[IGSREPORT-29094] Wk 2238 IGS Final Orbits
acc
acc at igs.org
Wed Dec 21 05:29:13 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2238 (Nov 27, 2022 - Dec 03, 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:
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.CLS 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_20223310000_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 | AREQ SCUB
0 | GFZ | 8 16 AREQ ASCG MAYG SEYG SYOG AREQ SEYG
0 | GRG | 16 16 SCUB
1 | ESA | LPGS
1 | GFZ | MAYG LAUT
1 | GRG | KIRI
2 | COD | DAV1 HYDE
2 | ESA | FAIR FAIR
2 | GFZ | 5 25 5 CZTG STK2 POVE
2 | GRG | FAIR KIRI SVTL
3 | COD | DAV1
3 | ESA | CZTG FAIR HOFN CZTG FAIR LPGS STJ3 YEL2
3 | GRG | DAV1 DJIG DYNG FAIR KIRI
4 | COD | ADIS AREQ
4 | ESA | FAIR BAKE FAIR KARR
4 | GFZ | 12 25 12 25 AREQ ASCG MAYG AREQ
4 | GRG | 16 CZTG KIRI CZTG DAV1 KIRI METG
5 | COD | HOB2 KOKB
5 | ESA | CPVG CPVG PIE1
5 | GFZ | KOKB KOKB MKEA PIE1
5 | GRG | PIE1 CPVG GAMB KIRI SCOR
6 | COD | 16 SCUB
6 | ESA | SCUB HYDE SCUB
6 | GFZ | GUAM MAYG WTZR
6 | GRG | KIRI SVTL
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. 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.
7. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.1 -.9 -.0 -29 -7 -1 .07
ESA | 0 | -.7 -.1 -.9 4 -3 7 -.42
GFZ | 0 | -.6 -1.0 .0 -45 -3 1 .14
GRG | 0 | .3 -.6 .5 -12 19 23 -.02
JPL | 0 | 4.0 3.2 7.2 -23 52 -25 .53
MIT | 0 | 4.3 1.3 21.2 -21 -2 18 -.18
NGS | 0 | 6.9 2.9 7.5 -30 4 -4 .05
SIO | 0 | 9.7 8.9 29.9 99 -231 49 -.20
COD | 1 | -.3 -1.0 .1 -26 -9 -8 .04
ESA | 1 | .2 -1.2 -2.0 -4 -9 2 -.40
GFZ | 1 | .4 -1.2 -.4 -39 -9 0 .19
GRG | 1 | .5 -.6 .1 -9 -3 19 -.04
JPL | 1 | 4.4 7.3 12.6 -19 50 -44 .81
MIT | 1 | 2.6 6.2 22.5 5 -11 -8 -.10
NGS | 1 | 2.5 7.2 13.2 -6 39 -35 -.01
SIO | 1 | 5.4 12.4 22.8 161 -170 129 -.06
COD | 2 | -.5 -.9 -.4 -29 -7 -3 .06
ESA | 2 | .3 -.7 -1.8 -3 6 -3 -.36
GFZ | 2 | .2 -.7 -.3 -43 -6 8 .48
GRG | 2 | .2 .2 .4 13 -14 2 .03
JPL | 2 | -.6 4.5 10.2 -12 41 -41 .70
MIT | 2 | 3.9 -.6 17.6 -19 2 13 .27
NGS | 2 | 9.5 10.5 13.3 7 -4 -26 .17
SIO | 2 | 7.1 9.4 21.3 109 -154 58 .31
COD | 3 | -.4 -.6 -.4 -31 -4 -4 .03
ESA | 3 | .3 -1.2 -1.3 -8 6 8 -.13
GFZ | 3 | .5 -.6 -.4 -39 -5 8 .34
GRG | 3 | .6 .2 .2 -17 -5 21 .02
JPL | 3 | 9.9 8.9 7.4 -8 42 -31 .83
MIT | 3 | 5.5 5.0 17.4 -4 -5 2 .06
NGS | 3 | 7.2 11.9 9.0 17 12 -37 .28
SIO | 3 | 12.5 9.0 16.1 97 -153 76 .17
COD | 4 | -.2 -.6 -.0 -35 0 6 .10
ESA | 4 | .9 -.3 -.9 -4 0 -1 -.33
GFZ | 4 | .6 -.3 -.6 -39 -5 15 .21
GRG | 4 | 1.6 -.3 .2 -3 -2 24 .06
JPL | 4 | 9.6 2.4 9.4 0 53 -21 .68
MIT | 4 | 6.2 3.9 14.5 -25 -8 9 .08
NGS | 4 | 10.3 6.6 1.7 12 -20 -4 .20
SIO | 4 | 15.1 11.7 15.9 101 -176 121 .27
COD | 5 | .2 -.3 -.2 -25 -15 9 .06
ESA | 5 | .1 -.4 -1.3 -10 -2 8 -.26
GFZ | 5 | .6 -1.3 -.5 -45 0 20 .33
GRG | 5 | .9 -.3 .5 -18 -1 35 .10
JPL | 5 | 7.0 2.3 11.7 -20 57 -25 .87
MIT | 5 | 4.1 3.7 15.1 5 -11 -3 .19
NGS | 5 | 6.7 9.5 2.1 18 9 -38 .23
SIO | 5 | 10.6 9.9 16.6 77 -158 95 .37
COD | 6 | -.4 .2 -.4 -22 -12 -11 .19
ESA | 6 | .2 -.3 -1.0 1 -6 5 -.50
GFZ | 6 | -.1 -1.2 -.9 -35 -10 12 .18
GRG | 6 | .4 -.2 .5 -13 9 26 .13
JPL | 6 | 6.9 4.5 5.2 -7 49 -49 .52
MIT | 6 | 2.7 1.4 16.6 -15 -11 13 .02
NGS | 6 | 4.6 7.9 5.2 14 6 -27 .06
SIO | 6 | 7.4 7.1 13.0 36 -124 58 .12
8. 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.
9. 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.
The GFZ solution started to show high orbit residuals compared to the other
centres starting from GPS week 2237. The GFZ orbit solution is excluded from
the IGS orbit combinations from GPS week 2237 until TBA.
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 1.2238.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2238.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 2.2238.[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 3.2238.[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 5.2238.0-6). 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 2238 summary. (Nov 27, 2022 - Dec 03, 2022)
Table 1.2238.a GPS week: 2238 MJD: 59910.000-59916.000
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 854| -1 0 2 6 -17 -15 .07 8 8 | -516 -74 5 79
| 0 0 0 7 13 14 .02 | 224 261
esa 149| 0 0 9 10 6 -27 -.02 10 10 | -632 -273 7 93
| 0 0 1 18 22 17 .04 | 340 616
gfz 135| -3 2 2 26 12 -37 .19 25 24 | -53 276 12 90
| 1 1 1 17 22 18 .13 | 123 302
grg 122| 0 -3 -6 12 -2 -34 -.02 9 9 | -143 254 10 127
| 0 0 0 17 20 21 .02 | 66 307
igr n/a| 0 0 0 26 -3 -18 .04 6 5 | 233 -20 12 110
| 0 0 1 20 20 12 .01 | 1085 504
jpl 80| -1 0 -1 2 1 -18 .18 25 25 | -356 -74 79 166
| 2 1 2 14 20 16 .03 | 1052 574
mit 358| 0 1 0 -5 0 5 -.02 6 6 | -14921 175 861 8066
| 0 0 1 16 18 50 .01 | 47924 1030
ngs 283| 0 1 0 3 3 -39 -.02 9 8 | -495 -129 912 1718
| 0 0 3 24 26 17 .01 | 115 142
sio 623| 0 0 -5 -18 9 104 .03 8 8 | --- --- --- ---
| 0 0 0 28 41 41 .01 | --- ---
Table 1.2238.b GPS week : 2238 MJD: 59910.000-59916.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 3 3 4 4 |
2 | 3 4 3 3 3 3 3 |
3 | 4 4 4 4 3 3 4 |
4 | 4 3 3 3 4 4 3 |
5 | 4 3 3 3 3 4 3 |
6 | 4 4 4 4 3 4 3 |
7 | 4 3 4 3 4 3 3 |
8 | 4 3 3 3 3 3 3 |
9 | 4 3 3 3 3 3 4 |
10 | 4 4 4 3 4 3 3 |
11 | 6 6 5 5 5 5 5 |
12 | 4 4 4 5 4 6 5 |
13 | 3 3 3 3 3 3 3 |
14 | 7 7 8 9 7 6 6 |
15 | 3 3 3 3 3 3 3 |
16 | 4 4 4 4 5 5 5 |
17 | 4 4 4 3 3 4 3 |
18 | 5 5 4 4 4 4 4 |
19 | 4 4 4 3 4 4 4 |
20 | 4 4 4 4 5 5 4 |
21 | 4 4 4 4 4 4 4 |
22 | 3 3 3 3 3 3 3 |
23 | 4 4 4 4 4 4 4 |
24 | 3 3 3 3 3 3 3 |
25 | 5 6 5 5 5 5 4 |
26 | 4 4 4 4 4 5 4 |
27 | 4 4 3 3 3 3 3 |
29 | 4 4 4 4 4 4 3 |
30 | 4 3 3 3 3 4 3 |
31 | 4 4 4 3 3 3 3 |
32 | 4 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 2.2238.0 GPS week: 2238 Day: 0 MJD: 59910.000
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 856| -1 0 3 21 -36 -24 .02 9 9 | -516 19 5 80
esa 149| -1 0 9 38 3 -17 .04 11 11 | -1118 247 8 93
gfz 136| -3 2 3 40 38 -39 -.06 29 30 | -42 502 14 104
grg 117| 0 -3 -6 42 7 -57 .00 10 10 | -70 140 14 138
igr n/a| 0 -1 1 47 0 -30 .06 7 6 | 1931 -996 12 123
jpl 80| -1 -1 -5 9 7 -19 .17 25 25 | 453 -619 79 170
mit 358| 0 1 0 -8 14 27 -.02 7 6 | 7974 -454 53 12504
ngs 285| 0 1 0 3 24 -42 -.02 9 8 | -513 15 962 1906
sio 620| 0 0 -5 -77 -41 76 .04 9 9 | --- --- --- ---
Table 2.2238.1 GPS week: 2238 Day: 1 MJD: 59911.000
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 856| -1 0 2 1 -25 -2 .06 8 8 | -513 -155 5 66
esa 150| -1 0 10 7 -26 -9 .02 12 11 | -394 -523 9 93
gfz 138| -5 4 1 28 9 -3 .22 27 24 | 156 -151 15 93
grg 126| 1 -4 -6 7 -14 -24 -.04 9 9 | -133 6 14 112
igr n/a| 0 0 -3 20 -12 1 .04 6 6 | 563 259 14 121
jpl 80| -1 -2 -1 -9 -15 -24 .20 25 25 | -404 813 80 168
mit 358| 1 1 0 -2 11 -61 -.03 7 6 | -123138 -1206 71 1049
ngs 285| 0 1 3 -10 4 -12 -.02 10 9 | -501 -184 745 1595
sio 623| -1 0 -6 -1 42 176 .02 9 9 | --- --- --- ---
Table 2.2238.2 GPS week: 2238 Day: 2 MJD: 59912.000
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 859| 0 0 3 0 -2 -5 .07 7 7 | -577 -60 5 75
esa 149| 0 0 9 2 18 -31 -.03 11 11 | -385 -378 8 100
gfz 137| -4 2 0 15 13 -24 .29 30 30 | -162 410 12 83
grg 125| 0 -3 -6 4 -1 -28 -.01 9 7 | -108 306 11 121
igr n/a| 0 0 -3 20 7 -13 .04 6 5 | 894 -60 13 117
jpl 80| -6 0 1 -7 4 0 .17 26 26 | 466 566 85 177
mit 358| 0 0 0 -9 -2 -9 -.03 6 5 | 10255 57 66 9678
ngs 284| 0 1 3 25 -40 -32 -.01 10 9 | -588 -52 1325 1819
sio 617| 0 0 -6 -12 32 99 .03 8 7 | --- --- --- ---
Table 2.2238.3 GPS week: 2238 Day: 3 MJD: 59913.000
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 857| 0 0 2 2 -14 -6 .06 8 8 | -862 338 5 78
esa 149| 0 0 11 19 12 -20 -.03 10 10 | -660 -215 8 92
gfz 133| -4 2 3 41 15 -37 .22 24 25 | 14 7 11 90
grg 126| 0 -3 -7 16 6 -16 -.02 10 8 | -184 397 10 124
igr n/a| 0 0 0 50 -23 -13 .06 6 6 | 471 -89 13 108
jpl 80| 1 1 -4 17 -4 -18 .17 25 25 | 620 -239 81 164
mit 358| 0 0 0 -17 -19 -17 -.02 6 6 | 2258 80 68 10500
ngs 281| 0 1 0 38 22 -24 -.03 9 7 | -650 23 898 1603
sio 621| 0 0 -5 -31 5 81 .04 7 6 | --- --- --- ---
Table 2.2238.4 GPS week: 2238 Day: 4 MJD: 59914.000
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 854| -1 0 2 9 -8 -40 .08 8 8 | -148 -332 5 78
esa 149| 0 0 10 23 -1 -60 -.06 10 9 | -711 285 7 100
gfz 134| -3 1 3 20 -17 -60 .28 20 18 | -226 712 11 99
grg 120| 0 -3 -5 21 -6 -70 -.03 9 8 | -265 851 8 121
igr n/a| 0 0 0 35 -8 -34 .04 5 5 | -48 -79 11 98
jpl 80| -1 0 0 24 0 -23 .22 24 24 | -12 -742 75 172
mit 358| 0 0 1 -27 -9 72 -.00 6 5 | -1533 339 1117 5805
ngs 283| 1 0 -2 7 10 -55 -.01 8 7 | -287 -86 922 1784
sio 625| 0 0 -6 -8 17 114 .02 9 8 | --- --- --- ---
Table 2.2238.5 GPS week: 2238 Day: 5 MJD: 59915.000
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 851| -1 0 4 2 -29 -5 .09 8 7 | -644 101 5 88
esa 149| 0 -1 10 -2 -9 -14 -.06 9 10 | -985 147 7 88
gfz 133| 0 0 2 43 -11 -46 .27 20 19 | -79 102 12 84
grg 118| 1 -3 -6 6 -38 -12 .00 9 10 | -87 -59 7 143
igr n/a| 0 0 0 18 -24 -13 .04 5 5 | -1173 169 11 105
jpl 80| -1 1 2 -9 -21 2 .20 25 25 | -1727 -155 76 171
mit 358| 0 1 2 3 24 -37 -.01 6 6 | -8 2179 4595 10056
ngs 282| 1 1 -5 -5 -24 -43 -.04 9 8 | -486 -310 780 1722
sio 630| 0 0 -4 -9 61 131 .04 8 7 | --- --- --- ---
Table 2.2238.6 GPS week: 2238 Day: 6 MJD: 59916.000
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 849| 0 0 2 7 -2 -21 .08 9 8 | -354 -430 5 89
esa 149| 0 0 8 -18 45 -39 -.04 9 9 | -174 -1476 6 90
gfz 134| 0 0 2 -4 42 -52 .10 21 20 | -35 351 10 83
grg 127| 0 -3 -5 -12 27 -28 -.03 8 8 | -154 137 7 131
igr n/a| 0 0 0 -8 35 -26 .03 6 5 | -1002 651 13 102
jpl 80| 0 0 -1 -10 41 -48 .14 24 24 | -1893 -143 77 144
mit 358| 0 0 1 24 -23 62 .00 6 5 | -259 233 57 6873
ngs 283| 0 1 -1 -34 29 -62 -.01 8 7 | -440 -314 755 1598
sio 631| 0 1 -4 9 -50 48 .05 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 3.2238.0 GPS week: 2238 Day: 0 MJD: 59910.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jpl mit ngs sio IGS | cod esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 9 9 22 9 6 10 5 8 10 3 | 24 25 32 22 24 23 25 25 33 24
2 | 7 7 22 5 6 13 4 8 7 3 | 31 29 37 32 32 33 31 28 33 30
3 | 6 12 20 9 7 12 9 9 9 4 | 27 31 31 23 26 27 28 24 31 25
4 | 8 7 25 9 7 49 5 10 8 3 | 38 39 51 41 39 49 43 41 52 41
5 | 9 8 21 9 8 11 6 6 9 3 | 32 26 38 33 31 31 31 27 35 29
6 | 10 9 31 10 8 10 5 9 8 3 | 45 43 54 44 43 43 38 41 41 41
7 | 8 11 19 10 5 9 5 8 7 3 | 67 68 70 60 64 67 63 63 65 64
8 | 7 10 26 7 6 11 4 14 10 4 | 24 27 39 23 24 25 25 23 32 24
9 | 9 7 16 10 6 14 5 7 8 3 | 28 31 30 30 29 39 31 30 41 30
10 | 7 10 22 8 6 12 7 7 8 3 | 30 32 33 24 31 33 27 27 31 26
11 | 14 17 35 13 8 59 15 12 8 6 | 48 54 58 56 51 61 46 52 52 49
12E | 13 10 42 9 6 11 5 9 10 4 | 106 109 117 105 108 107 109 105 107 107
13 | 6 6 44 9 7 8 7 9 5 3 | 19 20 36 19 20 23 20 19 25 18
14E | 10 24 46 18 8 51 11 14 11 6 | 76 81 89 72 76 78 80 76 80 76
15 | 7 9 28 8 6 9 5 8 5 3 | 42 47 54 40 43 46 39 42 47 41
16E | 10 13 16 9 8 13 6 8 6 4 | 72 78 77 73 75 74 74 72 79 74
17 | 8 9 21 14 6 10 5 9 10 4 | 28 26 38 26 28 29 28 29 36 27
18 | 9 15 13 11 5 57 10 9 6 4 | 39 45 45 46 41 55 42 43 41 41
19 | 12 7 25 13 8 14 5 11 8 4 | 29 32 42 29 30 31 32 33 37 30
20 | 9 7 29 13 5 10 5 8 10 4 | 26 22 34 27 24 23 22 26 32 23
21 | 10 7 29 10 7 10 6 8 9 3 | 26 24 37 24 27 25 27 29 34 26
22 | 6 6 26 7 5 10 5 8 7 3 | 21 22 31 19 21 22 23 20 31 21
23 | 8 11 22 8 6 60 6 11 8 4 | 40 46 46 46 42 65 40 34 48 41
24 | 8 9 14 8 5 9 3 7 8 3 | 25 26 28 23 24 29 24 23 30 23
25E | 15 16 37 11 13 9 7 10 11 5 | 95 92 106 93 94 87 91 94 90 91
26E | 9 9 60 10 6 15 6 13 10 4 | 33 32 65 35 34 34 32 31 30 30
27 | 6 10 49 8 7 10 5 9 10 3 | 25 28 46 24 26 27 26 23 30 25
29 | 13 6 19 8 7 14 3 8 10 3 | 30 31 31 31 31 31 35 33 37 32
30 | 8 9 20 12 4 9 5 6 7 3 | 33 35 43 31 31 34 30 35 38 32
31 | 9 8 20 8 9 12 6 7 8 3 | 50 54 51 43 46 55 48 49 51 48
32 | 5 10 24 8 5 18 9 8 8 3 | 33 37 39 30 36 43 32 34 41 32
------+---------------------------------------------------+----------------------------------------------------
RMS | 9 11 29 10 7 25 7 9 9 |T 40 41 49 39 40 43 40 39 44 39
WRMS | 9 11 30 10 6 25 6 8 9 |NE 33 34 41 32 33 37 32 32 38 32
MEDI | 9 9 24 9 6 11 5 8 8 |MD 32 32 42 31 31 34 32 33 37 30
Table 3.2238.1 GPS week: 2238 Day: 1 MJD: 59911.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jpl mit ngs sio IGS | cod esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 7 12 22 8 6 10 7 10 10 4 | 22 24 28 20 23 23 19 21 29 20
2 | 7 9 15 6 6 14 6 11 8 3 | 21 18 27 22 20 21 20 20 25 20
3 | 6 14 20 6 4 11 6 6 10 3 | 25 29 27 23 24 25 22 24 34 23
4 | 6 7 21 6 5 52 7 7 8 3 | 31 30 42 33 33 36 34 34 44 33
5 | 6 7 22 8 6 9 7 9 7 3 | 29 23 38 28 27 26 23 24 32 25
6 | 7 9 21 7 6 10 4 12 10 3 | 45 44 52 43 42 43 38 40 47 41
7 | 8 10 18 7 7 8 7 8 5 3 | 40 39 44 37 37 40 36 37 38 37
8 | 8 9 14 6 5 9 5 7 8 3 | 20 25 26 21 21 23 20 22 30 20
9 | 8 9 13 7 5 13 5 8 7 3 | 22 25 24 24 24 33 22 27 34 23
10 | 6 11 24 6 5 11 6 7 9 3 | 26 29 31 25 26 27 22 30 30 24
11 | 10 17 34 12 7 59 10 14 11 5 | 37 39 47 39 37 42 34 36 41 35
12E | 7 12 19 10 4 10 6 8 8 3 | 74 74 78 73 73 71 69 71 75 71
13 | 6 7 39 8 5 9 4 9 6 3 | 17 20 27 18 17 21 15 19 24 16
14E | 8 28 56 18 7 55 12 14 10 7 | 47 52 65 46 46 51 53 49 56 49
15 | 5 7 23 9 5 10 4 9 5 3 | 28 28 37 25 27 30 27 29 37 27
16E | 9 12 17 7 6 11 9 10 9 4 | 53 57 57 54 54 51 49 58 59 53
17 | 8 9 21 9 5 10 5 10 8 3 | 24 21 34 22 22 26 22 21 31 21
18 | 9 16 19 9 6 55 6 11 7 4 | 26 29 30 31 24 34 27 27 32 27
19 | 10 5 25 10 8 14 7 13 8 4 | 22 21 29 20 22 23 22 21 30 20
20 | 7 9 27 11 5 11 6 10 13 4 | 22 19 31 25 19 20 18 21 28 19
21 | 9 12 31 10 6 10 6 10 8 4 | 19 19 31 18 20 20 17 21 28 17
22 | 5 6 22 5 4 10 5 9 8 3 | 16 17 31 15 18 16 12 22 25 15
23 | 8 13 20 8 7 57 4 14 8 4 | 34 36 42 38 32 47 32 29 40 33
24 | 6 8 13 7 5 10 6 11 6 3 | 21 21 27 19 18 27 18 22 25 18
25E | 13 19 41 11 14 --- 10 16 17 6 | 69 70 71 72 69 --- 74 71 77 71
26E | 7 8 61 12 6 12 6 11 11 4 | 28 28 65 29 27 27 29 26 33 27
27 | 7 11 38 8 5 10 5 7 8 3 | 22 26 34 23 22 25 19 22 29 21
29 | 10 8 22 7 5 14 7 13 11 4 | 23 23 24 24 24 25 25 25 29 23
30 | 6 10 11 9 5 8 6 6 5 3 | 26 27 30 28 25 28 23 25 30 24
31 | 7 8 17 8 8 13 7 8 14 4 | 35 36 37 32 29 42 32 35 37 33
32 | 7 10 19 6 5 17 5 8 8 3 | 28 30 36 26 29 37 23 32 33 26
------+---------------------------------------------------+----------------------------------------------------
RMS | 8 12 27 9 6 25 7 10 9 |T 30 31 38 30 30 32 28 31 36 29
WRMS | 8 11 24 9 6 25 6 9 9 |NE 26 26 33 26 25 29 23 26 32 24
MEDI | 7 9 21 8 5 11 6 10 8 |MD 26 28 34 25 25 27 23 26 32 24
Table 3.2238.2 GPS week: 2238 Day: 2 MJD: 59912.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jpl mit ngs sio IGS | cod esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 8 9 22 7 6 11 5 9 7 3 | 29 30 29 28 28 30 28 28 34 28
2 | 7 7 13 6 4 12 4 7 7 2 | 30 27 36 29 29 29 28 27 30 28
3 | 6 13 19 8 5 11 4 7 7 3 | 23 29 28 23 23 25 24 25 28 23
4 | 5 6 15 5 4 51 5 8 6 2 | 22 21 28 23 21 33 26 21 29 23
5 | 6 7 22 9 8 13 7 8 7 3 | 26 22 38 26 26 24 24 26 27 24
6 | 8 11 21 7 4 10 7 12 6 3 | 32 34 38 32 31 34 30 33 36 31
7 | 7 9 16 6 6 11 6 9 8 3 | 55 54 58 53 51 57 54 52 53 53
8 | 5 10 16 5 4 10 3 8 6 2 | 28 30 29 28 28 29 29 26 36 28
9 | 7 7 14 8 4 14 4 9 6 3 | 23 25 28 24 23 34 25 27 30 24
10 | 8 9 20 6 5 12 5 7 9 3 | 25 26 21 22 23 23 23 23 27 22
11 | 12 15 24 10 7 63 12 13 8 5 | 33 38 42 36 34 44 37 39 38 35
12E | 9 10 31 10 6 9 7 8 9 4 | 38 38 49 38 37 41 36 36 39 36
13 | 4 6 31 6 5 10 7 11 7 3 | 24 25 28 24 25 27 24 27 28 24
14E | 9 30 45 23 10 55 13 14 11 7 | 72 77 81 68 70 74 79 73 79 74
15 | 5 8 13 7 5 10 4 10 6 3 | 37 37 39 33 36 39 36 37 39 36
16E | 9 15 34 9 6 13 7 8 8 4 | 35 40 50 40 37 39 34 39 41 36
17 | 6 11 20 9 5 12 6 9 11 3 | 29 28 38 25 28 31 27 28 36 27
18 | 9 14 22 9 6 60 6 12 7 4 | 32 33 35 32 32 42 34 34 36 32
19 | 8 7 26 9 6 14 9 10 7 3 | 27 28 32 24 27 25 26 27 33 25
20 | 7 8 26 10 5 13 7 9 11 4 | 25 24 35 28 25 24 24 28 31 25
21 | 11 7 26 8 7 9 5 12 6 3 | 29 26 32 28 29 27 28 31 35 28
22 | 4 5 43 5 4 10 3 8 6 2 | 27 28 59 26 28 29 26 29 32 27
23 | 7 13 16 8 6 61 4 15 7 4 | 30 35 36 36 31 49 31 23 39 31
24 | 4 9 15 7 5 9 4 6 7 2 | 30 30 33 27 30 34 30 30 31 29
25E | 8 17 99 7 9 19 7 17 13 5 | 58 58 111 57 60 59 56 61 53 56
26E | 5 9 44 12 5 12 6 12 9 4 | 33 34 49 33 32 34 34 33 36 33
27 | 6 10 20 7 3 10 3 10 5 3 | 25 26 24 25 25 26 25 25 31 25
29 | 9 6 21 7 4 14 5 9 10 3 | 35 31 35 33 34 33 34 32 34 33
30 | 5 10 14 9 5 9 5 6 8 3 | 31 31 34 31 29 35 30 28 32 29
31 | 6 10 11 8 7 11 4 8 11 3 | 47 46 48 41 42 51 43 46 48 44
32 | 6 8 20 7 5 20 6 8 5 3 | 21 22 34 18 21 33 18 21 26 19
------+---------------------------------------------------+----------------------------------------------------
RMS | 7 11 30 9 6 26 6 10 8 |T 32 33 40 31 32 35 32 32 36 31
WRMS | 7 11 30 7 5 26 5 9 7 |NE 29 30 35 29 29 33 29 29 33 28
MEDI | 7 9 21 8 5 12 5 9 7 |MD 30 30 35 28 29 33 29 28 34 28
Table 3.2238.3 GPS week: 2238 Day: 3 MJD: 59913.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jpl mit ngs sio IGS | cod esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 6 10 16 7 5 11 5 7 7 3 | 20 22 23 19 20 22 20 21 26 20
2 | 8 7 17 6 5 11 5 11 7 3 | 25 23 35 25 24 26 22 25 30 23
3 | 7 14 20 6 4 9 6 4 10 3 | 20 26 27 18 20 20 20 18 28 19
4 | 7 7 13 5 5 51 6 7 4 2 | 13 14 17 18 14 34 19 17 23 16
5 | 7 9 16 8 7 10 6 5 9 3 | 21 16 29 20 19 21 18 18 25 18
6 | 11 10 21 11 8 13 6 10 5 4 | 53 52 56 46 48 50 49 48 57 49
7 | 7 10 13 7 6 9 6 5 4 3 | 48 50 50 44 47 48 45 45 48 46
8 | 5 9 24 6 4 8 5 7 6 3 | 20 22 23 21 19 23 20 19 28 20
9 | 7 8 13 6 5 16 6 6 3 2 | 14 17 23 14 16 29 17 15 21 15
10 | 5 10 15 6 5 10 5 5 6 3 | 19 23 17 18 20 21 19 20 25 19
11 | 11 17 12 10 6 63 9 9 8 4 | 17 26 26 24 20 35 27 24 29 23
12E | 11 11 41 11 8 9 7 9 10 4 | 40 41 54 40 42 41 39 45 43 40
13 | 4 7 13 6 6 7 6 5 6 2 | 14 13 20 14 14 17 12 13 20 12
14E | 11 23 36 32 9 47 11 24 11 8 | 55 63 69 52 56 61 62 65 66 59
15 | 5 9 10 7 4 7 4 7 7 3 | 33 37 35 32 33 34 33 33 36 33
16E | 8 13 43 8 6 11 6 8 7 3 | 32 34 56 35 34 31 28 32 33 31
17 | 6 8 20 8 7 11 5 6 6 3 | 24 22 39 21 24 26 21 25 29 22
18 | 11 13 21 8 7 55 4 12 6 4 | 21 31 30 26 22 39 26 25 29 24
19 | 9 8 22 9 6 12 7 6 5 3 | 24 24 24 20 23 24 22 23 29 22
20 | 8 9 17 11 6 11 6 11 12 4 | 25 24 29 25 24 25 24 28 31 24
21 | 10 9 12 9 5 11 4 9 7 3 | 21 20 21 20 20 24 22 25 27 21
22 | 5 6 54 6 5 9 5 9 7 2 | 14 15 63 12 14 13 15 14 21 13
23 | 7 11 17 9 6 62 5 11 7 3 | 28 31 27 34 29 52 30 24 36 29
24 | 4 10 15 6 5 9 5 8 4 2 | 22 23 27 19 20 26 19 20 25 20
25E | 12 12 48 15 7 21 11 10 9 5 | 31 33 44 36 32 33 30 32 32 30
26E | 9 9 36 15 6 10 6 11 7 4 | 24 23 28 24 24 23 21 22 25 21
27 | 6 9 11 6 5 11 5 5 5 2 | 20 22 23 20 20 23 19 19 24 19
29 | 11 7 17 7 6 16 6 10 7 3 | 25 21 28 24 25 25 24 26 25 23
30 | 7 10 14 7 5 9 7 6 5 3 | 24 24 27 22 21 27 23 21 28 22
31 | 8 7 12 7 7 11 6 7 7 3 | 43 45 46 36 37 45 39 43 42 40
32 | 6 7 20 7 4 15 5 6 6 2 | 15 16 31 13 15 28 12 14 21 13
------+---------------------------------------------------+----------------------------------------------------
RMS | 8 10 24 10 6 25 6 9 7 |T 25 27 33 25 25 30 25 26 31 25
WRMS | 8 10 25 8 6 25 6 7 6 |NE 23 25 30 23 23 29 23 23 29 23
MEDI | 7 9 17 7 6 11 6 7 7 |MD 24 23 28 22 22 26 22 24 28 22
Table 3.2238.4 GPS week: 2238 Day: 4 MJD: 59914.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jpl mit ngs sio IGS | cod esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 6 10 17 7 4 12 6 8 7 3 | 21 22 20 20 20 26 24 23 27 21
2 | 8 7 17 6 4 11 5 7 8 3 | 22 20 34 19 22 21 23 23 29 21
3 | 6 11 20 6 4 10 6 7 8 3 | 19 22 28 17 18 20 19 20 26 18
4 | 9 6 19 7 5 49 6 8 8 3 | 18 19 26 21 18 33 20 22 27 19
5 | 7 7 12 8 3 10 5 7 7 3 | 20 16 28 19 19 21 19 21 25 19
6 | 8 10 23 6 7 11 5 6 8 3 | 28 27 43 26 28 29 22 27 27 25
7 | 9 8 13 5 4 12 4 7 11 3 | 49 48 49 44 47 51 48 43 49 46
8 | 6 10 29 6 3 10 4 7 7 3 | 23 23 27 21 22 23 25 23 28 23
9 | 7 7 11 5 4 14 4 7 7 2 | 14 15 23 13 16 28 18 18 20 15
10 | 7 11 13 7 5 11 5 5 9 3 | 20 22 22 18 19 20 19 18 24 18
11 | 10 15 12 9 6 62 8 9 11 4 | 26 31 32 31 27 37 31 26 35 28
12E | 10 11 34 13 4 9 6 7 9 4 | 41 43 41 38 42 41 40 40 43 40
13 | 5 6 12 6 4 9 6 8 8 3 | 18 17 29 17 17 20 19 19 24 18
14E | 11 16 21 19 10 41 15 17 20 7 | 90 85 83 92 90 85 95 88 99 91
15 | 6 7 11 8 4 9 5 7 5 3 | 31 34 32 31 31 34 32 30 32 31
16E | 10 14 29 19 3 11 7 9 7 5 | 32 37 47 40 33 34 33 35 36 33
17 | 6 8 19 9 5 11 4 8 8 3 | 23 21 34 21 22 23 24 24 33 22
18 | 10 14 24 8 7 55 5 10 8 4 | 24 30 33 30 24 38 31 28 33 28
19 | 9 7 18 10 7 10 5 12 6 4 | 22 21 23 20 22 20 23 26 31 21
20 | 8 8 17 12 4 13 8 12 12 4 | 19 18 24 19 19 19 23 21 29 19
21 | 10 8 11 9 4 14 6 8 7 3 | 20 17 22 18 20 24 25 21 28 20
22 | 6 5 35 5 3 9 3 5 8 2 | 21 22 47 21 23 24 26 22 28 22
23 | 8 13 18 8 5 57 7 11 9 4 | 28 31 28 30 28 45 30 27 38 29
24 | 4 10 13 6 3 8 3 5 5 2 | 25 25 30 23 23 28 24 21 25 23
25E | 12 13 37 9 6 15 9 10 9 4 | 32 34 37 33 33 27 36 34 34 33
26E | 8 9 29 11 6 11 4 9 13 4 | 29 29 35 27 29 31 33 30 34 30
27 | 4 10 19 5 3 9 4 6 7 2 | 19 21 30 17 19 21 20 18 24 18
29 | 10 7 14 5 5 13 7 8 10 3 | 28 26 32 24 27 27 28 27 31 27
30 | 8 9 16 7 4 11 4 4 11 3 | 25 25 27 21 23 28 26 21 27 23
31 | 7 5 11 7 4 12 4 4 8 2 | 40 43 46 36 39 49 40 40 44 40
32 | 6 8 15 6 5 15 4 6 8 3 | 15 15 27 14 16 28 14 15 21 13
------+---------------------------------------------------+----------------------------------------------------
RMS | 8 10 20 9 5 24 6 8 9 |T 27 27 33 26 26 30 28 27 32 26
WRMS | 8 9 18 8 5 24 5 7 8 |NE 23 24 30 22 23 28 25 24 29 23
MEDI | 8 9 17 7 4 11 5 7 8 |MD 23 23 30 21 23 28 25 23 29 23
Table 3.2238.5 GPS week: 2238 Day: 5 MJD: 59915.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jpl mit ngs sio IGS | cod esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 7 10 19 8 6 17 7 9 6 3 | 20 21 20 18 19 21 19 19 27 18
2 | 7 6 16 6 4 12 5 9 7 3 | 21 20 29 19 21 19 20 22 25 20
3 | 6 13 19 7 4 13 5 7 5 3 | 20 24 29 19 18 20 18 18 25 18
4 | 6 12 27 6 4 49 7 9 6 3 | 30 29 34 32 30 35 36 33 36 31
5 | 6 6 17 7 5 11 7 8 12 3 | 22 17 29 21 20 20 20 20 29 20
6 | 7 11 24 6 7 12 5 8 9 3 | 29 30 44 27 29 31 24 28 36 27
7 | 7 10 16 6 4 11 5 8 8 3 | 44 43 43 39 43 46 39 41 45 41
8 | 6 9 22 6 3 13 5 7 7 3 | 18 22 19 19 19 21 19 18 29 18
9 | 7 9 12 7 5 15 6 8 6 3 | 19 19 28 18 19 29 22 22 27 19
10 | 6 9 10 6 4 12 5 6 7 3 | 21 23 25 20 21 23 21 21 26 20
11 | 10 15 23 10 5 64 7 10 9 4 | 34 38 42 40 35 42 39 36 41 36
12E | 10 7 28 19 5 8 9 9 14 5 | 110 112 114 110 111 111 114 109 114 111
13 | 4 8 15 5 4 8 7 6 5 2 | 14 13 26 12 13 18 12 12 19 11
14E | 15 14 19 16 7 45 10 14 13 6 | 61 67 66 64 63 63 65 64 76 64
15 | 5 9 15 6 5 9 5 7 6 3 | 20 21 20 18 19 23 20 18 25 18
16E | 10 13 28 12 3 10 7 11 7 4 | 67 68 74 61 66 67 69 66 71 66
17 | 8 7 19 10 5 11 5 7 8 3 | 24 20 35 20 23 25 25 24 31 22
18 | 10 12 13 7 6 58 6 8 7 3 | 31 33 34 35 31 41 34 29 35 32
19 | 9 6 17 9 6 13 6 9 7 3 | 23 23 29 20 24 24 26 29 32 23
20 | 6 8 14 13 7 10 6 8 15 4 | 35 33 39 34 34 36 37 34 42 34
21 | 11 8 25 10 5 17 6 7 5 3 | 17 16 33 16 17 19 18 18 26 16
22 | 6 5 16 4 4 10 4 8 8 2 | 15 12 24 14 15 12 15 17 23 14
23 | 8 11 14 7 7 59 6 10 7 3 | 29 33 37 35 30 41 31 28 39 31
24 | 6 9 12 6 5 8 6 5 5 2 | 19 19 22 17 19 24 19 19 22 17
25E | 10 12 18 9 5 15 10 11 7 4 | 36 39 38 37 35 31 36 36 41 36
26E | 7 8 42 12 6 9 8 11 11 4 | 23 23 40 21 23 23 24 24 29 22
27 | 5 8 27 7 4 13 6 6 8 3 | 18 21 39 19 18 24 19 17 24 18
29 | 10 5 14 5 4 14 7 9 8 3 | 19 18 28 18 20 20 19 23 25 18
30 | 7 9 15 8 3 11 5 6 10 3 | 21 21 23 17 19 26 19 18 26 18
31 | 7 6 10 6 4 12 8 8 6 3 | 35 35 37 32 33 41 31 34 38 33
32 | 7 7 14 6 3 17 5 8 6 3 | 29 28 30 26 27 37 28 27 32 27
------+---------------------------------------------------+----------------------------------------------------
RMS | 8 9 20 9 5 25 6 9 8 |T 29 30 36 28 29 32 30 29 36 29
WRMS | 7 10 19 10 5 25 6 8 7 |NE 24 24 30 23 23 27 24 24 30 23
MEDI | 7 9 17 7 5 12 6 8 7 |MD 23 23 33 20 23 25 24 24 29 22
Table 3.2238.6 GPS week: 2238 Day: 6 MJD: 59916.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod esa gfz grg igr jpl mit ngs sio IGS | cod esa gfz grg igr jpl mit ngs sio IGS
------+---------------------------------------------------+----------------------------------------------------
1 | 9 9 16 6 5 12 6 8 8 3 | 20 21 23 21 21 22 19 20 24 20
2 | 7 7 10 6 5 12 4 7 7 2 | 26 22 27 23 25 23 23 22 25 23
3 | 9 13 17 7 4 12 6 8 7 3 | 20 25 27 19 19 20 17 18 20 17
4 | 7 7 29 7 5 49 7 8 6 3 | 38 36 40 40 37 51 40 36 40 37
5 | 7 7 12 8 6 10 5 7 8 3 | 23 18 25 21 22 23 21 22 24 20
6 | 10 9 20 5 6 14 5 7 6 3 | 29 29 38 28 29 31 25 27 32 27
7 | 8 8 16 6 6 12 5 6 6 2 | 63 63 63 56 61 64 58 57 58 59
8 | 6 9 12 6 5 11 5 4 7 2 | 21 23 20 20 22 21 20 22 21 20
9 | 8 7 15 9 6 17 7 9 9 3 | 23 23 28 21 24 32 24 24 28 22
10 | 6 9 16 5 4 13 4 7 8 3 | 22 26 29 21 22 25 20 24 22 21
11 | 13 13 28 9 8 58 6 10 11 4 | 49 53 59 53 48 59 51 50 48 50
12E | 9 8 24 16 9 10 10 6 10 4 | 140 143 139 138 143 145 143 142 145 142
13 | 5 8 19 5 4 8 7 6 6 2 | 15 18 29 14 15 20 18 16 17 15
14E | 14 17 18 12 7 47 6 15 9 5 | 94 98 97 96 96 94 98 97 100 97
15 | 5 8 14 6 3 8 5 6 6 2 | 39 42 37 35 36 42 39 36 35 37
16E | 15 8 13 13 6 15 8 9 12 5 | 84 88 88 81 86 84 84 89 85 85
17 | 9 6 21 9 7 11 4 5 6 3 | 27 24 35 25 27 26 24 27 26 25
18 | 9 11 17 7 6 55 6 9 8 3 | 46 49 50 48 44 59 50 47 46 47
19 | 13 6 20 9 7 13 5 7 9 3 | 29 28 35 26 28 29 28 31 29 27
20 | 8 9 16 11 6 13 5 7 13 4 | 35 34 36 29 34 34 33 32 35 32
21 | 11 8 25 10 6 13 5 9 8 4 | 22 20 37 21 23 23 23 26 26 21
22 | 8 5 18 3 5 9 4 8 7 2 | 20 21 23 21 22 23 23 27 25 22
23 | 9 12 16 7 6 60 5 12 7 4 | 36 42 39 41 37 60 37 33 42 38
24 | 6 9 13 5 4 9 5 7 5 2 | 23 22 25 19 21 27 20 19 21 20
25E | 10 13 19 8 4 12 7 12 8 4 | 53 56 64 55 53 41 55 50 54 53
26E | 7 8 61 12 5 12 5 12 11 4 | 31 32 63 31 31 32 32 31 29 30
27 | 5 9 31 5 5 10 4 5 8 2 | 20 22 41 19 21 20 19 22 19 19
29 | 9 6 17 6 6 16 7 8 7 3 | 22 21 33 21 23 23 24 25 25 22
30 | 7 8 10 7 4 10 6 6 7 3 | 25 27 28 21 24 28 23 23 23 22
31 | 8 6 10 6 4 13 5 7 6 3 | 48 49 49 41 44 54 44 41 46 44
32 | 7 7 13 6 5 15 5 6 6 2 | 33 36 35 30 35 42 31 36 35 32
------+---------------------------------------------------+----------------------------------------------------
RMS | 9 9 21 8 6 24 6 8 8 |T 37 39 43 36 37 41 37 37 38 36
WRMS | 8 9 20 8 5 24 5 7 7 |NE 29 30 35 28 29 33 29 29 30 28
MEDI | 8 8 17 7 5 12 5 7 7 |MD 29 28 36 26 28 31 25 27 29 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 4.2238 GPS week: 2238 MJD: 59910.0-59916.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 9 24 | 13 15 45 | 9 11 33 |
esa | esa 2976 | 17 13 49 | 14 20 49 | 11 19 37 |
gfz | gfz 2975 | 17 18 35 | 19 15 58 | 15 15 40 |
grg | grg 2973 | 9 9 23 | 13 17 42 | 8 9 23 |
igr | igr 2975 | 9 8 24 | 13 15 41 | 9 11 29 |
igs | igs 2962 | 9 8 23 | 13 15 40 | 9 10 27 |
jpl | jpl 2962 | 20 19 46 |U 14 21 51 | 14 16 44 |
mit | mit 2976 | 56 46 106 | 61 40 174 | 52 58 105 |
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 5.2238.0 GPS week: 2238 Day: 0 MJD: 59910.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 15 28 | ---- ---- ---- | 10 14 37 |
esa | esa 2976 | 17 17 48 | ---- ---- ---- | 12 22 38 |
gfz | gfz 2976 | 26 17 38 | ---- ---- ---- | 19 16 55 |
grg | grg 2976 | 11 14 25 | ---- ---- ---- | 8 8 24 |
igr | igr 2976 | 11 12 29 | ---- ---- ---- | 10 14 33 |
igs | igs 2976 | 11 12 25 | ---- ---- ---- | 8 11 28 |
jpl | jpl 2976 | 21 20 41 | ---- ---- ---- | 12 14 42 |
mit | mit 2976 | 12 12 20 | ---- ---- ---- | 12 18 43 |
Table 5.2238.1 GPS week: 2238 Day: 1 MJD: 59911.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 10 25 | ---- ---- ---- | 10 15 42 |
esa | esa 2976 | 18 15 51 | ---- ---- ---- | 12 23 40 |
gfz | gfz 2971 | 21 26 41 | ---- ---- ---- | 14 19 40 |
grg | grg 2959 | 12 11 25 | ---- ---- ---- | 10 12 26 |
igr | igr 2976 | 11 9 26 | ---- ---- ---- | 10 13 37 |
igs | igs 2976 | 11 8 23 | ---- ---- ---- | 9 13 34 |
jpl | jpl 2880 | 22 21 54 | ---- ---- ---- | 15 21 47 |
mit | mit 2976 | 14 8 22 | ---- ---- ---- | 11 21 39 |
Table 5.2238.2 GPS week: 2238 Day: 2 MJD: 59912.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 10 24 | 14 15 37 | 10 13 35 |
esa | esa 2976 | 16 14 48 | 15 18 50 | 11 18 38 |
gfz | gfz 2976 | 18 24 42 | 19 12 49 | 13 20 33 |
grg | grg 2976 | 9 11 22 | 13 15 37 | 8 9 25 |
igr | igr 2973 | 10 10 23 | 15 14 40 | 9 9 28 |
igs | igs 2880 | 10 9 23 | 14 14 37 | 9 12 31 |
jpl | jpl 2976 | 21 21 48 | 13 18 47 | 15 19 43 |
mit | mit 2976 | 13 9 23 | 19 16 43 | 12 15 36 |
Table 5.2238.3 GPS week: 2238 Day: 3 MJD: 59913.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 25 | 13 19 40 | 9 8 29 |
esa | esa 2976 | 17 14 47 | 16 31 43 | 11 17 33 |
gfz | gfz 2976 | 14 17 36 | 20 21 45 | 16 14 35 |
grg | grg 2976 | 9 9 21 | 14 30 40 | 8 7 19 |
igr | igr 2976 | 9 8 23 | 13 24 38 | 9 8 25 |
igs | igs 2976 | 9 8 21 | 13 27 37 | 9 8 24 |
jpl | jpl 2976 | 20 20 42 | 16 33 48 | 13 14 46 |
mit | mit 2976 | 10 13 23 | 18 17 44 | 10 9 24 |
Table 5.2238.4 GPS week: 2238 Day: 4 MJD: 59914.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 9 25 | 10 10 56 | 9 11 29 |
esa | esa 2976 | 16 11 51 | 12 13 58 | 11 20 36 |
gfz | gfz 2976 | 13 11 30 | 16 15 67 | 15 11 40 |
grg | grg 2976 | 8 8 24 | 10 11 42 | 8 11 19 |
igr | igr 2976 | 8 7 25 | 10 8 47 | 9 13 26 |
igs | igs 2976 | 8 7 24 | 10 8 45 | 9 11 23 |
jpl | jpl 2976 | 18 18 45 | 12 17 59 | 13 17 43 |
mit | mit 2976 | 161 179 430 | 108 115 319 | 159 203 365 |
Table 5.2238.5 GPS week: 2238 Day: 5 MJD: 59915.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 9 7 24 | 13 15 50 | 9 7 31 |
esa | esa 2976 | 17 10 49 | 15 16 44 | 10 15 38 |
gfz | gfz 2976 | 15 13 33 | 19 13 68 | 14 7 42 |
grg | grg 2976 | 8 7 24 | 14 15 49 | 8 8 22 |
igr | igr 2976 | 9 7 24 | 13 13 44 | 8 8 26 |
igs | igs 2976 | 8 6 23 | 13 13 45 | 8 7 25 |
jpl | jpl 2976 | 21 16 47 | 14 18 45 | 14 12 47 |
mit | mit 2976 | 171 94 200 | 139 35 413 | 147 124 198 |
Table 5.2238.6 GPS week: 2238 Day: 6 MJD: 59916.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 7 22 | 15 13 42 | 9 10 31 |
esa | esa 2976 | 17 13 50 | 14 21 51 | 11 18 38 |
gfz | gfz 2976 | 13 20 24 | 21 15 61 | 13 15 40 |
grg | grg 2975 | 7 7 20 | 14 13 42 | 8 9 24 |
igr | igr 2976 | 8 6 21 | 13 14 39 | 8 12 25 |
igs | igs 2976 | 8 6 20 | 14 13 38 | 8 10 26 |
jpl | jpl 2976 | 21 19 44 | 14 21 54 | 14 16 39 |
mit | mit 2976 | 9 9 26 | 20 16 49 | 10 14 31 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.2238 GPS week: 2238 MJD: 59910.500-59916.500
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 | 15 0 -21 32 3 | 7 23
| 16 14 65 60 3 | 3
esa uuuuu | -9 -10 -98 -2 -9 | 24 34
| 12 9 75 49 3 | 7
gfz xxxxx | -12 -1 -245 69 6 | 5 30
| 12 17 123 76 16 | 5
grg uuuuu | -8 9 -79 58 2 | 6 22
| 14 11 57 55 3 | 3
igr xxxxx | 3 -27 -71 59 -3 | 0 25
| 17 8 39 40 5 | 5
irf xxxxx | 3 -1 -51 -13 1 | -1 24
| 8 5 31 12 5 | 5
jpl xxxxx | 3 1 41 28 3 | 23 30
| 20 24 76 107 15 | 2
mit uuuuu | 6 -1 113 -99 -6 | 14 25
| 18 18 21 38 2 | 5
ngs uuuuu | -9 -2 -2 68 5 | 11 27
| 29 21 89 50 2 | 3
sio xxxxx | 190 -96 -288 -124 2 | 24 32
| 37 30 88 99 8 | 4
Table 7.2238.0 GPS week: 2238 Day: 0 MJD: 59910.500
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 -1 45 -4 2 | 10 26
esa uuuuu | -9 -6 -256 -72 -14 | 34 43
gfz xxxxx | -17 21 -419 149 -25 | 14 38
grg uuuuu | -16 0 -145 4 4 | 9 26
igr xxxxx | -5 -21 -135 -6 -9 | 7 28
irf xxxxx | 11 -7 -119 -10 -8 | 6 29
jpl xxxxx | -22 12 41 -62 17 | 21 29
mit uuuuu | 3 -1 123 -29 -6 | 20 31
ngs uuuuu | -20 10 95 117 4 | 14 30
sio xxxxx | 234 -90 -420 -234 2 | 30 40
Table 7.2238.1 GPS week: 2238 Day: 1 MJD: 59911.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 7 5 -1 61 7 | 7 23
esa uuuuu | -2 2 -101 -75 -9 | 29 37
gfz xxxxx | -15 1 -273 74 1 | 6 32
grg uuuuu | -26 0 0 -9 -3 | 7 23
igr xxxxx | -2 -27 -40 87 -3 | 3 25
irf xxxxx | 13 2 -36 -17 -3 | 1 25
jpl xxxxx | 3 16 157 -12 10 | 21 28
mit uuuuu | 38 -5 116 -66 -8 | 16 27
ngs uuuuu | -48 2 -130 113 9 | 11 27
sio xxxxx | 221 -146 -152 -53 -13 | 26 34
Table 7.2238.2 GPS week: 2238 Day: 2 MJD: 59912.500
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 -2 -100 10 1 | 10 26
esa uuuuu | -28 -12 -79 37 -11 | 30 38
gfz xxxxx | -5 -22 -104 171 9 | 7 33
grg uuuuu | -18 -4 -15 88 5 | 9 25
igr xxxxx | -12 -31 -62 64 -6 | 5 26
irf xxxxx | -5 6 -39 -7 -2 | 2 26
jpl xxxxx | 40 32 75 242 7 | 26 33
mit uuuuu | 5 32 125 -118 -6 | 18 28
ngs uuuuu | 44 -47 -8 85 5 | 14 31
sio xxxxx | 166 -96 -303 -100 0 | 27 35
Table 7.2238.3 GPS week: 2238 Day: 3 MJD: 59913.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 13 21 -11 22 3 | 9 27
esa uuuuu | -3 -13 -77 25 -9 | 26 38
gfz xxxxx | 1 -26 -98 50 16 | 5 33
grg uuuuu | -8 24 -57 68 2 | 8 25
igr xxxxx | 34 -37 -82 57 -3 | 2 28
irf xxxxx | 4 -3 -23 -24 4 | -1 27
jpl xxxxx | 10 10 47 -82 -5 | 26 33
mit uuuuu | 3 -18 142 -114 -4 | 15 29
ngs uuuuu | -11 -8 -102 77 3 | 13 31
sio xxxxx | 177 -102 -316 -93 5 | 24 34
Table 7.2238.4 GPS week: 2238 Day: 4 MJD: 59914.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 11 -8 70 60 5 | 2 20
esa uuuuu | 7 -28 -104 27 -7 | 17 27
gfz xxxxx | 4 -4 -202 -17 22 | -2 23
grg uuuuu | 0 12 -110 79 4 | 1 18
igr xxxxx | 15 -37 -54 123 -3 | -6 22
irf xxxxx | 5 -7 -41 -33 7 | -8 21
jpl xxxxx | 7 -39 43 45 -8 | 21 29
mit uuuuu | 8 3 85 -143 -10 | 8 20
ngs uuuuu | -29 13 -20 65 5 | 6 22
sio xxxxx | 225 -111 -243 -247 1 | 18 25
Table 7.2238.5 GPS week: 2238 Day: 5 MJD: 59915.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 7 9 -66 132 6 | 5 20
esa uuuuu | -7 -3 -34 13 -7 | 17 27
gfz xxxxx | -27 8 -370 -29 16 | 0 25
grg uuuuu | -4 19 -99 25 0 | 3 18
igr xxxxx | 1 -19 -20 39 -2 | -5 22
irf xxxxx | 2 0 -50 3 6 | -5 20
jpl xxxxx | 0 0 24 44 20 | 22 29
mit uuuuu | 7 -23 87 -109 -4 | 9 21
ngs uuuuu | -7 5 80 -32 2 | 7 23
sio xxxxx | 173 -81 -352 -171 5 | 20 26
Table 7.2238.6 GPS week: 2238 Day: 6 MJD: 59916.500
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 | 39 -24 -85 -57 -1 | 6 20
esa uuuuu | -21 -11 -34 30 -7 | 17 27
gfz xxxxx | -25 14 -248 85 2 | 2 25
grg uuuuu | 16 10 -131 149 6 | 4 18
igr xxxxx | -13 -16 -103 47 7 | -6 22
irf xxxxx | -8 5 -47 -5 1 | -4 20
jpl xxxxx | -18 -23 -99 25 -22 | 25 31
mit uuuuu | -26 5 114 -114 -8 | 9 21
ngs uuuuu | 4 14 67 52 6 | 9 22
sio xxxxx | 136 -46 -230 28 14 | 21 27
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