[IGSREPORT-21527] Wk 1722 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jan 25 10:02:02 PST 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1722 (Jan 06, 2013 - Jan 12, 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:
igs1722[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1722[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1722[0-6].cls IGS GPS clock combination summary report.
igs17227.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17227.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 | 3 6 26 3 6 26
0 | ESA | 3 6 26 3 6 26
0 | GFZ | LHAZ
0 | JPL | 6
1 | COD | 3 6 26 6 26 KOUC FLRS KOUC XMIS
1 | ESA | 3 6 26 6 26 MATE MATE
1 | GFZ | 3 6 26 BOGT SFER UNSA
1 | GRG | YELL WIND YELL
1 | JPL | 6
1 | MIT | 3 6 30 3 6 30
2 | COD | 3 6 26 3 6 26 XMIS FLRS HOB2 REUN XMIS
2 | ESA | 3 6 26 3 6 26 UNSA
2 | GFZ | 3 6 26 ALGO BOGT DUBO HOB2
2 | GRG | ONSA MCM4 ONSA
2 | JPL | 26 ISPA NYAL
2 | MIT | REUN
3 | COD | 6 26 3 6 26 KOUC AREQ KOUC REUN SOFI
3 | EMR | AREQ
3 | ESA | 3 6 26 3 6 26 AREQ
3 | GFZ | 3 6 26 ALRT BOGT POLV
3 | GRG | NICO USNO BOGT CEDU KARR KIT3 LHAZ MCM4 NICO SOFI
3 | GRG | USNO
3 | JPL | AREQ
3 | MIT | 3 3 ALRT WROC ALRT NICO WROC
4 | COD | 6 6 AREQ
4 | EMR | 3 3 AREQ
4 | ESA | 6 6 AREQ UNSA
4 | GFZ | 3 6 26 ASPA BOGT HOLM NKLG POLV TIDB WES2
4 | GRG | 3 3 NKLG NKLG
4 | JPL | 3 AREQ
4 | MIT | 3 3 SYDN
5 | COD | KOUC KOUC
5 | ESA | UNSA
5 | GFZ | 3 6 BOGT POLV SYOG TIDB
5 | GRG | 3 6 3 6 AREQ MDVJ SOFI ADIS AREQ MDVJ SOFI WTZR
5 | JPL | 6 NYAL
5 | MIT | 3 6 15 3 6 15 SYDN MANA SYDN
6 | COD | 2 3 10 2 3 10 KOUC XMIS KOUC XMIS
6 | EMR | 4 6 4 6 HERS
6 | ESA | 4 4 UNSA
6 | GFZ | 6 BOGT GUAM IRKT SSIA
6 | GRG | 3 6 3 6 DARW SOFI USNO DARW HOB2 SOFI USNO
6 | JPL | 3 6 GMAS
6 | MIT | 3 6 9 3 6 9 DARW DARW
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following 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
----+------------+----------
G05 | 2013_01_10 | 2013003
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G26 | | | | | 1 | 1 | |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.2 .2 -.8 -44 0 -4 .05
EMR | 0 | -.2 11.3 7.4 2 11 -1 .11
ESA | 0 | -2.7 7.1 .6 117 -60 51 .15
GFZ | 0 | .1 .0 -.3 -50 -32 -21 .01
GRG | 0 | 6.0 -1.6 6.2 -1 33 -14 .14
JPL | 0 | 4.7 -1.9 11.5 -70 -7 -51 .02
MIT | 0 | 1.9 7.5 5.3 -11 7 -41 .05
NGS | 0 | -1.0 -3.5 -7.6 35 -6 1 .74
SIO | 0 | 5.2 5.3 -48.9 242 -329 73 .40
COD | 1 | -1.2 -.1 -1.3 -49 18 -6 .05
EMR | 1 | 2.9 9.7 12.1 2 9 -8 .05
ESA | 1 | -1.0 7.9 -2.9 126 -147 80 .19
GFZ | 1 | .0 -.6 -.6 -52 -21 -17 .06
GRG | 1 | 6.7 5.4 -.6 -14 32 -11 .44
JPL | 1 | -1.1 9.4 8.5 -78 -8 -77 -.23
MIT | 1 | 4.3 4.8 6.9 -11 8 -31 .13
NGS | 1 | -2.3 .2 -7.6 48 2 -17 .66
SIO | 1 | 8.0 6.2 -51.6 245 -291 110 .23
COD | 2 | -1.0 .6 -1.6 -54 15 -13 -.06
EMR | 2 | 3.6 13.4 2.8 14 1 4 .06
ESA | 2 | 1.1 6.9 -3.3 110 -165 88 .14
GFZ | 2 | .5 .3 -.4 -50 -25 -25 -.02
GRG | 2 | 12.8 2.3 11.7 -32 27 -43 .54
JPL | 2 | .8 11.5 13.1 -113 58 -10 -.15
MIT | 2 | 8.1 6.2 6.4 -5 -7 -38 .30
NGS | 2 | 3.4 -1.8 -15.8 76 -28 34 .56
SIO | 2 | 13.7 9.3 -47.7 125 -373 21 .35
COD | 3 | -1.0 .3 -1.5 -48 20 -10 -.14
EMR | 3 | 2.8 6.3 8.4 7 9 9 .09
ESA | 3 | 3.6 2.8 -4.0 51 -210 114 .14
GFZ | 3 | .5 .5 -.6 -63 -28 -26 .04
GRG | 3 | 4.5 1.9 5.6 -45 29 -26 .37
JPL | 3 | 3.6 -1.4 14.6 -43 -10 -20 .12
MIT | 3 | 4.3 5.4 5.9 -8 1 -34 .12
NGS | 3 | 4.2 -4.2 -9.4 50 -32 47 .48
SIO | 3 | 6.5 1.4 -43.4 138 -277 -32 .21
COD | 4 | -.6 .9 -.8 -46 10 3 -.08
EMR | 4 | -.8 5.2 3.9 5 2 -3 .25
ESA | 4 | 2.1 5.6 -6.2 89 -175 84 .04
GFZ | 4 | .4 .3 -.8 -61 -29 -33 .0
GRG | 4 | 9.3 3.2 5.2 -49 71 -51 .17
JPL | 4 | -2.6 -1.8 10.3 -72 33 -46 .14
MIT | 4 | 4.8 5.0 4.1 -8 3 -34 .21
NGS | 4 | -.9 -6.4 -5.3 5 -1 -3 .70
SIO | 4 | 4.5 3.7 -29.7 189 -200 23 .33
COD | 5 | -.8 .1 -1.3 -52 5 -7 -.18
EMR | 5 | -.3 4.5 13.6 4 23 1 .02
ESA | 5 | 1.1 .0 -3.1 7 -146 102 .08
GFZ | 5 | .3 -.3 -1.0 -62 -40 -25 .10
GRG | 5 | .6 -7.0 -.6 -55 58 -34 .46
JPL | 5 | 3.5 -1.2 18.4 -73 50 -11 .03
MIT | 5 | 2.3 3.9 2.9 -14 1 -34 .19
NGS | 5 | -4.6 -9.9 -1.0 -39 21 -39 .83
SIO | 5 | .9 4.0 -45.1 170 -225 -134 .51
COD | 6 | -.6 -.1 -.7 -48 -5 -8 -.29
EMR | 6 | 5.3 10.2 16.3 -3 12 8 -.19
ESA | 6 | 3.4 2.1 -3.9 57 -192 110 .04
GFZ | 6 | -.1 .0 -.8 -57 -39 -17 -.11
GRG | 6 | 2.5 -8.9 -1.1 -38 37 -7 .21
JPL | 6 | 1.8 1.4 22.6 -33 10 -25 -.10
MIT | 6 | 4.2 4.1 6.9 -10 7 -23 .08
NGS | 6 | 4.1 -5.2 6.7 -49 -23 39 .41
SIO | 6 | 5.6 2.3 -38.6 122 -271 94 .30
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
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 1.1722.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1722.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 2.1722.[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 3.1722.[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 5.1722.0-6). 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 1722 summary. (Jan 06, 2013 - Jan 12, 2013)
Table 1.1722.a GPS week: 1722 MJD: 56298.000-56304.000
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 263| 0 0 5 -17 9 5 -.45 11 11 | -1349 558 19 87
| 0 0 1 20 24 24 .05 | 886 1232
emr 80| 0 0 6 -49 26 -5 .16 15 15 | 3096 -213 15 94
| 0 2 1 22 14 13 .02 | 627 567
esa 174| 0 0 0 75 -63 4 .05 6 5 | -20 26 12 110
| 0 0 0 21 22 18 .01 | 1028 1207
gfz 190| -1 -1 -5 -69 -45 14 -.37 11 10 | -142743 -9298 21 121
| 0 1 1 27 22 11 .01 | 378014 23996
grg 139| 1 0 -2 -12 42 -2 .62 15 14 | -272 248 20 140
| 0 1 4 11 14 13 .04 | 323 477
igr n/a| 0 0 -1 -19 91 -26 -.17 4 4 | 8442 -690 17 88
| 0 0 1 28 17 10 .02 | 1210 512
jpl 80| -1 -1 3 -6 40 -15 .27 14 13 | 3640 -333 16 108
| 1 1 0 32 16 15 .03 | 509 444
mit 240| 0 0 -1 -10 20 5 -.18 6 6 | -408 506 24 175
| 0 0 1 9 18 10 .02 | 274 398
ngs 245| 0 0 -1 -26 61 -23 .36 10 9 | -1183 297 1859 3655
| 0 0 2 29 39 17 .03 | 790 1079
sio 256| -1 -2 4 158 -191 30 -.44 21 18 | --- --- --- ---
| 1 0 1 48 58 88 .04 | --- ---
Table 1.1722.b GPS week : 1722 MJD: 56298.000-56304.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 3 3 4 3 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 5 4 4 6 5 6 7 |
4 | 3 3 3 3 3 4 3 |
5 | 4 4 4 4 0 4 4 |
6 | 4 4 4 5 5 7 6 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 3 3 3 4 3 |
10 | 4 3 3 3 3 4 3 |
11 | 4 4 4 4 4 4 4 |
12 | 5 4 5 5 5 5 4 |
13 | 3 3 3 3 3 4 4 |
14 | 3 4 3 3 4 3 3 |
15 | 5 5 4 5 5 4 5 |
16 | 4 4 4 4 4 4 4 |
17 | 4 4 4 5 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 5 4 4 4 |
20 | 3 3 3 3 3 3 4 |
21 | 3 4 3 3 3 4 4 |
22 | 3 3 3 3 3 3 3 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 5 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 5 5 6 5 4 |
27 | 0 0 0 0 0 0 0 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 4 5 5 5 5 |
30 | 3 3 3 3 3 4 4 |
31 | 4 4 4 4 4 4 4 |
32 | 3 2 3 3 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
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1722.0 GPS week: 1722 Day: 0 MJD: 56298.000
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 6 -20 -1 17 -.40 11 11 | -1236 7 19 86
emr 80| 0 -1 5 -71 20 4 .17 15 15 | 3477 52 13 110
esa 174| 1 0 0 96 -16 8 .06 6 5 | 471 -608 11 112
gfz 185| 0 -1 -6 -69 -65 13 -.36 9 9 | -999999 -63704 26 108
grg 139| 2 0 0 4 22 8 .60 16 14 | -366 328 18 111
igr n/a| 0 0 0 -51 63 -14 -.18 4 4 | 9977 -361 17 89
jpl 80| -2 0 1 -33 21 -10 .29 14 13 | 4337 -259 15 112
mit 240| 0 0 0 -12 -4 7 -.20 7 7 | -437 361 25 194
ngs 241| 0 0 -3 -25 73 -32 .30 10 8 | -1153 -162 2213 3900
sio 280| -2 -3 4 229 -245 68 -.41 21 17 | --- --- --- ---
Table 2.1722.1 GPS week: 1722 Day: 1 MJD: 56299.000
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| -1 0 5 0 -5 3 -.37 11 11 | -2034 1878 20 87
emr 80| 0 0 6 -46 20 -10 .16 15 15 | 3169 -160 14 85
esa 174| 0 1 -1 72 -63 -17 .05 6 6 | -535 1343 13 110
gfz 187| -1 0 -3 -46 -35 16 -.34 9 8 | 182 -61 21 135
grg 138| 2 1 -7 -12 27 -7 .57 15 14 | -199 409 21 176
igr n/a| 0 0 1 -47 75 -33 -.18 4 4 | 9354 -743 17 90
jpl 80| -1 -3 2 -34 34 -4 .29 13 13 | 3749 -369 17 114
mit 240| 1 0 0 -25 31 9 -.19 6 6 | -480 577 28 191
ngs 243| 0 0 -2 3 63 0 .35 10 8 | -1802 1494 1948 3821
sio 247| -3 -1 5 211 -194 119 -.42 20 18 | --- --- --- ---
Table 2.1722.2 GPS week: 1722 Day: 2 MJD: 56300.000
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 266| -1 0 7 -44 0 37 -.42 10 10 | -1615 958 21 84
emr 80| 1 -1 4 -84 18 0 .15 15 15 | 3349 311 16 94
esa 174| 2 1 0 97 -65 -21 .06 5 5 | 1212 -768 15 97
gfz 190| -1 -1 -8 -34 -4 27 -.37 9 9 | 90 441 19 113
grg 141| 1 0 3 -25 54 -25 .68 14 13 | -381 468 26 130
igr n/a| 0 0 0 -34 97 -17 -.17 5 5 | 8891 -318 16 78
jpl 80| -2 -3 2 -50 61 7 .27 14 13 | 3700 -28 18 90
mit 240| 0 0 0 -6 32 14 -.20 6 6 | -455 611 22 166
ngs 243| 0 0 -4 -29 3 -43 .36 10 9 | -1412 685 1639 3528
sio 210| -3 -1 4 106 -278 45 -.40 20 18 | --- --- --- ---
Table 2.1722.3 GPS week: 1722 Day: 3 MJD: 56301.000
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| 0 0 5 12 10 21 -.48 11 11 | -1697 958 22 80
emr 80| 0 0 6 -27 32 -23 .12 16 16 | 3613 -282 13 72
esa 174| 0 0 0 56 -75 7 .05 5 5 | 369 -1248 13 109
gfz 193| -1 -3 -5 -96 -44 6 -.38 11 10 | 330 -411 22 126
grg 139| 0 1 1 -5 44 -8 .64 14 11 | -124 -161 17 139
igr n/a| 0 0 -2 0 97 -40 -.18 5 4 | 8535 -504 17 90
jpl 80| 0 0 4 33 39 -18 .26 14 13 | 3566 -43 17 99
mit 240| 0 0 -2 0 49 6 -.20 6 6 | -249 381 20 180
ngs 246| 0 1 -5 -80 23 -26 .36 11 9 | -1497 561 2119 3940
sio 263| -2 -1 3 122 -186 -35 -.43 19 19 | --- --- --- ---
Table 2.1722.4 GPS week: 1722 Day: 4 MJD: 56302.000
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| 0 1 5 -38 42 12 -.47 10 10 | 589 -1949 21 93
emr 80| 0 -2 4 -36 18 15 .15 15 15 | 3607 -1401 18 95
esa 174| 0 0 0 98 -89 4 .06 6 6 | -2033 2044 13 116
gfz 192| -2 -2 -4 -101 -60 14 -.36 13 11 | 557 -810 20 114
grg 140| 0 0 -3 -18 59 -1 .62 15 15 | 342 -569 22 136
igr n/a| 0 0 -1 -7 96 -15 -.16 4 4 | 8573 -1593 17 97
jpl 80| 0 -1 3 -1 48 -42 .23 15 14 | 4012 -1072 16 117
mit 240| 0 0 -1 -15 14 0 -.16 6 5 | 116 -230 22 153
ngs 248| 0 1 0 -26 69 -13 .41 10 9 | 552 -1896 1717 3505
sio 264| 0 -1 2 165 -120 30 -.43 22 18 | --- --- --- ---
Table 2.1722.5 GPS week: 1722 Day: 5 MJD: 56303.000
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| 1 2 2 -5 -21 -32 -.48 11 11 | -1718 925 17 89
emr 80| 0 0 7 -25 20 -4 .17 16 16 | 2479 194 16 101
esa 174| 0 0 1 60 -62 27 .07 6 6 | 306 -507 13 133
gfz 193| -2 0 -6 -92 -67 29 -.37 10 10 | 196 -937 19 119
grg 140| 2 -2 -4 -4 35 2 .61 15 14 | -616 912 20 146
igr n/a| 0 0 -2 29 90 -30 -.14 4 4 | 7390 -169 17 84
jpl 80| -2 -1 3 20 18 -15 .22 14 14 | 3407 194 16 117
mit 240| 0 0 -1 -12 13 -15 -.15 6 5 | -690 996 25 179
ngs 248| 1 0 1 8 127 -7 .37 10 8 | -1580 713 1848 3499
sio 264| 0 -2 4 165 -123 -129 -.51 20 17 | --- --- --- ---
Table 2.1722.6 GPS week: 1722 Day: 6 MJD: 56304.000
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 266| 0 0 2 -25 41 -19 -.51 11 10 | -1733 1131 18 93
emr 80| 0 4 9 -53 56 -19 .17 16 16 | 1982 -205 17 106
esa 174| 1 0 0 47 -73 23 .03 5 5 | 65 -70 11 93
gfz 196| -1 -3 -4 -43 -37 -5 -.37 14 13 | -557 391 22 137
grg 140| 1 -3 -5 -25 53 16 .61 16 15 | -561 349 22 145
igr n/a| 0 0 -3 -28 119 -30 -.15 4 4 | 6377 -1144 20 92
jpl 80| 1 1 3 18 57 -25 .31 15 14 | 2713 -754 16 110
mit 240| 0 0 -2 3 5 16 -.17 6 5 | -661 852 28 166
ngs 248| 0 0 2 -33 65 -44 .38 12 9 | -1394 684 1530 3397
sio 264| 0 -3 2 111 -193 116 -.49 22 19 | --- --- --- ---
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 3.1722.0 GPS week: 1722 Day: 0 MJD: 56298.000
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 12 5 9 10 4 15 8 9 17 3 | 47 54 58 58 61 55 60 57 57 52 56
2 | 8 15 6 15 12 3 14 4 7 32 3 | 21 23 21 25 23 19 22 20 21 32 20
3E | 11 18 8 16 20 5 16 9 8 30 4 | 43 38 38 47 26 41 36 40 37 43 37
4 | 8 9 4 9 16 3 12 5 9 16 3 | 40 42 44 49 48 41 44 43 41 42 43
5 | 13 16 5 8 13 4 14 5 11 18 3 | 18 21 12 9 17 15 19 11 16 15 14
6E | 12 14 7 11 16 3 17 7 10 42 4 | 72 65 66 75 56 68 62 67 64 64 66
7 | 12 14 5 9 21 3 13 8 10 18 4 | 16 24 21 13 34 16 22 16 25 19 17
8 | 9 8 5 6 14 4 10 5 12 12 3 | 18 23 18 15 22 17 22 19 20 15 17
9 | 8 10 5 8 17 4 9 6 11 24 3 | 30 34 31 30 32 28 34 27 35 26 30
10 | 16 8 5 10 12 5 9 6 7 21 3 | 25 23 23 29 30 23 26 26 22 23 24
11 | 9 15 7 7 16 6 11 10 11 19 4 | 27 41 39 38 49 34 41 34 37 33 35
12 | 10 17 5 11 19 3 20 10 11 18 4 | 19 30 23 24 34 20 32 21 26 16 22
13E | 9 11 5 10 13 3 11 5 10 13 3 | 35 40 36 37 40 35 39 36 38 36 36
14E | 8 9 4 5 11 2 9 5 6 17 2 | 34 37 34 32 35 33 35 34 35 37 33
15 | 20 21 5 9 18 5 18 8 12 15 5 | 25 35 25 19 30 21 29 19 26 25 22
16 | 9 15 6 11 16 4 18 6 10 22 4 | 22 30 25 19 27 22 32 22 26 30 22
17E | 9 16 5 8 15 3 15 6 13 14 4 | 24 31 26 28 30 25 29 26 30 30 26
18 | 8 13 5 15 14 3 12 6 8 27 3 | 24 33 30 33 29 29 31 29 31 32 28
19 | 14 17 9 8 20 3 13 8 8 16 4 | 26 31 23 27 35 26 30 26 30 28 25
20 | 9 9 5 9 9 3 11 9 11 32 3 | 31 39 35 31 38 33 39 34 35 35 34
21 | 6 13 6 5 8 4 14 8 10 23 3 | 23 26 25 24 28 23 27 22 26 25 22
22 | 6 13 4 7 12 5 13 5 9 21 3 | 21 28 26 25 30 24 29 24 27 32 24
23E | 10 19 5 11 12 5 16 9 12 21 4 | 68 66 70 66 69 66 67 63 69 55 66
24 | 14 20 4 7 16 5 13 8 9 17 4 | 31 26 28 31 35 29 35 29 34 19 29
25 | 9 18 4 6 17 2 14 5 8 15 3 | 21 27 24 24 28 22 32 22 25 18 22
26E | 14 17 6 10 16 5 15 10 10 20 4 | 52 50 45 53 49 48 53 49 45 46 48
X27 | 7 --- --- --- --- 70 --- --- --- --- 0 | 44 --- --- --- --- 31 --- --- --- --- 46
28 | 10 16 7 10 22 4 16 7 9 17 4 | 27 33 25 20 31 24 31 26 26 25 24
29E | 14 19 6 7 19 3 19 7 12 18 4 | 28 30 30 28 30 26 28 27 36 27 27
30 | 10 10 6 9 14 5 11 6 7 20 3 | 13 18 13 12 15 12 20 13 15 21 11
31 | 9 14 6 9 19 4 15 7 8 14 3 | 16 23 18 14 36 16 23 15 20 15 15
32 | 6 8 5 6 10 3 8 6 10 24 2 | 13 22 20 20 28 17 23 17 22 23 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 9 16 4 14 7 10 21 |T 29 33 30 30 34 29 33 29 32 30 30
WRMS | 11 15 5 9 14 4 13 7 8 17 |NE 25 29 26 25 32 24 30 24 27 25 26
MEDI | 9 14 5 9 16 4 14 7 10 18 |MD 25 31 26 28 31 25 31 26 30 28 25
Table 3.1722.1 GPS week: 1722 Day: 1 MJD: 56299.000
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 10 5 5 12 3 13 7 9 15 3 | 39 39 41 39 46 39 43 39 37 38 39
2 | 11 14 7 14 11 3 15 4 9 33 3 | 20 17 17 20 18 13 18 14 15 26 15
3E | 12 17 5 9 14 5 14 8 9 25 4 | 41 35 35 42 33 38 35 37 33 35 35
4 | 9 9 4 7 11 3 10 3 9 15 2 | 29 29 32 30 34 29 32 28 30 32 30
5 | 15 16 6 8 13 5 16 6 10 17 4 | 13 19 11 11 14 12 19 9 13 13 12
6E | 14 16 5 13 15 6 16 7 8 35 4 | 68 64 66 72 59 67 61 65 61 60 65
7 | 10 18 5 8 20 4 12 5 9 15 3 | 18 25 18 13 34 15 21 16 23 16 16
8 | 8 10 6 6 12 4 10 4 9 15 3 | 19 24 17 17 22 17 22 18 18 19 18
9 | 9 11 6 7 11 4 10 5 13 15 3 | 24 28 23 24 26 22 26 23 31 26 24
10 | 9 8 4 7 11 4 9 3 6 22 2 | 17 19 17 16 24 17 19 14 18 20 16
11 | 8 15 7 11 19 5 10 7 12 16 4 | 26 34 29 27 42 26 32 27 25 27 27
12 | 11 17 6 11 19 3 16 7 11 18 4 | 17 27 22 23 33 20 26 19 29 14 20
13E | 9 10 4 8 13 3 9 5 9 12 3 | 27 25 24 22 30 22 27 23 22 26 23
14E | 10 12 5 8 12 2 10 7 13 17 3 | 18 24 21 23 22 17 19 18 24 27 19
15 | 22 21 7 9 15 5 18 7 10 15 5 | 22 30 20 18 28 16 28 17 25 19 19
16 | 11 15 5 9 16 6 15 6 11 19 3 | 19 27 20 17 26 20 26 19 26 24 19
17E | 11 18 6 8 12 4 20 6 10 13 4 | 36 36 33 33 39 33 35 33 39 34 33
18 | 15 13 6 15 13 3 15 8 10 27 4 | 23 26 20 27 23 19 23 19 23 20 20
19E | 14 18 7 10 17 7 12 9 9 15 4 | 19 28 31 25 29 25 27 26 28 29 25
20 | 8 9 7 8 9 3 11 5 8 33 3 | 21 26 24 20 27 19 29 20 24 27 22
21 | 12 14 6 9 11 3 14 4 8 23 3 | 15 19 18 17 22 14 22 12 19 20 14
22 | 9 12 4 7 11 4 12 7 13 20 3 | 15 21 19 17 24 15 22 14 19 21 16
23 | 9 22 6 8 14 6 14 7 9 19 4 | 47 49 48 46 51 43 49 43 48 47 46
24 | 9 21 6 9 16 5 12 6 8 16 3 | 22 25 23 24 32 21 26 22 31 19 22
25 | 12 15 5 10 19 3 13 5 9 18 3 | 22 24 25 27 33 22 32 23 32 16 24
26E | 15 18 5 10 15 6 18 9 7 22 4 | 46 44 45 46 42 43 42 43 38 43 42
X27 | 6 --- --- --- --- 73 --- --- --- --- 0 | 53 --- --- --- --- 41 --- --- --- --- 54
28 | 11 13 4 10 20 3 13 4 9 15 3 | 24 27 21 19 31 19 24 19 23 21 20
29E | 11 18 9 10 19 4 17 9 15 22 4 | 27 33 29 30 33 27 31 28 37 30 28
30 | 10 9 8 7 11 7 10 6 11 16 3 | 14 20 16 16 18 15 20 16 21 18 15
31 | 6 13 5 9 21 4 13 6 7 15 3 | 12 21 15 12 38 12 20 13 20 14 14
32 | 7 8 4 5 10 3 8 3 7 22 2 | 12 17 15 12 21 10 19 11 15 22 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 9 15 4 13 6 10 20 |T 25 28 25 25 30 24 28 23 27 25 25
WRMS | 11 15 6 8 14 4 13 6 8 18 |NE 22 25 21 20 28 20 25 19 24 21 21
MEDI | 10 14 6 9 13 4 13 6 9 17 |MD 22 26 22 23 30 20 26 19 25 24 20
Table 3.1722.2 GPS week: 1722 Day: 2 MJD: 56300.000
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 | 16 13 4 5 8 4 14 6 8 14 3 | 32 41 42 47 41 42 43 43 41 39 41
2 | 12 15 6 13 12 4 15 6 10 31 4 | 20 22 16 20 16 16 21 17 19 26 16
3E | 11 18 6 14 14 5 16 8 11 25 4 | 39 35 38 41 26 37 36 37 37 32 35
4 | 10 9 4 9 12 3 10 4 10 17 3 | 32 39 36 41 39 39 41 37 37 40 37
5 | 16 15 6 9 13 3 14 5 7 15 3 | 19 20 12 13 11 13 20 12 17 15 14
6E | 12 14 5 15 15 5 18 7 10 32 4 | 63 58 59 66 47 60 56 60 58 50 58
7 | 9 20 4 10 14 7 12 6 12 21 3 | 20 30 22 14 35 18 25 23 30 14 21
8 | 11 10 6 8 13 5 12 5 9 11 3 | 21 28 18 16 25 17 29 19 24 18 20
9 | 11 9 3 7 13 3 11 3 12 14 3 | 17 22 17 16 23 14 22 16 20 18 16
10 | 7 8 5 8 12 2 9 5 10 18 2 | 18 24 20 25 25 22 24 21 25 23 21
11 | 8 17 4 8 17 4 11 6 12 16 3 | 21 32 27 31 39 27 31 27 30 26 27
12 | 12 18 5 13 19 5 19 10 9 19 4 | 21 30 20 22 31 19 31 19 27 15 21
13E | 8 12 3 9 11 3 8 5 12 14 3 | 32 36 29 27 36 28 31 30 32 27 29
14E | 6 10 5 7 10 4 8 4 14 14 3 | 36 39 39 37 44 37 40 39 35 39 38
15 | 17 21 5 8 19 6 15 6 9 16 4 | 20 30 18 15 28 16 24 15 22 21 17
16 | 9 16 4 9 11 8 18 6 10 21 3 | 19 27 22 18 25 20 27 21 27 25 20
17E | 7 21 5 7 16 4 21 7 13 16 4 | 21 31 24 23 31 23 33 24 32 26 25
18 | 7 13 5 11 14 4 13 5 10 28 3 | 24 29 25 25 25 24 28 23 29 23 24
19E | 8 20 7 12 17 5 14 5 9 15 4 | 24 27 26 28 34 23 25 22 26 25 23
20 | 9 10 4 9 7 4 11 5 6 33 2 | 23 29 26 23 29 23 33 25 29 29 25
21 | 7 12 4 8 7 4 14 5 8 25 2 | 17 23 24 23 24 20 24 18 24 19 19
22 | 4 11 4 6 10 4 12 6 10 18 2 | 19 26 21 18 24 20 24 18 19 25 18
23 | 7 18 5 8 16 6 13 5 10 20 3 | 21 30 26 25 34 23 28 22 31 23 24
24 | 12 22 5 9 15 4 15 4 7 15 3 | 21 24 21 23 28 21 26 21 28 17 20
25 | 13 16 6 8 16 6 14 4 8 16 3 | 25 27 27 23 28 24 33 24 30 18 25
26E | 14 19 9 14 18 5 22 10 8 20 5 | 58 58 56 58 55 56 56 54 55 60 54
X27 | 8 --- --- --- --- 121 --- --- --- --- 0 | 91 --- --- --- --- 55 --- --- --- --- 91
28 | 10 14 5 10 18 3 12 4 11 15 3 | 22 30 20 20 33 21 28 21 29 24 23
29E | 11 18 6 6 14 2 16 6 12 19 4 | 28 30 27 25 30 25 30 27 37 22 27
30 | 7 9 4 7 11 5 10 5 10 17 2 | 16 20 16 14 18 14 20 15 23 23 16
31 | 11 13 4 8 18 5 12 5 11 17 3 | 19 22 18 15 38 15 21 18 28 26 19
32 | 9 9 4 6 11 4 9 3 7 24 2 | 11 20 17 17 21 12 20 13 19 22 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 5 9 14 5 14 6 10 20 |T 27 30 26 26 30 25 30 25 29 26 27
WRMS | 10 15 5 9 13 5 13 6 9 18 |NE 24 27 21 21 28 22 27 21 26 23 25
MEDI | 9 14 5 8 14 4 13 5 10 17 |MD 21 29 24 23 29 22 28 22 29 24 23
Table 3.1722.3 GPS week: 1722 Day: 3 MJD: 56301.000
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 | 12 14 5 10 8 4 15 6 8 11 3 | 36 46 49 46 47 48 50 49 44 45 45
2 | 12 14 6 16 10 5 15 7 8 33 4 | 19 21 17 23 19 18 21 18 20 27 17
3E | 11 29 5 22 16 6 18 10 12 22 5 | 42 40 37 47 28 39 36 39 40 33 36
4 | 7 9 5 8 12 3 8 5 8 18 2 | 35 35 34 41 35 35 33 36 42 42 36
5 | 9 15 5 9 9 6 15 5 11 19 3 | 14 21 14 10 16 12 22 11 20 20 13
6E | 13 19 6 17 16 6 17 9 13 25 4 | 67 61 62 69 53 63 57 64 60 50 61
7 | 10 16 5 10 16 5 13 5 9 24 3 | 20 28 21 18 36 17 23 19 27 25 20
8 | 8 10 5 8 11 4 9 4 9 11 2 | 20 28 21 20 26 20 26 22 26 20 22
9 | 11 12 3 7 13 4 8 4 10 13 3 | 38 41 38 37 37 37 38 35 39 35 36
10 | 6 7 6 7 9 2 8 3 10 19 2 | 22 21 22 23 24 21 21 21 23 22 22
11 | 7 16 4 7 17 3 11 4 12 11 3 | 25 36 31 31 40 31 35 31 34 30 30
12 | 14 15 4 13 19 5 17 8 15 20 4 | 22 31 25 28 32 23 31 22 40 18 25
13E | 7 12 6 11 11 4 10 7 11 12 3 | 38 39 37 38 45 35 39 36 35 40 36
14E | 9 10 5 8 10 4 9 6 11 16 3 | 61 65 62 62 63 61 63 60 59 63 60
15 | 22 20 5 10 16 4 16 6 15 18 5 | 26 33 24 18 30 19 27 19 29 26 22
16 | 10 18 5 12 11 6 18 7 12 18 4 | 23 33 24 24 27 24 31 24 32 26 23
17E | 11 22 6 9 14 4 22 7 8 13 4 | 28 35 31 30 39 28 34 30 34 32 30
18 | 7 13 5 16 13 3 13 4 12 27 3 | 25 29 28 32 27 26 29 26 33 27 27
19E | 12 28 5 11 12 4 12 9 9 15 4 | 21 31 21 20 27 20 22 17 27 21 18
20 | 8 11 5 11 9 4 11 3 9 31 3 | 29 34 33 27 32 28 36 28 31 33 30
21 | 5 12 5 9 9 5 14 6 9 24 3 | 21 26 24 27 27 23 27 23 28 22 23
22 | 5 13 4 8 8 3 10 3 6 17 2 | 22 29 25 24 27 23 28 23 27 28 24
23 | 6 25 5 10 16 3 15 6 10 15 4 | 20 32 25 18 34 20 31 21 25 23 21
24 | 19 23 5 11 19 6 11 7 11 19 4 | 28 23 22 25 28 23 26 22 35 19 22
25 | 11 17 5 11 14 6 13 6 13 16 4 | 20 26 27 31 29 26 32 26 37 21 26
26E | 16 20 7 12 15 7 22 9 11 26 5 | 80 74 69 75 72 71 74 73 65 65 72
X27 | 8 --- --- --- --- 83 --- --- --- --- 0 | 55 --- --- --- --- 43 --- --- --- --- 58
28 | 10 13 4 11 18 3 14 6 10 14 3 | 28 30 25 21 32 23 29 25 27 26 25
29E | 13 17 7 10 20 4 20 9 15 14 4 | 37 40 41 41 40 37 42 41 41 37 39
30 | 9 11 4 11 15 4 10 4 13 14 3 | 14 22 18 18 18 17 21 17 26 19 16
31 | 10 12 5 10 21 5 12 7 10 14 3 | 17 22 19 13 37 16 22 17 24 16 17
32 | 8 10 3 8 11 3 8 5 10 21 2 | 13 19 17 16 22 14 21 14 17 22 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 5 11 14 5 14 6 11 19 |T 30 33 30 30 33 29 33 29 33 30 30
WRMS | 11 16 5 10 11 4 13 6 9 19 |NE 25 28 25 24 29 24 28 24 30 25 25
MEDI | 10 14 5 10 13 4 13 6 10 18 |MD 25 31 25 27 32 23 31 24 32 26 25
Table 3.1722.4 GPS week: 1722 Day: 4 MJD: 56302.000
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 | 12 13 6 9 11 3 15 3 7 14 3 | 40 43 44 42 47 43 47 45 45 42 43
2 | 11 14 7 17 10 4 16 8 7 34 4 | 21 20 16 22 17 16 20 16 15 25 15
3E | 13 20 8 14 26 6 16 7 16 22 5 | 43 38 39 44 34 40 38 41 44 34 38
4 | 7 8 5 13 14 3 11 4 7 17 3 | 25 31 29 33 32 30 30 30 28 36 29
X5 | 8 --- --- --- --- 38 --- --- --- --- 0 | 24 --- --- --- --- 27 --- --- --- --- 24
6E | 17 19 7 17 20 5 18 7 16 20 5 | 66 64 64 70 52 64 59 64 64 58 62
7 | 8 15 5 9 18 4 17 5 8 31 3 | 16 23 18 13 36 16 26 17 23 29 18
8 | 9 13 4 9 11 3 12 7 8 16 3 | 17 25 16 16 21 14 25 16 18 17 17
9 | 10 12 4 12 13 4 13 5 10 14 3 | 22 32 23 27 27 24 35 28 29 27 27
10 | 6 10 6 12 7 3 9 5 11 23 3 | 17 22 18 21 23 19 24 19 17 22 19
11 | 10 15 6 10 18 3 13 8 10 14 4 | 29 38 34 31 44 31 37 30 32 30 31
12 | 15 15 7 14 19 4 17 5 8 19 4 | 20 30 23 29 32 20 28 22 26 20 22
13E | 9 11 5 9 11 3 11 4 8 21 3 | 41 44 40 44 43 40 45 40 44 44 41
14 | 10 12 6 13 14 5 12 7 9 14 3 | 81 81 82 85 85 79 83 82 76 80 81
15 | 18 18 5 12 18 6 15 6 15 19 4 | 20 32 21 19 30 20 29 20 33 28 21
16 | 10 16 6 13 13 3 15 5 10 18 3 | 23 32 26 21 29 25 32 23 28 26 24
17E | 8 19 5 11 13 5 24 6 12 12 4 | 17 27 20 20 29 18 27 20 27 21 20
18 | 7 12 4 20 14 3 13 4 11 28 3 | 24 28 27 35 27 25 28 26 29 26 26
19E | 7 21 6 12 15 4 14 5 9 14 4 | 18 26 19 23 26 19 21 17 23 22 18
20 | 8 9 7 11 8 4 11 4 11 32 3 | 29 33 32 25 34 30 35 30 36 29 31
21 | 5 12 4 12 10 4 15 4 8 26 3 | 20 25 22 22 28 20 26 20 25 25 21
22 | 8 10 4 12 10 4 11 3 10 17 3 | 22 26 25 24 31 23 28 23 26 27 24
23 | 6 19 6 9 17 3 16 5 9 16 3 | 23 29 24 20 33 22 29 22 29 23 23
24 | 11 22 5 10 17 5 13 7 12 20 4 | 23 21 21 26 30 21 27 26 29 19 23
25 | 12 16 5 16 16 3 14 5 11 13 4 | 21 29 24 31 30 22 32 25 27 20 25
26E | 12 23 11 14 20 9 25 10 11 52 5 | 100 103 98 105 104 95 106 100 102 89 102
X27 | 8 --- --- --- --- 52 --- --- --- --- 0 | 64 --- --- --- --- 31 --- --- --- --- 65
28 | 8 15 5 12 16 3 13 5 10 13 3 | 23 31 23 18 32 21 29 21 29 20 22
29E | 13 21 6 13 20 4 21 7 10 12 4 | 42 48 42 43 45 44 47 43 51 45 43
30 | 8 11 4 12 14 3 12 3 9 13 3 | 14 23 17 16 15 17 21 15 25 19 16
31 | 12 14 5 13 18 4 14 6 10 19 4 | 16 23 18 17 35 18 22 15 26 19 16
32 | 7 9 5 8 13 3 8 3 12 18 3 | 14 21 19 18 26 17 22 17 20 21 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 6 13 15 4 15 6 10 22 |T 30 34 30 32 35 29 35 30 34 31 31
WRMS | 10 15 6 11 15 4 14 5 9 18 |NE 23 28 23 23 30 23 28 23 27 24 25
MEDI | 9 14 5 12 14 4 14 5 10 18 |MD 23 29 23 24 31 22 29 23 28 26 24
Table 3.1722.5 GPS week: 1722 Day: 5 MJD: 56303.000
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 19 4 8 11 3 16 3 7 13 3 | 33 34 33 31 37 31 36 30 30 30 30
2 | 12 16 7 13 10 4 14 7 6 34 3 | 19 19 11 18 12 12 19 16 16 28 13
3E | 16 23 10 19 18 7 18 8 22 27 6 | 43 39 37 46 30 38 34 39 43 35 37
4 | 13 10 5 11 11 4 14 4 10 14 3 | 16 21 19 25 23 19 22 19 20 22 19
5 | 11 16 7 10 11 6 17 5 6 23 3 | 14 16 7 10 9 11 17 8 8 14 10
X6E | 18 --- 8 19 22 8 20 12 29 56 7 | 65 --- 61 67 52 62 57 65 68 72 62
7 | 12 16 8 10 16 4 15 6 9 28 4 | 21 25 22 12 35 17 24 17 27 24 18
8 | 11 14 5 8 10 4 11 4 10 18 3 | 20 26 21 18 25 19 27 20 25 19 21
9 | 9 11 5 9 13 4 15 6 9 18 3 | 23 28 23 22 24 22 28 23 27 24 23
10 | 13 10 8 10 10 4 9 7 9 24 3 | 19 18 18 23 22 18 19 18 19 22 18
11 | 10 19 6 8 18 3 11 5 11 12 3 | 23 32 26 25 38 23 29 22 32 23 24
12 | 10 18 8 11 20 5 17 7 12 20 4 | 18 28 17 23 32 16 30 16 24 16 18
13E | 12 13 7 10 12 5 11 6 8 26 3 | 54 60 58 51 60 51 57 51 61 47 54
14 | 6 10 4 6 18 3 8 5 7 13 2 | 27 25 27 25 36 26 31 25 27 27 25
15 | 16 22 5 10 17 3 16 5 7 16 4 | 24 29 16 15 27 13 25 15 21 21 16
16 | 13 16 6 12 13 5 15 8 12 17 4 | 23 26 19 19 26 19 26 19 27 22 19
17E | 9 19 7 8 17 4 18 5 11 14 4 | 32 40 33 32 41 31 38 34 37 35 34
18M | 7 14 5 16 15 3 13 3 8 27 3 | 23 26 25 32 23 24 26 23 26 24 24
19E | 13 13 5 12 13 3 9 5 10 13 3 | 13 20 17 17 24 17 20 15 26 20 15
20 | 10 12 5 11 9 3 11 7 7 28 3 | 27 28 27 19 29 25 30 24 28 22 24
21M | 11 13 4 9 11 5 14 6 8 24 3 | 21 22 18 22 27 17 25 18 21 29 18
22M | 5 10 5 8 13 3 13 4 13 16 3 | 19 25 23 19 28 21 25 18 26 25 20
23 | 10 18 6 8 14 4 15 5 10 9 3 | 18 26 24 18 30 21 27 20 28 18 20
24 | 11 21 5 8 20 4 14 5 9 20 4 | 24 24 23 25 33 22 27 24 28 19 23
25 | 10 14 7 11 17 4 14 4 10 16 3 | 17 22 19 24 26 17 31 19 21 17 19
26 | 14 18 7 9 21 6 19 8 9 22 4 | 60 63 55 63 63 52 66 57 52 63 59
X27 | 8 --- --- --- --- 55 --- --- --- --- 0 | 43 --- --- --- --- 43 --- --- --- --- 45
28 | 11 12 7 11 18 2 17 4 10 15 4 | 27 30 25 19 34 21 27 20 26 19 22
29E | 12 20 8 9 22 4 21 7 10 15 4 | 69 76 69 68 80 69 72 75 72 69 72
30 | 10 10 8 12 16 5 12 6 15 16 4 | 14 17 15 14 16 13 18 14 20 18 12
31 | 11 14 6 9 20 4 15 5 8 17 3 | 16 22 13 14 35 14 21 16 21 15 14
32 | 8 10 4 6 11 2 8 7 8 18 2 | 13 17 16 13 22 14 21 15 19 20 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 6 10 15 4 14 6 10 20 |T 27 29 26 26 32 25 30 25 29 27 26
WRMS | 11 16 6 10 14 4 14 5 8 17 |NE 21 24 19 19 26 19 25 18 23 20 20
MEDI | 11 14 6 10 15 4 14 5 9 18 |MD 23 26 23 22 29 21 27 20 26 22 20
Table 3.1722.6 GPS week: 1722 Day: 6 MJD: 56304.000
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 | 12 24 4 12 14 4 14 6 7 12 4 | 49 57 55 54 62 56 56 57 53 56 55
2 | 8 17 6 18 14 5 17 7 10 36 4 | 25 29 23 27 25 22 26 26 21 38 24
3E | 16 24 7 15 21 7 22 6 34 27 6 | 53 48 52 52 43 50 48 47 51 51 46
4 | 7 12 4 14 13 3 12 6 11 16 3 | 32 36 35 43 41 35 35 35 29 41 35
5 | 11 16 5 12 13 5 14 5 8 27 3 | 15 18 10 10 9 9 16 9 7 19 11
6E | 18 19 7 16 21 7 23 8 25 27 5 | 74 74 74 79 65 73 74 74 83 70 74
7 | 11 15 4 15 16 4 14 4 10 31 3 | 18 26 22 16 35 18 26 19 24 25 20
8 | 8 12 3 11 12 4 12 4 10 16 3 | 21 32 23 23 28 22 31 24 25 22 25
9 | 7 11 3 15 12 6 12 3 10 22 3 | 32 38 33 30 30 29 41 32 32 29 32
10 | 12 10 4 13 10 4 9 5 12 27 3 | 22 21 23 29 29 23 26 23 22 28 23
11 | 8 18 6 14 20 5 10 6 9 12 4 | 34 41 38 39 48 37 38 37 40 38 37
12 | 10 15 5 18 22 5 17 6 9 23 4 | 27 34 26 33 34 27 34 28 30 25 28
13 | 10 18 5 15 19 5 10 7 10 15 4 | 66 69 60 67 65 61 65 61 65 62 63
14 | 8 15 4 11 18 3 8 5 8 11 3 | 30 37 31 32 36 32 32 31 32 33 31
15 | 19 20 6 14 18 4 16 7 12 24 4 | 31 43 30 24 34 27 38 29 35 37 30
16 | 14 14 5 17 19 5 15 4 10 20 4 | 29 34 29 24 29 28 35 28 29 30 27
17E | 10 17 6 10 14 5 20 7 15 12 4 | 31 35 33 36 42 32 38 36 41 34 35
18 | 6 12 4 20 17 3 12 4 10 33 3 | 31 34 31 36 30 29 32 31 34 43 32
19E | 9 18 7 12 15 5 14 6 9 14 3 | 16 22 23 21 23 20 21 18 22 24 17
20 | 10 12 7 13 9 3 11 7 11 30 3 | 35 38 37 34 38 35 39 37 36 38 36
21 | 11 13 4 13 12 4 14 7 8 24 3 | 28 31 29 31 33 26 31 31 29 29 30
22 | 7 11 3 10 18 5 11 6 8 17 3 | 24 29 27 29 35 26 30 30 28 33 28
23 | 9 20 6 12 18 4 15 5 5 12 4 | 27 34 28 24 36 27 34 25 30 26 27
24 | 10 20 4 11 18 4 15 5 11 20 4 | 29 26 26 30 31 27 30 30 31 24 28
25 | 12 14 5 15 18 3 15 7 11 20 4 | 27 32 29 34 30 29 36 32 35 25 30
26 | 8 13 9 10 13 4 17 6 16 31 4 | 33 39 38 31 37 33 38 30 35 42 32
X27 | 8 --- --- --- --- 52 --- --- --- --- 0 | 58 --- --- --- --- 47 --- --- --- --- 61
28 | 8 14 6 11 16 4 13 6 11 14 3 | 30 37 31 29 39 27 35 29 32 30 31
29E | 18 20 5 15 22 4 22 6 10 18 5 | 47 48 45 46 50 44 47 45 49 44 45
30 | 9 13 5 15 16 4 11 4 8 17 3 | 20 29 20 22 22 20 26 20 23 24 21
31 | 11 12 4 13 19 4 13 4 10 16 3 | 20 26 17 15 37 19 24 17 23 19 18
32 | 11 11 4 10 13 4 8 5 13 26 3 | 13 20 19 22 29 18 23 21 21 32 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 5 14 16 4 15 6 12 22 |T 32 36 32 32 36 31 35 32 33 34 32
WRMS | 10 16 5 13 15 4 14 5 9 19 |NE 28 32 27 28 33 27 32 28 28 30 29
MEDI | 10 15 5 13 16 4 14 6 10 20 |MD 29 34 29 30 35 27 34 30 31 32 30
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 4.1722 GPS week: 1722 MJD: 56298.0-56304.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 |U 4 5 14 | ---- ---- ---- |U 7 10 17 |
emr | emr 2938 | 7 8 18 | ---- ---- ---- | 9 11 19 |
esa | esa 2962 | 5 5 14 | ---- ---- ---- | 6 8 15 |
gfz | gfz 2946 |U 5 5 16 | ---- ---- ---- |U 6 10 15 |
grg | grg 2962 |U 9 8 23 | ---- ---- ---- | 9 11 21 |
igr | igr 2962 | 5 5 14 | ---- ---- ---- | 6 10 15 |
igs | igs 2936 | 5 5 16 | ---- ---- ---- | 7 11 17 |
jpl | jpl 2951 | 5 6 16 | ---- ---- ---- | 7 10 20 |
mit | mit 2962 | 6 6 20 | ---- ---- ---- |U 8 11 19 |
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 5.1722.0 GPS week: 1722 Day: 0 MJD: 56298.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 4 5 13 | ---- ---- ---- | 6 5 15 |
emr | emr 2964 | 7 8 18 | ---- ---- ---- | 7 7 19 |
esa | esa 2976 | 5 4 13 | ---- ---- ---- | 5 4 16 |
gfz | gfz 2934 | 5 4 14 | ---- ---- ---- | 6 8 19 |
grg | grg 2976 | 7 4 19 | ---- ---- ---- | 7 7 22 |
igr | igr 2975 | 4 4 13 | ---- ---- ---- | 5 5 16 |
igs | igs 2969 | 5 4 16 | ---- ---- ---- | 6 6 17 |
jpl | jpl 2964 | 6 6 15 | ---- ---- ---- | 9 7 23 |
mit | mit 2976 | 6 5 18 | ---- ---- ---- | 7 10 21 |
Table 5.1722.1 GPS week: 1722 Day: 1 MJD: 56299.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 4 5 12 | ---- ---- ---- | 8 11 16 |
emr | emr 2964 | 7 6 18 | ---- ---- ---- | 11 14 22 |
esa | esa 2976 | 6 5 12 | ---- ---- ---- | 7 8 12 |
gfz | gfz 2963 | 5 4 13 | ---- ---- ---- | 7 13 15 |
grg | grg 2976 | 9 6 21 | ---- ---- ---- | 10 13 23 |
igr | igr 2976 | 5 5 12 | ---- ---- ---- | 7 12 14 |
igs | igs 2961 | 6 5 17 | ---- ---- ---- | 9 14 17 |
jpl | jpl 2963 | 5 6 15 | ---- ---- ---- | 8 12 22 |
mit | mit 2976 | 7 7 19 | ---- ---- ---- | 10 14 20 |
Table 5.1722.2 GPS week: 1722 Day: 2 MJD: 56300.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 5 7 17 | ---- ---- ---- | 9 10 13 |
emr | emr 2964 | 7 8 16 | ---- ---- ---- | 11 13 19 |
esa | esa 2976 | 6 7 14 | ---- ---- ---- | 8 9 13 |
gfz | gfz 2965 | 6 7 16 | ---- ---- ---- | 8 11 14 |
grg | grg 2976 | 9 9 26 | ---- ---- ---- | 11 11 23 |
igr | igr 2976 | 6 8 14 | ---- ---- ---- | 8 10 13 |
igs | igs 2947 | 6 7 17 | ---- ---- ---- | 9 12 16 |
jpl | jpl 2962 | 6 7 11 | ---- ---- ---- | 8 11 19 |
mit | mit 2976 | 8 8 19 | ---- ---- ---- | 9 13 17 |
Table 5.1722.3 GPS week: 1722 Day: 3 MJD: 56301.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 4 5 16 | ---- ---- ---- | 10 10 17 |
emr | emr 2964 | 7 8 22 | ---- ---- ---- | 12 14 23 |
esa | esa 2976 | 5 6 19 | ---- ---- ---- | 8 8 14 |
gfz | gfz 2962 | 6 5 19 | ---- ---- ---- | 8 10 14 |
grg | grg 2976 | 9 10 29 | ---- ---- ---- | 12 11 20 |
igr | igr 2976 | 5 6 17 | ---- ---- ---- | 9 13 20 |
igs | igs 2947 | 5 6 21 | ---- ---- ---- | 10 11 21 |
jpl | jpl 2964 | 6 6 19 | ---- ---- ---- | 10 11 26 |
mit | mit 2976 | 5 7 26 | ---- ---- ---- | 10 15 23 |
Table 5.1722.4 GPS week: 1722 Day: 4 MJD: 56302.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2952 | 4 4 14 | ---- ---- ---- | 6 8 15 |
emr | emr 2872 | 9 9 19 | ---- ---- ---- | 8 9 16 |
esa | esa 2880 | 5 4 14 | ---- ---- ---- | 5 7 13 |
gfz | gfz 2867 | 5 4 15 | ---- ---- ---- | 5 8 15 |
grg | grg 2880 | 11 8 23 | ---- ---- ---- | 9 11 21 |
igr | igr 2880 | 4 5 15 | ---- ---- ---- | 5 7 12 |
igs | igs 2857 | 5 5 16 | ---- ---- ---- | 8 10 16 |
jpl | jpl 2872 | 5 7 16 | ---- ---- ---- | 6 7 14 |
mit | mit 2880 | 6 7 19 | ---- ---- ---- | 6 7 14 |
Table 5.1722.5 GPS week: 1722 Day: 5 MJD: 56303.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 5 6 15 | ---- ---- ---- | 6 16 25 |
emr | emr 2876 | 8 8 17 | ---- ---- ---- | 7 17 20 |
esa | esa 2976 | 4 5 14 | ---- ---- ---- | 5 17 25 |
gfz | gfz 2965 | 5 6 26 | ---- ---- ---- | 5 12 17 |
grg | grg 2976 | 9 11 25 | ---- ---- ---- | 10 19 28 |
igr | igr 2976 | 4 5 16 | ---- ---- ---- | 5 16 23 |
igs | igs 2946 | 5 5 14 | ---- ---- ---- | 5 16 24 |
jpl | jpl 2967 | 5 7 18 | ---- ---- ---- | 5 18 24 |
mit | mit 2976 | 5 5 21 | ---- ---- ---- | 7 14 24 |
Table 5.1722.6 GPS week: 1722 Day: 6 MJD: 56304.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 3 5 10 | ---- ---- ---- | 5 8 14 |
emr | emr 2968 | 7 9 19 | ---- ---- ---- | 7 4 13 |
esa | esa 2976 | 4 4 11 | ---- ---- ---- | 4 6 9 |
gfz | gfz 2967 | 4 4 10 | ---- ---- ---- | 4 6 11 |
grg | grg 2976 | 8 12 21 | ---- ---- ---- | 7 5 11 |
igr | igr 2976 | 4 4 12 | ---- ---- ---- | 5 7 9 |
igs | igs 2926 | 4 4 11 | ---- ---- ---- | 5 6 9 |
jpl | jpl 2966 | 5 6 15 | ---- ---- ---- | 5 8 13 |
mit | mit 2976 | 5 3 14 | ---- ---- ---- | 8 6 15 |
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 6.1722 GPS week: 1722 MJD: 56298.500-56304.500
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 -31 154 94 1 | 4 10
| 22 21 66 106 5 | 2
emr uuuuu | -4 25 -210 -134 -3 | -12 17
| 22 23 67 80 14 | 4
esa uuuuu | -20 -11 29 -77 2 | -3 9
| 34 35 36 34 3 | 2
gfz uuuuu | 44 58 -21 28 -5 | 9 13
| 24 22 163 61 4 | 2
grg uuuux | 7 -12 49 29 13 | -4 21
| 13 12 73 46 14 | 2
igr xxxxx | -59 8 -28 31 -3 | 1 8
| 18 20 43 57 3 | 2
irf xxxxx | 4 -9 14 12 5 | -2 8
| 18 17 22 28 3 | 2
jpl uuuuu | -13 6 -160 -15 -7 | -3 12
| 22 31 59 76 14 | 4
mit uuuuu | 14 -8 0 37 10 | 0 11
| 21 27 72 41 9 | 2
ngs uuuuu | -43 7 10 38 -1 | 1 7
| 30 49 151 147 4 | 1
sio xxxxx | 234 -211 -381 177 -9 | 18 20
| 53 59 70 82 3 | 3
Table 7.1722.0 GPS week: 1722 Day: 0 MJD: 56298.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 22 -34 197 30 4 | 0 9
emr uuuuu | 30 53 -146 -53 -7 | -9 16
esa uuuuu | -88 -48 68 -106 3 | -6 10
gfz uuuuu | 92 60 -120 77 -2 | 8 14
grg uuuux | 23 -21 71 81 -6 | -1 23
igr xxxxx | -27 33 41 41 -5 | 0 10
irf xxxxx | 34 3 -1 25 7 | -4 8
jpl uuuuu | 9 34 -85 45 0 | -1 12
mit uuuuu | 48 26 -74 -7 11 | -2 10
ngs uuuuu | -45 -21 37 86 -8 | 1 7
sio xxxxx | 286 -267 -455 178 -8 | 19 22
Table 7.1722.1 GPS week: 1722 Day: 1 MJD: 56299.500
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 | 19 -50 91 -102 9 | 3 9
emr uuuuu | 11 25 -174 -14 -17 | -8 15
esa uuuuu | -33 -41 58 -89 1 | -3 8
gfz uuuuu | 42 58 36 69 -7 | 11 14
grg uuuux | 12 -1 125 88 -5 | -3 22
igr xxxxx | -49 32 -54 45 -8 | 3 9
irf xxxxx | 19 17 13 44 2 | -3 8
jpl uuuuu | -9 16 -94 51 -12 | 2 10
mit uuuuu | 34 33 -58 50 2 | -2 11
ngs uuuuu | -67 -31 -5 7 3 | 2 6
sio xxxxx | 248 -288 -264 335 -12 | 21 23
Table 7.1722.2 GPS week: 1722 Day: 2 MJD: 56300.500
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 | 38 -30 142 200 -2 | 6 11
emr uuuuu | 5 54 -269 -98 -12 | -8 15
esa uuuuu | -16 -43 28 -22 -1 | -1 7
gfz uuuuu | 40 36 167 72 -8 | 12 15
grg uuuux | -14 1 92 -3 27 | -5 21
igr xxxxx | -80 3 -5 105 -4 | 3 9
irf xxxxx | 0 -1 37 41 9 | -1 8
jpl uuuuu | -48 41 -121 26 -9 | 1 10
mit uuuuu | 6 -2 -33 -14 26 | -1 11
ngs uuuuu | -15 29 -105 -143 -1 | 3 8
sio xxxxx | 314 -152 -375 138 -8 | 21 22
Table 7.1722.3 GPS week: 1722 Day: 3 MJD: 56301.500
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 -64 281 198 2 | 4 11
emr uuuuu | -37 4 -197 -172 -14 | -12 18
esa uuuuu | 7 6 5 -40 8 | -3 8
gfz uuuuu | 21 23 182 74 -5 | 9 14
grg uuuux | 3 -18 75 53 15 | -7 19
igr xxxxx | -75 -4 -32 85 -4 | 1 9
irf xxxxx | -14 -19 21 21 5 | -2 8
jpl uuuuu | -33 -19 -209 -43 -9 | -2 11
mit uuuuu | 3 -22 -55 47 8 | -1 11
ngs uuuuu | -21 102 -116 -162 -3 | 1 8
sio xxxxx | 199 -202 -353 232 -9 | 18 20
Table 7.1722.4 GPS week: 1722 Day: 4 MJD: 56302.500
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 -3 138 71 -3 | 4 11
emr uuuuu | -21 33 -332 -189 1 | -15 20
esa uuuuu | 9 -14 60 -97 1 | -2 9
gfz uuuuu | 45 69 -24 -32 -10 | 8 13
grg uuuux | -2 -2 69 20 23 | -6 20
igr xxxxx | -60 10 -75 -63 -4 | 0 8
irf xxxxx | 7 -20 45 -5 7 | -1 8
jpl uuuuu | -21 16 -235 -57 -15 | -4 11
mit uuuuu | -1 -29 110 62 17 | 0 12
ngs uuuuu | -19 19 -157 167 3 | 1 7
sio xxxxx | 166 -222 -475 116 -12 | 17 20
Table 7.1722.5 GPS week: 1722 Day: 5 MJD: 56303.500
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 | 66 -19 134 135 1 | 4 11
emr uuuuu | -14 -7 -168 -224 19 | -17 20
esa uuuuu | -23 36 -33 -111 5 | -2 9
gfz uuuuu | 42 79 -129 -71 1 | 6 10
grg uuuux | 11 -32 5 -2 21 | -3 21
igr xxxxx | -53 -25 3 -1 3 | -1 7
irf xxxxx | 1 -35 -1 -27 6 | 0 9
jpl uuuuu | 1 2 -190 30 -24 | -7 11
mit uuuuu | 21 -32 42 21 6 | 3 13
ngs uuuuu | -98 -35 199 221 2 | 1 7
sio xxxxx | 194 -223 -368 105 -8 | 15 18
Table 7.1722.6 GPS week: 1722 Day: 6 MJD: 56304.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 6 -19 96 125 -7 | 4 11
emr uuuuu | -3 15 -181 -190 12 | -15 18
esa uuuuu | 7 30 16 -76 -1 | -2 8
gfz uuuuu | 23 85 -260 6 0 | 5 10
grg uuuux | 18 -8 -95 -34 19 | -3 21
igr xxxxx | -70 6 -73 5 -2 | -1 7
irf xxxxx | -18 -8 -15 -15 1 | 0 9
jpl uuuuu | 10 -47 -186 -157 21 | -10 17
mit uuuuu | -11 -28 68 102 1 | 4 13
ngs uuuuu | -34 -16 219 94 -2 | -1 8
sio xxxxx | 234 -123 -378 135 -5 | 13 18
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