[IGSREPORT-25478] Wk 1962 IGS Final Orbits
acc
acc at igs.org
Thu Aug 31 18:06:21 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1962 (Aug 13, 2017 - Aug 19, 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:
igs1962[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1962[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1962[0-6].cls IGS GPS clock combination summary report.
igs19627.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19627.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 | TIXI MAL2 REUN TIXI
0 | EMR | CHUR HERS KERG
0 | ESA | FAA1 REUN
0 | GFZ | LHAZ SAVO LHAZ MAL2 SAVO
0 | GRG | DAEJ FAA1 GLSV DAEJ GLSV REUN
1 | COD | GLSV TIXI GLSV TIXI
1 | EMR | ALBH HERS
1 | ESA | UFPR KARR UFPR
1 | GFZ | HARB POVE SALU SYOG HARB PIE1 POVE SALU SYOG TRO1
1 | GRG | 17 21 17 21 DAEJ GLSV PIE1 SEYG SYOG TASH TRO1 ULAB
1 | GRG | DAEJ GLSV PIE1 SEYG SYOG TASH TRO1 ULAB
1 | MIT | KARR KARR
2 | COD | 31 TIXI TIXI
2 | EMR | 31 HERS
2 | ESA | MAL2 MAL2
2 | GFZ | MAL2 MAL2 THU3
2 | GRG | 13 13 DAEJ GLSV LHAZ SYOG DAEJ GLSV SYOG
3 | COD | ALRT TIXI ALRT TIXI
3 | EMR | ALGO HERS
3 | ESA | DGAR DGAR
3 | GFZ | MAL2 MAL2
3 | GRG | ADIS ARTU DAEJ GLSV LPGS MAL2 PIE1 SYOG ADIS ARTU
3 | GRG | DAEJ FAA1 GLSV LPGS MAL2 SYOG
3 | MIT | NRIL RBAY NRIL RBAY
4 | COD | TIXI LHAZ TIXI
4 | EMR | 26 26 CHUR KIRU MAS1
4 | ESA | FAA1 KOUR LHAZ MAL2 ONSA SAVO FAA1 KOUR MAL2 ONSA
4 | ESA | SAVO
4 | GFZ | GRAZ LHAZ ONSA TRO1 GRAZ ONSA TRO1
4 | GRG | DAEJ KIRU MAC1 MAL2 MGUE NNOR SYOG TRO1 ALRT DAEJ
4 | GRG | GLSV KIRU LHAZ MAL2 MAS1 MGUE NNOR PIE1 SYOG TRO1
4 | MIT | ALRT ALRT
5 | COD | 26 26 INEG SEYG TIXI TIXI
5 | EMR | FAIR FAIR TWTF
5 | ESA | FAA1 LHAZ SFER FAA1 LHAZ LMMF SEYG SFER
5 | GFZ | BRMU FAA1 MAL2 SFER FAA1 MAL2 SFER ZECK
5 | GRG | DAEJ GLSV MAL2 SYOG TRO1 DAEJ GLSV LHAZ MAL2 SYOG
5 | GRG | TRO1
6 | COD | BAKE BAKE
6 | EMR | 25 11 25 CHUR HERS YAKT ALBH CHUR FAIR HERS MAS1
6 | EMR | SUWN TWTF WHIT YAKT YELL
6 | ESA | BAKE MAW1 BAKE MAW1
6 | GFZ | MAL2 MDVJ SYOG MAL2 MDVJ
6 | GRG | 5 13 5 13 ADIS DAEJ GLSV MAC1 MAL2 MAW1 SYOG TEHN
6 | GRG | ADIS DAEJ GLSV MAC1 MAL2 MAW1 TEHN
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. 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
----+--------+---------------
4 | GRG | 26
4 | NGS | 26
7. 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 G01 | | | | | | | 4 |
PRN G02 | | | | | | | 4 |
PRN G03 | | | | | | | 4 |
PRN G04 | | | | | | | 4 |
PRN G05 | | | | | | | 4 |
PRN G06 | | | | | | | 4 |
PRN G07 | | | | | | | 4 |
PRN G08 | | | | | | | 4 |
PRN G09 | 4 | 4 | | | | | 4 |
PRN G10 | | | | | | | 4 |
PRN G11 | | | | | | | 4 |
PRN G12 | | | | | | | 4 |
PRN G13 | | | | | | | 4 |
PRN G14 | | | | | | | 4 |
PRN G15 | | | | | | | 4 |
PRN G16 | | | | | | | 4 |
PRN G17 | | | | | | | 4 |
PRN G18 | | | | | | | 4 |
PRN G19 | | | | | | | 4 |
PRN G20 | | | | | | | 4 |
PRN G21 | | | | | | | 4 |
PRN G22 | | | | | | | 4 |
PRN G23 | | | | | | | 4 |
PRN G24 | | | | | | | 4 |
PRN G25 | | | | | | | 4 |
PRN G26 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G27 | | | | | | | 4 |
PRN G28 | | | | | | | 4 |
PRN G29 | | | | | | | 4 |
PRN G30 | | | | | | | 4 |
PRN G31 | | | | | | | 4 |
PRN G32 | | | | | | | 4 |
8. 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.
9. 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 | .0 .0 1.1 6 13 5 -.54
EMR | 0 | 3.2 -8.9 -4.7 -16 -3 -21 -.44
ESA | 0 | .5 -.4 .0 -11 1 -5 -.51
GFZ | 0 | .7 .4 .9 -3 -29 -10 -.43
GRG | 0 | -.3 5.5 6.5 39 6 7 -.23
JPL | 0 | 5.7 -6.0 -2.8 -33 -10 43 .09
MIT | 0 | -5.2 .4 -.5 -13 28 -15 -.36
NGS | 0 | -3.0 -8.6 -5.8 -16 -9 5 -.50
SIO | 0 | -5.1 1.4 -18.2 -28 -10 -10 -.59
COD | 1 | .0 -.3 .9 2 2 10 -.57
EMR | 1 | 2.3 -8.4 -5.1 15 -4 -17 -.41
ESA | 1 | .3 .6 -.5 14 -10 0 -.58
GFZ | 1 | .7 .2 .6 -5 -41 -5 -.37
GRG | 1 | -.5 3.3 -4.2 65 13 3 -.22
JPL | 1 | -.1 -6.1 -7.6 -52 -40 38 .30
MIT | 1 | -2.9 -1.1 .7 12 27 -31 -.27
NGS | 1 | -2.7 -4.1 -6.7 14 -10 -21 -.23
SIO | 1 | -4.6 .8 -15.2 -20 -20 6 -.33
COD | 2 | -.0 -.0 .9 6 -2 2 -.66
EMR | 2 | 1.3 -3.2 -8.3 2 -4 -17 -.46
ESA | 2 | -.6 .8 -.7 1 -2 -5 -.72
GFZ | 2 | .7 .6 1.2 8 -23 -8 -.56
GRG | 2 | -2.5 -1.6 -2.8 44 14 -3 -.28
JPL | 2 | 6.7 -3.3 -9.1 -27 -39 93 -.09
MIT | 2 | -4.1 -3.0 .5 2 7 -19 -.29
NGS | 2 | -6.5 -7.1 -4.5 39 -30 -19 -.34
SIO | 2 | -5.4 -.5 -10.0 -17 7 4 -.32
COD | 3 | .2 -.2 1.1 2 4 2 -.51
EMR | 3 | -5.2 3.1 -9.4 1 30 -24 -.40
ESA | 3 | -.7 -.2 -.3 -8 8 -9 -.53
GFZ | 3 | .7 .4 .9 2 -33 -17 -.43
GRG | 3 | -2.8 -.7 7.6 53 12 44 -.18
JPL | 3 | 9.3 -3.6 -5.1 8 -68 81 -.02
MIT | 3 | -3.4 -.7 1.5 -11 32 -4 -.16
NGS | 3 | -6.3 -12.9 -6.3 32 -8 -9 -.21
SIO | 3 | -1.5 -4.1 -13.9 -7 10 -10 -.20
COD | 4 | .5 -.0 1.3 5 5 -4 -.68
EMR | 4 | -4.3 7.4 -6.0 -13 23 -1 -.48
ESA | 4 | -.5 -.7 -.7 -6 15 2 -.50
GFZ | 4 | .5 -.0 1.1 -10 -39 -2 -.51
GRG | 4 | .7 7.5 4.1 43 28 23 -.33
JPL | 4 | 11.2 .3 -6.6 -18 -52 72 .03
MIT | 4 | -.6 -1.6 2.5 -8 47 -13 -.26
NGS | 4 | -4.0 -11.1 .3 20 -6 -17 -.29
SIO | 4 | -1.1 -4.0 -7.7 -9 -16 9 -.19
COD | 5 | .4 .3 1.1 11 1 -8 -.57
EMR | 5 | -9.7 7.9 -1.1 3 35 3 -.25
ESA | 5 | -.6 -.5 -.5 9 1 -4 -.50
GFZ | 5 | 1.1 .2 .9 5 -50 -8 -.47
GRG | 5 | .3 2.1 .9 53 20 17 -.34
JPL | 5 | 4.1 .3 -4.1 -17 -58 72 .26
MIT | 5 | -1.7 1.8 -1.3 -15 42 -8 -.14
NGS | 5 | -9.0 -.9 .6 11 -10 -5 -.16
SIO | 5 | -4.8 -.2 -9.1 3 -12 -11 -.22
COD | 6 | .2 -.1 .8 4 -1 1 -.50
EMR | 6 | -14.0 11.0 1.6 5 24 11 -.24
ESA | 6 | -.3 -.4 -1.7 21 -24 -17 -.41
GFZ | 6 | .6 .3 .5 0 -38 0 -.40
GRG | 6 | -6.7 5.3 10.9 44 10 23 -.11
JPL | 6 | .2 1.7 -1.0 -23 -35 94 .07
MIT | 6 | -3.1 2.0 -6.0 -7 30 -6 -.17
NGS | 6 | -3.9 -4.0 -2.1 27 -30 -12 -.20
SIO | 6 | -3.7 3.3 -10.8 6 -21 -8 -.23
10. 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.
11. 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 1.1962.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1962.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 2.1962.[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 3.1962.[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 5.1962.0-6). 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 1962 summary. (Aug 13, 2017 - Aug 19, 2017)
Table 1.1962.a GPS week: 1962 MJD: 57978.000-57984.000
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 276| 1 0 2 4 -4 5 .05 10 9 | -524 -252 10 97
| 0 0 1 15 21 8 .03 | 438 676
emr 84| -2 0 -1 15 3 -3 .15 16 16 | -720 -157 21 139
| 3 3 2 12 9 12 .04 | 472 868
esa 150| 0 0 -2 -2 7 -1 .01 10 10 | -1198 -492 9 153
| 0 0 1 13 10 5 .03 | 885 1416
gfz 199| -1 1 0 -10 -11 4 .13 11 10 | -262 -13 12 120
| 0 0 0 8 16 7 .03 | 190 491
grg 110| 1 0 5 -22 10 -9 -.33 18 15 | 146 -80 14 190
| 0 0 5 8 10 22 .03 | 162 203
igr n/a| 0 0 0 -10 -8 7 .00 5 4 | -2931 283 12 74
| 0 0 1 7 8 6 .03 | 859 594
jpl 80| 0 0 -2 25 -9 33 .25 12 12 | -650 -190 39 207
| 1 1 1 14 15 18 .04 | 464 906
mit 349| 0 0 0 -4 -11 0 -.07 12 11 | -637 -121 40 315
| 1 0 1 13 22 11 .03 | 269 128
ngs 220| 0 0 -2 10 15 14 -.02 12 8 | -507 -293 937 2104
| 0 0 2 17 12 17 .04 | 383 668
sio 352| 0 -1 0 -4 -12 -20 .01 12 11 | --- --- --- ---
| 0 0 1 25 28 32 .06 | --- ---
Table 1.1962.b GPS week : 1962 MJD: 57978.000-57984.000
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 3 3 4 3 3 3 |
2 | 5 5 5 6 6 6 6 |
3 | 3 4 3 4 4 4 4 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 4 4 4 4 4 |
6 | 4 4 4 4 4 4 4 |
7 | 5 5 5 4 5 5 5 |
8 | 4 3 4 3 3 3 3 |
9 | 4 3 3 4 4 4 4 |
10 | 3 3 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 6 5 5 6 5 5 6 |
13 | 4 3 4 4 4 4 4 |
14 | 4 5 5 5 5 5 5 |
15 | 4 4 4 5 5 4 5 |
16 | 6 6 6 6 6 6 6 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 6 6 6 5 5 |
19 | 5 6 5 6 6 6 6 |
20 | 4 4 5 4 4 4 4 |
21 | 4 4 5 5 5 5 5 |
22 | 5 5 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 3 4 3 3 4 4 |
25 | 5 5 5 5 5 5 8 |
26 | 6 6 6 7 15 6 5 |
27 | 4 3 3 3 3 3 3 |
28 | 5 4 5 5 4 4 4 |
29 | 5 5 5 5 5 6 5 |
30 | 3 3 3 3 3 3 4 |
31 | 5 5 6 5 5 4 5 |
32 | 4 4 4 4 4 4 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 2.1962.0 GPS week: 1962 Day: 0 MJD: 57978.000
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 273| 0 0 3 -9 -4 19 .07 10 9 | -681 -4 9 96
emr 85| 0 0 -1 20 -4 -8 .19 14 14 | -172 -231 18 144
esa 150| 0 0 -1 -2 13 8 .01 9 9 | -1506 1273 8 144
gfz 197| -1 1 1 -22 4 8 .08 10 9 | -392 -34 13 141
grg 110| 1 1 8 -13 13 -27 -.31 17 16 | 34 -20 16 207
igr n/a| 0 0 1 -3 -2 8 .01 4 4 | -4121 183 13 81
jpl 80| 2 0 -2 30 11 20 .28 11 11 | -187 -591 37 187
mit 349| 0 0 2 19 -12 -1 -.02 13 13 | -297 -95 41 337
ngs 215| 0 0 -3 -13 -3 -13 -.04 9 8 | -732 147 917 1872
sio 348| 1 0 -2 22 0 -6 -.04 12 9 | --- --- --- ---
Table 2.1962.1 GPS week: 1962 Day: 1 MJD: 57979.000
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 274| 1 0 3 33 17 6 .06 9 9 | -576 42 10 95
emr 85| 0 -1 -2 13 0 -3 .19 15 15 | -504 307 17 162
esa 150| 0 0 0 8 7 -4 .03 9 9 | -357 -1573 8 156
gfz 197| -1 2 0 -14 2 6 .16 11 10 | -606 313 11 117
grg 110| 0 1 0 -16 20 -31 -.33 17 15 | -130 97 13 207
igr n/a| 0 0 2 -16 -3 8 .02 4 4 | -4080 929 11 75
jpl 80| 0 -1 -2 10 9 19 .28 15 15 | -932 291 35 188
mit 348| 0 0 3 -19 -28 -11 -.07 12 11 | -643 -19 40 332
ngs 218| 0 0 -5 2 14 0 -.06 9 8 | -569 43 1203 2009
sio 354| 0 0 0 -24 -43 15 -.07 11 11 | --- --- --- ---
Table 2.1962.2 GPS week: 1962 Day: 2 MJD: 57980.000
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 278| 2 0 1 -2 -7 10 .11 10 9 | -745 -183 11 91
emr 85| 0 -2 -2 13 2 -10 .16 15 15 | -113 -1992 20 128
esa 150| 0 0 -2 -1 13 -1 .04 9 10 | -1895 -390 10 156
gfz 199| -2 1 1 4 7 -6 .13 11 11 | -42 -1098 12 93
grg 111| 1 1 3 -34 8 -30 -.36 17 15 | 251 -450 14 191
igr n/a| 0 0 1 -16 -3 15 -.04 5 5 | -3058 -953 14 75
jpl 80| 0 0 -4 20 -15 65 .21 11 11 | 103 -2016 37 207
mit 349| 0 0 0 -14 -29 6 -.08 12 11 | -964 -294 41 302
ngs 221| 0 0 -1 15 8 27 -.06 8 7 | -506 -638 1160 2644
sio 357| 0 -2 0 -9 -7 -8 -.03 12 10 | --- --- --- ---
Table 2.1962.3 GPS week: 1962 Day: 3 MJD: 57981.000
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 278| 1 1 3 -9 -48 0 .05 10 9 | 319 -1558 11 92
emr 85| -1 -2 -4 39 -8 -2 .15 16 16 | -792 -201 23 149
esa 150| 0 0 -2 -14 -3 -7 .01 10 9 | -531 -385 9 155
gfz 200| -1 1 -1 -13 -31 -1 .17 11 10 | -137 200 12 121
grg 110| 1 1 15 -15 11 -2 -.30 19 16 | 303 -79 16 172
igr n/a| 0 0 -1 0 -21 7 .02 4 4 | -2600 510 12 74
jpl 80| 3 -2 -4 51 -20 37 .29 12 12 | -561 -174 38 217
mit 349| 0 0 0 -15 33 4 -.08 12 10 | -486 48 38 333
ngs 223| -1 -1 -6 42 22 38 -.05 10 9 | 235 -1530 820 2213
sio 356| 0 -2 1 -21 33 -21 .02 12 11 | --- --- --- ---
Table 2.1962.4 GPS week: 1962 Day: 4 MJD: 57982.000
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 276| 1 0 1 13 0 6 .01 13 10 | -225 -680 12 107
emr 85| -2 2 0 13 14 14 .16 16 16 | -1174 36 23 139
esa 150| 1 -1 -4 -7 22 -5 .03 12 11 | -1300 -2047 11 174
gfz 203| -1 1 0 -17 -27 0 .16 11 10 | -307 277 13 117
grg 113| 1 0 4 -21 22 -10 -.37 22 14 | 256 -112 14 192
igr n/a| 0 0 -1 -8 -19 -5 .03 6 4 | -2293 385 15 68
jpl 80| 2 1 -1 35 -31 28 .28 12 12 | -1001 72 39 197
mit 349| 0 -1 1 0 -1 7 -.06 13 10 | -344 -96 35 298
ngs 223| -1 0 -1 10 25 9 .00 28 8 | -298 -584 659 1949
sio 351| 0 -1 1 -2 -48 -14 .06 13 12 | --- --- --- ---
Table 2.1962.5 GPS week: 1962 Day: 5 MJD: 57983.000
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 279| 0 0 1 0 -1 -6 .05 10 10 | -773 109 12 107
emr 85| -4 3 1 -2 7 -21 .09 18 18 | -1303 314 23 137
esa 150| 1 -1 -1 -20 3 -1 -.02 10 10 | -201 -1759 8 153
gfz 203| 0 0 0 -5 -24 7 .13 10 9 | -154 134 14 145
grg 114| 2 0 0 -32 4 9 -.32 16 14 | 261 -174 14 204
igr n/a| 0 0 1 -18 -4 9 .00 4 4 | -2321 323 13 69
jpl 80| 0 0 0 16 -10 13 .26 11 11 | -1176 376 39 242
mit 350| 1 0 0 -5 -15 -17 -.11 11 10 | -894 -289 42 315
ngs 223| -1 0 0 13 34 19 .00 9 7 | -778 113 1103 2089
sio 350| 0 -1 -1 35 -22 -17 .08 13 12 | --- --- --- ---
Table 2.1962.6 GPS week: 1962 Day: 6 MJD: 57984.000
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 279| 2 0 1 9 13 2 .00 11 10 | -988 508 11 91
emr 81| -10 6 1 12 17 9 .12 19 19 | -987 668 25 114
esa 150| 0 0 -1 20 -8 3 -.03 10 11 | -2602 1434 9 139
gfz 200| 0 0 0 -5 -8 15 .11 11 9 | -198 117 11 111
grg 104| 0 0 4 -19 -9 27 -.28 18 14 | 48 178 14 157
igr n/a| 0 0 0 -8 -5 9 -.01 4 4 | -2044 606 12 77
jpl 80| 0 -1 0 14 -6 51 .17 13 13 | -802 711 53 215
mit 350| 2 0 -1 4 -23 16 -.07 12 12 | -833 -108 47 291
ngs 222| 0 0 -1 2 7 18 .04 8 7 | -906 398 701 1952
sio 354| 1 -2 0 -32 2 -87 .09 12 11 | --- --- --- ---
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 3.1962.0 GPS week: 1962 Day: 0 MJD: 57978.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 12 5 9 15 4 9 9 8 11 3 | 28 28 28 27 31 25 30 25 26 32 27
2 | 12 11 7 14 19 4 11 14 9 16 4 | 29 29 29 32 31 29 29 32 30 29 28
3 | 9 9 7 8 15 5 9 10 6 8 3 | 29 28 28 28 28 26 28 25 26 27 26
X4 | 2 --- --- --- --- 22 20 --- --- --- 0 | 28 --- --- --- --- 27 27 --- --- --- 27
5 | 8 13 7 8 14 3 11 11 9 13 3 | 34 35 32 37 36 33 32 37 33 32 33
6 | 9 11 7 10 22 3 8 10 5 9 3 | 28 32 29 26 36 27 32 27 25 30 27
7 | 13 11 10 11 14 5 8 12 12 15 4 | 42 45 39 35 39 36 43 32 36 38 37
8 | 6 13 6 8 12 3 9 10 9 9 3 | 23 22 21 21 20 20 23 21 21 21 20
9 | 8 10 9 7 10 5 10 10 10 8 3 | 238 240 235 239 235 237 198 232 229 233 235
10 | 6 13 5 5 12 3 10 9 5 9 3 | 37 36 38 37 39 37 39 38 35 39 36
11 | 6 9 11 9 13 2 10 13 8 9 3 | 31 34 31 33 26 30 34 32 33 26 30
12E | 14 24 7 11 27 5 18 13 12 10 5 | 29 31 35 39 32 35 32 33 38 32 33
13 | 8 10 12 8 10 4 9 12 8 9 3 | 22 28 19 26 21 22 26 31 23 26 23
14 | 8 10 12 10 12 4 10 16 7 15 4 | 37 36 33 35 37 36 35 43 36 38 35
15 | 11 12 11 9 9 4 14 14 10 14 4 | 58 62 59 55 57 56 62 51 58 57 57
16E | 13 27 9 14 26 6 13 19 13 13 6 | 48 47 44 46 49 43 53 43 45 45 44
17 | 9 11 10 13 20 4 9 15 10 14 4 | 24 26 24 28 23 24 27 26 27 22 24
18 | 9 24 8 11 15 5 16 19 10 13 5 | 35 37 34 35 33 33 35 33 35 31 32
19 | 11 17 8 13 19 4 11 15 11 20 5 | 22 28 25 33 24 27 27 26 27 26 24
20 | 10 13 5 8 15 3 14 8 11 10 3 | 87 85 86 89 83 87 85 89 89 90 87
21 | 8 8 10 8 23 4 7 13 9 13 4 | 27 26 26 28 33 27 26 30 25 27 26
22 | 10 9 9 9 19 5 7 17 10 12 4 | 61 60 56 57 60 57 59 58 55 57 57
23 | 11 20 9 12 8 5 14 15 9 14 4 | 34 29 31 35 32 32 29 37 33 34 31
24 | 4 8 12 8 13 3 11 11 9 7 3 | 23 29 29 25 22 24 31 27 23 28 24
25E | 12 16 11 6 26 3 9 9 7 6 4 | 63 61 60 60 66 59 58 60 58 62 60
26E | 15 15 13 17 32 4 10 13 9 9 6 | 344 346 339 343 345 342 224 343 342 341 342
27 | 8 11 8 7 14 3 9 10 6 10 3 | 23 24 24 23 23 22 26 24 24 25 23
28E | 12 9 7 11 26 2 7 11 9 10 4 | 21 25 24 24 27 22 24 22 28 23 22
29 | 8 21 12 11 12 4 15 12 11 14 4 | 23 23 21 29 24 23 23 23 21 27 22
30 | 7 9 8 8 7 4 7 9 9 7 3 | 26 33 30 26 25 27 31 26 27 29 27
31 | 11 16 13 14 12 4 12 13 10 18 5 | 39 46 42 33 42 37 44 35 36 33 38
32 | 8 12 11 10 11 4 13 12 7 12 3 | 35 44 39 42 36 39 43 40 36 42 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 9 10 17 4 11 13 9 12 |T 50 53 51 52 52 50 47 51 50 51 49
WRMS | 9 14 9 9 16 4 11 13 8 9 |NE 39 42 40 40 40 38 39 40 38 40 38
MEDI | 9 12 9 9 14 4 10 12 9 11 |MD 29 33 31 33 33 30 32 32 33 32 30
Table 3.1962.1 GPS week: 1962 Day: 1 MJD: 57979.000
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 4 8 15 2 9 8 8 9 3 | 26 28 29 29 26 27 31 24 28 29 26
2 | 12 13 8 16 17 4 10 13 10 15 4 | 29 32 27 35 29 28 29 32 30 28 28
3 | 8 10 7 7 20 5 10 7 7 8 3 | 24 27 26 26 28 24 29 23 25 26 24
X4 | 3 --- --- --- --- 26 24 --- --- --- 0 | 29 --- --- --- --- 23 28 --- --- --- 27
5 | 10 14 6 9 13 3 11 11 7 12 3 | 34 34 31 38 31 32 34 35 33 31 32
6 | 8 12 6 10 15 3 10 10 6 8 3 | 26 28 25 25 24 24 31 25 24 27 24
7 | 14 15 11 10 12 4 9 12 10 15 4 | 35 37 31 33 29 30 35 27 29 33 30
8 | 9 12 7 7 10 3 10 8 8 9 3 | 25 23 24 24 24 22 28 19 22 23 21
9 | 7 10 9 5 11 3 --- 9 7 8 3 | 219 221 218 221 216 219 --- 217 218 221 219
10 | 8 11 6 8 11 4 10 8 6 7 3 | 30 31 28 31 29 30 34 29 28 31 29
11 | 7 9 12 9 12 2 9 9 6 9 3 | 27 30 29 29 26 27 33 23 27 23 25
12E | 11 31 7 9 17 4 15 11 11 9 5 | 22 24 25 32 22 25 25 27 29 29 25
13 | 8 8 10 9 7 5 7 11 7 8 3 | 23 28 23 30 20 23 30 28 22 27 24
14 | 8 13 12 16 14 5 12 13 8 16 4 | 38 37 36 35 38 35 37 36 37 39 36
15 | 9 14 10 9 12 3 14 13 10 12 4 | 36 39 33 37 35 34 40 33 37 37 34
16E | 10 28 8 14 32 4 52 19 11 11 6 | 46 45 42 44 52 43 77 44 45 44 43
17 | 10 14 11 13 15 4 10 15 10 15 4 | 25 28 23 28 19 24 31 24 26 21 22
18 | 10 28 6 12 18 6 16 16 10 12 5 | 27 36 30 31 31 28 33 25 26 25 26
19 | 13 18 9 15 17 5 12 15 11 19 5 | 19 23 20 27 18 20 24 20 21 19 18
20 | 8 12 5 9 25 3 10 11 8 10 4 | 93 90 90 91 84 90 88 92 90 92 90
21 | 9 9 9 8 21 4 21 14 9 13 4 | 29 27 25 29 32 26 34 27 26 26 26
22 | 11 10 10 10 19 5 9 16 10 11 4 | 56 51 49 48 53 49 52 46 48 48 49
23 | 10 23 10 11 9 3 16 15 9 12 4 | 24 28 26 25 23 22 28 22 24 26 22
24 | 6 11 8 7 10 4 11 11 7 12 3 | 22 28 23 24 23 21 29 27 22 32 24
25E | 8 15 11 12 27 4 9 9 7 12 4 | 50 51 49 54 58 51 50 51 51 53 51
26E | 11 10 14 18 41 3 10 9 13 9 6 | 267 269 265 267 272 268 193 268 271 266 267
27 | 9 13 8 7 8 4 8 8 7 8 3 | 25 25 27 23 24 25 29 22 24 25 23
28E | 14 11 6 10 19 4 8 9 11 8 4 | 21 27 24 26 23 23 27 25 23 25 22
29 | 8 21 11 10 14 4 14 14 8 13 4 | 23 22 20 30 22 22 24 25 22 29 23
30 | 5 11 8 7 8 3 7 7 6 8 2 | 28 32 28 28 23 26 33 22 26 27 26
31 | 9 15 14 12 13 4 11 12 9 14 4 | 31 36 29 29 30 27 34 26 27 30 27
32 | 8 13 10 12 11 4 13 9 8 9 3 | 31 38 35 34 30 33 39 32 35 36 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 9 11 17 4 15 12 9 11 |T 45 47 44 47 44 43 40 44 45 46 43
WRMS | 9 15 9 10 15 4 15 11 8 11 |NE 35 38 35 37 34 34 31 34 35 37 34
MEDI | 9 13 9 10 14 4 10 11 8 11 |MD 28 31 28 30 29 27 33 27 27 29 26
Table 3.1962.2 GPS week: 1962 Day: 2 MJD: 57980.000
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 11 6 11 13 3 10 9 5 10 3 | 25 27 26 20 23 21 28 22 22 29 23
2 | 12 11 7 15 18 6 11 11 10 18 4 | 27 30 28 33 25 29 27 31 30 28 27
3 | 8 9 8 9 17 3 12 6 5 9 3 | 24 25 24 23 26 21 26 22 22 24 22
X4 | 2 --- --- --- --- 21 25 --- --- --- 0 | 39 --- --- --- --- 32 43 --- --- --- 38
5 | 7 12 7 9 13 4 13 9 9 14 3 | 31 31 29 35 29 31 29 32 31 28 30
6 | 7 13 6 12 16 4 11 10 6 10 3 | 24 28 25 21 26 21 27 23 21 25 22
7 | 11 14 12 12 12 4 10 12 10 16 4 | 33 34 30 26 30 26 35 25 27 30 28
8 | 8 16 7 10 11 3 9 10 5 6 3 | 23 24 21 22 20 19 25 19 18 21 19
9 | 8 11 9 7 10 4 11 9 6 9 3 | 75 77 77 77 75 77 133 76 76 72 76
10 | 10 13 10 6 12 3 9 13 7 7 3 | 38 40 37 39 39 39 41 40 38 41 38
11 | 8 12 12 10 10 2 9 10 5 7 3 | 26 30 23 24 22 21 31 23 23 22 23
12E | 10 27 8 10 20 7 16 13 9 10 5 | 17 17 19 20 13 19 16 21 22 22 18
13 | 6 10 10 11 9 4 10 10 8 8 3 | 21 25 19 29 19 21 23 24 20 24 21
14 | 9 13 12 13 11 4 11 14 7 16 4 | 28 28 27 27 28 28 27 30 29 28 26
15 | 8 13 11 10 12 5 13 14 9 12 4 | 40 44 40 39 40 37 46 37 39 42 39
16E | 13 29 9 14 22 6 14 18 10 15 6 | 40 44 38 42 41 39 32 40 39 37 38
17 | 8 12 9 13 18 5 10 16 9 17 4 | 24 26 21 25 17 20 27 23 24 23 21
18 | 12 27 9 10 20 7 13 17 10 13 5 | 30 36 30 29 34 27 31 25 28 27 27
19 | 9 17 9 14 18 6 12 16 11 19 5 | 19 27 21 25 15 18 23 19 18 20 18
20 | 20 12 8 9 24 8 12 10 9 9 5 | 131 132 129 135 127 128 128 130 130 130 130
21 | 9 12 8 8 25 5 8 13 9 14 4 | 27 25 24 27 34 24 25 25 26 22 24
22 | 12 11 8 11 19 5 12 15 8 10 4 | 54 54 50 52 55 50 50 48 50 47 50
23 | 10 23 11 10 10 5 17 15 8 13 4 | 31 29 29 31 29 27 27 28 30 29 28
24 | 9 11 10 6 8 3 9 12 5 11 3 | 21 26 21 21 18 18 24 23 18 24 20
25E | 9 15 14 11 32 7 10 9 7 8 5 | 41 46 46 46 44 46 40 44 45 44 43
26E | 9 12 13 16 30 5 12 15 15 10 5 | 263 261 258 259 262 262 153 267 262 263 262
27 | 8 14 8 6 10 4 11 8 5 9 3 | 24 24 23 21 21 20 28 20 20 26 21
28E | 15 16 7 11 22 7 7 9 7 11 4 | 22 28 24 23 25 25 23 26 27 21 22
29 | 7 20 11 10 19 7 15 12 10 11 4 | 24 23 17 24 23 21 22 24 23 25 21
30 | 9 10 7 7 11 3 10 7 6 8 3 | 22 25 23 22 20 21 28 21 24 25 21
X31 | 10 16 11 --- 18 7 11 17 12 --- 6 | 64 67 65 --- 61 62 65 65 63 --- 63
32 | 7 12 11 6 9 3 8 11 8 11 3 | 32 33 29 25 25 26 33 28 29 33 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 9 11 17 5 11 12 8 12 |T 41 44 41 41 40 39 41 41 41 41 40
WRMS | 9 15 10 11 15 5 11 11 7 10 |NE 30 32 29 28 28 28 35 29 29 29 29
MEDI | 9 13 9 10 16 5 11 12 8 10 |MD 27 29 27 26 26 26 28 25 27 27 26
Table 3.1962.3 GPS week: 1962 Day: 3 MJD: 57981.000
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 9 6 11 15 4 10 6 7 12 3 | 34 36 37 32 40 33 42 35 36 42 35
2 | 14 11 8 18 18 6 13 11 11 20 5 | 32 32 32 37 38 31 29 33 35 34 31
3 | 10 10 7 8 14 3 11 8 9 9 3 | 31 32 31 33 37 29 33 33 30 34 31
X4 | 3 --- --- --- --- 46 16 --- --- --- 0 | 24 --- --- --- --- 26 26 --- --- --- 23
5 | 10 12 8 7 12 4 14 9 8 15 4 | 34 34 35 38 40 35 31 39 35 35 35
6 | 11 12 6 13 20 4 11 10 5 11 4 | 31 30 31 28 37 29 33 27 29 34 29
7 | 11 14 11 10 10 3 10 11 12 13 4 | 40 46 38 37 35 37 42 34 35 37 36
8 | 8 12 8 6 11 3 9 8 8 7 3 | 27 26 24 25 25 24 30 25 24 27 24
9 | 8 13 11 6 7 2 9 11 13 9 4 | 82 87 83 85 84 83 53 87 89 87 84
10 | 9 15 9 8 13 4 8 7 9 9 3 | 27 27 29 30 34 27 31 29 29 34 28
11 | 8 11 13 10 13 4 12 8 8 12 4 | 29 34 29 30 30 29 37 29 30 28 28
12E | 13 28 10 11 21 4 14 12 12 9 5 | 22 25 24 30 25 24 25 28 32 30 25
13 | 11 11 10 10 10 5 10 8 9 8 3 | 29 34 27 36 29 28 30 33 28 33 30
14 | 8 14 13 18 12 4 11 15 9 17 5 | 32 28 29 33 33 31 31 33 34 36 30
15 | 10 16 12 10 16 4 15 12 13 13 4 | 47 52 49 47 46 47 53 44 50 47 46
16E | 12 23 9 12 28 3 11 15 12 11 5 | 42 41 41 42 43 40 43 41 45 41 40
17 | 10 15 10 12 21 5 11 14 9 17 5 | 28 28 27 30 29 27 32 27 31 27 27
18 | 11 28 8 13 25 7 16 15 10 11 5 | 39 40 36 39 52 35 40 33 35 34 35
19 | 11 21 9 16 18 6 14 14 11 21 5 | 21 27 24 31 26 24 27 22 24 27 23
20E | 10 12 6 8 13 4 12 9 9 8 3 | 94 92 92 97 89 94 89 94 91 94 93
21 | 9 10 8 9 25 5 9 12 10 14 4 | 30 30 29 32 40 29 30 32 28 30 29
22 | 10 9 8 11 19 4 10 13 11 10 4 | 60 58 57 61 68 57 61 58 57 59 58
23 | 9 25 11 11 8 5 14 15 12 14 5 | 37 34 35 42 39 37 32 40 35 40 36
24 | 8 10 9 8 10 3 9 9 7 6 3 | 26 29 30 26 26 26 32 26 29 30 27
25E | 9 12 12 12 39 3 13 7 11 8 5 | 35 39 39 37 42 37 37 38 42 39 37
26E | 15 11 16 12 47 5 15 15 18 11 7 | 202 196 193 195 202 195 328 197 199 194 197
27 | 8 11 7 5 15 2 8 10 6 8 3 | 29 28 27 27 28 26 32 27 26 32 27
28E | 18 19 7 12 20 4 9 11 10 12 5 | 29 36 34 34 33 32 33 32 34 36 31
29 | 8 24 12 11 19 4 17 17 13 11 5 | 28 28 23 32 27 24 26 29 23 30 25
30 | 7 11 6 8 8 3 8 9 6 12 3 | 26 31 29 30 24 27 31 27 27 33 27
31 | 10 15 14 15 12 6 14 13 10 12 4 | 41 46 40 53 40 38 46 35 39 54 38
32 | 6 11 11 12 10 3 15 11 8 11 3 | 29 28 28 26 31 27 37 30 26 34 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 10 11 19 4 12 12 10 12 |T 41 43 41 43 44 40 46 41 42 44 40
WRMS | 9 16 9 10 16 4 12 10 9 11 |NE 33 35 33 35 35 32 34 33 33 36 32
MEDI | 10 12 9 11 15 4 11 11 10 11 |MD 31 34 31 33 37 29 32 33 34 34 30
Table 3.1962.4 GPS week: 1962 Day: 4 MJD: 57982.000
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 7 8 8 3 10 5 7 12 3 | 77 78 82 77 79 76 79 75 79 80 78
2 | 14 11 10 13 24 5 13 13 11 19 5 | 72 71 71 79 71 72 70 72 78 74 72
3 | 8 11 6 9 15 3 10 6 6 13 3 | 73 72 74 76 80 73 72 72 76 73 74
X4 | 1 --- --- --- --- 36 25 --- --- --- 0 | 63 --- --- --- --- 55 66 --- --- --- 64
5 | 10 12 10 9 15 3 11 12 8 14 4 | 71 70 68 74 71 71 68 72 73 68 71
6 | 7 17 6 8 21 3 14 9 9 9 4 | 70 70 71 73 74 69 69 67 71 70 70
7 | 13 14 12 9 9 4 12 13 10 14 4 | 78 83 80 79 77 77 81 76 77 76 78
8 | 8 11 9 7 7 3 10 7 7 10 3 | 69 72 69 68 71 69 72 66 72 69 69
9 | 10 11 11 4 9 4 9 9 6 10 3 | 134 136 133 135 133 134 118 130 151 134 134
10 | 9 12 8 11 20 4 11 9 6 7 3 | 72 72 74 69 78 72 74 71 74 72 72
11 | 7 9 15 9 9 3 10 9 7 13 4 | 74 73 76 70 74 72 75 68 73 68 72
12E | 13 26 9 11 19 5 14 9 14 11 5 | 77 80 83 87 78 81 79 80 84 82 81
13 | 8 12 12 8 7 3 9 9 9 10 3 | 63 63 62 67 62 64 66 64 66 64 64
14 | 5 15 14 16 13 5 11 12 10 18 5 | 76 77 77 79 76 77 76 78 81 76 77
15 | 11 14 13 11 12 2 13 11 10 16 4 | 73 71 75 72 73 72 75 69 75 72 72
16E | 11 27 9 10 27 4 19 10 9 12 5 | 72 73 74 73 72 71 72 70 72 70 71
17 | 9 17 10 10 17 4 11 15 10 15 4 | 71 68 73 74 72 71 74 68 74 71 71
18 | 11 25 9 12 20 7 16 18 9 12 5 | 86 89 88 86 90 84 89 81 87 84 85
19 | 10 23 9 11 21 5 14 15 12 21 5 | 69 68 73 74 72 69 70 63 69 69 69
20E | 13 10 9 9 18 3 9 8 8 13 4 | 83 85 85 87 84 85 84 85 87 82 85
21 | 8 11 9 9 25 4 9 10 8 17 4 | 71 74 74 75 78 71 73 71 74 72 73
22 | 8 11 10 8 14 6 11 14 8 11 4 | 110 108 107 107 108 106 107 103 110 105 107
23 | 13 25 13 9 9 5 12 15 9 15 5 | 70 70 72 72 72 70 68 72 73 70 71
24 | 6 11 11 8 7 4 11 8 6 11 3 | 68 67 70 70 70 66 69 64 68 67 68
25E | 9 13 13 8 34 5 19 7 10 12 5 | 78 79 82 83 82 79 84 79 82 81 80
26E | 47 21 29 28 80 25 --- 38 152 21 15 | 650 643 640 640 655 646 --- 651 635 646 645
27 | 9 12 10 6 10 4 10 7 7 9 3 | 68 72 69 70 73 69 71 66 70 68 69
28E | 8 18 8 8 14 2 11 8 9 11 4 | 73 69 74 72 73 71 73 70 75 72 72
29 | 9 21 11 12 18 4 14 16 10 10 5 | 69 67 66 73 70 68 67 69 71 67 69
30 | 6 12 9 7 7 3 11 6 6 9 3 | 70 74 74 74 71 72 75 67 72 70 71
31 | 9 14 15 12 14 5 14 10 9 13 4 | 72 75 73 69 73 70 75 68 72 66 71
32 | 16 10 14 9 11 4 12 8 8 11 4 | 74 71 73 72 69 71 75 71 77 73 72
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 16 12 11 22 6 12 13 28 13 |T 93 94 95 96 96 92 76 92 96 93 93
WRMS | 10 16 11 10 14 4 12 10 8 12 |NE 73 74 75 75 75 73 74 72 76 73 73
MEDI | 9 12 10 9 14 4 11 9 9 12 |MD 72 72 74 74 73 71 74 71 74 72 72
Table 3.1962.5 GPS week: 1962 Day: 5 MJD: 57983.000
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 13 4 6 14 2 9 6 7 8 3 | 132 134 137 135 136 135 137 130 138 134 134
X2 | 13 15 10 --- 18 7 10 16 12 --- 6 | 126 121 122 --- 126 124 128 120 126 --- 123
3 | 9 18 9 8 12 3 9 7 6 8 3 | 132 131 134 133 135 132 132 127 134 132 132
X4 | 1 --- --- --- --- 48 15 --- --- --- 0 | 132 --- --- --- --- 123 135 --- --- --- 132
5 | 9 13 9 9 24 3 13 9 7 13 4 | 133 134 135 138 135 135 136 132 136 132 134
6 | 8 23 9 7 13 4 11 14 6 9 4 | 133 130 133 134 134 131 134 128 131 131 131
7 | 13 16 11 9 12 5 10 13 8 14 4 | 138 139 137 137 137 135 138 134 135 133 136
8 | 9 12 6 4 11 2 8 7 7 8 3 | 128 129 127 127 129 127 130 122 128 124 126
X9 | 6 13 9 4 7 4 8 11 --- 11 3 | 133 134 133 135 132 133 136 133 --- 133 133
10 | 8 12 8 7 20 3 9 9 5 9 3 | 139 139 139 140 144 138 140 132 141 136 138
11 | 6 15 14 7 13 4 9 8 6 11 3 | 127 128 129 127 130 127 131 122 131 125 127
12E | 16 28 6 11 18 5 16 10 10 13 5 | 124 123 125 130 127 126 126 123 130 125 126
13 | 9 14 11 9 9 4 10 9 8 11 3 | 122 121 123 129 121 123 125 123 124 123 123
14 | 8 19 14 12 17 5 8 15 9 13 5 | 132 130 131 133 130 130 133 127 131 130 130
15 | 10 15 13 9 10 4 14 10 9 14 4 | 127 126 130 131 126 127 129 126 130 125 128
16E | 18 29 8 14 19 4 14 12 11 14 5 | 135 135 135 139 131 134 138 132 133 134 134
17 | 13 14 14 13 15 5 8 16 8 17 5 | 130 128 131 130 130 130 133 124 133 129 129
18E | 8 21 8 13 22 8 14 13 8 10 4 | 146 145 146 148 148 145 146 136 147 140 144
19 | 15 25 11 14 18 6 13 17 10 23 6 | 129 125 128 131 129 128 131 122 129 129 128
20E | 11 13 7 10 14 5 10 9 7 11 3 | 145 148 146 151 144 145 147 144 146 143 146
21 | 10 13 7 11 20 5 13 12 8 17 4 | 134 136 135 138 139 133 139 131 135 133 134
22E | 9 14 7 10 16 5 10 10 8 9 3 | 142 141 144 143 145 142 145 137 145 141 142
23 | 12 25 11 9 9 5 14 15 9 15 5 | 132 133 132 132 130 130 132 130 132 129 131
24 | 8 12 11 8 9 3 8 7 5 13 3 | 124 120 126 125 125 123 126 119 125 120 123
25E | 12 15 16 9 28 4 --- 10 13 7 5 | 135 129 131 139 140 134 --- 131 140 133 134
26E | 9 22 12 14 19 8 --- 14 17 11 5 | 411 419 408 409 414 411 --- 412 417 407 410
27 | 10 9 7 5 13 3 8 8 9 8 3 | 132 131 134 132 132 131 135 128 132 130 131
28E | 8 23 7 8 11 3 12 10 7 11 3 | 130 130 131 133 130 131 133 129 136 131 131
29 | 12 24 11 13 13 5 15 16 10 19 5 | 127 126 127 132 129 129 132 127 131 133 128
30 | 6 14 8 8 6 4 9 7 6 8 3 | 133 133 133 135 132 132 136 130 133 131 132
31 | 10 14 12 11 15 4 13 10 9 13 4 | 139 138 140 137 139 139 142 136 139 137 138
32 | 8 15 11 7 14 3 10 7 6 11 3 | 135 134 137 137 134 135 140 132 138 135 135
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 10 10 16 4 11 11 9 13 |T 141 140 141 144 142 140 134 138 143 140 140
WRMS | 10 18 10 9 14 4 11 10 7 12 |NE 131 130 131 132 131 130 133 127 132 130 130
MEDI | 9 15 9 9 14 4 10 10 8 11 |MD 132 131 133 134 132 131 134 130 133 132 132
Table 3.1962.6 GPS week: 1962 Day: 6 MJD: 57984.000
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 13 6 7 11 3 9 7 4 8 2 | 186 186 188 187 187 184 189 182 187 189 186
2 | 13 16 9 15 18 6 11 16 8 20 5 | 181 179 180 182 180 178 182 177 180 178 179
3 | 8 17 9 6 13 5 15 7 7 7 3 | 185 182 187 185 181 184 182 181 186 187 184
X4 | 1 --- --- --- --- 41 26 --- --- --- 0 | 191 --- --- --- --- 174 183 --- --- --- 190
5E | 8 15 8 7 26 6 14 12 6 10 4 | 192 187 190 195 195 190 190 188 193 190 190
6 | 7 22 7 7 14 2 12 15 5 7 4 | 187 184 187 187 189 185 186 183 188 188 186
7 | 13 16 14 10 14 4 10 13 11 13 5 | 194 193 195 190 189 190 193 187 192 190 190
8 | 8 13 8 5 10 3 8 8 7 8 3 | 178 179 180 180 180 178 181 174 182 182 179
9 | 10 17 12 6 9 3 8 10 6 10 3 | 194 195 196 197 192 195 188 194 186 197 195
10 | 7 14 9 9 16 3 15 11 6 7 3 | 196 198 198 195 194 195 198 187 198 199 195
11 | 6 16 14 9 11 3 10 9 8 13 4 | 177 176 176 176 177 175 179 173 177 179 176
12E | 12 33 8 12 26 5 15 13 8 10 5 | 178 177 179 183 178 178 180 178 184 183 179
13 | 8 15 13 9 7 4 9 10 8 8 3 | 183 179 178 186 175 178 180 179 181 182 180
14 | 10 15 13 15 15 5 15 14 9 13 5 | 182 181 183 181 181 181 186 178 186 183 181
15 | 12 14 11 11 12 4 12 14 9 13 4 | 188 188 188 188 187 187 189 183 191 187 187
16E | 21 27 7 15 19 4 22 14 8 10 5 | 199 192 193 195 191 193 199 192 196 197 194
17 | 12 14 13 12 15 4 10 13 8 14 4 | 186 184 187 186 185 184 187 180 186 186 184
18E | 9 23 10 12 16 7 15 15 9 12 4 | 188 191 189 189 188 186 191 176 192 182 186
19 | 12 23 10 15 19 5 12 15 9 19 5 | 182 181 183 186 183 182 185 177 183 185 182
20E | 9 14 7 9 19 5 10 10 9 10 4 | 206 208 204 210 203 205 206 202 209 206 205
21 | 8 15 10 10 22 4 22 17 8 16 5 | 188 189 188 190 188 185 181 182 189 187 187
22E | 9 15 10 10 14 4 11 10 8 7 3 | 205 204 205 206 205 203 208 201 206 203 204
23 | 14 26 11 10 11 3 15 16 9 15 5 | 190 184 189 189 188 187 189 189 190 188 188
24 | 8 14 10 8 8 2 8 9 7 10 3 | 176 177 180 181 178 176 179 173 179 180 177
25E | 15 36 13 8 58 6 12 10 14 13 8 | 183 201 186 191 187 186 191 187 189 192 187
26E | 10 20 12 19 16 9 19 13 13 10 5 | 372 361 365 365 367 364 320 370 368 370 368
27 | 9 14 6 7 8 4 9 9 8 8 3 | 183 184 185 184 185 182 187 179 187 185 183
28E | 14 19 8 9 15 3 9 10 10 9 4 | 181 186 185 186 190 184 185 182 188 186 184
29 | 7 24 11 15 19 5 15 15 9 14 5 | 179 180 178 183 177 179 182 178 181 183 179
30 | 8 15 11 6 8 3 9 6 7 11 3 | 187 190 191 190 187 189 190 185 191 190 188
31 | 11 16 14 11 16 6 12 10 10 11 4 | 203 201 202 196 196 200 205 198 205 200 201
32 | 6 13 10 9 10 4 11 9 6 8 3 | 191 192 194 191 191 191 194 188 197 194 192
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 19 10 11 18 4 13 12 8 12 |T 193 193 193 194 192 191 192 189 195 194 192
WRMS | 10 19 11 9 14 4 13 12 7 11 |NE 186 185 186 186 185 184 186 182 187 187 185
MEDI | 9 16 10 9 15 4 12 11 8 10 |MD 187 186 188 188 187 185 187 182 188 187 186
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 4.1962 GPS week: 1962 MJD: 57978.0-57984.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 |U 9 10 27 |U 6 7 26 |U 9 10 23 |
emr | emr 2974 |U 10 13 29 |U 7 8 28 |U 10 12 21 |
esa | esa 2976 | 9 11 27 |U 7 8 27 | 10 10 22 |
gfz | gfz 2948 |U 11 12 26 |U 7 8 27 |U 11 10 28 |
grg | grg 2973 |U 10 11 29 |U 9 10 32 | 10 9 27 |
igr | igr 2973 | 10 11 27 | 6 7 26 | 10 10 21 |
igs | igs 2973 | 9 10 26 | 6 7 26 | 10 9 22 |
jpl | jpl 3017 | 10 13 28 |U 7 8 26 |U 11 12 25 |
mit | mit 2976 | 11 12 32 |U 9 10 34 |U 11 11 27 |
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 5.1962.0 GPS week: 1962 Day: 0 MJD: 57978.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 4 3 12 | 5 6 19 | 9 11 27 |
emr | emr 2976 | 6 6 13 | 5 7 21 | 9 14 23 |
esa | esa 2976 | 5 5 12 | 4 7 18 | 10 11 26 |
gfz | gfz 2976 | 5 4 11 | 4 5 19 | 10 11 27 |
grg | grg 2976 | 5 4 13 | 6 7 18 | 11 12 33 |
igr | igr 2976 | 5 4 12 | 4 5 18 | 10 11 26 |
igs | igs 2976 | 5 4 11 | 4 5 17 | 9 11 26 |
jpl | jpl 3072 | 6 5 15 | 5 7 22 | 9 13 26 |
mit | mit 2976 | 7 6 26 | 5 6 18 | 12 11 32 |
Table 5.1962.1 GPS week: 1962 Day: 1 MJD: 57979.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 11 17 | 7 7 25 | 7 8 17 |
emr | emr 2976 | 8 15 19 | 6 7 24 | 7 12 16 |
esa | esa 2976 | 7 12 15 | 7 7 24 | 8 8 15 |
gfz | gfz 2976 | 7 11 15 | 7 7 21 | 9 8 18 |
grg | grg 2976 | 8 15 19 | 8 9 38 | 9 9 18 |
igr | igr 2976 | 7 11 15 | 7 6 22 | 8 8 15 |
igs | igs 2976 | 7 12 15 | 6 6 22 | 8 8 16 |
jpl | jpl 2976 | 8 16 23 | 7 7 24 | 9 11 16 |
mit | mit 2976 | 7 13 18 | 7 9 27 | 8 10 19 |
Table 5.1962.2 GPS week: 1962 Day: 2 MJD: 57980.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 8 8 34 | 3 5 17 | 7 8 21 |
emr | emr 2971 | 8 12 39 | 5 5 21 | 7 9 19 |
esa | esa 2976 | 9 9 41 | 3 4 17 | 7 7 22 |
gfz | gfz 2880 | 14 11 28 | 4 4 19 | 7 6 21 |
grg | grg 2969 | 11 11 44 | 13 10 30 | 8 7 30 |
igr | igr 2963 | 10 10 41 | 3 4 16 | 7 8 21 |
igs | igs 2962 | 9 9 40 | 3 3 17 | 7 7 22 |
jpl | jpl 3072 | 8 11 34 | 4 6 22 | 8 9 24 |
mit | mit 2976 | 9 9 39 | 12 7 41 | 8 10 27 |
Table 5.1962.3 GPS week: 1962 Day: 3 MJD: 57981.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 7 10 19 | 5 6 21 | 8 8 17 |
emr | emr 2976 | 7 14 22 | 6 7 20 | 7 11 14 |
esa | esa 2976 | 7 10 17 | 7 8 19 | 8 8 14 |
gfz | gfz 2976 | 7 9 17 | 5 8 21 | 9 7 17 |
grg | grg 2976 | 7 10 18 | 6 7 18 | 10 8 19 |
igr | igr 2976 | 7 10 16 | 5 7 19 | 9 8 14 |
igs | igs 2976 | 7 10 17 | 5 7 18 | 8 7 15 |
jpl | jpl 3072 | 9 13 21 | 6 8 20 | 9 11 17 |
mit | mit 2976 | 8 11 20 | 10 12 32 | 9 8 15 |
Table 5.1962.4 GPS week: 1962 Day: 4 MJD: 57982.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 9 9 36 | 4 7 20 | 7 8 20 |
emr | emr 2976 | 11 11 33 | 6 7 28 | 8 8 21 |
esa | esa 2976 | 10 8 33 | 5 8 21 | 8 7 21 |
gfz | gfz 2976 | 10 8 35 | 5 8 23 | 9 7 20 |
grg | grg 2976 | 11 8 38 | 5 8 21 | 8 7 24 |
igr | igr 2975 | 10 7 36 | 4 7 23 | 8 8 21 |
igs | igs 2976 | 10 8 34 | 4 7 21 | 7 7 20 |
jpl | jpl 2976 | 9 12 34 | 6 9 24 | 8 8 21 |
mit | mit 2976 | 10 9 36 | 6 8 23 | 7 8 22 |
Table 5.1962.5 GPS week: 1962 Day: 5 MJD: 57983.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 14 17 34 | 9 9 38 | 13 12 28 |
emr | emr 2971 | 13 20 38 | 10 9 40 | 14 10 23 |
esa | esa 2976 | 13 18 33 | 9 11 41 | 13 12 27 |
gfz | gfz 2880 | 14 25 37 | 11 9 39 | 22 20 48 |
grg | grg 2970 | 13 17 33 | 11 11 42 | 12 11 30 |
igr | igr 2969 | 13 18 33 | 9 9 41 | 12 11 27 |
igs | igs 2971 | 13 18 32 | 10 9 40 | 13 12 28 |
jpl | jpl 2880 | 14 19 37 | 12 13 42 | 17 13 37 |
mit | mit 2976 | 16 18 42 | 11 20 47 | 17 13 39 |
Table 5.1962.6 GPS week: 1962 Day: 6 MJD: 57984.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 15 14 34 | 11 11 41 | 14 14 30 |
emr | emr 2976 | 16 13 37 | 13 12 46 | 20 18 32 |
esa | esa 2976 | 16 13 36 | 12 12 48 | 15 15 32 |
gfz | gfz 2976 | 18 17 41 | 12 12 49 | 14 14 41 |
grg | grg 2973 | 16 14 35 | 13 16 60 | 14 13 35 |
igr | igr 2976 | 16 14 37 | 11 11 46 | 14 14 28 |
igs | igs 2976 | 15 12 33 | 12 12 47 | 14 14 28 |
jpl | jpl 3072 | 17 15 33 | ---- ---- ---- | 16 16 30 |
mit | mit 2976 | 20 16 42 | 13 12 52 | 18 14 38 |
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 6.1962 GPS week: 1962 MJD: 57978.500-57984.500
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 | 21 3 14 209 -2 | 18 22
| 19 15 65 127 4 | 1
emr uuuuu | -19 -12 96 -97 -2 | 19 29
| 22 9 163 74 16 | 4
esa uuuuu | -7 -1 85 86 2 | 26 29
| 9 13 23 35 4 | 2
gfz uuuuu | -6 6 120 -163 3 | 34 37
| 18 19 85 138 8 | 2
grg uuuuu | -10 7 -46 -29 2 | 1 13
| 15 14 47 83 2 | 2
igr xxxxx | 2 19 34 -32 5 | -2 13
| 11 16 39 51 3 | 2
irf xxxxx | -2 0 -34 -41 -3 | 0 14
| 10 14 20 22 4 | 2
jpl xxxxx | 0 -2 -1 -10 9 | 38 41
| 30 32 75 44 13 | 4
mit uuuuu | -3 9 -74 -91 -4 | 30 33
| 15 14 50 33 4 | 1
ngs uuuuu | -22 -16 -52 -105 -8 | 19 24
| 23 41 105 161 8 | 4
sio uuuux | 44 9 -144 119 16 | 64 67
| 11 18 61 46 4 | 7
Table 7.1962.0 GPS week: 1962 Day: 0 MJD: 57978.500
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 | 33 3 -7 362 -6 | 20 24
emr uuuuu | -27 -16 -16 -119 12 | 15 28
esa uuuuu | -13 0 61 146 0 | 26 30
gfz uuuuu | -15 1 105 -219 -14 | 35 38
grg uuuuu | -13 -23 24 -5 4 | 1 14
igr xxxxx | -11 2 30 -62 2 | -3 14
irf xxxxx | -9 -26 -13 -40 1 | -1 16
jpl xxxxx | -38 -20 -50 9 8 | 34 37
mit uuuuu | -8 0 -50 -99 0 | 29 33
ngs uuuuu | 1 7 -1 -249 -15 | 26 30
sio uuuux | 22 11 -162 82 14 | 56 59
Table 7.1962.1 GPS week: 1962 Day: 1 MJD: 57979.500
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 -20 77 197 1 | 18 23
emr uuuuu | -45 -11 -29 -38 14 | 16 28
esa uuuuu | -3 -13 104 83 2 | 25 30
gfz uuuuu | -5 3 229 -118 2 | 33 37
grg uuuuu | -1 8 -63 63 -1 | 0 14
igr xxxxx | 1 44 -20 -57 10 | -4 14
irf xxxxx | -2 1 -18 -13 1 | -1 16
jpl xxxxx | -25 38 -86 -8 26 | 34 37
mit uuuuu | -8 -5 -34 -66 -1 | 30 33
ngs uuuuu | 5 32 -189 -221 -15 | 24 29
sio uuuux | 41 4 -136 101 22 | 58 61
Table 7.1962.2 GPS week: 1962 Day: 2 MJD: 57980.500
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 | 15 -6 -1 207 3 | 17 22
emr uuuuu | -13 -14 -65 -7 14 | 17 29
esa uuuuu | -8 -7 51 79 0 | 24 29
gfz uuuuu | -36 -26 203 -282 1 | 32 36
grg uuuuu | -10 20 -81 94 2 | -1 14
igr xxxxx | -7 28 -7 -64 5 | -4 14
irf xxxxx | 4 7 -9 -24 -5 | -1 16
jpl xxxxx | 10 -30 98 12 7 | 35 39
mit uuuuu | 9 11 0 -102 -9 | 29 33
ngs uuuuu | -8 18 -103 -99 -18 | 20 27
sio uuuux | 48 3 -37 117 14 | 60 62
Table 7.1962.3 GPS week: 1962 Day: 3 MJD: 57981.500
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 | 56 23 129 350 -7 | 16 21
emr uuuuu | -43 -22 55 -212 -3 | 18 31
esa uuuuu | 4 12 95 29 2 | 23 26
gfz uuuuu | -17 8 111 -284 5 | 32 35
grg uuuuu | -37 7 -81 -64 6 | -2 13
igr xxxxx | -3 5 74 -80 6 | -4 14
irf xxxxx | -7 -6 -44 -81 -1 | -1 15
jpl xxxxx | 9 -38 -51 -49 18 | 36 40
mit uuuuu | 8 1 -102 -126 -5 | 28 32
ngs uuuuu | -55 -29 -146 -26 -8 | 17 21
sio uuuux | 52 -8 -122 137 15 | 62 65
Table 7.1962.4 GPS week: 1962 Day: 4 MJD: 57982.500
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 -6 -51 -20 -3 | 18 22
emr uuuuu | -8 6 95 -66 -18 | 23 30
esa uuuuu | -25 -1 82 103 11 | 26 28
gfz uuuuu | 7 38 1 -208 10 | 33 36
grg uuuuu | -8 4 -78 -63 2 | 1 12
igr xxxxx | 23 4 84 66 6 | -1 12
irf xxxxx | 11 2 -46 -31 0 | 2 13
jpl xxxxx | 54 -17 0 34 19 | 41 44
mit uuuuu | 8 13 -81 -32 0 | 31 33
ngs uuuuu | -22 -43 111 161 -4 | 17 22
sio uuuux | 53 5 -134 49 20 | 68 70
Table 7.1962.5 GPS week: 1962 Day: 5 MJD: 57983.500
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 | 25 12 -25 168 1 | 18 22
emr uuuuu | -13 -7 378 -174 -22 | 23 30
esa uuuuu | -1 18 84 72 -2 | 27 29
gfz uuuuu | 0 1 28 -150 5 | 35 37
grg uuuuu | -13 12 -62 -119 4 | 2 11
igr xxxxx | 3 22 50 -4 1 | 0 11
irf xxxxx | 8 21 -50 -48 -11 | 2 12
jpl xxxxx | 4 15 -24 22 -4 | 43 46
mit uuuuu | 2 38 -104 -91 -10 | 31 33
ngs uuuuu | -31 -88 30 -10 -1 | 16 21
sio uuuux | 38 48 -237 175 12 | 71 73
Table 7.1962.6 GPS week: 1962 Day: 6 MJD: 57984.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 10 13 -25 200 -2 | 19 23
emr uuuuu | 16 -19 254 -65 -13 | 23 30
esa uuuuu | -2 -18 116 88 2 | 28 30
gfz uuuuu | 21 17 162 116 9 | 36 39
grg uuuuu | 12 18 19 -110 1 | 4 14
igr xxxxx | 7 28 25 -22 4 | 2 12
irf xxxxx | -18 2 -57 -54 -7 | 2 12
jpl xxxxx | -16 37 107 -89 -9 | 44 47
mit uuuuu | -33 5 -147 -123 -4 | 30 33
ngs uuuuu | -47 -12 -70 -290 2 | 16 20
sio uuuux | 52 -2 -181 172 15 | 75 77
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