[IGSREPORT-23272] Wk 1824 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Jan 8 11:25:21 PST 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1824 (Dec 21, 2014 - Dec 27, 2014)
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:
igs1824[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1824[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1824[0-6].cls IGS GPS clock combination summary report.
igs18247.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18247.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 | ESA | BJFS BJFS TIXI
0 | GFZ | 1 2 3 6 9 30 1 3 6 30 ALBH ALGO ALIC ALRT ARTU AUCK
0 | GFZ | BAKE BAKO BJFS BOGT BOR1 BRFT BRMU CAS1 CHTI CHUR
0 | GFZ | CONZ CORD CRO1 DAEJ DARW DAV1 DGAR DRAG DRAO DUBO
0 | GFZ | FAIR FLIN GLSV GOLD GOPE GRAS GRAZ GUAM GUAT GUUG
0 | GFZ | HARB HOB2 HOFN HOLB HOLM HRAO HYDE IISC INVK IRKJ
0 | GFZ | ISPA KELY KERG KIRU KOUR LAMA MAC1 MAG0 MAL2 MAS1
0 | GFZ | MATE MAW1 MDVJ MIZU NANO NICO NKLG NOVM NRIL NTUS
0 | GFZ | NYA1 ONSA PDEL PERT PIE1 PIMO POL2 PRDS QAQ1 RABT
0 | GFZ | REUN SCH2 SFER SOFI SSIA STJO SUWN SYOG THTI THU3
0 | GFZ | TIDB TLSE TOW2 TRO1 TWTF USUD VILL WES2 WHIT WILL
0 | GFZ | WSRT WTZR WUHN XMIS YELL YIBL ZECK ZIMM
0 | GRG | 13 13 DAV1 MCM4 SYOG DAV1 KOUC NOVM
0 | JPL | CHUR
0 | MIT | BRFT BRFT REUN
1 | COD | SYOG
1 | ESA | SCH2 BJFS SCH2 SYOG
1 | GFZ | 1 2 3 6 9 30 1 3 6 30 ALBH BAKE BAKO BJFS BOGT BRAZ
1 | GFZ | BRFT CHTI CHUM CRO1 DARW DRAG DRAO DUBO FLIN GOPE
1 | GFZ | GUAM GUUG HOFN IRKJ ISPA JPLM KERG KOUR MAC1 MAG0
1 | GFZ | MAL2 MDVJ NANO NICO NOVM ONSA PARC PDEL PIE1 REUN
1 | GFZ | SANT SFER STJO SYOG THTI TIDB TOW2 TWTF WHIT WSRT
1 | GFZ | WTZR WUHN XMIS ZECK
1 | GRG | 13 13 DARW FLIN KERG KOKB KOUC MDVJ NYA1 SCH2 SYOG
1 | GRG | FLIN KOUC NYA1
1 | JPL | TIXI
1 | MIT | INVK INVK MDVJ SCH2 SYOG
2 | COD | HOB2 HOB2 REUN
2 | ESA | 21 21 REUN
2 | GFZ | 1 2 3 6 8 9 30 1 3 6 8 30 BOR1 BRFT CAS1 CHUM DARW
2 | GFZ | DGAR GLPS GUAM GUUG HARB ISPA KOUR MAW1 NOVM NRIL
2 | GFZ | REUN THTI TIDB TOW2 XMIS BOR1
2 | GRG | DAV1 HARB MCM4 REUN DAV1 KELY
2 | JPL | 21
2 | MIT | 8 22 27 6 8 27 KOUR REUN HARB HOB2 KOUR REUN
3 | COD | DAV1 DAV1
3 | ESA | KELY
3 | GFZ | 1 2 3 6 9 30 1 3 6 30 ASPA DAV1 GUUG KELY KERG MAW1
3 | GFZ | NOVM SYOG THTI TOW2
3 | GRG | 13 21 21 27 BOR1 HARB MAL2 MAW1 TRO1 MAL2 MAW1 NOVM
3 | GRG | NYA1 TRO1
3 | MIT | 1 8 28 1 8 19 28 MAW1 TOW2 MAW1 TOW2
4 | COD | 27 SYOG
4 | EMR | 27 27
4 | ESA | TIXI
4 | GFZ | 1 2 3 6 9 30 1 3 6 30 ARTU BAKE BJFS BOGT BRFT CAS1
4 | GFZ | CONZ DARW GUUG KELY KERG KOUR NOVM QAQ1 REUN SYOG
4 | GFZ | TEHN THTI WES2 XMIS YIBL ZAMB SYOG YIBL
4 | GRG | RABT KELY RABT ZAMB
4 | MIT | 8
5 | COD | CAS1 INVK
5 | ESA | BJFS BJFS MAL2 NOVM
5 | GFZ | 1 2 3 6 30 1 3 6 30 CAS1 GUUG NOVM
5 | GRG | 13 13 BRST KOUC SYOG BRST KOUC SYOG
5 | MIT | 8 8 SANT ALIC KERG MONP SANT SYOG
6 | COD | 17 17 HOB2 GRAZ HOB2
6 | ESA | BJFS BJFS
6 | GFZ | 1 2 3 6 9 30 1 3 6 30 BAKE DAV1 GRAZ GUAM GUUG HOB2
6 | GFZ | INVK KELY NKLG NOVM TEHN THTI XMIS HOB2
6 | GRG | 13 13 DARW GRAZ KOUC DAV1 GRAZ KOUC
6 | MIT | 8 8 HOB2 HOB2
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
----+--------+--------+-------------
1 | ESA | ~14:50 | ~ 0.11 ns
1 | GFZ | ~05:30 | ~ -0.20 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
----+--------+---------------
3 | GRG | 27
4 | GRG | 27
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 G27 | 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 | -2.4 .4 -1.1 -37 18 -11 .20
EMR | 0 | -2.1 5.1 2.9 37 24 -22 .23
ESA | 0 | .0 1.4 .0 -28 -30 80 -.24
GFZ | 0 | .3 1.5 -.9 -34 -95 0 -.20
GRG | 0 | -3.7 6.1 -22.1 -19 -38 16 .44
JPL | 0 | -3.4 -4.2 4.0 -48 25 13 -.30
MIT | 0 | 3.6 .3 -3.4 -9 0 -39 .44
NGS | 0 | .0 -.6 -10.0 4 5 -9 .27
SIO | 0 | 1.4 2.2 -2.9 -20 10 -20 .41
COD | 1 | -1.2 -1.5 -1.0 -63 9 -27 .20
EMR | 1 | -5.2 3.0 6.1 44 4 -7 -.27
ESA | 1 | -1.0 -1.5 -.5 -37 -10 17 -.14
GFZ | 1 | .7 .6 -1.5 -21 -91 -3 .09
GRG | 1 | -9.0 5.5 -8.8 -14 -48 -14 .56
JPL | 1 | -3.8 -2.1 -.4 -54 0 -17 -.09
MIT | 1 | 3.3 3.1 -1.2 -20 -6 -41 .42
NGS | 1 | 1.4 -2.8 .8 -21 -4 -16 .32
SIO | 1 | 4.9 2.9 6.0 -36 -15 -33 .38
COD | 2 | -2.0 -.1 -.8 -58 20 -9 .14
EMR | 2 | -7.8 6.7 9.0 37 19 -14 .05
ESA | 2 | -1.1 .2 1.0 -48 8 19 -.13
GFZ | 2 | -.8 1.0 -.8 -19 -76 -10 .18
GRG | 2 | -5.1 8.0 -18.2 -30 -17 22 .72
JPL | 2 | -6.2 -2.9 3.6 -83 13 -2 -.06
MIT | 2 | 1.3 .4 -3.2 -4 -6 -34 .65
NGS | 2 | -3.0 2.7 -1.7 -5 12 -18 .48
SIO | 2 | 4.2 -.7 16.1 -13 -13 -24 .35
COD | 3 | -1.7 -.9 -.7 -50 11 -7 .28
EMR | 3 | 1.9 3.0 13.1 36 17 -4 .0
ESA | 3 | -.5 -.1 .8 -30 9 34 -.12
GFZ | 3 | -.6 1.6 -.3 -25 -90 -7 -.04
GRG | 3 | -.5 7.5 -12.1 -15 -6 38 .65
JPL | 3 | 3.6 -4.0 4.2 -2 1 11 .21
MIT | 3 | 1.2 2.7 -2.3 25 11 -13 .39
NGS | 3 | 8.1 -3.1 5.9 -28 -16 0 .30
SIO | 3 | 7.5 -1.2 10.0 -24 -6 -8 .10
COD | 4 | -2.7 .0 -1.2 -40 7 14 .36
EMR | 4 | -4.9 7.5 11.3 46 13 -4 -.06
ESA | 4 | -.8 .0 .3 -35 -20 46 -.01
GFZ | 4 | -.9 1.0 -.5 -29 -83 -18 .22
GRG | 4 | .7 6.5 -3.0 -12 -9 4 .51
JPL | 4 | 4.7 2.3 3.9 -73 -5 10 .30
MIT | 4 | 3.5 1.6 .4 25 6 -15 .38
NGS | 4 | 2.7 1.3 7.6 -21 -3 -11 .32
SIO | 4 | 6.3 3.6 7.8 -4 -9 -22 .29
COD | 5 | -2.3 .5 -.7 -35 6 2 .51
EMR | 5 | -8.3 4.5 18.0 40 21 -1 .47
ESA | 5 | -.8 .0 .2 -42 -25 45 .17
GFZ | 5 | -.6 .8 -.6 -23 -106 11 .39
GRG | 5 | .8 2.4 -.3 -14 4 -10 .57
JPL | 5 | -3.0 -.1 15.0 -78 33 -12 1.10
MIT | 5 | 3.6 4.3 6.5 27 15 -14 .53
NGS | 5 | 3.9 -2.8 7.5 -32 -6 -9 .53
SIO | 5 | 7.9 2.9 9.0 -2 -4 7 .66
COD | 6 | -1.5 -.1 -1.0 -29 -9 -16 .74
EMR | 6 | -6.2 3.2 24.9 47 27 10 .35
ESA | 6 | -.5 -1.8 .6 -44 -17 39 .61
GFZ | 6 | -.7 1.0 -1.0 -25 -91 8 .37
GRG | 6 | -3.4 -3.1 -.8 -16 -15 27 .76
JPL | 6 | -.1 -4.6 20.5 -11 -16 -34 .15
MIT | 6 | 3.8 -.4 6.9 13 11 -30 .62
NGS | 6 | -1.1 -1.7 15.9 -41 3 -20 .62
SIO | 6 | 1.9 -3.2 16.1 -20 7 -28 .74
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 1.1824.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1824.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 2.1824.[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 3.1824.[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 5.1824.0-6). 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 1824 summary. (Dec 21, 2014 - Dec 27, 2014)
Table 1.1824.a GPS week: 1824 MJD: 57012.000-57018.000
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 244| 0 0 0 -2 11 -7 .00 9 9 | -548 -838 15 111
| 0 0 1 12 15 18 .03 | 418 803
emr 79| -1 0 5 0 -6 10 .13 12 12 | 3111 670 16 138
| 1 2 1 14 17 19 .06 | 934 1383
esa 150| 0 0 5 -21 4 5 -.34 12 12 | -6 -87 10 147
| 0 0 1 15 14 16 .03 | 799 1272
gfz 194| -1 0 -6 25 -26 20 .07 11 11 | 73 -119 12 169
| 0 0 1 23 9 14 .01 | 469 624
grg 170| 3 -1 -4 -13 24 -23 .16 16 14 | 9 177 16 156
| 0 0 2 15 19 13 .04 | 278 423
igr n/a| 0 0 0 15 28 -4 -.13 5 5 | 1508 991 14 78
| 0 0 2 15 5 9 .02 | 1919 1180
jpl 80| 0 0 7 3 19 -12 .14 12 12 | 3151 662 16 116
| 1 1 1 25 27 16 .03 | 920 1391
mit 349| 0 0 -4 2 -6 15 -.04 11 11 | -388 73 25 176
| 1 0 0 25 18 18 .03 | 284 467
ngs 221| 0 0 -1 -20 6 -16 .02 9 8 | -492 -848 1194 3017
| 0 0 3 21 11 17 .05 | 482 1028
sio 313| 0 0 -4 22 -37 18 -.21 14 13 | --- --- --- ---
| 0 0 3 30 31 20 .04 | --- ---
Table 1.1824.b GPS week : 1824 MJD: 57012.000-57018.000
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 3 4 4 |
2 | 5 5 5 5 5 5 5 |
3 | 4 4 5 4 4 4 5 |
4 | 6 3 4 4 5 4 4 |
5 | 4 5 4 4 4 4 4 |
6 | 4 3 4 3 4 3 3 |
7 | 5 5 4 4 4 4 4 |
8 | 5 4 6 6 5 5 6 |
9 | 3 3 3 4 3 4 4 |
10 | 3 4 3 3 3 3 3 |
11 | 4 5 4 5 4 4 4 |
12 | 5 5 5 5 4 5 5 |
13 | 4 4 4 5 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 5 5 4 4 4 4 |
16 | 5 5 5 5 5 5 5 |
17 | 4 4 4 4 4 4 4 |
18 | 5 4 5 5 5 5 5 |
19 | 4 4 4 3 4 4 4 |
20 | 5 4 4 4 4 4 4 |
21 | 5 5 6 6 5 5 5 |
22 | 4 3 4 4 3 4 4 |
23 | 4 4 5 4 4 4 4 |
24 | 4 4 4 4 4 5 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 5 5 9 7 5 4 |
28 | 4 4 4 4 4 4 4 |
29 | 4 4 4 4 4 4 5 |
30 | 4 4 4 4 3 4 4 |
31 | 4 4 4 4 4 4 4 |
32 | 4 4 4 4 5 5 5 |
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 2.1824.0 GPS week: 1824 Day: 0 MJD: 57012.000
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 250| 1 0 3 -1 2 -4 -.04 9 9 | -230 -1141 16 117
emr 80| -2 -1 4 8 3 48 .12 12 12 | 3722 -870 18 154
esa 150| 0 1 8 -9 10 27 -.33 14 14 | -1229 2273 11 154
gfz 196| -1 -1 -2 3 -32 24 .07 10 10 | -62 -84 16 189
grg 172| 2 0 -4 -11 28 -31 .19 16 14 | 330 -349 16 172
igr n/a| 0 0 4 7 24 -19 -.15 5 5 | 250 -753 15 72
jpl 80| 0 0 5 10 37 -20 .12 12 12 | 3771 -892 17 127
mit 350| 0 -2 -4 3 6 0 -.04 12 12 | 14 -456 22 164
ngs 224| 0 2 -7 -18 10 -31 .09 9 9 | -204 -1232 1198 3398
sio 332| 0 0 0 -9 -86 -6 -.27 14 13 | --- --- --- ---
Table 2.1824.1 GPS week: 1824 Day: 1 MJD: 57013.000
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 244| 0 0 0 -21 0 -10 .01 9 9 | -85 -1614 14 101
emr 80| -1 -2 5 4 17 16 .07 13 13 | 3534 -481 16 119
esa 150| 0 2 4 -26 11 17 -.36 13 13 | 1018 -1681 12 179
gfz 198| -1 1 -6 32 -41 23 .05 11 11 | 252 -545 13 179
grg 174| 3 0 0 3 4 -14 .17 15 14 | 344 -71 18 152
igr n/a| 0 0 2 16 36 0 -.15 5 5 | 106 177 14 84
jpl 80| 1 0 5 -20 15 1 .11 10 10 | 3507 -482 15 96
mit 350| -1 -1 -4 12 6 2 -.03 11 11 | -131 -52 22 142
ngs 222| 0 0 -1 -3 0 -14 .05 9 8 | -12 -1718 1054 2863
sio 287| -1 0 -1 28 -23 24 -.19 14 13 | --- --- --- ---
Table 2.1824.2 GPS week: 1824 Day: 2 MJD: 57014.000
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| 0 1 0 10 40 -13 .01 11 11 | -953 -491 16 110
emr 80| 0 1 5 -21 -10 17 .05 12 12 | 2335 -657 16 119
esa 150| 1 1 6 -40 21 -11 -.37 13 12 | 408 -170 11 110
gfz 196| -1 0 -5 22 -15 20 .09 10 10 | 125 -263 13 173
grg 173| 3 -2 -5 -17 42 -24 .19 15 14 | -102 411 20 169
igr n/a| 0 -1 2 2 26 -12 -.10 5 5 | -320 865 15 78
jpl 80| 0 -2 9 -24 0 -3 .11 11 11 | 2412 -688 16 110
mit 349| -1 -1 -4 15 -10 47 -.02 11 10 | -786 891 30 231
ngs 221| 0 0 -3 -9 -8 -41 .05 9 8 | -280 -1258 1253 2558
sio 305| 1 -1 -5 54 -34 32 -.15 14 13 | --- --- --- ---
Table 2.1824.3 GPS week: 1824 Day: 3 MJD: 57015.000
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| 0 1 0 11 14 -42 .01 9 8 | -690 -472 16 98
emr 79| 1 -1 3 -6 0 -6 .15 12 12 | 1652 1560 15 116
esa 150| 0 1 4 -24 18 1 -.37 12 12 | 141 -381 11 123
gfz 195| -2 1 -6 60 -15 22 .07 11 11 | 115 475 13 162
grg 171| 2 -1 -8 -40 25 -23 .17 24 14 | -438 787 17 156
igr n/a| 0 0 0 11 30 4 -.14 5 5 | 322 2232 15 82
jpl 80| 0 -2 6 24 6 0 .12 14 14 | 1696 1565 17 126
mit 349| -1 0 -3 1 -20 34 -.02 12 11 | -374 -121 29 167
ngs 223| 1 0 0 -42 -4 -3 -.01 11 8 | -1056 410 935 3118
sio 303| 0 -1 -1 7 -42 34 -.20 14 14 | --- --- --- ---
Table 2.1824.4 GPS week: 1824 Day: 4 MJD: 57016.000
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 245| 0 0 2 0 22 17 -.03 8 8 | -1220 667 16 119
emr 79| -2 3 6 13 -1 3 .20 13 13 | 2566 1637 16 147
esa 150| 1 0 5 5 -4 -17 -.35 12 12 | 109 50 10 154
gfz 192| -2 0 -7 29 -23 -5 .06 12 12 | 734 -1206 12 167
grg 170| 3 -2 -7 -23 -9 -42 .19 15 14 | -104 433 16 146
igr n/a| 0 -1 0 18 28 -8 -.10 5 5 | 1973 2657 16 79
jpl 80| 0 0 7 -16 44 -12 .17 12 12 | 2631 1618 16 113
mit 349| -1 0 -4 21 -20 15 -.03 9 9 | -493 406 23 161
ngs 223| 0 0 -1 -41 7 2 -.00 8 7 | -1143 651 1027 3137
sio 315| 0 0 -3 25 -67 0 -.22 15 14 | --- --- --- ---
Table 2.1824.5 GPS week: 1824 Day: 5 MJD: 57017.000
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 243| 0 0 0 -14 3 2 .02 9 9 | -287 -1491 13 119
emr 80| -1 2 8 12 -18 1 .19 13 13 | 3727 766 17 152
esa 150| 0 0 4 -21 -14 10 -.31 12 12 | -943 472 9 151
gfz 192| -1 1 -6 39 -27 12 .09 11 11 | -832 593 13 164
grg 165| 4 -1 -1 3 36 -24 .08 16 15 | 130 -297 16 161
igr n/a| 0 0 -2 46 33 -3 -.12 5 5 | 4038 493 14 76
jpl 80| -1 0 7 12 -23 -45 .15 11 11 | 3762 778 17 119
mit 350| 0 0 -4 -52 20 9 -.08 12 11 | -282 203 28 195
ngs 219| 0 0 -2 9 11 -1 -.03 9 8 | -10 -2046 1267 2669
sio 323| 0 -2 -6 -13 4 44 -.19 15 14 | --- --- --- ---
Table 2.1824.6 GPS week: 1824 Day: 6 MJD: 57018.000
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| 0 0 -1 -2 0 2 .05 9 9 | -375 -1325 14 118
emr 80| 0 3 7 -16 -36 -9 .16 13 13 | 4243 2741 15 161
esa 150| 0 0 6 -31 -12 11 -.31 12 12 | 450 -1174 10 162
gfz 193| -1 0 -8 -11 -33 43 .08 11 10 | 185 194 10 151
grg 168| 3 -2 -3 -4 43 0 .17 14 14 | -94 327 13 142
igr n/a| 0 0 -2 3 21 6 -.14 5 5 | 4190 1266 14 79
jpl 80| 1 0 8 41 53 -8 .18 11 11 | 4278 2741 15 124
mit 350| 0 0 -6 16 -29 -1 -.08 12 11 | -668 -355 24 175
ngs 221| 0 0 2 -40 25 -27 -.04 9 7 | -744 -746 1630 3381
sio 327| 0 0 -9 65 -13 0 -.25 14 13 | --- --- --- ---
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 3.1824.0 GPS week: 1824 Day: 0 MJD: 57012.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 15 8 10 5 6 9 8 14 3 | 28 32 28 26 30 25 31 27 27 27 27
2 | 13 12 19 12 14 6 13 12 10 17 4 | 25 30 25 36 30 27 29 35 32 32 28
X3 | 8 7 11 11 --- 5 12 9 10 10 3 | 72 70 66 66 --- 67 74 71 66 64 68
4 | 7 9 15 11 44 6 13 14 9 16 5 | 22 22 18 21 31 15 24 25 20 24 20
5 | 9 13 15 10 8 6 11 13 9 12 4 | 35 42 34 35 36 35 38 41 39 38 36
6 | 8 9 14 10 10 4 9 13 7 10 3 | 32 38 33 33 34 32 38 26 33 29 32
7 | 7 22 10 9 16 4 12 12 9 10 4 | 30 36 24 26 33 27 32 28 30 24 27
X8 | 10 14 10 8 --- 14 12 6 12 --- 4 | 32 27 26 26 --- 30 20 23 28 --- 25
9 | 7 10 11 8 14 4 8 9 9 7 3 | 37 42 39 35 41 36 42 36 35 39 37
10 | 7 7 13 9 9 5 9 11 6 10 3 | 30 33 29 33 34 30 33 35 36 35 32
11 | 7 11 17 10 20 6 7 11 11 9 4 | 37 45 31 38 51 33 41 43 36 36 38
12 | 13 12 17 10 16 5 12 15 10 17 4 | 18 27 19 24 28 16 25 24 22 23 20
13 | 9 11 14 7 24 5 9 8 10 12 4 | 24 29 20 26 38 23 25 22 26 24 24
14 | 6 10 11 8 13 5 12 13 7 16 3 | 20 21 18 22 28 18 20 22 23 15 19
15 | 10 13 12 8 16 4 11 13 9 18 4 | 23 31 21 24 30 21 25 27 24 23 23
16 | 12 17 12 13 15 5 13 14 9 16 4 | 25 24 18 23 23 18 23 24 21 19 19
17E | 9 13 8 7 19 4 15 13 10 14 4 | 18 22 13 18 22 15 23 19 18 23 17
18 | 8 11 14 22 15 5 9 11 9 10 4 | 23 23 20 38 24 21 19 29 29 20 23
19E | 10 10 9 11 13 6 16 14 8 16 4 | 23 25 18 22 20 18 23 23 21 28 20
20 | 10 8 14 12 10 3 22 10 10 14 4 | 28 28 27 26 27 25 31 31 33 28 27
21 | 9 12 19 11 15 7 13 12 10 16 4 | 30 31 25 36 38 27 29 30 30 29 29
22 | 9 10 13 9 13 6 9 11 11 9 3 | 34 35 29 36 41 30 33 41 39 33 35
23 | 7 15 8 11 18 6 12 9 10 16 4 | 32 31 25 30 34 28 31 30 33 22 28
24 | 8 10 15 10 13 5 9 12 8 13 3 | 30 30 30 31 29 27 28 27 29 33 28
25 | 8 10 18 8 14 5 10 11 9 12 4 | 18 26 25 20 24 17 21 21 20 23 20
26 | 9 10 14 8 11 8 12 9 10 13 3 | 24 27 22 22 21 22 27 21 27 28 23
27E | 10 16 15 13 13 8 11 10 10 17 4 | 671 672 669 671 665 671 614 671 670 614 670
28 | 11 12 13 8 15 5 13 14 10 9 4 | 26 29 19 19 29 19 27 19 24 17 21
29E | 9 13 11 11 15 5 13 12 8 13 4 | 18 21 13 24 22 13 19 20 19 24 17
30 | 6 7 15 8 8 5 9 19 7 9 3 | 43 40 46 40 43 40 41 36 42 42 41
31 | 7 11 10 11 18 5 10 10 10 9 3 | 22 28 17 26 37 21 24 23 26 19 23
32 | 10 8 10 11 11 6 11 15 8 22 4 | 16 23 17 22 24 16 24 24 24 22 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 14 10 16 5 12 12 9 14 |T 48 51 45 49 52 45 47 49 49 47 47
WRMS | 9 12 14 10 14 5 12 12 9 13 |NE 29 32 26 30 32 26 30 30 30 28 28
MEDI | 9 11 13 10 14 5 11 12 9 13 |MD 26 29 25 26 30 25 27 27 28 27 25
Table 3.1824.1 GPS week: 1824 Day: 1 MJD: 57013.000
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 12 16 8 13 5 8 10 7 9 3 | 21 29 22 21 28 19 26 21 23 23 22
2 | 12 13 16 14 13 5 14 12 10 18 4 | 22 26 25 29 25 22 28 28 27 25 24
X3 | 5 8 12 11 --- 5 12 9 9 13 3 | 58 63 61 59 --- 59 67 63 62 67 61
4 | 5 14 13 8 11 5 6 9 8 11 3 | 21 24 22 21 22 19 22 21 21 25 20
5 | 13 12 14 16 9 5 11 13 10 12 4 | 24 23 22 25 21 19 26 24 26 20 21
6 | 8 10 12 8 10 5 8 10 8 11 3 | 23 28 23 21 26 21 28 23 24 25 23
7 | 6 27 11 13 18 4 13 7 11 12 4 | 25 38 24 31 32 24 30 26 29 26 26
X8 | 8 14 9 7 --- 22 10 11 9 --- 4 | 30 28 25 26 --- 18 23 22 25 --- 24
9 | 8 9 12 6 15 4 9 7 10 8 3 | 38 40 42 38 42 37 41 38 40 41 39
10 | 10 9 11 10 9 5 8 9 10 10 3 | 23 24 23 25 23 22 26 25 29 21 23
11 | 6 22 24 12 21 5 9 11 9 9 5 | 30 40 33 34 43 29 35 34 31 29 31
12 | 14 15 14 10 18 6 11 15 9 17 4 | 21 24 19 22 27 17 24 21 22 19 19
13 | 7 11 11 10 20 5 10 10 10 13 4 | 23 25 17 22 35 18 24 23 21 17 21
14 | 7 11 10 9 15 4 10 11 7 16 3 | 18 21 16 16 26 16 21 18 17 17 16
15 | 10 15 14 9 15 6 12 15 9 14 4 | 24 26 22 23 25 20 23 25 22 16 21
16 | 13 13 12 12 17 3 13 13 13 17 4 | 25 22 18 23 24 16 25 20 19 20 18
17E | 9 13 6 9 16 6 12 12 10 17 4 | 20 23 18 21 24 17 24 19 24 25 20
18 | 11 11 11 18 15 5 11 11 8 12 4 | 22 16 16 28 14 15 16 20 19 15 16
19E | 6 18 7 9 15 5 10 8 8 19 4 | 23 24 16 23 25 18 24 22 25 30 21
20 | 8 8 12 10 9 6 8 9 8 18 3 | 22 22 25 25 23 23 25 24 25 31 22
21 | 10 11 16 9 15 7 11 13 10 18 4 | 28 27 22 25 28 23 27 24 21 28 23
22 | 7 9 12 10 11 6 9 11 8 9 3 | 27 26 22 25 29 24 26 30 27 24 25
23 | 8 13 10 10 18 5 13 11 8 16 4 | 29 29 29 29 32 26 32 27 28 26 26
24 | 12 10 15 9 11 5 11 11 9 13 4 | 30 26 28 26 24 23 26 23 24 21 24
25 | 10 11 18 8 17 4 11 11 5 12 4 | 20 25 27 20 26 19 26 23 24 22 22
26 | 9 11 12 12 11 5 11 9 9 13 3 | 21 24 20 20 17 19 23 18 20 24 19
27E | 13 14 15 11 16 5 10 11 13 14 4 | 482 489 482 486 482 487 482 486 487 479 485
28 | 9 15 12 9 15 7 8 16 8 15 4 | 25 29 21 21 30 20 29 20 26 16 22
29E | 9 14 7 10 18 4 12 12 9 10 4 | 24 21 20 22 21 18 21 21 21 21 20
30 | 7 9 14 10 13 3 8 12 11 12 3 | 30 29 35 30 32 28 30 29 31 31 29
31 | 9 14 11 11 17 3 11 10 8 8 4 | 24 31 17 25 36 20 25 22 21 21 23
32 | 9 10 9 10 12 4 9 15 7 20 4 | 16 20 18 16 21 14 22 25 22 23 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 13 10 15 5 10 11 9 14 |T 39 41 38 39 42 36 41 39 40 39 38
WRMS | 9 13 13 10 14 5 10 11 8 13 |NE 25 28 24 25 27 22 27 25 25 24 24
MEDI | 9 12 12 10 15 5 10 11 9 13 |MD 24 26 22 25 26 20 26 23 24 24 22
Table 3.1824.2 GPS week: 1824 Day: 2 MJD: 57014.000
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 14 12 15 4 8 11 6 10 3 | 21 27 21 19 25 19 25 19 19 21 20
2 | 12 12 17 9 13 6 13 11 10 19 4 | 27 28 26 31 28 25 26 28 27 29 25
X3 | 11 9 13 12 --- 8 13 18 7 5 4 | 66 61 68 65 --- 64 62 62 64 64 63
4 | 9 10 10 10 14 3 6 6 6 19 3 | 22 25 19 20 27 19 22 22 20 26 20
5 | 11 10 10 9 10 5 13 10 11 11 3 | 26 29 28 27 25 26 28 26 31 25 26
6 | 14 8 12 7 11 5 10 13 8 10 3 | 28 26 25 22 25 22 28 24 26 22 23
7 | 7 13 9 11 15 5 12 11 8 7 3 | 24 28 20 25 29 22 28 22 25 20 22
X8 | 14 17 12 10 --- 6 11 12 15 --- 5 | 25 22 21 18 --- 16 20 17 25 --- 18
9 | 8 8 12 6 15 4 8 9 6 9 3 | 30 34 34 31 34 30 35 29 31 29 31
10 | 11 7 11 8 8 6 8 8 9 10 3 | 26 26 25 30 28 25 26 29 32 29 27
11 | 11 10 15 13 22 4 7 10 9 13 4 | 30 34 25 33 43 27 31 32 28 30 29
12 | 15 14 13 11 16 5 16 13 9 14 4 | 22 25 20 24 26 18 25 21 23 19 20
13 | 8 11 11 10 22 5 10 10 9 18 4 | 23 27 17 22 35 18 24 21 24 20 20
14 | 8 8 9 8 14 5 11 13 8 13 3 | 20 21 16 21 26 18 22 19 22 16 18
15 | 11 15 14 8 12 6 14 18 10 15 4 | 20 29 19 21 24 17 25 24 22 15 19
16 | 14 16 13 13 18 7 14 9 14 18 5 | 23 23 16 22 20 15 23 16 23 16 16
17E | 8 9 7 9 18 5 14 13 8 15 4 | 24 23 19 20 22 17 24 22 21 26 20
18 | 10 13 13 15 15 7 11 9 11 12 4 | 15 22 18 25 20 16 14 20 24 16 17
19E | 8 15 7 13 13 3 11 9 8 17 4 | 18 26 18 21 23 18 23 17 23 27 19
20 | 14 10 12 11 11 5 10 10 7 14 3 | 25 22 21 23 20 21 22 24 22 28 20
21 | 14 24 21 10 19 5 17 14 13 18 6 | 22 37 23 26 30 22 24 22 26 20 22
22 | 10 10 10 9 13 5 8 9 9 8 3 | 28 28 22 30 30 24 24 29 29 26 26
23 | 9 17 10 9 20 6 14 12 8 15 4 | 22 25 18 22 25 18 26 20 21 17 18
24 | 12 12 16 8 11 5 11 12 12 13 4 | 30 26 30 28 26 25 25 23 27 26 25
25 | 16 10 16 7 13 5 10 14 6 13 4 | 23 23 26 21 23 18 22 20 21 22 20
26 | 8 11 13 10 11 8 9 9 11 16 4 | 21 25 20 20 20 18 24 19 22 27 20
27E | 11 15 17 12 17 6 12 8 13 15 4 | 561 560 562 560 557 562 475 562 562 481 561
28 | 12 11 12 8 17 5 11 12 7 14 4 | 27 29 22 20 31 21 28 21 23 18 22
29E | 11 14 7 9 15 4 12 10 7 11 3 | 19 22 15 21 19 15 19 18 21 22 17
30 | 6 10 14 10 11 4 8 9 9 7 3 | 32 33 37 30 34 31 31 31 33 34 32
31 | 13 10 10 8 19 6 12 12 10 11 4 | 25 28 18 25 36 21 25 23 27 19 23
32 | 10 8 8 9 13 4 9 16 7 19 4 | 15 22 16 18 20 15 20 25 18 21 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 12 13 10 15 5 11 11 9 14 |T 41 44 40 41 44 38 39 40 42 39 39
WRMS | 11 12 12 10 14 5 11 10 8 13 |NE 25 28 23 25 27 22 26 24 26 24 23
MEDI | 11 10 12 9 14 5 11 11 9 13 |MD 24 26 21 22 26 19 25 22 24 22 20
Table 3.1824.3 GPS week: 1824 Day: 3 MJD: 57015.000
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 15 12 17 5 8 8 6 13 3 | 22 28 27 24 29 22 29 23 25 26 23
2 | 11 13 14 11 15 6 18 11 9 17 4 | 31 32 31 38 34 32 30 35 32 38 31
X3 | 8 11 12 12 --- 5 14 7 8 10 4 | 46 44 45 44 --- 45 47 44 45 48 44
4 | 7 11 12 10 14 5 9 7 8 14 3 | 24 26 22 23 27 20 24 24 18 26 21
5 | 7 8 12 9 10 4 13 12 10 12 3 | 33 34 31 33 33 30 33 33 33 33 31
6 | 6 7 11 8 14 6 10 8 7 11 3 | 28 32 28 31 29 26 33 29 29 29 28
7 | 7 14 7 15 17 4 14 10 6 13 4 | 28 34 23 33 34 25 31 31 28 22 27
X8 | 13 15 14 18 --- 7 11 11 14 --- 5 | 23 26 28 26 --- 19 25 21 28 --- 23
9 | 8 8 11 10 13 5 7 11 8 13 3 | 40 44 45 41 45 41 45 42 43 41 41
10 | 7 7 12 9 8 6 9 6 6 11 3 | 27 28 25 31 30 24 26 28 26 29 26
11 | 6 13 16 13 25 7 10 10 7 11 4 | 34 42 32 36 50 33 40 39 33 34 35
12 | 8 12 14 9 18 6 16 11 10 17 4 | 24 29 23 27 29 21 27 24 25 26 23
13 | 7 13 11 13 22 5 12 14 11 18 4 | 25 29 18 23 35 19 27 22 23 18 21
14 | 8 9 9 8 14 4 12 14 10 14 3 | 24 23 20 22 29 19 21 22 23 17 19
15 | 7 12 12 9 15 5 15 15 11 13 4 | 26 30 24 23 26 20 29 25 23 21 22
16 | 11 15 10 11 17 4 12 11 11 16 4 | 26 24 22 23 23 18 24 20 20 18 19
17E | 9 11 7 7 16 5 14 14 9 18 4 | 24 24 19 22 25 19 21 25 21 28 20
18 | 7 15 11 21 16 5 15 11 14 12 5 | 26 28 23 36 29 22 23 27 18 21 22
19E | 7 12 7 10 12 5 11 8 6 12 3 | 25 23 19 24 28 21 26 20 22 25 21
20 | 8 10 12 12 11 5 7 10 12 16 3 | 30 31 30 32 30 29 28 33 30 33 28
21 | 10 11 14 10 39 7 13 16 21 16 6 | 34 36 32 37 43 33 30 36 37 30 31
22 | 7 10 10 9 14 6 9 10 11 13 3 | 36 32 30 35 40 30 31 34 29 31 31
23 | 7 14 10 13 20 5 13 11 7 14 4 | 29 33 27 33 34 26 32 29 31 26 28
24 | 9 9 14 10 15 7 12 9 10 15 4 | 26 27 27 27 28 24 23 21 24 23 23
25 | 8 9 17 7 14 3 12 15 8 18 4 | 26 30 30 26 29 23 26 27 26 29 25
26 | 10 9 11 9 11 8 11 10 11 16 3 | 23 25 21 21 18 19 25 21 19 27 20
27E | 18 23 19 14 96 7 43 15 24 13 8 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
28 | 8 12 14 9 19 6 11 8 9 18 4 | 25 29 21 22 33 20 29 20 23 19 22
29E | 8 14 6 8 11 5 12 11 10 10 3 | 26 23 20 27 25 19 21 23 24 25 22
30 | 9 12 14 8 10 3 8 10 8 11 3 | 31 33 34 27 36 29 31 31 30 28 29
31 | 7 11 8 10 19 5 11 13 9 10 3 | 25 27 18 23 36 19 24 26 23 21 23
32 | 8 7 9 9 15 4 9 16 10 20 4 | 22 23 21 24 27 19 25 29 19 28 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 12 12 11 24 5 14 11 11 14 |T 28 29 26 28 31 24 28 27 26 27 25
WRMS | 8 12 12 11 14 5 14 11 8 14 |NE 28 30 27 29 32 25 29 28 27 27 26
MEDI | 8 11 12 10 15 5 12 11 9 13 |MD 26 29 25 27 29 22 27 27 25 26 23
Table 3.1824.4 GPS week: 1824 Day: 4 MJD: 57016.000
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 12 15 9 11 4 7 8 5 12 3 | 19 25 23 16 25 17 24 18 17 19 18
2 | 11 15 15 15 14 6 13 11 7 16 4 | 28 30 29 38 31 29 28 30 31 34 28
X3 | 9 9 12 10 --- 4 13 8 7 12 3 | 39 36 37 36 --- 37 39 34 36 32 35
4 | 7 9 10 13 12 4 26 10 8 13 4 | 20 22 19 20 22 18 37 21 18 20 19
5 | 10 13 11 12 11 5 11 9 10 13 4 | 27 28 28 29 26 26 30 25 29 31 26
6 | 7 8 12 11 11 4 8 11 6 13 3 | 23 27 25 25 26 22 30 23 23 21 23
7 | 6 18 7 14 16 5 13 8 7 17 4 | 26 35 21 30 31 21 30 24 27 21 25
X8 | 12 14 13 16 --- 8 11 10 13 --- 5 | 22 27 25 22 --- 20 24 21 26 --- 21
9 | 7 9 11 7 12 4 7 8 10 9 3 | 39 43 42 41 42 37 43 39 35 38 39
10 | 11 8 11 9 9 4 7 6 8 12 3 | 25 21 22 26 27 21 24 22 24 25 22
11 | 10 9 15 11 20 6 8 9 7 11 3 | 33 38 30 36 47 31 36 34 29 31 32
12 | 8 17 13 13 17 5 14 9 7 16 4 | 21 29 21 25 29 21 27 23 23 24 22
13 | 7 12 10 14 22 4 11 9 7 16 4 | 19 26 16 22 32 17 24 19 19 17 18
14 | 8 13 9 10 14 5 12 10 6 18 3 | 21 29 20 21 25 20 25 22 21 19 20
15 | 8 16 12 10 14 4 15 8 8 14 4 | 23 29 23 23 26 21 25 20 24 21 21
16 | 12 14 11 12 14 4 11 9 13 17 4 | 21 24 19 22 22 16 22 16 23 20 17
17E | 9 10 7 9 17 4 14 12 7 14 4 | 22 24 18 22 27 17 27 21 24 24 21
18 | 5 14 11 22 15 5 12 10 9 13 4 | 19 23 20 35 18 20 17 23 28 21 20
19E | 7 20 9 12 13 5 12 7 8 15 4 | 19 25 20 21 28 18 22 20 18 27 19
20 | 11 8 12 12 9 5 7 7 7 16 3 | 18 19 21 22 21 17 19 20 20 18 18
21 | 10 14 16 10 13 8 15 9 10 19 4 | 26 32 28 32 35 29 31 29 26 27 26
22 | 7 11 11 9 11 6 8 8 7 13 3 | 25 30 26 32 27 24 25 29 27 25 26
23 | 8 13 9 11 19 5 13 8 11 17 4 | 25 30 23 23 31 21 30 22 24 19 23
24 | 8 14 14 12 13 5 10 7 4 16 3 | 21 25 26 26 24 21 21 20 21 22 20
25 | 6 12 16 12 14 4 11 9 5 14 3 | 21 28 30 23 26 22 25 24 23 25 23
26 | 10 9 11 13 12 6 10 9 9 21 4 | 21 24 23 23 16 21 25 22 19 28 20
X27E | 10 22 18 16 91 6 --- 16 14 --- 7 | 878 877 874 877 868 876 --- 872 878 --- 877
28 | 9 11 11 11 18 4 9 7 5 13 3 | 23 28 21 22 29 18 27 17 21 17 20
29E | 8 15 7 10 15 3 13 10 6 9 3 | 25 24 19 28 30 21 24 23 24 22 22
30 | 7 10 13 11 13 3 9 6 7 10 3 | 26 27 32 26 32 24 30 25 28 25 27
31 | 7 11 10 12 18 4 10 9 9 12 3 | 28 33 19 28 35 23 28 27 27 27 26
32 | 11 12 9 15 13 5 9 21 5 21 4 | 12 20 14 16 19 12 20 21 12 15 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 12 12 15 5 12 9 8 15 |T 50 54 50 52 55 48 27 50 50 23 49
WRMS | 8 13 12 12 14 5 12 9 7 14 |NE 23 28 24 26 27 22 27 23 24 23 23
MEDI | 8 12 11 12 14 5 11 9 7 14 |MD 23 27 23 25 27 21 25 22 24 22 22
Table 3.1824.5 GPS week: 1824 Day: 5 MJD: 57017.000
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 16 13 9 12 5 9 12 7 9 3 | 23 34 25 25 23 21 27 20 22 23 23
2 | 10 13 16 12 13 6 14 13 9 17 4 | 28 27 24 29 24 27 30 28 27 31 25
X3 | 7 8 10 11 --- 3 13 12 5 9 3 | 35 37 41 37 --- 35 36 35 36 38 35
4 | 7 17 11 12 18 6 7 12 9 16 4 | 18 31 17 20 22 17 21 19 17 23 18
5 | 9 10 11 12 10 5 11 11 9 14 3 | 26 28 26 27 21 24 30 22 26 27 24
6 | 5 9 13 8 10 4 8 10 7 13 3 | 23 29 23 22 25 20 30 21 22 23 22
7 | 8 17 8 13 19 6 14 10 7 12 4 | 27 33 23 30 32 25 32 25 26 24 25
X8 | 14 15 12 10 --- 12 10 9 14 --- 5 | 27 31 23 22 --- 21 23 21 24 --- 22
9 | 8 11 11 9 13 4 9 9 8 12 3 | 37 40 40 38 35 36 42 34 35 35 36
10 | 8 8 11 10 13 5 9 5 6 11 3 | 28 25 23 28 24 26 27 22 28 26 24
11 | 6 10 15 11 19 4 8 10 7 12 3 | 26 35 24 32 35 26 32 26 25 28 27
12 | 8 13 15 12 23 4 15 14 8 19 4 | 22 28 20 24 30 18 28 22 20 22 21
13 | 8 13 10 12 21 4 11 8 8 15 4 | 22 28 18 22 31 18 26 18 22 17 20
14 | 9 15 9 11 15 5 11 13 8 17 4 | 22 24 19 25 27 20 26 23 22 22 21
15 | 7 13 12 9 13 5 12 10 9 18 4 | 20 26 20 20 21 16 24 16 22 17 18
16 | 11 13 10 13 20 6 13 11 13 15 4 | 21 24 20 26 26 19 26 19 22 18 19
17E | 7 13 8 9 14 3 13 14 8 13 3 | 25 30 24 27 23 25 27 26 27 26 25
18 | 9 11 10 20 14 4 11 16 8 15 4 | 18 19 20 28 16 15 19 22 17 24 16
19E | 7 17 7 12 14 5 11 11 8 20 4 | 24 26 23 26 22 23 26 22 24 30 22
20 | 9 9 12 14 9 3 7 10 9 17 3 | 20 22 23 23 16 20 23 19 20 22 19
21 | 9 13 14 13 13 5 14 15 9 18 4 | 24 27 24 25 24 20 26 23 24 24 21
22 | 9 9 9 11 11 4 6 11 10 8 3 | 23 22 20 24 22 19 24 25 19 20 20
23 | 7 16 10 10 18 5 14 10 9 15 4 | 29 35 29 28 29 28 36 24 27 25 27
24 | 11 21 15 9 19 5 11 13 10 21 5 | 27 30 28 25 32 21 26 22 24 24 23
25 | 9 12 15 10 20 5 11 13 7 13 4 | 23 31 26 18 32 20 27 22 22 25 23
26 | 10 11 12 10 16 5 11 14 7 15 4 | 20 24 20 19 20 18 25 19 18 25 19
27E | 8 13 17 14 18 5 11 11 14 17 4 | 992 991 989 988 970 992 886 991 990 886 990
28 | 9 9 11 10 19 3 10 9 7 12 3 | 24 30 22 23 30 21 30 19 21 19 22
29E | 9 14 6 10 15 5 17 17 9 10 4 | 28 23 21 23 19 19 23 29 27 25 22
30 | 9 12 12 12 15 4 9 11 7 8 3 | 29 32 34 30 33 28 29 29 27 31 28
31 | 8 12 9 9 26 5 9 12 9 13 4 | 24 29 16 23 40 20 25 22 20 20 21
32 | 10 9 9 12 18 3 7 22 8 20 4 | 20 22 18 20 22 17 22 26 18 21 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 12 11 16 5 11 12 9 15 |T 54 58 53 55 57 52 54 53 53 52 53
WRMS | 9 13 12 11 15 5 11 11 8 14 |NE 24 28 23 25 26 22 27 22 23 24 22
MEDI | 8 13 11 11 15 5 11 11 8 15 |MD 24 28 23 25 24 20 26 22 22 24 22
Table 3.1824.6 GPS week: 1824 Day: 6 MJD: 57018.000
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 8 17 8 11 5 9 11 6 9 3 | 21 28 23 22 25 19 25 21 19 22 20
2 | 11 14 14 12 13 6 13 11 8 20 4 | 34 33 29 41 34 34 31 40 34 43 33
X3 | 9 9 14 12 --- 4 14 17 6 10 4 | 47 49 49 48 --- 46 47 50 45 49 46
4 | 6 11 12 11 12 4 8 9 9 13 3 | 25 32 20 25 28 22 26 27 25 29 25
5 | 9 9 10 10 10 4 10 9 8 11 3 | 37 36 34 35 35 34 37 35 37 36 35
6 | 7 7 12 10 11 3 9 10 6 13 3 | 27 33 27 26 31 23 33 26 29 26 27
7 | 8 15 9 9 10 4 12 9 8 8 3 | 27 31 20 29 31 24 30 25 25 23 25
X8 | 12 16 11 14 --- 10 11 11 16 --- 5 | 22 27 22 20 --- 19 20 21 25 --- 20
9 | 8 8 10 10 16 5 9 11 8 12 3 | 45 49 48 44 47 43 49 44 44 45 45
10 | 9 6 10 9 10 4 7 5 5 8 2 | 27 28 26 32 33 27 28 31 30 30 28
11 | 8 11 16 12 21 4 8 11 10 10 4 | 38 44 31 42 50 35 39 39 37 36 38
12 | 11 16 12 12 18 5 13 15 9 16 4 | 27 33 26 29 32 24 28 30 27 27 27
13 | 6 13 13 10 20 4 10 8 7 15 4 | 23 32 20 23 38 20 25 23 22 17 22
14 | 8 15 10 11 13 4 13 13 12 13 4 | 31 35 27 29 33 27 32 36 32 26 29
15 | 6 15 13 8 13 4 12 13 8 15 4 | 23 33 26 23 24 19 26 18 22 18 22
16 | 10 14 13 13 15 7 11 13 8 16 4 | 24 29 21 24 23 19 25 21 18 20 20
17E | 8 13 9 11 13 5 14 13 7 17 4 | 28 26 26 29 29 23 27 30 28 34 27
18 | 7 13 11 19 15 4 13 13 8 11 4 | 19 22 19 32 19 17 15 26 23 19 19
19E | 7 21 9 11 12 5 12 11 8 13 4 | 20 28 19 22 20 19 21 23 22 24 20
20 | 9 8 12 12 9 3 7 14 7 16 3 | 19 25 21 26 19 20 17 28 22 27 21
21 | 7 14 14 9 14 7 14 13 15 17 4 | 30 33 27 33 38 29 28 32 33 32 29
22 | 8 9 12 10 12 5 9 10 8 9 3 | 29 32 27 34 33 26 26 35 29 28 29
23 | 8 16 10 9 16 5 13 16 10 12 4 | 19 31 22 19 28 18 30 23 22 19 21
24 | 12 15 13 8 13 5 12 11 11 14 4 | 30 30 28 28 28 25 23 26 27 27 26
25 | 11 11 16 8 17 3 11 12 9 14 4 | 23 31 29 22 28 21 24 24 24 24 24
26 | 9 10 11 9 13 7 10 12 8 15 3 | 18 27 24 20 17 19 20 19 19 24 19
27E | 9 14 18 13 17 5 11 7 8 13 4 | 905 901 907 907 888 904 820 906 903 830 905
28 | 10 12 11 8 15 4 8 11 7 14 3 | 26 33 23 25 31 21 27 22 24 19 24
29E | 11 16 8 10 16 7 15 20 10 11 4 | 30 28 20 24 23 20 21 28 26 28 23
30 | 9 11 13 7 10 4 9 9 7 10 3 | 29 32 32 27 31 26 28 28 26 29 28
31 | 9 12 8 10 18 5 8 8 10 11 3 | 31 38 23 30 41 26 31 33 30 27 30
32 | 10 9 9 12 12 4 7 23 8 23 4 | 16 27 17 20 22 15 22 25 19 21 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 12 11 14 5 11 12 9 14 |T 54 59 53 55 58 52 52 56 54 53 53
WRMS | 9 13 12 10 14 5 11 11 7 13 |NE 27 32 26 28 30 24 28 28 27 27 26
MEDI | 9 12 12 10 13 4 11 11 8 13 |MD 27 32 26 27 31 23 27 27 26 27 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 4.1824 GPS week: 1824 MJD: 57012.0-57018.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 8 8 16 |U 11 12 40 |U 6 7 14 |
emr | emr 3071 | 11 9 23 |U 13 12 40 | 7 9 20 |
esa | esa 3072 | 8 8 19 |U 12 12 39 |U 7 8 20 |
gfz | gfz 3071 |U 8 9 19 |U 11 13 39 |U 6 8 15 |
grg | grg 2879 | 13 13 34 |U 12 14 37 |U 7 8 19 |
igr | igr 3071 | 8 8 17 | 11 12 38 | 6 7 15 |
igs | igs 3072 | 8 9 18 | 11 12 38 | 6 7 16 |
jpl | jpl 3057 | 9 9 22 |U 12 13 38 |U 7 8 19 |
mit | mit 3072 | 9 9 19 |U 12 14 41 |U 7 9 18 |
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 5.1824.0 GPS week: 1824 Day: 0 MJD: 57012.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 3 5 16 | 10 13 29 | 6 8 15 |
emr | emr 3072 | 6 5 22 | 12 14 31 | 7 9 18 |
esa | esa 3072 | 4 5 16 | 11 14 34 | 8 9 22 |
gfz | gfz 3071 | 5 5 19 | 11 14 31 | 6 8 16 |
grg | grg 2880 | 6 5 22 | 11 14 31 | 7 10 20 |
igr | igr 3072 | 4 5 17 | 10 13 29 | 6 7 17 |
igs | igs 3072 | 4 6 19 | 10 13 31 | 6 8 16 |
jpl | jpl 3070 | 5 6 20 | 12 14 32 | 7 8 18 |
mit | mit 3072 | 5 4 14 | 12 12 31 | 7 8 17 |
Table 5.1824.1 GPS week: 1824 Day: 1 MJD: 57013.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 4 16 | 9 12 46 | 5 8 15 |
emr | emr 3072 | 9 6 21 | 12 11 39 | 7 12 24 |
esa | esa 3072 | 7 5 19 | 9 11 45 | 7 10 22 |
gfz | gfz 3072 | 8 6 19 | 9 13 44 | 7 9 18 |
grg | grg 2880 | 10 6 32 | 12 14 45 | 8 11 19 |
igr | igr 3072 | 7 4 17 | 9 11 45 | 6 9 18 |
igs | igs 3072 | 7 5 18 | 9 11 43 | 6 9 19 |
jpl | jpl 3071 | 7 6 22 | 10 12 45 | 8 11 24 |
mit | mit 3072 | 9 5 21 | 10 18 45 | 8 11 19 |
Table 5.1824.2 GPS week: 1824 Day: 2 MJD: 57014.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 4 5 12 | 7 10 30 | 5 6 13 |
emr | emr 3072 | 8 8 19 | 9 8 29 | 6 9 22 |
esa | esa 3072 | 5 5 14 | 9 9 32 | 6 7 19 |
gfz | gfz 3071 | 5 6 13 | 8 9 29 | 5 6 14 |
grg | grg 2880 | 9 4 30 | 10 9 32 | 7 7 18 |
igr | igr 3072 | 4 5 12 | 7 9 30 | 5 6 15 |
igs | igs 3072 | 5 5 13 | 8 9 29 | 5 6 16 |
jpl | jpl 3071 | 5 6 18 | 8 9 31 | 7 7 20 |
mit | mit 3072 | 7 11 19 | 8 10 28 | 7 9 18 |
Table 5.1824.3 GPS week: 1824 Day: 3 MJD: 57015.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 5 4 15 | 11 16 42 | 7 9 17 |
emr | emr 3072 | 7 6 23 | 11 12 37 | 8 10 21 |
esa | esa 3072 | 5 6 18 | 11 14 37 | 9 11 21 |
gfz | gfz 3072 | 5 5 17 | 11 14 40 | 8 10 19 |
grg | grg 2880 | 8 4 18 | 12 15 38 | 7 9 24 |
igr | igr 3072 | 5 5 16 | 11 13 36 | 8 9 17 |
igs | igs 3072 | 5 5 17 | 10 14 38 | 8 10 19 |
jpl | jpl 3072 | 6 7 22 | 10 13 37 | 9 10 21 |
mit | mit 3072 | 6 6 17 | 14 14 49 | 10 12 23 |
Table 5.1824.4 GPS week: 1824 Day: 4 MJD: 57016.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 4 6 17 | 8 12 40 | 5 5 12 |
emr | emr 3071 | 7 7 25 | 11 11 41 | 7 8 19 |
esa | esa 3072 | 5 5 18 | 9 10 32 | 7 8 22 |
gfz | gfz 3072 | 5 7 23 | 9 12 43 | 6 7 17 |
grg | grg 2880 | 9 10 27 | 11 13 35 | 7 8 16 |
igr | igr 3070 | 4 7 18 | 8 11 36 | 6 6 15 |
igs | igs 3072 | 5 7 21 | 9 12 40 | 5 6 16 |
jpl | jpl 2975 | 5 6 22 | 9 13 33 | 6 5 16 |
mit | mit 3072 | 5 6 18 | 10 12 43 | 7 8 19 |
Table 5.1824.5 GPS week: 1824 Day: 5 MJD: 57017.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 4 6 13 | 28 16 68 | 5 6 12 |
emr | emr 3072 | 6 7 18 | 28 20 70 | 6 6 19 |
esa | esa 3072 | 4 5 13 | 27 17 63 | 6 6 17 |
gfz | gfz 3072 | 4 6 14 | 26 16 63 | 5 7 14 |
grg | grg 2877 | 15 26 46 | 20 20 53 | 5 6 20 |
igr | igr 3072 | 3 6 12 | 26 17 62 | 5 6 14 |
igs | igs 3072 | 4 7 13 | 25 17 62 | 5 6 15 |
jpl | jpl 3070 | 4 7 16 | 26 19 63 | 7 8 19 |
mit | mit 3072 | 4 7 13 | 28 21 61 | 5 8 17 |
Table 5.1824.6 GPS week: 1824 Day: 6 MJD: 57018.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 28 24 26 | 7 9 27 | 5 6 11 |
emr | emr 3071 | 31 25 34 | 10 9 32 | 7 7 17 |
esa | esa 3072 | 29 27 33 | 8 9 33 | 7 7 16 |
gfz | gfz 3072 | 28 27 30 | 7 10 25 | 6 7 11 |
grg | grg 2880 | 36 36 65 | 7 11 26 | 7 5 15 |
igr | igr 3071 | 28 27 28 | 7 9 27 | 6 7 11 |
igs | igs 3072 | 28 26 29 | 7 9 27 | 6 6 12 |
jpl | jpl 3071 | 29 28 33 | 8 10 30 | 8 9 16 |
mit | mit 3072 | 28 26 30 | 7 11 30 | 6 8 12 |
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 6.1824 GPS week: 1824 MJD: 57012.500-57018.500
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 | -19 -2 68 69 3 | 10 20
| 20 16 76 99 4 | 3
emr uuuuu | 4 13 -66 -29 -6 | 21 29
| 17 16 68 78 22 | 7
esa uuuuu | -1 23 20 29 0 | 10 19
| 16 18 66 37 3 | 3
gfz uuxux | 10 -7 -47 -84 0 | 14 20
| 18 22 202 103 4 | 2
grg uuuuu | 3 6 20 -85 -4 | 17 24
| 13 20 91 121 4 | 5
igr xxxxx | -22 0 -13 66 1 | 1 17
| 13 19 56 44 3 | 3
irf xxxxx | 12 5 8 16 0 | 1 16
| 7 5 46 56 3 | 3
jpl uuuuu | -19 -4 -48 -10 1 | 12 21
| 34 22 66 55 4 | 3
mit uuuuu | 17 -13 -10 72 -1 | 19 25
| 17 16 88 140 5 | 3
ngs uuxuu | 6 -15 203 -19 -2 | 10 18
| 28 42 311 49 8 | 3
sio uuxxx | 3 21 -270 16 -1 | 26 30
| 18 15 85 99 5 | 3
Table 7.1824.0 GPS week: 1824 Day: 0 MJD: 57012.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 0 4 76 38 -3 | 10 20
emr uuuuu | -20 1 -76 -35 -14 | 30 36
esa uuuuu | -6 -1 75 -25 0 | 11 20
gfz uuxux | 1 -27 249 -158 -2 | 16 22
grg uuuuu | 2 -16 81 -56 -5 | 23 29
igr xxxxx | -25 -2 43 27 -1 | 2 17
irf xxxxx | 22 -4 28 59 1 | 2 16
jpl uuuuu | -24 -22 -84 -4 1 | 15 23
mit uuuuu | 39 -43 -56 223 4 | 20 26
ngs uuxuu | -6 70 -244 -1 4 | 10 18
sio uuxxx | 19 13 -329 -16 3 | 26 29
Table 7.1824.1 GPS week: 1824 Day: 1 MJD: 57013.500
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 | -33 14 141 -34 5 | 8 20
emr uuuuu | -3 0 -190 137 -38 | 28 35
esa uuuuu | -26 22 42 79 -2 | 8 19
gfz uuxux | -14 -40 177 -247 -5 | 13 19
grg uuuuu | 24 -18 97 15 -7 | 19 25
igr xxxxx | -40 3 41 103 2 | -1 17
irf xxxxx | 12 4 -13 96 2 | -1 16
jpl uuuuu | -6 13 13 14 -1 | 12 21
mit uuuuu | 26 -11 -118 217 5 | 17 24
ngs uuxuu | 17 3 -47 -90 8 | 8 17
sio uuxxx | 27 18 -257 51 5 | 25 28
Table 7.1824.2 GPS week: 1824 Day: 2 MJD: 57014.500
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 | -51 -20 114 -56 7 | 10 21
emr uuuuu | 31 37 -28 -80 -21 | 24 33
esa uuuuu | -12 42 6 37 3 | 10 20
gfz uuxux | -5 -12 -229 -13 4 | 14 19
grg uuuuu | 12 9 48 -69 -7 | 20 26
igr xxxxx | -27 17 -57 113 4 | 1 18
irf xxxxx | 4 10 -55 58 2 | 1 17
jpl uuuuu | 12 16 -40 -91 0 | 13 22
mit uuuuu | 6 -13 -78 151 2 | 19 26
ngs uuxuu | 13 -43 311 68 1 | 10 19
sio uuxxx | -5 22 -244 132 5 | 26 30
Table 7.1824.3 GPS week: 1824 Day: 3 MJD: 57015.500
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 -23 108 132 7 | 15 22
emr uuuuu | 0 31 -30 -12 -11 | 24 33
esa uuuuu | -2 33 15 71 3 | 14 20
gfz uuxux | 8 10 -242 -155 7 | 17 21
grg uuuuu | 4 28 -156 -294 -2 | 21 27
igr xxxxx | -9 30 -28 51 3 | 5 17
irf xxxxx | 2 7 -40 10 2 | 5 15
jpl uuuuu | -35 -21 -8 -46 -5 | 16 23
mit uuuuu | -9 -12 -52 118 2 | 23 28
ngs uuxuu | 55 -37 526 -7 -1 | 14 19
sio uuxxx | -24 34 -336 143 -2 | 30 33
Table 7.1824.4 GPS week: 1824 Day: 4 MJD: 57016.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -22 17 -80 193 0 | 11 20
emr uuuuu | 12 16 -81 -56 20 | 16 27
esa uuuuu | 18 -1 115 21 -3 | 11 18
gfz uuxux | 32 7 -219 -18 2 | 14 19
grg uuuuu | -3 35 -51 -207 -8 | 16 23
igr xxxxx | -12 -6 -64 43 2 | 1 16
irf xxxxx | 15 6 56 -48 -4 | 1 15
jpl uuuuu | -56 7 0 -34 8 | 12 21
mit uuuuu | 18 -15 86 -37 -5 | 20 25
ngs uuxuu | 14 -37 570 -19 -4 | 11 18
sio uuxxx | -11 10 -264 -2 -5 | 26 30
Table 7.1824.5 GPS week: 1824 Day: 5 MJD: 57017.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -22 3 96 39 3 | 6 17
emr uuuuu | -9 3 -81 -69 20 | 10 16
esa uuuuu | 15 39 -27 19 -3 | 5 16
gfz uuxux | 15 -10 -83 -34 -4 | 10 17
grg uuuuu | -17 3 63 14 -4 | 9 17
igr xxxxx | -36 -23 -76 8 -4 | -4 16
irf xxxxx | 12 0 61 -23 -2 | -4 17
jpl uuuuu | 33 18 -179 85 0 | 6 16
mit uuuuu | 9 -8 114 -40 -3 | 14 22
ngs uuxuu | -20 -52 326 -28 -16 | 6 17
sio uuxxx | 14 45 -357 -95 -4 | 21 28
Table 7.1824.6 GPS week: 1824 Day: 6 MJD: 57018.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 9 -9 19 173 3 | 11 20
emr uuuuu | 19 1 27 -91 5 | 16 24
esa uuuuu | 10 26 -87 0 -1 | 10 18
gfz uuxux | 35 21 18 34 -1 | 14 20
grg uuuuu | 1 3 58 5 2 | 12 20
igr xxxxx | -6 -19 52 114 3 | 0 15
irf xxxxx | 19 10 20 -41 -5 | 1 16
jpl uuuuu | -57 -37 -40 5 3 | 11 19
mit uuuuu | 31 11 32 -129 -8 | 19 25
ngs uuxuu | -28 -7 -24 -58 -5 | 9 18
sio uuxxx | -1 3 -104 -103 -9 | 26 31
More information about the IGSREPORT
mailing list