[IGSREPORT-25519] Wk 1965 IGS Final Orbits
acc
acc at igs.org
Sun Sep 24 06:31:21 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 1965 (Sep 03, 2017 - Sep 09, 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:
igs1965[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1965[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1965[0-6].cls IGS GPS clock combination summary report.
igs19657.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs19657.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 | 3 10 3 10 ABMF HARB LHAZ TIXI ABMF LHAZ TIXI
0 | EMR | 3 10 3 10 MAS1 NLIB SFER
0 | ESA | DGAR FAA1 MAL2 SEYG DGAR FAA1 MAL2 SEYG
0 | GFZ | HARB
0 | GRG | BRUX DAEJ GLSV SYOG BRUX DAEJ GLSV SYOG
1 | COD | PALM THU2 TIXI PALM THU2 TIXI
1 | EMR | MAS1
1 | ESA | ABMF AREQ AUCK BAKE BRST MAL2 ABMF AREQ AUCK BAKE
1 | ESA | BRST MAL2
1 | GFZ | SFER SFER
1 | GRG | DAEJ GLSV KIT3 MAL2 MAW1 OUS2 RABT SEYG SYOG DAEJ
1 | GRG | GLSV KIT3 LHAZ MAL2 MAW1 RABT SEYG SYOG
1 | JPL | AREQ AREQ
2 | COD | GODE PALM TIXI PALM TIXI
2 | EMR | MAS1 SFER
2 | ESA | AREQ MAL2 OHI3 ABMF AREQ KOUR MAL2 OHI3
2 | GFZ | 13 13 ABMF FAA1 MAL2 FAA1 MAL2
2 | GRG | CRO1 DAEJ FAA1 GLSV GODE KIT3 SYOG CRO1 DAEJ FAA1
2 | GRG | GLSV GODE KIT3 SYOG
2 | MIT | MAW1 OHI3 MAW1 OHI3
3 | COD | ABMF GODE HYDE PALM TIXI ABMF GODE HYDE PALM TIXI
3 | EMR | HERS SFER HERS MAS1 SFER
3 | ESA | AREQ BRAZ CHTI AREQ BRAZ
3 | GFZ | AUCK SYOG AUCK SYOG
3 | GRG | 5 5 CHTI DAEJ DGAR GLSV GODE KIT3 PIE1 SUTH SYOG
3 | GRG | CHTI DAEJ DGAR GLSV GODE KIT3 MAL2 PIE1 RABT SUTH
3 | GRG | SYOG
3 | MIT | AMC2 AMC2 SUTH
4 | COD | ABMF DGAR MAL2 PALM ABMF DGAR MAL2 PALM
4 | EMR | 20 20 KERG MAS1 STJO THTI
4 | ESA | AREQ CHTI CHTI
4 | GFZ | DGAR SYOG AREQ CHTI DGAR MKEA SYOG
4 | GRG | CHTI DAEJ GLSV KIT3 MAC1 REUN SYOG GLSV MAC1 POHN
4 | GRG | REUN SYOG
4 | MIT | FAIR MKEA FAIR MKEA
5 | COD | DGAR HOFN MAL2 NAIN PALM TIXI DGAR HOFN PALM
5 | EMR | 20 20 KERG MCM4 QAQ1 SCH2 WHIT ALBH KERG MAS1 MCM4
5 | EMR | QAQ1 SCH2 WHIT WILL YELL
5 | ESA | AREQ CHTI MAW1 TRO1 WHIT CHTI MAW1 TRO1 WHIT
5 | GFZ | ALGO FAA1 GODE KOUR MAL2 POHN ALGO FAA1 GODE KOUR
5 | GFZ | POHN
5 | GRG | BAKE BRFT CHTI DAEJ FAIR GLSV KIT3 KRGG MAC1 MAW1
5 | GRG | SYOG BAKE BRFT DAEJ FAIR GLSV KIT3 KRGG MAC1 MAW1
5 | MIT | CHUR NRIL CHUR NRIL OHI3
6 | COD | PALM TIXI PALM TIXI
6 | EMR | MAS1 SYOG
6 | ESA | AREQ MAL2 AREQ CHTI MAL2
6 | GFZ | 5 5 ALBH MAL2 ALBH CHTI MAL2
6 | GRG | CHTI DAEJ GLSV KIT3 SEYG SYOG DAEJ GLSV SEYG SYOG
6 | MIT | REUN REUN
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 table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G13 | 2017_09_07 | 2017097
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 G10 | 4 | 4 | 4 | 4 | | | 4 |
PRN G13 | 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 | .5 .3 1.3 12 2 -11 -.58
EMR | 0 | -4.1 -3.6 .1 0 6 27 -.39
ESA | 0 | -.2 -.3 -.5 0 9 -7 -.56
GFZ | 0 | .4 -.1 .3 -12 -10 -3 -.36
GRG | 0 | -.1 2.7 10.9 42 -2 61 -.33
JPL | 0 | 6.9 .4 -2.8 30 -92 15 -.20
MIT | 0 | -1.8 2.1 2.2 -7 57 -5 -.42
NGS | 0 | .4 -4.5 14.5 47 -13 -9 -.49
SIO | 0 | -3.0 3.9 7.1 -9 0 -3 -.32
COD | 1 | .7 .2 1.1 6 -6 -5 -.50
EMR | 1 | 10.0 .7 9.0 -7 0 -6 -.49
ESA | 1 | -.1 -.5 -.9 2 0 -15 -.50
GFZ | 1 | 1.0 .2 .8 -6 -22 -16 -.61
GRG | 1 | 5.4 -5.9 18.4 46 37 44 -.34
JPL | 1 | 3.6 4.1 3.7 -25 -71 22 .30
MIT | 1 | .5 -.3 .3 20 27 -24 -.28
NGS | 1 | 1.5 -5.2 15.6 21 -27 -21 -.47
SIO | 1 | 2.0 1.4 7.1 -2 -17 -5 -.33
COD | 2 | .7 .3 1.4 6 -1 -8 -.66
EMR | 2 | 7.3 1.3 1.2 8 45 -13 -.31
ESA | 2 | .3 -.1 -.0 4 10 -4 -.50
GFZ | 2 | .6 .1 .9 -9 -21 -2 -.48
GRG | 2 | 7.8 -1.8 -6.7 33 19 23 -.34
JPL | 2 | 6.7 -1.1 -1.0 11 -40 49 .05
MIT | 2 | 3.1 -.0 -.5 7 46 -19 -.27
NGS | 2 | 4.5 -4.1 9.0 41 -14 -5 -.46
SIO | 2 | 1.5 6.8 3.3 -3 2 -2 -.42
COD | 3 | .8 .4 1.0 9 -2 -17 -.48
EMR | 3 | 9.6 .2 .4 -16 26 -34 -.34
ESA | 3 | .5 -.1 -.6 -9 -12 -5 -.50
GFZ | 3 | .4 .1 1.0 -14 -8 -14 -.41
GRG | 3 | 11.5 7.5 -5.5 48 8 37 -.47
JPL | 3 | 9.8 -8.9 -2.3 -21 -51 76 .36
MIT | 3 | .4 2.1 -1.7 -9 27 0 -.20
NGS | 3 | 2.7 -5.9 7.6 31 -52 -29 -.33
SIO | 3 | 2.7 4.7 -2.2 -4 -25 6 -.21
COD | 4 | .9 -.1 1.4 3 -4 -9 -.67
EMR | 4 | -2.1 4.5 1.8 7 45 -5 -.40
ESA | 4 | .1 -.5 -1.1 4 -2 2 -.45
GFZ | 4 | .7 .2 .6 -8 -20 -10 -.45
GRG | 4 | -.4 7.1 -3.8 67 1 61 -.19
JPL | 4 | 5.3 -3.2 -2.6 -23 -48 70 -.0
MIT | 4 | -.5 5.5 -.2 -7 33 12 -.41
NGS | 4 | 2.2 -3.3 12.6 -11 -30 -6 -.51
SIO | 4 | -4.6 6.8 -1.4 -15 -18 -8 -.34
COD | 5 | .6 -.1 1.3 3 -2 -1 -.63
EMR | 5 | 6.5 8.4 7.3 -17 4 -7 -.39
ESA | 5 | -1.2 -.4 -1.4 2 8 0 -.47
GFZ | 5 | .3 -.2 .8 -25 -5 -3 -.50
GRG | 5 | .9 1.4 2.6 33 37 61 -.45
JPL | 5 | -.5 3.4 -3.1 -13 -56 34 .08
MIT | 5 | -6.8 3.2 2.5 -17 32 -8 -.42
NGS | 5 | .6 -1.8 2.2 11 -19 -10 -.48
SIO | 5 | -3.5 6.0 -4.2 -21 -7 6 -.44
COD | 6 | .8 -.4 1.7 -3 -2 6 -.76
EMR | 6 | 12.8 -.3 3.8 2 13 -21 -.39
ESA | 6 | -.6 -.8 -.5 -10 -4 13 -.66
GFZ | 6 | .9 .1 1.2 -10 -24 -9 -.64
GRG | 6 | 2.2 .0 8.7 45 3 51 -.27
JPL | 6 | 5.3 3.9 -4.9 14 -86 44 .0
MIT | 6 | -.6 .9 -1.5 1 51 -20 -.47
NGS | 6 | -.2 -1.8 7.0 -10 -26 -9 -.58
SIO | 6 | -4.1 6.6 -8.7 -10 -25 8 -.47
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 1.1965.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1965.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 2.1965.[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 3.1965.[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 5.1965.0-6). 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 1965 summary. (Sep 03, 2017 - Sep 09, 2017)
Table 1.1965.a GPS week: 1965 MJD: 57999.000-58005.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 275| 1 0 -1 5 -10 0 .00 11 10 | -636 -43 11 109
| 0 0 1 9 22 15 .03 | 169 228
emr 79| -1 0 3 8 0 -4 .25 17 17 | 43848 -76 22 126
| 2 3 1 25 17 11 .10 | 72721 576
esa 150| 0 0 -1 3 16 -5 -.02 10 10 | -1216 -253 8 187
| 0 0 1 11 10 8 .02 | 1508 2174
gfz 199| 0 0 1 6 2 -6 .06 11 10 | 95 -299 10 149
| 1 1 1 15 18 8 .02 | 306 641
grg 110| 1 0 0 -5 1 45 -.35 18 14 | 99 -89 13 190
| 0 0 7 20 19 19 .03 | 110 333
igr n/a| 0 0 0 -14 -8 0 -.02 4 4 | -5961 -393 13 81
| 0 0 0 10 11 11 .02 | 995 727
jpl 80| 0 0 0 13 -45 19 .19 12 13 | 922 -62 42 233
| 1 1 0 23 27 15 .02 | 365 562
mit 348| 0 -1 0 -22 -8 21 -.00 13 11 | -955 13 42 334
| 0 0 0 26 35 20 .02 | 267 381
ngs 216| 0 0 1 9 -10 -14 .05 9 8 | -636 -63 939 2196
| 0 0 1 13 11 14 .04 | 113 184
sio 349| 0 -1 -2 -24 -3 -2 .06 14 13 | --- --- --- ---
| 0 0 1 38 35 26 .03 | --- ---
Table 1.1965.b GPS week : 1965 MJD: 57999.000-58005.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 6 5 5 5 5 6 5 |
3 | 6 9 6 5 5 4 5 |
4 | 0 0 0 0 0 0 0 |
5 | 5 5 4 7 5 4 5 |
6 | 4 4 4 4 4 4 4 |
7 | 4 5 5 5 5 4 4 |
8 | 4 4 3 4 3 4 4 |
9 | 4 4 4 4 3 3 3 |
10 | 8 7 6 5 5 5 5 |
11 | 4 5 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 4 4 5 0 5 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 6 6 6 5 5 |
17 | 6 5 5 4 5 5 4 |
18 | 6 5 4 5 5 5 5 |
19 | 6 6 6 5 6 6 5 |
20 | 4 4 5 5 4 4 5 |
21 | 5 4 5 4 5 5 5 |
22 | 5 5 4 4 4 5 4 |
23 | 6 6 6 6 6 6 6 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 5 4 6 5 5 5 5 |
27 | 4 4 4 4 4 3 3 |
28 | 4 4 4 5 4 5 4 |
29 | 7 8 8 8 7 8 8 |
30 | 4 3 3 4 3 4 3 |
31 | 4 5 5 5 5 5 4 |
32 | 3 4 4 4 3 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 2.1965.0 GPS week: 1965 Day: 0 MJD: 57999.000
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 0 0 -1 -49 -17 .06 14 12 | -848 422 14 103
emr 79| -5 -6 2 1 -1 -12 .08 18 18 | 902 298 27 137
esa 150| 0 0 0 4 10 -11 .00 10 10 | -3255 1491 9 174
gfz 199| 1 1 -1 -11 -2 2 .04 10 10 | 51 284 10 133
grg 106| 0 0 3 0 -15 48 -.30 18 14 | -5 176 16 167
igr n/a| 0 0 0 -25 -18 -15 .02 4 4 | -4894 202 15 85
jpl 80| -3 0 0 12 -67 -11 .20 12 12 | 439 680 49 238
mit 349| 0 0 -1 3 24 41 -.01 13 11 | -774 283 56 347
ngs 218| 0 2 2 6 0 -29 .07 9 8 | -774 309 832 2192
sio 345| 0 -1 -3 12 17 11 .02 15 14 | --- --- --- ---
Table 2.1965.1 GPS week: 1965 Day: 1 MJD: 58000.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 275| 1 0 -3 17 16 5 -.04 11 10 | -704 26 12 111
emr 80| 0 1 4 16 24 4 .28 17 17 | 1281 -887 22 122
esa 150| 0 0 -4 14 26 -5 -.04 11 10 | -288 -1728 7 211
gfz 200| 0 0 0 30 3 -8 .06 10 10 | 334 -945 11 237
grg 112| 0 0 10 24 32 47 -.36 23 17 | 222 -227 13 194
igr n/a| 0 0 0 -21 4 4 -.01 5 4 | -4663 -1477 13 79
jpl 80| -2 2 0 19 -27 16 .21 12 12 | 1248 -752 39 243
mit 349| 0 -1 0 -53 -50 22 -.04 13 10 | -923 -116 45 293
ngs 217| -1 0 4 11 -10 -25 .07 8 7 | -697 7 1084 2258
sio 352| 0 -2 -4 -74 -48 18 .02 15 15 | --- --- --- ---
Table 2.1965.2 GPS week: 1965 Day: 2 MJD: 58001.000
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| 2 0 -3 4 -28 -26 .01 11 10 | -701 -47 9 106
emr 80| -2 2 4 27 -7 -18 .30 16 16 | 686 -109 22 133
esa 150| 0 0 -2 15 -1 -13 -.05 10 10 | -2984 699 8 180
gfz 198| -1 0 2 -4 -20 -6 .05 11 11 | -290 -161 10 121
grg 110| 1 0 -1 -3 -2 76 -.34 17 14 | 29 -260 13 187
igr n/a| 0 0 0 -11 -24 -7 -.04 4 4 | -5950 -703 13 78
jpl 80| 1 1 -1 41 -43 15 .16 13 13 | 653 -353 41 206
mit 349| 1 -1 0 -25 49 31 -.01 13 11 | -1066 -178 39 360
ngs 218| 0 0 1 18 -16 -13 .09 9 8 | -684 -87 788 2146
sio 347| 0 0 0 -42 40 13 .07 14 13 | --- --- --- ---
Table 2.1965.3 GPS week: 1965 Day: 3 MJD: 58002.000
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 0 0 8 2 .03 11 10 | -356 -255 11 106
emr 80| 0 2 4 16 3 -15 .32 16 16 | 1472 -622 20 102
esa 150| 0 0 -1 -19 18 -3 -.04 10 10 | -1229 1746 8 167
gfz 201| 0 0 2 2 22 -16 .04 11 11 | -153 476 11 105
grg 108| 1 0 -11 -27 7 36 -.35 20 16 | 126 439 14 183
igr n/a| 0 0 1 -25 0 3 -.02 4 4 | -5931 -1066 12 78
jpl 80| 1 0 0 0 1 27 .21 12 12 | 963 -655 44 259
mit 348| 0 -1 0 4 -17 48 -.00 14 12 | -673 634 39 339
ngs 219| 0 0 1 8 -25 -26 .04 8 7 | -435 -205 817 2137
sio 351| 0 -1 0 2 -9 18 .04 14 14 | --- --- --- ---
Table 2.1965.4 GPS week: 1965 Day: 4 MJD: 58003.000
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| 1 -1 0 -5 -7 2 -.02 11 9 | -460 -209 12 109
emr 78| -5 3 2 46 19 0 .14 17 17 | 149973 255 25 111
esa 150| 0 0 -1 2 29 -6 -.00 9 10 | -523 -644 10 188
gfz 199| 0 -2 1 23 28 -7 .07 11 10 | 534 -843 11 140
grg 111| 1 0 -5 10 8 59 -.37 16 15 | 262 -576 14 197
igr n/a| 0 0 0 2 -2 7 -.01 4 4 | -7401 27 14 81
jpl 80| 0 -1 -1 8 -36 34 .20 13 14 | 616 226 46 253
mit 348| 1 0 -1 -61 -43 13 .00 14 12 | -675 -510 41 315
ngs 218| 0 0 4 23 -14 -14 .08 8 8 | -556 -108 1072 1816
sio 351| 0 -2 -2 -73 -43 -22 .08 14 13 | --- --- --- ---
Table 2.1965.5 GPS week: 1965 Day: 5 MJD: 58004.000
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 0 20 3 9 -.02 11 10 | -654 -178 12 122
emr 80| 0 1 4 -27 -16 12 .31 17 17 | 150626 792 20 148
esa 150| 0 0 0 -1 14 -12 .00 10 10 | 1025 -4323 9 202
gfz 201| 0 0 2 -7 6 -13 .07 11 11 | 323 -1067 10 167
grg 112| 0 0 0 -33 9 32 -.37 14 11 | -22 -219 13 230
igr n/a| 0 0 0 -12 -16 -9 -.02 4 4 | -6984 564 15 94
jpl 80| 0 -1 0 -28 -79 26 .19 12 12 | 1105 532 41 219
mit 349| 0 -1 0 -11 -14 -1 .01 13 9 | -1326 -222 39 357
ngs 214| 0 0 -1 19 -14 -8 .05 10 9 | -607 -254 1079 2159
sio 349| 1 -1 -1 6 -14 -3 .09 14 13 | --- --- --- ---
Table 2.1965.6 GPS week: 1965 Day: 6 MJD: 58005.000
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| 0 0 0 5 -17 17 -.01 11 10 | -729 -66 11 106
emr 80| 2 -1 2 -19 -24 -1 .34 17 17 | 2002 -260 21 135
esa 150| 0 0 -1 9 16 11 -.01 10 10 | -1259 985 8 187
gfz 197| -1 0 0 10 -19 6 .08 10 10 | -130 159 10 143
grg 111| 1 0 5 -9 -28 16 -.40 16 14 | 86 42 14 177
igr n/a| 0 0 0 -4 0 16 -.04 4 4 | -5906 -304 13 77
jpl 80| 0 0 0 37 -63 27 .19 12 12 | 1433 -117 40 219
mit 349| 0 -1 0 -11 -5 -4 .03 14 11 | -1251 200 40 330
ngs 214| 0 0 1 -17 10 13 -.04 9 8 | -705 -104 902 2666
sio 351| 0 0 -3 0 34 -53 .09 12 12 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1965.0 GPS week: 1965 Day: 0 MJD: 57999.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 12 7 7 9 4 8 9 6 16 3 | 28 32 30 30 27 27 31 28 28 38 29
2 | 21 12 11 14 17 3 10 15 11 23 6 | 23 28 23 38 19 27 29 36 33 28 27
3E | 14 25 12 14 34 6 15 8 13 12 6 | 41 46 45 45 58 42 42 44 44 46 44
X4 | 3 --- --- --- --- 23 22 --- --- --- 0 | 44 --- --- --- --- 49 43 --- --- --- 45
5E | 27 14 7 8 16 3 9 10 9 10 5 | 121 121 120 119 119 119 121 121 119 121 120
6 | 9 12 8 8 15 4 11 15 9 13 4 | 30 32 28 27 26 27 31 29 30 25 27
7 | 8 15 13 9 9 2 11 11 9 13 4 | 27 26 24 24 24 23 28 22 24 26 23
8 | 8 14 7 8 15 3 7 7 9 16 3 | 29 31 30 27 27 28 33 28 31 33 28
9 | 11 14 9 6 11 3 10 11 5 12 3 | 28 30 32 29 25 29 34 30 32 35 30
10E | 26 26 11 11 48 8 --- 8 14 16 8 | 530 525 527 526 532 527 --- 525 526 528 527
11 | 12 16 14 7 11 3 12 10 8 13 4 | 46 45 38 49 40 42 46 46 43 45 43
12E | 14 24 7 11 17 5 19 13 7 13 4 | 65 64 60 63 62 62 63 61 60 62 61
13 | 11 14 13 10 8 3 11 11 8 12 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
14 | 7 21 12 13 16 4 11 12 9 18 5 | 31 30 27 35 29 31 29 35 34 32 29
15 | 12 13 12 11 13 3 11 11 9 17 4 | 38 41 41 34 33 36 41 34 34 36 35
16E | 11 31 7 15 15 4 17 13 8 13 5 | 37 43 39 42 39 39 42 38 41 40 38
17 | 21 17 12 13 17 4 9 13 12 17 5 | 40 37 33 38 36 36 38 39 39 35 35
18E | 19 23 8 12 31 5 14 13 12 14 6 | 25 36 34 34 31 32 31 34 33 33 30
19 | 19 18 11 14 19 6 11 16 12 20 6 | 45 43 41 43 46 42 42 44 43 41 41
20E | 18 12 7 9 10 3 12 8 9 12 4 | 55 53 52 48 53 50 52 52 50 51 51
21 | 8 14 11 10 15 4 13 11 10 18 4 | 27 32 25 34 21 29 30 33 30 31 28
22E | 10 19 8 11 21 3 15 10 9 9 4 | 47 49 50 52 44 51 49 51 52 51 49
23 | 13 31 11 14 14 3 16 17 11 17 6 | 20 25 19 28 22 22 23 32 27 26 22
24 | 10 12 11 9 13 4 10 12 9 12 4 | 27 29 29 31 27 28 32 30 30 34 28
25E | 10 20 8 6 14 4 11 9 11 13 4 | 28 29 32 28 32 27 27 27 30 27 28
26E | 13 18 9 11 15 4 12 12 7 17 4 | 41 45 45 44 45 42 43 43 45 42 43
27 | 8 11 6 6 13 3 8 8 9 14 3 | 27 32 30 26 28 27 31 27 29 33 27
28E | 9 14 8 8 16 4 11 10 6 14 4 | 33 29 30 32 32 30 28 31 30 34 30
29 | 12 25 12 13 16 8 17 37 12 14 7 | 31 38 32 31 33 32 35 36 32 29 28
30 | 11 11 11 9 8 4 10 8 7 13 3 | 26 29 26 26 23 25 32 26 28 30 26
31 | 10 16 12 11 9 5 12 9 9 15 4 | 29 30 24 24 23 25 31 25 26 28 24
32 | 7 15 9 5 11 4 8 7 8 11 3 | 41 50 48 44 40 43 44 43 46 50 45
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 18 10 10 18 4 12 13 9 15 |T 53 56 53 55 53 53 39 55 54 55 52
WRMS | 12 18 10 10 14 4 12 11 8 14 |NE 31 33 30 32 28 31 34 32 32 33 31
MEDI | 11 15 11 10 15 4 11 11 9 14 |MD 31 32 32 34 32 32 33 34 33 34 30
Table 3.1965.1 GPS week: 1965 Day: 1 MJD: 58000.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 9 8 11 13 3 7 8 8 16 3 | 26 31 25 23 23 24 29 24 25 36 24
2 | 13 11 10 17 21 5 9 13 9 21 5 | 20 28 23 33 18 26 25 30 25 27 24
3E | 27 22 19 14 66 10 --- 14 16 14 9 | 47 53 49 47 69 48 --- 53 46 54 47
X4 | 2 --- --- --- --- 23 --- --- --- --- 0 | 40 --- --- --- --- 45 --- --- --- --- 40
5E | 20 14 7 12 17 4 11 10 7 13 4 | 118 118 118 115 116 116 116 117 116 121 116
6 | 9 13 9 10 18 4 10 12 6 16 4 | 27 32 26 25 22 24 29 26 25 27 25
7 | 9 16 13 9 9 4 11 11 10 14 4 | 20 23 17 20 16 18 22 19 20 24 18
8 | 7 9 7 6 13 3 10 7 7 18 3 | 25 28 26 26 26 25 28 26 25 37 26
9 | 10 14 11 8 11 5 7 9 6 15 4 | 28 34 32 28 29 27 34 28 27 33 28
10E | 9 23 13 11 59 8 19 7 11 15 7 | 417 420 415 416 403 417 53 415 420 414 415
11 | 9 13 14 16 16 5 12 7 7 16 4 | 26 31 20 28 20 25 33 27 24 26 23
12E | 14 25 6 8 22 4 17 12 8 16 5 | 48 48 46 47 41 45 47 46 45 47 45
13 | 11 13 13 9 8 2 12 11 7 12 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
14 | 7 13 14 13 17 4 13 12 8 17 4 | 27 32 27 30 31 30 33 32 31 33 28
15 | 13 12 11 11 19 4 13 12 8 16 4 | 32 36 31 31 35 30 36 31 33 33 31
16E | 8 29 9 12 13 4 19 12 8 14 5 | 33 37 34 32 30 33 33 36 36 35 33
17 | 11 15 11 13 21 6 9 13 9 18 5 | 32 32 29 32 30 31 31 32 32 29 29
18E | 15 21 8 8 28 5 12 9 9 13 5 | 20 28 29 27 25 27 28 28 26 30 25
19 | 12 17 11 13 21 6 13 15 10 22 5 | 32 35 33 35 37 33 33 35 34 34 32
20E | 15 12 6 9 14 3 9 12 6 9 4 | 39 41 41 40 46 40 40 42 42 39 40
21 | 9 14 10 9 21 4 11 11 8 17 4 | 25 29 21 26 19 24 27 26 25 23 23
22E | 9 17 8 11 30 5 11 9 8 11 4 | 37 37 39 42 38 40 39 39 39 40 37
23 | 11 31 12 11 19 4 15 17 11 17 6 | 19 28 17 19 20 17 22 25 21 22 18
24 | 7 14 13 6 13 3 7 13 5 14 4 | 23 29 25 27 22 23 29 27 26 30 25
25E | 9 14 8 4 11 4 9 6 7 14 3 | 25 31 33 29 31 27 29 30 28 29 28
26E | 10 18 10 7 16 4 10 10 8 18 4 | 35 42 39 37 37 37 36 41 37 37 36
27 | 8 14 7 6 13 3 10 6 9 13 3 | 25 30 25 27 23 25 28 28 26 30 25
28E | 8 12 9 5 18 3 10 9 8 11 3 | 26 28 26 28 30 28 28 29 30 28 26
29 | 10 25 11 13 24 6 17 42 11 15 7 | 26 27 22 28 26 23 25 36 27 23 21
30 | 6 10 11 7 10 4 7 6 6 13 3 | 23 30 25 24 21 22 29 23 25 29 24
31 | 8 16 12 11 10 4 13 9 10 19 4 | 29 32 23 24 22 25 33 26 25 30 24
32 | 7 13 10 6 12 3 9 8 6 15 3 | 32 42 38 35 36 35 38 35 37 39 35
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 11 10 23 5 12 13 8 15 |T 44 49 45 46 44 44 34 47 45 47 44
WRMS | 10 17 10 10 17 4 12 10 7 15 |NE 26 31 25 27 25 26 29 28 27 29 26
MEDI | 9 14 10 10 17 4 11 11 8 15 |MD 27 32 27 28 29 27 31 30 27 30 28
Table 3.1965.2 GPS week: 1965 Day: 2 MJD: 58001.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 13 7 8 10 4 7 10 7 13 3 | 29 33 31 33 31 30 33 29 31 39 31
2 | 11 13 11 17 14 5 12 11 9 19 5 | 22 30 23 39 22 29 27 32 32 32 27
3E | 13 15 13 11 38 5 16 10 9 11 6 | 25 30 27 26 33 25 34 23 26 24 24
X4 | 3 --- --- --- --- 34 32 --- --- --- 0 | 36 --- --- --- --- 43 43 --- --- --- 36
5E | 12 16 7 10 16 4 11 6 6 11 4 | 69 75 72 71 71 72 72 73 72 68 71
6 | 8 15 8 9 11 3 11 11 7 13 3 | 24 33 24 25 24 22 30 24 24 30 24
7 | 9 16 11 11 12 4 11 13 8 15 4 | 22 27 17 18 20 19 25 21 23 25 20
8 | 7 11 7 7 13 4 9 6 7 11 3 | 25 29 27 25 24 24 28 26 27 29 25
9 | 8 12 10 7 11 5 9 9 7 11 3 | 23 29 24 21 23 21 28 22 21 30 22
10E | 8 15 13 15 37 6 12 9 12 15 6 | 184 186 184 186 182 186 32 186 184 185 184
11 | 9 14 15 8 10 3 15 10 8 10 4 | 31 33 25 32 29 29 34 31 32 30 29
12E | 15 27 6 12 11 4 18 12 8 13 5 | 44 44 42 44 37 41 44 41 41 40 41
13 | 12 12 13 11 9 3 15 12 7 13 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
14 | 7 15 11 15 17 4 12 14 9 19 5 | 23 28 22 30 26 24 26 29 27 27 24
15 | 15 13 10 14 13 5 14 11 9 14 4 | 36 39 33 28 37 31 39 32 32 34 32
16E | 11 25 8 15 25 5 21 16 10 16 5 | 25 34 28 30 20 26 27 31 30 34 27
17 | 13 18 11 14 14 5 9 12 11 16 5 | 37 39 33 39 34 36 38 40 38 41 36
18E | 11 19 8 10 13 2 18 8 6 11 4 | 22 30 29 30 29 27 25 28 29 28 27
19 | 15 21 11 15 15 6 15 15 13 19 5 | 43 44 40 42 42 39 43 39 40 42 40
20E | 21 13 7 10 12 4 10 12 7 9 4 | 37 40 37 37 37 36 34 39 39 41 37
21 | 8 15 12 9 12 3 11 12 8 18 4 | 28 33 24 29 26 27 28 30 30 29 27
22E | 10 14 7 11 17 3 11 10 8 11 4 | 38 38 38 42 39 37 35 38 37 43 38
23 | 14 28 12 14 13 5 17 19 11 18 6 | 19 27 18 25 23 20 22 27 25 23 20
24 | 9 14 12 8 10 3 7 10 6 10 3 | 23 31 26 27 25 25 29 26 27 33 26
25E | 8 15 9 5 17 4 12 9 6 11 3 | 23 30 30 27 28 25 28 26 27 26 26
26E | 11 13 9 10 30 6 11 13 11 18 5 | 36 43 43 39 48 38 41 43 39 41 39
27 | 8 14 8 7 13 4 7 6 8 15 3 | 23 31 25 24 24 23 27 27 23 33 24
28E | 8 15 8 7 11 5 10 11 8 11 3 | 25 30 27 28 27 25 27 29 30 28 27
29 | 11 22 11 14 20 8 18 44 12 14 7 | 27 30 23 23 22 23 28 37 26 18 19
30 | 6 13 9 8 10 4 9 8 4 12 3 | 25 33 26 25 22 25 30 23 26 33 26
31 | 8 15 12 15 12 4 14 11 10 18 4 | 27 31 22 23 26 23 32 25 26 29 24
32 | 7 9 9 9 13 4 9 8 10 14 3 | 31 35 33 29 28 31 35 30 35 36 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 10 11 17 4 13 13 9 14 |T 34 39 35 36 35 34 33 36 36 38 34
WRMS | 10 16 10 11 14 4 13 11 8 13 |NE 27 32 26 28 26 27 31 28 28 31 27
MEDI | 9 15 10 10 13 4 11 11 8 13 |MD 27 33 27 29 27 27 30 29 30 32 27
Table 3.1965.3 GPS week: 1965 Day: 3 MJD: 58002.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 9 9 8 9 3 8 10 8 16 3 | 25 28 24 28 25 24 29 25 25 35 25
2 | 12 12 10 14 15 4 12 14 8 18 4 | 27 36 30 42 33 36 36 42 36 34 33
3E | 13 11 13 10 25 5 14 9 8 9 4 | 40 43 42 39 44 38 32 38 36 43 39
X4 | 1 --- --- --- --- 36 34 --- --- --- 0 | 41 --- --- --- --- 31 31 --- --- --- 41
5E | 15 17 5 12 55 5 14 12 8 9 6 | 57 61 58 61 79 59 60 61 61 59 59
6 | 18 11 7 9 9 5 8 10 6 14 4 | 29 32 22 24 22 23 30 27 24 30 24
7 | 7 17 12 11 14 5 13 12 9 13 4 | 23 27 21 20 22 20 26 21 22 24 21
8 | 8 12 7 9 15 3 8 7 5 14 3 | 37 40 38 35 34 36 39 35 35 42 36
9 | 9 12 10 9 14 4 8 8 6 10 3 | 26 32 31 24 30 25 33 24 26 33 27
10E | 9 15 12 11 32 4 11 10 8 12 5 | 186 186 186 184 186 184 40 183 184 185 185
11 | 8 14 14 10 10 2 11 9 8 16 4 | 46 45 38 48 47 43 47 43 45 45 43
12E | 9 23 6 10 17 4 18 14 8 13 4 | 52 52 50 55 46 52 53 54 51 53 51
13 | 12 13 12 9 11 3 14 13 10 14 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
14 | 6 13 13 14 17 3 12 14 8 16 4 | 23 29 23 26 31 23 28 26 24 25 22
15 | 9 12 11 12 16 4 11 13 8 17 4 | 38 44 41 32 46 36 43 33 39 35 37
16E | 8 29 6 16 27 4 18 13 7 17 5 | 33 35 35 36 36 34 33 38 37 39 34
17 | 11 15 11 12 13 5 9 11 7 14 4 | 32 35 30 34 27 31 34 32 33 35 31
18E | 19 20 8 10 19 5 14 10 9 11 5 | 26 34 35 35 37 34 32 34 36 33 32
19 | 13 20 10 14 13 6 14 15 9 18 5 | 34 39 33 36 31 32 37 32 34 34 33
20E | 21 11 6 10 13 3 8 13 8 8 4 | 28 31 30 28 29 28 29 33 31 30 29
21 | 10 12 11 11 14 5 10 11 8 16 4 | 29 38 28 39 34 34 34 38 36 35 33
22E | 9 11 8 8 17 4 12 10 7 10 3 | 32 39 32 36 30 33 32 36 34 36 33
23 | 11 28 11 17 16 4 17 21 11 16 6 | 18 26 16 22 17 15 21 22 19 18 16
24 | 8 13 13 6 10 4 9 11 4 12 3 | 23 31 24 27 20 26 30 26 27 28 25
25E | 8 15 7 6 21 5 12 8 8 14 4 | 30 34 33 30 27 29 34 28 28 30 29
26E | 9 15 9 13 25 4 9 16 7 17 5 | 31 34 35 33 32 33 32 35 34 31 31
27 | 8 13 7 10 12 3 9 8 7 15 3 | 36 42 37 33 33 35 38 35 33 42 35
28E | 7 15 8 10 31 4 11 12 8 10 4 | 43 42 46 45 42 44 43 44 43 42 43
29 | 12 23 12 12 18 7 16 44 11 17 7 | 40 44 37 38 35 37 43 46 36 37 35
30 | 8 11 10 10 10 5 7 8 6 11 3 | 28 35 27 28 21 29 34 26 29 32 27
31 | 10 16 11 14 13 5 13 11 9 18 4 | 23 27 20 21 22 21 28 21 22 27 20
32 | 6 10 9 8 13 2 10 9 5 13 3 | 32 35 35 31 37 32 35 27 32 38 32
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 10 11 20 4 12 14 8 14 |T 37 41 37 39 38 37 35 38 38 40 37
WRMS | 10 16 10 11 16 4 12 12 7 14 |NE 30 35 29 30 29 29 33 30 30 33 29
MEDI | 9 13 10 10 15 4 11 11 8 14 |MD 32 35 33 33 32 33 34 33 34 35 33
Table 3.1965.4 GPS week: 1965 Day: 4 MJD: 58003.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 10 9 9 15 4 9 12 9 15 4 | 28 34 29 35 28 30 33 35 33 41 31
2 | 11 14 10 17 18 4 13 14 9 20 5 | 28 37 30 44 27 34 32 42 36 35 33
3E | 12 12 12 9 25 4 12 10 7 10 4 | 34 39 40 33 33 34 32 36 31 38 34
X4 | 1 --- --- --- --- 22 23 --- --- --- 0 | 45 --- --- --- --- 43 40 --- --- --- 45
5E | 19 17 5 11 15 3 12 10 6 9 4 | 59 62 59 59 65 58 60 63 59 64 60
6 | 8 18 6 9 15 4 9 10 7 13 3 | 29 36 29 33 26 31 33 33 31 37 30
7 | 10 19 11 10 12 4 14 13 8 15 4 | 24 31 24 23 19 22 27 22 24 31 23
8 | 7 13 7 8 10 4 9 9 6 9 3 | 38 40 39 38 35 36 40 39 39 40 38
9 | 9 11 8 6 10 4 11 10 7 11 3 | 33 39 36 34 35 34 38 34 33 38 34
10E | 12 17 11 9 27 4 11 10 7 12 5 | 83 86 86 83 86 83 42 84 81 84 83
11 | 8 12 13 10 11 2 11 9 8 12 4 | 39 45 39 45 38 41 46 45 39 45 40
12E | 10 26 8 10 14 3 20 14 8 12 4 | 56 57 57 62 55 59 61 57 58 59 57
X13 | 1 --- --- --- --- 18 --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
14 | 6 14 12 12 18 4 15 15 10 18 5 | 21 25 23 26 25 23 25 27 27 27 22
15 | 14 15 11 13 12 4 13 11 8 15 4 | 39 43 39 31 38 35 44 37 36 37 35
16E | 11 31 9 13 17 5 21 13 9 17 5 | 35 43 39 42 37 37 36 40 40 41 38
17 | 14 17 9 15 17 4 11 12 9 15 5 | 45 46 45 49 43 46 48 47 49 47 46
18E | 18 20 7 10 19 4 14 12 9 9 4 | 26 32 32 35 30 31 33 35 32 31 30
19 | 16 21 10 18 17 5 16 15 10 21 5 | 49 51 50 51 48 48 50 45 48 48 48
20E | 17 10 5 9 9 4 11 9 7 11 3 | 32 35 34 35 32 32 35 38 33 35 33
21 | 8 17 11 9 16 5 20 16 9 15 4 | 28 33 26 33 25 30 38 38 30 31 28
22E | 11 13 8 9 20 3 14 13 8 9 4 | 34 42 38 40 31 37 37 42 42 40 38
23 | 10 28 10 13 15 4 22 21 11 16 5 | 20 30 18 22 16 19 24 24 21 17 18
24 | 8 12 12 10 9 3 8 10 4 13 3 | 26 31 26 28 23 26 31 28 29 34 26
25E | 8 14 8 6 15 5 12 7 10 11 3 | 28 34 34 33 31 30 33 31 32 30 30
26E | 11 16 8 8 25 4 10 13 8 18 5 | 60 64 62 62 64 60 61 59 61 57 60
27 | 7 14 5 8 13 4 9 9 9 10 3 | 37 41 40 40 38 37 38 41 38 41 38
28E | 7 15 6 10 20 5 10 10 8 11 4 | 31 38 30 36 34 33 34 32 35 34 32
29 | 10 22 12 14 19 6 19 44 10 16 7 | 35 36 33 35 36 32 32 39 33 32 30
30 | 8 14 8 8 8 4 8 10 6 12 3 | 32 40 33 32 28 31 36 31 35 35 32
31 | 6 15 12 11 14 3 12 13 11 18 4 | 22 27 18 22 21 20 28 23 22 25 20
32 | 5 10 8 7 10 3 10 8 7 12 3 | 38 40 40 38 38 38 41 38 36 43 38
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 9 11 16 4 13 14 8 14 |T 36 41 37 39 36 37 38 39 38 39 37
WRMS | 9 17 10 10 15 4 14 12 8 13 |NE 32 37 32 34 30 32 36 35 33 36 32
MEDI | 9 15 9 10 15 4 12 11 8 12 |MD 34 39 34 35 33 34 36 38 35 37 34
Table 3.1965.5 GPS week: 1965 Day: 5 MJD: 58004.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 14 8 10 12 3 9 7 12 16 4 | 33 39 34 35 27 32 34 32 34 44 33
2 | 12 15 10 18 14 6 11 15 11 21 5 | 34 39 32 45 32 39 38 43 42 39 37
3E | 7 14 9 7 20 5 12 7 7 7 3 | 35 34 35 35 35 32 33 33 35 34 33
X4 | 1 --- --- --- --- 31 20 --- --- --- 0 | 41 --- --- --- --- 41 34 --- --- --- 40
5E | 14 14 7 12 12 4 15 8 9 9 4 | 59 63 59 59 65 59 59 62 59 62 60
6 | 11 15 8 14 12 4 10 11 6 10 4 | 34 38 31 34 28 30 36 36 31 36 32
7 | 10 17 12 10 7 5 12 11 11 14 4 | 23 25 22 21 16 20 25 22 22 24 20
8 | 8 13 6 10 10 2 7 8 11 11 3 | 28 30 26 24 25 24 28 25 27 29 25
9 | 8 11 9 7 10 4 9 7 9 10 3 | 27 32 28 26 24 26 33 26 28 34 27
10E | 10 16 12 7 21 4 12 9 10 9 4 | 152 150 149 149 148 150 42 150 149 150 149
11 | 10 15 14 9 11 3 10 8 10 12 4 | 29 38 29 30 27 29 34 29 31 32 29
12E | 12 27 6 9 14 4 20 14 9 14 5 | 73 74 67 67 66 68 71 67 68 67 68
13 | 12 15 11 12 8 4 18 14 8 15 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
14 | 9 16 13 15 13 3 9 12 12 16 5 | 18 23 19 26 19 21 23 24 23 27 20
15 | 12 17 9 12 12 3 13 11 10 17 4 | 34 39 31 28 29 28 38 30 29 32 30
16E | 8 30 7 14 15 5 16 12 10 13 5 | 45 46 44 45 46 42 45 44 44 46 44
17 | 12 18 12 12 10 4 10 10 9 15 4 | 44 43 41 43 42 42 46 44 43 42 42
18E | 16 19 7 9 20 5 12 11 7 10 4 | 20 25 27 27 25 25 24 27 27 28 24
19 | 13 20 11 14 12 5 15 16 10 20 5 | 65 66 62 62 66 64 68 66 64 63 63
20E | 15 10 6 8 15 4 8 10 9 8 4 | 31 31 31 30 32 30 31 31 33 32 30
21 | 12 12 10 10 11 5 12 17 9 16 4 | 23 30 23 28 22 24 27 29 25 26 24
22E | 11 15 9 10 25 5 14 12 13 10 5 | 36 42 38 43 36 39 35 42 40 41 38
23 | 11 27 10 15 11 6 19 16 11 14 5 | 20 27 20 25 22 22 23 24 23 23 21
24 | 7 12 12 7 9 4 9 13 8 16 4 | 24 28 25 25 19 24 29 30 26 36 25
25E | 10 15 7 7 17 4 13 7 10 14 4 | 27 35 32 29 36 29 33 27 30 33 30
26E | 12 16 8 10 22 4 11 16 10 14 5 | 40 40 45 41 47 41 41 51 40 49 43
27 | 10 13 6 8 8 3 8 8 8 8 3 | 31 34 30 28 27 26 29 28 30 30 29
28E | 11 17 7 11 22 3 8 10 9 10 4 | 37 36 37 41 38 39 39 41 42 42 38
29 | 12 24 10 16 18 8 14 41 15 21 7 | 36 41 34 38 34 34 36 43 35 34 33
30 | 9 13 11 10 6 3 8 5 7 13 3 | 24 29 24 21 18 21 27 21 23 28 22
31 | 9 17 11 10 7 3 12 11 9 19 4 | 25 28 20 23 16 22 28 25 22 29 22
32 | 7 15 10 7 7 4 10 9 12 9 3 | 41 45 43 41 37 40 40 40 39 44 41
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 10 11 14 4 12 13 10 14 |T 38 41 37 38 36 37 36 39 38 41 37
WRMS | 10 17 10 11 11 4 12 9 9 13 |NE 31 35 30 31 27 30 33 32 31 34 30
MEDI | 10 15 9 10 12 4 12 11 10 14 |MD 34 36 31 30 29 30 34 31 31 34 32
Table 3.1965.6 GPS week: 1965 Day: 6 MJD: 58005.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 8 11 10 8 12 4 8 7 9 14 3 | 45 47 44 48 40 43 47 46 44 58 46
2 | 13 11 10 12 18 6 12 13 10 18 5 | 38 44 39 54 35 47 45 53 50 44 44
3E | 10 16 10 7 27 5 11 9 7 7 4 | 42 48 48 43 42 43 40 45 41 48 43
X4 | 1 --- --- --- --- 27 25 --- --- --- 0 | 54 --- --- --- --- 56 50 --- --- --- 54
5E | 18 16 6 11 17 5 14 9 10 9 4 | 125 129 125 124 127 125 128 127 125 127 125
6 | 8 15 7 8 12 4 9 11 7 11 3 | 33 40 33 36 31 35 40 40 35 41 35
7 | 10 14 12 10 9 4 11 12 9 9 4 | 34 40 31 35 31 34 36 37 34 37 34
8 | 6 16 6 10 10 2 8 12 5 8 3 | 49 54 51 48 48 48 51 51 48 55 49
9 | 7 11 10 8 10 4 11 10 7 8 3 | 42 47 45 40 43 40 46 42 40 51 43
10E | 9 14 12 7 26 4 10 10 8 9 4 | 197 197 197 197 196 196 46 198 197 200 197
11 | 9 11 15 10 14 4 11 10 8 13 4 | 63 64 57 66 58 61 66 65 60 68 62
12E | 13 25 5 11 11 4 18 12 9 10 4 | 67 70 66 70 62 67 66 67 66 64 66
13 | 10 14 13 11 10 5 12 12 10 13 4 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
14 | 9 12 12 12 15 4 14 13 9 15 4 | 27 30 26 28 26 24 25 28 25 28 25
15 | 12 14 10 11 13 5 11 15 11 14 4 | 56 60 56 51 59 53 60 57 58 58 55
16E | 11 31 7 12 15 3 19 13 10 9 5 | 41 44 44 45 39 43 44 46 44 46 43
17 | 11 15 9 10 14 4 8 12 9 13 4 | 47 52 46 48 47 47 50 51 49 49 47
18E | 20 19 6 10 22 4 15 12 11 12 5 | 33 43 44 44 38 43 42 45 46 48 42
19 | 13 20 9 11 17 5 12 14 11 17 5 | 58 62 57 55 60 55 59 56 54 55 56
20E | 19 14 6 9 19 4 8 13 12 11 5 | 78 79 76 72 75 75 78 76 75 77 75
21 | 10 12 12 10 14 4 10 15 9 15 4 | 40 45 39 48 37 42 45 47 44 47 42
22E | 9 14 10 9 17 4 14 12 8 8 4 | 64 64 65 69 62 66 63 67 67 71 66
23 | 12 30 9 13 14 5 20 16 10 14 5 | 32 43 30 29 32 28 32 28 25 32 28
24 | 9 14 12 7 9 3 9 15 7 10 4 | 45 48 47 47 41 45 49 52 45 54 47
25E | 8 13 8 6 21 4 11 8 7 8 3 | 40 44 46 41 48 40 45 38 39 41 41
26E | 11 15 8 8 28 4 15 17 9 9 5 | 57 57 59 59 68 56 57 59 54 59 57
27 | 9 14 6 8 12 3 10 8 7 6 3 | 50 54 52 49 49 49 50 50 49 53 50
28E | 8 16 8 8 15 3 9 9 10 7 3 | 40 41 40 39 41 39 39 40 40 42 39
29 | 13 22 10 15 22 8 14 41 12 17 7 | 47 50 45 44 48 42 46 44 40 39 41
30 | 7 11 10 8 6 3 7 6 5 9 3 | 41 46 37 40 37 39 45 42 40 45 40
31 | 7 16 12 10 10 4 12 11 10 13 4 | 32 34 30 24 25 25 33 25 24 31 26
32 | 9 12 9 6 10 3 13 9 8 10 3 | 51 55 59 55 52 55 55 52 54 61 54
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 17 10 10 16 4 12 14 9 12 |T 53 57 54 54 53 53 50 55 53 57 53
WRMS | 10 17 10 10 14 4 12 11 8 12 |NE 44 48 43 44 42 43 46 45 43 47 43
MEDI | 9 14 10 10 14 4 11 12 9 10 |MD 45 48 46 48 43 45 46 47 45 49 46
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 4.1965 GPS week: 1965 MJD: 57999.0-58005.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3056 |U 7 9 19 |U 6 7 24 |U 9 9 19 |
emr | emr 2961 |U 9 9 22 |U 7 9 26 |U 9 7 21 |
esa | esa 2962 | 7 8 18 |U 6 8 25 | 10 8 21 |
gfz | gfz 2962 |U 7 8 18 |U 7 9 26 |U 10 8 20 |
grg | grg 2962 |U 8 8 19 |U 7 8 28 | 11 11 25 |
igr | igr 2958 | 7 8 17 | 6 8 23 | 9 8 19 |
igs | igs 2962 | 7 8 18 | 6 8 24 | 9 8 20 |
jpl | jpl 3017 | 10 10 20 |U 6 8 21 | 11 10 24 |
mit | mit 2962 | 7 8 18 |U 7 10 28 |U 12 10 24 |
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 5.1965.0 GPS week: 1965 Day: 0 MJD: 57999.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 12 16 | 8 9 47 | 9 9 16 |
emr | emr 2976 | 9 10 18 | 11 11 53 | 8 4 22 |
esa | esa 2976 | 8 9 16 | 9 10 51 | 10 8 18 |
gfz | gfz 2976 | 6 8 14 | 8 12 48 | 9 8 16 |
grg | grg 2976 | 10 11 17 | 9 9 53 | 10 12 21 |
igr | igr 2948 | 7 9 14 | 9 10 47 | 9 9 18 |
igs | igs 2975 | 7 9 15 | 9 10 51 | 9 8 17 |
jpl | jpl 2976 | 11 13 20 | 5 7 24 | 11 13 24 |
mit | mit 2976 | 6 8 13 | 10 13 47 | 10 8 20 |
Table 5.1965.1 GPS week: 1965 Day: 1 MJD: 58000.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 7 11 22 | 5 7 21 | 10 14 14 |
emr | emr 2976 | 8 10 18 | 7 6 29 | 9 8 19 |
esa | esa 2976 | 6 8 18 | 5 6 19 | 10 12 16 |
gfz | gfz 2976 | 6 8 18 | 5 8 23 | 10 12 13 |
grg | grg 2976 | 7 9 22 | 6 8 22 | 12 18 18 |
igr | igr 2976 | 6 8 17 | 5 7 21 | 10 11 13 |
igs | igs 2976 | 6 8 17 | 5 6 19 | 10 11 15 |
jpl | jpl 2880 | 8 9 16 | 5 8 21 | 11 13 20 |
mit | mit 2976 | 10 11 23 | 7 7 24 | 11 14 20 |
Table 5.1965.2 GPS week: 1965 Day: 2 MJD: 58001.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 7 8 21 | 9 8 28 | 7 6 16 |
emr | emr 2976 | 10 8 24 | 7 9 28 | 8 6 16 |
esa | esa 2976 | 6 7 20 | 9 8 31 | 7 4 17 |
gfz | gfz 2976 | 6 7 21 | 9 9 33 | 8 5 16 |
grg | grg 2975 | 8 9 24 | 9 8 33 | 10 6 23 |
igr | igr 2976 | 7 7 22 | 8 9 28 | 8 5 15 |
igs | igs 2976 | 7 7 21 | 8 9 31 | 8 4 17 |
jpl | jpl 3072 | 8 8 21 | 9 11 28 | 8 5 18 |
mit | mit 2976 | 7 7 20 | 8 11 34 | 9 4 16 |
Table 5.1965.3 GPS week: 1965 Day: 3 MJD: 58002.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 8 7 24 | 3 5 14 | 9 8 17 |
emr | emr 2976 | 10 5 28 | 5 6 17 | 11 6 19 |
esa | esa 2976 | 8 4 22 | 4 5 14 | 9 7 19 |
gfz | gfz 2976 | 8 6 23 | 4 6 16 | 10 7 19 |
grg | grg 2976 | 9 7 24 | 5 6 19 | 11 11 22 |
igr | igr 2976 | 8 5 22 | 4 5 15 | 9 6 18 |
igs | igs 2976 | 8 6 23 | 4 5 15 | 9 7 18 |
jpl | jpl 3072 | 11 6 25 | 4 6 16 | 11 9 22 |
mit | mit 2976 | 7 3 20 | 5 8 18 | 22 11 29 |
Table 5.1965.4 GPS week: 1965 Day: 4 MJD: 58003.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2973 | 7 10 17 | 6 8 18 | 9 6 18 |
emr | emr 2877 | 11 12 26 | 8 10 22 | 7 5 21 |
esa | esa 2880 | 8 10 17 | 6 9 19 | 10 7 21 |
gfz | gfz 2880 | 7 10 18 | 6 9 20 | 10 6 23 |
grg | grg 2879 | 8 11 17 | 8 8 21 | 12 8 25 |
igr | igr 2880 | 7 10 17 | 6 9 18 | 10 6 22 |
igs | igs 2880 | 7 10 17 | 6 9 18 | 10 6 21 |
jpl | jpl 2976 | 10 12 20 | 7 10 20 | 10 6 27 |
mit | mit 2880 | 8 9 15 | 8 12 24 | 12 12 31 |
Table 5.1965.5 GPS week: 1965 Day: 5 MJD: 58004.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 6 14 | 4 8 22 | 12 11 31 |
emr | emr 2976 | 9 8 19 | 7 8 21 | 10 11 31 |
esa | esa 2976 | 6 5 14 | 4 8 22 | 12 12 33 |
gfz | gfz 2976 | 8 9 16 | 5 9 21 | 12 11 33 |
grg | grg 2976 | 5 5 15 | 5 9 29 | 12 12 36 |
igr | igr 2976 | 6 5 13 | 4 8 20 | 11 11 30 |
igs | igs 2976 | 5 5 14 | 4 7 21 | 11 11 31 |
jpl | jpl 3072 | ---- ---- ---- | 4 8 24 | 12 14 35 |
mit | mit 2976 | 6 5 15 | 5 10 28 | 12 14 29 |
Table 5.1965.6 GPS week: 1965 Day: 6 MJD: 58005.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 8 9 17 | 7 8 17 | 9 10 19 |
emr | emr 2976 | 8 8 20 | 6 10 13 | 9 9 17 |
esa | esa 2976 | 8 9 17 | 7 8 18 | 10 9 20 |
gfz | gfz 2976 | 11 8 15 | 8 9 18 | 10 10 22 |
grg | grg 2976 | 10 8 17 | 8 10 20 | 12 13 27 |
igr | igr 2976 | 8 9 17 | 7 8 15 | 9 9 19 |
igs | igs 2976 | 8 9 17 | 7 8 16 | 10 9 20 |
jpl | jpl 3072 | 9 9 19 | 6 7 16 | 11 11 24 |
mit | mit 2976 | 8 9 17 | 7 9 19 | 10 8 24 |
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 6.1965 GPS week: 1965 MJD: 57999.500-58005.500
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 | 18 -8 -24 100 0 | 24 31
| 21 13 41 50 4 | 4
emr uuuux | 21 -34 219 147 18 | 47 58
| 32 16 152 30 40 | 7
esa uuuuu | -17 -4 42 61 7 | 29 37
| 8 13 53 45 5 | 4
gfz uuuuu | -15 -27 68 -121 -1 | 35 42
| 27 17 66 120 5 | 4
grg uuuuu | -2 0 11 -12 -5 | 4 21
| 26 21 48 91 2 | 5
igr xxxxx | -1 16 3 -19 4 | -2 24
| 8 9 30 60 6 | 4
irf xxxxx | 14 19 -57 -10 4 | -3 23
| 12 9 21 25 5 | 5
jpl xxxxx | 34 -4 29 40 7 | 27 35
| 16 24 77 47 16 | 3
mit uuuuu | 1 41 -132 -70 1 | 27 35
| 18 25 54 59 2 | 5
ngs uuuuu | 0 -11 -7 -47 5 | 19 31
| 38 20 75 134 7 | 3
sio uuuux | 15 50 -147 14 -10 | 97 99
| 13 25 49 36 9 | 8
Table 7.1965.0 GPS week: 1965 Day: 0 MJD: 57999.500
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 | 59 -20 1 172 -1 | 33 44
emr uuuux | 61 -47 402 169 -53 | 50 59
esa uuuuu | -14 -29 144 145 0 | 36 49
gfz uuuuu | -47 -8 30 -259 -4 | 44 54
grg uuuuu | 4 -25 -34 -130 -4 | 14 31
igr xxxxx | 7 25 -10 -14 1 | 6 33
irf xxxxx | 15 26 -96 -38 -7 | 7 35
jpl xxxxx | 47 -8 83 5 4 | 33 44
mit uuuuu | -25 79 -185 -175 2 | 38 50
ngs uuuuu | -6 -14 -68 59 9 | 26 43
sio uuuux | 17 78 -229 33 -16 | 111 114
Table 7.1965.1 GPS week: 1965 Day: 1 MJD: 58000.500
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 2 -58 55 -3 | 26 35
emr uuuux | -9 -34 285 110 38 | 39 51
esa uuuuu | -19 -3 9 58 8 | 29 40
gfz uuuuu | 27 -22 -55 -33 -4 | 37 46
grg uuuuu | -2 1 -13 25 -8 | 7 25
igr xxxxx | 0 26 -31 -81 9 | -2 27
irf xxxxx | 32 27 -32 -1 2 | -2 27
jpl xxxxx | 18 -2 174 -46 21 | 28 39
mit uuuuu | -9 23 -41 -52 1 | 30 39
ngs uuuuu | -4 3 20 -104 12 | 19 33
sio uuuux | 15 28 -75 26 -7 | 103 105
Table 7.1965.2 GPS week: 1965 Day: 2 MJD: 58001.500
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 | 28 -2 -71 70 -3 | 21 29
emr uuuux | 53 -40 231 127 36 | 38 51
esa uuuuu | -7 -6 23 79 2 | 25 34
gfz uuuuu | 10 -11 97 -6 -3 | 32 40
grg uuuuu | -40 18 -31 -74 -5 | 2 20
igr xxxxx | 3 18 48 -48 -3 | -5 24
irf xxxxx | 23 13 -53 27 7 | -7 23
jpl xxxxx | 20 -31 -16 39 -15 | 25 34
mit uuuuu | 30 7 -145 5 -1 | 25 33
ngs uuuuu | -65 5 52 -172 14 | 15 28
sio uuuux | 30 25 -135 42 -8 | 98 100
Table 7.1965.3 GPS week: 1965 Day: 3 MJD: 58002.500
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 6 -68 172 9 | 21 29
emr uuuux | 45 -49 262 137 42 | 44 57
esa uuuuu | -10 8 15 73 3 | 24 33
gfz uuuuu | -4 -59 125 -5 -7 | 31 39
grg uuuuu | -27 22 70 -76 -6 | 1 20
igr xxxxx | -15 11 35 -82 7 | -6 24
irf xxxxx | 2 22 -64 15 6 | -7 23
jpl xxxxx | 19 5 -45 72 2 | 23 32
mit uuuuu | 8 38 -150 -25 -1 | 24 32
ngs uuuuu | -22 -12 3 -234 5 | 16 29
sio uuuux | 34 62 -185 61 -12 | 96 98
Table 7.1965.4 GPS week: 1965 Day: 4 MJD: 58003.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 21 4 27 69 -2 | 24 29
emr uuuux | -22 -31 -35 123 -21 | 53 61
esa uuuuu | -20 12 6 7 12 | 28 33
gfz uuuuu | -41 -29 127 -76 6 | 34 39
grg uuuuu | 29 -15 81 125 -7 | 3 18
igr xxxxx | -6 19 16 -29 6 | -2 20
irf xxxxx | -2 10 -64 -19 9 | -4 19
jpl xxxxx | 29 15 2 85 19 | 26 32
mit uuuuu | 7 32 -189 -57 6 | 26 32
ngs uuuuu | 18 -6 23 -67 3 | 20 28
sio uuuux | 6 31 -126 -19 6 | 94 96
Table 7.1965.5 GPS week: 1965 Day: 5 MJD: 58004.500
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 -26 -7 79 0 | 23 28
emr uuuux | 3 -35 323 165 29 | 51 59
esa uuuuu | -23 -4 84 25 8 | 28 33
gfz uuuuu | -30 -29 105 -182 -1 | 33 39
grg uuuuu | -9 21 26 -31 -3 | 1 18
igr xxxxx | 5 5 -18 33 -5 | -3 20
irf xxxxx | 12 27 -52 -21 7 | -5 19
jpl xxxxx | 60 31 28 54 -11 | 27 32
mit uuuuu | 4 68 -128 -72 0 | 25 30
ngs uuuuu | 55 -53 -147 67 1 | 19 27
sio uuuux | 0 85 -151 -16 -21 | 91 93
Table 7.1965.6 GPS week: 1965 Day: 6 MJD: 58005.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 11 -19 10 83 1 | 22 26
emr uuuux | 18 0 68 195 57 | 54 65
esa uuuuu | -29 -4 11 40 12 | 29 35
gfz uuuuu | -20 -30 44 -285 6 | 32 36
grg uuuuu | 28 -19 -19 76 -2 | 0 16
igr xxxxx | -4 5 -22 84 10 | -5 18
irf xxxxx | 14 5 -40 -32 7 | -5 18
jpl xxxxx | 43 -37 -25 73 25 | 25 30
mit uuuuu | -9 43 -83 -112 1 | 24 29
ngs uuuuu | 24 2 68 123 -7 | 19 28
sio uuuux | 4 39 -130 -32 -11 | 88 89
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