[IGSREPORT-22520] Wk 1778 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Feb 21 07:47:43 PST 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1778 (Feb 02, 2014 - Feb 08, 2014)
Contacts: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs1778[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1778[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1778[0-6].cls IGS GPS clock combination summary report.
igs17787.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs17787.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 | NKLG
0 | EMR | 8 9 8 9
0 | ESA | MONP MONP
0 | GFZ | 8 NRIL TIDB ARTU NRIL TIDB
0 | GRG | 1 9 1 9 BRAZ IRKJ BRAZ IRKJ
0 | JPL | 2 8
0 | MIT | 2 5 6 8 9 14 2 9
1 | COD | 9 ALIC
1 | EMR | 8 24 8 9 24
1 | ESA | 9 NTUS BOGT NTUS
1 | GFZ | 8 8 ALRT ARTU BOGT TIDB ALRT ARTU TIDB
1 | GRG | 1 DUBO IRKJ DUBO IRKJ
1 | JPL | 8 9 IISC
1 | MIT | 2 8 9 10 24 26 32 2 7 8 9 10 24 25 26 32 ALIC BUCU
1 | MIT | MAC1 ALIC BUCU MAC1 SYDN
2 | COD | BOGT
2 | EMR | 8 9 8 9 WROC
2 | ESA | BOGT
2 | GFZ | 8 8 24 SYOG REUN SYOG
2 | GRG | 9 9 KELY NOVM KELY
2 | JPL | 8 9
2 | MIT | 1 2 8 9 24 1 2 8 9 24 BUCU MDVJ USNO WROC BUCU MDVJ
2 | MIT | USNO
3 | EMR | 8 9 8 9
3 | ESA | ARTU
3 | GFZ | 9 8 9 MCIL MCIL
3 | GRG | 9 9 ARTU NOVM NTUS NYA1 USNO NOVM NTUS NYA1 USNO
3 | JPL | 8
3 | MIT | 1 2 8 9 18 22 26 1 2 8 9 18 22 26 NTUS TOW2 NTUS
3 | MIT | TOW2
4 | COD | 1
4 | EMR | 8 9 1 8 9 29 MCM4 TSKB HERS MCM4 TSKB
4 | ESA | NOVM MCIL NOVM
4 | GFZ | 8 8 MAL2 MAL2
4 | GRG | 9 9 BUCU DUBO FAA1 GUUG KELY USNO DUBO FAA1 GUUG
4 | GRG | MCIL NOVM
4 | JPL | 8 9 17 29 CUSV
4 | MIT | 1 2 6 11 12 18 19 22 25 28 31 1 2 3 6 8 9 11 12 16
4 | MIT | 18 19 22 25 28 31
5 | COD | 1 1 NKLG
5 | EMR | 8 9 8 9 HERS
5 | ESA | FLIN FLIN
5 | GFZ | 8 9 8 9 BOGT KELY BOGT KELY
5 | GRG | 9 9 IRKJ KARR NOVM FLIN IRKJ NOVM
5 | JPL | 8 9 BOGT POL2
5 | MIT | 1 2 8 9 1 2 8 9 11 19 23 31 MDVJ
6 | EMR | 8 9 8 9 MCM4 YELL
6 | GFZ | 8 8 MCIL MCIL
6 | GRG | 9 9 IRKJ ISPA MCM4 NOVM HOB2 IRKJ NOVM
6 | JPL | 2 8 9 ARTU
6 | MIT | 1 2 8 9 10 11 17 18 22 25 31 32 1 2 17 18 32 MDVJ
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
0 | MIT | ~23:40 | ~ 0.10 ns
6 | MIT | ~00:00 | ~ -0.08 ns
6. 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.
7. 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
----+------------+----------
G21 | 2014_02_07 | 2014011
8. 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
----+--------+---------------
2 | NGS | 24
9. 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 G24 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
10. 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.
11. 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 | -1.0 -.5 -1.0 -36 -19 -31 .36
EMR | 0 | .0 1.3 25.6 33 25 2 .51
ESA | 0 | 2.0 4.9 -2.1 -14 -3 55 .10
GFZ | 0 | .5 -.7 -2.3 -20 -44 -22 .46
GRG | 0 | 5.2 -.8 -3.1 -44 -3 27 1.00
JPL | 0 | 3.6 3.3 27.7 -48 51 -34 .23
MIT | 0 | 5.5 -2.7 11.2 -15 12 -54 .39
NGS | 0 | -3.5 -1.1 20.0 -54 17 -22 .43
SIO | 0 | 4.8 -2.8 15.6 38 -188 -321 .45
COD | 1 | -1.3 .0 -2.2 -20 -18 -24 .73
EMR | 1 | 6.2 .6 20.4 29 27 -18 .59
ESA | 1 | 1.4 5.8 .0 -15 -3 45 .28
GFZ | 1 | .7 .2 -1.7 -6 -52 -11 .21
GRG | 1 | -2.8 -.7 .2 -1 7 -17 .63
JPL | 1 | 9.1 5.2 21.5 -58 -36 -54 .19
MIT | 1 | 5.1 1.6 12.9 -41 13 -28 .49
NGS | 1 | 4.9 -1.5 15.3 -48 -28 9 .55
SIO | 1 | 2.9 -5.7 16.5 25 -273 -248 .45
COD | 2 | -1.2 .5 -2.4 -21 -8 -36 .69
EMR | 2 | 3.9 -6.6 15.3 21 24 -21 .57
ESA | 2 | 9.0 5.4 -5.3 1 -10 72 .40
GFZ | 2 | .8 -.1 -1.4 -24 -63 -10 .04
GRG | 2 | 7.4 -3.7 -9.8 -17 -5 16 .71
JPL | 2 | 13.9 2.6 19.3 -57 -38 47 .56
MIT | 2 | 3.6 -1.8 10.8 -6 1 -30 .50
NGS | 2 | -3.2 1.2 2.3 -8 16 -18 .77
SIO | 2 | 5.8 -1.9 1.9 74 -241 -134 .26
COD | 3 | -.6 .0 -1.4 -18 -21 -32 .54
EMR | 3 | 6.9 -2.0 17.6 29 36 -22 .51
ESA | 3 | 7.2 6.2 3.7 -17 -40 72 .12
GFZ | 3 | .7 -.4 -1.0 -30 -55 -10 -.08
GRG | 3 | 5.2 -.2 -4.3 -11 -8 -6 .47
JPL | 3 | 18.3 .9 24.7 -36 6 -25 .30
MIT | 3 | .4 -.6 12.8 1 -25 -26 .30
NGS | 3 | 4.5 2.7 15.2 -34 -24 15 .57
SIO | 3 | 4.3 -1.5 -2.3 -20 -297 -30 .37
COD | 4 | -.6 -1.1 -1.7 -33 -30 -29 .46
EMR | 4 | 8.2 1.6 10.1 22 37 4 .21
ESA | 4 | 9.5 2.1 2.5 -16 -89 51 .33
GFZ | 4 | .2 .2 -2.0 -32 -44 -18 .11
GRG | 4 | 3.5 5.1 -3.1 -32 -7 21 .49
JPL | 4 | 3.2 -3.6 22.8 -49 -53 56 .58
MIT | 4 | 2.6 3.6 7.6 -22 -17 -23 .22
NGS | 4 | 3.2 -4.1 17.4 -69 -13 -1 .47
SIO | 4 | 2.5 .4 -3.0 120 -81 14 .20
COD | 5 | -.8 -1.1 -1.3 -41 -5 -8 .60
EMR | 5 | 5.7 2.8 14.4 32 37 -3 .29
ESA | 5 | 10.7 4.0 3.3 -10 -81 33 .20
GFZ | 5 | .3 .0 -2.4 -28 -34 -11 .42
GRG | 5 | 5.4 -3.3 -4.6 -31 -13 16 .47
JPL | 5 | 8.4 3.3 23.1 -24 -17 -35 .37
MIT | 5 | .2 .6 6.4 -1 -3 -3 .37
NGS | 5 | 3.0 -3.4 6.9 -34 -7 4 .75
SIO | 5 | 3.0 1.6 -2.3 170 19 21 .43
COD | 6 | -.2 .4 -.9 -10 -4 -19 .35
EMR | 6 | 7.8 .3 10.6 37 39 -7 .43
ESA | 6 | 4.7 5.2 -7.7 -17 -28 40 .23
GFZ | 6 | -.3 -.1 -2.3 -21 -29 -35 .69
GRG | 6 | 2.1 -9.2 -3.4 -5 -12 12 .69
JPL | 6 | 7.5 3.1 16.9 33 8 -4 .50
MIT | 6 | -.2 .3 3.6 -3 1 -11 .44
NGS | 6 | 1.3 2.3 -1.5 8 -5 7 .65
SIO | 6 | 2.5 -.3 7.7 23 -199 132 .54
12. 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.
13. 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 1.1778.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1778.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 2.1778.[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 3.1778.[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 5.1778.0-6). 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 1778 summary. (Feb 02, 2014 - Feb 08, 2014)
Table 1.1778.a GPS week: 1778 MJD: 56690.000-56696.000
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 250| 0 1 0 -5 38 -10 .13 11 11 | -987 51 20 127
| 1 1 2 26 5 10 .05 | 280 701
emr 79| 1 -1 6 -26 0 2 .02 18 17 | 3190 -294 19 145
| 1 1 3 11 12 4 .04 | 1144 897
esa 150| 0 1 1 5 -20 24 -.22 7 7 | -380 -370 12 132
| 0 0 1 11 31 14 .02 | 1249 1264
gfz 192| 0 0 -5 19 -1 -22 .15 10 10 | 87 -37 14 121
| 0 0 0 15 14 11 .02 | 494 610
grg 181| 5 0 -1 -2 -28 -6 .18 16 15 | -108 53 18 145
| 1 1 1 28 17 8 .03 | 280 466
igr n/a| 0 0 -1 -5 39 8 -.17 5 5 | -3042 -17 17 100
| 0 0 0 9 13 10 .02 | 846 1073
jpl 80| 0 -1 0 15 25 1 .05 16 15 | 3176 -310 20 136
| 2 0 1 28 16 23 .05 | 1173 884
mit 299| 0 -2 -3 19 1 -17 -.14 13 12 | -242 130 30 272
| 1 0 1 14 42 20 .01 | 323 455
ngs 230| -1 0 3 -53 1 7 .05 14 11 | -3260 8439 1742 3442
| 1 0 5 67 62 21 .06 | 6330 22427
sio 453| -1 -2 -7 38 -153 -99 -.51 22 21 | --- --- --- ---
| 2 1 3 61 120 148 .03 | --- ---
Table 1.1778.b GPS week : 1778 MJD: 56690.000-56696.000
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 13 5 5 5 5 5 |
2 | 5 5 5 4 4 5 5 |
3 | 4 4 4 4 4 5 4 |
4 | 5 4 4 4 4 5 4 |
5 | 4 4 5 4 4 4 5 |
6 | 4 4 4 4 4 4 4 |
7 | 4 4 5 4 5 4 4 |
8 | 6 6 6 6 7 6 5 |
9 | 7 8 8 8 8 7 7 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 5 5 5 3 4 |
12 | 5 5 5 5 5 5 5 |
13 | 4 5 5 5 5 4 5 |
14 | 5 5 5 5 5 5 5 |
15 | 5 5 5 5 5 5 5 |
16 | 5 5 6 5 5 5 5 |
17 | 5 5 5 6 5 5 6 |
18 | 4 5 5 5 4 4 5 |
19 | 4 4 5 5 5 5 5 |
20 | 5 5 5 5 5 4 5 |
21 | 4 4 4 5 4 21 5 |
22 | 4 4 5 5 5 4 4 |
23 | 4 5 5 5 5 4 4 |
24 | 5 6 15 5 5 5 4 |
25 | 4 4 4 4 4 4 4 |
26 | 4 4 5 5 5 4 4 |
27 | 4 5 5 4 4 5 5 |
28 | 4 5 5 5 5 5 5 |
29 | 6 5 5 5 5 5 5 |
30 | 0 0 0 0 0 0 0 |
31 | 5 4 4 4 6 6 5 |
32 | 5 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 2.1778.0 GPS week: 1778 Day: 0 MJD: 56690.000
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| -1 1 0 30 30 -8 .11 11 10 | -1284 549 21 114
emr 80| 0 0 13 -4 -4 4 -.04 18 17 | 4192 53 15 139
esa 150| 1 1 0 21 -4 32 -.22 6 6 | -816 48 10 129
gfz 190| 0 0 -5 29 -19 -32 .13 10 9 | -284 -53 18 128
grg 178| 6 0 -1 -8 -24 -1 .14 16 15 | -184 22 16 135
igr n/a| -1 0 -1 -10 39 12 -.16 6 6 | -2186 -29 21 114
jpl 80| -2 -2 0 7 21 -10 .10 14 13 | 4237 61 17 132
mit 299| 0 -2 -3 22 55 -29 -.13 13 13 | -443 362 32 250
ngs 226| 0 0 8 -161 -32 5 .14 14 11 | -1076 227 1490 3261
sio 457| 0 -3 -10 35 -146 -312 -.49 22 21 | --- --- --- ---
Table 2.1778.1 GPS week: 1778 Day: 1 MJD: 56691.000
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 251| 0 0 -1 27 44 -14 .07 10 10 | -975 -41 21 115
emr 80| 2 -1 7 -17 16 4 .00 17 17 | 4609 -431 15 123
esa 150| 0 1 0 -7 -5 13 -.21 7 6 | 638 -1142 9 120
gfz 195| 0 0 -4 19 -14 -15 .16 9 10 | -34 320 12 122
grg 184| 3 -1 -1 54 -5 -3 .19 15 15 | -214 291 16 141
igr n/a| -1 0 0 -8 24 17 -.20 4 4 | -1922 -591 15 86
jpl 80| 0 -1 1 13 8 42 .06 16 15 | 4657 -476 17 134
mit 300| 1 -1 -4 39 12 -19 -.13 13 13 | -297 440 32 281
ngs 230| -1 0 8 -132 -54 5 .12 14 11 | -17603 59277 1886 3532
sio 456| 2 -2 -12 33 -262 -261 -.49 22 21 | --- --- --- ---
Table 2.1778.2 GPS week: 1778 Day: 2 MJD: 56692.000
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 2 1 -36 40 -9 .18 10 10 | -1143 502 23 144
emr 76| -1 -3 7 -32 -8 6 .01 19 18 | 4020 -946 14 145
esa 150| 1 1 0 5 9 40 -.25 8 8 | -948 351 13 167
gfz 196| 0 0 -4 39 0 -13 .14 10 9 | 328 -183 12 124
grg 183| 4 0 0 -5 -15 -6 .14 15 15 | 317 -134 14 163
igr n/a| 0 0 0 -22 26 10 -.18 5 5 | -2647 -953 17 101
jpl 80| 6 -2 -1 -37 26 15 -.03 19 18 | 3974 -937 21 157
mit 300| -1 -2 -1 -5 -3 -29 -.12 12 12 | 52 215 25 286
ngs 235| -3 0 1 17 -69 -24 .06 14 11 | -1036 437 1509 3355
sio 460| 0 -3 -6 35 -222 -141 -.56 21 19 | --- --- --- ---
Table 2.1778.3 GPS week: 1778 Day: 3 MJD: 56693.000
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 254| -2 2 -4 -24 38 -29 .21 13 13 | -1140 443 21 131
emr 80| 2 -1 7 -29 8 -7 -.00 17 17 | 3310 -1398 16 166
esa 150| 0 1 0 -10 -28 33 -.18 7 6 | -1365 467 10 132
gfz 194| 0 0 -4 24 -14 -22 .18 11 10 | 155 -250 12 114
grg 184| 7 0 0 6 -34 -14 .19 19 18 | -34 -298 17 171
igr n/a| 0 0 -1 -1 36 -8 -.16 5 5 | -3594 -996 16 99
jpl 80| 0 -1 0 52 10 -23 .06 15 15 | 3278 -1429 17 136
mit 299| 0 -1 -2 29 -9 -13 -.13 11 10 | 102 -362 29 288
ngs 235| 0 0 3 -38 64 -1 .03 15 11 | -879 179 1535 3734
sio 462| 0 0 -6 -53 -274 -60 -.52 20 18 | --- --- --- ---
Table 2.1778.4 GPS week: 1778 Day: 4 MJD: 56694.000
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| 0 0 0 -19 48 -11 .12 10 9 | -408 -1462 23 117
emr 80| 1 -2 2 -35 4 2 -.00 20 19 | 2351 -798 46 140
esa 150| 0 2 3 13 -54 35 -.23 9 8 | 1394 -2496 21 113
gfz 192| 1 0 -5 24 11 -43 .15 9 9 | 1011 -1197 18 112
grg 183| 5 1 -3 -30 -61 8 .19 18 16 | 134 -629 34 144
igr n/a| -1 0 0 3 61 2 -.20 5 5 | -3758 -415 19 107
jpl 80| 0 -2 -3 34 49 8 .02 16 15 | 2300 -772 34 124
mit 299| 0 -1 -3 16 -66 -43 -.14 12 11 | 52 -615 35 271
ngs 226| 0 0 7 -33 74 47 .00 14 11 | -269 -1567 2090 3603
sio 448| -3 0 -6 101 -80 -20 -.52 21 21 | --- --- --- ---
Table 2.1778.5 GPS week: 1778 Day: 5 MJD: 56695.000
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 7 36 -4 .11 10 10 | -970 106 16 112
emr 80| 0 0 5 -34 -21 3 .07 17 17 | 1586 1319 17 150
esa 150| 1 2 2 9 -68 5 -.21 6 6 | 516 -1064 11 132
gfz 191| 0 0 -5 -7 14 -18 .15 11 11 | -35 496 13 119
grg 180| 3 0 -4 -30 -30 -14 .18 15 16 | -551 794 16 132
igr n/a| 0 0 -1 -3 35 2 -.14 5 4 | -4199 1879 17 89
jpl 80| -1 -1 0 26 48 2 .10 14 14 | 1544 1268 17 133
mit 299| -1 -2 -3 12 47 19 -.15 15 13 | -759 661 29 242
ngs 227| -2 0 0 -4 63 7 -.03 15 14 | -1028 235 1906 3486
sio 441| -5 -3 -4 127 70 -7 -.48 23 23 | --- --- --- ---
Table 2.1778.6 GPS week: 1778 Day: 6 MJD: 56696.000
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| -2 0 3 -21 34 5 .13 12 12 | -991 260 19 157
emr 80| 3 0 4 -34 9 0 .08 18 18 | 2264 141 15 154
esa 150| 0 1 2 8 10 8 -.22 7 7 | -2082 1243 10 133
gfz 192| 1 -2 -5 7 12 -14 .12 11 10 | -531 606 16 129
grg 180| 3 0 0 -7 -29 -12 .21 14 12 | -227 327 16 135
igr n/a| 0 0 -1 5 50 22 -.17 5 5 | -2988 984 16 109
jpl 80| 1 0 1 11 15 -21 .05 15 14 | 2248 109 18 140
mit 300| 0 -2 -4 24 -25 -6 -.16 13 12 | -406 213 31 291
ngs 233| -1 1 -5 -18 -32 15 .04 12 11 | -933 290 1784 3124
sio 452| -3 -3 -4 -7 -162 106 -.50 25 25 | --- --- --- ---
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 3.1778.0 GPS week: 1778 Day: 0 MJD: 56690.000
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 19 7 11 17 7 13 13 17 23 4 | 53 52 49 52 50 44 23 40 52 35 48
2 | 12 22 5 12 17 4 9 18 10 12 4 | 39 39 28 33 35 28 31 32 33 23 31
3 | 8 14 4 7 17 4 8 13 6 23 3 | 33 34 32 34 36 30 33 34 35 34 32
4 | 12 17 10 8 17 6 13 7 16 26 4 | 39 41 32 36 38 34 36 34 35 43 34
5 | 12 17 7 9 12 5 13 12 12 26 4 | 54 57 47 50 49 48 52 50 53 48 50
6 | 9 12 5 7 16 4 11 11 7 25 3 | 29 30 31 31 34 30 33 35 34 36 30
7E | 8 16 6 8 16 6 16 11 14 20 4 | 47 47 45 49 51 45 47 45 47 51 46
8E | 15 21 9 9 16 8 17 15 24 19 5 | 53 52 49 51 51 49 50 53 50 49 49
9E | 16 31 11 9 18 11 21 18 35 14 7 | 76 82 78 75 78 73 78 79 78 77 76
10 | 9 13 5 10 13 3 10 10 12 16 3 | 26 24 24 31 30 26 27 34 27 27 26
11E | 8 15 6 8 15 6 13 9 15 15 4 | 36 42 36 38 39 36 39 33 42 26 36
12 | 12 19 6 9 19 5 17 10 11 22 4 | 34 30 29 36 40 28 34 36 33 31 31
13 | 7 16 6 9 18 6 13 15 11 18 4 | 49 47 49 52 54 48 52 52 45 49 48
14 | 7 20 6 11 15 7 15 13 12 17 4 | 45 42 49 57 55 49 47 54 47 49 48
15 | 8 22 8 10 14 8 17 14 14 22 4 | 29 33 28 35 35 30 34 26 35 29 28
16 | 14 15 6 6 16 6 15 14 11 19 4 | 32 27 29 32 33 28 32 29 34 23 29
17 | 13 16 7 10 20 5 24 9 11 17 5 | 36 34 28 40 41 31 33 32 34 25 32
18 | 8 16 6 12 14 5 13 13 13 30 4 | 24 25 23 32 22 20 26 25 27 18 23
19 | 7 11 4 9 22 6 15 12 11 18 4 | 30 30 29 36 39 32 30 31 34 24 30
20 | 9 17 8 18 11 4 14 13 9 32 4 | 19 25 20 27 21 19 23 22 19 27 18
21 | 12 17 4 9 12 6 13 12 13 17 4 | 27 27 20 23 25 24 24 22 33 17 26
22 | 7 16 5 6 11 7 11 14 13 34 3 | 26 26 23 29 24 24 26 28 26 27 24
23 | 7 16 7 10 14 5 12 11 15 30 4 | 44 41 44 51 48 45 45 44 41 39 44
24E | 9 20 7 17 12 12 12 10 17 17 4 | 502 362 505 500 504 504 503 503 497 208 501
25 | 7 16 4 8 15 4 14 12 13 15 4 | 32 33 30 30 38 29 39 34 34 28 31
26 | 7 17 5 8 18 6 8 14 12 25 4 | 33 28 36 41 46 35 37 40 31 41 35
X27 | 10 14 5 7 --- 6 11 11 9 11 3 | 25 28 25 26 --- 24 31 29 28 22 25
28 | 10 18 7 9 16 6 15 11 12 13 4 | 28 34 32 34 40 29 34 33 32 29 31
29 | 15 21 6 13 19 6 21 15 15 18 5 | 33 30 26 39 38 25 29 32 29 23 29
X30 | 3 --- --- --- --- 60 --- --- --- --- 0 | 61 --- --- --- --- 43 --- --- --- --- 59
31E | 13 15 5 7 22 7 15 14 12 13 4 | 72 63 63 64 64 64 64 63 65 62 64
32 | 11 11 8 6 16 6 8 21 12 29 4 | 31 29 27 29 31 26 30 27 32 26 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 18 6 10 16 6 14 13 14 22 |T 53 48 50 54 56 50 52 52 52 40 51
WRMS | 10 17 6 9 15 6 13 13 11 21 |NE 34 33 31 36 37 31 33 34 34 30 33
MEDI | 9 16 6 9 16 6 13 13 12 19 |MD 33 34 31 36 39 30 34 34 34 29 31
Table 3.1778.1 GPS week: 1778 Day: 1 MJD: 56691.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 24 23 --- --- 35 14 --- 23 20 --- 12 | 57 55 --- --- 53 41 --- 41 44 --- 45
2 | 15 17 7 8 14 4 13 15 10 14 4 | 32 28 22 25 31 23 25 23 31 19 25
3 | 6 11 8 6 17 4 11 12 10 23 3 | 23 27 25 26 30 24 24 26 26 31 24
4 | 11 13 9 8 15 6 14 7 13 20 4 | 33 34 27 33 35 31 36 28 40 34 31
5 | 6 17 5 9 11 5 14 11 11 24 4 | 35 42 33 36 38 34 40 33 43 35 35
6 | 7 13 6 8 16 5 11 14 10 25 3 | 23 27 24 26 31 24 27 29 29 34 25
7E | 9 17 5 9 13 5 17 9 13 23 4 | 40 35 34 38 36 34 36 37 44 40 36
8E | 14 26 9 13 19 5 17 14 26 19 6 | 42 52 33 37 37 36 46 43 47 35 38
9E | 18 30 10 13 20 6 22 18 31 16 7 | 54 58 55 52 52 52 59 55 66 53 53
10 | 9 12 6 8 12 3 11 10 9 16 3 | 24 26 24 26 27 23 29 29 30 23 25
11E | 7 15 7 7 16 4 14 8 10 25 3 | 32 33 30 31 36 29 30 28 33 23 30
12 | 11 15 7 9 19 4 17 13 12 23 4 | 30 29 25 31 35 24 27 31 31 26 28
13 | 9 17 6 9 18 3 16 12 10 15 4 | 36 37 34 36 44 32 38 38 31 33 34
14 | 10 19 6 12 13 5 19 14 12 20 4 | 33 34 33 41 37 35 33 34 37 31 34
15 | 12 19 7 9 15 5 18 11 10 22 4 | 27 29 20 29 31 23 29 20 30 21 24
16 | 17 17 7 6 16 4 19 13 13 20 5 | 32 28 25 30 31 25 27 24 28 21 26
17 | 11 20 7 12 17 4 22 11 12 19 5 | 30 30 24 35 37 26 28 28 34 23 28
18 | 9 15 8 11 14 3 15 12 16 30 4 | 20 23 18 26 16 17 21 20 28 18 19
19 | 5 13 5 7 19 3 18 11 6 20 3 | 24 26 24 28 35 24 22 23 27 22 24
20 | 9 14 9 15 12 4 15 15 16 31 4 | 13 18 12 16 15 11 18 14 22 23 11
21 | 8 13 4 9 14 3 12 13 12 17 3 | 22 18 15 19 24 17 19 20 27 15 18
22 | 10 14 5 6 9 2 13 12 15 33 4 | 22 24 17 21 21 18 21 22 21 26 19
23 | 10 16 6 11 16 4 18 9 17 24 4 | 33 32 30 36 36 29 32 32 25 25 30
24E | 14 22 8 14 17 5 14 16 17 19 5 | 544 317 549 551 547 550 553 549 555 252 549
25 | 10 13 6 7 15 3 14 10 8 19 3 | 28 30 27 26 34 26 32 28 31 24 28
26 | 7 14 5 8 14 4 14 13 12 28 4 | 27 27 26 31 33 27 26 30 33 32 27
X27 | 8 16 9 8 --- 4 15 15 11 12 4 | 23 25 19 23 --- 18 29 24 23 19 21
28 | 10 20 7 8 15 4 16 13 12 12 4 | 27 33 25 30 35 25 31 29 29 25 27
29 | 10 25 7 10 18 3 22 14 11 18 5 | 24 26 20 31 31 21 27 29 28 21 23
X30 | 3 --- --- --- --- 97 --- --- --- --- 0 | 58 --- --- --- --- 111 --- --- --- --- 57
31E | 9 13 7 7 14 4 15 15 16 14 4 | 51 48 49 50 51 48 50 52 55 42 50
32 | 10 8 5 5 15 5 13 17 10 31 4 | 30 30 27 28 29 26 35 28 33 29 28
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 7 9 15 4 16 13 14 22 |T 47 41 44 48 50 46 48 46 50 35 46
WRMS | 10 17 6 10 15 4 15 13 11 21 |NE 29 29 23 28 31 28 27 27 30 25 27
MEDI | 10 16 7 8 15 4 15 13 12 20 |MD 30 30 25 30 35 26 29 29 31 25 28
Table 3.1778.2 GPS week: 1778 Day: 2 MJD: 56692.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 12 22 8 13 13 4 --- 11 14 17 5 | 40 47 42 45 38 37 --- 33 38 32 38
2 | 14 22 7 9 15 5 14 12 10 15 4 | 36 31 25 25 30 23 22 25 30 18 26
3 | 8 12 7 9 16 4 15 11 13 24 4 | 24 27 22 25 26 24 23 27 26 31 23
4 | 7 18 8 8 16 6 16 7 11 18 4 | 30 33 28 29 30 28 29 29 33 32 28
5 | 12 19 7 12 8 6 15 12 16 25 4 | 38 43 33 34 37 32 40 35 42 38 35
6 | 7 10 9 7 15 6 13 13 13 26 4 | 24 26 26 24 28 23 23 27 25 32 24
7E | 8 19 9 7 17 5 20 8 9 25 4 | 46 41 42 46 42 41 43 42 48 46 42
8E | 11 21 8 11 18 7 20 15 23 19 5 | 42 47 38 42 42 38 47 44 49 37 41
9E | 15 38 13 9 19 11 26 20 32 12 8 | 46 59 42 45 46 42 54 47 60 42 44
10 | 8 17 7 10 12 4 10 9 12 13 4 | 19 23 17 21 19 18 16 20 26 20 18
11E | 12 22 7 8 13 4 17 8 14 14 4 | 28 40 27 30 33 30 31 30 34 22 29
12 | 12 20 10 9 17 4 26 12 6 24 5 | 28 27 23 30 36 23 32 28 28 25 25
13 | 8 17 8 7 20 4 22 11 14 15 4 | 43 41 41 45 46 39 43 42 45 39 42
14 | 16 17 7 13 13 5 20 15 7 19 5 | 35 39 42 51 46 42 45 43 42 39 41
15 | 11 22 8 11 16 5 18 12 11 21 5 | 27 29 25 32 31 26 30 23 28 23 25
X16 | 14 17 7 --- 17 6 22 12 14 --- 5 | 32 28 25 --- 32 25 30 25 25 --- 26
17 | 11 20 9 9 18 4 24 10 13 20 5 | 29 29 27 34 37 27 29 29 36 19 29
18 | 11 18 11 13 11 3 17 12 15 28 5 | 21 22 20 30 21 18 25 18 23 17 20
19 | 9 14 5 7 19 5 20 10 13 16 4 | 30 28 25 28 34 27 24 29 29 23 26
20 | 10 16 9 17 10 4 17 13 12 30 5 | 17 22 16 22 19 14 22 18 18 25 15
21 | 11 15 7 7 13 6 16 12 12 15 4 | 28 23 20 20 23 18 25 20 20 15 21
22 | 10 17 9 9 9 4 18 14 12 32 4 | 22 22 20 26 23 20 26 20 25 25 20
23 | 8 16 6 10 12 4 21 11 15 23 4 | 38 36 37 44 39 36 35 37 39 32 37
X24E | 26 --- 32 33 35 17 55 17 178 --- 14 | 690 --- 701 689 697 692 697 696 682 --- 696
25 | 10 13 7 6 16 5 19 10 9 16 4 | 29 31 29 29 38 27 37 29 29 25 29
26 | 7 16 7 10 19 2 15 14 11 26 4 | 33 30 35 38 42 32 30 36 32 36 34
X27 | 12 15 9 7 --- 6 13 14 10 12 4 | 22 25 20 21 --- 18 23 23 23 19 20
28 | 7 21 8 10 16 5 16 10 13 13 4 | 26 32 27 30 36 26 30 28 27 25 27
29 | 7 21 5 10 15 6 23 11 11 18 4 | 29 26 22 32 33 21 28 28 24 18 25
X30 | 4 --- --- --- --- 116 --- --- --- --- 0 | 70 --- --- --- --- 71 --- --- --- --- 69
31E | 6 15 7 6 16 4 21 10 11 16 4 | 48 46 45 48 45 45 46 46 51 43 46
32 | 12 12 7 6 19 6 11 10 12 24 4 | 28 25 20 24 23 21 23 24 30 28 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 19 8 10 15 5 19 12 14 21 |T 53 32 50 54 55 50 53 51 53 28 51
WRMS | 10 18 8 9 15 5 18 12 11 19 |NE 30 29 26 31 32 27 29 27 29 26 28
MEDI | 10 17 8 9 16 5 18 12 12 19 |MD 29 29 27 30 34 27 30 29 30 25 27
Table 3.1778.3 GPS week: 1778 Day: 3 MJD: 56693.000
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 | 14 18 6 10 13 6 13 7 17 16 4 | 32 43 36 40 36 38 21 37 41 31 37
2 | 14 15 4 8 16 4 12 12 10 15 4 | 41 41 37 34 40 33 36 31 37 28 35
3 | 9 11 4 7 25 8 14 9 7 24 4 | 29 31 28 32 43 28 26 33 32 34 30
4 | 11 13 7 11 21 6 13 8 12 16 4 | 37 40 35 39 40 36 37 37 41 39 37
5 | 13 17 6 9 11 6 16 11 9 25 4 | 46 50 41 42 46 40 47 40 45 44 43
6 | 7 12 6 8 24 6 12 11 13 26 4 | 33 35 35 34 43 31 32 37 35 38 34
7E | 8 16 6 8 13 5 16 8 14 20 4 | 51 49 47 51 45 46 52 48 50 51 48
8E | 14 23 8 8 18 4 14 14 33 16 6 | 54 56 48 49 45 47 50 52 61 46 49
9E | 16 36 12 11 18 10 19 14 40 10 8 | 56 71 58 58 57 55 62 61 72 59 57
10 | 8 10 4 9 16 5 9 11 11 14 3 | 26 25 25 27 29 24 24 28 25 24 24
11E | 11 22 9 9 20 3 13 11 12 14 4 | 33 38 32 34 39 32 34 33 34 24 32
12 | 14 17 6 11 21 6 19 12 8 23 5 | 36 31 30 34 41 29 32 35 30 31 31
13 | 9 15 6 10 18 4 15 12 15 17 4 | 49 47 49 53 54 47 47 49 41 45 47
14 | 16 18 9 16 13 5 16 10 17 19 5 | 47 45 50 58 52 50 44 51 48 48 48
15 | 15 18 8 11 16 6 18 15 9 22 5 | 26 28 23 32 33 27 32 24 26 28 24
16 | 17 16 5 8 21 4 18 9 11 21 4 | 38 33 31 33 38 30 32 31 33 27 31
17 | 28 20 7 14 22 4 22 9 11 16 6 | 43 33 33 42 44 33 34 36 37 28 35
18 | 10 17 9 17 13 4 15 9 13 28 4 | 26 24 19 32 21 18 23 20 22 19 20
19 | 9 16 4 12 28 3 19 9 11 14 4 | 31 32 30 38 44 30 28 32 32 24 30
20 | 10 15 6 16 11 4 13 11 17 29 4 | 17 22 14 22 19 15 20 18 17 25 15
21 | 15 14 6 9 23 4 8 10 13 14 4 | 25 25 20 24 32 22 23 20 26 14 24
22 | 6 17 6 13 12 4 14 13 16 32 4 | 29 23 25 30 29 25 25 25 22 28 24
23 | 10 19 6 11 15 4 16 12 10 23 4 | 44 43 44 49 47 43 40 44 38 37 42
24E | 13 13 7 17 24 5 21 14 9 --- 5 | 304 503 305 300 311 303 305 306 307 --- 304
25 | 9 15 6 8 17 4 14 7 8 16 3 | 36 32 32 30 41 30 36 33 31 30 32
26 | 11 14 6 10 26 4 12 13 11 26 4 | 38 29 35 40 47 35 32 37 32 39 35
X27 | 10 14 5 7 --- 5 13 12 10 14 4 | 27 28 24 25 --- 23 29 28 27 23 25
28 | 12 22 6 11 17 5 12 10 15 12 4 | 32 38 35 35 41 32 33 33 34 31 33
29 | 11 20 6 14 21 5 19 12 8 17 5 | 29 30 28 39 39 27 28 33 33 23 30
X30 | 5 --- --- --- --- 119 --- --- --- --- 0 | 61 --- --- --- --- 82 --- --- --- --- 60
31E | 9 14 7 10 10 5 16 13 14 13 4 | 79 77 81 76 77 74 79 83 78 75 78
32 | 12 9 5 10 24 7 8 7 12 27 4 | 29 29 26 25 35 25 30 26 29 31 26
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 17 7 11 19 5 15 11 15 20 |T 46 52 43 47 50 44 44 45 45 34 44
WRMS | 13 17 6 10 18 5 15 10 11 18 |NE 34 32 31 35 38 32 31 32 32 30 32
MEDI | 11 16 6 10 18 5 14 11 12 17 |MD 36 33 33 35 41 32 32 33 34 31 33
Table 3.1778.4 GPS week: 1778 Day: 4 MJD: 56694.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 15 23 7 10 14 7 --- 12 13 20 5 | 44 47 41 40 35 37 --- 34 43 31 38
2 | 10 18 7 8 15 3 11 15 11 15 4 | 36 34 28 28 28 28 28 29 38 23 29
3 | 8 19 8 8 21 5 12 11 11 25 4 | 37 35 35 35 37 33 40 35 42 36 34
4 | 5 17 8 9 22 5 13 10 13 17 4 | 36 37 34 37 38 35 35 34 41 37 35
5 | 7 20 9 8 11 5 15 9 16 25 4 | 40 45 41 39 39 37 43 38 49 41 40
6 | 6 17 10 8 21 6 10 12 10 27 4 | 33 35 36 32 38 32 35 36 35 36 32
7E | 9 23 7 9 12 6 17 14 10 12 4 | 72 69 67 68 70 66 68 69 69 66 68
8E | 17 27 11 9 17 6 19 13 25 15 6 | 53 56 45 45 45 45 50 51 49 43 46
9E | 17 35 15 13 20 6 22 15 34 13 7 | 76 85 75 74 74 72 81 79 72 73 74
10 | 6 12 8 6 16 3 9 13 11 15 3 | 22 17 14 21 28 17 19 23 22 20 17
11E | 8 30 10 8 17 4 16 8 17 16 5 | 37 41 33 33 38 33 31 34 45 27 33
12 | 9 18 6 8 21 5 18 12 12 24 4 | 34 31 33 36 40 29 33 33 33 30 32
13 | 10 20 10 9 18 3 19 12 9 19 4 | 44 45 40 45 53 42 44 45 43 41 42
14 | 11 19 9 9 14 5 13 12 13 19 4 | 44 46 44 53 48 46 46 45 39 45 44
15 | 13 18 8 11 17 7 17 15 9 24 5 | 31 28 25 36 31 28 34 22 30 30 26
16 | 12 23 6 8 17 5 19 9 11 22 4 | 33 33 32 36 37 32 34 32 33 28 31
17 | 9 21 7 12 21 3 20 13 12 15 5 | 28 29 31 39 40 31 32 33 34 27 31
18 | 10 18 7 12 12 4 16 7 9 30 4 | 22 22 20 25 17 18 25 16 23 16 18
19 | 6 16 6 9 20 3 18 11 12 16 4 | 34 29 31 35 38 32 29 32 39 27 31
20 | 6 17 10 15 14 5 15 10 10 30 4 | 15 19 15 23 21 16 25 17 15 23 14
21 | 10 16 6 9 12 4 14 10 9 17 4 | 23 25 21 25 28 17 28 22 27 17 20
22 | 8 18 8 8 10 4 16 15 14 32 4 | 21 22 22 26 22 20 23 23 20 22 19
23 | 9 19 8 8 15 4 19 11 8 24 4 | 39 39 36 44 44 38 42 39 36 34 38
24E | 10 13 9 12 21 7 15 11 12 --- 4 | 265 192 270 272 267 267 272 272 271 --- 269
25 | 8 14 9 7 16 4 15 9 10 17 4 | 34 33 34 32 38 31 37 32 36 29 33
26 | 9 15 5 9 24 3 12 14 11 26 4 | 33 29 33 40 44 35 40 37 29 38 34
X27 | 7 20 10 7 --- 6 13 10 10 13 4 | 27 31 27 25 --- 25 33 29 28 23 25
28 | 8 23 7 6 17 5 14 14 16 11 4 | 26 34 28 32 36 27 31 29 31 26 28
29 | 9 20 5 11 20 6 18 11 8 16 4 | 35 29 31 36 38 30 32 33 37 22 31
X30 | 3 --- --- --- --- 100 --- --- --- --- 0 | 91 --- --- --- --- 52 --- --- --- --- 88
31E | 11 16 21 11 12 11 17 19 19 17 6 | 66 57 62 60 62 57 62 60 63 63 59
32 | 7 12 6 5 24 5 10 12 13 27 4 | 21 19 15 20 30 16 22 18 18 21 16
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 20 9 9 18 5 16 12 14 21 |T 45 41 41 44 46 41 45 42 44 33 42
WRMS | 9 19 8 9 16 5 15 11 11 21 |NE 33 31 29 33 35 30 33 30 32 28 31
MEDI | 9 18 8 9 17 5 15 12 11 17 |MD 34 34 33 36 38 32 34 33 36 29 32
Table 3.1778.5 GPS week: 1778 Day: 5 MJD: 56695.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 10 19 8 7 12 5 --- 11 16 25 4 | 35 37 34 35 30 33 --- 30 39 31 32
2 | 15 19 5 8 14 3 11 24 13 18 5 | 39 37 29 28 29 28 26 28 29 25 29
3 | 6 14 6 9 18 5 14 13 18 24 4 | 28 27 24 24 27 24 29 30 31 35 25
4 | 14 16 8 12 15 6 21 15 10 24 5 | 34 37 31 35 26 30 38 30 30 34 30
5 | 10 18 5 13 10 5 13 11 13 24 4 | 35 39 31 32 31 30 36 28 32 31 31
6 | 6 12 6 10 16 4 14 14 12 26 4 | 24 26 23 21 24 21 26 29 25 33 22
7E | 7 17 6 7 11 4 13 10 16 17 4 | 49 49 46 47 51 45 44 46 55 45 48
8E | 14 25 7 14 17 3 17 16 28 19 6 | 34 42 31 38 33 31 36 36 40 27 32
9E | 14 33 11 20 17 6 18 17 27 17 7 | 60 73 59 66 68 59 65 65 64 58 61
10 | 12 11 4 7 11 4 9 11 11 17 3 | 18 23 17 21 18 18 22 21 17 24 17
11E | 5 14 5 8 13 2 10 9 10 24 3 | 28 30 26 28 29 27 31 29 29 26 27
12 | 8 17 5 11 21 5 14 13 13 26 4 | 32 30 25 34 38 25 33 27 29 25 28
13 | 8 16 6 10 18 5 16 12 8 19 4 | 34 40 35 41 46 34 39 37 36 34 37
14 | 15 16 7 13 12 4 13 13 17 18 4 | 34 40 40 48 43 38 42 43 38 40 39
15 | 15 18 6 13 16 5 18 16 16 20 5 | 26 30 21 28 28 22 30 21 29 25 23
16 | 7 18 8 10 15 6 19 10 16 21 4 | 28 28 25 27 30 23 29 23 27 19 24
17 | 12 17 6 15 19 5 16 13 8 19 5 | 29 33 29 37 38 28 30 31 28 22 29
18 | 8 18 5 16 9 4 12 10 15 30 4 | 17 24 17 28 18 16 21 16 16 19 16
19 | 6 14 8 10 19 4 15 13 17 19 4 | 27 27 26 30 34 25 29 29 27 23 25
20 | 10 17 8 14 8 4 13 9 12 30 4 | 18 25 13 21 18 14 21 16 17 27 15
X21 | 14 --- --- --- --- 15 --- --- 28 --- 20 | 29 --- --- --- --- 32 --- --- 47 --- 29
22 | 5 16 6 10 8 3 12 15 19 34 4 | 19 25 20 26 22 19 25 24 24 30 20
23 | 9 17 7 11 11 4 17 11 11 24 4 | 31 36 32 38 36 32 34 33 30 28 32
24E | 11 12 7 12 18 6 12 14 15 --- 4 | 175 183 168 169 180 172 168 169 181 --- 172
25 | 9 13 5 10 15 3 14 12 11 16 4 | 29 28 27 28 33 26 37 26 27 23 28
26 | 10 10 4 11 16 5 10 13 17 27 4 | 24 27 26 30 32 26 26 28 22 31 25
X27 | 10 15 8 10 --- 6 12 11 14 13 4 | 24 26 21 19 --- 18 30 23 23 23 21
28 | 12 18 8 9 16 3 14 12 12 13 4 | 25 33 28 27 34 24 29 27 25 23 26
29 | 11 21 5 9 19 4 17 13 7 17 4 | 26 27 23 30 33 22 27 27 24 18 24
X30 | 3 --- --- --- --- 91 --- --- --- --- 0 | 78 --- --- --- --- 34 --- --- --- --- 78
31E | 9 16 8 10 11 5 15 35 18 28 6 | 72 70 64 68 69 69 66 80 71 76 68
32 | 8 14 5 7 14 5 9 15 9 29 3 | 20 23 17 20 23 17 24 22 17 26 18
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 10 17 6 11 15 5 14 15 15 23 |T 36 39 33 37 38 33 37 35 36 30 35
WRMS | 10 17 6 11 16 4 14 13 14 23 |NE 28 29 25 29 30 25 29 26 27 26 27
MEDI | 10 16 6 10 15 5 14 13 14 21 |MD 29 30 26 30 32 26 30 28 29 27 28
Table 3.1778.6 GPS week: 1778 Day: 6 MJD: 56696.000
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
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 8 21 10 13 13 7 --- 13 11 25 5 | 43 46 48 44 41 41 --- 44 45 35 44
2E | 16 17 8 9 22 6 13 16 13 19 5 | 42 36 30 31 34 29 29 27 33 33 31
3 | 9 11 6 9 15 5 10 13 12 27 4 | 34 33 35 34 41 33 30 38 30 34 34
4E | 10 17 7 9 14 5 14 11 10 18 4 | 44 49 46 47 46 45 48 46 49 47 46
5 | 16 18 6 10 10 5 13 16 13 28 4 | 56 59 52 49 51 50 54 50 57 55 52
6 | 8 12 6 11 14 5 12 11 12 29 4 | 34 34 38 35 41 34 31 37 30 37 34
7E | 9 22 7 9 13 3 15 7 11 23 4 | 73 66 68 71 69 68 67 70 70 66 69
8E | 12 22 8 10 12 5 14 11 21 21 5 | 65 66 60 60 60 59 63 63 62 56 61
9E | 11 35 10 15 14 9 17 18 26 16 6 | 86 99 85 86 87 83 93 92 85 86 87
10 | 13 10 4 10 11 4 7 9 12 20 3 | 16 20 17 25 21 18 17 24 26 26 19
11E | 9 15 6 8 14 3 15 12 13 22 4 | 40 42 38 38 40 38 38 40 42 30 38
12 | 11 19 7 12 17 4 19 9 11 29 4 | 37 31 33 39 41 31 35 35 31 36 33
13 | 10 17 7 9 14 4 16 12 11 16 4 | 51 55 52 58 61 54 56 55 51 51 53
14 | 16 18 7 13 13 5 16 12 11 19 5 | 51 49 57 67 61 57 51 57 58 54 56
15 | 12 20 7 10 16 5 18 14 8 24 4 | 28 29 23 32 33 26 30 25 25 30 25
16 | 16 19 6 11 16 4 18 11 12 26 5 | 35 35 34 36 41 33 36 33 33 31 33
17 | 19 21 7 13 18 3 20 11 9 20 5 | 41 38 39 46 45 37 35 41 37 30 38
18 | 10 19 6 15 10 6 15 11 11 30 4 | 23 28 20 34 22 22 25 22 25 21 22
19 | 10 14 7 9 15 4 16 12 13 22 4 | 38 34 36 39 43 36 32 36 34 31 35
20 | 10 17 7 12 9 6 17 13 9 29 4 | 17 20 17 21 19 17 21 23 21 24 16
X21 | 10 12 7 --- --- 4 11 11 13 --- 4 | 12 10 5 --- --- 6 9 4 6 --- 12
22 | 10 17 8 10 8 4 14 16 10 35 4 | 25 26 24 30 27 24 25 29 27 30 24
23 | 11 17 8 11 10 3 16 10 10 24 4 | 46 46 48 57 52 48 47 49 44 42 47
24E | 8 13 6 12 15 5 11 14 14 19 4 | 240 181 241 240 242 240 239 240 237 122 240
25 | 7 15 6 8 11 4 14 10 11 19 3 | 34 35 37 35 41 35 41 35 39 31 36
26 | 11 16 4 9 19 5 11 11 9 32 4 | 38 34 39 47 52 40 36 43 39 45 40
X27 | 10 16 8 9 --- 5 14 6 13 18 4 | 28 30 30 25 --- 26 32 27 25 25 27
28 | 10 20 8 9 15 4 15 13 14 13 4 | 35 38 35 37 40 32 36 35 33 34 34
29 | 9 21 6 12 15 5 21 12 10 19 4 | 35 35 33 42 43 32 32 36 35 25 34
X30 | 3 --- --- --- --- 97 --- --- --- --- 0 | 62 --- --- --- --- 30 --- --- --- --- 61
31E | 12 18 9 10 12 5 16 21 9 44 5 | 77 70 68 73 74 70 70 77 76 80 72
32 | 14 11 5 9 15 6 8 16 11 31 4 | 24 22 17 21 25 18 21 25 26 32 19
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 18 7 11 14 5 15 13 12 25 |T 47 45 45 49 51 44 45 47 46 42 46
WRMS | 12 18 7 10 12 5 14 12 11 25 |NE 35 34 33 38 40 32 33 34 33 34 34
MEDI | 10 17 7 10 14 5 15 12 11 22 |MD 38 35 37 39 41 34 35 37 35 34 35
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 4.1778 GPS week: 1778 MJD: 56690.0-56696.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3013 |U 5 4 16 |U 12 12 39 |U 8 7 17 |
emr | emr 2939 | 9 9 23 |U 13 13 37 | 9 8 21 |
esa | esa 2948 | 7 7 20 |U 12 12 38 | 9 7 21 |
gfz | gfz 2913 |U 8 7 22 |U 13 12 40 |U 7 7 19 |
grg | grg 2848 | 7 6 21 |U 13 13 42 |U 11 11 28 |
igr | igr 2954 | 6 6 20 | 12 11 38 | 7 6 18 |
igs | igs 2933 | 7 7 20 | 13 12 39 | 7 7 17 |
jpl | jpl 2885 | 10 10 25 |U 13 15 42 |U 11 10 30 |
mit | mit 2962 | 11 11 27 |U 14 15 44 |U 40 18 48 |
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 5.1778.0 GPS week: 1778 Day: 0 MJD: 56690.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3024 | ---- ---- ---- | 12 11 40 | 6 4 15 |
emr | emr 2968 | ---- ---- ---- | 12 13 32 | 7 6 17 |
esa | esa 2976 | ---- ---- ---- | 12 12 36 | 8 5 20 |
gfz | gfz 2967 | ---- ---- ---- | 14 12 35 | 7 6 21 |
grg | grg 2869 | ---- ---- ---- | 13 12 37 | 13 27 37 |
igr | igr 2969 | ---- ---- ---- | 13 11 35 | 7 5 21 |
igs | igs 2933 | ---- ---- ---- | 12 11 33 | 5 4 17 |
jpl | jpl 2968 | ---- ---- ---- | 15 16 39 | 10 9 23 |
mit | mit 2976 | ---- ---- ---- | 13 12 39 | 9 8 22 |
Table 5.1778.1 GPS week: 1778 Day: 1 MJD: 56691.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3020 | ---- ---- ---- | 10 7 30 | 9 8 19 |
emr | emr 2958 | ---- ---- ---- | 11 12 32 | 8 10 15 |
esa | esa 2880 | ---- ---- ---- | 9 10 30 | 10 8 28 |
gfz | gfz 2873 | ---- ---- ---- | 10 10 32 | 8 8 23 |
grg | grg 2864 | ---- ---- ---- | 11 11 31 | 9 9 20 |
igr | igr 2939 | ---- ---- ---- | 10 9 29 | 8 5 19 |
igs | igs 2907 | ---- ---- ---- | 11 9 35 | 7 7 17 |
jpl | jpl 2871 | ---- ---- ---- | 11 11 31 | 9 10 24 |
mit | mit 2976 | ---- ---- ---- | 11 15 30 | ---- ---- ---- |
Table 5.1778.2 GPS week: 1778 Day: 2 MJD: 56692.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3040 | 4 3 10 | 9 9 40 | 10 6 20 |
emr | emr 2872 | 9 7 16 | 9 6 37 | 11 10 21 |
esa | esa 2976 | 6 6 11 | 9 6 40 | 12 6 22 |
gfz | gfz 2872 | 5 7 12 | 11 6 41 | 9 8 25 |
grg | grg 2880 | 6 5 16 | 10 8 43 | 12 7 24 |
igr | igr 2971 | 4 5 10 | 9 7 39 | 8 6 18 |
igs | igs 2968 | 7 5 12 | 9 6 39 | 8 7 19 |
jpl | jpl 2872 | 11 10 23 | 10 10 48 | 10 10 27 |
mit | mit 2976 | 7 4 12 | 15 15 46 | 66 24 73 |
Table 5.1778.3 GPS week: 1778 Day: 3 MJD: 56693.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3028 | 4 6 17 | 15 16 40 | 8 6 14 |
emr | emr 2968 | 8 8 22 | 15 19 44 | 8 5 17 |
esa | esa 2976 | 6 7 19 | 13 15 47 | 9 6 16 |
gfz | gfz 2968 | 6 6 19 | 14 14 40 | 9 7 16 |
grg | grg 2880 | 6 6 19 | 13 16 63 | 7 5 16 |
igr | igr 2975 | 5 7 19 | 15 16 42 | 8 6 15 |
igs | igs 2928 | 6 7 19 | 15 17 44 | 7 6 15 |
jpl | jpl 2968 | 8 9 23 | 18 19 45 | 8 8 19 |
mit | mit 2976 | 13 18 49 | 15 17 54 | 11 8 18 |
Table 5.1778.4 GPS week: 1778 Day: 4 MJD: 56694.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3025 | 5 4 18 | 10 10 31 | 7 5 18 |
emr | emr 2967 | 11 9 22 | 10 10 29 | 9 7 28 |
esa | esa 2976 | 6 5 17 | 9 10 31 | 9 6 23 |
gfz | gfz 2967 | 8 6 19 | 9 10 37 | 5 5 17 |
grg | grg 2879 | 5 5 17 | 11 11 37 | 11 8 35 |
igr | igr 2974 | 6 5 16 | 10 9 34 | 6 6 21 |
igs | igs 2970 | 7 6 18 | 12 10 45 | 7 5 18 |
jpl | jpl 2871 | 10 8 24 | 12 14 37 | 14 11 41 |
mit | mit 2976 | 8 8 22 | 12 12 38 | 78 37 78 |
Table 5.1778.5 GPS week: 1778 Day: 5 MJD: 56695.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2922 | 6 5 19 | 13 12 34 | 10 10 20 |
emr | emr 2872 | 11 12 34 | 12 12 25 | 7 10 24 |
esa | esa 2880 | 8 9 32 | 12 12 30 | 6 9 19 |
gfz | gfz 2872 | 9 10 36 | 12 12 32 | 8 10 21 |
grg | grg 2784 | 10 9 34 | 13 12 38 | 13 12 35 |
igr | igr 2880 | 8 9 33 | 12 11 32 | 8 9 19 |
igs | igs 2861 | 8 9 32 | 12 10 30 | 7 10 20 |
jpl | jpl 2775 | 12 13 32 | 12 16 34 | 11 12 39 |
mit | mit 2880 | 20 19 30 | 13 15 30 | 44 22 59 |
Table 5.1778.6 GPS week: 1778 Day: 6 MJD: 56696.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3034 | 5 5 17 | 17 16 55 | 7 7 14 |
emr | emr 2968 | 7 8 21 | 20 18 62 | 13 8 26 |
esa | esa 2976 | 8 7 20 | 17 17 52 | 9 7 20 |
gfz | gfz 2872 | 10 7 23 | 18 18 61 | 6 7 14 |
grg | grg 2784 | 7 5 19 | 19 18 44 | 13 7 31 |
igr | igr 2976 | 7 6 19 | 17 16 52 | 7 6 15 |
igs | igs 2964 | 7 6 19 | 18 17 50 | 6 7 14 |
jpl | jpl 2871 | 10 7 22 | 17 21 60 | 12 9 35 |
mit | mit 2976 | 9 7 21 | 20 21 69 | 30 13 38 |
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 6.1778 GPS week: 1778 MJD: 56690.500-56696.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -34 12 -174 31 1 | 14 19
| 14 26 85 71 6 | 3
emr uuuuu | 5 12 170 63 -3 | 23 28
| 34 31 93 174 17 | 2
esa uuuuu | 1 12 24 -76 4 | 1 13
| 19 10 34 69 4 | 3
gfz uuuuu | 13 -28 42 -34 -2 | 10 16
| 21 14 85 79 4 | 2
grg uuuuu | 32 0 8 27 0 | 5 13
| 14 20 61 68 4 | 1
igr xxxxx | -10 -3 -15 2 -3 | 5 12
| 16 13 42 61 3 | 2
irf xxxxx | 18 1 10 38 4 | 3 13
| 8 10 35 34 3 | 3
jpl uuuux | -40 -47 86 -24 -18 | 30 35
| 35 23 39 65 21 | 5
mit uuuuu | 9 -20 -4 112 9 | 15 20
| 28 30 113 87 6 | 4
ngs uuuuu | 20 57 -75 10 -6 | 5 11
| 57 72 75 100 6 | 2
sio xxxxx | 146 -50 101 -34 16 | 48 51
| 118 66 111 77 5 | 7
Table 7.1778.0 GPS week: 1778 Day: 0 MJD: 56690.500
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 | -17 -21 -76 81 1 | 10 15
emr uuuuu | 58 15 68 311 -12 | 26 30
esa uuuuu | -8 -7 18 -135 5 | -4 11
gfz uuuuu | -20 -21 55 -195 -1 | 8 13
grg uuuuu | 13 3 -74 4 -1 | 2 10
igr xxxxx | -36 9 -88 -19 1 | 2 10
irf xxxxx | 15 -21 19 28 5 | -1 9
jpl uuuux | 7 -21 66 28 -1 | 32 34
mit uuuuu | -23 -76 60 85 7 | 9 12
ngs uuuuu | 39 182 -157 197 -4 | 3 8
sio xxxxx | 161 -62 185 38 16 | 38 39
Table 7.1778.1 GPS week: 1778 Day: 1 MJD: 56691.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -37 -17 -86 41 -5 | 11 17
emr uuuuu | -25 -44 309 176 -4 | 25 30
esa uuuuu | 4 16 -39 -92 7 | -1 14
gfz uuuuu | 12 -11 -81 -8 0 | 9 16
grg uuuuu | 19 -40 -41 5 -6 | 4 12
igr xxxxx | 7 -7 -18 59 1 | 3 12
irf xxxxx | 9 -2 7 13 1 | 0 12
jpl uuuux | -7 -62 62 69 -19 | 35 37
mit uuuuu | -28 21 68 -3 3 | 11 16
ngs uuuuu | 69 94 7 -35 1 | 4 10
sio xxxxx | 239 -6 182 -70 12 | 42 45
Table 7.1778.2 GPS week: 1778 Day: 2 MJD: 56692.500
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 | -48 40 -143 -16 6 | 11 16
emr uuuuu | 44 53 143 239 -12 | 24 28
esa uuuuu | -32 25 6 -186 -1 | 0 13
gfz uuuuu | 3 -50 -9 -51 -8 | 9 16
grg uuuuu | 56 18 -8 136 2 | 4 12
igr xxxxx | 1 18 -43 70 -7 | 4 12
irf xxxxx | 30 10 68 105 8 | 1 12
jpl uuuux | -86 -22 133 -20 -47 | 35 37
mit uuuuu | 27 -18 154 166 15 | 12 17
ngs uuuuu | 72 -52 -138 -13 -4 | 5 10
sio xxxxx | 239 -49 212 27 20 | 45 47
Table 7.1778.3 GPS week: 1778 Day: 3 MJD: 56693.500
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 40 -311 -49 12 | 14 20
emr uuuuu | -14 38 108 -48 -19 | 23 27
esa uuuuu | 6 14 30 -71 8 | 2 14
gfz uuuuu | 45 -27 -4 16 4 | 11 17
grg uuuuu | 30 -15 104 71 -7 | 6 15
igr xxxxx | -14 -9 31 53 -2 | 6 13
irf xxxxx | 25 3 32 58 7 | 4 15
jpl uuuux | -29 -75 102 -19 -32 | 32 35
mit uuuuu | 34 -26 41 124 14 | 16 22
ngs uuuuu | -66 37 -13 59 -9 | 7 12
sio xxxxx | 266 32 146 -49 18 | 51 54
Table 7.1778.4 GPS week: 1778 Day: 4 MJD: 56694.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -34 18 -184 -42 -1 | 16 21
emr uuuuu | -24 -5 269 -118 -10 | 21 27
esa uuuuu | 21 16 59 11 5 | 4 13
gfz uuuuu | 32 -43 190 43 -1 | 12 17
grg uuuuu | 41 10 0 49 2 | 5 15
igr xxxxx | -25 -9 -24 -46 -6 | 7 13
irf xxxxx | 10 6 -13 7 8 | 5 15
jpl uuuux | -40 -73 19 -28 -36 | 29 35
mit uuuuu | 5 -9 -109 15 15 | 17 23
ngs uuuuu | -13 76 -153 31 -8 | 7 13
sio xxxxx | 9 -104 -12 -178 21 | 53 56
Table 7.1778.5 GPS week: 1778 Day: 5 MJD: 56695.500
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 -2 -165 145 -2 | 17 21
emr uuuuu | 10 21 86 -81 29 | 20 27
esa uuuuu | 23 13 35 -8 6 | 4 12
gfz uuuuu | 8 -19 69 -45 0 | 11 17
grg uuuuu | 26 14 65 -82 2 | 5 15
igr xxxxx | -2 -3 24 -93 -2 | 6 14
irf xxxxx | 22 5 2 23 5 | 6 14
jpl uuuux | -84 -42 102 -138 9 | 24 34
mit uuuuu | 46 -29 -87 243 8 | 19 24
ngs uuuuu | -34 41 -74 -118 -18 | 6 13
sio xxxxx | -37 -160 71 34 12 | 55 57
Table 7.1778.6 GPS week: 1778 Day: 6 MJD: 56696.500
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 25 -256 60 -3 | 17 21
emr uuuuu | -11 3 205 -41 10 | 22 29
esa uuuuu | -7 7 60 -54 -1 | 5 13
gfz uuuuu | 9 -29 71 5 -5 | 11 16
grg uuuuu | 38 9 8 9 5 | 5 14
igr xxxxx | 0 -21 15 -8 -3 | 5 12
irf xxxxx | 12 5 -44 31 -1 | 6 15
jpl uuuux | -39 -38 115 -57 -3 | 24 34
mit uuuuu | 4 -6 -155 156 0 | 20 25
ngs uuuuu | 71 20 3 -50 0 | 4 12
sio xxxxx | 145 0 -80 -43 10 | 56 59
More information about the IGSREPORT
mailing list