[IGSREPORT-23488] Wk 1836 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Apr 3 14:50:19 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1836 (Mar 15, 2015 - Mar 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:
igs1836[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1836[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1836[0-6].cls IGS GPS clock combination summary report.
igs18367.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18367.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 | MDVJ MDVJ
0 | ESA | DAV1 KELY DAV1 KELY
0 | GFZ | HOB2 ALRT HOB2
0 | GRG | ALRT CHUR KOUC CHUR KOUC MONP
1 | COD | CAS1 NKLG CAS1 NKLG
1 | ESA | BJFS GLPS BJFS GLPS
1 | GFZ | DRAG SCH2 YELL
1 | GRG | CAS1 DARW DAV1 GLPS ISPA KOUR MONP NKLG XMIS CAS1
1 | GRG | DAV1 NKLG
1 | MIT | CAS1 DAV1
2 | COD | NRIL
2 | ESA | BJFS ONSA BJFS
2 | GFZ | MAC1 MAC1
2 | GRG | HYDE NRIL PDEL BRAZ HYDE NRIL PDEL
2 | JPL | BAKE DUBO SCOR WILL
2 | MIT | ARTU ARTU
3 | ESA | MAC1 MAC1 TIXI UNSA
3 | GFZ | NKLG
3 | GRG | 10 10 MAW1 NKLG SYOG WES2 MAW1 NKLG SYOG WES2
3 | JPL | MAC1
4 | COD | FAIR CHUR FAIR
4 | EMR | 10
4 | ESA | CHUR NTUS TIXI UNSA
4 | GFZ | NTUS KOUC
4 | GRG | 10 10 INVK MAC1 NOVM INVK MAC1
4 | JPL | FLIN MAC1
4 | MIT | DAV1 CHUR DAV1
5 | COD | NTUS CHUR
5 | EMR | 10 10
5 | ESA | CHUR TIXI
5 | GFZ | CHUR TLSE TLSE
5 | GRG | 10 10 CHUR DAV1 DRAG WES2 DAV1 DRAG WES2
5 | JPL | 10 YELL
5 | MIT | RBAY RBAY
6 | COD | 4
6 | EMR | 10 10
6 | ESA | TIXI
6 | GFZ | 13
6 | GRG | 10 13 10 13 BRST DAV1 HYDE BRST DARW DAV1 HYDE KELY
6 | GRG | MONP WUHN
6 | JPL | 10
6 | MIT | YIBL
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 table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G32 | 2015_03_20 | 2015018
7. 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
----+--------+---------------
0 | MIT | 26
8. 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 G03 | 4 | | 4 | | | | |
9. 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.
10. 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 | -1.8 -1.8 -3.3 -61 -2 -22 .67
EMR | 0 | 6.0 11.0 9.7 28 -15 12 .47
ESA | 0 | 1.4 -1.1 -.4 -24 -31 49 .49
GFZ | 0 | .2 -.7 -1.9 -14 -90 -10 .67
GRG | 0 | 12.3 3.7 3.9 30 0 -35 1.17
JPL | 0 | 9.8 -.7 10.6 8 20 35 1.07
MIT | 0 | 4.8 1.8 3.0 14 -9 -57 .75
NGS | 0 | 8.1 .1 13.4 -29 -68 28 .67
SIO | 0 | 7.2 -1.7 -13.9 2 -14 -15 .50
COD | 1 | -1.6 -1.1 -2.6 -40 16 -21 .70
EMR | 1 | 5.9 3.7 8.1 35 -16 33 .69
ESA | 1 | .9 -1.2 .6 7 -36 51 .82
GFZ | 1 | 1.2 -1.4 -1.9 -18 -95 -56 .77
GRG | 1 | 13.4 -6.0 11.1 18 -3 -28 1.30
JPL | 1 | 2.7 -6.0 8.2 -38 31 33 1.23
MIT | 1 | 6.7 -1.5 3.1 7 -2 -19 .80
NGS | 1 | 7.1 1.4 21.8 -61 -83 37 .86
SIO | 1 | 8.0 -6.1 -15.4 -13 -7 -44 .65
COD | 2 | -1.3 -1.4 -2.1 -48 -7 -4 .79
EMR | 2 | 3.7 3.0 15.1 27 -9 27 .51
ESA | 2 | .8 -.6 1.0 19 -36 62 .76
GFZ | 2 | -.1 -.8 -1.9 -15 -69 -36 .69
GRG | 2 | 16.4 -10.5 17.8 19 15 -8 .80
JPL | 2 | 10.5 -9.9 11.3 -10 55 -2 1.14
MIT | 2 | 4.2 -7.0 4.8 -15 4 -46 .81
NGS | 2 | 5.2 -8.2 18.2 -103 -62 -14 .79
SIO | 2 | 9.5 -9.5 -6.7 -24 4 -32 .81
COD | 3 | -1.4 -1.6 -1.8 -30 -9 3 .70
EMR | 3 | 5.3 -5.0 9.3 11 9 5 .63
ESA | 3 | .1 -.5 1.4 6 -37 58 .68
GFZ | 3 | .2 -.9 -1.9 -6 -69 -49 .63
GRG | 3 | 14.4 -8.2 5.6 6 -22 -14 1.13
JPL | 3 | 6.8 -7.3 9.8 -1 15 24 1.17
MIT | 3 | 5.8 -4.8 4.9 -1 -5 -60 .78
NGS | 3 | 7.7 -6.9 8.3 -64 -60 32 .68
SIO | 3 | 7.0 -7.6 -9.9 -36 -7 -39 .73
COD | 4 | -1.2 -1.2 -2.6 -35 -12 -4 .97
EMR | 4 | 4.5 -1.4 7.6 19 -4 11 .65
ESA | 4 | .2 -1.8 -.2 -29 -28 31 .76
GFZ | 4 | .3 -1.3 -1.7 -4 -69 -38 .71
GRG | 4 | 12.1 -7.9 8.1 8 1 -40 1.11
JPL | 4 | 3.4 -3.0 9.9 -59 43 31 1.45
MIT | 4 | -1.0 -5.8 2.4 -15 6 -30 .77
NGS | 4 | 2.3 -4.0 8.5 -44 -32 -17 .89
SIO | 4 | 5.5 -3.7 -11.5 -34 -12 -30 .77
COD | 5 | -.6 -1.3 -2.0 -29 -20 -24 .93
EMR | 5 | -6.2 -4.4 13.5 13 -3 5 .79
ESA | 5 | .4 -2.3 .6 3 -20 34 .84
GFZ | 5 | .2 -1.9 -2.2 -15 -92 -21 .85
GRG | 5 | 4.5 -9.5 16.8 -3 10 -13 1.28
JPL | 5 | -1.0 -7.3 11.7 25 -16 34 1.15
MIT | 5 | .5 -8.1 2.1 4 5 -56 .84
NGS | 5 | 4.0 -4.9 13.4 -45 -78 9 .95
SIO | 5 | -.4 -5.1 -9.1 -29 -17 -42 1.00
COD | 6 | -1.0 -1.0 -1.7 -25 -18 -11 .79
EMR | 6 | -4.5 -1.1 3.8 21 5 21 .53
ESA | 6 | .8 -2.1 .0 -23 -19 31 .67
GFZ | 6 | .1 -1.4 -1.3 -9 -80 -9 .56
GRG | 6 | .3 3.8 8.9 -1 13 8 .68
JPL | 6 | .4 -3.8 7.1 -8 5 13 .92
MIT | 6 | .8 -2.5 1.5 -5 4 -33 .72
NGS | 6 | .8 -1.1 9.9 -48 -33 -20 .65
SIO | 6 | -2.2 -3.7 -5.2 -38 4 -41 .47
11. 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.
12. 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 1.1836.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1836.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 2.1836.[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 3.1836.[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 5.1836.0-6). 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 1836 summary. (Mar 15, 2015 - Mar 21, 2015)
Table 1.1836.a GPS week: 1836 MJD: 57096.000-57102.000
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 249| 0 0 -1 -9 2 8 -.04 15 14 | -845 -232 18 108
| 0 0 1 22 21 18 .07 | 367 570
emr 80| 0 0 1 6 -17 38 .12 12 12 | 4020 140 13 147
| 1 1 1 16 14 8 .01 | 1228 1105
esa 150| 0 1 -1 -8 1 -2 -.41 12 12 | -637 563 10 154
| 0 0 0 23 12 18 .06 | 807 1228
gfz 203| 0 0 -4 16 -16 -14 .07 12 11 | -101 189 11 75
| 0 1 0 16 16 16 .04 | 398 775
grg 176| 2 0 11 -21 16 -20 .26 16 15 | -12 252 16 139
| 1 0 4 19 31 13 .04 | 199 370
igr n/a| 0 0 -3 -21 -4 4 -.05 5 5 | -1922 492 16 77
| 0 0 0 16 16 7 .04 | 1198 953
jpl 80| 0 0 3 13 4 28 .23 11 11 | 4068 148 17 110
| 0 1 1 15 28 22 .03 | 1235 1100
mit 350| 0 -1 -1 -3 4 -9 -.11 12 11 | -510 40 44 181
| 0 0 0 25 33 17 .03 | 381 506
ngs 234| 0 0 1 0 6 -18 -.01 10 9 | -902 -56 1391 3095
| 0 0 2 27 33 15 .02 | 320 452
sio 321| -1 1 -5 -7 -10 -10 -.11 13 12 | --- --- --- ---
| 0 0 1 16 22 25 .07 | --- ---
Table 1.1836.b GPS week : 1836 MJD: 57096.000-57102.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 3 4 4 4 |
2 | 5 5 5 4 5 5 5 |
3 | 5 5 5 5 4 4 5 |
4 | 4 4 3 4 4 4 4 |
5 | 4 5 4 4 4 4 4 |
6 | 4 4 3 3 3 4 4 |
7 | 4 4 4 4 4 4 5 |
8 | 5 4 6 5 5 5 6 |
9 | 3 4 3 3 3 4 4 |
10 | 4 4 4 6 8 9 8 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 5 5 6 6 5 |
13 | 4 5 5 4 4 5 5 |
14 | 5 4 5 5 5 5 5 |
15 | 5 5 5 4 5 5 5 |
16 | 5 5 5 5 4 5 5 |
17 | 5 4 5 4 5 5 5 |
18 | 5 5 5 5 4 5 4 |
19 | 6 6 5 6 5 6 6 |
20 | 4 4 4 4 4 4 3 |
21 | 5 5 5 5 5 4 5 |
22 | 5 4 4 3 4 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 4 4 4 4 4 |
25 | 5 5 4 4 5 4 4 |
26 | 8 0 --- --- --- --- --- |
27 | 4 4 4 4 3 3 4 |
28 | 4 5 4 4 4 4 4 |
29 | 6 6 6 5 6 6 6 |
30 | 3 4 4 4 4 3 4 |
31 | 5 5 4 4 4 5 5 |
32 | 4 4 4 4 4 0 5 |
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 2.1836.0 GPS week: 1836 Day: 0 MJD: 57096.000
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 -1 -29 -25 0 -.04 16 15 | -1189 227 19 109
emr 80| 0 1 0 2 -36 24 .13 12 12 | 4786 1115 15 171
esa 150| 0 0 -1 -30 -21 -29 -.33 11 11 | -448 895 9 140
gfz 203| 0 -2 -3 32 -48 -8 .13 12 11 | -296 760 11 83
grg 179| 2 0 11 -50 -38 -35 .24 17 16 | -316 707 17 137
igr n/a| 0 0 -3 0 -27 2 -.01 6 5 | -2709 1657 17 70
jpl 80| 0 0 2 -15 50 38 .27 10 10 | 4840 1104 18 113
mit 350| 0 -1 -1 3 17 -8 -.14 13 12 | -1311 793 47 199
ngs 235| 0 1 0 26 54 -17 -.05 10 10 | -922 -60 1804 3215
sio 323| -1 0 -5 13 -15 8 -.19 14 13 | --- --- --- ---
Table 2.1836.1 GPS week: 1836 Day: 1 MJD: 57097.000
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 253| 0 0 -1 -15 -27 16 .03 16 16 | -1465 775 21 114
emr 80| 1 0 0 5 1 43 .10 12 12 | 4887 -149 13 143
esa 150| 0 0 -2 -11 -5 -5 -.34 12 12 | -285 256 9 159
gfz 208| 0 0 -3 4 -16 -28 .11 12 11 | -523 1241 10 74
grg 178| 3 0 11 1 -11 -34 .24 16 15 | -163 532 18 172
igr n/a| -1 0 -3 -32 -15 5 -.01 5 5 | -1922 338 15 79
jpl 80| 0 0 0 8 14 40 .27 10 10 | 4958 -145 16 111
mit 350| 0 -1 -1 21 13 22 -.15 12 11 | -492 93 44 170
ngs 234| -1 1 5 -3 6 -26 -.03 10 9 | -1578 926 1507 3369
sio 327| -2 1 -7 -14 -18 -22 -.20 13 14 | --- --- --- ---
Table 2.1836.2 GPS week: 1836 Day: 2 MJD: 57098.000
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 253| 0 0 -5 -22 3 40 .02 13 13 | -474 -805 17 112
emr 80| -1 3 2 12 -23 34 .12 12 12 | 4543 -1725 15 160
esa 150| 1 0 -3 19 -5 3 -.38 11 11 | 80 -172 9 144
gfz 205| -1 -1 -5 7 -4 -12 .06 11 11 | 462 -997 10 70
grg 178| 2 0 18 -21 25 -25 .23 15 15 | 145 97 17 127
igr n/a| 0 0 -4 -22 -7 13 -.10 6 5 | -1830 -1001 16 82
jpl 80| 0 0 2 30 3 -16 .23 11 11 | 4572 -1698 18 106
mit 350| 0 -2 -1 -37 3 -13 -.12 12 10 | -241 -575 45 174
ngs 234| 0 0 3 14 11 -13 -.02 9 8 | -600 -375 1433 3174
sio 326| -2 0 -8 -26 -28 11 -.14 13 12 | --- --- --- ---
Table 2.1836.3 GPS week: 1836 Day: 3 MJD: 57099.000
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 252| 0 0 0 5 12 13 -.01 15 14 | -687 -486 19 109
emr 80| 0 0 1 17 -13 33 .11 12 12 | 2454 151 12 136
esa 150| -1 0 -1 24 7 25 -.40 12 12 | -178 -446 9 152
gfz 205| 0 -2 -3 29 -18 -25 .03 11 10 | -527 441 10 72
grg 176| 2 0 15 -28 44 -19 .21 17 16 | 72 -94 17 132
igr n/a| -1 0 -4 0 18 3 -.05 5 5 | -3180 470 16 78
jpl 80| 0 2 3 27 -14 16 .22 11 11 | 2512 155 18 114
mit 350| 0 -1 0 3 52 -24 -.11 12 11 | -500 457 45 191
ngs 238| 0 0 0 -47 -57 -5 -.01 9 7 | -912 -176 1258 2964
sio 326| -2 1 -5 -29 28 -22 -.06 13 12 | --- --- --- ---
Table 2.1836.4 GPS week: 1836 Day: 4 MJD: 57100.000
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 252| 0 0 -2 0 28 -2 -.09 15 12 | -842 -373 17 95
emr 80| 0 -1 1 2 -34 36 .14 12 12 | 2291 988 11 128
esa 150| 0 1 -2 -29 6 -14 -.47 12 12 | -64 -907 11 163
gfz 202| -1 0 -4 21 6 -28 .04 12 11 | -238 182 14 72
grg 180| 2 0 9 2 31 -17 .26 14 13 | -94 -321 14 127
igr n/a| 0 0 -3 -24 11 11 -.08 5 5 | -2906 1046 17 73
jpl 80| 0 0 4 13 19 44 .22 11 11 | 2298 1000 16 105
mit 350| 0 -1 -1 -13 -36 5 -.10 12 11 | -533 222 48 187
ngs 234| 0 1 -1 20 14 -45 .02 11 10 | -844 -371 1386 2933
sio 323| 0 2 -3 -4 -39 25 -.08 12 10 | --- --- --- ---
Table 2.1836.5 GPS week: 1836 Day: 5 MJD: 57101.000
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 242| 0 1 0 -31 3 -17 -.16 17 12 | -468 -789 18 113
emr 80| 0 -2 2 -23 -9 46 .10 13 12 | 3771 1313 13 148
esa 150| -1 2 0 -32 11 13 -.45 13 13 | -1967 2045 12 172
gfz 202| 0 0 -3 -9 -18 -12 .07 12 11 | 86 -638 13 87
grg 171| 1 -1 6 -18 46 -17 .29 16 16 | -8 369 16 149
igr n/a| -1 1 -3 -44 -12 1 -.00 6 5 | -1210 1345 16 93
jpl 80| 0 -1 5 24 -41 31 .18 12 12 | 3849 1332 17 109
mit 350| 0 -1 -1 31 23 -19 -.09 12 12 | -347 -548 43 179
ngs 231| 0 0 0 14 -7 1 .01 10 9 | -677 -276 1026 2666
sio 311| 0 2 -5 7 9 -22 -.05 13 12 | --- --- --- ---
Table 2.1836.6 GPS week: 1836 Day: 6 MJD: 57102.000
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 241| 0 0 0 29 19 10 -.01 16 13 | -795 -177 18 107
emr 80| -1 -1 0 27 -6 48 .11 12 12 | 5413 -708 14 144
esa 150| 0 1 -1 -3 15 -8 -.48 13 13 | -1601 2275 11 151
gfz 202| 0 0 -3 31 -15 18 .02 12 11 | 328 335 11 70
grg 176| 4 -1 5 -36 19 5 .32 17 16 | 279 478 15 131
igr n/a| 0 0 -3 -28 1 -9 -.08 5 5 | 299 -406 17 67
jpl 80| 0 0 3 8 2 45 .23 12 12 | 5450 -709 17 116
mit 350| 0 0 -1 -32 -40 -25 -.06 13 12 | -148 -157 41 173
ngs 232| 0 1 1 -26 21 -21 -.02 10 8 | -782 -60 1323 3344
sio 311| -2 1 -4 2 -10 -49 -.04 13 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 3.1836.0 GPS week: 1836 Day: 0 MJD: 57096.000
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 14 11 8 10 5 10 7 11 10 3 | 29 28 30 26 32 28 32 28 32 31 28
2 | 12 12 8 19 18 6 10 11 10 18 4 | 19 21 16 27 21 16 21 19 20 12 16
X3 | 17 12 9 15 --- 5 12 11 14 13 5 | 177 176 173 180 --- 174 174 178 178 180 176
4 | 16 10 12 9 15 6 9 11 10 15 4 | 31 27 27 31 35 28 30 29 35 34 29
5 | 8 12 10 10 20 5 15 12 9 10 4 | 38 42 39 41 40 37 39 38 36 38 37
6 | 11 10 11 11 11 3 7 7 9 11 3 | 40 39 40 35 36 37 40 33 34 39 36
7 | 10 10 12 11 15 4 10 9 8 12 3 | 29 32 23 32 34 26 29 27 28 22 26
X8 | 15 10 12 14 14 8 8 15 15 --- 5 | 29 24 23 27 4 24 23 25 25 --- 22
9 | 9 7 12 7 10 4 10 7 8 11 3 | 34 36 32 36 37 34 37 38 38 40 35
10 | 12 14 9 11 16 6 7 12 9 13 4 | 87 83 86 82 84 84 84 85 90 83 84
11 | 12 9 16 9 18 5 9 8 12 8 4 | 42 48 39 46 61 41 46 42 49 40 44
12 | 14 15 7 12 22 6 14 13 10 11 4 | 39 40 33 44 54 38 43 42 40 36 39
13 | 13 12 11 13 14 5 12 10 10 15 4 | 32 35 32 37 35 32 37 30 29 29 31
14 | 28 9 12 13 13 4 9 13 13 17 5 | 46 37 35 48 38 39 37 41 36 43 38
15 | 20 11 11 15 13 6 12 17 11 17 5 | 44 38 35 36 37 36 39 34 34 30 34
16 | 15 10 9 15 18 6 13 15 12 20 5 | 22 21 17 24 30 20 23 28 28 24 20
17 | 11 15 12 16 15 7 13 14 11 14 4 | 25 30 24 34 33 24 30 29 26 25 26
18 | 16 16 9 12 27 6 11 13 10 13 5 | 22 25 20 25 34 19 24 22 22 20 19
19 | 21 11 10 13 17 8 13 24 13 18 5 | 27 28 22 26 31 20 26 24 28 20 22
20E | 7 13 8 11 16 5 9 12 10 9 3 | 22 21 21 25 26 21 23 28 28 24 22
21 | 25 10 8 16 20 5 9 10 8 18 5 | 30 24 20 29 33 21 27 20 24 17 21
22 | 30 13 10 8 24 5 9 11 10 10 5 | 30 22 19 27 25 20 23 23 23 20 20
23 | 13 10 12 14 12 6 10 17 16 16 4 | 26 32 27 33 25 27 30 27 31 26 26
24 | 12 8 11 8 12 4 8 11 8 10 3 | 24 26 24 25 30 24 26 20 22 23 23
25E | 22 20 12 13 20 17 10 10 9 9 5 | 97 96 95 94 97 97 93 91 92 94 94
X26 | 18 13 12 --- --- 15 --- 6852 10 --- 7 | --- --- --- --- --- --- --- --- --- --- 0
27 | 11 6 12 10 12 5 7 9 8 10 3 | 27 33 24 30 40 26 29 26 29 24 27
28 | 11 13 7 11 20 6 8 12 8 11 4 | 31 31 25 30 39 27 30 26 27 25 27
29 | 17 10 12 14 17 7 13 22 13 21 5 | 31 32 25 33 35 25 30 31 28 34 27
30 | 12 9 11 7 9 3 10 9 7 10 3 | 27 33 30 29 35 28 32 27 28 27 28
31 | 14 9 13 14 18 3 14 17 12 16 5 | 26 31 22 31 36 25 33 24 26 21 24
32 | 16 7 8 11 12 6 8 10 11 11 3 | 30 24 23 23 25 25 24 25 28 25 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 12 11 12 17 6 10 13 10 14 |T 39 39 35 40 37 36 39 37 38 36 36
WRMS | 15 12 11 11 16 5 10 12 10 13 |NE 31 32 28 34 34 28 32 29 30 28 28
MEDI | 13 10 11 12 15 5 10 11 10 12 |MD 30 32 25 31 35 27 30 28 28 26 27
Table 3.1836.1 GPS week: 1836 Day: 1 MJD: 57097.000
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 10 11 10 10 5 8 6 7 12 3 | 32 33 32 29 33 29 35 27 30 31 30
2 | 15 12 9 19 14 4 10 11 11 16 4 | 24 23 16 27 21 18 23 18 22 12 17
X3 | 15 14 9 12 --- 6 11 12 13 11 4 | 122 126 124 128 --- 126 122 126 125 131 125
4 | 12 7 12 10 18 6 8 7 9 12 3 | 29 28 27 28 31 28 31 26 29 31 27
5 | 12 16 10 8 17 4 16 9 10 10 4 | 53 59 55 58 58 54 57 55 52 58 55
6 | 13 14 11 10 11 3 6 9 8 10 3 | 31 32 34 30 35 31 37 30 30 31 31
7 | 10 9 11 11 16 4 10 9 8 15 4 | 28 31 24 30 31 25 30 28 25 24 25
X8 | 10 7 13 11 --- 8 7 11 10 --- 4 | 27 26 26 27 --- 24 25 22 21 --- 23
9 | 11 8 12 9 13 5 6 12 5 13 3 | 34 37 32 36 36 32 36 34 31 36 33
10 | 19 12 9 10 16 6 9 12 7 10 4 | 64 58 56 55 53 58 55 56 57 59 56
11 | 15 9 17 12 19 6 8 7 11 12 4 | 31 37 33 35 48 31 38 31 35 32 33
12 | 22 17 9 12 20 4 13 14 11 12 5 | 34 35 25 34 43 30 35 30 29 28 30
13 | 18 13 12 11 12 6 11 12 12 16 4 | 36 30 25 24 30 23 33 19 21 22 24
14 | 14 9 13 13 14 4 9 10 11 16 4 | 40 42 40 51 40 42 43 40 42 41 41
15 | 18 13 13 13 13 4 11 15 12 18 5 | 40 34 34 36 33 32 36 34 31 27 31
16 | 15 12 12 12 20 7 12 16 8 16 4 | 30 30 25 30 33 26 27 29 26 25 25
17 | 12 12 11 15 12 7 12 9 11 13 4 | 22 29 22 27 27 21 30 21 25 19 22
18E | 19 16 11 13 30 6 12 12 11 10 5 | 25 26 20 27 26 21 25 23 21 22 21
19 | 22 11 12 13 18 8 11 23 10 15 5 | 29 28 24 27 23 22 28 22 22 17 22
20E | 21 12 6 12 17 4 8 14 8 11 4 | 27 22 19 23 26 21 20 25 21 20 19
21 | 17 13 11 16 18 4 10 9 11 15 4 | 30 26 22 28 33 23 30 23 23 18 23
22E | 18 11 10 9 20 6 10 10 9 9 4 | 22 21 16 23 22 18 20 20 20 19 18
23 | 16 10 12 15 13 4 10 20 11 18 5 | 26 29 23 27 23 21 29 24 19 17 21
24 | 15 8 15 7 11 4 10 10 10 8 3 | 27 30 32 33 36 31 30 28 30 31 30
25E | 16 16 14 6 16 4 10 9 13 13 4 | 38 38 40 39 37 38 38 37 35 38 36
X26 | 2 --- --- --- --- 245 --- --- --- --- 0 | --- --- --- --- --- --- --- --- --- --- 0
27 | 19 7 14 11 13 7 6 8 9 10 3 | 26 28 21 25 31 20 28 21 24 19 23
28 | 16 15 7 12 20 5 10 12 12 9 4 | 40 32 29 33 39 30 35 30 28 28 30
29 | 16 13 15 13 17 6 13 22 12 16 5 | 30 28 22 28 29 22 27 22 24 26 23
30 | 12 10 11 7 13 4 11 8 5 10 3 | 31 33 32 30 31 30 34 32 30 30 31
31 | 22 10 13 10 20 5 11 12 12 16 4 | 37 32 27 31 36 27 34 24 28 19 27
32 | 14 11 11 12 11 5 9 9 8 11 3 | 27 25 25 23 22 23 24 25 27 28 25
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 12 12 12 16 5 10 12 10 13 |T 35 35 31 34 33 31 35 31 31 31 31
WRMS | 16 12 12 11 15 5 10 11 9 14 |NE 30 31 26 30 31 26 32 26 26 25 26
MEDI | 15 12 11 12 16 5 10 11 10 12 |MD 30 30 26 30 33 27 31 27 28 27 27
Table 3.1836.2 GPS week: 1836 Day: 2 MJD: 57098.000
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 12 11 10 9 4 9 7 9 10 3 | 25 25 26 24 26 24 28 20 27 26 23
2 | 14 13 9 16 17 5 11 11 10 15 4 | 25 26 20 25 23 19 26 19 22 19 19
X3 | 16 17 12 12 --- 13 13 15 13 13 5 | 180 184 178 184 --- 178 182 180 184 183 181
4 | 11 9 11 9 12 4 9 6 7 11 3 | 25 25 23 27 31 25 26 22 29 26 24
5E | 17 12 13 9 15 8 14 11 8 9 4 | 104 99 96 107 100 97 98 105 100 98 99
6 | 9 10 11 10 12 4 8 6 7 12 3 | 38 36 39 37 35 37 38 36 36 44 36
7 | 9 11 10 13 16 5 11 13 10 16 4 | 30 28 23 30 28 24 31 22 31 21 24
X8 | 15 13 15 14 --- 6 11 11 14 --- 5 | 26 26 22 23 --- 20 24 21 26 --- 21
9 | 8 7 10 8 10 6 8 9 6 14 3 | 31 29 28 29 30 29 34 29 31 31 28
10 | 10 16 10 13 16 7 11 14 7 13 4 | 71 72 69 71 74 71 72 70 69 70 70
11 | 8 10 17 10 15 6 9 9 8 8 3 | 32 38 31 36 48 32 37 31 37 29 33
12 | 19 16 7 11 23 5 16 11 10 13 5 | 40 40 28 39 46 33 42 38 38 35 36
13 | 12 13 11 10 14 6 12 11 13 16 4 | 33 35 31 32 32 30 37 28 31 26 29
14 | 17 15 12 15 15 5 8 11 10 16 4 | 39 37 32 48 34 37 37 34 39 39 36
15 | 10 12 15 12 12 4 12 13 11 17 4 | 37 34 31 38 36 30 36 35 34 30 32
16 | 16 11 9 14 16 8 11 16 10 17 4 | 25 23 19 27 26 20 23 22 24 18 20
17 | 14 13 12 12 13 6 13 15 10 15 4 | 28 32 22 24 31 21 33 29 25 19 24
18E | 12 16 7 14 20 6 13 10 10 11 4 | 27 29 23 29 28 24 28 25 26 28 25
19 | 17 9 12 15 14 7 10 25 12 14 5 | 26 28 21 27 29 20 26 22 24 17 21
20E | 8 11 7 10 13 4 11 12 8 10 3 | 21 20 15 21 23 17 20 23 23 18 18
21 | 17 11 11 12 20 5 9 9 11 15 4 | 23 26 20 23 31 18 25 17 24 14 19
22E | 11 10 9 8 18 5 9 6 10 11 3 | 18 18 12 19 24 14 20 16 21 23 16
23 | 9 12 10 13 12 5 10 15 15 16 4 | 28 29 24 27 20 23 32 22 28 21 23
24 | 13 9 14 8 16 4 10 8 6 9 3 | 25 28 24 27 26 24 28 23 26 26 24
25E | 13 10 14 6 17 6 12 7 8 8 4 | 36 32 34 31 31 31 31 29 32 32 30
27 | 17 7 14 10 10 7 7 7 8 10 3 | 26 29 22 27 35 23 28 23 26 21 24
28 | 11 13 7 10 19 6 11 17 7 9 4 | 27 28 23 27 30 24 29 17 28 22 22
29 | 19 11 14 12 16 8 13 22 10 19 5 | 28 31 26 29 33 24 30 26 28 33 27
30 | 13 10 12 9 14 5 9 17 9 10 4 | 39 38 39 38 35 34 41 32 43 34 35
31 | 10 9 13 12 19 4 10 10 10 14 4 | 24 28 19 26 36 23 31 22 25 19 23
32 | 9 10 9 9 12 5 10 9 9 10 3 | 22 21 21 18 26 24 23 23 26 21 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 12 11 11 15 6 11 12 9 13 |T 37 37 33 37 34 33 38 34 37 34 34
WRMS | 13 12 11 11 15 5 11 10 8 12 |NE 30 31 27 31 31 26 32 26 30 26 27
MEDI | 12 11 11 11 15 5 11 11 10 13 |MD 28 29 24 27 31 24 31 23 28 26 24
Table 3.1836.3 GPS week: 1836 Day: 3 MJD: 57099.000
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 11 11 7 13 5 7 4 5 10 3 | 27 32 28 27 32 26 33 25 27 30 28
2 | 12 12 10 14 15 4 12 10 9 15 4 | 24 26 18 23 24 18 27 17 18 15 18
X3E | 13 16 13 10 --- 10 11 13 9 9 4 | 113 116 111 115 --- 113 115 115 113 117 113
4 | 11 9 11 7 17 4 9 8 6 11 3 | 30 31 27 29 38 27 31 27 30 30 29
5E | 9 12 7 8 17 5 17 11 10 9 4 | 44 46 40 43 47 43 49 41 42 43 43
6 | 11 10 11 9 13 5 7 7 6 10 3 | 35 36 36 32 35 34 39 33 32 38 34
7 | 16 10 13 12 15 4 12 9 8 13 4 | 28 30 23 30 30 26 29 27 26 24 25
X8 | 9 9 14 14 --- 8 7 9 11 --- 4 | 26 27 26 28 --- 27 29 23 27 --- 25
9 | 10 8 13 9 15 4 7 6 6 12 3 | 37 39 35 38 39 37 40 39 40 42 38
10E | 22 20 11 12 19 8 15 14 12 15 5 | 67 68 69 67 67 71 71 74 74 68 68
11 | 10 9 18 7 20 6 8 6 8 9 3 | 40 46 37 44 57 38 46 39 45 39 42
12 | 19 17 8 10 20 3 15 14 11 13 5 | 48 49 38 48 57 45 51 49 47 45 46
13 | 7 15 12 14 12 5 12 12 10 13 4 | 29 35 28 30 32 29 35 28 25 26 28
14 | 16 12 13 16 13 4 11 12 9 15 4 | 41 39 37 50 37 40 40 36 37 39 39
15 | 9 14 14 13 11 4 12 11 9 15 4 | 42 42 39 41 41 38 41 39 41 32 38
16 | 13 13 10 12 19 7 9 11 11 21 4 | 26 26 22 25 31 23 25 22 22 22 22
17 | 10 11 12 11 14 6 15 12 9 14 4 | 27 31 22 26 30 21 33 29 26 24 25
18E | 18 14 8 13 24 7 11 12 9 12 4 | 31 28 24 26 28 23 27 23 20 23 23
19 | 20 10 12 16 22 7 9 24 10 17 5 | 26 26 20 26 29 19 26 19 21 15 20
20E | 12 14 8 8 21 5 9 15 8 9 4 | 23 26 21 22 31 21 25 29 26 25 23
21 | 18 11 11 11 17 5 9 11 10 17 4 | 31 29 25 31 35 26 30 26 27 23 26
22E | 15 8 9 10 11 5 9 7 6 9 3 | 24 23 19 22 24 19 22 22 24 22 21
23 | 9 12 11 19 11 5 10 15 11 16 4 | 27 33 27 34 28 27 33 26 29 25 27
24 | 10 9 13 8 15 3 8 7 10 9 3 | 24 27 25 28 30 25 26 23 26 28 25
25E | 14 10 13 7 18 5 11 8 8 11 4 | 31 29 31 28 32 29 29 27 30 26 28
27 | 14 9 13 10 16 5 7 8 5 10 3 | 27 33 26 29 38 25 31 24 26 23 27
28 | 20 12 7 10 21 5 8 11 6 8 4 | 35 29 25 31 39 29 32 27 27 28 28
29 | 14 13 15 11 18 7 11 22 11 18 5 | 29 30 23 27 33 23 30 27 24 32 25
30 | 25 9 14 7 14 4 9 12 6 9 4 | 29 23 25 22 28 23 27 23 21 21 22
31 | 14 10 14 10 19 5 9 8 8 14 4 | 28 31 22 28 35 25 32 22 27 21 25
32 | 14 9 9 8 15 6 8 9 8 11 3 | 29 28 25 21 27 27 27 29 22 30 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 12 12 11 17 5 11 12 9 13 |T 34 35 31 34 35 32 36 32 32 32 32
WRMS | 14 12 12 10 16 5 11 11 7 12 |NE 31 32 27 31 33 27 33 28 28 27 28
MEDI | 13 11 12 10 16 5 9 11 9 12 |MD 29 31 26 29 32 27 31 27 27 26 27
Table 3.1836.4 GPS week: 1836 Day: 4 MJD: 57100.000
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 10 12 9 9 3 11 8 10 10 3 | 20 26 22 19 25 19 25 20 23 25 21
2 | 14 16 8 17 13 4 12 11 9 14 4 | 23 26 16 22 22 17 24 17 16 14 17
X3E | 13 14 14 10 --- 7 9 9 9 7 4 | 102 107 98 101 --- 100 104 105 102 104 102
4 | 12 9 14 7 12 4 9 8 12 10 3 | 30 29 25 29 29 25 28 22 29 29 26
5E | 10 13 9 10 12 5 15 10 8 8 3 | 26 27 17 22 25 20 25 23 21 23 22
6 | 9 10 13 8 8 4 8 10 8 6 3 | 30 36 32 30 34 31 34 30 30 30 31
7 | 10 11 13 10 13 3 11 8 8 14 4 | 22 26 18 23 27 18 24 20 18 13 18
X8 | 13 11 17 9 --- 8 9 6 13 --- 4 | 23 27 23 20 --- 20 23 20 25 --- 21
9 | 8 10 13 9 8 4 8 6 9 11 3 | 30 37 32 34 37 32 33 34 32 36 33
10E | 47 19 14 17 15 7 18 17 12 16 7 | 76 67 67 64 61 66 67 64 68 62 63
11 | 11 9 19 9 14 5 10 8 12 6 4 | 39 44 35 42 50 37 45 35 43 38 40
12E | 16 19 9 12 25 7 17 12 12 11 5 | 61 59 53 58 59 56 60 59 55 57 57
13 | 8 13 9 14 12 5 12 12 10 14 4 | 26 32 26 26 30 26 32 26 27 22 25
14 | 14 13 14 14 12 4 11 9 15 15 4 | 40 36 34 49 38 40 38 40 43 37 38
15 | 13 14 12 15 11 4 13 13 11 14 4 | 38 38 33 33 34 30 38 33 30 30 32
16 | 12 12 10 13 15 5 11 14 11 13 4 | 29 29 20 30 33 26 30 26 26 20 25
17 | 9 16 12 14 11 7 12 15 10 13 4 | 24 32 21 24 27 21 29 30 22 22 23
18E | 18 11 9 13 16 5 10 10 12 10 4 | 26 30 25 26 31 25 29 25 27 25 26
19 | 16 12 12 14 14 8 11 23 11 15 5 | 23 27 20 26 23 19 26 21 19 18 20
20E | 14 14 8 11 15 6 10 10 9 8 4 | 26 26 22 24 26 22 23 26 25 24 23
21 | 14 10 12 12 15 3 11 12 14 17 4 | 22 23 18 22 28 17 25 21 20 12 18
22E | 12 10 8 9 11 5 10 6 12 9 3 | 21 19 17 22 22 18 20 17 22 23 19
23 | 10 11 11 12 10 4 13 13 14 17 4 | 23 26 20 23 22 19 26 20 26 18 20
24 | 11 9 14 7 12 3 7 9 11 5 3 | 20 23 22 24 27 21 24 20 21 20 21
25E | 12 12 16 26 13 6 11 9 11 11 5 | 30 26 29 39 27 27 26 24 27 24 26
27 | 12 9 13 8 10 5 8 7 7 6 3 | 23 31 23 26 32 24 30 23 23 22 25
28 | 14 9 8 10 21 5 7 14 7 6 4 | 28 24 17 24 39 22 25 27 21 24 23
29 | 16 13 13 10 18 7 15 20 12 17 5 | 30 28 22 26 26 22 29 26 25 33 24
30 | 12 9 14 8 10 4 9 10 6 6 3 | 20 23 21 18 24 17 22 19 18 15 18
31 | 12 12 15 10 18 5 10 7 11 11 4 | 21 29 20 28 35 24 30 25 25 22 24
32 | 12 13 9 9 13 5 9 11 14 11 4 | 28 34 29 26 31 24 29 31 27 33 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 15 12 12 12 14 5 11 12 11 12 |T 31 33 28 31 31 28 33 29 30 29 29
WRMS | 12 12 12 11 13 5 11 11 10 10 |NE 27 30 24 28 29 24 29 26 26 23 25
MEDI | 12 12 12 10 13 5 11 10 11 11 |MD 26 29 22 26 29 24 29 25 25 24 24
Table 3.1836.5 GPS week: 1836 Day: 5 MJD: 57101.000
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
------+--------------------------------------------------------+---------------------------------------------------------
1M | 9 9 14 7 14 9 11 7 8 7 3 | 22 26 22 21 27 21 26 22 19 23 22
2 | 9 13 12 17 15 4 12 12 9 16 4 | 18 25 16 22 22 18 25 18 14 11 16
X3E | 13 14 14 9 --- 7 11 9 10 11 4 | 98 104 99 99 --- 100 99 101 96 102 99
4M | 15 8 12 7 22 7 9 9 8 11 4 | 27 25 24 24 31 26 29 23 23 28 25
5E | 8 13 7 14 19 4 15 11 9 11 4 | 25 30 25 30 25 26 29 24 24 25 25
6 | 8 10 14 11 11 5 7 10 7 10 3 | 29 36 32 28 32 29 34 31 30 28 30
7 | 11 11 13 10 15 5 10 14 8 14 4 | 25 28 23 26 30 24 26 24 22 20 23
X8M | 13 13 15 14 --- 8 6 8 12 --- 4 | 26 31 25 22 --- 26 26 21 23 --- 23
9 | 8 7 14 10 14 4 10 9 8 14 3 | 35 36 36 36 37 34 34 33 33 39 34
10E | 61 33 17 19 17 8 19 18 15 19 9 | 72 74 71 71 66 69 71 71 71 66 67
11 | 10 10 19 10 18 8 11 7 8 10 4 | 31 37 29 35 44 31 38 30 30 30 31
12E | 22 18 12 14 28 5 15 13 10 11 5 | 37 38 30 37 40 34 36 37 36 34 33
13 | 8 15 11 16 12 5 13 11 11 16 4 | 23 30 24 23 30 22 30 23 22 21 22
14 | 17 12 14 15 15 7 13 15 11 14 5 | 50 50 48 61 50 51 53 52 57 53 52
15M | 13 13 14 15 12 3 14 14 11 15 4 | 36 42 39 38 38 38 42 37 36 29 36
16 | 17 11 9 14 18 7 11 11 9 19 4 | 53 49 49 51 53 51 51 56 51 54 50
17 | 8 14 13 12 12 7 15 14 10 13 4 | 23 33 20 24 27 22 29 28 22 20 23
18E | 25 10 8 13 18 6 13 13 9 13 5 | 33 26 22 27 28 22 25 23 23 23 23
19 | 16 12 14 15 20 8 12 25 12 16 5 | 23 27 21 23 24 18 24 18 16 14 18
20E | 10 18 8 9 13 7 10 13 6 10 4 | 22 32 20 23 24 23 26 24 24 23 23
21 | 11 13 11 14 16 4 11 9 7 14 4 | 25 27 22 25 29 22 26 23 20 19 21
22E | 11 9 8 8 13 4 12 8 9 12 3 | 20 21 18 19 24 18 20 16 17 21 18
23 | 12 16 11 13 14 5 11 11 12 20 4 | 25 32 25 25 28 25 28 21 21 21 23
24M | 11 10 14 6 13 3 10 10 10 8 3 | 24 28 27 28 31 27 28 23 25 28 25
25E | 21 11 15 8 15 5 9 12 9 10 4 | 32 28 28 33 28 28 26 26 26 25 26
27M | 8 9 13 8 12 4 8 7 9 7 3 | 19 28 20 22 30 20 25 20 22 19 20
28 | 14 8 8 8 16 5 8 11 6 9 3 | 36 34 31 33 39 33 35 33 32 31 32
29 | 15 15 14 13 19 7 14 21 11 17 5 | 28 32 24 29 29 26 31 25 27 35 27
30 | 13 9 13 6 11 5 8 4 7 8 3 | 23 24 23 19 24 20 23 19 21 16 20
31M | 10 14 16 12 22 7 12 7 11 12 4 | 25 33 23 30 38 29 31 23 25 23 26
X32 | 3 --- --- --- --- 29 --- --- --- --- 0 | 28 --- --- --- --- 27 --- --- --- --- 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 17 13 13 12 16 6 12 12 10 13 |T 32 35 30 32 33 30 34 30 30 30 30
WRMS | 12 12 13 11 16 5 12 12 9 12 |NE 27 32 26 28 31 26 30 26 25 25 26
MEDI | 11 12 13 12 15 5 11 11 9 12 |MD 26 31 24 27 30 26 29 24 24 25 25
Table 3.1836.6 GPS week: 1836 Day: 6 MJD: 57102.000
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 11 13 8 11 4 11 7 6 10 3 | 24 25 22 20 27 21 25 21 21 26 21
2 | 10 14 11 16 14 5 13 17 10 14 4 | 19 26 18 27 28 18 27 25 20 14 19
X3E | 15 15 14 12 --- 7 11 7 12 9 4 | 108 110 104 107 --- 107 108 107 109 112 107
4 | 13 10 12 7 25 6 10 13 9 12 4 | 31 25 23 27 40 24 27 24 30 27 26
5E | 11 12 10 10 20 5 17 11 7 9 4 | 33 32 27 28 36 27 31 31 32 32 29
6 | 10 8 13 8 13 3 8 13 6 10 3 | 32 36 33 31 32 32 34 30 32 34 31
7 | 7 9 15 11 17 3 10 19 9 12 4 | 26 26 20 27 30 21 27 26 22 21 22
X8 | 12 17 16 13 --- 8 8 9 15 --- 5 | 23 25 20 25 --- 21 23 20 24 --- 20
9 | 10 11 14 10 14 5 8 10 7 13 3 | 29 31 30 30 34 29 32 33 30 37 30
10E | 50 13 15 17 18 6 16 15 12 16 7 | 102 93 96 93 96 94 94 93 100 93 94
11 | 11 9 19 9 18 4 9 8 10 7 4 | 46 46 43 47 58 42 49 41 47 41 44
12E | 19 18 8 13 26 4 14 9 13 9 5 | 39 35 29 37 39 32 36 33 37 33 33
13 | 12 14 10 17 14 6 14 10 13 17 4 | 31 35 31 35 38 30 35 30 34 26 30
14 | 16 12 17 14 18 5 12 11 14 14 5 | 43 38 34 51 44 42 38 40 42 41 40
15 | 10 12 13 14 13 5 15 10 12 15 4 | 46 46 43 47 50 43 48 44 45 43 44
16E | 17 11 9 13 17 5 12 12 10 21 4 | 43 42 37 45 49 39 44 44 39 42 41
17 | 9 14 14 15 11 6 15 13 9 13 4 | 26 30 21 33 33 24 33 33 28 24 27
18E | 14 12 7 14 21 5 14 12 6 11 4 | 39 35 31 36 36 31 35 27 31 30 31
19 | 18 11 12 15 19 8 11 24 11 18 5 | 29 28 22 28 28 21 29 22 21 17 22
20E | 9 11 8 10 11 3 10 10 6 9 3 | 25 21 17 23 25 19 22 26 21 22 20
21 | 15 13 11 14 18 6 12 13 9 14 4 | 28 27 23 28 33 22 27 23 26 22 23
22E | 12 11 8 9 16 4 11 8 10 7 3 | 19 19 16 21 21 16 20 16 19 19 17
23 | 15 10 13 17 16 7 11 12 10 17 4 | 24 26 21 30 25 22 26 20 21 20 20
24 | 11 10 15 7 20 4 13 13 7 8 4 | 25 25 22 26 27 20 22 23 23 26 21
25E | 14 10 17 8 16 6 11 9 7 10 4 | 40 39 43 43 41 41 40 39 39 38 39
27 | 10 7 14 10 15 4 8 7 8 10 3 | 33 37 31 36 43 32 35 34 32 30 33
28E | 13 9 8 11 17 7 7 8 9 8 3 | 37 36 33 37 38 32 37 31 33 31 33
29 | 14 15 14 13 16 7 16 21 13 15 5 | 30 31 22 30 33 25 31 30 30 33 27
30 | 12 9 14 10 12 3 9 7 7 6 3 | 24 24 23 23 26 20 26 17 22 21 20
31 | 13 13 15 12 19 5 14 8 12 12 4 | 26 30 19 28 35 24 32 23 25 20 24
32E | 12 12 12 15 14 8 14 16 12 15 4 | 22 12 6 8 5 22 13 6 7 9 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 16 12 13 12 17 5 12 13 10 13 |T 35 35 30 35 36 32 35 32 33 32 32
WRMS | 13 12 13 11 16 5 12 12 8 11 |NE 29 31 26 32 34 26 31 28 28 27 27
MEDI | 12 11 13 12 16 5 11 11 10 12 |MD 30 31 23 30 34 25 32 30 30 27 27
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 4.1836 GPS week: 1836 MJD: 57096.0-57102.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2979 |U 7 6 17 |U 7 11 27 |U 8 10 23 |
emr | emr 2973 | 6 8 20 |U 8 9 24 | 7 7 18 |
esa | esa 2976 | 6 6 19 |U 7 10 26 | 7 7 18 |
gfz | gfz 2960 |U 5 5 15 |U 8 9 28 |U 7 8 17 |
grg | grg 2783 | 7 6 16 |U 9 11 31 |U 9 10 21 |
igr | igr 2968 | 6 5 17 | 7 9 25 | 6 7 16 |
igs | igs 2966 | 5 5 16 | 7 9 25 | 6 8 16 |
jpl | jpl 2960 | 7 7 18 |U 7 10 27 |U 8 6 19 |
mit | mit 2976 | 6 5 17 |U 8 10 29 |U 6 9 17 |
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 5.1836.0 GPS week: 1836 Day: 0 MJD: 57096.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3036 | 6 7 16 | 6 13 27 | 9 12 30 |
emr | emr 3068 | 5 6 17 | 6 10 20 | 8 9 23 |
esa | esa 3072 | 6 6 13 | 5 11 22 | 8 10 22 |
gfz | gfz 2976 | 5 4 11 | 5 11 25 | 8 12 20 |
grg | grg 2880 | 6 6 11 | 8 11 29 | 10 14 21 |
igr | igr 3034 | 5 6 17 | 5 11 22 | 8 10 21 |
igs | igs 3049 | 5 5 13 | 5 10 23 | 7 11 21 |
jpl | jpl 2976 | 6 5 13 | 5 11 27 | 10 10 29 |
mit | mit 3072 | 7 7 24 | 6 11 28 | 7 12 20 |
Table 5.1836.1 GPS week: 1836 Day: 1 MJD: 57097.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3039 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
emr | emr 2976 | 5 7 20 | 8 8 28 | 5 4 12 |
esa | esa 2976 | 6 5 17 | 7 9 26 | 4 4 10 |
gfz | gfz 2976 | 5 4 14 | 7 8 26 | 5 5 12 |
grg | grg 2784 | 5 4 21 | 10 10 32 | 7 6 17 |
igr | igr 2976 | 5 4 15 | 7 8 25 | 5 4 11 |
igs | igs 2976 | 5 5 15 | 7 8 26 | 4 3 10 |
jpl | jpl 2976 | 7 8 15 | 7 9 28 | 7 3 14 |
mit | mit 2976 | 4 3 12 | 7 10 26 | 5 6 13 |
Table 5.1836.2 GPS week: 1836 Day: 2 MJD: 57098.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 6 18 | 8 12 37 | 8 9 21 |
emr | emr 2976 | 7 12 19 | 8 10 34 | 7 8 20 |
esa | esa 2976 | 5 7 18 | 7 11 34 | 7 8 19 |
gfz | gfz 2976 | 5 6 15 | 8 10 38 | 7 7 16 |
grg | grg 2784 | 7 6 17 | 9 11 40 | 11 10 22 |
igr | igr 2976 | 6 6 14 | 7 9 35 | 7 7 17 |
igs | igs 2976 | 6 8 15 | 7 10 35 | 7 8 16 |
jpl | jpl 2976 | 9 12 17 | 7 12 36 | 8 6 20 |
mit | mit 2976 | 7 5 16 | 8 10 42 | 7 9 17 |
Table 5.1836.3 GPS week: 1836 Day: 3 MJD: 57099.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 5 4 15 | 9 13 28 | 7 11 22 |
emr | emr 2976 | 4 8 19 | 9 9 22 | 7 6 17 |
esa | esa 2976 | 4 4 19 | 8 9 27 | 7 6 16 |
gfz | gfz 2972 | 4 4 16 | 8 9 25 | 7 9 18 |
grg | grg 2784 | 7 6 15 | 11 16 33 | 8 11 25 |
igr | igr 2976 | 4 5 15 | 7 9 23 | 7 8 18 |
igs | igs 2976 | 3 4 15 | 8 9 23 | 7 8 17 |
jpl | jpl 2976 | 5 6 17 | 8 11 27 | 9 8 17 |
mit | mit 2976 | 5 4 13 | 8 10 25 | 6 9 19 |
Table 5.1836.4 GPS week: 1836 Day: 4 MJD: 57100.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 7 6 18 | 9 10 27 | 6 9 21 |
emr | emr 2972 | 6 7 19 | 8 9 23 | 7 7 20 |
esa | esa 2976 | 6 7 20 | 8 11 29 | 7 6 21 |
gfz | gfz 2972 | 6 6 16 | 12 10 39 | 7 9 20 |
grg | grg 2783 | 7 7 16 | 10 11 31 | 9 8 19 |
igr | igr 2976 | 7 6 17 | 8 11 27 | 6 7 19 |
igs | igs 2976 | 6 6 17 | 8 11 27 | 6 8 19 |
jpl | jpl 2972 | 8 8 19 | 8 10 28 | 7 5 21 |
mit | mit 2976 | 7 5 15 | 10 11 35 | 6 8 18 |
Table 5.1836.5 GPS week: 1836 Day: 5 MJD: 57101.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2880 | 8 6 17 | 7 8 24 | 7 9 22 |
emr | emr 2876 | 7 5 20 | 9 7 23 | 8 8 22 |
esa | esa 2880 | 7 5 22 | 9 8 19 | 9 9 21 |
gfz | gfz 2876 | 6 4 17 | 8 10 24 | 7 9 16 |
grg | grg 2688 | 9 8 16 | 8 9 30 | 8 8 21 |
igr | igr 2864 | 6 4 16 | 8 10 20 | 7 7 16 |
igs | igs 2849 | 6 3 18 | 8 9 19 | 7 8 17 |
jpl | jpl 2875 | 9 6 20 | 9 6 21 | 9 8 20 |
mit | mit 2880 | 6 3 17 | 9 9 24 | 7 10 20 |
Table 5.1836.6 GPS week: 1836 Day: 6 MJD: 57102.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 8 5 20 | 6 12 24 | 9 9 23 |
emr | emr 2972 | 8 8 23 | 6 9 19 | 6 7 15 |
esa | esa 2976 | 8 6 24 | 6 9 23 | 6 7 14 |
gfz | gfz 2972 | 7 5 18 | 7 8 22 | 7 9 15 |
grg | grg 2784 | 8 5 18 | 7 12 24 | 8 10 21 |
igr | igr 2976 | 7 6 22 | 6 8 21 | 6 6 13 |
igs | igs 2966 | 7 5 20 | 6 9 19 | 6 7 14 |
jpl | jpl 2972 | 9 7 22 | 8 9 22 | 7 5 15 |
mit | mit 2976 | 7 5 20 | 7 9 24 | 6 8 14 |
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 6.1836 GPS week: 1836 MJD: 57096.500-57102.500
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 27 -40 76 -8 | 20 23
| 25 16 85 131 8 | 2
emr uuuuu | 12 -30 136 52 1 | 12 18
| 13 25 127 55 10 | 3
esa uuuuu | 1 12 63 79 -8 | 34 35
| 25 23 42 85 10 | 2
gfz uuuuu | -20 -53 175 -181 -2 | 19 22
| 21 19 98 79 6 | 1
grg uuuux | -11 27 -238 37 22 | 40 44
| 24 14 59 126 33 | 7
igr xxxxx | 7 24 30 62 0 | 3 10
| 22 16 40 58 5 | 1
irf xxxxx | 12 -10 -1 -25 -1 | 2 10
| 11 9 48 27 4 | 1
jpl uuuuu | 14 -7 111 -3 -1 | 37 39
| 30 15 60 89 10 | 1
mit uuuuu | 9 18 -80 -85 0 | 21 23
| 21 12 80 66 5 | 1
ngs uuuuu | -19 -5 -156 81 2 | 7 12
| 26 31 87 83 2 | 2
sio uuuux | 19 33 -55 -56 5 | 55 57
| 29 22 61 76 10 | 4
Table 7.1836.0 GPS week: 1836 Day: 0 MJD: 57096.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 4 52 -112 -110 -17 | 23 25
emr uuuuu | 21 -61 282 110 -7 | 17 19
esa uuuuu | 40 28 128 187 8 | 34 35
gfz uuuuu | 7 -81 99 -211 8 | 19 21
grg uuuux | 26 31 -200 87 -5 | 34 37
igr xxxxx | 23 7 80 29 9 | 3 8
irf xxxxx | 26 5 -70 -7 6 | 2 7
jpl uuuuu | -45 7 150 76 17 | 36 37
mit uuuuu | 18 17 -200 -63 9 | 22 23
ngs uuuuu | -61 1 -170 -29 -1 | 9 12
sio uuuux | 16 37 -159 -137 24 | 50 51
Table 7.1836.1 GPS week: 1836 Day: 1 MJD: 57097.500
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 | 44 38 -151 59 1 | 21 24
emr uuuuu | -14 -54 338 99 -12 | 15 18
esa uuuuu | 28 14 8 116 -3 | 35 36
gfz uuuuu | 4 -39 58 -69 3 | 20 21
grg uuuux | 13 22 -302 176 20 | 33 37
igr xxxxx | 26 49 18 53 -2 | 3 8
irf xxxxx | 6 -11 -53 -75 -1 | 2 7
jpl uuuuu | 4 -35 181 -34 2 | 37 38
mit uuuuu | -27 37 -137 -224 -3 | 22 23
ngs uuuuu | -14 5 -147 77 4 | 7 11
sio uuuux | -9 51 -51 -143 8 | 52 54
Table 7.1836.2 GPS week: 1836 Day: 2 MJD: 57098.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -25 26 3 -63 -4 | 18 22
emr uuuuu | 16 -27 108 64 -9 | 10 17
esa uuuuu | 2 -15 35 -25 -4 | 33 34
gfz uuuuu | -34 -34 139 -191 -1 | 18 20
grg uuuux | -12 33 -210 173 20 | 34 38
igr xxxxx | 11 28 27 18 -3 | 1 10
irf xxxxx | 29 -19 19 -2 0 | 0 10
jpl uuuuu | 26 -12 4 121 -4 | 35 37
mit uuuuu | 29 7 -46 -22 -2 | 19 21
ngs uuuuu | -29 -13 -13 19 4 | 4 9
sio uuuux | 31 66 -113 -42 4 | 52 54
Table 7.1836.3 GPS week: 1836 Day: 3 MJD: 57099.500
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 | -33 31 -78 105 -3 | 21 24
emr uuuuu | 10 -36 -6 17 7 | 11 18
esa uuuuu | -19 -26 38 126 -9 | 36 38
gfz uuuuu | -35 -62 196 -284 -5 | 21 23
grg uuuux | -23 15 -168 44 12 | 41 44
igr xxxxx | -37 1 57 -18 1 | 4 11
irf xxxxx | -2 -11 54 -9 -5 | 3 11
jpl uuuuu | 26 -1 72 -66 -3 | 38 40
mit uuuuu | 28 1 30 -49 -3 | 22 24
ngs uuuuu | -13 48 -137 102 1 | 8 13
sio uuuux | 47 32 -4 49 4 | 57 58
Table 7.1836.4 GPS week: 1836 Day: 4 MJD: 57100.500
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 | -8 17 -32 278 -5 | 19 23
emr uuuuu | 25 -9 47 17 14 | 11 17
esa uuuuu | -21 30 109 -44 -17 | 35 36
gfz uuuuu | -50 -72 340 -240 -11 | 21 22
grg uuuux | -12 13 -290 -10 0 | 44 47
igr xxxxx | -4 22 60 148 -6 | 4 11
irf xxxxx | 12 -17 53 -38 -7 | 3 11
jpl uuuuu | 10 9 158 -76 -10 | 38 40
mit uuuuu | 20 28 -9 -76 -5 | 22 24
ngs uuuuu | -33 -42 -290 236 2 | 8 13
sio uuuux | 62 28 -54 -47 -6 | 59 60
Table 7.1836.5 GPS week: 1836 Day: 5 MJD: 57101.500
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 26 108 157 -20 | 18 23
emr uuuuu | 18 11 66 -39 9 | 10 16
esa uuuuu | -22 30 69 67 -14 | 32 34
gfz uuuuu | -20 -43 262 -82 -4 | 19 22
grg uuuux | -46 22 -191 -26 93 | 41 44
igr xxxxx | 10 25 3 104 -3 | 2 11
irf xxxxx | 8 -1 -6 -39 3 | 1 12
jpl uuuuu | 54 -6 94 -107 -11 | 36 39
mit uuuuu | 6 19 -131 -99 4 | 20 23
ngs uuuuu | -3 -40 -222 106 3 | 6 12
sio uuuux | 0 15 -6 31 8 | 58 59
Table 7.1836.6 GPS week: 1836 Day: 6 MJD: 57102.500
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 | -10 0 -19 106 -5 | 17 22
emr uuuuu | 11 -37 118 96 6 | 12 18
esa uuuuu | -3 25 57 124 -20 | 31 34
gfz uuuuu | -11 -38 132 -187 -2 | 19 22
grg uuuux | -25 53 -307 -185 18 | 52 61
igr xxxxx | 18 32 -36 99 2 | 2 11
irf xxxxx | 8 -16 -3 -2 -3 | 2 12
jpl uuuuu | 21 -12 122 64 5 | 37 39
mit uuuuu | -12 18 -64 -59 0 | 21 24
ngs uuuuu | 22 8 -110 56 2 | 8 13
sio uuuux | -12 -1 0 -100 -3 | 60 61
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