[IGSREPORT-29393] Wk 2267 IGS Final Orbits
acc
acc at igs.org
Sun Jul 9 22:57:05 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2267 (Jun 18, 2023 - Jun 24, 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_20231690000_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 | DARW GAMB OUS2
0 | ESA | AREQ MAW1 NNOR
0 | GFZ | GAMB AREQ GAMB LAUT
0 | GRG | KIRI CZTG DAV1 KIRI SVTL ULAB WIND
1 | COD | DAV1
1 | GFZ | AREQ IRKJ LAUT
1 | GRG | DAV1 KIRI AREQ DAV1 KIRI KITG SGOC
2 | COD | 23 DAV1 VOIM
2 | ESA | AREQ NRMD
2 | GFZ | POHN
2 | GRG | 8 21 8 21 KIRI KIRI SCUB
2 | MIT | 16
3 | COD | HYDE LHAZ
3 | ESA | AREQ
3 | GFZ | JFNG SUTH TUVA
3 | GRG | CZTG
3 | JPL | TIDB
4 | COD | 3 WIND
4 | ESA | DAV1 DAV1 DYNG NRMD SUTH
4 | GFZ | 3 10 3
4 | GRG | CZTG GAMB KIRI LHAZ SCUB CZTG GAMB KIRI LHAZ MAW1
4 | GRG | SCUB SVTL
5 | GFZ | LAUT
5 | GRG | DAV1 DAV1 SVTL
6 | COD | CPVG WTZR
6 | ESA | AREQ
6 | GFZ | LAUT
6 | GRG | KIRI HYDE KIRI TASH
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
----+--------+---------------
2 | GRG | 8
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G08 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
8. 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.
9. 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 | .6 -.2 .6 5 -6 -2 .07
ESA | 0 | 1.0 .0 .1 9 -27 16 -.13
GFZ | 0 | .6 -.8 -.3 -17 -7 24 .49
GRG | 0 | .8 -1.1 -1.2 -2 -9 16 .22
JPL | 0 | 7.6 -5.0 -7.2 7 55 -42 .72
MIT | 0 | -.8 -9.3 5.6 -6 -13 0 .24
NGS | 0 | 4.8 -5.7 7.0 -42 -2 21 .22
SIO | 0 | .9 -3.8 -10.2 -32 -25 -3 .25
COD | 1 | .1 -.1 -.1 9 -6 -8 .05
ESA | 1 | .6 .4 -.6 17 -8 4 -.22
GFZ | 1 | .4 -.4 -1.2 -11 -16 19 .26
GRG | 1 | .5 -1.6 -1.2 5 -13 14 .09
JPL | 1 | 11.6 -2.6 -.6 9 56 -37 .60
MIT | 1 | .8 -5.7 5.2 -13 -2 -5 .20
NGS | 1 | 6.3 -2.9 -3.0 -3 -27 19 .26
SIO | 1 | 1.8 1.8 -3.9 -32 1 -15 .07
COD | 2 | .4 -.3 -.4 12 -2 -16 .05
ESA | 2 | .5 1.2 -.1 12 -15 12 -.17
GFZ | 2 | .3 -.3 -1.4 -17 -9 6 .46
GRG | 2 | .2 -1.6 -1.1 6 4 17 .16
JPL | 2 | 8.2 -8.8 -3.5 4 35 -28 .72
MIT | 2 | 1.8 -6.5 8.3 -20 -1 -9 .47
NGS | 2 | .0 -6.1 -4.2 -21 -9 13 .34
SIO | 2 | -5.7 -10.9 -4.5 -83 -50 43 .13
COD | 3 | .3 .1 .4 11 -6 -10 .09
ESA | 3 | .9 .4 .1 5 -8 10 -.53
GFZ | 3 | -.2 -.7 -.3 -27 -9 5 .55
GRG | 3 | 1.3 -1.6 -1.0 1 5 19 -.03
JPL | 3 | 6.6 -5.2 -1.8 -4 60 -13 .83
MIT | 3 | 3.6 -8.0 10.0 -12 7 4 .38
NGS | 3 | 5.5 -2.9 3.4 -26 -13 12 .35
SIO | 3 | 1.7 -3.0 .3 -90 76 11 .14
COD | 4 | .3 .1 .3 -1 -3 -6 .06
ESA | 4 | .7 .5 .2 5 -15 12 -.25
GFZ | 4 | .1 -.8 -.6 -18 -20 21 .50
GRG | 4 | 1.2 -1.3 -.7 -2 5 15 .03
JPL | 4 | 6.0 -9.6 -7.3 -7 38 -33 .93
MIT | 4 | .8 -3.2 6.2 -12 -3 -1 .35
NGS | 4 | 6.8 -4.3 1.8 -25 -14 21 .30
SIO | 4 | .6 1.7 -6.1 34 16 37 .41
COD | 5 | .3 .1 .4 -3 -7 -7 .03
ESA | 5 | .3 .5 -.2 14 -10 -3 -.16
GFZ | 5 | -.1 -.5 -.8 -17 -14 11 .62
GRG | 5 | .6 -1.5 -1.7 -6 0 18 .22
JPL | 5 | 3.3 -4.3 -8.1 2 46 -26 .91
MIT | 5 | -1.3 -9.5 8.5 -5 -9 -18 .43
NGS | 5 | 8.0 -2.3 2.3 -19 -21 18 .39
SIO | 5 | 2.0 -2.8 -4.3 -70 -15 22 .33
COD | 6 | .5 .2 .8 -5 -8 -5 .02
ESA | 6 | .8 .3 -.0 11 -21 5 -.31
GFZ | 6 | -.5 -1.0 -.6 -15 -24 12 .48
GRG | 6 | .9 -1.4 -1.0 -10 -2 10 .15
JPL | 6 | 12.3 -2.7 -6.4 -7 42 -34 .65
MIT | 6 | 5.8 -6.0 7.4 -8 4 10 .39
NGS | 6 | 5.3 -3.2 -5.9 -2 -18 11 .26
SIO | 6 | 2.3 4.5 -6.6 19 30 -7 .27
10. 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.
11. 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.
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 1.2267.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2267.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 2.2267.[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 3.2267.[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 5.2267.0-6). 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 2267 summary. (Jun 18, 2023 - Jun 24, 2023)
Table 1.2267.a GPS week: 2267 MJD: 60113.000-60119.000
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 858| 0 0 0 7 -10 11 -.01 7 6 | -811 186 5 93
| 0 0 0 6 7 13 .01 | 127 140
esa 150| 0 0 5 10 -2 8 -.04 9 9 | -1671 1140 4 77
| 0 0 0 12 13 13 .02 | 323 544
gfz 126| -1 -1 0 19 -1 14 .08 10 10 | 36 97 9 83
| 0 0 1 14 12 13 .02 | 338 650
grg 122| 5 0 3 -7 22 0 .04 19 10 | -83 -34 9 133
| 0 0 1 14 14 9 .03 | 232 397
igr n/a| 0 0 1 -6 9 24 .03 4 4 | 3595 -249 10 72
| 0 0 0 8 10 9 .01 | 1177 1203
jpl n/a| 0 -1 -2 5 5 28 .17 24 24 | -1137 -267 74 155
| 1 2 1 12 13 15 .03 | 1182 1042
mit 360| 0 0 -7 -27 -6 -38 .01 8 7 | 6591 -30 107 12565
| 0 0 1 26 23 27 .01 | 7164 678
ngs 298| 0 0 0 -5 7 11 -.07 12 9 | -894 241 774 1675
| 1 0 3 15 13 21 .04 | 192 237
sio 360| 0 0 -2 -23 -16 7 -.01 11 9 | --- --- --- ---
| 1 1 1 22 11 35 .02 | --- ---
Table 1.2267.b GPS week : 2267 MJD: 60113.000-60119.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 3 3 3 3 3 3 |
2 | 4 4 4 4 4 4 4 |
3 | 6 6 6 7 6 7 6 |
4 | 3 3 3 3 3 3 3 |
5 | 4 5 4 5 4 4 4 |
6 | 3 3 3 3 3 3 3 |
7 | 3 3 3 3 2 3 3 |
8 | 4 4 22 4 4 4 4 |
9 | 3 3 3 3 2 3 3 |
10 | 5 6 6 6 6 6 7 |
11 | 4 4 4 4 3 4 4 |
12 | 4 4 4 5 4 4 4 |
13 | 3 3 3 3 3 3 3 |
14 | 5 5 5 5 4 5 4 |
15 | 4 3 4 3 3 4 4 |
16 | 5 5 5 5 5 4 4 |
17 | 4 4 4 4 4 4 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 4 4 4 4 |
20 | 4 4 3 4 3 4 5 |
21 | 4 4 4 4 4 4 4 |
22 | 4 4 4 4 4 4 4 |
23 | 7 8 10 10 8 7 6 |
24 | 5 3 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 4 4 3 4 4 4 |
28 | 4 3 3 4 4 3 3 |
29 | 3 4 4 4 3 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 4 4 4 4 4 4 |
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 2.2267.0 GPS week: 2267 Day: 0 MJD: 60113.000
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 863| 0 0 -1 -1 -2 -1 -.01 6 6 | -784 351 5 94
esa 150| 0 0 4 16 -3 -3 -.07 9 8 | -1736 1845 4 68
gfz 125| 0 0 0 33 0 19 .08 10 11 | 100 -243 9 79
grg 125| 4 0 2 4 30 9 .08 9 8 | -53 -158 9 127
igr n/a| 0 0 1 3 19 8 .03 4 4 | 3050 1473 10 81
jpl n/a| 0 1 -4 14 17 16 .17 24 24 | -1302 1277 73 158
mit 360| 0 0 -9 -43 -11 -2 -.00 8 8 | 8257 844 60 11595
ngs 301| -1 -1 4 -15 -3 -32 -.04 11 10 | -786 352 895 1603
sio 359| 0 0 -4 -23 -30 -34 -.02 10 9 | --- --- --- ---
Table 2.2267.1 GPS week: 2267 Day: 1 MJD: 60114.000
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 860| -1 0 0 6 -12 -3 -.02 6 6 | -697 82 5 101
esa 150| 0 0 6 9 10 -5 -.06 9 8 | -1093 760 5 74
gfz 126| -1 -2 1 24 0 11 .10 11 11 | -130 647 9 92
grg 121| 4 0 2 -11 18 6 .07 9 8 | -8 43 8 137
igr n/a| 0 0 2 -17 15 26 .04 3 3 | 4676 30 11 69
jpl n/a| -1 0 0 6 11 34 .14 23 24 | 58 -132 73 161
mit 360| 0 1 -7 -11 -22 -19 .01 8 7 | 14272 -56 178 14839
ngs 300| 0 0 -4 -27 12 14 -.08 11 9 | -809 122 914 1840
sio 360| 0 0 -3 -15 -22 -40 -.03 10 7 | --- --- --- ---
Table 2.2267.2 GPS week: 2267 Day: 2 MJD: 60115.000
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 860| 0 0 0 0 -3 18 -.00 9 5 | -878 151 5 92
esa 150| 0 0 5 27 -21 5 -.06 12 8 | -1829 1559 5 77
gfz 126| -2 -2 2 25 -21 -4 .05 13 10 | 11 690 10 92
grg 121| 5 0 1 9 -6 8 .07 73 9 | -231 400 9 135
igr n/a| 0 0 1 2 -4 19 .01 7 4 | 4496 872 10 75
jpl n/a| -1 -4 -2 20 -21 28 .13 27 27 | -299 800 76 154
mit 360| 0 0 -6 -66 39 -50 .02 11 7 | 1132 850 210 15414
ngs 295| -2 0 0 2 8 32 -.13 17 11 | -894 134 879 1712
sio 362| -4 -2 -3 -41 -24 35 .01 20 11 | --- --- --- ---
Table 2.2267.3 GPS week: 2267 Day: 3 MJD: 60116.000
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 1 16 -23 13 -.03 6 6 | -1054 409 5 88
esa 150| 0 0 4 -9 19 14 -.04 9 9 | -1447 316 5 76
gfz 128| -1 0 -3 -6 22 12 .09 11 12 | 653 -1110 10 86
grg 120| 5 0 2 -20 31 -3 .04 11 10 | 301 -680 9 145
igr n/a| 0 0 0 -7 14 28 .02 4 4 | 5210 -2101 11 77
jpl n/a| 0 -1 -2 -8 19 46 .19 24 25 | 275 -1797 76 160
mit 360| 0 0 -5 -7 -36 -46 .01 9 7 | 6743 -985 108 14028
ngs 298| 0 0 1 13 9 6 -.02 13 10 | -895 130 978 1909
sio 362| 0 0 0 -42 -25 23 -.03 11 10 | --- --- --- ---
Table 2.2267.4 GPS week: 2267 Day: 4 MJD: 60117.000
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| 0 0 1 9 -9 28 -.02 6 6 | -672 31 6 97
esa 150| 0 0 5 20 -6 35 -.04 9 9 | -2100 1376 5 80
gfz 123| 0 0 -1 31 -1 37 .07 9 8 | -456 494 9 80
grg 122| 5 1 4 5 30 6 .05 10 10 | -360 26 10 130
igr n/a| 0 0 1 1 4 37 .02 4 4 | 2929 -459 10 68
jpl n/a| 0 -4 -3 6 0 48 .19 24 24 | -1757 -426 76 154
mit 360| 0 0 -6 -50 4 -87 .01 7 6 | 2226 -210 61 10065
ngs 294| 0 0 1 8 -15 15 -.04 10 9 | -1315 740 585 1706
sio 354| 0 1 -1 17 -1 44 .01 9 8 | --- --- --- ---
Table 2.2267.5 GPS week: 2267 Day: 5 MJD: 60118.000
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 855| -1 0 0 8 -7 24 -.01 6 6 | -806 124 5 92
esa 150| 0 0 4 5 -6 5 -.03 9 9 | -1846 1392 5 91
gfz 128| -1 -1 0 22 -5 3 .10 9 8 | -90 384 10 85
grg 123| 4 1 4 -24 16 -7 -.00 11 10 | -305 450 10 125
igr n/a| 0 1 1 -13 0 23 .03 4 3 | 2676 -361 10 67
jpl n/a| 1 1 -2 11 5 14 .18 24 24 | -2081 -622 76 149
mit 360| 0 0 -6 -18 -10 -44 .00 8 7 | 16687 -111 71 13360
ngs 300| 0 0 0 -1 25 32 -.09 11 9 | -801 140 620 1425
sio 360| 0 0 0 -45 -3 34 -.03 9 7 | --- --- --- ---
Table 2.2267.6 GPS week: 2267 Day: 6 MJD: 60119.000
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 -1 12 -16 -1 -.02 6 6 | -786 155 6 87
esa 150| 0 0 6 0 -7 7 -.01 9 8 | -1648 732 4 75
gfz 126| 0 -1 0 7 -1 21 .06 9 8 | 170 -178 9 71
grg 123| 4 1 6 -18 36 -13 -.01 11 11 | 70 -323 11 133
igr n/a| 0 0 1 -15 20 25 .04 4 4 | 2131 -1201 11 69
jpl n/a| 0 -1 -2 -13 1 8 .21 23 24 | -2858 -969 74 149
mit 360| -1 0 -6 4 -8 -19 .01 8 7 | -3178 -548 61 8656
ngs 299| 0 0 -3 -17 16 10 -.06 10 8 | -763 69 553 1532
sio 364| 0 0 -1 -15 -9 -14 .01 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 3.2267.0 GPS week: 2267 Day: 0 MJD: 60113.000
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 12 7 4 8 9 12 8 4 | 28 32 33 29 30 31 31 31 30 29
2 | 5 6 12 9 5 11 11 13 10 4 | 20 21 21 25 22 23 24 24 25 21
3E | 7 13 28 10 4 10 9 12 10 6 | 94 94 91 92 92 42 90 89 92 91
4 | 5 6 6 7 3 46 5 8 10 3 | 60 62 58 61 61 72 60 60 57 60
5E | 5 5 11 8 4 10 6 10 10 3 | 45 44 47 46 46 43 47 49 47 46
6 | 4 8 5 7 3 9 6 10 6 3 | 24 27 24 24 24 26 22 25 22 24
7 | 5 5 6 6 3 9 6 11 9 3 | 36 33 38 35 35 37 36 40 40 36
8 | 5 8 6 9 3 11 5 14 11 3 | 541 542 538 567 541 544 541 544 544 541
9 | 4 7 7 8 3 9 6 7 8 3 | 36 37 36 38 36 39 38 36 37 36
10E | 8 11 21 8 4 8 6 9 7 5 | 41 43 48 44 42 39 42 38 42 42
11 | 5 7 7 8 3 58 7 12 5 3 | 34 37 37 37 34 46 37 32 35 35
12 | 6 5 9 14 3 9 11 11 9 4 | 47 45 50 48 48 49 50 50 49 47
13 | 5 6 6 6 2 11 6 9 8 2 | 27 27 27 29 28 34 28 30 29 28
14 | 7 15 7 9 3 56 17 12 7 5 | 47 55 50 46 48 63 38 48 47 46
15 | 8 5 6 7 3 10 6 14 10 3 | 55 49 51 50 50 51 54 44 45 51
16 | 5 8 12 14 4 11 10 11 13 4 | 19 17 20 21 17 16 19 20 19 17
17 | 4 9 10 8 6 10 9 8 9 3 | 29 25 35 28 27 29 32 29 30 29
18 | 7 9 7 8 2 58 7 10 14 3 | 37 39 40 40 39 46 40 37 42 38
19 | 5 10 8 8 6 11 7 10 6 3 | 35 31 37 33 32 31 35 31 33 33
20E | 8 6 9 6 3 8 9 11 9 3 | 46 43 42 44 44 42 44 47 44 44
21 | 4 6 9 9 4 9 7 14 9 3 | 21 21 21 25 21 23 23 24 26 21
22M | 5 5 10 10 6 9 6 10 --- 3 | 17 17 21 21 17 20 18 17 --- 18
23E | 8 21 12 10 5 53 16 20 21 6 | 113 116 113 112 113 114 113 115 117 113
24M | 12 7 11 10 5 13 8 10 9 4 | 28 26 35 25 29 37 24 29 26 27
25 | 4 9 7 12 3 10 11 9 8 4 | 20 23 20 26 20 21 20 22 19 20
26 | 4 9 9 10 4 9 9 11 11 4 | 20 19 17 21 18 19 20 19 19 18
27 | 6 6 10 8 3 11 7 13 9 3 | 35 37 36 39 35 37 35 33 34 35
X28M | 5 4 --- 9 4 52 10 8 6 3 | 55 52 --- 55 53 65 52 56 54 54
29 | 4 8 4 7 4 11 7 10 9 3 | 33 31 36 36 33 34 32 36 34 33
30 | 5 7 7 6 4 14 5 11 6 3 | 24 25 23 23 26 33 21 27 23 23
31M | 4 5 9 6 3 9 8 7 8 3 | 43 43 41 43 41 48 43 42 42 42
32 | 6 6 5 10 3 8 6 9 3 3 | 35 33 33 34 33 37 33 33 32 33
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 9 10 9 4 24 8 11 10 |T 54 54 55 56 54 55 54 54 55 54
WRMS | 6 8 11 8 4 24 8 10 9 |NE 32 33 33 34 32 36 33 33 33 32
MEDI | 5 7 9 8 3 10 7 10 9 |MD 35 33 36 36 34 37 35 33 35 35
Table 3.2267.1 GPS week: 2267 Day: 1 MJD: 60114.000
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 | 4 8 6 7 3 7 6 9 8 3 | 20 23 21 21 20 23 20 18 22 20
2 | 6 6 11 10 4 9 7 11 10 3 | 15 14 18 20 15 15 15 18 17 15
3E | 6 14 23 9 4 9 5 12 11 5 | 76 80 77 77 76 37 76 75 78 76
4 | 6 5 7 7 3 46 5 8 7 2 | 43 44 43 44 43 48 42 43 42 43
5E | 10 9 19 8 3 10 8 13 9 5 | 37 36 40 37 35 38 36 35 34 35
6 | 6 9 6 7 3 7 5 9 9 3 | 18 21 19 18 18 21 17 17 18 18
7 | 5 4 4 6 2 8 5 7 7 2 | 21 19 24 21 21 21 23 21 23 21
8 | 6 7 12 11 2 11 4 13 10 4 | 474 475 474 494 472 473 473 469 472 473
9 | 4 6 6 8 4 9 5 5 7 2 | 24 26 24 25 25 27 24 25 26 24
10E | 8 12 26 7 5 9 9 10 11 5 | 37 37 46 36 36 34 40 35 40 37
11 | 7 7 7 9 2 57 6 11 10 3 | 16 19 21 22 17 23 19 20 22 18
12 | 6 6 8 13 3 9 9 10 11 4 | 38 36 38 40 39 42 43 44 44 39
13 | 6 5 6 6 2 10 6 7 10 2 | 22 24 24 24 25 31 26 24 25 24
14 | 7 16 8 9 4 56 12 10 8 4 | 37 41 41 39 38 47 33 37 39 37
15 | 5 4 6 7 3 8 5 12 11 3 | 32 28 32 31 30 32 31 27 28 30
16 | 6 6 14 16 3 12 10 10 14 4 | 19 17 21 19 17 17 19 18 20 16
17 | 7 10 7 8 5 11 9 10 9 4 | 23 18 25 21 21 23 24 21 26 21
18 | 6 8 7 7 3 58 8 11 8 3 | 20 20 22 23 18 25 23 18 24 20
19 | 6 11 8 8 5 10 7 10 9 3 | 27 26 30 27 27 25 27 25 28 26
20E | 7 5 9 8 2 10 8 11 9 3 | 32 30 31 31 30 29 32 30 31 30
21 | 6 7 9 10 3 8 5 10 10 3 | 15 14 18 19 14 17 15 17 17 14
22 | 4 4 8 11 3 9 5 13 --- 3 | 14 13 16 17 16 16 15 20 --- 14
23E | 8 22 17 9 4 53 20 20 21 7 | 112 115 113 110 110 111 114 113 116 113
24 | 6 5 9 8 4 13 6 10 11 3 | 18 19 27 16 23 31 20 22 20 19
25 | 4 9 8 11 3 8 9 5 9 3 | 19 22 21 23 19 23 21 19 20 20
26 | 5 8 8 10 3 8 7 9 9 3 | 21 19 19 20 19 21 19 17 20 18
27 | 6 6 11 8 3 11 8 12 10 4 | 27 29 28 29 27 29 29 27 30 27
X28 | 4 4 --- 8 5 53 7 8 10 3 | 45 47 --- 46 47 53 47 49 48 46
29 | 6 7 5 9 3 9 7 15 8 3 | 29 26 27 30 28 29 27 29 30 27
30 | 5 6 7 6 3 15 4 9 5 2 | 19 19 20 17 20 29 16 19 18 18
31 | 3 5 7 6 4 8 6 8 8 2 | 29 28 28 28 29 32 31 29 31 29
32 | 5 7 7 12 2 7 6 9 9 3 | 27 24 27 23 24 27 25 22 26 24
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 9 11 9 3 23 8 11 10 |T 43 44 45 45 43 45 44 43 46 43
WRMS | 6 8 11 8 3 24 7 9 7 |NE 24 24 25 25 23 27 24 23 25 23
MEDI | 6 7 8 8 3 9 6 10 9 |MD 24 24 27 24 25 29 25 24 26 24
Table 3.2267.2 GPS week: 2267 Day: 2 MJD: 60115.000
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 | 3 8 6 9 3 8 7 10 16 3 | 36 38 38 38 39 39 39 37 38 37
2 | 5 5 10 10 4 11 7 18 16 4 | 26 27 29 29 29 29 27 28 31 27
3E | 7 16 24 9 5 9 10 20 18 6 | 89 90 88 88 89 40 91 90 88 89
4 | 5 6 6 8 3 45 5 11 17 3 | 49 49 49 50 49 58 50 47 49 49
5E | 5 8 8 11 3 9 12 12 14 4 | 31 31 33 30 32 30 38 35 36 32
6 | 3 9 7 6 3 7 5 11 7 3 | 29 32 31 28 29 31 29 30 28 29
7 | 4 6 5 6 2 9 6 8 13 2 | 25 24 27 24 26 26 27 28 32 25
8 | 41 41 47 404 32 71 39 52 69 21 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
9 | 3 7 6 7 3 9 7 9 14 3 | 40 39 40 40 39 41 42 37 41 39
10E | 6 12 22 8 4 8 8 15 12 5 | 48 51 55 48 49 62 49 51 57 49
11 | 5 8 8 8 3 58 6 12 9 3 | 26 30 28 30 28 36 31 27 29 28
12 | 4 6 8 13 3 8 9 11 9 3 | 37 34 39 37 36 37 40 38 38 37
13 | 5 4 7 9 3 11 6 9 11 3 | 22 25 25 25 25 30 25 27 27 24
14 | 7 15 8 10 4 60 10 12 10 4 | 34 40 38 35 36 49 33 36 34 35
15 | 7 6 7 10 3 9 5 14 10 3 | 38 33 36 35 35 36 37 29 33 35
16 | 7 7 8 16 3 10 10 16 23 4 | 26 26 26 23 25 26 27 25 34 24
17 | 6 10 8 7 4 8 7 13 10 3 | 30 29 33 30 31 31 32 28 33 30
18 | 5 8 6 8 2 54 9 16 17 3 | 30 33 34 34 32 39 32 31 36 32
19 | 7 10 7 8 5 7 7 17 9 4 | 31 29 35 32 31 30 33 29 33 31
20E | 5 6 7 6 4 9 6 10 11 3 | 22 24 24 22 22 21 21 21 23 22
21 | 5 5 11 11 4 10 6 17 20 3 | 27 28 30 30 29 30 28 29 34 27
22 | 5 8 10 11 5 10 6 17 --- 4 | 17 17 22 18 18 19 20 24 --- 18
23E | 8 29 14 12 6 54 29 35 47 9 | 69 69 67 72 68 67 68 71 72 67
24 | 5 6 11 11 3 13 5 12 7 3 | 19 21 29 22 23 31 22 21 22 21
25 | 4 9 8 8 3 9 9 11 6 3 | 23 27 26 25 24 26 23 23 24 23
26 | 6 9 10 11 3 8 7 11 18 4 | 23 25 27 23 23 26 23 19 29 22
27 | 6 7 8 10 3 12 8 13 26 3 | 30 29 28 28 28 32 28 25 29 27
X28 | 4 5 --- 7 5 51 8 10 10 3 | 38 38 --- 38 38 48 40 39 40 38
29 | 4 10 12 6 4 9 7 16 9 4 | 31 32 36 32 32 32 30 30 32 31
30 | 4 7 4 7 3 15 3 10 9 2 | 21 21 20 21 22 30 20 20 23 20
31 | 4 6 6 7 3 6 6 9 16 2 | 31 32 33 30 31 35 33 30 35 31
32 | 5 8 12 12 2 9 7 14 10 4 | 45 45 47 45 46 48 44 47 46 45
------+---------------------------------------------------+----------------------------------------------------
RMS | 9 12 13 73 7 27 11 17 20 |T 33 34 35 34 34 35 34 33 36 33
WRMS | 5 8 10 9 4 27 7 11 11 |NE 30 31 32 31 31 34 31 30 33 30
MEDI | 5 8 8 9 3 9 7 12 12 |MD 30 31 33 30 31 32 32 29 33 31
Table 3.2267.3 GPS week: 2267 Day: 3 MJD: 60116.000
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 | 4 7 8 9 3 8 5 10 7 3 | 24 25 21 29 23 27 23 24 21 23
2 | 6 5 13 13 5 10 5 11 7 4 | 18 19 19 24 18 22 21 22 20 18
3E | 8 15 25 11 4 --- 8 17 10 6 | 67 69 73 68 66 --- 63 67 64 66
4 | 6 4 6 7 2 46 6 7 9 2 | 22 23 22 26 22 37 25 22 25 22
5E | 8 6 17 15 3 10 9 12 8 5 | 30 30 35 32 30 29 30 30 31 29
6 | 4 8 8 7 3 9 6 10 6 3 | 20 24 21 22 21 23 19 22 21 20
7 | 5 5 4 7 2 8 5 8 7 2 | 21 21 23 23 22 25 22 25 21 21
8 | 7 7 8 13 2 14 6 14 7 4 | 536 537 540 539 540 536 538 542 538 539
9 | 4 6 11 7 3 8 7 7 8 3 | 24 24 25 26 24 29 25 26 25 24
10E | 8 15 19 14 6 --- 13 18 18 6 | 49 49 56 51 49 --- 49 48 49 48
11 | 7 7 8 9 2 59 6 12 7 3 | 22 28 28 28 25 34 26 25 26 25
12 | 7 8 12 15 4 9 7 13 8 4 | 24 20 30 26 24 24 24 25 23 23
13 | 4 6 8 6 3 11 5 6 7 2 | 20 19 20 20 20 25 20 22 19 19
14 | 7 13 9 14 5 56 11 15 8 5 | 31 35 32 33 31 47 26 41 28 31
15 | 6 6 8 7 4 8 6 10 8 3 | 41 39 45 39 40 42 39 37 37 40
16 | 6 6 11 15 4 9 11 11 10 4 | 19 18 21 21 17 18 20 22 20 17
17 | 8 10 5 10 5 10 8 11 7 4 | 26 20 28 24 23 25 27 26 27 24
18 | 7 8 9 9 3 54 9 14 15 4 | 24 25 28 25 23 36 27 25 29 24
19 | 8 10 7 10 5 8 8 12 8 4 | 27 23 26 25 23 24 28 26 28 25
20E | 8 4 15 9 3 9 9 10 14 4 | 31 33 37 33 32 30 30 31 32 31
21 | 5 5 12 13 4 8 8 12 11 4 | 20 19 20 25 19 23 21 23 23 19
22 | 6 6 9 12 5 8 7 13 --- 4 | 14 14 21 13 13 16 16 18 --- 13
23E | 9 30 18 8 8 57 26 32 32 9 | 62 63 63 63 61 61 68 70 72 63
24 | 7 6 10 11 3 13 6 14 8 4 | 18 23 27 21 22 29 19 27 19 20
25 | 6 9 7 11 3 10 8 12 7 3 | 21 23 21 25 21 23 20 24 20 20
26 | 6 7 11 12 4 8 8 10 9 4 | 18 20 20 19 17 21 19 20 19 17
27 | 5 6 6 11 2 11 6 11 8 3 | 31 32 31 30 30 33 31 28 33 30
X28 | 5 7 --- 10 3 51 7 10 10 3 | 19 21 --- 19 19 34 20 25 22 20
29 | 6 9 6 10 4 10 9 11 10 3 | 26 21 26 27 25 25 26 29 27 24
30 | 4 6 5 8 3 14 5 9 6 2 | 18 19 19 18 20 28 16 23 14 18
31 | 4 5 6 9 3 8 6 7 8 2 | 26 27 28 24 26 29 26 25 23 26
32 | 6 9 7 13 2 9 6 8 9 3 | 28 25 28 27 26 32 25 23 23 25
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 9 11 11 4 24 9 13 11 |T 43 43 46 44 42 46 43 45 44 42
WRMS | 6 9 12 10 4 25 7 10 10 |NE 23 23 25 25 23 28 24 25 24 23
MEDI | 6 7 8 10 3 10 7 11 8 |MD 24 23 27 25 23 28 25 25 25 24
Table 3.2267.4 GPS week: 2267 Day: 4 MJD: 60117.000
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 | 5 7 7 9 2 8 4 8 7 3 | 32 34 31 35 32 35 32 31 32 32
2 | 8 4 11 12 4 11 5 9 9 3 | 20 21 25 24 21 22 20 23 21 20
3E | 7 15 15 11 5 --- 9 18 14 5 | 102 106 104 102 103 --- 98 100 100 101
4 | 5 6 5 7 3 47 4 8 10 2 | 48 49 49 51 48 58 46 51 47 48
5E | 5 8 8 9 3 9 6 13 6 3 | 30 28 31 29 28 30 25 28 26 28
6 | 5 9 7 7 3 8 5 8 8 3 | 23 25 24 22 23 25 20 22 22 22
7 | 3 5 5 5 3 9 3 7 8 2 | 23 22 25 22 23 24 23 25 26 23
8 | 7 7 7 13 2 13 4 13 8 3 | 951 949 947 984 949 947 947 946 949 949
9 | 4 6 5 6 3 8 4 5 8 2 | 39 40 38 40 39 42 37 40 39 39
10E | 8 13 13 17 7 22 10 19 11 5 | 39 43 43 40 38 34 39 40 42 39
11 | 5 7 7 8 3 56 4 9 10 3 | 22 26 26 27 24 32 24 23 27 24
12 | 5 7 9 15 3 9 6 10 10 3 | 42 40 43 42 42 44 44 48 43 42
13 | 5 6 7 7 4 11 4 7 6 2 | 20 22 22 21 20 28 22 24 23 20
14 | 7 14 5 10 3 54 8 9 7 4 | 35 41 36 37 36 49 32 35 36 35
15 | 6 6 6 9 5 9 5 9 6 3 | 32 30 37 31 32 36 34 30 32 32
16 | 7 5 11 16 4 12 10 9 11 4 | 22 19 23 22 19 20 20 19 22 19
17 | 7 9 6 8 5 10 7 9 11 3 | 27 23 26 26 24 27 26 25 29 25
18 | 7 8 6 11 3 53 7 12 10 3 | 23 25 27 29 25 35 26 22 29 24
19 | 7 10 7 8 7 11 6 9 9 3 | 27 25 28 28 26 27 27 26 31 26
20E | 6 6 6 5 3 8 7 10 8 3 | 22 22 25 22 21 21 21 23 21 21
21 | 8 5 12 12 4 10 5 10 8 4 | 22 21 26 24 21 23 19 23 22 20
22 | 8 9 13 12 5 11 6 12 --- 4 | 14 17 20 13 15 16 14 20 --- 14
23E | 7 29 13 12 9 57 17 16 16 7 | 56 57 57 56 55 59 61 58 65 57
24 | 7 5 14 9 3 11 5 10 9 4 | 17 22 33 20 23 30 19 24 20 21
25 | 5 10 8 10 3 10 8 9 7 3 | 21 23 22 25 20 22 19 21 23 20
26 | 6 7 8 12 3 9 9 9 9 3 | 21 22 22 19 21 25 24 19 25 20
27 | 7 6 8 11 2 11 4 11 8 3 | 31 29 29 30 29 31 27 31 27 28
X28 | 5 6 --- 7 4 49 6 9 6 3 | 41 41 --- 41 41 47 42 43 42 41
29 | 6 8 6 9 2 10 7 8 8 3 | 25 23 28 29 26 25 25 27 27 25
30 | 4 5 5 7 3 13 3 8 9 2 | 21 22 20 20 22 29 20 21 23 20
31 | 4 6 5 7 3 9 5 9 6 2 | 32 32 33 29 33 37 35 28 34 32
32 | 6 8 8 10 3 10 6 7 7 3 | 41 40 41 40 40 44 37 39 40 39
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 9 9 10 4 24 7 10 9 |T 60 60 62 61 59 62 59 60 62 59
WRMS | 6 9 8 10 4 24 6 9 8 |NE 28 28 29 29 27 31 27 28 29 27
MEDI | 6 7 7 9 3 11 6 9 8 |MD 27 25 28 29 26 30 26 26 29 25
Table 3.2267.5 GPS week: 2267 Day: 5 MJD: 60118.000
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 | 5 7 6 11 2 7 4 9 7 3 | 41 40 40 39 39 39 41 37 39 39
2 | 6 4 10 12 4 9 5 10 8 3 | 29 28 30 30 29 29 30 27 30 28
3E | 9 17 18 15 5 --- 14 23 9 7 | 111 111 113 111 111 --- 115 118 114 112
4 | 4 7 9 8 2 48 6 8 9 3 | 57 57 56 56 57 61 59 54 57 56
5E | 6 8 11 9 3 10 6 13 7 4 | 25 26 26 26 25 26 25 33 26 25
6 | 5 8 6 7 4 10 6 8 6 3 | 39 40 38 39 39 41 39 41 40 39
7 | 4 6 4 5 3 9 9 6 3 2 | 36 33 37 34 36 35 39 36 37 36
8 | 5 7 10 9 3 13 6 12 7 3 | 759 756 758 770 757 756 757 758 755 758
9 | 4 7 5 6 3 8 6 4 5 2 | 48 48 50 48 49 49 51 47 50 48
10E | 9 12 14 21 5 14 10 17 13 6 | 60 60 61 62 61 55 63 68 66 61
11 | 7 7 7 9 3 57 7 10 9 3 | 31 33 32 35 31 35 33 34 35 32
12 | 5 6 8 12 2 9 10 11 12 4 | 38 37 43 40 39 42 44 40 44 40
13 | 8 5 7 9 4 11 5 7 9 3 | 26 25 22 24 25 31 24 27 23 24
14 | 7 13 6 10 4 54 11 8 7 4 | 44 47 46 45 45 52 43 46 44 44
15 | 6 6 8 10 5 8 5 12 7 3 | 31 27 33 25 29 30 31 28 27 29
16 | 5 6 10 15 3 11 11 8 10 4 | 37 35 37 34 36 37 39 36 40 36
17 | 7 10 8 9 4 10 8 9 8 3 | 38 36 40 38 37 37 38 39 40 37
18 | 6 7 7 9 2 56 10 12 11 3 | 33 34 37 35 35 37 37 33 35 34
19 | 8 11 8 10 6 10 8 9 10 4 | 40 37 39 40 38 38 40 38 41 38
20E | 9 7 8 8 4 8 7 12 7 3 | 30 30 27 29 28 27 32 34 29 29
21 | 5 4 9 12 4 8 6 11 5 3 | 31 29 32 31 30 32 32 29 32 30
22 | 6 8 10 10 4 10 7 15 --- 4 | 22 21 25 23 22 23 25 27 --- 22
23E | 9 25 12 14 5 59 11 14 12 6 | 70 70 68 70 69 72 72 73 75 70
24 | 7 5 14 12 3 12 7 6 12 4 | 22 25 36 20 26 33 24 24 24 24
25 | 3 10 8 11 2 11 9 7 10 3 | 33 35 32 34 33 33 33 35 31 33
26 | 5 7 9 10 3 7 8 9 10 3 | 28 26 28 27 27 29 27 25 29 26
27 | 5 6 9 10 2 11 8 10 4 3 | 29 28 27 30 26 30 26 25 28 26
X28 | 4 7 --- 7 5 52 7 8 7 3 | 37 36 --- 38 36 41 36 36 37 36
29 | 5 7 7 9 3 10 8 10 12 3 | 47 45 45 46 46 45 46 46 45 45
30 | 4 5 5 7 4 14 7 7 6 2 | 23 23 24 23 24 32 24 24 22 23
31 | 3 7 8 5 3 7 5 8 7 2 | 39 40 38 38 37 41 38 39 37 38
32 | 6 8 11 10 2 8 7 10 5 3 | 52 51 54 49 52 54 53 51 51 51
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 9 9 11 4 24 8 11 9 |T 62 61 63 62 61 62 63 62 63 61
WRMS | 6 9 8 10 3 24 7 9 7 |NE 36 36 37 36 36 38 37 36 37 36
MEDI | 5 7 8 10 3 10 7 9 8 |MD 37 35 37 35 36 37 38 36 37 36
Table 3.2267.6 GPS week: 2267 Day: 6 MJD: 60119.000
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 | 5 7 5 11 4 6 6 9 7 3 | 36 36 36 37 36 37 36 36 37 35
2 | 7 5 8 13 5 11 9 12 11 4 | 27 26 26 30 27 28 30 29 29 27
3E | 7 13 15 22 7 15 10 16 12 6 | 103 100 100 104 103 71 101 103 99 101
4 | 5 7 6 10 3 49 6 8 7 3 | 68 67 65 68 67 75 66 68 64 67
5E | 7 6 11 8 4 11 12 9 9 4 | 41 41 41 42 43 42 44 43 45 41
6 | 5 7 6 8 3 9 7 9 7 3 | 32 34 31 31 32 35 31 33 33 31
7 | 5 6 6 4 3 7 4 5 7 2 | 45 41 48 42 44 46 46 43 48 44
8E | 6 6 8 13 3 11 8 12 6 4 | 830 830 829 851 829 830 828 830 829 830
9 | 4 7 5 7 3 10 7 6 6 2 | 48 47 46 48 48 50 49 48 47 47
10E | 10 11 24 16 7 13 10 16 12 6 | 52 51 57 49 52 45 53 52 53 51
11 | 7 6 7 10 2 55 7 9 7 3 | 38 40 41 39 38 48 38 39 40 38
12 | 4 7 7 11 4 10 8 10 12 3 | 48 45 48 48 46 47 52 46 51 47
13 | 7 7 9 8 5 12 6 6 6 3 | 24 24 23 28 26 32 27 28 28 25
14 | 7 12 7 11 4 52 11 9 8 4 | 43 48 46 43 44 63 37 42 42 42
15 | 7 6 9 9 3 8 6 9 5 3 | 55 54 55 51 54 56 55 52 53 54
16 | 4 7 8 15 4 9 11 8 11 4 | 23 21 25 24 22 22 22 21 23 21
17 | 7 9 7 9 4 10 8 8 8 3 | 33 28 31 31 30 31 31 30 33 30
18 | 6 6 6 10 2 54 9 8 9 3 | 41 41 43 42 41 49 42 43 44 41
19 | 6 10 5 11 4 10 8 10 9 4 | 35 29 35 35 32 31 36 29 35 33
20E | 12 5 13 8 4 10 11 5 11 4 | 44 42 44 41 43 41 43 45 45 42
21 | 5 4 9 12 4 10 8 11 7 3 | 28 26 26 28 26 29 28 29 29 26
22 | 8 5 11 11 4 9 10 11 --- 4 | 23 23 25 26 21 28 24 19 --- 22
23E | 8 24 9 11 5 58 10 17 11 6 | 81 86 83 83 82 84 83 80 81 82
24 | 7 7 9 9 3 11 6 7 9 3 | 29 34 37 28 33 39 31 33 36 31
25 | 4 9 6 8 3 12 9 8 9 3 | 24 26 24 27 24 25 24 23 23 23
26 | 5 7 7 11 4 7 9 9 10 3 | 22 21 21 25 21 25 20 19 19 20
27 | 6 6 11 12 4 11 11 12 10 4 | 39 40 40 44 38 39 41 38 40 39
X28 | 4 7 --- 7 3 50 5 8 7 3 | 49 49 --- 52 47 58 48 46 50 49
29 | 5 7 5 10 4 10 7 12 10 3 | 33 30 34 35 32 32 31 33 33 32
30 | 5 7 7 5 4 13 6 8 4 3 | 30 30 31 27 31 39 29 31 29 29
31 | 3 7 7 5 4 9 5 10 5 3 | 52 54 50 51 50 57 52 47 50 51
32 | 6 9 6 13 3 7 6 9 7 3 | 52 49 50 46 51 52 50 48 49 49
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 9 9 11 4 23 8 10 9 |T 66 66 67 67 66 68 66 65 68 65
WRMS | 6 8 8 11 4 24 7 8 7 |NE 37 36 37 37 36 40 37 36 37 36
MEDI | 6 7 7 10 4 10 8 9 8 |MD 39 40 41 41 38 41 38 39 42 39
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 4.2267 GPS week: 2267 MJD: 60113.0-60119.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 |U 13 9 30 |U 8 12 33 |U 9 12 43 |
esa | esa 3072 | 13 11 35 |U 8 13 42 |U 11 11 51 |
gfz | gfz 2975 |U 11 9 30 |U 7 9 30 | 10 10 45 |
grg | grg 3072 |U 11 11 31 |U 8 9 37 | 9 9 48 |
igr | igr 3072 | 12 10 29 | 7 10 31 | 8 9 44 |
igs | igs 3056 | 11 9 29 | 7 10 32 | 8 9 41 |
jpl | jpl 3017 | 17 15 35 | 9 16 44 | 13 11 55 |
mit | mit 3072 |U 23 31 66 |U 14 28 62 |U 21 25 53 |
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 5.2267.0 GPS week: 2267 Day: 0 MJD: 60113.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 8 28 | 7 11 29 | 8 11 40 |
esa | esa 3072 | 12 12 33 | 6 12 35 | 9 8 46 |
gfz | gfz 2976 | 9 7 26 | 6 8 26 | 9 10 43 |
grg | grg 3072 | 11 8 30 | 6 7 29 | 8 9 45 |
igr | igr 3072 | 11 10 25 | 5 9 25 | 6 7 38 |
igs | igs 3072 | 10 9 26 | 5 9 26 | 7 8 39 |
jpl | jpl 3072 | 18 18 33 | 7 14 34 | 12 9 48 |
mit | mit 3072 | 15 19 42 | 13 29 58 | 15 16 45 |
Table 5.2267.1 GPS week: 2267 Day: 1 MJD: 60114.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 7 30 | 8 13 29 | 6 9 34 |
esa | esa 3072 | 12 8 33 | 6 15 37 | 10 9 41 |
gfz | gfz 2976 | 9 8 27 | 7 10 26 | 8 8 33 |
grg | grg 3072 | 11 9 27 | 7 10 34 | 7 8 42 |
igr | igr 3072 | 11 8 29 | 6 11 28 | 6 6 33 |
igs | igs 3072 | 11 7 28 | 6 11 28 | 6 7 35 |
jpl | jpl 3072 | 19 14 40 | 7 17 31 | 13 8 45 |
mit | mit 3072 | 17 17 47 | 15 30 67 | 20 27 47 |
Table 5.2267.2 GPS week: 2267 Day: 2 MJD: 60115.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 15 9 32 | 12 19 50 | 13 21 70 |
esa | esa 3072 | 14 11 40 | 12 15 62 | 11 7 49 |
gfz | gfz 2976 | 10 10 32 | 10 10 36 | 13 11 61 |
grg | grg 3072 | 10 10 31 | 12 9 54 | 11 12 67 |
igr | igr 3072 | 10 9 30 | 11 11 44 | 12 13 75 |
igs | igs 3071 | 13 10 34 | 12 13 53 | 10 11 57 |
jpl | jpl 3072 | 17 15 39 | 17 25 74 | 16 20 83 |
mit | mit 3072 | 66 99 187 | 16 22 67 | 44 45 138 |
Table 5.2267.3 GPS week: 2267 Day: 3 MJD: 60116.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 14 9 31 | 8 12 26 | 9 11 43 |
esa | esa 3072 | 13 8 33 | 7 13 34 | 11 14 56 |
gfz | gfz 2973 | 20 9 38 | 7 7 27 | 15 12 53 |
grg | grg 3072 | 13 10 35 | 9 9 29 | 9 11 48 |
igr | igr 3072 | 12 8 29 | 7 9 23 | 8 10 44 |
igs | igs 3072 | 12 8 31 | 7 9 24 | 9 10 44 |
jpl | jpl 2880 | 17 12 31 | 8 15 42 | 15 10 47 |
mit | mit 3072 | 18 14 43 | 15 33 49 | 24 34 54 |
Table 5.2267.4 GPS week: 2267 Day: 4 MJD: 60117.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 16 13 33 | ---- ---- ---- | 9 10 30 |
esa | esa 3072 | 17 20 42 | ---- ---- ---- | 12 12 45 |
gfz | gfz 2976 | 12 11 34 | ---- ---- ---- | 10 9 30 |
grg | grg 3072 | 19 21 38 | ---- ---- ---- | 10 8 35 |
igr | igr 3072 | 16 18 35 | ---- ---- ---- | 9 7 29 |
igs | igs 2967 | 12 12 32 | ---- ---- ---- | 7 8 21 |
jpl | jpl 2976 | 15 15 35 | ---- ---- ---- | 13 9 48 |
mit | mit 3072 | 21 30 45 | ---- ---- ---- | 16 14 26 |
Table 5.2267.5 GPS week: 2267 Day: 5 MJD: 60118.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 9 33 | 8 11 29 | 7 13 47 |
esa | esa 3072 | 13 9 37 | 9 10 46 | 10 15 64 |
gfz | gfz 2976 | 11 9 34 | 7 9 28 | 9 14 52 |
grg | grg 3072 | 9 10 34 | 8 8 38 | 10 13 58 |
igr | igr 3072 | 11 10 33 | 6 10 31 | 8 12 50 |
igs | igs 3071 | 11 9 33 | 7 9 31 | 8 13 50 |
jpl | jpl 2976 | 17 17 34 | 8 14 42 | 12 11 61 |
mit | mit 3072 | 15 24 56 | 12 14 44 | 12 22 34 |
Table 5.2267.6 GPS week: 2267 Day: 6 MJD: 60119.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 8 24 | 5 10 33 | 8 10 34 |
esa | esa 3072 | 13 10 25 | 6 11 41 | 11 14 58 |
gfz | gfz 2976 | 8 7 23 | 5 9 38 | 8 9 40 |
grg | grg 3072 | 7 9 25 | 7 8 40 | 10 7 43 |
igr | igr 3072 | 10 9 20 | 4 10 32 | 8 8 39 |
igs | igs 3072 | 9 8 21 | 4 9 30 | 8 9 39 |
jpl | jpl 3072 | 18 15 30 | 7 15 42 | 13 12 57 |
mit | mit 3072 | 10 14 39 | 15 41 85 | 14 16 30 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.2267 GPS week: 2267 MJD: 60113.500-60119.500
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 -15 -6 89 -1 | -8 27
| 14 12 47 36 3 | 3
esa uuuuu | 1 -16 68 -16 1 | 0 25
| 9 6 44 47 5 | 3
gfz uuuuu | -9 -22 2 -81 -1 | 3 25
| 12 11 118 121 2 | 3
grg uuuuu | -23 11 1 -28 2 | 3 24
| 8 4 30 76 7 | 2
igr xxxxx | -15 8 -16 8 4 | -6 27
| 9 6 17 30 5 | 3
irf xxxxx | -7 12 14 -16 3 | -2 25
| 9 8 18 18 3 | 3
mit uuuuu | 17 33 -15 -21 2 | 12 26
| 23 9 26 40 4 | 3
ngs uuuuu | -17 16 -73 1 -3 | 6 27
| 35 17 200 72 8 | 4
sio xxxxx | -11 91 -53 42 3 | 12 27
| 54 63 52 72 7 | 4
Table 7.2267.0 GPS week: 2267 Day: 0 MJD: 60113.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 14 -6 9 107 -5 | -5 28
esa uuuuu | 2 -17 21 -41 -6 | 3 27
gfz uuuuu | -6 -5 -207 -33 -5 | 5 28
grg uuuuu | -32 8 -8 -55 10 | 3 25
igr xxxxx | -25 3 2 -31 5 | -5 28
irf xxxxx | -16 8 -12 -28 4 | -2 27
mit uuuuu | 17 25 -58 -21 3 | 12 28
ngs uuuuu | -9 -5 303 -41 2 | 9 28
sio xxxxx | 6 101 -86 -19 0 | 14 32
Table 7.2267.1 GPS week: 2267 Day: 1 MJD: 60114.500
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 | 29 -18 -43 56 0 | -6 27
esa uuuuu | -8 -20 36 38 -3 | 2 26
gfz uuuuu | -13 -26 22 -75 -1 | 5 28
grg uuuuu | -12 8 -6 -65 5 | 3 26
igr xxxxx | -21 14 -22 33 8 | -5 28
irf xxxxx | -2 12 20 -15 4 | -2 27
mit uuuuu | 10 36 8 -25 3 | 12 28
ngs uuuuu | -35 24 10 35 -5 | 9 28
sio xxxxx | -20 98 -29 -12 -12 | 12 30
Table 7.2267.2 GPS week: 2267 Day: 2 MJD: 60115.500
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 -2 28 159 0 | -6 27
esa uuuuu | 18 -25 104 7 1 | 1 26
gfz uuuuu | -15 -17 -29 -287 -3 | 5 27
grg uuuuu | -23 7 -4 -155 11 | 4 26
igr xxxxx | -5 3 -8 -28 4 | -4 28
irf xxxxx | 7 4 -6 -44 5 | -2 27
mit uuuuu | 39 17 -23 53 8 | 12 28
ngs uuuuu | -26 28 -187 75 -19 | 9 28
sio xxxxx | 89 130 -48 -9 9 | 11 29
Table 7.2267.3 GPS week: 2267 Day: 3 MJD: 60116.500
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 | 31 -34 -67 63 -4 | -12 26
esa uuuuu | -6 -7 126 31 1 | -4 23
gfz uuuuu | -24 -11 171 -151 -2 | 0 24
grg uuuuu | -16 13 12 -18 2 | 0 23
igr xxxxx | -7 3 -18 25 -4 | -9 26
irf xxxxx | -21 25 35 -27 7 | -6 25
mit uuuuu | -17 45 16 0 1 | 8 25
ngs uuuuu | 16 13 -326 15 1 | 2 24
sio xxxxx | -86 147 8 163 7 | 7 25
Table 7.2267.4 GPS week: 2267 Day: 4 MJD: 60117.500
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 -11 72 73 1 | -12 26
esa uuuuu | 7 -18 41 -1 -2 | -3 22
gfz uuuuu | -14 -29 22 -121 0 | 1 22
grg uuuuu | -33 8 -54 0 1 | 2 21
igr xxxxx | -6 6 -43 42 1 | -8 25
irf xxxxx | -7 0 11 -6 4 | -3 22
mit uuuuu | -5 34 -23 -27 3 | 10 23
ngs uuuuu | 38 4 -128 69 -4 | 3 24
sio xxxxx | -37 -16 -146 -6 5 | 9 23
Table 7.2267.5 GPS week: 2267 Day: 5 MJD: 60118.500
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 -7 -35 98 2 | -13 27
esa uuuuu | -1 -16 111 -68 5 | -4 22
gfz uuuuu | -6 -36 -47 8 2 | 0 23
grg uuuuu | -18 18 41 9 -5 | 1 21
igr xxxxx | -13 17 4 22 11 | -9 26
irf xxxxx | -2 18 25 0 2 | -3 22
mit uuuuu | 42 38 -30 -68 -4 | 10 23
ngs uuuuu | -50 4 -19 -14 0 | 1 25
sio xxxxx | 9 151 -61 66 4 | 10 23
Table 7.2267.6 GPS week: 2267 Day: 6 MJD: 60119.500
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 -29 -8 69 -1 | -5 26
esa uuuuu | -4 -9 35 -78 9 | 3 26
gfz uuuuu | 14 -28 84 89 0 | 7 26
grg uuuuu | -24 12 26 90 -7 | 8 24
igr xxxxx | -27 13 -27 -7 5 | 0 27
irf xxxxx | -6 14 29 6 -3 | 4 24
mit uuuuu | 34 33 4 -60 -3 | 17 28
ngs uuuuu | -56 44 -165 -133 3 | 8 28
sio xxxxx | -35 26 -9 109 7 | 18 29
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