[IGSREPORT-21476] Wk 1719 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Mon Jan 7 09:47:10 PST 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1719 (Dec 16, 2012 - Dec 22, 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 at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1719[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1719[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1719[0-6].cls IGS GPS clock combination summary report.
igs17197.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17197.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | KOUC WROC
0 | ESA | AREQ UNSA
0 | GFZ | BOGT POLV
0 | GRG | 26 ADIS
0 | JPL | 26
0 | MIT | 26
1 | COD | BOR1
1 | EMR | HERS MCM4 WUHN
1 | ESA | HOLM
1 | GFZ | BOGT MAS1 TLSE
1 | GRG | 26 ADIS IRKT KIT3 LHAZ LPGS NICO TLSE WROC
1 | JPL | 24 26
1 | MIT | 26 NKLG
2 | COD | KOUC
2 | ESA | GUUG
2 | GFZ | BOGT COCO GRAS HARB MATE
2 | GRG | 26 HARB KOUC TIDB USNO WIND
2 | JPL | 26
2 | MIT | 7 23 26 30 GMAS
3 | COD | 26
3 | EMR | MCM4
3 | ESA | 26 AREQ
3 | GFZ | 26 30 26 30 AREQ BOGT POLV ZAMB BOGT POLV ZAMB
3 | GRG | AREQ BAKE CEDU MCM4 TIDB TLSE
3 | JPL | 26 AREQ
3 | MIT | 5 14 22
4 | COD | HNPT YELL FLRS HNPT YELL
4 | EMR | HARB HARB
4 | GFZ | BOGT HARB MATE NTUS
4 | GRG | 26 26 KARR KIT3 LHAZ MATE NTUS RAMO
4 | JPL | 26 BOR1
4 | MIT | 5 21 26 5 21 26 NTUS
5 | GFZ | BOGT NYAL RESO WHIT WSRT YAKT
5 | GRG | 26 26 ADIS KOUC LHAZ NKLG TIDB
5 | MIT | 26 26 NTUS
6 | COD | 26 KOUC KOUC MCM4
6 | EMR | THTI WUHN
6 | ESA | 26 26
6 | GFZ | BOGT YAKT
6 | GRG | MATE MATE
6 | JPL | MCM4
6 | MIT | 1 26 1 26 JPLM
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G03 | 2012_12_20 | 2012085
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G26 | | 4 | | | | | |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.6 .3 -.5 -72 -7 9 -.02
EMR | 0 | -.1 9.3 19.6 12 12 8 .27
ESA | 0 | 1.5 5.2 13.5 68 -46 98 .04
GFZ | 0 | .1 .0 .0 -81 -18 -11 -.03
GRG | 0 | 1.9 4.8 -4.6 -10 44 -31 .14
JPL | 0 | 3.3 10.7 16.0 -17 -90 -2 -.02
MIT | 0 | 4.3 7.0 7.8 -8 8 -29 .19
NGS | 0 | 4.2 6.6 9.9 -36 -16 35 .79
SIO | 0 | 4.9 12.0 61.3 33 195 -26 .02
COD | 1 | -1.1 1.0 -1.3 -65 1 17 .02
EMR | 1 | .1 10.9 23.2 11 9 -1 .30
ESA | 1 | 5.9 4.0 11.2 67 -150 138 .20
GFZ | 1 | -.8 .0 -.5 -77 -45 -3 .14
GRG | 1 | 6.3 3.6 -5.0 -14 47 -22 .16
JPL | 1 | 4.6 7.5 16.6 91 -19 -41 .13
MIT | 1 | 8.3 7.6 7.7 -9 10 -14 .18
NGS | 1 | 1.8 8.1 7.2 -10 -4 7 .68
SIO | 1 | -.4 10.1 53.4 -1 207 -139 .30
COD | 2 | -1.1 1.2 -.8 -63 -2 5 -.07
EMR | 2 | 4.8 13.2 21.3 13 15 -11 .25
ESA | 2 | 3.8 9.5 12.0 151 -106 99 .07
GFZ | 2 | -.7 -.2 -.5 -89 -48 -15 .09
GRG | 2 | 1.4 1.6 -4.1 -4 22 -34 .19
JPL | 2 | 1.3 14.4 14.1 -84 49 -25 -.20
MIT | 2 | 5.2 8.9 10.7 4 -2 -38 .31
NGS | 2 | 3.8 10.4 5.4 9 -17 28 .56
SIO | 2 | 1.2 12.3 45.3 64 138 -42 .15
COD | 3 | -1.5 -.2 -1.2 -80 0 14 .04
EMR | 3 | 8.0 8.8 19.2 15 16 -13 .36
ESA | 3 | 3.6 7.7 14.2 129 -93 68 .11
GFZ | 3 | .3 .0 -.8 -88 -46 -15 .15
GRG | 3 | 3.2 2.1 -1.5 -8 38 3 .31
JPL | 3 | 6.8 7.0 25.9 -91 -30 -3 -.07
MIT | 3 | 4.8 6.2 9.5 -4 4 -24 .30
NGS | 3 | 8.9 9.5 7.3 8 -34 62 .50
SIO | 3 | 3.8 10.9 25.7 100 16 6 .24
COD | 4 | -1.0 -.1 -.3 -57 -13 3 .03
EMR | 4 | 5.1 7.1 20.6 9 -1 -3 .40
ESA | 4 | 6.3 7.8 10.4 133 -157 74 .19
GFZ | 4 | .0 .0 -1.1 -75 -45 -26 .06
GRG | 4 | 9.5 6.8 -4.0 -32 24 -22 .26
JPL | 4 | 5.8 8.3 24.3 -62 27 -34 .31
MIT | 4 | 2.3 6.0 10.7 4 9 -30 .19
NGS | 4 | -2.7 6.4 11.9 -36 20 -27 .65
SIO | 4 | .7 6.1 11.2 82 5 85 .22
COD | 5 | -1.0 .3 -.9 -61 -14 -7 .20
EMR | 5 | 1.0 10.7 13.8 8 9 0 .43
ESA | 5 | 1.0 4.5 9.3 88 -92 109 .32
GFZ | 5 | -.1 -.5 -1.8 -68 -51 -33 .27
GRG | 5 | 4.8 -2.1 -3.4 -10 33 -35 .22
JPL | 5 | 4.7 .5 14.4 -67 -7 -27 .22
MIT | 5 | 5.6 6.7 8.1 4 11 -34 .39
NGS | 5 | 1.8 11.8 -2.1 90 -21 30 .65
SIO | 5 | 2.9 9.6 14.8 140 -28 28 .27
COD | 6 | -1.3 -.6 -1.7 -68 4 -15 .04
EMR | 6 | 2.5 13.7 7.2 2 2 0 .25
ESA | 6 | 2.0 7.7 1.3 123 -151 63 .15
GFZ | 6 | -.7 -.1 -1.3 -68 -45 -38 .11
GRG | 6 | 2.6 -.4 -13.7 -24 35 -14 .30
JPL | 6 | 1.3 -.3 10.3 -40 -9 -24 .15
MIT | 6 | 4.2 7.4 3.2 -2 7 -34 .42
NGS | 6 | 10.0 3.6 1.3 22 -69 99 .51
SIO | 6 | .3 9.0 1.9 149 -24 -35 .24
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1719.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1719.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 2.1719.[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 3.1719.[0-6]). The first type of satellite RMS is
based on orbit combination and the second RMS type is a result of the 7-day
arc evaluation of each centre ephemerides. The fourth part, Table 4, is a
weekly summary of the daily precise navigation summaries for centres
providing both orbit and clock solutions. It contains weekly station RMS
w.r.t. the initial coordinates for the Latitude, Longitude and Height
components for up to three IGS stations (Table 4.1307). The fifth part,
Table 5, is similar to Table 4 and contains daily precise navigation
statistics (Tables 5.1719.0-6). The sixth part, Table 6, is a weekly
summary of daily ERP combination statistics. The seventh part, Table 7,
contains the daily ERP statistics. But this is not the IGS official ERP
combination products (which come from the accompanying SINEX combination)
but provided to check combination consistency, etc.
In Tables 1-3, the most important statistic which is meaningful for intra
centre/satellite analysis is labeled WRMS. It is a weighted RMS where
normalized weights are based on accuracy codes given in the SP3 files, and
should not be affected by downweighted/problem satellites when acknowledged
by individual centres in their SP3 file.
Table 1: Week 1719 summary. (Dec 16, 2012 - Dec 22, 2012)
Table 1.1719.a GPS week: 1719 MJD: 56277.000-56283.000
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 264| 1 0 1 -9 20 18 -.41 13 12 | -942 -60 21 84
| 0 0 1 29 22 9 .06 | 671 995
emr 79| 2 0 10 -28 20 -4 .23 15 15 | 2485 -348 12 92
| 1 1 1 20 18 14 .01 | 1115 562
esa 173| 1 1 0 97 -33 -2 .04 6 6 | -430 292 11 94
| 0 0 0 25 43 9 .02 | 762 1123
gfz 191| -2 0 -3 -103 -52 1 -.42 11 10 | 80 119 19 118
| 0 1 1 58 55 7 .04 | 403 656
grg 137| 0 0 -8 -9 34 -9 .60 17 15 | -44 46 16 130
| 0 0 3 17 19 12 .06 | 377 426
igr n/a| 0 0 -1 -10 57 -23 -.16 4 4 | 8136 -198 16 83
| 0 0 0 31 11 16 .03 | 745 683
jpl 80| 0 -2 2 2 24 0 .34 13 13 | 147308 -411 16 111
| 0 1 1 30 35 16 .03 | 247452 700
mit 239| 0 0 -2 -13 -1 17 -.19 6 6 | -262 254 22 187
| 0 0 0 28 41 23 .05 | 219 435
ngs 234| 0 0 1 -49 64 -26 .33 13 9 | -143735 312606 1817 3508
| 0 0 2 17 33 38 .03 | 377577 827075
sio 285| 0 1 4 56 97 -22 -.48 20 18 | --- --- --- ---
| 0 1 1 61 113 60 .04 | --- ---
Table 1.1719.b GPS week : 1719 MJD: 56277.000-56283.000
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 | 5 4 5 5 4 4 5 |
3 | 4 4 5 4 0 3 4 |
4 | 3 4 4 3 3 3 3 |
5 | 4 4 4 4 4 4 4 |
6 | 4 4 4 4 4 4 4 |
7 | 4 5 4 5 4 4 4 |
8 | 4 4 3 3 3 4 3 |
9 | 4 4 4 3 4 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 3 4 4 4 4 |
12 | 5 5 5 5 6 5 5 |
13 | 3 4 3 4 3 4 3 |
14 | 4 4 3 3 4 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 5 5 4 5 5 4 5 |
17 | 4 4 5 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 5 5 5 4 5 4 5 |
20 | 4 4 3 4 4 3 4 |
21 | 3 4 4 3 3 3 3 |
22 | 4 4 3 3 4 3 3 |
23 | 5 5 3 4 4 3 3 |
24 | 5 5 4 4 4 4 4 |
25 | 4 5 4 4 4 4 4 |
26 | 9 8 6 7 7 10 10 |
27 | 0 0 0 0 0 0 0 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 4 4 5 4 4 |
30 | 4 7 5 4 4 4 4 |
31 | 5 5 4 4 4 4 4 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1719.0 GPS week: 1719 Day: 0 MJD: 56277.000
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| 2 -2 1 -31 31 14 -.50 13 13 | -1807 1120 22 92
emr 80| 0 1 12 -59 32 2 .23 14 14 | 3326 -236 13 106
esa 173| 1 2 0 58 27 0 .03 7 6 | -667 -537 14 84
gfz 188| -2 0 -4 -68 -133 -4 -.46 12 12 | -673 1286 20 119
grg 136| 0 0 -13 -40 17 -9 .56 17 16 | -646 651 17 147
igr n/a| 0 0 -2 -13 58 -39 -.18 5 5 | 7767 454 17 79
jpl 80| -2 -3 2 -3 85 -6 .32 13 12 | 509588 233 16 117
mit 239| 0 0 -2 39 -77 33 -.21 7 7 | -284 -232 21 175
ngs 247| 0 0 5 -37 62 -53 .37 13 8 | -1709 914 1586 3419
sio 285| 0 1 3 33 192 -25 -.50 20 18 | --- --- --- ---
Table 2.1719.1 GPS week: 1719 Day: 1 MJD: 56278.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 265| 1 0 1 27 -19 11 -.43 11 11 | -1527 1013 20 76
emr 80| 0 0 11 2 -7 5 .22 15 15 | 3048 332 15 89
esa 173| 1 1 0 118 -52 12 .03 8 7 | -611 -400 13 93
gfz 193| -3 1 -5 -184 -14 0 -.44 12 12 | 585 -266 23 128
grg 138| -1 -1 -10 -21 65 -19 .56 16 15 | -104 154 18 118
igr n/a| 0 -1 -2 44 45 -41 -.18 4 4 | 8500 554 18 94
jpl 80| 0 -1 4 50 -27 -15 .37 12 12 | 3029 188 18 122
mit 238| 0 0 -4 -52 46 58 -.26 8 8 | -506 1031 23 148
ngs 243| 0 0 2 -36 54 -84 .32 12 9 | -1089 -99 1499 4147
sio 293| 1 0 4 -57 273 -131 -.50 22 20 | --- --- --- ---
Table 2.1719.2 GPS week: 1719 Day: 2 MJD: 56279.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 265| 1 0 3 -24 18 12 -.38 12 12 | -91 -1512 21 72
emr 80| 2 1 12 -40 13 -33 .22 15 15 | 3837 -507 13 81
esa 173| 1 1 0 93 -35 -11 .05 6 5 | -1704 1978 13 100
gfz 194| -2 1 -3 -58 -46 -4 -.43 10 11 | 18 406 20 117
grg 140| 0 0 -11 -13 26 -22 .70 17 16 | 449 -274 14 117
igr n/a| 0 0 -1 -31 53 -43 -.12 4 4 | 9333 -275 15 74
jpl 80| 0 -3 4 -50 23 9 .34 14 13 | 3523 -632 16 97
mit 239| 0 -1 -1 4 -4 19 -.14 6 6 | -324 435 23 202
ngs 231| 0 -1 1 -83 105 28 .36 12 10 | -999999 2188236 1951 3450
sio 289| 0 0 3 58 171 -48 -.41 21 13 | --- --- --- ---
Table 2.1719.3 GPS week: 1719 Day: 3 MJD: 56280.000
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 269| 1 -1 1 -36 11 22 -.42 11 11 | -191 -737 21 85
emr 80| 3 0 10 -36 46 2 .24 15 15 | 3164 -1464 11 104
esa 173| 1 2 0 119 5 -16 -.00 6 6 | 27 -83 9 97
gfz 190| -2 0 -4 -62 -88 0 -.45 10 10 | 237 -610 19 120
grg 140| 0 0 -7 -2 19 -5 .67 14 14 | 308 -526 14 130
igr n/a| 0 0 -1 -24 65 -8 -.11 4 4 | 8805 -1426 17 90
jpl 80| -1 -3 1 -6 48 -4 .28 14 13 | 509493 -1831 15 121
mit 240| 0 0 -1 -24 -5 11 -.11 6 6 | 124 -140 23 221
ngs 223| 0 -1 2 -53 12 0 .34 11 9 | -389 -499 1847 3065
sio 280| -1 2 4 45 32 0 -.43 19 18 | --- --- --- ---
Table 2.1719.4 GPS week: 1719 Day: 4 MJD: 56281.000
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 268| 1 0 4 -37 35 37 -.44 14 14 | -697 -802 23 93
emr 80| 4 -1 12 -32 25 4 .23 15 15 | 1711 -92 11 87
esa 173| 1 1 0 84 -65 0 .04 6 6 | -229 1485 12 100
gfz 192| -3 0 -5 -46 -53 18 -.40 10 9 | -106 438 18 107
grg 137| 0 1 -4 1 27 -13 .56 17 16 | -377 516 23 136
igr n/a| 0 0 -1 -48 60 -7 -.17 4 4 | 7653 195 16 74
jpl 80| 0 -4 0 11 2 27 .33 14 13 | 1700 -87 17 100
mit 240| 0 0 -2 -15 21 -13 -.17 6 6 | -459 442 21 182
ngs 246| -1 0 1 -58 104 -42 .31 11 9 | -940 -443 1954 3495
sio 286| 0 1 2 68 27 57 -.52 19 19 | --- --- --- ---
Table 2.1719.5 GPS week: 1719 Day: 5 MJD: 56282.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 264| 0 -1 0 26 50 18 -.35 13 12 | -1449 465 23 85
emr 80| 1 0 8 -12 30 2 .23 14 14 | 1065 -60 13 88
esa 173| 1 1 0 81 -15 -1 .07 6 5 | 790 -1070 10 95
gfz 189| -2 -1 -1 -125 -71 0 -.40 10 9 | 116 57 19 123
grg 137| -1 1 -5 10 27 -10 .54 18 16 | 20 3 17 147
igr n/a| 0 0 -1 -15 75 -15 -.19 4 4 | 7509 -343 16 86
jpl 80| -1 0 2 18 24 9 .37 14 13 | 2027 -355 17 109
mit 239| 0 0 -1 -18 -26 -3 -.19 6 6 | -77 -16 22 191
ngs 230| 0 0 -3 -31 72 -2 .30 14 8 | -1252 247 1834 3636
sio 284| 0 3 7 122 -31 22 -.52 20 20 | --- --- --- ---
Table 2.1719.6 GPS week: 1719 Day: 6 MJD: 56283.000
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 0 6 13 14 -.35 12 11 | -836 33 20 91
emr 79| 1 -1 7 -19 2 -16 .22 15 14 | 1245 -411 12 93
esa 173| 1 1 0 129 -98 -1 .06 6 6 | -620 676 11 89
gfz 192| -3 -1 -2 -176 40 0 -.36 11 9 | 383 -478 20 118
grg 137| 0 0 -8 0 60 16 .59 17 15 | 37 -200 15 121
igr n/a| 0 0 -1 18 42 -9 -.19 4 4 | 7390 -546 17 84
jpl 80| 0 -1 4 0 15 -16 .37 14 13 | 1797 -398 15 115
mit 240| 0 0 -2 -27 35 15 -.22 6 5 | -313 260 24 196
ngs 224| 0 0 2 -45 42 -31 .30 15 9 | -768 -112 2054 3346
sio 283| 0 3 5 126 18 -35 -.50 22 19 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1719.0 GPS week: 1719 Day: 0 MJD: 56277.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 11 6 14 9 6 18 6 8 32 4 | 77 72 77 75 84 78 77 79 73 73 76
2 | 14 11 5 20 18 5 13 6 11 32 4 | 28 33 36 44 42 36 36 35 34 30 35
3 | 11 11 5 11 13 4 9 6 11 14 3 | 41 38 37 28 45 38 41 32 41 34 39
4 | 9 8 5 10 14 4 10 6 9 29 3 | 32 33 36 37 45 35 35 35 33 32 35
5 | 15 15 7 10 17 5 13 7 10 20 4 | 27 38 26 23 39 25 38 23 34 29 27
6 | 13 12 5 13 12 5 9 7 12 15 3 | 24 29 25 22 29 24 29 21 28 21 23
7 | 11 13 6 11 18 4 13 9 12 13 4 | 24 31 28 27 41 25 28 25 31 24 26
8 | 11 12 5 8 13 4 9 6 13 25 3 | 40 43 39 45 44 39 42 43 42 50 41
9 | 16 11 5 10 16 5 12 8 9 16 4 | 20 30 23 24 27 22 31 22 27 24 23
10 | 6 10 4 10 15 5 10 7 8 31 3 | 21 29 27 25 33 26 29 23 30 38 25
11 | 9 16 5 13 13 6 12 7 11 17 4 | 46 47 50 50 61 50 50 51 46 47 48
12E | 19 20 7 11 15 6 22 11 11 12 5 | 63 58 56 54 58 59 59 57 58 59 56
13E | 7 12 4 11 14 4 9 8 8 18 3 | 43 52 46 46 55 46 47 42 50 46 45
14E | 9 10 5 11 21 4 12 7 8 13 3 | 23 26 26 21 28 23 26 20 24 21 22
15E | 11 13 5 9 19 3 13 6 11 12 3 | 64 75 71 71 76 71 75 69 76 71 71
16E | 14 20 7 14 21 4 14 10 10 16 4 | 22 25 23 17 32 20 24 16 26 20 18
17 | 16 10 7 11 17 4 12 5 12 16 4 | 26 30 25 22 42 25 29 23 32 19 25
18 | 15 14 6 12 15 3 12 6 8 22 3 | 41 47 39 28 38 35 42 33 40 42 36
19 | 13 22 7 8 17 5 15 8 12 14 4 | 20 30 24 19 31 20 27 19 24 19 20
20 | 8 15 8 13 12 4 15 8 9 16 4 | 28 39 28 26 32 27 37 26 33 30 27
21 | 10 10 7 9 12 3 8 6 13 38 3 | 29 33 36 34 39 35 34 30 37 47 33
22 | 11 12 6 10 14 4 10 6 8 19 3 | 28 44 36 25 42 32 40 29 40 33 33
23E | 6 15 6 13 26 5 18 9 6 13 4 | 28 33 31 29 33 28 30 27 31 26 28
24 | 20 23 5 11 20 6 13 8 10 24 5 | 34 30 29 28 32 28 34 27 27 25 26
25 | 11 18 5 9 20 5 14 7 6 15 4 | 36 36 36 38 41 34 40 35 35 33 35
26E | 27 22 17 14 19 8 17 10 46 11 8 | 90 92 92 94 91 86 87 91 84 87 89
X27E | 8 --- --- --- --- 47 --- --- --- --- 0 | 59 --- --- --- --- 43 --- --- --- --- 60
28E | 10 13 7 12 20 5 13 5 10 12 4 | 22 27 22 24 36 21 26 22 29 24 22
29 | 17 17 8 13 16 5 14 5 13 18 4 | 19 25 22 21 31 20 23 18 27 24 19
30 | 16 12 7 9 11 4 11 6 13 14 4 | 24 32 24 25 27 24 26 23 28 24 24
31 | 16 14 5 14 22 3 13 8 9 20 4 | 29 35 27 30 42 27 32 27 32 24 28
32 | 11 7 5 9 12 4 7 5 4 16 2 | 22 24 19 13 21 18 23 18 21 20 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 14 7 12 17 5 13 7 13 20 |T 35 39 36 34 42 35 38 33 37 35 35
WRMS | 13 14 6 12 16 5 12 7 8 18 |NE 31 36 32 30 39 31 35 30 34 32 31
MEDI | 11 13 6 11 16 4 13 7 10 16 |MD 28 33 29 28 39 28 34 27 33 30 28
Table 3.1719.1 GPS week: 1719 Day: 1 MJD: 56278.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 7 14 10 5 18 5 10 33 4 | 54 47 53 50 54 53 52 53 47 42 50
2 | 10 10 8 16 16 3 12 7 11 29 4 | 22 23 27 28 27 23 26 25 25 24 24
3 | 9 13 8 13 12 4 10 7 8 22 3 | 43 48 39 39 52 42 48 41 42 36 44
4 | 8 7 5 9 16 4 9 7 13 27 3 | 28 27 29 27 37 29 31 30 28 27 29
5 | 10 13 10 9 17 4 12 5 12 21 4 | 21 30 24 17 33 19 30 20 29 20 23
6 | 10 14 7 15 9 3 8 8 7 19 3 | 22 28 19 27 23 19 25 22 22 12 21
7 | 12 14 9 15 20 3 12 10 10 14 4 | 29 30 28 27 37 24 29 27 28 23 26
8 | 11 12 5 10 13 5 9 6 10 27 3 | 33 34 33 30 31 31 33 33 32 34 31
9 | 12 12 5 11 16 4 10 8 8 20 3 | 25 26 21 17 23 20 27 23 25 21 22
10 | 9 8 6 8 11 4 7 7 11 29 3 | 23 22 20 14 23 18 23 17 21 28 19
11 | 6 15 6 12 10 4 11 5 9 19 3 | 36 38 36 35 42 36 36 36 33 29 35
12 | 12 19 7 11 18 4 20 9 14 15 5 | 70 71 70 69 71 70 74 71 72 70 70
13E | 10 12 6 14 15 4 9 10 10 15 4 | 45 48 48 38 53 47 49 45 44 45 45
14E | 7 11 8 11 14 3 8 9 11 16 3 | 19 23 20 19 24 17 19 15 22 19 17
15E | 8 13 7 10 23 3 13 8 10 12 4 | 73 74 72 71 71 73 71 71 73 74 72
16E | 10 18 7 16 16 5 15 9 10 30 4 | 19 27 21 29 30 18 26 21 25 21 21
17 | 15 12 8 10 17 4 9 6 14 19 4 | 32 28 23 16 36 23 28 22 29 17 24
18 | 15 15 7 13 12 3 13 8 9 23 4 | 28 32 20 20 27 21 31 22 26 23 24
19 | 11 25 11 13 15 5 15 10 9 21 5 | 23 32 23 23 29 19 26 22 24 18 20
20 | 12 14 6 13 14 3 12 9 13 15 4 | 28 32 25 27 27 25 29 23 24 20 24
21 | 7 12 8 11 11 4 9 9 15 42 4 | 24 23 19 27 20 21 21 22 23 37 20
22 | 8 13 6 12 9 3 11 6 8 23 3 | 24 32 19 18 32 20 32 20 25 18 23
23E | 7 13 6 13 25 5 12 10 11 14 4 | 24 33 28 25 29 26 28 24 31 21 25
24 | 12 20 7 10 22 6 12 9 9 17 4 | 31 29 26 25 31 24 34 26 28 22 26
25 | 10 20 7 10 20 4 14 6 8 14 4 | 25 29 25 27 34 24 31 24 26 23 24
26E | 26 26 15 16 19 7 18 11 36 14 8 | 52 45 46 49 42 46 46 45 55 42 45
X27 | 7 --- --- --- --- 73 --- --- --- --- 0 | 47 --- --- --- --- 52 --- --- --- --- 45
28E | 10 11 7 14 17 5 10 8 10 17 4 | 37 38 37 36 42 34 38 34 39 35 36
29 | 11 16 10 15 13 5 13 7 10 19 4 | 21 24 16 21 22 15 21 19 18 22 17
X30 | 19 23 --- 14 13 5 --- 9 13 --- 6 | 24 26 --- 21 25 19 --- 20 23 --- 20
31 | 10 14 9 12 19 4 14 10 13 20 4 | 27 35 25 26 41 24 31 27 33 19 27
32 | 8 7 5 9 14 2 6 7 9 13 3 | 21 22 20 19 24 20 20 18 20 13 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 8 12 16 4 12 8 12 22 |T 32 34 30 29 35 29 33 29 32 28 30
WRMS | 11 15 7 12 15 4 12 8 9 20 |NE 28 30 25 25 31 24 30 25 27 24 25
MEDI | 10 13 7 12 15 4 12 8 10 19 |MD 27 30 25 27 31 24 30 24 28 23 24
Table 3.1719.2 GPS week: 1719 Day: 2 MJD: 56279.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 14 12 6 10 10 4 21 4 11 13 4 | 53 54 57 61 64 56 62 58 53 54 56
2 | 17 11 5 24 16 4 14 5 13 29 4 | 26 29 32 38 31 30 29 30 36 28 30
3 | 9 17 8 12 39 6 13 7 13 49 5 | 88 72 68 64 73 89 72 62 63 61 90
4 | 12 7 7 12 13 3 9 5 16 26 3 | 26 29 33 33 36 30 31 29 32 28 30
5 | 12 18 6 11 13 4 15 5 14 21 4 | 30 36 25 24 36 26 35 26 29 31 26
6 | 9 12 6 11 14 4 12 6 10 13 3 | 21 28 24 27 29 25 30 24 25 21 23
7 | 11 13 5 7 17 3 14 5 9 14 3 | 26 31 25 23 36 25 27 26 29 25 25
8 | 13 11 4 6 13 4 9 6 8 24 3 | 37 39 35 32 36 35 35 35 33 40 34
9 | 14 9 5 10 14 3 9 4 14 15 3 | 27 32 29 29 30 29 30 28 35 34 28
10 | 9 10 5 10 11 3 9 5 11 29 3 | 21 27 23 23 26 24 26 24 25 35 23
11 | 6 16 6 7 12 3 13 4 10 13 3 | 34 40 39 42 49 39 42 39 38 37 38
12 | 9 20 5 8 21 5 26 7 13 12 4 | 33 39 34 30 40 31 38 29 31 31 30
13E | 9 10 3 5 16 3 13 6 10 20 3 | 32 38 32 32 42 33 35 31 32 37 32
14E | 7 12 5 8 16 4 11 6 8 13 3 | 22 28 27 22 33 26 24 24 28 29 24
15E | 12 14 5 6 21 4 14 7 17 14 4 | 64 68 65 66 66 64 66 62 66 66 65
16 | 10 19 6 15 19 5 16 6 9 17 4 | 25 28 25 25 30 23 25 20 27 19 22
17 | 14 13 8 13 20 3 14 8 13 15 4 | 25 28 26 23 37 24 26 23 30 19 24
18 | 14 17 6 9 14 3 14 6 8 20 3 | 34 36 30 26 30 29 35 29 35 36 29
19 | 13 22 8 8 18 5 19 8 12 16 4 | 24 32 26 24 32 23 28 23 30 21 22
20 | 9 14 6 9 11 3 12 5 10 15 3 | 29 32 25 26 26 24 32 27 27 27 25
21 | 14 11 7 9 11 4 11 7 13 40 3 | 25 31 31 28 34 31 32 31 30 45 29
22 | 7 14 5 7 13 4 11 5 11 20 3 | 24 35 29 22 35 27 34 25 36 32 27
23E | 7 15 4 8 17 3 12 7 7 13 3 | 26 32 28 26 33 28 27 29 32 25 27
24 | 12 21 4 10 18 4 11 6 13 17 4 | 28 31 30 28 33 28 31 29 32 32 28
25 | 8 17 4 7 16 4 17 4 10 11 3 | 29 37 35 33 36 35 37 34 37 30 33
26E | 29 27 7 10 22 6 17 8 22 15 6 | 73 62 66 65 57 66 65 66 69 65 64
X27 | 6 --- --- --- --- 28 --- --- --- --- 0 | 34 --- --- --- --- 27 --- --- --- --- 35
28 | 11 11 5 10 14 5 16 7 9 11 3 | 40 46 43 40 48 38 42 38 45 42 41
29 | 17 18 5 8 15 4 17 5 13 23 4 | 25 29 26 23 29 23 22 22 26 32 22
X30 | 10 17 6 12 14 4 --- 6 19 --- 4 | 23 32 27 24 27 23 --- 21 29 --- 23
31 | 13 13 5 9 18 4 13 7 17 16 4 | 27 31 27 29 41 26 28 25 30 25 26
32 | 7 8 4 7 14 3 7 5 8 13 2 | 20 24 20 17 21 20 20 20 24 21 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 6 10 17 4 14 6 12 21 |T 32 36 33 32 37 33 35 31 35 34 32
WRMS | 12 15 5 11 16 4 13 6 10 13 |NE 30 34 31 30 35 31 33 30 33 32 30
MEDI | 11 14 5 9 15 4 13 6 11 15 |MD 27 32 29 28 35 28 31 29 32 31 28
Table 3.1719.3 GPS week: 1719 Day: 3 MJD: 56280.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 14 7 14 10 6 22 6 8 13 4 | 65 60 62 68 66 63 62 64 57 59 62
2 | 11 12 6 25 17 3 12 4 8 29 4 | 25 27 31 42 34 32 28 31 35 28 31
3 | 9 16 7 10 18 10 11 12 10 31 4 | 80 56 57 56 57 81 55 50 55 50 78
4 | 9 8 5 9 15 4 8 5 10 25 3 | 30 33 33 38 40 33 34 33 33 29 33
5 | 7 16 6 7 13 4 14 4 10 19 3 | 19 29 19 16 33 17 26 18 24 25 20
6 | 11 14 6 10 11 4 10 7 8 12 3 | 18 23 21 21 22 19 23 17 24 18 18
7 | 16 14 8 12 18 3 16 7 10 14 4 | 22 23 21 21 32 17 19 20 24 18 18
8 | 11 11 4 6 16 3 8 5 9 24 3 | 20 23 17 20 24 17 20 21 22 27 19
9 | 9 12 5 7 11 4 9 6 7 20 2 | 19 27 20 21 23 19 22 21 21 24 20
10 | 9 9 3 9 14 2 9 4 16 28 3 | 15 21 17 22 27 18 21 20 23 31 18
11 | 7 16 7 9 13 3 13 6 12 13 3 | 39 42 41 44 48 41 42 41 35 38 40
12 | 14 23 6 9 16 4 27 7 12 12 5 | 17 29 16 17 29 16 31 18 19 20 16
13E | 9 11 6 8 12 3 12 6 12 23 3 | 20 28 22 18 29 20 27 23 27 29 21
14E | 7 12 5 7 10 4 12 6 10 12 3 | 15 19 16 16 24 17 20 15 21 20 15
15E | 14 14 5 6 13 3 14 7 12 15 3 | 48 52 51 55 54 52 50 53 50 52 51
16 | 9 21 6 14 21 5 19 7 10 16 4 | 19 26 19 19 26 17 22 18 20 21 16
17 | 10 14 5 6 18 3 12 6 13 13 3 | 16 22 16 16 34 15 19 15 26 15 16
18 | 13 15 8 9 12 5 15 7 9 19 3 | 28 33 26 20 27 22 30 24 28 29 24
19 | 12 17 6 8 14 3 14 5 13 16 4 | 22 27 21 21 28 20 21 19 21 16 18
20 | 12 15 5 9 11 3 14 6 10 14 3 | 22 29 17 20 21 17 28 16 19 19 17
21 | 8 13 8 8 10 3 10 5 8 37 3 | 20 25 27 27 29 24 26 22 25 40 23
22 | 8 12 5 7 8 5 13 5 12 20 3 | 17 32 21 16 30 19 28 20 27 24 21
23E | 7 15 6 7 13 3 12 6 11 14 3 | 26 33 30 28 30 26 28 27 26 25 27
24 | 10 19 4 8 14 4 11 6 9 11 3 | 20 23 20 21 27 20 25 22 22 21 19
25 | 10 20 4 8 13 4 13 6 10 12 3 | 27 27 25 23 30 24 31 26 28 24 24
26E | 24 27 8 10 18 6 16 10 30 14 6 | 55 50 49 49 35 47 45 50 51 49 47
X27 | 7 --- --- --- --- 71 --- --- --- --- 0 | 48 --- --- --- --- 40 --- --- --- --- 49
28 | 8 12 6 10 17 3 17 6 8 12 3 | 18 26 18 21 32 19 22 22 26 20 20
29 | 16 18 7 8 13 3 15 4 10 22 4 | 17 22 16 15 23 12 14 13 17 25 12
30 | 12 16 6 7 16 3 12 5 12 14 3 | 20 30 21 19 23 20 26 18 24 23 20
31 | 9 13 4 9 18 4 12 5 7 14 3 | 18 26 23 22 37 21 21 21 27 20 21
32 | 10 8 7 7 12 3 8 4 9 12 3 | 16 21 16 14 16 14 17 15 17 14 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 15 6 10 14 4 14 6 11 19 |T 26 30 26 26 31 26 28 25 28 27 26
WRMS | 11 15 6 10 14 4 13 6 9 18 |NE 25 29 25 26 31 25 27 24 27 26 25
MEDI | 10 14 6 8 13 3 12 6 10 14 |MD 20 27 21 21 29 20 26 21 25 24 20
Table 3.1719.4 GPS week: 1719 Day: 4 MJD: 56281.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 11 6 10 11 6 19 7 7 26 3 | 50 53 57 60 57 56 57 56 51 57 55
2 | 15 12 6 21 14 4 12 4 10 26 4 | 22 25 28 37 29 27 29 27 29 26 27
X3 | 8 --- --- --- --- 27 --- --- --- --- 0 | 32 --- --- --- --- 40 --- --- --- --- 31
4 | 11 7 7 10 15 3 10 5 11 22 3 | 26 28 29 32 34 28 33 29 29 27 29
5 | 17 18 8 8 13 4 17 5 11 20 4 | 19 28 17 14 30 14 29 14 23 20 18
6 | 11 17 6 12 16 4 11 5 9 12 3 | 21 28 24 30 26 24 28 24 28 23 24
7 | 13 12 7 12 24 5 15 6 13 13 4 | 22 21 17 18 33 14 22 18 20 17 17
8 | 12 10 5 9 16 6 8 4 9 25 3 | 20 20 14 17 21 14 21 17 16 24 16
9 | 14 11 7 7 15 5 10 8 8 16 3 | 14 25 20 18 27 18 22 18 22 17 18
10 | 14 8 7 7 14 4 10 5 8 27 3 | 16 20 20 22 23 17 24 18 19 30 18
11 | 8 17 4 10 15 5 11 5 8 17 3 | 31 37 36 42 41 34 39 34 31 34 34
12 | 13 23 7 10 22 5 28 8 13 13 5 | 25 33 23 23 35 22 36 22 27 23 23
13E | 9 10 5 10 16 4 12 5 10 16 3 | 21 27 21 22 25 20 28 20 26 18 21
14E | 9 13 6 7 16 5 11 7 10 14 3 | 18 21 20 17 25 18 21 22 27 26 19
15E | 12 13 6 5 13 3 17 7 11 17 3 | 28 30 30 30 36 31 32 30 36 34 30
16 | 11 19 6 16 21 4 15 6 10 15 4 | 20 27 20 23 26 17 24 16 23 22 17
17 | 20 11 6 8 18 3 12 5 8 13 3 | 20 23 17 13 31 14 23 15 24 15 17
18 | 14 15 6 11 13 4 13 6 7 19 3 | 28 32 24 18 26 19 27 18 26 23 21
19 | 13 20 5 15 20 4 14 7 10 15 4 | 23 26 16 22 23 15 21 13 19 16 14
20 | 9 16 6 12 14 4 13 6 9 20 3 | 20 29 17 22 20 17 27 17 20 19 18
21 | 17 11 5 6 12 4 8 5 6 36 3 | 21 21 25 28 29 25 26 24 26 37 24
22 | 10 15 5 13 10 4 10 5 13 23 3 | 17 32 22 14 28 16 27 16 26 22 19
23E | 9 15 5 10 14 4 12 6 14 17 3 | 28 32 32 29 37 29 32 29 37 27 30
24 | 16 19 7 6 19 4 17 6 9 16 4 | 21 22 18 21 30 17 26 19 22 17 18
25 | 12 17 6 6 19 4 14 6 8 11 3 | 27 27 25 25 32 24 33 23 29 22 25
26E | 33 25 9 10 22 7 18 7 30 11 7 | 83 74 78 77 73 77 77 81 74 80 76
X27 | 8 --- --- --- --- 114 --- --- --- --- 0 | 103 --- --- --- --- 29 --- --- --- --- 105
28 | 10 12 6 12 25 5 16 8 11 13 4 | 23 27 20 23 38 24 29 22 23 24 22
29 | 28 18 4 6 10 4 14 6 13 21 4 | 29 24 16 15 20 15 18 14 18 24 15
30 | 12 14 7 8 13 4 12 5 12 12 3 | 15 25 21 17 22 20 23 18 22 17 17
31 | 12 17 5 9 26 3 13 6 8 15 4 | 21 25 22 22 41 21 23 21 28 17 20
32 | 7 9 4 9 14 3 8 6 8 15 2 | 12 18 12 17 18 10 20 11 14 14 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 15 6 10 17 4 14 6 11 19 |T 27 28 24 25 31 23 29 23 27 25 26
WRMS | 14 15 6 9 16 4 13 6 9 19 |NE 22 26 22 23 29 21 27 21 24 23 22
MEDI | 12 14 6 10 15 4 12 6 10 16 |MD 21 27 21 22 29 20 27 19 26 23 20
Table 3.1719.5 GPS week: 1719 Day: 5 MJD: 56282.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 13 7 10 13 3 20 6 12 37 4 | 46 48 47 47 49 46 53 47 44 45 46
2 | 9 12 5 24 14 2 12 4 9 27 4 | 23 24 25 38 23 24 24 25 27 22 25
3 | 9 11 5 9 14 2 12 5 6 13 3 | 14 10 8 14 9 14 11 9 10 11 12
4 | 10 8 4 7 13 4 7 4 9 22 2 | 26 25 25 25 28 23 27 24 30 20 25
5 | 9 14 7 9 15 3 14 5 12 21 3 | 18 28 20 16 33 15 28 19 23 23 20
6 | 9 14 5 11 13 4 12 6 11 17 3 | 34 32 31 26 30 30 38 30 29 30 30
7 | 14 11 6 9 25 4 16 6 10 16 4 | 22 19 15 15 33 14 23 16 21 18 16
8 | 18 11 6 7 17 5 11 5 7 26 3 | 21 18 14 14 20 13 20 16 17 23 14
9 | 11 10 5 9 13 4 10 5 7 16 3 | 16 21 18 17 24 17 21 18 21 15 17
10 | 9 8 4 7 12 3 8 4 9 29 2 | 20 18 16 15 20 14 20 17 19 30 16
11 | 13 16 6 7 16 3 13 6 11 20 3 | 33 39 32 34 39 32 39 33 37 30 33
12 | 12 21 6 7 24 5 26 9 14 15 5 | 19 27 15 19 35 15 29 15 23 20 16
13E | 11 11 4 6 34 3 11 3 10 15 3 | 17 19 17 17 38 14 24 16 19 15 17
14E | 8 12 7 13 23 4 12 7 6 10 3 | 13 15 13 18 21 12 17 14 23 14 13
15E | 11 14 5 7 19 2 14 4 9 17 3 | 41 42 39 45 39 40 42 40 41 41 40
16 | 10 17 7 15 21 4 18 6 7 17 4 | 16 22 17 19 25 13 24 12 20 17 14
17 | 13 11 6 8 15 4 12 6 11 12 3 | 17 21 15 14 30 12 23 16 25 16 16
18 | 18 16 7 11 12 4 15 5 8 17 4 | 23 29 17 17 23 16 27 16 22 21 18
19 | 12 16 6 9 22 3 14 9 9 16 4 | 22 23 17 18 25 15 20 17 21 18 16
20 | 10 13 6 10 10 3 13 5 6 18 3 | 22 23 16 21 21 14 24 16 16 19 16
21 | 11 10 5 10 10 3 12 4 8 35 3 | 24 26 23 26 26 24 25 25 27 38 24
22 | 7 13 4 10 9 3 11 4 9 20 3 | 18 28 20 14 29 16 28 17 25 19 19
23E | 6 11 5 7 15 3 13 5 7 17 3 | 31 36 34 32 41 31 34 35 36 27 34
24 | 11 19 5 6 18 6 11 5 8 12 3 | 20 22 21 19 30 19 26 20 23 17 19
25 | 11 17 4 9 18 4 12 7 11 11 3 | 25 26 21 26 31 23 31 24 29 23 23
26E | 32 28 14 10 26 10 22 11 57 33 9 | 90 85 84 90 87 84 85 86 99 94 85
X27 | 6 --- --- --- --- 31 --- --- --- --- 0 | 53 --- --- --- --- 31 --- --- --- --- 53
28 | 15 11 5 11 24 4 15 7 12 14 4 | 18 19 16 18 32 11 23 15 15 14 15
29 | 21 14 4 9 13 4 14 5 11 20 4 | 22 18 12 16 22 11 16 14 22 24 13
30 | 13 13 5 13 15 5 11 5 9 14 3 | 18 25 17 17 23 16 23 16 24 15 17
31 | 16 12 5 10 26 3 13 6 9 15 4 | 15 23 17 19 40 16 24 16 26 15 17
32 | 8 8 4 10 14 4 7 4 8 15 2 | 17 17 13 16 21 13 18 16 16 16 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 14 6 10 18 4 14 6 14 20 |T 25 26 22 23 30 21 27 22 26 24 23
WRMS | 12 14 5 9 16 4 13 6 8 20 |NE 22 24 20 21 27 19 25 20 24 22 20
MEDI | 11 13 5 9 15 4 12 5 9 17 |MD 21 23 17 18 29 16 24 17 23 20 17
Table 3.1719.6 GPS week: 1719 Day: 6 MJD: 56283.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 12 5 7 10 5 17 6 12 48 3 | 73 73 73 75 78 75 77 77 70 76 74
2 | 12 12 5 25 15 3 12 6 9 28 4 | 32 33 36 48 39 37 35 35 35 30 36
3 | 9 12 6 10 13 4 11 5 17 18 3 | 16 17 12 17 16 15 16 13 16 13 15
4 | 7 7 4 9 13 4 7 5 8 24 2 | 36 34 35 38 43 35 39 35 34 28 36
5 | 11 14 7 7 16 3 16 5 12 25 3 | 19 31 18 15 34 16 31 18 24 26 20
6 | 11 12 7 10 12 4 12 7 14 22 3 | 26 30 27 29 31 25 33 26 21 22 27
7 | 8 12 6 9 22 4 13 5 9 17 3 | 23 24 22 20 32 18 22 19 21 20 20
8 | 9 11 5 6 17 6 9 3 9 25 3 | 19 25 17 16 20 17 22 18 17 24 19
9 | 11 10 3 13 15 4 7 5 9 16 3 | 19 29 21 20 28 21 26 21 23 19 22
10 | 13 8 4 9 11 5 7 6 9 30 3 | 24 23 22 26 28 20 25 21 18 35 22
11 | 9 15 6 6 14 5 13 7 11 20 3 | 48 49 46 47 54 45 50 47 43 44 46
12 | 16 22 6 12 23 6 23 9 14 15 5 | 28 34 25 26 37 24 35 24 27 23 26
13E | 6 9 4 10 16 3 11 4 9 14 3 | 19 24 17 16 30 17 23 18 21 19 19
14E | 9 11 6 10 18 5 13 8 9 11 3 | 15 19 18 21 18 15 19 16 25 16 16
15E | 19 15 5 6 20 4 15 4 10 13 4 | 46 47 46 46 46 46 47 45 46 45 46
16 | 11 17 6 15 17 3 18 6 12 20 4 | 28 31 24 23 30 22 31 21 29 27 24
17 | 13 13 6 6 16 4 12 5 12 14 3 | 24 28 20 15 36 18 24 18 27 20 21
18 | 14 12 5 12 12 3 13 5 10 19 3 | 31 33 21 23 25 21 31 22 28 25 24
19 | 9 20 6 12 19 3 13 7 19 14 4 | 22 28 21 19 30 17 23 18 25 19 20
20 | 10 14 5 10 12 3 13 6 7 20 3 | 24 30 18 21 22 19 27 20 21 24 20
21 | 10 11 5 8 12 3 11 4 11 39 3 | 29 32 31 34 38 31 31 30 30 44 31
22 | 6 13 5 10 9 5 12 5 10 25 3 | 19 32 21 19 31 18 30 18 25 22 21
23E | 6 11 6 7 17 2 13 5 8 11 3 | 37 38 39 33 43 37 38 36 40 29 38
24 | 10 20 5 7 20 5 11 4 10 14 3 | 26 28 26 24 34 25 31 26 31 22 26
25 | 11 15 5 8 21 3 13 5 12 11 3 | 34 35 34 34 36 32 38 31 39 27 34
26E | 30 34 16 12 25 7 24 11 59 28 9 | 98 80 91 83 76 87 83 89 97 94 85
X27 | 5 --- --- --- --- 63 --- --- --- --- 0 | 53 --- --- --- --- 35 --- --- --- --- 54
28 | 10 10 6 10 23 3 14 6 11 14 3 | 24 25 23 22 35 22 28 21 23 22 23
29 | 16 16 5 14 13 5 14 6 11 19 4 | 28 26 19 14 26 15 20 19 19 24 19
30 | 15 13 6 9 14 5 10 4 10 19 3 | 24 29 20 18 24 19 27 18 23 18 21
31 | 12 13 7 10 22 6 15 7 7 18 4 | 24 27 25 26 43 21 26 23 30 20 25
32 | 8 9 7 10 13 3 8 5 8 13 3 | 12 18 13 13 20 11 17 12 16 14 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 6 11 17 4 14 6 15 22 |T 30 32 28 28 34 27 32 27 30 28 29
WRMS | 11 14 6 9 15 4 13 5 9 19 |NE 27 31 26 26 33 24 30 25 27 26 26
MEDI | 10 12 6 10 16 4 13 5 10 19 |MD 24 30 22 23 32 21 30 21 25 24 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 4.1719 GPS week: 1719 MJD: 56277.0-56283.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3012 |U 4 4 11 | 0 0 0 |U 25 68 103 |
emr | emr 2956 | 7 6 15 | 0 0 0 | 26 68 108 |
esa | esa 2948 | 6 6 13 | 0 0 0 | 25 68 105 |
gfz | gfz 2955 |U 6 5 12 | 0 0 0 |U 24 68 104 |
grg | grg 2958 |U 8 7 19 | 0 0 0 | 28 71 112 |
igr | igr 2960 | 6 4 14 | 0 0 0 | 24 66 104 |
igs | igs 2954 | 5 5 11 | 0 0 0 | 25 68 105 |
jpl | jpl 2929 | 7 6 17 | 0 0 0 |U 26 67 108 |
mit | mit 2962 | 6 5 14 | 0 0 0 |U 26 72 108 |
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 5.1719.0 GPS week: 1719 Day: 0 MJD: 56277.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3017 | 4 4 13 | ---- ---- ---- | 8 6 14 |
emr | emr 2972 | 9 6 16 | ---- ---- ---- | 9 6 17 |
esa | esa 2976 | 6 6 16 | ---- ---- ---- | 9 7 17 |
gfz | gfz 2972 | 6 4 14 | ---- ---- ---- | 8 4 18 |
grg | grg 2976 | 10 11 27 | ---- ---- ---- | 8 10 22 |
igr | igr 2976 | 6 4 14 | ---- ---- ---- | 7 5 16 |
igs | igs 2975 | 6 5 13 | ---- ---- ---- | 8 6 16 |
jpl | jpl 2972 | 8 6 16 | ---- ---- ---- | 9 5 18 |
mit | mit 2976 | 5 3 12 | ---- ---- ---- | 11 15 24 |
Table 5.1719.1 GPS week: 1719 Day: 1 MJD: 56278.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3015 | 5 4 15 | ---- ---- ---- | 7 6 13 |
emr | emr 2964 | 9 6 20 | ---- ---- ---- | 8 5 20 |
esa | esa 2880 | 7 7 20 | ---- ---- ---- | 8 6 21 |
gfz | gfz 2964 | 7 5 17 | ---- ---- ---- | 7 4 17 |
grg | grg 2967 | 10 5 19 | ---- ---- ---- | 11 14 29 |
igr | igr 2968 | 7 4 19 | ---- ---- ---- | 6 4 14 |
igs | igs 2967 | 6 5 16 | ---- ---- ---- | 7 5 15 |
jpl | jpl 2874 | 11 9 24 | ---- ---- ---- | 8 7 21 |
mit | mit 2976 | 6 5 15 | ---- ---- ---- | 9 10 19 |
Table 5.1719.2 GPS week: 1719 Day: 2 MJD: 56279.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 3 3 10 | ---- ---- ---- | 7 6 10 |
emr | emr 2966 | 8 6 14 | ---- ---- ---- | 10 8 17 |
esa | esa 2976 | 4 6 9 | ---- ---- ---- | 7 7 13 |
gfz | gfz 2965 | 5 5 9 | ---- ---- ---- | 7 5 10 |
grg | grg 2970 | 6 5 17 | ---- ---- ---- | 10 11 21 |
igr | igr 2970 | 4 5 12 | ---- ---- ---- | 6 5 12 |
igs | igs 2967 | 5 5 9 | ---- ---- ---- | 7 6 12 |
jpl | jpl 2873 | 7 6 14 | ---- ---- ---- | 8 6 16 |
mit | mit 2976 | 5 7 10 | ---- ---- ---- | 8 11 18 |
Table 5.1719.3 GPS week: 1719 Day: 3 MJD: 56280.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 4 5 11 | ---- ---- ---- | 7 7 11 |
emr | emr 2972 | 7 8 14 | ---- ---- ---- | 10 13 22 |
esa | esa 2976 | 5 7 11 | ---- ---- ---- | 8 9 15 |
gfz | gfz 2970 | 6 5 9 | ---- ---- ---- | 7 9 14 |
grg | grg 2976 | 7 10 17 | ---- ---- ---- | 11 12 23 |
igr | igr 2976 | 5 6 13 | ---- ---- ---- | 8 8 15 |
igs | igs 2949 | 6 6 10 | ---- ---- ---- | 9 11 18 |
jpl | jpl 2972 | 7 8 15 | ---- ---- ---- | 8 9 16 |
mit | mit 2976 | 7 7 18 | ---- ---- ---- | 11 14 21 |
Table 5.1719.4 GPS week: 1719 Day: 4 MJD: 56281.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2945 | 4 4 9 | ---- ---- ---- | 8 10 21 |
emr | emr 2876 | 8 5 13 | ---- ---- ---- | 10 11 22 |
esa | esa 2880 | 6 4 10 | ---- ---- ---- | 8 11 20 |
gfz | gfz 2876 | 6 4 9 | ---- ---- ---- | 7 10 17 |
grg | grg 2878 | 9 5 19 | ---- ---- ---- | 12 14 19 |
igr | igr 2880 | 6 3 11 | ---- ---- ---- | 8 10 19 |
igs | igs 2879 | 6 4 9 | ---- ---- ---- | 9 13 21 |
jpl | jpl 2875 | 7 5 18 | ---- ---- ---- | 9 12 25 |
mit | mit 2880 | 8 5 20 | ---- ---- ---- | 9 15 22 |
Table 5.1719.5 GPS week: 1719 Day: 5 MJD: 56282.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 4 4 13 | ---- ---- ---- | 6 6 11 |
emr | emr 2971 | 6 5 14 | ---- ---- ---- | 7 5 16 |
esa | esa 2976 | 5 5 13 | ---- ---- ---- | 5 5 11 |
gfz | gfz 2971 | 5 5 12 | ---- ---- ---- | 6 7 12 |
grg | grg 2968 | 7 7 19 | ---- ---- ---- | 9 14 31 |
igr | igr 2975 | 6 4 15 | ---- ---- ---- | 5 4 12 |
igs | igs 2974 | 5 5 13 | ---- ---- ---- | 5 4 12 |
jpl | jpl 2971 | 6 4 17 | ---- ---- ---- | 7 10 21 |
mit | mit 2976 | 5 5 14 | ---- ---- ---- | 7 12 13 |
Table 5.1719.6 GPS week: 1719 Day: 6 MJD: 56283.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3013 | 5 4 10 | ---- ---- ---- | 130 439 640 |
emr | emr 2972 | 6 6 15 | ---- ---- ---- | 130 431 643 |
esa | esa 2976 | 6 5 12 | ---- ---- ---- | 130 432 639 |
gfz | gfz 2971 | 6 5 11 | ---- ---- ---- | 129 438 638 |
grg | grg 2976 | 8 8 19 | ---- ---- ---- | 133 426 639 |
igr | igr 2976 | 6 4 13 | ---- ---- ---- | 130 429 639 |
igs | igs 2968 | 5 4 11 | ---- ---- ---- | 130 432 641 |
jpl | jpl 2971 | 6 5 13 | ---- ---- ---- | 131 424 641 |
mit | mit 2976 | 6 5 11 | ---- ---- ---- | 130 430 640 |
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 6.1719 GPS week: 1719 MJD: 56277.500-56283.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -38 -21 51 -170 7 | 2 20
| 18 25 97 60 13 | 3
emr uuuuu | -3 -7 53 244 -3 | 3 27
| 20 16 79 61 14 | 6
esa uuuuu | -18 -19 29 -66 4 | -1 22
| 36 20 80 40 13 | 3
gfz uuuuu | 74 76 4 -34 10 | 6 21
| 21 19 101 100 12 | 2
grg uuuux | -27 -12 -5 9 -11 | -9 27
| 29 13 62 110 41 | 6
igr xxxxx | -58 -4 34 -22 3 | 0 20
| 15 19 80 61 10 | 3
irf xxxxx | -4 -3 11 6 2 | 0 14
| 12 8 23 29 3 | 3
jpl uuuux | 6 -32 22 147 -14 | 19 32
| 19 22 92 63 17 | 8
mit uuuuu | 34 -2 -82 -16 -1 | -2 11
| 22 11 97 88 11 | 2
ngs uuuuu | -67 24 16 63 0 | 6 17
| 50 37 96 61 11 | 3
sio xxxxx | -91 -75 15 -6 8 | 5 19
| 118 70 103 95 7 | 3
Table 7.1719.0 GPS week: 1719 Day: 0 MJD: 56277.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -12 -24 190 -116 -3 | 3 19
emr uuuuu | -1 -12 63 194 7 | 9 28
esa uuuuu | -70 3 45 -74 7 | -1 21
gfz uuuuu | 59 60 118 -74 20 | 4 20
grg uuuux | 5 -23 -62 -123 18 | -16 32
igr xxxxx | -30 -24 -92 -12 3 | 1 20
irf xxxxx | 11 -7 5 -29 1 | 2 14
jpl uuuux | 39 -55 -71 181 -10 | 25 32
mit uuuuu | 41 12 -99 10 -5 | 1 8
ngs uuuuu | -5 11 -119 52 3 | 8 19
sio xxxxx | -212 -11 -55 -157 10 | 1 19
Table 7.1719.1 GPS week: 1719 Day: 1 MJD: 56278.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -34 -33 136 -249 31 | 2 18
emr uuuuu | 10 -22 65 216 21 | 7 26
esa uuuuu | -2 -10 147 -92 30 | -2 21
gfz uuuuu | 47 57 135 -235 30 | 4 20
grg uuuux | -77 6 -86 -72 11 | -14 32
igr xxxxx | -77 -32 137 -66 22 | 0 19
irf xxxxx | -17 -8 48 -21 8 | 1 13
jpl uuuux | -2 -44 -107 114 12 | 23 32
mit uuuuu | 72 -9 -250 142 -19 | 0 8
ngs uuuuu | -82 76 0 150 17 | 6 16
sio xxxxx | -242 -15 220 -37 22 | 2 20
Table 7.1719.2 GPS week: 1719 Day: 2 MJD: 56279.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -39 -7 -75 -104 12 | 7 21
emr uuuuu | 25 -23 36 363 -18 | 10 28
esa uuuuu | -20 -28 -79 11 5 | 4 22
gfz uuuuu | 86 99 1 25 6 | 10 22
grg uuuux | -37 -8 -36 -38 38 | -7 24
igr xxxxx | -58 9 25 33 1 | 5 20
irf xxxxx | -2 8 1 -19 0 | 4 13
jpl uuuux | 11 3 156 80 -20 | 28 34
mit uuuuu | 40 -2 -18 -136 -4 | 0 8
ngs uuuuu | -136 -15 188 50 9 | 11 18
sio xxxxx | -169 0 -15 -54 7 | 8 19
Table 7.1719.3 GPS week: 1719 Day: 3 MJD: 56280.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -19 1 40 -152 -4 | 3 19
emr uuuuu | -36 -8 201 217 -8 | 2 25
esa uuuuu | -44 -46 62 -53 -13 | 0 20
gfz uuuuu | 103 94 -147 49 -1 | 7 21
grg uuuux | -17 -16 -15 -51 9 | -1 18
igr xxxxx | -54 3 76 -15 -8 | 1 19
irf xxxxx | -5 4 -25 31 0 | 0 14
jpl uuuux | -6 -19 78 238 -43 | 22 31
mit uuuuu | 17 14 -125 -39 8 | -3 12
ngs uuuuu | -1 -4 62 -25 0 | 8 17
sio xxxxx | -76 -94 84 -27 2 | 6 19
Table 7.1719.4 GPS week: 1719 Day: 4 MJD: 56281.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -61 -2 -11 -244 -5 | 0 20
emr uuuuu | -17 -14 74 281 -7 | -2 26
esa uuuuu | 28 -19 -41 -69 -2 | -4 23
gfz uuuuu | 75 89 -84 19 0 | 5 22
grg uuuux | -17 -15 70 194 -63 | -3 18
igr xxxxx | -70 21 -51 74 0 | -3 21
irf xxxxx | -8 4 5 36 2 | -3 15
jpl uuuux | 23 -55 75 182 -22 | 15 33
mit uuuuu | 8 1 23 -88 9 | -4 13
ngs uuuuu | -108 1 -10 52 -7 | 5 17
sio xxxxx | -25 -80 -21 59 7 | 4 19
Table 7.1719.5 GPS week: 1719 Day: 5 MJD: 56282.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -46 -71 -34 -129 3 | 0 20
emr uuuuu | 8 12 -36 193 -17 | -2 26
esa uuuuu | -41 6 -25 -117 -1 | -3 23
gfz uuuuu | 94 78 -20 30 1 | 5 21
grg uuuux | 2 -28 68 90 -69 | -9 28
igr xxxxx | -61 4 64 -80 -3 | -2 21
irf xxxxx | 9 -16 26 36 5 | -3 15
jpl uuuux | -8 -40 30 173 -16 | 13 33
mit uuuuu | 42 -16 18 -11 12 | -4 13
ngs uuuuu | -65 25 37 27 -14 | 5 17
sio xxxxx | 36 -161 -63 30 4 | 6 19
Table 7.1719.6 GPS week: 1719 Day: 6 MJD: 56283.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -55 -11 108 -195 15 | -2 20
emr uuuuu | -14 19 -29 242 0 | -6 26
esa uuuuu | 23 -40 91 -72 1 | -5 23
gfz uuuuu | 55 55 22 -54 11 | 5 21
grg uuuux | -46 3 29 61 -19 | -16 37
igr xxxxx | -60 -12 79 -90 6 | -4 20
irf xxxxx | -20 -5 19 8 0 | -3 15
jpl uuuux | -13 -13 -7 61 -2 | 7 27
mit uuuuu | 17 -11 -120 8 -7 | -4 14
ngs uuuuu | -70 75 -44 134 -7 | 2 16
sio xxxxx | 51 -165 -42 141 6 | 5 19
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