[IGSREPORT-25348] Wk 1952 IGS Final Orbits
acc
acc at igs.org
Sun Jun 25 18:51:31 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1952 (Jun 04, 2017 - Jun 10, 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:
igs1952[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1952[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1952[0-6].cls IGS GPS clock combination summary report.
igs19527.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19527.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 | AUCK TIXI OHI3 TIXI
0 | EMR | HERS SYOG YAKT
0 | ESA | MAL2 SAVO ULAB
0 | GFZ | GODE MAL2 POHN AUCK GODE POHN
0 | GRG | ADIS ALRT CCJ2 CHTI FAA1 GLSV HRAO INVK KRGG LHAZ
0 | GRG | NAIN NLIB REUN SHAO SSIA STJO SUTH SYOG ULAB XMIS
0 | GRG | ADIS CHTI FAA1 GLSV LHAZ STJO SYOG
0 | MIT | 23 23
1 | COD | MATE TIXI MATE TIXI
1 | EMR | HERS HERS MAS1
1 | ESA | FAA1 MAL2 LHAZ
1 | GFZ | GODE MAL2 MAS1 NTUS POHN GODE MAS1 NTUS POHN
1 | GRG | GLSV LHAZ OHI3 STJO SYOG GLSV LHAZ OHI3 STJO SYOG
1 | MIT | 21 21
2 | COD | SFER TIXI FAA1 SFER SYOG TIXI
2 | EMR | HERS
2 | ESA | MAL2 MAS1 MAL2 MAS1
2 | GFZ | 21 21 28 GODE IRKJ MAL2 MAS1 POHN FAA1 GODE IRKJ
2 | GFZ | MAL2 MAS1 POHN
2 | GRG | ADIS CCJ2 GLSV MAS1 NAIN SYOG TUVA ADIS CCJ2 GLSV
2 | GRG | IRKJ MAS1 NAIN SYOG TUVA
2 | MIT | MAS1 MAS1
3 | COD | FAA1 PIE1 SFER TIXI FAA1 PIE1 SFER TIXI
3 | EMR | HERS MAS1 SFER
3 | ESA | MAS1 MAL2 MAS1 SOFI
3 | GFZ | GODE MAS1 POHN GODE MAS1 POHN SYOG
3 | GRG | 17 17 ADIS GLSV INVK NAIN SYOG ADIS GLSV INVK NAIN
3 | GRG | SYOG
3 | MIT | AREG MAS1 AREG MAS1
4 | COD | AUCK HRAO MATE SYOG TIXI AUCK HRAO MATE SYOG TIXI
4 | EMR | ALBH KERG MAS1 NIST SFER
4 | ESA | MAR6 ONSA MAR6 ONSA
4 | GFZ | GODE POHN GODE POHN
4 | GRG | 13 GLSV LHAZ SYOG GLSV SYOG
4 | MIT | 11
5 | COD | TIXI TIXI
5 | EMR | YAR2 NIST SFER WHIT YAR2
5 | ESA | ARTU FAA1 OHI3 ARTU MAL2 OHI3
5 | GFZ | FAA1 GODE POHN AUCK GODE POHN
5 | GRG | GLSV MAL2 SYOG GLSV MAL2 SYOG TASH
6 | COD | MATE TIXI MATE PIMO TIXI
6 | EMR | HERS NIST
6 | ESA | MAL2 MAL2 SYOG
6 | GFZ | GODE MAL2 POHN GODE MAL2 POHN
6 | GRG | 21 FAA1 GLSV LHAZ SYOG FAA1 GLSV LHAZ SYOG
6 | JPL | MAL2
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
7. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .0 -.1 .6 5 19 1 -.10
EMR | 0 | 1.6 .7 -4.5 -10 25 4 .25
ESA | 0 | .1 -.6 .3 -5 15 -10 -.17
GFZ | 0 | -.3 .2 .0 -1 -7 -3 -.04
GRG | 0 | 4.6 2.1 6.8 27 6 40 -.19
JPL | 0 | 1.1 .7 -3.1 -15 -49 65 .45
MIT | 0 | -.0 -2.3 1.7 -25 31 0 .24
NGS | 0 | -2.7 -3.6 -6.6 26 -10 4 .11
SIO | 0 | .1 -1.8 -9.6 -20 16 -9 -.02
COD | 1 | .2 -.3 -.0 -7 1 2 -.14
EMR | 1 | -6.4 -2.3 -9.5 -14 19 -3 .12
ESA | 1 | .3 -.2 -.2 -12 27 -20 -.14
GFZ | 1 | .2 -.1 .2 -8 -25 7 -.08
GRG | 1 | 2.8 -2.3 .1 32 41 28 -.17
JPL | 1 | -.0 -5.5 1.6 -42 -77 50 .33
MIT | 1 | 1.1 -6.7 2.6 -24 50 12 .24
NGS | 1 | -6.0 -7.8 .1 2 -10 -21 .19
SIO | 1 | -2.8 -3.9 -7.8 -15 13 -7 .03
COD | 2 | -.1 .2 .2 0 15 -1 -.10
EMR | 2 | 1.3 -2.7 -7.3 -28 30 5 .15
ESA | 2 | -.1 -.3 .0 -16 13 -10 -.18
GFZ | 2 | -.2 .1 .2 -6 -4 0 -.01
GRG | 2 | 1.4 4.8 9.1 35 27 20 -.16
JPL | 2 | 2.3 -11.2 -5.0 -3 12 46 .61
MIT | 2 | -2.4 -3.8 3.4 -30 63 3 .18
NGS | 2 | -4.3 -11.2 2.5 11 -3 -32 .16
SIO | 2 | -3.4 1.0 -10.0 -20 14 -7 .08
COD | 3 | -.6 .1 .5 6 25 -5 -.10
EMR | 3 | -.0 -2.9 -3.3 10 30 28 .28
ESA | 3 | -.3 -.6 -.1 -20 20 -1 -.14
GFZ | 3 | -.5 -.2 .3 -11 -1 -9 -.01
GRG | 3 | .6 -3.6 5.8 36 13 25 -.06
JPL | 3 | .6 -9.5 -8.7 14 -4 13 .58
MIT | 3 | -.9 -6.6 5.8 -8 54 -8 .20
NGS | 3 | -3.2 -12.5 .3 14 -17 -31 .21
SIO | 3 | -.2 -3.3 -11.6 -10 -1 -2 .06
COD | 4 | -.5 .3 -.1 -1 8 -5 -.18
EMR | 4 | -.8 -7.0 -5.5 8 44 28 .10
ESA | 4 | -.8 -.4 -.0 -10 11 1 -.17
GFZ | 4 | -.6 -.0 .1 -6 -4 8 -.12
GRG | 4 | 5.3 -6.9 -2.3 71 17 31 -.05
JPL | 4 | .8 -12.8 4.4 -28 -29 51 .47
MIT | 4 | -4.7 -5.2 1.2 -28 43 14 .15
NGS | 4 | -4.0 -2.6 -2.6 10 -6 8 -.02
SIO | 4 | -4.0 -2.3 -9.4 -19 13 -19 .03
COD | 5 | -.3 -.1 .5 1 21 0 -.09
EMR | 5 | .9 -.1 -5.8 0 20 22 .22
ESA | 5 | -1.3 -.2 .0 -11 8 -6 -.13
GFZ | 5 | .0 -.0 .4 -11 -17 -14 -.15
GRG | 5 | 1.5 -1.0 -14.4 63 17 34 -.24
JPL | 5 | 7.7 -3.7 -6.7 -5 -7 42 .29
MIT | 5 | -4.2 -3.2 -2.7 -17 28 12 .10
NGS | 5 | -6.4 -8.9 -3.1 36 -30 -26 .07
SIO | 5 | .4 -1.8 -12.1 -14 3 -9 -.0
COD | 6 | .3 .2 .2 4 5 2 -.12
EMR | 6 | -.4 -2.2 -14.8 4 17 17 .13
ESA | 6 | -.3 -.5 -.1 -9 6 -4 -.15
GFZ | 6 | .4 -.2 -.0 -15 -20 -3 -.13
GRG | 6 | -.4 -4.5 -5.8 53 -6 24 -.22
JPL | 6 | 13.1 -3.8 -9.5 21 -38 112 .75
MIT | 6 | .7 -3.9 2.5 -5 15 12 .01
NGS | 6 | -5.2 -5.8 -4.4 26 -30 -13 -.16
SIO | 6 | -3.3 -3.4 -12.9 -9 -1 -1 -.06
8. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1952.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1952.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 2.1952.[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 3.1952.[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 5.1952.0-6). 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 1952 summary. (Jun 04, 2017 - Jun 10, 2017)
Table 1.1952.a GPS week: 1952 MJD: 57908.000-57914.000
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 272| 0 0 6 17 0 -5 .00 11 10 | -549 -96 11 94
| 0 0 1 25 8 11 .05 | 193 250
emr 84| -2 0 -5 -4 1 27 .27 15 15 | 615 35 19 104
| 2 1 1 18 16 8 .03 | 299 406
esa 150| 0 0 -6 13 -4 -6 -.02 9 9 | -1252 235 9 148
| 0 0 1 16 13 9 .04 | 1202 1197
gfz 197| 0 1 1 6 10 -2 .07 10 9 | 52 -307 10 120
| 0 0 0 14 20 10 .01 | 73 431
grg 108| 1 0 1 -2 -4 -21 -.37 16 14 | 58 -73 13 166
| 0 0 5 18 22 16 .03 | 173 308
igr n/a| 0 0 0 20 -10 -3 .06 4 4 | 7969 116 12 74
| 0 0 1 13 12 9 .02 | 554 474
jpl 80| -1 0 -2 22 -14 32 .25 11 11 | 398 45 38 190
| 2 0 1 15 27 12 .02 | 320 409
mit 350| 1 -1 5 -9 -6 12 .02 12 11 | -477 -145 36 287
| 0 0 0 13 23 10 .02 | 584 319
ngs 219| -1 0 -3 -25 13 6 .04 9 8 | -580 -32 859 2062
| 0 1 2 60 51 22 .05 | 164 245
sio 336| 1 0 0 -3 -16 7 -.05 12 12 | --- --- --- ---
| 0 0 1 13 23 14 .04 | --- ---
Table 1.1952.b GPS week : 1952 MJD: 57908.000-57914.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 3 3 3 4 3 |
2 | 4 4 4 4 4 4 5 |
3 | 4 3 4 4 4 4 4 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 3 4 4 4 4 |
6 | 3 3 3 3 3 3 4 |
7 | 5 4 4 4 4 5 4 |
8 | 4 5 5 5 5 6 6 |
9 | 4 3 3 3 3 4 3 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 5 5 5 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 8 8 7 7 8 8 8 |
17 | 5 4 5 5 4 4 5 |
18 | 4 4 4 4 4 4 4 |
19 | 5 4 4 4 4 5 5 |
20 | 4 4 4 4 4 5 4 |
21 | 6 5 5 5 5 5 5 |
22 | 3 3 3 4 4 4 4 |
23 | 5 5 5 5 5 6 6 |
24 | 5 4 4 6 5 5 5 |
25 | 4 3 4 5 4 4 4 |
26 | 3 3 3 3 3 3 4 |
27 | 4 4 4 4 4 5 5 |
28 | 5 5 5 6 5 5 5 |
29 | 5 5 5 6 6 6 6 |
30 | 4 4 4 4 4 6 4 |
31 | 5 5 5 5 5 4 5 |
32 | 3 3 4 4 3 3 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1952.0 GPS week: 1952 Day: 0 MJD: 57908.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 270| 0 0 6 71 -8 8 .08 9 9 | -211 -413 10 81
emr 84| -3 2 -4 26 -29 16 .24 14 14 | 866 -590 13 113
esa 150| 0 0 -6 45 -22 6 .03 9 9 | -1019 484 10 135
gfz 198| 0 1 2 15 -21 0 .08 10 8 | 176 -607 9 134
grg 110| 1 0 5 7 -49 -25 -.42 16 15 | 410 -581 14 155
igr n/a| 0 0 0 48 -28 -2 .08 4 4 | 7910 -742 13 72
jpl 80| -2 0 -3 29 -63 36 .23 11 11 | 631 -565 38 167
mit 350| 1 -1 5 -13 -7 25 -.02 13 11 | -356 -654 34 310
ngs 218| 0 0 -5 -159 119 -40 -.03 9 8 | -242 -335 670 1907
sio 335| 2 -1 0 -9 -9 24 -.10 14 13 | --- --- --- ---
Table 2.1952.1 GPS week: 1952 Day: 1 MJD: 57909.000
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 269| 0 0 5 5 -6 -1 .03 10 9 | -711 293 10 84
emr 85| -5 0 -6 -29 5 19 .27 15 15 | 472 382 15 88
esa 150| 0 0 -7 2 9 -7 .03 8 8 | -3813 1587 10 123
gfz 197| 0 1 0 -1 9 7 .08 9 9 | -30 1 9 98
grg 108| 2 -1 0 -22 24 -47 -.36 13 13 | -74 251 12 181
igr n/a| 0 0 0 15 -21 -18 .09 4 4 | 7346 599 11 67
jpl 80| -1 0 -2 12 -24 44 .27 11 11 | 146 381 38 171
mit 350| 1 -2 4 0 -13 15 .01 12 11 | -1316 83 38 283
ngs 220| -1 0 0 8 12 15 -.01 9 8 | -722 420 623 1691
sio 336| 1 -1 2 15 -37 6 -.06 12 13 | --- --- --- ---
Table 2.1952.2 GPS week: 1952 Day: 2 MJD: 57910.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 268| 0 0 4 -5 -13 4 -.03 9 9 | -555 -199 9 82
emr 85| -3 0 -5 -19 1 28 .25 15 15 | 353 -38 15 87
esa 150| 0 1 -6 22 -17 -19 -.01 9 9 | -1263 1668 10 145
gfz 198| 0 0 0 4 8 4 .09 10 9 | 56 -577 9 96
grg 109| 1 0 10 -5 -5 -24 -.39 16 15 | 18 -124 14 187
igr n/a| 0 0 -2 24 -13 0 .07 4 4 | 7360 251 12 75
jpl 80| -4 0 -3 43 -6 16 .26 13 13 | 38 65 42 193
mit 350| 1 -2 4 -19 9 17 .00 12 10 | -787 -29 33 291
ngs 221| -1 0 -2 11 21 0 .02 9 7 | -584 -121 871 1950
sio 340| 1 0 -2 -9 -20 10 -.08 13 14 | --- --- --- ---
Table 2.1952.3 GPS week: 1952 Day: 3 MJD: 57911.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 270| 0 0 5 2 10 -6 -.00 11 10 | -705 116 11 87
emr 85| -1 1 -6 3 -4 35 .31 15 15 | 794 39 20 102
esa 150| 0 0 -7 3 -9 -2 -.04 8 8 | -821 150 10 133
gfz 197| 0 1 1 -18 40 -9 .08 11 10 | 34 -1 11 90
grg 105| 2 0 5 -27 4 -28 -.31 17 15 | -42 228 14 158
igr n/a| -1 1 -1 13 -10 0 .06 4 4 | 8082 110 12 79
jpl 80| 0 0 -2 42 -18 24 .27 11 11 | 535 108 39 184
mit 350| 1 -1 4 -2 18 -7 .02 12 11 | 12 -46 34 280
ngs 218| -1 -1 -2 4 -20 6 .04 9 8 | -708 118 879 1893
sio 340| 2 0 0 12 -41 2 -.09 12 11 | --- --- --- ---
Table 2.1952.4 GPS week: 1952 Day: 4 MJD: 57912.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 272| 0 0 6 6 6 -21 -.07 11 10 | -719 -16 11 93
emr 85| -1 -1 -3 0 2 21 .24 15 15 | 445 -312 22 98
esa 150| -1 0 -4 12 -2 -4 -.03 8 8 | -415 -1611 8 161
gfz 199| 0 1 1 4 30 9 .07 10 9 | 126 -941 10 125
grg 106| 1 0 0 27 -2 -12 -.39 16 16 | -62 -209 13 153
igr n/a| 0 0 0 9 -3 -12 .04 4 4 | 7923 -145 12 71
jpl 80| 0 -1 0 13 -14 39 .27 11 11 | 303 -421 36 199
mit 350| 1 -1 7 -25 -29 7 .02 12 10 | -1011 -363 45 305
ngs 219| -1 0 -7 -19 15 16 .08 9 8 | -680 -119 973 2489
sio 335| 1 0 1 -1 -33 6 -.05 12 12 | --- --- --- ---
Table 2.1952.5 GPS week: 1952 Day: 5 MJD: 57913.000
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 0 10 20 4 -17 -.03 14 11 | -374 -344 16 121
emr 85| 1 0 -4 4 13 36 .31 16 16 | 293 620 24 129
esa 150| -1 0 -5 0 -1 -17 -.07 9 10 | -1271 247 10 181
gfz 198| 0 0 3 21 -5 -16 .06 10 9 | -1 -319 10 178
grg 109| 1 -1 -7 1 0 -17 -.38 15 14 | 159 -254 13 193
igr n/a| -1 0 2 13 -6 3 .04 5 5 | 8188 658 15 85
jpl 80| -1 0 -2 2 29 19 .23 12 12 | 190 575 41 228
mit 350| 0 -1 5 -19 19 6 .04 12 10 | -202 -316 34 260
ngs 219| -2 2 -2 -1 -15 30 .12 10 8 | -575 2 779 2182
sio 334| 2 0 1 -16 0 23 .01 13 12 | --- --- --- ---
Table 2.1952.6 GPS week: 1952 Day: 6 MJD: 57914.000
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 6 21 1 -4 .02 11 11 | -571 -114 15 110
emr 84| -1 -1 -5 -16 23 34 .26 16 15 | 1086 149 24 111
esa 150| 0 0 -6 5 14 0 -.06 9 9 | -168 -878 11 162
gfz 198| 0 0 2 21 8 -15 .06 11 9 | 7 295 12 123
grg 110| 1 -1 0 0 -1 5 -.34 15 13 | 0 176 14 137
igr n/a| 0 0 2 16 11 8 .03 5 5 | 8980 82 13 71
jpl 80| 2 0 -1 15 -4 49 .25 11 11 | 944 174 36 189
mit 350| 1 -1 5 11 -40 20 .03 13 11 | 320 305 40 281
ngs 221| -1 0 -3 -22 -36 18 .10 10 8 | -552 -190 1220 2324
sio 335| 0 0 2 -19 22 -19 .01 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 3.1952.0 GPS week: 1952 Day: 0 MJD: 57908.000
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 8 6 6 8 4 9 5 7 13 2 | 13 18 15 15 13 15 19 15 13 17 14
2 | 9 11 8 11 15 3 11 13 12 15 4 | 13 14 12 16 13 13 15 15 14 12 11
3 | 7 12 10 7 10 3 12 8 6 12 3 | 12 24 12 15 7 14 26 12 12 18 13
X4 | 5 --- --- --- --- 37 31 --- --- --- 0 | 19 --- --- --- --- 19 22 --- --- --- 19
5 | 6 10 10 6 9 4 11 11 8 11 3 | 17 17 14 15 10 15 17 16 14 18 15
6 | 6 10 6 6 8 3 11 6 10 10 3 | 16 22 18 16 15 16 19 16 17 19 16
7E | 13 14 6 8 19 3 13 11 11 11 4 | 11 11 7 9 15 8 11 9 9 11 8
8E | 9 14 11 9 20 5 10 8 6 10 4 | 15 20 20 15 12 17 19 17 16 13 15
9 | 8 11 7 6 10 4 10 14 7 11 3 | 22 27 22 24 23 25 29 25 24 24 23
10 | 4 9 6 5 9 3 10 12 8 11 3 | 20 27 19 17 9 18 28 12 14 22 17
11 | 9 18 11 9 13 3 11 8 6 16 4 | 12 19 10 12 14 11 13 12 10 8 9
12 | 12 21 5 12 17 4 16 12 12 18 5 | 15 16 11 16 10 13 14 14 13 10 11
13 | 11 13 11 11 17 5 10 12 11 18 4 | 13 14 13 14 13 13 18 15 13 11 10
14 | 8 13 9 13 15 4 9 10 9 17 4 | 13 17 11 14 13 12 13 14 14 13 11
15 | 8 15 12 12 14 5 13 13 12 14 4 | 26 33 25 20 24 23 32 17 20 19 22
16 | 13 23 8 17 22 6 11 37 13 18 7 | 16 15 13 15 12 13 12 29 14 15 8
17E | 11 15 6 9 21 2 12 14 12 8 4 | 13 12 10 14 15 10 12 14 12 8 10
18 | 9 18 8 6 9 5 10 14 8 12 4 | 15 8 12 12 8 11 10 16 11 16 12
19E | 11 14 6 7 25 4 13 13 16 7 4 | 13 14 12 13 22 11 14 12 13 11 9
20 | 7 12 11 11 10 5 11 13 10 12 4 | 15 9 13 8 7 10 10 13 12 13 10
21 | 10 11 12 12 16 4 13 14 8 29 5 | 12 15 11 14 12 11 14 14 13 17 10
22 | 5 7 9 7 8 3 9 8 9 13 3 | 10 11 10 10 7 10 12 7 11 12 9
23 | 11 26 7 12 15 4 13 11 10 19 5 | 15 16 14 23 17 18 19 21 18 17 16
24E | 9 12 12 7 26 7 10 9 8 15 4 | 10 14 14 11 16 12 14 12 12 14 11
25 | 7 11 6 8 13 4 8 10 9 13 3 | 11 14 11 11 10 9 13 10 11 10 9
26 | 8 9 5 10 13 4 8 7 5 10 3 | 17 19 16 16 13 15 16 15 15 14 15
27E | 10 12 10 9 22 5 9 7 5 10 4 | 18 21 22 17 23 19 19 20 18 17 18
28 | 8 13 8 8 19 4 10 13 10 19 4 | 14 18 13 15 12 14 18 15 16 9 12
29E | 14 21 6 15 17 6 17 10 13 9 5 | 12 16 10 13 13 11 13 12 14 8 10
30E | 11 12 10 8 23 4 10 9 6 9 4 | 18 21 22 18 16 19 20 19 17 22 18
31E | 15 11 8 11 20 4 8 10 10 10 4 | 14 15 12 15 15 13 14 13 15 16 12
32 | 6 10 7 6 10 4 8 8 7 12 3 | 10 15 9 13 9 10 13 10 9 15 10
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 9 10 16 4 11 13 9 14 |T 14 17 13 14 13 14 16 14 14 14 12
WRMS | 9 14 9 8 15 4 11 11 8 13 |NE 15 17 14 15 12 14 17 15 14 15 13
MEDI | 9 12 8 9 15 4 10 11 9 12 |MD 14 16 13 15 13 13 14 14 14 14 11
Table 3.1952.1 GPS week: 1952 Day: 1 MJD: 57909.000
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 11 5 9 7 4 9 6 8 12 3 | 10 14 11 10 10 10 14 11 12 13 10
2 | 8 12 8 11 14 3 10 10 10 13 4 | 12 13 11 13 13 12 15 15 12 9 11
3 | 7 12 9 6 9 2 12 6 6 12 3 | 10 21 11 12 8 11 21 11 10 15 10
X4E | 3 --- --- --- --- 29 28 --- --- --- 0 | 30 --- --- --- --- 32 30 --- --- --- 30
5 | 9 9 9 6 10 3 9 11 8 9 3 | 18 15 14 16 10 14 15 16 15 18 14
6 | 5 10 5 6 7 4 11 7 8 8 2 | 16 22 16 17 14 17 22 17 18 19 16
7E | 11 15 6 10 12 3 12 10 10 10 4 | 9 12 7 8 12 8 11 10 9 12 7
8E | 15 24 11 8 15 5 10 7 6 7 4 | 14 27 20 14 14 16 21 17 16 13 15
9 | 5 14 6 5 9 3 11 14 8 7 3 | 20 24 18 19 17 21 26 24 18 23 19
10 | 5 11 7 6 9 3 11 10 7 11 3 | 14 27 16 16 9 17 26 11 13 21 15
11 | 8 16 8 8 11 4 9 7 6 11 3 | 12 18 11 12 12 11 13 12 11 7 10
12 | 12 20 5 11 15 3 16 10 9 14 4 | 14 15 11 15 11 13 16 15 14 8 11
13 | 11 12 12 11 14 4 12 12 10 16 4 | 12 16 12 15 14 14 19 14 12 9 10
14 | 12 9 10 11 15 4 10 11 12 12 4 | 13 13 11 12 13 11 12 14 14 11 11
15 | 10 14 12 11 14 6 12 13 10 13 4 | 24 29 24 20 19 19 27 17 17 18 20
16 | 14 22 10 15 21 8 12 36 15 19 7 | 14 13 13 13 13 13 15 32 14 17 7
17E | 14 16 7 8 14 3 13 12 10 7 4 | 12 12 10 13 13 11 12 16 14 11 10
18 | 7 19 8 8 8 3 14 13 9 10 4 | 11 9 12 9 6 9 9 14 7 14 8
19E | 16 14 7 8 13 5 11 10 11 9 4 | 10 12 10 11 13 11 13 13 12 10 8
20 | 8 12 11 8 9 4 11 12 11 9 3 | 13 8 11 10 9 9 9 13 12 11 9
21 | 9 13 10 11 15 3 10 14 9 16 4 | 11 15 11 15 12 11 14 14 12 12 10
22 | 6 7 8 7 9 4 5 7 8 13 3 | 8 12 9 12 7 10 11 8 11 13 9
23 | 9 25 9 11 14 3 15 10 10 15 4 | 14 16 12 19 13 16 18 19 16 17 14
24E | 12 12 11 7 15 7 11 8 10 10 4 | 12 17 13 14 10 12 15 12 15 17 12
25 | 6 10 5 7 11 4 11 11 6 8 3 | 9 12 9 13 9 9 13 9 9 12 9
26 | 7 10 4 5 10 3 9 7 7 8 2 | 16 20 16 15 14 16 19 15 14 14 14
27E | 13 15 9 6 15 4 11 8 6 7 3 | 15 22 22 16 16 17 22 19 17 18 17
28 | 12 15 7 11 15 4 9 11 10 21 4 | 11 17 12 14 11 13 17 15 15 13 11
29E | 12 20 6 12 18 4 16 10 10 9 4 | 12 17 9 14 18 10 13 12 11 9 11
30E | 11 14 9 10 12 3 9 10 9 6 3 | 14 17 16 14 12 15 18 16 14 16 13
31E | 13 13 6 7 20 3 8 11 11 11 4 | 11 15 9 12 12 11 13 13 12 15 9
32 | 7 11 8 8 10 4 9 9 9 10 3 | 10 13 8 10 9 8 11 9 8 12 8
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 8 9 13 4 11 12 9 12 |T 13 16 12 13 12 13 16 14 13 13 12
WRMS | 9 15 8 9 13 4 11 11 8 13 |NE 13 16 12 14 11 13 16 14 13 14 11
MEDI | 9 13 8 8 13 4 11 10 9 10 |MD 12 15 11 14 12 12 15 14 13 13 11
Table 3.1952.2 GPS week: 1952 Day: 2 MJD: 57910.000
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 6 6 10 4 10 5 8 13 3 | 9 15 12 11 12 11 16 11 11 13 10
2 | 7 14 8 9 13 3 13 8 8 13 3 | 11 14 11 14 13 12 15 14 12 8 10
3 | 9 13 9 6 11 3 12 6 10 14 3 | 7 20 10 14 9 11 19 10 10 16 10
X4E | 2 --- --- --- --- 30 33 --- --- --- 0 | 34 --- --- --- --- 28 28 --- --- --- 34
5 | 8 9 8 7 10 3 11 11 8 11 3 | 16 15 14 14 8 14 15 15 13 17 13
6 | 6 9 6 4 9 3 8 8 7 7 2 | 15 22 17 16 15 16 21 16 18 17 16
7E | 12 13 5 9 11 4 15 8 9 9 3 | 9 12 7 9 10 8 12 10 10 11 7
8E | 9 20 11 9 23 5 10 10 4 10 4 | 15 25 20 15 21 16 21 17 16 14 16
9 | 6 11 7 6 11 4 8 5 7 10 2 | 23 25 22 22 23 23 29 23 24 25 22
10 | 6 12 8 7 10 2 14 9 5 12 3 | 13 26 16 13 9 16 26 12 14 21 14
11 | 9 15 10 8 13 4 9 7 5 15 3 | 12 16 12 12 13 11 15 12 12 8 10
12 | 11 20 6 13 18 4 17 11 10 18 5 | 13 16 10 13 12 12 16 15 14 8 11
13 | 13 11 13 11 14 5 17 12 9 16 4 | 13 15 13 15 14 13 19 14 11 11 10
14 | 7 11 12 13 18 3 12 8 9 16 4 | 14 14 13 14 15 12 12 14 15 14 12
15 | 11 16 11 12 17 4 16 13 9 15 4 | 26 30 22 18 20 21 30 17 18 21 20
16 | 13 24 8 15 24 7 14 36 13 17 7 | 13 13 12 12 12 12 14 31 13 15 7
17E | 11 16 8 7 16 3 14 17 11 9 4 | 12 15 10 12 12 11 14 17 13 11 10
18 | 7 22 9 9 9 3 18 11 6 11 4 | 11 9 10 9 8 9 11 15 11 15 10
19E | 13 15 6 6 18 4 15 10 13 8 4 | 10 11 11 11 13 10 13 13 12 10 9
20 | 9 12 12 11 10 4 10 16 8 10 4 | 11 9 12 9 8 9 8 13 13 9 8
21 | 10 13 10 13 19 3 12 13 9 18 4 | 12 14 11 13 13 11 12 13 13 14 10
22 | 8 9 9 6 9 4 6 8 9 13 3 | 6 11 9 10 9 9 12 8 13 14 8
23 | 11 26 9 11 12 4 16 12 10 18 5 | 15 17 12 21 17 16 19 20 17 18 15
24E | 7 18 11 10 19 4 10 7 8 12 4 | 11 23 13 11 11 11 12 14 13 18 12
25 | 6 14 6 15 17 5 10 11 9 11 4 | 10 16 10 13 11 10 12 8 12 11 9
26 | 7 8 5 5 15 2 9 7 5 9 3 | 15 19 16 15 14 15 18 15 15 13 14
27E | 12 14 10 7 19 4 11 10 4 7 4 | 17 23 23 19 20 19 23 21 18 20 19
28 | 13 14 9 10 17 4 12 11 11 23 5 | 11 19 13 17 12 14 17 17 17 12 12
29E | 8 22 5 13 23 5 18 10 10 10 4 | 11 13 10 14 11 10 13 11 14 8 10
30E | 10 13 10 9 15 3 10 8 6 6 3 | 15 18 19 15 14 16 19 15 15 18 15
31E | 10 9 7 11 27 4 10 13 8 12 4 | 11 13 10 12 15 11 12 14 12 14 11
32 | 6 10 9 9 13 2 8 8 8 12 3 | 11 15 10 13 10 9 12 9 10 13 10
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 9 10 16 4 13 12 9 13 |T 13 16 13 13 13 13 16 14 13 14 12
WRMS | 9 15 9 9 15 4 13 10 7 14 |NE 13 16 13 14 12 13 16 14 14 14 11
MEDI | 9 13 9 9 15 4 12 10 8 12 |MD 12 15 12 13 12 12 15 14 13 14 10
Table 3.1952.3 GPS week: 1952 Day: 3 MJD: 57911.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 8 5 7 9 3 8 6 7 10 2 | 14 19 14 13 13 14 17 15 15 15 14
2 | 7 11 8 9 13 3 10 7 9 11 3 | 12 15 11 14 12 12 14 15 13 11 11
3 | 11 12 8 7 10 4 12 7 8 14 3 | 9 21 11 15 9 13 21 13 14 17 12
X4E | 3 --- --- --- --- 27 25 --- --- --- 0 | 26 --- --- --- --- 34 29 --- --- --- 27
5 | 7 12 8 9 13 3 11 8 7 11 3 | 15 16 13 15 8 15 15 15 16 18 14
6 | 6 9 4 5 7 3 8 9 6 6 2 | 16 23 16 16 14 17 21 17 18 17 16
7E | 14 14 5 10 15 4 13 9 8 8 4 | 11 13 8 9 15 8 11 11 11 12 9
8E | 13 24 11 10 23 4 10 7 6 8 5 | 16 27 20 16 21 17 19 17 17 13 16
9 | 5 9 6 8 12 2 8 6 5 7 2 | 17 25 17 18 19 18 24 19 18 17 18
10 | 7 11 6 6 11 3 12 9 8 12 3 | 13 27 14 14 11 16 26 15 17 22 16
11 | 14 11 9 8 12 4 9 7 6 10 3 | 15 17 14 13 12 13 15 15 13 11 12
12 | 13 21 5 13 19 3 15 11 14 18 5 | 13 16 11 14 11 12 15 15 15 9 11
13 | 12 12 10 11 14 3 12 10 9 15 4 | 12 16 14 16 13 12 19 14 14 9 11
14 | 8 12 9 10 21 3 13 11 11 16 4 | 14 18 12 17 14 14 15 18 17 15 14
15 | 11 17 10 12 16 5 14 14 12 15 5 | 28 33 27 22 22 25 34 20 23 23 24
16 | 14 24 9 16 22 7 16 37 12 17 7 | 17 14 13 15 14 13 14 31 17 18 10
17E | 13 15 5 8 25 4 14 11 8 11 4 | 13 14 11 12 14 12 14 15 14 10 10
18 | 6 22 6 10 8 3 15 13 8 10 4 | 11 12 8 9 9 9 11 14 13 14 10
19E | 14 15 5 8 20 4 12 11 10 10 4 | 11 13 11 10 16 11 14 13 13 10 9
20 | 6 15 9 14 9 3 10 15 10 10 4 | 12 12 11 10 8 9 9 13 14 11 9
21 | 10 13 8 13 16 4 11 14 9 16 4 | 13 16 13 13 14 12 15 15 13 14 11
22 | 6 8 8 6 9 4 6 9 10 15 3 | 10 11 10 14 8 11 12 11 15 17 11
23 | 10 24 8 12 13 3 13 11 10 15 4 | 18 19 15 25 19 19 21 23 20 20 18
24E | 14 18 12 9 28 6 11 10 11 15 5 | 15 19 17 13 23 14 14 17 16 19 15
25 | 8 8 6 26 14 4 8 11 8 7 4 | 12 14 11 15 13 11 13 9 12 9 10
26 | 8 9 6 6 13 3 7 10 8 9 3 | 17 20 16 17 15 16 19 16 18 15 16
27E | 15 15 10 6 20 4 9 9 5 5 4 | 18 23 21 18 18 19 20 20 20 18 18
X28 | 12 14 6 --- 15 6 11 13 14 --- 5 | 12 17 13 --- 13 15 19 16 16 --- 13
29E | 14 26 7 13 22 4 19 16 11 10 5 | 14 16 12 15 13 12 13 14 13 10 12
30E | 14 13 10 9 12 5 10 9 5 5 4 | 18 22 20 16 12 17 19 18 16 18 17
31E | 12 11 5 10 29 3 5 14 8 10 4 | 12 16 10 13 12 12 13 14 13 14 11
32 | 7 9 7 8 12 4 7 10 7 12 3 | 12 16 11 15 10 12 13 12 10 17 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 8 11 17 4 11 12 9 12 |T 14 18 13 14 13 14 17 15 15 14 13
WRMS | 10 15 8 10 15 4 11 10 8 11 |NE 14 18 13 15 12 14 17 16 15 15 13
MEDI | 10 13 8 9 14 4 11 10 8 10 |MD 13 16 13 15 13 13 15 15 15 15 12
Table 3.1952.4 GPS week: 1952 Day: 4 MJD: 57912.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 12 7 9 8 4 10 7 8 11 3 | 21 24 21 19 19 21 25 22 22 23 21
2 | 7 14 8 10 15 3 12 9 8 12 3 | 13 17 13 16 15 14 17 16 14 14 13
3 | 9 12 8 7 11 3 11 8 7 11 3 | 10 20 13 13 10 12 20 12 14 14 12
X4E | 4 --- --- --- --- 28 26 --- --- --- 0 | 24 --- --- --- --- 30 28 --- --- --- 25
5 | 12 15 9 8 12 4 14 8 7 9 3 | 17 21 19 21 16 19 19 19 22 22 19
6 | 4 9 4 5 9 3 10 9 8 6 2 | 18 25 20 19 18 18 27 18 18 22 19
7E | 14 13 7 6 10 3 12 7 10 7 3 | 17 18 14 17 17 16 20 18 15 18 16
8E | 12 18 9 9 24 6 8 8 6 10 4 | 18 23 19 15 17 17 22 18 18 16 16
9 | 7 12 6 4 14 3 13 4 8 9 3 | 20 27 20 20 19 22 25 23 24 23 21
10 | 5 11 6 7 7 4 11 7 6 8 2 | 15 26 16 16 11 16 27 16 15 20 16
11 | 12 13 10 10 12 5 11 7 5 14 4 | 16 18 15 14 13 14 19 18 15 15 14
12 | 11 23 6 13 17 3 14 11 9 16 4 | 19 21 16 18 18 18 22 20 20 18 17
13 | 17 13 11 11 19 5 13 13 11 15 5 | 14 20 14 16 18 15 21 14 15 12 13
14 | 10 12 11 13 18 3 10 11 10 17 4 | 18 20 18 19 18 19 19 21 21 21 19
15 | 12 14 12 10 17 4 12 13 11 17 5 | 28 32 28 24 24 25 31 20 24 23 24
16 | 15 27 8 15 22 7 14 37 12 15 7 | 23 22 21 24 18 20 20 34 20 23 18
17E | 12 18 5 8 17 3 12 11 9 9 4 | 22 24 19 20 19 20 22 22 20 19 19
18 | 9 21 7 10 9 3 12 13 8 11 4 | 11 10 9 9 8 8 11 16 10 13 9
19E | 12 13 5 7 21 4 11 9 9 10 4 | 19 20 19 18 23 18 22 21 16 18 18
20 | 8 11 9 12 11 5 11 14 11 11 4 | 14 14 13 13 12 12 12 15 15 15 12
21 | 9 12 10 10 16 3 12 10 9 18 4 | 19 20 17 18 16 16 19 17 18 18 16
22 | 6 8 9 7 11 4 6 9 8 15 3 | 14 15 14 12 12 14 17 14 17 18 14
23 | 12 24 9 11 16 5 13 11 11 15 5 | 18 21 18 25 17 21 20 25 20 23 20
24E | 10 21 11 16 20 5 12 12 10 11 5 | 20 22 17 20 19 17 17 22 23 24 18
25 | 8 14 6 13 14 6 11 6 8 15 4 | 12 16 12 14 13 11 14 12 14 13 11
26 | 7 10 5 5 12 2 10 11 7 7 3 | 20 22 20 21 16 19 21 19 21 20 19
27E | 11 14 10 7 25 5 9 13 6 9 4 | 23 22 21 20 25 18 21 22 18 21 20
28 | 15 13 9 12 19 5 10 13 9 19 5 | 12 18 13 9999 15 15 20 19 19 9999 14
29E | 21 26 8 16 19 4 14 13 16 12 6 | 18 15 13 16 14 14 16 14 15 12 13
30E | 13 13 11 7 18 4 10 9 7 7 4 | 18 21 22 20 15 19 24 20 18 20 18
31E | 12 11 8 9 28 5 8 13 10 11 4 | 13 13 10 13 15 13 12 16 15 14 11
32 | 8 8 9 7 13 4 7 7 7 10 3 | 14 15 14 15 16 14 16 15 17 17 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 8 10 16 4 11 12 9 12 |T 17 20 16 17 16 17 20 18 17 18 16
WRMS | 10 15 8 9 16 4 11 10 8 12 |NE 16 20 16 17 15 16 20 18 18 18 16
MEDI | 10 13 8 9 16 4 11 10 8 11 |MD 18 20 17 18 16 17 20 18 18 18 16
Table 3.1952.5 GPS week: 1952 Day: 5 MJD: 57913.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 10 6 9 13 3 8 5 9 10 3 | 13 18 13 12 15 13 15 12 14 16 12
2 | 7 11 9 12 16 4 10 10 9 12 4 | 13 13 10 14 15 13 15 13 14 10 11
3 | 12 13 9 9 8 3 13 8 7 11 3 | 9 21 9 16 9 14 22 12 16 16 12
X4E | 6 --- --- --- --- 26 24 --- --- --- 0 | 21 --- --- --- --- 27 25 --- --- --- 21
5 | 8 14 9 7 10 2 12 9 9 10 3 | 15 15 12 17 10 15 15 14 21 19 14
6 | 7 10 5 7 8 4 9 6 8 8 2 | 18 25 18 19 19 18 22 23 21 22 19
7E | 19 15 4 9 18 5 15 10 8 7 4 | 17 15 10 10 16 11 13 12 12 13 11
8 | 26 24 11 9 18 8 11 7 7 8 5 | 34 36 28 29 22 26 29 28 29 30 27
9 | 11 11 6 9 9 4 8 6 8 12 3 | 17 26 18 19 18 21 25 21 21 22 19
10 | 7 11 6 8 11 4 12 7 8 10 3 | 13 26 14 14 11 14 24 14 15 18 14
11E | 14 10 10 7 13 3 10 7 6 10 3 | 16 16 15 13 11 14 16 16 16 12 13
12 | 11 20 8 13 17 5 14 9 14 17 5 | 16 18 13 14 15 14 17 17 16 13 13
13 | 11 13 15 9 14 4 12 11 11 21 5 | 13 18 14 15 15 14 19 13 14 12 11
14 | 9 13 12 15 17 4 9 12 9 15 5 | 18 19 14 17 13 15 16 18 17 20 15
15 | 11 17 11 10 14 3 14 13 13 16 5 | 26 29 25 22 23 23 29 20 22 22 22
16 | 17 25 9 16 20 8 16 37 13 19 7 | 14 17 12 17 13 12 14 31 14 17 8
17E | 13 17 7 8 17 4 12 10 9 12 4 | 16 18 12 15 14 14 17 17 18 16 14
18 | 7 18 8 9 10 5 15 14 11 10 4 | 11 9 7 9 9 8 8 18 10 14 9
19E | 13 17 6 8 18 7 10 11 12 12 4 | 13 17 13 13 17 14 18 15 18 12 13
20 | 8 15 10 11 12 5 12 14 11 10 4 | 12 9 8 8 10 9 7 13 11 11 7
21 | 12 10 10 10 20 3 13 14 10 18 5 | 12 13 12 15 14 12 17 16 16 12 11
22 | 9 9 10 7 10 3 6 8 11 13 3 | 11 13 9 11 9 12 14 10 18 17 11
23 | 15 25 8 14 16 4 15 14 10 15 5 | 17 20 15 27 17 21 20 25 21 22 19
24E | 11 14 12 11 21 6 12 14 12 12 5 | 13 16 15 13 17 13 16 21 13 21 14
25 | 7 10 6 8 13 10 11 7 11 12 3 | 13 15 11 9 14 10 14 12 11 12 11
26 | 7 9 6 6 10 6 7 12 6 10 3 | 17 22 17 20 15 16 19 14 16 14 16
27 | 21 16 10 8 18 5 12 10 6 16 5 | 27 28 26 27 23 24 24 28 25 32 26
28 | 20 11 10 11 20 4 10 12 10 18 5 | 13 17 13 9999 13 14 20 19 17 9999 13
29E | 11 29 7 13 19 5 17 11 12 11 5 | 12 15 8 11 12 10 12 12 12 7 9
30E | 31 16 10 8 17 7 12 11 8 8 5 | 24 20 19 16 17 16 18 16 17 19 16
31E | 8 12 10 7 16 4 9 12 7 9 3 | 15 17 11 11 21 11 13 12 13 15 12
32 | 10 10 8 8 11 4 8 8 8 9 3 | 11 14 9 10 9 8 11 9 10 12 9
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 15 9 10 15 5 12 12 10 13 |T 15 18 13 15 14 14 17 16 16 16 14
WRMS | 11 15 10 9 14 5 12 10 8 12 |NE 14 17 13 15 13 14 17 16 15 16 13
MEDI | 11 13 9 9 16 4 12 10 9 12 |MD 14 17 13 14 15 14 17 16 16 16 13
Table 3.1952.6 GPS week: 1952 Day: 6 MJD: 57914.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 5 8 9 4 8 10 9 10 3 | 17 24 18 16 18 18 24 18 20 23 18
2 | 9 15 9 12 16 5 11 18 9 13 4 | 14 16 13 16 16 14 17 16 15 12 12
3 | 9 15 11 8 10 3 11 7 8 9 3 | 13 24 10 15 9 15 25 16 20 20 15
X4E | 4 --- --- --- --- 30 23 --- --- --- 0 | 21 --- --- --- --- 27 27 --- --- --- 22
5 | 9 14 10 7 6 4 8 11 11 10 3 | 21 22 19 25 17 21 22 20 27 24 21
6 | 11 10 6 6 8 4 8 21 7 7 3 | 23 32 25 24 22 24 28 30 26 28 25
7E | 14 14 7 10 11 4 13 15 11 8 4 | 16 16 13 15 18 14 15 18 16 16 14
8 | 13 22 12 9 34 6 10 9 6 9 5 | 24 27 26 23 19 23 25 23 22 23 21
9 | 8 11 8 7 8 3 9 7 7 6 3 | 18 26 18 20 19 21 25 20 21 20 19
10 | 8 11 9 6 10 5 11 6 8 7 3 | 22 33 18 20 14 21 33 20 20 24 20
11E | 11 10 9 8 6 5 10 12 6 8 3 | 21 20 15 16 16 16 18 15 17 17 16
12 | 14 22 7 14 16 3 14 10 11 17 5 | 20 24 17 17 20 17 22 20 19 18 17
13 | 12 15 12 10 14 6 10 12 10 16 5 | 14 20 14 18 13 16 19 17 16 14 13
14 | 7 10 9 13 20 6 10 11 12 15 4 | 17 19 15 16 16 16 19 19 20 20 16
15 | 9 15 13 11 11 4 12 12 11 14 4 | 28 33 29 22 22 24 31 19 24 22 24
16 | 15 23 9 18 21 8 13 37 13 18 7 | 19 19 17 20 15 16 18 30 16 19 13
17E | 15 16 7 14 17 3 11 10 10 9 4 | 20 22 17 22 23 19 22 21 20 17 18
18 | 6 18 7 11 10 6 11 13 10 10 4 | 15 12 10 11 9 12 11 21 12 18 12
19E | 17 14 6 12 18 4 9 13 11 11 5 | 20 19 19 19 18 19 23 20 20 18 17
20 | 7 14 10 9 6 4 8 12 7 9 3 | 15 13 14 12 12 12 13 15 13 15 13
21 | 11 11 9 15 16 5 10 14 10 17 4 | 15 16 12 18 13 13 17 16 14 16 12
22 | 9 9 9 7 9 4 7 11 7 12 3 | 13 17 11 15 10 14 18 12 19 20 14
23 | 13 26 9 14 14 4 15 16 10 17 5 | 18 18 13 25 16 20 19 23 20 22 18
24E | 14 19 11 12 17 6 13 13 11 11 5 | 16 20 15 15 16 14 18 19 17 20 15
25 | 9 13 5 13 8 7 8 9 8 7 3 | 16 20 14 13 13 12 16 13 12 14 13
26 | 9 13 6 9 15 5 8 9 9 8 3 | 18 21 17 20 15 16 20 17 16 19 17
27 | 11 12 11 9 24 6 11 9 7 8 4 | 24 24 25 23 22 23 24 23 21 24 22
28 | 14 13 8 15 16 6 10 12 13 20 5 | 12 16 14 9999 14 15 20 19 17 9999 14
29E | 9 34 6 13 18 3 16 14 10 9 5 | 14 20 9 10 15 11 13 14 14 10 10
30E | 13 13 11 8 17 4 10 10 11 5 4 | 19 18 21 17 16 18 20 18 18 19 18
31E | 11 11 5 10 18 4 8 13 15 8 4 | 11 17 11 13 12 12 15 15 18 16 12
32 | 11 9 9 7 11 5 6 7 7 9 3 | 11 13 9 7 10 8 12 9 12 14 9
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 9 11 15 5 11 13 10 12 |T 17 20 16 17 15 16 20 18 18 18 16
WRMS | 11 15 9 9 13 5 11 11 8 11 |NE 17 20 15 17 14 16 20 18 18 19 15
MEDI | 11 14 9 10 14 4 10 12 10 9 |MD 17 20 15 17 16 16 19 19 18 19 16
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 4.1952 GPS week: 1952 MJD: 57908.0-57914.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 8 7 18 |U 5 6 18 |U 7 7 19 |
emr | emr 2975 |U 8 11 24 |U 6 7 25 | 9 7 21 |
esa | esa 2976 | 7 8 20 |U 5 7 20 | 7 6 18 |
gfz | gfz 2960 |U 7 9 20 |U 6 7 21 |U 7 9 20 |
grg | grg 2970 |U 8 11 22 |U 6 8 24 | 7 7 20 |
igr | igr 2973 | 7 8 20 | 5 6 19 | 7 6 18 |
igs | igs 2975 | 7 8 20 | 5 6 20 | 7 6 18 |
jpl | jpl 3072 | 9 9 22 | 5 7 23 |U 8 6 18 |
mit | mit 2976 |U 8 9 23 |U 7 8 27 |U 10 8 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 5.1952.0 GPS week: 1952 Day: 0 MJD: 57908.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 14 18 | 6 8 23 | 8 11 28 |
emr | emr 2976 | 10 12 36 | 6 8 28 | 11 7 27 |
esa | esa 2976 | 9 14 29 | 6 9 24 | 8 7 22 |
gfz | gfz 2976 | 10 14 29 | 6 9 25 | 9 7 22 |
grg | grg 2976 | 10 13 27 | 6 10 26 | 8 7 22 |
igr | igr 2976 | 9 13 29 | 6 9 24 | 9 7 22 |
igs | igs 2976 | 10 15 30 | 6 9 24 | 8 7 22 |
jpl | jpl 3072 | 10 11 24 | 6 9 27 | 10 6 23 |
mit | mit 2976 | 10 13 31 | 7 9 21 | 26 18 47 |
Table 5.1952.1 GPS week: 1952 Day: 1 MJD: 57909.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 5 11 | 6 8 24 | 6 4 16 |
emr | emr 2976 | 6 7 17 | 7 9 29 | 6 5 19 |
esa | esa 2976 | 4 5 13 | 6 8 23 | 6 5 14 |
gfz | gfz 2966 | 4 4 12 | 7 8 24 | 9 17 29 |
grg | grg 2959 | 5 7 15 | 7 10 29 | 6 5 18 |
igr | igr 2976 | 4 5 13 | 6 7 24 | 6 5 15 |
igs | igs 2976 | 4 4 12 | 6 8 24 | 6 4 15 |
jpl | jpl 3072 | 8 7 18 | 6 9 27 | 7 5 16 |
mit | mit 2976 | 6 6 15 | 11 10 32 | 7 5 17 |
Table 5.1952.2 GPS week: 1952 Day: 2 MJD: 57910.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 7 18 | 4 6 17 | 8 10 22 |
emr | emr 2976 | 8 11 22 | 5 9 22 | 9 10 25 |
esa | esa 2976 | 7 9 21 | 5 7 19 | 8 11 22 |
gfz | gfz 2976 | 9 9 22 | 8 8 25 | 7 12 23 |
grg | grg 2975 | 10 19 30 | 6 9 22 | 9 10 27 |
igr | igr 2976 | 6 8 21 | 5 6 18 | 8 11 22 |
igs | igs 2976 | 7 8 21 | 5 7 18 | 8 11 22 |
jpl | jpl 3072 | 10 10 24 | 6 8 23 | 8 9 21 |
mit | mit 2976 | 7 9 26 | 5 7 24 | 8 8 22 |
Table 5.1952.3 GPS week: 1952 Day: 3 MJD: 57911.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 7 6 17 | 4 5 18 | 7 4 16 |
emr | emr 2969 | 8 11 22 | 6 7 26 | 9 5 18 |
esa | esa 2976 | 6 7 18 | 5 6 21 | 7 5 18 |
gfz | gfz 2880 | 6 8 19 | 7 9 19 | 7 5 16 |
grg | grg 2967 | 6 9 20 | 7 7 27 | 7 7 18 |
igr | igr 2957 | 6 7 18 | 4 6 18 | 7 4 17 |
igs | igs 2969 | 6 7 18 | 5 6 20 | 7 4 16 |
jpl | jpl 3072 | 8 9 20 | 5 7 21 | 8 5 17 |
mit | mit 2976 | 7 9 21 | 5 6 19 | 7 4 17 |
Table 5.1952.4 GPS week: 1952 Day: 4 MJD: 57912.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 6 22 | 3 4 15 | 8 4 18 |
emr | emr 2976 | 8 12 25 | 6 5 25 | 9 5 23 |
esa | esa 2976 | 6 7 21 | 4 5 19 | 7 5 19 |
gfz | gfz 2976 | 7 9 22 | 6 6 20 | 7 7 20 |
grg | grg 2971 | 7 10 21 | 5 6 24 | 7 6 21 |
igr | igr 2976 | 6 8 22 | 4 4 17 | 8 4 19 |
igs | igs 2976 | 6 7 21 | 4 5 18 | 7 4 19 |
jpl | jpl 3072 | 8 8 27 | 5 6 25 | 8 6 19 |
mit | mit 2976 | 7 7 24 | 9 10 49 | 9 5 18 |
Table 5.1952.5 GPS week: 1952 Day: 5 MJD: 57913.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 8 25 | 3 5 15 | 7 7 16 |
emr | emr 2976 | 10 11 28 | 6 6 23 | 8 6 17 |
esa | esa 2976 | 9 8 25 | 4 5 16 | 8 6 15 |
gfz | gfz 2976 | 8 7 24 | 4 5 18 | 7 6 14 |
grg | grg 2976 | 9 8 24 | 5 6 21 | 8 8 15 |
igr | igr 2976 | 8 7 24 | 3 4 15 | 7 6 16 |
igs | igs 2976 | 8 7 24 | 4 5 17 | 8 7 14 |
jpl | jpl 3072 | 11 9 28 | 4 6 17 | 7 6 15 |
mit | mit 2976 | 8 7 26 | 5 6 19 | 8 8 16 |
Table 5.1952.6 GPS week: 1952 Day: 6 MJD: 57914.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 8 14 | 5 6 18 | 7 7 18 |
emr | emr 2976 | 8 14 18 | 8 7 23 | 9 7 19 |
esa | esa 2976 | 6 9 13 | 5 6 19 | 7 6 17 |
gfz | gfz 2976 | 7 10 16 | 6 6 19 | 7 7 16 |
grg | grg 2972 | 7 9 17 | 6 7 21 | 7 6 19 |
igr | igr 2976 | 6 10 14 | 6 6 18 | 7 8 18 |
igs | igs 2976 | 6 9 14 | 5 6 19 | 7 8 17 |
jpl | jpl 3072 | 7 9 15 | 6 7 22 | 8 7 18 |
mit | mit 2976 | 8 11 15 | 6 10 23 | 7 7 17 |
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 6.1952 GPS week: 1952 MJD: 57908.500-57914.500
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 -15 84 146 -3 | 12 17
| 19 20 75 108 4 | 5
emr uuuuu | -4 20 19 83 -7 | 40 43
| 15 19 78 59 6 | 5
esa uuuuu | 1 -11 -42 -11 -8 | 24 27
| 12 12 38 34 2 | 5
gfz uuuuu | -18 -4 70 -75 -3 | 21 24
| 27 12 147 165 4 | 4
grg uuuuu | 4 15 -2 -29 2 | -4 12
| 18 22 61 87 2 | 3
igr xxxxx | 1 -25 36 -1 -10 | 8 15
| 20 7 58 32 2 | 6
irf xxxxx | 1 -14 -14 -86 -3 | 1 14
| 7 8 19 17 8 | 6
jpl xxxxx | 9 -36 134 91 9 | 22 24
| 30 17 56 96 7 | 2
mit uuuuu | -24 -14 -31 -188 -4 | 27 29
| 8 7 65 50 5 | 5
ngs uuuuu | 3 -3 38 47 4 | 12 15
| 14 24 100 122 2 | 3
sio uuuux | 36 35 -158 6 -2 | 61 62
| 18 11 77 44 4 | 4
Table 7.1952.0 GPS week: 1952 Day: 0 MJD: 57908.500
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 -44 19 247 6 | 19 24
emr uuuuu | 1 -17 103 103 -19 | 47 50
esa uuuuu | -4 -15 -61 27 -7 | 30 34
gfz uuuuu | -19 -4 251 -129 2 | 25 29
grg uuuuu | 28 33 -11 50 1 | 0 13
igr xxxxx | -14 -22 31 -37 -7 | 16 21
irf xxxxx | 4 -14 -14 -101 -14 | 10 19
jpl xxxxx | 19 -44 140 125 -1 | 22 25
mit uuuuu | -15 -4 -43 -224 -6 | 33 36
ngs uuuuu | 9 41 -40 -54 0 | 16 20
sio uuuux | 30 53 -298 -74 0 | 66 67
Table 7.1952.1 GPS week: 1952 Day: 1 MJD: 57909.500
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 -15 50 314 -5 | 19 24
emr uuuuu | -9 21 19 62 -4 | 45 48
esa uuuuu | 2 -18 14 -18 -5 | 31 34
gfz uuuuu | -5 -23 220 -192 -1 | 26 29
grg uuuuu | 10 34 -92 78 2 | -1 13
igr xxxxx | 38 -30 -53 33 -10 | 16 21
irf xxxxx | 5 -18 -13 -83 -11 | 8 19
jpl xxxxx | 49 -44 61 228 14 | 23 25
mit uuuuu | -35 -9 11 -194 -6 | 32 35
ngs uuuuu | -10 3 -88 -28 4 | 15 20
sio uuuux | 5 38 -212 1 -5 | 66 67
Table 7.1952.2 GPS week: 1952 Day: 2 MJD: 57910.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 5 11 52 49 -8 | 14 16
emr uuuuu | 17 38 -66 204 -1 | 40 42
esa uuuuu | 14 -30 -3 -53 -7 | 26 27
gfz uuuuu | -45 -15 153 -332 -4 | 22 23
grg uuuuu | 3 26 -5 -7 3 | -4 8
igr xxxxx | 10 -26 12 10 -9 | 10 12
irf xxxxx | 8 -19 -4 -59 -5 | 2 10
jpl xxxxx | -2 -46 130 139 3 | 21 22
mit uuuuu | -23 -18 -12 -95 -6 | 28 29
ngs uuuuu | -2 3 -57 237 2 | 12 12
sio uuuux | 45 28 -133 36 0 | 61 61
Table 7.1952.3 GPS week: 1952 Day: 3 MJD: 57911.500
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 -5 68 37 -5 | 12 13
emr uuuuu | 5 24 -59 56 -7 | 41 42
esa uuuuu | -1 -2 -67 -31 -9 | 25 26
gfz uuuuu | -60 -2 97 -119 -10 | 21 22
grg uuuuu | -14 35 -7 -16 2 | -5 8
igr xxxxx | 2 -34 57 26 -10 | 9 11
irf xxxxx | 4 -17 5 -82 -3 | 0 8
jpl xxxxx | 22 -57 68 70 12 | 21 23
mit uuuuu | -16 -24 -4 -165 -6 | 26 27
ngs uuuuu | 29 -21 93 205 7 | 11 12
sio uuuux | 63 22 -150 -13 -9 | 60 61
Table 7.1952.4 GPS week: 1952 Day: 4 MJD: 57912.500
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 3 102 87 -4 | 7 14
emr uuuuu | 0 13 68 80 -6 | 37 41
esa uuuuu | 14 -9 -94 -8 -7 | 20 24
gfz uuuuu | -19 15 -114 81 -2 | 17 21
grg uuuuu | 13 -13 -12 -24 -2 | -8 13
igr xxxxx | -1 -12 92 25 -9 | 3 13
irf xxxxx | 0 -22 -8 -78 8 | -5 12
jpl xxxxx | 29 -19 189 139 19 | 19 21
mit uuuuu | -33 -20 50 -185 6 | 21 24
ngs uuuuu | -8 -6 104 -22 6 | 9 12
sio uuuux | 25 24 -71 -1 4 | 56 57
Table 7.1952.5 GPS week: 1952 Day: 5 MJD: 57913.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -17 -20 245 85 -3 | 7 13
emr uuuuu | -18 34 -46 23 -6 | 35 38
esa uuuuu | 5 4 -30 41 -11 | 18 22
gfz uuuuu | 20 5 -57 132 -2 | 17 21
grg uuuuu | -25 3 -1 -165 4 | -7 13
igr xxxxx | -5 -18 -6 -38 -12 | 2 13
irf xxxxx | -11 3 -55 -112 3 | -5 13
jpl xxxxx | -42 -9 136 -45 10 | 20 23
mit uuuuu | -19 -14 -153 -256 -3 | 22 25
ngs uuuuu | -5 -36 179 26 5 | 10 13
sio uuuux | 44 43 -153 27 -1 | 57 58
Table 7.1952.6 GPS week: 1952 Day: 6 MJD: 57914.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 18 -33 51 202 -2 | 9 16
emr uuuuu | -28 31 116 54 -6 | 37 40
esa uuuuu | -22 -3 -56 -34 -8 | 18 22
gfz uuuuu | 0 -1 -63 35 -2 | 19 24
grg uuuuu | 9 -13 115 -123 5 | -4 14
igr xxxxx | -24 -30 117 -29 -13 | 2 13
irf xxxxx | -7 -11 -9 -86 0 | -3 14
jpl xxxxx | -10 -30 213 -19 9 | 25 29
mit uuuuu | -25 -9 -66 -195 -4 | 24 27
ngs uuuuu | 5 -1 71 -35 5 | 13 18
sio uuuux | 37 35 -87 65 -1 | 58 60
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