33 36 34 33 41 34
7E | 7 17 7 6 10 3 11 8 6 7 3 | 40 33 38 37 44 37 34 39 40 41 37
8 | 8 13 7 10 10 6 9 12 9 18 3 | 27 30 27 29 28 25 29 26 27 32 26
9 | 7 7 13 6 6 4 6 6 5 9 2 | 22 25 23 21 20 20 26 19 19 21 21
10 | 8 10 10 7 5 4 9 9 6 6 3 | 24 33 22 23 28 25 35 27 27 31 26
11E | 10 12 9 9 7 4 7 8 9 12 3 | 65 58 60 61 58 59 63 61 58 65 60
12 | 16 15 6 12 11 4 7 18 12 19 4 | 35 32 28 32 29 29 32 33 31 33 30
13 | 8 12 11 10 9 4 9 15 11 14 4 | 34 41 31 29 37 36 40 36 38 40 35
14 | 9 7 9 10 9 3 7 16 12 17 3 | 31 33 32 34 34 34 32 38 40 37 33
15 | 11 10 9 11 8 4 8 17 12 18 4 | 55 60 55 54 48 49 57 46 45 45 51
16 | 12 21 7 9 10 4 9 14 11 18 4 | 32 26 26 28 27 27 28 31 30 29 26
17 | 7 11 6 13 15 3 9 14 10 11 3 | 23 25 21 30 23 24 25 26 27 25 23
X18 | 13 13 9 11 13 5 8 12 13 --- 4 | 33 31 30 35 28 29 32 36 29 --- 30
19 | 11 12 6 11 14 3 7 16 10 14 4 | 28 25 24 29 25 23 25 23 25 23 24
20 | 12 9 7 9 5 4 7 14 11 16 3 | 25 25 24 23 29 25 26 31 28 33 25
21 | 9 13 6 11 9 5 10 14 10 14 3 | 30 31 28 31 29 27 30 30 27 29 28
22 | 7 10 7 7 4 4 6 14 11 18 3 | 25 25 23 26 23 24 24 29 26 29 24
23 | 10 19 11 6 6 6 7 15 12 19 4 | 23 21 19 24 22 23 20 29 29 29 22
24E | 8 9 12 9 11 5 7 15 5 10 3 | 24 23 27 23 20 22 21 23 22 25 22
25 | 15 14 5 9 7 3 8 9 6 10 3 | 26 24 23 25 21 23 25 21 19 25 22
26 | 13 10 4 11 9 3 9 9 8 14 3 | 28 27 25 23 27 25 28 23 24 28 24
27 | 10 11 6 8 11 6 10 13 11 16 3 | 24 27 24 24 25 24 26 27 25 29 23
28 | 6 12 9 8 10 2 7 19 10 14 3 | 20 25 22 24 19 21 23 22 24 24 20
29 | 13 20 5 9 10 5 12 17 12 18 4 | 25 25 23 26 24 23 24 26 26 24 23
30E | 20 19 10 20 21 6 11 10 7 13 5 | 40 35 33 31 27 28 29 30 28 28 28
31E | 17 10 5 10 14 3 8 19 8 11 4 | 45 49 49 50 46 48 48 53 49 52 47
32 | 7 7 11 6 8 3 6 7 7 10 2 | 21 26 20 19 19 18 24 16 21 23 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 8 10 10 4 8 13 9 14 |T 31 31 29 31 29 29 31 31 30 32 29
WRMS | 10 13 8 10 10 4 8 12 9 13 |NE 30 30 28 29 27 28 31 28 28 30 28
MEDI | 10 12 7 9 10 4 8 14 10 14 |MD 28 30 26 29 27 25 29 29 27 29 26
Table 3.2030.1 GPS week: 2030 Day: 1 MJD: 58455.000
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 11 6 10 11 3 7 7 6 13 3 | 19 26 19 23 23 20 23 21 22 28 21
2 | 12 13 5 15 11 4 11 14 9 14 4 | 41 38 37 42 40 37 37 38 39 40 38
3 | 8 9 8 9 8 3 8 6 6 14 3 | 21 28 21 21 19 20 29 21 22 28 22
X4 | 10 13 --- --- --- 19 --- --- --- --- 11 | 30 17 --- --- --- 28 --- --- --- --- 27
5 | 11 9 8 8 8 5 7 17 12 22 4 | 32 30 29 31 26 28 33 30 31 36 29
6 | 11 9 5 14 10 3 9 8 9 12 3 | 22 27 21 24 24 22 25 23 24 30 23
7E | 7 17 5 11 14 4 14 12 10 12 4 | 33 30 35 36 36 33 29 34 36 38 32
8 | 8 10 6 11 11 2 10 13 8 17 3 | 27 30 26 25 27 25 30 26 30 30 26
9 | 7 7 10 11 7 2 8 8 7 11 3 | 21 27 21 19 19 19 26 19 19 21 20
10 | 9 11 9 8 8 3 9 9 7 14 3 | 24 30 19 23 24 21 29 23 20 25 22
11E | 7 8 7 9 11 4 6 10 10 12 3 | 37 39 37 40 40 38 38 39 38 40 38
12 | 15 15 7 12 13 3 7 19 12 16 4 | 27 27 27 32 26 27 29 31 28 28 27
13 | 9 11 8 12 10 5 10 17 14 19 4 | 21 31 21 21 23 25 31 24 26 27 23
14 | 9 7 8 12 8 3 8 16 13 17 3 | 32 30 30 33 32 31 31 34 32 35 30
15 | 10 11 7 8 8 5 10 16 13 23 4 | 43 48 42 43 38 40 45 39 37 38 41
16 | 13 23 8 10 12 4 10 15 12 22 4 | 27 20 21 23 22 22 19 24 23 19 19
17 | 8 12 5 11 14 2 8 17 13 13 4 | 22 25 18 27 21 20 25 21 24 21 21
X18 | 9 10 8 15 --- 7 8 12 15 --- 4 | 22 24 23 27 --- 23 28 31 29 --- 24
19 | 13 10 5 11 16 4 8 17 14 15 4 | 20 19 17 25 20 16 18 20 18 19 17
20 | 9 9 7 7 7 3 7 14 11 23 3 | 21 20 19 21 22 20 20 22 21 26 19
21 | 8 11 5 22 11 3 9 15 13 17 4 | 23 21 22 30 27 22 23 23 20 24 21
22 | 7 9 6 11 7 3 6 12 10 19 3 | 22 22 17 18 18 19 22 21 21 26 18
23 | 10 20 10 10 7 6 8 15 12 22 4 | 25 18 16 22 22 21 20 25 23 24 19
24E | 12 10 11 11 12 5 8 13 8 13 3 | 21 21 25 25 20 21 20 21 18 27 20
25 | 14 13 6 14 8 3 9 10 5 10 3 | 18 22 19 24 18 18 22 17 15 17 18
26 | 8 13 5 9 11 2 10 10 8 13 3 | 23 27 22 21 22 21 24 20 21 24 21
27 | 8 12 6 11 12 3 10 12 7 19 3 | 23 23 22 20 21 20 22 24 23 29 21
28 | 11 11 10 9 10 4 8 21 9 11 4 | 22 23 20 22 17 19 25 20 20 18 19
29 | 22 20 5 16 13 4 8 21 17 23 5 | 24 19 17 28 19 18 19 20 22 19 18
30E | 18 9 8 13 21 5 12 12 10 15 4 | 38 29 28 26 28 25 27 24 30 28 27
31E | 7 11 4 10 14 5 10 20 8 15 4 | 39 37 35 38 35 37 38 38 35 38 36
32 | 9 8 10 7 9 3 7 8 7 13 3 | 19 24 16 16 19 16 23 16 16 28 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 7 11 11 4 9 14 10 16 |T 26 26 23 26 24 24 26 25 25 27 24
WRMS | 11 12 7 11 11 4 9 12 10 15 |NE 24 25 22 25 22 22 26 23 23 25 23
MEDI | 9 11 7 11 11 3 8 13 10 15 |MD 23 26 21 25 22 21 25 23 23 27 21
Table 3.2030.2 GPS week: 2030 Day: 2 MJD: 58456.000
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 12 5 11 13 5 10 7 6 15 3 | 36 40 34 34 31 33 36 34 34 43 34
2 | 14 14 7 12 13 4 12 15 12 18 4 | 51 53 51 52 46 51 52 52 51 48 49
3 | 7 9 9 11 10 3 9 7 9 10 3 | 36 39 33 33 30 31 37 32 33 35 33
X4 | 2 --- --- --- --- 21 --- --- --- --- 0 | 44 --- --- --- --- 49 --- --- --- --- 44
5 | 8 10 10 9 7 5 9 17 13 19 4 | 40 43 42 42 38 39 45 40 42 41 40
6 | 10 8 10 14 10 3 10 8 8 13 3 | 46 48 46 46 41 45 46 45 42 45 44
7E | 6 18 9 15 16 4 14 9 11 14 4 | 36 38 35 41 29 37 37 38 40 37 35
8 | 15 14 6 9 14 4 10 13 7 21 4 | 34 36 29 28 28 28 31 32 28 38 29
9 | 8 7 13 8 10 2 8 7 9 8 3 | 29 36 33 31 29 29 37 30 27 32 30
10 | 7 12 10 8 10 4 9 9 7 12 3 | 29 38 26 30 27 29 37 31 29 38 29
11E | 21 11 9 10 17 6 8 9 8 13 4 | 46 36 38 41 34 37 37 33 39 37 36
12 | 17 18 6 9 14 4 7 17 13 15 4 | 33 34 31 37 30 32 33 33 31 31 31
13 | 9 14 12 9 12 3 12 14 13 16 4 | 40 47 38 30 36 41 43 43 41 43 39
14 | 5 8 8 9 11 4 7 15 12 16 3 | 34 34 31 33 33 35 35 40 37 42 34
15 | 10 11 8 7 11 4 14 16 15 19 4 | 45 51 47 48 44 43 51 39 40 39 44
16 | 10 26 10 8 14 5 11 14 10 19 4 | 41 38 35 39 40 39 41 39 37 36 37
17 | 10 15 7 10 13 2 9 12 10 12 3 | 39 42 38 42 37 40 40 42 41 40 39
X18 | 17 10 9 22 12 6 11 17 14 --- 5 | 49 43 42 47 39 40 43 46 39 --- 41
19 | 13 14 7 10 14 4 9 14 12 15 4 | 35 36 32 34 31 33 32 33 30 34 31
20 | 7 11 9 7 10 3 7 12 11 16 3 | 28 33 30 33 29 31 32 34 33 37 30
21 | 8 14 5 12 12 4 10 12 11 15 3 | 38 39 39 43 42 38 42 39 38 36 38
22 | 10 9 10 12 8 5 9 14 11 24 4 | 35 34 29 31 29 31 33 32 33 36 30
23 | 9 21 12 8 11 5 7 13 14 18 4 | 32 31 29 33 28 32 31 35 33 33 30
24E | 10 13 14 9 10 3 8 11 6 14 3 | 27 34 32 27 24 28 27 28 26 28 26
25 | 15 11 4 7 10 3 9 9 8 10 3 | 27 30 28 33 26 28 33 28 25 31 28
26 | 8 10 8 11 13 3 10 6 9 14 3 | 31 35 30 34 33 31 36 31 31 34 31
27 | 10 13 7 9 13 4 11 11 8 22 4 | 34 39 32 32 32 33 37 37 32 39 33
28 | 12 16 11 9 9 4 7 15 15 16 4 | 29 35 32 35 29 32 36 32 36 28 31
29 | 13 26 7 9 10 5 10 13 15 18 4 | 39 36 37 41 35 35 37 36 36 35 35
30E | 18 7 10 15 19 4 10 9 7 12 4 | 32 31 30 29 21 26 28 25 25 29 25
31E | 12 12 6 9 16 4 8 11 9 9 3 | 44 46 44 48 40 45 48 45 46 47 44
32 | 5 9 11 7 12 4 7 6 9 9 3 | 28 35 29 28 27 28 34 27 27 32 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 9 10 12 4 10 12 11 16 |T 36 38 34 36 32 35 37 35 34 36 34
WRMS | 10 14 9 10 12 4 10 11 11 15 |NE 36 39 35 36 33 35 38 35 34 36 35
MEDI | 10 12 9 9 12 4 9 12 10 15 |MD 35 36 33 34 31 33 37 34 34 36 33
Table 3.2030.3 GPS week: 2030 Day: 3 MJD: 58457.000
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 4 10 9 3 10 9 9 13 3 | 26 27 23 22 26 22 26 28 25 31 24
2 | 10 14 5 11 11 4 10 15 10 15 4 | 35 33 33 37 33 33 32 36 31 34 32
3 | 8 7 11 6 11 4 8 7 7 13 3 | 24 30 24 24 23 23 31 28 27 35 25
X4 | 10 --- --- --- --- 14 10 --- --- --- 10 | 27 --- --- --- --- 25 14 --- --- --- 25
5 | 9 8 9 9 10 4 8 19 11 20 4 | 35 39 37 38 35 34 41 35 31 40 35
6 | 11 10 9 17 12 4 8 9 6 12 3 | 23 27 22 25 23 21 26 22 21 28 22
7E | 11 16 9 13 12 3 15 10 10 12 4 | 38 34 38 44 41 38 35 40 40 40 37
8 | 11 11 5 9 12 4 9 12 8 12 3 | 27 28 25 24 25 24 26 26 25 27 24
9 | 9 8 12 10 10 3 7 7 6 12 3 | 23 28 27 28 24 22 28 25 24 32 25
10 | 6 10 11 8 8 4 9 11 6 12 3 | 20 30 18 19 21 19 29 20 20 25 20
11E | 16 10 9 9 9 5 9 10 14 10 4 | 63 62 65 63 66 63 65 63 65 66 64
12 | 14 15 5 14 12 5 6 20 13 15 4 | 32 29 25 32 27 27 29 26 28 27 27
13 | 10 15 8 8 11 5 11 16 12 14 4 | 23 32 17 20 23 23 28 27 25 28 22
14 | 9 7 9 6 11 4 6 16 11 18 3 | 36 35 33 37 40 37 36 41 41 39 36
15 | 11 12 7 10 10 6 11 14 13 23 4 | 55 59 51 55 48 46 59 42 44 41 50
16 | 10 23 7 11 13 5 10 16 14 19 4 | 20 23 20 23 22 19 20 20 25 16 19
17 | 11 14 5 12 14 4 8 13 12 11 4 | 27 28 27 32 27 26 29 29 29 30 27
X18 | 15 12 10 17 12 6 8 12 17 --- 5 | 30 30 24 29 26 24 29 33 32 --- 26
19 | 14 16 5 9 15 5 7 15 12 14 4 | 26 25 25 25 24 22 25 24 24 24 23
20 | 8 9 9 8 8 5 7 16 10 20 3 | 21 20 19 20 22 21 21 21 22 26 18
21 | 7 10 6 11 14 5 12 15 10 11 3 | 24 25 25 26 26 24 27 24 23 24 23
22 | 8 8 10 7 9 3 6 16 11 18 3 | 28 26 23 25 25 25 28 31 23 33 25
23 | 9 20 11 12 9 5 7 14 13 21 4 | 29 23 23 32 29 29 27 34 31 36 27
24E | 9 10 12 14 12 5 6 9 7 9 3 | 18 20 24 19 20 20 21 19 19 21 18
25 | 11 11 5 7 7 5 9 11 8 11 3 | 23 23 20 23 18 20 23 17 20 20 19
26 | 9 10 4 10 9 2 8 10 8 12 3 | 21 29 23 22 24 21 26 22 22 23 22
27 | 12 11 5 9 13 3 9 12 9 14 3 | 22 25 22 23 23 21 24 23 22 21 21
28 | 10 14 11 12 12 6 6 19 10 14 4 | 20 27 22 25 21 20 24 23 22 24 20
29 | 15 21 5 10 11 7 15 17 13 18 5 | 23 24 20 23 21 22 23 23 25 20 20
30E | 13 8 9 17 16 4 9 7 5 11 4 | 28 30 29 22 25 23 25 24 25 29 24
31E | 7 9 7 10 11 4 6 11 9 11 3 | 35 37 36 36 34 37 37 38 38 41 36
32 | 9 8 11 9 10 4 7 9 7 11 3 | 23 28 21 19 23 20 28 19 21 26 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 8 11 11 4 9 13 10 15 |T 28 30 27 28 27 26 29 28 28 30 26
WRMS | 10 13 8 11 11 4 9 13 10 13 |NE 26 29 25 27 25 24 27 25 25 27 25
MEDI | 10 10 9 10 11 4 8 12 10 13 |MD 26 28 24 25 25 23 27 26 25 28 24
Table 3.2030.4 GPS week: 2030 Day: 4 MJD: 58458.000
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 14 6 10 10 4 9 8 8 15 3 | 21 23 23 21 23 20 25 25 21 32 22
2 | 9 14 4 12 12 3 9 14 10 14 3 | 48 47 48 48 54 46 45 47 46 49 47
3 | 7 8 13 7 9 3 7 7 5 11 3 | 21 30 23 20 21 20 30 24 21 29 23
X4 | 2 --- --- --- --- 29 --- --- --- --- 0 | 33 --- --- --- --- 35 --- --- --- --- 32
5 | 8 9 12 6 8 3 11 17 12 18 4 | 29 35 29 31 28 28 37 30 29 33 30
6 | 11 12 7 15 15 4 9 6 10 8 3 | 34 37 31 33 31 31 35 31 32 36 32
7E | 8 19 6 10 12 4 14 10 11 15 4 | 28 34 31 34 36 31 31 34 35 34 31
8 | 8 12 8 9 11 5 11 13 8 16 3 | 28 25 21 25 23 22 24 25 23 27 23
9 | 7 8 13 9 10 3 7 6 5 9 3 | 18 26 23 23 21 19 28 20 21 21 21
10 | 7 11 12 7 6 4 8 12 5 14 3 | 23 29 16 18 20 19 28 22 19 26 20
11E | 12 14 11 11 11 6 9 15 11 14 4 | 49 48 51 50 48 48 49 51 49 55 49
12 | 10 19 6 9 11 3 7 17 11 14 4 | 25 25 21 28 24 22 24 22 22 26 23
13 | 8 15 10 10 9 3 12 15 12 16 4 | 27 37 23 28 28 27 34 31 29 29 27
14 | 6 9 9 6 8 4 8 15 10 15 3 | 25 26 23 23 28 27 24 32 30 32 25
15 | 9 13 8 9 8 4 9 16 12 18 4 | 50 57 50 54 47 46 53 42 43 44 48
16 | 12 21 10 13 14 5 12 15 14 22 5 | 30 26 23 28 27 26 26 26 28 25 24
17 | 8 12 6 10 13 3 8 13 13 12 3 | 25 28 26 27 27 27 30 32 32 32 27
X18 | 12 13 10 17 14 4 11 18 12 --- 5 | 36 30 30 35 29 29 32 37 27 --- 29
19 | 11 16 7 8 13 5 8 13 13 13 4 | 26 24 24 23 24 21 24 23 24 20 22
20 | 8 10 9 7 6 4 7 16 11 24 4 | 18 19 17 16 19 17 20 26 21 31 18
21 | 9 10 6 10 10 4 8 13 9 13 3 | 24 25 27 26 30 24 25 26 23 24 24
22 | 6 10 8 7 9 4 7 14 9 17 3 | 20 20 17 19 20 19 21 23 20 24 19
23 | 8 20 11 9 10 5 6 14 11 18 4 | 19 18 18 26 25 23 22 27 24 24 21
24E | 7 10 13 10 14 5 7 12 6 13 3 | 22 27 27 25 24 24 26 23 23 28 24
25 | 10 12 6 8 7 4 8 7 7 7 3 | 18 21 22 21 19 20 23 17 19 19 19
26 | 8 15 8 10 10 3 9 9 8 10 3 | 26 28 26 27 24 25 25 23 25 26 24
27 | 11 12 6 9 14 5 11 12 7 16 3 | 25 24 21 23 21 22 22 24 21 24 21
28 | 10 12 8 9 13 4 8 16 13 11 4 | 18 26 20 23 21 21 24 23 27 26 21
29 | 14 23 6 9 13 6 10 16 12 16 4 | 28 24 23 27 24 23 25 24 23 20 22
30E | 10 9 10 15 15 4 10 10 8 12 4 | 25 26 27 21 24 21 23 23 23 27 22
31E | 7 12 7 10 12 4 7 9 9 10 3 | 33 36 35 35 32 35 34 36 36 36 34
32 | 7 9 11 10 9 4 7 8 5 11 3 | 19 25 18 14 20 16 24 15 18 26 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 9 10 11 4 9 13 10 14 |T 27 29 26 27 27 26 28 27 26 29 26
WRMS | 9 13 9 9 11 4 9 12 10 13 |NE 27 29 25 27 25 25 28 26 26 27 25
MEDI | 8 12 8 9 11 4 8 13 10 14 |MD 25 26 23 26 24 23 25 25 24 27 23
Table 3.2030.5 GPS week: 2030 Day: 5 MJD: 58459.000
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 10 6 8 10 4 8 9 7 10 3 | 28 26 25 24 24 24 28 29 27 27 25
2 | 19 11 7 14 10 9 13 14 10 9 4 | 94 97 97 95 94 95 99 99 95 97 96
3M | 11 7 11 8 7 5 8 10 7 12 3 | 34 36 29 31 26 28 35 28 27 36 30
X4 | 2 --- --- --- --- 16 --- --- --- --- 0 | 35 --- --- --- --- 27 --- --- --- --- 34
5 | 9 10 11 10 7 4 13 17 12 18 4 | 26 33 30 36 27 27 34 29 29 32 29
6 | 8 10 6 12 10 4 8 11 10 9 3 | 42 44 40 38 41 40 43 42 41 39 40
7E | 6 13 6 11 11 3 15 10 8 11 3 | 30 33 32 36 33 33 31 34 37 34 32
8 | 12 12 6 10 8 3 11 14 8 15 3 | 27 25 22 25 24 23 27 26 24 26 23
9 | 7 7 12 7 7 3 7 8 9 8 3 | 24 30 26 23 21 23 31 24 22 28 24
10M | 11 9 11 10 5 3 11 15 6 12 3 | 27 34 26 31 25 27 35 27 24 30 27
11E | 7 10 9 9 9 4 8 9 11 11 3 | 83 83 87 85 86 85 85 86 83 90 85
12 | 10 19 6 9 10 4 8 16 15 12 4 | 23 26 21 26 24 24 29 27 27 27 24
13 | 11 12 11 9 8 3 13 16 13 14 4 | 32 39 34 41 33 35 41 34 35 37 34
14M | 9 8 8 10 12 3 7 18 12 15 4 | 28 28 25 27 29 28 28 31 34 31 27
15 | 11 13 9 8 8 4 10 17 14 17 4 | 50 55 50 48 48 46 53 41 42 45 47
16 | 13 22 6 10 10 5 11 14 12 20 4 | 32 29 27 30 31 30 28 31 28 26 27
17 | 7 13 7 8 14 4 8 15 15 12 4 | 28 32 29 32 28 29 32 32 34 31 29
X18 | 12 15 11 16 11 7 10 18 14 --- 5 | 47 50 41 46 43 43 47 50 45 --- 44
19 | 8 18 6 12 14 5 8 16 14 14 4 | 23 25 25 25 25 23 26 23 23 24 23
20M | 10 10 8 14 10 4 11 19 12 20 4 | 38 37 37 40 35 34 35 30 34 33 34
21 | 10 10 7 17 16 4 9 15 11 13 4 | 50 45 47 52 46 46 46 45 46 44 46
22M | 10 8 8 10 8 4 7 14 11 17 3 | 32 30 25 28 24 28 30 28 26 31 27
23M | 11 22 10 7 9 4 7 26 14 17 5 | 33 26 25 30 27 29 30 41 33 32 29
X24E | 2 --- --- --- --- 30 --- --- --- --- 0 | 15 --- --- --- --- 17 --- --- --- --- 17
25 | 11 11 6 10 6 2 8 8 10 9 3 | 16 23 22 23 21 21 26 19 21 21 20
26 | 11 15 6 11 7 3 12 8 9 11 3 | 28 28 26 27 25 26 27 24 27 26 25
27 | 14 15 5 13 11 5 13 11 8 17 4 | 32 29 27 28 27 28 29 31 25 29 26
28 | 7 16 11 9 11 4 9 18 15 12 4 | 22 29 27 29 23 26 28 27 32 25 25
29 | 15 23 6 9 12 4 8 16 13 14 4 | 29 23 26 29 28 26 25 27 25 26 25
30E | 11 8 10 17 14 3 10 10 10 8 4 | 23 23 25 17 20 20 23 21 23 20 20
31E | 8 13 6 16 11 3 6 11 9 11 3 | 44 44 43 47 39 43 44 46 43 47 43
32M | 7 10 11 14 6 3 8 9 7 11 3 | 25 30 24 21 21 22 29 20 23 27 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 8 11 10 4 10 14 11 14 |T 34 36 34 35 33 33 36 35 34 35 33
WRMS | 10 13 8 11 10 4 10 13 11 14 |NE 29 31 28 30 28 28 31 29 28 29 28
MEDI | 10 11 7 10 10 4 8 14 11 12 |MD 29 30 27 30 27 28 30 29 28 31 27
Table 3.2030.6 GPS week: 2030 Day: 6 MJD: 58460.000
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 16 7 8 12 4 9 9 5 13 3 | 28 34 30 27 27 27 30 32 29 39 29
2E | 8 12 5 14 14 5 8 16 12 14 4 | 107 104 104 101 106 104 103 110 106 107 105
3 | 8 10 12 8 9 4 9 7 7 9 3 | 32 38 32 29 27 31 38 32 34 37 32
X4 | 3 --- --- --- --- 18 --- --- --- --- 0 | 30 --- --- --- --- 31 --- --- --- --- 30
5 | 6 9 10 9 7 4 12 21 12 15 4 | 39 46 43 41 39 37 46 34 35 37 39
6 | 8 8 8 8 9 4 10 9 10 11 3 | 42 47 44 44 41 44 46 46 46 49 44
7E | 6 14 6 11 15 4 13 12 11 9 4 | 38 35 39 44 41 39 36 42 42 42 39
8 | 7 13 5 10 11 5 10 11 8 11 3 | 33 29 29 32 27 29 33 31 28 36 30
9 | 8 7 13 8 9 3 8 10 7 8 3 | 26 35 31 30 27 28 34 28 29 31 29
10 | 6 10 10 8 5 4 9 10 8 12 3 | 33 40 30 34 32 31 41 33 31 37 33
11E | 10 12 10 8 14 3 8 10 7 14 3 | 82 80 82 80 84 80 79 78 79 79 80
12 | 10 16 5 8 11 4 8 20 11 14 4 | 35 35 28 31 32 29 33 29 31 28 30
X13 | 7 13 10 --- 8 4 12 18 15 17 4 | 43 53 42 --- 44 46 49 45 50 46 45
14 | 9 8 9 9 7 3 5 15 12 16 3 | 26 28 23 28 29 30 28 38 37 41 29
15 | 6 12 8 7 8 4 9 18 12 18 4 | 65 72 65 61 60 59 68 57 55 56 62
16 | 10 20 8 11 11 5 10 14 13 20 4 | 36 34 33 33 34 34 33 39 38 33 33
17 | 6 9 5 8 12 3 8 17 11 12 3 | 31 34 34 35 31 34 36 36 37 40 34
X18E | 14 12 13 20 16 10 11 17 13 --- 5 | 59 57 54 57 52 53 55 57 55 --- 55
19 | 9 14 5 10 13 4 9 17 14 15 4 | 27 27 26 28 26 24 28 24 25 25 25
20 | 8 8 9 10 8 5 6 15 12 21 4 | 39 42 38 39 45 37 39 44 40 48 39
21E | 6 9 5 13 8 4 6 14 9 10 3 | 43 43 43 43 43 41 41 41 41 43 41
22 | 7 8 8 6 8 4 8 14 11 17 3 | 29 31 28 28 26 31 32 34 35 36 29
23 | 10 20 9 8 10 4 5 16 12 18 4 | 33 30 30 35 34 35 32 42 39 40 33
24E | 6 9 10 9 13 5 7 10 8 7 3 | 16 17 14 14 15 17 17 15 15 19 17
25 | 11 12 5 11 7 3 9 11 10 9 3 | 25 24 22 25 23 22 26 20 22 22 22
26 | 9 11 6 12 8 3 9 8 9 10 3 | 26 32 28 29 27 27 31 26 27 31 27
27 | 6 14 6 11 13 4 10 12 6 14 3 | 36 34 33 35 29 34 34 39 34 38 33
28 | 7 12 9 10 12 4 7 19 10 12 3 | 27 30 26 32 25 28 29 29 33 34 28
29 | 16 28 7 9 12 6 7 17 19 15 5 | 34 33 28 32 29 29 30 29 27 29 28
30E | 11 8 13 13 16 4 7 13 10 8 4 | 30 25 30 21 25 23 24 25 26 25 24
31E | 8 11 6 10 12 4 7 13 9 11 3 | 57 59 57 56 52 57 60 57 60 58 57
32 | 8 10 11 9 8 3 8 8 8 10 3 | 30 37 27 30 27 28 36 30 30 36 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 8 10 11 4 9 14 10 13 |T 38 40 37 38 37 37 40 39 39 40 37
WRMS | 9 13 8 10 10 4 9 13 10 13 |NE 34 37 33 34 32 33 36 34 34 35 33
MEDI | 8 12 8 9 11 4 8 14 10 12 |MD 33 35 31 32 31 31 34 34 35 37 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 4.2030 GPS week: 2030 MJD: 58454.0-58460.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 |U 8 11 21 |U 11 14 41 |U 11 10 30 |
emr | emr 2976 |U 19 24 42 |U 15 19 48 |U 20 21 51 |
esa | esa 2962 | 10 13 25 |U 11 16 42 | 15 11 30 |
gfz | gfz 2948 |U 10 11 23 |U 11 16 41 |U 14 14 33 |
grg | grg 2933 |U 9 12 27 |U 11 15 47 | 14 11 29 |
igr | igr 2955 | 9 12 22 | 11 15 40 | 13 10 29 |
igs | igs 2973 | 10 14 24 | 11 15 41 | 15 11 31 |
jpl | jpl 2976 |U 15 21 33 |U 12 19 47 |U 21 17 44 |
mit | mit 2962 |U 29 24 41 |U 20 30 81 |U 19 19 46 |
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 5.2030.0 GPS week: 2030 Day: 0 MJD: 58454.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 8 12 22 | 10 16 40 | 11 15 32 |
emr | emr 2976 | 13 19 42 | 8 21 33 | 18 22 51 |
esa | esa 2976 | 8 12 26 | 8 13 36 | 14 14 31 |
gfz | gfz 2975 | 7 10 20 | 10 16 35 | 11 12 29 |
grg | grg 2976 | 6 10 24 | 9 14 40 | 12 10 26 |
igr | igr 2976 | 7 12 23 | 9 15 34 | 12 13 31 |
igs | igs 2971 | 7 13 25 | 8 12 34 | 13 14 32 |
jpl | jpl 2976 | 14 20 32 | 8 17 36 | 19 21 46 |
mit | mit 2976 | 89 78 80 | 42 85 180 | 19 23 54 |
Table 5.2030.1 GPS week: 2030 Day: 1 MJD: 58455.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 12 25 | 10 11 52 | 10 8 38 |
emr | emr 3072 | 20 27 54 | 14 19 47 | 20 25 59 |
esa | esa 2976 | 9 11 25 | 10 12 53 | 13 11 39 |
gfz | gfz 2976 | 10 10 23 | 10 13 50 | 16 39 64 |
grg | grg 2880 | 10 11 26 | 10 11 53 | 12 11 40 |
igr | igr 2953 | 9 11 23 | 10 12 48 | 11 10 38 |
igs | igs 2973 | 10 12 25 | 11 12 47 | 13 12 42 |
jpl | jpl 2976 | 14 18 30 | 12 16 52 | 18 19 55 |
mit | mit 2976 | 48 20 67 | 22 29 79 | 14 19 54 |
Table 5.2030.2 GPS week: 2030 Day: 2 MJD: 58456.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 12 20 | 9 15 48 | 11 11 25 |
emr | emr 2976 | 21 25 41 | 15 22 65 | 16 20 49 |
esa | esa 2976 | 9 14 24 | 9 16 50 | 13 10 26 |
gfz | gfz 2976 | 7 11 19 | 8 16 48 | 12 10 26 |
grg | grg 2880 | 7 12 28 | 9 16 54 | 13 10 28 |
igr | igr 2970 | 8 14 19 | 8 14 49 | 12 10 26 |
igs | igs 2975 | 8 16 24 | 9 15 51 | 14 9 26 |
jpl | jpl 2976 | 15 26 32 | 10 20 59 | 22 15 39 |
mit | mit 2976 | 12 18 22 | 11 21 66 | 14 13 32 |
Table 5.2030.3 GPS week: 2030 Day: 3 MJD: 58457.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 9 21 | 16 18 50 | 13 9 28 |
emr | emr 2976 | 13 19 33 | 21 21 68 | 21 18 44 |
esa | esa 2976 | 7 10 25 | 16 20 50 | 17 10 28 |
gfz | gfz 2976 | 5 7 20 | 16 22 50 | 14 8 27 |
grg | grg 2971 | 7 9 26 | 16 19 58 | 15 10 27 |
igr | igr 2971 | 6 9 20 | 17 18 50 | 14 8 28 |
igs | igs 3067 | 6 10 23 | 16 19 51 | 16 10 29 |
jpl | jpl 3072 | 11 16 32 | 16 22 58 | 23 19 41 |
mit | mit 2976 | 13 12 29 | 16 21 63 | 21 15 56 |
Table 5.2030.4 GPS week: 2030 Day: 4 MJD: 58458.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 13 17 | 16 10 36 | 12 10 34 |
emr | emr 2976 | 21 31 34 | 23 18 49 | 22 21 59 |
esa | esa 2976 | 8 14 20 | 19 20 46 | 15 10 35 |
gfz | gfz 2976 | 8 10 16 | 19 19 47 | 13 8 32 |
grg | grg 2976 | 8 14 21 | 20 18 47 | 14 11 33 |
igr | igr 2975 | 7 11 16 | 18 20 39 | 12 9 28 |
igs | igs 2976 | 8 15 19 | 20 17 44 | 15 11 35 |
jpl | jpl 2976 | 13 23 28 | 20 19 46 | 21 18 47 |
mit | mit 2976 | 14 17 34 | 31 25 99 | 15 10 47 |
Table 5.2030.5 GPS week: 2030 Day: 5 MJD: 58459.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2973 | 11 11 22 | 8 16 30 | 10 7 30 |
emr | emr 2880 | 28 24 40 | 11 13 36 | 24 16 42 |
esa | esa 2880 | 18 15 30 | 8 17 30 | 19 9 21 |
gfz | gfz 2880 | 16 14 34 | 8 15 30 | 19 14 23 |
grg | grg 2875 | 15 13 39 | 8 13 39 | 17 11 19 |
igr | igr 2878 | 15 14 26 | 7 17 29 | 15 8 25 |
igs | igs 2877 | 17 15 28 | 7 16 32 | 17 8 24 |
jpl | jpl 2880 | 25 24 38 | 9 23 40 | 23 12 36 |
mit | mit 2880 | 15 15 25 | 9 12 34 | 34 41 52 |
Table 5.2030.6 GPS week: 2030 Day: 6 MJD: 58460.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 9 9 23 | 8 12 29 | 11 10 26 |
emr | emr 2976 | 17 23 53 | 12 18 41 | 23 21 52 |
esa | esa 2976 | 11 14 30 | 9 13 28 | 15 13 31 |
gfz | gfz 2880 | 15 15 27 | 8 14 28 | 11 9 29 |
grg | grg 2976 | 13 15 29 | 8 15 35 | 12 12 28 |
igr | igr 2968 | 10 12 25 | 8 12 29 | 13 10 27 |
igs | igs 2976 | 11 14 28 | 8 13 31 | 14 12 30 |
jpl | jpl 2976 | 14 21 39 | 11 18 37 | 22 15 43 |
mit | mit 2976 | 10 10 32 | 11 19 43 | 16 13 27 |
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 6.2030 GPS week: 2030 MJD: 58454.500-58460.500
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 | -9 -24 59 -38 -1 | 4 21
| 10 10 78 71 7 | 4
emr uuuuu | 9 47 1 85 -5 | 27 34
| 24 11 120 49 11 | 3
esa uuuuu | -14 0 -88 -98 -5 | 14 23
| 10 9 68 33 1 | 4
gfz uuuuu | -11 -16 61 -114 -1 | 11 23
| 19 11 45 79 5 | 4
grg uuuuu | 28 22 20 134 0 | -3 16
| 19 11 55 45 4 | 3
igr xxxxx | -1 -11 20 -8 2 | -9 22
| 8 8 61 23 3 | 4
irf xxxxx | 4 -14 -5 56 5 | -4 21
| 7 7 28 17 5 | 4
jpl uuuuu | -15 -29 49 -59 7 | 23 31
| 15 14 60 35 11 | 5
mit uuuuu | 20 -9 -62 131 2 | 13 24
| 18 10 60 46 5 | 4
ngs uuuuu | 26 11 56 87 2 | 6 21
| 26 18 119 65 3 | 4
sio uuuux | -24 23 -143 -33 4 | 42 45
| 25 22 42 57 9 | 4
Table 7.2030.0 GPS week: 2030 Day: 0 MJD: 58454.500
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 | -3 -37 109 -137 9 | 5 24
emr uuuuu | 3 38 54 54 6 | 28 35
esa uuuuu | -19 2 -97 -133 -6 | 18 29
gfz uuuuu | -2 0 68 -53 -5 | 14 27
grg uuuuu | 13 26 25 210 1 | 0 19
igr xxxxx | 3 2 -11 30 -2 | -7 23
irf xxxxx | 2 -4 -2 60 -2 | -1 23
jpl uuuuu | -13 -21 70 -51 -5 | 26 37
mit uuuuu | 15 -17 -59 164 -4 | 17 27
ngs uuuuu | 24 5 -49 22 -1 | 9 25
sio uuuux | -16 17 -158 27 3 | 40 44
Table 7.2030.1 GPS week: 2030 Day: 1 MJD: 58455.500
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 -26 104 -88 0 | 7 24
emr uuuuu | 4 27 81 73 0 | 30 36
esa uuuuu | -28 -11 -8 -130 -5 | 19 29
gfz uuuuu | 6 -16 0 -32 -8 | 15 27
grg uuuuu | 39 23 72 143 4 | 1 19
igr xxxxx | 8 -12 65 -12 2 | -7 23
irf xxxxx | 16 -6 -7 84 0 | -1 23
jpl uuuuu | -9 -9 -18 -64 6 | 27 37
mit uuuuu | 12 -3 -62 197 -3 | 17 28
ngs uuuuu | 30 36 -45 64 3 | 9 25
sio uuuux | -24 -16 -193 1 18 | 41 45
Table 7.2030.2 GPS week: 2030 Day: 2 MJD: 58456.500
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 | -20 -22 66 -94 2 | 1 20
emr uuuuu | 9 54 104 43 -6 | 24 32
esa uuuuu | -17 11 -211 -130 -6 | 12 23
gfz uuuuu | 8 -13 20 -73 2 | 8 21
grg uuuuu | 65 0 64 176 -3 | -5 17
igr xxxxx | -5 -17 19 -3 5 | -13 23
irf xxxxx | 3 -25 29 68 11 | -8 21
jpl uuuuu | -24 -42 147 -82 -5 | 20 30
mit uuuuu | -12 -19 42 139 6 | 11 22
ngs uuuuu | 56 20 -105 170 5 | 3 21
sio uuuux | -69 45 -66 -84 11 | 38 42
Table 7.2030.3 GPS week: 2030 Day: 3 MJD: 58457.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 5 -29 50 -32 -3 | -1 18
emr uuuuu | -35 51 -125 37 5 | 23 29
esa uuuuu | 2 -1 -73 -51 -4 | 9 18
gfz uuuuu | -6 -24 105 -74 2 | 6 18
grg uuuuu | 26 36 -33 110 -5 | -7 15
igr xxxxx | -10 -20 -58 -38 5 | -14 22
irf xxxxx | 6 -19 -9 40 9 | -9 20
jpl uuuuu | -28 -29 54 -72 5 | 17 26
mit uuuuu | 17 -21 -59 123 1 | 9 20
ngs uuuuu | 45 21 130 119 6 | 1 17
sio uuuux | -36 17 -140 -138 -6 | 39 42
Table 7.2030.4 GPS week: 2030 Day: 4 MJD: 58458.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 -21 37 58 5 | 2 19
emr uuuuu | 12 47 -25 121 -21 | 26 33
esa uuuuu | -20 8 -115 -91 -4 | 10 19
gfz uuuuu | -11 -20 107 -128 5 | 7 20
grg uuuuu | 21 19 -74 107 -3 | -6 15
igr xxxxx | -11 -13 -45 9 3 | -12 23
irf xxxxx | -4 -12 -58 59 8 | -7 21
jpl uuuuu | -22 -31 59 -77 5 | 18 26
mit uuuuu | 33 -6 -150 134 3 | 10 21
ngs uuuuu | 17 15 184 6 1 | 3 20
sio uuuux | -8 20 -148 -20 3 | 40 44
Table 7.2030.5 GPS week: 2030 Day: 5 MJD: 58459.500
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 | -19 -27 142 20 -9 | 6 20
emr uuuuu | 32 61 -194 94 0 | 29 34
esa uuuuu | -4 -13 -16 -76 -5 | 13 21
gfz uuuuu | -38 -4 25 -201 4 | 11 22
grg uuuuu | 13 31 22 98 -1 | -3 15
igr xxxxx | 0 -11 83 -27 5 | -8 21
irf xxxxx | 10 -18 -7 33 2 | -2 21
jpl uuuuu | 15 -50 65 16 20 | 23 29
mit uuuuu | 44 0 -114 53 0 | 14 23
ngs uuuuu | -26 -6 105 66 1 | 7 21
sio uuuux | 10 51 -179 -9 -8 | 45 48
Table 7.2030.6 GPS week: 2030 Day: 6 MJD: 58460.500
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 | -2 -6 -99 6 -9 | 10 19
emr uuuuu | 39 50 110 175 -21 | 32 37
esa uuuuu | -8 1 -100 -77 -7 | 16 22
gfz uuuuu | -36 -33 98 -238 -6 | 14 24
grg uuuuu | 17 19 61 92 5 | 0 14
igr xxxxx | 6 -4 89 -14 -2 | -4 20
irf xxxxx | -5 -16 21 49 4 | 2 20
jpl uuuuu | -25 -19 -32 -81 23 | 29 35
mit uuuuu | 29 4 -35 103 9 | 17 25
ngs uuuuu | 34 -17 173 163 2 | 11 21
sio uuuux | -27 30 -119 -10 6 | 48 50
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