[IGSREPORT-23992] Wk 1866 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Oct 30 12:42:30 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1866 (Oct 11, 2015 - Oct 17, 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:
igs1866[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1866[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1866[0-6].cls IGS GPS clock combination summary report.
igs18667.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18667.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 | REUN REUN
0 | EMR | 32 32
0 | ESA | 10 22 29 32 10 ASPA HOB2
0 | GFZ | HOB2 NOVM SEY1 UFPR
0 | GRG | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
0 | GRG | 21 22 23 24 25 26 27 28 29 30 31 32 1 2 3 4 5 6 7
0 | GRG | 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24
0 | GRG | 25 26 27 28 29 30 31 32
0 | JPL | 32
0 | MIT | BRST BRST HOB2
1 | EMR | 32 32
1 | ESA | 10 10 HOB2 HOB2
1 | GRG | 8 9 32 8 32 DARW DAV1 DRAG HOLB KARR MCM4 PIMO TONG
1 | GRG | YELL DAV1 DRAG
1 | JPL | 32 SCOR UFPR
2 | COD | MATE
2 | EMR | 32 32
2 | ESA | 10 10 DUBO
2 | GFZ | MAL2 TONG MAL2 TONG
2 | GRG | 6 10 31 32 10 31 32 FAIR NRMD REUN FAIR NRMD REUN
2 | JPL | 32 FAIR TUVA
3 | COD | KOUC REUN XMIS HOB2 KOUC MAC1 REUN XMIS
3 | EMR | 32 32
3 | ESA | 10 10 DRAG
3 | GFZ | 13 21 13 21 DRAG MAC1 SUTH TONG HOB2 SUTH TONG
3 | GRG | 13 32 13 32 DRAG MAC1
3 | JPL | 32
3 | MIT | SUTH NYAL SUTH
4 | COD | KOUC NYA1 GLSV HOB2 KOUC NYA1
4 | ESA | 10 10 TIXI
4 | GFZ | STHL NOVM STHL TONG
4 | GRG | 23 32 23 32 MAC1 MCM4 NRIL NRMD KIRU MAC1 MCM4 NRIL
4 | GRG | NRMD
5 | COD | 10 KOUC KOUC
5 | ESA | 10 10 KIRU KIRU
5 | GFZ | 13 13 NOVM TONG
5 | GRG | DRAG NRMD DRAG
5 | JPL | KIRU TUVA
5 | MIT | ABPO ABPO
6 | COD | KOUC SOFI FLRS KOUC NYA1 SOFI
6 | GFZ | 13 HOB2 NOVM NRMD
6 | GRG | 13 20 13 20
6 | JPL | HOB2 NRMD
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. 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.
7. 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 -2.2 -1.5 -46 11 27 .35
EMR | 0 | -3.6 1.7 1.8 42 4 18 .32
ESA | 0 | -.9 -.2 -1.5 63 -41 68 .05
GFZ | 0 | .1 -1.2 -2.0 -37 -84 8 .32
GRG | 0 | 5.8 -1.0 -4.2 -51 -6 21 .23
JPL | 0 | -3.8 -7.6 -4.4 -12 15 16 .50
MIT | 0 | 3.0 2.5 6.0 28 -15 -19 .24
NGS | 0 | -2.7 2.0 9.0 -29 -11 -35 .35
SIO | 0 | 6.1 6.3 3.8 -4 -31 7 .14
COD | 1 | -1.5 -1.8 -2.7 -35 0 13 .52
EMR | 1 | -.5 10.6 4.0 13 3 9 .32
ESA | 1 | -.8 -.4 -1.1 58 -53 58 .13
GFZ | 1 | -.2 -1.0 -2.2 -42 -102 -8 .34
GRG | 1 | -3.4 2.0 -6.9 -57 -19 3 .33
JPL | 1 | -.7 1.0 -2.8 4 24 24 .49
MIT | 1 | -1.1 1.1 5.1 45 -12 -15 .50
NGS | 1 | -4.3 .1 13.1 -68 -17 -42 .32
SIO | 1 | .3 5.4 .4 7 -22 -21 .44
COD | 2 | -1.3 -2.3 -2.6 -45 23 -4 .45
EMR | 2 | 1.2 4.4 2.5 16 24 -15 .34
ESA | 2 | -.1 -.2 -.6 76 -57 80 .06
GFZ | 2 | 1.1 -1.1 -1.9 -25 -123 -7 .40
GRG | 2 | 1.7 2.7 -9.7 -45 -1 37 .52
JPL | 2 | -.9 -6.6 -3.7 15 -3 43 .52
MIT | 2 | -.3 .5 6.1 43 -17 -23 .35
NGS | 2 | -6.4 .4 11.1 -57 -8 -71 .29
SIO | 2 | 1.1 5.2 4.4 -19 -30 -1 .25
COD | 3 | -1.3 -1.7 -2.6 -41 43 8 .55
EMR | 3 | -4.7 2.8 14.8 27 13 11 .52
ESA | 3 | -.5 -.2 -.2 63 -60 78 .23
GFZ | 3 | .2 -1.4 -2.0 -48 -105 -1 .45
GRG | 3 | 2.5 -1.1 -15.4 -61 -30 1 .78
JPL | 3 | .8 -11.4 1.2 1 29 29 .75
MIT | 3 | -2.9 .6 8.2 37 -16 -20 .57
NGS | 3 | -6.3 -3.2 15.4 -92 -11 -75 .47
SIO | 3 | 1.4 3.0 9.0 -24 -24 -14 .27
COD | 4 | -1.0 -2.2 -2.5 -31 10 33 .68
EMR | 4 | -2.8 -1.7 11.4 44 0 31 .47
ESA | 4 | -.9 .1 .3 54 -65 77 .28
GFZ | 4 | .3 -.8 -1.5 -39 -82 3 .53
GRG | 4 | -.9 -1.3 -10.3 -83 -21 -26 .38
JPL | 4 | -1.8 -12.9 10.6 2 -16 10 .63
MIT | 4 | -1.3 1.5 12.5 36 -4 -24 .57
NGS | 4 | -1.1 4.1 16.9 -79 -43 -5 .38
SIO | 4 | 3.4 2.6 20.0 -23 -33 13 .32
COD | 5 | -.7 -1.8 -2.5 -42 -4 10 .66
EMR | 5 | 1.9 -4.5 14.9 29 -2 38 .63
ESA | 5 | -.3 -1.2 .9 33 -77 62 .51
GFZ | 5 | .0 -1.8 -2.1 -52 -97 -2 .57
GRG | 5 | 5.6 -3.2 -10.5 -68 -4 -4 .26
JPL | 5 | 1.8 -8.9 3.5 -29 8 52 .33
MIT | 5 | 1.8 -2.5 9.7 55 -19 25 .88
NGS | 5 | 1.4 -5.2 11.9 -87 -49 -7 .65
SIO | 5 | 2.4 .8 15.8 1 -10 12 .42
COD | 6 | -.5 -1.9 -1.9 -39 17 10 .60
EMR | 6 | -.8 -.7 16.4 29 -1 44 .69
ESA | 6 | -.4 -1.1 -.7 47 -70 45 .56
GFZ | 6 | .4 -2.4 -1.8 -44 -98 -24 .56
GRG | 6 | -.6 2.8 -7.2 -62 0 33 .42
JPL | 6 | .6 -8.6 6.6 -10 24 49 .35
MIT | 6 | -2.0 -1.9 6.5 -17 -4 -71 .57
NGS | 6 | .1 -6.4 13.5 -94 -39 -34 .68
SIO | 6 | 1.9 1.0 14.7 -24 -35 7 .24
8. 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.
9. 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 1.1866.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1866.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 2.1866.[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 3.1866.[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 5.1866.0-6). 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 1866 summary. (Oct 11, 2015 - Oct 17, 2015)
Table 1.1866.a GPS week: 1866 MJD: 57306.000-57312.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 245| 2 0 1 8 21 11 -.04 11 10 | -544 231 15 126
| 1 0 1 20 5 10 .03 | 1136 834
emr 80| 0 -1 1 -9 -24 0 .28 11 11 | 6846 -290 11 107
| 0 2 2 8 20 6 .02 | 780 480
esa 150| 0 0 0 -16 7 -1 -.37 11 11 | -738 682 7 135
| 0 0 0 15 13 12 .02 | 983 1565
gfz 193| 0 0 -3 25 -12 -5 -.03 11 11 | 74 -124 11 93
| 0 0 1 9 21 12 .03 | 527 725
grg 117| 2 0 -7 -25 32 58 -.09 19 19 | 48986 -123947 142877 143024
| 3 0 2 8 11 95 .08 | 129123 327918
igr n/a| 0 0 -3 0 0 -13 -.05 4 4 | 4535 -831 13 61
| 0 0 1 14 10 12 .02 | 1527 319
jpl 80| -1 0 0 9 12 20 .26 10 10 | 6861 -280 14 103
| 1 1 2 22 13 12 .02 | 772 472
mit 348| 1 -1 0 -9 -1 -19 -.18 11 10 | 725 -272 42 400
| 0 0 1 35 20 13 .01 | 2671 593
ngs 209| -1 1 2 6 -5 -5 -.01 8 7 | 603340 201337 1224 2709
| 0 0 1 29 15 18 .03 | 1019105 469911
sio 310| 0 -1 0 -17 -13 -27 .01 14 13 | --- --- --- ---
| 0 1 1 26 9 29 .02 | --- ---
Table 1.1866.b GPS week : 1866 MJD: 57306.000-57312.000
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 3 3 3 3 3 |
2 | 5 4 4 5 5 5 5 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 3 4 4 4 4 |
5 | 4 4 4 4 4 4 4 |
6 | 4 4 3 4 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 3 4 4 4 4 4 |
9 | 3 4 3 4 4 4 3 |
10 | 7 7 9 6 7 9 7 |
11 | 4 4 4 4 4 4 4 |
12 | 4 5 5 5 5 5 6 |
13 | 4 4 4 5 4 4 5 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 4 4 5 4 |
16 | 4 5 5 4 5 5 5 |
17 | 5 5 4 5 5 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 5 5 5 5 5 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 3 3 3 3 4 4 3 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 3 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 3 4 4 3 4 4 3 |
28 | 4 4 4 4 4 4 3 |
29 | 5 5 5 5 5 5 5 |
30 | 3 3 3 3 3 3 3 |
31 | 5 5 5 5 5 4 4 |
32 | 4 5 4 5 5 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1866.0 GPS week: 1866 Day: 0 MJD: 57306.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 246| 1 0 3 -7 10 30 .01 10 10 | -615 -652 12 104
emr 80| 0 -2 -2 3 -30 2 .25 11 11 | 8287 -920 11 97
esa 150| 0 0 0 -18 3 7 -.40 11 11 | 687 -1536 7 156
gfz 195| 0 -1 0 5 -1 20 -.05 10 10 | 654 -1460 9 116
grg 116| -1 1 -5 -14 46 1 .01 18 18 | 0 0 999999 999999
igr n/a| 0 0 -1 -6 -8 1 -.06 4 4 | 6730 -1134 13 52
jpl 80| 0 1 -2 9 12 2 .25 11 11 | 8295 -908 14 88
mit 349| 1 0 0 -16 16 -4 -.18 11 9 | 6762 -1477 56 469
ngs 214| -1 1 2 15 -13 -30 .00 7 7 | 1246014 249132 1272 2417
sio 308| 1 -2 0 -3 -10 -31 .01 15 15 | --- --- --- ---
Table 2.1866.1 GPS week: 1866 Day: 1 MJD: 57307.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 244| 3 0 3 16 26 8 -.09 11 10 | -1095 71 17 124
emr 80| -1 2 0 -13 1 6 .25 11 11 | 7450 -825 9 75
esa 150| 0 0 0 -9 10 -22 -.36 12 12 | -1975 2115 8 133
gfz 194| -1 -1 -4 19 -27 -10 .01 10 10 | -790 720 11 101
grg 118| -1 0 -7 -14 38 267 .02 32 32 | 254 -82 26 182
igr n/a| 0 0 -3 6 -7 -28 -.03 4 4 | 5765 -811 14 71
jpl 80| 0 2 -2 25 8 17 .24 10 10 | 7462 -788 14 115
mit 348| 0 -2 -1 -15 -8 -17 -.19 11 10 | -372 -319 42 424
ngs 200| 0 0 5 -17 -1 -4 .02 8 7 | -305642 814219 1442 3350
sio 310| 1 -2 -3 -17 -3 -31 .03 15 14 | --- --- --- ---
Table 2.1866.2 GPS week: 1866 Day: 2 MJD: 57308.000
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| 3 1 1 6 24 12 -.05 10 10 | -988 -160 16 121
emr 80| 0 -1 1 -10 -1 -6 .28 10 10 | 6919 -405 11 104
esa 150| 0 0 0 -1 13 6 -.36 11 11 | -474 373 7 129
gfz 193| -1 -1 -2 25 -27 -5 .02 11 11 | 27 -162 11 80
grg 117| 2 0 -7 -21 14 43 -.18 16 15 | 341811 -867597 25 212
igr n/a| 0 0 -2 15 -3 -24 -.06 4 4 | 5338 -820 14 64
jpl 80| -1 0 -2 10 21 43 .25 9 9 | 6917 -423 15 103
mit 349| 0 -1 1 17 -22 -43 -.19 12 11 | -678 53 40 396
ngs 200| 0 1 3 -7 -6 -17 .01 8 7 | -412666 558935 1206 2666
sio 312| 0 -1 0 -35 -21 -20 .03 14 13 | --- --- --- ---
Table 2.1866.3 GPS week: 1866 Day: 3 MJD: 57309.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 247| 1 0 1 40 22 13 -.02 12 11 | 1998 1993 19 132
emr 80| 0 0 2 -16 -45 0 .31 11 11 | 6093 438 11 125
esa 150| 0 0 0 4 13 -4 -.38 11 11 | -1543 1645 7 145
gfz 193| 0 0 -3 25 -39 -17 -.03 12 12 | -175 -60 15 130
grg 118| 5 0 -7 -28 27 19 -.11 17 16 | 97 102 21 185
igr n/a| 0 0 -3 -2 -7 -17 -.07 4 4 | 4467 -288 14 68
jpl 80| 0 -2 0 20 30 10 .26 10 10 | 6133 431 14 104
mit 348| 0 -1 0 -35 -5 -6 -.19 12 11 | -295 -92 40 408
ngs 212| -1 1 2 19 9 19 -.01 9 8 | 1913 2100 1399 2818
sio 311| 0 -1 -1 -64 -3 -57 -.00 13 13 | --- --- --- ---
Table 2.1866.4 GPS week: 1866 Day: 4 MJD: 57310.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 246| 1 1 0 2 25 11 -.03 11 11 | -869 -99 17 128
emr 80| 0 -2 1 -5 -13 -2 .30 11 11 | 6297 -297 12 116
esa 150| 0 0 1 -22 30 16 -.39 11 11 | -712 689 7 135
gfz 194| 0 0 -4 32 26 -3 -.05 11 11 | -48 4 11 78
grg 116| 4 0 -5 -31 24 14 -.16 17 16 | 347 -255 23 200
igr n/a| 0 0 -4 -27 20 -10 -.03 4 4 | 3905 -1287 14 60
jpl 80| -3 0 0 6 13 24 .23 10 10 | 6316 -279 15 107
mit 348| 1 0 1 41 -20 -16 -.17 11 10 | 12 -130 36 381
ngs 215| -1 1 3 -41 -36 -15 .01 9 8 | -1017 93 1140 2281
sio 312| 0 -1 0 6 -29 -8 .03 14 14 | --- --- --- ---
Table 2.1866.5 GPS week: 1866 Day: 5 MJD: 57311.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 244| 0 0 -1 21 25 7 -.05 10 10 | -1100 166 15 148
emr 80| -1 -3 3 -21 -49 -9 .30 10 10 | 6478 -57 12 118
esa 150| 0 0 1 -31 -11 -2 -.35 11 11 | -1432 2576 7 121
gfz 193| -1 0 -3 31 -8 -5 -.07 12 12 | 65 583 10 78
grg 119| 6 0 -12 -30 38 0 -.09 18 17 | 110 380 26 193
igr n/a| 0 0 -3 10 1 -20 -.05 4 4 | 3210 -729 13 58
jpl 80| -1 0 1 -36 17 19 .30 10 10 | 6506 -50 14 96
mit 349| 1 -1 1 6 -5 -22 -.16 12 10 | -328 427 42 389
ngs 215| -1 0 3 38 7 -2 -.07 9 8 | 2109708 -631050 1191 2455
sio 309| 0 0 0 -17 -16 23 .01 13 12 | --- --- --- ---
Table 2.1866.6 GPS week: 1866 Day: 6 MJD: 57312.000
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 242| 2 1 0 -21 18 -3 -.02 11 11 | -1145 302 15 131
emr 80| 0 -1 4 -5 -35 7 .30 11 11 | 6398 35 14 116
esa 150| 0 1 2 -38 -3 -8 -.37 12 12 | 283 -1086 8 128
gfz 194| -1 0 -5 35 -9 -12 -.01 11 11 | 785 -498 10 70
grg 120| 3 0 -7 -34 40 60 -.09 18 17 | 288 -177 23 200
igr n/a| 0 1 -5 4 3 5 -.05 4 4 | 2330 -753 15 54
jpl 80| 0 0 2 34 -12 25 .26 10 10 | 6403 53 15 114
mit 348| 1 0 1 -64 35 -29 -.17 12 11 | -23 -367 38 336
ngs 213| -1 1 0 34 -1 15 -.05 8 8 | 1585076 415934 918 2978
sio 310| 0 0 -1 12 -9 -64 -.03 12 12 | --- --- --- ---
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 3.1866.0 GPS week: 1866 Day: 0 MJD: 57306.000
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 11 6 13 3 7 12 4 20 3 | 34 42 33 37 39 36 40 34 37 47 36
2 | 14 10 13 11 20 5 10 12 9 20 4 | 30 37 29 35 39 32 33 32 33 31 31
3E | 14 15 11 8 21 2 10 9 6 13 4 | 64 71 70 68 66 68 69 65 64 72 67
4 | 9 7 10 7 16 3 7 9 6 18 3 | 35 35 34 34 35 33 35 35 33 38 33
5E | 15 12 7 12 17 3 14 8 8 13 4 | 102 108 103 108 105 104 108 103 103 108 105
6 | 11 8 12 8 19 5 9 9 6 11 3 | 39 44 35 40 46 39 41 38 37 42 38
7 | 9 12 11 10 17 2 13 12 9 14 4 | 35 39 28 32 35 31 34 28 33 35 31
8 | 6 9 12 10 14 3 8 6 6 13 3 | 29 36 32 26 26 29 34 28 29 37 29
9 | 8 8 12 8 19 4 8 7 7 10 3 | 36 38 40 35 34 34 41 34 37 38 36
X10 | 21 16 18 18 15 9 13 11 20 --- 6 | 30 27 27 32 24 26 21 26 32 --- 24
11 | 9 9 14 10 16 2 8 7 6 19 3 | 35 42 35 41 47 38 42 38 37 38 37
12E | 11 15 7 10 18 4 13 16 7 15 4 | 29 31 26 32 27 26 30 26 29 29 27
13 | 11 9 14 8 24 3 12 12 9 11 4 | 26 34 25 29 39 25 33 28 29 27 27
14 | 8 13 11 11 18 4 10 12 8 17 4 | 29 29 24 27 33 24 29 27 27 24 25
15 | 12 10 10 12 21 4 12 9 10 19 4 | 28 27 22 26 27 23 28 22 24 24 23
16E | 7 13 8 12 21 3 13 11 6 15 4 | 40 40 38 37 49 38 39 40 39 39 38
17 | 14 11 14 11 18 3 11 13 9 18 4 | 34 37 28 36 38 32 35 35 35 37 33
18 | 18 11 5 12 24 5 9 8 7 15 4 | 35 32 25 33 34 29 33 28 31 26 29
19 | 10 12 14 14 16 3 14 15 8 20 4 | 28 33 27 34 33 27 31 31 25 28 27
20 | 15 9 7 9 18 3 9 10 6 11 3 | 31 28 25 26 32 26 29 27 28 26 26
21 | 7 9 12 9 15 3 10 8 9 17 3 | 32 38 32 34 42 32 36 33 32 38 33
22 | 7 10 6 10 16 3 9 7 8 12 3 | 26 27 22 25 28 24 28 23 24 25 24
23 | 10 14 9 13 20 3 15 15 9 17 4 | 26 32 24 18 23 23 31 21 22 24 22
24 | 10 7 15 7 16 5 7 11 8 12 3 | 24 29 26 25 30 23 30 29 26 27 25
25E | 8 9 13 6 18 5 9 9 7 13 3 | 43 46 47 41 45 41 41 42 40 37 42
26E | 9 9 15 8 14 3 11 14 6 12 3 | 24 21 29 21 27 21 23 24 21 21 21
27 | 10 7 13 7 15 2 8 4 5 13 3 | 28 30 28 25 27 26 28 25 27 30 26
28E | 10 13 8 8 15 3 10 12 5 11 3 | 30 34 28 27 32 27 28 28 26 29 27
29 | 10 12 12 11 15 6 12 14 10 18 4 | 39 42 38 36 34 35 38 35 35 35 35
30 | 8 6 12 8 17 3 10 7 6 13 3 | 27 30 26 25 29 24 27 27 27 31 26
31 | 7 16 13 9 17 4 12 15 8 18 4 | 27 35 25 25 30 23 32 27 27 27 25
32E | 9 15 12 11 19 5 13 9 6 16 4 | 41 46 41 39 35 40 42 42 40 45 40
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 11 10 18 4 11 11 7 15 |T 34 38 33 34 37 33 36 33 34 35 33
WRMS | 10 11 11 10 18 4 11 9 7 15 |NE 30 33 28 29 32 28 32 29 29 31 28
MEDI | 10 10 12 10 17 3 10 10 7 15 |MD 30 35 28 32 34 29 33 28 31 31 29
Table 3.1866.1 GPS week: 1866 Day: 1 MJD: 57307.000
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 | 9 6 14 9 33 4 6 11 6 14 3 | 33 37 29 35 43 33 37 29 31 41 33
2M | 12 8 12 11 35 4 9 11 9 18 4 | 29 37 30 35 39 31 33 31 32 31 31
3 | 9 9 12 7 34 4 11 11 8 14 3 | 58 61 60 58 68 58 60 59 57 60 58
4 | 11 10 10 9 32 3 6 9 7 15 3 | 34 33 32 31 40 30 32 32 30 32 31
5 | 11 13 8 9 35 4 12 11 7 10 4 | 46 49 42 47 61 47 50 46 46 47 46
6 | 8 7 13 6 33 4 8 10 7 11 3 | 30 42 30 33 44 34 38 31 34 35 33
7 | 11 11 12 11 32 3 12 12 9 12 4 | 35 38 28 32 42 29 36 28 31 31 31
8 | 5 9 14 9 27 4 7 8 5 13 3 | 32 37 33 30 35 31 37 30 33 39 32
9M | 8 7 13 9 30 3 9 9 6 8 3 | 39 43 42 37 41 40 44 35 37 43 39
X10 | 17 17 17 29 28 7 9 13 13 --- 6 | 28 32 25 39 37 29 29 29 30 --- 26
11 | 10 10 15 11 30 4 8 7 8 16 4 | 30 39 29 33 44 32 40 32 28 36 32
12E | 14 12 6 14 35 4 14 15 9 16 4 | 26 27 27 35 40 28 29 27 29 30 27
13 | 9 11 12 11 38 4 12 9 7 10 4 | 24 35 24 28 42 26 34 26 29 27 27
14 | 7 9 11 11 30 4 10 13 8 18 4 | 30 34 28 33 39 29 33 33 30 31 30
15 | 12 9 10 12 33 4 11 9 7 20 4 | 31 32 26 30 31 28 32 28 30 32 28
16E | 17 17 7 13 29 4 13 16 8 16 5 | 58 55 52 56 69 54 55 61 58 64 56
17 | 14 12 12 12 33 4 11 14 10 18 4 | 27 35 27 33 36 28 33 27 28 34 28
18 | 14 10 6 9 31 4 9 9 7 15 3 | 37 37 32 36 39 31 36 32 35 31 33
19 | 10 11 14 16 30 4 12 16 11 19 5 | 26 32 25 30 31 25 32 27 21 25 24
20 | 17 9 8 9 33 4 8 11 7 14 4 | 34 30 28 30 37 28 32 30 31 29 29
21 | 6 10 13 9 28 4 8 11 8 17 3 | 28 35 30 32 40 28 35 28 30 36 30
22M | 9 8 7 9 37 3 8 8 5 13 3 | 32 32 25 30 38 28 31 26 31 24 28
23 | 12 15 10 15 33 4 15 16 9 17 5 | 35 36 29 29 32 29 36 28 31 25 29
24 | 10 6 16 6 34 3 8 7 5 14 3 | 24 31 27 27 32 26 29 27 28 33 27
25E | 10 9 13 8 30 4 9 7 7 14 3 | 46 48 49 51 53 47 50 47 49 52 48
26E | 12 10 15 8 31 4 10 12 9 16 4 | 24 25 31 24 30 24 26 25 27 25 24
27 | 12 11 13 11 30 5 6 6 5 12 3 | 29 34 28 27 36 27 31 28 28 31 28
28E | 7 12 7 10 27 4 11 13 6 12 3 | 24 30 23 25 27 23 28 20 23 30 23
29 | 9 14 14 12 29 3 14 16 11 21 5 | 31 34 28 35 33 29 33 32 30 37 29
30 | 5 7 13 8 30 3 8 9 6 13 3 | 24 30 25 25 29 25 28 24 24 31 25
31M | 10 16 12 10 31 6 12 16 8 18 4 | 27 36 26 27 36 25 33 23 24 28 25
32E | 12 18 11 9 35 5 14 11 7 18 4 | 45 45 44 45 33 43 44 45 48 42 43
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 12 10 32 4 10 11 8 15 |T 33 36 31 34 39 32 36 32 32 35 32
WRMS | 10 11 12 10 32 4 10 10 7 14 |NE 30 34 28 31 36 28 33 29 29 32 29
MEDI | 10 10 12 9 31 4 9 11 7 15 |MD 30 35 28 32 38 29 33 29 30 32 29
Table 3.1866.2 GPS week: 1866 Day: 2 MJD: 57308.000
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 8 12 8 10 3 6 11 6 16 3 | 33 39 32 35 36 34 40 34 36 39 35
2 | 9 8 11 10 15 4 9 12 9 16 3 | 29 36 30 35 32 30 34 31 34 29 31
3 | 10 8 11 8 19 3 7 13 6 13 3 | 40 43 43 40 47 39 44 40 40 43 40
4 | 9 8 10 9 13 4 6 10 7 14 3 | 32 33 32 31 31 32 32 32 33 26 31
5 | 14 12 6 13 21 4 11 11 8 8 4 | 40 44 36 46 48 40 43 39 40 40 40
6M | 7 6 12 6 11 5 5 10 5 10 2 | 34 42 32 36 41 34 40 37 37 34 36
7M | 10 10 12 14 13 3 12 12 8 12 4 | 36 37 28 35 32 29 37 29 32 31 31
8 | 7 10 12 13 12 4 7 10 8 11 3 | 35 42 38 34 32 35 42 37 36 42 37
9M | 8 7 13 8 13 3 7 11 5 9 3 | 50 54 52 47 42 49 54 47 51 55 50
X10 | 38 11 16 21 13 9 --- 19 24 --- 9 | 44 32 34 32 29 31 --- 31 30 --- 28
11 | 8 9 14 12 15 3 8 8 8 13 3 | 37 43 36 40 42 37 45 37 38 37 38
12E | 12 14 6 12 20 4 13 15 15 15 5 | 30 29 26 34 28 27 26 25 34 27 27
13 | 10 9 13 10 26 4 11 11 6 13 4 | 28 37 25 31 39 26 35 28 28 28 29
14 | 9 10 9 11 16 5 10 10 7 15 3 | 34 36 31 35 32 30 34 30 31 24 30
15 | 11 11 9 11 19 3 10 11 9 15 4 | 35 39 30 36 34 32 37 30 32 30 32
16E | 12 16 6 16 19 4 12 16 7 18 4 | 44 41 44 45 39 41 42 40 40 35 40
17M | 15 10 11 12 16 4 9 14 9 16 4 | 34 34 28 37 37 30 34 29 32 30 30
18 | 15 8 6 9 19 4 8 13 6 13 3 | 40 41 33 41 39 36 39 36 36 29 36
19 | 11 12 13 18 16 3 12 16 9 17 4 | 32 36 28 37 34 30 37 33 31 29 31
20 | 12 10 14 8 19 3 7 9 7 12 3 | 32 32 30 33 33 29 33 29 31 28 30
21 | 9 9 12 10 14 4 9 14 11 16 4 | 33 39 31 35 36 31 37 34 32 35 33
22M | 8 9 5 10 17 3 8 6 7 12 3 | 34 34 33 37 46 31 34 31 30 27 32
23 | 14 14 9 14 19 4 13 19 10 14 5 | 35 39 28 32 36 30 35 30 30 30 30
24 | 9 9 15 7 14 3 8 10 8 13 3 | 27 33 26 28 27 25 31 27 27 25 26
25E | 11 8 13 7 12 6 7 9 6 10 3 | 41 43 44 41 42 38 40 38 38 35 40
26E | 6 9 15 10 15 4 9 9 9 15 3 | 25 25 32 29 21 26 26 24 28 22 24
27 | 12 7 11 12 15 3 6 7 7 9 3 | 32 36 35 34 32 32 35 32 32 34 32
28E | 9 11 5 10 16 3 11 12 7 13 3 | 27 29 25 26 22 24 27 28 29 29 25
29 | 10 11 13 11 16 4 12 16 9 20 4 | 41 42 36 37 29 35 41 36 36 36 36
30 | 7 8 12 10 8 3 9 9 4 10 3 | 28 33 26 26 30 25 31 28 29 31 27
31 | 11 13 11 11 14 5 10 17 9 19 4 | 31 39 27 31 33 28 37 29 30 29 29
32E | 11 16 12 12 12 4 13 10 7 17 4 | 67 71 68 65 78 66 68 66 65 69 66
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 10 11 11 16 4 9 12 8 14 |T 35 38 33 36 36 33 37 33 34 33 33
WRMS | 10 10 11 11 15 4 9 11 7 13 |NE 34 37 31 33 33 31 36 32 32 31 31
MEDI | 10 9 12 10 15 4 9 11 7 13 |MD 34 37 32 35 34 31 37 31 32 30 31
Table 3.1866.3 GPS week: 1866 Day: 3 MJD: 57309.000
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 | 9 9 11 10 12 4 6 9 6 14 3 | 32 38 28 33 36 32 36 33 34 39 33
2 | 13 9 12 16 17 6 9 13 11 15 4 | 27 34 27 33 33 31 31 31 32 30 29
3 | 15 8 10 9 19 5 10 13 9 12 4 | 36 40 37 35 37 34 39 31 33 39 34
4 | 10 7 10 13 13 4 6 9 8 13 3 | 35 32 33 33 34 32 32 36 33 33 32
5 | 17 12 8 12 20 4 11 10 8 10 4 | 38 42 34 39 44 37 39 37 38 37 37
6 | 8 7 12 9 14 5 9 11 10 8 3 | 30 40 28 35 38 33 38 34 34 30 33
7 | 10 10 10 12 16 3 11 13 8 13 4 | 35 38 27 30 33 28 35 28 31 32 30
8 | 9 7 11 13 13 4 9 9 7 14 3 | 34 42 37 32 32 34 40 35 35 42 36
9 | 12 11 13 8 14 4 8 12 8 11 3 | 56 58 57 52 52 53 58 52 54 55 54
X10 | 19 10 16 19 12 8 16 11 11 --- 5 | 29 28 25 33 26 27 25 26 26 --- 23
11 | 9 8 13 13 14 5 7 7 7 13 3 | 37 42 35 41 44 38 42 38 35 39 37
12E | 15 14 9 15 20 5 14 15 12 13 5 | 26 26 22 32 22 23 24 23 30 23 23
13 | 10 14 13 10 25 3 11 11 9 11 4 | 25 33 21 26 35 22 32 24 22 20 24
14 | 9 13 12 10 18 4 10 11 9 14 4 | 27 33 25 29 32 25 29 26 25 18 25
15 | 10 12 8 12 22 4 11 9 9 14 4 | 33 32 25 29 32 27 31 26 28 24 26
16E | 11 14 7 13 18 4 12 13 10 13 4 | 46 47 44 48 43 45 47 44 46 47 45
17 | 13 14 13 14 18 6 13 15 13 16 5 | 29 31 24 33 31 28 30 30 29 28 26
18 | 11 13 5 11 18 5 9 14 8 13 4 | 32 33 22 30 32 25 30 28 29 23 27
19 | 18 13 13 17 14 4 12 16 10 17 5 | 29 32 23 30 27 25 30 28 23 21 24
20 | 13 12 9 10 19 3 9 9 7 11 3 | 27 26 20 27 30 23 25 25 25 20 22
21 | 9 9 12 9 13 4 8 13 10 14 3 | 29 34 27 31 35 29 32 32 28 30 29
22 | 8 11 7 9 16 4 8 6 6 14 3 | 31 30 25 29 32 28 30 26 30 24 27
23 | 16 10 10 13 21 3 13 18 11 14 5 | 33 32 27 27 26 24 33 26 31 19 26
24 | 10 10 15 8 15 5 7 9 5 11 3 | 26 30 25 25 27 22 30 27 25 24 25
25E | 12 10 12 13 12 5 9 8 9 11 3 | 39 40 41 41 41 37 39 36 35 39 37
26E | 9 16 14 8 14 6 11 9 9 11 4 | 24 27 28 23 18 22 27 23 25 20 22
27 | 9 6 12 8 13 3 7 6 8 10 3 | 26 31 28 25 26 25 30 27 24 27 26
28E | 13 9 6 14 17 4 11 12 9 10 4 | 22 26 20 23 23 20 22 22 25 22 20
29 | 10 12 12 13 15 6 13 16 12 14 4 | 36 36 32 33 30 29 36 33 32 29 31
30 | 8 8 11 9 13 3 7 10 5 10 3 | 26 29 22 21 24 22 27 23 27 28 23
31 | 12 11 12 11 15 4 11 14 14 17 4 | 31 35 23 30 31 25 35 25 32 25 27
32E | 11 15 12 15 19 6 14 10 9 20 4 | 92 97 94 90 102 95 93 96 97 95 94
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 11 12 17 4 10 12 9 13 |T 33 36 30 33 34 31 35 32 32 31 31
WRMS | 11 11 11 12 16 4 10 11 8 13 |NE 30 33 26 29 31 27 31 29 28 27 27
MEDI | 10 10 12 12 15 4 10 11 9 13 |MD 31 33 27 31 32 28 32 28 30 28 27
Table 3.1866.4 GPS week: 1866 Day: 4 MJD: 57310.000
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 7 13 10 11 4 7 8 7 14 3 | 32 41 34 34 37 34 40 33 34 41 35
2 | 12 9 13 12 17 4 10 14 10 16 4 | 31 39 31 40 31 34 34 31 36 30 32
3 | 9 9 12 7 22 4 9 10 8 12 3 | 34 39 41 36 42 35 36 33 35 41 36
4 | 9 8 10 12 20 5 7 11 9 15 3 | 33 36 35 32 35 32 33 33 34 32 32
5 | 12 14 8 12 17 4 12 10 8 11 4 | 35 44 33 39 36 36 39 35 39 33 36
6 | 12 9 13 6 12 3 9 8 8 10 3 | 29 41 30 36 36 34 38 30 35 34 33
7 | 13 10 11 11 16 4 12 13 10 13 4 | 32 39 27 30 33 30 36 29 31 34 31
8 | 7 9 11 14 13 2 7 9 8 14 3 | 34 41 37 28 35 33 37 34 36 39 34
9 | 10 9 13 7 12 4 8 12 6 7 3 | 46 51 52 47 49 49 50 44 46 50 47
X10 | 14 11 19 19 23 9 11 27 23 --- 7 | 30 30 26 26 32 24 24 37 30 --- 24
11 | 7 9 14 11 14 4 8 8 9 15 3 | 34 45 37 40 44 38 43 36 38 42 38
12E | 13 18 10 15 17 7 16 14 12 14 5 | 29 32 25 32 21 28 28 27 29 26 26
13 | 11 10 12 12 24 3 12 10 6 13 4 | 26 36 25 27 37 26 35 26 27 27 27
14 | 7 14 10 11 17 5 11 11 9 18 4 | 31 33 29 33 31 29 31 30 29 27 28
15 | 12 11 9 14 23 3 10 11 8 14 4 | 35 36 28 32 33 31 34 28 32 31 30
16E | 11 15 8 14 20 3 12 15 8 15 4 | 33 31 33 32 31 32 31 40 35 39 32
17 | 17 13 11 13 18 4 11 12 12 16 4 | 33 35 27 35 32 28 32 28 29 32 29
18 | 15 10 7 11 21 5 8 13 7 16 4 | 38 36 30 36 37 32 36 31 35 30 32
19 | 10 13 12 14 16 3 13 15 11 17 4 | 29 34 27 32 28 27 31 28 27 28 27
20 | 10 12 10 11 18 4 10 9 7 12 3 | 32 32 28 34 32 29 31 31 32 26 29
21 | 9 9 13 10 12 4 8 12 10 16 4 | 37 42 33 36 36 34 37 34 34 40 35
22 | 9 11 7 9 18 3 10 8 6 16 3 | 26 29 23 25 29 24 28 21 25 21 23
23 | 15 13 10 13 20 4 13 16 11 13 4 | 28 30 25 20 26 22 29 18 23 19 21
24 | 10 10 15 9 12 4 8 10 7 12 3 | 28 32 31 25 28 27 30 27 29 27 27
25E | 9 12 13 10 16 4 8 8 10 10 3 | 34 37 39 35 33 33 35 33 33 34 34
26E | 12 9 14 10 17 5 9 10 10 12 4 | 25 30 33 26 19 27 28 25 29 25 26
27 | 13 8 12 9 15 4 9 6 9 13 3 | 31 33 30 27 27 29 32 29 32 32 29
28E | 9 10 9 11 18 4 9 8 7 10 3 | 24 29 25 25 27 24 26 24 26 28 24
29 | 11 14 14 14 16 4 12 18 11 17 5 | 40 40 35 38 33 35 38 38 37 37 35
30 | 9 7 11 8 12 4 8 8 6 12 3 | 24 30 25 23 26 25 28 25 27 31 25
31 | 7 15 14 10 17 5 11 14 8 17 4 | 35 39 30 34 35 31 38 29 33 31 31
32E | 7 14 10 11 23 5 14 7 10 17 4 | 92 91 90 94 85 89 93 93 91 90 91
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 11 11 17 4 10 11 9 14 |T 33 37 32 34 34 32 35 32 34 34 32
WRMS | 11 11 11 11 16 4 10 10 8 14 |NE 31 35 30 30 32 29 33 30 31 31 29
MEDI | 10 10 11 11 17 4 10 10 8 14 |MD 32 36 30 32 33 31 34 30 32 32 31
Table 3.1866.5 GPS week: 1866 Day: 5 MJD: 57311.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 7 13 9 12 3 6 7 9 13 3 | 26 34 24 26 33 26 34 27 27 33 27
2 | 13 9 11 16 18 3 9 14 11 15 4 | 31 32 29 36 28 29 30 27 29 29 28
3 | 9 10 13 6 21 5 9 9 7 11 3 | 32 35 36 34 38 34 35 31 33 37 32
4 | 6 7 11 10 16 3 5 11 9 13 3 | 27 29 27 25 32 26 28 29 28 26 26
5 | 10 15 8 13 19 4 10 10 9 10 4 | 37 37 31 40 41 35 37 32 35 36 34
6 | 9 6 12 11 16 4 6 9 9 8 3 | 27 34 26 33 34 29 33 27 29 28 28
7 | 11 10 11 11 17 4 11 12 11 16 4 | 39 41 34 35 39 34 40 31 38 36 35
8 | 6 8 11 11 14 3 7 12 8 13 3 | 28 37 29 24 33 27 34 28 31 36 29
9 | 10 9 13 9 14 4 8 8 8 6 3 | 93 93 93 92 96 90 92 89 91 93 92
X10 | 44 22 19 23 19 11 15 11 21 --- 9 | 55 29 29 22 26 20 21 27 28 --- 23
11 | 7 9 15 12 16 4 7 9 10 14 3 | 29 37 29 32 40 29 37 29 29 34 30
12E | 10 19 7 15 20 3 14 13 14 14 5 | 28 31 21 31 21 25 28 22 29 29 24
13 | 12 11 10 13 24 4 11 10 7 11 4 | 23 30 20 24 35 21 31 24 21 21 22
14 | 8 11 10 12 17 4 10 14 8 15 4 | 24 28 22 26 30 22 27 26 22 23 22
15 | 12 10 8 15 23 4 11 10 8 19 4 | 30 30 22 25 29 24 29 24 24 25 23
16E | 11 11 6 15 20 5 12 16 8 14 4 | 35 34 35 38 36 34 34 37 35 38 34
17 | 10 10 12 14 16 4 11 10 13 15 4 | 26 28 22 29 30 23 29 21 25 23 23
18 | 13 9 6 11 17 5 9 15 7 12 3 | 32 31 23 30 32 26 31 27 30 23 26
19 | 8 12 13 16 17 3 12 15 11 17 4 | 26 31 21 27 29 22 30 26 21 20 22
20 | 9 16 8 12 17 4 10 10 8 13 4 | 26 26 21 29 28 23 26 25 25 21 22
21 | 8 8 11 10 14 4 10 15 10 13 4 | 30 33 28 31 30 27 32 26 28 32 28
22 | 8 9 9 8 19 6 9 10 6 12 3 | 25 26 19 24 29 21 25 21 25 17 20
23 | 13 13 8 13 22 4 12 17 13 16 5 | 30 29 21 21 26 22 27 21 24 16 20
24 | 9 10 14 9 14 3 8 8 7 11 3 | 26 29 27 21 26 23 29 25 27 28 25
25E | 10 11 12 11 17 6 9 7 7 12 3 | 31 34 35 30 34 30 35 27 32 35 31
26E | 10 7 12 11 17 6 7 11 6 12 3 | 21 23 27 21 20 20 22 21 20 18 20
27 | 11 8 11 9 14 3 8 8 9 9 3 | 28 30 25 21 28 23 28 25 25 26 24
28E | 8 9 6 12 14 3 11 10 11 9 3 | 19 26 20 20 18 19 23 20 23 24 20
29 | 11 11 13 15 21 5 12 20 12 16 5 | 35 32 27 34 27 28 31 35 31 32 29
30 | 7 8 12 8 13 3 7 9 9 8 3 | 22 27 23 20 22 21 26 22 27 25 22
31 | 9 10 13 10 14 5 9 14 9 15 4 | 28 34 22 27 27 23 33 24 25 26 24
32 | 6 10 11 7 33 6 12 8 9 13 4 | 105 106 104 106 110 105 106 107 106 101 104
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 10 11 12 18 4 10 12 9 13 |T 33 35 30 32 34 30 34 30 31 31 30
WRMS | 10 10 11 12 17 4 10 10 8 12 |NE 29 30 24 25 29 24 29 26 26 26 24
MEDI | 9 10 11 11 17 4 9 10 9 13 |MD 28 31 26 27 30 25 30 26 28 28 25
Table 3.1866.6 GPS week: 1866 Day: 6 MJD: 57312.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 8 13 9 12 4 6 7 7 12 3 | 31 39 30 34 41 34 38 35 32 36 34
2 | 10 10 12 14 21 4 10 15 8 19 4 | 33 35 30 37 44 34 34 35 33 32 33
3 | 10 10 13 8 21 3 8 11 6 8 3 | 31 35 34 31 33 32 35 29 33 37 31
4 | 8 8 12 13 13 4 6 12 9 11 3 | 30 33 31 35 37 33 33 36 33 30 32
5 | 8 19 10 11 20 4 12 9 9 11 4 | 36 41 30 38 43 36 38 36 37 36 35
6 | 7 8 13 9 18 4 8 12 9 12 3 | 36 42 30 38 46 38 40 37 36 35 36
7 | 12 10 13 10 17 3 10 13 8 10 4 | 33 36 27 32 33 28 33 31 32 29 29
8 | 8 8 13 9 16 4 6 12 8 10 3 | 33 41 37 30 30 32 38 32 34 36 34
9 | 9 10 15 8 14 2 8 10 5 5 3 | 94 92 92 92 89 93 94 92 95 91 92
X10 | 24 11 --- 21 11 9 10 17 11 --- 6 | 32 27 --- 34 21 22 22 28 22 --- 22
11 | 7 10 15 12 17 5 7 10 9 11 3 | 37 45 36 45 52 40 44 41 39 41 40
12E | 20 16 7 15 22 5 15 16 13 13 5 | 30 28 27 31 26 26 27 32 29 24 26
13 | 9 14 11 13 28 4 12 11 7 14 4 | 19 29 19 25 36 20 30 22 21 20 21
14 | 8 12 11 11 15 4 9 9 7 14 3 | 25 30 25 30 29 24 28 25 27 22 24
15 | 13 10 7 14 22 4 10 11 8 13 4 | 29 30 24 27 30 27 31 21 26 20 24
16E | 18 13 8 14 16 6 10 15 9 13 4 | 40 42 44 43 40 41 40 45 42 42 41
17 | 11 11 13 11 19 4 12 13 10 12 4 | 32 34 26 36 39 30 33 30 33 27 30
18 | 18 9 7 10 17 5 10 13 8 13 4 | 32 30 19 29 30 24 30 26 28 21 25
19 | 10 12 14 15 18 3 14 15 12 14 4 | 28 31 23 33 33 25 30 31 25 25 25
20 | 7 17 11 12 17 4 9 11 9 12 4 | 23 24 18 29 30 22 26 25 25 19 21
21 | 7 9 14 9 14 4 9 16 8 12 4 | 32 36 29 36 39 30 34 34 29 34 32
22 | 7 7 9 7 17 5 9 9 8 10 3 | 22 24 18 25 26 21 24 21 24 18 20
23 | 15 14 10 11 22 3 12 16 9 15 4 | 30 30 25 19 24 22 28 18 23 16 20
24 | 21 11 14 10 17 5 8 9 7 9 4 | 26 27 26 22 29 21 28 26 25 21 23
25E | 10 11 13 9 16 4 9 6 6 9 3 | 31 37 37 34 34 30 34 35 31 31 33
26E | 18 11 13 9 14 6 8 9 7 10 4 | 22 23 26 24 16 21 24 23 23 18 21
27 | 10 9 12 7 13 4 7 8 7 7 3 | 27 29 27 27 26 25 29 25 26 25 25
28E | 8 9 7 10 15 3 8 10 7 9 3 | 25 31 23 26 26 25 29 23 27 27 25
29 | 11 13 10 14 16 5 13 18 11 16 4 | 37 37 35 36 31 32 36 35 31 29 32
30 | 8 9 12 8 13 3 8 11 5 9 3 | 23 28 22 22 26 22 27 24 26 27 23
31 | 9 11 13 11 14 4 11 12 9 15 4 | 29 36 24 33 34 26 35 30 30 27 28
32 | 8 12 11 10 24 4 9 8 9 10 4 | 91 90 93 87 93 89 88 90 85 89 89
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 12 11 18 4 10 12 8 12 |T 33 36 31 35 36 32 35 33 33 31 32
WRMS | 11 11 12 11 17 4 10 11 8 12 |NE 29 32 26 30 32 26 31 28 27 26 26
MEDI | 9 10 12 10 17 4 9 11 8 12 |MD 31 33 27 32 33 27 33 30 29 27 28
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 4.1866 GPS week: 1866 MJD: 57306.0-57312.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 |U 4 4 14 |U 6 7 24 |U 7 7 16 |
emr | emr 3070 | 7 7 18 |U 7 7 25 | 8 9 17 |
esa | esa 3058 | 6 6 16 |U 7 7 24 | 8 9 18 |
gfz | gfz 3069 |U 5 6 15 |U 7 8 29 |U 8 9 18 |
grg | grg 3071 |U 8 7 19 |U 7 10 30 | 9 11 19 |
igr | igr 3037 | 5 5 14 | 6 7 24 | 8 8 16 |
igs | igs 3066 | 5 5 15 | 6 7 25 | 8 8 15 |
jpl | jpl 3053 | 6 7 18 |U 7 7 25 |U 8 8 17 |
mit | mit 3072 |U 10 9 24 |U 10 11 35 |U 9 8 21 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1866.0 GPS week: 1866 Day: 0 MJD: 57306.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 4 3 15 | 6 9 22 | 9 11 18 |
emr | emr 3068 | 7 6 19 | 6 10 26 | 8 9 17 |
esa | esa 3072 | 6 6 16 | 7 11 23 | 9 11 21 |
gfz | gfz 3068 | 5 6 15 | 6 9 26 | 9 10 17 |
grg | grg 3072 | 7 7 19 | 6 11 32 | 9 12 18 |
igr | igr 3044 | 5 5 16 | 6 10 25 | 9 11 17 |
igs | igs 3072 | 5 5 16 | 6 9 25 | 9 10 17 |
jpl | jpl 3068 | 7 7 18 | 6 9 25 | 10 9 15 |
mit | mit 3072 | 28 18 51 | 9 11 32 | 11 10 27 |
Table 5.1866.1 GPS week: 1866 Day: 1 MJD: 57307.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 | 5 3 13 | 4 5 18 | 8 9 16 |
emr | emr 3068 | 8 9 20 | 5 8 22 | 9 9 16 |
esa | esa 3072 | 7 6 17 | 5 6 20 | 9 10 14 |
gfz | gfz 3068 | 6 5 15 | 5 6 22 | 9 10 18 |
grg | grg 3072 | 7 5 17 | 6 6 25 | 9 9 18 |
igr | igr 3060 | 6 5 14 | 4 7 21 | 9 9 14 |
igs | igs 3064 | 6 6 16 | 5 6 21 | 8 9 15 |
jpl | jpl 3068 | 8 7 19 | 5 6 21 | 9 7 15 |
mit | mit 3072 | 18 14 36 | 6 7 22 | 18 13 31 |
Table 5.1866.2 GPS week: 1866 Day: 2 MJD: 57308.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3047 | 6 5 16 | 5 6 19 | 7 10 15 |
emr | emr 3068 | 8 9 22 | 5 5 21 | 8 9 15 |
esa | esa 3072 | 8 7 20 | 5 6 21 | 8 11 17 |
gfz | gfz 3068 | 6 7 17 | 5 6 19 | 8 11 16 |
grg | grg 3071 | 7 5 19 | 5 7 21 | 9 14 24 |
igr | igr 3064 | 6 6 17 | 5 6 19 | 8 10 15 |
igs | igs 3063 | 6 6 18 | 5 5 17 | 8 12 14 |
jpl | jpl 2970 | 7 7 20 | 5 6 20 | 9 8 15 |
mit | mit 3072 | 7 7 22 | 9 8 28 | 7 9 20 |
Table 5.1866.3 GPS week: 1866 Day: 3 MJD: 57309.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 4 4 14 | 8 8 23 | 7 6 16 |
emr | emr 3070 | 6 6 17 | 9 7 25 | 9 8 19 |
esa | esa 3072 | 5 6 17 | 8 7 22 | 8 8 19 |
gfz | gfz 3069 | 5 9 14 | 11 11 51 | 9 8 19 |
grg | grg 3072 | 11 11 24 | 11 17 34 | 10 11 21 |
igr | igr 3023 | 5 6 15 | 7 6 23 | 8 6 17 |
igs | igs 3051 | 5 7 16 | 8 7 23 | 8 7 17 |
jpl | jpl 3064 | 5 6 20 | 8 7 23 | 9 7 20 |
mit | mit 3072 | 4 6 17 | 8 8 25 | 7 6 20 |
Table 5.1866.4 GPS week: 1866 Day: 4 MJD: 57310.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 5 3 14 | 7 8 28 | 8 5 15 |
emr | emr 3072 | 7 5 15 | 8 7 27 | 8 7 16 |
esa | esa 3072 | 6 3 13 | 7 8 25 | 8 9 17 |
gfz | gfz 3068 | 5 4 12 | 6 8 29 | 9 7 22 |
grg | grg 3072 | 8 8 19 | 7 8 32 | 10 10 19 |
igr | igr 3017 | 5 3 13 | 6 7 28 | 8 7 15 |
igs | igs 3072 | 5 3 12 | 7 7 28 | 8 6 15 |
jpl | jpl 3069 | 5 5 13 | 7 8 27 | 8 7 18 |
mit | mit 3072 | 6 3 12 | 7 10 44 | 9 8 15 |
Table 5.1866.5 GPS week: 1866 Day: 5 MJD: 57311.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 | 4 5 13 | 8 8 26 | 5 5 13 |
emr | emr 3072 | 6 7 15 | 9 8 23 | 6 7 15 |
esa | esa 3072 | 5 7 15 | 8 7 26 | 6 7 16 |
gfz | gfz 3072 | 5 9 15 | 8 9 24 | 6 6 15 |
grg | grg 3071 | 6 8 16 | 8 11 27 | 9 9 16 |
igr | igr 3024 | 4 6 12 | 8 8 25 | 6 5 14 |
igs | igs 3072 | 4 6 12 | 8 8 25 | 6 5 13 |
jpl | jpl 3068 | 6 8 15 | 9 8 26 | 7 6 17 |
mit | mit 3072 | 5 7 14 | 25 22 63 | 7 7 16 |
Table 5.1866.6 GPS week: 1866 Day: 6 MJD: 57312.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3042 | 5 4 12 | 7 7 33 | 7 6 16 |
emr | emr 3072 | 7 5 16 | 8 5 32 | 9 11 18 |
esa | esa 2976 | 5 6 16 | 7 6 33 | 8 10 20 |
gfz | gfz 3072 | 5 6 14 | 7 7 31 | 10 10 19 |
grg | grg 3070 | 8 8 18 | 7 8 37 | 9 10 20 |
igr | igr 3032 | 5 5 13 | 7 6 32 | 8 9 17 |
igs | igs 3072 | 5 5 13 | 7 6 32 | 8 8 17 |
jpl | jpl 3070 | 6 7 19 | 7 7 33 | 7 9 18 |
mit | mit 3072 | 5 6 14 | 9 9 34 | 7 8 20 |
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 6.1866 GPS week: 1866 MJD: 57306.500-57312.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -17 -4 6 68 -1 | 20 30
| 16 16 56 138 7 | 6
emr uuuuu | 32 17 38 30 5 | 72 77
| 20 25 68 51 11 | 4
esa uuuuu | -6 18 68 48 0 | 30 37
| 15 18 24 31 4 | 5
gfz uuuuu | -2 -42 47 -124 -2 | 21 31
| 13 14 41 148 4 | 4
grg uuuuu | -22 14 77 4 -1 | 30 35
| 14 9 46 72 9 | 4
igr xxxxx | 10 -3 35 45 -1 | 0 23
| 9 8 44 39 3 | 5
irf xxxxx | 12 -3 -30 25 0 | -1 24
| 9 13 28 16 4 | 5
jpl uuuuu | 1 -9 -29 51 0 | 49 55
| 15 26 24 35 10 | 4
mit uuuuu | 6 11 -141 45 0 | 27 35
| 19 17 71 38 5 | 5
ngs uuuuu | -3 -6 -12 -53 1 | 17 29
| 22 32 38 101 6 | 7
sio uuuux | 4 15 10 -38 -18 | 93 96
| 11 28 55 50 8 | 5
Table 7.1866.0 GPS week: 1866 Day: 0 MJD: 57306.500
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 | 0 15 -18 117 6 | 19 25
emr uuuuu | 49 8 -63 39 -12 | 75 76
esa uuuuu | -8 20 86 33 -6 | 30 33
gfz uuuuu | 4 -26 19 52 -9 | 23 27
grg uuuuu | -26 6 109 81 10 | 29 32
igr xxxxx | 10 4 53 16 -6 | 0 16
irf xxxxx | 17 4 -17 48 -4 | -1 16
jpl uuuuu | -5 -23 -45 33 -13 | 50 52
mit uuuuu | 7 27 -94 49 -7 | 28 33
ngs uuuuu | -27 -13 18 -235 6 | 14 22
sio uuuux | 13 -2 101 15 -22 | 102 104
Table 7.1866.1 GPS week: 1866 Day: 1 MJD: 57307.500
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 | 6 -12 -32 174 -7 | 15 24
emr uuuuu | 16 7 75 56 -8 | 69 72
esa uuuuu | -5 10 28 63 -3 | 25 31
gfz uuuuu | 2 -34 60 -263 1 | 17 26
grg uuuuu | -8 30 114 92 0 | 25 29
igr xxxxx | 19 -7 -15 15 0 | -5 21
irf xxxxx | 10 -1 -49 40 3 | -6 20
jpl uuuuu | 4 -32 10 93 -2 | 46 51
mit uuuuu | -5 10 -178 59 -4 | 23 30
ngs uuuuu | -15 33 18 -77 9 | 10 22
sio uuuux | 8 -7 -9 -18 -21 | 95 98
Table 7.1866.2 GPS week: 1866 Day: 2 MJD: 57308.500
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 4 1 31 -1 | 12 21
emr uuuuu | -1 -11 141 -40 17 | 64 67
esa uuuuu | -15 1 56 41 2 | 22 28
gfz uuuuu | -6 -58 85 -237 -1 | 15 24
grg uuuuu | -8 2 141 -7 -7 | 24 28
igr xxxxx | 0 0 -16 -5 -2 | -8 21
irf xxxxx | 28 13 -80 37 8 | -9 20
jpl uuuuu | -3 -7 -34 93 -6 | 43 47
mit uuuuu | 31 11 -273 106 -1 | 19 27
ngs uuuuu | 10 31 -38 0 5 | 9 21
sio uuuux | 11 15 -11 -2 -24 | 90 93
Table 7.1866.3 GPS week: 1866 Day: 3 MJD: 57309.500
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 -32 79 205 1 | 18 31
emr uuuuu | 36 52 13 26 12 | 72 78
esa uuuuu | -21 0 62 6 2 | 29 39
gfz uuuuu | 9 -33 0 -312 -6 | 20 33
grg uuuuu | -19 16 76 -15 -6 | 30 37
igr xxxxx | 6 5 29 40 -4 | -1 26
irf xxxxx | 10 -3 -25 10 2 | -2 27
jpl uuuuu | -18 1 -28 -2 6 | 48 54
mit uuuuu | 30 -5 -111 54 1 | 25 36
ngs uuuuu | -6 -24 -31 15 3 | 16 32
sio uuuux | -4 48 -4 -10 -23 | 93 96
Table 7.1866.4 GPS week: 1866 Day: 4 MJD: 57310.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -13 1 -80 157 8 | 25 36
emr uuuuu | 35 -3 88 94 2 | 75 83
esa uuuuu | -21 12 75 73 -1 | 35 44
gfz uuuuu | -29 -59 -5 -114 2 | 25 37
grg uuuuu | -21 17 24 14 -15 | 35 41
igr xxxxx | 11 4 18 104 0 | 5 26
irf xxxxx | -2 -10 -30 21 -2 | 4 28
jpl uuuuu | 11 -13 -14 44 -9 | 53 60
mit uuuuu | -21 14 -99 -4 5 | 31 41
ngs uuuuu | 38 10 42 -131 0 | 24 35
sio uuuux | -10 39 -19 -124 -13 | 93 97
Table 7.1866.5 GPS week: 1866 Day: 5 MJD: 57311.500
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 | -37 -12 29 -31 -3 | 27 36
emr uuuuu | 60 52 -9 -36 7 | 75 82
esa uuuuu | 21 33 103 95 5 | 35 44
gfz uuuuu | 1 -31 79 -19 -1 | 25 37
grg uuuuu | -27 11 58 -12 -2 | 34 41
igr xxxxx | 25 -16 84 74 2 | 5 26
irf xxxxx | 6 -27 -11 11 -2 | 5 28
jpl uuuuu | -10 42 -23 64 13 | 52 59
mit uuuuu | -1 -13 -164 -2 6 | 32 41
ngs uuuuu | -9 -50 -63 -1 -9 | 25 36
sio uuuux | -11 -27 68 -83 -1 | 90 94
Table 7.1866.6 GPS week: 1866 Day: 6 MJD: 57312.500
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 | -36 9 65 -181 -11 | 26 36
emr uuuuu | 29 10 19 68 13 | 73 81
esa uuuuu | 4 50 63 26 2 | 34 43
gfz uuuuu | 5 -55 90 21 1 | 24 36
grg uuuuu | -48 14 19 -125 12 | 33 40
igr xxxxx | 0 -12 93 72 4 | 4 26
irf xxxxx | 13 2 5 8 -5 | 3 29
jpl uuuuu | 26 -34 -68 32 12 | 51 58
mit uuuuu | -3 35 -66 51 -2 | 31 41
ngs uuuuu | -16 -29 -28 54 -6 | 24 35
sio uuuux | 17 39 -58 -47 -22 | 86 90
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