[IGSREPORT-29297] Wk 2258 IGS Final Orbits
acc
acc at igs.org
Fri May 5 06:38:39 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2258 (Apr 16, 2023 - Apr 22, 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_20231060000_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 | 18
0 | ESA | HYDE MAL2
0 | GFZ | JFNG MAL2 PTVL
0 | GRG | 1 21 1 21 CZTG DAV1 DGAR SEYG CZTG DAV1 DGAR MAL2
0 | GRG | SEYG
1 | COD | 21 HYDE KIRI LMMF NKLG SGOC
1 | ESA | GODE JFNG
1 | GFZ | 13 13 GODE LAUT
1 | GRG | CZTG DGAR KIRI SEYG CZTG DGAR JFNG KIRI SVTL
2 | ESA | ULAB
2 | GFZ | GODE
2 | GRG | 21 KIRI ULAB GODE KIRI REUN SFER ULAB WIND
3 | COD | LMMF TASH
3 | ESA | 28
3 | GFZ | 13 13 AREQ
3 | GRG | KIRI CZTG KIRI REUN
4 | COD | HYDE
4 | ESA | GODE SEYG NNOR SEYG
4 | GFZ | 5 JFNG JFNG PTVL
4 | GRG | 13 21
5 | COD | AREQ CHPI
5 | ESA | FAIR MAL2 FAIR JFNG MAL2
5 | GFZ | 15 JFNG
5 | GRG | 5 21 5 21 CZTG CZTG JFNG WIND
6 | COD | HYDE
6 | GFZ | TASH
6 | GRG | 13 13 21 KIRI KIRI
6 | MIT | 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. 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 G01 | | | 4 | 4 | 4 | 4 | 4 |
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 | -.3 -.0 -.0 11 -7 2 .16
ESA | 0 | .5 .4 -.8 -2 -3 -10 -.21
GFZ | 0 | -.2 -.1 -.3 -25 8 2 .43
GRG | 0 | .4 -1.5 -.9 -9 -14 29 .19
JPL | 0 | 4.7 -13.6 1.3 5 57 -33 .33
MIT | 0 | .8 -5.2 27.8 -42 -2 10 .44
NGS | 0 | 4.0 -8.6 14.7 -83 9 43 .37
SIO | 0 | -2.3 .5 -1.3 -32 56 -40 .11
COD | 1 | -.8 -.2 .1 11 -14 -5 .22
ESA | 1 | .2 .2 -.5 3 -5 -3 -.14
GFZ | 1 | -.0 -.1 -.1 -9 0 13 .43
GRG | 1 | .3 -1.2 -.5 -21 -6 -1 .13
JPL | 1 | 3.5 -9.4 -1.5 7 30 -33 .67
MIT | 1 | 2.4 -2.8 27.5 -36 -14 4 .24
NGS | 1 | -1.3 1.9 10.3 -23 29 -2 .09
SIO | 1 | -4.5 4.5 4.3 66 66 -27 .16
COD | 2 | -.9 .2 .4 10 -16 -1 .26
ESA | 2 | -.1 -.1 -.6 4 -13 5 -.15
GFZ | 2 | -.3 -.0 -.4 -31 -4 5 .45
GRG | 2 | .4 -1.1 -.9 -17 -16 30 .08
JPL | 2 | 7.3 -9.2 -.3 -12 19 -51 .76
MIT | 2 | 4.1 -.0 30.8 6 -3 -7 .34
NGS | 2 | 2.2 6.3 7.2 1 -7 -1 .41
SIO | 2 | .1 7.4 -3.4 97 -70 -20 .34
COD | 3 | -.8 .4 .5 8 -21 -1 .28
ESA | 3 | .2 .2 -1.4 -19 -26 14 -.07
GFZ | 3 | .1 -.4 -.3 -12 -6 14 .39
GRG | 3 | .1 -1.2 -.6 -3 -1 10 .04
JPL | 3 | 6.4 -6.0 -.5 -8 19 -47 .94
MIT | 3 | 6.8 -6.1 27.5 -51 -33 -9 .33
NGS | 3 | 5.5 -4.4 14.9 -47 26 25 .28
SIO | 3 | -2.2 2.1 -3.1 13 -15 10 .34
COD | 4 | -.4 .6 .3 13 -16 -2 .19
ESA | 4 | .1 .3 -.8 -10 0 10 -.23
GFZ | 4 | -.5 .3 -.6 5 12 -6 .44
GRG | 4 | .6 -1.0 -.3 1 2 -1 .08
JPL | 4 | 7.5 -9.9 12.6 -4 25 -40 .78
MIT | 4 | 3.2 -6.7 27.5 -26 -21 7 .23
NGS | 4 | -2.1 -1.3 19.2 -60 60 -15 .16
SIO | 4 | -1.1 -1.2 7.4 -30 14 18 .03
COD | 5 | .0 .5 .6 6 -22 -5 .06
ESA | 5 | .5 .6 -1.3 1 -2 -20 -.05
GFZ | 5 | -.4 -.2 -.6 -21 -2 0 .45
GRG | 5 | .4 -.6 -.2 4 -8 7 .20
JPL | 5 | 6.1 -5.7 8.6 2 54 -34 .69
MIT | 5 | 1.4 -8.1 24.7 -31 -2 -16 .42
NGS | 5 | 4.9 -4.2 16.8 -55 14 5 .48
SIO | 5 | -2.1 -.4 7.3 -14 55 -21 .20
COD | 6 | .4 .5 .9 10 -22 -1 .07
ESA | 6 | .4 .1 -.6 2 -3 -1 -.21
GFZ | 6 | -.3 -.8 -.8 -10 -6 5 .36
GRG | 6 | .1 -.6 -.6 -11 3 2 .22
JPL | 6 | 8.7 4.0 10.7 8 48 -50 .69
MIT | 6 | 1.1 -6.6 22.1 -19 -16 10 .36
NGS | 6 | 4.1 -.8 20.3 -62 27 -6 -.01
SIO | 6 | 1.2 -.9 6.0 6 -16 11 -.11
9. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
10. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.atx
The JPL solution did not use IGS20/igs20.atx until GPS Week TBA, which caused
their orbit and clock residuals to be higher during that period than for the other
centres; from GPS Week 2238 through TBA, the JPL solution is excluded from the
weekly SINEX combination, as well as from orbit and clock combinations.
Since swithing to IGS20/igs20.atx, SIO orbits suffered from high Y rotations
with respect to the combined orbits, possibly impacting the alignment of the
combined orbits with respect to the IGS20 frame. As a result, SIO orbits are
excluded from the final combinations until the issue is fixed.
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 1.2258.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2258.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 2.2258.[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 3.2258.[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 5.2258.0-6). 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 2258 summary. (Apr 16, 2023 - Apr 22, 2023)
Table 1.2258.a GPS week: 2258 MJD: 60050.000-60056.000
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 864| 0 0 0 19 0 5 .01 7 6 | -690 125 5 99
| 0 0 0 8 10 15 .02 | 154 208
esa 150| 0 0 3 6 2 -4 -.04 10 10 | -1051 552 5 73
| 0 0 1 5 11 16 .02 | 273 489
gfz 119| 0 0 -1 24 -1 -6 .11 12 11 | 44 -61 12 95
| 0 1 3 13 13 10 .04 | 259 354
grg 116| 1 0 -3 -3 25 9 -.00 10 8 | 11 -141 7 122
| 0 0 2 14 15 14 .04 | 157 253
igr n/a| 0 0 -2 -3 2 10 .05 5 5 | 2882 296 13 74
| 0 0 1 9 10 13 .02 | 1006 458
jpl n/a| 1 -1 0 7 -9 12 .17 24 25 | -458 77 80 161
| 1 2 2 13 13 11 .02 | 417 321
mit 358| 0 0 -3 -42 -8 -6 -.03 11 8 | 13872 338 201 11305
| 0 0 1 24 31 47 .01 | 9933 292
ngs 287| 0 0 5 -19 -32 -4 -.08 11 10 | -719 145 872 1761
| 1 0 2 15 18 30 .03 | 83 158
sio 375| 0 0 -3 -107 110 -14 -.05 14 11 | --- --- --- ---
| 0 0 1 12 63 20 .02 | --- ---
Table 1.2258.b GPS week : 2258 MJD: 60050.000-60056.000
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 | 10 6 6 5 6 6 5 |
2 | 5 4 5 5 5 5 4 |
3 | 3 3 3 4 4 4 3 |
4 | 3 3 3 4 3 3 3 |
5 | 4 3 3 4 4 4 4 |
6 | 5 4 6 7 6 5 4 |
7 | 4 5 7 5 5 5 5 |
8 | 4 3 3 4 4 4 4 |
9 | 3 3 3 3 3 3 3 |
10 | 3 4 4 4 4 4 4 |
11 | 8 9 10 11 10 8 9 |
12 | 4 3 3 3 4 3 4 |
13 | 4 3 4 4 5 4 4 |
14 | 4 4 5 5 5 4 4 |
15 | 4 4 4 4 4 4 4 |
16 | 4 3 4 4 3 3 4 |
17 | 4 4 3 4 4 4 4 |
18 | 10 9 8 8 8 7 6 |
19 | 4 4 4 4 4 4 4 |
20 | 4 3 3 4 4 4 4 |
21 | 6 5 6 5 6 5 5 |
22 | 4 5 4 4 5 4 4 |
23 | 4 4 4 4 5 5 5 |
24 | 4 4 4 4 4 5 5 |
25 | 3 4 4 4 4 4 4 |
26 | 4 4 4 4 4 4 4 |
27 | 4 3 3 5 3 3 4 |
28 | 6 6 6 6 6 5 6 |
29 | 4 3 3 3 3 3 3 |
30 | 4 4 5 5 4 4 5 |
31 | 4 4 4 4 5 5 5 |
32 | 3 3 3 3 4 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2258.0 GPS week: 2258 Day: 0 MJD: 60050.000
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 864| 0 0 0 33 -12 4 -.02 8 6 | -354 -197 6 100
esa 150| 0 0 6 8 12 -28 -.05 11 9 | -1116 705 6 73
gfz 123| -1 0 2 0 13 -8 .16 11 10 | -1 -20 11 81
grg 116| 2 -1 -7 12 43 7 -.01 9 7 | 10 -92 6 118
igr n/a| -1 1 0 -5 1 14 .03 5 5 | 1815 -108 12 71
jpl n/a| 0 -4 -2 24 14 12 .19 25 26 | -714 -214 81 164
mit 358| -2 1 -2 -78 -66 -5 -.05 13 10 | 15302 -54 107 11541
ngs 296| 0 -1 5 -3 0 33 -.08 13 11 | -571 79 732 1740
sio 375| 0 0 -2 -115 167 -50 -.04 19 14 | --- --- --- ---
Table 2.2258.1 GPS week: 2258 Day: 1 MJD: 60051.000
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 864| 0 0 -1 19 15 11 .01 6 6 | -701 272 5 94
esa 150| 0 0 5 8 -8 -5 -.02 10 10 | -1036 560 7 77
gfz 124| 0 0 2 35 -7 5 .12 10 10 | -241 188 12 89
grg 115| 1 0 -7 -7 2 -11 -.04 8 7 | -129 -68 7 114
igr n/a| 0 0 0 -13 -6 5 .06 5 5 | 1671 583 13 69
jpl n/a| 3 -4 -1 -3 -28 22 .16 24 25 | -983 243 82 147
mit 358| -1 0 -2 -32 29 -5 -.03 11 8 | 28647 379 66 14307
ngs 292| 1 0 5 -31 -46 4 -.06 11 10 | -718 247 817 1708
sio 380| 0 0 0 -112 158 -12 -.04 13 11 | --- --- --- ---
Table 2.2258.2 GPS week: 2258 Day: 2 MJD: 60052.000
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 864| 0 0 0 10 -12 8 .04 6 6 | -738 224 5 89
esa 150| 0 0 4 6 11 20 -.04 11 9 | -1468 1014 5 69
gfz 117| 0 0 -2 14 -14 -2 .09 12 12 | -197 129 12 100
grg 113| 1 -1 -3 15 22 19 -.04 10 8 | -212 317 8 131
igr n/a| 0 0 -2 1 6 16 .08 5 5 | 2624 578 13 71
jpl n/a| 2 -3 0 -7 -1 31 .18 25 25 | -335 124 86 152
mit 358| 0 0 -1 -24 11 -62 -.03 11 8 | 12946 839 446 7845
ngs 289| 0 1 1 -41 -33 23 -.07 12 10 | -758 264 821 1790
sio 378| 0 -1 -2 -119 45 -8 -.05 13 10 | --- --- --- ---
Table 2.2258.3 GPS week: 2258 Day: 3 MJD: 60053.000
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 866| 0 0 0 18 -4 23 .03 7 6 | -812 310 6 106
esa 150| 0 0 1 6 0 0 -.01 11 11 | -1262 911 6 75
gfz 116| 0 0 0 24 5 -5 .12 13 13 | 82 55 12 100
grg 113| 1 -1 -2 0 44 31 -.03 10 9 | 155 -187 8 117
igr n/a| 0 1 -2 2 -9 11 .06 6 5 | 3191 -436 14 75
jpl n/a| 1 0 0 1 -11 7 .21 24 25 | -372 -485 83 180
mit 358| 0 0 -3 -58 -28 -33 -.03 13 8 | -3955 346 580 8943
ngs 282| -1 0 5 -4 -39 -34 -.08 12 10 | -809 302 725 1594
sio 375| -1 0 -4 -106 138 15 -.07 14 10 | --- --- --- ---
Table 2.2258.4 GPS week: 2258 Day: 4 MJD: 60054.000
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 864| -1 0 0 25 9 -20 .01 6 6 | -703 212 5 106
esa 150| 0 0 1 1 18 5 -.06 10 10 | -1047 841 5 75
gfz 113| 0 2 -5 40 -22 -12 .13 13 14 | 234 -294 16 104
grg 115| 1 0 -2 -13 30 8 .01 11 9 | 151 -234 7 118
igr n/a| 0 1 -4 8 6 -9 .05 5 5 | 2876 305 14 90
jpl n/a| 0 0 0 15 -5 8 .17 23 24 | -757 162 75 168
mit 358| 0 0 -4 -30 -4 55 -.03 12 9 | 20311 148 71 9329
ngs 276| 1 0 6 -30 -56 -18 -.05 11 9 | -649 71 695 1594
sio 372| 0 0 -3 -86 151 0 -.03 14 10 | --- --- --- ---
Table 2.2258.5 GPS week: 2258 Day: 5 MJD: 60055.000
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 864| 0 0 0 20 3 20 .02 6 6 | -739 -151 5 97
esa 150| 1 0 3 14 -5 -3 -.04 10 10 | -701 -386 5 72
gfz 117| 0 0 -3 27 11 3 .06 11 11 | -72 266 13 96
grg 116| 0 0 -1 0 14 14 .06 11 10 | -83 -192 7 115
igr n/a| 0 0 -3 0 -2 31 .05 6 5 | 3364 924 13 77
jpl n/a| 0 0 2 24 -14 13 .17 24 25 | -351 475 77 150
mit 358| 0 0 -3 -63 -8 -52 -.04 10 8 | 10511 544 70 12574
ngs 287| 0 0 4 -17 -24 8 -.09 11 9 | -740 -150 1169 1958
sio 375| 0 0 -5 -117 114 -19 -.06 12 9 | --- --- --- ---
Table 2.2258.6 GPS week: 2258 Day: 6 MJD: 60056.000
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 864| -1 0 0 7 1 -8 .02 6 6 | -788 208 5 105
esa 150| 0 0 3 -2 -11 -22 -.06 10 10 | -729 220 6 76
gfz 124| 0 0 -2 25 2 -24 .06 11 10 | 503 -753 12 101
grg 125| 2 0 -2 -27 24 -2 .05 10 9 | 186 -534 8 144
igr n/a| 0 0 -2 -16 21 0 .03 5 5 | 4638 226 12 70
jpl n/a| 0 0 3 -4 -16 -4 .13 24 24 | 306 237 79 167
mit 358| 0 0 -3 -8 6 54 -.03 10 7 | 13342 165 67 14599
ngs 289| 1 0 7 -5 -24 -47 -.14 12 11 | -788 207 1146 1949
sio 375| 0 0 -5 -94 0 -22 -.09 13 10 | --- --- --- ---
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 3.2258.0 GPS week: 2258 Day: 0 MJD: 60050.000
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 | 20 18 32 12 6 --- 22 28 24 9 | 138 137 143 129 134 --- 135 140 133 135
2E | 7 12 13 10 9 10 14 12 21 5 | 30 38 37 30 36 31 32 37 33 32
3 | 5 9 6 6 3 11 5 12 14 3 | 39 41 39 39 41 45 38 41 39 39
4 | 5 5 6 6 6 53 8 9 13 3 | 66 67 69 68 66 76 69 71 63 68
5 | 7 7 9 5 5 10 9 10 15 3 | 47 46 49 47 46 50 48 46 47 47
6E | 8 8 12 13 8 19 11 14 18 5 | 26 26 27 27 26 32 28 28 33 25
7E | 7 11 7 8 6 12 10 12 12 4 | 53 55 58 57 56 56 59 56 61 56
8 | 6 8 7 4 3 12 7 15 14 3 | 29 33 30 31 31 35 30 31 32 30
9 | 4 8 5 5 4 13 7 6 15 2 | 26 27 28 25 28 37 29 28 29 27
10 | 5 9 6 5 4 10 10 8 19 3 | 43 43 43 42 43 45 42 43 41 43
11E | 11 20 15 13 6 55 33 13 41 8 | 40 45 44 42 40 44 47 38 52 41
12 | 7 7 10 7 6 13 8 10 13 3 | 43 41 46 44 44 42 45 44 48 43
13 | 5 9 8 7 5 13 10 13 16 3 | 32 34 36 32 35 38 32 40 32 33
14 | 6 11 9 9 4 54 9 10 11 4 | 32 40 36 39 36 59 36 34 41 35
15 | 7 6 9 5 5 8 11 9 20 3 | 57 60 60 56 58 63 58 55 53 57
16 | 5 6 6 5 6 12 10 14 19 3 | 31 31 32 32 29 32 30 34 35 31
17 | 7 5 9 7 6 10 10 7 13 3 | 40 40 45 43 45 45 41 40 42 41
18E | 7 31 14 14 12 58 40 24 44 10 | 61 65 59 64 62 62 65 67 64 61
19 | 6 5 11 7 4 9 11 11 16 3 | 35 36 43 36 39 39 37 35 37 36
20 | 7 6 8 7 6 10 10 11 15 3 | 36 37 39 37 37 35 36 37 37 37
21E | 8 12 9 22 7 10 10 12 15 6 | 26 32 26 28 30 32 29 33 30 28
X22 | 6 --- 9 8 10 11 4 12 --- 4 | 32 --- 37 33 35 34 35 34 --- 33
23 | 7 9 9 8 3 55 14 11 24 4 | 57 60 63 59 60 69 61 61 64 60
24 | 8 8 10 5 4 10 9 8 16 3 | 33 33 30 34 32 32 31 34 29 31
25 | 6 10 9 5 4 9 4 7 11 3 | 36 39 37 37 35 36 35 35 38 36
26 | 6 10 13 6 5 12 9 11 13 4 | 50 52 54 49 49 50 47 54 50 50
27 | 6 9 8 5 3 12 8 16 13 4 | 33 38 34 37 35 39 36 36 37 35
X28 | 9 17 --- 10 6 62 14 10 16 6 | 123 126 --- 123 121 129 118 122 81 122
29 | 6 7 8 7 4 9 8 9 14 3 | 33 31 36 32 32 33 33 31 31 32
30E | 6 8 11 8 4 13 9 14 14 4 | 39 38 47 43 39 36 40 37 45 40
31E | 9 7 12 8 4 9 9 11 11 4 | 65 62 63 66 63 65 62 66 61 63
32 | 6 8 8 3 3 11 7 8 14 3 | 42 41 41 38 39 45 37 41 34 39
------+---------------------------------------------------+----------------------------------------------------
RMS | 8 11 11 9 5 25 13 13 19 |T 46 48 46 46 46 47 46 47 46 46
WRMS | 6 9 10 7 5 25 10 11 14 |NE 44 46 42 45 45 48 44 46 43 44
MEDI | 6 8 9 7 5 12 9 11 15 |MD 39 40 41 39 39 42 37 38 41 39
Table 3.2258.1 GPS week: 2258 Day: 1 MJD: 60051.000
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 | 10 11 13 8 9 23 17 15 9 5 | 124 118 119 123 120 120 121 117 118 120
2E | 4 11 9 6 7 11 11 13 16 4 | 16 21 19 16 20 19 15 23 23 16
3 | 6 10 6 5 3 12 6 8 11 3 | 20 22 21 18 21 29 18 20 25 19
4 | 5 6 6 6 5 49 8 11 12 3 | 47 47 48 48 45 48 47 50 44 47
5 | 5 6 10 6 4 8 7 6 9 3 | 27 22 25 25 24 29 24 25 30 24
6E | 6 7 16 9 4 12 8 10 10 4 | 28 26 28 23 25 25 26 23 30 25
7E | 8 12 7 10 7 11 13 12 11 4 | 31 30 33 35 32 31 37 32 41 31
8 | 4 9 6 6 4 12 5 12 9 3 | 20 23 19 19 21 26 20 22 27 19
9 | 5 7 6 3 4 11 6 10 8 2 | 17 19 15 15 17 25 17 18 19 16
10 | 6 9 11 6 3 10 8 11 12 3 | 22 24 27 23 22 29 20 22 23 22
11E | 12 23 21 14 4 54 26 15 34 8 | 34 39 40 36 33 34 41 29 43 33
12 | 6 8 6 7 3 10 7 10 7 3 | 29 26 30 28 30 30 31 29 31 28
13 | 5 7 8 7 4 12 9 8 12 3 | 20 22 24 19 23 30 22 24 26 21
14 | 7 11 9 10 4 53 10 11 10 4 | 23 25 23 30 22 38 27 25 30 24
15 | 5 6 9 6 3 10 11 11 14 3 | 33 33 35 32 32 38 32 29 31 31
16 | 5 7 5 6 8 14 7 9 9 3 | 21 23 23 20 23 23 23 22 26 21
17 | 6 6 9 8 4 12 8 7 13 3 | 30 30 33 30 30 32 29 30 34 29
18E | 8 25 18 10 11 56 30 18 30 8 | 39 39 34 38 35 40 46 41 49 36
19 | 5 5 15 8 4 11 8 11 11 4 | 21 20 30 19 21 22 19 24 23 21
20 | 4 5 9 8 4 8 9 10 15 3 | 20 17 20 19 19 20 18 24 27 19
21E | 7 10 8 17 8 13 9 16 11 5 | 15 18 15 20 17 20 16 22 21 15
X22 | 9 --- 19 6 7 14 5 10 --- 5 | 19 --- 27 20 18 27 19 21 --- 18
23 | 6 10 9 7 4 57 11 11 12 4 | 28 30 30 31 26 34 30 27 33 28
24 | 8 8 7 9 4 12 8 9 14 3 | 22 21 20 22 20 25 18 19 20 19
25 | 7 12 13 7 3 11 6 8 7 4 | 23 29 27 23 22 25 21 24 24 23
26 | 4 10 11 4 5 11 8 10 11 3 | 29 33 32 29 31 32 28 29 34 29
27 | 4 9 6 7 3 9 5 11 9 3 | 27 31 27 27 28 32 29 28 31 27
X28 | 6 18 --- 14 5 59 12 8 15 6 | 88 87 --- 91 86 90 86 84 59 87
29 | 6 7 6 7 3 8 6 9 11 3 | 19 17 20 17 19 20 16 21 21 17
30E | 7 8 8 7 4 14 7 17 6 4 | 36 39 38 38 37 40 39 40 43 37
31E | 7 9 10 8 6 11 7 9 9 4 | 44 40 43 46 43 48 41 43 41 42
32 | 5 9 9 3 3 11 9 8 9 3 | 28 30 30 28 29 37 26 32 23 28
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 10 10 8 5 24 11 11 13 |T 31 32 30 31 30 34 31 31 33 30
WRMS | 6 10 10 7 5 25 8 10 11 |NE 28 30 27 28 28 32 27 29 29 27
MEDI | 6 9 9 7 4 12 8 10 11 |MD 27 26 27 25 24 30 26 25 30 24
Table 3.2258.2 GPS week: 2258 Day: 2 MJD: 60052.000
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 | 11 9 19 11 6 16 16 13 15 6 | 159 158 154 161 157 136 162 153 163 158
2E | 7 13 15 7 6 10 11 11 11 4 | 16 19 21 18 17 17 20 20 23 16
3 | 6 9 10 7 4 12 5 8 8 3 | 24 26 25 24 25 30 25 24 27 24
4 | 5 5 7 6 5 50 6 11 11 3 | 50 52 50 53 50 56 50 52 54 51
5 | 5 5 9 6 4 9 7 7 9 3 | 26 24 31 24 27 28 25 28 29 25
6E | 7 9 18 11 6 9 21 15 23 6 | 25 25 27 25 24 23 26 27 29 23
7 | 8 10 12 26 6 13 13 17 13 6 | 29 31 30 40 31 32 34 34 40 30
8 | 4 9 9 6 3 10 6 9 7 3 | 21 23 22 22 22 23 22 21 28 21
9 | 4 8 8 4 4 9 5 11 9 3 | 22 22 25 22 23 28 22 22 25 22
10 | 6 10 8 7 4 9 9 9 12 3 | 23 25 22 24 23 26 22 23 24 22
11E | 7 32 25 14 7 62 28 26 31 10 | 51 60 61 56 52 56 59 54 58 53
12 | 6 6 9 7 5 11 8 8 8 3 | 36 34 37 35 35 37 34 34 36 34
13 | 6 7 10 10 5 10 8 10 11 3 | 22 22 28 23 23 29 25 24 25 23
14 | 8 12 12 9 5 54 11 12 8 4 | 24 32 36 31 29 44 30 29 33 28
15 | 7 8 9 6 3 8 9 8 13 3 | 41 44 43 42 42 47 40 41 42 41
16 | 6 7 8 8 7 12 6 11 7 3 | 25 25 23 23 24 23 25 26 29 23
17 | 6 6 6 8 4 9 9 7 10 3 | 25 22 24 24 23 28 24 25 26 23
18E | 8 26 19 10 11 56 24 14 24 7 | 32 31 28 30 28 32 39 33 41 30
19 | 7 6 13 8 4 9 8 15 9 4 | 22 22 29 22 23 25 22 24 25 22
20 | 6 4 8 8 4 9 8 8 14 3 | 20 20 21 22 20 20 21 24 29 19
21E | 7 13 11 24 7 16 9 12 10 6 | 20 24 22 21 22 25 26 23 30 20
X22 | 6 --- 10 6 7 10 7 9 --- 3 | 28 --- 28 26 26 27 30 24 --- 26
23 | 7 10 13 9 5 57 9 10 9 4 | 25 28 30 28 27 38 31 25 33 26
24 | 7 7 6 9 5 14 6 11 10 3 | 28 26 24 29 25 29 26 25 32 25
25 | 5 11 9 6 5 9 7 7 14 3 | 25 28 26 26 26 28 24 25 29 24
26 | 7 11 11 5 6 13 8 12 8 4 | 29 30 29 28 27 30 29 30 32 28
27 | 5 9 6 8 4 11 6 8 8 3 | 26 30 27 27 27 29 28 26 32 26
X28 | 6 16 --- 14 6 62 10 12 20 6 | 80 81 --- 79 80 84 81 83 62 80
29 | 6 5 11 7 4 8 6 6 10 3 | 24 19 27 21 22 22 22 23 23 22
30 | 6 9 15 9 4 14 8 15 8 4 | 36 39 36 35 36 37 37 36 42 35
31E | 5 10 13 7 7 9 6 11 12 4 | 51 46 48 51 47 49 48 56 49 49
32 | 4 8 9 5 4 10 6 8 8 3 | 33 32 34 32 31 37 29 34 33 32
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 11 12 10 5 25 11 12 13 |T 34 35 34 35 34 36 35 35 38 33
WRMS | 6 9 12 8 5 25 8 10 10 |NE 31 31 29 31 30 34 31 31 33 30
MEDI | 6 9 10 8 5 10 8 11 10 |MD 25 28 28 26 26 29 26 26 32 25
Table 3.2258.3 GPS week: 2258 Day: 3 MJD: 60053.000
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 9 18 11 6 12 12 17 14 5 | 197 197 194 203 197 177 196 193 198 197
2E | 7 16 10 9 7 10 8 10 9 4 | 25 28 26 24 25 24 27 31 27 25
3 | 5 8 12 9 5 10 8 9 12 3 | 30 31 30 26 31 34 28 30 31 28
4 | 6 5 13 7 7 49 9 12 12 4 | 34 35 37 33 36 40 35 36 40 34
5 | 4 7 14 5 5 9 7 10 10 3 | 32 34 34 32 33 37 33 30 36 32
6E | 7 8 25 14 6 10 18 13 19 6 | 26 26 32 24 26 26 32 29 34 25
7 | 6 8 11 16 5 13 10 12 11 5 | 33 36 39 36 35 35 37 40 40 34
8 | 6 9 12 6 3 9 8 14 9 4 | 25 28 28 26 26 28 26 31 27 26
9 | 5 7 11 7 5 9 6 10 10 3 | 27 32 30 26 30 34 27 30 28 27
10M | 5 9 15 5 4 11 9 10 9 4 | 31 33 30 28 31 32 30 35 31 30
11E | 13 27 19 15 9 58 46 19 49 11 | 27 35 37 31 28 34 51 33 54 29
12 | 5 7 11 8 5 12 8 4 10 3 | 33 33 40 34 35 36 35 35 37 34
13 | 6 6 8 11 5 10 10 8 13 3 | 27 29 31 28 30 33 31 31 30 28
14M | 8 13 10 10 5 51 9 8 7 4 | 32 41 35 37 35 54 37 33 39 35
15 | 6 6 7 8 4 9 10 8 14 3 | 47 49 50 44 48 52 46 46 49 46
16 | 5 7 12 10 7 13 9 10 9 4 | 27 29 34 28 29 26 29 34 32 29
17 | 6 6 8 7 8 9 6 11 7 3 | 29 30 31 27 31 34 31 31 29 29
18E | 9 28 20 11 9 58 19 19 17 8 | 37 40 37 38 36 38 46 46 44 38
19 | 7 6 10 6 5 7 9 12 7 3 | 26 27 30 24 28 28 27 29 28 26
20 | 6 7 10 8 4 10 10 14 14 4 | 25 26 27 25 26 27 28 29 35 26
21E | 10 11 11 11 8 9 8 9 8 4 | 24 28 23 27 25 25 25 29 23 24
X22 | 5 --- 12 5 7 13 7 7 --- 3 | 26 --- 35 27 29 29 27 34 --- 28
23 | 6 9 13 9 3 57 10 10 9 4 | 27 32 29 33 31 49 34 36 34 31
24 | 7 8 10 11 5 11 9 11 13 4 | 33 33 33 33 33 34 31 34 34 32
25 | 4 12 11 7 4 8 5 7 9 3 | 29 34 33 30 31 33 32 31 35 30
26 | 5 11 14 5 4 15 7 12 9 4 | 33 34 40 33 34 31 32 38 34 34
27M | 6 10 12 9 4 9 7 15 10 4 | 30 31 29 31 30 31 30 35 29 29
X28 | 8 16 --- 13 8 62 8 10 --- 5 | 37 42 --- 39 38 44 42 42 --- 39
29 | 5 6 9 5 3 7 7 9 9 3 | 27 25 29 27 26 27 27 27 27 26
30 | 5 10 11 18 6 12 10 12 9 5 | 33 36 36 36 32 36 34 38 37 34
31 | 8 9 10 10 6 12 9 9 10 4 | 54 53 58 53 55 53 55 53 57 53
32 | 4 8 12 6 6 15 7 7 12 3 | 26 29 28 26 29 32 26 27 33 26
------+---------------------------------------------------+----------------------------------------------------
RMS | 7 11 13 10 6 24 13 12 14 |T 35 38 38 36 37 39 38 39 40 36
WRMS | 6 11 13 9 5 25 8 10 10 |NE 30 32 33 30 31 34 31 33 33 30
MEDI | 6 8 11 9 5 11 9 10 10 |MD 29 33 33 30 31 34 31 33 34 29
Table 3.2258.4 GPS week: 2258 Day: 4 MJD: 60054.000
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 9 22 12 9 10 17 13 16 5 | 386 387 394 388 388 395 393 379 392 387
2E | 7 13 11 8 6 9 11 8 13 4 | 31 34 29 29 32 33 31 33 33 30
3 | 5 9 12 7 4 9 5 11 11 3 | 34 34 35 32 35 37 30 34 36 33
4 | 5 5 6 7 6 48 7 9 10 3 | 61 60 59 59 61 62 56 61 63 60
5M | 6 6 14 8 4 8 9 7 14 3 | 38 34 38 36 37 37 35 34 39 35
6E | 5 8 28 12 6 8 9 12 8 5 | 29 28 33 25 28 28 25 28 31 26
7 | 6 9 12 13 4 9 10 13 14 4 | 34 33 36 34 35 35 34 38 39 34
8 | 5 11 11 6 3 12 6 10 8 3 | 30 32 30 28 30 30 27 33 30 29
9 | 4 8 9 6 3 10 6 8 11 3 | 29 29 29 25 28 32 24 26 30 26
10 | 7 9 10 9 5 11 10 6 14 3 | 46 48 50 46 48 50 45 45 51 46
11E | 11 20 18 15 9 51 44 20 44 10 | 48 45 49 48 44 44 48 45 55 43
12 | 6 7 9 8 4 10 6 11 7 3 | 49 46 48 47 47 48 44 50 45 47
13 | 8 5 11 21 5 12 8 9 13 5 | 29 29 29 32 30 34 26 32 32 28
14 | 7 16 9 11 6 55 10 11 10 5 | 49 51 47 52 52 61 47 51 48 49
15 | 6 6 13 9 3 7 10 9 15 4 | 49 48 52 44 48 48 42 44 48 46
16 | 5 7 7 10 7 14 7 8 9 3 | 36 36 34 33 35 36 34 33 37 34
17 | 7 5 9 9 5 9 6 7 9 3 | 39 36 39 38 39 42 36 41 40 38
18E | 12 25 17 12 9 57 17 12 20 7 | 46 46 42 45 43 46 48 44 52 44
19 | 6 6 9 6 4 9 10 9 8 3 | 32 30 34 31 32 36 30 35 31 31
20M | 5 6 12 10 4 9 8 9 19 3 | 33 29 35 32 32 33 31 33 39 31
21E | 8 11 13 20 8 9 10 13 11 5 | 30 33 35 29 34 29 29 35 35 30
X22 | 5 --- 15 5 7 10 6 12 --- 4 | 28 --- 33 28 28 32 28 31 --- 28
23 | 5 9 15 10 4 55 13 11 14 4 | 36 37 39 38 36 45 37 35 41 36
24 | 6 8 9 11 4 11 10 7 15 3 | 33 34 34 34 33 34 28 32 30 32
25 | 5 12 8 8 4 11 5 7 12 3 | 38 40 37 40 37 39 34 37 34 37
26 | 6 10 10 7 6 12 10 12 11 4 | 44 42 43 41 41 42 40 41 42 41
27 | 4 9 11 5 4 10 6 9 10 3 | 40 43 43 39 41 42 39 43 45 40
X28 | 7 15 --- 14 6 59 11 13 --- 6 | 83 81 --- 81 81 84 77 77 --- 80
29 | 4 4 12 6 4 9 5 6 7 2 | 31 28 31 29 30 32 26 30 28 29
30 | 4 8 8 13 4 13 9 11 10 4 | 35 34 34 36 34 35 33 34 38 34
31M | 9 8 14 11 6 9 7 15 9 4 | 64 63 63 61 63 63 61 59 68 62
32 | 4 6 15 6 4 10 10 10 12 4 | 39 38 40 38 40 44 34 38 42 37
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 10 13 11 5 23 12 11 14 |T 50 51 50 49 50 52 48 50 52 49
WRMS | 6 10 14 9 5 24 9 9 10 |NE 40 40 38 38 39 42 36 39 38 38
MEDI | 6 8 11 9 4 10 9 10 11 |MD 36 36 37 36 36 37 34 35 39 35
Table 3.2258.5 GPS week: 2258 Day: 5 MJD: 60055.000
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 | 5 9 25 13 7 11 13 11 15 5 | 761 769 780 769 764 746 781 754 768 768
2E | 7 12 11 8 8 10 11 9 10 4 | 20 21 22 18 19 22 24 25 18 20
3 | 4 8 7 7 4 9 7 12 10 3 | 22 22 21 21 22 24 19 21 22 20
4 | 6 6 5 7 6 51 8 10 10 3 | 37 38 38 40 36 42 41 36 37 38
5 | 5 6 10 7 3 10 8 14 10 3 | 55 55 56 56 55 57 55 55 56 54
6E | 5 8 19 13 5 8 8 12 9 4 | 31 28 26 27 28 29 26 32 28 27
7 | 6 10 14 12 5 12 6 12 12 4 | 23 24 29 28 24 25 25 28 31 24
8 | 5 10 8 12 4 11 5 14 6 4 | 22 23 20 21 22 24 17 24 20 19
9 | 4 6 5 4 3 9 6 7 13 2 | 24 23 24 25 24 27 20 22 29 22
10 | 6 9 7 11 4 8 9 7 11 3 | 56 54 57 54 54 56 55 56 52 55
11E | 9 18 14 18 8 51 31 17 36 8 | 65 67 67 64 65 67 68 66 72 64
12 | 6 5 7 10 5 10 7 8 7 3 | 28 27 28 31 27 30 29 25 28 27
13 | 7 7 10 10 5 12 9 13 13 4 | 30 29 32 32 29 31 27 33 31 29
14 | 7 13 7 11 5 52 9 9 8 4 | 91 91 92 94 91 96 94 91 91 92
15 | 6 7 15 9 4 9 11 7 14 4 | 34 36 41 31 36 37 31 32 34 34
16 | 4 7 6 11 7 16 6 9 11 3 | 22 21 22 21 21 20 19 21 22 20
17 | 7 7 10 11 5 8 9 8 11 3 | 21 19 26 20 23 26 21 24 21 20
18E | 8 23 15 10 10 58 15 12 15 6 | 23 26 22 25 22 27 32 26 30 23
19 | 7 7 10 9 4 7 12 6 8 3 | 19 21 23 19 21 25 25 23 22 20
20 | 6 6 10 7 6 10 14 13 17 4 | 20 19 22 18 20 22 23 22 27 19
21E | 9 12 9 9 6 8 12 11 8 4 | 19 21 21 19 20 19 18 24 22 18
X22 | 6 --- 9 6 8 8 6 10 --- 3 | 29 --- 27 29 24 26 26 26 --- 26
23 | 6 9 12 12 6 58 12 10 10 4 | 34 37 33 35 35 40 36 36 37 34
24 | 8 8 8 17 5 13 9 8 13 4 | 24 26 25 28 25 28 23 25 26 24
25 | 6 12 9 11 5 10 5 9 8 4 | 22 27 23 26 22 26 21 20 22 22
26 | 6 9 9 9 6 16 8 14 6 4 | 22 23 23 24 20 23 22 23 21 21
27 | 3 8 8 11 4 10 5 9 8 3 | 28 31 28 27 29 32 28 30 30 28
X28 | 8 13 --- 12 6 60 8 8 --- 5 | 79 80 --- 80 80 86 81 80 --- 79
29 | 4 4 6 9 4 12 5 8 8 2 | 22 21 21 21 21 26 19 22 21 21
30 | 4 8 13 11 3 13 7 12 11 4 | 24 28 25 27 25 26 23 26 30 24
31 | 10 6 14 10 7 10 6 11 9 4 | 50 48 52 52 49 51 52 54 50 51
32 | 5 6 9 6 4 11 6 6 9 2 | 23 24 23 25 23 30 24 25 23 23
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 10 11 11 6 24 10 11 12 |T 55 57 56 56 55 57 56 56 57 55
WRMS | 6 10 11 10 5 25 8 9 9 |NE 28 29 26 29 28 31 27 28 26 27
MEDI | 6 8 9 10 5 10 8 10 10 |MD 24 27 26 27 24 27 25 26 28 24
Table 3.2258.6 GPS week: 2258 Day: 6 MJD: 60056.000
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 21 11 6 11 12 12 11 5 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
2E | 6 13 8 8 7 8 7 12 10 4 | 20 20 19 21 17 19 26 22 22 20
3 | 3 9 7 7 4 8 6 12 9 3 | 31 30 31 28 31 32 33 29 28 30
4 | 6 3 10 6 7 51 7 10 9 3 | 65 65 64 66 63 71 67 67 63 66
5 | 5 6 5 8 4 8 9 13 14 3 | 81 80 80 79 80 80 79 81 78 80
6E | 7 8 16 10 5 11 7 12 8 4 | 41 39 44 39 39 40 42 42 39 40
7 | 5 9 13 12 6 10 7 17 12 4 | 33 33 34 34 34 34 34 37 36 33
8 | 5 9 10 10 5 14 6 14 7 4 | 29 29 28 27 27 29 28 28 26 28
9 | 5 7 6 4 5 11 7 10 10 3 | 27 27 26 30 28 34 28 29 27 27
10 | 5 9 10 9 5 9 9 9 13 3 | 85 87 84 86 86 86 85 85 87 85
11E | 12 18 17 13 8 50 31 17 39 8 | 95 97 96 97 95 97 107 95 106 97
12 | 6 8 10 13 5 12 7 13 10 4 | 48 47 51 52 49 51 48 49 47 49
13 | 7 5 7 8 4 11 9 10 14 3 | 34 34 34 37 36 38 38 39 38 35
14 | 6 14 8 9 6 54 6 12 10 4 | 131 134 133 134 132 139 131 132 131 132
15 | 7 6 7 7 3 10 10 8 15 3 | 54 53 49 50 52 56 52 45 49 51
16 | 4 6 6 10 7 15 6 16 8 3 | 36 36 33 36 35 36 36 33 32 35
17 | 6 6 8 10 5 10 6 11 7 3 | 29 28 31 29 30 34 31 31 29 29
18E | 6 22 10 8 8 56 14 15 15 6 | 35 38 34 41 35 40 42 38 39 37
19 | 7 6 12 8 3 10 8 12 11 4 | 27 27 31 27 27 31 27 30 28 27
20 | 6 5 8 8 4 8 10 12 15 3 | 23 22 24 24 24 24 26 28 28 23
21E | 8 12 12 14 6 9 7 14 12 5 | 30 30 31 31 29 31 34 35 29 31
X22 | 7 --- 10 4 8 7 4 9 --- 3 | 35 --- 35 35 34 36 37 34 --- 35
23 | 7 10 18 9 4 54 12 9 14 5 | 36 39 34 36 38 52 41 38 40 36
24 | 8 9 11 13 4 9 8 13 10 4 | 38 37 33 37 35 37 39 35 37 36
25 | 7 12 7 12 5 8 5 9 9 4 | 36 38 36 39 35 40 37 38 37 37
26 | 6 10 12 8 5 13 6 15 8 4 | 35 38 37 38 34 38 37 36 35 36
27 | 4 8 10 7 4 13 6 14 8 3 | 42 41 40 42 40 41 40 40 39 40
X28 | 8 13 --- 14 7 62 9 13 13 5 | 120 121 --- 123 120 126 123 120 114 121
29 | 5 4 7 10 5 9 6 10 7 3 | 29 25 28 28 26 29 25 26 25 27
30 | 5 10 16 11 5 13 6 18 11 4 | 33 36 33 35 34 36 33 39 34 34
31 | 9 7 10 16 5 9 7 12 10 4 | 82 79 80 86 80 81 82 84 80 82
32 | 5 8 9 6 5 11 7 9 10 3 | 35 37 36 36 35 41 36 36 34 36
------+---------------------------------------------------+----------------------------------------------------
RMS | 6 10 11 10 5 24 10 12 13 |T 47 48 44 48 47 50 49 48 47 47
WRMS | 6 10 10 9 5 24 7 11 10 |NE 41 41 36 41 40 45 42 41 40 41
MEDI | 6 8 10 9 5 11 7 12 10 |MD 35 37 34 37 35 38 37 38 37 36
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 4.2258 GPS week: 2258 MJD: 60050.0-60056.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 |U 10 10 26 |U 11 19 40 |U 12 7 28 |
esa | esa 2976 | 13 17 33 |U 11 22 40 |U 12 12 31 |
gfz | gfz 2973 |U 9 10 22 |U 11 17 39 | 12 8 30 |
grg | grg 3067 |U 10 12 27 |U 12 20 39 | 12 9 29 |
igr | igr 3069 | 9 11 22 | 10 18 36 | 10 8 24 |
igs | igs 3071 | 9 11 23 | 11 19 37 | 11 7 25 |
jpl | jpl 3058 | 12 13 35 | 11 21 35 | 13 13 33 |
mit | mit 3072 |U 23 24 49 |U 31 39 121 |U 35 30 95 |
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 5.2258.0 GPS week: 2258 Day: 0 MJD: 60050.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 13 24 | 15 32 57 | 14 7 29 |
esa | esa 2976 | 13 20 26 | 15 31 58 | 12 12 31 |
gfz | gfz 2976 | 9 12 18 | 17 29 60 | 12 8 31 |
grg | grg 3072 | 10 16 30 | 14 29 47 | 14 13 31 |
igr | igr 3072 | 9 15 19 | 15 30 57 | 11 8 26 |
igs | igs 3071 | 9 13 20 | 15 30 57 | 12 9 26 |
jpl | jpl 2976 | 14 19 32 | 14 30 48 | 14 14 29 |
mit | mit 3072 | 17 25 44 | 74 59 250 | 142 84 374 |
Table 5.2258.1 GPS week: 2258 Day: 1 MJD: 60051.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 8 22 | 12 21 41 | 12 6 29 |
esa | esa 2976 | 13 15 28 | 12 25 54 | 12 13 28 |
gfz | gfz 2975 | 8 6 17 | 12 18 40 | 12 8 26 |
grg | grg 3069 | 11 9 24 | 14 21 42 | 12 8 27 |
igr | igr 3062 | 9 9 16 | 11 19 37 | 10 8 22 |
igs | igs 3072 | 10 9 18 | 12 20 39 | 11 7 26 |
jpl | jpl 3072 | 11 12 31 | 14 22 38 | 12 14 30 |
mit | mit 3072 | 17 16 46 | 15 27 62 | 21 13 53 |
Table 5.2258.2 GPS week: 2258 Day: 2 MJD: 60052.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 10 27 | ---- ---- ---- | 11 8 30 |
esa | esa 2976 | 12 13 26 | ---- ---- ---- | 12 15 31 |
gfz | gfz 2970 | 9 8 25 | ---- ---- ---- | 12 11 34 |
grg | grg 3062 | 11 13 30 | ---- ---- ---- | 13 12 33 |
igr | igr 3072 | 8 9 20 | ---- ---- ---- | 10 9 24 |
igs | igs 3072 | 9 9 22 | ---- ---- ---- | 12 9 28 |
jpl | jpl 3072 | 10 10 25 | ---- ---- ---- | 13 15 29 |
mit | mit 3072 | 21 50 70 | ---- ---- ---- | 34 48 83 |
Table 5.2258.3 GPS week: 2258 Day: 3 MJD: 60053.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3067 | 10 8 19 | 10 17 36 | 9 7 29 |
esa | esa 2976 | 13 15 31 | 9 19 32 | 11 12 27 |
gfz | gfz 2973 | 10 12 12 | 9 12 34 | 13 11 33 |
grg | grg 3065 | 8 8 16 | 11 18 36 | 10 8 28 |
igr | igr 3061 | 8 8 13 | 9 15 33 | 9 9 23 |
igs | igs 3066 | 8 8 14 | 9 16 32 | 9 7 24 |
jpl | jpl 3072 | 11 10 30 | 9 18 33 | 12 15 30 |
mit | mit 3072 | 57 20 58 | 42 64 199 | 11 35 52 |
Table 5.2258.4 GPS week: 2258 Day: 4 MJD: 60054.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 12 46 | ---- ---- ---- | 13 7 23 |
esa | esa 2976 | 13 19 56 | ---- ---- ---- | 13 11 37 |
gfz | gfz 2972 | 9 13 45 | ---- ---- ---- | 13 7 29 |
grg | grg 3067 | 10 14 49 | ---- ---- ---- | 13 8 26 |
igr | igr 3072 | 9 14 48 | ---- ---- ---- | 11 8 24 |
igs | igs 3072 | 9 13 47 | ---- ---- ---- | 12 7 23 |
jpl | jpl 3072 | 11 16 55 | ---- ---- ---- | 15 12 39 |
mit | mit 3072 | 10 9 36 | ---- ---- ---- | 14 12 25 |
Table 5.2258.5 GPS week: 2258 Day: 5 MJD: 60055.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 11 23 | 8 13 26 | 11 7 28 |
esa | esa 2976 | 17 18 31 | 8 18 26 | 11 10 29 |
gfz | gfz 2975 | 10 9 18 | 7 11 23 | 10 6 29 |
grg | grg 3071 | 12 11 21 | 11 15 34 | 11 6 29 |
igr | igr 3072 | 11 11 19 | 7 13 21 | 9 7 25 |
igs | igs 3072 | 12 11 20 | 7 14 23 | 10 6 26 |
jpl | jpl 3072 | 15 14 35 | 7 17 24 | 14 10 32 |
mit | mit 3072 | 16 16 41 | 10 18 39 | 12 12 42 |
Table 5.2258.6 GPS week: 2258 Day: 6 MJD: 60056.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 12 22 | 9 13 40 | 11 8 26 |
esa | esa 2976 | 14 19 34 | 10 18 30 | 11 13 33 |
gfz | gfz 2976 | 8 11 21 | 11 14 37 | 11 8 29 |
grg | grg 3063 | 9 12 22 | 11 15 34 | 12 9 29 |
igr | igr 3072 | 9 12 22 | 10 13 33 | 9 9 25 |
igs | igs 3072 | 9 12 21 | 9 14 35 | 10 7 24 |
jpl | jpl 3072 | 13 12 41 | 10 16 31 | 12 12 40 |
mit | mit 3072 | 20 30 45 | 12 26 55 | 11 9 35 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.2258 GPS week: 2258 MJD: 60050.500-60056.500
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 | -4 -21 56 3 3 | 6 20
| 16 14 18 39 5 | 3
esa uuuuu | 4 -14 65 108 0 | 23 31
| 13 7 36 37 3 | 4
gfz uuuuu | -8 -23 -37 -3 -2 | 11 25
| 13 10 43 99 7 | 4
grg uuuuu | -30 3 -43 8 0 | 14 23
| 18 8 53 113 6 | 4
igr xxxxx | -2 -7 33 38 1 | 1 19
| 13 7 39 26 3 | 3
irf xxxxx | 11 3 -38 5 -5 | 0 20
| 9 9 26 15 10 | 6
mit uuuuu | 19 54 -84 -185 -8 | 23 31
| 15 22 26 66 9 | 6
ngs uuuuu | 31 11 -9 114 1 | 9 20
| 31 21 106 127 3 | 3
sio xxxxx | -12 22 -338 -103 -16 | 24 38
| 49 57 134 77 22 | 9
Table 7.2258.0 GPS week: 2258 Day: 0 MJD: 60050.500
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 -38 77 -49 0 | 3 17
esa uuuuu | 9 -4 18 167 -3 | 22 29
gfz uuuuu | -22 -14 2 31 5 | 10 21
grg uuuuu | -33 -2 26 -34 3 | 12 21
igr xxxxx | 5 -3 42 20 -1 | -2 16
irf xxxxx | 10 12 -65 27 -9 | 1 20
mit uuuuu | 22 54 -112 -183 -15 | 25 31
ngs uuuuu | 29 36 -92 109 0 | 8 17
sio xxxxx | -44 53 -267 -35 -48 | 33 42
Table 7.2258.1 GPS week: 2258 Day: 1 MJD: 60051.500
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 -20 76 60 4 | 6 18
esa uuuuu | 22 -18 98 129 -1 | 25 32
gfz uuuuu | -11 -43 -15 -145 2 | 13 24
grg uuuuu | -32 12 8 -162 -3 | 16 24
igr xxxxx | 8 2 -22 50 2 | 2 17
irf xxxxx | 29 -9 -63 17 -14 | 4 19
mit uuuuu | 20 47 -65 -110 -17 | 27 33
ngs uuuuu | 79 28 -191 298 2 | 11 19
sio xxxxx | -76 -47 -84 -102 -28 | 31 42
Table 7.2258.2 GPS week: 2258 Day: 2 MJD: 60052.500
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 | 6 4 63 -26 13 | 8 20
esa uuuuu | -6 -20 45 71 -2 | 27 33
gfz uuuuu | 2 -22 -74 -146 -9 | 15 25
grg uuuuu | -31 -10 -36 -14 -7 | 19 26
igr xxxxx | -15 -12 11 11 2 | 4 18
irf xxxxx | 2 -4 -45 0 -14 | 5 19
mit uuuuu | -6 12 -115 -88 -16 | 28 33
ngs uuuuu | 42 33 99 256 3 | 12 21
sio xxxxx | 54 -70 -380 -4 -38 | 31 41
Table 7.2258.3 GPS week: 2258 Day: 3 MJD: 60053.500
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 -21 25 29 3 | 10 21
esa uuuuu | -4 -7 34 99 2 | 27 33
gfz uuuuu | -8 -27 23 41 6 | 15 25
grg uuuuu | -62 0 -68 -44 -8 | 18 26
igr xxxxx | 8 -6 55 22 7 | 5 18
irf xxxxx | 11 -5 -26 15 -12 | 4 19
mit uuuuu | 46 59 -68 -179 -13 | 27 33
ngs uuuuu | 13 2 55 61 2 | 13 21
sio xxxxx | 4 27 -427 -175 -13 | 27 41
Table 7.2258.4 GPS week: 2258 Day: 4 MJD: 60054.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -15 -37 43 -2 0 | 9 20
esa uuuuu | -17 -16 87 58 -4 | 25 31
gfz uuuuu | 4 -21 -45 70 -6 | 14 24
grg uuuuu | -32 11 -79 7 6 | 16 23
igr xxxxx | 2 -18 4 88 -2 | 5 18
irf xxxxx | 3 11 -51 -15 -2 | 0 18
mit uuuuu | 21 85 -96 -228 -3 | 24 30
ngs uuuuu | 55 -1 34 132 2 | 12 20
sio xxxxx | -7 81 -411 -111 -5 | 23 37
Table 7.2258.5 GPS week: 2258 Day: 5 MJD: 60055.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 -23 55 -24 -1 | 3 23
esa uuuuu | 8 -15 114 124 -1 | 17 29
gfz uuuuu | -28 -17 -100 72 -10 | 7 27
grg uuuuu | -2 1 -127 171 6 | 10 22
igr xxxxx | 2 -11 97 43 -2 | -1 22
irf xxxxx | 14 13 -27 -8 8 | -8 23
mit uuuuu | 11 65 -84 -237 2 | 16 27
ngs uuuuu | 17 -4 79 -39 1 | 6 22
sio xxxxx | -55 52 -488 -225 12 | 13 33
Table 7.2258.6 GPS week: 2258 Day: 6 MJD: 60056.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 -17 51 33 1 | 2 23
esa uuuuu | 15 -22 60 107 6 | 16 29
gfz uuuuu | 4 -20 -48 59 -5 | 5 28
grg uuuuu | -21 7 -22 133 4 | 9 22
igr xxxxx | -25 -6 43 30 -3 | -3 23
irf xxxxx | 11 3 8 -1 9 | -9 23
mit uuuuu | 16 57 -46 -268 3 | 14 27
ngs uuuuu | -18 -18 -50 -16 -6 | 5 22
sio xxxxx | 39 56 -309 -68 4 | 11 31
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