[IGSREPORT-25055] Wk 1932 IGS Final Orbits
acc at igs.org
acc at igs.org
Thu Feb 2 17:08:27 PST 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1932 (Jan 15, 2017 - Jan 21, 2017)
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:
igs1932[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1932[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1932[0-6].cls IGS GPS clock combination summary report.
igs19327.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19327.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 | 21 21 NRMD SYOG
0 | EMR | SYOG
0 | ESA | DAV1 FAA1 MAL2 SYOG
0 | GFZ | 25 BJNM FAA1 GODE KERG MAL2 BJNM GODE KERG MAL2 SYOG
0 | GRG | 21 CHTI GLSV SYOG
0 | JPL | TUVA
0 | MIT | DAV1 DAV1
1 | COD | SYOG NICO SYOG
1 | EMR | SYOG SYOG
1 | GFZ | BJNM CHTI DAV1 MAL2 ALRT BJNM CEDU CHTI DAV1 MAL2
1 | GRG | 21 21 ALRT CHTI GLSV KOUR MAL2 MCM4 NICO SYOG ALRT
1 | GRG | CHTI GLSV MAL2 MCM4 SYOG
1 | JPL | TUVA
2 | COD | 2 2 GLSV SYOG GLSV SYOG
2 | ESA | FAA1 FAA1
2 | GFZ | BJNM FAA1 GODE WTZR BJNM CHTI FAA1 GODE MDVJ WTZR
2 | GRG | GLSV SYOG GLSV REUN SYOG
2 | JPL | TUVA
2 | MIT | DAV1 GLSV
3 | COD | 21 NICO YELL NICO YELL
3 | EMR | 6 6 FAIR
3 | ESA | FAA1 REUN DRAG REUN TIXI
3 | GFZ | CHTI DRAG GMSD CHTI GMSD SYOG
3 | GRG | CRO1 GLSV CHTI CRO1 DRAG GLSV
3 | JPL | 6 TUVA
4 | COD | 1 1 DAV1 CEDU DAV1 INVK
4 | ESA | FAA1 FAA1
4 | GFZ | AUCK BJNM GMSD NRMD AUCK BJNM GMSD NRMD
4 | GRG | 17 DAV1 GLSV KOUR NKLG SYOG DAV1 GLSV KOUR NKLG SYOG
5 | COD | BJNM MAG0 NICO BJNM MAG0 NICO
5 | ESA | NKLG BJNM MAL2
5 | GFZ | DUBO FAA1 GMSD NKLG CCJ2 CHTI DUBO FAA1 GMSD MAL2
5 | GFZ | NKLG
5 | GRG | DUBO GLSV INVK KOUR SYOG CHTI DUBO GLSV INVK KOUR
5 | GRG | NKLG SYOG
5 | MIT | CHUM PTBB CHUM NICO
6 | COD | NKLG SYOG NKLG SYOG
6 | EMR | SYOG
6 | ESA | TIXI
6 | GFZ | BJNM CHTI GMSD GODE AUCK BJNM CEDU CHTI GMSD GODE
6 | GRG | CHTI GLSV LPGS CHTI GLSV LPGS
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 | GRG | ~16:35 | ~ 0.12 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 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
----+------------+----------
G23 | 2017_01_17 | 2017004
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 G06 | | | | 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 | -1.4 -.0 -3.9 -22 36 -15 .70
EMR | 0 | 1.4 3.2 20.5 70 -17 32 .56
ESA | 0 | .2 .3 -1.3 16 -5 -1 .40
GFZ | 0 | 1.5 -.6 -1.0 -26 -99 -50 .90
GRG | 0 | 3.7 6.2 16.4 110 4 -38 .41
JPL | 0 | -3.5 6.6 1.3 -25 -16 25 .37
MIT | 0 | 4.6 1.1 6.1 34 -11 -38 1.13
NGS | 0 | -7.0 7.5 .4 36 -6 -71 .69
SIO | 0 | 1.5 3.0 1.1 -2 -40 -37 .42
COD | 1 | -1.2 .2 -4.2 -11 41 7 .79
EMR | 1 | 2.3 1.4 17.8 94 -22 80 1.22
ESA | 1 | -1.5 .1 1.2 119 -67 83 .47
GFZ | 1 | .3 .8 -.2 -23 -101 -47 .98
GRG | 1 | -.8 5.6 9.0 86 19 -16 .79
JPL | 1 | -1.7 5.1 7.0 -19 70 12 .80
MIT | 1 | 3.7 4.2 11.3 46 -13 -53 1.22
NGS | 1 | -2.7 3.7 5.5 12 -33 -20 1.06
SIO | 1 | .8 3.6 8.2 15 -42 0 .96
COD | 2 | -.9 -.1 -4.6 -16 33 3 .75
EMR | 2 | 3.7 -1.9 17.5 102 -1 52 1.13
ESA | 2 | -1.0 -.7 -.3 18 -2 5 .70
GFZ | 2 | -.1 -.5 -.5 -31 -111 -28 1.05
GRG | 2 | 1.1 2.4 10.0 49 3 -16 .53
JPL | 2 | -5.0 2.6 1.4 -53 74 52 .70
MIT | 2 | 2.4 4.3 9.8 31 -10 -41 1.32
NGS | 2 | -3.1 1.2 -.0 34 -20 -23 .80
SIO | 2 | 1.8 8.3 1.1 1 -33 -19 1.03
COD | 3 | -2.4 -.7 -4.3 -26 43 -2 .63
EMR | 3 | 13.9 14.6 16.6 103 10 44 .84
ESA | 3 | -.8 .9 .3 37 -23 43 .17
GFZ | 3 | .9 -.1 .1 -32 -100 -36 .76
GRG | 3 | 5.0 7.5 15.7 77 20 25 .59
JPL | 3 | 6.5 9.1 7.1 -52 5 -15 .71
MIT | 3 | 7.6 6.0 10.9 44 -17 -19 .84
NGS | 3 | 2.2 8.0 6.3 14 -50 -8 .74
SIO | 3 | 3.3 8.0 7.0 13 -32 -26 .71
COD | 4 | -2.9 -1.4 -3.9 -29 58 -30 .73
EMR | 4 | 8.6 8.6 13.5 110 6 44 .83
ESA | 4 | -.9 -.3 -.8 39 5 23 .54
GFZ | 4 | .2 .0 -1.7 -29 -99 -61 1.00
GRG | 4 | 8.4 6.9 13.8 76 18 37 .79
JPL | 4 | .6 1.9 8.2 -44 -3 -29 1.03
MIT | 4 | 4.1 4.5 11.1 59 -13 -38 .90
NGS | 4 | 5.0 1.4 8.6 15 -59 23 .90
SIO | 4 | 1.3 2.9 2.3 29 -5 -14 1.00
COD | 5 | -2.9 -1.1 -3.6 -36 36 19 .68
EMR | 5 | 9.8 3.0 16.2 107 -17 78 .46
ESA | 5 | -.7 .7 .0 58 -24 51 .32
GFZ | 5 | .3 .2 -.5 -23 -102 -21 .69
GRG | 5 | 6.0 1.0 -.3 56 42 100 .35
JPL | 5 | 9.5 1.5 11.6 -18 1 22 .46
MIT | 5 | 4.0 2.7 13.2 41 -27 -14 .81
NGS | 5 | 8.8 1.4 5.6 19 -77 55 .75
SIO | 5 | 6.2 3.8 5.5 15 -27 31 .70
COD | 6 | -2.7 -1.3 -2.9 -22 30 7 .62
EMR | 6 | 9.4 -.9 16.7 87 -1 32 .73
ESA | 6 | -.6 .5 -.6 49 -45 65 .21
GFZ | 6 | .6 -.3 -.4 -20 -110 -32 .68
GRG | 6 | 4.7 2.8 -4.4 102 11 112 .57
JPL | 6 | 6.5 .0 10.8 -20 64 6 .82
MIT | 6 | 6.1 4.0 11.8 28 -43 -21 .87
NGS | 6 | 11.4 .2 14.5 -24 -74 50 .81
SIO | 6 | 9.2 4.4 12.5 15 -23 -18 .70
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 1.1932.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1932.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 2.1932.[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 3.1932.[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 5.1932.0-6). 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 1932 summary. (Jan 15, 2017 - Jan 21, 2017)
Table 1.1932.a GPS week: 1932 MJD: 57768.000-57774.000
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 231| 0 1 -1 1 10 3 .12 11 11 | -834 -292 16 139
| 0 0 2 19 13 14 .03 | 192 254
emr 80| 0 1 3 -11 -37 4 .35 11 11 | 1008 -35 15 141
| 2 4 1 15 11 17 .04 | 358 471
esa 150| 0 0 1 19 17 30 -.47 7 7 | -29 -1382 9 213
| 0 0 1 15 17 14 .02 | 878 1800
gfz 196| 0 0 -2 4 -3 14 .21 12 12 | -550 78 12 111
| 0 1 0 13 21 14 .04 | 244 406
grg 113| 1 0 1 5 36 10 -.28 14 11 | 18 43 26 218
| 1 1 6 20 24 11 .03 | 114 142
igr n/a| 0 0 -1 -28 33 -7 .01 5 5 | 11109 -622 18 93
| 0 1 0 14 8 16 .03 | 1350 570
jpl 80| 0 0 4 10 38 -61 .35 10 10 | 696 -33 15 137
| 2 1 0 20 32 29 .05 | 379 440
mit 349| 1 0 -4 -27 -24 1 -.05 15 14 | -62 -111 47 297
| 1 0 0 38 33 18 .06 | 279 135
ngs 206| -1 0 -1 -29 -30 0 .06 10 8 | -813 -312 1085 2251
| 1 0 2 12 29 24 .06 | 183 263
sio 285| 0 -3 -7 -3 -42 -5 -.00 15 14 | --- --- --- ---
| 1 0 1 34 51 33 .04 | --- ---
Table 1.1932.b GPS week : 1932 MJD: 57768.000-57774.000
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 6 4 4 3 |
2 | 4 4 5 4 4 4 4 |
3 | 4 3 3 3 3 3 3 |
4 | 0 0 0 0 0 0 0 |
5 | 5 5 5 5 5 4 5 |
6 | 4 4 4 7 6 4 5 |
7 | 4 4 4 4 4 4 4 |
8 | 4 3 3 3 4 3 3 |
9 | 4 3 3 3 3 3 3 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 4 4 5 4 |
12 | 4 4 4 4 4 5 5 |
13 | 4 4 4 4 4 4 4 |
14 | 5 4 4 4 4 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 4 5 4 4 5 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 5 5 5 |
20 | 4 4 4 5 4 4 4 |
21 | 4 4 4 6 3 5 4 |
22 | 7 5 5 5 5 5 5 |
23 | 4 4 0 4 4 4 3 |
24 | 4 3 4 4 3 4 4 |
25 | 4 3 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 3 3 3 3 3 4 3 |
28 | 5 4 4 4 4 4 4 |
29 | 5 4 4 5 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 4 4 4 4 4 4 4 |
32 | 3 3 3 3 3 3 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 2.1932.0 GPS week: 1932 Day: 0 MJD: 57768.000
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 233| 0 1 -2 20 21 5 .09 10 10 | -1159 46 18 128
emr 80| 0 -1 4 -14 -22 -26 .33 11 11 | 1330 -212 15 143
esa 150| 0 0 0 -4 42 14 -.49 7 7 | -1503 1678 9 153
gfz 196| -1 1 -1 -15 -2 6 .14 13 13 | -607 139 15 106
grg 112| 1 1 6 13 24 0 -.22 19 15 | -168 239 27 262
igr n/a| 0 0 -1 -33 30 0 -.05 5 5 | 13351 -1105 18 100
jpl 80| 0 0 5 14 -6 -65 .32 11 11 | 776 -247 15 115
mit 350| 3 -1 -5 28 -8 21 -.03 15 15 | -409 -123 50 264
ngs 207| -1 1 -3 -45 -29 25 .14 10 8 | -1141 35 1306 2613
sio 285| 1 -2 -4 40 -52 6 -.01 15 14 | --- --- --- ---
Table 2.1932.1 GPS week: 1932 Day: 1 MJD: 57769.000
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 232| 1 1 0 -14 30 3 .11 10 10 | -808 -340 17 142
emr 80| -2 -1 4 3 -33 0 .32 11 11 | 1049 -569 16 144
esa 150| 1 0 2 33 22 45 -.49 7 7 | 87 -1637 8 187
gfz 197| -1 0 -4 26 25 -3 .20 12 11 | -571 98 12 108
grg 117| 2 0 1 19 31 9 -.26 11 10 | 128 -141 28 214
igr n/a| 0 0 -1 -16 48 -34 -.01 5 4 | 12427 -1441 20 98
jpl 80| -1 0 6 -9 62 -80 .29 10 10 | 622 -639 16 138
mit 350| 2 0 -4 -58 -47 -24 .00 15 14 | -68 -358 46 297
ngs 206| -1 0 -2 -29 -48 26 .11 9 8 | -791 -338 1124 2532
sio 287| 0 -3 -7 -32 -101 5 .00 15 15 | --- --- --- ---
Table 2.1932.2 GPS week: 1932 Day: 2 MJD: 57770.000
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 231| 0 2 0 17 15 9 .16 9 9 | -738 -600 16 151
emr 80| 0 -3 6 -7 -50 22 .36 11 11 | 508 434 14 145
esa 150| 0 0 0 12 7 12 -.47 7 7 | -653 432 8 176
gfz 198| 0 1 -3 4 -11 30 .27 12 11 | -805 567 13 118
grg 115| 2 2 6 23 2 17 -.29 12 11 | -88 189 26 242
igr n/a| 0 0 -2 -4 28 1 .03 5 5 | 11012 -217 16 92
jpl 80| -1 -2 3 -9 67 -33 .31 10 10 | 68 439 15 129
mit 350| 2 0 -3 -21 16 -16 -.01 14 13 | 42 35 40 286
ngs 207| -2 0 -4 -25 -49 -26 .11 11 9 | -728 -604 1193 2380
sio 288| 0 -1 -6 -5 0 -12 -.03 15 13 | --- --- --- ---
Table 2.1932.3 GPS week: 1932 Day: 3 MJD: 57771.000
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 231| -1 0 0 -4 7 -12 .14 12 11 | -1028 54 17 162
emr 80| 3 8 1 -23 -57 25 .35 14 14 | 953 217 16 156
esa 150| 0 0 0 11 23 49 -.43 8 8 | 1323 -3213 8 236
gfz 199| -2 -1 -2 13 23 8 .20 12 12 | -181 -331 11 137
grg 116| 0 0 5 22 31 28 -.27 12 10 | 76 7 26 206
igr n/a| -1 -2 -2 -35 38 -2 .02 5 5 | 10556 20 21 104
jpl 80| 3 0 4 15 32 -83 .38 11 11 | 983 206 17 164
mit 350| 0 -1 -4 -12 -62 13 -.02 15 15 | 104 -59 59 287
ngs 209| -2 0 0 -42 0 -35 .04 11 9 | -960 7 1075 1969
sio 290| -2 -3 -8 -2 -52 -4 .05 14 13 | --- --- --- ---
Table 2.1932.4 GPS week: 1932 Day: 4 MJD: 57772.000
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 232| 0 0 -3 -20 3 -9 .09 10 10 | -814 -307 15 131
emr 80| -1 5 2 10 -35 7 .43 11 11 | 1213 -88 16 146
esa 150| 0 -1 1 42 19 38 -.46 7 6 | -39 -1590 12 303
gfz 198| 0 -2 -3 8 -6 4 .21 12 11 | -309 -460 10 124
grg 115| 2 0 3 5 34 12 -.29 13 10 | -25 113 24 220
igr n/a| 0 -2 -2 -25 23 12 .05 5 4 | 10651 -489 17 78
jpl 80| -1 2 5 10 -2 -91 .44 10 10 | 732 212 15 150
mit 350| 1 -1 -4 -39 9 19 -.07 14 14 | 95 -87 44 313
ngs 203| 0 -1 0 -28 -41 0 .02 10 9 | -631 -630 826 1940
sio 284| 0 -3 -7 -47 3 28 .03 14 14 | --- --- --- ---
Table 2.1932.5 GPS week: 1932 Day: 5 MJD: 57773.000
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 232| -1 0 0 -13 6 -1 .13 11 10 | -655 -513 17 140
emr 80| 1 3 3 -34 -30 -1 .34 11 11 | 1434 -619 13 129
esa 150| 0 0 3 18 18 30 -.47 7 7 | 391 -2682 11 249
gfz 193| 0 -1 -1 -1 -28 31 .25 13 12 | -524 -64 12 103
grg 118| 1 0 -3 -32 55 11 -.33 13 11 | 83 -1 30 192
igr n/a| 0 -1 0 -42 27 -27 .02 5 5 | 10457 -1034 18 89
jpl 80| -1 1 4 49 47 -65 .37 9 9 | 1252 -550 17 145
mit 350| 0 -2 -2 -1 -65 -11 -.10 15 15 | -476 16 50 312
ngs 204| 0 0 -1 -23 16 13 -.01 10 9 | -810 -270 887 2038
sio 282| 0 -4 -7 -17 -110 10 .02 16 14 | --- --- --- ---
Table 2.1932.6 GPS week: 1932 Day: 6 MJD: 57774.000
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 232| 0 1 -6 28 -13 31 .12 15 15 | -642 -386 15 125
emr 80| 0 -1 4 -11 -35 3 .34 10 10 | 571 589 16 129
esa 150| 1 0 3 20 -13 24 -.48 8 8 | 186 -2666 11 191
gfz 192| 0 0 -3 -2 -23 27 .19 12 12 | -856 601 11 83
grg 104| 1 1 -9 -11 78 -5 -.28 14 11 | 121 -101 27 191
igr n/a| 0 0 -2 -43 36 -3 .03 4 4 | 9310 -88 16 91
jpl 80| -1 0 4 2 70 -9 .33 9 9 | 445 348 15 121
mit 349| 0 0 -3 -89 -10 9 -.16 15 14 | 274 -205 41 326
ngs 207| 0 0 4 -9 -65 3 .03 10 8 | -632 -386 1187 2285
sio 285| 0 -3 -7 42 15 -75 -.09 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 3.1932.0 GPS week: 1932 Day: 0 MJD: 57768.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 12 7 8 22 5 12 10 10 9 3 | 49 52 44 46 42 44 49 49 52 48 47
2E | 12 11 6 9 17 4 13 16 9 14 4 | 28 29 29 29 32 27 31 25 23 31 27
3 | 10 8 6 8 24 6 12 7 7 13 3 | 18 24 17 18 28 14 27 18 17 24 16
X4 | 2 --- --- --- --- 38 --- --- --- --- 0 | 39 --- --- --- --- 27 --- --- --- --- 39
5 | 7 11 9 16 15 5 12 20 14 19 4 | 42 49 43 34 41 39 49 30 41 37 39
6E | 9 9 9 9 26 5 10 12 8 12 4 | 120 122 121 120 120 122 120 121 121 120 120
7 | 12 12 6 9 20 4 12 11 8 16 4 | 29 25 19 25 27 22 25 23 27 19 21
8 | 11 10 6 9 14 6 11 11 7 11 3 | 19 23 12 18 21 16 25 19 21 18 16
9 | 9 9 7 12 17 5 10 7 8 16 3 | 55 56 49 53 46 51 54 51 51 55 51
10 | 8 9 4 9 12 4 8 8 7 12 3 | 17 21 15 18 17 12 19 14 17 11 13
11E | 16 12 11 7 20 9 9 12 8 12 4 | 39 41 36 38 39 37 38 34 39 33 36
12 | 12 10 7 15 13 4 10 15 11 16 4 | 25 25 17 24 21 19 25 20 19 18 18
13 | 8 9 10 14 10 5 11 18 10 13 4 | 39 42 40 45 35 41 41 39 38 40 38
14 | 8 13 9 19 11 3 8 13 11 26 4 | 38 36 32 50 33 36 35 38 43 38 35
15 | 6 12 8 14 11 4 11 17 10 17 4 | 41 40 40 46 34 42 40 43 38 44 39
16 | 14 12 6 17 18 7 12 19 11 17 4 | 28 22 19 22 25 18 23 19 24 14 18
17 | 9 12 8 19 21 6 10 19 14 11 4 | 21 29 19 32 23 22 26 22 28 20 21
18 | 11 11 8 16 13 5 10 20 12 20 4 | 26 28 26 33 28 24 26 31 27 32 25
19 | 10 11 7 16 18 6 11 19 14 14 4 | 20 26 17 27 22 18 24 20 25 16 18
20 | 8 11 9 16 11 6 10 20 10 16 4 | 34 29 32 39 29 31 29 35 32 40 30
21E | 9 11 6 10 19 5 18 13 7 11 4 | 21 18 17 18 20 17 26 20 18 18 17
22 | 11 12 10 14 54 8 12 25 9 19 6 | 32 35 33 37 62 34 35 37 33 31 31
23 | 7 6 10 11 9 5 8 10 9 18 3 | 15 14 17 8 11 13 10 10 12 10 11
24 | 10 11 7 6 11 4 10 14 8 13 3 | 22 23 12 21 18 16 21 27 23 22 18
25 | 10 14 6 19 12 5 10 13 9 16 4 | 22 24 13 26 18 19 22 17 20 26 17
26 | 7 12 4 10 14 5 13 15 7 9 3 | 26 26 20 21 21 21 25 29 27 24 22
27 | 8 10 4 8 10 4 10 12 8 11 3 | 21 24 11 18 17 16 23 21 22 19 16
28 | 15 12 6 19 18 5 8 15 13 12 4 | 22 28 20 29 24 19 23 22 18 18 19
29 | 14 14 5 13 15 6 10 16 12 19 4 | 29 25 17 22 24 19 25 17 23 21 19
30 | 7 14 6 9 19 4 13 12 11 9 3 | 20 22 13 20 27 17 22 23 25 19 17
31 | 11 14 6 12 16 5 8 19 8 12 4 | 28 29 20 28 26 23 26 28 27 25 23
32 | 6 8 6 9 11 5 9 13 5 12 3 | 53 56 48 57 51 52 55 60 57 54 53
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 7 13 19 5 11 15 10 15 |T 32 33 28 32 31 29 32 31 31 30 29
WRMS | 10 11 7 13 15 5 11 15 8 14 |NE 28 30 23 29 28 25 29 27 28 26 25
MEDI | 9 11 7 12 15 5 10 14 9 13 |MD 28 28 20 28 27 22 26 25 27 24 21
Table 3.1932.1 GPS week: 1932 Day: 1 MJD: 57769.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 9 10 8 11 13 4 10 11 9 7 3 | 37 36 30 39 35 32 40 34 37 34 35
2E | 15 10 7 11 11 4 12 17 11 18 4 | 31 26 26 26 31 23 28 25 27 13 24
3 | 9 6 5 7 8 4 8 8 5 12 2 | 19 22 16 20 16 13 22 18 16 26 17
X4 | 3 --- --- --- --- 44 --- --- --- --- 0 | 28 --- --- --- --- 38 --- --- --- --- 27
5 | 7 8 9 15 13 3 11 20 14 21 4 | 31 36 30 29 33 29 38 21 27 30 28
6E | 7 9 9 12 18 5 8 10 9 12 3 | 110 112 112 112 112 112 110 111 111 113 110
7 | 10 15 6 9 15 6 12 13 8 17 4 | 28 25 19 29 17 22 26 21 25 17 21
8 | 11 10 6 8 8 5 10 13 7 11 3 | 22 23 15 23 15 17 26 19 19 22 18
9 | 10 9 5 11 8 4 12 9 4 16 3 | 37 41 29 35 29 32 40 35 32 42 33
10 | 8 9 5 6 6 3 8 11 7 14 2 | 12 18 15 18 15 11 17 14 10 16 11
11E | 12 10 9 10 14 4 9 12 9 13 3 | 37 32 26 34 32 31 35 29 32 29 31
12 | 11 10 5 13 13 3 9 15 9 14 3 | 27 24 16 27 20 19 24 19 20 15 19
13 | 6 10 11 13 9 5 12 15 11 13 4 | 27 35 28 33 22 28 34 28 29 27 28
14 | 8 10 7 15 8 4 8 12 10 13 3 | 24 24 23 38 21 24 25 27 29 26 24
15 | 6 10 8 11 8 4 11 15 12 19 4 | 26 29 23 30 22 26 29 26 27 28 25
16 | 15 12 7 13 15 7 10 19 11 20 4 | 27 21 20 20 23 17 20 17 19 14 16
17 | 9 11 7 18 17 4 9 19 11 12 4 | 20 27 19 31 21 20 26 16 24 21 20
18 | 12 12 7 14 9 5 11 22 14 22 4 | 22 23 22 29 21 21 23 20 18 22 18
19 | 11 11 7 18 15 5 12 18 16 14 4 | 22 26 17 26 21 17 26 15 24 15 18
20 | 6 9 9 14 8 3 12 19 10 15 4 | 28 26 26 30 24 25 26 23 28 29 25
21E | 14 13 6 10 13 5 13 11 8 11 4 | 24 17 16 17 23 14 16 18 18 16 15
22 | 10 10 10 12 9 6 9 28 10 19 4 | 26 28 26 27 27 24 28 29 20 22 22
23 | 13 5 11 10 8 3 5 12 9 20 3 | 15 12 17 11 12 12 10 8 6 7 11
24 | 8 11 6 6 11 3 9 15 5 14 3 | 21 23 11 23 18 16 21 26 21 22 18
25 | 9 16 6 8 8 4 8 12 5 12 3 | 22 23 11 24 16 17 23 17 18 21 17
26 | 9 8 5 10 14 7 12 18 7 14 3 | 20 24 18 22 22 20 24 23 20 24 18
27 | 8 11 6 6 5 3 10 14 6 16 3 | 21 26 17 23 15 19 27 20 19 25 19
28 | 10 8 7 18 14 5 9 14 10 12 4 | 21 25 22 32 20 20 25 19 21 16 20
29 | 15 12 6 14 9 4 10 16 11 20 4 | 27 25 19 25 20 20 25 16 21 22 19
30 | 9 13 8 6 15 4 12 11 7 12 3 | 22 19 14 24 17 17 24 22 22 16 18
31 | 12 15 6 11 13 6 8 18 10 15 4 | 21 23 13 24 17 16 23 19 22 22 16
32 | 7 10 3 9 8 5 10 11 8 11 3 | 27 36 28 35 29 28 34 35 30 32 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 7 12 11 5 10 15 9 15 |T 27 28 23 29 24 24 28 24 25 25 24
WRMS | 10 11 7 11 10 4 10 14 8 15 |NE 23 25 19 26 20 21 25 21 21 22 20
MEDI | 9 10 7 11 11 4 10 14 9 14 |MD 24 25 19 27 21 20 26 21 22 22 19
Table 3.1932.2 GPS week: 1932 Day: 2 MJD: 57770.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 11 7 10 15 7 13 10 14 10 4 | 34 34 23 30 28 27 33 27 34 29 28
2E | 9 17 5 9 19 5 18 16 12 14 4 | 53 51 48 46 54 47 51 51 51 50 49
3 | 10 6 6 7 10 5 8 6 7 18 3 | 21 25 15 20 19 15 23 19 19 27 17
X4 | 3 --- --- --- --- 30 --- --- --- --- 0 | 42 --- --- --- --- 30 --- --- --- --- 41
5 | 9 11 8 15 11 4 10 18 12 22 4 | 37 43 35 29 38 32 40 28 33 36 34
6E | 9 10 9 10 18 5 11 10 14 12 4 | 111 110 106 109 106 107 111 109 109 114 109
7 | 8 13 4 13 11 4 10 10 10 15 3 | 29 24 17 28 19 22 24 22 22 16 20
8 | 7 8 6 6 8 4 10 8 7 8 2 | 21 23 12 19 15 16 22 19 21 22 17
9 | 6 9 4 10 9 4 10 6 9 15 3 | 41 43 35 39 32 37 42 38 36 39 37
10 | 6 8 4 8 9 3 8 10 7 11 2 | 17 21 18 17 15 14 19 19 19 17 15
11E | 16 8 10 11 12 7 11 11 10 14 4 | 40 36 31 37 35 33 34 33 37 33 33
12 | 12 12 5 16 11 4 9 14 11 15 4 | 30 33 20 27 25 22 29 25 24 21 23
13 | 8 10 10 12 8 3 9 16 11 12 3 | 32 34 34 34 26 32 35 30 33 32 31
14 | 5 13 8 15 8 3 9 12 12 13 3 | 32 32 31 40 31 32 31 34 38 32 31
15 | 9 11 7 13 8 3 11 15 10 17 4 | 37 33 32 39 28 32 33 33 31 37 32
16 | 14 11 5 14 16 5 14 15 12 17 4 | 32 28 22 25 29 21 23 25 27 22 23
17 | 10 12 7 16 15 4 8 18 11 10 4 | 23 31 21 32 22 23 29 24 27 22 23
18 | 11 11 7 17 12 4 10 20 14 23 4 | 27 26 26 32 23 25 27 26 30 30 24
19 | 10 11 6 18 15 4 9 18 11 14 4 | 22 28 18 29 21 18 26 23 23 16 20
20 | 7 12 8 16 8 5 8 18 11 16 4 | 32 28 29 34 25 29 30 29 33 37 29
X21E | 6 14 5 13 13 6 13 11 8 --- 4 | 30 30 26 29 32 27 32 28 31 --- 28
22 | 9 9 10 14 11 5 9 28 12 22 5 | 26 30 28 31 22 26 29 33 27 26 24
X23 | 3 --- --- --- --- 26 --- --- --- --- 0 | 58 --- --- --- --- 38 --- --- --- --- 55
24 | 10 10 5 10 8 7 11 14 8 13 3 | 23 27 16 26 20 21 27 29 25 25 21
25 | 8 12 8 7 9 4 11 9 7 16 3 | 25 28 18 25 19 20 26 21 25 26 21
26 | 8 9 6 11 13 4 10 17 10 12 3 | 31 33 26 26 27 26 31 33 33 32 28
27 | 6 8 5 9 12 6 11 12 7 11 3 | 21 25 12 20 18 18 25 20 22 22 18
28 | 11 9 6 14 14 6 7 13 11 12 3 | 23 26 18 27 21 18 23 22 21 14 19
29 | 14 13 6 17 8 5 10 15 11 19 4 | 31 29 22 27 24 24 29 23 27 25 24
30 | 7 13 4 6 17 3 9 10 10 8 3 | 18 23 11 18 24 16 22 23 18 15 16
31 | 12 12 4 11 12 7 9 16 10 14 4 | 26 29 21 28 23 23 28 24 30 28 23
32 | 7 10 5 11 7 3 11 9 10 15 3 | 43 47 41 45 42 42 47 48 49 48 44
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 11 7 12 12 5 10 14 11 15 |T 33 33 27 32 28 28 32 30 31 30 29
WRMS | 9 11 7 11 11 5 10 13 9 13 |NE 29 29 23 28 24 24 28 26 27 26 26
MEDI | 9 11 6 11 11 4 10 13 10 14 |MD 30 29 22 29 24 25 29 26 27 27 24
Table 3.1932.3 GPS week: 1932 Day: 3 MJD: 57771.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 16 22 7 8 27 6 18 11 14 10 5 | 44 52 39 43 41 42 51 39 44 41 41
2E | 9 15 4 10 10 6 15 21 9 17 4 | 34 38 35 37 38 35 38 43 36 45 36
3 | 7 11 6 5 8 4 9 9 5 16 3 | 20 29 20 20 22 17 26 20 21 29 20
X4 | 2 --- --- --- --- 74 --- --- --- --- 0 | 59 --- --- --- --- 27 --- --- --- --- 57
5 | 8 11 10 17 9 5 9 18 11 19 4 | 36 39 32 24 34 29 39 24 30 32 30
6E | 25 20 10 15 16 7 20 15 24 12 6 | 201 203 204 203 206 202 198 199 201 200 201
7 | 11 17 6 9 13 4 11 15 11 19 4 | 26 31 17 23 22 20 24 21 22 17 18
8 | 7 14 5 7 9 3 13 12 5 12 3 | 21 28 13 19 16 17 23 21 18 23 17
9 | 9 15 4 8 7 4 11 11 7 11 3 | 46 54 43 45 39 44 51 44 45 45 44
10 | 9 10 6 7 8 3 7 10 6 12 3 | 21 27 19 19 20 17 22 17 20 16 17
11E | 15 13 11 8 17 5 10 14 9 12 4 | 49 52 46 49 52 48 45 44 47 44 46
12 | 8 15 7 12 11 5 11 14 12 12 4 | 25 28 17 26 19 20 25 22 21 19 19
13 | 7 11 11 15 8 4 9 15 9 11 3 | 33 37 34 35 27 32 33 31 30 30 30
14 | 8 12 9 16 8 5 9 12 9 15 4 | 24 30 29 38 25 28 26 31 27 30 26
15 | 5 12 10 13 7 4 9 12 11 15 3 | 34 37 33 36 30 34 33 35 32 36 32
16 | 22 14 6 14 12 6 11 15 11 17 4 | 34 31 21 21 22 20 22 20 20 17 19
17 | 10 14 8 16 16 4 8 19 11 9 4 | 24 33 23 32 21 22 27 22 24 24 22
18 | 12 13 9 15 10 6 10 21 14 20 4 | 22 31 25 29 21 22 23 27 20 28 21
19 | 11 13 9 17 15 5 9 18 12 13 4 | 23 29 21 26 22 18 25 18 20 16 18
20 | 11 14 8 16 10 6 10 21 12 16 4 | 34 35 29 36 32 29 29 31 28 34 29
21E | 24 9 8 16 24 9 9 14 14 12 5 | 34 28 21 25 36 21 24 19 26 14 22
22 | 11 13 10 14 10 5 11 27 10 21 5 | 30 38 31 34 26 28 31 34 26 27 27
X23 | 6 8 8 10 8 4 7 12 --- --- 3 | 20 28 19 14 20 15 17 14 --- --- 16
24 | 7 13 8 8 12 4 11 15 9 13 3 | 22 26 14 24 20 20 22 29 23 23 19
25 | 11 22 7 11 8 5 11 12 7 13 4 | 22 29 16 23 21 18 24 21 19 24 19
26 | 11 13 4 8 9 4 10 16 8 11 3 | 24 32 18 21 23 23 24 28 24 27 21
27 | 9 12 5 8 6 3 10 13 7 14 3 | 22 29 12 18 15 17 24 20 19 23 16
28 | 10 14 7 15 12 6 8 13 10 10 3 | 20 30 17 26 20 19 23 21 17 16 18
29 | 11 15 6 15 12 4 11 13 13 20 4 | 29 30 21 27 23 23 27 20 27 21 22
30 | 11 15 4 8 14 3 10 13 9 7 3 | 20 28 11 18 22 16 22 23 19 15 15
31 | 16 11 5 13 11 3 7 15 12 15 4 | 25 25 16 27 19 19 22 21 23 23 18
32 | 8 14 7 9 8 4 11 8 6 14 3 | 39 49 42 44 39 43 45 48 42 48 42
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 14 8 12 12 5 11 15 11 14 |T 34 39 30 34 32 30 34 32 32 32 31
WRMS | 11 14 8 12 10 5 11 15 9 13 |NE 27 32 22 27 23 23 27 25 24 25 24
MEDI | 10 13 7 12 10 4 10 14 10 13 |MD 25 31 21 26 22 22 25 23 24 24 21
Table 3.1932.4 GPS week: 1932 Day: 4 MJD: 57772.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 11 7 9 12 5 12 11 10 9 3 | 48 53 46 51 45 50 51 49 51 51 48
2E | 12 11 5 10 18 5 12 17 9 16 4 | 38 39 31 29 39 32 38 39 35 35 33
3 | 7 5 6 6 8 5 8 6 5 15 2 | 20 26 15 17 21 17 25 20 20 29 19
X4 | 3 --- --- --- --- 57 --- --- --- --- 0 | 42 --- --- --- --- 47 --- --- --- --- 41
5 | 9 11 10 18 10 5 9 18 12 20 4 | 35 42 36 29 34 31 42 27 33 36 33
6E | 9 12 9 13 37 9 12 13 12 12 5 | 92 91 87 84 101 86 87 89 87 86 88
7 | 8 11 4 9 11 4 11 14 11 17 3 | 30 27 19 23 21 22 27 24 27 17 22
8 | 12 12 3 9 8 3 11 13 11 11 3 | 25 28 12 15 15 17 25 20 22 22 18
9 | 8 10 5 10 11 4 11 9 8 14 3 | 41 46 37 39 34 38 45 37 39 40 39
10 | 6 10 5 9 9 4 6 14 9 7 3 | 20 27 17 18 20 17 22 23 21 19 18
11E | 15 12 10 8 16 4 8 10 12 12 4 | 87 89 87 87 86 87 89 87 92 85 87
12 | 10 15 6 13 15 4 9 13 11 14 4 | 27 29 16 25 22 19 26 21 20 21 19
13 | 10 11 10 13 7 3 9 12 10 11 3 | 27 32 26 25 24 25 30 27 26 25 25
14 | 7 10 7 20 6 5 8 10 10 13 3 | 30 31 25 44 22 29 28 29 24 30 27
15 | 7 12 8 10 6 4 10 12 11 16 3 | 32 34 29 31 27 31 30 31 30 38 30
16 | 22 9 5 14 15 6 10 13 12 17 4 | 35 27 18 20 22 19 24 19 18 16 19
17 | 7 14 7 17 14 3 10 16 12 11 4 | 20 31 19 31 23 20 27 20 21 20 20
18 | 11 11 8 16 10 4 9 22 14 20 4 | 26 29 22 26 21 20 25 27 17 25 20
19 | 7 15 7 18 16 5 12 16 12 15 4 | 22 29 18 28 26 19 27 20 17 22 20
20 | 8 11 9 15 8 5 10 17 12 16 4 | 29 30 24 30 25 24 28 26 26 27 25
21E | 10 7 6 10 8 6 8 8 10 9 3 | 20 21 14 13 18 14 18 17 18 18 15
22 | 11 8 9 13 11 7 9 26 10 19 4 | 31 34 28 29 25 25 29 29 24 24 25
X23 | 9 9 9 9 8 4 8 11 8 --- 3 | 22 19 18 11 16 15 15 14 11 --- 17
24 | 8 10 6 6 7 4 9 15 5 12 3 | 25 24 11 21 16 18 22 28 22 22 18
25 | 9 20 4 8 7 5 11 9 4 14 3 | 24 30 14 24 19 20 25 19 21 23 19
26 | 14 9 4 10 10 4 10 12 9 12 3 | 29 27 17 19 21 21 26 24 21 24 20
27 | 8 8 5 9 7 4 11 12 10 13 3 | 22 28 13 16 17 18 25 20 21 23 18
28 | 8 11 6 14 11 3 7 13 9 13 3 | 20 26 15 24 21 17 23 20 17 13 17
29 | 15 13 6 16 9 5 10 14 12 21 4 | 32 28 19 26 24 22 26 19 23 23 22
30 | 8 12 5 8 17 4 9 13 10 8 3 | 24 22 13 19 23 18 24 24 23 17 18
31 | 9 11 5 11 12 5 8 15 10 15 3 | 25 30 16 24 21 20 25 21 23 29 20
32 | 8 12 5 6 7 4 9 9 6 10 2 | 39 45 37 43 36 40 43 45 40 43 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 7 12 13 5 10 14 10 14 |T 32 34 25 29 28 28 32 29 28 30 28
WRMS | 10 11 6 11 10 4 10 14 9 14 |NE 27 30 20 25 22 23 27 24 23 25 23
MEDI | 9 11 6 10 10 4 9 13 10 13 |MD 27 29 19 25 22 20 26 24 23 24 20
Table 3.1932.5 GPS week: 1932 Day: 5 MJD: 57773.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 13 9 9 8 18 9 9 11 7 14 3 | 45 49 42 47 40 46 50 44 46 49 44
2E | 13 10 5 11 17 4 9 15 10 15 4 | 37 38 31 31 37 33 33 38 31 37 31
3 | 8 10 5 10 8 5 7 9 5 16 3 | 19 24 12 14 16 15 21 18 16 29 14
X4 | 2 --- --- --- --- 52 --- --- --- --- 0 | 30 --- --- --- --- 43 --- --- --- --- 29
5 | 9 9 10 13 8 4 9 19 12 20 4 | 32 37 30 25 26 28 34 26 27 32 28
6E | 6 10 10 12 24 5 10 12 8 11 4 | 108 110 109 109 111 110 109 113 110 112 109
7 | 9 11 5 10 14 5 9 16 11 15 3 | 26 26 17 22 24 21 23 22 23 17 19
8 | 11 8 5 8 10 5 9 13 7 13 3 | 22 28 13 19 16 19 25 20 20 25 18
9 | 8 10 6 8 8 5 11 10 8 14 3 | 39 45 34 38 34 35 44 33 36 39 36
10 | 8 9 5 12 8 5 8 18 5 14 3 | 21 28 18 18 19 19 24 24 18 22 17
11E | 23 12 9 9 17 7 9 12 8 14 4 | 113 113 111 114 110 112 115 110 112 111 112
12 | 12 13 5 17 19 4 8 19 13 15 4 | 28 31 16 29 30 21 26 24 23 24 21
13 | 9 9 9 17 9 5 10 16 12 14 4 | 27 31 26 27 31 25 29 25 22 27 24
14 | 8 11 7 22 7 5 8 12 11 13 4 | 26 29 26 42 24 27 27 26 26 26 25
15 | 5 11 10 11 6 4 10 13 10 15 3 | 27 29 26 29 27 26 27 26 26 29 24
16 | 19 11 6 17 19 7 10 14 11 18 5 | 33 30 20 24 31 22 23 19 22 19 20
17 | 9 13 8 17 13 4 9 19 12 13 4 | 21 32 21 28 22 21 25 18 23 22 20
18 | 11 8 9 18 13 5 11 22 16 22 5 | 23 27 19 23 22 17 22 23 15 25 16
19 | 8 13 7 20 14 4 10 18 13 16 4 | 20 30 18 27 21 19 24 17 19 21 18
20 | 10 10 8 17 10 6 8 18 13 17 4 | 25 27 19 24 24 19 23 21 18 26 19
21E | 24 7 8 15 24 7 8 12 15 13 5 | 33 26 18 17 31 19 16 21 21 19 18
22 | 9 15 8 14 13 4 7 26 11 23 5 | 27 34 26 28 26 24 28 27 25 25 24
23 | 9 8 9 8 8 3 6 12 8 18 3 | 21 20 16 11 15 14 15 13 12 14 14
24 | 8 10 7 10 10 6 10 18 10 16 3 | 21 26 14 26 22 21 23 29 26 23 20
25 | 8 19 6 8 10 3 10 12 6 12 3 | 22 30 15 24 21 20 24 23 20 28 19
26 | 9 11 4 11 16 4 9 11 7 14 3 | 24 30 17 22 26 23 25 26 24 27 21
27 | 9 9 5 9 10 5 10 12 8 17 3 | 20 27 13 19 18 19 25 20 22 28 18
28 | 8 15 7 14 12 5 8 14 10 12 4 | 21 31 19 24 21 20 25 21 20 16 18
29 | 11 10 7 13 11 4 9 15 12 26 4 | 29 31 21 26 27 23 25 21 22 29 22
30 | 7 11 5 10 17 3 10 15 13 9 3 | 23 22 11 19 23 17 23 23 22 17 17
31 | 12 12 6 12 10 5 7 14 11 15 3 | 20 27 18 23 21 18 24 16 21 24 18
32 | 9 9 5 9 6 3 9 13 7 11 3 | 27 39 26 34 27 29 36 35 30 31 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 7 13 13 5 9 15 10 16 |T 31 35 26 31 30 28 32 29 28 31 27
WRMS | 10 11 7 12 11 5 9 15 9 14 |NE 24 29 19 24 23 22 25 22 22 24 21
MEDI | 9 10 7 12 11 5 9 14 10 15 |MD 26 30 19 25 24 21 25 23 22 26 20
Table 3.1932.6 GPS week: 1932 Day: 6 MJD: 57774.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 14 8 8 8 12 6 7 11 9 6 3 | 42 44 34 43 39 41 44 40 45 42 40
2E | 13 9 5 11 19 4 8 15 9 13 4 | 43 40 36 37 35 37 40 37 39 42 38
3 | 14 7 6 8 8 4 6 9 7 18 3 | 26 25 17 20 19 20 28 20 23 34 22
X4 | 4 --- --- --- --- 40 --- --- --- --- 0 | 34 --- --- --- --- 32 --- --- --- --- 33
5 | 10 9 11 16 12 6 10 21 11 19 4 | 45 46 43 34 38 38 48 33 41 42 40
6E | 17 10 8 11 32 4 9 10 6 8 4 | 113 113 108 110 117 111 110 110 112 113 111
7 | 13 11 5 13 13 3 11 16 9 15 4 | 36 24 20 29 22 23 28 24 23 22 23
8 | 13 8 7 7 11 4 9 13 7 11 3 | 25 27 16 19 17 19 25 22 19 25 20
9 | 10 9 6 7 10 4 8 11 7 11 3 | 55 58 50 54 50 53 57 51 52 55 53
10 | 15 9 7 7 7 4 7 14 7 8 3 | 29 28 16 18 18 18 28 16 23 19 20
11 | 16 13 8 7 16 7 8 11 8 12 3 | 52 56 50 52 52 51 55 50 52 49 51
12 | 16 11 9 15 17 4 9 17 15 14 4 | 32 30 18 27 25 21 28 23 22 20 21
13 | 10 9 10 17 7 4 9 18 11 10 4 | 34 39 32 39 31 34 37 36 32 33 33
14 | 13 8 8 18 6 4 9 14 8 14 4 | 31 30 28 43 30 31 29 35 29 33 30
15 | 7 9 11 12 6 4 8 13 9 16 3 | 38 39 38 42 38 40 38 39 36 41 37
16 | 23 10 5 14 18 5 11 13 11 14 4 | 33 24 19 22 29 20 23 21 21 18 20
17 | 18 9 8 17 20 3 7 19 12 10 4 | 32 33 24 33 23 25 29 26 26 25 25
18 | 15 11 8 13 12 4 11 21 15 19 4 | 28 29 23 26 24 21 27 27 22 27 22
19 | 16 11 10 18 18 4 11 20 12 14 5 | 27 30 19 27 22 21 30 24 21 21 21
20 | 12 10 9 14 7 6 11 16 12 13 4 | 35 30 26 34 29 28 30 29 28 33 28
21E | 15 7 7 12 21 5 9 10 11 10 4 | 26 23 15 17 26 16 22 17 21 15 18
22 | 12 8 10 11 12 5 7 25 11 16 4 | 33 37 31 33 28 30 32 36 30 30 30
23 | 10 6 10 8 9 3 6 11 7 13 3 | 22 16 16 12 14 14 14 13 12 9 16
24 | 11 9 9 7 9 3 8 17 5 11 3 | 27 25 11 22 18 19 24 29 21 20 20
25 | 16 17 5 8 8 4 10 12 10 8 3 | 26 28 15 24 19 20 26 20 22 23 20
26 | 17 10 4 11 12 3 7 11 9 11 3 | 32 30 21 23 27 24 27 30 26 25 25
27 | 11 8 6 8 11 4 9 10 6 10 3 | 22 28 16 17 16 19 26 19 19 23 19
28 | 22 11 8 15 19 4 6 14 9 10 4 | 29 27 18 28 25 19 24 25 21 15 20
29 | 19 15 9 15 10 5 10 14 13 17 4 | 34 29 20 28 22 22 27 21 23 22 22
30 | 20 8 5 9 17 4 10 16 6 7 3 | 34 24 13 21 23 18 25 25 23 19 20
31 | 13 10 8 11 11 4 9 16 10 13 3 | 24 27 16 24 19 20 24 19 23 22 19
32 | 20 8 5 9 9 3 8 12 6 10 3 | 46 53 45 50 51 49 51 58 49 55 49
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 10 8 12 14 4 9 15 10 13 |T 35 35 27 32 30 29 34 31 30 31 30
WRMS | 15 10 8 12 11 4 9 14 8 12 |NE 32 31 23 28 26 25 30 27 26 27 26
MEDI | 14 9 8 11 12 4 9 14 9 12 |MD 32 30 20 28 25 22 28 26 23 25 22
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 4.1932 GPS week: 1932 MJD: 57768.0-57774.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2962 |U 4 5 10 |U 11 13 34 |U 7 7 15 |
emr | emr 2962 | 6 6 13 |U 13 20 40 | 7 7 18 |
esa | esa 2962 | 5 5 11 |U 13 20 42 | 8 9 20 |
gfz | gfz 2962 |U 5 5 11 |U 12 20 39 |U 7 8 17 |
grg | grg 2962 |U 6 7 12 |U 13 20 43 | 8 9 20 |
igr | igr 2961 | 5 5 10 | 11 13 36 | 7 8 16 |
igs | igs 2962 | 5 5 10 | 13 20 40 | 7 8 17 |
jpl | jpl 2962 | 6 7 13 |U 13 19 41 | 8 8 19 |
mit | mit 2962 | 5 5 11 |U 16 25 49 |U 10 10 22 |
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 5.1932.0 GPS week: 1932 Day: 0 MJD: 57768.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 6 9 | 20 16 57 | 5 4 14 |
emr | emr 2976 | 7 8 15 | 22 19 57 | 7 6 17 |
esa | esa 2976 | 6 7 12 | 19 18 59 | 8 8 20 |
gfz | gfz 2976 | 7 7 10 | 17 18 53 | 6 7 17 |
grg | grg 2976 | 8 9 13 | 21 17 60 | 8 8 20 |
igr | igr 2976 | 6 7 11 | 18 17 50 | 6 5 15 |
igs | igs 2976 | 6 7 11 | 19 17 56 | 6 6 16 |
jpl | jpl 2976 | 6 9 13 | 19 18 58 | 7 8 18 |
mit | mit 2976 | 7 5 12 | 19 18 57 | 8 11 21 |
Table 5.1932.1 GPS week: 1932 Day: 1 MJD: 57769.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 6 12 | 9 11 21 | 6 5 15 |
emr | emr 2976 | 6 8 14 | 11 10 24 | 6 4 19 |
esa | esa 2976 | 5 7 12 | 11 11 25 | 6 6 23 |
gfz | gfz 2976 | 6 6 9 | 10 11 21 | 6 5 20 |
grg | grg 2976 | 6 8 13 | 9 12 20 | 6 4 18 |
igr | igr 2976 | 5 7 11 | 11 10 23 | 5 5 18 |
igs | igs 2976 | 5 7 11 | 10 10 22 | 6 4 18 |
jpl | jpl 2976 | 6 10 13 | 11 10 23 | 7 5 19 |
mit | mit 2976 | 5 6 10 | 16 12 31 | 6 5 18 |
Table 5.1932.2 GPS week: 1932 Day: 2 MJD: 57770.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 5 5 11 | 17 20 42 | 7 12 17 |
emr | emr 2880 | 7 6 15 | 18 18 46 | 7 10 20 |
esa | esa 2880 | 5 6 12 | 16 18 46 | 7 11 19 |
gfz | gfz 2879 | 5 5 11 | 16 18 46 | 7 11 19 |
grg | grg 2880 | 6 7 12 | 15 16 46 | 8 10 19 |
igr | igr 2880 | 5 4 11 | 17 18 44 | 6 11 17 |
igs | igs 2880 | 5 5 11 | 16 18 44 | 7 12 19 |
jpl | jpl 2880 | 7 7 13 | 16 15 41 | 8 12 21 |
mit | mit 2880 | 5 5 11 | 16 16 45 | 7 11 19 |
Table 5.1932.3 GPS week: 1932 Day: 3 MJD: 57771.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 6 10 | 8 9 32 | 7 10 18 |
emr | emr 2976 | 7 7 12 | 11 12 33 | 8 11 23 |
esa | esa 2976 | 5 6 11 | 10 10 38 | 8 14 25 |
gfz | gfz 2976 | 4 6 12 | 9 11 37 | 9 11 21 |
grg | grg 2976 | 5 8 11 | 10 12 35 | 7 12 23 |
igr | igr 2976 | 5 7 11 | 10 11 39 | 9 13 19 |
igs | igs 2975 | 5 6 9 | 10 11 35 | 7 12 22 |
jpl | jpl 2976 | 5 9 12 | 11 12 39 | 9 13 26 |
mit | mit 2976 | 5 6 10 | 20 38 57 | 8 11 22 |
Table 5.1932.4 GPS week: 1932 Day: 4 MJD: 57772.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 3 3 9 | 6 12 27 | 8 7 14 |
emr | emr 2976 | 5 4 11 | 17 55 52 | 8 7 15 |
esa | esa 2976 | 4 3 9 | 18 57 58 | 9 8 19 |
gfz | gfz 2976 | 3 2 8 | 16 55 59 | 8 7 15 |
grg | grg 2976 | 4 6 10 | 21 59 70 | 10 9 21 |
igr | igr 2972 | 3 3 8 | 6 12 32 | 9 6 18 |
igs | igs 2976 | 4 3 9 | 18 58 58 | 8 7 15 |
jpl | jpl 2976 | 4 5 11 | 19 54 56 | 9 6 18 |
mit | mit 2976 | 4 3 9 | 21 61 61 | 10 10 17 |
Table 5.1932.5 GPS week: 1932 Day: 5 MJD: 57773.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 4 4 10 | 6 10 37 | 8 8 14 |
emr | emr 2976 | 6 6 15 | 7 12 35 | 9 8 18 |
esa | esa 2976 | 5 4 12 | 6 12 39 | 9 9 20 |
gfz | gfz 2976 | 4 4 11 | 6 10 32 | 8 9 16 |
grg | grg 2976 | 6 5 11 | 7 12 40 | 11 12 27 |
igr | igr 2976 | 5 4 11 | 5 11 33 | 8 8 17 |
igs | igs 2976 | 5 5 12 | 6 11 35 | 8 8 17 |
jpl | jpl 2976 | 6 6 15 | 6 12 40 | 10 7 16 |
mit | mit 2976 | 6 7 16 | 9 13 58 | 12 14 32 |
Table 5.1932.6 GPS week: 1932 Day: 6 MJD: 57774.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 3 4 7 | 9 15 27 | 6 6 12 |
emr | emr 2976 | 4 5 10 | 8 13 33 | 7 5 14 |
esa | esa 2976 | 4 3 8 | 10 14 30 | 7 7 15 |
gfz | gfz 2976 | 7 9 15 | 9 15 29 | 6 6 14 |
grg | grg 2976 | 5 6 11 | 9 14 30 | 7 5 15 |
igr | igr 2976 | 4 4 8 | 9 14 29 | 6 5 13 |
igs | igs 2976 | 4 5 8 | 9 14 28 | 7 5 12 |
jpl | jpl 2976 | 5 4 11 | 10 14 30 | 8 6 14 |
mit | mit 2976 | 5 4 8 | 11 16 34 | 19 9 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 6.1932 GPS week: 1932 MJD: 57768.500-57774.500
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 | -7 12 63 8 4 | -3 16
| 12 22 62 144 4 | 2
emr uuuuu | 42 9 -54 68 4 | 36 41
| 38 21 79 83 9 | 3
esa uuuuu | -16 -23 31 36 3 | 6 16
| 15 11 55 39 6 | 2
gfz uuuuu | 1 -13 35 -20 -3 | 6 15
| 28 10 134 97 5 | 1
grg uuuuu | -22 -7 -18 66 -3 | -1 15
| 36 27 26 83 11 | 2
igr xxxxx | -38 32 -4 44 2 | 0 14
| 13 11 59 25 9 | 3
irf xxxxx | 18 -9 -20 -60 -2 | 4 16
| 15 16 23 34 3 | 2
jpl uuuuu | -28 -26 -75 39 4 | 23 30
| 47 44 129 118 9 | 3
mit uuuuu | -7 7 -7 -203 8 | 17 23
| 28 15 54 29 5 | 4
ngs uuuuu | 30 21 5 -12 -6 | 2 13
| 55 29 176 69 5 | 2
sio uuxux | 22 51 -345 -125 -3 | 46 48
| 19 18 88 56 10 | 2
Table 7.1932.0 GPS week: 1932 Day: 0 MJD: 57768.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -17 -7 109 121 1 | -4 21
emr uuuuu | 32 3 -103 121 -3 | 32 42
esa uuuuu | -42 -6 81 101 -9 | 5 20
gfz uuuuu | -11 -28 294 -107 -11 | 6 21
grg uuuuu | 10 -39 21 -119 20 | -3 17
igr xxxxx | -39 21 -78 14 -6 | -5 20
irf xxxxx | 9 -7 -57 -121 -1 | 2 20
jpl uuuuu | -2 -73 -30 -14 0 | 21 31
mit uuuuu | -54 8 -102 -228 3 | 13 21
ngs uuuuu | 78 74 -269 -2 -10 | 3 18
sio uuxux | 4 56 -392 -175 -15 | 49 52
Table 7.1932.1 GPS week: 1932 Day: 1 MJD: 57769.500
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 35 96 162 6 | -2 19
emr uuuuu | 20 25 -166 57 -3 | 37 42
esa uuuuu | -16 -29 105 38 0 | 7 19
gfz uuuuu | -35 -19 -24 -152 -5 | 8 20
grg uuuuu | 9 -16 -19 90 0 | 2 16
igr xxxxx | -54 40 -65 65 6 | -1 14
irf xxxxx | -6 -31 -12 -71 -2 | 5 17
jpl uuuuu | -72 -43 -150 58 -4 | 24 32
mit uuuuu | -37 -12 54 -223 12 | 15 21
ngs uuuuu | 104 46 45 -74 -6 | 5 16
sio uuxux | 14 13 -396 -86 -9 | 49 52
Table 7.1932.2 GPS week: 1932 Day: 2 MJD: 57770.500
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 | 5 -10 128 185 8 | -4 14
emr uuuuu | 17 18 -132 13 -1 | 35 39
esa uuuuu | -10 -16 6 70 5 | 5 12
gfz uuuuu | 1 2 -55 -83 4 | 5 13
grg uuuuu | 7 -26 -27 75 -5 | 0 13
igr xxxxx | -31 22 -54 23 20 | -2 12
irf xxxxx | 26 -23 -35 -77 0 | 3 14
jpl uuuuu | -104 -4 -215 -202 -4 | 21 27
mit uuuuu | 8 3 -44 -182 8 | 15 20
ngs uuuuu | 71 3 254 84 -7 | 2 10
sio uuxux | 15 64 -471 -187 -13 | 45 46
Table 7.1932.3 GPS week: 1932 Day: 3 MJD: 57771.500
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 2 83 -44 8 | -5 14
emr uuuuu | 116 34 31 222 -4 | 34 38
esa uuuuu | -19 -29 59 -8 11 | 3 12
gfz uuuuu | -19 -10 -33 -17 -3 | 5 13
grg uuuuu | -13 -29 -61 107 -9 | -2 14
igr xxxxx | -34 25 25 43 3 | 0 11
irf xxxxx | 13 -6 -30 -18 0 | 3 14
jpl uuuuu | 7 23 -184 152 3 | 21 26
mit uuuuu | -3 12 -7 -194 13 | 14 20
ngs uuuuu | -16 -8 71 -127 -11 | 0 11
sio uuxux | 10 55 -336 -94 1 | 43 44
Table 7.1932.4 GPS week: 1932 Day: 4 MJD: 57772.500
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 34 52 -106 3 | -3 15
emr uuuuu | 69 -31 -8 76 21 | 36 40
esa uuuuu | -24 -39 18 -3 7 | 6 15
gfz uuuuu | -1 -6 -94 44 -5 | 6 14
grg uuuuu | -40 13 -30 87 -10 | -1 14
igr xxxxx | -42 26 36 20 -3 | 2 13
irf xxxxx | 31 -6 -11 -44 -1 | 5 15
jpl uuuuu | 23 18 -119 76 21 | 23 28
mit uuuuu | 11 -12 8 -154 12 | 18 24
ngs uuuuu | -1 17 139 -6 -4 | 1 11
sio uuxux | 11 43 -224 -33 9 | 44 46
Table 7.1932.5 GPS week: 1932 Day: 5 MJD: 57773.500
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 36 -55 -104 5 | -3 15
emr uuuuu | 14 15 17 -28 7 | 38 42
esa uuuuu | -9 -15 -59 30 5 | 6 15
gfz uuuuu | 51 -14 122 91 1 | 5 14
grg uuuuu | -41 31 -5 95 -6 | -2 15
igr xxxxx | -16 46 48 74 -3 | 3 12
irf xxxxx | 38 22 17 -34 -3 | 5 15
jpl uuuuu | -2 -90 143 109 10 | 26 31
mit uuuuu | 23 25 49 -205 6 | 20 26
ngs uuuuu | -46 13 -144 17 -5 | 0 11
sio uuxux | 56 70 -238 -144 10 | 44 46
Table 7.1932.6 GPS week: 1932 Day: 6 MJD: 57774.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 14 -8 26 -162 -4 | 0 14
emr uuuuu | 24 0 -13 16 9 | 41 45
esa uuuuu | 7 -23 6 22 4 | 8 16
gfz uuuuu | 22 -16 36 86 1 | 7 14
grg uuuuu | -86 16 -7 128 -8 | 0 13
igr xxxxx | -51 47 62 66 -4 | 4 12
irf xxxxx | 18 -8 -14 -54 -9 | 7 14
jpl uuuuu | -48 -12 32 92 2 | 28 33
mit uuuuu | 1 25 -6 -236 -2 | 23 27
ngs uuuuu | 19 0 -60 20 5 | 0 11
sio uuxux | 42 54 -356 -155 -2 | 46 48
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