[IGSREPORT-25503] Wk 1964 IGS Final Orbits
acc
acc at igs.org
Thu Sep 14 18:55:57 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1964 (Aug 27, 2017 - Sep 02, 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:
igs1964[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1964[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1964[0-6].cls IGS GPS clock combination summary report.
igs19647.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19647.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 | HARB PALM FAA1 HARB PALM
0 | ESA | AREQ AREQ
0 | GFZ | DGAR MAL2 TRO1 DGAR FAA1 MAL2 PIE1 TRO1
0 | GRG | DAEJ GLSV LMMF MAL2 SEYG SYOG TRO1 DAEJ GLSV LMMF
0 | GRG | MAL2 REUN SEYG SYOG TRO1
1 | COD | PALM TIXI TLSE PALM TIXI
1 | ESA | AREQ FAA1 MAR6 TLSE AREQ FAA1 MAR6
1 | GFZ | FAA1 MAL2 YELL FAA1 MAL2 THTI TRO1 YELL
1 | GRG | DAEJ DGAR GLSV MAL2 RABT SEYG SYOG TRO1 XMIS DAEJ
1 | GRG | DGAR GLSV MAL2 RABT SEYG SYOG TRO1 XMIS
1 | MIT | 29 29 DGAR DGAR
2 | COD | PALM TIXI PALM REUN TIXI
2 | EMR | HERS WHIT HERS
2 | ESA | AREQ CHUR DGAR MAL2 WHIT AREQ CHUR DGAR MAL2
2 | GFZ | NTUS NTUS
2 | GRG | 5 13 5 13 CHTI DAEJ GLSV MAL2 NLIB SYOG TRO1 CHTI
2 | GRG | DAEJ GLSV MAL2 NLIB PIE1 REUN SYOG TRO1
3 | COD | PALM TIXI PALM TIXI
3 | EMR | HERS
3 | ESA | AREQ MAL2 ABMF AREQ CHTI MAL2
3 | GFZ | GMSD GODE KOUR TRO1 GMSD GODE KOUR TRO1
3 | GRG | DAEJ FAA1 GLSV SYOG TRO1 DAEJ GLSV LPGS REUN SYOG
3 | GRG | TRO1
4 | COD | LHAZ MAL2 PALM TRO1 LHAZ MAL2 PALM
4 | EMR | GODE HERS MCM4 WHIT GODE HERS MCM4 WHIT
4 | ESA | DGAR FAA1 SCUB COCO DGAR FAA1 MAC1 SCUB
4 | GFZ | ABMF NYA1
4 | GRG | CCJ2 GLSV GODE MAL2 MAW1 SYOG TRO1 DAEJ GLSV GODE
4 | GRG | MAL2 MAW1 SYOG
4 | JPL | WHIT
4 | MIT | COCO DGAR NYA1 COCO DGAR NYA1
5 | COD | 18 22 18 22 DGAR LHAZ PALM PDEL TIXI DGAR LHAZ PALM
5 | COD | PDEL SFER TIXI
5 | EMR | FAIR HERS FAIR HERS SFER
5 | ESA | AREQ AUCK FAA1 KOUR MAL2 AREQ
5 | GFZ | ALBH
5 | GRG | DAEJ DGAR FAA1 GLSV LHAZ NICO SHAO SYOG ALRT DAEJ
5 | GRG | DGAR FAA1 GLSV LHAZ NICO SYOG
5 | JPL | DGAR DGAR
5 | MIT | DGAR LHAZ PDEL DGAR LHAZ PDEL
6 | COD | FAA1 LHAZ PALM REUN SEYG TIXI FAA1 LHAZ PALM SEYG
6 | COD | TIXI
6 | EMR | SFER
6 | ESA | AREQ MAW1 AREQ FAA1 MAW1
6 | GFZ | FAA1 GODE
6 | GRG | DAEJ GLSV MAL2 RABT SYOG DAEJ GLSV LHAZ MAL2 RABT
6 | GRG | SYOG
6 | JPL | MAL2
6 | MIT | DGAR DGAR
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 | COD | 5
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 G05 | | | | | 4 | 4 | 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 | .5 -.0 1.2 5 -3 2 -.62
EMR | 0 | 9.8 -10.7 1.0 -8 12 38 -.24
ESA | 0 | -.4 -.4 -.7 -2 17 -1 -.62
GFZ | 0 | .8 .5 1.3 0 -28 -7 -.48
GRG | 0 | -1.2 8.5 3.0 70 -6 35 -.36
JPL | 0 | 1.8 -2.6 2.4 -23 -51 63 .0
MIT | 0 | -4.7 -3.9 6.2 -5 60 13 -.17
NGS | 0 | -4.3 -9.6 8.3 14 -10 -19 -.36
SIO | 0 | -7.0 -2.8 -1.1 -11 -19 11 -.16
COD | 1 | .4 -.2 .6 3 -2 2 -.52
EMR | 1 | 3.2 -4.7 5.1 -18 21 49 -.13
ESA | 1 | .4 -.5 -.7 13 8 -15 -.52
GFZ | 1 | .7 .3 1.0 1 -25 -5 -.55
GRG | 1 | .9 7.7 -11.3 37 -11 21 -.45
JPL | 1 | 5.6 -2.2 -.7 -24 -41 93 .16
MIT | 1 | -4.9 1.9 6.3 -27 38 6 -.26
NGS | 1 | -6.5 -10.8 10.2 7 -36 -32 -.22
SIO | 1 | -4.4 4.4 -1.3 -20 -18 14 -.15
COD | 2 | .4 .1 1.3 8 2 1 -.65
EMR | 2 | 1.9 -4.7 5.5 -8 12 34 -.28
ESA | 2 | -.4 -.1 -.2 10 -30 -10 -.61
GFZ | 2 | .4 .5 1.1 2 -18 -13 -.45
GRG | 2 | -1.4 4.2 -14.7 77 13 65 -.37
JPL | 2 | 4.1 -4.5 3.3 -24 -54 76 .05
MIT | 2 | -4.3 .4 3.0 -4 22 7 -.33
NGS | 2 | -6.1 -6.4 15.1 13 -31 -9 -.32
SIO | 2 | -3.4 1.5 4.3 -8 -10 15 -.39
COD | 3 | .8 -.1 1.6 -2 -4 3 -.74
EMR | 3 | 1.3 -8.0 -2.4 -6 6 8 -.24
ESA | 3 | .1 -.2 -.1 12 -13 4 -.71
GFZ | 3 | .4 .1 1.9 -1 -21 -2 -.60
GRG | 3 | 1.7 4.2 6.2 89 -35 51 -.20
JPL | 3 | 6.6 -1.7 1.9 -16 -53 77 -.05
MIT | 3 | -3.3 1.8 4.5 -5 32 -11 -.28
NGS | 3 | -3.2 -.4 15.7 6 -17 -25 -.48
SIO | 3 | -3.5 4.0 -4.5 -9 -21 3 -.27
COD | 4 | .5 -.1 1.4 -2 2 5 -.63
EMR | 4 | -1.6 -3.7 4.0 -9 -13 12 -.38
ESA | 4 | .1 -.6 -.1 -8 -10 2 -.56
GFZ | 4 | 1.1 .1 1.4 -15 -35 -8 -.50
GRG | 4 | 2.3 1.1 -5.8 99 -19 34 -.02
JPL | 4 | 2.4 -2.4 1.7 -9 -73 86 .11
MIT | 4 | -2.2 3.1 4.8 -12 55 -1 -.27
NGS | 4 | -3.1 -2.4 7.3 16 -22 -2 -.35
SIO | 4 | -2.2 6.6 -2.5 -4 -38 -13 -.30
COD | 5 | .4 .3 .9 12 -7 5 -.51
EMR | 5 | 1.0 -1.8 4.2 -8 -7 15 -.47
ESA | 5 | .2 -.8 -.7 -5 11 1 -.52
GFZ | 5 | .8 .6 .7 1 -21 -13 -.52
GRG | 5 | 3.4 3.5 -9.9 74 10 42 -.15
JPL | 5 | 9.0 -1.7 1.0 -21 -19 82 -.14
MIT | 5 | -.4 -2.1 .5 -20 57 -15 -.31
NGS | 5 | -1.0 -11.8 8.0 31 -26 -23 -.50
SIO | 5 | -.4 3.6 4.1 16 -5 -4 -.38
COD | 6 | .2 .1 1.0 3 -5 7 -.61
EMR | 6 | 1.9 -3.1 3.9 -11 -15 24 -.20
ESA | 6 | -.3 -.6 -.1 2 13 0 -.58
GFZ | 6 | .7 .6 .6 0 -17 -20 -.49
GRG | 6 | -.7 1.9 -4.3 52 -30 29 -.28
JPL | 6 | 7.8 -5.1 4.5 -8 -52 47 .04
MIT | 6 | -1.0 1.0 .9 -3 46 -34 -.21
NGS | 6 | -2.5 -7.0 16.3 26 -30 -23 -.47
SIO | 6 | .3 2.4 -2.9 -9 -14 -4 -.29
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 1.1964.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1964.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 2.1964.[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 3.1964.[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 5.1964.0-6). 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 1964 summary. (Aug 27, 2017 - Sep 02, 2017)
Table 1.1964.a GPS week: 1964 MJD: 57992.000-57998.000
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 279| 0 1 -3 0 -10 9 .03 10 9 | -642 -70 10 104
| 0 0 1 11 19 8 .02 | 120 205
emr 80| -1 -3 1 16 2 13 .20 16 16 | 933 -52 18 131
| 2 1 1 16 10 14 .05 | 795 358
esa 149| 0 0 0 6 17 -3 .02 10 10 | -1924 1320 8 183
| 0 0 1 11 14 18 .01 | 871 1432
gfz 201| 0 0 1 1 -1 7 .11 11 10 | -284 145 10 135
| 1 0 0 9 16 8 .03 | 198 311
grg 110| 1 1 -5 -3 7 7 -.26 15 14 | -8 132 13 185
| 0 1 3 12 17 21 .03 | 89 225
igr n/a| 0 0 0 -15 -10 10 -.02 4 4 | -2714 -488 13 79
| 0 0 0 8 11 8 .01 | 1480 222
jpl 80| 0 0 0 19 -28 32 .17 11 11 | 1092 -46 37 232
| 1 1 0 20 17 17 .02 | 760 364
mit 349| 0 -1 2 -22 7 8 -.05 11 10 | -591 127 37 323
| 0 0 0 19 35 9 .01 | 254 148
ngs 220| -1 1 4 10 -10 -17 -.05 9 8 | -651 -64 1059 2137
| 0 0 1 10 25 7 .04 | 97 164
sio 350| 0 -1 -1 -11 -4 -23 .04 16 16 | --- --- --- ---
| 0 0 1 26 29 33 .03 | --- ---
Table 1.1964.b GPS week : 1964 MJD: 57992.000-57998.000
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 3 3 3 |
2 | 5 5 5 5 5 5 5 |
3 | 5 4 4 6 4 4 4 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 5 4 0 5 4 |
6 | 4 4 4 4 4 4 4 |
7 | 5 5 5 5 5 5 4 |
8 | 4 4 4 4 3 3 3 |
9 | 4 3 4 4 4 4 4 |
10 | 4 5 5 5 4 5 5 |
11 | 5 4 4 5 4 4 4 |
12 | 6 5 5 5 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 6 6 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 5 5 5 5 5 |
19 | 6 5 6 6 5 6 6 |
20 | 4 4 6 5 4 4 4 |
21 | 5 5 4 5 5 5 5 |
22 | 5 5 5 5 5 6 4 |
23 | 6 6 6 6 6 6 6 |
24 | 4 4 4 4 4 3 4 |
25 | 7 4 4 4 4 4 4 |
26 | 5 5 5 5 4 5 5 |
27 | 4 3 3 4 4 3 3 |
28 | 4 5 5 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 3 3 4 3 4 3 3 |
31 | 5 5 5 5 5 4 5 |
32 | 4 3 4 4 3 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 2.1964.0 GPS week: 1964 Day: 0 MJD: 57992.000
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 280| 0 1 -5 -4 -18 6 .03 10 9 | -663 -170 11 99
emr 80| 5 -4 0 7 -10 25 .13 19 17 | 2087 -593 17 127
esa 150| 0 0 0 11 10 -5 .02 10 10 | -1696 1627 10 188
gfz 202| -1 2 1 -5 0 3 .12 10 10 | -25 -405 10 151
grg 114| 2 1 -6 -16 -19 -22 -.24 14 13 | 99 4 14 179
igr n/a| -1 0 0 -4 -21 8 -.02 4 4 | -528 -868 13 70
jpl 80| -2 -1 1 7 -59 31 .18 11 11 | 2224 -600 35 228
mit 349| 0 -2 3 -5 7 2 -.02 12 11 | -301 28 38 326
ngs 220| 0 0 5 12 20 -11 -.05 8 7 | -660 -170 1132 2215
sio 352| 0 -2 0 -12 -17 -28 .05 19 18 | --- --- --- ---
Table 2.1964.1 GPS week: 1964 Day: 1 MJD: 57993.000
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 282| 1 0 -4 -18 6 0 .03 9 9 | -501 -305 11 90
emr 80| -1 -3 2 0 17 18 .15 15 15 | 1769 -100 17 127
esa 150| 0 0 0 19 18 -14 .01 10 10 | -155 -1675 9 225
gfz 201| -1 1 1 -1 9 18 .06 11 10 | -232 232 12 198
grg 110| 1 1 -7 -19 14 -15 -.25 17 15 | -47 243 15 222
igr n/a| 0 0 1 -14 -11 28 -.01 4 4 | -1385 -361 12 69
jpl 80| -1 0 0 20 -20 41 .17 11 11 | 1901 -84 37 229
mit 350| 0 -1 2 1 30 1 -.04 11 10 | -329 153 37 312
ngs 219| 0 0 3 0 -60 -9 -.06 8 7 | -545 -205 1015 2024
sio 351| 0 -1 -1 12 2 -11 .04 18 17 | --- --- --- ---
Table 2.1964.2 GPS week: 1964 Day: 2 MJD: 57994.000
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 285| 1 0 -5 -7 7 26 .04 10 9 | -510 -189 12 108
emr 80| -2 -1 2 30 12 10 .17 16 16 | 1287 -447 18 132
esa 150| 0 0 0 6 18 -24 .01 9 10 | -2582 1237 8 176
gfz 203| 0 0 2 -4 15 -1 .15 11 10 | -621 423 11 106
grg 112| 1 3 -10 -5 23 26 -.24 17 14 | 6 158 14 186
igr n/a| 0 0 0 -26 2 8 -.04 4 4 | -2177 -479 14 84
jpl 80| -1 0 0 20 -20 20 .12 12 12 | 1412 -440 39 225
mit 350| 0 -1 2 -38 -32 17 -.06 11 11 | -629 250 40 303
ngs 222| -1 2 5 24 -7 -25 -.12 10 9 | -553 -135 1058 2471
sio 352| 1 -2 -1 -11 -23 1 .09 17 16 | --- --- --- ---
Table 2.1964.3 GPS week: 1964 Day: 3 MJD: 57995.000
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 284| 0 1 -5 13 -14 2 .05 10 10 | -580 -187 12 105
emr 80| -1 -4 -2 34 -3 4 .22 17 17 | 108 122 19 135
esa 150| 0 0 -1 13 -2 -21 .03 10 10 | -2630 1388 8 191
gfz 203| 1 1 1 8 -8 17 .14 12 11 | -249 -181 10 142
grg 111| 0 0 0 8 -11 15 -.28 13 13 | -34 -39 13 150
igr n/a| 0 0 0 -11 -3 11 -.03 5 5 | -2996 -259 15 90
jpl 80| 0 0 0 52 -33 4 .16 11 11 | 312 116 37 243
mit 350| 0 -1 1 -34 38 23 -.05 11 10 | -547 -58 37 299
ngs 223| -1 1 5 -6 0 -24 -.03 9 8 | -583 -187 840 2158
sio 349| 1 -2 -1 -35 22 4 .04 17 16 | --- --- --- ---
Table 2.1964.4 GPS week: 1964 Day: 4 MJD: 57996.000
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 280| 1 1 -2 0 9 11 .05 10 9 | -802 132 10 105
emr 80| -2 -3 2 5 -5 2 .25 15 15 | 129 58 18 113
esa 150| 0 0 1 -3 21 8 .04 10 10 | -2284 2880 8 149
gfz 202| 0 0 0 -6 -2 0 .07 12 12 | -110 291 13 101
grg 110| 2 0 -2 7 26 -7 -.23 12 12 | -28 282 13 170
igr n/a| 0 0 0 -18 -18 2 -.02 4 4 | -3059 -702 13 68
jpl 80| -1 0 0 -9 -40 60 .17 11 11 | 403 39 37 256
mit 350| 0 -1 1 -26 -22 12 -.05 11 9 | -525 301 36 361
ngs 220| -1 0 1 19 3 -23 -.06 8 8 | -778 66 1056 1978
sio 352| 1 -1 0 0 -46 2 .06 14 13 | --- --- --- ---
Table 2.1964.5 GPS week: 1964 Day: 5 MJD: 57997.000
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 277| 0 1 -1 -2 -34 9 .00 10 9 | -656 -49 9 119
emr 80| -2 -2 2 2 -1 -4 .25 14 14 | 758 425 20 143
esa 150| 0 0 -1 -13 9 18 .03 10 10 | -1686 1623 7 183
gfz 200| 0 0 0 4 -33 10 .13 11 10 | -423 333 9 130
grg 108| 1 0 -4 -8 14 29 -.32 15 14 | -156 472 13 207
igr n/a| 0 0 1 -25 -24 4 -.03 4 4 | -4081 -299 14 96
jpl 80| 1 0 0 9 -20 35 .16 11 11 | 831 446 36 232
mit 349| 1 -2 2 -6 59 1 -.06 12 10 | -787 251 37 330
ngs 221| -2 1 3 7 -19 -20 -.07 9 8 | -668 -66 962 1971
sio 350| 1 0 -4 22 41 -41 -.01 16 16 | --- --- --- ---
Table 2.1964.6 GPS week: 1964 Day: 6 MJD: 57998.000
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 13 -32 11 -.01 9 9 | -785 276 10 108
emr 80| -3 -5 2 35 11 36 .20 16 16 | 399 170 20 141
esa 149| 0 0 0 12 44 17 .01 10 10 | -2437 2161 9 175
gfz 199| 1 0 0 19 6 4 .11 10 10 | -329 325 11 123
grg 107| 1 0 -4 12 5 26 -.27 15 14 | 102 -196 13 184
igr n/a| 0 1 1 -5 2 11 -.02 4 4 | -4777 -449 13 80
jpl 80| 0 -2 0 37 -7 31 .19 12 12 | 564 195 42 213
mit 349| 1 0 1 -47 -24 3 -.06 11 10 | -1025 -36 40 333
ngs 221| -1 2 4 12 -8 -7 .02 9 8 | -773 244 1350 2146
sio 347| 0 -1 -1 -54 -8 -88 -.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 3.1964.0 GPS week: 1964 Day: 0 MJD: 57992.000
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 12 8 8 10 3 8 10 5 22 3 | 55 57 54 55 24 53 57 30 27 75 24
2 | 11 15 10 16 14 6 17 11 10 24 5 | 41 45 42 49 19 43 47 24 21 40 17
3E | 14 12 11 9 16 3 9 10 8 17 4 | 98 96 96 96 26 96 99 26 30 70 30
X4 | 3 --- --- --- --- 51 22 --- --- --- 0 | 45 --- --- --- --- 45 45 --- --- --- 24
5E | 12 16 7 11 12 4 12 11 8 16 4 | 84 56 85 63 22 85 61 19 24 30 41
6 | 9 13 6 7 12 4 11 12 7 20 4 | 55 59 57 53 29 54 58 38 26 75 25
7 | 10 16 12 10 11 4 11 10 9 19 4 | 75 75 74 75 41 73 75 43 45 79 45
8 | 9 13 10 10 11 3 9 8 4 18 3 | 62 62 64 63 20 62 62 28 20 72 19
9 | 7 13 10 6 8 4 9 10 7 17 3 | 82 86 83 84 16 83 85 26 19 81 20
10E | 10 17 12 9 15 5 8 9 7 15 4 | 105 106 110 108 37 107 107 27 44 48 42
11 | 11 11 16 9 10 2 10 9 6 21 4 | 39 42 31 38 28 35 42 25 29 44 26
12E | 17 27 5 12 27 6 11 15 12 17 6 | 26 26 19 20 59 19 18 70 52 107 50
13 | 8 11 13 9 10 3 12 11 8 15 4 | 67 70 65 73 29 68 68 46 39 88 34
14 | 6 13 14 13 11 5 9 17 9 21 4 | 82 86 81 81 37 81 81 47 47 78 43
15 | 10 14 10 12 14 3 13 12 10 21 4 | 88 89 84 86 48 87 87 34 43 64 42
16E | 11 32 6 13 23 7 17 18 10 18 6 | 24 23 21 21 59 21 19 70 57 104 53
17 | 10 17 11 13 15 3 10 10 9 22 4 | 53 55 51 63 46 59 55 53 48 66 45
18E | 11 22 8 10 13 5 10 11 10 17 4 | 141 144 139 138 84 139 143 66 85 47 85
19 | 12 24 10 13 14 4 13 14 10 25 5 | 46 47 45 42 25 41 46 40 32 64 26
20E | 10 14 5 8 13 3 10 13 8 14 4 | 178 176 178 178 108 179 179 83 111 69 109
21 | 8 9 11 9 17 4 9 15 9 16 4 | 74 73 74 72 52 71 73 41 49 51 52
22E | 15 14 7 11 14 3 8 13 8 15 4 | 166 165 165 164 88 164 168 71 94 39 93
23 | 11 27 11 11 7 4 14 19 9 24 5 | 73 75 73 71 28 71 73 38 37 70 32
24 | 11 11 11 7 11 3 7 11 4 19 4 | 65 67 69 66 19 67 71 29 23 77 21
25E | 11 48 12 8 18 4 13 10 11 20 6 | 68 91 70 70 29 71 73 34 33 71 31
26E | 14 16 10 10 21 7 10 13 10 24 5 | 73 71 75 76 25 73 74 27 24 70 21
27 | 9 11 9 6 10 4 10 8 5 21 3 | 61 65 65 63 25 62 63 31 29 75 27
28E | 9 16 5 7 12 3 11 10 6 16 3 | 50 49 48 49 34 49 51 46 30 76 30
29 | 6 25 11 12 17 3 12 14 9 18 5 | 49 53 49 52 21 49 51 35 21 73 20
30 | 7 12 9 6 7 3 9 7 4 18 3 | 77 76 74 74 26 73 75 36 30 87 30
31 | 8 17 11 12 11 5 10 12 10 20 4 | 69 76 71 61 42 64 72 46 37 93 39
32 | 5 13 11 10 10 3 9 12 7 14 3 | 89 93 91 90 18 90 90 28 24 76 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 10 10 14 4 11 12 8 19 |T 73 75 74 74 37 72 74 40 39 69 38
WRMS | 9 17 10 10 13 4 11 11 7 18 |NE 64 67 64 65 29 63 65 35 32 71 30
MEDI | 10 14 10 10 12 4 10 11 8 18 |MD 68 71 71 70 29 68 71 36 32 72 30
Table 3.1964.1 GPS week: 1964 Day: 1 MJD: 57993.000
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 | 4 10 8 9 12 4 8 6 6 24 3 | 46 47 46 44 21 45 47 21 23 58 30
2 | 9 12 8 19 17 6 10 11 10 23 5 | 36 39 35 43 19 36 38 20 24 34 26
3E | 10 9 11 10 22 3 9 9 7 16 4 | 76 70 73 73 34 73 73 18 38 53 42
X4 | 2 --- --- --- --- 19 15 --- --- --- 0 | 38 --- --- --- --- 37 35 --- --- --- 30
5E | 9 11 6 10 20 3 14 10 8 13 4 | 64 41 63 40 28 64 41 17 27 29 49
6 | 9 13 5 9 18 3 10 10 5 13 3 | 44 49 43 45 23 44 46 30 22 50 29
7 | 9 15 12 11 13 3 10 11 11 17 4 | 51 53 49 53 28 51 51 27 33 58 41
8 | 7 14 8 9 11 3 8 6 8 14 3 | 47 48 48 50 21 47 48 18 27 50 33
9 | 5 12 9 6 10 4 8 10 6 14 3 | 59 59 60 62 17 60 62 20 28 54 35
10E | 11 14 12 8 27 5 8 8 8 12 4 | 76 75 78 76 52 77 76 24 49 36 51
11 | 9 11 15 10 10 4 10 7 6 22 4 | 33 35 27 30 20 29 37 15 20 36 28
12E | 10 22 6 10 12 3 15 10 8 20 4 | 21 21 22 24 27 22 21 47 22 80 19
13 | 7 10 12 10 11 3 11 12 9 17 4 | 53 57 51 59 26 55 55 32 36 64 39
14 | 8 15 13 14 17 5 9 17 10 20 5 | 61 59 61 58 38 61 62 37 44 59 48
15 | 11 13 11 13 17 3 12 13 9 18 4 | 62 61 58 63 34 60 61 23 37 46 38
16E | 11 24 6 13 27 6 15 14 11 16 5 | 20 21 22 22 32 20 19 52 27 81 23
17 | 10 15 10 14 16 3 10 11 10 17 4 | 43 43 38 46 33 43 41 41 39 55 35
18E | 9 24 9 11 14 5 13 11 9 17 4 | 110 110 107 105 83 107 109 58 81 44 87
19 | 10 20 8 14 17 4 14 14 12 23 5 | 37 39 34 36 18 34 38 25 23 49 27
20E | 10 13 6 12 20 3 10 13 6 17 4 | 129 128 128 127 93 128 127 56 94 36 95
21 | 8 12 9 12 23 6 13 21 9 17 5 | 71 72 71 77 60 70 70 46 54 49 64
22E | 12 11 7 12 25 4 8 12 8 19 4 | 119 113 117 115 79 116 117 52 82 38 84
23 | 12 26 10 14 11 3 15 18 10 23 5 | 58 56 58 57 29 56 57 32 35 52 42
24 | 8 10 9 9 9 3 7 10 5 18 3 | 43 49 47 48 21 47 48 22 25 54 31
25E | 7 14 9 5 14 3 8 7 6 16 3 | 67 69 71 69 43 70 67 28 45 48 51
26E | 14 15 9 10 17 6 8 10 7 19 4 | 52 55 57 60 26 56 56 19 31 53 33
27 | 9 14 8 7 7 4 9 7 6 14 3 | 48 50 51 50 25 49 50 22 30 55 35
28E | 12 13 6 10 26 4 12 11 6 15 4 | 38 37 36 36 22 36 36 28 19 58 20
29 | 7 23 10 15 13 5 15 12 8 19 4 | 37 39 35 43 17 38 38 23 22 53 26
30 | 5 11 10 9 11 3 9 6 5 15 3 | 54 56 52 52 22 52 54 26 28 62 36
31 | 9 13 12 13 14 5 10 12 10 20 4 | 49 53 51 48 28 48 54 28 28 61 36
32 | 6 8 11 7 11 5 11 10 5 14 3 | 64 68 67 65 25 66 67 20 30 50 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 10 11 17 4 11 11 8 18 |T 56 57 56 57 33 56 56 29 36 51 40
WRMS | 9 15 10 10 15 4 11 10 7 17 |NE 49 51 49 51 26 48 50 26 30 52 35
MEDI | 9 13 9 10 14 4 10 11 8 17 |MD 51 53 51 52 27 51 51 26 30 53 35
Table 3.1964.2 GPS week: 1964 Day: 2 MJD: 57994.000
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 | 4 9 7 7 11 3 8 6 10 19 3 | 45 47 47 46 19 43 48 22 29 47 26
2 | 9 11 9 18 17 4 11 12 12 21 5 | 40 47 42 51 14 41 45 22 28 32 20
3E | 14 10 11 7 16 3 8 5 9 16 4 | 47 49 52 49 29 49 52 19 43 44 32
X4 | 3 --- --- --- --- 19 19 --- --- --- 0 | 39 --- --- --- --- 40 38 --- --- --- 19
5E | 12 10 8 14 20 4 11 12 11 13 4 | 52 50 52 53 20 49 53 14 20 25 25
6 | 6 12 7 8 10 2 8 15 8 18 4 | 46 50 49 47 20 45 50 22 32 38 25
7 | 13 15 11 12 9 4 11 11 11 18 4 | 52 49 47 52 31 49 52 31 47 45 41
8 | 8 12 9 8 12 3 9 5 8 14 3 | 43 45 43 43 20 42 45 16 25 35 20
9 | 7 10 10 7 9 4 8 13 7 16 3 | 43 45 45 46 22 44 48 19 31 43 23
10E | 14 17 11 7 20 4 9 8 10 14 4 | 57 57 59 58 37 57 58 24 47 30 39
11 | 8 11 14 6 10 4 10 8 10 16 4 | 42 48 41 43 23 41 48 23 30 34 25
12E | 7 22 7 8 23 3 16 10 14 16 5 | 37 34 38 39 32 36 36 43 26 75 23
13 | 10 10 12 12 14 5 12 11 8 13 4 | 43 48 41 50 20 43 47 26 37 42 30
14 | 9 18 12 14 16 5 10 14 11 21 5 | 48 53 51 51 26 49 52 35 45 46 39
15 | 11 16 11 14 16 4 14 15 11 15 5 | 56 56 57 54 43 52 60 33 40 39 37
16E | 7 25 6 12 19 3 16 11 11 14 4 | 38 39 40 41 35 38 40 41 24 72 20
17 | 12 14 10 14 15 7 12 13 10 22 5 | 47 51 48 53 35 50 51 41 42 59 35
18E | 11 25 7 12 14 5 14 11 13 15 5 | 80 85 80 80 63 82 85 49 71 34 65
19 | 12 22 8 16 17 6 15 16 12 25 5 | 36 39 37 40 22 36 42 26 28 45 21
20E | 8 15 6 11 48 5 13 15 9 10 6 | 79 81 80 79 77 80 83 46 74 34 68
X21 | 7 12 8 --- 13 6 10 11 9 --- 4 | 54 57 55 --- 30 52 55 27 40 --- 38
22E | 15 12 6 9 15 3 11 14 11 16 4 | 77 77 79 77 56 77 78 47 75 30 63
23 | 10 26 10 14 9 5 15 16 12 20 5 | 43 44 44 47 25 43 45 32 39 45 30
24 | 9 9 11 10 13 4 8 9 11 15 4 | 40 43 41 39 18 36 42 20 27 40 24
25E | 6 15 8 6 14 4 11 10 9 14 3 | 45 49 45 44 21 44 44 22 30 44 24
26E | 15 13 9 10 18 5 10 8 10 15 4 | 47 45 46 44 25 46 47 18 35 47 26
27 | 6 10 7 8 11 4 8 6 7 17 3 | 45 49 49 48 24 46 48 18 32 41 28
28E | 8 20 6 10 25 4 11 11 8 15 4 | 44 48 45 45 23 43 47 20 26 51 22
29 | 8 26 12 12 10 6 18 16 11 15 5 | 36 37 34 40 21 33 39 28 26 38 20
30 | 7 10 9 11 8 4 8 5 8 15 3 | 45 47 46 49 22 45 50 22 39 42 32
31 | 9 11 11 13 16 5 12 13 10 19 4 | 51 53 51 45 34 46 53 24 35 47 34
32 | 6 12 11 8 10 4 12 7 8 17 3 | 49 52 52 51 22 49 53 20 32 41 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 9 11 17 4 12 11 10 17 |T 48 50 49 50 29 47 51 27 37 42 31
WRMS | 9 16 10 10 14 4 12 11 9 16 |NE 44 48 46 47 24 44 48 25 34 42 28
MEDI | 8 12 9 10 14 4 11 11 10 16 |MD 45 49 47 47 24 45 48 24 32 42 26
Table 3.1964.3 GPS week: 1964 Day: 3 MJD: 57995.000
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 | 4 9 9 9 10 4 8 8 9 22 3 | 61 62 64 63 28 61 64 24 23 51 41
2 | 9 11 9 18 19 5 10 11 10 25 5 | 56 56 55 66 25 57 62 22 24 40 42
3E | 9 38 10 8 14 4 9 9 7 13 5 | 64 79 66 61 28 62 68 24 24 39 38
X4 | 3 --- --- --- --- 21 23 --- --- --- 0 | 58 --- --- --- --- 51 56 --- --- --- 40
5E | 11 13 5 11 15 2 9 11 6 12 4 | 78 75 77 77 35 77 77 23 38 27 55
6 | 7 16 7 10 13 3 10 10 6 19 4 | 62 65 60 60 28 59 64 22 23 36 39
7 | 17 11 11 11 13 4 9 11 11 19 5 | 73 70 68 68 27 66 68 25 27 38 43
8 | 7 13 9 8 9 3 11 6 11 18 3 | 56 60 59 58 23 56 60 23 21 43 44
9 | 10 14 10 8 10 3 8 13 7 15 4 | 63 67 61 64 21 59 64 22 20 36 42
10E | 14 13 12 11 13 4 9 6 10 14 4 | 63 64 70 66 32 66 68 23 34 33 39
11 | 7 12 16 8 10 4 10 10 11 21 4 | 57 61 58 59 22 57 62 20 19 41 38
12E | 14 24 7 12 17 5 15 10 8 13 5 | 60 54 59 58 29 56 61 31 27 52 45
13 | 10 11 11 11 9 4 11 11 8 12 4 | 58 59 57 64 26 59 63 36 34 46 45
14 | 7 17 12 15 13 5 10 15 10 20 5 | 59 64 61 64 23 64 66 32 31 40 40
15 | 11 14 11 14 13 5 11 12 10 17 4 | 71 70 68 67 39 65 70 26 30 39 48
16E | 6 26 8 16 18 5 18 8 9 14 5 | 52 56 54 51 33 51 56 32 24 56 41
17 | 13 16 10 14 13 6 11 12 11 17 5 | 65 63 63 66 28 63 67 35 36 50 45
18E | 11 25 8 12 15 6 12 10 10 15 5 | 93 96 95 94 64 94 96 46 62 36 70
19 | 12 21 10 16 16 5 13 16 12 20 5 | 63 61 61 62 32 58 65 32 32 45 47
20E | 11 16 6 10 15 6 12 21 8 11 4 | 74 72 72 73 48 71 74 39 42 35 54
21 | 9 12 9 14 16 5 9 9 8 19 4 | 59 59 60 64 26 59 61 20 23 33 44
22E | 13 21 8 9 13 3 13 13 10 16 4 | 71 73 70 71 40 71 76 31 39 30 41
23 | 11 28 13 12 12 5 16 19 12 19 6 | 69 69 65 71 28 66 69 37 33 43 45
24 | 8 12 9 8 10 3 8 6 5 14 3 | 59 62 61 62 19 60 65 19 24 38 40
25E | 8 15 8 7 14 4 9 9 8 15 4 | 80 76 79 79 51 77 79 50 49 67 69
26E | 10 12 10 14 14 6 9 9 8 20 4 | 55 56 57 54 21 55 58 16 17 38 35
27 | 10 11 8 11 10 4 11 5 6 15 3 | 53 58 57 56 17 54 57 19 19 39 35
28E | 10 18 6 10 11 4 9 8 8 14 4 | 59 52 54 55 21 53 54 23 21 41 38
29 | 8 20 11 16 16 8 13 17 10 15 5 | 57 56 55 62 23 57 59 30 27 36 44
30 | 8 10 10 8 6 3 8 5 6 14 3 | 66 65 64 63 17 62 66 16 18 30 38
31 | 11 14 12 16 14 7 11 10 9 16 4 | 66 72 66 62 33 64 72 31 27 49 45
32 | 9 10 12 10 9 5 14 7 9 13 3 | 56 63 60 59 23 58 64 19 22 34 42
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 10 12 13 5 11 11 9 17 |T 63 65 63 64 29 62 65 27 28 40 44
WRMS | 10 17 10 11 13 5 11 10 8 16 |NE 61 63 61 63 25 59 64 25 25 40 42
MEDI | 10 14 10 11 13 4 10 10 9 15 |MD 61 63 61 63 28 59 64 24 27 39 42
Table 3.1964.4 GPS week: 1964 Day: 4 MJD: 57996.000
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 9 9 7 7 2 8 7 6 13 3 | 70 73 72 70 23 68 73 24 29 41 23
2 | 10 13 9 18 15 6 8 14 11 20 5 | 63 66 64 69 23 63 64 28 29 37 22
3E | 10 14 10 12 13 4 11 7 7 10 4 | 79 78 80 83 25 80 81 24 42 47 32
X4 | 2 --- --- --- --- 57 19 --- --- --- 0 | 60 --- --- --- --- 71 61 --- --- --- 27
X5E | >>>> --- 1 --- --- 5 --- --- --- --- 0 | 9999 --- 9999 --- --- 9999 --- --- --- --- 9999
6 | 7 11 8 11 13 4 10 11 8 11 3 | 66 66 67 67 29 63 68 27 28 42 25
7 | 11 12 12 11 12 4 9 11 11 15 4 | 81 86 82 84 40 82 84 37 51 50 42
8 | 9 11 7 9 9 3 8 7 6 13 3 | 67 68 66 66 23 65 69 22 29 43 22
9 | 7 10 11 9 10 4 8 11 6 10 3 | 72 75 72 75 17 71 73 22 29 37 22
10E | 12 14 10 10 17 4 8 8 8 12 4 | 81 85 88 89 36 83 86 28 50 36 41
11 | 9 13 16 7 9 3 12 8 8 14 4 | 60 66 63 59 17 60 66 21 25 24 18
12E | 13 22 7 11 14 5 14 10 9 15 4 | 62 61 59 63 39 60 63 47 26 79 30
13 | 10 11 11 13 9 4 12 11 8 13 4 | 64 71 65 74 24 67 67 35 41 48 30
14 | 14 19 13 14 15 5 10 13 11 18 5 | 83 80 81 83 30 79 80 39 49 48 38
15 | 11 13 9 16 12 4 12 10 10 15 4 | 73 75 73 75 31 72 74 31 31 49 30
16E | 7 22 8 13 15 4 15 12 7 10 4 | 62 64 63 62 48 59 63 54 29 84 35
17 | 9 12 10 14 14 5 8 14 8 16 4 | 83 82 80 89 49 83 85 55 44 62 47
18E | 15 22 8 11 10 5 12 11 8 13 4 | 106 108 107 106 59 105 107 50 70 40 63
19 | 7 18 10 15 14 5 11 16 9 19 5 | 75 74 74 78 37 74 79 41 34 52 33
20E | 10 13 6 11 10 5 13 8 10 11 3 | 109 110 110 113 53 108 110 45 80 44 66
21 | 8 12 10 13 16 5 10 11 9 18 4 | 74 77 74 73 36 70 75 25 48 30 38
22E | 14 16 6 11 13 5 11 11 10 12 4 | 103 98 101 103 51 101 102 46 75 33 63
23 | 12 24 10 14 14 4 12 19 11 19 5 | 75 77 77 77 26 75 76 37 41 44 32
24 | 7 9 11 8 11 3 8 7 6 15 3 | 65 66 65 66 18 63 67 26 32 47 24
25E | 11 10 8 9 10 3 10 8 8 14 3 | 67 67 67 67 20 64 66 28 26 64 18
26E | 10 13 10 11 14 3 8 10 6 12 4 | 76 74 74 74 16 73 74 18 31 49 20
27 | 9 9 8 8 9 5 8 10 7 14 3 | 66 69 68 67 21 64 67 21 31 41 24
28E | 8 18 6 14 13 4 11 14 7 10 4 | 69 75 74 75 24 72 74 31 32 49 24
29 | 9 24 10 13 10 7 17 12 11 14 4 | 71 70 69 74 26 68 69 33 25 45 25
30 | 6 13 10 12 10 3 10 8 6 11 3 | 72 77 75 74 23 71 76 24 38 43 27
31 | 9 14 10 14 13 5 12 11 10 16 4 | 77 79 77 76 35 74 77 34 44 54 38
32 | 8 8 11 6 7 4 11 6 8 11 3 | 75 73 76 76 20 74 77 22 28 42 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 10 12 12 4 11 11 8 14 |T 74 76 75 76 30 73 75 32 38 46 32
WRMS | 9 15 10 12 12 4 11 9 8 13 |NE 71 73 72 73 27 70 72 30 35 43 29
MEDI | 9 13 10 11 12 4 11 11 8 13 |MD 72 74 74 74 26 71 74 28 32 44 30
Table 3.1964.5 GPS week: 1964 Day: 5 MJD: 57997.000
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 | 4 8 7 8 10 3 9 7 6 20 3 | 87 90 89 86 21 88 90 23 22 55 31
2 | 12 11 9 14 16 5 9 14 12 22 5 | 78 81 77 81 16 78 78 22 25 32 29
3E | 9 11 11 12 14 3 9 8 8 12 4 | 98 98 99 96 21 97 100 19 24 48 18
X4 | 2 --- --- --- --- 31 17 --- --- --- 0 | 79 --- --- --- --- 79 80 --- --- --- 29
X5E | 9 --- 6 8 --- 9 --- 10 --- --- 5 | 309 --- 9999 77 --- 9999 --- 13 --- --- 9999
6 | 8 13 6 8 12 4 8 11 7 14 3 | 84 84 83 83 23 82 83 29 22 50 31
7 | 10 12 11 11 12 2 9 13 10 16 4 | 86 90 85 87 26 86 87 32 29 58 24
8 | 5 11 8 6 12 2 8 4 8 15 3 | 86 88 86 87 21 87 87 23 23 51 32
9 | 7 10 10 6 10 3 7 14 5 14 3 | 92 93 94 93 15 92 92 22 20 55 25
10E | 11 13 12 10 22 5 12 6 11 13 4 | 107 110 110 110 35 109 110 23 44 42 30
11 | 8 12 14 9 13 3 10 8 8 17 4 | 79 85 79 77 14 79 83 15 18 27 26
12E | 15 22 5 13 15 4 17 13 11 16 5 | 85 86 86 85 49 85 86 61 51 89 64
13 | 9 14 12 13 11 4 12 12 7 13 4 | 85 91 84 93 16 89 88 30 25 53 27
14 | 9 13 13 13 15 3 10 14 10 21 5 | 95 95 96 96 22 94 96 34 26 52 22
15 | 9 13 11 13 14 4 11 11 9 21 4 | 92 96 94 96 31 94 94 30 40 45 42
16E | 7 26 8 13 20 4 18 10 13 16 5 | 85 87 86 83 43 85 80 51 40 77 52
17 | 11 13 10 11 16 5 8 12 12 17 4 | 90 88 89 91 31 88 88 34 35 48 44
18E | 13 20 9 9 19 6 13 11 10 14 5 | 131 133 129 129 73 129 132 56 66 48 59
19 | 13 18 9 12 17 5 10 16 13 20 5 | 85 80 83 84 23 82 82 28 21 48 31
20E | 14 13 5 9 13 3 11 10 8 11 4 | 130 130 129 132 65 131 129 45 65 36 53
21 | 8 9 9 12 19 3 9 12 9 18 4 | 94 95 93 93 35 92 92 22 25 37 24
22E | 22 12 7 12 13 4 10 19 9 13 5 | 148 145 147 144 83 146 148 67 86 40 75
23 | 12 26 12 12 11 5 16 21 10 19 5 | 87 89 89 81 18 85 87 32 20 48 24
24 | 7 7 10 7 10 3 12 8 4 16 3 | 81 84 83 83 16 82 87 23 26 54 30
25E | 8 13 8 6 14 4 10 7 10 14 3 | 81 84 85 82 28 83 83 36 32 65 40
26E | 8 14 10 10 19 4 10 10 10 17 4 | 88 87 88 85 19 88 85 22 19 54 19
27 | 6 7 8 7 10 4 9 4 9 12 3 | 86 87 87 84 24 85 85 30 27 52 22
28E | 4 10 6 11 18 4 8 12 10 10 4 | 83 86 86 88 20 85 86 31 25 57 30
29 | 8 24 10 13 18 6 16 14 12 17 5 | 84 89 85 86 25 85 84 33 31 52 41
30 | 5 11 10 8 8 3 9 8 7 13 3 | 85 89 87 88 21 86 88 27 20 61 23
31 | 8 11 11 14 15 5 12 9 8 18 4 | 89 93 89 87 23 88 89 31 22 64 27
32 | 7 7 11 8 11 3 13 7 6 16 3 | 105 106 107 107 38 107 109 37 44 58 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 10 11 15 4 11 12 9 16 |T 99 94 93 92 29 92 93 31 32 51 34
WRMS | 9 14 10 10 14 4 11 10 8 16 |NE 87 89 87 88 22 87 88 27 26 50 30
MEDI | 8 12 10 11 14 4 10 11 9 16 |MD 86 89 87 87 23 87 87 30 25 52 30
Table 3.1964.6 GPS week: 1964 Day: 6 MJD: 57998.000
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 9 7 7 9 4 10 5 7 15 3 | 126 130 130 126 28 127 132 30 23 61 27
2 | 13 11 11 15 14 4 10 15 11 20 5 | 125 126 127 128 22 125 130 25 28 34 22
3E | 6 14 11 11 15 3 13 7 12 9 4 | 142 145 145 143 39 142 144 30 50 57 38
X4 | 2 --- --- --- --- 28 19 --- --- --- 0 | 126 --- --- --- --- 128 129 --- --- --- 28
X5E | 12 12 8 9 --- 6 11 13 8 8 4 | 248 96 9999 122 --- 9999 97 14 9 8 9999
6 | 8 12 7 8 12 3 9 11 7 10 3 | 132 133 137 134 36 133 135 34 28 68 30
7 | 9 13 12 10 11 3 10 12 10 12 4 | 141 144 143 141 48 141 143 44 51 69 46
8 | 5 11 8 8 12 3 9 7 10 10 3 | 130 135 131 132 28 131 136 30 33 60 32
9 | 7 12 9 6 11 3 10 11 8 9 3 | 133 136 136 134 22 134 136 27 26 70 23
10E | 17 15 14 10 19 5 11 7 14 10 5 | 153 159 161 160 51 157 161 34 69 44 54
11 | 9 14 15 8 13 4 11 7 7 11 4 | 123 127 122 123 19 122 129 18 18 23 19
12E | 15 23 5 10 16 5 16 14 8 12 5 | 134 135 135 135 55 135 137 72 47 107 58
13 | 9 12 13 11 11 3 12 12 9 10 4 | 129 134 129 138 28 132 132 50 42 83 34
14 | 7 18 13 15 12 4 11 12 10 17 5 | 140 141 142 143 41 141 143 49 50 64 41
15 | 11 13 11 12 13 3 12 14 9 15 4 | 138 142 141 142 40 139 142 32 45 57 42
16E | 6 24 8 14 28 5 20 9 11 9 5 | 132 138 137 134 51 133 136 67 43 98 52
17 | 10 16 10 12 18 4 10 14 10 16 4 | 135 134 135 138 40 136 136 50 48 62 48
18E | 11 20 7 9 23 5 15 10 12 10 4 | 181 183 184 183 99 182 188 78 96 57 93
19 | 13 19 9 13 17 5 13 17 11 20 5 | 134 133 135 137 34 134 136 42 37 58 35
20E | 12 12 6 8 13 4 10 10 8 9 3 | 186 187 187 190 106 186 188 75 111 44 103
21 | 10 13 11 10 14 4 10 10 10 17 4 | 138 140 140 138 39 137 140 25 35 28 30
22E | 6 16 6 9 20 4 15 8 8 9 3 | 191 192 193 190 117 191 191 89 125 54 113
23 | 12 28 10 11 14 5 18 20 12 17 6 | 134 132 135 134 34 134 134 45 39 58 34
24 | 7 10 11 8 8 4 6 9 6 10 3 | 129 135 134 134 22 133 135 24 29 63 25
25E | 7 15 10 9 15 4 11 6 8 8 3 | 127 129 130 130 25 129 131 35 25 68 26
26E | 8 14 9 11 25 5 10 9 11 14 4 | 131 130 133 130 28 131 131 22 31 61 21
27 | 6 14 7 8 10 3 10 5 8 9 3 | 135 140 138 138 33 137 140 28 39 61 29
28E | 5 12 6 9 15 3 9 10 8 9 3 | 133 135 137 137 27 137 136 42 31 67 27
29 | 7 24 10 11 15 5 16 14 10 14 4 | 123 127 126 125 25 126 125 38 30 64 33
30 | 7 10 10 7 7 2 8 6 6 11 3 | 136 138 140 139 28 138 139 30 36 75 27
31 | 7 15 12 14 11 6 13 10 10 16 4 | 140 143 142 140 49 139 142 51 43 86 44
32 | 8 9 11 8 7 4 8 6 9 10 3 | 151 153 155 153 38 152 155 35 44 69 44
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 10 10 15 4 12 11 9 13 |T 142 140 142 141 41 140 140 40 43 60 41
WRMS | 9 16 10 10 14 4 12 10 8 12 |NE 133 136 135 135 32 134 136 35 36 60 33
MEDI | 8 14 10 10 13 4 11 10 9 10 |MD 134 135 137 137 34 135 136 35 39 61 34
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1964 GPS week: 1964 MJD: 57992.0-57998.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 |U 9 9 20 |U 6 8 24 |U 10 11 22 |
emr | emr 2947 |U 10 9 21 |U 8 10 32 |U 10 9 26 |
esa | esa 2976 | 9 9 19 |U 7 9 27 | 10 10 24 |
gfz | gfz 2947 |U 9 8 22 |U 8 10 29 |U 10 10 23 |
grg | grg 2932 |U 10 8 23 |U 7 9 25 | 10 10 23 |
igr | igr 2972 | 9 8 19 | 7 9 28 | 10 10 23 |
igs | igs 2973 | 8 8 17 | 6 8 21 | 8 8 20 |
jpl | jpl 3044 | 10 9 21 |U 7 10 28 | 10 11 26 |
mit | mit 2962 | 9 10 20 |U 7 9 27 |U 9 9 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 5.1964.0 GPS week: 1964 Day: 0 MJD: 57992.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 4 14 | 6 6 17 | 9 10 24 |
emr | emr 2976 | 8 6 14 | 8 9 21 | 11 10 29 |
esa | esa 2976 | 7 6 14 | 6 7 18 | 10 10 26 |
gfz | gfz 2975 | 7 6 17 | 6 8 18 | 9 10 24 |
grg | grg 2975 | 7 6 17 | 7 7 21 | 12 12 25 |
igr | igr 2976 | 6 5 14 | 6 7 17 | 9 10 25 |
igs | igs 2976 | 7 5 15 | 6 7 18 | 9 10 25 |
jpl | jpl 3072 | 8 7 13 | 6 8 15 | 10 11 29 |
mit | mit 2976 | 7 5 14 | 9 7 24 | 9 11 26 |
Table 5.1964.1 GPS week: 1964 Day: 1 MJD: 57993.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 8 14 | 5 5 19 | 10 9 20 |
emr | emr 2976 | 6 6 17 | 6 7 21 | 10 10 21 |
esa | esa 2976 | 6 6 14 | 4 6 17 | 10 10 21 |
gfz | gfz 2974 | 5 5 12 | 5 6 20 | 10 9 19 |
grg | grg 2973 | 5 5 14 | 5 7 21 | 12 13 26 |
igr | igr 2976 | 5 5 12 | 4 5 17 | 10 8 19 |
igs | igs 2976 | 5 5 12 | 4 6 18 | 9 10 19 |
jpl | jpl 3072 | 7 7 17 | 5 7 19 | 12 12 23 |
mit | mit 2976 | 6 7 16 | 6 6 25 | 10 9 20 |
Table 5.1964.2 GPS week: 1964 Day: 2 MJD: 57994.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 9 14 17 | 6 8 25 | 8 6 17 |
emr | emr 2970 | 9 15 23 | 6 9 30 | 8 6 17 |
esa | esa 2976 | 8 14 18 | 6 9 26 | 8 7 19 |
gfz | gfz 2879 | 9 12 34 | 7 11 26 | 11 8 17 |
grg | grg 2968 | 13 13 44 | 9 15 36 | 10 9 21 |
igr | igr 2968 | 8 13 18 | 6 9 25 | 8 6 18 |
igs | igs 2970 | 7 12 16 | 6 9 24 | 9 6 17 |
jpl | jpl 3072 | 10 15 20 | 7 9 27 | 9 7 19 |
mit | mit 2976 | 8 13 19 | 7 10 29 | 10 6 18 |
Table 5.1964.3 GPS week: 1964 Day: 3 MJD: 57995.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 10 13 27 | 5 6 22 | 8 9 17 |
emr | emr 2976 | 11 13 21 | 7 10 37 | 9 8 24 |
esa | esa 2976 | 10 11 23 | 6 7 24 | 8 8 20 |
gfz | gfz 2976 | 11 11 25 | 7 10 25 | 7 6 18 |
grg | grg 2975 | 11 10 24 | 6 7 20 | 8 8 21 |
igr | igr 2976 | 10 11 23 | 6 7 22 | 8 8 18 |
igs | igs 2976 | 10 10 22 | 5 6 20 | 6 6 18 |
jpl | jpl 3072 | 11 14 25 | 6 9 26 | 8 9 19 |
mit | mit 2976 | 10 11 24 | 6 8 26 | 7 8 26 |
Table 5.1964.4 GPS week: 1964 Day: 4 MJD: 57996.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 21 | 6 9 26 | 9 12 20 |
emr | emr 2880 | 10 6 26 | 7 11 32 | 9 8 21 |
esa | esa 2976 | 8 6 23 | 7 9 22 | 8 11 21 |
gfz | gfz 2879 | 9 7 25 | 7 9 26 | 10 12 20 |
grg | grg 2879 | 12 8 24 | 5 8 22 | 8 9 20 |
igr | igr 2967 | 9 7 23 | 6 9 24 | 9 11 20 |
igs | igs 2967 | 9 7 22 | 5 8 20 | 7 8 18 |
jpl | jpl 2976 | 10 6 28 | 6 11 31 | 8 11 24 |
mit | mit 2880 | 10 10 28 | 6 9 28 | 9 10 19 |
Table 5.1964.5 GPS week: 1964 Day: 5 MJD: 57997.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 8 22 | 8 11 28 | 11 13 27 |
emr | emr 2880 | 11 8 20 | 13 12 43 | 10 8 33 |
esa | esa 2976 | 11 8 15 | 14 14 44 | 12 13 29 |
gfz | gfz 2976 | 11 7 15 | 14 14 51 | 11 11 29 |
grg | grg 2880 | 11 9 20 | 11 11 30 | 11 10 25 |
igr | igr 2970 | 11 8 19 | 17 17 55 | 12 12 30 |
igs | igs 2976 | 9 7 16 | 9 10 26 | 8 8 22 |
jpl | jpl 2976 | 11 8 19 | 14 13 46 | 11 13 34 |
mit | mit 2976 | 10 9 17 | 10 10 31 | 9 7 21 |
Table 5.1964.6 GPS week: 1964 Day: 6 MJD: 57998.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 9 23 | 9 12 34 | 14 15 30 |
emr | emr 2976 | 15 10 23 | 9 12 37 | 12 11 36 |
esa | esa 2976 | 14 9 24 | 9 12 37 | 14 14 32 |
gfz | gfz 2975 | 13 8 24 | 9 12 38 | 14 13 32 |
grg | grg 2880 | 11 8 20 | 7 9 25 | 7 9 23 |
igr | igr 2976 | 13 9 24 | 9 12 36 | 14 14 31 |
igs | igs 2976 | 10 8 19 | 6 7 22 | 6 6 21 |
jpl | jpl 3072 | 14 8 25 | 8 12 35 | 14 14 34 |
mit | mit 2976 | 12 13 23 | 7 11 27 | 9 10 24 |
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 6.1964 GPS week: 1964 MJD: 57992.500-57998.500
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 4 10 -6 1 | 24 40
| 23 16 55 54 5 | 3
emr uuuuu | 18 -18 183 68 20 | 27 49
| 24 24 174 72 11 | 10
esa uuuuu | -8 -8 37 63 -4 | 30 46
| 19 8 32 38 5 | 3
gfz uuuuu | -10 -12 21 -99 -2 | 38 50
| 19 10 53 146 6 | 3
grg uuuuu | -12 -1 -4 -77 1 | 6 32
| 19 7 34 37 2 | 2
igr xxxxx | 11 19 21 -7 -6 | 3 32
| 12 4 18 45 6 | 3
irf xxxxx | 10 4 -48 -1 -8 | 4 35
| 6 9 24 14 4 | 2
jpl xxxxx | 37 -20 22 93 -4 | 29 43
| 19 24 69 59 4 | 4
mit uuuuu | -15 28 -100 -69 -7 | 34 48
| 13 17 57 70 5 | 2
ngs uuuuu | 5 -10 -22 7 -9 | 24 41
| 26 25 69 77 7 | 2
sio uuuux | 47 20 -102 186 1 | 101 107
| 10 19 49 78 20 | 5
Table 7.1964.0 GPS week: 1964 Day: 0 MJD: 57992.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -9 14 49 -60 6 | 24 38
emr uuuuu | -25 -1 314 20 7 | 18 42
esa uuuuu | 2 -4 35 97 -9 | 35 45
gfz uuuuu | -8 -2 17 -104 -9 | 43 51
grg uuuuu | 18 5 -32 -75 5 | 7 29
igr xxxxx | 28 17 -7 39 -5 | 7 27
irf xxxxx | 18 6 -80 10 -6 | 6 30
jpl xxxxx | 66 4 65 220 -12 | 36 45
mit uuuuu | -6 26 -180 -16 1 | 35 46
ngs uuuuu | -4 -29 -32 20 -9 | 28 39
sio uuuux | 66 17 -83 213 34 | 96 102
Table 7.1964.1 GPS week: 1964 Day: 1 MJD: 57993.500
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 | -24 19 -46 -31 0 | 22 38
emr uuuuu | -3 -9 118 116 23 | 17 43
esa uuuuu | -17 -21 62 57 -10 | 30 45
gfz uuuuu | -32 3 -77 -67 -8 | 38 50
grg uuuuu | -32 -1 -6 -135 -1 | 5 31
igr xxxxx | 11 17 18 65 -4 | 3 30
irf xxxxx | 4 -6 -70 1 -3 | 3 34
jpl xxxxx | 7 -11 91 55 -2 | 29 43
mit uuuuu | -6 31 -139 -58 1 | 32 46
ngs uuuuu | 57 -25 122 -18 -6 | 25 40
sio uuuux | 52 21 -141 245 22 | 96 102
Table 7.1964.2 GPS week: 1964 Day: 2 MJD: 57994.500
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 | -22 24 -59 -47 3 | 20 37
emr uuuuu | 18 -60 286 141 21 | 19 45
esa uuuuu | 8 -11 16 74 -5 | 28 44
gfz uuuuu | -6 -8 -11 15 4 | 36 47
grg uuuuu | -12 0 52 -58 1 | 3 30
igr xxxxx | 11 27 14 -35 0 | 2 30
irf xxxxx | 12 -1 -26 -15 -5 | 2 33
jpl xxxxx | 34 -27 -12 61 -3 | 27 40
mit uuuuu | -14 33 -49 -141 -7 | 32 46
ngs uuuuu | 13 -26 -46 -17 -15 | 24 39
sio uuuux | 43 37 -78 106 -3 | 98 104
Table 7.1964.3 GPS week: 1964 Day: 3 MJD: 57995.500
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 -19 100 -9 3 | 25 42
emr uuuuu | 41 15 -187 -41 28 | 25 51
esa uuuuu | 7 -15 0 65 -6 | 31 46
gfz uuuuu | -3 -11 78 5 2 | 39 51
grg uuuuu | -9 -3 28 -102 1 | 6 33
igr xxxxx | -8 20 41 -27 -9 | 5 32
irf xxxxx | 8 -8 -27 11 -12 | 6 35
jpl xxxxx | 25 -69 90 92 -2 | 29 43
mit uuuuu | -13 -1 -63 -32 -12 | 35 49
ngs uuuuu | -17 43 -8 -73 -10 | 26 41
sio uuuux | 42 -18 -40 293 -1 | 102 109
Table 7.1964.4 GPS week: 1964 Day: 4 MJD: 57996.500
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 | -8 -5 24 -2 6 | 25 42
emr uuuuu | 32 -34 259 130 37 | 30 52
esa uuuuu | 9 -7 78 105 -2 | 29 46
gfz uuuuu | 21 -19 22 52 -8 | 38 51
grg uuuuu | -15 -13 -37 -33 2 | 6 33
igr xxxxx | 22 18 11 -50 -15 | 2 33
irf xxxxx | 2 7 -41 -13 -10 | 4 36
jpl xxxxx | 56 -6 35 96 -5 | 28 43
mit uuuuu | -44 49 -55 -173 -9 | 34 49
ngs uuuuu | -10 -6 -79 -66 -19 | 24 41
sio uuuux | 48 33 -154 70 -6 | 103 109
Table 7.1964.5 GPS week: 1964 Day: 5 MJD: 57997.500
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 | 37 -7 -13 106 -7 | 25 42
emr uuuuu | 29 -23 252 106 20 | 33 53
esa uuuuu | -19 4 67 52 2 | 27 46
gfz uuuuu | -5 -23 60 -271 2 | 35 50
grg uuuuu | -37 8 -30 -96 4 | 3 35
igr xxxxx | 7 16 46 -47 -10 | -1 37
irf xxxxx | 16 15 -67 -18 -8 | 1 39
jpl xxxxx | 34 -23 -14 71 -2 | 25 43
mit uuuuu | -13 46 -159 -88 -10 | 31 49
ngs uuuuu | -18 -16 -82 51 -8 | 20 43
sio uuuux | 45 19 -58 165 -10 | 103 109
Table 7.1964.6 GPS week: 1964 Day: 6 MJD: 57998.500
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 3 14 -1 -2 | 29 43
emr uuuuu | 37 -16 237 7 6 | 43 56
esa uuuuu | -42 -2 4 -10 3 | 32 48
gfz uuuuu | -36 -22 58 -325 2 | 39 53
grg uuuuu | 5 -5 -3 -40 -2 | 9 34
igr xxxxx | 7 21 24 8 1 | 2 36
irf xxxxx | 13 12 -25 15 -13 | 5 37
jpl xxxxx | 40 -7 -99 54 -1 | 29 44
mit uuuuu | -10 15 -55 23 -11 | 35 50
ngs uuuuu | 14 -9 -28 150 5 | 23 43
sio uuuux | 35 34 -158 207 -26 | 109 113
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