[IGSREPORT-27971] Wk 2158 IGS Final Orbits
acc
acc at igs.org
Sat Jun 5 03:40:43 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2158 (May 16, 2021 - May 22, 2021)
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:
igs2158[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2158[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2158[0-6].cls IGS GPS clock combination summary report.
igs21587.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs21587.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 | 2 21 2 21 TIXI ZECK TIXI
0 | EMR | 19 MDVJ MDVJ NIST
0 | ESA | PTBB PTBB
0 | GFZ | 21 ANKR ANKR
0 | GRG | SCUB SVTL SVTL
0 | JPL | ZECK
1 | COD | CHOF CPVG FAA1 GMSD MAJU MAS1 NRC1 SEYG TIXI ZECK
1 | COD | CHOF CPVG TIXI
1 | EMR | CHUR LPGS NRC1 ZECK
1 | ESA | ANKR ASCG MAS1 PTBB ASCG MAS1 PTBB
1 | GFZ | MAS1 WTZR MAS1 WTZR
1 | GRG | 6 BAKE HOLB HOLB HYDE
1 | JPL | SVTL BADG DAV1 MCM4 SVTL
2 | COD | CHUR FAA1 IENG MAS1 SFER TIXI TONG TIXI
2 | EMR | MDVJ IENG MAS1 MDVJ
2 | ESA | FLIN KIRU PTBB SFER CPVG FLIN KIRU MAS1 PTBB SFER
2 | GFZ | ANKR BOGT HOFN JOG2 MAS1 ANKR BOGT HOFN HOLB JOG2
2 | GFZ | MAS1 SFER
2 | GRG | BOGT CZTG SFER BOGT CZTG HOLB SFER SVTL
2 | JPL | CHUR CPVG FAIR
3 | COD | ASCG GMSD HYDE
3 | EMR | 19 19 KERG
3 | ESA | THU2
3 | GFZ | 21
3 | GRG | 21 CZTG JOG2 CZTG JOG2
3 | JPL | THU2
4 | COD | MCM4 NYAL POVE
4 | EMR | MDVJ CHUR MDVJ
4 | ESA | GRAZ MAC1 MAC1
4 | GFZ | IRKJ POVE
4 | GRG | FLIN FLIN IRKJ
4 | JPL | MCM4 MCM4 NYAL
5 | COD | 1 6 1 ABMF ALIC ARTU ASCG BOGT CAS1 CCJ2 CRO1 DGAR
5 | COD | GLSV GRAZ JFNG KARR KOKV KOUR KRGG MAJU MOBS NKLG
5 | COD | NLIB NNOR OHI3 OUS2 SALU SEYG SFER SGOC SSIA SUTH
5 | COD | TIXI TONG ULAB UNSA VILL WUH2 YAKT TIXI
5 | EMR | YELL
5 | ESA | 1 6 1 ANKR NANO PTBB YEL2 ANKR NANO PTBB YEL2
5 | GFZ | 1 6 1 MIZU USN7 KOUR MIZU USN7
5 | GRG | JOG2
5 | JPL | MCM4
6 | COD | 18 18 CHPG KIT3 NYA1 NYAL TIXI TONG TRO1 NYAL TIXI
6 | COD | TRO1
6 | EMR | MDVJ
6 | ESA | KIT3 MCIL PTBB PTBB
6 | GFZ | 18 21 18 21 LHAZ LHAZ
6 | GRG | 21 21 KIT3 SVTL KIT3 SVTL
6 | JPL | MCM4 KIT3 MCM4 NYAL
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. 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
----+--------+---------------
2 | GFZ | 18
3 | GFZ | 18
4 | GFZ | 18
5 | GFZ | 18
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .3 .1 .4 9 0 0 -.29
EMR | 0 | 5.8 3.6 -1.5 -31 19 2 -.02
ESA | 0 | -.6 -1.2 -1.1 -18 19 16 -.26
GFZ | 0 | -.1 -.1 .3 15 6 20 -.26
GRG | 0 | 1.6 1.1 -12.0 14 -44 18 .10
JPL | 0 | 7.4 -5.3 7.1 1 -12 14 -.07
MIT | 0 | 5.4 6.0 -2.1 -15 14 4 .09
NGS | 0 | 6.6 -1.2 7.4 -9 -39 -11 -.01
SIO | 0 | .0 5.5 2.5 94 -9 66 -.13
COD | 1 | .3 .1 .3 11 2 -1 -.28
EMR | 1 | 3.7 9.8 -.3 -21 12 -15 .28
ESA | 1 | -.8 -1.2 -1.2 -32 7 21 -.26
GFZ | 1 | -.1 -.2 -.0 13 -2 13 -.08
GRG | 1 | 4.1 3.2 -2.2 22 -23 2 .04
JPL | 1 | 6.8 .7 -.1 9 -6 -3 -.05
MIT | 1 | 5.9 5.1 -2.0 -15 6 5 .26
NGS | 1 | 5.8 3.1 3.5 -6 -4 -8 .02
SIO | 1 | 1.4 6.1 10.2 113 -45 67 .03
COD | 2 | .2 .2 .2 6 1 -1 -.20
EMR | 2 | 4.2 2.0 -.1 -1 -3 -15 .27
ESA | 2 | -.9 -.9 -.9 -22 23 22 -.10
GFZ | 2 | .1 -.0 .2 11 0 8 -.09
GRG | 2 | 6.5 .5 -4.6 21 -24 6 -.0
JPL | 2 | 6.9 3.0 3.6 -4 -4 -9 -.08
MIT | 2 | 8.0 2.7 -1.5 -15 8 3 .19
NGS | 2 | 4.8 .2 15.4 13 -53 32 .10
SIO | 2 | 1.2 5.2 10.6 91 -40 46 -.12
COD | 3 | .3 .2 .3 5 -1 6 -.27
EMR | 3 | -5.2 5.5 .9 -8 20 -7 .21
ESA | 3 | -1.0 -1.3 -.8 -9 23 16 -.20
GFZ | 3 | -.3 -.1 .3 11 4 14 -.14
GRG | 3 | 1.0 -2.2 -8.1 21 -9 -4 .09
JPL | 3 | 4.5 -.4 3.3 1 -7 -15 -.07
MIT | 3 | 2.5 2.0 1.9 -4 17 3 .18
NGS | 3 | 1.0 -5.7 9.3 -3 4 -13 -.02
SIO | 3 | -2.5 2.5 6.3 28 26 31 .03
COD | 4 | .0 .2 .3 4 2 0 -.27
EMR | 4 | -2.8 12.8 5.0 -19 22 -6 .21
ESA | 4 | -.6 -1.4 -1.1 -21 30 15 -.16
GFZ | 4 | -.2 -.3 .4 3 2 20 -.17
GRG | 4 | 1.2 1.7 -6.1 26 -14 13 .0
JPL | 4 | 9.2 -.1 -.6 6 0 -20 -.18
MIT | 4 | 3.2 2.8 -1.0 -9 28 -17 .14
NGS | 4 | .9 -1.1 8.3 -1 16 -4 -.01
SIO | 4 | -2.3 4.7 9.9 82 9 50 .09
COD | 5 | .3 .2 .2 4 -1 -3 -.29
EMR | 5 | 1.9 1.3 3.5 -5 24 1 .16
ESA | 5 | -.8 -.7 -1.1 -33 8 23 -.18
GFZ | 5 | -.2 .0 .1 7 -2 14 -.07
GRG | 5 | 3.0 1.9 -3.9 26 -9 19 -.01
JPL | 5 | 12.1 -2.2 3.8 -5 18 2 -.26
MIT | 5 | 1.5 1.1 .1 -10 15 6 .18
NGS | 5 | .7 -2.2 5.1 -16 0 4 .07
SIO | 5 | -2.8 3.9 16.8 46 3 55 -.03
COD | 6 | .2 .0 .5 6 2 6 -.26
EMR | 6 | 1.4 -5.9 4.0 -11 14 6 -.03
ESA | 6 | -1.0 -.8 -.9 -20 12 34 -.19
GFZ | 6 | -.1 .1 -.0 10 -4 20 -.13
GRG | 6 | 2.8 1.7 7.8 30 -7 7 -.07
JPL | 6 | -.6 -6.9 .2 7 0 -16 -.31
MIT | 6 | 2.3 .1 5.0 -14 11 -9 .04
NGS | 6 | 2.0 -7.1 10.1 -71 16 -14 .02
SIO | 6 | -4.5 3.7 16.5 46 42 47 -.01
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 1.2158.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2158.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 2.2158.[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 3.2158.[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 5.2158.0-6). 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 2158 summary. (May 16, 2021 - May 22, 2021)
Table 1.2158.a GPS week: 2158 MJD: 59350.000-59356.000
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 744| 0 0 -1 9 0 -12 -.01 7 7 | -655 131 6 91
| 0 0 0 14 15 9 .01 | 63 229
emr 79| -2 2 1 -1 3 18 .14 13 13 | 177147 -61 14 117
| 1 3 1 11 10 9 .02 | 1284 1128
esa 150| 0 0 -1 6 -1 9 -.06 7 7 | -1092 848 7 81
| 0 0 2 14 16 13 .01 | 236 523
gfz 241| 1 0 0 -1 -14 -11 .10 12 12 | 58 106 12 73
| 0 0 0 11 17 7 .02 | 202 309
grg 120| 2 0 -3 8 4 -17 -.07 10 9 | -1 108 8 143
| 0 0 2 8 15 10 .03 | 143 156
igr n/a| 0 0 -1 0 -4 -14 -.01 4 4 | 1726 -649 11 78
| 0 0 0 7 18 12 .01 | 2281 1264
jpl 80| 0 0 2 3 -8 -11 .17 10 10 | 564 68 8 77
| 2 2 1 8 12 17 .02 | 1948 896
mit 359| 0 0 0 -3 -1 3 -.02 7 6 | 1337 -631 29 1350
| 0 0 0 17 27 14 .02 | 2037 1172
ngs 208| 0 0 4 0 17 -24 -.06 10 9 | -647 138 698 1392
| 1 0 1 21 17 8 .02 | 103 192
sio 416| 0 0 1 -12 -13 31 -.04 8 7 | --- --- --- ---
| 0 0 2 25 52 21 .01 | --- ---
Table 1.2158.b GPS week : 2158 MJD: 59350.000-59356.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 5 5 4 5 4 6 |
2 | 4 5 3 3 3 4 3 |
3 | 3 2 2 3 3 3 3 |
4 | 4 4 4 4 4 4 4 |
5 | 3 3 3 2 3 3 3 |
6 | 4 4 4 5 6 6 5 |
7 | 3 3 3 3 3 3 3 |
8 | 3 3 2 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 3 3 2 3 3 3 |
12 | 4 3 3 3 3 4 3 |
13 | 3 3 3 3 3 3 3 |
14 | 4 3 4 4 4 4 4 |
15 | 3 3 3 3 3 3 3 |
16 | 4 4 4 3 4 4 4 |
17 | 3 3 3 3 3 3 3 |
18 | 7 7 6 6 6 7 12 |
19 | 3 3 3 4 3 3 3 |
20 | 3 5 3 3 3 3 3 |
21 | 3 4 3 3 3 3 4 |
22 | 3 3 3 3 3 3 3 |
23 | 3 3 3 3 3 3 4 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 3 4 3 |
26 | 3 3 3 3 3 3 4 |
27 | 3 3 3 3 3 3 3 |
28 | 3 3 3 3 0 5 3 |
29 | 3 3 3 3 3 3 3 |
30 | 4 3 4 3 3 4 3 |
31 | 4 4 3 4 4 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 2.2158.0 GPS week: 2158 Day: 0 MJD: 59350.000
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 754| 0 0 -1 15 12 -6 -.02 7 7 | -678 273 6 90
emr 80| 0 1 0 -11 7 19 .12 12 12 | 177023 137 17 127
esa 150| 0 0 0 3 17 -11 -.06 7 7 | -733 -235 8 88
gfz 243| 1 0 1 -2 -8 -22 .11 14 14 | 100 202 14 71
grg 122| 2 0 -6 -4 8 0 -.08 9 8 | 91 5 8 148
igr n/a| 0 0 0 -9 13 -29 -.00 4 4 | 2638 416 11 73
jpl 80| 2 -2 4 1 -15 3 .18 9 9 | 1342 468 8 83
mit 359| 0 0 0 14 -37 -5 .01 8 8 | 2437 378 32 1748
ngs 209| 0 0 4 -5 33 -9 -.07 9 9 | -500 -5 539 1328
sio 426| -2 0 0 -35 -23 29 -.03 9 8 | --- --- --- ---
Table 2.2158.1 GPS week: 2158 Day: 1 MJD: 59351.000
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 751| 0 0 -1 14 1 -25 -.03 6 6 | -649 147 6 88
emr 80| -2 2 0 18 20 29 .16 12 12 | 176792 1740 15 123
esa 150| 0 0 -1 17 12 0 -.07 7 7 | -1259 1333 7 83
gfz 245| 1 0 0 8 6 -12 .11 12 14 | -10 429 13 78
grg 123| 2 0 -1 17 27 -27 -.10 11 10 | -146 361 8 163
igr n/a| 0 0 -2 13 25 -20 .00 4 4 | 2776 1166 10 81
jpl 80| 0 -2 3 17 13 6 .17 9 9 | 1361 1352 7 62
mit 359| 0 0 -1 -20 -7 19 -.03 6 6 | 2241 1080 23 1280
ngs 204| 0 1 4 -2 35 -27 -.03 14 12 | -656 160 1031 1455
sio 423| -1 0 2 -45 -98 27 -.07 8 8 | --- --- --- ---
Table 2.2158.2 GPS week: 2158 Day: 2 MJD: 59352.000
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 745| 0 -1 -2 -1 13 -4 -.00 6 6 | -771 342 7 100
emr 80| -4 2 0 4 -2 20 .12 12 12 | 178342 490 14 112
esa 150| 0 0 0 13 -6 5 -.06 8 8 | -1062 738 8 83
gfz 242| 1 0 0 0 -7 -17 .09 13 15 | 344 -476 12 94
grg 119| 2 0 -4 2 13 -7 -.06 10 9 | 90 -72 8 140
igr n/a| 0 0 -1 6 -3 -7 -.01 4 4 | 3812 -40 12 78
jpl 80| 0 2 2 5 -7 1 .16 9 9 | 2587 519 8 78
mit 359| 0 0 -1 -10 23 -19 -.02 6 6 | 2924 -130 23 1153
ngs 207| 1 0 7 29 -12 -28 -.08 9 9 | -562 -32 679 1432
sio 418| -1 0 1 -5 -33 36 -.04 7 7 | --- --- --- ---
Table 2.2158.3 GPS week: 2158 Day: 3 MJD: 59353.000
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 743| 0 0 0 -16 7 -3 .00 6 6 | -637 145 6 93
emr 80| -3 4 2 1 9 13 .15 14 14 | 178898 -1351 15 112
esa 150| 0 0 0 11 9 18 -.07 8 8 | -1013 1100 7 85
gfz 241| 1 0 0 -24 -24 -4 .12 12 11 | 120 27 12 69
grg 120| 3 0 -4 16 13 -17 -.08 10 8 | 189 -11 9 141
igr n/a| 0 0 -1 0 -13 -9 -.01 4 4 | 3735 -1979 12 78
jpl 80| -1 1 3 -3 -12 -22 .17 9 9 | 2852 -1284 8 69
mit 359| 0 0 0 12 -5 16 -.01 7 6 | 2686 -1856 23 1527
ngs 208| 0 -1 3 27 18 -16 -.04 8 8 | -781 362 765 1414
sio 418| 0 0 0 -31 -20 -5 -.05 7 7 | --- --- --- ---
Table 2.2158.4 GPS week: 2158 Day: 4 MJD: 59354.000
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 739| -2 0 0 16 10 -22 -.01 7 7 | -565 -358 7 92
emr 80| -3 8 2 -16 -3 30 .14 14 14 | 177484 -861 14 113
esa 150| 0 -1 0 0 1 16 -.07 7 7 | -1025 772 7 75
gfz 242| 0 -1 0 -2 -20 0 .08 10 10 | 175 10 12 73
grg 121| 2 -1 -4 11 -11 -25 -.03 9 9 | 23 107 9 135
igr n/a| 0 0 -1 -4 -9 6 -.03 4 4 | 1698 -1752 11 83
jpl 80| 0 1 0 -10 -16 -41 .17 10 11 | -1297 -364 10 74
mit 359| 0 0 0 -2 3 1 -.02 7 6 | 1886 -1647 27 1152
ngs 211| 0 0 3 -13 23 -26 -.06 8 8 | -586 -117 643 1314
sio 406| 0 0 0 17 -19 60 -.04 8 8 | --- --- --- ---
Table 2.2158.5 GPS week: 2158 Day: 5 MJD: 59355.000
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 741| -1 0 -1 14 -15 -7 .02 8 8 | -671 234 7 96
emr 79| -2 1 4 -9 0 4 .12 14 14 | 176530 -1198 12 104
esa 150| 0 0 -4 -19 -27 7 -.05 8 8 | -1054 1044 7 83
gfz 238| 0 0 0 10 1 -14 .12 10 10 | -6 115 10 60
grg 119| 2 0 -4 12 0 -14 -.06 9 9 | -39 99 9 145
igr n/a| 0 0 -3 -5 -15 -15 -.02 5 5 | -120 -1967 11 78
jpl 80| 3 -1 1 6 4 -14 .13 10 10 | -2014 -713 9 93
mit 359| 0 0 -1 10 -30 -2 -.04 8 7 | -142 -1841 48 1357
ngs 210| -1 0 4 -11 25 -34 -.09 9 9 | -703 261 553 1459
sio 412| 0 0 3 -3 35 50 -.04 9 7 | --- --- --- ---
Table 2.2158.6 GPS week: 2158 Day: 6 MJD: 59356.000
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 739| 0 0 -2 26 -28 -20 -.01 7 7 | -615 137 6 82
emr 80| -3 -2 0 0 -10 12 .14 14 14 | 174964 614 13 134
esa 150| 0 0 -5 22 -19 28 -.06 8 8 | -1500 1188 6 70
gfz 242| 0 1 1 -3 -45 -4 .07 10 9 | -312 435 12 67
grg 122| 3 1 1 0 -18 -29 -.11 11 9 | -220 267 9 134
igr n/a| 0 0 -2 2 -26 -26 .00 4 4 | -2456 -387 11 78
jpl 80| -4 -4 0 9 -22 -15 .18 10 10 | -882 501 8 84
mit 359| 0 0 1 -29 40 16 -.01 6 6 | -2669 -403 29 1234
ngs 213| 0 0 2 -30 1 -26 -.08 10 9 | -747 342 679 1342
sio 415| 0 1 5 18 65 21 -.05 9 8 | --- --- --- ---
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 3.2158.0 GPS week: 2158 Day: 0 MJD: 59350.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 9 8 36 7 3 7 8 10 8 4 | 32 33 29 33 38 30 14 33 32 35 32
2E | 7 11 16 19 11 6 10 8 13 8 4 | 26 27 28 30 29 27 28 30 35 28 27
3 | 5 8 6 9 7 2 8 6 8 7 2 | 22 29 22 27 21 24 29 24 22 26 23
4 | 6 17 5 9 9 2 19 8 9 7 3 | 70 67 66 70 66 66 68 66 71 67 67
5 | 6 7 5 8 7 4 8 6 6 9 2 | 46 46 45 44 43 45 48 42 43 41 44
6E | 7 13 6 30 9 4 8 4 12 8 4 | 49 46 49 48 46 48 43 47 47 51 47
7 | 7 12 9 10 12 5 8 8 9 8 3 | 30 29 29 33 32 30 29 33 29 31 29
8 | 4 9 7 9 9 3 8 9 7 5 2 | 23 26 23 21 25 23 26 23 24 22 23
9 | 7 8 5 9 6 1 9 5 6 7 2 | 24 30 23 24 21 24 31 22 25 24 24
X10 | 6 --- 9 9 9 3 8 7 7 10 3 | 28 --- 30 30 24 29 30 29 28 28 27
12 | 8 18 5 11 8 4 9 8 9 9 3 | 31 32 31 30 28 30 31 30 27 33 29
13 | 7 10 5 9 8 4 10 5 7 9 2 | 24 28 24 27 24 25 30 24 26 26 24
14 | 8 12 9 15 10 5 9 11 13 10 3 | 66 64 63 68 72 65 62 62 67 68 65
15 | 4 10 5 10 6 5 7 8 7 9 2 | 34 39 35 33 31 34 36 33 29 32 33
16 | 8 20 6 9 12 6 13 7 12 7 3 | 28 29 30 30 25 29 28 26 30 27 26
17 | 5 8 6 10 6 4 7 8 7 13 2 | 21 24 18 23 22 21 26 23 23 21 20
X18E | 9 25 11 35 18 6 13 14 15 --- 6 | 28 35 33 37 30 29 32 32 33 --- 28
19 | 6 11 6 11 7 4 8 7 9 11 3 | 28 30 27 30 27 26 29 30 30 30 28
20 | 7 10 6 9 8 5 8 10 7 10 3 | 25 26 24 23 25 24 25 26 24 31 24
21E | 8 11 7 13 12 8 11 8 9 7 3 | 22 28 27 29 32 28 28 30 27 26 26
22 | 5 8 6 10 8 3 7 8 7 6 2 | 21 29 22 26 24 24 27 22 25 26 23
23 | 8 11 7 10 11 3 9 9 8 10 3 | 64 64 64 64 62 64 65 67 69 70 65
24 | 10 10 7 11 10 3 10 8 11 10 3 | 30 26 27 28 27 27 27 30 21 33 26
25 | 7 13 8 11 7 3 8 9 9 7 3 | 25 30 26 26 23 24 26 24 20 26 24
26 | 8 10 6 10 9 4 9 7 8 6 2 | 22 22 24 24 22 23 23 21 25 23 21
27 | 5 9 7 9 11 4 8 9 8 8 2 | 21 24 24 23 26 22 25 24 23 24 22
28 | 7 11 6 11 7 5 6 8 11 9 3 | 19 20 17 21 18 19 20 21 16 20 20
29 | 7 18 5 8 8 4 12 6 10 10 3 | 28 31 27 29 26 28 28 29 28 28 27
30 | 7 14 7 9 10 4 13 8 11 10 3 | 34 32 36 34 36 33 33 33 31 34 33
31 | 6 10 6 14 19 4 8 12 10 7 3 | 22 25 21 29 23 23 24 27 27 29 22
32 | 5 10 5 8 8 3 8 8 6 11 2 | 20 30 22 24 21 21 28 22 21 25 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 12 7 14 9 4 9 8 9 9 |T 31 33 31 32 31 31 32 31 31 32 30
WRMS | 7 12 7 14 8 4 9 8 9 8 |NE 31 33 30 32 30 30 32 31 30 32 30
MEDI | 7 10 6 10 9 4 8 8 9 8 |MD 28 29 27 29 26 27 28 29 27 28 26
Table 3.2158.1 GPS week: 2158 Day: 1 MJD: 59351.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 8 8 36 9 4 8 8 9 8 4 | 24 25 24 29 30 24 17 24 24 27 24
2E | 7 11 16 8 14 7 10 7 30 9 4 | 27 27 29 27 27 27 26 28 43 27 27
3 | 4 8 6 9 8 3 6 4 6 8 2 | 22 27 23 25 22 23 28 23 24 27 23
4 | 5 18 5 10 10 3 19 8 9 8 3 | 48 48 47 49 50 47 49 47 52 48 47
5 | 6 8 6 10 7 4 10 7 10 8 2 | 34 35 30 31 29 32 36 31 35 31 31
6E | 6 10 8 27 14 4 8 5 13 8 4 | 44 43 45 44 39 43 34 43 43 45 42
7 | 5 10 8 10 11 4 9 8 10 10 3 | 30 31 28 32 31 30 28 32 29 36 30
8 | 6 12 7 9 8 4 9 5 10 6 2 | 21 24 22 21 22 20 23 20 20 26 21
9 | 5 9 5 9 7 3 9 3 10 10 2 | 23 29 23 22 22 23 28 20 25 24 22
10 | 5 7 9 9 7 4 7 4 6 9 2 | 27 24 31 27 24 29 28 25 27 28 26
12 | 6 16 9 7 8 3 7 6 9 6 3 | 29 28 29 30 27 28 31 25 28 30 27
13 | 6 9 5 11 5 4 8 5 9 7 2 | 24 29 26 29 26 26 29 24 27 30 25
14 | 7 12 8 14 10 5 9 7 12 7 3 | 45 45 43 48 47 44 46 44 45 44 44
15 | 5 13 5 8 6 5 7 6 13 7 2 | 23 27 23 26 23 23 24 23 26 25 23
16 | 7 21 8 9 12 6 10 5 9 9 3 | 24 22 25 24 22 24 23 21 25 26 22
17 | 5 9 6 10 9 5 8 6 7 7 2 | 21 25 20 25 21 21 25 20 22 22 21
X18E | 8 23 10 39 18 5 14 11 19 --- 6 | 29 33 25 36 29 23 27 27 30 --- 25
19 | 5 11 5 12 10 4 8 5 15 8 3 | 29 29 28 32 27 27 29 28 35 32 28
20 | 8 11 5 9 10 4 9 9 45 9 5 | 25 23 22 23 23 22 25 24 48 26 22
21E | 8 9 9 8 22 4 7 7 7 8 3 | 25 26 23 24 29 24 24 25 26 28 24
22 | 5 7 7 10 9 3 7 5 9 8 2 | 20 26 21 23 24 22 26 21 26 25 22
23 | 7 11 6 8 10 4 9 8 12 9 3 | 48 48 49 49 49 49 48 50 55 54 49
24 | 8 11 7 10 9 3 9 6 18 9 3 | 31 29 29 27 30 28 31 30 32 31 29
25 | 6 12 8 9 9 3 9 6 9 8 3 | 27 31 27 27 26 25 30 24 25 32 26
26 | 7 14 7 8 10 3 9 5 10 5 3 | 22 23 24 24 22 22 25 20 22 25 21
27 | 6 8 8 8 9 4 9 7 8 9 2 | 20 22 19 19 22 19 21 20 22 24 19
28 | 6 13 7 7 9 5 8 6 19 6 3 | 19 21 18 19 19 20 22 19 22 19 20
29 | 6 20 7 9 8 4 10 4 15 8 3 | 23 23 18 23 20 19 22 19 28 26 21
30 | 7 13 6 9 10 4 12 8 9 6 3 | 35 33 34 34 35 34 33 33 31 35 33
31 | 6 11 6 11 20 4 7 8 9 10 3 | 23 25 20 29 25 24 26 26 27 30 24
32 | 6 8 6 9 6 3 10 8 8 12 3 | 21 29 22 26 21 24 30 23 26 28 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 12 7 12 11 4 9 6 14 8 |T 27 29 27 29 27 27 28 27 30 30 27
WRMS | 6 12 7 14 10 4 9 6 12 8 |NE 27 29 26 28 27 27 29 26 30 30 26
MEDI | 6 11 7 9 9 4 9 6 10 8 |MD 25 27 25 27 26 24 28 24 27 28 24
Table 3.2158.2 GPS week: 2158 Day: 2 MJD: 59352.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 10 9 41 11 3 6 7 9 8 4 | 23 26 21 32 29 22 15 23 23 25 23
2E | 6 9 13 10 8 6 9 8 9 9 3 | 22 22 22 22 18 21 23 21 21 22 20
3 | 5 9 7 8 8 2 7 3 6 5 2 | 16 22 17 19 16 16 23 16 17 17 16
4 | 4 18 6 9 8 3 20 8 9 8 3 | 51 54 49 52 52 51 57 48 53 53 51
5 | 6 9 6 11 7 5 7 6 7 7 2 | 35 37 32 34 33 34 37 35 33 32 33
6E | 7 12 8 31 9 5 8 5 11 4 3 | 38 35 35 32 34 34 38 36 38 36 35
7 | 6 11 9 11 11 5 8 8 11 7 3 | 21 22 19 26 24 21 21 27 23 23 21
8 | 4 11 6 9 7 3 8 5 6 4 2 | 17 22 19 16 18 16 22 17 18 17 17
9 | 5 10 6 11 5 5 10 4 8 9 2 | 20 29 19 22 20 21 29 18 21 22 20
10 | 5 9 8 9 6 4 7 5 9 8 2 | 20 20 19 16 17 19 22 18 20 19 18
12 | 5 16 8 9 8 3 9 5 7 5 2 | 21 24 18 23 21 21 23 20 21 21 20
13 | 6 9 6 10 8 3 7 6 10 7 2 | 16 24 16 21 17 16 23 19 22 18 18
14 | 9 12 10 16 12 5 10 8 14 10 3 | 48 48 46 48 53 46 45 46 47 48 46
15 | 5 11 8 9 6 5 7 7 8 8 2 | 26 29 27 27 24 25 26 26 25 25 25
16 | 6 21 9 12 12 6 10 5 10 8 3 | 21 22 22 23 19 19 20 18 20 19 18
17 | 5 15 9 8 7 3 7 6 12 7 3 | 20 26 18 24 22 21 25 22 26 23 21
X18E | 10 28 11 55 14 8 13 14 20 --- 6 | 26 33 28 41 23 23 27 30 36 --- 25
19 | 4 12 8 10 7 3 7 5 7 6 2 | 25 26 27 30 26 25 25 26 29 27 25
20 | 7 11 7 8 9 4 8 10 6 10 3 | 23 26 22 21 21 21 24 26 24 27 22
21E | 6 10 9 11 18 6 8 5 8 8 3 | 14 18 16 18 20 15 15 16 15 18 15
22 | 5 9 9 7 10 3 6 5 7 8 2 | 18 24 19 21 20 20 23 19 21 21 19
23 | 7 12 8 8 11 4 9 10 9 9 3 | 43 42 41 44 43 42 42 44 46 47 43
24 | 7 10 8 8 11 3 7 6 10 6 2 | 22 21 23 20 22 22 23 21 17 21 20
25 | 7 15 7 9 9 3 8 5 9 7 2 | 19 27 20 22 21 18 21 18 16 20 18
26 | 7 12 8 15 8 3 10 6 10 7 3 | 19 21 20 22 21 18 20 17 20 20 18
27 | 5 10 7 9 7 3 8 5 6 7 2 | 19 21 19 19 20 18 21 18 19 19 18
28 | 6 12 8 9 9 4 8 6 14 8 3 | 15 19 15 16 16 16 20 17 18 18 16
29 | 7 17 5 10 8 4 10 4 9 6 3 | 22 23 21 24 18 21 20 19 21 22 20
30 | 6 16 7 13 10 3 11 8 12 6 3 | 25 23 26 27 27 23 23 27 23 24 23
31 | 7 11 7 9 21 5 7 6 8 7 3 | 18 21 15 21 23 18 19 20 21 23 17
32 | 5 10 8 8 6 5 9 6 6 7 2 | 16 26 19 17 15 19 25 16 17 20 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 12 8 13 10 4 9 6 9 7 |T 23 26 23 25 24 23 25 24 24 24 23
WRMS | 6 12 8 15 9 4 9 6 9 7 |NE 23 26 23 25 24 23 26 23 24 24 23
MEDI | 6 11 8 9 8 4 8 6 9 7 |MD 21 24 20 22 21 21 23 20 21 22 20
Table 3.2158.3 GPS week: 2158 Day: 3 MJD: 59353.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 6 10 9 30 9 4 9 5 13 6 3 | 25 30 25 25 30 25 15 27 23 27 26
2E | 6 12 14 7 12 5 9 8 11 6 3 | 26 28 29 28 25 25 28 31 35 28 28
3 | 5 8 8 9 5 3 9 5 7 7 2 | 19 25 21 22 19 19 25 18 17 18 19
4 | 6 20 6 12 8 4 22 8 7 8 4 | 43 45 39 41 40 40 47 39 42 42 41
5 | 5 10 7 9 7 4 7 5 6 5 2 | 37 36 35 38 36 35 38 34 31 33 35
X6E | 5 12 6 29 10 5 --- 8 15 9 4 | 55 53 52 52 51 54 --- 53 53 54 53
7 | 6 11 9 14 11 4 9 8 7 8 3 | 24 25 22 30 28 24 22 28 25 27 25
8 | 9 10 7 9 6 3 7 5 4 6 2 | 24 26 22 21 22 22 25 20 19 20 21
9 | 7 12 7 11 4 5 12 5 5 9 2 | 18 29 18 19 19 19 28 18 19 18 19
10 | 6 11 6 8 6 4 7 5 5 6 2 | 18 22 19 19 18 18 21 16 17 18 17
12 | 7 16 8 9 8 5 8 6 9 7 3 | 21 23 20 23 20 21 23 21 20 22 20
13 | 7 11 7 10 8 4 9 5 8 6 2 | 16 24 17 22 15 17 23 17 18 16 17
14 | 8 14 12 14 12 6 11 8 11 10 3 | 55 56 55 60 64 56 54 55 56 59 56
15 | 6 11 7 11 5 5 8 8 6 7 2 | 29 32 29 31 27 30 29 29 27 27 28
16 | 5 19 8 8 11 7 10 6 10 8 3 | 21 22 19 22 19 20 20 20 20 20 19
17 | 6 12 5 12 8 4 8 5 8 5 2 | 21 29 18 26 19 20 24 19 21 18 20
X18E | 9 23 13 59 19 7 15 18 12 --- 6 | 26 31 25 41 27 24 29 33 24 --- 24
19 | 6 32 9 17 11 4 9 7 9 8 4 | 26 35 30 34 23 26 28 22 29 25 25
20 | 7 12 7 9 8 5 6 11 8 9 3 | 21 23 20 22 20 20 23 26 22 25 21
21E | 5 11 10 10 20 7 7 5 6 7 3 | 15 19 16 17 21 17 16 17 20 17 16
22 | 6 9 9 9 8 3 8 5 9 7 2 | 18 27 20 19 19 20 24 20 22 21 19
23 | 6 12 6 8 10 5 8 12 7 6 3 | 43 45 40 44 42 40 43 42 42 43 42
24 | 6 11 7 13 10 6 8 6 9 6 2 | 23 23 24 26 23 24 22 22 23 21 22
25 | 6 13 7 7 7 3 8 8 8 8 2 | 21 25 21 23 21 20 21 21 21 21 20
26 | 5 11 7 14 8 5 8 5 9 6 2 | 20 22 20 24 20 20 22 19 19 19 19
27 | 5 11 6 10 7 3 6 4 8 8 2 | 23 27 24 25 24 23 25 22 24 23 23
28 | 6 16 7 10 11 5 10 6 9 8 3 | 19 24 17 17 18 18 21 21 20 20 19
29 | 7 16 4 12 8 4 7 6 12 5 3 | 24 29 23 28 24 24 24 24 25 25 23
30 | 7 16 6 15 10 3 11 7 7 7 3 | 23 23 25 28 28 23 24 25 22 25 23
31 | 8 10 8 11 17 4 6 9 13 12 3 | 21 21 16 21 22 18 19 22 22 23 19
32 | 5 11 6 7 4 5 9 6 8 10 2 | 17 29 19 18 17 18 28 18 19 17 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 14 8 12 10 4 9 7 8 7 |T 25 29 25 27 25 25 26 25 25 25 25
WRMS | 6 14 8 11 8 4 9 6 8 7 |NE 24 28 24 27 24 24 27 24 24 24 24
MEDI | 6 12 7 10 8 4 8 6 8 7 |MD 23 27 22 25 22 22 24 22 22 22 21
Table 3.2158.4 GPS week: 2158 Day: 4 MJD: 59354.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 7 11 8 34 7 3 --- 6 14 9 5 | 37 40 39 45 38 38 --- 37 36 38 37
2E | 7 15 10 8 8 4 7 10 10 9 3 | 34 36 34 32 37 33 32 38 36 33 34
3 | 7 10 6 6 4 4 10 5 7 7 2 | 40 45 42 41 39 41 47 41 41 43 41
4 | 6 22 5 7 7 4 22 8 8 6 3 | 48 53 47 49 47 47 51 48 50 49 48
5 | 7 12 6 9 6 4 7 6 7 7 2 | 50 52 51 52 50 51 52 49 51 51 50
X6E | 9 17 10 23 12 6 --- 11 20 16 5 | 65 62 62 66 58 61 --- 61 56 64 60
7 | 7 13 8 10 11 5 7 8 8 6 3 | 51 51 51 53 51 50 50 53 49 51 50
8 | 9 10 7 10 6 4 9 4 6 6 2 | 36 42 39 37 38 38 39 39 36 38 37
9 | 8 11 5 9 6 4 10 5 7 6 2 | 35 42 36 36 33 36 42 35 37 35 35
10 | 6 11 7 9 8 3 6 6 5 7 2 | 42 37 43 44 40 43 43 41 40 46 41
12 | 7 20 7 7 6 5 9 5 6 11 3 | 39 40 38 40 36 41 38 39 39 40 38
13 | 8 10 6 13 10 4 8 5 6 9 3 | 41 45 42 48 42 42 41 41 43 44 42
14 | 8 15 10 17 11 5 14 8 13 7 4 | 58 62 59 64 65 60 58 61 62 63 61
15 | 7 13 8 11 7 4 12 9 6 9 3 | 41 42 42 44 38 42 40 41 40 41 40
16 | 5 21 8 9 11 5 11 7 12 7 3 | 35 37 37 37 36 37 36 36 39 38 36
17 | 8 15 5 7 10 3 11 5 8 7 2 | 34 41 35 34 33 34 38 36 34 35 34
X18E | 8 27 11 60 13 9 16 19 10 --- 6 | 40 43 38 50 34 38 38 41 40 --- 36
19 | 7 14 6 11 11 4 9 4 6 9 3 | 45 50 43 44 44 44 44 45 45 45 44
20 | 7 12 7 9 6 4 7 10 8 6 2 | 39 40 39 39 36 39 37 40 40 37 38
21E | 7 11 9 13 8 4 8 6 6 7 3 | 37 41 39 37 34 38 41 40 40 38 38
22 | 7 10 4 9 8 3 11 4 6 9 2 | 34 42 36 34 35 36 41 37 36 39 36
23 | 7 13 5 10 10 4 8 11 8 10 3 | 64 64 61 65 62 63 61 62 61 69 62
24 | 7 15 7 12 10 5 8 6 8 10 3 | 42 44 42 41 39 43 38 42 40 42 40
25 | 8 17 6 11 6 3 7 6 5 6 2 | 41 44 43 43 40 44 41 40 42 43 41
26 | 6 13 7 13 11 3 9 5 11 6 3 | 34 37 35 38 35 37 36 36 38 37 35
27 | 5 11 7 9 9 3 8 4 6 9 2 | 36 41 37 37 37 36 37 38 36 38 37
X28 | 2 --- --- --- --- 39 --- --- --- --- 0 | 18 --- --- --- --- 71 --- --- --- --- 19
29 | 7 19 3 10 7 5 9 6 7 6 2 | 38 43 38 44 39 40 40 40 42 40 39
30 | 7 17 6 10 9 3 11 5 9 7 3 | 51 55 54 52 53 52 51 52 48 54 51
31 | 10 12 8 8 16 4 8 7 10 10 3 | 37 38 35 39 38 37 38 39 41 43 37
32 | 7 11 6 11 7 4 11 5 5 6 2 | 37 44 39 39 38 40 43 38 39 41 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 7 10 9 4 10 7 8 8 |T 41 45 42 44 41 43 42 42 42 43 41
WRMS | 7 14 7 10 9 4 11 6 8 8 |NE 41 45 42 43 41 44 43 42 42 44 41
MEDI | 7 13 7 10 8 4 9 6 7 7 |MD 39 42 39 41 38 41 41 40 40 41 38
Table 3.2158.5 GPS week: 2158 Day: 5 MJD: 59355.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 9 19 8 8 10 5 --- 7 19 8 4 | 30 38 32 35 30 31 --- 29 29 28 29
2E | 10 11 12 10 7 6 8 10 11 11 3 | 41 46 45 41 43 43 43 43 45 42 42
3 | 7 9 7 8 6 3 9 5 4 9 2 | 18 22 19 18 17 17 24 17 17 19 18
4 | 7 21 6 10 7 5 22 8 6 7 4 | 50 52 51 52 50 50 53 51 51 50 50
5 | 7 11 8 10 7 4 8 5 5 6 2 | 26 26 25 27 23 25 29 23 23 24 24
6E | 15 17 11 20 13 7 17 12 20 15 5 | 69 67 62 64 57 63 44 64 67 66 63
7 | 6 13 6 8 10 4 8 9 10 6 3 | 19 17 17 21 22 18 17 20 21 22 19
8 | 7 8 8 9 7 3 7 5 7 5 2 | 22 25 24 24 22 21 23 22 22 22 22
9 | 9 11 7 8 6 5 10 7 5 10 3 | 23 32 24 26 21 24 31 23 20 19 23
10 | 6 12 6 8 7 4 6 7 8 6 2 | 18 22 19 19 17 17 22 17 19 17 17
12 | 7 18 8 12 9 5 8 9 8 10 3 | 27 27 24 27 24 25 26 27 27 25 24
13 | 8 12 9 11 7 3 7 6 8 7 3 | 14 21 15 25 13 15 21 15 16 17 16
14 | 10 16 11 14 12 6 14 10 12 6 4 | 38 40 38 39 46 39 38 40 39 38 38
15 | 7 12 9 7 7 4 12 8 8 9 3 | 24 25 28 28 23 26 26 25 26 25 25
16 | 7 22 9 10 10 7 9 7 10 8 3 | 19 16 21 20 19 20 20 18 22 18 18
17 | 8 8 6 8 12 5 9 12 7 10 3 | 40 42 37 41 41 39 42 44 43 39 40
X18E | 20 25 15 58 14 6 21 17 10 --- 7 | 25 32 21 45 19 19 26 26 21 --- 18
19 | 8 15 6 9 10 5 9 5 8 10 3 | 20 24 18 17 20 18 23 19 23 17 18
20 | 7 14 8 10 8 5 8 8 9 8 3 | 25 29 25 27 28 25 27 27 27 28 26
21E | 8 13 11 11 7 6 9 8 9 9 3 | 22 27 26 26 26 26 27 26 26 26 24
22 | 8 11 6 7 7 3 9 5 9 10 2 | 25 32 26 27 26 26 30 26 28 29 26
23 | 8 13 7 9 10 5 8 13 9 8 3 | 43 43 41 44 41 40 42 41 44 43 41
24 | 7 11 7 14 13 5 6 7 9 5 3 | 24 24 24 24 22 23 23 23 19 20 21
25 | 8 24 7 9 8 5 7 6 8 14 3 | 22 33 20 19 19 18 21 19 19 24 19
26 | 7 11 8 12 11 4 10 7 11 6 3 | 20 21 22 23 22 20 24 19 21 18 20
27 | 6 9 8 8 10 4 8 4 8 6 2 | 20 26 24 23 22 20 24 20 20 21 21
X28 | 7 12 8 9 11 6 --- 11 --- --- 4 | 18 19 15 18 15 19 --- 19 --- --- 19
29 | 7 17 5 9 7 5 10 6 7 7 3 | 21 21 15 22 17 18 19 16 19 19 17
30 | 6 23 7 9 10 3 10 7 9 6 3 | 20 25 22 21 23 20 22 19 20 20 19
31 | 11 9 7 7 17 4 9 6 11 11 3 | 23 18 14 21 23 18 19 18 22 19 18
32 | 6 11 6 12 6 4 12 6 8 5 2 | 16 25 16 12 14 14 27 15 19 15 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 8 10 9 5 10 8 9 9 |T 26 29 26 28 25 25 28 26 27 26 25
WRMS | 8 14 8 10 9 5 10 7 9 7 |NE 24 27 24 25 24 23 26 23 25 24 23
MEDI | 7 12 8 9 9 5 9 7 8 8 |MD 23 26 24 25 22 21 26 23 22 22 21
Table 3.2158.6 GPS week: 2158 Day: 6 MJD: 59356.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 13 20 11 13 24 11 --- 5 18 16 5 | 36 36 32 47 48 34 --- 35 33 38 34
2E | 7 10 10 9 10 4 9 8 10 9 3 | 41 42 42 42 40 40 40 41 39 39 40
3 | 7 8 6 6 6 3 8 5 7 9 2 | 20 24 21 20 19 20 26 19 20 23 19
4 | 4 20 6 8 9 5 22 7 7 7 3 | 64 67 64 66 65 64 67 64 67 64 64
5 | 8 10 8 9 9 5 8 5 8 10 3 | 44 43 43 42 40 43 47 39 39 38 41
6E | 12 14 8 15 26 5 15 7 14 10 4 | 60 56 56 56 58 58 38 58 56 60 56
7 | 5 12 6 11 10 4 10 6 9 9 3 | 24 24 22 30 27 24 26 27 24 25 24
8 | 7 10 7 6 7 2 9 5 7 6 2 | 31 33 30 30 29 29 32 29 26 29 29
9 | 7 11 5 8 7 3 13 6 7 7 2 | 28 40 31 31 28 31 42 29 31 28 30
10 | 6 13 8 7 7 4 5 5 13 7 2 | 31 31 30 29 26 29 31 29 29 30 29
12 | 6 19 7 10 10 3 9 6 7 9 3 | 29 26 29 31 27 29 28 29 30 29 28
13 | 7 6 8 10 9 3 6 4 9 7 2 | 20 26 22 28 19 21 25 22 23 24 22
14 | 9 16 11 15 11 6 15 8 14 11 4 | 63 65 63 67 71 65 64 68 69 65 65
15 | 5 15 8 8 6 4 12 7 9 9 3 | 37 41 41 40 35 39 40 36 34 34 37
16 | 7 24 10 9 13 6 10 6 8 8 3 | 25 29 28 25 25 25 26 25 27 25 25
17 | 7 9 5 8 8 4 11 5 9 6 2 | 39 43 36 38 40 38 43 40 43 40 39
X18E | 33 29 34 22 14 8 40 26 45 --- 12 | 57 36 31 44 37 38 35 50 74 --- 40
19 | 6 12 6 10 8 3 10 6 11 7 3 | 32 36 32 34 31 31 34 31 34 32 32
20 | 6 14 7 8 10 6 8 8 13 10 3 | 30 28 28 33 33 28 30 29 35 31 29
21E | 8 14 11 9 10 5 8 6 12 11 3 | 25 30 25 24 30 25 25 28 25 28 25
22 | 8 11 6 8 10 3 8 6 6 12 3 | 28 33 26 27 31 27 32 27 28 34 28
23 | 7 15 7 7 11 4 10 11 14 8 3 | 71 68 68 71 70 70 70 71 74 73 70
24 | 5 11 7 12 9 3 8 5 7 8 2 | 26 26 30 30 26 27 25 25 24 27 26
25 | 6 17 7 13 9 3 8 6 8 10 3 | 27 33 27 28 26 26 27 25 24 27 26
26 | 8 17 9 12 11 4 9 6 11 6 3 | 24 29 28 27 25 26 27 24 27 23 24
27 | 4 9 8 9 9 4 7 5 7 6 2 | 30 30 30 31 29 29 33 30 27 30 29
X28 | 7 11 7 8 11 5 9 7 7 --- 3 | 14 18 16 17 16 15 18 19 13 --- 15
29 | 7 19 4 8 9 5 9 7 10 8 3 | 34 37 32 37 32 32 34 32 35 33 33
30 | 8 16 6 12 10 3 11 5 7 7 3 | 26 26 27 29 29 25 27 26 24 25 25
31 | 11 12 7 15 19 4 8 6 8 10 3 | 23 22 21 25 25 22 24 23 21 22 21
32 | 8 13 5 7 5 4 12 5 10 10 3 | 25 36 28 29 25 27 36 25 28 26 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 10 11 4 10 6 10 9 |T 34 35 33 35 34 33 35 34 34 34 33
WRMS | 7 14 8 9 9 4 10 6 9 8 |NE 32 35 32 34 32 32 35 32 32 33 32
MEDI | 7 13 7 9 10 4 9 6 9 9 |MD 30 33 30 31 29 29 32 29 29 30 29
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 4.2158 GPS week: 2158 MJD: 59350.0-59356.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 |U 11 10 22 |U 9 12 30 |U 10 16 32 |
emr | emr 2948 |U 16 15 37 |U 16 21 54 |U 14 19 52 |
esa | esa 2962 | 11 13 32 |U 9 16 30 | 12 17 28 |
gfz | gfz 2961 |U 11 10 24 |U 9 14 37 |U 10 14 29 |
grg | grg 2961 |U 11 11 27 |U 8 14 34 | 9 15 27 |
igr | igr 2948 | 10 11 22 | 8 13 28 | 9 15 25 |
igs | igs 2955 | 10 10 22 | 8 13 31 | 9 14 27 |
jpl | jpl 2880 |U 11 15 30 |U 10 18 39 | 11 18 37 |
mit | mit 2962 |U 10 10 22 |U 8 12 36 |U 11 15 31 |
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 5.2158.0 GPS week: 2158 Day: 0 MJD: 59350.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 12 11 21 | 7 11 26 | 11 13 35 |
emr | emr 2880 | 13 16 31 | 16 31 50 | 15 15 63 |
esa | esa 2976 | 14 14 37 | 11 25 36 | 11 17 28 |
gfz | gfz 2976 | 11 11 21 | 10 21 33 | 10 11 28 |
grg | grg 2976 | 11 12 22 | 10 25 29 | 11 15 32 |
igr | igr 2976 | 11 13 23 | 9 24 31 | 10 13 30 |
igs | igs 2976 | 11 12 22 | 10 24 33 | 10 13 32 |
jpl | jpl 2976 | 12 15 32 | 11 27 42 | 12 19 42 |
mit | mit 2976 | 12 12 23 | 10 22 36 | 10 12 33 |
Table 5.2158.1 GPS week: 2158 Day: 1 MJD: 59351.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 12 10 19 | 10 11 28 | 13 24 37 |
emr | emr 2976 | 15 14 40 | 15 19 36 | 14 27 46 |
esa | esa 2976 | 11 13 34 | 10 15 29 | 12 22 29 |
gfz | gfz 2976 | 11 10 21 | 9 11 37 | 12 19 30 |
grg | grg 2976 | 10 9 22 | 8 14 31 | 11 22 27 |
igr | igr 2976 | 10 11 23 | 9 12 27 | 11 22 31 |
igs | igs 2976 | 11 11 23 | 9 12 28 | 11 22 31 |
jpl | jpl 2976 | 11 13 30 | 11 17 35 | 11 24 40 |
mit | mit 2976 | 11 10 23 | 9 10 29 | 12 22 38 |
Table 5.2158.2 GPS week: 2158 Day: 2 MJD: 59352.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 8 20 | 8 10 30 | 11 12 27 |
emr | emr 2976 | 17 14 34 | 15 20 52 | 11 12 65 |
esa | esa 2976 | 12 12 34 | 7 15 26 | 12 15 26 |
gfz | gfz 2976 | 10 8 20 | 8 10 36 | 9 10 24 |
grg | grg 2976 | 10 9 21 | 7 12 33 | 10 13 22 |
igr | igr 2976 | 9 9 21 | 7 11 26 | 9 12 23 |
igs | igs 2976 | 9 9 21 | 8 10 30 | 10 11 25 |
jpl | jpl 2976 | 10 12 28 | 9 16 32 | 11 16 44 |
mit | mit 2976 | 9 9 21 | 7 10 33 | 11 12 28 |
Table 5.2158.3 GPS week: 2158 Day: 3 MJD: 59353.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 9 20 | 8 12 33 | 10 15 31 |
emr | emr 2976 | 15 13 38 | 17 18 61 | 15 19 55 |
esa | esa 2976 | 9 10 30 | 9 12 31 | 11 15 32 |
gfz | gfz 2976 | 12 11 33 | 8 12 40 | 9 13 29 |
grg | grg 2972 | 12 13 40 | 9 13 38 | 8 14 24 |
igr | igr 2976 | 8 9 20 | 8 10 32 | 9 14 26 |
igs | igs 2976 | 9 9 21 | 8 10 34 | 9 14 28 |
jpl | jpl 2880 | 9 16 28 | 9 14 45 | 13 18 35 |
mit | mit 2976 | 9 7 21 | 9 10 39 | 10 13 26 |
Table 5.2158.4 GPS week: 2158 Day: 4 MJD: 59354.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 10 9 22 | 11 13 34 | 9 16 34 |
emr | emr 2880 | 19 18 39 | 20 19 61 | 14 21 49 |
esa | esa 2880 | 10 14 30 | 11 16 32 | 15 19 30 |
gfz | gfz 2880 | 11 10 22 | 11 13 43 | 14 22 43 |
grg | grg 2880 | 9 10 23 | 10 10 41 | 10 14 31 |
igr | igr 2880 | 9 11 21 | 10 11 32 | 8 15 26 |
igs | igs 2880 | 8 11 23 | 10 11 36 | 9 15 30 |
jpl | jpl 2688 | 10 18 27 | 11 17 42 | 11 19 36 |
mit | mit 2880 | 10 10 23 | 10 10 39 | 12 16 38 |
Table 5.2158.5 GPS week: 2158 Day: 5 MJD: 59355.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 15 14 28 | 9 13 32 | 10 19 34 |
emr | emr 2976 | 23 17 43 | 14 19 62 | 15 29 45 |
esa | esa 2976 | 14 19 33 | 8 14 25 | 11 18 25 |
gfz | gfz 2976 | 14 13 24 | 8 11 37 | 9 16 29 |
grg | grg 2976 | 14 11 26 | 7 13 32 | 9 17 27 |
igr | igr 2879 | 13 15 24 | 7 11 25 | 9 16 19 |
igs | igs 2926 | 14 13 25 | 7 11 30 | 9 16 21 |
jpl | jpl 2784 | 14 22 32 | 9 17 38 | 13 19 34 |
mit | mit 2976 | 14 11 24 | 7 10 36 | 9 13 25 |
Table 5.2158.6 GPS week: 2158 Day: 6 MJD: 59356.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 10 8 21 | 7 12 30 | 9 15 28 |
emr | emr 2976 | 12 14 35 | 15 23 54 | 12 11 45 |
esa | esa 2976 | 10 12 29 | 7 16 28 | 11 14 29 |
gfz | gfz 2973 | 12 12 29 | 7 16 30 | 8 8 22 |
grg | grg 2972 | 12 16 37 | 7 12 35 | 8 11 24 |
igr | igr 2975 | 9 10 20 | 7 11 27 | 9 12 22 |
igs | igs 2976 | 9 10 20 | 7 12 30 | 8 11 22 |
jpl | jpl 2880 | 10 13 30 | 9 19 37 | 10 12 29 |
mit | mit 2976 | 8 9 19 | 8 15 39 | 12 16 28 |
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 6.2158 GPS week: 2158 MJD: 59350.500-59356.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -17 -10 68 -87 0 | 7 28
| 11 15 36 55 10 | 4
emr uuxxu | 4 -44 324 341 8 | 18 35
| 38 35 67 152 15 | 3
esa uuuuu | 7 3 60 80 1 | 14 30
| 13 17 64 37 3 | 3
gfz uuuuu | 14 17 -25 19 -1 | 20 33
| 13 16 173 69 3 | 2
grg uuuuu | -5 4 14 -60 2 | 4 26
| 14 7 40 34 6 | 3
igr xxxxx | 3 3 26 13 -1 | -2 26
| 9 6 40 49 3 | 3
irf xxxxx | 11 0 -36 9 -2 | -1 28
| 9 11 28 16 4 | 3
jpl uuuuu | 17 -17 124 125 -1 | 38 45
| 24 26 65 60 8 | 2
mit uuuuu | 3 10 -156 -35 -5 | 27 39
| 12 15 12 27 5 | 3
ngs uuuuu | -15 25 -53 -4 -5 | 14 30
| 19 29 184 108 5 | 4
sio xxxxx | 20 -119 -82 -20 -14 | 29 39
| 35 26 114 106 4 | 6
Table 7.2158.0 GPS week: 2158 Day: 0 MJD: 59350.500
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 | -18 -26 3 -95 -11 | 12 27
emr uuxxu | -23 -17 313 190 18 | 15 35
esa uuuuu | 2 4 12 73 2 | 16 29
gfz uuuuu | 14 41 -252 30 3 | 22 34
grg uuuuu | 5 7 54 -66 -5 | 7 25
igr xxxxx | 1 6 70 14 2 | 1 24
irf xxxxx | 20 2 -19 2 0 | 1 27
jpl uuuuu | 39 -1 123 138 7 | 38 45
mit uuuuu | 21 18 -160 -13 1 | 29 39
ngs uuuuu | -38 -5 162 -45 0 | 16 30
sio xxxxx | 39 -100 -244 -86 -7 | 35 42
Table 7.2158.1 GPS week: 2158 Day: 1 MJD: 59351.500
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 -11 90 -97 -9 | 11 27
emr uuxxu | -15 -22 182 254 23 | 16 36
esa uuuuu | 7 -2 107 10 -1 | 16 29
gfz uuuuu | 2 20 -129 144 -1 | 22 34
grg uuuuu | 4 11 -28 -44 -4 | 7 24
igr xxxxx | -11 0 -26 -44 -4 | 1 24
irf xxxxx | 1 -15 -36 -10 -3 | 1 27
jpl uuuuu | 24 0 50 117 9 | 38 46
mit uuuuu | 3 -12 -144 -57 -1 | 30 40
ngs uuuuu | -43 51 25 84 0 | 17 30
sio xxxxx | 65 -149 -208 -73 -8 | 35 41
Table 7.2158.2 GPS week: 2158 Day: 2 MJD: 59352.500
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 | -31 4 77 -11 -4 | 7 28
emr uuxxu | 16 -34 336 241 14 | 15 36
esa uuuuu | 9 -11 93 98 0 | 13 30
gfz uuuuu | 14 -5 117 57 -3 | 19 33
grg uuuuu | -28 15 30 -129 3 | 3 26
igr xxxxx | -2 2 9 -15 -5 | -2 26
irf xxxxx | 18 -13 -18 -6 1 | -1 29
jpl uuuuu | 36 -9 125 181 -10 | 38 46
mit uuuuu | 14 -2 -138 -67 1 | 27 39
ngs uuuuu | -17 34 -265 -114 -3 | 14 30
sio xxxxx | 38 -149 -127 -127 -16 | 31 39
Table 7.2158.3 GPS week: 2158 Day: 3 MJD: 59353.500
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 | -18 8 43 -49 -2 | 8 27
emr uuxxu | 18 -54 385 385 20 | 19 36
esa uuuuu | -4 -12 113 131 -2 | 15 29
gfz uuuuu | 24 2 235 -73 -2 | 21 33
grg uuuuu | -20 -3 17 -45 7 | 4 25
igr xxxxx | 12 -6 72 -37 -2 | -1 25
irf xxxxx | 14 4 -33 16 -8 | 2 27
jpl uuuuu | 30 -13 214 190 0 | 40 46
mit uuuuu | 2 12 -170 -55 -10 | 30 39
ngs uuuuu | -2 23 -313 -96 -12 | 16 30
sio xxxxx | -14 -77 -9 -85 -17 | 31 39
Table 7.2158.4 GPS week: 2158 Day: 4 MJD: 59354.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -27 -9 59 -93 3 | 4 30
emr uuxxu | 61 -3 354 619 4 | 21 35
esa uuuuu | -11 -7 127 94 -1 | 12 31
gfz uuuuu | 26 10 -4 -24 -2 | 19 34
grg uuuuu | 5 -1 13 -42 11 | 2 27
igr xxxxx | 13 6 55 54 -2 | -4 29
irf xxxxx | 18 7 -56 34 -5 | -1 31
jpl uuuuu | 20 0 43 116 -10 | 38 46
mit uuuuu | -9 14 -163 -6 -11 | 27 40
ngs uuuuu | -1 -1 -63 -49 -7 | 12 33
sio xxxxx | 37 -113 -41 -21 -19 | 27 41
Table 7.2158.5 GPS week: 2158 Day: 5 MJD: 59355.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -3 112 -74 14 | 7 32
emr uuxxu | 26 -82 360 447 -16 | 25 38
esa uuuuu | 29 35 -29 77 4 | 14 33
gfz uuuuu | -7 27 -181 -2 1 | 22 36
grg uuuuu | 7 1 -49 -67 6 | 5 29
igr xxxxx | 12 13 -16 90 4 | -1 29
irf xxxxx | 9 16 -87 20 -4 | 0 32
jpl uuuuu | -28 -72 198 126 -4 | 39 47
mit uuuuu | -13 36 -166 -46 -8 | 28 41
ngs uuuuu | -9 3 145 0 -10 | 14 34
sio xxxxx | 8 -115 -14 159 -15 | 26 40
Table 7.2158.6 GPS week: 2158 Day: 6 MJD: 59356.500
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 -34 92 -189 11 | 1 23
emr uuxxu | -57 -96 341 250 -5 | 17 28
esa uuuuu | 18 13 0 74 6 | 9 25
gfz uuuuu | 29 26 40 1 -5 | 17 29
grg uuuuu | -6 0 60 -26 0 | 0 22
igr xxxxx | -2 -2 19 29 1 | -6 25
irf xxxxx | -4 -1 -5 3 4 | -7 25
jpl uuuuu | 0 -24 114 8 -2 | 34 39
mit uuuuu | 6 7 -150 -2 -5 | 21 31
ngs uuuuu | 5 71 -61 189 -6 | 6 24
sio xxxxx | -33 -127 68 90 -13 | 18 30
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