[IGSREPORT-23341] Wk 1828 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Feb 5 07:32:07 PST 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1828 (Jan 18, 2015 - Jan 24, 2015)
Contacts: igs.acc at noaa.gov
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:
igs1828[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1828[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1828[0-6].cls IGS GPS clock combination summary report.
igs18287.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18287.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 | MDVJ
0 | EMR | 8
0 | GFZ | 1 2 3 6 9 30 1 3 6 30 BOGT CEDU INVK MDVJ BOGT MDVJ
0 | GRG | BOGT BRST HOB2 MCM4 QAQ1 BOGT BRST HOB2 MCM4 QAQ1
0 | JPL | 8 HOB2
0 | MIT | 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20
0 | MIT | 21 22 23 24 25 27 28 29 30 31 32 1 2 3 4 5 6 7 8
0 | MIT | 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25
0 | MIT | 27 28 29 30 31 32
1 | COD | TLSE
1 | EMR | 8 8
1 | GFZ | 1 2 3 6 9 30 1 3 6 8 30 ALBH ALGO ALIC ALRT ARTU
1 | GFZ | ASPA AUCK BAKE BARH BJFS BOGT BOR1 BRFT BRMU CAS1
1 | GFZ | CEDU CHTI CHUR CONZ CORD CRO1 DARW DAV1 DRAG DRAO
1 | GFZ | DUBO FAIR FLIN GLPS GLSV GODE GOLD GOPE GRAS GRAZ
1 | GFZ | GUAM GUUG HARB HNPT HOB2 HOFN HOLB HOLM IISC INVK
1 | GFZ | IRKJ ISPA KELY KERG KIRU KOUC KOUR LAMA MAC1 MAG0
1 | GFZ | MAL2 MANA MAS1 MATE MAW1 MCM4 MDVJ NANO NICO NKLG
1 | GFZ | NLIB NOVM NRIL NTUS NYA1 NYAL ONSA OPMT PDEL PERT
1 | GFZ | PIE1 POL2 QAQ1 RABT REUN REYK SANT SCH2 SCOR SFER
1 | GFZ | SOFI SSIA STHL STJO SUWN SYOG THTI THU3 TIDB TOW2
1 | GFZ | TRO1 TWTF USUD VILL WES2 WHIT WILL WSRT WTZR XMIS
1 | GFZ | YAKT YELL ZECK NTUS TLSE
1 | GRG | REUN KOUC REUN
1 | MIT | 1 10 19 27 10 19 27 CONZ
2 | COD | 7 BOR1 GRAZ
2 | EMR | 8
2 | ESA | HOB2 MAG0
2 | GFZ | 1 2 3 6 30 1 3 6 8 30 BOR1 HYDE
2 | GRG | 15 DARW HYDE MCM4 DARW
2 | JPL | 15
2 | MIT | 8 15 19 1 8 15 18 19 TLSE
3 | COD | 31 NRIL
3 | EMR | 8
3 | ESA | NTUS NTUS
3 | GFZ | 1 2 3 6 9 30 1 3 6 8 30 HOB2 TOW2 HOB2
3 | GRG | DAV1 MCM4 TLSE DAV1 MAL2 TLSE
3 | JPL | 8 MAG0
3 | MIT | 2 11 20 2 8 11 20 CONZ HARB
4 | COD | TRO1
4 | EMR | 8 30
4 | ESA | 4 22 29 31 4 PIMO TRO1 MAG0
4 | GFZ | 1 2 3 6 9 30 1 3 6 8 30 ALRT
4 | GRG | MCM4 REUN TLSE TRO1 USNO WES2 REUN TLSE TRO1 USNO
4 | GRG | WES2
4 | JPL | 8 30 TIXI TLSE
4 | MIT | 11 19 3 11 15 19 MOBS
5 | COD | 30 MCM4 MCM4
5 | EMR | 30
5 | ESA | 8 MDVJ
5 | GFZ | 1 2 3 6 8 9 30 1 3 6 30
5 | GRG | DRAG MDVJ NLIB DRAG MDVJ SCH2
5 | MIT | 8 19 19 30
6 | ALL | 30
6 | COD | 8 BOR1
6 | ESA | 8 TIXI
6 | GFZ | 1 2 3 6 1 3 6 BOR1 NRMD NRMD
6 | GRG | DAV1 DAV1 IISC
6 | MIT | 5 8 10 11 15 19 28 1 5 8 9 10 11 12 14 15 18 19 27
6 | MIT | 28 31 KOUR MDVJ
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
4 | GFZ | ~23:55 | ~ -0.12 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
0 | COD | 24
4 | COD | 30
6 | ESA | 30
8. 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 G24 | 4 | | | | | | |
PRN G30 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
9. 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.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.7 -1.4 -2.3 -16 18 -11 .74
EMR | 0 | 4.5 -3.0 14.4 11 12 2 .46
ESA | 0 | -.3 -.9 .0 -27 -16 45 .23
GFZ | 0 | .0 -1.3 -2.9 -27 -59 22 .75
GRG | 0 | 1.5 -.2 -11.4 18 -16 38 .63
JPL | 0 | 3.2 -5.8 7.3 -2 -5 12 .45
MIT | 0 | 6.6 -4.3 9.1 15 12 -22 .74
NGS | 0 | -2.4 .6 11.6 -8 26 -12 .71
SIO | 0 | -.9 -11.1 25.5 58 2 -10 .54
COD | 1 | -1.7 -1.0 -1.6 -7 7 -23 .44
EMR | 1 | 5.8 -6.0 13.5 24 13 -12 .35
ESA | 1 | -.3 -.8 -.1 -16 -23 55 .17
GFZ | 1 | .3 -.1 -2.5 -34 -72 8 .65
GRG | 1 | 3.8 -6.2 -11.3 3 -22 43 .40
JPL | 1 | 2.4 -4.6 9.3 -64 0 -18 -.03
MIT | 1 | 5.6 -4.0 4.8 -1 15 -30 .55
NGS | 1 | -.1 -1.4 9.8 -22 3 -9 .39
SIO | 1 | -.1 -4.7 19.0 10 5 -4 .33
COD | 2 | -1.1 -1.4 -1.4 -13 -8 -2 .67
EMR | 2 | .5 -.7 15.0 7 16 8 .46
ESA | 2 | .2 -.8 -.4 -15 -11 70 .21
GFZ | 2 | .6 -1.1 -3.3 -26 -76 23 .78
GRG | 2 | -3.9 -1.2 -4.3 -21 -31 56 .51
JPL | 2 | 1.8 -5.2 9.3 0 -10 32 .27
MIT | 2 | 3.5 -1.7 8.7 8 14 -34 .63
NGS | 2 | .0 -5.9 13.0 -45 0 -20 .31
SIO | 2 | 2.2 -3.5 21.0 17 6 -15 .61
COD | 3 | -1.1 -1.3 -1.9 -23 -4 -11 .72
EMR | 3 | 7.2 -2.3 15.6 35 11 8 .34
ESA | 3 | .3 -1.2 -.3 -20 -10 56 .22
GFZ | 3 | .4 -.2 -2.6 -36 -63 5 .61
GRG | 3 | 9.8 .3 -9.3 1 -35 66 .56
JPL | 3 | 15.6 -5.0 9.9 -39 2 -19 .26
MIT | 3 | 9.2 .8 5.4 2 8 -27 .66
NGS | 3 | 7.1 -4.3 19.0 -50 -5 25 .69
SIO | 3 | 5.9 -3.1 19.6 10 11 -26 .45
COD | 4 | -1.3 -.4 -1.9 -23 1 -9 .58
EMR | 4 | 12.1 -5.4 15.6 41 8 10 .24
ESA | 4 | 1.2 -1.2 .0 -28 -27 77 .41
GFZ | 4 | .6 -.7 -2.2 -36 -52 6 .99
GRG | 4 | 6.0 -1.7 -10.8 4 -22 33 .97
JPL | 4 | 9.3 -6.9 9.3 -116 3 -19 .31
MIT | 4 | 6.9 -4.8 3.4 3 9 -32 .68
NGS | 4 | 7.7 -.9 15.5 -36 -26 31 .64
SIO | 4 | 6.0 -4.9 18.9 -9 39 -10 .55
COD | 5 | -2.2 -.6 -1.4 -45 -6 -18 .62
EMR | 5 | 9.8 .7 22.1 51 6 4 .30
ESA | 5 | .6 -.7 .0 -32 -19 54 .49
GFZ | 5 | .2 -.3 -2.8 -51 -67 3 .83
GRG | 5 | 1.0 -8.3 -5.2 1 -36 35 .91
JPL | 5 | 7.3 -3.4 20.7 -28 18 16 .78
MIT | 5 | 1.4 -2.8 1.2 -2 15 -40 .72
NGS | 5 | 5.9 -1.5 6.8 -30 -16 21 .50
SIO | 5 | 4.4 -7.8 15.2 -18 28 -17 .68
COD | 6 | -2.0 -.1 -.5 -36 5 1 .60
EMR | 6 | 5.4 6.3 20.3 33 -2 4 .48
ESA | 6 | .8 -.8 .0 -31 -16 56 .30
GFZ | 6 | .4 -.6 -2.6 -41 -78 14 .93
GRG | 6 | 3.8 -4.7 -5.4 -13 -18 63 .82
JPL | 6 | 5.9 -1.5 20.1 -28 25 -34 .99
MIT | 6 | 1.7 -2.6 4.3 19 16 -14 .73
NGS | 6 | -6.0 4.5 11.6 -24 15 -27 .50
SIO | 6 | 1.9 -7.1 18.7 3 7 -24 .71
11. 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.
12. 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.
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 1.1828.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1828.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 2.1828.[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 3.1828.[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 5.1828.0-6). 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 1828 summary. (Jan 18, 2015 - Jan 24, 2015)
Table 1.1828.a GPS week: 1828 MJD: 57040.000-57046.000
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 246| -1 2 1 16 8 0 -.04 15 13 | -320 -1602 18 120
| 0 1 1 9 19 12 .02 | 404 922
emr 80| 1 -2 3 -16 -11 19 .15 13 13 | 96124 434 20 157
| 1 2 1 21 9 11 .02 | 242618 589
esa 150| 0 0 5 -10 -3 1 -.33 12 12 | 260 -298 13 168
| 0 2 3 8 12 7 .02 | 716 1463
gfz 197| 1 0 -5 19 -8 8 .06 11 10 | -134 96 15 175
| 0 0 1 13 13 15 .02 | 527 944
grg 173| 3 0 -7 -25 17 -36 .12 17 16 | -36 203 20 170
| 1 1 3 8 24 11 .08 | 183 409
igr n/a| 0 0 -1 -17 2 -5 -.15 5 5 | 7168 82 16 98
| 0 0 1 12 16 6 .05 | 613 588
jpl 80| 1 0 3 -8 -5 0 .15 11 11 | 543280 -729 18 120
| 1 1 1 21 22 34 .04 | 1425576 2688
mit 349| 0 0 -3 31 0 7 -.08 14 12 | -135 -190 35 221
| 1 0 1 38 23 12 .02 | 175 418
ngs 221| -1 0 3 -20 3 -13 .01 10 9 | -302 -1523 1259 2791
| 1 0 2 23 33 19 .04 | 510 1035
sio 325| -1 -1 -4 20 -7 10 -.11 15 15 | --- --- --- ---
| 1 0 2 25 35 20 .01 | --- ---
Table 1.1828.b GPS week : 1828 MJD: 57040.000-57046.000
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 5 |
2 | 4 4 4 4 5 4 4 |
3 | 4 4 4 4 4 4 4 |
4 | 5 4 4 4 5 4 4 |
5 | 4 4 5 5 4 5 5 |
6 | 4 4 4 4 4 4 5 |
7 | 4 5 4 5 5 5 5 |
8 | 8 9 9 8 7 9 9 |
9 | 4 4 4 4 4 4 4 |
10 | 3 4 4 4 4 4 5 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 5 5 5 5 5 5 |
14 | 5 5 5 5 6 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 4 4 4 5 |
17 | 5 5 5 5 5 5 5 |
18 | 4 4 5 5 5 5 4 |
19 | 4 4 4 4 4 4 4 |
20 | 5 4 4 4 4 4 5 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 11 6 5 5 5 5 4 |
25 | 4 5 5 4 4 4 4 |
27 | 4 5 5 4 4 5 4 |
28 | 4 5 5 4 4 4 5 |
29 | 5 5 5 6 5 5 5 |
30 | 4 5 6 6 5 8 0 |
31 | 5 5 5 4 4 4 4 |
32 | 4 4 3 3 3 3 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1828.0 GPS week: 1828 Day: 0 MJD: 57040.000
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 249| -1 3 0 31 -4 -5 -.04 12 12 | -198 -1447 14 120
emr 80| -1 -4 4 -28 -13 25 .13 11 11 | 4093 724 18 124
esa 150| -1 1 8 -28 -28 10 -.36 11 10 | -603 1549 11 152
gfz 203| 2 0 -5 15 -4 20 .02 11 10 | -1271 2024 15 179
grg 174| 5 1 -12 -16 37 -51 .06 17 17 | -147 1007 18 166
igr n/a| 0 0 0 -14 7 -14 -.14 5 4 | 7488 756 15 98
jpl 80| 1 1 1 -8 -25 5 .18 11 11 | 4125 708 17 130
mit 349| 1 0 -3 7 31 -3 -.11 14 13 | 188 37 68 358
ngs 182| -1 0 3 4 35 -35 .02 10 8 | -533 -842 1227 3011
sio 329| -1 -2 -6 24 -18 24 -.12 16 15 | --- --- --- ---
Table 2.1828.1 GPS week: 1828 Day: 1 MJD: 57041.000
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 251| 0 2 0 25 18 11 -.01 13 12 | -909 -305 14 112
emr 80| 2 -4 4 -20 -7 30 .15 13 13 | 3549 148 17 166
esa 150| -1 1 2 -2 -10 5 -.34 12 12 | -788 1478 11 150
gfz 200| 0 0 -5 8 12 9 .07 10 9 | 17 -184 11 168
grg 174| 6 1 -11 -19 35 -27 .06 19 18 | -60 319 18 178
igr n/a| 0 0 0 -24 0 -9 -.15 5 5 | 7059 5 16 100
jpl 80| 2 0 1 -15 -35 -49 .15 12 12 | 3565 153 17 112
mit 349| 1 0 -1 29 -35 12 -.07 15 13 | -367 319 30 186
ngs 232| -2 1 4 -2 29 0 .00 9 8 | -604 -759 1188 2678
sio 327| -1 0 -3 -12 -34 21 -.11 14 13 | --- --- --- ---
Table 2.1828.2 GPS week: 1828 Day: 2 MJD: 57042.000
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 247| -1 3 0 19 -6 -14 -.04 13 12 | -225 -2280 13 109
emr 80| 0 -3 4 -41 -22 32 .12 12 12 | 3197 920 19 155
esa 150| 0 1 1 -10 0 -13 -.35 11 11 | 735 -979 13 167
gfz 200| 0 0 -6 20 -30 8 .09 12 11 | -180 152 14 180
grg 176| 3 1 -6 -32 25 -48 .03 17 16 | 125 -237 17 195
igr n/a| -1 0 0 -30 -21 -9 -.16 5 5 | 6701 448 15 92
jpl 80| 1 0 5 15 -4 39 .17 12 12 | 3217 915 16 105
mit 349| 0 -1 -1 31 28 21 -.04 14 12 | -89 -250 30 170
ngs 230| -2 0 4 -32 -3 -35 .04 11 10 | -386 -2017 1296 2569
sio 330| -1 0 -3 39 0 8 -.11 14 15 | --- --- --- ---
Table 2.1828.3 GPS week: 1828 Day: 3 MJD: 57043.000
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 241| -1 3 2 9 -6 -3 -.08 16 13 | -383 -1260 17 126
emr 80| 1 -3 1 -37 5 22 .13 12 12 | 3975 -229 16 149
esa 150| 0 2 4 -8 9 0 -.31 12 12 | 246 -549 11 182
gfz 194| 0 0 -4 23 -2 -22 .08 11 11 | -83 154 12 184
grg 175| 2 0 -8 -16 43 -28 .11 16 15 | -23 37 17 178
igr n/a| -1 0 -2 -27 0 1 -.17 5 5 | 6977 10 17 104
jpl 80| 1 -1 2 -28 -17 17 .08 11 11 | 4056 -257 16 122
mit 350| 0 -1 -3 58 -7 -1 -.09 12 12 | -217 18 27 192
ngs 225| -3 0 4 -31 0 0 .07 10 9 | -257 -1526 1339 2813
sio 325| 0 -1 -2 49 -36 -1 -.10 15 15 | --- --- --- ---
Table 2.1828.4 GPS week: 1828 Day: 4 MJD: 57044.000
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 241| -1 4 1 1 0 14 -.04 20 13 | -567 -1274 18 118
emr 81| 2 -5 4 2 -8 15 .17 14 14 | 646326 1273 15 148
esa 150| 0 0 4 -5 -3 0 -.31 11 11 | 1168 -2683 10 224
gfz 195| 1 0 -8 47 -13 14 .06 10 9 | 204 -1080 15 185
grg 174| 2 0 -7 -38 -20 -24 .17 16 15 | -361 -76 19 155
igr n/a| 0 0 -1 -15 12 -5 -.19 5 5 | 6280 660 17 108
jpl 80| 0 -1 3 -37 17 -43 .20 12 12 | 3776184 -6732 17 114
mit 350| -2 -1 -4 11 -10 27 -.08 12 12 | -222 -1017 32 220
ngs 230| -1 1 4 6 30 -27 .00 9 9 | -972 -513 1184 2829
sio 321| -3 -1 -1 -8 -13 35 -.09 16 16 | --- --- --- ---
Table 2.1828.5 GPS week: 1828 Day: 5 MJD: 57045.000
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 242| 0 1 5 15 13 -11 -.03 16 13 | -377 -1413 17 128
emr 79| 1 1 3 16 -18 12 .13 13 13 | 5728 504 16 170
esa 150| 0 0 5 -6 7 5 -.33 12 12 | 678 -566 9 155
gfz 196| 1 -1 -6 8 -1 2 .04 10 9 | 311 -224 9 159
grg 171| 1 0 -2 -22 2 -46 .16 15 14 | 198 36 15 156
igr n/a| 0 0 -1 -11 28 3 -.03 5 5 | 8159 -459 15 78
jpl 80| 0 0 5 20 3 28 .15 11 11 | 5760 475 17 132
mit 349| -1 0 -4 -15 0 -1 -.07 13 12 | -189 -171 27 180
ngs 228| 0 0 0 -31 0 -11 -.02 11 9 | 10 -1452 1175 2809
sio 323| -1 -2 -4 7 -18 14 -.10 16 15 | --- --- --- ---
Table 2.1828.6 GPS week: 1828 Day: 6 MJD: 57046.000
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 251| -1 0 2 13 46 12 -.06 13 13 | 416 -3240 34 132
emr 80| 0 1 3 -8 -18 -1 .18 13 13 | 6000 -299 44 188
esa 150| 1 -4 10 -9 -2 2 -.34 14 14 | 384 -339 30 147
gfz 196| 0 0 -4 14 -18 25 .06 11 11 | 63 -167 31 171
grg 170| 2 -1 -5 -32 -4 -27 .25 16 15 | 10 340 37 165
igr n/a| 0 0 -3 4 -11 -7 -.19 5 5 | 7514 -842 21 107
jpl 80| 1 2 4 -2 24 0 .15 12 12 | 6056 -371 28 127
mit 349| 0 -1 -5 101 -6 -4 -.09 14 13 | -49 -272 35 245
ngs 226| -1 0 0 -55 -62 12 -.06 8 8 | 627 -3553 1406 2832
sio 323| 0 -1 -8 45 69 -27 -.11 15 15 | --- --- --- ---
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 3.1828.0 GPS week: 1828 Day: 0 MJD: 57040.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 10 13 10 18 4 7 12 7 16 4 | 28 30 34 24 38 26 31 30 27 37 29
2 | 13 11 8 10 20 5 12 15 8 11 4 | 29 27 17 23 27 19 27 22 24 21 22
X3 | 8 10 12 10 --- 3 12 10 8 10 3 | 17 17 20 16 --- 14 22 18 15 17 14
4 | 12 13 8 11 16 5 8 18 7 21 4 | 51 55 50 51 49 48 52 61 49 57 51
5 | 8 12 12 12 13 4 11 16 10 16 4 | 38 41 40 40 36 37 43 38 38 42 38
6 | 9 7 13 7 16 4 12 15 6 11 3 | 32 35 35 28 34 29 38 27 32 29 31
7E | 20 13 9 7 17 3 8 12 10 13 4 | 55 58 58 60 62 57 60 59 61 60 58
X8E | 36 17 17 14 18 8 16 14 23 --- 7 | 56 36 34 31 14 35 34 27 40 --- 33
9 | 8 8 15 7 16 3 8 9 9 8 3 | 29 36 30 29 34 28 38 29 29 31 30
10 | 7 7 9 6 13 4 8 11 7 10 3 | 27 24 23 26 29 22 25 28 24 23 24
11E | 10 6 8 10 19 4 8 13 6 14 3 | 42 40 37 40 47 37 40 46 42 40 40
12 | 19 9 10 14 23 4 11 14 10 13 4 | 30 29 24 28 32 23 29 27 25 27 25
13 | 10 16 14 11 23 4 14 12 11 17 5 | 26 35 24 30 42 25 36 28 21 26 27
14 | 10 11 13 13 18 5 14 21 11 19 5 | 31 31 28 41 40 29 32 34 28 32 31
15 | 14 13 12 12 16 5 12 14 11 23 5 | 46 49 43 41 39 40 46 40 42 49 42
16 | 20 12 8 14 20 5 11 13 13 19 5 | 31 23 18 22 22 17 23 17 18 14 17
17 | 10 13 9 14 21 5 12 17 9 14 4 | 29 32 21 26 36 23 34 14 25 25 25
18 | 13 12 10 9 16 7 10 9 12 18 4 | 24 22 19 28 25 19 23 22 29 26 22
19 | 9 12 7 10 18 4 11 15 8 16 4 | 25 24 19 21 26 18 25 22 21 22 19
20 | 10 9 11 14 14 4 8 16 11 20 4 | 28 26 25 26 31 21 26 29 20 25 24
21 | 14 9 7 9 18 6 11 10 9 15 4 | 27 24 20 25 30 21 24 20 22 16 21
22 | 10 8 10 8 14 6 10 10 10 18 3 | 27 27 26 32 34 26 29 27 32 31 28
23 | 11 13 12 14 17 4 10 13 13 22 4 | 27 30 21 29 30 21 29 24 21 16 22
X24E | 79 19 22 17 32 10 --- 18 42 24 11 | 195 181 175 171 179 175 --- 177 171 189 174
25 | 11 13 15 8 18 4 11 10 11 10 4 | 21 31 28 21 29 23 28 21 27 23 24
27 | 15 12 13 8 14 3 12 12 6 17 4 | 29 25 31 25 25 23 25 24 25 29 24
28 | 8 11 11 10 16 5 11 18 8 11 4 | 24 31 21 25 34 22 31 27 25 26 25
29 | 17 15 7 12 19 5 14 14 12 15 5 | 27 23 18 26 23 19 25 18 22 21 20
30E | 12 13 15 9 19 4 9 10 8 16 4 | 548 53 544 48 53 546 52 47 49 47 545
31E | 10 10 9 8 13 4 11 23 11 13 4 | 41 43 37 43 45 39 42 56 42 46 42
32 | 10 12 8 10 15 5 7 9 6 14 3 | 19 24 16 17 22 16 22 16 18 21 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 11 11 11 17 5 11 14 10 16 |T 53 37 49 35 38 48 33 34 34 35 49
WRMS | 12 11 10 10 17 4 11 13 8 15 |NE 28 30 26 28 31 24 30 26 26 27 26
MEDI | 10 12 11 10 17 4 11 13 10 15 |MD 29 31 26 28 34 23 29 27 27 26 25
Table 3.1828.1 GPS week: 1828 Day: 1 MJD: 57041.000
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 | 13 13 13 11 16 3 8 12 6 17 4 | 30 34 35 28 32 28 33 26 30 38 30
2 | 14 14 8 9 19 5 11 15 10 10 4 | 25 24 17 21 22 17 24 22 22 19 19
X3 | 8 10 11 11 --- 3 14 10 8 7 3 | 15 16 18 16 --- 13 20 12 17 15 12
4 | 10 15 9 7 20 7 9 15 8 14 4 | 30 41 31 30 30 32 33 33 33 37 31
5 | 9 11 14 12 12 5 12 16 8 14 4 | 29 32 26 27 24 25 31 32 29 29 27
6 | 8 11 10 9 16 4 11 12 7 12 3 | 28 32 32 25 33 25 32 26 26 30 27
7E | 18 15 10 9 19 3 12 11 12 10 4 | 65 61 63 65 61 63 61 65 67 63 63
X8E | 25 25 18 15 --- 9 --- 17 22 --- 9 | 45 36 31 29 --- 32 --- 27 40 --- 31
9 | 12 8 15 5 15 2 9 8 7 8 3 | 27 28 23 23 27 22 30 24 26 24 24
10 | 6 9 11 9 16 4 10 11 6 13 3 | 22 20 22 22 23 18 23 24 21 19 20
11E | 13 11 9 6 17 6 8 15 7 13 3 | 34 37 34 34 37 33 35 33 35 34 33
12 | 19 12 13 10 24 4 12 18 8 13 5 | 24 24 15 19 28 15 26 21 21 17 18
13 | 7 15 15 11 21 4 15 13 11 9 4 | 26 33 21 25 36 21 35 23 24 23 25
14 | 13 13 14 10 18 5 13 22 10 16 5 | 25 29 22 31 31 22 28 25 24 25 24
15 | 10 14 15 10 15 6 16 17 10 16 4 | 28 35 31 28 28 26 35 29 28 34 28
16 | 20 13 13 13 23 5 12 11 11 17 5 | 27 22 18 19 22 15 22 15 18 12 15
17 | 7 16 6 12 23 4 18 16 8 10 4 | 26 32 19 24 35 20 36 15 24 19 22
18 | 10 11 12 12 17 5 11 12 11 17 4 | 21 20 20 26 19 17 21 20 18 19 18
19 | 9 10 10 9 21 5 16 14 9 15 4 | 21 22 17 19 26 16 25 19 18 15 16
20 | 10 13 12 10 12 4 10 16 8 17 4 | 24 24 22 19 24 18 26 26 21 21 20
21 | 12 12 10 9 17 7 10 13 10 13 4 | 21 22 16 22 26 15 20 16 18 15 16
22 | 10 9 10 9 18 5 12 13 10 15 4 | 21 23 20 25 26 19 23 20 23 21 20
23 | 10 13 13 13 18 5 12 12 9 22 4 | 25 29 21 27 23 20 31 24 23 13 21
X24E | 24 12 15 11 21 7 20 11 14 --- 6 | 67 58 60 59 60 59 29 58 61 --- 58
25 | 13 13 16 10 20 4 12 12 8 11 4 | 17 24 21 23 26 16 25 17 19 15 18
27 | 14 15 16 11 18 4 13 12 8 16 4 | 28 26 29 24 26 20 23 21 22 23 22
28 | 9 16 11 10 19 5 13 18 10 10 4 | 21 31 19 19 31 19 30 23 24 19 21
29 | 21 15 9 10 19 6 13 16 10 19 5 | 27 20 15 24 24 16 23 19 22 18 18
30E | 15 20 16 12 23 5 12 10 9 7 5 | 332 45 336 40 40 335 41 43 46 41 332
31E | 16 12 11 11 17 5 13 29 9 13 5 | 41 40 34 42 40 37 36 57 41 42 40
32 | 7 11 8 8 21 4 9 8 7 12 3 | 16 20 15 16 21 14 21 16 16 15 14
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 13 12 10 19 5 12 15 9 14 |T 38 30 35 27 30 33 29 26 27 24 34
WRMS | 12 13 12 9 18 5 12 13 8 13 |NE 24 26 21 23 26 19 27 21 22 21 21
MEDI | 12 13 12 10 18 5 12 13 9 13 |MD 26 29 22 25 27 20 28 24 24 21 22
Table 3.1828.2 GPS week: 1828 Day: 2 MJD: 57042.000
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 9 12 11 17 6 8 10 10 13 4 | 23 27 27 21 28 22 27 22 24 29 23
2 | 13 13 7 11 16 6 13 14 9 12 4 | 23 27 18 23 19 19 25 21 24 20 20
X3 | 6 10 10 13 --- 5 12 8 7 9 3 | 14 17 17 14 --- 12 18 13 17 14 12
4 | 11 12 9 13 17 5 9 15 9 16 4 | 26 32 27 27 28 25 29 33 28 32 27
5 | 7 12 12 14 14 6 14 14 10 16 4 | 30 36 31 33 26 30 38 35 37 35 32
6 | 11 9 12 11 15 3 10 12 9 15 4 | 32 36 33 26 30 28 35 29 32 27 30
7E | 14 15 8 12 18 4 12 8 12 11 4 | 50 44 45 45 49 43 46 49 49 49 45
X8E | 20 20 18 13 --- 11 --- 14 25 --- 8 | 43 37 34 35 --- 36 --- 29 40 --- 33
9 | 9 8 12 7 15 4 8 8 11 10 3 | 26 29 24 24 29 23 34 24 23 24 25
10 | 8 8 8 12 10 4 11 11 8 12 3 | 22 22 21 23 22 18 21 26 22 21 21
11E | 9 10 8 12 16 5 9 17 9 12 4 | 29 31 28 30 31 28 31 29 32 27 28
12 | 17 12 11 12 26 4 9 17 16 13 5 | 29 27 21 26 31 22 26 26 29 22 23
13 | 8 17 14 14 21 4 14 14 12 14 5 | 25 36 23 31 39 25 34 26 22 26 26
14 | 11 13 13 13 17 6 12 22 12 20 5 | 28 31 27 40 33 28 32 34 31 31 30
15 | 10 14 12 14 15 6 14 16 10 18 4 | 35 40 35 33 30 31 39 33 34 37 33
16 | 16 10 10 14 17 6 12 11 11 17 4 | 27 23 20 24 24 18 22 17 16 10 17
17 | 8 17 5 13 23 4 15 15 10 14 4 | 25 32 20 24 35 22 34 14 25 21 23
18 | 14 11 9 12 14 4 9 12 14 17 4 | 21 21 20 25 17 21 21 21 28 22 20
19 | 10 11 9 8 19 4 12 12 9 15 4 | 25 25 18 21 29 17 25 20 21 22 20
20 | 10 12 10 13 11 4 11 14 9 17 4 | 20 23 21 20 15 17 21 21 18 20 17
21 | 12 12 7 10 16 6 11 12 10 12 4 | 22 25 17 22 24 18 24 21 20 18 19
22 | 12 7 10 9 14 6 10 12 12 16 4 | 24 26 25 31 28 25 25 24 33 24 25
23 | 11 11 12 15 16 6 13 10 11 20 4 | 25 27 22 28 24 20 28 22 19 14 20
24E | 24 9 14 12 17 5 13 9 14 11 5 | 60 56 55 53 55 53 20 54 51 44 53
25 | 13 15 14 8 16 6 12 12 11 11 4 | 19 27 23 19 26 19 23 19 25 20 20
27 | 12 13 14 9 15 3 11 10 12 16 4 | 27 25 29 29 27 25 24 25 30 23 25
28 | 9 13 9 11 18 3 14 15 10 14 4 | 22 30 20 24 34 21 31 23 25 18 23
29 | 21 16 8 12 19 6 12 14 11 15 5 | 26 24 14 21 26 17 21 19 21 20 17
30E | 25 13 18 15 23 5 12 10 12 7 5 | 517 35 507 35 38 506 33 34 34 34 515
31E | 13 12 10 8 12 5 13 25 11 12 4 | 56 55 52 54 58 54 57 66 56 58 56
32 | 10 7 7 9 15 4 7 7 7 15 3 | 18 22 16 18 25 15 21 14 19 17 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 11 12 17 5 12 14 11 14 |T 44 30 41 28 30 40 28 27 28 25 41
WRMS | 12 12 11 11 16 5 12 12 10 15 |NE 24 27 22 25 27 21 27 23 24 22 22
MEDI | 11 12 10 12 16 5 12 12 11 14 |MD 26 27 23 26 28 22 26 24 25 22 23
Table 3.1828.3 GPS week: 1828 Day: 3 MJD: 57043.000
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 | 11 9 13 9 15 5 9 8 6 19 4 | 21 23 28 21 27 19 22 24 22 32 22
2 | 13 13 7 11 17 4 14 13 10 11 4 | 24 25 17 20 23 17 24 20 21 22 19
X3 | 8 8 10 12 --- 4 10 7 8 13 3 | 11 14 17 14 --- 11 17 10 15 14 11
4 | 10 14 9 9 15 5 8 12 10 17 4 | 24 29 24 23 21 22 28 30 27 31 25
5 | 6 10 13 11 16 6 13 16 10 19 4 | 33 36 33 32 33 31 37 35 36 35 33
6 | 8 9 10 11 13 3 9 11 10 16 3 | 27 32 33 25 31 26 30 25 28 29 27
7E | 24 21 10 8 25 4 15 8 11 8 5 | 76 74 73 74 75 73 73 76 76 75 74
X8E | 31 16 17 11 --- 10 18 16 20 --- 7 | 53 35 31 30 --- 32 36 25 33 --- 30
9 | 10 8 14 7 14 4 9 9 9 12 3 | 27 29 26 24 29 24 32 26 26 26 25
10 | 6 10 9 16 10 4 11 11 8 13 4 | 19 23 21 26 23 20 22 27 22 20 21
11E | 10 15 8 8 16 4 10 11 7 15 4 | 23 24 18 20 29 18 23 26 23 27 21
12 | 21 10 11 12 20 6 12 15 9 19 5 | 26 26 16 24 29 19 25 23 25 20 20
13 | 12 15 14 15 20 4 15 16 11 15 5 | 27 33 23 32 39 26 35 30 23 31 27
14 | 14 10 15 14 15 5 12 25 11 15 5 | 23 27 21 37 33 26 26 31 28 25 26
15 | 13 13 15 12 15 5 13 15 11 19 5 | 39 44 40 36 34 36 43 33 35 40 36
16 | 17 10 11 9 18 6 10 9 10 17 4 | 25 22 19 20 22 17 21 16 21 13 17
17 | 9 20 8 15 21 5 16 14 12 10 5 | 26 33 20 26 33 21 31 14 27 19 22
18 | 16 10 13 11 14 4 8 12 12 19 4 | 21 21 19 20 18 15 19 16 22 18 16
19 | 11 10 11 11 17 5 13 10 9 16 4 | 21 24 17 22 21 17 23 15 19 17 17
20 | 11 11 10 12 12 5 10 11 9 19 4 | 22 24 22 22 24 21 22 25 23 19 20
21 | 10 11 10 9 18 4 11 12 9 15 4 | 20 25 15 20 27 16 20 16 18 12 17
22 | 12 9 12 8 12 4 9 14 11 14 4 | 21 24 21 24 27 22 25 21 25 20 21
23 | 11 10 13 13 17 5 12 10 12 23 4 | 21 28 20 27 26 20 29 24 20 12 20
24E | 26 8 16 13 19 6 11 9 12 14 5 | 58 55 56 54 59 54 18 52 55 45 53
25 | 17 12 13 7 13 6 11 12 8 13 4 | 17 27 22 20 23 16 23 19 20 19 19
27 | 13 13 13 11 13 6 10 7 9 15 4 | 25 27 26 24 21 22 27 20 25 24 23
28 | 9 13 10 10 14 3 13 12 10 9 4 | 21 29 20 22 29 19 27 22 22 18 21
29 | 25 17 10 15 14 6 14 17 13 18 5 | 29 24 13 24 22 16 22 21 22 21 18
30E | 36 12 16 11 21 5 10 9 13 7 5 | 530 41 529 40 42 531 36 38 40 38 528
31E | 18 11 9 9 17 6 9 12 12 13 4 | 82 82 81 84 86 80 79 82 80 78 81
32 | 10 8 8 10 12 3 6 7 7 12 3 | 20 21 19 22 18 17 22 17 22 15 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 12 12 11 16 5 11 12 10 15 |T 45 31 43 29 31 42 29 27 29 27 42
WRMS | 13 12 12 11 15 5 11 12 9 15 |NE 23 26 22 24 26 20 26 22 23 22 21
MEDI | 12 11 11 11 15 5 11 12 10 15 |MD 24 27 21 24 27 21 25 24 23 21 21
Table 3.1828.4 GPS week: 1828 Day: 4 MJD: 57044.000
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 | 11 11 11 9 12 5 8 10 7 20 3 | 23 26 27 22 26 19 25 19 23 32 22
2 | 14 14 8 10 16 5 15 14 11 14 4 | 27 27 18 24 22 18 27 19 23 19 20
X3 | 7 9 9 11 --- 3 14 7 7 13 3 | 24 22 25 25 --- 22 31 20 27 20 21
4 | 11 18 8 8 19 6 9 15 10 19 4 | 24 33 24 24 24 20 30 30 24 32 24
5 | 8 11 12 12 15 5 14 12 10 16 4 | 31 37 29 32 28 30 38 35 37 34 31
6 | 9 10 11 10 14 4 14 14 10 15 4 | 31 37 36 29 34 29 43 28 32 30 31
7E | 18 20 6 9 16 4 17 8 8 8 4 | 46 38 36 42 44 36 37 38 43 37 38
X8E | 27 19 13 10 --- 8 16 16 18 --- 7 | 46 34 30 32 --- 32 39 26 39 --- 30
9 | 11 9 14 6 11 6 11 8 8 12 3 | 26 31 26 25 29 22 34 25 26 24 25
10 | 8 10 8 11 16 4 12 11 9 14 4 | 20 20 20 23 23 16 22 24 19 18 18
11E | 15 15 8 8 14 4 8 9 9 16 4 | 26 24 17 20 25 17 24 18 22 22 19
12 | 23 12 11 11 21 6 10 15 9 16 5 | 25 25 17 24 27 17 27 22 22 21 20
13 | 11 16 14 14 23 4 14 16 8 14 5 | 22 33 22 32 39 21 34 27 23 23 24
14 | 15 14 14 13 18 5 14 23 11 13 5 | 26 28 23 41 36 25 29 33 29 26 28
15 | 15 13 13 13 16 4 15 14 10 19 5 | 36 41 35 33 33 32 39 30 34 37 33
16 | 15 11 11 10 13 6 11 10 9 18 4 | 25 21 17 20 20 14 23 17 20 16 15
17 | 11 16 8 13 18 4 17 13 11 15 4 | 28 32 23 27 32 22 34 16 27 24 23
18 | 17 18 13 12 16 4 13 8 9 20 5 | 22 21 18 25 19 16 19 17 21 22 16
19 | 10 13 9 7 16 5 13 10 9 12 3 | 20 24 16 20 21 15 25 15 20 16 17
20 | 9 11 10 12 11 4 11 13 10 18 4 | 20 25 22 23 22 17 23 22 19 17 18
21 | 12 16 10 9 16 3 12 11 8 13 4 | 21 25 15 24 29 16 24 17 21 18 18
22 | 13 10 11 11 15 5 13 11 10 15 4 | 25 23 20 30 26 20 22 22 24 21 21
23 | 11 11 13 11 15 5 12 9 11 25 4 | 24 27 22 23 23 18 28 22 20 12 18
24E | 22 9 15 10 20 6 10 7 8 14 4 | 38 38 40 37 45 36 19 36 33 36 36
25 | 15 14 13 6 16 6 11 11 6 14 4 | 18 24 23 20 22 16 25 18 19 22 18
27 | 17 14 13 11 14 6 10 8 10 13 4 | 28 25 26 24 21 20 28 19 24 22 22
28 | 11 10 12 9 13 4 12 12 8 15 4 | 22 29 23 24 30 21 31 23 26 17 23
29 | 19 18 10 9 16 5 16 18 11 16 5 | 28 26 18 25 21 19 30 19 26 21 20
30E | 80 20 14 9 16 10 13 11 13 11 5 | 520 52 534 43 48 537 43 43 46 43 524
31E | 15 12 8 7 17 3 10 13 10 11 4 | 55 57 57 58 60 57 56 60 56 61 57
32 | 10 10 7 6 10 4 10 9 7 12 3 | 19 23 18 18 19 15 23 16 20 14 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 20 14 11 10 16 5 12 12 9 16 |T 43 29 41 28 29 39 30 25 27 25 40
WRMS | 13 14 11 9 15 5 12 12 9 16 |NE 24 27 22 25 26 20 28 22 24 22 21
MEDI | 13 13 11 10 16 5 12 11 9 14 |MD 25 27 23 25 26 20 28 22 24 22 22
Table 3.1828.5 GPS week: 1828 Day: 5 MJD: 57045.000
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 | 11 11 14 8 13 2 9 9 8 18 4 | 20 26 27 21 27 21 24 19 18 32 21
2 | 12 15 7 7 15 6 11 13 11 19 4 | 28 27 19 26 25 22 27 26 23 29 23
X3 | 10 6 13 10 --- 4 11 10 9 12 4 | 19 18 23 16 --- 16 20 15 14 18 15
4 | 11 10 10 8 17 4 9 12 6 16 3 | 23 29 22 21 24 22 26 29 20 31 23
5 | 14 12 13 9 14 5 10 13 12 17 4 | 28 30 25 26 25 26 32 31 28 34 26
6 | 12 8 11 7 15 4 7 17 8 12 3 | 30 31 33 27 34 28 32 29 28 31 29
7E | 25 14 9 13 18 5 12 11 15 13 5 | 43 47 45 46 41 43 46 45 45 46 43
X8E | 34 17 14 11 --- 11 --- 17 26 --- 9 | 52 35 29 30 --- 36 --- 26 39 --- 30
9 | 13 7 16 8 12 4 9 9 8 11 3 | 25 29 23 23 28 22 30 24 21 25 23
10 | 9 10 10 7 15 4 10 16 6 17 4 | 25 26 24 24 26 24 23 32 27 28 25
11E | 10 11 10 7 14 4 8 10 6 14 3 | 21 28 20 24 28 21 24 20 20 26 21
12 | 17 12 10 11 17 7 11 12 12 17 4 | 26 27 20 25 29 22 27 25 25 25 23
13 | 11 14 15 12 22 5 12 11 10 13 4 | 22 33 23 27 38 25 32 25 28 28 26
14 | 10 13 15 14 17 7 12 23 11 13 5 | 24 26 22 35 31 25 29 32 26 23 26
15 | 17 14 14 11 14 7 13 14 13 21 5 | 35 35 29 29 30 29 34 26 27 35 28
16 | 13 13 12 9 12 6 10 12 11 17 4 | 23 22 18 19 22 16 23 17 18 18 16
17 | 11 14 8 11 15 5 11 16 12 16 4 | 28 31 21 27 31 25 30 14 28 25 24
18 | 13 12 14 12 13 5 10 9 10 19 4 | 22 20 19 20 17 17 21 18 21 21 17
19 | 10 11 8 9 13 4 13 10 11 12 3 | 21 21 13 19 20 15 22 14 16 16 15
20 | 10 10 13 13 10 6 9 14 9 18 4 | 18 21 20 20 15 17 21 18 17 18 16
21 | 16 13 9 10 17 4 10 11 10 15 4 | 24 19 16 20 29 17 24 19 18 22 18
22 | 10 10 13 9 13 6 9 10 8 14 3 | 22 20 19 22 21 19 22 21 22 19 19
23 | 8 12 14 11 15 6 12 11 10 22 4 | 22 26 19 20 23 18 27 20 18 14 17
24E | 25 9 16 12 15 5 9 11 13 15 5 | 43 40 43 37 41 40 16 42 41 43 40
25 | 10 9 12 7 12 8 10 10 8 15 3 | 18 25 23 18 25 20 23 20 20 26 20
27 | 19 13 14 8 14 4 10 10 10 14 4 | 25 22 27 20 20 20 23 22 22 24 20
28 | 10 16 13 9 14 4 10 13 9 15 4 | 23 28 20 23 28 20 28 21 22 21 21
29 | 18 17 7 9 12 6 14 17 12 18 5 | 28 26 19 24 23 22 27 24 24 29 22
30E | 45 22 14 11 28 10 13 14 18 17 7 | 921 73 871 75 74 865 71 70 73 71 931
31E | 15 11 9 9 18 6 9 12 12 13 4 | 67 69 71 71 74 71 69 73 73 73 70
32 | 8 9 8 7 9 4 7 9 8 11 3 | 27 27 24 23 23 22 28 21 24 21 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 13 12 10 15 5 11 13 11 16 |T 56 30 52 27 30 51 29 27 27 29 53
WRMS | 13 13 12 9 14 5 11 12 9 15 |NE 24 25 21 23 25 21 26 22 22 24 21
MEDI | 12 12 13 9 14 5 10 12 10 15 |MD 25 27 23 24 27 22 27 24 23 25 23
Table 3.1828.6 GPS week: 1828 Day: 6 MJD: 57046.000
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 | 13 14 17 8 15 5 13 11 6 17 4 | 22 26 30 22 31 20 22 21 22 30 22
2 | 10 13 7 12 16 4 16 13 8 12 4 | 24 25 15 22 25 19 25 23 23 23 20
X3 | 13 5 14 8 --- 3 12 12 8 11 4 | 25 23 28 19 --- 22 23 21 27 21 22
4 | 12 8 11 7 21 4 12 14 7 16 4 | 24 29 26 23 30 22 26 29 27 30 25
5 | 12 12 15 13 13 6 15 11 8 19 4 | 40 42 36 36 37 36 42 39 37 41 37
6 | 12 10 16 10 14 4 9 20 8 13 4 | 31 35 37 26 35 27 34 30 29 28 30
7E | 17 17 19 13 14 5 12 16 11 14 5 | 48 45 45 45 46 46 47 50 47 48 45
X8E | 36 20 15 16 --- 9 16 19 19 --- 8 | 51 37 30 32 --- 32 37 26 34 --- 31
9 | 11 9 21 10 11 8 9 13 6 11 4 | 30 33 31 26 31 27 33 28 28 26 27
10 | 11 9 15 8 21 3 13 18 7 13 4 | 24 26 30 28 35 23 26 36 23 27 26
11E | 10 13 16 6 15 5 10 13 7 17 4 | 27 29 30 25 33 24 25 23 29 25 25
12 | 15 13 11 16 16 5 11 15 8 15 4 | 25 26 17 25 30 18 25 24 21 18 21
13 | 11 15 19 14 21 3 14 18 10 13 5 | 22 34 23 33 43 25 34 31 27 28 27
14 | 11 14 16 14 17 4 13 21 9 13 5 | 27 29 24 41 39 30 28 36 32 29 30
15 | 14 15 15 11 15 4 17 15 9 19 5 | 48 50 46 40 40 42 49 39 45 45 43
16 | 15 13 12 10 15 5 12 14 10 16 4 | 28 28 21 22 24 21 25 18 23 18 21
17 | 12 15 9 12 16 6 14 20 9 12 4 | 27 33 21 27 32 22 31 21 26 25 25
18 | 12 11 12 11 15 4 11 10 8 18 4 | 21 22 19 27 24 18 20 20 20 21 19
19 | 9 13 13 8 14 5 12 13 8 12 4 | 23 26 23 23 21 19 24 16 21 19 20
20 | 13 12 16 11 15 6 11 18 9 21 4 | 25 30 26 28 31 25 30 33 25 25 26
21 | 14 12 9 10 18 3 11 12 7 11 4 | 22 22 15 22 31 17 21 17 20 14 18
22 | 11 11 15 9 11 4 12 10 9 15 4 | 23 27 26 31 33 26 28 28 28 30 26
23 | 10 10 18 14 13 6 11 15 9 20 4 | 22 27 20 28 28 20 28 26 21 12 21
24E | 14 10 16 9 22 6 9 12 8 12 4 | 44 43 44 45 43 42 19 43 44 38 42
25 | 12 11 13 13 14 4 10 10 5 14 4 | 22 28 23 21 26 18 25 19 20 17 20
27 | 14 12 13 10 10 4 10 10 8 15 4 | 27 27 30 25 23 23 27 22 26 28 25
28 | 17 16 15 10 13 5 11 15 7 11 4 | 28 32 26 25 30 21 28 26 22 23 24
29 | 16 19 7 13 15 5 15 14 12 20 5 | 26 27 17 22 22 17 25 20 24 20 20
X30E | 3 --- 685 --- --- 671 --- --- --- --- 0 | 9999 --- 9999 --- --- 9999 --- --- --- --- 9999
31E | 13 12 11 9 20 3 10 13 10 11 4 | 65 67 69 68 76 67 66 69 66 65 66
32 | 10 11 12 8 12 3 7 10 8 12 3 | 24 24 24 24 26 20 27 25 23 24 23
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 13 14 11 16 5 12 14 8 15 |T 29 31 28 29 33 26 30 28 28 27 27
WRMS | 13 13 14 11 15 5 12 13 8 15 |NE 26 29 25 26 30 23 28 25 25 24 24
MEDI | 12 12 15 10 15 5 12 13 8 14 |MD 25 28 26 26 31 22 27 26 26 25 25
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 4.1828 GPS week: 1828 MJD: 57040.0-57046.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 |U 7 7 19 |U 14 20 53 |U 8 9 20 |
emr | emr 2958 | 10 8 20 |U 15 19 53 | 7 6 17 |
esa | esa 2976 | 7 6 20 |U 13 18 50 | 7 7 17 |
gfz | gfz 2958 |U 9 7 18 |U 14 18 52 |U 6 7 15 |
grg | grg 2779 | 7 6 16 |U 15 17 53 |U 7 7 19 |
igr | igr 2948 | 7 6 14 | 13 18 51 | 6 7 15 |
igs | igs 2939 | 7 6 16 | 14 18 49 | 6 8 16 |
jpl | jpl 2904 | 10 7 19 |U 14 17 50 |U 7 8 17 |
mit | mit 2962 | 9 8 20 |U 17 21 55 |U 7 9 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 5.1828.0 GPS week: 1828 Day: 0 MJD: 57040.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 9 24 | 9 14 28 | 10 11 23 |
emr | emr 2972 | 12 7 16 | 13 12 36 | 10 9 22 |
esa | esa 2976 | 6 4 11 | 9 11 27 | 8 9 21 |
gfz | gfz 2972 | 8 5 9 | 9 9 34 | 8 8 19 |
grg | grg 2850 | 7 6 14 | 14 10 29 | 11 12 23 |
igr | igr 2976 | 5 4 10 | 9 10 28 | 7 10 23 |
igs | igs 2976 | 5 3 9 | 10 10 27 | 9 10 20 |
jpl | jpl 2876 | 13 7 16 | 11 10 32 | 9 10 24 |
mit | mit 2976 | 10 12 18 | 24 29 47 | 9 12 20 |
Table 5.1828.1 GPS week: 1828 Day: 1 MJD: 57041.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 9 21 | 16 21 62 | 7 6 17 |
emr | emr 2972 | 11 8 18 | 17 22 79 | 6 5 11 |
esa | esa 2976 | 6 7 18 | 15 17 62 | 6 4 12 |
gfz | gfz 2972 | 7 7 18 | 15 16 65 | 5 4 11 |
grg | grg 2784 | 10 6 16 | 17 16 70 | 7 5 16 |
igr | igr 2976 | 6 6 13 | 15 17 73 | 5 3 9 |
igs | igs 2976 | 7 6 14 | 16 17 64 | 5 4 9 |
jpl | jpl 2880 | 8 7 16 | 15 17 65 | 6 4 11 |
mit | mit 2976 | 6 7 16 | 17 16 61 | 6 6 13 |
Table 5.1828.2 GPS week: 1828 Day: 2 MJD: 57042.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 5 16 | 9 13 43 | 6 7 17 |
emr | emr 2972 | 9 5 15 | 12 15 39 | 7 5 15 |
esa | esa 2976 | 5 5 14 | 9 13 42 | 5 6 15 |
gfz | gfz 2971 | 6 4 14 | 9 13 44 | 5 7 14 |
grg | grg 2783 | 6 4 11 | 14 15 46 | 7 6 18 |
igr | igr 2975 | 6 3 10 | 9 12 42 | 5 5 14 |
igs | igs 2971 | 5 3 9 | 10 13 40 | 5 6 13 |
jpl | jpl 2880 | 7 5 12 | 9 12 40 | 6 6 15 |
mit | mit 2976 | 9 7 12 | 10 18 53 | 5 7 15 |
Table 5.1828.3 GPS week: 1828 Day: 3 MJD: 57043.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 6 16 | 16 28 58 | 6 8 18 |
emr | emr 2972 | 7 10 16 | 15 25 59 | 4 5 14 |
esa | esa 2976 | 7 9 20 | 15 23 52 | 5 7 13 |
gfz | gfz 2972 | 9 7 14 | 16 25 59 | 4 6 13 |
grg | grg 2784 | 5 9 15 | 14 21 58 | 6 7 17 |
igr | igr 2976 | 6 7 13 | 15 25 61 | 5 7 13 |
igs | igs 2960 | 6 7 16 | 15 23 52 | 5 7 14 |
jpl | jpl 2972 | 10 10 16 | 14 20 59 | 7 7 14 |
mit | mit 2976 | 8 8 18 | 17 21 59 | 6 8 15 |
Table 5.1828.4 GPS week: 1828 Day: 4 MJD: 57044.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 6 17 | 22 33 80 | 8 10 17 |
emr | emr 2972 | 11 8 27 | 22 34 79 | 6 6 18 |
esa | esa 2976 | 8 5 26 | 19 33 81 | 6 7 14 |
gfz | gfz 2973 | 14 12 28 | 21 38 81 | 6 7 13 |
grg | grg 2784 | 7 6 22 | 22 36 75 | 6 6 20 |
igr | igr 2975 | 7 5 19 | 20 33 81 | 5 7 14 |
igs | igs 2973 | 7 5 23 | 23 35 81 | 5 6 15 |
jpl | jpl 2972 | 8 5 20 | 22 38 79 | 7 9 16 |
mit | mit 2976 | 11 6 28 | 24 40 83 | 8 12 17 |
Table 5.1828.5 GPS week: 1828 Day: 5 MJD: 57045.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 7 8 18 | 10 13 45 | 8 12 26 |
emr | emr 2972 | 9 7 23 | 10 15 44 | 6 8 19 |
esa | esa 2976 | 8 7 23 | 11 15 42 | 9 8 22 |
gfz | gfz 2973 | 9 7 19 | 10 13 41 | 6 9 17 |
grg | grg 2784 | 6 7 17 | 10 12 49 | 8 9 23 |
igr | igr 2878 | 7 7 16 | 10 16 40 | 6 9 16 |
igs | igs 2853 | 7 6 18 | 10 16 41 | 7 9 18 |
jpl | jpl 2878 | 11 8 23 | 11 14 42 | 8 10 22 |
mit | mit 2976 | 8 7 20 | 11 13 44 | 7 9 17 |
Table 5.1828.6 GPS week: 1828 Day: 6 MJD: 57046.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2972 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
emr | emr 2876 | 12 9 28 | 14 13 38 | 7 7 20 |
esa | esa 2976 | 10 8 27 | 17 15 44 | 8 7 20 |
gfz | gfz 2876 | 11 6 25 | 15 11 38 | 6 6 18 |
grg | grg 2688 | 9 7 19 | 14 12 46 | 7 6 19 |
igr | igr 2880 | 10 8 18 | 14 10 36 | 7 7 17 |
igs | igs 2866 | 11 9 25 | 14 11 41 | 7 13 26 |
jpl | jpl 2876 | 14 8 26 | 14 11 35 | 7 8 17 |
mit | mit 2880 | 14 8 27 | 14 14 38 | 7 7 19 |
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 6.1828 GPS week: 1828 MJD: 57040.500-57046.500
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 | -16 -5 75 -8 -3 | 7 12
| 13 16 71 144 5 | 1
emr uuuuu | 7 9 69 4 -1 | 31 35
| 35 21 160 80 9 | 2
esa uuuuu | 2 24 -111 -27 0 | 13 17
| 23 11 58 66 4 | 1
gfz uuuuu | -33 -23 -28 -149 3 | 11 15
| 13 16 140 101 7 | 3
grg uuuuu | 7 39 -144 134 2 | 21 24
| 10 16 101 108 6 | 3
igr xxxxx | -17 14 43 15 -2 | -2 11
| 27 15 65 56 3 | 1
irf xxxxx | 12 -3 -1 61 1 | 3 11
| 7 4 29 35 3 | 2
jpl uuuuu | 1 -18 135 -51 -8 | 37 39
| 42 18 79 86 11 | 2
mit uuuuu | 37 -16 -50 160 4 | 18 21
| 13 15 77 51 4 | 2
ngs uuuuu | 1 9 1 34 -2 | 14 18
| 54 27 184 133 4 | 2
sio uuxxx | 12 -4 -157 37 4 | 41 42
| 19 25 105 80 4 | 3
Table 7.1828.0 GPS week: 1828 Day: 0 MJD: 57040.500
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 | -14 -30 128 -84 -1 | 7 10
emr uuuuu | 23 -5 348 -53 -16 | 35 39
esa uuuuu | 15 39 -137 -18 -5 | 14 17
gfz uuuuu | -26 -40 72 -78 1 | 8 12
grg uuuuu | 0 24 -81 126 7 | 16 20
igr xxxxx | -22 32 120 7 -1 | -2 10
irf xxxxx | 22 -1 -36 113 2 | 2 9
jpl uuuuu | 36 -11 132 28 -3 | 40 41
mit uuuuu | 52 -4 -151 214 4 | 15 17
ngs uuuuu | -83 41 -290 -29 1 | 13 17
sio uuxxx | 50 -23 -50 107 8 | 36 37
Table 7.1828.1 GPS week: 1828 Day: 1 MJD: 57041.500
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 -1 -47 4 -4 | 7 10
emr uuuuu | 27 6 125 15 1 | 31 34
esa uuuuu | 13 7 -141 -33 -4 | 12 15
gfz uuuuu | -34 -31 134 -33 2 | 7 11
grg uuuuu | 21 19 -38 256 7 | 17 21
igr xxxxx | 14 23 111 125 0 | -3 8
irf xxxxx | 12 -1 -38 83 4 | 1 9
jpl uuuuu | 63 -4 222 -98 -8 | 38 39
mit uuuuu | 44 -1 -148 194 8 | 15 18
ngs uuuuu | -54 23 -128 -84 1 | 12 16
sio uuxxx | -1 -9 -38 -47 2 | 37 38
Table 7.1828.2 GPS week: 1828 Day: 2 MJD: 57042.500
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 -3 160 -61 -1 | 9 12
emr uuuuu | 57 34 44 120 -8 | 32 36
esa uuuuu | -27 20 -97 -37 -2 | 14 17
gfz uuuuu | -41 -37 83 -160 4 | 10 14
grg uuuuu | 7 61 -106 231 1 | 22 25
igr xxxxx | 6 24 92 13 2 | 0 9
irf xxxxx | 12 -11 34 94 4 | 5 12
jpl uuuuu | -8 -29 48 -43 1 | 39 41
mit uuuuu | 52 -35 -35 201 9 | 19 22
ngs uuuuu | -22 31 -110 -113 -5 | 16 19
sio uuxxx | 17 -33 -60 112 3 | 41 42
Table 7.1828.3 GPS week: 1828 Day: 3 MJD: 57043.500
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 | -14 -14 40 -105 -7 | 6 11
emr uuuuu | -17 35 -81 -31 -1 | 27 32
esa uuuuu | -22 14 -42 -90 1 | 11 15
gfz uuuuu | -54 -25 -254 -325 11 | 8 13
grg uuuuu | -11 29 -61 238 -4 | 19 23
igr xxxxx | -25 13 -3 -42 2 | -4 10
irf xxxxx | 10 -4 -15 34 -1 | 2 10
jpl uuuuu | 29 -5 257 64 -26 | 36 37
mit uuuuu | 24 -18 -76 72 -1 | 17 20
ngs uuuuu | 47 -6 179 224 4 | 11 16
sio uuxxx | 4 -1 -257 -95 4 | 40 41
Table 7.1828.4 GPS week: 1828 Day: 4 MJD: 57044.500
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 24 47 -165 -9 | 8 13
emr uuuuu | 20 22 -152 64 12 | 29 34
esa uuuuu | -1 24 -44 -86 4 | 13 17
gfz uuuuu | -35 -24 -147 -235 9 | 11 18
grg uuuuu | 14 49 -189 65 -3 | 22 25
igr xxxxx | -27 14 -54 -37 -7 | -1 12
irf xxxxx | 3 0 16 24 -1 | 4 13
jpl uuuuu | -29 4 126 -8 3 | 36 37
mit uuuuu | 22 -34 31 156 0 | 19 23
ngs uuuuu | 35 -32 220 207 1 | 14 19
sio uuxxx | 0 17 -179 36 -1 | 42 44
Table 7.1828.5 GPS week: 1828 Day: 5 MJD: 57045.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 8 1 132 104 0 | 8 13
emr uuuuu | -14 -11 108 38 -2 | 31 36
esa uuuuu | -3 31 -111 -35 -1 | 15 19
gfz uuuuu | -17 5 -87 -111 1 | 15 20
grg uuuuu | 9 38 -320 19 11 | 24 27
igr xxxxx | -65 5 9 2 -4 | 0 12
irf xxxxx | 7 -6 16 42 3 | 6 13
jpl uuuuu | -46 -40 99 -127 -7 | 37 39
mit uuuuu | 25 -17 17 168 6 | 21 24
ngs uuuuu | 52 -13 92 40 -8 | 16 21
sio uuxxx | -3 38 -282 62 8 | 44 45
Table 7.1828.6 GPS week: 1828 Day: 6 MJD: 57046.500
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 | -34 -13 65 254 5 | 6 13
emr uuuuu | -48 -16 89 -123 6 | 29 35
esa uuuuu | 40 32 -205 107 7 | 13 18
gfz uuuuu | -22 -7 1 -100 -10 | 14 20
grg uuuuu | 12 56 -212 6 -2 | 24 26
igr xxxxx | -1 -12 29 36 -4 | -3 13
irf xxxxx | 18 1 16 35 -2 | 4 13
jpl uuuuu | -36 -38 58 -173 -19 | 34 36
mit uuuuu | 42 -2 13 117 0 | 20 24
ngs uuuuu | 32 19 46 -6 -5 | 13 20
sio uuxxx | 15 -19 -232 85 2 | 43 45
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