[IGSREPORT-24199] Wk 1879 IGS Final Orbits
IGS ACC
acc at igs.org
Thu Jan 28 14:06:21 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1879 (Jan 10, 2016 - Jan 16, 2016)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1879[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1879[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1879[0-6].cls IGS GPS clock combination summary report.
igs18797.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18797.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 | NICO
0 | ESA | POHN TIXI
0 | GFZ | ARTU TONG ARTU TONG
0 | GRG | 10 10 INVK KIT3 NICO POTS REUN INVK KIT3 POHN REUN
0 | JPL | TUVA
0 | MIT | INVK INVK NICO
1 | ALL | 10
1 | COD | INVK ZAMB INVK ZAMB
1 | ESA | BRAZ BRAZ POHN
1 | GFZ | POHN TONG TONG
1 | GRG | NRMD NRMD POHN
1 | JPL | INVK TUVA
1 | MIT | KARR KARR
2 | ALL | 10 10
2 | COD | MATE
2 | EMR | 1 2 3 5 6 7 8 9 11 12 13 14 15 16 17 18 19 20 21
2 | EMR | 22 23 24 25 26 27 28 29 30 31 32 1 2 3 5 6 7 8 9
2 | EMR | 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27
2 | EMR | 28 29 30 31 32
2 | ESA | HOFN KARR ONSA HOFN KARR ONSA POHN
2 | GFZ | MATE TONG
2 | GRG | DGAR HOFN DGAR HOFN POHN REUN SYOG
2 | JPL | TUVA
3 | COD | HOLM HOLM
3 | ESA | POHN
3 | GFZ | TONG TONG
3 | GRG | 10 10 ARTU INVK NRMD REUN ARTU INVK NRMD REUN
3 | JPL | 21 PARC
4 | GFZ | 13 GLSV TONG GLSV TONG
4 | GRG | 10 10 DRAG GLSV NRMD DRAG GLSV INVK NRMD REUN
4 | MIT | BRAZ BRAZ INVK
5 | ALL | 10 10
5 | COD | MAL2 MATE
5 | GFZ | TONG
5 | GRG | MAC1 DARW MAC1
5 | JPL | TUVA
6 | ALL | 10
6 | COD | MDVJ VILL VILL
6 | ESA | ARTU
6 | GFZ | SYOG MDVJ SYOG TONG
6 | GRG | 6 ARTU REUN REUN
6 | JPL | TUVA
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G28 | 2016_01_15 | 2016005
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G28 | | | | | | 4 | |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .3 -2.1 -1.7 -47 4 -13 .76
EMR | 0 | 4.6 1.7 15.9 -22 3 17 .34
ESA | 0 | -.2 -1.8 -.1 -43 -41 13 .36
GFZ | 0 | .5 -1.0 -1.3 -63 -96 -35 .54
GRG | 0 | 9.6 -2.1 -11.3 -13 12 57 1.27
JPL | 0 | 7.7 -1.3 14.2 16 18 6 1.00
MIT | 0 | 5.9 -5.1 6.2 -1 -4 -25 .72
NGS | 0 | 5.6 -4.1 9.2 -79 -25 13 .58
SIO | 0 | 4.6 -8.6 12.9 -22 -19 -20 .39
COD | 1 | -.4 -1.8 -.5 -43 -16 -1 .58
EMR | 1 | 3.3 -5.7 13.7 -8 -2 43 .62
ESA | 1 | .4 -1.0 .7 -8 -49 34 .43
GFZ | 1 | .3 -1.3 -.9 -51 -85 -18 .73
GRG | 1 | 4.5 -6.6 -15.0 6 19 40 .92
JPL | 1 | 3.8 .4 5.2 -11 21 -20 .39
MIT | 1 | 3.3 -2.2 5.7 48 13 -26 .97
NGS | 1 | 2.6 -3.5 6.0 -28 -42 8 .75
SIO | 1 | 1.6 -8.1 12.0 27 -31 -5 .79
COD | 2 | -.3 -1.9 -.9 -46 -24 -17 .53
EMR | 2 | -.9 -8.7 15.7 -4 -15 31 .56
ESA | 2 | -.2 -1.4 -.1 -37 -43 26 .40
GFZ | 2 | .5 -1.5 -1.3 -59 -100 -6 .56
GRG | 2 | 3.1 -4.6 -13.6 9 8 58 .60
JPL | 2 | -5.7 -2.3 1.7 -16 46 -1 .70
MIT | 2 | 1.5 -5.0 4.0 23 19 -52 .77
NGS | 2 | .7 -.1 1.4 -4 -9 7 .71
SIO | 2 | -.4 -8.2 6.5 8 -47 -3 .76
COD | 3 | -1.3 -1.8 -1.8 -44 -13 12 .63
EMR | 3 | 7.7 .3 13.0 -9 -6 34 .63
ESA | 3 | -.3 -.9 -.1 -28 -47 36 .28
GFZ | 3 | .8 -1.0 -1.5 -46 -97 -12 .68
GRG | 3 | 5.6 -4.4 -15.9 -13 29 60 .88
JPL | 3 | 6.1 -.6 4.4 -20 13 32 .59
MIT | 3 | 6.2 -1.4 4.3 35 2 -35 1.01
NGS | 3 | 3.5 .9 10.8 -62 -40 30 .85
SIO | 3 | -1.9 -2.8 6.4 -5 -25 -45 .77
COD | 4 | -1.1 -1.3 -1.4 -44 -7 13 .52
EMR | 4 | 2.3 -.0 9.8 -10 -8 49 .52
ESA | 4 | -.5 -1.2 -1.2 -33 -22 4 .24
GFZ | 4 | .5 -1.6 -1.3 -64 -96 2 .56
GRG | 4 | 7.2 2.2 -17.2 -23 11 72 1.07
JPL | 4 | 1.3 .4 -2.5 19 7 4 .69
MIT | 4 | 1.7 2.3 4.1 8 9 0 .94
NGS | 4 | 1.3 .9 2.8 -31 13 2 .81
SIO | 4 | -2.1 -2.0 -5.9 -14 -32 -11 .82
COD | 5 | -.8 -1.8 -2.9 -21 -11 -19 .84
EMR | 5 | 1.5 1.6 17.9 4 -21 1 .81
ESA | 5 | .3 -1.3 -.5 -23 -43 53 .57
GFZ | 5 | .9 -1.9 -1.5 -74 -104 -18 .72
GRG | 5 | 5.4 -2.2 -13.9 -30 -1 62 1.22
JPL | 5 | 1.9 5.7 4.5 -30 -10 11 .88
MIT | 5 | 2.1 3.4 7.3 33 10 -31 1.02
NGS | 5 | 2.8 2.3 8.8 -33 -23 12 .68
SIO | 5 | .6 -.5 .0 -17 -24 -10 .73
COD | 6 | -.6 -1.8 -2.1 -34 -18 6 .66
EMR | 6 | 6.2 -1.9 24.3 -15 2 15 .81
ESA | 6 | .3 -1.4 -.9 -31 -33 42 .61
GFZ | 6 | .1 -1.1 -1.0 -54 -75 -6 .77
GRG | 6 | 5.8 -2.8 -21.7 -20 -10 36 1.14
JPL | 6 | -.1 -2.2 8.6 22 28 -5 .78
MIT | 6 | 2.7 2.8 5.7 17 4 -23 .85
NGS | 6 | -.9 -2.5 7.4 -51 -7 -32 .74
SIO | 6 | .1 .4 .6 -14 -13 8 .94
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.1879.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1879.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 2.1879.[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 3.1879.[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 5.1879.0-6). 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 1879 summary. (Jan 10, 2016 - Jan 16, 2016)
Table 1.1879.a GPS week: 1879 MJD: 57397.000-57403.000
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| 0 1 3 1 4 -3 -.01 11 11 | -756 -434 13 143
| 0 0 2 14 17 18 .04 | 76 208
emr 80| 0 -1 4 3 -33 -11 .20 11 11 | 4143 -117 15 150
| 0 0 0 15 14 15 .01 | 5833 764
esa 150| 0 0 4 -5 -8 23 -.32 11 11 | 264 -736 9 152
| 0 0 0 15 18 12 .04 | 386 880
gfz 207| 0 -1 -3 11 -2 3 .06 11 10 | -224 98 9 96
| 0 0 1 13 5 17 .03 | 201 331
grg 118| 2 3 -7 -21 45 26 -.06 17 17 | -115 -25 14 205
| 1 0 2 18 24 12 .03 | 132 170
igr n/a| 0 0 0 2 20 -3 -.01 4 4 | 6280 -628 14 76
| 0 0 1 20 10 9 .01 | 1400 643
jpl 80| 0 0 6 4 28 9 .18 11 11 | 4419 -108 15 116
| 0 0 1 25 14 22 .02 | 352 649
mit 349| 0 -1 -7 14 -6 -20 -.15 12 11 | 70 -160 44 350
| 0 0 0 38 23 8 .02 | 129 193
ngs 220| -1 0 0 -21 6 -4 .03 9 8 | -769 -439 844 1983
| 0 0 1 27 21 13 .05 | 87 224
sio 298| 0 -2 -3 4 -19 -9 -.02 14 14 | --- --- --- ---
| 0 0 1 39 38 21 .05 | --- ---
Table 1.1879.b GPS week : 1879 MJD: 57397.000-57403.000
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 3 4 3 3 |
2 | 5 4 4 4 4 5 5 |
3 | 3 4 4 4 4 4 4 |
5 | 4 4 5 4 4 4 5 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 4 4 4 4 3 |
9 | 4 4 3 4 3 3 4 |
10 | 12 13 13 12 11 12 13 |
11 | 3 3 4 4 4 4 4 |
12 | 5 4 5 4 5 5 5 |
13 | 5 5 5 5 5 5 5 |
14 | 4 4 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 4 5 5 5 5 5 5 |
17 | 5 4 5 5 4 4 4 |
18 | 5 5 5 5 5 5 5 |
19 | 5 4 5 5 4 4 5 |
20 | 5 4 5 5 5 4 5 |
21 | 4 4 4 4 4 4 4 |
22 | 5 5 5 5 5 5 5 |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 4 5 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 3 3 4 4 4 4 3 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 0 5 |
29 | 5 5 5 5 6 5 5 |
30 | 5 4 4 4 4 4 4 |
31 | 3 4 4 4 4 4 4 |
32 | 4 4 4 3 4 4 3 |
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 2.1879.0 GPS week: 1879 Day: 0 MJD: 57397.000
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 1 0 4 28 -19 -.03 11 11 | -840 -410 14 127
emr 80| 0 -1 6 13 -49 16 .20 12 12 | 6794 -1275 19 166
esa 150| 0 0 3 -10 -7 29 -.39 11 11 | 461 -1455 10 137
gfz 208| 0 0 -2 12 -11 -13 .10 10 10 | -374 -220 9 77
grg 123| 1 2 -3 -23 49 19 -.04 16 16 | 14 -249 14 174
igr n/a| 0 0 -2 -12 27 0 -.02 4 4 | 8465 -1538 14 67
jpl 80| 0 0 7 21 9 4 .17 10 10 | 4533 -761 15 112
mit 350| 1 -1 -8 3 -1 -15 -.19 13 12 | 218 -462 48 345
ngs 223| 0 0 0 -28 0 0 .06 8 7 | -839 -415 690 1765
sio 297| 0 -2 -5 10 -4 2 -.05 14 15 | --- --- --- ---
Table 2.1879.1 GPS week: 1879 Day: 1 MJD: 57398.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| -1 1 3 -13 17 -30 -.05 11 11 | -788 -570 13 138
emr 80| 1 0 4 9 -35 -14 .21 12 12 | 5641 704 19 190
esa 150| 0 1 5 8 -17 12 -.35 11 11 | 515 -1519 10 149
gfz 207| 0 -1 -2 27 0 0 .05 10 10 | -336 580 9 75
grg 116| 2 2 -8 -24 43 20 -.07 18 18 | -283 145 14 210
igr n/a| 0 0 0 -14 1 -14 .00 4 4 | 7101 21 13 63
jpl 80| 0 0 6 -31 45 36 .15 10 10 | 3973 967 15 100
mit 350| 0 -2 -7 6 -11 -21 -.14 13 12 | -145 -9 48 333
ngs 219| 0 0 0 -1 -2 2 .09 8 7 | -824 -502 971 1974
sio 296| 0 -1 -5 3 -21 -9 -.06 13 13 | --- --- --- ---
Table 2.1879.2 GPS week: 1879 Day: 2 MJD: 57399.000
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 240| 0 1 7 -14 17 -5 -.05 11 10 | -638 -607 13 168
emr 80| 0 -1 4 4 -11 -1 .19 13 13 | -9058 477 0 0
esa 150| 0 0 3 -27 -8 9 -.31 12 12 | 355 -707 10 167
gfz 206| 1 -1 -2 -6 0 -14 .02 10 10 | -245 140 9 157
grg 116| 1 3 -5 -35 44 31 -.11 17 17 | -126 72 15 225
igr n/a| 0 0 0 12 25 -18 -.01 4 4 | 6671 -94 14 97
jpl 80| 1 1 5 40 12 -19 .20 13 13 | 4447 376 16 126
mit 349| 0 -1 -7 59 -27 -29 -.11 12 11 | 99 -263 46 350
ngs 221| -1 0 -3 -40 24 8 .07 8 8 | -708 -557 667 1734
sio 300| -1 -1 -2 43 -50 14 .04 14 14 | --- --- --- ---
Table 2.1879.3 GPS week: 1879 Day: 3 MJD: 57400.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 243| 0 2 5 1 -15 21 -.04 11 11 | -805 -230 14 153
emr 80| 1 -1 4 23 -31 -17 .19 11 11 | 6262 -167 17 180
esa 150| 0 0 4 0 -33 12 -.30 12 12 | 571 -658 9 156
gfz 205| -1 -2 -3 16 -6 -5 .03 11 10 | -77 -402 9 79
grg 117| 3 3 -6 -44 93 34 -.08 17 16 | -38 -27 15 204
igr n/a| 0 0 0 40 17 2 -.03 4 4 | 6906 -1423 15 102
jpl 80| 0 0 4 16 25 36 .19 10 10 | 5099 -739 15 133
mit 350| 0 -1 -7 -54 41 -35 -.15 12 11 | 9 97 45 325
ngs 218| -2 1 -1 19 -35 -2 .02 10 9 | -812 -225 784 1770
sio 298| 0 -2 -1 -48 20 -22 .06 14 14 | --- --- --- ---
Table 2.1879.4 GPS week: 1879 Day: 4 MJD: 57401.000
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| 0 1 2 19 -10 16 .01 10 10 | -794 -99 12 139
emr 80| 0 -1 3 -20 -52 -13 .23 11 11 | 6164 245 16 155
esa 150| 0 0 4 -11 24 22 -.29 12 12 | 412 -1630 9 147
gfz 208| 0 -1 -4 1 -6 31 .07 11 10 | -523 349 10 83
grg 120| 3 3 -6 14 45 20 -.02 18 17 | -262 -34 15 227
igr n/a| 0 0 0 4 32 -5 -.04 4 4 | 5444 -674 14 73
jpl 80| 1 0 5 -8 42 -10 .18 12 12 | 4391 -126 15 115
mit 349| 1 -1 -6 55 -4 -11 -.14 12 11 | 148 -209 40 359
ngs 219| -1 0 1 -65 20 -31 .01 9 9 | -790 -109 1182 2420
sio 295| 0 -3 -1 42 -42 -24 -.05 15 14 | --- --- --- ---
Table 2.1879.5 GPS week: 1879 Day: 5 MJD: 57402.000
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 3 20 7 -2 .04 12 12 | -772 -451 15 143
emr 80| 1 -2 3 6 -25 -20 .20 10 10 | 6553 248 16 177
esa 150| 1 0 6 16 0 41 -.31 11 11 | 69 167 9 155
gfz 208| -1 0 -5 28 -2 2 .10 11 10 | -50 50 11 117
grg 119| 3 4 -10 -13 14 50 -.04 18 18 | -173 164 15 196
igr n/a| 0 0 0 3 28 3 -.00 4 4 | 4742 -64 14 59
jpl 80| 0 0 5 -22 38 19 .15 10 10 | 4177 136 16 117
mit 350| 1 0 -7 9 -21 -16 -.15 13 12 | -22 -17 44 357
ngs 219| -1 0 1 -14 27 -9 -.01 8 8 | -814 -474 822 2058
sio 301| 0 -3 -4 -49 -70 -41 -.06 14 13 | --- --- --- ---
Table 2.1879.6 GPS week: 1879 Day: 6 MJD: 57403.000
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 241| 0 3 2 -3 -13 -5 .05 11 11 | -660 -672 14 139
emr 80| 0 0 4 -12 -28 -32 .20 11 11 | 6645 -1051 19 184
esa 150| 0 0 5 -16 -19 35 -.28 11 11 | -530 644 9 157
gfz 208| 0 -1 -3 2 4 21 .10 11 11 | 36 194 9 86
grg 120| 0 2 -11 -22 27 11 -.03 18 18 | 57 -249 15 204
igr n/a| 0 0 0 -16 13 8 .00 4 4 | 4636 -628 14 73
jpl 80| 2 0 7 15 23 0 .19 12 12 | 4316 -613 15 109
mit 350| 0 0 -7 20 -20 -14 -.13 12 11 | 187 -262 42 386
ngs 222| -1 0 0 -17 10 2 -.04 9 8 | -596 -795 798 2160
sio 304| -1 -3 -4 28 35 13 -.01 13 13 | --- --- --- ---
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 3.1879.0 GPS week: 1879 Day: 0 MJD: 57397.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 14 11 9 12 4 9 11 7 13 3 | 22 28 27 19 25 21 26 23 19 33 23
2 | 11 13 9 10 16 4 13 17 10 13 4 | 41 40 34 38 40 37 40 41 35 40 38
3 | 9 9 13 7 10 5 8 8 7 10 3 | 27 37 25 28 33 27 34 31 29 35 29
5 | 8 11 13 11 15 5 11 18 10 15 4 | 48 52 46 47 38 47 51 38 48 47 46
6 | 9 9 13 10 16 4 8 9 7 13 3 | 27 31 32 23 26 26 30 23 26 26 26
7E | 9 11 4 8 21 5 11 9 8 12 3 | 21 28 18 25 23 22 25 23 26 18 21
8 | 10 12 13 9 13 4 9 13 6 10 3 | 35 36 36 32 33 34 36 30 33 36 33
9 | 9 9 15 10 13 2 7 10 4 12 3 | 25 33 24 24 28 25 32 29 26 27 26
X10 | 22 20 20 --- 44 8 20 26 43 --- 12 | 19 26 20 --- 58 21 26 17 53 --- 25
11E | 9 12 8 6 13 5 8 11 6 6 3 | 20 28 17 18 23 18 21 23 17 20 19
12 | 16 11 10 12 19 3 10 14 10 13 4 | 25 26 16 23 24 20 24 18 21 20 20
13 | 8 17 14 12 20 3 12 14 7 12 4 | 27 40 27 38 44 31 39 33 32 33 32
14 | 12 10 13 11 15 4 10 14 8 17 4 | 28 31 26 37 36 32 31 37 29 30 30
15 | 12 14 13 14 16 4 14 17 9 22 5 | 44 49 44 41 39 41 49 39 38 46 41
16 | 12 11 9 11 17 4 9 11 9 21 4 | 25 24 19 22 23 19 23 17 18 15 18
17 | 12 12 9 12 20 3 13 15 9 13 4 | 25 32 18 26 26 22 29 19 23 20 22
18 | 14 10 11 11 16 4 10 13 9 20 4 | 27 25 23 26 27 23 22 30 24 29 24
19 | 13 12 7 15 19 3 12 14 8 13 4 | 25 28 19 23 24 21 28 22 22 18 21
20 | 11 11 12 11 20 4 11 14 8 20 4 | 30 27 25 37 33 31 27 35 28 38 29
21 | 16 12 7 9 19 4 11 12 7 13 4 | 28 25 20 24 28 23 25 27 21 24 23
22 | 10 10 12 9 15 5 8 22 9 22 4 | 30 31 28 32 32 30 28 35 26 35 28
23 | 7 10 13 10 14 4 10 12 8 19 4 | 24 29 23 25 24 22 26 22 21 15 21
24E | 12 10 14 8 17 4 8 10 7 11 3 | 22 25 28 23 27 23 23 25 22 25 23
X25 | 8 12 14 9 12 7 11 8 10 --- 4 | 20 27 25 22 24 22 25 18 18 --- 21
26 | 8 12 12 7 12 4 8 10 7 8 3 | 24 30 28 22 24 24 26 21 25 25 24
27 | 10 12 14 9 11 4 10 9 7 10 3 | 26 30 30 25 22 24 26 22 24 24 25
28 | 11 11 11 10 17 5 8 12 8 9 3 | 22 30 18 22 26 21 27 20 20 17 22
29 | 14 17 6 10 20 3 14 11 9 18 4 | 31 25 18 23 23 22 26 19 23 30 22
X30E | 11 14 15 8 17 6 10 10 11 --- 4 | 26 25 27 22 26 21 23 25 22 --- 21
31E | 8 11 7 8 10 5 9 12 7 11 3 | 28 26 23 29 26 28 27 26 27 31 26
32 | 12 10 8 6 11 3 8 16 6 11 3 | 27 23 22 25 25 22 25 14 23 16 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 11 10 16 4 10 13 8 14 |T 27 30 25 27 29 25 29 25 26 27 25
WRMS | 11 12 11 10 16 4 10 12 7 15 |NE 27 31 25 27 29 26 29 25 26 27 26
MEDI | 11 11 12 10 16 4 10 12 8 13 |MD 26 28 25 25 26 23 26 23 24 26 24
Table 3.1879.1 GPS week: 1879 Day: 1 MJD: 57398.000
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 | 13 10 11 9 16 4 8 9 6 12 3 | 19 24 25 20 22 21 23 22 19 29 21
2 | 11 13 6 9 18 4 10 15 8 12 4 | 44 43 39 44 44 41 43 42 40 41 41
3 | 10 8 12 14 16 5 9 9 7 17 4 | 22 29 18 21 29 20 29 24 23 33 22
5 | 6 12 13 8 16 4 10 16 9 14 4 | 31 39 31 34 29 32 37 30 37 37 33
6 | 9 9 11 8 19 2 8 8 9 11 3 | 27 27 31 22 25 25 27 23 25 26 25
7E | 11 13 4 12 16 4 13 13 8 8 4 | 26 27 22 31 20 25 25 22 27 24 23
8 | 13 10 11 10 12 3 9 12 6 7 3 | 28 32 30 25 23 26 29 25 26 31 26
9 | 10 9 15 8 13 3 10 8 8 10 3 | 23 29 21 22 25 22 29 23 23 22 22
X10 | 19 19 20 --- 43 8 19 27 47 --- 12 | 16 24 19 --- 40 18 23 14 40 --- 20
11E | 10 8 7 5 16 3 9 10 6 6 3 | 14 19 12 16 20 15 20 18 17 15 15
12 | 12 14 10 13 21 5 11 14 7 13 4 | 25 27 14 23 25 20 23 16 20 13 18
13 | 8 15 15 11 21 4 14 16 8 13 4 | 22 35 21 27 34 25 34 25 25 23 25
14 | 11 13 13 11 14 4 11 15 11 13 4 | 22 26 19 28 23 21 24 28 23 21 21
15 | 8 15 13 13 15 5 17 18 10 19 5 | 30 35 30 31 25 28 35 24 28 28 28
16 | 17 11 10 12 19 3 10 12 9 20 4 | 27 23 15 19 20 16 20 16 18 14 15
17 | 9 13 7 11 21 3 11 10 9 11 4 | 24 29 16 25 27 21 28 16 25 18 21
18 | 15 12 12 13 16 5 9 13 8 17 4 | 22 21 19 24 19 18 19 21 20 20 18
19 | 10 15 6 14 23 3 11 11 9 10 4 | 21 25 15 23 24 19 24 19 22 15 18
20 | 9 12 12 11 17 6 12 15 7 16 4 | 22 25 21 29 22 22 22 27 24 29 23
21 | 18 11 6 11 18 3 11 13 7 10 4 | 29 28 22 27 28 24 24 27 25 26 24
22 | 11 11 14 9 18 4 9 23 9 18 4 | 20 24 20 21 23 19 22 24 19 20 17
23 | 6 10 14 9 17 4 9 9 10 19 4 | 22 27 20 24 21 20 25 19 22 12 18
24E | 12 14 14 11 23 4 9 10 9 10 4 | 23 25 29 24 31 23 21 25 22 23 23
25 | 8 11 13 7 17 4 10 14 6 11 3 | 21 27 26 22 26 21 24 22 20 18 21
26 | 8 10 12 6 15 3 10 9 7 8 3 | 24 29 26 23 25 23 25 22 23 26 23
27 | 9 13 14 7 16 2 10 8 8 9 3 | 23 28 27 22 21 22 24 21 22 24 22
28 | 9 11 8 11 20 2 9 12 8 8 3 | 22 27 18 22 26 19 25 19 19 16 20
29 | 14 12 7 14 20 3 13 12 10 13 4 | 29 25 17 25 22 22 25 17 24 22 21
30E | 13 15 14 9 18 5 10 10 9 7 4 | 27 28 28 26 22 23 23 24 24 23 23
31E | 10 9 7 8 12 3 9 17 7 8 3 | 21 22 17 26 22 22 23 20 23 23 20
32 | 8 11 8 6 18 4 8 14 6 10 3 | 18 23 16 17 15 18 20 18 17 18 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 11 10 18 4 10 13 8 13 |T 24 27 22 24 25 22 25 22 23 23 22
WRMS | 11 12 11 10 18 4 10 12 7 13 |NE 23 27 21 24 24 21 25 21 23 22 21
MEDI | 10 12 12 10 17 4 10 12 8 11 |MD 23 27 21 24 24 22 24 22 23 23 21
Table 3.1879.2 GPS week: 1879 Day: 2 MJD: 57399.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 11 12 8 17 4 14 9 5 9 3 | 21 24 25 19 23 19 25 20 19 27 20
2 | 11 14 6 9 17 2 17 13 8 13 4 | 42 43 35 44 38 40 42 41 41 43 40
3 | 8 10 13 11 12 5 9 9 7 16 3 | 27 33 22 23 29 24 31 27 28 36 26
5 | 6 13 14 12 17 5 15 14 11 14 4 | 37 40 34 36 29 34 42 33 37 39 35
6 | 7 10 12 9 19 3 10 9 7 15 3 | 27 27 32 24 26 26 31 23 24 29 25
7E | 13 13 5 10 17 5 13 10 9 8 4 | 23 24 19 29 23 23 27 22 28 19 22
8 | 8 9 11 9 13 5 12 10 9 13 3 | 30 33 34 28 30 30 33 26 33 33 30
9 | 8 9 13 8 11 3 10 8 7 13 3 | 24 30 22 24 27 23 32 24 25 24 24
X10 | 21 20 19 --- 48 8 21 26 46 --- 12 | 16 23 18 --- 49 18 22 15 44 --- 20
11E | 8 17 10 7 16 6 12 12 6 10 3 | 18 21 16 18 22 15 21 19 16 19 16
12 | 11 11 12 12 20 3 13 13 8 14 4 | 25 25 18 24 26 21 26 18 20 21 20
13 | 8 18 16 12 21 4 17 16 8 12 5 | 23 38 22 30 37 25 36 29 28 27 27
14 | 10 11 14 12 16 5 12 14 10 18 4 | 22 26 21 30 28 22 26 29 23 24 22
15 | 9 16 13 14 16 3 18 18 9 18 5 | 37 41 37 36 31 34 41 30 33 38 33
16 | 18 10 9 10 19 4 10 13 8 20 4 | 27 21 17 18 25 17 23 18 19 14 17
17 | 8 18 8 13 22 3 16 10 9 11 4 | 23 30 19 27 28 22 31 19 27 20 22
18 | 10 12 12 13 14 3 14 11 11 19 4 | 18 22 20 24 21 19 23 22 24 22 19
19 | 10 17 8 16 23 4 15 11 9 11 4 | 24 28 20 25 26 22 31 25 27 19 22
20 | 10 13 12 10 16 4 13 14 11 15 4 | 24 27 24 33 26 24 27 32 28 33 26
21 | 12 11 9 10 17 3 14 10 8 10 4 | 24 23 21 25 27 22 26 24 25 23 22
22 | 13 9 13 11 17 5 10 22 10 19 5 | 21 26 22 25 27 21 25 25 22 24 21
23 | 12 10 14 11 14 3 11 9 10 17 4 | 23 25 22 25 23 20 26 19 22 13 19
24E | 12 12 12 9 19 3 10 9 9 9 3 | 21 20 27 22 28 21 22 25 20 24 21
25 | 9 10 15 6 14 5 10 10 7 13 3 | 17 22 22 17 22 17 22 16 17 20 17
26 | 12 10 14 8 16 3 11 8 7 7 3 | 23 27 29 20 25 22 25 20 23 25 22
27 | 8 11 13 9 15 4 15 9 9 13 4 | 22 25 27 20 22 21 28 18 23 23 21
28 | 8 17 9 9 20 3 11 12 8 11 4 | 22 28 19 22 25 19 27 17 18 18 20
29 | 15 17 9 15 20 3 17 13 10 18 5 | 26 23 16 22 21 18 24 16 21 23 18
30E | 14 16 12 7 19 5 13 10 7 9 4 | 20 29 27 22 22 20 25 24 22 21 20
31E | 18 9 8 10 13 4 9 16 8 11 4 | 24 21 16 25 21 20 24 19 21 27 19
32 | 10 10 8 6 20 3 9 15 6 11 3 | 20 19 17 16 25 16 19 10 18 13 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 13 12 10 17 4 13 12 8 14 |T 24 27 23 25 26 22 27 22 25 24 22
WRMS | 10 13 12 10 17 4 13 11 8 14 |NE 24 27 23 24 27 22 28 22 25 24 22
MEDI | 10 11 12 10 17 4 13 11 8 13 |MD 23 26 22 24 26 21 26 22 23 23 21
Table 3.1879.3 GPS week: 1879 Day: 3 MJD: 57400.000
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 11 7 12 4 8 6 8 14 3 | 23 27 26 21 19 21 25 19 24 33 23
2 | 12 11 5 9 20 3 12 11 9 13 4 | 51 49 46 50 50 48 48 48 48 49 48
3 | 8 8 12 13 11 6 8 10 6 15 3 | 27 33 23 27 28 25 33 27 28 35 27
5 | 5 11 12 10 18 4 10 12 11 14 4 | 44 47 40 39 31 39 44 36 44 42 40
6 | 11 7 12 7 18 4 8 7 7 11 3 | 33 32 35 27 26 29 30 24 29 29 28
7E | 13 13 6 9 20 4 11 9 12 10 4 | 30 31 26 31 24 29 31 23 33 27 27
8 | 10 9 12 5 9 4 8 11 10 11 3 | 37 36 37 30 30 32 36 30 33 36 33
9 | 9 8 16 7 12 4 8 8 7 11 3 | 28 32 25 27 24 27 32 27 28 26 26
X10 | 18 17 15 --- 44 6 17 24 46 --- 11 | 21 26 22 --- 51 22 25 18 53 --- 25
11E | 7 11 10 6 13 5 9 10 10 11 3 | 24 26 18 23 25 22 26 24 27 25 23
12 | 12 11 10 11 20 4 8 12 9 14 4 | 27 30 21 28 25 24 28 18 26 20 23
13 | 7 14 16 12 21 3 13 14 10 16 4 | 31 39 26 34 41 31 37 32 37 32 32
14 | 9 11 13 14 19 4 12 14 9 16 4 | 29 30 27 40 34 32 29 35 31 27 29
15 | 10 13 13 14 14 4 12 16 11 20 4 | 42 44 39 34 33 37 42 33 39 37 37
16 | 20 11 9 10 17 4 9 14 10 20 4 | 32 24 19 22 22 20 24 19 21 17 19
17 | 8 17 12 15 19 4 10 11 8 12 4 | 27 33 26 30 27 25 30 17 28 22 25
18 | 13 11 11 16 18 4 9 13 11 17 4 | 27 25 26 28 23 22 23 27 28 26 24
19 | 11 17 11 16 21 4 10 13 9 13 4 | 27 32 27 28 27 25 29 22 28 22 25
20 | 12 11 13 13 19 5 10 14 10 15 4 | 31 27 27 38 30 30 27 33 33 35 30
21 | 12 11 8 11 20 3 9 10 8 11 3 | 29 31 25 29 32 28 28 28 32 27 28
22 | 10 10 13 11 18 6 9 19 13 18 4 | 29 29 26 30 30 27 28 28 27 25 26
23 | 7 10 13 9 13 4 10 11 12 18 4 | 23 30 24 26 19 24 30 24 27 14 22
24E | 10 11 11 9 16 6 8 9 7 9 3 | 26 26 31 26 28 26 24 25 27 27 25
25 | 10 11 13 9 15 7 8 10 8 13 3 | 21 27 25 25 22 21 26 18 22 21 22
26 | 13 11 13 7 17 4 8 12 9 11 4 | 25 30 30 24 24 24 27 22 23 26 24
27 | 10 11 15 6 13 3 10 7 12 13 3 | 28 30 32 23 23 25 27 22 25 26 25
28 | 6 12 10 11 20 3 9 12 9 10 3 | 24 29 22 22 27 22 26 21 25 19 24
29 | 16 14 8 13 22 6 14 15 11 16 5 | 35 32 27 32 28 29 34 24 29 27 28
30E | 15 10 13 8 18 5 8 8 9 9 4 | 30 30 32 27 23 28 30 27 31 26 27
31E | 13 12 9 10 14 5 7 20 10 11 4 | 27 28 24 30 26 27 27 27 30 32 26
32 | 8 8 10 6 15 5 7 12 7 9 3 | 19 24 19 20 17 18 23 15 20 16 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 12 11 17 4 10 12 10 14 |T 29 31 27 29 28 27 29 25 30 27 27
WRMS | 11 11 12 10 16 4 10 11 9 14 |NE 28 31 27 28 27 26 29 24 29 26 26
MEDI | 10 11 12 10 18 4 9 12 9 13 |MD 28 30 26 28 27 26 28 24 28 26 26
Table 3.1879.4 GPS week: 1879 Day: 4 MJD: 57401.000
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 12 10 14 3 14 6 8 11 3 | 21 30 28 21 22 22 30 22 24 31 24
2 | 12 12 7 9 23 4 15 12 8 14 4 | 49 52 46 49 54 47 51 49 49 52 49
3 | 9 8 13 9 13 4 11 13 9 16 4 | 26 33 23 24 27 24 31 27 26 34 26
5 | 5 12 11 11 20 4 12 12 10 16 4 | 37 43 37 36 33 37 44 33 40 39 37
6 | 8 8 11 7 20 4 10 11 8 12 3 | 28 31 33 25 29 27 29 23 27 27 27
7E | 11 13 7 11 18 4 12 9 9 9 4 | 23 27 18 27 21 20 25 22 24 26 21
8 | 10 9 11 10 8 4 10 10 8 12 3 | 30 34 31 31 27 28 31 27 31 33 30
9 | 9 7 14 6 9 3 9 9 5 12 3 | 25 29 21 22 25 23 30 26 24 25 24
X10 | 16 17 17 --- 44 8 17 24 44 --- 11 | 16 28 21 --- 46 20 27 18 42 --- 22
11E | 8 11 13 8 13 3 12 8 9 7 3 | 19 22 16 19 22 16 23 19 20 15 17
12 | 13 10 12 13 23 5 12 12 11 15 4 | 27 25 17 26 27 21 25 18 23 18 21
13 | 9 13 15 12 20 4 14 14 9 16 4 | 26 36 27 27 35 26 36 29 26 27 27
14 | 10 12 13 11 18 5 15 14 10 23 4 | 30 33 28 38 33 29 31 37 32 34 30
15 | 8 11 13 13 19 5 14 16 10 18 4 | 36 42 37 34 27 34 41 32 35 36 34
16 | 11 10 9 10 16 5 10 13 11 24 4 | 22 22 17 17 22 18 21 16 25 16 17
17 | 6 11 8 14 15 2 12 9 9 13 3 | 20 28 15 26 22 19 25 15 23 17 20
18 | 16 13 10 13 20 4 11 12 12 17 4 | 24 22 19 25 23 19 22 23 22 21 20
19 | 7 11 8 17 15 3 13 10 10 14 4 | 17 26 16 25 19 19 25 17 21 16 18
20 | 8 12 12 15 23 5 13 13 8 16 4 | 25 28 26 35 31 25 28 32 28 33 27
21 | 14 11 7 11 21 3 13 12 9 12 4 | 31 31 28 32 33 29 32 31 30 26 29
22 | 9 8 14 9 17 5 10 19 10 16 4 | 27 31 24 29 28 25 27 30 28 27 26
23 | 9 9 14 9 13 4 11 16 9 14 4 | 22 28 23 26 24 23 28 26 24 18 22
24E | 10 9 15 12 21 5 11 10 12 15 4 | 24 24 30 24 27 23 24 24 25 26 23
25 | 10 9 14 7 15 4 12 11 8 14 3 | 19 23 22 19 21 18 23 18 21 17 19
26 | 9 9 12 9 13 3 12 10 9 11 3 | 26 31 28 23 28 25 28 24 29 24 26
27 | 8 10 12 9 17 4 12 8 7 14 3 | 24 26 26 22 20 22 28 21 25 25 23
X28 | 6 10 9 12 --- 5 11 11 9 --- 4 | 25 28 17 22 --- 19 23 20 19 --- 24
29 | 21 15 8 16 24 10 15 12 12 17 5 | 31 24 16 24 20 23 25 17 21 21 20
30E | 9 9 12 8 22 5 14 9 7 9 3 | 23 22 27 24 21 20 21 22 20 23 20
31E | 11 9 11 9 16 4 12 15 12 13 4 | 24 25 20 27 24 23 27 23 25 29 23
32 | 9 12 9 6 13 4 11 14 8 11 3 | 19 25 18 16 15 17 24 18 19 20 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 12 11 18 4 12 12 9 15 |T 25 29 24 26 26 23 28 24 26 26 24
WRMS | 10 11 12 10 17 4 12 11 9 14 |NE 25 29 23 26 26 23 28 24 26 25 24
MEDI | 9 10 12 10 17 4 12 12 9 14 |MD 25 28 23 25 25 23 27 23 25 26 23
Table 3.1879.5 GPS week: 1879 Day: 5 MJD: 57402.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 10 12 8 13 3 9 6 7 10 3 | 20 24 25 21 24 21 23 20 20 29 21
2 | 22 9 9 12 22 10 13 17 9 13 5 | 110 109 109 108 115 107 111 112 108 114 110
3 | 8 8 14 9 9 3 9 9 8 12 3 | 25 32 23 25 30 25 32 27 27 35 27
5 | 8 13 12 11 21 4 10 12 10 16 4 | 32 39 30 36 26 30 37 28 31 37 32
6 | 9 7 13 7 20 2 6 8 6 15 3 | 27 27 33 27 27 27 28 23 27 30 26
7E | 7 13 5 10 26 2 11 7 8 6 3 | 31 30 27 36 30 30 30 28 32 32 29
8 | 13 9 11 9 11 3 9 9 8 10 3 | 29 30 30 24 30 26 28 25 26 31 27
9 | 10 8 15 7 10 3 9 10 6 8 3 | 27 31 23 26 28 25 32 24 23 26 25
X10 | 18 19 18 --- 45 9 19 28 45 --- 12 | 21 26 22 --- 44 21 27 18 37 --- 23
11E | 9 13 11 6 9 3 10 12 8 6 3 | 16 18 13 17 18 14 19 19 15 15 14
12 | 19 10 8 13 24 4 10 13 9 15 4 | 30 26 17 25 26 19 24 19 20 20 20
13 | 6 16 15 11 21 5 11 14 8 13 4 | 24 37 26 32 36 28 35 27 25 28 27
14 | 12 9 13 15 18 4 11 14 10 16 4 | 25 26 22 35 29 25 27 30 24 25 24
15 | 9 13 15 10 14 5 11 16 10 19 4 | 33 37 34 30 26 29 35 28 28 36 30
16 | 17 11 9 15 15 4 10 16 10 23 5 | 29 23 18 24 22 18 22 18 20 17 17
17 | 8 9 9 14 21 4 9 10 8 10 3 | 23 27 19 31 27 22 25 18 25 19 22
18 | 13 12 12 14 18 5 9 14 8 16 4 | 22 22 21 26 22 20 22 22 23 24 20
19 | 10 11 8 16 21 5 10 13 10 11 4 | 23 26 21 30 27 22 26 23 25 19 22
20 | 15 11 12 10 18 5 8 15 9 15 4 | 33 33 30 40 30 31 32 33 30 37 31
21 | 11 9 6 12 19 4 8 12 5 14 3 | 35 36 34 41 39 37 37 38 37 37 36
22 | 9 9 13 14 16 4 11 21 8 18 4 | 26 22 22 28 27 22 23 25 21 25 21
23 | 8 9 13 11 13 4 10 14 9 15 4 | 26 26 23 25 21 22 26 22 20 20 21
24E | 12 13 16 9 20 5 8 9 8 7 4 | 22 23 27 23 27 22 20 23 21 24 21
25 | 11 10 13 8 14 4 8 11 6 13 3 | 18 22 22 20 22 18 21 20 18 17 18
26 | 9 8 12 9 13 4 6 10 8 11 3 | 24 27 27 20 24 22 26 21 23 27 23
27 | 11 10 12 9 11 3 9 10 10 14 3 | 23 26 26 20 23 21 24 21 23 23 22
X28 | 2 --- --- --- --- 78 --- --- --- --- 0 | 13 --- --- --- --- 13 --- --- --- --- 13
29 | 20 14 6 14 23 6 13 15 11 18 5 | 33 26 19 26 23 22 27 19 27 24 22
30E | 10 8 12 7 23 4 8 8 11 9 3 | 29 27 34 32 27 27 27 28 30 23 27
31E | 13 10 7 10 17 4 12 14 7 15 4 | 25 23 17 26 28 22 26 19 25 30 22
32 | 11 7 9 6 17 3 8 15 6 11 3 | 22 20 18 21 26 17 19 14 19 12 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 10 11 11 18 4 10 13 8 14 |T 28 30 27 30 30 25 29 26 27 28 26
WRMS | 12 10 11 10 18 4 10 12 8 13 |NE 25 27 24 27 27 23 27 23 24 26 23
MEDI | 10 10 12 10 18 4 9 12 8 13 |MD 25 26 23 26 27 22 26 23 25 25 22
Table 3.1879.6 GPS week: 1879 Day: 6 MJD: 57403.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 10 7 13 4 12 5 8 11 3 | 21 22 24 18 21 20 26 19 18 29 20
2E | 16 11 8 8 32 4 13 15 8 11 4 | 97 95 94 95 100 94 94 97 97 98 96
3 | 8 8 14 10 9 3 9 9 6 12 3 | 34 36 28 32 38 31 36 32 29 39 32
5 | 11 12 13 10 20 4 15 16 10 17 4 | 45 50 44 42 36 42 51 38 43 44 42
6 | 14 8 14 8 23 8 11 7 6 10 4 | 45 49 52 48 46 46 51 45 45 48 47
7E | 14 14 6 11 16 3 13 10 12 8 4 | 26 28 20 29 27 24 27 21 29 22 23
8 | 10 8 9 10 9 4 10 8 9 10 3 | 34 33 33 28 33 32 34 28 29 34 30
9 | 9 9 14 9 10 2 9 15 5 8 3 | 28 35 26 29 33 28 35 29 28 27 28
X10 | 20 19 19 --- 51 8 16 29 48 --- 12 | 24 29 25 --- 66 28 30 20 62 --- 31
11E | 12 10 11 6 11 5 11 11 8 9 3 | 21 19 13 15 17 14 21 20 14 19 15
12 | 20 11 9 15 21 7 13 15 11 17 5 | 31 26 19 28 26 22 27 19 25 20 21
13 | 9 14 14 11 24 3 15 12 10 13 4 | 26 40 29 37 47 31 38 35 32 34 33
14 | 10 9 13 16 16 4 13 15 11 17 4 | 31 33 31 45 40 33 30 40 33 36 33
15 | 11 13 12 12 18 5 16 16 10 20 5 | 44 46 44 41 34 42 47 37 40 43 40
16 | 14 10 9 14 17 4 15 14 11 19 4 | 28 22 18 20 24 19 21 20 21 15 18
17 | 6 10 9 14 23 5 11 10 9 13 4 | 19 26 18 27 25 21 25 18 24 23 20
18 | 12 12 11 14 15 4 11 12 11 19 4 | 23 24 21 30 24 21 21 26 18 26 20
19 | 9 13 8 17 23 5 12 11 10 15 4 | 20 25 21 27 24 21 25 22 24 25 21
20 | 14 12 12 12 20 4 12 13 10 14 4 | 25 26 25 36 36 27 26 34 24 32 26
21 | 12 10 9 11 23 5 11 10 8 9 4 | 88 88 86 90 88 85 86 90 86 92 87
22 | 9 8 12 13 17 5 11 19 11 18 4 | 30 32 26 36 31 29 27 35 25 31 28
23 | 9 10 13 10 11 3 10 14 8 17 4 | 27 30 24 28 28 26 30 24 24 19 24
24E | 10 10 12 7 21 4 12 9 7 9 3 | 25 26 29 26 28 25 23 27 25 27 25
25 | 7 15 13 10 15 6 10 12 9 10 4 | 16 24 23 20 24 19 23 20 16 17 18
26 | 9 8 12 9 14 3 9 10 6 8 3 | 23 27 28 19 25 24 25 22 25 25 23
27 | 8 9 11 11 12 4 12 12 10 14 4 | 24 26 27 18 24 22 25 24 19 24 22
X28 | 8 10 10 13 23 4 9 13 13 --- 4 | 12 13 11 6 5 9 11 3 3 --- 11
29 | 18 16 7 15 21 5 15 12 12 17 5 | 28 24 15 22 21 18 23 15 18 19 17
30E | 10 8 13 10 19 2 10 9 9 9 3 | 24 27 30 25 29 24 27 27 25 23 25
31E | 13 9 7 10 16 4 10 8 9 14 3 | 23 23 17 26 20 21 24 21 25 29 21
32 | 6 9 9 6 17 5 9 13 6 8 3 | 17 20 15 16 22 15 19 20 15 15 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 11 11 18 4 12 12 9 13 |T 30 33 29 31 33 29 32 29 30 32 29
WRMS | 11 11 11 11 18 4 12 11 8 13 |NE 29 32 28 30 32 28 31 28 29 31 28
MEDI | 10 10 11 10 17 4 11 12 9 13 |MD 26 27 25 28 28 24 27 24 25 27 24
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 4.1879 GPS week: 1879 MJD: 57397.0-57403.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 |U 8 7 17 |U 8 9 31 |U 6 5 11 |
emr | emr 2962 | 10 8 19 |U 10 9 30 | 6 6 15 |
esa | esa 2962 | 9 8 19 |U 9 11 30 | 6 6 15 |
gfz | gfz 2866 |U 9 8 17 |U 9 11 33 |U 6 6 15 |
grg | grg 2948 |U 9 9 18 |U 9 12 36 | 7 6 18 |
igr | igr 2962 | 9 8 16 | 9 11 28 | 5 5 12 |
igs | igs 2907 | 9 7 16 | 9 10 30 | 5 6 13 |
jpl | jpl 2962 | 10 8 19 | 9 12 31 | 6 6 14 |
mit | mit 2962 | 9 8 17 |U 10 12 36 |U 6 7 16 |
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 5.1879.0 GPS week: 1879 Day: 0 MJD: 57397.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 19 | 8 12 39 | 6 6 13 |
emr | emr 2976 | 10 10 20 | 11 12 39 | 5 7 17 |
esa | esa 2976 | 8 10 18 | 8 13 32 | 6 6 14 |
gfz | gfz 2880 | 8 9 17 | 10 12 34 | 5 7 14 |
grg | grg 2976 | 7 10 19 | 10 16 30 | 6 6 18 |
igr | igr 2976 | 7 8 14 | 9 17 27 | 5 5 13 |
igs | igs 2976 | 7 8 14 | 8 12 34 | 4 6 12 |
jpl | jpl 2976 | 10 8 17 | 13 27 33 | 5 7 13 |
mit | mit 2976 | 8 8 12 | 10 17 45 | 7 10 14 |
Table 5.1879.1 GPS week: 1879 Day: 1 MJD: 57398.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 13 | 7 9 20 | 6 3 9 |
emr | emr 2976 | 8 4 16 | 11 7 27 | 8 7 14 |
esa | esa 2976 | 6 5 15 | 7 10 23 | 7 7 14 |
gfz | gfz 2880 | 6 4 12 | 7 8 22 | 6 6 14 |
grg | grg 2976 | 8 8 16 | 9 10 27 | 8 8 18 |
igr | igr 2976 | 5 5 13 | 7 9 21 | 6 4 11 |
igs | igs 2880 | 5 3 12 | 8 8 22 | 6 6 13 |
jpl | jpl 2976 | 7 5 19 | 8 8 23 | 6 5 13 |
mit | mit 2976 | 5 4 11 | 8 14 27 | 6 4 13 |
Table 5.1879.2 GPS week: 1879 Day: 2 MJD: 57399.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 5 12 | 9 9 32 | 6 6 11 |
emr | emr 2976 | 7 6 17 | 9 9 29 | 7 4 13 |
esa | esa 2976 | 6 6 16 | 10 9 33 | 8 5 13 |
gfz | gfz 2880 | 6 5 11 | 9 8 32 | 6 4 13 |
grg | grg 2976 | 6 7 13 | 9 10 41 | 9 8 19 |
igr | igr 2976 | 5 5 12 | 10 9 32 | 7 5 12 |
igs | igs 2880 | 5 5 11 | 10 9 32 | 7 5 12 |
jpl | jpl 2976 | 7 6 14 | 10 9 32 | 7 5 13 |
mit | mit 2976 | 7 7 17 | 10 10 32 | 9 8 23 |
Table 5.1879.3 GPS week: 1879 Day: 3 MJD: 57400.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 4 13 | 8 10 28 | 6 7 14 |
emr | emr 2976 | 7 7 15 | 9 7 27 | 5 6 17 |
esa | esa 2976 | 7 6 16 | 8 12 29 | 6 7 15 |
gfz | gfz 2880 | 6 6 14 | 8 15 36 | 5 7 19 |
grg | grg 2976 | 6 6 15 | 9 15 35 | 6 4 14 |
igr | igr 2976 | 6 5 14 | 8 11 28 | 5 6 13 |
igs | igs 2976 | 6 5 13 | 8 11 29 | 5 6 13 |
jpl | jpl 2976 | 8 5 15 | 8 13 28 | 6 7 15 |
mit | mit 2976 | 5 5 12 | 8 9 32 | 5 6 15 |
Table 5.1879.4 GPS week: 1879 Day: 4 MJD: 57401.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 13 | 8 9 34 | 6 4 11 |
emr | emr 2976 | 7 6 16 | 8 8 30 | 6 5 14 |
esa | esa 2976 | 7 6 16 | 8 9 34 | 6 6 14 |
gfz | gfz 2880 | 6 5 14 | 8 9 42 | 6 6 13 |
grg | grg 2880 | 6 6 15 | 9 9 43 | 6 4 18 |
igr | igr 2976 | 6 5 14 | 8 8 31 | 6 4 12 |
igs | igs 2976 | 6 5 13 | 8 8 33 | 6 5 11 |
jpl | jpl 2976 | 7 6 15 | 8 9 35 | 7 6 15 |
mit | mit 2976 | 7 5 14 | 9 8 34 | 7 7 13 |
Table 5.1879.5 GPS week: 1879 Day: 5 MJD: 57402.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 26 20 30 | 6 9 25 | 4 5 12 |
emr | emr 2880 | 25 19 32 | 7 7 25 | 6 7 17 |
esa | esa 2880 | 25 18 33 | 7 9 26 | 6 5 19 |
gfz | gfz 2783 | 24 19 34 | 6 9 23 | 6 6 16 |
grg | grg 2879 | 25 20 36 | 8 12 29 | 8 4 21 |
igr | igr 2880 | 26 20 32 | 6 8 22 | 5 5 13 |
igs | igs 2784 | 25 19 34 | 6 8 23 | 5 6 15 |
jpl | jpl 2880 | 26 22 33 | 7 7 26 | 5 5 17 |
mit | mit 2880 | 26 21 36 | 9 11 37 | 6 7 23 |
Table 5.1879.6 GPS week: 1879 Day: 6 MJD: 57403.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 16 | 13 10 39 | 5 8 11 |
emr | emr 2976 | 8 7 19 | 14 12 36 | 5 7 12 |
esa | esa 2976 | 7 7 20 | 14 12 34 | 6 8 14 |
gfz | gfz 2880 | 7 7 17 | 12 13 44 | 6 8 16 |
grg | grg 2976 | 6 8 13 | 12 15 45 | 8 5 20 |
igr | igr 2976 | 7 6 17 | 13 12 37 | 5 6 11 |
igs | igs 2880 | 7 6 16 | 13 12 38 | 5 8 13 |
jpl | jpl 2976 | 8 6 17 | 13 11 39 | 6 9 13 |
mit | mit 2976 | 6 6 16 | 14 15 42 | 5 8 14 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.1879 GPS week: 1879 MJD: 57397.500-57403.500
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 7 -16 97 3 | 2 18
| 17 19 137 97 5 | 2
emr uuuuu | 7 -4 55 -8 4 | 35 40
| 14 21 116 46 9 | 3
esa uuuuu | 6 21 -149 -64 -2 | 11 20
| 17 19 80 43 5 | 2
gfz uuuuu | -37 -28 11 -238 -3 | 9 17
| 15 19 108 39 7 | 2
grg uuuuu | -10 31 -185 -4 0 | 29 33
| 18 21 43 71 7 | 2
igr xxxxx | -18 0 44 26 -1 | -5 15
| 14 17 51 56 4 | 1
irf xxxxx | 28 -5 -21 -6 1 | 0 16
| 9 7 30 8 2 | 2
jpl uuuuu | -21 -29 94 -15 -6 | 21 29
| 17 32 96 85 8 | 2
mit uuuuu | 16 -15 -17 48 2 | 19 24
| 21 18 60 53 3 | 2
ngs uuuuu | 12 7 180 106 0 | 9 16
| 15 24 141 55 6 | 2
sio uuuux | 24 28 -164 71 -1 | 41 44
| 19 30 65 52 10 | 2
Table 7.1879.0 GPS week: 1879 Day: 0 MJD: 57397.500
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 | -25 -3 -153 186 -4 | 2 16
emr uuuuu | 9 -43 198 -15 15 | 33 36
esa uuuuu | -2 22 -183 -95 -11 | 14 19
gfz uuuuu | -46 -52 102 -233 2 | 10 15
grg uuuuu | 2 24 -158 -48 2 | 29 32
igr xxxxx | -28 11 49 -27 1 | -4 12
irf xxxxx | 37 0 11 -1 3 | -1 14
jpl uuuuu | -15 -29 74 -112 -5 | 25 30
mit uuuuu | 40 0 36 72 2 | 18 22
ngs uuuuu | 15 33 48 123 4 | 7 13
sio uuuux | 41 67 -91 124 5 | 39 41
Table 7.1879.1 GPS week: 1879 Day: 1 MJD: 57398.500
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 | 9 17 82 223 2 | -1 17
emr uuuuu | 6 5 -18 -79 8 | 32 36
esa uuuuu | 18 12 -209 -25 -7 | 10 19
gfz uuuuu | -51 -24 -76 -274 0 | 8 15
grg uuuuu | -6 58 -250 -77 2 | 27 30
igr xxxxx | -6 24 57 -12 0 | -7 15
irf xxxxx | 36 -8 -24 -15 2 | -2 15
jpl uuuuu | -47 0 101 71 -12 | 22 29
mit uuuuu | 25 -28 -20 32 1 | 16 21
ngs uuuuu | 18 -15 280 22 3 | 5 13
sio uuuux | 35 11 -204 90 -4 | 39 41
Table 7.1879.2 GPS week: 1879 Day: 2 MJD: 57399.500
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 30 -175 154 0 | 4 19
emr uuuuu | -12 -20 157 -56 2 | 36 41
esa uuuuu | 22 41 -180 -31 -3 | 13 22
gfz uuuuu | -38 -2 -157 -300 -4 | 12 19
grg uuuuu | -12 23 -189 -59 -12 | 32 36
igr xxxxx | -10 -18 61 59 -3 | -2 16
irf xxxxx | 18 -2 -72 -11 2 | 3 17
jpl uuuuu | 9 -87 218 53 -3 | 23 31
mit uuuuu | -21 -10 -48 51 7 | 21 26
ngs uuuuu | 18 9 325 97 5 | 10 17
sio uuuux | 1 -4 -158 72 7 | 44 46
Table 7.1879.3 GPS week: 1879 Day: 3 MJD: 57400.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 24 23 -7 96 1 | 1 18
emr uuuuu | 4 2 -61 26 13 | 34 40
esa uuuuu | 19 50 -227 -73 1 | 10 19
gfz uuuuu | -49 -5 -39 -233 -15 | 9 18
grg uuuuu | -48 54 -215 -19 -4 | 29 33
igr xxxxx | -28 -7 59 -47 -4 | -5 16
irf xxxxx | 21 -15 1 -1 1 | 0 16
jpl uuuuu | -21 -16 -5 -72 4 | 21 29
mit uuuuu | 15 -48 62 148 2 | 19 24
ngs uuuuu | 35 -9 363 51 7 | 9 17
sio uuuux | 5 -14 -120 127 -5 | 42 44
Table 7.1879.4 GPS week: 1879 Day: 4 MJD: 57401.500
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 -22 -86 36 7 | 0 18
emr uuuuu | 33 13 13 37 4 | 37 42
esa uuuuu | -27 14 -145 -10 -1 | 10 19
gfz uuuuu | -39 -39 24 -237 -9 | 8 18
grg uuuuu | -11 -4 -139 -8 8 | 29 33
igr xxxxx | -41 -20 124 27 -7 | -6 16
irf xxxxx | 39 -12 9 -12 0 | 0 16
jpl uuuuu | -19 -55 229 -119 3 | 18 26
mit uuuuu | 19 0 22 12 1 | 20 25
ngs uuuuu | -14 47 98 178 -2 | 9 17
sio uuuux | 50 43 -103 61 -12 | 43 45
Table 7.1879.5 GPS week: 1879 Day: 5 MJD: 57402.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 -9 216 -51 10 | 2 19
emr uuuuu | 9 15 -72 -11 -6 | 40 45
esa uuuuu | 6 -9 -109 -86 1 | 11 20
gfz uuuuu | -7 -31 82 -205 3 | 8 18
grg uuuuu | 2 24 -210 63 -2 | 31 35
igr xxxxx | -4 -7 -24 89 2 | -5 16
irf xxxxx | 20 -1 -44 -10 -3 | 1 17
jpl uuuuu | -20 6 14 75 -20 | 22 29
mit uuuuu | -1 -21 -62 -22 -1 | 22 27
ngs uuuuu | 3 0 130 153 -3 | 11 18
sio uuuux | 15 44 -204 42 -13 | 43 45
Table 7.1879.6 GPS week: 1879 Day: 6 MJD: 57403.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 3 11 12 34 6 | 2 19
emr uuuuu | -4 -2 168 40 -7 | 37 42
esa uuuuu | 8 16 8 -129 5 | 8 18
gfz uuuuu | -31 -44 145 -186 0 | 7 17
grg uuuuu | 2 36 -136 121 9 | 30 35
igr xxxxx | -8 16 -18 93 3 | -6 16
irf xxxxx | 24 2 -29 8 4 | 0 16
jpl uuuuu | -34 -22 25 -1 -6 | 19 27
mit uuuuu | 31 0 -108 46 5 | 20 26
ngs uuuuu | 6 -14 15 115 -11 | 10 18
sio uuuux | 18 48 -269 -22 14 | 41 43
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