[IGSREPORT-21297] Wk 1710 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat Nov 3 06:40:35 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1710 (Oct 14, 2012 - Oct 20, 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:
igs1710[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1710[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1710[0-6].cls IGS GPS clock combination summary report.
igs17107.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17107.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 | COD | HOB2 MATE HOB2 MATE
0 | COF | HOB2 KOUC MATE BRMU HOB2 KOUC MATE SUTM
0 | EMR | LPGS HOB2 LPGS YELL
0 | ESA | HOB2 MATE HOB2 MATE
0 | GFZ | ADIS AREQ BOGT LPGS MATE SANT TIXI
0 | GRG | 13 USNO WSRT BRMU MAC1 MAL2 USNO WIND WSRT
0 | MIT | 19 19 MAC1 SOFI
1 | COF | HNPT KOUC HNPT KOUC NKLG
1 | EMR | USNO
1 | ESA | ALRT
1 | GFZ | ALRT BOGT LHAZ SOFI
1 | GRG | 13 13 MCM4 WROC LPGS MCM4 NRMD SOFI VESL WROC WSRT
1 | JPL | NKLG
1 | MIT | 13 15 JOZ2 KERG USNO ALRT JOZ2 USNO
2 | COF | HOB2 HERT HOB2 JOZ2
2 | EMR | HOB2
2 | ESA | NOVM
2 | GFZ | ARTU ASPA SANT
2 | GRG | AREQ WROC AREQ SOFI WROC
2 | JPL | ARTU
2 | MIT | 27 27 JOZ2 JOZ2
3 | COD | NICO NICO
3 | COF | HERT HNPT JOZ2
3 | EMR | KERG MCM4 CRO1 KERG MCM4 YELL
3 | ESA | AREQ
3 | GFZ | BOGT KOSG LHAZ
3 | GRG | NRMD WROC NRMD SOFI THTI WROC
3 | MIT | 7 7 DARW MDVJ SOFI DARW REUN
4 | COD | KOUC KOUC
4 | COF | KOUC MATE KOUC MATE
4 | EMR | 30 MCM4 MCM4
4 | GFZ | 30 BOGT MATE MIZU
4 | GRG | 9 HYDE MATE WROC ALIC ALRT AMC2 ANKR ARTU AUCK BAKE
4 | GRG | BARH BOGT BRFT BRMU BRUX BUCU CAGZ CAS1 CEDU CHPI
4 | GRG | CHTI CHUR COCO CONZ CRO1 DARW DAV1 DRAO DUBO FAIR
4 | GRG | GLSV GOLD GOPE GUAM GUAT GUUG HERT HNPT HOFN HOLM
4 | GRG | HYDE IISC IRKJ IRKT KARR KIT3 KOKB KOUC LAMA LHAZ
4 | GRG | LPGS MAC1 MAL2 MAR6 MAS1 MATE MAW1 MBAR MCM4 MDO1
4 | GRG | MDVJ MKEA NANO NOVM NRC1 NRIL NRMD NTUS NYAL OHI2
4 | GRG | ONSA PALM PDEL PIMO POTS QAQ1 RAMO RESO SCH2 SCOR
4 | GRG | SCUB SEY1 SFER SOFI SPT0 STJO STR1 SYOG THTI THU3
4 | GRG | TIDB TIXI TOW2 TRO1 UNSA URUM USN3 WES2 WHIT WIND
4 | GRG | WROC WSRT WTZR YEBE YELL ZECK
4 | JPL | 30
4 | MIT | 30 30 NICO GMAS NICO
5 | COF | 30 30 KOUC KOUC
5 | EMR | TLSE
5 | ESA | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
5 | ESA | 21 22 23 25 26 28 29 30 31 32 1 2 3 4 5 6 7 8 9 10
5 | ESA | 11 12 13 14 15 16 17 18 19 20 21 22 23 25 26 28 29
5 | ESA | 30 31 32 AREQ AREQ
5 | GFZ | 30 BOGT MDO1 METS SSIA THTI
5 | GRG | ARTU NICO
5 | JPL | 30
5 | MIT | NICO GMAS NICO
6 | COF | HERT KOUC HERT KOUC
6 | EMR | MCM4 TLSE
6 | ESA | AREQ
6 | GFZ | BOGT LHAZ SANT TLSE
6 | GRG | 6 6 MATE PDEL WROC MATE WROC
6 | MIT | MBAR MDVJ MBAR
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
----+--------+---------------
1 | GRG | 27
6 | GRG | 27
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 G03 | | | | | | 2 | |
PRN G24 | 4 | 4 | 4 | | | | 2 |
PRN G77 | | | | | 4 | 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 1.4 .8 -62 2 -10 -.29
COF | 0 | -.1 .9 .6 -66 6 -4 -.16
EMR | 0 | -4.5 .1 13.7 11 6 -6 -.10
ESA | 0 | 2.9 9.4 -9.1 168 -191 92 -.37
GFZ | 0 | -1.0 .2 .6 -55 -22 -25 -.28
GRG | 0 | 4.0 3.0 14.7 -3 56 -18 .04
JPL | 0 | -1.2 10.1 14.6 -61 34 6 .04
MIT | 0 | 5.0 9.5 7.1 10 4 -21 -.17
NGS | 0 | 2.1 -8.7 14.1 -127 -17 -3 .23
COD | 1 | .0 .9 .7 -70 8 -7 -.22
COF | 1 | .4 1.0 1.3 -74 1 -2 -.24
EMR | 1 | -5.8 6.9 11.5 12 5 4 -.05
ESA | 1 | 2.5 10.7 -4.9 153 -191 88 -.39
GFZ | 1 | -.6 .1 1.1 -68 -28 -13 -.23
GRG | 1 | -4.1 8.6 10.3 -22 57 -23 -.07
JPL | 1 | -.1 11.5 15.5 7 -2 -7 .17
MIT | 1 | 2.7 9.0 11.0 4 2 -36 -.11
NGS | 1 | -6.9 1.4 8.7 -61 20 -62 -.02
COD | 2 | -.3 .8 .4 -67 8 1 -.29
COF | 2 | -.3 1.0 .2 -66 12 -2 -.30
EMR | 2 | -1.3 8.6 7.9 18 5 9 -.04
ESA | 2 | 2.8 13.2 -10.0 211 -200 69 -.34
GFZ | 2 | -.5 .2 .2 -58 -38 -16 -.13
GRG | 2 | -2.7 4.4 11.6 1 29 -25 -.06
JPL | 2 | 4.5 4.2 16.0 -23 -3 30 .41
MIT | 2 | 2.7 12.5 10.3 -5 -3 -22 -.03
NGS | 2 | 3.7 3.6 6.9 -33 -19 28 .28
COD | 3 | -.1 .8 .3 -71 2 -2 -.30
COF | 3 | -.1 .6 .1 -71 9 -4 -.29
EMR | 3 | 3.5 3.2 11.0 23 5 3 -.07
ESA | 3 | 6.6 9.0 -5.9 185 -226 99 -.26
GFZ | 3 | -.4 1.0 .1 -54 -24 -35 -.10
GRG | 3 | 3.1 10.5 15.7 6 35 -42 -.19
JPL | 3 | .3 1.7 14.9 -21 -1 48 -.04
MIT | 3 | 7.3 6.1 7.8 -4 -6 -23 -.04
NGS | 3 | 3.1 -.2 14.2 -87 -17 19 .25
COD | 4 | -.6 1.0 .0 -61 5 6 -.26
COF | 4 | -.3 1.2 .1 -56 3 11 -.21
EMR | 4 | 4.5 6.4 8.0 13 -2 8 .08
ESA | 4 | 5.7 1.5 -11.4 67 -264 146 -.20
GFZ | 4 | -.5 .9 .9 -59 -23 -36 -.15
GRG | 4 | 4.3 5.1 18.7 -8 54 -17 -.14
JPL | 4 | 6.2 11.2 18.4 -12 15 30 .13
MIT | 4 | 8.4 6.8 5.6 -2 0 -24 -.11
NGS | 4 | 4.6 1.5 7.3 -43 -24 35 .45
COD | 5 | -.4 1.1 .0 -50 -4 12 -.29
COF | 5 | -.3 1.3 .2 -43 -6 19 -.20
EMR | 5 | 3.9 1.8 5.8 4 0 4 -.05
ESA | 5 | 3.8 2.3 -13.0 103 -223 128 -.43
GFZ | 5 | -.6 .5 .4 -68 -21 -34 -.25
GRG | 5 | 2.9 5.1 8.5 -23 39 -44 -.17
JPL | 5 | 3.3 3.9 15.5 -15 13 48 -.31
MIT | 5 | 8.2 6.9 8.8 -1 3 -32 -.15
NGS | 5 | 2.6 -5.0 5.0 -56 -15 23 .22
COD | 6 | -.5 .8 -.2 -47 3 15 -.34
COF | 6 | -.5 1.1 -.3 -45 8 15 -.45
EMR | 6 | 6.2 7.5 8.3 0 2 0 .02
ESA | 6 | 6.7 1.2 -7.1 61 -230 123 -.61
GFZ | 6 | -.4 .7 .1 -51 -30 -25 -.23
GRG | 6 | .8 -2.0 16.2 -16 64 -39 -.02
JPL | 6 | 6.9 4.1 20.5 -23 20 -20 .05
MIT | 6 | 9.0 7.8 8.7 -1 1 -32 -.17
NGS | 6 | -1.0 -4.9 10.6 -100 -3 -24 .39
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 1.1710.a). It also displays the computed satellite
position sigmas for the combined orbits (table 1.1710.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 2.1710.[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 3.1710.[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 5.1710.0-6).
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 1710 summary. (Oct 14, 2012 - Oct 20, 2012)
Table 1.1710.a GPS week: 1710 MJD: 56214.000-56220.000
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 1 107 -44 0 -.48 11 11 | -973 180 34 94
| 0 0 1 53 36 21 .04 | 479 665
cof 257| 0 0 0 95 -125 9 -.47 12 12 | -922 173 19 87
| 0 0 1 51 38 11 .03 | 487 667
emr 79| -1 0 5 -46 -24 0 .25 18 18 | 1675 161 20 99
| 1 1 1 37 26 10 .03 | 881 1181
esa 174| 0 0 1 -185 207 -7 .02 8 8 | -1326 1043 25 132
| 0 0 1 108 48 16 .03 | 1450 2340
gfz 189| -2 0 -4 82 -22 12 -.42 12 12 | -86 293 22 153
| 0 0 1 62 80 23 .02 | 544 748
grg 130| 1 1 6 3 -120 -11 .41 16 15 | -160 242 17 158
| 1 1 1 46 50 25 .05 | 277 636
igr n/a| 0 0 -1 -2 -55 -24 -.18 5 5 | 4697 32 18 95
| 0 0 1 34 26 13 .02 | 1007 1231
jpl 80| 0 -1 -1 23 -42 21 .40 15 14 | 2392 82 20 127
| 1 1 1 54 40 22 .03 | 963 1270
mit 240| 0 0 -3 -16 -27 -11 -.18 8 8 | -247 322 21 202
| 0 0 0 19 41 23 .02 | 363 539
ngs 241| 0 0 1 136 -39 -4 .36 11 9 | -917 136 1799 3383
| 0 1 2 58 41 28 .02 | 353 506
sio 276| -1 1 -6 -27 -42 -16 -.40 21 20 | --- --- --- ---
| 1 1 1 24 36 12 .03 | --- ---
Table 1.1710.b GPS week : 1710 MJD: 56214.000-56220.000
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 | 5 5 4 4 5 5 4 |
2 | 5 5 5 5 5 5 5 |
3 | 5 4 4 4 4 6 3 |
4 | 4 4 4 3 4 4 4 |
5 | 5 5 5 5 4 4 5 |
6 | 4 4 4 4 4 4 3 |
7 | 5 5 5 5 5 5 5 |
8 | 4 4 5 4 5 5 4 |
9 | 4 4 4 4 4 4 4 |
10 | 4 4 4 4 4 5 5 |
11 | 5 4 4 4 4 4 4 |
12 | 5 5 5 6 5 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 5 5 5 5 5 5 4 |
15 | 5 5 4 4 5 5 4 |
16 | 5 5 5 5 5 5 5 |
17 | 5 4 4 5 5 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 5 4 4 4 4 4 3 |
20 | 4 5 5 5 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 5 4 4 4 4 4 4 |
23 | 5 4 4 5 5 5 5 |
24 | 32 34 38 27 23 30 34 |
25 | 5 5 5 6 6 5 5 |
26 | 4 4 4 4 4 4 4 |
27 | 5 6 7 0 0 0 0 |
28 | 4 5 4 4 5 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 4 5 |
31 | 5 5 5 5 5 5 5 |
32 | 5 4 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
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 2.1710.0 GPS week: 1710 Day: 0 MJD: 56214.000
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 -1 113 0 -14 -.54 12 12 | -1043 106 33 106
| 59 -21 |
cof 255| 0 0 0 99 -105 1 -.47 10 10 | -994 99 19 107
| 38 98 |
emr 80| -4 -3 6 -103 -14 1 .25 19 19 | 3473 -1891 13 89
| 65 -17 |
esa 174| 0 0 1 -297 165 -14 -.04 8 8 | 281 -2535 11 130
| 92 78 |
gfz 189| -1 1 -4 122 -39 10 -.46 13 12 | 992 -1188 19 145
| -80 -45 |
grg 131| 2 0 5 12 -98 0 .46 14 14 | 124 -193 15 176
| 25 17 |
igr n/a| 0 0 -2 -12 -19 -30 -.21 5 5 | 6490 -1794 18 100
| -21 57 |
jpl 80| 0 -3 -2 83 -58 8 .39 15 15 | 4226 -1938 19 126
| 28 0 |
mit 240| 0 0 -4 -19 3 -19 -.19 10 9 | -82 371 24 232
| 15 -8 |
ngs 242| 1 0 2 220 13 6 .39 10 9 | -972 2 2193 3512
| -93 59 |
sio 272| 1 0 -8 -22 -47 -32 -.42 21 19 | --- --- --- ---
| 12 65 |
Table 2.1710.1 GPS week: 1710 Day: 1 MJD: 56215.000
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 0 169 0 18 -.52 12 11 | -798 327 39 85
| 22 -18 |
cof 255| 0 0 -1 158 -62 28 -.54 11 11 | -752 328 17 78
| 50 76 |
emr 80| -1 0 7 -11 16 -5 .22 18 18 | 1379 1265 14 82
| 8 -18 |
esa 174| 0 0 3 -194 172 -24 .02 7 7 | -3007 4296 12 120
| 65 86 |
gfz 190| -2 0 -4 60 -89 43 -.41 12 11 | -657 1146 21 158
| -78 -14 |
grg 131| 2 1 8 78 -86 16 .41 15 14 | -537 758 16 130
| -18 3 |
igr n/a| 0 0 -1 17 -31 -14 -.20 5 5 | 4495 1498 18 90
| 1 75 |
jpl 80| 2 -3 -2 -3 27 39 .37 15 14 | 1958 1480 18 132
| 33 -1 |
mit 240| 0 0 -4 -51 -37 -32 -.16 10 9 | -698 1194 22 192
| 26 -9 |
ngs 239| -1 0 -2 148 -65 -5 .36 10 8 | -932 487 1692 3364
| -40 20 |
sio 270| 1 2 -7 -27 0 -11 -.45 21 20 | --- --- --- ---
| 1 24 |
Table 2.1710.2 GPS week: 1710 Day: 2 MJD: 56216.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 259| 0 0 2 175 -47 32 -.50 12 11 | -567 -257 35 86
| 26 -6 |
cof 258| 0 0 0 160 -153 15 -.46 13 13 | -518 -267 20 80
| 66 103 |
emr 80| -2 2 5 -3 -17 22 .23 19 19 | 1744 373 14 75
| 7 -30 |
esa 174| 0 -1 1 -283 154 -28 .01 8 8 | 594 -530 15 139
| 114 70 |
gfz 189| 0 0 -7 66 47 44 -.43 12 11 | 182 56 23 153
| -56 -19 |
grg 129| 2 2 6 49 -71 17 .43 15 15 | -65 122 16 163
| 6 18 |
igr n/a| 0 0 0 62 -62 -7 -.17 5 5 | 5073 404 19 96
| -5 61 |
jpl 80| -1 -1 -1 104 -16 51 .41 15 14 | 2565 504 17 130
| 10 -22 |
mit 240| 0 0 -2 -15 -23 -42 -.17 7 7 | 165 -211 20 211
| 21 -20 |
ngs 244| 1 0 2 149 -27 18 .36 11 10 | -563 -210 1542 3372
| -86 58 |
sio 266| -1 -1 -6 -18 -54 -28 -.41 19 19 | --- --- --- ---
| 13 60 |
Table 2.1710.3 GPS week: 1710 Day: 3 MJD: 56217.000
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 1 0 121 -63 -28 -.43 12 12 | -751 -668 31 88
| 26 34 |
cof 257| 0 0 1 102 -162 0 -.46 10 11 | -707 -677 17 79
| 23 122 |
emr 79| 0 -1 4 -75 -47 -8 .27 18 18 | 1767 -212 18 93
| 22 -19 |
esa 174| 0 0 0 -292 209 -10 .03 9 9 | -1203 527 14 152
| 97 54 |
gfz 192| -2 0 -4 153 83 13 -.38 11 11 | -314 358 21 143
| -82 0 |
grg 130| 1 1 6 -32 -85 -47 .46 16 15 | 55 374 16 134
| 44 31 |
igr n/a| 0 0 -3 -19 -86 -10 -.16 5 5 | 5217 -755 16 91
| -7 77 |
jpl 80| 0 0 -1 32 -46 39 .44 14 14 | 2912 -631 17 128
| 25 6 |
mit 240| 0 0 -3 13 20 -18 -.16 6 6 | -1 -194 23 194
| -8 -21 |
ngs 245| 0 0 5 122 -76 28 .37 11 11 | -815 -337 1692 3303
| -26 56 |
sio 271| -3 1 -8 21 -4 -2 -.40 20 19 | --- --- --- ---
| -22 44 |
Table 2.1710.4 GPS week: 1710 Day: 4 MJD: 56218.000
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 3 79 -87 1 -.48 12 10 | -589 -210 39 100
| 58 31 |
cof 260| 1 0 2 67 -161 -3 -.43 13 13 | -503 -217 25 84
| 45 109 |
emr 80| 0 0 4 -68 -67 -3 .21 17 17 | 1192 86 50 125
| 25 12 |
esa 174| 0 0 0 -57 287 1 .04 7 7 | -867 114 21 123
| -50 -9 |
gfz 193| -3 0 -4 142 -87 -6 -.44 11 11 | -236 270 27 160
| -80 -16 |
grg 131| 0 0 7 -54 -180 -17 .35 16 15 | 39 -742 21 221
| 75 39 |
igr n/a| 0 0 -2 -38 -80 -27 -.17 5 5 | 4198 -424 25 99
| -24 58 |
jpl 80| -1 -3 -1 -40 -92 -13 .38 15 15 | 1960 -422 37 136
| 46 4 |
mit 240| 0 0 -3 -10 -65 7 -.19 9 9 | 63 -164 25 155
| -18 -30 |
ngs 243| 1 1 0 27 -40 7 .34 11 10 | -457 -450 2056 3523
| -43 48 |
sio 289| -2 1 -5 -44 -104 -26 -.37 20 20 | --- --- --- ---
| 15 70 |
Table 2.1710.5 GPS week: 1710 Day: 5 MJD: 56219.000
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 1 68 -28 -14 -.44 10 10 | -1955 1357 32 101
| 47 -1 |
cof 260| 0 0 0 53 -91 13 -.49 12 12 | -1914 1355 19 92
| 61 83 |
emr 79| -1 0 4 -18 -13 -2 .28 17 17 | 1533 -255 17 129
| 15 -14 |
esa 174| 0 0 0 -100 247 6 .07 7 7 | -2117 2353 93 154
| -3 33 |
gfz 189| -1 1 -2 58 -118 -7 -.43 13 13 | -108 570 24 156
| -57 2 |
grg 130| 1 3 4 -6 -120 -13 .35 17 16 | -202 151 18 151
| 63 9 |
igr n/a| 0 0 0 4 -34 -37 -.16 4 4 | 4017 -323 19 100
| -9 75 |
jpl 80| -1 -1 0 16 -35 13 .42 14 14 | 1836 -130 18 120
| 49 3 |
mit 240| 0 0 -2 -9 -93 4 -.19 7 7 | -626 594 19 210
| -21 -16 |
ngs 242| 0 -2 2 117 11 -29 .35 12 10 | -1482 709 1625 3257
| -70 38 |
sio 282| -1 1 -4 -52 -60 -7 -.35 21 21 | --- --- --- ---
| 14 42 |
Table 2.1710.6 GPS week: 1710 Day: 6 MJD: 56220.000
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 2 27 -84 11 -.45 10 9 | -1114 610 35 96
| 63 50 |
cof 256| 2 0 1 26 -141 9 -.46 11 11 | -1067 596 21 95
| 56 90 |
emr 79| 0 0 2 -44 -26 -9 .27 16 16 | 640 1767 16 100
| -21 -39 |
esa 174| 1 0 1 -68 217 15 .04 7 7 | -2963 3081 10 106
| -28 35 |
gfz 185| -3 1 -3 -28 46 -9 -.42 13 13 | -463 842 23 161
| -19 -22 |
grg 130| 0 0 5 -20 -199 -38 .36 18 17 | -536 1224 18 137
| 38 88 |
igr n/a| 0 0 0 -32 -75 -43 -.19 5 4 | 3390 1623 17 91
| -21 61 |
jpl 80| -2 0 -4 -27 -78 9 .42 14 13 | 1288 1714 17 121
| 22 11 |
mit 240| 0 0 -2 -23 6 23 -.23 8 7 | -553 670 20 223
| -21 -49 |
ngs 237| 0 -1 1 168 -91 -54 .33 10 8 | -1199 755 1798 3354
| -114 67 |
sio 286| -3 1 -5 -46 -26 -7 -.41 24 22 | --- --- --- ---
| -21 42 |
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 3.1710.0 GPS week: 1710 Day: 0 MJD: 56214.000
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 | 12 13 21 11 10 13 5 14 12 9 16 4 | 23 26 25 33 28 42 29 44 31 38 30 32
2 | 10 8 20 8 15 13 6 17 11 11 22 4 | 17 19 28 24 24 28 19 24 19 23 19 20
3 | 10 10 15 7 14 13 6 14 9 13 27 4 | 29 26 30 27 24 33 28 31 27 38 22 28
4 | 12 10 13 7 10 12 5 12 8 11 23 3 | 16 18 20 21 28 17 20 18 20 20 21 19
5 | 14 8 20 7 11 17 5 19 12 10 18 4 | 42 43 49 44 46 48 41 43 43 45 38 43
6 | 11 10 14 8 15 9 4 12 8 11 18 4 | 20 19 24 23 27 26 20 28 22 23 23 20
7 | 12 10 19 10 10 14 4 17 9 9 18 4 | 33 34 39 33 34 38 36 38 37 37 34 34
8 | 17 10 16 7 13 13 7 12 13 9 19 4 | 10 15 20 15 19 16 12 15 14 20 20 13
9 | 14 11 16 8 14 16 6 13 7 9 18 4 | 11 13 23 19 20 24 18 24 17 23 18 17
10 | 11 8 14 5 14 13 4 13 9 12 29 4 | 19 19 21 18 29 17 20 20 22 26 28 20
11 | 8 10 16 8 12 17 6 17 8 12 11 4 | 24 25 38 32 31 45 28 40 28 33 31 31
12 | 12 11 22 9 12 17 9 19 9 8 18 4 | 31 35 45 36 37 37 35 37 36 35 38 35
13 | 9 8 15 7 10 16 5 15 10 10 21 4 | 23 24 31 27 26 34 24 30 25 25 23 24
14 | 11 12 18 9 14 16 5 14 8 12 18 4 | 22 27 30 29 30 32 25 28 25 32 27 27
15 | 13 10 19 8 12 16 4 20 10 11 21 4 | 21 25 32 31 28 35 25 31 24 30 17 26
16 | 12 11 22 7 15 15 6 18 11 10 21 5 | 32 34 40 32 27 42 30 37 29 36 29 32
17 | 12 11 20 9 13 12 6 18 10 9 34 4 | 21 23 28 26 31 24 23 25 22 24 23 23
18 | 11 8 18 10 14 16 5 14 8 8 13 4 | 27 29 30 27 32 27 27 29 27 29 29 27
19 | 10 11 18 9 12 10 4 15 10 12 26 4 | 15 19 29 24 22 24 20 27 19 24 19 20
20 | 10 11 17 7 9 12 4 18 10 8 15 4 | 57 59 62 59 61 64 58 60 57 59 63 59
21 | 11 8 12 8 12 17 5 12 10 12 14 4 | 15 16 18 13 21 19 11 17 12 15 14 12
22 | 9 9 22 9 16 18 6 11 6 7 10 4 | 39 40 39 36 43 38 36 38 38 36 41 36
23 | 10 12 17 9 9 11 5 17 10 14 24 4 | 34 37 40 34 36 38 33 39 34 39 35 35
X24 | 45 25 --- --- --- 39 70 --- --- --- --- 31 | 48 42 --- --- --- 51 40 --- --- --- --- 44
25 | 10 13 30 10 10 16 7 16 9 5 24 5 | 34 35 43 38 34 35 33 37 32 34 43 34
26 | 11 10 15 8 15 13 5 11 8 12 15 4 | 18 19 25 25 26 30 19 25 21 21 19 22
X27 | 15 10 18 10 17 17 8 13 10 --- --- 5 | 33 28 15 13 17 9999 25 16 13 --- --- 32
28 | 11 6 18 8 16 17 5 14 8 8 14 4 | 24 23 30 25 27 32 22 25 23 26 26 23
29 | 15 13 22 7 12 13 5 18 10 9 32 4 | 23 25 29 18 26 20 21 27 23 23 22 20
30 | 14 11 18 7 10 14 5 13 9 8 29 4 | 26 30 31 29 29 29 27 29 27 30 37 28
31 | 13 12 24 7 13 16 3 18 8 10 15 5 | 18 20 26 18 22 28 16 24 14 22 15 17
32 | 11 12 20 8 10 12 5 15 12 9 23 4 | 24 27 31 24 28 24 24 32 24 26 29 25
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 10 19 8 13 14 5 15 10 10 21 |T 25 27 31 27 29 32 26 30 25 29 27 27
WRMS | 12 10 19 8 12 14 5 15 9 9 19 |NE 20 22 26 24 25 30 22 27 21 25 21 23
MEDI | 11 10 18 8 12 14 5 15 9 10 18 |MD 23 25 30 27 28 32 25 29 24 26 26 26
Table 3.1710.1 GPS week: 1710 Day: 1 MJD: 56215.000
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 | 10 13 23 7 10 12 5 13 8 9 13 4 | 20 24 22 30 30 39 25 39 28 33 27 28
2M | 9 10 20 7 12 13 4 16 11 12 32 4 | 25 26 29 29 29 33 25 28 25 32 31 27
3M | 9 11 12 5 11 9 4 12 8 6 23 3 | 33 32 34 33 31 33 31 34 30 37 33 31
4 | 8 11 13 4 7 11 4 11 10 11 20 3 | 15 17 16 13 22 14 15 18 17 18 19 15
5 | 12 8 18 5 8 16 5 17 14 10 14 4 | 25 29 31 27 27 36 26 31 24 33 24 27
6M | 8 11 12 7 14 10 4 11 10 11 18 4 | 19 21 25 22 25 26 21 28 21 31 23 21
7M | 23 10 17 7 10 24 6 18 9 11 18 4 | 60 67 68 69 69 58 67 69 67 69 64 65
8 | 15 12 15 6 12 9 6 14 12 8 16 4 | 11 16 17 12 16 13 10 19 13 16 20 12
9 | 14 13 14 8 13 17 5 12 12 7 17 4 | 10 12 20 13 15 21 14 19 18 20 19 13
10 | 11 9 18 4 11 12 5 14 9 10 29 4 | 20 21 22 18 27 20 19 18 20 19 25 17
11 | 10 9 19 7 10 15 5 10 9 10 12 4 | 21 21 35 25 26 40 22 33 24 27 25 25
12M | 12 10 19 7 12 14 5 16 10 11 38 4 | 35 33 38 33 37 40 30 35 33 36 38 33
13M | 10 11 16 5 11 21 4 13 8 12 15 4 | 15 19 28 19 25 33 16 29 19 26 13 20
14M | 10 12 19 6 15 14 4 18 8 8 16 4 | 22 28 31 26 27 28 22 29 21 25 28 24
15 | 15 16 17 9 12 16 6 17 11 7 19 4 | 16 19 27 21 23 31 19 27 20 26 16 20
16M | 13 12 20 8 13 19 5 18 9 9 22 4 | 20 24 31 24 26 33 20 25 20 24 22 22
17 | 8 8 18 8 13 11 3 15 10 11 32 4 | 15 14 21 17 25 16 15 21 18 15 21 16
18 | 10 6 15 6 13 15 3 14 6 10 12 4 | 24 26 24 24 23 20 23 23 20 28 24 22
19 | 8 12 16 6 9 9 5 12 8 12 23 3 | 15 16 21 16 19 17 14 23 13 20 14 14
20E | 28 16 17 7 12 20 8 15 11 10 13 4 | 71 80 82 82 78 82 77 81 79 81 79 79
21M | 7 7 14 7 11 20 4 13 8 11 11 4 | 15 17 20 13 15 22 13 19 12 19 14 13
22 | 9 11 16 7 13 16 4 12 6 7 9 4 | 29 30 28 26 28 27 25 27 23 30 28 25
23M | 8 11 18 8 10 14 4 17 8 10 25 4 | 23 29 32 28 22 29 23 32 23 30 29 25
X24 | 64 28 --- --- --- 39 72 --- --- --- --- 33 | 40 42 --- --- --- 50 52 --- --- --- --- 43
25M | 11 13 31 8 9 16 7 19 9 12 28 5 | 37 38 42 36 39 41 34 41 35 35 44 36
26 | 9 14 14 6 11 12 4 11 9 7 14 3 | 18 18 23 21 22 25 20 24 21 22 22 20
X27M | 17 15 18 10 16 >>>> 6 14 12 --- --- 6 | 34 28 14 15 14 9999 35 17 13 --- --- 29
28 | 11 7 18 6 17 16 5 13 12 10 10 4 | 17 18 22 19 26 27 16 20 19 20 21 18
29M | 10 15 18 9 9 13 4 17 10 6 33 4 | 17 24 22 16 18 14 16 23 17 20 19 15
30M | 15 11 16 8 12 14 3 15 9 11 21 4 | 50 53 51 51 54 54 48 50 52 50 52 51
31 | 10 12 20 10 13 17 4 20 10 12 12 5 | 15 17 24 19 20 26 11 27 14 24 16 15
32M | 13 10 19 8 9 11 5 14 11 7 25 4 | 25 28 30 29 28 25 25 30 24 30 35 26
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 11 18 7 12 15 5 15 10 10 21 |T 25 27 30 26 28 31 25 30 25 29 28 26
WRMS | 11 11 18 7 11 14 5 14 9 8 20 |NE 17 19 22 18 22 26 19 24 18 21 20 19
MEDI | 10 11 18 7 12 14 5 14 9 10 18 |MD 20 24 27 24 26 28 22 27 21 26 24 22
Table 3.1710.2 GPS week: 1710 Day: 2 MJD: 56216.000
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 13 22 8 11 15 4 13 5 10 15 4 | 24 26 24 30 26 39 27 41 29 35 29 29
2 | 10 13 22 8 14 16 5 18 6 11 22 4 | 24 26 28 24 26 27 24 27 25 28 27 23
3 | 10 13 15 7 11 13 3 12 6 14 21 4 | 32 33 36 31 35 30 30 35 32 33 25 31
4 | 11 11 16 8 8 12 3 10 5 9 17 3 | 20 24 21 20 23 18 21 22 25 26 23 21
5 | 14 11 20 8 10 18 6 19 8 11 16 4 | 28 31 35 24 27 29 26 32 29 30 29 26
6 | 9 12 15 8 13 11 3 12 6 15 13 4 | 27 28 31 26 27 28 23 33 26 23 21 24
7 | 18 14 16 8 12 17 4 18 8 11 14 4 | 35 27 32 24 29 33 28 31 33 32 25 28
8 | 15 11 21 9 13 13 6 12 9 10 17 4 | 15 18 22 15 20 15 14 20 17 22 22 15
9 | 14 13 15 8 13 15 5 11 6 6 18 3 | 15 16 20 20 16 21 15 22 19 22 22 16
10 | 13 11 20 8 12 14 4 12 7 10 26 4 | 23 25 25 22 29 19 22 24 24 24 27 22
11 | 10 13 18 11 8 18 4 10 5 10 17 4 | 25 25 38 30 29 41 27 38 29 31 31 29
12 | 13 14 21 8 13 17 5 18 9 11 17 5 | 31 34 37 35 34 39 31 35 35 34 33 33
13 | 7 13 15 9 12 17 4 13 6 11 15 4 | 21 23 30 19 21 35 21 31 23 25 16 21
14 | 11 15 19 9 11 16 4 15 6 12 18 4 | 23 27 32 24 25 28 23 30 27 28 29 25
15 | 15 10 18 10 11 16 4 17 6 9 19 4 | 19 22 29 24 22 31 21 30 24 29 19 23
16 | 14 17 21 7 12 16 5 16 7 11 19 4 | 26 30 35 25 26 33 25 31 27 33 28 26
17 | 12 14 21 7 12 10 5 16 7 9 29 4 | 22 24 27 21 28 23 22 27 27 23 26 23
18 | 10 15 16 6 12 17 4 14 5 13 16 4 | 26 27 29 25 25 30 28 28 28 33 29 26
19 | 9 14 14 8 8 11 4 14 6 12 23 4 | 20 23 26 19 20 20 17 28 22 25 17 19
20E | 21 11 18 10 11 14 7 16 8 10 15 4 | 45 61 63 60 58 63 58 63 59 59 61 59
21 | 10 9 16 5 11 17 5 12 5 12 11 3 | 18 19 21 14 15 21 13 19 17 20 20 13
22 | 11 12 16 6 12 18 4 11 6 8 18 4 | 26 29 25 21 24 28 24 25 25 23 25 22
23 | 8 13 17 11 10 12 4 18 5 11 22 4 | 31 35 35 30 30 36 31 39 31 32 31 30
X24 | 69 32 --- --- --- 43 56 --- --- --- --- 37 | 109 99 --- --- --- 114 84 --- --- --- --- 103
25 | 10 17 27 8 8 16 5 17 9 11 17 5 | 32 34 32 35 30 37 31 37 33 36 39 32
26 | 9 15 16 9 11 13 5 11 7 10 11 4 | 15 15 19 18 14 22 15 20 17 19 19 15
X27 | 21 18 --- 10 15 --- 8 17 9 --- --- 6 | 42 38 --- 12 14 --- 45 21 12 --- --- 36
28 | 12 10 22 7 15 14 5 15 7 7 13 4 | 22 23 29 20 26 29 21 28 24 26 25 22
29 | 12 17 21 9 13 16 5 19 10 13 27 5 | 23 29 25 20 24 22 19 28 23 24 18 20
30 | 17 15 16 7 13 17 7 12 8 10 28 4 | 28 30 34 25 25 29 26 33 27 32 32 26
31 | 13 15 24 10 14 17 4 19 5 8 12 5 | 23 26 27 19 20 29 18 27 21 25 17 19
32 | 11 11 16 10 11 12 7 14 9 11 19 4 | 20 23 25 23 23 23 21 30 23 24 27 21
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 13 19 8 12 15 5 15 7 11 19 |T 27 29 29 24 25 32 26 30 26 28 26 27
WRMS | 11 13 19 8 11 15 5 14 7 10 19 |NE 27 28 25 21 22 33 25 27 23 25 22 27
MEDI | 11 13 18 8 12 16 5 14 6 11 17 |MD 24 26 29 24 25 29 23 30 25 26 25 23
Table 3.1710.3 GPS week: 1710 Day: 3 MJD: 56217.000
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 11 22 9 12 16 6 11 5 10 18 4 | 33 35 33 36 32 41 36 45 34 41 37 35
2 | 10 6 21 11 13 14 5 18 6 10 23 4 | 21 22 30 24 22 26 23 27 21 26 22 22
3 | 11 11 14 5 11 13 3 12 6 13 21 3 | 51 48 53 46 45 49 48 52 48 54 43 48
4 | 9 8 15 7 9 13 4 11 6 7 20 3 | 24 25 25 23 23 23 25 25 23 26 22 23
5 | 9 6 20 8 9 22 4 18 7 9 17 4 | 27 25 35 24 26 35 25 34 25 29 25 26
6 | 10 9 14 6 12 10 3 8 4 14 14 3 | 20 20 31 25 25 27 23 31 23 25 21 23
7 | 11 12 18 8 13 15 4 17 7 11 16 4 | 44 45 50 43 42 49 45 47 45 51 44 44
8 | 13 10 16 10 12 12 5 13 8 11 18 4 | 19 20 27 16 19 17 21 23 18 25 23 18
9 | 14 9 17 10 14 13 5 13 7 12 16 4 | 19 22 29 22 17 28 20 26 19 28 23 20
10 | 11 10 19 6 10 20 5 11 6 11 27 4 | 32 32 35 30 32 30 32 31 31 33 34 30
11 | 10 9 18 9 10 17 4 10 4 15 13 4 | 27 29 39 31 31 43 31 38 30 39 34 32
12 | 16 9 24 11 17 20 6 21 8 12 21 5 | 36 42 46 41 44 41 41 42 41 45 41 41
13 | 9 10 15 8 13 19 3 13 5 12 15 4 | 28 30 37 28 30 40 29 37 28 30 23 29
14 | 14 12 19 15 14 17 6 14 10 13 18 5 | 26 28 32 29 29 35 28 30 24 31 26 26
15 | 11 10 16 10 9 15 6 17 6 8 20 4 | 29 31 34 30 27 37 27 36 24 32 24 28
16 | 12 14 20 10 11 14 4 16 6 15 19 4 | 28 30 33 24 23 34 26 32 26 35 27 27
17 | 17 14 18 9 10 12 2 16 7 11 31 4 | 23 22 31 26 25 22 25 30 24 29 26 24
18 | 9 7 19 8 10 15 4 15 5 11 14 4 | 69 72 71 69 72 73 68 71 68 70 68 69
19 | 10 11 18 9 10 10 5 12 6 15 23 4 | 20 21 31 25 23 25 22 26 20 22 20 21
20E | 8 12 19 9 12 11 6 14 9 12 13 4 | 53 58 60 57 56 59 59 61 55 58 59 56
21 | 12 6 14 9 7 17 4 13 5 10 17 3 | 17 21 25 20 19 27 20 24 19 22 20 19
22 | 12 7 19 10 12 17 4 11 5 8 14 4 | 44 48 50 49 52 50 46 47 46 50 47 48
23 | 11 13 18 10 11 14 5 17 5 11 23 4 | 30 32 37 30 29 32 31 38 30 32 29 30
X24 | 64 20 --- --- --- 36 67 --- --- --- --- 27 | 113 135 --- --- --- 141 157 --- --- --- --- 135
25 | 13 17 27 10 10 21 6 17 8 15 23 5 | 46 53 54 50 50 49 47 49 47 51 58 48
26 | 8 8 14 10 10 14 5 9 6 11 11 3 | 24 26 31 27 28 33 26 28 25 30 24 26
X27 | 71 13 --- --- --- --- 420 --- --- --- --- 0 | 111 84 --- --- --- --- 125 --- --- --- --- 84
28 | 11 9 20 9 13 15 3 14 6 12 14 4 | 24 25 34 26 26 30 27 32 25 29 24 25
29 | 15 11 18 9 10 16 5 18 7 12 31 4 | 30 31 34 31 30 30 30 35 30 32 28 29
30 | 11 12 14 5 10 13 5 11 6 10 28 3 | 42 44 43 43 41 40 39 41 41 47 42 42
31 | 13 9 21 9 11 18 3 19 7 8 17 4 | 22 22 29 18 19 28 20 27 19 26 18 19
32 | 12 10 21 8 10 13 4 13 6 10 20 4 | 28 30 36 26 27 25 29 36 27 32 34 27
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 10 18 9 11 16 5 14 6 11 20 |T 36 37 37 32 32 39 39 36 31 36 32 36
WRMS | 12 11 18 9 11 15 5 14 6 11 19 |NE 31 34 31 25 24 39 36 30 23 29 25 33
MEDI | 11 10 18 9 11 15 5 13 6 11 18 |MD 28 30 34 28 28 34 29 34 26 32 26 28
Table 3.1710.4 GPS week: 1710 Day: 4 MJD: 56218.000
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 14 21 8 11 15 5 16 6 12 12 4 | 26 28 21 29 25 40 27 40 29 36 30 28
2 | 8 8 22 7 14 15 6 18 6 9 22 4 | 16 18 29 19 20 25 19 26 19 27 21 18
3 | 10 14 10 4 10 12 4 11 6 10 25 3 | 46 44 47 47 42 46 45 49 45 47 45 46
4 | 8 10 15 8 8 15 4 13 7 6 20 3 | 15 16 19 17 20 15 16 15 18 18 17 14
5E | 11 7 18 7 9 11 5 20 11 9 20 4 | 27 32 39 33 34 39 33 41 34 40 36 33
6 | 8 13 11 5 12 11 3 11 8 12 17 3 | 18 19 28 24 24 26 22 28 24 28 20 22
7 | 9 15 16 7 11 18 4 15 9 11 18 4 | 20 19 25 20 22 30 18 26 19 28 15 19
8 | 12 11 15 8 13 14 6 15 11 12 22 4 | 13 14 21 14 14 15 13 18 17 22 22 14
9 | 11 10 15 7 13 15 5 16 7 10 16 4 | 14 16 23 19 17 22 16 24 17 24 16 16
10 | 14 10 19 6 11 21 4 13 8 9 29 4 | 23 26 29 20 25 31 22 24 25 23 28 21
11 | 10 10 16 7 10 18 3 11 7 15 10 4 | 22 22 34 25 26 39 24 34 26 27 26 25
12 | 13 12 22 8 11 19 6 19 10 14 17 5 | 28 30 39 35 32 32 35 37 38 38 34 33
13 | 8 13 15 6 12 17 3 13 9 11 19 4 | 22 24 29 26 24 35 23 30 26 23 15 24
14 | 9 15 17 5 20 14 5 14 12 9 16 4 | 18 21 28 22 28 27 22 28 23 24 20 22
15 | 10 10 15 8 12 16 4 17 8 12 20 4 | 17 16 25 21 20 31 18 26 19 25 17 19
16 | 10 14 22 6 11 15 7 16 10 9 19 4 | 21 21 28 20 25 29 19 26 26 26 19 21
17 | 10 13 20 8 11 12 3 18 9 8 28 4 | 19 18 22 20 24 17 20 22 21 21 22 18
18E | 28 20 12 4 12 13 9 13 9 10 13 4 | 104 106 105 104 105 104 101 105 106 103 102 104
19 | 9 13 13 5 10 10 4 14 8 12 24 3 | 14 17 25 20 22 18 17 27 21 18 16 18
20E | 10 14 14 5 11 21 3 15 8 8 17 4 | 34 35 35 35 35 36 34 35 33 33 35 34
21 | 8 9 14 4 10 16 4 12 8 11 21 3 | 16 17 20 14 19 21 15 18 17 19 24 15
22E | 22 13 13 6 12 15 5 9 8 6 10 3 | 75 72 72 73 75 75 71 75 74 72 73 72
23 | 11 15 17 9 12 14 4 16 10 12 26 4 | 19 23 28 23 23 27 22 28 24 23 15 22
X24 | 47 18 --- --- --- 29 77 --- --- --- --- 23 | 150 146 --- --- --- 156 162 --- --- --- --- 150
25 | 13 21 27 8 11 19 5 17 9 10 18 5 | 35 39 40 38 37 36 38 38 38 39 37 35
26 | 8 12 13 6 9 12 3 9 8 13 12 3 | 16 17 21 18 20 26 17 23 19 20 19 17
X27 | >>>> 12 --- --- --- --- >>>> --- --- --- --- 0 | 6 447 --- --- --- --- 568 --- --- --- --- 448
28 | 10 12 18 7 13 17 4 16 9 9 15 4 | 20 20 25 21 23 28 21 25 23 23 23 20
29 | 9 13 18 9 9 15 8 19 11 10 28 4 | 22 24 28 24 23 20 25 28 29 28 21 22
30 | 11 14 13 6 9 13 3 10 9 12 24 4 | 26 28 32 29 31 29 29 30 36 29 31 29
31 | 9 12 18 7 13 22 4 18 10 13 16 5 | 16 18 25 18 22 29 17 26 19 25 18 17
32 | 12 11 16 6 9 16 4 12 8 9 18 4 | 20 21 27 18 20 21 18 25 20 21 25 19
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 13 17 7 11 16 5 15 9 11 20 |T 29 44 32 28 29 36 48 32 29 31 28 44
WRMS | 10 13 17 7 11 15 5 15 9 10 20 |NE 28 29 23 20 21 36 30 25 20 23 20 29
MEDI | 10 13 16 7 11 15 4 15 8 10 18 |MD 20 21 28 21 24 29 22 27 24 25 22 22
Table 3.1710.5 GPS week: 1710 Day: 5 MJD: 56219.000
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 | 10 12 21 8 12 14 5 12 6 12 15 4 | 28 28 30 37 30 42 32 43 32 41 37 34
2 | 7 13 18 6 15 16 6 16 6 10 22 4 | 15 18 21 17 20 23 15 22 15 24 22 15
3 | 16 19 20 7 13 37 8 17 7 18 32 6 | 71 73 68 69 62 60 66 68 64 67 68 65
4 | 7 10 15 6 11 13 4 9 5 10 20 3 | 14 16 18 16 22 17 14 16 17 15 16 14
5E | 10 9 17 7 11 11 3 16 9 8 14 4 | 26 31 33 32 34 33 29 33 29 34 31 30
6 | 8 12 11 5 12 13 2 10 5 11 15 3 | 17 17 25 24 15 22 21 28 18 26 17 19
7 | 12 15 14 10 12 24 3 18 7 11 17 5 | 34 37 40 38 34 44 35 43 35 39 37 36
8 | 11 11 18 9 13 18 4 13 10 13 21 4 | 12 15 22 16 16 16 10 20 13 18 20 12
9 | 9 10 17 7 15 14 4 11 8 11 25 4 | 12 12 23 12 18 21 10 20 15 20 17 12
10E | 14 14 19 5 16 17 5 14 8 13 33 4 | 28 29 35 29 39 33 29 32 32 29 34 29
11 | 8 11 16 8 8 16 5 12 7 13 14 4 | 21 21 40 27 24 40 23 38 26 31 27 27
12 | 13 10 21 10 15 15 4 18 7 12 14 5 | 28 28 32 32 32 34 29 31 29 38 24 30
13 | 10 12 13 7 12 20 5 13 6 8 21 4 | 19 22 29 23 23 34 21 31 23 23 13 22
14 | 10 13 14 7 14 18 4 14 10 12 15 4 | 19 22 27 26 21 25 21 28 18 25 21 21
15 | 10 13 15 9 13 18 3 12 8 13 25 4 | 15 19 24 21 24 32 18 28 18 25 18 19
16 | 8 12 16 7 13 19 4 15 6 13 20 4 | 19 19 24 20 21 26 18 26 19 25 19 18
17 | 10 9 18 7 13 13 4 14 6 8 29 4 | 19 16 21 15 21 19 14 20 17 15 17 15
18E | 12 8 14 7 14 15 5 14 8 10 13 4 | 47 50 47 46 40 46 47 51 45 46 44 45
19 | 10 14 13 6 9 13 3 12 5 15 25 4 | 17 18 25 19 18 20 15 26 17 25 15 17
20E | 8 12 12 5 12 14 4 14 7 14 15 4 | 26 29 31 30 25 31 26 31 26 30 23 27
21 | 8 9 14 6 12 17 4 13 7 9 30 4 | 14 16 25 17 19 25 16 25 18 19 32 16
22E | 9 9 15 7 12 15 4 13 8 8 12 3 | 30 31 31 27 27 28 28 31 27 27 28 26
23 | 10 13 15 7 15 16 5 16 8 13 25 4 | 17 23 26 22 19 25 18 28 19 21 11 18
X24 | 49 22 --- --- --- 40 50 --- --- --- --- 30 | 101 95 --- --- --- 110 95 --- --- --- --- 98
25 | 10 20 24 8 10 17 3 16 9 13 20 5 | 26 31 27 25 26 29 24 29 26 33 28 25
26 | 8 12 13 6 11 14 3 9 7 15 14 4 | 22 24 26 23 27 30 21 29 24 25 26 23
X27 | 46 10 --- --- --- --- 73 --- --- --- --- 0 | 5 217 --- --- --- --- 257 --- --- --- --- 217
28 | 8 8 16 8 13 18 5 12 8 10 17 4 | 17 18 23 19 20 26 16 23 18 19 19 17
29 | 9 14 21 9 13 14 4 17 8 9 31 4 | 19 23 30 19 22 20 17 24 20 25 19 19
30 | 12 11 12 7 10 13 4 10 7 10 23 3 | 34 33 36 33 33 32 32 39 35 36 39 33
31 | 13 13 15 6 13 23 6 14 8 13 17 4 | 17 18 26 17 18 28 15 23 13 22 16 15
32 | 13 10 18 6 12 15 5 12 7 9 19 4 | 21 22 31 23 22 26 20 30 23 24 29 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 12 17 7 13 17 4 14 7 12 21 |T 25 33 29 25 25 32 32 30 24 28 25 32
WRMS | 10 12 17 7 13 16 4 14 7 10 21 |NE 24 25 25 20 21 33 23 26 19 23 20 25
MEDI | 10 12 15 7 12 16 4 13 7 11 20 |MD 19 22 27 23 22 28 21 28 20 25 22 22
Table 3.1710.6 GPS week: 1710 Day: 6 MJD: 56220.000
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 | 10 10 18 8 11 18 4 13 7 13 20 4 | 30 32 32 36 30 46 33 48 33 40 42 35
2 | 7 8 22 8 18 18 5 15 7 11 30 4 | 24 25 31 21 20 26 21 28 21 26 34 21
3 | 11 12 10 5 11 12 6 9 6 9 25 3 | 57 55 53 53 54 51 54 52 53 52 55 52
4 | 9 9 14 6 11 13 4 8 8 11 20 3 | 18 19 23 16 19 17 16 20 18 18 17 16
5E | 10 12 20 7 14 17 6 18 8 10 18 4 | 34 36 34 29 31 31 31 34 28 34 27 30
6 | 9 11 10 5 14 11 4 8 5 9 16 3 | 21 21 29 25 28 28 24 30 25 32 23 25
7 | 9 15 16 8 13 22 4 19 8 10 20 5 | 23 25 31 23 23 32 22 32 24 27 21 23
8 | 12 8 15 7 11 18 4 11 8 7 23 3 | 16 19 25 17 15 23 16 24 17 22 25 17
9 | 9 12 17 6 14 15 4 11 8 11 30 4 | 16 19 23 15 18 25 15 22 16 21 19 15
10E | 15 14 20 7 16 17 6 16 9 12 30 5 | 28 31 39 28 26 38 28 35 28 33 29 28
11 | 8 8 13 8 10 20 4 13 7 13 17 4 | 26 27 41 32 30 44 29 41 31 32 34 31
12 | 7 14 19 6 14 19 5 18 8 10 20 4 | 29 32 33 27 26 35 25 31 26 32 25 27
13 | 8 9 14 7 14 21 3 15 6 9 23 4 | 25 27 35 28 28 40 26 34 26 30 22 27
14 | 9 15 13 5 13 20 4 14 9 8 17 4 | 18 26 27 21 27 33 20 27 19 25 18 22
15 | 8 8 16 9 12 18 6 15 9 6 31 4 | 17 19 27 24 24 36 21 28 20 26 27 21
16 | 8 12 20 7 15 18 4 16 6 7 19 4 | 25 27 32 24 23 30 22 28 23 28 21 24
17 | 9 10 18 5 13 12 4 13 7 7 30 3 | 24 25 28 21 28 21 21 26 21 22 25 22
18E | 9 12 11 6 14 16 3 14 7 8 16 4 | 39 44 44 42 41 44 41 42 42 41 45 40
19 | 11 14 11 4 11 12 5 11 5 7 29 3 | 22 23 28 24 23 22 21 27 20 25 22 21
20E | 7 9 14 7 11 13 3 12 9 9 15 3 | 49 51 53 51 52 52 50 54 52 53 57 51
21 | 8 7 14 6 15 16 4 12 5 7 31 3 | 14 16 25 16 17 25 12 21 14 17 27 15
22E | 9 8 17 5 13 16 3 10 7 9 18 3 | 50 50 48 47 47 49 47 50 48 43 53 46
23 | 10 13 18 9 14 19 3 17 6 10 28 4 | 27 31 34 30 28 35 27 33 29 30 29 28
X24 | 49 27 --- --- --- 43 61 --- --- --- --- 34 | 130 118 --- --- --- 146 107 --- --- --- --- 128
25 | 11 16 23 10 12 21 4 16 9 10 28 5 | 50 52 49 49 47 54 48 51 49 52 56 49
26 | 7 10 13 7 11 14 4 8 7 8 18 3 | 18 20 22 19 21 29 18 23 19 20 21 18
X27 | 85 11 --- --- --- >>>> 108 --- --- --- --- 0 | 6 209 --- --- --- 504 241 --- --- --- --- 209
28 | 9 7 14 7 13 18 4 11 8 8 15 3 | 22 23 26 22 21 28 21 27 21 29 23 22
29 | 11 15 14 11 14 15 5 16 8 11 35 4 | 22 24 27 29 29 24 22 26 23 27 20 23
30 | 19 15 15 7 15 25 8 13 10 11 40 4 | 70 65 67 61 55 69 56 67 57 64 61 61
31 | 8 14 17 8 15 26 6 14 10 10 13 5 | 17 18 24 15 17 32 15 23 14 22 17 15
32 | 12 10 13 7 11 18 5 15 8 10 25 4 | 20 24 29 21 20 31 21 31 20 24 34 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 11 16 7 13 18 5 14 8 10 24 |T 30 38 33 28 28 53 36 33 27 31 30 37
WRMS | 9 11 16 7 13 17 4 13 7 8 22 |NE 29 30 27 21 22 39 27 28 20 25 24 30
MEDI | 9 11 15 7 13 18 4 13 8 9 20 |MD 24 26 31 24 26 32 22 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 4.1710 GPS week: 1710 MJD: 56214.0-56220.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 |U 5 5 12 |U 6 9 22 |U 7 9 20 |
cof | cof 3036 |U 5 5 13 |U 6 9 23 |U 7 8 19 |
emr | emr 2906 | 7 6 18 |U 8 8 25 | 10 12 22 |
esa | esa 2921 | 5 5 15 |U 6 9 23 | 8 10 20 |
gfz | gfz 2919 |U 5 5 15 |U 6 8 23 |U 8 9 19 |
grg | grg 2989 |U 8 8 20 |U 8 12 29 | 10 11 26 |
igr | igr 2929 | 5 5 15 | 6 8 22 | 8 9 18 |
igs | igs 2989 | 5 6 15 | 6 8 22 | 8 10 21 |
jpl | jpl 2920 | 6 6 19 |U 7 8 24 | 10 11 22 |
mit | mit 2921 | 6 5 14 |U 6 9 24 |U 9 10 23 |
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 5.1710.0 GPS week: 1710 Day: 0 MJD: 56214.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 4 3 11 | 5 10 15 | 7 8 22 |
cof | cof 3072 | 4 4 12 | 6 9 16 | 7 8 21 |
emr | emr 2976 | 5 5 16 | 6 8 16 | 8 8 23 |
esa | esa 2976 | 4 4 13 | 5 9 17 | 7 8 21 |
gfz | gfz 2975 | 4 3 12 | 6 8 17 | 7 7 21 |
grg | grg 3070 | 7 6 19 | 7 13 24 | 11 11 27 |
igr | igr 2976 | 4 4 13 | 5 9 17 | 7 7 19 |
igs | igs 3072 | 4 4 12 | 5 9 16 | 8 9 23 |
jpl | jpl 2976 | 4 4 18 | 6 7 17 | 8 9 21 |
mit | mit 2976 | 4 4 13 | 5 9 17 | 8 8 24 |
Table 5.1710.1 GPS week: 1710 Day: 1 MJD: 56215.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 5 4 14 | 6 9 21 | 6 9 19 |
cof | cof 3070 | 6 4 14 | 6 8 21 | 5 8 18 |
emr | emr 2976 | 7 5 20 | 7 7 26 | 7 10 21 |
esa | esa 2976 | 6 4 16 | 6 9 24 | 6 10 18 |
gfz | gfz 2976 | 6 4 17 | 6 8 23 | 6 9 19 |
grg | grg 2976 | 11 10 19 | 8 12 29 | 11 11 24 |
igr | igr 2976 | 6 4 16 | 6 7 20 | 7 9 17 |
igs | igs 3072 | 6 4 14 | 6 8 23 | 6 9 18 |
jpl | jpl 2976 | 5 4 17 | 7 9 22 | 8 10 18 |
mit | mit 2976 | 6 4 16 | 6 8 27 | 7 8 21 |
Table 5.1710.2 GPS week: 1710 Day: 2 MJD: 56216.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 9 17 | 6 11 22 | 8 8 19 |
cof | cof 3072 | 7 9 17 | 5 11 21 | 8 7 18 |
emr | emr 2880 | 7 8 20 | 8 9 23 | 10 12 24 |
esa | esa 2976 | 6 8 18 | 6 9 23 | 10 9 18 |
gfz | gfz 2975 | 6 8 17 | 6 8 24 | 9 8 18 |
grg | grg 2976 | 7 8 17 | 7 14 29 | 10 7 22 |
igr | igr 2976 | 6 8 17 | 6 8 22 | 10 9 18 |
igs | igs 3035 | 7 8 17 | 6 9 21 | 9 9 19 |
jpl | jpl 2976 | 6 9 20 | 6 8 24 | 10 10 22 |
mit | mit 2976 | 6 7 17 | 7 8 24 | 9 8 18 |
Table 5.1710.3 GPS week: 1710 Day: 3 MJD: 56217.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
cof | cof 3036 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
emr | emr 2880 | 7 8 26 | 10 8 28 | 11 14 25 |
esa | esa 2880 | 5 5 20 | 7 12 25 | 8 11 24 |
gfz | gfz 2880 | 6 6 21 | 7 9 24 | 8 11 24 |
grg | grg 2975 | 6 6 22 | 8 13 25 | 8 10 28 |
igr | igr 2941 | 6 5 21 | 7 10 24 | 8 11 22 |
igs | igs 2976 | 5 5 21 | 8 10 23 | 9 13 26 |
jpl | jpl 2880 | 6 7 25 | 7 11 26 | 9 14 26 |
mit | mit 2880 | 8 6 21 | 8 10 26 | 9 12 35 |
Table 5.1710.4 GPS week: 1710 Day: 4 MJD: 56218.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 11 | 9 9 32 | 7 8 19 |
cof | cof 2976 | 5 5 11 | 9 9 31 | 6 6 17 |
emr | emr 2880 | 6 5 16 | 11 8 30 | 10 10 18 |
esa | esa 2880 | 5 7 12 | 9 9 29 | 7 7 16 |
gfz | gfz 2878 | 6 4 11 | 9 7 30 | 7 6 15 |
grg | grg 2976 | 11 9 24 | 10 11 37 | 8 6 28 |
igr | igr 2880 | 5 6 12 | 9 9 30 | 7 6 16 |
igs | igs 2880 | 6 11 18 | 8 9 29 | 7 8 15 |
jpl | jpl 2880 | 8 7 23 | 8 9 30 | 9 8 21 |
mit | mit 2880 | 6 7 13 | 8 8 31 | 8 7 19 |
Table 5.1710.5 GPS week: 1710 Day: 5 MJD: 56219.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3019 | 4 3 11 | 7 8 23 | 9 12 25 |
cof | cof 3019 | 4 4 11 | 6 7 22 | 9 13 24 |
emr | emr 2880 | 7 6 18 | 9 7 23 | 12 16 27 |
esa | esa 2880 | 5 5 13 | 6 9 23 | 10 14 23 |
gfz | gfz 2880 | 5 5 12 | 6 8 23 | 10 14 22 |
grg | grg 2976 | 6 9 16 | 7 11 29 | 12 13 34 |
igr | igr 2879 | 5 5 14 | 5 8 21 | 10 14 21 |
igs | igs 2933 | 4 5 12 | 6 8 21 | 9 13 26 |
jpl | jpl 2879 | 6 5 16 | 7 7 26 | 12 15 25 |
mit | mit 2880 | 4 5 11 | 6 8 22 | 12 13 24 |
Table 5.1710.6 GPS week: 1710 Day: 6 MJD: 56220.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3013 | 5 4 10 | 6 9 22 | 7 8 18 |
cof | cof 3013 | 4 4 10 | 5 8 25 | 7 7 17 |
emr | emr 2876 | 9 6 13 | 7 6 26 | 11 15 20 |
esa | esa 2880 | 5 5 11 | 5 8 21 | 9 11 17 |
gfz | gfz 2873 | 6 6 13 | 5 6 22 | 9 10 16 |
grg | grg 2975 | 9 7 22 | 6 10 28 | 9 14 21 |
igr | igr 2880 | 5 5 12 | 5 7 21 | 9 11 16 |
igs | igs 2960 | 5 6 11 | 5 7 22 | 8 10 18 |
jpl | jpl 2876 | 8 7 13 | 6 7 22 | 11 13 20 |
mit | mit 2880 | 6 6 10 | 5 9 23 | 11 11 19 |
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 6.1710 GPS week: 1710 MJD: 56214.500-56220.500
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 | 12 -41 -68 242 1 | -2 12
| 32 30 139 107 6 | 2
cof uuuuu | -75 -46 137 -260 -5 | 2 13
| 17 22 53 116 7 | 2
emr uuuxu | 40 -15 84 471 -11 | 21 27
| 20 23 72 76 5 | 4
esa uuuuu | -27 -39 -64 -233 -7 | 10 17
| 27 53 103 89 6 | 2
gfz uuuuu | 38 67 -36 12 0 | 4 12
| 19 33 106 57 3 | 2
grg uuuux | -7 -31 13 96 -30 | -6 31
| 32 43 67 39 51 | 9
igr xxxxx | -44 15 -25 35 1 | -2 11
| 10 11 67 64 4 | 2
irf xxxxx | 22 2 3 129 3 | 5 12
| 7 14 11 29 5 | 3
jpl uuuuu | 22 -28 -50 229 2 | 30 32
| 13 24 85 91 7 | 3
mit uuuuu | 44 3 12 204 11 | 0 13
| 12 12 87 68 10 | 5
ngs uuuuu | -27 70 -20 31 0 | 10 15
| 17 32 48 111 3 | 2
sio xxxxx | -27 1 78 -238 -4 | 21 24
| 19 20 161 109 7 | 2
Table 7.1710.0 GPS week: 1710 Day: 0 MJD: 56214.500
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 | 53 -47 -315 262 -7 | -1 11
cof uuuuu | -66 -26 58 -217 -5 | 4 11
emr uuuxu | 49 -53 226 480 -10 | 27 30
esa uuuuu | -46 -80 -86 -315 -9 | 11 17
gfz uuuuu | 77 92 -153 60 -2 | 3 11
grg uuuux | 15 -13 -95 142 28 | -21 48
igr xxxxx | -25 33 -107 145 0 | -4 12
irf xxxxx | 32 12 5 138 6 | 2 11
jpl uuuuu | 32 -16 56 344 -8 | 34 36
mit uuuuu | 40 -3 113 226 14 | -5 12
ngs uuuuu | -27 105 -45 9 4 | 8 13
sio xxxxx | -33 0 -115 -158 -13 | 23 25
Table 7.1710.1 GPS week: 1710 Day: 1 MJD: 56215.500
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 -10 -63 243 -3 | -2 11
cof uuuuu | -50 -38 126 -233 -13 | 3 11
emr uuuxu | 44 4 55 567 -17 | 25 28
esa uuuuu | -60 -53 57 -253 -2 | 9 16
gfz uuuuu | 40 90 -182 60 1 | 3 10
grg uuuux | 23 30 -45 107 21 | -14 43
igr xxxxx | -49 11 -28 -45 3 | -4 12
irf xxxxx | 26 12 0 187 10 | 2 11
jpl uuuuu | 27 -21 -127 335 -5 | 31 34
mit uuuuu | 35 -14 54 338 18 | -5 12
ngs uuuuu | 6 52 -39 -157 3 | 9 13
sio xxxxx | 2 11 -63 -102 -11 | 22 25
Table 7.1710.2 GPS week: 1710 Day: 2 MJD: 56216.500
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 -9 -8 336 -1 | -1 11
cof uuuuu | -82 -49 229 -386 -1 | 3 11
emr uuuxu | 51 10 65 535 -13 | 23 27
esa uuuuu | -49 -97 -21 -314 -3 | 11 16
gfz uuuuu | 40 73 -94 -13 2 | 4 10
grg uuuux | 3 11 34 121 -2 | -4 31
igr xxxxx | -40 22 -88 9 10 | -3 10
irf xxxxx | 21 17 10 107 0 | 4 11
jpl uuuuu | 43 7 -146 178 1 | 31 33
mit uuuuu | 41 -4 10 212 3 | -2 13
ngs uuuuu | -37 103 -23 119 1 | 10 14
sio xxxxx | -39 4 169 -167 -6 | 22 25
Table 7.1710.3 GPS week: 1710 Day: 3 MJD: 56217.500
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 | -6 -15 -114 417 -3 | -2 11
cof uuuuu | -94 -12 110 -267 -6 | 3 11
emr uuuxu | 47 -11 6 523 -14 | 22 27
esa uuuuu | -26 -86 -235 -319 -7 | 11 17
gfz uuuuu | 28 93 4 38 -5 | 5 11
grg uuuux | -3 -33 85 96 -10 | 5 15
igr xxxxx | -49 18 15 42 2 | -1 10
irf xxxxx | 28 11 12 124 9 | 5 11
jpl uuuuu | 22 -14 -34 146 4 | 29 32
mit uuuuu | 49 19 36 150 23 | -1 12
ngs uuuuu | -28 37 67 179 -4 | 12 14
sio xxxxx | -16 33 -72 -204 -4 | 22 25
Table 7.1710.4 GPS week: 1710 Day: 4 MJD: 56218.500
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 | -20 -72 -137 154 8 | -6 11
cof uuuuu | -98 -59 119 -418 5 | -1 13
emr uuuxu | -1 -39 36 439 -14 | 16 23
esa uuuuu | 20 36 -155 -158 -3 | 7 15
gfz uuuuu | 27 66 75 61 0 | 2 11
grg uuuux | -28 -89 -13 17 -77 | 2 17
igr xxxxx | -47 10 8 87 -2 | -4 11
irf xxxxx | 11 -14 15 130 -3 | 5 11
jpl uuuuu | 7 -60 67 284 3 | 25 27
mit uuuuu | 41 4 62 203 -1 | 0 12
ngs uuuuu | -37 29 -6 67 1 | 8 13
sio xxxxx | -59 -29 120 -306 0 | 17 20
Table 7.1710.5 GPS week: 1710 Day: 5 MJD: 56219.500
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 -49 67 118 5 | -2 14
cof uuuuu | -66 -63 165 -228 -15 | 3 17
emr uuuxu | 31 -17 125 388 -5 | 19 25
esa uuuuu | -16 1 -34 -165 -19 | 11 19
gfz uuuuu | 15 55 56 -48 -1 | 5 14
grg uuuux | 8 -65 43 90 -87 | -2 22
igr xxxxx | -58 7 -59 25 -2 | 0 12
irf xxxxx | 17 -2 -4 124 4 | 9 14
jpl uuuuu | 14 -51 -102 192 8 | 29 32
mit uuuuu | 33 19 -37 164 18 | 5 13
ngs uuuuu | -21 68 -88 52 3 | 12 18
sio xxxxx | -25 -16 222 -327 -3 | 21 25
Table 7.1710.6 GPS week: 1710 Day: 6 MJD: 56220.500
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 | -31 -82 93 163 7 | -3 14
cof uuuuu | -71 -75 153 -70 -1 | 1 18
emr uuuxu | 58 2 75 367 -5 | 17 25
esa uuuuu | -16 9 24 -108 -4 | 9 20
gfz uuuuu | 41 0 46 -75 4 | 5 15
grg uuuux | -69 -57 84 101 -83 | -12 39
igr xxxxx | -42 2 87 -18 -1 | 0 12
irf xxxxx | 19 -19 -18 96 -3 | 9 14
jpl uuuuu | 8 -41 -65 123 10 | 29 32
mit uuuuu | 68 2 -155 135 1 | 7 13
ngs uuuuu | -48 95 -5 -54 -4 | 12 18
sio xxxxx | -23 2 288 -405 7 | 20 24
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