[IGSREPORT-23420] Wk 1832 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Mon Mar 9 13:15:48 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1832 (Feb 15, 2015 - Feb 21, 2015)
Contacts: igs.acc 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:
igs1832[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1832[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1832[0-6].cls IGS GPS clock combination summary report.
igs18327.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18327.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.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
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 | 4 4 BOR1 HYDE BOR1 HYDE
0 | EMR | 8 8
0 | ESA | 4 21 4 21
0 | GFZ | HOB2
0 | GRG | 8 8 BRST MAW1 NOVM BRST MAW1 NOVM
0 | JPL | 4 8 21
1 | COD | 4 4
1 | EMR | 8 8
1 | ESA | 4 4 GRAZ MATE MAW1 GRAZ MATE MAW1
1 | GFZ | HOB2 HOB2
1 | GRG | BJFS GRAZ HOB2 HYDE KELY MAW1 BJFS GRAZ HYDE KELY
1 | GRG | MAW1 TLSE
1 | JPL | 4 8
2 | COD | 4 4 CHUR NRIL OHI3 SOFI XMIS CHUR OHI3 SOFI XMIS
2 | ESA | 4 4 BRST BRST
2 | GFZ | YKRO
2 | GRG | MCM4 NRIL MCM4 NRIL
2 | JPL | 4 CHUR
3 | COD | 4 4
3 | EMR | 1 1
3 | ESA | 4 4 TRO1 TRO1
3 | GFZ | MATE MATE TLSE
3 | GRG | MATE MATE
3 | JPL | 4
4 | COD | 4 4 KOUC OHI3 KOUC OHI3
4 | ESA | 4 4
4 | GFZ | 25
4 | GRG | MAL2 MAW1 TLSE BOGT MAL2 MAW1 TLSE
4 | JPL | 4 25 RECF
5 | COD | 4 4 ALRT KOUC MDVJ XMIS YKRO ALRT KOUC MDVJ XMIS
5 | COD | YKRO
5 | ESA | 4 4
5 | GRG | ALRT NRC1 ONSA ALRT MAL2 NRC1 ONSA
5 | JPL | 4 ALRT
5 | MIT | RBAY RBAY
6 | COD | HOB2 KOUC MAR6 NNOR NRIL HOB2 KOUC MAR6 NNOR NRIL
6 | ESA | UNSA
6 | GFZ | 4 4
6 | GRG | 4 4 BRST BRST WES2
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
3 | GRG | 11
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G11 | 4 | 4 | 4 | 4 | 8 | 4 | 4 |
PRN G29 | | | | | | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -1.2 -1.5 -1.7 -48 -16 -23 .61
EMR | 0 | 4.9 5.2 14.1 49 15 22 .33
ESA | 0 | .3 -2.5 -.2 -21 -11 53 .60
GFZ | 0 | .8 -.8 -1.8 -15 -79 -29 .67
GRG | 0 | -.7 -7.6 -14.2 -23 10 -10 .96
JPL | 0 | 2.0 -4.1 14.8 -7 -24 -32 .46
MIT | 0 | 6.0 -1.7 -2.4 13 -19 -37 .79
NGS | 0 | 5.4 -2.1 9.5 14 -36 2 .75
SIO | 0 | 3.3 -2.3 -1.3 2 -19 -39 .59
COD | 1 | -1.6 -1.3 -3.5 -10 -6 -5 .87
EMR | 1 | 10.6 8.5 16.6 26 11 0 .41
ESA | 1 | .0 -1.8 -.6 -23 -14 47 .74
GFZ | 1 | .6 -1.0 -1.5 3 -76 3 .74
GRG | 1 | 13.9 1.6 -9.2 -19 7 -5 .65
JPL | 1 | 7.7 -5.9 15.8 -12 12 -18 .87
MIT | 1 | 6.8 -3.8 2.8 -4 7 -12 .51
NGS | 1 | 10.6 -10.9 11.7 -29 -54 14 .79
SIO | 1 | 6.8 -1.8 7.0 -7 -18 -36 .69
COD | 2 | -2.3 -1.7 -4.0 -37 1 -40 .69
EMR | 2 | 1.9 13.9 18.4 30 10 1 .64
ESA | 2 | 1.0 -2.5 -.4 -36 -13 48 .67
GFZ | 2 | .1 -.5 -1.9 -10 -61 2 .86
GRG | 2 | 11.1 -6.9 -16.4 -2 -26 -16 .76
JPL | 2 | -2.0 -8.0 11.6 13 6 -10 1.07
MIT | 2 | 6.8 -1.8 2.6 1 1 -26 .69
NGS | 2 | .9 -1.0 17.8 -40 -38 -14 .76
SIO | 2 | 4.8 -3.1 11.5 -7 -18 -16 .79
COD | 3 | -2.1 -1.2 -3.2 -27 -6 -13 .41
EMR | 3 | 6.0 9.8 12.7 28 29 21 .40
ESA | 3 | .7 -2.0 -.2 -42 -22 60 .55
GFZ | 3 | .9 -1.3 -2.3 -26 -76 12 .56
GRG | 3 | 3.4 -8.2 -14.8 -26 -2 -33 .94
JPL | 3 | .6 -9.6 6.9 7 61 5 .54
MIT | 3 | 2.6 -3.8 -1.1 -1 12 -40 .56
NGS | 3 | 2.4 -4.6 8.2 -19 -12 -8 .54
SIO | 3 | 3.8 -4.7 8.0 -8 -38 -12 .59
COD | 4 | -1.1 -1.7 -2.8 -9 -1 -54 .57
EMR | 4 | -1.0 10.9 7.2 0 30 4 .16
ESA | 4 | .9 -1.7 -.3 -42 -28 63 .47
GFZ | 4 | .9 -1.1 -2.2 -20 -91 6 .64
GRG | 4 | 3.0 -1.5 -23.8 7 7 -9 .60
JPL | 4 | 2.8 -6.0 13.5 1 56 -4 .58
MIT | 4 | 1.2 -5.5 -1.9 -5 9 -24 .66
NGS | 4 | .2 -6.0 6.5 -15 -10 -25 .70
SIO | 4 | 1.5 -1.2 11.4 -16 -11 -37 .55
COD | 5 | -1.2 -.8 -2.3 -1 2 -48 .52
EMR | 5 | -3.0 12.6 14.9 25 45 11 .26
ESA | 5 | .8 -1.4 -.1 -38 -11 39 .43
GFZ | 5 | .8 -1.0 -2.1 8 -83 24 .43
GRG | 5 | -2.1 .7 -17.6 2 11 -25 .60
JPL | 5 | 3.3 -.9 8.0 8 13 11 .59
MIT | 5 | -1.0 -4.1 -1.3 -1 7 -40 .46
NGS | 5 | 2.6 -9.2 7.3 -21 -10 -22 .62
SIO | 5 | -.9 .7 10.3 -28 -20 -38 .38
COD | 6 | -.6 -1.0 -2.0 -6 -19 -28 .51
EMR | 6 | 2.2 7.6 15.7 39 45 16 -.04
ESA | 6 | .4 -1.6 .1 -30 -21 35 .47
GFZ | 6 | .4 -1.0 -1.8 -5 -82 20 .35
GRG | 6 | -3.4 .3 -23.2 -7 15 -31 .90
JPL | 6 | 1.0 -3.7 11.8 11 0 17 .37
MIT | 6 | .1 -7.1 1.1 11 19 -35 .27
NGS | 6 | -1.2 -2.1 14.3 -20 4 -21 .57
SIO | 6 | -1.3 -1.4 9.0 -11 -4 -42 .24
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
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 1.1832.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1832.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 2.1832.[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 3.1832.[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 5.1832.0-6). 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 1832 summary. (Feb 15, 2015 - Feb 21, 2015)
Table 1.1832.a GPS week: 1832 MJD: 57068.000-57074.000
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 248| -1 0 -3 14 22 4 .02 15 13 | -754 -389 17 115
| 1 0 1 14 38 12 .03 | 513 884
emr 79| 1 3 5 -33 -6 15 .20 13 13 | 5230 -611 15 133
| 1 1 1 14 15 18 .03 | 2183 1226
esa 150| 0 1 1 2 -5 2 -.35 12 12 | -1031 764 10 139
| 1 0 0 13 25 17 .02 | 1354 1251
gfz 196| 0 -2 -5 32 -1 4 .05 13 12 | -205 -35 11 89
| 1 0 1 14 18 22 .02 | 416 996
grg 172| 1 0 -7 -30 16 -38 .20 18 17 | 43 -165 16 145
| 1 0 1 24 22 16 .03 | 255 728
igr n/a| 0 0 -3 -20 -2 2 -.02 5 5 | 1003 -867 16 85
| 0 0 1 11 18 8 .02 | 2564 1146
jpl 80| 0 0 6 -14 36 11 .20 12 12 | 5271 -631 17 117
| 1 1 1 15 48 36 .02 | 2177 1224
mit 349| 0 -2 -3 5 -3 8 -.09 13 12 | -278 -241 67 261
| 1 0 1 34 22 14 .04 | 612 859
ngs 231| -2 0 1 -5 -27 -26 -.01 10 9 | -537 -515 1443 2998
| 0 1 2 27 23 22 .02 | 349 661
sio 317| 0 0 0 11 -25 14 -.26 13 13 | --- --- --- ---
| 1 0 1 38 28 36 .05 | --- ---
Table 1.1832.b GPS week : 1832 MJD: 57068.000-57074.000
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 4 4 4 4 4 4 |
2 | 4 5 5 5 5 5 5 |
3 | 6 6 6 6 6 6 6 |
4 | 7 7 7 7 7 8 9 |
5 | 5 5 5 5 5 5 5 |
6 | 4 4 5 4 5 4 4 |
7 | 5 4 4 5 5 4 5 |
8 | 7 9 8 7 6 5 5 |
9 | 4 4 4 4 4 4 4 |
10 | 4 4 4 4 4 4 4 |
11 | 5 5 4 5 0 5 4 |
12 | 5 5 5 5 5 5 5 |
13 | 5 4 5 5 5 5 5 |
14 | 4 5 5 4 4 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 5 5 5 4 5 |
17 | 5 5 5 5 5 4 4 |
18 | 6 6 6 6 6 6 6 |
19 | 5 5 5 6 6 5 5 |
20 | 5 5 5 5 5 5 4 |
21 | 4 4 4 4 4 4 4 |
22 | 5 5 5 5 5 5 5 |
23 | 4 4 4 4 4 4 4 |
24 | 5 4 4 4 5 4 4 |
25 | 4 5 5 5 7 4 4 |
26 | 8 8 8 10 9 8 9 |
27 | 4 4 4 4 4 4 4 |
28 | 5 4 5 4 5 5 4 |
29 | 6 5 6 5 5 5 5 |
30 | 4 4 4 4 4 4 4 |
31 | 4 4 4 4 5 4 5 |
32 | 4 4 4 4 4 4 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1832.0 GPS week: 1832 Day: 0 MJD: 57068.000
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 247| -2 1 -1 1 18 3 .07 16 14 | -558 -301 16 111
emr 80| 3 1 4 -28 -1 0 .22 12 12 | 7230 262 16 151
esa 150| 0 0 2 8 28 5 -.31 12 12 | -2219 -116 9 132
gfz 198| 0 -2 -7 21 2 -35 .07 13 12 | -234 662 11 85
grg 175| 1 -1 -5 4 37 -35 .17 17 17 | -64 77 17 144
igr n/a| 0 0 -3 -32 16 13 -.00 5 5 | 3553 200 16 89
jpl 80| 0 0 6 -30 -17 -47 .22 13 13 | 7285 255 18 122
mit 350| 2 -2 -6 47 24 19 -.13 13 11 | -380 332 85 305
ngs 233| -2 0 2 -2 -30 -2 -.02 11 9 | -321 -940 1700 3334
sio 317| -2 -2 1 -30 -34 77 -.16 13 12 | --- --- --- ---
Table 2.1832.1 GPS week: 1832 Day: 1 MJD: 57069.000
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 249| -3 0 -4 1 85 14 .01 16 14 | -37 -1564 19 116
emr 79| 2 4 6 -44 -10 7 .15 13 13 | 7731 -2060 15 110
esa 150| -1 0 2 17 18 26 -.33 13 13 | 355 -280 10 137
gfz 196| 0 -2 -6 39 14 -6 .05 12 12 | 508 -2178 12 92
grg 175| 1 0 -5 -65 16 -53 .22 17 16 | 428 -1579 17 152
igr n/a| -1 0 -3 -28 28 14 -.00 5 5 | 3749 -2341 18 90
jpl 80| 1 0 6 -32 44 -8 .20 11 11 | 7709 -2077 17 118
mit 350| 0 0 -2 28 -43 23 -.13 12 11 | 840 -1481 57 260
ngs 231| -2 0 0 -31 -63 -35 .01 11 9 | -51 -1574 2024 3659
sio 318| 0 0 0 62 -51 18 -.24 13 12 | --- --- --- ---
Table 2.1832.2 GPS week: 1832 Day: 2 MJD: 57070.000
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 248| 0 0 -6 23 64 15 -.02 16 14 | -311 -1464 18 116
emr 79| 0 5 6 -24 -11 26 .17 13 13 | 6807 -658 16 111
esa 150| 0 0 1 10 12 5 -.36 12 12 | -2563 2174 10 134
gfz 196| 0 -3 -7 53 11 15 .07 13 11 | -669 638 12 94
grg 169| 2 0 -8 -9 -4 -18 .19 18 17 | -311 526 17 136
igr n/a| 0 0 -6 -31 -2 -4 -.00 5 5 | 2720 -812 16 86
jpl 80| 0 0 3 10 -9 7 .23 11 11 | 6864 -676 18 108
mit 348| 1 -2 -2 -38 17 13 -.12 13 13 | 117 -1040 53 350
ngs 233| -2 0 7 -8 -51 -66 .01 10 8 | -534 -680 1071 2453
sio 324| 0 -1 -3 -18 0 46 -.32 15 13 | --- --- --- ---
Table 2.1832.3 GPS week: 1832 Day: 3 MJD: 57071.000
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 245| -1 1 -4 -2 -9 0 -.02 14 13 | -1297 -6 17 108
emr 80| 1 3 7 -34 -17 44 .23 13 13 | 5432 -1744 16 124
esa 150| 1 1 2 -9 -14 18 -.34 12 12 | -1553 408 11 149
gfz 198| 0 -2 -5 13 -8 11 .05 14 13 | -527 137 11 78
grg 172| 4 0 -6 -20 2 -37 .24 22 18 | 133 -550 17 135
igr n/a| 0 0 -3 -19 -23 -3 -.03 5 4 | 1214 -1604 16 102
jpl 80| -1 1 5 -23 74 -12 .22 11 11 | 5509 -1764 17 115
mit 350| 0 -2 -2 44 -2 8 -.08 13 12 | -875 -235 51 230
ngs 232| -2 -2 0 -21 -1 -40 .01 11 10 | -373 -734 1454 3194
sio 318| -1 -1 0 44 -59 3 -.29 14 14 | --- --- --- ---
Table 2.1832.4 GPS week: 1832 Day: 4 MJD: 57072.000
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 250| -1 0 -2 20 -12 -19 .03 16 14 | -794 -305 20 120
emr 80| 0 3 4 -29 -28 30 .22 13 13 | 4444 -1376 17 143
esa 150| 2 1 0 8 -14 -22 -.37 13 13 | 546 -412 10 138
gfz 200| 0 -1 -2 47 19 -6 .07 14 13 | 179 -254 13 93
grg 174| 0 0 -7 -25 -10 -17 .17 18 18 | 268 -248 17 143
igr n/a| 0 0 -1 -4 -5 -3 -.04 5 5 | 323 -1760 17 85
jpl 80| 0 1 7 -10 119 38 .17 14 14 | 4499 -1383 20 116
mit 350| 0 -3 -3 -26 -13 16 -.05 13 12 | -494 -131 57 243
ngs 231| -1 -1 1 11 -30 -8 -.02 10 9 | -491 -118 1231 2754
sio 319| 0 0 1 -3 -30 -13 -.28 14 13 | --- --- --- ---
Table 2.1832.5 GPS week: 1832 Day: 5 MJD: 57073.000
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 250| 0 1 -2 23 6 17 .02 15 13 | -1484 988 16 123
emr 80| 0 1 5 -57 18 3 .21 13 13 | 2713 -100 17 143
esa 150| 2 2 0 -21 -34 -16 -.34 13 13 | 232 808 10 140
gfz 189| 0 -1 -5 27 -13 31 .01 12 10 | -457 474 12 95
grg 169| 1 0 -10 -49 18 -47 .17 18 17 | 31 154 17 153
igr n/a| 0 0 -2 -23 -8 -1 -.02 5 5 | -1740 -678 16 75
jpl 80| 0 0 7 -8 39 54 .20 12 12 | 2750 -149 17 119
mit 350| 0 -2 -2 1 -11 -11 -.05 12 12 | -935 1142 111 261
ngs 228| -2 0 1 45 -5 -23 -.03 10 8 | -1003 310 1323 2484
sio 313| -1 0 1 -19 -22 -22 -.27 14 13 | --- --- --- ---
Table 2.1832.6 GPS week: 1832 Day: 6 MJD: 57074.000
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 248| 0 0 -2 34 2 1 .02 13 14 | -797 -71 19 111
emr 80| 1 1 5 -14 2 -6 .22 12 12 | 2253 1396 12 151
esa 150| 0 0 1 6 -32 -1 -.37 12 12 | -2016 2772 10 148
gfz 198| -2 -1 -5 23 -33 19 .06 13 12 | -241 271 12 89
grg 170| 2 0 -7 -47 53 -59 .21 18 17 | -178 463 16 152
igr n/a| 0 0 -3 -7 -19 0 -.04 5 5 | -2797 920 17 73
jpl 80| 0 0 4 -4 6 44 .18 11 11 | 2286 1377 17 126
mit 350| 0 -2 -1 -14 3 -13 -.06 12 12 | -225 -275 57 179
ngs 230| -1 1 1 -32 -8 -11 -.01 9 7 | -987 127 1302 3112
sio 314| 0 -1 0 48 21 -8 -.26 12 11 | --- --- --- ---
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 3.1832.0 GPS week: 1832 Day: 0 MJD: 57068.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 15 11 16 14 14 6 12 8 10 9 4 | 22 19 26 21 22 20 18 17 16 19 18
2E | 10 11 7 11 18 5 13 14 10 9 4 | 21 24 16 20 22 18 19 19 21 22 19
X3 | 15 13 8 16 --- 8 15 18 12 25 6 | 127 136 129 120 --- 126 135 121 130 132 128
4E | 45 14 12 13 16 6 17 12 19 14 7 | 46 30 30 29 29 26 24 28 31 28 25
5 | 10 12 17 16 15 5 12 16 9 12 4 | 25 34 30 17 22 22 33 22 27 25 24
6E | 10 13 13 11 18 6 11 10 8 9 4 | 17 23 23 14 24 19 20 17 18 22 18
7 | 16 18 6 11 17 5 17 8 9 9 4 | 32 27 19 25 30 24 26 23 26 20 23
X8E | 31 15 14 16 24 9 13 13 14 --- 6 | 126 119 115 116 17 119 117 120 121 --- 118
9 | 13 10 11 10 9 5 10 11 6 9 3 | 61 53 52 60 61 55 53 59 51 52 54
10 | 5 12 12 9 19 4 11 11 6 5 3 | 20 19 16 24 29 19 16 24 18 20 19
11 | 17 10 11 11 17 3 12 12 8 15 4 | 9999 20 12 18 30 86 20 14 16 11 9999
12 | 16 11 12 13 22 4 10 12 8 13 4 | 24 24 14 21 26 16 22 15 19 16 16
13 | 11 12 12 11 18 3 13 13 11 11 4 | 36 36 27 36 42 32 36 32 29 28 31
14 | 12 10 12 13 17 4 12 12 11 13 4 | 32 30 26 40 39 32 28 31 32 32 30
15 | 12 13 14 17 17 4 13 15 15 18 5 | 31 33 24 38 37 29 31 31 27 32 28
16 | 13 13 6 20 18 5 14 11 12 16 4 | 25 24 15 21 21 17 23 16 22 10 16
17 | 10 15 10 17 15 5 12 15 10 12 4 | 25 32 23 34 33 25 31 27 29 23 26
18 | 20 14 12 19 21 6 14 17 14 16 5 | 33 32 25 42 41 30 29 30 29 26 28
19 | 15 11 10 17 17 5 16 20 12 14 5 | 24 30 20 29 27 21 25 23 24 22 22
20 | 10 17 14 14 21 4 14 18 8 13 5 | 58 59 55 59 64 57 58 58 58 57 57
21E | 14 11 5 11 21 6 15 8 10 9 4 | 23 20 17 19 21 17 23 16 17 19 16
22 | 17 12 13 14 18 5 14 13 11 15 5 | 37 35 30 42 45 36 33 39 32 33 34
23 | 8 11 11 12 13 5 12 11 11 12 4 | 30 31 29 34 34 30 29 31 25 24 27
24 | 13 10 13 9 14 5 11 10 16 15 4 | 23 25 23 19 24 22 22 21 25 22 21
25 | 10 18 14 9 14 4 11 9 8 12 4 | 20 28 24 19 22 20 24 14 18 23 19
X26 | 16 12 20 --- --- 9 --- 12 18 --- 8 | 35 30 30 --- --- 32 --- 32 34 --- 29
27 | 17 10 12 14 15 4 11 8 10 11 4 | 22 30 21 22 25 21 25 19 21 22 20
28 | 9 12 11 14 19 4 13 15 11 11 4 | 19 30 17 27 31 21 27 21 27 19 22
29 | 20 14 11 15 20 6 13 17 11 19 5 | 38 37 31 28 30 30 34 25 30 30 28
30 | 17 12 12 9 19 7 12 8 8 7 4 | 30 25 30 22 26 23 26 21 22 22 23
31 | 13 10 9 8 20 4 12 10 7 14 4 | 25 26 15 25 36 23 25 21 23 21 21
32 | 10 8 7 12 14 5 9 14 8 10 3 | 13 17 13 18 18 12 15 17 12 14 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 12 12 13 17 5 13 13 11 13 |T 35 35 30 34 30 33 33 31 32 28 31
WRMS | 14 12 12 12 17 5 13 11 9 12 |NE 32 33 26 32 29 32 31 28 29 27 28
MEDI | 13 12 12 13 17 5 12 12 10 12 |MD 25 30 24 25 29 23 26 23 25 22 23
Table 3.1832.1 GPS week: 1832 Day: 1 MJD: 57069.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 14 12 14 9 19 7 9 9 9 9 4 | 24 18 24 21 23 18 19 18 17 18 18
2E | 18 8 7 13 18 4 10 15 12 11 4 | 22 19 15 20 17 15 19 19 21 18 16
X3 | 15 15 11 17 --- 7 14 18 12 19 5 | 78 87 81 74 --- 78 87 81 79 86 81
4E | 38 17 15 11 20 8 16 12 21 18 6 | 41 29 25 24 30 21 23 24 27 21 21
5 | 14 12 17 13 18 6 13 17 13 14 5 | 28 27 27 20 22 19 28 22 25 24 22
6E | 14 11 15 9 17 5 10 10 8 9 4 | 19 22 26 18 22 19 21 19 19 22 19
7 | 12 13 9 9 19 5 15 9 10 12 4 | 29 22 18 23 29 21 25 22 20 17 19
X8E | 39 17 19 23 --- 10 15 24 15 --- 9 | 104 86 81 82 --- 83 86 69 82 --- 81
9 | 12 10 14 9 13 4 9 13 6 9 3 | 39 39 33 35 39 36 39 39 36 34 35
10 | 7 11 13 8 19 4 11 12 8 7 3 | 16 16 17 18 19 14 13 21 17 20 15
11 | 21 13 12 10 15 4 9 13 9 12 4 | 9999 20 13 18 21 87 19 13 12 13 9999
12 | 18 17 11 15 19 5 10 12 14 15 5 | 28 28 17 24 27 19 23 18 22 15 18
13 | 13 12 12 10 16 6 14 13 10 8 4 | 22 32 22 28 35 22 31 22 21 23 24
14 | 14 10 14 14 15 4 8 11 11 15 4 | 35 27 24 34 29 26 26 26 29 24 26
15 | 17 11 13 16 15 4 13 13 11 15 5 | 27 30 21 31 29 22 27 23 22 26 23
16 | 19 13 8 15 15 5 9 9 12 14 4 | 33 24 18 21 24 21 24 18 22 16 19
17 | 10 13 12 17 16 4 13 12 13 14 4 | 23 29 21 28 29 23 29 21 28 20 23
18 | 16 16 15 18 20 5 11 15 13 15 5 | 28 26 22 35 33 24 26 23 21 24 23
19 | 16 11 14 12 15 7 10 21 13 14 5 | 27 25 20 24 21 19 24 17 17 19 18
20 | 8 17 14 11 18 4 12 15 12 14 4 | 68 70 66 68 70 68 70 68 70 67 68
21E | 20 14 7 12 21 6 8 6 10 11 4 | 29 24 20 24 22 23 27 19 21 23 20
22 | 12 15 14 14 18 5 10 11 11 13 4 | 30 27 22 35 34 27 28 28 28 25 26
23 | 7 9 12 12 12 5 10 15 7 13 4 | 25 23 24 24 20 22 23 22 19 19 20
24 | 13 13 13 11 14 6 9 9 13 13 4 | 23 24 22 20 22 18 18 22 20 23 18
25 | 13 21 16 11 13 4 11 9 12 11 4 | 21 28 21 21 21 17 22 13 18 16 16
X26 | 22 10 17 --- --- 8 --- 12 17 --- 8 | 33 25 21 --- --- 24 --- 25 33 --- 25
27 | 10 11 13 8 9 5 8 6 10 10 3 | 19 24 21 21 22 19 24 16 18 21 19
28 | 10 14 10 13 17 4 12 10 8 13 4 | 21 30 16 21 29 18 25 18 20 17 19
29 | 20 13 11 14 18 5 11 13 10 20 5 | 31 28 23 26 25 23 27 22 25 25 23
30 | 9 9 13 7 21 5 9 9 8 9 3 | 24 21 28 20 30 21 24 22 21 22 21
31 | 14 10 10 8 18 4 9 9 8 14 4 | 27 21 14 24 34 20 22 19 22 17 19
32 | 9 10 10 11 15 5 7 12 8 8 3 | 16 14 14 17 14 11 13 13 14 10 11
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 13 13 12 17 5 11 12 11 13 |T 31 30 26 29 27 28 29 25 27 24 26
WRMS | 14 13 13 12 16 5 11 11 9 12 |NE 28 27 22 26 25 27 26 23 23 22 23
MEDI | 14 12 13 12 17 5 10 12 11 13 |MD 27 25 21 24 25 21 24 22 21 21 20
Table 3.1832.2 GPS week: 1832 Day: 2 MJD: 57070.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 19 11 14 11 14 6 9 11 8 10 4 | 21 20 25 19 21 18 21 18 20 17 18
2E | 16 10 10 11 24 5 10 17 8 12 4 | 26 23 18 19 27 17 22 18 18 20 18
X3 | 19 15 8 16 --- 7 16 16 9 23 5 | 106 112 105 98 --- 102 113 100 108 111 106
4E | 39 15 12 12 17 6 17 14 17 20 6 | 40 26 25 26 28 23 27 25 31 27 23
5 | 10 15 14 16 19 5 16 16 13 15 5 | 27 34 29 24 25 22 31 25 28 25 25
6E | 20 12 14 11 18 4 10 13 6 10 4 | 23 21 26 20 28 19 22 21 20 20 19
7 | 8 14 8 11 17 5 14 11 8 10 4 | 33 28 24 29 29 25 28 23 27 21 24
X8E | 30 18 16 19 --- 10 18 14 12 --- 7 | 107 100 98 93 --- 99 103 97 101 --- 98
9 | 11 10 13 12 11 5 9 16 6 11 4 | 49 45 40 46 49 43 47 45 39 42 43
10 | 10 11 13 10 21 4 10 11 8 17 4 | 27 19 20 25 25 19 18 23 19 23 19
11 | 17 12 11 9 20 6 9 12 7 13 4 | 9999 19 15 20 27 122 23 13 19 13 9999
12 | 14 15 11 15 19 3 11 13 12 15 4 | 26 27 19 25 28 19 26 18 24 19 20
13 | 11 14 13 12 15 4 14 16 9 10 4 | 29 32 26 30 36 25 33 29 23 28 26
14 | 12 7 12 17 18 4 10 12 10 22 4 | 32 29 27 40 33 30 31 30 27 37 29
15 | 11 14 14 16 15 4 13 14 10 16 4 | 27 28 25 35 31 24 29 27 24 30 25
16 | 22 12 9 15 20 5 8 8 11 14 4 | 30 23 17 21 24 17 21 17 19 14 17
17 | 12 14 10 19 16 4 12 9 10 18 4 | 26 35 24 34 32 24 34 25 30 21 27
18 | 20 15 12 20 22 6 13 18 13 19 5 | 31 30 24 39 34 27 29 28 23 24 25
19 | 20 12 11 14 18 7 11 21 10 16 5 | 27 27 20 26 26 19 27 21 25 21 22
20 | 10 13 12 13 20 3 11 14 9 17 4 | 55 56 52 54 56 53 56 56 52 52 53
21E | 12 11 8 12 20 6 11 9 8 11 4 | 25 26 25 24 29 24 27 22 24 25 23
22 | 15 12 13 13 21 5 11 13 9 13 4 | 30 28 24 35 39 29 29 32 24 29 27
23 | 9 10 10 12 13 7 11 12 9 18 4 | 31 29 29 30 28 28 30 26 25 23 26
24 | 13 8 14 11 12 5 10 10 7 12 3 | 41 37 42 42 39 40 40 41 40 40 39
25 | 13 25 14 8 15 4 9 12 10 14 5 | 22 31 25 23 23 20 23 17 20 23 19
X26 | 26 10 12 --- --- 13 --- 15 15 --- 8 | 30 27 29 --- --- 33 --- 29 33 --- 28
27 | 12 11 13 9 13 6 9 8 7 12 3 | 24 28 21 23 24 20 26 18 22 19 21
28 | 10 11 13 15 18 4 11 11 12 16 4 | 20 29 21 28 31 18 26 16 24 19 20
29 | 23 15 11 14 17 5 12 16 11 19 5 | 38 34 30 31 29 30 35 27 30 30 29
30 | 7 13 15 8 18 5 9 8 7 8 3 | 29 27 35 29 28 27 29 25 29 25 27
31 | 11 15 9 9 19 4 11 10 9 12 4 | 27 25 20 27 35 22 26 22 24 19 22
32 | 14 9 10 10 15 5 9 10 8 10 3 | 14 16 14 20 20 12 17 14 14 15 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 13 12 13 18 5 11 13 10 15 |T 34 33 30 33 30 32 33 29 30 27 30
WRMS | 14 13 12 11 17 5 11 13 8 13 |NE 31 31 26 31 28 33 30 26 28 27 27
MEDI | 13 12 12 12 18 5 11 12 9 14 |MD 29 28 25 28 28 24 28 25 24 23 25
Table 3.1832.3 GPS week: 1832 Day: 3 MJD: 57071.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 10 15 14 11 18 6 11 11 6 11 4 | 21 27 27 22 30 22 23 19 22 15 21
2E | 19 11 8 16 18 4 11 15 11 14 5 | 30 27 17 23 26 21 22 22 20 23 20
X3 | 16 13 9 17 --- 7 16 11 11 20 5 | 122 125 124 113 --- 117 127 115 120 123 121
4E | 35 17 15 12 22 5 17 15 21 19 7 | 38 26 25 23 34 24 25 26 31 19 22
5 | 9 13 15 14 17 5 12 16 13 13 4 | 26 34 29 24 28 23 31 26 25 26 25
6E | 12 11 15 12 18 6 9 10 10 13 4 | 19 23 27 22 29 21 22 23 19 22 21
7 | 9 14 9 10 20 6 15 12 10 17 4 | 27 24 18 25 30 23 27 21 23 19 20
X8 | 17 16 17 16 --- 10 14 13 17 --- 6 | 98 101 94 93 --- 93 105 100 96 --- 97
9M | 6 9 13 14 13 3 10 9 7 10 3 | 50 49 41 51 55 48 47 50 48 43 47
10 | 8 10 11 11 16 4 11 10 9 12 4 | 18 22 17 23 26 20 19 23 22 19 19
11 | 11 14 14 11 75 7 11 11 9 12 4 | 9999 21 13 17 58 239 19 13 16 11 9999
12 | 17 12 10 13 19 3 10 15 10 14 4 | 30 28 17 25 29 22 25 21 23 16 21
13 | 16 14 12 11 14 5 13 17 14 13 5 | 36 34 25 31 35 27 33 32 29 23 28
14 | 8 11 13 16 19 4 10 9 9 15 4 | 30 28 24 40 36 29 27 29 31 29 28
15 | 12 17 11 16 12 4 11 13 10 15 4 | 31 31 25 34 31 26 28 28 25 24 26
16 | 22 12 10 19 18 5 9 12 12 15 5 | 31 25 17 20 24 19 24 19 21 14 18
17M | 7 12 12 18 14 5 11 8 12 18 4 | 28 36 29 37 38 30 34 31 33 25 30
18 | 17 16 12 22 24 4 15 17 13 17 6 | 26 28 21 37 33 23 25 25 21 23 22
19 | 18 11 14 13 19 6 9 22 16 16 5 | 26 29 19 25 27 19 26 22 24 21 21
20M | 8 14 13 14 20 3 11 13 10 13 4 | 98 103 96 98 97 98 103 96 98 101 98
21E | 12 10 8 14 19 5 11 9 13 9 4 | 20 20 13 17 19 17 22 17 20 17 16
22 | 15 13 14 14 21 3 10 14 11 15 5 | 27 29 23 35 39 26 27 32 26 26 26
23M | 10 9 11 15 15 4 9 11 10 17 4 | 29 30 27 35 35 28 30 29 26 24 27
24 | 9 10 15 8 12 4 9 10 7 12 3 | 43 47 46 49 49 47 46 40 50 41 45
25 | 12 22 14 8 13 4 8 10 9 11 4 | 23 30 25 23 24 21 25 19 19 22 20
X26 | 24 15 23 --- --- 15 --- 14 23 --- 10 | 32 30 26 --- --- 23 --- 32 41 --- 28
27 | 17 11 14 10 17 4 8 9 9 9 4 | 23 30 21 22 27 21 26 19 26 20 22
28 | 8 13 11 14 16 5 7 9 13 13 4 | 22 32 19 27 31 20 28 22 21 21 22
29M | 19 12 10 16 18 5 12 16 12 17 5 | 37 35 29 28 31 29 35 23 29 29 28
30 | 9 13 14 7 19 6 9 11 9 10 4 | 25 24 28 22 27 22 26 23 23 23 22
31 | 8 17 12 8 21 3 13 10 10 11 4 | 24 26 17 26 36 22 26 21 24 18 22
32 | 9 9 11 10 16 2 7 9 10 12 3 | 18 23 18 19 19 18 20 19 21 15 17
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 14 13 12 14 22 5 11 13 11 14 |T 35 36 31 35 34 38 35 32 33 28 32
WRMS | 13 13 12 13 18 4 11 12 10 14 |NE 31 32 26 31 31 41 31 27 28 26 28
MEDI | 12 13 12 14 18 5 11 11 10 13 |MD 28 29 25 25 31 23 26 23 24 22 22
Table 3.1832.4 GPS week: 1832 Day: 4 MJD: 57072.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 15 15 10 12 6 16 8 7 8 4 | 19 22 22 20 20 16 18 18 17 15 16
2E | 13 14 9 14 16 6 12 14 8 12 4 | 24 26 15 24 23 19 27 22 21 19 20
X3 | 22 15 8 15 --- 8 18 12 12 19 5 | 103 106 100 94 --- 97 102 93 99 102 99
4E | 39 14 16 10 19 5 14 15 14 19 6 | 43 30 27 28 29 24 24 31 29 28 25
5M | 10 12 15 12 16 5 15 15 11 15 4 | 33 38 34 28 28 29 40 28 28 32 29
6E | 12 14 15 13 16 4 12 10 9 14 4 | 22 20 25 24 24 20 23 20 21 22 20
7 | 12 15 11 9 23 5 16 10 7 13 4 | 29 24 20 27 31 22 26 21 22 18 21
X8 | 16 17 12 12 --- 5 15 9 11 --- 5 | 74 84 75 75 --- 76 81 72 78 --- 76
9 | 8 9 13 13 13 4 10 9 8 11 3 | 37 41 32 38 46 36 41 40 34 35 36
10 | 11 9 11 13 20 5 12 12 8 14 4 | 28 26 25 30 30 24 22 32 23 30 25
X11 | 2 --- --- --- --- >>>> --- --- --- --- 0 | 9999 --- --- --- --- 9999 --- --- --- --- 9999
12 | 17 10 11 11 19 4 11 13 11 12 4 | 27 27 17 22 26 18 26 20 21 11 19
13M | 11 13 13 12 11 5 16 16 10 11 4 | 33 33 27 35 35 28 35 31 28 27 29
14 | 9 13 14 13 17 4 11 9 9 14 4 | 27 29 21 36 30 24 25 29 28 27 26
15M | 11 16 11 15 11 4 15 12 9 17 4 | 32 30 25 33 28 26 31 30 29 25 27
16 | 24 11 13 15 19 6 12 12 9 19 5 | 30 24 20 23 22 18 23 19 18 12 18
17 | 9 11 15 17 14 3 14 8 12 17 4 | 27 31 23 32 32 24 31 25 28 23 26
18 | 18 17 14 14 22 5 16 16 12 15 5 | 25 27 19 29 30 19 25 22 19 15 19
19 | 24 14 15 14 21 6 14 22 14 17 6 | 30 27 21 28 28 21 26 24 26 24 22
20 | 11 19 12 16 17 6 13 14 8 15 5 | 83 80 81 82 90 84 77 87 84 86 82
21E | 10 13 9 10 16 3 13 8 10 9 4 | 21 26 19 22 25 20 23 19 20 22 20
22 | 17 13 16 10 20 3 13 13 10 13 4 | 24 27 20 28 34 22 25 29 23 20 23
23 | 13 9 12 13 14 5 10 14 9 16 4 | 25 24 23 27 26 21 26 23 20 17 21
24M | 16 13 14 12 25 6 13 15 7 9 4 | 91 89 89 85 73 84 89 89 88 85 86
25 | 14 18 19 34 17 5 34 14 11 13 7 | 25 26 27 48 24 23 50 16 18 18 23
X26M | 22 13 12 --- --- 16 --- 16 20 --- 8 | 31 25 26 --- --- 29 --- 29 35 --- 26
27 | 16 10 16 8 18 4 12 10 5 8 4 | 20 26 21 22 23 18 27 19 19 17 19
28 | 8 13 12 15 17 4 14 10 10 12 4 | 17 29 17 27 28 18 25 19 22 18 19
29 | 19 13 11 15 16 4 13 13 11 17 5 | 88 87 87 88 86 86 91 84 88 83 86
30 | 11 11 16 9 19 6 10 11 7 8 4 | 23 22 30 24 29 22 23 20 21 18 21
31 | 12 11 13 7 21 3 12 10 13 11 4 | 24 24 17 27 35 20 25 20 25 16 21
32 | 14 9 13 9 16 4 12 11 9 9 4 | 14 18 13 14 15 11 17 17 12 13 12
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 13 13 14 18 5 14 13 10 14 |T 36 37 32 37 33 32 37 33 33 30 32
WRMS | 14 13 13 13 18 5 14 12 9 13 |NE 29 30 25 31 27 25 31 26 26 23 25
MEDI | 12 13 13 13 17 5 13 12 10 13 |MD 27 27 23 28 28 22 26 24 23 22 23
Table 3.1832.5 GPS week: 1832 Day: 5 MJD: 57073.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 16 12 14 7 13 5 10 8 5 7 3 | 21 21 22 18 24 18 20 17 17 12 17
2E | 14 12 9 14 24 5 13 13 8 13 4 | 24 24 17 18 28 19 23 18 21 22 18
X3 | 14 16 8 12 --- 6 16 17 15 23 6 | 98 105 95 93 --- 95 107 93 99 104 98
4E | 47 13 14 11 21 5 17 14 20 20 7 | 49 29 27 26 27 25 29 29 34 22 24
5 | 12 12 14 13 18 5 15 14 10 14 4 | 25 29 24 18 23 19 29 21 18 22 20
6E | 9 11 14 10 22 4 9 13 7 11 4 | 22 26 26 20 34 22 25 23 19 22 22
7 | 13 11 9 12 18 4 16 10 8 13 4 | 25 24 15 24 31 20 24 19 20 13 19
X8 | 10 13 14 13 --- 7 10 10 10 --- 4 | 51 61 53 53 --- 51 55 47 52 --- 52
9 | 10 9 12 12 11 4 11 6 6 16 3 | 36 43 33 36 44 34 38 35 32 36 35
10 | 9 11 12 8 19 3 10 10 4 13 3 | 22 19 19 20 26 18 17 22 17 21 18
X11 | 10 10 14 15 22 17 9 11 11 --- 4 | 9999 18 11 19 12 619 15 9 13 --- 9999
12 | 17 15 10 13 22 5 14 11 11 12 4 | 30 27 18 24 30 21 26 22 21 18 21
13 | 14 15 10 13 17 5 17 14 11 13 5 | 34 33 27 30 36 28 31 27 27 27 27
14 | 8 12 15 12 18 4 11 12 12 16 4 | 24 26 20 31 28 24 23 27 29 22 24
15 | 12 18 12 14 14 5 15 13 13 16 5 | 30 29 26 28 29 25 27 26 28 23 24
16 | 14 11 10 13 16 5 12 12 8 15 4 | 25 24 18 20 22 19 23 18 20 11 18
17 | 9 11 14 15 14 5 10 9 9 14 4 | 27 34 24 32 32 26 32 28 27 23 27
18 | 17 18 12 17 22 5 16 17 13 17 5 | 24 27 18 28 30 19 25 21 19 20 19
19 | 14 12 13 13 17 6 12 22 11 17 5 | 23 26 18 24 22 17 22 21 17 22 18
20 | 8 17 13 12 19 5 12 14 8 14 4 | 83 83 82 84 85 82 81 83 81 87 82
21E | 18 11 9 11 21 5 11 9 12 10 4 | 23 23 15 15 24 15 19 13 16 13 14
22 | 14 13 15 11 21 4 13 13 8 14 4 | 25 26 20 24 33 20 23 25 21 18 21
23 | 9 8 12 10 13 3 9 15 8 14 4 | 24 27 24 21 24 22 25 25 21 14 21
24 | 13 8 13 11 14 4 11 9 9 17 4 | 72 69 71 69 67 68 70 70 73 69 70
25 | 11 13 15 6 17 6 7 9 8 11 3 | 22 28 27 23 25 24 26 18 17 23 21
X26 | 22 13 16 --- --- 12 --- 13 17 --- 8 | 33 30 23 --- --- 28 --- 26 38 --- 28
27 | 12 9 15 6 14 5 10 8 8 7 3 | 22 27 18 18 23 19 23 18 18 15 18
28 | 9 26 11 14 20 6 11 12 9 11 5 | 19 34 17 25 29 19 23 20 18 16 18
29 | 16 12 13 13 21 6 15 15 10 17 5 | 192 191 188 187 188 190 188 188 189 187 188
30 | 13 12 14 7 17 5 9 9 4 7 3 | 25 23 26 19 28 21 24 19 20 16 20
31 | 13 10 11 9 23 5 9 11 10 14 4 | 22 27 15 22 37 20 25 20 24 19 21
32 | 8 8 11 10 16 4 9 11 8 8 3 | 14 18 15 14 18 15 17 15 16 12 13
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 13 13 12 18 5 12 12 10 14 |T 37 38 32 34 36 51 36 33 33 32 33
WRMS | 13 13 13 10 17 5 12 12 8 13 |NE 28 29 23 26 26 61 27 24 24 23 24
MEDI | 13 12 13 12 18 5 11 12 9 14 |MD 25 27 22 24 28 21 25 22 21 22 21
Table 3.1832.6 GPS week: 1832 Day: 6 MJD: 57074.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1E | 11 11 13 11 11 6 11 9 8 5 3 | 29 28 28 23 25 25 26 22 26 19 24
2E | 17 12 6 15 21 5 10 13 9 11 4 | 32 31 21 26 34 24 27 25 26 26 25
X3 | 17 20 8 15 --- 8 17 18 13 18 6 | 129 136 126 118 --- 124 137 119 127 131 127
X4E | 47 17 16 16 20 6 --- 16 21 20 8 | 60 38 38 37 38 37 --- 40 41 35 35
5 | 9 12 15 15 20 5 12 14 9 12 4 | 34 40 35 25 32 29 41 32 31 33 31
6E | 8 11 13 11 23 6 10 15 4 11 4 | 30 31 35 28 38 31 29 34 30 31 30
7 | 12 14 8 10 19 5 12 16 7 14 4 | 31 26 22 27 30 25 26 27 24 22 24
X8 | 13 14 14 14 --- 9 7 11 12 --- 5 | 91 93 87 86 --- 89 89 87 90 --- 89
9 | 9 8 12 12 12 5 8 11 5 13 3 | 54 52 47 56 59 52 53 53 47 50 51
10 | 9 12 11 10 19 4 10 11 5 9 3 | 24 24 22 27 34 23 21 27 22 21 22
11 | 14 10 13 9 18 3 8 11 7 13 4 | 9999 22 14 18 12 355 19 11 14 7 9999
12 | 17 11 10 14 19 5 10 12 9 12 4 | 30 32 20 27 32 24 29 23 24 14 23
13 | 14 14 12 13 18 6 14 13 10 12 4 | 38 37 32 41 47 36 37 37 34 32 35
14 | 11 10 13 13 16 5 11 15 9 22 4 | 30 31 25 38 36 28 27 35 26 33 28
15 | 12 14 11 17 15 7 15 12 10 15 4 | 34 34 27 40 39 30 32 34 30 30 31
16 | 15 13 12 13 19 5 10 11 9 15 4 | 25 22 17 20 22 18 22 19 20 13 17
17 | 8 13 12 17 14 5 9 9 9 13 4 | 32 37 28 40 33 31 35 33 33 23 31
18 | 21 14 12 18 22 4 14 17 13 15 5 | 30 30 22 38 39 26 26 29 23 21 25
19 | 20 12 12 12 16 6 11 22 11 17 5 | 30 29 21 28 27 21 27 25 24 26 23
20 | 6 18 12 13 16 4 9 13 7 13 4 | 69 72 68 73 72 69 68 71 69 69 69
21E | 9 9 9 11 17 5 10 8 10 9 3 | 25 26 20 23 31 22 26 24 20 25 22
22 | 18 11 13 13 22 3 12 13 9 12 4 | 29 29 27 38 45 30 27 37 28 28 29
23 | 9 10 12 11 16 5 8 10 9 13 3 | 46 45 43 49 48 46 47 46 41 39 43
24 | 15 11 13 13 13 5 11 11 8 14 4 | 58 66 60 63 67 61 63 59 61 55 60
25 | 10 12 15 8 13 6 8 8 8 6 3 | 24 27 27 22 25 24 26 18 24 22 22
X26 | 23 13 18 --- --- 10 --- 14 16 --- 8 | 40 32 30 --- --- 32 --- 33 36 --- 32
27 | 12 10 14 8 15 3 9 9 7 7 3 | 25 31 26 24 27 24 30 25 25 21 25
28 | 7 15 13 15 14 5 10 9 8 9 4 | 21 28 16 28 27 17 23 20 20 16 19
29 | 20 12 12 13 18 8 11 12 11 12 4 | 307 308 309 308 307 306 308 308 305 315 308
30 | 15 17 14 8 18 4 9 11 7 8 4 | 31 27 32 27 27 25 26 23 24 24 24
31 | 21 15 14 11 22 4 11 11 9 10 4 | 32 29 18 28 39 23 27 25 24 19 24
32 | 11 9 10 12 16 4 8 12 6 8 3 | 21 22 18 22 24 18 22 23 19 16 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 12 13 17 5 11 12 9 12 |T 48 47 42 46 45 53 46 44 43 40 44
WRMS | 14 12 12 12 17 5 11 12 7 11 |NE 34 34 28 33 29 50 32 30 29 27 30
MEDI | 12 12 12 13 18 5 10 12 9 12 |MD 31 31 27 28 34 28 27 29 26 25 28
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 4.1832 GPS week: 1832 MJD: 57068.0-57074.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 |U 5 5 15 |U 9 10 34 |U 7 8 20 |
emr | emr 3053 | 6 5 15 |U 9 11 34 | 7 8 18 |
esa | esa 3058 | 6 5 14 |U 8 10 34 | 7 7 18 |
gfz | gfz 2957 |U 6 5 15 |U 8 8 33 |U 6 6 16 |
grg | grg 2783 | 7 6 18 |U 10 11 40 |U 9 11 29 |
igr | igr 3040 | 6 5 13 | 8 9 31 | 6 6 17 |
igs | igs 3054 | 6 4 13 | 8 9 33 | 5 7 16 |
jpl | jpl 2944 | 6 5 15 |U 8 9 34 |U 8 9 18 |
mit | mit 3058 | 15 10 26 |U 11 13 50 |U 9 22 26 |
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 5.1832.0 GPS week: 1832 Day: 0 MJD: 57068.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 8 5 19 | 9 12 33 | 6 8 24 |
emr | emr 3064 | 6 6 18 | 10 13 32 | 5 9 19 |
esa | esa 3072 | 6 6 16 | 9 14 34 | 7 9 21 |
gfz | gfz 2969 | 6 7 16 | 8 12 30 | 5 8 18 |
grg | grg 2880 | 6 5 11 | 11 14 40 | 8 12 32 |
igr | igr 3071 | 5 5 14 | 9 11 30 | 6 8 18 |
igs | igs 3065 | 6 5 12 | 9 13 30 | 4 8 18 |
jpl | jpl 2968 | 6 5 14 | 10 14 36 | 7 11 17 |
mit | mit 3072 | 36 21 41 | 12 14 47 | 10 10 33 |
Table 5.1832.1 GPS week: 1832 Day: 1 MJD: 57069.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3056 | 5 5 11 | 9 8 21 | 7 10 25 |
emr | emr 3066 | 6 4 15 | 10 10 26 | 7 9 24 |
esa | esa 3072 | 7 4 12 | 8 7 27 | 7 8 21 |
gfz | gfz 2969 | 6 4 13 | 8 6 24 | 7 8 21 |
grg | grg 2784 | 8 6 12 | 11 11 36 | 8 12 32 |
igr | igr 3054 | 7 4 13 | 7 6 22 | 7 7 19 |
igs | igs 3066 | 6 3 12 | 8 7 24 | 6 8 20 |
jpl | jpl 2970 | 5 4 12 | 8 7 26 | 8 12 19 |
mit | mit 3072 | 11 7 19 | 13 19 39 | 10 11 34 |
Table 5.1832.2 GPS week: 1832 Day: 2 MJD: 57070.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3046 | 6 6 18 | 8 9 35 | 8 5 18 |
emr | emr 3067 | 12 7 15 | 9 9 28 | 6 6 14 |
esa | esa 3072 | 11 8 17 | 7 8 26 | 6 6 16 |
gfz | gfz 2969 | 8 7 14 | 7 7 31 | 6 4 15 |
grg | grg 2784 | 8 6 21 | 11 8 30 | 9 10 29 |
igr | igr 3042 | 11 7 15 | 6 7 26 | 7 5 16 |
igs | igs 3067 | 11 7 14 | 7 7 30 | 5 5 14 |
jpl | jpl 2972 | 9 6 12 | 7 8 28 | 6 8 17 |
mit | mit 3072 | 11 11 18 | 8 8 45 | 7 5 16 |
Table 5.1832.3 GPS week: 1832 Day: 3 MJD: 57071.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3055 | 4 2 12 | 7 8 29 | 6 6 15 |
emr | emr 3068 | 6 4 12 | 7 8 36 | 7 8 18 |
esa | esa 3072 | 4 4 14 | 8 9 32 | 6 6 18 |
gfz | gfz 2972 | 5 5 14 | 8 7 35 | 6 7 17 |
grg | grg 2784 | 6 4 17 | 9 8 29 | 9 7 22 |
igr | igr 3055 | 4 4 11 | 7 8 30 | 7 6 15 |
igs | igs 3067 | 5 4 12 | 7 7 32 | 6 7 16 |
jpl | jpl 2972 | 5 5 15 | 7 7 31 | 8 8 17 |
mit | mit 3072 | 7 5 21 | 8 8 40 | 7 7 18 |
Table 5.1832.4 GPS week: 1832 Day: 4 MJD: 57072.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2966 | 5 5 16 | 9 10 38 | 7 9 21 |
emr | emr 2972 | 6 5 17 | 7 8 35 | 7 9 18 |
esa | esa 2976 | 5 6 16 | 7 10 41 | 6 7 17 |
gfz | gfz 2877 | 6 5 14 | 7 8 39 | 5 7 16 |
grg | grg 2688 | 10 5 26 | 8 10 44 | 9 12 25 |
igr | igr 2967 | 4 4 12 | 7 9 37 | 6 7 18 |
igs | igs 2973 | 5 4 16 | 7 8 37 | 5 8 16 |
jpl | jpl 2876 | 6 6 17 | 7 8 39 | 8 11 22 |
mit | mit 2976 | 9 12 38 | 14 14 80 | 14 105 51 |
Table 5.1832.5 GPS week: 1832 Day: 5 MJD: 57073.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3046 | 6 4 13 | 10 12 39 | 6 7 19 |
emr | emr 3068 | 6 7 17 | 10 16 38 | 7 6 18 |
esa | esa 3072 | 5 5 13 | 10 12 35 | 7 5 14 |
gfz | gfz 2972 | 5 5 16 | 10 11 38 | 7 6 13 |
grg | grg 2784 | 6 6 18 | 12 15 56 | 10 11 30 |
igr | igr 3041 | 5 5 12 | 9 11 33 | 6 6 15 |
igs | igs 3068 | 5 5 13 | 10 11 37 | 6 6 15 |
jpl | jpl 2972 | 6 7 17 | 9 11 33 | 8 8 16 |
mit | mit 3072 | 27 13 30 | 11 17 54 | 7 6 13 |
Table 5.1832.6 GPS week: 1832 Day: 6 MJD: 57074.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3046 | 4 6 15 | 10 8 41 | 6 7 17 |
emr | emr 3068 | 5 5 15 | 11 11 44 | 7 8 15 |
esa | esa 3072 | 4 4 13 | 9 8 41 | 7 6 18 |
gfz | gfz 2972 | 4 5 19 | 8 8 37 | 6 5 16 |
grg | grg 2782 | 7 7 23 | 12 11 43 | 12 14 35 |
igr | igr 3056 | 4 3 12 | 9 7 39 | 6 6 16 |
igs | igs 3072 | 4 4 12 | 9 8 40 | 6 6 15 |
jpl | jpl 2880 | 5 6 17 | 9 11 42 | 8 9 18 |
mit | mit 3072 | 5 5 14 | 10 11 44 | 6 7 20 |
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 6.1832 GPS week: 1832 MJD: 57068.500-57074.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -31 -23 134 -47 -1 | 15 20
| 50 15 42 186 7 | 1
emr uuuuu | 6 18 91 14 3 | 48 51
| 23 29 79 99 14 | 3
esa uuuuu | -3 -6 28 28 2 | 16 19
| 20 16 59 61 2 | 2
gfz uuuuu | -12 -41 42 27 -1 | 11 15
| 23 21 64 117 4 | 1
grg uuuuu | 12 33 -152 -91 -6 | 44 45
| 20 21 143 86 6 | 2
igr xxxxx | 2 0 47 38 -1 | 2 11
| 14 16 28 68 4 | 1
irf xxxxx | 22 1 -14 -6 1 | -2 10
| 8 7 23 27 4 | 1
jpl uuuuu | -49 -10 96 18 0 | 31 36
| 57 19 106 54 5 | 3
mit uuuuu | 21 2 -68 -23 0 | 18 20
| 16 12 61 66 6 | 1
ngs uuuuu | 34 9 -32 84 1 | 9 14
| 40 38 97 62 6 | 1
sio uuuux | 11 32 -198 -93 -22 | 62 64
| 17 18 27 86 8 | 4
Table 7.1832.0 GPS week: 1832 Day: 0 MJD: 57068.500
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 | -55 -3 84 -232 0 | 15 20
emr uuuuu | -17 -17 176 -3 4 | 48 50
esa uuuuu | -29 -25 71 54 3 | 15 18
gfz uuuuu | -7 -47 66 101 2 | 12 16
grg uuuuu | 0 10 -147 -128 -6 | 46 48
igr xxxxx | -15 11 10 153 2 | 1 12
irf xxxxx | 23 -3 -31 39 -3 | -2 10
jpl uuuuu | 7 17 155 52 3 | 30 35
mit uuuuu | 42 -11 -143 80 -8 | 19 22
ngs uuuuu | 44 13 -55 89 0 | 9 17
sio uuuux | -3 61 -219 -130 -7 | 65 66
Table 7.1832.1 GPS week: 1832 Day: 1 MJD: 57069.500
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 | -103 -27 120 -257 -12 | 16 20
emr uuuuu | 17 -2 179 108 -23 | 48 50
esa uuuuu | -8 -20 -10 -8 0 | 16 19
gfz uuuuu | 18 -62 -13 189 3 | 12 16
grg uuuuu | 4 56 -239 -103 -2 | 46 47
igr xxxxx | -4 0 71 64 2 | 1 12
irf xxxxx | 9 3 -26 9 -1 | -2 10
jpl uuuuu | -35 -1 112 45 -3 | 29 34
mit uuuuu | 4 12 -45 -13 -3 | 19 21
ngs uuuuu | 70 44 -24 61 8 | 8 15
sio uuuux | 5 11 -173 -170 -15 | 66 67
Table 7.1832.2 GPS week: 1832 Day: 2 MJD: 57070.500
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 | -85 -10 129 -199 -9 | 15 20
emr uuuuu | 10 19 -15 112 -6 | 47 50
esa uuuuu | -30 -7 93 14 0 | 16 19
gfz uuuuu | -28 -71 157 -19 -1 | 12 16
grg uuuuu | 46 15 90 6 -18 | 46 47
igr xxxxx | -4 29 27 -64 4 | 2 12
irf xxxxx | 18 -5 -36 12 -3 | -2 10
jpl uuuuu | -7 -20 -73 1 8 | 30 34
mit uuuuu | 19 -18 -143 37 -6 | 19 21
ngs uuuuu | 53 53 16 13 10 | 9 15
sio uuuux | -2 28 -224 -34 -28 | 65 66
Table 7.1832.3 GPS week: 1832 Day: 3 MJD: 57071.500
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 -17 176 -49 -2 | 13 19
emr uuuuu | 38 2 59 55 -1 | 45 47
esa uuuuu | 3 2 -34 15 -1 | 15 18
gfz uuuuu | -28 -21 -5 -83 -1 | 10 14
grg uuuuu | 27 41 -165 -45 -4 | 43 45
igr xxxxx | 24 -4 67 -2 -6 | 1 10
irf xxxxx | 21 15 -23 -14 2 | -3 10
jpl uuuuu | -93 -30 249 -89 0 | 30 34
mit uuuuu | 6 5 -61 -17 -1 | 16 19
ngs uuuuu | 28 22 -142 185 2 | 7 13
sio uuuux | 43 9 -177 -23 -27 | 62 65
Table 7.1832.4 GPS week: 1832 Day: 4 MJD: 57072.500
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 | 21 -29 115 79 1 | 13 19
emr uuuuu | 27 46 29 -14 19 | 46 49
esa uuuuu | 18 -17 84 108 0 | 16 19
gfz uuuuu | -46 -42 84 -85 3 | 10 14
grg uuuuu | -11 12 -25 -260 -13 | 42 44
igr xxxxx | -6 -16 81 13 -7 | 2 11
irf xxxxx | 22 -1 9 -30 5 | -3 10
jpl uuuuu | -152 8 147 75 -4 | 31 36
mit uuuuu | 9 14 -12 -79 4 | 16 19
ngs uuuuu | 74 -25 -131 136 -5 | 8 13
sio uuuux | 10 42 -206 -112 -27 | 60 62
Table 7.1832.5 GPS week: 1832 Day: 5 MJD: 57073.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 -28 108 194 5 | 13 19
emr uuuuu | -6 66 159 18 10 | 50 53
esa uuuuu | 14 21 42 -73 5 | 17 20
gfz uuuuu | -7 -32 22 -64 -6 | 11 15
grg uuuuu | 21 62 -261 -57 -2 | 40 42
igr xxxxx | 0 0 52 76 0 | 1 11
irf xxxxx | 34 3 25 -33 5 | -2 10
jpl uuuuu | -54 -16 -1 6 4 | 32 37
mit uuuuu | 23 11 13 -56 6 | 17 19
ngs uuuuu | 12 -57 -35 14 -4 | 9 14
sio uuuux | 3 34 -163 28 -26 | 57 60
Table 7.1832.6 GPS week: 1832 Day: 6 MJD: 57074.500
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 -48 206 132 7 | 16 21
emr uuuuu | -23 9 50 -180 15 | 53 56
esa uuuuu | 13 4 -52 87 4 | 20 22
gfz uuuuu | 12 -14 -19 152 -4 | 13 16
grg uuuuu | 1 37 -321 -52 -1 | 42 44
igr xxxxx | 18 -18 18 24 -2 | 4 11
irf xxxxx | 30 -4 -19 -27 4 | 0 11
jpl uuuuu | -5 -30 79 33 -5 | 37 40
mit uuuuu | 43 2 -89 -111 7 | 19 22
ngs uuuuu | -43 14 144 92 -5 | 11 15
sio uuuux | 25 36 -227 -209 -21 | 56 59
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