[IGSREPORT-29470] Wk 2274 IGS Final Orbits
acc
acc at igs.org
Mon Aug 28 04:38:22 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2274 (Aug 06, 2023 - Aug 12, 2023)
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:
IGS0OPSFIN_${yyyy}${doy}0000_01D_15M_ORB.SP3 IGS GPS ephemeris files in SP3
format.
IGS0OPSFIN_${yyyy}${doy}0000_01D_05M_CLK.CLK IGS GPS satellite and station
clocks in clock RINEX format.
IGS0OPSFIN_${yyyy}${doy}0000_01D_01D_CLS.SUM IGS GPS clock combination summary
report.
IGS0OPSFIN_${yyyy}${doy}0000_07D_01D_ERP.ERP Earth Rotation Parameters (ERP)
and their rates as well as
Universal Time (UT1-UTC) and
Length Of Day (LOD) associated
with IGS ephemerides.
IGS0OPSFIN_20232180000_07D_01D_SUM.SUM Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, 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.
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 | 15 DAV1 LHAZ
0 | GFZ | JFNG UNSA
0 | GRG | 13 13 KIRI COCO GAMB KIRI SGOC WIND
1 | COD | JFNG KIRI
1 | ESA | CZTG KITG NNOR
1 | GFZ | JFNG JFNG
1 | GRG | KIRI COCO CZTG KIRI
2 | COD | DJIG PIE1
2 | ESA | WIND
2 | GFZ | GAMB JFNG GAMB
2 | GRG | KIRI GAMB KIRI SVTL
3 | COD | JFNG LHAZ
3 | ESA | NRMD
3 | GFZ | 5 5 JFNG LAUT
3 | GRG | CZTG KIRI LHAZ CZTG GAMB KIRI LHAZ SCUB SVTL
4 | COD | HYDE MATE
4 | ESA | JFNG JFNG
4 | GRG | 17 17 CZTG CZTG KIRI SCUB SVTL
4 | MIT | 2 21
5 | COD | 9 28 SCUB
5 | ESA | JFNG
5 | GFZ | JFNG SCUB SCUB
5 | GRG | 13 13 AREQ KIRI SVTL
6 | ALL | 28
6 | COD | HYDE
6 | ESA | AREQ NRMD
6 | GFZ | 1 32 1 32 OUS2 SYOG OUS2 POHN SCUB
6 | GRG | 21 21 28 COCO JFNG AREQ COCO JFNG KIRI NYA2 ULAB
6 | MIT | 28
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 orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
6 | GFZ | 1
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.
Starting 28-Nov-2022, all IGS products, are based on the IGS realization of
the ITRF2020 reference frame (IGS20). Starting from the same date, the IGS
products are based on the repro3 standards, including long filename formats.
For more information see IGSMAIL #8238, #8256, #8274 and #8282.
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 | .7 -1.2 1.0 8 -12 12 .14
ESA | 0 | .5 -.2 .5 15 -8 14 -.31
GFZ | 0 | .4 -.8 -.3 -17 -13 24 .39
GRG | 0 | 1.2 -.6 -1.6 7 2 38 -.01
JGX | 0 | 5.6 -2.8 12.4 -7 -4 25 -.05
JPL | 0 | 9.1 -1.5 -.2 -2 75 -37 .39
MIT | 0 | 6.7 -2.5 6.1 -12 -2 8 .15
NGS | 0 | 6.4 -1.8 2.0 -21 -15 6 -.03
SIO | 0 | 5.5 -2.4 -3.1 7 90 3 -.22
COD | 1 | .9 -1.2 1.1 -1 -10 6 .02
ESA | 1 | .3 .2 .5 11 -16 11 -.36
GFZ | 1 | .1 -1.2 -.3 -7 -14 32 .37
GRG | 1 | .9 -1.3 -1.0 4 0 31 -.01
JGX | 1 | 4.9 -7.9 14.0 -9 -10 36 -.07
JPL | 1 | .8 -3.7 -2.1 -15 64 -30 .57
MIT | 1 | 4.5 -8.3 9.1 -24 -12 17 .12
NGS | 1 | 1.0 -6.4 3.9 -29 7 9 -.10
SIO | 1 | 2.5 -3.3 -.9 11 41 -17 -.18
COD | 2 | .4 -1.2 1.2 4 -10 2 -.10
ESA | 2 | .3 .2 .6 0 -10 4 -.46
GFZ | 2 | -.2 -1.9 -.6 -14 -21 21 .30
GRG | 2 | .9 -1.3 -1.0 2 0 27 -.03
JGX | 2 | 7.6 -6.5 15.8 -9 -8 32 -.21
JPL | 2 | -.8 -6.3 1.0 -1 63 -34 .55
MIT | 2 | 2.8 -9.4 8.2 -5 4 17 -.03
NGS | 2 | -1.6 -6.4 2.1 -31 18 8 -.09
SIO | 2 | 1.4 -7.9 4.4 -58 -20 -11 -.01
COD | 3 | .5 -1.2 .8 -1 -15 5 -.13
ESA | 3 | .1 .1 .4 11 -7 -4 -.54
GFZ | 3 | -.2 -.9 -.6 -10 -14 19 .35
GRG | 3 | .9 -1.3 -1.1 13 -4 36 -.15
JGX | 3 | 5.0 -.0 9.3 -10 -15 30 -.30
JPL | 3 | 2.2 -7.5 -.0 2 57 -32 .57
MIT | 3 | 2.1 -5.8 10.5 -16 7 -4 -.05
NGS | 3 | -.7 -.7 4.6 -9 14 -2 -.12
SIO | 3 | 4.6 -.3 -6.1 57 -3 -9 -.17
COD | 4 | .2 -.7 .9 2 -9 7 -.15
ESA | 4 | .2 .4 .5 5 -9 2 -.56
GFZ | 4 | -.4 -.6 -.1 -18 -2 19 .34
GRG | 4 | .8 -.8 -.7 -2 -2 18 -.06
JGX | 4 | 4.3 -3.2 9.7 -10 3 18 -.23
JPL | 4 | .4 -2.5 2.5 -13 25 -42 .41
MIT | 4 | 1.3 -5.9 13.2 -13 -1 -5 -.06
NGS | 4 | 7.1 -2.4 5.8 -23 -16 -9 -.18
SIO | 4 | 2.0 -.4 .7 -28 12 -10 .00
COD | 5 | .2 -.6 .6 2 5 10 -.12
ESA | 5 | -.1 .6 .6 -2 -4 -5 -.35
GFZ | 5 | .4 -1.0 -.9 -20 -19 15 .14
GRG | 5 | 1.0 -.7 -.7 2 3 17 -.11
JGX | 5 | 3.4 -1.9 14.9 -22 7 20 -.11
JPL | 5 | 5.3 -3.4 7.2 14 49 -46 .56
MIT | 5 | 1.9 -8.2 14.9 -32 5 -7 -.10
NGS | 5 | 2.2 -3.4 10.2 -24 1 6 -.08
SIO | 5 | 4.9 2.3 -1.0 10 -16 -4 .05
COD | 6 | .6 -.5 .5 -4 5 -1 -.14
ESA | 6 | .8 .2 .6 5 -16 -5 -.47
GFZ | 6 | -.0 -.8 -.6 -25 -16 15 .26
GRG | 6 | .7 -.7 -.8 8 -1 23 .07
JGX | 6 | 5.4 -2.5 11.8 -1 -4 18 -.24
JPL | 6 | 10.6 -5.9 5.7 -38 57 -56 .37
MIT | 6 | 4.0 -2.8 8.5 -20 11 -5 -.03
NGS | 6 | 6.8 -3.5 4.2 -19 -8 -4 -.10
SIO | 6 | 8.3 1.0 -10.2 91 -40 3 -.00
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
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.atx
The JPL solution did not use IGS20/igs20.atx until GPS Week TBA, which caused
their orbit and clock residuals to be higher during that period than for the other
centres; from GPS Week 2238 through TBA, the JPL solution is excluded from the
weekly SINEX combination, as well as from orbit and clock combinations.
Since swithing to IGS20/igs20.atx, SIO orbits suffered from high Y rotations
with respect to the combined orbits, possibly impacting the alignment of the
combined orbits with respect to the IGS20 frame. As a result, SIO orbits are
excluded from the final combinations until the issue is fixed.
Since switching to IGS20/igs20.atx, EMR paused their participation to the IGS
combinations until they complete internal tests. They restarted submitting
products from GPS week 2263. The EMR orbit and clock solutions are excluded
from the final combinations until the IGS assessments are completed. The
EMR solutions are, however, included for comparison statistics only.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the final combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 1.2274.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2274.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 2.2274.[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 3.2274.[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 5.2274.0-6). 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 2274 summary. (Aug 06, 2023 - Aug 12, 2023)
Table 1.2274.a GPS week: 2274 MJD: 60162.000-60168.000
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 856| -1 0 0 6 -10 26 .01 6 6 | -845 142 6 92
| 0 0 1 11 10 28 .01 | 101 109
esa 150| 0 -1 2 4 0 2 -.05 9 9 | -1431 922 5 76
| 0 0 0 8 12 20 .01 | 561 653
gfz 127| -1 0 2 33 2 5 .11 68 10 | -30 102 8 89
| 0 0 1 11 15 23 .03 | 347 544
grg 122| 4 0 -1 5 15 9 .08 9 8 | -175 98 8 128
| 0 0 2 12 7 9 .01 | 239 320
igr n/a| 0 0 0 -3 2 21 .02 4 4 | 2877 -259 10 80
| 0 0 0 5 7 28 .01 | 1307 1120
jgx n/a| 0 0 0 20 -8 -35 -.02 12 12 | -145 98 52 1723
| 0 0 1 14 13 38 .02 | 238 345
jpl n/a| 0 0 3 13 -2 19 .18 24 24 | 793 -292 77 171
| 0 1 2 9 14 17 .03 | 1380 1120
mit 359| 0 0 -5 -37 -23 -57 -.10 9 8 | 7870 -880 842 11602
| 0 0 0 20 46 96 .01 | 14672 1888
ngs 288| 0 0 2 -11 3 10 -.04 10 8 | -849 149 835 1890
| 0 0 1 16 12 28 .02 | 193 275
sio 357| 0 0 -3 -28 -20 11 -.16 10 8 | --- --- --- ---
| 0 0 1 17 15 27 .02 | --- ---
Table 1.2274.b GPS week : 2274 MJD: 60162.000-60168.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 5 4 4 4 4 4 |
2 | 4 5 4 5 4 5 4 |
3 | 4 4 4 4 4 4 4 |
4 | 6 6 7 7 7 7 7 |
5 | 3 3 3 3 3 3 3 |
6 | 4 4 3 3 3 4 3 |
7 | 3 4 3 3 3 3 4 |
8 | 4 5 5 4 4 4 4 |
9 | 4 4 6 6 6 5 5 |
10 | 4 4 4 3 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 3 3 3 3 3 3 3 |
13 | 4 4 5 4 3 4 3 |
14 | 3 3 3 3 4 4 3 |
15 | 4 5 5 4 3 5 4 |
16 | 4 4 3 4 3 3 3 |
17 | 5 4 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 5 4 |
20 | 3 3 3 4 3 3 3 |
21 | 4 4 4 4 4 6 4 |
22 | 6 7 --- --- --- --- --- |
23 | 4 4 4 4 4 4 4 |
24 | 4 4 4 3 4 4 3 |
25 | 3 4 4 4 3 3 3 |
26 | 3 3 4 3 3 3 3 |
27 | 4 4 4 4 4 4 4 |
28 | 4 4 4 4 4 5 5 |
29 | 3 4 3 4 4 4 5 |
30 | 3 4 4 3 3 3 3 |
31 | 4 3 4 4 4 4 3 |
32 | 4 4 7 8 6 7 6 |
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 2.2274.0 GPS week: 2274 Day: 0 MJD: 60162.000
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 862| -2 0 0 29 -11 6 .01 7 7 | -795 87 7 94
esa 150| 0 0 2 7 16 1 -.05 8 8 | -1409 828 5 75
gfz 128| -1 0 2 14 26 -10 .09 7 7 | -132 44 9 112
grg 126| 3 0 0 -15 28 -1 .09 8 8 | -151 23 8 135
igr n/a| 0 0 1 -9 14 0 .03 4 4 | 4456 -383 10 81
jgx n/a| 0 0 2 30 8 -66 -.05 13 13 | -136 49 50 1751
jpl n/a| 0 0 2 12 16 9 .18 24 24 | 2298 -276 76 166
mit 359| 0 1 -5 -22 -103 18 -.11 9 9 | 23789 -4621 5507 15861
ngs 297| 0 0 1 -23 24 -10 -.06 9 8 | -801 101 780 1926
sio 363| 0 0 -2 -44 -12 34 -.16 10 9 | --- --- --- ---
Table 2.2274.1 GPS week: 2274 Day: 1 MJD: 60163.000
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 867| -1 0 -2 1 -7 -18 .03 6 6 | -766 115 6 97
esa 150| 0 0 1 15 3 -17 -.06 9 9 | -1118 390 5 73
gfz 128| 0 0 3 47 -2 0 .09 9 9 | 119 -239 8 91
grg 124| 3 -1 1 -1 19 5 .07 8 8 | -23 -229 10 143
igr n/a| 0 0 0 4 9 -12 .01 4 4 | 4127 -998 10 86
jgx n/a| 0 0 0 40 3 -90 -.02 14 14 | 22 -274 55 1727
jpl n/a| 0 0 0 16 2 2 .20 24 24 | 2149 -913 76 179
mit 359| 0 0 -5 -64 -29 67 -.11 9 9 | -3596 -810 93 13035
ngs 291| -1 1 2 -21 0 -37 -.01 10 9 | -794 152 760 1865
sio 362| -1 1 -2 -24 -32 -9 -.16 10 8 | --- --- --- ---
Table 2.2274.2 GPS week: 2274 Day: 2 MJD: 60164.000
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 865| -1 0 -2 10 -1 12 .00 7 6 | -881 177 6 93
esa 150| 0 0 2 -7 -5 -11 -.04 8 8 | -1467 1443 4 67
gfz 129| -1 0 3 36 -13 -5 .15 11 9 | 148 146 8 85
grg 123| 4 0 0 8 9 9 .08 9 8 | -81 42 9 124
igr n/a| 0 0 0 -2 -4 10 .02 4 3 | 3671 -1209 9 74
jgx n/a| 0 0 0 25 -7 -40 -.04 14 14 | -23 -38 62 1718
jpl n/a| -1 0 1 18 -16 8 .18 24 24 | 1607 -755 74 179
mit 359| 0 0 -5 -9 -11 0 -.11 9 8 | -2501 -560 61 8425
ngs 293| 0 0 0 -35 6 3 -.04 9 8 | -878 171 650 1709
sio 360| 0 0 -2 -52 -12 -35 -.15 10 10 | --- --- --- ---
Table 2.2274.3 GPS week: 2274 Day: 3 MJD: 60165.000
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 861| -1 0 0 -7 -4 31 .02 6 5 | -819 158 6 90
esa 150| -1 -1 3 14 -1 -21 -.03 9 9 | -1319 873 5 70
gfz 129| -2 0 3 44 -4 -22 .08 12 13 | 12 384 10 89
grg 124| 5 0 0 24 19 7 .07 8 8 | -31 -74 9 147
igr n/a| 0 0 0 2 2 3 .01 4 4 | 2562 -1132 11 89
jgx n/a| 0 0 -3 16 -6 -54 -.02 13 13 | 11 -108 48 1675
jpl n/a| 0 0 3 20 7 33 .18 24 24 | 943 -1400 76 170
mit 359| 0 0 -5 -64 -23 -22 -.09 9 8 | 28110 -902 64 16094
ngs 297| -1 0 0 5 6 9 -.06 10 8 | -811 149 803 1670
sio 363| 0 0 -6 -16 -9 -1 -.18 9 8 | --- --- --- ---
Table 2.2274.4 GPS week: 2274 Day: 4 MJD: 60166.000
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 853| -1 1 0 8 -8 38 -.01 6 5 | -743 36 5 87
esa 150| 0 -2 3 -3 0 26 -.04 8 8 | -1559 725 5 85
gfz 129| -1 0 0 27 20 34 .15 10 11 | 418 -500 8 84
grg 119| 4 0 -2 6 13 0 .08 9 8 | -300 146 7 126
igr n/a| 0 0 0 -9 0 37 .02 3 3 | 1348 552 9 75
jgx n/a| 0 0 -2 11 -27 -17 -.02 12 12 | -164 18 48 1705
jpl n/a| -1 -2 6 5 -14 51 .13 23 24 | -765 274 78 151
mit 359| 0 0 -4 -30 -19 -153 -.11 9 8 | 16427 526 51 11882
ngs 286| -1 0 2 -15 -8 27 -.06 9 8 | -625 -184 920 1903
sio 356| -1 0 -3 -23 0 37 -.15 9 7 | --- --- --- ---
Table 2.2274.5 GPS week: 2274 Day: 5 MJD: 60167.000
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 845| -1 0 0 2 -5 57 .00 7 6 | -1044 364 5 89
esa 150| 0 0 2 0 10 25 -.06 9 9 | -2502 2073 6 87
gfz 121| -2 1 2 36 8 41 .11 10 11 | -706 1144 9 84
grg 120| 4 0 -4 5 14 23 .11 10 9 | -661 777 9 122
igr n/a| 0 0 0 -6 -2 63 .04 4 4 | 1107 1881 12 82
jgx n/a| 0 0 0 19 -3 9 -.00 11 11 | -663 797 48 1738
jpl n/a| 0 0 4 24 3 21 .20 25 26 | -1248 1941 80 186
mit 359| 0 0 -5 -36 -30 -185 -.10 9 8 | 1666 1405 67 7598
ngs 279| 0 0 4 0 -12 40 -.05 11 8 | -1252 702 1026 2135
sio 347| -1 0 -3 -1 -31 22 -.13 10 8 | --- --- --- ---
Table 2.2274.6 GPS week: 2274 Day: 6 MJD: 60168.000
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 843| -1 0 0 -2 -34 57 .00 6 6 | -868 63 7 94
esa 150| 0 -1 4 7 -21 12 -.05 9 9 | -645 128 7 78
gfz 128| -2 0 0 29 -14 3 .12 413 9 | -70 -261 9 81
grg 121| 4 0 -3 10 4 22 .07 9 8 | 22 3 7 100
igr n/a| 0 0 1 -2 -3 47 .02 4 4 | 2874 -524 12 76
jgx n/a| 0 0 0 -3 -25 10 -.01 11 11 | -63 242 53 1749
jpl n/a| 0 -2 6 -3 -20 9 .20 25 25 | 570 -919 79 168
mit 359| 0 0 -3 -36 54 -123 -.09 8 7 | -8801 -1199 55 8319
ngs 279| 0 0 3 8 6 39 -.03 10 8 | -788 -43 909 2022
sio 352| 0 1 -3 -39 -42 32 -.17 9 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 3.2274.0 GPS week: 2274 Day: 0 MJD: 60162.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jgx jpl mit ngs sio IGS | cod esa gfz grg igr jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 8 7 7 4 --- 11 10 8 --- 3 | 25 25 318 25 23 --- 28 25 24 --- 23
2 | 6 6 10 10 3 10 11 10 12 9 4 | 26 24 30 27 25 27 28 29 26 28 26
3 | 8 10 6 12 4 10 9 7 9 8 4 | 25 25 23 25 22 21 26 23 19 21 22
4E | 10 19 9 10 3 12 52 12 12 15 5 | 34 42 36 37 31 34 38 35 32 32 34
5 | 5 5 4 5 4 9 9 5 7 7 2 | 31 27 31 31 29 32 35 28 31 27 29
6 | 7 9 10 6 3 7 10 7 10 8 3 | 25 26 31 27 25 27 29 24 23 22 25
7 | 7 6 6 10 3 11 8 9 6 8 3 | 64 62 61 59 61 61 65 60 61 57 61
8 | 8 8 6 10 7 9 13 10 9 11 3 | 26 25 24 21 24 22 24 25 23 24 23
9E | 8 6 6 10 3 15 8 8 9 12 3 | 46 48 51 49 47 47 24 52 50 49 48
10 | 5 9 7 8 3 12 9 8 7 12 3 | 27 27 29 23 25 28 28 28 21 26 25
11 | 8 11 9 6 3 12 57 8 10 8 4 | 23 25 28 26 24 25 30 24 24 24 24
12 | 6 4 5 7 3 22 8 7 7 12 2 | 44 41 42 40 42 51 46 45 41 44 42
13E | 7 7 7 7 4 13 9 9 10 10 3 | 57 61 62 61 59 60 62 62 60 60 60
14 | 7 5 6 7 4 12 52 8 6 9 3 | 30 32 35 34 32 37 41 34 33 35 32
15E | 10 5 5 9 4 12 14 12 12 15 4 | 56 59 59 59 58 57 60 62 59 60 58
16 | 6 4 8 7 3 23 8 12 6 12 3 | 17 17 21 18 17 19 17 22 19 20 18
17E | 10 7 12 8 5 10 11 9 11 8 4 | 26 28 34 26 28 27 26 25 27 23 26
18 | 6 9 6 8 4 12 53 9 11 10 3 | 32 32 33 35 32 33 39 32 33 29 32
19E | 6 7 8 7 3 18 10 9 12 7 3 | 37 34 36 36 36 38 37 36 39 35 35
20 | 9 5 5 5 4 11 11 8 11 12 3 | 20 18 20 20 19 20 24 23 20 21 19
21 | 7 7 9 10 3 9 10 9 13 8 4 | 25 22 27 25 23 22 26 27 23 26 24
X22E | 12 7 13 --- 5 --- 10 8 14 --- 5 | --- --- --- --- --- --- --- --- --- --- 0
23 | 6 10 6 8 3 11 57 6 8 8 3 | 29 33 31 33 31 30 51 30 29 30 30
24 | 6 9 6 7 4 9 10 8 7 10 3 | 25 25 22 25 23 24 29 23 23 22 23
25 | 6 8 6 7 4 11 10 7 8 10 3 | 17 19 20 19 19 18 25 17 15 16 17
26 | 7 6 6 7 3 11 9 8 7 10 3 | 20 21 19 20 20 23 27 19 22 20 19
27E | 7 6 9 9 3 10 11 9 8 11 3 | 60 63 62 64 61 59 61 61 62 59 62
X28 | 8 5 --- 8 3 12 51 7 8 9 3 | 53 54 --- 52 53 19 61 55 54 24 53
29E | 5 7 5 5 3 21 9 10 9 10 3 | 55 54 55 55 54 58 54 52 55 55 54
30 | 7 8 6 7 2 7 8 9 7 9 3 | 23 21 20 19 21 19 27 22 21 18 20
31 | 7 5 7 8 2 11 10 10 11 10 3 | 61 59 58 57 58 58 61 55 55 54 57
32E | 9 6 7 5 4 14 10 9 8 12 3 | 47 49 53 52 48 45 26 53 54 49 51
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 8 7 8 4 13 24 9 9 10 |T 35 35 45 35 34 34 37 35 34 33 34
WRMS | 7 8 7 8 4 13 24 9 8 9 |NE 30 30 43 30 29 29 34 30 29 28 29
MEDI | 7 7 6 7 3 11 10 9 9 10 |MD 29 28 31 31 29 28 29 29 29 27 29
Table 3.2274.1 GPS week: 2274 Day: 1 MJD: 60163.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jgx jpl mit ngs sio IGS | cod esa gfz grg igr jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 9 18 9 4 --- 10 8 9 --- 4 | 20 21 303 19 19 --- 23 19 16 --- 18
2 | 7 8 14 11 3 10 11 9 10 13 4 | 21 18 27 19 19 19 20 19 23 23 19
3 | 6 10 7 10 4 11 13 9 11 9 4 | 21 21 20 22 19 19 24 17 20 17 19
4E | 11 22 7 10 4 14 49 14 13 16 6 | 24 27 24 26 20 24 26 30 23 25 24
5 | 4 6 6 5 4 9 9 6 11 5 2 | 22 21 21 22 21 26 26 19 23 19 21
6 | 6 9 8 6 4 9 9 7 12 9 3 | 19 21 22 21 19 18 22 18 20 16 19
7 | 4 7 8 7 4 12 6 11 8 5 3 | 39 38 40 35 37 38 39 36 37 34 37
8 | 5 9 13 14 5 14 12 11 9 11 4 | 22 23 24 21 21 21 22 20 23 22 19
9E | 7 7 9 9 3 14 9 9 9 7 3 | 33 36 38 36 33 33 24 40 33 36 35
10 | 5 10 8 7 4 13 10 8 8 9 3 | 24 25 26 22 24 27 26 21 23 23 22
11 | 7 9 7 7 4 12 58 9 12 5 3 | 13 16 19 19 14 18 24 16 16 16 15
12 | 6 7 6 7 4 20 9 8 8 10 3 | 22 21 24 22 23 26 27 23 23 23 22
13E | 8 6 9 7 3 11 11 9 11 11 3 | 38 41 43 42 41 41 41 43 40 43 41
14 | 6 5 10 6 3 11 53 8 7 6 3 | 17 19 24 21 18 22 21 20 19 19 18
15E | 8 6 15 9 5 12 11 10 10 10 4 | 39 37 35 39 38 38 39 41 39 38 38
16 | 5 5 7 7 4 24 11 13 9 15 3 | 16 16 18 16 16 18 15 20 20 23 16
17E | 5 7 9 8 3 12 8 8 13 5 3 | 31 31 33 31 31 35 32 29 32 29 30
18 | 7 10 9 8 6 14 54 8 13 11 4 | 17 19 21 22 17 23 23 18 19 20 18
19E | 8 7 11 8 3 18 11 10 14 9 4 | 28 25 28 24 25 27 25 23 26 23 24
20 | 4 6 6 5 5 10 11 8 10 8 3 | 16 17 16 16 14 19 21 15 17 14 15
21 | 5 8 11 10 4 11 11 9 9 17 4 | 19 17 21 17 16 17 19 18 19 23 16
X22E | 10 --- 9 --- 13 --- 71 13 16 --- 7 | --- --- --- --- --- --- --- --- --- --- 0
23 | 6 10 7 8 4 12 57 7 9 7 3 | 21 21 24 23 20 24 31 22 20 23 21
24 | 6 10 7 6 3 10 10 8 7 7 3 | 20 20 15 18 17 17 23 18 17 14 17
25 | 8 9 4 5 3 13 10 7 10 7 3 | 15 19 20 20 17 18 24 14 15 14 16
26 | 5 6 8 6 3 12 9 9 7 8 3 | 19 19 19 20 20 20 25 17 19 17 18
27E | 7 7 8 11 4 15 15 10 10 7 4 | 58 57 57 58 58 65 61 61 60 59 58
X28 | 5 6 --- 9 4 12 50 7 13 9 4 | 43 43 --- 44 42 19 46 45 44 23 43
29E | 6 8 7 5 5 22 10 9 10 8 3 | 40 39 39 42 38 43 39 36 41 40 38
30 | 4 9 10 6 2 8 7 11 10 8 3 | 20 17 19 16 17 18 23 18 17 14 16
31 | 5 6 4 7 2 14 9 10 9 9 3 | 46 43 44 42 44 44 47 44 43 42 43
32E | 6 8 6 6 3 14 8 11 10 11 3 | 33 34 37 35 32 32 24 38 32 33 34
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 9 9 8 4 14 24 9 10 10 |T 26 26 36 26 25 26 28 26 26 25 25
WRMS | 6 9 9 8 4 14 24 9 9 8 |NE 22 22 36 22 21 22 25 21 22 20 21
MEDI | 6 8 8 7 4 12 11 9 10 9 |MD 22 21 24 22 20 23 24 20 23 23 21
Table 3.2274.2 GPS week: 2274 Day: 2 MJD: 60164.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jgx jpl mit ngs sio IGS | cod esa gfz grg igr jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 6 8 11 7 3 --- 9 9 9 --- 3 | 33 35 284 33 34 --- 35 32 32 --- 33
2 | 6 6 11 9 4 13 11 11 10 12 4 | 31 31 34 31 30 36 32 33 32 26 31
3 | 6 10 10 8 3 12 9 8 9 9 3 | 31 32 31 34 30 31 33 30 29 26 30
4E | 12 21 9 13 4 14 52 14 13 16 6 | 44 48 44 43 41 46 46 44 41 40 43
5 | 5 5 5 7 3 9 11 6 6 9 2 | 33 32 36 36 34 37 36 32 34 32 33
6 | 5 8 9 7 3 10 8 7 9 11 3 | 38 39 40 40 37 39 40 38 35 35 38
7 | 5 5 9 9 3 13 7 8 5 10 3 | 51 51 53 49 49 50 52 47 49 46 49
8 | 5 8 9 15 4 11 12 10 10 9 4 | 33 34 33 34 33 33 32 31 34 27 32
9E | 8 8 23 11 3 17 10 11 8 11 5 | 56 55 56 54 54 56 34 54 54 50 54
10 | 4 9 8 7 3 13 10 7 9 9 3 | 33 32 36 31 31 35 33 34 31 32 32
11 | 5 9 7 7 4 12 60 7 10 12 3 | 33 37 37 37 35 39 41 38 36 34 35
12 | 6 5 6 8 3 18 7 7 8 10 3 | 45 44 47 44 45 48 45 47 45 42 45
13E | 16 8 8 9 4 12 10 10 7 11 4 | 62 70 68 71 68 70 71 69 65 66 67
14 | 7 4 8 7 5 11 54 8 9 11 3 | 34 34 36 36 33 38 39 35 33 32 34
15E | 8 8 12 11 5 11 10 14 9 14 4 | 57 58 56 61 57 59 58 66 55 61 58
16 | 5 6 6 8 3 27 9 9 10 10 3 | 29 29 32 29 29 32 29 29 32 24 29
17E | 6 7 12 6 4 14 11 8 9 9 3 | 35 34 38 37 34 36 35 35 34 33 34
18 | 7 9 8 10 4 16 52 8 10 8 4 | 33 35 37 35 33 35 41 37 34 33 34
19E | 6 9 8 6 4 18 11 8 10 10 3 | 31 31 31 31 30 32 32 29 29 25 30
20 | 6 5 6 6 3 12 12 7 10 9 3 | 31 31 33 31 31 34 33 30 32 28 30
21 | 7 7 10 8 4 13 11 7 10 11 3 | 33 32 35 32 33 36 34 32 33 26 32
23 | 6 10 9 8 3 14 53 6 9 6 3 | 27 28 30 30 27 29 37 30 27 27 28
24 | 5 9 6 8 2 9 11 7 11 9 3 | 35 35 34 35 34 35 38 33 34 30 34
25 | 5 9 5 7 3 10 10 10 10 9 3 | 30 30 32 33 31 31 35 33 27 28 30
26 | 6 8 6 7 3 15 9 9 10 9 3 | 28 25 28 28 27 30 33 27 32 22 27
27 | 9 6 7 9 4 11 12 9 11 10 4 | 91 90 89 89 90 87 88 89 92 86 90
X28 | 6 6 --- 8 5 14 49 8 8 9 3 | 37 39 --- 41 38 27 46 41 42 28 39
29E | 4 7 9 5 4 24 11 9 8 8 3 | 25 23 31 27 25 25 27 26 28 23 25
30 | 5 9 8 9 3 8 9 8 7 11 3 | 37 36 37 35 35 34 38 35 34 33 35
31 | 6 7 7 9 4 12 9 10 9 8 3 | 47 45 44 46 46 48 49 44 48 41 45
32E | 11 8 29 9 4 17 9 12 11 17 6 | 52 51 61 51 52 50 33 54 54 54 53
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 8 11 9 4 14 24 9 9 10 |T 39 39 49 40 38 40 40 39 39 36 39
WRMS | 6 8 9 8 3 14 24 8 8 10 |NE 34 34 48 35 34 36 37 34 34 31 34
MEDI | 6 8 8 8 4 13 11 8 9 10 |MD 33 35 36 35 34 36 36 35 34 32 34
Table 3.2274.3 GPS week: 2274 Day: 3 MJD: 60165.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jgx jpl mit ngs sio IGS | cod esa gfz grg igr jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 8 16 8 5 --- 9 8 11 --- 4 | 23 25 285 24 23 --- 26 22 22 --- 22
2 | 4 5 15 11 4 11 10 10 13 10 4 | 24 24 30 25 23 26 24 24 24 23 23
3 | 7 10 7 8 2 9 8 8 10 9 3 | 21 24 22 23 20 21 24 18 19 17 20
4E | 12 20 8 12 5 15 49 15 14 14 6 | 21 32 26 23 20 23 27 24 22 21 22
5 | 4 4 6 6 5 10 11 7 8 8 2 | 27 26 29 29 28 27 31 23 28 24 26
6 | 5 10 8 7 4 10 9 5 9 6 3 | 25 26 28 26 24 23 28 22 22 20 24
7 | 6 9 8 8 4 11 9 8 6 8 3 | 50 50 50 46 48 50 50 46 47 48 48
8 | 4 9 8 12 4 12 11 11 10 7 4 | 23 26 25 22 24 24 25 22 24 21 22
9E | 7 9 28 8 3 15 9 10 12 10 6 | 36 39 41 35 36 36 33 34 35 32 35
10 | 4 9 8 7 6 11 11 9 7 5 3 | 20 23 26 22 21 23 24 19 20 17 20
11 | 6 10 8 7 4 11 57 7 7 6 3 | 15 18 20 21 17 19 26 18 15 17 17
12 | 5 5 6 7 3 18 11 8 6 7 3 | 37 34 32 33 33 39 37 33 33 33 33
13E | 8 6 10 7 4 12 13 8 11 8 3 | 31 33 38 35 32 33 31 34 34 31 33
14 | 4 6 6 6 4 10 51 7 7 6 2 | 20 21 22 22 20 24 28 20 22 22 20
15E | 6 8 11 11 3 13 12 7 12 8 4 | 35 33 31 35 34 36 35 35 36 34 34
16 | 5 5 8 7 3 23 9 9 11 13 3 | 15 18 21 17 18 21 18 19 23 21 17
17E | 6 8 11 7 3 11 11 8 10 12 3 | 24 21 27 25 22 23 23 23 25 26 23
18 | 7 10 9 9 4 11 53 8 8 8 3 | 14 19 20 20 17 19 29 19 15 20 16
19E | 6 9 7 7 4 16 11 7 10 13 3 | 31 30 29 31 30 30 28 27 32 29 29
20 | 6 5 8 7 4 11 11 12 10 6 3 | 22 20 24 20 23 22 23 20 24 19 20
21 | 6 6 11 10 4 10 12 9 14 11 4 | 26 24 29 24 24 25 27 23 24 23 24
23 | 5 10 7 8 4 11 54 6 10 5 3 | 19 25 25 25 22 24 42 22 22 23 22
24 | 4 10 7 7 3 8 11 8 7 6 3 | 27 27 23 25 24 25 29 23 24 22 24
25 | 6 9 6 7 3 10 13 6 10 6 3 | 16 20 18 18 17 17 25 16 19 17 16
26 | 4 6 6 6 3 14 10 7 8 9 3 | 20 21 23 19 20 23 27 20 21 22 20
27 | 6 7 8 10 4 13 13 10 9 5 3 | 37 40 39 39 38 36 39 38 41 37 38
X28 | 6 8 --- 10 5 11 48 7 10 7 4 | 20 24 --- 24 21 25 39 24 22 20 22
29E | 7 7 7 8 4 24 11 10 10 14 3 | 23 22 26 26 24 25 21 24 28 29 23
30 | 4 9 6 6 4 7 9 8 5 8 3 | 25 22 23 23 22 23 25 22 23 22 22
31 | 5 7 6 8 3 13 11 11 10 6 3 | 43 43 44 45 44 47 50 41 40 44 42
32E | 12 11 40 14 4 15 8 10 14 10 8 | 25 28 50 30 27 30 33 29 31 27 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 9 12 8 4 13 24 9 10 9 |T 25 27 37 26 25 27 29 25 26 25 25
WRMS | 5 9 13 8 4 13 24 8 8 8 |NE 24 25 39 25 24 26 29 23 24 23 23
MEDI | 6 8 8 8 4 11 11 8 10 8 |MD 24 25 26 25 23 24 28 23 24 22 23
Table 3.2274.4 GPS week: 2274 Day: 4 MJD: 60166.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jgx jpl mit ngs sio IGS | cod esa gfz grg igr jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 7 7 8 3 --- 9 8 10 --- 3 | 21 22 281 20 19 --- 24 20 17 --- 19
2 | 5 4 12 10 3 10 12 9 12 11 4 | 18 17 23 19 17 19 21 20 19 16 17
3 | 6 9 6 9 3 9 8 8 10 9 3 | 18 20 19 19 17 16 20 16 16 13 16
4E | 10 24 9 13 4 13 52 13 11 13 6 | 25 30 23 23 22 24 29 28 22 24 24
5 | 5 5 6 6 4 11 11 10 10 6 3 | 22 21 25 23 22 21 27 20 26 21 22
6 | 5 8 6 7 3 9 9 6 8 7 3 | 25 24 24 24 22 24 26 24 23 20 23
7 | 5 7 10 8 3 12 8 8 6 6 3 | 42 40 43 40 41 42 42 40 40 39 40
8 | 3 7 10 13 3 9 13 9 10 6 4 | 21 22 21 20 20 19 22 20 20 17 19
9E | 9 7 26 11 5 14 11 12 11 13 6 | 47 48 56 47 49 47 34 52 50 48 48
10 | 5 9 11 9 3 10 10 8 6 4 3 | 17 19 20 16 16 18 20 17 15 14 16
11 | 6 9 7 8 3 9 58 9 9 8 3 | 16 19 22 23 17 20 24 22 15 19 18
12 | 4 4 5 7 3 16 9 7 6 7 2 | 32 31 37 33 32 36 32 34 32 31 32
13E | 6 5 9 5 4 13 11 9 8 7 3 | 38 39 41 41 37 38 39 43 39 36 39
14 | 4 4 10 8 3 8 50 8 11 6 3 | 22 22 29 25 23 26 32 28 22 23 24
15E | 6 7 7 5 3 11 13 7 7 9 3 | 43 43 45 46 43 42 44 48 42 41 44
16 | 4 6 7 7 3 21 9 9 7 13 3 | 15 15 15 13 14 16 14 17 16 18 14
17E | 3 8 10 8 3 12 10 7 10 5 3 | 21 19 21 23 21 21 20 21 23 18 20
18 | 5 9 7 9 3 12 52 9 9 9 3 | 17 20 21 23 20 20 28 23 21 22 19
19E | 3 8 9 9 4 18 11 9 8 6 3 | 23 24 26 27 25 26 24 27 28 25 24
20 | 6 4 6 5 3 10 11 7 11 8 3 | 16 17 20 18 17 18 20 18 18 15 16
21 | 6 5 10 7 3 8 11 8 9 11 3 | 20 18 23 19 18 19 22 20 19 17 18
23 | 5 11 10 9 3 11 52 6 8 5 3 | 15 21 22 22 18 17 33 19 15 18 17
24 | 6 9 8 8 2 8 10 7 9 6 3 | 25 23 22 23 23 21 27 23 23 17 23
25 | 5 8 6 7 3 10 11 7 6 6 3 | 16 18 19 18 17 13 23 19 15 12 16
26 | 3 6 8 8 3 12 9 8 7 9 3 | 14 14 17 16 15 17 23 13 15 12 14
27 | 3 7 11 13 3 10 13 10 9 7 4 | 57 56 55 54 56 55 55 58 55 57 55
X28 | 4 7 --- 9 3 --- 51 7 8 7 3 | 36 39 --- 37 36 --- 57 37 37 25 36
29E | 9 9 7 10 4 20 10 10 11 10 4 | 31 26 32 30 27 29 26 27 32 29 29
30 | 3 7 9 6 3 6 8 8 7 12 3 | 21 21 25 21 21 20 24 22 20 22 20
31 | 6 5 8 9 3 10 10 11 9 8 3 | 41 41 43 41 40 43 42 37 44 39 41
32E | 9 10 20 7 3 12 7 11 13 15 5 | 29 31 34 33 30 30 26 36 29 32 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 8 10 9 3 12 23 9 9 9 |T 25 26 36 27 25 26 29 27 26 24 25
WRMS | 5 8 11 8 3 12 24 8 8 7 |NE 22 22 36 23 22 22 27 23 22 20 21
MEDI | 5 7 8 8 3 11 11 8 9 7 |MD 22 22 23 23 22 21 26 23 22 21 22
Table 3.2274.5 GPS week: 2274 Day: 5 MJD: 60167.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jgx jpl mit ngs sio IGS | cod esa gfz grg igr jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 6 9 --- 8 3 --- 13 6 9 --- 3 | 18 20 --- 19 18 --- 24 14 17 --- 16
2 | 5 6 12 11 4 11 13 10 14 11 4 | 19 18 24 19 19 21 22 17 20 19 17
3 | 4 10 7 9 3 11 9 9 7 11 3 | 18 21 20 19 17 18 22 14 16 14 17
4E | 11 25 13 15 4 8 53 17 12 18 7 | 24 31 21 25 22 23 26 29 25 23 23
5 | 5 4 7 7 3 7 9 7 9 5 3 | 24 21 25 24 23 24 28 20 26 20 22
6 | 6 8 8 8 3 9 10 5 11 6 3 | 19 21 21 22 19 18 23 17 20 15 19
7 | 5 6 8 9 3 11 7 9 5 7 3 | 33 32 35 33 33 34 35 29 31 32 32
8 | 4 8 9 14 5 8 16 11 12 6 4 | 20 22 21 20 21 20 23 17 19 17 18
9E | 9 8 11 10 5 8 --- 10 20 14 5 | 38 42 42 41 40 40 --- 41 44 42 40
10 | 6 9 9 7 3 12 9 8 7 7 3 | 17 22 20 18 18 20 22 14 19 15 17
11 | 8 11 10 8 5 8 59 7 10 6 4 | 13 16 21 21 14 16 20 17 14 16 15
12 | 6 5 5 8 3 14 9 9 8 9 3 | 27 24 27 24 26 27 28 28 27 20 25
13E | 6 6 10 6 4 11 12 10 9 8 3 | 35 37 39 36 36 35 38 40 40 38 37
14 | 5 6 10 8 3 7 53 8 12 9 3 | 19 20 26 21 20 23 20 19 21 20 19
15E | 7 8 13 11 5 8 14 7 14 9 4 | 44 43 44 42 44 43 45 47 44 42 44
16 | 5 6 9 8 4 20 8 9 5 11 3 | 14 14 16 13 13 16 13 13 13 14 13
17E | 8 8 8 9 5 11 9 8 13 9 4 | 32 27 27 29 27 28 29 25 29 28 27
18 | 6 10 8 9 5 11 53 8 9 7 3 | 19 18 21 24 18 23 23 18 15 18 18
19E | 8 9 10 8 5 16 10 9 16 8 4 | 37 35 36 37 38 37 35 33 41 33 35
20 | 6 5 8 5 4 8 10 7 8 8 3 | 17 16 20 18 18 17 21 14 16 15 16
21 | 5 9 9 24 7 9 16 8 16 19 5 | 18 18 21 34 19 19 23 15 19 25 18
23 | 6 10 7 7 3 9 53 6 9 7 3 | 20 22 24 24 21 22 31 20 17 22 20
24 | 6 9 6 7 2 7 8 8 12 9 3 | 21 21 21 20 20 17 25 18 18 15 19
25 | 5 9 6 8 4 9 10 6 8 7 3 | 15 18 16 16 17 13 24 14 17 12 15
26 | 5 7 6 9 3 8 8 8 5 9 3 | 17 18 19 17 18 18 23 14 17 15 16
27 | 5 6 7 10 4 9 14 10 9 6 3 | 45 42 44 46 42 44 43 47 39 42 44
X28 | 8 8 --- 10 4 --- --- 12 12 --- 5 | 38 46 --- 46 43 --- --- 49 45 --- 44
29E | 8 8 9 12 4 18 10 8 10 8 4 | 41 40 38 43 41 42 38 33 43 39 39
30 | 4 8 6 7 2 6 8 8 6 7 3 | 18 20 20 18 18 18 23 16 18 16 17
31 | 7 7 6 10 2 9 10 9 7 10 3 | 35 35 35 36 34 36 37 32 33 33 34
32E | 12 14 29 6 6 11 --- 8 20 14 7 | 34 36 46 34 34 31 --- 41 42 37 36
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 10 10 4 11 25 9 11 10 |T 25 26 27 27 25 25 27 24 25 24 24
WRMS | 6 9 11 9 4 11 26 8 8 8 |NE 20 21 22 23 21 21 24 19 20 18 20
MEDI | 6 8 8 8 4 9 10 8 9 8 |MD 20 22 24 24 21 23 24 19 20 20 19
Table 3.2274.6 GPS week: 2274 Day: 6 MJD: 60168.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jgx jpl mit ngs sio IGS | cod esa gfz grg igr jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 8 2266 7 4 --- 10 6 8 --- 3 | 23 27 9999 24 24 --- 26 22 22 --- 23
2 | 5 6 12 12 3 11 12 7 10 9 4 | 23 22 26 25 21 25 26 23 24 21 22
3 | 5 10 6 8 3 11 11 7 10 13 3 | 21 24 20 22 20 20 24 18 17 20 19
4E | 10 24 10 13 4 11 53 12 16 16 6 | 39 48 41 42 39 41 43 43 39 41 41
5 | 5 4 6 8 4 7 10 6 6 7 2 | 28 25 29 28 26 27 32 24 28 25 26
6 | 7 8 7 7 4 9 11 7 8 7 3 | 27 29 31 29 26 26 31 29 27 25 28
7 | 5 6 10 9 4 10 11 8 7 6 3 | 56 56 58 56 56 56 59 52 55 56 55
8 | 4 7 8 14 4 7 14 7 10 8 4 | 21 21 22 24 20 20 22 18 19 17 19
9E | 5 10 8 12 5 14 --- 12 12 12 4 | 61 61 66 60 60 61 --- 67 59 64 62
10 | 8 9 8 7 4 8 10 7 8 6 3 | 23 23 22 19 19 20 25 19 19 18 20
11 | 7 9 8 8 3 9 57 7 9 11 3 | 17 23 24 25 20 21 30 25 21 23 21
12 | 5 5 5 8 3 16 8 8 10 10 3 | 45 42 45 41 41 48 46 44 40 39 42
13E | 4 7 8 6 4 9 10 8 5 12 3 | 57 59 60 59 58 57 58 61 61 61 59
14 | 5 5 6 7 3 8 50 5 8 6 2 | 24 26 28 27 26 28 39 26 28 25 26
15E | 7 9 8 6 6 8 12 7 11 12 3 | 69 68 69 70 69 67 70 70 70 72 69
16 | 5 5 7 7 4 20 7 9 8 9 3 | 13 14 17 12 13 13 16 15 17 16 13
17 | 6 8 7 10 7 12 12 10 10 9 3 | 55 55 56 55 54 54 55 57 59 49 55
18 | 4 10 7 10 4 11 55 6 10 7 3 | 24 25 27 28 23 26 36 25 24 25 24
19E | 5 9 8 6 5 16 14 7 10 9 3 | 28 26 29 29 27 27 26 26 28 27 27
20 | 6 5 7 6 4 7 12 6 7 9 2 | 18 18 22 18 18 16 24 18 20 17 18
21 | 5 8 10 12 4 8 11 6 9 10 3 | 25 24 28 29 23 24 27 22 24 22 24
23 | 6 10 9 6 3 9 53 6 11 8 3 | 28 32 31 31 29 27 49 28 25 31 29
24 | 5 10 7 7 3 8 9 6 9 9 3 | 29 28 28 28 27 25 33 29 25 25 27
25 | 6 9 5 6 3 6 11 5 8 6 3 | 16 19 17 17 17 13 25 14 14 13 15
26 | 5 7 5 8 4 8 10 8 6 7 3 | 15 18 18 17 16 16 25 15 18 18 16
27 | 5 7 8 12 4 6 14 6 8 7 3 | 52 50 51 51 51 49 52 52 50 50 50
X28 | 11 8 --- 9 5 --- 56 6 15 --- 5 | 58 60 --- 59 58 --- 62 61 60 --- 59
29E | 7 8 15 11 5 19 10 8 10 4 4 | 46 44 44 47 43 46 43 40 47 45 44
30 | 4 8 9 8 3 6 9 5 7 6 3 | 22 22 26 22 22 21 27 22 20 23 21
31 | 5 6 6 10 3 9 9 8 9 10 3 | 57 56 57 58 56 56 58 56 54 56 56
32E | 7 9 17 10 3 9 --- 14 22 12 6 | 53 56 62 55 54 51 --- 55 57 53 55
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 9 413 9 4 11 25 8 10 9 |T 34 35 36 35 34 33 37 34 34 33 34
WRMS | 6 9 9 8 4 11 25 7 8 7 |NE 27 28 28 29 27 26 33 27 27 25 27
MEDI | 5 8 8 8 4 9 11 7 9 9 |MD 28 27 29 29 26 27 32 26 27 25 27
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2274 GPS week: 2274 MJD: 60162.0-60168.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3000 |U 9 8 32 |U 7 8 36 |U 9 12 30 |
esa | esa 2989 | 12 11 32 |U 9 12 44 |U 12 17 36 |
gfz | gfz 2891 |U 12 9 33 |U 7 10 37 | 9 9 30 |
grg | grg 2974 |U 9 10 36 |U 8 12 44 | 10 10 32 |
igr | igr 2999 | 8 8 29 | 7 10 36 | 9 11 29 |
igs | igs 2999 | 8 8 30 | 7 10 35 | 8 10 27 |
jgx | jgx 2838 |U 9 10 34 |U 8 11 36 | 10 11 30 |
jpl | jpl 2934 | 14 13 35 | 11 20 55 | 13 16 36 |
mit | mit 3003 |U 14 16 48 |U 126 161 570 |U 129 108 104 |
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 5.2274.0 GPS week: 2274 Day: 0 MJD: 60162.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 9 32 | 7 7 31 | 11 12 28 |
esa | esa 3072 | 12 10 34 | 9 16 47 | 12 17 30 |
gfz | gfz 2976 | 8 9 33 | 9 14 46 | 10 11 29 |
grg | grg 2975 | 9 8 36 | 11 17 60 | 10 9 34 |
igr | igr 3072 | 8 7 29 | 9 14 41 | 10 11 26 |
igs | igs 3072 | 8 7 30 | 9 15 42 | 9 10 27 |
jgx | jgx 2880 | 9 8 33 | 9 17 48 | 7 9 28 |
jpl | jpl 3072 | 15 10 36 | 13 22 61 | 13 15 33 |
mit | mit 3072 | 16 31 112 | 819 1061 3726 | 497 401 462 |
Table 5.2274.1 GPS week: 2274 Day: 1 MJD: 60163.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3061 | 8 7 34 | 7 7 36 | 10 10 29 |
esa | esa 2976 | 11 8 29 | 8 9 43 | 15 20 34 |
gfz | gfz 2963 | 6 7 33 | 6 7 36 | 10 8 31 |
grg | grg 2976 | 8 8 38 | 7 9 43 | 12 10 36 |
igr | igr 3061 | 7 7 30 | 6 8 32 | 10 10 27 |
igs | igs 3061 | 7 6 32 | 6 8 33 | 10 10 26 |
jgx | jgx 2880 | 7 9 35 | 7 10 33 | 10 11 31 |
jpl | jpl 3072 | 13 10 38 | 11 15 54 | 14 18 37 |
mit | mit 3072 | 12 10 34 | 9 9 40 | 17 12 41 |
Table 5.2274.2 GPS week: 2274 Day: 2 MJD: 60164.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 10 37 | 8 6 40 | 7 16 26 |
esa | esa 2976 | 12 11 34 | 7 9 44 | 9 20 34 |
gfz | gfz 2880 | 8 10 37 | 6 7 39 | 8 10 22 |
grg | grg 2976 | 8 11 42 | 7 10 42 | 9 10 29 |
igr | igr 2976 | 8 9 35 | 6 7 37 | 7 13 23 |
igs | igs 2976 | 8 10 35 | 6 7 36 | 7 12 23 |
jgx | jgx 2880 | 7 14 40 | 7 9 35 | 8 12 27 |
jpl | jpl 2976 | 15 11 38 | 12 21 55 | 13 19 38 |
mit | mit 2976 | 11 11 42 | 12 13 53 | 10 22 33 |
Table 5.2274.3 GPS week: 2274 Day: 3 MJD: 60165.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 8 28 | 8 9 35 | 12 10 42 |
esa | esa 2976 | 13 14 28 | 9 12 45 | 12 18 44 |
gfz | gfz 2880 | 10 11 28 | 7 10 34 | 13 11 44 |
grg | grg 2976 | 8 11 32 | 7 12 37 | 9 7 36 |
igr | igr 2976 | 8 8 24 | 7 10 35 | 9 9 34 |
igs | igs 2976 | 8 8 25 | 7 9 33 | 8 9 34 |
jgx | jgx 2880 | 8 8 29 | 7 13 34 | 14 13 36 |
jpl | jpl 2976 | 14 13 30 | 11 20 52 | 13 21 44 |
mit | mit 2976 | 14 12 31 | 13 10 36 | 13 19 44 |
Table 5.2274.4 GPS week: 2274 Day: 4 MJD: 60166.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 25 | 7 9 37 | 9 15 28 |
esa | esa 2976 | 11 11 30 | 8 13 45 | 12 17 35 |
gfz | gfz 2880 | 8 6 25 | 7 9 41 | 8 11 27 |
grg | grg 2976 | 7 9 31 | 8 11 44 | 14 15 31 |
igr | igr 2976 | 7 7 25 | 7 11 38 | 9 13 24 |
igs | igs 2976 | 7 7 24 | 7 9 37 | 8 13 25 |
jgx | jgx 2784 | 8 8 29 | 7 11 40 | 9 12 25 |
jpl | jpl 2976 | 12 10 34 | 10 22 58 | 13 17 31 |
mit | mit 2976 | 14 12 36 | 12 14 46 | 339 277 80 |
Table 5.2274.5 GPS week: 2274 Day: 5 MJD: 60167.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2965 | 9 9 32 | 6 8 28 | 8 10 30 |
esa | esa 2976 | 9 11 33 | 8 13 34 | 10 13 32 |
gfz | gfz 2784 | 27 12 35 | 6 9 24 | 8 7 31 |
grg | grg 2964 | 10 10 34 | 7 10 28 | 9 8 31 |
igr | igr 2962 | 8 9 28 | 6 9 26 | 7 8 28 |
igs | igs 2964 | 9 8 29 | 6 9 23 | 7 8 27 |
jgx | jgx 2784 | 9 10 34 | 7 8 23 | 9 9 34 |
jpl | jpl 2688 | 13 16 31 | 9 18 43 | 13 14 33 |
mit | mit 2976 | 15 17 41 | 8 9 29 | 13 13 32 |
Table 5.2274.6 GPS week: 2274 Day: 6 MJD: 60168.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2975 | 14 8 39 | 10 10 46 | 10 14 27 |
esa | esa 2976 | 14 12 37 | 12 14 50 | 11 15 39 |
gfz | gfz 2875 | 14 10 37 | 9 12 43 | 9 9 28 |
grg | grg 2975 | 14 10 38 | 10 12 58 | 10 10 30 |
igr | igr 2970 | 13 8 35 | 9 12 44 | 13 14 38 |
igs | igs 2970 | 13 8 35 | 9 12 44 | 9 11 25 |
jgx | jgx 2784 | 14 12 38 | 9 12 42 | 13 12 29 |
jpl | jpl 2784 | 17 23 41 | 14 22 62 | 14 11 39 |
mit | mit 2976 | 16 15 42 | 9 11 60 | 11 11 35 |
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 6.2274 GPS week: 2274 MJD: 60162.500-60168.500
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 -16 125 1 2 | 1 23
| 11 19 41 44 3 | 3
esa uuuuu | 5 -15 76 60 -2 | 10 26
| 4 4 24 36 3 | 3
gfz uuuuu | -11 -37 64 33 0 | 12 27
| 14 8 68 43 4 | 3
grg uuuuu | -28 -4 -3 -177 -5 | 19 32
| 9 8 49 49 3 | 4
igr xxxxx | -4 -2 62 57 -2 | 2 25
| 12 7 25 31 5 | 3
irf xxxxx | -7 12 -77 -30 -2 | 1 24
| 3 9 22 18 7 | 4
jgx xxxxx | -2 -25 64 8 2 | 17 30
| 7 12 44 64 3 | 3
mit uuuuu | 4 56 -289 -34 4 | 33 40
| 10 17 33 66 5 | 3
ngs uuuuu | 25 25 -50 133 1 | 14 28
| 17 32 98 112 4 | 4
sio xxxxx | -33 11 22 -45 -7 | 28 36
| 54 65 53 69 9 | 7
Table 7.2274.0 GPS week: 2274 Day: 0 MJD: 60162.500
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 -47 121 -54 4 | 4 18
esa uuuuu | 5 -17 102 18 3 | 13 22
gfz uuuuu | -12 -29 133 86 -2 | 15 24
grg uuuuu | -16 6 -38 -140 -4 | 23 30
igr xxxxx | 8 4 50 92 1 | 4 22
irf xxxxx | -6 23 -76 -10 -11 | 7 17
jgx xxxxx | 4 -38 3 -28 -2 | 20 27
mit uuuuu | -10 71 -252 94 -1 | 36 40
ngs uuuuu | 16 48 -176 -4 -6 | 20 26
sio xxxxx | -122 33 92 17 -9 | 39 40
Table 7.2274.1 GPS week: 2274 Day: 1 MJD: 60163.500
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 -15 166 64 5 | 3 19
esa uuuuu | 6 -18 59 43 -2 | 12 22
gfz uuuuu | 0 -46 58 -48 -3 | 14 24
grg uuuuu | -29 -5 42 -91 -3 | 22 30
igr xxxxx | -13 -1 36 50 5 | 3 22
irf xxxxx | -11 12 -80 -15 -7 | 5 19
jgx xxxxx | -15 -35 60 22 2 | 19 27
mit uuuuu | 8 54 -288 -4 0 | 35 39
ngs uuuuu | 37 50 -179 20 -2 | 18 26
sio xxxxx | -75 57 -49 -172 -9 | 36 39
Table 7.2274.2 GPS week: 2274 Day: 2 MJD: 60164.500
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 -30 169 -5 1 | -1 24
esa uuuuu | 6 -8 59 112 -2 | 8 26
gfz uuuuu | 6 -37 0 27 5 | 10 28
grg uuuuu | -33 -8 12 -227 -8 | 18 32
igr xxxxx | 0 -7 65 44 3 | 0 26
irf xxxxx | -9 14 -81 -52 -5 | 0 26
jgx xxxxx | -5 -37 88 26 6 | 15 29
mit uuuuu | 9 31 -248 -71 -2 | 31 39
ngs uuuuu | 27 66 -81 177 3 | 12 28
sio xxxxx | 4 98 47 -28 -25 | 30 38
Table 7.2274.3 GPS week: 2274 Day: 3 MJD: 60165.500
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 7 113 48 2 | 5 24
esa uuuuu | 7 -18 69 61 -2 | 13 28
gfz uuuuu | -3 -38 -34 10 -1 | 15 30
grg uuuuu | -24 -16 71 -185 -9 | 22 34
igr xxxxx | -5 -12 101 18 -3 | 6 25
irf xxxxx | -10 -5 -89 -32 -4 | 4 26
jgx xxxxx | -5 -17 108 -49 6 | 20 33
mit uuuuu | -4 44 -286 -17 2 | 35 43
ngs uuuuu | 31 16 -22 83 7 | 16 30
sio xxxxx | -20 -79 65 -92 -7 | 30 38
Table 7.2274.4 GPS week: 2274 Day: 4 MJD: 60166.500
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 -17 78 18 -4 | 2 24
esa uuuuu | 9 -11 87 28 -4 | 11 28
gfz uuuuu | -32 -43 103 56 4 | 13 30
grg uuuuu | -21 4 -42 -172 -3 | 19 33
igr xxxxx | 0 2 66 50 -7 | 4 26
irf xxxxx | -4 20 -101 -38 3 | 1 27
jgx xxxxx | 4 -12 54 -77 2 | 18 32
mit uuuuu | 0 61 -343 -70 9 | 33 41
ngs uuuuu | 34 22 54 144 3 | 13 29
sio xxxxx | -53 41 38 -18 2 | 25 35
Table 7.2274.5 GPS week: 2274 Day: 5 MJD: 60167.500
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 -16 70 -24 3 | -2 25
esa uuuuu | -3 -16 109 56 -7 | 6 27
gfz uuuuu | -27 -45 147 49 -6 | 10 29
grg uuuuu | -28 2 -64 -233 -4 | 14 31
igr xxxxx | 9 7 31 107 -5 | -2 26
irf xxxxx | -5 17 -84 -52 8 | -4 26
jgx xxxxx | 3 -24 15 55 2 | 14 30
mit uuuuu | 6 83 -313 -104 12 | 29 37
ngs uuuuu | 40 -9 29 319 4 | 9 27
sio xxxxx | -2 -7 -32 -48 2 | 21 32
Table 7.2274.6 GPS week: 2274 Day: 6 MJD: 60168.500
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 4 155 -40 3 | -2 25
esa uuuuu | 7 -17 44 105 0 | 5 27
gfz uuuuu | -11 -24 38 50 -1 | 9 29
grg uuuuu | -43 -12 0 -192 -6 | 13 30
igr xxxxx | -25 -5 84 42 -7 | -2 26
irf xxxxx | -4 6 -30 -12 3 | -4 26
jgx xxxxx | -2 -10 119 108 -2 | 14 30
mit uuuuu | 21 49 -291 -66 5 | 30 38
ngs uuuuu | -10 -19 27 196 -1 | 10 28
sio xxxxx | 36 -65 -8 30 -1 | 19 30
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