[IGSREPORT-29657] Wk 2292 IGS Final Orbits
acc
acc at igs.org
Sun Dec 31 02:41:36 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2292 (Dec 10, 2023 - Dec 16, 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_20233440000_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 | COD | CZTG
0 | ESA | HRAO PTBB
0 | GFZ | HRAO POHN HERS HRAO POHN TASH
0 | GRG | JFNG JFNG PALM SCRZ SVTL
0 | JGX | CAS1 CZTG CAS1 CZTG DAV1 NRMD NYA2
1 | COD | GAMB MIKL NYA2
1 | ESA | MAYG
1 | GFZ | OUS2 POHN SCUB CZTG HERS HRAO IISC POHN RIO2 SCUB
1 | GRG | ASCG CPVG HRAO SCRZ SGOC ULAB ASCG CPVG GAMB HRAO
1 | GRG | SCRZ SGOC ULAB
1 | JGX | NYA2 MIZU NIUM NYA2 RIO2 SAMO SCUB VOIM
2 | COD | 27 MIKL OUS2
2 | ESA | PTBB VOIM
2 | GFZ | 5 5 LAUT OUS2 HERS LAUT OUS2
2 | GRG | 27 27 OUS2 BAKE OUS2 SGOC VOIM
2 | JGX | CAS1 DAV1 SCOR BAKE CAS1 DAV1 IISC MAC1 NYA2 SALU
2 | JGX | SCOR
2 | MIT | YELL
3 | COD | MIKL NRMD
3 | EMR | NRMD
3 | ESA | PTBB UFPR
3 | GFZ | DGAR HERS NRMD POHN
3 | GRG | BOGT DAV1 DAV1 PALM TASH VOIM
3 | JGX | DAV1 MAC1 NYA2 SGOC CAS1 DAV1 GAMB IISC IQAL MAC1
3 | JGX | NYA2 SGOC VOIM
4 | COD | 23 ABMF MIKL
4 | ESA | FAIR FAIR
4 | GRG | 3 3 PALM
4 | JGX | AREQ DAV1 MAC1 NYA2 QAQ1 SCOR BAKE CAS1 CZTG DAV1
4 | JGX | IQAL KOUR MAC1 NYA2 QAQ1 SAMO SCH2 SCOR THTG TRO1
5 | COD | SGOC
5 | ESA | 3 10
5 | GFZ | 3 POHN HERS POHN
5 | GRG | 3 10 STK2 PALM STK2
5 | JGX | 3 8 CAS1 DAV1 NYA2 BAKE CAS1 DAV1 IQAL MAC1 NYA2
5 | JGX | SCOR YEL2
5 | MIT | 23
6 | COD | DAV1
6 | GFZ | 5 5 HERS
6 | GRG | CZTG DAV1 CZTG DAV1
6 | JGX | 2 3 8 18 21 27 32 BAKE CCJ2 GUAM IQAL SCOR
6 | MIT | 19 20
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
----+--------+---------------
2 | COD | 27
2 | GRG | 27
4 | GRG | 3
4 | JGX | 3
7. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G03 | 4 | | 4 | 4 | 4 | 4 | 4 |
PRN G04 | | | | | | | 4 |
PRN G27 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
PRN G28 | | | | | | | 4 |
PRN G31 | | | | | 4 | 4 | 4 |
8. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
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.
9. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | -.4 -.8 .1 -34 -3 -9 .23
EMR | 0 | 4.5 5.9 -2.7 6 -8 6 .33
ESA | 0 | -.0 -.2 .7 -9 -20 -8 -.47
GFZ | 0 | .3 -1.0 .0 -30 -5 0 .33
GRG | 0 | .5 -.9 -.4 -6 -6 18 .07
JGX | 0 | -.6 9.4 3.1 -11 -21 7 .02
JPL | 0 | 2.2 6.1 7.4 -28 20 -32 .82
MIT | 0 | 6.3 1.9 20.3 4 -7 9 .16
NGS | 0 | 5.4 7.9 4.4 25 -8 -23 .18
SIO | 0 | 6.6 6.4 13.2 128 -71 -1 .13
COD | 1 | -.0 -.8 .1 -34 8 -14 .06
EMR | 1 | 2.5 3.0 -4.8 12 -7 0 .25
ESA | 1 | -.2 .1 .5 -11 -18 -2 -.32
GFZ | 1 | .9 -.8 -.4 -15 15 21 .29
GRG | 1 | .6 -.6 -.9 -14 1 26 .18
JGX | 1 | 1.4 2.8 7.5 7 -17 15 -.03
JPL | 1 | 3.9 10.1 10.4 -7 38 -43 .75
MIT | 1 | 4.4 1.7 20.3 9 -6 -11 -.01
NGS | 1 | 3.1 8.9 9.6 11 17 -28 .14
SIO | 1 | 2.7 6.1 13.4 41 -40 -23 .11
COD | 2 | .1 -.7 -.0 -25 5 -17 .07
EMR | 2 | 4.8 -.5 -1.7 6 -12 0 .35
ESA | 2 | .4 -.1 .8 -17 -10 -22 -.43
GFZ | 2 | -.4 -1.2 -.4 -11 -11 15 .27
GRG | 2 | .9 -.5 -.1 -8 -18 20 -.08
JGX | 2 | 2.5 -2.8 4.5 0 -16 10 .14
JPL | 2 | 2.4 4.3 6.2 -10 44 -48 .58
MIT | 2 | 7.4 -5.9 20.1 -9 -11 5 .15
NGS | 2 | -4.4 4.5 7.4 -11 38 -43 .07
SIO | 2 | 4.3 1.3 8.3 11 -51 -11 .32
COD | 3 | .2 -.3 -.2 -19 13 -22 .06
EMR | 3 | -.7 3.8 -.6 6 -8 10 .16
ESA | 3 | -.2 -.8 .4 8 -20 -21 -.38
GFZ | 3 | -.5 -1.0 .8 -7 -16 -16 .65
GRG | 3 | .8 -.7 -1.5 -16 -11 6 .01
JGX | 3 | 2.3 1.2 -.8 16 -30 5 .02
JPL | 3 | -.4 8.0 2.4 -18 48 -35 .79
MIT | 3 | 3.4 -2.1 17.1 -10 -21 1 .13
NGS | 3 | 5.2 5.4 2.3 12 -24 -29 .06
SIO | 3 | 2.3 7.3 .7 87 -70 14 .14
COD | 4 | -.1 -.5 -.7 -23 4 -14 .04
EMR | 4 | 6.2 8.3 1.9 2 -12 12 .25
ESA | 4 | .3 -.6 .0 -4 -11 -27 -.58
GFZ | 4 | -.0 -.5 .4 -21 0 -20 .54
GRG | 4 | .8 -.6 -1.0 -3 3 3 .06
JGX | 4 | 5.8 2.0 10.8 -12 7 2 -.08
JPL | 4 | .2 13.0 2.5 -20 43 -33 .77
MIT | 4 | 9.6 6.3 23.7 8 2 -8 .17
NGS | 4 | 3.3 3.8 6.4 -15 13 -41 .15
SIO | 4 | 6.6 8.3 7.9 20 -109 33 .03
COD | 5 | -.5 -.8 -1.2 -19 7 -20 -.03
EMR | 5 | -1.6 -2.5 10.0 0 -8 -9 .26
ESA | 5 | .0 -1.2 .1 5 -23 -29 -.26
GFZ | 5 | .3 -1.2 -.3 -24 -6 -7 .69
GRG | 5 | .9 -.8 -1.4 -4 -1 18 .23
JGX | 5 | 5.8 .8 11.1 -9 12 6 -.03
JPL | 5 | -.2 4.9 7.7 -35 28 -44 .83
MIT | 5 | 8.5 2.1 24.0 4 -13 11 .37
NGS | 5 | 8.6 4.6 15.0 -16 20 -36 .10
SIO | 5 | 8.4 7.3 13.5 98 -69 39 .21
COD | 6 | -.8 -.8 -1.5 -11 8 -23 .03
EMR | 6 | -4.1 .4 9.9 7 -9 6 .11
ESA | 6 | .1 -1.3 .4 4 -20 -6 -.71
GFZ | 6 | -.5 -1.1 .4 -24 8 -8 .30
GRG | 6 | .8 -.4 -.8 -1 -11 26 .01
JGX | 6 | 6.4 6.1 11.4 -8 12 7 -.27
JPL | 6 | -.9 7.4 13.5 -12 50 -57 .52
MIT | 6 | 7.2 2.0 20.0 4 -22 -6 -.10
NGS | 6 | -.3 7.1 18.7 -5 52 -57 -.17
SIO | 6 | 8.2 7.2 16.0 23 -115 42 .00
10. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
11. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
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 1.2292.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2292.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 2.2292.[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 3.2292.[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 5.2292.0-6). 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 2292 summary. (Dec 10, 2023 - Dec 16, 2023)
Table 1.2292.a GPS week: 2292 MJD: 60288.000-60294.000
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 811| 0 0 2 -13 1 1 .00 10 7 | -543 -78 6 97
| 0 0 1 14 5 13 .01 | 213 361
emr 102| -2 0 0 2 -3 -4 .08 13 13 | -222 -1609 50 119
| 1 2 4 14 17 17 .03 | 1380 2318
esa 150| 0 0 6 -13 2 -10 -.07 10 9 | -333 -880 6 73
| 0 0 1 11 8 10 .02 | 553 811
gfz 120| 0 1 2 16 12 -2 .12 11 10 | 138 70 9 84
| 0 0 1 7 8 8 .02 | 171 214
grg 121| 0 -4 -9 -12 16 5 -.03 14 8 | -15 -55 7 118
| 0 0 2 16 17 9 .02 | 101 169
igr n/a| 0 0 0 6 12 14 .03 4 4 | 6078 522 10 88
| 0 0 0 6 10 13 .01 | 1010 662
jgx n/a| 0 0 3 34 -24 -22 -.01 12 12 | -32 49 19 80
| 0 0 1 13 14 33 .02 | 134 249
jpl n/a| -1 1 -1 -6 0 -6 .16 25 25 | -440 456 73 159
| 0 2 1 12 12 20 .04 | 869 807
mit 366| 1 1 -5 -5 -7 10 .03 9 8 | 6810 -16 453 13353
| 1 1 0 39 20 37 .01 | 9883 1228
ngs 282| 0 0 0 14 -4 21 -.05 13 10 | -571 -76 807 1873
| 0 1 2 17 9 31 .03 | 193 295
sio 341| 1 1 -6 20 20 12 .04 13 10 | --- --- --- ---
| 0 0 1 22 24 25 .03 | --- ---
Table 1.2292.b GPS week : 2292 MJD: 60288.000-60294.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 5 4 4 5 5 4 4 |
2 | 4 4 4 4 4 4 4 |
3 | 5 4 6 6 15 9 7 |
4 | 3 3 3 4 4 4 4 |
5 | 5 5 5 6 5 4 4 |
6 | 3 4 3 3 3 4 3 |
7 | 3 3 3 3 3 3 3 |
8 | 3 3 3 4 3 4 4 |
9 | 3 3 3 3 4 4 4 |
10 | 4 5 5 6 7 8 6 |
11 | 4 4 4 4 4 4 4 |
12 | 5 5 6 5 6 4 4 |
13 | 3 3 3 3 3 3 3 |
14 | 4 5 4 4 5 4 4 |
15 | 4 4 3 4 4 4 4 |
16 | 5 5 4 5 4 4 4 |
17 | 3 3 3 3 4 3 4 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 4 3 4 4 4 |
20 | 4 4 4 4 4 4 4 |
21 | 3 4 4 4 4 3 3 |
22 | 3 4 3 4 3 4 3 |
23 | 5 6 6 9 9 8 7 |
24 | 3 3 3 4 4 3 3 |
25 | 4 4 4 4 4 3 4 |
26 | 3 3 3 4 0 5 3 |
27 | 3 3 10 8 3 3 3 |
28 | 4 4 4 4 3 3 3 |
29 | 4 4 4 4 5 4 4 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 4 3 4 3 3 |
32 | 3 3 3 3 3 3 4 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2292.0 GPS week: 2292 Day: 0 MJD: 60288.000
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 812| 0 0 2 -28 1 11 -.02 8 8 | -227 -469 7 103
emr 105| -1 0 -3 0 -7 16 .05 11 11 | 448 -3078 48 124
esa 150| 0 0 5 -10 -7 -5 -.08 9 9 | -811 -534 6 78
gfz 118| 0 0 2 19 15 3 .12 9 8 | 432 -197 12 89
grg 120| 0 -3 -7 3 15 21 -.01 8 9 | 108 -338 7 113
igr n/a| 0 0 0 6 10 10 .01 4 4 | 4670 757 10 80
jgx n/a| -1 0 2 26 -35 -45 -.01 10 10 | 5 -35 21 80
jpl n/a| 0 -1 -1 -14 -12 5 .14 24 25 | -1315 592 75 153
mit 366| 0 0 -4 -22 7 -14 .02 7 7 | 16108 -2640 1274 8984
ngs 288| 0 1 0 33 -4 21 -.06 11 9 | -192 -583 829 1960
sio 346| 0 0 -6 10 22 9 .03 11 10 | --- --- --- ---
Table 2.2292.1 GPS week: 2292 Day: 1 MJD: 60289.000
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 810| 0 0 2 -13 2 -8 -.01 7 7 | -391 -405 7 94
emr 106| -2 0 -3 -16 8 -16 .05 11 11 | 1015 -3043 49 110
esa 150| 0 0 5 -22 2 -18 -.07 10 10 | 375 -1994 7 73
gfz 119| -1 1 5 9 17 1 .14 10 9 | 190 67 9 94
grg 120| 1 -5 -8 -30 34 7 -.05 8 9 | 93 -86 7 122
igr n/a| 0 0 -1 4 13 -7 .02 4 3 | 5506 889 11 84
jgx n/a| -1 0 3 42 -45 -67 .01 10 10 | 10 -8 19 72
jpl n/a| -1 0 -2 -18 0 -5 .16 24 24 | -716 676 74 165
mit 366| 1 0 -5 16 -14 75 .03 8 7 | -9136 665 59 18788
ngs 288| 0 1 -3 4 -6 -12 -.01 12 10 | -545 -121 877 2006
sio 346| 0 1 -7 1 52 -23 .06 11 10 | --- --- --- ---
Table 2.2292.2 GPS week: 2292 Day: 2 MJD: 60290.000
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 810| 0 0 3 -8 -9 11 .00 15 7 | -788 350 7 98
emr 106| -2 0 -2 20 -4 -23 .08 12 12 | -1425 796 43 118
esa 150| 0 0 4 -13 15 -17 -.11 10 9 | -823 80 6 64
gfz 121| 0 2 0 19 22 4 .11 12 11 | 194 -23 10 76
grg 122| 0 -4 -6 -11 5 8 -.04 29 9 | -50 100 7 113
igr n/a| 0 0 0 17 15 26 .04 4 4 | 6139 315 11 91
jgx n/a| -1 0 3 37 -26 -44 .01 11 11 | -171 249 19 78
jpl n/a| 0 0 0 7 -6 9 .12 25 26 | -408 160 75 136
mit 366| 1 0 -4 -2 -1 -2 .04 8 7 | 1724 365 57 14321
ngs 278| -1 1 1 -19 -1 40 -.02 11 10 | -747 287 672 1712
sio 343| 0 0 -3 1 33 -1 .04 12 10 | --- --- --- ---
Table 2.2292.3 GPS week: 2292 Day: 3 MJD: 60291.000
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 812| 0 0 3 -28 2 8 .01 12 8 | -611 -61 6 89
emr 106| -3 1 -1 6 30 -1 .06 11 11 | 1591 -4665 43 115
esa 150| 0 0 4 -3 13 -2 -.06 10 10 | 241 -1278 6 70
gfz 123| -2 2 3 28 16 -9 .10 11 10 | 130 354 9 86
grg 123| 0 -4 -7 7 40 -7 -.06 10 8 | 21 121 7 129
igr n/a| 0 0 0 12 28 16 .04 4 4 | 6576 -776 10 84
jgx n/a| -1 0 1 41 -26 -20 -.00 9 9 | 13 120 14 83
jpl n/a| -1 1 -3 -1 26 -8 .15 25 25 | -143 -1059 74 160
mit 366| 3 0 -3 -59 -43 10 .03 11 8 | 4624 -336 1540 11895
ngs 281| 0 0 -2 20 -8 46 -.06 13 11 | -613 -61 1068 1966
sio 345| 1 1 -5 0 43 18 .07 13 11 | --- --- --- ---
Table 2.2292.4 GPS week: 2292 Day: 4 MJD: 60292.000
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 817| -1 0 1 2 2 -2 .01 10 8 | -557 -158 6 100
emr 97| 0 1 -2 -15 -24 16 .09 19 19 | -1741 1233 59 116
esa 150| 0 0 5 -34 -3 3 -.07 11 11 | -1001 96 7 71
gfz 121| 0 0 2 10 0 8 .15 12 13 | 110 -155 10 88
grg 122| 0 -2 -10 -33 7 -3 -.04 28 9 | -87 -184 7 134
igr n/a| 0 0 0 2 -5 31 .03 7 4 | 5205 1259 12 95
jgx n/a| 0 0 5 7 -19 -22 -.03 18 18 | -169 -86 22 89
jpl n/a| -2 5 -3 4 -10 19 .12 26 28 | -1637 1528 76 171
mit 366| 3 2 -6 65 0 -34 .02 13 9 | 17747 877 134 14020
ngs 281| 0 -1 0 14 12 68 -.03 16 12 | -503 -234 884 1911
sio 345| 2 2 -6 22 -7 57 .06 19 12 | --- --- --- ---
Table 2.2292.5 GPS week: 2292 Day: 5 MJD: 60293.000
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 811| -1 0 0 -26 2 14 .00 8 7 | -808 468 6 95
emr 100| -5 -6 5 17 -14 -23 .15 15 15 | 257 -2765 59 131
esa 150| 0 0 8 1 0 -25 -.04 9 8 | -284 -909 7 81
gfz 121| -1 1 3 23 1 -5 .13 12 9 | -138 320 9 86
grg 121| 0 -3 -10 -2 21 4 -.02 10 7 | -11 -83 7 104
igr n/a| 0 -1 -1 4 16 18 .04 4 4 | 6931 887 11 89
jgx n/a| 0 0 4 41 0 24 -.04 11 11 | -124 441 21 74
jpl n/a| -1 1 0 -1 -2 -33 .19 25 25 | 312 992 72 164
mit 366| 2 1 -5 -31 -23 -2 .02 10 8 | 1569 766 57 14740
ngs 284| 0 0 0 21 0 5 -.11 14 11 | -767 250 792 1732
sio 330| 1 1 -6 51 2 26 -.01 12 9 | --- --- --- ---
Table 2.2292.6 GPS week: 2292 Day: 6 MJD: 60294.000
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 811| -1 0 2 6 7 -23 .00 7 6 | -419 -274 7 105
emr 100| -2 -1 5 2 -10 2 .10 13 13 | -1699 259 51 121
esa 150| 0 0 7 -13 -3 -7 -.04 9 9 | -29 -1626 7 78
gfz 120| 0 0 1 7 13 -16 .12 11 9 | 50 127 8 71
grg 123| 0 -3 -12 -24 -9 5 -.02 8 7 | -182 79 8 117
igr n/a| 0 -1 -1 -2 7 2 .05 4 3 | 7520 323 10 99
jgx n/a| 0 0 6 43 -18 15 -.03 13 13 | 206 -334 23 86
jpl n/a| 0 0 1 -25 3 -32 .22 24 24 | 826 303 71 166
mit 366| 1 3 -4 -4 18 45 .02 9 8 | 15035 191 54 10729
ngs 276| -1 0 5 24 -20 -15 -.07 12 10 | -631 -71 532 1829
sio 333| 2 2 -6 52 -4 1 .02 12 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 3.2292.0 GPS week: 2292 Day: 0 MJD: 60288.000
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 10 11 16 5 6 --- 11 7 9 --- 4 | 22 23 21 25 20 20 --- 23 22 23 --- 21
2 | 8 8 6 8 10 3 9 11 10 10 9 3 | 17 18 18 22 20 20 20 18 22 22 23 19
3E | 8 13 16 13 9 4 9 12 9 14 17 4 | 245 247 246 247 245 245 246 20 247 247 246 246
4 | 7 11 6 6 6 4 5 44 5 9 12 2 | 54 53 53 56 57 54 55 67 59 53 59 55
5E | 7 9 9 8 13 6 10 7 8 19 10 4 | 92 92 92 91 92 93 92 93 95 94 94 92
6 | 7 8 8 10 6 3 8 8 5 9 7 3 | 23 20 21 22 19 19 18 25 19 19 21 19
7 | 8 9 7 6 7 2 9 9 5 9 9 3 | 35 35 34 34 29 33 35 38 33 32 31 33
8 | 11 10 9 7 7 4 6 11 6 7 13 3 | 22 22 25 20 21 22 23 23 21 23 26 21
9 | 7 9 9 5 5 3 8 8 5 8 10 2 | 34 35 32 33 32 31 31 36 34 28 34 32
10E | 9 10 11 12 13 3 8 11 8 8 11 4 | 38 40 38 44 38 37 37 35 35 37 33 37
11 | 7 11 10 8 8 3 10 61 7 12 9 3 | 41 39 38 39 42 39 40 46 42 40 41 40
12 | 8 12 8 11 13 3 19 10 5 12 9 4 | 32 28 26 30 33 27 30 31 29 31 30 29
13 | 7 11 9 8 5 5 8 12 9 8 18 3 | 26 34 23 26 30 26 26 33 30 24 32 26
14 | 8 12 15 8 9 4 12 61 7 10 7 4 | 40 38 47 41 47 42 40 61 38 44 45 42
15 | 8 7 4 9 7 2 11 8 9 8 15 3 | 53 49 51 53 49 51 52 53 50 52 47 51
16 | 7 12 12 15 11 6 16 10 7 11 13 4 | 25 23 23 38 27 25 29 25 29 28 28 27
17 | 6 12 6 8 5 3 7 13 6 6 7 2 | 25 24 19 27 24 23 23 26 23 23 26 23
18 | 10 13 9 7 6 3 10 55 8 15 11 3 | 61 62 58 61 62 59 62 65 61 57 54 60
19 | 6 12 6 13 8 3 12 11 8 7 7 3 | 24 23 23 27 23 22 25 25 26 23 27 23
20E | 9 10 7 7 8 3 7 11 9 17 15 4 | 54 51 51 48 49 51 49 49 53 54 58 50
21 | 9 8 4 6 8 3 9 11 6 10 6 3 | 16 19 17 19 19 18 19 18 19 20 22 17
22 | 8 10 7 10 7 3 8 12 5 7 5 3 | 32 30 29 35 32 30 32 32 30 32 34 31
23E | 9 11 19 11 12 4 12 54 10 14 13 5 | 104 103 102 102 104 102 99 102 103 101 103 102
24 | 6 16 8 9 6 3 9 13 6 9 9 3 | 18 32 20 26 19 20 20 32 18 18 24 19
25 | 7 12 13 9 7 3 10 12 6 13 10 3 | 23 24 29 26 25 23 20 24 23 23 26 23
26 | 9 11 9 7 8 4 6 9 5 8 11 3 | 22 20 22 18 21 21 20 19 19 20 23 21
27 | 8 12 8 4 5 3 6 11 6 8 14 2 | 220 218 220 219 220 219 222 219 219 219 223 220
X28 | 8 21 4 --- 7 4 10 51 8 9 6 3 | 40 26 37 --- 40 39 40 58 38 42 40 39
29 | 10 10 7 6 8 4 16 11 7 11 11 4 | 35 37 38 39 36 38 36 38 37 40 39 36
30 | 7 11 8 5 6 4 6 13 5 6 9 2 | 17 27 20 21 20 20 19 29 22 20 24 19
31 | 7 9 6 5 5 3 12 9 7 9 9 3 | 46 48 46 45 45 44 47 51 44 44 43 45
32 | 8 9 8 7 8 2 8 10 5 10 9 3 | 24 29 25 24 23 23 22 29 20 23 23 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 11 9 9 8 4 10 24 7 11 11 |T 48 49 48 50 48 48 49 45 48 48 50 48
WRMS | 8 11 9 8 9 4 10 25 7 9 10 |NE 39 39 38 40 39 38 40 42 39 39 41 38
MEDI | 8 11 8 8 7 3 9 11 7 9 10 |MD 32 32 29 34 32 30 32 32 30 31 33 31
Table 3.2292.1 GPS week: 2292 Day: 1 MJD: 60289.000
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 8 9 14 6 5 --- 11 7 13 --- 4 | 20 22 23 27 20 22 --- 21 26 24 --- 21
2 | 8 7 8 10 8 3 8 10 12 15 11 4 | 16 17 20 22 19 19 19 17 25 21 23 18
3E | 5 11 17 9 10 3 7 12 9 15 16 4 | 131 134 134 132 134 131 132 20 135 132 135 132
4 | 6 11 6 7 6 3 6 47 6 11 9 3 | 41 42 42 42 44 41 43 49 49 40 46 43
5E | 7 8 12 8 15 6 11 7 9 13 12 4 | 57 61 59 56 64 58 58 60 58 57 62 58
6 | 8 9 9 9 7 3 7 7 7 10 9 3 | 23 23 23 23 21 22 20 24 25 23 24 22
7 | 3 9 6 8 5 2 8 8 6 6 10 2 | 28 31 30 34 27 28 27 31 28 26 27 28
8 | 6 12 11 8 5 2 7 11 6 11 10 3 | 21 24 27 21 23 21 22 23 25 20 23 22
9 | 5 9 8 6 5 3 8 7 8 10 13 3 | 32 35 32 32 31 32 30 36 37 28 34 32
10E | 7 11 11 20 17 4 9 11 9 12 12 5 | 37 40 40 38 38 37 36 34 41 39 40 38
11 | 8 12 11 6 8 4 11 61 8 14 10 4 | 29 31 33 31 32 30 32 33 35 29 33 31
12 | 8 12 9 14 11 3 20 10 8 10 13 4 | 32 29 26 37 34 29 30 31 31 30 31 30
13 | 6 12 9 7 5 4 8 12 8 11 17 3 | 20 27 17 23 20 20 20 30 25 17 24 20
14 | 8 10 17 6 10 3 11 61 6 15 8 4 | 35 33 38 35 37 34 32 49 35 31 36 34
15 | 7 6 7 8 7 3 11 7 9 12 11 3 | 43 40 39 41 41 39 41 41 40 40 38 40
16 | 7 10 10 13 11 4 15 11 9 17 13 4 | 23 22 24 32 24 22 27 24 31 21 25 25
17 | 6 9 7 9 5 5 9 10 5 9 6 3 | 26 25 22 29 24 25 25 26 28 22 28 24
18 | 9 13 8 8 7 4 10 53 9 12 10 3 | 64 60 58 60 60 59 63 60 63 55 58 60
19 | 7 10 6 10 7 3 12 8 8 10 8 3 | 24 24 24 27 22 24 26 24 30 24 28 24
20E | 7 12 10 11 8 4 9 11 10 9 15 3 | 37 33 35 36 34 35 33 34 33 36 37 34
21 | 8 6 7 8 8 3 10 9 8 11 8 3 | 16 20 20 20 18 18 20 18 22 19 21 18
22 | 7 8 8 10 8 3 10 11 6 12 6 3 | 27 25 26 29 26 26 24 25 29 29 27 26
23E | 12 12 19 14 12 4 13 52 15 15 17 5 | 72 70 74 69 72 70 68 71 74 73 72 71
24 | 6 18 8 8 4 4 9 14 7 11 8 3 | 20 34 21 25 20 22 20 33 22 19 23 20
25 | 6 12 12 14 6 4 10 13 9 13 13 4 | 24 24 28 30 25 23 22 25 25 24 23 24
26 | 5 13 9 9 6 4 7 8 8 10 8 3 | 22 22 22 21 20 20 21 21 21 17 20 21
27 | 9 11 8 6 4 3 8 11 8 9 11 3 | 225 228 229 226 229 228 228 228 229 228 231 228
X28 | 6 22 6 --- 7 3 10 51 8 10 8 3 | 33 24 30 --- 34 31 33 41 31 34 33 32
29 | 10 11 7 9 8 5 16 11 10 8 12 4 | 30 32 32 36 29 32 31 33 32 31 33 31
30 | 6 11 8 6 6 3 7 12 7 6 9 2 | 23 30 22 24 21 21 19 31 21 20 23 21
31 | 5 10 8 6 5 3 10 10 5 9 10 2 | 39 45 39 40 39 41 40 45 45 41 43 40
32 | 8 10 9 8 7 2 9 10 5 10 10 3 | 23 27 25 23 22 23 21 28 25 23 24 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 11 10 10 8 4 10 24 8 12 11 |T 40 41 41 42 40 40 40 39 43 39 42 40
WRMS | 7 11 10 9 9 3 10 24 7 10 10 |NE 36 38 37 39 36 36 37 39 39 36 39 36
MEDI | 7 11 8 8 7 3 9 11 8 11 10 |MD 28 30 28 32 27 28 30 31 31 28 31 28
Table 3.2292.2 GPS week: 2292 Day: 2 MJD: 60290.000
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 12 9 10 4 4 --- 10 8 8 --- 3 | 18 20 20 20 17 18 --- 20 19 20 --- 18
2 | 6 9 6 10 7 3 7 10 12 10 13 3 | 15 16 17 21 17 17 18 16 20 19 21 17
3E | 8 11 14 25 12 3 8 11 7 15 15 5 | 165 165 164 165 171 162 165 17 165 163 164 165
4 | 7 12 7 5 7 3 6 47 6 15 9 3 | 47 48 49 51 50 49 49 59 52 55 53 50
5E | 9 11 9 12 16 6 10 6 8 11 11 4 | 58 61 58 62 62 60 58 58 60 59 61 59
6 | 7 9 8 8 5 2 7 8 6 8 8 3 | 23 23 23 25 20 22 21 25 22 22 23 21
7 | 5 9 8 9 4 4 8 9 6 9 8 2 | 37 38 37 37 34 36 36 40 36 38 36 36
8 | 5 9 10 9 5 3 8 11 6 10 14 3 | 19 20 23 17 19 19 21 22 18 21 21 19
9 | 5 8 10 7 6 3 6 8 5 16 9 3 | 28 30 28 28 27 28 28 31 29 31 29 28
10E | 7 9 13 24 15 4 9 11 8 9 12 5 | 23 24 28 28 24 22 23 20 25 24 29 24
11 | 8 11 10 7 6 3 10 63 8 11 9 3 | 22 23 24 25 26 23 23 29 26 22 26 23
12M | 9 12 8 20 16 3 18 10 8 11 8 5 | 27 23 20 26 26 22 23 28 22 28 22 22
13 | 4 12 8 9 5 3 8 16 9 7 13 3 | 21 28 18 27 23 23 22 32 24 23 24 21
14 | 10 11 16 10 8 3 12 61 6 10 10 4 | 30 29 36 37 33 33 30 47 31 29 34 31
15 | 7 8 6 9 8 2 8 10 10 5 11 3 | 52 50 52 53 51 52 52 54 51 53 51 51
16 | 7 11 9 10 12 6 14 10 8 13 12 4 | 22 16 20 25 21 19 24 22 25 26 24 22
17 | 7 10 5 9 4 3 8 11 6 8 6 2 | 29 29 25 32 27 28 28 28 28 28 29 27
18 | 8 14 8 9 7 3 10 55 7 13 10 3 | 39 43 42 41 39 40 40 46 40 42 43 40
19 | 7 12 5 10 5 3 12 11 6 13 7 3 | 23 20 19 26 19 22 23 20 21 27 24 21
20E | 8 14 9 7 7 3 7 11 9 16 13 3 | 31 25 29 29 29 27 28 25 33 33 34 29
21 | 9 7 6 10 8 3 9 8 9 8 11 3 | 15 17 16 19 16 16 17 16 16 18 20 15
22 | 7 11 7 9 7 4 8 11 5 9 7 3 | 23 21 21 24 22 23 23 24 20 24 23 21
23E | 10 12 19 15 12 5 12 56 20 13 23 6 | 57 59 59 55 58 58 56 60 59 58 59 56
24M | 5 15 8 12 7 3 9 15 7 8 7 3 | 16 30 18 25 14 18 15 30 15 18 17 16
25M | 6 9 12 10 7 2 7 9 5 11 7 3 | 21 22 25 21 19 20 17 25 19 21 19 19
26 | 5 11 9 9 7 4 7 10 8 12 9 3 | 21 18 20 17 19 19 18 20 18 19 20 19
27 | 74 29 14 16 151 13 34 28 12 15 26 9 | 595 615 615 615 585 612 603 614 615 610 615 611
X28M | 8 21 5 --- 8 3 10 53 8 14 9 4 | 25 20 29 --- 31 30 29 42 33 32 33 29
29 | 5 11 6 9 8 4 16 9 6 17 8 4 | 40 34 36 37 36 37 36 37 39 41 39 37
30 | 8 13 8 7 6 5 7 12 6 7 9 3 | 28 32 27 29 26 27 25 34 27 27 29 26
31M | 8 10 8 7 6 3 12 12 5 11 10 3 | 31 31 32 29 29 29 30 36 28 33 27 30
32 | 7 11 8 8 7 3 7 10 5 9 8 3 | 16 22 19 17 16 16 16 21 14 17 17 15
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 15 12 10 12 29 4 11 25 8 11 12 |T 50 51 51 53 50 50 51 49 51 52 53 50
WRMS | 7 12 9 11 9 4 11 26 7 10 10 |NE 54 55 55 57 53 55 56 58 55 56 58 54
MEDI | 7 11 8 9 7 3 8 11 7 11 9 |MD 25 25 25 28 26 23 25 28 26 27 29 24
Table 3.2292.3 GPS week: 2292 Day: 3 MJD: 60291.000
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 | 12 11 9 11 7 5 --- 10 10 21 --- 5 | 23 22 22 23 19 21 --- 23 21 26 --- 20
2 | 9 7 6 9 6 4 7 10 13 19 15 4 | 16 18 19 23 17 19 19 19 22 25 24 18
3E | 7 11 14 22 16 3 7 15 13 19 17 6 | 296 295 296 299 297 294 295 22 295 292 295 297
4M | 8 12 8 9 6 3 6 49 7 14 11 3 | 32 31 33 31 34 33 32 50 37 35 40 33
5E | 9 13 10 9 18 7 12 8 21 13 17 5 | 65 62 61 59 64 62 61 62 69 67 67 63
6 | 8 9 8 5 5 3 7 9 7 7 9 2 | 25 23 24 26 22 24 22 24 24 25 25 23
7 | 7 10 7 6 5 4 12 11 6 8 9 3 | 36 35 35 37 32 35 31 35 35 32 36 34
8 | 8 10 10 9 7 4 9 11 6 15 16 3 | 20 20 24 19 20 19 21 21 21 19 23 19
9M | 5 10 9 7 6 2 5 9 7 9 12 3 | 22 24 24 22 18 21 19 25 23 21 26 20
10E | 9 10 12 19 17 4 7 13 10 14 14 5 | 39 39 39 36 41 37 37 36 40 38 41 37
11 | 11 17 8 11 5 3 9 60 8 13 11 3 | 16 21 21 27 23 19 19 28 22 19 26 20
12 | 13 13 8 11 13 4 17 11 11 10 11 5 | 27 24 21 26 26 23 22 26 24 25 26 23
13 | 5 13 9 8 5 3 7 12 6 8 15 2 | 24 32 21 28 29 25 25 33 29 25 26 25
14 | 8 10 16 6 8 3 11 60 6 13 9 4 | 31 33 39 34 38 33 31 54 32 31 39 33
15 | 10 8 7 7 9 3 9 8 8 12 16 3 | 36 38 40 41 36 38 39 41 39 39 44 38
16 | 8 13 9 14 11 5 11 11 9 16 13 4 | 24 19 20 30 20 20 23 22 25 19 22 21
17 | 7 11 6 6 6 4 7 14 6 9 9 2 | 31 28 25 29 26 26 27 30 28 27 30 27
18 | 12 13 7 6 9 4 11 50 8 12 10 4 | 80 77 79 75 76 76 76 82 81 76 80 77
19 | 8 11 6 9 5 3 9 13 7 10 11 3 | 23 20 20 24 20 20 20 21 21 23 25 20
20E | 9 15 8 11 10 4 7 13 8 12 12 3 | 27 25 26 25 26 25 25 27 29 28 30 25
21 | 10 6 7 7 7 3 9 8 9 17 13 4 | 16 20 19 20 17 18 19 19 20 24 23 18
22 | 6 9 7 13 7 3 9 13 5 11 8 3 | 24 23 23 27 22 23 23 26 23 23 29 22
23E | 11 11 25 22 21 5 9 56 34 14 34 9 | 49 53 54 55 56 52 51 52 59 54 61 51
24 | 5 17 8 11 7 4 6 15 8 13 10 3 | 21 34 23 30 20 24 20 36 22 22 23 21
25 | 9 8 11 9 8 3 7 10 9 12 13 4 | 24 25 27 26 24 24 20 28 23 22 27 23
26 | 7 9 9 9 6 5 7 10 8 14 9 3 | 22 22 24 23 22 20 20 25 24 20 24 20
27 | 46 15 12 14 9 3 12 16 11 11 13 8 | 372 359 356 358 356 358 361 358 360 358 358 359
X28 | 7 20 4 --- 4 5 11 51 5 13 7 3 | 42 25 42 --- 43 42 44 62 44 43 44 43
29 | 8 12 8 6 9 5 15 10 8 15 12 4 | 31 25 28 30 31 29 27 27 31 28 33 29
30 | 6 13 8 9 6 4 6 14 7 6 10 2 | 16 28 19 20 17 19 16 28 18 17 24 16
31 | 8 9 7 7 4 4 9 11 5 15 10 3 | 90 88 89 84 88 88 87 92 88 88 88 88
32 | 6 10 8 6 8 4 8 12 7 10 10 3 | 23 27 24 21 22 22 21 28 20 20 25 21
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 12 11 10 11 10 4 9 25 11 13 13 |T 50 50 50 51 50 49 50 45 51 50 54 49
WRMS | 8 11 10 10 8 4 9 25 8 11 11 |NE 44 44 44 45 43 43 44 47 44 43 48 43
MEDI | 8 11 8 9 7 4 9 12 8 13 11 |MD 25 25 24 28 26 24 25 28 25 25 29 23
Table 3.2292.4 GPS week: 2292 Day: 4 MJD: 60292.000
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 14 9 8 7 6 --- --- 14 16 --- 5 | 21 26 24 20 22 21 --- --- 29 23 --- 21
2 | 7 11 6 10 10 4 8 9 17 14 14 4 | 16 18 18 21 19 18 21 18 25 20 25 18
3E | 31 79 32 29 147 32 83 --- 23 37 39 15 | 628 630 632 627 572 630 633 --- 645 632 640 632
4 | 7 13 10 6 6 5 8 50 13 16 13 4 | 23 25 24 25 26 23 24 36 31 27 29 24
5E | 6 10 6 9 16 6 8 15 9 27 12 5 | 40 43 40 41 48 41 44 43 43 50 44 41
6 | 5 10 8 10 5 3 8 8 9 9 9 3 | 25 26 25 24 23 23 23 26 25 24 23 23
7 | 5 13 7 9 6 2 8 12 8 11 11 3 | 40 39 39 39 34 38 38 38 39 35 37 38
8 | 6 12 9 9 5 3 7 10 6 12 10 3 | 27 27 29 24 27 26 26 29 27 27 28 26
9 | 6 11 11 7 4 3 7 8 12 14 11 3 | 38 38 38 36 36 36 38 37 43 35 40 37
10E | 20 15 14 22 17 5 7 23 15 19 23 7 | 39 38 38 37 39 37 36 43 38 42 39 35
11 | 7 12 10 11 7 3 9 63 8 11 9 3 | 25 27 27 30 29 26 27 34 32 25 30 27
12 | 20 14 9 17 13 6 18 11 10 17 11 6 | 38 29 28 35 32 29 29 30 31 32 29 30
13 | 5 12 9 6 6 2 8 14 7 9 17 3 | 21 29 20 22 25 21 23 33 25 22 22 22
14 | 8 12 17 8 8 3 10 61 7 16 9 4 | 36 35 39 38 41 36 31 54 35 37 41 36
15 | 6 9 5 7 8 3 8 10 10 15 14 3 | 57 53 53 55 52 54 56 55 52 59 49 55
16 | 8 11 9 10 8 4 15 10 8 16 10 4 | 25 23 24 29 27 25 26 27 28 27 27 25
17 | 8 14 8 9 6 4 7 13 7 12 6 3 | 33 30 25 30 28 28 25 32 27 30 28 28
18 | 8 15 9 8 7 4 12 50 10 15 14 4 | 25 27 24 29 31 28 31 27 28 23 21 26
19 | 8 13 7 13 7 3 9 11 10 11 8 3 | 28 25 26 31 24 26 25 27 27 25 28 26
20E | 8 10 8 10 7 3 9 10 9 19 12 4 | 30 27 30 32 27 29 29 30 33 36 32 29
21 | 9 10 5 9 8 3 9 10 13 13 12 4 | 17 20 18 22 19 18 20 20 24 20 23 18
22 | 5 10 7 8 8 4 8 13 7 13 9 3 | 26 23 22 26 24 23 24 27 24 23 26 23
23E | 18 17 16 13 15 6 18 52 40 22 66 8 | 69 70 72 68 69 68 66 71 81 69 96 69
24 | 6 12 8 14 6 4 9 15 9 20 12 4 | 23 37 28 35 25 28 24 36 27 28 28 26
25 | 6 9 11 9 7 3 8 12 11 10 11 3 | 27 31 31 30 30 28 25 33 30 31 27 28
X26 | 1 --- --- --- --- 10 --- --- --- --- --- 0 | 27 --- --- --- --- 27 --- --- --- --- --- 27
27 | 7 10 7 8 4 2 6 10 7 13 18 3 | 402 401 401 403 400 402 399 402 402 403 398 402
X28 | 5 24 5 --- 8 4 8 53 7 12 11 3 | 73 53 71 --- 72 71 70 81 74 73 73 72
29 | 7 12 7 7 8 3 14 13 16 15 13 4 | 43 37 39 43 40 41 40 40 43 44 41 40
30 | 6 17 7 8 7 3 6 14 10 10 10 3 | 25 33 24 24 21 23 23 30 25 22 24 23
31 | 5 11 7 8 7 3 9 11 10 14 13 3 | 237 236 234 238 235 235 236 236 238 236 238 236
32 | 4 10 8 7 7 3 9 11 6 9 11 3 | 28 31 29 27 27 27 29 30 24 27 23 27
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 10 19 11 12 28 7 18 26 13 16 19 |T 69 70 70 71 68 68 71 56 72 71 73 68
WRMS | 8 19 11 13 9 4 18 28 9 12 12 |NE 47 48 47 49 48 46 49 52 49 48 49 46
MEDI | 7 12 8 9 7 3 8 12 10 14 11 |MD 28 31 29 30 29 28 29 33 31 30 29 27
Table 3.2292.5 GPS week: 2292 Day: 5 MJD: 60293.000
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 16 8 8 5 4 --- 9 9 8 --- 3 | 25 27 27 26 23 26 --- 26 23 23 --- 24
2 | 6 14 6 10 8 4 10 9 16 10 9 4 | 20 21 21 25 18 21 20 20 21 20 20 19
3E | 12 26 16 39 29 7 12 --- 16 22 12 9 | 433 427 428 422 429 430 425 --- 433 428 434 430
4 | 8 12 7 4 7 4 10 50 10 14 11 3 | 44 44 46 45 45 44 46 51 49 42 50 44
5E | 6 13 7 7 7 5 11 10 9 23 13 4 | 107 110 107 105 110 108 109 108 105 108 106 107
6 | 6 14 9 12 6 3 9 8 8 12 10 3 | 31 33 30 28 26 29 28 31 27 27 30 27
7 | 6 9 6 8 6 3 12 11 6 14 8 3 | 40 44 42 41 39 39 39 44 40 38 40 40
8 | 7 18 8 11 5 4 8 12 9 12 11 3 | 23 22 24 23 21 22 21 21 21 20 21 21
9 | 7 11 9 7 7 3 9 7 8 15 8 3 | 26 33 29 29 28 26 28 31 28 24 26 27
10E | 19 32 13 26 24 7 13 --- 18 17 29 8 | 81 77 81 80 80 77 78 --- 82 83 86 79
11 | 8 15 10 6 7 4 9 60 8 11 8 3 | 32 32 31 32 32 30 32 31 31 28 31 30
12 | 8 12 7 10 14 4 16 8 7 10 9 4 | 25 24 22 27 29 23 23 26 25 29 24 24
13 | 5 14 7 5 4 2 10 12 6 10 12 2 | 19 28 18 18 19 18 18 29 20 20 20 18
14 | 7 11 14 7 7 3 11 60 6 13 8 4 | 36 35 39 38 38 37 34 52 36 39 39 36
15 | 7 11 6 8 9 2 10 9 7 13 12 3 | 43 45 45 46 43 43 43 46 43 48 41 43
16 | 7 15 7 11 10 5 13 11 9 13 14 4 | 22 21 22 30 25 22 24 26 25 24 22 23
17 | 7 13 6 9 5 4 10 12 6 10 6 3 | 36 38 32 36 33 33 31 33 31 32 32 32
18 | 8 14 8 6 7 2 12 50 9 14 11 3 | 40 44 41 43 41 41 43 42 40 41 41 40
19 | 9 13 5 9 5 3 11 9 8 11 5 3 | 25 22 21 25 24 22 21 23 22 23 25 22
20E | 7 13 10 9 7 4 10 9 9 23 13 4 | 47 42 42 43 44 44 43 41 44 48 46 43
21 | 6 13 5 9 7 3 10 10 10 9 10 3 | 19 24 22 24 20 21 21 22 19 22 20 20
22 | 6 9 7 9 8 4 11 9 7 13 8 3 | 22 19 20 24 22 21 22 22 22 23 24 21
23E | 20 20 17 18 12 5 20 48 22 21 21 7 | 104 104 108 109 107 105 101 106 111 110 111 106
24 | 5 19 9 8 6 4 10 15 7 10 8 3 | 19 33 21 21 17 20 18 32 18 15 19 17
25 | 7 14 11 4 7 2 9 9 6 10 10 3 | 24 24 26 25 24 23 23 25 24 22 22 23
X26 | 8 --- 8 8 --- 4 --- --- 7 --- --- 4 | 18 --- 19 17 --- 16 --- --- 16 --- --- 16
27 | 6 15 7 8 4 3 8 12 8 13 10 3 | 382 384 383 385 383 384 384 383 381 382 383 383
X28 | 7 22 5 --- 6 3 9 52 5 9 9 3 | 117 121 119 --- 121 120 120 122 121 120 120 119
29 | 6 13 6 6 8 3 16 11 8 12 9 3 | 42 41 42 44 40 43 41 42 41 48 42 41
30 | 5 15 6 7 7 4 8 14 9 9 11 3 | 27 34 29 29 29 27 26 37 25 29 29 27
31 | 6 14 8 4 5 2 10 9 8 11 7 3 | 376 379 374 375 378 376 377 375 380 377 378 376
32 | 6 14 9 5 5 3 10 8 6 9 7 3 | 23 32 26 23 21 23 23 27 20 27 24 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 15 9 12 10 4 11 25 10 14 12 |T 72 76 73 72 74 72 75 64 72 74 76 71
WRMS | 7 15 8 9 7 4 11 25 8 11 9 |NE 46 49 46 47 47 45 48 50 45 48 49 45
MEDI | 7 14 7 8 7 4 10 11 8 12 10 |MD 31 34 30 30 32 29 31 32 28 29 31 27
Table 3.2292.6 GPS week: 2292 Day: 6 MJD: 60294.000
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 | 6 12 9 8 4 5 --- 11 9 9 --- 3 | 21 25 25 22 21 23 --- 23 23 23 --- 21
2 | 6 12 7 11 11 4 11 10 15 11 9 4 | 17 21 20 24 19 19 19 19 25 21 24 18
3E | 10 13 20 33 10 4 16 --- 11 17 17 7 | 451 453 450 458 437 452 453 --- 453 451 452 451
4 | 6 15 8 8 8 5 12 48 10 10 12 3 | 151 150 151 153 152 151 151 155 154 151 152 152
5E | 6 11 10 9 6 3 14 9 13 11 18 4 | 127 130 127 127 131 127 127 130 132 129 132 128
6 | 5 13 9 9 7 3 11 8 6 9 11 3 | 29 28 31 27 27 28 29 30 30 28 33 28
7 | 5 8 6 6 7 3 13 7 6 10 9 3 | 45 47 46 44 40 45 45 47 45 45 42 44
8 | 8 15 9 8 8 3 13 9 9 10 10 3 | 25 26 26 23 25 23 23 26 24 24 26 23
9 | 7 9 10 10 6 4 11 9 9 14 11 3 | 33 36 34 36 30 32 35 37 34 30 32 32
10E | 10 13 12 28 8 5 10 --- 12 15 23 6 | 67 68 68 71 68 67 64 --- 67 69 71 66
11 | 7 14 10 7 7 3 12 59 6 12 9 3 | 48 49 50 48 50 47 48 56 50 48 50 48
12 | 6 12 8 9 12 3 17 11 9 9 12 4 | 30 27 23 30 33 27 28 28 29 30 28 28
13 | 4 15 8 8 5 3 13 12 5 10 9 3 | 20 31 17 18 23 19 22 29 23 24 22 20
14 | 6 11 13 6 8 3 15 58 8 11 7 4 | 49 44 55 50 54 50 44 71 44 51 53 49
15 | 6 11 5 8 9 3 11 10 8 14 13 3 | 62 60 62 63 57 61 63 61 58 67 59 61
16 | 4 14 6 8 9 5 15 11 8 9 8 3 | 22 24 23 29 25 21 23 24 25 26 24 23
17 | 7 12 7 12 5 4 13 13 6 10 10 3 | 35 36 34 38 34 34 30 36 33 33 39 33
18 | 7 15 8 6 8 2 13 51 10 14 14 3 | 41 47 43 45 44 43 44 44 43 40 45 42
19 | 7 12 7 13 5 3 14 11 8 10 8 3 | 28 25 26 33 27 27 26 28 27 28 30 27
20E | 7 14 9 10 8 4 12 8 8 11 10 3 | 61 56 60 61 60 60 57 57 62 62 62 60
21 | 5 12 5 10 7 3 12 8 8 11 7 3 | 17 22 20 24 18 19 19 20 22 21 22 18
22 | 5 9 8 8 5 4 14 10 6 10 7 3 | 22 19 20 25 22 22 24 20 20 22 23 20
23E | 14 16 18 12 14 5 18 50 19 29 21 7 | 122 118 123 120 121 121 118 121 120 128 121 121
24 | 4 16 10 8 5 3 11 13 6 12 9 3 | 22 35 26 25 23 24 22 35 26 25 25 23
25 | 5 10 11 8 7 2 11 10 6 11 10 3 | 30 30 28 30 31 28 26 30 30 27 30 28
26 | 5 10 8 6 6 3 13 11 7 7 7 3 | 17 18 19 17 14 16 15 18 16 14 15 15
27 | 6 17 7 8 4 3 9 11 8 12 10 3 | 411 413 411 414 412 413 413 413 412 412 414 412
X28 | 5 --- 6 --- 7 4 10 52 7 9 7 3 | 243 --- 241 --- 241 242 242 247 241 242 242 241
29 | 7 15 6 7 9 3 17 14 10 12 10 4 | 46 45 45 47 43 45 43 45 45 45 50 44
30 | 5 15 7 5 7 3 12 13 7 7 9 3 | 26 37 28 29 30 28 27 37 30 28 31 27
31 | 4 9 7 6 5 2 12 10 7 10 7 3 | 502 504 499 500 501 501 502 499 502 500 503 501
32 | 6 11 9 10 8 4 15 10 5 13 7 3 | 27 32 30 28 25 29 32 33 24 30 26 27
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 13 9 11 8 4 13 24 9 12 12 |T 88 85 89 85 88 88 90 80 89 89 92 88
WRMS | 6 13 9 9 7 3 13 24 8 10 9 |NE 50 52 51 52 50 50 52 54 50 51 54 50
MEDI | 6 12 8 8 7 3 13 11 8 11 10 |MD 33 36 34 36 33 32 35 36 33 30 39 32
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 4.2292 GPS week: 2292 MJD: 60288.0-60294.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 10 11 24 |U 14 18 45 |U 9 8 25 |
emr | emr 3022 |U 17 17 38 |U 20 30 76 | 15 17 46 |
esa | esa 3058 | 10 15 45 |U 14 20 64 |U 15 15 41 |
gfz | gfz 2961 |U 10 12 32 |U 13 16 46 | 11 9 30 |
grg | grg 3044 |U 11 11 32 |U 14 21 64 | 9 8 31 |
igr | igr 3054 | 9 10 28 | 13 17 48 | 10 9 28 |
igs | igs 3055 | 9 11 25 | 13 17 45 | 9 8 28 |
jgx | jgx 2948 |U 11 14 27 |U 14 17 56 | 11 9 30 |
jpl | jpl 2962 | 15 20 44 | 16 22 51 | 15 17 58 |
mit | mit 3058 |U 114 94 281 |U 78 83 215 |U 35 41 188 |
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 5.2292.0 GPS week: 2292 Day: 0 MJD: 60288.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 11 26 | 14 18 41 | 9 7 20 |
emr | emr 3072 | 10 12 34 | 15 21 52 | 12 13 42 |
esa | esa 3072 | 11 18 51 | 16 21 57 | 16 16 41 |
gfz | gfz 2976 | 10 11 33 | 14 16 42 | 11 7 28 |
grg | grg 3072 | 9 11 35 | 13 16 50 | 9 7 28 |
igr | igr 3072 | 8 11 30 | 13 18 45 | 9 9 26 |
igs | igs 3072 | 8 10 29 | 13 17 43 | 10 7 26 |
jgx | jgx 2976 | 8 11 27 | 13 17 43 | 8 7 30 |
jpl | jpl 3072 | 14 14 47 | 17 24 53 | 15 16 61 |
mit | mit 3072 | 421 210 1059 | 148 60 346 | 117 86 711 |
Table 5.2292.1 GPS week: 2292 Day: 1 MJD: 60289.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 10 21 | 18 21 53 | 9 9 23 |
emr | emr 3071 | 9 9 29 | 21 26 65 | 10 15 41 |
esa | esa 3072 | 10 15 46 | 20 21 63 | 16 18 44 |
gfz | gfz 2975 | 9 8 24 | 17 18 51 | 9 10 30 |
grg | grg 3072 | 8 10 26 | 19 22 52 | 7 9 32 |
igr | igr 3072 | 9 9 26 | 17 20 51 | 9 11 29 |
igs | igs 3072 | 8 9 23 | 17 20 52 | 9 10 29 |
jgx | jgx 2976 | 8 10 22 | 18 18 53 | 8 9 30 |
jpl | jpl 3072 | 13 15 41 | 22 26 55 | 14 16 56 |
mit | mit 3072 | 9 10 28 | 22 35 60 | 13 17 50 |
Table 5.2292.2 GPS week: 2292 Day: 2 MJD: 60290.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 11 24 | 16 25 40 | 7 9 21 |
emr | emr 3072 | 20 41 43 | 19 28 52 | 19 16 59 |
esa | esa 3072 | 10 15 51 | 15 29 56 | 13 15 42 |
gfz | gfz 2971 | 9 9 29 | 14 24 45 | 8 8 26 |
grg | grg 3072 | 8 8 32 | 16 25 49 | 7 8 30 |
igr | igr 3072 | 8 10 29 | 16 26 44 | 7 9 27 |
igs | igs 3062 | 8 11 28 | 15 25 43 | 7 9 26 |
jgx | jgx 2976 | 11 21 28 | 17 24 43 | 11 14 38 |
jpl | jpl 3072 | 20 35 51 | 20 29 51 | 23 15 71 |
mit | mit 3072 | 10 22 39 | 16 27 64 | 8 13 49 |
Table 5.2292.3 GPS week: 2292 Day: 3 MJD: 60291.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 8 25 | 17 15 51 | 10 6 25 |
emr | emr 3062 | 9 10 33 | 16 20 58 | 17 16 51 |
esa | esa 3072 | 8 13 45 | 17 16 61 | 15 15 41 |
gfz | gfz 2976 | 9 11 33 | 14 13 46 | 10 7 33 |
grg | grg 3072 | 7 8 26 | 14 14 55 | 8 8 32 |
igr | igr 3072 | 7 7 26 | 15 15 53 | 9 8 29 |
igs | igs 3072 | 7 6 24 | 15 14 52 | 9 7 29 |
jgx | jgx 2976 | 8 8 24 | 15 15 49 | 10 7 29 |
jpl | jpl 3072 | 11 13 44 | 18 24 62 | 14 12 59 |
mit | mit 3072 | 286 351 707 | 310 380 726 | 67 131 342 |
Table 5.2292.4 GPS week: 2292 Day: 4 MJD: 60292.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 11 11 31 | 9 15 41 | 11 9 33 |
emr | emr 2961 | 35 20 59 | 21 56 162 | 15 16 53 |
esa | esa 2976 | 9 17 43 | 8 17 51 | 18 16 44 |
gfz | gfz 2880 | 10 15 36 | 10 12 38 | 12 8 32 |
grg | grg 2976 | 18 16 42 | 13 11 87 | 12 8 35 |
igr | igr 2976 | 10 7 27 | 9 14 46 | 11 7 31 |
igs | igs 2976 | 9 11 29 | 8 13 33 | 11 7 31 |
jgx | jgx 2880 | 14 20 29 | 17 16 104 | 15 8 36 |
jpl | jpl 2784 | 18 23 48 | 15 24 52 | 16 20 58 |
mit | mit 2976 | 18 24 47 | 25 40 91 | 13 13 62 |
Table 5.2292.5 GPS week: 2292 Day: 5 MJD: 60293.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 16 21 | 10 9 28 | 9 8 26 |
emr | emr 2960 | 18 13 38 | 34 45 104 | 15 23 43 |
esa | esa 3072 | 11 14 44 | 12 14 76 | 15 16 42 |
gfz | gfz 2976 | 11 14 44 | 8 9 32 | 11 10 30 |
grg | grg 2976 | 11 11 44 | 12 29 73 | 10 9 30 |
igr | igr 3047 | 10 12 39 | 7 8 32 | 11 11 29 |
igs | igs 3062 | 9 15 25 | 8 8 29 | 10 9 28 |
jgx | jgx 2880 | 12 13 40 | 8 9 34 | 10 9 22 |
jpl | jpl 2784 | 16 23 43 | 11 12 39 | 15 22 53 |
mit | mit 3072 | 34 25 57 | 10 14 61 | 12 11 39 |
Table 5.2292.6 GPS week: 2292 Day: 6 MJD: 60294.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 13 20 | 11 22 58 | 10 7 25 |
emr | emr 2959 | 18 18 30 | 12 15 41 | 15 21 36 |
esa | esa 3072 | 11 16 34 | 14 19 81 | 12 14 37 |
gfz | gfz 2975 | 15 14 25 | 13 22 70 | 13 11 29 |
grg | grg 3072 | 15 15 23 | 14 29 83 | 12 9 29 |
igr | igr 3072 | 14 14 21 | 11 23 68 | 12 10 27 |
igs | igs 3071 | 12 13 20 | 11 24 66 | 10 9 27 |
jgx | jgx 2976 | 14 14 21 | 13 23 70 | 13 9 26 |
jpl | jpl 2880 | 15 18 34 | 12 17 48 | 12 17 49 |
mit | mit 3072 | 18 15 30 | 14 27 159 | 13 15 63 |
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 6.2292 GPS week: 2292 MJD: 60288.500-60294.500
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 | -2 17 43 -85 -1 | -5 17
| 5 24 58 54 2 | 1
emr xxxxx | 7 3 -33 81 18 | -11 23
| 42 21 112 140 20 | 4
esa uuuuu | 8 14 -12 80 1 | 12 20
| 14 6 54 49 5 | 1
gfz uuuuu | -16 -28 87 30 -1 | 10 18
| 9 23 92 95 2 | 1
grg uuuuu | -4 12 -28 43 -4 | 14 22
| 10 5 54 97 3 | 2
igr xxxxx | -12 -9 -8 14 3 | 2 15
| 11 7 38 21 8 | 1
irf xxxxx | -17 -1 -21 -8 0 | 3 17
| 11 11 29 16 4 | 1
jgx uuuuu | 17 -36 -29 -49 0 | 10 20
| 9 14 39 30 5 | 1
mit uuuuu | -18 8 -52 -59 2 | 22 28
| 11 15 53 37 7 | 1
ngs uuuuu | 33 -4 7 116 3 | 15 23
| 19 26 178 191 8 | 1
sio xxxxx | 58 -49 -70 -98 5 | 42 46
| 34 41 102 75 11 | 2
Table 7.2292.0 GPS week: 2292 Day: 0 MJD: 60288.500
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 50 59 -34 -3 | -6 20
emr xxxxx | -6 18 -31 -29 10 | -15 26
esa uuuuu | 13 13 12 15 3 | 11 22
gfz uuuuu | -2 -35 192 116 -2 | 10 20
grg uuuuu | -3 3 -86 48 1 | 15 25
igr xxxxx | -2 -7 18 41 2 | 0 18
irf xxxxx | -15 7 18 -18 1 | 2 20
jgx uuuuu | 28 -28 28 -48 5 | 8 21
mit uuuuu | -17 4 -32 -48 4 | 20 28
ngs uuuuu | -2 -21 -212 -62 -10 | 16 27
sio xxxxx | 62 -79 -159 -185 -5 | 41 46
Table 7.2292.1 GPS week: 2292 Day: 1 MJD: 60289.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 3 33 -26 -72 -1 | -5 20
emr xxxxx | -31 25 31 88 4 | -13 25
esa uuuuu | 9 14 40 105 0 | 12 22
gfz uuuuu | -14 -64 195 -10 -3 | 11 20
grg uuuuu | -11 12 46 127 -5 | 17 25
igr xxxxx | -16 -6 -54 20 1 | 2 17
irf xxxxx | -27 8 -20 -20 0 | 3 19
jgx uuuuu | 30 -53 -9 -64 4 | 9 21
mit uuuuu | -30 28 -75 -81 4 | 21 29
ngs uuuuu | 33 0 -202 13 4 | 14 25
sio xxxxx | 21 -29 1 -8 6 | 41 46
Table 7.2292.2 GPS week: 2292 Day: 2 MJD: 60290.500
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 | -1 11 -20 -82 2 | -4 19
emr xxxxx | -10 -8 89 -24 8 | -12 24
esa uuuuu | -3 14 -45 87 -5 | 13 22
gfz uuuuu | -16 -39 159 202 -1 | 11 20
grg uuuuu | 18 8 -84 136 -5 | 16 25
igr xxxxx | -22 -22 -44 -7 0 | 3 17
irf xxxxx | -24 -10 2 -15 1 | 3 20
jgx uuuuu | 17 -54 -26 -91 3 | 10 22
mit uuuuu | -34 15 48 -98 7 | 22 29
ngs uuuuu | 42 34 8 -107 0 | 15 25
sio xxxxx | 23 5 -129 -135 10 | 41 46
Table 7.2292.3 GPS week: 2292 Day: 3 MJD: 60291.500
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 | 7 29 144 -82 -2 | -4 19
emr xxxxx | -43 -5 3 65 2 | -11 24
esa uuuuu | -18 5 -84 18 -4 | 13 22
gfz uuuuu | -22 -41 58 -50 1 | 11 21
grg uuuuu | -10 12 -70 148 -4 | 16 25
igr xxxxx | -31 -11 -36 -14 -5 | 5 17
irf xxxxx | -28 -18 -5 -30 1 | 3 20
jgx uuuuu | 18 -36 3 -72 3 | 12 22
mit uuuuu | -15 10 -29 -70 7 | 23 30
ngs uuuuu | 60 29 1 143 2 | 16 24
sio xxxxx | 54 -89 -117 18 3 | 42 47
Table 7.2292.4 GPS week: 2292 Day: 4 MJD: 60292.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -3 -22 53 -82 0 | -7 16
emr xxxxx | 20 20 48 -67 23 | -14 23
esa uuuuu | 11 25 34 81 1 | 10 18
gfz uuuuu | -32 -9 30 -39 -4 | 9 16
grg uuuuu | -8 18 -36 -75 -8 | 12 18
igr xxxxx | 1 -9 47 1 -3 | 1 12
irf xxxxx | -6 11 -28 11 4 | 1 16
jgx uuuuu | 11 -16 -60 -44 -6 | 9 19
mit uuuuu | -1 1 -84 -47 8 | 21 27
ngs uuuuu | 38 -5 70 401 17 | 13 20
sio xxxxx | 97 -31 114 -150 23 | 39 43
Table 7.2292.5 GPS week: 2292 Day: 5 MJD: 60293.500
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 25 66 -199 0 | -5 12
emr xxxxx | 75 -37 -211 304 58 | -9 17
esa uuuuu | 27 15 -72 152 6 | 12 16
gfz uuuuu | -10 -10 -15 -37 -1 | 9 15
grg uuuuu | -12 14 21 -69 -6 | 13 18
igr xxxxx | -9 1 -5 32 19 | 2 11
irf xxxxx | -20 -7 -61 4 -3 | 3 11
jgx uuuuu | 4 -25 -77 -12 -5 | 11 17
mit uuuuu | -20 -20 -114 12 -2 | 24 26
ngs uuuuu | 31 -30 306 329 7 | 16 19
sio xxxxx | 41 -104 -164 -101 12 | 44 45
Table 7.2292.6 GPS week: 2292 Day: 6 MJD: 60294.500
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 -6 23 -44 1 | -6 12
emr xxxxx | 46 7 -161 232 19 | -2 19
esa uuuuu | 16 10 33 103 7 | 12 16
gfz uuuuu | -19 0 -8 25 0 | 9 15
grg uuuuu | -3 15 11 -13 1 | 12 17
igr xxxxx | -6 -9 19 26 8 | 4 12
irf xxxxx | 1 -1 -52 9 -8 | 3 11
jgx uuuuu | 13 -40 -64 -12 -5 | 11 17
mit uuuuu | -9 20 -80 -84 -11 | 24 26
ngs uuuuu | 29 -32 79 93 -1 | 17 20
sio xxxxx | 107 -15 -35 -125 -9 | 45 47
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