[IGSREPORT-23469] Wk 1835 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Mar 26 09:05:26 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1835 (Mar 08, 2015 - Mar 14, 2015)
Contacts: igs.acc at noaa.gov
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1835[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1835[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1835[0-6].cls IGS GPS clock combination summary report.
igs18357.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18357.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 | SYOG SYOG
0 | ESA | NTUS NTUS TIXI
0 | GRG | DAV1 KELY SYOG DAV1 KELY NKLG SYOG
0 | MIT | HYDE
1 | COD | MATE
1 | ESA | BOGT MATE MATE SEY1
1 | GRG | DAV1 KOUC MATE ONSA SYOG DAV1 KOUC ONSA SYOG
1 | MIT | TSKB TSKB
2 | COD | NTUS NTUS
2 | ESA | SOFI SOFI
2 | GFZ | HOLB HOLB
2 | GRG | BOR1 DARW DAV1 GRAZ IRKJ ONSA TIDB TLSE BOR1 DAV1
2 | GRG | GRAZ ONSA THTI TIDB TLSE
2 | JPL | CAS1
3 | COD | BRST CHUR DAV1 BRST CHUR DAV1
3 | ESA | UNSA
3 | GFZ | NRIL TLSE
3 | GRG | DARW DAV1 HYDE DAV1 HYDE
4 | COD | MAG0
4 | ESA | MAG0
4 | GFZ | 8
4 | GRG | BRST ONSA WES2 WSRT BRST ONSA WSRT
5 | COD | CAS1 CAS1
5 | GFZ | GRAZ GRAZ
5 | GRG | GRAZ IISC WES2 GRAZ IISC TLSE WES2
6 | ESA | 8 8
6 | GFZ | REUN BOGT REUN
6 | GRG | BOGT FAIR GOPE GRAZ REUN BOGT DAV1 FAIR GOPE GRAZ
6 | GRG | MONP REUN
6 | JPL | BOGT
6 | MIT | BAKO RBAY BAKO RBAY
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G29 | 2015_03_12 | 2015016
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 G10 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.6 -.9 -2.4 -43 -1 6 .73
EMR | 0 | 1.2 .4 14.0 64 -14 62 .67
ESA | 0 | 1.1 -1.5 -.7 -2 -21 77 .64
GFZ | 0 | .1 -1.1 -2.2 -26 -65 -4 .80
GRG | 0 | 7.8 -.1 3.5 7 8 13 1.13
JPL | 0 | 3.3 2.9 12.3 16 5 4 .98
MIT | 0 | 3.2 -2.3 -1.3 11 15 -39 .80
NGS | 0 | 4.7 -.1 4.8 -10 -22 26 .76
SIO | 0 | -1.1 .7 -10.1 -10 -14 -35 .75
COD | 1 | -1.1 -.8 -2.4 -55 17 -37 .69
EMR | 1 | 3.9 -.2 12.5 66 -13 43 .59
ESA | 1 | .7 -1.3 -.7 -13 -22 40 .59
GFZ | 1 | .4 -1.1 -.8 -25 -77 -31 .63
GRG | 1 | 8.2 -1.4 -5.2 16 -7 -3 1.04
JPL | 1 | -1.9 -5.6 8.6 -2 44 -1 .74
MIT | 1 | 4.2 -3.5 1.0 5 -15 -52 .67
NGS | 1 | 3.4 -1.4 13.0 -36 -51 -14 .52
SIO | 1 | .9 -.1 -13.6 -2 -19 -31 .54
COD | 2 | -1.3 -.9 -3.0 -39 9 -17 .81
EMR | 2 | 1.2 4.2 10.3 50 -1 49 .50
ESA | 2 | 1.2 -1.5 -.3 6 -24 36 .67
GFZ | 2 | .2 -.7 -1.3 -22 -66 -35 .69
GRG | 2 | 6.5 -.7 4.4 -3 23 -4 1.05
JPL | 2 | -4.7 -6.0 9.2 -31 31 11 .87
MIT | 2 | 7.3 -.9 4.6 5 3 -48 .79
NGS | 2 | 4.1 -.8 22.9 -84 -79 -13 .70
SIO | 2 | 3.6 1.7 -11.5 -22 -20 -51 .67
COD | 3 | -1.9 -.8 -2.0 -22 -2 -7 .77
EMR | 3 | 5.2 3.9 16.1 65 -12 69 .63
ESA | 3 | .7 -1.6 .2 -17 -19 38 .64
GFZ | 3 | -.2 -1.3 -1.2 -17 -52 -13 .77
GRG | 3 | .6 -2.5 1.9 -8 -6 -38 1.12
JPL | 3 | -.2 -1.8 9.1 -6 29 15 .99
MIT | 3 | 7.4 -3.7 7.2 4 -17 -65 .85
NGS | 3 | 4.7 -.2 15.3 -38 -69 8 .84
SIO | 3 | 3.0 -3.8 -9.8 -13 -23 -70 .77
COD | 4 | -1.8 -1.1 -2.8 -45 -5 -13 .76
EMR | 4 | 3.6 1.8 15.7 56 -11 42 .63
ESA | 4 | .9 -2.1 -.4 -32 -16 17 .74
GFZ | 4 | -.2 -1.5 -1.9 -29 -66 -13 .82
GRG | 4 | 4.6 -3.9 .2 -11 -6 -47 1.08
JPL | 4 | 2.8 -3.7 10.7 -4 8 -13 1.06
MIT | 4 | 6.7 -5.8 7.0 3 -9 -44 .78
NGS | 4 | 1.1 -4.4 8.4 -28 -26 -28 .86
SIO | 4 | -2.1 -1.1 -18.4 -18 -23 -39 .59
COD | 5 | -1.3 -1.0 -2.0 -27 -15 -22 .82
EMR | 5 | 6.1 -.5 16.5 25 -9 13 .63
ESA | 5 | 1.1 -1.8 .0 -14 -25 56 .82
GFZ | 5 | .3 -.4 -1.9 5 -69 -47 .90
GRG | 5 | 2.9 -1.7 10.6 2 -17 -42 1.24
JPL | 5 | 4.9 -2.3 14.7 -41 50 4 1.33
MIT | 5 | 8.1 -2.8 5.9 7 4 -58 .89
NGS | 5 | 5.4 -1.9 20.8 -62 -71 -9 .84
SIO | 5 | .4 -.7 -8.2 -19 -3 -51 .85
COD | 6 | -1.6 -1.3 -2.1 -40 -4 -35 .71
EMR | 6 | 1.7 -.3 10.5 47 -4 24 .54
ESA | 6 | 1.6 -.8 .7 15 -58 69 .64
GFZ | 6 | .5 -.8 -1.3 -4 -79 -31 .76
GRG | 6 | 10.1 -.4 13.3 -6 -3 -39 1.12
JPL | 6 | 8.7 -2.4 15.1 -29 51 25 1.00
MIT | 6 | 10.7 -3.9 5.6 0 -17 -44 .67
NGS | 6 | 8.3 -2.4 17.8 -74 -82 17 .56
SIO | 6 | 5.5 -1.7 -11.4 -9 -39 -25 .56
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 1.1835.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1835.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 2.1835.[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 3.1835.[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 5.1835.0-6). 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 1835 summary. (Mar 08, 2015 - Mar 14, 2015)
Table 1.1835.a GPS week: 1835 MJD: 57089.000-57095.000
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 249| 0 0 -3 0 24 -7 .03 13 13 | -951 -18 16 115
| 0 1 2 13 22 16 .03 | 331 510
emr 80| 0 0 2 19 -17 49 .13 12 12 | 2597 739 14 167
| 0 1 1 14 11 17 .02 | 1859 720
esa 150| 0 0 -1 -9 -5 8 -.35 11 11 | -590 168 9 148
| 0 0 1 15 13 13 .02 | 1102 452
gfz 205| 0 0 -1 11 -10 -3 .08 11 11 | 25 3 9 78
| 0 0 1 8 10 7 .03 | 455 795
grg 175| 3 -2 5 -26 6 -12 .28 18 17 | -12 81 15 141
| 0 2 3 18 26 16 .13 | 244 742
igr n/a| 0 0 -3 -12 -6 2 -.02 5 5 | -5184 690 15 77
| 0 0 0 14 11 14 .01 | 1866 792
jpl 80| 0 1 4 -9 11 26 .22 11 11 | 2660 732 17 111
| 0 1 1 16 22 14 .02 | 1882 730
mit 350| 1 -2 0 1 -3 -12 -.09 13 13 | -351 -262 45 189
| 1 0 0 13 31 17 .02 | 359 696
ngs 234| 0 0 2 -1 -3 -31 -.11 10 9 | -938 31 1528 3048
| 0 0 2 15 33 19 .04 | 354 527
sio 322| -1 0 -5 -9 -4 -17 -.22 14 14 | --- --- --- ---
| 0 0 1 23 34 27 .02 | --- ---
Table 1.1835.b GPS week : 1835 MJD: 57089.000-57095.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 4 5 5 5 5 5 5 |
3 | 6 5 5 5 6 5 5 |
4 | 4 4 4 4 5 5 5 |
5 | 4 4 4 5 5 4 4 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 5 5 5 4 7 5 5 |
9 | 4 4 3 4 4 4 4 |
10 | 4 7 4 4 4 4 5 |
11 | 4 4 4 4 5 4 4 |
12 | 5 5 5 6 6 5 5 |
13 | 4 5 4 5 4 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 4 4 5 4 5 |
18 | 5 5 5 5 5 5 5 |
19 | 6 6 6 6 6 6 5 |
20 | 4 5 4 4 4 4 4 |
21 | 5 5 4 5 5 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 4 5 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 5 4 5 |
26 | --- --- --- 0 13 9 19 |
27 | 4 4 4 4 3 3 4 |
28 | 4 4 4 5 4 4 4 |
29 | 6 6 5 6 0 6 6 |
30 | 3 4 3 4 4 4 4 |
31 | 4 5 5 5 5 5 4 |
32 | 4 4 3 4 4 4 5 |
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 2.1835.0 GPS week: 1835 Day: 0 MJD: 57089.000
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 249| 0 1 0 -12 -4 23 .06 13 13 | -726 -342 19 115
emr 80| 0 0 4 13 -32 26 .15 12 12 | 534 -151 12 146
esa 150| 0 0 -2 -5 0 26 -.33 12 12 | -989 -101 9 130
gfz 205| 0 0 -2 14 -7 0 .10 10 10 | 494 -1409 9 78
grg 180| 3 0 6 -9 28 -18 .07 20 18 | 40 -1003 14 149
igr n/a| 0 0 -2 -23 -22 -27 -.03 5 5 | -7145 -613 15 76
jpl 80| 0 2 6 16 8 15 .21 11 11 | 571 -147 17 120
mit 350| 0 -3 0 7 -2 -32 -.08 12 11 | 33 -830 44 204
ngs 238| 0 0 -2 -17 18 -25 -.04 9 8 | -578 -585 1390 3030
sio 327| 0 0 -3 -17 -24 -13 -.26 14 13 | --- --- --- ---
Table 2.1835.1 GPS week: 1835 Day: 1 MJD: 57090.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 246| 0 2 -1 -1 12 -15 .02 13 13 | -1107 180 17 108
emr 80| 0 -1 1 29 -2 53 .13 13 13 | 842 1186 12 171
esa 150| 0 1 -2 -3 6 0 -.35 12 11 | 134 810 9 145
gfz 204| 0 0 0 11 -7 -7 .13 11 12 | -437 791 10 73
grg 177| 3 0 0 0 44 8 .20 17 16 | -185 715 14 125
igr n/a| 0 0 -3 -15 -2 11 -.02 5 5 | -7198 1096 15 84
jpl 80| 0 -1 5 -28 12 48 .24 13 13 | 842 1180 18 100
mit 350| 0 -2 -1 7 26 -35 -.08 12 12 | -813 363 46 195
ngs 231| 0 2 2 -27 -67 -51 -.07 10 9 | -1045 53 1331 2880
sio 321| -1 0 -4 9 16 27 -.23 14 14 | --- --- --- ---
Table 2.1835.2 GPS week: 1835 Day: 2 MJD: 57091.000
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| 0 0 -4 21 28 -14 .01 11 11 | -992 -97 15 115
emr 80| -1 0 2 20 -14 78 .11 11 11 | 1216 679 12 176
esa 150| 0 0 -4 10 -9 4 -.32 11 11 | 146 -317 9 153
gfz 205| 0 -1 -1 9 -16 9 .09 11 10 | -46 262 9 73
grg 172| 4 -1 4 -38 26 0 .22 16 15 | -314 868 15 137
igr n/a| 0 0 -3 -15 -16 3 -.03 5 5 | -6478 687 13 71
jpl 80| 0 1 3 -31 1 7 .21 11 11 | 1298 665 18 103
mit 350| 0 -3 -1 -6 -14 -3 -.08 12 13 | -583 -636 43 207
ngs 233| 0 0 6 1 17 -60 -.14 10 9 | -1137 380 1523 2719
sio 319| -1 0 -6 -20 -31 -16 -.19 14 13 | --- --- --- ---
Table 2.1835.3 GPS week: 1835 Day: 3 MJD: 57092.000
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| 0 0 -2 10 33 -9 -.00 13 13 | -1099 524 17 115
emr 80| 0 0 1 25 -21 60 .14 12 12 | 2021 1999 16 171
esa 150| 0 1 -3 -11 -15 7 -.35 11 11 | 357 -290 9 135
gfz 206| 0 0 -1 13 0 2 .07 12 11 | 410 -245 10 79
grg 168| 3 -1 4 -35 -12 -39 .25 17 17 | 400 -833 16 132
igr n/a| 0 1 -2 9 -6 7 -.03 6 6 | -5663 1967 16 87
jpl 80| 1 1 3 0 30 31 .20 11 11 | 2091 2025 19 105
mit 350| 1 -2 0 -15 8 -19 -.08 13 12 | -26 -613 44 185
ngs 235| -1 0 1 3 -13 -5 -.12 11 10 | -906 250 1362 3358
sio 324| -1 0 -3 -35 -1 -63 -.21 14 15 | --- --- --- ---
Table 2.1835.4 GPS week: 1835 Day: 4 MJD: 57093.000
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 253| 1 0 -4 -7 60 4 .05 13 13 | -1505 658 17 117
emr 80| -1 0 2 35 -6 48 .13 12 12 | 4389 401 16 167
esa 150| -1 0 0 -35 15 -15 -.37 12 11 | -926 714 10 181
gfz 208| 0 0 -2 6 1 -7 .05 11 11 | 564 -577 10 89
grg 178| 3 -2 6 -52 -27 -19 .36 17 17 | -210 464 17 146
igr n/a| 0 1 -3 4 -4 9 .01 5 5 | -3361 307 16 76
jpl 80| 0 2 3 -4 39 17 .26 11 11 | 4484 389 18 114
mit 350| 2 -3 0 13 -44 -10 -.07 14 14 | -729 990 44 174
ngs 235| 0 0 0 3 -24 -20 -.10 10 9 | -1537 739 2061 3213
sio 329| -2 0 -5 -1 -47 -25 -.22 15 14 | --- --- --- ---
Table 2.1835.5 GPS week: 1835 Day: 5 MJD: 57094.000
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 249| 0 0 -7 7 3 -19 .07 13 13 | -733 -258 16 116
emr 80| 0 -1 2 21 -30 43 .11 12 12 | 4512 936 18 186
esa 150| 0 0 0 -21 -18 14 -.35 11 11 | -2779 195 9 136
gfz 204| 0 0 -1 24 -28 -14 .06 11 11 | -429 624 10 86
grg 175| 2 -2 7 -23 -15 -17 .36 17 16 | 40 417 16 158
igr n/a| 0 1 -3 -19 -6 14 -.03 5 5 | -3436 952 15 75
jpl 80| 0 1 3 -13 -30 22 .23 10 10 | 4566 919 18 120
mit 350| 2 -2 0 -15 40 1 -.11 14 13 | -16 -245 46 199
ngs 234| 0 0 2 18 25 -20 -.15 10 9 | -887 134 1699 3284
sio 318| 0 0 -7 -32 54 -4 -.21 13 12 | --- --- --- ---
Table 2.1835.6 GPS week: 1835 Day: 6 MJD: 57095.000
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 1 -4 -17 36 -25 .03 13 13 | -495 -795 17 119
emr 80| -2 0 0 -10 -13 33 .12 12 12 | 4671 124 13 155
esa 150| 0 0 -2 1 -18 18 -.39 11 11 | -75 171 10 157
gfz 204| 0 -1 -3 -3 -14 -3 .07 11 11 | -378 575 9 69
grg 179| 3 -6 11 -27 4 0 .47 22 19 | 142 -60 19 140
igr n/a| 0 0 -3 -27 12 -1 -.02 6 5 | -3012 437 15 70
jpl 80| 0 1 3 -5 20 42 .22 10 10 | 4770 99 17 118
mit 350| 3 -1 0 18 -37 8 -.12 15 15 | -328 -869 48 164
ngs 234| 1 1 5 10 16 -39 -.13 10 9 | -479 -749 1336 2857
sio 319| 0 0 -6 28 5 -23 -.23 14 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 3.1835.0 GPS week: 1835 Day: 0 MJD: 57089.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 12 14 6 14 7 10 7 6 8 3 | 35 34 41 35 35 35 36 34 33 34 34
2 | 11 14 7 12 21 4 11 14 7 16 4 | 27 24 21 21 25 21 28 21 20 19 20
X3 | 23 18 10 13 --- 5 16 12 11 15 5 | 61 66 65 68 --- 64 75 70 60 68 66
4 | 14 10 11 8 19 4 9 8 9 15 4 | 34 36 36 32 30 34 38 34 32 42 34
5 | 8 14 8 10 25 4 14 11 8 12 4 | 36 32 27 36 44 32 33 36 31 31 32
6 | 13 9 12 8 12 5 9 15 8 11 3 | 43 40 46 39 41 41 41 40 39 43 40
7 | 10 10 11 8 17 4 8 9 8 12 3 | 27 30 21 26 27 23 29 23 24 25 24
X8 | 11 12 14 13 20 9 7 11 10 --- 4 | 21 31 22 23 6 20 25 17 20 --- 20
9 | 9 11 13 10 13 5 7 5 8 14 3 | 47 46 40 47 49 43 48 45 43 46 44
10 | 15 13 9 11 19 5 8 15 6 11 4 | 214 214 212 210 148 213 213 212 212 213 212
11 | 13 8 17 8 26 4 10 10 9 10 4 | 28 31 20 28 40 22 33 22 25 20 25
12 | 19 15 10 11 25 2 16 12 10 11 5 | 29 30 17 30 38 23 29 24 26 22 24
13 | 9 14 9 13 15 4 15 10 10 13 4 | 41 40 40 43 44 38 43 36 36 35 38
14 | 15 11 13 11 15 2 12 11 14 20 4 | 33 33 31 42 35 34 30 38 39 41 34
15 | 16 14 12 15 16 4 16 12 11 19 5 | 36 33 27 34 31 27 34 26 25 31 28
16 | 15 12 12 12 23 5 12 17 10 19 5 | 27 26 20 26 30 21 26 24 25 19 22
17 | 11 11 12 12 17 6 14 12 10 17 4 | 29 36 24 35 33 26 35 33 33 26 30
18 | 22 15 9 14 23 4 15 10 10 15 5 | 24 20 15 26 31 20 22 22 21 21 18
19 | 19 11 13 10 22 7 10 25 11 19 5 | 27 28 22 24 31 20 28 22 23 20 22
20 | 12 13 8 9 19 5 10 14 6 10 4 | 44 45 41 45 50 43 43 43 42 40 42
21 | 9 15 8 14 25 5 13 11 10 18 4 | 20 24 18 16 28 18 26 18 19 19 17
22 | 16 12 9 8 23 4 13 9 9 11 4 | 23 25 21 26 35 23 23 27 25 27 23
23 | 11 9 12 12 14 4 10 8 9 14 3 | 33 34 31 38 36 32 36 32 33 33 32
24 | 11 10 14 6 13 3 11 12 7 14 3 | 26 31 29 29 28 26 33 26 27 28 27
25 | 11 13 16 7 16 4 9 9 7 9 3 | 25 31 29 28 33 24 30 24 27 23 26
27 | 11 8 16 7 18 4 8 7 6 8 3 | 28 32 26 28 39 26 33 30 29 28 29
28 | 10 9 10 11 25 5 10 11 8 10 4 | 23 29 17 29 37 20 26 26 23 17 23
29 | 17 13 13 15 24 6 15 19 12 22 5 | 33 28 20 23 25 22 28 22 23 31 25
30 | 12 9 12 6 13 4 8 8 5 8 3 | 29 33 33 32 32 29 34 29 29 30 30
31 | 12 11 12 11 20 4 11 11 7 12 4 | 26 32 23 26 35 25 32 25 27 21 25
32 | 15 10 10 6 21 5 8 9 7 11 3 | 41 45 42 43 47 41 45 44 41 46 43
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 12 10 20 5 11 12 9 14 |T 37 39 34 38 38 35 39 36 35 36 35
WRMS | 13 12 12 10 18 5 11 11 8 13 |NE 37 39 34 38 37 34 39 36 35 36 35
MEDI | 12 12 12 11 19 4 10 11 9 12 |MD 29 32 27 30 35 26 33 27 27 28 28
Table 3.1835.1 GPS week: 1835 Day: 1 MJD: 57090.000
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 15 13 7 12 4 14 8 10 10 4 | 30 28 33 29 32 30 33 27 30 30 29
2 | 13 10 8 13 19 4 15 14 10 15 4 | 23 25 20 18 24 19 28 18 22 15 19
X3 | 18 19 9 14 --- 8 15 13 11 13 5 | 49 53 53 57 --- 51 61 56 51 53 53
4 | 11 10 10 9 19 6 14 9 7 16 4 | 24 26 24 22 23 24 32 25 25 33 24
5 | 8 13 9 9 18 3 15 11 9 11 4 | 30 28 20 27 37 26 32 29 28 28 26
6 | 10 12 11 8 11 5 11 14 12 11 4 | 29 32 31 28 33 29 34 28 30 32 29
7 | 12 13 13 10 14 3 11 10 7 15 4 | 25 30 18 24 28 20 25 21 22 20 21
X8 | 9 17 14 8 --- 7 13 14 9 --- 5 | 22 29 24 20 --- 19 25 15 19 --- 20
9 | 8 10 12 8 11 4 10 6 7 14 3 | 30 34 28 30 35 28 34 29 30 30 30
X10 | 16 20 17 15 --- 12 24 20 21 18 7 | 400 392 398 390 --- 389 391 400 389 395 393
11 | 9 9 16 9 24 6 12 9 9 9 4 | 23 29 19 25 36 20 29 21 23 18 22
12 | 17 15 9 13 22 5 18 12 13 11 5 | 25 26 14 27 32 20 26 20 24 17 20
13 | 10 12 9 14 13 4 18 11 13 16 4 | 30 32 27 28 31 26 32 24 26 22 25
14 | 15 11 14 14 15 5 11 12 10 19 4 | 28 25 24 32 27 26 27 25 26 26 25
15 | 13 14 9 13 11 3 18 12 10 17 4 | 29 31 25 31 27 25 34 25 24 26 25
16 | 17 16 11 14 18 6 12 13 9 20 5 | 26 26 16 23 25 17 22 21 21 19 19
17 | 11 13 11 16 15 5 14 10 13 15 4 | 25 28 23 31 26 22 30 23 26 22 24
18 | 16 14 7 14 20 6 13 10 13 14 4 | 23 19 17 25 26 18 22 20 24 19 19
19 | 20 13 11 13 20 8 11 24 13 16 5 | 28 27 20 20 23 18 26 18 22 15 19
20 | 9 11 12 13 16 4 13 11 16 14 4 | 42 45 41 47 50 42 44 46 42 41 43
21 | 10 17 10 13 22 5 15 11 9 16 4 | 19 22 16 16 28 18 23 17 19 17 16
22 | 17 13 7 10 19 5 12 10 11 12 4 | 22 21 17 23 29 19 21 20 19 21 19
23 | 9 9 12 9 10 4 13 8 9 15 3 | 24 27 24 24 25 22 28 22 23 18 22
24 | 10 9 13 9 13 4 11 13 9 10 4 | 23 24 24 26 27 23 27 22 25 24 23
25 | 10 11 15 7 12 4 9 8 8 9 3 | 22 24 27 25 27 22 24 18 21 18 21
27 | 12 9 14 8 16 5 9 7 8 7 3 | 25 28 21 23 30 21 28 22 24 22 24
28 | 10 16 10 11 18 4 10 11 9 9 4 | 16 23 15 23 30 17 23 19 16 17 17
29 | 15 13 13 13 20 6 15 18 14 20 5 | 25 26 19 20 21 19 26 18 21 24 21
30 | 14 11 12 8 11 3 7 9 9 9 3 | 25 29 27 22 28 24 30 23 22 25 24
31 | 17 20 15 16 20 4 11 10 11 14 5 | 30 32 23 30 35 24 32 23 28 20 25
32 | 14 11 9 10 15 7 10 11 8 9 3 | 39 43 39 41 41 39 40 38 38 41 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 13 12 11 17 5 13 12 10 14 |T 39 40 36 38 29 36 41 36 37 36 36
WRMS | 13 13 11 12 16 5 13 12 9 14 |NE 38 40 36 38 29 35 41 36 37 36 36
MEDI | 12 13 11 11 16 5 13 11 10 14 |MD 25 28 24 25 28 22 28 22 24 22 24
Table 3.1835.2 GPS week: 1835 Day: 2 MJD: 57091.000
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 11 12 8 13 6 10 8 7 11 3 | 34 30 38 31 31 32 33 31 31 36 32
2 | 15 14 9 14 16 4 10 14 10 13 4 | 27 23 21 19 21 18 24 17 20 15 18
X3 | 14 17 9 14 --- 8 15 14 13 15 5 | 62 63 63 65 --- 61 68 65 55 65 61
4 | 7 7 11 8 20 4 9 11 9 18 4 | 26 27 29 25 22 25 29 27 26 38 26
5 | 8 13 8 10 18 3 14 15 7 12 4 | 32 33 25 32 38 28 30 33 28 27 29
6 | 11 10 12 11 10 5 9 12 6 11 3 | 37 37 40 32 33 34 37 31 33 36 34
7 | 8 10 11 10 17 2 12 13 7 13 4 | 26 27 19 25 31 21 27 22 25 19 22
X8 | 7 10 11 12 --- 9 8 11 13 --- 4 | 18 27 21 22 --- 19 25 17 27 --- 20
9 | 8 8 13 8 11 5 8 6 5 15 3 | 38 38 34 39 40 37 38 35 34 38 36
10 | 10 11 11 9 16 5 9 12 9 11 3 | 223 229 222 226 295 226 223 229 217 228 225
11 | 7 8 16 8 21 6 8 11 11 10 4 | 22 27 21 23 36 19 26 19 26 16 21
12 | 15 12 9 13 24 4 15 13 12 13 5 | 27 28 18 31 36 24 29 23 34 21 24
13 | 8 12 9 12 15 3 12 12 12 15 4 | 30 36 31 31 37 29 36 29 32 28 30
14 | 11 11 11 15 15 6 11 14 11 19 4 | 31 29 28 39 32 29 29 31 27 35 29
15 | 12 13 12 14 13 4 12 12 12 18 4 | 33 31 27 32 29 26 31 26 27 30 27
16 | 20 12 10 12 17 5 12 14 12 18 5 | 30 25 19 22 27 19 26 22 23 18 20
17 | 12 11 12 13 13 5 12 13 11 14 4 | 22 29 20 25 27 19 28 22 26 18 21
18 | 11 13 8 16 19 5 13 10 12 16 4 | 25 21 19 30 30 20 22 22 24 23 20
19 | 18 10 11 12 19 6 11 25 12 19 5 | 28 26 23 22 26 18 26 18 24 15 21
20 | 7 15 10 12 17 4 11 10 11 12 4 | 42 38 38 46 45 39 38 42 42 33 39
21 | 14 11 10 13 17 4 9 10 10 17 4 | 23 22 17 15 25 16 21 17 18 15 15
22 | 8 13 8 10 20 5 11 9 10 10 4 | 22 21 20 26 30 20 20 23 19 22 20
23 | 9 12 11 12 10 4 10 12 12 15 4 | 29 31 28 34 29 29 31 25 27 25 27
24 | 10 9 13 9 16 4 10 12 12 10 4 | 24 26 26 28 30 24 27 24 28 24 24
25 | 10 15 14 8 11 4 10 10 8 10 4 | 27 29 29 30 30 26 28 22 28 24 26
27 | 11 7 13 8 14 3 13 8 11 8 3 | 27 29 27 26 34 25 30 26 32 23 27
28 | 11 7 10 9 16 5 10 9 10 10 3 | 21 24 14 25 31 18 24 22 21 17 20
29 | 13 12 12 14 18 7 12 19 12 18 5 | 26 25 19 23 19 20 22 18 23 25 22
30 | 9 10 12 5 12 3 11 9 6 9 3 | 25 28 30 27 31 26 32 27 30 28 27
31 | 11 20 14 15 20 4 12 14 10 12 5 | 29 35 24 32 36 26 32 24 31 22 26
32 | 10 7 9 9 13 6 8 10 7 12 3 | 45 47 48 50 47 46 47 50 43 51 47
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 11 11 16 5 11 12 10 14 |T 35 36 33 36 40 32 36 33 34 33 33
WRMS | 11 11 11 10 15 5 11 13 9 13 |NE 35 36 33 36 40 32 36 33 34 33 33
MEDI | 10 11 11 12 16 5 11 12 11 13 |MD 27 29 26 30 31 25 29 24 27 24 26
Table 3.1835.3 GPS week: 1835 Day: 3 MJD: 57092.000
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 12 8 12 6 10 7 9 12 3 | 33 33 37 32 32 33 35 34 31 36 33
2 | 16 14 10 15 18 5 10 15 11 15 4 | 31 26 24 22 23 21 27 19 21 21 21
X3 | 17 15 8 14 --- 6 13 12 15 12 5 | 61 67 65 65 --- 63 70 71 63 68 65
4 | 11 8 11 9 18 5 8 12 13 17 4 | 27 29 30 25 27 26 30 30 26 37 27
5 | 11 16 8 9 18 4 15 13 9 11 4 | 32 32 25 32 35 28 30 30 31 30 29
6 | 12 9 12 9 12 4 8 11 9 12 3 | 45 40 43 38 38 38 41 35 41 41 39
7 | 10 10 15 8 15 5 11 12 9 12 4 | 30 32 26 29 31 25 30 27 26 23 26
X8 | 11 9 11 9 --- 7 9 12 12 --- 4 | 22 26 20 23 --- 21 23 19 20 --- 20
9 | 7 10 14 7 11 4 8 7 7 16 3 | 37 40 34 39 40 38 39 38 35 41 37
10 | 14 11 11 10 18 7 10 13 8 12 4 | 246 245 244 243 182 243 243 248 243 244 244
11 | 8 10 15 10 19 10 9 10 11 12 4 | 25 31 22 23 38 20 30 23 24 21 24
12 | 18 16 7 15 25 5 17 15 14 14 5 | 29 27 19 30 33 24 29 25 26 23 23
13 | 13 12 10 14 15 5 13 11 10 16 4 | 34 36 33 34 36 32 37 29 31 30 31
14 | 14 10 11 16 15 7 10 15 12 19 4 | 34 30 31 40 35 32 31 37 32 35 32
15 | 12 13 10 15 15 5 14 13 11 16 4 | 32 31 26 31 28 27 34 27 30 28 27
16 | 10 13 9 13 17 6 12 10 11 21 4 | 23 22 16 26 28 20 23 22 24 22 20
17 | 11 11 12 11 14 7 10 14 12 15 4 | 27 29 22 27 31 22 31 29 24 27 25
18 | 16 15 6 16 21 7 13 13 9 17 5 | 24 19 17 26 30 19 21 24 21 20 18
19 | 16 11 10 15 18 7 11 24 15 17 5 | 26 26 21 24 26 20 26 20 21 18 20
20 | 10 15 9 10 16 5 10 11 9 13 4 | 45 44 42 48 50 43 45 47 45 42 44
21 | 14 13 7 16 22 6 12 10 9 16 4 | 26 23 18 17 24 19 26 19 19 19 17
22 | 11 11 9 11 21 5 12 11 10 14 4 | 20 22 21 27 32 21 22 27 24 25 22
23 | 11 10 12 12 10 6 10 14 13 15 4 | 32 32 31 33 29 30 34 30 26 26 28
24 | 10 10 14 10 18 5 10 13 9 9 4 | 24 25 26 27 26 24 29 25 23 27 24
25 | 10 13 15 9 15 6 9 11 10 12 4 | 25 24 27 27 29 25 26 24 22 24 23
X26 | 2 --- --- --- --- 43 --- --- --- --- 0 | 31 --- --- --- --- 24 --- --- --- --- 30
27 | 13 6 11 10 11 3 8 8 11 8 3 | 32 33 27 31 37 28 31 28 29 26 29
28 | 15 16 7 12 20 4 11 12 10 14 4 | 31 27 20 28 34 21 27 28 25 25 24
29 | 18 12 13 14 20 8 13 22 12 20 5 | 24 25 19 22 22 19 25 16 17 24 19
30 | 13 14 13 6 9 3 10 10 10 10 4 | 27 35 30 29 31 27 31 27 27 30 28
31 | 11 9 13 12 23 4 11 15 10 13 4 | 30 28 24 32 36 27 32 27 25 21 26
32 | 10 8 9 8 17 8 8 12 12 14 3 | 82 80 80 81 82 81 78 84 75 85 80
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 11 12 17 6 11 13 11 14 |T 38 39 36 39 38 35 39 37 36 37 36
WRMS | 13 12 11 11 17 6 11 12 10 15 |NE 38 39 35 38 38 35 39 37 36 37 35
MEDI | 11 11 11 11 17 5 10 12 10 14 |MD 30 30 26 29 32 25 30 27 26 26 26
Table 3.1835.4 GPS week: 1835 Day: 4 MJD: 57093.000
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 | 14 12 11 9 11 5 10 11 9 14 4 | 30 28 31 24 31 28 30 28 25 34 27
2 | 13 13 10 13 15 5 9 17 10 15 4 | 28 26 21 24 22 21 26 16 20 18 19
X3 | 22 17 9 13 --- 5 13 19 14 16 5 | 52 54 55 55 --- 54 58 60 48 61 54
4 | 11 11 13 10 23 6 10 14 10 16 4 | 25 28 24 21 27 23 27 26 25 33 24
5 | 11 16 7 9 17 5 15 17 10 13 4 | 30 30 20 33 38 28 30 31 29 29 27
6 | 12 10 12 8 11 5 10 10 6 13 3 | 37 33 37 32 31 35 33 29 33 36 32
7 | 11 12 14 8 15 6 8 13 9 14 4 | 29 29 20 27 31 23 27 25 24 22 23
X8 | 17 12 11 31 --- 6 13 16 15 --- 7 | 22 28 23 45 --- 23 27 17 23 --- 22
9 | 11 11 17 5 13 5 9 7 8 13 3 | 32 34 26 32 35 31 36 32 31 35 31
10 | 15 10 12 9 20 6 11 12 10 11 4 | 166 160 161 163 149 161 160 168 155 160 161
11 | 15 9 15 10 18 5 10 12 11 10 4 | 25 31 22 26 40 23 31 23 21 22 24
12 | 18 15 8 15 25 6 17 17 13 15 5 | 29 25 17 28 32 21 28 22 21 16 20
13 | 10 12 10 11 14 5 12 12 11 17 4 | 30 36 28 31 35 30 36 26 31 26 29
14 | 11 14 10 17 16 4 11 16 10 17 4 | 30 24 26 37 28 27 27 29 26 29 26
15 | 11 14 11 14 16 4 12 14 11 17 4 | 32 32 26 33 31 28 33 27 24 26 27
16 | 15 11 8 11 14 4 10 13 12 22 4 | 27 23 18 24 27 19 24 18 23 21 20
17 | 14 12 11 12 12 7 12 17 8 19 4 | 27 29 22 26 26 20 29 26 20 30 23
18 | 16 17 6 17 24 4 13 14 11 16 5 | 23 19 15 27 29 17 21 18 15 15 15
19 | 18 12 11 14 19 8 10 27 12 18 5 | 29 26 23 23 27 20 26 19 18 14 19
20 | 11 18 10 10 17 5 11 11 9 12 4 | 45 38 36 45 47 39 38 43 43 40 40
21 | 12 13 8 14 18 4 13 15 9 16 4 | 21 20 15 19 24 16 24 15 14 13 13
22 | 9 12 9 10 22 3 11 13 7 13 4 | 18 18 15 25 30 17 21 20 19 18 17
23 | 11 9 13 11 11 6 8 18 14 15 4 | 30 29 26 32 27 28 32 28 28 26 26
24 | 9 10 14 9 22 5 8 16 7 11 4 | 21 23 24 23 28 22 25 21 20 23 21
25 | 8 14 15 10 16 6 10 15 12 13 4 | 25 25 27 25 25 22 27 20 21 19 21
X26 | 41 16 16 --- --- 11 --- 23 28 --- 13 | 42 22 20 --- --- 18 --- 14 24 --- 16
27 | 10 8 10 8 11 4 7 9 8 8 3 | 26 31 26 27 37 24 30 25 22 23 26
28 | 13 9 9 6 16 6 8 13 9 11 3 | 23 23 18 21 29 18 23 23 22 20 19
X29 | 4 --- --- --- --- 33 --- --- --- --- 0 | 22 --- --- --- --- 18 --- --- --- --- 23
30 | 14 13 14 7 12 5 9 13 12 10 4 | 27 29 26 22 27 23 27 24 25 25 23
31 | 13 10 14 11 20 4 9 15 10 17 4 | 31 31 22 26 35 23 31 23 24 22 24
32 | 13 11 11 8 18 7 9 11 11 12 4 | 71 73 71 68 65 68 73 67 69 68 69
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 12 11 17 5 11 14 10 15 |T 34 34 30 34 36 30 35 31 30 31 30
WRMS | 13 12 11 11 17 5 11 14 9 14 |NE 34 33 30 34 35 29 35 30 30 31 29
MEDI | 12 12 11 10 16 5 10 14 10 14 |MD 29 29 24 27 30 23 28 25 24 25 23
Table 3.1835.5 GPS week: 1835 Day: 5 MJD: 57094.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 10 10 10 13 3 9 9 6 10 3 | 31 30 31 26 30 28 32 29 29 29 29
2 | 14 14 11 14 16 5 10 15 11 14 4 | 26 26 21 21 23 21 28 17 20 17 19
X3 | 16 16 10 12 --- 6 14 14 12 14 5 | 57 60 59 57 --- 58 67 63 55 62 59
4 | 12 8 11 8 26 5 7 13 12 16 4 | 27 26 25 22 31 24 28 27 25 34 25
5 | 7 13 9 9 16 4 13 17 9 11 4 | 27 29 19 29 35 24 30 29 26 24 25
6 | 13 13 12 8 12 4 7 11 7 11 3 | 36 35 32 28 29 30 33 26 27 30 29
7 | 8 12 11 9 15 5 9 9 8 14 3 | 27 28 19 26 30 22 27 22 23 20 22
X8 | 15 12 11 10 --- 8 7 12 15 --- 5 | 21 25 18 19 --- 19 22 16 20 --- 17
9 | 7 9 13 7 11 5 7 8 7 15 3 | 33 34 27 30 35 28 35 31 31 38 31
10 | 14 11 10 10 24 7 7 13 8 10 4 | 177 174 173 174 139 171 175 178 172 173 174
11 | 11 8 15 9 20 4 9 12 9 11 4 | 22 31 22 26 40 21 32 23 25 16 24
12 | 21 15 8 14 24 5 14 15 12 14 5 | 31 26 15 25 31 20 28 19 22 15 20
13 | 10 14 11 15 15 5 11 12 10 15 4 | 25 31 25 25 32 24 32 23 19 24 23
14 | 13 11 11 14 15 5 10 14 10 19 4 | 28 23 22 32 23 26 27 25 21 28 23
15 | 9 14 10 15 14 4 12 16 12 17 4 | 29 28 24 30 27 24 30 26 22 23 23
16 | 19 9 8 12 16 5 10 11 10 16 4 | 28 20 15 22 27 18 23 19 22 16 18
17 | 10 12 11 12 14 4 12 15 11 13 4 | 23 28 21 21 26 20 30 22 21 20 21
18 | 16 14 6 13 20 6 12 12 11 14 4 | 24 19 15 21 27 18 22 19 18 17 17
19 | 20 11 9 16 18 6 9 26 12 18 5 | 29 26 21 23 25 20 27 18 18 17 20
20 | 10 20 9 10 15 5 9 12 9 11 4 | 71 70 69 70 73 71 71 72 69 69 70
21 | 15 14 9 11 17 5 10 13 14 14 4 | 21 19 13 16 27 15 24 17 17 15 14
22 | 13 11 9 9 22 4 9 12 9 10 4 | 18 19 15 19 29 17 21 20 17 21 17
23 | 10 12 12 11 11 6 9 19 12 15 4 | 27 26 22 24 22 23 30 27 25 25 23
24 | 10 9 14 9 17 4 8 11 10 9 3 | 23 25 24 24 27 22 27 21 21 24 22
25 | 7 11 14 8 18 4 9 9 6 9 3 | 20 24 26 23 25 21 26 17 19 17 20
X26 | 21 14 19 --- --- 19 --- 18 17 --- 9 | 23 13 22 --- --- 22 --- 14 26 --- 15
27 | 11 8 13 11 13 4 6 9 7 8 3 | 25 30 24 27 35 23 27 23 26 21 24
28 | 16 13 9 11 18 4 8 11 9 12 4 | 25 23 14 23 30 18 24 21 21 17 19
29 | 18 12 11 15 18 8 13 21 12 18 5 | 23 20 15 10 12 15 20 8 10 7 11
30 | 11 13 12 8 15 4 9 8 8 8 3 | 24 30 27 25 27 25 28 23 25 24 24
31 | 11 12 13 14 19 4 11 14 12 13 4 | 27 29 20 27 34 22 29 21 22 18 22
32 | 11 8 9 7 20 4 8 12 8 14 3 | 61 61 62 62 65 62 63 66 62 66 62
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 11 11 17 5 10 14 10 13 |T 34 34 29 32 35 30 36 30 30 30 30
WRMS | 13 12 11 11 16 5 10 13 9 12 |NE 32 32 28 31 33 29 34 29 29 29 28
MEDI | 12 12 11 11 16 5 9 12 10 14 |MD 27 26 22 25 29 22 28 22 22 21 22
Table 3.1835.6 GPS week: 1835 Day: 6 MJD: 57095.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 11 12 9 17 4 9 11 8 10 3 | 35 29 34 28 36 32 33 31 32 34 30
2 | 11 12 9 14 18 6 12 17 10 17 4 | 27 25 20 24 26 21 26 17 20 16 19
X3 | 18 15 11 12 --- 5 11 14 10 13 5 | 66 68 70 68 --- 67 74 74 65 76 69
4 | 12 9 13 8 40 4 8 15 8 15 4 | 27 27 26 25 46 25 27 27 25 33 25
5 | 11 13 10 9 19 5 12 16 12 12 4 | 31 34 24 35 38 29 34 33 34 31 30
6 | 8 14 11 9 15 4 8 12 7 10 3 | 40 42 41 34 35 39 40 33 35 40 37
7 | 11 9 12 10 16 6 9 11 8 12 3 | 29 31 21 30 33 24 29 25 24 24 25
X8 | 14 11 14 9 --- 9 6 11 10 --- 4 | 21 27 20 19 --- 20 22 16 20 --- 18
9 | 9 8 12 8 17 5 8 9 10 13 3 | 43 42 37 43 45 40 42 43 40 47 41
10 | 13 12 11 9 40 6 8 14 8 11 4 | 170 175 169 171 155 170 170 177 166 172 172
11 | 11 11 17 8 19 9 8 14 10 10 4 | 33 39 27 33 51 28 37 31 33 26 32
12 | 16 17 9 13 23 6 13 17 14 13 5 | 27 28 18 28 38 22 29 25 26 24 23
13 | 11 13 10 11 16 5 13 13 12 18 4 | 40 41 38 40 42 36 42 34 39 34 37
14 | 9 9 13 14 21 4 9 14 11 17 4 | 35 32 31 43 40 36 33 34 36 37 33
15 | 10 13 12 15 16 3 13 19 11 19 5 | 38 35 31 38 36 33 37 33 30 32 32
16 | 16 11 7 14 17 4 10 12 10 17 4 | 27 24 18 27 31 21 24 17 24 16 20
17 | 10 14 11 13 14 7 12 17 10 15 4 | 29 30 24 30 35 24 32 30 26 26 26
18 | 17 15 8 17 25 5 12 13 11 16 5 | 26 22 15 27 35 19 21 20 20 17 18
19 | 13 10 11 12 23 7 11 28 11 17 5 | 24 29 24 25 36 22 28 21 21 19 22
20E | 12 12 9 11 21 10 11 16 10 12 4 | 104 96 98 106 102 99 96 100 104 104 100
21 | 23 12 9 15 23 5 12 15 11 18 5 | 31 21 17 20 31 18 22 18 19 16 16
22 | 12 10 9 13 25 4 9 12 10 10 4 | 19 18 16 23 36 19 20 21 21 21 18
23 | 12 10 10 12 15 4 10 21 11 16 4 | 35 35 33 39 36 34 37 37 28 35 33
24 | 10 9 15 8 22 4 10 13 11 12 4 | 22 27 26 23 32 23 26 23 22 25 22
25 | 11 15 16 8 22 4 10 11 13 13 4 | 23 30 28 25 36 24 29 22 21 23 24
X26 | 31 34 23 --- --- 12 --- 21 59 --- 19 | 34 25 25 --- --- 20 --- 9 34 --- 20
X27 | 9 6 14 8 18 6 7 9 --- 9 3 | 31 38 33 35 48 31 34 29 --- 28 33
28 | 10 13 8 10 18 5 10 11 11 13 4 | 20 26 16 24 34 19 26 23 24 18 21
29 | 18 11 12 13 21 7 11 23 13 20 5 | 24 20 17 11 18 15 19 10 8 10 14
30 | 14 9 12 7 13 5 9 10 5 12 3 | 23 30 26 23 30 23 29 25 22 25 24
31 | 7 10 14 10 26 3 10 12 11 12 4 | 24 31 22 28 40 25 30 23 26 20 24
32 | 11 10 11 8 35 5 8 13 8 14 4 | 48 50 47 49 66 48 47 50 45 50 48
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 11 11 22 6 10 15 10 14 |T 37 38 34 37 43 34 38 34 35 35 34
WRMS | 13 12 11 11 19 5 10 15 9 14 |NE 35 36 32 35 41 32 36 32 32 33 32
MEDI | 11 11 11 10 19 5 10 13 10 13 |MD 29 30 26 28 36 24 30 25 26 26 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 4.1835 GPS week: 1835 MJD: 57089.0-57095.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3006 |U 7 5 15 |U 10 11 34 |U 7 9 20 |
emr | emr 3002 | 6 5 14 |U 10 11 33 | 7 8 18 |
esa | esa 3003 | 6 5 13 |U 9 11 34 | 7 7 17 |
gfz | gfz 2962 |U 5 4 11 |U 10 11 33 |U 6 8 15 |
grg | grg 2770 | 7 6 14 |U 11 12 43 |U 8 8 23 |
igr | igr 2990 | 6 5 13 | 9 10 32 | 7 8 17 |
igs | igs 3001 | 5 4 12 | 9 11 32 | 6 8 15 |
jpl | jpl 2962 | 6 6 13 |U 10 10 31 |U 9 8 20 |
mit | mit 3003 | 6 7 15 |U 9 12 33 |U 7 9 17 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1835.0 GPS week: 1835 Day: 0 MJD: 57089.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 12 | 6 11 22 | 7 8 19 |
emr | emr 2976 | 5 4 12 | 8 10 20 | 6 6 16 |
esa | esa 2976 | 5 6 12 | 7 9 21 | 7 6 15 |
gfz | gfz 2976 | 5 5 10 | 7 9 21 | 5 6 12 |
grg | grg 2880 | 6 5 12 | 10 11 48 | 8 6 22 |
igr | igr 2976 | 5 5 11 | 7 8 19 | 5 6 12 |
igs | igs 2976 | 5 5 10 | 7 9 18 | 5 6 13 |
jpl | jpl 2975 | 5 6 14 | 7 9 19 | 8 6 17 |
mit | mit 2976 | 5 5 12 | 7 8 21 | 5 7 16 |
Table 5.1835.1 GPS week: 1835 Day: 1 MJD: 57090.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 8 19 | 7 6 29 | 10 14 30 |
emr | emr 2976 | 9 7 19 | 5 6 25 | 8 9 20 |
esa | esa 2976 | 7 7 17 | 6 5 27 | 8 8 17 |
gfz | gfz 2976 | 8 8 18 | 6 5 21 | 7 8 15 |
grg | grg 2688 | 11 8 25 | 7 6 29 | 9 11 29 |
igr | igr 2976 | 8 7 16 | 5 5 22 | 10 12 27 |
igs | igs 2976 | 8 7 17 | 6 5 22 | 7 8 16 |
jpl | jpl 2976 | 7 9 15 | 7 7 21 | 9 8 18 |
mit | mit 2976 | 10 14 28 | 7 9 25 | 9 11 27 |
Table 5.1835.2 GPS week: 1835 Day: 2 MJD: 57091.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 4 19 | 11 9 36 | 6 8 22 |
emr | emr 2976 | 7 4 16 | 11 8 33 | 7 9 19 |
esa | esa 2976 | 7 4 16 | 11 9 35 | 7 7 18 |
gfz | gfz 2976 | 6 2 14 | 11 10 35 | 6 7 16 |
grg | grg 2782 | 6 4 15 | 12 10 44 | 7 7 20 |
igr | igr 2976 | 6 2 15 | 11 9 34 | 6 7 17 |
igs | igs 2976 | 6 3 15 | 11 8 33 | 6 8 17 |
jpl | jpl 2976 | 7 5 16 | 11 8 33 | 9 8 21 |
mit | mit 2976 | 5 4 15 | 11 11 32 | 6 9 17 |
Table 5.1835.3 GPS week: 1835 Day: 3 MJD: 57092.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 5 4 14 | 12 17 37 | 6 8 18 |
emr | emr 2976 | 4 5 12 | 12 18 42 | 6 8 16 |
esa | esa 2976 | 4 4 12 | 11 17 36 | 6 7 16 |
gfz | gfz 2976 | 4 4 11 | 12 17 41 | 6 8 14 |
grg | grg 2784 | 5 5 14 | 11 17 51 | 7 7 22 |
igr | igr 2976 | 4 4 12 | 11 17 37 | 6 7 14 |
igs | igs 2976 | 3 4 11 | 12 17 39 | 6 8 15 |
jpl | jpl 2976 | 4 6 12 | 11 15 36 | 9 8 19 |
mit | mit 2976 | 5 5 16 | 11 18 40 | 6 8 12 |
Table 5.1835.4 GPS week: 1835 Day: 4 MJD: 57093.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2960 | 7 6 15 | 12 12 36 | 8 8 17 |
emr | emr 2975 | 6 4 11 | 14 13 36 | 9 8 16 |
esa | esa 2976 | 6 5 11 | 12 12 36 | 8 7 15 |
gfz | gfz 2880 | 5 3 7 | 12 12 35 | 7 8 13 |
grg | grg 2688 | 7 7 12 | 14 14 42 | 9 8 22 |
igr | igr 2956 | 6 4 11 | 11 11 34 | 7 7 16 |
igs | igs 2976 | 5 4 10 | 12 12 34 | 8 8 13 |
jpl | jpl 2879 | 7 7 12 | 12 11 32 | 11 7 20 |
mit | mit 2976 | 5 6 11 | 12 14 34 | 7 8 14 |
Table 5.1835.5 GPS week: 1835 Day: 5 MJD: 57094.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 7 4 12 | 10 14 38 | 6 7 23 |
emr | emr 3069 | 8 7 17 | 11 14 44 | 7 8 25 |
esa | esa 3072 | 7 5 13 | 9 13 43 | 7 7 23 |
gfz | gfz 2976 | 6 4 10 | 12 16 44 | 6 9 23 |
grg | grg 2784 | 5 4 12 | 11 13 45 | 7 9 25 |
igr | igr 3058 | 7 5 14 | 9 13 43 | 6 7 21 |
igs | igs 3055 | 6 4 12 | 9 14 42 | 6 8 21 |
jpl | jpl 2976 | 8 7 14 | 10 13 41 | 10 7 29 |
mit | mit 3072 | 6 8 12 | 8 12 45 | 7 10 20 |
Table 5.1835.6 GPS week: 1835 Day: 6 MJD: 57095.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3050 | 6 5 14 | 11 10 41 | 7 8 14 |
emr | emr 3072 | 5 5 14 | 7 8 34 | 8 9 15 |
esa | esa 3072 | 5 5 11 | 9 9 38 | 7 8 14 |
gfz | gfz 2976 | 5 5 9 | 9 9 36 | 7 10 16 |
grg | grg 2784 | 6 6 11 | 10 12 41 | 8 9 22 |
igr | igr 3018 | 5 5 11 | 9 8 37 | 7 9 15 |
igs | igs 3072 | 4 4 10 | 9 8 35 | 7 9 13 |
jpl | jpl 2976 | 5 5 11 | 10 9 38 | 10 7 18 |
mit | mit 3072 | 5 5 15 | 9 10 34 | 8 11 14 |
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 6.1835 GPS week: 1835 MJD: 57089.500-57095.500
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 | -8 9 19 238 0 | 22 26
| 22 17 106 105 6 | 3
emr uuuuu | 22 -23 88 117 -10 | 24 27
| 17 23 114 40 7 | 7
esa uuuuu | 25 13 58 213 6 | 30 33
| 14 12 66 57 4 | 2
gfz uuuuu | -2 -37 151 -111 4 | 16 21
| 8 13 94 138 4 | 1
grg uuuuu | 0 32 -285 -17 8 | 31 36
| 23 15 98 49 14 | 1
igr xxxxx | 18 9 90 35 2 | 1 13
| 13 15 59 14 4 | 1
irf xxxxx | 5 -14 -24 -93 6 | -4 14
| 8 12 25 27 5 | 2
jpl uuuuu | -11 -6 107 63 5 | 31 33
| 31 13 80 36 7 | 2
mit uuuuu | -1 1 -110 -211 2 | 19 23
| 19 13 80 55 4 | 2
ngs uuuuu | -19 3 -87 -125 -4 | 11 16
| 39 20 149 199 2 | 2
sio uuuux | -1 33 -104 -192 9 | 44 46
| 18 26 63 57 8 | 2
Table 7.1835.0 GPS week: 1835 Day: 0 MJD: 57089.500
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 21 11 301 3 | 27 32
emr uuuuu | 34 -51 215 190 -7 | 33 39
esa uuuuu | 13 23 -15 153 11 | 31 36
gfz uuuuu | -1 -17 9 -126 5 | 17 25
grg uuuuu | -7 8 -170 -82 -14 | 32 38
igr xxxxx | 30 35 14 21 5 | 3 17
irf xxxxx | 11 4 -17 -121 3 | -2 20
jpl uuuuu | -17 -9 -45 53 3 | 34 37
mit uuuuu | -22 -5 -35 -226 2 | 23 29
ngs uuuuu | -6 7 11 1 -4 | 14 20
sio uuuux | -19 46 -98 -272 -3 | 47 51
Table 7.1835.1 GPS week: 1835 Day: 1 MJD: 57090.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 4 16 15 287 -11 | 26 31
emr uuuuu | -3 -56 126 77 -11 | 30 36
esa uuuuu | 0 18 87 145 2 | 31 35
gfz uuuuu | -1 -28 211 -51 -1 | 16 23
grg uuuuu | -20 22 -361 -19 34 | 29 34
igr xxxxx | 5 5 138 35 5 | 2 16
irf xxxxx | 0 -1 -8 -47 3 | -4 17
jpl uuuuu | -34 -10 185 -13 -2 | 33 36
mit uuuuu | -7 22 -77 -117 -2 | 20 26
ngs uuuuu | 42 2 -133 -161 -1 | 13 19
sio uuuux | 3 26 -176 -107 4 | 45 48
Table 7.1835.2 GPS week: 1835 Day: 2 MJD: 57091.500
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 -5 -86 58 -2 | 21 23
emr uuuuu | 25 -2 104 135 -18 | 25 28
esa uuuuu | 31 5 -46 226 9 | 28 31
gfz uuuuu | 13 -34 92 -7 11 | 13 19
grg uuuuu | -24 35 -329 -41 6 | 29 34
igr xxxxx | 30 10 138 39 2 | 0 12
irf xxxxx | -2 -25 -3 -70 12 | -7 14
jpl uuuuu | 24 9 123 63 -6 | 30 31
mit uuuuu | -21 -5 -24 -166 5 | 17 20
ngs uuuuu | -41 -21 61 -152 -6 | 10 15
sio uuuux | 23 50 -80 -148 9 | 42 43
Table 7.1835.3 GPS week: 1835 Day: 3 MJD: 57092.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -16 -10 14 365 4 | 20 23
emr uuuuu | 46 -8 -58 132 -11 | 23 27
esa uuuuu | 38 17 92 280 5 | 29 32
gfz uuuuu | 3 -36 177 69 2 | 15 20
grg uuuuu | 24 41 -296 74 4 | 30 35
igr xxxxx | 28 -11 94 17 1 | 0 12
irf xxxxx | 10 -26 6 -86 8 | -5 12
jpl uuuuu | -43 -5 63 95 10 | 29 31
mit uuuuu | 27 3 -68 -236 4 | 18 21
ngs uuuuu | -63 -20 26 -500 -6 | 10 15
sio uuuux | 11 56 -134 -229 5 | 42 44
Table 7.1835.4 GPS week: 1835 Day: 4 MJD: 57093.500
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 2 220 289 2 | 21 24
emr uuuuu | 19 -20 -43 104 -19 | 22 25
esa uuuuu | 23 19 147 281 5 | 31 33
gfz uuuuu | -9 -39 73 -78 6 | 16 20
grg uuuuu | 27 54 -431 -47 10 | 31 36
igr xxxxx | 17 -5 19 31 8 | 1 12
irf xxxxx | 14 -20 -44 -118 8 | -4 13
jpl uuuuu | -39 -29 95 78 6 | 30 33
mit uuuuu | 6 1 -148 -280 4 | 19 22
ngs uuuuu | 7 -1 -2 -196 -3 | 10 15
sio uuuux | 12 55 -176 -210 17 | 43 45
Table 7.1835.5 GPS week: 1835 Day: 5 MJD: 57094.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 3 0 57 216 6 | 20 22
emr uuuuu | 33 -1 43 75 -7 | 17 19
esa uuuuu | 35 21 71 232 8 | 29 32
gfz uuuuu | -6 -60 273 -298 5 | 15 19
grg uuuuu | 20 27 -172 2 5 | 30 35
igr xxxxx | 20 11 162 59 -3 | 0 12
irf xxxxx | 11 -10 -37 -99 9 | -4 13
jpl uuuuu | 33 8 143 77 7 | 30 32
mit uuuuu | -5 -21 -188 -203 5 | 18 21
ngs uuuuu | -64 25 -281 46 -6 | 8 13
sio uuuux | -28 1 -7 -219 18 | 43 45
Table 7.1835.6 GPS week: 1835 Day: 6 MJD: 57095.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -21 38 -102 149 1 | 22 24
emr uuuuu | 4 -24 228 107 1 | 15 18
esa uuuuu | 37 -10 71 172 0 | 33 34
gfz uuuuu | -13 -44 218 -286 2 | 18 20
grg uuuuu | -20 35 -240 -9 9 | 32 36
igr xxxxx | -5 15 67 41 -1 | 2 10
irf xxxxx | -7 -18 -64 -112 -2 | 0 9
jpl uuuuu | 0 -8 181 84 15 | 32 34
mit uuuuu | 18 9 -233 -250 -7 | 21 22
ngs uuuuu | -9 32 -290 86 -3 | 9 13
sio uuuux | -8 -5 -57 -157 16 | 47 48
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