[IGSREPORT-21356] Wk 1713 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Nov 22 07:59:30 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1713 (Nov 04, 2012 - Nov 10, 2012)
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. 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, no satellite L1/L2 delay calibration should be
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. 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 3 weeks (21 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:
igs1713[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1713[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1713[0-6].cls IGS GPS clock combination summary report.
igs17137.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17137.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL.
The other centres are excluded because of poorer consistency (GRG), they provide
broadcast clocks (NGS), or clock corrections are not provided (SIO). The clock
information not used is still compared to 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 12-Aug-2012 (GPS Week 1701, day 0, MJD 56151), GRG clocks are included
after changing their procedures to generate estimates in the center-of-figure
frame instead of the center-of-mass frame. Starting 16-Sep-2012 (GPS Week 1706,
day 0, MJD 56186) the CODE Analysis Center began submitting two solutions: COD
(1d SNX with 3d orbital arcs) and COF (1d SNX with 1d orbital arcs). The COD
clocks and orbits are included for comparison only; the COF solution is
included with weight, and is the reference clock center.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new solution from CNES/GRGS (GRG) is included with
weight except for the clock and LOD combinations.
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 | COF | 32 10 32 KOUC FLRS KOUC
0 | EMR | 30 30 HERS
0 | ESA | 32 10 32
0 | GFZ | 10 ALGO ASPA DGAR GUAT KIRU PIMO SANT STJO YAKT ZIMM
0 | GRG | 13 30 13 30 MCM4 SOFI ZECK ADIS KIT3 MCM4 SOFI ZECK
0 | JPL | 10 30 32
0 | MIT | 30 30
1 | COF | 10 10 FLRS GUAT MCM4
1 | EMR | 30 32 32
1 | ESA | 10 32 10 32 BAN2
1 | GFZ | 10 30 32 ASPA LHAZ
1 | GRG | 30 MCM4 NICO ADIS KARR MCM4 THTI
1 | JPL | 10 30 32
1 | MIT | 3 6 13 18 21 26 30 32 3 6 11 13 18 21 26 30 32 GMAS
1 | MIT | MDVJ
2 | ALL | 13
2 | COD | KOUC MCM4 KOUC MCM4
2 | COF | 10 19 30 10 19 30 KOUC MCM4 NICO KOUC MCM4 NRMD
2 | EMR | 32 METS METS
2 | ESA | 10 30 10 30 MATE BAN2 NICO TLSE
2 | GFZ | 10 30 32 LHAZ PIMO SYOG
2 | GRG | 21 13 21 NICO
2 | JPL | 6
2 | MIT | 8 32 8 TLSE
3 | COF | 10 30 10 30 KOUC KOUC XMIS
3 | EMR | HERS HERS
3 | ESA | 10 30 10 30 NKLG WIND
3 | GFZ | 10 30 32 COCO GUUG NTUS YAKT
3 | GRG | 32 32 KOUC SPT0 ASPA KOUC SPT0
3 | JPL | 8 10 CHAN
3 | MIT | MAC1
4 | COF | 10 30 32 10 30 32 HERT KOUC SOFI HERT KOUC
4 | EMR | 32 32
4 | ESA | 10 30 32 10 30 32 MATE MATE NICO
4 | GFZ | 10 30 32 ADIS MATE NKLG YAKT
4 | GRG | MCM4 NICO NYAL WROC WSRT ASPA GUAT KIT3 MCM4 NYAL
4 | GRG | POTS RAMO SOFI WROC WSRT
4 | JPL | 32 RAMO
4 | MIT | 10 23 10 23 NICO SOFI NICO SOFI
5 | COD | MCM4
5 | COF | 10 30 32 10 30 32 KOUC FLRS KOUC MCM4
5 | EMR | 32 32
5 | ESA | 10 30 32 10 30 32 TLSE TLSE
5 | GFZ | 10 30 32 OHI2 TLSE WILL YAKT
5 | GRG | IRKT WROC IRKT USNO WROC
5 | JPL | 17 32
6 | COF | 10 30 10 30 XMIS FLRS XMIS
6 | EMR | 32 32
6 | ESA | 10 30 10 30
6 | GFZ | 10 30 32 BOGT IRKT OHI2 YAKT
6 | GRG | 12 32 12
6 | JPL | 10 32
6 | MIT | 10 24 32 10 24
5. 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
----+--------+---------------
0 | SIO | ALL (high Transformation - See Table 2)
1 | SIO | ALL (high Transformation - See Table 2)
2 | ESA | ALL (high Transformation - See Table 2)
2 | SIO | ALL (high Transformation - See Table 2)
3 | SIO | ALL (high Transformation - See Table 2)
4 | SIO | ALL (high Transformation - See Table 2)
5 | SIO | ALL (high Transformation - See Table 2)
6 | SIO | ALL (high Transformation - See Table 2)
6. 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 | | | |
7. 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.
8. Small rotations were applied to all the AC orbit and ERP values in order
to align them to the current IGS reference frame. These 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 .0 -50 -2 -5 -.18
COF | 0 | .7 .4 .5 -62 -3 4 -.09
EMR | 0 | 9.6 6.3 -5.9 9 24 3 .22
ESA | 0 | 3.6 5.3 -20.1 122 -267 111 -.02
GFZ | 0 | .6 -.3 .7 -36 -44 -9 -.11
GRG | 0 | -1.7 .2 -5.7 -24 54 -32 .27
JPL | 0 | 5.2 6.7 5.9 -74 -25 36 -.01
MIT | 0 | 2.0 8.1 -4.9 -7 2 -24 .20
NGS | 0 | 5.6 5.3 -7.5 51 -18 59 .15
SIO | 0 | -.2 1.8 -42.6 77 -203 -5 .08
COD | 1 | .1 .1 -.2 -50 -7 -7 -.21
COF | 1 | .0 .2 .1 -42 -6 -12 -.32
EMR | 1 | 3.1 5.1 -5.6 16 30 1 -.04
ESA | 1 | 5.4 6.6 -20.7 189 -292 123 -.16
GFZ | 1 | .1 .2 1.1 -49 -38 -21 -.36
GRG | 1 | 3.4 -2.2 -5.2 -8 41 -27 .11
JPL | 1 | 7.0 -3.1 3.1 -49 38 13 .04
MIT | 1 | 4.0 7.2 -1.9 -3 -5 -23 -.11
NGS | 1 | 6.3 2.7 -14.4 87 -25 67 .05
SIO | 1 | 3.3 2.2 -45.5 141 -332 67 -.18
COD | 2 | -.2 .6 -.9 -40 -6 -21 -.20
COF | 2 | -.1 .9 -1.0 -44 -7 -22 -.23
EMR | 2 | 10.3 .0 -4.5 10 33 -1 -.02
ESA | 2 | 5.9 4.8 -17.2 138 -305 106 -.03
GFZ | 2 | -.6 1.2 .2 -34 -26 -27 -.26
GRG | 2 | 3.2 -3.0 -6.5 -13 46 -31 .14
JPL | 2 | 7.3 -1.8 1.6 -43 -2 0 .09
MIT | 2 | 6.1 5.8 -2.4 -6 0 -24 -.06
NGS | 2 | 15.2 -3.7 -5.0 18 -50 110 .12
SIO | 2 | 7.2 .7 -56.4 157 -427 70 .04
COD | 3 | -.5 .2 -1.0 -40 -4 -19 -.03
COF | 3 | -.7 .4 -1.3 -39 1 -21 .0
EMR | 3 | 10.2 4.0 -4.7 1 29 9 .05
ESA | 3 | 2.3 5.6 -17.0 159 -233 102 .11
GFZ | 3 | -.1 .3 -.4 -46 -44 -20 .03
GRG | 3 | -.2 3.8 -2.8 -11 56 -47 .27
JPL | 3 | 9.6 -1.6 2.2 -23 13 10 .07
MIT | 3 | 5.6 7.1 1.8 -7 1 -22 .03
NGS | 3 | 8.4 6.9 -3.0 30 -27 84 .36
SIO | 3 | 8.1 .0 -44.4 168 -365 222 .11
COD | 4 | -.5 .7 -1.3 -37 -5 -17 .04
COF | 4 | -.3 .4 -1.3 -30 -12 -20 .14
EMR | 4 | 4.4 3.8 -1.9 -4 20 8 .10
ESA | 4 | 2.7 5.3 -20.2 153 -281 135 .05
GFZ | 4 | .3 .4 -.2 -38 -67 -18 .08
GRG | 4 | -6.3 4.9 -11.7 -7 20 -33 .42
JPL | 4 | 1.2 5.0 7.2 -28 7 4 .38
MIT | 4 | 3.6 3.2 -1.3 -13 0 -24 .26
NGS | 4 | 3.6 3.3 -.3 10 -7 36 .24
SIO | 4 | 1.4 1.2 -63.7 74 -444 142 .24
COD | 5 | .1 1.5 -.5 -40 -12 -2 -.09
COF | 5 | .1 1.4 -.9 -31 -8 2 -.03
EMR | 5 | -3.1 7.9 -3.1 0 15 1 .22
ESA | 5 | -4.1 5.0 -14.5 129 -155 97 .21
GFZ | 5 | .3 .7 -.7 -47 -74 -14 .03
GRG | 5 | -8.2 8.7 1.4 -5 31 -40 .41
JPL | 5 | -6.2 6.9 4.7 -72 21 -11 .29
MIT | 5 | -.1 7.1 -.8 -6 0 -21 .13
NGS | 5 | -.5 -2.2 -8.7 41 0 5 .38
SIO | 5 | -3.3 4.0 -51.7 137 -287 -21 .16
COD | 6 | -.1 1.9 -.7 -38 -12 8 -.15
COF | 6 | .3 1.6 -.2 -38 -14 11 -.20
EMR | 6 | 1.3 10.9 -3.5 3 19 12 .29
ESA | 6 | 1.0 7.4 -11.9 151 -229 118 -.15
GFZ | 6 | .6 .6 -.1 -53 -61 -10 -.23
GRG | 6 | -5.3 5.4 4.8 -17 34 -46 .43
JPL | 6 | -1.5 6.7 7.9 -63 17 19 -.08
MIT | 6 | 2.9 9.5 -.5 -9 -1 -26 .10
NGS | 6 | 6.8 10.1 -3.6 48 -27 58 .31
SIO | 6 | 1.9 4.8 -55.4 172 -349 -97 .22
9. 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 navigation solution is still based on the SP3 clocks but this will soon
adopt the clock RINEX files as well.
10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products
are aligned to the IGS reference frame products (station coordinates and ERPs
as generated by IGN). For more information see IGSMAIL #2750. Because of this
change in alignment, Table 2 has been enhanced with one additional line per AC.
This additional line shows daily X- and Y-rotations, i.e. RX_sp3(ac) and
RY_sp3(ac), used to align each daily AC orbit to the combined SINEX prior to
the orbit combination. These a-priori rotations are derived from three sources:
the daily AC polar motion estimates, XPO(ac) and YPO(ac), provided in their ERP
files; the combined polar motion values, XPO(cmb) and YPO(cmb), from the SINEX
combination; along with the AC TRF rotations, RX_snx(ac) and RY(ac), also from
the SINEX combination:
RX_sp3(ac) = YPO(ac) - YPO(cmb) + RX_snx(ac)
RY_sp3(ac) = XPO(ac) - XPO(cmb) + RY_snx(ac)
Thus, the total rotation of the individual AC orbits w.r.t. the IGS combined
orbit is the sum of the values in the two lines of Table 2.
Starting on 19-Aug-2012 (GPS Week 1702; mjd=56158), the AC TRF rotations are
daily values, instead of weekly ones, based on the combination of daily AC
SINEX files.
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; since GPS Week 1632 the JPL solution is excluded from
the weekly SINEX combination.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) the igs08.atx absolute
antenna model file gives updated (IGSMAIL #6662) values for the JPSREGANT_DD
and JPSREGANT_SD antennas, plus updates for GPS IIF transmit antennas. This
updated file should be used in conjunction with IGb08. Though, igs08.atx is
also still consistent with IGS08.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of five 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 1.1713.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1713.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 2.1713.[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 3.1713.[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 and final
part, Table 5, is similar to Table 4 and contains daily precise navigation
statistics (tables 5.1713.0-6).
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 1713 summary. (Nov 04, 2012 - Nov 10, 2012)
Table 1.1713.a GPS week: 1713 MJD: 56235.000-56241.000
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 4 99 -35 -3 -.43 11 11 | -964 -220 40 94
| 0 0 1 39 48 14 .03 | 510 851
cof 258| 0 0 2 89 -75 2 -.41 11 11 | -925 -215 19 84
| 0 0 1 38 43 13 .03 | 512 850
emr 79| -2 0 0 -11 -112 -3 .32 16 16 | 3511 156 12 89
| 1 1 0 33 36 14 .02 | 842 689
esa 175| 1 0 1 -154 218 0 .04 6 6 | -1664 1265 11 99
| 0 0 0 47 97 14 .02 | 357 927
gfz 190| 0 -1 0 95 20 8 -.43 11 11 | 233 180 19 122
| 0 0 1 67 62 8 .04 | 500 800
grg 129| 0 0 0 27 -130 -31 .44 15 14 | -171 44 15 148
| 0 0 2 33 41 12 .04 | 271 580
igr n/a| 0 0 1 11 -37 -36 -.17 5 5 | 8732 893 17 88
| 0 0 0 37 49 8 .03 | 2257 742
jpl 80| -1 0 0 113 -63 3 .37 15 14 | 3062 142 15 94
| 1 1 1 60 70 14 .04 | 831 769
mit 239| 0 0 0 42 -45 -7 -.19 7 6 | -269 40 22 202
| 0 0 0 27 37 9 .02 | 263 430
ngs 240| 0 0 -3 -81 2 15 .33 11 9 | -831 -398 1939 3956
| 1 0 2 38 55 19 .02 | 421 726
sio 280| -1 0 9 -271 655 26 -.29 19 18 | --- --- --- ---
| 2 2 1 114 171 102 .03 | --- ---
Table 1.1713.b GPS week : 1713 MJD: 56235.000-56241.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 4 4 5 4 4 4 4 |
3 | 3 3 4 3 4 4 4 |
4 | 3 3 3 3 3 3 3 |
5 | 4 4 5 4 4 5 5 |
6 | 3 3 4 3 3 4 3 |
7 | 4 4 5 4 4 5 4 |
8 | 3 3 4 3 3 4 3 |
9 | 3 3 3 3 3 4 4 |
10 | 5 5 5 5 5 5 5 |
11 | 3 3 4 4 4 4 4 |
12 | 5 5 6 5 5 5 5 |
13 | 4 4 5 4 4 4 5 |
14 | 5 4 4 4 4 4 4 |
15 | 4 4 4 4 4 5 5 |
16 | 5 4 5 4 4 5 4 |
17 | 3 4 5 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 6 4 4 5 4 |
20 | 3 3 4 4 4 4 3 |
21 | 4 4 4 4 4 5 4 |
22 | 4 3 3 3 4 4 4 |
23 | 4 4 5 4 4 5 5 |
24 | 7 0 0 0 0 0 7 |
25 | 5 5 5 5 5 5 5 |
26 | 3 3 4 3 4 4 4 |
27 | 0 0 0 0 0 0 0 |
28 | 3 3 4 3 4 5 4 |
29 | 4 4 5 4 5 5 5 |
30 | 4 4 5 4 4 5 5 |
31 | 4 4 5 4 5 5 5 |
32 | 5 7 6 5 5 5 5 |
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 2.1713.0 GPS week: 1713 Day: 0 MJD: 56235.000
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| -2 0 2 93 -63 -19 -.45 10 10 | -960 -214 43 89
| 74 -19 |
cof 253| -1 0 1 124 -72 15 -.46 12 11 | -918 -215 19 81
| 46 28 |
emr 80| -1 0 0 -17 -111 -25 .33 16 16 | 2570 -958 15 92
| -11 -8 |
esa 175| 0 0 0 -75 251 5 .02 6 6 | -1842 791 12 93
| -19 47 |
gfz 179| 0 0 0 21 -36 13 -.44 12 12 | 443 -655 21 123
| -24 -45 |
grg 130| 1 0 0 4 -160 -36 .51 14 13 | 30 -385 15 138
| 45 20 |
igr n/a| 0 0 1 -3 -38 -48 -.17 4 4 | 5697 -260 17 100
| 13 53 |
jpl 80| -1 -2 2 111 10 21 .42 14 14 | 2277 -1161 14 86
| 44 -16 |
mit 239| 0 0 0 23 -108 -1 -.19 5 5 | -26 -276 23 177
| 4 -21 |
ngs 240| 0 -1 -2 -100 26 7 .33 10 9 | -859 -345 1899 4208
| -44 -27 |
sio 282| 2 -3 9 -181 345 -1 -.30 20 19 | --- --- --- ---
| 135 -201 |
Table 2.1713.1 GPS week: 1713 Day: 1 MJD: 56236.000
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 0 4 163 -88 2 -.42 13 12 | -904 387 38 96
| 34 9 |
cof 259| 0 0 0 135 -127 -3 -.41 13 12 | -866 409 17 85
| 59 13 |
emr 79| -4 -1 0 -4 -163 -19 .33 16 16 | 2421 266 15 99
| 21 -9 |
esa 175| 0 0 1 -195 250 22 .05 6 5 | -1155 -329 11 101
| 67 35 |
gfz 192| 0 -1 0 144 57 15 -.38 10 9 | 572 63 19 115
| -75 -44 |
grg 129| 0 1 2 77 -174 -37 .42 13 12 | -165 164 16 167
| 31 44 |
igr n/a| 0 0 1 50 -95 -42 -.17 4 4 | 6277 1012 17 101
| -1 57 |
jpl 80| -4 0 1 176 -172 -20 .36 18 16 | 1950 402 17 96
| -4 51 |
mit 240| 0 0 0 65 -38 -3 -.19 5 5 | -309 323 26 216
| -30 -15 |
ngs 242| 1 0 -4 -124 -70 -3 .31 10 8 | -719 118 1832 3775
| -99 10 |
sio 279| 0 -3 8 -272 631 48 -.28 20 18 | --- --- --- ---
| 189 -344 |
Table 2.1713.2 GPS week: 1713 Day: 2 MJD: 56237.000
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 264| 0 0 3 33 14 1 -.42 11 11 | -1058 -1235 29 92
| 51 -45 |
cof 261| 0 0 1 28 -14 -9 -.41 12 12 | -1019 -1236 16 87
| 50 14 |
emr 80| -2 0 -1 -76 -84 -4 .29 15 15 | 3161 138 14 91
| -10 3 |
esa 175| 0 0 1 -192 383 -4 .05 9 9 | -1960 2527 13 108
| 12 15 |
gfz 190| 0 -1 1 130 77 11 -.41 10 10 | 939 -966 19 123
| -92 -51 |
grg 129| 1 0 0 -16 -96 -26 .47 13 12 | 185 -787 15 141
| 44 44 |
igr n/a| 0 0 2 -63 19 -23 -.17 5 5 | 7668 730 19 104
| -2 40 |
jpl 80| -1 1 0 24 26 3 .38 14 13 | 2691 190 17 91
| 28 18 |
mit 240| 1 0 0 15 -20 -14 -.19 6 6 | -317 -306 24 229
| -30 -33 |
ngs 241| 1 0 -1 -136 82 34 .32 10 9 | -939 -1420 2401 4235
| 19 44 |
sio 281| -1 -1 8 -350 848 45 -.24 19 17 | --- --- --- ---
| 185 -459 |
Table 2.1713.3 GPS week: 1713 Day: 3 MJD: 56238.000
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 0 5 117 -49 -8 -.40 11 10 | -675 -465 38 88
| 16 9 |
cof 260| 0 0 0 98 -110 -17 -.40 9 9 | -638 -455 17 81
| 64 69 |
emr 80| -1 0 0 22 -124 -4 .34 16 16 | 4263 -17 13 71
| 0 -20 |
esa 175| 1 1 2 -147 150 9 .07 6 6 | -1597 1720 12 96
| 37 76 |
gfz 191| 0 -1 0 117 52 4 -.41 11 11 | 241 187 17 125
| -73 -44 |
grg 130| 1 0 -3 35 -145 -52 .41 15 15 | 24 -171 15 154
| 55 32 |
igr n/a| 0 0 1 30 -51 -42 -.16 5 5 | 9232 878 17 82
| -1 33 |
jpl 80| -3 -2 0 92 -75 15 .39 15 14 | 3713 60 16 91
| 30 -11 |
mit 240| 0 0 0 14 -7 -19 -.18 7 7 | 143 -502 19 168
| -28 -43 |
ngs 240| 1 0 -5 -53 -7 28 .30 11 10 | -651 -417 1826 3901
| -84 47 |
sio 281| -2 -1 9 -387 727 184 -.25 18 18 | --- --- --- ---
| 191 -392 |
Table 2.1713.4 GPS week: 1713 Day: 4 MJD: 56239.000
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 264| 0 -1 5 73 -58 -23 -.44 12 11 | -1908 1339 43 105
| 72 20 |
cof 261| 0 -1 3 59 -93 3 -.38 12 11 | -1860 1327 24 89
| 34 52 |
emr 80| -2 1 0 -23 -115 9 .33 16 16 | 4472 -285 10 79
| 23 0 |
esa 175| 1 0 1 -203 253 0 .06 6 6 | -1887 1707 10 86
| 29 43 |
gfz 195| 0 0 -1 192 -69 -1 -.42 10 10 | -616 935 20 120
| -23 -58 |
grg 130| 0 2 -3 7 -147 -15 .45 15 14 | -433 686 15 149
| 57 18 |
igr n/a| 0 0 0 4 -44 -30 -.20 5 5 | 10455 372 17 92
| -11 18 |
jpl 80| 0 0 0 55 -93 16 .35 14 14 | 4140 -433 16 105
| 25 41 |
mit 240| 0 0 0 87 -48 1 -.22 7 6 | -576 725 23 253
| -20 -26 |
ngs 243| -3 0 0 -66 -23 -13 .34 13 11 | -1596 835 1578 4001
| -64 -40 |
sio 254| -3 0 7 -58 816 93 -.29 18 18 | --- --- --- ---
| 36 -450 |
Table 2.1713.5 GPS week: 1713 Day: 5 MJD: 56240.000
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 4 102 47 18 -.46 11 10 | -1035 -531 54 100
| 10 -52 |
cof 256| 0 0 1 70 -17 17 -.44 12 12 | -1022 -491 22 88
| 75 49 |
emr 80| -1 1 -1 15 -49 7 .31 16 16 | 3429 1091 11 99
| -15 27 |
esa 175| 1 0 3 -115 87 -22 .02 6 6 | -1200 776 13 109
| 37 170 |
gfz 194| 0 0 0 20 -25 -4 -.48 15 15 | -118 1271 23 125
| -13 -107 |
grg 126| 0 0 0 24 -53 -21 .40 16 15 | -571 859 15 132
| 52 -15 |
igr n/a| 0 0 0 20 34 -38 -.19 5 5 | 9998 2043 17 61
| -13 26 |
jpl 80| 0 0 -1 183 -29 -1 .30 15 14 | 2874 1168 15 79
| -20 28 |
mit 240| 1 0 -1 44 -81 3 -.22 8 8 | -565 255 24 210
| -60 -3 |
ngs 240| -1 0 -3 -42 55 24 .36 11 9 | -874 -634 1842 3778
| -41 26 |
sio 297| -4 2 8 -319 548 -48 -.32 19 17 | --- --- --- ---
| 142 -306 |
Table 2.1713.6 GPS week: 1713 Day: 6 MJD: 56241.000
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 264| -1 0 7 108 -50 5 -.40 12 10 | -209 -827 35 93
| 54 -16 |
cof 261| 0 -1 4 109 -90 10 -.41 10 10 | -153 -844 19 83
| 14 30 |
emr 80| -2 0 0 5 -138 10 .30 16 16 | 4265 861 11 97
| -1 2 |
esa 175| 1 0 2 -152 152 -10 .04 6 6 | -2009 1669 12 102
| 27 83 |
gfz 193| 0 -2 0 45 87 19 -.47 11 11 | 176 429 19 128
| -40 -72 |
grg 131| 1 0 4 60 -132 -33 .43 16 15 | -267 -54 16 158
| 22 5 |
igr n/a| 0 0 2 38 -85 -32 -.12 5 5 | 11797 1478 17 78
| -3 46 |
jpl 80| -1 0 0 148 -111 -7 .40 16 15 | 3793 770 16 112
| 26 10 |
mit 240| 0 0 -1 43 -15 -18 -.15 8 7 | -234 66 17 167
| -19 -26 |
ngs 239| 0 2 -6 -47 -45 33 .33 11 9 | -182 -928 2201 3800
| -9 59 |
sio 289| -1 3 12 -327 674 -134 -.31 19 18 | --- --- --- ---
| 174 -370 |
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 3.1713.0 GPS week: 1713 Day: 0 MJD: 56235.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 9 11 15 8 10 12 6 12 5 10 17 3 | 42 41 49 52 42 57 47 56 47 50 46 48
2 | 10 12 17 7 15 13 2 16 7 11 24 4 | 16 16 22 10 14 15 12 21 14 16 16 10
3 | 7 8 9 5 14 12 3 9 5 9 20 3 | 25 26 30 25 35 31 25 29 27 30 24 26
4 | 7 10 9 6 12 9 2 8 4 7 26 2 | 31 32 34 35 37 38 32 33 34 36 39 34
5E | 6 8 15 5 13 12 3 17 5 11 15 3 | 12 11 18 11 16 17 8 19 10 16 13 9
6 | 8 8 9 5 12 13 4 9 5 12 17 3 | 25 25 31 29 34 35 27 33 28 30 26 28
7 | 7 10 19 5 12 12 4 13 5 9 16 3 | 19 21 25 18 21 28 15 24 16 25 16 17
8 | 9 8 9 6 10 12 4 11 6 11 20 3 | 9 11 19 14 15 16 11 20 13 18 18 11
9 | 10 11 13 7 10 9 3 12 3 7 17 3 | 18 17 17 16 17 17 14 15 17 17 16 13
10E | 14 14 19 7 11 15 6 18 7 16 23 4 | 51 55 71 58 53 70 56 68 56 66 52 59
11 | 6 7 16 5 9 13 4 12 4 9 25 3 | 34 35 38 36 33 42 33 37 33 35 31 34
12 | 14 14 23 7 10 15 5 24 8 10 22 5 | 21 22 28 17 20 30 18 27 19 24 23 18
13 | 8 9 15 7 13 15 5 14 5 10 18 3 | 25 24 32 24 29 39 23 32 23 26 19 24
14 | 7 17 18 7 13 13 4 12 7 15 18 4 | 20 24 31 26 22 32 24 28 22 28 18 24
15 | 13 12 17 7 10 16 4 19 5 9 15 4 | 22 21 26 19 18 25 18 24 18 24 16 18
16 | 8 11 21 6 14 17 4 15 5 14 19 4 | 18 18 28 16 23 28 16 20 17 25 20 17
17 | 8 8 17 6 9 8 3 15 4 6 27 3 | 27 28 31 30 31 33 28 31 28 34 27 29
18E | 11 15 10 8 11 19 3 12 4 11 19 4 | 21 25 23 26 23 25 22 28 20 26 18 23
19 | 21 19 12 5 12 9 4 12 4 8 30 3 | 25 24 25 25 28 26 24 25 23 24 30 23
20E | 8 10 10 5 10 12 5 9 3 9 14 3 | 25 24 31 24 31 29 25 27 26 31 29 26
21 | 8 9 15 5 13 13 3 16 3 11 26 3 | 20 22 35 27 20 34 22 35 21 30 16 26
22E | 6 11 17 6 10 17 3 11 5 8 18 3 | 18 22 25 25 17 30 20 27 17 26 16 22
23 | 12 12 16 6 15 15 5 17 5 11 21 4 | 29 31 33 25 27 31 24 33 27 25 21 25
X24 | 31 18 --- 9 --- --- 14 --- 6 --- --- 7 | 16 --- --- --- --- --- --- --- 5 --- --- 13
25 | 8 14 25 8 13 21 4 14 5 11 17 4 | 26 27 35 31 34 31 28 32 26 32 29 28
26 | 9 10 12 6 8 11 4 9 4 8 12 3 | 17 16 16 16 14 20 15 17 14 15 15 14
X27 | 49 11 --- --- --- --- 61 --- --- --- --- 0 | 39 65 --- --- --- --- 46 --- --- --- --- 64
28 | 6 6 11 4 9 15 4 11 4 8 16 3 | 18 19 26 25 25 38 21 25 23 31 26 24
29 | 9 10 16 6 12 13 6 16 7 12 29 4 | 20 23 25 27 27 24 28 24 25 32 24 25
30E | 13 14 15 6 13 16 4 14 7 11 19 4 | 27 31 30 31 27 30 29 29 26 29 28 27
31 | 8 12 15 6 16 16 3 13 5 12 16 4 | 19 21 27 22 25 32 22 27 18 26 19 22
32E | 18 20 21 6 12 16 6 20 7 9 17 4 | 48 55 45 48 49 43 47 44 49 44 44 47
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 12 16 6 12 14 4 14 5 10 20 |T 24 26 30 26 26 31 25 29 23 29 24 25
WRMS | 10 11 16 6 12 13 4 14 5 9 19 |NE 23 24 28 25 25 30 23 28 23 27 23 23
MEDI | 8 11 15 6 12 13 4 13 5 10 18 |MD 21 24 28 25 25 30 24 27 23 26 21 24
Table 3.1713.1 GPS week: 1713 Day: 1 MJD: 56236.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 9 14 18 7 9 9 5 13 5 10 18 3 | 27 28 35 34 29 39 31 42 31 38 35 31
2 | 12 14 18 6 13 11 2 17 7 11 25 4 | 21 22 24 16 17 17 15 24 16 23 19 14
3 | 10 7 12 4 11 10 2 8 7 8 19 3 | 26 28 30 26 26 29 26 30 26 30 25 25
4 | 13 12 10 3 8 9 4 11 5 10 26 3 | 26 29 31 26 26 29 25 27 27 32 36 26
5E | 10 8 16 5 8 14 3 25 4 9 14 3 | 19 22 24 15 15 17 13 24 13 22 17 13
6 | 10 9 12 3 12 13 3 7 7 10 15 3 | 24 26 29 23 27 28 24 29 25 28 25 24
7 | 11 10 15 5 10 16 3 17 5 9 14 3 | 19 22 27 17 19 29 16 24 17 27 18 17
8 | 12 10 13 5 8 13 4 11 3 6 17 3 | 18 22 26 17 15 21 16 24 19 27 21 16
9 | 9 10 12 5 8 13 4 12 4 9 14 3 | 14 17 21 15 16 17 16 20 17 24 17 14
10E | 20 23 23 7 12 13 5 18 7 16 21 5 | 53 58 68 54 49 64 52 67 52 65 46 55
11 | 8 6 16 3 8 12 4 13 4 12 22 3 | 26 28 33 23 26 27 26 30 25 29 23 23
12 | 16 10 22 6 8 13 7 26 7 10 21 4 | 25 25 30 21 21 31 20 30 20 32 24 21
13 | 6 9 14 7 13 19 3 17 6 9 17 4 | 25 29 34 26 27 40 25 32 25 29 21 25
14 | 8 11 16 6 9 15 4 15 6 8 16 3 | 15 17 30 19 16 32 17 26 19 27 14 19
15 | 8 11 15 5 8 18 4 18 5 9 17 3 | 17 22 26 19 17 31 17 23 18 25 17 17
16 | 10 12 18 5 15 13 3 15 5 12 20 4 | 21 23 30 22 22 30 20 25 21 27 27 21
17 | 12 9 17 6 9 8 3 16 4 11 28 3 | 26 26 34 26 26 29 25 32 25 31 23 25
18E | 12 16 12 7 9 18 3 13 4 5 19 3 | 21 31 28 28 26 29 25 27 26 32 27 27
19 | 26 27 16 4 9 7 4 14 7 8 28 4 | 27 32 24 16 21 19 17 24 16 18 18 16
20E | 11 8 10 4 11 15 5 9 4 7 14 3 | 34 39 39 34 37 36 34 36 36 38 39 34
21 | 11 10 15 6 9 9 4 15 5 10 29 3 | 20 22 35 23 21 32 21 33 22 31 13 24
22E | 10 8 12 4 6 12 3 10 5 8 10 3 | 15 18 25 20 14 25 17 22 16 26 16 18
23 | 9 10 15 7 13 16 4 18 5 9 18 4 | 24 29 30 24 24 29 22 30 22 24 22 22
X24 | 155 13 --- --- --- --- >>>> --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- --- 1
25 | 26 16 29 7 12 12 6 17 6 10 24 4 | 39 49 48 44 43 48 42 52 44 46 52 42
26 | 8 7 13 4 8 10 4 10 3 7 13 2 | 14 18 24 12 13 20 13 19 15 21 15 12
X27 | 36 13 --- --- --- --- 54 --- --- --- --- 0 | 51 70 --- --- --- --- 39 --- --- --- --- 70
28 | 10 7 11 5 8 12 3 14 4 6 15 3 | 24 25 32 26 19 38 23 30 23 32 28 24
29 | 9 12 22 6 8 11 5 18 5 11 27 4 | 16 20 28 19 17 16 15 23 18 25 19 16
30E | 15 13 18 7 12 14 4 15 9 10 19 4 | 23 24 28 23 33 28 24 25 22 30 24 23
31 | 16 16 17 5 11 17 3 17 5 11 15 4 | 16 20 28 20 19 34 19 29 19 31 19 19
32E | 19 20 22 10 12 17 6 50 8 10 23 6 | 41 43 40 34 42 38 35 47 36 35 32 34
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 13 13 16 6 10 13 4 18 5 10 20 |T 24 28 31 24 24 30 23 30 23 30 24 24
WRMS | 12 12 16 5 9 12 4 16 5 8 18 |NE 21 24 28 21 21 27 20 27 21 27 21 20
MEDI | 11 10 15 5 9 13 4 15 5 9 18 |MD 23 25 30 23 21 29 22 27 22 29 22 22
Table 3.1713.2 GPS week: 1713 Day: 2 MJD: 56237.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 11 12 13 9 9 8 5 12 5 14 16 4 | 34 34 39 37 30 43 34 42 34 39 37 35
2 | 11 7 15 6 14 12 3 13 6 11 23 4 | 14 16 25 15 17 16 16 22 17 18 17 15
3 | 9 9 7 7 9 12 4 9 5 10 17 3 | 22 21 28 24 22 29 22 28 23 29 22 24
4 | 9 7 8 6 10 10 5 9 4 10 27 3 | 23 24 29 25 28 31 25 26 27 27 35 26
5E | 8 9 13 6 10 14 3 20 6 9 13 4 | 16 19 23 16 16 17 14 24 16 18 20 14
6 | 10 10 8 4 9 10 3 9 4 10 13 3 | 23 22 29 27 22 32 24 30 24 29 23 25
7 | 9 11 17 7 9 15 5 14 5 6 14 4 | 22 21 28 18 22 27 19 23 22 23 19 20
8 | 11 10 11 7 8 9 5 9 4 8 15 3 | 14 14 22 16 15 16 15 20 17 19 22 14
9 | 8 6 12 7 6 9 4 12 4 5 13 3 | 20 17 20 17 16 20 16 18 19 17 21 15
10E | 13 14 19 7 8 13 8 17 8 13 19 5 | 48 49 68 54 50 65 52 64 53 58 49 55
11 | 9 7 14 8 11 12 6 12 6 12 21 4 | 30 29 33 28 29 33 26 29 28 28 27 27
12 | 11 13 20 9 6 17 5 27 8 11 19 6 | 23 26 34 23 24 34 26 31 23 33 24 24
13 | 7 12 14 8 12 16 4 13 8 9 16 4 | 21 23 31 22 24 34 21 27 23 23 19 22
14 | 7 9 13 11 11 13 6 13 7 9 17 4 | 17 19 29 22 20 31 21 26 20 26 17 21
15 | 9 7 14 8 8 13 6 19 7 6 19 4 | 21 22 31 23 19 30 23 30 25 24 28 22
16 | 8 12 16 5 13 19 4 15 7 14 17 5 | 17 19 27 20 19 32 18 23 18 26 23 19
17 | 11 14 19 10 11 12 5 16 5 8 29 4 | 20 29 31 24 28 29 25 27 25 30 19 26
18E | 11 9 9 10 9 19 4 12 7 8 17 4 | 15 16 23 22 15 28 18 22 16 23 22 17
19 | 25 31 11 9 13 8 6 11 8 10 28 6 | 30 29 23 21 22 20 19 21 21 20 22 18
20E | 8 12 9 7 8 16 4 11 4 8 21 4 | 22 25 22 22 26 24 21 24 23 24 29 23
21 | 11 10 13 21 8 11 5 14 5 9 28 4 | 17 19 31 25 17 30 18 28 19 24 16 21
22E | 8 10 10 8 6 12 3 10 4 8 15 3 | 18 19 24 20 18 26 16 24 20 21 18 19
23 | 8 12 16 9 13 15 5 18 8 12 17 5 | 25 28 31 22 20 26 22 29 24 25 22 22
X24 | 17 6 --- 22 --- --- 22 --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- --- 1
25E | 13 9 25 8 8 13 6 15 6 7 10 5 | 27 34 41 31 31 33 32 34 33 33 31 30
26 | 10 9 12 6 9 12 5 8 6 10 9 3 | 18 16 26 20 19 23 19 21 22 22 23 19
X27 | 44 6 --- --- --- --- 194 --- --- --- --- 0 | 88 107 --- --- --- --- 160 --- --- --- --- 107
28 | 9 10 14 6 9 16 4 9 5 9 12 4 | 21 21 31 24 22 40 23 26 24 31 27 24
29 | 8 9 18 10 10 10 7 15 7 11 27 4 | 18 18 27 22 19 21 21 21 22 23 21 18
30E | 15 13 12 7 11 14 5 13 7 12 21 4 | 23 25 24 23 29 22 23 23 22 24 23 20
31 | 10 13 14 7 12 15 3 16 5 9 15 4 | 14 17 26 17 20 30 17 25 17 25 16 18
32E | 14 18 26 9 10 15 7 18 9 10 21 6 | 34 34 32 30 36 26 30 33 31 25 26 28
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 11 12 15 9 10 13 5 14 6 10 19 |T 23 26 29 23 23 28 26 27 23 26 23 24
WRMS | 11 12 15 9 10 12 5 13 6 9 17 |NE 21 22 28 22 21 27 21 25 22 24 22 21
MEDI | 10 10 13 8 9 13 5 13 6 9 17 |MD 21 22 28 22 22 29 21 26 22 24 22 21
Table 3.1713.3 GPS week: 1713 Day: 3 MJD: 56238.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 9 12 15 9 12 13 3 14 6 10 15 4 | 35 36 46 43 35 50 42 50 41 38 39 40
2 | 10 8 18 5 14 12 3 15 9 14 23 4 | 20 18 26 19 23 21 16 23 18 27 18 18
3 | 9 6 10 4 11 17 4 11 6 10 20 3 | 26 26 36 29 32 35 28 37 31 31 28 30
4 | 9 7 10 6 12 11 6 9 8 8 28 3 | 32 34 38 37 36 37 33 33 35 39 41 34
5E | 7 5 17 7 9 12 3 20 6 11 11 4 | 17 17 27 19 19 23 16 24 19 22 18 16
6 | 8 6 10 3 9 13 4 9 8 10 15 3 | 25 26 34 31 32 35 27 35 31 32 28 30
7 | 7 8 19 6 13 17 3 16 9 12 13 4 | 17 21 26 18 21 26 15 23 16 21 15 16
8 | 11 8 14 5 6 13 5 10 5 7 13 3 | 15 19 24 17 15 18 16 23 18 20 21 16
9 | 7 6 10 6 7 9 6 12 7 10 14 3 | 18 17 23 19 16 19 16 20 17 23 18 16
10E | 12 12 20 5 12 16 6 14 7 12 15 4 | 54 55 72 59 51 69 57 69 56 64 52 59
11 | 11 7 17 5 9 18 4 14 5 13 21 4 | 30 32 38 32 31 38 30 36 31 28 26 30
12 | 20 10 21 5 9 14 5 26 11 14 18 5 | 42 54 54 47 56 52 49 53 50 54 48 50
13 | 9 9 15 6 11 21 5 14 7 13 15 4 | 21 24 32 21 24 37 20 30 20 24 16 21
14 | 7 10 15 7 10 16 3 15 10 12 15 4 | 19 22 30 23 21 33 21 31 24 28 18 22
15 | 10 7 13 6 8 15 7 18 7 12 18 3 | 23 23 34 29 26 35 25 32 26 29 26 25
16 | 7 8 19 7 13 17 4 13 6 10 19 4 | 18 17 28 19 24 30 18 23 23 23 17 19
17 | 10 9 16 6 14 8 4 17 7 10 27 4 | 31 29 37 32 35 36 31 35 31 38 25 31
18E | 11 8 14 8 10 21 6 14 5 8 12 3 | 26 29 35 32 31 31 27 37 28 34 31 29
19 | 10 7 15 5 9 11 5 14 8 11 27 3 | 23 26 29 23 29 27 21 29 23 19 21 22
20E | 8 9 11 7 10 17 4 9 6 9 14 3 | 22 24 28 21 26 26 22 27 25 23 27 22
21 | 10 9 14 5 14 9 5 15 8 12 28 4 | 24 26 34 26 27 31 22 34 24 31 15 25
22E | 9 8 11 5 8 13 4 11 6 9 11 3 | 18 21 24 22 20 23 19 25 18 24 20 19
23 | 10 10 16 7 13 17 4 16 6 12 18 4 | 21 25 31 20 20 26 18 29 19 24 17 19
X24 | 33 11 --- --- --- --- --- --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- --- 1
25E | 10 10 26 5 15 11 5 16 9 15 11 4 | 33 35 38 32 32 34 35 39 37 34 33 32
26 | 8 7 13 7 9 12 5 11 5 7 10 3 | 18 17 26 21 19 25 18 23 19 21 19 17
X27E | 57 11 --- --- --- --- 66 --- --- --- --- 0 | 68 93 --- --- --- --- 115 --- --- --- --- 95
28 | 11 9 13 4 8 16 4 9 6 8 14 3 | 24 23 33 25 25 40 24 29 27 35 24 26
29 | 7 10 17 5 9 12 6 16 6 14 25 4 | 22 27 33 22 30 25 25 30 28 26 23 24
30E | 17 12 14 5 10 12 6 14 8 11 16 3 | 23 25 26 23 29 26 20 23 25 25 24 22
31 | 13 11 14 6 12 16 4 16 8 11 15 4 | 15 15 27 18 22 32 17 29 20 24 19 18
32E | 17 19 19 7 13 19 6 18 9 11 22 5 | 41 42 40 38 43 38 40 44 40 39 31 38
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 11 9 16 6 11 15 5 15 7 11 18 |T 25 28 33 27 28 32 28 32 27 30 25 27
WRMS | 10 9 16 6 11 15 5 14 7 10 18 |NE 22 24 31 25 26 30 23 30 24 27 22 23
MEDI | 10 9 15 6 10 13 5 14 7 11 15 |MD 23 25 32 23 26 31 22 30 25 27 23 22
Table 3.1713.4 GPS week: 1713 Day: 4 MJD: 56239.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 11 16 13 8 10 13 4 12 6 10 12 4 | 25 30 37 42 34 44 36 40 33 38 34 37
2 | 13 8 15 8 11 11 3 14 7 13 24 4 | 14 17 24 20 19 14 18 23 17 27 14 18
3 | 11 7 10 5 11 15 3 10 8 11 18 3 | 19 18 31 22 27 26 23 28 20 31 22 23
4 | 14 8 8 5 10 11 5 8 6 12 27 3 | 24 25 33 34 34 34 29 31 28 32 35 31
5E | 13 8 18 4 11 16 4 17 6 15 12 4 | 12 12 22 16 17 16 13 21 12 27 13 14
6 | 11 8 11 3 10 12 4 12 5 12 16 3 | 19 20 31 25 27 32 24 29 24 32 24 25
7 | 9 10 17 4 11 15 3 14 5 12 15 3 | 22 22 29 25 22 29 22 25 20 30 20 23
8 | 11 8 11 4 7 13 5 11 5 11 12 3 | 15 18 24 23 19 19 20 23 16 28 18 19
9 | 10 10 12 6 9 9 5 13 6 10 15 3 | 12 15 20 19 16 15 17 16 15 25 14 16
10E | 14 14 22 7 10 14 6 16 7 15 21 4 | 49 49 67 56 50 64 53 66 51 62 53 56
11 | 8 9 15 5 11 15 4 12 6 13 15 3 | 21 23 29 29 29 31 26 28 25 28 19 26
12E | 15 10 20 9 10 14 5 24 9 13 16 5 | 23 28 32 27 27 29 25 30 27 33 23 25
13 | 9 11 14 7 9 19 3 13 7 12 16 4 | 20 19 32 25 21 38 22 29 21 30 19 23
14 | 13 10 15 6 12 15 6 13 5 10 17 3 | 21 28 33 32 20 34 26 30 24 36 22 28
15 | 10 8 16 7 8 13 6 20 6 8 17 4 | 15 15 25 21 17 26 19 24 16 28 18 18
16 | 12 11 16 5 10 17 5 13 8 15 16 4 | 32 31 39 35 36 41 35 36 34 41 36 35
17 | 16 15 17 6 13 11 4 16 5 10 26 4 | 23 27 32 30 34 32 29 31 28 34 24 29
18E | 12 7 13 6 10 19 4 13 6 14 17 4 | 26 29 27 31 26 25 27 29 24 35 25 28
19 | 12 11 12 3 11 10 4 13 6 11 25 3 | 18 21 25 20 25 18 21 24 18 25 18 20
20E | 12 13 12 5 11 14 6 10 6 12 12 3 | 29 29 35 31 29 31 30 28 27 35 29 29
21 | 11 6 15 6 10 9 4 14 5 13 28 3 | 21 21 35 30 24 34 26 33 25 31 17 28
22E | 12 9 13 6 9 15 4 11 5 11 11 3 | 24 25 30 32 22 30 27 30 25 35 27 28
23 | 13 14 15 6 13 14 4 14 7 15 17 4 | 18 18 28 20 18 26 19 24 17 25 17 19
X24E | 129 9 --- --- --- --- 45 --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- --- 1
25E | 12 11 25 7 9 12 4 17 6 15 13 4 | 23 24 30 30 26 26 26 31 26 34 26 26
26 | 6 12 12 5 11 12 5 11 6 11 13 3 | 12 13 21 15 19 16 14 17 15 26 14 14
X27E | 43 9 --- --- --- --- 105 --- --- --- --- 0 | 41 50 --- --- --- --- 116 --- --- --- --- 53
28 | 12 9 17 5 9 26 5 12 6 13 11 4 | 23 25 35 33 31 51 30 32 28 34 29 31
29 | 10 15 18 6 9 13 6 17 7 15 26 4 | 24 28 31 26 23 27 26 27 25 31 20 25
30E | 16 14 13 6 10 14 7 14 6 17 18 4 | 19 22 23 23 23 22 20 22 20 22 19 20
31 | 12 16 18 6 12 19 4 18 8 15 16 5 | 18 23 30 24 17 35 22 31 21 30 22 23
32E | 22 21 21 6 11 20 6 16 11 11 15 5 | 40 41 40 41 40 39 39 37 39 43 35 39
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 12 16 6 10 15 5 14 7 13 18 |T 21 24 31 27 25 30 28 29 24 32 23 25
WRMS | 11 11 16 6 10 14 5 14 6 11 18 |NE 19 21 28 25 23 27 23 27 21 29 20 23
MEDI | 12 10 15 6 10 14 4 13 6 12 16 |MD 21 23 30 26 24 29 26 29 24 31 22 25
Table 3.1713.5 GPS week: 1713 Day: 5 MJD: 56240.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 9 14 14 4 15 14 4 14 6 11 18 4 | 35 38 41 41 34 44 40 45 40 42 31 38
2 | 8 6 15 6 17 11 2 14 9 8 25 4 | 18 20 24 22 17 21 19 24 17 22 19 18
3 | 8 8 11 6 18 16 5 9 11 13 16 4 | 21 27 30 29 23 28 30 30 29 35 23 27
4 | 8 10 8 5 12 13 5 9 8 7 26 3 | 24 27 31 30 29 33 30 31 29 33 37 29
5E | 7 12 18 7 16 16 4 24 7 11 10 5 | 16 18 21 22 15 20 17 27 11 19 13 13
6 | 9 9 11 5 17 14 5 9 9 15 12 4 | 23 28 29 32 25 32 31 32 29 36 25 28
7 | 14 16 18 5 19 20 6 15 7 10 14 4 | 20 23 27 24 22 30 22 26 20 24 19 19
8 | 12 12 12 6 13 18 8 11 8 11 14 4 | 20 26 26 25 20 26 24 28 22 29 22 22
9 | 6 9 14 4 14 11 4 12 9 9 19 3 | 19 22 20 22 14 19 20 20 19 23 17 17
10E | 12 13 25 6 16 16 6 14 8 10 23 4 | 47 50 67 54 50 59 53 63 51 58 51 54
11 | 7 7 16 5 15 16 3 12 7 14 18 4 | 29 34 30 30 31 31 30 29 29 31 21 27
12E | 13 10 18 7 12 17 5 21 11 11 15 4 | 24 25 31 28 27 28 26 30 27 34 24 26
13 | 10 11 14 7 16 21 6 13 9 9 17 4 | 23 28 32 28 25 36 26 31 25 29 22 25
14 | 8 11 15 7 13 16 5 15 9 11 15 4 | 17 21 28 24 18 31 20 26 19 26 16 20
15 | 12 15 17 7 8 13 10 18 10 9 22 4 | 16 21 23 24 17 27 21 24 18 22 19 17
16E | 5 12 19 6 21 16 4 14 6 10 35 4 | 28 36 36 34 21 34 31 33 25 37 18 29
17 | 10 9 17 5 16 10 3 16 6 11 26 4 | 25 31 30 29 27 30 28 33 26 36 22 28
18E | 9 13 10 6 15 19 3 14 6 9 10 4 | 15 20 25 26 21 27 21 25 20 29 21 21
19 | 17 18 14 4 18 11 6 10 10 13 25 4 | 22 24 24 25 26 20 24 23 22 26 20 20
20E | 9 11 10 4 11 14 4 9 7 11 16 3 | 26 28 26 27 28 29 25 26 23 27 25 23
21 | 6 8 17 7 14 15 5 16 9 14 27 4 | 20 22 36 28 17 33 22 33 20 29 15 24
22E | 7 11 8 7 12 16 5 12 6 9 11 3 | 17 20 24 24 21 23 19 24 18 26 20 19
23 | 9 12 16 7 20 19 7 17 8 9 21 4 | 24 31 31 28 22 27 25 31 24 27 20 23
X24E | 16 8 --- --- --- --- --- --- --- --- --- 0 | 1 --- --- --- --- --- --- --- --- --- --- 1
25E | 7 15 24 6 9 10 5 20 8 8 13 4 | 19 23 23 23 16 23 20 28 17 24 18 17
26 | 7 8 14 5 10 11 5 12 8 11 13 3 | 21 25 25 27 17 23 23 25 18 22 19 19
X27E | 57 8 --- --- --- --- 72 --- --- --- --- 0 | 35 68 --- --- --- --- 47 --- --- --- --- 68
28E | 23 7 22 6 13 21 6 10 9 10 8 4 | 48 49 57 50 52 53 49 51 52 55 52 51
29 | 8 14 19 5 17 12 6 16 8 10 22 4 | 22 29 26 27 22 24 24 28 22 28 18 22
30E | 18 16 18 6 19 18 3 15 9 9 14 4 | 24 29 30 31 30 29 28 27 27 27 24 25
31 | 13 14 17 9 18 16 5 17 8 8 21 4 | 14 16 29 23 16 29 18 25 13 25 17 17
32E | 17 20 17 9 14 19 7 18 9 10 18 5 | 44 47 42 46 49 40 43 41 44 40 38 42
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 11 12 16 6 15 16 5 15 8 11 19 |T 23 29 30 29 25 30 27 30 25 30 23 25
WRMS | 10 12 16 6 15 15 5 14 8 9 17 |NE 21 25 28 27 22 28 25 28 23 28 21 23
MEDI | 9 11 16 6 15 16 5 14 8 10 17 |MD 22 27 29 27 22 29 25 28 22 28 20 23
Table 3.1713.6 GPS week: 1713 Day: 6 MJD: 56241.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod cof emr esa gfz grg igr jpl mit ngs sio IGS | cod cof emr esa gfz grg igr jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
1 | 13 13 13 8 10 14 4 14 6 11 14 4 | 42 44 52 52 47 56 49 52 48 49 44 48
2 | 9 8 14 7 11 14 3 16 9 11 27 4 | 17 16 23 16 16 19 14 24 15 17 22 15
3 | 6 5 12 6 9 16 4 12 6 10 18 3 | 21 21 28 22 22 30 21 29 21 30 22 22
4 | 9 9 7 5 10 13 4 10 7 9 24 3 | 33 33 38 35 38 41 36 37 35 36 42 35
5E | 8 10 20 6 13 14 4 24 8 15 12 4 | 14 17 26 11 18 17 12 25 16 20 17 12
6 | 10 7 10 4 11 15 4 12 6 9 14 3 | 25 24 31 26 26 36 26 32 26 33 25 26
7 | 7 10 16 5 10 19 4 17 9 10 16 4 | 19 22 23 16 20 27 15 23 17 19 14 16
8 | 13 8 10 5 5 16 6 12 7 9 11 3 | 15 17 20 15 14 20 13 21 13 19 14 13
9 | 11 10 12 6 10 14 5 10 7 13 17 3 | 25 24 24 20 18 21 19 25 18 23 19 17
10E | 16 13 21 6 12 18 8 16 9 13 25 4 | 56 57 75 63 54 68 59 74 59 63 58 61
11 | 8 7 15 5 7 18 3 15 6 14 19 3 | 33 35 38 35 35 41 35 33 34 36 30 33
12E | 17 8 21 7 9 24 6 23 8 16 20 5 | 27 26 35 26 28 36 24 32 24 31 25 25
13 | 10 14 14 7 11 22 5 14 9 9 21 4 | 22 24 29 21 21 35 18 29 19 22 16 20
14 | 10 8 15 6 12 14 4 14 10 11 17 4 | 19 19 30 21 20 34 20 30 23 26 17 21
15 | 11 7 17 6 8 19 7 21 8 14 22 4 | 25 25 37 24 24 34 24 37 26 37 26 26
16E | 7 9 17 5 14 17 4 18 7 11 16 4 | 21 20 30 23 28 32 23 28 23 25 24 22
17 | 12 12 16 6 11 9 5 17 7 11 27 4 | 32 34 39 32 37 36 34 35 33 36 28 33
18E | 11 10 12 6 13 19 4 15 5 8 9 3 | 17 18 23 19 21 27 18 26 18 22 19 18
19 | 7 9 16 4 11 11 4 16 7 7 27 3 | 24 26 27 25 28 28 24 24 25 27 26 24
20E | 11 9 11 4 12 13 5 9 6 11 15 3 | 32 30 34 25 31 31 27 31 30 25 31 26
21 | 10 7 15 5 13 8 3 19 8 10 28 3 | 24 25 33 24 25 32 23 35 23 28 20 24
22E | 10 11 11 5 10 14 4 12 7 12 11 3 | 27 25 28 23 21 26 23 27 22 30 26 22
23 | 13 11 16 6 14 20 6 17 8 9 22 4 | 23 25 30 19 18 27 19 28 21 22 17 18
X24E | 15 12 --- 8 --- --- 14 --- 10 --- --- 7 | 1 --- --- --- --- --- --- --- 6 --- --- 1
25E | 11 13 24 6 10 13 3 17 9 11 14 4 | 33 32 38 32 34 32 31 38 32 31 34 31
26 | 10 7 15 9 9 12 5 10 6 11 13 3 | 26 26 35 27 27 30 25 34 27 28 28 25
X27E | 23 11 --- --- --- --- 68 --- --- --- --- 0 | 62 70 --- --- --- --- 57 --- --- --- --- 69
28E | 10 6 18 4 7 17 6 10 6 5 16 3 | 45 45 53 48 52 55 47 48 50 49 48 49
29 | 9 12 21 6 12 15 4 19 6 11 26 4 | 35 38 37 29 36 31 32 30 33 35 29 31
30E | 15 15 17 5 14 16 6 15 10 7 19 4 | 25 26 31 21 28 25 21 29 23 19 27 21
31 | 12 10 18 8 16 19 4 20 10 13 18 5 | 18 21 31 22 20 35 19 28 19 25 18 19
32E | 26 20 19 8 12 24 4 15 8 12 14 5 | 57 52 46 45 52 47 48 46 48 45 45 45
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 10 16 6 11 16 5 16 8 11 19 |T 27 29 34 27 28 33 27 33 26 30 27 27
WRMS | 10 10 16 6 11 15 5 15 7 9 18 |NE 25 26 31 25 25 32 24 30 25 28 24 24
MEDI | 10 10 15 6 11 15 4 15 7 11 17 |MD 25 25 31 24 26 32 24 30 23 28 25 24
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 4.1713 GPS week: 1713 MJD: 56235.0-56241.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 |U 5 5 14 |U 7 9 26 |U 8 7 17 |
cof | cof 2966 |U 5 5 14 |U 7 9 26 |U 8 6 16 |
emr | emr 2868 | 11 13 18 |U 8 9 27 | 9 9 21 |
esa | esa 2921 | 6 6 14 |U 7 10 27 | 8 8 19 |
gfz | gfz 2867 |U 7 5 14 |U 7 9 29 |U 10 10 21 |
grg | grg 2879 |U 13 14 21 |U 9 11 33 | 10 13 27 |
igr | igr 2906 | 6 5 14 | 7 9 27 | 8 8 19 |
igs | igs 2886 | 11 14 16 | 8 9 27 | 9 10 19 |
jpl | jpl 2867 | 11 14 19 |U 9 12 29 | 8 9 19 |
mit | mit 2907 | 15 16 23 |U 8 10 27 |U 9 10 21 |
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 5.1713.0 GPS week: 1713 Day: 0 MJD: 56235.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 5 4 16 | 8 9 31 | 9 8 21 |
cof | cof 3024 | 5 4 16 | 8 9 31 | 8 8 21 |
emr | emr 2868 | 8 7 18 | 9 12 31 | 11 13 24 |
esa | esa 2976 | 5 4 18 | 8 11 33 | 9 9 24 |
gfz | gfz 2869 | 6 4 17 | 8 10 35 | 8 9 24 |
grg | grg 2880 | 7 7 18 | 9 13 42 | 14 21 43 |
igr | igr 2971 | 6 3 18 | 8 10 32 | 9 9 23 |
igs | igs 2968 | 7 7 17 | 8 10 33 | 10 12 23 |
jpl | jpl 2868 | 7 7 19 | 8 11 30 | 9 11 24 |
mit | mit 2976 | 10 8 20 | 9 12 31 | 10 12 21 |
Table 5.1713.1 GPS week: 1713 Day: 1 MJD: 56236.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2930 | 5 5 14 | 8 9 23 | 9 5 15 |
cof | cof 2930 | 6 5 14 | 8 9 24 | 9 5 15 |
emr | emr 2868 | 9 8 17 | 10 10 27 | 8 8 20 |
esa | esa 2880 | 4 5 13 | 8 8 24 | 7 6 18 |
gfz | gfz 2867 | 5 6 10 | 8 7 24 | 7 7 21 |
grg | grg 2880 | 8 8 15 | 10 11 35 | 10 12 23 |
igr | igr 2852 | 5 5 12 | 8 8 25 | 6 5 16 |
igs | igs 2854 | 9 10 14 | 9 8 28 | 11 9 25 |
jpl | jpl 2867 | 8 9 17 | 12 14 33 | 8 7 18 |
mit | mit 2880 | 17 18 59 | 8 11 31 | 12 11 32 |
Table 5.1713.2 GPS week: 1713 Day: 2 MJD: 56237.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2914 | 5 5 15 | 6 9 19 | 8 7 18 |
cof | cof 2914 | 5 5 14 | 6 10 19 | 8 7 18 |
emr | emr 2868 | 10 13 17 | 7 8 22 | 9 11 25 |
esa | esa 2976 | 5 6 12 | 6 9 22 | 8 10 21 |
gfz | gfz 2867 | 8 6 16 | 6 7 19 | 10 11 20 |
grg | grg 2879 | 12 16 19 | 7 9 30 | 9 13 20 |
igr | igr 2924 | 6 5 15 | 6 9 18 | 8 10 20 |
igs | igs 2873 | 10 14 14 | 6 8 20 | 9 12 19 |
jpl | jpl 2868 | 10 14 19 | 8 11 20 | 9 11 20 |
mit | mit 2880 | 15 16 16 | 6 8 20 | 9 13 21 |
Table 5.1713.3 GPS week: 1713 Day: 3 MJD: 56238.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2997 | 4 6 12 | 4 6 21 | 9 6 18 |
cof | cof 2997 | 3 6 11 | 5 6 22 | 9 6 17 |
emr | emr 2868 | 14 18 17 | 5 7 21 | 12 8 24 |
esa | esa 2880 | 5 8 12 | 5 7 24 | 9 8 21 |
gfz | gfz 2867 | 6 4 13 | 6 7 29 | 12 9 20 |
grg | grg 2880 | 17 19 19 | 6 8 27 | 9 14 30 |
igr | igr 2880 | 5 6 11 | 5 7 24 | 8 7 22 |
igs | igs 2869 | 15 19 15 | 5 6 22 | 9 9 21 |
jpl | jpl 2868 | 14 20 20 | 8 9 29 | 11 8 24 |
mit | mit 2880 | 17 21 15 | 7 7 23 | 10 11 23 |
Table 5.1713.4 GPS week: 1713 Day: 4 MJD: 56239.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2943 | 7 4 12 | 10 10 40 | 8 7 16 |
cof | cof 2943 | 7 3 11 | 10 9 38 | 8 6 16 |
emr | emr 2868 | 16 17 19 | 10 10 32 | 8 10 21 |
esa | esa 2880 | 8 4 12 | 10 10 33 | 8 9 17 |
gfz | gfz 2868 | 8 4 13 | 9 10 34 | 13 13 24 |
grg | grg 2880 | 15 16 23 | 11 10 34 | 9 11 20 |
igr | igr 2879 | 8 4 14 | 10 9 33 | 8 8 18 |
igs | igs 2847 | 15 17 14 | 10 9 31 | 7 8 14 |
jpl | jpl 2868 | 15 17 17 | 9 9 30 | 8 8 16 |
mit | mit 2880 | 16 14 15 | 10 10 33 | 9 12 16 |
Table 5.1713.5 GPS week: 1713 Day: 5 MJD: 56240.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2926 | 4 5 14 | 8 12 27 | 7 6 16 |
cof | cof 2926 | 4 5 13 | 8 12 26 | 8 7 16 |
emr | emr 2868 | 10 13 17 | 9 10 26 | 7 7 17 |
esa | esa 2880 | 6 7 14 | 8 13 31 | 7 8 15 |
gfz | gfz 2869 | 6 6 13 | 8 10 36 | 10 12 21 |
grg | grg 2879 | 14 20 28 | 10 13 33 | 9 9 23 |
igr | igr 2878 | 5 6 13 | 8 12 31 | 6 7 17 |
igs | igs 2849 | 13 17 17 | 9 11 30 | 6 7 15 |
jpl | jpl 2868 | 10 15 19 | 13 17 42 | 7 8 17 |
mit | mit 2880 | 15 15 17 | 9 11 30 | 6 6 14 |
Table 5.1713.6 GPS week: 1713 Day: 6 MJD: 56241.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 5 5 17 | 7 11 21 | 8 7 13 |
cof | cof 3031 | 5 5 17 | 7 11 21 | 8 6 14 |
emr | emr 2868 | 12 12 25 | 7 9 27 | 9 9 18 |
esa | esa 2976 | 7 7 18 | 7 10 21 | 9 8 14 |
gfz | gfz 2866 | 8 7 18 | 7 10 26 | 12 10 18 |
grg | grg 2880 | 14 11 25 | 7 12 33 | 11 15 29 |
igr | igr 2963 | 6 8 18 | 6 10 23 | 9 8 16 |
igs | igs 2943 | 12 14 22 | 6 11 24 | 9 10 18 |
jpl | jpl 2868 | 11 13 22 | 6 11 22 | 9 10 18 |
mit | mit 2976 | 16 16 22 | 7 11 23 | 9 8 18 |
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 6.1713 GPS week: 1713 MJD: 56235.500-56241.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 27 -44 -89 187 3 | -3 10
| 38 25 161 114 8 | 1
cof uuuuu | -22 -49 48 -98 7 | -7 13
| 20 22 52 126 5 | 2
emr uuuuu | 15 -1 33 -112 5 | 24 28
| 14 15 48 94 9 | 3
esa uuuuu | -53 -27 28 -118 1 | -5 13
| 34 27 74 58 7 | 1
gfz uuuuu | 74 49 -25 10 -2 | 1 10
| 39 28 75 66 5 | 2
grg uuuux | -7 -44 35 125 12 | -11 32
| 37 12 48 124 11 | 5
igr xxxxx | -25 3 -9 85 -2 | -2 11
| 27 10 57 63 6 | 2
irf xxxxx | 14 0 7 7 3 | -3 8
| 18 4 11 36 2 | 1
jpl uuuuu | -3 -18 -73 59 -13 | 34 37
| 30 22 118 96 13 | 4
mit uuuuu | 38 26 -62 50 1 | -4 8
| 16 19 95 67 10 | 2
ngs uuuuu | -3 46 26 181 -4 | 4 10
| 36 43 102 111 4 | 2
sio xxxxx | 374 -150 59 107 0 | 30 32
| 87 58 99 33 9 | 3
Table 7.1713.0 GPS week: 1713 Day: 0 MJD: 56235.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 19 -74 17 40 0 | -3 9
cof uuuuu | -28 -46 46 75 0 | -8 11
emr uuuuu | 8 11 39 -15 6 | 21 26
esa uuuuu | -47 19 -58 -98 -3 | -4 10
gfz uuuuu | 45 24 51 -40 -6 | 4 8
grg uuuux | -20 -45 28 -47 22 | -5 37
igr xxxxx | -53 -13 7 8 -7 | 0 8
irf xxxxx | 0 0 2 -4 2 | -1 7
jpl uuuuu | 16 -44 99 -50 -1 | 39 40
mit uuuuu | 21 -4 -2 79 4 | -1 7
ngs uuuuu | 27 44 -82 48 3 | 7 9
sio xxxxx | 201 -135 83 116 8 | 25 29
Table 7.1713.1 GPS week: 1713 Day: 1 MJD: 56236.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -1 -37 55 290 13 | -3 9
cof uuuuu | -5 -62 73 30 10 | -8 12
emr uuuuu | 17 -24 114 0 15 | 23 26
esa uuuuu | -27 -70 54 -55 7 | -4 11
gfz uuuuu | 52 72 -125 4 3 | 3 9
grg uuuux | -36 -34 -5 37 5 | -4 37
igr xxxxx | -49 -2 26 13 1 | -1 10
irf xxxxx | 8 -3 7 -6 1 | -2 8
jpl uuuuu | -43 1 -116 21 -6 | 38 39
mit uuuuu | 23 27 -47 -3 -6 | -2 8
ngs uuuuu | -2 96 56 50 -6 | 6 9
sio xxxxx | 352 -192 206 140 11 | 28 30
Table 7.1713.2 GPS week: 1713 Day: 2 MJD: 56237.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 43 -58 -227 62 2 | -2 9
cof uuuuu | -16 -57 26 -205 7 | -8 12
emr uuuuu | -5 3 -14 -268 -8 | 22 26
esa xxxxx | -17 -19 0 -122 -3 | -5 11
gfz uuuuu | 49 85 -52 42 -1 | 1 7
grg uuuux | -46 -51 7 29 22 | -9 34
igr xxxxx | -42 -5 -24 117 -1 | -2 9
irf xxxxx | -2 -7 12 -5 3 | -3 7
jpl uuuuu | -20 -35 -117 -15 -20 | 37 38
mit uuuuu | 31 23 19 70 4 | -4 8
ngs uuuuu | -46 -26 84 177 -5 | 4 8
sio xxxxx | 457 -192 -38 78 -2 | 30 32
Table 7.1713.3 GPS week: 1713 Day: 3 MJD: 56238.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 10 -15 -79 265 6 | -4 11
cof uuuuu | -50 -63 27 -17 12 | -10 13
emr uuuuu | 39 1 15 -145 18 | 20 24
esa uuuuu | -57 -36 115 -124 12 | -8 13
gfz uuuuu | 63 74 -121 -35 7 | -1 9
grg uuuux | -13 -54 15 131 2 | -15 29
igr xxxxx | -14 2 93 68 4 | -4 11
irf xxxxx | 19 1 5 -24 0 | -5 9
jpl uuuuu | 30 -29 -26 6 0 | 32 35
mit uuuuu | 62 29 -181 37 -16 | -6 9
ngs uuuuu | -28 85 160 268 -5 | 2 10
sio xxxxx | 411 -190 48 62 6 | 30 32
Table 7.1713.4 GPS week: 1713 Day: 4 MJD: 56239.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -16 -67 -351 252 -9 | -2 12
cof uuuuu | -48 -29 -22 -224 7 | -7 14
emr uuuuu | 4 -18 61 -119 5 | 25 30
esa uuuuu | -39 -24 -72 -61 -1 | -5 15
gfz uuuuu | 62 28 40 -39 -5 | 1 11
grg uuuux | -14 -52 -7 184 18 | -15 29
igr xxxxx | -14 16 -74 187 -8 | -3 12
irf xxxxx | 4 5 28 -16 2 | -4 10
jpl uuuuu | -37 -20 25 168 -21 | 34 37
mit uuuuu | 30 25 64 -48 3 | -6 9
ngs uuuuu | 44 69 -59 356 -2 | 4 11
sio xxxxx | 454 -31 -93 128 -9 | 33 35
Table 7.1713.5 GPS week: 1713 Day: 5 MJD: 56240.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 102 -8 97 102 -5 | -3 12
cof uuuuu | 1 -73 145 -218 0 | -6 14
emr uuuuu | 23 17 -27 -169 -2 | 26 31
esa uuuuu | -120 -35 107 -229 -7 | -6 15
gfz uuuuu | 157 15 16 144 -8 | 1 11
grg uuuux | 65 -50 108 264 -4 | -14 30
igr xxxxx | 24 15 -29 112 -10 | -4 12
irf xxxxx | 50 2 -5 82 7 | -4 9
jpl uuuuu | 22 22 -111 207 -36 | 31 34
mit uuuuu | 53 62 -165 165 17 | -7 9
ngs uuuuu | 24 43 -91 165 -10 | 3 11
sio xxxxx | 356 -140 116 85 -12 | 32 34
Table 7.1713.6 GPS week: 1713 Day: 6 MJD: 56241.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 35 -51 -132 298 10 | -2 11
cof uuuuu | -11 -11 39 -126 11 | -4 13
emr uuuuu | 17 4 40 -70 0 | 29 33
esa uuuuu | -64 -24 52 -139 2 | -5 14
gfz uuuuu | 91 43 19 -6 -6 | 0 11
grg uuuux | 14 -19 99 276 18 | -15 30
igr xxxxx | -27 6 -64 89 5 | -4 12
irf xxxxx | 19 3 2 22 3 | -2 9
jpl uuuuu | 9 -23 -266 79 -9 | 29 34
mit uuuuu | 45 22 -120 49 0 | -4 9
ngs uuuuu | -40 12 114 204 -2 | 4 11
sio xxxxx | 389 -171 92 144 -4 | 32 34
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