[IGSREPORT-25462] Wk 1961 IGS Final Orbits
acc
acc at igs.org
Fri Aug 25 03:02:20 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1961 (Aug 06, 2017 - Aug 12, 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:
igs1961[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1961[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1961[0-6].cls IGS GPS clock combination summary report.
igs19617.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19617.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 | BJCO HYDE MAL2 TIXI BJCO HYDE TIXI
0 | EMR | HERS MAS1 SFER
0 | ESA | DGAR KOUR LHAZ DGAR FAA1 KOUR LHAZ
0 | GFZ | 13 PDEL SYOG PDEL SYOG
0 | GRG | GLSV MAL2 SYOG FAA1 GLSV NKLG PDEL SYOG
0 | MIT | AREG DGAR AREG DGAR PDEL
1 | COD | TIXI CHTI MAL2 TIXI
1 | EMR | 21 ALBH HERS MAS1 SYOG TWTF
1 | ESA | FAA1 THU2 FAA1
1 | GFZ | FAA1 KOUR MAL2 AUCK KOUR NICO
1 | GRG | CHTI GLSV LMMF MAL2 PDEL SYOG TRO1 CHTI FAA1 GLSV
1 | GRG | LMMF MAL2 PDEL SYOG TRO1
2 | COD | TIXI LMMF SYOG TIXI
2 | EMR | NRC1 YAR2 ALBH MAS1 NIST NRC1 SFER YAR2
2 | GFZ | GRAZ KOUR MAL2 GRAZ KOUR MAL2 STHL
2 | GRG | GLSV MAL2 SYOG GLSV MAL2 SYOG
3 | COD | SYOG TIXI FAA1 NTUS SYOG TIXI
3 | EMR | HERS MAS1 SFER
3 | ESA | BAKE DGAR BAKE DGAR REUN
3 | GFZ | BAKE SALU TRO1
3 | GRG | 12 12 GLSV MAL2 NKLG SYOG GLSV LMMF MAL2 NKLG SYOG
4 | COD | FAA1 SAVO SYOG TIXI BAKE FAA1 SYOG TIXI
4 | EMR | HERS MAS1 NIST SFER
4 | ESA | MAL2 MAL2 REUN
4 | GFZ | SAVO
4 | GRG | 15 15 BAKE DAEJ FAA1 GLSV MAL2 SCUB SYOG TRO1 BAKE
4 | GRG | DAEJ FAA1 GLSV MAL2 SCUB SYOG
5 | COD | 9 FAA1 TIXI FAA1 TIXI
5 | EMR | MAS1
5 | ESA | DGAR LHAZ DGAR LHAZ
5 | GFZ | 21 DRAO FAA1 MAL2 DRAO FAA1 MAL2 NTUS SAVO
5 | GRG | 9 9 DAEJ MAL2 SYOG DAEJ MAL2 SYOG
5 | MIT | 9 9 REUN REUN
6 | COD | LHAZ NTUS TIXI LHAZ NTUS TIXI
6 | EMR | HERS MAS1
6 | ESA | SAVO SAVO
6 | GFZ | ALBH MAL2 SFER TRO1 ALBH MAL2 SFER TRO1
6 | GRG | DAEJ MAL2 PIE1 TRO1 DAEJ GLSV MAL2 PIE1 REUN TRO1
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
7. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.1 .6 .9 16 10 -9 -.43
EMR | 0 | -2.2 .5 -3.7 -2 53 -37 -.15
ESA | 0 | -.2 -.5 -.9 -4 -6 -10 -.49
GFZ | 0 | .1 .6 1.3 12 -13 -4 -.42
GRG | 0 | -.3 1.2 7.1 27 26 5 -.52
JPL | 0 | -.1 1.4 -10.3 -37 -60 49 .01
MIT | 0 | -2.2 -6.3 1.4 -17 29 2 -.20
NGS | 0 | -.7 -6.9 -5.5 7 -2 13 -.21
SIO | 0 | -5.1 -4.8 -10.4 -22 -9 -2 -.35
COD | 1 | .3 .2 .9 2 7 -7 -.44
EMR | 1 | -3.6 5.3 -12.8 12 47 3 -.08
ESA | 1 | -.7 -.4 -.9 -4 3 -13 -.48
GFZ | 1 | .8 -.0 .7 -6 -34 0 -.39
GRG | 1 | 3.8 -.3 -10.4 43 14 33 -.38
JPL | 1 | 2.2 -1.3 -8.4 3 -28 93 .01
MIT | 1 | -1.5 -5.5 1.1 8 40 6 -.07
NGS | 1 | -5.1 -7.6 1.7 10 -31 -8 -.26
SIO | 1 | -3.0 -4.5 -9.3 -7 -10 9 -.14
COD | 2 | .0 .1 .8 8 11 -1 -.37
EMR | 2 | 7.3 -2.6 -7.3 18 42 -7 -.31
ESA | 2 | -.1 -.7 -1.1 -7 -5 -2 -.43
GFZ | 2 | .9 .3 .9 2 -40 -5 -.46
GRG | 2 | -5.1 -7.9 18.9 46 -15 46 -.22
JPL | 2 | 6.9 -5.7 -5.3 -1 -78 106 -.24
MIT | 2 | -2.0 -9.3 3.5 -1 32 9 -.23
NGS | 2 | -2.4 -11.0 -3.8 27 -3 0 -.19
SIO | 2 | -1.4 -2.7 -4.9 -11 -12 -6 -.46
COD | 3 | .1 .1 1.3 10 18 3 -.37
EMR | 3 | 4.0 -4.8 -7.3 21 40 -23 -.58
ESA | 3 | -.4 -.1 -1.1 -15 6 -20 -.53
GFZ | 3 | .4 .5 .6 7 -31 -6 -.41
GRG | 3 | -.2 -6.0 -.9 17 10 45 -.39
JPL | 3 | 11.9 -4.1 -4.3 -55 -44 72 -.04
MIT | 3 | -3.7 -6.5 4.8 -8 17 5 -.15
NGS | 3 | 1.4 -6.0 -8.7 30 -1 -5 -.29
SIO | 3 | -2.5 -2.6 -8.7 0 -28 0 -.16
COD | 4 | .0 .3 .9 7 12 -9 -.41
EMR | 4 | 3.5 -2.5 -9.1 11 54 -36 -.15
ESA | 4 | -.5 -.2 -.8 -10 17 -14 -.52
GFZ | 4 | .4 .5 1.0 10 -30 -3 -.41
GRG | 4 | 2.5 .8 10.0 49 19 27 -.17
JPL | 4 | 9.5 -6.5 -.0 -33 -40 46 -.07
MIT | 4 | -.5 -6.8 5.1 -12 46 2 -.11
NGS | 4 | 2.0 -4.2 -1.0 4 -3 -15 -.23
SIO | 4 | 1.4 -1.7 -3.7 -19 -5 -4 -.40
COD | 5 | .7 -.1 1.2 5 4 -9 -.43
EMR | 5 | -2.5 2.7 -11.0 -21 46 4 -.16
ESA | 5 | -.3 -.9 -1.0 -12 3 -6 -.42
GFZ | 5 | .9 .3 1.1 0 -36 -8 -.41
GRG | 5 | -5.6 7.4 1.9 23 17 43 -.35
JPL | 5 | -1.1 -2.1 -8.7 -8 -28 98 .19
MIT | 5 | -1.8 -3.7 3.7 -36 22 15 -.20
NGS | 5 | -2.4 -9.7 -2.2 31 -12 7 -.21
SIO | 5 | -5.4 -.6 -7.1 -44 -18 0 -.24
COD | 6 | .3 .2 .9 8 -2 -2 -.58
EMR | 6 | -1.2 -1.3 -10.3 15 22 -16 -.39
ESA | 6 | -.1 -.7 -.2 4 -1 -15 -.54
GFZ | 6 | .5 .2 .9 0 -27 -3 -.42
GRG | 6 | -6.3 5.3 4.7 34 1 45 -.45
JPL | 6 | 5.6 -7.4 -5.9 -35 -40 76 .08
MIT | 6 | .7 -6.2 -.3 -15 30 8 -.19
NGS | 6 | -1.3 -4.0 -8.9 -6 1 -26 -.39
SIO | 6 | -1.9 -3.9 -10.9 -28 11 4 -.25
8. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
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 1.1961.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1961.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 2.1961.[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 3.1961.[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 5.1961.0-6). 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 1961 summary. (Aug 06, 2017 - Aug 12, 2017)
Table 1.1961.a GPS week: 1961 MJD: 57971.000-57977.000
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 275| 1 0 3 7 10 -7 .03 10 10 | -535 -355 11 102
| 0 0 2 16 19 6 .02 | 360 493
emr 80| 0 2 -3 25 3 5 .15 16 16 | 612 -410 20 144
| 1 1 0 20 14 13 .04 | 1121 448
esa 150| 0 0 -3 -1 0 -11 -.02 9 9 | -1431 -235 8 153
| 0 0 1 13 15 9 .02 | 1035 997
gfz 196| -1 1 1 -11 1 7 .12 10 10 | -158 -103 11 128
| 0 0 1 16 5 7 .04 | 356 642
grg 107| 1 0 4 -11 0 21 -.32 17 16 | 65 -63 13 175
| 0 0 6 17 15 20 .04 | 268 395
igr n/a| 0 0 1 -9 -12 3 .02 4 4 | -5050 -17 12 81
| 0 0 0 10 11 14 .01 | 688 599
jpl 80| 0 0 -2 21 -14 32 .22 12 12 | 408 -336 40 206
| 1 0 2 31 17 21 .02 | 706 481
mit 349| 0 -2 3 -8 -10 21 -.14 13 11 | -482 -67 37 326
| 0 0 0 30 26 5 .04 | 600 416
ngs 216| 0 0 -2 5 0 0 .08 8 7 | -529 -369 959 2238
| 0 0 1 17 13 11 .07 | 321 464
sio 351| 0 0 0 -7 -11 -12 -.04 11 11 | --- --- --- ---
| 0 0 1 24 36 21 .05 | --- ---
Table 1.1961.b GPS week : 1961 MJD: 57971.000-57977.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 3 4 4 |
2 | 5 5 5 5 4 5 5 |
3 | 3 3 3 3 3 3 3 |
4 | 0 0 0 0 0 0 0 |
5 | 4 5 4 4 4 4 4 |
6 | 5 4 4 4 4 5 4 |
7 | 5 5 5 5 5 5 5 |
8 | 3 3 3 4 3 4 3 |
9 | 4 4 4 3 4 4 4 |
10 | 3 3 3 3 3 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 3 4 4 4 4 |
14 | 4 4 4 4 4 4 5 |
15 | 4 4 4 4 6 4 4 |
16 | 5 6 5 5 6 5 5 |
17 | 5 5 6 6 5 5 5 |
18 | 6 5 5 5 6 6 6 |
19 | 5 6 6 6 6 6 6 |
20 | 4 4 4 4 4 4 4 |
21 | 5 5 5 5 5 6 5 |
22 | 5 5 5 5 5 5 5 |
23 | 5 4 5 4 5 5 5 |
24 | 3 3 3 3 3 3 4 |
25 | 4 4 4 4 4 4 6 |
26 | 6 5 5 4 5 5 5 |
27 | 3 3 3 4 4 4 3 |
28 | 5 4 4 4 4 4 4 |
29 | 5 5 5 5 5 5 5 |
30 | 3 3 3 3 3 3 3 |
31 | 7 7 7 6 6 6 6 |
32 | 4 4 4 4 4 3 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1961.0 GPS week: 1961 Day: 0 MJD: 57971.000
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 275| 1 0 4 43 16 -11 .05 10 10 | -553 -310 10 99
emr 80| -2 2 -4 29 -4 7 .12 16 16 | 2748 -558 17 121
esa 150| 0 0 -5 -4 -16 -6 -.03 9 9 | -681 -890 9 177
gfz 196| 0 1 0 -8 -1 6 .19 11 12 | -158 -15 11 112
grg 106| 1 0 10 -10 -3 8 -.33 17 15 | -128 361 14 205
igr n/a| 0 0 0 -1 -26 2 .02 5 5 | -4306 -346 11 89
jpl 80| -1 0 -4 29 -25 18 .19 12 12 | 1904 -580 39 211
mit 350| 0 -1 2 -36 -8 17 -.20 14 12 | -49 -88 37 359
ngs 218| -1 -1 -2 5 5 6 .13 8 7 | -540 -294 906 1850
sio 352| 0 0 0 -31 -6 -7 -.11 11 11 | --- --- --- ---
Table 2.1961.1 GPS week: 1961 Day: 1 MJD: 57972.000
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 275| 0 0 7 -4 -17 -8 .04 10 9 | -632 -212 12 107
emr 80| 0 4 -3 17 22 18 .15 16 16 | 1501 -1018 24 136
esa 150| 0 0 -3 -25 0 -7 -.04 9 9 | -2050 -437 9 158
gfz 196| 0 0 -1 -29 1 5 .07 10 10 | -537 -343 11 149
grg 107| 1 0 -7 -2 9 30 -.33 18 17 | 19 -118 14 164
igr n/a| 0 0 2 -23 -8 -3 .02 5 5 | -5326 -761 14 85
jpl 80| 0 0 -2 54 10 -3 .25 12 12 | 595 -997 40 207
mit 350| 1 -2 4 37 3 14 -.16 14 11 | -555 -133 41 309
ngs 218| 0 0 -1 0 -1 -8 .15 9 8 | -729 100 815 2487
sio 350| 0 0 2 29 2 -13 -.08 11 11 | --- --- --- ---
Table 2.1961.2 GPS week: 1961 Day: 2 MJD: 57973.000
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 268| 1 0 4 -1 13 -6 .01 10 10 | -673 -282 12 106
emr 79| 0 2 -2 37 23 24 .11 15 15 | 438 -189 23 165
esa 150| 0 0 -4 4 9 -20 -.04 9 9 | -1032 513 8 154
gfz 193| -1 1 1 0 -1 -4 .12 9 9 | -526 704 11 128
grg 107| 1 0 9 -2 3 34 -.37 19 19 | -107 110 15 167
igr n/a| 0 0 1 -8 -2 -13 .03 4 4 | -5993 441 12 74
jpl 80| 1 0 -4 56 -28 17 .20 12 12 | -155 37 43 206
mit 350| 0 -1 2 3 -43 16 -.15 13 10 | -1027 353 36 311
ngs 217| -1 0 -3 -14 20 8 .15 8 7 | -652 -313 898 2356
sio 354| 0 0 0 -7 -28 -11 -.04 11 10 | --- --- --- ---
Table 2.1961.3 GPS week: 1961 Day: 3 MJD: 57974.000
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 278| 1 0 2 1 33 3 .01 9 9 | -672 -167 11 88
emr 80| 1 0 -3 27 -2 -17 .11 15 15 | -142 325 22 126
esa 150| 0 0 -3 -11 -16 -28 -.01 9 9 | -690 -1540 9 153
gfz 198| -2 0 2 -2 -6 4 .13 9 9 | -305 648 11 147
grg 108| 1 -1 2 -34 -31 54 -.38 19 19 | -159 296 14 155
igr n/a| 0 0 2 -21 -28 -1 .02 4 4 | -5535 831 13 82
jpl 80| 0 0 1 -20 -38 40 .20 12 12 | 355 345 40 198
mit 350| 1 -1 3 17 19 28 -.16 13 11 | -1017 462 36 342
ngs 218| 0 0 -3 0 -2 -4 .06 8 7 | -737 -74 1008 2306
sio 358| 0 0 2 12 4 11 -.03 11 10 | --- --- --- ---
Table 2.1961.4 GPS week: 1961 Day: 4 MJD: 57975.000
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 279| 0 0 0 -2 27 -9 .06 9 9 | -916 148 13 117
emr 81| 0 1 -2 15 2 -5 .15 15 15 | -135 -773 21 161
esa 150| 0 0 -1 2 20 -1 -.02 8 9 | -2264 540 7 137
gfz 199| -1 0 1 8 10 13 .11 10 10 | 133 -1005 11 117
grg 110| 2 0 9 0 6 19 -.29 18 16 | -52 51 13 176
igr n/a| 0 0 1 -13 -11 16 .00 4 4 | -5085 -595 12 80
jpl 80| -1 -2 -2 8 -11 52 .23 12 12 | 73 -750 39 218
mit 349| 0 -2 3 -28 -48 23 -.13 13 11 | -1044 63 36 305
ngs 221| 0 0 -3 19 -2 -16 .03 8 7 | -715 -343 992 2222
sio 352| 0 0 0 -34 -60 6 -.01 12 10 | --- --- --- ---
Table 2.1961.5 GPS week: 1961 Day: 5 MJD: 57976.000
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 276| 2 0 0 6 13 -14 -.00 11 11 | 230 -1420 14 114
emr 79| -1 3 -3 -8 -11 3 .19 16 16 | -314 -130 20 154
esa 150| 0 0 -1 2 17 -7 .01 9 9 | -3062 1186 8 146
gfz 198| -1 1 1 -37 3 15 .12 10 10 | -173 -1 13 142
grg 108| 1 0 4 -38 15 -4 -.26 15 14 | 529 -756 13 182
igr n/a| 0 0 0 4 0 -4 .03 4 4 | -5103 446 15 91
jpl 80| 1 -1 -1 -17 -13 50 .22 11 11 | -71 0 44 208
mit 349| 0 -2 2 -6 -8 20 -.09 13 10 | 515 -748 37 364
ngs 214| 0 0 -1 36 1 3 -.01 9 8 | 167 -1356 1283 2451
sio 344| 0 0 0 7 -44 -16 .02 12 12 | --- --- --- ---
Table 2.1961.6 GPS week: 1961 Day: 6 MJD: 57977.000
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 274| 1 0 5 11 -13 -2 .04 11 10 | -530 -243 11 87
emr 84| 0 0 -2 56 -9 3 .20 16 15 | 193 -531 16 150
esa 150| 0 0 -2 18 -9 -4 .02 8 8 | -238 -1023 8 146
gfz 197| -1 2 2 -9 3 14 .10 11 11 | 457 -710 11 106
grg 108| 1 0 3 5 5 5 -.31 16 15 | 357 -388 14 182
igr n/a| 0 0 1 0 -10 29 -.01 5 5 | -4007 -140 13 68
jpl 80| 0 0 -1 36 3 48 .24 11 11 | 155 -409 36 195
mit 349| 1 -2 4 -48 11 27 -.11 14 12 | -203 -378 41 298
ngs 212| 0 0 -3 -8 -24 16 .03 9 8 | -500 -307 812 1995
sio 352| -1 -1 0 -26 48 -53 -.00 11 10 | --- --- --- ---
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 3.1961.0 GPS week: 1961 Day: 0 MJD: 57971.000
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 8 9 15 4 10 8 7 6 3 | 35 36 34 34 36 34 36 33 36 34 34
2 | 12 15 6 13 21 6 12 15 9 13 4 | 32 35 32 35 31 32 34 33 33 32 31
3 | 8 14 6 8 10 5 12 8 7 8 3 | 35 33 36 35 36 35 38 32 37 34 34
X4 | 4 --- --- --- --- 30 24 --- --- --- 0 | 70 --- --- --- --- 71 69 --- --- --- 70
5 | 11 10 7 13 14 6 9 10 9 11 4 | 30 30 28 31 27 28 31 23 30 22 26
6 | 12 16 9 14 22 4 11 11 7 10 4 | 38 42 38 38 35 37 39 37 38 36 37
7 | 13 16 10 11 15 5 8 16 9 14 4 | 41 42 38 40 41 38 39 34 38 38 38
8 | 6 13 8 7 10 4 9 8 8 8 3 | 32 32 31 35 33 32 31 30 35 31 32
9 | 8 14 9 10 10 5 10 9 7 9 3 | 51 51 44 52 48 49 49 50 49 51 50
10 | 7 12 5 7 15 4 8 10 7 8 3 | 38 39 38 37 33 36 40 35 39 41 37
11 | 7 11 11 10 15 4 10 10 7 10 3 | 43 44 40 45 39 43 45 45 44 43 42
12E | 11 29 7 11 20 6 18 11 8 11 5 | 55 55 58 61 59 60 54 65 64 64 60
13 | 9 12 12 14 9 5 12 8 9 12 4 | 41 40 39 42 38 40 39 41 41 41 40
14 | 9 12 10 13 9 4 10 12 6 10 3 | 44 41 41 44 42 42 38 47 45 44 43
15 | 8 14 10 12 9 4 15 12 9 12 4 | 64 69 67 54 66 65 68 61 64 52 64
16E | 11 22 7 14 24 5 19 13 10 9 5 | 27 29 36 40 28 35 29 39 35 36 33
17 | 9 14 8 16 20 5 9 14 8 14 4 | 40 42 39 41 34 41 41 47 41 28 40
18 | 11 27 9 14 18 6 16 20 9 12 5 | 36 43 39 38 33 38 41 38 41 40 37
19 | 12 21 7 15 18 6 11 15 8 20 5 | 32 38 33 39 32 35 36 39 35 34 33
20 | 8 12 7 10 16 3 8 11 9 10 3 | 29 28 28 26 26 25 29 22 27 25 25
21 | 8 11 7 11 26 4 9 17 8 11 4 | 35 38 36 40 33 35 38 38 36 34 34
22 | 14 13 9 10 18 6 9 15 11 13 4 | 30 26 27 32 29 31 28 28 35 28 28
23 | 11 24 10 9 8 6 15 13 9 12 4 | 34 37 35 41 35 36 31 41 41 38 37
24 | 6 13 7 12 10 4 12 8 5 5 3 | 32 34 33 33 30 31 35 32 33 34 32
25E | 9 11 9 8 23 5 10 11 8 8 4 | 24 28 28 25 26 24 27 27 25 27 25
26E | 17 17 10 14 32 4 10 9 8 10 5 | 24 31 27 27 25 23 23 24 25 25 24
27 | 9 10 8 6 11 5 10 9 9 8 3 | 30 29 28 30 30 28 29 29 33 30 29
28E | 15 12 6 12 19 4 9 9 10 9 4 | 40 34 34 34 39 34 35 34 33 33 34
29 | 10 25 9 14 15 5 19 18 10 11 5 | 35 36 34 36 34 34 35 37 34 35 34
30 | 6 13 6 9 9 2 10 7 6 6 3 | 34 38 34 33 36 32 35 32 36 35 34
31 | 10 18 13 12 16 6 16 38 12 11 6 | 38 42 40 41 39 37 41 50 35 36 36
32 | 8 14 10 8 10 4 10 12 6 10 3 | 31 38 29 38 30 33 38 36 34 37 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 9 11 17 5 12 14 8 11 |T 37 38 36 37 35 37 38 37 37 36 37
WRMS | 10 16 9 12 15 5 12 12 7 11 |NE 38 38 36 38 35 37 39 37 38 35 37
MEDI | 9 14 8 11 15 5 10 11 8 10 |MD 35 38 35 38 34 35 36 36 36 35 34
Table 3.1961.1 GPS week: 1961 Day: 1 MJD: 57972.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 14 7 6 18 3 11 9 9 7 3 | 20 25 20 21 20 19 25 20 22 20 20
2 | 13 14 7 12 17 6 11 14 8 16 4 | 23 26 23 26 22 24 24 26 24 26 22
3 | 7 13 6 7 16 5 9 9 8 6 3 | 20 22 20 20 24 18 26 19 20 22 19
X4 | 4 --- --- --- --- 50 18 --- --- --- 0 | 67 --- --- --- --- 88 75 --- --- --- 66
5 | 10 9 8 12 24 5 7 11 9 14 4 | 19 20 15 19 23 16 22 11 20 13 15
6 | 10 20 7 8 10 4 9 9 5 7 3 | 24 33 25 22 23 22 29 26 23 25 23
7 | 13 16 13 13 18 5 10 16 11 14 5 | 30 33 27 27 30 24 33 23 28 27 26
8 | 5 12 7 6 11 3 9 7 10 8 3 | 20 23 19 21 16 19 21 19 21 16 19
9 | 10 15 9 7 9 4 9 9 5 11 3 | 36 42 34 35 32 34 44 35 37 40 36
10 | 7 10 5 6 17 5 10 10 7 8 3 | 25 27 25 29 23 24 28 27 29 31 26
11 | 8 12 13 8 15 3 7 10 9 10 4 | 27 31 29 28 25 27 32 30 30 27 27
12E | 10 28 6 12 16 4 22 10 8 8 4 | 37 37 40 43 39 40 37 43 43 41 39
13 | 7 11 12 6 10 4 9 8 9 11 3 | 20 23 18 24 18 20 23 20 25 25 20
14 | 5 12 11 11 15 3 10 14 6 9 3 | 27 22 26 25 24 25 22 29 28 29 25
15 | 7 13 11 12 16 4 18 11 8 12 4 | 41 44 42 37 46 44 44 39 43 37 42
16E | 12 26 8 15 30 6 16 12 11 10 5 | 23 23 24 30 29 26 21 27 29 26 23
17 | 10 20 10 14 19 4 9 13 11 14 5 | 33 38 32 38 28 35 36 40 38 19 34
18 | 9 24 8 14 21 6 16 20 9 11 5 | 18 27 21 22 24 19 27 24 23 21 18
19 | 13 23 9 15 19 5 12 13 10 21 5 | 19 30 20 25 21 21 23 22 22 20 19
20 | 8 10 8 12 21 4 10 13 11 10 4 | 17 16 15 18 21 15 17 16 16 18 14
21 | 11 20 8 10 24 5 13 16 9 13 5 | 22 25 22 27 16 22 25 27 27 26 21
22 | 10 12 11 10 22 5 9 16 11 10 4 | 17 19 17 18 22 15 20 12 16 13 13
23 | 10 22 10 8 6 5 14 14 8 13 4 | 14 18 17 20 15 18 17 19 23 20 16
24 | 7 10 7 8 9 3 13 9 5 7 2 | 15 20 16 17 16 15 24 12 18 20 15
25E | 7 11 9 8 23 6 10 9 10 9 4 | 19 22 22 22 22 20 20 22 22 21 20
26E | 19 13 13 12 23 5 10 8 8 9 5 | 26 23 24 25 22 21 20 24 24 24 22
27 | 8 11 8 6 15 3 9 8 9 8 3 | 17 19 16 17 15 15 20 16 18 17 16
28E | 12 16 7 12 20 4 10 10 7 8 4 | 22 23 20 21 31 19 24 19 21 20 19
29 | 10 22 11 10 15 4 16 15 12 13 5 | 24 21 16 21 18 19 21 23 21 21 19
30 | 7 12 5 9 11 3 9 7 5 7 3 | 25 30 25 24 26 23 32 23 27 29 25
31 | 11 20 11 12 21 7 15 39 12 13 6 | 20 30 21 24 26 20 27 36 23 20 18
32 | 6 13 9 6 12 2 12 13 5 12 3 | 19 30 20 22 17 21 30 21 23 28 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 9 10 18 5 12 14 9 11 |T 24 26 22 24 23 24 27 24 25 23 23
WRMS | 9 16 9 10 17 5 12 11 8 11 |NE 24 26 22 24 22 24 28 23 24 23 23
MEDI | 10 13 8 10 17 4 10 11 9 10 |MD 22 25 21 24 23 21 24 23 23 22 20
Table 3.1961.2 GPS week: 1961 Day: 2 MJD: 57973.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 11 7 8 24 4 10 7 9 9 4 | 30 35 32 35 37 32 33 31 36 33 32
2 | 15 13 6 14 22 5 9 12 8 15 5 | 36 34 34 36 30 33 32 32 36 31 32
3 | 6 11 7 7 18 4 9 7 8 7 3 | 36 38 35 39 41 34 35 35 37 36 36
X4 | 2 --- --- --- --- 26 27 --- --- --- 0 | 107 --- --- --- --- 108 101 --- --- --- 107
5 | 10 10 8 9 16 4 9 10 7 13 3 | 35 36 33 33 35 33 36 31 35 29 32
6 | 10 23 7 10 22 4 10 9 7 8 4 | 35 40 33 32 35 31 36 33 33 34 33
7 | 12 15 13 10 17 4 12 15 11 14 5 | 36 41 34 38 36 34 39 34 37 37 35
8 | 8 12 6 4 17 3 8 5 9 8 3 | 31 31 32 33 31 31 31 30 34 30 31
9 | 10 12 11 7 10 6 11 7 6 9 3 | 42 45 33 41 35 39 42 38 41 40 39
10 | 7 10 6 8 17 2 9 9 5 7 3 | 32 36 33 36 33 32 35 33 33 38 33
11 | 10 9 12 9 20 2 9 8 9 11 4 | 33 37 32 38 34 34 37 34 38 33 34
12E | 15 25 8 9 14 4 18 10 11 10 4 | 26 25 22 27 22 25 25 28 31 28 25
13 | 7 11 12 7 10 3 7 7 7 8 3 | 40 42 38 39 34 40 41 42 43 44 40
14 | 9 10 11 12 14 5 12 13 6 10 4 | 44 44 40 45 44 44 41 42 44 44 43
15 | 8 14 11 8 12 3 14 10 7 12 3 | 73 75 75 55 73 74 78 74 77 58 74
16E | 15 23 9 13 23 5 18 13 8 11 5 | 33 35 32 34 35 32 29 34 34 32 32
X17 | 7 17 9 --- 22 6 10 12 12 --- 5 | 35 37 33 --- 34 32 37 34 38 --- 35
18 | 10 22 9 11 21 5 17 20 8 11 5 | 27 32 27 26 29 24 29 30 26 26 25
19 | 11 22 10 13 21 4 12 13 11 24 5 | 29 34 30 36 28 30 31 33 34 32 30
20 | 8 11 8 8 17 3 10 15 9 8 3 | 38 36 36 36 36 35 37 37 38 35 36
21 | 10 11 8 8 33 5 11 18 7 13 5 | 30 32 31 32 35 29 32 31 31 30 29
22 | 10 10 10 11 21 4 10 15 10 10 4 | 32 34 31 35 36 30 32 30 31 28 30
23 | 8 22 12 9 12 5 19 11 9 11 4 | 37 40 34 41 39 37 35 36 41 36 37
24 | 7 13 11 6 10 3 9 9 5 9 3 | 34 36 34 34 32 34 36 34 36 38 34
25E | 10 11 10 8 22 3 7 9 9 7 4 | 38 40 37 36 39 36 36 38 36 38 36
26E | 16 13 12 12 30 4 9 9 8 9 5 | 41 43 39 41 41 38 36 37 38 39 38
27 | 8 11 6 6 15 3 10 5 7 5 3 | 29 31 30 30 29 29 32 30 33 29 30
28E | 12 14 7 12 22 4 21 9 8 9 4 | 24 28 27 28 30 25 36 28 28 29 26
29 | 8 23 10 10 14 3 13 11 9 11 4 | 42 42 41 43 40 41 42 45 43 43 42
30 | 8 12 8 6 12 3 11 7 8 6 3 | 31 37 33 34 32 33 37 32 37 35 34
31 | 12 19 13 12 19 5 16 35 9 14 6 | 37 40 34 35 34 34 38 39 35 33 32
32 | 8 12 9 7 10 4 10 12 5 10 3 | 25 33 26 32 28 29 32 31 29 34 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 9 9 19 4 12 13 8 11 |T 37 37 34 36 35 36 38 35 36 35 36
WRMS | 10 15 9 9 19 4 12 10 7 10 |NE 38 38 34 36 35 37 39 35 37 35 37
MEDI | 10 12 9 9 17 4 10 10 8 10 |MD 35 36 33 35 35 33 36 34 36 34 33
Table 3.1961.3 GPS week: 1961 Day: 3 MJD: 57974.000
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 | 5 11 8 7 24 3 11 8 5 9 3 | 28 30 28 28 30 27 29 28 28 29 27
2 | 12 14 9 13 21 6 11 13 8 14 4 | 26 30 29 32 26 27 26 27 30 27 27
3 | 8 9 7 7 22 6 10 7 5 8 3 | 28 29 26 29 31 27 32 27 24 29 27
X4 | 2 --- --- --- --- 28 21 --- --- --- 0 | 51 --- --- --- --- 57 51 --- --- --- 50
5 | 9 12 8 8 14 3 10 10 9 9 3 | 27 29 24 27 28 24 28 22 23 23 24
6 | 12 18 7 9 24 3 10 9 9 9 4 | 28 33 28 28 29 28 30 30 31 31 28
7 | 12 16 11 11 21 5 14 13 10 16 5 | 34 36 32 32 37 29 33 26 30 30 30
8 | 7 12 8 7 17 5 9 8 8 9 3 | 28 27 26 27 28 25 28 25 29 29 27
9 | 8 13 9 7 11 5 10 7 5 10 3 | 37 43 27 41 34 37 39 37 36 39 37
10 | 6 11 5 8 19 3 10 11 6 8 3 | 27 29 27 28 29 26 31 27 28 32 27
11 | 7 9 13 9 20 3 10 11 6 11 4 | 35 34 29 36 28 32 34 34 34 33 32
12E | 10 26 6 8 17 3 18 12 9 10 4 | 27 29 27 29 31 26 28 29 31 29 27
13 | 8 9 11 8 12 3 8 9 6 10 3 | 28 30 28 34 29 29 32 31 31 35 30
14 | 8 13 11 12 11 3 11 15 6 12 4 | 25 27 25 29 26 26 26 31 26 28 26
15 | 8 12 11 11 14 3 13 12 9 12 4 | 40 43 41 39 39 37 44 36 38 44 39
16E | 12 22 8 11 25 3 16 12 9 11 4 | 22 27 27 28 26 26 24 26 25 27 24
X17 | 10 23 12 14 25 6 10 14 12 --- 6 | 50 52 48 53 47 48 52 50 50 --- 49
18 | 9 24 7 12 21 5 17 21 9 11 5 | 26 33 26 26 29 24 31 26 25 25 24
19 | 13 20 10 14 21 5 12 15 12 25 6 | 27 29 28 33 27 27 28 29 29 28 27
20 | 10 13 6 9 19 4 11 15 8 10 4 | 26 28 24 24 26 22 29 26 24 26 24
21 | 9 11 7 7 29 5 10 16 9 11 4 | 25 26 26 28 26 26 29 26 30 25 25
22 | 10 10 8 11 26 5 10 17 7 13 4 | 24 24 24 25 30 23 25 23 23 24 22
23 | 8 21 9 10 10 5 15 13 6 14 4 | 28 28 26 32 27 27 24 28 28 29 27
24 | 7 12 9 6 11 3 12 12 4 10 3 | 26 28 28 28 25 26 29 27 27 32 27
25E | 10 13 8 5 16 3 8 11 7 8 3 | 28 29 28 26 28 26 28 26 28 28 26
26E | 13 15 12 10 19 3 10 9 7 7 4 | 23 29 27 28 25 24 23 25 25 23 24
27 | 7 13 7 7 19 4 9 8 7 8 3 | 24 24 25 23 24 22 28 25 26 27 24
28E | 12 14 7 10 22 3 12 10 8 11 4 | 28 25 27 30 28 25 30 27 24 30 26
29 | 7 21 11 10 15 4 15 13 9 12 4 | 28 30 26 27 27 27 30 26 29 28 26
30 | 9 11 6 7 12 3 10 6 4 7 2 | 31 35 31 34 32 29 35 28 31 31 31
31 | 12 19 12 12 15 5 14 31 10 13 5 | 33 35 31 29 34 28 33 33 31 29 28
32 | 7 13 10 8 9 2 10 12 7 10 3 | 26 32 23 27 23 27 34 31 26 32 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 9 9 19 4 12 13 8 11 |T 29 31 28 30 29 28 31 28 29 29 28
WRMS | 9 15 9 9 19 4 12 11 7 10 |NE 30 31 28 30 29 29 32 29 29 29 29
MEDI | 9 13 8 9 19 3 10 12 8 10 |MD 28 29 27 28 28 27 29 27 28 29 27
Table 3.1961.4 GPS week: 1961 Day: 4 MJD: 57975.000
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 | 5 10 5 8 20 3 12 8 6 9 3 | 28 30 28 29 29 27 31 26 27 33 27
2 | 10 10 8 14 19 4 11 13 9 14 4 | 24 23 23 31 23 24 24 24 26 25 23
3 | 8 10 6 8 17 3 11 7 5 8 3 | 27 25 24 24 26 23 28 21 25 26 24
X4 | 2 --- --- --- --- 24 28 --- --- --- 0 | 75 --- --- --- --- 75 71 --- --- --- 74
5 | 7 11 8 9 13 4 10 12 9 13 3 | 26 25 20 26 22 22 25 18 24 24 21
6 | 11 15 6 11 25 3 12 8 7 10 4 | 23 28 23 24 26 23 27 24 23 27 23
7 | 11 15 9 10 14 4 10 13 10 14 4 | 25 29 23 23 24 22 30 19 22 23 22
8 | 8 12 6 7 12 3 8 7 6 8 3 | 22 25 23 23 23 21 27 22 22 25 22
9 | 8 14 9 6 8 3 12 8 9 9 3 | 27 36 40 31 25 28 48 33 26 33 28
10 | 8 12 6 9 16 5 9 10 6 8 3 | 27 29 26 27 28 25 30 25 26 30 26
11 | 5 8 11 9 15 4 9 11 6 11 3 | 29 31 27 29 24 28 33 30 27 28 27
12E | 7 25 6 11 23 2 19 11 9 8 4 | 30 30 28 33 32 28 30 32 29 32 29
13 | 8 10 10 9 7 3 6 10 9 8 3 | 27 27 26 26 25 26 28 30 27 29 26
14 | 5 10 10 11 9 3 9 13 7 12 3 | 34 31 31 35 31 33 30 36 34 34 33
X15 | 9 11 12 --- 19 6 13 18 12 --- 5 | 83 84 86 --- 79 84 87 83 87 --- 84
16E | 13 30 8 15 27 5 17 13 11 11 5 | 14 23 19 24 20 19 18 22 21 20 17
17 | 9 16 10 14 21 5 13 15 9 17 5 | 26 28 22 27 22 23 30 27 27 38 23
18 | 11 24 7 15 19 6 17 22 10 15 5 | 24 27 23 24 26 21 27 25 24 26 21
19 | 11 21 8 16 19 6 13 13 9 22 5 | 23 27 23 28 19 22 26 25 25 25 22
20 | 10 10 6 10 18 4 12 15 9 10 4 | 26 22 22 21 23 21 23 19 23 21 21
21 | 8 9 9 9 28 6 9 18 10 15 5 | 24 23 20 26 23 23 25 24 26 24 20
22 | 12 10 7 12 19 4 12 17 9 13 4 | 24 21 20 22 24 20 22 18 22 20 18
23 | 8 23 8 10 8 5 16 14 8 13 4 | 20 23 19 26 20 21 21 25 24 25 21
24 | 8 10 9 7 13 4 10 10 4 10 3 | 22 25 21 24 19 22 27 21 22 29 22
25E | 8 11 9 5 19 3 10 9 7 8 3 | 18 25 21 20 22 19 22 23 19 21 19
26E | 13 12 11 9 33 4 9 10 7 9 4 | 21 25 22 23 28 19 20 23 17 21 19
27 | 11 12 8 9 14 3 11 9 7 9 3 | 21 23 23 21 21 20 25 22 21 25 21
28E | 11 11 6 11 19 3 8 10 8 9 3 | 27 26 26 25 27 25 26 26 25 25 24
29 | 8 21 12 12 16 3 15 13 11 12 4 | 36 34 33 36 33 33 37 36 35 36 34
30 | 7 12 7 6 10 3 7 6 7 8 3 | 24 31 26 26 26 25 32 23 29 27 25
31 | 10 17 11 11 12 6 13 30 10 16 5 | 23 30 22 23 20 22 29 26 20 23 19
32 | 6 13 9 9 8 3 10 10 6 11 3 | 24 31 23 24 23 24 31 28 24 32 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 15 8 10 18 4 12 13 8 12 |T 28 28 26 26 26 27 30 26 26 26 26
WRMS | 9 15 9 10 16 4 12 11 7 10 |NE 29 29 26 26 26 28 32 27 27 27 27
MEDI | 8 12 8 9 17 4 11 11 9 10 |MD 24 27 23 25 24 23 27 25 25 25 23
Table 3.1961.5 GPS week: 1961 Day: 5 MJD: 57976.000
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 12 6 8 16 3 9 7 7 9 3 | 26 27 26 24 23 23 27 25 25 30 25
2 | 15 10 8 15 22 4 12 15 12 16 5 | 23 26 21 31 17 24 20 23 27 21 21
3 | 9 10 7 7 11 3 10 5 6 9 3 | 23 27 22 23 26 21 26 20 22 23 22
X4 | 1 --- --- --- --- 38 21 --- --- --- 0 | 42 --- --- --- --- 44 40 --- --- --- 42
5 | 9 12 9 7 9 3 9 11 9 12 3 | 23 25 19 24 20 20 22 12 18 16 18
6 | 13 17 8 14 22 3 9 9 7 11 4 | 24 31 22 26 21 21 26 23 23 25 22
7 | 22 15 8 10 16 5 10 12 11 15 5 | 32 30 23 23 22 23 26 22 24 26 23
8 | 7 13 7 9 12 3 8 7 9 12 3 | 19 20 21 19 18 17 21 17 18 22 18
X9 | 11 14 --- 8 11 7 --- 8 8 12 4 | 91 88 --- 86 83 85 --- 87 83 89 87
10 | 7 17 7 9 15 3 10 13 5 11 3 | 22 27 19 22 24 20 23 22 21 24 20
11 | 6 11 11 8 12 4 8 10 8 9 3 | 25 27 23 24 24 22 27 25 24 22 23
12E | 13 25 7 8 23 2 18 12 12 13 5 | 24 28 30 36 26 30 27 33 37 34 31
13 | 12 12 13 7 7 4 9 11 7 10 4 | 24 32 24 28 22 26 26 30 23 29 25
14 | 8 11 10 13 9 5 11 15 7 13 4 | 35 34 32 33 34 35 34 40 37 41 34
15 | 9 11 11 7 8 3 14 12 9 14 4 | 52 57 51 71 54 52 51 51 48 74 51
16E | 14 29 8 13 16 4 14 11 9 9 5 | 13 23 18 22 16 16 13 16 19 18 15
17 | 11 15 10 13 19 3 12 13 9 17 5 | 38 36 34 29 35 32 40 33 33 21 32
18 | 12 25 10 13 19 5 16 22 9 12 5 | 18 27 19 19 23 15 21 19 15 16 14
19 | 14 21 9 14 19 4 14 14 10 20 5 | 19 26 20 27 14 21 21 22 22 19 19
20 | 11 10 7 7 13 3 9 17 7 9 3 | 24 23 19 22 25 20 23 15 17 19 18
X21 | 9 --- 9 10 25 5 22 20 7 14 5 | 18 --- 17 23 19 18 27 21 21 18 16
22 | 11 15 9 10 17 4 10 16 9 11 4 | 18 21 16 19 25 16 18 13 14 9 13
23 | 12 22 9 11 7 5 14 12 8 13 4 | 14 24 18 24 19 19 19 22 21 21 18
24 | 8 11 10 5 9 3 8 11 5 11 3 | 23 27 25 25 18 24 25 25 22 33 24
25E | 11 14 10 5 23 4 9 9 9 9 4 | 24 24 23 23 28 23 25 24 22 26 22
26E | 13 14 11 10 20 4 9 8 9 11 4 | 23 28 26 25 26 23 25 23 26 27 23
27 | 11 15 7 8 11 4 11 6 8 10 3 | 21 23 24 18 20 20 26 22 24 27 21
28E | 14 13 6 9 12 3 13 8 9 10 3 | 23 22 19 20 18 18 21 22 21 22 18
29 | 12 16 11 12 14 4 14 13 11 14 4 | 31 32 27 34 29 30 31 30 28 37 30
30 | 10 13 5 8 13 4 11 5 8 8 3 | 24 28 23 20 19 22 25 20 25 25 22
31 | 12 16 11 13 15 6 13 31 12 15 6 | 21 29 19 20 18 20 27 23 19 23 16
32 | 6 12 9 8 9 4 10 11 7 9 3 | 17 29 20 20 18 19 28 24 20 26 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 9 10 15 4 11 13 9 12 |T 26 30 23 27 25 25 26 25 25 27 25
WRMS | 11 16 9 10 14 4 11 10 8 12 |NE 27 31 23 28 25 26 26 26 25 28 25
MEDI | 11 14 9 9 14 4 11 11 9 11 |MD 23 27 22 24 22 21 26 23 22 24 22
Table 3.1961.6 GPS week: 1961 Day: 6 MJD: 57977.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 11 6 8 15 2 8 7 7 8 3 | 31 36 35 34 31 32 37 34 32 39 33
2 | 12 11 7 19 19 6 9 15 11 13 5 | 35 34 35 43 33 35 33 36 38 37 35
3 | 6 10 7 7 16 5 10 7 6 7 3 | 36 41 34 36 41 34 35 36 32 40 36
X4 | 3 --- --- --- --- 21 24 --- --- --- 0 | 60 --- --- --- --- 62 61 --- --- --- 60
5 | 8 13 7 8 16 4 10 11 9 14 4 | 39 41 34 39 41 35 35 35 34 37 36
6 | 11 13 7 11 21 3 9 11 9 9 4 | 37 35 36 35 34 32 36 35 32 36 34
7 | 12 15 9 11 11 4 8 13 10 13 4 | 42 43 38 36 40 36 43 32 38 36 37
8 | 8 12 6 8 12 3 9 7 6 7 3 | 31 32 30 29 30 29 33 30 29 32 30
9 | 9 12 8 7 10 5 12 12 8 8 3 | 142 139 130 142 141 141 131 143 141 142 141
10 | 10 12 6 6 15 5 8 14 7 7 3 | 34 38 32 35 36 31 37 34 34 43 34
11 | 7 9 10 9 13 3 8 12 8 11 3 | 44 47 44 47 40 44 49 47 45 46 44
12E | 13 27 6 10 16 5 17 14 10 11 5 | 22 26 27 32 26 28 24 34 32 30 27
13 | 7 11 10 7 10 3 9 10 8 8 3 | 43 47 43 44 40 43 46 47 43 47 44
14 | 6 10 11 18 11 4 12 16 9 15 4 | 47 43 43 46 44 45 43 50 47 48 45
15 | 10 11 11 10 9 2 11 12 12 14 4 | 69 71 71 61 70 69 73 68 71 67 69
16E | 15 25 6 14 20 6 16 13 10 12 5 | 25 29 25 27 31 22 23 23 23 27 23
17 | 14 13 9 16 21 6 9 16 12 15 5 | 57 53 55 49 50 50 56 49 53 43 52
18 | 13 28 8 13 21 7 15 22 11 12 5 | 28 37 28 24 32 24 31 24 24 26 24
19 | 15 18 8 18 22 7 11 17 12 20 6 | 33 34 34 41 29 34 35 37 38 39 34
20 | 10 10 7 10 13 3 11 12 10 10 3 | 42 40 40 43 45 39 39 40 41 42 41
21 | 8 9 7 10 23 5 8 22 8 13 4 | 30 31 28 35 35 29 33 32 31 34 29
22 | 11 13 8 10 19 4 10 17 10 12 4 | 34 37 32 30 41 29 33 28 25 29 30
23 | 11 23 8 11 8 5 13 13 9 12 4 | 34 41 34 38 36 34 34 36 35 35 34
24 | 6 12 9 9 8 4 8 10 8 8 3 | 36 40 39 38 35 37 41 37 36 43 37
25E | 12 43 9 7 20 5 9 11 7 8 6 | 48 64 45 47 50 46 47 47 46 48 47
26E | 19 11 12 17 23 6 10 9 11 7 5 | 46 47 45 45 50 42 43 43 44 47 45
27 | 9 13 7 9 12 4 10 9 4 6 3 | 31 33 33 30 32 30 35 34 31 36 32
28E | 14 12 7 12 17 5 8 8 8 8 4 | 29 31 31 32 28 28 29 27 28 33 29
29 | 8 19 10 14 13 4 12 15 10 14 4 | 42 41 39 45 41 40 43 43 39 49 41
30 | 6 12 5 7 7 4 11 5 6 6 2 | 36 39 36 38 37 36 42 34 36 39 36
31 | 11 16 10 13 13 5 13 30 11 16 5 | 37 42 36 31 39 32 40 31 31 33 32
32 | 8 12 10 10 9 4 12 13 9 9 3 | 31 37 32 34 32 32 41 38 33 38 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 8 11 16 5 11 14 9 11 |T 41 43 40 41 41 40 42 40 40 42 40
WRMS | 10 15 8 11 15 5 11 12 8 10 |NE 43 44 41 42 42 41 44 41 41 43 41
MEDI | 10 12 8 10 15 4 10 12 9 11 |MD 36 40 35 38 37 34 37 36 35 39 35
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 4.1961 GPS week: 1961 MJD: 57971.0-57977.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 |U 7 6 15 |U 6 7 22 |U 8 10 19 |
emr | emr 2958 |U 9 7 19 |U 7 9 27 |U 9 11 20 |
esa | esa 2962 | 8 6 16 |U 6 8 24 | 8 10 19 |
gfz | gfz 2945 |U 8 6 15 |U 6 8 23 |U 8 9 18 |
grg | grg 2972 |U 8 7 15 |U 6 8 24 | 9 11 21 |
igr | igr 2971 | 8 6 15 | 6 7 21 | 8 9 19 |
igs | igs 2971 | 8 6 14 | 5 7 22 | 8 9 19 |
jpl | jpl 3058 | 8 7 18 |U 6 8 24 |U 9 12 21 |
mit | mit 2976 | 8 7 17 |U 7 8 27 |U 9 12 21 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.1961.0 GPS week: 1961 Day: 0 MJD: 57971.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 5 14 | 10 9 24 | 8 12 20 |
emr | emr 2976 | 7 5 14 | 9 8 28 | 7 13 21 |
esa | esa 2976 | 7 5 12 | 9 10 23 | 8 11 21 |
gfz | gfz 2976 | 8 5 12 | 9 9 22 | 8 11 19 |
grg | grg 2976 | 7 5 14 | 9 10 26 | 10 12 23 |
igr | igr 2976 | 8 4 13 | 10 10 21 | 7 10 20 |
igs | igs 2976 | 7 5 12 | 9 9 22 | 8 11 20 |
jpl | jpl 3072 | 7 5 13 | 9 10 23 | 8 13 24 |
mit | mit 2976 | 7 5 13 | 10 11 26 | 9 13 22 |
Table 5.1961.1 GPS week: 1961 Day: 1 MJD: 57972.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 5 11 | 8 8 31 | 8 9 20 |
emr | emr 2974 | 9 8 19 | 7 10 32 | 8 7 14 |
esa | esa 2976 | 6 6 12 | 7 8 31 | 8 10 20 |
gfz | gfz 2976 | 6 6 10 | 8 8 32 | 8 9 19 |
grg | grg 2976 | 6 6 11 | 7 8 31 | 8 10 20 |
igr | igr 2971 | 6 5 11 | 7 7 30 | 8 9 20 |
igs | igs 2971 | 5 5 10 | 7 8 31 | 7 9 19 |
jpl | jpl 3072 | 6 6 16 | 7 8 33 | 9 9 21 |
mit | mit 2976 | 7 11 22 | 11 11 43 | 9 13 21 |
Table 5.1961.2 GPS week: 1961 Day: 2 MJD: 57973.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 7 17 | 4 7 19 | 8 13 20 |
emr | emr 2976 | 10 6 21 | 6 11 30 | 11 15 23 |
esa | esa 2976 | 9 7 17 | 4 9 22 | 7 12 20 |
gfz | gfz 2878 | 9 7 18 | 4 8 24 | 8 13 22 |
grg | grg 2976 | 8 7 16 | 5 7 21 | 8 15 23 |
igr | igr 2976 | 9 8 17 | 4 7 19 | 8 13 21 |
igs | igs 2976 | 9 7 16 | 4 8 20 | 7 13 21 |
jpl | jpl 3072 | 8 6 18 | 5 10 23 | 8 15 21 |
mit | mit 2976 | 10 7 18 | 4 8 24 | 9 16 25 |
Table 5.1961.3 GPS week: 1961 Day: 3 MJD: 57974.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3066 | 7 4 16 | 4 5 19 | 8 11 19 |
emr | emr 2970 | 9 9 20 | 6 6 24 | 9 14 18 |
esa | esa 2976 | 7 4 14 | 5 5 20 | 9 11 17 |
gfz | gfz 2970 | 7 4 14 | 4 5 20 | 10 11 18 |
grg | grg 2970 | 7 4 14 | 5 7 21 | 9 12 20 |
igr | igr 2970 | 8 4 14 | 4 4 20 | 9 11 16 |
igs | igs 2970 | 8 4 13 | 4 4 18 | 8 11 16 |
jpl | jpl 3072 | 7 6 18 | 5 5 20 | 8 13 19 |
mit | mit 2976 | 7 4 15 | 6 6 21 | 9 12 16 |
Table 5.1961.4 GPS week: 1961 Day: 4 MJD: 57975.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 8 9 15 | 5 7 22 | 7 9 19 |
emr | emr 2969 | 10 7 22 | 7 10 28 | 9 9 17 |
esa | esa 2976 | 9 9 16 | 6 8 24 | 7 9 18 |
gfz | gfz 2880 | 9 9 16 | 5 9 25 | 8 8 16 |
grg | grg 2970 | 9 9 16 | 6 8 22 | 8 9 20 |
igr | igr 2969 | 9 9 17 | 5 7 21 | 7 8 19 |
igs | igs 2969 | 9 9 16 | 5 8 22 | 7 8 17 |
jpl | jpl 3072 | 9 8 16 | 6 10 23 | 9 11 18 |
mit | mit 2976 | 9 9 16 | 5 7 23 | 9 9 19 |
Table 5.1961.5 GPS week: 1961 Day: 5 MJD: 57976.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 7 3 17 | 5 6 20 | 9 8 16 |
emr | emr 2869 | 8 5 19 | 6 7 27 | 10 9 25 |
esa | esa 2880 | 7 4 24 | 5 7 24 | 9 7 18 |
gfz | gfz 2965 | 9 4 15 | 5 7 21 | 10 8 16 |
grg | grg 2965 | 7 4 17 | 6 7 25 | 10 8 24 |
igr | igr 2960 | 8 3 14 | 5 6 20 | 9 7 19 |
igs | igs 2965 | 8 3 15 | 5 6 21 | 9 7 18 |
jpl | jpl 2976 | 8 6 24 | 5 7 24 | 10 10 22 |
mit | mit 2976 | 7 4 16 | 6 7 27 | 10 8 22 |
Table 5.1961.6 GPS week: 1961 Day: 6 MJD: 57977.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 9 18 | 5 6 21 | 9 9 18 |
emr | emr 2976 | 10 9 22 | 6 8 23 | 9 12 23 |
esa | esa 2976 | 10 9 18 | 5 7 22 | 9 9 19 |
gfz | gfz 2973 | 10 9 18 | 5 6 21 | 9 7 17 |
grg | grg 2976 | 10 10 18 | 6 8 23 | 10 9 19 |
igr | igr 2976 | 11 9 18 | 5 6 19 | 9 8 18 |
igs | igs 2976 | 10 9 18 | 5 6 20 | 9 8 18 |
jpl | jpl 3072 | 11 9 19 | 6 8 23 | 10 12 21 |
mit | mit 2976 | 10 9 16 | 7 6 24 | 10 11 22 |
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 6.1961 GPS week: 1961 MJD: 57971.500-57977.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 -9 71 166 -3 | 22 30
| 22 15 50 119 5 | 4
emr uuuuu | -7 -11 -25 -102 1 | 16 31
| 14 19 81 75 19 | 8
esa uuuuu | 3 8 20 102 -2 | 27 34
| 9 12 30 51 3 | 4
gfz uuuuu | -13 13 133 -91 2 | 34 39
| 13 16 25 79 9 | 3
grg uuuuu | 13 -22 -24 8 -3 | 4 20
| 22 18 22 75 3 | 4
igr xxxxx | 2 18 34 -51 -2 | -2 19
| 12 8 55 30 2 | 4
irf xxxxx | 1 -17 -16 -66 8 | -6 22
| 11 8 19 23 5 | 4
jpl xxxxx | 25 -20 3 39 1 | 33 38
| 37 42 69 33 8 | 3
mit uuuuu | -1 -14 -49 -148 5 | 27 34
| 26 16 24 66 3 | 4
ngs uuuuu | -15 -2 33 -116 1 | 23 30
| 30 20 62 78 11 | 3
sio uuuux | 34 17 -229 88 7 | 53 57
| 12 10 61 51 10 | 4
Table 7.1961.0 GPS week: 1961 Day: 0 MJD: 57971.500
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 -44 104 191 2 | 29 32
emr uuuuu | 2 0 28 -159 -27 | 31 38
esa uuuuu | 15 18 7 140 -4 | 33 36
gfz uuuuu | -37 16 123 -230 16 | 36 39
grg uuuuu | -9 4 -55 -103 -1 | 10 18
igr xxxxx | 2 11 62 -61 0 | 4 14
irf xxxxx | 11 -33 11 -75 1 | 0 18
jpl xxxxx | 45 -33 -10 49 3 | 37 41
mit uuuuu | 30 -37 -7 -81 -1 | 33 37
ngs uuuuu | -31 7 56 -64 13 | 24 30
sio uuuux | 52 23 -285 58 -5 | 59 61
Table 7.1961.1 GPS week: 1961 Day: 1 MJD: 57972.500
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 | 10 -2 20 25 -3 | 25 31
emr uuuuu | 10 -38 41 8 -12 | 23 36
esa uuuuu | -7 27 -8 19 0 | 29 35
gfz uuuuu | -10 36 115 -126 -1 | 35 39
grg uuuuu | -8 -46 -15 -4 -2 | 7 19
igr xxxxx | -5 21 90 -72 0 | 1 16
irf xxxxx | 7 -18 7 -62 8 | -5 20
jpl xxxxx | 26 -75 78 23 11 | 34 39
mit uuuuu | 16 -29 -47 -98 5 | 29 35
ngs uuuuu | -35 -14 50 31 11 | 22 29
sio uuuux | 45 10 -177 99 3 | 55 58
Table 7.1961.2 GPS week: 1961 Day: 2 MJD: 57973.500
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 | 11 -5 82 253 -6 | 21 31
emr uuuuu | -16 -6 -72 -176 -8 | 15 34
esa uuuuu | 12 -4 21 81 0 | 25 34
gfz uuuuu | 6 -5 117 -21 8 | 31 38
grg uuuuu | 27 -41 -12 30 -7 | 3 23
igr xxxxx | 2 14 42 -12 -2 | -3 22
irf xxxxx | 5 -7 -36 -69 15 | -9 24
jpl xxxxx | 74 -76 -45 52 7 | 32 38
mit uuuuu | 3 -20 -78 -156 9 | 25 34
ngs uuuuu | -52 27 107 -188 10 | 20 29
sio uuuux | 33 16 -288 110 4 | 51 56
Table 7.1961.3 GPS week: 1961 Day: 3 MJD: 57974.500
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 -5 40 190 -4 | 18 26
emr uuuuu | 4 -21 31 -173 1 | 9 26
esa uuuuu | 12 12 34 89 2 | 22 31
gfz uuuuu | -7 -5 176 -94 6 | 30 36
grg uuuuu | 34 -10 14 -45 -4 | -1 20
igr xxxxx | 14 17 87 -33 -1 | -6 20
irf xxxxx | 8 -18 -11 -47 12 | -11 22
jpl xxxxx | 58 11 48 20 -14 | 29 35
mit uuuuu | 27 -14 -63 -106 3 | 22 29
ngs uuuuu | -30 11 -81 -115 3 | 19 28
sio uuuux | 32 9 -151 129 -4 | 48 52
Table 7.1961.4 GPS week: 1961 Day: 4 MJD: 57975.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -21 -1 139 115 5 | 17 26
emr uuuuu | -20 15 -71 -130 6 | 8 25
esa uuuuu | 2 7 -8 167 -3 | 23 32
gfz uuuuu | -10 2 121 -124 -3 | 31 38
grg uuuuu | 44 -27 -37 122 -6 | -1 20
igr xxxxx | 20 34 -61 -56 -2 | -6 20
irf xxxxx | 7 -16 -37 -52 12 | -10 23
jpl xxxxx | 20 11 -122 102 3 | 29 34
mit uuuuu | -25 -3 -61 -164 5 | 23 30
ngs uuuuu | 12 -7 24 -151 -2 | 21 29
sio uuuux | 33 7 -231 108 13 | 48 51
Table 7.1961.5 GPS week: 1961 Day: 5 MJD: 57976.500
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 0 5 33 -11 | 22 30
emr uuuuu | -3 1 39 -43 32 | 12 27
esa uuuuu | -8 6 15 144 -7 | 27 35
gfz uuuuu | -19 26 161 -42 -6 | 36 41
grg uuuuu | 11 -9 -31 77 -6 | 3 20
igr xxxxx | -5 15 -14 -25 -6 | -2 19
irf xxxxx | -16 -14 -27 -44 5 | -3 21
jpl xxxxx | -16 26 47 3 -4 | 34 38
mit uuuuu | -28 0 -58 -152 7 | 28 34
ngs uuuuu | 30 -36 -6 -140 -14 | 25 32
sio uuuux | 28 23 -174 126 14 | 53 57
Table 7.1961.6 GPS week: 1961 Day: 6 MJD: 57977.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 36 -9 105 356 -4 | 23 31
emr uuuuu | -26 -28 -168 -44 14 | 15 33
esa uuuuu | -1 -9 77 72 -2 | 28 35
gfz uuuuu | -15 22 120 2 -8 | 37 43
grg uuuuu | -7 -25 -32 -19 1 | 4 21
igr xxxxx | -16 12 32 -101 0 | -1 20
irf xxxxx | -14 -15 -17 -111 3 | -1 23
jpl xxxxx | -28 -2 25 20 2 | 36 40
mit uuuuu | -27 6 -31 -278 6 | 30 37
ngs uuuuu | 4 -2 79 -185 -11 | 27 33
sio uuuux | 13 33 -294 -15 24 | 56 60
More information about the IGSREPORT
mailing list