[IGSREPORT-23243] Wk 1822 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat Dec 27 07:38:39 PST 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1822 (Dec 07, 2014 - Dec 13, 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:
igs1822[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1822[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1822[0-6].cls IGS GPS clock combination summary report.
igs18227.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18227.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 | 26
0 | ESA | 26 NRIL
0 | GFZ | 1 2 3 6 9 26 30 1 3 6 26 30 NRIL XMIS XMIS
0 | GRG | BJFS BOR1 BRST DARW GRAZ INVK KELY MAL2 MANA BJFS
0 | GRG | BOR1 BRST GRAZ INVK KELY
0 | JPL | 26
0 | MIT | 8 KOUR NRIL KOUR NRIL PARC
1 | COD | 26 HOB2 ZECK
1 | ESA | 3 3 26 BJFS BRST DAV1
1 | GFZ | 1 2 3 6 9 30 1 3 6 30 HOB2 REUN HOB2
1 | GRG | BRST GRAZ HOB2 KELY KERG KOUC KOUR MCM4 RABT THTI
1 | GRG | ZECK GRAZ KELY KOUC KOUR
1 | MIT | 3 4 3 4 6 8 HOB2
2 | COD | 26 HOB2
2 | ESA | 3 3 26 HOB2 GRAZ PIMO TIXI TRO1
2 | GFZ | 1 2 3 6 9 16 26 30 1 3 6 13 16 26 30 HOB2 INVK WAB2
2 | GFZ | YIBL HOB2 INVK WAB2
2 | GRG | 13 13 BOR1 GRAZ KOUC MANA MAS1 MCM4 XMIS BOR1 GRAZ
2 | GRG | HOB2 KOUC XMIS
2 | JPL | 26 CHUR
2 | MIT | 3 3 8 HOB2 MAW1 HOB2 MAW1
3 | COD | 26 26 TLSE
3 | ESA | 26 26 BJFS BJFS
3 | GFZ | 1 2 3 6 9 30 1 3 6 26 30 BRFT GUUG NRIL RIOP THTI
3 | GFZ | BRFT CAS1
3 | GRG | BRFT BRFT TLSE
3 | MIT | 3 7 8 3 7 8
4 | COD | 26 NYA1 RBAY
4 | ESA | 26 26 HOB2 KIRU HOB2 KIRU
4 | GFZ | 1 2 3 6 30 1 3 6 26 30
4 | GRG | KELY MCM4 RBAY TRO1 BRFT HNPT KELY NYA1
4 | MIT | 3 8 18 21 3 8 18 21 BRFT TOW2
5 | COD | HOB2 MAC1 HOB2 MAC1
5 | EMR | 3 26
5 | GFZ | 1 2 3 6 30 1 3 6 30 DRAG HOB2 SYOG HOB2 THU2
5 | GRG | 26 BRFT FAIR HOB2 HYDE KOUC SYOG BRFT DRAG FAIR HYDE
5 | GRG | KOUC
5 | JPL | NRIL
5 | MIT | 3 3 6 26 SYOG HOB2
6 | COD | BOR1
6 | EMR | 26
6 | ESA | 32 32
6 | GFZ | 1 2 3 6 9 30 1 3 6 30 ALIC ARTU ASPA AUCK BAKE BARH
6 | GFZ | BJFS BRAZ BRFT BRMU CAS1 CEDU CHTI CHUR CONZ CORD
6 | GFZ | CRO1 DARW DAV1 DGAR DRAG DUBO FLIN GMSD GODE GOLD
6 | GFZ | GUAM GUUG HARB HNPT HOB2 HOFN HYDE INVK ISPA KERG
6 | GFZ | KIRU MAC1 MAL2 MANA MAS1 MAW1 MDVJ NANO NICO NKLG
6 | GFZ | NOVM NRIL ONSA PDEL PERT PIE1 PIMO QAQ1 REUN SCOR
6 | GFZ | SFER SOFI STJO SYOG THTI TIDB TLSE TOW2 TRO1 VILL
6 | GFZ | WTZR WUHN XMIS
6 | GRG | 13 26 KELY KELY
6 | JPL | 26
6 | MIT | 1 8 16 17 24 26 27 31 32 1 8 16 17 24 26 27 31 32
6 | MIT | CRO1 DUBO MONP
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
----+--------+--------+-------------
3 | GFZ | ~00:30 | ~ -0.15 ns
4 | GFZ | ~23:00 | ~ -0.14 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 table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G15 | 2014_12_11 | 2014089
8. 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
----+--------+---------------
1 | ESA | 3
9. 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 G09 | | | | | 4 | | |
PRN G10 | 4 | 4 | 4 | 4 | | | |
10. 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.
11. 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 | -1.5 -.4 -2.5 -26 -12 21 .30
EMR | 0 | 6.5 .4 3.2 10 44 26 .17
ESA | 0 | -.1 -.8 .5 35 -44 85 .22
GFZ | 0 | .6 .3 -1.2 -19 -95 19 .12
GRG | 0 | 1.3 3.0 -8.0 1 0 11 .54
JPL | 0 | .7 -5.2 3.3 -60 9 -14 .20
MIT | 0 | 9.7 3.1 2.3 7 -5 -17 .59
NGS | 0 | .1 1.2 -5.3 29 3 -5 .81
SIO | 0 | 5.7 .7 16.3 -9 14 -27 .48
COD | 1 | -1.2 .5 -1.6 -13 10 4 .36
EMR | 1 | 1.3 4.9 3.8 10 27 26 .42
ESA | 1 | .3 .0 -.1 -16 -33 63 .10
GFZ | 1 | .4 .9 -1.9 -20 -94 16 .06
GRG | 1 | 4.4 1.3 -11.3 -4 -23 14 .83
JPL | 1 | 1.8 -3.4 1.1 -26 34 -7 .17
MIT | 1 | 7.5 2.5 1.1 9 2 -26 .65
NGS | 1 | 9.2 2.7 1.9 16 -40 39 .82
SIO | 1 | 3.7 4.5 13.8 2 21 -22 .50
COD | 2 | -1.8 -1.0 -1.9 -29 9 8 .40
EMR | 2 | 3.6 6.6 6.8 10 27 32 .21
ESA | 2 | .5 .1 .4 -19 -27 60 .14
GFZ | 2 | -.1 .6 -2.0 -32 -97 14 .30
GRG | 2 | -.7 .0 -.6 6 -7 -7 .41
JPL | 2 | 1.1 -.6 8.8 -59 19 1 .11
MIT | 2 | 6.5 5.6 .2 9 -3 -23 .55
NGS | 2 | 3.9 3.0 -.9 23 -18 18 .79
SIO | 2 | 4.8 4.5 11.0 -1 -5 0 .51
COD | 3 | -1.2 .1 -1.2 -27 10 -11 .25
EMR | 3 | 4.8 6.1 8.5 18 17 39 -.03
ESA | 3 | -.2 -1.0 .8 17 -54 74 .06
GFZ | 3 | .3 .8 -.9 -34 -101 24 .07
GRG | 3 | 2.2 6.8 -12.2 17 -2 0 .27
JPL | 3 | -6.0 -3.9 7.3 -21 52 15 .10
MIT | 3 | 6.5 7.3 .5 16 0 -32 .26
NGS | 3 | -2.5 3.3 .1 16 10 -20 .44
SIO | 3 | 6.0 3.4 6.6 -1 -4 -2 .34
COD | 4 | -1.4 -.3 -1.2 -41 19 1 .16
EMR | 4 | -3.3 2.8 .6 16 7 34 -.10
ESA | 4 | .0 .6 .5 -24 -42 60 .05
GFZ | 4 | -.2 1.1 -1.6 -14 -91 13 .09
GRG | 4 | -.8 1.0 -12.2 13 -5 -20 .59
JPL | 4 | -3.8 -2.5 3.5 -19 23 -21 .01
MIT | 4 | 5.5 2.1 -1.6 12 -2 -25 .43
NGS | 4 | 4.1 1.7 -2.0 23 -17 14 .72
SIO | 4 | 6.3 .8 13.2 -9 16 -17 .46
COD | 5 | -1.0 .5 -.7 -29 13 2 .22
EMR | 5 | -2.3 3.1 3.4 33 -2 26 -.14
ESA | 5 | .2 .2 -.7 -6 -32 63 -.08
GFZ | 5 | .5 .5 -1.8 -41 -93 3 .09
GRG | 5 | 6.0 3.3 -9.6 -1 8 -14 .44
JPL | 5 | -.2 -11.3 3.3 -81 -6 -22 -.30
MIT | 5 | 5.7 1.8 -.3 16 2 -32 .36
NGS | 5 | -.7 -1.5 -9.4 40 7 -10 .36
SIO | 5 | 3.1 -.2 -1.1 -6 27 -28 .37
COD | 6 | -.8 .8 -1.3 -34 4 -20 .41
EMR | 6 | 3.6 4.7 -.7 11 12 21 -.05
ESA | 6 | .0 .4 -.5 -16 -27 72 -.08
GFZ | 6 | .9 .7 -2.1 -31 -103 19 -.18
GRG | 6 | 9.9 6.5 -21.9 -32 32 -19 .66
JPL | 6 | -.4 -.9 -2.6 -83 45 -29 -.34
MIT | 6 | 5.8 4.0 -.1 7 1 -25 .39
NGS | 6 | 6.5 4.8 -.1 33 -29 32 .48
SIO | 6 | 4.7 4.6 5.6 -4 9 -17 .36
12. 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.
13. 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 1.1822.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1822.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 2.1822.[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 3.1822.[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 5.1822.0-6). 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 1822 summary. (Dec 07, 2014 - Dec 13, 2014)
Table 1.1822.a GPS week: 1822 MJD: 56998.000-57004.000
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 250| 0 0 2 -4 4 2 -.03 11 10 | -683 -630 16 119
| 0 0 1 19 13 21 .04 | 425 549
emr 80| 0 -2 0 -22 -3 3 .21 13 13 | 3223 453 14 153
| 0 0 1 6 11 9 .04 | 1191 890
esa 150| 0 0 7 -10 -9 0 -.37 13 13 | -1493 1188 10 173
| 0 0 1 19 12 13 .01 | 560 850
gfz 198| 0 0 -6 -9 -23 36 .07 11 10 | -44 48 13 182
| 1 0 1 18 14 11 .02 | 327 581
grg 165| 0 -1 -5 -11 4 -39 .27 16 14 | 118 -77 16 165
| 1 1 3 12 16 7 .06 | 373 506
igr n/a| 0 0 2 -1 0 -10 -.17 5 5 | 440 241 15 86
| 0 0 1 10 12 13 .01 | 673 834
jpl 80| 0 0 3 4 36 -20 .18 12 12 | 3277 456 16 120
| 1 1 1 21 40 17 .02 | 1193 885
mit 349| 1 0 0 13 -2 15 -.10 12 11 | -369 69 24 173
| 0 1 0 34 24 19 .01 | 417 553
ngs 226| 0 1 -2 -3 -2 -17 -.01 9 8 | -551 -763 1413 3193
| 0 1 2 12 22 8 .04 | 389 555
sio 322| 0 0 1 33 -7 22 -.18 12 11 | --- --- --- ---
| 1 0 1 24 24 31 .03 | --- ---
Table 1.1822.b GPS week : 1822 MJD: 56998.000-57004.000
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 3 3 4 4 4 4 |
2 | 5 5 5 5 5 5 5 |
3 | 9 8 10 5 5 5 4 |
4 | 4 4 4 4 4 4 4 |
5 | 5 4 5 4 5 4 5 |
6 | 4 3 4 3 4 4 4 |
7 | 4 4 4 4 4 4 4 |
8 | 6 5 5 6 7 5 8 |
9 | 4 4 3 3 5 4 4 |
10 | 4 6 4 4 4 4 4 |
11 | 4 4 4 4 5 4 5 |
12 | 5 5 5 5 5 5 5 |
13 | 3 3 3 3 3 3 4 |
14 | 4 3 4 3 4 4 4 |
15 | 5 5 5 5 0 5 5 |
16 | 5 4 5 5 5 4 5 |
17 | 4 4 4 4 5 4 5 |
18 | 5 4 5 4 6 4 5 |
19 | 4 4 4 4 5 4 5 |
20 | 4 4 5 4 4 4 4 |
21 | 4 4 4 4 4 4 5 |
22 | 4 4 4 4 4 4 4 |
23 | 4 4 4 5 4 5 5 |
24 | 5 4 4 4 4 5 4 |
25 | 5 4 4 4 4 4 4 |
26 | 5 5 5 5 5 5 5 |
27 | 5 5 5 4 4 4 4 |
28 | 4 4 4 4 4 5 4 |
29 | 5 4 5 4 5 4 5 |
30 | 4 3 3 3 3 3 3 |
31 | 4 4 4 5 5 5 5 |
32 | 4 4 4 4 4 4 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 2.1822.0 GPS week: 1822 Day: 0 MJD: 56998.000
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| -1 0 2 -30 -5 -23 -.08 9 10 | -1229 27 15 116
emr 80| 0 -4 2 -26 15 9 .18 14 14 | 1809 -316 18 162
esa 150| 0 0 6 12 -9 -8 -.37 13 13 | -2296 -308 10 141
gfz 199| -1 0 -6 -4 -37 50 .11 12 11 | -17 101 14 177
grg 162| 0 -2 -6 -3 -5 -47 .20 16 16 | 426 -301 17 162
igr n/a| 0 0 0 13 14 -32 -.17 5 5 | -18 -720 14 74
jpl 80| 0 1 6 -14 -24 -53 .20 11 11 | 1864 -333 16 135
mit 348| 1 -3 -1 54 28 34 -.08 14 12 | -1091 993 26 158
ngs 226| -1 3 -5 -17 21 -30 .04 10 9 | -218 -1264 1476 3477
sio 319| 1 -1 1 46 0 85 -.16 12 12 | --- --- --- ---
Table 2.1822.1 GPS week: 1822 Day: 1 MJD: 56999.000
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| 0 0 2 -19 11 -8 -.07 10 9 | -650 -742 15 117
emr 80| 0 -2 0 -30 6 11 .25 12 12 | 1948 324 15 169
esa 150| 1 0 8 -14 13 27 -.37 13 13 | -1154 1786 10 139
gfz 199| -1 0 -8 11 -9 18 .04 10 10 | 207 -912 12 164
grg 161| 0 0 -6 6 -25 -49 .24 16 12 | 148 -288 16 161
igr n/a| -1 1 1 1 12 8 -.16 5 5 | -283 -32 15 80
jpl 80| 0 -1 2 -1 70 -30 .16 12 12 | 1992 320 15 129
mit 349| 1 -1 -1 27 -35 35 -.10 13 12 | -170 -301 25 167
ngs 228| -1 1 0 -10 -10 -15 .02 8 7 | -659 -744 1569 3566
sio 322| 1 0 1 59 -48 37 -.17 13 11 | --- --- --- ---
Table 2.1822.2 GPS week: 1822 Day: 2 MJD: 57000.000
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 0 4 13 -20 -14 -.04 10 10 | -656 -958 15 110
emr 80| 0 -1 2 -11 -7 15 .20 13 13 | 2225 2088 15 153
esa 150| 0 1 6 -8 -2 -5 -.39 13 14 | -1276 1841 10 132
gfz 199| -1 0 -5 9 -7 38 .06 12 11 | -346 747 14 177
grg 166| 1 -2 -9 -23 1 -33 .25 15 13 | -36 -23 16 151
igr n/a| -1 0 1 5 -12 -23 -.19 5 5 | -377 1713 15 81
jpl 80| -1 0 3 30 29 -15 .20 11 11 | 2290 2088 16 123
mit 348| 1 0 0 -22 19 37 -.12 11 10 | -645 352 23 144
ngs 227| 0 0 -3 10 -17 -23 .01 8 8 | -640 -974 1481 2893
sio 314| 0 -1 1 -17 8 20 -.14 13 12 | --- --- --- ---
Table 2.1822.3 GPS week: 1822 Day: 3 MJD: 57001.000
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 252| 0 0 2 -8 15 1 -.02 9 9 | -1137 -52 15 115
emr 80| 0 -1 1 -26 -19 -2 .21 14 14 | 4025 -260 15 151
esa 150| 1 0 5 -36 -18 -12 -.39 13 14 | -812 1271 10 176
gfz 195| 0 0 -6 -26 -31 33 .08 10 10 | 2 570 14 197
grg 168| 0 -3 -7 -25 21 -32 .26 15 14 | -416 893 16 164
igr n/a| 0 0 3 -17 0 -7 -.17 5 5 | 898 -268 16 90
jpl 80| -3 1 5 21 64 -10 .17 12 12 | 4058 -244 17 107
mit 349| 0 0 0 37 -10 -1 -.10 11 10 | -485 461 22 180
ngs 226| 0 0 -1 0 2 -15 -.01 8 7 | -1127 -84 1590 3119
sio 321| 0 0 0 34 -18 16 -.16 12 11 | --- --- --- ---
Table 2.1822.4 GPS week: 1822 Day: 4 MJD: 57002.000
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 1 -14 5 7 -.03 14 13 | -27 -1411 18 136
emr 80| -1 -3 1 -21 -4 -12 .15 12 12 | 4181 -355 15 146
esa 150| 1 0 8 -33 -8 -5 -.37 13 14 | -1073 327 11 236
gfz 199| 0 1 -6 -36 -16 47 .06 11 9 | 439 -488 12 186
grg 168| 0 0 -2 -3 6 -35 .25 14 15 | 560 -603 17 171
igr n/a| 0 0 3 -9 -14 -4 -.16 6 6 | 1128 -364 19 89
jpl 80| 0 0 3 23 27 -6 .18 11 11 | 4267 -325 17 118
mit 349| 0 0 0 4 20 2 -.11 12 10 | 192 -484 23 174
ngs 229| 0 0 -4 5 -33 -11 -.03 9 8 | -8 -1407 1419 3263
sio 322| 0 0 2 37 29 12 -.22 12 12 | --- --- --- ---
Table 2.1822.5 GPS week: 1822 Day: 5 MJD: 57003.000
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 252| 0 1 4 0 12 13 -.02 9 9 | -781 -239 16 124
emr 80| 0 -2 0 -15 -8 -3 .23 13 13 | 3707 852 13 156
esa 150| 1 0 7 -6 -25 9 -.35 13 13 | -2105 1850 11 253
gfz 199| 1 1 -4 -23 -19 29 .08 10 9 | -549 42 13 189
grg 168| -1 -2 0 -20 11 -34 .37 17 15 | -269 224 17 184
igr n/a| 0 0 3 -7 -13 0 -.18 5 5 | 504 664 16 98
jpl 80| 0 -2 2 -1 1 -23 .16 12 12 | 3737 857 19 122
mit 350| 0 0 0 30 -17 5 -.08 11 11 | -291 -64 25 184
ngs 227| -1 0 -5 -19 30 -4 -.05 9 8 | -878 46 1217 2929
sio 326| -1 0 0 43 -3 -8 -.21 12 11 | --- --- --- ---
Table 2.1822.6 GPS week: 1822 Day: 6 MJD: 57004.000
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 0 2 27 14 42 .04 15 14 | -306 -1037 18 115
emr 80| -1 -2 -2 -24 -3 5 .26 13 13 | 4672 842 13 139
esa 150| 0 0 8 10 -12 -1 -.37 13 13 | -1740 1554 10 138
gfz 198| 1 0 -6 2 -45 40 .08 12 11 | -46 278 13 187
grg 167| 0 -1 -5 -6 21 -44 .33 17 15 | 413 -442 15 165
igr n/a| 0 1 2 3 9 -15 -.18 6 6 | 1234 699 15 93
jpl 80| 0 0 0 -25 88 -1 .20 12 12 | 4733 835 15 107
mit 350| 0 0 0 -39 -20 -6 -.09 12 12 | -97 -472 30 210
ngs 225| 0 1 0 6 -10 -20 -.05 9 8 | -331 -915 1139 3107
sio 330| -1 -2 0 31 -17 -6 -.21 11 11 | --- --- --- ---
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 3.1822.0 GPS week: 1822 Day: 0 MJD: 56998.000
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 | 9 11 13 12 13 5 9 9 6 9 3 | 27 34 28 32 38 28 33 35 31 33 30
2 | 11 12 15 15 15 4 12 22 11 16 5 | 25 30 25 41 35 26 29 33 32 32 29
X3 | 14 16 --- 11 --- 43 --- 17 23 --- 8 | 125 131 --- 127 --- 136 --- 122 132 --- 127
4 | 9 10 12 17 11 5 8 11 8 10 3 | 31 37 32 35 38 31 36 35 35 33 33
5 | 11 16 16 11 13 5 13 17 11 13 4 | 39 43 41 34 36 36 43 39 33 38 36
6 | 8 11 14 8 13 3 8 9 9 9 3 | 27 35 25 33 38 27 33 30 33 29 29
7 | 8 15 11 10 19 4 9 18 7 10 4 | 25 31 21 27 32 22 29 17 28 25 24
X8 | 15 15 12 12 --- 5 10 9 18 --- 5 | 24 25 21 20 --- 18 23 20 24 --- 20
9E | 7 13 12 8 15 4 8 8 9 12 3 | 108 111 110 111 111 107 110 110 109 115 110
10 | 8 9 11 17 15 4 8 11 9 12 4 | 173 171 170 171 177 171 173 175 176 154 173
11 | 8 13 17 11 18 5 9 10 10 9 4 | 47 55 45 51 60 48 53 54 50 54 50
12 | 12 18 14 13 21 4 13 17 11 16 5 | 19 25 16 28 29 16 24 22 23 20 19
13E | 7 10 8 11 12 4 9 7 10 7 3 | 23 27 17 27 29 20 27 20 25 23 23
14E | 8 9 7 9 12 6 9 16 6 12 3 | 30 30 27 33 30 28 29 32 31 25 28
15E | 12 18 7 16 20 6 18 13 9 14 5 | 26 32 22 25 25 27 29 25 23 23 28
16 | 8 16 12 12 20 6 15 13 12 18 5 | 21 27 17 25 25 18 25 22 20 21 18
17 | 9 15 10 8 16 4 12 10 7 11 4 | 43 46 37 48 51 42 45 44 45 47 44
18 | 11 10 17 20 15 7 11 15 10 14 5 | 30 35 27 49 39 29 33 36 34 30 33
19 | 8 16 8 10 19 6 15 12 9 12 4 | 23 34 22 24 28 21 31 23 26 22 23
20 | 10 11 14 11 10 4 11 14 9 15 4 | 30 35 29 35 36 30 34 37 35 33 32
21 | 9 10 16 9 15 5 9 15 8 14 4 | 27 31 28 35 40 27 32 33 33 30 30
22 | 11 10 14 9 14 5 9 16 13 11 4 | 40 44 38 47 50 38 44 48 43 41 42
23E | 8 19 8 12 15 5 12 14 9 10 4 | 24 30 24 23 25 22 26 24 25 24 23
24 | 10 16 16 9 17 4 10 18 9 14 4 | 31 34 36 31 30 27 32 30 30 29 30
25 | 11 12 17 9 19 5 11 12 11 11 4 | 19 24 27 22 24 18 22 17 21 18 19
26E | 9 19 11 15 19 9 18 17 12 10 5 | 110 118 113 115 114 110 117 107 112 111 112
27 | 11 21 13 12 17 6 11 19 10 9 5 | 32 34 35 32 33 32 36 33 33 33 31
28 | 9 15 9 9 21 3 11 15 8 13 4 | 21 26 16 22 33 17 26 21 20 17 19
29E | 11 17 11 11 14 5 16 11 13 16 4 | 37 36 29 40 37 33 34 37 40 30 34
30 | 6 12 13 10 15 3 9 11 7 9 3 | 34 35 37 34 37 33 37 33 36 40 35
31 | 7 13 13 13 21 6 12 12 7 12 4 | 25 32 20 30 38 23 30 26 27 24 25
32 | 10 7 11 8 16 5 8 11 9 14 3 | 18 26 23 29 33 21 25 30 27 25 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 13 12 16 5 11 14 10 12 |T 41 45 37 44 45 40 41 42 43 39 41
WRMS | 10 14 13 11 16 5 11 12 9 12 |NE 38 43 33 42 42 37 38 40 41 35 39
MEDI | 9 13 12 11 15 5 11 13 9 12 |MD 27 34 27 33 36 27 32 33 32 30 30
Table 3.1822.1 GPS week: 1822 Day: 1 MJD: 56999.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 10 12 8 15 5 7 9 6 10 3 | 19 27 21 24 29 21 27 22 22 21 21
2 | 10 11 16 16 13 5 10 22 7 17 4 | 19 24 21 36 19 19 24 24 22 25 22
X3 | 16 14 86 12 --- 12 26 14 16 --- 7 | 89 87 136 77 --- 86 116 81 91 --- 85
4 | 11 10 11 13 11 10 9 10 6 10 3 | 21 29 25 27 29 21 32 27 26 23 25
5 | 8 15 15 10 11 4 13 12 7 16 4 | 22 28 27 23 24 21 28 21 22 20 21
6 | 8 7 14 8 10 5 9 7 5 9 3 | 21 27 21 30 27 21 28 21 23 21 22
7 | 10 13 14 11 17 3 10 16 9 9 4 | 24 29 21 26 29 21 26 16 27 20 22
X8 | 12 13 17 9 --- 6 8 15 11 --- 5 | 27 26 26 24 --- 21 23 18 24 --- 21
9E | 9 8 12 9 18 5 8 7 7 12 3 | 66 64 65 63 61 64 63 64 66 66 64
10 | 10 10 14 14 44 6 15 11 6 14 5 | 307 307 311 314 296 309 308 310 312 325 308
11 | 9 12 18 9 20 5 8 9 7 9 4 | 31 44 32 37 48 34 41 37 35 35 36
12 | 12 16 13 12 13 4 15 16 8 16 4 | 20 27 19 27 28 19 27 22 24 16 20
13E | 8 10 9 8 14 4 9 8 9 8 3 | 22 26 16 23 28 18 24 20 23 23 21
14E | 7 10 6 5 14 4 8 13 6 8 3 | 18 21 19 22 25 17 20 17 19 17 17
15E | 11 19 10 12 13 6 19 19 11 14 5 | 23 31 22 24 29 24 29 23 23 23 24
16 | 9 13 10 12 14 6 12 15 8 16 4 | 20 23 17 25 24 17 24 20 23 15 19
17 | 7 14 9 8 17 4 12 8 6 9 3 | 41 44 34 44 50 40 45 41 41 44 41
18 | 8 10 14 17 10 4 13 12 8 15 4 | 20 26 24 37 24 21 24 25 25 21 23
19 | 8 12 11 10 19 5 13 10 9 15 4 | 23 32 23 29 31 21 28 25 27 29 25
20 | 9 10 15 11 11 4 10 11 7 16 4 | 23 29 27 26 26 25 30 28 28 26 25
21 | 9 11 16 9 8 4 16 16 8 13 4 | 21 24 23 25 25 17 27 24 20 18 20
22 | 8 9 14 7 11 5 8 12 7 13 3 | 25 30 28 32 31 25 30 31 29 26 27
23E | 8 15 9 11 15 5 12 12 9 14 4 | 19 25 21 26 23 18 27 17 22 22 19
24 | 8 10 16 6 10 6 12 16 9 15 4 | 24 27 30 25 25 24 26 22 25 21 23
25 | 9 10 16 7 12 4 10 11 5 10 3 | 20 26 28 25 25 21 27 20 23 21 22
26E | 17 22 12 12 17 6 17 11 8 11 5 | 80 93 85 83 83 84 90 82 82 81 83
27 | 16 12 16 10 21 9 10 21 8 16 5 | 56 58 57 57 52 54 55 56 55 63 55
28 | 10 16 11 9 16 5 11 13 7 11 4 | 23 28 18 24 32 20 26 21 22 20 21
29E | 10 16 8 9 12 3 14 12 8 14 4 | 29 33 26 34 36 27 33 30 29 27 28
30 | 8 9 12 9 12 3 7 7 5 8 3 | 25 29 30 27 31 24 29 25 26 28 26
31 | 7 13 11 9 16 5 12 12 11 10 4 | 25 30 22 28 36 22 30 24 29 22 25
32 | 10 9 11 9 14 4 7 14 5 13 3 | 17 24 21 21 21 19 21 24 22 19 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 12 13 10 16 5 12 13 8 13 |T 38 43 40 42 41 37 43 38 40 37 38
WRMS | 9 12 13 10 12 5 12 12 7 11 |NE 37 42 41 42 40 36 43 38 40 36 38
MEDI | 9 11 12 9 14 5 10 12 7 13 |MD 23 28 24 27 29 21 28 24 25 22 23
Table 3.1822.2 GPS week: 1822 Day: 2 MJD: 57000.000
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 10 13 11 14 5 7 8 5 10 3 | 22 27 23 25 30 23 29 24 24 24 23
2 | 9 10 17 14 14 7 12 21 9 14 4 | 23 26 25 33 30 24 28 27 27 27 25
X3 | 21 17 36 13 --- 14 16 20 33 --- 9 | 102 105 75 97 --- 103 80 94 104 --- 100
4 | 6 9 12 12 11 4 7 11 5 15 3 | 26 30 25 28 33 24 32 30 27 28 27
5 | 13 15 16 10 13 5 13 11 9 15 4 | 30 32 32 26 25 27 34 27 23 29 26
6 | 11 11 13 8 13 4 9 9 6 13 3 | 22 32 21 26 31 21 30 24 23 24 23
7 | 9 15 11 12 17 4 10 14 9 11 4 | 24 27 18 21 27 18 25 14 25 18 19
X8 | 12 18 16 12 --- 12 14 9 10 --- 5 | 23 21 26 20 --- 22 27 18 19 --- 19
9E | 8 9 13 8 12 4 8 5 5 12 3 | 69 70 72 71 66 70 72 69 70 71 70
X10 | 8 9 12 10 13 7 9 10 8 --- 3 | 217 213 212 219 215 214 215 219 217 --- 216
11 | 9 10 19 12 18 5 8 8 7 10 4 | 39 45 37 45 51 38 45 41 39 40 41
12 | 13 17 13 13 18 4 16 13 9 16 5 | 17 26 19 28 28 17 28 22 20 22 20
13E | 7 12 9 10 11 4 10 5 8 7 3 | 25 26 18 24 26 20 26 20 23 22 22
14E | 8 10 9 7 11 4 10 15 10 6 3 | 17 19 16 18 19 14 20 21 18 19 16
15 | 10 20 9 12 23 6 16 14 8 13 5 | 46 41 38 38 43 44 39 35 37 35 45
16 | 15 15 10 13 15 7 12 13 12 15 4 | 23 22 16 25 22 16 23 21 20 22 18
17 | 9 14 8 9 18 4 15 8 6 9 3 | 37 43 34 40 49 37 43 42 43 41 40
18 | 9 10 18 21 12 6 9 8 10 16 4 | 20 26 21 43 28 21 27 26 23 26 24
19 | 9 17 9 11 18 5 11 10 8 13 4 | 25 28 19 25 28 19 27 25 23 25 22
20 | 15 9 15 14 9 5 9 10 13 15 4 | 30 31 27 30 33 28 33 30 32 28 28
21 | 9 11 18 8 11 5 10 15 7 14 4 | 22 24 20 25 29 18 24 25 19 22 20
22 | 8 9 18 12 11 6 7 13 8 15 4 | 29 29 27 35 36 28 31 34 26 31 29
23E | 8 14 7 13 15 4 13 12 8 13 4 | 27 29 26 28 30 26 32 25 26 28 25
24 | 9 9 15 10 12 8 10 12 9 15 4 | 25 27 29 27 25 22 27 21 23 22 23
25 | 5 12 16 8 12 5 10 7 9 12 3 | 19 24 27 22 23 18 25 20 20 27 21
26E | 18 18 12 10 18 5 17 11 10 11 5 | 69 73 64 61 60 62 72 62 65 64 65
27E | 17 13 16 17 15 5 12 9 8 11 4 | 31 28 32 29 24 24 29 25 24 28 25
28 | 9 15 10 9 17 6 14 11 7 13 4 | 26 28 19 23 30 21 31 22 22 20 22
29 | 13 19 13 10 14 6 16 11 9 13 4 | 28 32 26 33 31 25 30 29 27 25 26
30 | 7 9 13 9 13 2 8 5 5 9 3 | 28 28 30 27 30 25 31 25 28 27 27
31 | 7 16 15 12 15 4 10 10 11 10 4 | 23 28 17 26 34 19 26 23 25 21 22
32 | 12 8 12 13 11 5 8 12 8 12 3 | 17 22 19 26 26 18 26 26 23 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 13 13 12 15 5 11 11 8 13 |T 36 39 34 38 38 34 39 36 36 28 35
WRMS | 10 13 14 11 13 5 11 10 8 12 |NE 36 39 34 39 38 34 39 36 36 25 35
MEDI | 9 12 13 11 13 5 10 11 8 13 |MD 25 28 26 27 30 23 29 25 24 26 24
Table 3.1822.3 GPS week: 1822 Day: 3 MJD: 57001.000
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 10 16 11 16 4 9 6 6 12 3 | 23 28 24 31 31 24 28 26 27 27 25
2 | 8 13 16 11 13 7 13 21 9 15 4 | 26 28 26 34 30 22 27 30 27 29 26
X3 | 8 12 15 9 --- 15 13 16 6 --- 4 | 110 112 89 102 --- 114 96 102 104 --- 106
4 | 8 9 12 11 14 5 9 10 9 10 3 | 27 31 28 30 32 26 29 31 29 26 28
5 | 10 17 15 9 12 7 16 10 8 14 4 | 33 38 36 29 32 31 39 32 33 33 32
6 | 7 9 13 10 13 5 9 5 5 9 3 | 25 31 26 28 32 23 29 27 26 24 25
7 | 8 13 12 12 17 5 10 15 8 10 4 | 24 27 22 26 27 20 24 17 26 20 21
X8 | 23 12 12 13 --- 10 15 9 10 --- 6 | 34 20 22 16 --- 21 20 17 21 --- 19
9E | 8 9 14 11 14 5 7 7 6 12 3 | 105 106 108 109 107 106 105 107 104 109 106
10 | 7 8 12 9 12 6 10 10 6 13 3 | 189 192 192 197 194 191 191 197 190 174 192
11 | 8 15 18 9 20 4 10 8 9 9 4 | 40 47 38 43 51 37 43 41 40 39 41
12 | 10 20 13 11 16 6 18 14 8 17 5 | 16 26 17 23 29 17 26 23 20 22 19
13E | 9 11 8 7 12 5 10 6 8 10 3 | 21 25 16 20 24 15 20 19 20 18 18
14E | 9 11 6 7 12 5 10 11 6 12 3 | 14 19 14 17 20 12 16 19 18 15 14
15 | 9 18 9 10 17 5 22 12 7 16 4 | 24 35 30 32 34 21 34 30 30 31 23
16 | 13 16 14 15 17 5 14 11 9 16 4 | 24 24 19 26 24 17 22 19 21 15 18
17 | 6 12 8 9 20 5 14 9 7 8 3 | 64 68 63 69 70 64 67 68 66 69 66
18 | 10 12 16 15 13 5 12 8 9 13 4 | 31 31 28 39 34 24 28 29 31 28 29
19 | 7 17 10 10 16 5 12 8 9 8 3 | 24 29 22 27 31 22 30 23 28 23 24
20 | 11 10 15 11 12 5 9 13 9 16 4 | 29 31 27 36 34 28 29 31 34 31 30
21 | 9 12 18 8 12 6 13 14 6 15 4 | 24 26 24 26 31 19 26 26 24 24 23
22 | 10 9 14 7 14 5 7 10 5 12 3 | 36 37 36 40 44 31 35 41 36 35 36
23E | 11 19 8 15 17 4 13 11 9 10 4 | 29 32 26 29 32 27 30 25 29 27 26
24 | 8 10 14 5 12 6 16 20 9 14 4 | 33 37 40 34 37 32 33 35 32 32 33
25 | 8 11 17 8 13 4 10 10 7 10 3 | 16 24 27 16 25 17 21 20 23 21 19
26E | 18 21 10 13 15 8 17 11 9 15 5 | 79 88 79 85 79 81 86 78 76 77 80
27E | 10 12 18 10 17 6 12 5 5 7 3 | 27 25 29 26 24 24 29 22 24 22 24
28 | 7 15 13 9 18 5 12 11 8 14 4 | 22 27 15 22 31 17 24 21 22 15 19
29 | 8 18 9 8 18 4 16 12 7 11 4 | 43 45 41 46 50 41 44 44 42 41 42
30 | 6 8 13 8 12 5 10 5 4 8 3 | 32 32 37 32 33 30 31 29 32 34 32
31 | 7 16 16 17 18 5 10 11 9 14 4 | 24 31 22 29 36 21 28 24 25 22 24
32 | 8 10 13 8 12 5 8 15 5 14 3 | 21 24 21 28 32 20 22 26 24 21 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 14 13 10 15 5 12 11 8 12 |T 39 43 38 42 43 37 41 39 40 36 38
WRMS | 9 14 14 10 14 5 12 10 7 11 |NE 37 40 36 39 40 34 38 37 38 33 36
MEDI | 8 12 13 10 14 5 12 10 8 12 |MD 27 31 27 29 32 24 29 27 28 27 25
Table 3.1822.4 GPS week: 1822 Day: 4 MJD: 57002.000
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 9 14 9 13 5 8 11 7 9 3 | 26 27 22 25 30 22 28 24 26 23 24
2 | 14 11 16 14 13 7 11 22 8 14 5 | 24 26 22 31 24 19 24 23 25 20 22
X3 | 13 10 12 12 --- 10 14 13 12 --- 5 | 98 97 83 92 --- 94 91 89 92 --- 93
4 | 10 6 11 9 14 4 7 10 8 14 3 | 25 28 25 26 36 25 29 30 27 28 27
5 | 14 12 15 9 10 7 14 11 8 18 4 | 25 33 33 26 26 28 34 29 28 33 28
6 | 7 11 14 6 12 6 8 8 9 9 3 | 24 31 21 24 30 20 27 23 25 21 23
7 | 14 13 11 10 15 5 12 15 10 9 4 | 25 26 19 25 26 19 23 18 26 18 20
X8 | 26 18 12 14 --- 10 9 10 16 --- 6 | 32 32 18 22 --- 17 19 17 20 --- 19
9 | 18 13 12 10 16 11 9 22 13 20 5 | 160 150 149 151 149 147 151 149 153 152 151
10 | 14 8 11 8 13 5 9 9 8 12 3 | 141 140 139 145 140 139 140 144 142 126 140
11 | 11 9 19 10 20 5 11 11 10 11 4 | 38 43 34 42 51 36 43 40 37 38 39
12 | 10 18 14 9 15 7 15 12 10 15 4 | 18 26 16 25 28 17 24 21 22 17 19
13E | 12 9 8 8 12 4 9 7 7 8 3 | 19 22 15 20 25 16 22 18 22 18 18
14E | 10 11 9 10 11 5 10 11 8 7 3 | 19 17 14 18 21 13 15 15 17 12 14
X15 | 1 --- --- --- --- 26 --- --- --- --- 0 | 32 --- --- --- --- 25 --- --- --- --- 34
16 | 20 14 13 14 16 5 14 13 13 17 5 | 23 22 13 23 22 14 21 17 19 13 15
17E | 20 14 8 8 21 11 14 8 7 8 4 | 107 103 100 104 100 94 102 100 100 100 101
18 | 16 11 15 26 11 5 12 13 12 12 5 | 22 28 22 47 27 22 28 27 23 19 25
19 | 11 20 10 10 18 3 14 10 10 10 4 | 24 30 21 27 29 21 27 23 25 22 23
20 | 15 9 14 12 10 7 11 11 9 15 4 | 28 28 25 28 28 26 29 29 30 27 27
21 | 12 10 18 10 11 6 10 13 9 13 4 | 16 25 22 26 26 17 24 23 21 18 20
22 | 12 9 15 10 10 5 10 12 9 13 4 | 28 32 28 33 35 28 35 34 29 30 30
23E | 14 12 8 12 15 6 12 12 8 9 4 | 62 62 62 61 64 59 61 62 61 61 61
24 | 11 9 15 8 9 6 10 9 8 14 3 | 26 25 28 26 26 23 26 22 24 20 23
25 | 14 11 17 6 11 5 10 9 10 10 4 | 22 24 25 20 22 17 20 17 19 16 18
26E | 21 19 12 9 11 7 19 12 12 11 5 | 52 60 52 50 53 50 56 50 46 50 50
27E | 16 9 17 9 12 4 10 10 8 11 4 | 19 23 25 23 23 21 20 18 18 18 19
28 | 10 12 9 11 16 4 13 11 7 16 4 | 22 25 16 24 31 18 26 19 20 17 20
29 | 16 16 10 11 24 8 14 12 14 10 5 | 57 49 48 52 47 47 51 53 51 50 50
30 | 12 8 13 8 11 2 11 6 4 5 3 | 28 24 28 27 29 23 25 23 27 25 25
31 | 12 14 14 12 17 6 11 13 10 11 4 | 25 29 18 25 34 20 24 21 23 13 21
32 | 16 8 13 10 15 4 8 17 6 10 4 | 11 24 19 23 29 18 22 27 21 18 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 12 13 11 14 6 11 12 9 12 |T 39 42 37 41 41 36 40 38 39 35 38
WRMS | 13 12 14 9 15 6 11 10 8 12 |NE 32 35 30 35 34 29 34 32 32 26 31
MEDI | 13 11 13 10 13 5 11 11 9 11 |MD 25 28 25 26 29 22 27 23 25 21 23
Table 3.1822.5 GPS week: 1822 Day: 5 MJD: 57003.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 11 14 10 21 4 8 8 7 10 3 | 19 27 19 22 30 17 28 19 22 22 21
2 | 10 11 17 12 13 6 12 21 9 16 5 | 14 24 20 26 20 17 24 19 19 22 18
X3 | 12 13 13 9 --- 8 14 16 10 --- 5 | 90 92 63 87 --- 89 84 81 88 --- 88
4 | 7 11 11 10 24 6 9 11 7 12 4 | 20 23 19 21 31 17 25 20 22 18 19
5 | 7 14 15 10 12 6 15 11 8 13 4 | 31 35 30 28 29 26 36 28 27 31 28
6 | 8 10 14 7 13 4 9 6 10 12 3 | 22 30 19 25 32 20 31 25 24 23 23
7 | 7 15 11 12 14 4 10 17 10 11 4 | 26 29 21 27 26 20 28 17 26 20 22
X8 | 11 17 13 11 --- 10 16 9 10 --- 5 | 25 32 23 22 --- 19 31 21 20 --- 21
9 | 7 10 10 10 22 6 9 7 10 15 4 | 85 84 82 83 85 80 84 81 80 83 82
10 | 8 10 12 8 20 5 8 10 7 12 3 | 135 137 134 138 137 136 136 140 137 119 136
11 | 9 14 18 8 22 6 11 9 7 9 4 | 32 42 29 35 45 29 38 33 33 34 33
12 | 12 17 13 11 13 6 15 12 11 17 4 | 18 28 18 26 28 16 26 22 22 23 20
13E | 7 10 9 10 13 6 10 7 11 6 3 | 22 25 17 24 29 18 25 21 23 21 21
14E | 8 12 7 8 19 5 11 7 10 8 3 | 15 20 15 21 23 13 18 18 25 17 17
X15 | 10 16 8 11 20 6 16 10 --- --- 5 | 14 19 9 13 11 11 18 10 --- --- 14
16 | 10 13 13 11 15 4 12 11 10 13 4 | 21 25 14 23 22 14 23 17 19 14 16
17E | 9 14 7 8 20 4 13 10 9 9 4 | 50 52 47 53 54 50 51 51 51 54 50
18 | 9 12 15 19 12 4 11 8 8 12 4 | 25 27 24 43 28 23 27 26 24 23 26
19 | 6 19 7 10 25 5 13 7 7 12 4 | 35 40 31 36 45 32 39 32 35 32 34
20 | 9 10 14 9 11 5 11 14 9 16 4 | 25 28 22 20 26 20 30 24 24 29 23
21 | 9 10 17 9 11 5 10 14 8 13 4 | 18 23 21 23 24 16 24 20 19 18 18
22 | 8 9 14 9 10 5 11 10 7 10 3 | 26 33 29 33 33 25 33 33 32 32 30
23 | 6 23 6 10 22 5 15 10 10 11 4 | 47 53 49 49 52 47 51 49 46 48 47
24 | 9 15 14 6 14 5 11 14 12 17 4 | 25 29 29 27 25 21 26 20 26 25 23
25 | 10 8 17 7 12 4 11 10 9 9 3 | 22 27 28 23 26 20 24 21 22 21 22
26E | 15 21 11 11 14 8 18 12 11 16 5 | 72 79 73 72 74 73 77 73 75 73 73
27E | 8 9 14 10 15 4 9 7 6 10 3 | 21 22 23 23 23 18 22 17 23 19 19
28 | 10 14 11 12 15 5 14 12 8 17 4 | 26 29 19 26 30 18 29 22 19 15 21
29E | 9 11 9 9 22 6 12 10 10 8 3 | 31 33 26 34 32 29 30 31 35 28 30
30 | 7 11 13 9 13 3 9 6 5 7 3 | 28 28 31 29 27 25 31 26 27 28 27
31 | 10 16 14 14 15 5 13 14 8 9 4 | 26 32 19 29 35 22 28 26 26 21 24
32 | 9 9 11 6 21 5 8 15 6 10 3 | 21 25 19 20 32 16 25 25 23 19 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 9 13 13 10 17 5 12 11 9 12 |T 33 38 31 36 37 31 37 33 35 32 33
WRMS | 9 13 13 9 15 5 12 11 8 11 |NE 31 36 29 34 34 28 35 31 32 28 31
MEDI | 9 12 13 10 15 5 11 10 9 12 |MD 25 29 23 26 29 20 28 24 25 23 23
Table 3.1822.6 GPS week: 1822 Day: 6 MJD: 57004.000
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 | 15 8 14 11 18 4 9 12 7 11 4 | 27 29 25 29 35 25 31 28 26 28 26
2 | 22 11 16 15 12 8 13 22 8 15 5 | 30 31 28 39 34 30 30 32 30 35 30
X3 | 15 9 15 12 --- 6 13 11 6 7 4 | 127 129 105 124 --- 122 114 120 120 6 124
4 | 17 10 11 12 23 4 7 13 8 9 4 | 25 30 23 28 37 23 27 30 29 28 26
5 | 15 13 15 13 14 6 15 11 9 15 4 | 38 43 43 35 37 37 45 39 35 42 38
6 | 17 9 14 8 16 5 9 8 5 10 3 | 27 34 25 30 35 26 32 28 27 28 27
7 | 11 13 10 14 15 4 12 14 9 10 4 | 26 28 22 23 25 19 28 15 21 17 19
X8 | 23 14 15 11 --- 10 15 12 26 --- 7 | 32 23 22 19 --- 16 26 18 24 --- 18
9 | 13 13 11 10 19 4 9 9 12 13 4 | 152 148 149 150 149 148 150 147 154 152 150
10 | 15 6 13 9 20 5 8 10 7 8 3 | 142 140 138 143 144 138 139 143 138 131 140
11 | 15 12 18 10 24 5 10 12 9 14 4 | 43 52 39 49 60 43 49 49 46 48 46
12 | 18 15 13 13 14 7 14 12 9 14 4 | 22 24 18 27 28 18 25 23 22 20 19
13E | 10 11 10 10 19 6 9 7 7 7 3 | 26 27 17 22 27 16 24 19 22 22 21
14E | 11 12 8 9 21 7 10 13 7 7 3 | 18 20 18 21 24 16 20 19 20 16 17
15 | 11 15 10 13 20 6 17 9 12 12 4 | 14 19 9 13 12 12 21 9 6 7 11
16 | 16 15 11 12 16 5 12 11 16 13 4 | 24 26 17 24 25 16 25 18 23 17 18
17E | 13 14 9 8 24 6 14 12 13 10 4 | 38 38 33 38 36 33 38 39 41 41 37
18 | 10 10 14 26 14 7 10 10 13 13 5 | 31 34 28 53 38 29 33 33 30 28 32
19 | 23 17 10 14 18 13 14 11 12 11 5 | 97 93 89 90 88 81 94 84 85 90 89
20 | 13 8 15 13 12 5 9 15 7 14 4 | 33 35 28 34 36 30 36 34 35 34 32
21 | 14 12 17 12 12 7 14 14 13 12 4 | 31 29 25 31 36 23 30 29 29 26 27
22 | 15 9 14 7 13 6 9 11 7 9 3 | 38 40 36 44 49 36 42 45 41 39 40
23 | 11 21 8 10 21 5 14 11 10 9 4 | 31 36 34 36 36 31 34 34 36 34 33
24 | 14 9 15 10 12 7 9 10 9 14 4 | 29 27 30 30 26 23 27 19 25 21 23
25 | 14 9 16 9 14 5 10 7 7 8 3 | 23 26 28 20 27 18 22 19 20 24 21
26E | 15 22 15 14 16 8 19 11 10 12 5 | 75 79 67 70 70 69 78 68 67 71 70
27E | 16 11 16 11 13 6 8 8 10 6 4 | 29 26 32 28 26 26 30 22 24 24 25
28 | 12 13 9 12 16 5 11 13 7 12 4 | 28 28 19 28 31 18 27 23 19 19 21
29E | 14 14 10 10 20 6 15 12 9 8 4 | 39 38 36 41 40 36 39 38 40 37 37
30 | 10 8 13 9 11 5 8 8 6 6 3 | 35 31 33 33 29 28 33 28 32 30 30
31 | 13 16 11 11 17 6 13 18 8 9 4 | 29 30 22 26 35 22 28 25 25 21 23
32 | 17 9 13 12 22 5 10 20 10 16 5 | 19 29 21 30 39 21 27 29 24 26 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 13 13 12 17 6 12 12 9 11 |T 43 44 39 44 43 38 43 40 41 37 40
WRMS | 14 13 13 11 15 6 12 12 8 11 |NE 41 43 37 43 42 36 42 39 39 34 38
MEDI | 14 12 13 11 16 6 10 11 9 11 |MD 30 30 28 30 35 26 30 29 29 28 27
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 4.1822 GPS week: 1822 MJD: 56998.0-57004.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 |U 5 6 15 |U 9 12 35 |U 7 7 16 |
emr | emr 3054 | 9 9 20 |U 10 11 33 | 8 9 23 |
esa | esa 3044 | 7 7 18 |U 10 11 38 | 8 8 23 |
gfz | gfz 3053 |U 6 6 19 |U 9 12 37 |U 8 8 19 |
grg | grg 2865 | 9 8 20 |U 11 12 35 |U 9 10 23 |
igr | igr 3008 | 6 7 16 | 9 11 35 | 7 7 18 |
igs | igs 3048 | 6 6 17 | 9 11 36 | 9 10 21 |
jpl | jpl 3039 | 7 7 21 |U 10 12 38 |U 8 9 23 |
mit | mit 3058 | 7 7 18 |U 11 14 43 |U 10 9 25 |
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 5.1822.0 GPS week: 1822 Day: 0 MJD: 56998.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 4 17 | 8 11 26 | 6 5 11 |
emr | emr 3067 | 8 6 16 | 10 13 28 | 9 7 18 |
esa | esa 2976 | 8 6 15 | 8 11 26 | 8 6 18 |
gfz | gfz 3068 | 6 6 18 | 8 12 26 | 6 6 14 |
grg | grg 2880 | 6 6 16 | 10 11 27 | 10 10 18 |
igr | igr 2976 | 6 5 13 | 7 11 26 | 6 5 12 |
igs | igs 3067 | 6 5 16 | 7 11 26 | 9 8 14 |
jpl | jpl 2972 | 7 6 17 | 8 11 25 | 7 6 18 |
mit | mit 3072 | 9 6 16 | 8 13 29 | 11 9 16 |
Table 5.1822.1 GPS week: 1822 Day: 1 MJD: 56999.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 4 5 12 | 8 7 30 | 8 8 16 |
emr | emr 3068 | 7 6 14 | 7 8 22 | 9 8 24 |
esa | esa 3072 | 5 5 12 | 9 8 30 | 9 9 23 |
gfz | gfz 3068 | 4 6 16 | 8 8 28 | 9 8 18 |
grg | grg 2880 | 11 11 32 | 9 8 28 | 11 10 22 |
igr | igr 3039 | 4 6 12 | 8 7 26 | 8 8 18 |
igs | igs 3070 | 5 5 12 | 7 7 27 | 10 9 18 |
jpl | jpl 3067 | 5 6 13 | 8 8 29 | 9 8 22 |
mit | mit 3072 | 6 6 13 | 10 9 42 | 10 7 25 |
Table 5.1822.2 GPS week: 1822 Day: 2 MJD: 57000.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 5 17 | 7 11 33 | 8 9 20 |
emr | emr 3068 | 9 8 22 | 7 9 24 | 10 10 24 |
esa | esa 3072 | 7 6 17 | 8 11 27 | 9 10 27 |
gfz | gfz 3066 | 6 7 16 | 8 10 34 | 10 10 22 |
grg | grg 2875 | 10 7 15 | 9 11 30 | 10 10 27 |
igr | igr 3066 | 6 6 15 | 7 10 31 | 9 9 22 |
igs | igs 3069 | 6 5 19 | 7 10 30 | 9 10 24 |
jpl | jpl 3067 | 7 7 24 | 8 12 30 | 8 9 25 |
mit | mit 3072 | 7 5 16 | 9 11 37 | 11 11 29 |
Table 5.1822.3 GPS week: 1822 Day: 3 MJD: 57001.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3068 | 6 9 17 | 7 9 30 | 6 6 16 |
emr | emr 3068 | 9 12 23 | 8 8 24 | 7 5 22 |
esa | esa 3072 | 7 9 19 | 8 8 31 | 7 4 21 |
gfz | gfz 3068 | 6 7 18 | 7 9 30 | 7 5 18 |
grg | grg 2880 | 9 14 23 | 11 9 29 | 9 7 19 |
igr | igr 2976 | 6 8 17 | 7 9 29 | 7 6 18 |
igs | igs 3071 | 7 11 19 | 7 8 28 | 9 8 19 |
jpl | jpl 3067 | 8 10 24 | 8 7 29 | 7 6 21 |
mit | mit 3072 | 7 10 19 | 7 8 31 | 8 6 17 |
Table 5.1822.4 GPS week: 1822 Day: 4 MJD: 57002.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 14 | 9 12 36 | 7 10 14 |
emr | emr 2972 | 11 8 25 | 10 12 32 | 9 17 28 |
esa | esa 2976 | 8 7 23 | 10 12 38 | 8 10 23 |
gfz | gfz 2972 | 8 5 23 | 10 13 41 | 7 8 16 |
grg | grg 2784 | 12 7 23 | 10 16 38 | 10 17 29 |
igr | igr 2976 | 7 7 19 | 10 12 38 | 7 9 15 |
igs | igs 2974 | 6 6 21 | 10 11 37 | 11 18 30 |
jpl | jpl 2971 | 8 7 25 | 10 13 41 | 12 18 27 |
mit | mit 2976 | 10 8 21 | 11 13 38 | 14 18 36 |
Table 5.1822.5 GPS week: 1822 Day: 5 MJD: 57003.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 5 4 12 | 16 20 53 | 6 7 18 |
emr | emr 3067 | 7 9 22 | 17 19 62 | 7 7 24 |
esa | esa 3072 | 7 6 21 | 18 17 70 | 8 8 25 |
gfz | gfz 3068 | 8 4 24 | 16 20 57 | 7 10 19 |
grg | grg 2880 | 9 6 17 | 16 19 53 | 9 6 19 |
igr | igr 3047 | 5 6 16 | 16 19 53 | 6 6 19 |
igs | igs 3025 | 5 5 16 | 16 19 63 | 7 7 19 |
jpl | jpl 3067 | 6 7 21 | 17 20 73 | 8 6 24 |
mit | mit 3072 | 6 6 19 | 15 19 59 | 9 8 22 |
Table 5.1822.6 GPS week: 1822 Day: 6 MJD: 57004.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 5 8 16 | 10 12 38 | 6 7 20 |
emr | emr 3068 | 8 12 19 | 10 11 39 | 7 8 24 |
esa | esa 3072 | 6 10 21 | 11 11 42 | 8 8 26 |
gfz | gfz 3066 | 7 8 22 | 10 13 39 | 7 8 25 |
grg | grg 2879 | 7 9 15 | 9 13 37 | 9 6 26 |
igr | igr 2976 | 6 10 19 | 10 12 41 | 6 8 21 |
igs | igs 3061 | 6 8 19 | 10 11 40 | 6 7 22 |
jpl | jpl 3067 | 6 9 23 | 10 12 42 | 9 8 26 |
mit | mit 3072 | 6 8 19 | 19 26 66 | 9 8 30 |
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 6.1822 GPS week: 1822 MJD: 56998.500-57004.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -7 0 -8 59 -3 | 5 16
| 13 20 115 125 5 | 2
emr uuuuu | -33 49 -200 -149 -9 | 41 45
| 18 24 146 71 13 | 3
esa uuuuu | 19 16 -7 95 -4 | 9 18
| 14 23 31 70 3 | 2
gfz uuuux | 8 9 118 -107 -2 | 24 28
| 24 18 116 89 4 | 2
grg uuuuu | 6 5 -85 6 5 | 12 20
| 14 14 125 128 10 | 1
igr xxxxx | 6 11 -13 39 4 | -4 15
| 26 14 66 49 4 | 1
irf xxxxx | 7 -4 14 11 -2 | 3 14
| 6 9 46 27 2 | 2
jpl uuuuu | -40 -4 -97 -14 -1 | 20 27
| 37 32 46 74 9 | 2
mit uuuuu | 8 -13 -20 43 0 | 20 24
| 16 12 99 50 4 | 2
ngs uuuuu | 34 -20 172 24 3 | 6 16
| 33 15 174 70 7 | 2
sio uuxxx | -15 -31 25 79 -7 | 37 41
| 17 18 64 49 7 | 3
Table 7.1822.0 GPS week: 1822 Day: 0 MJD: 56998.500
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 | 10 31 -56 109 -7 | 8 19
emr uuuuu | -49 68 -285 -89 -7 | 39 45
esa uuuuu | 5 -9 -22 64 -5 | 10 20
gfz uuuux | -2 17 -39 -238 2 | 25 30
grg uuuuu | 9 -15 -191 27 -9 | 14 22
igr xxxxx | -21 -6 8 40 3 | -5 17
irf xxxxx | 12 -12 -51 17 1 | 2 16
jpl uuuuu | 11 24 -60 -25 16 | 17 27
mit uuuuu | 33 -31 -153 76 6 | 17 23
ngs uuuuu | -13 -33 498 31 6 | 4 16
sio uuxxx | -4 -55 72 62 2 | 37 42
Table 7.1822.1 GPS week: 1822 Day: 1 MJD: 56999.500
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 | -12 24 -135 183 -10 | 7 18
emr uuuuu | -57 23 24 -165 -6 | 40 46
esa uuuuu | 8 15 -17 50 -1 | 9 19
gfz uuuux | 5 -4 37 -91 0 | 24 29
grg uuuuu | 15 15 -222 -130 -1 | 12 19
igr xxxxx | -5 12 -155 81 5 | -6 17
irf xxxxx | 1 -3 29 -8 -2 | 2 16
jpl uuuuu | -68 -13 -95 9 -6 | 18 29
mit uuuuu | -15 -17 69 9 -1 | 18 24
ngs uuuuu | 86 -4 173 23 11 | 3 16
sio uuxxx | -22 -40 -6 113 -6 | 38 43
Table 7.1822.2 GPS week: 1822 Day: 2 MJD: 57000.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 13 -11 -3 166 -2 | 7 18
emr uuuuu | -35 43 -147 -130 -16 | 44 48
esa uuuuu | 2 24 -45 33 -9 | 11 19
gfz uuuux | -23 -10 191 -219 2 | 26 30
grg uuuuu | 17 11 3 47 -2 | 12 19
igr xxxxx | -19 -8 -1 -52 2 | -4 16
irf xxxxx | 0 -2 64 -16 -1 | 4 16
jpl uuuuu | -32 -18 -167 -101 4 | 21 30
mit uuuuu | -3 -8 103 36 3 | 20 25
ngs uuuuu | 45 -3 26 88 10 | 6 17
sio uuxxx | -12 -14 111 93 -7 | 40 44
Table 7.1822.3 GPS week: 1822 Day: 3 MJD: 57001.500
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 6 -98 87 -2 | 8 18
emr uuuuu | -6 39 -102 -161 -8 | 46 48
esa uuuuu | 33 29 2 219 -6 | 11 19
gfz uuuux | 22 -4 298 -94 -1 | 27 31
grg uuuuu | -10 19 -166 -155 9 | 13 19
igr xxxxx | -7 6 40 37 13 | -2 14
irf xxxxx | 16 -4 66 -20 -1 | 5 15
jpl uuuuu | -72 -55 -29 -97 0 | 24 30
mit uuuuu | 18 -5 30 -51 2 | 22 25
ngs uuuuu | 12 -7 -9 111 0 | 9 16
sio uuxxx | 9 -2 81 -16 -8 | 41 45
Table 7.1822.4 GPS week: 1822 Day: 4 MJD: 57002.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -17 -18 173 -75 -8 | 5 18
emr uuuuu | -12 28 -161 -50 -34 | 43 47
esa uuuuu | 22 55 -34 47 -3 | 8 19
gfz uuuux | -1 43 192 -33 -4 | 25 29
grg uuuuu | 24 15 -97 64 20 | 11 18
igr xxxxx | 13 22 27 22 1 | -3 14
irf xxxxx | 7 3 15 16 -4 | 3 15
jpl uuuuu | -38 -20 -129 -43 -4 | 22 28
mit uuuuu | 11 -13 -36 58 -3 | 21 25
ngs uuuuu | 44 -39 54 32 -1 | 7 16
sio uuxxx | -43 -33 -4 71 -21 | 38 42
Table 7.1822.5 GPS week: 1822 Day: 5 MJD: 57003.500
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 -18 124 94 2 | 3 12
emr uuuuu | -34 53 -346 -270 4 | 38 40
esa uuuuu | 25 5 34 85 -1 | 6 14
gfz uuuux | 5 11 104 -76 -10 | 23 26
grg uuuuu | -3 2 -60 -33 5 | 12 21
igr xxxxx | 45 20 18 103 5 | -3 13
irf xxxxx | 4 9 -38 42 -5 | 2 11
jpl uuuuu | 3 16 -124 88 -9 | 20 24
mit uuuuu | 14 5 -144 72 -6 | 20 23
ngs uuuuu | 12 -23 201 -15 1 | 6 15
sio uuxxx | -11 -30 -65 141 -7 | 34 36
Table 7.1822.6 GPS week: 1822 Day: 6 MJD: 57004.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -18 -14 -61 -152 5 | 2 11
emr uuuuu | -34 92 -385 -181 1 | 38 39
esa uuuuu | 37 -10 32 163 -4 | 5 14
gfz uuuux | 54 10 44 0 -5 | 21 25
grg uuuuu | -11 -11 136 223 15 | 12 21
igr xxxxx | 34 28 -26 39 -1 | -3 13
irf xxxxx | 12 -18 10 47 -3 | 1 12
jpl uuuuu | -83 38 -76 70 -6 | 19 24
mit uuuuu | 1 -24 -12 97 -3 | 19 22
ngs uuuuu | 56 -30 260 -101 -8 | 7 15
sio uuxxx | -24 -44 -15 89 -6 | 34 36
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