[IGSREPORT-21413] Wk 1702 IGS Final Orbits [Resubmission]
IGS ACC
igs.acc at noaa.gov
Mon Dec 17 07:17:08 PST 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1702 (Aug 19, 2012 - Aug 25, 2012)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
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:
igs1702[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1702[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1702[0-6].cls IGS GPS clock combination summary report.
igs17027.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17027.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, 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 | 9 27 9 27 KOUC KOUC
0 | EMR | 9 9
0 | ESA | 9 27 9 27 TLSE NNOR TLSE
0 | GFZ | 9 23 27 LHAZ TLSE
0 | GRG | CAGZ CAGZ NRMD
0 | JPL | 9
0 | MIT | 18 26 28 18 26 28 MAC1
1 | COD | 9 27 9 27 KOUC FLRS KOUC XMIS
1 | EMR | 9 YELL
1 | ESA | 9 27 9 27 HOLM YAKT
1 | GFZ | 9 23 27 ARTU HOB2 LHAZ NRMD NYAL SCOR THTI YELL
1 | GRG | USNO WROC YEBE HOLM SOFI USNO WROC
1 | JPL | 27
1 | MIT | 26 28 26 28 TLSE SOFI TLSE
2 | COD | 27 27 FLRS TLSE
2 | EMR | 9 9 THTI
2 | ESA | 27 27 NNOR THTI
2 | GFZ | 9 23 27 SANT
2 | GRG | 9 9 THTI WROC WROC
2 | JPL | 9
2 | MIT | 9 26 9 26 IRKJ GMAS
3 | COD | 9 27 9 27 KOUC FLRS KOUC
3 | ESA | 9 27 9 27 MATE ARTU OHI2
3 | GFZ | 9 27 BOR1 HOB2 MATE SANT TWTF UNSA
3 | GRG | HOB2 SPT0 BRUX HOB2 IRKJ SPT0 WIND
3 | JPL | 9 27
3 | MIT | IRKJ
4 | COD | 9 27 9 27 KOUC KARR KOUC
4 | EMR | 9 9
4 | ESA | 9 27 9 27 NNOR
4 | GFZ | 9 23 27 NYAL
4 | GRG | WROC KIT3 LHAZ WROC
4 | JPL | REUN
4 | MIT | 1 1 KARR
5 | COD | 9 27 9 27 KOUC KOUC
5 | EMR | CHUR CHUR MATE
5 | ESA | 9 27 9 27 IRKJ MATE NNOR
5 | GFZ | 9 23 27 HOB2 THTI WUHN
5 | GRG | 13 13 HOB2 MATE WROC BUCU HOB2 WROC
5 | MIT | 28 28 SPT0 BAKO SPT0
6 | COD | 9 27 8 9 27 CHUR CHUR FLRS
6 | EMR | MCM4 MCM4 THTI
6 | ESA | 8 9 27 8 9 27 TIXI
6 | GFZ | 8 9 23 27 30 ALRT INVK IRKJ
6 | GRG | USNO YEBE BRMU GOLD KIT3 LHAZ USNO
6 | JPL | 8
6 | MIT | 28 28 DAV1 IRKJ
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
7. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
EMR | 0 | 1.0 -3.4 -9.6 -13 16 -16 -.27
ESA | 0 | 6.0 -2.0 24.2 -22 -4 134 -.65
GFZ | 0 | -.5 1.2 .5 -48 -18 -18 -.53
GRG | 0 | 7.3 -5.1 24.6 -43 24 -32 -.44
JPL | 0 | 1.6 .9 -2.5 -22 -3 -17 -.18
MIT | 0 | 2.3 -2.5 13.9 -16 17 -40 -.44
NGS | 0 | 6.8 -2.4 21.6 -17 -42 -4 -.25
EMR | 1 | 2.2 -.8 -2.8 -6 -1 -10 -.29
ESA | 1 | 4.6 2.3 22.3 58 -33 110 -.60
GFZ | 1 | -.4 .7 .4 -67 -22 -23 -.41
GRG | 1 | 7.1 -15.5 21.5 -30 18 -25 -.48
JPL | 1 | -2.2 3.8 .4 -73 -21 -22 -.20
MIT | 1 | 3.9 3.2 10.6 -17 20 -50 -.43
NGS | 1 | -.2 5.2 14.4 25 2 -4 -.21
EMR | 2 | -.4 -7.6 -1.5 -4 5 -12 -.27
ESA | 2 | 3.0 5.4 21.3 101 3 71 -.52
GFZ | 2 | -.7 2.0 -.4 -30 -21 -20 -.34
GRG | 2 | .0 -10.2 20.1 -36 -6 -32 -.30
JPL | 2 | -6.4 2.4 -2.4 5 -69 10 -.27
MIT | 2 | 2.2 .4 10.7 -14 14 -48 -.43
NGS | 2 | 4.0 -.8 13.0 -19 -35 -2 -.15
EMR | 3 | 2.8 -4.3 -1.1 -4 6 -14 -.24
ESA | 3 | -1.5 3.5 18.6 82 24 101 -.71
GFZ | 3 | -.2 .7 -.1 -40 -18 -19 -.51
GRG | 3 | 3.7 -1.1 18.7 -37 23 -16 -.15
JPL | 3 | -2.3 11.0 -.5 24 1 -14 -.22
MIT | 3 | 3.5 .7 11.7 -17 9 -48 -.50
NGS | 3 | .8 4.9 16.3 13 -20 -2 -.37
EMR | 4 | 3.1 3.2 -3.7 -8 5 -3 -.12
ESA | 4 | -2.1 4.4 26.4 95 88 74 -.90
GFZ | 4 | -1.3 .8 -.3 -61 0 -17 -.39
GRG | 4 | 4.6 -5.9 14.5 -29 22 -8 -.33
JPL | 4 | -3.9 6.7 .3 39 12 14 -.14
MIT | 4 | 4.2 3.3 13.2 -18 15 -42 -.46
NGS | 4 | -3.0 -.2 5.4 -35 6 -3 -.17
EMR | 5 | .4 -5.2 -1.3 -7 14 -16 -.16
ESA | 5 | -2.0 6.3 23.6 135 70 74 -.66
GFZ | 5 | -.8 .9 .9 -37 -6 -17 -.50
GRG | 5 | 4.3 -2.6 22.4 -49 37 -35 -.46
JPL | 5 | .6 4.5 2.2 17 0 14 -.09
MIT | 5 | 3.3 3.0 12.7 -19 16 -51 -.31
NGS | 5 | 3.4 1.5 18.9 -14 -38 6 -.20
EMR | 6 | 3.1 -.3 4.2 -7 9 -10 -.24
ESA | 6 | 2.6 .6 20.7 43 -19 105 -.52
GFZ | 6 | -.6 .6 .5 -45 -12 -8 -.39
GRG | 6 | 2.8 3.3 14.0 -35 19 5 -.50
JPL | 6 | -.2 6.0 3.2 -28 -6 -18 -.19
MIT | 6 | 3.6 1.3 12.9 -21 18 -70 -.24
NGS | 6 | 1.8 -6.4 7.5 -67 -22 -2 -.27
8. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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.
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 1.1702.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1702.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 2.1702.[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 3.1702.[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 5.1702.0-6). 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 1702 summary. (Aug 19, 2012 - Aug 25, 2012)
Table 1.1702.a GPS week: 1702 MJD: 56158.000-56164.000
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 257| 0 0 2 71 -9 25 -.53 12 11 | -485 86 19 72
| 0 0 2 24 19 21 .02 | 534 916
emr 78| -1 -2 -7 -25 -15 -21 .15 16 16 | 2832 -309 15 106
| 0 1 2 20 18 7 .02 | 1223 895
esa 177| 0 0 0 66 40 5 .03 7 7 | -1101 387 17 133
| 1 0 2 34 26 21 .02 | 346 419
gfz 187| -1 1 -2 -1 -65 -10 -.46 10 9 | 60 214 23 150
| 0 0 0 16 24 14 .01 | 374 587
grg n/a| 2 0 11 -23 -25 10 .35 14 13 | 90 -7 18 148
| 1 0 1 23 17 9 .06 | 225 516
igr n/a| 0 0 0 -4 -8 -6 -.23 4 4 | 8278 -526 22 93
| 0 0 0 15 25 11 .05 | 1681 755
jpl 80| 0 0 -4 12 2 11 .34 14 13 | 3336 -435 20 121
| 1 1 2 24 27 19 .03 | 1581 853
mit 239| 0 0 0 -11 13 4 -.27 10 10 | -3 -51 23 183
| 0 0 0 12 16 18 .03 | 257 551
ngs 234| 0 0 1 -62 19 -5 .22 11 9 | -519 107 2055 3614
| 0 1 4 22 23 14 .04 | 477 833
sio 273| 1 2 -2 -16 -15 16 -.29 20 19 | --- --- --- ---
| 1 1 1 25 12 17 .03 | --- ---
Table 1.1702.b GPS week : 1702 MJD: 56158.000-56164.000
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 | 5 5 5 5 5 5 5 |
2 | 5 4 5 5 5 4 5 |
3 | 4 4 4 4 4 4 4 |
4 | 4 5 4 4 4 4 3 |
5 | 4 4 5 4 4 5 4 |
6 | 5 4 4 4 4 4 4 |
7 | 5 6 5 5 5 6 5 |
8 | 4 4 4 4 5 5 5 |
9 | 5 5 5 5 5 5 6 |
10 | 4 3 4 4 3 4 4 |
11 | 4 4 5 4 5 4 4 |
12 | 6 5 4 5 5 5 5 |
13 | 4 4 4 5 5 5 4 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 5 4 |
17 | 5 5 5 5 5 5 4 |
18 | 4 4 4 4 4 4 4 |
19 | 5 5 5 5 5 5 4 |
20 | 4 5 5 4 4 5 5 |
21 | 5 4 5 6 5 5 5 |
22 | 4 4 4 4 4 4 4 |
23 | 5 5 5 5 5 5 5 |
25 | 5 5 5 4 5 5 4 |
26 | 4 4 4 4 4 4 4 |
27 | 5 5 6 5 5 6 6 |
28 | 5 4 5 5 5 5 5 |
29 | 5 5 5 5 5 5 4 |
30 | 4 4 4 4 4 5 3 |
31 | 5 5 5 5 5 5 5 |
32 | 4 4 4 4 4 5 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1702.0 GPS week: 1702 Day: 0 MJD: 56158.000
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 257| 0 0 -1 119 -18 26 -.52 11 11 | -335 3 21 86
emr 72| -3 -2 -11 11 -2 -15 .18 16 16 | 4088 -993 16 97
esa 177| 2 0 0 18 12 30 .02 7 7 | -640 -88 17 151
gfz 188| -1 2 -1 -27 -36 -18 -.44 9 9 | 503 -119 22 160
grg n/a| 3 0 12 8 -25 1 .33 15 14 | 327 -200 18 129
igr n/a| 0 0 -1 27 -22 -22 -.31 5 5 | 10837 -1370 25 99
jpl 80| -1 2 -8 65 -34 15 .34 14 13 | 5629 -1278 20 118
mit 240| 0 0 0 -8 18 -10 -.31 10 10 | 228 -291 27 164
ngs 235| 0 -1 5 -33 45 -15 .28 10 8 | -492 399 2111 3801
sio 275| 1 2 -3 7 -31 -7 -.25 22 19 | --- --- --- ---
Table 2.1702.1 GPS week: 1702 Day: 1 MJD: 56159.000
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 257| 0 -1 1 77 25 61 -.53 14 13 | -1115 1011 26 87
emr 80| 0 -2 -8 -43 8 -10 .16 16 16 | 2526 842 13 111
esa 177| 0 0 2 73 13 24 .05 7 6 | -1504 291 17 164
gfz 188| -1 1 -2 5 -75 -33 -.46 9 8 | -47 207 24 159
grg n/a| 3 0 12 0 9 14 .33 15 14 | 30 -186 18 152
igr n/a| 0 0 0 -18 26 -10 -.27 4 4 | 8991 246 24 119
jpl 80| 0 0 -4 7 -2 9 .37 14 13 | 3847 343 19 129
mit 240| 0 0 0 -8 15 -16 -.28 9 9 | -186 92 21 178
ngs 230| 0 0 0 -96 47 13 .24 10 9 | -1050 820 2117 3629
sio 270| 1 3 -2 -15 -2 -2 -.27 21 18 | --- --- --- ---
Table 2.1702.2 GPS week: 1702 Day: 2 MJD: 56160.000
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 257| 0 -1 1 68 -1 2 -.55 12 10 | 118 -1020 23 70
emr 81| -1 -5 -9 -40 -29 -22 .13 16 16 | 4482 470 14 105
esa 177| -1 1 0 75 65 4 .02 7 7 | -793 352 17 124
gfz 187| -1 2 -1 2 -74 -6 -.45 10 9 | -45 556 24 144
grg n/a| 2 0 10 -33 -49 -4 .26 15 14 | -44 513 19 157
igr n/a| 0 0 0 -19 12 1 -.23 5 4 | 9439 204 23 88
jpl 80| 3 -1 -3 17 13 24 .31 14 13 | 4495 482 21 109
mit 238| 0 0 0 -9 29 -5 -.26 12 12 | 65 120 23 177
ngs 233| 0 1 2 -76 -13 -2 .21 10 8 | 45 -969 2219 3643
sio 271| 2 1 -3 -31 -6 19 -.30 20 19 | --- --- --- ---
Table 2.1702.3 GPS week: 1702 Day: 3 MJD: 56161.000
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 257| 0 0 4 60 -4 28 -.54 12 10 | -994 458 18 74
emr 76| -1 -3 -7 -9 -9 -20 .14 16 16 | 3230 -441 17 116
esa 177| -1 -1 0 63 29 19 .05 7 7 | -1588 988 16 120
gfz 189| 0 2 -3 6 -75 -16 -.46 9 8 | -531 1023 22 157
grg n/a| 4 -1 11 -26 -29 21 .32 14 13 | -208 781 20 152
igr n/a| 0 0 0 -5 -2 -4 -.27 5 4 | 8511 -557 20 82
jpl 80| 0 0 -4 3 35 5 .35 13 13 | 3799 -559 19 110
mit 239| 0 0 0 -16 32 -3 -.29 9 9 | -408 815 26 223
ngs 234| 0 2 2 -59 -1 -9 .21 10 9 | -992 360 1920 3612
sio 269| 1 3 0 -8 -5 33 -.29 19 20 | --- --- --- ---
Table 2.1702.4 GPS week: 1702 Day: 4 MJD: 56162.000
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 257| 0 -1 3 68 -35 -1 -.54 12 11 | -975 1300 14 65
emr 81| -1 -1 -7 -43 -4 -18 .11 16 16 | 2628 -842 15 121
esa 177| 0 0 3 78 83 -31 -.00 8 8 | -1078 691 18 126
gfz 186| -1 2 -2 18 -99 6 -.47 10 10 | -63 174 25 142
grg n/a| 0 0 10 -22 -34 13 .39 12 11 | -88 156 17 159
igr n/a| 0 0 1 -6 -7 -10 -.18 4 4 | 7454 -768 21 85
jpl 80| 1 0 -4 6 37 16 .30 14 13 | 2665 -837 21 130
mit 239| 0 0 0 -4 -16 9 -.22 11 12 | -180 259 23 194
ngs 238| -1 0 -2 -80 2 16 .14 9 9 | -929 1192 1813 3490
sio 273| 0 1 -2 -20 -30 20 -.33 19 18 | --- --- --- ---
Table 2.1702.5 GPS week: 1702 Day: 5 MJD: 56163.000
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 257| 0 0 2 37 -23 29 -.49 12 10 | 115 -1059 16 56
emr 81| -2 -3 -7 -32 -42 -31 .15 15 15 | 1934 -1586 17 93
esa 177| 0 0 -3 123 45 -1 .06 8 8 | -1117 -164 20 129
gfz 187| -1 1 -1 -21 -29 -14 -.46 9 9 | 567 -838 23 144
grg n/a| 1 0 13 -63 -22 11 .42 14 13 | 235 -511 19 143
igr n/a| 0 0 0 0 -53 12 -.20 4 4 | 6832 -1572 20 78
jpl 80| 0 0 -5 -5 -23 34 .36 14 13 | 1941 -1594 19 112
mit 240| 0 1 0 -37 10 30 -.25 10 10 | 273 -885 22 179
ngs 234| 0 0 8 -48 31 -22 .21 12 10 | 31 -958 2092 3627
sio 276| 0 0 -4 -61 -6 38 -.30 20 18 | --- --- --- ---
Table 2.1702.6 GPS week: 1702 Day: 6 MJD: 56164.000
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 257| 0 0 5 71 -7 31 -.52 12 11 | -214 -91 16 67
emr 81| 0 -1 -3 -23 -27 -30 .13 16 16 | 940 386 18 102
esa 177| 0 0 1 33 29 -5 .04 7 6 | -987 642 16 119
gfz 188| 0 0 -2 6 -66 6 -.45 12 11 | 36 498 25 144
grg n/a| 2 0 12 -26 -26 18 .42 15 14 | 384 -605 19 147
igr n/a| 0 0 1 -8 -11 -10 -.17 4 4 | 5884 130 22 104
jpl 80| 0 1 -1 -7 -8 -25 .36 15 14 | 982 398 21 139
mit 240| 1 0 1 3 3 26 -.24 6 6 | 181 -468 22 166
ngs 235| 0 0 -6 -42 22 -16 .25 11 9 | -250 -95 2117 3501
sio 278| 0 1 0 15 -22 15 -.32 21 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 3.1702.0 GPS week: 1702 Day: 0 MJD: 56158.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 13 25 8 9 15 4 14 9 8 11 5 | 45 43 48 38 46 41 47 40 46 46 43
2 | 13 16 9 8 17 4 16 13 11 23 5 | 27 34 27 24 37 24 33 28 28 24 27
3 | 9 14 7 6 14 4 12 11 11 17 4 | 14 23 15 11 17 11 26 14 18 21 14
4 | 16 12 6 8 10 4 13 12 8 29 4 | 69 80 72 71 75 71 81 71 76 78 76
5 | 8 14 5 8 11 3 13 10 8 33 4 | 29 36 32 32 39 30 37 28 35 44 33
6 | 7 15 8 7 14 4 11 10 14 20 4 | 14 27 17 14 22 13 26 16 23 21 19
7E | 11 18 9 9 13 6 18 10 11 17 5 | 19 28 24 21 32 20 27 24 26 24 22
8 | 12 12 5 7 13 3 10 11 7 26 3 | 43 53 42 44 42 43 55 41 45 39 45
9E | 16 19 7 8 17 7 15 12 12 24 5 | 36 35 35 40 32 36 35 35 36 35 33
10 | 14 9 6 6 15 4 8 11 7 16 3 | 29 30 30 29 41 29 33 23 28 22 29
11E | 6 14 5 8 11 4 12 9 10 10 4 | 22 28 25 21 26 21 26 19 30 25 23
12 | 16 15 8 11 18 6 15 11 18 32 5 | 20 31 23 27 24 20 29 26 24 20 21
13 | 7 12 7 8 18 5 15 8 9 14 4 | 14 21 13 13 30 12 24 13 18 13 12
14 | 7 18 9 12 14 4 17 10 13 21 5 | 18 26 19 18 25 15 25 15 22 19 16
15 | 17 18 8 9 14 5 17 9 8 26 4 | 17 27 16 17 24 13 24 17 19 20 15
16 | 9 20 9 12 16 4 16 12 10 30 5 | 16 26 17 20 24 13 25 13 19 20 17
17 | 10 17 11 8 16 4 18 11 11 18 5 | 14 25 18 13 24 14 29 13 24 16 17
18 | 10 13 6 8 13 5 11 10 8 28 4 | 17 22 19 22 23 18 24 20 19 22 17
19 | 10 18 7 7 15 5 12 11 9 23 4 | 22 28 20 15 30 18 27 18 26 19 20
20 | 10 12 6 11 12 3 14 8 11 30 4 | 25 27 26 27 32 25 31 24 30 29 25
21 | 10 15 7 11 16 4 15 10 8 20 4 | 22 32 22 21 28 21 31 24 22 27 20
22 | 9 12 6 8 11 4 13 9 8 21 3 | 25 25 25 23 34 24 29 25 25 24 24
23 | 7 16 7 9 14 5 18 9 8 21 4 | 13 23 15 13 22 12 24 17 21 12 14
25 | 13 21 7 9 19 4 13 10 10 16 5 | 23 28 24 25 28 22 32 27 21 22 21
26 | 8 16 7 9 12 4 8 8 8 14 3 | 16 25 19 20 27 17 22 19 19 20 18
27E | 17 22 8 9 13 8 15 10 11 21 5 | 35 36 35 40 33 36 36 34 34 33 33
28 | 10 17 8 12 13 4 14 9 11 25 4 | 17 29 23 29 23 21 29 19 20 22 23
29 | 11 19 7 13 16 5 18 9 12 21 5 | 28 29 24 25 27 22 32 24 30 25 22
30 | 9 13 5 7 11 3 9 11 7 20 3 | 20 23 22 22 22 19 25 23 22 30 21
31E | 11 18 9 10 20 4 17 7 9 13 5 | 26 36 31 23 40 26 32 23 33 26 28
32 | 9 12 7 8 11 3 8 9 8 16 3 | 17 22 19 15 27 16 24 17 21 21 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 16 7 9 15 5 14 10 10 22 |T 24 30 25 24 30 23 31 24 27 26 24
WRMS | 11 16 7 9 14 5 13 10 8 19 |NE 22 29 24 23 30 21 30 22 26 25 23
MEDI | 10 16 7 8 14 4 14 10 9 21 |MD 22 28 23 22 28 21 29 23 24 22 21
Table 3.1702.1 GPS week: 1702 Day: 1 MJD: 56159.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 12 26 7 8 15 5 12 10 8 12 5 | 30 32 34 30 37 30 38 30 40 32 32
2 | 13 14 6 9 16 3 13 8 9 23 4 | 23 27 23 19 33 19 28 21 26 19 23
3 | 8 10 4 7 9 4 13 11 10 15 3 | 12 20 15 13 18 11 24 14 20 20 15
4 | 27 14 6 9 24 4 13 10 13 35 5 | 98 111 106 104 103 102 112 104 103 114 105
5 | 11 12 7 8 12 4 12 11 7 29 4 | 21 31 25 24 31 22 34 24 31 32 26
6 | 9 10 4 5 11 4 12 9 8 15 3 | 11 23 16 13 20 13 27 15 22 20 17
7E | 11 21 6 12 15 6 17 10 17 21 5 | 24 28 24 28 28 21 28 25 30 32 24
8 | 14 13 5 7 11 5 12 11 10 22 4 | 28 42 30 29 33 31 39 34 33 37 32
9E | 19 18 8 9 13 8 16 9 9 25 4 | 36 37 36 39 30 35 32 39 35 35 35
10 | 15 7 5 7 11 3 8 9 10 15 3 | 17 18 20 20 20 16 21 17 20 13 17
11E | 9 14 6 7 16 4 11 9 11 10 4 | 18 26 25 20 26 20 24 19 33 20 22
12 | 18 16 8 9 18 4 15 8 11 27 4 | 18 29 17 23 22 13 27 19 24 17 19
13 | 8 13 6 8 17 5 13 9 9 14 4 | 12 22 15 17 29 11 25 12 18 13 14
14 | 11 16 7 13 15 3 17 8 8 22 4 | 12 23 14 18 21 12 22 15 22 18 16
15 | 18 20 9 10 14 3 18 9 10 23 5 | 15 26 20 19 21 16 24 20 24 18 19
16 | 10 14 9 12 18 4 16 9 10 27 5 | 12 23 19 18 22 12 25 13 18 13 15
17 | 10 16 6 10 17 3 16 9 12 15 4 | 11 23 12 12 22 8 23 10 24 13 12
18 | 10 12 6 9 10 5 13 8 10 30 3 | 12 20 16 17 15 13 19 18 17 18 16
19 | 14 16 6 10 16 5 15 11 11 19 4 | 14 26 21 15 31 15 25 16 27 16 19
20 | 10 12 7 11 14 4 14 9 14 24 4 | 17 22 23 22 22 18 25 18 26 25 20
21 | 8 18 5 9 17 3 13 7 7 19 4 | 19 23 15 19 21 15 23 18 17 21 16
22 | 9 13 5 7 10 5 12 7 10 20 3 | 15 21 17 17 23 14 24 18 18 18 18
23 | 8 17 7 10 14 4 19 11 10 20 5 | 14 25 18 19 24 12 27 14 20 14 16
25 | 15 21 3 7 18 4 13 10 7 20 4 | 14 25 18 21 25 15 29 21 24 19 20
26 | 9 14 9 8 10 3 10 7 11 18 4 | 13 22 21 18 23 15 24 20 24 19 20
27E | 21 18 8 11 12 9 16 9 9 18 4 | 36 39 36 41 31 36 34 39 42 37 37
28 | 11 13 6 10 12 2 13 9 9 22 4 | 12 25 16 20 20 16 23 17 21 16 16
29 | 28 20 6 9 15 4 16 9 10 20 4 | 14 23 14 18 21 13 23 19 20 18 15
30 | 10 9 5 6 13 4 7 9 11 17 3 | 18 23 22 19 23 17 26 22 22 22 21
31E | 11 20 9 11 17 4 16 7 14 15 5 | 22 31 25 22 29 22 30 23 35 30 25
32 | 10 13 7 7 13 4 8 10 12 15 4 | 15 23 24 17 23 18 25 17 23 22 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 16 7 9 15 4 14 9 10 21 |T 20 28 23 23 27 20 29 22 27 24 23
WRMS | 13 16 6 8 14 4 13 9 9 18 |NE 18 27 22 22 26 18 28 21 26 22 21
MEDI | 11 14 6 9 14 4 13 9 10 20 |MD 15 25 20 19 23 16 25 19 24 19 19
Table 3.1702.2 GPS week: 1702 Day: 2 MJD: 56160.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 9 22 7 11 17 5 13 13 11 10 5 | 33 33 38 31 41 33 39 36 38 35 34
2 | 11 14 7 9 14 3 15 11 9 25 4 | 22 32 27 20 30 22 30 27 28 26 24
3 | 8 13 6 10 14 5 13 12 9 15 4 | 13 24 16 11 19 14 27 17 21 23 17
4 | 14 11 5 9 9 5 11 13 9 19 3 | 42 52 46 47 49 47 52 51 46 51 46
5 | 8 14 7 10 12 4 13 13 12 27 4 | 20 32 30 26 30 25 35 29 30 28 28
6 | 8 13 6 9 15 5 12 11 8 13 4 | 12 26 17 14 20 14 28 21 20 23 18
7E | 11 20 7 11 11 5 17 12 11 10 5 | 18 27 19 17 23 14 23 16 24 18 17
8 | 15 13 7 6 14 4 12 14 6 19 4 | 57 68 58 60 60 60 68 65 64 65 60
9E | 22 17 8 11 15 8 16 10 10 21 5 | 37 37 36 41 30 35 31 37 35 30 32
10 | 8 8 5 6 15 4 8 9 8 15 3 | 19 21 21 22 29 22 25 23 23 17 20
11E | 7 20 7 9 18 4 12 13 10 8 5 | 18 29 23 18 24 17 20 21 21 20 18
12 | 15 15 6 9 16 4 13 9 8 25 4 | 15 27 19 21 22 16 25 21 23 16 18
13 | 7 14 6 7 18 6 14 11 8 16 4 | 11 23 14 14 29 11 23 14 15 13 14
14 | 10 18 7 11 13 5 17 10 7 24 4 | 12 24 18 17 21 15 23 21 21 17 14
15 | 12 19 11 10 14 5 17 11 12 23 5 | 18 26 18 21 24 15 24 20 18 18 15
16 | 11 17 8 10 17 4 17 11 9 28 5 | 13 24 18 17 22 14 27 18 17 16 16
17 | 10 13 6 10 19 4 15 13 10 15 4 | 13 21 13 13 22 12 23 19 23 15 13
18 | 10 12 7 8 11 3 13 11 7 33 4 | 14 21 21 19 16 17 24 22 21 20 17
19 | 7 14 8 8 20 4 15 12 8 18 4 | 16 26 20 14 33 15 30 20 25 17 21
20 | 10 11 7 12 12 4 16 10 11 24 4 | 19 26 23 24 27 23 27 23 30 26 24
21 | 9 15 6 11 16 6 13 13 10 24 4 | 20 30 26 22 26 22 28 28 24 25 21
22 | 10 14 5 6 9 3 12 9 7 22 3 | 15 21 21 21 21 19 26 25 21 18 19
23 | 9 19 7 9 15 4 18 14 7 21 5 | 12 26 16 15 24 11 24 17 17 11 15
25 | 15 24 6 8 20 6 14 11 8 19 5 | 17 27 23 20 26 17 29 25 20 21 18
26 | 7 12 7 11 14 4 9 10 12 14 4 | 12 22 21 16 23 16 23 22 23 16 17
27E | 22 19 8 12 13 8 17 9 18 17 5 | 47 49 46 52 40 45 43 48 55 42 44
28 | 10 12 9 12 15 3 15 14 11 21 5 | 12 22 22 23 21 16 23 18 17 19 17
29 | 12 18 7 11 15 4 18 13 12 18 5 | 16 23 14 13 22 13 23 21 21 19 13
30 | 10 12 5 5 13 4 8 13 10 16 4 | 17 21 21 15 22 16 26 21 20 18 19
31E | 13 18 8 11 18 4 16 12 11 16 5 | 16 29 25 21 29 21 27 28 27 24 21
32 | 9 11 7 11 13 4 11 10 8 18 4 | 16 23 22 20 25 20 26 21 23 22 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 7 10 15 5 14 12 10 20 |T 20 28 24 22 27 21 29 25 26 23 22
WRMS | 10 16 7 9 14 4 13 12 8 19 |NE 17 26 21 19 25 18 27 23 23 21 20
MEDI | 10 14 7 10 15 4 14 11 9 19 |MD 16 26 21 20 24 17 26 21 23 20 18
Table 3.1702.3 GPS week: 1702 Day: 3 MJD: 56161.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 22 8 9 16 5 12 9 10 12 5 | 35 35 41 35 43 35 40 34 36 37 36
2 | 10 15 6 10 16 3 14 10 10 22 4 | 23 32 26 23 33 24 31 27 29 24 26
3 | 6 13 6 6 11 4 10 9 10 16 3 | 15 19 17 15 16 11 22 14 18 20 17
4 | 12 10 8 9 9 5 9 11 11 18 4 | 53 62 60 59 61 56 61 57 60 59 58
5 | 10 14 5 9 13 4 12 13 7 25 4 | 23 33 29 27 34 24 33 25 31 22 28
6 | 7 12 5 6 10 3 10 8 10 12 3 | 15 24 18 15 19 14 25 16 21 21 19
7E | 11 21 7 10 13 5 18 11 13 11 5 | 35 37 31 30 34 30 35 30 39 30 30
8 | 19 12 6 7 11 9 12 11 9 17 4 | 90 99 94 97 93 92 99 90 90 89 93
9E | 22 19 10 6 11 7 14 7 11 24 4 | 35 34 30 35 25 33 32 31 32 25 29
10 | 10 9 7 6 13 4 10 10 9 14 3 | 18 24 22 21 29 20 25 19 22 16 21
11E | 9 15 8 6 14 3 10 9 7 11 4 | 19 30 28 23 27 22 27 21 26 19 23
12 | 13 15 8 10 16 4 14 8 11 23 4 | 16 28 21 22 25 18 28 20 25 14 20
13 | 9 15 7 8 18 4 14 9 12 17 4 | 13 26 17 18 31 14 26 12 18 14 15
14 | 10 14 8 11 15 5 15 10 12 22 4 | 16 24 19 22 24 16 22 18 23 19 18
15 | 11 18 11 13 11 4 16 9 14 23 5 | 19 26 21 22 24 15 24 18 21 18 19
16 | 11 19 10 13 14 4 17 9 12 26 5 | 15 26 22 23 23 15 26 16 19 14 19
17 | 9 17 5 10 15 4 14 9 13 12 4 | 10 25 14 12 21 11 23 9 23 12 14
18 | 10 12 7 8 11 4 13 10 9 26 4 | 17 21 19 20 21 17 21 21 20 20 18
19 | 8 15 6 8 16 5 12 10 10 18 4 | 19 25 20 14 30 17 25 18 24 16 20
20 | 8 11 8 9 13 4 14 8 9 20 4 | 20 29 28 27 31 25 29 22 30 28 25
21 | 11 24 10 12 16 5 15 9 13 21 5 | 16 32 21 16 22 15 26 19 19 21 20
22 | 10 13 6 6 11 4 12 8 6 23 3 | 23 24 23 23 27 21 26 24 24 22 22
23 | 8 18 8 11 17 3 16 12 10 20 5 | 12 27 21 18 26 14 27 15 19 16 17
25 | 10 20 5 7 16 4 13 8 8 18 4 | 15 26 22 18 27 17 30 21 24 18 21
26 | 10 10 8 9 11 5 9 8 9 13 3 | 16 22 22 19 27 17 25 20 21 17 20
27E | 22 19 10 10 12 6 15 7 14 19 5 | 31 30 30 33 26 30 31 28 31 26 27
28 | 9 14 8 12 13 4 15 10 9 20 4 | 14 27 23 28 22 20 29 18 23 21 21
29 | 14 17 8 10 12 4 18 10 12 16 5 | 15 23 14 15 21 12 24 18 25 20 18
30 | 11 13 6 8 14 4 7 9 11 15 4 | 24 27 26 23 25 21 29 25 26 24 25
31E | 11 19 6 9 18 6 18 9 11 14 5 | 35 41 36 38 42 35 39 35 41 33 36
32 | 9 14 6 9 12 4 8 9 7 15 3 | 16 26 25 20 28 20 24 18 23 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 7 9 14 5 13 9 10 19 |T 23 31 27 26 30 23 31 24 28 24 25
WRMS | 10 16 7 8 13 4 13 9 9 20 |NE 19 27 23 22 27 19 28 20 24 21 22
MEDI | 10 15 7 9 13 4 14 9 10 18 |MD 18 27 22 22 27 20 27 20 24 21 21
Table 3.1702.4 GPS week: 1702 Day: 4 MJD: 56162.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 25 7 7 13 3 15 12 10 11 5 | 30 29 35 30 38 32 36 35 39 29 33
2 | 9 15 9 11 13 2 13 9 10 20 4 | 18 27 24 21 32 22 27 26 31 22 22
3 | 11 13 7 9 12 5 11 12 11 16 4 | 13 21 16 14 15 14 23 18 21 21 14
4 | 14 11 6 11 10 4 11 12 11 21 4 | 30 43 33 34 39 33 41 32 38 43 34
5 | 7 14 7 11 9 4 12 12 9 28 4 | 22 33 29 28 32 26 34 29 30 17 27
6 | 9 12 8 8 13 5 11 11 9 12 4 | 13 27 19 14 20 16 26 18 24 22 18
7E | 10 21 7 11 14 5 16 11 11 13 5 | 20 32 23 24 31 23 28 28 32 30 20
8E | 19 13 9 12 12 6 14 14 9 30 4 | 74 81 76 80 79 76 81 81 82 84 76
9E | 23 17 12 10 13 8 14 10 12 23 5 | 36 38 39 38 29 34 36 34 37 31 32
10 | 11 9 4 7 9 4 7 10 8 14 3 | 16 21 25 25 24 22 22 20 23 13 19
11E | 8 18 8 8 13 4 11 13 11 9 4 | 12 29 23 20 25 19 23 19 28 17 19
12 | 14 15 6 9 12 5 14 11 8 23 4 | 16 30 20 23 25 20 28 25 27 20 18
13 | 9 15 9 10 15 5 14 12 10 19 4 | 13 26 19 19 31 16 25 17 20 15 15
14 | 10 15 6 11 12 4 17 11 8 19 4 | 14 24 18 21 26 17 24 20 21 19 15
15 | 15 17 10 14 11 5 19 11 9 27 5 | 19 28 21 25 27 20 28 23 26 26 18
16 | 12 18 11 12 11 5 17 11 10 27 5 | 16 26 18 23 22 17 28 17 20 14 18
17 | 7 16 9 9 12 4 17 11 10 12 5 | 12 25 20 14 23 14 26 16 21 15 14
18 | 10 12 7 13 10 4 15 10 8 23 4 | 14 24 19 23 18 18 25 21 18 20 14
19 | 8 15 8 10 12 3 15 13 8 17 4 | 18 25 19 15 29 19 28 22 25 16 19
20 | 10 12 6 10 13 3 13 11 8 20 4 | 19 25 25 23 29 23 28 26 24 29 22
21 | 9 17 7 14 14 5 14 11 9 19 5 | 18 27 18 22 25 19 26 23 22 26 17
22 | 9 13 7 9 9 4 15 9 10 22 4 | 16 23 23 24 25 20 23 23 18 18 18
23 | 8 17 9 11 13 4 16 10 10 20 5 | 11 24 18 17 26 15 24 19 20 15 15
25 | 10 22 6 9 12 5 13 11 6 18 4 | 19 27 25 24 27 20 32 26 27 21 20
26 | 8 12 8 11 9 4 9 11 7 16 4 | 14 22 23 21 26 17 22 20 21 12 18
27E | 24 18 10 15 15 7 14 10 10 16 5 | 40 42 40 43 38 38 40 39 42 38 36
28 | 12 13 10 13 10 4 14 9 11 19 4 | 12 26 24 27 24 20 26 18 25 21 20
29 | 18 19 7 11 12 4 12 13 9 16 4 | 10 24 16 20 19 16 23 24 23 25 15
30 | 14 11 6 7 12 4 6 10 9 15 3 | 16 24 21 26 24 21 26 28 25 23 20
31E | 12 17 8 12 15 5 17 11 10 14 5 | 18 29 24 23 27 24 27 22 30 24 21
32 | 12 13 6 8 11 3 11 10 9 15 4 | 16 23 22 19 27 20 28 22 23 22 20
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 8 10 12 4 14 11 9 19 |T 19 29 25 25 28 22 29 25 27 24 22
WRMS | 11 16 8 10 11 4 13 12 9 18 |NE 16 26 22 22 26 19 27 22 24 20 19
MEDI | 10 15 7 11 12 4 14 11 9 19 |MD 16 26 23 23 26 20 27 23 25 21 19
Table 3.1702.5 GPS week: 1702 Day: 5 MJD: 56163.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 11 22 9 7 18 4 12 12 9 14 5 | 29 26 33 29 40 29 37 32 33 27 29
2 | 8 14 7 9 14 3 13 10 9 20 4 | 18 29 24 21 34 22 29 25 30 18 22
3 | 9 12 8 6 16 4 11 10 8 19 4 | 12 23 19 13 19 15 25 20 23 22 16
4 | 13 12 5 9 9 4 10 10 13 21 4 | 42 49 45 41 47 45 49 45 43 52 45
5 | 8 15 7 10 11 4 14 10 11 30 4 | 20 34 29 26 33 24 33 26 32 13 26
6 | 9 11 6 5 15 4 10 7 8 17 3 | 14 25 20 15 21 17 24 19 25 22 18
7E | 12 24 9 10 19 5 19 11 16 20 6 | 31 37 29 32 37 30 35 33 39 34 29
8E | 21 13 9 10 11 5 15 10 13 25 4 | 61 68 60 63 64 62 68 67 63 64 61
9E | 22 16 12 9 14 5 14 9 14 29 5 | 39 34 35 38 29 33 33 37 32 23 31
10 | 9 8 5 6 12 2 9 10 9 15 3 | 16 18 17 18 24 18 19 21 20 16 17
11E | 6 11 9 6 16 4 10 9 13 12 4 | 15 21 20 15 28 15 18 18 21 17 17
12 | 11 13 7 9 13 6 13 9 13 24 4 | 19 31 23 23 26 23 30 25 25 19 21
13 | 8 15 6 9 17 3 14 9 11 16 4 | 13 25 15 16 32 16 26 17 19 13 15
14 | 7 15 7 10 16 3 15 10 14 19 5 | 14 22 17 19 24 15 23 20 24 16 16
15 | 16 20 10 10 10 5 18 11 13 28 5 | 18 31 23 22 27 19 26 23 25 23 19
16 | 10 16 9 12 16 4 17 8 15 28 5 | 15 25 20 18 24 15 27 17 21 10 16
17 | 9 15 10 11 13 4 15 10 12 11 5 | 13 20 13 10 24 13 22 15 26 12 13
18 | 8 12 7 11 10 5 14 9 8 23 4 | 14 23 18 21 18 18 21 21 20 19 15
19 | 10 16 9 8 16 4 14 10 7 17 4 | 19 29 22 15 33 20 29 21 27 14 20
20 | 9 14 7 10 14 4 13 11 14 19 4 | 18 26 23 23 29 22 26 26 29 27 22
21 | 9 15 6 11 18 5 17 9 10 21 5 | 22 28 24 22 28 21 25 27 25 22 22
22 | 8 14 8 7 12 4 16 7 11 20 4 | 15 22 20 20 22 16 21 21 20 14 17
23 | 8 17 6 12 16 4 16 9 11 19 5 | 14 26 19 17 27 17 26 18 23 17 16
25 | 9 20 6 8 15 4 14 9 17 20 5 | 20 29 23 24 26 22 34 26 24 19 20
26 | 9 14 7 10 10 3 8 10 13 17 4 | 15 24 21 21 26 19 24 22 22 14 19
27E | 23 19 12 12 14 6 16 10 13 23 5 | 35 32 33 36 27 32 31 36 32 23 29
28 | 12 15 10 12 13 4 13 9 12 21 5 | 11 22 20 20 22 14 22 14 16 18 16
29 | 17 18 7 10 11 4 15 11 15 18 5 | 15 25 17 18 23 17 24 23 29 21 17
30 | 12 12 5 8 17 5 12 8 14 19 4 | 34 43 40 36 36 37 45 35 44 40 38
31E | 9 14 6 9 14 5 15 10 13 12 4 | 21 25 22 21 30 20 26 25 29 21 22
32 | 9 12 9 7 16 4 11 10 13 16 4 | 16 24 22 18 27 20 26 21 22 21 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 15 8 9 14 4 14 10 12 20 |T 21 28 24 23 29 22 29 25 27 22 22
WRMS | 10 15 8 9 13 4 13 10 10 18 |NE 18 27 22 21 27 20 27 23 25 20 20
MEDI | 9 15 7 9 14 4 14 10 13 19 |MD 18 26 22 21 27 20 26 23 25 19 19
Table 3.1702.6 GPS week: 1702 Day: 6 MJD: 56164.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 10 21 5 11 17 4 14 6 11 13 4 | 38 37 46 40 48 40 47 38 49 41 40
2 | 8 13 7 12 16 3 17 6 12 19 4 | 20 31 30 25 40 26 33 25 31 21 25
3 | 10 12 5 10 17 4 13 5 13 18 4 | 12 25 20 13 20 16 27 16 26 28 16
4 | 15 12 5 13 11 4 10 4 7 25 3 | 32 40 36 36 39 34 40 35 36 41 35
5 | 8 14 7 12 13 3 14 6 11 34 4 | 25 36 36 34 40 32 37 29 35 22 32
6 | 9 12 5 10 15 4 12 5 12 21 3 | 13 25 15 11 18 14 24 14 23 26 16
7E | 9 19 6 12 14 4 19 6 11 14 4 | 35 42 39 37 41 35 41 35 44 42 35
8E | 17 16 10 14 15 6 16 7 11 22 5 | 97 94 97 101 95 92 95 94 93 101 93
9E | 24 17 12 13 15 6 16 6 20 31 5 | 39 39 38 41 27 36 39 35 36 31 34
10 | 8 8 5 10 15 3 9 5 11 16 3 | 21 24 26 29 35 25 27 24 25 22 25
11E | 7 19 7 7 16 4 12 7 8 7 4 | 15 30 23 18 26 17 23 15 26 19 18
12 | 14 16 8 12 11 8 18 7 10 24 4 | 22 33 25 24 30 26 32 25 26 21 22
13 | 8 16 7 8 18 4 13 6 7 17 4 | 18 31 25 23 35 20 31 19 22 20 20
14 | 8 15 6 13 15 3 18 5 11 23 4 | 15 23 17 19 25 15 25 15 23 22 16
15 | 13 21 9 17 12 5 18 7 14 29 5 | 23 31 24 33 33 23 30 22 28 26 22
16 | 12 15 7 13 13 4 17 6 9 29 4 | 17 26 23 25 25 18 28 16 26 17 20
17 | 9 16 7 11 13 4 18 5 8 12 4 | 18 26 21 13 25 16 30 15 24 20 17
18 | 7 13 6 13 9 4 13 5 10 24 3 | 17 26 23 22 25 20 25 18 24 25 18
19 | 9 16 5 10 14 4 13 5 8 16 3 | 23 32 24 18 36 24 33 24 28 22 23
20 | 11 12 7 12 17 4 14 7 14 15 4 | 26 38 38 40 44 35 39 33 42 40 33
21 | 7 18 7 14 18 4 14 4 11 16 4 | 18 29 25 15 31 21 28 21 21 21 19
22 | 7 13 6 9 12 4 15 4 12 22 4 | 19 24 22 22 29 19 25 19 22 21 20
23 | 12 16 6 11 16 4 17 6 12 21 4 | 16 30 22 23 32 19 31 18 25 24 19
25 | 7 22 5 7 11 4 12 8 10 18 4 | 19 28 25 21 33 23 34 25 26 21 22
26 | 9 12 7 13 13 4 11 5 8 14 3 | 18 21 24 20 31 20 23 20 21 18 21
27E | 24 21 12 13 17 4 19 6 17 26 5 | 34 38 33 37 31 32 39 32 30 33 30
28 | 10 14 8 14 11 4 17 6 11 24 4 | 16 28 28 31 27 23 31 21 28 29 23
29 | 21 18 6 10 12 4 16 6 12 18 4 | 14 27 19 18 27 18 27 19 30 27 18
30 | 12 11 4 8 13 5 9 4 9 13 3 | 20 30 28 29 30 24 31 25 27 24 28
31E | 10 17 6 6 21 5 18 6 12 11 4 | 16 27 21 20 27 18 25 19 28 19 20
32 | 9 12 7 12 16 3 8 6 7 15 3 | 19 33 30 32 36 28 32 27 33 31 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 16 7 12 15 4 15 6 11 21 |T 23 32 29 28 33 26 33 25 30 28 26
WRMS | 11 16 6 11 14 4 14 6 9 17 |NE 19 29 26 24 31 23 30 22 28 25 23
MEDI | 9 16 7 12 15 4 14 6 11 18 |MD 19 30 25 24 31 23 31 22 27 24 22
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 4.1702 GPS week: 1702 MJD: 56158.0-56164.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3010 |U 6 7 18 |U 35 23 234 |U 21 18 45 |
emr | emr 2967 | 8 8 21 |U 55 34 317 | 21 20 50 |
esa | esa 2976 | 6 6 19 |U 35 23 240 | 20 15 40 |
gfz | gfz 2965 |U 6 6 19 |U 47 31 290 |U 22 17 44 |
grg | grg 2976 |U 8 8 26 |U 51 36 296 | 21 17 47 |
igr | igr 2976 | 6 6 18 | 37 23 273 | 20 17 44 |
igs | igs 2959 | 6 6 19 | 43 26 252 | 21 17 44 |
jpl | jpl 2966 | 7 7 20 |U 47 28 281 | 20 18 48 |
mit | mit 2976 | 7 7 19 |U 52 33 306 |U 23 21 45 |
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 5.1702.0 GPS week: 1702 Day: 0 MJD: 56158.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3043 | 5 6 18 | 9 12 35 | ---- ---- ---- |
emr | emr 2968 | 6 6 20 | 22 12 59 | ---- ---- ---- |
esa | esa 2976 | 4 6 18 | 9 12 38 | ---- ---- ---- |
gfz | gfz 2968 | 5 6 20 | 9 11 37 | ---- ---- ---- |
grg | grg 2976 | 6 8 28 | 19 17 46 | ---- ---- ---- |
igr | igr 2976 | 5 6 19 | 9 12 39 | ---- ---- ---- |
igs | igs 2945 | 5 6 19 | 18 10 52 | ---- ---- ---- |
jpl | jpl 2968 | 6 8 20 | 26 12 60 | ---- ---- ---- |
mit | mit 2976 | 5 5 18 | 20 12 50 | ---- ---- ---- |
Table 5.1702.1 GPS week: 1702 Day: 1 MJD: 56159.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3041 | 7 6 16 | 7 6 22 | ---- ---- ---- |
emr | emr 2968 | 8 8 19 | 14 13 31 | ---- ---- ---- |
esa | esa 2976 | 6 7 18 | 7 8 20 | ---- ---- ---- |
gfz | gfz 2967 | 6 7 19 | 10 12 24 | ---- ---- ---- |
grg | grg 2976 | 10 10 28 | 15 14 36 | ---- ---- ---- |
igr | igr 2976 | 6 8 19 | 7 7 21 | ---- ---- ---- |
igs | igs 2944 | 6 7 18 | 13 10 31 | ---- ---- ---- |
jpl | jpl 2968 | 7 7 20 | 15 10 33 | ---- ---- ---- |
mit | mit 2976 | 7 7 19 | 15 11 41 | ---- ---- ---- |
Table 5.1702.2 GPS week: 1702 Day: 2 MJD: 56160.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3037 | 5 7 20 | 204 118 1506 | ---- ---- ---- |
emr | emr 2968 | 8 10 23 | 283 169 1989 | ---- ---- ---- |
esa | esa 2976 | 6 8 21 | 208 113 1544 | ---- ---- ---- |
gfz | gfz 2966 | 6 7 21 | 259 133 1860 | ---- ---- ---- |
grg | grg 2976 | 7 8 26 | 266 164 1848 | ---- ---- ---- |
igr | igr 2976 | 6 7 21 | 222 115 1772 | ---- ---- ---- |
igs | igs 2953 | 6 7 21 | 210 118 1565 | ---- ---- ---- |
jpl | jpl 2968 | 8 8 23 | 223 130 1753 | ---- ---- ---- |
mit | mit 2976 | 7 8 22 | 268 161 1923 | ---- ---- ---- |
Table 5.1702.3 GPS week: 1702 Day: 3 MJD: 56161.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | 7 6 17 | 6 7 22 | ---- ---- ---- |
emr | emr 2968 | 8 7 21 | 12 10 32 | ---- ---- ---- |
esa | esa 2976 | 6 5 16 | 6 7 24 | ---- ---- ---- |
gfz | gfz 2967 | 6 5 16 | 13 14 29 | ---- ---- ---- |
grg | grg 2976 | 7 8 24 | 14 14 30 | ---- ---- ---- |
igr | igr 2976 | 6 5 15 | 6 6 24 | ---- ---- ---- |
igs | igs 2973 | 6 5 16 | 12 9 29 | ---- ---- ---- |
jpl | jpl 2966 | 8 6 18 | 19 13 34 | ---- ---- ---- |
mit | mit 2976 | 6 5 16 | 15 11 33 | ---- ---- ---- |
Table 5.1702.4 GPS week: 1702 Day: 4 MJD: 56162.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 16 | 5 6 14 | 46 28 96 |
emr | emr 2968 | 8 8 22 | 17 9 35 | 44 31 100 |
esa | esa 2976 | 7 6 18 | 5 7 13 | 41 20 81 |
gfz | gfz 2964 | 7 6 18 | 15 16 30 | 43 24 91 |
grg | grg 2976 | 8 9 24 | 14 15 26 | 40 19 83 |
igr | igr 2976 | 7 6 17 | 5 7 14 | 41 24 91 |
igs | igs 2973 | 7 6 18 | 12 10 21 | 43 26 90 |
jpl | jpl 2965 | 8 8 21 | 12 7 26 | 41 27 96 |
mit | mit 2976 | 8 6 16 | 13 11 23 | 49 34 89 |
Table 5.1702.5 GPS week: 1702 Day: 5 MJD: 56163.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 8 22 | 8 7 18 | 9 17 22 |
emr | emr 2966 | 9 8 23 | 19 11 33 | 10 17 28 |
esa | esa 2976 | 7 7 21 | 7 6 20 | 10 15 21 |
gfz | gfz 2963 | 7 6 20 | 10 15 27 | 13 17 25 |
grg | grg 2976 | 9 8 33 | 16 14 47 | 12 20 37 |
igr | igr 2976 | 7 6 21 | 7 7 18 | 10 17 24 |
igs | igs 2974 | 7 6 21 | 17 13 33 | 9 15 23 |
jpl | jpl 2964 | 8 6 21 | 15 9 27 | 11 16 26 |
mit | mit 2976 | 7 8 20 | 18 13 38 | 11 19 28 |
Table 5.1702.6 GPS week: 1702 Day: 6 MJD: 56164.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 6 7 19 | 5 7 19 | 8 9 19 |
emr | emr 2964 | 9 7 19 | 19 11 38 | 10 12 23 |
esa | esa 2976 | 6 6 18 | 5 9 18 | 9 10 17 |
gfz | gfz 2963 | 6 6 18 | 12 15 24 | 9 9 16 |
grg | grg 2976 | 9 8 21 | 16 16 40 | 12 11 22 |
igr | igr 2976 | 7 6 17 | 5 7 20 | 9 9 17 |
igs | igs 2957 | 6 6 18 | 16 12 33 | 10 11 19 |
jpl | jpl 2963 | 8 8 19 | 21 18 35 | 10 10 21 |
mit | mit 2976 | 7 7 20 | 15 13 37 | 10 11 19 |
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 6.1702 GPS week: 1702 MJD: 56158.500-56164.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -2 -89 25 -8 6 | 8 16
| 19 26 74 49 9 | 5
emr uuuuu | -17 30 -150 -31 7 | 18 25
| 13 15 82 57 5 | 7
esa uuuuu | 9 -49 70 121 4 | 15 20
| 25 42 52 37 4 | 6
gfz uuuuu | 20 0 -16 -60 2 | 7 15
| 17 26 103 60 4 | 5
grg uuuux | 35 7 -93 -12 -11 | 46 57
| 22 24 42 74 44 | 3
igr xxxxx | -4 10 -5 -8 9 | 5 17
| 23 16 43 53 5 | 8
irf xxxxx | 2 -5 42 -6 -8 | 6 13
| 13 17 68 24 5 | 3
jpl uuuuu | -24 -8 -51 2 7 | 48 50
| 25 35 58 50 13 | 6
mit uuuuu | -18 -11 154 -3 -12 | 19 22
| 13 22 135 49 10 | 3
ngs uuuuu | -11 69 -61 -75 -2 | 13 18
| 38 41 186 137 4 | 5
sio xxxxx | 25 16 60 -119 12 | 41 44
| 11 24 73 71 5 | 9
Table 7.1702.0 GPS week: 1702 Day: 0 MJD: 56158.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -18 -125 -12 -14 0 | 1 12
emr uuuuu | -17 13 -252 69 13 | 8 17
esa uuuuu | 30 28 35 145 -4 | 7 13
gfz uuuuu | 43 -46 126 -34 -1 | 0 11
grg uuuux | 10 -23 -112 -68 -47 | 46 56
igr xxxxx | -11 -6 -20 -39 0 | -5 13
irf xxxxx | 6 -31 177 15 -6 | 1 12
jpl uuuuu | -2 -58 -27 -14 -10 | 40 42
mit uuuuu | -10 -50 430 43 -9 | 15 18
ngs uuuuu | -79 107 -376 -200 4 | 5 14
sio xxxxx | 35 -23 -40 -97 12 | 28 31
Table 7.1702.1 GPS week: 1702 Day: 1 MJD: 56159.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -6 -115 40 -11 3 | 2 13
emr uuuuu | -40 20 -92 -15 4 | 11 21
esa uuuuu | 42 -51 -23 53 6 | 8 14
gfz uuuuu | 11 -9 68 -81 -1 | 1 12
grg uuuux | 16 -18 -47 -7 -55 | 46 56
igr xxxxx | -26 28 -32 16 11 | -4 14
irf xxxxx | -21 -13 60 14 -3 | 2 12
jpl uuuuu | 9 -31 19 -17 5 | 42 43
mit uuuuu | -44 -12 167 60 -3 | 16 19
ngs uuuuu | -30 138 -161 -47 -8 | 8 16
sio xxxxx | 10 -8 7 -69 9 | 32 35
Table 7.1702.2 GPS week: 1702 Day: 2 MJD: 56160.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -15 -92 140 -51 0 | 5 16
emr uuuuu | -15 35 -87 -54 13 | 14 24
esa uuuuu | -6 -70 81 124 8 | 12 18
gfz uuuuu | -2 -6 43 46 1 | 5 14
grg uuuux | 50 13 -53 -90 -58 | 44 55
igr xxxxx | -21 32 -37 88 13 | 0 17
irf xxxxx | -6 23 37 -1 -10 | 6 14
jpl uuuuu | -30 -24 20 -8 -7 | 45 47
mit uuuuu | -17 18 98 10 -15 | 18 22
ngs uuuuu | 27 81 -170 -148 -6 | 11 17
sio xxxxx | 10 39 128 -152 12 | 37 40
Table 7.1702.3 GPS week: 1702 Day: 3 MJD: 56161.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -10 -61 -5 23 0 | 9 16
emr uuuuu | -17 35 -211 -40 5 | 20 26
esa uuuuu | 15 -42 60 175 7 | 17 21
gfz uuuuu | 17 -1 -52 -118 -3 | 8 14
grg uuuux | 18 5 -79 -97 -19 | 42 55
igr xxxxx | -16 16 -16 -71 11 | 5 16
irf xxxxx | 5 -8 40 -31 -5 | 8 13
jpl uuuuu | -67 15 -54 -2 8 | 48 49
mit uuuuu | -6 -25 145 -6 -6 | 20 23
ngs uuuuu | 17 52 34 -24 0 | 15 18
sio xxxxx | 21 12 33 -158 13 | 42 45
Table 7.1702.4 GPS week: 1702 Day: 4 MJD: 56162.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 39 -84 42 -87 11 | 9 17
emr uuuuu | 2 45 -243 -14 6 | 24 29
esa uuuuu | -29 -60 104 122 2 | 19 25
gfz uuuuu | 25 38 -67 -31 3 | 10 16
grg uuuux | 41 9 -167 84 33 | 44 56
igr xxxxx | 6 -5 14 -40 12 | 9 20
irf xxxxx | 7 2 32 17 -8 | 9 15
jpl uuuuu | -37 -23 -92 113 7 | 50 53
mit uuuuu | -18 -8 174 9 -13 | 21 24
ngs uuuuu | 25 36 93 -262 0 | 17 20
sio xxxxx | 36 18 113 9 16 | 45 49
Table 7.1702.5 GPS week: 1702 Day: 5 MJD: 56163.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | -5 -53 70 51 23 | 10 18
emr uuuuu | -10 51 -98 -37 7 | 24 30
esa uuuuu | -12 -110 97 105 6 | 20 25
gfz uuuuu | 39 16 -46 -69 10 | 11 16
grg uuuux | 38 50 -115 50 34 | 49 60
igr xxxxx | 42 7 84 -29 11 | 11 20
irf xxxxx | 22 4 -26 -14 -19 | 9 15
jpl uuuuu | -21 42 -133 -33 24 | 52 54
mit uuuuu | -5 1 20 -60 -33 | 20 24
ngs uuuuu | -29 40 165 26 -2 | 16 20
sio xxxxx | 30 27 159 -195 19 | 48 51
Table 7.1702.6 GPS week: 1702 Day: 6 MJD: 56164.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod xxxxx | 0 -94 -99 31 9 | 15 20
emr uuuuu | -25 13 -65 -123 0 | 26 31
esa uuuuu | 23 -37 134 125 1 | 23 26
gfz uuuuu | 8 6 -186 -129 3 | 14 17
grg uuuux | 71 9 -79 43 36 | 52 63
igr xxxxx | -1 -4 -29 20 5 | 15 20
irf xxxxx | 0 -12 -25 -44 -6 | 9 15
jpl uuuuu | -23 21 -91 -24 23 | 56 58
mit uuuuu | -24 0 43 -74 -7 | 19 24
ngs uuuuu | -5 29 -12 132 -2 | 18 21
sio xxxxx | 34 44 22 -169 3 | 53 55
More information about the IGSREPORT
mailing list