[IGSREPORT-23958] Wk 1864 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sun Oct 18 21:08:42 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1864 (Sep 27, 2015 - Oct 03, 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:
igs1864[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1864[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1864[0-6].cls IGS GPS clock combination summary report.
igs18647.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18647.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | COD | 32 5 32 PIMO PIMO
0 | ESA | 10 32 10 32
0 | GFZ | TONG
0 | GRG | 10 10
0 | JPL | PIMO
1 | COD | 32 10 32
1 | ESA | 10 32 10 32
1 | GFZ | TONG TONG
1 | GRG | 6 NRMD
1 | JPL | GUAM TUVA
2 | COD | 32 32 MAC1
2 | ESA | 32 32 UFPR
2 | GFZ | GRAZ NOVM TONG
2 | GRG | 3 29 MAL2 NRMD MAC1 MAL2
2 | JPL | GUAM
3 | COD | 26 32 26 32
3 | ESA | 32 32 GLPS GLPS
3 | GFZ | 13 13 TONG NRMD TONG
3 | GRG | NRMD NRMD
3 | JPL | 32 TUVA
4 | COD | 26 32 10 26 32 BRST SUWN BRST NRMD SUWN
4 | EMR | 26 26
4 | ESA | 10 32 10 32 CHUR HYDE CHUR HYDE
4 | GFZ | 32 PRDS TONG PRDS SUWN TONG
4 | GRG | 29 HYDE DARW HYDE
4 | JPL | 32 SCOR
4 | MIT | GLPS GLPS
5 | COD | 10 10 HOB2
5 | EMR | 25 32 25 32
5 | ESA | 10 10 HOB2
5 | GFZ | 32 32 TONG TONG
5 | GRG | 32 32
5 | JPL | 25 GUUG
5 | MIT | CHPI CHPI
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | GFZ | ~19:00 | ~ -0.23 ns
2 | GFZ | ~07:00 | ~ -0.21 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
1 | COD | 3
3 | COD | 26
3 | GRG | 26
3 | NGS | 26
4 | COD | 26 32
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G03 | 4 | | 4 | | | | |
PRN G26 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.1 -2.2 -2.8 -43 14 6 .73
EMR | 0 | -3.0 -5.8 7.2 8 17 62 .67
ESA | 0 | -.1 -1.1 -.6 47 -60 58 .35
GFZ | 0 | -.2 -1.4 -2.2 -39 -89 -17 .67
GRG | 0 | -2.6 -5.8 4.0 -43 15 -21 .51
JPL | 0 | -1.8 -9.6 5.2 -7 42 142 .70
MIT | 0 | -1.6 -2.8 3.8 16 -1 -27 .66
NGS | 0 | .4 -2.0 11.9 -66 -33 -22 .74
SIO | 0 | -1.9 -.3 .0 -44 -14 -29 .55
COD | 1 | -.7 -2.3 -1.9 -51 5 -7 .55
EMR | 1 | -1.5 -1.5 6.0 26 11 51 .52
ESA | 1 | .1 -1.0 -.4 56 -59 60 .33
GFZ | 1 | .8 -1.6 -2.3 -35 -78 -28 .41
GRG | 1 | -3.6 6.4 5.0 -51 21 -29 .24
JPL | 1 | 2.3 .5 .3 -21 38 -48 .58
MIT | 1 | -5.7 -1.3 -.5 38 -19 -36 .77
NGS | 1 | -7.1 -1.2 7.6 -41 12 -86 .60
SIO | 1 | -3.6 2.8 -1.8 -15 -9 -15 .52
COD | 2 | -1.5 -2.5 -2.4 -80 -3 23 .71
EMR | 2 | 1.0 -1.6 3.5 36 4 45 .77
ESA | 2 | .2 -1.2 -.3 58 -50 91 .47
GFZ | 2 | .0 -1.3 -2.8 -47 -92 -17 .65
GRG | 2 | 3.6 8.1 -3.9 -46 24 -26 .60
JPL | 2 | 2.6 -3.2 -3.2 -28 3 38 .59
MIT | 2 | -1.6 2.2 1.1 11 -7 -40 .94
NGS | 2 | -3.0 -.1 6.9 -33 -12 -33 .68
SIO | 2 | -2.8 2.6 -4.0 -40 -10 5 .43
COD | 3 | -1.4 -1.9 -1.9 -52 5 -6 .74
EMR | 3 | -5.3 -3.1 4.3 9 -2 28 .69
ESA | 3 | -1.1 -1.3 -.7 61 -59 66 .40
GFZ | 3 | -.1 -1.5 -2.1 -31 -90 -9 .62
GRG | 3 | 1.5 4.8 -4.3 -7 33 16 .38
JPL | 3 | -5.6 -4.3 2.5 11 -29 49 .67
MIT | 3 | .7 -3.5 -1.3 10 -1 -20 .86
NGS | 3 | -7.2 -3.0 -.8 -1 24 -68 .49
SIO | 3 | 1.5 -.2 1.7 -11 -19 -34 .64
COD | 4 | -.7 -1.6 -1.3 -49 -8 -18 .73
EMR | 4 | 6.4 3.0 .6 -7 9 11 .60
ESA | 4 | -.5 -.7 -1.0 60 -66 77 .49
GFZ | 4 | .5 -1.3 -3.0 -21 -107 -14 .62
GRG | 4 | 1.2 3.9 -.9 -44 37 -26 .24
JPL | 4 | 1.1 -11.7 -1.5 -9 20 33 .78
MIT | 4 | .1 -.8 -1.4 0 -1 -18 .99
NGS | 4 | -4.0 -2.7 2.8 -20 -3 -50 .87
SIO | 4 | -1.0 3.0 -13.6 -21 -24 -21 .56
COD | 5 | -.6 -1.0 -1.9 -38 -7 -3 .64
EMR | 5 | -.1 -1.4 8.0 -22 26 16 .60
ESA | 5 | -.7 -.5 .2 78 -61 91 .35
GFZ | 5 | .7 -.8 -1.9 -23 -117 -10 .46
GRG | 5 | 7.9 11.1 .0 -44 9 -33 .28
JPL | 5 | .2 -9.2 7.8 6 41 -2 .50
MIT | 5 | .7 1.9 -.7 30 -3 -21 .65
NGS | 5 | -3.5 -.2 4.6 -17 -6 -23 .46
SIO | 5 | 1.8 3.5 -11.8 -21 -27 9 .51
COD | 6 | -.7 -1.4 -1.8 -35 -1 17 .66
EMR | 6 | .5 3.6 4.9 -3 9 17 .62
ESA | 6 | -1.0 -1.2 .6 89 -65 85 .28
GFZ | 6 | .0 -.7 -2.0 -16 -108 0 .57
GRG | 6 | -2.9 7.3 2.0 -39 27 -14 .71
JPL | 6 | 1.0 -7.2 1.3 2 12 35 .92
MIT | 6 | -2.9 1.4 -2.1 20 8 -26 .71
NGS | 6 | -5.3 2.9 5.2 -2 7 -51 .49
SIO | 6 | -2.0 4.0 -18.0 -12 -27 20 .23
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1864.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1864.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 2.1864.[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 3.1864.[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 5.1864.0-6). 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 1864 summary. (Sep 27, 2015 - Oct 03, 2015)
Table 1.1864.a GPS week: 1864 MJD: 57292.000-57298.000
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 242| 1 2 1 13 14 -1 -.04 14 11 | -797 -374 15 123
| 1 1 4 17 18 18 .03 | 149 228
emr 79| -1 -1 3 -7 -12 13 .18 11 11 | 3395 -253 12 122
| 1 2 1 13 13 10 .09 | 990 922
esa 150| 0 -1 0 -11 4 7 -.36 13 13 | -787 209 9 137
| 0 1 2 22 16 14 .04 | 575 639
gfz 197| -2 0 -2 7 -27 -19 .04 11 11 | -1579 4284 38 141
| 0 0 1 20 20 18 .03 | 3775 11401
grg 115| 0 1 0 -26 45 6 -.05 16 15 | 232 -176 16 166
| 1 1 2 25 51 29 .03 | 114 225
igr n/a| 0 0 0 -6 5 -3 -.05 5 4 | 494 314 17 100
| 0 0 0 24 8 10 .01 | 1334 1067
jpl 80| 0 0 2 17 21 11 .21 11 11 | 3401 -233 16 118
| 2 1 1 25 28 62 .03 | 995 926
mit 348| 1 -1 -1 -22 -12 -10 -.14 12 10 | 519 560 44 432
| 0 0 1 29 23 18 .02 | 1346 714
ngs 217| 0 1 -1 17 -3 18 -.03 9 8 | -785 -458 1036 2713
| 1 0 0 16 21 42 .07 | 172 308
sio 305| 0 -1 -2 -12 -19 -30 .14 14 13 | --- --- --- ---
| 0 0 3 34 19 28 .04 | --- ---
Table 1.1864.b GPS week : 1864 MJD: 57292.000-57298.000
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 3 4 3 |
2 | 5 5 5 5 5 5 5 |
3 | 6 8 6 5 4 4 4 |
4 | 4 4 4 4 3 4 3 |
5 | 4 4 4 4 4 5 5 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 3 4 4 4 3 4 4 |
9 | 3 3 3 3 3 3 3 |
10 | 6 6 6 7 6 7 6 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 4 5 5 6 5 |
13 | 5 4 5 4 4 4 4 |
14 | 4 4 4 5 5 5 5 |
15 | 5 4 5 5 4 4 4 |
16 | 5 5 5 6 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 4 4 3 4 4 4 4 |
19 | 5 5 5 5 5 5 5 |
20 | 4 4 4 4 5 4 4 |
21 | 4 4 4 4 5 4 4 |
22 | 4 4 3 3 3 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 4 5 5 10 5 5 5 |
26 | 5 5 9 25 10 6 5 |
27 | 4 4 4 4 4 4 4 |
28 | 4 5 4 4 4 4 4 |
29 | 5 5 5 5 5 6 5 |
30 | 3 3 3 3 3 3 3 |
31 | 4 5 5 5 5 4 5 |
32 | 5 5 6 7 6 8 6 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1864.0 GPS week: 1864 Day: 0 MJD: 57292.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 244| 2 2 1 19 12 -18 -.03 13 11 | -671 -706 14 114
emr 78| -2 -4 5 -15 5 12 .11 11 11 | 5257 -1842 12 129
esa 150| 0 0 0 -1 1 -18 -.32 13 12 | -114 155 9 148
gfz 198| -1 1 -4 38 -24 -42 .09 11 10 | -281 166 37 169
grg 118| 0 2 1 -34 -18 11 -.03 15 15 | 267 -48 17 156
igr n/a| 0 0 0 0 14 -20 -.04 4 4 | 846 -1373 16 97
jpl 80| 0 0 3 55 29 115 .17 11 11 | 5271 -1846 15 146
mit 347| 0 -1 -1 -29 -12 -10 -.16 12 10 | 963 -182 43 429
ngs 220| 0 1 0 -13 7 -17 .02 9 7 | -569 -931 904 2452
sio 306| 0 -1 -3 -26 -21 -27 .09 13 12 | --- --- --- ---
Table 2.1864.1 GPS week: 1864 Day: 1 MJD: 57293.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 245| 2 2 2 31 28 3 -.01 12 11 | -882 -460 16 117
emr 78| -1 -4 4 -17 -7 15 .10 11 11 | 3217 -864 12 125
esa 150| 0 0 -1 -29 1 -1 -.35 12 13 | -1008 -274 9 137
gfz 199| -2 1 -3 -6 -52 -40 .07 11 11 | -128 -820 36 166
grg 113| 0 2 2 -43 16 -7 -.05 16 16 | 238 -454 16 166
igr n/a| 0 0 0 15 -4 12 -.07 4 4 | -563 -337 15 104
jpl 80| 3 0 2 23 55 -86 .17 11 11 | 3211 -853 15 96
mit 347| 1 -1 -2 5 -29 -25 -.13 12 10 | -474 879 44 475
ngs 220| 0 0 0 17 -14 110 .02 9 7 | -811 -544 1134 2575
sio 308| 0 -1 -2 -18 1 -24 .12 14 13 | --- --- --- ---
Table 2.1864.2 GPS week: 1864 Day: 2 MJD: 57294.000
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 2 0 27 33 35 -.02 13 12 | -1018 -224 16 132
emr 80| 1 -3 2 5 -13 14 .09 11 11 | 2786 -590 12 106
esa 150| 0 0 -1 -4 10 21 -.37 12 12 | -1035 461 10 142
gfz 200| -3 1 0 10 -5 -13 .06 11 10 | -796 511 35 139
grg 115| 0 0 -3 -40 32 -42 -.07 16 15 | 9 22 16 175
igr n/a| 0 0 0 23 7 0 -.03 5 5 | -520 -328 16 112
jpl 80| 4 0 1 7 20 19 .19 12 12 | 2774 -533 16 108
mit 349| 0 -1 0 -34 -10 -41 -.11 10 9 | -519 -516 40 376
ngs 221| 0 1 -1 35 -13 10 .05 9 7 | -1028 -326 1017 2731
sio 307| 0 -2 1 -56 -27 -11 .17 14 13 | --- --- --- ---
Table 2.1864.3 GPS week: 1864 Day: 3 MJD: 57295.000
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| 3 1 -6 15 22 -17 -.06 14 12 | -556 -639 15 118
emr 80| -2 1 4 16 -10 18 .15 11 11 | 2313 258 11 95
esa 150| 1 -3 -3 -31 20 7 -.41 14 14 | -526 153 12 136
gfz 196| -2 0 0 15 -20 -13 .02 11 11 | -75 261 40 124
grg 116| 0 2 0 -17 113 43 -.07 17 16 | 248 -196 17 151
igr n/a| 0 0 -1 -14 18 1 -.05 5 4 | -715 720 17 95
jpl 80| 1 0 4 46 -31 35 .21 11 11 | 2343 275 16 104
mit 348| 2 -1 0 -55 1 -10 -.13 11 9 | -742 677 49 400
ngs 216| -1 2 -2 12 -15 -6 -.02 9 7 | -571 -777 992 2810
sio 300| 2 -3 2 -22 -26 -49 .20 15 14 | --- --- --- ---
Table 2.1864.4 GPS week: 1864 Day: 4 MJD: 57296.000
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| 1 3 1 -3 2 -1 -.09 22 11 | -846 -142 17 126
emr 80| 0 1 2 -23 -39 23 .27 12 12 | 2915 146 13 117
esa 150| 0 -1 0 -40 -27 15 -.40 13 13 | -1827 -502 10 133
gfz 197| -2 0 -1 -26 -49 -2 .01 11 12 | 270 -241 37 146
grg 118| 0 0 4 18 117 -15 -.00 16 14 | 238 -45 16 177
igr n/a| -1 0 0 -50 1 -4 -.03 5 5 | 205 842 20 114
jpl 80| 0 -3 2 -15 12 -4 .21 10 10 | 2893 183 18 126
mit 348| 1 -2 -1 22 31 2 -.15 11 10 | 126 777 52 454
ngs 214| 0 2 -2 27 -24 6 -.06 9 8 | -927 -82 1121 2585
sio 304| 0 -2 -4 51 12 -30 .16 15 15 | --- --- --- ---
Table 2.1864.5 GPS week: 1864 Day: 5 MJD: 57297.000
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 239| 0 1 4 -16 25 -5 -.02 13 10 | -776 -269 15 120
emr 79| -3 0 4 -10 -6 17 .27 13 12 | 3143 980 14 136
esa 150| 1 0 1 11 8 22 -.33 12 12 | -263 1474 10 142
gfz 197| -1 0 -2 10 -39 -29 .02 12 12 | 63 -5 39 122
grg 114| 3 0 -2 -12 27 19 -.05 14 13 | 231 9 17 172
igr n/a| 0 0 -1 -13 -1 0 -.05 5 5 | 1191 1896 20 95
jpl 80| -2 0 4 -3 46 -30 .25 11 11 | 3154 990 17 142
mit 349| 2 -2 -3 -11 -30 -3 -.12 13 11 | 1247 1647 39 459
ngs 216| 0 0 -2 31 -2 23 -.11 9 8 | -745 -356 1007 2948
sio 308| 0 -1 -3 -26 -40 9 .16 17 16 | --- --- --- ---
Table 2.1864.6 GPS week: 1864 Day: 6 MJD: 57298.000
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 0 6 18 -21 -5 -.06 15 12 | -830 -179 15 134
emr 80| -2 0 3 -6 -11 -9 .27 10 10 | 4140 137 15 148
esa 150| 0 0 3 15 18 6 -.34 12 12 | -736 1 8 125
gfz 196| -2 0 -2 11 -2 5 -.01 11 11 | -10108 30122 43 123
grg 113| 1 0 1 -58 29 32 -.10 16 14 | 399 -525 17 166
igr n/a| 0 0 0 -9 2 -9 -.04 4 4 | 3020 778 17 89
jpl 80| -1 0 2 11 15 27 .23 10 10 | 4163 151 16 108
mit 349| 1 -2 -4 -51 -35 14 -.16 12 11 | 3037 641 44 431
ngs 214| 1 2 -1 11 39 3 -.11 10 8 | -847 -193 1077 2892
sio 305| 0 0 -6 14 -35 -80 .10 13 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 3.1864.0 GPS week: 1864 Day: 0 MJD: 57292.000
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 9 13 9 12 3 8 11 9 14 3 | 28 29 26 35 31 27 32 28 29 37 29
2 | 9 10 15 12 18 7 11 10 9 18 4 | 34 41 35 51 46 42 40 41 40 37 39
3E | 30 14 17 13 21 6 13 11 13 8 5 | 208 201 204 205 201 205 185 206 203 204 203
4 | 8 11 12 11 14 4 9 11 7 8 3 | 38 34 37 45 39 37 35 40 39 37 37
5E | 12 10 9 10 14 3 13 10 7 18 4 | 53 49 47 52 53 50 53 47 51 57 50
6 | 9 10 13 7 15 4 9 9 6 12 3 | 23 30 23 30 30 25 28 27 25 27 25
7 | 12 10 14 10 14 3 10 11 10 11 4 | 34 30 25 34 30 28 33 26 29 28 27
8 | 6 8 14 8 12 3 8 11 5 12 3 | 29 32 29 33 33 31 33 30 31 35 30
9 | 10 8 15 7 13 3 9 7 5 12 3 | 31 27 29 27 22 25 31 26 29 31 26
X10 | 19 22 19 18 13 7 11 13 12 --- 6 | 34 28 20 38 28 25 23 33 28 --- 25
11 | 8 11 15 12 15 3 9 10 10 17 4 | 57 57 55 66 65 58 60 59 59 56 58
12E | 13 16 9 10 18 4 13 12 11 12 4 | 29 32 27 32 29 27 28 27 30 28 27
13 | 12 10 15 9 19 4 11 17 9 12 4 | 26 37 24 32 40 27 36 29 28 31 29
14 | 8 12 12 11 11 5 11 17 10 13 4 | 25 26 24 31 26 22 28 31 26 23 24
15 | 17 10 12 10 16 4 10 13 11 17 4 | 42 37 37 33 30 34 38 27 37 36 33
16E | 15 14 6 16 15 4 13 14 7 14 4 | 27 31 25 30 26 26 28 29 26 29 26
17 | 15 11 14 12 17 4 14 14 9 17 4 | 32 35 32 44 40 35 37 38 37 35 35
18E | 11 11 6 10 10 4 10 17 7 9 3 | 36 34 34 41 35 35 37 30 38 36 34
19 | 10 15 14 17 13 4 13 13 9 19 5 | 33 31 27 42 33 29 32 34 30 28 30
20E | 12 11 8 8 18 4 9 11 9 8 3 | 31 32 32 37 30 34 35 33 35 37 33
21 | 8 10 13 11 15 4 11 10 11 15 4 | 46 43 40 48 48 43 44 46 44 44 43
22E | 11 12 8 10 14 3 9 17 8 8 4 | 31 32 30 37 37 32 34 30 35 31 31
23 | 14 13 12 11 16 4 13 17 11 15 4 | 29 27 20 24 25 20 29 22 20 20 20
24 | 11 7 13 8 14 6 9 11 7 11 3 | 29 32 24 33 35 28 34 31 33 34 30
25E | 11 10 14 9 17 5 10 10 8 7 3 | 58 59 63 61 61 61 54 61 58 57 59
26E | 15 11 15 16 17 5 13 11 11 9 4 | 687 530 674 678 681 677 266 679 675 676 677
27 | 10 10 12 10 11 5 8 10 4 14 3 | 38 34 35 42 39 37 38 40 37 42 37
28E | 19 9 8 9 17 3 11 9 7 9 4 | 30 25 22 27 25 24 28 22 26 28 24
29 | 10 13 12 13 14 4 13 13 10 14 4 | 38 36 34 39 34 35 36 39 36 38 35
30 | 6 8 13 8 10 3 7 6 5 8 3 | 28 28 26 27 30 26 30 26 28 28 26
31 | 8 15 12 12 13 4 11 14 8 14 4 | 26 33 20 28 29 25 34 28 26 29 25
32E | 17 18 13 12 24 4 13 10 15 12 5 | 64 70 66 64 63 64 69 62 63 64 64
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 11 12 11 15 4 11 12 9 13 |T 61 56 57 63 61 59 48 60 60 62 59
WRMS | 11 11 12 10 15 4 11 10 7 12 |NE 33 33 29 37 34 31 34 33 32 33 31
MEDI | 11 11 13 10 14 4 11 11 9 12 |MD 32 32 29 37 33 31 34 31 33 35 30
Table 3.1864.1 GPS week: 1864 Day: 1 MJD: 57293.000
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 14 9 10 4 8 14 7 16 3 | 27 29 27 28 25 26 30 23 27 40 27
2 | 8 13 16 14 18 5 12 12 8 18 4 | 24 30 24 35 31 27 29 27 27 27 26
X3E | 70 13 22 15 21 10 --- 15 25 14 7 | 173 149 158 146 148 146 --- 150 144 150 148
4 | 12 11 11 10 13 4 8 11 7 11 3 | 28 23 26 29 23 25 25 26 27 28 25
5E | 7 10 8 8 13 4 11 16 7 10 3 | 35 33 34 36 37 34 32 33 36 38 34
6 | 9 7 13 5 14 3 10 10 8 11 3 | 19 21 17 19 20 18 23 19 19 21 18
7 | 12 12 12 10 15 3 9 10 10 12 4 | 33 28 21 26 27 23 31 19 24 27 24
8 | 9 8 14 12 14 4 7 10 9 15 3 | 21 28 23 24 25 22 27 23 23 32 23
9 | 9 7 15 6 12 4 8 8 4 11 3 | 26 26 26 24 22 22 27 21 22 25 23
X10 | 25 15 17 20 15 15 13 11 13 --- 6 | 29 23 22 26 26 23 25 28 25 --- 21
11 | 10 11 15 12 15 4 8 11 8 18 4 | 35 37 34 40 40 35 40 35 36 39 36
12E | 15 12 8 12 16 4 13 15 10 15 4 | 22 21 14 25 19 18 23 16 21 22 17
13 | 10 11 15 9 20 4 11 13 8 14 4 | 25 30 20 23 31 19 29 20 23 25 22
14 | 9 12 13 13 13 5 11 15 10 14 4 | 23 23 23 24 22 19 24 24 21 20 20
15 | 14 9 11 11 17 4 11 13 8 19 4 | 34 31 30 30 26 27 31 23 28 29 27
16E | 12 15 8 14 21 6 12 13 9 14 4 | 25 28 24 27 25 21 23 30 24 29 24
17 | 13 12 14 13 19 5 14 13 10 17 5 | 26 28 26 32 29 26 29 26 27 27 26
18E | 11 12 5 8 12 4 11 8 6 12 3 | 30 28 27 31 31 27 27 25 31 25 27
19 | 15 16 13 15 15 3 12 14 10 21 5 | 27 27 21 26 23 21 25 23 21 22 21
20E | 12 10 9 7 15 3 10 10 6 9 3 | 29 25 26 31 30 27 28 28 30 27 27
21 | 10 11 13 11 16 5 10 11 10 15 4 | 35 32 30 34 35 31 33 31 31 31 31
22E | 9 17 6 9 12 4 9 15 7 11 3 | 28 26 25 30 28 25 28 24 28 25 25
23 | 16 13 12 12 19 4 14 19 12 17 5 | 28 26 22 20 23 19 27 21 18 21 19
24 | 10 8 13 8 14 3 7 11 8 10 3 | 21 23 19 22 25 19 24 22 24 23 20
25E | 15 10 15 12 15 4 12 11 13 12 4 | 48 47 52 50 47 48 45 47 46 45 47
26E | 16 14 16 17 19 6 13 11 8 12 5 | 774 555 756 763 767 759 334 762 758 759 760
27 | 12 7 12 8 15 5 7 10 6 14 3 | 32 32 31 31 35 32 33 34 33 35 31
28E | 22 12 10 11 20 3 10 10 13 12 4 | 27 25 24 24 25 20 24 19 21 27 21
29 | 11 11 13 15 16 5 15 13 9 14 4 | 31 30 27 33 25 27 32 31 29 30 27
30 | 10 9 13 6 12 3 7 6 7 10 3 | 26 25 24 23 26 22 28 22 22 28 23
31 | 9 14 13 19 16 8 14 14 8 15 4 | 25 30 22 27 26 21 30 22 24 26 22
32E | 16 13 12 12 24 4 14 9 15 14 5 | 59 59 58 62 52 59 60 58 61 59 58
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 12 11 16 4 11 12 9 14 |T 57 49 53 56 55 52 39 53 54 56 53
WRMS | 11 11 13 11 16 4 11 10 7 13 |NE 27 27 24 27 26 24 28 24 25 27 24
MEDI | 11 11 13 11 15 4 11 11 8 14 |MD 28 28 25 28 26 25 28 24 27 27 25
Table 3.1864.2 GPS week: 1864 Day: 2 MJD: 57294.000
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 7 13 8 9 4 8 11 7 17 3 | 25 26 23 27 27 25 28 25 28 39 26
2 | 14 11 13 17 17 4 13 12 8 18 4 | 28 33 29 41 38 30 32 32 32 28 30
3E | 17 16 20 12 28 8 22 8 16 12 6 | 169 166 165 171 158 169 186 169 170 168 167
4 | 9 10 12 9 12 5 9 9 7 11 3 | 32 29 30 33 34 31 31 33 34 31 31
5E | 8 10 8 8 17 3 12 14 8 13 4 | 46 44 41 44 39 44 46 41 46 49 43
6 | 10 8 13 7 15 5 11 9 6 13 3 | 21 24 19 22 26 19 25 23 22 21 21
7 | 16 9 12 12 14 2 12 10 9 14 4 | 32 29 21 30 26 25 30 22 25 30 24
8 | 9 8 12 10 16 4 6 7 9 16 3 | 23 29 24 23 28 23 28 25 25 34 24
9 | 13 7 14 6 11 4 8 6 6 8 3 | 29 27 27 22 21 23 30 22 25 26 24
X10 | 19 12 --- 14 16 16 11 18 12 --- 6 | 36 26 --- 27 26 24 24 34 30 --- 26
11 | 15 9 15 10 15 4 9 9 9 14 4 | 43 48 45 51 56 46 50 46 48 48 47
12E | 12 13 9 9 14 5 11 11 9 11 4 | 24 24 20 27 18 21 24 21 22 26 21
13 | 14 11 13 13 19 4 12 11 8 14 4 | 25 28 19 25 31 22 28 23 23 24 22
14 | 11 10 13 11 11 6 11 12 8 13 4 | 23 25 22 26 21 18 26 23 21 20 21
15 | 14 12 12 13 18 6 14 12 9 20 4 | 36 34 33 28 31 29 36 26 32 31 29
16E | 14 12 6 11 25 4 13 13 7 14 4 | 26 26 23 26 22 24 26 33 27 36 25
17 | 15 13 14 13 18 6 13 11 10 17 4 | 30 30 28 36 32 30 29 29 29 29 28
18E | 12 11 7 8 11 4 9 7 7 11 3 | 28 29 26 32 28 29 30 26 31 29 27
19 | 11 13 12 14 13 5 13 12 10 20 4 | 30 30 25 31 31 26 29 27 26 26 25
20E | 14 10 8 7 16 4 9 9 5 10 3 | 27 25 24 26 27 24 26 26 27 28 24
21 | 12 11 15 11 15 9 10 12 10 14 4 | 39 39 33 42 42 37 39 37 34 35 35
22E | 9 10 6 8 12 4 10 6 7 7 3 | 30 28 24 31 29 27 30 23 31 28 26
23 | 15 12 12 11 18 4 16 14 10 14 4 | 27 26 18 20 21 18 28 17 19 18 18
24 | 10 9 14 8 11 4 9 9 8 12 3 | 22 28 24 26 25 22 26 26 26 22 23
25E | 13 11 15 10 13 6 19 8 16 9 4 | 57 50 54 55 50 53 62 52 54 51 52
X26E | 49 16 17 16 27 6 --- 13 18 12 8 | 793 768 781 788 796 784 --- 780 792 782 785
27 | 11 8 11 9 18 4 6 10 6 11 3 | 29 30 31 28 33 29 29 31 31 33 29
28E | 11 12 7 12 21 4 13 9 7 7 4 | 22 25 21 28 23 22 25 21 25 28 22
29 | 14 14 14 14 14 6 12 15 12 15 5 | 34 33 29 34 30 29 33 35 34 31 30
30 | 9 7 12 9 13 3 9 6 4 7 3 | 24 25 22 25 25 23 25 22 24 27 22
31 | 9 14 12 14 14 5 14 14 8 16 4 | 27 31 20 26 26 22 32 24 23 23 23
32E | 23 12 14 12 22 6 17 12 11 20 5 | 62 55 56 61 53 56 57 54 59 57 55
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 11 12 11 16 5 12 10 9 14 |T 59 58 56 59 58 56 37 57 58 59 56
WRMS | 12 11 12 10 15 5 12 9 7 13 |NE 29 30 26 29 30 26 30 27 28 28 26
MEDI | 12 11 12 11 15 4 11 11 8 13 |MD 29 29 25 28 28 25 29 26 28 29 26
Table 3.1864.3 GPS week: 1864 Day: 3 MJD: 57295.000
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 15 9 10 3 8 9 8 20 3 | 37 37 34 37 35 35 36 34 36 45 35
2 | 9 10 14 16 18 5 13 9 8 18 4 | 35 39 34 43 40 38 38 39 40 37 37
3E | 15 10 18 9 22 5 13 9 12 16 4 | 97 102 99 99 98 98 97 97 101 102 99
4 | 10 9 13 10 12 4 9 8 8 13 3 | 46 39 41 44 40 40 37 43 43 40 41
5E | 13 15 7 8 14 5 12 10 6 16 4 | 64 57 55 57 60 57 59 54 57 64 57
6 | 7 7 16 6 16 3 8 12 10 14 3 | 27 31 25 26 31 27 30 32 27 31 28
7 | 14 10 12 12 13 4 11 10 8 17 4 | 34 32 23 29 28 28 33 27 27 33 28
8 | 10 8 13 10 17 5 6 6 6 17 3 | 32 34 32 29 30 29 31 29 31 40 30
9 | 10 7 13 7 15 3 7 5 7 9 3 | 39 36 37 31 28 32 37 33 34 38 34
X10 | 21 11 --- 18 17 9 16 18 12 --- 6 | 47 32 --- 39 35 36 29 38 41 --- 34
11 | 8 9 17 10 14 4 8 9 9 17 4 | 57 57 55 58 61 56 56 56 56 55 56
12E | 11 15 12 11 18 5 12 12 10 14 4 | 32 35 27 35 34 32 35 28 36 36 31
13 | 12 10 15 13 20 4 12 10 7 12 4 | 23 33 20 24 33 24 33 25 26 32 25
14 | 11 12 18 13 15 5 10 10 10 15 4 | 21 28 21 27 25 20 26 23 21 21 21
15 | 17 9 14 13 20 3 13 11 10 16 4 | 41 37 36 27 33 33 38 27 38 29 32
16E | 21 17 12 9 22 7 18 22 8 19 5 | 44 32 38 29 28 30 30 49 31 49 34
17 | 11 11 15 14 20 4 15 12 12 16 4 | 35 35 31 39 35 33 33 35 36 33 33
18E | 18 12 9 9 18 4 10 9 7 13 4 | 32 29 28 31 30 27 28 28 31 30 28
19 | 13 14 13 18 15 3 15 11 8 19 5 | 38 34 32 36 33 30 32 33 31 32 31
20E | 15 10 10 9 15 3 11 9 7 9 3 | 31 28 28 30 32 29 30 31 35 34 30
21 | 11 10 16 11 16 5 11 12 9 14 4 | 45 39 41 42 44 39 40 45 40 41 40
22E | 12 10 9 8 14 3 8 7 6 9 3 | 35 30 30 30 29 30 32 29 33 34 30
23 | 20 12 11 11 23 4 11 14 11 19 5 | 32 28 23 18 22 20 29 19 20 23 20
24 | 10 8 17 11 15 5 8 6 8 12 3 | 28 32 21 29 31 27 34 30 28 30 28
X25E | 60 15 18 12 19 9 --- 17 19 15 9 | 88 50 57 53 52 53 --- 60 53 57 55
X26E | 361 --- 36 60 111 31 --- 32 340 32 24 | 9999 --- 9999 9999 9999 9999 --- 9999 9999 9999 9999
27 | 14 7 14 8 20 6 5 10 6 14 3 | 45 37 40 38 40 38 38 41 38 41 38
28E | 8 10 10 11 16 4 11 7 6 11 3 | 29 36 29 33 32 30 34 33 33 31 31
29 | 13 13 17 14 17 5 14 20 11 16 5 | 38 36 35 39 33 35 37 43 35 40 35
30 | 8 7 13 8 10 4 8 5 4 10 2 | 23 27 23 26 26 24 27 26 26 31 25
31 | 10 13 20 12 17 6 11 15 8 14 4 | 23 35 24 28 32 24 35 30 30 34 27
32E | 38 20 17 11 22 6 16 13 10 19 6 | 73 66 63 63 60 61 65 57 60 59 60
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 11 14 11 17 5 11 11 9 15 |T 41 38 36 37 37 35 37 37 37 40 36
WRMS | 12 11 14 11 16 4 11 9 7 14 |NE 35 35 31 33 34 31 34 33 33 35 32
MEDI | 12 10 14 11 17 4 11 10 8 15 |MD 35 35 32 33 33 32 34 33 35 34 32
Table 3.1864.4 GPS week: 1864 Day: 4 MJD: 57296.000
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 15 8 8 4 7 7 5 17 3 | 27 35 30 30 29 29 33 30 31 38 31
2 | 10 13 14 18 18 7 15 12 9 20 5 | 36 39 34 42 32 37 37 33 37 32 35
3E | 17 11 16 10 15 6 10 9 7 13 4 | 95 98 103 94 92 95 95 94 93 99 96
4 | 8 8 13 9 12 5 7 9 5 12 3 | 35 37 36 38 33 36 36 39 39 36 36
5E | 12 13 9 11 15 6 11 10 10 16 4 | 45 53 49 50 44 50 47 42 47 53 47
6 | 11 10 13 11 15 5 8 12 10 12 4 | 22 32 25 25 25 25 30 23 26 24 25
7 | 11 13 12 10 13 3 9 10 8 16 4 | 31 35 28 30 29 28 34 24 27 28 28
8 | 9 9 12 10 11 3 6 8 5 15 3 | 24 32 26 24 25 26 30 25 27 34 26
9 | 8 10 13 9 12 5 6 6 6 10 3 | 27 36 35 30 22 30 34 27 28 35 30
X10 | 15 14 16 21 15 14 11 22 10 --- 6 | 33 30 33 28 26 31 28 37 28 --- 27
11 | 8 9 15 9 13 5 7 8 7 15 3 | 45 52 46 48 49 46 51 48 47 47 47
12E | 14 11 10 14 25 5 15 16 11 11 5 | 31 35 29 32 32 31 33 27 32 27 29
13 | 10 11 15 11 18 4 13 9 9 12 4 | 29 37 30 30 35 30 36 28 27 29 29
14 | 9 13 18 14 12 6 11 11 10 20 4 | 25 31 26 28 24 23 29 22 21 21 23
15 | 9 11 12 13 18 5 12 10 10 14 4 | 38 42 38 33 30 38 40 29 37 37 35
16E | 23 12 10 15 20 4 13 13 13 16 5 | 31 30 29 29 29 28 27 24 30 24 26
17 | 13 13 15 14 16 4 11 12 10 18 4 | 31 37 32 35 28 32 33 29 31 30 30
18E | 18 9 8 10 15 4 9 9 9 16 4 | 33 33 31 30 25 31 31 28 35 34 30
19 | 11 13 12 16 13 4 12 11 9 21 4 | 29 35 28 32 25 27 33 29 25 29 27
20E | 18 13 10 8 21 4 10 11 9 10 4 | 29 33 26 28 25 30 29 25 32 26 27
21 | 12 10 16 11 15 5 10 14 10 17 4 | 39 41 35 37 38 36 38 37 36 35 36
22E | 7 11 8 9 10 5 9 9 8 11 3 | 31 32 29 27 31 30 32 31 36 31 31
23 | 17 13 10 13 18 4 13 16 10 18 5 | 29 31 24 22 24 24 32 19 21 20 22
24 | 13 12 17 10 15 5 10 8 8 12 4 | 31 34 25 26 29 28 31 28 26 31 27
X25E | 15 15 16 13 16 7 --- 13 9 10 5 | 48 49 52 44 42 45 --- 49 44 42 45
X26E | 86 26 43 12 35 18 --- 9 15 14 9 | 654 869 643 646 639 645 --- 644 644 640 644
27 | 9 9 12 7 18 4 7 9 6 14 3 | 28 34 33 31 30 32 34 32 33 35 31
28E | 10 12 8 11 14 4 8 9 6 12 3 | 30 35 28 27 24 29 30 26 30 27 28
29 | 10 12 16 12 18 6 14 18 12 19 5 | 34 38 34 37 26 34 36 39 32 34 33
30 | 8 8 12 8 13 4 7 7 6 10 3 | 28 34 29 27 31 28 31 28 27 33 28
31 | 9 14 20 13 15 5 12 12 10 19 4 | 25 37 22 27 29 24 33 23 24 27 25
32E | 98 22 15 13 19 11 14 16 13 21 6 | 87 50 39 38 39 38 44 40 34 38 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 22 12 13 11 16 5 10 11 9 15 |T 55 64 53 53 51 53 36 51 52 54 52
WRMS | 11 12 13 12 14 5 10 10 8 15 |NE 30 36 30 31 29 30 34 29 30 31 30
MEDI | 11 12 13 11 15 5 10 10 9 15 |MD 31 35 30 30 29 30 33 29 31 33 30
Table 3.1864.5 GPS week: 1864 Day: 5 MJD: 57297.000
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 9 3 8 6 5 20 3 | 25 30 26 26 29 26 30 27 27 38 27
2 | 13 13 12 14 17 5 12 14 10 20 4 | 29 34 26 34 28 30 32 29 31 28 28
3E | 17 10 12 9 11 4 11 8 8 16 4 | 79 78 82 78 79 79 76 81 78 85 79
4 | 7 9 12 10 11 4 6 9 6 14 3 | 27 29 29 29 30 28 29 32 31 30 28
5E | 15 15 6 14 13 5 15 13 9 14 4 | 35 38 34 39 37 36 39 36 39 42 36
6 | 9 11 12 10 10 4 8 10 9 16 3 | 19 26 17 20 21 18 24 21 19 23 19
7 | 11 11 11 10 12 3 11 14 8 16 4 | 31 32 22 29 24 24 32 24 24 29 25
8 | 6 8 12 11 12 4 6 8 5 19 3 | 22 29 23 21 24 23 28 22 22 34 23
9 | 8 9 12 6 9 4 8 9 6 11 3 | 24 30 27 24 24 23 27 23 24 32 24
X10 | 23 10 20 19 11 21 11 21 16 --- 6 | 33 25 26 25 21 25 25 31 25 --- 22
11 | 8 9 15 13 13 5 10 8 8 19 4 | 35 44 38 42 45 39 42 39 38 38 38
12E | 23 13 8 13 15 6 15 19 13 13 5 | 33 29 26 34 22 27 33 25 31 25 26
13 | 9 12 13 10 17 3 12 11 8 14 4 | 22 32 22 25 32 22 34 23 20 28 24
14 | 9 14 13 13 13 5 10 13 8 21 4 | 22 31 22 26 22 22 28 19 22 20 21
15 | 11 11 11 9 17 4 10 12 8 17 4 | 32 34 28 29 26 27 34 25 27 30 28
16E | 16 11 6 14 19 5 15 13 12 17 4 | 24 26 21 26 24 22 26 24 26 27 22
17 | 12 14 12 14 14 5 15 12 10 18 4 | 27 30 23 27 26 24 31 25 25 28 24
18E | 15 10 6 9 16 6 12 10 7 19 4 | 30 31 27 33 29 28 34 26 30 34 29
19 | 11 13 12 17 13 4 14 13 10 26 5 | 26 30 21 27 24 22 29 25 20 23 22
20E | 24 13 8 9 14 4 8 10 10 9 4 | 33 29 27 32 25 28 32 29 31 30 28
21 | 12 10 14 9 12 6 9 14 9 20 4 | 36 39 32 35 34 33 40 36 35 35 34
22E | 13 10 6 7 12 5 10 7 8 14 3 | 40 40 36 40 39 38 41 37 39 39 38
23 | 14 11 11 16 15 4 12 15 10 16 4 | 26 27 18 20 22 18 27 14 18 17 18
24 | 10 12 15 8 11 3 9 10 8 11 3 | 25 30 25 24 24 24 34 24 27 26 25
25E | 16 15 13 16 16 9 15 9 16 10 5 | 59 57 60 59 51 55 50 56 57 54 56
26E | 26 16 16 22 21 12 13 10 13 13 6 | 9999 715 988 994 987 989 330 989 992 989 989
27 | 8 7 12 7 12 3 7 11 7 14 3 | 23 27 24 23 24 24 28 25 25 27 23
28E | 10 11 7 9 15 4 11 10 6 11 3 | 20 27 19 22 21 20 25 23 22 23 21
29 | 14 15 14 13 13 4 13 23 12 18 5 | 30 33 28 33 23 27 31 36 28 28 27
30 | 7 8 12 9 11 2 7 7 6 12 3 | 22 27 21 23 22 22 27 24 20 28 22
31 | 6 12 14 11 12 6 11 12 9 20 4 | 24 33 20 22 25 23 33 19 24 24 22
32E | 14 40 12 11 19 7 16 31 13 23 7 | 54 65 51 51 48 49 53 66 50 56 52
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 13 12 12 14 5 11 13 9 17 |T 31 55 59 61 59 59 43 60 60 63 59
WRMS | 10 12 12 12 13 5 11 11 8 16 |NE 26 31 24 26 26 24 30 25 25 28 24
MEDI | 11 11 12 10 13 4 11 11 8 16 |MD 27 30 26 27 25 25 32 25 27 29 25
Table 3.1864.6 GPS week: 1864 Day: 6 MJD: 57298.000
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 6 14 8 13 3 6 7 6 14 3 | 30 34 26 32 31 29 33 30 30 40 30
2 | 14 11 13 14 18 5 11 14 10 19 4 | 34 40 32 45 42 38 37 38 37 35 36
3E | 21 10 13 8 14 4 9 8 8 11 4 | 78 82 80 82 77 81 80 80 81 83 80
4 | 8 8 14 7 13 4 5 8 9 10 3 | 36 35 33 37 38 36 36 39 40 37 36
5E | 19 13 8 13 16 3 14 10 9 12 4 | 39 45 38 44 45 41 44 41 43 49 42
6 | 13 7 12 8 16 6 8 15 8 9 3 | 26 28 21 25 28 24 26 28 21 25 23
7 | 12 10 10 9 15 3 12 13 10 13 4 | 33 34 24 31 29 27 32 25 25 29 27
8 | 9 9 13 11 10 4 5 11 8 13 3 | 24 30 22 21 26 22 27 22 22 32 23
9 | 10 8 12 7 11 4 7 9 6 7 3 | 35 38 37 34 29 33 39 30 33 37 34
X10 | 24 12 17 18 12 11 10 17 10 --- 5 | 35 24 23 30 25 23 25 30 26 --- 24
11 | 10 7 16 11 15 5 8 9 7 15 4 | 55 57 51 60 61 56 57 56 56 54 55
12E | 25 9 8 13 20 5 12 17 11 11 5 | 34 30 28 36 28 29 31 27 30 31 28
13 | 8 11 13 12 17 6 12 13 10 8 4 | 22 34 23 33 35 24 33 25 22 24 25
14 | 12 11 13 10 15 4 11 11 13 16 4 | 25 29 24 30 28 23 28 25 24 24 24
15 | 11 11 10 13 21 5 11 12 8 14 4 | 38 41 36 33 31 33 41 31 36 37 35
16E | 18 13 9 11 16 5 15 14 13 12 4 | 30 34 24 30 27 27 29 27 31 27 27
17 | 16 10 12 13 16 4 12 13 13 16 4 | 33 34 28 40 36 33 32 32 32 33 31
18E | 18 9 6 10 21 4 8 9 8 9 4 | 32 34 32 37 31 33 34 32 36 37 33
19 | 10 11 14 15 16 3 13 14 10 18 4 | 31 33 27 37 30 29 33 32 27 30 29
20E | 23 12 8 10 13 4 7 11 10 8 4 | 33 29 26 34 28 30 31 32 34 34 29
21 | 10 10 13 9 12 5 9 14 10 15 4 | 40 45 39 46 46 41 44 45 42 43 42
22E | 14 12 6 9 14 4 8 9 11 8 3 | 32 34 33 34 35 32 36 31 37 39 33
23 | 14 12 10 15 17 4 13 15 11 15 4 | 28 27 19 23 22 19 29 15 17 16 18
24 | 10 8 16 8 13 5 9 11 9 12 3 | 25 28 24 27 28 25 29 26 25 26 25
25E | 13 10 13 14 16 6 10 11 14 10 4 | 47 47 53 51 45 49 39 49 49 47 47
26E | 18 13 18 18 19 6 12 11 14 9 5 | 866 632 847 849 850 849 281 849 853 851 850
27 | 11 12 12 12 13 5 7 7 6 9 3 | 28 29 28 26 29 27 30 29 28 27 26
28E | 18 8 6 10 18 3 10 8 9 11 4 | 29 29 21 24 25 23 26 22 24 21 22
29 | 12 13 12 15 14 5 13 17 10 15 4 | 35 34 31 42 30 33 34 40 33 34 32
30 | 8 7 11 8 15 3 8 10 5 11 3 | 27 31 24 24 29 25 27 24 22 31 25
31 | 7 13 14 13 14 4 10 14 9 15 4 | 28 35 22 29 30 25 34 22 21 29 25
32E | 24 15 14 13 19 5 15 25 13 15 6 | 59 62 56 54 57 57 60 67 59 61 58
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 10 12 11 16 4 10 12 10 13 |T 60 55 57 61 60 58 43 59 59 62 58
WRMS | 12 10 12 11 14 4 10 11 8 12 |NE 31 34 28 33 32 29 33 30 29 32 29
MEDI | 12 10 12 11 15 4 10 11 10 12 |MD 33 34 28 34 30 29 33 30 31 34 29
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 4.1864 GPS week: 1864 MJD: 57292.0-57298.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3051 |U 6 5 13 |U 6 8 27 |U 8 8 15 |
emr | emr 3054 | 8 6 16 |U 8 10 34 | 10 10 19 |
esa | esa 3044 | 6 5 14 |U 8 10 34 | 10 9 19 |
gfz | gfz 3068 |U 6 5 13 |U 8 9 32 |U 9 8 16 |
grg | grg 3072 |U 7 7 17 |U 8 9 36 | 10 10 19 |
igr | igr 3013 | 6 6 14 | 7 9 34 | 9 8 17 |
igs | igs 3059 | 6 5 13 | 7 9 33 | 8 9 15 |
jpl | jpl 2981 | 7 7 16 |U 7 9 31 |U 10 8 17 |
mit | mit 3072 | 11 6 18 |U 9 11 44 |U 9 9 18 |
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 5.1864.0 GPS week: 1864 Day: 0 MJD: 57292.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3048 | 5 4 11 | 5 8 29 | 9 9 14 |
emr | emr 3068 | 6 5 19 | 6 10 33 | 10 10 15 |
esa | esa 3072 | 6 4 13 | 6 9 34 | 11 10 18 |
gfz | gfz 3068 | 5 3 11 | 6 9 34 | 8 8 13 |
grg | grg 3072 | 7 5 17 | 6 10 34 | 9 10 22 |
igr | igr 2974 | 5 4 11 | 5 9 31 | 9 9 14 |
igs | igs 3072 | 5 3 13 | 5 9 28 | 9 9 14 |
jpl | jpl 3067 | 6 5 13 | 6 9 35 | 9 10 14 |
mit | mit 3072 | 6 3 12 | 8 10 37 | 9 9 15 |
Table 5.1864.1 GPS week: 1864 Day: 1 MJD: 57293.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3045 | 6 7 18 | 6 8 23 | 8 8 19 |
emr | emr 3068 | 7 6 15 | 13 14 65 | 12 11 18 |
esa | esa 3072 | 6 6 14 | 14 13 69 | 11 8 20 |
gfz | gfz 3068 | 7 7 15 | 13 12 44 | 10 7 17 |
grg | grg 3072 | 9 9 20 | 13 12 53 | 10 12 17 |
igr | igr 2973 | 6 6 14 | 12 12 64 | 9 8 14 |
igs | igs 3036 | 6 6 14 | 13 11 67 | 9 9 14 |
jpl | jpl 2969 | 8 7 15 | 7 8 29 | 11 9 13 |
mit | mit 3072 | 6 6 16 | 7 8 25 | 8 7 15 |
Table 5.1864.2 GPS week: 1864 Day: 2 MJD: 57294.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3054 | 5 4 10 | 5 8 24 | 8 8 13 |
emr | emr 3068 | 6 5 14 | 5 10 24 | 12 11 19 |
esa | esa 2976 | 5 5 13 | 6 9 30 | 10 9 18 |
gfz | gfz 3068 | 6 6 11 | 5 9 22 | 9 7 14 |
grg | grg 3072 | 7 7 16 | 6 8 30 | 11 13 17 |
igr | igr 3035 | 6 5 12 | 5 9 27 | 10 8 14 |
igs | igs 3071 | 6 4 11 | 5 9 20 | 8 8 13 |
jpl | jpl 2969 | 8 7 15 | 6 9 31 | 13 10 16 |
mit | mit 3072 | 8 6 16 | 13 21 79 | 9 8 16 |
Table 5.1864.3 GPS week: 1864 Day: 3 MJD: 57295.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 6 5 14 | 5 7 29 | 7 9 14 |
emr | emr 2972 | 7 5 19 | 6 8 33 | 9 9 18 |
esa | esa 2976 | 5 4 16 | 6 8 24 | 9 7 16 |
gfz | gfz 3068 | 5 3 14 | 7 8 41 | 8 9 11 |
grg | grg 3072 | 8 5 19 | 6 7 38 | 9 7 17 |
igr | igr 3004 | 5 3 14 | 6 8 34 | 7 6 14 |
igs | igs 3042 | 5 4 15 | 6 7 31 | 7 7 14 |
jpl | jpl 2876 | 6 5 19 | 7 7 28 | 9 6 15 |
mit | mit 3072 | 6 4 17 | 7 8 34 | 8 8 14 |
Table 5.1864.4 GPS week: 1864 Day: 4 MJD: 57296.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3053 | 7 9 14 | 8 10 29 | 7 5 15 |
emr | emr 3068 | 9 7 16 | 9 9 30 | 11 13 26 |
esa | esa 3072 | 7 7 17 | 8 11 31 | 11 12 24 |
gfz | gfz 3068 | 6 7 15 | 8 8 31 | 9 12 18 |
grg | grg 3072 | 8 10 18 | 8 8 34 | 10 12 21 |
igr | igr 3013 | 6 7 15 | 7 9 31 | 9 10 23 |
igs | igs 3066 | 7 7 15 | 8 9 29 | 8 10 18 |
jpl | jpl 2870 | 8 10 18 | 8 9 34 | 10 8 20 |
mit | mit 3072 | 7 6 19 | 13 9 69 | 10 12 21 |
Table 5.1864.5 GPS week: 1864 Day: 5 MJD: 57297.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 6 5 12 | 7 7 27 | 8 7 15 |
emr | emr 3068 | 8 5 15 | 10 12 33 | 9 6 18 |
esa | esa 3072 | 6 4 14 | 8 11 27 | 9 6 21 |
gfz | gfz 3068 | 7 5 12 | 8 9 26 | 8 5 18 |
grg | grg 3072 | 7 5 12 | 8 11 25 | 9 7 20 |
igr | igr 3030 | 9 9 16 | 8 10 28 | 11 9 24 |
igs | igs 3062 | 6 4 11 | 8 10 33 | 8 6 16 |
jpl | jpl 3062 | 7 5 15 | 8 10 36 | 9 5 19 |
mit | mit 3072 | 8 5 16 | 8 11 31 | 9 5 19 |
Table 5.1864.6 GPS week: 1864 Day: 6 MJD: 57298.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 8 4 13 | 6 9 27 | 9 9 17 |
emr | emr 3068 | 11 8 16 | 5 8 23 | 10 12 19 |
esa | esa 3072 | 8 5 13 | 6 9 26 | 10 12 18 |
gfz | gfz 3068 | 8 7 12 | 6 9 27 | 10 10 19 |
grg | grg 3072 | 7 5 16 | 7 9 34 | 11 12 23 |
igr | igr 3064 | 7 7 13 | 6 8 26 | 10 10 17 |
igs | igs 3068 | 7 7 14 | 6 9 26 | 10 11 20 |
jpl | jpl 3060 | 8 9 17 | 5 10 26 | 10 11 19 |
mit | mit 3072 | 41 13 30 | 7 10 32 | 11 13 24 |
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 6.1864 GPS week: 1864 MJD: 57292.500-57298.500
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 | -12 -9 -4 84 -1 | 24 27
| 24 19 121 36 5 | 2
emr uuuux | 8 43 -65 3 34 | 18 27
| 32 22 139 74 23 | 9
esa uuuuu | -18 13 54 -60 -1 | 33 35
| 21 21 65 66 4 | 2
gfz uuuuu | -3 -39 154 -208 0 | 29 31
| 16 14 73 154 2 | 1
grg uuuuu | -19 14 112 88 0 | 25 27
| 32 32 108 48 7 | 2
igr xxxxx | -5 13 31 5 2 | -3 12
| 14 13 48 68 5 | 2
irf xxxxx | 20 -6 -8 16 4 | -1 13
| 11 5 29 19 3 | 2
jpl uuuuu | -13 -6 -35 -36 -5 | 43 47
| 47 29 98 93 24 | 6
mit uuuuu | 22 15 -87 88 4 | 31 34
| 35 18 50 46 3 | 1
ngs uuuuu | -1 -14 -31 14 0 | 19 23
| 51 36 66 172 6 | 2
sio uuuux | 35 -9 -45 91 10 | 91 92
| 27 23 68 73 7 | 4
Table 7.1864.0 GPS week: 1864 Day: 0 MJD: 57292.500
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 -11 80 20 3 | 22 27
emr uuuux | -24 10 160 67 13 | 9 20
esa uuuuu | -1 10 44 1 4 | 33 36
gfz uuuuu | 2 -63 57 -180 3 | 29 32
grg uuuuu | 33 36 -58 50 -7 | 27 29
igr xxxxx | -12 19 -58 -59 -7 | -2 15
irf xxxxx | 11 -5 -59 8 5 | -2 16
jpl uuuuu | -15 -45 -121 -47 -30 | 51 54
mit uuuuu | -31 8 -82 59 2 | 30 34
ngs uuuuu | 37 49 1 -7 4 | 16 22
sio uuuux | 1 5 -106 86 2 | 83 86
Table 7.1864.1 GPS week: 1864 Day: 1 MJD: 57293.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -20 -29 -45 138 6 | 25 29
emr uuuux | 2 56 17 39 18 | 12 22
esa uuuuu | 5 33 48 60 -1 | 35 38
gfz uuuuu | 11 -17 64 -243 2 | 31 34
grg uuuuu | 4 17 151 36 -2 | 27 29
igr xxxxx | 14 8 19 -49 6 | -2 15
irf xxxxx | 8 -5 -40 8 2 | -1 16
jpl uuuuu | -85 -36 -38 -152 -34 | 50 53
mit uuuuu | 11 -2 -144 79 0 | 32 35
ngs uuuuu | 41 16 16 -19 4 | 19 24
sio uuuux | 25 -50 -15 154 12 | 87 89
Table 7.1864.2 GPS week: 1864 Day: 2 MJD: 57294.500
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 | -35 -7 -30 71 1 | 24 29
emr uuuux | -8 45 -150 13 12 | 13 23
esa uuuuu | -26 7 161 -75 -2 | 34 37
gfz uuuuu | -2 -41 221 -112 -2 | 29 32
grg uuuuu | -16 28 188 92 -7 | 25 27
igr xxxxx | -1 -8 45 -75 2 | -3 14
irf xxxxx | 24 -2 11 23 7 | -1 16
jpl uuuuu | -34 -6 -103 -163 -21 | 45 50
mit uuuuu | 29 13 -89 176 7 | 30 34
ngs uuuuu | 26 -27 -68 -71 7 | 18 23
sio uuuux | 38 11 10 140 0 | 90 91
Table 7.1864.3 GPS week: 1864 Day: 3 MJD: 57295.500
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 | -19 -32 197 86 -7 | 27 29
emr uuuux | 50 14 -13 102 22 | 16 24
esa uuuuu | -58 41 -3 -108 -4 | 35 37
gfz uuuuu | 4 -36 232 -34 -3 | 30 33
grg uuuuu | -44 24 81 124 1 | 24 27
igr xxxxx | -14 32 72 36 1 | -2 14
irf xxxxx | 8 0 10 38 4 | 1 14
jpl uuuuu | 74 -8 -161 -41 5 | 42 48
mit uuuuu | 7 42 -26 120 6 | 32 35
ngs uuuuu | -52 -21 -120 -145 3 | 21 24
sio uuuux | 27 -4 -62 -10 6 | 93 93
Table 7.1864.4 GPS week: 1864 Day: 4 MJD: 57296.500
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 | -15 -9 -6 97 -6 | 22 23
emr uuuux | 58 56 -50 -27 65 | 15 22
esa uuuuu | -4 26 86 -78 -5 | 31 32
gfz uuuuu | 2 -39 181 -92 -3 | 26 28
grg uuuuu | -66 -47 232 57 10 | 22 24
igr xxxxx | -25 18 85 85 7 | -6 9
irf xxxxx | 32 -7 5 40 7 | -3 10
jpl uuuuu | -4 27 56 47 -2 | 37 40
mit uuuuu | 75 37 -145 82 6 | 29 30
ngs uuuuu | -89 -59 -93 -133 -2 | 19 21
sio uuuux | 75 14 -132 154 16 | 90 91
Table 7.1864.5 GPS week: 1864 Day: 5 MJD: 57297.500
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 | -27 23 -26 100 2 | 23 24
emr uuuux | -15 65 -268 -105 59 | 24 35
esa uuuuu | -19 -12 79 -116 1 | 32 33
gfz uuuuu | -1 -40 121 -311 0 | 27 29
grg uuuuu | -21 -11 188 79 -4 | 25 26
igr xxxxx | -8 5 51 5 6 | -4 8
irf xxxxx | 32 -9 10 8 6 | 0 9
jpl uuuuu | -21 35 96 65 22 | 36 39
mit uuuuu | 56 3 -103 52 4 | 31 32
ngs uuuuu | -1 -39 -25 130 -8 | 20 22
sio uuuux | 67 -6 -70 123 17 | 94 94
Table 7.1864.6 GPS week: 1864 Day: 6 MJD: 57298.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 38 6 -198 74 -5 | 25 26
emr uuuux | -7 56 -153 -65 46 | 36 46
esa uuuuu | -22 -10 -40 -101 3 | 34 35
gfz uuuuu | -39 -35 199 -484 0 | 28 30
grg uuuuu | -20 49 1 175 6 | 26 27
igr xxxxx | 12 19 5 90 0 | -1 9
irf xxxxx | 23 -14 8 -13 -2 | 3 10
jpl uuuuu | -9 -7 27 36 25 | 39 43
mit uuuuu | 9 2 -21 47 1 | 33 34
ngs uuuuu | 33 -16 68 344 -10 | 22 23
sio uuuux | 14 -30 61 -11 17 | 97 98
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