[IGSREPORT-25437] Wk 1959 IGS Final Orbits
acc
acc at igs.org
Fri Aug 11 13:25:41 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1959 (Jul 23, 2017 - Jul 29, 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:
igs1959[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1959[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1959[0-6].cls IGS GPS clock combination summary report.
igs19597.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19597.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 | ABMF TIXI ABMF TIXI
0 | EMR | HERS ALBH CHUR DARW DRAO FAIR HARB HERS HOB2 KERG
0 | EMR | MAS1 MCM4 NNOR QAQ1 SFER STJO TIDB WHIT YAR2 YELL
0 | GFZ | GODE MAL2 POHN AUCK GODE POHN
0 | GRG | 13 21 25 13 21 25 FAA1 LPGS MAL2 PIE1 SYOG TUVA FAA1
0 | GRG | LPGS PIE1 SYOG
0 | MIT | RBAY
1 | EMR | HERS ALBH HERS KERG MAS1 SFER TWTF
1 | ESA | NNOR NTUS NNOR
1 | GFZ | FAA1 GODE POHN FAA1 GODE POHN TRO1
1 | GRG | 11 21 11 21 GLSV MAL2 MAW1 RABT SYOG TRO1 FAA1 GLSV
1 | GRG | MAW1 NNOR RABT SYOG TRO1
1 | JPL | INVK INVK
1 | MIT | INVK INVK
2 | COD | SYOG TIXI BRFT SYOG TIXI
2 | EMR | ALBH HERS KERG MAS1 NIST SFER TWTF
2 | GFZ | GODE POHN GODE POHN TRO1
2 | GRG | GLSV MAL2 SYOG TRO1 BRST GLSV MAL2 SYOG TRO1
3 | COD | DUBO FAA1 TIXI FAA1 TIXI
3 | EMR | MAS1 NIST SFER
3 | ESA | FAA1 MAL2 FAA1 MAL2
3 | GFZ | ABMF GODE MAL2 POHN ABMF DUBO GODE MAL2 POHN TRO1
3 | GRG | 13 13 DUBO GLSV LHAZ SYOG TRO1 DUBO GLSV LHAZ SYOG
3 | GRG | TRO1
4 | COD | ABMF CHTI GODE TIXI ABMF CHTI GODE TIXI
4 | EMR | DAEJ DAEJ HERS MAS1 SFER
4 | ESA | FAA1 FAA1
4 | GFZ | AUCK HERS POHN TRO1 WTZR DRAO HERS POHN TRO1 WTZR
4 | GRG | GLSV LHAZ PIE1 SYOG TRO1 ZIM2 GLSV LHAZ MAL2 PIE1
4 | GRG | SYOG TRO1 ZIM2
4 | MIT | BOR1 GODZ INEG BOR1 GODZ INEG
5 | COD | CEDU SCUB TIXI AUCK CEDU SCUB TIXI
5 | EMR | SFER
5 | ESA | CHTI MAL2 CHTI MAL2
5 | GFZ | GODE POHN SYOG CHTI GODE POHN
5 | GRG | 21 21 GLSV MAL2 MAW1 SYOG TRO1 GLSV MAL2 MAW1 TRO1
6 | COD | TIXI TIXI
6 | ESA | 22 MAL2 REUN SAVO MAL2 REUN SAVO
6 | GFZ | FAA1 SYOG FAA1 PIE1 SYOG THU2
6 | GRG | ADIS FAA1 GLSV REUN SEYG SYOG ADIS FAA1 GLSV NKLG
6 | GRG | REUN SEYG SYOG
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. 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 G29 | | | | | | 4 | 4 |
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 | .4 .1 1.3 18 12 -12 -.59
EMR | 0 | 1.8 -.6 -9.9 -25 15 24 -.19
ESA | 0 | -.5 -.5 -.5 -4 4 -10 -.58
GFZ | 0 | .9 .5 .9 10 -31 -15 -.54
GRG | 0 | -2.2 2.5 -26.7 69 -35 54 -.35
JPL | 0 | 6.4 -1.9 -8.6 -9 -34 32 .06
MIT | 0 | -6.5 -4.8 -2.5 -13 8 5 -.16
NGS | 0 | -1.9 -7.7 -3.0 32 1 -5 -.18
SIO | 0 | -8.6 -1.6 -17.3 -10 -30 -10 -.22
COD | 1 | .5 .1 1.0 1 8 -13 -.63
EMR | 1 | 2.5 1.7 -5.5 -30 14 18 -.04
ESA | 1 | -1.5 -.1 -1.3 -11 -7 6 -.66
GFZ | 1 | .7 .3 1.1 -8 -26 -4 -.53
GRG | 1 | -.3 -3.9 -6.2 89 -47 70 -.25
JPL | 1 | 7.4 -1.3 -6.0 -43 -71 94 .12
MIT | 1 | -4.7 -5.7 .0 -25 10 -5 -.32
NGS | 1 | 2.6 -6.2 1.4 15 -27 29 -.16
SIO | 1 | -9.2 1.8 -21.6 -16 -30 -10 -.29
COD | 2 | .6 .4 1.2 5 2 -17 -.62
EMR | 2 | -1.1 -8.1 -8.2 -15 12 8 -.14
ESA | 2 | -1.8 .3 -1.0 -16 -9 9 -.59
GFZ | 2 | .9 .2 1.1 -7 -32 -2 -.52
GRG | 2 | -.2 1.6 -14.1 59 -40 26 -.37
JPL | 2 | -.0 -2.9 -12.6 14 -52 68 .22
MIT | 2 | -4.1 -10.0 -2.4 -22 14 -12 -.35
NGS | 2 | -4.7 -15.5 -12.2 23 -9 0 -.38
SIO | 2 | -3.0 -3.1 -20.3 -29 -2 5 -.44
COD | 3 | .7 .3 1.1 10 4 -14 -.64
EMR | 3 | 1.5 -7.5 -9.4 -13 14 20 -.09
ESA | 3 | -1.4 .2 -.9 -12 -15 2 -.72
GFZ | 3 | 1.0 .3 1.0 -1 -32 -1 -.53
GRG | 3 | -1.3 -2.8 10.3 63 -33 6 -.53
JPL | 3 | -.8 -2.3 -9.3 -17 -71 71 .21
MIT | 3 | -4.5 -7.1 .4 -7 21 12 -.37
NGS | 3 | -6.8 -14.4 -2.0 16 -24 -16 -.34
SIO | 3 | -3.2 -2.9 -23.1 -17 -2 41 -.43
COD | 4 | .4 .1 1.1 6 15 -11 -.50
EMR | 4 | -.1 -11.8 -11.7 -40 39 33 -.27
ESA | 4 | -.7 -.5 -.8 -13 -9 6 -.64
GFZ | 4 | .8 .5 .7 1 -40 -3 -.51
GRG | 4 | 1.6 -1.0 .9 52 -47 57 -.61
JPL | 4 | -7.4 -1.3 -.8 -23 -96 93 .10
MIT | 4 | -7.1 -5.9 4.7 -16 20 6 -.34
NGS | 4 | -8.0 -9.7 -5.2 27 -22 -13 -.41
SIO | 4 | -9.0 -.7 -21.1 -16 -17 8 -.31
COD | 5 | .1 .2 .6 5 13 -1 -.41
EMR | 5 | -3.6 -8.2 -2.0 -43 57 24 -.13
ESA | 5 | -.6 -.3 -.3 -4 -5 2 -.55
GFZ | 5 | .4 .2 .5 -5 -29 0 -.46
GRG | 5 | -4.9 -5.4 7.5 33 -28 54 -.28
JPL | 5 | 1.6 -1.7 -6.4 -41 -36 31 .18
MIT | 5 | -4.8 -6.2 5.5 6 21 1 -.34
NGS | 5 | -4.3 -10.4 -2.3 29 -13 6 -.38
SIO | 5 | -7.8 -3.0 -21.1 -14 -26 -17 -.27
COD | 6 | .2 .2 .7 8 9 -7 -.49
EMR | 6 | -7.1 -12.4 -3.0 -34 35 38 -.32
ESA | 6 | -.1 .2 .3 9 -7 3 -.59
GFZ | 6 | .6 .5 .9 11 -31 -13 -.47
GRG | 6 | 3.8 2.9 -4.5 52 -27 53 -.37
JPL | 6 | -3.2 -9.9 -1.4 -42 -82 27 .28
MIT | 6 | -5.0 -6.7 6.1 -1 22 -4 -.18
NGS | 6 | -4.9 -12.0 -5.0 52 -20 4 -.26
SIO | 6 | -8.5 -5.2 -16.8 2 -22 0 -.30
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 1.1959.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1959.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 2.1959.[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 3.1959.[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 5.1959.0-6). 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 1959 summary. (Jul 23, 2017 - Jul 29, 2017)
Table 1.1959.a GPS week: 1959 MJD: 57957.000-57963.000
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 274| 1 0 5 0 3 -10 .03 10 9 | -620 -227 11 109
| 0 0 2 11 11 11 .05 | 179 273
emr 84| 0 -1 -5 -2 5 26 .19 17 16 | 22311 -560 21 129
| 2 2 1 12 14 14 .04 | 56549 508
esa 149| 0 0 -4 -3 3 -5 -.02 9 9 | -186 -1969 8 170
| 0 0 1 11 7 9 .02 | 777 1664
gfz 195| -1 1 0 -16 2 -1 .14 11 10 | 18 -241 12 120
| 0 0 1 7 9 13 .02 | 173 400
grg 108| 0 0 -1 -21 -6 29 -.35 17 16 | 154 -137 13 174
| 0 0 8 17 16 35 .05 | 121 165
igr n/a| 0 0 3 -9 -1 -10 .03 4 4 | -5275 -823 12 113
| 0 0 0 12 12 11 .02 | 2313 715
jpl 80| -1 0 -2 -1 -17 42 .22 13 13 | 1048 -450 42 229
| 1 1 0 14 42 7 .03 | 1697 473
mit 348| 1 -1 3 -7 -16 6 .00 13 11 | -416 -117 39 324
| 0 0 1 9 23 5 .01 | 428 183
ngs 215| 0 0 0 17 9 -4 .03 8 8 | -631 -166 949 2247
| 0 0 2 8 13 12 .07 | 140 249
sio 345| 0 0 0 2 -14 -14 -.10 11 11 | --- --- --- ---
| 0 1 1 9 21 27 .01 | --- ---
Table 1.1959.b GPS week : 1959 MJD: 57957.000-57963.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 5 4 5 4 4 4 |
2 | 5 4 4 8 4 4 5 |
3 | 4 3 3 3 3 3 3 |
4 | 0 0 0 0 0 0 0 |
5 | 5 4 5 4 5 4 4 |
6 | 5 5 4 4 4 5 4 |
7 | 5 5 5 5 4 5 5 |
8 | 4 4 4 3 3 3 3 |
9 | 3 3 3 3 3 3 3 |
10 | 3 4 3 3 3 3 4 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 6 6 |
13 | 4 4 4 4 4 4 4 |
14 | 5 4 4 4 4 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 5 5 6 6 6 6 6 |
17 | 5 5 4 5 5 5 5 |
18 | 6 6 7 6 7 6 6 |
19 | 5 5 5 5 5 6 6 |
20 | 5 5 5 5 5 5 4 |
21 | 5 5 4 4 5 4 5 |
22 | 5 5 5 5 5 5 5 |
23 | 4 4 4 4 4 4 4 |
24 | 3 3 3 3 3 3 3 |
25 | 4 4 4 5 4 4 4 |
26 | 5 5 5 5 6 5 6 |
27 | 3 4 3 4 3 4 4 |
28 | 4 4 4 4 4 4 5 |
29 | 5 5 5 5 5 5 5 |
30 | 4 3 3 4 3 3 3 |
31 | 6 6 6 6 6 6 6 |
32 | 5 5 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 2.1959.0 GPS week: 1959 Day: 0 MJD: 57957.000
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 273| 0 0 6 6 6 -14 -.03 10 9 | -781 7 12 110
emr 84| 2 0 -4 -4 2 20 .16 18 18 | 150522 -399 23 128
esa 150| 0 1 -2 -5 7 -3 -.04 9 9 | -872 -189 8 162
gfz 199| -2 1 1 -19 -12 -14 .14 11 9 | -172 -66 11 107
grg 109| 1 0 -16 -27 -18 56 -.36 17 17 | 116 58 14 192
igr n/a| -1 0 3 -9 -17 -19 .06 4 4 | -2243 -633 12 67
jpl 80| 0 0 -3 -12 -29 48 .21 13 13 | 2934 -138 42 227
mit 349| 2 0 4 -16 -24 10 .01 14 12 | -215 -36 39 336
ngs 220| 0 0 0 23 29 2 .10 8 7 | -785 23 734 2263
sio 348| 0 -2 0 -3 -22 -7 -.09 11 11 | --- --- --- ---
Table 2.1959.1 GPS week: 1959 Day: 1 MJD: 57958.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 276| 1 0 7 -23 10 -14 -.01 11 9 | -811 -91 12 116
emr 85| 2 2 -4 -4 14 9 .18 16 16 | 3079 -1256 25 132
esa 150| 0 0 -6 -15 16 -18 -.03 10 10 | 1061 -4158 8 181
gfz 195| -2 1 -1 -17 13 -10 .15 10 9 | 52 -187 12 123
grg 109| 0 0 -3 10 -22 89 -.36 17 17 | 264 -230 12 146
igr n/a| 0 0 2 -18 17 -21 .04 4 4 | -2864 -1437 14 348
jpl 80| 0 1 -2 1 20 40 .26 12 12 | 2897 -1018 39 230
mit 349| 0 -1 2 0 -46 13 .03 13 11 | -283 -10 41 288
ngs 217| 0 0 4 20 21 -13 .07 8 7 | -750 -189 696 2123
sio 341| 0 -1 -1 15 -36 -5 -.10 11 12 | --- --- --- ---
Table 2.1959.2 GPS week: 1959 Day: 2 MJD: 57959.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 275| 1 1 7 -2 8 -27 .00 10 9 | -579 -253 11 115
emr 85| 0 -3 -2 18 -7 24 .17 15 15 | 1770 -420 23 153
esa 150| 0 0 -4 1 -3 4 -.02 8 8 | -951 462 6 145
gfz 195| -1 1 0 -10 3 -5 .13 11 9 | 13 73 12 130
grg 110| 0 0 -6 -14 -24 19 -.44 17 17 | 217 -103 13 190
igr n/a| 0 0 4 8 6 -19 .04 4 4 | -4008 -1005 12 72
jpl 80| 0 2 -1 17 -26 51 .22 11 11 | 2027 -396 38 237
mit 348| 2 -1 2 -16 1 1 -.00 12 11 | -127 -53 39 314
ngs 217| 0 0 -3 11 8 9 .09 9 8 | -580 -196 1133 2147
sio 341| 0 -1 3 -5 -5 -3 -.10 12 12 | --- --- --- ---
Table 2.1959.3 GPS week: 1959 Day: 3 MJD: 57960.000
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 272| 0 0 1 10 -2 -7 .05 10 9 | -704 78 11 106
emr 85| 2 -2 -4 -6 -3 11 .13 20 17 | 1368 -1001 23 131
esa 150| 0 2 -7 -20 -5 -15 -.02 10 10 | 19 -2839 10 171
gfz 195| 0 2 0 -9 8 -9 .13 10 9 | 209 -554 14 126
grg 110| 0 0 8 -27 16 40 -.37 17 17 | 220 -263 14 166
igr n/a| 0 1 2 1 -8 -14 .04 4 4 | -5210 -1868 13 88
jpl 80| -1 0 -3 -5 59 29 .18 14 14 | 1550 -997 45 225
mit 348| 2 -2 2 -7 0 0 -.01 12 10 | -1147 -63 35 343
ngs 215| -1 0 1 17 -2 -20 .02 8 7 | -611 -83 1202 2537
sio 344| 0 0 0 4 3 29 -.10 12 11 | --- --- --- ---
Table 2.1959.4 GPS week: 1959 Day: 4 MJD: 57961.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 274| 1 0 5 6 19 -12 .05 10 9 | -539 -385 12 106
emr 85| 0 -2 -6 -18 21 36 .22 16 16 | -276 159 21 130
esa 150| 0 1 -4 1 7 -11 -.03 8 9 | -701 -1582 8 146
gfz 194| -1 2 0 -5 11 8 .15 11 10 | -115 -25 12 115
grg 110| 0 0 2 -15 1 6 -.34 15 14 | -49 33 15 173
igr n/a| 0 1 4 -6 8 -5 .02 4 4 | -7274 -180 12 70
jpl 80| -4 0 -2 17 -49 44 .24 13 13 | -617 0 42 220
mit 348| 0 -1 2 -6 -35 9 .00 13 11 | -325 -156 37 334
ngs 214| -1 0 0 21 -3 -8 .02 9 8 | -667 96 738 2034
sio 348| 1 0 -1 -8 -38 -16 -.10 11 10 | --- --- --- ---
Table 2.1959.5 GPS week: 1959 Day: 5 MJD: 57962.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 274| 1 0 3 3 1 8 .03 9 9 | -648 -217 11 100
emr 85| -2 -1 -6 -10 25 46 .24 16 16 | -20 -893 16 117
esa 149| -1 0 -4 -1 6 -3 .02 9 9 | -471 -2162 8 160
gfz 195| -3 1 1 -20 -8 23 .13 12 11 | 276 -1005 12 130
grg 106| 1 0 5 -38 -11 1 -.29 18 16 | 44 -63 15 168
igr n/a| 0 0 2 -11 -3 6 .00 4 4 | -7471 -875 13 85
jpl 80| -2 0 -3 -20 -32 40 .23 13 13 | -596 -738 44 230
mit 349| 1 -2 1 8 18 7 .00 12 10 | -866 13 40 307
ngs 212| 0 0 1 2 -2 -14 -.05 8 7 | -668 -142 1400 2522
sio 342| 1 -1 -1 15 -21 -43 -.09 12 10 | --- --- --- ---
Table 2.1959.6 GPS week: 1959 Day: 6 MJD: 57963.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 274| 1 0 7 0 -16 -3 .12 11 10 | -280 -734 13 113
emr 85| -5 -2 -5 9 -11 39 .20 16 15 | -263 -113 17 112
esa 150| 0 0 -3 12 0 8 .00 8 8 | 609 -3315 11 227
gfz 193| -2 1 0 -28 3 0 .17 11 10 | -134 77 12 111
grg 103| 2 1 -1 -40 12 -10 -.31 19 17 | 271 -394 14 184
igr n/a| 0 0 2 -30 -12 1 .02 4 4 | -7860 232 12 67
jpl 80| 0 0 -3 -5 -62 38 .21 14 14 | -856 133 45 240
mit 349| 1 -1 5 -18 -30 0 -.01 13 11 | 47 -516 47 350
ngs 213| 0 0 -1 28 15 10 -.07 8 8 | -356 -675 743 2107
sio 352| 0 0 -1 -2 18 -52 -.08 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 3.1959.0 GPS week: 1959 Day: 0 MJD: 57957.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 18 9 7 19 5 13 9 6 8 3 | 32 36 36 30 33 30 31 32 31 33 32
2E | 18 18 10 9 17 7 14 15 10 13 5 | 26 23 26 29 25 26 26 30 28 29 25
3 | 7 16 8 6 14 3 10 13 4 9 3 | 22 32 27 24 23 23 29 27 24 28 24
X4M | 4 --- --- --- --- 48 20 --- --- --- 0 | 22 --- --- --- --- 37 26 --- --- --- 22
5M | 9 12 12 13 18 3 10 13 9 14 4 | 29 36 33 32 39 30 37 28 30 28 30
6E | 14 19 10 9 13 2 11 14 7 11 4 | 37 40 40 38 34 37 37 37 38 37 37
7 | 11 15 10 12 20 4 10 12 8 15 4 | 29 31 29 31 31 28 31 29 29 26 28
8M | 8 16 7 10 17 5 10 8 8 10 3 | 23 28 24 23 27 22 27 21 23 26 23
9 | 6 16 9 7 11 3 13 10 6 6 3 | 19 33 20 22 14 22 32 24 23 22 21
10 | 6 11 7 9 14 4 8 8 4 7 3 | 18 24 22 22 22 20 22 19 19 23 20
11M | 7 15 10 6 15 5 9 19 7 10 4 | 31 34 33 34 28 32 36 35 32 30 31
12M | 7 28 8 10 15 3 22 14 8 7 4 | 37 32 35 42 35 38 34 41 42 41 38
13 | 10 13 10 8 11 3 11 10 6 15 4 | 17 21 18 24 18 19 24 19 19 26 18
14 | 7 11 9 19 15 5 10 13 8 14 4 | 19 18 17 16 17 15 16 24 21 19 16
15 | 6 16 10 9 10 3 15 11 7 11 3 | 25 28 29 28 24 26 30 26 25 28 26
16M | 10 20 11 11 23 4 17 10 8 12 4 | 31 31 35 38 36 36 32 35 39 37 34
17M | 9 15 9 13 16 4 12 12 8 14 4 | 28 33 26 34 28 30 33 35 35 30 29
18 | 8 32 11 17 20 5 21 25 10 13 6 | 24 33 27 34 25 27 29 31 29 25 24
19M | 12 20 8 13 15 5 15 11 9 20 5 | 21 28 24 28 25 24 28 26 26 21 22
20M | 9 14 10 13 24 4 13 21 8 12 5 | 28 24 24 29 25 27 25 26 28 27 24
21E | 13 13 7 15 21 4 9 12 8 8 4 | 23 23 25 31 25 24 24 24 22 24 23
22 | 11 15 11 10 18 3 13 15 9 16 4 | 19 24 18 26 22 21 21 28 24 19 19
23M | 7 25 8 6 9 3 15 13 7 9 3 | 16 17 17 21 15 17 16 21 23 18 17
24M | 6 15 6 8 15 4 10 11 6 4 3 | 23 27 22 24 28 24 25 25 23 22 23
25M | 8 16 9 6 19 5 13 14 10 8 4 | 93 92 91 91 93 91 92 95 90 93 91
26M | 16 19 9 12 17 3 11 7 8 8 4 | 79 66 65 71 73 69 67 72 67 69 69
27M | 7 11 7 5 14 3 9 9 6 9 3 | 24 25 24 24 23 22 25 23 21 24 22
28M | 11 15 6 8 11 3 12 8 10 9 3 | 24 25 26 26 27 25 29 26 27 25 25
29M | 9 24 8 11 11 5 15 23 9 11 4 | 35 38 32 32 35 33 37 30 29 30 31
30 | 9 16 6 8 20 4 11 7 8 7 3 | 23 30 28 26 30 26 30 24 30 25 26
31M | 11 18 9 15 25 5 15 31 10 13 6 | 20 26 17 27 29 21 26 26 21 16 17
32 | 6 15 8 14 15 4 13 17 6 15 4 | 18 30 19 19 18 18 30 23 22 29 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 18 9 11 17 4 13 14 8 11 |T 28 31 29 31 29 29 31 31 30 30 28
WRMS | 9 18 9 9 17 4 13 12 7 11 |NE 21 27 23 24 22 22 26 24 24 24 21
MEDI | 8 16 9 10 15 4 12 12 8 11 |MD 24 30 26 28 27 26 29 26 27 26 24
Table 3.1959.1 GPS week: 1959 Day: 1 MJD: 57958.000
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 14 10 8 29 4 11 9 5 7 4 | 33 36 35 35 35 32 33 33 33 31 32
2E | 16 14 7 8 15 4 10 10 9 11 4 | 22 29 25 25 25 23 23 26 24 28 24
3 | 8 15 7 6 14 4 8 7 5 8 3 | 19 28 21 21 17 18 27 21 20 21 19
X4 | 4 --- --- --- --- 67 27 --- --- --- 0 | 23 --- --- --- --- 38 26 --- --- --- 23
5 | 8 12 13 10 16 4 8 12 8 10 4 | 24 27 26 24 24 23 28 23 23 21 22
6E | 19 19 11 11 22 4 15 9 4 10 5 | 34 40 39 34 30 34 39 35 37 35 34
7 | 10 15 8 9 19 4 11 13 8 16 4 | 24 27 23 27 21 23 28 27 26 22 23
8 | 7 13 5 10 17 3 9 8 8 10 3 | 18 20 19 20 20 18 23 18 22 19 18
9 | 7 15 7 9 9 4 12 9 5 8 3 | 19 33 20 20 15 20 33 23 23 22 20
10 | 9 10 8 9 15 5 7 9 7 12 3 | 19 24 20 24 19 19 23 20 23 25 19
11 | 6 13 9 9 16 3 7 12 6 7 3 | 26 28 29 29 24 26 31 28 28 23 26
12 | 7 24 7 8 21 4 18 13 8 9 4 | 36 34 37 41 34 36 33 40 39 41 37
13 | 10 12 13 9 10 4 9 8 7 12 4 | 14 17 16 25 14 16 19 16 20 23 17
14 | 8 10 10 16 10 2 9 11 7 10 4 | 14 13 14 16 13 13 16 19 17 13 12
15 | 8 16 13 9 8 4 14 10 6 10 3 | 17 17 20 23 16 19 19 20 21 21 18
16 | 10 21 8 12 23 5 15 10 10 14 5 | 29 26 33 36 23 34 30 32 37 33 31
17 | 10 14 11 12 19 5 9 13 9 15 4 | 20 27 20 25 20 22 28 29 29 20 22
18 | 8 26 13 13 18 5 19 25 10 12 5 | 26 33 29 32 31 30 33 32 33 29 27
19 | 13 17 9 15 15 6 14 11 8 20 5 | 18 25 20 25 19 21 28 24 23 20 19
20 | 10 14 13 11 19 5 12 21 9 11 5 | 26 22 19 25 24 23 24 20 23 20 20
21E | 14 14 8 13 27 4 10 10 7 8 4 | 19 21 21 26 24 21 24 24 23 23 19
22 | 11 16 11 10 14 4 10 12 8 16 4 | 18 22 17 27 18 22 24 24 25 20 19
23 | 7 25 9 7 10 4 13 11 7 10 4 | 16 16 18 17 12 15 16 18 19 17 15
24 | 9 11 7 6 11 4 11 7 8 4 3 | 22 27 24 25 18 23 29 24 26 23 23
25 | 8 17 10 7 15 5 12 10 7 7 3 | 65 68 66 63 65 65 67 66 64 65 64
26E | 23 19 11 12 16 5 9 6 8 8 5 | 94 91 85 88 89 87 89 85 90 88 87
27 | 11 12 6 10 13 2 10 7 7 9 3 | 21 20 20 20 17 18 24 19 21 20 18
28 | 10 15 8 9 15 3 8 8 9 10 3 | 23 24 23 22 22 22 26 24 23 21 21
29 | 11 23 9 11 11 6 16 14 11 12 4 | 60 63 61 59 57 58 62 61 58 59 59
30 | 5 15 5 6 19 3 13 7 6 5 3 | 26 31 27 25 26 24 33 26 27 24 25
31 | 12 16 12 15 21 6 14 30 12 11 6 | 19 24 17 26 17 20 26 26 23 16 16
32 | 7 15 13 13 11 4 16 15 8 19 5 | 19 31 21 21 18 20 32 24 23 32 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 10 10 17 4 12 13 8 11 |T 26 30 27 29 26 27 31 29 29 28 26
WRMS | 9 16 10 9 17 4 12 11 7 12 |NE 19 25 20 23 18 20 26 22 23 22 19
MEDI | 9 15 9 10 15 4 11 10 8 10 |MD 22 27 21 25 21 22 28 24 23 23 21
Table 3.1959.2 GPS week: 1959 Day: 2 MJD: 57959.000
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 9 8 27 4 11 8 8 9 4 | 21 28 26 24 24 23 24 24 22 26 23
2E | 14 13 6 9 13 4 10 10 10 8 4 | 23 26 24 25 24 23 23 25 27 24 23
3 | 8 12 5 6 15 4 8 5 9 9 3 | 23 30 26 24 20 22 26 24 22 23 23
X4 | 4 --- --- --- --- 52 17 --- --- --- 0 | 24 --- --- --- --- 32 24 --- --- --- 24
5 | 10 10 11 13 16 5 9 12 8 15 4 | 25 30 26 23 28 21 28 22 24 19 22
6E | 12 13 9 9 21 3 11 8 8 7 4 | 24 28 28 24 17 22 25 25 25 25 23
7 | 10 12 8 12 23 4 11 13 11 14 4 | 23 26 22 26 23 24 27 28 28 23 23
8 | 7 10 5 10 17 3 9 7 9 9 3 | 22 21 21 23 18 21 22 22 23 19 20
9 | 6 13 7 9 11 3 12 6 7 8 3 | 16 31 19 18 12 19 30 20 21 22 19
10 | 7 11 6 7 13 4 9 9 6 9 3 | 18 24 22 23 20 20 22 19 22 23 20
11 | 6 10 9 8 21 3 8 12 9 8 3 | 24 27 27 25 26 26 27 26 24 23 24
12 | 9 25 7 10 20 5 20 12 9 8 4 | 43 41 44 46 39 43 39 43 46 44 43
13 | 6 11 10 9 8 3 7 7 8 11 3 | 16 20 16 23 13 16 19 18 16 21 16
14 | 10 9 9 14 15 4 7 13 9 14 4 | 15 13 16 11 18 12 11 18 18 14 13
15 | 6 15 10 11 10 4 13 12 7 12 4 | 21 23 19 23 19 19 22 20 22 21 19
16 | 13 24 8 15 23 5 16 10 11 14 5 | 23 23 28 30 20 25 25 26 29 24 24
17 | 8 12 8 11 17 4 10 12 9 16 4 | 19 26 18 24 17 22 25 27 24 19 20
18 | 9 25 11 19 23 6 17 25 14 16 6 | 18 20 18 26 23 16 20 23 18 18 13
19 | 9 15 8 12 17 5 13 11 9 21 4 | 16 24 17 21 16 19 24 22 20 19 16
20 | 8 13 10 11 20 5 10 20 11 11 4 | 30 31 27 30 24 26 29 28 26 27 26
21E | 13 13 7 11 20 3 9 9 9 7 4 | 16 22 19 26 20 19 20 21 22 20 18
22 | 11 12 9 10 19 5 9 12 11 18 4 | 19 19 18 22 16 19 20 22 21 20 17
23 | 7 21 8 8 11 4 13 9 9 9 3 | 15 13 15 17 14 16 14 18 19 17 15
24 | 7 13 7 6 11 4 13 11 5 5 3 | 20 27 20 20 20 20 25 22 22 20 20
25 | 7 13 8 8 14 6 12 13 10 9 3 | 106 107 108 107 109 106 106 109 107 108 107
26E | 22 13 9 15 21 4 11 6 8 8 5 | 43 39 36 40 37 37 38 38 36 37 37
27 | 9 12 6 7 14 4 8 8 8 8 3 | 19 20 19 17 14 18 20 20 22 19 18
28 | 12 13 6 11 18 4 10 9 10 9 4 | 23 24 22 21 22 20 22 21 20 21 20
29 | 9 24 8 11 13 4 15 11 11 12 4 | 81 83 79 76 78 80 79 80 77 78 79
30 | 7 12 5 6 16 3 12 6 6 8 3 | 22 24 24 22 23 21 24 22 22 22 22
31 | 12 16 10 13 22 6 12 30 13 15 6 | 18 24 17 22 21 18 23 24 23 15 15
32 | 7 15 8 9 13 4 10 13 9 14 4 | 16 29 16 14 16 17 28 21 23 26 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 15 8 11 17 4 11 12 9 12 |T 26 29 27 28 25 26 28 28 28 27 25
WRMS | 9 15 8 9 17 4 11 11 8 12 |NE 18 23 19 21 18 18 22 21 21 21 18
MEDI | 8 13 8 10 17 4 11 11 9 9 |MD 21 26 22 23 20 21 24 22 22 22 20
Table 3.1959.3 GPS week: 1959 Day: 3 MJD: 57960.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 16 10 8 31 4 13 8 6 9 4 | 27 27 28 25 30 23 25 25 24 27 24
2E | 20 53 24 10 14 6 13 14 11 8 7 | 28 63 45 31 26 30 29 27 30 29 30
3 | 9 15 6 5 14 4 14 5 6 9 3 | 20 28 23 22 17 19 26 19 21 24 20
X4 | 1 --- --- --- --- 34 22 --- --- --- 0 | 23 --- --- --- --- 39 20 --- --- --- 23
5 | 9 14 13 9 15 4 8 11 9 14 4 | 28 32 28 24 24 23 29 22 23 20 23
6E | 8 16 10 7 22 3 14 9 8 9 4 | 25 29 27 23 21 23 25 25 24 25 23
7 | 14 14 11 8 13 5 11 10 11 17 4 | 26 28 24 23 26 21 27 23 22 19 21
8 | 6 12 5 12 13 3 27 7 6 8 3 | 19 20 17 22 19 18 31 18 19 17 17
9 | 8 17 8 7 10 4 13 5 6 11 3 | 21 31 18 20 15 19 33 20 20 26 20
10 | 6 14 7 7 13 2 9 7 5 9 3 | 20 25 22 21 19 19 25 18 21 25 20
11 | 9 11 10 8 19 4 11 12 6 9 3 | 22 24 24 22 24 22 26 24 21 19 21
12 | 10 27 8 9 19 4 19 13 11 11 5 | 46 47 46 47 46 46 45 45 46 45 45
13 | 6 8 11 11 10 4 10 8 7 12 3 | 16 16 14 27 15 16 19 18 18 23 17
14 | 7 10 10 9 10 4 9 14 9 12 3 | 15 14 14 11 18 12 14 21 16 14 13
15 | 5 14 12 7 8 3 14 12 6 11 3 | 22 19 21 22 15 18 21 19 21 22 19
16 | 9 35 9 14 24 5 17 11 7 15 5 | 24 28 26 27 25 26 24 24 28 23 23
17 | 6 18 11 11 16 3 15 13 8 15 4 | 19 27 18 22 21 20 25 23 22 17 19
18 | 10 24 12 17 18 6 18 24 10 13 6 | 18 24 19 26 22 19 26 26 23 20 17
19 | 8 18 10 10 17 4 20 12 10 21 4 | 15 21 17 21 18 17 24 20 18 17 15
20 | 8 13 13 9 18 4 14 19 10 11 4 | 23 21 18 21 20 19 23 22 20 23 18
21E | 8 16 8 9 23 3 10 9 7 9 4 | 30 33 35 35 34 32 33 34 34 34 32
22 | 12 14 10 10 18 4 15 12 9 16 4 | 18 20 16 23 18 18 21 21 20 18 16
23 | 9 24 9 6 9 5 11 7 7 9 3 | 14 16 15 15 17 13 14 16 15 16 13
24 | 11 14 8 4 12 3 10 9 6 7 3 | 21 25 20 20 18 19 20 20 20 22 19
25E | 16 15 10 8 22 7 13 11 6 6 4 | 114 104 108 106 104 108 108 107 106 109 108
26E | 18 18 11 14 24 5 9 7 7 8 5 | 37 34 31 33 37 32 31 31 31 30 31
27 | 9 12 6 10 16 5 10 6 7 7 3 | 20 20 20 19 20 18 21 18 19 18 18
28 | 9 17 6 10 16 4 13 7 6 10 3 | 27 33 25 24 36 26 30 26 25 26 25
29 | 8 25 11 9 16 5 15 12 10 14 4 | 96 101 94 95 95 93 98 99 95 94 95
30 | 6 12 8 10 14 3 11 6 8 14 3 | 24 28 25 24 27 23 29 24 26 29 24
31 | 11 16 11 11 15 6 14 30 11 12 5 | 18 23 17 22 16 18 23 24 19 16 14
32 | 7 14 9 8 10 4 13 12 9 15 4 | 15 28 15 23 17 17 30 19 15 28 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 10 10 17 4 14 12 8 12 |T 27 31 28 28 27 27 30 28 27 28 26
WRMS | 9 17 10 9 17 4 14 10 7 11 |NE 19 23 19 22 19 18 24 20 20 22 18
MEDI | 8 15 10 9 16 4 13 11 7 11 |MD 22 27 22 23 21 19 25 23 21 23 20
Table 3.1959.4 GPS week: 1959 Day: 4 MJD: 57961.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1E | 8 14 10 6 16 4 13 10 7 9 3 | 24 27 27 25 24 24 26 26 26 28 25
2E | 13 9 6 12 8 5 14 10 8 10 3 | 18 23 21 21 18 18 21 23 24 24 20
3 | 7 11 7 6 11 4 13 5 6 6 2 | 20 29 24 21 20 19 26 20 21 23 21
X4 | 3 --- --- --- --- 28 30 --- --- --- 0 | 27 --- --- --- --- 26 20 --- --- --- 26
5 | 12 11 9 14 15 5 11 11 10 12 4 | 28 31 26 26 28 23 31 22 24 21 24
6E | 14 14 10 11 15 4 11 9 7 7 4 | 23 30 27 24 18 23 26 27 26 26 24
7 | 9 13 9 9 17 4 9 12 10 12 4 | 27 30 25 27 25 25 29 29 27 24 25
8 | 7 12 5 6 12 2 10 8 6 8 3 | 20 25 21 21 20 20 27 22 20 21 20
9 | 7 14 7 8 7 3 12 6 8 8 3 | 18 31 17 19 15 18 32 19 19 21 18
10 | 7 13 7 7 9 4 8 10 6 8 3 | 15 24 19 18 17 16 21 16 17 20 16
11 | 8 9 10 7 15 4 9 13 7 8 3 | 23 25 24 23 22 24 28 28 25 21 22
12 | 8 23 5 9 27 3 19 15 11 8 5 | 50 51 48 52 50 49 50 48 51 49 49
13 | 8 10 9 15 11 4 10 12 11 10 4 | 16 19 17 31 14 17 20 21 16 24 18
14 | 11 10 10 9 6 4 11 14 10 12 4 | 18 10 14 10 11 10 10 18 13 11 11
15 | 7 13 10 10 14 4 17 14 10 10 4 | 26 24 25 27 20 22 26 23 25 23 23
16 | 10 30 8 14 22 4 15 12 10 14 5 | 25 23 25 27 25 25 23 24 28 23 23
17 | 8 14 9 14 14 5 12 13 10 17 4 | 21 26 20 27 20 22 26 24 24 19 20
18 | 12 27 12 17 20 8 16 26 14 15 6 | 19 22 14 27 15 18 19 25 23 20 14
19 | 10 16 7 14 17 5 14 12 11 20 5 | 15 22 16 23 15 17 23 21 17 17 14
20 | 8 13 10 10 19 4 10 22 12 12 5 | 32 30 29 30 27 28 32 29 31 29 28
21E | 11 11 7 13 25 3 13 11 10 9 4 | 24 30 25 30 25 26 30 31 28 29 25
22 | 13 15 8 12 17 5 11 11 10 16 4 | 17 20 18 25 18 19 23 21 20 20 16
23 | 7 23 8 7 8 4 13 8 8 9 3 | 16 14 15 18 15 15 16 17 18 19 15
24 | 6 14 7 7 11 5 14 9 8 4 3 | 23 27 21 24 20 23 23 25 24 23 22
25E | 8 15 9 6 20 5 13 11 7 9 4 | 102 103 102 102 101 102 100 100 101 100 101
26E | 18 18 11 15 26 4 12 8 6 10 5 | 37 36 32 32 38 31 31 31 30 30 31
27 | 9 12 7 9 10 3 10 8 8 6 3 | 20 21 20 17 18 18 25 19 18 21 18
28 | 7 15 6 11 12 4 12 7 9 10 3 | 28 34 28 31 35 30 33 31 31 29 30
29 | 7 24 9 11 15 4 16 14 11 11 4 | 121 123 121 118 120 120 126 125 121 120 121
30 | 5 10 5 6 12 4 10 7 8 8 3 | 22 26 24 23 24 21 27 24 24 24 23
31 | 12 16 10 12 13 6 12 32 10 11 5 | 17 26 16 22 16 17 24 25 19 16 14
32 | 7 12 9 7 8 3 13 12 12 14 4 | 16 26 16 18 11 14 27 18 14 24 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 16 8 11 15 4 13 13 9 11 |T 28 31 28 30 27 27 31 30 29 29 27
WRMS | 9 16 9 10 14 4 13 11 8 10 |NE 19 23 19 22 17 18 23 21 19 21 18
MEDI | 8 14 9 10 14 4 12 11 10 10 |MD 22 26 24 25 20 22 26 24 24 23 22
Table 3.1959.5 GPS week: 1959 Day: 5 MJD: 57962.000
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 | 5 16 7 8 27 4 11 10 7 9 4 | 30 32 32 31 32 28 30 31 27 33 29
2E | 14 10 5 10 17 4 11 10 8 9 4 | 20 21 20 23 16 19 19 20 20 20 18
3 | 6 9 6 8 11 4 10 5 6 6 2 | 26 29 23 22 18 21 28 21 21 23 22
X4 | 2 --- --- --- --- 31 18 --- --- --- 0 | 19 --- --- --- --- 21 25 --- --- --- 19
5 | 10 11 9 12 11 5 10 9 8 12 3 | 24 25 22 24 18 21 27 20 20 20 20
6E | 12 14 10 12 26 3 11 10 8 8 4 | 31 35 33 32 32 30 32 31 31 32 31
7 | 11 14 8 12 18 5 9 13 11 16 4 | 28 32 25 31 22 27 30 32 30 31 27
8 | 7 12 7 8 10 3 10 7 6 11 3 | 20 27 22 20 21 20 25 21 23 23 21
9 | 6 13 8 8 11 4 11 8 8 9 3 | 18 31 20 23 15 18 31 18 15 25 19
10 | 6 12 6 10 13 4 9 10 5 9 3 | 20 29 22 21 21 20 26 21 21 25 21
11 | 7 13 12 9 12 4 7 11 6 10 3 | 26 26 29 24 22 25 28 30 24 23 24
12 | 8 28 6 11 36 4 22 14 10 9 5 | 67 66 65 64 64 65 65 66 66 67 65
13 | 8 8 10 14 8 4 9 11 8 11 3 | 15 19 16 27 14 16 18 20 15 24 17
14 | 9 11 12 13 10 4 12 11 8 11 4 | 18 17 20 15 20 15 18 20 16 18 16
15 | 5 16 10 11 10 2 17 11 7 9 3 | 20 20 18 24 14 17 20 19 16 20 18
16 | 11 25 8 17 25 6 13 11 9 16 5 | 30 28 34 36 32 33 31 34 36 33 31
17 | 8 14 9 14 17 4 9 13 9 14 4 | 26 29 24 31 24 26 29 29 25 25 25
18 | 9 30 10 17 23 6 18 25 11 14 6 | 20 25 20 27 22 20 23 27 22 23 18
19 | 12 17 8 14 20 6 14 13 12 22 5 | 20 26 22 28 20 21 24 22 19 21 19
20 | 7 13 9 12 15 5 13 18 9 12 4 | 24 22 23 27 25 23 24 19 23 19 21
21E | 12 14 7 10 24 4 10 10 7 8 4 | 23 25 26 30 32 25 26 29 26 27 25
22 | 12 13 11 11 12 5 10 10 10 19 4 | 19 17 17 24 18 18 19 19 19 18 15
23 | 8 22 9 10 11 5 13 8 7 9 3 | 12 15 15 18 12 15 13 16 15 15 13
24 | 9 10 5 8 10 3 9 8 5 7 3 | 25 27 24 24 23 24 28 24 24 26 24
25E | 7 13 7 6 23 4 10 9 7 6 3 | 77 78 76 75 76 76 77 76 75 78 76
26E | 18 16 11 16 29 4 11 7 5 8 5 | 37 37 34 34 41 32 33 33 32 31 33
27 | 9 12 8 12 17 4 14 6 8 5 3 | 22 24 24 16 24 18 26 23 18 22 20
28 | 10 15 5 12 15 5 23 9 8 9 3 | 41 49 37 43 44 42 42 41 41 38 40
29 | 7 21 9 12 15 4 19 13 10 10 4 | 151 154 155 154 149 152 152 156 153 150 153
30 | 7 12 6 8 14 3 10 6 5 12 3 | 23 29 26 25 22 25 30 24 22 28 24
31 | 12 15 10 16 18 7 11 33 12 12 6 | 21 27 18 23 19 20 24 28 21 18 17
32 | 6 13 9 10 10 5 14 10 8 15 3 | 18 29 19 18 18 16 29 19 18 27 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 16 9 12 18 4 13 12 8 12 |T 30 33 31 32 30 29 32 31 30 31 29
WRMS | 9 16 9 11 16 4 13 10 7 10 |NE 20 25 20 23 18 19 24 21 19 23 19
MEDI | 8 13 8 11 15 4 11 10 8 10 |MD 23 27 23 25 22 21 27 24 22 25 21
Table 3.1959.6 GPS week: 1959 Day: 6 MJD: 57963.000
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 14 7 8 18 3 12 7 7 8 3 | 36 37 37 36 40 35 37 36 37 38 36
2E | 23 10 6 14 21 4 12 13 9 9 5 | 21 21 22 27 22 22 20 25 23 25 21
3 | 7 12 5 7 12 4 8 10 6 8 3 | 29 30 26 29 28 25 28 26 26 31 27
X4 | 5 --- --- --- --- 23 21 --- --- --- 0 | 32 --- --- --- --- 33 35 --- --- --- 31
5 | 10 10 9 11 12 3 10 9 9 11 3 | 28 31 29 25 28 24 31 23 24 23 24
6E | 9 11 8 9 20 3 10 11 7 9 3 | 33 36 35 35 32 33 36 32 35 33 33
7 | 14 14 8 12 19 4 9 11 10 14 4 | 33 36 32 31 31 30 36 35 30 31 30
8 | 9 13 6 9 11 3 10 8 6 7 3 | 29 26 28 27 30 25 29 25 26 27 26
9 | 6 13 7 9 10 5 13 7 7 9 3 | 19 32 19 22 16 19 33 21 14 24 19
10 | 7 15 5 8 12 3 11 13 6 8 3 | 20 31 23 23 25 20 26 19 22 26 21
11 | 7 10 10 9 14 3 11 10 6 8 3 | 29 32 32 32 27 30 35 29 31 28 29
12 | 9 32 8 10 28 5 19 14 10 9 5 | 91 88 92 94 87 92 87 93 92 93 91
13 | 7 8 11 8 11 4 9 10 7 12 3 | 20 21 16 25 14 17 19 24 19 27 19
14 | 11 13 10 12 11 3 9 11 7 12 4 | 20 21 19 19 21 15 17 15 15 17 16
15 | 9 14 8 8 12 3 13 11 9 10 3 | 26 28 26 26 21 23 26 25 24 27 24
16 | 12 26 6 16 27 4 14 13 12 14 5 | 30 31 33 37 30 34 32 33 37 33 31
17 | 11 13 8 15 23 4 11 15 8 17 5 | 23 27 22 30 24 25 29 31 26 23 23
18 | 11 29 9 17 19 5 23 26 12 16 6 | 20 27 19 28 21 18 25 28 20 23 17
19 | 11 19 7 15 22 4 17 14 10 23 5 | 21 26 20 29 22 21 28 26 23 23 19
20 | 11 14 8 9 11 4 15 19 7 13 4 | 32 29 27 34 31 29 28 29 29 29 28
21E | 12 11 6 12 27 5 10 11 8 11 4 | 18 22 21 26 25 21 20 27 24 28 22
22 | 14 14 8 12 15 4 10 14 9 17 4 | 21 19 15 25 24 18 20 24 20 17 17
23 | 8 22 9 9 9 6 13 9 7 11 4 | 18 15 19 24 14 17 15 18 18 19 17
24 | 5 10 5 7 13 3 10 11 6 7 3 | 20 24 22 21 19 20 24 23 21 25 21
25E | 10 11 9 6 18 4 12 9 5 5 3 | 77 77 76 76 73 76 76 77 75 75 75
26E | 21 16 10 18 30 3 11 8 8 9 5 | 38 35 33 36 37 32 33 31 32 30 31
27 | 11 12 7 7 26 4 37 6 6 6 3 | 22 22 23 19 33 20 35 20 21 19 20
28 | 11 15 7 13 34 5 10 10 9 11 5 | 33 35 27 27 54 29 32 27 27 24 28
29 | 11 23 9 9 10 3 17 15 11 11 4 | 203 206 203 199 203 201 206 203 199 201 202
30 | 7 9 7 9 14 3 9 6 8 6 3 | 22 27 26 23 29 22 28 23 23 24 23
31 | 13 17 12 12 15 6 10 34 12 12 6 | 19 28 20 26 19 18 24 29 20 19 16
32 | 8 11 8 7 11 3 11 11 7 12 3 | 20 33 21 26 20 19 31 18 20 29 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 8 11 19 4 14 13 8 11 |T 34 37 34 36 35 33 36 35 33 35 33
WRMS | 10 15 8 10 17 4 14 11 8 10 |NE 22 27 22 25 22 20 26 23 21 25 21
MEDI | 10 13 8 9 15 4 11 11 8 11 |MD 23 29 26 27 27 23 29 26 24 27 23
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 4.1959 GPS week: 1959 MJD: 57957.0-57963.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 8 7 18 |U 5 6 19 |U 7 7 15 |
emr | emr 2976 |U 10 8 20 |U 6 8 20 |U 8 8 18 |
esa | esa 2976 | 8 7 17 |U 5 7 18 | 7 7 15 |
gfz | gfz 2973 |U 8 7 17 |U 5 7 21 |U 7 8 20 |
grg | grg 2971 |U 9 9 21 |U 13 17 47 | 8 8 32 |
igr | igr 2976 | 8 7 17 | 5 6 18 | 7 7 15 |
igs | igs 2976 | 8 7 17 | 5 6 18 | 7 7 15 |
jpl | jpl 3072 | 9 8 20 |U 5 7 19 |U 7 8 19 |
mit | mit 2976 | 9 9 22 |U 8 8 26 |U 8 8 17 |
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 5.1959.0 GPS week: 1959 Day: 0 MJD: 57957.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 8 16 | 5 4 20 | 7 9 14 |
emr | emr 2976 | 12 9 14 | 5 7 19 | 8 8 20 |
esa | esa 2976 | 8 7 12 | 4 4 16 | 6 8 13 |
gfz | gfz 2975 | 7 7 12 | 5 5 20 | 9 10 40 |
grg | grg 2973 | 12 12 24 | 6 9 31 | 10 10 105 |
igr | igr 2976 | 8 7 13 | 4 4 17 | 7 8 13 |
igs | igs 2976 | 8 6 12 | 4 4 17 | 7 8 13 |
jpl | jpl 3072 | 8 8 19 | 4 5 19 | 6 9 16 |
mit | mit 2976 | 8 9 16 | 8 5 24 | 7 8 13 |
Table 5.1959.1 GPS week: 1959 Day: 1 MJD: 57958.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 7 6 15 | 4 5 19 | 6 5 16 |
emr | emr 2976 | 12 7 23 | 7 6 18 | 8 6 17 |
esa | esa 2976 | 8 6 16 | 4 5 17 | 6 6 17 |
gfz | gfz 2976 | 7 6 15 | 5 6 19 | 6 6 16 |
grg | grg 2975 | 8 8 20 | 27 35 93 | 8 7 19 |
igr | igr 2976 | 7 6 16 | 4 5 17 | 6 5 17 |
igs | igs 2976 | 7 7 17 | 4 5 18 | 6 5 16 |
jpl | jpl 3072 | 8 6 16 | 5 6 17 | 7 5 20 |
mit | mit 2976 | 9 10 20 | 7 5 26 | 12 7 17 |
Table 5.1959.2 GPS week: 1959 Day: 2 MJD: 57959.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 9 20 | 5 8 19 | 7 6 12 |
emr | emr 2976 | 13 10 20 | 7 10 19 | 7 5 17 |
esa | esa 2976 | 10 9 16 | 5 8 18 | 6 6 14 |
gfz | gfz 2976 | 9 9 15 | 5 8 20 | 6 7 13 |
grg | grg 2976 | 8 8 14 | 31 36 99 | 8 7 16 |
igr | igr 2976 | 10 9 15 | 5 8 19 | 6 6 12 |
igs | igs 2976 | 9 8 15 | 5 7 18 | 6 6 12 |
jpl | jpl 3072 | 11 11 22 | 5 10 17 | 7 7 19 |
mit | mit 2976 | 11 11 27 | 8 14 29 | 9 9 15 |
Table 5.1959.3 GPS week: 1959 Day: 3 MJD: 57960.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 7 11 20 | 4 7 16 | 7 9 17 |
emr | emr 2976 | 10 10 25 | 5 7 20 | 10 10 19 |
esa | esa 2976 | 8 11 22 | 4 8 14 | 7 8 18 |
gfz | gfz 2970 | 7 11 21 | 5 7 19 | 7 8 16 |
grg | grg 2962 | 7 11 21 | 9 10 25 | 8 8 20 |
igr | igr 2976 | 7 11 21 | 4 6 15 | 8 9 16 |
igs | igs 2976 | 7 11 21 | 4 7 15 | 7 8 16 |
jpl | jpl 3072 | 12 14 27 | 4 6 17 | 8 10 21 |
mit | mit 2976 | 7 10 23 | 5 8 16 | 9 9 19 |
Table 5.1959.4 GPS week: 1959 Day: 4 MJD: 57961.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 6 23 | 7 8 21 | 9 8 17 |
emr | emr 2976 | 8 6 20 | 7 10 26 | 8 10 19 |
esa | esa 2976 | 8 6 22 | 7 9 21 | 8 7 16 |
gfz | gfz 2966 | 8 7 22 | 7 9 24 | 9 11 21 |
grg | grg 2963 | 10 8 32 | 8 11 27 | 12 10 28 |
igr | igr 2976 | 9 7 22 | 7 8 21 | 8 7 17 |
igs | igs 2976 | 9 7 22 | 7 8 22 | 8 7 17 |
jpl | jpl 3072 | 10 6 21 | 8 9 21 | 9 9 19 |
mit | mit 2976 | 9 7 22 | 9 9 26 | 8 8 19 |
Table 5.1959.5 GPS week: 1959 Day: 5 MJD: 57962.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 5 17 | 5 6 21 | 7 7 17 |
emr | emr 2976 | 5 6 19 | 6 9 20 | 7 9 19 |
esa | esa 2976 | 6 6 18 | 5 7 22 | 6 7 17 |
gfz | gfz 2975 | 6 6 18 | 6 6 23 | 7 7 20 |
grg | grg 2974 | 10 14 24 | 5 8 28 | 7 6 15 |
igr | igr 2976 | 6 6 16 | 5 6 20 | 6 6 19 |
igs | igs 2976 | 5 6 17 | 5 6 20 | 7 6 17 |
jpl | jpl 3072 | 5 6 14 | 6 7 22 | 7 8 18 |
mit | mit 2976 | 5 5 21 | 11 9 31 | 7 6 16 |
Table 5.1959.6 GPS week: 1959 Day: 6 MJD: 57963.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 6 16 | 4 6 19 | 8 9 13 |
emr | emr 2976 | 11 7 18 | 5 7 19 | 7 11 15 |
esa | esa 2976 | 10 6 15 | 5 7 19 | 7 8 13 |
gfz | gfz 2976 | 10 5 15 | 5 6 21 | 7 8 12 |
grg | grg 2976 | 9 6 15 | 5 7 25 | 7 8 20 |
igr | igr 2976 | 10 5 15 | 5 6 19 | 8 9 14 |
igs | igs 2976 | 9 5 15 | 5 6 19 | 7 8 13 |
jpl | jpl 3072 | 10 7 20 | 5 7 22 | 8 12 20 |
mit | mit 2976 | 16 11 26 | 9 10 29 | 8 9 21 |
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 6.1959 GPS week: 1959 MJD: 57957.500-57963.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 -7 50 157 2 | 19 22
| 14 15 56 91 5 | 2
emr uuuuu | 13 12 79 83 0 | 28 33
| 16 16 88 54 16 | 4
esa uuuuu | 4 11 -19 99 3 | 22 25
| 7 11 42 44 4 | 3
gfz uuuuu | -23 -4 160 -187 -3 | 32 35
| 18 21 151 73 9 | 1
grg uuuuu | 25 -2 27 15 -2 | 2 11
| 20 23 47 87 3 | 2
igr xxxxx | -5 9 -2 2 -5 | 9 14
| 10 13 29 50 9 | 1
irf xxxxx | -6 -16 -9 -47 -1 | 4 13
| 12 6 36 29 4 | 2
jpl xxxxx | 42 -5 114 128 -5 | 32 35
| 22 18 95 58 8 | 1
mit uuuuu | 0 3 -36 -118 5 | 29 32
| 27 20 44 64 5 | 3
ngs uuuuu | -10 -20 -61 -122 -2 | 21 25
| 38 28 131 148 9 | 2
sio uuuux | 23 20 -126 68 2 | 50 51
| 17 17 44 93 4 | 1
Table 7.1959.0 GPS week: 1959 Day: 0 MJD: 57957.500
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 | -1 -17 74 215 0 | 19 22
emr uuuuu | 43 4 143 96 -18 | 36 39
esa uuuuu | 0 20 -40 75 7 | 20 24
gfz uuuuu | -3 13 153 -80 12 | 32 34
grg uuuuu | 32 -16 123 12 -5 | 5 12
igr xxxxx | 17 8 32 30 7 | 9 13
irf xxxxx | 17 -12 41 -5 4 | 5 14
jpl xxxxx | 60 25 -6 123 -3 | 33 36
mit uuuuu | 53 23 26 -38 11 | 27 30
ngs uuuuu | -75 -42 -121 -262 7 | 18 23
sio uuuux | 51 34 -155 87 -1 | 51 52
Table 7.1959.1 GPS week: 1959 Day: 1 MJD: 57958.500
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 | 0 11 86 141 1 | 19 22
emr uuuuu | 12 4 205 77 -20 | 33 36
esa uuuuu | -8 24 -19 98 6 | 21 25
gfz uuuuu | -18 8 19 -112 7 | 33 36
grg uuuuu | 52 -39 -21 12 -3 | 4 12
igr xxxxx | -12 16 -30 100 5 | 10 15
irf xxxxx | -18 -10 -72 -13 3 | 4 14
jpl xxxxx | 14 9 49 90 4 | 34 36
mit uuuuu | -3 35 -117 -49 10 | 28 32
ngs uuuuu | -20 -55 56 -151 4 | 19 25
sio uuuux | 24 22 -185 49 0 | 51 52
Table 7.1959.2 GPS week: 1959 Day: 2 MJD: 57959.500
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 11 128 182 1 | 18 22
emr uuuuu | 21 -11 33 54 -1 | 28 33
esa uuuuu | 14 9 -79 141 8 | 20 24
gfz uuuuu | -41 14 -65 -230 -7 | 32 35
grg uuuuu | 33 -12 -10 -136 -3 | 1 11
igr xxxxx | -12 -4 -24 -2 1 | 9 14
irf xxxxx | -9 -28 -31 -67 2 | 3 14
jpl xxxxx | 36 -24 86 45 -12 | 33 36
mit uuuuu | -3 -7 -47 -93 8 | 27 31
ngs uuuuu | 0 -41 169 -107 5 | 19 25
sio uuuux | 8 34 -168 16 -1 | 50 51
Table 7.1959.3 GPS week: 1959 Day: 3 MJD: 57960.500
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 -28 75 4 11 | 16 20
emr uuuuu | 5 24 9 11 -10 | 26 30
esa uuuuu | 10 18 -35 73 5 | 19 23
gfz uuuuu | -47 -11 146 -269 -5 | 30 33
grg uuuuu | 9 2 38 73 -3 | -1 11
igr xxxxx | -8 -6 -15 -31 -4 | 8 14
irf xxxxx | -8 -15 -1 -46 0 | 1 13
jpl xxxxx | 43 -6 88 199 -17 | 33 36
mit uuuuu | 2 -6 -30 -102 3 | 26 30
ngs uuuuu | 22 -12 -72 117 1 | 19 25
sio uuuux | 26 40 -119 94 4 | 47 49
Table 7.1959.4 GPS week: 1959 Day: 4 MJD: 57961.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -17 -6 -20 75 2 | 19 23
emr uuuuu | 8 18 158 159 13 | 25 29
esa uuuuu | 2 11 -32 27 3 | 22 25
gfz uuuuu | -36 -40 333 -250 -9 | 32 35
grg uuuuu | 35 4 14 108 -1 | 0 11
igr xxxxx | -10 10 -8 -33 -10 | 9 14
irf xxxxx | -16 -15 -17 -56 -2 | 3 13
jpl xxxxx | 62 -21 97 171 3 | 30 33
mit uuuuu | -30 1 -36 -164 3 | 29 32
ngs uuuuu | 27 9 -205 -33 -5 | 22 26
sio uuuux | 16 8 -63 114 6 | 49 50
Table 7.1959.5 GPS week: 1959 Day: 5 MJD: 57962.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -7 -19 24 231 -5 | 21 23
emr uuuuu | -9 38 -30 142 21 | 25 29
esa uuuuu | 3 -6 46 129 -3 | 24 26
gfz uuuuu | -6 -24 348 -215 -13 | 32 35
grg uuuuu | 19 17 35 -52 2 | 1 10
igr xxxxx | -8 9 47 -5 -16 | 9 14
irf xxxxx | -10 -17 -1 -86 -6 | 5 11
jpl xxxxx | 14 -4 237 85 -11 | 31 33
mit uuuuu | -27 -4 -46 -194 0 | 31 33
ngs uuuuu | 17 22 -171 -82 -16 | 23 27
sio uuuux | 1 -5 -95 -93 -3 | 50 51
Table 7.1959.6 GPS week: 1959 Day: 6 MJD: 57963.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 22 2 -20 254 2 | 22 25
emr uuuuu | 13 7 35 40 13 | 26 32
esa uuuuu | 8 3 23 148 -2 | 26 28
gfz uuuuu | -13 11 187 -153 -5 | 33 35
grg uuuuu | -7 31 12 91 1 | 2 12
igr xxxxx | -2 32 -14 -47 -15 | 9 14
irf xxxxx | 1 -15 19 -53 -8 | 6 12
jpl xxxxx | 67 -13 249 187 2 | 31 33
mit uuuuu | 6 -23 -5 -185 -2 | 33 35
ngs uuuuu | -44 -19 -83 -332 -14 | 24 27
sio uuuux | 37 10 -98 209 6 | 51 52
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