[IGSREPORT-21393] Wk 1715 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat Dec 8 08:14:07 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1715 (Nov 18, 2012 - Nov 24, 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:
igs1715[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1715[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1715[0-6].cls IGS GPS clock combination summary report.
igs17157.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17157.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 KOUC KOUC MAC1
0 | EMR | 32 32 HERS WROC HERS WROC
0 | ESA | 32 NTUS
0 | GFZ | 30 BOGT HARB MATE
0 | GRG | 30 30 MAC1 USNO MAL2 NICO NTUS OHI2 RAMO USNO
0 | JPL | 24 32
0 | MIT | 29 30 18 29 30 NICO NTUS NICO NTUS
1 | COF | 30 30 HERT HNPT KOUC WROC HERT HNPT KOUC WROC
1 | ESA | 30 30 ONSA UNSA
1 | GFZ | 30 BOGT KARR METS PIMO YAKT
1 | GRG | NICO LHAZ NICO
1 | JPL | 24 PALM
1 | MIT | 21 30 21 30 GMAS JPLM
2 | COD | SOFI SOFI
2 | COF | 6 6 MOBS SOFI WROC MOBS REUN SOFI WROC
2 | EMR | TLSE
2 | ESA | 30 TRO1
2 | GFZ | 30 BOGT GRAS HARB LHAZ YAKT
2 | GRG | NICO SYOG WROC YELL NICO SYOG WROC YELL
2 | JPL | 24
2 | MIT | 30 30 MAC1 MAC1
3 | COF | KOUC KOUC YELL
3 | EMR | YELL HERS MATE
3 | GFZ | BOGT NRMD RIOP STJO YELL
3 | GRG | LPGS MATE LPGS MATE NOVM
3 | JPL | 9 24
3 | MIT | 23 30 23 30 TLSE JPLM TLSE
4 | COD | YELL MCM4 YELL
4 | COF | 4 4 KOUC YELL HARB KOUC MCM4 YELL
4 | EMR | WUHN
4 | ESA | 4
4 | GFZ | 4 30 ABPO BOGT LHAZ SEY1 SUTM
4 | GRG | USNO NOVM SCOR USNO WIND
4 | JPL | 24
4 | MIT | 30 4 30 NYAL NICO NYAL
5 | COD | MCM4
5 | COF | MCM4 NRMD SUTM
5 | ESA | BOGT POTS
5 | GFZ | 23 NRMD
5 | GRG | NICO LHAZ
5 | JPL | 23 24
5 | MIT | 2 13 23 30 2 13 23 30 TIDB SYOG TIDB
6 | COF | HERT SCH2 SOFI FLRS HERT SCH2 SOFI
6 | EMR | HERS
6 | GFZ | BOGT QAQ1 SOFI YAKT
6 | GRG | SPT0 USNO LHAZ MCM4 SPT0 USNO
6 | JPL | 25
6 | MIT | 12 30 2 12 30 SOFI SOFI USNO
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
2 | COF | ~01:25 | ~ -0.37 ns
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. 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
----+------------+----------
G32 | 2012_11_21 | 2012074
7. 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 | SIO | ALL (high Transformation - See Table 2)
3 | SIO | ALL (high Transformation - See Table 2)
5 | SIO | ALL (high Transformation - See Table 2)
6 | SIO | ALL (high Transformation - See Table 2)
8. 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 G32 | | | | 1 | | | |
9. 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.
10. 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 | -.6 .6 -.8 -44 -9 7 -.18
COF | 0 | -.6 .7 -.6 -41 -6 9 -.25
EMR | 0 | 2.2 10.6 3.5 4 3 3 .01
ESA | 0 | 3.6 4.2 -18.4 95 -263 95 -.09
GFZ | 0 | .3 1.3 -.5 -47 -56 -37 -.13
GRG | 0 | 2.0 2.5 3.9 -16 58 -62 .30
JPL | 0 | 5.9 -1.1 8.8 -56 -19 -52 .04
MIT | 0 | 4.6 6.8 -.4 -1 -7 -20 .17
NGS | 0 | 1.8 .0 -3.2 15 -10 21 .52
SIO | 0 | -.4 5.9 -46.5 211 -275 -32 .23
COD | 1 | -.9 .2 -.8 -49 -4 11 -.19
COF | 1 | -.7 .2 -.5 -48 -9 10 -.25
EMR | 1 | 3.7 4.5 -6.1 4 -1 18 .0
ESA | 1 | .1 4.6 -15.9 118 -209 95 -.02
GFZ | 1 | .1 1.6 -.3 -41 -55 -24 -.23
GRG | 1 | -2.1 3.5 -6.9 -2 44 -57 .09
JPL | 1 | .1 10.4 1.7 -62 -58 -40 -.03
MIT | 1 | 1.0 5.8 .5 1 2 -28 -.05
NGS | 1 | 3.4 11.3 -6.6 79 -18 49 .45
SIO | 1 | 1.9 4.8 -51.1 273 -327 138 .0
COD | 2 | -.9 1.1 -.8 -44 -11 0 -.16
COF | 2 | -1.3 1.3 -1.0 -45 -6 9 -.16
EMR | 2 | -2.0 10.4 5.0 -5 13 4 -.01
ESA | 2 | -3.0 3.2 -10.8 100 -129 122 .02
GFZ | 2 | .0 1.8 -.1 -35 -36 -23 -.17
GRG | 2 | -6.9 2.5 -1.4 -14 33 -15 .15
JPL | 2 | 1.0 12.7 8.8 -83 -49 -71 .21
MIT | 2 | 1.4 6.1 1.5 7 1 -23 -.03
NGS | 2 | .0 7.0 -4.1 45 -4 7 .42
SIO | 2 | -.7 6.9 -29.9 206 -187 42 .04
COD | 3 | -.9 .5 -1.1 -51 -6 -1 -.15
COF | 3 | -.8 .4 -1.3 -47 -7 1 -.14
EMR | 3 | 4.4 9.6 2.0 -1 11 13 -.06
ESA | 3 | .0 2.9 -13.5 122 -181 111 .06
GFZ | 3 | .0 .9 -.5 -46 -63 -30 -.08
GRG | 3 | -4.1 1.6 -.4 -11 48 -43 .35
JPL | 3 | -.7 6.8 9.4 -83 -19 38 .25
MIT | 3 | -2.1 6.2 -3.2 -2 -5 -16 .09
NGS | 3 | 6.0 9.8 -2.3 38 -23 58 .41
SIO | 3 | 1.5 -.3 -49.6 160 -355 149 -.01
COD | 4 | -.4 .2 -1.3 -42 -19 12 -.15
COF | 4 | -.3 .4 -1.4 -32 -17 13 -.16
EMR | 4 | 1.4 10.1 3.9 3 13 6 -.07
ESA | 4 | -.1 -.2 -13.1 73 -191 145 .08
GFZ | 4 | -.4 1.1 -1.0 -43 -60 -31 -.15
GRG | 4 | -6.4 -.2 -3.7 -4 54 -55 .13
JPL | 4 | -6.7 7.2 5.9 -47 11 79 .46
MIT | 4 | 1.2 3.7 3.3 1 6 -38 -.03
NGS | 4 | -1.2 -1.2 -6.5 33 0 -3 .44
SIO | 4 | -1.5 3.6 -34.1 157 -179 77 .05
COD | 5 | -.5 .2 -.8 -54 -14 -11 -.20
COF | 5 | -.4 .2 -.9 -43 -14 -6 -.16
EMR | 5 | .7 6.9 12.3 1 8 5 -.04
ESA | 5 | 3.5 -.4 -8.2 48 -217 119 .09
GFZ | 5 | -.3 .6 -1.0 -40 -53 -44 -.06
GRG | 5 | -5.0 3.7 -1.8 0 49 -38 .34
JPL | 5 | -4.8 6.1 6.9 -80 -31 -24 .38
MIT | 5 | -1.3 7.1 1.8 -10 8 -39 .01
NGS | 5 | -2.3 2.4 -4.0 28 10 -8 .38
SIO | 5 | -1.0 4.1 -40.3 169 -228 77 .07
COD | 6 | -.5 .4 -.7 -47 -10 -3 -.20
COF | 6 | -.7 .6 -.7 -47 -8 -8 -.23
EMR | 6 | 3.6 6.3 7.2 2 14 4 -.03
ESA | 6 | 6.0 2.8 -9.0 98 -239 129 -.11
GFZ | 6 | .1 .6 -.8 -65 -60 -45 -.16
GRG | 6 | -7.2 8.3 -3.1 -12 64 -41 .34
JPL | 6 | .7 3.2 7.2 -49 38 -47 .28
MIT | 6 | -2.1 4.4 -3.3 -6 6 -35 .06
NGS | 6 | 1.8 2.1 -11.8 72 -5 34 .43
SIO | 6 | 3.0 2.0 -22.3 45 -215 -132 .03
11. 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.
12. 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.
13. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center
variations are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed
IGS products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which
caused their RMS clock residuals to be higher during that period than for
the other centres; 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 1.1715.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1715.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 2.1715.[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 3.1715.[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 5.1715.0-6).
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 1715 summary. (Nov 18, 2012 - Nov 24, 2012)
Table 1.1715.a GPS week: 1715 MJD: 56249.000-56255.000
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 261| 0 0 5 116 -63 -3 -.42 10 9 | -1115 -25 35 97
| 0 0 1 20 31 18 .02 | 639 583
cof 258| 0 0 4 102 -59 3 -.39 11 10 | -1061 -28 19 92
| 0 1 2 29 31 14 .04 | 605 588
emr 79| 1 1 3 14 -118 -10 .30 15 15 | 1997 97 13 95
| 1 1 2 16 29 11 .03 | 678 564
esa 175| 1 0 2 -112 189 17 .09 5 5 | -1365 1390 11 104
| 0 0 0 39 80 13 .03 | 1264 1439
gfz 189| -1 0 -3 69 13 -5 -.40 9 9 | 182 -117 20 135
| 0 0 1 53 84 11 .03 | 402 339
grg 129| 0 0 -5 26 -186 -17 .49 16 15 | -74 -49 17 154
| 0 1 1 27 42 19 .03 | 317 293
igr n/a| 0 0 0 20 -66 -43 -.16 4 4 | 10336 -440 16 84
| 0 0 0 15 26 12 .01 | 647 641
jpl 79| 0 0 2 136 -58 5 .38 14 14 | 2422 -19 17 122
| 1 0 2 31 61 30 .04 | 633 557
mit 239| 0 0 -2 13 -85 -9 -.19 8 8 | -320 293 22 204
| 0 0 0 25 35 17 .01 | 263 296
ngs 240| 0 0 -1 -74 -60 -21 .36 12 10 | -1071 -96 1924 3736
| 1 1 1 55 64 8 .05 | 553 452
sio 279| -1 0 2 -334 413 30 -.46 19 19 | --- --- --- ---
| 0 2 1 126 128 95 .02 | --- ---
Table 1.1715.b GPS week : 1715 MJD: 56249.000-56255.000
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 4 4 4 4 3 |
3 | 4 3 3 3 3 3 3 |
4 | 3 4 3 4 3 3 3 |
5 | 4 4 4 4 4 4 4 |
6 | 4 3 4 3 3 3 3 |
7 | 4 5 4 4 4 4 4 |
8 | 4 4 4 4 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 5 4 4 4 4 4 3 |
11 | 3 4 3 4 5 4 3 |
12 | 5 5 4 5 5 4 4 |
13 | 4 4 4 4 4 4 4 |
14 | 4 4 4 3 4 4 4 |
15 | 5 5 4 4 5 4 4 |
16 | 5 5 4 4 4 4 4 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 3 3 4 4 4 |
19 | 4 5 4 4 5 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 3 4 3 3 |
22 | 3 3 3 3 3 3 4 |
23 | 5 5 4 4 5 4 4 |
24 | 4 4 4 4 4 4 4 |
25 | 5 4 4 4 4 4 7 |
26 | 4 4 3 4 3 3 3 |
27 | 0 0 0 0 0 0 0 |
28 | 3 4 4 3 3 3 3 |
29 | 5 4 4 4 4 4 4 |
30 | 6 7 7 7 7 6 6 |
31 | 5 4 4 5 4 4 4 |
32 | 5 6 4 0 4 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 2.1715.0 GPS week: 1715 Day: 0 MJD: 56249.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 262| 0 0 5 118 -96 15 -.42 10 9 | -974 37 40 103
| 4 17 |
cof 261| 1 0 7 103 -62 6 -.45 12 11 | -935 33 26 105
| 43 -42 |
emr 79| 1 3 1 11 -167 8 .26 16 16 | 1517 -269 15 96
| 17 65 |
esa 175| 1 0 2 -106 295 5 .04 6 5 | -2466 2180 11 104
| 50 -62 |
gfz 190| -1 0 -5 -17 -116 6 -.43 14 14 | -88 386 22 141
| -58 -95 |
grg 131| 0 -1 -2 35 -242 -40 .47 15 14 | -15 57 17 154
| 0 11 |
igr n/a| 0 0 0 27 -85 -44 -.17 4 4 | 11091 -793 16 86
| -25 23 |
jpl 80| -3 -1 0 140 -82 12 .30 14 13 | 2157 -407 17 114
| 12 0 |
mit 239| 0 0 -2 -2 -120 6 -.21 8 7 | -352 274 25 206
| -19 1 |
ngs 244| 0 -1 -2 19 -13 -13 .38 12 11 | -926 24 1712 3475
| -110 -46 |
sio 281| -1 -2 0 -445 433 -34 -.45 22 21 | --- --- --- ---
| 210 -239 |
Table 2.1715.1 GPS week: 1715 Day: 1 MJD: 56250.000
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 6 123 -75 2 -.41 10 9 | -909 62 34 89
| 42 1 |
cof 259| 0 0 6 122 -47 10 -.38 11 11 | -875 62 17 83
| 5 -30 |
emr 80| 0 0 0 27 -127 -1 .28 16 16 | 1332 -32 16 107
| -27 31 |
esa 175| 1 0 2 -161 197 -3 .08 6 6 | -2049 1708 12 106
| 60 4 |
gfz 190| -1 -1 -3 104 -51 12 -.42 9 8 | 576 -645 18 137
| -67 -119 |
grg 129| 0 0 -5 29 -177 -33 .48 16 15 | 140 -485 18 143
| 34 -11 |
igr n/a| 0 0 0 19 -56 -31 -.15 4 4 | 10628 -681 16 91
| -15 3 |
jpl 80| -1 0 0 114 -5 4 .39 15 14 | 2047 -306 17 123
| 47 6 |
mit 239| 0 0 -1 68 -94 -2 -.20 10 10 | -143 25 22 204
| -13 -15 |
ngs 239| 0 1 0 -146 15 -23 .32 12 10 | -811 -179 1677 3437
| -42 -13 |
sio 284| -1 -1 2 -471 560 136 -.47 21 19 | --- --- --- ---
| 242 -300 |
Table 2.1715.2 GPS week: 1715 Day: 2 MJD: 56251.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 262| -1 0 5 115 -27 -10 -.42 10 9 | -2360 1134 42 137
| -3 14 |
cof 262| 0 0 6 121 -9 20 -.43 11 11 | -2215 1138 24 117
| 8 -2 |
emr 80| 0 2 2 24 -98 -22 .31 16 16 | 2037 872 13 100
| -8 62 |
esa 175| 1 0 2 -115 69 22 .10 5 5 | -1112 1199 10 112
| 23 90 |
gfz 188| -1 -1 -6 42 17 0 -.43 8 8 | 658 84 21 148
| -75 -95 |
grg 129| 0 0 -5 59 -116 7 .53 15 14 | 8 172 18 161
| -5 -12 |
igr n/a| 0 0 1 22 -25 -40 -.17 4 4 | 10646 541 17 95
| -40 34 |
jpl 80| 0 0 4 159 31 -19 .40 14 14 | 2477 518 17 129
| 27 -3 |
mit 238| 0 0 0 12 -38 -30 -.18 9 8 | -451 807 20 215
| -15 -10 |
ngs 242| 0 1 -2 -89 -29 -19 .29 11 9 | -2184 854 1758 4255
| -114 32 |
sio 279| -2 -1 3 -399 319 20 -.44 20 19 | --- --- --- ---
| 186 -143 |
Table 2.1715.3 GPS week: 1715 Day: 3 MJD: 56252.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 262| 0 -1 2 158 -95 11 -.42 9 8 | -597 -634 32 92
| -12 38 |
cof 260| 0 -2 1 142 -78 5 -.35 10 9 | -557 -639 19 87
| -16 21 |
emr 80| 0 2 3 33 -123 -23 .28 15 15 | 2478 -744 13 92
| -14 49 |
esa 175| 1 0 1 -153 129 16 .08 5 5 | 639 -81 10 101
| 36 59 |
gfz 190| -1 0 -2 62 104 -10 -.38 9 9 | 254 -114 21 145
| -73 -120 |
grg 130| -1 0 -5 55 -176 -11 .50 16 17 | -174 190 16 146
| 11 23 |
igr n/a| 0 0 0 42 -79 -33 -.15 4 4 | 10729 -1140 20 105
| -24 42 |
jpl 80| -1 0 3 193 -51 51 .41 14 14 | 2565 -635 18 118
| -30 19 |
mit 238| 0 0 -3 -8 -61 -17 -.19 8 7 | -460 566 24 218
| -11 -27 |
ngs 242| 0 1 0 -33 -101 -29 .37 13 11 | -777 -361 2377 3874
| -135 58 |
sio 273| -1 0 3 -300 615 128 -.50 18 17 | --- --- --- ---
| 130 -310 |
Table 2.1715.4 GPS week: 1715 Day: 4 MJD: 56253.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 262| 0 0 5 103 -77 -7 -.41 10 9 | -1575 58 37 86
| -22 14 |
cof 256| 0 -2 2 76 -109 -6 -.36 12 11 | -1538 58 20 81
| -6 19 |
emr 80| 1 0 3 13 -134 -16 .31 15 15 | 1153 605 14 102
| -41 -7 |
esa 175| 1 0 1 -62 143 32 .10 5 5 | -1144 -117 10 101
| -7 33 |
gfz 188| -2 0 -3 141 123 -14 -.38 9 9 | -517 -95 19 121
| -89 -113 |
grg 130| -1 1 -6 17 -227 -39 .47 17 16 | -688 77 18 197
| 35 36 |
igr n/a| 0 0 0 10 -103 -63 -.15 4 4 | 9127 221 18 72
| -38 29 |
jpl 80| 0 0 4 108 -148 16 .40 14 14 | 1417 753 16 117
| -23 -7 |
mit 239| 0 0 -3 8 -59 -34 -.18 9 8 | -738 89 20 214
| -4 -30 |
ngs 240| 0 2 -1 -71 -168 -13 .40 12 9 | -1427 -143 2336 3940
| -103 72 |
sio 278| -1 0 2 -286 283 28 -.47 16 17 | --- --- --- ---
| 132 -165 |
Table 2.1715.5 GPS week: 1715 Day: 5 MJD: 56254.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 261| 0 0 4 100 -48 4 -.47 11 10 | -644 -474 31 84
| -14 4 |
cof 255| 1 0 4 56 -71 12 -.40 11 10 | -603 -480 16 81
| 2 13 |
emr 80| 1 0 5 -17 -94 -8 .29 15 15 | 2565 440 12 100
| -25 15 |
esa 175| 1 0 2 -60 218 16 .09 5 5 | -3043 4020 12 108
| -17 24 |
gfz 192| -1 -1 -4 46 31 -22 -.36 8 8 | 94 0 19 133
| -37 -132 |
grg 128| 0 1 -5 -18 -201 1 .44 15 13 | -117 106 17 156
| 32 41 |
igr n/a| 0 0 0 -6 -76 -56 -.17 4 4 | 10078 -206 14 75
| -41 34 |
jpl 80| 0 0 4 121 -39 16 .40 14 13 | 2911 399 17 137
| 6 -10 |
mit 240| 0 0 -1 11 -85 2 -.20 7 7 | -158 274 19 192
| -16 -12 |
ngs 239| -2 0 -1 -72 -96 -35 .34 11 8 | -654 -474 1857 3810
| -81 -24 |
sio 277| -2 2 3 -343 353 67 -.48 18 18 | --- --- --- ---
| 150 -196 |
Table 2.1715.6 GPS week: 1715 Day: 6 MJD: 56255.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 260| 0 0 6 99 -20 -40 -.40 10 9 | -746 -360 32 93
| 16 -29 |
cof 256| 0 0 3 94 -40 -23 -.35 10 9 | -707 -373 16 90
| 3 7 |
emr 80| 2 1 6 9 -81 -7 .36 14 14 | 2902 -187 13 70
| -14 -2 |
esa 175| 1 0 1 -128 271 32 .12 5 5 | -383 826 12 101
| 43 21 |
gfz 191| -1 0 0 110 -9 -6 -.36 8 8 | 298 -439 20 121
| -87 -113 |
grg 129| 0 2 -5 7 -164 -8 .50 17 15 | 327 -460 17 123
| 32 -5 |
igr n/a| 0 0 0 23 -42 -31 -.14 5 4 | 10054 -1026 15 68
| -37 52 |
jpl 79| 0 0 1 115 -112 -45 .39 14 14 | 3383 -456 17 122
| 11 -5 |
mit 240| 0 0 -1 6 -140 7 -.18 6 6 | 62 17 24 182
| -28 -5 |
ngs 237| -2 0 -5 -125 -27 -18 .42 15 11 | -724 -399 1753 3366
| -70 28 |
sio 285| -1 3 2 -94 330 -137 -.43 21 19 | --- --- --- ---
| 31 -179 |
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 3.1715.0 GPS week: 1715 Day: 0 MJD: 56249.000
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 13 15 7 16 10 4 16 6 12 21 4 | 39 38 47 50 44 54 46 55 46 46 40 48
2 | 7 9 13 4 16 13 3 13 7 11 29 3 | 29 30 32 30 26 28 26 31 27 30 29 27
3 | 6 7 10 4 13 17 3 9 6 14 20 3 | 20 20 26 21 27 28 20 28 22 23 23 23
4 | 8 11 9 5 11 11 5 8 9 11 31 3 | 27 29 34 31 34 39 32 34 32 35 35 31
5 | 7 10 20 7 13 16 3 17 7 10 15 4 | 28 29 32 29 19 27 24 29 22 28 30 25
6 | 6 8 9 3 18 14 4 8 7 18 17 3 | 26 25 29 25 34 32 26 29 27 23 27 27
7 | 11 12 17 5 17 16 4 12 7 12 13 4 | 22 27 28 23 25 28 20 26 19 25 19 22
8 | 10 10 13 6 12 15 5 13 5 13 15 3 | 16 20 26 20 17 19 16 24 16 23 15 18
9 | 9 9 11 4 14 10 3 11 7 8 14 3 | 17 19 23 17 17 19 16 26 15 17 15 18
10 | 11 9 15 7 14 13 4 17 13 11 21 4 | 23 26 27 23 19 23 19 28 18 23 28 22
11 | 5 6 15 5 10 11 4 12 4 13 40 3 | 41 42 46 41 43 49 41 46 41 41 44 42
12E | 13 15 20 6 16 19 5 22 8 9 19 5 | 25 28 28 20 28 28 18 27 19 28 22 20
13 | 10 12 13 5 15 21 3 12 8 13 8 4 | 15 19 24 20 14 35 13 24 12 19 11 17
14 | 6 9 13 4 13 17 4 14 6 11 22 3 | 16 19 24 19 10 30 17 26 16 21 16 20
15 | 9 13 18 6 12 19 5 17 8 14 17 4 | 15 16 20 17 9 28 13 26 12 23 15 16
16E | 6 7 21 5 17 21 5 13 9 17 20 4 | 18 18 26 20 21 21 18 24 17 25 28 19
17 | 6 12 16 6 14 9 4 16 7 11 26 4 | 28 33 33 32 33 38 30 35 30 32 31 30
18 | 9 13 13 6 15 14 4 13 9 8 16 4 | 33 36 33 30 18 32 26 33 25 32 29 29
19 | 19 20 17 5 13 9 5 13 6 12 31 4 | 26 26 25 24 31 27 24 29 26 21 31 23
20 | 8 12 12 6 15 16 4 11 8 10 19 4 | 32 35 31 29 25 26 26 32 26 27 29 27
21 | 6 10 12 5 16 10 4 14 8 15 29 4 | 26 27 34 29 27 29 26 33 26 33 25 28
22 | 7 7 9 4 12 15 3 10 5 12 16 3 | 24 27 29 28 19 33 25 32 24 32 25 26
23 | 12 14 15 6 16 18 4 15 9 11 13 4 | 19 23 26 24 10 24 18 24 15 20 18 22
24 | 9 9 18 6 12 14 4 17 7 13 11 4 | 46 47 45 46 47 45 43 47 43 49 46 45
25E | 14 18 28 6 10 17 5 17 10 9 15 5 | 36 37 39 32 35 37 32 40 31 35 32 32
26 | 8 11 16 6 16 11 3 9 4 14 13 3 | 20 22 27 17 16 21 15 24 15 21 18 19
X27E | 32 11 --- --- --- --- 49 --- --- --- --- 0 | 35 63 --- --- --- --- 70 --- --- --- --- 63
28E | 5 8 14 4 12 17 3 9 4 10 17 3 | 27 30 33 31 25 32 27 33 24 34 34 28
29 | 9 17 20 6 15 14 5 16 7 11 24 4 | 23 30 27 22 29 25 23 25 24 25 19 23
X30E | 19 17 --- 7 15 17 10 19 11 23 19 6 | 60 61 --- 57 59 56 56 64 51 59 59 55
31 | 8 12 20 5 13 19 3 13 10 12 25 4 | 22 25 36 27 22 35 23 29 25 28 23 27
32E | 26 15 20 7 14 21 6 21 8 12 32 5 | 21 27 35 33 28 27 28 29 31 31 26 31
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 12 16 6 14 15 4 14 8 12 22 |T 26 29 30 27 26 31 26 32 25 29 27 28
WRMS | 9 11 16 5 14 14 4 13 7 11 21 |NE 25 27 30 26 24 30 24 31 24 27 25 26
MEDI | 9 11 15 6 14 15 4 13 7 12 19 |MD 25 27 29 27 25 28 24 29 24 28 27 26
Table 3.1715.1 GPS week: 1715 Day: 1 MJD: 56250.000
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 | 8 8 15 9 10 13 4 15 7 15 17 4 | 24 25 33 30 32 40 28 42 30 28 26 29
2 | 9 10 15 6 11 14 4 14 8 9 26 4 | 16 15 22 20 21 18 18 23 17 20 17 19
3 | 8 6 9 4 6 17 4 10 10 9 17 3 | 13 14 23 18 19 23 16 21 17 24 16 19
4 | 6 9 10 5 10 12 4 10 12 14 26 3 | 18 20 27 24 26 27 22 25 22 22 22 23
5 | 9 11 18 6 7 17 3 17 8 11 16 4 | 22 25 25 22 19 25 17 27 18 23 23 20
6 | 8 6 10 3 7 13 3 7 9 14 14 3 | 16 17 23 19 23 23 18 23 21 27 18 21
7 | 9 12 16 6 10 18 5 17 10 10 13 4 | 18 21 24 19 20 26 18 22 18 27 16 19
8 | 9 8 13 5 7 17 4 11 7 11 13 3 | 12 16 21 17 17 16 15 21 16 23 16 16
9 | 8 9 12 7 6 11 5 10 7 10 15 3 | 14 15 19 13 16 16 14 19 14 22 15 14
10 | 9 10 16 7 7 13 4 16 15 11 23 4 | 16 19 22 16 16 15 13 21 14 20 23 16
11 | 4 5 16 6 7 11 5 11 8 20 37 4 | 22 21 30 24 23 30 22 30 23 28 33 24
12E | 12 10 19 5 8 15 6 23 10 10 14 4 | 24 25 27 22 25 26 22 28 24 27 29 22
13 | 9 10 16 5 8 21 2 16 9 9 11 4 | 10 12 23 16 13 34 12 22 13 20 11 15
14 | 8 5 13 6 8 17 3 13 7 8 21 3 | 13 12 22 17 12 28 13 20 14 23 16 17
15 | 15 17 15 9 8 19 3 16 9 11 20 4 | 17 19 21 13 15 27 12 20 13 23 19 12
16E | 6 6 18 6 12 20 4 16 10 13 24 4 | 12 11 24 15 20 24 14 21 18 24 21 17
17 | 7 10 16 6 8 11 4 17 8 11 25 4 | 17 21 28 22 23 29 21 28 21 27 20 22
18 | 10 10 13 5 8 15 4 12 13 8 17 3 | 20 24 24 21 18 30 17 27 22 21 20 20
19 | 19 21 16 7 9 12 3 13 10 10 27 4 | 17 18 23 20 21 21 15 21 16 19 22 18
20 | 9 11 13 7 9 15 3 11 11 6 15 3 | 23 26 18 18 22 19 17 20 21 20 20 17
21 | 5 8 14 5 7 11 3 12 9 10 29 3 | 15 17 29 24 21 25 19 27 22 26 19 22
22 | 6 8 10 4 6 17 2 8 8 8 17 3 | 14 16 21 19 16 29 15 22 18 23 16 17
23 | 10 12 17 6 11 20 4 20 10 9 15 4 | 14 16 24 19 13 25 14 24 14 21 17 16
24 | 9 12 16 6 9 17 5 16 6 8 16 4 | 32 35 33 33 35 36 31 38 32 39 34 32
25E | 9 11 21 6 6 11 3 16 8 9 15 4 | 32 32 36 30 31 32 31 36 32 38 31 32
26 | 10 11 13 6 7 13 3 10 9 12 17 3 | 15 16 21 15 15 22 13 20 15 19 17 15
X27E | 82 10 --- --- --- --- 109 --- --- --- --- 0 | 37 72 --- --- --- --- 33 --- --- --- --- 71
28E | 8 9 14 4 8 19 4 13 6 10 18 3 | 18 20 26 20 20 24 19 22 20 31 22 20
29 | 9 9 17 5 10 16 4 17 10 10 23 4 | 17 20 24 17 22 18 21 22 22 27 17 19
30E | 18 20 29 8 10 17 6 20 14 24 25 6 | 51 50 49 51 56 55 53 54 48 56 48 52
31 | 6 12 18 5 10 19 3 13 8 11 19 4 | 16 18 31 20 19 31 17 26 17 25 17 20
32E | 21 20 20 9 12 25 11 21 14 11 27 5 | 49 44 51 48 43 47 42 51 49 46 43 46
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 11 16 6 9 16 4 15 10 12 21 |T 20 22 26 22 22 27 20 26 21 26 22 23
WRMS | 9 11 16 6 8 15 4 14 10 10 19 |NE 17 19 24 19 19 25 17 24 18 23 19 19
MEDI | 9 10 16 6 8 16 4 14 9 10 17 |MD 17 19 24 20 20 26 17 23 18 24 20 19
Table 3.1715.2 GPS week: 1715 Day: 2 MJD: 56251.000
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 10 15 4 8 14 6 16 6 11 21 3 | 42 38 38 41 41 41 40 44 38 42 39 40
2 | 11 14 17 4 11 14 3 14 8 8 25 4 | 19 20 25 24 27 20 22 25 21 28 23 23
3 | 8 6 9 4 6 17 4 8 10 11 17 3 | 14 14 19 17 22 26 16 19 18 20 17 17
4 | 7 11 9 4 6 11 3 9 12 10 26 3 | 21 22 29 28 30 33 26 28 26 30 25 27
5 | 6 11 18 5 7 14 3 16 7 8 16 3 | 23 28 27 24 22 26 22 28 22 31 29 23
6 | 7 7 9 3 9 13 4 8 11 12 14 3 | 18 18 21 21 27 29 21 21 23 25 20 21
7 | 9 12 17 5 7 18 3 13 9 7 14 3 | 18 22 27 22 22 29 19 26 19 25 20 20
8 | 9 10 13 5 7 15 2 11 7 12 13 3 | 10 13 20 15 14 16 12 20 13 20 16 13
9 | 8 7 11 5 7 10 4 13 8 9 13 3 | 13 13 20 14 15 18 14 22 15 20 16 14
10 | 10 10 13 6 7 15 5 16 11 7 21 3 | 16 21 23 17 18 18 14 23 14 20 23 16
11 | 7 6 15 3 10 12 3 12 6 11 37 3 | 30 29 34 30 35 37 29 34 30 33 39 31
12E | 10 11 19 5 6 11 6 22 10 12 12 4 | 21 22 28 27 31 30 29 25 22 40 25 25
13 | 9 11 14 4 7 21 3 12 8 11 12 3 | 10 14 22 17 12 34 12 24 14 21 13 15
14 | 10 9 16 7 8 14 4 14 7 11 21 3 | 10 12 24 16 14 27 12 22 13 23 17 14
15 | 9 11 18 5 7 14 3 20 8 10 15 4 | 12 13 21 12 13 26 9 23 12 21 18 11
16E | 7 7 20 5 10 12 4 13 8 11 16 3 | 16 15 24 17 21 28 17 21 19 27 23 18
17 | 7 7 16 8 7 10 4 18 8 12 25 4 | 24 28 33 29 30 35 28 33 28 37 28 28
18 | 9 9 14 4 7 14 2 13 5 9 15 3 | 25 27 30 25 17 28 22 31 21 24 27 22
19 | 9 11 16 4 7 10 4 15 9 9 24 3 | 21 23 24 23 24 26 20 26 21 20 25 22
20 | 8 11 9 5 9 17 3 12 10 7 11 3 | 25 26 22 21 20 22 19 26 21 23 21 18
21 | 7 9 14 4 8 8 3 14 7 17 32 3 | 18 18 28 24 22 24 20 29 21 25 26 21
22 | 9 9 9 4 6 16 3 10 6 11 15 3 | 16 21 25 21 19 30 20 29 20 28 22 20
23 | 11 13 15 4 10 20 4 14 8 8 16 4 | 15 18 26 21 16 30 16 24 18 24 20 18
24 | 11 11 18 5 10 14 6 18 9 11 13 4 | 40 40 39 40 40 40 37 45 38 42 39 38
25E | 10 15 20 6 7 16 3 15 9 10 16 4 | 32 31 38 34 37 41 31 35 31 37 30 33
26 | 10 14 12 4 6 9 3 11 7 10 12 3 | 14 15 20 14 16 18 12 23 13 20 19 14
X27E | 65 10 --- --- --- --- 99 --- --- --- --- 0 | 37 68 --- --- --- --- 28 --- --- --- --- 68
28E | 7 9 11 4 8 20 3 9 6 11 19 3 | 16 20 21 19 22 21 19 21 18 31 25 18
29 | 10 11 19 5 9 14 3 16 9 12 23 4 | 19 21 23 18 25 22 19 19 20 23 15 17
30E | 25 24 28 9 8 20 9 23 16 24 28 6 | 39 39 33 36 47 39 35 38 43 52 40 38
31 | 11 18 15 7 8 17 4 13 9 9 20 4 | 17 23 27 20 19 32 18 27 19 25 21 18
X32 | 18 13 13 5 8 --- 9 --- 12 7 --- 4 | 30 36 36 39 37 --- 30 --- 28 33 --- 37
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 11 16 5 8 15 4 14 9 11 20 |T 21 24 26 23 24 28 21 27 21 28 24 23
WRMS | 9 11 16 5 8 14 4 14 8 9 19 |NE 19 21 25 22 22 27 19 26 20 26 23 20
MEDI | 9 11 15 5 7 14 3 13 8 11 16 |MD 18 21 25 21 22 28 20 25 21 25 23 20
Table 3.1715.3 GPS week: 1715 Day: 3 MJD: 56252.000
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 | 7 8 17 5 8 13 4 17 6 12 13 3 | 35 36 38 39 41 46 38 43 40 40 35 39
2 | 10 9 13 4 13 17 3 15 8 11 26 3 | 25 25 28 25 26 25 24 30 25 26 26 24
3 | 7 7 10 3 7 15 2 9 7 12 18 3 | 19 20 21 17 22 28 18 23 20 20 22 19
4 | 8 10 8 5 10 13 3 9 8 18 22 3 | 27 31 32 30 32 36 31 33 30 36 28 30
5 | 6 8 16 5 8 17 3 19 6 12 14 3 | 24 22 26 22 21 28 20 30 22 28 26 21
6 | 8 8 11 3 8 13 3 7 9 14 13 3 | 24 26 24 22 28 30 23 26 25 23 25 23
7 | 8 12 16 4 8 18 4 12 8 10 14 3 | 21 26 23 19 22 29 20 24 22 26 20 20
8 | 8 10 11 5 9 20 4 12 6 9 10 3 | 17 19 21 14 18 22 16 24 18 23 19 15
9 | 6 8 11 4 7 15 4 12 8 10 10 3 | 16 15 23 15 15 23 16 23 16 22 19 15
10 | 8 5 13 4 12 16 4 16 9 11 20 3 | 21 20 25 18 26 22 16 28 19 22 24 18
11 | 8 8 15 2 9 13 4 13 6 19 35 3 | 34 35 37 35 38 44 36 39 40 38 40 36
12E | 12 12 17 5 10 15 4 24 9 10 12 4 | 32 35 31 29 29 32 26 34 25 31 28 27
13 | 9 9 12 4 7 23 3 12 8 13 13 3 | 12 16 23 15 16 35 11 22 14 21 13 14
14 | 6 8 14 4 9 17 4 12 6 9 16 3 | 9 10 21 14 11 28 11 20 14 23 14 13
15 | 9 7 17 5 10 19 5 20 8 14 11 4 | 11 10 21 12 12 27 9 21 15 22 14 10
16E | 6 6 20 4 11 18 4 13 9 11 18 4 | 16 16 22 17 20 22 16 19 19 26 28 17
17 | 8 10 16 6 10 12 4 15 7 16 22 4 | 29 35 32 28 31 37 28 31 28 31 32 29
18 | 7 8 15 3 8 15 3 16 5 8 15 3 | 24 26 32 24 21 27 22 31 23 31 30 24
19 | 15 14 14 5 7 12 4 14 9 12 23 3 | 23 22 22 20 24 22 20 23 22 25 23 19
20 | 6 9 12 5 11 17 3 11 6 13 10 3 | 27 28 25 24 25 25 20 25 22 24 26 22
21 | 6 7 13 3 8 13 3 11 6 11 31 3 | 21 23 29 25 24 27 23 29 24 32 27 25
22 | 7 7 12 3 9 19 2 11 4 11 16 3 | 18 19 26 19 18 28 18 25 18 25 23 19
23 | 11 11 14 5 7 21 6 14 9 13 17 4 | 13 17 22 18 12 26 12 22 14 18 15 14
24 | 7 7 18 5 11 19 4 14 7 13 9 4 | 39 40 42 41 40 42 39 38 37 47 40 38
25E | 7 8 24 7 7 18 5 15 9 8 15 4 | 26 28 34 26 27 36 26 33 27 31 27 26
26 | 9 9 14 4 10 11 4 11 9 14 13 3 | 17 16 26 16 21 24 18 25 17 24 20 17
X27E | 38 11 --- --- --- --- 59 --- --- --- --- 0 | 31 47 --- --- --- --- 30 --- --- --- --- 46
28E | 7 6 13 3 9 16 3 10 5 15 16 3 | 24 26 29 24 25 31 23 29 23 34 30 24
29 | 9 9 19 5 8 11 5 18 8 8 24 3 | 23 24 27 19 27 25 23 25 24 28 18 20
30E | 22 23 26 6 9 18 8 22 12 29 19 6 | 53 53 36 50 56 51 51 54 54 58 59 50
31 | 8 12 16 9 8 19 5 13 10 17 19 4 | 20 23 30 26 24 33 20 28 22 28 19 22
X32 | 85 11 --- --- --- --- 81 --- --- --- --- 0 | 14 17 --- --- --- --- 15 --- --- --- --- 15
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 9 10 15 5 9 16 4 14 8 13 18 |T 23 25 27 23 25 30 22 28 23 28 25 23
WRMS | 8 9 15 5 9 17 4 14 7 11 17 |NE 21 23 27 22 23 29 21 27 22 27 23 21
MEDI | 8 8 14 4 9 16 4 13 8 12 16 |MD 23 23 26 22 24 28 20 26 22 26 25 21
Table 3.1715.4 GPS week: 1715 Day: 4 MJD: 56253.000
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 | 6 10 14 9 10 15 7 17 8 12 11 4 | 33 33 37 35 38 43 36 42 37 40 32 35
2 | 9 10 14 4 11 16 3 14 8 11 24 4 | 25 29 30 25 23 25 25 30 25 33 23 23
3 | 7 5 9 3 9 18 3 9 7 9 15 3 | 14 16 22 17 20 25 17 22 19 23 19 18
4 | 8 12 9 5 8 15 5 8 9 10 15 3 | 28 32 34 30 28 35 31 33 32 33 29 29
5 | 8 9 18 6 8 16 3 16 9 8 11 3 | 18 21 30 20 18 27 17 30 18 27 21 18
6 | 7 5 9 4 10 16 2 10 7 8 12 3 | 19 20 24 21 26 28 21 23 23 25 21 22
7 | 8 10 15 5 10 20 3 14 7 8 14 3 | 21 22 25 19 20 28 19 26 20 24 18 18
8 | 8 6 9 5 7 16 3 12 8 13 11 3 | 15 17 22 15 13 22 16 25 18 22 17 13
9 | 7 12 9 6 6 15 4 10 5 11 11 3 | 15 20 23 17 17 22 17 25 19 26 18 16
10 | 10 10 11 6 11 16 4 15 10 6 16 3 | 16 19 23 18 23 21 16 26 17 20 22 16
11 | 7 7 15 6 10 14 7 11 11 14 33 4 | 32 34 36 31 37 38 32 36 32 36 40 32
12E | 11 15 19 5 10 16 7 22 10 13 11 4 | 18 29 27 21 21 26 19 24 17 31 16 18
13 | 9 10 12 6 7 26 4 13 10 11 11 3 | 14 16 24 15 11 37 14 25 16 24 14 13
14 | 7 10 13 3 10 21 5 15 7 11 14 3 | 11 12 23 17 13 34 14 25 15 26 14 15
15 | 18 16 18 6 8 22 4 20 8 13 11 4 | 21 20 24 14 13 31 16 27 17 31 15 13
16E | 7 9 16 6 12 22 5 17 11 7 16 4 | 13 20 21 17 17 24 14 21 16 27 22 15
17 | 9 10 17 6 6 12 4 15 8 9 21 3 | 28 27 32 27 27 34 29 32 28 36 30 26
18 | 11 15 12 3 9 12 3 13 6 11 13 3 | 24 28 28 23 17 26 22 27 20 35 27 22
19 | 18 19 18 6 9 16 4 16 10 9 23 4 | 19 23 23 19 25 23 19 25 20 24 22 18
20 | 10 10 12 7 9 16 5 9 11 9 10 3 | 23 24 24 18 19 22 18 24 21 23 23 17
21 | 8 8 13 4 9 10 4 12 8 11 29 3 | 22 23 29 27 22 26 23 32 23 34 23 23
22 | 8 8 11 3 8 17 3 13 8 11 13 3 | 15 15 23 19 14 27 16 26 18 24 20 17
23 | 10 13 17 6 11 24 6 16 10 11 16 4 | 13 16 25 17 12 29 13 25 15 22 17 14
24 | 8 14 21 7 10 22 4 13 5 10 13 4 | 35 41 39 36 37 40 35 37 36 41 36 34
25E | 10 10 22 5 11 13 5 13 7 9 14 3 | 33 31 38 30 31 37 31 36 34 38 35 31
26 | 9 10 14 5 7 14 3 9 8 12 11 3 | 16 17 27 17 19 26 17 26 19 24 19 17
X27E | 19 10 --- --- --- --- 48 --- --- --- --- 0 | 20 38 --- --- --- --- 36 --- --- --- --- 37
28E | 6 7 12 4 9 17 3 11 7 10 16 3 | 17 19 24 18 15 23 18 22 17 27 20 17
29 | 10 14 16 5 10 14 5 17 10 10 20 4 | 21 25 27 19 23 26 20 26 21 24 16 18
30E | 22 25 28 7 11 19 7 22 10 32 15 6 | 40 44 37 37 41 39 39 45 39 56 42 39
31 | 8 16 15 6 8 20 4 14 10 10 17 4 | 21 25 26 20 19 33 19 29 19 29 18 18
X32 | 14 12 12 8 10 17 6 10 11 8 --- 4 | 13 12 12 9 15 13 13 13 14 14 --- 10
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 12 15 5 9 17 4 14 9 12 16 |T 21 24 27 21 21 28 21 27 22 29 22 21
WRMS | 9 11 15 5 9 16 4 14 8 9 17 |NE 20 23 27 21 21 29 20 28 21 28 22 20
MEDI | 8 10 14 6 9 16 4 13 8 10 14 |MD 19 22 25 19 20 27 19 26 19 27 21 18
Table 3.1715.5 GPS week: 1715 Day: 5 MJD: 56254.000
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 10 14 5 8 8 7 17 9 11 16 3 | 29 32 32 33 36 35 33 38 32 35 28 32
2 | 9 8 14 4 9 15 4 15 7 8 29 3 | 20 19 27 27 29 21 24 27 22 31 22 24
3 | 11 7 11 2 7 12 2 8 5 8 15 2 | 14 16 22 18 19 20 17 19 17 22 19 17
4 | 9 12 8 3 6 11 5 11 7 6 15 3 | 21 26 28 28 28 29 26 27 25 26 25 27
5 | 9 10 18 5 9 15 3 12 6 11 16 3 | 20 21 28 22 20 29 20 24 20 26 21 20
6 | 9 8 13 5 10 11 3 8 7 9 12 3 | 18 18 24 22 23 23 20 21 21 22 19 20
7 | 7 10 18 5 7 21 4 14 6 7 16 3 | 18 21 22 21 20 28 17 22 17 23 15 17
8 | 9 8 11 5 6 14 5 12 5 6 10 3 | 12 14 18 15 15 16 14 20 16 17 14 13
9 | 5 6 10 6 7 12 4 11 5 8 11 2 | 12 13 19 15 15 17 14 18 12 18 15 14
10 | 7 7 11 8 7 12 3 14 7 9 17 3 | 18 18 24 21 21 21 18 26 19 23 25 19
11 | 8 8 15 5 5 10 4 12 6 15 36 3 | 25 27 32 27 29 31 27 29 25 27 34 26
12E | 12 13 17 4 12 19 6 16 8 10 13 4 | 20 26 25 25 25 21 22 23 21 32 22 22
13 | 8 11 15 5 5 23 5 12 8 10 13 3 | 11 17 23 18 15 37 14 23 14 23 12 16
14 | 7 8 12 5 6 23 3 13 5 9 14 3 | 12 13 23 19 13 35 15 22 15 27 15 17
15 | 12 15 16 5 6 20 4 19 8 10 15 4 | 15 14 22 16 14 29 13 23 14 24 13 14
16E | 7 9 16 6 10 22 4 15 7 9 16 4 | 18 19 24 23 22 21 20 22 22 27 26 21
17 | 11 13 16 6 7 10 5 15 8 10 24 3 | 19 24 28 22 23 29 20 26 21 26 25 22
18 | 14 13 14 4 10 12 2 12 4 12 17 3 | 23 23 27 23 15 23 19 22 16 26 24 19
19 | 12 13 18 3 7 9 3 17 7 10 25 3 | 17 19 25 19 22 21 19 22 18 20 20 18
20 | 9 12 15 5 11 15 4 11 7 10 14 3 | 21 25 27 20 22 23 17 22 18 23 21 18
21 | 6 9 12 5 6 9 2 11 5 12 32 3 | 16 16 25 25 20 22 19 26 19 23 18 21
22 | 7 8 14 4 6 18 4 9 5 10 14 3 | 13 14 23 20 15 27 16 21 15 22 17 17
23 | 11 11 18 5 8 21 5 15 8 12 17 4 | 14 19 26 21 17 31 16 23 16 24 16 18
24 | 8 9 20 7 8 19 3 14 5 7 12 3 | 30 32 32 34 33 35 31 38 31 34 32 31
25E | 24 12 22 9 9 11 4 13 7 14 16 4 | 41 44 45 43 44 41 42 46 42 49 42 42
26 | 8 8 14 6 7 11 4 11 7 9 11 3 | 17 18 25 19 22 23 17 23 16 23 18 19
X27E | 62 8 --- --- --- --- 69 --- --- --- --- 0 | 19 53 --- --- --- --- 21 --- --- --- --- 53
28E | 8 6 12 3 6 13 3 9 5 11 15 2 | 12 16 22 19 17 21 17 21 17 25 20 18
29 | 7 8 19 4 11 11 4 18 7 10 22 4 | 22 24 26 21 26 24 24 26 24 26 17 21
30E | 24 23 23 8 8 13 8 23 9 29 17 6 | 41 41 30 40 44 38 40 45 41 48 44 39
31 | 11 12 16 8 8 20 4 13 7 9 18 4 | 15 21 26 24 19 32 19 26 18 27 19 21
32 | 9 12 13 6 7 13 3 12 6 7 24 3 | 11 13 12 11 15 10 10 11 10 14 9 10
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 11 11 15 5 8 15 4 14 7 11 18 |T 19 22 25 22 22 26 20 25 20 26 21 22
WRMS | 10 10 15 5 8 13 4 13 7 8 18 |NE 18 20 25 22 21 26 19 24 19 24 20 20
MEDI | 9 9 15 5 7 13 4 13 7 10 16 |MD 18 19 25 21 21 24 19 23 18 25 20 19
Table 3.1715.6 GPS week: 1715 Day: 6 MJD: 56255.000
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 | 8 7 15 8 9 12 5 19 4 14 29 3 | 44 46 47 53 48 53 49 55 50 52 42 50
2 | 8 8 12 5 7 17 4 12 5 9 29 3 | 29 28 31 34 31 32 31 33 32 36 32 31
3 | 6 4 11 4 6 15 5 10 4 8 16 2 | 18 22 24 24 23 29 21 23 21 26 21 22
4 | 8 10 7 4 4 14 4 11 5 14 16 3 | 31 34 40 39 38 48 39 42 39 42 36 39
5 | 6 7 16 6 8 19 4 14 6 11 16 3 | 24 24 28 28 23 27 23 27 23 27 25 23
6 | 7 5 11 4 7 11 3 9 4 9 12 2 | 27 28 28 30 29 33 27 28 28 31 25 28
7 | 6 9 14 6 8 21 4 14 4 8 15 3 | 25 28 27 27 26 29 22 27 23 27 21 23
8 | 9 8 11 5 6 16 4 11 7 8 8 3 | 18 17 23 21 17 20 20 24 17 22 17 18
9 | 7 8 10 5 7 14 4 10 4 11 10 3 | 19 17 24 20 17 23 17 22 17 18 15 18
10 | 7 7 10 5 7 14 3 14 5 9 17 3 | 21 21 24 21 24 19 18 23 22 21 27 19
11 | 6 4 15 4 7 12 4 13 4 15 45 3 | 42 42 45 47 47 52 46 46 45 49 47 45
12E | 10 8 13 4 8 17 6 16 6 11 15 3 | 19 26 22 24 26 23 23 21 21 31 24 22
13 | 11 8 10 4 6 23 4 11 7 11 10 3 | 17 20 25 23 15 35 18 26 18 24 15 19
14 | 5 9 13 5 11 18 3 13 6 14 16 3 | 15 16 23 20 15 30 16 23 16 22 19 17
15 | 10 7 18 5 7 17 6 26 5 16 15 4 | 17 17 23 19 17 29 16 27 17 26 15 17
16E | 7 7 15 5 11 23 4 13 6 9 11 3 | 18 21 22 23 22 22 19 21 19 26 23 20
17 | 10 10 17 5 5 12 5 15 5 12 21 3 | 32 37 35 32 33 42 32 35 33 36 35 33
18 | 12 13 12 5 9 19 2 16 5 13 17 3 | 35 35 34 33 22 31 28 34 27 31 36 30
19 | 12 14 19 5 9 12 4 14 8 11 28 4 | 20 21 27 27 26 25 24 26 24 27 28 23
20 | 9 11 16 4 11 17 4 15 5 12 20 3 | 27 29 29 23 24 23 22 29 23 23 26 22
21 | 7 8 14 5 8 11 3 15 5 9 31 3 | 27 26 35 30 27 30 26 36 27 30 29 28
22 | 5 8 12 5 7 21 4 12 5 14 13 3 | 22 21 29 26 20 32 22 29 23 23 25 23
23 | 12 11 14 5 9 19 4 13 7 11 16 3 | 18 20 26 24 15 28 17 26 17 24 19 20
X24 | 8 8 21 6 9 21 4 --- 5 13 13 4 | 39 42 42 42 42 41 41 --- 38 42 42 40
25E | 14 12 22 12 12 23 10 18 12 38 19 6 | 87 94 101 100 96 94 92 93 94 97 94 96
26 | 8 9 17 4 5 14 4 12 6 9 13 3 | 19 17 29 20 20 23 18 22 20 22 21 19
X27E | 30 8 --- --- --- --- 64 --- --- --- --- 0 | 38 44 --- --- --- --- 27 --- --- --- --- 44
28E | 8 7 12 4 7 15 3 12 6 10 14 3 | 16 16 22 20 19 21 17 18 16 27 22 18
29 | 9 11 18 5 10 10 6 19 5 12 27 4 | 26 30 27 27 34 32 29 26 28 36 21 27
30E | 21 20 20 8 11 15 8 18 8 37 23 6 | 45 44 31 44 50 45 45 48 47 58 46 45
31 | 8 11 18 6 10 18 6 13 7 13 22 4 | 18 23 27 26 22 32 21 25 20 27 24 22
32 | 14 11 9 5 5 13 4 11 3 12 25 3 | 15 18 15 19 18 11 15 16 14 15 11 17
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 10 14 5 8 16 5 14 6 15 21 |T 27 28 31 30 28 32 27 31 27 32 28 28
WRMS | 9 9 14 5 7 15 4 14 6 11 19 |NE 25 26 30 28 26 31 25 29 25 29 26 26
MEDI | 8 8 14 5 8 16 4 13 5 11 16 |MD 22 24 27 26 24 30 22 26 23 27 25 23
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1715 GPS week: 1715 MJD: 56249.0-56255.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3014 |U 5 6 15 |U 8 10 26 |U 8 7 15 |
cof | cof 3014 |U 5 6 15 |U 8 10 26 |U 8 7 15 |
emr | emr 2944 | 9 9 18 |U 9 9 26 | 9 9 19 |
esa | esa 2962 | 6 7 13 |U 8 10 26 | 8 7 15 |
gfz | gfz 2956 |U 6 7 12 |U 8 11 27 |U 8 7 15 |
grg | grg 2948 |U 8 11 23 |U 10 13 35 | 11 15 28 |
igr | igr 2947 | 6 7 13 | 8 10 25 | 8 7 15 |
igs | igs 2956 | 6 7 13 | 8 9 25 | 8 8 16 |
jpl | jpl 2929 | 10 10 19 |U 9 12 30 | 9 10 21 |
mit | mit 2962 | 7 8 18 |U 8 10 27 |U 9 12 25 |
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 5.1715.0 GPS week: 1715 Day: 0 MJD: 56249.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3011 | 5 8 16 | 8 13 30 | 10 8 18 |
cof | cof 3011 | 5 8 15 | 8 13 30 | 10 8 19 |
emr | emr 2878 | 9 8 21 | 10 10 31 | 9 10 22 |
esa | esa 2976 | 5 7 15 | 8 14 32 | 9 7 18 |
gfz | gfz 2968 | 5 7 14 | 9 13 33 | 12 9 19 |
grg | grg 2976 | 10 9 23 | 9 13 40 | 22 22 42 |
igr | igr 2879 | 5 6 15 | 8 13 34 | 9 6 18 |
igs | igs 2942 | 5 7 16 | 8 12 30 | 10 7 18 |
jpl | jpl 2968 | 7 5 16 | 8 13 31 | 10 10 27 |
mit | mit 2976 | 5 8 14 | 9 15 36 | 12 13 31 |
Table 5.1715.1 GPS week: 1715 Day: 1 MJD: 56250.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3044 | 4 5 13 | 7 7 23 | 8 7 13 |
cof | cof 3044 | 4 5 12 | 7 8 24 | 8 7 13 |
emr | emr 2972 | 9 8 16 | 8 9 22 | 10 13 22 |
esa | esa 2976 | 5 6 14 | 7 10 27 | 8 7 13 |
gfz | gfz 2968 | 5 6 12 | 8 10 24 | 9 8 15 |
grg | grg 2976 | 6 8 20 | 8 8 31 | 10 15 27 |
igr | igr 2976 | 4 6 13 | 7 9 22 | 8 7 11 |
igs | igs 2972 | 5 6 11 | 7 9 23 | 9 12 19 |
jpl | jpl 2972 | 7 7 15 | 8 15 37 | 9 13 25 |
mit | mit 2976 | 4 5 11 | 7 10 21 | 12 17 29 |
Table 5.1715.2 GPS week: 1715 Day: 2 MJD: 56251.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 7 9 18 | 10 10 36 | 8 5 16 |
cof | cof 3030 | 7 9 17 | 11 10 36 | 7 5 15 |
emr | emr 2972 | 10 12 19 | 10 10 33 | 7 10 22 |
esa | esa 2976 | 7 10 13 | 10 9 32 | 6 6 14 |
gfz | gfz 2971 | 8 10 14 | 10 9 32 | 6 5 13 |
grg | grg 2880 | 10 15 25 | 12 14 42 | 10 10 23 |
igr | igr 2971 | 7 10 13 | 10 9 31 | 7 5 14 |
igs | igs 2975 | 8 11 13 | 9 9 32 | 6 11 21 |
jpl | jpl 2872 | 11 10 19 | 11 13 34 | 9 15 25 |
mit | mit 2976 | 15 19 49 | 10 8 37 | 8 13 29 |
Table 5.1715.3 GPS week: 1715 Day: 3 MJD: 56252.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2923 | 6 7 18 | 11 10 26 | 8 6 15 |
cof | cof 2923 | 6 7 18 | 11 10 26 | 8 6 15 |
emr | emr 2876 | 10 12 21 | 11 9 32 | 9 6 18 |
esa | esa 2880 | 7 9 15 | 10 9 30 | 8 6 17 |
gfz | gfz 2876 | 7 10 16 | 10 10 29 | 8 6 18 |
grg | grg 2880 | 10 12 24 | 11 10 28 | 10 9 21 |
igr | igr 2880 | 7 9 17 | 10 10 28 | 8 7 16 |
igs | igs 2880 | 7 9 16 | 10 9 28 | 8 6 16 |
jpl | jpl 2876 | 11 12 20 | 12 11 38 | 9 6 16 |
mit | mit 2880 | 9 10 21 | 11 10 31 | 8 10 21 |
Table 5.1715.4 GPS week: 1715 Day: 4 MJD: 56253.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3031 | 4 4 12 | 8 11 23 | 7 7 13 |
cof | cof 3031 | 4 4 13 | 8 10 23 | 7 7 14 |
emr | emr 2972 | 8 8 13 | 8 10 24 | 6 6 15 |
esa | esa 2976 | 5 6 9 | 8 10 23 | 6 6 13 |
gfz | gfz 2971 | 6 6 9 | 10 14 30 | 7 6 12 |
grg | grg 2975 | 8 11 26 | 16 23 56 | 9 23 35 |
igr | igr 2976 | 5 7 11 | 8 10 23 | 7 7 14 |
igs | igs 2976 | 6 6 10 | 8 10 22 | 6 7 13 |
jpl | jpl 2972 | 15 14 24 | 9 11 29 | 7 6 16 |
mit | mit 2976 | 6 6 9 | 8 9 23 | 7 9 20 |
Table 5.1715.5 GPS week: 1715 Day: 5 MJD: 56254.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 5 6 16 | 7 11 18 | 8 7 12 |
cof | cof 3039 | 6 6 17 | 6 11 18 | 8 7 12 |
emr | emr 2972 | 7 9 17 | 6 8 19 | 9 7 18 |
esa | esa 2976 | 5 6 15 | 6 9 17 | 9 8 13 |
gfz | gfz 2970 | 5 6 12 | 7 10 20 | 8 7 13 |
grg | grg 2976 | 7 12 25 | 7 11 22 | 11 16 21 |
igr | igr 2976 | 5 6 14 | 6 8 16 | 9 8 14 |
igs | igs 2976 | 4 6 13 | 6 9 16 | 8 7 14 |
jpl | jpl 2972 | 9 12 19 | 7 10 18 | 9 8 20 |
mit | mit 2976 | 5 5 12 | 6 9 18 | 9 10 22 |
Table 5.1715.6 GPS week: 1715 Day: 6 MJD: 56255.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 4 6 13 | 6 8 24 | 8 8 17 |
cof | cof 3025 | 4 6 13 | 6 8 23 | 7 7 16 |
emr | emr 2972 | 10 6 17 | 7 9 25 | 10 9 17 |
esa | esa 2976 | 6 4 11 | 6 8 20 | 8 8 15 |
gfz | gfz 2972 | 6 4 11 | 6 10 23 | 9 9 16 |
grg | grg 2976 | 7 8 18 | 7 12 24 | 8 11 26 |
igr | igr 2976 | 6 4 11 | 7 8 22 | 8 8 17 |
igs | igs 2976 | 6 4 11 | 6 8 20 | 8 8 15 |
jpl | jpl 2876 | 10 6 18 | 7 10 22 | 8 9 18 |
mit | mit 2976 | 7 4 12 | 7 10 23 | 8 11 26 |
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 6.1715 GPS week: 1715 MJD: 56249.500-56255.500
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 -15 -93 -15 3 | 6 10
| 20 14 79 33 5 | 1
cof uuuuu | -6 -19 99 124 3 | 8 11
| 18 14 29 141 8 | 1
emr uuuuu | -38 3 -107 -118 -7 | 15 21
| 32 15 69 148 4 | 5
esa uuuuu | -32 -40 43 76 2 | 7 10
| 34 20 31 79 5 | 1
gfz uuuuu | 105 56 -35 30 3 | 6 10
| 19 19 101 93 6 | 1
grg uuuux | -19 -33 65 5 10 | -14 30
| 27 23 65 61 16 | 3
igr xxxxx | -39 18 -36 9 0 | 4 8
| 16 8 61 25 5 | 1
irf xxxxx | -8 -13 19 -54 -2 | 3 8
| 16 12 18 41 9 | 2
jpl uuuuu | -8 -20 -78 -98 -5 | 6 17
| 17 21 94 57 11 | 3
mit uuuuu | 6 2 -38 -120 -4 | -2 13
| 24 16 69 68 22 | 4
ngs uuuxu | -23 80 22 -24 3 | 6 9
| 33 29 117 251 6 | 1
sio xxuuu | 211 -168 46 -162 -15 | 15 20
| 63 63 97 84 5 | 6
Table 7.1715.0 GPS week: 1715 Day: 0 MJD: 56249.500
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 | -44 -2 -43 -3 0 | 5 11
cof uuuuu | 15 -41 139 301 6 | 7 11
emr uuuuu | -92 -15 -33 -277 -12 | 23 29
esa uuuuu | 35 -48 61 148 4 | 5 10
gfz uuuuu | 68 60 159 -116 9 | 5 10
grg uuuux | -38 2 -40 -126 21 | -12 31
igr xxxxx | -50 27 -21 44 5 | 3 9
irf xxxxx | -27 2 7 -78 -9 | 7 9
jpl uuuuu | -27 -10 -102 -116 -25 | 12 20
mit uuuuu | -28 21 -113 -110 -17 | 5 9
ngs uuuxu | 19 112 -57 232 12 | 6 10
sio xxxxx | 212 -208 199 -255 -25 | 24 26
Table 7.1715.1 GPS week: 1715 Day: 1 MJD: 56250.500
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 | -24 -40 -45 17 10 | 5 11
cof uuuuu | 7 -3 125 214 14 | 6 9
emr uuuuu | -54 29 -165 -263 -5 | 18 25
esa uuuuu | -27 -58 65 153 8 | 4 9
gfz uuuuu | 96 69 11 -52 9 | 4 9
grg uuuux | -12 -32 78 36 16 | -14 30
igr xxxxx | -26 17 6 30 7 | 3 9
irf xxxxx | -23 2 3 -89 -12 | 5 8
jpl uuuuu | -29 -45 -110 -140 -4 | 7 18
mit uuuuu | -8 15 -120 -163 -31 | 2 9
ngs uuuxu | -10 44 31 303 4 | 5 9
sio xxxxx | 277 -240 12 -279 -13 | 19 22
Table 7.1715.2 GPS week: 1715 Day: 2 MJD: 56251.500
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 | 0 -15 -121 -50 7 | 7 12
cof uuuuu | 16 -26 111 252 4 | 9 11
emr uuuuu | -48 -10 -29 -245 -8 | 17 24
esa uuuuu | -76 -41 59 84 8 | 7 9
gfz uuuuu | 109 57 -118 22 5 | 6 10
grg uuuux | 26 -13 3 33 21 | -12 30
igr xxxxx | -20 22 5 26 3 | 5 9
irf xxxxx | 14 -18 -6 -98 -5 | 4 8
jpl uuuuu | 17 -45 1 -121 -2 | 8 18
mit uuuuu | 24 -3 -91 -173 -13 | -2 12
ngs uuuxu | -18 96 68 63 -7 | 7 9
sio xxxxx | 157 -204 109 -184 -13 | 18 22
Table 7.1715.3 GPS week: 1715 Day: 3 MJD: 56252.500
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 | -28 -5 -74 5 5 | 7 12
cof uuuuu | -11 -1 69 57 7 | 8 11
emr uuuuu | -39 -3 -134 -133 -8 | 14 22
esa uuuuu | -49 -53 15 32 -2 | 8 9
gfz uuuuu | 130 56 -148 140 0 | 7 10
grg uuuux | -13 -28 137 -16 13 | -12 30
igr xxxxx | -32 7 -45 -12 -1 | 5 9
irf xxxxx | 10 -17 36 -44 -1 | 3 9
jpl uuuuu | -9 13 -190 -91 0 | 6 17
mit uuuuu | 37 -6 39 -94 0 | -4 15
ngs uuuxu | -48 118 199 -390 -3 | 6 10
sio xxxxx | 320 -147 54 -106 -16 | 14 20
Table 7.1715.4 GPS week: 1715 Day: 4 MJD: 56253.500
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 | -15 -7 -76 20 5 | 4 8
cof uuuuu | -20 -23 101 113 4 | 8 10
emr uuuuu | 6 12 -158 64 -9 | 9 16
esa uuuuu | -34 -22 -13 134 0 | 6 9
gfz uuuuu | 112 60 -36 34 -3 | 6 9
grg uuuux | -37 -64 105 36 -20 | -13 29
igr xxxxx | -30 9 33 -15 -6 | 3 7
irf xxxxx | -1 -29 38 -66 -5 | 2 8
jpl uuuuu | 6 -6 -54 -168 7 | 2 14
mit uuuuu | 29 -25 8 -220 -9 | -4 15
ngs uuuxu | -73 74 69 -54 6 | 4 8
sio xxuuu | 164 -161 0 -147 -13 | 10 17
Table 7.1715.5 GPS week: 1715 Day: 5 MJD: 56254.500
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 -6 -259 -33 -5 | 7 9
cof uuuuu | -28 -22 92 -99 -7 | 10 12
emr uuuuu | -30 5 -184 27 -1 | 11 16
esa uuuuu | -39 -3 47 46 -2 | 8 10
gfz uuuuu | 117 17 -35 50 2 | 7 10
grg uuuux | -56 -52 50 44 -2 | -17 30
igr xxxxx | -49 21 -83 7 -2 | 3 7
irf xxxxx | -15 -20 30 -20 0 | 2 8
jpl uuuuu | -5 -26 77 -55 1 | 5 15
mit uuuuu | -3 -4 31 -43 2 | -5 15
ngs uuuxu | 9 61 -178 -48 2 | 6 10
sio xxxxx | 181 -170 -114 -38 -13 | 10 17
Table 7.1715.6 GPS week: 1715 Day: 6 MJD: 56255.500
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 | 18 -29 -30 -63 0 | 7 9
cof uuuuu | -18 -16 58 27 -7 | 10 12
emr uuuuu | -9 1 -44 1 -7 | 11 16
esa uuuuu | -32 -56 70 -66 -3 | 8 10
gfz uuuuu | 102 74 -78 134 -6 | 8 10
grg uuuux | -6 -45 121 30 25 | -19 31
igr xxxxx | -63 24 -144 -21 -5 | 4 7
irf xxxxx | -11 -13 28 17 16 | 1 8
jpl uuuuu | -6 -24 -168 1 -16 | 5 15
mit uuuuu | -6 15 -18 -39 40 | -6 15
ngs uuuxu | -39 57 25 -273 6 | 6 10
sio xxxxx | 168 -44 60 -126 -10 | 8 16
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