[IGSREPORT-23820] Wk 1856 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sun Aug 23 07:10:58 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1856 (Aug 02, 2015 - Aug 08, 2015)
Contacts: igs.acc 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:
igs1856[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1856[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1856[0-6].cls IGS GPS clock combination summary report.
igs18567.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18567.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 | 4 MATE
0 | ESA | 4 MATE WTZR POHN TONG
0 | GRG | 1 2 3 4 5 6 7 9 10 11 12 13 14 15 16 17 18 19 20
0 | GRG | 21 22 23 24 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7
0 | GRG | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
0 | GRG | 26 27 28 29 30 31 32
0 | JPL | 4
0 | MIT | IRKJ
1 | COD | 4 HOB2
1 | ESA | 4 HOB2 POHN
1 | GFZ | HOB2 MDVJ MDVJ
1 | GRG | 1 2 3 4 5 6 7 9 10 11 12 13 14 15 16 17 18 19 20
1 | GRG | 21 22 23 24 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7
1 | GRG | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
1 | GRG | 26 27 28 29 30 31 32
1 | JPL | 4
1 | MIT | HOB2
2 | COD | 4 4 BRMU BRMU REUN
2 | ESA | 4 4 DRAG TONG
2 | GFZ | IRKJ BRMU IRKJ PIMO POHN
2 | GRG | NRMD BRST CCJ2 NRMD TONG
2 | JPL | 4 HOB2 POHN
2 | MIT | BRMU BRMU
3 | COD | 4 4 BRST
3 | ESA | 4 HOB2 IRKJ
3 | GFZ | HOB2 HOB2
3 | GRG | 6 BRST DARW PIMO POHN
3 | JPL | 4 TUVA
4 | ALL | 8
4 | COD | 4 4 REUN
4 | ESA | 4 4 REUN REUN
4 | MIT | PTBB PTBB
5 | ALL | 8
5 | EMR | 4 4
5 | ESA | WTZR
5 | GFZ | 4 4 FAIR
5 | GRG | 1 2 3 4 5 6 7 9 11 12 13 14 15 16 17 18 19 20 21
5 | GRG | 22 23 24 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7 9
5 | GRG | 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27
5 | GRG | 28 29 30 31 32
5 | JPL | 4 YELL
5 | MIT | FAIR FAIR
6 | COD | 2 4 2 4
6 | ESA | 4 4
6 | GRG | 3 POHN
6 | JPL | 8
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
3 | ESA | ~23:45 | ~ -0.10 ns
6. 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.
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G08 | | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.7 -.7 -1.3 -13 20 -26 .43
EMR | 0 | .4 8.1 8.5 55 -37 3 .16
ESA | 0 | -.3 .1 .2 38 -4 20 -.04
GFZ | 0 | -.2 -.4 -1.6 8 -64 -4 .20
GRG | 0 | 3.6 -4.8 15.8 -31 -11 -35 -.09
JPL | 0 | -3.0 -4.6 4.4 -10 13 33 .52
MIT | 0 | -3.4 -7.5 9.4 18 0 -14 .47
NGS | 0 | -.6 -1.3 14.7 -39 -41 -9 .50
SIO | 0 | 1.2 1.8 17.7 -28 3 -7 .37
COD | 1 | .1 -.9 -1.2 -24 15 -30 .33
EMR | 1 | 3.6 4.7 10.4 49 -38 21 .24
ESA | 1 | -.4 -.9 -.1 17 -9 44 .0
GFZ | 1 | -.3 -.6 -1.3 3 -78 -21 .29
GRG | 1 | 3.2 -2.8 12.9 -40 -13 -19 .10
JPL | 1 | 8.4 -8.3 3.0 26 4 45 .39
MIT | 1 | .3 -6.5 11.7 19 -3 -43 .53
NGS | 1 | -2.0 -3.2 22.1 -126 -22 -58 .52
SIO | 1 | .8 1.0 10.4 -20 7 8 .37
COD | 2 | .6 -1.0 -.3 -38 -3 -24 .39
EMR | 2 | -.3 3.7 3.0 49 -39 33 .39
ESA | 2 | -.3 -1.5 -.6 2 -10 8 .05
GFZ | 2 | 1.0 -1.3 -.7 -37 -79 -28 .24
GRG | 2 | 9.0 -3.5 8.5 -45 -21 -22 .23
JPL | 2 | -.4 -5.1 2.4 8 0 18 .63
MIT | 2 | 2.3 -2.9 13.7 35 -12 -31 .38
NGS | 2 | -5.4 -6.9 12.3 -62 -6 -63 .53
SIO | 2 | .2 4.5 13.5 9 -15 35 .13
COD | 3 | .5 -1.0 -1.0 -41 -17 -25 .44
EMR | 3 | 7.9 -1.2 3.8 43 -30 15 .46
ESA | 3 | -.6 -1.2 -.6 -14 -3 -7 .17
GFZ | 3 | .7 -2.0 -2.4 -54 -94 -19 .46
GRG | 3 | 8.0 -2.4 .5 1 -15 4 .35
JPL | 3 | .7 -1.1 -2.6 9 27 7 .34
MIT | 3 | 2.9 -3.9 11.2 18 -16 -49 .49
NGS | 3 | -4.3 -3.3 8.7 -60 6 -76 .61
SIO | 3 | .4 4.8 13.3 -22 7 -5 .36
COD | 4 | .4 -.6 -1.1 -17 11 3 .33
EMR | 4 | 7.1 3.4 6.2 -5 -26 -11 .31
ESA | 4 | -1.4 -.6 -.6 23 -6 41 .09
GFZ | 4 | .3 -.8 -2.6 -13 -75 -12 .42
GRG | 4 | 10.8 -1.0 4.1 19 0 -54 .11
JPL | 4 | -6.8 -5.4 .3 -45 37 -17 .40
MIT | 4 | 1.8 -1.9 6.5 11 6 -42 .51
NGS | 4 | -2.6 .1 15.3 -59 -4 -44 .57
SIO | 4 | 2.6 6.4 4.0 -28 -1 -6 .32
COD | 5 | .7 -1.0 -.9 -22 -7 25 .23
EMR | 5 | 4.7 2.9 4.3 1 -23 -7 .45
ESA | 5 | -.4 -1.4 -1.0 -7 3 9 .07
GFZ | 5 | .8 -1.2 -1.2 -38 -79 -33 .42
GRG | 5 | 8.2 -.1 16.3 -40 11 23 .13
JPL | 5 | 3.1 -2.9 4.3 7 22 -1 .49
MIT | 5 | 3.0 -2.3 9.1 20 2 -31 .47
NGS | 5 | -1.9 -1.9 18.4 -98 -19 -38 .53
SIO | 5 | 3.7 .9 12.3 -27 -8 12 .25
COD | 6 | -.3 -1.7 -1.5 -34 7 -8 .35
EMR | 6 | 6.1 9.2 12.5 -15 -5 -11 .23
ESA | 6 | -.3 -1.2 -1.0 -6 -1 22 .02
GFZ | 6 | .3 -1.0 -1.5 -36 -73 -35 .33
GRG | 6 | 8.3 -4.0 10.8 -22 -2 -21 .48
JPL | 6 | -2.1 .3 3.7 -2 6 -7 .48
MIT | 6 | 7.8 -4.2 7.1 11 15 -58 .75
NGS | 6 | -3.6 1.4 11.0 -16 -15 -63 .31
SIO | 6 | 2.6 .9 13.8 -35 -6 12 .43
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1856.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1856.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 2.1856.[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 3.1856.[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 5.1856.0-6). 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 1856 summary. (Aug 02, 2015 - Aug 08, 2015)
Table 1.1856.a GPS week: 1856 MJD: 57236.000-57242.000
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 232| 1 0 -3 5 9 11 .02 12 11 | -1142 -255 14 119
| 1 0 1 19 19 22 .03 | 177 265
emr 80| 0 1 0 11 -42 13 .24 12 12 | 4674 135 14 138
| 0 1 1 9 15 10 .04 | 511 536
esa 150| 0 0 -5 -13 4 -11 -.34 12 12 | -410 -315 8 162
| 0 0 1 17 11 13 .02 | 373 720
gfz 191| -1 0 1 4 0 -2 .11 12 10 | -201 111 12 82
| 1 0 1 16 13 11 .04 | 185 482
grg 114| 3 -1 7 -16 26 47 .05 16 15 | 404 -72 2130 2774
| 1 1 2 18 24 33 .03 | 1051 360
igr n/a| 0 0 -2 -20 -14 8 -.01 4 4 | 3624 -119 15 60
| 0 0 0 15 14 15 .01 | 866 643
jpl 80| 0 0 0 -22 27 19 .22 10 10 | 4683 125 15 103
| 1 1 1 24 21 18 .03 | 500 540
mit 349| 0 -1 0 1 -13 -28 -.25 13 12 | -679 0 41 398
| 1 1 1 16 31 18 .04 | 364 433
ngs 215| 0 0 2 28 -1 -13 -.04 10 8 | -1042 -305 948 2269
| 0 0 3 11 24 19 .04 | 186 358
sio 301| 0 0 -3 -2 -13 -27 -.12 13 13 | --- --- --- ---
| 0 0 1 28 26 18 .03 | --- ---
Table 1.1856.b GPS week : 1856 MJD: 57236.000-57242.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 3 4 4 4 |
2 | 5 4 4 4 4 6 6 |
3 | 4 3 3 4 3 3 3 |
4 | 5 5 5 5 5 6 7 |
5 | 5 5 5 5 4 5 5 |
6 | 4 4 4 4 4 4 7 |
7 | 4 5 5 5 5 5 4 |
8 | 0 0 0 0 13 13 10 |
9 | 3 3 3 3 3 3 3 |
10 | 4 7 --- --- --- --- --- |
11 | 4 4 3 3 3 4 4 |
12 | 5 5 6 5 6 6 6 |
13 | 4 4 4 4 5 5 5 |
14 | 5 4 4 4 4 4 4 |
15 | 5 5 4 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 4 4 5 5 4 5 |
18 | 6 5 5 6 6 5 6 |
19 | 5 4 4 5 4 5 5 |
20 | 5 4 4 5 5 5 5 |
21 | 4 4 4 4 4 4 4 |
22 | 5 4 4 4 5 5 5 |
23 | 4 4 4 4 4 4 4 |
24 | 4 3 4 3 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 4 3 4 3 4 4 |
28 | 5 5 4 5 5 4 4 |
29 | 5 4 5 5 5 5 5 |
30 | 4 5 4 4 4 4 4 |
31 | 4 4 4 4 4 4 5 |
32 | 4 4 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
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 2.1856.0 GPS week: 1856 Day: 0 MJD: 57236.000
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 233| 0 0 -4 26 0 10 -.02 12 11 | -1114 -532 16 105
emr 80| 0 1 0 6 -59 -1 .18 12 12 | 4601 303 16 122
esa 150| 0 0 -6 16 -6 -22 -.37 13 13 | -598 561 9 139
gfz 192| 0 0 1 20 6 3 .05 12 11 | -100 -294 12 80
grg 116| 1 0 10 -5 43 22 .02 16 16 | 142 -152 14547 16057
igr n/a| 0 0 -2 -35 -24 -21 -.01 4 4 | 4576 208 15 49
jpl 80| 0 1 0 -30 9 24 .17 10 10 | 4624 317 16 96
mit 349| 0 0 1 -20 8 -8 -.20 14 13 | -1129 -503 44 359
ngs 214| 0 -1 2 36 -14 -4 .04 11 9 | -1115 97 1023 2254
sio 300| -1 0 -2 -46 21 -9 -.09 14 13 | --- --- --- ---
Table 2.1856.1 GPS week: 1856 Day: 1 MJD: 57237.000
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 229| 1 0 -5 -19 -6 -15 -.01 11 10 | -1367 27 13 117
emr 80| 0 2 0 -5 -38 4 .18 12 12 | 5207 -911 13 135
esa 150| 0 -1 -7 -22 -3 0 -.37 12 12 | -656 -259 8 152
gfz 188| 0 0 0 22 21 7 .08 11 10 | -139 -381 13 83
grg 117| 1 -1 8 -6 57 30 .04 14 14 | 2777 -713 204 2267
igr n/a| 0 -1 -3 -29 -14 14 -.01 4 4 | 5086 -1431 14 57
jpl 80| 0 0 0 -4 34 45 .21 10 10 | 5200 -920 14 93
mit 349| -1 -1 1 14 -33 -19 -.21 13 12 | -1146 402 41 407
ngs 214| -1 0 8 11 -17 -44 -.00 10 8 | -808 -809 851 2201
sio 298| 0 0 -5 21 -15 -10 -.11 13 12 | --- --- --- ---
Table 2.1856.2 GPS week: 1856 Day: 2 MJD: 57238.000
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 231| 1 0 -3 -4 5 -3 .03 11 11 | -1197 -67 14 126
emr 80| 0 1 0 18 -65 21 .25 11 11 | 4221 -36 13 133
esa 150| -1 -2 -5 -12 1 -11 -.31 12 12 | -575 -443 8 164
gfz 192| -1 0 2 -10 -1 -16 .10 12 10 | -451 637 13 80
grg 116| 2 -1 2 -48 54 -1 .05 15 14 | 23 -54 20 195
igr n/a| 0 0 -1 -10 -17 16 -.02 4 4 | 3514 -411 14 60
jpl 80| 0 -1 2 -10 12 27 .20 10 10 | 4198 -46 15 105
mit 349| 0 0 1 0 5 -32 -.23 12 11 | -311 -333 37 387
ngs 216| 0 0 2 33 -1 2 -.06 9 8 | -1286 103 872 2433
sio 299| 0 0 -3 9 4 -12 -.13 13 13 | --- --- --- ---
Table 2.1856.3 GPS week: 1856 Day: 3 MJD: 57239.000
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 235| 0 -1 -2 -3 -12 2 .01 11 11 | -906 -540 13 117
emr 80| 0 0 0 4 -31 19 .24 12 12 | 3912 240 14 154
esa 150| 0 -1 -4 -39 15 -19 -.35 12 12 | 139 -1481 9 226
gfz 192| -1 0 2 -6 -22 4 .14 12 10 | -177 -418 12 82
grg 112| 4 -3 5 -13 4 68 .01 16 15 | -1 -220 21 208
igr n/a| 0 0 0 -12 -17 12 -.01 4 4 | 2878 -137 17 66
jpl 80| 0 1 0 -12 70 1 .25 10 10 | 3955 218 13 110
mit 349| 0 0 1 10 -66 -31 -.26 13 11 | -709 -446 40 406
ngs 215| 0 0 0 37 29 7 -.08 9 8 | -826 -675 1018 2182
sio 304| -1 0 -2 19 -39 -26 -.09 14 13 | --- --- --- ---
Table 2.1856.4 GPS week: 1856 Day: 4 MJD: 57240.000
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 236| 1 0 -4 31 17 19 .06 12 12 | -960 -405 16 117
emr 80| 0 1 0 17 -49 7 .27 12 12 | 4494 423 14 158
esa 150| 0 0 -4 -17 8 7 -.32 12 12 | -913 518 9 160
gfz 193| -2 0 1 -8 -7 -1 .15 13 12 | -465 705 13 85
grg 113| 3 -1 5 10 0 39 .06 14 13 | -20 40 18 223
igr n/a| 0 0 -2 -44 -34 -2 -.00 4 4 | 2870 332 15 60
jpl 80| -1 0 0 -75 9 -9 .24 11 11 | 4521 359 16 102
mit 349| 0 0 -1 -13 9 -11 -.27 12 10 | -685 51 38 413
ngs 216| 0 0 4 39 12 0 -.06 9 8 | -957 -360 966 1988
sio 303| 0 0 -3 1 -12 -60 -.09 13 13 | --- --- --- ---
Table 2.1856.5 GPS week: 1856 Day: 5 MJD: 57241.000
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 231| -1 0 -2 -10 43 56 .02 12 12 | -1351 88 14 109
emr 80| 1 1 1 22 -34 25 .26 11 11 | 5028 826 15 136
esa 150| 0 0 -7 -11 23 -30 -.33 13 13 | -64 -836 9 147
gfz 189| -3 -1 0 -8 -1 -19 .11 12 11 | 25 396 12 91
grg 114| 4 -1 7 -28 6 92 .06 19 16 | -183 467 82 250
igr n/a| 0 -1 -2 -9 1 10 .00 5 4 | 3278 379 15 58
jpl 80| 1 1 0 -12 26 21 .27 10 10 | 5042 853 15 100
mit 349| 0 -2 0 26 -36 -29 -.29 13 12 | -577 581 47 410
ngs 215| 0 0 4 12 18 -33 -.08 10 9 | -1228 -100 889 2302
sio 300| 0 0 -5 14 -54 -41 -.15 13 12 | --- --- --- ---
Table 2.1856.6 GPS week: 1856 Day: 6 MJD: 57242.000
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 234| 2 0 -3 17 21 8 .06 15 12 | -1100 -362 16 144
emr 80| 0 4 3 16 -22 18 .29 12 12 | 5256 100 13 129
esa 150| 0 0 -3 -6 -8 -3 -.35 13 13 | -209 -269 8 148
gfz 192| 0 -1 0 25 -2 7 .13 12 10 | -105 138 11 78
grg 113| 4 0 9 -21 18 79 .11 15 15 | 93 123 22 224
igr n/a| 0 -1 -2 -1 8 28 -.01 5 4 | 3171 226 17 72
jpl 80| -1 3 0 -11 32 25 .20 11 11 | 5242 98 16 119
mit 349| 1 -2 0 -9 17 -65 -.31 13 12 | -199 246 42 407
ngs 215| -1 -1 0 27 -40 -21 -.05 11 9 | -1074 -396 1022 2523
sio 304| 0 0 -2 -38 0 -30 -.15 13 13 | --- --- --- ---
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 3.1856.0 GPS week: 1856 Day: 0 MJD: 57236.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 12 8 13 8 15 3 5 7 8 11 3 | 25 27 30 26 31 24 26 22 26 21 24
2E | 16 9 8 10 20 5 10 11 13 12 4 | 28 33 28 37 30 31 33 26 35 30 30
3 | 8 6 15 9 11 4 7 9 8 14 3 | 26 30 22 25 28 23 30 23 25 26 24
4E | 16 14 12 11 13 4 12 16 15 15 5 | 51 53 47 45 49 45 44 49 47 49 47
5 | 10 12 16 12 15 4 12 13 10 11 4 | 36 39 38 30 28 34 39 22 26 33 31
6E | 11 9 15 7 15 5 8 9 10 9 3 | 20 23 26 21 24 21 22 19 23 18 20
7E | 15 11 7 13 15 4 11 11 12 11 4 | 54 49 48 53 51 50 51 51 51 52 50
X8 | 3 --- --- --- --- 65 --- --- --- --- 0 | 40 --- --- --- --- 26 --- --- --- --- 40
9 | 11 7 11 9 12 5 8 8 9 10 3 | 43 46 36 45 50 41 44 41 41 41 42
X10 | 10 16 13 12 12 6 7 7 11 --- 4 | 13 17 9 10 11 12 6 8 16 --- 9
11E | 11 9 10 10 12 3 8 12 8 11 3 | 25 28 22 26 32 23 27 20 26 26 24
12 | 13 11 9 12 21 7 9 28 9 13 5 | 35 32 27 31 30 27 29 31 27 24 26
13 | 11 11 16 11 13 5 9 10 13 13 4 | 28 34 23 37 37 28 33 32 35 34 31
14 | 12 11 13 13 16 4 9 13 11 20 4 | 31 29 27 36 35 29 29 33 36 26 30
15 | 11 12 15 15 15 4 13 14 11 21 5 | 44 41 37 48 41 40 42 40 43 45 40
16 | 12 14 10 20 17 4 16 15 9 19 5 | 26 24 18 33 23 19 22 21 20 17 19
17 | 10 13 14 17 14 4 9 12 13 12 4 | 20 21 15 28 22 18 21 15 20 12 17
18 | 13 19 11 17 15 6 13 25 12 15 5 | 27 29 24 34 34 26 30 39 34 28 28
19 | 12 12 10 15 15 3 12 11 12 14 4 | 25 27 18 21 23 18 27 16 19 13 18
20 | 10 14 14 14 15 6 11 13 11 14 4 | 36 38 32 47 46 37 40 44 42 37 39
21E | 11 11 8 11 13 3 10 10 9 9 3 | 23 29 21 29 27 24 26 24 29 22 25
22 | 9 15 13 14 16 3 13 13 10 12 4 | 36 37 33 44 45 36 40 42 41 33 38
23 | 9 10 12 12 14 4 10 10 8 17 4 | 27 29 21 25 27 22 28 22 24 26 23
24 | 15 11 14 10 17 7 8 15 9 10 4 | 23 23 26 23 23 22 20 21 22 17 20
25 | 10 14 16 7 17 6 9 12 8 12 4 | 20 29 24 21 25 20 24 21 20 23 21
26 | 7 10 14 16 15 3 10 15 8 12 4 | 19 23 23 23 20 19 23 16 19 21 19
27 | 12 11 12 7 14 3 8 14 8 15 4 | 26 28 26 22 24 22 26 18 24 29 23
28 | 8 13 14 14 16 5 12 12 13 16 4 | 20 25 16 29 28 20 21 21 26 20 20
29 | 12 13 12 12 22 4 13 17 12 14 5 | 30 30 25 26 20 24 30 20 24 19 23
30E | 15 15 14 8 14 4 10 10 11 9 4 | 29 30 31 26 24 26 28 24 29 23 26
31E | 13 11 10 13 16 4 9 11 12 11 4 | 27 31 22 33 28 26 29 23 28 24 26
32 | 9 9 11 8 16 4 8 12 6 14 3 | 26 30 22 28 32 25 28 27 28 28 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 13 12 16 4 10 14 11 14 |T 29 31 26 31 30 26 29 26 29 27 27
WRMS | 11 12 13 11 16 4 10 13 9 13 |NE 28 30 24 30 29 25 28 26 27 26 26
MEDI | 11 11 13 12 15 4 10 12 10 12 |MD 27 29 25 29 28 24 28 23 26 26 25
Table 3.1856.1 GPS week: 1856 Day: 1 MJD: 57237.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 12 8 13 6 12 4 6 7 11 14 3 | 24 25 28 25 29 23 24 19 23 20 22
2E | 16 11 8 10 16 6 9 12 11 11 4 | 27 30 24 32 29 27 30 26 31 29 27
3 | 7 6 14 6 12 4 8 9 8 12 3 | 21 26 17 22 24 20 27 18 22 22 20
4E | 15 15 11 11 11 5 13 13 16 14 4 | 37 44 37 35 42 35 38 36 40 37 37
5 | 9 13 17 9 14 4 12 13 15 11 4 | 26 31 30 25 26 25 31 20 23 25 24
6E | 12 12 15 7 14 5 9 9 8 10 3 | 20 21 24 23 23 18 21 19 21 20 19
7E | 19 15 8 12 14 5 11 12 11 11 4 | 53 54 50 55 50 50 53 47 52 47 50
X8 | 3 --- --- --- --- 78 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
9 | 8 9 12 8 9 4 7 8 5 9 3 | 28 33 25 31 35 28 33 30 33 30 30
X10 | 18 10 --- 13 14 14 --- 9 19 --- 6 | 14 10 --- 14 9 8 --- 6 17 --- 6
11E | 9 13 8 7 12 5 7 9 8 10 3 | 27 33 24 28 33 25 29 23 28 25 26
12 | 10 11 12 10 19 5 9 27 10 15 5 | 32 33 25 31 33 28 34 27 31 29 27
13 | 13 9 15 14 12 3 9 10 10 15 4 | 21 30 20 32 29 22 30 23 28 27 24
14 | 11 12 12 11 13 5 8 16 8 17 4 | 23 23 21 23 22 19 23 25 24 19 21
15 | 10 11 13 15 13 4 11 13 10 17 4 | 26 29 23 34 24 26 29 23 31 33 26
16 | 12 15 10 18 15 4 12 12 11 22 5 | 25 24 18 27 22 18 24 20 18 20 18
17 | 10 10 11 16 15 4 9 13 9 13 4 | 18 21 16 29 22 18 24 18 20 14 17
18 | 9 13 14 15 13 7 10 23 10 14 5 | 23 26 22 24 26 21 26 27 26 22 22
19 | 12 11 8 15 15 4 13 11 9 13 4 | 24 28 20 22 27 19 29 18 23 17 20
20 | 9 13 14 10 13 6 10 13 8 13 4 | 28 33 25 30 34 27 33 31 32 29 29
21E | 10 11 8 12 15 4 9 8 10 11 3 | 24 27 20 27 25 22 25 21 28 20 23
22 | 9 11 14 11 14 3 11 14 8 10 4 | 25 29 25 28 33 25 30 28 29 23 26
23 | 9 12 12 10 12 3 9 10 9 14 3 | 23 26 21 22 22 19 26 18 22 22 20
24 | 9 9 13 6 14 3 9 10 6 10 3 | 22 24 25 23 22 20 23 21 22 20 21
25 | 10 11 17 7 12 4 10 9 9 17 4 | 24 29 25 21 24 20 25 21 22 28 22
26 | 8 8 15 10 14 3 7 8 8 12 3 | 20 22 24 24 24 20 23 18 20 23 20
27 | 8 9 12 7 9 3 8 12 10 10 3 | 22 26 24 21 25 21 26 16 19 25 21
28 | 15 11 12 13 17 5 10 13 12 13 4 | 21 26 18 29 29 21 25 24 22 23 21
29 | 9 13 12 9 16 6 11 13 9 15 4 | 24 28 21 22 22 21 27 20 25 20 21
30E | 18 20 14 9 17 4 8 11 6 11 4 | 27 27 27 25 22 23 25 23 26 20 22
31E | 13 12 8 12 15 3 11 10 10 9 4 | 24 26 17 27 22 21 25 20 30 20 22
32 | 8 8 10 7 16 4 8 11 6 14 3 | 21 24 21 24 24 21 25 21 24 26 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 12 11 14 4 10 13 10 13 |T 24 28 23 26 26 22 28 22 26 24 23
WRMS | 10 12 12 10 14 4 10 12 8 12 |NE 23 26 22 25 25 21 27 21 24 23 21
MEDI | 10 11 12 10 14 4 9 11 9 13 |MD 24 27 24 25 25 21 26 21 24 23 22
Table 3.1856.2 GPS week: 1856 Day: 2 MJD: 57238.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 12 8 13 8 13 4 7 8 9 10 3 | 25 28 30 27 28 26 26 23 28 22 25
2E | 14 10 8 11 18 6 13 11 11 9 4 | 30 29 27 32 26 29 31 27 33 28 28
3 | 6 6 13 10 11 5 7 10 5 12 3 | 26 32 22 26 28 25 32 22 28 26 26
4E | 13 16 11 14 11 5 13 13 15 14 4 | 39 49 40 40 40 39 39 42 42 42 40
5 | 10 11 15 13 13 4 13 14 9 12 4 | 25 28 27 19 23 22 29 13 23 19 21
6E | 16 9 16 6 17 5 7 11 11 10 4 | 20 17 21 18 21 17 18 17 23 16 16
7 | 20 12 8 13 18 7 9 10 9 10 4 | 123 117 117 122 119 118 120 119 124 119 119
X8 | 2 --- --- --- --- 55 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
9 | 8 9 12 9 11 5 7 8 8 11 3 | 35 41 32 37 40 35 41 34 33 33 35
11E | 11 10 9 8 15 4 7 9 6 10 3 | 30 34 28 31 35 29 31 26 31 31 29
12 | 16 14 12 14 20 6 12 27 12 12 5 | 39 38 31 40 38 34 37 33 35 32 32
13 | 11 10 14 12 12 4 10 10 11 12 4 | 24 33 22 32 29 26 33 27 28 31 27
14 | 10 9 12 10 13 3 10 13 9 15 4 | 25 23 23 24 21 22 25 24 24 18 21
15 | 5 12 14 11 14 2 12 10 10 17 4 | 29 33 28 32 28 28 34 29 31 36 29
16 | 12 13 10 20 19 2 11 10 8 20 5 | 24 23 18 28 25 19 23 20 21 15 19
17 | 8 11 10 18 14 4 10 10 9 16 4 | 20 24 17 29 21 19 24 17 20 14 18
18 | 10 17 13 16 12 6 12 22 13 15 5 | 25 28 22 26 25 22 27 27 24 22 23
19 | 12 11 10 10 16 3 10 11 9 17 4 | 27 31 23 24 28 20 29 19 24 18 22
20 | 10 12 13 14 12 5 12 10 10 15 4 | 35 35 28 39 36 31 36 33 36 32 33
21E | 11 11 8 11 14 5 10 9 10 11 3 | 27 29 26 30 30 27 30 27 31 25 27
22 | 8 12 14 12 16 3 10 14 9 14 4 | 27 30 27 31 32 26 31 31 28 24 27
23 | 10 8 13 12 15 4 8 11 8 16 4 | 27 28 25 25 24 24 29 21 22 25 23
24 | 12 9 12 9 14 4 8 8 7 10 3 | 23 24 24 21 22 20 20 19 20 19 20
25 | 11 11 15 6 13 3 10 7 7 13 3 | 21 27 24 21 26 21 24 19 20 24 21
26 | 12 8 14 11 16 3 6 9 7 14 3 | 22 24 24 18 23 19 24 16 21 17 19
27 | 10 7 12 8 12 3 8 11 7 10 3 | 24 25 24 20 22 20 26 17 22 23 21
28 | 10 11 11 11 17 6 12 11 9 13 4 | 20 25 17 25 29 22 24 22 24 19 20
29 | 14 13 13 12 18 5 11 12 12 14 4 | 29 27 22 22 20 20 25 17 22 18 19
30E | 11 11 12 10 17 5 8 7 7 7 3 | 24 24 28 24 25 24 24 23 26 20 23
31E | 11 9 10 12 15 3 8 10 9 10 3 | 22 24 16 25 23 20 23 17 25 20 20
32 | 9 8 10 9 18 3 5 10 5 15 3 | 28 28 26 27 27 25 30 24 27 29 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 12 12 15 4 10 12 9 13 |T 29 31 27 30 30 27 31 26 29 27 27
WRMS | 11 11 12 10 14 4 10 11 8 13 |NE 26 28 24 26 27 23 28 23 25 23 23
MEDI | 11 11 12 11 14 4 10 10 9 12 |MD 25 28 24 26 26 24 29 23 25 23 23
Table 3.1856.3 GPS week: 1856 Day: 3 MJD: 57239.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 8 14 7 12 3 7 7 7 9 3 | 29 30 33 31 29 29 30 26 30 26 28
2E | 9 12 8 15 17 5 13 11 12 8 4 | 32 34 32 38 29 32 35 27 37 34 32
3 | 9 6 14 9 10 4 6 12 6 14 3 | 28 31 23 30 25 24 32 24 25 28 26
4E | 9 18 12 12 11 4 13 12 14 13 4 | 38 45 37 38 44 37 40 37 40 37 38
5 | 8 15 15 12 15 4 13 15 10 13 4 | 34 37 37 28 28 29 37 21 25 28 29
6E | 10 10 18 11 19 6 8 8 9 12 4 | 24 27 29 28 26 26 28 23 30 24 25
7 | 15 12 8 10 23 4 12 10 12 10 4 | 73 73 67 73 76 72 72 70 69 70 70
X8 | 1 --- --- --- --- 23 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
9 | 7 7 14 9 10 4 6 6 9 11 3 | 39 44 32 42 42 37 43 37 34 39 38
11E | 7 11 11 7 13 4 6 9 5 8 3 | 36 35 30 37 37 32 37 30 33 30 33
12 | 11 14 10 12 20 5 11 27 10 13 5 | 30 32 21 29 28 24 28 24 25 19 22
13 | 13 12 14 14 14 6 10 13 8 13 4 | 29 33 23 35 34 27 33 28 27 30 28
14 | 10 8 13 12 14 5 8 14 10 21 4 | 25 25 25 27 24 23 26 25 25 20 23
15 | 10 11 13 12 15 4 12 13 9 20 4 | 43 41 34 42 37 38 41 36 39 40 37
16 | 17 15 9 17 22 4 10 12 10 20 5 | 27 28 20 32 26 21 28 20 21 17 21
17 | 12 12 12 16 15 4 10 11 10 16 4 | 22 23 16 28 19 18 25 14 20 15 17
18 | 12 17 13 17 14 5 12 22 12 19 5 | 28 31 26 37 30 27 32 34 28 24 27
19 | 14 12 10 15 21 3 10 13 8 17 4 | 30 31 21 24 26 21 31 19 21 14 21
20 | 11 13 13 14 16 5 11 13 9 16 4 | 40 39 33 45 40 36 39 40 38 35 37
21E | 6 13 7 9 17 3 10 10 6 9 3 | 32 34 30 36 32 31 34 30 34 28 31
22 | 8 13 14 12 16 4 10 15 9 15 4 | 35 36 32 42 38 36 37 39 36 31 35
23 | 11 8 13 12 16 4 8 10 9 16 4 | 26 27 22 27 21 21 30 20 22 23 22
24 | 8 11 11 7 13 3 8 9 6 10 3 | 24 28 29 24 26 23 27 23 25 26 24
25 | 9 12 14 9 13 4 8 8 7 16 3 | 21 31 24 23 25 20 25 18 21 20 21
26 | 10 8 14 11 19 3 7 11 5 11 3 | 26 26 27 24 27 23 28 19 22 22 23
27 | 7 8 13 9 14 4 7 11 6 14 3 | 24 27 26 25 24 22 28 21 22 28 23
28 | 15 11 10 13 19 6 12 13 12 15 4 | 23 26 20 33 32 22 26 24 30 21 23
29 | 11 14 12 12 19 5 13 12 10 16 4 | 32 32 26 26 22 26 31 22 26 21 24
30E | 11 13 13 8 13 4 10 10 9 9 3 | 31 31 33 27 33 28 30 25 32 24 28
31E | 13 9 13 10 15 4 6 19 9 10 4 | 48 49 45 51 45 46 49 45 51 44 46
32 | 11 9 11 9 16 5 7 9 8 14 3 | 27 30 25 32 28 25 31 24 26 29 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 12 12 16 4 10 13 9 14 |T 31 33 29 33 31 29 33 28 30 28 29
WRMS | 11 12 12 10 15 4 10 11 8 13 |NE 29 31 25 31 28 25 31 25 26 25 26
MEDI | 10 12 13 12 15 4 10 11 9 13 |MD 29 31 27 31 28 26 31 24 27 26 26
Table 3.1856.4 GPS week: 1856 Day: 4 MJD: 57240.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 12 7 14 11 16 4 9 7 6 10 3 | 24 28 28 31 33 25 26 22 25 24 25
2E | 8 15 6 11 16 5 13 9 10 10 4 | 33 34 33 41 35 33 36 33 38 38 35
3 | 7 7 13 11 10 5 8 7 5 14 3 | 22 28 19 26 27 22 28 18 22 25 22
4E | 11 20 12 12 13 6 16 10 14 14 5 | 35 44 34 35 33 32 38 33 37 34 34
5 | 6 13 13 15 14 3 13 15 8 10 4 | 26 29 27 25 22 23 30 19 19 20 22
6E | 12 9 17 11 12 4 9 9 7 11 3 | 20 23 27 26 28 21 23 21 24 21 22
7 | 18 13 8 12 17 3 12 10 10 11 4 | 42 41 35 41 47 39 40 36 41 40 39
X8 | 15 --- --- --- --- 27 11 --- --- --- 13 | 9999 --- --- --- --- 9999 64 --- --- --- 9999
9 | 8 6 12 11 7 3 7 6 6 9 3 | 33 40 32 37 38 34 40 35 36 35 35
11E | 8 9 10 8 12 5 8 10 5 14 3 | 32 33 28 33 39 30 32 29 30 33 31
12 | 13 14 9 15 16 5 13 27 13 12 5 | 30 29 23 31 28 25 29 25 28 23 22
13 | 12 11 11 13 13 5 12 13 10 16 4 | 24 33 24 32 29 25 32 26 28 31 26
14 | 13 9 12 14 11 3 9 10 7 19 4 | 28 25 26 28 25 24 25 27 27 28 25
15 | 6 12 11 15 13 3 13 13 9 18 4 | 31 37 31 36 30 32 36 31 34 36 32
16 | 21 11 9 21 16 5 10 11 9 21 5 | 33 27 22 30 30 22 25 24 23 18 22
17 | 9 11 10 23 14 6 10 9 11 17 4 | 21 26 20 34 20 20 25 19 20 20 19
18 | 12 16 15 18 13 6 14 22 12 15 5 | 34 31 28 39 33 30 31 32 33 26 30
19 | 12 10 10 13 15 3 10 12 8 15 4 | 26 30 23 22 28 22 28 19 21 21 21
20 | 11 12 13 16 13 6 14 12 10 14 4 | 40 39 34 45 42 36 36 40 39 34 37
21E | 11 12 6 12 17 3 11 9 8 9 3 | 29 29 27 29 36 28 30 27 33 25 28
22 | 13 11 15 14 16 4 12 15 11 13 4 | 37 36 32 41 37 33 37 35 39 28 34
23 | 14 7 12 12 12 3 9 10 8 16 4 | 29 29 23 28 24 24 30 22 23 26 24
24 | 13 10 12 11 15 5 7 10 7 9 3 | 25 26 30 26 26 26 27 24 26 22 24
25 | 9 10 13 8 11 4 8 8 9 10 3 | 23 23 25 21 24 20 26 19 22 22 21
26 | 16 12 14 14 15 4 8 7 7 9 4 | 28 29 30 23 31 25 30 22 25 26 25
27 | 9 8 13 7 11 3 9 8 7 10 3 | 27 30 31 26 29 26 28 22 26 28 26
28 | 11 16 10 16 16 4 11 10 11 15 4 | 25 28 21 34 30 24 27 27 26 24 24
29 | 11 15 10 15 15 6 12 11 11 15 4 | 29 33 26 26 25 24 32 20 26 26 24
30E | 16 12 12 9 14 4 9 9 8 9 4 | 38 33 35 34 34 34 34 30 36 31 33
31 | 11 14 13 13 19 3 9 13 9 10 4 | 34 36 30 34 37 31 34 27 37 33 32
32 | 9 8 10 9 14 5 8 8 6 13 3 | 29 31 25 30 31 25 30 24 28 31 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 12 13 14 4 11 12 9 13 |T 29 31 27 31 31 27 31 26 29 27 27
WRMS | 12 12 12 12 13 4 11 10 8 13 |NE 28 30 26 30 29 25 31 25 27 26 25
MEDI | 11 11 12 12 14 4 10 10 8 13 |MD 29 30 27 31 30 25 30 25 27 26 25
Table 3.1856.5 GPS week: 1856 Day: 5 MJD: 57241.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 6 15 9 15 5 8 10 9 7 3 | 24 26 28 27 28 23 26 19 25 19 23
2E | 11 13 10 11 51 5 12 14 10 13 6 | 32 30 30 37 48 30 31 24 35 34 30
3 | 5 6 13 7 11 4 7 8 7 12 3 | 24 28 19 25 22 21 28 17 22 19 21
4E | 19 20 12 12 26 8 17 12 15 14 5 | 39 46 37 37 42 35 43 34 41 34 36
5 | 11 10 16 14 16 3 12 14 11 13 4 | 24 25 27 23 19 19 26 20 18 22 20
6E | 16 9 18 12 16 4 10 9 8 9 4 | 24 24 27 28 28 22 24 20 22 19 22
7 | 19 13 12 10 18 4 10 13 10 10 4 | 46 43 35 43 52 42 44 42 46 40 41
X8 | 16 --- --- --- --- 31 9 --- --- --- 12 | 9999 --- --- --- --- 9999 46 --- --- --- 9999
9 | 8 8 13 10 12 4 6 8 7 8 3 | 27 33 24 30 34 27 34 29 27 28 28
11E | 9 12 12 7 16 5 7 12 8 10 3 | 26 28 21 26 31 22 27 21 25 21 23
12 | 17 12 8 15 20 6 11 27 12 12 5 | 30 29 19 32 28 23 26 24 25 19 20
13 | 12 11 15 12 14 5 12 17 11 17 4 | 33 36 28 33 38 30 36 30 34 36 32
14 | 10 8 14 11 13 4 7 12 7 16 3 | 25 23 22 22 24 19 20 19 22 20 19
15 | 9 12 12 15 13 4 14 13 10 19 4 | 33 34 29 33 29 29 34 27 28 33 29
16 | 14 13 9 20 20 5 10 17 11 21 5 | 28 28 19 32 26 21 25 21 24 19 21
17 | 10 11 13 16 15 5 9 9 9 16 4 | 23 23 17 29 21 18 23 14 22 11 17
18 | 14 13 15 14 16 6 11 23 10 15 5 | 31 31 24 30 28 26 30 25 28 20 25
19 | 10 11 13 13 18 4 10 13 10 18 4 | 23 27 20 22 26 19 27 16 23 13 18
20 | 13 10 14 14 16 6 13 12 10 17 4 | 34 35 30 37 36 31 34 32 33 30 31
21E | 10 13 9 10 17 4 11 9 8 7 3 | 33 29 25 30 24 27 27 26 32 24 26
22 | 13 12 17 13 21 3 10 16 9 12 4 | 30 31 24 32 30 26 31 26 31 23 26
23 | 10 10 12 10 18 5 8 12 9 16 4 | 25 26 24 27 21 20 27 17 21 23 21
24 | 13 8 11 8 11 4 7 13 8 10 3 | 23 21 25 22 20 20 24 17 20 21 20
25 | 9 12 14 7 12 5 9 9 9 9 3 | 21 28 23 23 23 19 23 16 20 21 20
26 | 13 6 14 13 15 4 9 9 8 10 3 | 23 24 22 21 22 20 25 14 22 16 19
27 | 9 7 15 7 15 4 8 12 9 9 3 | 25 26 26 24 23 21 25 18 25 23 22
28 | 11 13 12 14 16 4 11 10 10 13 4 | 21 26 19 29 27 21 23 20 23 17 20
29 | 15 14 11 13 17 5 14 13 13 14 4 | 32 30 25 28 21 24 31 18 27 21 23
30E | 17 14 14 8 21 3 8 7 5 8 4 | 37 33 36 35 36 33 34 32 37 31 33
31 | 10 14 12 14 21 3 6 12 9 10 4 | 26 26 18 28 34 23 25 21 28 23 23
32 | 8 8 10 7 17 5 8 9 10 12 3 | 24 25 21 25 20 19 26 19 22 24 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 13 12 19 5 10 13 10 13 |T 28 29 24 29 28 24 29 22 26 23 24
WRMS | 12 11 13 11 16 4 10 12 9 12 |NE 26 28 23 27 25 22 28 20 24 21 22
MEDI | 11 11 13 12 16 4 10 12 9 12 |MD 26 28 24 28 27 22 27 20 25 21 22
Table 3.1856.6 GPS week: 1856 Day: 6 MJD: 57242.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 15 11 15 8 12 4 10 11 14 12 4 | 33 36 35 36 32 30 33 29 33 30 32
2E | 35 14 8 16 15 5 11 13 13 13 5 | 48 46 43 53 53 45 50 43 48 51 46
3 | 8 7 14 6 10 3 7 12 7 12 3 | 28 33 23 32 31 26 33 24 28 29 28
X4E | 29 25 9 9 18 7 --- 12 17 18 7 | 51 61 52 52 50 49 --- 53 50 58 51
5 | 10 10 16 10 12 5 13 15 16 14 4 | 32 34 35 27 26 28 34 20 24 24 26
6E | 38 13 19 14 16 5 14 17 14 7 6 | 36 27 28 30 23 22 28 23 28 21 23
7 | 18 13 9 9 17 4 10 10 9 11 4 | 51 47 39 49 53 46 48 45 51 43 46
X8 | 18 --- --- --- 14 31 11 --- --- --- 10 | 9999 --- --- --- 5 9999 51 --- --- --- 9999
9 | 7 9 13 9 13 3 9 7 8 9 3 | 46 50 39 45 52 43 47 45 42 46 44
11E | 8 15 11 8 19 4 8 13 11 11 4 | 33 37 29 35 37 30 30 28 31 27 30
12 | 15 16 9 14 17 5 13 27 12 10 5 | 31 31 20 32 25 24 27 25 25 19 21
13 | 11 11 13 14 11 4 13 9 12 15 4 | 30 38 25 39 38 29 37 29 32 34 32
14 | 13 10 11 12 12 5 9 11 9 15 4 | 32 31 29 34 34 29 29 29 33 27 29
15 | 10 12 13 18 11 4 13 12 15 16 5 | 43 44 38 45 40 39 42 38 41 40 39
16 | 12 13 11 16 16 4 11 14 11 18 5 | 32 32 24 37 36 27 29 29 29 23 27
17 | 13 14 10 16 12 6 10 13 10 17 4 | 29 33 23 36 26 24 30 21 26 20 24
18 | 15 15 15 15 17 7 13 21 12 14 5 | 39 39 32 43 44 35 38 39 40 31 36
19 | 11 13 13 12 16 4 9 11 12 19 4 | 28 34 23 25 30 22 31 20 23 20 23
20 | 14 15 14 12 17 5 13 12 12 16 5 | 47 46 38 52 50 43 44 47 46 38 44
21E | 11 13 8 9 20 5 10 15 8 8 4 | 32 41 32 38 34 34 36 34 38 31 34
22 | 12 12 16 11 18 4 10 14 11 12 4 | 41 44 37 50 52 41 45 45 48 36 43
23 | 8 10 14 9 12 4 8 13 8 14 3 | 29 31 26 29 25 25 30 24 24 27 25
24 | 13 10 11 9 13 5 9 8 9 12 3 | 31 28 31 28 27 26 30 21 28 23 26
25 | 12 13 14 8 13 5 9 8 8 13 3 | 24 30 25 27 26 23 23 18 25 25 22
26 | 10 11 14 10 15 5 8 8 8 9 3 | 26 30 26 26 29 23 27 19 23 23 23
27 | 10 8 15 7 14 4 9 8 11 9 3 | 36 35 33 30 30 28 33 24 31 31 30
28 | 12 11 12 12 17 4 11 10 10 11 4 | 30 35 26 39 38 31 34 33 32 27 31
29 | 13 14 12 12 16 6 14 12 9 13 4 | 40 40 34 33 28 31 39 24 32 28 31
30 | 18 17 15 6 12 4 9 7 8 8 4 | 40 40 43 38 37 39 37 36 37 38 37
31 | 13 15 10 12 22 4 9 13 8 11 4 | 41 41 33 43 44 38 39 32 41 35 37
32 | 9 10 12 7 19 4 7 12 9 13 4 | 28 32 25 32 37 26 32 27 27 29 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 12 13 12 15 5 11 13 11 13 |T 35 37 31 37 35 31 35 30 33 31 32
WRMS | 12 12 13 10 15 4 11 12 9 13 |NE 33 35 29 35 33 29 34 28 31 28 30
MEDI | 12 13 13 10 15 4 10 12 10 12 |MD 32 35 31 36 34 29 33 29 32 29 30
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 4.1856 GPS week: 1856 MJD: 57236.0-57242.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2973 |U 7 8 19 |U 5 7 23 |U 7 8 21 |
emr | emr 2901 | 8 9 22 |U 6 7 24 | 8 9 23 |
esa | esa 2893 | 8 8 22 |U 5 6 22 | 8 8 22 |
gfz | gfz 2901 |U 7 8 21 |U 5 7 23 |U 8 9 21 |
grg | grg 2730 |U 8 9 23 |U 6 8 27 | 9 9 26 |
igr | igr 2903 | 7 8 21 | 5 6 21 | 8 8 21 |
igs | igs 2904 | 7 8 21 | 5 7 22 | 8 8 21 |
jpl | jpl 2917 | 8 8 23 |U 6 7 25 |U 8 8 24 |
mit | mit 2907 | 8 8 21 |U 6 8 27 |U 8 9 21 |
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 5.1856.0 GPS week: 1856 Day: 0 MJD: 57236.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 5 5 14 | 4 5 21 | 6 7 18 |
emr | emr 2972 | 5 7 14 | 8 8 20 | 7 7 16 |
esa | esa 2976 | 4 5 12 | 5 6 18 | 6 7 17 |
gfz | gfz 2972 | 5 5 11 | 5 7 17 | 7 6 18 |
grg | grg 2139 | 5 5 14 | 5 9 23 | 8 9 32 |
igr | igr 2975 | 4 5 11 | 5 6 18 | 6 6 17 |
igs | igs 2974 | 5 5 11 | 5 7 17 | 6 7 17 |
jpl | jpl 2972 | 5 5 14 | 5 7 19 | 7 7 18 |
mit | mit 2976 | 6 7 12 | 6 7 18 | 7 9 16 |
Table 5.1856.1 GPS week: 1856 Day: 1 MJD: 57237.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2964 | 5 7 18 | 4 5 19 | 9 7 29 |
emr | emr 2960 | 7 6 21 | 6 6 24 | 11 8 33 |
esa | esa 2880 | 6 5 21 | 4 5 27 | 10 7 31 |
gfz | gfz 2960 | 5 6 20 | 5 5 22 | 10 7 29 |
grg | grg 2778 | 8 8 22 | 5 7 23 | 10 8 28 |
igr | igr 2959 | 5 6 19 | 4 5 21 | 10 6 29 |
igs | igs 2964 | 5 5 19 | 4 5 21 | 10 7 30 |
jpl | jpl 2876 | 6 6 22 | 5 6 26 | 10 6 33 |
mit | mit 2976 | 6 7 20 | 5 6 26 | 11 7 30 |
Table 5.1856.2 GPS week: 1856 Day: 2 MJD: 57238.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 9 9 24 | 5 6 28 | 6 8 20 |
emr | emr 2876 | 11 13 29 | 7 9 36 | 7 10 24 |
esa | esa 2880 | 10 11 28 | 6 7 34 | 7 8 23 |
gfz | gfz 2876 | 9 11 28 | 6 8 33 | 7 8 23 |
grg | grg 2880 | 9 11 29 | 7 9 35 | 8 10 33 |
igr | igr 2879 | 9 10 28 | 6 7 28 | 7 8 24 |
igs | igs 2876 | 9 11 28 | 6 8 32 | 7 9 23 |
jpl | jpl 2876 | 10 10 27 | 7 8 39 | 8 8 27 |
mit | mit 2880 | 9 8 26 | 6 9 37 | 8 11 24 |
Table 5.1856.3 GPS week: 1856 Day: 3 MJD: 57239.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 6 6 13 | 5 6 23 | 7 11 24 |
emr | emr 2876 | 7 6 14 | 5 8 19 | 8 11 24 |
esa | esa 2880 | 6 7 17 | 5 6 20 | 8 11 22 |
gfz | gfz 2877 | 6 6 15 | 5 8 21 | 8 12 26 |
grg | grg 2880 | 7 10 15 | 7 10 28 | 9 14 25 |
igr | igr 2879 | 6 7 14 | 5 7 20 | 8 12 21 |
igs | igs 2876 | 6 7 14 | 5 7 19 | 7 11 23 |
jpl | jpl 2876 | 7 8 17 | 5 8 22 | 8 10 25 |
mit | mit 2880 | 6 7 17 | 6 10 30 | 8 12 22 |
Table 5.1856.4 GPS week: 1856 Day: 4 MJD: 57240.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 8 5 16 | 4 7 21 | 7 5 18 |
emr | emr 2876 | 9 7 21 | 5 8 16 | 8 7 18 |
esa | esa 2880 | 9 6 19 | 5 7 13 | 7 6 16 |
gfz | gfz 2876 | 8 5 18 | 4 8 18 | 7 7 17 |
grg | grg 2880 | 8 7 19 | 5 8 21 | 8 7 19 |
igr | igr 2879 | 8 6 18 | 4 7 17 | 7 6 15 |
igs | igs 2876 | 8 6 18 | 4 7 14 | 7 5 15 |
jpl | jpl 2971 | 9 8 22 | 5 7 15 | 8 6 18 |
mit | mit 2880 | 8 7 18 | 5 9 23 | 8 6 18 |
Table 5.1856.5 GPS week: 1856 Day: 5 MJD: 57241.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 15 25 | 4 7 18 | 6 7 20 |
emr | emr 2876 | 12 15 31 | 5 6 24 | 7 9 22 |
esa | esa 2880 | 12 15 31 | 5 5 13 | 8 9 22 |
gfz | gfz 2876 | 12 15 31 | 4 7 19 | 7 8 18 |
grg | grg 2580 | 13 18 32 | 5 6 25 | 8 10 25 |
igr | igr 2879 | 11 15 29 | 5 6 14 | 7 9 18 |
igs | igs 2833 | 12 16 30 | 4 6 18 | 7 8 18 |
jpl | jpl 2972 | 12 15 34 | 5 5 21 | 8 10 23 |
mit | mit 2880 | 11 16 29 | 5 7 22 | 8 9 18 |
Table 5.1856.6 GPS week: 1856 Day: 6 MJD: 57242.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 23 | 7 11 31 | 9 9 20 |
emr | emr 2876 | 9 7 25 | 8 7 30 | 10 13 21 |
esa | esa 2880 | 8 7 27 | 8 7 27 | 10 10 22 |
gfz | gfz 2876 | 7 6 25 | 7 8 35 | 9 11 19 |
grg | grg 2976 | 7 7 27 | 8 8 35 | 9 8 19 |
igr | igr 2876 | 7 6 27 | 6 6 25 | 9 10 20 |
igs | igs 2932 | 8 6 25 | 7 7 30 | 10 11 20 |
jpl | jpl 2880 | 8 6 26 | 8 8 35 | 11 11 25 |
mit | mit 2880 | 8 6 25 | 9 8 36 | 8 8 18 |
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 6.1856 GPS week: 1856 MJD: 57236.500-57242.500
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 | -23 -9 81 -60 3 | 16 28
| 20 21 78 91 3 | 3
emr uuuuu | 64 -22 108 115 6 | 39 45
| 19 6 41 66 7 | 3
esa uuuuu | 3 17 -46 81 1 | 12 25
| 7 12 67 44 1 | 2
gfz uuuuu | -9 -9 29 50 -2 | 17 30
| 20 17 74 67 6 | 2
grg uuuuu | -34 13 -37 -250 9 | 51 57
| 22 25 84 154 5 | 5
igr xxxxx | 15 37 6 -15 1 | -2 22
| 13 11 49 11 3 | 2
irf xxxxx | 20 -5 -76 -13 0 | -2 23
| 6 9 35 15 5 | 3
jpl uuuuu | -29 28 51 9 -4 | 31 38
| 19 26 54 50 9 | 2
mit uuuuu | -12 1 -131 -83 -1 | 25 33
| 18 20 80 90 5 | 2
ngs uuuuu | 21 -23 5 8 -4 | 14 26
| 19 26 88 65 5 | 2
sio uuuux | 7 20 -122 54 -8 | 78 80
| 14 27 42 64 5 | 3
Table 7.1856.0 GPS week: 1856 Day: 0 MJD: 57236.500
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 -15 -19 -9 4 | 13 29
emr uuuuu | 59 -24 151 97 -3 | 36 44
esa uuuuu | 7 -1 -166 140 1 | 8 27
gfz uuuuu | -14 -33 156 142 -4 | 15 32
grg uuuuu | -52 -11 103 -468 6 | 45 53
igr xxxxx | 23 54 18 -11 -2 | -4 25
irf xxxxx | 14 -24 -26 15 7 | -6 25
jpl uuuuu | -15 43 86 -42 -13 | 29 37
mit uuuuu | 8 -22 -56 56 4 | 23 32
ngs uuuuu | 13 0 -141 -51 2 | 13 28
sio uuuux | -6 55 -116 16 -7 | 80 83
Table 7.1856.1 GPS week: 1856 Day: 1 MJD: 57237.500
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 19 70 -89 -1 | 18 30
emr uuuuu | 77 -29 102 111 5 | 38 46
esa uuuuu | 6 17 -40 70 0 | 13 27
gfz uuuuu | -26 -12 46 47 -4 | 18 33
grg uuuuu | -62 -5 61 -364 8 | 50 56
igr xxxxx | 16 31 11 -12 2 | -1 23
irf xxxxx | 19 3 -72 -15 4 | -2 24
jpl uuuuu | -4 2 90 39 4 | 32 38
mit uuuuu | -16 11 -135 -69 2 | 26 35
ngs uuuuu | 23 -24 -69 138 -4 | 16 29
sio uuuux | -14 42 -179 -51 -10 | 82 84
Table 7.1856.2 GPS week: 1856 Day: 2 MJD: 57238.500
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 | -17 0 130 72 0 | 13 26
emr uuuuu | 84 -24 105 137 15 | 35 42
esa uuuuu | 4 24 -17 138 2 | 9 24
gfz uuuuu | -33 15 -5 -21 -9 | 15 31
grg uuuuu | -54 44 -81 -365 12 | 47 53
igr xxxxx | 10 29 98 -7 -3 | -4 23
irf xxxxx | 14 1 -98 -20 5 | -5 24
jpl uuuuu | -25 33 80 -42 -8 | 30 36
mit uuuuu | 7 -23 -189 -44 2 | 23 32
ngs uuuuu | -9 -40 21 -42 -1 | 13 27
sio uuuux | 30 5 -137 85 -7 | 76 79
Table 7.1856.3 GPS week: 1856 Day: 3 MJD: 57239.500
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 | 7 1 -8 -44 6 | 15 25
emr uuuuu | 29 -15 155 43 14 | 39 43
esa uuuuu | -3 37 -50 19 1 | 12 22
gfz uuuuu | 28 -2 25 33 -4 | 17 29
grg uuuuu | -5 2 -71 -208 10 | 50 55
igr xxxxx | 23 31 -37 -36 1 | -2 20
irf xxxxx | 30 -1 -123 -7 -4 | -2 20
jpl uuuuu | -64 24 80 7 8 | 31 36
mit uuuuu | 7 2 -221 -72 -5 | 25 31
ngs uuuuu | 5 -55 89 39 -11 | 15 25
sio uuuux | 14 43 -148 102 -3 | 77 79
Table 7.1856.4 GPS week: 1856 Day: 4 MJD: 57240.500
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 | -28 -46 197 -2 6 | 20 29
emr uuuuu | 59 -14 89 80 6 | 43 49
esa uuuuu | -4 12 57 76 1 | 16 25
gfz uuuuu | -2 1 73 110 -5 | 22 32
grg uuuuu | -17 -11 -62 -189 4 | 57 61
igr xxxxx | 32 50 10 -26 2 | 2 22
irf xxxxx | 20 2 -99 -27 -3 | 2 20
jpl uuuuu | -33 76 7 15 0 | 35 41
mit uuuuu | -25 35 -200 -179 0 | 29 35
ngs uuuuu | 31 -51 -24 -17 -4 | 18 27
sio uuuux | 5 15 -141 132 -1 | 80 82
Table 7.1856.5 GPS week: 1856 Day: 5 MJD: 57241.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -46 2 66 -169 4 | 16 28
emr uuuuu | 59 -26 35 88 0 | 39 46
esa uuuuu | -6 12 -30 57 4 | 10 24
gfz uuuuu | 1 0 -72 80 3 | 15 29
grg uuuuu | -19 44 -110 -33 19 | 52 56
igr xxxxx | 10 27 -5 -10 6 | -4 22
irf xxxxx | 26 -3 -82 -28 -2 | -2 23
jpl uuuuu | -31 0 68 101 0 | 30 38
mit uuuuu | -31 8 -115 -216 -7 | 24 33
ngs uuuuu | 33 -3 105 12 -9 | 13 25
sio uuuux | 12 -14 -79 12 -15 | 74 78
Table 7.1856.6 GPS week: 1856 Day: 6 MJD: 57242.500
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 | -50 -20 130 -178 0 | 19 28
emr uuuuu | 78 -18 120 249 7 | 42 48
esa uuuuu | 13 22 -79 65 -1 | 13 24
gfz uuuuu | -21 -28 -22 -42 8 | 18 29
grg uuuuu | -31 32 -104 -124 4 | 57 60
igr xxxxx | -8 39 -54 -4 3 | -2 20
irf xxxxx | 19 -10 -37 -11 -4 | 0 21
jpl uuuuu | -32 18 -54 -13 -16 | 31 39
mit uuuuu | -32 -6 -2 -58 -6 | 26 33
ngs uuuuu | 48 10 51 -25 2 | 13 25
sio uuuux | 10 -4 -57 84 -11 | 74 78
More information about the IGSREPORT
mailing list