[IGSREPORT-24457] Wk 1895 IGS Final Orbits
IGS ACC
acc at igs.org
Thu May 19 15:59:41 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1895 (May 01, 2016 - May 07, 2016)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1895[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1895[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1895[0-6].cls IGS GPS clock combination summary report.
igs18957.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18957.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 | MAL2 BJNM MAC1 MAL2
0 | ESA | CHUR
0 | GFZ | 18 32 32 ALGO BJNM HOB2 MAC1 MAG0 MAL2 NRMD POHN
0 | GFZ | BJNM HOB2 NRMD YSSK
0 | GRG | 13 13 HARB DARW HARB KELY MAC1
0 | JPL | SCOR
1 | COD | MAL2 HOFN NRIL TRO1
1 | EMR | SYOG
1 | ESA | SYOG TWTF NRIL SYOG TIXI TWTF
1 | GFZ | 18 32 18 32 CGGN DARW ISPA MAL2 NRIL NRMD ONSA PIMO
1 | GFZ | REUN TRO1 TWTF TWTF
1 | GRG | KARR KIRU POHN TOW2 KARR KIRU POHN TOW2
1 | MIT | TWTF TWTF
2 | COD | 15 15 MAL2 SYOG
2 | EMR | SYOG
2 | ESA | SYOG BJNM DRAG YKRO
2 | GFZ | 18 21 32 18 32 ALBH ARTU BAKE BRAZ BRUX DRAG DUBO
2 | GFZ | FAIR GRAZ HOFN HOLB IENG IRKJ ISPA KIRU KOUR MAS1
2 | GFZ | MATE MCIL NANO NICO NKLG NRC1 NRIL NTUS NYA1 ONSA
2 | GFZ | OPMT PIMO PTBB REUN SFER SSIA SYOG TLSE USUD VILL
2 | GFZ | WILL WTZR YELL YKRO ALBH BJNM MAL2 TWTF
2 | GRG | 32 DARW NNOR POHN SYOG DARW INVK NKLG NNOR POHN
3 | COD | ARTU SYOG
3 | EMR | YAKT
3 | ESA | KARR SYOG ARTU KARR
3 | GFZ | 13 18 32 13 18 32 MAL2 KARR MAL2 SYOG
3 | GRG | 13 13 ARTU CAS1 MAL2 POHN SYOG BRFT CAS1 MAL2 POHN
4 | COD | 32 KARR
4 | EMR | CHUR
4 | ESA | SYOG
4 | GFZ | 18 32 13 32 KARR SYOG SYOG
4 | GRG | 13 13 DARW HARB KARR POHN DARW HARB HRAO KARR POHN
4 | GRG | SYOG
4 | MIT | REUN REUN
5 | COD | 9 MAW1
5 | EMR | 9 SYOG TWTF
5 | ESA | ARTU SYOG
5 | GFZ | 18 32 18 32 ARTU BJNM POHN TWTF BJNM TWTF
5 | GRG | DARW HARB KARR ARTU DARW HOFN KARR POHN
5 | JPL | 9
6 | COD | GLSV
6 | EMR | SYOG YAKT
6 | ESA | IRKJ SYOG IRKJ SYOG
6 | GFZ | 18 32 18 32 BJNM HYDE SYOG WUHN
6 | GRG | 13 13 GLSV POHN WIND POHN WIND
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 | GFZ | ~00:30 | ~ -0.12 ns
6 | GFZ | ~19:30 | ~ -0.12 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. 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
----+--------+---------------
1 | COD | 32
2 | COD | 32
2 | GRG | 32
3 | COD | 32
3 | GRG | 32
4 | COD | 32
4 | GRG | 32
4 | NGS | 32
5 | COD | 32
5 | NGS | 32
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G27 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G32 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.1 -1.6 -1.9 -44 -6 2 .76
EMR | 0 | 11.3 -18.7 3.4 -9 -13 -25 .99
ESA | 0 | .2 -3.1 -.0 -5 -43 46 .48
GFZ | 0 | 1.3 -.6 -2.4 -36 -104 -63 .92
GRG | 0 | 14.7 -10.2 18.6 -68 11 32 .75
JPL | 0 | 9.3 -11.1 5.8 47 23 21 .44
MIT | 0 | 3.8 -11.2 4.8 5 -16 -16 .99
NGS | 0 | 13.4 -10.5 9.6 -34 -83 66 .75
SIO | 0 | 10.8 -11.1 -30.9 -30 -138 -137 .81
COD | 1 | -1.3 -2.2 -1.4 -46 -1 -9 .83
EMR | 1 | 1.8 -16.1 .5 7 -28 3 .95
ESA | 1 | .3 -2.5 .4 -6 -28 39 .69
GFZ | 1 | 1.4 -2.0 -2.3 -69 -107 -30 .96
GRG | 1 | 17.9 -12.9 14.9 -39 1 9 .48
JPL | 1 | 13.6 -6.9 9.6 15 -7 45 .48
MIT | 1 | 2.3 -10.7 -3.3 -18 -15 -3 1.06
NGS | 1 | 12.0 -12.2 20.2 -107 -82 51 .82
SIO | 1 | 8.5 -10.7 -43.1 -160 -33 36 .85
COD | 2 | -.5 -2.3 -1.7 -48 -17 9 .65
EMR | 2 | -.9 -10.6 -1.4 2 -26 -1 1.12
ESA | 2 | .2 -2.0 -.3 -9 -37 41 .70
GFZ | 2 | .6 -1.9 -2.2 -71 -104 11 .84
GRG | 2 | 13.2 -10.5 8.8 -40 -18 -15 .57
JPL | 2 | 5.1 -11.7 8.8 -46 5 -18 .52
MIT | 2 | 1.6 -11.1 -.6 -10 -13 -14 1.03
NGS | 2 | 10.4 -10.4 18.7 -112 -86 31 .89
SIO | 2 | 4.6 -11.6 -28.8 -45 -121 28 .90
COD | 3 | -1.5 -1.6 -2.0 -39 -1 -16 .82
EMR | 3 | 3.5 -8.8 15.8 16 -4 -19 1.05
ESA | 3 | -.1 -1.7 .3 -2 -26 17 .58
GFZ | 3 | .8 -1.8 -1.6 -55 -100 -22 .83
GRG | 3 | 11.6 -9.5 -2.0 -7 22 14 .65
JPL | 3 | 4.5 -10.1 7.8 19 62 60 1.04
MIT | 3 | -1.8 -14.6 5.7 -5 -18 -31 .98
NGS | 3 | -.2 -11.4 24.3 -144 -80 -52 .63
SIO | 3 | -2.7 -15.4 -36.2 -47 -24 60 1.01
COD | 4 | -.5 -1.6 -1.4 -53 -9 -28 .73
EMR | 4 | -2.5 -16.8 4.0 11 -13 -1 1.09
ESA | 4 | .0 -2.6 -.5 -44 -35 22 .68
GFZ | 4 | .4 -1.4 -1.9 -79 -88 -28 .96
GRG | 4 | 11.2 -4.7 7.4 -25 10 5 .62
JPL | 4 | -.7 -12.4 8.1 -15 -11 22 .91
MIT | 4 | .3 -17.0 7.8 32 -24 2 1.15
NGS | 4 | 9.8 -11.5 14.5 -108 -79 11 .75
SIO | 4 | 3.6 -15.3 -19.4 -51 -74 -46 1.13
COD | 5 | -1.2 -1.7 -1.6 -53 -7 -1 1.00
EMR | 5 | .1 -19.9 6.4 -2 -6 -10 1.12
ESA | 5 | -.4 -1.5 -.2 -15 -45 48 .79
GFZ | 5 | .5 -1.5 -2.5 -74 -96 -37 1.08
GRG | 5 | 5.4 -4.2 22.8 -2 6 19 .64
JPL | 5 | 3.7 -20.7 5.6 -84 45 -35 1.18
MIT | 5 | 2.7 -15.6 10.7 -13 -13 -25 .96
NGS | 5 | 1.0 -13.7 19.3 -140 -54 -27 .99
SIO | 5 | 7.4 -8.6 7.3 -49 -22 -4 .70
COD | 6 | -.8 -1.5 -1.0 -50 -7 -22 .82
EMR | 6 | 7.1 -4.9 16.4 7 -18 -21 1.13
ESA | 6 | -.1 -2.2 -.4 -18 -25 38 .55
GFZ | 6 | .4 -1.3 -1.9 -70 -89 -39 .82
GRG | 6 | 1.1 -3.1 19.7 -39 -28 20 .57
JPL | 6 | 13.2 -7.4 12.1 -2 -17 -4 .89
MIT | 6 | 2.0 -11.6 10.9 8 -23 2 .93
NGS | 6 | 10.8 -13.1 18.7 -134 -83 12 1.02
SIO | 6 | 5.7 -7.5 -7.1 -18 5 1 1.03
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1895.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1895.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 2.1895.[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 3.1895.[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 5.1895.0-6). 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 1895 summary. (May 01, 2016 - May 07, 2016)
Table 1.1895.a GPS week: 1895 MJD: 57509.000-57515.000
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 244| 0 1 -4 11 19 -17 .00 17 11 | -1182 173 14 136
| 1 0 2 14 21 14 .02 | 363 492
emr 80| -1 -4 0 11 -11 24 .30 14 13 | 3761 -189 15 149
| 3 3 2 16 8 14 .03 | 614 511
esa 149| 0 0 -7 -3 5 10 -.53 9 9 | 620 -2967 10 156
| 1 1 1 20 10 18 .03 | 1501 3956
gfz 207| 0 1 1 -21 -10 9 .06 11 10 | -251 -233 12 179
| 1 1 1 19 11 21 .05 | 261 294
grg 121| 2 1 9 -6 62 30 .13 17 14 | -25 -82 14 197
| 1 0 6 11 29 25 .07 | 215 335
igr n/a| 0 1 -3 6 25 -6 -.06 5 5 | 6427 -87 18 101
| 1 0 1 10 8 9 .01 | 508 587
jpl 80| 0 -1 0 27 20 11 .36 11 11 | 2391 -182 16 135
| 3 1 0 26 15 37 .06 | 1312 521
mit 350| 0 -2 0 -3 -21 -18 -.17 17 15 | -15 -235 48 369
| 1 1 1 32 31 33 .03 | 286 415
ngs 225| 0 1 6 -8 -26 -9 .06 13 9 | -1209 197 1052 2265
| 1 0 3 21 31 18 .06 | 391 545
sio 300| -2 1 -4 -16 -30 -44 .13 16 15 | --- --- --- ---
| 1 0 2 62 43 79 .10 | --- ---
Table 1.1895.b GPS week : 1895 MJD: 57509.000-57515.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 3 3 3 3 3 |
2 | 4 4 4 4 4 4 4 |
3 | 3 3 3 3 3 4 3 |
4 | 0 0 0 0 0 0 0 |
5 | 5 5 5 5 5 5 4 |
6 | 3 3 3 3 3 3 3 |
7 | 6 6 6 6 7 7 6 |
8 | 4 4 4 4 4 4 4 |
9 | 4 3 4 5 5 9 5 |
10 | 3 4 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 6 5 6 6 6 |
13 | 4 4 5 4 4 4 4 |
14 | 5 6 7 7 7 5 5 |
15 | 4 5 5 5 5 4 4 |
16 | 5 5 5 4 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 6 5 5 5 6 6 5 |
19 | 4 5 5 4 4 4 4 |
20 | 5 5 5 5 5 5 5 |
21 | 4 4 4 4 4 5 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 7 4 |
24 | 3 4 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 3 3 |
27 | 4 4 4 10 4 5 5 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 6 5 5 5 |
30 | 3 3 3 3 3 3 3 |
31 | 6 5 5 4 5 5 5 |
32 | 7 18 13 16 14 16 6 |
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 2.1895.0 GPS week: 1895 Day: 0 MJD: 57509.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 245| -1 3 -3 13 47 -1 .04 12 11 | -1478 578 14 148
emr 80| 1 -5 0 1 -1 43 .32 11 11 | 4338 23 14 151
esa 149| 0 0 -6 -13 15 33 -.49 9 8 | 3501 -10657 11 165
gfz 205| 0 1 2 -39 6 0 .11 12 11 | -180 -248 14 173
grg 118| 2 1 13 -7 45 33 .14 15 14 | -224 278 14 211
igr n/a| 0 1 -2 -16 36 -5 -.06 4 4 | 7028 -83 18 87
jpl 80| 0 -2 0 39 22 27 .42 10 10 | 4392 -2 18 138
mit 350| 0 0 -1 -27 -35 6 -.21 16 14 | 2 -206 48 321
ngs 225| -1 1 1 0 -14 -12 -.02 10 9 | -1476 587 1253 2172
sio 299| -1 0 -2 2 -112 -159 .03 13 13 | --- --- --- ---
Table 2.1895.1 GPS week: 1895 Day: 1 MJD: 57510.000
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| 0 1 -2 10 22 -24 .02 11 11 | -1129 45 15 131
emr 80| -5 -9 -1 13 -4 2 .28 13 13 | 3862 -392 14 146
esa 149| 0 0 -9 1 5 8 -.49 9 9 | 43 -2462 11 160
gfz 208| 0 2 0 -19 -30 -6 .08 11 10 | -302 -539 12 143
grg 125| 3 1 7 -7 82 -5 .06 14 13 | 33 -394 13 189
igr n/a| 0 0 -3 5 18 -6 -.05 5 5 | 6526 -633 18 114
jpl 80| 2 0 0 60 0 50 .36 10 10 | 3894 -374 16 131
mit 350| 0 0 0 -30 -22 -33 -.21 17 14 | 76 -447 43 377
ngs 224| 0 2 7 -6 -39 -1 .01 10 9 | -1145 67 1278 2463
sio 306| -3 0 -5 -74 -5 28 .19 17 16 | --- --- --- ---
Table 2.1895.2 GPS week: 1895 Day: 2 MJD: 57511.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 246| 1 1 -2 -3 -6 0 -.01 25 12 | -904 -102 14 149
emr 80| -5 -4 -4 12 -13 16 .30 17 14 | 4303 -43 14 139
esa 150| 1 0 -7 11 -3 0 -.50 9 8 | 1200 -2910 10 154
gfz 208| 0 1 1 -23 -18 39 .08 12 10 | 164 -518 11 147
grg 125| 2 1 7 -8 51 17 .07 23 13 | 180 -247 14 201
igr n/a| 0 0 -1 15 20 -17 -.07 5 4 | 6818 -231 17 101
jpl 80| -3 -3 0 12 10 -40 .44 12 12 | 2347 -356 16 145
mit 350| 1 -1 0 -27 34 14 -.16 18 14 | 233 -535 45 386
ngs 224| 1 1 9 2 -1 -32 .03 10 8 | -998 15 971 1970
sio 298| -1 1 -5 -2 -22 29 .20 16 15 | --- --- --- ---
Table 2.1895.3 GPS week: 1895 Day: 3 MJD: 57512.000
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 2 -5 1 40 -28 -.00 12 11 | -1155 -23 14 131
emr 80| 3 0 1 0 -8 13 .25 12 12 | 4319 -1047 14 139
esa 150| -2 -1 -8 -7 21 -24 -.53 10 10 | 551 -2920 9 146
gfz 207| -3 0 2 -44 -1 13 -.03 11 9 | -249 -442 13 234
grg 124| 4 1 0 -4 14 11 .09 15 14 | 5 -153 14 200
igr n/a| -1 1 -2 5 32 -6 -.08 4 4 | 6566 -741 20 103
jpl 80| 1 1 0 53 43 61 .33 10 10 | 2161 -826 16 128
mit 350| -1 -2 0 -30 -66 -54 -.18 18 15 | -79 -106 45 388
ngs 227| 0 0 10 21 -30 -21 .05 10 8 | -935 -384 1018 2520
sio 298| -4 0 -7 -19 -52 31 .26 19 16 | --- --- --- ---
Table 2.1895.4 GPS week: 1895 Day: 4 MJD: 57513.000
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 244| 2 1 -7 -1 -5 -40 -.01 31 12 | -1674 766 14 133
emr 80| -5 -5 0 15 -9 41 .30 18 15 | 3411 -565 17 158
esa 150| 0 0 -6 -37 -8 12 -.56 10 9 | -1077 1471 10 148
gfz 207| 0 1 2 -11 -7 37 .05 11 10 | -559 248 14 209
grg 119| 4 3 5 -26 83 31 .10 22 14 | -269 351 13 184
igr n/a| 1 1 -2 7 14 10 -.05 5 5 | 5982 -337 19 104
jpl 80| -4 0 0 18 5 10 .39 13 13 | 1622 -675 18 148
mit 350| 1 -2 1 38 -18 12 -.12 17 15 | -351 481 49 388
ngs 226| 3 1 4 -6 23 -5 .08 28 9 | -1858 980 736 2251
sio 294| -3 0 0 47 -42 -123 .19 15 15 | --- --- --- ---
Table 2.1895.5 GPS week: 1895 Day: 5 MJD: 57514.000
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 2 -5 36 8 -17 -.01 16 12 | -1352 582 16 131
emr 80| -2 -8 -1 -5 -25 26 .34 13 13 | 2753 303 17 155
esa 150| 2 2 -5 -6 -1 22 -.53 9 9 | -660 734 10 150
gfz 208| -1 3 0 -23 -11 -2 .08 12 11 | -569 24 14 173
grg 120| 2 1 17 -2 104 62 .22 15 14 | -198 109 17 194
igr n/a| 0 1 -4 15 30 -3 -.04 5 5 | 5534 643 19 106
jpl 80| -2 -1 0 -16 29 -20 .34 11 11 | 712 528 18 126
mit 350| 1 -2 -3 26 -7 -67 -.16 18 16 | -387 -26 66 374
ngs 227| 0 0 5 -18 -54 25 .14 12 8 | -1372 605 1041 2396
sio 301| 0 2 -4 50 10 -83 .01 16 15 | --- --- --- ---
Table 2.1895.6 GPS week: 1895 Day: 6 MJD: 57515.000
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| -1 1 -7 25 25 -10 -.01 11 10 | -586 -629 13 133
emr 80| 1 0 3 45 -18 28 .32 11 11 | 3341 395 17 155
esa 150| 0 0 -5 26 7 22 -.57 9 9 | 782 -4028 9 169
gfz 206| -2 0 0 13 -6 -13 .03 12 11 | -62 -160 11 180
grg 121| 0 1 18 11 56 61 .26 15 14 | 298 -519 15 202
igr n/a| 0 0 -5 10 27 -14 -.05 5 5 | 6540 768 18 98
jpl 80| 2 0 0 22 34 -7 .26 10 10 | 1610 428 16 135
mit 350| 0 -3 0 28 -36 -7 -.15 17 15 | 395 -807 42 355
ngs 224| 0 0 3 -48 -67 -17 .12 10 9 | -685 -488 1072 2087
sio 305| 0 0 -5 -120 12 -36 .04 13 14 | --- --- --- ---
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 3.1895.0 GPS week: 1895 Day: 0 MJD: 57509.000
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 7 6 9 9 4 5 7 7 8 2 | 42 46 37 48 49 43 50 44 46 44 44
2 | 9 10 12 12 11 4 10 14 11 17 4 | 31 30 27 27 28 25 30 32 31 30 27
3 | 7 8 6 10 7 3 8 7 7 9 2 | 37 40 34 37 38 35 42 34 37 40 36
X4 | 4 --- --- --- --- 34 --- --- --- --- 0 | 35 --- --- --- --- 30 --- --- --- --- 35
5 | 9 12 10 16 14 4 11 18 11 13 4 | 43 46 42 35 38 37 43 30 34 39 37
6 | 7 7 4 8 8 5 9 9 6 11 2 | 38 41 32 41 43 34 42 39 40 37 38
7 | 11 10 10 12 15 7 8 48 12 13 6 | 38 36 32 39 38 35 37 47 35 32 31
8 | 9 10 8 10 13 5 9 14 10 16 3 | 35 39 34 37 35 36 39 40 36 47 36
9E | 11 14 6 9 11 3 10 10 9 12 3 | 75 69 66 74 72 70 70 69 73 76 70
10 | 10 7 5 8 12 3 6 12 6 11 3 | 25 31 24 26 23 24 31 21 21 25 23
11 | 8 7 15 10 15 5 9 7 8 10 3 | 40 43 34 43 49 39 48 37 42 39 40
12 | 11 14 7 15 16 4 16 20 12 14 5 | 28 33 23 36 29 25 28 21 28 25 24
13E | 15 10 7 14 14 5 11 15 10 12 4 | 28 27 21 23 32 21 30 28 24 30 24
14E | 16 10 5 10 26 3 9 9 10 14 4 | 29 29 24 32 28 26 31 33 31 41 28
15E | 13 11 8 12 14 3 10 10 11 13 4 | 61 55 61 56 54 55 56 56 57 54 55
16 | 18 17 9 14 17 5 9 12 10 15 4 | 30 30 22 29 26 26 31 26 26 24 24
17 | 8 9 8 10 12 4 11 8 10 12 3 | 34 33 26 36 37 31 35 27 30 29 29
18 | 18 14 12 16 22 5 11 25 14 20 5 | 36 39 32 41 43 31 38 34 36 33 34
19 | 13 11 8 10 13 5 11 11 11 22 4 | 29 28 24 23 29 24 30 20 24 20 21
20 | 14 11 11 16 16 4 11 19 10 14 4 | 36 35 32 41 40 31 35 39 36 33 34
21 | 14 9 11 10 16 3 12 12 12 13 4 | 34 35 31 33 38 29 36 30 31 34 31
22 | 9 10 11 10 14 4 9 11 8 15 3 | 38 38 33 42 46 37 40 34 39 35 36
23E | 20 14 8 17 16 3 12 11 10 14 4 | 31 28 26 32 29 26 31 25 28 35 26
24 | 9 9 5 9 14 3 8 9 6 13 3 | 25 30 21 25 24 22 28 22 25 26 22
25 | 7 12 7 18 16 8 12 7 13 10 4 | 24 28 19 32 25 21 24 22 22 24 21
26 | 11 12 7 12 11 4 10 11 8 9 3 | 29 33 23 30 29 27 33 26 28 29 26
27 | 10 15 6 7 15 4 8 8 8 12 3 | 272 274 273 175 189 275 279 277 275 178 275
28 | 9 11 7 10 17 4 7 11 10 12 3 | 30 28 21 31 32 24 28 25 25 25 24
29 | 19 15 6 13 18 4 13 16 11 13 5 | 35 31 24 24 23 21 27 18 21 21 21
30 | 7 8 7 8 13 4 7 7 8 11 3 | 32 28 24 33 33 27 30 24 29 29 26
31 | 13 12 8 11 18 5 10 37 12 16 5 | 38 43 37 43 42 38 43 41 40 42 36
X32E | 29 --- 10 18 28 8 16 16 17 16 7 | 781 --- 779 785 785 784 702 783 784 785 782
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 9 12 15 4 10 16 10 13 |T 66 44 62 64 65 62 66 64 65 63 63
WRMS | 11 11 8 11 14 4 10 14 9 13 |NE 43 45 38 40 40 39 45 40 41 37 39
MEDI | 10 10 8 10 14 4 10 11 10 13 |MD 35 33 31 36 37 30 35 32 31 33 31
Table 3.1895.1 GPS week: 1895 Day: 1 MJD: 57510.000
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 11 6 11 4 7 11 8 12 3 | 24 34 18 26 29 23 32 24 27 28 25
2 | 8 8 12 13 9 5 8 12 9 15 3 | 26 29 26 22 22 24 29 25 28 26 24
3 | 7 13 7 7 9 3 7 9 7 16 3 | 36 36 32 34 35 34 37 35 35 42 34
X4 | 2 --- --- --- --- 53 --- --- --- --- 0 | 56 --- --- --- --- 35 --- --- --- --- 56
5 | 10 12 11 14 13 5 10 17 10 20 4 | 29 36 27 25 28 26 36 16 26 28 26
6 | 9 11 6 9 9 5 8 10 10 12 3 | 26 32 18 25 30 24 34 25 27 28 26
7 | 12 10 11 12 14 7 12 49 10 18 6 | 32 31 24 28 30 27 34 42 30 23 24
8 | 6 10 8 10 12 4 8 14 10 16 3 | 27 32 26 24 31 26 33 28 27 35 27
9E | 9 10 7 7 11 4 9 10 7 15 3 | 65 67 62 65 67 63 64 63 66 70 65
10 | 7 9 9 7 11 4 10 11 7 17 3 | 21 25 21 23 19 20 24 19 21 22 20
11 | 8 10 17 8 15 5 9 8 11 11 4 | 22 31 23 26 33 23 32 20 26 27 24
12 | 14 16 6 17 17 5 14 21 13 18 5 | 30 32 22 30 21 24 28 20 26 25 23
13E | 12 14 7 13 14 5 11 12 9 13 4 | 27 31 23 26 28 25 29 26 30 32 26
14E | 16 22 8 8 21 6 14 34 9 30 6 | 31 34 25 27 26 26 25 48 28 50 27
15E | 13 18 8 12 16 4 13 14 12 15 4 | 43 49 46 44 39 42 41 42 40 38 42
16 | 17 16 10 12 16 4 10 13 11 17 4 | 26 23 17 18 22 17 22 19 20 19 17
17 | 10 11 8 10 14 3 11 11 8 18 4 | 34 37 30 30 32 30 37 24 32 26 29
18 | 13 15 14 13 16 6 11 23 11 19 5 | 28 31 25 24 27 23 27 22 25 22 23
19 | 13 15 10 9 16 5 11 15 10 25 4 | 27 32 22 20 26 23 30 17 23 16 21
20 | 9 12 11 14 10 5 10 17 12 15 4 | 25 27 22 26 22 22 27 25 28 20 23
21 | 10 9 12 9 11 5 9 11 11 13 3 | 29 29 24 26 26 24 27 22 29 25 24
22 | 9 11 14 8 14 3 9 10 9 20 4 | 24 25 19 21 26 20 26 18 24 21 19
23E | 18 14 8 14 12 4 12 11 9 16 4 | 24 24 20 23 22 22 26 23 23 31 22
24 | 8 14 6 9 9 4 9 9 9 15 3 | 24 25 16 25 21 22 25 20 23 20 20
25 | 8 11 6 9 13 7 11 7 14 11 3 | 21 25 16 25 18 20 23 22 23 24 20
26 | 15 15 7 7 11 5 9 10 11 11 4 | 29 26 20 23 24 22 27 21 26 25 23
27 | 7 16 8 7 11 4 9 10 10 14 3 | 354 356 355 233 231 354 356 357 354 238 355
28 | 9 12 9 9 18 3 11 12 8 15 4 | 24 28 21 22 27 20 28 18 23 23 20
29 | 17 15 8 15 16 4 13 14 12 17 5 | 28 28 16 24 17 20 24 16 21 21 18
30 | 7 11 7 5 9 3 7 9 7 13 3 | 26 29 17 22 24 21 29 19 25 26 22
31 | 10 11 8 10 17 3 9 29 10 16 4 | 30 32 24 29 32 26 34 22 29 27 26
X32E | 83 59 26 34 55 18 --- 26 52 34 17 | 704 653 689 694 699 690 --- 695 692 693 695
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 9 11 14 5 10 17 10 17 |T 61 62 56 55 55 56 41 57 59 56 57
WRMS | 11 13 9 10 13 5 10 14 9 16 |NE 42 44 36 34 34 37 43 37 40 33 38
MEDI | 9 12 8 9 13 4 10 12 10 16 |MD 27 31 23 25 27 24 29 22 27 26 24
Table 3.1895.2 GPS week: 1895 Day: 2 MJD: 57511.000
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 9 5 5 12 6 6 11 9 11 3 | 31 38 28 34 37 31 40 30 40 35 34
2 | 10 12 11 10 11 4 10 14 10 15 4 | 23 25 22 20 18 19 29 23 22 22 20
3 | 8 11 6 8 11 3 11 8 6 14 3 | 36 40 32 33 36 33 41 33 34 42 34
X4 | 1 --- --- --- --- 29 --- --- --- --- 0 | 35 --- --- --- --- 31 --- --- --- --- 35
5 | 12 16 10 13 14 3 12 19 11 17 4 | 33 42 29 23 28 27 38 21 26 32 27
6 | 12 11 5 9 10 3 9 10 8 12 3 | 27 31 23 29 32 25 34 28 29 26 27
7 | 14 13 9 10 16 6 10 50 11 17 6 | 35 33 26 29 31 28 33 47 32 27 26
8 | 13 10 7 8 13 4 9 9 9 14 3 | 31 37 28 27 28 26 36 31 29 40 29
9E | 9 10 6 12 12 3 10 12 7 11 3 | 41 44 41 43 38 40 40 45 40 39 41
10 | 10 11 5 6 10 3 11 12 6 17 3 | 16 24 16 18 15 16 24 17 17 18 16
11 | 10 9 14 8 14 5 7 10 11 9 4 | 29 36 31 33 36 29 38 25 37 34 32
12 | 11 20 6 19 19 4 18 20 11 18 5 | 27 29 21 31 22 22 34 21 24 24 22
13E | 15 16 6 11 20 5 13 12 8 14 4 | 29 32 24 25 30 25 33 27 26 28 26
14E | 21 23 8 9 29 6 10 35 10 29 6 | 34 37 29 30 36 30 36 50 36 49 33
15E | 22 16 10 10 15 4 16 22 6 6 5 | 62 58 60 54 59 57 57 59 59 54 57
16 | 19 24 8 11 14 3 11 14 9 18 5 | 29 30 20 23 22 22 28 25 24 22 21
17 | 11 14 8 11 17 4 13 10 8 14 4 | 28 31 24 26 29 24 31 20 25 23 23
18 | 16 15 10 14 16 4 14 23 12 18 5 | 32 34 31 32 32 29 34 30 34 25 30
19 | 16 12 8 11 16 4 11 12 9 21 4 | 29 33 26 24 26 23 31 20 22 19 22
20 | 9 16 11 16 13 3 14 18 11 16 4 | 30 29 27 30 31 27 33 30 31 25 27
21 | 11 8 11 8 13 3 9 11 9 11 3 | 25 27 24 26 27 23 29 23 27 26 24
22 | 13 10 11 10 17 4 7 11 9 20 4 | 29 31 26 28 33 28 32 25 30 31 26
23E | 19 12 7 12 17 5 12 15 10 14 4 | 25 24 21 22 19 20 25 23 23 27 20
24 | 10 11 6 11 11 5 12 11 7 15 3 | 21 25 18 25 22 20 29 21 22 21 20
25 | 7 12 6 11 16 4 12 10 9 13 3 | 22 22 16 26 23 18 25 20 25 20 20
26 | 15 18 5 7 10 3 8 11 7 12 3 | 24 25 17 23 21 21 27 21 24 24 20
27 | 15 13 5 10 11 3 11 10 7 14 3 | 269 264 266 206 184 266 264 264 268 198 266
28 | 8 14 7 9 19 4 8 10 10 19 4 | 23 26 21 24 27 20 28 20 24 24 21
29 | 17 18 8 11 17 5 12 14 11 14 4 | 28 25 20 24 16 20 26 19 25 23 20
30 | 10 12 7 6 10 3 9 11 9 13 3 | 26 29 20 24 27 22 28 26 27 27 24
31 | 11 14 8 11 17 5 9 25 10 16 4 | 32 35 27 32 33 28 36 23 32 31 28
32E | 120 54 24 31 102 14 27 32 28 29 13 | 9999 982 993 990 9999 989 9999 980 990 981 991
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 25 17 9 12 23 5 12 18 10 16 |T 37 70 64 64 33 63 40 66 67 65 64
WRMS | 12 14 8 10 13 4 12 14 8 15 |NE 38 40 34 34 33 34 41 35 37 33 34
MEDI | 11 13 8 10 14 4 11 12 9 14 |MD 29 31 26 27 28 25 33 25 27 27 26
Table 3.1895.3 GPS week: 1895 Day: 3 MJD: 57512.000
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 7 6 8 5 9 11 5 18 3 | 29 40 26 37 35 30 38 30 36 37 32
2 | 6 10 13 10 11 2 7 16 12 16 4 | 24 25 25 26 18 22 25 27 30 24 22
3 | 9 9 7 6 10 4 8 9 5 19 3 | 40 39 38 39 38 38 40 37 40 48 38
X4 | 4 --- --- --- --- 40 --- --- --- --- 0 | 35 --- --- --- --- 30 --- --- --- --- 33
5 | 11 14 11 15 14 4 10 20 11 17 4 | 38 41 37 32 35 33 38 24 27 33 31
6 | 9 9 8 6 7 5 7 11 10 14 3 | 24 34 26 31 32 29 36 31 39 32 30
7 | 11 13 10 11 16 6 12 50 11 17 6 | 30 29 25 30 31 27 33 41 30 29 24
8 | 13 12 10 9 13 4 11 10 6 23 4 | 34 27 30 29 31 29 30 32 30 48 28
9E | 16 15 10 12 12 3 12 10 10 18 4 | 80 76 77 81 79 79 79 81 80 86 79
10 | 7 9 9 6 11 4 10 17 6 23 3 | 20 19 21 18 19 18 20 21 21 22 16
11 | 11 10 15 8 13 4 12 10 7 18 4 | 25 37 26 33 36 27 36 25 33 36 29
12 | 10 14 8 19 17 5 15 20 14 16 5 | 21 24 15 28 24 16 25 12 22 17 16
13E | 9 13 7 11 15 4 10 13 8 14 3 | 26 28 24 25 30 22 26 28 28 32 24
14E | 17 13 10 10 22 6 14 42 10 42 7 | 28 26 26 28 22 25 25 55 29 60 26
15E | 18 11 11 14 13 6 10 14 10 16 4 | 40 37 34 33 30 32 38 36 36 36 33
16 | 11 14 10 11 16 5 10 11 9 17 4 | 25 20 20 24 24 20 22 21 25 21 19
17 | 10 10 9 9 14 4 7 10 10 15 3 | 30 27 27 30 33 26 29 26 28 27 26
18 | 17 12 14 14 18 5 10 24 11 21 5 | 31 29 24 28 24 23 27 29 29 24 24
19 | 14 10 11 8 16 4 7 12 12 22 4 | 28 25 25 23 29 23 27 21 23 18 21
20 | 6 13 14 15 13 4 13 17 11 19 4 | 26 28 25 38 25 26 29 29 34 24 26
21 | 9 8 11 10 11 3 7 11 10 11 3 | 26 27 21 27 22 22 25 24 27 26 22
22 | 11 10 12 9 13 4 11 11 8 22 4 | 24 32 23 31 27 26 28 23 31 27 24
23E | 14 13 10 12 20 4 11 11 8 20 4 | 21 21 23 24 21 20 19 24 22 33 19
24 | 10 10 8 8 12 5 6 10 9 16 3 | 20 25 14 22 23 17 23 19 25 20 18
25 | 7 9 8 7 17 3 9 8 9 13 3 | 19 21 14 24 26 16 21 16 22 19 17
26 | 14 12 7 7 12 4 9 9 9 9 3 | 25 24 19 24 23 21 25 19 27 24 21
X27 | 18 40 24 21 --- 14 34 20 21 28 10 | 807 809 805 659 --- 802 811 804 805 653 805
28 | 7 12 10 8 20 4 12 9 9 17 4 | 23 22 20 22 29 19 23 18 24 29 19
29 | 16 20 9 14 19 3 12 14 15 17 5 | 30 25 19 24 21 18 22 13 24 18 17
30 | 9 9 8 6 12 4 8 15 6 13 3 | 27 25 18 23 26 22 26 20 24 27 20
31 | 9 10 11 11 16 4 11 19 9 18 4 | 30 33 28 33 34 29 35 23 32 34 28
X32E | 159 --- 22 33 103 19 --- 28 38 23 15 | 653 --- 619 616 627 617 --- 614 607 614 611
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 10 11 15 4 10 18 10 19 |T 73 55 70 69 49 68 56 71 73 70 68
WRMS | 11 12 10 9 14 4 10 15 8 16 |NE 60 62 58 55 26 57 63 58 62 54 57
MEDI | 10 11 10 10 13 4 10 12 10 17 |MD 27 27 25 28 27 25 27 25 29 29 24
Table 3.1895.4 GPS week: 1895 Day: 4 MJD: 57513.000
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 14 6 6 11 5 8 11 8 11 3 | 26 42 25 31 35 27 38 33 32 35 30
2 | 11 14 12 11 10 4 13 14 11 15 4 | 20 26 20 21 17 18 29 25 23 23 19
3 | 10 12 4 8 9 4 8 5 8 13 3 | 35 37 31 31 32 31 36 32 33 35 32
X4 | 5 --- --- --- --- 36 --- --- --- --- 0 | 37 --- --- --- --- 27 --- --- --- --- 34
5 | 9 16 11 13 14 4 14 20 10 18 4 | 37 45 34 30 32 31 42 24 30 33 32
6 | 10 10 5 6 7 5 8 8 7 10 2 | 24 33 23 31 31 25 36 28 30 32 28
7 | 12 15 11 11 16 8 9 50 13 15 6 | 27 33 23 27 27 24 29 42 28 22 21
8 | 14 13 7 9 13 5 9 4 9 15 3 | 30 31 23 26 29 25 30 25 27 37 26
X9E | 19 21 7 13 15 5 --- 8 16 11 5 | 65 67 61 69 62 62 --- 57 62 69 62
10 | 14 12 9 6 14 6 10 12 9 12 3 | 23 30 24 22 22 20 25 21 23 27 21
11 | 13 13 14 9 17 5 8 9 8 9 4 | 26 37 24 28 35 24 35 27 29 30 27
12 | 12 25 8 19 20 4 17 21 11 19 6 | 23 32 19 26 22 18 31 17 20 15 18
13E | 10 15 6 9 14 4 12 13 8 16 4 | 21 31 22 23 26 20 28 26 20 29 22
14E | 22 35 11 10 22 8 14 32 13 30 7 | 30 46 28 29 26 24 27 49 28 54 27
15E | 15 12 9 14 17 6 13 12 9 11 4 | 35 31 31 26 28 26 30 28 26 26 27
16 | 15 22 8 12 15 5 9 13 9 14 4 | 26 24 16 20 20 18 24 19 20 22 17
17 | 9 14 9 9 15 4 11 11 9 13 3 | 24 23 16 21 25 18 24 16 20 17 17
18 | 16 17 13 13 20 5 12 25 12 20 5 | 28 31 23 22 16 17 28 19 19 19 18
19 | 14 11 9 9 15 4 10 12 9 17 4 | 26 21 21 19 24 18 25 16 19 14 17
20 | 9 14 12 13 13 4 13 19 9 18 4 | 19 27 22 26 19 19 27 23 22 18 19
21 | 10 9 10 9 13 4 10 12 9 16 3 | 22 24 19 20 19 17 25 19 17 26 19
22 | 10 14 11 11 14 4 10 9 10 17 4 | 23 31 22 26 24 22 29 22 23 25 22
23E | 20 15 8 12 17 4 13 9 10 14 4 | 27 29 27 29 27 26 29 27 28 36 26
24 | 7 13 8 8 13 3 11 6 9 14 3 | 19 26 18 20 20 17 28 21 20 20 19
25 | 9 16 8 9 18 3 12 9 7 15 4 | 20 29 22 26 22 19 28 22 20 24 21
26 | 12 14 6 8 14 5 9 8 9 11 3 | 28 24 18 24 22 21 28 21 24 27 21
27 | 13 16 7 6 13 5 12 8 8 11 3 | 431 435 427 509 590 430 436 432 427 513 432
28 | 9 16 7 6 18 4 10 8 9 12 3 | 19 25 14 17 25 16 24 17 20 19 16
29 | 15 23 7 12 20 5 16 13 10 14 5 | 29 31 21 23 16 19 29 17 22 19 19
30 | 10 13 6 6 11 4 9 15 7 9 3 | 20 27 11 18 22 18 24 22 21 22 17
31 | 13 15 10 11 18 4 14 25 11 14 5 | 36 37 27 36 36 31 42 24 36 36 31
32E | 156 48 24 29 88 14 36 23 149 20 13 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 31 18 10 11 22 5 13 17 28 15 |T 40 45 37 42 45 36 43 39 38 44 37
WRMS | 12 15 9 10 14 5 13 14 9 15 |NE 43 47 39 46 49 38 47 40 41 46 39
MEDI | 12 14 8 9 15 4 11 12 9 14 |MD 26 31 22 26 25 21 29 23 23 26 21
Table 3.1895.5 GPS week: 1895 Day: 5 MJD: 57514.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1M | 9 9 7 8 15 5 9 10 7 11 3 | 27 39 22 29 41 26 36 32 33 31 31
2 | 11 12 10 14 12 5 9 15 11 12 4 | 22 21 20 17 22 17 24 23 24 17 19
3M | 11 8 7 9 16 5 9 8 8 12 3 | 43 46 41 42 43 41 45 42 41 44 42
X4 | 4 --- --- --- --- 61 --- --- --- --- 0 | 56 --- --- --- --- 38 --- --- --- --- 58
5 | 11 12 12 14 17 3 10 17 11 17 4 | 35 38 28 28 28 29 35 22 25 31 28
6 | 8 11 7 7 12 6 8 7 7 12 3 | 24 33 17 26 35 22 32 23 27 32 26
7 | 11 12 11 12 15 7 11 49 10 17 6 | 27 33 21 26 28 23 30 41 28 20 21
8 | 10 11 8 8 13 6 13 7 6 15 3 | 29 35 25 25 31 26 34 26 28 34 28
9E | 37 25 14 16 26 8 19 17 40 14 8 | 119 127 123 121 133 122 129 126 126 119 123
10 | 7 8 6 6 10 5 9 18 9 20 3 | 15 21 14 14 15 14 20 21 17 24 15
11 | 9 9 15 8 17 4 10 11 10 15 4 | 22 32 22 22 36 21 32 23 26 31 24
12 | 11 14 10 22 18 5 16 22 11 17 5 | 23 23 17 25 23 17 26 20 22 15 16
13E | 12 15 6 11 17 4 10 14 11 13 4 | 22 31 18 19 25 20 26 25 21 25 22
14E | 13 11 10 12 14 5 10 20 9 22 4 | 27 28 25 26 27 24 25 26 26 29 25
15E | 8 13 8 13 15 3 14 8 7 11 3 | 26 32 29 24 24 26 30 27 25 26 27
16 | 17 16 6 14 12 4 11 14 10 16 4 | 26 26 18 21 22 20 27 23 24 17 20
17 | 9 11 8 8 15 7 12 10 10 17 4 | 23 25 17 22 27 20 26 16 21 26 20
18 | 16 15 11 15 16 5 13 29 12 22 5 | 25 28 21 20 25 18 25 22 21 15 19
19 | 12 16 8 10 13 8 9 10 10 19 4 | 24 25 17 18 25 19 22 17 17 22 18
20 | 12 14 11 13 15 5 11 19 9 18 4 | 21 27 23 21 28 20 25 20 23 16 21
21 | 13 10 11 10 14 4 8 20 10 17 4 | 21 22 21 18 23 19 24 22 21 22 19
22M | 19 9 11 12 17 3 8 10 10 15 4 | 22 30 25 26 32 22 30 26 26 25 24
23E | 46 13 11 14 20 4 10 13 11 15 6 | 44 27 21 27 24 22 27 26 24 30 21
24 | 11 10 6 10 13 4 9 15 6 14 3 | 23 29 17 22 20 20 25 27 22 26 22
25 | 8 13 6 9 15 3 11 11 10 10 3 | 23 26 19 25 20 20 26 22 22 24 20
26 | 12 12 4 8 12 4 8 11 7 8 3 | 26 27 18 22 26 21 26 21 25 21 22
X27 | 10 14 5 --- 14 7 9 17 8 --- 4 | 573 569 572 --- 411 572 573 571 574 --- 572
28 | 10 10 7 9 15 4 11 13 8 22 4 | 19 25 15 19 26 16 23 19 19 19 17
29 | 16 21 7 15 21 4 14 14 11 12 5 | 28 25 17 19 20 17 24 18 21 19 17
30 | 9 12 5 9 9 4 10 10 5 9 3 | 22 34 16 21 23 20 27 22 25 24 22
31 | 11 13 7 11 14 4 11 29 9 16 4 | 37 41 34 36 38 33 40 32 34 31 33
X32E | 116 --- 19 30 59 14 --- 28 113 26 16 | 9999 --- 9999 9999 9999 9999 --- 9999 9999 9999 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 13 9 12 15 5 11 18 12 16 |T 47 50 43 26 43 43 49 46 46 28 44
WRMS | 12 13 9 11 14 5 11 16 8 15 |NE 49 52 44 22 43 45 52 47 48 23 46
MEDI | 11 12 8 11 15 5 10 14 10 15 |MD 25 28 21 22 26 21 26 23 24 25 22
Table 3.1895.6 GPS week: 1895 Day: 6 MJD: 57515.000
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 7 10 6 9 4 8 11 4 8 2 | 34 40 22 38 45 33 40 39 38 39 35
2 | 7 8 12 15 12 3 9 11 13 12 4 | 23 26 21 27 26 21 26 27 26 23 22
3 | 9 7 7 8 11 4 8 9 6 8 2 | 44 46 38 39 43 41 47 42 43 46 42
X4 | 4 --- --- --- --- 36 --- --- --- --- 0 | 36 --- --- --- --- 36 --- --- --- --- 36
5 | 9 10 11 15 15 5 8 17 9 14 4 | 45 49 42 36 36 40 46 34 37 45 40
6 | 7 7 8 9 9 5 8 10 8 11 3 | 29 38 25 35 41 30 36 36 39 34 33
7 | 14 13 10 13 14 7 9 48 11 16 6 | 28 30 21 25 27 23 28 41 29 21 21
8 | 12 11 9 8 15 4 9 10 10 12 3 | 32 31 29 28 31 28 31 25 30 33 27
9E | 19 8 6 15 18 11 10 10 12 10 4 | 100 98 104 104 101 101 96 98 103 97 99
10 | 7 6 6 9 8 3 6 19 9 15 3 | 24 27 23 23 22 23 26 25 23 31 22
11 | 9 7 18 10 16 4 8 8 8 15 4 | 30 38 28 37 47 32 38 35 35 42 34
12 | 16 12 10 22 18 6 13 25 13 14 5 | 27 26 17 29 22 18 24 21 20 17 17
13E | 10 13 6 13 13 5 10 11 11 12 4 | 21 28 16 19 29 20 25 25 23 31 22
14E | 9 19 9 12 17 5 11 13 10 14 4 | 22 27 18 21 25 18 19 17 20 24 17
15E | 9 13 7 14 20 4 12 9 8 8 4 | 32 35 31 28 29 29 32 34 31 35 31
16 | 9 15 8 14 14 3 12 15 11 15 4 | 21 23 14 18 20 17 23 19 20 16 16
17 | 8 8 8 8 17 7 11 12 10 14 3 | 25 23 19 23 30 21 25 20 21 29 20
18 | 13 11 11 15 18 5 10 25 11 20 5 | 24 27 21 26 34 20 25 23 22 21 22
19 | 13 7 9 10 17 7 13 10 11 16 4 | 26 22 21 20 27 21 24 19 19 24 18
20 | 7 12 12 15 17 5 10 16 10 20 4 | 26 29 28 36 41 25 28 29 30 30 28
21 | 12 9 11 11 13 5 8 16 11 14 4 | 25 26 22 27 29 20 26 27 25 25 23
22 | 9 10 12 11 14 5 9 15 10 14 4 | 28 30 24 31 36 26 30 34 29 26 27
23E | 7 13 9 10 16 4 12 11 8 10 3 | 33 37 38 39 49 36 37 42 38 44 39
24 | 7 8 6 13 14 5 7 20 8 10 3 | 19 25 11 20 19 18 22 29 20 22 18
25 | 5 9 6 11 17 3 12 9 10 10 3 | 18 25 12 24 24 18 23 22 18 23 19
26 | 8 9 6 9 14 4 9 8 7 7 3 | 24 27 17 21 22 21 26 19 24 23 21
27 | 8 24 7 7 13 5 8 8 13 12 4 | 456 457 455 515 346 452 453 452 454 510 453
28 | 7 8 8 11 15 5 8 12 10 17 3 | 18 22 12 20 24 15 19 16 19 16 15
29 | 12 17 7 15 23 4 12 12 11 11 4 | 23 21 15 20 22 16 21 16 17 22 16
30 | 9 8 7 9 13 4 6 12 7 8 3 | 22 27 13 20 23 19 24 21 23 24 20
31 | 6 10 10 11 11 4 11 28 11 12 4 | 30 36 25 30 31 27 32 30 28 28 27
32E | 26 12 7 14 19 4 14 14 16 14 5 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 9 12 15 5 10 17 10 13 |T 43 46 39 45 43 40 45 43 43 46 41
WRMS | 10 11 9 11 14 5 10 15 9 14 |NE 44 47 40 48 42 41 46 44 44 48 42
MEDI | 9 10 8 11 15 5 9 12 10 12 |MD 26 27 21 27 29 23 26 27 25 26 22
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 4.1895 GPS week: 1895 MJD: 57509.0-57515.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2985 |U 5 6 13 |U 6 9 24 |U 7 8 18 |
emr | emr 2934 | 6 8 16 |U 7 9 38 | 9 9 21 |
esa | esa 2976 | 5 6 14 |U 6 9 26 | 8 8 19 |
gfz | gfz 2962 |U 5 5 15 |U 7 10 31 |U 8 8 20 |
grg | grg 2960 |U 6 6 17 |U 7 11 30 | 11 11 24 |
igr | igr 2962 | 5 6 14 | 6 8 26 | 8 9 19 |
igs | igs 2975 | 5 6 14 | 6 9 24 | 8 8 19 |
jpl | jpl 2921 | 6 7 15 |U 7 9 36 | 9 9 22 |
mit | mit 2976 | 6 7 15 |U 8 11 38 |U 10 11 22 |
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 5.1895.0 GPS week: 1895 Day: 0 MJD: 57509.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 6 6 16 | 6 7 25 | 5 6 14 |
emr | emr 2880 | 7 6 14 | 7 8 29 | 7 6 16 |
esa | esa 2976 | 6 6 14 | 6 7 29 | 5 5 14 |
gfz | gfz 2976 | 5 6 15 | 7 8 30 | 5 5 15 |
grg | grg 2973 | 5 7 19 | 7 13 39 | 8 6 20 |
igr | igr 2976 | 6 7 16 | 6 7 28 | 5 5 15 |
igs | igs 2976 | 6 7 15 | 6 7 26 | 5 5 15 |
jpl | jpl 2976 | 7 9 16 | 6 7 30 | 7 7 19 |
mit | mit 2976 | 6 8 23 | 8 9 35 | 11 12 24 |
Table 5.1895.1 GPS week: 1895 Day: 1 MJD: 57510.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 10 12 | 5 8 20 | 6 8 21 |
emr | emr 2976 | 6 11 14 | 5 8 22 | 8 8 23 |
esa | esa 2976 | 5 9 12 | 4 6 17 | 7 8 22 |
gfz | gfz 2976 | 5 10 14 | 5 9 18 | 7 8 22 |
grg | grg 2976 | 5 10 16 | 5 8 22 | 10 10 30 |
igr | igr 2976 | 6 10 14 | 4 7 16 | 7 9 23 |
igs | igs 2976 | 5 10 12 | 4 7 16 | 7 8 23 |
jpl | jpl 2880 | 6 10 13 | 5 6 21 | 9 10 24 |
mit | mit 2976 | 7 11 12 | 5 7 20 | 8 10 25 |
Table 5.1895.2 GPS week: 1895 Day: 2 MJD: 57511.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 15 | 6 7 24 | 8 9 16 |
emr | emr 2976 | 7 5 21 | 7 7 31 | 9 10 19 |
esa | esa 2976 | 6 4 17 | 7 11 33 | 8 8 19 |
gfz | gfz 2975 | 5 4 15 | 8 16 24 | 8 8 16 |
grg | grg 2970 | 7 4 20 | 7 10 30 | 13 11 23 |
igr | igr 2976 | 6 4 17 | 6 9 31 | 9 9 18 |
igs | igs 2976 | 6 4 17 | 7 10 30 | 9 9 18 |
jpl | jpl 2976 | 7 5 19 | 8 9 29 | 10 8 20 |
mit | mit 2976 | 6 3 14 | 6 11 32 | 11 12 23 |
Table 5.1895.3 GPS week: 1895 Day: 3 MJD: 57512.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 3 8 | 5 7 26 | 9 11 18 |
emr | emr 2880 | 5 6 12 | 6 6 27 | 12 13 25 |
esa | esa 2976 | 4 5 7 | 6 8 25 | 10 11 20 |
gfz | gfz 2976 | 4 4 9 | 7 8 29 | 11 12 22 |
grg | grg 2878 | 5 5 15 | 10 12 40 | 14 18 31 |
igr | igr 2976 | 4 4 7 | 6 7 22 | 10 12 21 |
igs | igs 2976 | 4 3 7 | 6 7 23 | 11 13 22 |
jpl | jpl 2880 | 5 4 9 | 7 6 27 | 11 13 26 |
mit | mit 2976 | 6 9 17 | 8 9 27 | 12 15 23 |
Table 5.1895.4 GPS week: 1895 Day: 4 MJD: 57513.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 4 9 | 6 11 23 | 5 4 17 |
emr | emr 2976 | 5 7 14 | 5 9 33 | 10 4 24 |
esa | esa 2976 | 4 3 11 | 6 11 30 | 6 4 18 |
gfz | gfz 2976 | 3 3 12 | 7 12 29 | 6 4 17 |
grg | grg 2975 | 4 3 12 | 7 12 23 | 9 9 22 |
igr | igr 2973 | 3 4 10 | 5 11 29 | 6 5 17 |
igs | igs 2976 | 3 4 10 | 6 11 26 | 6 4 17 |
jpl | jpl 2880 | 5 7 10 | 7 10 34 | 7 4 19 |
mit | mit 2976 | 4 3 8 | 8 15 37 | 8 7 19 |
Table 5.1895.5 GPS week: 1895 Day: 5 MJD: 57514.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 5 7 14 | 5 11 29 | 7 9 20 |
emr | emr 2880 | 5 9 21 | 14 16 94 | 9 11 21 |
esa | esa 2976 | 5 5 16 | 6 11 24 | 8 11 18 |
gfz | gfz 2879 | 6 7 18 | 9 10 59 | 8 9 23 |
grg | grg 2975 | 7 5 19 | 7 12 27 | 11 11 22 |
igr | igr 2882 | 4 6 16 | 8 10 33 | 7 9 20 |
igs | igs 2972 | 4 6 17 | 6 11 24 | 8 10 20 |
jpl | jpl 2880 | 6 7 20 | 12 17 86 | 9 9 21 |
mit | mit 2976 | 6 5 18 | 16 16 92 | 9 12 17 |
Table 5.1895.6 GPS week: 1895 Day: 6 MJD: 57515.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 18 | 7 8 23 | 9 10 20 |
emr | emr 2976 | 6 10 18 | 6 9 29 | 12 10 20 |
esa | esa 2976 | 7 7 19 | 6 9 25 | 10 11 22 |
gfz | gfz 2976 | 5 5 19 | 7 8 28 | 10 9 23 |
grg | grg 2975 | 6 5 19 | 8 11 28 | 12 13 25 |
igr | igr 2975 | 6 7 18 | 6 8 24 | 10 11 21 |
igs | igs 2976 | 6 6 17 | 6 9 24 | 10 10 21 |
jpl | jpl 2976 | 7 7 20 | 6 11 27 | 11 10 23 |
mit | mit 2976 | 6 6 17 | 6 8 23 | 10 11 23 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1895 GPS week: 1895 MJD: 57509.500-57515.500
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 -16 87 106 4 | 11 23
| 25 14 62 150 4 | 2
emr uuxuu | 9 31 -328 100 -8 | 31 39
| 49 50 379 156 10 | 4
esa uuuuu | -27 0 -7 -118 0 | 21 30
| 18 14 46 123 10 | 3
gfz uuuuu | -11 25 -61 -192 -1 | 18 28
| 18 16 123 134 5 | 2
grg uuuxx | -52 -10 1 82 4 | 54 60
| 32 17 59 243 28 | 2
igr xxxxx | -27 2 -24 27 1 | 1 21
| 16 16 82 102 5 | 3
irf xxxxx | 10 -6 -29 19 -3 | 2 21
| 10 8 34 64 3 | 2
jpl uuuuu | -7 -25 -62 138 -10 | 47 51
| 23 16 101 133 15 | 2
mit uuuuu | 9 -10 -33 30 -1 | 29 35
| 16 20 86 133 5 | 2
ngs uuuxu | 54 0 37 188 2 | 9 23
| 25 33 134 247 6 | 2
sio uuuxx | 48 3 56 162 8 | 89 91
| 11 25 74 248 21 | 8
Table 7.1895.0 GPS week: 1895 Day: 0 MJD: 57509.500
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 | -52 -32 60 32 5 | 11 17
emr uuxuu | 5 24 33 127 -16 | 38 41
esa uuuuu | -10 3 51 -60 3 | 20 24
gfz uuuuu | 8 16 65 -76 -4 | 19 24
grg uuuxx | -49 10 4 107 27 | 50 58
igr xxxxx | -15 28 -110 -9 6 | -2 16
irf xxxxx | -4 -11 -16 -60 2 | 2 17
jpl uuuuu | -17 -1 -58 95 12 | 47 50
mit uuuuu | -3 4 -44 -157 6 | 29 33
ngs uuuxu | 43 -6 -136 32 -5 | 12 18
sio uuuxx | 61 -22 101 72 27 | 78 81
Table 7.1895.1 GPS week: 1895 Day: 1 MJD: 57510.500
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 | -31 -9 79 119 8 | 6 20
emr uuxuu | -61 -39 47 144 -12 | 31 39
esa uuuuu | -39 -8 24 -165 9 | 16 25
gfz uuuuu | 6 28 -74 -257 -2 | 14 26
grg uuuxx | -37 -15 50 139 -22 | 53 58
igr xxxxx | -13 13 -28 31 8 | -4 21
irf xxxxx | 10 -3 -41 -73 -3 | -1 22
jpl uuuuu | 38 -37 -50 304 -15 | 44 48
mit uuuuu | -12 5 -66 -135 -6 | 25 32
ngs uuuxu | 75 45 14 157 -5 | 6 22
sio uuuxx | 45 27 26 -149 23 | 78 80
Table 7.1895.2 GPS week: 1895 Day: 2 MJD: 57511.500
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 | -11 -7 179 242 2 | 11 25
emr uuxuu | -44 68 -723 -41 -19 | 34 42
esa uuuuu | -20 -18 -11 -97 8 | 22 31
gfz uuuuu | -2 2 37 -143 6 | 19 30
grg uuuxx | -20 -8 -47 304 -11 | 57 62
igr xxxxx | -23 0 -74 95 1 | 2 23
irf xxxxx | 8 -12 -75 65 -8 | 4 23
jpl uuuuu | -11 -11 -84 90 4 | 48 52
mit uuuuu | 4 -32 -126 103 -6 | 30 36
ngs uuuxu | 54 25 -27 420 -3 | 10 25
sio uuuxx | 43 -27 112 256 14 | 87 90
Table 7.1895.3 GPS week: 1895 Day: 3 MJD: 57512.500
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 | -49 3 146 268 6 | 11 25
emr uuxuu | 32 35 -258 335 -3 | 31 40
esa uuuuu | -56 0 -84 -351 7 | 22 32
gfz uuuuu | -41 25 -30 -449 -9 | 19 30
grg uuuxx | -22 -2 34 307 -18 | 55 60
igr xxxxx | -33 4 -76 87 -6 | 3 23
irf xxxxx | 1 -11 18 14 -5 | 4 23
jpl uuuuu | -4 -41 -41 342 -11 | 48 52
mit uuuuu | -1 -5 72 -11 -2 | 30 36
ngs uuuxu | 99 -10 -72 387 0 | 9 24
sio uuuxx | 51 -3 152 -159 24 | 90 93
Table 7.1895.4 GPS week: 1895 Day: 4 MJD: 57513.500
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 -24 96 195 1 | 13 25
emr uuxuu | 4 104 -850 -136 -16 | 31 40
esa uuuuu | -27 22 -7 -154 -1 | 24 33
gfz uuuuu | -8 25 32 -47 0 | 20 30
grg uuuxx | -48 8 -108 229 -21 | 55 60
igr xxxxx | -10 2 -61 172 -2 | 4 22
irf xxxxx | 9 -12 -4 98 -2 | 4 23
jpl uuuuu | -15 -42 -259 78 -9 | 49 53
mit uuuuu | 23 -45 75 181 4 | 31 37
ngs uuuxu | 36 -25 104 495 6 | 10 24
sio uuuxx | 42 -10 70 348 12 | 95 97
Table 7.1895.5 GPS week: 1895 Day: 5 MJD: 57514.500
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 -32 -11 54 -4 | 12 24
emr uuxuu | 58 47 -548 67 8 | 28 37
esa uuuuu | -4 16 -45 26 -14 | 24 32
gfz uuuuu | -25 56 -221 -200 3 | 18 28
grg uuuxx | -108 -40 36 -251 22 | 54 59
igr xxxxx | -46 -23 82 -54 0 | 4 21
irf xxxxx | 22 3 -15 53 -3 | 2 21
jpl uuuuu | -38 -21 -21 -19 -19 | 47 51
mit uuuuu | 22 -2 -4 125 -1 | 30 35
ngs uuuxu | 28 -51 260 -121 10 | 9 23
sio uuuxx | 64 25 -18 482 -22 | 97 99
Table 7.1895.6 GPS week: 1895 Day: 6 MJD: 57515.500
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 | -56 -9 61 -167 6 | 10 23
emr uuxuu | 71 -24 3 204 2 | 26 35
esa uuuuu | -30 -12 23 -26 -14 | 21 31
gfz uuuuu | -12 24 -235 -171 0 | 16 27
grg uuuxx | -82 -20 40 -262 47 | 55 60
igr xxxxx | -47 -11 98 -131 3 | 2 21
irf xxxxx | 24 6 -68 38 -1 | 0 20
jpl uuuuu | -5 -20 78 74 -33 | 44 49
mit uuuuu | 29 5 -136 101 -2 | 28 34
ngs uuuxu | 41 25 119 -53 9 | 8 23
sio uuuxx | 33 35 -52 284 -22 | 95 98
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