[IGSREPORT-21786] Wk 1736 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri May 3 05:27:45 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1736 (Apr 14, 2013 - Apr 20, 2013)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1736[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1736[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1736[0-6].cls IGS GPS clock combination summary report.
igs17367.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17367.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 | 10 10 KOUC KOUC
0 | EMR | MATE WUHN
0 | ESA | 10 10 MATE UNSA
0 | GFZ | 10 LHAZ
0 | GRG | NKLG MATE NKLG NRMD
0 | JPL | RAMO
0 | MIT | 30 30 NICO USNO
1 | COD | 10 10 32
1 | EMR | WUHN
1 | ESA | 10 32 10 32 NTUS MAL2 UNSA
1 | GFZ | 10 32 NKLG
1 | GRG | 30 AREQ BRST CAS1 NICO NKLG AREQ BRST CAS1 HYDE NICO
1 | GRG | NKLG NOVM REUN
1 | JPL | 32
2 | COD | 10 10 32 SUTM TSKB
2 | EMR | WUHN
2 | ESA | 10 32 10 32 UNSA
2 | GFZ | 10 32 NOVM POTS
2 | GRG | BARH DARW HYDE LHAZ POLV
2 | MIT | NTUS HYDE NTUS
3 | COD | 10 10 32 JOZ2 KOUC JOZ2 KOUC
3 | EMR | WUHN
3 | ESA | 10 32 10 32 HYDE ABMF HYDE WIND
3 | GFZ | 10 32 HYDE
4 | COD | 10 32 10 32 KOUC KOUC
4 | EMR | THTI
4 | ESA | 10 32 10 32 THTI FAA1
4 | GFZ | 10 30 32 ADIS IRKT LHAZ MIZU NTUS
4 | GRG | GOPE POLV THTI
4 | MIT | REUN
5 | COD | 10 32 10 32 XMIS FLRS
5 | ESA | 10 32 10 32 CAGZ NTUS CAGZ NTUS UNSA
5 | GFZ | 10 32
5 | GRG | LHAZ POTS
5 | MIT | HNPT TSKB TSKB
6 | COD | 10 32 10 32 XMIS XMIS
6 | EMR | PRDS PRDS
6 | ESA | 10 32 10 32 HERS MATE HERS MATE NTUS UNSA
6 | GFZ | 10 32
6 | GRG | ADIS
6 | MIT | 20 20 NTUS
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. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G32 | 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 RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.4 .9 -1.8 -49 -9 25 .27
EMR | 0 | 3.3 -6.9 14.9 -7 -10 11 .50
ESA | 0 | 4.7 2.6 23.1 50 1 -12 .42
GFZ | 0 | .0 .6 -.4 -31 -28 5 -.15
GRG | 0 | 8.9 -2.9 19.0 -37 16 5 .54
JPL | 0 | 8.2 -1.3 22.9 -60 33 44 .42
MIT | 0 | .6 -7.0 20.0 -8 0 -19 .20
NGS | 0 | 7.5 -1.1 15.2 -95 -73 60 .94
SIO | 0 | .6 -4.6 -40.7 -149 -372 26 .36
COD | 1 | -.6 .3 -1.3 -45 -13 24 .24
EMR | 1 | -.3 -8.3 17.9 3 0 34 .51
ESA | 1 | 1.1 -.8 30.2 -16 -41 4 .21
GFZ | 1 | .2 1.3 .1 -35 -31 2 -.52
GRG | 1 | 4.7 -4.8 29.0 -50 11 -28 .41
JPL | 1 | 8.1 -2.8 22.9 -35 67 29 .52
MIT | 1 | 4.5 -8.6 24.2 -15 -7 -16 .47
NGS | 1 | .2 -4.9 19.8 -145 -35 -10 .87
SIO | 1 | 2.9 -7.1 -35.9 -208 -401 48 .39
COD | 2 | -.9 1.5 -2.1 -38 -13 5 .22
EMR | 2 | .7 -9.1 13.8 9 0 22 .52
ESA | 2 | 5.2 1.8 28.7 42 -26 -4 .41
GFZ | 2 | -.4 .5 -.4 -32 -21 8 -.11
GRG | 2 | 7.7 -4.1 25.4 -28 11 -11 .65
JPL | 2 | -1.4 1.0 15.8 -23 -61 30 .28
MIT | 2 | 4.0 -5.8 19.4 -6 -2 -28 .34
NGS | 2 | 5.0 -8.6 15.6 -138 -58 16 .66
SIO | 2 | .2 -5.9 -35.2 -196 -363 54 .39
COD | 3 | -1.2 1.0 -2.0 -30 3 -13 .26
EMR | 3 | 2.4 -9.8 5.4 -3 -3 23 .54
ESA | 3 | 2.0 5.1 28.1 41 -46 20 .44
GFZ | 3 | -.5 .7 -.1 -43 -30 2 -.15
GRG | 3 | 7.8 -7.7 21.9 -31 7 -17 .56
JPL | 3 | -.3 -8.6 14.8 -38 -10 -49 .55
MIT | 3 | 5.0 -2.1 18.9 -5 0 -25 .41
NGS | 3 | 6.5 -2.5 19.8 -126 -80 45 .85
SIO | 3 | 1.6 -3.1 -48.9 -129 -431 52 .58
COD | 4 | -1.1 .6 -2.6 -47 -5 15 .21
EMR | 4 | -4.5 -8.4 12.4 -2 0 23 .40
ESA | 4 | .7 -1.0 27.1 81 -88 60 .51
GFZ | 4 | -.6 .2 -.7 -49 -22 4 .26
GRG | 4 | -1.8 -2.2 26.9 -24 11 -24 .76
JPL | 4 | 2.0 -2.0 21.8 -63 21 -16 .23
MIT | 4 | 4.2 -2.2 16.4 -4 -5 -23 .27
NGS | 4 | -.9 -1.9 12.1 -94 -17 -7 .76
SIO | 4 | .9 -5.6 -34.3 -180 -346 50 .35
COD | 5 | -1.9 1.0 -1.6 -43 19 11 .14
EMR | 5 | -1.5 -7.9 15.0 -3 2 5 .23
ESA | 5 | 3.0 2.4 27.5 52 -24 -6 .40
GFZ | 5 | -.6 .5 -.5 -42 -24 0 .10
GRG | 5 | -1.2 -.9 21.2 -31 7 -9 .55
JPL | 5 | 2.1 -1.4 19.3 -37 -10 52 .33
MIT | 5 | 1.5 .5 15.7 7 -9 -14 .32
NGS | 5 | .1 1.6 7.3 -47 -13 13 .69
SIO | 5 | 1.1 -.6 -21.2 -117 -300 41 .35
COD | 6 | -1.8 1.3 -2.2 -51 27 7 .01
EMR | 6 | -1.6 -13.4 13.8 -2 3 9 .32
ESA | 6 | -1.5 -.1 24.5 29 -38 -15 .30
GFZ | 6 | -.8 .8 -.3 -43 -16 3 -.30
GRG | 6 | -1.9 -2.4 11.4 -40 13 11 .64
JPL | 6 | 5.0 4.0 16.1 -78 5 -5 .27
MIT | 6 | 1.8 -.1 15.8 8 -1 -26 .25
NGS | 6 | 3.5 -7.2 11.5 -125 -44 7 .76
SIO | 6 | -2.0 -.5 -22.9 -99 -244 91 .37
9. 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.
10. 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 1.1736.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1736.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 2.1736.[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 3.1736.[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 5.1736.0-6). 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 1736 summary. (Apr 14, 2013 - Apr 20, 2013)
Table 1.1736.a GPS week: 1736 MJD: 56396.000-56402.000
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 266| 0 0 0 4 -36 4 -.39 11 11 | -935 -163 25 89
| 0 0 1 18 9 9 .04 | 382 543
emr 80| 0 -3 -2 -31 -26 0 .27 14 14 | 1518 118 13 97
| 0 1 1 14 10 15 .04 | 1252 1161
esa 150| 0 1 5 13 2 3 .12 7 7 | -963 739 49 146
| 0 0 1 13 8 11 .01 | 1071 1644
gfz 199| 0 0 -3 -23 -22 3 -.37 10 9 | 286 -150 20 95
| 0 0 1 43 45 5 .03 | 470 696
grg 137| 3 1 8 -4 1 -18 .59 15 13 | 91 -223 20 136
| 1 0 1 13 18 10 .02 | 272 401
igr n/a| 0 0 -3 18 30 -18 -.10 4 4 | 701 520 19 87
| 0 0 0 10 12 9 .02 | 1706 1270
jpl 80| 0 0 -9 -16 -7 0 .37 15 15 | 1281 114 18 104
| 2 1 1 16 22 15 .03 | 1343 1279
mit 237| 0 0 0 16 11 -5 -.55 11 10 | 683 -3810 23 177
| 0 1 1 21 17 10 .02 | 1635 7340
ngs 241| 0 0 -2 16 53 -7 .32 10 9 | -939 -220 1794 3554
| 1 0 3 27 27 11 .03 | 369 526
sio 285| 0 2 -6 -194 -356 34 -.21 17 17 | --- --- --- ---
| 0 0 1 50 74 34 .02 | --- ---
Table 1.1736.b GPS week : 1736 MJD: 56396.000-56402.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 3 3 4 4 4 4 |
2 | 5 5 5 4 5 5 5 |
3 | 4 3 3 4 4 4 4 |
4 | 4 3 3 3 3 4 3 |
5 | 5 5 5 5 5 4 4 |
6 | 3 3 3 3 4 4 4 |
7 | 4 4 4 4 5 5 5 |
8 | 3 3 3 3 3 4 4 |
9 | 4 4 4 4 3 4 4 |
10 | 5 5 5 5 5 4 5 |
11 | 4 4 4 4 4 4 4 |
12 | 6 6 6 5 6 6 6 |
13 | 4 4 4 4 4 5 4 |
14 | 4 4 4 4 4 4 4 |
15 | 5 5 6 8 5 6 7 |
16 | 5 4 4 4 4 4 4 |
17 | 5 5 5 5 5 5 5 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 5 4 4 4 4 4 4 |
21 | 5 4 5 5 4 5 4 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 5 5 5 |
24 | 5 5 4 4 4 4 4 |
25 | 4 4 5 5 5 4 4 |
26 | 4 3 3 3 4 3 3 |
27 | 0 0 0 0 0 0 0 |
28 | 4 4 4 4 4 4 4 |
29 | 5 6 5 5 5 5 5 |
30 | 5 7 5 8 14 10 14 |
31 | 6 5 5 5 4 4 4 |
32 | 5 5 5 5 4 5 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
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1736.0 GPS week: 1736 Day: 0 MJD: 56396.000
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| 0 1 0 38 -39 18 -.39 12 12 | -862 -211 29 85
emr 80| 1 -1 0 -22 -33 -13 .22 15 15 | 2573 -1252 20 100
esa 150| 0 0 4 26 11 -4 .12 7 7 | 587 -33 42 149
gfz 199| 0 0 -3 -60 -12 5 -.37 10 10 | -184 -503 20 93
grg 135| 4 1 6 -23 8 -16 .59 14 13 | 473 -1046 25 151
igr n/a| 0 0 -4 26 36 -28 -.13 5 5 | 286 -1344 19 81
jpl 80| -4 0 -11 -26 12 -1 .31 16 16 | 2229 -1647 21 102
mit 240| 0 -3 0 19 0 -11 -.56 12 11 | 358 -750 23 160
ngs 245| -2 0 -1 9 31 3 .32 11 10 | -877 -256 1870 3350
sio 282| 1 2 -5 -200 -385 1 -.23 18 17 | --- --- --- ---
Table 2.1736.1 GPS week: 1736 Day: 1 MJD: 56397.000
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 267| 0 0 -1 -17 -49 14 -.44 12 12 | -951 -131 26 76
emr 80| 0 -1 -2 -54 -42 25 .28 14 14 | 1730 -394 12 95
esa 150| 0 2 4 15 -6 -17 .13 7 7 | -976 1076 54 159
gfz 196| 0 0 -5 1 6 5 -.42 9 9 | -39 759 21 93
grg 137| 3 1 6 -19 27 -30 .58 14 13 | -8 7 21 141
igr n/a| 0 1 -3 15 23 -25 -.08 4 4 | -191 0 19 90
jpl 80| -3 0 -9 -19 -30 15 .38 16 16 | 1288 -403 20 95
mit 236| 0 -2 0 6 -16 -6 -.56 11 10 | -1315 2547 23 183
ngs 241| 0 0 2 33 70 0 .35 9 8 | -961 -184 1913 3665
sio 274| 0 2 -5 -256 -417 27 -.24 17 17 | --- --- --- ---
Table 2.1736.2 GPS week: 1736 Day: 2 MJD: 56398.000
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| 0 0 -1 2 -37 -2 -.38 10 10 | -1343 389 26 93
emr 80| 0 -2 -1 -34 -21 2 .30 14 14 | 1292 -92 12 97
esa 150| -1 1 4 19 0 11 .10 6 7 | -2367 3449 53 139
gfz 200| 0 -1 -4 -23 16 -4 -.39 11 10 | 403 277 19 93
grg 139| 4 1 8 -4 16 -9 .62 13 13 | 183 -40 18 116
igr n/a| 0 1 -4 17 30 -29 -.09 5 5 | -118 553 18 84
jpl 80| 1 0 -10 -2 -24 1 .38 15 15 | 918 41 20 106
mit 237| 0 -2 1 4 0 -6 -.55 11 10 | -241 603 21 194
ngs 239| 0 0 -1 3 27 -11 .27 10 9 | -1260 216 1475 3721
sio 265| 0 2 -5 -250 -389 25 -.21 17 16 | --- --- --- ---
Table 2.1736.3 GPS week: 1736 Day: 3 MJD: 56399.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 265| 0 0 -1 7 -36 6 -.38 12 10 | -646 -840 27 102
emr 80| 0 -4 -4 -26 -32 8 .30 14 14 | 728 -363 15 100
esa 150| 0 1 6 5 -7 3 .12 8 8 | -2309 2303 51 139
gfz 202| 0 0 -3 15 8 3 -.34 8 8 | 576 -720 22 95
grg 140| 3 2 8 11 1 -28 .62 15 12 | 123 -158 25 141
igr n/a| 0 1 -4 24 7 -15 -.10 4 4 | -225 236 20 79
jpl 80| 0 1 -9 -7 -27 -28 .35 15 15 | 314 -217 19 108
mit 237| 0 -1 -1 9 37 4 -.52 10 10 | 2979 -14401 25 188
ngs 245| 0 1 2 -16 22 -7 .35 10 9 | -680 -855 1692 3644
sio 272| 0 1 -7 -170 -432 46 -.19 17 16 | --- --- --- ---
Table 2.1736.4 GPS week: 1736 Day: 4 MJD: 56400.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 265| 0 0 0 -14 -41 -5 -.32 10 10 | -1557 697 24 81
emr 80| 0 -4 -3 -45 -23 8 .31 15 15 | -648 2239 12 101
esa 150| 0 1 6 -14 16 15 .13 7 7 | -935 177 50 136
gfz 203| 1 -1 -2 34 -73 6 -.34 10 10 | -156 623 21 91
grg 140| 4 2 10 9 -13 -23 .57 15 15 | -417 130 17 117
igr n/a| 0 0 -2 -2 34 -16 -.10 4 4 | -874 2706 18 82
jpl 80| 1 0 -10 -47 14 1 .42 15 15 | -849 2401 16 84
mit 236| 0 0 0 51 20 -12 -.54 10 9 | -281 267 27 175
ngs 243| 0 0 -6 11 67 -10 .32 11 8 | -1582 680 1975 3308
sio 294| 0 2 -6 -201 -351 24 -.19 16 18 | --- --- --- ---
Table 2.1736.5 GPS week: 1736 Day: 5 MJD: 56401.000
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 267| -1 0 1 7 -17 1 -.44 13 13 | -655 -460 25 94
emr 80| 0 -3 -1 -13 -9 -16 .23 14 14 | 1748 1080 13 89
esa 150| 0 0 8 18 2 5 .13 6 6 | -331 -1079 50 145
gfz 204| 0 -1 -4 -84 -99 -3 -.35 9 9 | 1127 -1019 20 106
grg 138| 1 3 11 -5 -27 -20 .60 16 15 | 48 -34 22 178
igr n/a| 0 0 -2 17 49 -4 -.09 4 4 | 2077 1447 21 94
jpl 80| 0 -1 -8 0 19 20 .38 15 15 | 1766 1033 19 119
mit 238| 0 1 0 -10 14 -17 -.57 10 10 | 2880 -14485 21 162
ngs 244| 0 0 -7 68 97 4 .33 10 9 | -673 -505 1891 3680
sio 293| 0 2 -5 -173 -289 13 -.21 17 17 | --- --- --- ---
Table 2.1736.6 GPS week: 1736 Day: 6 MJD: 56402.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 263| -1 0 0 3 -34 -1 -.40 12 12 | -536 -586 24 95
emr 80| 0 -4 -2 -22 -22 -14 .23 14 14 | 3203 -387 12 98
esa 150| 0 1 5 21 0 10 .10 6 6 | -415 -715 43 155
gfz 189| 0 0 -2 -48 -6 12 -.41 10 9 | 280 -469 20 96
grg 135| 1 1 7 -1 -3 0 .58 15 13 | 237 -424 15 111
igr n/a| 0 0 -2 30 33 -11 -.13 4 4 | 3957 47 19 100
jpl 80| 0 2 -7 -16 -16 -5 .38 15 14 | 3302 -405 17 117
mit 237| 1 1 -1 36 22 13 -.58 12 12 | 401 -454 21 180
ngs 236| 0 -1 -3 6 58 -30 .31 11 10 | -540 -640 1744 3511
sio 316| 0 2 -8 -107 -226 105 -.20 18 17 | --- --- --- ---
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 3.1736.0 GPS week: 1736 Day: 0 MJD: 56396.000
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 9 6 7 11 4 13 10 13 16 3 | 25 31 23 21 34 26 38 23 35 27 25
2 | 10 18 8 12 15 3 22 17 8 19 5 | 30 38 38 37 40 34 41 30 37 34 34
3 | 10 8 4 9 13 3 9 8 13 13 3 | 17 20 19 16 25 14 17 13 21 13 16
4 | 4 11 5 10 12 5 14 9 7 21 3 | 11 14 16 11 17 10 17 19 17 25 12
5E | 8 20 7 9 11 5 21 11 10 15 4 | 27 32 28 25 34 25 31 33 31 32 27
6 | 10 9 4 9 9 2 10 9 12 18 3 | 18 22 22 17 26 16 19 20 21 16 18
7 | 14 12 8 9 17 5 11 10 13 17 4 | 15 21 15 13 30 12 20 15 23 18 14
8 | 10 12 5 7 11 4 13 6 8 12 3 | 15 22 15 13 17 12 21 14 21 14 13
9 | 8 9 6 11 18 3 15 8 8 14 3 | 13 19 12 13 21 10 22 14 15 13 12
10E | 16 14 7 11 14 6 17 19 7 17 5 | 44 48 45 47 45 46 47 55 46 46 45
11 | 9 14 6 8 13 4 13 14 13 17 4 | 40 47 47 43 56 41 45 45 41 42 43
12 | 14 22 7 10 20 5 27 11 15 16 5 | 20 22 15 17 30 13 26 15 21 12 14
13 | 8 16 6 11 14 3 15 11 10 21 4 | 20 28 24 28 36 23 30 25 22 29 23
14 | 10 18 7 11 11 8 18 9 11 22 4 | 32 29 32 38 33 35 31 34 27 32 30
15 | 19 18 7 10 16 7 20 12 13 28 5 | 22 25 22 18 32 18 27 17 22 28 18
16 | 12 16 7 8 13 4 21 9 11 18 4 | 17 22 16 13 26 11 22 9 21 12 14
17 | 12 19 9 14 9 4 17 12 11 21 4 | 21 25 30 30 28 23 24 31 26 24 24
18E | 8 14 4 7 17 4 15 9 14 12 4 | 34 29 30 31 34 31 34 29 43 27 31
19 | 8 11 6 11 10 4 14 7 14 23 3 | 18 22 25 21 26 20 21 17 22 15 20
20E | 11 12 7 9 10 6 12 19 11 10 4 | 19 17 15 15 19 13 18 18 19 18 14
21 | 9 15 7 8 18 4 18 12 15 17 4 | 17 19 21 21 32 18 21 22 19 21 17
22E | 11 13 4 7 15 5 14 6 11 16 3 | 19 13 13 16 18 14 17 14 21 14 12
23 | 9 15 7 12 11 5 12 14 10 19 4 | 18 26 24 27 29 22 27 23 24 26 22
24 | 12 14 5 9 15 5 16 16 16 11 4 | 16 27 17 18 27 16 26 20 25 17 18
25 | 11 18 6 11 12 4 11 12 9 12 4 | 13 24 16 16 25 11 22 12 18 13 13
26 | 10 10 5 9 13 3 12 9 11 14 3 | 16 19 19 18 26 18 19 19 20 19 17
X27 | 7 --- --- --- --- 74 --- --- --- --- 0 | 69 --- --- --- --- 28 --- --- --- --- 69
28 | 8 12 6 8 19 6 16 11 9 13 4 | 14 18 15 14 30 12 19 17 19 12 13
29 | 12 16 7 11 12 4 20 15 8 26 4 | 24 25 27 25 30 21 24 20 22 23 22
30 | 22 12 9 15 13 6 13 9 12 --- 5 | 42 44 14 33 42 37 18 38 19 --- 39
31 | 24 16 9 9 19 6 15 15 10 17 5 | 33 26 20 18 36 19 26 18 27 14 21
32E | 19 18 8 12 14 7 17 10 10 17 5 | 158 153 156 151 156 158 153 153 160 151 154
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 7 10 14 5 16 12 11 18 |T 28 29 26 26 34 25 29 26 29 26 27
WRMS | 12 15 7 10 13 5 16 11 10 17 |NE 22 24 22 21 29 19 25 20 23 20 21
MEDI | 10 14 7 9 13 4 15 11 11 17 |MD 19 25 21 18 30 18 24 20 22 19 18
Table 3.1736.1 GPS week: 1736 Day: 1 MJD: 56397.000
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 6 10 2 12 8 8 15 3 | 20 24 19 15 26 17 30 17 28 18 18
2 | 9 17 8 10 16 3 21 15 9 18 5 | 41 45 43 36 45 39 47 42 47 40 41
3 | 10 10 5 9 11 3 11 7 9 13 3 | 8 17 13 9 16 10 17 10 20 13 11
4 | 11 10 4 7 14 4 10 10 8 20 3 | 23 20 17 15 18 17 23 20 19 26 18
5E | 12 16 9 8 16 5 19 17 7 13 4 | 34 35 29 29 30 29 36 25 26 28 28
6 | 9 9 6 8 9 4 12 7 10 15 3 | 9 20 14 8 18 11 17 15 20 15 12
7 | 11 11 9 8 17 4 12 12 11 16 4 | 16 24 15 15 30 15 24 17 22 20 16
8 | 9 9 6 8 10 4 13 8 6 13 3 | 19 21 15 12 16 13 25 16 24 18 15
9 | 8 9 6 8 17 4 12 6 6 11 3 | 20 22 18 17 18 16 25 20 23 19 17
10E | 16 15 7 10 17 6 16 15 8 19 4 | 49 47 45 50 46 46 51 52 43 53 46
11 | 11 14 7 10 15 4 15 9 10 14 4 | 27 37 29 30 43 28 36 30 32 29 29
12 | 16 21 7 8 20 3 25 12 12 18 5 | 21 23 16 12 27 14 26 17 26 15 14
13 | 11 14 6 9 15 4 12 10 13 17 4 | 21 29 19 18 32 18 30 18 21 22 19
14 | 8 18 8 11 11 5 18 8 8 22 4 | 19 25 24 26 27 23 26 22 25 24 21
15 | 12 18 7 11 14 5 19 7 8 28 4 | 18 26 17 19 26 16 26 17 22 23 17
16 | 6 11 6 9 15 3 20 12 9 20 4 | 10 23 15 13 24 12 23 10 21 14 13
17 | 15 20 10 13 10 4 20 11 10 22 5 | 31 25 22 21 22 18 27 23 24 21 20
18E | 9 11 6 9 19 4 13 8 9 12 3 | 37 43 39 37 43 37 39 38 39 41 38
19 | 9 13 7 8 9 3 15 7 9 23 3 | 10 22 17 10 19 13 23 11 23 13 14
20E | 9 12 6 9 11 4 11 16 11 10 4 | 12 14 11 10 15 10 19 18 24 12 10
21 | 7 15 8 7 16 3 17 10 9 15 4 | 13 21 15 15 24 13 20 19 20 17 13
22E | 8 11 8 9 15 5 14 10 8 15 3 | 19 16 13 18 13 13 18 18 15 18 13
23 | 11 13 7 11 13 2 12 11 11 16 4 | 18 25 18 17 27 17 27 19 20 22 18
24 | 18 13 6 9 19 5 16 13 11 10 4 | 26 21 17 12 26 14 23 17 27 15 15
25 | 9 16 7 11 12 5 12 11 12 14 4 | 10 23 14 13 22 11 24 13 21 14 12
26 | 13 8 5 9 13 3 10 7 4 14 3 | 20 19 17 21 22 18 22 19 20 19 17
X27 | 7 --- --- --- --- 52 --- --- --- --- 0 | 66 --- --- --- --- 27 --- --- --- --- 66
28 | 12 12 7 10 17 5 16 11 7 13 4 | 17 21 15 13 27 12 23 16 21 14 13
29 | 25 18 7 9 12 5 19 16 10 27 5 | 31 25 20 14 21 15 23 12 29 19 18
X30 | 14 14 --- 14 16 18 --- 11 --- --- 7 | 30 40 --- 27 33 29 --- 26 --- --- 30
31 | 10 17 9 8 18 4 16 16 9 17 4 | 17 25 17 15 35 14 25 16 26 12 17
32E | 15 13 8 11 12 7 14 12 11 17 4 | 143 138 138 140 137 140 137 140 136 139 138
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 7 9 14 4 16 11 9 17 |T 26 29 24 22 29 22 30 24 28 25 24
WRMS | 12 14 7 9 13 4 16 10 8 17 |NE 21 24 18 16 25 16 25 18 24 19 19
MEDI | 11 13 7 9 15 4 14 11 9 15 |MD 20 24 17 15 26 16 25 18 23 19 17
Table 3.1736.2 GPS week: 1736 Day: 2 MJD: 56398.000
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 8 5 8 11 4 14 7 10 11 3 | 24 24 19 18 26 20 32 18 27 20 20
2 | 9 17 7 13 13 4 20 12 12 17 4 | 29 39 37 33 44 31 41 33 40 33 35
3 | 8 9 6 10 10 2 11 8 8 13 3 | 12 19 17 15 20 13 18 14 20 13 14
4 | 6 10 3 9 10 4 10 12 9 21 3 | 18 18 17 12 18 13 18 20 18 27 15
5E | 8 20 6 9 13 5 21 15 11 10 4 | 24 29 25 26 24 25 27 28 21 27 23
6 | 7 10 7 9 10 3 10 8 7 15 3 | 14 20 20 16 23 15 18 18 20 15 16
7 | 9 12 8 12 17 5 14 9 11 15 4 | 15 22 14 16 30 14 19 15 24 18 15
8 | 7 11 5 6 10 4 11 7 8 11 3 | 21 23 18 18 18 18 23 23 26 22 19
9 | 7 10 5 8 17 3 12 9 8 12 3 | 18 21 14 14 17 14 20 20 19 19 15
10E | 11 15 8 11 14 4 17 13 9 17 4 | 42 41 40 46 32 40 35 48 34 45 39
11 | 7 13 5 8 14 5 13 6 10 13 3 | 34 39 38 33 48 34 39 35 36 34 35
12 | 12 21 6 10 20 4 26 14 11 17 5 | 18 23 15 15 26 14 25 22 22 17 14
13 | 9 13 6 12 14 3 13 11 13 18 4 | 18 27 20 22 33 19 30 20 24 24 20
14 | 9 17 6 13 11 7 16 7 12 21 4 | 24 24 26 31 27 25 27 24 23 25 23
15 | 26 18 7 10 16 6 20 11 9 30 5 | 20 24 16 17 25 14 22 14 18 23 14
16 | 5 14 6 9 15 4 20 11 9 18 4 | 11 19 14 11 25 11 19 12 22 13 12
17 | 10 17 9 16 10 5 16 13 14 22 5 | 18 25 22 27 22 18 23 28 19 21 18
18E | 5 12 5 9 11 6 12 11 11 14 3 | 35 34 32 34 32 32 34 30 37 32 32
19 | 8 13 7 9 11 3 14 7 8 24 3 | 14 21 21 16 20 15 21 15 21 14 16
20E | 7 14 5 8 12 3 12 10 11 10 3 | 18 22 20 20 21 18 21 23 23 22 19
21 | 9 16 9 11 13 3 17 13 10 16 4 | 18 20 19 20 27 15 21 16 21 15 16
22E | 6 12 6 11 13 5 12 10 10 14 3 | 14 14 11 17 13 11 14 14 17 15 10
23 | 7 12 5 14 12 5 15 16 11 17 4 | 19 25 19 22 27 19 24 19 25 22 19
24 | 8 13 7 12 15 6 13 12 8 8 4 | 17 24 16 16 25 14 23 19 22 17 16
25 | 8 19 7 11 12 4 12 17 14 13 4 | 14 25 13 14 25 12 23 19 20 17 13
26 | 8 9 6 8 11 3 11 7 7 13 3 | 19 19 20 19 22 19 19 19 20 23 18
X27 | 6 --- --- --- --- 53 --- --- --- --- 0 | 47 --- --- --- --- 18 --- --- --- --- 47
28 | 7 14 7 10 16 8 14 7 10 10 4 | 13 20 15 15 28 15 22 18 20 14 13
29 | 11 20 10 11 14 4 21 12 11 24 5 | 17 25 21 19 24 17 24 17 20 19 17
30 | 12 14 8 12 14 4 16 10 13 --- 4 | 40 45 15 30 41 38 22 36 17 --- 39
31 | 12 17 7 13 17 5 14 15 9 15 4 | 20 25 16 18 35 16 24 16 22 14 17
32E | 14 15 4 10 15 6 15 15 9 16 4 | 86 81 77 85 70 79 75 83 72 76 79
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 14 6 11 13 5 15 11 10 17 |T 23 27 22 23 28 21 25 23 24 23 22
WRMS | 10 14 7 10 13 5 15 10 9 16 |NE 19 23 19 19 26 17 23 19 22 19 19
MEDI | 8 14 6 10 13 4 14 11 10 15 |MD 18 24 19 18 25 17 23 19 22 20 17
Table 3.1736.3 GPS week: 1736 Day: 3 MJD: 56399.000
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 10 6 7 10 4 15 5 11 10 3 | 19 25 18 17 26 19 29 17 26 20 18
2 | 8 15 8 12 13 3 19 7 8 17 4 | 54 59 56 53 60 54 59 54 57 53 55
3 | 9 9 7 8 8 2 11 9 10 16 3 | 13 17 18 13 20 11 16 10 16 12 12
4 | 9 11 5 6 12 3 10 10 7 20 3 | 17 18 17 14 20 15 20 20 20 27 16
5E | 11 15 7 9 17 4 22 9 11 12 4 | 22 24 18 21 23 19 24 22 18 21 19
6 | 7 8 9 7 8 2 11 10 10 18 3 | 15 18 22 17 25 14 20 16 18 14 16
7 | 10 11 8 8 17 3 11 9 12 15 4 | 18 23 19 15 31 17 22 16 25 20 18
8 | 9 12 6 6 10 4 14 7 6 13 3 | 15 22 13 11 16 11 19 11 18 14 12
9 | 7 11 7 6 15 3 13 10 8 11 3 | 14 20 12 13 15 10 21 18 15 15 12
10E | 14 17 7 9 14 4 18 10 8 17 4 | 50 50 48 51 43 47 46 51 48 47 47
11 | 9 14 5 8 13 4 13 4 12 13 3 | 35 43 44 40 53 38 43 38 44 38 40
12 | 14 20 6 7 18 3 24 12 9 16 5 | 19 22 16 14 27 13 24 18 22 16 14
13 | 10 14 6 10 16 4 12 9 8 18 4 | 18 30 22 24 35 22 30 21 19 24 22
14 | 6 16 9 8 12 6 15 7 8 21 3 | 25 28 27 30 28 29 29 26 25 27 26
15 | 41 19 10 10 16 6 17 14 13 28 7 | 27 26 18 19 27 16 23 18 25 24 16
16 | 6 12 7 7 11 4 19 13 9 22 4 | 11 19 15 12 26 10 23 9 19 12 12
17 | 17 20 9 10 9 6 16 13 8 22 5 | 26 23 29 26 26 21 22 27 26 21 22
18E | 7 10 8 8 21 5 12 10 9 15 4 | 16 17 16 18 22 15 17 14 22 15 14
19 | 7 14 9 7 8 3 16 7 12 23 3 | 14 21 23 16 23 15 21 14 20 14 17
20E | 8 14 6 9 22 7 13 13 10 10 4 | 28 30 30 27 34 30 29 28 33 30 29
21 | 8 14 11 10 15 4 15 11 11 17 4 | 23 24 24 25 30 21 23 22 20 20 20
22E | 5 11 7 7 16 3 12 9 8 18 3 | 15 16 14 17 18 12 16 15 15 18 12
23 | 9 14 6 12 17 4 11 12 11 17 4 | 16 26 22 24 31 21 25 19 20 21 20
24 | 8 12 9 8 18 3 14 11 8 10 4 | 22 26 22 16 27 16 25 20 22 19 18
25 | 10 19 8 8 14 4 12 16 9 13 4 | 18 26 21 18 27 15 25 22 22 19 17
26 | 7 10 6 6 13 3 11 7 10 12 3 | 17 21 17 17 21 16 18 19 16 20 16
X27 | 6 --- --- --- --- 48 --- --- --- --- 0 | 38 --- --- --- --- 17 --- --- --- --- 39
28 | 11 14 6 7 18 4 15 8 7 11 4 | 17 22 18 17 32 15 20 15 21 14 15
29 | 9 17 10 9 16 4 19 11 10 22 4 | 19 26 27 22 29 18 23 19 28 19 21
X30 | 14 17 --- 16 20 27 --- 8 --- --- 7 | 60 61 --- 57 65 49 --- 55 --- --- 59
31 | 8 17 9 9 17 5 13 11 13 15 4 | 20 25 17 18 35 17 24 17 21 16 17
32E | 13 13 6 8 19 6 13 15 8 15 4 | 142 139 142 139 142 142 138 142 148 139 141
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 8 8 15 4 15 10 10 17 |T 26 30 26 26 33 24 29 26 28 25 26
WRMS | 10 14 8 8 12 4 15 10 9 16 |NE 21 25 22 20 28 18 25 20 23 20 20
MEDI | 9 14 7 8 15 4 13 10 9 16 |MD 19 24 19 18 27 17 23 19 21 20 18
Table 3.1736.4 GPS week: 1736 Day: 4 MJD: 56400.000
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 9 6 10 13 3 14 6 12 11 4 | 21 23 21 15 23 16 27 14 24 18 16
2 | 8 17 8 12 14 2 20 7 10 18 4 | 53 61 60 51 60 56 61 56 55 61 55
3 | 8 8 7 10 13 3 9 8 15 14 3 | 13 18 21 19 23 15 16 13 22 15 15
4 | 7 10 5 6 13 5 11 10 6 18 3 | 18 23 23 17 23 18 20 20 19 27 19
5E | 9 20 8 11 15 5 19 9 9 13 4 | 21 28 21 23 22 22 26 22 22 20 20
6 | 6 10 6 11 11 3 10 8 16 16 3 | 16 20 26 22 27 18 19 18 20 16 19
7 | 14 14 8 10 18 4 12 12 11 14 4 | 13 21 14 15 29 12 19 13 20 16 12
8 | 6 10 5 7 9 4 12 7 7 13 3 | 11 23 20 16 18 15 21 16 19 19 15
9 | 6 10 5 9 13 4 12 9 9 10 3 | 10 18 14 12 17 9 18 15 15 14 10
10E | 12 17 7 10 16 3 15 10 9 11 4 | 30 30 30 32 22 28 28 32 29 24 27
11 | 9 13 6 10 17 5 12 4 13 12 3 | 36 44 47 43 52 38 43 38 39 37 40
12 | 16 24 7 11 19 4 29 12 12 16 6 | 22 26 18 15 27 14 27 19 18 15 15
13 | 10 16 6 10 17 4 14 10 12 21 4 | 13 27 21 21 35 19 29 21 21 23 19
14 | 5 16 8 14 13 4 13 8 9 21 4 | 24 28 30 32 28 26 28 24 27 24 25
15 | 15 19 7 7 16 5 17 13 14 27 5 | 29 26 22 15 27 17 22 19 21 24 17
16 | 5 15 5 12 15 4 19 11 8 20 4 | 13 23 23 20 26 16 26 14 22 17 17
17 | 11 19 8 11 11 4 18 11 10 22 4 | 16 27 27 24 22 18 23 24 20 19 19
18E | 7 10 4 10 18 3 13 7 7 13 3 | 19 20 20 18 16 16 19 16 22 21 16
19 | 8 13 8 9 12 5 13 7 13 26 4 | 15 23 26 22 25 18 21 16 23 15 19
20E | 9 16 7 8 14 6 13 10 10 13 4 | 19 18 20 18 16 15 20 20 19 19 15
21 | 7 15 7 10 18 4 16 9 12 17 4 | 20 25 27 24 30 23 23 24 18 24 21
22E | 6 12 6 10 17 4 11 8 9 16 3 | 17 17 19 17 18 14 15 15 14 17 13
23 | 13 14 7 12 15 3 14 14 10 17 4 | 15 25 21 21 28 18 25 17 25 20 17
24 | 8 14 6 10 17 4 14 10 10 9 4 | 15 25 19 16 28 14 25 15 19 16 15
25 | 8 18 5 9 19 4 15 16 8 12 4 | 23 30 27 24 29 24 31 29 28 27 24
26 | 8 11 6 9 13 3 13 8 8 12 3 | 14 19 21 21 21 18 22 15 23 15 16
X27 | 5 --- --- --- --- 44 --- --- --- --- 0 | 44 --- --- --- --- 25 --- --- --- --- 45
28 | 8 13 6 7 16 4 13 7 12 10 3 | 12 22 17 15 28 12 20 15 22 13 13
29 | 10 19 7 10 20 4 23 7 8 22 4 | 18 27 25 23 27 19 25 18 21 19 20
X30E | 22 24 --- 42 29 31 --- 15 --- --- 13 | 40 38 --- 58 37 47 --- 39 --- --- 38
31 | 12 14 7 11 22 4 12 7 8 13 4 | 30 32 31 29 39 27 33 23 32 26 27
32E | 12 13 4 9 12 4 13 10 11 16 4 | 87 90 88 90 85 89 90 93 87 89 88
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 7 10 15 4 15 10 11 16 |T 23 28 26 25 29 23 27 23 25 23 23
WRMS | 10 15 7 10 15 4 15 9 8 18 |NE 20 26 25 22 28 20 26 20 23 21 21
MEDI | 8 14 6 10 15 4 13 9 10 14 |MD 18 25 21 21 27 18 23 19 22 19 19
Table 3.1736.5 GPS week: 1736 Day: 5 MJD: 56401.000
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 | 7 10 6 8 14 3 13 7 12 15 3 | 12 20 14 13 24 14 28 11 21 17 13
2 | 12 20 10 11 20 4 21 11 9 20 5 | 90 94 93 88 90 89 96 85 96 84 91
3 | 10 9 6 10 16 4 9 9 10 18 3 | 12 15 16 12 22 12 15 12 17 13 11
4 | 8 11 5 7 12 3 9 12 12 20 3 | 12 15 16 15 20 12 17 17 20 25 13
5E | 11 15 6 10 13 5 20 9 8 13 4 | 18 19 13 20 17 14 18 22 18 18 14
6 | 10 8 6 9 14 3 9 7 10 18 3 | 13 17 19 16 24 14 18 15 16 13 14
7 | 12 12 7 11 19 2 10 16 11 15 4 | 18 21 14 17 31 14 23 14 25 16 14
8 | 12 11 5 7 12 3 13 9 6 14 3 | 19 22 15 13 20 14 25 14 22 16 15
9 | 8 8 6 7 16 3 13 10 9 10 3 | 17 17 12 11 17 12 21 18 21 15 12
10E | 12 14 6 8 15 4 14 11 7 9 4 | 49 44 48 48 43 46 43 51 47 45 46
11 | 12 14 6 7 17 4 11 8 9 13 3 | 30 41 40 32 52 34 43 35 38 33 36
12 | 15 22 7 7 19 3 31 11 9 16 5 | 18 23 15 14 25 13 27 19 23 17 14
13 | 16 15 6 10 18 6 12 12 10 21 4 | 15 27 19 19 36 19 30 18 24 19 19
14 | 8 14 6 9 15 4 18 12 7 21 4 | 18 22 19 21 27 20 26 23 22 20 18
15 | 33 18 7 10 16 8 21 10 12 28 6 | 25 23 19 19 29 19 26 19 25 22 17
16 | 8 12 6 12 16 4 17 15 7 25 4 | 12 17 14 14 24 12 19 15 21 16 11
17 | 8 19 7 11 12 3 17 12 11 22 4 | 22 25 22 21 27 18 24 24 23 18 18
18E | 7 12 6 10 18 4 15 10 9 13 4 | 17 17 17 17 18 14 20 13 27 17 15
19 | 10 13 8 7 18 3 13 6 10 24 4 | 14 20 21 15 28 16 20 12 21 12 16
20E | 13 16 6 7 16 2 13 10 13 17 4 | 19 19 18 18 22 20 19 22 28 23 18
21 | 10 16 8 10 15 6 18 10 11 15 4 | 14 21 19 20 28 16 22 17 19 14 15
22E | 6 10 7 9 15 3 14 11 11 14 3 | 12 12 10 15 12 9 13 16 19 13 8
23 | 15 14 6 14 18 3 13 12 11 17 4 | 17 24 18 19 29 17 24 14 22 14 16
24 | 13 11 5 8 16 3 15 10 7 14 3 | 24 21 18 14 28 15 24 19 20 18 16
25 | 8 18 5 8 12 4 13 11 9 12 4 | 18 25 21 12 25 18 25 21 22 18 17
26 | 9 10 5 7 11 5 12 9 7 13 3 | 21 16 12 18 17 14 18 17 22 13 14
X27 | 7 --- --- --- --- 77 --- --- --- --- 0 | 78 --- --- --- --- 20 --- --- --- --- 78
28 | 9 12 5 8 18 3 14 7 10 11 3 | 22 22 17 16 32 17 25 18 27 15 17
29 | 16 17 7 9 16 4 19 7 10 25 4 | 23 21 19 16 24 15 20 14 19 19 15
X30E | 23 14 --- 18 31 28 --- 13 --- --- 9 | 38 44 --- 43 47 43 --- 32 --- --- 39
31 | 13 13 7 10 21 4 12 11 9 13 4 | 20 22 19 19 36 17 23 17 23 15 17
32E | 18 12 4 12 20 5 14 11 11 16 4 | 146 141 145 143 141 146 143 147 148 143 144
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 14 6 9 16 4 15 10 10 17 |T 27 28 25 25 32 24 29 25 29 24 25
WRMS | 13 14 6 9 15 4 15 10 9 17 |NE 23 24 21 19 29 19 26 20 25 20 21
MEDI | 10 13 6 9 16 4 13 10 10 15 |MD 18 21 18 17 27 16 23 18 22 17 16
Table 3.1736.6 GPS week: 1736 Day: 6 MJD: 56402.000
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 9 6 8 9 3 14 7 14 15 3 | 21 25 16 17 25 17 29 17 28 21 18
2 | 7 18 8 10 11 4 21 11 10 23 4 | 41 49 50 47 54 46 50 49 49 54 47
3 | 10 9 6 13 14 3 10 10 15 17 4 | 12 17 17 17 24 13 15 11 16 12 13
4 | 7 11 4 6 12 3 11 9 9 23 3 | 19 18 19 15 25 15 22 18 22 26 17
5E | 8 14 5 8 17 4 18 12 10 13 4 | 24 22 17 21 22 16 21 24 19 19 18
6 | 8 8 5 11 12 2 9 10 15 17 3 | 17 21 23 22 30 18 20 19 14 14 19
7 | 15 12 8 12 18 4 13 18 14 14 5 | 18 23 15 17 31 14 23 19 20 16 15
8 | 8 12 8 8 10 3 11 9 10 17 3 | 14 25 14 11 18 10 23 13 18 16 13
9 | 6 9 5 7 17 3 11 13 8 11 3 | 15 20 14 15 16 12 23 19 17 15 14
10E | 10 13 8 11 13 5 14 16 10 11 4 | 59 55 57 64 50 55 51 60 49 61 56
11 | 11 13 6 11 12 4 13 10 10 16 4 | 45 52 55 51 63 49 55 49 45 47 50
12 | 13 23 7 10 20 4 25 14 8 15 5 | 22 26 21 20 31 16 28 20 23 16 18
13 | 10 15 6 12 16 3 14 12 10 23 4 | 18 28 22 28 37 22 32 25 23 27 22
14 | 9 13 5 8 12 4 12 12 9 21 3 | 23 27 28 32 32 29 29 32 26 26 27
15 | 38 18 8 8 15 7 19 14 12 28 6 | 25 27 19 21 27 16 26 20 21 27 18
16 | 8 16 5 11 14 3 14 14 8 21 4 | 12 18 15 16 25 11 18 11 17 12 13
17 | 12 21 8 11 10 6 17 11 13 23 4 | 30 27 32 29 31 26 27 32 28 25 26
18E | 7 11 4 8 25 5 12 9 9 17 4 | 18 20 18 20 23 17 18 20 20 20 17
19 | 7 12 8 13 13 4 15 7 12 26 4 | 12 20 22 21 22 16 21 13 16 13 16
20E | 12 13 7 9 15 5 15 12 12 19 4 | 20 16 16 17 20 16 17 18 23 23 15
21 | 8 14 6 11 15 4 17 8 9 16 4 | 23 26 25 28 37 25 26 25 23 21 23
22E | 5 12 6 8 12 5 11 16 11 19 3 | 18 17 13 15 15 13 17 20 19 20 12
23 | 12 14 7 15 16 5 13 12 10 18 4 | 17 26 20 26 29 19 26 20 23 23 19
24 | 12 13 4 8 15 3 13 16 9 12 4 | 20 29 20 20 29 18 28 20 22 20 20
25 | 9 20 5 7 12 4 10 11 8 12 4 | 21 30 23 16 28 17 27 15 22 19 20
26 | 7 11 4 6 9 3 10 12 11 13 3 | 20 23 19 22 22 20 22 26 25 22 20
X27 | 6 --- --- --- --- 59 --- --- --- --- 0 | 46 --- --- --- --- 18 --- --- --- --- 45
28 | 7 11 6 9 19 4 15 9 9 12 4 | 16 21 19 18 34 14 23 16 20 13 16
29 | 10 17 7 10 13 4 20 11 8 29 4 | 22 26 25 24 30 19 23 23 24 29 21
X30E | 19 26 --- --- 25 34 --- 25 --- --- 13 | 75 61 --- --- 68 57 --- 84 --- --- 69
31 | 10 11 6 8 19 3 13 8 12 14 4 | 18 23 18 19 35 15 22 15 23 15 18
32E | 17 14 5 11 12 5 13 12 9 21 4 | 167 164 163 166 163 162 159 166 160 161 164
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 6 10 15 4 15 12 11 18 |T 29 31 27 28 35 25 30 29 28 27 28
WRMS | 12 14 6 9 13 4 14 12 10 17 |NE 21 26 22 23 30 19 26 21 23 22 21
MEDI | 9 13 6 9 14 4 13 12 10 17 |MD 20 25 19 20 29 17 23 20 22 20 18
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 4.1736 GPS week: 1736 MJD: 56396.0-56402.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 |U 6 6 14 |U 6 9 23 |U 6 6 16 |
emr | emr 2967 | 8 8 18 |U 11 18 34 | 8 7 18 |
esa | esa 2907 | 6 7 18 |U 6 8 23 | 6 6 17 |
gfz | gfz 2941 |U 6 7 18 |U 7 9 24 |U 6 6 16 |
grg | grg 2976 |U 9 13 27 |U 13 18 39 | 9 9 21 |
igr | igr 2934 | 7 7 18 | 6 9 22 | 5 5 16 |
igs | igs 2974 | 6 7 16 | 10 21 41 | 6 5 16 |
jpl | jpl 2899 | 9 9 21 |U 10 19 33 |U 7 7 19 |
mit | mit 2976 | 8 8 27 |U 31 45 95 |U 7 6 18 |
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 5.1736.0 GPS week: 1736 Day: 0 MJD: 56396.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 7 7 14 | 6 5 22 | 6 5 16 |
emr | emr 2970 | 9 10 20 | 11 14 24 | 8 6 16 |
esa | esa 2976 | 6 7 16 | 5 4 18 | 5 6 17 |
gfz | gfz 2968 | 6 6 16 | 5 5 18 | 6 5 15 |
grg | grg 2976 | 10 12 25 | 11 17 38 | 9 9 22 |
igr | igr 2974 | 6 7 16 | 4 5 18 | 6 5 15 |
igs | igs 2975 | 6 8 17 | 7 14 21 | 6 6 15 |
jpl | jpl 2970 | 8 10 20 | 7 13 25 | 8 7 20 |
mit | mit 2976 | 6 9 15 | 8 18 30 | 6 6 18 |
Table 5.1736.1 GPS week: 1736 Day: 1 MJD: 56397.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 | 9 9 16 | 9 7 26 | 6 6 14 |
emr | emr 2968 | 10 9 18 | 14 14 39 | 9 8 18 |
esa | esa 2880 | 9 10 24 | 9 7 32 | 6 6 15 |
gfz | gfz 2941 | 9 11 24 | 9 7 26 | 6 7 17 |
grg | grg 2976 | 13 21 36 | 14 15 29 | 9 12 20 |
igr | igr 2948 | 9 10 23 | 8 7 28 | 5 5 15 |
igs | igs 2972 | 7 8 17 | 12 22 42 | 7 6 16 |
jpl | jpl 2872 | 8 11 24 | 11 16 33 | 7 6 18 |
mit | mit 2976 | 6 9 16 | 12 24 45 | ---- ---- ---- |
Table 5.1736.2 GPS week: 1736 Day: 2 MJD: 56398.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | 6 6 12 | 7 9 25 | 6 5 19 |
emr | emr 2968 | 8 8 18 | 12 23 42 | 8 6 16 |
esa | esa 2976 | 6 6 15 | 7 10 25 | 5 6 18 |
gfz | gfz 2969 | 5 6 16 | 6 9 22 | 5 5 15 |
grg | grg 2976 | 9 12 24 | 13 23 52 | 9 9 20 |
igr | igr 2976 | 6 7 15 | 6 9 23 | 5 5 19 |
igs | igs 2974 | 5 6 17 | 11 24 53 | 6 4 15 |
jpl | jpl 2968 | 7 7 16 | 9 22 30 | 7 7 22 |
mit | mit 2976 | 5 6 14 | 11 24 62 | 6 4 18 |
Table 5.1736.3 GPS week: 1736 Day: 3 MJD: 56399.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 6 6 16 | 5 8 18 | 5 5 12 |
emr | emr 2968 | 8 9 19 | 11 17 36 | 7 5 17 |
esa | esa 2880 | 8 7 16 | 6 8 22 | 5 5 13 |
gfz | gfz 2957 | 8 7 16 | 5 8 21 | 5 4 12 |
grg | grg 2976 | 7 10 20 | 11 15 38 | 8 10 20 |
igr | igr 2939 | 8 7 16 | 5 8 19 | 5 4 12 |
igs | igs 2975 | 6 7 15 | 9 19 57 | 5 4 12 |
jpl | jpl 2872 | 15 11 22 | 8 18 22 | 6 5 16 |
mit | mit 2976 | 8 7 51 | 9 18 52 | 7 4 19 |
Table 5.1736.4 GPS week: 1736 Day: 4 MJD: 56400.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3023 | 8 6 17 | 6 13 27 | 6 6 15 |
emr | emr 2967 | 9 8 22 | 14 23 41 | 7 6 16 |
esa | esa 2880 | 6 7 24 | 6 7 26 | 5 6 15 |
gfz | gfz 2931 | 7 6 21 | 6 9 26 | 6 6 15 |
grg | grg 2976 | 10 14 37 | 13 16 45 | 10 12 21 |
igr | igr 2909 | 7 7 24 | 6 9 25 | 5 4 15 |
igs | igs 2975 | 7 6 22 | 12 24 46 | 6 5 14 |
jpl | jpl 2872 | 11 9 29 | 19 33 66 | 7 6 18 |
mit | mit 2976 | ---- ---- ---- | 154 185 395 | 7 9 19 |
Table 5.1736.5 GPS week: 1736 Day: 5 MJD: 56401.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3008 | 3 4 10 | 7 17 25 | 7 7 16 |
emr | emr 2968 | 5 5 13 | 8 23 27 | 9 9 21 |
esa | esa 2880 | 4 5 15 | 7 16 22 | 6 8 18 |
gfz | gfz 2953 | 4 5 15 | 9 16 31 | 6 8 16 |
grg | grg 2976 | 8 12 28 | 15 22 41 | 11 10 22 |
igr | igr 2920 | 4 6 14 | 7 16 23 | 7 9 18 |
igs | igs 2976 | 4 5 13 | 9 26 34 | 6 7 16 |
jpl | jpl 2871 | 5 5 17 | 7 18 25 | 8 8 21 |
mit | mit 2976 | 16 8 39 | 13 28 41 | 7 7 16 |
Table 5.1736.6 GPS week: 1736 Day: 6 MJD: 56402.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3032 | 6 7 13 | 4 6 19 | 6 6 22 |
emr | emr 2964 | 7 8 16 | 9 12 29 | 7 7 22 |
esa | esa 2880 | 6 8 19 | 5 6 19 | 6 7 22 |
gfz | gfz 2872 | 7 8 19 | 5 10 22 | 6 6 22 |
grg | grg 2976 | 8 8 18 | 11 15 34 | 8 4 25 |
igr | igr 2878 | 7 8 20 | 5 6 20 | 6 7 20 |
igs | igs 2975 | 6 7 16 | 10 20 38 | 6 5 21 |
jpl | jpl 2872 | 7 9 20 | 8 17 28 | 8 9 22 |
mit | mit 2976 | ---- ---- ---- | 11 18 42 | ---- ---- ---- |
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 6.1736 GPS week: 1736 MJD: 56396.500-56402.500
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 | 35 -9 116 76 -3 | 12 21
| 16 14 89 67 5 | 1
emr uuuuu | 7 34 110 7 -2 | 22 26
| 14 11 58 47 10 | 1
esa uuuuu | -8 -4 -37 7 -2 | 24 30
| 7 5 64 53 2 | 1
gfz uuuuu | 43 16 107 -89 1 | 14 16
| 12 8 51 41 3 | 1
grg uuuux | 10 -5 58 -64 12 | -19 34
| 14 20 63 38 11 | 3
igr xxxxx | -46 -3 8 -50 1 | 1 10
| 10 15 53 31 3 | 1
irf xxxxx | 6 -8 -20 6 0 | 5 10
| 6 7 27 21 2 | 1
jpl uuuuu | -8 13 -60 -4 9 | 33 36
| 22 11 96 62 5 | 5
mit uuuuu | 8 -15 -154 78 3 | 18 19
| 19 16 83 46 3 | 2
ngs uuuuu | -75 -15 -68 -23 -2 | 12 15
| 22 26 124 91 5 | 1
sio xxxxx | 380 212 -332 78 11 | 57 58
| 85 62 85 76 3 | 4
Table 7.1736.0 GPS week: 1736 Day: 0 MJD: 56396.500
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 | 41 -38 78 17 -6 | 11 21
emr uuuuu | -6 23 136 7 -21 | 24 27
esa uuuuu | -6 -12 -57 25 -1 | 22 29
gfz uuuuu | 26 27 122 -83 -2 | 13 16
grg uuuux | 6 17 -27 -119 21 | -20 36
igr xxxxx | -57 -5 10 -90 -4 | 0 10
irf xxxxx | 2 -12 -18 -10 2 | 3 10
jpl uuuuu | -12 28 -194 -60 13 | 28 31
mit uuuuu | 10 -18 -128 60 8 | 14 17
ngs uuuuu | -61 1 71 87 2 | 10 13
sio xxxxx | 413 225 -341 103 13 | 51 51
Table 7.1736.1 GPS week: 1736 Day: 1 MJD: 56397.500
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 | 59 -2 251 81 -6 | 10 21
emr uuuuu | 9 35 115 0 5 | 22 27
esa uuuuu | -5 4 -174 52 -5 | 23 29
gfz uuuuu | 67 18 61 -94 -4 | 13 16
grg uuuux | -3 10 29 -94 -1 | -16 33
igr xxxxx | -33 3 -41 -67 4 | 0 10
irf xxxxx | 14 -7 -33 13 -4 | 4 9
jpl uuuuu | 6 11 -51 -49 11 | 29 33
mit uuuuu | 12 -5 -136 97 -1 | 16 18
ngs uuuuu | -116 -53 52 -48 3 | 11 14
sio xxxxx | 438 278 -311 105 11 | 53 53
Table 7.1736.2 GPS week: 1736 Day: 2 MJD: 56398.500
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 | 41 -7 61 119 5 | 10 22
emr uuuuu | -13 26 176 39 1 | 22 26
esa uuuuu | -14 -5 -5 -58 2 | 24 30
gfz uuuuu | 43 14 89 -63 1 | 14 17
grg uuuux | 0 -8 113 -20 21 | -16 33
igr xxxxx | -54 -5 76 -49 0 | 1 11
irf xxxxx | 11 -3 -18 18 0 | 5 10
jpl uuuuu | 1 -5 -78 43 15 | 31 35
mit uuuuu | 37 -12 -181 104 4 | 18 20
ngs uuuuu | -86 6 -120 -113 -11 | 13 16
sio xxxxx | 424 258 -294 161 14 | 55 56
Table 7.1736.3 GPS week: 1736 Day: 3 MJD: 56399.500
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 | 8 -15 145 124 -4 | 11 22
emr uuuuu | 26 44 43 73 8 | 21 26
esa uuuuu | -9 -6 -12 21 -3 | 24 30
gfz uuuuu | 42 14 108 -135 2 | 13 16
grg uuuux | -2 -24 86 -50 19 | -17 33
igr xxxxx | -38 -20 61 -34 -2 | 1 11
irf xxxxx | 7 -3 -48 43 -2 | 5 10
jpl uuuuu | -8 5 -3 -73 2 | 33 37
mit uuuuu | 26 -15 -272 149 2 | 18 20
ngs uuuuu | -77 0 -46 -108 -4 | 12 16
sio xxxxx | 485 186 -500 161 13 | 57 58
Table 7.1736.4 GPS week: 1736 Day: 4 MJD: 56400.500
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 | 37 3 29 67 2 | 13 21
emr uuuuu | -1 39 177 32 -3 | 23 26
esa uuuuu | -11 0 -9 65 -4 | 25 31
gfz uuuuu | 44 24 186 -141 0 | 14 16
grg uuuux | 21 -40 154 -64 -4 | -18 33
igr xxxxx | -39 -12 43 -13 0 | 2 10
irf xxxxx | 1 -2 -33 -10 0 | 6 9
jpl uuuuu | -34 13 112 6 10 | 36 38
mit uuuuu | -3 6 -215 7 4 | 20 20
ngs uuuuu | -47 -47 -212 -60 -3 | 13 16
sio xxxxx | 359 269 -364 22 10 | 60 60
Table 7.1736.5 GPS week: 1736 Day: 5 MJD: 56401.500
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 | 30 -10 212 157 -8 | 13 21
emr uuuuu | 22 48 37 -38 -6 | 22 25
esa uuuuu | 6 -2 -17 -75 0 | 25 30
gfz uuuuu | 34 2 149 -21 5 | 14 16
grg uuuux | 35 4 46 -86 8 | -22 34
igr xxxxx | -45 27 -47 -14 5 | 1 10
irf xxxxx | 11 -5 36 4 -2 | 5 9
jpl uuuuu | -33 13 -125 102 11 | 37 39
mit uuuuu | -11 -13 -8 87 -1 | 19 20
ngs uuuuu | -62 -22 -234 -36 1 | 11 15
sio xxxxx | 299 149 -240 39 6 | 60 61
Table 7.1736.6 GPS week: 1736 Day: 6 MJD: 56402.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 29 2 34 -36 -5 | 13 21
emr uuuuu | 11 19 85 -66 0 | 21 24
esa uuuuu | -13 -6 15 16 -2 | 26 31
gfz uuuuu | 44 12 36 -86 3 | 15 17
grg uuuux | 17 6 6 -18 22 | -23 34
igr xxxxx | -57 -8 -44 -83 0 | 1 10
irf xxxxx | -1 -22 -29 -15 2 | 5 9
jpl uuuuu | 28 24 -81 0 3 | 40 42
mit uuuuu | -11 -47 -137 40 5 | 20 21
ngs uuuuu | -75 8 14 120 -3 | 11 15
sio xxxxx | 244 119 -275 -45 11 | 62 62
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