[IGSREPORT-24308] Wk 1886 IGS Final Orbits
IGS ACC
acc at igs.org
Thu Mar 17 15:52:04 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1886 (Feb 28, 2016 - Mar 05, 2016)
Contacts: acc at igs.org
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:
igs1886[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1886[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1886[0-6].cls IGS GPS clock combination summary report.
igs18867.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18867.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 | 32 POTS
0 | EMR | YELL
0 | ESA | KELY MAL2 KELY MAL2
0 | GFZ | ALGO POHN TONG ALGO TONG
0 | GRG | 10 10 DRAG
1 | ALL | 13 13
1 | COD | 32
1 | GFZ | ALGO NYA1 TONG ALGO
1 | GRG | 10 10 ALRT CAS1 RABT ALRT CAS1 RABT XMIS
1 | MIT | NYA1
2 | COD | ARTU
2 | ESA | ARTU SYOG
2 | GFZ | ALGO ARTU NICO POHN SYOG TONG ALGO NRMD POHN PRDS
2 | GRG | 10 10 NICO POTS SYOG MAL2 NICO POTS SYOG
2 | JPL | THTI
3 | COD | SYOG HARB TLSE
3 | EMR | 26 13 26 SYOG
3 | ESA | TWTF POTS QAQ1 TWTF UFPR
3 | GFZ | ALGO HARB KARR POTS SYOG ALGO
3 | GRG | 10 10 KARR KARR
3 | JPL | TIXI
3 | MIT | 31 31
4 | COD | KARR KARR
4 | EMR | TWTF TWTF
4 | ESA | TWTF TWTF
4 | GFZ | ALGO BOGT MAL2 ONSA STHL TONG ALGO NICO ONSA TONG
4 | GRG | 10 10 ARTU KARR REUN TLSE ARTU KARR REUN TLSE
4 | MIT | NICO XMIS NICO XMIS
5 | COD | 32 32 NICO
5 | ESA | SCOR SCOR
5 | GFZ | ALGO KOUR NANO POHN TONG ALGO KOUR REUN TONG
5 | GRG | 10 10 MAL2 MAL2
5 | MIT | NICO
6 | COD | 32 32 POTS
6 | GFZ | ALGO MAL2 NRIL POHN TONG ALGO HOB2 MAL2 POHN
6 | GRG | 10 10 XMIS XMIS
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
----+------------+----------
G15 | 2016_03_04 | 2016020
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | COD | 13
0 | GFZ | 13
0 | GRG | 13
0 | MIT | 13
1 | COD | 13
2 | COD | 32
2 | GRG | 10
2 | NGS | 32
3 | GRG | 10
5 | GRG | 10
6 | GRG | 10
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G10 | | | | | | | 4 |
PRN G13 | 4 | 4 | 4 | | | | |
PRN G32 | | | 4 | 4 | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These 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 -2.1 -1.8 -62 -11 -16 .71
EMR | 0 | 3.8 -1.9 8.2 5 -16 -5 .87
ESA | 0 | .4 -1.7 -.4 -19 -27 8 .41
GFZ | 0 | 1.0 -1.2 -.6 -59 -109 -18 .83
GRG | 0 | 7.8 3.9 -19.0 23 -53 64 .65
JPL | 0 | -3.7 4.4 6.2 16 25 36 .31
MIT | 0 | 5.8 1.5 14.3 16 -8 -35 .93
NGS | 0 | 3.5 -.6 5.9 -8 -26 23 .84
SIO | 0 | 8.0 1.4 5.8 1 -47 13 .27
COD | 1 | -2.1 -1.9 -2.3 -72 0 -26 .74
EMR | 1 | 4.4 -3.6 6.8 9 -17 -13 .88
ESA | 1 | -.2 -1.1 -.7 -26 -35 36 .46
GFZ | 1 | .8 -.7 -1.3 -57 -119 -41 .90
GRG | 1 | 13.9 2.8 -28.8 36 -37 68 .50
JPL | 1 | 1.1 1.9 5.1 -5 19 27 .46
MIT | 1 | 6.6 -.3 5.4 22 -15 -33 1.06
NGS | 1 | 9.2 -1.2 8.1 -6 -76 76 .88
SIO | 1 | 8.0 .4 -5.6 -5 -35 22 .58
COD | 2 | -1.7 -2.0 -.9 -59 -25 -5 .58
EMR | 2 | 4.6 -5.3 17.0 -6 7 -33 .79
ESA | 2 | -.2 -1.8 -.0 -51 -43 25 .46
GFZ | 2 | .3 -.8 -1.9 -43 -103 -24 .82
GRG | 2 | 12.8 -.2 -18.6 -7 -60 55 .73
JPL | 2 | -.9 -2.1 8.5 1 61 -8 .83
MIT | 2 | 6.7 -2.6 14.4 1 -7 -41 .97
NGS | 2 | 4.1 -2.8 9.9 -62 -33 23 .87
SIO | 2 | 6.6 -5.3 .4 -44 -19 17 .45
COD | 3 | -1.4 -1.2 -1.3 -26 -27 -2 .91
EMR | 3 | 4.1 -6.3 10.5 -2 -25 -9 .85
ESA | 3 | .3 -2.9 -.6 -25 -45 8 .43
GFZ | 3 | .6 -1.4 -.5 -56 -99 -38 .74
GRG | 3 | 6.2 -5.6 -21.0 10 -43 70 .77
JPL | 3 | 1.4 -4.9 2.3 -47 10 11 .99
MIT | 3 | .9 -4.4 11.2 25 -8 -35 .86
NGS | 3 | 3.6 -4.5 13.3 -89 -46 -5 .98
SIO | 3 | 3.4 -.3 -4.5 -27 -6 23 .46
COD | 4 | -.9 -.7 -.7 -39 5 -3 .94
EMR | 4 | 6.0 2.4 9.1 -14 -21 -1 .76
ESA | 4 | -1.1 -1.8 -.2 -4 -29 19 .61
GFZ | 4 | 1.2 -2.1 -.7 -70 -110 -24 .69
GRG | 4 | 6.2 -.3 -11.9 25 -63 68 1.06
JPL | 4 | .5 1.9 5.2 -71 3 62 .83
MIT | 4 | -1.4 -1.8 15.1 9 20 -45 .94
NGS | 4 | .2 1.9 7.5 -27 -14 -7 .80
SIO | 4 | -2.6 -2.8 -3.7 -36 -30 12 .47
COD | 5 | .1 -1.9 -1.2 -51 -34 -2 .68
EMR | 5 | 5.4 2.8 5.8 -1 -11 -1 .74
ESA | 5 | -.7 -2.1 -1.0 -38 -27 22 .49
GFZ | 5 | 1.9 -1.9 -1.3 -79 -129 -57 .77
GRG | 5 | 6.1 -.0 .8 17 -72 56 1.16
JPL | 5 | -2.2 .3 5.4 -40 27 54 .88
MIT | 5 | -.7 -2.7 14.1 -7 2 -53 .77
NGS | 5 | -.0 -2.2 18.2 -91 -31 -52 .68
SIO | 5 | 1.2 .6 -2.3 -19 -26 11 .45
COD | 6 | -.3 -1.5 -.8 -61 -35 -4 .66
EMR | 6 | 2.1 -1.9 6.4 -1 -21 -3 .84
ESA | 6 | -.5 -2.1 -.2 -13 -34 30 .46
GFZ | 6 | 1.4 -1.6 -1.8 -60 -103 -63 .84
GRG | 6 | 5.8 -4.0 -14.9 2 -80 70 1.19
JPL | 6 | -8.0 1.9 2.0 15 37 69 .47
MIT | 6 | 3.4 -4.4 7.5 -11 2 -62 .86
NGS | 6 | 3.9 -7.1 8.4 -64 -26 5 .69
SIO | 6 | -2.8 .7 -7.8 -24 -15 -19 .69
11. 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.
12. 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 1.1886.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1886.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 2.1886.[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 3.1886.[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 5.1886.0-6). 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 1886 summary. (Feb 28, 2016 - Mar 05, 2016)
Table 1.1886.a GPS week: 1886 MJD: 57446.000-57452.000
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 245| 0 0 0 9 -6 0 .02 12 11 | -959 14 15 143
| 0 0 1 20 22 14 .06 | 162 292
emr 80| 0 0 2 -7 -7 -18 .19 11 11 | 3757 262 14 152
| 0 1 1 15 13 14 .02 | 338 507
esa 150| 0 0 -1 -25 -22 34 -.32 12 12 | -102 144 9 163
| 0 0 1 16 6 8 .02 | 514 936
gfz 205| 0 0 -1 5 -13 7 .05 11 10 | -451 81 11 147
| 0 0 1 11 7 14 .03 | 254 324
grg 125| 0 2 -8 0 40 24 .13 17 16 | -185 79 14 221
| 1 1 3 13 34 14 .05 | 215 305
igr n/a| 0 0 -3 6 6 4 .00 4 4 | -1408 -74 14 87
| 0 0 0 26 14 14 .01 | 1174 672
jpl 80| -1 0 3 34 31 17 .28 10 10 | 1559 296 14 136
| 1 1 1 26 18 34 .02 | 441 527
mit 349| 0 -1 1 -6 -2 -33 -.24 11 10 | -36 10 41 426
| 0 0 1 19 26 18 .02 | 397 353
ngs 226| 0 0 0 -23 -2 -8 -.06 9 8 | -943 45 1018 2250
| 0 0 3 24 21 22 .03 | 234 275
sio 305| 0 0 -1 4 -12 1 -.13 13 12 | --- --- --- ---
| 0 0 4 25 36 31 .05 | --- ---
Table 1.1886.b GPS week : 1886 MJD: 57446.000-57452.000
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 | 3 4 4 4 3 4 4 |
2 | 5 4 4 5 5 4 4 |
3 | 4 4 4 4 4 4 4 |
4 | 0 0 0 0 0 0 0 |
5 | 4 4 4 4 4 5 4 |
6 | 3 4 4 4 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 4 3 4 3 3 |
9 | 4 4 4 4 4 3 4 |
10 | 8 9 7 7 9 6 6 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 0 0 4 5 5 4 4 |
14 | 4 5 5 4 4 4 5 |
15 | 4 4 5 5 5 0 5 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 5 4 4 4 5 |
19 | 5 4 4 5 5 5 5 |
20 | 3 4 4 4 4 4 4 |
21 | 4 4 4 4 4 4 5 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 4 4 4 3 4 |
25 | 3 4 4 4 4 4 4 |
26 | 4 4 4 4 5 4 4 |
27 | 3 3 4 3 3 3 3 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 3 3 |
31 | 5 4 5 4 4 4 5 |
32 | 8 10 19 0 12 9 10 |
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 2.1886.0 GPS week: 1886 Day: 0 MJD: 57446.000
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 247| 0 0 -1 -9 -9 -11 .08 12 11 | -946 240 14 132
emr 80| 0 0 3 -37 -13 -6 .18 11 11 | 3598 282 14 144
esa 150| 0 0 0 -35 -20 20 -.31 11 11 | 19 -14 8 166
gfz 206| 0 0 0 3 -16 26 .05 10 10 | -163 -48 10 112
grg 127| 0 3 -8 4 44 15 .05 21 20 | -25 12 15 233
igr n/a| 0 0 -3 5 12 -2 .02 4 4 | -192 257 14 116
jpl 80| -1 0 5 71 24 14 .24 9 9 | 1206 814 15 156
mit 350| 1 -1 2 -20 -25 -9 -.21 11 10 | -182 462 39 414
ngs 229| 0 0 -5 -18 30 -19 -.07 9 8 | -657 -79 1119 2052
sio 305| 0 1 -2 29 -18 -15 -.10 13 13 | --- --- --- ---
Table 2.1886.1 GPS week: 1886 Day: 1 MJD: 57447.000
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 245| -1 0 0 15 -8 -1 .01 13 12 | -827 -282 15 136
emr 80| 1 0 1 -12 -10 -41 .21 11 11 | 3642 521 15 138
esa 150| 0 1 -2 -28 -17 37 -.29 12 12 | -650 1103 9 145
gfz 204| 0 -1 0 15 -9 5 .05 10 10 | -664 484 11 115
grg 127| 3 3 -14 -10 83 27 .10 18 16 | -22 -200 16 232
igr n/a| 0 0 -2 2 30 -9 -.00 4 4 | -240 -24 15 77
jpl 80| 0 0 3 56 20 7 .27 9 9 | 1784 465 14 143
mit 350| 1 -2 0 -24 14 -12 -.21 11 10 | 398 -490 39 317
ngs 224| 0 0 5 -6 -33 -7 -.07 9 8 | -1035 54 803 2183
sio 305| -1 2 -6 -30 12 14 -.14 13 13 | --- --- --- ---
Table 2.1886.2 GPS week: 1886 Day: 2 MJD: 57448.000
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 246| 0 0 -1 0 -21 14 .10 13 12 | -1131 362 17 161
emr 80| 1 -2 3 6 -4 -31 .22 13 13 | 3943 642 15 146
esa 150| 0 0 -1 -32 -32 34 -.32 12 12 | -823 926 9 142
gfz 207| 0 0 0 22 -7 7 .10 10 9 | -388 132 12 137
grg 125| 1 2 -10 6 76 34 .16 18 16 | -612 677 15 246
igr n/a| 0 0 -3 13 0 8 .01 5 5 | -384 -272 15 89
jpl 80| -2 2 5 34 32 -21 .29 11 11 | 2233 265 15 144
mit 350| 1 -1 1 4 -17 -48 -.22 11 10 | 599 227 53 375
ngs 227| 0 0 0 -48 11 20 -.09 9 8 | -1262 466 969 2432
sio 302| 0 0 -7 -1 -24 35 -.22 13 13 | --- --- --- ---
Table 2.1886.3 GPS week: 1886 Day: 3 MJD: 57449.000
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 246| 0 1 -1 43 -9 15 .02 12 11 | -1213 340 12 126
emr 80| 1 -1 2 1 -3 -6 .18 11 11 | 4067 -357 17 150
esa 150| 0 0 -1 -41 -28 30 -.35 12 12 | 96 -354 9 147
gfz 209| 1 0 -1 -14 -8 19 .03 10 9 | -603 92 10 104
grg 123| 0 0 -9 -7 36 28 .18 17 16 | -66 -243 13 190
igr n/a| 0 0 -3 -30 10 26 -.02 4 4 | -1536 -1000 14 65
jpl 80| -1 0 2 7 0 -12 .27 11 11 | 1495 -261 14 129
mit 350| 0 -2 0 31 13 -40 -.24 12 10 | -366 -440 36 369
ngs 226| 0 0 2 -37 4 -26 -.06 10 9 | -1214 353 1029 2072
sio 309| -1 0 -3 16 5 20 -.13 13 12 | --- --- --- ---
Table 2.1886.4 GPS week: 1886 Day: 4 MJD: 57450.000
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 246| 0 0 -1 -6 42 5 .03 11 10 | -887 -306 19 181
emr 80| 0 0 4 -2 17 -25 .18 11 11 | 3927 -526 14 141
esa 150| 0 0 -1 9 -18 42 -.32 11 11 | 391 26 10 174
gfz 206| 0 -1 -2 0 -10 15 .03 12 11 | -56 -541 16 225
grg 126| 0 2 -8 26 -9 23 .11 16 16 | -118 102 12 206
igr n/a| 0 0 -4 -19 9 22 .00 4 4 | -1957 -821 15 91
jpl 80| 1 0 3 0 54 4 .29 10 10 | 1677 -569 15 122
mit 350| 0 0 4 -8 -40 -27 -.26 11 10 | -495 218 39 375
ngs 229| 0 0 -2 2 7 -9 -.09 10 9 | -826 -325 1105 2207
sio 311| 0 0 1 -21 -87 -23 -.07 15 13 | --- --- --- ---
Table 2.1886.5 GPS week: 1886 Day: 5 MJD: 57451.000
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 246| -1 -1 -1 30 -27 -25 -.01 13 11 | -756 -170 14 136
emr 80| 0 2 0 -10 -27 -11 .16 10 10 | 3108 785 13 183
esa 150| 0 0 -5 -31 -23 46 -.33 11 10 | -302 884 9 162
gfz 204| 1 0 -2 5 -12 -14 .03 11 10 | -616 126 10 158
grg 123| 1 2 -2 -10 47 -2 .10 16 15 | -330 191 13 229
igr n/a| 0 0 -3 37 -18 -5 .01 4 4 | -3179 803 15 109
jpl 80| -1 0 3 19 35 55 .28 9 9 | 845 779 14 134
mit 350| 0 -1 1 -15 32 -36 -.26 11 10 | -167 60 45 556
ngs 225| 0 0 2 -1 -15 -38 -.04 10 8 | -730 -75 969 2132
sio 300| 0 0 0 0 0 26 -.13 13 11 | --- --- --- ---
Table 2.1886.6 GPS week: 1886 Day: 6 MJD: 57452.000
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 242| 0 0 2 -7 -8 1 -.07 12 10 | -957 -86 17 133
emr 80| 0 0 0 5 -11 -8 .20 11 11 | 4015 492 14 164
esa 150| 0 0 0 -19 -14 31 -.34 11 11 | 555 -1557 11 205
gfz 205| 0 -1 -4 5 -29 -5 .05 11 11 | -673 326 13 181
grg 126| 0 0 -8 -10 5 42 .17 16 15 | -126 16 15 211
igr n/a| 0 0 -1 39 5 -5 .01 5 5 | -2372 539 14 65
jpl 80| -1 1 3 50 48 72 .31 11 11 | 1675 579 16 130
mit 349| 1 -1 0 -10 6 -61 -.25 11 11 | -45 33 41 579
ngs 227| 0 0 0 -58 -19 21 .01 10 9 | -879 -78 1136 2673
sio 307| 0 0 5 39 23 -50 -.10 12 11 | --- --- --- ---
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 3.1886.0 GPS week: 1886 Day: 0 MJD: 57446.000
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 12 7 15 5 8 4 8 13 3 | 34 33 33 30 29 31 34 29 31 37 31
2 | 13 12 9 17 19 4 10 12 10 15 4 | 33 32 28 38 30 30 35 31 29 30 30
3 | 11 9 12 9 19 5 10 12 10 14 4 | 39 38 36 36 32 35 38 36 36 33 35
X4E | 1 --- --- --- --- 37 --- --- --- --- 0 | 45 --- --- --- --- 54 --- --- --- --- 43
5 | 8 13 7 9 26 5 12 13 10 11 4 | 34 35 32 34 33 31 33 30 33 32 31
6 | 7 11 12 7 15 3 8 8 7 9 3 | 37 35 34 33 32 33 36 32 33 34 33
7 | 8 11 13 11 21 5 9 17 8 14 4 | 50 47 44 49 47 46 46 47 42 46 45
8 | 11 6 12 8 21 5 7 9 7 9 3 | 37 36 34 34 34 32 35 33 33 35 33
9 | 9 9 14 7 16 5 6 9 9 11 3 | 81 76 78 76 79 77 76 73 73 75 76
X10 | 16 17 9 --- 57 10 8 26 15 --- 8 | 63 71 66 --- 57 64 68 82 64 --- 67
11 | 8 11 17 7 23 6 8 7 9 10 3 | 49 51 44 47 53 45 48 46 49 49 47
12E | 17 14 7 15 26 4 13 12 10 14 5 | 41 36 31 33 34 32 36 31 29 35 32
X13 | 203 --- --- 233 136 308 --- 130 4 --- 0 | 9999 --- --- 470 155 428 --- 249 225 --- 367
14 | 11 10 12 13 21 4 9 11 9 16 4 | 39 39 37 38 45 38 38 43 37 44 38
15 | 8 13 11 12 17 4 13 10 10 14 4 | 30 33 32 28 22 27 27 24 26 21 28
16 | 27 11 8 15 22 7 9 13 10 16 5 | 99 94 97 91 91 92 92 94 93 96 93
17 | 12 12 13 11 14 6 9 13 10 15 4 | 40 38 34 39 35 34 40 39 34 35 36
18 | 11 11 8 12 25 5 9 11 7 11 4 | 37 38 33 37 45 34 37 38 35 35 36
X19 | 11 12 11 13 15 8 10 16 11 --- 4 | 38 40 35 41 36 34 43 41 36 --- 37
20 | 8 8 9 7 20 4 9 9 8 8 3 | 53 52 53 52 53 50 52 50 50 50 51
21 | 11 11 7 9 24 2 9 11 8 12 3 | 32 32 30 34 30 30 32 30 30 30 30
22 | 16 10 8 6 29 4 8 10 10 15 4 | 31 30 26 26 31 27 29 28 30 25 27
23 | 12 10 12 10 24 4 9 18 13 18 4 | 45 43 42 42 42 41 44 37 39 38 40
24 | 13 9 14 6 24 4 10 11 5 12 4 | 32 29 29 30 36 28 30 31 28 31 28
25E | 11 7 11 8 14 4 9 8 7 11 3 | 38 36 36 36 34 34 36 34 33 36 34
26E | 12 10 13 9 25 5 9 10 11 11 4 | 35 34 37 34 31 34 34 32 31 30 32
27 | 10 7 13 7 20 4 6 7 5 8 3 | 35 38 34 34 36 33 38 34 33 33 34
28 | 16 14 10 10 16 4 7 13 6 12 4 | 69 70 69 70 71 67 69 62 68 68 67
29 | 15 12 9 17 20 4 10 13 11 22 5 | 38 36 31 42 35 33 37 33 34 41 34
30 | 9 10 13 9 18 4 7 11 6 11 3 | 40 40 39 40 39 38 39 35 37 36 37
31 | 10 13 11 12 23 4 11 13 8 16 4 | 38 42 35 40 39 37 43 38 35 37 37
X32 | 17 --- 12 22 --- 8 --- 13 13 --- 8 | 30 --- 25 27 --- 24 --- 33 26 --- 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 11 10 21 4 9 11 9 13 |T 43 43 40 55 45 52 42 47 45 40 50
WRMS | 11 11 11 10 20 4 9 10 8 13 |NE 39 40 36 60 44 55 40 47 45 38 53
MEDI | 11 11 11 9 21 4 9 11 9 12 |MD 38 38 34 37 36 34 38 35 34 35 35
Table 3.1886.1 GPS week: 1886 Day: 1 MJD: 57447.000
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 | 10 10 12 9 12 5 10 5 7 12 3 | 28 28 32 23 30 26 31 23 25 29 26
2 | 11 11 7 13 14 5 10 13 8 16 4 | 29 32 26 30 23 26 29 29 29 26 27
3 | 13 10 11 8 13 4 9 9 7 10 3 | 31 35 35 29 33 31 37 25 32 34 31
X4E | 1 --- --- --- --- 31 --- --- --- --- 0 | 48 --- --- --- --- 39 --- --- --- --- 48
5 | 12 11 9 9 22 5 12 12 7 11 4 | 32 30 25 26 29 25 30 25 28 28 26
6 | 9 17 12 6 15 4 8 7 7 9 3 | 24 28 27 22 23 23 26 22 24 25 23
7 | 7 8 13 8 16 6 7 16 7 15 4 | 37 37 35 33 37 33 36 32 32 36 33
8 | 11 7 14 9 14 5 7 8 7 8 3 | 28 30 29 24 28 24 30 25 26 26 26
9 | 7 7 13 7 14 5 6 14 6 15 3 | 44 45 44 41 47 43 45 40 44 46 42
X10 | 18 13 9 --- 57 11 9 27 16 --- 8 | 64 71 64 --- 55 62 67 76 60 --- 65
11 | 10 10 18 8 22 5 8 7 10 11 4 | 31 35 33 30 39 30 34 30 35 32 32
12E | 19 15 6 14 24 4 14 12 13 13 5 | 38 33 30 31 29 30 35 26 32 28 29
X13 | >>>> --- --- 1 --- 612 --- --- --- --- 0 | 9999 --- --- 764 --- 516 --- --- --- --- 741
14 | 11 11 11 16 19 5 9 12 9 16 4 | 36 37 35 39 38 36 36 34 31 36 34
15 | 9 13 9 15 14 4 12 10 10 16 4 | 24 27 25 22 15 20 25 19 23 18 21
16E | 22 10 9 15 31 6 9 13 10 16 5 | 46 42 40 39 51 40 41 41 41 42 40
17 | 15 12 12 9 13 4 9 12 8 12 4 | 28 28 26 27 24 24 28 23 25 24 24
18 | 17 8 8 10 21 5 11 12 9 11 4 | 37 31 28 31 33 29 33 31 28 27 29
19 | 13 11 12 11 13 5 10 15 8 17 4 | 26 31 26 28 24 26 30 31 28 36 26
20 | 13 7 5 9 19 4 10 9 7 8 3 | 62 62 59 60 59 59 61 61 61 57 60
21 | 13 11 10 12 18 4 8 10 10 11 4 | 29 28 22 27 25 23 29 25 25 22 24
22 | 15 10 8 9 25 4 8 9 8 11 4 | 31 27 25 25 34 25 26 24 24 27 25
23 | 10 10 11 11 17 5 9 16 12 20 4 | 31 34 33 29 35 29 36 28 30 34 30
24 | 9 10 14 9 17 4 8 10 6 10 3 | 28 30 26 28 26 27 28 24 27 26 26
25E | 12 9 12 7 16 4 9 8 8 10 3 | 33 32 32 32 27 30 31 28 32 27 30
26E | 16 10 16 10 17 4 8 8 9 11 4 | 29 29 31 25 25 26 29 23 27 24 26
27 | 9 7 16 7 12 4 6 7 6 6 3 | 29 31 30 28 28 28 31 26 32 26 28
28E | 12 14 8 8 16 4 7 9 8 10 3 | 35 37 32 36 40 36 37 36 36 38 35
29 | 17 13 12 13 15 3 12 15 11 22 5 | 40 37 33 37 28 32 37 36 33 41 34
30 | 11 10 12 10 17 4 10 12 7 10 3 | 32 30 31 28 30 29 31 27 28 29 28
31 | 11 11 13 10 21 3 11 10 9 14 4 | 35 39 31 33 38 33 38 28 34 29 32
X32 | 17 --- 16 27 --- 11 --- 15 19 --- 9 | 32 --- 29 39 --- 26 --- 28 19 --- 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 11 12 10 18 4 9 11 9 13 |T 34 35 32 55 32 46 34 30 31 31 53
WRMS | 12 11 12 10 16 4 9 10 8 13 |NE 31 32 30 66 29 52 32 27 28 30 64
MEDI | 12 10 12 9 17 4 9 10 8 11 |MD 32 32 31 29 30 29 31 28 29 28 29
Table 3.1886.2 GPS week: 1886 Day: 2 MJD: 57448.000
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 | 10 10 12 8 11 3 12 6 8 12 3 | 27 29 30 22 27 26 34 24 26 29 26
2 | 12 14 9 14 14 4 10 11 9 13 4 | 29 32 25 29 27 26 31 27 29 26 27
3 | 11 20 12 7 19 5 12 7 6 9 4 | 35 39 37 32 40 33 39 33 34 36 35
X4E | 2 --- --- --- --- 28 --- --- --- --- 0 | 39 --- --- --- --- 43 --- --- --- --- 39
5 | 9 14 10 8 25 3 15 11 8 10 4 | 32 31 26 30 33 28 32 25 29 32 28
6 | 8 20 13 8 16 4 9 6 6 12 4 | 30 34 29 23 29 28 32 25 27 32 27
7 | 9 9 14 7 18 6 8 13 11 13 4 | 33 33 30 30 41 30 35 27 26 29 29
8 | 12 9 14 8 13 5 7 10 6 9 3 | 30 35 30 29 32 29 33 32 27 31 30
9 | 6 9 14 6 15 4 8 11 8 15 3 | 42 44 41 43 48 40 45 39 39 44 41
X10 | 21 11 10 --- 101 9 11 23 15 --- 7 | 62 68 61 --- 84 59 65 76 60 --- 64
11 | 11 13 19 8 17 6 9 8 12 10 4 | 41 43 35 39 43 38 46 38 42 35 39
12E | 23 15 7 12 29 5 13 12 11 13 5 | 42 39 32 31 36 34 36 30 29 34 32
X13 | 9 13 10 10 --- 6 10 11 8 --- 4 | 9999 35 33 198 --- 159 35 182 169 --- 207
14 | 13 17 12 15 17 5 12 10 8 16 4 | 37 34 32 35 36 33 31 28 30 35 31
15 | 11 15 12 11 13 3 15 12 9 17 4 | 28 33 30 27 16 27 26 25 29 19 28
16E | 19 12 8 15 17 4 12 10 9 15 4 | 52 48 47 45 46 46 50 46 45 48 47
17 | 12 12 13 12 10 5 9 13 10 13 4 | 27 32 26 29 27 24 31 28 27 28 26
18 | 13 13 8 9 23 5 15 11 9 11 4 | 48 46 42 42 46 44 46 45 46 44 44
19 | 13 12 11 12 11 5 11 14 9 17 4 | 29 32 27 26 29 26 34 31 28 19 27
20E | 16 9 10 8 20 6 13 9 8 8 4 | 85 81 79 85 81 80 80 81 82 83 80
21 | 13 12 9 11 15 2 11 9 7 12 3 | 30 29 24 28 27 25 28 25 27 25 26
22 | 13 12 9 9 20 4 10 10 8 12 4 | 34 37 28 27 34 29 35 29 32 31 31
23 | 11 13 13 10 23 6 9 17 11 20 5 | 32 36 34 34 39 30 35 27 27 33 31
24 | 11 10 15 8 16 4 9 9 6 10 3 | 28 29 24 26 32 27 28 26 25 29 25
25E | 16 11 14 6 20 6 10 6 5 10 3 | 34 34 31 28 29 31 31 26 28 29 29
26E | 14 12 14 11 16 4 10 10 9 14 4 | 27 29 30 25 24 27 28 26 27 27 26
27 | 10 8 15 10 13 4 6 8 12 10 3 | 31 37 31 32 34 31 37 32 38 32 33
28E | 15 9 8 10 18 3 10 9 6 12 3 | 49 51 46 46 58 48 52 51 50 55 50
29 | 14 13 12 11 15 5 13 13 11 20 4 | 38 36 30 34 26 30 36 32 31 38 32
30 | 14 9 13 8 15 5 10 11 8 9 3 | 30 31 29 26 35 28 34 28 27 28 28
31 | 14 12 12 10 20 5 12 10 9 17 4 | 34 35 27 31 41 30 36 25 29 30 29
X32 | >>>> --- --- 19 --- 33 --- 18 151 --- 18 | 1 --- --- 1 --- 1 --- 1 1 --- 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 13 12 10 18 5 11 11 9 13 |T 36 38 34 37 37 37 38 37 37 34 40
WRMS | 12 13 12 9 16 5 11 10 8 13 |NE 30 34 29 37 32 34 34 35 35 30 39
MEDI | 12 12 12 10 17 5 10 10 9 12 |MD 33 35 30 30 34 30 35 28 29 31 31
Table 3.1886.3 GPS week: 1886 Day: 3 MJD: 57449.000
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 11 8 14 3 10 5 8 11 3 | 42 43 42 39 43 41 42 39 39 42 40
2 | 12 12 11 15 17 3 12 12 11 15 4 | 41 42 40 43 40 39 41 37 40 36 38
3 | 9 14 12 8 12 3 10 7 9 7 3 | 46 49 48 46 45 47 44 45 48 48 46
X4E | 3 --- --- --- --- 24 --- --- --- --- 0 | 49 --- --- --- --- 54 --- --- --- --- 49
5 | 8 12 11 8 18 4 15 11 9 12 4 | 42 43 39 39 39 40 43 39 39 40 39
6 | 9 13 13 8 17 5 8 13 9 13 4 | 42 44 42 40 38 41 42 40 43 41 40
7 | 8 10 14 8 15 4 9 14 10 13 4 | 49 52 47 49 47 48 48 45 46 46 47
8 | 9 8 14 6 14 4 7 7 7 8 3 | 42 45 42 41 41 41 43 40 40 40 41
9 | 8 9 12 5 14 4 8 13 8 11 3 | 53 54 50 52 53 53 52 52 51 52 51
X10 | 13 11 7 --- 122 9 11 23 14 --- 6 | 80 81 79 --- 105 79 84 89 75 --- 81
11 | 8 13 17 8 18 5 9 7 11 8 4 | 50 54 47 50 53 50 50 47 51 47 49
12E | 23 15 9 12 20 4 12 14 12 12 5 | 46 43 40 42 42 42 40 39 40 42 40
13 | 8 12 14 13 22 5 10 12 11 14 4 | 844 33 26 132 124 111 33 86 84 17 138
14 | 10 13 11 10 16 4 10 11 10 15 4 | 44 46 43 46 51 45 47 47 45 46 45
15 | 8 13 15 10 14 4 12 12 12 18 4 | 24 28 29 24 18 24 24 21 23 16 23
16E | 23 12 9 15 19 4 12 14 11 17 5 | 53 50 48 45 52 48 51 47 43 47 46
17 | 12 9 12 11 12 6 11 12 10 14 4 | 43 46 43 47 42 43 47 42 44 42 43
18 | 11 11 9 9 23 6 13 11 10 11 4 | 50 47 46 48 57 48 49 47 48 46 48
19 | 12 10 11 12 14 5 12 13 12 16 4 | 42 45 41 45 41 41 47 42 41 34 41
20E | 9 9 9 8 15 4 11 12 7 8 3 | 61 62 60 60 58 61 59 60 62 58 60
21 | 12 10 11 10 19 4 14 11 11 15 4 | 42 42 40 42 45 40 44 37 39 38 39
22 | 17 10 7 9 22 4 9 9 10 10 4 | 39 39 35 37 45 38 37 36 39 37 37
23 | 12 10 11 10 17 4 9 20 13 19 4 | 48 50 46 47 48 47 48 42 46 43 45
24 | 11 7 16 6 16 4 7 12 8 9 3 | 35 36 35 35 38 36 35 37 36 37 35
25E | 9 8 14 7 15 5 9 12 9 12 3 | 40 40 42 43 43 42 42 41 41 41 40
26E | 16 9 16 11 16 5 10 9 10 12 4 | 43 42 44 40 38 41 41 37 36 37 39
27 | 7 6 14 5 14 4 7 6 8 4 2 | 44 44 41 44 43 42 43 40 39 40 41
28E | 13 10 7 8 19 4 9 9 9 8 3 | 50 50 49 49 50 49 52 46 49 48 48
29 | 13 12 14 12 16 5 13 14 11 21 5 | 42 44 41 46 44 42 44 42 44 47 42
30 | 9 10 14 8 15 3 10 11 7 7 3 | 37 42 40 38 40 38 40 36 39 36 38
31 | 13 11 14 9 20 4 9 11 9 13 4 | 44 45 39 43 50 43 47 38 41 39 41
X32 | 3 --- --- --- --- 40 --- --- --- --- 0 | 1 --- --- --- --- 9999 --- --- --- --- 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 12 10 17 4 11 12 10 13 |T 69 46 43 46 49 46 45 44 45 40 46
WRMS | 11 11 12 9 16 4 11 10 9 12 |NE 80 43 40 47 47 45 43 42 43 38 46
MEDI | 9 10 12 9 16 4 10 12 10 12 |MD 43 44 42 44 44 42 44 41 41 41 41
Table 3.1886.4 GPS week: 1886 Day: 4 MJD: 57450.000
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 10 10 10 12 4 9 5 8 13 3 | 38 36 37 38 36 35 38 32 35 38 35
2 | 9 13 8 18 14 4 11 11 10 18 4 | 30 33 30 37 27 29 33 29 25 25 28
3 | 9 10 10 10 12 4 9 9 8 13 3 | 38 39 41 38 37 38 39 36 39 38 37
X4E | 2 --- --- --- --- 27 --- --- --- --- 0 | 38 --- --- --- --- 36 --- --- --- --- 37
5 | 9 14 9 10 18 5 14 10 8 16 4 | 42 38 36 40 41 39 36 38 39 35 37
6 | 11 9 12 10 13 4 6 7 10 11 3 | 32 32 34 32 27 31 32 28 29 30 30
7 | 9 11 13 12 15 2 9 12 13 15 4 | 40 41 36 38 41 36 40 34 35 32 36
8 | 8 8 11 7 20 5 7 9 12 12 3 | 33 37 33 34 34 33 36 32 38 34 33
9 | 8 13 12 11 9 5 7 9 9 17 3 | 39 37 35 38 39 36 36 33 37 36 35
X10 | 19 15 10 --- 58 11 8 22 13 --- 9 | 70 79 75 --- 82 74 76 82 72 --- 74
11 | 9 10 16 8 19 5 8 6 7 10 3 | 45 46 40 43 49 40 46 40 43 42 42
12E | 17 13 7 15 20 3 13 12 11 16 5 | 41 38 31 35 32 33 35 33 33 32 33
13 | 9 12 10 16 15 3 11 13 12 15 4 | 676 34 31 82 67 86 33 78 75 19 77
14 | 10 9 11 15 17 4 10 11 10 15 4 | 39 36 37 44 37 38 36 35 36 38 36
X15 | 9 11 13 12 --- 5 --- 12 10 --- 5 | 37 39 37 40 --- 33 --- 30 33 --- 34
16E | 20 11 9 16 20 4 10 14 11 17 5 | 46 40 41 40 44 40 38 36 38 37 39
17 | 10 12 12 12 12 5 10 14 10 14 4 | 37 37 35 38 34 35 39 36 35 33 34
18E | 12 11 8 13 22 4 11 12 9 12 4 | 64 62 60 67 71 65 63 66 68 63 64
19 | 9 11 13 13 13 6 11 14 12 17 4 | 33 36 34 35 29 33 36 34 32 27 31
20E | 8 9 8 9 21 5 12 13 9 11 4 | 39 38 36 39 36 35 36 37 35 32 36
21 | 15 8 10 13 17 4 8 10 11 14 4 | 38 34 31 34 30 31 34 31 30 29 31
22 | 10 15 8 9 19 4 8 10 9 12 4 | 42 43 40 45 48 42 43 44 41 41 42
23 | 9 10 12 14 19 5 10 22 12 20 5 | 39 41 38 37 39 36 40 31 34 30 35
24 | 9 8 16 9 12 3 8 10 6 11 3 | 33 33 32 34 35 31 33 31 28 29 31
25E | 11 10 14 7 14 5 11 8 9 13 3 | 31 34 34 33 32 30 32 30 31 28 30
26E | 17 11 15 12 15 4 9 7 10 13 4 | 34 35 39 35 33 34 31 32 33 29 32
27 | 8 10 13 8 14 3 7 8 9 7 3 | 33 38 34 37 35 33 35 35 35 29 34
28E | 9 13 6 9 18 4 5 9 9 10 3 | 39 39 35 36 45 38 39 33 40 31 36
29 | 12 14 11 14 15 4 10 13 12 27 5 | 36 38 30 37 29 31 35 32 31 39 31
30 | 9 10 14 6 10 3 7 11 8 9 3 | 34 35 33 34 36 33 35 31 33 28 32
31 | 12 10 11 11 19 4 10 12 10 14 4 | 36 38 31 35 35 32 38 29 33 26 31
X32 | 19 --- --- 29 --- 27 --- 12 19 --- 11 | 9999 --- --- 1 --- 1 --- 1 1 --- 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 11 12 16 4 10 11 10 15 |T 59 39 37 38 40 37 38 36 37 33 37
WRMS | 10 11 11 11 16 4 10 10 9 13 |NE 69 36 34 37 36 34 36 33 33 31 35
MEDI | 9 11 11 11 15 4 9 11 10 13 |MD 38 38 35 37 36 35 36 33 35 32 35
Table 3.1886.5 GPS week: 1886 Day: 5 MJD: 57451.000
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 15 11 9 13 3 9 7 9 11 3 | 31 34 29 28 31 27 33 23 26 30 28
2 | 11 12 8 15 12 5 10 11 11 16 4 | 29 28 24 28 25 25 29 24 26 21 24
3 | 6 12 11 9 23 4 9 9 7 10 3 | 65 65 64 60 64 63 63 59 61 63 62
X4E | 3 --- --- --- --- 50 --- --- --- --- 0 | 32 --- --- --- --- 56 --- --- --- --- 30
5E | 10 12 8 10 26 7 12 14 10 10 4 | 47 46 42 46 47 47 45 48 46 45 45
6 | 8 11 12 9 12 5 7 8 6 12 3 | 28 26 29 26 25 27 29 22 27 27 26
7 | 9 10 11 10 13 4 9 11 9 15 3 | 45 41 37 41 41 41 43 34 40 34 38
8 | 9 7 11 6 16 4 7 9 8 9 3 | 28 32 27 28 32 28 31 26 28 27 28
9 | 7 8 12 7 10 5 7 7 10 14 3 | 42 44 40 42 45 43 46 39 43 44 42
X10 | 15 13 7 --- 66 10 8 20 15 --- 6 | 135 140 137 --- 124 138 136 143 131 --- 137
11 | 11 9 17 10 18 3 8 7 10 10 4 | 40 41 35 41 47 36 43 32 37 34 37
12E | 20 15 7 16 20 5 13 12 13 14 5 | 35 33 26 35 30 29 32 28 32 30 29
13 | 9 11 11 11 13 4 10 11 13 12 4 | 863 32 26 82 60 73 31 57 57 18 85
14 | 11 9 11 12 15 4 8 11 11 14 4 | 30 29 27 33 29 27 28 26 27 28 27
X15 | 3 --- --- --- --- 47 --- --- --- --- 0 | 13 --- --- --- --- 15 --- --- --- --- 12
16E | 23 9 6 17 18 6 9 16 11 15 5 | 41 34 32 34 36 34 35 34 35 33 32
17 | 11 12 12 13 13 3 10 13 9 14 4 | 32 34 27 34 34 30 36 29 32 27 30
18E | 17 11 6 12 14 5 8 11 9 9 4 | 46 41 35 43 37 39 40 38 39 37 38
19 | 13 11 13 13 12 4 11 14 13 19 4 | 30 33 27 29 29 28 36 29 32 25 28
20E | 11 8 7 9 16 4 9 11 8 7 3 | 43 43 38 41 39 42 40 40 43 37 40
21 | 14 9 10 10 17 4 8 11 9 14 4 | 30 27 23 28 30 25 28 23 23 22 24
22E | 15 8 7 10 18 4 8 12 8 9 3 | 32 23 22 32 29 26 28 25 27 26 24
23 | 12 10 11 13 15 5 10 21 10 19 5 | 34 35 29 31 32 31 36 24 31 25 29
24 | 10 8 13 8 11 4 7 7 5 9 3 | 28 27 25 28 26 26 27 24 25 21 25
25E | 15 9 14 8 19 5 11 7 9 10 4 | 28 29 30 29 25 27 30 25 26 22 26
26E | 15 9 14 9 18 5 8 7 7 10 3 | 30 29 34 31 30 30 29 26 27 24 28
27 | 9 8 12 5 14 4 6 6 8 9 3 | 28 31 27 29 32 29 32 27 29 26 28
28E | 13 9 6 9 14 4 7 12 8 11 3 | 30 31 25 28 36 29 32 29 32 25 29
29 | 13 14 13 12 16 4 11 15 12 22 5 | 32 32 24 29 26 26 29 24 26 32 26
30 | 10 10 12 7 9 4 7 12 9 8 3 | 37 36 35 35 34 36 37 30 36 30 34
31 | 12 11 12 8 21 4 11 12 9 16 4 | 35 36 28 34 36 31 37 26 29 28 30
X32 | 18 --- 14 25 --- 15 --- 11 16 --- 8 | 1 --- 57 9999 --- 1 --- 1 1 --- 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 10 11 11 16 4 9 11 10 13 |T 62 38 35 35 38 36 38 33 35 30 36
WRMS | 11 10 10 10 15 4 9 10 8 11 |NE 71 33 30 34 34 30 33 27 30 27 31
MEDI | 11 10 11 10 15 4 9 11 9 11 |MD 32 33 29 32 32 29 33 27 31 27 29
Table 3.1886.6 GPS week: 1886 Day: 6 MJD: 57452.000
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 10 11 9 10 6 10 6 9 10 3 | 38 37 38 34 36 36 38 34 37 38 36
2 | 10 15 8 15 16 5 9 10 8 13 4 | 33 36 32 37 30 31 36 33 31 31 32
3E | 11 10 11 9 15 5 10 8 9 7 3 | 58 63 66 60 58 61 60 58 61 64 61
X4E | 2 --- --- --- --- 30 --- --- --- --- 0 | 41 --- --- --- --- 48 --- --- --- --- 43
5E | 13 13 8 11 17 5 15 14 9 10 4 | 53 50 46 52 50 49 50 47 47 51 48
6 | 6 12 12 11 12 4 10 7 7 11 3 | 34 35 38 31 35 34 38 33 32 38 34
7 | 11 9 11 9 14 4 9 11 8 13 3 | 48 50 48 50 54 48 52 46 47 44 47
8 | 7 7 12 6 14 5 8 7 12 7 3 | 35 41 37 38 42 36 40 39 39 37 38
9 | 8 10 13 9 12 5 8 6 10 10 3 | 49 50 47 54 54 50 52 47 49 49 49
X10E | 16 8 10 --- 135 6 11 14 9 --- 5 | 151 158 158 --- 166 157 158 166 152 --- 157
11 | 9 11 18 7 18 4 8 7 10 7 3 | 52 56 47 51 60 51 55 49 57 50 52
12E | 15 15 6 13 31 3 14 12 11 12 5 | 46 48 41 45 45 43 48 39 42 43 43
13 | 7 11 10 13 17 4 12 11 11 11 4 | 786 32 26 86 70 81 32 74 72 18 93
14 | 12 10 12 12 14 2 11 13 11 17 4 | 44 45 43 52 49 47 46 46 45 45 45
X15 | 9 13 12 18 13 6 12 15 12 --- 5 | 15 17 15 5 3 14 16 3 4 --- 11
16E | 18 12 6 16 16 6 13 13 11 16 4 | 53 50 48 46 50 46 48 46 44 46 47
17 | 7 13 13 11 11 6 10 12 8 12 4 | 39 44 40 42 41 40 45 44 43 42 42
18E | 18 12 5 14 17 5 13 14 10 10 4 | 57 53 51 58 59 56 53 58 54 55 54
19 | 8 11 12 15 12 5 14 13 10 15 4 | 34 38 33 37 34 34 39 39 35 29 35
20E | 10 9 7 11 20 4 12 10 7 6 3 | 48 48 43 49 46 48 48 47 47 49 47
21 | 16 11 10 13 16 4 13 13 10 15 4 | 41 39 33 39 40 36 38 39 37 34 36
22E | 18 9 7 11 17 5 9 10 10 8 4 | 41 40 37 39 46 39 38 40 40 41 39
23 | 13 11 11 13 17 5 12 22 13 16 5 | 43 45 42 44 44 42 44 38 42 38 41
24 | 10 9 15 11 16 3 9 7 10 7 3 | 32 35 34 38 40 33 38 33 33 33 34
25E | 10 9 17 14 15 4 10 7 10 8 4 | 37 37 44 38 39 36 38 33 35 33 36
26E | 16 14 15 11 17 6 9 9 8 9 4 | 38 41 42 34 33 36 37 36 37 32 36
27 | 5 7 13 7 13 5 7 6 7 6 3 | 40 43 41 43 45 41 42 42 42 41 42
28E | 10 12 6 11 19 6 10 13 9 8 4 | 40 40 39 39 49 41 42 40 40 40 39
29 | 14 13 11 10 15 5 16 16 11 20 5 | 42 42 38 42 38 41 43 42 41 46 40
30 | 8 9 12 6 12 4 8 10 7 7 3 | 36 43 40 39 44 38 43 38 38 37 39
31 | 10 15 13 9 20 4 11 11 12 15 4 | 41 46 37 41 48 39 46 35 42 35 39
X32 | 22 --- 15 29 --- 7 --- 12 15 --- 9 | 9999 --- 60 1 --- 9999 --- 9999 1 --- 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 11 11 16 5 11 11 10 12 |T 69 46 44 42 48 46 46 45 44 40 46
WRMS | 10 11 11 11 15 5 11 11 9 11 |NE 78 40 38 40 42 40 41 39 38 38 41
MEDI | 10 11 11 11 16 5 10 11 10 10 |MD 41 43 41 41 45 41 43 40 42 40 41
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 4.1886 GPS week: 1886 MJD: 57446.0-57452.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2984 |U 4 5 12 |U 15 16 39 |U 6 6 16 |
emr | emr 2837 | 6 6 14 |U 15 16 41 | 8 8 20 |
esa | esa 2893 | 5 5 14 |U 15 15 42 | 8 8 19 |
gfz | gfz 2833 |U 4 5 12 |U 15 15 42 |U 7 8 17 |
grg | grg 2819 |U 7 7 16 |U 15 16 44 | 10 11 20 |
igr | igr 2895 | 4 5 11 | 15 15 40 | 7 7 16 |
igs | igs 2919 | 4 5 11 | 15 15 41 | 7 8 17 |
jpl | jpl 2825 | 6 7 15 |U 15 15 41 | 9 7 21 |
mit | mit 2934 | 5 6 14 |U 17 17 47 |U 7 8 17 |
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 5.1886.0 GPS week: 1886 Day: 0 MJD: 57446.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3001 | 3 5 11 | 7 14 24 | 6 8 15 |
emr | emr 2784 | 4 6 13 | 7 16 29 | 9 9 21 |
esa | esa 2880 | 4 5 14 | 7 15 27 | 9 9 21 |
gfz | gfz 2843 | 4 4 12 | 8 14 27 | 8 11 17 |
grg | grg 2843 | 9 7 14 | 9 15 28 | 11 11 20 |
igr | igr 2939 | 4 5 11 | 7 14 26 | 8 8 15 |
igs | igs 2939 | 4 5 11 | 7 15 26 | 8 9 17 |
jpl | jpl 2784 | 6 9 17 | 8 18 33 | 11 7 22 |
mit | mit 2976 | 4 4 12 | 9 19 27 | 7 8 16 |
Table 5.1886.1 GPS week: 1886 Day: 1 MJD: 57447.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 | 3 4 10 | 12 19 49 | 6 5 16 |
emr | emr 2784 | 5 4 12 | 14 20 55 | 10 8 28 |
esa | esa 2880 | 4 4 11 | 15 20 58 | 8 7 23 |
gfz | gfz 2807 | 4 4 8 | 14 18 59 | 8 7 20 |
grg | grg 2784 | 7 5 16 | 15 22 60 | 9 10 21 |
igr | igr 2880 | 3 3 10 | 15 19 55 | 7 6 19 |
igs | igs 2880 | 3 3 8 | 15 19 55 | 8 6 21 |
jpl | jpl 2784 | 4 5 13 | 15 20 53 | 10 7 27 |
mit | mit 2880 | 9 11 16 | 15 22 59 | 9 11 21 |
Table 5.1886.2 GPS week: 1886 Day: 2 MJD: 57448.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2938 | 5 6 14 | 11 10 37 | 5 5 15 |
emr | emr 2880 | 7 6 15 | 13 12 44 | 8 8 20 |
esa | esa 2880 | 6 5 14 | 11 10 41 | 7 7 20 |
gfz | gfz 2856 | 5 7 12 | 12 10 48 | 6 8 15 |
grg | grg 2784 | 7 6 15 | 14 15 42 | 9 10 23 |
igr | igr 2880 | 6 5 12 | 12 9 40 | 5 6 17 |
igs | igs 2930 | 6 5 12 | 12 10 42 | 6 7 17 |
jpl | jpl 2880 | 6 6 15 | 13 9 47 | 8 8 21 |
mit | mit 2976 | 6 5 15 | 21 19 63 | 7 10 17 |
Table 5.1886.3 GPS week: 1886 Day: 3 MJD: 57449.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 | 5 5 16 | 18 16 43 | 6 6 11 |
emr | emr 2872 | 7 7 18 | 18 16 44 | 7 7 16 |
esa | esa 2880 | 6 6 18 | 18 17 48 | 7 8 15 |
gfz | gfz 2784 | 5 5 14 | 18 16 46 | 7 8 14 |
grg | grg 2880 | 6 8 18 | 16 14 54 | 9 8 15 |
igr | igr 2880 | 5 6 14 | 18 15 47 | 6 6 11 |
igs | igs 2880 | 5 6 15 | 17 15 47 | 6 7 12 |
jpl | jpl 2880 | 6 7 18 | 17 16 45 | 9 8 17 |
mit | mit 2880 | 4 5 14 | 18 18 51 | 6 6 11 |
Table 5.1886.4 GPS week: 1886 Day: 4 MJD: 57450.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 4 5 11 | 23 18 49 | 7 7 20 |
emr | emr 2879 | 6 5 14 | 21 21 48 | 9 8 22 |
esa | esa 2880 | 4 5 13 | 22 18 50 | 8 7 22 |
gfz | gfz 2880 | 5 5 11 | 20 18 45 | 7 7 21 |
grg | grg 2784 | 7 7 15 | 20 17 49 | 10 11 22 |
igr | igr 2880 | 4 5 10 | 21 19 46 | 7 7 19 |
igs | igs 2954 | 4 5 10 | 22 19 50 | 8 8 20 |
jpl | jpl 2784 | 6 7 13 | 22 16 49 | 9 7 20 |
mit | mit 2976 | 4 4 12 | 22 19 50 | 7 9 20 |
Table 5.1886.5 GPS week: 1886 Day: 5 MJD: 57451.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2937 | 4 4 11 | 13 15 31 | 6 6 14 |
emr | emr 2784 | 6 7 14 | 13 15 31 | 7 5 16 |
esa | esa 2880 | 5 5 14 | 12 13 32 | 7 6 14 |
gfz | gfz 2784 | 4 4 11 | 12 15 31 | 6 5 13 |
grg | grg 2784 | 5 8 15 | 13 14 38 | 9 9 17 |
igr | igr 2836 | 4 5 11 | 12 13 31 | 6 5 13 |
igs | igs 2880 | 4 5 11 | 12 14 31 | 5 5 12 |
jpl | jpl 2784 | 5 8 14 | 11 13 28 | 8 5 17 |
mit | mit 2880 | 4 6 14 | 12 13 35 | 5 6 12 |
Table 5.1886.6 GPS week: 1886 Day: 6 MJD: 57452.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 5 6 12 | 20 19 43 | 7 10 19 |
emr | emr 2879 | 7 8 13 | 19 16 37 | 9 10 20 |
esa | esa 2976 | 5 6 13 | 20 15 36 | 9 12 19 |
gfz | gfz 2880 | 5 6 13 | 19 13 37 | 8 11 21 |
grg | grg 2880 | 8 8 21 | 17 16 35 | 13 16 26 |
igr | igr 2976 | 5 6 11 | 19 17 35 | 8 10 20 |
igs | igs 2976 | 5 6 12 | 19 14 34 | 8 11 20 |
jpl | jpl 2880 | 6 8 16 | 18 12 36 | 10 10 22 |
mit | mit 2976 | 8 9 16 | 20 13 40 | 8 10 23 |
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 6.1886 GPS week: 1886 MJD: 57446.500-57452.500
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 | 4 -4 -29 61 -1 | 24 46
| 24 17 72 99 7 | 6
emr uuuuu | 31 -24 68 189 -2 | 30 47
| 25 23 123 45 5 | 7
esa uuuuu | 19 26 52 54 -2 | 37 52
| 11 19 31 59 4 | 6
gfz uuuuu | -12 -31 205 -108 4 | 18 40
| 21 14 56 137 3 | 5
grg uuuux | -28 -1 31 -136 25 | 47 58
| 32 9 90 69 33 | 4
igr xxxxx | -3 -1 57 63 0 | 2 38
| 29 24 82 79 4 | 5
irf xxxxx | 19 -1 -16 -21 -1 | 1 38
| 7 9 35 29 5 | 6
jpl uuuuu | -16 -32 50 103 8 | 38 53
| 28 35 131 73 7 | 4
mit uuuuu | 11 19 -81 -67 -1 | 18 41
| 20 12 74 54 4 | 5
ngs uuuuu | -12 25 -117 -76 -3 | 11 38
| 49 28 116 154 5 | 6
sio uuuux | 2 27 -190 -75 9 | 56 66
| 14 18 85 51 9 | 3
Table 7.1886.0 GPS week: 1886 Day: 0 MJD: 57446.500
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 | 21 20 -76 82 4 | 29 45
emr uuuuu | 57 -26 62 165 -1 | 39 50
esa uuuuu | 22 55 23 138 2 | 42 53
gfz uuuuu | -19 -10 160 -13 6 | 23 38
grg uuuux | -21 -10 -31 -213 -20 | 47 56
igr xxxxx | -25 14 65 15 6 | 6 33
irf xxxxx | 22 6 20 -67 -9 | 7 34
jpl uuuuu | 9 -81 -75 178 6 | 40 52
mit uuuuu | 18 4 2 -140 -2 | 23 40
ngs uuuuu | -65 49 -12 -208 -9 | 18 36
sio uuuux | -9 14 -115 -103 -2 | 59 67
Table 7.1886.1 GPS week: 1886 Day: 1 MJD: 57447.500
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 -11 84 192 -12 | 33 48
emr uuuuu | 61 8 -154 236 -2 | 42 53
esa uuuuu | 2 33 89 42 4 | 46 56
gfz uuuuu | -23 -35 184 -53 1 | 27 41
grg uuuux | -76 8 -133 -197 1 | 50 58
igr xxxxx | -54 10 139 -35 -5 | 10 35
irf xxxxx | 16 5 36 -4 -7 | 10 35
jpl uuuuu | -6 -44 -98 33 10 | 45 56
mit uuuuu | 32 16 21 -1 5 | 26 43
ngs uuuuu | -35 26 15 -235 -3 | 21 37
sio uuuux | -3 7 -58 2 14 | 61 70
Table 7.1886.2 GPS week: 1886 Day: 2 MJD: 57448.500
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 -6 1 112 7 | 22 50
emr uuuuu | 46 -23 -38 140 4 | 29 49
esa uuuuu | 29 21 49 115 -1 | 36 54
gfz uuuuu | 2 -48 159 34 0 | 16 43
grg uuuux | -51 -13 40 -54 46 | 40 55
igr xxxxx | 8 -16 182 138 2 | 1 43
irf xxxxx | 22 -17 -34 -1 3 | 0 43
jpl uuuuu | 0 -45 107 35 -4 | 36 53
mit uuuuu | 32 27 -144 -101 1 | 17 44
ngs uuuuu | -75 36 4 -134 -6 | 11 41
sio uuuux | 25 42 -210 -75 17 | 52 65
Table 7.1886.3 GPS week: 1886 Day: 3 MJD: 57449.500
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 | 2 -25 -95 94 -1 | 24 48
emr uuuuu | 25 -26 112 176 1 | 29 49
esa uuuuu | 20 33 12 60 -6 | 37 54
gfz uuuuu | -38 -14 202 -245 0 | 18 42
grg uuuux | -42 1 88 -134 64 | 44 56
igr xxxxx | -1 18 67 141 -4 | 3 40
irf xxxxx | 12 4 -65 -15 1 | 1 41
jpl uuuuu | 16 -10 255 89 10 | 36 53
mit uuuuu | 17 17 -185 -51 0 | 19 43
ngs uuuuu | -10 8 -181 49 -3 | 11 41
sio uuuux | -3 31 -267 -65 22 | 55 65
Table 7.1886.4 GPS week: 1886 Day: 4 MJD: 57450.500
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 | -48 6 -46 -106 3 | 18 44
emr uuuuu | -10 3 144 266 -5 | 23 43
esa uuuuu | 35 -10 85 -38 -1 | 31 48
gfz uuuuu | -10 -39 253 -267 6 | 13 38
grg uuuux | 6 -8 85 -193 16 | 45 58
igr xxxxx | 33 26 -11 154 1 | -3 37
irf xxxxx | 31 -9 -8 -57 7 | -5 37
jpl uuuuu | -29 24 83 184 5 | 32 49
mit uuuuu | -4 9 -75 -122 0 | 14 38
ngs uuuuu | 48 -19 -268 147 -7 | 5 37
sio uuuux | 19 43 -241 -69 7 | 52 62
Table 7.1886.5 GPS week: 1886 Day: 5 MJD: 57451.500
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 | 9 -22 38 -33 -1 | 20 45
emr uuuuu | 23 -43 159 182 -10 | 25 45
esa uuuuu | 10 25 72 37 -4 | 33 50
gfz uuuuu | -25 -37 307 -240 5 | 16 40
grg uuuux | -26 11 27 -118 6 | 50 63
igr xxxxx | 18 -32 -41 35 -1 | -1 38
irf xxxxx | 11 7 -34 -12 0 | -2 39
jpl uuuuu | -43 -12 -62 172 18 | 36 52
mit uuuuu | 9 39 -100 -40 -4 | 16 40
ngs uuuuu | 38 11 -173 49 1 | 6 37
sio uuuux | -2 48 -290 -165 -1 | 56 66
Table 7.1886.6 GPS week: 1886 Day: 6 MJD: 57452.500
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 | 16 9 -109 84 -10 | 19 44
emr uuuuu | 16 -58 190 162 -4 | 23 42
esa uuuuu | 17 25 33 24 -5 | 31 48
gfz uuuuu | 28 -32 169 27 7 | 16 40
grg uuuux | 14 5 138 -41 63 | 51 64
igr xxxxx | 2 -28 -3 -3 -2 | -2 37
irf xxxxx | 21 -5 -25 7 0 | -3 37
jpl uuuuu | -57 -56 136 30 12 | 37 54
mit uuuuu | -23 22 -86 -16 -7 | 14 38
ngs uuuuu | 15 65 -207 -197 7 | 5 36
sio uuuux | -13 5 -148 -46 3 | 55 65
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