[IGSREPORT-22079] Wk 1753 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Aug 30 06:24:24 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1753 (Aug 11, 2013 - Aug 17, 2013)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
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:
igs1753[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1753[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1753[0-6].cls IGS GPS clock combination summary report.
igs17537.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17537.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 | 9 9 ARTU KOUC MOBS REYK ARTU KOUC MOBS REYK XMIS
0 | EMR | 8
0 | ESA | 9 9 IRKJ KOUC IRKJ KOUC UNSA
0 | GFZ | 9 9 GRAS GRAS TSKB
0 | GRG | 8 21 IRKJ NTUS IRKJ NRMD NTUS
0 | JPL | 8 21 KOUC
0 | MIT | 3 11 21 22 3 8 11 19 21 22 ALGO BREW CAS1 DAEJ DARW
0 | MIT | DAV1 DRAO GLSV GODE GRAZ HNPT IENG IRKT KOUR LAMA
0 | MIT | MAC1 MDVJ MIZU NRC1 NTUS NYAL OPMT PRDS PTBB SCH2
0 | MIT | SFER SYOG TIDB TSKB TWTF VILL WAB2 WSRT ZIMM DAEJ
0 | MIT | GOPE MDVJ NTUS TWTF USNO
1 | COD | 8 KOUC XMIS REYK
1 | EMR | 9 9 HARB HARB
1 | ESA | 8 CAGZ IRKJ KOUC CAGZ IRKJ KOUC UNSA
1 | GFZ | 9 8 9 DAEJ WES2 DGAR MATE WES2
1 | GRG | 9 9 HARB IRKJ LPGS HARB IRKJ LPGS
1 | JPL | 9
1 | MIT | 9 28 9 28 NICO NICO
2 | COD | 6 KOUC KOUC ZAMB
2 | EMR | 8
2 | ESA | IRKJ KOUC IRKJ KOUC
2 | GRG | 8 IRKJ IRKJ
2 | JPL | 8
2 | MIT | 15 19 28 8 15 19 28 NICO MDVJ NICO SCH2
3 | COD | 9 8 9 KOUC XMIS KOUC NKLG XMIS
3 | EMR | KERG MATE KERG MATE
3 | ESA | 9 8 9 IRKJ KOUC IRKJ KOUC MATE NKLG
3 | GFZ | 8 9 8 9 BRAZ KERG TSKB BRAZ KERG TSKB
3 | GRG | 21 21 IRKJ LPGS NKLG REUN IRKJ LPGS REUN
3 | JPL | 9
3 | MIT | 3 21 3 21 BOR1 SYDN BOR1 SYDN
4 | COD | 9 26 9 26 KOUC KOUC
4 | EMR | 8 HERS HERS MCM4 YELL
4 | ESA | 9 26 9 26 CAGZ IRKJ KOUC CAGZ IRKJ KERG KOUC WES2
4 | GFZ | 9 26 9 26 BRAZ BRAZ KERG YAKT
4 | GRG | IRKJ LPGS IRKJ
4 | JPL | 8 24 26
4 | MIT | 21 26 8 21 26 NICO NICO
5 | COD | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
5 | COD | 21 22 23 24 25 26 27 28 29 31 32 1 2 3 4 5 6 7 8
5 | COD | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
5 | COD | 26 27 28 29 31 32
5 | EMR | 24 24 YELL HARB YELL
5 | ESA | 8 9 8 9 CHUR IRKJ KOUC NTUS SCOR IRKJ KOUC SCOR UNSA
5 | GFZ | 9 8 9 MAW1 MCM4 THTI CHUR MAW1 MCM4 THTI
5 | GRG | NTUS CHUR NTUS
5 | JPL | 8 9 YELL
5 | MIT | MAW1 OPMT USNO MAW1 MDVJ OPMT SYOG USNO
6 | COD | 8 KOUC KOUC
6 | ESA | 8 IRKJ KOUC NTUS IRKJ KOUC NTUS UNSA
6 | GFZ | 8 8
6 | GRG | AREQ IRKJ MAW1 USNO AREQ IRKJ MAW1 USNO
6 | MIT | 9 9 15
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | MIT | ~05:30 | ~ 0.37 ns
1 | COD | ~13:50 | ~ -0.72 ns
4 | GRG | ~14:10 | ~ 0.16 ns
5 | GRG | ~12:30 | ~ -0.22 ns
6. 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.
7. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G09 | 2013_08_13 | 2013045
8. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
4 | COD | 24
9. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G24 | 4 | | 4 | 4 | 4 | 4 | 4 |
10. 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.
11. 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 | .2 -.7 .2 -17 45 -11 .09
EMR | 0 | 2.2 -.8 -8.1 -11 -14 -26 .01
ESA | 0 | -3.0 -2.9 8.2 67 -5 -25 -.22
GFZ | 0 | .4 .1 -.3 -15 -22 -19 -.37
GRG | 0 | -4.2 -1.5 7.0 -21 49 -28 .23
JPL | 0 | -5.8 -1.5 -3.4 -45 53 -27 .34
MIT | 0 | -1.8 -3.3 4.9 -3 16 -47 .18
NGS | 0 | -1.8 -7.2 -1.8 -29 21 -35 .18
SIO | 0 | -2.7 -1.1 -12.5 -41 -48 -87 .07
COD | 1 | .3 1.2 -.9 -17 25 -30 .35
EMR | 1 | -4.5 3.6 -5.4 -6 -21 -17 .28
ESA | 1 | -1.4 .2 16.3 87 -63 -4 .09
GFZ | 1 | .5 -.7 -.4 -19 -40 3 -.28
GRG | 1 | -.7 -10.8 16.8 -37 36 -19 .53
JPL | 1 | -9.4 -2.5 -4.0 -67 37 -21 .12
MIT | 1 | -.5 -.7 3.0 -12 12 -63 .29
NGS | 1 | 1.2 -3.4 9.8 -62 -21 -10 .28
SIO | 1 | -5.5 -2.6 -18.1 -57 -23 -118 .27
COD | 2 | .2 .1 -.5 -21 29 -11 .14
EMR | 2 | -.9 2.1 1.9 -4 -12 -13 .12
ESA | 2 | 1.4 -1.3 14.3 81 -38 -19 -.19
GFZ | 2 | .2 -.1 -.5 -19 -38 0 -.49
GRG | 2 | 3.3 -5.9 18.8 -32 36 -10 .14
JPL | 2 | -2.3 6.6 6.8 -66 9 -5 .06
MIT | 2 | 2.2 -.2 5.9 -1 27 -50 .12
NGS | 2 | -1.2 -4.4 8.3 -59 -2 -18 .22
SIO | 2 | -2.6 -1.4 -8.3 -28 -38 -85 .01
COD | 3 | .0 1.4 -.7 -22 55 -15 .14
EMR | 3 | 1.4 1.3 -.2 -1 -8 -1 .11
ESA | 3 | 1.9 -.3 16.7 91 -51 -15 .07
GFZ | 3 | .1 .1 -.6 -21 -37 2 -.34
GRG | 3 | .9 -3.0 4.6 -25 11 -4 .19
JPL | 3 | -.9 6.0 -6.2 -88 35 -22 .10
MIT | 3 | .3 6.2 7.7 -1 17 -49 .14
NGS | 3 | -2.5 -2.7 5.5 -44 9 -18 .26
SIO | 3 | -.5 2.4 6.3 3 -12 -141 -.03
COD | 4 | .1 -.3 -.6 -29 30 6 .14
EMR | 4 | -12.1 2.7 -.3 0 -19 -10 .15
ESA | 4 | -5.6 2.1 21.6 89 -133 58 -.05
GFZ | 4 | .7 -.2 -.4 -18 -34 1 -.49
GRG | 4 | -5.4 .3 24.4 -39 26 1 .26
JPL | 4 | -8.8 1.3 9.9 -78 14 -34 .08
MIT | 4 | -4.9 6.1 10.2 1 23 -59 -.04
NGS | 4 | -1.5 5.3 9.7 -18 9 16 .07
SIO | 4 | -2.3 2.0 -21.9 -31 -87 -229 -.24
COD | 5 | -.3 .7 -.3 -28 48 0 .09
EMR | 5 | 11.4 4.1 6.8 -13 -3 -24 -.08
ESA | 5 | .1 -1.8 18.9 54 -54 -26 -.20
GFZ | 5 | .5 .2 .1 -39 -36 -8 -.62
GRG | 5 | 5.3 -7.7 20.1 -23 40 7 .23
JPL | 5 | -4.2 .0 5.9 -56 51 -36 .24
MIT | 5 | 2.0 3.4 10.9 -9 10 -50 .14
NGS | 5 | 4.0 -1.9 12.9 -72 -25 17 .02
SIO | 5 | -1.6 1.5 -12.3 -43 -51 -183 .02
COD | 6 | -.5 .4 -.6 -32 42 -6 .02
EMR | 6 | -2.1 2.6 6.0 -12 -6 -32 -.07
ESA | 6 | 1.3 1.4 19.6 73 -77 -8 -.23
GFZ | 6 | .4 -.1 .3 -38 -30 -1 -.80
GRG | 6 | 5.5 -5.8 16.4 -32 27 -6 .10
JPL | 6 | -3.7 5.4 6.5 -96 54 -36 .14
MIT | 6 | -3.0 .5 6.3 -7 14 -49 .03
NGS | 6 | 1.0 4.1 13.8 -39 -15 13 .14
SIO | 6 | -1.8 2.1 -8.8 -6 -22 -86 -.04
12. 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.
13. 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.
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 1.1753.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1753.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 2.1753.[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 3.1753.[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 5.1753.0-6). 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 1753 summary. (Aug 11, 2013 - Aug 17, 2013)
Table 1.1753.a GPS week: 1753 MJD: 56515.000-56521.000
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 0 29 19 .23 10 10 | -1199 -85 465 617
| 0 0 1 13 15 13 .03 | 526 597
emr 80| 0 0 -2 14 2 9 .11 16 16 | 1377 111 15 99
| 2 1 1 26 15 16 .03 | 825 1220
esa 150| 0 0 0 28 -25 -11 -.10 7 6 | -507 -149 17 142
| 0 0 1 15 23 8 .02 | 919 1254
gfz 192| 0 2 -1 -4 -19 -14 -.55 11 10 | 66 -84 13 92
| 1 0 2 33 34 10 .04 | 363 589
grg 133| 1 0 9 -9 14 14 .44 14 14 | -41 -34 19 152
| 1 0 1 20 19 20 .07 | 247 303
igr n/a| 0 0 0 -13 14 -8 -.33 5 5 | -11412 -130 17 77
| 0 0 1 17 21 15 .02 | 1231 1104
jpl 80| 0 0 -4 -20 18 -16 .17 15 15 | 761 19 16 101
| 2 0 2 11 20 14 .04 | 801 1057
mit 231| 0 0 0 8 16 6 -.10 11 10 | -28 -93 27 249
| 1 0 1 26 26 22 .05 | 366 310
ngs 240| 0 0 0 -45 -12 -6 .10 12 10 | 169595 -61751 1692 3413
| 1 0 1 38 49 27 .03 | 519009 464684
sio 443| 1 0 -2 -14 -46 -151 -.60 19 19 | --- --- --- ---
| 1 0 1 56 27 77 .04 | --- ---
Table 1.1753.b GPS week : 1753 MJD: 56515.000-56521.000
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 4 4 4 4 4 4 |
2 | 4 4 4 5 5 5 5 |
3 | 4 4 3 4 4 4 4 |
4 | 3 3 3 3 4 4 4 |
5 | 4 4 4 4 4 5 5 |
6 | 4 4 11 3 4 4 4 |
7 | 4 5 4 4 5 5 4 |
8 | 4 4 4 4 5 6 7 |
9 | 4 5 0 6 5 6 6 |
10 | 3 3 3 3 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 4 4 4 4 6 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 4 5 4 4 4 4 5 |
15 | 4 5 5 5 5 5 5 |
16 | 5 7 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 4 4 5 5 4 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 5 4 4 |
21 | 5 5 5 6 5 5 5 |
22 | 4 4 4 4 4 5 5 |
23 | 4 5 5 4 4 4 5 |
24 | 5 5 5 4 12 5 5 |
25 | 4 5 4 3 4 4 4 |
26 | 3 4 4 4 4 4 4 |
27 | 4 5 5 5 5 5 4 |
28 | 4 5 4 4 5 5 5 |
29 | 5 5 4 4 5 5 5 |
31 | 5 6 4 4 6 5 5 |
32 | 4 3 3 3 4 4 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 2.1753.0 GPS week: 1753 Day: 0 MJD: 56515.000
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 263| 0 -1 1 20 41 36 .21 10 10 | -1147 178 23 433
emr 80| 0 0 -5 57 17 33 .11 16 16 | 1772 263 13 129
esa 150| 0 0 2 55 26 -18 -.09 6 6 | -567 646 17 168
gfz 192| 0 2 0 -66 -61 -30 -.53 9 9 | -248 626 13 110
grg 134| 2 0 6 -8 23 0 .38 15 14 | 102 -210 18 164
igr n/a| 0 0 1 14 9 7 -.30 4 4 | -9881 -354 18 91
jpl 80| 1 0 -2 -2 37 -11 .20 14 14 | 1191 341 15 126
mit 238| 0 0 0 -24 -6 26 -.01 12 11 | -75 -243 39 387
ngs 240| 0 0 -3 -49 -59 -11 .15 9 8 | -1155 229 1689 2954
sio 442| 0 0 -1 -66 -67 -72 -.57 20 17 | --- --- --- ---
Table 2.1753.1 GPS week: 1753 Day: 1 MJD: 56516.000
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 265| 1 -1 1 -3 4 8 .19 10 10 | -1258 676 19 98
emr 80| -1 0 -4 16 1 17 .10 15 15 | 2376 307 15 95
esa 150| 0 0 1 18 -31 -21 -.10 8 7 | 682 -1280 19 202
gfz 196| 1 0 -3 36 38 -22 -.56 11 10 | 625 126 12 90
grg 136| 0 0 9 -37 37 9 .38 14 13 | 13 244 22 170
igr n/a| 0 0 1 -17 -12 1 -.35 5 5 | -10012 -158 19 73
jpl 80| 0 1 -3 -33 20 4 .16 14 13 | 1768 228 15 96
mit 237| 0 -1 0 52 31 26 -.06 11 10 | 27 238 25 219
ngs 243| 0 0 0 -72 -58 -6 .09 12 10 | -965 329 1469 3608
sio 449| 0 0 -2 -37 -38 -125 -.58 19 18 | --- --- --- ---
Table 2.1753.2 GPS week: 1753 Day: 2 MJD: 56517.000
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 263| 1 0 0 7 24 8 .26 9 9 | -1023 -118 17 95
emr 80| 0 0 0 -3 -19 16 .07 15 15 | 2408 -2118 15 96
esa 150| 0 0 0 22 -39 -10 -.11 6 6 | 335 -1633 18 147
gfz 193| -2 3 0 -25 -33 -10 -.60 11 11 | 173 -994 12 80
grg 133| 0 0 10 -32 22 -14 .42 14 14 | 318 -417 17 156
igr n/a| 0 0 1 -9 -7 8 -.32 5 5 | -10580 -2101 16 80
jpl 80| 1 0 -8 -14 6 -13 .21 14 15 | 1699 -2066 16 100
mit 235| 0 0 0 -5 8 27 -.11 9 9 | 665 -432 29 217
ngs 241| -2 2 0 17 52 -31 .08 11 10 | -147729 567698 1471 2891
sio 448| 1 0 -2 -40 -78 -79 -.68 18 18 | --- --- --- ---
Table 2.1753.3 GPS week: 1753 Day: 3 MJD: 56518.000
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| 1 -1 0 -4 18 17 .28 9 9 | -492 -874 20 92
emr 80| 1 0 0 -5 14 0 .14 15 15 | 1252 -626 17 102
esa 150| 0 0 -1 25 -37 -14 -.06 6 6 | 104 -1340 18 122
gfz 196| -2 1 1 -1 -2 -10 -.59 10 10 | 386 -669 11 92
grg 139| 1 0 8 -10 -12 11 .41 16 14 | -93 -111 16 133
igr n/a| 0 0 1 -25 16 -12 -.32 6 5 | -11812 -610 16 75
jpl 80| 1 0 -2 -36 21 -15 .18 15 15 | 469 -385 16 100
mit 227| 0 0 1 6 27 -1 -.11 11 10 | -334 55 22 246
ngs 243| -2 1 0 -11 21 23 .10 11 9 | 1340049 -999999 1869 3898
sio 442| 1 1 0 -26 -14 -170 -.57 18 18 | --- --- --- ---
Table 2.1753.4 GPS week: 1753 Day: 4 MJD: 56519.000
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 -1 3 -14 40 36 .23 10 10 | -835 -706 19 93
emr 80| -5 2 -2 -18 18 -6 .16 16 16 | 668 368 16 83
esa 150| 0 -1 0 14 -26 -1 -.09 6 6 | -893 1170 18 119
gfz 193| 0 1 -4 9 -49 0 -.49 10 10 | -389 523 14 89
grg 135| 3 1 12 -1 19 24 .46 15 14 | -277 298 21 144
igr n/a| 0 -1 0 -27 48 -8 -.31 5 5 | -12201 301 20 65
jpl 80| -2 0 -4 -21 34 -10 .19 16 16 | 448 360 18 97
mit 229| 1 -1 -1 22 43 7 -.11 11 9 | -123 41 22 195
ngs 241| 0 0 0 -33 -72 -50 .11 15 14 | -776 -752 1638 3755
sio 446| 4 0 -4 -45 -78 -257 -.61 20 18 | --- --- --- ---
Table 2.1753.5 GPS week: 1753 Day: 5 MJD: 56520.000
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 255| 0 0 3 -12 24 25 .22 10 10 | -2155 -322 3139 3416
emr 81| 3 0 -2 38 -10 -13 .08 17 17 | 363 790 15 101
esa 150| 0 0 -2 42 -35 -14 -.10 7 6 | -1670 90 18 120
gfz 190| -2 2 -3 -3 3 -9 -.55 12 11 | -180 -96 15 97
grg 129| 2 0 7 14 24 48 .43 13 13 | 70 -324 21 155
igr n/a| 0 0 0 4 18 -21 -.35 5 5 | -12731 554 19 90
jpl 80| 0 0 -3 -11 -22 -39 .12 15 15 | -11 277 17 102
mit 229| 0 0 0 -14 37 -7 -.15 12 10 | 115 -534 23 239
ngs 238| -1 0 0 -85 4 7 .06 13 11 | -806 -316 1741 3268
sio 435| 0 0 -3 16 -24 -252 -.63 20 21 | --- --- --- ---
Table 2.1753.6 GPS week: 1753 Day: 6 MJD: 56521.000
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 253| 0 -1 1 11 51 5 .20 10 10 | -1486 569 24 94
emr 80| -2 -1 -2 13 -5 15 .11 16 16 | 806 1797 17 91
esa 150| 2 0 0 17 -36 3 -.14 7 7 | -1543 1304 17 121
gfz 188| 0 2 -2 17 -29 -17 -.55 12 11 | 96 -107 16 92
grg 130| 2 0 9 11 -12 22 .58 15 14 | -421 279 24 142
igr n/a| 0 0 1 -32 31 -33 -.34 5 4 | -12668 1452 16 67
jpl 80| -3 1 -4 -21 29 -32 .12 15 15 | -237 1384 16 90
mit 228| -1 0 -1 18 -27 -32 -.17 14 13 | -474 218 30 246
ngs 236| 1 0 1 -84 25 23 .14 11 9 | -1451 551 1968 3520
sio 445| 1 0 -5 101 -22 -104 -.56 22 21 | --- --- --- ---
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 3.1753.0 GPS week: 1753 Day: 0 MJD: 56515.000
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 17 5 7 11 6 10 10 8 9 3 | 21 22 17 10 24 12 22 15 20 14 15
2 | 12 16 5 9 14 4 16 15 10 19 4 | 29 26 19 16 28 19 22 22 27 20 20
3 | 9 11 5 7 15 5 9 14 5 19 3 | 28 31 23 17 24 21 29 25 26 29 23
4 | 7 13 4 8 10 5 11 8 6 20 3 | 17 26 15 14 20 17 25 19 18 24 16
5 | 8 16 5 7 8 6 14 7 8 23 3 | 30 34 29 29 32 28 35 28 30 29 29
6 | 8 12 6 7 17 5 10 16 8 21 3 | 22 27 19 12 22 16 24 18 22 20 19
7E | 8 18 6 10 13 3 17 13 9 9 4 | 35 36 29 26 36 29 34 35 33 28 30
8E | 9 14 8 8 12 3 13 10 7 20 3 | 30 38 35 38 29 35 37 32 32 30 33
9E | 11 21 6 9 14 4 14 13 6 21 4 | 22 28 13 15 15 18 21 16 15 14 21
10 | 8 10 3 6 13 4 7 8 10 14 3 | 22 27 24 25 35 26 25 24 29 22 24
11E | 8 15 5 8 15 4 11 14 11 8 4 | 29 30 21 15 33 19 28 26 26 20 23
12 | 10 14 6 9 18 5 16 9 8 26 4 | 24 26 22 21 30 20 27 21 24 26 21
13 | 9 17 5 7 15 4 14 9 6 18 3 | 26 31 24 20 39 22 30 22 24 18 24
14 | 10 16 5 12 15 4 17 11 7 25 4 | 25 27 25 28 34 25 24 29 27 32 24
15 | 9 18 6 10 16 5 17 9 11 24 4 | 32 37 28 30 37 27 38 30 32 27 30
16 | 13 20 7 9 19 5 17 15 6 35 4 | 29 30 22 25 30 21 29 23 28 34 23
17 | 17 15 4 12 17 5 15 11 10 16 4 | 33 26 19 15 32 19 29 22 28 19 22
18 | 12 16 7 10 10 4 15 20 11 28 4 | 20 21 21 22 24 20 22 33 21 26 19
19 | 8 15 6 8 19 4 13 11 10 17 4 | 27 30 19 15 31 18 26 19 25 17 21
20 | 9 13 6 13 13 4 13 11 7 16 3 | 28 29 27 30 34 28 30 30 27 25 28
21 | 11 20 11 13 19 4 16 15 12 19 5 | 20 23 21 13 25 16 20 17 17 18 15
22 | 12 17 4 8 12 3 15 15 10 26 4 | 29 26 26 28 36 27 28 37 28 32 27
23 | 8 18 6 9 15 3 17 10 7 21 4 | 23 27 22 18 32 19 26 18 22 17 20
24E | 8 14 6 13 19 5 11 15 12 12 4 | 221 219 220 220 223 220 160 220 137 10 219
25 | 10 12 7 7 18 4 13 16 10 14 4 | 19 23 21 14 31 19 29 22 23 16 20
26 | 7 12 6 7 11 2 9 7 11 13 3 | 20 24 19 16 25 17 23 21 24 13 19
X27 | 10 14 3 11 --- 6 11 16 9 15 4 | 45 48 43 39 --- 40 47 39 41 43 42
28 | 10 16 5 12 17 4 14 8 13 27 4 | 26 29 23 28 32 22 29 26 27 27 24
29 | 11 21 6 11 15 4 18 14 12 20 4 | 21 28 14 15 23 16 26 21 24 18 16
31E | 11 17 5 11 22 6 18 9 9 11 4 | 27 26 18 17 21 17 25 23 24 15 19
32 | 14 9 4 8 14 4 8 8 6 15 3 | 19 20 12 12 23 11 18 15 14 13 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 6 9 15 4 14 12 9 20 |T 32 34 28 27 35 27 31 30 28 22 29
WRMS | 10 16 6 9 14 4 14 11 8 17 |NE 25 27 22 20 29 21 27 23 25 23 22
MEDI | 9 16 6 9 15 4 14 11 9 19 |MD 26 27 22 18 30 20 27 23 26 20 22
Table 3.1753.1 GPS week: 1753 Day: 1 MJD: 56516.000
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 17 8 8 14 6 12 9 15 12 4 | 21 22 18 20 22 15 21 19 23 17 17
2 | 12 15 7 9 14 5 16 7 9 16 4 | 22 20 18 14 26 15 19 16 22 14 16
3 | 7 11 8 9 14 6 9 9 11 15 3 | 24 25 23 18 24 17 24 22 23 20 21
4 | 6 11 6 7 9 5 13 10 9 17 3 | 21 22 17 12 18 15 22 18 18 20 17
5 | 11 14 7 7 10 6 13 8 9 22 3 | 25 25 20 19 21 20 24 18 22 20 19
6 | 7 11 8 8 13 5 9 10 11 12 3 | 21 25 19 17 22 17 24 21 21 19 19
7E | 7 15 7 12 10 3 17 14 10 11 4 | 24 23 21 19 26 20 24 25 27 20 21
8E | 10 13 9 12 11 5 13 7 12 20 4 | 26 33 30 36 24 31 31 28 30 26 28
9E | 10 21 9 15 12 6 12 14 14 21 5 | 25 30 14 18 19 16 23 21 24 21 25
10 | 9 7 4 7 11 4 7 6 7 14 2 | 16 15 12 17 17 14 16 15 17 16 13
11E | 7 14 7 8 14 4 12 10 15 10 4 | 26 26 19 18 32 17 25 21 27 19 21
12 | 10 14 6 10 16 4 16 12 8 26 4 | 22 23 21 20 27 18 26 18 24 24 20
13 | 7 16 7 9 17 4 14 8 11 17 4 | 18 25 18 14 33 15 26 17 22 15 18
14 | 14 17 9 10 14 5 13 14 14 20 5 | 18 24 22 18 29 19 24 25 20 25 19
15 | 10 17 8 14 12 6 18 8 14 23 4 | 25 28 22 23 28 20 29 22 25 18 22
16 | 12 19 26 14 17 6 18 9 16 35 6 | 27 24 39 22 24 18 24 18 23 30 21
17 | 20 16 7 10 14 6 15 15 10 15 5 | 34 24 20 17 32 20 26 26 30 19 23
18 | 9 15 7 13 11 3 12 17 12 28 4 | 15 19 20 17 21 15 21 24 15 22 15
19 | 5 16 6 9 18 5 14 9 14 14 4 | 23 25 20 12 31 16 24 19 23 15 19
20 | 9 13 8 14 13 3 14 11 11 14 4 | 30 28 26 28 29 25 27 26 29 25 26
21 | 8 19 7 13 19 4 10 12 10 18 4 | 14 23 13 19 26 12 18 16 18 19 13
22 | 9 16 5 9 13 5 11 10 11 28 4 | 19 22 21 19 27 19 24 24 20 24 19
23 | 7 18 9 9 13 3 18 9 10 21 4 | 19 24 18 14 27 13 24 16 20 14 16
24E | 10 11 9 15 12 5 12 16 18 12 5 | 121 123 121 119 117 121 115 121 95 13 120
25 | 9 12 6 7 16 4 14 15 13 12 4 | 17 23 20 14 26 17 30 18 21 16 18
26 | 6 10 7 11 11 4 10 9 13 10 3 | 18 19 15 15 20 13 18 16 19 12 15
X27 | 11 14 9 10 --- 7 13 12 11 12 4 | 35 35 35 28 --- 30 37 29 34 31 32
28 | 11 15 7 14 13 5 14 9 12 26 4 | 25 24 22 24 26 18 25 22 26 27 22
29 | 11 21 6 15 16 5 16 12 12 16 5 | 18 25 14 20 22 15 23 19 20 14 15
31E | 21 16 8 10 19 6 15 10 14 12 5 | 35 25 20 18 20 21 24 16 26 19 20
32 | 12 9 4 8 11 4 9 8 10 15 3 | 17 14 12 8 18 12 13 13 13 15 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 8 11 14 5 14 11 12 19 |T 25 27 23 21 27 21 26 23 25 19 22
WRMS | 10 15 7 10 13 5 13 10 10 18 |NE 21 23 20 17 24 17 23 19 21 19 18
MEDI | 9 15 7 10 13 5 13 10 11 16 |MD 22 24 20 18 26 17 24 19 23 19 19
Table 3.1753.2 GPS week: 1753 Day: 2 MJD: 56517.000
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 24 6 8 10 7 11 7 11 13 4 | 17 27 13 10 22 12 21 13 17 12 13
2 | 9 14 6 10 12 4 18 10 10 15 4 | 23 20 15 16 25 15 20 18 22 11 17
3 | 5 12 4 9 12 4 10 11 10 16 3 | 25 28 21 16 23 19 28 22 27 20 22
4 | 5 11 4 10 9 4 13 7 9 18 3 | 14 21 12 13 16 12 20 16 17 20 13
5 | 10 14 6 6 10 5 15 8 13 21 3 | 24 28 24 22 26 21 28 21 28 22 23
X6 | 16 17 --- --- 27 16 --- 12 33 --- 10 | 25 25 --- --- 35 22 --- 18 40 --- 22
7E | 7 15 5 8 10 4 14 13 9 12 3 | 18 18 15 16 19 16 21 19 20 18 16
8E | 8 13 10 11 15 4 12 8 9 19 4 | 27 33 31 37 24 31 34 28 27 25 28
X9E | 4 --- --- --- --- 70 --- --- --- --- 0 | 48 --- --- --- --- 51 --- --- --- --- 47
10 | 5 7 3 9 11 4 8 5 9 11 2 | 18 20 18 22 26 21 17 20 23 18 19
11E | 7 14 6 10 13 6 13 10 7 8 3 | 26 26 22 15 33 20 25 24 25 21 23
12 | 10 15 7 12 15 4 14 9 13 25 4 | 22 19 19 17 28 17 24 19 24 23 18
13 | 6 18 7 11 15 4 19 7 12 16 4 | 20 27 19 19 34 18 27 17 21 15 19
14 | 11 16 8 14 10 4 16 10 10 20 4 | 20 21 20 25 29 16 21 21 19 22 19
15 | 11 16 7 12 11 7 20 9 14 20 4 | 27 29 22 23 30 22 33 24 27 20 23
16 | 14 21 7 12 18 4 16 9 11 33 5 | 28 26 23 21 28 17 26 19 22 28 20
17 | 11 16 6 13 14 4 16 14 16 12 4 | 27 21 13 11 28 13 22 18 29 13 17
18 | 11 12 6 11 10 4 14 10 8 23 3 | 18 20 15 19 20 12 20 18 18 15 15
19 | 7 17 5 10 18 5 13 8 12 12 4 | 23 26 16 14 32 16 24 17 21 13 18
20 | 9 13 6 14 12 4 15 9 14 19 4 | 28 27 25 29 30 24 27 25 26 22 25
21 | 12 17 5 14 15 6 14 11 11 11 4 | 19 21 13 18 27 12 20 13 22 13 14
22 | 10 16 4 10 10 4 17 8 9 27 3 | 21 22 19 24 24 17 23 23 20 24 19
23 | 7 19 7 12 13 3 20 9 10 20 4 | 20 25 17 17 27 16 25 15 22 15 17
24E | 9 9 6 17 18 7 14 14 16 10 4 | 206 203 204 207 205 205 163 205 163 18 205
25 | 6 11 6 13 14 4 12 6 6 10 3 | 23 22 21 18 28 16 31 16 20 14 19
26 | 8 9 7 8 15 4 12 9 11 9 3 | 16 19 15 14 22 13 17 18 17 12 14
X27 | 8 14 5 12 --- 6 13 12 14 12 4 | 37 38 30 30 --- 32 38 31 39 33 33
28 | 8 16 4 13 14 4 14 9 14 25 4 | 24 24 21 23 26 17 27 23 20 26 21
29 | 11 19 7 10 15 5 14 8 9 11 4 | 19 22 13 16 22 13 19 15 23 12 14
31E | 11 14 5 12 19 5 14 8 12 14 4 | 28 21 18 13 19 17 24 22 25 17 19
32 | 9 10 4 11 13 5 8 6 11 16 3 | 15 14 11 14 18 10 16 13 14 13 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 6 11 14 5 14 9 11 18 |T 29 29 25 25 31 24 29 25 27 18 25
WRMS | 9 15 6 11 14 5 15 9 10 18 |NE 22 23 18 18 26 16 23 18 23 18 18
MEDI | 9 14 6 11 13 4 14 9 11 16 |MD 23 22 19 18 26 17 24 19 22 18 19
Table 3.1753.3 GPS week: 1753 Day: 3 MJD: 56518.000
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 | 10 20 5 7 12 6 10 6 12 11 3 | 22 24 17 16 25 13 21 17 24 16 17
2 | 13 15 7 8 14 5 21 13 9 15 4 | 23 20 18 16 28 14 23 22 22 14 18
3 | 7 13 5 12 12 5 11 12 8 13 3 | 24 24 19 14 22 16 25 22 23 21 19
4 | 8 12 6 7 10 4 12 10 8 18 3 | 19 24 19 15 20 13 22 18 16 21 17
5 | 8 16 6 9 11 3 14 11 7 22 3 | 31 32 28 27 28 26 32 25 28 28 27
6 | 8 13 5 8 13 6 11 7 8 13 3 | 20 21 18 13 18 10 23 15 22 16 15
7E | 9 17 5 11 11 5 17 11 10 14 4 | 32 25 23 27 29 23 28 28 27 27 25
8E | 9 14 7 13 15 5 17 11 11 20 4 | 27 29 28 37 23 29 30 28 25 24 27
9E | 10 18 9 11 14 20 15 11 30 16 5 | 36 34 25 26 33 35 35 29 43 26 34
10 | 8 8 3 9 14 5 10 6 8 12 3 | 16 19 16 22 25 18 20 21 17 19 17
11E | 8 13 6 7 12 4 13 9 9 8 3 | 27 25 21 17 34 17 24 24 27 21 22
12 | 11 13 5 7 14 4 16 11 8 25 3 | 25 23 22 19 28 18 27 22 27 27 21
13 | 5 17 5 9 17 5 15 8 10 16 4 | 21 26 18 23 37 19 27 19 22 18 20
14 | 9 17 5 12 12 4 13 9 10 21 4 | 23 25 23 29 29 22 26 24 23 25 23
15 | 12 19 7 12 15 3 22 9 13 21 4 | 28 34 23 22 30 22 36 23 26 24 24
16 | 14 18 5 13 14 6 16 10 10 34 4 | 29 23 23 23 26 17 24 18 23 28 20
17 | 10 15 7 11 14 5 18 21 13 13 5 | 32 24 20 20 32 20 24 26 27 18 22
18 | 12 13 5 10 9 3 16 9 7 24 3 | 20 20 18 21 22 14 20 21 17 16 17
19 | 6 17 5 12 15 4 13 10 9 12 4 | 23 25 17 10 29 13 22 17 22 14 17
20 | 9 13 6 12 13 5 17 13 12 15 4 | 25 25 23 25 30 22 28 26 23 21 23
21 | 11 17 4 10 45 6 17 11 9 11 6 | 17 19 15 14 47 10 18 12 21 12 14
22 | 10 16 4 8 10 3 14 11 12 27 3 | 26 25 23 28 29 22 25 27 18 28 23
23 | 7 18 5 11 14 4 16 9 9 21 4 | 21 24 18 20 29 16 24 18 18 21 18
24E | 11 13 5 10 15 5 18 12 13 18 4 | 262 256 257 258 262 257 206 262 352 17 259
25 | 9 11 5 6 14 3 13 6 9 10 3 | 22 24 22 13 26 16 30 16 20 14 19
26 | 8 13 7 7 13 3 13 12 10 11 3 | 18 19 16 17 21 13 18 21 16 15 15
X27 | 9 14 7 12 --- 6 15 12 13 12 4 | 42 42 36 32 --- 34 42 35 35 39 36
28 | 9 18 6 13 14 5 14 12 8 25 4 | 27 25 26 29 32 20 27 27 29 28 25
29 | 9 21 5 10 12 4 16 9 9 12 4 | 24 23 18 18 22 14 23 17 25 17 18
31E | 9 15 5 8 20 5 17 9 11 16 4 | 24 20 15 14 19 13 23 17 23 20 16
32 | 9 8 5 10 13 6 9 9 10 16 3 | 17 14 13 12 18 11 15 12 10 14 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 6 10 16 6 15 11 11 18 |T 32 32 28 28 35 26 31 29 33 20 28
WRMS | 9 15 6 10 14 5 15 10 9 18 |NE 23 24 20 19 27 17 24 20 22 20 19
MEDI | 9 15 5 10 14 5 15 10 10 16 |MD 24 24 20 20 28 17 24 22 23 21 20
Table 3.1753.4 GPS week: 1753 Day: 4 MJD: 56519.000
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 15 6 10 10 5 11 6 12 12 3 | 21 24 20 16 23 18 26 21 23 19 18
2 | 11 15 7 9 12 5 21 13 13 15 4 | 25 23 19 17 26 17 21 23 23 17 19
3 | 8 15 4 7 14 7 14 12 13 19 4 | 25 30 24 19 26 19 33 24 27 23 23
4 | 10 11 4 10 13 5 10 7 15 20 3 | 20 24 17 19 16 15 20 18 18 21 17
5 | 8 15 7 7 9 7 16 7 11 21 3 | 21 28 23 23 24 24 27 20 24 24 21
6 | 9 14 4 9 11 6 14 8 14 18 3 | 21 23 21 17 24 19 25 19 22 18 19
7E | 8 14 7 12 16 5 18 15 14 9 4 | 22 23 16 15 21 14 23 22 21 17 16
8E | 10 14 10 11 13 5 16 11 14 33 4 | 25 34 30 38 23 30 34 29 29 34 27
X9E | 11 19 8 8 11 12 17 11 --- 20 4 | 30 35 26 26 29 28 32 31 --- 30 28
10 | 10 11 6 8 13 5 14 7 16 14 3 | 16 25 20 20 26 21 24 22 26 17 20
11E | 9 11 5 9 12 5 11 8 12 13 3 | 26 27 25 18 34 20 30 28 27 24 24
12 | 13 18 7 15 15 5 18 16 17 27 5 | 22 31 19 19 26 16 25 24 25 24 18
13 | 6 17 4 7 17 4 15 9 15 17 4 | 21 29 19 19 37 19 29 19 21 18 20
14 | 6 19 5 11 12 4 15 8 16 23 4 | 24 31 28 26 33 23 23 23 23 25 23
15 | 12 18 7 11 15 6 19 9 18 25 4 | 32 32 31 26 32 24 31 27 29 20 26
16 | 14 23 7 10 13 5 20 11 14 35 5 | 24 26 20 21 25 15 27 19 23 28 18
17 | 9 15 5 13 17 7 20 11 13 13 4 | 27 33 25 21 29 20 31 25 26 16 24
18 | 14 17 7 10 8 5 20 10 16 24 4 | 21 28 26 22 24 20 24 21 22 16 20
19 | 6 20 5 8 15 4 14 9 14 15 4 | 22 26 18 14 31 15 26 18 20 14 17
20 | 6 14 6 10 16 5 19 16 18 15 4 | 29 24 23 24 28 22 25 30 23 21 23
21 | 8 24 7 10 16 5 19 14 13 15 5 | 22 32 20 22 32 18 26 23 19 23 20
22 | 9 18 4 9 10 4 19 11 13 30 4 | 22 29 26 26 27 23 26 25 19 24 22
23 | 7 17 5 9 15 3 18 9 14 21 4 | 20 25 16 15 28 14 25 15 19 15 16
X24E | 101 25 15 32 43 11 21 29 --- --- 12 | 611 613 613 611 619 610 483 608 --- --- 610
25 | 9 12 5 8 12 3 13 9 13 13 3 | 18 27 19 15 24 16 26 17 21 14 17
26 | 11 12 6 9 12 4 15 11 17 7 4 | 25 22 23 17 28 18 19 23 21 17 20
X27 | 6 15 5 11 --- 8 18 13 12 18 4 | 34 36 28 29 --- 28 37 30 30 33 29
28 | 11 20 6 12 13 6 19 10 16 26 4 | 26 34 24 29 29 24 30 29 20 28 24
29 | 12 20 5 12 13 6 17 10 13 14 4 | 22 27 15 18 20 14 21 16 18 16 15
31E | 10 16 5 11 32 6 17 12 14 15 5 | 23 24 17 16 24 15 22 21 20 17 16
32 | 8 10 6 7 15 5 11 7 14 17 3 | 17 14 15 14 17 12 15 13 15 16 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 6 10 15 5 16 11 15 20 |T 42 46 40 39 46 38 40 41 22 20 39
WRMS | 10 16 6 10 14 5 16 9 14 18 |NE 23 27 21 20 26 18 25 21 22 20 20
MEDI | 9 15 6 10 13 5 17 10 14 17 |MD 22 27 21 19 26 19 26 23 22 19 20
Table 3.1753.5 GPS week: 1753 Day: 5 MJD: 56520.000
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 15 7 10 11 7 13 6 14 12 3 | 28 27 21 21 32 20 28 24 27 20 23
2 | 9 15 7 14 17 4 17 18 12 15 5 | 28 28 25 25 32 23 28 25 26 23 24
3 | 6 14 5 8 14 6 11 9 13 19 3 | 28 27 23 18 26 20 27 24 25 25 23
4 | 7 13 5 11 11 5 13 7 11 19 3 | 22 26 18 16 23 19 27 21 21 27 19
5 | 17 18 8 17 8 6 17 13 10 24 5 | 24 29 19 22 26 19 28 20 20 22 20
6 | 8 14 5 6 14 6 12 8 14 19 3 | 23 22 18 16 22 17 22 18 22 18 18
7E | 9 15 6 10 9 4 16 20 13 12 4 | 24 22 20 19 25 18 23 22 26 17 19
8E | 11 19 11 12 15 6 14 17 19 20 5 | 26 39 28 36 28 31 35 32 34 27 29
9E | 10 27 11 12 17 7 15 15 28 19 6 | 33 43 26 25 38 29 39 29 47 28 32
10 | 7 10 5 11 11 4 10 7 12 18 3 | 17 19 15 14 20 16 19 15 12 15 14
11E | 8 22 8 9 11 4 13 8 8 11 4 | 31 39 25 24 35 25 31 31 30 29 28
12 | 9 17 9 11 13 4 18 16 13 27 4 | 27 28 20 20 28 18 30 23 24 26 21
13 | 7 16 5 11 16 6 18 7 11 17 4 | 21 30 17 17 35 19 29 17 24 17 20
14 | 9 19 7 14 11 6 16 6 12 24 4 | 23 24 21 25 29 20 23 20 21 22 20
15 | 9 20 7 15 9 5 19 8 9 25 4 | 29 31 22 23 31 23 32 24 25 22 24
16 | 17 20 8 10 12 5 15 12 11 36 4 | 33 28 27 27 29 24 28 23 28 30 25
17 | 15 15 5 14 15 5 17 14 10 13 4 | 28 25 18 15 30 14 24 21 20 16 19
18 | 11 19 7 11 8 4 19 12 11 28 4 | 25 23 22 22 24 20 27 18 20 14 20
19 | 6 19 8 10 16 4 13 10 14 14 4 | 27 27 20 17 33 18 24 22 25 18 21
20 | 7 12 5 13 12 4 15 11 14 17 4 | 28 32 25 28 32 24 33 28 25 26 27
21 | 9 20 5 12 17 7 16 14 9 16 4 | 26 25 23 28 33 24 30 26 27 29 24
22 | 12 19 4 9 11 4 15 15 10 30 4 | 27 26 22 23 28 23 28 24 25 28 23
23 | 7 16 5 10 13 4 17 9 7 22 3 | 20 26 16 14 26 16 26 16 20 17 17
X24E | 11 18 4 17 11 11 --- 10 16 --- 5 | 433 426 423 425 429 420 --- 426 292 --- 425
25 | 7 11 5 7 12 4 13 13 13 14 3 | 26 24 23 20 26 20 31 19 25 18 22
26 | 6 15 5 16 9 3 11 13 7 11 3 | 21 24 16 25 26 16 21 20 21 16 19
X27 | 10 16 5 10 --- 8 12 11 15 18 4 | 40 38 31 26 --- 30 37 34 37 37 33
28 | 8 18 7 15 13 7 17 13 7 28 4 | 27 29 21 29 33 21 29 25 23 28 23
29 | 8 21 6 12 11 6 19 12 11 14 4 | 24 25 18 22 23 17 26 18 23 21 19
31E | 7 13 5 10 23 5 18 15 14 14 5 | 23 21 16 17 20 17 21 22 27 20 18
32 | 11 11 7 9 16 5 13 9 13 19 4 | 17 19 14 13 16 11 20 13 15 15 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 7 12 13 5 15 12 13 20 |T 39 40 33 34 41 33 27 35 33 22 34
WRMS | 10 17 6 11 13 5 15 10 11 21 |NE 25 26 20 21 27 19 27 21 23 22 21
MEDI | 9 16 6 11 12 5 15 12 12 18 |MD 26 27 21 22 28 20 28 22 25 22 21
Table 3.1753.6 GPS week: 1753 Day: 6 MJD: 56521.000
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 15 6 9 16 5 14 13 10 17 4 | 30 29 28 25 36 25 32 27 32 23 27
2 | 14 14 7 12 20 4 14 23 7 21 5 | 52 52 49 49 57 48 45 55 54 41 50
3 | 8 12 4 11 15 5 12 12 9 18 3 | 24 23 17 17 24 15 26 21 21 22 19
4 | 7 14 6 10 15 6 16 12 9 24 4 | 24 33 23 26 31 24 34 23 29 28 25
5 | 8 17 8 15 14 4 17 10 8 25 4 | 36 37 33 35 39 33 37 35 32 32 33
6 | 7 12 6 8 14 4 12 15 9 20 3 | 20 19 17 11 22 13 22 17 20 18 16
7E | 8 16 5 11 12 4 14 18 11 11 4 | 23 22 18 21 30 18 22 23 25 20 20
8E | 15 15 17 14 14 6 12 20 24 25 6 | 27 33 30 37 23 29 35 36 35 25 27
9E | 11 20 12 12 14 6 16 12 26 18 6 | 39 43 32 31 42 33 43 37 44 29 36
10 | 8 10 4 12 15 3 10 8 6 26 3 | 21 24 21 27 34 22 27 24 25 17 24
11E | 8 22 5 9 14 3 12 9 8 14 4 | 36 44 33 29 43 31 37 34 36 30 34
12 | 10 17 8 13 15 5 17 20 9 27 5 | 20 23 20 22 30 18 24 29 21 27 19
13 | 7 14 5 11 16 4 17 10 11 23 4 | 28 32 26 29 46 25 31 24 28 20 27
14 | 11 18 8 12 12 3 16 14 10 23 4 | 27 26 31 31 39 28 24 30 29 32 27
15 | 9 19 8 22 13 5 21 12 7 25 5 | 31 34 29 36 38 29 36 29 31 26 29
16 | 15 17 6 13 16 3 15 14 9 35 4 | 27 23 22 25 29 18 24 21 21 27 20
17 | 11 14 7 12 15 4 16 10 13 19 4 | 26 26 21 21 31 17 25 23 29 20 22
18 | 11 15 5 12 9 5 15 15 8 23 4 | 20 20 18 22 27 18 22 22 22 16 18
19 | 8 15 6 13 14 3 15 9 10 18 4 | 26 25 21 21 34 18 26 21 24 18 22
20 | 9 14 7 13 13 3 15 14 12 18 4 | 39 38 37 38 43 35 37 37 33 32 36
21 | 11 20 5 11 20 7 15 21 11 19 5 | 20 21 15 14 33 15 21 16 22 21 15
22 | 12 18 5 10 8 4 16 22 9 30 4 | 25 24 23 26 32 21 27 30 24 33 23
23 | 8 17 6 12 13 3 17 11 11 25 4 | 20 26 20 23 35 18 24 18 21 18 20
24E | 15 16 7 18 18 5 12 8 12 --- 5 | 430 420 421 426 423 423 512 424 272 --- 423
25 | 8 12 7 8 12 5 13 13 8 16 3 | 19 22 22 17 27 19 24 17 19 17 19
26 | 8 12 4 8 14 4 10 10 9 13 3 | 21 20 20 21 31 19 22 24 19 20 20
X27 | 6 13 5 11 --- 6 13 15 9 21 4 | 40 42 35 32 --- 35 44 39 41 45 38
28 | 12 17 7 13 14 4 17 11 7 29 4 | 32 33 27 38 39 28 33 35 30 28 30
29 | 11 23 7 9 13 5 19 13 11 14 4 | 18 24 13 17 21 12 24 17 20 20 14
31E | 12 12 6 10 17 5 14 16 12 14 4 | 26 19 19 14 26 15 21 19 24 17 18
32 | 10 10 4 11 16 5 10 11 11 19 3 | 23 20 20 18 26 18 20 18 19 17 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 7 12 15 5 15 14 11 22 |T 40 41 37 38 46 36 44 39 35 24 37
WRMS | 10 16 7 11 14 4 15 13 9 21 |NE 26 27 24 25 33 22 28 26 26 24 24
MEDI | 9 15 6 12 14 4 15 13 9 20 |MD 26 26 22 25 32 21 26 24 25 22 23
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 4.1753 GPS week: 1753 MJD: 56515.0-56521.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2948 |U 7 7 16 |U 5 8 23 | 0 0 0 |
emr | emr 2954 | 8 9 20 |U 9 11 31 | 0 0 0 |
esa | esa 2948 | 7 7 17 |U 7 8 25 | 0 0 0 |
gfz | gfz 2941 |U 7 7 16 |U 8 10 27 |U 0 0 0 |
grg | grg 2864 |U 21 21 56 |U 19 24 59 | 0 0 0 |
igr | igr 2953 | 7 7 17 | 7 8 26 | 0 0 0 |
igs | igs 2933 | 7 7 16 | 7 9 28 | 0 0 0 |
jpl | jpl 2927 | 10 11 24 |U 10 12 33 | 0 0 0 |
mit | mit 2962 | 8 8 18 |U 35 14 78 |U 0 0 0 |
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 5.1753.0 GPS week: 1753 Day: 0 MJD: 56515.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 12 | 5 8 25 | ---- ---- ---- |
emr | emr 2968 | 8 7 18 | 9 14 35 | ---- ---- ---- |
esa | esa 2976 | 6 5 14 | 6 8 27 | ---- ---- ---- |
gfz | gfz 2968 | 6 5 13 | 6 9 24 | ---- ---- ---- |
grg | grg 2880 | 10 8 26 | 13 15 41 | ---- ---- ---- |
igr | igr 2966 | 7 5 15 | 6 10 28 | ---- ---- ---- |
igs | igs 2954 | 6 5 13 | 6 6 26 | ---- ---- ---- |
jpl | jpl 2967 | 12 9 32 | 9 10 35 | ---- ---- ---- |
mit | mit 2976 | 7 7 16 | 192 16 336 | ---- ---- ---- |
Table 5.1753.1 GPS week: 1753 Day: 1 MJD: 56516.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 24 | 5 6 19 | ---- ---- ---- |
emr | emr 2968 | 8 8 27 | 8 10 25 | ---- ---- ---- |
esa | esa 2976 | 7 6 24 | 6 8 18 | ---- ---- ---- |
gfz | gfz 2968 | 7 7 24 | 7 8 16 | ---- ---- ---- |
grg | grg 2880 | 10 16 29 | 14 15 31 | ---- ---- ---- |
igr | igr 2976 | 7 6 24 | 6 7 19 | ---- ---- ---- |
igs | igs 2900 | 7 7 25 | 7 10 20 | ---- ---- ---- |
jpl | jpl 2968 | 8 8 25 | 7 9 21 | ---- ---- ---- |
mit | mit 2976 | 7 8 26 | 7 12 22 | ---- ---- ---- |
Table 5.1753.2 GPS week: 1753 Day: 2 MJD: 56517.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2784 | 8 8 18 | 5 6 22 | ---- ---- ---- |
emr | emr 2871 | 7 10 17 | 8 5 26 | ---- ---- ---- |
esa | esa 2784 | 7 7 18 | 6 4 20 | ---- ---- ---- |
gfz | gfz 2780 | 8 7 18 | 7 6 20 | ---- ---- ---- |
grg | grg 2771 | 11 13 32 | 11 11 32 | ---- ---- ---- |
igr | igr 2841 | 8 8 18 | 5 4 20 | ---- ---- ---- |
igs | igs 2803 | 7 7 17 | 6 4 20 | ---- ---- ---- |
jpl | jpl 2779 | 8 8 17 | 11 11 35 | ---- ---- ---- |
mit | mit 2880 | 9 10 22 | 9 10 33 | ---- ---- ---- |
Table 5.1753.3 GPS week: 1753 Day: 3 MJD: 56518.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 7 12 | 5 6 25 | ---- ---- ---- |
emr | emr 2968 | 8 8 19 | 9 11 32 | ---- ---- ---- |
esa | esa 2976 | 7 8 13 | 5 6 24 | ---- ---- ---- |
gfz | gfz 2969 | 8 8 14 | 5 7 27 | ---- ---- ---- |
grg | grg 2880 | 9 8 21 | 12 16 38 | ---- ---- ---- |
igr | igr 2974 | 7 7 12 | 5 6 27 | ---- ---- ---- |
igs | igs 2966 | 8 8 12 | 7 9 31 | ---- ---- ---- |
jpl | jpl 2968 | 9 8 18 | 9 14 34 | ---- ---- ---- |
mit | mit 2976 | 7 9 14 | 9 13 37 | ---- ---- ---- |
Table 5.1753.4 GPS week: 1753 Day: 4 MJD: 56519.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 17 | 5 11 26 | ---- ---- ---- |
emr | emr 2968 | 9 8 22 | 9 12 33 | ---- ---- ---- |
esa | esa 2976 | 7 6 16 | 5 12 22 | ---- ---- ---- |
gfz | gfz 2968 | 6 6 15 | 5 12 23 | ---- ---- ---- |
grg | grg 2880 | 62 44 144 | 41 43 110 | ---- ---- ---- |
igr | igr 2975 | 7 5 17 | 5 11 22 | ---- ---- ---- |
igs | igs 2962 | 7 6 16 | 5 11 22 | ---- ---- ---- |
jpl | jpl 2968 | 10 19 34 | 13 16 41 | ---- ---- ---- |
mit | mit 2976 | 6 5 15 | 8 18 38 | ---- ---- ---- |
Table 5.1753.5 GPS week: 1753 Day: 5 MJD: 56520.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 15 | 6 8 25 | ---- ---- ---- |
emr | emr 2968 | 9 10 23 | 10 13 32 | ---- ---- ---- |
esa | esa 2976 | 7 8 16 | 16 12 40 | ---- ---- ---- |
gfz | gfz 2967 | 7 8 15 | 17 14 43 | ---- ---- ---- |
grg | grg 2880 | 34 49 118 | 33 59 120 | ---- ---- ---- |
igr | igr 2965 | 7 8 15 | 16 12 42 | ---- ---- ---- |
igs | igs 2975 | 6 8 15 | 14 14 39 | ---- ---- ---- |
jpl | jpl 2872 | 8 10 20 | 14 15 40 | ---- ---- ---- |
mit | mit 2976 | 6 9 14 | 14 14 39 | ---- ---- ---- |
Table 5.1753.6 GPS week: 1753 Day: 6 MJD: 56521.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 10 17 | 6 10 18 | ---- ---- ---- |
emr | emr 2968 | 9 11 16 | 8 12 36 | ---- ---- ---- |
esa | esa 2976 | 9 10 19 | 6 8 23 | ---- ---- ---- |
gfz | gfz 2968 | 8 11 17 | 9 16 33 | ---- ---- ---- |
grg | grg 2880 | 9 11 26 | 7 14 41 | ---- ---- ---- |
igr | igr 2976 | 9 10 18 | 6 8 22 | ---- ---- ---- |
igs | igs 2974 | 8 11 17 | 7 10 36 | ---- ---- ---- |
jpl | jpl 2968 | 15 14 21 | 8 10 28 | ---- ---- ---- |
mit | mit 2976 | 10 11 20 | 7 15 42 | ---- ---- ---- |
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 6.1753 GPS week: 1753 MJD: 56515.500-56521.500
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 -4 25 112 1 | 28 31
| 16 16 71 58 7 | 2
emr uuuuu | -7 -18 -41 -95 -6 | 34 36
| 33 21 86 64 4 | 2
esa uuuuu | 3 -28 33 52 0 | 16 20
| 14 15 27 78 5 | 1
gfz uuuuu | 0 23 26 -100 4 | 11 17
| 35 21 58 117 6 | 2
grg uuuux | 9 8 -56 -19 35 | -2 13
| 28 17 72 47 44 | 3
igr xxxxx | -22 26 35 -15 -1 | 8 15
| 24 17 31 41 4 | 2
irf xxxxx | -3 -4 -57 -57 -2 | 8 14
| 7 5 22 21 2 | 1
jpl uuuuu | -29 19 36 -74 -3 | 45 46
| 20 17 64 103 15 | 2
mit uuuuu | 5 -10 -114 -63 -1 | 28 30
| 19 13 56 50 4 | 2
ngs uuuuu | 25 44 47 48 -4 | 18 20
| 61 34 115 159 6 | 2
sio xxxxx | 67 16 48 -78 11 | 41 42
| 17 73 50 83 17 | 3
Table 7.1753.0 GPS week: 1753 Day: 0 MJD: 56515.500
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 | -29 -15 160 133 3 | 25 29
emr uuuuu | -46 -26 -37 -86 -10 | 36 38
esa uuuuu | -10 -43 33 -9 0 | 16 20
gfz uuuuu | 6 -9 4 52 2 | 9 17
grg uuuux | 8 15 -154 8 3 | -2 12
igr xxxxx | -7 37 -17 -48 4 | 6 16
irf xxxxx | -7 -11 -44 -69 -5 | 8 15
jpl uuuuu | -55 27 -46 -50 9 | 42 45
mit uuuuu | 29 2 -111 -134 0 | 25 29
ngs uuuuu | 66 79 -9 11 -4 | 17 21
sio xxxxx | 61 53 51 -146 4 | 36 39
Table 7.1753.1 GPS week: 1753 Day: 1 MJD: 56516.500
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 | -4 -14 25 34 -6 | 26 30
emr uuuuu | -23 -41 -6 -57 -3 | 34 37
esa uuuuu | -6 -22 61 176 0 | 15 20
gfz uuuuu | 45 18 90 -3 7 | 9 17
grg uuuux | -23 7 18 12 -1 | -3 11
igr xxxxx | -4 22 32 -9 4 | 6 16
irf xxxxx | 1 -7 -86 -24 -3 | 7 15
jpl uuuuu | -34 17 31 -36 3 | 43 45
mit uuuuu | 5 -26 -181 -58 1 | 25 29
ngs uuuuu | 31 83 -58 -229 -8 | 18 22
sio xxxxx | 65 79 8 -92 7 | 37 40
Table 7.1753.2 GPS week: 1753 Day: 2 MJD: 56517.500
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 2 31 73 10 | 29 31
emr uuuuu | -11 10 -77 -100 -8 | 36 38
esa uuuuu | 23 -23 76 -11 -3 | 18 20
gfz uuuuu | 27 12 51 17 -3 | 13 17
grg uuuux | 12 39 -138 9 17 | -3 11
igr xxxxx | 12 21 63 -32 -4 | 9 15
irf xxxxx | 2 -2 -48 -54 0 | 9 13
jpl uuuuu | -12 11 44 41 17 | 46 48
mit uuuuu | 5 -3 -109 -74 4 | 28 30
ngs uuuuu | -64 -2 9 44 0 | 19 22
sio xxxxx | 77 49 94 -72 10 | 41 42
Table 7.1753.3 GPS week: 1753 Day: 3 MJD: 56518.500
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 -2 8 151 5 | 30 31
emr uuuuu | -21 1 -109 -99 -2 | 36 38
esa uuuuu | 23 -10 32 107 4 | 17 20
gfz uuuuu | 4 22 56 -188 -1 | 12 17
grg uuuux | 27 -5 8 -22 25 | -4 9
igr xxxxx | -29 44 70 25 -1 | 9 15
irf xxxxx | -11 -8 -84 -75 -2 | 9 13
jpl uuuuu | -52 42 94 -230 -7 | 48 49
mit uuuuu | 0 -31 -173 -69 2 | 29 30
ngs uuuuu | -23 9 49 75 -5 | 20 22
sio xxxxx | 54 3 15 -30 10 | 42 43
Table 7.1753.4 GPS week: 1753 Day: 4 MJD: 56519.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 10 5 35 156 -10 | 30 31
emr uuuuu | 49 -3 -138 6 -1 | 33 35
esa uuuuu | 1 -18 16 106 -8 | 16 19
gfz uuuuu | -62 19 58 -192 14 | 10 16
grg uuuux | -30 16 -54 -114 34 | -4 10
igr xxxxx | -55 14 55 -55 -5 | 9 15
irf xxxxx | -12 5 -56 -60 1 | 8 13
jpl uuuuu | -12 -13 120 -31 -24 | 47 48
mit uuuuu | -31 -2 -140 -96 2 | 28 30
ngs uuuuu | 128 25 84 -20 -5 | 17 20
sio xxxxx | 88 67 113 -134 13 | 42 43
Table 7.1753.5 GPS week: 1753 Day: 5 MJD: 56520.500
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 23 -10 186 1 | 28 30
emr uuuuu | -21 -22 -48 -203 -9 | 31 33
esa uuuuu | 0 -55 0 23 6 | 15 18
gfz uuuuu | -28 52 -85 -230 10 | 11 16
grg uuuux | 15 -10 -84 -40 40 | -3 12
igr xxxxx | -25 0 21 -41 1 | 8 14
irf xxxxx | 0 -5 -56 -82 -3 | 7 12
jpl uuuuu | -4 27 -48 -207 -19 | 42 44
mit uuuuu | 14 -11 -38 -31 -6 | 27 29
ngs uuuuu | 25 60 285 278 -10 | 15 18
sio xxxxx | 40 -7 -24 -153 -13 | 43 44
Table 7.1753.6 GPS week: 1753 Day: 6 MJD: 56521.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -37 -26 -78 51 4 | 31 33
emr uuuuu | 28 -47 126 -124 -10 | 33 35
esa uuuuu | -7 -25 14 -29 -2 | 19 23
gfz uuuuu | 6 49 4 -156 0 | 16 21
grg uuuux | 52 -8 10 15 128 | 4 22
igr xxxxx | -48 44 19 53 -5 | 11 17
irf xxxxx | 6 -1 -25 -36 -4 | 9 15
jpl uuuuu | -34 19 54 -6 -5 | 44 46
mit uuuuu | 12 -3 -48 23 -7 | 30 32
ngs uuuuu | 15 53 -34 175 7 | 17 19
sio xxxxx | 85 -133 79 82 44 | 45 45
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