[IGSREPORT-22866] Wk 1798 IGS Final Orbits [Resubmission]
IGS ACC
igs.acc at noaa.gov
Sun Jul 13 03:27:48 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1798 (Jun 22, 2014 - Jun 28, 2014)
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:
igs1798[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1798[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1798[0-6].cls IGS GPS clock combination summary report.
igs17987.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17987.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 | 3 TSKB
0 | EMR | WUHN
0 | ESA | 3 NTUS NTUS UNSA
0 | GFZ | 1 2 6 30 1 6 30 IRKJ MCIL TSKB WUHN IRKJ
0 | GRG | 6 6 KOUC LPGS NRMD KOUC LPGS MCIL NRMD NTUS SOFI
0 | MIT | IRKJ IRKJ MDVJ
1 | COD | 3 CAS1 CAS1 WES2
1 | EMR | WES2 PRDS WES2 WUHN
1 | ESA | 3 WES2 MAL2 TIXI UNSA WES2
1 | GFZ | 1 2 6 30 1 6 30 GRAZ WES2 WUHN GRAZ
1 | GRG | 6 6 FAA1 LPGS NRMD RBAY FAA1 KOUC LPGS NRMD RBAY
1 | GRG | WUHN YIBL
1 | MIT | 9 MDVJ
2 | COD | 3 9
2 | EMR | WUHN
2 | ESA | 3 NTUS
2 | GFZ | 1 6 30 1 6 30 WUHN YELL YIBL WUHN YIBL
2 | GRG | 6 6 KELY LPGS REUN LPGS REUN
2 | JPL | 3 7
2 | MIT | 3 9 3 9
3 | COD | 3 3 ARTU
3 | EMR | YEBE
3 | ESA | 3 3 WTZR ARTU UNSA WTZR
3 | GFZ | 1 2 3 6 30 1 3 6 30 ARTU INVK IRKJ JPLM NRMD SOFI
3 | GFZ | INVK NRMD SOFI
3 | GRG | 6 6 ARTU GRAZ KOUC REYK GRAZ KOUC MAL2 REYK
3 | MIT | 9 9 IRKJ
4 | COD | 3
4 | ESA | 3 UNSA
4 | GFZ | 1 2 3 6 30 1 6 30 IRKJ MAL2 MCIL NYA1 YELL MCIL NYA1
4 | GFZ | RBAY
4 | GRG | 3 6 6 MAL2 NRMD BOR1 IRKJ NRMD TNML WUHN
4 | MIT | 6 9 6 9
5 | COD | 3 REUN REUN
5 | EMR | 3
5 | ESA | 3 21 UNSA
5 | GFZ | 1 2 3 6 30 1 3 6 30 THTI WUHN THTI WUHN
5 | GRG | 3 6 6 21 KELY WUHN KELY SOFI WUHN
5 | JPL | 21
5 | MIT | 3 6 9 9 21 ONSA FLIN MDVJ ONSA
6 | COD | 3 3
6 | EMR | 3 WUHN WUHN
6 | ESA | 3 3 UNSA
6 | GFZ | 1 2 6 30 1 6 30 IRKJ NRMD
6 | GRG | 6 6 FAA1 MAL2 WUHN ADIS FAA1 MAL2 WUHN
6 | MIT | 6 9 6 9 BAKO MDVJ MORP
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 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 | GRG | 6
1 | GRG | 6
2 | GRG | 6
3 | GRG | 6
4 | GRG | 6
5 | GRG | 6
6 | GRG | 6
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.5 .2 -.6 -39 17 -51 .29
EMR | 0 | 9.7 -1.5 14.4 -2 18 -48 .08
ESA | 0 | -.4 .3 -1.4 -1 -15 25 .07
GFZ | 0 | -.1 .4 -1.5 -20 -40 -23 -.20
GRG | 0 | 15.9 -13.4 19.3 -6 25 -10 .71
JPL | 0 | 7.6 2.7 12.8 -33 38 -25 .06
MIT | 0 | 3.9 -6.9 18.0 4 4 -40 .42
NGS | 0 | 3.8 -10.1 27.1 -119 -68 -21 .54
SIO | 0 | 5.0 .3 18.3 0 17 -20 .20
COD | 1 | -.4 .7 -.8 -34 23 -62 .24
EMR | 1 | 11.0 2.8 8.2 -10 19 -71 .14
ESA | 1 | -.6 .1 -1.7 -4 -26 26 .08
GFZ | 1 | -.1 .4 -1.9 -14 -29 -38 -.12
GRG | 1 | 17.5 -16.7 26.9 1 19 2 .58
JPL | 1 | 6.8 2.5 13.3 -34 24 0 -.07
MIT | 1 | 6.5 -5.4 16.3 7 3 -33 .33
NGS | 1 | 9.9 -7.0 26.6 -90 -104 30 .53
SIO | 1 | 5.2 -1.7 15.4 -2 11 -21 .28
COD | 2 | -.7 .6 -.8 -36 30 -49 .23
EMR | 2 | 5.0 -7.0 13.2 -14 15 -50 -.0
ESA | 2 | -.6 .8 -1.5 -5 -9 25 -.05
GFZ | 2 | .3 .1 -1.7 -12 -30 -22 .15
GRG | 2 | 13.2 -13.4 19.4 -2 15 -9 .74
JPL | 2 | 6.9 .9 12.1 -6 37 39 -.24
MIT | 2 | 1.9 -11.8 18.8 3 3 -47 .27
NGS | 2 | -5.4 -9.8 20.5 -103 -10 -58 .50
SIO | 2 | 2.7 -6.8 15.0 -3 6 -13 .29
COD | 3 | -.8 .1 -.9 -44 22 -40 .34
EMR | 3 | 4.4 -5.9 15.0 4 28 -60 .10
ESA | 3 | -.3 .1 -1.7 2 -3 26 .03
GFZ | 3 | -.1 .4 -1.6 -11 -22 -23 .05
GRG | 3 | 10.2 -16.2 19.3 -11 34 -32 .57
JPL | 3 | -2.2 -3.8 12.8 -69 -11 10 -.23
MIT | 3 | .1 -13.5 15.3 14 1 -47 .34
NGS | 3 | 6.6 -11.1 14.6 -56 -39 10 .61
SIO | 3 | -.7 -7.0 17.1 8 19 -28 .28
COD | 4 | -1.3 -.3 .2 -67 17 -27 .14
EMR | 4 | 2.0 -7.2 10.9 -7 6 -38 .16
ESA | 4 | -.2 .6 -1.0 -6 -11 31 -.14
GFZ | 4 | .5 1.0 -1.2 -13 -31 -13 -.10
GRG | 4 | 7.5 -23.3 22.5 -18 16 -15 .59
JPL | 4 | .2 -2.4 15.8 -41 -43 40 -.70
MIT | 4 | 1.1 -9.7 16.4 7 8 -48 .39
NGS | 4 | -1.8 -5.6 23.2 -89 -39 -28 .56
SIO | 4 | .8 -4.3 20.9 -14 21 -31 .26
COD | 5 | -1.6 .2 -.7 -29 29 -29 .25
EMR | 5 | 10.0 -8.1 3.1 -5 12 -67 .20
ESA | 5 | .0 .9 -1.3 -10 -14 11 -.08
GFZ | 5 | -.1 1.0 -1.9 -9 -25 -40 .22
GRG | 5 | 17.5 -20.1 27.1 -31 15 -49 .43
JPL | 5 | 5.2 -7.6 17.2 -59 75 -17 -.33
MIT | 5 | 6.2 -12.4 14.7 14 -4 -40 .48
NGS | 5 | 4.9 -10.4 17.6 -88 -26 3 .63
SIO | 5 | 4.5 -5.9 21.5 -16 17 -37 .24
COD | 6 | -.8 .6 -.5 -30 27 -12 .22
EMR | 6 | 8.5 -5.5 9.7 3 8 -61 .13
ESA | 6 | -.3 .8 -1.7 -2 -5 11 -.06
GFZ | 6 | .2 .8 -1.7 -10 -31 -14 -.18
GRG | 6 | 15.3 -16.2 31.3 -33 16 -64 .73
JPL | 6 | 3.6 -4.2 15.9 -65 54 -20 -.35
MIT | 6 | -.3 -10.6 16.2 7 -5 -42 .39
NGS | 6 | 5.6 -5.9 20.0 -77 -51 6 .53
SIO | 6 | 3.7 -6.9 18.1 -30 15 -22 .32
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1798.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1798.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 2.1798.[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 3.1798.[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 5.1798.0-6). 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 1798 summary. (Jun 22, 2014 - Jun 28, 2014)
Table 1.1798.a GPS week: 1798 MJD: 56830.000-56836.000
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| -1 0 -1 9 -2 -1 .04 9 9 | -1560 793 15 99
| 0 0 2 16 16 6 .02 | 301 457
emr 79| 1 -3 0 -20 -22 32 .18 12 12 | 2584 293 16 123
| 1 0 1 15 15 17 .03 | 1077 1502
esa 150| 0 0 -7 0 6 -6 -.37 12 12 | 274 -1170 10 153
| 0 0 1 12 9 10 .03 | 1133 1213
gfz 195| 0 1 0 0 -6 -19 .00 11 10 | -263 288 14 150
| 0 0 1 17 17 8 .04 | 373 970
grg 184| 3 0 11 23 -35 -6 .25 15 14 | -273 221 17 146
| 0 1 3 10 18 15 .05 | 198 783
igr n/a| 0 0 -3 6 -4 4 -.22 5 5 | -334 181 16 90
| 0 0 1 22 3 10 .02 | 1043 1367
jpl 80| 0 0 -6 -10 5 25 -.04 13 12 | 1996 432 18 134
| 1 0 1 30 18 18 .02 | 1056 1435
mit 300| 0 -1 3 1 -16 -3 -.04 12 11 | -387 257 19 200
| 1 0 1 18 15 15 .01 | 680 1141
ngs 231| 0 0 5 5 45 -19 .04 10 9 | -1211 498 1599 3296
| 1 0 3 20 24 15 .04 | 453 736
sio 480| 0 2 -2 -20 -22 -5 -.83 16 15 | --- --- --- ---
| 1 0 2 14 21 29 .04 | --- ---
Table 1.1798.b GPS week : 1798 MJD: 56830.000-56836.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 5 4 |
2 | 5 5 5 5 5 5 5 |
3 | 6 6 6 7 6 7 6 |
4 | 4 4 4 4 4 5 4 |
5 | 4 4 4 4 4 4 4 |
6 | 8 7 7 7 7 8 7 |
7 | 5 4 4 5 4 5 5 |
8 | 4 3 3 3 3 4 4 |
9 | 13 11 12 8 8 19 14 |
10 | 4 3 3 4 4 4 4 |
11 | 5 5 4 4 5 4 5 |
12 | 5 5 5 5 5 5 5 |
13 | 5 4 4 5 4 5 5 |
14 | 4 4 4 5 5 4 4 |
15 | 6 5 6 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 5 5 4 5 5 5 5 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 4 5 5 5 5 7 5 |
22 | 4 4 4 4 5 4 4 |
23 | 4 4 4 5 4 5 4 |
24 | 5 4 5 4 5 5 5 |
25 | 4 4 4 4 4 5 4 |
26 | 5 4 3 4 4 4 4 |
27 | 5 4 4 5 4 5 5 |
28 | 5 4 4 4 4 5 5 |
29 | 5 5 6 6 5 5 5 |
30 | 5 5 4 7 4 4 5 |
31 | 4 4 5 5 5 5 5 |
32 | 4 3 4 3 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 2.1798.0 GPS week: 1798 Day: 0 MJD: 56830.000
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| -1 0 -4 0 -11 -11 .06 9 9 | -2038 1244 19 99
emr 80| 2 -2 0 0 -31 40 .22 13 13 | 2182 874 14 101
esa 150| 2 0 -7 -8 -7 -9 -.40 11 11 | -249 -216 11 133
gfz 190| -1 1 0 -14 -42 -27 -.04 11 11 | -523 870 20 180
grg 184| 3 0 6 21 2 -14 .30 13 13 | -370 414 15 152
igr n/a| -1 0 -4 28 -8 0 -.23 6 5 | -160 558 19 99
jpl 80| -2 0 -6 29 17 37 -.01 13 12 | 1154 1071 18 115
mit 300| -1 0 1 17 1 -10 -.05 12 11 | -76 152 19 191
ngs 234| 0 0 8 -22 68 -12 -.01 11 9 | -2011 1212 1394 3558
sio 480| 0 3 -4 -9 -22 -8 -.85 15 14 | --- --- --- ---
Table 2.1798.1 GPS week: 1798 Day: 1 MJD: 56831.000
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 248| -2 1 -3 21 -12 0 .05 9 9 | -1817 1030 14 96
emr 80| 4 -2 -1 -18 -15 14 .20 13 13 | 2157 1358 15 114
esa 150| 0 0 -9 -7 -1 -5 -.36 11 11 | 1508 -3294 10 143
gfz 198| 0 0 -2 -11 1 -21 .01 11 10 | -273 242 13 138
grg 186| 2 0 12 24 -40 15 .30 14 14 | -438 351 16 144
igr n/a| 0 0 -4 18 -1 10 -.20 5 5 | -384 1018 16 79
jpl 80| 0 0 -7 4 26 3 -.00 14 12 | 1395 1534 17 114
mit 300| -1 0 2 -12 -33 22 -.04 10 9 | -1610 1969 18 197
ngs 237| 1 0 10 12 54 -24 .03 10 8 | -948 -110 1416 2812
sio 485| 0 1 -2 -32 -42 21 -.85 15 15 | --- --- --- ---
Table 2.1798.2 GPS week: 1798 Day: 2 MJD: 56832.000
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| -2 0 0 15 -23 -7 .05 9 8 | -1299 833 17 109
emr 80| 2 -1 1 -41 -12 4 .21 13 13 | 2932 1963 16 131
esa 150| 2 0 -8 7 9 7 -.40 13 13 | 1099 -1113 12 173
gfz 198| 0 2 -2 -8 -5 -7 -.05 11 10 | -432 1650 12 130
grg 187| 4 0 8 32 -50 -2 .29 15 14 | -458 1231 17 145
igr n/a| 0 1 -2 21 -3 20 -.22 5 5 | 31 1812 15 90
jpl 80| -2 0 -5 24 2 23 -.06 13 12 | 2440 2066 18 135
mit 300| 0 0 5 12 -13 -11 -.05 11 10 | 99 -84 19 202
ngs 233| 0 0 1 -21 60 3 .01 9 8 | -1461 1524 1695 3502
sio 489| 0 2 -1 -3 -38 7 -.87 16 13 | --- --- --- ---
Table 2.1798.3 GPS week: 1798 Day: 3 MJD: 56833.000
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 243| -2 1 0 28 2 1 .06 10 10 | -1332 1344 16 92
emr 80| 1 -3 0 -38 -1 35 .15 12 12 | 4005 1324 16 122
esa 150| 0 0 -7 7 12 3 -.34 11 11 | 1522 -1919 11 152
gfz 193| -1 2 0 -16 14 -17 .03 11 11 | 385 562 14 168
grg 185| 3 0 6 41 -56 11 .27 14 13 | -351 1059 18 137
igr n/a| -1 1 0 7 -6 11 -.19 6 6 | 956 1122 17 98
jpl 80| 1 0 -5 -32 3 31 -.05 13 11 | 3521 1179 18 126
mit 300| -1 -2 3 -7 -34 -22 -.07 12 11 | -470 1250 19 202
ngs 232| 1 1 2 18 22 -37 .03 10 9 | -706 517 1829 4011
sio 481| -1 2 1 -10 -44 -34 -.81 16 14 | --- --- --- ---
Table 2.1798.4 GPS week: 1798 Day: 4 MJD: 56834.000
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 243| 0 0 0 -20 5 0 .04 10 9 | -1358 604 14 93
emr 80| 0 -3 -1 -22 -47 30 .15 12 12 | 3679 -1694 18 129
esa 150| 0 0 -7 9 0 -3 -.34 11 11 | -1497 510 11 157
gfz 196| 0 2 0 3 -10 -17 .02 11 10 | -620 579 13 133
grg 186| 2 0 13 17 -37 -7 .22 17 16 | -56 -273 18 149
igr n/a| -1 0 -3 14 2 -1 -.20 5 5 | 449 -1672 16 87
jpl 80| 1 1 -6 -17 -31 49 -.07 13 11 | 3096 -1532 17 129
mit 300| 0 -1 3 0 4 -13 -.03 12 11 | 60 -1377 20 185
ngs 231| -1 0 4 30 71 -31 .09 10 9 | -896 762 1549 3451
sio 477| 1 2 -4 -20 12 -22 -.76 15 15 | --- --- --- ---
Table 2.1798.5 GPS week: 1798 Day: 5 MJD: 56835.000
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| -1 0 0 15 28 9 .02 11 11 | -1751 427 18 114
emr 79| 2 -4 -2 -13 -32 45 .18 12 12 | 2353 -1750 18 129
esa 150| 1 0 -6 -22 14 -19 -.41 14 12 | -358 -1126 10 156
gfz 198| -1 2 0 15 0 -31 .04 12 11 | 112 -1310 15 158
grg 181| 2 1 15 12 -30 -19 .20 16 15 | 62 -980 19 156
igr n/a| 0 1 -3 -35 -7 3 -.25 6 6 | -988 -1660 16 83
jpl 80| 0 0 -9 -49 17 38 -.02 14 13 | 1725 -1465 20 151
mit 300| 1 -2 2 25 -21 0 -.02 12 11 | -968 620 22 233
ngs 227| 0 1 1 17 5 -29 .06 10 9 | -996 -565 1775 3048
sio 471| 0 1 -5 -19 -6 -38 -.79 16 14 | --- --- --- ---
Table 2.1798.6 GPS week: 1798 Day: 6 MJD: 56836.000
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 -2 3 -3 -2 .01 8 8 | -1327 70 13 94
emr 79| 0 -4 -1 -7 -19 54 .16 12 12 | 786 -19 18 138
esa 150| 0 0 -9 9 18 -17 -.36 11 11 | -107 -1032 11 159
gfz 197| -1 2 0 30 -5 -12 .03 12 11 | -490 -575 13 146
grg 182| 2 1 13 16 -35 -25 .19 15 14 | -304 -253 18 143
igr n/a| 0 0 -3 -10 -7 -11 -.25 5 5 | -2247 94 15 94
jpl 80| -3 0 -7 -34 4 -2 -.04 14 13 | 646 176 20 168
mit 300| 0 -1 4 -26 -20 10 -.03 13 12 | 253 -728 20 194
ngs 229| 1 1 7 5 38 -1 .09 9 8 | -1460 151 1539 2696
sio 478| 0 2 -2 -43 -15 39 -.85 16 16 | --- --- --- ---
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 3.1798.0 GPS week: 1798 Day: 0 MJD: 56830.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 12 11 6 4 12 8 10 12 3 | 20 27 17 25 29 18 28 21 20 17 21
2 | 10 15 15 10 16 5 10 13 10 15 4 | 23 34 23 26 29 24 27 34 30 27 26
3E | 11 18 13 8 15 7 18 18 21 14 6 | 63 71 64 63 65 65 69 73 67 66 66
4 | 8 7 12 7 8 6 7 16 10 11 3 | 24 28 24 29 31 23 26 34 30 33 27
5 | 10 12 12 9 11 5 11 8 9 21 4 | 35 40 36 33 35 33 39 34 34 36 34
X6 | 17 --- 14 14 84 10 --- 14 13 32 7 | 55 --- 53 55 70 54 --- 56 53 52 54
7 | 10 12 12 11 15 7 13 13 9 13 4 | 22 27 14 24 30 16 21 23 19 16 19
8 | 8 9 13 8 11 3 10 7 8 20 3 | 20 24 19 16 17 15 16 16 17 22 16
X9 | 10 --- 15 --- --- 19 --- --- --- --- 12 | 54 --- 33 --- --- 59 --- --- --- --- 56
10 | 8 8 11 7 13 4 7 9 7 11 3 | 24 27 18 23 32 23 21 26 26 25 23
11 | 13 9 15 13 15 4 9 9 8 10 4 | 40 48 38 48 55 41 44 44 43 37 43
12 | 10 14 9 12 17 6 17 11 12 14 5 | 23 28 20 25 27 19 24 24 25 21 21
13E | 10 11 9 8 12 6 11 21 9 12 4 | 44 43 38 41 47 42 42 47 47 38 41
14 | 8 11 6 13 18 5 12 10 11 14 4 | 20 19 12 21 30 15 19 16 24 16 16
15 | 8 22 9 14 17 6 19 16 10 25 5 | 26 33 23 27 31 22 30 22 23 36 23
16 | 9 17 11 16 12 6 13 11 14 19 5 | 23 25 17 21 23 16 20 19 25 17 18
17E | 9 13 8 12 13 5 20 11 11 9 4 | 35 34 27 37 35 31 31 35 33 28 32
18 | 7 11 10 14 12 5 11 16 9 20 4 | 17 26 21 22 23 17 23 21 22 20 18
19E | 9 12 7 10 13 4 11 9 9 9 3 | 20 23 16 20 24 16 17 18 21 13 17
20 | 11 9 12 9 9 7 10 14 11 19 4 | 24 22 20 22 20 20 19 18 22 17 18
21 | 8 14 13 7 11 6 13 10 12 21 4 | 32 37 29 33 38 30 33 34 37 28 32
22 | 7 8 11 9 11 4 9 9 9 10 3 | 23 28 23 26 28 22 23 22 27 22 23
23 | 10 10 10 10 14 5 14 7 9 17 4 | 20 21 17 15 25 16 21 17 20 20 16
24 | 13 15 13 8 12 7 16 10 12 14 4 | 23 30 24 22 23 17 23 21 20 23 21
25 | 8 13 13 9 16 6 13 8 10 11 4 | 22 26 26 23 25 19 24 21 21 20 21
26E | 12 12 14 11 12 6 13 15 8 13 4 | 29 35 29 31 26 26 30 23 28 26 27
X27E | 10 12 15 11 --- 5 11 9 6 9 4 | 23 22 28 23 --- 17 22 22 22 16 22
28 | 8 12 12 12 17 6 14 10 10 16 4 | 23 27 17 22 29 15 21 20 20 18 19
29E | 11 15 9 12 15 5 25 10 12 13 5 | 24 26 17 28 27 20 27 23 30 20 22
X30 | 10 10 13 9 --- 8 12 23 7 11 5 | 26 29 30 25 --- 23 31 24 29 25 26
31 | 9 11 10 13 17 7 11 7 11 11 4 | 25 25 14 24 33 18 20 17 20 12 19
32 | 8 7 10 12 6 6 7 11 8 15 3 | 22 21 18 18 21 16 21 19 23 17 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 11 13 6 13 12 11 15 |T 28 30 25 28 32 25 27 27 28 25 26
WRMS | 9 13 11 11 13 5 12 11 9 14 |NE 26 28 23 26 30 23 24 25 26 24 25
MEDI | 9 12 12 11 13 6 12 10 10 14 |MD 23 27 23 25 29 20 23 22 25 22 22
Table 3.1798.1 GPS week: 1798 Day: 1 MJD: 56831.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 8 13 11 9 6 12 10 11 10 4 | 20 24 16 21 27 15 26 18 23 14 18
2 | 8 14 13 11 16 4 12 13 7 14 4 | 14 25 19 17 24 14 23 21 19 16 17
3E | 10 22 11 9 17 9 18 13 18 14 5 | 66 72 64 63 65 64 69 63 66 68 64
4 | 7 10 11 9 8 4 7 12 8 12 3 | 18 21 19 21 22 18 19 25 21 28 20
5 | 9 12 11 8 10 5 13 9 8 25 3 | 26 30 22 19 25 20 26 21 26 22 22
X6 | 14 --- 12 14 83 9 --- 14 11 31 6 | 39 --- 38 35 49 32 --- 37 38 38 36
7 | 9 12 11 11 16 5 14 11 10 14 4 | 21 26 15 23 30 15 20 22 24 15 18
8 | 6 8 9 7 11 3 9 6 7 20 3 | 18 22 17 16 17 14 16 14 18 21 15
X9 | 25 14 12 --- --- 14 --- 15 30 --- 10 | 72 40 34 --- --- 64 --- 46 45 --- 66
10 | 6 10 10 7 14 3 9 7 6 11 3 | 16 18 13 14 21 13 17 16 18 17 14
11 | 9 9 17 11 17 4 10 9 11 9 4 | 30 34 25 32 42 27 32 28 35 23 29
12 | 11 18 8 16 17 5 16 10 10 16 5 | 17 27 14 19 25 14 21 19 24 18 16
13 | 6 10 8 9 25 4 12 6 11 13 4 | 33 35 30 32 49 31 31 31 32 31 32
14 | 7 14 7 10 14 4 13 8 9 14 3 | 17 20 13 18 25 11 18 13 24 14 14
15 | 8 20 8 12 18 6 16 10 7 19 4 | 20 26 14 21 30 14 22 19 22 18 17
16 | 9 17 10 14 14 6 16 8 11 20 4 | 22 26 17 22 25 17 22 19 29 14 19
17E | 9 13 10 10 9 4 20 14 9 12 4 | 26 27 21 27 35 22 24 27 29 20 24
18 | 7 11 12 19 11 4 9 13 13 20 4 | 10 21 15 18 19 10 18 15 22 13 12
19E | 7 11 6 9 14 5 13 10 9 11 3 | 23 27 22 28 29 23 24 24 30 18 23
20 | 8 10 12 11 11 3 10 15 9 21 4 | 18 18 16 20 16 13 16 14 21 10 13
21 | 11 15 12 8 14 6 15 11 10 19 4 | 26 32 23 25 32 22 29 25 26 20 24
22 | 6 9 11 11 11 3 8 12 11 10 3 | 15 21 17 15 22 14 18 15 21 13 15
23 | 9 11 11 9 13 4 13 8 8 14 3 | 19 21 14 17 23 14 20 16 25 16 15
24 | 16 8 13 6 11 4 14 9 9 13 4 | 19 22 23 19 24 15 20 17 22 16 18
25 | 10 9 12 9 15 4 14 8 9 10 4 | 14 22 22 22 26 14 21 17 23 13 17
26 | 8 11 10 9 15 5 12 7 6 15 3 | 18 28 21 19 20 17 26 20 20 22 19
X27E | 9 12 14 8 --- 6 13 7 7 11 4 | 21 18 26 21 --- 17 21 20 25 15 20
28 | 9 14 11 11 18 5 11 8 6 17 4 | 21 25 15 19 28 14 19 19 19 18 17
29E | 9 17 6 10 16 6 25 9 10 13 5 | 24 26 23 26 26 21 28 26 37 22 24
X30 | 8 11 11 7 --- 6 11 15 10 13 4 | 21 28 25 19 --- 21 29 21 27 23 22
31 | 7 10 11 11 18 4 12 7 9 11 4 | 21 25 11 22 34 15 19 17 25 9 18
32 | 7 9 11 9 9 4 7 7 9 15 3 | 19 19 13 14 20 12 16 16 24 12 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 11 11 14 5 14 10 10 15 |T 23 26 21 22 28 20 23 22 26 19 22
WRMS | 9 13 11 10 14 5 12 9 8 15 |NE 22 24 18 20 26 18 21 20 24 17 20
MEDI | 8 11 11 10 14 4 12 9 9 14 |MD 20 25 19 21 25 15 21 19 24 18 18
Table 3.1798.2 GPS week: 1798 Day: 2 MJD: 56832.000
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 15 8 9 5 12 9 8 11 3 | 18 25 19 23 28 17 28 20 22 15 20
2 | 8 17 14 10 15 4 14 13 8 15 4 | 24 31 24 24 26 23 25 29 28 24 24
3E | 12 19 15 11 19 8 17 18 16 13 6 | 45 49 43 41 39 42 46 44 48 43 42
4 | 5 11 14 11 9 5 8 11 9 10 3 | 19 19 19 24 24 19 19 26 24 24 20
5 | 8 12 12 11 10 5 13 8 11 22 4 | 33 35 27 29 30 27 32 29 34 30 29
X6 | 12 --- 14 16 82 9 --- 14 12 34 6 | 43 --- 43 43 49 43 --- 48 45 44 43
7 | 6 11 12 12 15 5 15 9 8 13 4 | 22 23 15 26 31 18 18 22 25 12 20
8 | 5 10 11 9 9 4 10 5 7 25 3 | 20 25 20 18 19 16 18 16 23 24 18
X9 | 24 16 18 --- --- 15 --- 26 31 --- 12 | 82 58 56 --- --- 77 --- 41 61 --- 72
10 | 7 11 11 7 12 4 9 7 6 12 3 | 22 22 14 16 22 16 17 20 21 19 17
11 | 10 11 20 8 17 4 8 8 5 10 4 | 33 38 30 33 45 31 35 35 34 28 33
12 | 11 17 12 14 15 3 17 9 9 15 5 | 21 28 19 25 27 18 21 20 26 20 20
13 | 7 10 13 7 18 4 11 11 8 12 4 | 26 25 22 24 36 21 22 26 24 19 23
14 | 10 11 9 11 16 5 11 13 9 15 4 | 23 21 21 25 26 19 17 17 28 18 20
15 | 14 16 12 13 22 4 17 10 12 21 5 | 28 27 18 25 31 19 25 22 24 23 22
16 | 10 15 13 15 13 5 12 11 8 18 4 | 22 27 20 24 27 19 23 21 26 16 21
17E | 8 14 9 12 12 5 19 19 10 15 5 | 23 25 21 27 33 21 23 34 31 23 24
18 | 7 9 13 18 9 5 10 11 10 21 4 | 18 22 22 22 18 17 19 18 23 18 18
19E | 7 13 9 8 14 4 12 9 8 12 3 | 24 29 23 27 30 23 22 25 29 17 24
20 | 8 11 14 10 12 4 10 11 7 20 4 | 20 16 18 23 15 16 17 17 22 12 16
21 | 10 12 15 9 14 6 14 11 9 20 4 | 30 34 28 30 34 28 31 31 37 24 30
22 | 8 9 12 11 11 4 10 12 10 13 4 | 22 25 21 22 23 20 21 21 27 16 21
23 | 7 11 14 9 12 5 13 11 10 16 4 | 22 22 21 22 26 20 23 21 29 18 20
24 | 9 13 16 11 16 6 13 7 11 12 4 | 22 28 26 23 27 18 21 21 25 18 22
25 | 8 13 16 11 17 4 13 8 6 11 4 | 22 24 26 27 28 20 23 19 24 18 21
26 | 7 9 10 6 11 6 9 6 6 12 3 | 24 29 24 22 21 19 24 23 26 22 23
X27E | 11 12 16 7 --- 7 10 8 7 14 4 | 23 21 30 23 --- 21 21 22 24 21 22
28 | 7 15 12 12 16 2 13 10 7 20 4 | 20 26 17 23 29 16 21 20 24 21 19
29E | 8 16 11 14 25 8 24 13 8 10 5 | 26 28 23 31 24 23 29 27 36 21 25
X30 | 5 10 12 9 --- 5 12 12 7 14 4 | 28 30 30 26 --- 26 32 33 29 30 28
31 | 8 11 12 10 20 5 13 12 9 10 4 | 24 28 15 23 35 19 20 18 27 14 21
32 | 9 10 14 10 9 4 7 11 7 14 3 | 21 21 20 21 21 16 18 20 23 17 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 13 11 15 5 13 11 9 15 |T 26 27 24 25 28 23 23 25 29 21 24
WRMS | 8 13 13 10 14 5 12 10 8 13 |NE 26 27 23 24 27 23 22 24 28 20 24
MEDI | 8 11 13 11 14 5 12 11 8 14 |MD 23 26 21 24 27 19 22 22 26 20 21
Table 3.1798.3 GPS week: 1798 Day: 3 MJD: 56833.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 8 13 7 8 7 11 11 8 12 3 | 27 26 23 24 29 20 29 22 30 20 24
2 | 10 13 12 10 14 7 13 13 9 15 4 | 25 30 25 27 23 24 28 33 29 27 25
3E | 18 20 12 13 13 7 20 20 17 13 6 | 59 63 60 58 57 61 67 60 65 63 60
4 | 9 11 13 9 9 6 6 11 9 13 3 | 19 23 20 24 25 19 22 27 24 25 22
5 | 9 15 11 10 11 6 11 12 9 24 4 | 33 40 34 36 35 32 36 34 35 36 33
X6 | 14 --- 14 13 88 8 --- 16 14 32 7 | 47 --- 47 47 58 44 --- 48 46 42 45
7 | 9 13 11 11 16 7 16 11 8 14 4 | 23 26 16 26 31 19 21 22 22 14 20
8 | 6 9 12 8 9 5 9 7 9 23 3 | 19 23 21 17 21 15 18 18 19 26 17
X9 | 23 12 11 --- --- 22 --- 11 20 --- 8 | 61 43 56 --- --- 68 --- 42 57 --- 69
10 | 9 9 12 8 10 4 6 9 6 11 3 | 21 26 18 24 26 22 22 26 26 23 22
11 | 10 9 18 9 16 4 11 8 9 10 4 | 33 39 31 36 47 34 39 37 42 32 36
12 | 11 17 8 18 17 7 17 9 10 16 5 | 20 30 18 25 25 19 26 19 23 20 19
13 | 8 19 10 8 17 4 11 10 8 16 4 | 27 29 21 27 35 21 23 26 28 18 24
14 | 13 9 7 14 17 4 10 15 12 17 4 | 26 23 20 28 26 21 21 22 30 23 21
15 | 9 15 9 14 21 6 18 10 13 22 5 | 23 26 17 27 31 20 27 22 24 23 21
16 | 12 15 11 14 16 6 15 13 13 22 5 | 24 26 18 24 24 18 22 18 25 18 19
17E | 9 14 9 8 18 5 19 9 13 16 4 | 43 42 39 42 42 40 42 44 44 41 41
18 | 9 11 11 17 10 4 9 13 9 19 4 | 24 26 23 23 18 18 22 19 24 20 20
19E | 9 10 8 10 13 5 12 12 8 11 4 | 25 25 19 22 30 20 23 21 27 14 22
20 | 9 9 11 9 12 6 10 9 13 19 4 | 26 21 20 26 21 19 18 19 25 16 20
21 | 17 14 13 11 13 6 13 15 11 22 5 | 41 34 29 32 33 31 34 33 39 27 32
22 | 9 9 11 15 12 4 8 15 10 12 4 | 25 26 23 27 22 22 22 24 25 22 22
23 | 11 9 11 12 13 5 13 11 12 19 4 | 25 24 19 23 26 18 22 20 26 17 20
24 | 9 11 14 11 13 7 12 8 13 14 4 | 20 25 26 24 23 19 21 22 21 22 21
25 | 9 10 13 8 14 5 15 11 5 12 4 | 18 23 24 24 23 18 25 18 19 17 19
26 | 10 8 10 8 10 7 9 8 11 14 3 | 20 27 21 19 25 17 25 24 21 22 21
X27E | 17 13 16 8 --- 9 11 10 10 12 5 | 28 23 30 23 --- 21 23 22 29 21 23
28 | 9 12 11 12 15 5 11 11 9 15 4 | 21 25 15 21 30 16 21 21 24 18 18
29E | 12 16 6 15 13 7 23 17 9 11 5 | 27 28 22 30 28 24 28 29 30 24 25
X30 | 9 10 14 10 --- 8 14 31 10 14 6 | 43 49 47 45 --- 43 48 43 45 45 43
31 | 10 13 10 12 19 4 14 16 9 12 4 | 26 29 17 28 33 20 23 22 25 16 22
32 | 9 8 11 8 10 5 6 7 7 12 3 | 24 23 20 21 22 19 23 22 25 18 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 11 11 14 6 13 12 10 16 |T 28 29 26 28 29 25 27 27 30 24 27
WRMS | 10 12 11 11 13 6 11 11 9 14 |NE 27 28 25 27 28 24 25 26 29 23 26
MEDI | 9 11 11 10 13 6 11 11 9 14 |MD 25 26 21 26 26 20 23 22 26 22 22
Table 3.1798.4 GPS week: 1798 Day: 4 MJD: 56834.000
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 9 14 12 10 6 12 13 10 10 4 | 20 25 18 21 28 17 28 21 25 17 20
2 | 9 14 17 11 16 5 11 11 11 12 4 | 19 27 20 27 28 19 22 29 25 17 22
3E | 14 17 12 9 16 6 18 19 17 15 6 | 33 35 30 31 33 31 31 34 36 27 30
4 | 7 10 11 10 12 5 8 11 10 13 3 | 20 17 18 23 28 18 18 25 23 21 19
5 | 9 13 10 11 10 6 11 9 10 20 4 | 30 32 27 29 29 27 28 28 31 29 28
X6 | 13 --- 13 17 84 9 --- 14 11 33 6 | 38 --- 37 39 49 36 --- 38 35 34 36
7 | 10 13 8 11 18 5 14 10 6 12 4 | 21 23 13 25 30 16 17 21 22 12 17
8 | 8 10 8 7 14 4 10 7 7 20 3 | 22 24 17 14 18 14 16 16 18 22 16
X9 | 20 18 11 --- --- 21 --- 14 13 --- 8 | 37 34 46 --- --- 43 --- 28 38 --- 38
10 | 10 11 8 10 13 5 8 9 7 11 3 | 21 22 18 26 27 18 17 21 24 18 20
11 | 8 11 18 10 20 4 8 10 10 10 4 | 28 34 25 32 43 26 29 29 29 23 28
12 | 11 16 10 15 20 4 15 9 11 16 5 | 18 27 15 22 27 14 20 18 22 14 17
13 | 8 15 9 8 18 4 12 9 7 15 4 | 23 24 19 23 35 19 23 22 26 19 21
14 | 10 9 10 8 23 5 11 12 12 14 4 | 19 19 14 18 27 15 17 15 23 13 15
15 | 10 14 9 12 19 5 17 10 9 20 4 | 22 23 15 23 29 17 22 20 22 16 18
16 | 12 13 12 14 19 6 13 14 13 18 5 | 21 23 16 22 24 15 20 19 25 15 17
17E | 9 12 9 10 24 6 20 12 10 14 5 | 29 26 20 31 28 27 28 27 31 18 26
18 | 10 12 12 15 13 5 10 14 10 22 4 | 18 24 21 18 20 17 21 20 24 21 17
19E | 8 10 8 8 18 4 12 12 11 14 4 | 22 26 18 22 25 19 19 22 25 13 21
20 | 10 10 11 8 14 3 9 9 8 18 3 | 23 19 18 19 19 17 16 19 25 15 17
21 | 10 15 13 10 14 5 12 13 11 21 4 | 26 31 25 29 34 25 29 29 33 22 27
22 | 11 9 13 12 16 4 10 16 10 13 4 | 19 21 19 20 24 17 22 21 25 16 18
23 | 10 10 9 9 15 4 13 11 7 15 4 | 21 23 17 18 25 15 21 17 25 15 17
24 | 11 12 13 7 18 6 13 11 16 14 4 | 22 24 27 22 29 18 22 23 25 18 22
25 | 10 10 13 9 18 3 12 10 8 12 4 | 16 22 21 21 24 14 19 14 18 13 16
26 | 8 7 8 9 15 4 9 9 10 13 3 | 23 28 21 18 22 18 24 23 23 19 21
X27E | 10 11 14 8 --- 4 11 10 8 12 4 | 20 21 27 22 --- 19 19 20 25 18 20
28 | 7 13 10 11 17 3 10 13 6 18 4 | 20 24 15 22 30 17 19 20 24 18 18
29E | 12 15 9 13 17 5 22 10 10 10 5 | 27 24 17 27 24 19 23 23 27 15 21
X30 | 10 10 10 6 --- 4 13 9 6 16 4 | 23 28 26 21 --- 23 29 21 24 27 23
31 | 8 13 12 10 23 6 14 17 8 11 5 | 23 28 15 23 38 18 23 17 27 11 20
32 | 8 10 12 10 15 4 6 10 7 13 3 | 19 20 15 13 22 13 17 19 25 14 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 11 11 17 5 13 12 10 15 |T 23 25 20 23 28 20 21 22 25 18 21
WRMS | 9 12 11 10 16 5 11 11 9 15 |NE 22 24 20 22 28 19 21 21 25 18 20
MEDI | 10 12 11 10 17 5 12 11 10 14 |MD 22 24 18 22 28 18 21 21 25 18 20
Table 3.1798.5 GPS week: 1798 Day: 5 MJD: 56835.000
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 | 16 9 15 13 11 6 11 11 6 10 4 | 32 26 17 23 27 17 26 22 25 16 22
2 | 11 13 14 10 18 7 14 15 8 13 5 | 21 24 19 20 26 16 19 26 21 16 18
3E | 15 19 17 12 15 7 22 20 15 13 6 | 57 62 57 59 59 58 62 59 59 56 57
4 | 8 11 13 12 14 5 12 13 11 11 4 | 21 18 16 21 25 15 16 22 16 16 17
5 | 8 11 11 11 12 5 14 11 10 20 4 | 27 32 24 28 30 26 29 28 29 27 26
X6 | 14 --- 17 20 84 9 --- 18 13 34 8 | 41 --- 39 37 38 37 --- 45 38 41 38
7 | 11 14 10 11 18 5 15 9 8 12 4 | 20 25 12 23 30 14 19 21 23 10 18
8 | 8 11 12 10 14 4 11 7 7 20 3 | 21 25 19 17 20 15 19 19 21 23 18
X9 | 36 14 --- --- --- 18 --- 21 45 --- 19 | 33 22 --- --- --- 32 --- 15 57 --- 32
10 | 9 9 10 9 17 6 10 10 5 12 3 | 20 17 14 20 24 15 15 17 14 13 14
11 | 7 9 17 12 18 6 12 7 8 10 4 | 28 32 23 30 41 23 29 27 26 20 27
12 | 10 13 11 15 19 6 13 12 11 19 5 | 18 25 14 20 27 14 20 19 22 17 17
13 | 19 13 12 10 20 4 11 11 8 15 5 | 23 23 16 22 34 16 20 20 21 14 18
14 | 8 13 10 11 15 6 12 11 11 18 4 | 18 21 13 19 21 14 18 16 19 18 15
15 | 7 15 11 15 17 6 17 11 10 20 5 | 20 26 14 22 28 15 22 20 19 16 18
16 | 15 13 12 11 18 5 12 14 9 19 5 | 22 23 15 17 24 13 19 19 20 14 16
17E | 12 12 9 11 13 5 24 12 9 12 5 | 30 29 23 28 32 24 31 31 29 24 27
18 | 12 10 14 15 11 6 10 15 15 23 5 | 11 19 16 15 15 11 18 18 20 15 12
19E | 7 10 9 11 13 5 13 10 7 10 3 | 23 23 16 21 25 17 18 20 24 15 19
20 | 13 8 10 11 12 4 12 11 11 20 4 | 22 15 14 16 16 10 16 17 20 13 13
21 | 13 16 39 9 15 7 18 11 14 23 7 | 24 29 46 23 32 22 29 26 29 20 25
22 | 7 10 13 12 10 5 10 14 9 14 4 | 15 22 17 16 19 14 18 18 21 13 15
23 | 17 13 12 13 16 6 12 12 8 16 5 | 19 21 16 17 24 14 18 18 23 14 15
24 | 12 10 19 9 17 6 16 14 12 11 5 | 22 23 27 18 27 17 22 23 22 16 20
25 | 11 7 15 11 15 5 16 9 11 13 4 | 16 20 22 19 24 15 22 14 19 12 17
26 | 10 8 10 14 15 6 12 9 9 17 4 | 20 28 20 18 24 18 26 24 20 23 21
X27E | 9 11 15 15 --- 6 13 9 9 12 4 | 21 21 28 21 --- 19 19 20 21 18 20
28 | 8 15 11 16 17 5 12 9 6 18 4 | 20 26 16 25 31 15 23 21 21 17 19
29E | 12 17 10 12 17 7 20 12 10 12 5 | 21 21 16 27 22 16 21 21 25 16 19
X30 | 7 10 12 8 --- 5 12 9 7 14 4 | 30 33 33 30 --- 27 35 30 35 32 31
31 | 7 11 10 10 23 6 15 11 11 11 4 | 20 26 13 21 36 14 22 18 21 14 18
32 | 10 7 11 10 19 7 11 9 9 15 4 | 19 18 14 13 23 11 17 17 19 12 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 14 12 16 6 14 12 10 16 |T 23 25 20 22 27 18 22 22 24 19 21
WRMS | 11 12 12 11 15 6 13 11 9 14 |NE 22 23 19 21 26 17 21 21 24 17 19
MEDI | 10 11 12 11 16 6 12 11 9 14 |MD 21 23 16 21 26 15 20 20 21 16 18
Table 3.1798.6 GPS week: 1798 Day: 6 MJD: 56836.000
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 | 6 8 11 14 9 5 13 11 7 12 3 | 25 31 23 26 32 23 35 26 27 21 26
2 | 10 11 16 11 15 5 13 16 7 14 4 | 25 29 23 30 32 24 28 37 28 27 26
3E | 11 19 13 13 14 6 18 18 15 17 5 | 62 60 62 58 65 58 59 60 63 63 59
4 | 6 9 11 9 9 5 10 15 8 10 3 | 23 25 21 26 31 22 23 33 25 21 24
5 | 8 11 11 11 11 5 11 12 11 21 4 | 39 41 37 43 36 36 40 38 39 40 38
X6 | 14 --- 13 16 84 10 --- 17 10 36 7 | 49 --- 47 44 65 42 --- 52 45 47 45
7 | 11 14 9 12 17 4 15 11 8 15 4 | 23 29 17 28 33 18 24 25 23 15 22
8 | 7 8 11 9 12 4 13 15 8 22 4 | 30 30 28 25 26 25 20 28 25 33 26
X9 | 24 17 --- --- --- 11 --- 21 30 --- 14 | 33 27 --- --- --- 25 --- 29 37 --- 25
10 | 7 9 8 9 13 4 6 12 9 12 3 | 23 29 21 26 33 23 22 30 26 27 24
11 | 7 10 17 10 20 4 11 9 9 12 4 | 40 42 35 41 54 36 40 39 41 32 39
12 | 10 13 11 14 19 6 12 11 10 17 4 | 21 28 17 22 28 17 25 23 23 19 20
13 | 8 20 12 10 19 5 13 11 6 13 4 | 26 31 22 27 39 21 25 26 26 19 24
14 | 6 11 11 10 16 4 13 13 7 16 4 | 18 22 18 19 25 17 22 22 23 21 18
15 | 7 16 10 14 21 6 18 9 10 18 5 | 24 30 18 26 32 18 25 23 22 21 21
16 | 11 15 11 13 16 6 14 17 6 23 4 | 25 27 19 25 27 18 23 22 27 18 21
17E | 6 12 7 11 12 5 23 10 11 14 4 | 30 28 24 30 32 25 25 30 36 26 27
18 | 8 10 12 19 12 4 10 16 13 22 4 | 20 25 23 24 23 19 24 23 26 21 20
19E | 5 12 8 13 17 4 12 9 10 12 4 | 29 30 24 30 33 24 24 24 28 17 26
20 | 9 8 10 9 11 5 11 10 8 21 3 | 28 23 19 26 26 21 20 26 27 18 23
21 | 10 16 15 8 14 5 14 13 10 23 4 | 35 37 30 33 40 30 36 36 34 28 33
22 | 6 9 11 15 12 3 12 14 8 14 4 | 25 28 24 27 29 23 27 28 28 23 24
23 | 8 13 11 10 14 5 12 14 7 19 4 | 26 26 21 24 29 19 25 22 25 19 22
24 | 9 12 13 10 16 6 19 17 14 12 5 | 23 23 27 20 26 18 26 26 22 21 21
25 | 10 10 13 10 14 5 14 8 10 12 4 | 21 24 24 26 27 18 25 19 22 15 21
26 | 10 9 11 13 12 5 11 10 12 15 4 | 22 30 23 21 24 21 27 26 27 23 23
X27E | 6 12 16 16 --- 5 11 12 10 14 5 | 26 22 31 29 --- 21 19 22 30 22 24
28 | 6 12 11 13 18 4 16 10 9 15 4 | 24 27 21 26 33 22 23 23 26 19 22
29E | 9 15 8 11 19 7 24 10 10 12 5 | 28 26 22 30 26 22 26 26 32 21 25
X30 | 9 10 12 10 --- 4 15 10 11 14 4 | 27 31 33 28 --- 26 34 25 30 27 28
31 | 8 11 10 13 22 6 17 13 8 13 4 | 25 27 13 26 34 16 24 20 23 15 21
32 | 7 9 10 12 12 5 11 11 8 15 3 | 23 26 19 19 25 19 27 24 26 18 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 12 11 12 15 5 14 13 9 16 |T 28 29 25 28 33 23 27 28 29 24 26
WRMS | 8 12 11 11 14 5 13 12 8 16 |NE 27 28 24 27 32 23 26 27 28 23 25
MEDI | 8 11 11 11 14 5 13 12 9 15 |MD 25 28 23 26 32 22 25 26 27 21 24
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.1798 GPS week: 1798 MJD: 56830.0-56836.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3044 |U 7 6 15 |U 6 7 22 |U 9 10 23 |
emr | emr 2954 | 10 7 20 |U 6 6 23 | 10 8 24 |
esa | esa 3044 | 8 6 17 |U 6 7 21 | 9 10 23 |
gfz | gfz 2971 |U 7 6 15 |U 6 7 22 |U 9 9 22 |
grg | grg 2784 |U 11 8 21 |U 8 10 28 |U 11 11 26 |
igr | igr 3015 | 8 6 16 | 6 7 21 | 9 11 24 |
igs | igs 3029 | 7 6 16 | 6 7 23 | 9 10 23 |
jpl | jpl 2875 | 9 9 22 |U 5 7 23 |U 10 10 28 |
mit | mit 3058 | 32 30 72 |U 7 8 25 |U 8 10 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 5.1798.0 GPS week: 1798 Day: 0 MJD: 56830.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 7 6 12 | 5 5 18 | 9 9 20 |
emr | emr 2875 | 11 6 17 | 5 6 17 | 7 7 14 |
esa | esa 3072 | 8 5 15 | 5 6 19 | 8 9 17 |
gfz | gfz 2968 | 8 6 14 | 5 6 19 | 9 8 19 |
grg | grg 2784 | 10 9 19 | 7 8 18 | 11 9 23 |
igr | igr 2913 | 7 5 14 | 5 7 21 | 9 11 19 |
igs | igs 3024 | 8 6 14 | 5 6 19 | 8 9 18 |
jpl | jpl 2875 | 10 7 21 | 5 5 20 | 9 9 19 |
mit | mit 2976 | 7 6 14 | 6 7 27 | 7 9 20 |
Table 5.1798.1 GPS week: 1798 Day: 1 MJD: 56831.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 | 4 5 9 | 5 6 21 | 7 7 19 |
emr | emr 2966 | 9 6 16 | 5 5 22 | 9 6 19 |
esa | esa 3072 | 7 6 12 | 5 6 20 | 7 7 18 |
gfz | gfz 2972 | 5 6 9 | 5 6 22 | 7 6 19 |
grg | grg 2784 | 8 5 13 | 7 10 26 | 11 10 23 |
igr | igr 3053 | 5 5 8 | 5 5 17 | 7 9 20 |
igs | igs 3064 | 6 5 11 | 5 7 23 | 7 7 19 |
jpl | jpl 2876 | 8 7 17 | 4 6 21 | 8 5 22 |
mit | mit 3072 | 4 5 24 | 5 7 19 | 7 9 20 |
Table 5.1798.2 GPS week: 1798 Day: 2 MJD: 56832.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 15 8 25 | 7 10 28 | 8 10 19 |
emr | emr 2967 | 12 9 28 | 6 8 25 | 10 10 25 |
esa | esa 3072 | 8 7 25 | 6 10 25 | 8 11 22 |
gfz | gfz 2972 | 7 7 22 | 6 9 26 | 9 11 23 |
grg | grg 2784 | 23 7 35 | 8 9 37 | 11 12 24 |
igr | igr 3056 | 17 9 27 | 6 10 25 | 10 12 24 |
igs | igs 3062 | 8 6 24 | 5 8 25 | 9 11 22 |
jpl | jpl 2876 | 11 11 31 | 6 10 31 | 11 12 29 |
mit | mit 3072 | 44 30 77 | 6 8 27 | 9 11 18 |
Table 5.1798.3 GPS week: 1798 Day: 3 MJD: 56833.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 7 6 16 | 6 9 18 | 9 7 20 |
emr | emr 2970 | 9 7 17 | 5 6 20 | 9 7 23 |
esa | esa 3072 | 8 6 17 | 6 8 19 | 9 9 20 |
gfz | gfz 2972 | 6 5 14 | 5 10 15 | 9 8 21 |
grg | grg 2784 | 8 6 21 | 6 8 27 | 11 9 24 |
igr | igr 2975 | 6 5 14 | 5 10 18 | 8 7 20 |
igs | igs 3064 | 7 5 15 | 5 8 18 | 8 7 20 |
jpl | jpl 2875 | 8 7 18 | 5 8 19 | 8 9 28 |
mit | mit 3072 | 28 19 45 | 6 10 20 | 9 7 18 |
Table 5.1798.4 GPS week: 1798 Day: 4 MJD: 56834.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3051 | 7 7 14 | 6 6 20 | 8 11 23 |
emr | emr 2967 | 11 7 19 | 8 6 24 | 10 11 27 |
esa | esa 3072 | 8 7 16 | 5 6 20 | 9 12 23 |
gfz | gfz 2972 | 8 7 15 | 5 6 23 | 9 11 21 |
grg | grg 2784 | 11 9 23 | 8 10 27 | 10 13 28 |
igr | igr 3032 | 8 7 16 | 5 6 20 | 9 12 22 |
igs | igs 2968 | 9 6 15 | 5 5 21 | 8 12 22 |
jpl | jpl 2876 | 9 9 17 | 5 6 22 | 10 10 31 |
mit | mit 3072 | 48 58 111 | 6 5 26 | 9 12 20 |
Table 5.1798.5 GPS week: 1798 Day: 5 MJD: 56835.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 6 6 16 | 8 8 33 | 9 10 23 |
emr | emr 2969 | 10 10 20 | 9 8 29 | 10 7 22 |
esa | esa 2976 | 8 8 20 | 7 6 25 | 9 9 23 |
gfz | gfz 2972 | 5 6 16 | 7 7 31 | 9 8 21 |
grg | grg 2784 | 10 11 20 | 10 15 35 | 12 10 26 |
igr | igr 3044 | 6 6 18 | 7 7 27 | 8 11 24 |
igs | igs 2989 | 7 7 16 | 9 9 36 | 10 11 24 |
jpl | jpl 2876 | 11 13 23 | 6 7 32 | 9 9 28 |
mit | mit 3072 | 26 50 97 | 8 8 32 | 8 10 22 |
Table 5.1798.6 GPS week: 1798 Day: 6 MJD: 56836.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 5 7 12 | 7 6 19 | 11 14 36 |
emr | emr 2966 | 8 8 23 | 7 6 21 | 13 13 34 |
esa | esa 2976 | 7 6 17 | 8 5 22 | 11 14 35 |
gfz | gfz 2972 | 6 8 13 | 7 6 17 | 11 12 33 |
grg | grg 2784 | 9 9 18 | 10 8 26 | 14 14 39 |
igr | igr 3034 | 6 7 14 | 7 6 18 | 12 14 37 |
igs | igs 3037 | 6 7 13 | 7 5 17 | 11 13 35 |
jpl | jpl 2876 | 8 11 25 | 7 6 18 | 13 15 39 |
mit | mit 3072 | 64 41 138 | 9 7 22 | 10 12 32 |
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 6.1798 GPS week: 1798 MJD: 56830.500-56836.500
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 7 -50 101 1 | 12 16
| 15 26 135 75 5 | 2
emr uuuuu | 61 17 -49 58 -11 | 39 43
| 20 23 51 37 6 | 4
esa uuuuu | -22 -13 62 -99 -2 | 10 15
| 13 12 77 83 2 | 2
gfz uuuuu | 0 7 21 45 4 | -6 15
| 16 25 88 58 3 | 3
grg uuuuu | 25 -20 -50 65 -5 | 38 40
| 10 18 84 50 3 | 3
igr xxxxx | -10 -2 11 -121 -2 | 1 13
| 10 31 71 50 3 | 2
irf xxxxx | 2 -14 -22 -76 1 | -1 11
| 8 7 30 25 2 | 2
jpl uuuuu | -19 -6 39 -135 -5 | 8 18
| 16 32 49 64 9 | 4
mit uuuuu | -10 -3 -56 -129 -2 | 22 24
| 20 8 80 60 4 | 3
ngs uuuuu | -35 3 77 57 3 | 10 16
| 34 33 97 99 5 | 2
sio xxxxx | -4 13 20 -221 -6 | 44 46
| 23 19 39 82 7 | 4
Table 7.1798.0 GPS week: 1798 Day: 0 MJD: 56830.500
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 | 3 14 2 -39 11 | 14 18
emr uuuuu | 81 -27 -14 54 -14 | 45 48
esa uuuuu | -12 -23 159 -178 -2 | 14 17
gfz uuuuu | 31 15 110 55 2 | -2 15
grg uuuuu | 18 -17 -175 148 1 | 43 44
igr xxxxx | 3 -45 -27 -101 -3 | 4 11
irf xxxxx | 14 -2 -46 -35 -1 | 3 10
jpl uuuuu | -31 -39 -33 -60 -17 | 14 18
mit uuuuu | 6 9 -133 -31 -5 | 27 28
ngs uuuuu | -89 45 38 83 8 | 12 17
sio xxxxx | 17 -1 -54 -58 -3 | 51 52
Table 7.1798.1 GPS week: 1798 Day: 1 MJD: 56831.500
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 | 3 5 -127 47 4 | 14 18
emr uuuuu | 68 15 29 109 -11 | 44 46
esa uuuuu | -15 -6 102 -191 1 | 12 16
gfz uuuuu | -15 23 46 -75 0 | -4 15
grg uuuuu | 38 -24 -113 125 -7 | 41 43
igr xxxxx | -28 -20 84 -125 3 | 3 12
irf xxxxx | -3 -9 9 -68 0 | 1 10
jpl uuuuu | -32 -38 101 -168 -5 | 12 18
mit uuuuu | 0 -12 5 -64 -2 | 25 26
ngs uuuuu | -30 16 -10 202 3 | 11 16
sio xxxxx | 17 -4 66 -171 -10 | 49 50
Table 7.1798.2 GPS week: 1798 Day: 2 MJD: 56832.500
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 | 32 9 -131 116 -2 | 12 16
emr uuuuu | 29 45 -54 58 -12 | 39 43
esa uuuuu | -25 -31 158 -119 0 | 9 14
gfz uuuuu | -10 20 48 38 4 | -8 15
grg uuuuu | 32 -36 -32 23 -7 | 37 39
igr xxxxx | -5 -15 51 -144 -3 | 1 12
irf xxxxx | -8 -16 -28 -115 3 | -2 10
jpl uuuuu | -32 -36 89 -249 -13 | 8 17
mit uuuuu | -22 1 -82 -174 0 | 21 24
ngs uuuuu | -11 6 77 176 9 | 8 14
sio xxxxx | -8 9 16 -281 -1 | 44 45
Table 7.1798.3 GPS week: 1798 Day: 3 MJD: 56833.500
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 | 20 -11 -96 133 -3 | 9 14
emr uuuuu | 40 34 -103 55 -8 | 36 41
esa uuuuu | -13 -11 21 13 -4 | 7 13
gfz uuuuu | -12 28 -70 111 3 | -10 16
grg uuuuu | 21 -38 92 25 -7 | 34 36
igr xxxxx | -15 41 -122 -112 -5 | -2 12
irf xxxxx | -5 -11 7 -67 -2 | -4 10
jpl uuuuu | -17 20 -4 -164 8 | 5 17
mit uuuuu | -47 -6 54 -166 -8 | 19 21
ngs uuuuu | 10 -19 119 -30 4 | 7 13
sio xxxxx | -47 -9 37 -283 -10 | 41 42
Table 7.1798.4 GPS week: 1798 Day: 4 MJD: 56834.500
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 | -1 59 -237 154 -2 | 11 17
emr uuuuu | 77 12 -42 -11 -21 | 39 43
esa uuuuu | -9 -5 29 -19 -2 | 10 16
gfz uuuuu | 1 5 -53 82 7 | -8 17
grg uuuuu | 27 -18 -8 32 -3 | 36 39
igr xxxxx | -7 8 -14 -49 -2 | 1 14
irf xxxxx | 4 -19 10 -89 2 | -1 12
jpl uuuuu | 12 -9 27 -117 -7 | 7 20
mit uuuuu | -10 -13 15 -162 1 | 20 23
ngs uuuuu | -64 -43 268 0 5 | 10 17
sio xxxxx | 1 30 27 -257 3 | 42 44
Table 7.1798.5 GPS week: 1798 Day: 5 MJD: 56835.500
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 | -13 -20 129 185 0 | 11 17
emr uuuuu | 75 24 -40 86 -6 | 36 41
esa uuuuu | -36 2 -18 -43 -5 | 9 16
gfz uuuuu | 5 3 -74 48 9 | -6 15
grg uuuuu | 9 16 -76 56 -10 | 36 39
igr xxxxx | -15 33 48 -104 1 | 0 14
irf xxxxx | -1 -18 -53 -88 3 | -1 12
jpl uuuuu | -22 28 64 -103 1 | 6 20
mit uuuuu | -9 -7 -96 -187 4 | 20 23
ngs uuuuu | -14 -23 66 -49 -4 | 11 17
sio xxxxx | -16 27 44 -271 -1 | 42 44
Table 7.1798.6 GPS week: 1798 Day: 6 MJD: 56836.500
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 | 18 -9 110 108 0 | 11 16
emr uuuuu | 58 14 -119 54 -3 | 33 38
esa uuuuu | -42 -19 -17 -159 0 | 7 14
gfz uuuuu | 3 -45 141 53 4 | -6 16
grg uuuuu | 27 -22 -39 48 -4 | 35 37
igr xxxxx | -3 -17 54 -212 -2 | -1 13
irf xxxxx | 12 -21 -56 -67 0 | -2 12
jpl uuuuu | -14 31 27 -82 2 | 4 18
mit uuuuu | 15 4 -152 -119 -5 | 19 22
ngs uuuuu | -50 40 -20 18 -3 | 12 18
sio xxxxx | 10 41 1 -223 -17 | 41 43
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