[IGSREPORT-25683] Wk 1980 IGS Final Orbits
acc
acc at igs.org
Tue Jan 9 19:18:10 PST 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1980 (Dec 17, 2017 - Dec 23, 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:
igs1980[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1980[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1980[0-6].cls IGS GPS clock combination summary report.
igs19807.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19807.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 | ALRT MAW1 TIXI
0 | EMR | YELL
0 | ESA | BRAZ CHTI BRAZ CHTI
0 | GFZ | FAA1 GODE POHN FAA1 GODE POHN
0 | GRG | 6 8 6 ADIS BJFS BOGT BRFT BRST BRUX CAS1 CCJ2 CHTI
0 | GRG | COCO DARW DAV1 DGAR DUBO FAA1 GLPS GLSV GMSD HOFN
0 | GRG | HOLB HYDE INVK IRKJ KARR KIRU KRGG LHAZ LMMF LPGS
0 | GRG | MAS1 MAW1 MCIL MCM4 MGUE MOBS NAIN NKLG NNOR NRIL
0 | GRG | OHI3 OUS2 PDEL PIMO RABT REUN SCRZ SEYG SHAO SSIA
0 | GRG | SUTH TEHN TLSE TONG TOW2 TRO1 TUVA ULAB VILL XMIS
0 | GRG | YELL CHTI FAA1 KIRU KRGG NKLG REUN TONG TRO1
1 | COD | TIXI FAA1 TIXI
1 | EMR | 20 25 2 20 25
1 | ESA | REUN CHTI REUN
1 | GFZ | GODE MAL2 CHTI GODE MAL2
1 | GRG | ADIS DAV1 FAA1 GLSV HOLB JFNG NKLG ADIS DAV1 FAA1
1 | GRG | GLSV HOLB JFNG NKLG
2 | COD | TIXI TIXI
2 | ESA | FAA1 FAA1 MAL2
2 | GFZ | BOGT GODE MAL2 GODE MAL2 NIST
2 | GRG | ADIS BOGT FAA1 GLSV SEYG WIND ADIS BOGT FAA1 GLSV
2 | GRG | REUN SEYG TONG
2 | MIT | BOGT BOGT
3 | COD | GLSV OHI2 TIXI GLSV HARB OHI2 TIXI ZAMB
3 | EMR | 25
3 | ESA | FAA1 NTUS
3 | GFZ | GODE SAVO GODE SAVO
3 | GRG | 21 21 GLSV MAL2 REUN TASH WIND GLSV MAL2 REUN TASH
3 | GRG | TONG WIND
4 | COD | TIXI TIXI
4 | ESA | MAL2 JFNG MAL2 REUN
4 | GFZ | CAS1 FAA1 GODE MAL2 CAS1 FAA1 GODE MAL2
4 | GRG | FAA1 GLSV SEYG FAA1 GLSV MCIL SEYG TONG
5 | COD | HARB OHI2 TIXI HARB OHI2 TIXI
5 | ESA | HYDE HYDE
5 | GFZ | BJNM FAA1 GODE MAL2 REUN SAVO BJNM FAA1 GODE MAL2
5 | GFZ | REUN SAVO
5 | GRG | 6 FAA1 GLSV MAL2 SEYG TASH WIND FAA1 GLSV MAL2 SEYG
5 | GRG | TASH TONG WIND
6 | COD | OHI2 TIXI WTZR OHI2 TIXI WTZR
6 | EMR | 25 25
6 | ESA | AREQ FAA1 MAL2 AREQ FAA1 MAL2
6 | GFZ | 25 25 GODE GODE
6 | GRG | ADIS ALRT GLSV JFNG ADIS ALRT GLSV JFNG TONG VILL
6 | MIT | 26 26 AREQ AREQ KIRU
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | ESA | ~15:35 | ~ 0.06 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. 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.
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 .2 1.1 3 19 -8 -.43
EMR | 0 | -2.0 4.5 1.7 -13 -6 -7 -.17
ESA | 0 | .5 -.4 .8 7 4 6 -.46
GFZ | 0 | .5 .2 .5 -12 -36 -10 -.15
GRG | 0 | 8.5 1.8 -1.0 15 4 5 -.19
JPL | 0 | 12.1 12.3 1.3 1 -22 75 .28
MIT | 0 | 5.1 4.6 2.2 18 22 -28 -.04
NGS | 0 | 5.2 5.0 -4.9 31 -14 -20 -.17
SIO | 0 | 1.4 10.2 1.7 37 -36 -11 -.20
COD | 1 | -.1 .3 .6 7 7 -12 -.40
EMR | 1 | 4.8 5.8 2.2 -24 -11 1 -.20
ESA | 1 | -.4 -.7 1.2 -5 25 29 -.56
GFZ | 1 | .3 .3 .5 -12 -16 -7 -.13
GRG | 1 | 6.2 6.4 1.4 9 52 -8 -.19
JPL | 1 | 3.7 4.9 3.7 -22 -41 66 .25
MIT | 1 | 8.4 2.1 -1.2 -4 29 -7 -.17
NGS | 1 | -1.0 4.6 -3.0 33 -37 22 -.10
SIO | 1 | 2.0 8.0 -12.3 9 -5 -14 -.14
COD | 2 | -.2 .4 .2 7 10 -15 -.30
EMR | 2 | 4.8 3.3 .8 -7 -2 -9 -.13
ESA | 2 | .2 .0 1.1 -2 1 8 -.47
GFZ | 2 | -.1 -.1 .4 -24 -5 -1 -.20
GRG | 2 | 6.3 8.5 .4 29 -3 -32 -.05
JPL | 2 | 8.9 6.1 5.8 -20 -32 78 .10
MIT | 2 | 7.1 7.0 .2 -3 26 -12 .14
NGS | 2 | 1.4 8.8 5.9 42 -43 -6 -.09
SIO | 2 | 4.2 5.0 -10.5 29 -2 -31 .01
COD | 3 | .3 .2 .4 2 -5 1 -.24
EMR | 3 | 5.2 1.4 9.2 -16 6 -19 -.07
ESA | 3 | .3 .3 .3 4 22 -8 -.21
GFZ | 3 | -.2 -.1 .1 -18 -6 -1 -.11
GRG | 3 | 5.0 3.5 -10.2 28 9 1 .03
JPL | 3 | 8.3 7.9 5.7 17 -60 73 .23
MIT | 3 | 5.9 1.6 3.1 -9 54 -11 .16
NGS | 3 | 5.1 2.4 2.7 22 -10 -11 -.14
SIO | 3 | 3.1 3.7 -5.6 28 7 -23 -.06
COD | 4 | .4 .3 .4 9 -2 -3 -.17
EMR | 4 | 5.3 3.7 11.7 -13 2 -29 .08
ESA | 4 | .1 .4 .5 -4 17 0 -.27
GFZ | 4 | -.1 .0 -.0 -16 -7 0 -.04
GRG | 4 | 3.0 3.0 1.3 22 37 -31 -.12
JPL | 4 | 9.7 -4.5 8.7 -8 -42 95 .43
MIT | 4 | 6.9 2.4 9.1 -21 37 -12 .30
NGS | 4 | 6.6 6.1 .4 12 -17 -6 .08
SIO | 4 | 7.3 3.7 -2.2 -9 3 -6 -.06
COD | 5 | .1 .1 -.0 0 3 -7 -.13
EMR | 5 | 1.3 3.5 14.7 -9 11 0 .23
ESA | 5 | .3 .0 .5 -5 2 19 -.21
GFZ | 5 | .0 -.0 .1 -10 -8 0 -.04
GRG | 5 | 7.0 6.9 -4.2 23 28 -18 -.19
JPL | 5 | 12.4 -.7 8.6 10 -46 21 .41
MIT | 5 | 7.9 -.1 6.7 -26 51 -17 .17
NGS | 5 | 1.9 -1.5 -.4 -14 18 -21 .07
SIO | 5 | 6.1 .5 -4.9 1 -9 -14 -.07
COD | 6 | .3 .2 .5 2 0 2 -.38
EMR | 6 | 9.2 2.5 13.4 -21 -2 -12 -.01
ESA | 6 | -.2 -.1 -.1 -11 -10 24 -.29
GFZ | 6 | .0 .1 .5 -4 -12 3 -.20
GRG | 6 | 6.7 -3.2 1.3 22 13 13 .09
JPL | 6 | 10.5 4.9 11.7 3 3 65 .21
MIT | 6 | 6.7 .7 7.3 -31 33 23 .04
NGS | 6 | 2.7 1.8 -1.4 10 -10 1 -.07
SIO | 6 | 1.9 1.3 -5.3 11 -9 -9 -.07
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.
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 1.1980.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1980.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 2.1980.[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 3.1980.[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 5.1980.0-6). 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 1980 summary. (Dec 17, 2017 - Dec 23, 2017)
Table 1.1980.a GPS week: 1980 MJD: 58104.000-58110.000
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 269| -2 0 4 14 -11 -5 -.02 10 10 | -534 -215 10 102
| 0 0 1 14 10 7 .03 | 112 254
emr 79| 0 -1 8 -8 -19 -27 .24 15 15 | 152779 -260 17 141
| 1 1 2 14 6 12 .02 | 512 327
esa 150| 0 0 3 -9 11 0 -.06 10 10 | -1467 -547 7 191
| 0 0 1 6 18 4 .02 | 1747 1503
gfz 188| 0 -1 -2 21 5 -1 .08 11 10 | -323 78 11 142
| 0 0 1 10 12 8 .03 | 359 508
grg 107| 1 0 -4 -18 -6 3 -.39 13 11 | -17 205 12 210
| 0 0 3 14 14 24 .02 | 275 777
igr n/a| 0 0 1 -16 0 -5 -.01 4 4 | -12358 -724 12 74
| 0 0 0 11 10 10 .01 | 1415 313
jpl 80| 0 0 8 2 -6 -2 .26 13 13 | 48381 -71 46 258
| 1 1 1 10 23 17 .04 | 66483 397
mit 350| 0 1 -4 -4 5 -4 .07 10 10 | 34 -127 43 305
| 0 0 1 33 17 10 .01 | 229 214
ngs 204| 0 0 0 -6 5 13 .06 8 7 | -495 -318 849 2145
| 0 0 2 13 22 6 .04 | 98 137
sio 353| 0 -2 -3 0 -4 -4 .01 13 13 | --- --- --- ---
| 0 0 1 13 31 25 .03 | --- ---
Table 1.1980.b GPS week : 1980 MJD: 58104.000-58110.000
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 4 4 3 3 4 5 |
2 | 5 4 4 4 5 4 5 |
3 | 3 4 3 3 3 4 3 |
4 | 0 0 0 0 0 0 0 |
5 | 5 5 5 5 5 4 5 |
6 | 4 4 0 3 4 4 4 |
7 | 4 5 4 4 4 4 4 |
8 | 4 4 4 4 4 4 4 |
9 | 3 4 3 3 3 3 3 |
10 | 4 3 4 3 4 4 3 |
11 | 3 4 4 6 4 5 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 5 4 4 5 5 |
14 | 5 4 4 4 4 5 4 |
15 | 5 5 5 5 5 5 4 |
16 | 6 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 5 5 5 5 5 5 5 |
19 | 5 5 5 5 5 5 4 |
20 | 5 5 4 4 4 5 4 |
21 | 4 5 4 4 4 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 4 5 5 5 |
24 | 5 4 4 4 4 4 4 |
25 | 4 3 3 3 3 4 6 |
26 | 3 3 3 3 4 4 4 |
27 | 4 4 4 4 3 4 3 |
28 | 4 5 4 4 4 5 4 |
29 | 6 5 6 6 6 6 5 |
30 | 4 5 4 4 4 4 4 |
31 | 5 4 4 4 5 5 4 |
32 | 4 3 4 3 3 4 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1980.0 GPS week: 1980 Day: 0 MJD: 58104.000
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 267| -2 0 4 -2 -25 -2 .01 10 10 | -356 -463 11 102
emr 80| 0 -3 4 7 -16 -13 .26 15 15 | 153679 -631 16 155
esa 150| 0 0 3 -12 23 0 -.07 9 10 | 1318 -3594 7 169
gfz 186| -1 -1 -3 22 19 -2 .04 11 11 | 35 -203 13 125
grg 112| 1 0 -2 -12 -3 -28 -.39 13 12 | 96 -176 12 216
igr n/a| 0 0 1 -23 12 0 -.02 4 4 | -10067 -1186 12 72
jpl 80| 0 0 7 -4 23 -1 .25 12 12 | 143181 -546 45 258
mit 350| 1 1 -5 25 -12 -25 .05 12 11 | 230 -420 42 306
ngs 213| 1 1 0 -14 21 19 .10 8 7 | -319 -499 632 2028
sio 355| 1 -2 -3 4 -28 30 -.00 13 13 | --- --- --- ---
Table 2.1980.1 GPS week: 1980 Day: 1 MJD: 58105.000
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 269| -3 1 6 7 3 -15 -.06 11 11 | -427 -415 13 93
emr 80| 0 -2 7 -23 -14 -42 .28 16 16 | 153077 288 18 142
esa 150| 0 0 1 -13 45 2 -.02 10 10 | -3208 206 8 173
gfz 188| 0 -1 0 20 4 -4 .07 10 10 | -456 537 11 125
grg 92| 0 1 -4 -15 16 -13 -.40 12 11 | -69 269 13 213
igr n/a| -1 0 2 -29 4 -13 .00 4 4 | -11226 -297 13 75
jpl 80| -1 0 11 19 26 -25 .23 14 14 | 142605 336 52 254
mit 350| 1 1 -5 18 8 4 .07 11 10 | -68 72 43 299
ngs 203| 0 0 0 -4 -41 5 .09 8 7 | -500 -419 729 1836
sio 356| 0 -2 -1 7 -16 24 .07 13 12 | --- --- --- ---
Table 2.1980.2 GPS week: 1980 Day: 2 MJD: 58106.000
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 271| -2 0 3 10 -4 3 -.06 10 9 | -540 -298 10 114
emr 80| 0 -2 5 9 -9 -17 .25 15 15 | 152954 -545 18 123
esa 150| 0 0 1 1 1 -7 -.03 9 9 | -3382 501 7 200
gfz 186| -1 -2 -4 35 13 -17 .13 11 11 | -841 605 12 202
grg 110| 0 1 0 -1 -30 -10 -.40 12 11 | 68 -90 13 215
igr n/a| 0 0 1 -2 -4 -15 -.02 4 4 | -11766 -1079 13 74
jpl 80| 0 0 7 13 -14 -1 .31 13 14 | 1998 -575 46 269
mit 350| 0 1 -6 -31 9 0 .06 10 9 | 86 -132 43 300
ngs 203| 0 0 2 -1 1 17 .09 8 8 | -525 -317 890 2224
sio 352| 0 -3 -1 -22 14 5 .02 13 13 | --- --- --- ---
Table 2.1980.3 GPS week: 1980 Day: 3 MJD: 58107.000
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 270| -3 0 4 10 -21 -3 -.01 10 10 | -593 -39 11 104
emr 80| 1 -2 7 -8 -28 -18 .22 15 15 | 152530 -308 20 146
esa 150| 0 1 4 -3 17 -2 -.08 10 10 | -2808 -32 9 194
gfz 188| -1 -2 -1 15 -3 1 .07 11 10 | -11 -780 10 135
grg 109| 2 0 -11 -23 -11 0 -.40 13 10 | 137 -327 13 189
igr n/a| 0 0 0 -21 -19 1 -.02 4 4 | -12706 -603 11 70
jpl 80| 0 -1 7 -2 -11 -8 .21 12 12 | 45321 228 42 248
mit 350| 0 0 -4 2 17 4 .07 10 9 | -279 -195 40 314
ngs 199| 0 0 1 -10 17 7 .06 7 7 | -602 -54 715 2148
sio 355| 0 -2 -1 6 -3 -14 -.01 13 13 | --- --- --- ---
Table 2.1980.4 GPS week: 1980 Day: 4 MJD: 58108.000
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 271| -1 1 3 11 -8 -2 .00 10 10 | -611 -234 10 108
emr 80| 0 0 11 0 -21 -30 .24 16 16 | 152596 -476 16 136
esa 150| 0 0 1 -13 6 3 -.05 10 10 | -1176 555 7 205
gfz 189| 0 -2 -1 11 -9 4 .10 10 9 | -715 507 11 161
grg 110| 1 0 -5 -9 0 9 -.37 12 10 | -601 1844 12 207
igr n/a| 0 0 0 -3 -2 7 .00 4 4 | -12993 -671 12 81
jpl 80| 0 -2 9 6 -36 30 .23 13 13 | 1653 -196 48 258
mit 350| 0 1 -1 2 20 -9 .08 10 9 | 49 83 48 283
ngs 205| 0 0 -1 -3 2 14 .07 8 7 | -575 -319 883 2242
sio 354| 0 -3 -3 -16 9 -13 .01 13 14 | --- --- --- ---
Table 2.1980.5 GPS week: 1980 Day: 5 MJD: 58109.000
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 271| -1 0 3 42 -15 -1 -.01 10 10 | -526 -330 10 97
emr 80| 0 0 11 -23 -22 -44 .24 15 15 | 152075 -18 16 150
esa 150| 0 0 5 -15 -7 2 -.05 10 10 | -782 -1 8 211
gfz 189| 0 -1 0 10 21 8 .07 10 10 | -289 61 11 126
grg 109| 1 0 -6 -48 -4 31 -.41 14 12 | 242 -427 13 222
igr n/a| 0 0 1 -26 0 1 .02 4 4 | -13903 -496 12 70
jpl 80| 0 0 10 -3 -23 1 .31 13 13 | 1433 373 45 271
mit 350| 0 0 -2 20 15 -6 .09 10 9 | 390 -376 45 338
ngs 203| 0 0 -4 -28 28 7 .03 9 8 | -536 -305 1122 2229
sio 353| 0 -1 -5 8 -49 -27 -.01 15 14 | --- --- --- ---
Table 2.1980.6 GPS week: 1980 Day: 6 MJD: 58110.000
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 270| -1 0 3 19 -7 -17 .00 10 9 | -687 272 10 101
emr 79| 2 0 7 -22 -23 -25 .22 15 15 | 152545 -132 17 139
esa 150| 1 0 3 -6 -5 2 -.08 10 10 | -233 -1465 8 191
gfz 190| 0 0 -2 36 -6 -3 .07 11 10 | 10 -175 12 125
grg 112| 1 0 0 -21 -12 39 -.34 14 13 | 8 348 12 211
igr n/a| 0 0 1 -9 11 -18 -.00 4 4 | -13849 -742 12 76
jpl 80| 2 2 7 -8 -11 -13 .26 13 13 | 2479 -119 46 251
mit 350| 0 1 -3 -65 -25 0 .09 11 10 | -168 75 41 300
ngs 205| -1 0 -2 14 11 21 -.00 8 7 | -414 -318 972 2314
sio 351| 0 -1 -5 7 45 -35 -.03 12 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 3.1980.0 GPS week: 1980 Day: 0 MJD: 58104.000
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 14 7 10 10 4 13 6 6 12 3 | 32 35 34 29 30 29 36 34 35 40 33
2 | 14 17 7 11 13 3 14 14 8 13 4 | 29 29 27 32 32 28 28 29 30 32 28
3 | 4 11 11 10 7 5 11 6 5 10 3 | 32 40 33 31 27 33 40 34 38 37 33
X4 | 3 --- --- --- --- 36 --- --- --- --- 0 | 51 --- --- --- --- 41 --- --- --- --- 50
5 | 8 11 14 12 12 4 11 16 11 15 4 | 45 49 47 42 46 43 49 40 41 44 42
6 | 7 11 6 8 10 3 10 10 8 11 3 | 23 27 23 23 23 23 26 25 25 32 25
7E | 4 18 7 11 13 2 15 9 7 9 3 | 56 56 59 60 58 58 53 61 60 61 58
8 | 8 15 6 6 15 5 12 14 6 10 3 | 28 28 25 26 28 25 28 30 27 26 26
9 | 8 9 11 8 10 3 9 9 5 7 3 | 31 36 35 32 26 33 37 36 36 35 32
10 | 8 14 11 8 10 3 11 9 5 9 3 | 31 38 28 32 27 30 38 33 32 34 30
11E | 8 10 8 9 7 3 11 8 5 9 3 | 73 74 72 71 75 70 74 73 71 73 72
12 | 14 23 7 15 13 6 14 14 9 14 5 | 39 40 36 41 33 38 39 39 43 37 37
13 | 7 17 13 13 12 3 15 12 8 11 4 | 41 48 42 48 38 44 46 44 45 43 42
14 | 10 12 10 15 12 3 7 14 10 13 4 | 34 36 30 43 31 36 34 43 42 42 36
15 | 10 19 11 13 15 5 14 14 10 18 5 | 51 59 53 43 51 46 59 42 45 47 47
16 | 16 21 8 15 17 5 16 13 11 23 5 | 38 34 34 42 33 38 35 44 43 38 37
17 | 9 18 6 11 11 5 12 13 9 9 4 | 33 36 32 38 30 34 35 36 38 37 34
18 | 12 19 10 12 9 4 13 11 10 18 4 | 31 32 29 41 30 35 33 42 40 42 34
19 | 11 24 6 9 13 5 12 16 8 10 4 | 30 33 30 28 32 28 29 29 30 28 29
20 | 9 12 12 13 12 4 10 12 10 15 4 | 29 27 28 39 24 31 27 37 34 38 30
21 | 14 11 6 11 12 5 12 10 8 10 4 | 27 25 27 29 22 26 27 28 28 28 25
22 | 6 12 10 12 10 4 13 12 9 14 4 | 27 31 24 31 24 29 29 36 34 33 28
23 | 8 21 13 13 9 5 16 13 9 19 5 | 37 33 32 43 33 39 32 45 44 39 37
24E | 13 9 12 10 19 5 9 12 6 8 4 | 35 34 39 35 38 36 37 37 39 37 36
X25 | 9 15 5 8 8 3 13 10 6 --- 3 | 31 33 31 30 27 29 33 30 29 --- 29
26 | 9 12 5 8 13 3 10 6 5 8 3 | 39 41 37 37 34 35 39 38 40 37 37
27 | 6 12 7 6 14 4 13 9 6 14 3 | 30 30 28 29 27 27 29 29 30 27 28
28 | 7 15 9 12 14 3 11 16 8 11 4 | 38 39 40 40 36 39 39 38 42 39 38
X29 | 17 25 6 15 14 6 19 15 11 --- 6 | 29 28 25 32 24 26 27 29 29 --- 26
30E | 11 9 10 8 20 4 13 10 10 10 4 | 32 32 34 26 28 26 27 28 26 29 28
31E | 16 12 5 10 18 3 6 11 8 8 4 | 67 63 63 65 58 64 65 65 67 65 64
32 | 5 9 10 12 9 5 9 10 7 15 3 | 34 39 34 31 30 31 38 33 34 40 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 9 11 13 4 12 12 8 13 |T 36 38 35 37 34 35 37 38 38 39 36
WRMS | 10 15 10 11 11 4 12 11 7 13 |NE 35 36 34 36 31 34 36 36 37 36 34
MEDI | 8 14 8 11 12 4 12 12 8 11 |MD 32 35 33 35 30 33 35 36 38 37 33
Table 3.1980.1 GPS week: 1980 Day: 1 MJD: 58105.000
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 13 7 8 11 4 13 6 7 16 3 | 29 33 30 24 23 25 30 28 26 40 28
2 | 15 20 6 9 10 4 15 13 9 12 4 | 31 33 29 32 30 29 33 30 26 33 29
3 | 6 12 12 9 9 5 12 6 8 9 3 | 19 31 23 16 16 21 31 22 28 28 21
X4 | 4 --- --- --- --- 18 --- --- --- --- 0 | 31 --- --- --- --- 26 --- --- --- --- 31
5 | 12 10 13 13 12 5 13 17 12 17 5 | 33 36 32 32 32 31 39 31 34 39 31
6 | 11 13 9 8 8 4 11 10 7 10 3 | 21 26 24 22 23 21 27 23 24 31 22
7E | 15 19 9 10 21 4 16 9 10 9 5 | 29 31 31 37 29 32 33 37 36 33 32
8 | 8 14 7 8 10 7 16 11 9 11 3 | 20 26 19 19 18 20 26 23 20 25 19
9 | 16 10 13 6 8 5 9 6 7 6 3 | 21 28 20 17 15 19 27 21 21 19 18
10M | 7 10 11 6 8 3 10 8 5 11 3 | 18 29 19 20 17 19 29 20 22 23 19
11E | 6 14 9 7 13 4 11 10 6 12 3 | 56 58 57 59 59 58 60 58 58 60 57
12 | 15 23 9 15 11 5 16 14 8 13 5 | 25 27 23 27 20 26 26 27 28 25 24
13 | 9 16 15 12 10 3 17 10 9 13 4 | 20 29 18 26 22 22 27 24 25 25 22
14M | 11 9 11 13 11 3 7 14 8 13 4 | 24 23 25 31 24 25 27 25 28 27 24
15 | 9 18 14 9 10 4 16 12 11 22 5 | 33 41 37 30 32 31 41 28 31 35 31
16 | 12 21 10 11 10 5 16 11 8 24 5 | 22 18 17 24 15 21 17 24 24 23 18
17 | 12 15 7 11 13 4 12 12 9 11 4 | 21 25 23 29 19 24 23 26 27 26 23
18M | 14 21 13 11 8 5 17 11 10 17 4 | 29 29 29 33 25 29 32 32 34 32 28
19 | 11 25 6 12 17 5 13 16 8 12 5 | 20 26 20 19 24 18 21 21 20 19 19
20 | 11 14 11 12 10 3 15 12 9 15 4 | 14 17 18 27 13 19 19 26 22 31 20
21 | 20 15 7 11 11 6 14 9 9 11 4 | 29 19 19 21 17 17 22 18 17 16 17
22 | 7 12 11 11 9 4 12 8 9 16 4 | 21 25 20 18 18 19 25 24 24 24 20
23 | 8 21 15 11 8 4 14 12 8 15 4 | 26 21 20 28 24 24 23 29 27 24 24
24E | 12 10 13 8 15 5 11 10 6 10 4 | 30 26 34 30 29 31 31 29 29 33 29
25 | 10 14 8 6 7 3 19 7 7 11 3 | 20 24 23 23 19 21 25 21 22 24 20
26 | 6 12 5 10 11 3 11 8 5 8 3 | 23 28 20 22 14 21 24 23 24 23 21
27 | 5 13 8 8 8 4 15 8 7 14 3 | 23 26 21 22 16 19 22 22 20 27 20
28 | 9 16 12 13 11 4 12 13 8 15 4 | 16 24 21 27 18 21 23 22 26 26 21
29 | 14 30 7 10 12 5 22 13 12 14 5 | 24 22 21 23 20 21 22 23 20 30 20
30E | 13 11 12 9 24 5 12 8 9 11 4 | 23 28 29 19 23 22 25 23 24 25 22
31E | 14 12 6 8 15 3 7 9 6 8 3 | 39 38 38 39 31 38 38 39 36 41 37
32M | 9 9 11 9 8 2 8 8 5 10 3 | 17 24 17 13 16 17 25 18 20 24 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 10 10 12 4 14 11 8 13 |T 25 28 25 26 22 24 28 26 26 28 24
WRMS | 11 16 10 10 11 4 14 10 7 12 |NE 22 26 22 23 19 22 25 24 24 26 22
MEDI | 11 14 10 10 10 4 13 10 8 12 |MD 23 26 23 24 20 21 26 24 25 26 22
Table 3.1980.2 GPS week: 1980 Day: 2 MJD: 58106.000
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 11 7 11 11 4 11 8 9 11 3 | 25 32 29 26 26 27 31 27 26 36 27
2 | 12 14 6 10 13 2 17 12 8 13 4 | 33 33 29 28 27 28 31 28 29 26 28
3 | 7 11 11 9 9 3 9 6 4 6 3 | 25 34 27 28 21 27 35 29 31 30 27
X4 | 2 --- --- --- --- 18 --- --- --- --- 0 | 27 --- --- --- --- 30 --- --- --- --- 28
5 | 8 12 11 13 11 5 14 14 10 19 4 | 33 37 34 34 34 33 40 32 33 41 33
X6 | 2 --- --- --- --- 16 --- --- --- --- 0 | 36 --- --- --- --- 32 --- --- --- --- 38
7E | 10 18 7 10 13 5 17 8 10 9 4 | 36 35 37 39 38 36 35 40 41 39 37
8 | 8 14 5 8 12 4 14 10 8 12 3 | 23 28 24 25 21 23 27 24 25 27 23
9 | 6 9 11 8 9 3 7 6 7 11 3 | 23 33 27 25 23 26 32 31 29 30 26
10 | 5 11 10 9 13 3 9 7 5 10 3 | 18 29 19 20 26 20 28 22 24 26 21
11E | 9 13 8 9 15 4 13 10 8 8 3 | 57 55 55 57 54 56 58 57 52 56 55
12 | 11 24 9 14 13 5 18 11 9 14 4 | 33 32 26 33 23 28 30 31 31 30 28
13 | 8 16 12 14 13 4 15 14 7 15 4 | 20 32 21 32 19 25 29 28 26 29 24
14 | 9 8 11 14 7 4 8 13 8 12 4 | 20 23 20 34 21 23 23 28 25 29 23
15 | 10 19 11 14 9 4 15 13 9 21 5 | 46 54 48 43 46 44 52 40 44 47 44
16 | 13 24 8 12 11 5 13 11 8 23 5 | 22 22 21 24 24 21 23 24 23 22 20
17 | 7 14 6 15 18 2 12 9 9 10 4 | 24 27 24 31 19 25 26 26 30 24 24
18 | 12 20 10 13 7 3 15 10 9 17 4 | 27 30 27 33 29 28 29 33 31 34 28
19 | 9 25 7 14 17 5 16 12 10 13 5 | 22 26 23 25 22 21 24 24 25 22 22
20 | 7 13 12 13 8 4 14 11 8 15 4 | 25 27 25 36 25 28 24 33 27 36 27
21 | 14 11 4 10 11 3 13 9 9 12 4 | 25 23 22 22 18 20 26 20 22 19 19
22 | 8 10 10 13 8 3 7 10 8 15 4 | 26 27 25 29 23 27 28 31 28 28 26
23 | 8 21 12 13 10 4 15 10 9 20 4 | 29 26 27 38 30 32 30 37 34 32 31
24E | 13 9 12 8 17 6 14 9 6 8 4 | 30 29 33 31 28 29 31 30 30 33 29
25 | 8 13 8 9 6 5 14 7 6 11 3 | 29 28 27 28 23 27 28 27 28 22 26
26 | 7 10 4 9 7 3 13 6 8 8 2 | 21 26 23 25 22 24 28 25 25 24 23
27 | 6 15 7 7 7 4 13 7 11 13 3 | 22 27 23 23 22 21 24 23 22 26 21
28 | 7 16 11 14 11 3 10 10 9 11 4 | 18 26 24 29 19 22 25 25 25 22 22
29 | 18 28 7 13 17 5 23 12 10 17 5 | 26 22 21 26 18 21 20 25 27 27 22
30E | 12 9 8 9 18 5 11 6 6 12 4 | 32 31 33 27 23 27 32 29 27 30 28
31E | 10 10 5 9 17 4 9 7 5 8 3 | 32 33 32 35 31 34 35 35 35 36 32
32 | 8 8 10 11 9 2 7 9 7 13 3 | 22 27 22 20 19 21 28 21 24 29 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 9 11 12 4 13 10 8 13 |T 27 30 27 30 25 27 30 29 29 30 27
WRMS | 9 15 9 11 11 4 14 9 8 13 |NE 26 29 26 29 24 26 29 28 28 28 26
MEDI | 8 13 8 11 11 4 13 10 8 12 |MD 25 28 25 28 23 27 28 28 27 29 26
Table 3.1980.3 GPS week: 1980 Day: 3 MJD: 58107.000
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 12 8 7 11 3 11 6 5 11 3 | 24 28 27 23 24 23 29 26 25 32 25
2 | 11 14 8 9 9 3 15 10 7 12 3 | 44 41 40 41 43 41 41 42 40 39 40
3 | 7 11 10 9 5 6 10 7 6 8 3 | 23 34 23 22 23 26 33 25 29 27 25
X4 | 3 --- --- --- --- 21 --- --- --- --- 0 | 27 --- --- --- --- 24 --- --- --- --- 26
5 | 10 12 14 11 11 4 11 16 10 21 5 | 34 41 38 32 31 32 42 34 35 40 34
6 | 7 11 7 12 10 5 10 8 5 11 3 | 26 29 28 27 26 25 28 26 26 31 25
7E | 7 15 6 9 16 4 16 6 5 9 3 | 35 31 31 36 37 32 30 34 35 31 33
8 | 9 20 6 7 10 3 12 11 8 13 4 | 24 25 21 23 25 21 24 24 21 25 21
9 | 7 10 12 8 9 3 11 5 5 8 3 | 21 31 23 19 20 21 31 24 25 22 22
10 | 8 9 12 7 9 2 8 8 5 7 3 | 21 30 19 25 26 22 28 26 24 27 23
11E | 8 16 13 8 36 7 11 12 7 11 5 | 85 83 84 83 102 83 86 84 85 84 85
12 | 10 22 8 12 14 3 16 11 7 13 4 | 30 31 24 29 25 26 29 27 27 25 26
13 | 9 14 14 12 12 3 15 11 8 13 4 | 23 32 21 34 28 28 31 35 29 33 28
14 | 9 10 11 15 10 4 7 12 8 12 4 | 24 26 20 34 24 27 25 31 29 30 26
15 | 10 18 12 12 9 3 15 11 7 21 4 | 42 47 42 34 36 35 47 33 35 39 37
16 | 15 23 9 12 12 5 15 12 9 23 5 | 24 20 18 21 18 20 21 21 22 21 18
17 | 13 12 7 14 16 4 10 10 7 10 4 | 22 27 20 28 22 23 28 25 26 22 23
18 | 13 19 12 13 9 3 14 10 9 18 4 | 24 25 24 33 26 26 25 32 30 33 26
19 | 14 20 6 14 16 5 13 13 7 11 4 | 23 23 20 24 22 21 24 21 21 18 20
20 | 7 11 13 14 10 4 11 11 7 13 4 | 24 23 20 37 23 26 24 33 28 33 27
21 | 12 10 7 12 14 3 10 8 7 10 3 | 21 20 20 23 27 18 22 21 22 19 20
22 | 10 11 12 11 9 3 10 9 8 18 4 | 24 24 19 23 21 21 23 28 26 25 22
23 | 8 19 13 10 7 3 15 10 7 16 4 | 25 22 21 30 29 28 24 33 30 26 26
24E | 10 10 12 6 12 4 7 9 5 10 3 | 34 27 38 33 34 34 35 33 33 35 33
25 | 7 10 7 8 6 3 12 7 4 12 3 | 26 26 24 27 23 23 28 24 23 26 24
26 | 8 12 7 8 11 2 14 8 8 10 3 | 24 26 23 23 24 23 26 24 26 25 23
27 | 10 13 7 7 10 3 14 9 6 11 3 | 23 24 21 23 19 19 22 22 21 23 20
28 | 7 13 10 13 12 4 8 11 7 10 3 | 22 26 23 28 22 23 26 22 24 21 22
29 | 14 28 7 12 13 5 20 13 11 19 5 | 21 17 18 21 19 19 18 21 23 25 19
30E | 9 12 11 9 16 4 10 7 7 10 3 | 28 30 29 23 26 24 28 24 24 24 24
31E | 13 11 8 9 14 5 10 8 5 9 3 | 37 36 34 39 41 35 38 35 35 37 35
32 | 7 9 11 11 7 3 8 8 5 12 3 | 19 27 18 15 19 17 26 20 19 25 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 10 11 13 4 12 10 7 13 |T 28 30 26 29 28 27 30 29 28 29 27
WRMS | 10 15 10 10 10 4 12 9 7 13 |NE 25 27 23 26 23 24 27 26 26 26 24
MEDI | 9 12 10 11 11 3 11 10 7 11 |MD 24 27 23 27 25 24 28 26 26 26 25
Table 3.1980.4 GPS week: 1980 Day: 4 MJD: 58108.000
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 11 7 6 10 4 11 8 5 10 3 | 25 25 26 24 21 23 26 25 23 32 24
2E | 12 18 10 10 14 7 17 10 8 15 4 | 52 50 49 57 52 49 51 49 53 59 52
3 | 6 10 11 9 9 4 10 8 7 7 3 | 22 31 23 20 18 22 31 23 27 27 22
X4 | 2 --- --- --- --- 22 --- --- --- --- 0 | 31 --- --- --- --- 20 --- --- --- --- 31
5 | 8 13 14 12 8 4 14 14 9 17 4 | 34 35 29 28 28 28 36 32 31 34 30
6 | 9 11 7 10 14 4 9 7 6 9 3 | 24 25 23 22 19 20 25 22 22 26 22
7E | 9 19 8 9 15 5 17 7 7 10 3 | 28 25 29 34 28 30 27 32 35 31 30
8 | 11 13 6 5 9 4 12 10 7 12 3 | 22 21 20 20 16 19 23 21 20 23 19
9 | 4 9 11 7 8 3 9 5 5 8 2 | 19 28 21 19 16 21 28 23 22 23 20
10 | 7 10 12 7 7 3 11 10 7 10 3 | 27 33 26 30 25 29 34 32 31 32 28
11E | 10 19 8 9 9 3 11 12 6 8 4 | 57 57 53 57 53 55 57 59 55 58 55
12 | 14 22 8 11 14 4 15 11 9 12 4 | 26 26 22 26 22 25 26 26 27 26 24
13 | 7 15 14 12 11 4 16 12 8 13 4 | 26 30 25 33 26 28 29 32 31 31 28
14 | 11 10 11 15 7 5 9 13 9 12 4 | 16 20 16 35 19 24 21 26 27 26 22
15 | 8 17 12 11 8 3 17 12 7 20 4 | 40 48 40 35 36 35 47 34 33 40 36
16 | 14 22 9 11 13 4 14 12 10 23 5 | 21 17 16 20 15 17 18 20 20 20 15
17 | 6 15 9 12 17 2 11 10 8 10 4 | 22 23 23 29 20 24 25 27 27 26 23
18 | 12 23 11 11 10 4 14 13 11 19 5 | 26 26 24 32 24 28 25 34 33 36 28
19 | 9 21 7 11 18 3 14 13 7 10 4 | 20 21 20 20 22 18 22 19 20 17 18
20 | 9 12 14 11 10 4 11 10 8 14 4 | 24 22 21 32 20 24 22 31 29 34 25
21 | 16 10 6 11 12 3 10 9 10 9 4 | 23 19 19 21 19 19 20 19 17 15 17
22 | 8 9 12 10 10 5 8 9 8 16 4 | 22 22 20 24 18 23 23 27 24 26 22
23 | 9 23 12 10 10 4 17 10 9 17 4 | 24 21 20 29 27 27 22 31 30 26 25
24E | 7 16 11 5 11 4 10 8 6 10 3 | 26 27 29 26 25 26 28 26 27 30 26
25 | 9 13 7 7 8 2 12 7 5 12 3 | 19 27 21 22 18 19 24 20 19 21 19
26 | 13 11 6 9 10 3 12 9 8 9 3 | 21 24 19 20 16 18 23 21 20 21 19
27 | 9 13 7 6 11 4 13 8 6 11 3 | 21 21 19 19 14 17 19 20 18 21 18
28 | 7 15 12 16 10 4 11 9 8 11 4 | 17 21 21 27 16 18 20 20 19 18 18
29 | 15 28 10 13 16 4 22 12 10 14 5 | 20 19 18 21 19 17 19 21 21 23 18
30E | 13 11 10 7 21 5 10 5 7 11 4 | 25 21 26 19 21 20 23 21 22 19 20
31E | 14 13 9 9 20 5 9 10 8 14 4 | 36 35 33 37 33 35 37 37 38 40 35
32 | 6 10 11 9 5 3 11 8 5 12 3 | 15 24 15 13 10 15 24 17 18 23 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 10 10 12 4 13 10 8 13 |T 25 27 24 27 23 24 27 27 27 28 25
WRMS | 10 16 10 9 10 4 13 9 7 14 |NE 23 25 22 24 20 22 25 24 24 25 22
MEDI | 9 13 10 10 10 4 11 10 8 12 |MD 24 25 22 26 20 23 25 26 27 26 22
Table 3.1980.5 GPS week: 1980 Day: 5 MJD: 58109.000
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 15 7 9 16 4 10 6 5 16 3 | 25 32 27 26 29 25 32 26 26 35 26
2E | 8 17 8 8 16 4 15 9 8 15 4 | 50 47 48 49 52 48 52 50 47 49 48
3 | 10 9 12 8 9 3 9 8 4 12 3 | 24 31 23 24 21 24 32 24 24 30 23
X4 | 3 --- --- --- --- 16 --- --- --- --- 0 | 26 --- --- --- --- 27 --- --- --- --- 26
5 | 10 11 13 9 7 4 13 12 10 18 4 | 27 30 26 27 22 24 32 31 25 33 26
6 | 9 10 7 7 11 3 10 10 7 10 3 | 27 28 27 25 20 26 27 28 26 30 26
7E | 9 15 8 9 15 4 17 7 8 13 4 | 27 24 26 33 24 27 24 30 32 28 27
8 | 6 14 7 6 13 3 13 10 10 14 3 | 24 25 22 24 21 22 26 26 21 29 22
9 | 7 9 12 7 10 3 8 6 7 8 3 | 24 30 23 23 24 24 33 26 25 24 23
10 | 7 12 14 6 8 3 9 7 8 13 3 | 30 37 26 29 27 28 33 30 29 33 29
11E | 7 15 11 8 19 5 13 14 10 13 4 | 115 114 115 116 120 115 119 119 113 118 115
12 | 15 21 8 14 15 4 16 13 10 15 5 | 27 26 23 30 23 26 30 29 27 29 25
13 | 7 15 14 12 10 2 15 11 9 14 4 | 22 29 19 29 21 23 27 28 25 29 23
14 | 11 11 11 14 9 3 9 13 10 16 4 | 17 20 15 30 18 21 20 24 27 27 20
15 | 8 17 11 11 11 4 14 11 9 20 4 | 45 50 47 41 43 42 53 44 42 42 43
16 | 10 26 9 10 12 3 17 12 11 22 5 | 21 20 17 21 16 19 19 24 21 24 18
17 | 9 11 8 14 17 3 12 9 7 11 4 | 21 24 22 31 19 24 27 25 26 24 23
18 | 12 20 11 12 12 3 14 11 12 17 5 | 29 31 30 34 31 32 32 36 35 39 31
19 | 10 20 7 14 17 4 16 12 7 13 4 | 23 22 22 24 21 20 24 22 24 20 21
20 | 12 11 13 13 9 5 12 10 11 15 4 | 33 32 32 40 35 35 38 39 40 42 35
21E | 7 11 7 8 19 4 11 6 10 9 3 | 25 22 25 26 29 24 27 23 22 22 23
22 | 8 10 12 10 9 3 10 9 9 20 4 | 24 25 23 26 25 24 28 29 24 30 24
23 | 10 23 13 11 13 4 16 15 10 17 5 | 31 27 26 35 30 31 29 38 33 31 30
24E | 10 12 11 8 15 5 9 7 7 9 3 | 46 37 48 47 45 47 45 46 48 47 46
25 | 10 15 8 8 10 4 12 9 8 16 4 | 33 32 31 30 26 30 35 29 30 35 29
26 | 9 11 8 7 16 2 12 7 10 10 3 | 21 26 21 18 20 20 25 22 19 24 19
27 | 7 15 9 8 11 5 13 10 10 13 3 | 23 25 22 21 18 19 23 26 19 25 20
28 | 7 13 11 14 15 4 11 11 9 14 4 | 19 21 21 26 19 19 24 20 22 17 18
29 | 19 27 8 13 17 6 19 12 14 17 6 | 26 20 21 25 22 22 25 24 26 28 22
30E | 10 13 10 6 17 4 8 6 8 13 4 | 28 24 27 24 24 24 28 25 28 25 24
31E | 14 11 6 11 18 3 12 11 9 13 4 | 33 37 32 35 31 33 34 35 35 38 33
32 | 9 10 13 6 8 3 8 5 7 12 3 | 15 23 16 14 14 16 25 17 18 20 15
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 10 10 14 4 13 10 9 15 |T 30 31 29 31 28 29 33 32 30 33 29
WRMS | 10 15 10 10 12 4 13 9 8 14 |NE 26 27 24 27 23 25 29 28 26 28 24
MEDI | 9 13 10 9 13 4 12 10 9 14 |MD 26 27 25 27 24 24 28 28 26 29 24
Table 3.1980.6 GPS week: 1980 Day: 6 MJD: 58110.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 9 16 9 10 21 5 11 21 7 10 4 | 31 35 36 31 34 32 33 32 33 37 31
2E | 17 11 9 8 21 4 14 15 9 11 5 | 33 30 29 29 36 29 29 32 28 29 29
3 | 7 9 11 6 8 3 10 8 5 8 3 | 23 30 23 23 23 23 31 26 24 29 24
X4 | 2 --- --- --- --- 18 --- --- --- --- 0 | 26 --- --- --- --- 25 --- --- --- --- 26
5 | 10 12 13 11 11 5 14 12 11 17 4 | 42 45 43 35 38 36 50 37 37 39 38
6E | 11 11 10 6 14 4 10 7 7 7 3 | 28 26 27 25 29 26 25 25 25 28 27
7E | 7 14 8 9 15 5 16 7 8 10 3 | 34 32 34 39 32 37 31 40 42 40 36
8 | 9 12 7 6 16 2 12 12 8 11 3 | 25 22 22 23 25 22 24 22 22 24 21
9 | 5 10 11 6 9 2 10 9 4 7 3 | 23 30 23 22 22 22 30 25 22 25 22
10 | 5 11 13 4 9 3 8 9 5 9 3 | 33 35 29 32 27 31 35 32 29 34 30
11E | 8 18 8 10 13 4 11 15 8 10 4 | 112 115 114 114 116 113 113 115 113 115 114
12 | 17 21 9 14 15 4 17 13 9 13 5 | 31 30 27 31 27 28 30 29 31 29 28
13 | 9 18 12 10 14 2 16 11 8 14 4 | 29 37 27 37 28 32 36 37 36 35 32
14 | 6 9 12 15 12 4 11 11 7 13 4 | 25 26 21 39 25 30 25 34 33 31 28
15 | 9 15 11 12 10 4 13 11 7 17 4 | 56 60 56 45 51 47 60 47 46 47 50
16 | 14 22 7 11 17 5 13 12 9 18 5 | 19 19 17 22 21 20 17 25 24 22 18
17 | 6 12 9 13 14 4 10 9 7 8 3 | 23 27 20 29 20 23 25 25 26 23 23
18 | 11 20 13 12 10 4 16 12 9 15 4 | 24 24 22 32 25 26 23 35 30 34 26
19 | 10 21 7 13 14 5 14 12 7 11 4 | 22 25 21 21 23 19 22 21 21 18 20
20 | 8 10 14 13 10 4 11 10 7 15 4 | 31 31 30 41 35 35 33 42 36 43 35
21E | 11 10 7 8 19 3 10 7 7 7 3 | 25 25 27 24 30 25 28 26 26 26 25
22 | 6 11 12 9 10 4 19 11 9 16 4 | 27 26 22 31 24 28 34 34 30 30 27
23 | 8 22 10 10 9 4 15 14 9 16 4 | 30 25 26 38 28 33 27 39 35 32 31
X24 | 10 --- 10 8 15 8 11 11 7 11 4 | 44 --- 47 46 40 42 45 38 44 45 43
25 | 11 14 8 31 13 6 11 11 7 10 5 | 30 31 31 37 27 29 33 27 29 24 28
26 | 10 12 8 6 17 5 14 9 8 8 3 | 21 24 22 18 25 19 25 23 22 22 21
27 | 6 12 7 5 10 3 11 9 8 13 3 | 22 20 20 19 20 18 20 22 19 23 19
28 | 9 13 11 13 15 4 11 11 9 11 4 | 20 23 22 25 19 19 22 21 23 20 20
29 | 16 27 7 13 13 5 22 11 10 16 5 | 24 21 19 20 18 19 20 21 20 24 19
30E | 9 10 9 7 21 4 11 6 5 7 3 | 29 26 30 24 27 25 28 25 27 25 26
31E | 14 14 5 8 13 4 10 7 6 12 3 | 44 46 43 47 45 45 46 47 47 48 45
32 | 5 13 11 7 6 2 10 7 4 9 3 | 17 25 17 15 12 16 25 19 17 21 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 10 11 14 4 13 11 8 12 |T 31 32 30 32 30 30 33 33 32 32 30
WRMS | 9 15 10 10 13 4 13 10 7 12 |NE 27 29 26 28 26 26 29 29 27 28 26
MEDI | 9 12 9 10 13 4 11 11 7 11 |MD 27 26 27 31 27 26 29 29 29 29 27
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 4.1980 GPS week: 1980 MJD: 58104.0-58110.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 |U 8 9 19 |U 11 12 37 |U 12 9 25 |
emr | emr 2934 |U 14 18 37 |U 13 18 45 |U 21 18 45 |
esa | esa 2962 | 8 11 25 |U 11 14 39 | 14 10 26 |
gfz | gfz 2962 |U 8 8 20 |U 11 13 39 |U 10 9 27 |
grg | grg 2960 |U 8 9 27 |U 11 14 38 | 10 10 27 |
igr | igr 2962 | 7 10 20 | 11 13 37 | 12 9 25 |
igs | igs 2962 | 7 10 20 | 11 12 38 | 13 9 25 |
jpl | jpl 2962 | 13 18 34 |U 12 19 43 |U 21 15 40 |
mit | mit 2962 | 9 9 22 |U 12 14 42 |U 15 12 30 |
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 5.1980.0 GPS week: 1980 Day: 0 MJD: 58104.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 11 20 | 9 11 32 | 14 10 29 |
emr | emr 2976 | 16 20 34 | 14 17 36 | 19 19 43 |
esa | esa 2976 | 9 11 22 | 8 14 34 | 14 8 29 |
gfz | gfz 2974 | 8 9 16 | 8 12 34 | 11 6 28 |
grg | grg 2967 | 10 12 17 | 8 12 31 | 12 6 29 |
igr | igr 2976 | 9 11 16 | 8 12 32 | 13 7 27 |
igs | igs 2976 | 9 11 17 | 8 11 32 | 14 8 28 |
jpl | jpl 2976 | 15 19 34 | 11 20 37 | 20 16 41 |
mit | mit 2976 | 10 10 18 | 9 12 37 | 13 9 32 |
Table 5.1980.1 GPS week: 1980 Day: 1 MJD: 58105.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 8 7 20 | 10 11 38 | 12 10 23 |
emr | emr 2976 | 15 16 34 | 13 16 35 | 18 15 44 |
esa | esa 2976 | 6 7 24 | 11 13 36 | 13 8 23 |
gfz | gfz 2976 | 7 5 20 | 11 13 39 | 10 7 25 |
grg | grg 2969 | 7 8 27 | 11 10 34 | 9 10 23 |
igr | igr 2976 | 6 7 19 | 10 12 36 | 12 9 23 |
igs | igs 2976 | 6 7 21 | 10 11 36 | 12 8 22 |
jpl | jpl 2976 | 12 16 30 | 10 19 37 | 17 11 38 |
mit | mit 2976 | 8 6 24 | 11 14 35 | 14 15 35 |
Table 5.1980.2 GPS week: 1980 Day: 2 MJD: 58106.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2971 | 10 13 21 | 9 9 35 | 15 11 25 |
emr | emr 2880 | 17 25 45 | 11 16 44 | 23 18 38 |
esa | esa 2880 | 10 15 26 | 9 12 39 | 17 13 28 |
gfz | gfz 2880 | 11 11 18 | 9 10 35 | 12 9 26 |
grg | grg 2880 | 11 15 34 | 8 11 36 | 11 14 33 |
igr | igr 2880 | 9 13 21 | 8 10 34 | 14 12 26 |
igs | igs 2880 | 9 13 22 | 8 9 37 | 15 11 26 |
jpl | jpl 2880 | 15 24 39 | 9 18 48 | 21 18 39 |
mit | mit 2880 | 10 14 27 | 10 11 39 | 17 17 30 |
Table 5.1980.3 GPS week: 1980 Day: 3 MJD: 58107.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 7 7 19 | 9 11 31 | 10 10 29 |
emr | emr 2976 | 13 16 32 | 13 18 41 | 17 19 46 |
esa | esa 2976 | 7 8 24 | 10 13 32 | 13 11 30 |
gfz | gfz 2976 | 9 9 21 | 9 12 34 | 10 11 30 |
grg | grg 2976 | 7 9 23 | 10 14 30 | 10 16 29 |
igr | igr 2976 | 7 8 20 | 9 12 31 | 10 10 29 |
igs | igs 2976 | 6 8 20 | 10 12 31 | 12 11 29 |
jpl | jpl 2976 | 11 17 29 | 12 18 39 | 19 16 41 |
mit | mit 2976 | 8 6 20 | 11 14 38 | 12 10 32 |
Table 5.1980.4 GPS week: 1980 Day: 4 MJD: 58108.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 | 8 9 22 | 18 11 40 | 11 8 22 |
emr | emr 2976 | 12 16 44 | 19 21 58 | 23 16 53 |
esa | esa 2976 | 8 12 31 | 18 14 42 | 14 9 26 |
gfz | gfz 2976 | 9 9 25 | 17 12 40 | 10 9 27 |
grg | grg 2976 | 10 10 34 | 18 18 45 | 11 10 35 |
igr | igr 2976 | 8 10 26 | 18 12 40 | 11 8 24 |
igs | igs 2976 | 8 10 26 | 18 10 42 | 12 8 26 |
jpl | jpl 2976 | 12 15 44 | 18 18 47 | 22 15 46 |
mit | mit 2976 | 9 10 25 | 19 14 44 | 15 8 25 |
Table 5.1980.5 GPS week: 1980 Day: 5 MJD: 58109.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 7 8 16 | 12 16 51 | 11 8 18 |
emr | emr 2880 | 12 19 39 | 13 17 56 | 23 19 43 |
esa | esa 2976 | 8 10 23 | 12 15 52 | 14 10 22 |
gfz | gfz 2976 | 7 8 20 | 11 15 51 | 10 9 21 |
grg | grg 2976 | 8 7 29 | 11 17 56 | 9 8 23 |
igr | igr 2976 | 6 9 18 | 11 15 49 | 11 9 18 |
igs | igs 2976 | 7 9 19 | 11 14 52 | 12 10 20 |
jpl | jpl 2976 | 12 17 32 | 11 15 52 | 22 12 35 |
mit | mit 2976 | 8 6 21 | 13 15 57 | 12 14 26 |
Table 5.1980.6 GPS week: 1980 Day: 6 MJD: 58110.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 6 8 16 | 11 15 35 | 10 8 27 |
emr | emr 2876 | 13 18 30 | 11 23 44 | 24 20 50 |
esa | esa 2976 | 7 11 23 | 12 20 37 | 14 11 27 |
gfz | gfz 2976 | 6 9 20 | 12 16 37 | 10 10 30 |
grg | grg 2976 | 8 6 25 | 10 13 31 | 8 8 21 |
igr | igr 2976 | 6 10 17 | 11 16 35 | 11 10 27 |
igs | igs 2976 | 6 9 18 | 11 17 35 | 12 10 27 |
jpl | jpl 2976 | 12 18 30 | 14 23 41 | 23 15 41 |
mit | mit 2976 | 8 9 20 | 13 17 43 | 22 11 33 |
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 6.1980 GPS week: 1980 MJD: 58104.500-58110.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 7 9 45 42 -5 | 40 44
| 19 18 92 44 8 | 4
esa uuuuu | -15 7 -91 -27 -1 | 10 19
| 17 5 46 34 5 | 3
gfz uuuuu | -23 -34 33 -246 -1 | 10 20
| 22 19 68 70 2 | 3
grg uuuuu | 23 10 51 92 -2 | 1 17
| 18 7 32 67 3 | 3
igr xxxxx | 8 8 22 19 6 | -6 18
| 13 12 34 31 2 | 4
jpl xxxxx | 24 -43 161 4 4 | 18 26
| 31 25 94 70 9 | 5
mit uuuuu | 19 -14 46 112 4 | 20 27
| 13 23 55 48 3 | 4
ngs uuuuu | -1 -1 81 59 3 | 10 21
| 36 40 61 66 4 | 4
sio uuuux | 1 38 -220 -39 5 | 41 45
| 6 29 80 15 7 | 6
Table 7.1980.0 GPS week: 1980 Day: 0 MJD: 58104.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | -4 -13 150 55 -6 | 35 40
esa uuuuu | -23 8 -21 19 -8 | 7 20
gfz uuuuu | -39 -54 36 -215 0 | 5 18
grg uuuuu | 53 7 23 146 -1 | -3 16
igr xxxxx | -1 27 -25 34 5 | -13 21
jpl xxxxx | -12 -37 212 20 3 | 10 24
mit uuuuu | 18 -34 -68 114 8 | 13 22
ngs uuuuu | 7 34 48 -24 4 | 3 18
sio uuuux | 4 27 -158 -48 -3 | 31 37
Table 7.1980.1 GPS week: 1980 Day: 1 MJD: 58105.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | -26 13 88 -42 5 | 37 44
esa uuuuu | -45 14 -139 -39 -6 | 8 22
gfz uuuuu | -35 -53 141 -229 0 | 8 22
grg uuuuu | 5 5 40 180 -1 | 1 19
igr xxxxx | -2 23 -21 17 3 | -10 23
jpl xxxxx | -18 -77 213 1 6 | 12 27
mit uuuuu | 0 -28 68 166 5 | 17 28
ngs uuuuu | 71 27 -32 -4 3 | 7 22
sio uuuux | -6 24 -130 -25 11 | 34 41
Table 7.1980.2 GPS week: 1980 Day: 2 MJD: 58106.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | -2 -13 -69 34 1 | 43 47
esa uuuuu | -8 10 -60 -49 2 | 13 20
gfz uuuuu | -59 -47 76 -373 1 | 13 21
grg uuuuu | 35 22 80 99 -6 | 5 17
igr xxxxx | -6 4 53 2 4 | -5 17
jpl xxxxx | 21 -54 241 11 14 | 19 26
mit uuuuu | 19 -39 20 63 3 | 23 29
ngs uuuuu | 8 43 101 170 5 | 12 22
sio uuuux | 1 0 -252 -41 15 | 42 45
Table 7.1980.3 GPS week: 1980 Day: 3 MJD: 58107.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 30 10 3 36 1 | 46 49
esa uuuuu | -20 2 -109 18 -1 | 14 20
gfz uuuuu | -11 -18 -50 -311 1 | 14 21
grg uuuuu | 26 14 66 20 -6 | 5 17
igr xxxxx | 30 8 53 -39 6 | -3 17
jpl xxxxx | 47 -71 269 59 3 | 22 28
mit uuuuu | 30 -28 89 156 2 | 24 30
ngs uuuuu | -28 13 89 46 8 | 13 22
sio uuuux | 4 11 -180 -25 6 | 46 48
Table 7.1980.4 GPS week: 1980 Day: 4 MJD: 58108.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 26 19 -61 75 -6 | 43 46
esa uuuuu | -9 6 -97 -50 -1 | 12 19
gfz uuuuu | -2 -15 62 -171 -4 | 12 20
grg uuuuu | -1 0 1 -5 1 | 2 16
igr xxxxx | 14 -7 42 34 11 | -5 17
jpl xxxxx | 63 -23 45 104 -1 | 21 27
mit uuuuu | 35 0 78 152 1 | 22 28
ngs uuuuu | -31 -34 91 40 4 | 12 21
sio uuuux | 12 61 -181 -25 3 | 46 48
Table 7.1980.5 GPS week: 1980 Day: 5 MJD: 58109.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 8 8 152 37 -9 | 39 42
esa uuuuu | 9 -1 -148 -66 -2 | 8 16
gfz uuuuu | -20 -39 10 -212 -2 | 9 19
grg uuuuu | 22 7 89 127 0 | -1 16
igr xxxxx | 20 -1 44 59 6 | -6 18
jpl xxxxx | 51 -22 48 -78 13 | 18 26
mit uuuuu | 24 22 48 80 7 | 19 26
ngs uuuuu | -26 -29 101 107 3 | 9 19
sio uuuux | -4 72 -280 -65 6 | 43 45
Table 7.1980.6 GPS week: 1980 Day: 6 MJD: 58110.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
emr uuuuu | 16 37 50 96 -18 | 40 43
esa uuuuu | -8 7 -60 -25 6 | 9 16
gfz uuuuu | 3 -12 -41 -209 0 | 11 19
grg uuuuu | 21 15 61 76 -1 | 1 15
igr xxxxx | 2 2 9 29 5 | -2 14
jpl xxxxx | 17 -17 102 -91 -13 | 24 28
mit uuuuu | 5 5 85 50 1 | 22 28
ngs uuuuu | -11 -60 168 76 -4 | 12 20
sio uuuux | -5 69 -355 -47 -5 | 46 48
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