[IGSREPORT-29678] Wk 2294 IGS Final Orbits
acc
acc at igs.org
Fri Jan 12 05:39:23 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2294 (Dec 24, 2023 - Dec 30, 2023)
Contacts: acc at igs.org
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:
IGS0OPSFIN_${yyyy}${doy}0000_01D_15M_ORB.SP3 IGS GPS ephemeris files in SP3
format.
IGS0OPSFIN_${yyyy}${doy}0000_01D_05M_CLK.CLK IGS GPS satellite and station
clocks in clock RINEX format.
IGS0OPSFIN_${yyyy}${doy}0000_01D_01D_CLS.SUM IGS GPS clock combination summary
report.
IGS0OPSFIN_${yyyy}${doy}0000_07D_01D_ERP.ERP Earth Rotation Parameters (ERP)
and their rates as well as
Universal Time (UT1-UTC) and
Length Of Day (LOD) associated
with IGS ephemerides.
IGS0OPSFIN_20233580000_07D_01D_SUM.SUM Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, and JPL.
The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | ESA | BOGT SCH2
0 | GFZ | 5 5 GUAM GUAM HERS
0 | GRG | CZTG DGAR FAIR LPGS AREQ BOGT CZTG DGAR FAIR LPGS
0 | GRG | PALM
0 | JGX | BOGT CAS1 DAV1 MBAR NYA2 YEL2 CAS1 CHUR DAV1 IQAL
0 | JGX | MBAR NIUM NYA2 SCOR YEL2
1 | COD | HYDE
1 | GFZ | 5 13 5 13
1 | GRG | 13 13 BOGT DGAR JFNG OUS2 SIN1 BOGT CZTG OUS2 SIN1
1 | JGX | DGAR NYA2 SGOC FALK IISC IQAL NYA2 SGOC
2 | COD | AREQ GUAM
2 | GFZ | 13 13
2 | GRG | 13 13 AREQ CZTG DAV1 GUAM JFNG POL2 AREQ CZTG DAV1
2 | GRG | GUAM HRAO JFNG PALM SVTL
2 | JGX | AREQ CAS1 NYA2 POL2 AREQ BAKE CAS1 DAV1 HRAO NYA2
2 | JGX | POL2 SALU
3 | ESA | SCUB GAMB
3 | GFZ | 13 13 DGAR GAMB GUAM DGAR GAMB GUAM HERS
3 | GRG | 13 13 FAIR FAIR ONS1 PALM SVTL
3 | JGX | CAS1 SCUB AREQ CAS1 DAV1 DGAR GAMB IQAL NYA2 UNSA
3 | MIT | BHR4
4 | COD | AREQ NTUS PALM SCUB
4 | ESA | CZTG NRMD PTBB
4 | GFZ | 13 17 13 17 SCUB SCUB
4 | GRG | 13 13 AREQ AREQ GUAM SVTL
4 | JGX | CAS1 BAKE CAS1 IISC
5 | COD | ASCG
5 | ESA | 25 25 SCUB SCUB
5 | GFZ | SCUB
5 | GRG | CZTG FAIR CZTG FAIR PALM SCUB SVTL
5 | JGX | CAS1 NYA2 BAKE CAS1 CPVG IQAL NYA2
6 | COD | NOT1
6 | ESA | NNOR PTBB
6 | GRG | 10 CCJ2 CZTG CCJ2 CZTG NNOR PALM SVTL
6 | JGX | 8 17 29 CAS1 NYA2 CAS1 CCJ2 NYA2
5. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
6. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
6 | COD | 27
6 | GFZ | 27
6 | GRG | 27
7. 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.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
Starting 28-Nov-2022, all IGS products, are based on the IGS realization of
the ITRF2020 reference frame (IGS20). Starting from the same date, the IGS
products are based on the repro3 standards, including long filename formats.
For more information see IGSMAIL #8238, #8256, #8274 and #8282.
8. 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 | .3 -1.1 -.4 -10 2 -23 .05
EMR | 0 | 9.6 1.4 2.5 9 -32 15 .09
ESA | 0 | .0 -.8 .2 -2 -13 -15 -.53
GFZ | 0 | -.2 -.7 .4 -7 5 -5 .38
JGX | 0 | 6.8 1.9 2.0 13 -24 22 -.14
JPL | 0 | 3.3 .1 1.8 -10 32 -34 .70
MIT | 0 | 7.0 -1.9 19.9 -6 -22 2 .22
NGS | 0 | 5.9 4.5 10.7 1 7 -30 .03
SIO | 0 | 4.2 4.0 2.8 -78 25 -101 -.08
COD | 1 | .3 -.9 .2 -5 9 -21 .08
EMR | 1 | 9.6 -6.3 1.9 0 -6 -6 -.12
ESA | 1 | .4 .0 .2 1 -19 -5 -.51
GFZ | 1 | .6 .4 .3 -19 7 4 .39
JGX | 1 | 6.9 .6 7.2 -21 -8 25 .18
JPL | 1 | 3.3 -3.5 1.2 -42 46 -52 .70
MIT | 1 | 6.0 -1.3 19.5 12 -7 -3 -.01
NGS | 1 | 5.8 7.1 6.1 10 9 -19 .06
SIO | 1 | 4.5 4.2 10.0 -57 9 -132 -.12
COD | 2 | .3 -.9 -.1 -10 9 -25 .07
EMR | 2 | 5.0 -1.9 -2.1 11 -19 21 -.08
ESA | 2 | .3 -.5 .1 -10 -19 -9 -.59
GFZ | 2 | -.2 -.4 .3 -31 7 -20 .51
JGX | 2 | 5.8 1.8 5.2 0 -36 26 -.04
JPL | 2 | 1.1 -1.3 -1.3 -4 59 -32 .92
MIT | 2 | 3.5 -.8 19.1 -12 -12 20 .10
NGS | 2 | 3.3 7.1 2.1 9 -6 -36 .03
SIO | 2 | 4.1 2.4 5.4 62 -45 -101 -.15
COD | 3 | .0 -.4 -.5 -19 20 -24 -.01
EMR | 3 | 5.0 .2 -.4 1 -11 5 -.03
ESA | 3 | .2 -.7 .1 -9 -15 -27 -.57
GFZ | 3 | .3 -.2 .4 -19 -3 -15 .43
JGX | 3 | 4.6 1.4 5.7 5 -13 39 -.01
JPL | 3 | .8 .4 1.7 -1 56 -50 1.02
MIT | 3 | 4.7 -.2 15.1 -19 -20 5 .17
NGS | 3 | 5.4 1.6 5.3 0 -3 -33 .17
SIO | 3 | 4.8 3.2 6.1 -53 -9 -67 -.09
COD | 4 | -.3 -.3 -.4 -15 13 -24 -.04
EMR | 4 | 9.9 1.9 2.4 7 -10 12 .19
ESA | 4 | .0 -.1 .0 1 -18 -17 -.42
GFZ | 4 | .0 -.4 .5 -21 -8 -8 .64
JGX | 4 | 4.1 .7 .4 26 -26 47 .17
JPL | 4 | 3.9 .7 6.9 5 48 -57 1.05
MIT | 4 | 6.5 1.9 14.8 -13 -30 -5 .14
NGS | 4 | 2.5 7.3 9.4 11 17 -34 .07
SIO | 4 | 4.6 2.3 -1.1 24 -50 23 .04
COD | 5 | -.3 -.6 -.8 -22 24 -19 .08
EMR | 5 | 11.6 -7.6 -.9 5 -9 8 -.18
ESA | 5 | -.2 -.1 .2 -4 -17 8 -.56
GFZ | 5 | -.4 -.6 .1 -14 -15 5 .40
JGX | 5 | 4.5 -4.5 8.1 1 -15 29 .06
JPL | 5 | 4.5 .5 6.0 11 37 -16 .68
MIT | 5 | 8.1 -1.9 16.2 -8 -25 15 -.08
NGS | 5 | 8.2 1.7 10.5 -12 -8 -26 -.02
SIO | 5 | 8.9 3.6 4.4 -22 -47 0 -.28
COD | 6 | -.1 -.7 -.9 -17 16 -11 .10
EMR | 6 | 10.2 1.7 3.3 0 2 6 .10
ESA | 6 | -.0 -.2 .2 0 -16 14 -.36
GFZ | 6 | .4 -.4 .4 -12 1 20 .63
JGX | 6 | 6.4 -1.1 9.9 0 -13 21 .10
JPL | 6 | 3.9 6.6 7.5 3 60 -30 1.01
MIT | 6 | 9.6 .2 14.1 -9 -18 10 .26
NGS | 6 | 7.5 7.0 10.7 22 3 -18 .11
SIO | 6 | 6.5 5.9 .8 43 -47 31 .08
9. 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.
10. 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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.atx
The JPL solution did not use IGS20/igs20.atx until GPS Week TBA, which caused
their orbit and clock residuals to be higher during that period than for the other
centres; from GPS Week 2238 through TBA, the JPL solution is excluded from the
weekly SINEX combination, as well as from orbit and clock combinations.
Since swithing to IGS20/igs20.atx, SIO orbits suffered from high Y rotations
with respect to the combined orbits, possibly impacting the alignment of the
combined orbits with respect to the IGS20 frame. As a result, SIO orbits are
excluded from the final combinations until the issue is fixed.
Since switching to IGS20/igs20.atx, EMR paused their participation to the IGS
combinations until they complete internal tests. They restarted submitting
products from GPS week 2263. The EMR orbit and clock solutions are excluded
from the final combinations until the IGS assessments are completed. The
EMR solutions are, however, included for comparison statistics only.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
were excluded from the final combinations (only for comparisons) until the IGS ACC
assessments completed. Starting from GPS week 2289, JGX solutions are included with
weight in the IGS final combinations.
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 1.2294.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2294.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 2.2294.[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 3.2294.[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 5.2294.0-6). 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 2294 summary. (Dec 24, 2023 - Dec 30, 2023)
Table 1.2294.a GPS week: 2294 MJD: 60302.000-60308.000
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 797| 0 0 2 -9 5 14 -.00 8 7 | -651 101 6 98
| 0 0 0 8 6 10 .02 | 192 362
emr 108| 0 0 0 0 -2 -6 .07 10 10 | 251 -2261 55 137
| 0 0 1 16 6 12 .02 | 955 2059
esa 150| 0 0 8 -14 1 -10 -.05 9 9 | -358 -735 6 82
| 0 0 1 10 9 13 .02 | 326 532
gfz 121| -1 1 3 16 11 -10 .07 9 9 | 55 -7 9 86
| 0 0 1 13 10 18 .02 | 197 287
grg 121| 1 -3 -6 0 30 -24 -.03 8 8 | -69 -53 6 128
| 0 0 1 7 4 16 .04 | 117 288
igr n/a| 0 0 0 0 12 8 .02 3 3 | 7887 286 9 86
| 0 0 0 12 7 14 .01 | 831 605
jgx n/a| 0 0 4 32 -18 -5 .03 10 10 | -3 -22 19 81
| 1 0 1 10 10 31 .01 | 112 292
jpl n/a| -1 0 0 11 12 -2 .16 24 24 | -114 51 74 158
| 0 0 1 17 14 12 .02 | 567 601
mit 367| 1 1 -8 -5 -16 28 -.00 7 7 | 1005 242 138 11673
| 0 0 1 35 11 44 .01 | 5708 273
ngs 281| 0 1 -1 2 -19 0 -.07 12 11 | -676 104 909 2008
| 0 0 2 12 16 20 .02 | 158 331
sio 334| 0 1 -9 23 -2 -31 -.00 10 9 | --- --- --- ---
| 0 0 1 11 15 68 .01 | --- ---
Table 1.2294.b GPS week : 2294 MJD: 60302.000-60308.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 4 4 4 4 4 4 |
2 | 3 4 4 4 4 3 4 |
3 | 4 4 4 4 4 4 4 |
4 | 4 4 4 3 4 4 3 |
5 | 4 4 4 4 3 3 3 |
6 | 3 3 3 3 3 3 3 |
7 | 3 3 3 3 3 3 3 |
8 | 4 4 3 4 5 4 4 |
9 | 3 3 3 3 3 4 3 |
10 | 4 4 4 4 4 4 4 |
11 | 4 4 4 4 3 3 3 |
12 | 4 4 5 4 4 4 4 |
13 | 3 3 4 3 4 3 3 |
14 | 3 4 3 3 3 4 3 |
15 | 3 4 4 3 4 4 3 |
16 | 4 4 4 4 4 4 4 |
17 | 3 4 3 4 3 3 4 |
18 | 4 4 4 4 3 4 3 |
19 | 4 4 5 4 4 4 4 |
20 | 3 4 4 4 4 4 3 |
21 | 3 3 4 4 3 3 3 |
22 | 3 3 3 3 3 3 3 |
23 | 5 5 5 5 5 5 4 |
24 | 4 4 4 4 4 4 3 |
25 | 3 3 3 3 3 3 3 |
26 | 3 4 3 3 3 3 3 |
27 | 4 4 4 4 4 4 21 |
28 | 4 4 4 4 4 4 4 |
29 | 4 4 4 4 4 5 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 3 3 3 3 3 |
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 2.2294.0 GPS week: 2294 Day: 0 MJD: 60302.000
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 801| 0 0 3 -4 8 14 .03 8 7 | -917 759 6 104
emr 108| 0 0 0 -11 -10 0 .04 10 10 | 559 -3707 53 128
esa 150| 0 -1 6 -23 12 -8 -.08 9 9 | -401 -357 6 75
gfz 120| -1 1 5 -3 22 -11 .04 8 8 | -300 409 9 83
grg 123| 1 -3 -5 -2 33 -10 .01 9 8 | -77 -215 7 122
igr n/a| 0 0 0 -15 14 8 .01 3 3 | 7004 -221 10 90
jgx n/a| -2 0 3 28 -18 -52 .02 12 12 | -78 168 18 72
jpl n/a| -1 -1 -1 -7 3 5 .15 25 25 | -252 -334 74 149
mit 367| 2 0 -9 26 -23 17 .00 8 7 | -4083 507 533 12308
ngs 286| 0 1 -1 8 -41 23 -.05 10 9 | -942 710 1023 2112
sio 343| 1 0 -10 19 21 -48 .00 11 11 | --- --- --- ---
Table 2.2294.1 GPS week: 2294 Day: 1 MJD: 60303.000
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 805| -1 0 2 0 3 30 -.02 7 7 | -283 -437 6 90
emr 110| 0 -2 0 -22 -9 6 .07 11 11 | -1562 1227 66 144
esa 150| 0 0 8 -17 -6 -6 -.05 9 9 | -93 -1224 6 88
gfz 122| -1 2 5 9 27 5 .08 9 9 | 8 -68 9 70
grg 120| 0 -3 -7 -10 24 -5 -.02 8 7 | 80 -405 7 130
igr n/a| 0 0 0 -6 13 21 .02 3 3 | 6448 1375 9 96
jgx n/a| 0 0 5 14 -14 -17 .04 11 11 | 178 -523 21 90
jpl n/a| -1 -1 0 -15 15 7 .15 25 25 | -797 1150 75 169
mit 367| 1 1 -10 29 -28 -20 -.02 9 8 | -681 537 58 13819
ngs 287| 0 2 -3 0 -14 27 -.06 12 11 | -450 -211 851 1933
sio 342| 1 2 -10 10 -7 -110 .00 11 10 | --- --- --- ---
Table 2.2294.2 GPS week: 2294 Day: 2 MJD: 60304.000
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 805| 0 0 2 -20 10 18 .01 8 8 | -599 -30 6 104
emr 108| 0 0 0 17 -5 -4 .11 11 11 | 499 -2796 42 121
esa 150| 0 -1 10 -8 -9 -8 -.04 9 9 | 102 -986 6 108
gfz 123| -1 2 3 25 15 -18 .07 9 8 | 260 381 9 99
grg 120| 1 -3 -7 9 29 -8 -.07 8 7 | -171 359 6 125
igr n/a| 0 0 1 19 1 9 .02 3 3 | 8065 743 9 96
jgx n/a| 0 0 5 37 -39 -26 .04 10 10 | -133 291 19 84
jpl n/a| -1 0 -1 31 15 -1 .21 25 25 | 650 388 78 164
mit 367| 0 1 -9 -47 2 44 -.01 8 7 | -5426 391 125 14309
ngs 285| -1 2 -4 26 -28 -15 -.05 12 11 | -531 -292 742 1802
sio 333| 0 1 -11 46 4 -115 -.02 11 10 | --- --- --- ---
Table 2.2294.3 GPS week: 2294 Day: 3 MJD: 60305.000
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 796| 0 0 1 2 -1 0 .00 8 7 | -663 245 6 100
emr 107| 0 -1 2 -13 1 -11 .08 10 10 | 871 -3393 40 137
esa 150| 0 0 9 -30 13 -31 -.03 10 10 | -355 220 6 84
gfz 122| 0 1 2 12 1 -20 .09 11 11 | 261 -64 10 98
grg 121| 0 -2 -8 0 31 -46 -.11 8 8 | -148 226 6 139
igr n/a| 0 0 1 -3 25 7 .04 3 3 | 8564 -74 9 89
jgx n/a| -1 0 5 37 -7 0 .04 10 10 | 53 214 17 85
jpl n/a| 0 0 0 13 36 -7 .14 25 25 | 668 -601 75 163
mit 367| 1 1 -6 10 -27 86 -.00 7 7 | 8529 95 75 7017
ngs 282| 0 0 0 2 1 -18 -.09 13 11 | -665 250 1078 2113
sio 336| 0 2 -8 20 10 -39 .02 9 9 | --- --- --- ---
Table 2.2294.4 GPS week: 2294 Day: 4 MJD: 60306.000
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 792| 0 0 2 -18 -3 4 -.01 9 8 | -645 -15 5 92
emr 106| 1 0 1 17 7 5 .08 10 10 | 473 -3249 56 146
esa 150| 0 0 7 -5 8 -9 -.05 9 9 | -389 -1166 6 76
gfz 121| -1 1 3 25 0 17 .08 8 8 | -46 -174 9 87
grg 122| 1 -3 -7 11 26 -35 -.04 9 9 | -217 105 6 126
igr n/a| 0 0 0 7 12 15 .03 3 3 | 8174 306 9 73
jgx n/a| 0 0 3 49 -9 11 .03 10 10 | 51 -191 15 78
jpl n/a| -1 0 1 17 16 -17 .14 24 24 | -250 40 75 163
mit 367| 1 0 -7 -41 -17 3 -.01 7 6 | -1182 108 59 14947
ngs 281| -1 0 1 -6 -2 5 -.07 13 12 | -690 67 1002 2263
sio 333| 0 1 -9 18 -8 72 -.00 9 9 | --- --- --- ---
Table 2.2294.5 GPS week: 2294 Day: 5 MJD: 60307.000
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 791| -1 0 2 -12 6 22 -.00 8 7 | -693 13 6 99
emr 108| 0 0 -1 -7 -3 -8 .07 10 10 | 1332 -4012 70 138
esa 150| 0 0 8 -17 -1 11 -.03 9 8 | -422 -1086 6 76
gfz 121| -1 1 3 10 5 -3 .08 9 9 | 158 -305 9 77
grg 121| 0 -2 -5 -6 33 -24 -.01 9 8 | 71 -323 7 131
igr n/a| 0 0 0 -13 10 17 .02 3 3 | 8596 -358 10 81
jgx n/a| 0 0 5 29 -24 48 .01 10 10 | 27 -201 21 83
jpl n/a| -1 0 1 16 -11 13 .15 24 24 | -233 -462 72 146
mit 367| 1 1 -8 24 -9 -16 -.00 7 7 | 878 -234 57 10752
ngs 278| 0 0 0 -6 -13 -27 -.10 12 10 | -697 20 815 1804
sio 327| 1 2 -10 25 -10 12 .01 9 9 | --- --- --- ---
Table 2.2294.6 GPS week: 2294 Day: 6 MJD: 60308.000
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 791| -1 1 3 -10 12 12 -.02 7 7 | -758 178 7 101
emr 110| 0 0 3 14 -1 -29 .07 9 9 | -410 102 59 151
esa 150| 0 0 6 -1 -6 -23 -.08 9 9 | -951 -546 6 73
gfz 120| -2 0 1 37 9 -39 .04 8 9 | 46 -228 9 89
grg 120| 1 -3 -6 1 36 -39 -.00 9 8 | -22 -123 7 125
igr n/a| 0 0 0 8 13 -23 .01 3 3 | 8361 234 12 81
jgx n/a| 1 -1 5 31 -17 0 .02 10 10 | -119 88 22 80
jpl n/a| -2 -1 2 28 14 -20 .16 24 24 | -585 177 74 157
mit 367| 1 1 -8 -40 -12 82 .00 7 6 | 9006 292 61 8559
ngs 269| -1 2 0 -7 -35 0 -.05 11 10 | -759 185 853 2029
sio 324| 1 1 -7 22 -24 9 -.02 9 9 | --- --- --- ---
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 3.2294.0 GPS week: 2294 Day: 0 MJD: 60302.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 7 8 9 11 4 3 --- 7 8 9 --- 3 | 69 68 68 65 68 67 --- 66 69 66 --- 67
2 | 8 8 6 10 10 2 9 9 7 7 9 3 | 68 66 67 68 67 67 69 67 68 68 68 67
3E | 5 11 12 9 11 3 15 11 8 13 11 4 | 57 57 57 58 58 58 58 57 57 56 59 56
4 | 9 11 11 6 6 3 10 54 9 9 9 3 | 75 75 75 74 76 75 77 86 78 73 75 75
5E | 9 12 9 10 7 3 12 17 8 8 15 3 | 81 83 81 84 83 82 79 83 79 80 80 81
6 | 7 9 9 5 4 2 11 8 5 11 10 3 | 73 74 74 72 71 72 72 72 70 72 71 72
7 | 6 10 6 6 8 2 13 9 7 9 12 3 | 64 66 64 62 63 63 65 65 64 64 64 63
8E | 11 11 8 7 6 4 12 10 8 10 10 3 | 50 52 52 51 54 51 52 53 52 50 56 51
9 | 7 8 12 8 6 2 8 7 7 7 10 3 | 59 58 58 57 56 58 61 59 56 55 55 57
10E | 7 11 11 12 7 4 13 9 9 11 11 3 | 67 65 66 66 65 66 70 63 66 67 67 66
11 | 9 13 9 5 6 3 12 59 8 9 11 3 | 83 84 83 84 82 83 83 83 83 82 83 82
12 | 7 10 8 10 14 3 20 9 9 9 12 4 | 45 44 42 49 40 44 47 48 47 47 47 44
13 | 8 12 8 7 6 2 14 13 5 10 10 3 | 43 48 42 43 41 44 44 47 44 44 42 43
14 | 6 7 13 7 7 3 11 56 7 12 11 3 | 45 42 50 46 49 46 45 70 48 44 55 46
15 | 7 9 6 10 9 4 13 8 5 10 13 3 | 70 69 71 71 67 70 70 70 67 74 63 69
16 | 6 8 8 10 10 5 16 9 9 9 11 3 | 44 44 43 44 41 43 47 44 45 46 49 43
17E | 6 11 9 8 7 4 11 12 5 9 7 3 | 72 74 73 71 71 71 74 75 74 71 76 72
18 | 9 10 11 8 7 3 10 52 7 11 9 3 | 81 84 81 84 81 82 82 80 81 78 81 81
19 | 8 11 8 11 18 4 12 8 6 8 9 4 | 83 88 88 86 78 85 87 86 85 82 89 84
20E | 10 9 7 4 6 4 11 9 6 11 9 3 | 98 96 93 95 99 95 96 96 99 96 96 96
21 | 8 8 7 9 9 3 11 9 7 8 12 3 | 68 66 67 70 68 68 70 67 70 69 70 68
22 | 6 7 7 8 7 3 9 9 6 9 11 2 | 49 48 48 49 49 48 48 49 47 49 50 48
23E | 9 10 20 7 9 3 12 59 13 14 14 4 | 76 76 75 79 76 76 80 71 77 71 75 75
24 | 5 16 8 9 8 2 11 17 7 10 10 3 | 65 69 64 66 65 65 66 68 68 67 66 65
25 | 7 7 10 9 6 2 11 9 8 9 11 3 | 46 48 46 48 44 46 46 51 49 49 49 46
26 | 6 8 10 8 7 3 9 6 10 9 13 3 | 43 45 44 44 41 43 49 45 46 45 48 44
27E | 11 10 7 10 7 4 13 10 7 13 9 3 | 105 51 53 58 54 55 54 50 51 54 56 53
X28 | 7 17 5 --- 10 3 12 52 10 6 14 4 | 69 72 67 --- 68 68 68 74 67 68 67 68
29E | 9 9 11 7 15 4 17 9 8 14 12 4 | 56 58 58 60 55 58 58 60 56 59 61 57
30 | 7 13 7 5 6 4 8 14 6 7 10 3 | 64 66 64 62 64 63 64 65 62 64 64 63
31 | 6 9 5 6 5 3 14 9 10 9 14 3 | 66 69 66 69 66 66 68 69 69 69 68 67
32 | 6 8 9 7 5 2 10 8 8 9 9 3 | 55 54 54 54 52 53 57 54 50 51 51 53
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 10 9 8 9 3 12 25 8 10 11 |T 65 64 63 64 62 63 64 65 63 63 64 63
WRMS | 7 10 9 8 8 3 12 25 7 9 11 |NE 61 61 60 61 59 60 61 63 61 61 61 60
MEDI | 7 10 8 8 7 3 12 9 7 9 11 |MD 66 66 64 65 65 65 66 66 66 66 64 65
Table 3.2294.1 GPS week: 2294 Day: 1 MJD: 60303.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 7 9 8 9 5 4 --- 10 7 14 --- 3 | 29 29 29 26 28 28 --- 29 25 26 --- 27
2 | 10 8 6 11 8 4 7 8 7 13 9 3 | 27 27 27 31 28 29 30 28 27 29 30 27
3E | 3 10 11 9 8 4 14 11 8 11 12 3 | 37 38 42 37 38 38 38 38 35 36 39 37
4 | 7 9 11 8 7 3 9 53 10 14 9 3 | 57 59 60 58 60 59 59 68 61 55 60 58
5E | 8 11 11 10 6 4 11 15 10 12 14 3 | 42 40 44 42 41 41 43 41 41 45 40 42
6 | 6 8 8 7 4 2 9 8 8 13 8 3 | 34 36 34 33 32 33 32 36 31 38 31 33
7 | 6 10 4 10 8 3 10 8 10 10 10 3 | 30 33 30 34 29 31 31 32 26 30 25 29
8E | 9 13 8 9 5 3 10 13 7 13 9 3 | 39 42 42 37 37 40 42 41 39 36 39 38
9 | 5 10 9 10 5 4 8 11 7 10 9 3 | 47 48 47 46 47 47 48 52 44 45 44 46
10E | 9 13 10 9 7 3 12 10 10 15 11 4 | 28 28 32 32 31 29 29 27 27 29 29 28
11 | 8 10 11 7 7 3 9 59 8 14 11 3 | 40 43 41 43 42 42 40 43 41 43 42 41
12 | 7 11 6 9 12 3 18 9 9 12 13 4 | 44 40 39 44 43 41 44 43 40 46 41 41
13 | 5 11 8 10 6 4 10 11 6 9 10 3 | 38 43 36 39 38 38 37 43 36 37 38 37
14 | 8 9 13 6 7 3 10 55 10 14 9 3 | 52 51 52 49 52 51 48 64 51 48 55 50
15 | 8 8 7 11 9 3 11 9 7 13 10 3 | 53 53 53 52 55 54 53 55 50 58 51 53
16 | 6 12 6 13 10 4 15 9 8 16 10 4 | 45 44 44 44 44 42 47 44 43 47 43 43
17E | 8 14 10 10 7 3 9 15 7 9 8 3 | 54 52 48 55 52 52 51 51 50 53 53 51
18 | 8 11 10 7 7 3 10 51 9 15 11 3 | 38 41 37 40 40 39 41 40 38 38 37 38
19 | 10 11 8 13 10 6 10 10 9 10 12 4 | 103 97 99 99 99 97 100 98 98 101 93 99
20E | 7 11 9 10 9 5 7 10 10 15 12 3 | 73 71 69 71 74 70 69 71 73 74 71 71
21 | 9 8 5 9 7 3 10 7 6 11 9 3 | 26 27 26 29 26 27 29 26 26 30 28 26
22 | 5 8 6 8 7 3 9 10 8 10 8 2 | 47 49 45 48 46 47 47 49 45 48 46 46
23E | 9 11 20 7 9 3 12 59 12 15 15 4 | 23 26 36 27 29 26 27 35 27 26 28 26
24 | 5 16 8 10 7 4 10 17 11 12 11 3 | 34 45 35 32 35 35 35 46 34 30 32 34
25 | 8 9 10 6 5 3 10 11 7 11 11 3 | 43 43 43 42 42 41 41 45 41 45 43 42
26 | 5 10 8 10 8 3 11 8 7 13 9 3 | 42 43 40 39 39 38 44 43 38 39 40 39
27E | 11 12 6 7 5 4 11 12 10 14 7 3 | 106 36 35 41 36 37 36 35 30 33 35 33
X28 | 4 18 6 --- 9 3 11 54 7 8 14 4 | 33 31 33 --- 36 33 36 34 30 30 33 32
29E | 7 12 9 7 13 5 14 11 10 13 15 4 | 69 71 68 69 67 70 69 69 67 71 70 68
30 | 7 11 6 8 7 2 8 11 8 10 11 3 | 28 40 31 33 28 31 29 40 24 32 26 29
31 | 4 8 7 7 5 3 9 8 7 8 13 2 | 34 39 32 31 35 34 37 40 31 33 32 33
32 | 6 9 9 8 5 2 9 9 8 11 11 3 | 50 50 50 48 49 48 49 51 44 45 48 47
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 11 9 9 8 3 11 25 9 12 11 |T 45 44 43 43 43 42 43 45 41 43 42 42
WRMS | 7 11 9 9 7 3 11 25 8 11 10 |NE 39 41 39 40 39 39 40 43 37 39 39 38
MEDI | 7 10 8 9 7 3 10 11 8 12 11 |MD 40 42 40 41 39 39 41 43 38 38 40 38
Table 3.2294.2 GPS week: 2294 Day: 2 MJD: 60304.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 8 9 7 10 6 3 --- 9 6 15 --- 3 | 88 87 89 87 86 86 --- 84 89 86 --- 87
2 | 8 8 7 11 11 3 7 10 6 16 12 3 | 88 85 89 90 87 88 89 86 87 84 86 87
3E | 6 11 11 8 7 3 12 12 7 12 11 3 | 88 87 90 86 86 86 87 89 89 82 87 87
4 | 8 10 11 8 9 4 8 53 8 11 11 3 | 113 109 112 111 114 111 111 116 114 111 112 112
5E | 8 12 11 8 7 3 10 14 10 13 11 3 | 89 87 89 90 88 88 89 87 87 88 85 88
6 | 6 10 9 11 6 3 8 8 6 10 8 3 | 93 91 92 87 91 90 91 90 91 89 90 91
7 | 7 10 6 6 7 3 11 7 10 12 10 3 | 88 88 87 88 87 87 88 87 87 90 84 88
8E | 11 12 7 5 6 4 12 12 6 8 10 3 | 88 88 92 91 90 90 92 90 89 88 88 89
9 | 7 11 9 7 7 4 7 8 7 9 11 3 | 106 104 105 104 106 104 103 105 106 104 104 105
10E | 9 13 10 10 9 3 9 8 9 11 13 3 | 81 78 80 81 81 81 80 80 80 82 80 80
11 | 7 11 10 9 7 3 8 59 6 13 9 3 | 92 90 91 89 91 90 90 91 91 87 89 90
12 | 8 11 7 8 14 3 19 10 11 14 13 4 | 90 89 89 91 92 90 90 91 89 93 87 90
13 | 9 12 8 10 7 4 9 11 6 12 11 3 | 90 94 90 91 91 90 89 92 91 92 86 90
14 | 8 9 12 5 8 3 10 56 6 9 11 3 | 95 97 99 98 100 97 96 107 99 96 98 97
15 | 8 8 6 10 10 3 11 7 9 15 9 3 | 106 104 107 106 105 106 104 105 105 109 99 105
16 | 7 11 6 10 8 4 16 9 8 15 12 3 | 98 95 96 98 98 96 97 99 97 98 96 97
17E | 10 13 10 6 5 3 9 13 6 8 7 3 | 106 105 105 106 106 105 106 106 107 105 106 106
18 | 10 11 10 7 7 3 10 53 7 16 11 3 | 90 92 93 93 92 92 92 93 92 91 91 91
19E | 12 13 11 18 8 4 11 11 9 9 9 4 | 99 100 102 99 101 100 102 101 103 101 102 100
20E | 9 11 10 7 11 6 8 9 13 13 11 4 | 111 112 109 110 112 110 111 109 110 111 109 111
21 | 7 7 6 11 10 3 10 8 6 14 10 3 | 87 84 87 88 85 86 88 86 86 83 86 86
22 | 5 10 8 6 7 3 9 10 6 7 11 2 | 101 101 102 102 103 102 102 103 104 101 102 102
23E | 11 10 21 7 11 2 9 60 11 18 14 5 | 76 75 81 79 76 78 77 80 78 75 76 76
24 | 7 16 7 9 7 3 9 18 10 13 10 3 | 90 94 91 91 92 91 92 97 92 90 88 91
25 | 6 8 10 9 8 1 8 9 7 11 11 3 | 97 99 98 102 97 98 97 99 99 99 95 98
26 | 8 9 9 8 6 3 7 8 7 10 10 3 | 93 91 92 94 93 92 91 93 93 92 90 92
27E | 12 14 6 7 6 3 11 11 10 14 14 3 | 101 79 80 84 84 83 77 79 81 80 78 82
X28 | 5 18 7 --- 4 3 10 53 6 9 12 3 | 95 92 95 --- 97 94 93 95 96 95 93 95
29E | 10 12 10 7 11 5 15 10 11 15 12 4 | 97 99 100 100 98 99 98 99 98 100 97 99
30 | 8 14 8 5 6 3 6 12 6 8 9 3 | 89 92 88 87 88 88 88 92 88 89 85 88
31 | 6 10 6 9 4 2 9 10 6 9 8 2 | 94 92 91 93 94 92 92 95 94 95 91 93
32 | 6 7 9 6 5 2 8 9 7 6 9 2 | 105 102 104 106 104 104 101 104 102 106 102 104
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 11 9 9 8 3 10 25 8 12 11 |T 94 93 94 94 94 93 93 94 94 93 92 93
WRMS | 8 11 9 8 7 3 10 25 7 10 10 |NE 94 94 94 95 95 94 94 95 95 94 93 94
MEDI | 8 11 9 8 7 3 9 10 7 12 11 |MD 93 92 92 91 92 91 92 93 92 92 90 91
Table 3.2294.3 GPS week: 2294 Day: 3 MJD: 60305.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 9 10 10 11 6 4 --- 10 5 18 --- 4 | 34 36 35 40 33 35 --- 38 36 38 --- 35
2 | 9 8 7 10 10 2 6 10 7 17 9 3 | 31 34 35 37 31 33 33 35 37 36 36 33
3E | 7 12 12 9 7 2 12 13 8 16 12 3 | 36 37 40 34 34 36 38 38 37 41 38 36
4 | 8 8 11 7 7 3 7 51 6 13 10 3 | 30 32 31 33 33 31 29 49 33 34 33 31
5E | 9 12 10 8 8 3 8 16 7 12 10 3 | 37 34 38 38 35 37 36 37 42 38 40 36
6 | 6 9 8 11 6 2 9 8 6 8 11 3 | 33 34 35 33 30 32 32 34 34 31 35 32
7 | 5 7 6 8 8 4 8 8 6 11 7 2 | 33 32 32 37 31 34 34 33 34 33 33 32
8E | 11 12 9 15 9 4 15 11 6 16 8 4 | 30 32 34 29 28 31 32 34 34 29 30 30
9 | 6 9 9 8 6 3 6 7 7 11 11 3 | 34 34 34 33 29 33 32 35 32 30 30 31
10E | 6 14 10 18 7 4 8 9 8 14 11 4 | 36 34 37 32 34 34 33 35 39 39 37 34
11 | 9 11 10 7 7 3 9 59 7 15 10 3 | 29 31 31 31 30 29 29 31 34 30 33 30
12 | 6 10 6 9 13 3 17 9 7 12 7 4 | 36 36 37 38 38 35 37 36 37 36 36 36
13 | 8 12 8 12 6 3 7 12 6 9 10 3 | 31 36 31 35 32 32 30 39 36 29 32 32
14 | 8 7 14 8 8 4 7 59 7 10 7 3 | 40 37 42 44 41 41 37 62 43 38 42 40
15 | 7 9 6 13 7 4 9 8 6 13 8 3 | 39 37 40 39 37 39 38 40 38 41 37 38
16 | 5 9 7 7 10 4 15 9 8 17 10 3 | 33 32 33 33 32 32 33 33 35 35 36 32
17E | 13 9 12 9 6 4 9 9 5 13 9 3 | 51 50 49 51 49 49 47 51 49 50 51 49
18 | 8 10 10 9 8 4 7 50 7 14 8 3 | 31 33 35 36 34 34 33 38 36 32 34 33
19E | 12 12 11 17 8 3 11 10 8 9 13 4 | 40 41 39 40 39 40 40 42 42 39 43 39
20 | 11 11 8 12 11 4 8 11 9 10 10 4 | 51 50 51 53 51 51 50 49 55 49 51 50
21 | 9 8 7 8 9 3 9 8 6 17 8 3 | 32 36 35 38 32 34 35 37 36 38 34 34
22 | 7 8 9 9 7 4 7 9 5 8 6 2 | 32 34 31 36 30 33 33 34 34 31 34 32
23E | 10 9 22 13 11 4 9 59 9 17 8 4 | 33 34 43 37 40 36 36 42 39 40 37 36
24 | 4 18 8 13 8 2 6 18 7 11 6 3 | 34 44 36 31 32 34 32 45 37 31 37 34
25 | 9 7 10 12 7 3 7 11 6 13 7 3 | 34 34 35 36 33 32 31 34 34 32 32 32
26 | 6 6 8 10 7 2 7 10 6 14 8 3 | 33 34 34 33 31 32 31 33 32 32 31 31
27E | 9 11 6 11 9 4 12 12 8 15 9 3 | 92 30 31 38 29 33 29 34 33 32 32 32
X28 | 5 19 6 --- 5 3 9 50 8 9 14 3 | 27 27 28 --- 25 26 29 31 30 28 31 27
29E | 10 10 10 10 12 4 13 9 9 14 13 4 | 36 36 38 35 36 36 35 35 38 40 37 36
30 | 5 14 8 7 8 3 6 14 5 7 8 3 | 31 41 34 34 31 33 31 42 32 33 31 32
31 | 4 9 6 11 5 2 11 10 7 10 10 3 | 33 34 33 33 29 33 35 36 31 33 32 32
32 | 4 7 8 10 5 3 8 9 7 9 8 2 | 32 34 34 31 29 31 30 34 32 30 30 31
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 10 10 11 8 3 10 25 7 13 9 |T 36 35 35 36 33 34 34 38 36 35 35 34
WRMS | 7 10 10 11 8 3 10 25 7 11 9 |NE 32 34 34 35 31 33 32 37 34 33 33 32
MEDI | 8 9 8 10 7 3 8 10 7 13 9 |MD 33 34 35 36 32 33 33 36 36 33 34 32
Table 3.2294.4 GPS week: 2294 Day: 4 MJD: 60306.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 8 11 7 12 9 3 --- 10 5 12 --- 3 | 49 46 47 50 47 47 --- 50 50 49 --- 48
2 | 8 8 6 11 11 3 7 10 9 20 7 3 | 48 49 49 51 50 50 51 49 52 51 48 50
3E | 6 11 10 10 9 5 9 11 5 16 10 3 | 47 46 49 43 45 45 47 45 46 44 43 45
4 | 9 9 10 9 6 4 7 51 8 16 9 3 | 82 81 81 80 83 80 82 87 84 77 80 81
5E | 6 12 10 6 8 4 8 15 7 13 8 3 | 39 36 39 37 40 38 40 39 38 42 37 38
6 | 7 9 11 10 6 2 7 7 6 11 8 3 | 54 55 55 53 54 54 55 55 55 52 54 54
7 | 7 9 5 3 10 3 11 10 6 13 7 3 | 49 50 48 48 48 48 53 50 49 45 45 48
8E | 19 11 8 8 9 4 13 9 7 13 7 4 | 50 50 51 50 49 51 53 50 53 50 48 50
9 | 8 9 9 6 7 4 5 9 7 14 15 3 | 71 68 70 66 69 68 69 69 69 65 65 68
10E | 8 13 10 14 8 3 10 11 6 13 10 3 | 39 39 40 37 41 38 38 39 38 40 39 38
11 | 9 11 11 7 7 2 8 60 6 12 9 3 | 54 54 56 55 57 55 57 57 58 54 54 56
12 | 8 12 7 9 13 3 16 10 9 9 9 4 | 49 45 47 48 51 47 49 49 49 49 46 48
13 | 10 12 8 9 9 3 8 11 5 11 7 3 | 53 55 49 46 51 50 51 53 53 50 49 50
14 | 9 9 11 6 7 3 8 53 6 13 10 3 | 52 53 53 52 54 53 53 64 54 50 56 52
15 | 9 11 5 11 10 2 9 9 7 10 13 3 | 70 68 68 66 69 68 69 70 69 71 63 68
16 | 5 10 7 7 9 4 14 9 6 17 13 3 | 55 53 54 51 56 52 56 55 54 52 50 53
17E | 8 9 10 9 6 2 10 9 5 13 7 3 | 67 62 61 65 65 63 64 63 64 63 64 63
18 | 9 10 10 6 8 2 8 52 6 14 10 3 | 53 54 53 52 55 54 54 55 55 51 52 53
19E | 13 10 8 10 7 2 10 8 8 14 9 3 | 62 61 61 61 63 62 63 61 62 61 63 62
20 | 8 10 7 10 20 4 7 9 9 12 10 4 | 79 77 78 78 79 78 79 78 82 79 77 78
21 | 6 7 5 10 10 3 10 10 6 16 8 3 | 47 48 48 49 48 48 51 48 50 48 46 48
22 | 7 8 6 7 8 3 10 9 5 11 8 3 | 62 63 60 63 61 62 65 62 63 59 63 62
23E | 10 11 20 7 10 3 6 62 7 16 11 4 | 37 40 46 41 41 40 39 49 40 43 40 40
24 | 7 16 7 11 7 2 7 17 5 10 12 3 | 58 67 60 55 60 59 57 66 62 56 53 59
25 | 8 8 10 8 7 3 8 9 6 9 7 3 | 55 59 57 57 57 57 56 59 58 55 54 56
26 | 6 7 9 5 10 3 6 10 5 11 9 2 | 52 52 52 49 54 50 52 55 50 47 48 51
27E | 9 11 5 7 6 2 13 8 9 14 11 3 | 114 49 48 45 46 44 48 49 47 48 52 48
X28 | 5 18 7 --- 9 2 9 51 5 8 7 3 | 61 60 61 --- 63 60 62 63 60 57 57 60
29E | 8 10 9 8 11 2 16 7 8 10 10 4 | 70 69 68 68 69 69 68 68 71 68 67 69
30 | 8 14 7 6 8 2 7 14 5 7 6 3 | 49 57 52 51 49 51 52 58 50 47 49 50
31 | 5 7 5 5 6 2 10 9 7 10 10 2 | 59 61 58 56 59 58 60 62 58 54 56 58
32 | 6 7 9 8 6 2 7 11 5 8 7 2 | 66 66 65 66 65 65 64 68 64 64 63 65
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 9 10 9 8 9 3 10 24 7 13 9 |T 57 56 55 54 56 55 56 57 56 54 54 55
WRMS | 8 10 9 8 9 3 10 24 6 12 9 |NE 56 57 56 55 57 56 58 59 57 54 54 56
MEDI | 8 10 8 8 8 3 8 10 6 12 9 |MD 54 54 53 52 54 53 55 55 54 51 53 53
Table 3.2294.5 GPS week: 2294 Day: 5 MJD: 60307.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 11 8 7 9 7 4 --- 10 5 14 --- 3 | 31 32 32 34 29 32 --- 33 33 34 --- 31
2 | 9 7 4 10 10 4 7 11 8 11 9 3 | 31 33 33 38 33 34 32 34 36 32 34 33
3E | 7 11 11 8 9 4 10 11 7 14 9 3 | 39 41 42 38 36 36 37 39 41 36 39 38
4 | 8 9 11 7 5 4 10 53 9 15 11 3 | 57 58 60 62 61 59 57 66 65 58 65 59
5E | 8 12 8 11 6 3 10 14 6 10 9 3 | 34 33 34 35 34 34 33 31 36 36 36 34
6 | 10 8 8 8 6 2 8 9 6 10 8 3 | 36 37 35 33 35 33 33 37 35 34 33 34
7 | 4 9 5 6 8 3 7 6 6 10 7 2 | 33 35 33 37 34 34 33 36 38 34 35 34
8E | 11 10 8 8 6 4 14 9 7 16 9 3 | 40 43 44 45 41 43 42 45 44 41 41 42
9 | 7 8 9 7 5 3 8 9 9 17 10 3 | 54 56 54 56 55 55 51 58 60 57 57 55
10E | 7 13 8 14 4 3 8 9 9 12 8 3 | 29 28 30 26 30 28 25 30 32 31 27 28
11 | 10 10 9 6 6 2 9 58 6 13 9 3 | 38 41 38 38 41 38 39 39 44 37 43 39
12 | 7 9 8 9 14 3 18 10 9 11 12 4 | 45 45 46 46 48 44 46 46 45 50 45 45
13 | 6 9 8 10 7 2 11 10 9 10 9 3 | 40 46 42 47 44 42 39 47 49 46 44 43
14 | 10 9 9 6 8 2 8 54 9 12 9 3 | 52 54 53 55 57 54 50 66 58 53 56 54
15 | 8 8 5 12 10 3 9 7 6 12 8 3 | 56 53 55 54 57 55 53 56 58 58 56 55
16 | 5 10 6 10 9 4 15 8 8 14 9 3 | 49 47 50 52 50 49 48 50 53 52 49 49
17E | 10 11 9 7 5 3 9 11 6 10 7 3 | 53 52 47 53 51 51 48 52 51 50 52 50
18 | 7 10 9 8 9 2 11 48 6 13 7 3 | 42 45 44 43 46 43 46 43 48 41 43 44
19E | 13 10 8 13 6 3 11 9 9 12 11 4 | 48 49 49 46 51 48 48 51 53 49 49 49
20 | 8 8 6 10 15 4 8 10 9 10 9 3 | 69 69 69 70 74 68 69 66 77 67 74 70
21 | 7 6 5 11 8 3 7 9 5 10 10 2 | 29 33 32 37 31 32 32 35 33 29 28 31
22 | 8 8 7 8 6 3 9 9 8 8 12 3 | 52 56 51 55 54 53 51 55 58 53 53 53
23E | 9 12 19 8 12 3 10 59 7 15 9 4 | 27 30 39 31 34 32 30 40 33 30 31 31
24 | 4 15 7 19 7 3 7 16 5 8 6 3 | 36 49 42 32 39 38 37 49 41 37 39 38
25 | 6 7 9 8 7 3 7 10 6 9 9 3 | 46 48 50 48 49 47 46 49 50 48 46 48
26 | 4 6 8 9 9 3 9 8 7 10 10 3 | 43 43 43 42 43 41 39 45 44 43 41 42
27E | 8 11 6 10 5 3 13 9 8 13 6 3 | 178 47 47 53 41 40 44 49 40 38 45 39
X28 | 3 19 6 --- 6 2 8 50 5 7 8 3 | 40 37 42 --- 43 40 40 39 44 41 41 40
29E | 8 11 11 7 21 6 16 9 10 13 10 5 | 72 73 74 73 74 73 73 73 74 76 73 73
30 | 7 14 7 7 6 3 7 12 6 9 8 3 | 31 43 33 39 34 33 31 44 38 33 33 34
31 | 4 7 5 6 4 2 9 9 7 8 8 2 | 31 35 31 31 32 32 31 37 31 33 29 31
32 | 6 7 7 7 7 2 9 9 5 6 7 2 | 54 52 53 53 53 52 49 55 53 52 51 52
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 10 9 9 9 3 10 24 7 12 9 |T 47 45 44 45 44 43 42 46 46 44 44 43
WRMS | 7 10 8 9 8 3 10 24 7 10 9 |NE 42 44 43 44 44 42 42 46 46 43 43 42
MEDI | 7 9 8 8 7 3 9 10 7 11 9 |MD 40 45 43 45 43 41 42 45 44 41 43 42
Table 3.2294.6 GPS week: 2294 Day: 6 MJD: 60308.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 8 9 8 11 7 3 --- 10 7 15 --- 3 | 30 31 31 30 28 30 --- 30 29 32 --- 29
2 | 6 8 6 9 12 2 8 10 11 13 8 3 | 32 33 34 36 34 34 34 33 36 33 34 33
3E | 5 12 11 13 8 4 10 10 7 9 9 3 | 38 40 41 33 35 37 39 41 37 40 41 36
4 | 9 7 13 8 8 4 7 49 6 12 10 3 | 74 72 75 72 75 74 72 87 76 72 78 73
5E | 5 11 9 9 8 3 11 14 6 9 8 3 | 35 32 34 36 34 34 35 33 34 35 33 34
6 | 7 8 8 9 5 3 7 7 6 10 11 2 | 38 39 40 37 37 37 36 38 37 38 37 37
7 | 7 9 6 5 5 3 10 7 6 14 12 3 | 33 35 32 34 30 32 32 34 32 33 29 32
8E | 8 12 10 13 6 5 14 10 10 13 13 4 | 42 45 47 40 40 45 46 46 43 42 46 42
9 | 7 8 10 8 7 2 9 9 6 12 13 3 | 66 66 62 63 62 64 62 68 64 62 64 63
10E | 8 14 9 13 7 2 8 9 5 12 9 3 | 28 26 28 25 27 27 24 27 25 27 27 25
11 | 7 9 9 6 6 3 10 58 6 13 7 3 | 48 51 51 49 52 50 51 50 52 50 52 50
12 | 7 7 7 6 12 2 19 8 8 12 7 3 | 50 47 47 50 48 47 50 50 44 51 47 47
13 | 9 10 7 10 7 3 9 10 7 11 7 3 | 44 49 42 47 44 45 43 49 45 41 44 44
14 | 9 7 9 6 8 2 9 54 7 10 13 3 | 62 60 65 64 65 64 60 80 63 62 67 62
15 | 7 8 6 10 12 2 9 8 5 7 9 3 | 65 62 63 63 63 63 64 63 62 63 60 62
16 | 6 9 5 8 11 3 13 9 8 11 9 3 | 55 53 54 56 54 54 54 55 54 57 56 54
17E | 9 10 10 8 16 3 11 10 6 10 8 3 | 60 58 58 62 62 60 55 59 59 61 60 59
18 | 7 9 9 8 7 2 9 48 6 14 9 3 | 53 55 52 55 55 53 56 52 54 52 52 53
19E | 11 9 10 9 6 3 11 9 7 10 9 3 | 49 51 53 53 52 50 48 53 50 53 51 50
20 | 7 7 6 5 13 3 8 11 8 12 7 3 | 78 79 77 80 82 79 79 76 82 77 80 79
21 | 6 6 4 10 11 1 9 7 6 11 9 3 | 28 30 29 34 29 30 32 30 29 28 29 29
22 | 7 6 8 7 6 2 11 9 5 10 8 2 | 59 61 60 62 61 61 59 63 61 61 64 60
23E | 9 9 21 10 9 2 9 61 7 14 10 4 | 26 27 35 25 30 27 26 36 27 30 29 27
24 | 5 13 7 11 6 3 7 15 4 7 8 3 | 42 50 44 42 41 42 41 51 45 40 42 42
25 | 7 6 11 6 7 2 8 10 5 9 8 2 | 52 54 54 57 51 52 50 53 51 51 51 52
26 | 6 6 9 6 10 2 8 8 7 9 7 3 | 49 49 49 48 46 48 46 52 46 49 48 47
X27E | 929 --- --- 173 94 97 --- --- 15 28 88 20 | 519 --- --- 71 36 41 --- --- 59 64 99 60
X28 | 4 17 4 --- 7 3 7 50 6 6 10 3 | 48 45 48 --- 50 47 49 50 49 42 48 47
29E | 8 9 9 7 11 4 16 11 7 11 7 3 | 88 88 89 89 84 88 87 89 86 90 88 87
30 | 7 13 8 5 7 2 8 12 5 8 10 3 | 33 44 33 33 31 34 32 45 34 36 34 34
31 | 6 8 5 6 4 2 10 10 6 8 9 2 | 36 39 33 35 33 35 36 39 32 30 33 33
32 | 8 7 9 4 7 2 9 10 5 7 7 2 | 62 61 62 61 60 60 59 60 57 57 60 59
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 9 9 8 9 3 10 24 7 11 9 |T 63 49 49 49 47 48 48 51 48 48 51 48
WRMS | 7 9 9 9 8 3 10 24 6 10 9 |NE 48 49 48 48 47 48 48 51 47 47 49 47
MEDI | 7 9 9 8 7 3 9 10 6 11 9 |MD 48 49 48 49 46 47 48 50 46 49 48 47
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 4.2294 GPS week: 2294 MJD: 60302.0-60308.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3064 |U 10 18 26 |U 16 15 44 |U 9 10 25 |
emr | emr 3057 |U 13 16 34 |U 16 20 55 | 13 15 27 |
esa | esa 3058 | 11 19 45 |U 17 19 56 |U 14 12 34 |
gfz | gfz 2965 |U 10 17 36 |U 14 16 50 | 10 11 23 |
grg | grg 3061 |U 9 19 28 |U 15 18 54 | 10 10 24 |
igr | igr 3058 | 9 17 28 | 15 16 48 | 9 9 22 |
igs | igs 3064 | 9 16 28 | 14 16 47 | 9 10 22 |
jgx | jgx 2962 |U 10 17 26 |U 14 17 50 | 9 11 21 |
jpl | jpl 3058 | 15 18 42 | 16 20 60 | 14 13 38 |
mit | mit 3072 |U 35 30 103 |U 17 19 60 |U 28 28 53 |
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 5.2294.0 GPS week: 2294 Day: 0 MJD: 60302.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 28 23 | 15 15 50 | 10 10 22 |
emr | emr 3072 | 13 23 27 | 13 17 65 | 13 14 28 |
esa | esa 3072 | 11 24 40 | 15 20 64 | 15 13 34 |
gfz | gfz 2976 | 10 21 29 | 14 14 53 | 10 11 22 |
grg | grg 3072 | 11 27 26 | 16 16 63 | 15 15 35 |
igr | igr 3072 | 10 25 23 | 13 14 53 | 11 11 20 |
igs | igs 3072 | 10 24 24 | 14 14 53 | 10 10 20 |
jgx | jgx 2976 | 12 24 25 | 13 19 59 | 9 13 23 |
jpl | jpl 3072 | 15 24 32 | 13 21 75 | 15 14 40 |
mit | mit 3072 | 112 66 482 | 17 20 73 | 120 116 180 |
Table 5.2294.1 GPS week: 2294 Day: 1 MJD: 60303.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 18 32 | 16 19 49 | 11 12 22 |
emr | emr 3071 | 14 19 34 | 14 23 54 | 11 10 27 |
esa | esa 3072 | 12 20 52 | 18 24 58 | 17 13 37 |
gfz | gfz 2973 | 10 19 45 | 14 19 56 | 13 15 25 |
grg | grg 3069 | 10 21 28 | 16 23 67 | 9 7 22 |
igr | igr 3072 | 10 16 32 | 14 19 51 | 10 6 23 |
igs | igs 3072 | 9 16 32 | 14 19 51 | 10 8 22 |
jgx | jgx 2976 | 11 18 28 | 14 19 54 | 10 6 24 |
jpl | jpl 3072 | 16 17 48 | 15 24 63 | 14 10 42 |
mit | mit 3072 | 12 19 23 | 14 24 73 | 12 14 25 |
Table 5.2294.2 GPS week: 2294 Day: 2 MJD: 60304.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 21 16 | 18 21 53 | 8 8 27 |
emr | emr 3067 | 13 17 24 | 18 26 63 | 12 15 27 |
esa | esa 3072 | 11 19 36 | 21 22 62 | 13 13 33 |
gfz | gfz 2968 | 9 16 22 | 18 18 59 | 10 10 24 |
grg | grg 3070 | 9 20 19 | 19 22 60 | 8 12 26 |
igr | igr 3072 | 10 18 18 | 18 21 61 | 9 10 23 |
igs | igs 3072 | 10 17 17 | 18 22 57 | 9 10 23 |
jgx | jgx 2976 | 11 18 18 | 17 20 62 | 10 12 24 |
jpl | jpl 3072 | 15 16 33 | 17 22 70 | ---- ---- ---- |
mit | mit 3072 | 77 57 76 | 21 16 69 | 13 10 39 |
Table 5.2294.3 GPS week: 2294 Day: 3 MJD: 60305.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 12 35 | 15 18 50 | 10 9 26 |
emr | emr 3072 | 14 10 43 | 15 26 49 | 16 20 37 |
esa | esa 3072 | 11 14 53 | 16 21 59 | 14 10 38 |
gfz | gfz 2970 | 12 18 51 | 13 18 50 | 9 6 25 |
grg | grg 3066 | 8 13 34 | 13 20 54 | 9 9 24 |
igr | igr 3072 | 10 11 36 | 14 19 50 | 9 8 24 |
igs | igs 3072 | 9 9 37 | 13 19 49 | 9 8 23 |
jgx | jgx 2976 | 10 10 33 | 13 20 50 | 10 8 22 |
jpl | jpl 3072 | 14 12 52 | 15 22 56 | 16 14 41 |
mit | mit 3072 | 14 19 49 | 14 28 67 | 21 9 43 |
Table 5.2294.4 GPS week: 2294 Day: 4 MJD: 60306.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 13 26 | 13 15 39 | 9 14 24 |
emr | emr 3070 | 12 12 36 | 15 18 54 | 13 20 25 |
esa | esa 3072 | 9 16 46 | 13 17 50 | 11 15 31 |
gfz | gfz 2969 | 11 18 39 | 12 13 43 | 10 15 21 |
grg | grg 3059 | 9 16 37 | 11 20 44 | 9 14 20 |
igr | igr 3072 | 8 12 28 | 12 16 41 | 8 13 19 |
igs | igs 3072 | 8 12 30 | 11 15 41 | 8 14 19 |
jgx | jgx 2976 | 8 16 28 | 11 17 43 | 9 15 19 |
jpl | jpl 3072 | 12 13 46 | 13 18 44 | 13 19 36 |
mit | mit 3072 | 10 20 30 | 13 15 49 | 13 17 29 |
Table 5.2294.5 GPS week: 2294 Day: 5 MJD: 60307.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 20 26 | 12 8 33 | 7 8 26 |
emr | emr 3071 | 12 19 33 | 15 12 55 | 14 13 23 |
esa | esa 3072 | 10 23 42 | 14 12 46 | 12 10 35 |
gfz | gfz 2976 | 12 18 35 | 12 10 40 | 9 10 20 |
grg | grg 3072 | 9 22 28 | 11 12 42 | 9 10 19 |
igr | igr 3072 | 9 22 28 | 12 10 40 | 8 8 21 |
igs | igs 3072 | 9 19 28 | 11 9 39 | 8 9 20 |
jgx | jgx 2976 | 10 20 27 | 11 11 45 | 8 11 16 |
jpl | jpl 3072 | 14 23 37 | 15 15 59 | 13 12 35 |
mit | mit 3072 | 10 19 25 | 18 10 40 | 11 20 25 |
Table 5.2294.6 GPS week: 2294 Day: 6 MJD: 60308.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3021 | 8 15 27 | 20 12 38 | 9 7 29 |
emr | emr 2976 | 12 14 44 | 23 18 48 | 14 11 25 |
esa | esa 2976 | 13 19 45 | 22 17 50 | 13 11 35 |
gfz | gfz 2924 | 9 12 28 | 18 19 46 | 10 7 25 |
grg | grg 3021 | 9 15 29 | 19 15 45 | 10 7 23 |
igr | igr 2976 | 10 13 32 | 19 14 37 | 9 6 22 |
igs | igs 3021 | 8 13 29 | 19 12 40 | 9 8 25 |
jgx | jgx 2880 | 9 15 25 | 18 15 39 | 8 9 21 |
jpl | jpl 2976 | 17 18 44 | 22 15 53 | 13 10 34 |
mit | mit 3072 | 13 11 32 | 21 19 47 | 10 13 33 |
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 6.2294 GPS week: 2294 MJD: 60302.500-60308.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -6 8 72 -68 -1 | -10 43
| 7 19 32 61 4 | 6
emr uuuuu | 11 10 -66 70 4 | -8 45
| 12 14 54 37 10 | 7
esa uuuuu | 10 14 -2 142 -2 | 14 47
| 5 7 47 57 3 | 6
gfz uuuuu | -31 -38 62 -44 0 | 0 43
| 8 7 69 66 4 | 6
grg uuuuu | -38 3 -16 -127 -6 | 4 41
| 15 7 41 56 7 | 5
igr xxxxx | -13 0 -16 45 -4 | -2 45
| 6 7 43 40 5 | 6
irf xxxxx | -7 2 -19 74 7 | -3 43
| 5 7 14 12 12 | 9
jgx uuuuu | 6 -34 -5 -5 1 | 7 42
| 12 11 28 29 5 | 7
mit uuuuu | 14 15 -33 60 3 | 13 44
| 19 23 31 51 6 | 7
ngs uuuxu | 53 18 -45 343 1 | 8 44
| 21 25 111 135 6 | 7
sio xxxxx | 40 21 -45 -31 -8 | 28 51
| 49 65 85 38 13 | 6
Table 7.2294.0 GPS week: 2294 Day: 0 MJD: 60302.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -5 -13 36 -128 -3 | -6 16
emr uuuuu | 21 19 -48 97 3 | -1 24
esa uuuuu | 10 17 39 195 -6 | 18 25
gfz uuuuu | -35 -29 57 -76 -1 | 4 18
grg uuuuu | -16 2 -62 -50 3 | 8 20
igr xxxxx | -12 6 5 -13 -11 | 4 19
irf xxxxx | -15 3 -1 63 12 | -4 16
jgx uuuuu | 11 -40 29 -64 5 | 8 18
mit uuuuu | -22 22 -12 63 6 | 15 22
ngs uuuxu | 69 11 -49 144 -6 | 14 20
sio xxxxx | -28 105 11 -9 2 | 35 39
Table 7.2294.1 GPS week: 2294 Day: 1 MJD: 60303.500
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 | -15 -7 101 -162 0 | -13 36
emr uuuuu | -5 32 -48 -6 -2 | -9 38
esa uuuuu | 18 10 1 145 -3 | 10 36
gfz uuuuu | -32 -39 118 83 -2 | -3 34
grg uuuuu | -18 12 -5 -84 -6 | 2 33
igr xxxxx | -16 8 -80 29 -9 | -4 37
irf xxxxx | -13 9 -30 58 19 | -11 32
jgx uuuuu | 3 -20 -10 13 6 | 2 31
mit uuuuu | 4 -16 -73 73 9 | 7 32
ngs uuuxu | 91 51 -197 579 -5 | 5 34
sio xxxxx | -20 64 -20 -72 -2 | 26 42
Table 7.2294.2 GPS week: 2294 Day: 2 MJD: 60304.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -6 33 92 -25 -6 | -20 42
emr uuuuu | 3 15 -132 54 14 | -20 41
esa uuuuu | 16 19 -84 85 1 | 4 39
gfz uuuuu | -27 -47 146 -71 -4 | -10 39
grg uuuuu | -41 5 39 -173 -14 | -5 38
igr xxxxx | -1 -11 -51 10 -3 | -13 42
irf xxxxx | -3 -11 -19 80 23 | -16 35
jgx uuuuu | 28 -38 6 -15 -1 | -4 35
mit uuuuu | 13 -15 -28 160 10 | 1 34
ngs uuuxu | 44 49 -143 241 -2 | -3 38
sio xxxxx | 95 -77 -156 -31 8 | 17 39
Table 7.2294.3 GPS week: 2294 Day: 3 MJD: 60305.500
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 | 0 -10 49 -85 -1 | -13 48
emr uuuuu | 19 -3 36 98 -5 | -14 49
esa uuuuu | 1 25 9 192 3 | 11 50
gfz uuuuu | -20 -43 66 -40 7 | -3 46
grg uuuuu | -42 -8 -7 -132 -12 | 1 45
igr xxxxx | -21 0 -42 102 2 | -6 49
irf xxxxx | -7 10 -16 69 12 | -6 48
jgx uuuuu | -11 -44 -33 10 6 | 4 45
mit uuuuu | 20 42 -34 5 0 | 10 48
ngs uuuxu | 44 21 -108 367 3 | 4 47
sio xxxxx | 24 54 79 -36 -6 | 25 53
Table 7.2294.4 GPS week: 2294 Day: 4 MJD: 60306.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 5 30 113 3 -5 | -6 54
emr uuuuu | 9 -8 -107 79 19 | -7 54
esa uuuuu | 7 8 -5 205 -6 | 19 59
gfz uuuuu | -37 -43 90 -85 -2 | 4 55
grg uuuuu | -44 -4 -71 -201 -9 | 6 51
igr xxxxx | -15 -5 2 56 -4 | 1 56
irf xxxxx | -5 3 -40 95 -5 | 3 57
jgx uuuuu | -1 -49 15 -2 -6 | 13 55
mit uuuuu | 29 36 -62 9 1 | 17 57
ngs uuuxu | 31 14 38 375 7 | 11 56
sio xxxxx | 79 -2 -146 11 -22 | 31 62
Table 7.2294.5 GPS week: 2294 Day: 5 MJD: 60307.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -8 10 33 -68 5 | -5 53
emr uuuuu | 5 14 -78 95 9 | -3 54
esa uuuuu | 9 6 58 96 -4 | 21 60
gfz uuuuu | -22 -39 24 -2 1 | 6 55
grg uuuuu | -52 4 -31 -165 -6 | 8 51
igr xxxxx | -13 6 41 78 3 | 3 56
irf xxxxx | -5 1 -24 79 -3 | 7 56
jgx uuuuu | 7 -30 -51 22 -5 | 15 55
mit uuuuu | 33 23 -42 49 1 | 20 57
ngs uuuxu | 34 -5 109 376 -1 | 14 56
sio xxxxx | 77 48 -12 -88 -9 | 31 62
Table 7.2294.6 GPS week: 2294 Day: 6 MJD: 60308.500
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 | -12 16 81 -15 3 | -6 53
emr uuuuu | 28 -2 -86 69 -8 | -3 54
esa uuuuu | 7 10 -31 75 -2 | 19 59
gfz uuuuu | -41 -28 -67 -115 2 | 5 55
grg uuuuu | -51 8 25 -82 3 | 5 50
igr xxxxx | -16 -5 14 51 -8 | 0 56
irf xxxxx | 0 -3 -2 75 -8 | 6 56
jgx uuuuu | 6 -20 6 -3 0 | 13 55
mit uuuuu | 22 16 19 61 -7 | 20 57
ngs uuuxu | 59 -16 31 321 8 | 12 56
sio xxxxx | 54 -47 -72 9 -29 | 28 61
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