[IGSREPORT-23939] Wk 1863 IGS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Oct 9 10:13:27 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
Final IGS Orbit Combination - Week 1863 (Sep 20, 2015 - Sep 26, 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:
igs1863[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs1863[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs1863[0-6].cls IGS GPS clock combination summary report.
igs18637.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs18637.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 | 10 NRMD
0 | ESA | 10 10 KELY TUVA
0 | GFZ | ARTU BAKE DGAR HOB2 HYDE IRKJ MAC1 MAL2 MCIL NICO
0 | GFZ | NRMD PIMO SCOR TONG WHIT WHIT
0 | GRG | 10 10 ALRT INVK MAL2 ALRT INVK MAL2
0 | JPL | 32 INVK
0 | MIT | WHIT WHIT
1 | COD | MATE
1 | ESA | 10 10 MATE
1 | GFZ | 32 DUBO SAVO
1 | GRG | 3 3 WIND TONG WIND
1 | JPL | 32 TUVA
2 | COD | 10 REUN
2 | EMR | 32 32
2 | ESA | 10 10 REUN TLSE
2 | GFZ | 13 13 ASPA BRUX CAS1 DAV1 DGAR DUBO IRKJ KOUR MAL2
2 | GFZ | MAW1 PIMO REUN SCOR STHL SYOG TLSE TONG MAL2 TLSE
2 | GFZ | TONG
2 | GRG | MAL2 TRO1 BRUX MAL2 TRO1
2 | JPL | 32
2 | MIT | RBAY RBAY
3 | COD | 32 32 NRMD WTZR
3 | ESA | 32 32
3 | GFZ | 14 GMSD MCIL PIMO TLSE TONG WTZR TLSE TONG
3 | GRG | FAIR
3 | JPL | TUVA
4 | COD | 20 32 20 32 REUN REUN
4 | ESA | 32
4 | GFZ | TLSE TONG
4 | JPL | TUVA
5 | COD | 32 32
5 | ESA | 10 10 32
5 | GFZ | TONG
5 | GRG | 10 10 MAL2 NRMD MAL2 NRMD
5 | JPL | GUAM TUVA
5 | MIT | GLPS GLPS
6 | COD | 32 32 HOB2 HOB2
6 | ESA | 10 32 10 32 GLPS MAW1 GLPS
6 | GFZ | TONG
6 | GRG | MAC1 MAC1 XMIS
6 | JPL | TUVA
6 | MIT | REUN REUN
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
----+--------+--------+-------------
1 | GFZ | ~20:00 | ~ -0.16 ns
4 | ESA | ~07:35 | ~ 0.09 ns
4 | GFZ | ~00:30 | ~ -0.15 ns
5 | ESA | ~13:05 | ~ 0.13 ns
5 | GFZ | ~23:35 | ~ -0.17 ns
6 | GFZ | ~00:00 | ~ 0.18 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 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 | GRG | 10
0 | SIO | 8
1 | SIO | 8
2 | SIO | 8
3 | SIO | 8
4 | SIO | 8
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 G30 | | | | 4 | 4 | 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 | -.2 -2.3 -1.1 -66 11 -4 .34
EMR | 0 | 3.0 -1.0 -.9 62 -22 -3 .20
ESA | 0 | -.3 -.6 .5 58 -40 61 .09
GFZ | 0 | .2 -.9 -1.5 -39 -95 -12 .39
GRG | 0 | .6 -2.4 -4.6 -13 30 -49 .22
JPL | 0 | 9.8 -.5 -.3 24 26 31 .64
MIT | 0 | -2.8 -4.5 -.3 20 -20 -11 .34
NGS | 0 | 1.4 -9.4 6.6 -60 -12 -21 .32
SIO | 0 | -.7 2.3 -12.2 -34 -12 8 .06
COD | 1 | .2 -2.0 -1.5 -78 -17 -11 .52
EMR | 1 | 2.1 .8 2.3 52 -22 -18 .26
ESA | 1 | -1.2 -.1 -.2 -7 -9 -16 .07
GFZ | 1 | .3 -1.7 -1.6 -37 -108 -27 .45
GRG | 1 | 4.5 -5.1 .1 -33 3 -44 .59
JPL | 1 | 5.0 -12.7 4.7 -9 36 21 .50
MIT | 1 | -3.4 -5.0 -3.6 8 -1 -37 .58
NGS | 1 | .9 -7.9 -3.2 31 -7 -16 .51
SIO | 1 | -4.0 -2.9 -13.9 -43 -17 -10 .31
COD | 2 | .5 -1.2 -1.4 -64 -21 -8 .50
EMR | 2 | -7.6 -3.3 5.5 51 -19 17 .55
ESA | 2 | -1.0 -.6 -1.1 -4 -23 15 .35
GFZ | 2 | .0 -1.3 -2.4 -60 -120 -31 .53
GRG | 2 | .0 .2 .7 -56 -1 -5 .61
JPL | 2 | -.4 -3.8 2.3 -14 14 74 .66
MIT | 2 | -5.9 -2.4 2.4 14 4 -32 .51
NGS | 2 | -2.3 -2.2 5.8 -41 -3 -23 .71
SIO | 2 | -4.6 2.6 -12.2 -40 -11 6 .31
COD | 3 | .4 -1.0 -1.0 -43 4 1 .70
EMR | 3 | -1.9 5.7 9.1 43 -20 30 .54
ESA | 3 | -1.3 -1.1 -.4 44 -60 46 .44
GFZ | 3 | .5 -1.9 -2.3 -60 -124 -16 .54
GRG | 3 | -.2 -2.5 4.1 -31 26 -14 .35
JPL | 3 | .3 -1.7 4.0 8 21 57 .85
MIT | 3 | -8.7 -1.2 1.0 14 1 -27 .78
NGS | 3 | -2.0 -3.8 5.8 -53 -15 -33 .64
SIO | 3 | -1.4 2.6 -3.7 -47 -17 7 .23
COD | 4 | -.3 -1.3 -1.3 -37 11 0 .64
EMR | 4 | 1.4 .7 9.9 41 -17 25 .63
ESA | 4 | -1.3 -.4 .4 60 -63 62 .43
GFZ | 4 | -.4 -1.1 -1.4 -34 -103 0 .50
GRG | 4 | -1.0 1.8 7.6 -69 20 -26 .47
JPL | 4 | 8.4 1.4 2.4 -46 65 23 .32
MIT | 4 | -3.0 .8 -1.3 16 -10 -35 .83
NGS | 4 | -.3 -4.5 11.2 -70 -34 -11 .68
SIO | 4 | 2.5 -.3 5.6 -23 -27 19 .27
COD | 5 | -.3 -1.8 -1.6 -51 -1 7 .53
EMR | 5 | -1.2 -7.7 7.1 38 -19 21 .70
ESA | 5 | -.9 -.7 -.5 38 -62 48 .19
GFZ | 5 | .2 -1.1 -1.9 -26 -92 -25 .40
GRG | 5 | 4.8 -2.7 7.0 -63 15 -10 .64
JPL | 5 | 3.0 -4.2 2.6 -11 25 -39 .54
MIT | 5 | -6.7 -3.8 2.1 4 -5 -29 .57
NGS | 5 | -1.6 -7.2 9.2 -69 -28 -41 .46
SIO | 5 | .2 -3.3 -1.0 -27 -28 2 .32
COD | 6 | -.7 -1.8 -1.8 -39 11 8 .60
EMR | 6 | -5.3 -1.1 6.7 45 -18 30 .55
ESA | 6 | -1.2 -.2 -.5 54 -69 60 .18
GFZ | 6 | .1 -.6 -2.0 -19 -96 -29 .50
GRG | 6 | -1.6 -3.6 8.7 -52 23 -5 .45
JPL | 6 | 3.5 -5.8 2.8 11 19 19 .66
MIT | 6 | -4.9 -.5 -.2 29 -15 -28 .63
NGS | 6 | .2 -.3 6.1 -19 -21 -17 .55
SIO | 6 | -2.3 -.6 -1.7 -7 -21 -5 .59
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 1.1863.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.1863.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 2.1863.[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 3.1863.[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 5.1863.0-6). 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 1863 summary. (Sep 20, 2015 - Sep 26, 2015)
Table 1.1863.a GPS week: 1863 MJD: 57285.000-57291.000
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 241| 1 2 -2 10 9 -5 .02 12 11 | -155 -942 12 117
| 0 0 0 14 17 16 .04 | 2091 2075
emr 80| 0 -2 4 6 -3 -5 .10 11 11 | 5980 -103 11 117
| 1 0 1 6 14 15 .03 | 571 815
esa 150| 1 0 0 -33 10 2 -.27 12 12 | -237 37 8 156
| 0 0 1 9 12 25 .03 | 630 1384
gfz 196| 0 0 -3 11 -20 1 .09 10 10 | 97 31 10 108
| 0 0 1 21 9 8 .04 | 346 654
grg 115| 0 0 1 -17 45 26 -.01 15 14 | 144 48 13 177
| 1 0 1 13 18 21 .02 | 196 409
igr n/a| 0 0 -1 -12 2 0 .00 4 4 | 2224 -300 13 64
| 0 0 0 11 10 15 .02 | 659 608
jpl 80| 1 0 3 22 14 15 .26 11 11 | 5977 -80 14 127
| 1 1 1 27 16 24 .03 | 572 810
mit 348| 0 -1 -1 -8 -8 -6 -.23 12 10 | 2132 -3 36 417
| 0 0 1 30 10 15 .02 | 682 905
ngs 216| 0 1 -1 2 -8 0 -.03 9 8 | -158 -955 1261 2739
| 0 0 1 23 17 8 .05 | 2086 2067
sio 304| 0 -1 0 -15 -20 -8 -.05 35 14 | --- --- --- ---
| 0 0 2 21 19 37 .09 | --- ---
Table 1.1863.b GPS week : 1863 MJD: 57285.000-57291.000
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 3 3 4 3 3 3 |
2 | 5 5 5 5 5 5 5 |
3 | 4 5 4 5 4 4 5 |
4 | 4 4 3 4 3 3 3 |
5 | 4 4 4 4 4 5 4 |
6 | 3 4 4 4 4 4 3 |
7 | 4 4 4 4 4 4 4 |
8 | 4 4 3 4 3 4 3 |
9 | 3 3 3 3 3 3 3 |
10 | 6 7 7 8 8 7 8 |
11 | 4 5 4 4 4 4 4 |
12 | 5 6 5 5 5 5 5 |
13 | 4 5 4 4 4 4 5 |
14 | 4 4 4 4 4 4 4 |
15 | 4 5 4 4 4 4 5 |
16 | 5 5 5 5 5 5 5 |
17 | 5 5 5 5 5 5 5 |
18 | 4 4 4 4 4 4 4 |
19 | 5 5 5 5 5 5 5 |
20 | 4 4 4 4 4 4 4 |
21 | 4 4 4 4 4 4 4 |
22 | 3 4 4 4 5 4 4 |
23 | 5 5 5 5 5 5 5 |
24 | 4 4 4 4 4 4 3 |
25 | 3 3 4 3 3 4 4 |
26 | 4 4 4 4 4 4 5 |
27 | 4 4 4 4 4 3 3 |
28 | 4 5 4 4 4 4 4 |
29 | 5 5 5 5 5 5 4 |
30 | 4 4 4 5 4 3 3 |
31 | 4 5 4 5 5 5 5 |
32 | 6 5 5 5 5 5 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 2.1863.0 GPS week: 1863 Day: 0 MJD: 57285.000
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 238| 1 2 -2 20 -18 -16 .08 12 10 | -1021 -309 13 116
emr 80| 0 -3 2 10 3 -23 .12 10 10 | 5287 843 12 112
esa 150| 0 0 0 -45 31 52 -.22 12 13 | -459 835 10 161
gfz 190| -1 0 0 0 -14 -1 .10 11 11 | -527 1172 12 100
grg 116| 1 0 0 -32 59 2 -.00 15 14 | 42 120 14 194
igr n/a| -1 0 -1 -16 -7 -6 -.01 4 4 | 2577 468 16 66
jpl 80| 0 3 1 55 -14 39 .31 10 10 | 5297 850 15 128
mit 348| 0 -2 0 -28 -9 -22 -.22 12 11 | 2457 284 36 444
ngs 217| 0 0 -2 4 2 -7 -.12 9 8 | -1081 -206 1306 2770
sio 306| -1 -2 4 -8 -12 20 -.17 49 14 | --- --- --- ---
Table 2.1863.1 GPS week: 1863 Day: 1 MJD: 57286.000
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 239| 0 3 -3 23 6 3 .04 12 11 | -872 -98 14 120
emr 80| 0 -2 3 8 5 -24 .07 10 10 | 6013 869 10 110
esa 150| 0 0 -1 -25 9 -28 -.23 12 12 | -1036 1809 9 158
gfz 193| 0 1 -4 2 -33 1 .11 11 11 | 395 -8 11 113
grg 115| 0 1 3 -4 46 53 -.03 15 15 | -47 601 14 186
igr n/a| 0 0 0 -8 4 4 .03 4 4 | 2916 347 13 66
jpl 80| 1 0 4 -4 4 32 .25 10 10 | 5994 899 14 128
mit 348| 0 -2 0 9 -21 13 -.21 12 11 | 2860 369 38 389
ngs 216| -1 0 -2 1 8 -8 -.05 9 8 | -885 -75 1408 2733
sio 302| 0 -1 2 3 -46 10 -.12 47 14 | --- --- --- ---
Table 2.1863.2 GPS week: 1863 Day: 2 MJD: 57287.000
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 3 -2 -5 -3 -34 .02 12 10 | -1451 855 12 120
emr 80| -1 -3 3 16 -10 0 .06 12 12 | 6512 -213 12 129
esa 150| 2 0 -3 -30 6 -12 -.25 12 12 | -59 -35 8 165
gfz 196| 0 0 -3 3 -28 -14 .15 10 9 | -84 229 12 107
grg 113| 2 0 1 -15 56 35 .02 14 13 | 103 238 13 182
igr n/a| 0 1 -1 -10 -9 -11 .02 4 4 | 2880 -706 14 67
jpl 80| 0 0 1 -14 12 25 .27 11 11 | 6533 -212 15 137
mit 347| 0 -1 -1 -6 6 -14 -.22 12 11 | 2625 733 35 426
ngs 219| 0 1 0 34 5 16 -.03 8 7 | -1395 735 1296 2722
sio 309| 1 0 3 -23 -39 -23 -.13 41 13 | --- --- --- ---
Table 2.1863.3 GPS week: 1863 Day: 3 MJD: 57288.000
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| 1 2 -2 16 8 -6 -.01 12 10 | 4552 -5510 12 107
emr 80| 0 -2 4 3 -14 10 .09 10 10 | 6452 -409 13 133
esa 150| 1 0 0 -46 20 -6 -.28 12 12 | -286 -306 8 141
gfz 197| 0 0 -4 17 -18 4 .10 11 11 | 417 -696 10 115
grg 114| 0 1 3 1 35 41 .02 15 14 | 216 -240 14 187
igr n/a| 0 0 -2 0 8 -14 .01 4 4 | 2193 -453 13 59
jpl 80| 0 0 3 25 13 20 .26 10 10 | 6462 -382 15 118
mit 348| 0 -1 0 -15 -9 -27 -.26 11 10 | 2179 -584 44 414
ngs 211| 0 1 -1 0 6 3 -.02 9 8 | 4539 -5521 1424 3027
sio 305| 0 -1 0 -33 -33 -23 -.08 41 16 | --- --- --- ---
Table 2.1863.4 GPS week: 1863 Day: 4 MJD: 57289.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 245| 1 1 -1 1 29 4 .02 11 10 | -647 -725 12 114
emr 80| 1 -2 4 0 -24 -17 .11 11 11 | 6450 -1312 12 108
esa 150| 1 0 0 -27 -3 -5 -.29 13 13 | -374 -578 8 151
gfz 198| 0 0 -3 -20 -24 14 .10 10 9 | 383 -687 10 116
grg 118| 0 0 0 -24 56 0 -.02 14 14 | 552 -694 13 173
igr n/a| 0 0 -1 -26 6 -13 .00 5 4 | 2184 -1133 13 64
jpl 80| 3 1 4 8 22 5 .25 12 12 | 6439 -1286 14 123
mit 348| -1 -1 -3 17 -4 -5 -.23 11 10 | 2203 -1217 33 413
ngs 217| -1 0 0 23 -16 1 -.00 9 8 | -610 -781 966 2777
sio 306| 0 -1 2 -11 0 17 .02 40 15 | --- --- --- ---
Table 2.1863.5 GPS week: 1863 Day: 5 MJD: 57290.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 245| 0 1 -1 25 8 -3 -.00 13 11 | -777 -444 13 123
emr 80| 0 -3 5 9 2 4 .13 10 10 | 6037 -771 12 114
esa 150| 1 0 0 -25 -3 7 -.31 12 13 | 1023 -2471 8 172
gfz 200| 0 0 -2 43 -14 2 .04 10 9 | -52 402 9 99
grg 116| 1 0 0 -12 53 10 -.01 15 15 | 56 192 13 170
igr n/a| 0 1 -1 1 -7 27 -.01 4 4 | 1762 -722 14 63
jpl 80| 1 1 4 44 25 -33 .25 11 11 | 6004 -727 14 136
mit 348| 0 -2 -2 -63 1 1 -.21 11 9 | 1821 -870 33 450
ngs 216| 0 2 0 -3 -31 -7 -.01 8 8 | -777 -469 1129 2605
sio 301| 0 0 -2 -50 -4 20 .03 14 14 | --- --- --- ---
Table 2.1863.6 GPS week: 1863 Day: 6 MJD: 57291.000
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| 1 2 0 -9 32 14 -.03 13 11 | -874 -366 14 122
emr 80| -1 -2 5 -1 17 9 .15 11 11 | 5113 268 12 116
esa 150| 0 0 0 -32 9 7 -.30 12 13 | -471 1006 10 149
gfz 198| -1 0 -3 32 -5 5 .05 10 9 | 151 -189 9 112
grg 119| 0 0 4 -34 7 40 -.03 15 14 | 90 123 14 150
igr n/a| 0 0 -1 -25 20 7 -.03 4 4 | 1058 93 13 68
jpl 80| 1 -1 4 43 37 21 .19 11 11 | 5114 294 14 119
mit 349| 0 -1 -3 26 -19 7 -.24 12 10 | 785 1261 39 387
ngs 216| 0 1 -2 -39 -31 -1 .02 8 7 | -899 -370 1301 2541
sio 301| 0 0 -2 12 -5 -82 .05 12 11 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1863.0 GPS week: 1863 Day: 0 MJD: 57285.000
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 | 8 9 13 8 8 5 6 10 7 19 3 | 27 29 27 25 26 26 32 25 24 36 26
2 | 9 14 13 18 19 4 12 11 8 20 4 | 29 28 24 40 31 29 30 26 28 23 27
3E | 19 8 13 6 13 4 8 10 8 14 4 | 40 41 45 40 38 41 41 40 38 44 40
4 | 7 10 12 7 12 6 8 12 8 14 3 | 24 21 22 23 20 21 26 24 24 23 22
5E | 7 16 7 13 12 5 14 9 7 19 4 | 42 43 37 46 40 41 45 40 42 42 41
6 | 8 8 13 9 14 4 8 6 5 9 3 | 30 33 34 29 28 28 35 30 29 30 30
7 | 10 10 14 10 16 3 8 9 8 17 4 | 35 31 25 31 31 28 34 23 28 33 28
8 | 8 8 14 7 13 5 9 15 8 264 4 | 35 42 37 38 42 38 44 35 38 183 38
9 | 8 6 14 8 11 3 8 10 5 11 3 | 30 29 22 27 28 25 33 24 24 34 27
X10 | 12 14 12 15 171 11 --- 14 12 --- 6 | 28 29 24 33 112 27 --- 29 28 --- 26
11 | 9 9 17 10 15 3 7 10 9 24 4 | 44 46 41 48 53 44 50 45 46 49 45
12E | 14 14 6 14 14 6 15 17 11 14 4 | 27 29 23 29 24 25 31 26 27 24 24
13 | 10 11 13 13 14 6 11 14 7 12 4 | 31 38 29 37 41 30 41 37 29 38 34
14 | 8 11 14 13 12 4 10 13 10 15 4 | 37 36 32 40 33 33 37 35 36 33 34
15 | 16 9 11 13 16 3 13 12 10 11 4 | 43 36 35 33 32 34 41 28 34 31 33
16E | 19 11 11 14 18 3 10 20 10 14 5 | 34 26 25 35 30 29 30 34 32 27 28
17 | 15 12 12 14 15 4 9 15 11 16 4 | 31 32 26 38 33 33 35 33 34 31 31
18E | 12 10 8 13 13 5 9 11 11 14 4 | 33 35 30 38 37 32 37 24 35 30 32
19 | 10 11 13 13 15 4 10 10 10 24 4 | 28 31 24 33 32 26 33 27 25 30 26
20E | 17 8 8 14 9 6 10 13 9 9 4 | 53 53 52 61 52 54 56 47 56 51 53
21 | 9 8 14 11 13 5 10 14 9 12 3 | 32 31 26 38 33 30 34 33 32 25 30
22E | 13 7 6 8 14 4 8 9 8 9 3 | 39 42 39 43 44 41 45 42 47 38 41
23 | 13 10 13 10 17 4 11 15 11 16 4 | 30 31 22 30 32 26 35 29 25 26 26
24 | 10 8 14 13 9 3 12 10 6 12 3 | 26 29 25 25 25 24 31 26 25 31 26
25E | 6 10 12 9 13 5 7 8 9 9 3 | 26 24 27 23 22 23 29 22 26 22 24
26E | 13 9 14 9 17 5 11 10 8 12 4 | 31 31 35 31 32 31 34 27 29 25 29
27 | 9 6 16 6 16 5 6 8 7 18 3 | 33 34 28 35 37 34 37 34 34 31 33
28E | 13 8 9 13 18 4 9 9 7 14 4 | 25 21 17 23 19 22 24 22 26 19 21
29 | 10 11 14 14 14 3 13 21 10 16 4 | 33 28 23 37 23 26 30 34 25 27 26
30 | 8 8 13 10 14 2 7 7 5 16 3 | 104 104 101 105 106 104 107 102 105 110 104
31 | 8 11 14 13 17 4 10 14 9 16 4 | 35 43 35 39 41 37 43 37 37 40 37
32E | 15 13 13 10 28 5 16 15 14 12 5 | 69 69 69 69 63 68 73 72 70 69 68
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 10 12 11 15 4 10 12 9 49 |T 36 36 33 38 38 34 39 34 35 40 34
WRMS | 10 10 13 11 14 4 10 11 8 14 |NE 35 36 31 37 39 33 39 34 33 43 33
MEDI | 10 10 13 11 14 4 10 11 8 14 |MD 32 31 27 35 32 30 35 30 29 31 30
Table 3.1863.1 GPS week: 1863 Day: 1 MJD: 57286.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 7 9 12 8 8 3 5 8 4 22 3 | 27 28 28 24 25 26 30 25 26 33 26
2 | 8 12 12 15 17 4 13 12 12 19 4 | 23 25 23 30 21 22 27 22 22 19 22
3E | 14 9 13 6 30 4 10 10 7 17 4 | 27 30 32 28 26 28 29 30 29 28 27
4 | 8 9 12 7 13 5 7 12 5 15 3 | 23 22 24 23 21 22 24 25 23 23 22
5E | 10 11 6 13 13 4 12 11 9 11 3 | 33 32 29 35 28 31 34 28 34 29 31
6 | 7 8 13 8 15 4 8 12 6 10 3 | 29 30 30 27 26 27 32 27 27 26 27
7 | 16 8 11 10 15 3 10 11 8 19 4 | 34 30 25 28 28 26 33 22 27 28 26
8 | 8 7 14 8 10 4 6 11 7 245 3 | 31 34 29 33 31 31 37 31 32 156 31
9 | 9 8 12 7 11 3 8 8 6 14 3 | 23 24 20 23 22 21 27 20 20 27 21
X10 | 21 15 19 15 16 11 11 16 20 --- 6 | 34 28 23 24 33 26 27 31 35 --- 26
11 | 12 9 16 11 15 3 8 10 8 26 4 | 30 33 29 33 37 29 36 32 30 31 31
12E | 10 18 8 13 16 5 19 15 17 14 5 | 35 39 34 35 34 35 39 35 35 33 34
13 | 10 9 12 13 16 4 13 15 10 17 4 | 30 34 30 32 34 29 37 31 26 30 30
14 | 10 12 12 11 13 4 9 15 10 19 4 | 35 34 32 33 32 31 35 29 33 29 31
15 | 14 10 10 13 17 4 12 13 13 14 4 | 31 30 26 24 24 26 32 22 30 21 25
16E | 19 9 11 16 14 4 11 17 9 13 4 | 29 29 27 34 27 28 27 32 29 27 27
17 | 13 12 13 13 15 3 13 12 10 22 4 | 28 32 26 33 27 28 34 26 28 30 28
18E | 15 10 7 16 12 4 9 12 10 13 4 | 27 30 23 30 27 25 27 17 29 23 24
19 | 11 12 13 16 12 4 12 13 9 27 5 | 28 29 26 30 24 24 30 26 25 25 25
20E | 14 8 6 12 15 5 9 11 8 11 3 | 38 39 37 42 36 38 40 32 40 39 37
21 | 11 9 12 12 15 4 10 11 10 13 4 | 28 28 24 29 29 24 29 23 25 20 24
22E | 15 9 6 11 13 2 6 8 8 11 3 | 27 29 26 31 32 26 30 28 30 24 27
23 | 15 11 13 11 17 3 9 14 11 19 4 | 29 31 24 27 27 26 31 28 25 24 26
24 | 12 7 12 10 10 7 10 10 8 12 3 | 25 27 26 23 23 23 33 23 22 28 25
25E | 9 10 13 7 12 4 9 8 7 10 3 | 23 25 29 24 22 25 29 23 25 22 24
26E | 17 12 14 9 14 4 10 8 8 15 4 | 25 33 31 28 26 27 26 27 28 24 27
27 | 9 8 15 8 11 4 7 8 9 20 3 | 29 32 28 33 31 30 33 30 32 32 30
28E | 15 12 8 14 25 4 12 9 8 13 4 | 24 24 20 23 24 21 26 23 26 22 22
29 | 12 12 13 12 15 5 13 24 10 15 5 | 31 27 25 29 20 25 29 30 25 26 25
30 | 9 8 11 9 12 3 8 7 6 19 3 | 126 124 125 126 125 125 128 123 124 129 124
31 | 9 13 13 13 16 4 10 13 11 17 4 | 44 48 42 44 47 43 48 42 44 43 44
32E | 14 15 14 9 21 6 13 13 15 12 5 | 58 61 59 56 54 58 61 63 56 56 58
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 10 12 11 15 4 10 12 9 47 |T 33 34 31 33 31 31 35 31 32 35 31
WRMS | 11 10 12 11 15 4 10 11 8 14 |NE 34 34 31 33 32 31 36 31 32 39 31
MEDI | 11 9 12 11 15 4 10 11 9 15 |MD 29 30 27 30 27 26 31 28 28 28 27
Table 3.1863.2 GPS week: 1863 Day: 2 MJD: 57287.000
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 | 6 8 11 7 10 3 9 10 4 15 3 | 26 30 30 25 28 27 32 23 27 34 27
2 | 9 13 12 15 14 4 13 14 8 20 4 | 27 26 23 34 25 25 28 23 26 20 24
3E | 13 12 13 8 20 3 11 13 5 11 4 | 24 28 30 24 25 25 28 26 27 25 24
4 | 8 10 13 7 12 6 8 11 6 11 3 | 22 23 23 23 21 20 23 21 19 21 20
5E | 9 11 7 10 14 3 12 11 7 9 3 | 32 34 26 35 28 31 35 28 34 29 31
6 | 9 8 11 8 15 4 10 14 7 8 3 | 28 31 30 28 28 27 32 25 26 31 27
7 | 14 10 11 12 13 2 12 12 7 17 4 | 29 28 23 30 28 25 32 19 25 31 25
8 | 8 8 13 7 9 4 7 9 5 216 3 | 29 35 31 30 34 31 36 31 31 136 31
9 | 8 7 12 7 11 3 10 7 4 10 3 | 21 23 19 22 25 21 25 21 21 27 21
X10 | 19 18 19 26 14 12 14 8 21 --- 7 | 29 23 31 28 36 24 21 21 22 --- 20
11 | 9 11 15 9 16 4 11 11 8 19 4 | 29 34 29 34 40 30 37 33 29 32 31
12E | 17 21 9 12 15 5 15 16 12 11 5 | 34 33 21 30 28 26 33 25 29 26 26
13 | 10 13 14 10 13 4 12 18 8 12 4 | 33 39 30 36 38 32 38 32 32 30 33
14 | 9 11 15 10 13 4 10 13 9 14 4 | 28 28 28 31 28 27 32 26 26 28 27
15 | 12 11 14 12 13 4 10 10 8 10 4 | 33 34 30 31 27 30 34 25 27 26 28
16E | 21 11 9 12 21 5 13 19 9 12 5 | 31 29 24 26 27 24 28 26 23 26 24
17 | 11 13 12 12 14 3 15 12 8 17 4 | 30 34 30 38 32 30 36 27 31 35 30
18E | 20 11 7 12 9 4 14 11 10 11 4 | 31 30 25 32 28 25 31 21 26 27 25
19 | 11 13 12 13 13 4 14 13 9 21 4 | 25 27 23 28 25 22 28 23 21 24 22
20E | 18 9 9 10 9 5 10 11 8 8 3 | 45 43 42 46 41 43 43 39 45 43 42
21 | 11 11 13 11 13 4 11 10 9 13 4 | 31 28 23 33 31 25 29 24 23 21 25
22E | 18 11 6 9 11 4 9 9 8 8 3 | 29 32 30 34 35 30 33 31 32 30 30
23 | 14 12 12 10 16 5 12 15 10 16 4 | 27 31 26 27 31 26 31 27 26 27 26
24 | 13 9 15 9 9 6 9 10 8 11 3 | 26 24 23 21 23 23 27 22 20 22 21
25E | 10 10 14 6 14 4 10 8 7 8 3 | 21 18 27 21 19 22 27 19 21 19 20
26E | 16 13 16 7 11 7 12 13 8 13 4 | 24 31 31 27 25 27 29 23 27 23 25
27 | 8 7 14 7 10 4 7 7 6 21 3 | 25 29 25 30 30 28 30 27 27 29 27
28E | 12 12 8 10 14 4 12 10 8 13 3 | 24 22 19 25 24 20 25 21 25 27 22
29 | 10 13 14 13 11 6 14 18 9 15 4 | 28 26 24 34 26 25 27 31 25 25 24
30 | 8 8 12 10 11 2 9 12 6 12 3 | 122 123 123 122 126 123 124 123 122 123 123
31 | 9 13 16 10 17 5 11 12 8 15 4 | 35 36 32 34 37 32 39 26 32 34 32
32E | 15 15 15 8 23 7 15 13 16 12 5 | 62 66 63 62 60 62 66 63 65 59 62
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 12 12 10 14 4 11 12 8 41 |T 32 33 31 33 33 30 34 29 31 35 30
WRMS | 10 12 12 9 13 4 11 11 7 13 |NE 32 33 31 34 34 31 35 30 30 37 30
MEDI | 11 11 12 10 13 4 11 11 8 12 |MD 29 30 27 30 28 26 31 25 26 27 26
Table 3.1863.3 GPS week: 1863 Day: 3 MJD: 57288.000
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 | 5 7 13 7 11 3 7 7 8 21 3 | 27 29 29 26 29 26 30 25 29 30 27
2 | 7 14 12 15 17 4 14 14 9 20 4 | 22 26 20 33 22 23 27 23 23 17 22
3E | 17 9 14 5 20 4 8 13 9 18 4 | 26 27 31 26 24 26 27 29 30 24 25
4 | 7 8 13 7 13 4 9 10 7 14 3 | 21 22 23 24 21 20 24 20 23 17 21
5E | 11 10 8 10 14 3 12 12 7 13 3 | 37 37 33 40 40 37 39 33 40 34 36
6 | 7 8 11 9 13 4 10 13 6 16 3 | 30 33 29 28 28 26 34 28 26 25 28
7 | 13 8 12 11 15 4 7 10 9 19 4 | 31 29 24 29 29 26 31 22 26 27 25
8 | 7 8 14 6 15 3 8 10 6 214 3 | 48 51 49 47 46 49 53 49 51 125 49
9 | 9 8 12 6 11 3 6 8 7 15 3 | 20 23 20 22 23 19 25 19 23 26 20
X10 | 28 10 --- 22 13 18 10 20 20 --- 7 | 32 31 --- 27 39 25 27 29 41 --- 28
11 | 6 8 17 10 14 4 8 8 8 25 4 | 35 38 33 41 43 36 40 34 35 36 36
12E | 12 18 9 12 16 4 16 15 14 17 5 | 41 47 41 43 42 41 46 41 44 41 42
13 | 10 11 12 11 13 5 13 13 8 13 4 | 31 39 30 37 43 32 39 34 33 30 34
14 | 8 8 13 10 14 5 10 14 8 15 4 | 34 37 34 36 36 32 38 32 34 34 33
15 | 12 9 10 13 12 4 13 12 9 11 4 | 33 29 28 27 25 26 34 21 28 24 26
16E | 15 10 8 16 15 4 11 14 8 14 4 | 24 24 23 30 20 22 22 27 23 23 22
17 | 11 13 13 14 15 3 13 12 11 20 4 | 33 34 28 39 34 33 35 30 35 32 32
18E | 17 8 7 12 11 4 9 12 9 13 4 | 30 30 26 34 28 27 29 21 30 27 26
19 | 9 11 13 16 12 3 11 10 10 26 4 | 30 31 27 35 29 27 32 27 27 27 27
20E | 24 9 8 12 13 3 9 9 9 8 4 | 48 46 44 48 44 47 47 41 47 45 45
21 | 8 11 13 12 14 3 13 10 10 13 4 | 28 29 23 29 28 25 29 23 25 18 24
22E | 19 7 5 12 13 5 8 11 10 12 4 | 31 36 31 35 37 31 35 33 36 31 32
23 | 16 11 12 13 17 4 11 13 12 20 4 | 33 34 29 33 35 27 36 31 30 23 29
24 | 10 8 13 9 10 4 8 9 7 15 3 | 25 27 26 27 26 24 30 24 24 27 24
25E | 9 8 14 7 10 5 7 9 6 12 3 | 21 23 28 21 20 22 25 21 22 17 21
26E | 15 9 15 7 14 6 8 9 7 13 3 | 25 32 33 26 28 26 28 28 28 26 27
27 | 10 6 12 8 13 3 5 7 6 21 3 | 28 32 27 31 32 30 33 28 32 30 29
28E | 12 10 7 12 17 5 10 9 8 17 4 | 24 24 19 28 26 22 25 24 27 30 23
29 | 10 12 12 14 14 5 14 19 9 19 4 | 31 28 24 30 24 26 30 32 26 29 26
30 | 9 8 12 9 37 4 8 9 6 15 4 | 290 291 292 289 284 290 291 292 289 287 289
31 | 8 11 13 14 15 4 12 14 10 18 4 | 47 52 44 47 51 46 52 43 46 50 46
32E | 12 12 12 7 16 7 12 12 17 13 4 | 60 59 59 59 59 56 61 59 60 54 58
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 12 10 12 11 15 4 10 11 9 41 |T 39 41 38 41 40 38 42 38 40 40 38
WRMS | 10 10 12 11 14 4 10 10 8 16 |NE 43 45 41 44 44 41 46 41 43 45 41
MEDI | 10 9 12 11 14 4 10 11 8 15 |MD 31 31 29 31 29 26 32 28 30 29 27
Table 3.1863.4 GPS week: 1863 Day: 4 MJD: 57289.000
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 | 5 8 12 7 8 9 9 6 5 17 3 | 25 28 29 24 25 26 31 22 25 33 25
2 | 11 16 15 14 16 4 15 12 9 21 5 | 22 28 19 29 20 22 27 23 21 18 20
3E | 12 10 15 13 12 3 11 13 9 13 4 | 29 36 38 31 33 32 34 33 32 34 31
4 | 7 7 13 4 11 5 9 8 6 11 3 | 17 19 21 17 14 17 19 15 15 15 15
5E | 9 10 9 9 14 4 13 10 10 14 3 | 38 41 38 44 42 40 42 36 44 45 40
6 | 8 11 13 7 13 3 11 8 8 13 3 | 28 32 30 26 26 26 34 27 27 30 27
7 | 14 8 14 11 15 3 12 10 9 18 4 | 32 31 26 29 28 28 32 23 26 30 26
8 | 7 8 14 6 9 5 8 6 6 206 3 | 38 44 39 40 41 40 43 38 41 155 39
9 | 7 7 13 8 8 4 8 8 7 15 3 | 23 28 23 23 26 24 30 24 26 34 24
X10 | 26 17 --- 20 13 8 16 20 21 --- 8 | 36 30 --- 20 26 25 25 31 26 --- 24
11 | 7 8 17 8 13 4 10 8 9 22 4 | 28 34 29 31 38 29 34 27 27 32 28
12E | 19 16 8 12 15 5 18 16 13 14 5 | 34 39 33 36 30 34 36 33 33 29 32
13 | 8 11 15 10 16 5 13 13 7 14 4 | 30 38 31 38 40 32 38 35 29 38 33
14 | 8 9 13 7 15 7 18 14 10 16 4 | 33 36 33 33 36 31 38 29 30 29 31
15 | 12 9 13 10 15 5 11 11 8 12 4 | 30 30 28 28 25 26 31 23 24 26 25
16E | 15 13 10 13 16 5 16 13 10 14 4 | 23 25 21 29 23 21 25 27 25 28 23
17 | 11 13 14 10 12 3 16 12 11 22 4 | 28 32 25 33 32 30 33 29 32 32 28
18E | 10 12 7 10 15 5 11 11 7 14 3 | 30 33 32 36 30 31 33 25 33 33 30
19 | 13 11 13 12 13 4 14 11 9 31 5 | 26 29 23 28 25 22 28 23 21 29 22
20E | 10 13 9 6 18 5 13 11 7 12 4 | 75 72 73 76 70 73 72 74 73 77 73
21 | 9 9 13 12 12 4 11 9 9 14 3 | 23 26 20 25 24 20 27 18 19 16 20
22E | 19 13 7 8 21 4 12 8 9 12 4 | 31 37 34 35 30 34 37 32 37 29 32
23 | 14 11 12 10 15 3 12 14 10 20 4 | 33 37 31 32 36 32 36 32 30 32 31
24 | 10 8 15 9 14 3 12 6 8 11 3 | 23 27 25 22 23 23 30 23 23 24 23
25E | 7 11 14 7 10 6 10 8 6 10 3 | 25 27 33 25 22 26 29 26 25 23 25
26E | 12 10 14 10 15 4 12 7 8 15 4 | 22 30 33 26 26 25 27 23 25 20 24
27 | 6 7 14 5 12 3 8 5 10 19 3 | 26 30 27 28 27 28 29 27 27 27 26
28E | 12 10 9 9 11 4 15 8 7 14 3 | 20 25 22 26 28 24 28 25 27 26 23
29 | 9 15 15 11 11 4 14 18 10 16 4 | 25 26 23 27 21 23 28 31 19 27 22
30 | 8 9 14 7 15 4 11 7 6 15 3 | 240 239 240 241 241 241 243 237 240 247 240
31 | 10 11 12 13 18 4 13 12 9 17 4 | 41 45 40 39 41 40 46 39 36 41 39
32E | 14 13 11 7 19 5 14 11 11 11 4 | 57 61 60 58 56 58 63 60 59 60 58
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 11 11 13 10 14 5 12 11 9 40 |T 37 40 38 38 37 36 40 36 36 42 36
WRMS | 10 11 13 9 14 4 12 10 8 15 |NE 38 41 38 38 38 37 42 36 36 45 36
MEDI | 10 10 13 9 14 4 12 10 9 14 |MD 28 31 30 29 28 28 32 27 27 30 26
Table 3.1863.5 GPS week: 1863 Day: 5 MJD: 57290.000
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 | 4 7 13 7 12 6 9 8 5 14 3 | 23 26 25 24 24 23 29 20 21 31 23
2 | 12 10 16 12 16 5 11 14 9 22 4 | 23 24 20 29 23 23 26 21 21 18 20
3E | 17 10 16 10 17 3 10 12 9 9 4 | 28 32 35 29 30 27 32 30 28 30 29
4 | 10 8 11 9 13 4 9 8 7 9 3 | 21 18 19 20 18 16 21 15 18 17 17
5E | 14 11 8 9 15 5 10 15 8 22 4 | 35 34 33 37 32 35 37 34 38 39 34
6 | 9 9 14 7 13 4 10 9 9 11 3 | 28 29 27 27 25 23 30 22 25 24 24
7 | 14 10 11 10 13 4 12 10 9 14 4 | 32 28 23 28 29 24 33 19 24 25 24
8 | 8 7 12 7 19 5 7 7 7 18 3 | 35 37 35 32 33 33 37 32 33 90 34
9 | 9 7 13 5 15 3 9 6 6 10 3 | 23 23 20 20 23 19 27 20 22 25 20
X10 | 21 18 21 24 18 9 12 12 13 --- 6 | 32 25 28 32 38 25 21 25 23 --- 23
11 | 5 8 14 9 16 3 11 8 9 14 3 | 29 31 29 30 36 27 33 25 28 26 27
12E | 21 16 8 11 18 5 15 13 12 13 5 | 37 36 29 34 33 31 35 30 32 35 31
13 | 11 11 14 9 19 5 12 11 7 10 4 | 25 35 26 31 37 26 34 27 29 28 28
14 | 8 11 13 9 12 6 10 15 9 17 4 | 27 34 27 32 28 26 34 27 28 29 28
15 | 15 9 13 11 13 4 10 11 9 12 4 | 30 27 25 28 22 23 29 20 23 23 23
16E | 15 12 10 12 18 4 15 12 9 12 4 | 30 28 27 29 26 25 26 32 28 29 26
17 | 14 12 14 11 15 4 15 12 11 19 4 | 31 29 23 30 30 26 32 27 30 27 26
18E | 18 10 7 10 19 5 9 12 7 11 4 | 28 27 28 34 33 27 28 22 29 32 26
19 | 9 13 11 14 13 4 14 12 8 21 4 | 27 30 25 30 27 21 30 24 23 20 24
20E | 10 12 11 8 11 5 13 13 7 9 3 | 60 56 58 60 57 59 57 64 57 62 58
21 | 8 10 14 11 15 4 11 10 8 13 4 | 26 28 20 30 30 21 29 22 23 22 23
22E | 26 7 6 10 14 4 9 13 6 9 4 | 35 34 30 37 32 31 35 34 34 30 31
23 | 15 10 12 11 17 3 12 13 10 18 4 | 30 30 23 25 27 22 31 26 24 20 24
24 | 10 8 15 8 13 4 11 7 11 9 3 | 22 24 19 21 22 20 28 19 24 22 20
25E | 9 10 14 7 14 4 9 7 7 11 3 | 26 25 28 24 24 22 26 23 21 23 23
26E | 15 9 15 16 16 4 10 5 7 11 4 | 24 25 31 30 21 25 26 24 26 26 24
27 | 9 7 12 7 13 5 7 4 5 10 3 | 27 29 26 27 32 26 29 26 29 30 27
28E | 14 9 7 8 16 4 13 9 8 12 3 | 20 20 16 21 28 17 24 18 22 23 19
29 | 12 13 14 14 15 3 12 15 10 13 4 | 29 24 21 30 26 24 28 31 24 29 24
30 | 10 8 12 8 12 4 9 5 6 14 3 | 242 241 241 241 242 243 242 240 241 244 241
31 | 7 13 13 11 18 4 12 13 9 17 4 | 52 58 53 54 54 54 57 51 53 53 53
32E | 21 13 11 7 17 4 13 11 11 13 4 | 60 64 61 62 57 60 65 60 62 61 61
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 10 12 10 15 4 11 11 8 14 |T 37 37 35 38 37 34 39 34 35 38 34
WRMS | 11 10 13 9 15 4 11 9 8 14 |NE 38 39 35 39 39 35 40 35 36 40 35
MEDI | 11 10 13 9 15 4 11 11 8 13 |MD 28 29 27 30 29 25 30 25 26 28 24
Table 3.1863.6 GPS week: 1863 Day: 6 MJD: 57291.000
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 | 6 7 12 8 10 3 8 9 7 15 3 | 29 33 32 27 25 28 34 26 27 36 29
2 | 12 15 15 14 16 5 11 12 9 18 4 | 23 28 21 32 24 23 27 23 21 19 21
3E | 26 10 16 10 14 5 10 13 11 10 5 | 32 33 37 33 34 30 33 33 32 29 31
4 | 9 9 11 9 12 3 10 9 6 9 3 | 19 19 22 18 15 16 20 16 16 13 15
5E | 9 13 10 9 14 4 12 8 9 18 4 | 49 48 45 52 45 48 50 43 49 50 47
6 | 9 8 13 5 14 4 8 10 5 9 3 | 35 37 37 33 29 33 39 31 31 35 32
7 | 11 9 13 9 15 4 11 9 9 10 3 | 36 35 32 34 33 32 37 29 31 34 31
8 | 7 8 12 8 10 3 8 8 7 13 3 | 34 40 37 37 39 36 39 40 38 80 37
9 | 9 8 13 7 11 3 7 6 5 10 3 | 24 26 23 24 25 22 28 23 23 28 23
X10 | 30 24 15 --- 16 36 13 19 13 --- 8 | 38 37 26 --- 34 27 28 34 32 --- 30
11 | 8 9 15 10 14 3 11 10 8 11 3 | 35 35 32 40 43 34 37 37 37 30 35
12E | 20 16 9 14 17 4 15 13 10 12 5 | 33 32 28 37 27 29 31 32 29 32 29
13 | 12 10 15 8 18 4 12 15 10 15 4 | 35 44 35 42 45 37 42 41 36 39 38
14 | 7 11 12 11 12 5 11 14 9 14 4 | 40 43 39 47 41 39 45 42 42 38 40
15 | 19 9 13 11 17 4 9 13 8 13 4 | 35 29 28 28 25 25 28 21 24 26 24
16E | 16 12 8 14 15 6 13 15 9 9 4 | 29 29 28 33 28 28 28 38 31 33 29
17 | 13 12 14 13 15 4 15 11 11 15 4 | 36 37 35 46 39 37 37 38 41 35 36
18E | 10 10 8 8 15 5 11 11 9 12 3 | 35 37 34 40 37 33 36 29 35 36 33
19 | 11 13 14 13 12 4 14 13 8 19 4 | 30 34 29 35 30 28 33 32 28 26 28
20E | 9 10 9 7 21 4 11 12 5 7 3 | 67 68 69 74 74 70 73 74 71 72 71
21 | 7 11 14 9 13 4 12 9 7 11 3 | 25 30 23 32 29 25 31 25 25 25 25
22E | 14 9 6 10 20 4 8 21 8 9 4 | 47 49 47 52 52 48 52 49 52 46 48
23 | 16 11 12 11 15 4 13 14 11 15 4 | 34 37 31 36 37 32 38 38 32 32 33
24 | 10 8 15 6 15 4 9 5 7 8 3 | 24 30 27 27 28 26 32 26 28 26 26
25E | 10 12 13 8 11 7 9 10 6 8 3 | 29 31 36 31 29 31 30 28 30 27 29
26E | 17 11 15 16 14 4 11 11 8 9 4 | 27 31 35 32 26 28 28 30 29 25 27
27 | 9 8 12 7 13 3 8 8 6 12 3 | 31 35 33 35 36 33 34 36 36 36 33
28E | 14 8 9 9 18 5 12 9 10 10 4 | 27 28 28 34 31 27 31 30 31 34 29
29 | 11 12 14 12 14 2 13 12 9 11 4 | 32 31 26 36 29 29 30 34 28 32 29
30 | 7 7 13 7 11 4 8 6 8 9 3 | 200 200 204 201 196 201 202 201 201 199 200
31 | 9 13 13 12 23 8 13 14 8 14 4 | 97 96 90 92 88 93 99 96 96 99 95
32E | 18 18 13 7 13 4 13 11 10 15 4 | 65 74 66 66 66 66 73 64 65 65 66
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 13 11 12 10 15 4 11 12 8 12 |T 41 43 41 44 41 40 43 41 41 43 40
WRMS | 11 11 13 9 14 4 11 10 7 11 |NE 42 44 41 45 42 40 44 42 41 44 40
MEDI | 10 10 13 9 14 4 11 11 8 11 |MD 34 35 32 35 33 31 34 33 31 34 31
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 4.1863 GPS week: 1863 MJD: 57285.0-57291.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3063 |U 5 7 15 |U 5 9 24 |U 7 8 15 |
emr | emr 3068 | 7 9 20 |U 6 9 24 | 10 9 17 |
esa | esa 3044 | 6 7 16 |U 6 10 28 | 10 9 19 |
gfz | gfz 3054 |U 6 7 15 |U 6 10 25 |U 9 8 17 |
grg | grg 3071 |U 8 9 20 |U 7 12 32 | 10 9 22 |
igr | igr 3031 | 6 7 15 | 6 10 24 | 8 8 17 |
igs | igs 3068 | 6 7 16 | 6 10 24 | 9 8 16 |
jpl | jpl 3049 | 7 7 17 |U 6 11 25 |U 10 9 17 |
mit | mit 3072 | 6 7 16 |U 7 11 27 |U 9 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 5.1863.0 GPS week: 1863 Day: 0 MJD: 57285.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3057 | 5 7 11 | 4 6 24 | 9 9 16 |
emr | emr 3068 | 7 8 18 | 5 7 21 | 12 12 17 |
esa | esa 3072 | 5 7 17 | 6 7 24 | 11 10 16 |
gfz | gfz 3069 | 5 6 12 | 5 9 24 | 10 9 17 |
grg | grg 3072 | 6 8 15 | 6 10 28 | 12 10 19 |
igr | igr 3034 | 5 7 12 | 5 8 21 | 10 10 15 |
igs | igs 3070 | 5 7 14 | 5 8 21 | 11 10 16 |
jpl | jpl 2972 | 6 7 16 | 6 10 25 | 11 12 17 |
mit | mit 3072 | 6 5 11 | 8 8 24 | 11 10 16 |
Table 5.1863.1 GPS week: 1863 Day: 1 MJD: 57286.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 6 6 16 | 4 8 21 | 6 6 12 |
emr | emr 3068 | 9 9 21 | 5 7 20 | 8 8 16 |
esa | esa 3072 | 7 7 19 | 5 7 24 | 8 5 19 |
gfz | gfz 3069 | 7 6 17 | 4 8 22 | 7 6 12 |
grg | grg 3072 | 8 8 20 | 6 10 37 | 8 7 15 |
igr | igr 3068 | 7 7 17 | 4 8 21 | 6 5 15 |
igs | igs 3071 | 7 7 18 | 4 7 22 | 7 6 12 |
jpl | jpl 3066 | 7 6 21 | 5 8 20 | 8 7 15 |
mit | mit 3072 | 8 10 21 | 6 11 24 | 9 9 17 |
Table 5.1863.2 GPS week: 1863 Day: 2 MJD: 57287.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 7 6 18 | 5 8 20 | 7 6 13 |
emr | emr 3068 | 9 8 27 | 6 9 17 | 9 6 13 |
esa | esa 3072 | 7 5 18 | 5 9 20 | 9 7 14 |
gfz | gfz 3068 | 7 6 17 | 5 10 21 | 9 6 15 |
grg | grg 3072 | 10 11 26 | 7 10 34 | 11 7 22 |
igr | igr 2976 | 7 5 16 | 5 10 19 | 8 5 12 |
igs | igs 3067 | 7 6 19 | 5 9 18 | 8 6 13 |
jpl | jpl 3056 | 9 7 20 | 6 10 18 | 8 6 13 |
mit | mit 3072 | 8 7 17 | 7 9 21 | 8 7 15 |
Table 5.1863.3 GPS week: 1863 Day: 3 MJD: 57288.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3065 | 5 7 14 | 8 11 17 | 7 6 14 |
emr | emr 3068 | 7 9 19 | 9 9 19 | 8 6 13 |
esa | esa 2976 | 6 7 17 | 7 11 21 | 9 8 17 |
gfz | gfz 3068 | 6 8 15 | 7 12 19 | 8 6 14 |
grg | grg 3072 | 8 6 16 | 9 15 29 | 11 9 24 |
igr | igr 3040 | 6 8 15 | 7 12 17 | 7 6 13 |
igs | igs 3066 | 6 7 16 | 7 11 18 | 7 6 12 |
jpl | jpl 3062 | 8 9 18 | 7 11 19 | 9 8 13 |
mit | mit 3072 | 7 9 18 | 9 11 27 | 7 8 12 |
Table 5.1863.4 GPS week: 1863 Day: 4 MJD: 57289.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3059 | 5 8 16 | 6 12 32 | 8 10 22 |
emr | emr 3068 | 6 8 18 | 7 11 31 | 11 10 24 |
esa | esa 2976 | 5 7 15 | 7 12 38 | 11 11 22 |
gfz | gfz 3068 | 4 8 14 | 6 11 33 | 11 10 24 |
grg | grg 3072 | 6 10 19 | 8 14 38 | 12 10 27 |
igr | igr 3055 | 5 7 15 | 6 12 33 | 10 10 22 |
igs | igs 3068 | 5 7 14 | 6 12 31 | 11 11 22 |
jpl | jpl 3064 | 5 8 16 | 7 12 30 | 11 12 24 |
mit | mit 3072 | 5 6 16 | 7 14 30 | 10 11 21 |
Table 5.1863.5 GPS week: 1863 Day: 5 MJD: 57290.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3069 | 5 5 11 | 6 13 25 | 8 8 18 |
emr | emr 3068 | 7 7 15 | 7 12 30 | 11 8 20 |
esa | esa 3072 | 5 5 11 | 8 13 35 | 10 9 22 |
gfz | gfz 3068 | 6 6 12 | 6 12 25 | 11 8 20 |
grg | grg 3072 | 7 8 17 | 7 13 27 | 10 7 23 |
igr | igr 3069 | 5 5 11 | 7 14 26 | 9 8 19 |
igs | igs 3068 | 6 5 11 | 7 13 27 | 10 8 19 |
jpl | jpl 3063 | 6 6 12 | 7 14 30 | 11 9 19 |
mit | mit 3072 | 5 5 11 | 8 13 29 | 10 10 19 |
Table 5.1863.6 GPS week: 1863 Day: 6 MJD: 57291.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3062 | 6 10 17 | 4 7 31 | 7 9 13 |
emr | emr 3068 | 7 12 20 | 6 9 30 | 10 11 20 |
esa | esa 3072 | 6 8 17 | 6 9 33 | 10 11 21 |
gfz | gfz 2973 | 5 8 18 | 6 9 28 | 8 9 17 |
grg | grg 3071 | 9 13 23 | 6 10 34 | 9 13 24 |
igr | igr 2975 | 6 9 17 | 5 9 31 | 9 11 21 |
igs | igs 3068 | 6 9 18 | 5 9 28 | 8 10 17 |
jpl | jpl 3064 | 8 9 19 | 6 10 31 | 9 10 18 |
mit | mit 3072 | 6 9 20 | 6 9 34 | 9 12 21 |
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 6.1863 GPS week: 1863 MJD: 57285.500-57291.500
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 | -24 2 -56 34 3 | 23 35
| 12 12 40 69 4 | 4
emr uuuuu | 12 -17 150 54 -3 | 15 32
| 15 20 85 40 15 | 9
esa uuuuu | -14 26 87 19 1 | 34 41
| 14 11 53 72 3 | 4
gfz uuuuu | 6 -32 95 -84 -3 | 33 39
| 10 29 118 41 7 | 3
grg uuuuu | -31 16 32 -60 -2 | 27 33
| 19 9 31 67 5 | 3
igr xxxxx | -3 33 -36 -25 -4 | 2 24
| 8 15 62 46 7 | 4
irf xxxxx | 21 -3 -40 24 -4 | 3 23
| 9 7 23 26 5 | 4
jpl uuuuu | 7 -14 65 -6 -1 | 52 57
| 19 24 73 43 16 | 3
mit uuuuu | 0 22 -138 64 -2 | 33 39
| 28 12 39 97 8 | 3
ngs uuuuu | 6 -1 -92 -54 1 | 18 30
| 46 39 57 96 5 | 4
sio uuuux | 35 23 -155 84 21 | 71 76
| 39 23 111 93 13 | 7
Table 7.1863.0 GPS week: 1863 Day: 0 MJD: 57285.500
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 -16 -1 -50 7 | 24 37
emr uuuuu | 1 -7 31 29 -8 | 24 39
esa uuuuu | -32 7 152 -39 5 | 34 42
gfz uuuuu | -2 -27 327 -95 1 | 33 41
grg uuuuu | -57 23 50 -59 -9 | 26 34
igr xxxxx | -3 64 10 -61 5 | 3 25
irf xxxxx | 26 0 -6 24 1 | 5 24
jpl uuuuu | 19 -42 -84 21 18 | 47 52
mit uuuuu | 33 31 -90 94 8 | 32 38
ngs uuuuu | -18 27 -157 -25 -8 | 19 32
sio uuuux | 74 17 -130 143 28 | 60 63
Table 7.1863.1 GPS week: 1863 Day: 1 MJD: 57286.500
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 -6 -35 20 5 | 29 41
emr uuuuu | 4 -42 238 72 -16 | 26 40
esa uuuuu | -27 28 97 -103 4 | 39 46
gfz uuuuu | 20 -20 37 -133 1 | 37 44
grg uuuuu | -34 7 21 12 -1 | 31 36
igr xxxxx | -14 39 -75 -35 -1 | 8 25
irf xxxxx | 24 -3 -51 64 -9 | 9 25
jpl uuuuu | 23 6 64 22 14 | 54 58
mit uuuuu | 18 27 -153 209 -2 | 37 43
ngs uuuuu | -35 -7 -121 -165 3 | 23 33
sio uuuux | 80 26 -205 211 32 | 68 71
Table 7.1863.2 GPS week: 1863 Day: 2 MJD: 57287.500
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 21 -122 8 3 | 27 38
emr uuuuu | 19 -45 235 72 -22 | 22 34
esa uuuuu | -21 40 9 -5 2 | 38 45
gfz uuuuu | 17 -4 -9 -10 7 | 36 43
grg uuuuu | -35 8 60 -80 6 | 30 35
igr xxxxx | 1 26 -7 -83 -3 | 7 24
irf xxxxx | 30 1 -47 51 1 | 7 22
jpl uuuuu | 25 15 94 46 6 | 56 61
mit uuuuu | 16 31 -146 109 8 | 36 42
ngs uuuuu | -37 -50 -20 -135 1 | 22 32
sio uuuux | 46 38 -123 93 33 | 71 75
Table 7.1863.3 GPS week: 1863 Day: 3 MJD: 57288.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -31 8 -83 -41 -2 | 17 30
emr uuuuu | 35 -8 116 51 -9 | 9 30
esa uuuuu | -17 35 147 31 2 | 29 37
gfz uuuuu | 4 -31 27 -107 -2 | 28 36
grg uuuuu | -22 5 62 -107 3 | 22 29
igr xxxxx | -4 22 48 -46 -7 | -2 24
irf xxxxx | 27 -2 -18 22 0 | -2 22
jpl uuuuu | 7 -12 35 -83 3 | 49 55
mit uuuuu | 10 5 -83 129 -3 | 29 37
ngs uuuuu | -22 -10 -18 4 8 | 13 27
sio uuuux | 51 47 -352 158 25 | 67 72
Table 7.1863.4 GPS week: 1863 Day: 4 MJD: 57289.500
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 | -42 4 -49 72 5 | 21 32
emr uuuuu | 25 -20 201 -3 5 | 9 30
esa uuuuu | -5 29 76 95 -4 | 33 41
gfz uuuuu | 0 2 9 -82 -4 | 32 39
grg uuuuu | -43 23 53 -163 -1 | 26 32
igr xxxxx | -11 34 -49 31 -2 | 1 24
irf xxxxx | 24 6 -43 -7 -4 | 2 23
jpl uuuuu | 3 2 111 -34 -10 | 54 59
mit uuuuu | 2 9 -140 -26 -3 | 33 40
ngs uuuuu | 20 -43 -68 73 0 | 17 30
sio uuuux | 25 42 -201 24 19 | 75 80
Table 7.1863.5 GPS week: 1863 Day: 5 MJD: 57290.500
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 | -26 -3 -30 90 6 | 24 33
emr uuuuu | 4 11 51 36 8 | 10 30
esa uuuuu | -2 23 90 73 2 | 35 42
gfz uuuuu | -8 -66 151 -108 -10 | 34 40
grg uuuuu | -31 25 -8 -54 -3 | 29 33
igr xxxxx | 11 19 -32 -19 -6 | 3 23
irf xxxxx | 12 -17 -40 2 -7 | 3 23
jpl uuuuu | 0 -16 134 -12 -11 | 56 60
mit uuuuu | -30 14 -163 -11 -8 | 35 41
ngs uuuuu | 53 16 -124 24 1 | 19 30
sio uuuux | -2 14 -70 -50 17 | 80 84
Table 7.1863.6 GPS week: 1863 Day: 6 MJD: 57291.500
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 | -29 9 -68 137 -1 | 20 30
emr uuuuu | -6 -9 176 123 19 | 4 24
esa uuuuu | 5 19 38 78 -4 | 31 37
gfz uuuuu | 8 -76 125 -54 -14 | 29 35
grg uuuuu | 3 18 -10 32 -8 | 26 31
igr xxxxx | -1 25 -143 39 -16 | -2 21
irf xxxxx | 6 -6 -75 10 -8 | -3 20
jpl uuuuu | -29 -48 105 0 -27 | 51 56
mit uuuuu | -46 37 -191 -57 -14 | 31 36
ngs uuuuu | 78 60 -137 -155 5 | 15 26
sio uuuux | -26 -20 -6 9 -4 | 79 83
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