[IGSREPORT-28568] Wk 2200 IGS Final Orbits
acc
acc at igs.org
Sun Mar 27 22:20:18 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2200 (Mar 06, 2022 - Mar 12, 2022)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs2200[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2200[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2200[0-6].cls IGS GPS clock combination summary report.
igs22007.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs22007.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 | OHI2 SALU UNSA YELL OHI2 UNSA
0 | EMR | NIST YELL
0 | ESA | CHUR MAYG YEL2 CZTG YEL2
0 | GFZ | SALU
0 | GRG | GAMB GRAC SVTL SYOG WIND GAMB GRAC SVTL WIND
0 | JPL | BADG BADG MAC1 YELL
1 | COD | KIT3
1 | ESA | CPVG
1 | GRG | 4 ASCG BRST CPVG FLIN INVK FLIN GRAC SCRZ
1 | JPL | BADG BADG
2 | COD | ABMF DGAR GRAC SGOC ABMF DGAR OHI2
2 | ESA | ASCG CPVG DAV1 MAYG
2 | GFZ | DAV1
2 | GRG | 21 21 ASCG CCJ2 CPVG DAV1 KRGG SVTL WIND TONG WIND
2 | JPL | BADG
3 | COD | DAV1 MAYG SALU DAV1 SALU
3 | EMR | MDVJ
3 | ESA | CPVG DAV1 WES2 DAV1
3 | GFZ | KIT3 KIT3 SAVO
3 | GRG | 13 CPVG KRGG NYA2 SGOC SVTL TLSE CPVG NYA2 SGOC SVTL
4 | COD | MAYG MCIL WTZR MCIL
4 | EMR | MDVJ
4 | ESA | CPVG SVTL YEL2 SVTL YEL2
4 | GFZ | IISC WTZR
4 | GRG | 13 GRAC SYOG GRAC YEL2
4 | JPL | DAEJ
5 | COD | BAKE KARR MAYG OHI2 KARR MAYG OHI2
5 | EMR | KIRU MAS1 YELL
5 | ESA | CHUR SAVO CHUR SAVO
5 | GFZ | 3 3 7 30 KIT3 KIT3
5 | GRG | 4 CZTG HYDE NICO STK2 SVTL STK2 SVTL WIND
5 | JPL | BAKE
6 | COD | ASCG MAYG NTUS PIMO SAMO SGOC
6 | EMR | MAS1 MDVJ
6 | ESA | TRO1 WES2 TRO1
6 | GFZ | HERS HERS PIMO
6 | GRG | CPVG DUBO CPVG DUBO
6 | JPL | GAMB GAMB
6 | MIT | NIST
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G02 | 2022_03_11 | 2022010
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.0 .0 .3 4 4 -9 -.07
EMR | 0 | -.1 4.6 .3 -26 -23 -8 .08
ESA | 0 | -.7 -1.1 -.0 11 9 14 -.18
GFZ | 0 | .2 -.5 -.1 5 -9 -4 -.16
GRG | 0 | 2.8 .4 -15.0 27 19 -6 -.09
JPL | 0 | 3.5 2.1 -1.0 11 19 -4 -.33
MIT | 0 | -1.3 -1.6 9.3 19 -2 8 .05
NGS | 0 | -1.3 3.5 7.4 13 34 10 -.05
SIO | 0 | .5 -6.2 12.5 -68 -6 1 -.25
COD | 1 | .1 -.1 .2 10 1 5 -.10
EMR | 1 | -.5 8.0 -8.9 -9 -18 -8 .06
ESA | 1 | -.6 -1.3 -.0 -4 12 19 -.30
GFZ | 1 | .1 -.5 .5 -2 -7 3 -.23
GRG | 1 | 2.0 .9 -13.8 7 13 -19 .05
JPL | 1 | 9.5 2.2 -.2 2 17 -11 -.27
MIT | 1 | -1.3 .6 7.8 1 19 -3 .07
NGS | 1 | -4.4 3.0 4.6 -17 45 26 .04
SIO | 1 | -2.9 -3.0 11.2 2 68 38 -.32
COD | 2 | .0 -.0 .1 1 3 -1 -.12
EMR | 2 | -3.0 .7 .8 -28 -33 -24 .32
ESA | 2 | -.1 -.8 -.5 -11 10 4 -.20
GFZ | 2 | .3 -.2 -.0 13 -6 8 -.16
GRG | 2 | -4.0 1.2 -8.5 11 -4 -20 .09
JPL | 2 | 6.4 -1.3 2.7 -12 21 -6 -.12
MIT | 2 | 1.0 -.3 10.1 11 9 -1 .0
NGS | 2 | -.8 1.3 -2.2 0 34 3 -.03
SIO | 2 | .9 -3.9 14.9 -19 -27 21 -.36
COD | 3 | .0 .1 .2 2 4 -7 -.17
EMR | 3 | -5.8 8.1 .9 -27 -27 -8 .17
ESA | 3 | -.5 -1.2 -.6 -6 26 16 -.15
GFZ | 3 | .0 -.4 -.1 11 -4 14 -.09
GRG | 3 | -1.5 1.2 -1.9 2 -3 -13 .16
JPL | 3 | 6.2 3.1 5.9 -11 21 5 -.19
MIT | 3 | 1.5 2.2 8.7 -6 15 -25 .05
NGS | 3 | .1 -.7 6.4 -19 15 17 .12
SIO | 3 | 4.3 .7 15.3 60 -89 50 -.26
COD | 4 | -.0 .0 .1 5 7 -4 -.12
EMR | 4 | 7.5 8.1 -5.3 -47 -16 -23 .04
ESA | 4 | -.2 -1.5 .0 -4 11 13 -.20
GFZ | 4 | .0 -.2 -.0 3 -1 8 -.16
GRG | 4 | 4.1 -.4 -2.9 10 -6 -15 .01
JPL | 4 | 2.5 2.2 5.0 -4 15 -3 -.11
MIT | 4 | 2.5 1.3 6.4 5 10 -32 .05
NGS | 4 | 1.6 2.2 6.3 7 11 5 .13
SIO | 4 | 3.3 -2.9 9.7 -13 -60 48 -.21
COD | 5 | -.1 -.0 .1 4 1 -3 -.10
EMR | 5 | 2.0 -.0 -7.2 -35 -38 -25 -.22
ESA | 5 | -.4 -1.1 -.1 -1 11 36 -.28
GFZ | 5 | .2 -.1 .1 7 -2 17 -.31
GRG | 5 | 5.7 -1.3 -5.8 -1 3 -31 -.03
JPL | 5 | 5.2 1.3 .7 0 27 -7 -.33
MIT | 5 | 2.9 1.2 7.1 9 15 -31 -.01
NGS | 5 | 3.4 1.3 -1.2 -6 5 -2 .09
SIO | 5 | 4.7 .3 11.1 55 -84 42 -.38
COD | 6 | -.1 .1 -.1 -2 3 -1 -.12
EMR | 6 | .9 10.5 -8.6 -36 -47 -43 .05
ESA | 6 | .1 -1.0 .3 -12 9 16 -.25
GFZ | 6 | .1 .0 -.0 0 -9 7 -.19
GRG | 6 | 2.3 -4.0 -.6 14 0 -17 -.04
JPL | 6 | 4.9 -1.9 -3.3 -4 22 0 -.08
MIT | 6 | .5 3.0 5.9 22 10 -8 .10
NGS | 6 | 4.0 3.0 .3 16 -4 14 .06
SIO | 6 | -.8 1.2 12.2 60 -21 51 -.22
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/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:
https://files.igs.org/pub/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.2200.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2200.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 2.2200.[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 3.2200.[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 5.2200.0-6). 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 2200 summary. (Mar 06, 2022 - Mar 12, 2022)
Table 1.2200.a GPS week: 2200 MJD: 59644.000-59650.000
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 675| 0 0 3 -14 10 10 -.01 8 7 | -679 314 6 96
| 0 0 0 18 12 23 .02 | 186 459
emr 80| -1 6 -1 -19 20 1 .13 13 13 | 202780 -186 12 111
| 1 1 1 9 13 20 .04 | 987 869
esa 150| 0 0 0 -24 17 1 .00 7 7 | -279 -145 7 95
| 0 0 0 10 12 11 .01 | 233 563
gfz 244| 0 0 0 -13 8 -15 .11 10 10 | -86 107 13 78
| 1 0 1 26 14 10 .05 | 305 455
grg 118| 1 -2 -7 -22 27 -14 -.11 11 10 | -83 151 8 141
| 0 0 5 5 14 16 .02 | 189 343
igr n/a| 0 0 0 -17 15 -7 .03 5 5 | 3111 -432 11 105
| 0 0 1 11 13 15 .01 | 2162 940
jpl 80| 0 0 1 -28 15 -4 .12 8 8 | 2947 -234 7 72
| 1 0 1 14 16 12 .01 | 4187 927
mit 358| 0 0 1 -26 30 -7 -.06 7 7 | 13661 -2739 22 1620
| 0 0 1 32 7 24 .01 | 9920 9074
ngs 203| 0 0 0 -2 29 -17 -.05 9 9 | -622 165 808 1598
| 0 0 1 14 18 13 .02 | 159 353
sio 416| 0 0 -1 153 -156 37 -.06 9 8 | --- --- --- ---
| 0 0 1 23 41 36 .02 | --- ---
Table 1.2200.b GPS week : 2200 MJD: 59644.000-59650.000
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 | 3 3 3 3 3 3 3 |
2 | 4 4 4 4 7 0 5 |
3 | 3 3 3 3 3 3 3 |
4 | 5 5 6 5 4 4 5 |
5 | 3 3 3 3 3 3 3 |
6 | 3 3 3 3 3 3 3 |
7 | 3 3 3 3 3 3 3 |
8 | 4 4 4 4 4 3 4 |
9 | 3 3 3 3 3 4 3 |
10 | 3 3 3 3 3 3 3 |
11 | 6 7 6 7 11 9 7 |
12 | 3 3 3 3 3 3 2 |
13 | 4 4 3 5 4 4 3 |
14 | 3 3 3 3 3 3 3 |
15 | 4 4 5 4 4 4 4 |
16 | 3 3 3 3 3 3 3 |
17 | 4 4 3 4 4 3 3 |
18 | 4 4 5 4 5 5 4 |
19 | 4 3 3 4 4 3 3 |
20 | 3 3 3 3 3 3 3 |
21 | 3 3 3 3 4 3 3 |
22 | 3 3 3 3 3 3 3 |
23 | 3 3 3 3 3 3 3 |
24 | 3 3 3 3 4 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 3 3 3 3 3 |
27 | 3 3 4 4 3 3 3 |
28 | 3 4 4 4 3 3 4 |
29 | 4 3 4 4 4 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 3 3 3 3 3 |
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 2.2200.0 GPS week: 2200 Day: 0 MJD: 59644.000
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 671| -1 0 5 -16 18 34 -.03 7 7 | -473 130 8 101
emr 80| -1 6 0 -23 11 -15 .20 13 13 | 203229 1449 11 111
esa 150| 0 0 0 -29 6 10 .00 7 7 | -683 744 8 94
gfz 239| -1 0 -1 -43 -16 -19 .16 10 10 | -369 857 13 68
grg 120| 1 -2 -11 -17 46 -4 -.11 9 9 | -380 760 8 138
igr n/a| 0 0 0 -30 4 0 .03 4 4 | 4810 1266 11 99
jpl 80| 1 0 0 -22 32 10 .12 8 8 | -855 1469 7 79
mit 358| 0 0 3 0 30 -2 -.08 8 7 | 17594 2789 22 1450
ngs 203| 0 0 0 1 19 -25 -.08 10 9 | -705 444 563 1294
sio 416| 0 0 0 173 -168 -13 -.06 9 9 | --- --- --- ---
Table 2.2200.1 GPS week: 2200 Day: 1 MJD: 59645.000
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 671| 0 -1 4 -13 -11 8 -.01 8 8 | -610 166 7 97
emr 80| -1 7 0 -11 33 -32 .10 13 13 | 204366 -352 13 114
esa 150| 0 0 0 -23 24 -2 .01 7 7 | -208 139 8 93
gfz 248| -2 -1 -1 -19 17 -24 .19 10 10 | 155 -59 13 78
grg 120| 1 -2 -14 -23 40 -43 -.13 11 9 | 97 216 10 152
igr n/a| -1 0 1 -6 13 -22 .04 4 4 | 5861 -457 11 98
jpl 80| 1 0 1 -12 13 -26 .13 8 8 | 814 -510 8 85
mit 358| 0 0 2 -62 27 25 -.08 7 7 | 19911 998 22 1645
ngs 202| 0 0 1 11 11 -11 -.03 9 9 | -380 -251 688 1565
sio 418| 0 0 1 167 -137 57 -.06 8 8 | --- --- --- ---
Table 2.2200.2 GPS week: 2200 Day: 2 MJD: 59646.000
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 672| 0 0 4 18 16 29 -.02 8 8 | -577 270 7 100
emr 80| -1 4 0 -33 16 7 .09 13 13 | 203428 -657 11 128
esa 150| -1 1 0 -42 7 5 .01 8 8 | -346 139 7 90
gfz 248| 0 -1 0 -29 20 -14 .06 10 10 | -227 156 11 69
grg 120| 1 -2 -10 -30 24 -14 -.07 10 10 | -1 104 9 129
igr n/a| 0 0 -1 -34 24 17 .04 5 4 | 4652 -1199 11 109
jpl 80| -1 1 2 -53 21 0 .11 9 9 | -490 -775 8 73
mit 358| 0 0 2 -11 27 -11 -.06 8 7 | 21523 572 23 1676
ngs 204| 1 0 -2 -15 51 8 -.04 9 8 | -649 386 674 1618
sio 414| 0 -1 0 168 -175 -11 -.04 8 8 | --- --- --- ---
Table 2.2200.3 GPS week: 2200 Day: 3 MJD: 59647.000
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 676| 0 0 3 -8 23 -27 .02 8 7 | -546 -64 6 95
emr 80| -2 5 0 -23 37 7 .15 13 13 | 202937 -1388 12 115
esa 150| 0 0 0 -15 27 -8 .00 8 8 | -196 -715 8 106
gfz 248| 0 -1 2 2 17 -15 .09 11 12 | -293 -81 14 91
grg 121| 0 -2 -5 -25 32 -23 -.14 11 10 | -63 -187 7 145
igr n/a| 0 0 -2 -5 35 -23 .03 5 5 | 3440 -1711 12 138
jpl 80| 1 2 2 -26 22 -3 .12 8 8 | -980 -1529 8 71
mit 358| 0 0 0 -65 38 6 -.07 8 7 | 21005 -1288 24 1532
ngs 205| 1 -1 0 -14 42 -25 -.04 10 9 | -449 -227 854 1828
sio 415| 0 0 -3 164 -208 57 -.04 8 8 | --- --- --- ---
Table 2.2200.4 GPS week: 2200 Day: 4 MJD: 59648.000
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 676| -1 0 3 -17 3 25 -.02 7 7 | -724 366 6 88
emr 80| 0 7 -4 -4 0 8 .08 14 14 | 201796 -134 12 112
esa 150| 0 0 0 -16 10 -3 .01 8 7 | -446 -331 8 93
gfz 246| 0 1 -1 -32 -3 -7 .07 10 10 | -409 549 16 76
grg 119| 2 -3 -3 -25 3 11 -.09 12 10 | -152 -94 8 137
igr n/a| 0 0 -1 -14 5 -1 .04 5 5 | -68 -22 11 111
jpl 80| 0 0 1 -34 -12 -3 .12 9 9 | 7335 -122 7 66
mit 358| 0 0 0 -1 17 -46 -.06 6 6 | 16877 -23109 22 1936
ngs 204| 0 -1 2 -4 43 -23 -.06 9 9 | -629 140 938 1736
sio 415| 0 -2 -3 162 -101 78 -.06 10 8 | --- --- --- ---
Table 2.2200.5 GPS week: 2200 Day: 5 MJD: 59649.000
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 680| 0 0 2 -43 5 -13 -.00 8 7 | -808 28 6 97
emr 80| -2 7 -3 -14 29 32 .15 13 13 | 201809 164 13 92
esa 150| 0 0 1 -13 37 21 -.02 7 7 | 10 -912 8 100
gfz 236| 0 -1 -1 32 20 1 .15 12 12 | 310 -465 14 87
grg 118| 2 -2 -1 -19 25 -10 -.11 12 10 | -241 411 8 158
igr n/a| 0 0 0 -9 25 1 .03 5 4 | 1762 -330 10 83
jpl 80| 0 1 0 -13 29 3 .11 8 8 | 7338 192 7 69
mit 358| 0 0 1 -55 30 -29 -.06 6 6 | -1290 1271 22 1556
ngs 203| 0 0 -1 20 32 -15 -.03 8 9 | -694 -14 955 1610
sio 414| 0 0 -1 118 -194 34 -.07 8 7 | --- --- --- ---
Table 2.2200.6 GPS week: 2200 Day: 6 MJD: 59650.000
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 683| 0 0 3 -18 18 20 .01 7 7 | -1018 1305 5 98
emr 80| -2 6 -1 -26 17 1 .15 13 13 | 201901 -385 14 109
esa 150| 0 0 0 -28 4 -11 -.01 8 8 | -87 -85 7 90
gfz 245| 1 0 0 -1 0 -27 .07 10 9 | 228 -202 14 80
grg 114| 2 -4 0 -14 16 -14 -.09 11 10 | 158 -148 8 130
igr n/a| 0 0 -1 -19 0 -23 .04 5 5 | 1324 -575 11 102
jpl 80| 0 0 0 -37 -1 -15 .12 8 8 | 7470 -364 7 67
mit 358| 0 0 0 6 41 8 -.05 6 6 | 8 -408 22 1548
ngs 203| 0 -1 -1 -15 2 -31 -.03 9 9 | -848 677 990 1537
sio 420| -1 0 -2 122 -109 58 -.08 9 8 | --- --- --- ---
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 3.2200.0 GPS week: 2200 Day: 0 MJD: 59644.000
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 11 7 15 7 5 6 5 6 6 2 | 38 37 37 33 38 35 36 33 35 39 35
2 | 8 10 6 9 9 5 7 22 11 9 4 | 36 37 34 34 35 36 36 9999 32 39 34
3 | 5 7 8 10 5 6 7 4 6 7 2 | 44 46 45 44 44 44 46 42 45 44 43
4E | 10 16 10 19 12 5 12 10 19 17 5 | 32 36 38 39 34 36 36 36 36 42 34
5 | 7 10 9 7 5 6 7 6 9 10 2 | 55 55 57 57 53 56 57 52 55 53 54
6 | 5 8 7 11 4 6 6 7 6 10 2 | 41 43 42 41 40 40 43 40 40 43 40
7 | 6 13 7 9 8 4 7 6 9 6 2 | 54 50 46 48 47 49 53 49 47 53 49
8 | 9 19 5 9 13 5 10 9 8 12 3 | 49 48 48 49 48 46 46 48 47 53 47
9E | 6 11 6 12 9 4 9 6 15 7 3 | 32 34 29 27 28 29 28 29 30 35 28
10 | 7 6 6 10 7 3 7 5 8 6 2 | 34 39 36 38 35 34 35 30 31 37 33
X11 | 11 --- --- --- 11 9 10 8 --- --- 6 | 85 --- --- --- 82 78 83 58 --- --- 83
12 | 5 11 5 6 8 4 6 6 8 6 2 | 39 42 39 39 39 39 43 37 41 38 38
13E | 9 18 7 14 9 5 8 10 11 12 3 | 39 39 37 34 41 36 39 40 37 47 38
14 | 9 10 6 7 9 4 9 9 9 9 3 | 33 32 32 34 35 32 32 31 32 35 31
15E | 7 26 9 13 12 5 9 10 9 9 4 | 43 46 45 50 46 45 44 45 45 52 44
16 | 7 16 5 7 11 4 7 5 8 11 3 | 35 37 35 39 38 35 35 34 35 39 34
17E | 9 12 8 10 12 6 9 9 10 12 3 | 84 86 91 88 86 90 87 83 91 92 87
X18 | 12 15 12 9 11 5 9 8 7 --- 4 | 83 80 81 84 80 80 81 80 79 --- 81
19E | 8 13 8 8 12 5 9 8 10 15 3 | 77 74 71 75 77 73 74 74 71 73 73
20 | 6 11 6 7 6 4 5 6 12 8 2 | 48 49 47 49 46 48 49 47 48 49 47
21 | 5 17 5 10 9 5 7 7 7 8 3 | 34 33 34 34 36 32 33 34 35 36 33
22E | 6 10 6 7 8 4 8 8 7 5 2 | 29 29 28 28 29 28 26 28 29 34 27
23 | 7 8 6 11 6 3 8 4 7 10 2 | 61 59 58 60 59 59 61 60 62 68 60
24 | 6 15 8 10 8 3 11 7 7 9 3 | 35 45 39 33 36 34 36 34 33 38 35
25 | 6 9 6 10 9 3 8 5 14 6 3 | 35 38 36 37 36 35 40 32 38 34 35
26 | 8 9 7 6 9 3 9 7 6 12 3 | 36 39 36 37 38 35 38 32 31 37 34
27 | 7 12 8 8 11 3 9 8 5 9 3 | 45 43 47 42 44 44 43 43 42 46 43
X28 | 8 11 6 12 10 5 8 6 9 --- 3 | 35 38 34 36 38 35 39 34 35 --- 35
29E | 8 15 10 11 13 5 8 7 14 8 3 | 89 88 87 86 90 87 90 88 88 89 87
30 | 7 8 6 9 9 4 6 6 7 7 2 | 37 39 33 36 34 35 39 34 33 40 35
31 | 5 13 7 7 10 5 9 7 9 7 3 | 43 48 42 44 40 41 46 46 41 46 43
32E | 8 6 4 7 13 4 8 6 9 6 2 | 31 31 31 30 33 30 31 29 29 37 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 7 10 9 4 8 8 10 9 |T 46 46 45 45 46 45 47 44 44 47 45
WRMS | 7 13 7 10 9 4 8 7 9 9 |NE 45 44 42 43 44 43 45 42 41 43 43
MEDI | 7 11 7 9 9 5 8 7 9 9 |MD 39 42 39 39 39 36 40 40 38 42 38
Table 3.2200.1 GPS week: 2200 Day: 1 MJD: 59645.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 9 8 12 7 5 6 5 10 9 2 | 48 48 49 46 47 47 48 42 50 48 46
2 | 11 8 6 12 12 5 7 21 10 8 4 | 46 46 45 43 43 46 44 9999 43 47 45
3 | 7 12 7 9 7 4 8 4 8 6 2 | 64 64 64 62 65 63 63 62 66 64 63
4E | 13 20 9 22 18 5 11 9 17 13 5 | 66 70 71 74 72 69 68 66 70 70 68
5 | 7 14 7 9 8 5 7 5 9 8 3 | 73 73 70 72 72 72 73 70 71 70 70
6 | 6 10 7 12 7 5 7 4 5 10 2 | 39 43 40 38 38 38 40 36 40 39 38
7 | 9 12 7 9 9 4 8 7 8 7 3 | 35 34 33 34 33 33 34 33 32 39 33
8 | 9 17 7 9 14 4 11 7 9 9 3 | 53 51 54 51 52 51 50 49 51 55 51
9E | 10 11 5 12 12 3 9 6 11 7 3 | 53 53 52 53 56 52 50 51 53 54 51
10 | 7 9 8 9 6 2 6 6 6 9 2 | 52 56 52 52 53 52 53 48 49 53 50
X11 | 9 --- --- --- 12 14 13 10 --- --- 6 | 47 --- --- --- 48 46 50 37 --- --- 47
12 | 7 11 7 10 9 4 7 7 9 9 3 | 38 40 35 36 36 37 38 35 38 38 36
13E | 9 23 7 10 9 5 9 7 6 8 3 | 73 76 71 72 73 72 73 72 71 74 71
14 | 11 12 7 6 8 5 11 7 10 8 3 | 47 48 48 47 49 48 49 47 51 51 47
15 | 9 20 8 10 25 5 9 6 12 7 4 | 42 44 41 42 44 40 42 41 42 45 40
16 | 7 15 5 8 12 3 6 6 8 8 2 | 44 45 43 46 43 43 43 41 45 46 42
17E | 9 13 10 7 16 5 8 7 7 11 3 | 118 122 121 119 120 121 120 117 122 118 119
X18 | 12 13 11 8 14 4 9 9 8 --- 4 | 52 56 51 53 53 52 54 51 49 --- 51
19E | 9 12 8 8 10 4 8 6 9 9 3 | 32 30 28 32 26 31 29 31 31 34 29
20 | 5 14 6 8 9 4 8 5 8 9 2 | 65 66 63 63 63 65 67 62 63 61 63
21 | 6 15 6 11 9 5 6 5 10 7 3 | 48 50 48 51 48 48 49 46 51 50 48
22E | 8 8 7 9 8 3 8 8 8 7 2 | 48 52 52 48 48 51 50 50 48 50 49
23 | 6 11 7 10 6 4 8 5 7 8 2 | 47 49 46 47 45 47 49 47 49 54 47
24 | 7 12 8 11 9 6 8 4 7 8 3 | 41 44 40 39 39 41 44 39 40 39 39
25 | 8 11 8 8 12 4 7 6 10 8 3 | 36 40 37 38 37 37 41 34 35 40 36
26 | 9 9 7 8 9 2 7 8 5 9 2 | 45 46 44 44 45 45 46 42 42 46 43
27 | 9 12 7 11 10 3 10 7 7 7 3 | 48 47 49 49 50 49 48 46 46 52 47
X28 | 10 16 5 15 8 5 9 8 19 --- 4 | 40 44 42 42 38 41 44 39 45 --- 40
29E | 8 16 6 10 10 4 7 8 7 5 3 | 53 55 53 53 52 53 53 53 55 60 53
30 | 11 11 6 11 6 4 7 6 8 7 3 | 39 43 39 37 40 38 42 37 38 41 38
31 | 7 12 8 8 9 4 8 4 9 7 2 | 44 47 44 47 44 45 47 43 44 45 44
32E | 8 8 4 10 12 4 9 6 12 7 3 | 50 52 51 51 52 51 53 49 49 54 50
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 7 10 11 4 8 7 9 8 |T 50 52 50 51 50 50 51 48 50 53 49
WRMS | 8 13 7 10 9 4 8 7 9 8 |NE 47 49 47 47 47 47 48 44 47 48 46
MEDI | 8 12 7 10 9 4 8 6 8 8 |MD 47 48 48 47 48 47 49 46 49 50 47
Table 3.2200.2 GPS week: 2200 Day: 2 MJD: 59646.000
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 11 8 8 7 4 6 4 7 8 2 | 21 23 23 22 20 21 22 18 20 22 19
2 | 10 9 9 9 9 4 9 21 9 10 4 | 23 25 26 25 26 24 26 9999 26 27 21
3 | 6 9 8 8 6 4 7 6 6 6 2 | 24 31 29 27 24 26 30 21 24 31 25
4E | 13 17 10 21 22 6 13 11 16 14 5 | 26 31 33 30 33 28 32 29 25 33 27
5 | 7 11 11 7 6 5 7 7 9 7 2 | 36 39 35 33 35 37 38 32 35 42 35
6 | 7 11 8 10 7 5 9 5 9 9 3 | 26 27 26 24 24 24 25 21 22 26 23
7 | 8 13 7 9 10 4 10 6 6 8 3 | 31 35 30 32 28 31 32 32 33 38 31
8 | 11 16 7 15 13 5 11 9 9 9 4 | 23 26 23 22 25 21 21 24 22 29 21
9E | 8 9 7 9 9 5 9 7 11 8 3 | 27 27 27 28 27 26 28 24 27 27 25
10 | 7 6 7 7 5 2 8 5 6 8 2 | 22 24 24 26 22 22 24 19 22 26 22
X11 | 9 --- --- --- 12 18 14 7 --- --- 6 | 31 --- --- --- 35 32 33 24 --- --- 31
12 | 7 13 6 9 7 4 7 6 9 6 2 | 23 26 22 24 20 22 27 25 20 32 23
13E | 8 15 10 6 9 6 9 7 10 10 3 | 30 31 28 30 33 30 32 32 35 41 31
14 | 8 9 6 6 9 4 9 7 10 7 2 | 11 18 15 15 16 13 14 15 16 24 13
15 | 8 22 8 14 20 6 12 8 8 11 4 | 38 39 36 41 41 38 39 38 41 42 37
16 | 7 16 6 8 12 3 5 7 7 7 3 | 17 19 17 19 14 17 18 18 19 26 17
17E | 8 13 10 7 11 5 10 7 10 9 3 | 73 73 75 71 70 74 73 70 74 65 71
X18 | 10 13 14 11 14 5 9 8 13 --- 4 | 36 37 35 40 38 36 36 34 39 --- 35
19E | 7 13 6 8 11 4 7 9 7 9 3 | 45 43 44 42 46 45 42 45 44 50 44
20 | 5 12 8 7 7 4 6 6 9 8 2 | 22 25 27 26 22 25 26 23 28 35 25
21 | 7 18 7 9 9 5 8 5 7 6 3 | 17 23 19 23 20 20 21 18 22 20 18
22E | 7 8 8 8 6 4 9 10 10 6 3 | 16 19 20 18 21 19 16 23 19 27 18
23 | 7 8 9 12 6 4 9 5 8 9 3 | 43 41 42 48 42 42 43 44 47 49 43
24 | 7 12 7 8 8 6 7 5 8 8 2 | 28 30 26 26 24 27 28 24 27 28 25
25 | 6 9 6 7 7 4 9 7 9 7 2 | 18 25 23 19 20 22 28 22 20 29 21
26 | 9 10 8 6 9 2 8 7 7 7 3 | 15 23 19 16 15 17 24 14 16 21 16
27 | 9 11 9 13 10 4 11 6 10 8 3 | 21 22 23 20 22 21 22 20 21 28 20
X28 | 8 13 9 10 11 5 9 5 10 --- 3 | 22 29 22 22 20 21 26 21 22 --- 21
29E | 10 16 10 12 15 5 9 9 13 8 4 | 74 73 74 71 72 72 72 74 76 80 73
30 | 9 9 7 10 6 2 7 5 7 6 2 | 19 24 22 21 21 20 23 20 21 24 20
31 | 10 13 9 8 10 5 9 6 9 7 3 | 39 43 42 40 35 39 43 35 39 39 38
32E | 8 8 6 8 12 4 12 5 8 6 3 | 31 33 32 31 36 32 34 31 33 35 31
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 8 10 10 5 9 8 9 8 |T 29 31 30 30 29 29 31 28 30 34 28
WRMS | 8 13 8 10 10 4 9 7 8 8 |NE 24 27 25 25 24 25 27 23 25 29 24
MEDI | 8 12 8 8 9 4 9 7 9 8 |MD 24 27 26 26 24 25 28 24 25 29 25
Table 3.2200.3 GPS week: 2200 Day: 3 MJD: 59647.000
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 | 4 11 8 10 7 5 5 5 9 6 2 | 21 24 23 23 19 22 25 21 25 22 21
2 | 10 8 8 12 10 6 8 20 9 9 4 | 22 23 20 25 21 22 23 9999 23 24 19
3 | 5 9 8 14 6 6 7 7 9 5 2 | 27 31 29 33 24 26 30 27 26 26 27
4E | 10 17 10 19 17 7 11 10 14 13 4 | 21 28 28 24 26 23 28 27 28 27 24
5 | 7 10 7 8 8 6 7 11 10 9 3 | 55 56 56 57 54 57 57 57 55 53 55
6 | 7 8 7 9 7 4 8 4 4 8 2 | 19 24 22 20 19 20 22 19 19 20 19
7 | 8 12 7 13 9 3 8 5 8 8 3 | 41 38 34 33 32 37 39 37 38 40 36
8 | 9 17 6 9 14 3 11 6 11 11 3 | 22 23 23 22 24 20 20 21 22 25 20
9E | 7 11 6 14 9 7 9 6 10 6 3 | 23 24 21 21 22 22 22 19 22 22 20
10 | 7 6 8 10 6 3 5 6 7 8 2 | 20 24 22 24 18 20 23 20 16 22 20
X11 | 10 --- --- --- 14 8 13 7 --- --- 6 | 35 --- --- --- 35 33 33 22 --- --- 33
12 | 7 10 6 8 7 4 7 6 5 6 2 | 30 35 32 33 30 32 34 30 33 31 31
13E | 6 20 9 13 31 6 13 7 15 9 5 | 25 31 25 27 27 26 29 26 32 29 24
14 | 8 9 6 10 8 5 10 9 11 8 3 | 14 17 15 18 16 13 15 17 18 19 14
15 | 6 17 10 11 19 6 9 8 11 9 3 | 26 29 24 30 22 25 26 28 27 27 24
16 | 6 18 5 8 11 6 7 6 8 6 3 | 15 19 15 17 16 16 17 14 17 18 14
17 | 9 15 9 11 9 5 10 7 10 8 3 | 80 85 87 83 81 85 85 84 88 88 84
X18 | 12 12 11 10 16 7 9 7 8 --- 4 | 34 36 32 37 40 32 37 35 37 --- 34
19E | 7 12 9 12 11 6 9 6 11 10 3 | 38 40 37 41 39 37 36 38 40 38 37
20 | 8 16 6 8 8 5 6 7 14 8 3 | 26 31 26 27 24 25 27 28 27 30 26
21 | 6 16 6 9 9 6 5 7 7 7 2 | 20 23 19 22 18 20 20 23 22 22 20
22E | 10 10 7 10 9 5 8 8 9 5 3 | 25 28 25 26 25 25 25 28 28 27 25
23 | 7 9 9 10 7 5 8 7 9 10 3 | 38 37 34 38 40 34 37 40 37 43 37
24 | 5 11 8 10 8 5 7 8 9 12 3 | 27 27 26 25 25 24 28 21 28 25 24
25 | 6 9 7 16 7 4 8 4 7 7 2 | 23 27 25 25 22 23 29 24 27 25 23
26 | 10 9 8 8 10 8 8 6 10 6 3 | 17 25 18 18 16 18 22 14 17 16 16
27 | 7 15 9 12 9 4 10 5 9 10 3 | 21 22 23 22 21 20 22 19 22 27 20
X28 | 6 13 5 17 8 6 11 7 17 --- 4 | 15 21 15 23 15 15 24 15 24 --- 17
29E | 12 17 11 11 17 7 8 8 10 9 4 | 119 117 121 121 116 119 116 117 121 115 117
30 | 8 10 8 15 6 3 7 5 7 8 3 | 25 27 24 23 21 24 26 22 25 27 23
31 | 7 12 7 9 9 4 8 4 10 6 2 | 33 38 33 39 30 34 39 30 35 33 33
32E | 10 9 5 12 7 4 9 5 7 5 2 | 22 25 21 27 22 21 23 23 23 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 8 11 11 5 8 8 10 8 |T 30 33 30 32 30 30 32 30 32 32 29
WRMS | 7 13 8 12 10 5 8 7 9 8 |NE 26 28 25 27 25 25 28 25 26 27 25
MEDI | 7 11 8 10 9 5 8 7 9 8 |MD 25 27 25 25 24 24 26 24 27 27 24
Table 3.2200.4 GPS week: 2200 Day: 4 MJD: 59648.000
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 | 3 14 8 10 7 5 6 4 10 7 2 | 17 22 20 22 16 17 19 14 17 20 17
X2 | 11 --- 10 --- --- 10 --- 15 --- 11 7 | 21 --- 20 --- --- 21 --- 9999 --- 24 15
3 | 9 9 7 12 6 5 7 5 9 12 3 | 19 24 21 21 21 20 24 16 21 24 19
4E | 9 17 10 14 18 6 10 8 11 14 4 | 28 31 32 31 35 29 32 30 29 32 29
5 | 5 10 7 9 8 6 8 7 10 9 2 | 43 42 42 45 37 42 45 38 38 37 40
6 | 5 8 7 12 9 5 7 4 6 13 2 | 20 24 22 21 20 21 22 19 19 24 20
7 | 7 11 6 8 9 3 8 6 6 11 2 | 24 25 21 24 21 23 27 26 26 24 23
8 | 10 16 7 12 15 5 9 7 9 11 3 | 27 27 27 28 29 25 28 26 25 33 26
9E | 6 9 5 10 10 4 7 5 11 11 2 | 34 34 31 30 31 32 32 32 33 38 31
10 | 8 9 8 11 8 4 7 5 5 9 2 | 17 21 22 23 14 18 21 15 19 21 17
X11 | 15 --- --- --- 15 16 16 21 --- --- 10 | 35 --- --- --- 37 35 32 39 --- --- 39
12 | 6 13 6 8 7 3 6 4 7 7 2 | 28 32 27 28 26 27 30 26 26 28 27
13E | 7 18 9 10 25 5 10 7 12 9 4 | 32 39 33 33 45 33 37 34 32 41 34
14 | 7 10 6 10 8 4 9 5 9 7 2 | 12 15 14 19 15 12 10 13 12 21 12
15 | 8 25 8 11 15 5 11 7 11 9 4 | 31 34 29 35 33 30 32 32 31 34 30
16 | 7 17 6 9 13 6 6 6 11 11 3 | 18 22 17 20 18 19 19 19 23 25 17
17 | 5 13 8 11 16 5 9 6 11 9 3 | 49 53 53 52 49 53 53 50 56 54 51
X18 | 10 16 11 14 17 5 9 8 14 --- 4 | 37 41 36 38 42 37 41 40 43 --- 38
19E | 7 12 8 9 16 4 9 6 10 13 3 | 34 34 32 36 36 33 33 34 30 37 33
20 | 4 13 6 8 8 5 7 7 15 9 3 | 17 22 20 21 16 20 19 18 22 22 18
21 | 5 22 7 13 10 4 5 4 10 11 3 | 17 23 15 20 16 17 17 15 20 21 15
22E | 8 11 8 7 7 4 8 7 8 6 2 | 22 23 22 22 20 21 23 19 23 18 20
23 | 8 10 9 15 9 4 8 6 8 10 3 | 37 38 37 39 39 36 36 38 39 39 37
24 | 9 21 8 9 10 7 14 6 12 19 4 | 21 36 21 19 20 19 25 21 20 30 20
25 | 6 10 8 8 9 3 9 4 11 11 2 | 16 23 19 17 17 16 24 15 16 20 16
26 | 10 9 9 9 10 6 8 8 7 7 3 | 18 23 18 16 17 18 23 14 18 19 16
27 | 7 14 7 9 9 4 9 5 10 8 3 | 22 21 24 21 22 21 22 21 20 27 20
X28 | 6 13 5 11 8 5 9 6 9 --- 3 | 15 23 15 21 15 15 21 15 16 --- 16
29 | 12 18 10 12 15 6 10 8 10 9 4 | 118 122 123 117 120 118 120 118 118 119 119
30 | 7 11 7 6 6 3 8 4 7 7 2 | 21 27 20 19 19 19 24 19 20 23 20
31 | 4 12 8 7 10 5 8 5 5 8 2 | 27 32 25 27 26 25 31 25 29 28 26
32E | 8 9 6 7 9 6 9 5 8 6 2 | 27 31 28 29 30 29 30 27 30 29 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 10 12 5 9 6 9 10 |T 28 32 28 29 29 28 30 28 29 31 27
WRMS | 7 14 7 10 10 5 9 6 9 8 |NE 23 26 22 24 22 22 25 22 23 25 22
MEDI | 7 12 8 10 9 5 8 6 10 9 |MD 22 27 22 23 22 21 27 25 23 27 20
Table 3.2200.5 GPS week: 2200 Day: 5 MJD: 59649.000
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 | 4 11 9 16 10 6 7 4 7 7 3 | 19 23 21 23 19 19 21 17 18 17 18
X2 | 3 --- --- --- --- 19 --- --- --- --- 0 | 20 --- --- --- --- 24 --- 9999 --- --- 20
3 | 8 9 7 13 6 4 7 5 9 9 2 | 20 26 23 27 20 22 26 19 24 20 21
4E | 11 21 10 15 18 5 11 8 8 14 4 | 45 51 48 55 50 48 48 47 47 48 47
5 | 5 11 7 11 8 5 9 6 6 7 2 | 34 37 34 36 32 35 38 33 34 33 33
6 | 7 8 6 12 6 5 7 4 11 9 2 | 22 25 23 22 20 22 23 20 20 22 20
7 | 7 14 5 14 11 5 9 5 10 8 3 | 27 29 24 25 25 28 28 29 30 28 26
8 | 7 16 6 8 13 3 11 7 6 10 3 | 27 29 29 27 28 26 29 28 27 29 27
9 | 6 8 7 13 23 6 8 6 11 5 3 | 34 37 37 35 36 36 34 36 35 34 34
10 | 8 8 8 10 5 3 7 6 9 7 2 | 22 26 25 28 20 23 24 21 21 23 22
X11 | 10 --- --- --- 15 11 13 --- --- --- 8 | 44 --- --- --- 42 40 41 --- --- --- 40
12 | 6 14 5 9 8 4 7 4 9 6 2 | 38 41 38 39 35 38 41 38 38 40 38
13E | 8 13 8 13 19 7 8 9 6 10 3 | 58 61 57 55 55 57 61 62 60 61 58
14 | 8 10 6 8 8 5 9 7 10 8 3 | 15 20 17 21 18 15 18 19 16 22 16
15 | 9 17 10 12 19 4 8 8 10 8 3 | 26 26 22 24 32 24 27 26 30 29 25
16 | 5 17 5 9 11 4 5 7 8 7 2 | 23 28 25 24 23 21 25 23 23 28 23
17 | 6 12 7 11 13 3 8 5 4 9 3 | 54 53 54 55 53 54 53 52 55 55 53
X18 | 10 16 12 14 18 5 9 8 12 --- 4 | 40 44 42 40 42 41 43 41 44 --- 41
19E | 9 12 7 10 16 5 7 5 7 11 3 | 37 35 34 38 40 36 33 35 34 37 35
20 | 7 12 5 8 7 6 9 7 13 10 3 | 19 25 20 21 20 21 23 21 20 21 20
21 | 6 18 7 12 11 4 6 5 8 7 3 | 20 26 20 25 21 21 22 20 21 21 20
22E | 11 8 8 12 7 4 8 9 8 7 3 | 25 26 26 28 26 27 25 28 28 27 25
23 | 7 11 8 15 9 5 8 7 7 8 3 | 33 31 32 37 36 31 31 34 33 38 32
24 | 10 13 7 10 10 4 7 6 8 8 3 | 26 33 29 28 26 26 29 26 27 28 26
25 | 8 11 8 12 8 4 9 6 7 7 3 | 23 31 29 30 25 27 32 26 28 27 27
26 | 9 10 7 10 10 3 7 6 7 7 2 | 23 31 26 25 25 23 28 21 25 25 24
27 | 7 17 6 9 9 4 11 6 6 8 3 | 24 26 25 27 23 24 25 22 23 26 23
X28 | 5 10 5 10 9 6 8 5 15 --- 3 | 16 24 17 21 18 17 23 17 16 --- 17
29 | 10 21 8 18 22 4 10 8 12 7 4 | 69 67 65 65 68 65 66 66 68 69 66
30 | 7 9 7 17 7 5 7 5 10 6 3 | 28 30 30 32 29 29 31 29 30 30 28
31 | 6 13 8 10 10 4 7 5 5 6 2 | 29 35 32 35 31 32 36 28 35 32 31
32 | 10 8 6 11 9 3 8 6 7 5 2 | 33 35 34 36 32 34 36 34 35 33 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 7 12 12 5 8 6 8 8 |T 30 33 31 32 31 30 32 30 31 32 30
WRMS | 7 13 7 12 10 4 8 6 9 7 |NE 25 29 26 28 26 26 28 25 26 26 25
MEDI | 7 12 7 11 10 4 8 6 8 7 |MD 26 30 29 28 28 27 29 28 28 28 26
Table 3.2200.6 GPS week: 2200 Day: 6 MJD: 59650.000
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 11 7 11 8 4 7 5 8 7 2 | 23 26 23 24 22 22 26 20 19 20 21
X2 | 9 10 9 10 12 5 9 17 10 --- 4 | 19 16 14 14 14 19 14 8 13 --- 15
3 | 5 10 9 8 5 4 8 5 11 7 2 | 25 30 28 27 25 26 29 21 24 23 24
4E | 13 23 12 16 20 7 11 8 13 15 5 | 50 49 48 48 49 45 46 47 46 45 46
5 | 6 9 10 10 10 6 10 7 12 8 3 | 52 51 54 49 50 54 55 50 52 49 51
6 | 5 9 8 9 8 6 7 6 12 11 3 | 27 28 28 28 26 28 29 25 23 26 25
7 | 7 10 5 11 11 5 9 4 8 10 3 | 30 30 25 30 22 27 31 28 31 28 27
8 | 10 24 7 13 12 6 10 9 9 9 4 | 31 38 33 32 34 31 32 31 32 33 31
9 | 8 8 6 10 15 5 9 5 11 8 3 | 32 30 32 29 32 30 30 28 28 30 29
10 | 6 9 8 8 6 3 8 4 6 11 2 | 22 27 26 27 22 25 28 20 24 23 23
X11 | 7 --- --- --- 13 11 9 --- --- --- 7 | 72 --- --- --- 72 66 69 --- --- --- 70
12 | 4 13 6 8 8 4 7 5 6 6 2 | 32 37 33 34 31 33 36 32 32 37 33
13E | 9 13 9 8 10 6 9 8 7 8 3 | 56 56 51 52 51 51 54 56 54 57 54
14 | 6 10 6 8 11 7 10 6 8 10 3 | 27 34 28 32 25 30 28 30 27 28 27
15 | 7 16 10 14 18 6 9 6 10 7 3 | 32 33 29 34 36 31 32 31 35 35 31
16 | 7 17 5 6 9 4 6 6 9 7 2 | 21 26 22 22 22 21 22 20 20 26 21
17 | 5 13 8 10 10 5 7 7 5 9 3 | 54 56 54 53 52 55 55 52 51 55 53
X18 | 9 16 13 8 17 6 9 9 11 --- 4 | 73 74 71 71 73 71 73 72 72 --- 72
19E | 6 13 7 9 16 6 8 9 8 10 3 | 60 61 57 63 65 59 60 63 59 59 60
20 | 4 9 9 9 10 7 8 7 10 8 3 | 23 26 22 26 23 22 24 24 22 22 22
21 | 5 12 5 9 8 3 7 5 11 8 2 | 19 22 18 21 21 19 23 20 18 22 19
22E | 6 9 8 8 6 4 7 7 7 6 2 | 24 21 23 23 22 23 20 22 22 21 21
23 | 8 10 8 12 10 5 7 5 7 10 3 | 52 49 47 51 55 49 51 55 51 58 52
24 | 10 11 8 10 10 5 9 4 8 8 3 | 22 27 23 23 24 21 23 19 22 21 21
25 | 5 12 7 7 9 5 8 4 10 5 2 | 19 27 24 22 20 22 27 19 23 24 21
26 | 9 9 8 7 9 4 8 6 10 10 3 | 20 27 22 20 21 21 26 18 20 24 20
27 | 9 16 8 8 9 3 11 6 8 10 3 | 28 28 31 26 29 28 27 26 28 27 26
X28 | 7 9 5 15 10 9 8 6 12 --- 3 | 18 25 17 23 19 18 24 18 16 --- 18
29 | 7 17 8 10 19 5 9 6 6 8 3 | 99 98 98 94 98 95 97 95 99 98 97
30 | 8 7 6 8 8 4 6 5 9 6 2 | 24 27 25 25 23 25 27 23 27 25 24
31 | 5 12 8 9 8 4 8 5 10 8 2 | 30 31 27 30 26 26 33 29 29 28 28
32 | 7 10 5 9 15 4 8 6 7 7 3 | 28 27 27 28 31 27 28 25 25 27 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 10 11 5 8 6 9 9 |T 35 36 34 34 35 35 36 33 33 34 34
WRMS | 7 13 8 9 10 5 8 6 9 8 |NE 30 32 29 29 30 30 32 27 28 28 30
MEDI | 7 11 8 9 10 5 8 6 9 8 |MD 28 30 28 28 26 27 29 26 27 27 26
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 4.2200 GPS week: 2200 MJD: 59644.0-59650.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 7 9 20 |U 13 19 48 |U 9 10 33 |
emr | emr 2948 |U 13 19 34 |U 13 22 62 |U 13 11 45 |
esa | esa 2962 | 11 16 31 | 14 16 56 | 11 11 36 |
gfz | gfz 2948 |U 7 9 20 |U 12 14 43 |U 10 9 33 |
grg | grg 3044 |U 8 11 19 |U 13 18 46 | 9 9 30 |
igr | igr 2962 | 7 8 21 | 12 17 46 | 8 8 30 |
igs | igs 3058 | 7 8 19 | 13 17 45 | 8 9 30 |
jpl | jpl 3044 | 12 16 29 |U 13 19 55 | 11 9 41 |
mit | mit 3030 |U 28 26 58 |U 14 17 43 |U 9 12 34 |
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 5.2200.0 GPS week: 2200 Day: 0 MJD: 59644.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 7 18 | 10 13 34 | 10 12 36 |
emr | emr 2976 | 12 18 22 | 12 19 63 | 13 12 44 |
esa | esa 2976 | 11 13 26 | 12 12 52 | 11 9 36 |
gfz | gfz 2976 | 7 13 20 | 9 12 33 | 11 12 35 |
grg | grg 3072 | 8 9 16 | 9 15 43 | 10 11 35 |
igr | igr 2976 | 7 5 18 | 9 11 36 | 8 9 31 |
igs | igs 3072 | 7 6 15 | 9 12 36 | 8 9 31 |
jpl | jpl 3072 | 12 14 27 | 10 15 49 | 9 7 34 |
mit | mit 3072 | 6 5 14 | 10 13 29 | 11 14 33 |
Table 5.2200.1 GPS week: 2200 Day: 1 MJD: 59645.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 7 15 | 13 17 54 | 9 10 36 |
emr | emr 2976 | 13 22 36 | 13 22 69 | 12 11 46 |
esa | esa 2976 | 12 14 28 | 12 16 60 | 10 9 37 |
gfz | gfz 2976 | 8 12 15 | 11 14 48 | 9 10 35 |
grg | grg 3072 | 8 9 15 | 13 18 54 | 7 8 30 |
igr | igr 2976 | 7 5 15 | 12 15 50 | 8 7 32 |
igs | igs 3072 | 7 7 14 | 12 16 51 | 8 8 33 |
jpl | jpl 3072 | 12 15 22 | 12 16 57 | 10 8 44 |
mit | mit 3072 | 6 7 12 | 15 16 48 | 8 11 34 |
Table 5.2200.2 GPS week: 2200 Day: 2 MJD: 59646.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 7 19 | 9 14 41 | 10 12 36 |
emr | emr 2976 | 12 19 31 | 8 19 46 | 14 10 40 |
esa | esa 2976 | 11 14 31 | 9 13 43 | 12 13 42 |
gfz | gfz 2976 | 7 7 18 | 8 10 38 | 8 8 32 |
grg | grg 3072 | 8 13 22 | 9 12 38 | 11 10 33 |
igr | igr 2976 | 7 7 21 | 8 11 37 | 10 9 32 |
igs | igs 3072 | 7 7 18 | 8 12 35 | 10 9 33 |
jpl | jpl 3072 | 12 19 27 | 9 16 45 | 13 10 41 |
mit | mit 3072 | 6 8 15 | 10 12 35 | 10 12 33 |
Table 5.2200.3 GPS week: 2200 Day: 3 MJD: 59647.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 12 20 | 11 13 36 | 10 11 33 |
emr | emr 2976 | 12 20 33 | 11 18 56 | 13 12 50 |
esa | esa 2976 | 11 17 29 | 10 13 54 | 10 10 41 |
gfz | gfz 2976 | 8 9 19 | 10 9 31 | 11 10 32 |
grg | grg 3072 | 7 14 18 | 10 12 36 | 8 8 31 |
igr | igr 2976 | 7 10 20 | 9 14 38 | 9 8 32 |
igs | igs 3072 | 7 11 18 | 10 12 38 | 8 10 33 |
jpl | jpl 3072 | 12 16 28 | 10 17 51 | 11 11 48 |
mit | mit 3072 | 7 10 18 | 11 11 34 | 10 14 36 |
Table 5.2200.4 GPS week: 2200 Day: 4 MJD: 59648.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 9 20 | 12 28 75 | 9 11 27 |
emr | emr 2880 | 17 16 29 | 12 25 89 | 13 13 42 |
esa | esa 2976 | 11 15 32 | 12 21 83 | 11 12 32 |
gfz | gfz 2880 | 8 6 20 | 12 19 64 | 8 7 28 |
grg | grg 2976 | 8 12 19 | 12 23 65 | 9 7 23 |
igr | igr 2976 | 7 7 23 | 12 23 74 | 8 8 26 |
igs | igs 3072 | 7 8 19 | 12 24 72 | 8 8 25 |
jpl | jpl 2976 | 14 14 29 | 12 24 81 | 12 8 39 |
mit | mit 3072 | 159 129 300 | 12 21 71 | 12 13 46 |
Table 5.2200.5 GPS week: 2200 Day: 5 MJD: 59649.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 11 24 | 26 29 52 | 8 8 28 |
emr | emr 2880 | 16 22 37 | 20 26 60 | 15 13 41 |
esa | esa 2880 | 13 19 35 | 28 24 51 | 10 12 32 |
gfz | gfz 2879 | 8 8 22 | 26 25 50 | 11 10 36 |
grg | grg 2976 | 7 11 20 | 25 27 49 | 8 10 24 |
igr | igr 2880 | 8 10 25 | 26 26 46 | 7 8 25 |
igs | igs 2976 | 7 10 21 | 26 26 46 | 7 8 24 |
jpl | jpl 2976 | 12 20 36 | 25 29 54 | 12 12 37 |
mit | mit 2880 | 7 13 27 | 28 26 46 | 8 9 25 |
Table 5.2200.6 GPS week: 2200 Day: 6 MJD: 59650.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 6 11 25 | 12 19 43 | 9 10 33 |
emr | emr 2976 | 11 17 50 | 14 27 52 | 13 10 55 |
esa | esa 2976 | 10 17 34 | 12 16 50 | 12 12 36 |
gfz | gfz 2976 | 7 11 27 | 9 13 36 | 10 9 34 |
grg | grg 3072 | 8 11 26 | 12 19 40 | 10 9 32 |
igr | igr 2976 | 6 11 26 | 10 16 37 | 8 7 30 |
igs | igs 3072 | 6 10 24 | 10 17 38 | 8 9 32 |
jpl | jpl 3072 | 11 15 36 | 11 20 50 | 10 10 44 |
mit | mit 2976 | 5 11 22 | 11 18 38 | 9 11 31 |
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 6.2200 GPS week: 2200 MJD: 59644.500-59650.500
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 | 4 -13 72 10 -4 | 6 36
| 14 21 62 15 4 | 3
emr uuuuu | -19 -18 14 10 -4 | 55 73
| 15 22 83 46 17 | 5
esa uuuuu | 15 4 24 57 1 | 29 46
| 9 8 42 60 4 | 3
gfz uuuuu | 19 -14 3 18 1 | 25 44
| 11 37 132 75 6 | 2
grg uuuuu | 13 9 64 73 -3 | 5 35
| 17 10 35 29 5 | 3
igr xxxxx | 6 -2 -9 -15 -7 | 4 36
| 5 9 32 31 5 | 4
irf xxxxx | 7 1 -20 -13 8 | -4 37
| 7 6 23 13 5 | 3
jpl uuuuu | 4 9 80 -11 -1 | 34 44
| 10 11 46 39 12 | 3
mit uuuuu | -29 8 -65 -88 5 | 15 38
| 9 13 41 66 7 | 3
ngs uuuuu | 5 3 -167 -5 1 | 13 37
| 18 24 174 69 2 | 2
sio xxxxx | 37 4 -142 -138 -9 | 53 66
| 57 55 134 134 10 | 8
Table 7.2200.0 GPS week: 2200 Day: 0 MJD: 59644.500
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 -8 -14 20 -3 | 5 25
emr uuuuu | -22 -12 -6 -46 28 | 57 67
esa uuuuu | 22 17 1 56 8 | 26 35
gfz uuuuu | 33 43 -141 -43 12 | 23 35
grg uuuuu | -19 -7 2 33 0 | 4 22
igr xxxxx | 16 12 -13 -32 -2 | 5 25
irf xxxxx | 2 7 -33 -5 1 | -4 29
jpl uuuuu | -11 -2 127 -38 -23 | 35 42
mit uuuuu | -19 2 -55 10 -6 | 16 32
ngs uuuuu | 5 -36 76 -40 2 | 12 28
sio xxxxx | 32 101 -373 -21 -22 | 63 72
Table 7.2200.1 GPS week: 2200 Day: 1 MJD: 59645.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 34 -10 64 11 -8 | 11 36
emr uuuuu | -40 10 -134 -29 -19 | 64 79
esa uuuuu | 5 9 -10 -16 2 | 33 49
gfz uuuuu | 4 12 -97 38 6 | 29 47
grg uuuuu | 15 3 66 64 -9 | 11 35
igr xxxxx | 5 -9 28 -42 -10 | 10 36
irf xxxxx | -5 1 2 -2 4 | 0 37
jpl uuuuu | 18 13 15 -49 14 | 39 48
mit uuuuu | -38 -7 2 -13 7 | 19 39
ngs uuuuu | 3 -23 39 23 5 | 17 39
sio xxxxx | -80 6 -258 -61 -23 | 65 75
Table 7.2200.2 GPS week: 2200 Day: 2 MJD: 59646.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 1 -51 43 21 -6 | 6 39
emr uuuuu | -11 -17 141 46 -19 | 55 75
esa uuuuu | 26 8 -19 -35 3 | 29 48
gfz uuuuu | 22 -8 -83 51 -2 | 25 47
grg uuuuu | 28 5 97 99 -4 | 5 38
igr xxxxx | 2 5 -15 7 -11 | 4 40
irf xxxxx | 7 13 -37 -7 13 | -6 40
jpl uuuuu | 3 13 128 43 -1 | 35 47
mit uuuuu | -42 34 -78 -85 12 | 13 39
ngs uuuuu | -14 2 -159 -77 4 | 13 40
sio xxxxx | 33 31 14 24 -3 | 55 70
Table 7.2200.3 GPS week: 2200 Day: 3 MJD: 59647.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -8 -14 169 3 3 | 7 39
emr uuuuu | -35 -1 0 -23 0 | 54 75
esa uuuuu | 23 -3 9 77 -5 | 32 50
gfz uuuuu | 9 -33 -79 -107 2 | 27 48
grg uuuuu | 19 11 84 44 -7 | 7 38
igr xxxxx | 3 -15 -35 -29 -10 | 5 39
irf xxxxx | 5 -4 -42 -33 10 | -3 40
jpl uuuuu | 3 6 45 -52 -6 | 35 46
mit uuuuu | -31 9 -104 -80 10 | 15 40
ngs uuuuu | 27 17 -152 134 0 | 15 41
sio xxxxx | 70 -66 -61 -158 2 | 53 68
Table 7.2200.4 GPS week: 2200 Day: 4 MJD: 59648.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 -12 81 -21 -6 | 3 37
emr uuuuu | 1 -56 4 73 -15 | 48 69
esa uuuuu | 6 3 28 124 3 | 27 46
gfz uuuuu | 13 -6 176 47 -1 | 23 44
grg uuuuu | 32 16 30 103 -3 | 3 36
igr xxxxx | 8 -3 -5 44 2 | 0 37
irf xxxxx | 17 -4 -43 -3 11 | -7 38
jpl uuuuu | 16 6 120 11 6 | 29 41
mit uuuuu | -22 12 -118 -143 5 | 12 37
ngs uuuuu | -14 12 -258 -43 2 | 11 37
sio xxxxx | 77 21 -74 -197 -9 | 46 59
Table 7.2200.5 GPS week: 2200 Day: 5 MJD: 59649.500
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 21 132 23 -2 | 3 37
emr uuuuu | -6 -38 57 0 3 | 49 69
esa uuuuu | 9 4 89 89 -3 | 28 46
gfz uuuuu | 28 -70 144 126 -6 | 23 44
grg uuuuu | 7 26 87 102 -1 | 2 36
igr xxxxx | 2 4 -57 -13 -8 | -1 37
irf xxxxx | 11 -3 10 -12 12 | -7 38
jpl uuuuu | -3 0 44 -25 -1 | 30 41
mit uuuuu | -23 5 -69 -148 10 | 12 37
ngs uuuuu | -1 13 -378 -26 -1 | 11 37
sio xxxxx | 93 -42 -72 -178 -1 | 44 57
Table 7.2200.6 GPS week: 2200 Day: 6 MJD: 59650.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 -16 29 12 -4 | 5 37
emr uuuuu | -22 -14 39 51 -6 | 56 73
esa uuuuu | 12 -7 74 101 2 | 31 48
gfz uuuuu | 21 -38 99 12 -3 | 26 46
grg uuuuu | 9 7 80 68 6 | 5 37
igr xxxxx | 3 -5 33 -39 -9 | 1 37
irf xxxxx | 10 0 1 -30 1 | -1 38
jpl uuuuu | -1 30 80 31 4 | 32 44
mit uuuuu | -29 2 -30 -156 -2 | 17 39
ngs uuuuu | 30 34 -335 -4 -2 | 15 39
sio xxxxx | 33 -19 -167 -374 -10 | 47 60
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