[IGSREPORT-25549] Wk 1967 IGS Final Orbits
acc
acc at igs.org
Sun Oct 8 17:18:26 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1967 (Sep 17, 2017 - Sep 23, 2017)
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:
igs1967[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1967[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1967[0-6].cls IGS GPS clock combination summary report.
igs19677.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19677.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 | GRAS REUN TIXI GRAS REUN TIXI
0 | EMR | 25 25
0 | ESA | BAKE CHUR BAKE CHUR HARB MAL2
0 | GFZ | BJNM SYOG TIDB BJNM SYOG TIDB
0 | GRG | 3 13 25 3 13 25 DAEJ FAA1 GLSV MAW1 NKLG SYOG TRO1
0 | GRG | DAEJ FAA1 GLSV MAW1 NKLG SYOG TRO1
0 | JPL | TIDB
1 | COD | DRAO KOUR SYOG DRAO KOUR
1 | EMR | BJNM FAIR BJNM CHUR FAIR
1 | ESA | FAA1 CHTI
1 | GFZ | DRAO DRAO
1 | GRG | BAKE DAEJ GLSV LHAZ MAC1 SYOG BAKE DAEJ DGAR GLSV
1 | GRG | LHAZ
2 | COD | AREQ FAA1 LHAZ TIXI FAA1 LHAZ MAW1 TIXI
2 | EMR | AREQ MAS1
2 | ESA | OHI3 OHI3
2 | GFZ | 13 13 DGAR SYOG DGAR NICO SYOG
2 | GRG | DAEJ DGAR GLSV SYOG DAEJ DGAR GLSV SYOG
2 | MIT | TIDB TIDB
3 | COD | KRGG KRGG
3 | EMR | HOB2 ALBH HOB2 MAS1 TWTF
3 | ESA | CHUR FAA1 LHAZ CHTI CHUR FAA1
3 | GFZ | BJNM LHAZ NIST SYOG BJNM LHAZ NIST NTUS SOFI SYOG
3 | GRG | FAA1 GLSV MAL2 SYOG ADIS FAA1 GLSV MAL2 SYOG
4 | COD | TIXI CHTI TIXI
4 | EMR | KERG MAS1 TWTF YELL
4 | ESA | CHTI CHTI
4 | GFZ | 13 13 REUN AUCK REUN
4 | GRG | 13 13 DGAR GLSV KIT3 LHAZ SYOG DGAR GLSV KIT3 LHAZ
4 | GRG | LMMF SYOG
4 | MIT | DGAR DGAR
5 | COD | BJNM CHTI TIXI BJNM CHTI TIXI
5 | EMR | DAEJ MAS1 MDO1 SFER STJO SUWN TWTF
5 | ESA | DGAR DGAR
5 | GFZ | 13 13 AUCK AUCK
5 | GRG | 13 13 CHTI DAEJ PARC SYOG CHTI DAEJ PARC SYOG
5 | MIT | REUN
6 | COD | HARB SOFI TIXI HARB SOFI TIXI
6 | EMR | MAS1 SUWN
6 | GFZ | 13 BJNM BJNM
6 | GRG | DAEJ GLSV MAW1 SEYG DAEJ GLSV MAW1 SEYG
6 | MIT | BOR1 BOR1
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. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G06 | | | | | | | 4 |
PRN G07 | | | | | 4 | 4 | 4 |
PRN G15 | | | | 4 | 4 | 4 | 4 |
PRN G24 | | | | 4 | 4 | 4 | 4 |
PRN G30 | | | | | | 4 | 4 |
PRN G32 | | | | | | 4 | 4 |
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.
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 | .4 -.1 .9 -4 -3 0 -.46
EMR | 0 | 7.9 -3.8 .3 -6 14 -26 -.13
ESA | 0 | -.1 .1 -.6 -3 -27 9 -.55
GFZ | 0 | .4 .4 1.5 -5 -12 -11 -.52
GRG | 0 | 3.3 2.8 27.0 22 18 3 -.21
JPL | 0 | 10.3 -2.7 1.2 -4 -65 29 .08
MIT | 0 | 1.8 -1.6 3.8 -13 31 -9 -.21
NGS | 0 | 1.4 -4.8 3.3 0 -22 -2 -.20
SIO | 0 | .7 5.4 -7.3 11 -28 0 -.18
COD | 1 | .5 -.1 1.0 3 -2 -6 -.57
EMR | 1 | 4.2 -2.2 -3.6 -12 4 -10 -.15
ESA | 1 | -.1 -.4 .1 7 -7 11 -.49
GFZ | 1 | .8 -.0 1.2 -16 -25 -8 -.58
GRG | 1 | 5.6 9.4 9.7 34 -17 18 -.30
JPL | 1 | -1.2 -2.9 -.7 -25 -94 75 .08
MIT | 1 | 2.3 1.4 2.2 -1 26 -15 -.21
NGS | 1 | -.5 -4.6 .2 12 -31 8 -.22
SIO | 1 | 1.7 5.3 .5 10 -20 5 -.18
COD | 2 | .1 .4 1.2 4 5 -5 -.56
EMR | 2 | 8.3 1.4 3.8 -10 -3 -8 -.32
ESA | 2 | .4 -.3 -.2 0 -14 -2 -.53
GFZ | 2 | 1.0 .1 1.0 -11 -26 -10 -.52
GRG | 2 | 3.9 .9 7.5 30 -31 8 -.26
JPL | 2 | 5.4 -7.0 3.7 -12 -65 53 .07
MIT | 2 | .7 -1.2 8.1 -5 39 -26 -.16
NGS | 2 | -.6 -9.9 -3.6 16 -7 -23 -.29
SIO | 2 | 1.3 5.2 5.2 8 -27 -6 -.28
COD | 3 | -.1 .1 1.0 11 14 -2 -.46
EMR | 3 | 7.9 1.0 4.0 -10 5 -5 -.23
ESA | 3 | .5 -.0 .2 5 -1 0 -.46
GFZ | 3 | .5 .4 .6 -7 -13 -12 -.44
GRG | 3 | 7.6 1.0 10.0 7 -5 53 -.17
JPL | 3 | 5.6 -7.7 .0 -19 -78 41 .13
MIT | 3 | 1.5 -1.0 9.3 9 37 -10 -.18
NGS | 3 | 1.6 -4.1 -2.9 30 -7 21 -.27
SIO | 3 | .1 5.2 12.0 7 -35 -11 -.23
COD | 4 | .2 .3 1.1 14 10 -20 -.48
EMR | 4 | 2.3 -6.4 10.4 10 25 2 -.25
ESA | 4 | 1.0 -.4 .5 3 4 0 -.51
GFZ | 4 | .6 .2 1.0 -8 -20 -4 -.44
GRG | 4 | 5.5 .2 37.8 57 25 11 -.18
JPL | 4 | .8 -9.7 6.1 10 -28 28 .26
MIT | 4 | -3.9 .8 9.4 0 42 -13 -.16
NGS | 4 | -2.2 -8.4 .8 28 -19 1 -.26
SIO | 4 | -3.8 5.4 9.6 15 3 -19 -.33
COD | 5 | .1 .3 1.1 8 12 -13 -.48
EMR | 5 | 9.0 -4.8 12.5 37 8 -16 -.45
ESA | 5 | .6 -.2 .6 -5 17 3 -.54
GFZ | 5 | -.0 .2 .9 -4 -11 -3 -.49
GRG | 5 | 7.5 6.0 38.3 36 6 15 -.44
JPL | 5 | 3.4 -1.7 -.7 -1 -26 51 .03
MIT | 5 | -1.5 1.4 11.9 -4 28 -7 -.37
NGS | 5 | .5 -8.5 -.5 30 -12 -38 -.37
SIO | 5 | .1 5.2 11.7 27 -21 -4 -.52
COD | 6 | .1 .1 1.7 15 21 -4 -.57
EMR | 6 | 13.1 -3.2 6.3 11 9 1 -.39
ESA | 6 | .1 .3 .0 4 7 -3 -.56
GFZ | 6 | .5 .4 1.2 -10 -14 -12 -.47
GRG | 6 | 2.1 4.2 34.1 48 -12 37 -.34
JPL | 6 | 3.6 -5.2 .8 15 -57 18 .09
MIT | 6 | -2.3 3.6 11.3 -1 24 -11 -.36
NGS | 6 | 6.7 -1.3 7.1 11 -4 -28 -.15
SIO | 6 | 2.1 7.3 5.8 31 -16 6 -.36
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:
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 1.1967.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1967.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 2.1967.[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 3.1967.[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 5.1967.0-6). 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 1967 summary. (Sep 17, 2017 - Sep 23, 2017)
Table 1.1967.a GPS week: 1967 MJD: 58013.000-58019.000
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 269| 1 0 -2 -2 3 5 .01 10 10 | -725 -2 11 105
| 0 0 1 19 15 10 .02 | 89 83
emr 79| 1 0 3 0 -1 2 .19 16 15 | 2354 -380 16 136
| 1 2 1 17 11 15 .03 | 1190 1145
esa 150| 0 0 0 1 16 -3 -.03 9 9 | -2265 1202 7 162
| 0 0 0 11 17 8 .02 | 574 1241
gfz 193| -1 0 -3 0 -11 -8 .09 11 10 | -266 121 10 128
| 0 0 0 7 17 7 .02 | 256 522
grg 107| 1 0 12 -17 1 23 -.42 16 15 | -25 84 12 196
| 0 1 7 6 21 25 .04 | 162 263
igr n/a| 0 0 -1 -5 -6 2 .00 4 4 | -3839 -109 12 85
| 0 0 2 12 16 11 .02 | 692 1062
jpl 80| 0 0 1 7 -10 18 .23 12 12 | 1927 -255 42 221
| 1 1 1 17 38 46 .02 | 898 1072
mit 349| 0 -1 4 -16 -11 6 .00 12 11 | -577 -4 47 329
| 0 0 0 23 48 12 .04 | 295 311
ngs 218| 0 0 -2 21 -7 -11 .04 9 8 | -727 0 880 2044
| 1 0 1 9 24 13 .02 | 65 189
sio 340| 0 0 -1 -14 -6 1 .01 12 12 | --- --- --- ---
| 0 0 2 26 49 19 .02 | --- ---
Table 1.1967.b GPS week : 1967 MJD: 58013.000-58019.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 3 4 4 4 4 |
2 | 5 6 6 6 5 6 6 |
3 | 5 4 4 4 4 4 4 |
4 | 0 0 0 0 0 0 0 |
5 | 5 4 5 4 4 5 5 |
6 | 3 4 4 4 4 4 4 |
7 | 4 4 5 4 4 4 4 |
8 | 3 3 4 3 3 4 4 |
9 | 3 3 3 3 4 3 4 |
10 | 4 4 4 3 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 6 5 5 6 5 |
13 | 4 4 4 4 4 5 5 |
14 | 5 4 4 5 4 4 4 |
15 | 4 4 4 5 4 4 4 |
16 | 5 5 6 5 5 5 5 |
17 | 5 5 5 5 4 4 4 |
18 | 5 5 5 5 5 5 6 |
19 | 5 5 5 5 5 5 5 |
20 | 5 4 4 4 4 5 4 |
21 | 5 5 5 6 5 5 5 |
22 | 6 5 5 4 5 5 4 |
23 | 6 6 6 6 5 5 6 |
24 | 4 4 4 4 4 4 4 |
25 | 4 3 3 4 4 3 4 |
26 | 5 4 5 4 4 3 4 |
27 | 3 3 4 4 4 4 4 |
28 | 5 4 5 4 5 4 5 |
29 | 5 5 5 5 5 6 6 |
30 | 4 3 4 3 4 4 4 |
31 | 4 4 4 5 4 4 4 |
32 | 4 3 3 3 3 3 4 |
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 2.1967.0 GPS week: 1967 Day: 0 MJD: 58013.000
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 268| 0 0 -4 -26 -14 11 .04 10 10 | -554 -59 10 112
emr 80| 0 0 1 -14 11 -22 .20 15 15 | 2520 902 15 121
esa 150| 0 1 -1 14 12 -18 -.01 9 9 | -1799 1848 7 152
gfz 192| 0 0 -3 -2 -1 -16 .11 12 11 | -439 482 10 120
grg 111| 1 -1 11 -9 17 62 -.43 16 15 | -23 263 12 190
igr n/a| 0 0 -1 3 8 -11 .05 4 4 | -4446 1185 12 86
jpl 80| 2 0 1 17 -14 13 .23 13 12 | 2073 856 45 199
mit 348| 0 -2 3 -10 12 -1 -.07 14 13 | -288 133 57 328
ngs 218| -1 0 -2 11 -15 -22 -.00 9 8 | -626 117 743 1863
sio 342| 0 0 2 -3 -5 32 .03 12 12 | --- --- --- ---
Table 2.1967.1 GPS week: 1967 Day: 1 MJD: 58014.000
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 270| 1 0 -2 -4 7 -16 -.00 9 9 | -701 101 12 113
emr 79| 0 0 0 23 8 0 .20 15 15 | 3271 641 14 134
esa 150| 0 0 -1 12 34 1 -.02 9 10 | -2344 1545 7 162
gfz 195| -1 0 -3 -1 -25 -3 .11 10 10 | -251 202 11 135
grg 111| 1 0 4 -20 5 44 -.38 15 14 | 5 229 13 197
igr n/a| 0 0 0 -8 7 -12 -.01 4 4 | -3586 940 13 92
jpl 80| -2 0 0 1 69 -77 .22 11 11 | 2598 778 40 200
mit 349| 0 -1 4 -28 -12 5 -.03 11 12 | -391 71 43 327
ngs 214| 0 1 0 23 -18 -14 .04 9 8 | -723 228 760 1956
sio 340| 0 -2 1 -40 -7 9 -.03 12 11 | --- --- --- ---
Table 2.1967.2 GPS week: 1967 Day: 2 MJD: 58015.000
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 267| 1 0 0 -7 20 5 .04 10 9 | -844 105 12 108
emr 80| 1 2 5 -4 -8 21 .20 16 15 | 4453 -2448 18 140
esa 150| 0 0 0 2 12 -9 -.04 10 9 | -1987 2467 7 161
gfz 195| -1 0 -3 -3 -12 3 .08 11 11 | -407 427 10 126
grg 103| 0 -1 6 -12 -16 1 -.45 15 13 | 229 -84 12 193
igr n/a| 0 0 0 -14 -7 2 .00 4 4 | -2439 -1890 12 90
jpl 80| 0 0 1 -7 -24 48 .22 12 12 | 3567 -2171 44 237
mit 349| -1 -1 6 4 -51 27 -.01 11 11 | -661 -4 43 333
ngs 214| -1 0 -5 23 37 -27 .08 8 8 | -651 -341 779 2097
sio 340| 0 -1 -1 -10 -22 -1 -.02 12 12 | --- --- --- ---
Table 2.1967.3 GPS week: 1967 Day: 3 MJD: 58016.000
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 271| 1 0 0 0 -4 9 -.01 9 9 | -783 3 10 93
emr 80| 0 1 4 22 6 -3 .18 16 15 | 2063 -890 16 144
esa 150| 0 0 0 -5 22 -1 -.01 9 9 | -2159 -397 7 153
gfz 197| 0 0 -1 6 13 -16 .10 10 9 | -353 -93 9 125
grg 109| 0 0 2 -25 8 35 -.43 15 15 | -178 117 13 176
igr n/a| 0 0 0 10 0 -3 .00 4 4 | -4240 -142 12 78
jpl 80| 0 -2 3 33 -5 13 .24 12 12 | 1278 -177 43 221
mit 349| -1 -1 5 -29 -16 4 .04 13 11 | -745 152 56 321
ngs 216| -1 0 -3 24 -15 3 .03 9 8 | -757 -50 784 1876
sio 337| 1 0 -3 -28 -32 -18 .02 13 12 | --- --- --- ---
Table 2.1967.4 GPS week: 1967 Day: 4 MJD: 58017.000
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 272| 1 0 -2 -22 -4 2 .01 10 10 | -726 -1 11 109
emr 80| 0 1 5 -10 -13 -3 .12 16 16 | 1368 238 18 136
esa 150| 0 0 -1 -17 -7 4 -.04 9 9 | -2529 -504 7 169
gfz 195| -1 0 -4 3 -19 -4 .09 10 9 | -562 854 9 127
grg 99| 1 1 19 -16 1 22 -.48 17 15 | -275 486 13 241
igr n/a| 0 0 -1 -21 -27 12 -.03 4 4 | -4203 322 11 93
jpl 80| 0 -1 1 12 -32 58 .20 12 12 | 1306 241 45 228
mit 350| -1 -1 4 20 20 -4 .03 12 11 | -1098 421 43 329
ngs 216| 0 0 -2 5 -28 3 .06 9 8 | -787 83 867 1737
sio 344| 0 0 -5 36 56 -26 .02 12 12 | --- --- --- ---
Table 2.1967.5 GPS week: 1967 Day: 5 MJD: 58018.000
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 271| 1 0 -2 27 28 12 .00 10 10 | -720 -36 11 97
emr 80| 2 -1 3 2 1 3 .19 15 15 | 974 -232 19 143
esa 150| 0 0 0 1 41 4 -.07 8 9 | -1661 989 8 169
gfz 194| -2 0 -3 6 2 -11 .06 11 11 | -17 -385 10 107
grg 110| 1 1 20 -15 29 -10 -.38 17 16 | 6 -190 13 181
igr n/a| 0 0 -3 7 4 12 -.01 5 5 | -4256 -292 13 81
jpl 80| -1 2 0 12 -16 51 .25 12 12 | 1042 -243 41 220
mit 350| 0 -1 3 -47 -89 -6 .02 12 12 | -595 -263 41 347
ngs 227| -1 0 -3 30 14 -1 .05 9 8 | -795 88 1250 2418
sio 339| 0 0 -3 -41 -87 7 .03 12 11 | --- --- --- ---
Table 2.1967.6 GPS week: 1967 Day: 6 MJD: 58019.000
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 270| 0 0 -5 15 -6 12 -.01 10 10 | -753 -127 11 105
emr 80| 2 -3 4 -20 -17 20 .20 16 16 | 1832 -872 18 136
esa 150| 0 0 -2 6 -2 -6 -.03 9 9 | -3376 2467 8 174
gfz 189| -2 -1 -4 -14 -39 -8 .07 11 12 | 167 -635 11 160
grg 110| 1 2 20 -25 -33 11 -.42 17 16 | 56 -228 14 199
igr n/a| 0 0 -5 -12 -30 16 -.00 4 4 | -3705 -891 13 78
jpl 80| -1 0 0 -18 -51 23 .24 12 12 | 1629 -1075 42 242
mit 350| -1 -1 4 -24 59 19 .03 12 11 | -265 -538 48 320
ngs 222| 0 1 0 29 -26 -22 .04 9 8 | -752 -131 983 2365
sio 338| 0 0 -3 -12 51 4 .00 13 12 | --- --- --- ---
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 3.1967.0 GPS week: 1967 Day: 0 MJD: 58013.000
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 8 8 10 11 4 9 13 4 13 3 | 29 33 33 30 28 30 35 30 29 38 30
2 | 12 11 11 14 12 5 13 20 12 18 5 | 24 28 25 34 19 30 28 41 32 36 28
3E | 11 9 9 12 25 3 11 16 7 7 4 | 38 43 43 41 35 40 44 37 40 43 39
X4 | 3 --- --- --- --- 25 18 --- --- --- 0 | 24 --- --- --- --- 31 28 --- --- --- 24
5 | 18 15 7 12 20 4 13 12 8 8 4 | 37 41 38 43 34 40 41 42 40 39 38
6 | 6 9 9 7 9 3 7 10 7 9 3 | 28 32 29 27 23 28 32 30 29 32 28
7 | 10 14 10 11 15 2 11 13 9 13 4 | 45 46 44 43 41 43 46 42 43 43 43
8 | 8 10 5 8 12 3 10 10 9 8 3 | 27 31 30 27 26 28 29 30 27 30 28
9 | 9 10 6 9 12 4 10 11 6 7 3 | 32 32 33 31 26 32 34 30 35 35 31
10E | 6 14 8 12 22 4 9 9 10 7 4 | 52 54 57 53 50 53 55 51 57 55 53
11 | 9 10 12 11 14 4 11 11 7 10 4 | 26 31 26 29 18 26 30 27 27 24 25
12E | 8 27 6 11 11 5 19 14 9 11 4 | 120 120 119 125 122 121 121 123 121 119 121
13 | 9 11 13 11 12 3 11 12 7 10 4 | 30 35 31 31 24 29 33 26 29 26 28
14 | 8 8 12 13 17 3 10 12 11 13 4 | 23 25 24 28 23 24 25 28 26 28 24
15 | 8 12 10 11 12 5 12 16 9 12 4 | 32 36 31 28 28 30 35 23 30 27 28
16E | 8 27 6 15 18 4 16 12 12 10 5 | 42 42 43 43 41 42 43 41 40 42 41
17 | 13 10 8 12 17 4 11 13 10 14 4 | 30 29 23 26 24 25 28 27 26 26 25
18 | 8 22 5 13 18 4 14 15 9 14 4 | 23 24 24 30 23 25 25 27 26 25 23
19 | 13 16 7 14 15 4 14 15 11 15 5 | 29 34 28 33 26 31 30 36 35 33 30
20 | 13 10 6 13 20 3 12 11 9 10 4 | 23 22 22 25 24 22 27 25 22 22 21
21 | 8 12 10 12 16 4 11 19 9 15 4 | 23 28 24 30 19 25 28 32 26 27 24
22 | 10 9 7 14 34 5 11 19 9 11 5 | 24 25 25 30 35 23 26 28 24 27 24
23 | 13 29 8 14 14 4 20 20 10 17 5 | 24 32 24 23 20 21 26 27 25 23 22
24 | 7 10 13 5 11 4 9 13 7 12 4 | 35 37 37 34 33 35 39 33 35 36 34
X25 | 7 14 --- 7 10 4 13 10 8 --- 4 | 31 35 --- 30 33 32 33 29 34 --- 31
26 | 9 17 8 10 17 4 13 13 12 10 4 | 23 28 21 24 20 23 24 22 23 20 21
27 | 8 11 4 9 9 3 9 6 11 8 3 | 32 36 33 33 29 32 33 32 30 35 32
28E | 11 13 7 12 23 4 8 14 7 13 4 | 57 58 58 60 62 59 57 60 61 58 58
29 | 11 21 10 13 17 4 13 17 11 15 5 | 43 45 41 42 39 41 43 44 41 35 40
30 | 8 8 10 9 12 3 8 10 5 10 3 | 29 32 32 26 25 29 33 28 31 33 29
31 | 7 14 10 12 10 3 13 8 10 14 4 | 27 32 28 30 25 29 32 28 32 30 28
32 | 11 7 7 13 14 4 28 8 9 11 3 | 30 34 34 35 27 33 41 32 37 38 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 9 12 16 4 13 14 9 12 |T 34 37 35 36 32 34 37 35 35 36 33
WRMS | 10 15 9 11 15 4 12 13 8 12 |NE 29 32 29 30 26 29 32 30 30 30 28
MEDI | 8 11 8 12 14 4 11 13 9 11 |MD 29 33 31 30 26 30 33 30 31 33 28
Table 3.1967.1 GPS week: 1967 Day: 1 MJD: 58014.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 7 9 7 11 3 8 10 9 14 3 | 23 28 26 25 22 23 29 25 22 34 25
2 | 11 12 13 14 17 7 9 20 11 16 5 | 17 21 18 24 16 21 20 33 22 26 20
3 | 10 10 8 8 28 4 10 8 6 7 4 | 41 42 42 39 43 37 42 39 39 41 39
X4 | 1 --- --- --- --- 18 20 --- --- --- 0 | 25 --- --- --- --- 24 21 --- --- --- 26
5 | 13 17 7 11 15 3 12 10 9 8 4 | 29 35 30 33 33 31 33 33 31 32 31
6 | 9 7 8 9 13 4 10 8 7 11 3 | 21 24 23 19 15 19 27 21 21 27 21
7 | 8 11 11 10 11 5 10 13 9 13 4 | 33 36 33 32 30 32 36 32 33 34 32
8 | 7 12 5 8 14 4 8 10 7 8 3 | 24 26 24 21 21 23 26 27 24 27 23
9 | 8 10 6 6 11 4 10 8 6 9 3 | 24 29 26 22 23 23 29 24 27 27 25
10 | 7 12 8 5 19 4 11 7 7 7 3 | 30 35 34 34 38 31 33 33 33 31 32
11 | 7 12 13 12 14 4 11 9 10 10 4 | 19 27 19 24 13 20 27 22 23 18 19
12 | 9 25 6 11 14 6 19 11 8 14 4 | 101 102 102 102 100 101 100 102 103 100 101
13 | 9 10 13 10 12 3 10 12 9 15 4 | 18 28 22 26 20 22 28 23 25 21 22
14 | 8 9 10 11 17 4 8 10 11 15 4 | 20 22 21 24 20 20 22 24 24 20 20
15 | 7 11 9 10 12 4 11 13 10 13 4 | 25 26 22 25 25 22 28 20 24 22 22
16E | 10 28 5 15 19 6 14 12 10 11 5 | 48 52 52 52 48 50 50 49 52 49 49
17 | 15 11 8 12 15 6 8 12 9 13 4 | 23 21 16 24 15 19 23 23 23 18 19
18 | 9 22 5 11 17 3 15 11 9 14 4 | 26 23 25 30 22 25 22 29 26 24 24
19 | 15 20 7 13 14 6 12 14 12 16 5 | 20 24 20 24 18 21 23 26 25 22 21
20 | 9 10 8 11 14 3 8 10 6 11 3 | 20 22 19 21 22 19 21 24 20 21 19
21 | 9 11 12 10 12 5 9 18 9 12 4 | 22 24 20 23 19 20 24 28 22 22 20
22 | 9 12 8 12 22 4 11 15 8 10 4 | 28 32 30 35 32 29 30 34 31 31 30
23 | 10 30 8 13 17 5 18 18 10 15 5 | 21 31 22 22 23 19 26 24 20 19 19
24 | 7 9 13 5 9 4 7 11 8 14 3 | 32 36 32 31 28 30 35 32 33 36 32
25 | 7 11 7 5 12 4 13 6 6 12 3 | 18 24 43 19 20 18 24 18 18 43 18
X26 | 10 --- 8 10 14 4 10 12 10 10 4 | 23 --- 22 24 21 21 22 22 22 21 21
27 | 7 9 5 11 12 4 8 5 8 9 3 | 28 30 30 27 28 27 30 31 28 33 28
28E | 9 11 7 10 24 5 8 12 8 8 4 | 53 52 50 48 54 51 51 51 48 49 49
29 | 9 22 9 10 13 5 14 13 10 18 4 | 32 31 26 31 28 29 29 32 31 27 29
30 | 8 7 10 8 11 3 8 8 3 11 3 | 21 27 24 21 17 21 29 20 24 26 22
31 | 10 14 11 12 11 4 12 8 9 13 4 | 21 26 18 20 16 19 26 19 20 24 18
32 | 7 8 5 6 14 3 10 6 8 9 3 | 27 32 28 31 27 28 33 27 31 30 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 9 10 15 4 11 11 9 12 |T 28 32 29 30 27 27 31 30 29 30 28
WRMS | 9 15 10 10 14 4 11 12 8 11 |NE 23 27 24 25 22 23 26 25 25 26 23
MEDI | 9 11 8 10 14 4 10 11 9 12 |MD 24 28 25 25 22 23 28 27 25 27 23
Table 3.1967.2 GPS week: 1967 Day: 2 MJD: 58015.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 10 9 11 11 3 8 7 5 11 3 | 24 28 25 25 20 22 28 22 22 29 23
2 | 14 14 11 14 15 7 12 20 10 19 5 | 22 28 22 33 18 26 25 35 31 31 25
3 | 9 9 11 8 23 3 11 7 7 9 4 | 24 29 27 28 24 24 27 23 25 28 24
X4 | 1 --- --- --- --- 30 24 --- --- --- 0 | 30 --- --- --- --- 41 27 --- --- --- 30
5 | 15 19 8 11 14 4 11 11 8 10 4 | 41 40 36 43 38 38 40 41 43 41 39
6 | 8 9 9 10 14 3 6 9 9 10 3 | 18 25 20 17 16 18 24 18 21 26 19
7 | 9 17 12 12 12 3 10 13 10 14 4 | 38 42 36 36 33 36 40 36 38 39 36
8 | 10 15 6 11 15 5 11 5 8 9 3 | 21 28 24 23 19 23 25 25 23 28 22
9 | 7 12 8 8 9 3 10 8 5 8 3 | 38 36 37 36 35 36 39 36 36 41 37
10 | 7 13 9 6 19 3 10 8 8 7 3 | 22 25 22 24 18 21 25 24 21 21 21
11 | 9 12 14 9 12 2 11 8 7 10 4 | 19 28 21 19 16 20 27 21 21 17 19
12 | 14 27 5 14 22 4 18 13 8 17 5 | 55 54 54 61 56 57 56 59 56 53 55
13 | 8 14 13 9 8 4 13 10 7 10 3 | 16 25 17 18 14 16 25 19 17 16 16
14 | 10 9 12 10 12 3 9 11 9 15 4 | 16 19 15 19 15 14 18 20 17 14 14
15 | 8 12 10 9 14 5 12 12 9 14 4 | 29 30 28 29 29 29 31 24 34 29 28
16E | 14 32 6 15 17 9 18 14 9 11 5 | 85 83 83 84 81 83 81 89 84 86 84
17 | 10 18 10 13 15 3 11 12 9 12 4 | 21 23 17 26 16 20 22 23 23 17 19
18 | 9 22 6 12 21 5 14 11 9 16 5 | 23 20 21 29 19 22 19 27 23 21 21
19 | 12 19 11 14 17 4 15 14 11 15 5 | 23 26 21 29 20 22 23 26 26 23 22
20 | 10 11 7 10 15 4 10 10 7 11 3 | 24 23 25 27 24 22 25 25 25 24 23
21 | 7 12 12 12 14 6 11 17 11 14 4 | 22 23 19 25 16 22 23 30 26 24 21
22 | 10 10 9 12 21 3 13 12 11 11 4 | 21 23 22 28 19 22 21 25 26 22 22
23 | 10 32 11 14 13 5 21 18 10 15 5 | 21 32 23 18 17 18 25 21 18 18 18
24 | 9 10 13 5 7 4 9 11 7 13 3 | 42 44 43 40 36 42 43 43 44 48 42
25 | 7 11 7 8 12 3 13 8 7 10 3 | 19 26 38 20 19 19 26 20 19 37 19
X26 | 10 12 8 13 14 6 12 11 --- 10 4 | 22 24 21 23 22 21 24 23 --- 20 20
27 | 8 11 7 12 13 5 10 8 8 10 3 | 26 26 26 28 23 26 28 31 26 31 26
28E | 14 17 9 10 21 7 12 12 8 9 4 | 119 120 120 119 121 119 121 119 119 119 119
29 | 8 19 9 11 15 4 13 12 11 16 4 | 27 29 23 25 25 25 28 28 27 22 24
30 | 7 12 9 8 9 5 8 10 6 11 3 | 23 28 26 23 23 24 29 22 26 30 24
31 | 7 15 11 10 9 3 13 9 8 14 4 | 23 27 20 20 18 21 28 20 22 26 20
32 | 6 10 6 4 12 2 9 6 8 10 3 | 31 34 33 34 31 31 35 30 34 34 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 10 11 15 4 12 11 8 12 |T 30 33 31 32 28 30 33 32 32 32 30
WRMS | 9 15 9 11 13 4 12 11 8 12 |NE 25 28 25 26 22 25 27 26 26 27 24
MEDI | 9 12 9 11 14 4 11 11 8 11 |MD 23 28 24 27 20 22 27 25 26 28 23
Table 3.1967.3 GPS week: 1967 Day: 3 MJD: 58016.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 10 9 7 10 4 7 10 12 11 3 | 35 39 38 32 30 35 37 35 37 39 35
2 | 14 14 12 14 15 6 10 22 12 17 5 | 19 25 23 32 19 26 23 35 28 28 24
3 | 8 11 8 7 14 4 11 7 7 11 3 | 25 27 26 26 25 24 25 24 25 30 24
X4 | 1 --- --- --- --- 40 22 --- --- --- 0 | 33 --- --- --- --- 35 27 --- --- --- 33
5 | 9 18 8 11 15 2 13 10 8 11 4 | 27 33 28 33 28 29 29 31 30 30 29
6 | 9 12 10 10 13 4 7 9 10 9 4 | 36 42 40 40 40 38 42 37 41 39 39
7 | 6 13 9 11 14 4 11 14 10 14 4 | 138 140 140 134 140 137 138 135 136 137 137
8 | 6 10 6 7 12 4 9 5 6 11 3 | 27 26 27 24 18 24 27 27 25 29 25
9 | 6 10 7 7 11 3 10 8 7 9 3 | 26 28 28 25 26 26 30 26 29 32 26
10 | 4 13 7 5 17 3 11 10 5 7 3 | 24 28 26 26 25 24 29 25 24 24 24
11 | 7 10 13 10 10 3 11 8 9 11 3 | 20 27 20 21 17 20 27 23 22 20 20
12 | 10 26 6 12 15 3 19 13 10 15 5 | 41 41 43 48 38 44 43 47 46 43 43
13 | 9 16 12 11 14 4 12 11 10 10 4 | 17 27 21 23 22 19 28 22 20 20 19
14 | 10 11 10 11 21 4 9 13 11 15 4 | 28 30 28 26 30 25 29 29 23 26 25
15 | 10 14 9 12 14 4 11 16 10 14 4 | 181 185 181 181 181 181 184 176 180 176 180
16 | 7 32 5 13 21 6 20 15 9 12 5 | 67 66 69 69 60 68 63 68 68 67 67
17 | 14 14 8 11 14 5 10 12 11 13 4 | 24 25 19 24 16 20 25 23 24 19 20
18 | 11 21 6 10 19 3 16 14 8 18 5 | 26 25 25 28 25 25 25 30 26 27 25
19 | 15 18 8 12 15 5 14 16 12 17 5 | 26 30 24 26 19 23 27 25 24 24 23
20 | 7 12 10 11 12 4 10 12 8 13 4 | 19 20 23 25 20 21 22 25 21 21 20
21 | 10 11 11 13 19 6 9 29 11 14 5 | 21 24 21 27 16 22 26 39 24 26 22
22 | 8 10 8 11 23 4 13 11 8 12 4 | 19 22 21 25 21 21 22 22 24 20 20
23 | 8 30 9 14 12 4 19 18 9 15 5 | 23 32 23 22 22 21 26 24 23 20 21
24 | 9 9 10 5 15 3 9 13 5 12 3 | 188 188 190 188 188 189 191 192 188 194 189
25 | 12 14 5 4 11 2 13 7 8 13 3 | 21 27 36 24 20 23 27 24 22 37 22
26 | 9 14 7 10 18 5 13 13 8 12 4 | 24 26 23 24 23 23 24 26 23 24 22
27 | 8 11 5 9 13 5 10 12 9 9 3 | 27 27 29 24 22 26 30 30 25 31 25
28 | 8 16 7 8 9 8 9 14 11 10 4 | 115 114 115 114 108 113 116 113 113 113 113
29 | 9 20 9 10 16 4 13 13 11 17 4 | 26 29 24 23 19 21 25 25 24 19 22
30 | 7 9 9 8 8 4 8 9 8 12 3 | 49 50 50 49 49 49 52 50 52 52 50
31 | 8 13 9 16 12 3 13 10 12 16 4 | 28 30 24 27 24 25 32 28 25 32 25
32 | 5 10 4 4 13 3 10 8 8 10 3 | 57 60 61 60 58 59 61 58 59 62 59
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 9 10 15 4 12 13 9 13 |T 44 48 46 46 43 44 47 47 46 47 44
WRMS | 9 15 9 9 15 4 12 11 8 12 |NE 43 46 44 44 42 43 45 46 44 45 42
MEDI | 8 13 8 10 14 4 11 12 9 12 |MD 26 29 27 26 25 25 28 29 25 30 25
Table 3.1967.4 GPS week: 1967 Day: 4 MJD: 58017.000
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 11 10 7 15 3 7 7 9 10 3 | 51 50 54 50 51 49 53 51 50 51 51
2 | 12 14 11 11 19 7 11 21 12 15 5 | 23 27 25 29 24 28 25 36 34 29 26
3 | 10 14 7 7 20 4 12 8 6 12 3 | 25 25 24 26 30 23 28 23 22 31 24
X4 | 2 --- --- --- --- 42 31 --- --- --- 0 | 38 --- --- --- --- 38 34 --- --- --- 38
5 | 11 15 6 10 26 3 12 9 7 10 4 | 38 41 37 40 41 39 39 38 38 38 37
6 | 7 12 10 8 14 3 8 11 8 8 3 | 71 74 71 68 70 71 71 69 70 72 70
7 | 10 14 10 9 12 4 12 14 8 12 4 | 367 371 373 364 372 367 374 364 365 366 368
8 | 8 13 6 9 13 3 8 6 7 9 3 | 24 27 25 21 25 22 27 23 23 26 23
9 | 9 10 9 8 15 3 9 7 7 9 3 | 33 37 36 34 37 34 39 34 33 40 34
10 | 7 18 7 6 23 3 9 9 7 9 4 | 27 30 25 25 33 25 31 27 25 29 26
11 | 10 11 16 7 14 2 11 6 7 10 4 | 21 28 26 21 20 22 30 23 21 22 21
12 | 12 26 6 12 15 3 17 13 9 13 4 | 41 43 43 48 46 43 45 47 43 44 43
13 | 8 17 11 12 10 4 13 10 8 14 4 | 21 30 23 26 20 23 29 24 25 23 22
14 | 10 11 12 11 13 3 9 9 9 14 4 | 43 48 50 46 51 46 50 45 44 44 45
15 | 10 14 8 10 15 4 12 14 7 13 4 | 740 746 748 734 736 739 744 738 736 737 740
16 | 8 30 7 13 17 6 15 13 11 12 5 | 44 42 43 47 53 44 46 45 44 45 44
17 | 12 14 9 9 18 5 10 12 9 13 4 | 24 28 21 25 27 22 28 26 23 22 22
18 | 11 20 6 11 23 3 12 13 7 16 4 | 25 26 23 27 29 24 25 29 26 27 24
19 | 14 19 9 12 20 6 17 16 10 16 5 | 24 30 26 29 26 25 25 28 27 25 25
20 | 8 13 7 10 18 4 9 10 7 10 3 | 24 24 24 23 30 22 27 25 24 23 22
21 | 9 13 10 9 19 5 11 18 10 16 4 | 24 27 21 24 22 23 27 30 24 27 23
22 | 11 15 10 12 26 4 11 10 10 10 4 | 19 19 18 24 23 19 21 21 20 18 18
23 | 11 29 9 12 15 3 19 16 11 12 5 | 25 31 25 25 26 23 27 25 23 22 22
24 | 6 12 13 6 8 3 7 13 8 11 3 | 486 487 489 488 490 489 493 486 487 484 487
25 | 10 15 6 7 15 4 12 6 5 11 3 | 26 29 40 27 30 26 31 26 27 43 26
26 | 9 14 8 8 14 4 10 9 8 9 3 | 25 26 24 25 27 24 28 24 24 24 23
27 | 8 14 9 10 14 5 11 15 11 8 4 | 28 33 31 27 29 25 30 33 27 31 28
28 | 13 14 8 10 22 5 9 16 11 11 4 | 67 66 65 67 71 66 65 66 63 62 64
29 | 9 22 7 11 22 4 16 15 10 18 5 | 29 32 28 30 31 29 29 30 29 25 27
30 | 8 12 10 7 10 3 11 12 5 10 3 | 144 143 144 142 142 142 144 145 146 146 144
31 | 8 13 11 11 10 4 15 9 8 14 4 | 48 49 47 50 51 49 50 47 49 50 48
32 | 10 16 7 5 11 2 12 7 8 9 3 | 132 133 134 130 127 131 131 133 133 133 132
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 9 10 17 4 12 12 9 12 |T 86 90 89 88 90 86 88 89 87 89 85
WRMS | 10 16 9 9 15 4 12 11 8 12 |NE 94 99 98 97 98 94 97 98 97 98 94
MEDI | 9 14 9 10 15 4 11 11 8 11 |MD 28 32 31 29 31 28 31 33 29 31 27
Table 3.1967.5 GPS week: 1967 Day: 5 MJD: 58018.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 10 10 8 12 5 7 5 9 9 3 | 59 61 59 58 60 60 60 58 58 62 58
2 | 12 13 11 15 21 6 10 22 11 17 5 | 15 20 17 21 17 19 17 32 22 23 17
3 | 11 14 8 5 17 4 10 8 7 11 3 | 26 33 30 29 31 27 30 30 28 36 28
X4 | 3 --- --- --- --- 31 24 --- --- --- 0 | 26 --- --- --- --- 25 23 --- --- --- 25
5 | 20 11 8 16 26 5 10 9 10 10 5 | 33 31 26 31 32 28 30 31 29 33 28
6 | 10 11 8 8 19 3 7 9 10 8 4 | 104 109 105 110 104 106 108 104 104 109 105
7 | 8 13 10 12 8 4 11 12 9 12 4 | 649 651 655 641 656 646 652 644 648 646 648
8 | 8 13 5 7 16 5 7 9 9 8 3 | 20 24 22 20 24 20 24 26 21 27 21
9 | 8 11 6 8 12 3 11 8 5 8 3 | 40 40 40 38 36 39 41 39 42 43 40
10 | 6 12 6 5 21 3 11 12 6 6 3 | 21 26 22 20 24 20 24 23 22 22 21
11 | 11 12 13 8 14 4 10 7 8 10 4 | 15 26 16 16 15 16 26 18 15 15 15
12 | 18 28 6 12 15 4 17 16 8 13 5 | 43 37 39 43 41 40 39 45 40 40 40
13 | 11 18 10 11 18 4 16 10 8 13 4 | 22 29 22 29 27 25 31 28 27 24 24
14 | 11 8 11 11 12 4 9 11 9 15 4 | 58 66 72 61 67 67 69 65 65 65 64
15 | 8 15 9 12 11 4 11 14 8 15 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
16 | 5 29 5 11 12 5 16 11 7 10 4 | 32 28 31 33 34 32 29 32 34 30 30
17 | 10 11 7 11 19 5 9 10 9 11 4 | 19 23 17 22 19 19 24 24 21 15 18
18 | 11 22 5 13 25 5 14 16 7 15 5 | 25 24 22 28 27 24 23 30 26 24 23
19 | 12 18 7 13 19 4 14 14 13 14 5 | 19 24 19 24 18 20 22 26 21 22 19
20 | 11 10 7 15 22 5 13 11 9 11 4 | 19 18 19 21 25 17 20 23 20 19 18
21 | 7 11 12 11 20 5 8 22 10 15 5 | 20 21 17 21 20 20 23 30 22 25 19
22 | 12 14 9 12 23 5 11 11 10 11 4 | 19 26 23 32 29 24 23 29 26 27 24
23 | 11 28 9 13 12 5 19 15 9 16 5 | 18 26 18 19 17 16 21 18 18 14 15
24 | 7 9 12 10 12 4 7 14 7 13 4 | 824 826 835 821 825 825 831 821 824 819 825
25 | 8 11 5 6 12 4 12 6 5 11 3 | 22 26 45 23 25 21 26 23 22 45 23
26 | 9 13 7 6 11 4 10 7 10 7 3 | 23 22 21 22 22 21 24 24 22 22 21
27 | 9 12 6 10 14 6 9 14 8 11 3 | 23 25 23 21 26 21 26 30 21 30 23
28 | 12 13 6 11 15 5 13 14 7 10 4 | 32 33 31 31 33 31 32 36 33 37 32
29 | 8 23 8 13 18 5 14 16 12 19 5 | 27 26 23 27 27 24 23 29 27 24 24
30 | 8 8 9 10 10 5 10 10 8 8 3 | 257 255 256 256 258 257 256 260 255 259 257
31 | 10 13 11 10 9 4 13 11 12 15 4 | 83 87 85 84 84 84 88 85 85 86 84
32 | 8 16 4 4 13 4 9 12 7 7 3 | 209 217 219 213 211 212 212 212 210 212 213
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 8 11 17 5 12 12 9 12 |T 90 95 94 93 94 90 92 95 93 95 90
WRMS | 10 15 9 11 16 5 12 12 8 11 |NE 101 108 107 106 106 102 104 108 106 107 101
MEDI | 9 13 8 11 15 4 11 11 9 11 |MD 26 26 23 29 27 25 26 30 27 30 24
Table 3.1967.6 GPS week: 1967 Day: 6 MJD: 58019.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 12 9 10 13 4 6 7 5 11 3 | 97 99 98 98 94 97 98 99 98 100 97
2 | 12 12 11 17 20 5 12 21 12 18 5 | 26 27 26 33 22 27 27 36 29 29 26
3 | 5 15 6 6 19 4 9 7 6 10 3 | 40 44 40 42 42 40 41 37 39 46 40
X4 | 3 --- --- --- --- 34 38 --- --- --- 0 | 37 --- --- --- --- 28 36 --- --- --- 37
5 | 11 13 7 14 24 3 10 8 8 12 4 | 47 54 47 52 50 48 50 49 47 50 48
6 | 8 13 9 12 19 4 7 9 8 9 4 | 197 196 197 195 195 196 195 196 196 195 196
7 | 11 13 10 11 8 4 11 13 8 12 4 | 959 960 967 952 968 958 966 960 958 957 960
8 | 7 15 5 12 13 4 8 11 5 10 3 | 32 36 33 25 35 29 34 35 30 34 31
9 | 9 13 6 9 16 3 12 6 10 11 3 | 55 56 55 53 54 54 57 55 57 59 55
10 | 8 12 8 9 22 4 11 13 8 9 4 | 32 35 33 30 39 32 34 36 33 36 33
11 | 12 13 14 9 11 4 10 7 6 11 4 | 29 35 25 27 21 28 34 29 29 28 27
12 | 12 27 7 12 17 3 19 14 9 13 5 | 52 54 54 57 58 54 54 59 55 53 54
13 | 9 14 11 10 14 5 10 10 10 16 4 | 32 41 34 35 34 33 41 35 31 35 32
14 | 10 10 12 10 13 6 9 13 8 15 4 | 96 107 116 103 109 108 108 107 103 105 105
15 | 8 13 8 11 13 4 16 14 9 16 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
16 | 11 28 6 11 20 6 16 14 10 13 5 | 43 41 43 48 47 45 43 50 49 47 45
17 | 12 12 7 13 20 5 9 10 9 11 4 | 25 35 26 34 27 29 32 34 31 31 28
18 | 11 20 7 13 28 4 15 13 10 21 5 | 42 39 41 42 47 41 41 45 40 44 40
19 | 14 19 6 16 23 5 14 13 11 13 5 | 29 33 25 31 30 26 26 28 27 27 26
20 | 10 11 7 15 20 4 10 10 9 13 4 | 39 39 38 39 45 36 40 36 35 36 37
21 | 9 13 9 11 19 6 12 20 12 16 5 | 29 31 31 28 29 27 34 33 27 29 27
22 | 5 14 9 11 23 3 10 9 8 9 4 | 44 47 44 50 47 46 44 47 49 48 46
23 | 13 29 8 12 16 4 19 15 10 16 5 | 32 37 27 24 29 25 32 25 23 25 25
24 | 8 9 12 9 12 5 9 14 6 12 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
25 | 12 12 6 6 14 4 13 7 7 13 3 | 27 32 49 30 33 27 34 31 27 50 29
26 | 10 14 6 8 12 4 9 7 10 9 3 | 31 30 33 32 34 32 33 32 33 36 32
27 | 8 12 5 9 15 3 10 13 8 6 3 | 33 34 34 30 35 31 34 37 30 36 32
28 | 16 13 9 11 13 6 9 14 11 12 4 | 69 66 66 66 69 67 67 66 67 66 66
29 | 12 23 7 13 19 7 14 18 11 19 5 | 40 42 38 36 42 37 41 44 35 40 38
30 | 7 9 9 12 10 5 9 11 8 10 3 | 383 381 381 384 386 383 383 384 383 385 383
31 | 8 12 13 11 9 3 11 14 10 12 4 | 146 146 145 144 144 143 146 143 141 144 144
32 | 7 14 8 6 11 5 8 14 8 11 3 | 340 344 349 339 340 342 348 339 340 340 341
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 9 11 17 4 12 12 9 13 |T 102 107 106 105 107 102 105 107 104 107 102
WRMS | 10 16 9 12 16 4 12 11 8 12 |NE 113 120 119 117 118 113 116 119 116 119 113
MEDI | 9 13 8 11 16 4 10 13 9 12 |MD 40 41 41 42 45 37 41 44 39 46 38
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 4.1967 GPS week: 1967 MJD: 58013.0-58019.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 |U 5 6 16 |U 6 7 23 |U 7 7 16 |
emr | emr 2960 |U 7 8 20 |U 6 8 23 |U 8 9 18 |
esa | esa 2962 | 5 7 16 |U 6 7 24 | 8 8 17 |
gfz | gfz 2972 |U 6 6 17 |U 6 8 24 |U 7 7 16 |
grg | grg 2971 |U 12 15 23 |U 7 9 32 | 10 10 20 |
igr | igr 2973 | 6 7 17 | 5 7 23 | 7 7 16 |
igs | igs 2974 | 5 6 17 | 5 7 24 | 7 7 15 |
jpl | jpl 3072 | 6 7 19 |U 6 8 25 | 8 8 18 |
mit | mit 2976 | 6 7 18 |U 8 11 33 |U 10 10 22 |
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 5.1967.0 GPS week: 1967 Day: 0 MJD: 58013.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 5 3 12 | 5 5 20 | 8 10 14 |
emr | emr 2966 | 6 7 14 | 6 7 23 | 8 10 17 |
esa | esa 2880 | 6 5 11 | 5 6 22 | 9 12 17 |
gfz | gfz 2964 | 6 4 12 | 5 6 20 | 7 10 13 |
grg | grg 2962 | 7 6 13 | 14 13 54 | 10 13 17 |
igr | igr 2955 | 6 4 12 | 5 5 21 | 8 10 14 |
igs | igs 2966 | 6 4 12 | 5 5 22 | 8 9 13 |
jpl | jpl 3072 | 7 5 12 | 5 6 22 | 9 12 15 |
mit | mit 2976 | 7 7 17 | 10 19 30 | 12 12 25 |
Table 5.1967.1 GPS week: 1967 Day: 1 MJD: 58014.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 5 7 14 | 7 9 30 | 9 8 18 |
emr | emr 2880 | 6 10 21 | 8 10 29 | 10 9 22 |
esa | esa 2976 | 6 8 17 | 8 8 29 | 9 9 21 |
gfz | gfz 2976 | 6 9 17 | 7 9 30 | 9 7 21 |
grg | grg 2976 | 9 10 19 | 8 8 29 | 10 9 20 |
igr | igr 2976 | 6 9 18 | 8 8 29 | 9 8 20 |
igs | igs 2976 | 6 9 17 | 7 8 29 | 9 8 19 |
jpl | jpl 3072 | 7 9 19 | 8 8 29 | 10 10 21 |
mit | mit 2976 | 6 9 18 | 7 7 31 | 10 10 20 |
Table 5.1967.2 GPS week: 1967 Day: 2 MJD: 58015.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 5 5 15 | 8 11 32 | 8 8 16 |
emr | emr 2976 | 6 6 20 | 8 11 27 | 9 10 20 |
esa | esa 2976 | 6 6 15 | 8 10 32 | 8 9 18 |
gfz | gfz 2973 | 6 6 16 | 9 11 34 | 7 7 16 |
grg | grg 2974 | 26 33 40 | 8 10 33 | 9 8 22 |
igr | igr 2976 | 5 6 16 | 8 11 33 | 8 8 17 |
igs | igs 2976 | 6 6 16 | 8 11 33 | 8 7 17 |
jpl | jpl 3072 | 6 6 18 | 7 10 29 | 10 8 21 |
mit | mit 2976 | 6 5 17 | 8 9 36 | 9 9 19 |
Table 5.1967.3 GPS week: 1967 Day: 3 MJD: 58016.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 6 6 19 | 5 5 18 | 7 5 18 |
emr | emr 2976 | 8 8 27 | 5 6 18 | 9 10 18 |
esa | esa 2976 | 6 8 20 | 5 6 20 | 7 6 18 |
gfz | gfz 2976 | 7 7 21 | 5 6 20 | 7 5 18 |
grg | grg 2972 | 7 8 22 | 5 8 22 | 9 8 21 |
igr | igr 2976 | 7 8 21 | 5 6 19 | 7 6 17 |
igs | igs 2976 | 6 7 20 | 5 5 19 | 7 6 18 |
jpl | jpl 3072 | 8 8 23 | 6 7 22 | 8 8 19 |
mit | mit 2976 | 7 9 24 | 8 9 41 | 12 9 28 |
Table 5.1967.4 GPS week: 1967 Day: 4 MJD: 58017.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 7 16 | 5 7 23 | 7 6 13 |
emr | emr 2976 | 6 8 19 | 4 7 23 | 8 6 14 |
esa | esa 2976 | 5 7 16 | 5 6 22 | 7 7 15 |
gfz | gfz 2971 | 4 7 15 | 5 6 21 | 7 6 12 |
grg | grg 2970 | 24 33 38 | 5 8 24 | 10 7 14 |
igr | igr 2976 | 4 7 16 | 5 6 22 | 7 7 12 |
igs | igs 2976 | 4 7 16 | 5 6 21 | 7 6 12 |
jpl | jpl 3072 | 5 6 18 | ---- ---- ---- | 8 6 14 |
mit | mit 2976 | 4 7 15 | 5 7 25 | 8 7 15 |
Table 5.1967.5 GPS week: 1967 Day: 5 MJD: 58018.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 7 21 | 6 8 24 | 5 5 15 |
emr | emr 2976 | 8 9 25 | 5 9 24 | 6 8 18 |
esa | esa 2976 | 5 7 21 | 5 9 22 | 5 5 17 |
gfz | gfz 2974 | 6 7 20 | 6 9 24 | 5 5 15 |
grg | grg 2973 | 6 7 21 | 6 11 31 | 11 13 21 |
igr | igr 2976 | 6 7 22 | 5 7 20 | 4 5 16 |
igs | igs 2976 | 6 6 21 | 5 9 24 | 5 5 15 |
jpl | jpl 3072 | 6 8 24 | 6 9 25 | 5 8 20 |
mit | mit 2976 | 5 7 23 | 7 12 30 | 6 7 19 |
Table 5.1967.6 GPS week: 1967 Day: 6 MJD: 58019.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 5 15 | 4 6 18 | 7 7 15 |
emr | emr 2976 | 8 7 18 | 5 7 17 | 10 9 16 |
esa | esa 2976 | 5 6 16 | 4 7 19 | 7 8 17 |
gfz | gfz 2973 | 5 6 14 | 4 7 21 | 7 6 16 |
grg | grg 2971 | 5 6 13 | 4 8 30 | 12 11 26 |
igr | igr 2976 | 5 6 15 | 4 6 19 | 7 8 16 |
igs | igs 2976 | 5 6 14 | 4 6 20 | 7 7 15 |
jpl | jpl 3072 | 6 7 18 | 5 8 21 | 8 9 18 |
mit | mit 2976 | 6 8 16 | 9 10 37 | 11 15 31 |
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 6.1967 GPS week: 1967 MJD: 58013.500-58019.500
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 | 0 1 -4 93 -4 | 27 33
| 16 18 67 71 4 | 3
emr uuuuu | 8 -4 80 109 -11 | 49 55
| 7 39 168 107 6 | 9
esa uuuuu | -9 2 0 32 3 | 39 42
| 7 16 60 72 2 | 3
gfz uuuuu | 2 -12 66 -124 -3 | 29 34
| 26 15 98 125 2 | 5
grg uuuuu | 13 11 -15 110 -5 | -1 16
| 15 19 35 42 3 | 4
igr xxxxx | 8 7 -3 -1 -1 | 1 16
| 10 11 64 33 2 | 4
irf xxxxx | 9 -4 -44 6 5 | -2 18
| 13 10 23 18 8 | 4
jpl xxxxx | 46 -4 -10 154 -9 | 35 39
| 14 15 33 44 12 | 6
mit uuuuu | 10 10 -117 -13 5 | 23 28
| 23 9 71 55 7 | 4
ngs uuuuu | -10 -25 78 -128 11 | 16 24
| 26 12 67 110 3 | 4
sio uuuux | 2 33 -121 22 -5 | 82 83
| 10 24 106 54 5 | 4
Table 7.1967.0 GPS week: 1967 Day: 0 MJD: 58013.500
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 20 -92 97 -2 | 31 36
emr uuuuu | 18 61 -144 40 -9 | 61 69
esa uuuuu | -8 -22 46 53 3 | 43 46
gfz uuuuu | -4 -4 -70 -31 -5 | 36 41
grg uuuuu | -2 -2 -4 96 -1 | 5 16
igr xxxxx | -8 -16 48 42 2 | 6 16
irf xxxxx | -3 -17 -15 -31 -7 | 3 18
jpl xxxxx | 42 -18 30 200 -12 | 44 45
mit uuuuu | -3 9 -38 -117 -6 | 29 33
ngs uuuuu | -8 -34 154 -101 11 | 17 26
sio uuuux | -4 6 49 -27 -6 | 89 90
Table 7.1967.1 GPS week: 1967 Day: 1 MJD: 58014.500
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 -3 -57 85 -1 | 30 36
emr uuuuu | -2 17 -36 -34 -12 | 60 69
esa uuuuu | -12 -9 38 179 4 | 41 45
gfz uuuuu | 39 -1 -48 60 -5 | 33 39
grg uuuuu | 17 22 18 132 -6 | 3 17
igr xxxxx | 0 13 -55 13 0 | 4 17
irf xxxxx | -11 -3 -10 5 -2 | 0 20
jpl xxxxx | 45 2 -33 127 -1 | 40 43
mit uuuuu | -18 2 -13 -52 -2 | 26 32
ngs uuuuu | -1 -29 160 -304 18 | 16 25
sio uuuux | -14 38 -143 -29 -3 | 85 87
Table 7.1967.2 GPS week: 1967 Day: 2 MJD: 58015.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 12 7 77 195 2 | 28 33
emr uuuuu | 7 23 -73 11 -13 | 54 62
esa uuuuu | 1 -8 4 34 3 | 39 42
gfz uuuuu | 29 -6 47 -116 -4 | 30 34
grg uuuuu | 36 10 -43 109 -3 | 0 14
igr xxxxx | 13 14 -70 6 -1 | 2 15
irf xxxxx | 15 -5 -51 23 4 | -3 17
jpl xxxxx | 44 4 -36 139 -25 | 40 42
mit uuuuu | 1 0 -109 35 0 | 22 27
ngs uuuuu | -64 -27 100 -221 9 | 14 22
sio uuuux | 15 31 -124 12 -9 | 83 84
Table 7.1967.3 GPS week: 1967 Day: 3 MJD: 58016.500
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 6 4 123 -9 | 25 31
emr uuuuu | 2 -50 111 217 -19 | 44 47
esa uuuuu | -14 18 73 -12 5 | 36 38
gfz uuuuu | -21 -27 111 -177 -3 | 25 30
grg uuuuu | 6 28 -79 88 -6 | -3 14
igr xxxxx | 9 4 -35 -48 -1 | -1 13
irf xxxxx | 10 10 -65 -3 15 | -7 16
jpl xxxxx | 43 -5 -19 226 -12 | 33 37
mit uuuuu | -4 20 -145 -7 12 | 19 23
ngs uuuuu | 10 -42 59 -111 10 | 12 20
sio uuuux | 7 61 -267 0 3 | 80 81
Table 7.1967.4 GPS week: 1967 Day: 4 MJD: 58017.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -6 21 36 134 -4 | 22 29
emr uuuuu | 16 -30 165 250 -17 | 40 44
esa uuuuu | 2 13 -31 24 3 | 34 37
gfz uuuuu | -31 -36 156 -327 -2 | 23 28
grg uuuuu | 6 -24 -13 150 -8 | -5 16
igr xxxxx | 20 10 96 29 2 | -4 15
irf xxxxx | 10 8 -44 13 13 | -7 17
jpl xxxxx | 31 -27 25 163 -19 | 29 34
mit uuuuu | 16 16 -128 5 9 | 17 22
ngs uuuuu | 11 -14 -33 -48 10 | 12 20
sio uuuux | -2 34 -118 11 -5 | 77 78
Table 7.1967.5 GPS week: 1967 Day: 5 MJD: 58018.500
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 -20 -63 44 -2 | 24 31
emr uuuuu | 11 -37 297 145 -4 | 40 44
esa uuuuu | -14 22 -27 -35 0 | 36 39
gfz uuuuu | 11 -14 77 -81 1 | 24 30
grg uuuuu | 32 31 19 157 -8 | -4 16
igr xxxxx | 16 5 -49 -13 -5 | -2 15
irf xxxxx | 27 -5 -65 14 10 | -4 17
jpl xxxxx | 76 0 14 121 3 | 28 33
mit uuuuu | 38 20 -210 3 11 | 20 25
ngs uuuuu | -18 -7 39 -143 10 | 16 23
sio uuuux | 4 1 -32 118 -12 | 78 79
Table 7.1967.6 GPS week: 1967 Day: 6 MJD: 58019.500
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 -25 64 -27 -9 | 29 36
emr uuuuu | 8 -9 243 138 -2 | 44 49
esa uuuuu | -15 -1 -105 -18 2 | 42 46
gfz uuuuu | -6 6 191 -193 -2 | 30 36
grg uuuuu | 0 14 0 36 -3 | -1 18
igr xxxxx | 7 19 42 -35 -3 | 2 18
irf xxxxx | 18 -12 -55 19 3 | 2 22
jpl xxxxx | 43 19 -52 104 7 | 32 39
mit uuuuu | 43 4 -179 40 11 | 26 34
ngs uuuuu | -1 -23 70 30 6 | 23 31
sio uuuux | 9 62 -213 72 -6 | 81 83
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