[IGSREPORT-24983] Wk 1927 IGS Final Orbits
acc at igs.org
acc at igs.org
Fri Dec 30 13:49:29 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1927 (Dec 11, 2016 - Dec 17, 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:
igs1927[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1927[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1927[0-6].cls IGS GPS clock combination summary report.
igs19277.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19277.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 | ALL | 4
0 | COD | BJNM NRIL BJNM NRIL
0 | EMR | MCM4 MCM4
0 | ESA | SYOG SYOG
0 | GFZ | BJNM FAA1 GODE BJNM GODE
0 | GRG | FAA1 GLSV MAW1 MCM4 DARW GLSV INVK MAW1 MCM4 SYOG
0 | JPL | NRIL TUVA
0 | MIT | INVK INVK
1 | ALL | 4
1 | COD | BJNM BJNM
1 | GFZ | BJNM GMSD GODE HYDE BJNM GMSD GODE HYDE
1 | GRG | CAS1 GLSV MAS1 NICO NNOR REUN SCUB SYOG CAS1 GLSV
1 | GRG | MAS1 NNOR REUN SCUB SEYG SYOG
1 | JPL | CEDU TUVA
2 | ALL | 4
2 | COD | CRO1 CEDU MAL2
2 | ESA | 11 11
2 | GFZ | CHTI FAA1 GODE KOUR REUN TLSE CHTI FAA1 GODE KOUR
2 | GFZ | MAL2 REUN TLSE
2 | GRG | CHTI COCO GLSV MCM4 REUN SYOG CHTI COCO GLSV MCM4
2 | GRG | NRMD REUN SEYG SYOG
2 | JPL | TUVA
2 | MIT | TLSE
3 | ALL | 4
3 | COD | FAA1 SYOG FAA1 REUN
3 | EMR | HERS SYOG
3 | ESA | FAA1 FAA1
3 | GFZ | CHTI HERS KERG MAL2 REUN SYOG CHTI HERS KERG REUN
3 | GFZ | SYOG
3 | GRG | CHTI GLSV MCM4 SHAO SYOG TLSE CHTI GLSV MCM4 SEYG
3 | GRG | SHAO SYOG
3 | JPL | TUVA
4 | ALL | 4
4 | COD | ALRT NRMD ALRT NKLG
4 | ESA | MAL2 SYOG MAL2
4 | GFZ | FAA1 GMSD GODE HYDE MAL2 SYOG FAA1 GMSD GODE HYDE
4 | GFZ | MAL2
4 | GRG | FAA1 GLSV SYOG ALRT FAA1 GLSV
4 | JPL | ALRT
5 | ALL | 4
5 | COD | SYOG
5 | EMR | SYOG
5 | GFZ | GODE HYDE MAL2 SUWN GODE HYDE MAL2
5 | GRG | GLSV MAL2 NRMD SYOG TLSE GLSV MAL2 NRMD SYOG
6 | ALL | 4
6 | GFZ | AUCK GMSD GODE MAL2 NRMD AUCK CEDU GMSD GODE MAL2
6 | GFZ | NRMD
6 | GRG | DRAG GLSV MAL2 MAW1 NKLG SYOG DRAG GLSV MAL2 MAW1
6 | GRG | NKLG SYOG
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 orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | SIO | 27
7. 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.
8. 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 | -1.8 -.3 -2.7 13 17 -6 .76
EMR | 0 | 1.9 7.0 13.9 78 -17 40 .99
ESA | 0 | -.6 -.6 -1.7 2 -14 19 .37
GFZ | 0 | .1 -.3 -1.1 -27 -118 -18 .82
GRG | 0 | 5.1 3.9 -8.2 44 50 -54 .36
JPL | 0 | -1.0 5.4 4.1 -51 47 1 .28
MIT | 0 | 6.4 1.2 15.6 16 -18 -15 .78
NGS | 0 | -4.9 -2.1 17.8 -46 -3 -39 .65
SIO | 0 | -1.0 .8 32.1 -13 65 -51 .59
COD | 1 | -1.2 -.4 -1.9 13 8 28 .43
EMR | 1 | -2.2 1.4 19.2 83 -3 29 .98
ESA | 1 | -1.1 .3 -1.0 11 -7 36 .24
GFZ | 1 | 1.1 .2 -.6 -27 -129 -20 .60
GRG | 1 | -.1 3.2 7.5 17 65 -40 .44
JPL | 1 | 2.3 4.8 5.7 -56 46 32 .57
MIT | 1 | 3.4 1.2 17.8 20 -4 -79 .76
NGS | 1 | -1.4 2.9 19.8 -40 -17 -32 .72
SIO | 1 | 2.7 -1.7 34.3 -10 -1 18 .77
COD | 2 | -.7 -.8 -2.4 -23 9 -24 .62
EMR | 2 | -1.1 2.2 14.7 75 -13 35 1.09
ESA | 2 | -1.3 .1 -.9 40 -9 36 .26
GFZ | 2 | .7 -.1 -.6 -24 -120 -16 .79
GRG | 2 | .6 3.7 9.1 12 20 -90 .61
JPL | 2 | 4.1 4.9 15.9 -11 32 10 .32
MIT | 2 | 5.0 3.3 14.9 52 -10 -46 .78
NGS | 2 | -2.0 2.1 13.5 -21 -26 -32 .82
SIO | 2 | 4.8 -2.3 32.5 -35 -24 -7 .79
COD | 3 | -1.3 -.9 -3.9 -25 33 -10 .61
EMR | 3 | 4.0 -4.0 10.5 88 -19 35 .91
ESA | 3 | -.5 -.4 -1.0 5 -3 4 .21
GFZ | 3 | .6 .2 -.9 -34 -109 -36 .65
GRG | 3 | 2.9 2.9 -1.9 43 35 -73 .46
JPL | 3 | 6.6 3.1 14.9 -5 50 -30 .54
MIT | 3 | 6.1 .3 12.3 21 -18 -46 .39
NGS | 3 | .8 -.5 23.8 -134 -20 -35 .91
SIO | 3 | 5.7 2.9 37.3 -15 1 -103 .81
COD | 4 | -2.3 -.6 -2.8 -28 55 6 .44
EMR | 4 | 3.8 2.2 22.4 76 -9 42 .75
ESA | 4 | -.2 -.6 -1.6 14 -2 -12 .32
GFZ | 4 | .6 -.3 -.3 -27 -88 -29 .69
GRG | 4 | 6.9 5.7 8.0 32 47 -66 .20
JPL | 4 | 7.3 2.0 15.8 -7 47 18 .50
MIT | 4 | 6.7 2.3 14.5 34 -10 -67 .72
NGS | 4 | 2.8 .6 16.1 -58 -34 -21 .70
SIO | 4 | 8.5 -.6 31.9 -37 14 -85 .52
COD | 5 | -2.1 -.9 -3.5 -27 28 14 .41
EMR | 5 | 4.8 1.6 13.6 78 -20 42 .93
ESA | 5 | -.6 .3 .2 66 -30 32 .46
GFZ | 5 | .2 -.3 -1.4 -26 -100 -26 .67
GRG | 5 | 6.9 3.2 -6.5 47 54 -52 .14
JPL | 5 | 6.3 7.7 12.8 -45 58 26 .54
MIT | 5 | 7.1 1.6 12.4 27 -24 -44 .74
NGS | 5 | .5 .2 18.6 -86 -29 -15 .88
SIO | 5 | 6.3 -.7 28.6 1 -3 -16 .87
COD | 6 | -2.2 -1.2 -4.5 -36 60 5 .43
EMR | 6 | 1.6 4.6 12.7 89 -19 33 .81
ESA | 6 | .2 .1 .3 31 -25 10 .11
GFZ | 6 | .8 -.4 -.3 -23 -107 -15 .48
GRG | 6 | 10.3 4.9 -2.1 90 23 -48 .41
JPL | 6 | 4.3 1.6 10.9 -43 54 13 .67
MIT | 6 | 7.1 1.1 15.5 41 -30 -51 .80
NGS | 6 | 1.6 1.7 13.7 -38 -24 -13 .36
SIO | 6 | 8.3 -1.7 34.0 -13 8 -1 .86
9. 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.
10. 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 1.1927.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1927.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 2.1927.[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 3.1927.[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 5.1927.0-6). 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 1927 summary. (Dec 11, 2016 - Dec 17, 2016)
Table 1.1927.a GPS week: 1927 MJD: 57733.000-57739.000
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 236| 0 1 -6 1 5 13 .11 11 10 | -947 -389 13 115
| 0 0 1 24 15 15 .03 | 156 275
emr 80| 0 -2 5 -21 -18 -7 .26 12 11 | 2002 -186 18 120
| 1 2 1 13 26 30 .02 | 956 1136
esa 149| 0 0 2 20 6 27 -.43 7 7 | -738 64 9 160
| 0 0 1 13 7 14 .03 | 1195 1264
gfz 196| -1 0 -4 3 -17 -3 .18 11 10 | -438 6 11 138
| 0 0 1 18 15 15 .04 | 243 201
grg 115| 0 0 -7 0 27 12 -.39 15 13 | 98 39 26 181
| 0 1 5 10 18 20 .03 | 244 457
igr n/a| 0 0 -2 -5 29 3 .01 4 4 | 18959 142 16 87
| 0 0 0 12 4 12 .03 | 1034 1019
jpl 80| 0 1 7 -2 59 -12 .31 11 11 | 1814 -95 14 101
| 0 0 2 27 11 23 .01 | 954 891
mit 350| 0 0 -5 1 -34 -30 -.00 13 12 | 526 -875 47 356
| 1 0 0 22 23 21 .03 | 2688 1790
ngs 208| 0 0 6 -10 -5 0 .17 10 9 | -1848 139 1114 2278
| 0 0 3 24 27 11 .04 | 2531 1913
sio 297| 0 -2 -7 -19 -22 -24 -.05 15 13 | --- --- --- ---
| 0 0 2 52 13 30 .03 | --- ---
Table 1.1927.b GPS week : 1927 MJD: 57733.000-57739.000
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 | 3 3 4 4 4 4 4 |
2 | 5 4 4 4 4 4 4 |
3 | 4 4 3 3 4 4 4 |
4 | 14 17 12 10 20 23 18 |
5 | 4 3 3 3 3 3 3 |
6 | 3 4 3 4 4 3 3 |
7 | 5 5 5 4 5 4 5 |
8 | 4 4 4 4 5 4 4 |
9 | 3 4 3 4 3 3 4 |
10 | 3 3 3 3 3 3 3 |
11 | 4 5 4 4 4 4 4 |
12 | 4 4 4 4 4 4 4 |
13 | 4 4 4 5 5 4 4 |
14 | 4 5 5 4 4 6 5 |
15 | 4 5 5 5 5 5 5 |
16 | 5 5 5 5 5 4 4 |
17 | 4 5 4 5 5 5 4 |
18 | 4 4 4 4 3 3 3 |
19 | 5 4 4 5 5 5 5 |
20 | 4 4 4 5 4 4 4 |
21 | 4 4 5 4 4 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 3 4 7 4 5 5 |
25 | 5 3 4 3 4 4 3 |
26 | 4 3 3 4 3 3 3 |
27 | 4 4 3 3 3 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 4 4 4 4 4 3 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 2.1927.0 GPS week: 1927 Day: 0 MJD: 57733.000
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 238| -1 2 -2 17 20 29 .15 10 10 | -892 -597 14 114
emr 80| 2 -1 5 -41 24 -60 .23 11 11 | 2056 218 15 89
esa 150| -1 0 2 17 4 32 -.43 7 7 | 268 -754 10 169
gfz 199| -1 0 -3 12 -29 10 .20 10 10 | -578 -24 10 95
grg 117| 0 -1 -10 13 46 -9 -.42 16 14 | 80 -128 24 175
igr n/a| 0 0 -3 0 26 1 .01 4 4 | 17621 1284 16 89
jpl 80| 0 0 5 -23 50 19 .30 10 10 | 1467 535 13 89
mit 350| 2 0 -7 -4 -75 -5 -.05 14 13 | -515 -539 53 363
ngs 204| -1 1 5 -9 -37 -7 .14 10 8 | -864 -625 929 2330
sio 286| 1 -1 -11 14 -11 -35 -.07 24 16 | --- --- --- ---
Table 2.1927.1 GPS week: 1927 Day: 1 MJD: 57734.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 239| 0 1 -7 44 1 22 .07 11 10 | -950 -574 13 102
emr 80| 0 0 5 -18 -3 -29 .25 10 10 | 2719 166 19 130
esa 150| -1 0 1 32 4 47 -.42 7 7 | -1864 2536 10 153
gfz 199| -1 -1 -4 17 -33 0 .21 10 11 | -232 206 12 111
grg 114| 1 -1 0 -9 23 0 -.43 15 15 | -223 984 22 168
igr n/a| 0 0 -2 7 30 -2 .02 5 5 | 19198 763 16 83
jpl 80| 1 0 4 -42 73 -8 .31 11 11 | 2402 190 14 107
mit 350| 1 0 -5 15 -27 -70 -.01 15 13 | -1457 892 46 343
ngs 202| 0 1 8 -55 -22 -21 .17 10 9 | -647 -1565 808 1871
sio 288| 0 -3 -7 1 -17 0 -.09 14 13 | --- --- --- ---
Table 2.1927.2 GPS week: 1927 Day: 2 MJD: 57735.000
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 235| 0 2 -7 7 -8 19 .14 11 10 | -941 -315 12 120
emr 80| 1 -2 6 -15 -4 -17 .26 11 11 | 2529 920 16 120
esa 144| 0 0 1 26 14 34 -.47 7 7 | 424 -835 9 186
gfz 196| -1 -1 -5 26 -22 -17 .20 10 9 | -743 287 13 171
grg 115| 1 0 -2 1 48 -9 -.41 13 13 | -18 133 27 196
igr n/a| 0 0 -3 3 31 0 .06 4 4 | 19645 947 17 106
jpl 80| 1 0 9 15 50 -17 .30 11 11 | 2282 839 13 95
mit 350| 1 1 -4 -15 -11 -37 -.03 14 12 | 6515 -4759 44 345
ngs 209| -1 1 4 1 -34 7 .21 9 8 | -7575 4316 1181 2812
sio 299| 0 -2 -7 -97 -24 1 -.04 14 14 | --- --- --- ---
Table 2.1927.3 GPS week: 1927 Day: 3 MJD: 57736.000
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 236| 0 3 -6 -28 -1 28 .07 12 10 | -1059 -322 12 106
emr 80| 2 -7 1 -38 -21 24 .28 17 15 | 3168 -1119 21 108
esa 150| 0 1 1 7 0 12 -.39 7 7 | -2709 105 11 145
gfz 195| -1 -1 -6 1 -33 -14 .20 12 11 | -246 -235 11 75
grg 113| 0 0 -8 -5 22 29 -.36 13 11 | 400 -43 25 169
igr n/a| 0 0 -2 -29 36 5 -.02 5 5 | 20624 -1097 16 78
jpl 80| 1 0 10 -17 69 -35 .32 10 10 | 3291 -1176 16 110
mit 350| 0 0 -5 33 -41 -6 .00 13 12 | -373 -324 46 390
ngs 208| 0 0 12 2 4 12 .22 11 9 | -1068 -178 1425 2523
sio 293| 0 -2 -6 33 -19 -52 -.04 14 13 | --- --- --- ---
Table 2.1927.4 GPS week: 1927 Day: 4 MJD: 57737.000
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 238| -1 2 -6 -18 -1 7 .12 11 10 | -1154 101 13 131
emr 80| 0 -1 7 -6 -56 23 .24 11 11 | 1645 -833 19 118
esa 150| 0 0 2 34 5 4 -.42 7 7 | -91 -443 9 129
gfz 196| 0 0 -5 -3 -1 21 .16 11 11 | -655 -58 12 197
grg 113| 1 0 -1 -8 -7 41 -.38 14 12 | 36 -105 25 175
igr n/a| 0 0 -3 -1 25 30 .02 4 4 | 19055 -849 16 93
jpl 80| 0 2 8 36 55 -10 .31 11 11 | 1676 -810 15 101
mit 350| 0 0 -6 -32 -6 -29 -.01 13 12 | -219 -430 46 358
ngs 211| 0 0 2 20 28 0 .20 9 8 | -1144 43 989 2105
sio 306| 0 -2 -9 -88 -7 -65 -.08 14 14 | --- --- --- ---
Table 2.1927.5 GPS week: 1927 Day: 5 MJD: 57738.000
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 236| 0 1 -8 -5 -4 -1 .12 11 10 | -652 -734 14 121
emr 80| 0 0 5 -16 -35 -5 .29 11 11 | 1655 -1895 19 164
esa 150| 0 0 2 26 19 31 -.43 7 7 | -47 -1005 10 163
gfz 195| 0 0 -4 -30 -1 -21 .09 11 11 | -106 -225 10 142
grg 115| 0 0 -12 -8 28 5 -.35 15 13 | 455 -497 28 181
igr n/a| 0 0 -3 -9 22 -9 .00 4 4 | 18744 -837 18 79
jpl 80| 0 2 7 1 73 12 .29 10 10 | 1290 -1054 14 98
mit 350| 0 0 -6 17 -29 -36 .04 12 10 | 228 -712 45 330
ngs 213| 0 0 9 -27 -3 6 .14 10 9 | -678 -713 1173 2149
sio 305| 0 -3 -3 10 -47 -35 -.03 14 13 | --- --- --- ---
Table 2.1927.6 GPS week: 1927 Day: 6 MJD: 57739.000
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 236| 0 2 -7 -4 32 -9 .09 12 10 | -982 -288 16 113
emr 80| 0 -1 5 -10 -35 8 .26 11 11 | 245 1241 17 116
esa 150| 0 0 4 0 -2 27 -.45 7 7 | -1150 845 10 177
gfz 197| -1 0 -3 3 -2 -7 .17 11 10 | -511 95 11 181
grg 119| 1 1 -13 15 31 30 -.40 17 14 | -44 -66 32 209
igr n/a| -1 0 -1 -11 32 1 .00 5 4 | 17829 788 16 82
jpl 80| 0 1 7 14 46 -46 .31 11 11 | 294 810 14 109
mit 350| 0 -1 -4 0 -52 -27 .04 12 11 | -491 -255 55 369
ngs 209| 0 0 4 -7 28 3 .10 10 9 | -965 -301 1296 2157
sio 307| 0 -3 -5 -6 -28 15 -.03 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 3.1927.0 GPS week: 1927 Day: 0 MJD: 57733.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 9 7 8 7 4 7 13 8 18 3 | 25 28 18 28 20 22 28 32 24 32 23
2 | 13 13 10 13 12 5 11 15 12 21 4 | 28 25 20 26 19 20 23 20 21 21 19
3 | 8 13 6 13 10 5 13 9 7 12 3 | 66 64 59 65 57 61 64 68 59 65 62
X4 | 14 --- --- --- --- 58 13 --- --- --- 14 | 26 --- --- --- --- 49 19 --- --- --- 19
5 | 11 8 7 7 8 4 11 16 8 11 3 | 34 32 32 39 28 33 32 39 31 36 32
6 | 10 8 7 8 12 4 9 11 8 17 3 | 22 28 15 23 19 20 27 21 24 30 20
7E | 10 19 6 13 36 4 12 16 12 14 5 | 26 28 22 28 41 23 27 23 29 22 24
8E | 13 9 8 7 19 5 11 13 7 15 4 | 24 24 16 24 19 20 26 26 22 20 19
9 | 9 12 4 5 11 4 8 15 10 11 3 | 21 30 14 20 18 19 29 18 21 22 19
10 | 7 9 3 7 12 4 9 10 5 11 2 | 67 67 64 70 64 66 65 72 64 72 66
11 | 10 18 9 7 11 4 9 16 10 19 4 | 23 26 16 25 21 19 23 27 21 24 18
12 | 10 9 5 12 13 5 7 14 11 13 3 | 28 28 24 30 21 23 27 26 28 25 24
13 | 9 11 8 11 12 4 10 16 11 23 4 | 24 30 19 30 23 22 30 28 25 21 22
14 | 7 11 8 9 11 5 7 25 9 18 4 | 31 28 29 35 31 31 28 34 28 33 28
15 | 9 11 7 14 11 3 8 16 15 20 4 | 32 37 30 27 30 25 35 22 23 24 27
16 | 16 10 5 14 17 5 10 13 11 21 4 | 28 21 20 27 22 20 22 22 23 19 20
17E | 11 11 6 14 19 6 12 19 8 12 4 | 21 24 14 24 21 19 21 21 19 19 17
18 | 6 10 7 11 8 4 9 12 10 18 3 | 30 26 26 37 27 29 24 33 30 32 27
19E | 13 8 6 13 24 6 9 17 10 14 4 | 21 22 16 23 28 17 21 19 18 17 16
20 | 9 11 8 11 7 3 10 12 10 17 3 | 35 29 30 42 32 32 29 36 30 39 32
21 | 12 9 7 11 11 4 9 14 11 22 4 | 22 23 18 26 25 18 21 23 15 25 18
22 | 6 8 9 10 9 4 9 15 7 15 3 | 40 34 39 43 37 39 33 44 35 40 37
23 | 8 14 7 13 15 6 10 25 12 20 4 | 33 33 30 33 30 30 32 31 29 27 28
24E | 11 12 6 8 15 5 9 10 8 10 3 | 23 25 13 22 16 20 24 21 22 18 18
25 | 8 13 4 7 10 5 10 8 7 49 5 | 24 27 20 25 19 22 29 24 24 56 23
26 | 11 9 5 7 18 4 10 10 7 11 3 | 21 22 12 20 15 16 21 15 19 16 15
27E | 12 9 5 8 10 4 12 11 6 94 3 | 24 29 18 24 22 21 24 23 23 84 21
28 | 10 12 6 13 20 5 8 20 10 13 4 | 27 31 24 31 27 24 31 30 28 22 25
29E | 17 9 6 13 20 4 10 11 13 14 4 | 24 22 19 29 21 21 22 17 27 16 19
30E | 10 12 6 6 28 4 7 10 7 12 4 | 23 22 14 22 23 19 25 18 22 20 17
31E | 10 11 4 8 20 4 9 8 9 10 3 | 23 24 18 24 22 20 23 19 20 21 19
32 | 11 9 5 9 9 3 8 10 7 12 3 | 24 31 18 23 19 21 28 16 22 16 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 11 7 10 16 4 10 14 10 24 |T 28 29 23 30 26 26 28 28 26 30 24
WRMS | 10 11 7 10 14 4 10 13 8 16 |NE 30 31 26 32 27 28 30 30 28 31 27
MEDI | 10 11 6 10 12 4 9 13 9 15 |MD 24 28 19 27 22 21 27 23 24 24 20
Table 3.1927.1 GPS week: 1927 Day: 1 MJD: 57734.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 10 8 6 13 6 9 12 8 14 3 | 23 28 18 26 20 20 28 28 22 30 22
2 | 11 11 6 12 11 7 12 16 11 20 4 | 26 23 18 25 20 21 24 21 17 15 18
3 | 7 10 6 11 19 6 10 9 8 9 3 | 45 52 44 45 36 42 50 46 44 49 45
X4 | 17 --- --- --- --- 26 15 --- --- --- 16 | 39 --- --- --- --- 28 26 --- --- --- 27
5 | 6 7 6 11 11 4 9 15 9 12 3 | 25 26 22 33 18 24 23 29 24 25 24
6 | 12 8 10 7 9 5 9 18 10 13 3 | 23 27 15 22 18 19 28 21 23 25 20
7E | 13 11 6 12 23 4 15 13 12 12 4 | 26 27 21 31 34 25 28 27 28 28 24
8E | 13 9 7 5 11 4 11 10 11 11 3 | 25 26 18 27 20 23 26 27 27 24 22
9 | 9 9 8 7 11 3 10 13 11 11 3 | 23 28 20 24 19 21 30 21 24 23 22
10 | 12 9 4 6 10 4 10 9 8 10 3 | 43 50 42 46 35 44 48 46 44 48 44
X11 | 12 8 11 --- 14 5 --- 13 11 --- 5 | 23 23 18 --- 20 20 --- 22 22 --- 19
12 | 9 11 7 8 15 4 8 13 12 10 3 | 26 28 25 29 24 25 27 25 29 20 24
13 | 6 12 10 11 16 5 9 14 10 17 4 | 21 29 19 27 19 20 29 21 22 12 20
14 | 6 8 8 12 18 5 16 25 9 19 4 | 29 28 26 33 25 27 30 26 25 24 24
15 | 7 12 9 14 14 4 12 18 13 19 4 | 28 34 28 28 28 25 33 23 27 24 26
16 | 20 12 8 14 15 5 9 14 14 19 4 | 28 24 19 26 22 20 21 20 23 20 19
17E | 13 12 5 14 15 5 13 21 12 10 4 | 23 27 16 28 22 20 24 22 22 19 19
18 | 9 10 7 12 11 4 9 10 10 15 3 | 23 25 25 36 19 27 26 30 30 23 25
19E | 19 7 7 10 12 5 8 19 11 11 4 | 26 24 20 25 23 19 22 22 23 19 20
20 | 7 12 7 13 9 4 11 14 11 18 4 | 26 22 24 36 20 25 22 29 28 28 25
21 | 11 9 6 11 22 4 8 13 10 15 4 | 22 23 18 24 25 19 24 23 19 19 19
22 | 7 7 11 12 14 4 10 15 10 10 3 | 33 33 35 37 33 31 31 33 29 33 32
23 | 8 12 10 11 15 6 13 27 11 18 5 | 31 33 29 30 25 26 31 26 23 24 25
24E | 14 9 6 6 8 5 9 10 8 12 3 | 25 23 18 28 18 22 24 24 24 20 21
25 | 10 15 5 6 9 4 10 7 7 12 3 | 28 31 25 29 23 25 30 25 27 22 25
26 | 15 9 6 7 13 6 10 7 7 11 3 | 24 22 15 21 16 18 24 17 19 21 18
27E | 15 11 6 7 13 6 12 11 6 12 3 | 29 27 24 31 25 25 28 29 26 32 25
28 | 8 10 10 11 14 5 12 21 13 11 4 | 27 32 25 29 27 26 30 28 30 24 26
29E | 18 12 6 15 24 6 9 12 14 11 4 | 23 18 16 26 29 19 19 14 24 15 17
30E | 11 9 6 10 24 4 10 11 8 13 4 | 21 21 14 22 23 20 24 20 21 24 18
31E | 12 11 4 11 23 5 8 10 10 10 4 | 22 21 15 25 19 20 24 19 22 22 17
32 | 7 9 4 10 11 4 14 10 6 12 3 | 22 27 17 23 19 22 32 20 24 14 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 10 7 10 15 5 11 15 10 14 |T 26 27 22 29 23 24 27 25 25 24 23
WRMS | 10 10 7 11 15 5 11 13 9 13 |NE 27 29 23 29 23 25 29 26 26 24 24
MEDI | 11 10 7 11 14 5 10 13 10 12 |MD 25 27 20 28 22 22 27 24 24 23 22
Table 3.1927.2 GPS week: 1927 Day: 2 MJD: 57735.000
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 11 7 7 12 7 9 13 9 18 3 | 22 23 11 20 14 16 25 24 20 28 17
2 | 15 11 7 12 11 6 12 14 12 19 4 | 31 22 18 24 17 20 24 19 20 17 19
3 | 7 10 5 9 14 4 12 10 7 10 3 | 51 49 45 49 41 45 47 48 42 47 45
X4 | 31 --- --- --- --- 17 20 9 18 --- 12 | 40 --- --- --- --- 19 21 10 5 --- 21
5 | 7 9 7 9 8 3 8 14 8 12 3 | 27 25 25 31 23 26 24 30 25 28 25
6 | 9 7 6 7 13 4 10 14 9 10 3 | 23 25 12 20 19 18 26 21 23 23 18
7E | 14 12 6 12 27 3 12 11 10 10 4 | 25 27 17 26 33 22 27 24 29 24 23
8E | 17 9 6 6 12 4 11 11 11 10 3 | 29 25 21 26 21 22 28 27 24 21 22
9 | 11 11 7 6 11 4 10 9 6 9 3 | 24 24 12 19 15 17 25 16 21 19 17
10 | 5 12 6 5 11 3 11 9 7 10 3 | 54 52 49 53 46 50 49 52 50 54 50
X11 | 10 8 11 --- 13 7 10 10 9 --- 4 | 21 23 16 --- 19 18 23 19 21 --- 18
12 | 13 11 8 9 13 4 11 16 8 12 4 | 24 24 19 23 17 20 27 21 24 19 19
13 | 8 12 10 10 14 3 10 13 10 18 4 | 25 28 20 27 18 23 28 25 27 19 22
14 | 7 9 9 10 16 5 10 25 9 17 4 | 25 26 25 30 28 26 25 27 25 23 23
15 | 8 11 9 14 12 5 11 20 12 19 4 | 27 30 27 21 24 21 31 19 23 21 22
16 | 15 11 7 12 14 5 10 12 12 24 4 | 27 22 17 24 23 18 23 18 21 22 18
17E | 11 12 5 11 15 3 13 13 8 10 3 | 22 26 16 23 23 19 27 21 21 20 19
18 | 7 10 7 10 9 3 10 12 9 16 3 | 25 21 22 31 20 24 17 27 25 24 22
19E | 14 9 6 9 14 4 11 15 9 11 3 | 22 20 12 20 17 17 22 16 19 13 15
20 | 6 12 7 17 7 3 14 13 8 18 4 | 27 21 23 38 22 25 22 28 28 30 24
21 | 25 7 6 12 13 5 12 17 11 21 5 | 36 23 17 24 20 18 22 21 17 19 18
22 | 5 5 10 11 8 4 10 14 9 12 3 | 33 30 35 34 31 30 28 28 27 31 30
23 | 6 13 9 12 14 6 12 26 11 19 4 | 30 30 28 31 26 27 30 29 24 21 24
24E | 11 11 6 6 12 4 9 15 7 11 3 | 24 25 15 21 17 21 25 21 26 19 19
25 | 11 14 5 11 12 3 10 12 5 11 3 | 20 26 15 24 21 18 24 17 19 18 18
26 | 11 11 4 5 11 4 12 6 8 13 3 | 21 23 12 20 15 18 23 17 19 20 16
27E | 10 10 5 8 9 6 12 9 8 15 3 | 27 25 19 24 20 21 28 23 24 21 21
28 | 9 11 8 11 12 3 12 19 10 9 4 | 29 29 23 26 23 24 31 25 27 20 24
29E | 18 13 7 14 14 6 10 13 11 11 4 | 24 24 18 27 21 21 23 17 24 14 19
30E | 11 11 4 7 19 4 11 6 7 11 3 | 24 25 14 21 24 20 27 19 22 24 19
31E | 11 13 6 10 20 4 11 9 9 15 4 | 27 28 21 29 27 24 26 26 28 32 24
32 | 9 9 5 10 10 4 9 11 6 17 3 | 19 26 12 19 14 17 27 16 19 17 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 7 10 13 4 11 14 9 14 |T 27 26 20 26 22 22 26 23 24 23 22
WRMS | 10 11 7 9 13 4 11 12 8 14 |NE 28 27 21 28 22 23 27 24 24 24 22
MEDI | 10 11 7 10 12 4 11 13 9 12 |MD 25 25 18 24 21 21 25 21 24 21 19
Table 3.1927.3 GPS week: 1927 Day: 3 MJD: 57736.000
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 17 10 9 10 6 8 11 7 21 4 | 28 30 23 25 23 23 29 27 26 33 24
2 | 13 13 5 13 9 5 13 15 13 17 4 | 32 27 23 26 21 23 26 25 26 26 23
3 | 10 11 5 13 13 5 10 6 9 8 3 | 58 62 56 61 58 57 56 59 58 55 57
X4 | 13 --- --- --- --- 15 14 13 --- --- 9 | 26 --- --- --- --- 21 25 14 --- --- 22
5 | 6 12 7 11 8 4 9 11 11 11 3 | 33 33 31 36 31 30 28 36 30 35 31
6 | 11 12 7 8 12 5 8 14 9 12 3 | 26 28 21 22 22 23 30 28 30 30 24
7E | 14 15 5 11 17 3 11 13 13 11 4 | 35 40 32 35 37 32 36 36 36 34 33
8E | 13 14 7 8 20 3 9 11 10 11 4 | 29 31 19 26 31 23 27 28 25 23 24
9 | 11 13 7 8 15 4 8 9 9 9 3 | 27 29 21 25 22 22 30 25 27 26 24
10 | 6 13 4 8 8 4 11 9 7 8 3 | 58 66 56 59 57 59 55 61 50 61 57
X11 | 14 14 10 10 14 6 9 9 8 --- 4 | 27 31 24 24 22 23 24 23 24 --- 22
12 | 13 14 8 11 11 6 9 15 11 9 4 | 33 33 27 30 25 28 31 32 35 28 29
13 | 6 16 9 12 12 4 13 13 12 19 4 | 30 38 26 30 29 26 32 31 24 25 27
14 | 7 11 9 10 11 5 8 23 9 15 4 | 31 33 30 32 31 30 29 32 26 31 28
15 | 9 20 10 14 12 5 12 17 13 20 5 | 34 43 35 27 31 31 39 27 35 30 32
16 | 14 17 7 14 12 4 10 10 11 21 4 | 29 29 25 28 24 24 25 22 29 21 23
17E | 16 15 7 13 17 4 12 15 15 10 4 | 25 29 18 23 23 18 26 23 30 22 21
18 | 7 13 8 9 5 4 10 14 7 15 3 | 29 32 28 31 29 27 24 33 25 30 28
19E | 23 15 8 12 15 6 10 17 14 11 5 | 29 31 22 24 25 20 27 24 30 23 22
20 | 6 18 8 21 7 4 13 12 13 16 4 | 30 30 28 41 30 28 24 34 22 35 28
21 | 11 15 5 11 12 4 11 13 12 18 4 | 27 28 22 24 25 22 23 25 22 22 21
22 | 10 9 10 13 8 3 9 11 9 12 3 | 41 42 42 45 42 42 37 42 37 39 40
23 | 9 12 10 13 14 5 12 25 12 17 5 | 36 36 34 36 34 33 31 34 32 27 31
24E | 20 53 9 10 16 7 8 16 15 12 7 | 32 59 21 28 28 26 26 28 30 24 25
25 | 9 13 4 6 7 3 11 12 8 11 3 | 33 34 29 28 28 29 33 33 34 32 30
26 | 13 12 6 10 11 6 10 7 11 12 3 | 22 27 19 22 18 21 23 20 27 22 20
27E | 7 14 7 8 9 4 11 7 6 12 3 | 26 34 21 27 25 24 27 24 25 24 24
28 | 9 15 7 16 12 4 10 16 13 12 4 | 28 36 29 33 24 29 34 29 37 26 29
29E | 21 16 6 15 16 6 9 12 16 11 4 | 30 31 22 30 28 25 26 25 35 24 25
30E | 16 12 6 10 19 5 10 10 10 11 4 | 28 29 19 23 28 22 26 24 27 27 23
31E | 10 14 6 11 21 4 7 10 10 9 4 | 22 27 19 23 27 21 25 23 26 24 21
32 | 9 10 6 10 8 3 8 8 5 8 2 | 23 29 21 23 21 22 30 22 28 22 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 17 7 12 13 5 10 13 11 14 |T 31 35 27 30 29 27 30 29 30 29 27
WRMS | 10 15 7 11 11 5 10 12 9 13 |NE 32 35 29 32 29 29 31 31 31 31 29
MEDI | 10 14 7 11 12 4 10 12 11 12 |MD 29 31 24 28 28 24 27 27 29 26 24
Table 3.1927.4 GPS week: 1927 Day: 4 MJD: 57737.000
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 14 6 9 7 5 10 11 6 21 3 | 30 26 19 20 22 22 29 27 25 35 23
2 | 11 12 5 13 11 5 14 15 12 17 4 | 30 31 27 28 26 25 30 22 27 25 25
3 | 8 9 6 15 16 4 10 9 5 7 3 | 51 54 50 50 47 50 52 51 50 53 50
X4 | 19 --- --- --- --- 26 21 --- --- --- 20 | 34 --- --- --- --- 35 27 --- --- --- 24
5 | 8 11 7 9 11 3 10 9 8 11 3 | 31 25 28 32 24 27 24 30 34 30 27
6 | 11 7 7 10 8 4 10 14 10 12 3 | 31 32 21 29 26 25 33 25 31 31 27
7E | 16 11 6 13 25 4 12 12 13 13 4 | 33 26 26 28 33 26 29 22 30 25 25
8E | 14 13 8 9 27 5 12 12 11 11 4 | 34 28 24 28 40 26 30 29 31 26 27
9 | 10 9 6 10 11 4 8 9 7 12 3 | 27 28 18 19 19 20 29 22 23 23 21
10 | 5 11 6 6 11 3 11 10 6 12 3 | 53 50 47 51 46 49 50 52 51 55 49
11 | 9 7 8 10 14 4 10 8 8 17 3 | 29 24 20 23 21 20 28 23 25 28 22
12 | 15 12 8 13 11 4 10 13 11 10 4 | 29 33 28 32 29 27 31 31 33 31 28
13 | 10 13 9 14 14 4 13 13 11 19 4 | 27 30 23 28 24 24 31 25 23 24 23
14 | 8 10 9 11 10 5 10 24 9 17 4 | 27 25 26 30 25 25 28 30 28 31 25
15 | 8 12 8 12 12 5 11 16 12 21 4 | 35 42 32 28 38 28 39 26 28 32 31
16 | 16 11 6 14 16 5 12 12 12 20 4 | 33 23 25 26 25 21 24 19 23 21 21
17E | 11 12 6 13 21 4 17 15 12 11 4 | 26 29 22 27 32 22 29 25 28 24 24
18 | 6 9 8 9 7 4 11 11 8 16 3 | 29 24 23 29 22 24 20 28 29 27 24
19E | 17 10 6 12 17 6 12 16 11 12 4 | 28 29 22 24 29 21 27 24 26 23 23
20 | 7 12 8 15 10 5 13 9 9 17 4 | 31 20 24 34 23 26 21 25 30 30 24
21 | 9 12 6 12 12 5 13 13 11 17 4 | 27 25 20 23 25 19 24 22 23 23 20
22 | 9 9 11 13 11 3 8 12 8 12 3 | 33 30 32 35 33 32 27 28 27 32 29
23 | 8 12 10 13 16 4 10 25 10 16 4 | 31 32 32 30 30 28 33 31 29 26 28
24E | 13 9 7 12 13 3 8 15 6 12 3 | 26 28 18 26 21 22 24 28 24 28 22
25 | 9 13 4 8 8 3 13 13 7 13 3 | 22 30 21 19 25 23 29 26 27 27 23
26 | 9 10 4 11 10 2 10 7 6 8 3 | 25 26 17 19 19 19 25 18 23 18 19
27E | 10 10 4 9 12 4 11 6 6 10 3 | 30 28 23 27 27 25 27 27 31 26 25
28 | 10 11 8 11 14 3 12 14 10 13 4 | 29 30 28 26 26 26 33 25 31 22 26
29E | 25 13 6 13 16 5 9 11 12 12 4 | 32 25 19 26 27 22 26 19 26 21 21
30E | 11 8 6 10 18 2 11 8 6 10 3 | 27 25 20 24 27 21 28 21 24 23 22
31E | 10 11 5 10 19 3 9 8 8 9 3 | 24 25 19 22 23 19 26 20 22 22 20
32 | 9 9 6 9 8 3 9 9 6 10 3 | 25 30 19 18 19 19 30 20 20 20 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 7 11 14 4 11 13 9 14 |T 30 29 24 27 27 25 29 26 28 27 25
WRMS | 10 11 7 11 12 4 11 12 8 14 |NE 31 30 26 28 27 26 30 27 29 29 26
MEDI | 10 11 6 11 12 4 11 12 9 12 |MD 29 28 23 27 26 24 28 25 27 26 24
Table 3.1927.5 GPS week: 1927 Day: 5 MJD: 57738.000
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 6 9 13 5 9 6 6 22 3 | 25 25 16 23 21 20 26 23 22 34 22
2 | 12 11 5 12 8 5 12 14 11 14 4 | 30 25 19 23 19 19 26 22 22 21 21
3 | 8 12 5 19 11 5 12 15 6 10 4 | 39 45 37 37 43 39 42 43 36 39 38
X4 | 22 --- --- --- --- 32 23 --- --- --- 23 | 36 --- --- --- --- 28 21 --- --- --- 23
5 | 9 10 6 11 7 3 8 8 11 12 3 | 32 23 27 29 30 24 27 26 24 28 26
6 | 10 7 6 6 11 4 9 10 9 15 3 | 27 27 19 25 23 24 32 24 29 34 25
7E | 15 10 7 12 23 4 10 12 11 11 4 | 38 35 31 34 41 32 35 33 34 32 32
8E | 12 13 5 7 17 4 10 10 9 11 3 | 47 48 43 46 47 45 48 47 46 45 45
9 | 10 8 6 8 12 3 7 9 7 9 3 | 24 25 16 22 19 18 27 22 23 19 20
10 | 9 11 5 8 8 4 14 9 8 9 3 | 46 43 39 38 41 40 39 43 36 42 40
11 | 9 7 9 9 16 5 11 8 9 19 3 | 24 25 20 23 25 21 29 21 23 26 22
12 | 11 12 6 11 15 5 9 11 11 16 4 | 28 28 23 25 23 21 28 25 26 25 24
13 | 8 14 9 14 13 5 11 12 11 20 4 | 26 29 22 26 23 23 30 23 27 25 23
X14 | 9 --- 13 11 12 6 11 23 12 21 5 | 28 --- 25 28 27 25 27 28 26 32 24
15 | 8 13 9 16 15 5 12 14 12 19 4 | 29 36 30 24 30 24 35 26 28 27 28
16 | 13 12 7 13 17 5 8 11 13 17 4 | 26 21 17 20 19 17 22 16 23 17 17
17E | 14 10 7 14 23 4 13 14 12 11 4 | 28 29 20 25 32 22 28 24 26 24 23
18 | 7 10 9 9 7 4 10 10 7 12 3 | 27 21 22 24 23 21 20 24 19 21 21
19E | 21 10 7 15 24 5 9 15 13 12 5 | 34 31 23 26 38 23 28 25 30 24 25
20 | 6 11 7 14 9 3 10 8 8 15 3 | 27 24 24 30 27 23 24 25 21 26 24
21 | 10 12 6 13 11 6 11 12 11 17 4 | 24 23 17 22 20 16 22 19 16 18 17
22 | 7 6 10 15 8 5 7 15 10 11 3 | 30 32 31 36 39 32 31 33 29 31 31
23 | 8 10 10 11 17 6 11 26 13 15 5 | 26 29 25 25 27 24 28 30 25 22 23
24E | 16 17 8 12 15 4 10 12 10 15 4 | 27 31 18 23 24 22 24 22 26 22 22
25 | 10 16 5 8 9 5 11 9 8 14 3 | 26 31 23 23 23 23 31 25 28 28 25
26 | 6 9 6 8 13 3 10 6 6 7 2 | 18 23 14 18 14 16 23 18 22 19 17
27E | 8 12 5 8 19 4 12 7 10 12 3 | 42 45 41 43 43 40 41 43 40 39 40
28 | 11 9 8 10 13 4 10 14 11 12 3 | 25 28 23 26 24 24 32 26 31 23 25
29E | 21 13 7 16 25 5 11 10 11 13 5 | 26 23 15 25 29 18 21 17 24 20 18
30E | 14 8 6 8 21 4 9 6 9 6 3 | 24 21 13 21 25 19 24 20 24 18 18
31E | 13 7 4 8 19 4 8 8 8 8 3 | 22 22 16 21 22 18 24 20 21 22 19
32 | 7 7 7 7 9 3 10 10 7 7 2 | 20 28 18 17 18 18 25 20 21 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 7 11 15 4 10 12 10 14 |T 29 29 23 26 27 24 28 26 26 26 24
WRMS | 10 11 7 11 13 4 10 10 9 13 |NE 27 28 23 25 25 23 28 25 25 26 24
MEDI | 10 10 7 11 13 4 10 10 10 12 |MD 27 28 22 25 25 23 27 24 26 25 23
Table 3.1927.6 GPS week: 1927 Day: 6 MJD: 57739.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 10 8 9 10 4 10 9 7 16 3 | 23 27 22 22 21 20 24 23 21 29 21
2 | 10 9 6 11 10 4 14 13 12 14 4 | 27 23 17 24 19 19 26 22 20 22 19
3 | 9 12 5 12 10 5 13 14 7 11 3 | 61 64 55 59 60 57 59 63 53 61 58
X4 | 16 --- --- --- --- 35 18 --- --- --- 17 | 32 --- --- --- --- 20 22 --- --- --- 21
5 | 8 9 6 11 11 3 11 9 11 9 3 | 36 28 30 40 32 31 27 37 28 35 31
6 | 10 8 8 8 8 4 10 6 9 11 3 | 27 28 16 27 21 23 32 24 27 31 24
7E | 17 13 7 11 32 4 9 12 10 9 4 | 29 32 27 32 40 29 32 34 31 29 28
8E | 20 13 6 8 16 7 12 11 11 7 4 | 76 78 78 82 73 76 80 80 79 79 77
9 | 15 8 6 9 15 4 9 8 8 10 3 | 24 24 13 18 20 17 26 21 21 19 18
10 | 8 10 6 6 10 3 12 9 6 8 3 | 64 63 56 62 61 62 58 67 56 65 60
11 | 16 10 12 10 10 5 10 13 9 10 4 | 43 39 35 36 37 35 38 40 35 35 36
12 | 13 12 7 13 19 5 11 10 10 12 4 | 25 28 25 27 23 22 25 25 25 21 22
13 | 6 13 9 13 15 5 13 11 10 18 4 | 28 31 24 33 28 26 30 30 24 22 25
14 | 10 11 10 12 10 5 8 24 12 18 4 | 32 32 28 37 33 32 31 35 31 32 29
15 | 10 13 9 15 11 4 13 13 12 19 4 | 33 44 35 28 34 30 41 30 33 31 33
16 | 11 9 8 11 20 5 9 11 12 19 4 | 22 24 17 25 24 19 23 19 23 20 18
17E | 11 9 7 9 23 4 11 14 13 10 4 | 29 30 21 29 30 25 32 29 33 26 26
18 | 7 7 8 12 7 6 11 10 10 12 3 | 24 24 23 32 27 25 18 29 21 25 22
19E | 24 7 6 12 29 6 8 15 13 12 5 | 32 26 19 25 34 22 27 24 28 22 22
20 | 8 10 8 15 8 3 12 9 10 13 3 | 30 23 28 39 28 27 20 30 22 31 26
21 | 10 8 6 11 11 5 12 11 10 12 3 | 20 22 17 22 21 16 20 20 14 18 16
22 | 7 8 9 13 7 4 6 15 9 15 3 | 36 35 35 38 38 35 29 38 28 37 33
23 | 9 11 11 11 14 6 15 25 12 16 5 | 32 33 32 32 34 31 30 34 30 26 28
24E | 15 16 9 12 33 4 11 13 12 13 5 | 23 28 12 20 30 16 20 20 21 12 16
25 | 9 12 6 6 11 3 11 9 6 12 3 | 21 28 21 21 19 19 26 21 23 18 20
26 | 6 9 5 8 15 3 10 7 5 7 2 | 18 27 12 19 19 17 24 18 19 21 17
27 | 14 9 5 6 19 6 14 9 11 10 3 | 64 70 66 70 66 65 64 68 67 69 66
28 | 12 11 9 12 15 3 9 13 12 15 4 | 25 32 23 29 21 24 29 28 30 24 24
29E | 21 11 8 16 23 6 12 10 12 12 5 | 27 24 17 27 28 20 23 18 27 18 19
30E | 18 15 6 7 25 5 10 7 8 7 4 | 23 31 14 20 31 17 23 22 20 20 19
31E | 12 7 5 9 21 4 8 10 9 9 3 | 25 28 21 26 24 24 26 25 24 23 22
32 | 8 9 6 10 7 4 12 10 8 9 3 | 21 30 19 18 19 19 30 21 23 19 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 7 11 17 5 11 12 10 13 |T 32 34 27 32 32 28 31 32 30 30 28
WRMS | 10 11 7 10 14 4 11 11 9 12 |NE 30 32 26 31 29 27 29 30 27 29 27
MEDI | 10 10 7 11 14 4 11 11 10 12 |MD 27 28 23 28 28 24 27 28 27 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 4.1927 GPS week: 1927 MJD: 57733.0-57739.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 |U 5 6 12 |U 10 11 32 |U 7 9 15 |
emr | emr 2961 | 8 9 18 |U 13 12 35 | 8 7 19 |
esa | esa 2976 | 6 7 16 |U 11 13 33 | 7 7 19 |
gfz | gfz 2948 |U 6 8 20 |U 10 12 32 |U 7 7 16 |
grg | grg 2975 |U 7 8 17 |U 10 12 31 | 8 8 19 |
igr | igr 2998 | 5 7 13 | 10 12 32 | 7 7 16 |
igs | igs 2975 | 6 7 14 | 10 12 32 | 7 7 16 |
jpl | jpl 3057 | 6 8 16 |U 11 13 35 | 8 8 21 |
mit | mit 3003 | 7 10 18 |U 12 16 36 |U 9 11 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 5.1927.0 GPS week: 1927 Day: 0 MJD: 57733.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 7 11 17 | 16 16 47 | 9 10 15 |
emr | emr 2976 | 8 11 21 | 18 16 46 | 9 9 21 |
esa | esa 2976 | 8 11 19 | 15 16 43 | 8 8 22 |
gfz | gfz 2976 | 7 10 17 | 16 14 43 | 8 9 19 |
grg | grg 2976 | 8 12 20 | 15 14 39 | 9 10 24 |
igr | igr 2976 | 7 10 18 | 15 14 42 | 8 9 19 |
igs | igs 2976 | 7 10 18 | 16 15 44 | 8 9 19 |
jpl | jpl 3072 | 7 10 20 | 17 17 52 | 9 10 23 |
mit | mit 2976 | 11 19 19 | 16 17 46 | 12 14 25 |
Table 5.1927.1 GPS week: 1927 Day: 1 MJD: 57734.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 7 11 18 | 15 15 45 | 7 6 13 |
emr | emr 2972 | 10 10 22 | 16 20 50 | 8 6 14 |
esa | esa 2976 | 9 12 22 | 14 17 41 | 7 6 19 |
gfz | gfz 2880 | 8 12 21 | 14 16 45 | 7 7 18 |
grg | grg 2972 | 9 12 23 | 15 16 40 | 9 8 20 |
igr | igr 2972 | 8 12 20 | 14 18 42 | 7 7 15 |
igs | igs 2972 | 8 11 20 | 15 16 44 | 7 6 17 |
jpl | jpl 2976 | 7 9 19 | 17 19 51 | 8 6 19 |
mit | mit 2976 | 9 14 23 | 16 18 47 | 9 9 21 |
Table 5.1927.2 GPS week: 1927 Day: 2 MJD: 57735.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 6 13 | 12 12 29 | 7 8 13 |
emr | emr 2976 | 8 9 17 | 16 12 39 | 9 8 20 |
esa | esa 2976 | 5 7 14 | 16 19 37 | 6 7 21 |
gfz | gfz 2880 | 11 17 55 | 13 15 32 | 6 7 16 |
grg | grg 2976 | 6 7 15 | 12 16 35 | 7 9 20 |
igr | igr 3040 | 5 6 13 | 12 15 34 | 6 7 18 |
igs | igs 2976 | 5 7 14 | 13 14 32 | 6 7 17 |
jpl | jpl 3072 | 6 9 15 | 13 15 34 | 7 7 23 |
mit | mit 3072 | 5 7 16 | 15 17 42 | 8 10 18 |
Table 5.1927.3 GPS week: 1927 Day: 3 MJD: 57736.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 5 4 9 | 6 7 23 | 7 9 16 |
emr | emr 2976 | 7 11 21 | 9 8 25 | 8 7 22 |
esa | esa 2976 | 5 7 16 | 6 8 27 | 6 6 21 |
gfz | gfz 2975 | 5 5 13 | 6 8 25 | 7 7 19 |
grg | grg 2976 | 7 7 17 | 7 7 22 | 7 8 23 |
igr | igr 3070 | 4 5 11 | 7 7 23 | 6 7 19 |
igs | igs 2976 | 5 5 13 | 6 7 24 | 7 7 19 |
jpl | jpl 3070 | 7 7 17 | 7 8 25 | 9 9 25 |
mit | mit 3072 | 6 6 15 | 9 21 32 | 7 8 18 |
Table 5.1927.4 GPS week: 1927 Day: 4 MJD: 57737.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 4 8 | 5 6 23 | 6 8 14 |
emr | emr 2976 | 7 10 16 | 8 8 27 | 7 6 19 |
esa | esa 2976 | 4 5 12 | 5 6 25 | 6 6 18 |
gfz | gfz 2976 | 5 5 12 | 5 8 21 | 7 7 15 |
grg | grg 2976 | 7 8 15 | 5 7 20 | 7 8 15 |
igr | igr 2976 | 5 6 10 | 5 6 22 | 6 7 16 |
igs | igs 2976 | 5 5 11 | 5 6 22 | 6 6 15 |
jpl | jpl 3072 | 7 7 16 | 6 6 24 | 9 9 22 |
mit | mit 2976 | 4 4 13 | 6 8 20 | 7 8 16 |
Table 5.1927.5 GPS week: 1927 Day: 5 MJD: 57738.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 4 5 9 | 9 8 30 | 8 11 18 |
emr | emr 2880 | 8 7 14 | 12 8 28 | 9 6 21 |
esa | esa 2976 | 5 4 13 | 9 8 29 | 7 7 17 |
gfz | gfz 2976 | 5 5 12 | 10 9 32 | 7 8 16 |
grg | grg 2976 | 6 5 15 | 10 10 29 | 8 10 20 |
igr | igr 2976 | 4 5 10 | 10 8 30 | 7 8 15 |
igs | igs 2976 | 4 5 11 | 10 8 28 | 7 7 16 |
jpl | jpl 3072 | 6 8 16 | 10 9 28 | 8 7 19 |
mit | mit 2976 | 6 5 13 | 10 11 30 | 8 11 18 |
Table 5.1927.6 GPS week: 1927 Day: 6 MJD: 57739.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 6 4 12 | 8 14 29 | 7 8 14 |
emr | emr 2976 | 8 4 12 | 10 13 33 | 8 6 16 |
esa | esa 2976 | 5 3 14 | 8 14 31 | 6 6 14 |
gfz | gfz 2976 | 5 3 11 | 8 16 29 | 6 6 12 |
grg | grg 2976 | 8 5 17 | 8 16 32 | 7 5 13 |
igr | igr 2976 | 5 4 11 | 8 15 28 | 6 6 13 |
igs | igs 2976 | 5 3 11 | 8 14 30 | 5 6 12 |
jpl | jpl 3071 | 6 4 13 | 8 14 33 | 7 6 17 |
mit | mit 2976 | 10 12 24 | 11 18 35 | 9 15 35 |
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 6.1927 GPS week: 1927 MJD: 57733.500-57739.500
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 14 10 -37 -9 | 12 28
| 15 30 40 41 6 | 5
emr uuuuu | 32 29 6 7 -9 | 39 49
| 29 55 161 195 10 | 4
esa uuuuu | -16 -5 -76 -51 -9 | 22 34
| 11 21 87 65 5 | 4
gfz uuuuu | -12 -1 4 -103 -8 | 24 34
| 40 35 168 154 5 | 5
grg uuuuu | 6 -14 -3 49 -3 | -5 24
| 18 19 54 57 8 | 5
igr xxxxx | -29 12 -45 8 -13 | 9 27
| 3 12 62 35 7 | 6
irf xxxxx | 38 -6 1 18 -4 | 0 24
| 10 5 29 21 6 | 5
jpl uuuuu | -53 -35 104 51 1 | 36 42
| 19 29 43 81 5 | 3
mit uuuuu | 34 -16 -19 79 -2 | 15 26
| 23 20 85 52 3 | 4
ngs uuuuu | 31 17 1 69 13 | -3 18
| 34 43 185 154 4 | 6
sio uuuux | 9 20 3 -74 -4 | 31 37
| 26 25 117 118 4 | 4
Table 7.1927.0 GPS week: 1927 Day: 0 MJD: 57733.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -27 -11 30 -53 2 | 14 31
emr uuuuu | 8 43 -62 35 -15 | 43 53
esa uuuuu | -14 -19 40 2 -5 | 23 37
gfz uuuuu | 25 -29 65 87 -11 | 27 37
grg uuuuu | 3 -27 -63 57 -4 | -2 25
igr xxxxx | -25 -6 -79 -3 -23 | 14 28
irf xxxxx | 32 -2 -44 20 -11 | 5 25
jpl uuuuu | -65 -2 122 67 -8 | 38 43
mit uuuuu | 10 -1 -105 14 -7 | 18 29
ngs uuuuu | 74 40 -108 -37 18 | -6 23
sio uuuux | -21 3 -12 -288 2 | 33 40
Table 7.1927.1 GPS week: 1927 Day: 1 MJD: 57734.500
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 -38 68 -63 -14 | 15 30
emr uuuuu | 30 48 -136 159 -18 | 42 53
esa uuuuu | -9 -36 27 -16 -9 | 25 37
gfz uuuuu | 19 -49 188 2 0 | 27 37
grg uuuuu | 37 -13 103 96 -1 | -2 25
igr xxxxx | -34 5 -90 -35 -15 | 13 29
irf xxxxx | 27 -5 -37 32 -7 | 4 25
jpl uuuuu | -84 3 84 81 3 | 37 43
mit uuuuu | 10 3 -160 57 -2 | 17 29
ngs uuuuu | 51 98 -226 -197 14 | -4 22
sio uuuux | -25 2 65 -83 -8 | 34 40
Table 7.1927.2 GPS week: 1927 Day: 2 MJD: 57735.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -15 19 2 -98 -7 | 12 30
emr uuuuu | 11 -4 141 84 -18 | 38 51
esa uuuuu | -19 3 -73 13 -18 | 23 36
gfz uuuuu | 18 -7 -58 54 -13 | 25 36
grg uuuuu | -20 3 20 -53 -16 | -4 25
igr xxxxx | -31 19 -55 -34 -1 | 10 29
irf xxxxx | 27 -12 14 5 -8 | 0 25
jpl uuuuu | -59 -45 56 -84 3 | 36 42
mit uuuuu | 17 -20 6 77 -4 | 15 27
ngs uuuuu | 58 16 -68 73 19 | -13 16
sio uuuux | -6 27 106 -152 0 | 31 38
Table 7.1927.3 GPS week: 1927 Day: 3 MJD: 57736.500
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 31 -23 12 -14 | 18 29
emr uuuuu | -5 136 -212 -426 -7 | 44 52
esa uuuuu | -1 -13 -49 1 -7 | 28 36
gfz uuuuu | 16 21 -192 -102 -2 | 30 37
grg uuuuu | 3 -28 -6 85 -4 | 0 21
igr xxxxx | -31 23 -38 35 -16 | 15 29
irf xxxxx | 51 -12 19 52 -5 | 5 23
jpl uuuuu | -47 -65 181 158 5 | 41 46
mit uuuuu | 47 -10 13 171 0 | 20 28
ngs uuuuu | 0 -35 174 41 9 | 4 16
sio uuuux | 20 27 71 -61 -2 | 36 41
Table 7.1927.4 GPS week: 1927 Day: 4 MJD: 57737.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -22 54 -53 7 -10 | 12 24
emr uuuuu | 70 24 -25 42 10 | 38 46
esa uuuuu | -25 4 -135 -94 -10 | 23 31
gfz uuuuu | -58 54 -231 -224 -11 | 25 31
grg uuuuu | 19 17 -21 -5 -6 | -6 19
igr xxxxx | -26 9 79 11 -6 | 8 23
irf xxxxx | 49 -2 31 -13 -3 | -1 19
jpl uuuuu | -23 -69 98 114 6 | 37 41
mit uuuuu | 71 -56 72 87 -3 | 15 22
ngs uuuuu | -22 -19 253 132 10 | 2 14
sio uuuux | 38 -10 92 -30 -4 | 31 35
Table 7.1927.5 GPS week: 1927 Day: 5 MJD: 57738.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 8 11 40 -12 -9 | 5 26
emr uuuuu | 58 -17 97 84 -4 | 33 43
esa uuuuu | -33 -5 -183 -131 -7 | 17 31
gfz uuuuu | -60 22 166 -293 -11 | 18 30
grg uuuuu | -4 -13 -7 81 2 | -13 26
igr xxxxx | -28 8 -19 24 -19 | 0 26
irf xxxxx | 41 -5 10 26 5 | -7 25
jpl uuuuu | -53 -46 63 -12 2 | 32 38
mit uuuuu | 49 -9 -15 113 2 | 8 23
ngs uuuuu | 30 10 140 228 10 | -5 19
sio uuuux | 29 67 -213 30 -4 | 25 33
Table 7.1927.6 GPS week: 1927 Day: 6 MJD: 57739.500
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 | -41 32 6 -52 -14 | 6 26
emr uuuuu | 52 -28 241 73 -10 | 36 44
esa uuuuu | -9 30 -155 -133 -4 | 17 31
gfz uuuuu | -45 -19 94 -245 -9 | 19 31
grg uuuuu | 4 -37 -46 84 9 | -11 25
igr xxxxx | -29 28 -109 57 -14 | 0 26
irf xxxxx | 37 0 16 5 3 | -4 24
jpl uuuuu | -40 -23 123 33 -1 | 34 40
mit uuuuu | 31 -21 58 37 0 | 11 24
ngs uuuuu | 22 10 -154 241 9 | -1 19
sio uuuux | 25 26 -86 63 -11 | 26 34
More information about the IGSREPORT
mailing list