[IGSREPORT-29291] Wk 2257 IGS Final Orbits
acc
acc at igs.org
Sun Apr 30 23:57:27 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2257 (Apr 09, 2023 - Apr 15, 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_20230990000_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 | NNOR
0 | ESA | 21 21 NRMD NRMD
0 | GFZ | JFNG JFNG
0 | GRG | CZTG DAV1 DAV1 GUAM HYDE SGOC
0 | MIT | 21
1 | GFZ | 21 21 JFNG SEYG SEYG
1 | GRG | MAL2 CZTG MAL2 SVTL ULAB
1 | MIT | 22
2 | COD | SANT SEYG
2 | ESA | SEYG SEYG SGOC
2 | GFZ | JFNG
2 | GRG | CZTG HYDE MAL2
2 | MIT | MDVJ
3 | ESA | MAL2 SEYG
3 | GFZ | 21 SEYG SEYG
3 | GRG | CZTG DAV1 DJIG KOKB CZTG DAV1 DJIG GAMB SVTL
4 | COD | SEYG
4 | GFZ | 5 5 DRAO PTVL
4 | GRG | 13 13 DGAR DAV1 DGAR
5 | COD | AREQ SEYG SGOC
5 | ESA | HYDE
5 | GFZ | AREQ AREQ POHN
5 | GRG | NYA2 NYA2 SVTL
6 | COD | 6 DAV1 HYDE KITG QAQ1
6 | ESA | JFNG MAL2
6 | GFZ | 1 6 1 6 TASH
6 | GRG | KIRI SVTL WIND
6 | MIT | 11 MDVJ
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
6 | COD | 6
6 | GRG | 6
6 | MIT | 6
7. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
Starting 28-Nov-2022, all IGS products, are based on the IGS realization of
the ITRF2020 reference frame (IGS20). Starting from the same date, the IGS
products are based on the repro3 standards, including long filename formats.
For more information see IGSMAIL #8238, #8256, #8274 and #8282.
8. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.4 .2 -.1 21 -5 8 .21
ESA | 0 | 1.2 .3 -.9 4 -17 5 -.29
GFZ | 0 | .3 -1.2 -.1 -11 18 26 .59
GRG | 0 | .9 -.7 -1.2 -2 -20 28 -.01
JPL | 0 | 6.5 -7.1 -.3 -9 61 -32 .53
MIT | 0 | 7.6 .4 24.8 7 -7 -2 .19
NGS | 0 | 6.9 3.3 12.2 -13 16 -10 .06
SIO | 0 | 2.7 6.3 6.3 86 0 20 .07
COD | 1 | -.4 .1 .2 13 -6 -2 .19
ESA | 1 | .3 .5 -1.1 7 -11 3 -.28
GFZ | 1 | -.3 -.4 -.1 -15 10 12 .47
GRG | 1 | .7 -1.3 -.5 -7 -7 19 .18
JPL | 1 | 6.3 -7.0 3.1 -12 40 -43 .65
MIT | 1 | 5.1 -5.2 26.1 -10 -13 1 .34
NGS | 1 | 7.2 -4.1 3.7 -32 -21 43 .32
SIO | 1 | 3.4 1.0 6.4 11 -16 39 .43
COD | 2 | -.2 -.4 .4 17 -9 1 .22
ESA | 2 | .1 -.1 -.8 -3 -6 4 -.12
GFZ | 2 | .0 -.3 -.3 -12 -2 18 .50
GRG | 2 | .2 -.6 -1.1 1 -9 17 .28
JPL | 2 | 1.4 -7.5 -5.4 12 44 -26 .52
MIT | 2 | 4.3 -3.4 24.4 -17 -15 13 .33
NGS | 2 | 3.7 -7.1 2.5 -51 -7 16 .49
SIO | 2 | .9 2.5 6.9 52 19 42 .21
COD | 3 | -.2 -.5 .8 9 -16 -8 .19
ESA | 3 | .3 -.3 -1.4 7 -22 1 -.26
GFZ | 3 | .6 -.5 -.3 -11 9 14 .32
GRG | 3 | .5 .1 -1.0 26 -6 11 .03
JPL | 3 | 4.6 -5.1 -5.1 0 45 -48 .64
MIT | 3 | 1.0 -4.7 26.0 -3 7 -2 .16
NGS | 3 | .3 -3.8 3.1 -29 9 2 .14
SIO | 3 | -2.0 1.7 2.6 20 31 58 .03
COD | 4 | -.1 -.5 .9 11 -22 1 .17
ESA | 4 | .0 .5 -.5 8 -13 -2 -.08
GFZ | 4 | -.7 -.3 -1.0 13 1 -15 .42
GRG | 4 | .3 .0 -1.3 23 -25 -14 .37
JPL | 4 | -3.8 -2.9 1.1 8 40 -29 .73
MIT | 4 | .7 -3.2 24.9 4 1 -35 .29
NGS | 4 | -1.3 -5.3 11.5 -55 37 -22 .30
SIO | 4 | -2.2 4.9 -1.7 77 25 62 .30
COD | 5 | .0 -.2 .9 17 -24 0 .11
ESA | 5 | .2 .2 -1.0 3 -12 8 -.31
GFZ | 5 | .4 -.6 -.8 -12 -4 16 .38
GRG | 5 | .7 .3 -1.2 20 -5 -9 -.01
JPL | 5 | 1.1 -2.1 -.6 4 33 -23 .60
MIT | 5 | 4.8 -2.8 28.9 -17 0 3 .20
NGS | 5 | 6.4 -3.5 20.6 -81 30 18 .01
SIO | 5 | 3.9 3.9 2.7 33 -69 75 -.06
COD | 6 | -.1 -.1 .6 12 -13 3 .18
ESA | 6 | .6 .8 -.2 -10 -10 6 -.14
GFZ | 6 | .2 -.7 -.0 -16 12 16 .58
GRG | 6 | 1.0 -1.3 -1.4 -3 -14 18 .44
JPL | 6 | 1.6 -8.3 4.0 -5 26 -26 .51
MIT | 6 | 9.5 -8.4 33.5 -47 -20 53 .33
NGS | 6 | 7.9 -9.4 10.4 -73 -19 55 .21
SIO | 6 | 9.7 -5.2 -1.5 -98 -184 66 .14
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.atx
The JPL solution did not use IGS20/igs20.atx until GPS Week TBA, which caused
their orbit and clock residuals to be higher during that period than for the other
centres; from GPS Week 2238 through TBA, the JPL solution is excluded from the
weekly SINEX combination, as well as from orbit and clock combinations.
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 1.2257.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2257.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 2.2257.[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 3.2257.[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 5.2257.0-6). 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 2257 summary. (Apr 09, 2023 - Apr 15, 2023)
Table 1.2257.a GPS week: 2257 MJD: 60043.000-60049.000
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 857| 0 0 -1 14 -14 17 .01 7 6 | -689 231 5 94
| 0 0 0 9 20 21 .01 | 152 272
esa 150| 0 0 6 10 -3 1 -.03 9 9 | -974 623 5 75
| 0 0 0 9 16 22 .01 | 400 756
gfz 121| 0 0 0 25 10 5 .11 12 12 | 45 -161 12 87
| 0 0 1 7 12 21 .04 | 178 475
grg 115| 1 -1 -4 -1 28 -6 -.00 8 8 | -88 -71 7 120
| 0 0 1 13 20 15 .01 | 218 447
igr n/a| 0 0 0 -9 2 4 .02 5 5 | 668 114 11 74
| 0 0 0 11 15 21 .01 | 903 554
jpl n/a| -1 0 -1 4 0 26 .17 23 24 | -1475 74 73 148
| 0 1 1 12 26 25 .02 | 918 785
mit 359| 0 0 -2 -39 -5 -22 -.01 10 8 | -7192 284 102 13440
| 0 0 0 24 39 69 .01 | 8907 386
ngs 288| 0 0 3 -9 -6 0 -.07 11 9 | -732 285 894 1844
| 1 0 3 31 21 9 .03 | 238 384
sio 375| 0 0 -1 -135 144 41 -.03 13 11 | --- --- --- ---
| 0 0 1 40 48 32 .03 | --- ---
Table 1.2257.b GPS week : 2257 MJD: 60043.000-60049.000
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 | 7 6 5 6 6 6 7 |
2 | 5 4 5 4 5 4 4 |
3 | 3 3 4 3 3 4 3 |
4 | 4 4 3 4 3 4 4 |
5 | 4 4 3 4 4 4 3 |
6 | 6 7 7 7 7 7 --- |
7 | 3 3 4 4 4 4 5 |
8 | 4 3 4 3 3 3 3 |
9 | 4 3 3 3 3 4 3 |
10 | 4 4 4 4 4 4 4 |
11 | 5 6 6 6 7 8 9 |
12 | 4 4 4 4 4 4 4 |
13 | 4 4 3 4 4 4 4 |
14 | 4 4 4 4 4 4 4 |
15 | 4 4 3 4 4 4 4 |
16 | 4 3 3 4 4 3 3 |
17 | 4 3 4 3 4 4 4 |
18 | 6 7 7 7 6 8 7 |
19 | 3 3 3 3 4 3 5 |
20 | 4 4 4 4 4 4 4 |
21 | 5 4 5 4 4 5 5 |
22 | 4 5 4 4 5 4 4 |
23 | 4 4 4 4 4 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 4 4 4 3 4 |
27 | 4 4 4 3 4 3 3 |
28 | 7 7 7 6 6 6 7 |
29 | 4 4 4 4 7 8 3 |
30 | 4 4 5 5 4 4 5 |
31 | 4 4 4 4 4 5 4 |
32 | 4 3 4 3 4 4 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 2.2257.0 GPS week: 2257 Day: 0 MJD: 60043.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 853| 0 0 -1 26 -5 27 -.00 6 6 | -727 239 5 99
esa 150| 0 0 5 7 8 -6 -.03 8 8 | -1426 1561 5 69
gfz 123| 0 1 -1 37 32 8 .09 12 14 | -95 91 12 88
grg 121| 1 -2 -5 -23 42 11 -.00 9 8 | -271 180 7 128
igr n/a| -1 0 0 -13 10 2 .03 5 5 | -658 438 11 69
jpl n/a| -1 -1 -1 -11 48 19 .17 23 23 | -2498 132 77 145
mit 359| -1 0 -2 -29 -61 -50 -.01 9 8 | -13482 509 68 13405
ngs 290| 2 1 9 -16 -4 -12 -.07 13 12 | -734 217 963 1821
sio 375| 0 0 0 -144 114 -1 -.07 12 9 | --- --- --- ---
Table 2.2257.1 GPS week: 2257 Day: 1 MJD: 60044.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 853| 0 0 -1 20 13 24 .03 7 6 | -792 479 6 106
esa 150| 0 0 6 8 -20 -1 -.04 8 8 | -1564 1451 6 81
gfz 123| -1 0 0 21 11 -3 .05 12 13 | -9 257 13 93
grg 121| 1 -1 -4 -11 -1 -3 .02 8 8 | -194 148 7 128
igr n/a| -1 0 0 -6 -25 4 .03 5 5 | -200 523 11 78
jpl n/a| -2 0 0 -2 -27 38 .16 22 22 | -2370 462 71 139
mit 359| -1 0 -2 -39 35 -46 .01 9 8 | -12143 582 75 13844
ngs 290| 0 1 1 -6 -44 7 -.05 10 8 | -809 481 687 1529
sio 375| -1 0 0 -162 194 35 -.04 11 10 | --- --- --- ---
Table 2.2257.2 GPS week: 2257 Day: 2 MJD: 60045.000
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 852| 0 0 -1 4 -16 21 .03 7 6 | -685 233 6 96
esa 150| 0 0 7 16 16 6 -.03 9 9 | -748 334 5 81
gfz 119| 0 0 0 22 11 13 .14 12 11 | 140 -328 12 102
grg 122| 1 -1 -2 9 48 -25 .00 8 7 | -7 -100 7 134
igr n/a| 0 0 -1 -5 -5 7 .03 4 4 | 362 43 10 73
jpl n/a| -2 -2 -1 17 4 30 .17 23 23 | -1951 167 71 146
mit 359| -1 0 -1 -49 -49 -19 -.03 9 8 | -7388 153 284 10881
ngs 288| 0 0 -1 10 3 -13 -.09 10 9 | -662 202 675 1552
sio 374| 0 0 0 -113 149 55 -.04 11 9 | --- --- --- ---
Table 2.2257.3 GPS week: 2257 Day: 3 MJD: 60046.000
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 858| 0 0 -1 0 -30 51 .01 7 6 | -518 -265 6 102
esa 150| 0 0 6 24 -7 34 -.03 9 9 | -524 -241 6 80
gfz 124| 0 0 0 29 8 31 .18 13 12 | 3 -298 12 84
grg 114| 1 -1 -5 13 23 16 .01 8 8 | 179 -409 7 107
igr n/a| 0 0 0 8 12 27 .02 4 4 | 1003 -398 11 72
jpl n/a| 0 0 -1 24 8 43 .14 22 22 | -1200 -469 71 144
mit 359| 0 0 -2 -70 14 -109 -.02 8 7 | -1501 -61 97 9445
ngs 290| -1 1 3 38 0 1 -.12 10 9 | -499 -279 997 2256
sio 376| 0 0 0 -184 178 79 -.03 11 9 | --- --- --- ---
Table 2.2257.4 GPS week: 2257 Day: 4 MJD: 60047.000
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 -2 19 -38 15 .01 7 6 | -948 588 6 88
esa 150| 0 0 6 -2 6 20 -.02 9 8 | -1095 1180 6 72
gfz 121| 1 0 -1 11 8 18 .11 13 12 | -157 533 13 91
grg 108| 2 -1 -1 -7 35 -16 .00 8 8 | -408 685 9 117
igr n/a| 0 0 0 -16 15 25 .02 5 5 | 757 978 12 77
jpl n/a| -1 1 -2 5 -12 52 .15 24 24 | -1739 1548 76 154
mit 359| 0 0 -3 3 0 -53 -.01 11 9 | 8536 913 63 17024
ngs 289| -3 0 2 -49 8 13 -.07 11 10 | -1204 973 680 1521
sio 376| -1 0 -3 -70 175 60 -.00 13 12 | --- --- --- ---
Table 2.2257.5 GPS week: 2257 Day: 5 MJD: 60048.000
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 -2 10 -31 -8 .00 7 7 | -521 138 6 83
esa 150| 0 1 5 17 2 -5 -.03 9 9 | -627 193 6 74
gfz 121| 0 1 -3 25 14 8 .11 11 11 | 386 -585 14 73
grg 105| 2 -1 -4 7 48 -7 -.03 9 8 | 158 -630 9 117
igr n/a| 0 0 0 -5 17 -2 .01 5 4 | 1630 -547 13 77
jpl n/a| -1 -1 -4 1 8 28 .20 24 25 | -215 -638 71 153
mit 359| 0 0 -2 -62 -17 9 .00 11 8 | -18600 -66 57 20364
ngs 289| 0 0 6 6 19 0 -.07 10 8 | -502 74 1337 2054
sio 379| -1 0 -2 -107 144 61 .00 12 10 | --- --- --- ---
Table 2.2257.6 GPS week: 2257 Day: 6 MJD: 60049.000
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| -1 1 0 20 6 -10 .02 7 6 | -637 205 6 86
esa 150| 0 0 5 5 -27 -36 -.05 10 10 | -835 -111 6 71
gfz 120| 1 0 0 29 -11 -35 .08 9 9 | 49 -800 10 79
grg 115| 1 0 -4 1 4 -18 -.00 9 7 | -73 -373 9 111
igr n/a| 0 0 0 -30 -6 -36 .03 5 5 | 1783 -239 12 75
jpl n/a| -2 -1 1 -3 -28 -26 .17 24 24 | -356 -678 79 155
mit 359| 0 0 -1 -28 38 112 -.01 13 10 | -5772 -36 72 9122
ngs 280| 0 0 2 -47 -26 3 -.02 11 9 | -718 330 924 2181
sio 375| 0 -1 -4 -166 51 -2 -.04 20 17 | --- --- --- ---
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 3.2257.0 GPS week: 2257 Day: 0 MJD: 60043.000
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
------+---------------------------------------------------+----------------------------------------------------
1E | 7 8 31 9 5 11 12 18 12 6 | 61 62 64 60 63 30 63 67 68 62
2E | 7 13 11 11 6 9 7 10 11 4 | 42 47 46 44 44 42 44 45 45 44
3 | 5 8 7 5 4 9 8 11 13 3 | 32 33 31 33 33 35 33 34 36 32
4 | 8 8 7 9 6 51 9 12 11 4 | 59 60 60 60 57 68 60 59 57 59
5 | 4 6 9 6 2 8 9 13 14 3 | 53 51 55 53 52 54 51 49 54 51
6E | 6 9 28 7 6 10 7 14 7 5 | 70 65 70 65 66 34 67 71 71 67
7E | 6 6 8 7 4 12 7 10 12 3 | 16 18 19 18 17 17 19 22 27 17
8 | 5 8 7 9 3 10 7 16 12 3 | 22 24 22 24 22 25 22 26 26 22
9 | 5 8 7 6 4 9 7 15 11 3 | 29 27 26 29 26 32 28 27 29 27
10 | 4 8 9 8 3 10 9 8 10 3 | 33 32 34 35 32 34 34 35 36 33
11E | 8 16 11 10 4 55 10 15 18 5 | 48 52 51 48 48 51 48 49 50 49
12 | 8 6 8 10 4 10 5 10 11 3 | 35 37 39 40 36 37 38 37 41 37
13 | 6 5 7 8 5 12 8 15 11 3 | 31 33 33 37 34 39 33 37 39 33
14 | 8 9 6 11 5 50 6 17 10 4 | 30 38 35 36 34 58 37 33 37 34
15 | 6 4 9 7 4 7 10 15 13 3 | 51 51 55 50 52 55 49 54 46 51
16 | 7 5 9 8 7 12 7 12 12 3 | 17 16 21 20 16 16 19 21 24 17
17 | 6 4 10 8 5 9 8 12 11 3 | 28 27 33 30 30 34 30 30 32 29
18E | 10 17 10 9 3 54 17 14 18 6 | 33 40 35 37 34 39 34 36 40 34
19 | 4 4 8 6 4 7 7 12 6 3 | 34 33 38 34 33 34 37 40 37 35
20 | 5 5 9 6 5 10 8 13 15 3 | 30 29 35 31 30 31 30 34 37 30
21E | 8 8 7 17 7 10 10 17 11 5 | 45 47 46 40 46 42 45 45 47 44
X22 | 6 --- 12 5 7 12 6 9 --- 3 | 38 --- 40 38 37 42 37 38 --- 37
23 | 6 8 13 8 3 55 10 12 10 4 | 48 50 48 51 48 56 51 52 53 49
24E | 9 7 8 11 4 10 9 13 11 4 | 26 29 27 29 26 28 27 29 28 26
25 | 7 10 8 10 4 9 6 13 11 4 | 24 28 25 27 24 28 26 25 32 25
26 | 6 8 10 8 6 9 5 12 10 3 | 32 32 36 35 31 32 31 26 34 32
27 | 4 8 10 9 3 9 6 12 9 3 | 24 25 22 25 23 25 22 25 28 23
X28E | 10 18 --- 12 6 60 18 14 22 7 | 44 51 --- 48 46 52 48 49 50 46
29 | 5 5 8 8 5 9 9 16 8 3 | 28 25 24 27 27 26 24 27 28 27
30E | 7 10 8 9 4 11 10 13 13 4 | 26 25 28 30 25 25 27 26 31 26
31E | 5 5 13 7 5 7 7 18 8 4 | 33 34 31 35 34 35 37 41 39 34
32 | 5 8 11 6 4 8 8 9 9 3 | 24 25 25 23 24 28 21 25 25 23
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 8 12 9 5 23 9 13 12 |T 35 36 37 37 35 37 36 37 39 36
WRMS | 6 8 14 8 5 23 8 12 9 |NE 33 33 35 35 33 37 33 34 36 33
MEDI | 6 8 9 8 4 10 8 13 11 |MD 32 33 35 35 33 34 34 35 37 33
Table 3.2257.1 GPS week: 2257 Day: 1 MJD: 60044.000
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
------+---------------------------------------------------+----------------------------------------------------
1E | 7 9 22 10 5 9 12 12 13 5 | 43 45 44 41 44 24 42 46 47 43
2E | 5 11 11 8 5 10 12 10 11 4 | 33 35 38 35 35 32 34 37 38 34
3 | 6 8 7 6 4 10 8 6 8 3 | 24 27 23 24 23 26 27 24 30 24
4 | 6 6 7 8 5 46 9 9 10 3 | 44 44 42 46 41 47 44 40 45 43
5 | 6 5 11 8 5 11 9 7 15 3 | 30 28 33 28 30 33 31 31 39 29
6E | 7 10 34 13 6 11 11 18 11 7 | 52 48 49 49 48 27 50 51 56 48
7E | 6 7 10 4 4 12 7 7 10 3 | 18 18 23 18 19 19 21 21 27 18
8 | 5 8 9 7 3 8 5 8 8 3 | 17 20 16 20 17 20 18 16 24 17
9 | 5 7 8 5 4 8 6 10 9 3 | 25 23 20 25 22 29 23 24 25 23
10 | 8 8 8 9 3 8 8 9 10 3 | 24 20 22 21 20 25 20 17 27 20
11E | 11 16 13 10 5 52 11 13 18 5 | 28 31 27 30 29 33 30 30 36 28
12 | 8 5 9 9 4 11 8 10 11 3 | 28 25 31 28 28 29 33 32 37 28
13 | 8 4 10 8 6 13 9 6 13 3 | 22 25 28 28 27 32 26 30 30 25
14 | 7 9 7 9 6 51 6 11 9 4 | 25 27 27 29 25 39 27 21 31 25
15 | 5 5 8 7 5 7 11 8 13 3 | 33 30 33 29 31 34 29 34 32 30
16 | 6 5 10 8 6 11 5 10 9 3 | 15 13 18 15 13 14 17 15 22 14
17 | 5 4 9 8 5 9 8 5 9 3 | 21 18 23 23 21 26 22 21 27 21
18E | 13 19 12 10 4 51 22 13 21 7 | 22 25 23 24 21 27 28 21 32 21
19 | 5 4 10 7 4 8 8 10 7 3 | 23 21 24 21 21 24 23 24 27 22
20 | 7 4 12 8 5 8 9 8 18 3 | 22 19 24 19 21 23 22 19 33 19
21E | 6 7 11 10 4 9 11 10 8 4 | 34 36 37 31 35 34 31 33 38 33
X22 | 11 --- 9 6 6 11 7 10 --- 4 | 30 --- 29 28 28 31 29 29 --- 28
23 | 5 7 12 8 3 54 12 9 12 4 | 29 25 28 29 26 28 29 23 36 26
24E | 10 8 9 11 4 10 9 8 12 4 | 22 22 24 24 21 23 22 21 25 21
25 | 8 10 11 9 3 11 6 8 12 4 | 19 24 25 22 20 24 20 17 29 20
26 | 6 8 13 8 5 10 5 11 7 3 | 25 25 30 25 23 24 23 21 31 24
27 | 5 8 11 8 4 9 5 13 9 3 | 18 19 15 19 16 20 16 17 21 16
X28E | 10 18 --- 13 5 63 16 12 20 7 | 34 39 --- 35 33 39 36 29 38 32
29 | 5 6 10 10 4 11 7 8 6 3 | 21 17 22 18 20 22 17 20 22 19
30E | 8 9 11 8 5 11 9 10 12 4 | 20 21 27 23 21 23 23 23 28 21
31E | 6 6 8 8 5 8 8 8 8 3 | 32 31 28 31 31 34 35 35 38 31
32 | 4 7 11 5 4 8 10 6 9 3 | 17 20 20 18 19 23 18 20 26 17
------+---------------------------------------------------+----------------------------------------------------
RMS | 7 8 12 8 5 22 9 10 11 |T 26 26 27 26 25 27 27 26 32 25
WRMS | 6 8 13 8 5 22 8 8 10 |NE 24 23 25 24 23 27 24 23 29 23
MEDI | 6 7 10 8 5 10 8 9 10 |MD 24 25 27 25 23 26 26 23 31 24
Table 3.2257.2 GPS week: 2257 Day: 2 MJD: 60045.000
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
------+---------------------------------------------------+----------------------------------------------------
1E | 7 9 18 8 3 8 10 12 9 4 | 32 37 37 32 32 18 35 35 39 33
2E | 4 13 11 14 7 10 9 10 11 4 | 32 35 34 32 33 32 33 30 34 32
3 | 5 9 8 8 4 8 8 11 9 3 | 33 34 33 34 33 39 29 36 33 32
4 | 8 7 7 7 5 49 6 8 10 3 | 44 45 44 46 43 52 46 41 48 45
5 | 5 6 9 8 3 8 8 8 10 3 | 35 34 39 35 36 38 32 36 37 34
6E | 7 9 37 9 5 11 11 10 14 6 | 32 32 36 32 29 17 35 28 36 30
7E | 7 9 10 6 5 11 6 8 9 3 | 18 21 18 21 20 20 20 22 27 19
8 | 7 8 8 7 2 9 7 13 9 3 | 20 21 19 21 18 24 16 18 22 18
9 | 5 8 8 5 3 8 5 6 12 2 | 22 22 22 21 20 25 22 20 27 21
10 | 6 9 8 7 3 8 9 6 12 3 | 22 22 20 21 20 25 20 19 23 20
11E | 11 17 13 9 5 53 15 18 19 6 | 21 28 25 24 20 28 27 21 31 22
12 | 8 6 7 8 5 10 6 10 7 3 | 32 31 33 32 31 34 32 31 32 31
13 | 7 5 8 8 4 10 7 8 14 3 | 23 26 26 28 25 32 24 25 28 24
14 | 7 10 8 7 5 53 6 8 13 3 | 22 29 25 27 27 46 28 29 31 25
15 | 6 5 7 6 4 11 8 7 14 3 | 35 36 37 34 37 41 35 36 35 35
16 | 5 4 8 6 6 12 7 10 9 3 | 17 16 19 17 16 17 17 17 21 16
17 | 6 6 11 8 4 9 7 9 10 3 | 20 16 26 20 20 24 19 19 22 18
18E | 13 18 10 9 5 52 17 14 18 6 | 18 24 19 23 16 25 23 19 25 18
19 | 5 4 13 6 3 7 6 7 6 3 | 19 18 26 19 20 21 19 21 24 19
20 | 7 6 9 7 4 10 8 8 15 3 | 20 21 25 23 21 23 22 24 28 21
21E | 7 10 9 9 6 9 14 11 5 4 | 27 29 29 24 29 26 33 31 31 28
X22 | 8 --- 12 6 4 9 9 8 --- 4 | 34 --- 40 35 35 37 32 36 --- 34
23 | 8 8 10 7 3 53 10 9 11 4 | 18 23 26 22 19 29 23 17 28 20
24E | 8 8 9 8 4 10 9 12 10 4 | 29 27 24 30 27 30 28 27 29 27
25 | 7 10 9 8 3 7 6 7 7 3 | 21 24 22 22 20 25 21 19 23 20
26 | 4 8 12 6 3 9 8 11 6 3 | 24 26 30 25 24 24 26 19 26 24
27 | 5 8 7 10 3 8 8 14 11 4 | 22 23 19 24 21 24 18 20 20 19
X28E | 9 17 --- 10 5 63 16 13 17 6 | 31 41 --- 39 33 43 37 35 37 34
29 | 7 7 7 9 4 10 9 8 10 3 | 22 18 24 22 20 24 21 22 23 20
30E | 7 10 20 8 6 11 9 17 11 5 | 20 21 23 21 18 22 20 24 25 19
31E | 7 6 13 6 5 9 8 7 8 3 | 32 34 34 36 33 34 35 36 37 33
32 | 6 7 9 4 3 7 11 7 10 3 | 19 21 21 20 19 24 17 21 23 18
------+---------------------------------------------------+----------------------------------------------------
RMS | 7 9 12 8 4 23 9 10 11 |T 25 26 27 26 25 28 26 26 29 25
WRMS | 6 9 11 7 4 23 8 9 9 |NE 24 25 27 26 25 29 24 25 27 24
MEDI | 7 8 9 8 4 10 8 9 10 |MD 22 26 26 24 21 25 24 24 28 22
Table 3.2257.3 GPS week: 2257 Day: 3 MJD: 60046.000
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
------+---------------------------------------------------+----------------------------------------------------
1E | 7 10 30 8 5 11 12 14 16 6 | 21 24 22 19 19 19 20 20 23 19
2E | 5 13 11 10 6 12 7 11 11 4 | 31 33 33 30 31 32 30 32 33 31
3 | 6 9 6 6 4 9 5 8 10 3 | 24 28 25 26 26 30 25 29 28 25
4 | 8 5 6 9 4 49 8 8 9 3 | 25 26 25 24 25 42 26 24 32 24
5 | 5 8 8 10 4 8 11 7 13 4 | 40 37 41 39 38 43 39 35 43 38
6E | 6 10 33 7 5 11 12 15 17 6 | 28 26 27 26 25 22 23 29 22 23
7E | 5 10 10 8 5 12 6 10 9 3 | 17 20 21 18 19 18 22 25 28 19
8 | 6 8 8 5 3 9 4 12 6 3 | 17 20 17 20 17 21 17 17 26 16
9 | 5 7 8 6 3 8 6 8 7 3 | 18 19 19 19 19 23 19 20 25 17
10 | 8 9 11 9 4 9 7 11 9 4 | 19 19 21 21 18 21 17 18 25 18
11E | 10 18 15 12 4 51 16 12 19 6 | 22 30 25 23 23 28 26 24 31 22
12 | 7 7 6 8 3 10 6 10 10 3 | 29 30 33 31 30 33 29 35 33 30
13 | 8 6 12 9 5 13 9 11 9 4 | 21 23 24 25 24 29 24 28 26 23
14 | 7 10 7 9 4 52 7 9 11 3 | 21 29 27 27 24 49 25 24 31 24
15 | 8 6 6 6 3 11 9 9 9 3 | 40 40 41 38 38 45 36 35 40 38
16 | 5 6 9 6 6 11 8 12 12 3 | 16 15 21 16 16 17 19 19 24 16
17 | 5 7 10 7 3 8 7 7 8 3 | 20 17 26 20 20 24 18 20 23 18
18E | 10 18 15 11 5 47 17 15 19 6 | 15 23 17 18 15 22 21 19 26 15
19 | 5 5 6 6 3 8 6 7 6 2 | 21 19 22 19 20 22 20 19 26 19
20 | 7 5 9 8 4 9 8 8 14 3 | 19 19 25 19 20 20 21 21 30 19
21E | 9 9 11 7 4 9 6 10 9 4 | 21 25 28 22 23 23 23 27 26 22
X22 | 7 --- 10 7 6 8 5 9 --- 3 | 26 --- 29 25 26 27 26 27 --- 25
23 | 7 7 15 9 3 51 8 11 10 4 | 15 19 26 21 16 31 21 18 29 18
24E | 8 8 11 9 6 11 6 11 12 4 | 26 25 24 29 25 27 26 27 28 25
25 | 7 11 13 8 4 9 7 9 11 4 | 20 25 22 21 19 25 20 20 23 19
26 | 4 9 17 7 5 9 6 10 8 4 | 24 27 34 23 24 25 27 24 29 25
27 | 5 7 10 7 3 8 5 10 8 3 | 18 20 17 20 18 21 19 16 27 17
X28E | 7 15 --- 12 5 61 13 11 14 6 | 24 32 --- 29 25 37 26 24 31 25
29 | 6 6 12 8 4 11 7 10 9 3 | 21 17 26 20 20 24 23 22 24 19
30E | 6 10 11 10 5 13 7 15 9 4 | 20 20 23 22 20 20 20 22 28 19
31E | 7 5 11 8 5 10 7 9 9 3 | 28 30 32 31 31 32 32 31 36 29
32 | 4 7 11 4 3 8 6 7 10 3 | 19 19 18 18 18 24 18 17 23 17
------+---------------------------------------------------+----------------------------------------------------
RMS | 7 9 13 8 4 22 8 10 11 |T 22 24 25 23 22 27 23 24 28 22
WRMS | 6 9 12 8 4 22 7 9 9 |NE 22 23 25 23 22 28 23 23 28 22
MEDI | 7 8 11 8 4 10 7 10 10 |MD 21 24 25 22 20 24 23 24 28 19
Table 3.2257.4 GPS week: 2257 Day: 4 MJD: 60047.000
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
------+---------------------------------------------------+----------------------------------------------------
1E | 6 11 29 12 5 13 12 12 16 6 | 37 38 38 36 37 24 35 39 38 37
2E | 5 12 14 10 7 11 10 13 16 4 | 37 38 40 38 37 37 38 42 39 38
3 | 5 8 8 6 4 8 7 8 13 3 | 23 24 23 24 22 27 22 21 26 22
4 | 6 4 6 6 4 51 8 9 11 3 | 45 44 42 45 44 55 44 41 49 44
5 | 5 6 10 8 4 8 11 12 16 4 | 35 32 36 34 33 38 34 29 33 33
6E | 7 9 34 11 5 12 15 17 15 7 | 58 53 54 55 53 34 55 53 64 53
7E | 6 9 9 7 5 11 9 11 9 3 | 18 21 20 19 19 16 21 24 26 19
8 | 4 7 9 5 3 10 4 12 8 3 | 17 21 17 21 18 20 15 16 24 17
9 | 5 7 8 5 3 10 10 7 11 3 | 22 22 18 21 20 26 21 21 26 20
10 | 5 8 9 8 3 8 9 9 14 3 | 20 20 20 20 19 22 18 17 23 19
11E | 11 18 16 11 6 54 25 16 25 7 | 24 29 25 26 24 29 36 26 39 25
12 | 7 6 10 8 4 12 7 9 10 3 | 28 29 31 33 28 33 29 29 32 29
13 | 6 5 9 8 5 12 10 11 14 3 | 21 23 23 26 25 31 26 29 30 23
14 | 7 10 7 10 6 55 9 12 9 4 | 19 25 24 26 22 44 25 22 30 22
15 | 7 5 8 7 4 9 14 12 15 4 | 41 38 41 36 38 42 34 37 38 37
16 | 6 5 11 6 7 12 7 11 9 3 | 15 14 20 16 14 15 17 15 20 14
17 | 6 6 11 8 4 12 8 8 8 3 | 20 17 26 22 20 26 20 21 25 20
18E | 11 16 12 10 4 51 19 14 21 6 | 20 22 14 21 15 24 23 17 26 18
19 | 5 5 11 6 3 11 10 8 8 3 | 20 20 25 21 20 23 21 23 24 20
20 | 6 5 11 8 5 9 12 12 15 4 | 18 17 21 20 19 20 21 20 28 18
21E | 7 9 7 10 5 11 7 9 11 3 | 30 35 32 33 33 30 32 29 35 31
X22 | 7 --- 11 6 8 12 7 15 --- 4 | 29 --- 32 32 31 34 31 39 --- 31
23 | 8 5 12 9 4 54 12 12 13 4 | 20 21 26 24 19 29 22 18 26 20
24E | 6 7 10 9 5 10 9 12 12 4 | 37 34 32 32 36 40 36 42 36 35
25 | 7 10 10 7 3 10 7 8 10 3 | 20 23 21 21 19 26 20 18 21 19
26 | 5 7 10 6 3 10 6 12 9 3 | 23 25 27 25 23 24 22 22 22 23
27 | 3 8 12 6 3 9 7 12 8 3 | 18 22 23 22 20 23 20 20 23 19
X28E | 7 14 --- 11 5 62 14 13 14 6 | 25 32 --- 31 26 36 28 28 31 26
X29 | 7 7 --- --- 5 --- --- --- --- 7 | 27 21 --- --- 26 --- --- --- --- 25
30E | 7 9 10 7 5 14 9 17 10 4 | 19 21 24 23 18 19 19 21 26 19
31E | 8 7 7 8 6 7 9 10 10 3 | 35 35 35 37 36 36 36 42 38 35
32 | 7 8 11 6 3 8 8 7 13 3 | 19 22 19 19 19 26 17 20 22 18
------+---------------------------------------------------+----------------------------------------------------
RMS | 7 9 13 8 5 24 11 11 13 |T 26 27 27 27 26 29 27 27 30 25
WRMS | 6 8 12 8 5 24 9 10 12 |NE 23 24 25 25 23 29 23 23 27 23
MEDI | 6 7 10 8 4 11 9 12 11 |MD 22 23 25 25 22 27 23 23 26 22
Table 3.2257.5 GPS week: 2257 Day: 5 MJD: 60048.000
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
------+---------------------------------------------------+----------------------------------------------------
1E | 8 11 19 11 6 --- 13 15 16 5 | 44 44 47 43 44 --- 42 44 49 43
2E | 4 12 13 9 5 11 8 8 10 4 | 42 48 48 41 43 42 42 45 47 43
3 | 4 9 7 8 4 10 8 7 8 3 | 20 24 20 21 21 27 19 21 27 20
4 | 5 6 7 7 4 50 11 9 10 3 | 48 48 48 50 46 55 48 46 50 48
5 | 7 6 7 10 3 12 9 7 13 3 | 29 25 31 26 27 33 27 29 33 27
6E | 7 10 27 12 8 --- 12 17 13 6 | 54 46 51 47 46 --- 53 45 59 45
7E | 6 14 10 8 6 13 10 10 7 4 | 17 21 15 16 17 19 19 22 26 17
8 | 6 8 7 6 3 11 6 6 10 3 | 17 20 17 19 17 22 18 16 26 16
9 | 5 7 8 5 3 10 10 8 8 3 | 22 20 20 19 20 25 22 20 25 20
10 | 8 9 9 9 5 9 10 8 12 4 | 27 25 28 24 25 28 23 27 29 25
11E | 13 18 15 16 6 53 26 14 30 8 | 31 32 28 29 28 30 40 30 47 29
12 | 7 6 10 8 5 14 6 9 9 3 | 33 31 33 32 31 34 32 36 34 32
13 | 7 6 10 9 4 13 10 7 14 3 | 23 23 24 27 26 31 24 28 31 24
14 | 7 12 6 10 5 52 8 8 7 4 | 22 25 24 26 22 37 26 21 32 23
15 | 7 5 11 8 4 11 12 6 14 3 | 37 36 42 33 36 43 35 37 38 36
16 | 5 5 7 8 5 15 5 8 9 3 | 15 13 16 15 14 16 17 16 24 14
17 | 7 5 7 8 4 13 8 8 16 3 | 25 21 26 26 25 29 24 25 30 24
18E | 14 17 16 13 6 46 22 21 20 7 | 20 26 22 21 20 26 25 29 30 19
19 | 6 6 8 6 2 10 8 8 9 3 | 27 25 27 26 26 28 26 28 30 25
20 | 8 6 8 8 4 10 7 10 13 3 | 23 21 25 20 21 23 21 21 31 21
21E | 6 9 11 18 4 9 7 11 8 5 | 29 29 28 25 29 29 29 28 34 27
X22 | 7 --- 7 5 5 8 6 14 --- 4 | 26 --- 30 28 26 29 27 30 --- 27
23 | 7 9 10 10 4 50 12 9 12 4 | 33 35 37 34 32 33 33 33 38 33
24 | 7 7 9 9 5 10 7 9 10 3 | 26 26 28 26 25 27 26 28 29 25
25 | 6 11 12 7 5 11 7 7 9 3 | 21 25 19 20 19 26 19 23 20 20
26 | 5 8 8 8 4 11 5 6 6 3 | 22 26 26 23 22 25 23 24 27 23
27 | 4 8 6 6 4 11 7 9 9 3 | 19 21 18 19 18 23 20 18 25 18
X28E | 9 15 --- 12 4 63 12 10 14 6 | 34 38 --- 38 34 42 38 35 39 35
X29 | 10 --- 13 --- 10 --- 11 --- --- 8 | 19 --- 22 --- 17 --- 16 --- --- 17
30E | 6 9 8 8 5 13 10 10 9 4 | 22 20 24 22 21 21 22 21 27 20
31E | 12 7 11 8 5 8 8 17 8 5 | 35 31 27 33 32 34 35 35 39 31
32 | 9 8 11 5 3 9 6 9 12 3 | 19 20 21 16 17 25 16 20 25 17
------+---------------------------------------------------+----------------------------------------------------
RMS | 7 9 11 9 5 24 11 10 12 |T 27 28 28 27 26 29 27 28 33 26
WRMS | 7 9 11 8 4 25 8 8 10 |NE 25 25 26 25 24 29 24 25 30 24
MEDI | 7 8 9 8 4 11 8 9 10 |MD 25 25 26 26 25 28 25 28 30 24
Table 3.2257.6 GPS week: 2257 Day: 6 MJD: 60049.000
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
------+---------------------------------------------------+----------------------------------------------------
1E | 7 9 14 20 8 --- 14 22 23 6 | 53 56 63 53 59 --- 53 63 64 55
2E | 5 8 9 7 5 10 11 12 19 4 | 43 45 48 42 45 42 38 46 43 43
3 | 4 9 5 7 5 9 8 8 23 3 | 25 29 27 26 25 33 25 29 38 25
4 | 6 6 9 7 6 49 10 10 17 3 | 60 63 61 64 60 74 59 62 56 61
5 | 5 8 9 6 3 7 9 6 15 3 | 50 50 54 49 49 53 49 46 58 49
7E | 6 12 6 13 6 11 11 13 13 4 | 22 28 27 24 25 25 26 31 31 24
8 | 5 8 7 4 5 7 5 10 12 3 | 18 22 20 19 21 24 18 21 25 19
9 | 5 7 7 5 5 10 11 8 21 3 | 24 26 24 23 24 28 21 26 26 23
10 | 4 9 8 7 4 9 11 6 21 3 | 31 30 33 30 31 34 28 29 37 29
11E | 10 24 13 11 7 56 34 17 40 8 | 38 40 39 40 38 39 46 40 56 37
12 | 8 9 8 8 4 9 9 8 14 3 | 40 39 42 40 41 40 41 46 45 40
13 | 6 8 8 6 3 12 10 7 16 3 | 24 26 28 29 27 31 30 31 38 26
14 | 7 11 7 10 4 52 9 11 13 4 | 32 35 34 35 32 56 36 30 40 32
15 | 7 8 7 5 4 10 12 7 18 3 | 50 47 48 46 46 54 42 44 45 46
16 | 6 6 5 7 5 10 6 11 11 3 | 16 15 16 17 17 16 17 21 24 16
17 | 8 5 8 6 6 6 10 10 29 3 | 26 24 29 28 29 30 25 27 38 26
18E | 14 21 11 13 5 52 20 17 27 7 | 26 31 23 27 25 30 30 26 39 24
19 | 6 5 12 5 6 8 20 9 39 4 | 31 31 34 31 32 32 32 32 46 30
20 | 7 6 9 6 6 7 13 13 25 4 | 25 26 28 26 26 26 28 31 46 25
21E | 5 11 15 15 5 10 9 12 15 5 | 32 37 31 26 35 36 32 35 38 31
X22 | 7 --- 9 6 6 11 6 10 --- 4 | 35 --- 39 35 35 37 37 38 --- 36
23 | 7 8 13 8 3 56 15 9 22 4 | 46 48 48 46 47 56 47 48 56 45
24 | 7 9 10 9 5 12 10 11 15 4 | 32 31 33 33 31 31 31 33 31 31
25 | 7 10 10 5 4 10 6 10 13 3 | 20 25 21 20 20 22 21 24 28 20
26 | 5 9 11 4 3 9 8 10 13 3 | 25 26 32 25 24 26 22 24 26 24
27 | 6 9 6 5 3 8 10 7 11 3 | 21 22 21 20 21 26 19 21 24 20
X28E | 8 19 --- 12 5 61 13 10 21 6 | 56 57 --- 59 56 60 59 55 59 57
29 | 5 7 6 6 5 9 8 8 --- 3 | 18 11 20 14 17 16 15 14 --- 16
30E | 7 10 9 9 5 13 11 14 16 4 | 23 24 26 25 23 24 22 24 33 22
31E | 9 8 12 9 5 11 9 10 15 4 | 44 43 43 45 43 47 46 47 45 44
32 | 6 8 7 4 4 8 6 9 20 3 | 20 22 25 20 20 26 20 20 28 20
------+---------------------------------------------------+----------------------------------------------------
RMS | 7 10 9 9 5 24 13 11 20 |T 36 36 36 37 35 35 36 36 44 34
WRMS | 6 10 9 7 5 24 10 9 17 |NE 30 30 32 30 30 35 30 31 38 29
MEDI | 6 8 9 7 5 10 10 10 17 |MD 31 31 32 29 31 31 30 31 38 29
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 4.2257 GPS week: 2257 MJD: 60043.0-60049.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 11 11 28 |U 11 19 40 |U 10 10 27 |
esa | esa 2948 | 15 15 24 |U 12 23 43 |U 11 15 36 |
gfz | gfz 2961 |U 10 10 25 |U 11 17 40 | 10 10 30 |
grg | grg 3043 |U 12 12 32 |U 10 20 40 | 12 12 34 |
igr | igr 3056 | 11 11 23 | 11 20 40 | 9 10 27 |
igs | igs 3042 | 11 10 25 | 11 18 38 | 9 9 28 |
jpl | jpl 2989 | 14 12 32 | 11 21 43 | 12 14 35 |
mit | mit 3058 |U 34 32 123 |U 61 123 288 |U 18 17 62 |
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 5.2257.0 GPS week: 2257 Day: 0 MJD: 60043.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 13 28 | 9 14 33 | 9 12 31 |
esa | esa 2976 | 14 15 23 | 8 18 33 | 11 17 38 |
gfz | gfz 2976 | 8 11 24 | 8 12 33 | 9 10 31 |
grg | grg 3067 | 10 15 34 | 8 16 33 | 11 13 37 |
igr | igr 3071 | 9 13 23 | 8 15 34 | 8 11 30 |
igs | igs 3055 | 9 12 25 | 8 13 29 | 9 11 31 |
jpl | jpl 3072 | 12 12 30 | 8 18 38 | 13 15 34 |
mit | mit 3072 | 16 18 44 | 14 17 53 | 10 12 43 |
Table 5.2257.1 GPS week: 2257 Day: 1 MJD: 60044.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 11 28 | 11 17 41 | 10 12 31 |
esa | esa 2976 | 16 14 25 | 12 21 45 | 11 16 35 |
gfz | gfz 2975 | 11 8 25 | 11 16 41 | 11 11 33 |
grg | grg 3071 | 13 13 34 | 11 19 44 | 12 13 38 |
igr | igr 3072 | 11 10 24 | 12 18 43 | 9 12 31 |
igs | igs 3072 | 11 10 26 | 11 17 42 | 10 11 31 |
jpl | jpl 3072 | 13 11 35 | 12 19 46 | 11 19 34 |
mit | mit 3072 | 64 37 481 | 14 22 63 | 17 14 60 |
Table 5.2257.2 GPS week: 2257 Day: 2 MJD: 60045.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 12 32 | 10 18 40 | 10 10 22 |
esa | esa 2976 | 16 18 22 | 11 22 39 | 12 15 31 |
gfz | gfz 2976 | 11 12 28 | 10 19 40 | 8 9 24 |
grg | grg 3071 | 13 14 36 | 9 22 43 | 11 10 28 |
igr | igr 3072 | 11 13 25 | 10 19 40 | 8 9 21 |
igs | igs 3072 | 12 13 28 | 10 19 39 | 9 7 22 |
jpl | jpl 3072 | 14 12 31 | 11 21 44 | 11 14 32 |
mit | mit 3072 | 40 31 123 | 39 38 118 | 33 30 90 |
Table 5.2257.3 GPS week: 2257 Day: 3 MJD: 60046.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 11 28 | 10 22 35 | 9 10 28 |
esa | esa 2976 | 15 15 24 | 11 25 41 | 11 16 35 |
gfz | gfz 2976 | 10 11 23 | 11 18 36 | 11 11 30 |
grg | grg 3070 | 11 11 33 | 10 23 39 | 9 12 31 |
igr | igr 3063 | 10 10 20 | 10 21 36 | 7 12 27 |
igs | igs 3072 | 11 10 24 | 10 21 35 | 8 10 28 |
jpl | jpl 3072 | 14 13 31 | 9 23 35 | 10 16 38 |
mit | mit 3072 | 18 18 38 | 15 30 61 | 14 19 61 |
Table 5.2257.4 GPS week: 2257 Day: 4 MJD: 60047.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 10 27 | 15 20 43 | 11 9 26 |
esa | esa 2880 | 16 15 24 | 16 25 45 | 11 12 30 |
gfz | gfz 2880 | 11 9 27 | 15 20 44 | 10 8 33 |
grg | grg 2976 | 13 11 32 | 15 21 43 | 12 8 32 |
igr | igr 2976 | 10 9 22 | 15 21 44 | 8 8 26 |
igs | igs 2976 | 12 9 23 | 15 20 43 | 10 7 28 |
jpl | jpl 2976 | 13 11 29 | 14 23 41 | 13 10 36 |
mit | mit 2976 | 20 70 59 | 24 24 83 | 17 17 47 |
Table 5.2257.5 GPS week: 2257 Day: 5 MJD: 60048.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 8 26 | 11 22 51 | 11 10 31 |
esa | esa 2880 | 15 15 22 | 12 23 54 | 12 18 39 |
gfz | gfz 2974 | 9 8 21 | 12 17 51 | 11 11 35 |
grg | grg 2976 | 12 9 27 | 11 21 43 | 13 10 35 |
igr | igr 3072 | 10 9 20 | 11 21 49 | 9 11 29 |
igs | igs 3072 | 11 9 22 | 11 20 46 | 10 10 31 |
jpl | jpl 2784 | 13 11 35 | 13 22 54 | 13 11 38 |
mit | mit 3072 | 58 35 59 | 304 709 1552 | 23 16 100 |
Table 5.2257.6 GPS week: 2257 Day: 6 MJD: 60049.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 9 29 | 9 18 38 | 12 10 21 |
esa | esa 2976 | 15 14 31 | 11 25 41 | 12 14 41 |
gfz | gfz 2976 | 11 9 25 | 10 18 33 | 11 9 27 |
grg | grg 3072 | 13 10 28 | 10 20 35 | 17 15 36 |
igr | igr 3068 | 14 12 27 | 9 22 35 | 11 9 24 |
igs | igs 2976 | 13 9 25 | 10 18 35 | 8 9 24 |
jpl | jpl 2880 | 17 12 32 | 12 22 42 | 11 15 30 |
mit | mit 3072 | 22 13 55 | 19 21 87 | 15 9 34 |
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 6.2257 GPS week: 2257 MJD: 60043.500-60049.500
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 | 9 -18 52 -6 -2 | 7 15
| 26 18 61 95 3 | 2
esa uuuuu | 23 -19 78 184 -2 | 25 29
| 8 7 32 82 5 | 2
gfz uuuuu | -8 -35 159 78 -1 | 12 19
| 14 17 112 104 5 | 1
grg uuuuu | -30 1 27 -46 4 | 12 20
| 11 6 19 49 4 | 3
igr xxxxx | -7 -2 31 12 4 | -2 14
| 12 5 54 35 4 | 3
irf xxxxx | 6 9 -49 36 6 | -2 18
| 14 7 31 13 6 | 4
mit uuuuu | 20 53 -185 -102 6 | 24 29
| 35 9 65 57 6 | 3
ngs uuuuu | -19 25 -157 -115 -3 | 11 17
| 32 53 165 149 5 | 1
sio xxxxx | 39 5 -357 -168 7 | 30 36
| 84 57 121 149 20 | 5
Table 7.2257.0 GPS week: 2257 Day: 0 MJD: 60043.500
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 | 9 -33 87 -89 -4 | 4 15
esa uuuuu | 14 -7 60 107 3 | 22 26
gfz uuuuu | -33 -20 -57 37 -3 | 10 17
grg uuuuu | -25 14 41 7 9 | 7 15
igr xxxxx | -3 -3 65 -21 -3 | -6 15
irf xxxxx | 9 19 -70 18 12 | -9 17
mit uuuuu | 7 49 -216 -23 4 | 19 23
ngs uuuuu | 20 7 75 -5 -8 | 11 18
sio xxxxx | -13 -68 -312 -242 13 | 22 25
Table 7.2257.1 GPS week: 2257 Day: 1 MJD: 60044.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -34 -16 9 -23 1 | 5 17
esa uuuuu | 26 -18 109 114 0 | 24 29
gfz uuuuu | -17 -18 83 56 -5 | 11 18
grg uuuuu | -21 -6 26 -43 5 | 9 19
igr xxxxx | 11 -2 76 -23 3 | -5 15
irf xxxxx | 13 14 -36 29 16 | -7 19
mit uuuuu | 37 67 -158 -65 11 | 20 25
ngs uuuuu | 18 -6 -86 -37 -6 | 11 18
sio xxxxx | 33 47 -433 -173 20 | 25 30
Table 7.2257.2 GPS week: 2257 Day: 2 MJD: 60045.500
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 -2 -3 -100 -3 | 9 18
esa uuuuu | 12 -18 66 178 2 | 26 31
gfz uuuuu | -6 -16 159 196 2 | 13 20
grg uuuuu | -19 -3 -2 19 4 | 12 21
igr xxxxx | 4 3 -18 24 6 | -2 15
irf xxxxx | -10 4 -28 38 7 | -2 20
mit uuuuu | 3 47 -172 -66 7 | 24 30
ngs uuuuu | -12 -14 7 -170 -6 | 13 20
sio xxxxx | -22 3 -510 -236 13 | 29 35
Table 7.2257.3 GPS week: 2257 Day: 3 MJD: 60046.500
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 | 25 13 26 122 -4 | 10 17
esa uuuuu | 24 -30 118 278 0 | 28 32
gfz uuuuu | -2 -34 201 81 6 | 13 20
grg uuuuu | -26 -1 15 -80 4 | 13 21
igr xxxxx | -17 -10 -17 27 7 | -1 14
irf xxxxx | -7 5 -12 60 6 | 0 19
mit uuuuu | -12 60 -122 -117 10 | 25 30
ngs uuuuu | -20 -42 -216 -372 -8 | 13 20
sio xxxxx | -45 32 -278 -104 23 | 30 36
Table 7.2257.4 GPS week: 2257 Day: 4 MJD: 60047.500
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 | 30 -34 17 -44 -6 | 8 14
esa uuuuu | 24 -18 99 267 -1 | 27 29
gfz uuuuu | 12 -53 239 204 3 | 12 19
grg uuuuu | -31 1 26 -73 4 | 13 20
igr xxxxx | -22 4 -33 42 7 | -1 13
irf xxxxx | -1 13 -56 31 8 | -1 18
mit uuuuu | -8 57 -152 -192 11 | 25 30
ngs uuuuu | -48 76 -272 -162 1 | 10 15
sio xxxxx | 20 -36 -374 -15 22 | 32 39
Table 7.2257.5 GPS week: 2257 Day: 5 MJD: 60048.500
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 | 37 -24 171 -43 0 | 7 13
esa uuuuu | 34 -22 67 254 -7 | 27 29
gfz uuuuu | -2 -52 240 76 -3 | 14 19
grg uuuuu | -48 4 24 -32 -3 | 14 21
igr xxxxx | -8 -4 37 61 4 | 0 13
irf xxxxx | 5 0 -37 42 0 | 1 18
mit uuuuu | 23 40 -156 -107 1 | 27 31
ngs uuuuu | -69 57 -399 -151 4 | 10 14
sio xxxxx | 111 -39 -149 12 -13 | 35 42
Table 7.2257.6 GPS week: 2257 Day: 6 MJD: 60049.500
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 | -18 -32 54 133 2 | 6 13
esa uuuuu | 29 -20 28 88 -10 | 26 29
gfz uuuuu | -11 -54 249 -103 -9 | 12 18
grg uuuuu | -41 0 59 -120 5 | 13 20
igr xxxxx | -15 0 106 -25 2 | 0 13
irf xxxxx | 30 7 -106 34 -3 | 2 17
mit uuuuu | 90 51 -318 -147 -4 | 27 31
ngs uuuuu | -20 100 -208 88 4 | 10 14
sio xxxxx | 191 95 -445 -418 -28 | 36 42
More information about the IGSREPORT
mailing list