[IGSREPORT-28772] Wk 2215 IGS Final Orbits
acc
acc at igs.org
Fri Jul 8 06:19:41 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2215 (Jun 19, 2022 - Jun 25, 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:
igs2215[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2215[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2215[0-6].cls IGS GPS clock combination summary report.
igs22157.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs22157.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 | ADIS
0 | EMR | IRKJ IRKJ
0 | ESA | GAMB
0 | GRG | DAV1 SVTL DAV1 SVTL
0 | JPL | CHUR FLRS MBAR RIOP CHUR MBAR NYA1
1 | COD | DAV1
1 | EMR | CHUR MAR6 MDVJ TSKB USUD
1 | ESA | DAV1 IRKJ
1 | GFZ | DAV1 HERS MBAR POHN DAV1 HERS POHN
1 | JPL | CHUR DAV1 FLRS KERG NYA1 RIOP BADG CHUR DAV1 NYA1
2 | EMR | MDVJ
2 | ESA | YEL2 SGOC YEL2
2 | GFZ | 5 28 CUSV HERS MDVJ HERS POHN
2 | GRG | 5 5 HARB HARB
2 | JPL | BADG RIOP BADG
3 | COD | IRKJ IRKJ
3 | EMR | MDVJ
3 | GFZ | CRO1 CUSV GOLD GUAM HERS HOFN IISC KOKV POHN SAVO
3 | GFZ | CRO1 GUAM HERS HOFN IISC MKEA POHN
3 | GRG | IRKJ CRO1 IRKJ PIE1 SGOC
3 | JPL | BADG CHUR CRO1 RIOP BADG CHUR POHN
3 | MIT | KOKV
4 | COD | ADIS
4 | EMR | IRKJ IRKJ MDVJ
4 | ESA | BRFT KIT3 PTBB PTBB
4 | GFZ | 28 28 ADIS HERS HOFN IRKJ POHN HERS HOFN IRKJ POHN
4 | GRG | SGOC ULAB
4 | JPL | CHUR KERG RIOP CHUR NICO
5 | COD | SYOG UNSA
5 | ESA | DAV1 DAV1
5 | GFZ | DAV1 SYOG DAV1 GRAC
5 | GRG | SVTL SVTL
6 | COD | WIND
6 | EMR | TSKB YELL
6 | ESA | DAV1 MAW1 DAV1 MAW1 WIND
6 | GFZ | DAV1 HERS SCUB TSKB HERS POHN SCUB
6 | GRG | DAV1 SCUB YEL2 DAV1 SCUB STK2 SVTL YEL2
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
----+--------+--------+-------------
5 | JPL | ~05:05 | ~ -0.18 ns
6 | JPL | ~02:05 | ~ -0.18 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. 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 | .2 .1 .4 -1 -3 0 -.34
EMR | 0 | -4.0 -2.5 -.6 -28 -15 12 .18
ESA | 0 | -1.0 -1.9 .4 -59 -15 45 -.33
GFZ | 0 | -.3 -.1 .0 -3 -5 7 -.27
GRG | 0 | 7.0 -3.3 -13.3 20 19 -27 .23
JPL | 0 | 5.6 -9.2 -5.0 -15 -22 21 -.18
MIT | 0 | 4.1 1.3 -6.1 -28 -12 10 .03
NGS | 0 | 4.6 -8.8 6.2 -61 -8 41 -.17
SIO | 0 | 2.6 -1.7 -7.1 -37 30 18 -.11
COD | 1 | .4 .0 .7 -3 -2 -3 -.35
EMR | 1 | .6 -5.5 -1.8 -22 -6 17 .18
ESA | 1 | -1.4 -1.7 .0 -52 -11 42 -.32
GFZ | 1 | .1 -.3 .3 -4 -11 4 -.24
GRG | 1 | 5.3 -6.8 -16.3 9 -17 -42 .03
JPL | 1 | 4.6 -13.3 -5.0 -7 -11 20 .01
MIT | 1 | .0 -3.2 -8.0 -36 -11 8 .13
NGS | 1 | 4.8 -15.2 4.0 -61 0 74 -.16
SIO | 1 | -1.9 -.6 -10.9 -27 102 20 -.04
COD | 2 | .4 .1 .6 1 -2 1 -.37
EMR | 2 | -4.5 -10.4 -.2 -34 9 17 .08
ESA | 2 | -1.7 -1.9 -.3 -42 -5 47 -.48
GFZ | 2 | .2 -.7 .5 -4 -16 15 -.35
GRG | 2 | -.1 -8.3 -14.6 16 17 -7 -.03
JPL | 2 | 1.9 -17.0 -6.3 -6 -7 4 -.06
MIT | 2 | -3.5 -5.2 -4.7 -41 10 4 -.05
NGS | 2 | 5.4 -14.7 8.3 -78 36 73 -.27
SIO | 2 | -6.3 -3.8 -9.1 -77 115 -21 -.20
COD | 3 | .4 .1 .9 3 -3 4 -.39
EMR | 3 | -5.5 -3.2 1.9 -41 -4 11 .16
ESA | 3 | -1.6 -2.1 -.5 -38 7 53 -.44
GFZ | 3 | .1 -.5 .0 -6 -24 11 -.30
GRG | 3 | -1.1 -9.6 -13.0 13 32 -8 .05
JPL | 3 | -1.9 -10.8 -1.4 -8 -5 5 -.11
MIT | 3 | -2.3 -2.8 -7.5 -30 13 18 .01
NGS | 3 | 1.8 -11.2 4.1 -62 5 16 -.18
SIO | 3 | -5.7 -2.5 -10.1 -54 113 0 -.02
COD | 4 | .5 .1 .7 -1 -3 -4 -.38
EMR | 4 | -4.0 -4.6 .3 -54 -10 11 .05
ESA | 4 | -1.1 -1.6 -.1 -47 7 46 -.46
GFZ | 4 | .4 -.2 .5 -1 -13 9 -.27
GRG | 4 | 3.5 -6.8 -22.2 17 32 -9 .02
JPL | 4 | 5.9 -11.5 -.9 -1 8 -5 -.10
MIT | 4 | -1.3 -1.2 -11.4 -27 10 9 .02
NGS | 4 | 4.0 -15.4 1.4 -45 18 52 -.24
SIO | 4 | -6.3 .5 -17.3 -35 177 32 .08
COD | 5 | .3 -.1 .5 -1 -2 1 -.35
EMR | 5 | .1 -4.2 1.4 -66 -13 10 .20
ESA | 5 | -1.1 -1.1 -.7 -37 5 22 -.33
GFZ | 5 | .0 -.2 .7 -1 -3 9 -.24
GRG | 5 | .6 -7.6 -16.8 29 30 -13 .06
JPL | 5 | 5.1 -10.2 2.8 -1 3 8 -.10
MIT | 5 | -2.1 -3.4 -12.8 -26 13 5 .14
NGS | 5 | -.1 -15.4 8.7 -49 42 49 -.02
SIO | 5 | -3.5 -2.4 -6.9 -59 73 7 .06
COD | 6 | .3 .1 .3 2 -7 -3 -.27
EMR | 6 | -5.4 -9.4 -1.2 -29 -31 -8 .19
ESA | 6 | -.9 -1.4 -1.4 -17 12 49 -.31
GFZ | 6 | .3 -.3 .4 3 -10 9 -.25
GRG | 6 | -.7 -7.3 -22.4 19 37 -13 .04
JPL | 6 | .4 -9.7 3.3 0 1 6 -.09
MIT | 6 | -6.6 -4.7 -12.7 -14 19 17 .13
NGS | 6 | -7.3 -14.8 4.9 -65 44 41 -.07
SIO | 6 | -6.1 -3.3 -12.6 -73 155 -4 -.02
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 1.2215.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2215.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 2.2215.[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 3.2215.[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 5.2215.0-6). 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 2215 summary. (Jun 19, 2022 - Jun 25, 2022)
Table 1.2215.a GPS week: 2215 MJD: 59749.000-59755.000
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 670| 0 0 -3 -2 -27 20 .01 7 7 | -668 26 8 104
| 0 0 1 11 5 14 .02 | 119 206
emr 80| -3 1 5 26 0 10 .02 14 14 | 204777 516 14 141
| 1 2 0 14 9 8 .04 | 1887 890
esa 150| 0 0 0 0 -3 -1 -.04 8 8 | -1404 815 6 94
| 0 0 0 21 5 12 .02 | 288 445
gfz 237| 0 0 -1 5 -6 5 .10 11 11 | 131 135 11 119
| 0 0 1 17 18 7 .03 | 149 249
grg 120| 4 -1 -5 8 4 8 -.04 11 9 | 33 4 9 132
| 0 0 4 10 6 15 .02 | 143 261
igr n/a| 0 0 0 15 -14 -4 .01 4 4 | 4536 590 12 128
| 0 0 0 14 9 8 .01 | 2087 853
jpl 80| -1 0 3 12 -18 -9 .13 9 9 | 426 520 9 120
| 0 1 1 19 7 13 .01 | 1883 872
mit 367| 0 0 0 -32 -3 0 -.03 6 6 | 2912 632 22 1562
| 0 0 0 12 11 18 .01 | 2429 793
ngs 207| 0 0 7 17 7 -11 -.07 9 9 | -477 -13 680 1629
| 1 0 2 11 18 17 .02 | 246 431
sio 543| 0 0 0 12 51 -23 -.01 8 8 | --- --- --- ---
| 0 0 1 64 31 26 .01 | --- ---
Table 1.2215.b GPS week : 2215 MJD: 59749.000-59755.000
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 | 3 3 3 3 3 3 3 |
3 | 4 3 3 3 3 3 4 |
4 | 3 3 3 3 3 3 3 |
5 | 3 3 3 3 3 3 3 |
6 | 3 3 3 3 3 3 3 |
7 | 2 3 3 3 2 2 2 |
8 | 3 3 3 3 3 3 3 |
9 | 3 3 2 2 2 0 4 |
10 | 3 4 4 3 4 3 3 |
11 | 5 5 5 5 4 5 4 |
12 | 4 4 3 3 3 3 3 |
13 | 3 3 3 3 3 3 3 |
14 | 5 4 5 5 4 4 4 |
15 | 3 3 3 2 3 3 3 |
16 | 5 5 5 4 5 5 5 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 4 4 4 4 4 |
19 | 3 3 3 3 3 3 3 |
20 | 3 3 3 3 3 3 4 |
21 | 3 3 3 3 3 3 3 |
22 | 3 3 3 2 3 2 2 |
23 | 5 5 5 5 5 5 6 |
24 | 3 3 2 3 3 3 3 |
25 | 3 4 3 3 3 3 3 |
26 | 4 4 4 4 4 4 4 |
27 | 3 3 3 3 3 3 3 |
28 | 4 4 4 4 4 4 4 |
29 | 3 3 3 3 3 3 3 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 2 2 |
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 2.2215.0 GPS week: 2215 Day: 0 MJD: 59749.000
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 667| 0 0 -4 -18 -22 6 -.01 7 6 | -653 -90 8 100
emr 80| -6 0 6 29 5 8 .03 14 14 | 201670 1053 16 131
esa 150| 0 -1 0 36 4 -17 -.03 8 8 | -1377 823 7 111
gfz 233| 0 0 -2 26 17 1 .08 11 11 | 128 -269 12 124
grg 119| 4 -1 -1 3 15 -11 -.05 11 10 | 68 -334 10 123
igr n/a| 0 0 0 24 4 7 .02 5 4 | 1330 962 12 119
jpl 80| -1 0 2 3 -5 2 .15 9 9 | -2704 1120 9 117
mit 367| 0 1 0 -47 -23 0 -.05 8 7 | -446 1129 30 1481
ngs 205| 0 0 9 33 -18 -3 -.04 9 9 | -513 -134 648 1453
sio 540| 1 0 -1 -33 44 13 -.02 9 9 | --- --- --- ---
Table 2.2215.1 GPS week: 2215 Day: 1 MJD: 59750.000
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 678| -1 0 -4 -7 -30 16 .02 7 7 | -612 138 8 112
emr 80| -1 -1 6 18 0 10 .06 14 14 | 203102 989 13 131
esa 150| -1 0 0 -10 -7 -10 -.02 8 8 | -1482 1315 7 109
gfz 241| 0 0 -1 -6 0 1 .07 12 11 | -31 311 13 126
grg 120| 4 -1 -1 14 4 17 -.03 10 9 | 125 26 11 117
igr n/a| -1 0 0 11 -11 -6 .01 4 4 | 2641 881 11 127
jpl 80| -1 0 2 10 -15 -12 .12 9 9 | -1129 867 9 120
mit 367| 0 1 -1 -25 0 -10 -.03 7 6 | 808 985 25 1524
ngs 211| 2 0 6 9 2 5 -.08 9 9 | -563 106 758 1636
sio 542| 1 0 0 32 48 -20 -.02 9 8 | --- --- --- ---
Table 2.2215.2 GPS week: 2215 Day: 2 MJD: 59751.000
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 681| 0 0 -5 -7 -24 6 -.01 7 7 | -604 -219 10 116
emr 80| -4 -1 4 38 10 14 .08 14 14 | 204117 1145 14 140
esa 150| -1 0 0 12 -10 11 -.01 9 9 | -992 337 6 102
gfz 241| 0 0 0 23 12 -4 .05 11 12 | 65 129 10 121
grg 122| 5 -1 -1 23 6 7 -.05 10 9 | 68 -257 8 138
igr n/a| 0 0 0 28 -16 -4 .00 5 4 | 3565 1204 11 138
jpl 80| 0 0 1 39 -18 -22 .13 9 9 | -262 1059 10 115
mit 367| 0 0 -1 -43 0 24 -.02 6 6 | 1350 1159 22 1627
ngs 207| 0 0 7 24 1 -24 -.07 9 8 | -305 -579 735 1433
sio 551| 0 1 0 -38 32 -27 -.01 8 7 | --- --- --- ---
Table 2.2215.3 GPS week: 2215 Day: 3 MJD: 59752.000
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 678| 0 -1 -3 9 -23 29 .02 7 7 | -586 -77 9 113
emr 80| -4 3 7 27 -9 4 -.00 14 14 | 205265 1545 13 147
esa 150| 0 0 0 -4 -2 -10 -.02 8 9 | -1722 1473 6 94
gfz 239| -1 0 -3 3 -19 19 .13 11 10 | 25 443 13 129
grg 122| 3 -1 -2 3 3 12 -.06 11 9 | -257 421 9 123
igr n/a| 0 0 0 19 -16 -13 -.00 4 4 | 4824 1682 11 125
jpl 80| -1 1 4 9 -17 -17 .12 8 8 | 778 1527 9 112
mit 367| 0 0 0 -17 5 12 -.04 6 5 | 2846 1530 20 1827
ngs 208| 0 0 4 1 20 -30 -.07 9 8 | -921 448 622 1542
sio 534| 1 -1 0 5 37 -34 -.01 8 7 | --- --- --- ---
Table 2.2215.4 GPS week: 2215 Day: 4 MJD: 59753.000
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 668| 0 -1 -2 7 -38 8 .02 7 7 | -869 314 8 104
emr 80| -4 3 5 40 -11 26 -.01 14 14 | 206585 98 13 117
esa 150| 0 0 0 -2 1 0 -.05 8 8 | -1083 311 6 99
gfz 239| -1 0 0 0 -25 5 .11 10 9 | 176 337 11 125
grg 117| 4 0 -8 10 -7 -11 -.02 11 8 | 55 103 10 140
igr n/a| 0 0 0 19 -16 0 -.00 5 4 | 6285 493 13 142
jpl 80| 0 1 4 23 -30 -7 .12 9 9 | 2132 338 10 118
mit 367| 0 0 0 -44 -14 5 -.04 6 5 | 4843 498 21 1754
ngs 209| 0 0 3 27 28 -35 -.04 10 9 | -137 -133 635 1435
sio 546| 0 0 0 3 95 0 -.03 8 7 | --- --- --- ---
Table 2.2215.5 GPS week: 2215 Day: 5 MJD: 59754.000
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 660| 0 0 -3 -10 -23 44 .03 7 7 | -804 253 8 99
emr 80| -1 2 5 0 11 11 -.02 14 14 | 206450 -390 14 184
esa 150| 0 0 0 -33 -2 10 -.06 8 8 | -1747 800 7 75
gfz 234| 0 0 -1 -23 -5 11 .13 11 11 | 122 55 12 104
grg 119| 3 -1 -9 -9 6 26 -.03 10 9 | -17 181 9 142
igr n/a| 0 1 1 -14 -18 2 -.01 4 4 | 6720 -506 14 130
jpl 80| 0 0 4 -22 -19 13 .12 10 10 | 2262 -422 9 130
mit 367| 0 0 0 -30 4 -31 -.02 6 5 | 5161 -348 20 1330
ngs 206| 0 0 9 8 26 2 -.09 10 9 | -534 606 672 2104
sio 543| 0 0 0 145 9 -67 -.02 8 7 | --- --- --- ---
Table 2.2215.6 GPS week: 2215 Day: 6 MJD: 59755.000
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 659| 0 0 -2 13 -27 28 -.00 8 7 | -553 -132 8 90
emr 80| -3 2 4 33 -2 -2 -.03 14 14 | 206253 -826 17 140
esa 150| 0 0 1 3 -7 10 -.06 9 9 | -1426 652 7 68
gfz 237| 0 0 0 12 -28 5 .11 11 10 | 432 -60 11 105
grg 121| 3 -2 -11 12 0 19 -.01 11 11 | 195 -107 10 143
igr n/a| 0 0 0 16 -27 -17 .02 5 4 | 6387 -580 13 119
jpl 80| -1 2 4 21 -20 -20 .12 9 9 | 1909 -845 10 131
mit 367| 0 0 0 -21 4 -6 -.03 7 6 | 5826 -529 22 1395
ngs 209| -1 0 8 14 -8 4 -.10 10 9 | -371 -411 694 1800
sio 547| 0 0 -2 -30 90 -31 -.01 8 7 | --- --- --- ---
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 3.2215.0 GPS week: 2215 Day: 0 MJD: 59749.000
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 9 7 6 11 3 6 7 10 9 2 | 28 30 30 28 27 27 28 29 30 28 27
2 | 6 11 5 9 7 4 6 6 12 7 2 | 23 24 24 27 24 24 24 23 24 23 23
3E | 7 11 5 7 21 4 9 6 8 11 3 | 23 28 26 26 33 26 26 25 30 28 25
4 | 5 17 6 7 9 4 16 5 6 8 3 | 83 89 86 85 84 87 88 85 88 89 85
5E | 6 12 9 8 20 4 6 7 10 6 3 | 48 51 53 48 48 52 50 50 56 52 50
6 | 5 13 7 7 6 2 8 7 8 9 2 | 27 30 29 24 28 26 30 25 25 25 26
7 | 4 10 5 7 6 4 5 5 10 8 2 | 49 51 50 52 50 48 49 51 48 49 49
8 | 4 9 6 7 10 4 8 6 8 8 2 | 21 23 23 22 24 20 22 21 22 21 21
9 | 6 9 6 6 7 3 7 5 8 8 2 | 20 27 22 23 18 23 25 20 25 24 22
10E | 9 11 7 9 9 6 9 5 10 10 3 | 35 40 36 38 38 35 36 35 38 40 36
11 | 9 16 21 25 12 6 10 7 8 9 5 | 56 52 47 65 56 52 54 56 51 56 54
12E | 7 19 12 8 12 5 9 6 8 9 3 | 48 48 44 47 47 46 47 48 46 48 46
13 | 5 12 8 9 9 6 8 6 6 10 2 | 24 32 25 24 26 24 28 24 25 28 24
14E | 10 20 8 16 12 6 11 18 22 13 5 | 58 62 60 65 59 62 64 56 64 59 59
15 | 6 8 6 8 9 5 4 6 7 7 2 | 65 66 62 64 60 64 64 63 61 64 63
16E | 11 28 7 24 12 4 10 8 11 13 5 | 36 39 29 36 33 32 33 34 32 39 33
17 | 6 16 7 10 7 4 7 5 6 7 2 | 28 31 24 29 29 27 30 29 29 28 27
18 | 10 17 13 15 12 8 11 9 8 10 4 | 64 63 62 67 63 61 62 63 64 66 63
19 | 5 23 7 8 8 5 6 7 8 8 3 | 29 38 30 29 30 29 31 30 30 29 29
20E | 7 9 6 6 10 3 6 9 8 7 2 | 80 80 81 78 80 80 81 81 80 80 80
21 | 6 9 9 8 15 4 8 7 10 11 3 | 22 26 23 26 24 22 23 24 26 26 23
22 | 6 7 8 8 8 3 7 7 7 9 2 | 36 37 36 37 37 36 35 39 38 37 36
23E | 11 22 8 17 19 6 12 13 16 7 4 | 54 54 57 62 54 56 58 53 59 55 55
24 | 8 10 6 7 7 6 9 6 6 9 2 | 27 32 29 31 26 27 32 25 27 26 27
25E | 7 16 5 7 10 3 10 11 8 10 3 | 34 38 34 34 33 35 34 37 34 36 33
26 | 10 14 7 9 12 4 9 7 10 15 3 | 32 32 29 33 30 29 28 30 26 31 29
27 | 7 10 7 8 9 4 7 7 5 7 2 | 29 33 30 29 31 28 28 30 29 29 29
X28E | 7 10 11 12 10 6 11 7 9 --- 3 | 20 21 24 19 24 22 24 22 23 --- 21
29 | 6 16 7 7 9 5 9 7 6 9 3 | 33 34 31 34 32 31 30 32 31 31 31
30 | 5 9 7 7 8 4 7 5 9 9 2 | 24 29 24 27 22 24 28 24 23 26 24
31 | 5 9 6 6 7 4 8 6 6 10 2 | 55 56 57 55 53 55 57 53 52 48 53
32 | 6 10 6 7 10 3 8 5 7 7 2 | 24 32 26 26 22 25 30 23 25 24 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 11 11 5 9 8 9 9 |T 38 41 38 40 38 38 39 38 39 40 38
WRMS | 6 14 8 11 10 4 9 7 9 9 |NE 36 39 36 38 36 35 37 36 36 36 35
MEDI | 6 11 7 8 9 4 8 7 8 9 |MD 32 34 30 33 32 29 31 30 30 31 29
Table 3.2215.1 GPS week: 2215 Day: 1 MJD: 59750.000
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 7 8 11 3 9 5 7 7 2 | 22 23 22 23 24 21 22 21 20 22 20
2 | 7 10 5 10 6 3 6 6 8 7 2 | 17 18 19 23 17 17 18 17 17 18 17
3E | 5 18 5 7 15 3 9 6 9 9 3 | 22 28 22 22 29 22 24 21 22 23 22
4 | 6 17 7 9 9 2 16 6 7 7 3 | 63 68 64 64 66 66 67 65 65 66 65
5E | 8 14 9 9 6 4 9 8 8 10 3 | 43 48 47 44 48 46 44 46 48 47 46
6 | 5 9 7 8 6 4 8 5 9 11 2 | 22 25 24 22 23 22 26 19 22 21 21
7 | 6 9 5 9 6 3 6 6 8 10 2 | 28 29 25 32 27 27 28 28 27 29 27
8 | 5 10 7 11 11 2 8 4 8 10 2 | 23 22 23 25 23 21 19 20 20 20 20
9 | 6 8 6 7 6 3 9 6 8 9 2 | 19 25 21 21 18 22 26 18 18 19 21
10E | 6 10 6 14 10 5 9 7 12 13 3 | 33 32 31 34 35 30 31 33 30 38 32
11 | 9 14 20 22 11 5 10 6 8 10 4 | 29 32 29 35 30 28 32 29 28 31 29
12E | 6 20 12 9 12 5 9 7 9 9 3 | 43 45 40 41 40 41 43 43 45 45 42
13 | 6 13 7 9 8 3 9 6 4 8 2 | 21 28 21 19 24 21 27 21 23 24 22
14E | 9 21 8 13 13 6 10 13 15 12 4 | 48 51 51 57 51 51 52 50 50 53 51
15 | 8 10 6 10 7 4 6 8 7 8 2 | 43 43 40 43 41 41 41 43 41 40 41
16E | 11 30 7 29 13 5 10 12 8 17 5 | 28 36 26 37 26 26 26 31 26 30 26
17 | 6 12 6 7 8 5 8 5 10 7 2 | 19 19 15 21 19 18 21 20 20 20 18
18 | 10 16 13 15 11 6 12 7 10 11 4 | 37 40 38 39 34 37 41 37 39 38 36
19 | 6 16 7 8 9 6 9 6 10 9 3 | 16 20 17 19 17 17 19 18 19 19 16
20E | 6 12 6 7 8 3 7 6 5 7 2 | 67 67 67 68 68 68 66 66 69 65 67
21 | 7 11 9 10 15 4 9 6 6 8 3 | 17 19 16 19 22 16 18 17 15 19 15
22 | 6 7 7 8 6 3 9 6 7 8 2 | 31 31 30 30 32 30 29 32 32 32 31
23E | 9 20 9 20 21 5 13 10 17 7 5 | 45 49 48 52 50 47 51 47 49 49 47
24 | 8 12 8 7 6 4 9 6 8 7 2 | 23 32 27 20 21 22 31 20 21 20 22
25 | 8 15 7 6 13 2 10 8 11 9 3 | 20 29 23 22 21 21 24 22 21 23 21
26 | 7 20 6 9 14 4 9 9 11 13 3 | 26 32 23 26 28 23 23 22 22 25 23
27 | 5 10 7 12 8 3 7 5 7 7 2 | 25 29 28 29 28 26 25 26 27 25 26
X28E | 11 12 9 12 7 6 11 8 13 --- 4 | 26 25 24 22 24 23 25 25 26 --- 23
29 | 6 18 7 9 8 5 7 7 8 6 3 | 20 21 18 22 19 19 19 21 20 22 18
30 | 6 8 7 8 6 2 8 5 8 9 2 | 19 24 20 22 19 20 26 20 19 20 20
31 | 6 10 7 9 7 4 8 7 7 8 2 | 40 42 39 40 38 40 42 38 39 35 38
32 | 5 10 6 12 8 3 10 6 7 8 2 | 27 32 26 24 27 26 30 25 26 26 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 12 10 4 9 7 9 9 |T 30 33 30 31 30 29 31 30 30 31 29
WRMS | 7 14 8 11 9 4 9 6 9 8 |NE 26 29 26 28 27 26 28 26 26 26 26
MEDI | 6 12 7 9 8 4 9 6 8 9 |MD 26 29 25 25 27 23 26 25 26 25 23
Table 3.2215.2 GPS week: 2215 Day: 2 MJD: 59751.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 7 9 11 4 7 5 6 6 2 | 29 31 31 29 32 28 30 31 27 32 29
2 | 6 12 5 10 8 4 6 4 7 5 2 | 26 29 28 32 25 28 27 27 26 28 27
3E | 6 19 6 8 12 4 10 6 9 9 3 | 30 38 33 31 36 32 33 33 32 33 32
4 | 5 17 7 8 8 4 15 5 9 6 3 | 57 56 57 57 58 57 57 59 61 58 57
5E | 5 12 10 8 11 3 8 5 9 6 2 | 51 50 54 54 51 53 51 52 53 53 52
6 | 5 15 8 8 5 4 8 6 8 8 2 | 30 33 32 27 29 29 33 30 28 30 29
7 | 6 10 6 11 8 3 6 3 5 6 2 | 46 48 49 48 46 47 50 48 47 48 47
8 | 5 9 6 15 11 4 9 5 7 8 3 | 29 31 33 35 30 30 28 31 28 33 30
9 | 6 11 7 7 6 3 7 5 7 5 2 | 22 29 24 23 23 23 27 25 21 23 23
10E | 7 17 7 20 10 6 9 6 12 10 3 | 41 43 42 44 42 41 40 43 42 42 41
11 | 8 17 20 18 13 7 11 5 7 10 4 | 42 43 39 47 42 41 42 44 40 43 42
12E | 7 21 12 7 9 5 9 5 9 6 3 | 50 51 48 52 47 50 48 50 49 50 48
13 | 6 11 7 8 6 5 8 5 7 5 2 | 34 38 36 36 35 35 39 37 36 38 36
14E | 10 21 9 12 17 5 11 12 17 8 4 | 59 62 58 62 59 60 60 56 64 59 58
15 | 8 9 6 8 9 4 6 5 5 7 2 | 52 51 47 53 47 50 51 52 48 52 50
16E | 11 29 10 22 11 5 11 10 12 14 5 | 32 36 33 37 31 32 31 35 32 31 31
17 | 6 13 7 10 8 5 8 5 9 8 2 | 26 29 26 27 29 27 29 31 29 30 27
18 | 10 15 15 13 10 8 13 9 7 9 4 | 44 45 42 48 46 43 45 45 41 46 43
19 | 5 17 7 9 8 5 9 5 9 10 3 | 25 29 27 24 26 26 27 29 29 29 26
20E | 8 11 6 8 9 3 6 5 7 6 2 | 65 64 66 64 64 65 65 65 64 67 64
21 | 7 11 7 8 14 5 9 6 9 8 3 | 26 30 26 26 28 25 27 31 29 33 27
22 | 8 7 7 7 8 3 9 5 7 10 2 | 48 50 51 50 48 49 49 51 47 52 49
23E | 9 20 10 23 20 6 12 8 16 9 5 | 46 46 50 48 46 48 47 48 46 47 46
24 | 6 10 5 8 6 5 9 5 7 5 2 | 40 45 40 43 38 40 44 40 38 42 40
25 | 8 13 7 9 11 4 10 7 10 10 3 | 29 35 34 33 31 32 29 32 30 33 30
26 | 8 12 10 10 15 5 11 8 13 10 3 | 45 45 44 43 43 42 42 44 40 43 42
27 | 7 8 7 10 9 2 8 4 7 5 2 | 40 41 40 40 40 38 37 42 37 41 39
X28E | 8 11 7 19 9 6 9 8 13 --- 4 | 34 34 33 34 33 34 35 36 36 --- 33
29 | 6 18 7 8 9 6 8 6 6 6 2 | 28 28 28 29 27 29 26 29 30 30 27
30 | 7 11 7 8 9 3 8 5 9 7 2 | 28 32 29 31 28 29 34 28 29 28 28
31 | 5 12 8 8 6 4 9 7 9 6 2 | 57 58 56 53 53 54 57 56 47 51 54
32 | 7 9 7 11 10 2 8 5 5 8 2 | 34 39 36 32 31 34 36 33 31 37 33
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 9 11 10 5 9 6 9 8 |T 38 41 39 40 38 39 39 40 38 40 38
WRMS | 7 14 9 12 9 4 9 6 8 7 |NE 36 39 37 37 36 36 38 38 35 38 36
MEDI | 7 12 7 9 9 4 9 5 8 8 |MD 34 39 36 37 36 35 37 37 36 41 36
Table 3.2215.3 GPS week: 2215 Day: 3 MJD: 59752.000
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 8 7 8 11 4 6 5 6 9 2 | 22 23 21 22 23 20 22 21 19 22 20
2 | 6 15 6 10 6 3 7 4 6 9 2 | 20 24 21 26 20 20 21 19 21 21 19
3E | 6 10 5 8 17 3 9 5 11 9 3 | 17 18 17 18 24 17 20 17 20 19 17
4 | 6 13 4 8 7 4 14 5 5 6 2 | 38 39 38 40 40 37 38 40 41 41 39
5E | 8 12 11 10 11 2 7 5 8 6 3 | 28 31 31 25 32 29 29 30 32 30 29
6 | 5 13 6 12 6 3 7 5 9 10 3 | 24 26 25 25 22 22 25 20 21 22 22
7 | 5 9 5 13 6 3 8 3 4 8 2 | 37 38 39 48 37 38 39 40 37 38 38
8 | 5 10 6 5 14 3 6 3 6 7 2 | 24 24 24 24 24 22 22 21 24 23 22
9 | 4 8 5 8 6 3 8 5 5 7 2 | 18 23 18 21 15 17 23 16 16 16 18
10E | 7 13 6 13 12 6 8 6 12 9 3 | 25 26 23 27 26 24 25 25 26 26 23
11 | 8 18 23 23 12 5 11 6 7 12 4 | 44 44 40 55 47 43 43 46 45 47 44
12E | 7 18 11 8 8 5 7 5 7 6 3 | 51 50 46 51 47 49 47 51 53 49 49
13 | 9 12 6 8 6 4 7 4 10 5 2 | 16 24 16 17 17 15 23 18 16 19 17
14 | 12 22 8 15 16 6 12 9 13 10 4 | 60 61 61 65 61 61 60 60 62 63 60
15 | 8 10 6 9 7 4 5 5 7 4 2 | 54 52 50 54 49 52 49 51 52 51 51
16E | 9 26 8 14 14 4 9 10 9 12 4 | 24 27 22 25 24 22 24 26 26 24 23
17 | 7 14 6 7 8 5 8 5 8 8 2 | 24 26 21 24 23 23 25 24 26 27 23
18 | 10 18 15 12 10 7 11 8 11 10 4 | 48 46 44 53 48 45 47 49 44 47 47
19 | 7 21 8 10 7 5 7 5 11 8 3 | 21 26 21 23 21 21 21 22 24 26 21
20E | 6 10 7 10 11 3 6 4 7 7 2 | 30 31 30 30 31 30 31 31 30 32 30
21 | 7 8 7 9 14 5 6 5 6 6 2 | 17 20 18 21 21 18 19 20 16 20 17
22 | 5 8 5 8 7 3 5 5 8 6 2 | 19 22 20 24 18 19 19 21 21 20 20
23E | 8 22 10 21 20 5 12 8 19 8 4 | 25 26 29 36 26 29 31 24 32 28 26
24 | 9 13 5 7 6 4 9 5 9 7 2 | 19 26 21 25 18 18 26 18 22 18 20
25 | 6 14 7 9 9 4 12 7 8 6 3 | 22 30 26 20 24 23 24 23 22 24 22
26 | 7 13 8 11 15 4 10 7 12 12 3 | 24 22 23 25 22 22 21 21 23 23 21
27 | 7 11 8 9 10 3 6 5 8 5 2 | 24 27 24 23 23 21 23 22 22 24 22
X28E | 7 10 10 13 12 7 8 7 13 --- 3 | 28 29 28 29 28 27 29 28 31 --- 27
29 | 6 21 7 9 7 5 8 6 8 6 3 | 23 26 22 22 21 20 22 21 22 22 21
30 | 4 9 7 10 6 2 9 4 5 8 2 | 19 25 21 26 18 21 26 19 21 19 19
31 | 6 10 6 6 7 3 7 5 8 8 2 | 44 44 45 44 44 43 46 44 39 40 43
32 | 6 9 6 9 9 2 7 4 8 7 2 | 23 26 21 21 19 21 27 20 19 22 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 11 10 4 8 6 9 8 |T 28 30 28 30 28 27 29 28 28 29 27
WRMS | 7 14 9 10 9 4 8 5 8 7 |NE 27 29 26 30 26 26 28 26 26 27 26
MEDI | 7 12 7 9 9 4 8 5 8 8 |MD 24 26 23 25 24 22 25 22 24 24 22
Table 3.2215.4 GPS week: 2215 Day: 4 MJD: 59753.000
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 9 9 8 12 4 9 5 7 7 2 | 22 21 23 22 27 22 24 22 24 23 22
2 | 5 10 6 9 6 4 7 4 8 7 2 | 18 21 20 24 19 20 20 19 19 20 19
3E | 5 10 4 10 17 4 9 4 12 9 3 | 18 19 18 18 27 18 19 18 21 20 18
4 | 5 13 5 6 8 4 15 6 5 6 2 | 56 57 57 56 58 57 55 57 58 58 56
5E | 8 11 10 9 10 3 8 4 9 5 2 | 29 31 32 28 30 29 31 30 32 30 29
6 | 6 15 7 7 7 4 8 4 7 8 2 | 23 27 25 22 22 22 26 20 22 21 22
7 | 5 7 6 9 6 5 7 3 7 7 2 | 41 40 41 43 42 40 40 38 42 38 40
8 | 7 10 7 7 13 3 8 3 7 6 2 | 22 25 25 23 25 22 23 22 23 23 22
9 | 4 9 5 5 6 3 8 5 5 6 2 | 20 28 23 22 21 21 25 20 22 22 21
10E | 8 21 6 14 10 5 8 6 13 9 3 | 25 30 25 29 24 24 24 25 27 28 24
11 | 7 15 21 17 11 8 10 6 8 8 4 | 38 42 35 47 44 39 40 42 36 43 40
12E | 6 19 10 13 11 5 11 5 8 5 3 | 48 48 47 46 51 47 49 49 49 49 48
13 | 5 10 8 8 6 4 7 5 8 5 2 | 20 24 17 17 18 17 23 18 19 19 18
14 | 11 19 10 13 14 7 11 9 13 10 4 | 53 55 54 58 53 56 57 56 58 61 55
15 | 7 8 6 10 7 5 5 6 8 7 2 | 48 47 43 48 47 45 45 46 45 47 46
16E | 8 27 10 17 15 6 10 10 7 14 4 | 23 27 22 25 26 22 22 26 26 28 23
17 | 6 12 6 6 8 5 8 5 11 8 2 | 22 24 22 27 23 24 25 26 28 28 24
18 | 9 16 15 11 9 7 12 8 8 7 3 | 43 47 39 44 45 41 43 45 45 44 43
19 | 6 21 8 8 9 5 9 5 12 8 3 | 22 28 24 25 21 23 25 25 26 25 23
20E | 6 14 7 11 11 6 8 4 10 8 3 | 48 50 48 49 49 48 49 48 50 48 48
21 | 6 10 7 8 23 5 7 4 9 6 3 | 18 19 16 19 32 18 19 20 19 21 18
22 | 4 10 6 7 7 3 8 6 10 7 2 | 36 36 35 36 34 35 34 37 36 37 35
23E | 8 19 8 22 15 5 12 7 19 9 4 | 29 29 33 36 30 31 34 29 31 31 29
24 | 7 11 8 6 6 4 11 3 12 6 2 | 26 30 28 28 23 25 30 24 25 25 25
25 | 6 12 6 11 9 4 10 7 11 6 3 | 22 25 25 25 24 23 23 23 23 25 22
26 | 8 11 7 7 12 3 11 8 10 12 3 | 31 29 29 29 30 28 29 28 25 30 28
27 | 8 13 7 10 9 2 8 5 10 8 3 | 29 33 32 29 30 29 30 30 30 31 29
X28E | 7 10 9 10 13 6 9 8 11 --- 3 | 25 28 23 24 29 24 25 26 31 --- 24
29 | 6 18 7 9 8 5 10 6 9 9 3 | 23 25 20 26 23 23 22 23 28 24 22
30 | 7 10 7 7 7 4 10 6 9 8 2 | 20 25 19 21 19 19 26 16 18 20 18
31 | 6 9 6 7 5 4 9 3 10 5 2 | 46 44 44 46 45 44 47 43 42 43 44
32 | 6 9 7 10 8 2 8 6 10 7 2 | 23 25 19 22 23 20 27 20 21 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 10 11 5 9 6 10 8 |T 30 32 30 31 31 29 31 30 31 31 29
WRMS | 7 14 8 9 8 4 9 5 9 7 |NE 29 31 28 30 30 28 30 29 29 30 28
MEDI | 6 11 7 9 9 4 9 5 9 7 |MD 25 28 25 27 27 24 26 26 27 28 24
Table 3.2215.5 GPS week: 2215 Day: 5 MJD: 59754.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 10 8 7 9 4 8 10 9 6 3 | 24 25 25 24 26 23 26 23 23 23 23
2 | 7 11 5 9 7 3 7 4 10 8 2 | 18 21 21 24 19 19 20 19 20 21 19
3E | 6 10 6 8 19 3 10 6 10 7 3 | 19 20 20 19 29 18 22 19 21 20 20
4 | 5 13 5 9 8 4 14 6 10 6 3 | 58 57 57 59 53 58 60 55 56 57 56
5E | 7 10 8 9 8 3 9 5 7 6 2 | 43 47 44 46 42 45 46 46 43 44 44
6 | 6 14 7 9 7 3 8 5 9 9 2 | 23 27 24 22 22 21 25 21 23 22 22
7 | 6 9 4 9 6 2 6 4 8 7 2 | 36 39 37 40 37 36 37 35 36 36 36
8 | 7 10 7 8 13 3 10 4 8 7 2 | 21 21 22 24 22 19 20 19 20 21 19
X9 | 3 --- --- --- --- 10 --- --- --- --- 0 | 25 --- --- --- --- 32 --- --- --- --- 25
10E | 9 11 6 12 11 5 8 7 11 7 3 | 24 28 24 29 28 26 26 26 25 29 25
11 | 7 15 22 22 10 6 12 6 7 9 4 | 32 33 30 38 35 30 34 33 30 34 32
12E | 6 19 10 8 9 6 10 4 11 6 3 | 52 54 49 52 54 52 53 52 52 52 51
13 | 5 9 7 7 7 4 9 3 9 6 2 | 16 22 15 16 17 17 25 17 20 16 17
14 | 11 20 10 15 12 5 11 7 10 8 4 | 44 43 44 49 48 44 49 45 43 46 44
15 | 8 9 6 9 7 5 7 6 9 6 2 | 36 34 31 37 34 33 34 32 33 32 33
16E | 9 24 10 14 14 5 9 8 11 16 4 | 50 49 48 50 49 49 48 49 49 52 49
17 | 6 13 6 6 8 5 9 4 7 9 2 | 22 21 19 23 22 20 23 22 24 27 21
18 | 10 17 14 9 9 6 11 10 8 7 3 | 36 37 39 37 40 37 40 41 38 38 37
19 | 6 22 8 7 9 4 9 6 7 10 3 | 20 23 21 22 20 20 20 23 24 25 20
20E | 6 8 7 11 13 4 9 6 9 8 3 | 67 68 66 67 65 67 68 69 64 67 67
21 | 7 14 6 8 12 4 10 10 8 8 3 | 19 24 16 20 23 17 19 23 16 22 18
22 | 2 7 6 6 6 3 8 5 11 6 2 | 32 32 30 32 33 31 32 34 28 33 32
23E | 9 22 9 25 17 6 12 7 17 9 5 | 41 41 44 52 42 46 45 44 44 44 43
24 | 7 13 7 10 6 4 12 4 9 7 3 | 29 34 27 31 24 28 35 27 24 26 27
25 | 5 12 7 11 8 5 11 7 10 4 3 | 21 24 24 23 23 21 24 19 23 21 20
26 | 6 11 9 14 13 4 11 6 13 13 3 | 23 21 22 28 26 21 19 22 20 23 21
27 | 9 9 9 9 11 2 9 6 11 7 3 | 25 28 28 27 26 24 24 27 24 28 25
X28E | 8 10 9 11 11 6 10 6 7 --- 3 | 24 25 24 24 29 23 25 24 22 --- 23
29 | 6 19 8 8 5 5 11 6 9 12 3 | 21 22 17 23 21 19 21 22 21 23 19
30 | 5 10 7 8 6 3 8 5 8 6 2 | 23 26 23 24 20 21 27 19 20 22 21
31 | 5 8 6 7 5 4 8 3 9 6 2 | 37 42 38 41 40 38 42 41 37 38 39
32 | 4 8 7 7 7 2 9 5 9 6 2 | 24 26 20 21 25 21 27 21 18 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 8 11 10 4 10 6 10 8 |T 30 32 30 33 32 30 32 31 30 32 30
WRMS | 7 14 8 11 9 4 10 5 9 7 |NE 27 29 26 29 27 26 29 27 26 28 26
MEDI | 6 11 7 9 9 4 9 6 9 7 |MD 24 28 25 28 28 24 27 26 24 27 25
Table 3.2215.6 GPS week: 2215 Day: 6 MJD: 59755.000
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 7 6 7 11 3 7 7 8 9 2 | 32 32 32 32 34 31 34 31 29 32 31
2 | 4 9 5 12 7 4 7 6 10 8 2 | 29 30 31 32 29 31 32 30 29 31 30
3E | 7 9 5 8 19 4 11 8 12 6 3 | 37 39 38 40 43 37 41 38 36 39 38
4 | 6 13 5 5 9 4 12 7 9 8 3 | 88 89 87 86 84 88 90 85 89 84 86
5E | 7 11 8 9 14 5 9 6 13 6 3 | 76 78 79 77 75 79 78 76 80 76 77
6 | 6 15 7 10 7 4 8 6 11 9 3 | 35 37 37 34 33 34 38 32 30 32 33
7 | 6 9 5 10 6 2 6 3 7 6 2 | 53 55 55 58 57 54 54 53 51 56 54
8 | 9 8 9 7 14 3 8 6 11 6 3 | 35 33 35 35 32 32 31 31 31 34 32
X9 | 11 11 8 6 --- 5 7 8 7 --- 3 | 19 19 14 13 --- 14 19 11 13 --- 20
10E | 8 10 7 9 13 6 8 6 12 8 3 | 46 47 45 49 52 46 49 48 46 51 48
11 | 8 13 21 12 11 5 9 8 8 8 4 | 67 65 61 71 69 65 66 67 63 67 66
12 | 5 17 10 6 15 5 7 5 8 7 3 | 66 67 64 65 66 66 67 66 68 67 65
13 | 4 11 9 10 8 4 7 5 9 5 2 | 39 41 37 39 39 39 44 40 41 39 39
14 | 10 21 12 14 12 6 12 8 13 11 4 | 58 57 58 63 58 58 60 61 62 64 59
15 | 6 7 6 12 8 5 6 7 9 6 2 | 79 74 75 81 77 78 75 76 76 78 77
16E | 20 27 9 8 13 8 8 8 14 15 5 | 59 57 59 62 57 59 56 58 59 50 57
17 | 5 12 7 10 8 5 7 5 11 10 3 | 29 31 28 34 28 30 32 32 32 35 30
18 | 10 16 15 10 12 7 10 11 7 7 4 | 72 72 69 72 74 69 70 73 69 72 71
19 | 6 17 7 10 8 6 10 6 10 12 3 | 30 34 31 33 29 30 31 33 33 36 31
20E | 7 12 8 11 16 6 8 10 12 13 3 | 109 107 107 106 105 108 108 108 107 107 107
21 | 7 11 5 10 13 4 8 7 10 7 3 | 26 30 26 29 33 27 30 31 28 30 28
22 | 4 10 5 5 9 3 7 5 8 5 2 | 55 56 56 55 58 55 54 56 52 56 55
23E | 10 23 15 28 22 8 12 9 17 9 5 | 74 77 78 85 75 80 80 79 82 77 78
24 | 6 11 6 9 7 5 10 4 7 7 2 | 40 45 41 45 39 41 49 40 38 39 41
25 | 6 12 6 11 10 5 8 8 6 7 3 | 35 41 34 34 35 35 36 33 34 37 34
26 | 7 11 8 13 12 4 9 8 11 14 3 | 37 37 39 39 39 37 36 38 35 34 36
27 | 7 15 8 7 10 3 7 4 9 7 2 | 41 42 42 40 43 40 40 40 38 39 40
X28E | 8 9 9 14 15 11 11 10 14 --- 4 | 48 47 43 41 48 43 46 48 54 --- 46
29 | 5 19 7 10 7 5 10 7 7 9 3 | 31 35 28 34 29 32 32 33 31 32 30
30 | 7 10 7 11 7 3 9 5 9 7 2 | 35 35 32 37 33 34 38 31 31 35 33
31 | 5 11 4 9 6 3 6 4 8 6 2 | 59 63 63 60 62 60 62 62 53 60 60
32 | 4 12 7 7 11 3 7 6 9 4 2 | 47 51 48 49 51 50 51 47 48 49 48
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 9 11 11 5 9 7 10 8 |T 49 50 49 50 51 49 50 49 49 51 49
WRMS | 7 14 9 10 11 4 9 6 9 7 |NE 44 45 43 45 46 44 45 44 42 46 44
MEDI | 6 11 7 10 11 5 8 6 9 7 |MD 41 45 42 41 48 41 46 40 41 39 41
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 4.2215 GPS week: 2215 MJD: 59749.0-59755.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 12 11 35 |U 7 15 32 |U 0 0 0 |
emr | emr 3058 |U 17 15 45 |U 12 22 47 |U 0 0 0 |
esa | esa 3058 | 11 13 37 |U 8 19 39 | 0 0 0 |
gfz | gfz 3058 |U 11 11 34 |U 7 12 30 |U 0 0 0 |
grg | grg 3044 |U 12 12 38 |U 8 13 39 |U 0 0 0 |
igr | igr 3058 | 11 11 31 | 7 14 30 | 0 0 0 |
igs | igs 3058 | 11 10 33 | 7 14 30 | 0 0 0 |
jpl | jpl 3058 |U 13 13 39 |U 9 22 36 | 0 0 0 |
mit | mit 3058 |U 11 10 33 |U 7 12 30 |U 0 0 0 |
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 5.2215.0 GPS week: 2215 Day: 0 MJD: 59749.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 10 15 31 | 8 16 25 |
emr | emr 3072 | 24 19 52 | 14 23 46 |
esa | esa 3072 | 8 16 37 | 9 20 37 |
gfz | gfz 3072 | 8 13 26 | 8 9 25 |
grg | grg 3072 | 9 14 35 | 9 15 34 |
igr | igr 3072 | 8 15 29 | 8 14 28 |
igs | igs 3072 | 8 14 29 | 8 14 26 |
jpl | jpl 3072 | 12 17 42 | 10 24 33 |
mit | mit 3072 | 8 13 27 | 8 11 28 |
Table 5.2215.1 GPS week: 2215 Day: 1 MJD: 59750.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 11 6 35 | 7 18 32 |
emr | emr 3072 | 17 9 47 | 10 27 56 |
esa | esa 3072 | 10 10 37 | 6 23 36 |
gfz | gfz 3072 | 12 7 35 | 5 14 30 |
grg | grg 3072 | 13 7 35 | 8 16 40 |
igr | igr 3072 | 10 6 33 | 5 18 29 |
igs | igs 3072 | 9 6 35 | 6 17 29 |
jpl | jpl 3072 | 12 10 42 | 7 25 32 |
mit | mit 3072 | 11 7 36 | 6 15 30 |
Table 5.2215.2 GPS week: 2215 Day: 2 MJD: 59751.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 9 12 39 | 7 16 23 |
emr | emr 3072 | 12 14 47 | 11 21 34 |
esa | esa 3072 | 7 13 48 | 7 21 32 |
gfz | gfz 3071 | 9 10 38 | 5 11 21 |
grg | grg 3072 | 10 12 43 | 9 13 38 |
igr | igr 3072 | 8 12 38 | 6 15 20 |
igs | igs 3072 | 8 11 39 | 6 14 21 |
jpl | jpl 3072 | 9 14 47 | 9 22 24 |
mit | mit 3072 | 9 11 38 | 7 13 25 |
Table 5.2215.3 GPS week: 2215 Day: 3 MJD: 59752.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 20 12 36 | 7 14 31 |
emr | emr 3072 | 19 20 45 | 11 20 46 |
esa | esa 3072 | 18 16 34 | 8 18 35 |
gfz | gfz 3072 | 19 13 33 | 7 11 27 |
grg | grg 3072 | 21 12 37 | 7 10 40 |
igr | igr 3072 | 18 13 30 | 6 13 28 |
igs | igs 3072 | 20 12 31 | 6 13 28 |
jpl | jpl 3072 | 18 16 37 | 9 22 33 |
mit | mit 3072 | 21 12 30 | 7 11 28 |
Table 5.2215.4 GPS week: 2215 Day: 4 MJD: 59753.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 11 10 40 | 8 13 35 |
emr | emr 3072 | 13 15 46 | 13 16 40 |
esa | esa 3072 | 13 14 37 | 9 17 40 |
gfz | gfz 3071 | 12 11 38 | 7 11 30 |
grg | grg 3072 | 12 13 40 | 7 11 33 |
igr | igr 3072 | 11 9 32 | 7 13 32 |
igs | igs 3072 | 10 11 37 | 7 11 30 |
jpl | jpl 3072 | 13 12 42 | 10 20 41 |
mit | mit 3072 | 11 11 37 | 7 9 29 |
Table 5.2215.5 GPS week: 2215 Day: 5 MJD: 59754.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 2976 | 11 11 33 | 8 14 37 |
emr | emr 2976 | 17 18 48 | 13 19 56 |
esa | esa 2976 | 12 14 36 | 9 17 47 |
gfz | gfz 2976 | 10 13 34 | 8 11 33 |
grg | grg 2976 | 11 13 39 | 8 12 40 |
igr | igr 2976 | 11 12 29 | 7 14 36 |
igs | igs 2976 | 11 11 30 | 8 13 35 |
jpl | jpl 2976 | 16 15 35 | 9 21 48 |
mit | mit 2976 | 10 12 37 | 9 11 36 |
Table 5.2215.6 GPS week: 2215 Day: 6 MJD: 59755.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 11 9 32 | 7 16 42 |
emr | emr 3072 | 14 13 32 | 12 25 53 |
esa | esa 3072 | 11 8 32 | 8 19 48 |
gfz | gfz 3072 | 8 9 34 | 8 14 41 |
grg | grg 2976 | 10 11 35 | 9 15 45 |
igr | igr 3072 | 9 8 26 | 7 14 40 |
igs | igs 3072 | 9 8 27 | 6 15 39 |
jpl | jpl 3072 | 13 9 27 | 9 24 41 |
mit | mit 3072 | 10 8 29 | 7 12 37 |
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 6.2215 GPS week: 2215 MJD: 59749.500-59755.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 20 -12 51 -39 2 | 5 17
| 8 12 48 32 3 | 5
emr uuuuu | -27 -20 -47 165 -1 | 12 25
| 11 22 97 90 15 | 4
esa uuuuu | 10 2 36 125 0 | 9 18
| 10 13 74 70 2 | 4
gfz uuuuu | -12 -13 161 -200 -5 | 24 29
| 14 19 113 89 5 | 4
grg uuuuu | -9 -8 -11 -92 2 | 1 14
| 11 15 51 33 2 | 4
igr xxxxx | 9 -14 16 -20 -1 | -1 15
| 11 9 43 23 5 | 4
irf xxxxx | 4 2 -7 -23 -1 | -1 16
| 9 6 13 17 3 | 4
jpl uuuuu | 6 -23 24 90 1 | 27 31
| 9 13 34 48 9 | 3
mit uuuuu | -4 37 -32 -87 -4 | 18 23
| 13 9 58 55 3 | 3
ngs uuuuu | -11 2 -184 108 -2 | 11 17
| 27 19 180 73 3 | 4
sio xxxxx | -123 45 -152 -283 -9 | 25 29
| 48 25 150 115 7 | 4
Table 7.2215.0 GPS week: 2215 Day: 0 MJD: 59749.500
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 -3 120 -64 -3 | 12 26
emr uuuuu | -14 0 -193 190 6 | 19 37
esa uuuuu | 12 0 101 151 0 | 15 26
gfz uuuuu | -22 -30 112 -312 -6 | 31 37
grg uuuuu | -29 -11 26 -151 3 | 6 20
igr xxxxx | -8 -23 72 -46 -6 | 6 19
irf xxxxx | -4 -2 -21 -51 -5 | 4 20
jpl uuuuu | 19 6 -18 183 2 | 31 36
mit uuuuu | -9 29 -92 -137 -3 | 24 30
ngs uuuuu | 4 -11 -173 187 -1 | 18 24
sio xxxxx | -44 59 -365 -337 -4 | 33 38
Table 7.2215.1 GPS week: 2215 Day: 1 MJD: 59750.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 20 -18 80 -25 2 | 3 16
emr uuuuu | -43 9 -29 266 10 | 10 22
esa uuuuu | 18 -6 137 154 1 | 8 16
gfz uuuuu | -23 -19 281 -281 -7 | 23 27
grg uuuuu | -12 -36 72 -84 1 | 0 12
igr xxxxx | 9 -22 77 -3 0 | -1 15
irf xxxxx | -7 5 -8 -35 0 | -4 15
jpl uuuuu | -2 -25 19 124 -10 | 26 31
mit uuuuu | 2 51 -112 -96 -4 | 18 22
ngs uuuuu | -4 20 -387 -8 -3 | 11 16
sio xxxxx | -124 28 -129 -375 -6 | 26 29
Table 7.2215.2 GPS week: 2215 Day: 2 MJD: 59751.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 14 10 60 -61 1 | 0 14
emr uuuuu | -25 -33 -6 290 17 | 7 21
esa uuuuu | 22 -22 98 168 0 | 4 14
gfz uuuuu | -18 -37 330 -104 -12 | 20 26
grg uuuuu | 0 -11 1 -62 0 | -3 12
igr xxxxx | 19 -9 -39 -2 -7 | -5 15
irf xxxxx | -1 -4 -25 -30 3 | -6 16
jpl uuuuu | 5 -32 45 65 -2 | 22 28
mit uuuuu | -22 45 -62 -153 -3 | 15 21
ngs uuuuu | 16 20 -363 73 -5 | 8 15
sio xxxxx | -129 72 -345 -290 -5 | 23 28
Table 7.2215.3 GPS week: 2215 Day: 3 MJD: 59752.500
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 -24 76 -46 4 | 0 15
emr uuuuu | -19 -43 66 167 8 | 8 22
esa uuuuu | 12 6 -30 204 2 | 5 15
gfz uuuuu | 3 -18 160 -97 2 | 20 25
grg uuuuu | 1 -7 -10 -117 1 | -3 13
igr xxxxx | 7 -23 -15 5 1 | -5 14
irf xxxxx | 19 -7 -4 -26 -1 | -5 17
jpl uuuuu | -7 -28 53 47 -6 | 23 29
mit uuuuu | 2 40 -1 -119 -9 | 15 21
ngs uuuuu | -21 25 -276 64 -4 | 7 14
sio xxxxx | -120 20 -119 -356 -12 | 23 27
Table 7.2215.4 GPS week: 2215 Day: 4 MJD: 59753.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 33 -11 34 28 3 | 3 15
emr uuuuu | -16 -48 60 101 -20 | 12 24
esa uuuuu | -7 5 13 114 0 | 7 16
gfz uuuuu | -13 -7 130 -266 -1 | 22 27
grg uuuuu | -1 9 -48 -55 2 | 0 13
igr xxxxx | -3 -13 18 -54 1 | -3 14
irf xxxxx | 11 2 -1 -10 1 | -2 16
jpl uuuuu | 2 -27 -10 73 1 | 26 30
mit uuuuu | 13 34 -13 -63 -1 | 17 22
ngs uuuuu | -55 -4 -162 95 3 | 8 15
sio xxxxx | -184 10 37 -306 -5 | 23 27
Table 7.2215.5 GPS week: 2215 Day: 5 MJD: 59754.500
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 | 27 -23 -22 -48 7 | 6 14
emr uuuuu | -38 -12 -127 76 -15 | 13 22
esa uuuuu | 13 16 -21 99 -3 | 9 16
gfz uuuuu | -24 19 125 -208 -6 | 24 28
grg uuuuu | -4 -6 -33 -88 4 | 2 11
igr xxxxx | 16 -3 8 -18 -3 | -1 13
irf xxxxx | 9 8 6 -2 -4 | 0 14
jpl uuuuu | 9 -28 73 55 2 | 27 31
mit uuuuu | 5 31 18 -28 -6 | 18 23
ngs uuuuu | -35 -25 -47 171 -2 | 10 15
sio xxxxx | -85 55 -38 -285 -24 | 24 28
Table 7.2215.6 GPS week: 2215 Day: 6 MJD: 59755.500
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 -13 8 -53 3 | 9 20
emr uuuuu | -32 -15 -100 67 -14 | 16 25
esa uuuuu | -1 13 -46 -14 0 | 12 20
gfz uuuuu | 12 2 -9 -131 -2 | 26 31
grg uuuuu | -16 9 -84 -87 5 | 5 17
igr xxxxx | 20 -3 -7 -18 9 | 0 15
irf xxxxx | 3 10 7 -8 -2 | 2 17
jpl uuuuu | 15 -26 4 85 18 | 29 34
mit uuuuu | -19 27 40 -10 -2 | 20 26
ngs uuuuu | 17 -9 120 176 -5 | 13 20
sio xxxxx | -174 70 -102 -33 -5 | 23 27
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