[IGSREPORT-25423] Wk 1958 IGS Final Orbits
acc
acc at igs.org
Fri Aug 4 02:34:45 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1958 (Jul 16, 2017 - Jul 22, 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:
igs1958[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1958[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1958[0-6].cls IGS GPS clock combination summary report.
igs19587.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19587.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 | SYOG SYOG
0 | EMR | CHUR FAIR HERS MCM4 WHIT CHUR FAIR HERS MCM4 SFER
0 | EMR | SYOG WHIT YELL
0 | ESA | ABMF BAKE FAA1 MAL2 ABMF FAA1 KELY MAL2
0 | GFZ | ALBH MAL2 ALBH MAL2
0 | GRG | GLSV LHAZ MAC1 MAW1 SYOG TEHN CHTI GLSV KIRU LHAZ
0 | GRG | LPGS MAC1 MAW1 PARC SYOG TEHN
0 | MIT | REUN REUN
1 | COD | BRFT HRAO TIXI BRFT HRAO TIXI
1 | EMR | SYOG CHUR HERS SYOG WHIT
1 | ESA | MAC1 MKEA ABMF MAC1 MKEA
1 | GFZ | 21 ABMF BRFT KOUR MAW1 BRFT KOUR MAW1
1 | GRG | GLSV INVK LHAZ MAL2 MAW1 NAIN SYOG GLSV INVK LHAZ
1 | GRG | MAL2 MAW1 NAIN SYOG
1 | MIT | MKEA
2 | COD | TIXI MAL2 TIXI
2 | EMR | CHUR HERS
2 | ESA | IRKJ AUCK FAA1 IRKJ
2 | GFZ | ABMF IRKJ ABMF IRKJ
2 | GRG | 21 25 32 21 25 ADIS GLSV MAL2 NAIN PIE1 SYOG ADIS
2 | GRG | CHTI GLSV LPGS MAL2 NAIN PIE1 SYOG
2 | MIT | CHUR REUN CHUR REUN
3 | COD | PARC TIXI PARC TIXI
3 | EMR | DRAO MAS1 SFER
3 | ESA | REUN REUN
3 | GFZ | MAL2 DRAO MAL2
3 | GRG | 21 21 GLSV MAL2 SYOG GLSV MAL2 SYOG
3 | MIT | BJFS BJFS
4 | COD | FAA1 HRAO TIXI NAIN PDEL SYOG TIXI
4 | EMR | ALBH MAS1 PRDS SFER SYOG TWTF
4 | ESA | CHTI MAL2 CHTI MAL2
4 | GFZ | PDEL PDEL
4 | GRG | 21 21 GLSV MAL2 SYOG CHTI GLSV MAL2 SYOG TASH
4 | MIT | PDEL PDEL
5 | COD | TIXI TIXI TUVA
5 | EMR | HERS ALBH HERS MAS1 SFER TWTF
5 | ESA | SAVO
5 | GFZ | CHUR FAA1 GMSD GODE INEG CHUR GMSD GODE INEG
5 | GRG | 21 21 FAA1 GLSV KIRU MAW1 PIE1 REUN SYOG ALRT GLSV
5 | GRG | KIRU MAW1 NAIN PIE1 POHN REUN SYOG
5 | MIT | KIRI KIRI
6 | COD | POVE TIXI ABMF HYDE MAL2 TIXI
6 | EMR | ALBH CHUR MAS1 NIST NLIB PRDS SUWN TSKB TWTF WILL
6 | ESA | SAVO SAVO TUVA
6 | GFZ | ABMF AUCK GODE POHN UFPR AUCK GODE NAIN POHN POVE
6 | GFZ | SYOG TRO1 UFPR
6 | GRG | GLSV MAW1 OHI3 SYOG TRO1 FAA1 GLSV MAW1 OHI3 SYOG
6 | GRG | TRO1
6 | JPL | CEDU
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
2 | GRG | 25
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G04 | | | | | 4 | 4 | 4 |
PRN G25 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
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.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .2 .1 .8 4 6 -8 -.48
EMR | 0 | 1.3 -3.8 1.3 6 32 9 -.25
ESA | 0 | -.4 .4 -.7 -22 -2 4 -.49
GFZ | 0 | .6 .2 .7 -2 -21 -8 -.34
GRG | 0 | -1.7 -4.3 19.9 78 -5 73 -.33
JPL | 0 | 10.0 -9.7 -1.7 -20 -50 40 .38
MIT | 0 | -2.5 -5.3 3.3 8 31 -6 -.12
NGS | 0 | -4.3 -2.7 8.5 18 -17 12 -.25
SIO | 0 | -6.3 1.5 -5.5 -9 12 -7 -.18
COD | 1 | -.4 .4 .7 13 14 -4 -.32
EMR | 1 | 1.6 -7.9 -4.3 1 28 30 -.21
ESA | 1 | -.6 .5 -.8 -14 2 2 -.43
GFZ | 1 | .2 .4 .5 3 -14 -13 -.29
GRG | 1 | 6.1 -2.2 .2 86 7 36 -.16
JPL | 1 | 5.6 -6.6 -10.0 -21 -27 38 .32
MIT | 1 | -1.8 -4.6 -2.2 7 28 -4 -.10
NGS | 1 | -5.8 -11.5 6.1 35 -28 -9 -.20
SIO | 1 | -4.8 .5 -14.2 -10 7 -9 -.20
COD | 2 | -.0 .4 .8 11 14 -6 -.37
EMR | 2 | -2.0 -2.2 -7.7 -5 45 47 -.10
ESA | 2 | -1.0 .7 -1.1 1 -4 1 -.35
GFZ | 2 | .5 .3 .5 2 -26 -9 -.36
GRG | 2 | -1.4 -2.0 -13.6 60 3 61 -.32
JPL | 2 | 7.3 .2 -7.4 -35 -46 44 .46
MIT | 2 | -3.4 -1.3 .2 -13 26 12 -.02
NGS | 2 | -4.5 -6.9 -.3 32 -2 8 -.13
SIO | 2 | -6.3 .6 -15.6 0 -5 0 -.10
COD | 3 | .6 .2 .9 6 -4 -7 -.49
EMR | 3 | 2.7 2.4 2.2 -8 45 0 -.36
ESA | 3 | -.8 .3 -.9 -26 -7 -1 -.55
GFZ | 3 | .2 .5 .8 4 -28 -6 -.40
GRG | 3 | 9.1 -3.4 -.4 56 -28 79 -.29
JPL | 3 | 4.7 -.6 -1.9 -45 -64 73 .19
MIT | 3 | -2.3 -3.8 -.1 -15 21 14 -.18
NGS | 3 | -2.7 -1.4 -11.1 5 -20 -15 -.32
SIO | 3 | -4.2 .8 -10.9 8 -18 4 -.16
COD | 4 | .2 -.2 .3 -6 3 1 -.49
EMR | 4 | -3.7 4.4 -6.7 -13 34 50 -.28
ESA | 4 | -.3 .4 -.5 -8 -5 11 -.50
GFZ | 4 | .5 .4 .7 1 -21 5 -.44
GRG | 4 | 2.9 -8.9 -13.8 76 -36 67 -.18
JPL | 4 | 3.5 -2.9 -8.3 -38 -66 76 .05
MIT | 4 | -5.9 -3.7 -5.9 -11 36 9 -.09
NGS | 4 | -2.0 -5.3 -4.1 24 -1 -8 -.12
SIO | 4 | -6.7 -.7 -9.5 3 20 -9 -.33
COD | 5 | .3 -.0 .9 2 9 -4 -.54
EMR | 5 | -5.0 10.5 -3.3 -6 44 9 -.27
ESA | 5 | -.9 -.0 -.7 -7 -6 8 -.58
GFZ | 5 | .4 .3 .7 -4 -24 8 -.36
GRG | 5 | 2.2 -1.1 3.5 57 2 50 -.37
JPL | 5 | -3.4 2.6 -6.6 -23 -52 46 .06
MIT | 5 | -10.3 -1.8 -3.7 -6 31 7 -.23
NGS | 5 | -5.8 -5.5 .2 30 6 -7 .0
SIO | 5 | -8.4 2.7 -14.0 2 3 -7 -.28
COD | 6 | -.0 -.1 .7 4 12 -3 -.51
EMR | 6 | -2.0 1.0 -4.1 -15 27 18 -.32
ESA | 6 | -.8 -.5 -1.1 -11 6 -4 -.43
GFZ | 6 | .5 .3 .7 -4 -22 2 -.43
GRG | 6 | -4.6 -2.4 -25.5 56 -29 80 -.43
JPL | 6 | 2.0 2.7 -8.2 -33 -56 56 .14
MIT | 6 | -9.0 -5.3 -6.1 5 14 1 -.07
NGS | 6 | -.8 -6.4 .4 16 -4 4 -.24
SIO | 6 | -7.1 -2.5 -14.8 -1 21 -1 -.20
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
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 1.1958.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1958.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 2.1958.[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 3.1958.[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 5.1958.0-6). 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 1958 summary. (Jul 16, 2017 - Jul 22, 2017)
Table 1.1958.a GPS week: 1958 MJD: 57950.000-57956.000
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 276| 1 0 3 3 4 5 .04 9 9 | -748 -60 11 110
| 0 0 2 14 11 15 .03 | 321 465
emr 84| 0 0 -4 -6 5 44 .22 17 17 | 1574 304 21 123
| 1 2 2 12 13 6 .05 | 965 860
esa 150| 0 0 -3 0 0 -7 -.02 9 9 | -403 -1397 7 156
| 0 0 1 10 3 7 .03 | 825 1396
gfz 199| -1 0 2 -11 6 -10 .13 11 10 | -157 -298 11 125
| 0 0 1 7 7 8 .04 | 354 521
grg 110| 1 0 -3 -5 4 6 -.37 16 15 | 15 -70 13 162
| 1 0 8 17 10 10 .04 | 184 367
igr n/a| 0 0 2 -4 -7 -5 .06 4 4 | -2299 13 12 75
| 0 0 1 8 11 10 .01 | 670 832
jpl 80| 0 0 -2 0 -34 27 .27 12 12 | 1218 409 41 227
| 0 1 1 8 16 16 .04 | 1054 824
mit 349| 0 -1 0 -12 -6 2 -.04 11 10 | -552 -65 39 337
| 0 0 1 29 16 6 .03 | 313 301
ngs 219| 0 0 1 19 0 -2 .03 9 7 | -746 -55 920 2147
| 0 0 2 24 23 12 .06 | 227 243
sio 351| 0 -1 0 -1 -10 -10 -.11 12 12 | --- --- --- ---
| 0 0 2 28 27 16 .03 | --- ---
Table 1.1958.b GPS week : 1958 MJD: 57950.000-57956.000
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 | 6 4 4 4 4 4 4 |
2 | 5 4 3 4 4 4 5 |
3 | 3 3 3 3 3 3 3 |
4 | --- --- --- --- 0 0 0 |
5 | 5 5 5 4 4 4 4 |
6 | 7 5 4 5 5 5 4 |
7 | 4 4 6 5 5 5 5 |
8 | 4 4 3 3 3 3 3 |
9 | 3 3 4 4 4 3 3 |
10 | 4 4 4 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 6 5 6 6 5 5 5 |
13 | 5 4 5 4 5 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 6 6 5 6 6 6 5 |
17 | 5 5 4 5 5 4 4 |
18 | 6 7 7 6 6 6 6 |
19 | 5 5 5 5 5 5 5 |
20 | 5 5 5 5 5 5 5 |
21 | 5 4 4 4 4 4 5 |
22 | 4 5 5 5 5 5 5 |
23 | 4 4 4 4 4 4 4 |
24 | 3 3 4 3 3 3 3 |
25 | 4 3 7 3 4 3 4 |
26 | 4 4 5 4 5 5 4 |
27 | 4 3 3 3 4 4 4 |
28 | 4 4 4 4 4 4 4 |
29 | 5 5 5 5 4 5 5 |
30 | 3 4 4 4 3 4 4 |
31 | 5 5 5 5 5 5 5 |
32 | 4 4 4 4 4 4 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 2.1958.0 GPS week: 1958 Day: 0 MJD: 57950.000
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| 0 -1 0 2 -12 -19 .09 10 9 | -745 -107 12 122
emr 85| 1 0 -2 -22 14 50 .24 16 16 | 436 231 18 132
esa 150| -1 1 -5 -6 -6 -14 -.02 10 9 | -878 -83 8 167
gfz 200| -1 0 2 -13 -4 -20 .12 11 10 | -57 -248 12 128
grg 113| 0 0 11 8 10 13 -.35 16 14 | -107 124 14 173
igr n/a| 0 0 1 -11 1 -5 .07 4 4 | -2586 140 12 86
jpl 80| 0 -3 -4 10 -22 24 .32 14 13 | -76 346 43 232
mit 349| 0 -1 0 7 17 11 -.02 11 11 | -670 196 49 356
ngs 215| 0 1 2 16 -33 9 -.02 10 8 | -671 -224 941 1949
sio 349| 0 -1 -5 0 34 1 -.07 13 12 | --- --- --- ---
Table 2.1958.1 GPS week: 1958 Day: 1 MJD: 57951.000
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 277| 0 0 1 9 16 16 .07 10 10 | -496 -452 11 111
emr 85| 0 -3 -5 -18 3 43 .29 16 16 | 70 1229 17 120
esa 150| 0 0 -3 -1 -5 -20 -.02 9 10 | 31 -2255 7 149
gfz 200| -2 0 3 -16 6 -16 .14 10 9 | -597 -180 11 125
grg 111| 2 0 -2 11 19 10 -.33 15 15 | 169 -611 14 181
igr n/a| 0 0 0 -10 0 2 .06 4 4 | -2923 761 13 71
jpl 80| 0 -1 -5 -6 -29 9 .31 13 13 | -312 1098 41 235
mit 350| 0 0 0 -18 -8 7 -.04 11 10 | -506 -488 37 341
ngs 217| 0 1 4 37 -12 -9 -.02 9 8 | -683 57 1059 2568
sio 355| 0 0 0 -8 -16 8 -.12 12 11 | --- --- --- ---
Table 2.1958.2 GPS week: 1958 Day: 2 MJD: 57952.000
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 9 2 -4 .04 9 9 | -1405 917 10 97
emr 85| -1 -1 -3 15 14 43 .24 16 16 | 1713 529 19 118
esa 150| 0 0 -4 -5 2 -4 -.00 9 9 | -1770 968 9 165
gfz 201| -1 0 3 -4 16 -16 .18 11 10 | -40 -360 11 118
grg 112| 3 -1 -10 -35 3 10 -.39 17 17 | -233 530 15 186
igr n/a| 0 0 3 -1 -4 -4 .06 4 4 | -1745 -5 12 70
jpl 80| 0 0 -1 1 -26 46 .27 12 12 | 1258 650 42 220
mit 350| 0 0 1 -50 -14 -1 -.08 12 10 | -845 394 41 318
ngs 221| -1 1 3 57 -4 -16 -.02 9 8 | -1225 432 692 1909
sio 356| 0 -2 0 -44 -6 9 -.09 13 12 | --- --- --- ---
Table 2.1958.3 GPS week: 1958 Day: 3 MJD: 57953.000
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| 1 0 4 5 -3 0 .04 9 9 | -467 -373 10 115
emr 85| -2 1 0 0 9 42 .21 17 17 | 2008 354 21 114
esa 150| 0 1 -1 -4 4 -6 .02 9 9 | 366 -2086 8 165
gfz 202| -1 -1 3 -9 12 -2 .15 11 10 | -383 -64 12 127
grg 111| 3 0 -1 1 13 14 -.34 15 15 | 166 -223 12 157
igr n/a| 0 0 3 3 7 -7 .08 4 4 | -1895 160 13 79
jpl 80| -1 0 0 3 -21 25 .27 12 12 | 1569 615 40 227
mit 349| 0 -1 1 7 1 5 -.06 10 9 | -280 -228 39 336
ngs 222| 0 0 -4 -20 -8 -2 .02 8 7 | -508 -252 827 2199
sio 357| 0 -1 -1 45 -24 -26 -.13 13 14 | --- --- --- ---
Table 2.1958.4 GPS week: 1958 Day: 4 MJD: 57954.000
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 3 2 16 24 .01 9 9 | -659 -209 11 110
emr 84| -2 2 -4 -9 20 41 .19 17 17 | 2477 -61 25 137
esa 150| 0 0 -3 11 2 1 -.02 8 8 | -186 -1592 7 138
gfz 198| -1 0 4 -2 -3 0 .15 11 10 | 156 -308 12 133
grg 108| 3 0 -4 2 2 5 -.37 16 15 | 186 -175 15 141
igr n/a| 0 0 3 -15 -14 9 .06 4 4 | -1571 -521 12 68
jpl 80| 0 1 -3 -10 -28 43 .28 12 12 | 2384 -272 42 231
mit 350| 0 -1 0 -34 -36 -6 -.05 11 9 | -82 -252 40 298
ngs 220| 0 0 1 24 40 -16 .09 9 7 | -733 -93 912 2161
sio 348| 1 -1 1 -8 -50 -27 -.15 12 12 | --- --- --- ---
Table 2.1958.5 GPS week: 1958 Day: 5 MJD: 57955.000
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| 2 0 4 22 11 20 .01 9 9 | -875 84 12 114
emr 85| 0 5 -7 -7 -4 33 .19 18 18 | 2567 -1323 27 127
esa 150| 0 0 -2 19 -2 -5 -.03 10 10 | 541 -3155 8 162
gfz 199| -1 0 0 -10 7 -3 .09 9 8 | 344 -1332 11 123
grg 111| 0 -1 0 -2 -10 -14 -.43 16 15 | 116 -279 13 147
igr n/a| 0 0 2 8 -24 -21 .04 4 4 | -2008 -1479 12 80
jpl 80| 0 0 -2 10 -68 5 .23 13 13 | 2284 -1004 43 219
mit 349| 0 -2 -1 -34 -5 2 -.03 10 9 | -500 -150 37 360
ngs 218| 0 0 0 11 16 16 .09 8 7 | -778 -67 1169 2401
sio 343| 0 -1 0 -14 -22 -23 -.12 11 11 | --- --- --- ---
Table 2.1958.6 GPS week: 1958 Day: 6 MJD: 57956.000
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| 2 0 6 -26 -3 0 .03 10 9 | -594 -280 12 107
emr 84| 0 2 -6 -3 -17 53 .15 18 18 | 1747 1169 26 118
esa 150| 0 1 -4 -8 0 0 -.07 9 9 | -929 -1581 7 146
gfz 199| -1 0 1 -23 9 -11 .08 11 10 | -528 401 12 122
grg 107| 0 0 -14 -25 -6 5 -.39 17 15 | -187 138 14 155
igr n/a| 0 0 3 -3 -19 -14 .05 4 4 | -3367 1036 12 75
jpl 80| -1 0 -3 -7 -47 39 .20 12 12 | 1423 1430 41 226
mit 349| 0 -1 0 31 1 1 .03 10 9 | -986 71 35 352
ngs 220| 0 0 3 12 -1 0 .09 8 7 | -624 -244 844 1846
sio 349| 1 -1 2 19 9 -15 -.14 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 3.1958.0 GPS week: 1958 Day: 0 MJD: 57950.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 13 22 14 9 24 6 24 8 19 9 5 | 55 55 55 49 57 52 51 50 51 49 51
2E | 17 9 9 12 23 4 12 10 11 10 5 | 15 20 22 24 23 20 24 20 23 22 18
3 | 9 14 8 5 9 4 9 5 8 10 3 | 27 30 30 26 26 26 32 26 26 30 26
5 | 10 11 13 12 14 3 16 15 11 14 4 | 45 48 49 40 48 42 51 38 41 41 42
6E | 13 15 15 10 41 7 20 8 11 14 6 | 39 39 43 40 50 39 43 38 37 38 38
7 | 13 19 7 9 11 4 12 10 9 13 4 | 27 25 26 28 24 27 31 32 28 23 26
8 | 6 13 6 10 11 2 11 10 6 14 3 | 23 27 23 24 24 23 29 22 22 26 22
9 | 5 14 8 7 9 4 15 7 9 12 3 | 24 31 23 22 19 23 38 21 19 29 22
10 | 8 10 13 11 11 4 10 8 6 8 3 | 23 28 30 27 22 25 29 25 23 28 24
11 | 9 17 10 9 14 4 13 12 8 11 4 | 45 51 48 46 47 47 51 46 47 47 46
12 | 10 24 8 12 21 5 16 20 11 11 5 | 32 30 28 36 29 31 30 31 33 35 30
13 | 10 10 12 13 12 4 14 10 11 15 4 | 27 26 25 35 25 27 29 26 28 32 26
14 | 9 13 10 10 9 5 10 12 7 14 4 | 25 31 28 31 32 28 28 26 27 27 26
15 | 6 14 11 8 11 3 13 9 12 12 4 | 28 30 27 27 30 26 28 25 30 29 27
16 | 10 24 8 15 22 5 13 20 12 18 6 | 39 39 40 41 34 39 39 42 43 45 39
17 | 8 16 9 14 16 5 11 11 8 14 4 | 27 32 26 37 25 31 33 34 34 28 29
18 | 10 26 14 14 14 5 18 22 14 16 6 | 32 35 30 36 32 32 33 40 38 38 32
19 | 9 19 9 16 19 5 15 11 10 19 5 | 25 29 27 34 23 28 32 31 30 27 26
20 | 10 17 13 9 15 4 11 13 10 13 4 | 44 46 41 45 42 41 40 39 42 40 41
21E | 18 11 7 12 17 4 12 10 9 11 4 | 20 22 21 26 25 21 24 25 20 25 21
22 | 12 13 11 10 10 4 13 9 9 15 4 | 44 44 44 48 46 46 48 46 47 44 44
23 | 5 19 9 8 9 4 11 9 8 10 3 | 28 25 26 29 26 27 29 29 27 29 26
24 | 9 10 5 6 8 3 11 7 9 8 3 | 21 22 19 19 21 19 21 19 19 16 18
25 | 7 21 7 7 17 4 13 10 6 9 3 | 280 193 280 281 276 282 282 280 283 280 281
26 | 11 18 9 14 17 3 11 7 6 10 4 | 37 35 35 31 37 35 37 36 36 38 34
27 | 8 14 6 10 9 4 13 9 6 12 3 | 28 32 27 28 25 27 32 24 27 26 26
28 | 6 14 6 10 15 5 13 9 8 12 3 | 23 26 23 21 25 22 29 24 24 21 22
29 | 10 23 10 13 17 4 16 12 11 12 5 | 28 26 25 29 25 25 28 27 25 25 24
30 | 7 14 6 6 11 4 15 6 7 7 3 | 22 23 25 23 27 24 29 23 23 23 23
31 | 13 14 8 15 14 3 8 13 8 12 4 | 18 23 17 29 18 22 21 25 23 18 19
32 | 7 11 9 7 9 3 11 9 6 16 3 | 24 32 25 29 24 25 33 25 25 35 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 10 11 16 4 14 11 10 13 |T 37 37 38 40 38 38 41 38 38 39 37
WRMS | 9 16 9 10 14 4 13 11 8 12 |NE 38 37 38 40 38 38 42 39 39 40 38
MEDI | 9 14 9 10 14 4 13 10 9 12 |MD 27 30 27 29 26 27 32 27 28 29 26
Table 3.1958.1 GPS week: 1958 Day: 1 MJD: 57951.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 13 10 9 20 6 15 7 9 9 4 | 41 42 41 41 45 39 41 35 34 34 38
2E | 18 10 8 10 12 4 10 10 11 8 4 | 14 18 17 22 16 18 18 18 18 18 16
3 | 10 11 8 6 8 5 9 4 7 12 3 | 19 29 21 20 18 20 26 19 20 21 19
5 | 11 13 13 11 13 3 14 14 8 11 4 | 32 37 32 30 32 30 38 26 27 29 29
6E | 8 11 12 11 25 4 13 9 13 8 4 | 31 32 36 34 37 30 31 30 31 27 31
7 | 10 17 6 8 16 2 11 8 8 14 4 | 27 26 24 29 24 26 27 30 29 23 25
8 | 9 11 7 9 10 3 9 6 8 11 3 | 20 25 20 19 17 19 25 20 20 19 19
9 | 8 11 8 7 8 4 10 6 7 13 3 | 21 32 25 25 16 24 33 20 24 32 24
10 | 10 9 10 7 17 4 13 14 5 11 4 | 15 24 22 20 18 18 24 18 16 25 18
11 | 7 10 10 7 20 4 11 9 6 9 3 | 26 28 28 25 24 27 32 27 26 24 25
12 | 6 26 8 9 14 4 18 17 9 8 4 | 27 27 24 30 20 25 23 27 28 27 25
13 | 10 11 12 13 11 3 9 9 8 15 4 | 22 27 26 33 21 25 27 23 24 29 24
14 | 11 10 11 10 13 4 9 9 11 14 4 | 30 29 29 29 27 26 31 25 30 28 27
15 | 7 15 11 9 12 3 15 9 7 11 3 | 23 24 19 26 22 22 24 21 23 26 22
16 | 10 25 8 12 19 5 14 19 9 15 5 | 29 30 29 35 22 29 29 33 31 31 28
17 | 8 13 11 13 14 5 10 12 10 14 4 | 23 30 24 30 23 27 29 31 31 25 26
18 | 10 28 13 14 22 6 19 22 13 15 6 | 19 27 21 28 22 21 24 32 24 28 21
19 | 11 18 9 14 17 5 14 13 11 19 5 | 19 26 20 22 20 20 24 23 22 20 19
20 | 10 15 12 9 15 4 13 11 10 12 4 | 31 34 29 31 30 29 31 28 28 29 28
21E | 13 11 7 10 11 4 12 10 8 8 3 | 21 21 21 26 19 21 22 25 21 24 21
22 | 13 11 12 11 15 5 10 9 11 19 4 | 33 36 34 40 34 36 37 38 39 35 35
23 | 9 22 8 8 9 4 10 7 9 9 4 | 23 22 23 27 22 24 22 24 26 26 23
24 | 6 9 5 6 11 4 9 10 8 6 2 | 21 23 20 19 19 20 23 20 19 18 19
25 | 7 15 7 5 13 4 12 8 8 5 3 | 252 219 250 250 242 250 252 249 250 252 251
26 | 14 12 8 12 17 4 13 7 8 6 4 | 29 30 27 29 27 27 30 28 28 25 27
27 | 7 12 8 6 9 3 13 6 9 8 3 | 26 29 24 24 21 25 30 23 26 24 24
28 | 7 16 9 11 13 5 14 9 6 9 3 | 19 26 24 22 21 20 27 23 26 20 21
29 | 9 24 11 10 15 3 17 12 11 8 4 | 28 26 25 28 19 25 28 27 23 25 25
30 | 6 17 6 9 14 3 11 5 7 9 3 | 23 22 25 24 23 23 24 23 24 22 23
31 | 11 22 10 14 17 4 10 13 12 11 5 | 24 29 20 28 16 23 26 26 26 18 21
32 | 9 14 9 8 11 3 13 10 8 12 3 | 26 34 23 25 19 23 34 21 24 30 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 9 10 15 4 13 11 9 12 |T 32 34 32 34 30 32 35 32 32 32 31
WRMS | 10 16 10 9 15 4 13 10 8 11 |NE 32 35 32 35 30 32 36 33 33 33 32
MEDI | 10 13 9 9 14 4 12 9 8 11 |MD 24 28 24 28 22 25 27 25 26 25 24
Table 3.1958.2 GPS week: 1958 Day: 2 MJD: 57952.000
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 13 9 13 21 4 11 8 7 14 4 | 28 30 29 30 32 25 26 22 24 24 25
2E | 12 9 7 8 9 3 11 8 9 6 3 | 19 20 23 23 20 21 23 24 24 23 21
3 | 5 13 7 6 12 3 8 6 8 10 3 | 22 31 27 24 28 23 29 24 24 27 24
5 | 9 10 11 14 20 3 10 14 10 15 4 | 41 43 42 36 50 37 44 31 35 33 37
6E | 8 10 11 9 22 3 12 9 8 8 4 | 19 23 25 22 25 21 22 21 22 22 20
X7 | 13 14 7 --- 21 4 7 15 15 --- 6 | 35 34 32 --- 37 32 33 33 30 --- 31
8 | 6 11 6 12 10 5 9 7 5 9 3 | 21 27 22 23 17 22 25 20 22 20 20
9 | 5 13 9 10 10 3 11 5 10 13 3 | 24 34 24 23 19 24 37 22 29 33 25
10 | 11 9 10 8 16 3 10 11 7 10 4 | 24 29 29 27 31 26 30 26 24 28 26
11 | 6 12 9 8 17 3 8 11 7 8 3 | 30 36 34 33 32 32 35 34 31 30 31
12 | 9 29 7 12 21 4 19 19 10 10 5 | 25 27 20 24 21 21 24 20 22 20 19
13 | 9 9 10 17 14 3 6 10 10 16 4 | 21 25 22 37 18 22 23 20 24 31 22
14 | 9 12 10 11 14 3 7 9 8 13 4 | 17 16 14 13 16 13 13 16 15 18 13
15 | 7 14 10 10 16 4 12 11 7 14 4 | 22 24 22 28 25 21 22 19 18 23 20
16 | 10 22 7 14 19 6 17 19 8 14 5 | 29 32 28 31 25 29 29 30 31 29 27
17 | 9 15 9 10 13 4 12 11 11 15 4 | 27 35 28 35 26 32 36 37 32 32 30
18 | 10 27 13 18 22 5 19 22 14 16 6 | 27 32 26 33 28 27 30 36 29 31 26
19 | 8 20 8 13 13 5 13 12 9 20 4 | 25 32 26 30 26 27 32 30 26 27 25
20 | 13 15 10 13 21 4 12 13 12 12 5 | 30 31 28 33 30 29 30 28 28 28 27
21E | 13 13 7 9 17 4 12 12 9 12 4 | 16 21 22 25 19 19 19 23 19 24 19
22 | 13 12 10 12 17 4 10 13 10 19 5 | 35 37 37 39 34 35 39 37 35 37 35
23 | 5 20 10 7 10 3 9 9 8 13 4 | 27 25 26 29 24 26 27 28 27 29 26
24 | 7 10 6 10 20 5 9 10 7 6 3 | 18 20 17 19 28 18 21 17 16 16 16
X25 | 18 --- 11 9 149 24 57 18 20 11 7 | 911 --- 915 916 857 916 914 912 910 912 913
26 | 14 16 10 12 18 4 11 7 8 9 4 | 27 29 23 27 23 25 26 27 26 27 24
27 | 9 11 7 8 12 3 12 6 7 9 3 | 28 32 28 28 23 27 29 27 29 26 27
28 | 9 15 9 10 13 4 8 10 12 13 4 | 18 27 20 18 19 19 23 20 22 18 19
29 | 9 23 7 11 17 4 19 15 11 9 4 | 27 28 24 32 25 28 29 30 26 26 26
30 | 8 16 6 10 20 4 11 9 10 13 4 | 23 23 22 20 29 20 24 24 20 20 21
31 | 12 16 8 14 24 3 9 12 11 11 5 | 18 21 16 26 22 18 22 23 20 16 18
32 | 5 14 8 9 13 2 11 11 8 13 3 | 20 31 20 24 17 21 31 17 20 30 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 9 11 17 4 12 12 9 13 |T 53 28 53 56 52 53 56 54 53 55 52
WRMS | 9 16 9 10 17 4 12 10 8 12 |NE 58 29 58 61 56 58 61 58 58 60 57
MEDI | 9 13 9 10 17 4 11 11 9 12 |MD 25 29 25 27 25 25 29 24 24 27 25
Table 3.1958.3 GPS week: 1958 Day: 3 MJD: 57953.000
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 | 6 12 8 10 18 4 8 8 6 10 3 | 28 33 33 30 36 30 31 29 30 29 29
2E | 14 12 6 9 13 4 10 9 10 12 4 | 19 23 22 24 22 23 23 25 27 26 22
3 | 6 14 8 6 10 3 8 8 5 11 3 | 27 32 31 30 27 28 31 29 30 31 29
5 | 10 12 10 13 16 4 11 10 10 12 4 | 40 40 39 34 41 37 43 31 38 34 36
6E | 13 14 10 11 27 4 9 10 9 17 5 | 25 33 30 28 33 26 27 28 25 30 26
X7 | 11 16 7 9 14 3 11 13 10 --- 4 | 41 41 38 43 41 39 44 43 39 --- 39
8 | 7 11 5 11 10 4 9 7 5 10 3 | 26 30 28 28 28 27 30 24 25 25 25
9 | 12 14 9 6 11 3 11 5 6 14 3 | 27 35 31 29 20 30 36 27 27 33 27
10 | 7 10 8 8 13 4 8 8 6 6 3 | 31 33 32 33 28 30 33 30 35 30 31
11 | 7 11 11 6 16 5 6 10 5 9 3 | 32 36 34 34 35 32 36 35 33 32 33
12 | 9 31 6 13 20 4 19 18 9 11 5 | 26 29 22 26 22 24 26 20 25 22 21
13 | 8 10 10 12 10 3 8 8 7 13 3 | 23 28 21 33 19 23 26 22 24 30 23
14 | 8 10 9 16 11 4 10 6 7 11 3 | 22 23 21 21 21 19 21 21 27 21 21
15 | 7 16 9 9 11 3 16 8 5 12 3 | 25 25 23 26 25 23 26 23 27 25 24
16 | 9 24 9 14 23 6 15 19 13 16 5 | 30 28 27 28 24 27 25 27 30 30 25
17 | 9 17 10 13 14 4 8 13 8 17 4 | 29 35 28 37 29 32 36 35 32 29 30
18 | 9 32 11 15 19 5 21 19 12 14 6 | 28 32 26 34 25 27 27 33 30 26 26
19 | 12 20 8 14 14 5 14 13 9 23 5 | 27 33 29 34 27 30 33 31 29 30 27
20 | 10 14 10 13 19 6 13 10 9 11 4 | 29 28 25 31 24 25 26 25 24 24 24
21E | 9 15 7 9 18 3 11 9 7 10 3 | 22 24 21 24 18 20 23 22 25 24 21
22 | 11 13 12 11 12 5 10 10 11 20 4 | 27 31 27 33 25 28 30 30 29 27 27
23 | 7 23 10 7 10 3 10 10 8 9 4 | 26 23 28 29 22 26 24 24 24 24 24
24 | 6 12 5 5 11 4 10 6 6 7 2 | 22 26 25 24 23 25 26 22 26 24 23
25 | 7 13 8 6 15 4 11 9 7 8 3 | 447 678 453 453 464 452 449 451 454 454 452
26 | 13 11 10 11 18 4 12 7 10 8 4 | 28 28 23 28 26 25 26 26 27 24 25
27 | 6 10 5 9 11 4 11 5 5 8 2 | 29 30 29 29 27 28 31 27 27 28 27
28 | 7 13 9 10 11 4 10 9 8 10 3 | 23 30 28 25 26 25 28 26 25 26 24
29 | 9 24 8 15 18 5 19 14 8 9 4 | 25 27 23 27 25 23 25 26 23 22 23
30 | 6 20 7 6 14 3 10 8 9 12 3 | 25 28 27 25 27 26 29 29 26 28 25
31 | 9 15 9 16 18 3 12 11 9 18 4 | 20 26 19 27 19 21 22 24 23 18 20
32 | 6 16 9 10 11 3 14 6 7 16 3 | 24 35 23 23 22 24 33 22 28 32 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 9 11 15 4 12 10 8 13 |T 40 51 40 42 40 40 42 40 41 41 39
WRMS | 9 17 9 10 15 4 12 9 7 14 |NE 42 54 42 45 42 42 45 43 43 43 42
MEDI | 9 14 9 10 14 4 11 9 8 11 |MD 27 30 27 29 25 26 28 27 27 27 25
Table 3.1958.4 GPS week: 1958 Day: 4 MJD: 57954.000
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 | 6 12 7 10 17 4 10 10 7 9 3 | 41 41 39 38 43 39 39 36 38 36 38
2E | 16 12 6 11 12 3 12 10 8 9 4 | 22 22 24 25 21 24 23 28 26 24 23
3 | 7 19 7 5 9 3 10 7 6 11 3 | 26 33 29 27 25 27 33 26 27 30 27
X4 | 2 --- --- --- --- >>>> --- --- --- --- 0 | 9999 --- --- --- --- 319 --- --- --- --- 9999
5 | 8 10 11 14 15 4 11 11 9 10 4 | 37 40 36 35 38 35 40 36 33 32 34
X6E | 10 --- 10 9 23 4 10 8 9 9 4 | 35 --- 36 36 38 34 35 34 34 35 34
7 | 15 14 5 9 16 4 10 11 9 15 4 | 43 39 40 37 41 41 40 41 41 33 40
8 | 9 14 5 8 9 3 9 6 7 8 3 | 29 33 29 30 30 30 33 26 31 27 29
9 | 10 16 8 7 6 4 11 6 7 12 3 | 29 34 26 26 24 26 36 27 27 31 27
10 | 9 9 8 9 13 4 9 6 6 8 3 | 26 30 28 29 28 27 30 26 27 27 26
11 | 6 11 11 5 17 3 7 13 6 8 3 | 32 35 33 33 33 32 35 33 33 28 31
12 | 8 28 6 11 21 5 21 15 8 8 4 | 30 26 25 32 27 31 27 27 29 28 27
13 | 9 12 11 18 9 3 8 8 9 15 4 | 26 30 29 41 24 31 30 30 32 37 30
14 | 10 11 9 15 13 4 9 7 8 11 4 | 28 27 28 26 25 26 26 27 27 27 26
15 | 5 16 10 10 14 3 15 12 9 9 4 | 26 30 26 32 24 28 29 28 33 29 27
16 | 12 22 8 14 24 6 11 19 10 13 5 | 32 30 30 32 30 31 29 33 31 30 29
17 | 8 19 10 12 17 3 8 15 10 11 4 | 39 41 39 44 37 42 44 44 43 38 40
18 | 10 29 10 15 20 6 22 19 14 15 6 | 29 33 24 33 27 27 27 35 34 31 27
19 | 10 21 9 12 19 5 13 12 11 18 5 | 32 37 36 35 33 34 37 34 34 30 32
20 | 10 18 9 13 18 5 15 11 13 13 4 | 34 35 31 37 32 32 32 31 35 32 32
21E | 11 18 7 14 18 3 12 8 7 7 4 | 28 28 27 32 29 28 28 29 25 27 27
22 | 12 17 12 10 13 4 12 11 11 16 4 | 36 40 35 41 35 37 40 40 40 38 37
23 | 8 21 9 7 6 3 11 12 9 10 4 | 31 27 30 31 30 29 30 32 32 30 30
24 | 4 12 6 7 13 6 10 8 11 6 3 | 25 26 26 26 28 27 26 27 27 27 25
25 | 8 14 7 5 16 3 10 8 9 15 3 | 599 381 605 606 589 604 603 603 602 603 603
26 | 14 15 10 13 26 4 10 8 8 7 4 | 33 34 31 33 34 32 31 35 33 34 32
27 | 9 13 7 9 13 3 10 7 8 9 3 | 38 37 38 37 39 36 39 32 36 34 36
28 | 11 20 7 13 16 3 10 8 7 12 4 | 30 29 29 30 30 29 34 28 30 28 28
29 | 8 25 7 12 15 4 19 13 7 9 4 | 34 35 31 34 35 35 37 36 33 35 33
30 | 5 14 5 8 14 2 10 5 5 6 2 | 29 27 30 27 31 29 30 29 29 29 29
31 | 9 16 9 15 20 6 10 11 8 15 4 | 25 30 22 29 22 25 26 25 25 22 23
32 | 7 15 8 12 12 4 11 8 7 17 4 | 27 37 27 27 24 27 35 26 28 36 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 17 8 11 16 4 12 11 9 12 |T 49 44 49 51 48 57 51 49 50 49 48
WRMS | 9 17 8 10 15 4 12 9 7 12 |NE 52 45 51 53 50 61 54 52 53 52 51
MEDI | 9 15 8 11 15 4 10 10 8 10 |MD 30 33 30 32 30 31 33 31 32 30 29
Table 3.1958.5 GPS week: 1958 Day: 5 MJD: 57955.000
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 | 7 14 10 6 22 5 11 7 7 9 3 | 29 35 30 31 38 28 30 27 29 28 29
2E | 14 13 8 10 13 4 11 9 8 9 4 | 22 24 24 27 24 23 27 26 27 27 24
3 | 6 17 8 4 11 4 10 9 6 10 3 | 26 32 29 26 25 26 31 28 26 29 26
X4 | 3 --- --- --- --- 46 --- --- --- --- 0 | 9999 --- --- --- --- 168 --- --- --- --- 9999
5 | 10 12 12 11 12 3 12 8 9 11 4 | 31 36 29 33 30 30 35 28 31 31 30
6E | 9 19 10 7 26 4 12 10 7 8 4 | 24 32 24 24 26 20 23 25 22 24 22
7 | 10 16 10 9 23 3 9 12 9 16 4 | 28 27 22 24 26 23 26 24 24 16 23
8 | 7 15 7 8 13 4 11 6 8 7 3 | 19 26 21 19 19 19 23 17 18 20 18
9 | 4 14 10 6 8 2 11 7 7 7 3 | 30 39 32 30 24 31 41 31 31 33 31
10 | 7 12 9 4 11 4 10 5 7 7 2 | 25 28 26 26 28 26 27 27 26 28 26
11 | 6 14 12 9 14 4 11 12 7 7 3 | 28 33 30 31 28 27 31 29 28 27 28
12 | 7 32 10 6 17 4 20 14 7 6 4 | 23 25 20 25 19 22 21 20 27 24 21
13 | 9 14 14 12 9 3 8 7 7 16 4 | 16 22 18 29 15 18 22 16 22 29 19
14 | 9 9 11 9 10 3 10 8 7 11 3 | 15 16 16 11 12 13 15 15 17 16 13
15 | 7 22 12 11 8 5 15 9 6 10 4 | 20 25 20 25 19 21 22 20 24 22 21
16 | 11 23 11 11 21 5 11 19 12 14 5 | 21 23 23 27 21 21 19 25 23 23 20
17 | 8 16 11 11 18 4 15 11 9 14 4 | 20 27 19 25 15 23 31 25 25 16 20
18 | 10 29 13 15 21 7 24 17 12 15 6 | 30 36 26 37 29 29 29 37 32 31 29
19 | 9 20 10 10 18 4 16 10 9 17 4 | 20 28 20 24 19 21 27 23 23 18 19
20 | 8 20 12 12 16 5 16 10 9 12 4 | 29 33 26 33 31 27 28 25 26 27 27
21E | 13 16 7 13 21 4 13 10 7 7 4 | 22 24 24 29 24 25 24 25 26 24 23
22 | 14 16 12 8 16 4 11 12 10 17 5 | 32 34 34 34 38 34 35 36 36 34 33
23 | 6 22 13 5 9 3 12 12 7 10 4 | 28 25 32 29 27 29 25 31 28 30 29
24 | 7 14 6 6 13 4 12 5 5 6 2 | 18 25 19 19 21 21 28 18 19 19 18
25 | 6 18 7 4 13 4 11 7 8 8 3 | 548 454 548 547 546 548 546 545 547 544 547
26 | 16 16 11 10 22 5 12 9 10 7 4 | 29 30 28 25 29 27 28 26 26 26 26
27 | 8 12 9 6 15 3 10 9 8 9 3 | 20 25 20 22 18 18 21 18 20 21 19
28 | 12 16 8 10 15 5 13 8 8 11 4 | 20 23 20 18 21 18 24 20 17 18 17
29 | 8 28 10 12 19 5 19 16 8 9 5 | 22 25 20 22 18 20 23 25 20 20 19
30 | 8 23 7 5 17 4 12 5 6 12 3 | 22 28 25 22 26 22 26 23 22 23 22
31 | 9 19 11 15 22 5 13 10 8 13 4 | 21 26 18 24 19 19 22 21 20 14 18
32 | 7 14 8 7 11 3 12 9 6 16 3 | 20 34 21 23 21 22 34 20 23 32 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 18 10 9 16 4 13 10 8 11 |T 40 41 40 42 40 44 43 41 41 41 39
WRMS | 9 18 10 8 15 4 13 9 7 11 |NE 43 43 43 44 42 47 45 43 43 43 42
MEDI | 8 16 10 9 15 4 12 9 8 10 |MD 22 27 24 25 24 23 27 25 25 24 22
Table 3.1958.6 GPS week: 1958 Day: 6 MJD: 57956.000
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 | 7 19 8 8 15 3 10 6 7 7 3 | 32 38 33 31 34 30 31 29 30 30 30
2E | 15 16 8 9 21 4 13 9 8 12 4 | 28 30 32 34 30 31 30 33 34 33 30
3 | 5 17 7 6 11 3 8 7 5 8 3 | 37 39 38 35 39 36 38 39 36 39 37
X4 | 4 --- --- --- --- 63 --- --- --- --- 0 | 9999 --- --- --- --- 134 --- --- --- --- 9999
5 | 10 10 10 13 19 3 11 8 8 12 4 | 50 50 49 45 52 47 54 45 49 45 47
6E | 9 19 11 9 15 4 11 7 7 10 4 | 28 34 33 31 24 28 29 29 26 30 28
7 | 11 14 9 10 19 4 10 10 10 16 4 | 34 32 28 26 34 28 31 28 26 19 27
8 | 8 14 7 7 12 3 8 9 6 8 3 | 31 33 29 29 31 29 32 28 30 29 29
9 | 5 15 9 9 10 4 12 8 6 9 3 | 39 47 37 37 32 40 49 45 40 43 39
10 | 9 14 7 8 14 3 8 6 5 8 3 | 41 43 42 43 45 41 41 42 42 43 41
11 | 8 12 11 7 17 3 8 10 6 8 3 | 43 47 45 45 43 44 45 45 43 43 43
12 | 7 30 7 9 16 4 22 14 7 7 4 | 29 30 24 31 29 27 28 24 28 27 26
13 | 12 11 11 13 15 2 7 8 8 15 4 | 26 27 25 37 21 29 29 28 33 37 28
14 | 9 8 9 17 13 6 6 10 8 10 4 | 28 24 24 18 24 21 22 27 27 24 23
15 | 9 16 10 12 14 3 14 9 6 9 4 | 29 29 28 34 26 31 32 28 33 30 29
16 | 10 21 10 14 20 5 17 18 10 12 5 | 31 29 28 32 27 28 28 28 31 28 27
17 | 10 15 11 13 14 4 7 11 7 12 4 | 34 36 32 43 34 37 38 40 38 34 35
18 | 8 28 12 14 21 5 18 17 12 12 5 | 46 46 43 47 48 43 43 50 43 44 43
19 | 11 21 8 14 13 4 13 11 8 19 4 | 34 39 35 40 35 36 38 40 38 34 35
20 | 9 15 12 12 21 5 13 11 10 10 4 | 44 41 39 50 44 43 40 40 43 42 42
21E | 12 18 7 12 24 3 11 9 7 9 4 | 26 29 29 32 30 28 26 32 30 30 28
22 | 11 15 13 10 17 4 11 9 9 16 4 | 47 47 47 46 50 47 47 47 47 46 46
23 | 8 24 9 8 7 3 13 12 7 9 4 | 37 35 36 38 35 38 36 44 40 40 38
24 | 8 11 5 8 16 4 9 7 7 5 3 | 26 31 28 30 30 29 29 26 29 27 27
25 | 6 19 8 5 18 4 12 8 5 7 3 | 598 453 599 600 593 600 598 599 600 599 599
26 | 17 14 9 7 18 4 9 8 9 7 4 | 32 30 27 28 34 29 29 29 28 28 27
27 | 9 10 9 6 16 2 8 12 8 5 3 | 35 34 33 33 35 32 34 31 33 30 32
28 | 9 14 9 11 13 3 8 7 6 11 3 | 28 28 29 29 31 28 31 29 27 28 27
29 | 10 28 9 11 14 4 18 13 8 9 4 | 36 38 34 35 34 35 39 36 36 35 34
30 | 7 22 7 10 17 2 10 7 6 8 3 | 32 38 33 35 36 32 34 33 32 32 32
31 | 13 14 10 15 25 4 10 10 10 16 5 | 26 33 24 30 32 25 29 26 26 24 24
32 | 7 15 9 11 16 5 12 12 6 16 4 | 34 43 30 29 31 32 41 35 34 42 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 9 11 17 4 12 10 8 11 |T 52 49 51 53 52 54 53 52 52 52 51
WRMS | 9 18 9 10 15 4 12 9 7 10 |NE 55 51 54 56 55 57 56 56 56 55 54
MEDI | 9 15 9 10 16 4 11 9 7 9 |MD 34 35 33 34 34 32 34 33 33 33 32
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 4.1958 GPS week: 1958 MJD: 57950.0-57956.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3002 |U 8 9 20 |U 5 7 19 |U 7 6 16 |
emr | emr 2947 |U 12 9 24 |U 7 7 18 | 9 8 20 |
esa | esa 2976 | 9 9 21 |U 5 6 17 | 7 6 17 |
gfz | gfz 2961 |U 8 9 22 |U 6 7 20 |U 9 7 24 |
grg | grg 2973 |U 10 11 23 |U 9 10 29 | 8 6 19 |
igr | igr 2975 | 9 9 21 | 5 6 17 | 7 6 18 |
igs | igs 2975 | 9 9 20 | 5 7 18 | 7 6 17 |
jpl | jpl 2976 | 11 10 24 |U 6 7 17 |U 8 7 21 |
mit | mit 2976 | 11 12 23 |U 7 8 26 |U 13 16 108 |
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 5.1958.0 GPS week: 1958 Day: 0 MJD: 57950.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 6 13 | 7 6 21 | 10 8 24 |
emr | emr 2976 | 10 7 14 | 6 7 23 | 12 12 25 |
esa | esa 2976 | 9 8 16 | 5 6 18 | 9 8 23 |
gfz | gfz 2974 | 7 8 15 | 7 6 20 | 10 7 24 |
grg | grg 2967 | 8 8 16 | 7 8 22 | 10 7 24 |
igr | igr 2976 | 8 7 16 | 6 6 18 | 10 7 26 |
igs | igs 2976 | 8 7 14 | 7 6 20 | 10 7 24 |
jpl | jpl 2976 | 10 7 20 | 7 6 21 | 11 9 28 |
mit | mit 2976 | 8 7 17 | 7 7 23 | 10 7 23 |
Table 5.1958.1 GPS week: 1958 Day: 1 MJD: 57951.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 10 16 | 5 5 23 | 6 6 11 |
emr | emr 2976 | 9 10 16 | 5 7 18 | 7 8 19 |
esa | esa 2976 | 10 10 16 | 5 5 24 | 5 6 14 |
gfz | gfz 2976 | 11 10 16 | 5 5 22 | 6 6 12 |
grg | grg 2975 | 10 11 16 | 6 6 26 | 7 7 15 |
igr | igr 2976 | 10 10 17 | 4 5 20 | 5 6 12 |
igs | igs 2976 | 10 10 15 | 4 5 21 | 6 6 13 |
jpl | jpl 2976 | 9 11 20 | 5 7 19 | 6 6 17 |
mit | mit 2976 | 9 11 17 | 6 7 30 | 6 5 14 |
Table 5.1958.2 GPS week: 1958 Day: 2 MJD: 57952.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 12 | 6 7 18 | 7 6 16 |
emr | emr 2880 | 8 5 23 | 7 6 14 | 8 8 16 |
esa | esa 2976 | 5 4 13 | 6 7 15 | 7 5 17 |
gfz | gfz 2880 | 5 5 13 | 7 7 18 | 7 6 22 |
grg | grg 2976 | 5 6 13 | 16 15 36 | 7 6 18 |
igr | igr 2976 | 5 5 13 | 6 6 17 | 7 5 19 |
igs | igs 2976 | 5 5 13 | 6 7 16 | 7 5 16 |
jpl | jpl 2976 | 7 6 17 | 7 8 15 | 8 8 18 |
mit | mit 2976 | 6 6 17 | 7 9 21 | 8 6 16 |
Table 5.1958.3 GPS week: 1958 Day: 3 MJD: 57953.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2970 | 9 11 38 | 6 6 17 | 8 7 12 |
emr | emr 2971 | 14 12 40 | 6 5 20 | 9 9 14 |
esa | esa 2976 | 11 11 39 | 6 6 17 | 8 6 13 |
gfz | gfz 2971 | 10 11 48 | 7 7 21 | 8 5 15 |
grg | grg 2971 | 14 16 42 | 7 9 21 | 8 6 17 |
igr | igr 2971 | 11 11 39 | 6 6 16 | 7 5 13 |
igs | igs 2971 | 10 12 39 | 6 7 17 | 8 6 12 |
jpl | jpl 2976 | 12 12 40 | 6 7 15 | 9 8 17 |
mit | mit 2976 | 12 13 40 | 7 8 27 | 10 7 15 |
Table 5.1958.4 GPS week: 1958 Day: 4 MJD: 57954.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2978 | 11 12 21 | 4 8 21 | 7 6 18 |
emr | emr 2880 | 16 10 26 | 7 11 14 | 8 6 21 |
esa | esa 2976 | 13 13 23 | 5 8 17 | 7 6 17 |
gfz | gfz 2976 | 12 12 24 | 5 9 22 | 7 6 18 |
grg | grg 2976 | 14 18 34 | 5 9 29 | 7 7 22 |
igr | igr 2976 | 12 12 23 | 5 8 18 | 7 6 19 |
igs | igs 2976 | 12 12 23 | 4 8 19 | 7 6 18 |
jpl | jpl 2976 | 14 12 27 | 5 9 19 | 7 6 19 |
mit | mit 2976 | 18 16 20 | 8 10 37 | 9 8 16 |
Table 5.1958.5 GPS week: 1958 Day: 5 MJD: 57955.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 6 14 | 4 7 18 | 8 6 17 |
emr | emr 2976 | 9 6 17 | 7 10 16 | 8 9 23 |
esa | esa 2976 | 5 5 12 | 5 7 16 | 8 5 18 |
gfz | gfz 2976 | 5 5 12 | 5 7 19 | 8 5 18 |
grg | grg 2976 | 4 5 11 | 19 14 51 | 10 6 20 |
igr | igr 2976 | 5 5 13 | 5 7 15 | 8 5 18 |
igs | igs 2976 | 5 5 11 | 4 7 17 | 8 5 18 |
jpl | jpl 2976 | 7 7 15 | 4 8 15 | 9 6 25 |
mit | mit 2976 | 10 15 25 | 5 8 19 | 46 75 658 |
Table 5.1958.6 GPS week: 1958 Day: 6 MJD: 57956.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 13 25 | 5 6 14 | 6 7 17 |
emr | emr 2976 | 16 13 30 | 9 7 23 | 7 6 19 |
esa | esa 2976 | 12 14 26 | 6 6 15 | 6 6 16 |
gfz | gfz 2976 | 10 13 25 | 5 7 15 | 18 16 57 |
grg | grg 2976 | 12 14 27 | 5 6 21 | 6 5 18 |
igr | igr 2976 | 12 14 26 | 5 6 14 | 6 6 17 |
igs | igs 2976 | 11 14 26 | 5 6 15 | 6 5 16 |
jpl | jpl 2976 | 15 15 29 | 6 6 16 | 7 9 20 |
mit | mit 2976 | 13 14 26 | 7 8 21 | 5 8 15 |
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 6.1958 GPS week: 1958 MJD: 57950.500-57956.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -9 5 -3 102 1 | 14 19
| 10 13 54 95 4 | 2
emr uuuuu | 16 1 187 98 -4 | 34 37
| 32 26 128 101 17 | 1
esa uuuuu | 14 7 -46 121 3 | 14 19
| 3 6 29 54 2 | 2
gfz uuuuu | -41 -3 85 -262 3 | 26 28
| 15 10 145 149 3 | 2
grg uuuuu | -5 -1 22 -57 -4 | 4 12
| 19 16 47 79 3 | 2
igr xxxxx | 5 2 24 11 5 | 2 12
| 16 14 35 49 6 | 3
irf xxxxx | 1 -8 -8 -28 -2 | 2 13
| 7 9 29 38 3 | 2
jpl xxxxx | 48 -26 139 77 11 | 24 28
| 28 20 82 64 13 | 3
mit uuuuu | 7 11 -46 -71 -1 | 24 27
| 10 15 57 46 5 | 2
ngs uuuuu | 1 -18 -43 -44 5 | 13 18
| 37 22 141 157 7 | 3
sio uuuux | 24 0 -31 86 -5 | 52 53
| 17 15 76 94 5 | 3
Table 7.1958.0 GPS week: 1958 Day: 0 MJD: 57950.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -8 -10 34 69 1 | 15 19
emr uuuuu | -33 -42 389 241 11 | 34 37
esa uuuuu | 14 8 -33 83 0 | 15 19
gfz uuuuu | -39 -20 228 -341 3 | 26 28
grg uuuuu | -23 -25 -23 -23 -1 | 6 12
igr xxxxx | -19 11 -23 -20 16 | -1 12
irf xxxxx | 3 6 -70 15 -5 | 3 12
jpl xxxxx | 8 -32 20 24 38 | 23 27
mit uuuuu | -2 43 -158 -46 -3 | 26 28
ngs uuuuu | 34 8 -162 -33 -1 | 17 20
sio uuuux | 34 13 -102 161 -3 | 56 57
Table 7.1958.1 GPS week: 1958 Day: 1 MJD: 57951.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -20 9 76 181 1 | 16 19
emr uuuuu | 19 39 15 88 16 | 34 37
esa uuuuu | 15 6 -42 141 1 | 14 19
gfz uuuuu | -37 1 141 -322 -1 | 26 28
grg uuuuu | -16 -13 64 -91 -1 | 6 12
igr xxxxx | 5 19 48 11 10 | 1 12
irf xxxxx | -2 -17 17 -19 -7 | 3 12
jpl xxxxx | 37 2 141 -8 13 | 24 28
mit uuuuu | 5 3 -24 -70 -5 | 26 28
ngs uuuuu | 5 -20 -191 -110 -1 | 16 20
sio uuuux | 37 -16 27 177 -3 | 55 56
Table 7.1958.2 GPS week: 1958 Day: 2 MJD: 57952.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -24 15 -51 -11 0 | 13 18
emr uuuuu | 33 -6 79 205 10 | 32 35
esa uuuuu | 12 16 -3 46 0 | 12 17
gfz uuuuu | -60 -6 176 -395 4 | 24 26
grg uuuuu | -10 23 15 -61 0 | 3 11
igr xxxxx | 17 9 11 45 9 | -1 12
irf xxxxx | 0 -2 5 -24 -2 | 0 14
jpl xxxxx | 52 -6 73 123 12 | 21 25
mit uuuuu | 3 14 -43 -59 -5 | 23 26
ngs uuuuu | 39 -47 -133 171 -3 | 12 17
sio uuuux | 1 2 65 78 0 | 51 52
Table 7.1958.3 GPS week: 1958 Day: 3 MJD: 57953.500
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 | -2 -4 -35 77 6 | 13 18
emr uuuuu | 2 11 140 58 -26 | 34 37
esa uuuuu | 8 4 -71 77 6 | 13 18
gfz uuuuu | -63 -3 -97 -386 3 | 24 27
grg uuuuu | -5 -10 98 -20 -5 | 3 11
igr xxxxx | -14 -22 38 57 4 | 1 13
irf xxxxx | -12 -20 -13 -57 1 | 1 14
jpl xxxxx | 17 -56 214 17 3 | 23 27
mit uuuuu | -2 2 -64 -65 -2 | 23 26
ngs uuuuu | 36 11 83 136 5 | 11 15
sio uuuux | -1 -23 56 -24 -7 | 51 52
Table 7.1958.4 GPS week: 1958 Day: 4 MJD: 57954.500
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 | -13 2 -76 100 -6 | 13 18
emr uuuuu | -8 17 182 -62 -14 | 31 36
esa uuuuu | 16 4 -74 138 2 | 12 17
gfz uuuuu | -29 12 -67 -286 5 | 23 26
grg uuuuu | 35 4 28 51 -5 | 1 12
igr xxxxx | 21 10 -12 28 1 | 1 13
irf xxxxx | 6 -13 13 -41 -2 | -1 14
jpl xxxxx | 65 -21 244 141 5 | 22 27
mit uuuuu | 3 5 25 -101 -4 | 21 25
ngs uuuuu | -21 -22 160 -42 11 | 10 14
sio uuuux | 24 -4 -79 78 -11 | 48 50
Table 7.1958.5 GPS week: 1958 Day: 5 MJD: 57955.500
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 -5 27 268 1 | 16 18
emr uuuuu | 57 6 197 101 -7 | 34 38
esa uuuuu | 17 0 -77 193 4 | 16 19
gfz uuuuu | -36 4 -31 -83 -1 | 27 29
grg uuuuu | -8 12 7 -205 -8 | 3 11
igr xxxxx | 7 -3 26 -85 -1 | 5 10
irf xxxxx | 4 -6 -4 -90 -1 | 2 13
jpl xxxxx | 80 -38 192 110 8 | 26 29
mit uuuuu | 16 3 -9 -150 4 | 24 27
ngs uuuuu | -38 -18 66 -156 13 | 14 18
sio uuuux | 34 16 -88 -49 3 | 50 51
Table 7.1958.6 GPS week: 1958 Day: 6 MJD: 57956.500
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 | -2 25 7 28 6 | 16 20
emr uuuuu | 45 -15 306 54 -20 | 35 39
esa uuuuu | 14 14 -23 169 4 | 17 22
gfz uuuuu | -25 -6 243 -21 6 | 29 31
grg uuuuu | -6 5 -37 -47 -6 | 4 12
igr xxxxx | 19 -9 77 39 -1 | 6 13
irf xxxxx | 7 -2 -2 18 1 | 3 14
jpl xxxxx | 75 -30 86 135 1 | 29 33
mit uuuuu | 25 7 -46 -3 7 | 25 28
ngs uuuuu | -49 -38 -126 -273 8 | 15 21
sio uuuux | 36 9 -93 182 -11 | 51 52
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