[IGSREPORT-22715] Wk 1789 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat May 10 05:39:56 PDT 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1789 (Apr 20, 2014 - Apr 26, 2014)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1789[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1789[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1789[0-6].cls IGS GPS clock combination summary report.
igs17897.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17897.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 32
0 | ESA | 32 PIMO PIMO
0 | GFZ | 1 1 HNLC
0 | GRG | 12 HYDE HYDE MOBS NTUS REUN
0 | JPL | 32
0 | MIT | DAV1 MDVJ
1 | COD | 32 ARTU BJFS GUAT KARR
1 | EMR | WUHN YAKT
1 | ESA | 32 BJFS IRKJ IRKJ TIXI UNSA
1 | GFZ | 1 2 1 BJFS
1 | GRG | ARTU IRKJ WUHN ARTU BJFS IRKJ WUHN
1 | MIT | 21 21 DAV1 MAC1 DAV1 FLIN KOKB MAC1 MDVJ
2 | COD | 32 WUHN WUHN
2 | EMR | MCM4
2 | ESA | 32 UNSA WUHN
2 | GFZ | 1 1 IRKJ WUHN MAL2 WUHN YIBL
2 | GRG | 12 FAA1 GOPE HYDE MAL2 RBAY FAA1 GOPE HYDE MAL2 RBAY
2 | JPL | 10 32 SEY1
2 | MIT | HYDE IRKJ MDVJ HYDE MDVJ
3 | COD | WUHN
3 | EMR | 32 WUHN
3 | ESA | WUHN UNSA
3 | GFZ | 1 2 1 32 ALGO WSRT WUHN ALGO
3 | GRG | 32 BOGT DRAG MAL2 NICO WUHN BOGT DRAG MAL2 NICO WSRT
3 | GRG | WUHN
3 | JPL | 32
3 | MIT | 10 MDVJ NTUS GOPE MDVJ
4 | COD | ARTU
4 | EMR | 32 MCM4 NYAL
4 | ESA | SEY1
4 | GFZ | 1 2 1 32 HNLC MATE WUHN
4 | GRG | 32 ARTU MOBS RBAY WUHN ARTU CHUM MOBS RBAY WUHN
5 | EMR | 32 MCM4
5 | ESA | UNSA
5 | GFZ | 1 2 1 28 32 BOR1 HNLC
5 | GRG | 13 28 13 28 FAA1 FAA1
5 | MIT | MDVJ MATE MDVJ
6 | EMR | WUHN WUHN
6 | ESA | IRKJ IRKJ UNSA
6 | GFZ | 1 2 1 WUHN WUHN
6 | GRG | BOR1 IRKJ DAEJ
6 | JPL | 32
6 | MIT | 23 27 31 23 25 27 DRAG MDVJ MONP NTUS MDVJ
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
5 | GRG | 6
6 | GRG | 6
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G06 | | | | | 4 | | |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.8 1.1 -.5 -2 9 -33 .58
EMR | 0 | -3.0 -1.5 19.5 -14 19 -55 .43
ESA | 0 | -.4 .6 -.8 -21 0 6 .28
GFZ | 0 | .5 .2 -1.7 -7 -43 -6 .15
GRG | 0 | 3.2 -4.8 4.2 0 9 -20 1.01
JPL | 0 | 2.7 -8.1 13.5 -36 40 33 .48
MIT | 0 | -5.0 -9.5 21.3 131 16 -7 .61
NGS | 0 | 4.9 -7.9 23.3 -79 -88 -9 .64
COD | 1 | -.7 .7 -1.4 -9 -2 -35 .68
EMR | 1 | -2.2 -1.4 14.1 -11 18 -61 .62
ESA | 1 | 1.1 -.1 -1.0 -17 -12 1 .57
GFZ | 1 | .2 -.3 -1.8 -17 -42 -3 .31
GRG | 1 | -3.3 -6.7 7.8 -23 12 -11 .93
JPL | 1 | .5 -3.9 21.5 -29 -35 46 .52
MIT | 1 | -6.5 -3.5 22.3 106 9 -131 .68
NGS | 1 | .9 -8.5 27.0 -93 -76 -29 .67
COD | 2 | -1.5 .4 -1.4 -31 20 -32 .61
EMR | 2 | .6 -4.3 16.2 -14 15 -58 .73
ESA | 2 | 1.3 .6 -1.3 -4 -13 16 .52
GFZ | 2 | .9 -.2 -2.2 -22 -56 -19 .17
GRG | 2 | 2.9 -6.2 10.4 -9 24 -13 1.12
JPL | 2 | 9.3 -7.0 20.4 -3 7 15 .47
MIT | 2 | -1.8 -3.0 20.5 66 34 -58 .60
NGS | 2 | 4.9 -9.7 22.6 -87 -83 -11 .76
COD | 3 | -1.5 .5 -2.0 -31 16 -29 .62
EMR | 3 | .5 -1.4 13.6 -20 24 -70 .72
ESA | 3 | .6 1.1 -.4 -11 -2 21 .28
GFZ | 3 | 1.0 .1 -1.7 -25 -45 -20 .05
GRG | 3 | 4.4 .1 6.1 -1 0 4 1.09
JPL | 3 | -.8 -3.5 22.1 -78 5 6 .52
MIT | 3 | 2.3 .4 18.2 44 15 -2 .69
NGS | 3 | 4.1 -4.2 22.9 -84 -62 5 .89
COD | 4 | -1.3 -.4 -2.1 -50 9 -31 .75
EMR | 4 | .1 -7.9 12.2 -11 27 -56 .53
ESA | 4 | .8 .8 -1.1 -5 -11 18 .56
GFZ | 4 | .9 -.1 -1.5 -25 -39 -8 .01
GRG | 4 | 7.2 -5.9 10.4 -9 23 -26 .87
JPL | 4 | 4.8 -7.2 21.3 -78 10 17 .21
MIT | 4 | 2.9 -3.5 13.1 -3 11 -37 .79
NGS | 4 | 1.1 -13.5 19.8 -119 -45 -46 .95
COD | 5 | -.6 .3 -1.5 -16 3 -52 .62
EMR | 5 | 3.3 -.6 17.1 -18 8 -54 .47
ESA | 5 | .5 .3 -.7 -15 -14 13 .18
GFZ | 5 | .4 -.2 -1.2 -25 -25 -3 -.13
GRG | 5 | 2.3 -1.0 -1.3 9 -13 -24 .54
JPL | 5 | 4.1 -2.3 22.2 -37 85 -35 -.10
MIT | 5 | -.1 .6 16.6 37 28 -39 .60
NGS | 5 | 2.3 -1.9 23.5 -85 -61 4 .52
COD | 6 | -.3 .3 -.4 -28 4 -33 .70
EMR | 6 | 5.0 -6.0 20.7 -9 15 -68 .55
ESA | 6 | .0 .3 -1.1 -13 -1 13 .15
GFZ | 6 | -.1 .0 -2.2 -14 -35 -16 .29
GRG | 6 | 4.4 -5.8 16.0 16 21 -16 .98
JPL | 6 | 2.5 -.8 23.9 -77 -10 34 .40
MIT | 6 | 4.7 1.7 17.2 47 13 -11 .68
NGS | 6 | 2.4 -6.5 21.9 -108 -59 -12 .83
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1789.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1789.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 2.1789.[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 3.1789.[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 5.1789.0-6). 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 1789 summary. (Apr 20, 2014 - Apr 26, 2014)
Table 1.1789.a GPS week: 1789 MJD: 56767.000-56773.000
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 251| 0 0 0 16 0 -7 .06 11 11 | -1245 78 17 107
| 0 0 1 26 18 20 .02 | 364 549
emr 80| 0 -1 2 -11 -28 25 .17 13 13 | 3254 259 16 141
| 0 1 1 11 21 12 .03 | 988 1028
esa 150| 0 0 -3 -14 20 -8 -.31 12 13 | -2197 1594 11 179
| 0 0 1 13 8 8 .03 | 1821 1772
gfz 199| 0 -1 -2 -15 9 -1 .05 13 12 | -9 14 12 140
| 0 0 1 18 12 19 .03 | 455 787
grg 182| 1 1 0 -10 -4 -20 .25 15 15 | -101 -39 15 157
| 1 1 3 30 29 25 .04 | 426 764
igr n/a| 0 0 -3 -12 3 -1 -.27 6 6 | 7268 432 17 82
| 0 0 0 16 14 9 .02 | 1226 1064
jpl 80| 0 1 -4 -5 13 31 -.04 14 13 | 3024 233 17 146
| 1 0 0 23 39 26 .01 | 855 1075
mit 299| -1 -1 3 72 20 25 -.09 13 12 | -33 -311 22 224
| 0 1 1 40 26 40 .04 | 350 629
ngs 231| 0 0 4 -40 -34 -49 -.04 13 11 | -1203 96 1584 3344
| 0 0 2 55 86 18 .03 | 367 567
sio 501| 0 1 -8 -18 15 28 -.76 21 19 | --- --- --- ---
| 0 0 2 27 34 20 .08 | --- ---
Table 1.1789.b GPS week : 1789 MJD: 56767.000-56773.000
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 5 4 4 5 4 |
2 | 5 5 5 5 5 5 5 |
3 | 4 4 4 5 4 5 4 |
4 | 5 4 4 5 4 6 6 |
5 | 5 5 6 6 6 6 6 |
6 | 0 0 0 0 0 0 0 |
7 | 5 5 4 5 5 5 5 |
8 | 4 4 4 4 4 5 4 |
9 | 4 4 4 4 4 5 5 |
10 | 7 6 7 7 7 7 8 |
11 | 4 5 5 4 4 5 4 |
12 | 7 6 6 6 6 6 5 |
13 | 5 5 5 6 6 5 5 |
14 | 5 5 5 5 5 6 5 |
15 | 6 5 6 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 6 6 5 5 5 6 5 |
18 | 5 4 5 5 5 6 5 |
19 | 4 5 4 5 5 5 5 |
20 | 5 5 5 5 4 5 4 |
21 | 5 5 5 5 5 5 5 |
22 | 4 4 4 4 4 5 4 |
23 | 5 5 5 5 5 5 5 |
24 | 5 5 4 4 4 4 5 |
25 | 5 4 4 5 4 5 5 |
26 | 4 4 4 4 4 5 4 |
27 | 5 5 5 6 5 5 5 |
28 | 4 4 4 4 4 5 4 |
29 | 6 5 6 6 6 6 6 |
30 | 0 0 0 0 0 0 0 |
31 | 6 6 6 5 6 6 6 |
32 | 5 6 6 6 6 6 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 2.1789.0 GPS week: 1789 Day: 0 MJD: 56767.000
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 0 -3 4 24 -37 .06 12 12 | -921 -525 15 126
emr 80| -1 0 1 -12 -12 20 .15 14 14 | 1753 524 23 161
esa 150| 1 0 -2 -28 22 -13 -.35 12 12 | -3951 1684 10 175
gfz 198| 1 0 0 -27 3 14 .01 12 11 | 507 -997 11 123
grg 175| 0 0 -2 -13 32 -30 .29 14 13 | 145 -844 17 150
igr n/a| 0 1 -3 -35 1 4 -.29 7 7 | 5316 392 21 82
jpl 80| 0 3 -4 -40 11 63 -.03 14 13 | 1780 291 18 160
mit 300| -2 -3 4 148 57 56 -.03 14 13 | 137 -950 22 221
ngs 231| -1 0 6 -27 -128 -77 -.03 13 10 | -827 -586 1553 3380
sio 499| 0 1 -4 -26 2 21 -.71 21 20 | --- --- --- ---
Table 2.1789.1 GPS week: 1789 Day: 1 MJD: 56768.000
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 250| 1 0 0 21 -20 7 .07 10 10 | -843 -503 17 113
emr 80| -1 1 1 -25 -35 36 .15 13 13 | 2825 -337 15 125
esa 150| 1 0 -2 -28 18 -9 -.35 12 12 | -254 -396 11 178
gfz 201| 0 -3 -2 -39 6 19 .02 12 12 | 462 -998 9 120
grg 185| 1 0 0 -63 14 6 .27 14 14 | 361 -1044 16 166
igr n/a| 0 0 -3 11 -23 2 -.26 7 6 | 6475 -299 16 69
jpl 80| 0 1 -5 18 -33 49 -.02 15 14 | 2834 -691 16 129
mit 300| -2 -2 4 85 -3 -51 -.05 12 11 | 369 -1206 20 243
ngs 229| -1 0 2 0 80 -50 -.03 13 11 | -748 -590 1535 3649
sio 503| -1 1 -7 -69 -26 19 -.70 22 21 | --- --- --- ---
Table 2.1789.2 GPS week: 1789 Day: 2 MJD: 56769.000
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 254| 1 0 -1 27 2 -27 .04 10 10 | -1878 923 18 101
emr 80| 0 -1 1 -20 4 16 .13 13 13 | 2793 1977 15 130
esa 150| 0 0 -1 -5 26 -7 -.32 14 14 | -2530 3624 12 183
gfz 200| 0 -1 -3 -12 12 17 .05 13 12 | -674 940 11 121
grg 186| 0 0 1 -29 18 1 .23 14 13 | -562 768 17 178
igr n/a| 0 0 -2 -9 16 -5 -.29 6 6 | 6519 2205 16 98
jpl 80| 0 2 -4 -23 19 58 -.05 14 13 | 2558 1900 17 159
mit 300| -1 -2 4 86 30 13 -.08 14 12 | -282 274 19 247
ngs 235| 0 0 3 -20 -102 -49 -.08 12 10 | -1753 818 1315 2944
sio 504| 0 0 -10 -22 28 55 -.69 22 20 | --- --- --- ---
Table 2.1789.3 GPS week: 1789 Day: 3 MJD: 56770.000
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 254| 0 0 0 4 -13 20 .05 10 10 | -987 -324 18 109
emr 80| 0 -1 2 -22 -29 10 .17 13 13 | 4934 -1275 17 158
esa 150| 0 0 -2 -6 22 -18 -.29 12 12 | -177 -326 12 186
gfz 203| 0 -1 -4 0 20 -22 .08 12 12 | 86 101 13 220
grg 188| 2 4 3 -15 6 -65 .21 16 15 | 387 -199 16 163
igr n/a| 0 0 -3 -3 15 -19 -.26 6 6 | 8897 -1082 18 96
jpl 80| 0 2 -4 -22 25 2 -.03 13 13 | 4555 -1168 17 139
mit 300| 0 -1 4 67 33 68 -.09 13 11 | 398 -308 21 232
ngs 233| 0 0 2 -14 -87 -48 -.05 13 11 | -982 -263 1668 3544
sio 503| -1 1 -10 -11 67 2 -.75 21 19 | --- --- --- ---
Table 2.1789.4 GPS week: 1789 Day: 4 MJD: 56771.000
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 252| 0 1 0 48 -17 -5 .09 10 10 | -1406 185 16 99
emr 80| 0 -2 2 -3 -32 24 .17 13 13 | 3396 394 13 147
esa 150| 0 0 -2 4 5 -5 -.28 12 13 | -4246 3439 11 171
gfz 200| -1 -1 -3 -14 -12 -26 .06 13 13 | -492 782 13 133
grg 185| 2 1 0 3 -34 -2 .19 15 16 | -12 -318 15 155
igr n/a| -1 0 -3 -2 17 -1 -.27 6 5 | 7553 481 16 81
jpl 80| -1 1 -5 0 12 2 -.07 13 13 | 3102 274 18 133
mit 300| 0 0 2 26 3 53 -.12 13 11 | -23 -545 24 195
ngs 233| 0 -1 3 -75 71 -49 -.06 13 10 | -1405 368 1644 3302
sio 504| 0 0 -8 4 43 37 -.76 21 19 | --- --- --- ---
Table 2.1789.5 GPS week: 1789 Day: 5 MJD: 56772.000
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 251| 0 1 3 39 0 -16 .07 12 12 | -1437 308 17 101
emr 80| 0 -3 4 3 -63 47 .18 14 14 | 3860 -277 16 140
esa 150| 0 0 -5 -11 17 7 -.30 12 12 | -585 214 11 186
gfz 198| 1 -1 -3 14 9 -12 .07 13 12 | 213 -172 14 133
grg 179| 0 1 -2 18 -42 -29 .24 16 15 | -598 846 15 143
igr n/a| -1 0 -3 -23 0 0 -.27 6 5 | 8194 65 17 76
jpl 80| -1 1 -3 6 86 12 -.04 13 13 | 3488 -257 18 144
mit 300| -1 -1 2 62 38 16 -.13 14 12 | -456 473 21 198
ngs 227| 1 0 7 -151 -84 -15 -.05 15 13 | -1462 443 1501 3121
sio 493| -1 1 -9 18 18 51 -.86 21 19 | --- --- --- ---
Table 2.1789.6 GPS week: 1789 Day: 6 MJD: 56773.000
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 251| 0 2 0 -31 20 6 .05 11 11 | -1249 488 19 106
emr 80| 0 -3 3 -1 -32 19 .22 14 14 | 3223 813 15 128
esa 150| 0 1 -4 -28 33 -10 -.33 13 13 | -3636 2925 13 174
gfz 199| 0 -1 -3 -28 24 2 .07 14 13 | -166 442 15 130
grg 181| 0 0 6 25 -24 -21 .31 16 16 | -433 515 15 145
igr n/a| 0 0 -5 -23 0 7 -.24 6 6 | 7928 1262 18 77
jpl 80| 2 1 -4 20 -29 29 -.05 13 13 | 2853 1283 18 159
mit 299| 0 0 1 33 -17 22 -.13 14 12 | -380 83 30 235
ngs 230| -1 -1 2 3 5 -57 .00 13 11 | -1245 486 1872 3471
sio 504| 0 2 -11 -21 -24 8 -.89 21 18 | --- --- --- ---
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 3.1789.0 GPS week: 1789 Day: 0 MJD: 56767.000
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 12 11 10 9 5 11 8 10 14 3 | 26 33 23 27 30 22 31 25 28 20 26
2 | 12 13 13 12 11 5 13 11 14 36 4 | 24 30 25 31 29 26 28 30 32 37 26
3 | 8 8 11 13 10 5 10 9 16 40 4 | 25 24 19 23 23 19 21 21 29 36 22
4 | 18 8 14 8 10 6 8 13 12 13 4 | 38 30 27 33 35 27 29 32 32 28 30
5E | 12 16 8 15 14 5 21 13 11 13 5 | 26 31 25 35 32 25 31 30 35 26 28
X6E | 3 --- --- --- 286 58 --- --- --- --- 0 | 52 --- --- --- 120 31 --- --- --- --- 51
7 | 12 12 15 11 14 5 11 17 13 15 5 | 27 27 18 27 30 19 23 24 26 20 22
8 | 10 10 12 9 12 4 10 12 9 23 4 | 19 22 17 18 17 15 20 21 21 24 17
9 | 10 9 12 8 12 6 11 13 8 28 4 | 22 24 20 21 22 19 22 25 23 31 20
10E | 17 23 17 11 17 8 16 21 16 22 6 | 84 89 81 83 85 79 83 85 85 85 83
11 | 8 12 15 11 12 6 8 8 8 13 4 | 44 52 41 46 57 43 47 48 49 40 47
12E | 11 23 9 13 26 7 24 15 16 17 6 | 24 26 16 25 26 17 27 25 26 18 20
13 | 8 12 16 13 17 7 11 13 10 14 4 | 27 31 21 32 39 24 29 29 25 22 26
14 | 10 17 11 15 13 8 13 9 10 23 4 | 26 25 23 33 33 24 25 23 26 25 24
15 | 15 15 12 12 16 6 16 16 14 20 5 | 19 28 21 19 27 15 22 21 26 20 19
16E | 10 14 11 14 14 7 16 12 18 20 5 | 23 21 18 26 26 17 21 20 26 15 20
17 | 20 19 16 12 11 7 15 18 17 28 6 | 34 35 26 29 35 29 31 34 39 29 29
18E | 9 10 7 11 17 8 14 13 10 13 4 | 30 30 26 30 32 27 32 29 31 27 28
19 | 9 11 12 11 12 8 12 9 13 23 4 | 32 32 27 32 33 24 28 30 31 20 29
20E | 12 13 9 12 14 10 12 9 16 16 4 | 26 27 20 24 21 21 22 25 31 20 22
21 | 13 9 13 11 16 9 12 14 12 22 5 | 28 31 27 34 38 29 28 36 26 30 29
22E | 9 11 6 9 15 7 8 12 14 12 4 | 34 36 30 33 34 32 34 33 38 32 33
23 | 8 15 13 16 12 10 12 10 12 29 4 | 24 31 22 31 29 23 26 24 30 23 24
24 | 12 11 12 11 15 5 13 14 8 15 4 | 21 24 21 22 24 15 26 19 20 20 19
25E | 10 12 16 9 14 6 14 16 10 14 5 | 18 21 25 18 18 13 20 20 17 16 17
26 | 8 13 14 8 14 3 9 9 8 21 4 | 23 21 18 21 24 18 19 20 22 23 19
X27 | 10 7 13 14 --- 5 14 14 12 14 5 | 31 32 29 33 --- 29 35 33 32 26 31
28E | 8 12 10 9 10 5 10 10 8 11 3 | 29 30 22 22 29 22 25 26 29 22 25
29 | 14 14 12 16 13 10 19 21 10 24 6 | 32 33 31 35 33 29 33 32 30 32 29
X30 | 3 --- --- --- --- 21 --- --- --- --- 0 | 30 --- --- --- --- 27 --- --- --- --- 30
31 | 17 16 13 16 15 8 14 17 13 22 6 | 27 32 20 34 35 25 27 24 26 23 24
32E | 10 14 11 11 15 8 13 14 20 18 5 | 40 41 40 41 43 43 45 42 48 50 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 12 12 14 7 14 14 13 21 |T 30 31 25 30 35 25 29 29 31 28 28
WRMS | 12 14 12 11 13 7 13 13 10 20 |NE 27 29 23 29 31 23 27 27 28 26 25
MEDI | 10 12 12 11 14 7 12 13 12 18 |MD 27 30 23 30 30 24 27 25 29 24 26
Table 3.1789.1 GPS week: 1789 Day: 1 MJD: 56768.000
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 12 12 10 5 13 9 11 13 4 | 21 26 19 22 26 20 30 23 29 18 21
2 | 11 14 12 13 13 5 12 10 10 31 4 | 19 24 20 23 18 16 22 21 22 23 18
3 | 5 7 11 15 13 4 9 9 10 51 3 | 16 17 15 18 15 14 15 16 21 46 15
4 | 12 8 14 10 12 8 9 12 10 16 4 | 27 22 19 20 21 16 19 20 24 20 19
5E | 8 15 4 17 13 5 23 10 15 10 5 | 23 24 16 26 27 17 25 25 24 18 21
X6E | 2 --- --- --- 602 115 --- --- --- --- 0 | 116 --- --- --- 136 31 --- --- --- --- 115
7 | 10 11 15 11 14 6 12 8 11 15 4 | 24 26 15 23 27 17 22 20 26 16 20
8 | 8 10 14 9 14 4 12 9 10 24 4 | 18 19 15 15 16 13 18 19 23 25 15
9 | 8 11 14 8 12 5 11 8 11 26 4 | 19 22 19 20 19 18 21 21 27 27 18
10E | 13 19 16 12 15 10 15 21 19 22 6 | 69 69 69 71 69 63 69 73 73 74 68
11 | 9 9 16 13 12 7 10 8 14 19 4 | 27 37 25 31 36 28 32 30 33 28 29
12E | 9 17 7 11 24 5 26 13 11 16 5 | 23 26 15 24 22 16 25 23 26 15 19
13 | 7 11 14 13 16 6 14 15 9 16 4 | 19 28 19 25 33 19 24 22 23 17 20
14 | 9 19 12 13 13 9 15 8 15 22 5 | 19 23 19 26 26 19 23 20 25 23 19
15 | 11 16 11 13 17 7 16 14 14 23 5 | 18 28 16 20 27 13 20 19 23 22 18
16E | 7 14 6 15 13 5 21 11 14 14 5 | 22 16 14 22 22 13 20 19 26 13 16
17 | 12 16 15 12 14 7 16 16 12 27 5 | 26 29 20 22 28 18 26 21 26 18 20
18E | 7 10 5 13 17 6 15 12 11 15 4 | 27 25 24 25 30 24 26 29 31 27 25
19 | 7 11 12 18 15 6 13 9 14 22 4 | 21 25 22 27 21 19 22 22 27 17 21
20E | 10 11 8 14 13 7 13 12 15 17 4 | 29 27 23 27 25 24 26 28 33 22 25
21 | 10 12 14 12 15 9 13 14 12 20 4 | 24 22 22 26 24 21 23 25 27 21 21
22E | 5 10 6 9 13 5 9 9 10 13 3 | 26 30 26 27 35 26 30 28 34 29 28
23 | 8 15 12 17 15 8 16 12 12 33 5 | 19 27 17 23 27 15 22 20 22 27 18
24 | 8 11 12 7 16 7 15 11 13 15 4 | 19 21 20 21 26 16 26 18 23 13 18
25E | 8 10 15 9 12 6 13 13 9 14 4 | 18 20 24 17 19 14 22 17 22 15 17
26 | 10 11 12 9 15 4 11 7 11 19 4 | 20 16 17 19 20 16 17 16 21 21 17
X27 | 8 8 14 17 --- 5 14 13 8 13 4 | 21 25 21 27 --- 23 29 25 26 17 22
28E | 6 9 7 10 13 5 12 7 12 10 3 | 27 24 21 25 26 22 28 26 32 19 24
29 | 10 16 14 13 13 8 18 16 11 30 5 | 26 28 24 26 25 22 28 24 27 28 23
X30 | 2 --- --- --- --- 15 --- --- --- --- 0 | 37 --- --- --- --- 28 --- --- --- --- 36
31 | 18 15 12 13 15 10 14 14 18 28 5 | 24 32 21 30 33 23 26 21 35 24 23
32E | 13 15 11 11 14 4 13 15 21 17 5 | 32 31 33 31 32 35 34 33 38 42 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 12 12 14 7 15 12 13 22 |T 27 26 21 25 30 21 25 24 28 24 25
WRMS | 10 13 12 12 14 6 14 11 11 21 |NE 22 24 19 23 24 18 23 21 25 22 20
MEDI | 8 11 12 12 14 6 13 11 11 17 |MD 23 25 20 24 26 19 24 21 26 21 20
Table 3.1789.2 GPS week: 1789 Day: 2 MJD: 56769.000
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 14 14 11 5 14 12 10 13 4 | 23 30 22 25 30 22 31 26 27 19 24
2 | 12 13 15 11 11 7 13 13 15 28 5 | 21 26 21 25 24 21 24 22 29 22 21
3 | 8 8 12 12 11 4 8 11 7 42 3 | 20 22 19 23 21 18 18 21 25 38 20
4 | 11 10 14 8 8 6 11 13 13 14 4 | 26 25 21 24 27 20 24 24 27 23 22
5E | 10 21 9 17 14 6 20 15 12 11 5 | 28 32 24 32 33 25 30 31 33 23 28
X6E | 2 --- --- --- 554 85 --- --- --- --- 0 | 79 --- --- --- 113 31 --- --- --- --- 79
7 | 10 12 17 11 11 5 9 9 9 20 4 | 24 25 16 27 27 15 21 20 21 22 20
8 | 8 9 15 9 11 3 10 8 9 19 3 | 19 17 17 19 17 12 19 16 19 20 15
9 | 8 11 16 9 8 4 10 9 10 22 4 | 21 21 20 23 20 16 23 20 26 26 19
10E | 15 21 17 15 14 9 17 21 17 23 6 | 74 79 72 73 72 68 76 80 77 78 74
11 | 9 9 16 14 11 6 11 8 12 24 4 | 35 42 33 38 45 36 39 38 42 39 37
12E | 11 18 11 10 22 6 24 14 14 15 6 | 21 25 17 26 25 17 25 26 28 17 20
13 | 8 14 16 15 16 5 13 20 10 17 5 | 22 27 19 30 35 20 24 28 21 21 22
14 | 8 17 14 11 15 7 14 12 17 26 5 | 23 25 20 30 31 22 23 25 28 22 22
15 | 14 13 17 10 17 5 15 15 11 28 5 | 25 25 21 24 28 16 20 22 24 20 20
16E | 10 15 10 15 13 4 18 17 9 17 5 | 26 20 19 28 23 19 22 23 27 16 21
17 | 12 14 16 11 11 6 15 17 10 24 5 | 28 32 24 24 31 24 27 25 28 23 24
18E | 8 11 8 13 21 5 13 12 11 14 4 | 29 29 27 29 35 26 28 26 27 22 27
19 | 7 10 13 15 14 5 10 10 8 24 4 | 26 29 27 32 28 25 26 27 30 21 26
20E | 10 13 6 13 14 7 15 15 13 18 4 | 30 30 24 27 27 27 25 32 32 20 27
21 | 8 10 16 13 16 6 13 14 15 22 5 | 27 26 27 31 31 25 25 31 27 29 25
22E | 5 9 8 9 18 5 11 11 10 13 4 | 24 28 23 27 31 23 28 24 24 18 24
23 | 11 15 13 18 13 7 14 16 12 32 5 | 18 27 19 27 27 15 21 24 22 26 19
24 | 7 9 14 12 15 5 13 12 8 13 4 | 21 21 23 26 28 15 25 17 19 15 20
25E | 6 9 16 8 16 3 11 14 9 15 4 | 19 22 27 21 19 16 24 20 21 17 19
26 | 8 9 13 10 15 3 10 9 10 16 4 | 21 19 18 22 22 15 18 17 16 23 17
X27 | 8 8 12 17 --- 5 12 12 11 13 4 | 29 27 26 31 --- 27 32 29 30 22 28
28E | 10 12 10 9 13 4 13 10 8 13 4 | 25 24 19 22 24 18 22 23 22 22 20
29 | 11 13 15 14 12 6 18 17 13 26 5 | 30 30 27 32 28 24 28 28 27 30 26
X30 | 2 --- --- --- --- 14 --- --- --- --- 0 | 32 --- --- --- --- 22 --- --- --- --- 30
31 | 17 16 18 15 16 10 10 10 14 29 5 | 24 33 19 33 35 22 25 21 26 22 23
32E | 13 17 12 11 13 7 11 16 20 18 5 | 29 31 28 29 31 31 32 30 32 35 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 14 13 14 6 14 14 12 22 |T 28 28 23 28 32 22 26 26 27 25 26
WRMS | 10 13 14 12 13 6 13 12 10 20 |NE 24 26 21 27 28 20 24 24 25 24 22
MEDI | 8 12 14 12 14 5 13 12 11 18 |MD 25 26 21 27 28 22 25 24 27 22 22
Table 3.1789.3 GPS week: 1789 Day: 3 MJD: 56770.000
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 13 10 12 6 12 8 8 13 4 | 28 34 24 29 33 25 35 30 25 24 28
2 | 12 11 12 12 11 6 12 11 14 25 4 | 27 31 27 28 28 24 29 27 28 25 26
3 | 8 9 12 13 17 6 8 15 13 44 4 | 25 21 20 20 23 16 20 23 18 41 20
4 | 12 10 11 11 12 4 10 13 13 15 4 | 36 32 28 30 30 27 29 29 29 25 29
5E | 11 14 7 14 15 6 22 14 14 10 5 | 34 33 24 30 32 25 33 34 38 23 30
X6E | 1 --- --- --- 583 48 --- --- --- --- 0 | 46 --- --- --- 120 54 --- --- --- --- 46
7 | 11 12 15 14 14 6 10 10 10 18 4 | 29 29 20 32 29 21 25 24 24 27 24
8 | 9 9 13 11 9 5 10 10 8 19 4 | 24 21 20 25 17 17 21 19 23 24 20
9 | 10 11 13 11 9 5 9 9 8 20 4 | 31 25 23 29 20 22 22 23 27 27 24
10E | 16 21 13 15 15 7 16 22 15 24 6 | 73 79 74 74 71 70 76 82 77 80 75
11 | 7 10 15 13 17 7 10 7 10 21 4 | 39 46 34 41 50 36 42 41 35 38 39
12E | 11 15 9 11 19 6 23 15 15 14 5 | 25 26 18 28 23 17 25 27 24 17 21
13 | 7 16 14 14 19 7 13 21 10 13 5 | 27 31 23 33 37 22 29 31 26 24 26
14 | 10 19 15 11 17 7 10 8 9 21 4 | 26 29 22 32 32 23 25 27 24 24 24
15 | 9 12 12 11 17 6 15 12 13 24 4 | 23 29 21 24 28 17 22 24 26 22 22
16E | 10 17 9 14 15 4 17 11 17 15 5 | 24 21 17 25 19 15 19 21 23 18 18
17 | 10 13 14 13 15 7 15 15 14 26 5 | 34 36 29 36 34 29 31 29 34 23 30
18E | 9 9 7 13 20 5 15 11 11 14 4 | 35 38 34 36 37 33 38 34 35 34 34
19 | 9 11 12 15 18 8 15 9 11 23 4 | 29 28 25 26 30 22 26 27 24 22 25
20E | 11 11 8 11 20 5 12 9 11 17 4 | 60 61 55 63 57 56 60 59 61 52 58
21 | 12 12 14 11 16 7 13 13 9 24 4 | 26 31 26 33 32 26 27 32 25 30 27
22E | 10 11 9 9 17 5 7 10 13 13 4 | 35 41 36 41 44 34 39 37 39 35 38
23 | 10 16 12 17 15 7 13 12 10 28 5 | 24 30 22 32 28 18 25 23 23 25 22
24 | 7 9 12 10 15 7 13 11 10 11 4 | 25 28 24 25 27 20 29 24 26 20 24
25E | 8 9 17 13 18 4 11 12 13 15 5 | 21 25 26 22 19 17 22 24 19 19 20
26 | 8 10 11 13 12 3 9 10 9 19 4 | 27 24 21 27 22 21 20 23 24 26 22
X27 | 13 11 13 14 --- 5 14 15 17 13 5 | 34 28 26 31 --- 25 32 33 29 25 29
28E | 8 10 8 10 11 4 10 7 14 9 3 | 29 28 24 30 24 24 26 28 37 23 26
29 | 12 15 16 11 15 5 17 17 19 26 5 | 33 35 31 34 32 28 34 32 32 35 30
X30 | 1 --- --- --- --- 13 --- --- --- --- 0 | 28 --- --- --- --- 25 --- --- --- --- 27
31 | 16 12 14 12 19 8 11 9 14 26 5 | 26 34 22 32 37 23 29 25 29 24 26
32E | 11 18 10 11 15 5 11 15 25 20 5 | 37 34 34 38 36 36 35 37 46 46 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 12 12 16 6 13 13 13 21 |T 31 32 27 32 35 27 30 30 31 29 29
WRMS | 10 13 12 12 15 6 13 11 11 19 |NE 28 30 24 29 29 23 27 27 26 26 25
MEDI | 10 11 12 12 15 6 12 11 13 19 |MD 28 30 24 30 30 24 29 27 26 25 26
Table 3.1789.4 GPS week: 1789 Day: 4 MJD: 56771.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 10 12 12 9 4 14 8 10 11 4 | 20 28 18 22 28 18 28 19 22 14 20
2 | 13 11 13 18 12 6 14 10 13 23 5 | 21 26 20 25 20 17 22 19 25 18 19
3 | 6 8 11 12 15 6 9 12 16 39 4 | 16 15 15 16 19 13 16 16 18 33 14
4 | 9 10 11 14 15 6 8 10 7 10 4 | 28 27 24 33 24 22 23 21 26 19 24
5E | 12 18 8 17 17 6 19 15 13 13 5 | 27 32 22 26 30 23 29 28 30 23 25
X6E | 3 --- --- --- --- 1837 --- --- --- --- 0 | 306 --- --- --- --- 9999 --- --- --- --- 306
7 | 11 13 13 15 12 4 10 12 9 17 4 | 25 27 15 27 28 16 24 22 21 19 20
8 | 6 10 11 13 12 3 10 15 6 18 4 | 19 19 16 18 17 13 19 18 19 19 15
9 | 9 11 11 12 13 4 10 14 6 22 4 | 23 21 18 21 18 15 21 18 17 24 17
10E | 13 17 14 15 15 11 14 25 18 21 6 | 75 79 74 78 74 71 77 81 75 78 75
11 | 7 10 15 12 12 7 10 10 10 27 4 | 33 41 30 35 42 30 37 37 35 38 34
12E | 12 20 8 14 15 5 22 12 11 12 5 | 24 24 17 25 22 16 21 22 26 12 20
13 | 7 16 13 15 18 6 14 19 15 14 5 | 24 28 18 27 34 16 23 26 25 16 21
14 | 9 16 12 13 18 6 13 14 11 22 5 | 19 21 15 25 29 16 20 21 23 19 18
15 | 13 13 13 13 18 5 17 12 14 22 5 | 21 27 19 23 29 15 20 19 29 18 19
16E | 8 16 9 11 13 5 17 10 15 18 4 | 21 17 14 21 22 13 17 19 24 16 16
17 | 12 14 13 18 12 6 16 14 11 29 5 | 28 30 23 33 29 20 25 22 29 22 24
18E | 8 9 9 12 15 4 14 11 14 13 4 | 38 35 35 35 44 34 36 36 37 38 35
19 | 7 11 12 16 16 5 12 10 14 22 4 | 22 24 20 27 23 18 21 21 24 13 20
20 | 7 9 8 9 18 5 13 8 16 19 4 | 30 34 28 32 39 30 29 29 35 30 31
21 | 10 11 15 11 14 5 13 15 13 25 5 | 19 25 20 23 23 17 21 25 18 25 18
22E | 9 11 8 8 14 5 9 9 10 14 3 | 37 37 36 37 40 36 37 36 43 32 37
23 | 7 16 12 17 15 4 14 11 13 26 5 | 21 27 18 25 28 14 21 19 23 19 18
24 | 8 11 11 11 13 5 12 7 8 11 4 | 19 22 21 25 26 14 24 14 18 11 19
25E | 8 11 16 9 14 6 9 9 9 11 4 | 18 20 27 19 20 16 18 18 20 10 18
26 | 10 9 12 16 13 4 9 12 10 18 4 | 20 20 16 23 18 14 16 17 18 20 16
X27 | 10 9 13 11 --- 5 15 14 15 14 5 | 25 22 21 24 --- 19 26 25 23 17 22
28E | 7 14 8 12 14 5 11 7 10 10 4 | 27 29 23 29 29 23 25 27 30 22 26
29 | 9 14 15 13 16 5 16 16 13 30 5 | 27 29 23 28 26 22 27 24 26 25 24
X30 | 3 --- --- --- --- 14 --- --- --- --- 0 | 26 --- --- --- --- 20 --- --- --- --- 24
31 | 17 16 15 14 21 7 13 13 16 26 6 | 23 30 16 28 35 19 23 24 22 23 21
32E | 11 18 12 10 13 6 12 15 24 18 5 | 33 32 35 33 31 33 32 34 46 40 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 12 13 15 6 13 13 13 21 |T 34 28 23 28 29 21 25 25 27 23 32
WRMS | 10 13 13 13 16 5 13 11 10 19 |NE 22 25 19 25 26 17 22 21 23 20 20
MEDI | 9 11 12 13 14 5 13 12 13 18 |MD 24 27 20 25 28 18 23 22 24 19 20
Table 3.1789.5 GPS week: 1789 Day: 5 MJD: 56772.000
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 13 13 4 15 9 17 14 4 | 22 29 17 23 27 18 33 19 26 15 21
2 | 12 12 11 15 14 6 10 7 19 27 5 | 26 29 22 21 25 20 24 21 30 21 22
3 | 7 10 11 10 16 6 12 13 16 44 4 | 20 20 17 17 18 17 18 20 18 39 16
4 | 25 14 10 12 12 7 9 12 12 11 5 | 36 27 22 27 23 22 22 20 29 15 23
5E | 9 20 6 19 19 5 20 17 20 11 6 | 37 42 32 34 44 33 38 38 39 31 35
X6E | 3 --- --- --- 711 159 --- --- --- --- 0 | 90 --- --- --- 132 454 --- --- --- --- 88
7 | 8 14 13 17 14 4 11 9 13 19 4 | 25 28 19 27 31 17 22 19 22 21 21
8 | 6 12 11 11 11 3 11 17 10 17 4 | 20 21 21 22 19 16 19 19 22 17 18
9 | 10 12 11 11 11 3 12 15 10 18 4 | 22 22 23 26 23 19 18 20 23 21 20
10E | 15 14 13 16 16 13 13 36 15 22 7 | 78 78 75 77 76 72 79 93 77 80 78
11 | 10 10 15 13 16 4 13 10 19 21 5 | 33 40 27 36 41 28 38 34 30 34 33
12E | 10 18 7 13 20 6 20 11 12 11 5 | 26 25 19 28 22 19 22 23 25 16 21
13 | 8 18 12 16 19 5 12 13 12 13 5 | 22 30 20 30 38 18 25 23 22 13 23
14 | 11 17 12 16 17 7 14 14 14 22 5 | 23 25 18 29 28 18 20 25 25 20 21
15 | 12 13 11 11 19 5 14 11 14 18 5 | 22 28 18 25 30 16 20 24 27 16 21
16E | 11 15 10 12 20 5 17 11 15 19 5 | 24 20 18 24 21 16 19 21 25 20 19
17 | 13 14 13 17 13 5 15 13 15 28 5 | 30 35 25 31 31 22 27 21 28 22 25
18E | 12 16 8 13 23 8 13 16 16 16 5 | 59 60 56 57 66 54 58 56 58 52 58
19 | 9 13 12 15 17 6 14 9 13 19 5 | 22 26 21 26 23 18 22 21 20 16 21
20 | 10 11 7 13 15 3 13 9 15 24 4 | 52 51 43 52 48 46 44 49 56 35 49
21 | 12 11 15 9 12 5 13 15 13 27 5 | 20 26 20 21 22 17 25 24 20 25 19
22E | 12 16 11 12 18 8 6 10 10 12 4 | 73 76 73 74 80 73 72 75 74 69 74
23 | 9 18 10 17 14 5 15 9 18 30 5 | 20 30 17 25 27 14 22 16 24 23 19
24 | 10 11 12 9 14 6 12 9 10 14 4 | 23 23 25 28 29 20 27 20 24 17 23
25E | 10 10 16 9 12 7 12 12 17 13 4 | 26 24 31 23 25 18 20 21 24 17 23
26 | 11 10 13 11 14 4 11 10 16 26 4 | 24 21 20 24 22 18 18 22 23 28 20
X27 | 8 10 13 13 --- 4 14 12 11 14 4 | 26 26 21 26 --- 20 30 26 22 19 24
28E | 8 15 8 14 15 4 12 9 16 9 4 | 24 28 19 25 26 19 23 24 25 18 21
29 | 13 14 14 13 13 6 16 18 13 32 5 | 28 30 25 28 24 22 28 24 28 27 24
X30 | 3 --- --- --- --- 14 --- --- --- --- 0 | 27 --- --- --- --- 21 --- --- --- --- 25
31 | 20 16 16 15 21 6 10 10 17 21 6 | 27 33 22 31 37 20 25 26 26 17 25
32E | 14 20 12 9 16 6 14 14 24 20 6 | 26 29 32 31 31 30 29 27 41 36 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 12 13 16 6 13 14 15 21 |T 32 32 27 31 36 38 29 29 31 26 29
WRMS | 12 14 12 12 15 5 13 12 13 19 |NE 24 27 21 26 27 19 24 22 24 21 22
MEDI | 10 14 12 13 15 5 13 11 15 19 |MD 26 28 21 27 27 19 24 23 25 21 23
Table 3.1789.6 GPS week: 1789 Day: 6 MJD: 56773.000
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 8 14 14 14 7 13 9 10 19 4 | 27 34 24 31 34 23 34 25 22 25 26
2 | 14 11 12 16 12 5 13 9 14 26 5 | 24 30 22 30 29 23 27 25 35 19 24
3 | 7 9 11 13 14 5 9 8 13 45 4 | 23 21 17 23 25 19 18 20 25 40 20
4 | 26 11 12 13 11 9 10 16 9 12 5 | 42 32 25 34 36 27 28 29 33 22 30
5E | 13 24 11 18 14 6 20 17 14 19 6 | 46 53 46 48 48 42 50 49 51 45 46
X6E | 2 --- --- --- 707 111 --- --- --- --- 0 | 81 --- --- --- 144 291 --- --- --- --- 80
7 | 8 12 15 16 13 6 10 11 15 21 4 | 21 26 18 27 28 16 21 21 24 25 19
8 | 6 11 11 16 15 3 12 12 10 20 4 | 14 19 16 20 17 13 20 14 23 18 15
9 | 7 14 11 14 13 4 11 14 9 21 4 | 18 21 20 24 21 18 21 19 22 22 18
10E | 12 16 12 15 13 11 11 44 16 16 7 | 97 100 97 97 97 93 98 115 100 96 99
11 | 8 9 16 12 15 5 9 9 9 17 4 | 45 50 40 49 58 42 45 46 42 41 45
12E | 9 14 7 11 21 6 19 15 13 9 5 | 23 24 19 28 23 18 21 22 27 12 20
13 | 9 15 14 18 18 5 14 12 12 13 5 | 22 28 18 32 36 20 23 26 25 19 22
14 | 9 16 13 14 14 8 14 9 15 20 5 | 25 24 22 32 31 22 23 23 25 20 22
15 | 12 14 15 12 16 6 15 13 14 15 5 | 24 29 23 24 30 19 22 21 29 16 22
16E | 9 17 10 13 22 5 17 11 13 22 5 | 25 19 16 25 18 16 20 21 27 21 19
17 | 9 17 11 15 14 7 13 12 13 26 5 | 25 35 24 25 35 21 30 23 32 22 25
18 | 8 12 10 12 19 10 17 12 13 14 4 | 51 52 54 52 51 47 52 49 49 51 50
19 | 7 12 11 19 18 4 13 7 15 21 4 | 26 27 21 31 33 22 23 27 24 18 24
20 | 8 13 7 12 12 5 11 7 10 22 3 | 45 48 40 47 47 41 43 42 43 34 43
21 | 11 14 17 10 16 5 14 12 11 20 5 | 26 31 23 32 34 25 26 32 30 26 26
22 | 7 14 12 10 15 5 12 11 11 14 4 | 80 80 82 82 80 80 79 83 83 77 81
23 | 10 19 12 19 15 5 15 11 11 26 5 | 19 28 18 29 26 17 17 17 25 20 18
24 | 7 7 14 8 16 6 11 12 16 12 4 | 20 22 23 26 29 17 25 16 27 15 20
25E | 9 11 17 17 15 5 12 11 12 10 5 | 21 24 30 30 25 18 20 18 24 13 21
26 | 11 11 13 11 16 6 8 9 10 30 4 | 16 17 18 21 24 16 18 18 20 30 17
X27 | 7 11 13 14 --- 4 12 12 11 11 4 | 27 29 25 31 --- 26 31 32 29 20 27
28E | 8 13 11 14 13 5 9 9 9 10 4 | 29 30 27 30 34 25 32 26 32 22 27
29 | 14 14 16 11 18 5 19 18 11 29 5 | 35 35 33 34 33 29 35 30 32 32 30
X30 | 2 --- --- --- --- 28 --- --- --- --- 0 | 35 --- --- --- --- 20 --- --- --- --- 35
31 | 21 20 15 15 18 8 14 10 11 18 6 | 30 41 22 36 40 27 30 26 35 21 28
32E | 9 22 11 9 14 5 11 15 20 18 5 | 37 39 40 39 37 40 40 40 47 48 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 14 13 14 16 6 13 14 13 21 |T 33 34 30 35 40 36 32 31 34 29 32
WRMS | 11 14 13 13 16 6 13 12 11 18 |NE 25 28 22 29 31 22 25 24 27 23 24
MEDI | 9 13 12 14 15 5 12 11 12 19 |MD 26 29 23 31 33 22 26 25 29 22 25
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 4.1789 GPS week: 1789 MJD: 56767.0-56773.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3011 |U 6 6 14 |U 8 9 25 |U 7 9 18 |
emr | emr 2872 | 7 7 16 |U 9 9 26 | 7 8 20 |
esa | esa 2880 | 6 6 15 |U 8 9 28 | 8 10 19 |
gfz | gfz 2869 |U 6 6 15 |U 8 11 29 |U 8 9 20 |
grg | grg 2860 |U 44 31 73 |U 10 9 34 |U 10 11 22 |
igr | igr 2873 | 6 6 15 | 7 9 24 | 7 8 17 |
igs | igs 2874 | 6 6 14 | 8 9 28 | 8 9 18 |
jpl | jpl 2872 | 7 8 18 |U 8 10 30 |U 8 10 21 |
mit | mit 2880 | 6 6 15 |U 8 10 30 |U 8 10 19 |
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 5.1789.0 GPS week: 1789 Day: 0 MJD: 56767.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3030 | 7 8 16 | 8 15 27 | 7 7 19 |
emr | emr 2872 | 9 7 16 | 10 10 28 | 8 8 20 |
esa | esa 2880 | 7 6 14 | 9 12 33 | 8 7 17 |
gfz | gfz 2872 | 7 6 17 | 8 14 33 | 8 8 19 |
grg | grg 2880 | 36 22 68 | 10 11 39 | 10 10 23 |
igr | igr 2880 | 7 6 17 | 8 10 26 | 7 8 17 |
igs | igs 2876 | 7 5 16 | 8 12 26 | 8 8 18 |
jpl | jpl 2872 | 8 8 22 | 10 11 33 | 8 9 21 |
mit | mit 2880 | 7 7 16 | 10 11 48 | 8 8 18 |
Table 5.1789.1 GPS week: 1789 Day: 1 MJD: 56768.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3026 | 8 7 17 | 9 10 32 | 7 10 20 |
emr | emr 2872 | 6 5 21 | 12 10 33 | 7 10 22 |
esa | esa 2880 | 5 5 22 | 10 11 36 | 8 10 20 |
gfz | gfz 2872 | 5 5 16 | 10 11 34 | 9 9 25 |
grg | grg 2880 | 114 117 175 | 14 11 33 | 10 13 24 |
igr | igr 2879 | 5 5 16 | 9 10 31 | 7 9 18 |
igs | igs 2878 | 5 4 17 | 10 10 33 | 8 10 21 |
jpl | jpl 2872 | 6 6 22 | 10 11 34 | 8 10 22 |
mit | mit 2880 | 6 5 18 | 9 12 34 | 8 12 20 |
Table 5.1789.2 GPS week: 1789 Day: 2 MJD: 56769.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3008 | 6 5 16 | 6 9 26 | 7 10 15 |
emr | emr 2872 | 8 8 22 | 8 6 25 | 8 9 19 |
esa | esa 2880 | 7 6 21 | 7 8 26 | 10 13 23 |
gfz | gfz 2872 | 6 6 20 | 6 8 20 | 7 9 18 |
grg | grg 2880 | 21 9 51 | 8 8 37 | 11 14 22 |
igr | igr 2875 | 6 6 22 | 6 8 24 | 8 9 15 |
igs | igs 2877 | 7 6 19 | 6 7 28 | 8 10 16 |
jpl | jpl 2872 | 9 9 25 | 6 18 36 | 8 11 22 |
mit | mit 2880 | 6 6 17 | 6 8 28 | 9 11 16 |
Table 5.1789.3 GPS week: 1789 Day: 3 MJD: 56770.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3011 | 4 4 12 | 7 8 24 | 7 8 16 |
emr | emr 2870 | 5 5 12 | 8 8 27 | 7 10 22 |
esa | esa 2880 | 5 7 12 | 7 10 24 | 8 10 21 |
gfz | gfz 2873 | 5 6 11 | 9 10 33 | 7 7 19 |
grg | grg 2880 | 92 39 120 | 9 8 29 | 9 13 22 |
igr | igr 2877 | 6 6 11 | 7 9 25 | 7 8 19 |
igs | igs 2851 | 4 5 11 | 8 9 31 | 7 9 19 |
jpl | jpl 2872 | 5 7 15 | 8 10 24 | 6 10 25 |
mit | mit 2880 | 6 6 13 | 8 8 22 | 8 10 18 |
Table 5.1789.4 GPS week: 1789 Day: 4 MJD: 56771.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2972 | 5 6 11 | 10 7 26 | 8 8 17 |
emr | emr 2872 | 6 7 12 | 8 10 28 | 6 7 17 |
esa | esa 2880 | 5 7 10 | 10 9 31 | 8 8 18 |
gfz | gfz 2868 | 5 7 10 | 9 15 38 | 8 10 18 |
grg | grg 2774 | 8 6 11 | 10 10 28 | 9 11 18 |
igr | igr 2856 | 4 7 9 | 9 8 27 | 9 9 18 |
igs | igs 2876 | 5 7 9 | 9 8 34 | 8 8 17 |
jpl | jpl 2872 | 5 9 12 | 10 8 40 | 8 9 20 |
mit | mit 2880 | 5 6 10 | 9 9 30 | 9 13 22 |
Table 5.1789.5 GPS week: 1789 Day: 5 MJD: 56772.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | 6 6 16 | 7 8 22 | 8 6 19 |
emr | emr 2872 | 7 6 14 | 9 10 22 | 7 6 21 |
esa | esa 2880 | 6 7 15 | 7 9 24 | 9 8 19 |
gfz | gfz 2866 | 9 9 16 | 6 8 21 | 8 8 21 |
grg | grg 2866 | 25 17 59 | 11 8 51 | 9 9 23 |
igr | igr 2869 | 6 6 16 | 6 9 20 | 8 5 17 |
igs | igs 2880 | 5 5 13 | 7 8 21 | 8 6 18 |
jpl | jpl 2872 | 7 6 14 | 6 8 22 | 8 7 20 |
mit | mit 2880 | 6 4 14 | 8 9 23 | 9 8 21 |
Table 5.1789.6 GPS week: 1789 Day: 6 MJD: 56773.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3015 | 6 8 13 | 6 7 19 | 8 12 19 |
emr | emr 2876 | 8 8 17 | 7 7 21 | 7 9 19 |
esa | esa 2880 | 6 8 15 | 6 7 24 | 8 13 19 |
gfz | gfz 2865 | 6 8 13 | 7 8 24 | 8 11 18 |
grg | grg 2865 | 12 8 28 | 7 7 24 | 9 11 19 |
igr | igr 2880 | 6 8 15 | 5 7 18 | 7 9 17 |
igs | igs 2880 | 6 8 15 | 6 6 19 | 8 11 17 |
jpl | jpl 2875 | 8 12 16 | 6 5 19 | 7 11 21 |
mit | mit 2880 | 6 9 16 | 7 11 22 | 7 11 17 |
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 6.1789 GPS week: 1789 MJD: 56767.500-56773.500
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 | 24 -26 99 264 0 | 12 19
| 24 17 97 99 5 | 2
emr uuuuu | 37 -5 6 15 -7 | 31 38
| 26 24 73 59 13 | 5
esa uuuuu | -12 17 99 58 6 | 12 19
| 14 17 58 13 5 | 2
gfz uuuuu | -21 -7 131 -17 -5 | 19 26
| 22 31 83 99 5 | 3
grg uuuuu | -23 20 -173 -226 3 | 31 35
| 24 17 55 148 5 | 2
igr xxxxx | -8 37 63 -59 3 | -5 18
| 16 20 76 72 9 | 2
irf xxxxx | -5 3 -38 -83 -4 | -1 14
| 5 9 21 37 3 | 1
jpl uuuuu | -25 -12 30 -90 1 | 16 25
| 50 19 46 56 10 | 3
mit uuuuu | -28 -53 -127 -217 -8 | 28 32
| 14 35 35 65 8 | 1
ngs uuuuu | 35 82 -123 82 -1 | 4 12
| 78 53 120 138 4 | 2
sio xxxxx | -13 26 12 -193 -18 | 62 63
| 44 44 77 54 4 | 9
Table 7.1789.0 GPS week: 1789 Day: 0 MJD: 56767.500
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 | -14 -26 101 450 2 | 14 21
emr uuuuu | 27 20 -96 -70 -29 | 37 43
esa uuuuu | -16 27 163 41 2 | 11 19
gfz uuuuu | -4 28 70 67 -13 | 25 30
grg uuuuu | -47 15 -217 -262 9 | 31 36
igr xxxxx | -30 54 204 -191 -12 | -2 16
irf xxxxx | -10 12 -31 -71 0 | 1 14
jpl uuuuu | -14 15 38 -109 -1 | 20 29
mit uuuuu | -28 -119 -101 -184 4 | 29 32
ngs uuuuu | 87 45 -15 -46 2 | 7 13
sio xxxxx | -5 -2 -6 -206 -16 | 75 76
Table 7.1789.1 GPS week: 1789 Day: 1 MJD: 56768.500
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 -21 60 288 -9 | 12 19
emr uuuuu | 35 22 -3 28 -8 | 34 42
esa uuuuu | -3 29 3 76 5 | 9 18
gfz uuuuu | -10 18 163 29 -7 | 21 28
grg uuuuu | -36 49 -255 -466 3 | 30 35
igr xxxxx | 21 6 68 -74 8 | -6 18
irf xxxxx | -4 8 -20 -76 -4 | -1 15
jpl uuuuu | 38 -45 52 -93 18 | 17 27
mit uuuuu | -24 -82 -94 -228 -3 | 28 32
ngs uuuuu | -94 49 25 144 0 | 5 13
sio xxxxx | 66 100 28 -191 -26 | 69 71
Table 7.1789.2 GPS week: 1789 Day: 2 MJD: 56769.500
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 | 33 -34 64 315 -5 | 12 19
emr uuuuu | -5 2 40 -31 -12 | 35 43
esa uuuuu | -12 4 61 69 11 | 10 19
gfz uuuuu | -5 -3 66 98 -3 | 20 27
grg uuuuu | -44 29 -87 -292 0 | 31 36
igr xxxxx | -15 32 17 -3 -4 | -5 18
irf xxxxx | -7 10 -61 -41 -3 | 0 15
jpl uuuuu | -34 -7 69 -75 0 | 18 28
mit uuuuu | -55 -39 -146 -159 -6 | 29 32
ngs uuuuu | 87 56 -96 -101 0 | 5 13
sio xxxxx | -63 -4 86 -105 -21 | 65 68
Table 7.1789.3 GPS week: 1789 Day: 3 MJD: 56770.500
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 | 22 -23 -35 149 6 | 10 19
emr uuuuu | 35 1 72 89 -12 | 31 40
esa uuuuu | -10 11 117 47 9 | 11 19
gfz uuuuu | -19 -29 175 -6 -6 | 18 26
grg uuuuu | -39 24 -139 -270 -1 | 30 35
igr xxxxx | -1 24 60 27 8 | -7 19
irf xxxxx | -7 4 -55 -41 -1 | -1 16
jpl uuuuu | -30 2 22 -23 5 | 16 27
mit uuuuu | -31 -35 -162 -126 -5 | 28 32
ngs uuuuu | 61 67 -62 24 -5 | 5 13
sio xxxxx | -49 55 51 -171 -15 | 60 63
Table 7.1789.4 GPS week: 1789 Day: 4 MJD: 56771.500
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 | 38 -51 72 202 1 | 12 20
emr uuuuu | 39 -9 -94 -20 2 | 29 37
esa uuuuu | 12 -8 131 63 10 | 13 21
gfz uuuuu | -4 -36 259 -47 2 | 18 26
grg uuuuu | -5 19 -156 -158 7 | 31 36
igr xxxxx | -16 30 77 -90 12 | -6 20
irf xxxxx | 6 -14 -6 -141 -4 | 0 16
jpl uuuuu | -42 -7 86 -171 -2 | 15 25
mit uuuuu | -14 -21 -80 -317 -10 | 29 33
ngs uuuuu | -43 139 -251 307 -4 | 4 13
sio xxxxx | -40 6 103 -275 -18 | 58 60
Table 7.1789.5 GPS week: 1789 Day: 5 MJD: 56772.500
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 | 34 -29 153 228 4 | 9 17
emr uuuuu | 81 -33 47 30 15 | 23 28
esa uuuuu | -23 11 63 59 10 | 11 19
gfz uuuuu | -42 -48 162 -61 1 | 15 20
grg uuuuu | 2 8 -155 -137 5 | 29 34
igr xxxxx | -14 49 59 -64 12 | -8 19
irf xxxxx | -4 -1 -56 -95 -5 | -3 14
jpl uuuuu | -114 -13 -28 -20 1 | 11 19
mit uuuuu | -33 -31 -169 -246 -15 | 26 30
ngs uuuuu | 120 178 -163 87 -4 | 1 9
sio xxxxx | -9 -24 -77 -237 -19 | 52 54
Table 7.1789.6 GPS week: 1789 Day: 6 MJD: 56773.500
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 6 277 216 0 | 12 17
emr uuuuu | 48 -40 74 81 -6 | 27 31
esa uuuuu | -32 44 153 49 -3 | 16 19
gfz uuuuu | -60 25 19 -201 -8 | 18 21
grg uuuuu | 8 -6 -200 7 -3 | 34 36
igr xxxxx | 0 65 -47 -19 -1 | -4 15
irf xxxxx | -8 3 -36 -115 -10 | 0 11
jpl uuuuu | 22 -27 -32 -140 -16 | 14 19
mit uuuuu | -14 -45 -134 -260 -18 | 28 30
ngs uuuuu | 26 44 -297 158 6 | 3 8
sio xxxxx | 10 54 -98 -168 -13 | 51 53
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