[IGSREPORT-25144] Wk 1938 IGS Final Orbits
acc
acc at igs.org
Sun Mar 19 15:34:04 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1938 (Feb 26, 2017 - Mar 04, 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:
igs1938[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1938[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1938[0-6].cls IGS GPS clock combination summary report.
igs19387.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19387.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 | FAA1 SYOG TIXI SYOG TIXI
0 | EMR | 25 25 SYOG GRAZ HERS SYOG
0 | ESA | LMMF MATE CHTI LMMF MAL2 MATE
0 | GFZ | ALRT BJNM FAA1 GMSD HERS MAL2 MATE ALRT BJNM FAA1
0 | GFZ | GMSD HERS MAL2 MATE
0 | GRG | 10 16 10 16 KIT3 NICO REUN RIO2 SYOG XMIS CHTI FAA1
0 | GRG | KIT3 NICO REUN RIO2 SYOG XMIS
0 | MIT | MATE MATE
1 | COD | HOLB IENG KOUR MAR6 MGUE NNOR PETS TIXI HOLB IENG
1 | COD | MAR6 MGUE NNOR PETS TIXI
1 | EMR | BJNM
1 | ESA | CHTI OHI3
1 | GFZ | BJNM GMSD HERS BJNM GMSD HERS SYOG
1 | GRG | CRO1 GLSV KIRU KIT3 KOUR LHAZ MAW1 NICO RIO2 SYOG
1 | GRG | CHTI CRO1 FAA1 GLSV KIRU KIT3 LHAZ MAW1 NICO NRMD
1 | GRG | RIO2 SYOG
1 | MIT | NNOR VILL NNOR VILL
2 | COD | TIXI PIMO TIXI
2 | EMR | HERS SYOG
2 | ESA | AUCK HARB HOFN AUCK HARB SYOG
2 | GFZ | FAA1 GMSD HERS MAL2 FAA1 GMSD HERS HOFN MAL2
2 | GRG | ADIS CRO1 FAA1 GLSV KIT3 NICO NKLG RIO2 SYOG ADIS
2 | GRG | FAA1 GLSV KIT3 NICO NKLG PIMO RIO2 SYOG
2 | MIT | ALRT ALRT
3 | COD | FAA1 MAL2 WHIT CRO1 FAA1 MAL2 OPMT REUN WHIT YELL
3 | EMR | 25 25 YAR2 CHUR SYOG WHIT YAR2
3 | ESA | WHIT HOFN KOUR TRO1
3 | GFZ | FAA1 GMSD HERS MAL2 REUN CHTI FAA1 GMSD HERS MAL2
3 | GFZ | REUN
3 | GRG | ADIS CHTI GLSV HOFN KIT3 LHAZ NICO RIO2 STJO SYOG
3 | GRG | TRO1 ADIS CHTI GLSV LHAZ SYOG TRO1
3 | MIT | NICO SUTH TRO1 MAW1 SUTH TRO1
4 | COD | 12 12 KIRU LMMF SCH2 TIXI CHTI FAIR KIRU LMMF SCH2
4 | COD | TIXI
4 | EMR | 25 WHIT
4 | ESA | CHTI CHUR GOLD MAL2 WHIT CHTI CHUR GOLD MAL2 WHIT
4 | GFZ | FAA1 FAIR GMSD HERS KOUR MAL2 NKLG FAA1 FAIR GMSD
4 | GFZ | HERS KOUR MAL2 MAW1 NKLG
4 | GRG | ADIS FAA1 GLSV INVK SYOG YELL ADIS DGAR FAA1 GLSV
4 | GRG | INVK REUN SYOG YELL
4 | MIT | GOLD GRAS JPLM KOUR GOLD GRAS JPLM KOUR
5 | COD | 20 20 MAL2 MAL2
5 | EMR | SYOG LPGS SYOG YELL
5 | ESA | AUCK BAKE CHUR TRO1 AUCK CHUR TRO1
5 | GFZ | GMSD GODE MAL2 GMSD GODE MAL2 YAR2
5 | GRG | ADIS CHTI GLSV KIT3 RIO2 SYOG ADIS CHTI GLSV KIT3
5 | GRG | RIO2 SYOG
5 | MIT | AUCK AUCK
6 | COD | MAG0
6 | EMR | HERS
6 | ESA | AUCK KOUR REUN AUCK REUN
6 | GFZ | 5 14 5 14 GMSD GODE HOB2 MAL2 SYOG GMSD GODE HOB2
6 | GFZ | MAL2 REUN SYOG
6 | GRG | ALRT COCO GLSV KOUR MAS1 SYOG ALRT COCO FAA1 GLSV
6 | GRG | MAS1 SYOG
6 | JPL | ALRT
6 | MIT | AUCK
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 | .3 .4 .8 6 9 -7 -.29
EMR | 0 | -6.7 -5.1 4.6 12 39 -31 .03
ESA | 0 | -.7 -.3 -.7 -8 29 7 -.22
GFZ | 0 | .8 .5 -.0 -6 -40 -2 -.22
GRG | 0 | .8 -2.7 6.1 51 -43 115 .04
JPL | 0 | 6.2 .8 7.7 -24 -84 12 .41
MIT | 0 | -2.0 -7.7 1.9 -15 25 1 .03
NGS | 0 | -4.6 -1.2 .1 25 -7 -10 .13
SIO | 0 | -6.5 -9.4 .7 1 10 10 .06
COD | 1 | -.1 .6 .8 7 8 -11 -.32
EMR | 1 | -.7 -2.3 2.4 -6 42 -29 .39
ESA | 1 | -.4 -.3 -.6 -9 19 1 -.13
GFZ | 1 | .9 .6 -.1 -3 -41 1 -.21
GRG | 1 | 5.7 -.8 6.1 54 -32 86 -.02
JPL | 1 | -1.9 -2.6 1.1 -14 -19 24 .48
MIT | 1 | -1.6 -4.8 5.1 28 22 -17 .06
NGS | 1 | -1.5 -2.7 3.5 35 -4 -40 .16
SIO | 1 | -4.0 -4.3 -1.1 3 -8 13 .11
COD | 2 | .2 .4 .3 3 -3 -8 -.23
EMR | 2 | -.6 -9.3 4.2 -2 19 -42 .23
ESA | 2 | -.1 -.6 -.3 1 11 -3 -.28
GFZ | 2 | .8 .8 -.8 0 -47 -9 -.06
GRG | 2 | 6.9 -10.0 7.7 56 -14 105 .18
JPL | 2 | 3.3 -6.1 -2.0 -25 -51 15 .49
MIT | 2 | 1.7 -7.6 2.9 14 20 -20 .02
NGS | 2 | -.9 -1.1 .2 24 1 -21 .07
SIO | 2 | -3.1 -3.4 -7.4 13 -13 14 .08
COD | 3 | .0 .4 .2 11 2 0 -.11
EMR | 3 | 3.2 -5.0 -.2 -6 22 -16 .35
ESA | 3 | -.5 -.1 -.4 -1 -4 0 -.17
GFZ | 3 | .5 .7 -.7 13 -45 4 -.11
GRG | 3 | -1.3 -3.4 -1.4 22 -25 118 .14
JPL | 3 | 10.3 -3.8 -4.7 25 -13 -37 .68
MIT | 3 | .7 -4.1 2.4 15 10 -18 .19
NGS | 3 | -4.0 .7 -4.6 13 -26 -3 .12
SIO | 3 | -4.4 -.3 -9.1 12 -19 8 .34
COD | 4 | .5 .0 .3 -2 8 5 -.25
EMR | 4 | .5 -12.4 1.8 -13 26 -30 .37
ESA | 4 | -.2 -.1 -.2 -6 0 9 .01
GFZ | 4 | .6 .5 -.8 -1 -33 -2 -.01
GRG | 4 | 5.4 -9.4 1.9 59 -61 143 .15
JPL | 4 | 2.6 -10.8 -5.0 3 -20 35 .65
MIT | 4 | 2.1 -6.8 .9 3 11 -2 .10
NGS | 4 | 1.0 -6.5 -3.5 23 -23 -25 .07
SIO | 4 | -6.5 -6.6 -15.8 -17 -26 12 .16
COD | 5 | .1 .1 .3 -3 6 -2 -.10
EMR | 5 | -4.4 -1.0 .0 -16 36 -28 .62
ESA | 5 | -.5 -.5 -.3 -15 8 13 -.04
GFZ | 5 | .3 .5 -1.0 2 -33 2 .0
GRG | 5 | .8 -4.7 -3.6 42 -53 146 -.06
JPL | 5 | -1.5 -9.8 .3 -13 -18 27 .82
MIT | 5 | .5 -7.3 4.2 -1 -4 -10 .09
NGS | 5 | -7.4 -10.4 -.6 21 -42 2 .15
SIO | 5 | -4.1 -4.4 -10.8 12 -32 7 .14
COD | 6 | .5 .1 .3 2 0 7 -.21
EMR | 6 | -1.3 -4.1 1.1 -8 19 -27 .48
ESA | 6 | -.8 -.6 .0 11 -1 -1 -.13
GFZ | 6 | .4 .5 -.9 1 -39 -4 -.02
GRG | 6 | -6.1 -.2 8.8 57 -69 143 -.0
JPL | 6 | 2.2 -4.8 .3 -23 -9 -1 .55
MIT | 6 | -.5 -5.7 6.1 -2 -1 -5 -.03
NGS | 6 | -5.0 -6.5 7.7 42 -35 -6 .29
SIO | 6 | -3.5 -5.5 -15.8 -8 8 8 .20
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 1.1938.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1938.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 2.1938.[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 3.1938.[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 5.1938.0-6). 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 1938 summary. (Feb 26, 2017 - Mar 04, 2017)
Table 1.1938.a GPS week: 1938 MJD: 57810.000-57816.000
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 259| 0 0 1 -8 -2 0 -.03 10 9 | -430 -246 12 111
| 0 0 2 19 17 11 .02 | 188 274
emr 80| -1 -1 3 -3 4 3 .22 14 14 | 1747 436 17 118
| 1 2 1 15 13 11 .05 | 750 562
esa 150| 0 0 -1 -7 0 10 .00 11 12 | -196 -1171 8 180
| 0 0 0 13 8 12 .03 | 697 1561
gfz 191| 0 1 -2 -10 0 9 .10 11 10 | -553 66 10 111
| 0 0 0 11 15 15 .04 | 318 348
grg 110| 1 0 1 -12 12 4 -.43 15 13 | 40987 -48261 13 188
| 0 0 2 10 12 15 .04 | 113402 142859
igr n/a| 0 0 0 -20 -7 5 .02 5 5 | 11509 413 13 79
| 0 0 0 16 9 15 .03 | 514 593
jpl 80| 1 0 1 7 -15 0 .24 13 13 | 1083 471 42 253
| 1 1 1 10 18 16 .02 | 824 639
mit 350| 1 -1 -2 10 0 -2 -.03 13 11 | -391 -276 42 317
| 0 0 0 27 18 11 .02 | 449 166
ngs 220| 0 0 0 14 0 -10 .02 9 8 | -449 -226 1024 2149
| 1 0 1 21 17 10 .05 | 187 272
sio 322| 0 0 0 6 -10 -11 .12 13 13 | --- --- --- ---
| 0 0 1 32 23 41 .05 | --- ---
Table 1.1938.b GPS week : 1938 MJD: 57810.000-57816.000
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 | 5 5 5 5 5 5 5 |
3 | 5 5 5 4 5 5 5 |
4 | 0 0 0 0 0 0 0 |
5 | 5 4 4 4 5 5 5 |
6 | 3 4 3 3 3 4 3 |
7 | 4 4 4 5 5 5 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 4 4 3 3 3 |
10 | 4 5 5 5 4 5 6 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 6 |
13 | 5 5 5 4 5 5 5 |
14 | 5 5 5 6 5 5 5 |
15 | 5 5 5 4 5 5 5 |
16 | 6 6 6 6 6 8 5 |
17 | 5 5 5 5 5 5 5 |
18 | 4 5 4 5 4 5 5 |
19 | 5 5 5 6 5 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 5 5 4 4 4 5 5 |
22 | 4 4 3 3 4 4 4 |
23 | 7 6 6 7 7 8 8 |
24 | 3 4 3 3 4 4 4 |
25 | 7 7 6 6 5 5 5 |
26 | 6 5 6 5 5 7 5 |
27 | 4 3 3 3 3 3 3 |
28 | 5 5 4 4 4 5 4 |
29 | 5 5 5 5 5 5 5 |
30 | 3 3 3 3 3 3 3 |
31 | 5 5 5 5 5 5 5 |
32 | 4 4 3 4 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1938.0 GPS week: 1938 Day: 0 MJD: 57810.000
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 257| -1 -1 -1 10 5 -11 -.04 11 10 | -417 -332 12 116
emr 80| -3 0 7 13 12 -9 .13 16 15 | 868 43 19 113
esa 150| 0 1 0 -11 -7 5 -.06 11 11 | -536 -164 8 172
gfz 188| 0 1 -2 2 0 -5 .11 11 10 | -772 -31 10 118
grg 110| 1 0 -1 -7 1 24 -.38 16 14 | -10964 33045 14 179
igr n/a| 0 0 1 -20 -21 -11 .02 5 4 | 11168 -158 13 71
jpl 80| 2 0 1 24 -44 -17 .28 16 16 | 209 173 48 289
mit 350| 0 0 0 -7 -11 3 -.03 13 12 | -456 -221 48 314
ngs 222| 0 0 0 -5 1 -19 .08 9 8 | -432 -312 931 2290
sio 322| 1 0 1 -9 -27 29 .11 13 13 | --- --- --- ---
Table 2.1938.1 GPS week: 1938 Day: 1 MJD: 57811.000
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 258| 0 0 1 1 25 -10 -.06 10 10 | -351 -365 12 115
emr 80| 1 -1 3 -33 -6 12 .23 13 13 | 989 768 19 136
esa 150| 0 1 -1 -21 -4 10 -.02 11 12 | -451 -275 8 181
gfz 191| -1 2 -3 -27 -26 28 .09 11 9 | -646 -114 11 102
grg 113| 1 0 1 -17 18 7 -.45 15 14 | 297993 -371032 13 233
igr n/a| 0 0 0 -37 -9 14 -.02 5 5 | 11020 438 13 76
jpl 80| 0 0 2 14 10 -6 .23 12 12 | 331 669 41 317
mit 350| 0 0 -2 35 17 -23 -.04 13 12 | -129 -213 47 273
ngs 218| 0 0 1 18 -11 -11 .04 9 8 | -346 -372 1078 2342
sio 323| 0 0 1 19 -2 1 .11 14 13 | --- --- --- ---
Table 2.1938.2 GPS week: 1938 Day: 2 MJD: 57812.000
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 258| 0 0 0 -18 0 -5 -.04 10 9 | -104 -702 12 111
emr 80| -1 -3 2 -1 -6 -14 .18 13 13 | 1238 1015 15 101
esa 150| 0 1 -1 -10 -8 11 .02 11 11 | -357 -2970 7 149
gfz 191| 0 1 -4 -4 -12 2 .12 11 9 | -1047 398 11 107
grg 109| 2 0 4 -4 1 9 -.42 12 11 | -19 -172 13 169
igr n/a| 0 0 0 -41 -6 -10 -.01 5 5 | 10887 843 12 62
jpl 80| 1 0 0 4 -28 2 .24 13 13 | 456 1017 42 263
mit 350| 1 -2 -2 29 0 9 -.03 13 12 | -448 -579 38 319
ngs 223| 0 1 0 13 19 -21 .08 10 9 | -139 -663 972 2193
sio 323| 0 0 0 9 6 7 .11 14 14 | --- --- --- ---
Table 2.1938.3 GPS week: 1938 Day: 3 MJD: 57813.000
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 261| 0 0 0 19 -30 -9 -.04 10 9 | -485 -28 12 104
emr 80| -1 -1 2 6 0 5 .23 14 14 | 2506 -50 17 134
esa 150| 0 1 0 17 -7 -8 -.00 11 12 | -597 109 8 185
gfz 190| 0 0 -1 3 -2 17 .11 10 9 | -322 -25 10 108
grg 111| 1 0 0 1 14 -1 -.39 13 11 | 133 23 13 181
igr n/a| 0 0 0 -10 -15 -7 .04 4 4 | 11973 -61 13 86
jpl 80| 2 0 1 8 -26 -21 .22 13 13 | 1623 -110 43 245
mit 350| 2 -1 -1 -26 28 -3 -.02 13 11 | -138 -143 37 365
ngs 224| -2 0 0 0 20 -6 -.00 10 9 | -508 -40 1016 2080
sio 328| 0 0 1 -33 -8 -5 .11 13 12 | --- --- --- ---
Table 2.1938.4 GPS week: 1938 Day: 4 MJD: 57814.000
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 259| 0 0 3 -23 0 1 .00 9 9 | -729 152 12 114
emr 80| -2 -4 3 -9 28 9 .24 14 14 | 1975 648 17 127
esa 150| 0 1 -1 -19 9 12 .03 11 11 | 1275 -3788 10 210
gfz 194| 0 0 -3 -18 20 -9 .08 11 10 | -416 115 10 100
grg 105| 0 0 3 -27 33 -7 -.43 14 12 | -83 68 14 176
igr n/a| 0 0 0 1 7 7 .02 5 5 | 11583 523 14 86
jpl 80| 0 -2 2 2 -3 12 .23 11 11 | 2240 667 40 206
mit 350| 1 -1 -3 33 -18 0 .01 13 11 | -1346 -432 49 284
ngs 222| -1 0 -2 21 -28 8 .01 9 8 | -750 192 975 2116
sio 330| 0 0 2 39 -41 -15 .03 13 13 | --- --- --- ---
Table 2.1938.5 GPS week: 1938 Day: 5 MJD: 57815.000
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 260| 0 0 3 -9 -7 19 -.02 10 10 | -522 -131 14 113
emr 80| -1 2 3 1 12 7 .21 16 14 | 2812 -387 16 118
esa 150| 0 0 -1 -7 4 9 .04 12 12 | 56 -959 9 199
gfz 194| 0 1 -2 -10 6 7 .03 11 10 | -70 -471 10 127
grg 108| 1 1 -1 -22 19 -20 -.47 19 16 | -39 173 14 174
igr n/a| 0 0 0 -5 -7 17 .04 5 5 | 12289 -136 14 93
jpl 80| 0 -1 1 -11 -7 2 .26 12 12 | 1898 -468 45 251
mit 350| 2 -1 -1 -22 0 -8 -.02 13 10 | -77 -223 40 344
ngs 220| -1 0 -1 57 7 -14 -.01 9 8 | -546 -111 1121 2097
sio 319| 0 0 1 -30 -25 -2 .15 13 13 | --- --- --- ---
Table 2.1938.6 GPS week: 1938 Day: 6 MJD: 57816.000
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 262| 0 0 4 -36 -13 10 -.04 11 9 | -404 -317 12 107
emr 80| -1 -2 1 -5 -7 15 .30 14 14 | 1842 1019 20 101
esa 150| 0 0 0 -2 11 35 .01 12 13 | -764 -150 8 165
gfz 191| 0 1 -3 -17 7 27 .16 11 10 | -600 591 10 117
grg 115| 0 0 3 -12 0 17 -.47 14 12 | -107 62 14 204
igr n/a| 0 1 0 -30 1 26 .08 5 5 | 11649 1444 14 79
jpl 80| 1 0 -1 6 -11 27 .23 12 12 | 825 1350 41 201
mit 350| 1 -1 -2 28 -20 5 -.05 14 11 | -145 -127 37 321
ngs 215| 0 0 0 0 -11 -11 -.04 9 8 | -424 -277 1077 1931
sio 314| 0 0 -2 50 27 -99 .18 12 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 3.1938.0 GPS week: 1938 Day: 0 MJD: 57810.000
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 10 6 9 11 3 15 8 7 11 3 | 4 3 2 2 1 2 3 2 4 4 2
2 | 11 14 10 12 13 5 18 14 10 15 4 | 2 3 2 3 2 2 2 7 4 6 3
3E | 10 11 19 9 21 5 13 10 8 12 4 | 4 4 4 4 4 2 4 3 3 5 3
X4E | 1 --- --- --- --- 45 --- --- --- --- 0 | 6 --- --- --- --- 3 --- --- --- --- 6
5E | 9 16 6 12 26 4 20 12 6 11 4 | 3 6 3 4 3 3 4 3 4 5 3
6M | 6 12 7 9 8 5 10 11 4 10 3 | 2 5 3 2 3 2 4 4 2 5 2
7 | 10 13 12 10 10 3 10 11 10 15 4 | 2 2 2 2 1 2 2 2 2 3 2
8M | 7 8 5 7 13 4 15 9 8 7 3 | 1 3 2 3 2 2 2 3 2 2 2
9 | 7 10 9 9 8 4 10 9 5 13 3 | 3 2 3 3 1 1 2 2 2 3 2
10E | 10 12 17 7 17 6 13 10 7 7 4 | 3 6 4 3 3 3 4 4 3 4 3
11 | 7 14 16 8 10 4 13 12 7 10 4 | 2 2 2 2 1 1 3 2 2 1 1
12E | 18 17 6 11 23 3 20 13 7 11 5 | 4 5 3 5 4 3 3 5 3 6 3
13M | 7 15 10 13 15 4 33 13 9 15 4 | 1 3 1 3 2 1 2 4 2 2 2
14 | 9 17 13 18 10 4 11 12 9 19 5 | 2 5 1 2 1 1 2 2 2 2 1
15M | 10 15 12 12 19 4 22 15 8 14 4 | 1 3 1 2 1 1 2 4 3 3 1
16E | 20 15 9 14 28 8 16 16 12 15 6 | 3 3 2 3 4 2 3 2 3 4 3
17M | 10 14 12 14 13 6 16 16 8 15 5 | 3 5 3 3 2 2 3 4 4 6 3
18E | 8 23 5 9 11 4 18 12 7 9 4 | 3 5 3 3 4 2 3 3 3 4 3
19 | 12 20 13 13 13 5 14 13 11 15 5 | 2 3 2 3 2 1 2 4 4 5 3
20E | 10 11 6 10 14 4 16 15 6 12 4 | 2 4 2 3 3 2 3 5 3 5 2
21M | 15 13 9 12 12 4 11 16 9 15 4 | 2 2 3 2 3 2 2 3 3 4 2
22E | 7 11 7 9 23 5 11 14 9 10 4 | 2 3 3 3 5 2 3 4 3 4 2
23M | 13 24 12 14 13 5 12 30 14 17 6 | 3 2 4 1 2 1 2 2 2 3 1
24 | 5 10 7 8 9 3 10 7 6 13 3 | 2 5 2 2 1 2 2 3 4 5 2
25E | 11 33 20 8 25 6 24 14 12 14 6 | 4 7 4 3 4 2 45 6 3 2 3
26E | 13 16 20 8 19 11 20 15 13 15 5 | 5 5 3 2 5 3 3 2 3 3 2
27 | 6 10 6 5 13 3 10 8 8 16 3 | 3 3 3 2 1 2 3 2 2 3 2
28E | 14 13 8 10 18 6 13 12 10 9 4 | 4 4 2 3 5 3 3 3 3 3 2
29 | 13 22 10 11 11 4 18 15 12 16 5 | 2 2 2 3 1 2 2 2 2 4 2
30M | 7 9 5 8 13 3 11 10 9 8 3 | 3 3 3 3 2 2 3 3 5 2 3
31M | 10 19 13 12 13 4 13 11 10 19 5 | 4 3 3 3 2 2 4 3 3 2 2
32 | 8 16 9 7 11 2 8 9 5 11 3 | 2 4 1 3 1 1 2 4 1 3 1
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 11 11 16 5 16 13 9 13 |T 2 3 2 2 2 1 4 3 2 3 2
WRMS | 10 15 11 10 14 4 16 12 8 13 |NE 2 3 2 2 1 1 2 2 2 3 1
MEDI | 10 14 9 10 13 4 13 12 8 13 |MD 3 3 3 3 2 2 3 3 3 4 2
Table 3.1938.1 GPS week: 1938 Day: 1 MJD: 57811.000
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 | 11 8 6 9 9 5 13 9 6 11 3 | 4 3 2 3 2 2 2 3 5 5 3
2 | 8 14 10 15 16 6 11 17 10 17 5 | 3 3 2 4 2 3 3 7 4 6 3
3E | 10 8 19 6 21 6 9 9 9 12 4 | 5 7 6 6 6 5 6 5 7 7 6
X4E | 2 --- --- --- --- 82 --- --- --- --- 0 | 22 --- --- --- --- 5 --- --- --- --- 22
5E | 8 12 7 10 19 6 11 10 8 14 4 | 3 6 3 4 4 2 3 4 4 5 3
6 | 6 9 6 8 8 5 11 14 8 14 3 | 2 5 2 3 2 2 4 4 2 6 2
7 | 9 10 12 10 9 4 9 12 8 15 4 | 3 2 2 3 1 2 2 4 3 3 2
8 | 8 9 5 7 9 4 13 8 7 8 3 | 3 4 3 3 2 2 2 3 3 2 2
9 | 8 8 8 9 8 6 9 8 8 11 3 | 5 5 3 3 2 2 3 3 4 4 3
10E | 16 11 19 7 15 6 10 10 8 8 4 | 3 7 4 3 4 3 4 5 4 3 3
11 | 8 11 18 6 9 5 13 9 6 11 4 | 2 2 3 2 2 1 2 3 2 2 1
12E | 11 17 7 12 16 4 14 12 9 12 4 | 3 5 4 5 4 3 4 5 4 6 3
13 | 8 16 10 14 13 4 14 14 9 16 4 | 2 4 1 4 1 1 2 5 2 2 2
14 | 13 13 12 19 9 4 11 14 10 17 5 | 2 5 4 3 2 2 2 3 2 3 2
15 | 8 14 11 12 15 5 14 18 9 12 4 | 3 2 2 2 1 2 2 5 3 4 1
16E | 14 18 9 13 25 5 18 14 13 13 5 | 2 3 3 3 7 2 4 3 4 4 3
17 | 10 13 12 12 13 6 11 15 9 14 4 | 3 6 2 3 2 2 2 4 4 6 3
18E | 9 23 6 11 20 4 16 12 5 10 4 | 3 5 3 3 5 2 3 4 4 4 3
19 | 9 16 12 12 12 6 12 17 10 16 5 | 2 5 2 5 2 2 2 5 5 5 3
20E | 7 13 5 9 12 4 11 14 7 11 3 | 2 4 3 3 3 2 3 6 3 5 3
21 | 16 10 8 10 16 4 9 12 10 16 4 | 3 3 2 2 2 2 2 2 3 4 2
22E | 7 8 6 7 15 6 12 13 6 14 3 | 3 3 3 4 4 2 3 4 4 4 3
23 | 8 19 11 15 14 6 12 25 13 21 6 | 4 3 6 2 2 2 2 3 3 3 2
24 | 8 9 7 7 9 5 9 9 9 15 3 | 4 5 2 2 1 2 2 3 4 7 3
25E | 19 13 22 10 34 8 --- 19 19 12 7 | 4 6 4 3 5 3 --- 6 5 4 3
26E | 7 10 20 8 20 7 15 11 12 15 5 | 2 7 4 2 5 2 3 3 4 3 2
27 | 8 9 7 7 10 5 10 7 7 11 3 | 3 3 3 2 1 2 3 2 3 3 2
28E | 11 18 9 10 16 5 13 12 11 9 4 | 3 7 3 3 5 3 3 3 5 4 3
29 | 12 21 9 14 12 3 14 16 8 19 5 | 2 3 3 3 2 2 2 2 2 5 2
30 | 6 8 6 7 11 2 10 9 9 9 3 | 3 3 2 3 2 2 2 3 5 2 3
31 | 11 14 13 11 15 6 13 12 11 15 4 | 4 4 3 3 2 2 3 4 3 3 2
32 | 9 14 9 5 9 2 11 9 6 10 3 | 3 7 2 3 2 1 2 5 1 3 2
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 11 11 15 5 12 13 9 14 |T 3 4 2 3 2 2 2 3 3 4 3
WRMS | 10 13 12 9 14 5 12 12 8 13 |NE 3 3 2 3 1 1 2 3 3 4 2
MEDI | 8 13 9 10 13 5 11 12 9 13 |MD 3 4 3 3 2 2 2 4 4 4 3
Table 3.1938.2 GPS week: 1938 Day: 2 MJD: 57812.000
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 10 5 7 8 3 12 8 7 10 3 | 4 3 2 3 2 2 3 3 4 5 3
2 | 9 13 9 15 13 4 11 15 10 15 4 | 3 3 3 3 2 2 3 6 4 4 3
3E | 9 9 19 6 21 4 12 13 10 6 4 | 9 10 10 10 10 9 10 10 10 10 9
X4E | 1 --- --- --- --- 38 --- --- --- --- 0 | 17 --- --- --- --- 5 --- --- --- --- 17
5E | 7 15 8 12 14 6 15 12 7 11 4 | 3 5 3 3 4 2 3 4 5 4 3
6 | 7 10 6 6 10 5 8 12 5 13 3 | 3 4 3 3 2 2 4 3 2 5 2
7 | 9 12 12 9 9 5 11 15 10 16 4 | 2 3 3 3 1 2 2 4 3 3 2
8 | 6 8 6 5 8 4 11 8 8 9 2 | 4 3 3 3 2 3 3 3 3 3 3
9 | 8 12 8 6 7 5 9 12 9 13 3 | 5 9 4 3 2 2 3 3 4 4 3
10E | 9 10 19 6 16 5 11 9 9 9 4 | 2 6 4 3 3 3 5 5 5 4 3
11 | 7 11 17 6 8 5 14 10 9 10 4 | 2 2 3 2 2 2 3 3 3 2 2
12E | 20 17 6 12 10 4 18 13 11 12 5 | 6 6 5 5 5 4 5 6 5 6 4
13 | 9 15 9 14 8 3 14 14 8 19 4 | 2 5 2 3 1 1 2 3 2 2 2
14 | 11 11 11 19 10 3 11 16 12 17 5 | 2 4 3 3 2 2 2 3 2 2 2
15 | 9 16 13 11 9 4 18 14 10 16 4 | 3 2 2 2 2 2 3 3 3 4 2
16E | 17 16 10 13 19 8 16 14 16 11 5 | 3 3 4 3 6 3 4 4 4 6 3
17 | 10 12 10 13 10 6 10 16 9 16 4 | 3 5 2 3 2 2 2 4 2 4 2
18E | 10 21 5 12 11 3 19 12 8 11 4 | 3 4 3 3 5 2 3 4 4 4 3
19 | 11 16 9 14 10 5 14 17 10 19 5 | 2 4 3 4 2 2 3 5 3 5 3
20E | 8 13 7 8 10 4 15 12 9 13 3 | 2 3 4 4 4 3 4 5 4 5 3
21 | 13 11 8 12 11 4 12 11 9 16 4 | 2 4 2 3 2 2 2 2 2 4 2
22E | 6 11 6 8 11 3 12 12 8 8 3 | 2 4 3 4 3 2 3 4 4 4 3
23 | 7 22 14 12 12 6 13 28 13 20 6 | 4 3 5 2 1 2 2 5 3 6 2
24 | 8 7 7 7 8 2 11 7 7 15 3 | 4 4 2 2 2 1 2 2 3 6 2
25E | 9 12 22 9 22 7 23 15 17 11 6 | 4 5 5 3 5 3 9999 5 5 5 3
26E | 6 14 19 9 25 6 11 10 10 14 5 | 3 6 4 3 4 2 4 3 4 4 2
27 | 8 7 5 6 8 4 9 8 10 11 3 | 4 3 3 2 1 2 3 3 3 3 2
28E | 9 15 6 9 13 3 13 10 12 10 4 | 3 5 3 4 4 2 4 3 5 4 3
29 | 11 20 11 13 9 5 21 16 10 20 5 | 3 3 3 3 2 2 2 3 3 5 2
30 | 5 7 5 7 7 2 9 7 6 10 2 | 3 3 3 3 2 2 3 3 4 2 2
31 | 12 14 12 15 13 4 11 13 12 14 5 | 3 4 3 3 2 3 3 4 4 3 3
32 | 8 9 7 7 9 4 9 10 7 11 3 | 2 5 2 2 2 1 2 6 2 3 2
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 11 11 12 5 13 13 10 14 |T 3 4 3 3 2 2 3 4 3 4 3
WRMS | 9 13 11 9 11 5 13 12 9 14 |NE 3 3 2 2 1 1 2 3 3 3 2
MEDI | 9 12 9 9 10 4 12 12 9 13 |MD 3 4 3 3 2 2 3 4 4 4 3
Table 3.1938.3 GPS week: 1938 Day: 3 MJD: 57813.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 10 5 8 12 3 11 6 8 11 3 | 4 5 2 2 2 2 2 4 4 6 3
2 | 7 13 9 15 15 4 13 16 10 15 4 | 3 4 3 3 2 2 2 6 4 6 3
3E | 8 9 18 7 14 3 10 12 10 6 4 | 14 14 14 14 14 14 14 14 14 15 14
X4E | 2 --- --- --- --- 31 --- --- --- --- 0 | 6 --- --- --- --- 5 --- --- --- --- 6
5E | 10 11 9 11 18 4 14 13 7 9 4 | 4 4 4 3 5 3 4 5 5 4 3
6 | 5 9 6 5 7 4 9 11 9 13 3 | 3 3 3 3 2 2 3 2 3 5 2
7 | 8 12 13 10 9 5 13 14 9 17 4 | 2 3 2 2 2 2 2 5 3 4 2
8 | 7 8 5 5 9 3 10 6 7 9 2 | 3 4 3 2 3 3 3 4 4 4 3
9 | 5 15 7 7 7 4 14 10 7 11 3 | 4 7 3 4 2 2 2 3 2 4 3
10E | 13 7 20 7 16 4 9 8 8 7 4 | 3 4 4 4 4 3 4 4 4 3 3
11 | 6 12 15 7 8 3 11 7 11 7 3 | 3 2 3 2 2 2 2 2 3 3 2
12E | 11 16 7 13 14 4 16 13 9 11 4 | 6 7 6 6 6 5 6 7 6 7 5
13 | 7 16 11 12 9 3 15 10 8 15 4 | 1 6 1 3 1 1 2 3 4 3 2
14 | 13 12 13 17 8 4 11 18 12 19 5 | 3 4 3 2 1 1 2 3 3 4 1
15 | 7 16 14 10 8 5 15 11 8 13 4 | 2 2 2 2 2 2 2 3 3 4 2
16E | 17 17 9 12 24 6 13 13 21 15 6 | 2 3 3 3 4 3 4 3 4 5 3
17 | 8 15 12 12 12 5 11 15 9 15 4 | 3 5 3 4 2 2 2 5 3 7 3
18E | 13 21 6 11 13 2 14 10 8 7 4 | 3 3 2 3 4 2 3 3 3 3 2
19 | 12 17 12 14 11 5 14 17 12 19 5 | 3 4 3 3 2 2 3 6 2 8 3
20E | 8 14 8 8 13 4 14 10 6 9 3 | 2 4 3 3 4 2 4 4 4 5 3
21 | 15 10 9 10 10 4 10 13 9 13 4 | 2 3 2 2 2 1 2 2 2 3 1
22E | 6 10 7 7 7 5 13 11 8 12 3 | 2 4 3 3 4 2 3 4 4 5 3
23 | 10 23 12 13 12 6 14 30 14 20 6 | 3 2 4 2 2 2 1 5 2 5 2
24 | 6 7 7 7 8 4 6 7 8 11 3 | 2 3 2 2 2 1 2 2 3 5 1
25E | 13 11 19 9 21 5 16 17 14 11 5 | 5 6 5 5 6 4 9999 6 5 5 4
26E | 8 11 19 7 24 3 11 9 13 10 5 | 3 6 4 3 5 2 4 3 4 4 3
27 | 9 7 5 6 9 3 7 8 7 10 3 | 3 3 2 2 2 2 3 2 2 3 2
28E | 9 17 7 8 18 8 15 12 9 9 4 | 4 9 3 4 4 2 4 4 4 4 3
29 | 14 22 11 11 11 5 18 15 9 15 5 | 3 4 3 2 2 2 2 4 3 4 2
30 | 5 9 6 8 10 3 10 11 6 9 3 | 3 3 3 3 3 3 3 4 3 4 3
31 | 10 14 12 12 12 3 14 14 12 15 4 | 4 5 4 5 3 4 4 5 5 3 3
32 | 8 9 8 8 8 3 11 14 8 11 3 | 2 3 2 2 2 1 2 6 2 5 2
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 11 10 13 4 13 13 10 13 |T 3 4 3 3 3 2 3 4 3 4 3
WRMS | 9 14 12 9 11 4 13 11 9 12 |NE 2 3 2 2 1 1 2 3 2 4 2
MEDI | 8 12 9 9 11 4 13 12 9 11 |MD 3 4 3 3 2 2 3 4 3 4 3
Table 3.1938.4 GPS week: 1938 Day: 4 MJD: 57814.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 10 7 9 9 4 10 7 6 14 3 | 3 5 2 3 2 2 2 4 4 7 3
2 | 8 15 10 14 12 6 9 17 10 16 4 | 3 4 3 3 1 2 2 6 4 6 3
3E | 10 13 18 7 11 5 11 8 9 11 4 | 18 18 18 18 18 18 18 18 18 19 18
X4E | 2 --- --- --- --- 43 --- --- --- --- 0 | 4 --- --- --- --- 8 --- --- --- --- 4
5E | 9 12 10 13 25 6 12 19 11 10 5 | 3 4 4 3 7 3 4 4 5 5 3
6 | 8 11 5 6 6 5 10 10 8 14 3 | 3 4 3 3 2 2 3 3 3 4 2
7 | 8 13 13 11 13 5 14 15 11 17 4 | 2 2 2 1 2 1 2 4 3 3 1
8 | 9 10 6 9 8 4 10 6 7 8 3 | 3 4 3 3 3 3 3 4 3 4 3
9 | 5 9 7 6 10 4 10 11 7 11 3 | 3 4 2 3 2 2 2 3 2 3 2
10E | 13 8 19 6 13 3 8 6 7 7 4 | 3 4 4 3 4 2 3 3 4 3 3
11 | 6 12 15 9 9 4 10 6 6 12 3 | 3 2 3 2 2 2 2 2 2 3 2
12E | 8 20 7 12 19 4 17 13 7 9 4 | 8 7 7 7 8 7 7 8 7 8 7
13 | 8 17 11 12 11 6 14 12 12 17 4 | 1 6 1 3 2 2 2 3 4 3 2
14 | 14 13 10 18 8 4 10 14 11 17 5 | 2 3 2 3 1 1 1 2 3 3 1
15 | 11 16 12 12 11 5 13 14 9 14 4 | 3 3 2 3 2 2 2 4 2 3 2
16E | 9 18 8 11 28 8 14 13 16 12 5 | 3 4 3 3 4 3 3 3 4 4 3
17 | 7 14 13 11 12 6 12 15 9 15 4 | 3 6 3 3 2 2 2 5 4 6 3
18E | 12 19 6 11 9 4 10 9 6 10 4 | 3 4 2 3 3 2 3 4 3 4 2
19 | 8 16 12 13 14 7 14 16 13 18 5 | 3 4 3 3 2 2 2 6 4 7 3
20E | 9 13 7 9 17 4 12 11 9 8 4 | 2 3 3 3 5 2 3 3 4 4 3
21 | 9 8 10 11 12 5 9 14 7 15 4 | 2 4 2 2 2 2 2 3 2 4 1
22E | 8 11 7 8 12 4 12 8 8 11 3 | 4 4 4 4 4 3 3 4 3 5 3
23 | 10 24 11 15 15 9 14 35 13 19 7 | 3 3 5 2 1 1 1 6 2 5 2
24 | 10 11 7 10 10 5 6 11 8 14 3 | 2 4 2 2 2 1 2 1 2 5 1
25E | 7 13 19 11 16 5 13 17 10 11 5 | 5 7 6 6 7 5 9999 7 5 5 5
26E | 14 11 19 9 21 5 9 8 10 12 5 | 4 13 4 3 4 2 4 3 4 3 3
27 | 9 8 7 6 8 3 9 6 7 11 3 | 3 3 2 1 2 1 3 2 2 3 1
28E | 7 20 8 9 12 7 13 12 10 9 4 | 3 11 3 5 5 3 4 4 4 4 3
29 | 9 20 11 13 6 6 14 15 10 13 4 | 3 4 3 3 2 2 2 3 4 3 2
30 | 6 9 7 8 9 4 10 10 6 10 3 | 4 4 4 4 4 3 4 4 4 4 4
31 | 12 13 11 15 15 5 11 14 10 16 5 | 5 6 5 6 5 5 4 6 6 5 5
32 | 9 9 7 6 8 4 8 9 7 13 3 | 2 5 2 3 1 1 2 5 2 5 2
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 11 11 14 5 11 13 9 13 |T 3 5 3 3 3 3 3 4 3 4 3
WRMS | 9 14 11 10 12 5 11 11 8 13 |NE 2 3 2 2 1 1 2 3 2 4 1
MEDI | 9 13 10 11 12 5 11 12 9 12 |MD 3 4 3 3 2 2 2 4 4 4 3
Table 3.1938.5 GPS week: 1938 Day: 5 MJD: 57815.000
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 9 9 10 13 4 9 6 5 16 3 | 4 5 3 4 3 3 3 6 4 7 4
2 | 11 14 11 15 15 7 12 15 12 15 5 | 3 5 4 4 2 4 3 6 4 6 4
3E | 15 15 20 6 17 5 11 9 5 14 5 | 24 24 23 23 23 23 23 23 23 23 23
X4E | 2 --- --- --- --- 39 --- --- --- --- 0 | 5 --- --- --- --- 9 --- --- --- --- 6
5E | 11 15 9 11 18 6 13 12 7 11 4 | 3 7 5 4 5 4 4 5 4 5 4
6 | 9 11 8 7 9 5 8 11 7 12 3 | 3 4 4 4 3 3 4 4 4 4 3
7 | 10 12 12 9 14 5 14 13 9 17 4 | 3 3 3 3 3 3 3 4 3 3 3
8 | 6 8 5 8 13 4 9 8 6 8 3 | 5 5 5 4 5 4 4 4 4 5 4
9 | 7 10 8 8 11 3 8 8 8 9 3 | 3 4 3 3 2 2 3 4 3 4 3
10E | 15 10 20 7 17 4 10 6 8 7 4 | 4 7 6 4 4 4 4 4 6 6 4
11 | 7 11 15 8 11 4 11 6 8 10 3 | 3 3 4 3 2 3 3 3 3 4 3
12E | 6 20 9 9 20 5 20 12 9 10 4 | 10 9 9 9 13 9 9 10 9 9 9
13 | 11 17 11 12 11 5 13 11 11 17 4 | 3 6 3 4 3 3 3 4 3 3 3
14 | 10 12 12 18 11 4 10 13 12 16 5 | 3 3 3 3 2 2 2 3 3 3 2
15 | 11 15 13 14 14 4 13 12 10 15 5 | 5 4 3 3 4 3 3 5 4 4 3
16E | 8 17 7 12 59 8 14 10 15 12 7 | 5 5 4 4 12 4 4 4 5 5 4
17 | 12 11 14 12 15 4 12 16 8 13 4 | 4 6 4 3 3 3 3 4 5 5 3
18E | 12 23 5 14 20 4 14 11 9 11 5 | 4 5 3 4 5 3 4 4 4 5 4
19 | 12 15 15 12 15 5 15 17 10 17 5 | 4 5 4 3 3 3 3 5 4 5 3
20E | 11 13 7 12 13 5 13 9 7 8 3 | 4 4 3 3 4 3 4 5 4 4 3
21 | 14 11 9 11 14 6 10 11 9 15 4 | 3 4 3 3 3 3 3 3 3 6 3
22E | 8 12 8 10 14 3 13 6 7 14 3 | 5 5 5 4 4 4 4 4 4 5 4
23 | 12 25 15 15 18 8 15 37 13 21 7 | 4 4 4 3 2 2 3 8 3 7 3
24 | 8 7 6 9 10 5 10 8 9 16 3 | 3 4 3 3 3 3 3 3 3 5 3
25E | 11 12 18 11 24 5 12 14 7 13 5 | 6 8 8 7 9 7 9999 8 6 7 7
26E | 13 47 17 11 22 7 11 7 12 12 7 | 4 13 5 4 6 3 5 4 5 5 4
27 | 8 7 5 7 10 4 8 6 8 10 3 | 4 4 3 3 3 3 4 3 3 4 3
28E | 13 18 8 10 32 6 14 11 9 10 5 | 5 8 5 5 9 4 4 4 5 4 4
29 | 13 21 10 15 8 4 18 11 9 16 5 | 4 3 3 4 3 3 3 4 4 5 3
30 | 7 11 5 6 10 3 10 10 7 7 3 | 5 5 5 5 5 5 5 6 5 5 5
31 | 10 19 13 13 15 4 12 12 11 13 4 | 7 7 6 7 6 6 6 7 8 7 6
32 | 7 10 7 7 8 4 8 10 8 12 3 | 3 4 3 3 3 3 3 4 3 4 3
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 12 11 19 5 12 12 9 13 |T 4 5 4 4 5 4 4 5 4 5 4
WRMS | 10 14 12 10 16 5 12 10 8 13 |NE 3 3 3 3 2 2 3 4 3 4 3
MEDI | 10 12 9 11 14 5 12 11 9 13 |MD 4 5 4 4 3 3 3 4 4 5 3
Table 3.1938.6 GPS week: 1938 Day: 6 MJD: 57816.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 10 5 10 8 4 12 6 6 14 3 | 3 4 3 3 2 3 3 4 3 4 3
2 | 11 13 13 13 11 8 9 14 10 15 4 | 3 4 3 3 3 3 3 4 3 5 3
3E | 16 10 22 12 18 6 12 8 9 10 5 | 27 28 27 27 27 27 27 27 27 27 27
X4E | 3 --- --- --- --- 58 --- --- --- --- 0 | 5 --- --- --- --- 7 --- --- --- --- 5
5E | 13 12 10 10 20 7 13 12 9 13 4 | 3 6 4 4 5 4 4 4 4 5 4
6 | 8 10 6 9 8 5 10 9 6 11 3 | 3 4 3 3 3 3 4 3 3 3 3
7 | 8 13 12 10 10 3 14 11 10 14 4 | 3 3 3 3 3 3 3 3 3 4 3
8 | 7 9 4 8 9 6 14 6 6 7 2 | 5 4 5 4 5 5 4 4 5 5 5
9 | 7 9 7 7 10 5 8 10 7 9 3 | 3 4 3 3 3 3 3 4 3 4 3
10E | 14 14 22 11 22 5 11 11 10 6 5 | 4 7 5 4 8 4 5 4 5 5 4
11 | 6 11 14 11 7 5 12 7 7 8 3 | 3 3 3 3 2 3 3 3 3 3 2
12E | 13 15 8 11 26 4 14 19 8 9 5 | 10 10 10 10 12 10 10 11 10 10 10
13 | 10 16 13 10 9 8 13 13 10 16 4 | 3 5 3 3 3 3 3 3 3 3 3
14 | 12 11 12 17 8 4 12 11 11 17 4 | 3 4 3 3 3 3 3 3 3 3 3
15 | 9 15 14 10 12 6 15 14 10 12 4 | 5 4 3 4 3 4 4 4 3 4 4
16E | 16 19 7 12 15 6 14 10 14 9 5 | 4 4 4 3 6 3 4 4 4 4 3
17 | 10 14 12 12 10 6 12 15 9 12 4 | 3 4 3 3 3 3 3 3 3 3 3
18E | 13 20 6 11 15 4 13 11 8 8 4 | 3 5 4 4 5 3 4 4 4 5 4
19 | 9 16 12 14 10 5 16 17 11 18 5 | 3 3 4 3 3 3 3 3 3 3 3
20E | 9 14 9 8 13 6 14 15 9 8 4 | 3 4 3 3 3 3 4 4 4 4 3
21 | 14 9 9 11 14 5 10 14 9 17 4 | 3 3 3 3 3 3 3 3 3 5 3
22E | 9 12 8 8 11 7 12 5 8 9 3 | 4 4 4 3 5 3 4 4 4 4 3
23 | 13 23 11 16 18 9 16 41 14 20 7 | 3 3 3 3 3 2 3 6 2 5 2
24 | 7 8 10 9 11 6 8 11 9 12 3 | 2 3 3 3 3 3 3 2 3 4 2
25E | 12 12 19 9 16 5 10 14 9 11 5 | 8 9 9 8 7 7 9999 9 7 7 8
26E | 13 11 21 9 21 5 11 9 12 11 5 | 4 6 5 4 7 4 5 4 4 5 4
27 | 7 7 5 9 7 3 11 8 5 9 2 | 3 4 3 3 2 3 3 3 3 3 3
28E | 9 14 9 9 15 5 11 11 9 8 4 | 3 5 5 4 5 3 4 4 4 4 4
29 | 12 22 12 13 10 4 16 13 9 17 5 | 3 3 3 3 3 3 3 3 3 4 3
30 | 6 7 6 9 9 4 9 12 7 8 3 | 6 6 6 6 6 6 5 7 6 5 6
31 | 11 15 13 12 13 5 12 15 9 16 5 | 8 7 7 8 7 7 7 7 8 8 7
32 | 7 9 7 7 9 4 7 10 6 10 3 | 3 4 3 3 3 3 3 3 3 3 3
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 12 11 14 5 12 14 9 12 |T 4 5 4 4 5 4 4 4 4 5 4
WRMS | 9 14 13 10 12 5 12 11 8 12 |NE 2 3 3 3 2 3 3 3 3 3 2
MEDI | 9 12 10 10 11 5 12 11 9 11 |MD 3 4 3 3 3 3 3 4 3 4 3
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 4.1938 GPS week: 1938 MJD: 57810.0-57816.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 |U 6 6 15 |U 9 12 33 |U 8 10 18 |
emr | emr 2976 | 8 10 24 |U 10 13 34 | 9 13 21 |
esa | esa 2976 | 7 7 19 |U 9 13 35 | 8 9 19 |
gfz | gfz 2975 |U 7 7 16 |U 9 13 36 |U 9 11 21 |
grg | grg 2975 |U 8 8 18 |U 11 16 38 | 9 11 20 |
igr | igr 2974 | 7 7 17 | 9 12 34 | 8 10 19 |
igs | igs 2975 | 7 7 17 | 9 12 34 | 8 10 19 |
jpl | jpl 2962 | 8 9 20 |U 10 13 34 | 9 11 20 |
mit | mit 2976 | 7 8 17 |U 10 15 37 |U 12 15 26 |
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 5.1938.0 GPS week: 1938 Day: 0 MJD: 57810.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 6 6 16 | 8 11 29 | 6 9 16 |
emr | emr 2976 | 7 10 26 | 8 9 32 | 6 12 20 |
esa | esa 2976 | 6 7 18 | 7 9 30 | 6 8 16 |
gfz | gfz 2976 | 6 7 19 | 8 9 33 | 6 8 16 |
grg | grg 2976 | 8 10 18 | 11 25 43 | 6 9 16 |
igr | igr 2976 | 6 6 18 | 8 9 30 | 5 7 14 |
igs | igs 2975 | 6 7 18 | 7 9 31 | 6 9 15 |
jpl | jpl 2976 | 7 10 22 | 9 10 31 | 7 10 17 |
mit | mit 2976 | 7 7 19 | 9 11 34 | 6 8 15 |
Table 5.1938.1 GPS week: 1938 Day: 1 MJD: 57811.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 6 7 15 | 10 14 37 | 7 7 12 |
emr | emr 2976 | 6 8 20 | 13 15 38 | 7 11 13 |
esa | esa 2976 | 6 7 19 | 11 15 40 | 7 7 13 |
gfz | gfz 2976 | 6 6 15 | 12 13 41 | 7 8 14 |
grg | grg 2976 | 6 7 15 | 13 14 41 | 8 9 15 |
igr | igr 2976 | 6 8 18 | 11 14 39 | 8 8 11 |
igs | igs 2976 | 6 6 15 | 11 13 39 | 7 8 12 |
jpl | jpl 2880 | 6 8 18 | 11 15 41 | 8 9 14 |
mit | mit 2976 | 5 7 13 | 11 14 43 | 21 35 43 |
Table 5.1938.2 GPS week: 1938 Day: 2 MJD: 57812.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 7 11 | 8 10 24 | 6 7 18 |
emr | emr 2976 | 6 11 20 | 9 11 23 | 7 9 19 |
esa | esa 2976 | 6 7 16 | 8 12 25 | 7 7 17 |
gfz | gfz 2976 | 5 7 14 | 9 13 25 | 7 6 18 |
grg | grg 2976 | 7 8 17 | 10 12 24 | 7 7 18 |
igr | igr 2976 | 5 7 13 | 8 11 24 | 7 7 18 |
igs | igs 2976 | 6 9 15 | 8 11 24 | 7 7 17 |
jpl | jpl 2976 | 7 9 17 | 9 12 26 | 7 10 20 |
mit | mit 2976 | 6 7 15 | 8 15 30 | 8 8 18 |
Table 5.1938.3 GPS week: 1938 Day: 3 MJD: 57813.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 4 9 | 9 9 23 | 10 12 23 |
emr | emr 2976 | 7 6 19 | 11 10 25 | 10 15 19 |
esa | esa 2976 | 7 5 15 | 9 10 26 | 9 12 21 |
gfz | gfz 2975 | 6 4 12 | 9 12 27 | 9 11 21 |
grg | grg 2975 | 8 6 16 | 11 12 28 | 10 14 21 |
igr | igr 2976 | 7 4 13 | 9 10 23 | 9 11 21 |
igs | igs 2976 | 7 5 14 | 9 11 24 | 9 13 20 |
jpl | jpl 2976 | 7 5 17 | 10 10 25 | 10 14 22 |
mit | mit 2976 | 6 5 12 | 11 14 28 | 12 15 26 |
Table 5.1938.4 GPS week: 1938 Day: 4 MJD: 57814.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 7 6 17 | 12 20 49 | 9 12 20 |
emr | emr 2976 | 9 10 26 | 12 19 54 | 11 18 25 |
esa | esa 2976 | 8 6 20 | 12 21 51 | 9 12 21 |
gfz | gfz 2976 | 7 7 18 | 11 22 54 | 9 12 22 |
grg | grg 2976 | 8 7 18 | 12 19 50 | 10 15 23 |
igr | igr 2968 | 8 6 18 | 11 21 55 | 10 14 23 |
igs | igs 2976 | 8 7 19 | 11 21 51 | 10 13 22 |
jpl | jpl 2976 | 9 9 24 | 12 19 47 | 9 13 22 |
mit | mit 2976 | 8 10 20 | 13 25 55 | 10 14 23 |
Table 5.1938.5 GPS week: 1938 Day: 5 MJD: 57815.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 | 8 9 19 | 9 13 42 | 9 13 19 |
emr | emr 2976 | 11 15 29 | 11 18 44 | 11 18 29 |
esa | esa 2976 | 9 10 23 | 9 14 47 | 9 12 22 |
gfz | gfz 2976 | 9 10 21 | 9 14 47 | 11 14 24 |
grg | grg 2976 | 10 11 23 | 10 17 48 | 11 17 27 |
igr | igr 2976 | 9 10 21 | 9 14 44 | 10 14 22 |
igs | igs 2976 | 9 10 21 | 9 15 44 | 10 15 23 |
jpl | jpl 2976 | 10 11 25 | 9 14 39 | 10 14 23 |
mit | mit 2976 | 11 12 23 | 11 16 38 | 14 13 30 |
Table 5.1938.6 GPS week: 1938 Day: 6 MJD: 57816.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 6 6 15 | 6 6 25 | 6 7 19 |
emr | emr 2976 | 9 9 25 | 8 9 23 | 9 9 23 |
esa | esa 2976 | 7 6 19 | 7 8 28 | 8 7 20 |
gfz | gfz 2976 | 7 5 16 | 7 8 26 | 11 18 31 |
grg | grg 2976 | 7 6 19 | 11 16 34 | 8 8 21 |
igr | igr 2976 | 6 6 17 | 6 7 24 | 7 7 21 |
igs | igs 2976 | 7 6 17 | 7 7 26 | 8 7 22 |
jpl | jpl 2976 | 8 9 19 | 7 8 26 | 9 9 22 |
mit | mit 2976 | 6 5 15 | 7 10 32 | 10 10 28 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1938 GPS week: 1938 MJD: 57810.500-57816.500
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 | -3 -1 53 27 -1 | 10 28
| 24 10 57 84 5 | 3
emr uuuux | 1 40 -181 50 40 | 1 38
| 29 40 146 62 22 | 8
esa uuuuu | 3 11 -24 4 0 | 24 35
| 12 10 48 36 4 | 3
gfz uuuuu | -8 10 58 -96 1 | 21 33
| 23 11 56 125 4 | 2
grg uuuuu | -3 8 14 14 -5 | 4 26
| 8 12 59 39 2 | 2
igr xxxxx | 4 13 15 22 -1 | 3 26
| 17 17 59 35 6 | 2
irf xxxxx | 9 -12 41 -9 1 | 2 26
| 12 9 22 13 3 | 2
jpl xxxxx | 2 -22 25 -17 -8 | 28 34
| 27 20 46 42 14 | 3
mit uuuuu | 14 -28 85 35 5 | 22 34
| 13 16 52 32 3 | 2
ngs uuuuu | -11 -26 22 25 2 | 13 31
| 39 26 71 135 7 | 3
sio uuuux | 12 2 -106 -56 18 | 71 75
| 9 22 80 72 8 | 5
Table 7.1938.0 GPS week: 1938 Day: 0 MJD: 57810.500
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 | -39 -10 26 -113 -8 | 15 32
emr uuuux | 30 -42 125 114 2 | -4 36
esa uuuuu | 5 11 -12 -25 -9 | 28 38
gfz uuuuu | -50 -2 58 -211 3 | 21 33
grg uuuuu | 4 18 -84 16 -3 | 7 26
igr xxxxx | 25 26 -55 31 5 | 4 26
irf xxxxx | 20 -6 15 -5 -2 | 4 27
jpl xxxxx | 28 -36 30 44 -12 | 33 40
mit uuuuu | 14 -5 71 37 3 | 23 35
ngs uuuuu | 31 19 -61 199 12 | 12 30
sio uuuux | 15 -7 -101 -18 15 | 65 69
Table 7.1938.1 GPS week: 1938 Day: 1 MJD: 57811.500
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 | -30 -14 -46 41 -5 | 13 31
emr uuuux | 5 51 -250 -31 61 | -7 35
esa uuuuu | 13 7 50 -62 1 | 26 37
gfz uuuuu | -24 17 63 -286 -1 | 21 33
grg uuuuu | -10 -3 -13 -28 -5 | 5 25
igr xxxxx | 15 18 81 11 0 | 4 26
irf xxxxx | 13 -2 72 -27 -1 | 3 27
jpl xxxxx | -24 -41 34 1 -11 | 30 38
mit uuuuu | 26 -19 166 30 3 | 22 34
ngs uuuuu | 15 -43 81 222 9 | 13 30
sio uuuux | 14 38 -149 44 23 | 67 70
Table 7.1938.2 GPS week: 1938 Day: 2 MJD: 57812.500
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 11 78 -12 -4 | 7 22
emr uuuux | 42 46 -284 54 38 | -10 31
esa uuuuu | 9 12 -20 23 0 | 20 27
gfz uuuuu | -6 -1 169 -143 3 | 16 26
grg uuuuu | 7 2 17 16 -6 | 0 21
igr xxxxx | 14 27 69 91 3 | -1 20
irf xxxxx | 22 -1 61 13 4 | -3 20
jpl xxxxx | 30 -21 25 -94 -19 | 23 29
mit uuuuu | 19 -34 125 73 3 | 17 26
ngs uuuuu | -44 -32 -93 27 8 | 8 24
sio uuuux | 11 1 -84 -4 11 | 65 68
Table 7.1938.3 GPS week: 1938 Day: 3 MJD: 57813.500
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 | 26 -7 69 44 -3 | 12 28
emr uuuux | 1 56 -290 12 57 | -1 39
esa uuuuu | 9 4 -11 2 2 | 25 35
gfz uuuuu | 9 13 78 -43 6 | 22 34
grg uuuuu | -8 8 18 -37 -3 | 6 25
igr xxxxx | 8 27 67 20 4 | 5 26
irf xxxxx | 16 -25 46 -9 1 | 3 26
jpl xxxxx | 27 3 -45 -26 15 | 28 34
mit uuuuu | 29 -52 64 81 5 | 22 34
ngs uuuuu | -71 -2 32 -21 -2 | 15 32
sio uuuux | 10 -11 -71 -45 11 | 72 77
Table 7.1938.4 GPS week: 1938 Day: 4 MJD: 57814.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 2 6 136 36 6 | 11 28
emr uuuux | -36 68 -251 16 55 | 4 41
esa uuuuu | 11 12 -21 24 1 | 25 35
gfz uuuuu | 15 3 20 83 -3 | 23 34
grg uuuuu | 1 2 36 79 -8 | 5 25
igr xxxxx | -9 -16 -59 3 2 | 5 26
irf xxxxx | -9 -14 47 -13 3 | 3 26
jpl xxxxx | -6 -24 -4 0 9 | 28 34
mit uuuuu | -10 -14 106 -8 9 | 22 34
ngs uuuuu | -2 -51 44 -120 -1 | 15 32
sio uuuux | 7 2 -221 -86 19 | 74 79
Table 7.1938.5 GPS week: 1938 Day: 5 MJD: 57815.500
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 | 11 -1 31 22 2 | 7 29
emr uuuux | 0 76 -129 147 19 | 8 41
esa uuuuu | -5 31 -109 43 5 | 22 35
gfz uuuuu | 10 27 -2 -51 -4 | 20 35
grg uuuuu | -15 31 12 10 -6 | 2 29
igr xxxxx | -2 13 -2 18 -10 | 3 28
irf xxxxx | 5 -22 24 -6 5 | 1 28
jpl xxxxx | -1 6 29 -13 -20 | 27 34
mit uuuuu | 14 -39 52 26 9 | 20 34
ngs uuuuu | -32 -50 65 -51 -5 | 13 33
sio uuuux | 27 -29 34 -113 16 | 74 79
Table 7.1938.6 GPS week: 1938 Day: 6 MJD: 57816.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 15 6 78 170 2 | 9 30
emr uuuux | -33 28 -186 37 50 | 14 43
esa uuuuu | -22 1 -45 22 0 | 24 37
gfz uuuuu | -7 14 23 -24 5 | 21 36
grg uuuuu | 3 -3 115 38 -5 | 2 29
igr xxxxx | -24 -3 5 -23 -8 | 4 29
irf xxxxx | -3 -13 21 -20 0 | 3 30
jpl xxxxx | -37 -43 107 -34 -17 | 25 32
mit uuuuu | 3 -32 10 8 5 | 23 37
ngs uuuuu | 24 -24 87 -85 -4 | 15 34
sio uuuux | -3 18 -152 -170 32 | 77 82
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