[IGSREPORT-30064] Wk 2328 IGS Final Orbits
acc
acc at igs.org
Sun Sep 8 22:37:49 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2328 (Aug 18, 2024 - Aug 24, 2024)
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_20242310000_07D_01D_SUM.SUM Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, ESA, GFZ, and GRG.
The other centres are excluded because of either poorer consistency, or 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 | ASCG JFNG JFNG
0 | ESA | CHUR CHUR
0 | GFZ | PTVL PTVL
0 | GRG | 21 21 ASCG DAV1 TONG COCO DAV1 TONG
0 | MIT | CKSV DARW FLRS JOZ2 TLSE VNDP CKSV DARW FLRS JOZ2
0 | MIT | TLSE VNDP
1 | COD | HRAO SCUB CZTG HRAO
1 | ESA | AREQ CHUR MAW1 CHUR MAW1
1 | GFZ | LAUT LAUT
1 | GRG | AREQ CZTG JFNG TONG AREQ COCO CZTG JFNG SGOC TONG
1 | MIT | HERS JOZ2 METG REYK VNDP HERS JOZ2 METG REYK VNDP
2 | COD | SGOC WTZR SGOC WTZR
2 | EMR | HRAO HRAO
2 | ESA | CHUR CHUR
2 | GRG | 19 TONG COCO SCUB TONG
2 | JGX | HERS
2 | MIT | HERS SFER STJ3 TONG YAR3 HERS SFER STJ3 TONG YAR3
3 | COD | CHUR CKIS CKIS FAA1
3 | ESA | HRAO JFNG HRAO JFNG
3 | GFZ | HRAO HRAO
3 | GRG | 21 21 TONG TONG
3 | JGX | HERS JFNG JFNG
3 | MIT | CHTI LMMF MEDI PDEL RGDG STJ3 TONG CHTI LMMF MEDI
3 | MIT | PDEL RGDG STJ3 TLSE TONG
4 | COD | ASCG DAV1 LMMF PIE1 SEYG DAV1
4 | EMR | BADG
4 | ESA | GOLD THTG GOLD SEYG THTG
4 | GRG | 24 24 FAA1 JFNG MAYG TONG FAA1 JFNG TONG
4 | MIT | FLRS JOZ2 PDEL REYK SFER SVTL FLRS HERS JOZ2 PDEL
4 | MIT | REYK SFER SVTL
5 | COD | ADIS ASCG CZTG JFNG PDEL ADIS
5 | ESA | 4 11 18 21 CZTG JFNG
5 | GFZ | LAUT ALGO AREQ ASCG BAKE BRFT BRUX CCJ2 CHPI CHTI
5 | GFZ | CHUR CKIS COCO CPVG CRO1 CZTG DAEJ DAV1 DGAR DJIG
5 | GFZ | DRAO FAIR FALK GAMB GLPS GODE GOLD GUAM GUAT HOB2
5 | GFZ | HOFN HRAO INVK JFNG JOG2 KIRI KIRU KOUR LAUT MAC1
5 | GFZ | MADR MAL2 MAS1 MATE MAW1 MAYG MKEA NKLG NLIB NYA2
5 | GFZ | OUS2 PDEL PIE1 POL2 POVE PTVL QAQ1 REUN RIO2 SANT
5 | GFZ | SCOR SEYG STHL SUTH SYOG TASH THU2 TONG TOW2 TWTF
5 | GFZ | UNSA WARK WHIT WTZR YELL
5 | JGX | NRMD
5 | MIT | GAMG IISC SFER TLSE VNDP YEBE GAMG SFER TLSE VNDP
5 | MIT | YEBE
6 | COD | ASCG LAUT
6 | ESA | SVTL
6 | GRG | SVTL TONG
6 | JGX | CHUR
6 | MIT | BRST IISC KITG MAR6 SFER STJ3 YAR3 YEL2 BRST IISC
6 | MIT | KITG MAR6 SFER STJ3 YAR3 YEL2
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
5 | GFZ | ~09:00 | ~ 0.52 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following orbit solutions were excluded from the combination because they
were biasing the weighted average (generally indicated by long arc RMS). They
were still used for statistics computation.
Day | Centre | PRN list
----+--------+---------------
4 | GRG | 24
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G24 | 4 | 4 | 4 | 4 | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
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.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | 1.4 -.5 1.5 0 17 -18 -.12
EMR | 0 | 5.0 1.1 -19.9 11 -8 15 -.22
ESA | 0 | -.8 -.0 .3 20 -27 -1 -.26
GFZ | 0 | -.5 -.9 -.5 -15 -16 12 .27
GRG | 0 | .7 -.4 -1.5 17 -14 23 -.04
JGX | 0 | 2.0 2.4 .6 9 -20 28 -.08
JPL | 0 | 2.1 -.1 .4 8 50 -36 .48
MIT | 0 | 1.6 .2 21.5 27 -4 -3 -.01
NGS | 0 | 6.1 .1 7.1 -22 4 8 -.07
SIO | 0 | 1.5 6.5 -2.4 116 83 -70 -.00
COD | 1 | 1.7 -.5 1.6 17 1 -18 -.02
EMR | 1 | 6.1 -6.7 -18.8 5 -5 20 -.13
ESA | 1 | -.9 -.3 .3 10 -25 9 -.52
GFZ | 1 | -.1 -.3 -.2 -9 -27 3 .18
GRG | 1 | .6 -.7 -1.4 13 -5 29 -.12
JGX | 1 | 3.9 5.7 -1.0 11 -11 25 -.29
JPL | 1 | .7 -4.9 1.7 -5 55 -61 .58
MIT | 1 | 4.3 -.8 25.4 -12 -17 -14 -.28
NGS | 1 | 6.7 3.7 4.4 -5 -4 30 -.27
SIO | 1 | 3.2 4.8 -.4 108 26 -21 -.43
COD | 2 | 1.2 -.6 1.1 7 1 -7 -.22
EMR | 2 | 9.3 -5.2 -15.1 -3 -1 14 -.35
ESA | 2 | -.2 -.8 .3 -9 -21 4 -.56
GFZ | 2 | .8 -.9 -.6 -24 -27 -1 .22
GRG | 2 | .7 -2.1 -1.3 8 -5 25 -.27
JGX | 2 | 2.6 1.5 -1.7 0 -6 9 -.34
JPL | 2 | -2.1 -4.9 2.5 -7 47 -36 .57
MIT | 2 | -.7 -1.5 24.7 -12 -4 -8 -.22
NGS | 2 | -.4 -4.9 7.8 -40 40 2 -.25
SIO | 2 | 1.4 1.4 .6 30 -70 56 -.23
COD | 3 | 1.1 -1.1 1.4 8 7 -22 -.21
EMR | 3 | 5.3 -3.5 -14.6 12 -7 14 -.02
ESA | 3 | -1.0 -.3 .7 -12 -10 -15 -.74
GFZ | 3 | -.6 -.9 -.8 -20 -11 -16 -.03
GRG | 3 | .1 -1.6 -.8 0 -3 22 -.18
JGX | 3 | -2.3 .3 -4.2 3 3 -16 -.27
JPL | 3 | 1.6 -7.2 -.8 -20 51 -65 .43
MIT | 3 | 1.0 .4 24.9 -4 -6 -6 -.24
NGS | 3 | .6 -8.9 3.7 -62 20 8 -.51
SIO | 3 | -2.3 -4.1 -5.5 -19 -12 22 -.28
COD | 4 | 1.3 -.7 1.5 9 5 -25 -.23
EMR | 4 | 5.9 -5.7 -12.9 11 -7 15 -.48
ESA | 4 | -.5 -1.0 .7 -3 -5 -15 -.65
GFZ | 4 | -.1 -.9 -.1 -17 -12 -16 -.08
GRG | 4 | .1 -1.3 -1.3 20 11 15 -.28
JGX | 4 | -2.1 -1.3 -1.9 -1 11 0 -.42
JPL | 4 | -1.4 -9.1 4.7 -18 28 -67 .44
MIT | 4 | -2.0 -3.3 25.9 -18 2 -36 -.10
NGS | 4 | -.5 -.5 7.7 -40 46 -19 -.55
SIO | 4 | -1.3 -1.4 3.2 46 -6 46 -.06
COD | 5 | 1.5 -1.0 1.0 -1 -5 -10 -.18
EMR | 5 | 4.9 -2.0 -16.9 5 2 6 -.17
ESA | 5 | -.5 .0 .4 3 -11 -7 -.62
GFZ | 5 | -.1 .1 -.4 -23 -15 -22 -.15
GRG | 5 | .2 .2 -1.5 -2 0 25 -.35
JGX | 5 | 3.2 4.1 -3.4 4 -4 1 -.19
JPL | 5 | -1.5 .0 3.0 -29 58 -40 .29
MIT | 5 | -1.9 4.4 24.8 2 -4 -1 -.45
NGS | 5 | -.5 4.1 1.2 5 26 -19 -.29
SIO | 5 | -1.6 6.5 -3.6 51 -4 69 -.22
COD | 6 | 1.2 -.7 .5 6 -8 -24 -.09
EMR | 6 | 5.0 -4.6 -11.6 8 -9 14 -.12
ESA | 6 | -.0 .0 .2 4 -21 2 -.59
GFZ | 6 | .1 -1.0 -.7 -8 -22 2 .12
GRG | 6 | .9 -1.1 -2.0 29 -10 27 -.09
JGX | 6 | 4.8 5.5 -5.2 14 -19 13 -.33
JPL | 6 | 4.2 -4.3 -4.3 -12 48 -11 .43
MIT | 6 | -.2 -.3 25.7 -14 -4 -3 -.15
NGS | 6 | 5.3 4.2 4.6 -1 -13 -7 -.15
SIO | 6 | -.0 4.7 -1.5 93 -6 56 -.23
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
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 final solution has not yet adopted IGS20/igs20.atx after GPS Week 2238,
which causes their orbit and clock residuals to be higher than for the other
centres; from GPS Week 2238 and until they switch to IGS20/igs20.atx, the JPL
solution is excluded from the weekly SINEX combination, as well as from orbit
and clock 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 1.2328.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2328.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 2.2328.[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 3.2328.[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 5.2328.0-6). 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 2328 summary. (Aug 18, 2024 - Aug 24, 2024)
Table 1.2328.a GPS week: 2328 MJD: 60540.000-60546.000
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 777| -1 0 5 13 0 -2 -.04 8 7 | -704 83 6 87
| 0 0 0 10 18 20 .02 | 76 167
emr 107| 1 0 -6 3 14 7 -.01 10 10 | -1911 211 30 107
| 0 1 1 11 7 17 .01 | 741 1022
esa 150| 0 -1 -2 -10 3 -20 .01 10 10 | -1333 277 7 86
| 0 0 0 10 10 12 .03 | 379 570
gfz 124| -1 0 1 40 14 -44 .04 9 9 | -86 -16 12 120
| 0 0 2 13 10 19 .02 | 39 72
grg 116| 1 0 3 8 10 -11 .05 13 10 | 54 -114 10 126
| 0 0 2 15 8 8 .02 | 63 83
igr n/a| 0 0 0 8 10 -8 .01 3 3 | 3487 -711 10 68
| 0 0 0 12 8 13 .02 | 1665 538
jgx n/a| 0 0 -1 8 -6 -11 -.04 13 13 | 58 -114 31 94
| 0 1 0 7 15 62 .02 | 78 81
jpl n/a| 0 -1 3 8 -16 -4 .13 26 26 | -2071 -449 88 154
| 1 1 1 9 20 11 .02 | 1262 445
mit 373| 0 0 0 -18 -26 52 .02 6 6 | -3116 -640 38 66
| 0 0 1 21 15 22 .01 | 7197 1111
ngs 277| 0 0 0 -8 -1 -21 -.11 10 9 | 8351 106 491 719
| 1 0 1 10 12 24 .01 | 8478 219
sio 338| 0 0 0 -17 4 6 -.00 8 7 | --- --- --- ---
| 0 0 1 15 19 56 .01 | --- ---
Table 1.2328.b GPS week : 2328 MJD: 60540.000-60546.000
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 5 9 6 6 5 6 |
2 | 4 4 3 4 3 5 4 |
3 | 3 3 3 3 3 3 3 |
4 | 5 4 4 4 4 4 4 |
5 | 3 3 3 3 3 3 3 |
6 | 4 4 4 3 4 3 3 |
7 | 3 3 3 3 3 3 3 |
8 | 3 3 3 3 3 3 3 |
9 | 4 4 3 4 3 4 3 |
10 | 3 3 3 3 3 3 3 |
11 | 4 4 4 4 4 4 4 |
12 | 3 3 3 3 3 3 3 |
13 | 3 4 3 3 4 4 3 |
14 | 3 3 3 3 3 3 3 |
15 | 4 4 3 4 3 4 4 |
16 | 3 3 3 3 3 3 3 |
17 | 3 4 3 3 3 3 3 |
18 | 4 4 4 4 4 4 4 |
19 | 3 3 3 3 3 3 3 |
20 | 3 3 3 3 2 3 3 |
21 | 5 4 3 3 4 5 4 |
22 | 3 3 2 3 2 3 3 |
23 | 3 3 3 3 3 3 3 |
24 | 3 3 3 3 7 3 4 |
25 | 3 3 3 3 3 3 3 |
26 | 3 3 5 3 3 3 3 |
27 | 3 3 3 3 3 3 3 |
28 | 4 4 3 3 3 4 4 |
29 | 3 3 3 3 3 3 3 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 3 3 3 3 3 |
32 | 3 4 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 2.2328.0 GPS week: 2328 Day: 0 MJD: 60540.000
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 783| -1 0 5 -8 35 30 -.03 8 8 | -825 223 7 90
emr 107| 2 1 -7 -3 17 0 -.02 10 10 | -2325 601 30 113
esa 150| 0 0 -1 1 2 -3 .01 10 11 | -1177 65 8 87
gfz 121| -1 0 0 25 8 -7 .05 9 8 | -40 -132 9 106
grg 120| 2 0 4 6 10 0 .03 11 9 | 108 -89 10 123
igr n/a| 0 -1 0 -3 21 8 -.00 4 4 | 4939 90 10 74
jgx n/a| -1 -1 -2 0 -5 74 -.04 14 14 | 116 -103 34 99
jpl n/a| 0 -1 4 24 6 0 .10 26 26 | -510 -494 89 158
mit 373| 0 0 -3 14 -34 16 .01 6 6 | 5017 1043 43 76
ngs 272| 0 0 2 -12 17 8 -.11 11 9 | 14841 322 443 724
sio 346| 0 0 0 -21 -32 -77 -.00 7 7 | --- --- --- ---
Table 2.2328.1 GPS week: 2328 Day: 1 MJD: 60541.000
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 787| 0 0 5 10 5 3 -.05 9 8 | -629 -204 6 77
emr 108| 2 0 -6 22 20 19 .01 10 10 | -1715 -628 33 111
esa 150| 0 0 -2 -1 13 -12 -.00 10 10 | -2102 1482 7 87
gfz 124| -1 -1 -1 49 18 -58 .06 9 9 | -37 -35 11 120
grg 112| 1 0 7 21 8 -5 .07 12 11 | 102 -49 12 130
igr n/a| 0 0 0 21 25 -18 -.01 4 4 | 5090 -263 11 70
jgx n/a| -1 0 0 3 11 43 -.09 15 15 | 143 -149 38 106
jpl n/a| 0 0 4 15 1 -18 .11 26 26 | -865 -456 88 157
mit 373| 0 0 -1 -41 -39 54 .02 5 5 | 5666 758 37 74
ngs 279| 0 0 0 12 -11 -10 -.12 10 10 | 15632 -222 484 677
sio 349| 0 0 0 -5 13 -56 .00 8 8 | --- --- --- ---
Table 2.2328.2 GPS week: 2328 Day: 2 MJD: 60542.000
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 780| -1 0 4 23 -7 0 -.07 9 8 | -793 315 7 92
emr 107| 2 0 -5 0 12 -28 -.01 9 9 | -903 -899 27 98
esa 150| 0 -1 -3 -10 -5 -44 .05 11 10 | -1483 95 8 89
gfz 124| -1 0 1 59 1 -67 .05 9 9 | -116 41 11 116
grg 115| 1 0 3 33 17 -17 .04 10 10 | 92 4 9 121
igr n/a| 0 0 0 28 6 -29 -.00 4 4 | 4847 -725 11 74
jgx n/a| -1 0 -2 4 -4 -3 -.03 13 13 | 102 -8 33 93
jpl n/a| -1 -1 3 9 -26 -1 .14 26 26 | -1305 -538 89 158
mit 373| 0 0 0 -30 -8 55 .01 6 6 | -27 -780 36 61
ngs 284| 0 0 0 -9 -3 -44 -.12 9 8 | -800 315 415 695
sio 345| 0 0 0 -27 0 46 .01 7 7 | --- --- --- ---
Table 2.2328.3 GPS week: 2328 Day: 3 MJD: 60543.000
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 778| -2 0 4 21 3 1 -.05 8 7 | -691 149 6 84
emr 105| 1 0 -3 12 8 12 -.02 9 9 | -1304 39 41 103
esa 150| 0 -1 -1 -30 18 -21 .02 10 10 | -1144 -250 8 92
gfz 123| 0 0 0 46 27 -40 .05 8 8 | -143 81 9 121
grg 114| 1 0 4 2 8 -7 .05 11 10 | 100 -235 10 141
igr n/a| 0 1 0 1 7 -3 .02 4 4 | 3995 -1472 10 63
jgx n/a| -1 0 -2 6 -2 11 -.02 10 10 | 111 -234 28 90
jpl n/a| 0 0 4 4 -12 -9 .12 25 26 | -1842 -1148 86 153
mit 373| 0 0 0 2 -42 62 .01 6 6 | -2841 -1906 38 59
ngs 272| 0 0 -1 -15 5 -46 -.11 9 9 | 14998 330 533 774
sio 327| -1 0 -1 -44 0 -2 .00 8 7 | --- --- --- ---
Table 2.2328.4 GPS week: 2328 Day: 4 MJD: 60544.000
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 770| -1 0 5 10 -22 0 -.02 8 7 | -630 12 6 88
emr 107| 1 0 -5 -6 2 16 .00 10 10 | -1582 -558 28 115
esa 150| 0 -1 -1 -8 -1 -14 .04 10 9 | -1146 227 7 83
gfz 126| -1 0 3 38 20 -44 .01 8 9 | -78 -73 8 111
grg 110| 2 0 1 3 22 -12 .06 27 11 | 28 -206 9 112
igr n/a| 0 0 0 10 1 5 .02 3 3 | 2741 -1057 10 65
jgx n/a| 0 0 -1 16 -10 -27 -.02 10 10 | 15 -187 29 86
jpl n/a| 0 -1 5 8 -55 -3 .17 27 27 | -2986 -510 92 154
mit 373| 0 0 0 -32 -21 54 .04 7 6 | -6696 -1006 38 57
ngs 275| 1 0 0 -16 0 -46 -.13 10 9 | -631 12 486 666
sio 336| 0 0 -2 -19 19 31 -.03 8 6 | --- --- --- ---
Table 2.2328.5 GPS week: 2328 Day: 5 MJD: 60545.000
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 772| 0 0 4 16 -9 -24 -.04 8 7 | -673 35 5 84
emr 107| 1 -1 -6 10 14 24 .00 9 9 | -2548 991 27 104
esa 150| 0 0 -1 -14 8 -22 .02 10 10 | -1339 399 8 80
gfz 125| -1 0 4 20 21 -56 .01 13 13 | -111 29 28 149
grg 121| 2 0 2 -12 11 -25 .10 11 9 | 5 -99 10 133
igr n/a| 0 0 2 3 9 -2 .03 3 3 | 1946 -1082 11 67
jgx n/a| 0 1 -2 8 4 -74 -.04 12 12 | -9 -29 29 91
jpl n/a| -1 -2 3 -3 -11 17 .14 25 25 | -3254 -378 86 148
mit 373| 0 0 0 -6 -35 34 .02 6 6 | -9789 -1373 40 73
ngs 279| -1 0 -2 -3 5 -19 -.10 10 8 | 15116 -69 573 769
sio 333| -1 0 0 -5 9 80 -.01 7 7 | --- --- --- ---
Table 2.2328.6 GPS week: 2328 Day: 6 MJD: 60546.000
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 774| 0 -1 5 17 -5 -31 -.02 8 8 | -688 53 7 97
emr 111| 0 -2 -6 -8 24 8 -.02 9 9 | -3003 1931 27 106
esa 150| 0 -1 -1 -9 -9 -23 -.05 10 9 | -940 -79 8 89
gfz 126| -2 0 2 41 2 -33 .03 8 9 | -79 -23 9 118
grg 120| 2 0 1 2 -3 -9 .03 10 9 | -57 -128 10 128
igr n/a| 0 0 1 -1 5 -16 .02 3 3 | 857 -468 11 67
jgx n/a| 0 1 -2 20 -36 -102 -.06 13 13 | -67 -93 32 94
jpl n/a| -1 -2 1 0 -20 -15 .15 26 26 | -3741 377 88 150
mit 373| 0 0 0 -31 -4 87 .04 6 6 | -13147 -1218 38 68
ngs 279| -1 2 -3 -13 -20 9 -.10 11 9 | -694 59 504 734
sio 333| 0 0 0 2 25 21 -.01 7 6 | --- --- --- ---
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 3.2328.0 GPS week: 2328 Day: 0 MJD: 60540.000
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 16 --- --- 8 12 9 4 | 21 --- --- --- 21 21 --- --- 24 23 23 20
2E | 11 10 8 9 10 3 15 11 8 16 9 3 | 23 22 26 27 23 24 26 24 27 25 32 24
3 | 8 15 12 8 10 3 12 8 5 9 7 3 | 41 40 40 41 39 39 41 43 40 35 41 39
4 | 13 10 23 9 17 4 12 58 6 9 8 4 | 57 59 56 58 57 57 60 59 55 56 57 56
5 | 8 10 6 6 7 3 13 12 4 8 7 2 | 39 36 37 41 36 38 38 39 38 41 40 38
6 | 11 15 9 9 21 3 15 10 6 10 5 4 | 64 69 68 64 68 66 70 63 64 68 68 66
7 | 8 8 8 8 14 5 13 9 7 8 5 3 | 44 39 37 40 41 40 43 39 41 44 40 40
8 | 5 10 9 9 9 3 12 9 7 7 7 2 | 42 46 44 43 42 44 44 46 43 44 46 43
9 | 10 13 8 9 22 3 11 11 4 8 6 3 | 58 49 53 52 55 53 54 52 51 48 51 51
10 | 6 9 11 11 5 4 13 13 4 10 11 3 | 42 39 41 41 38 40 41 43 40 40 43 40
11 | 7 7 19 7 11 5 12 62 8 12 5 3 | 52 55 65 58 58 57 55 70 52 58 57 56
12 | 4 9 7 5 7 4 21 10 3 10 6 2 | 23 20 21 22 24 22 23 21 21 25 22 21
13E | 9 9 9 7 6 4 15 12 8 10 8 3 | 54 50 50 51 53 51 50 52 48 50 51 50
14 | 6 18 7 10 6 3 10 52 6 9 5 3 | 53 52 50 54 53 52 52 69 51 53 54 51
15 | 7 11 12 7 6 7 16 10 8 12 9 3 | 45 35 33 40 40 37 34 41 43 45 44 40
16 | 6 9 7 9 8 4 21 8 5 10 11 3 | 31 30 30 30 30 29 30 30 31 33 35 30
17 | 8 7 7 10 14 2 13 8 6 8 7 3 | 33 31 30 27 30 28 31 29 29 33 31 29
18 | 6 11 19 9 10 5 12 55 8 13 8 3 | 110 112 115 109 109 111 109 119 108 108 111 109
19 | 9 6 7 11 12 3 15 9 6 9 5 3 | 41 38 39 36 36 37 43 36 37 40 42 38
20 | 9 10 5 6 6 4 13 13 4 10 8 2 | 29 28 30 31 27 30 30 29 28 31 32 29
21E | 12 11 11 7 24 4 20 9 7 20 10 4 | 24 31 33 28 31 29 34 31 30 32 37 29
22 | 4 8 8 8 7 2 12 6 3 10 7 2 | 35 36 36 38 35 36 35 37 36 42 40 36
23 | 6 9 11 5 6 2 16 49 6 14 7 3 | 19 21 20 23 23 21 26 20 21 21 26 20
24 | 7 9 8 10 9 4 12 12 7 14 6 3 | 310 308 309 310 317 309 310 307 309 309 311 309
25 | 5 13 10 7 4 5 12 16 4 9 5 2 | 34 41 37 35 35 35 30 40 34 36 36 35
26 | 8 11 7 7 5 3 12 11 6 9 8 3 | 23 31 28 25 25 25 26 32 25 29 30 25
27 | 5 11 8 9 10 2 14 14 7 9 7 3 | 43 44 44 45 40 43 43 47 43 43 45 43
28 | 8 9 11 11 11 3 16 55 7 12 10 3 | 83 79 86 79 86 83 83 100 78 83 81 81
29 | 7 8 6 15 10 5 17 10 4 12 5 3 | 50 51 50 49 49 50 55 49 50 50 51 50
30 | 6 9 9 6 14 2 11 9 6 5 7 2 | 48 44 44 44 49 45 46 45 43 48 44 44
31 | 7 10 7 8 10 2 15 10 5 7 8 3 | 33 32 27 33 35 32 34 32 30 33 34 31
32 | 9 11 8 10 8 3 16 12 6 11 8 3 | 48 45 47 45 47 46 46 50 44 47 47 45
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 10 10 9 11 4 14 26 6 11 7 |T 51 52 52 52 51 50 52 54 50 52 53 50
WRMS | 8 10 11 8 9 4 14 26 6 9 7 |NE 50 50 50 51 50 49 51 53 49 51 51 49
MEDI | 7 10 8 9 9 3 13 11 6 10 7 |MD 42 40 40 41 39 39 43 43 40 42 42 40
Table 3.2328.1 GPS week: 2328 Day: 1 MJD: 60541.000
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 | 16 --- --- --- 8 19 --- --- 6 10 8 5 | 18 --- --- --- 18 23 --- --- 20 21 18 17
2E | 12 9 7 8 12 4 16 10 6 16 11 3 | 23 21 24 25 26 23 31 23 26 27 28 23
3 | 9 9 12 6 10 3 13 9 6 7 6 3 | 21 23 23 19 20 20 24 24 18 18 20 19
4 | 13 9 23 8 18 5 13 55 4 10 7 4 | 39 39 38 40 42 39 42 41 38 35 38 37
5 | 7 10 5 6 7 2 14 9 5 5 8 2 | 20 21 19 23 21 21 20 24 21 20 23 20
6 | 9 14 9 7 20 4 17 11 6 11 6 3 | 37 39 38 39 38 36 41 37 35 36 34 36
7 | 8 9 7 9 15 3 14 10 7 9 7 3 | 32 27 26 29 35 27 32 28 29 30 30 28
8 | 6 8 7 9 10 3 11 10 5 9 9 2 | 23 26 26 27 24 24 27 27 24 25 27 24
9 | 11 12 9 8 22 5 13 12 3 10 8 3 | 42 34 39 37 45 38 39 41 36 32 36 36
10 | 7 9 12 10 5 4 14 14 4 9 8 3 | 21 21 24 19 23 21 23 24 22 20 24 21
11 | 9 8 18 8 14 4 13 61 9 14 7 4 | 27 31 35 35 36 32 32 39 30 34 31 31
12 | 4 8 6 5 7 4 20 12 4 10 6 2 | 21 18 20 20 21 20 21 20 21 23 22 20
13E | 10 9 10 10 10 4 18 11 6 7 10 3 | 48 44 43 45 48 44 47 47 44 43 43 44
14 | 5 18 5 9 6 3 12 51 5 10 8 3 | 29 31 31 32 33 31 33 34 31 31 35 30
15 | 10 8 10 14 9 5 14 12 8 10 12 3 | 40 30 29 29 36 32 30 35 36 36 37 33
16 | 5 7 6 6 7 3 21 11 4 9 9 3 | 14 13 17 17 16 14 20 15 15 15 19 14
17 | 17 8 7 9 15 3 15 8 5 9 8 3 | 27 20 19 21 23 19 23 22 21 22 23 20
18 | 7 10 19 9 10 4 12 52 7 13 5 3 | 67 69 73 70 68 69 69 73 69 69 71 69
19 | 7 8 6 9 13 3 15 9 5 9 7 3 | 21 20 19 19 21 20 23 18 21 22 24 20
20 | 8 10 5 6 10 3 13 11 5 10 10 3 | 15 18 16 19 16 16 18 19 16 15 20 15
21E | 12 8 9 10 10 4 20 10 5 11 8 3 | 20 22 24 22 22 21 29 23 24 25 26 22
22 | 6 8 7 7 8 2 12 6 4 9 7 2 | 16 18 20 19 19 17 18 19 17 18 21 17
23 | 8 7 13 10 6 4 18 48 4 12 10 3 | 12 16 16 20 19 15 23 18 17 11 18 15
24 | 6 9 9 10 12 4 11 17 5 12 7 3 | 228 226 224 226 233 225 227 225 228 227 228 227
25 | 6 13 9 6 6 5 12 15 4 12 7 2 | 21 30 26 27 24 25 21 32 22 26 21 23
26 | 6 11 8 8 5 3 13 13 6 11 9 3 | 17 24 22 18 19 18 21 27 17 19 21 18
27 | 7 10 8 11 9 3 13 11 4 10 7 3 | 23 27 27 31 23 26 26 27 25 28 24 25
28 | 8 11 11 10 10 3 15 55 5 12 11 3 | 55 56 60 56 62 58 62 66 57 59 60 57
29 | 6 10 7 11 11 4 16 11 4 13 7 3 | 29 29 29 29 30 29 32 27 28 33 28 28
30 | 6 8 9 7 16 3 13 11 5 9 8 3 | 32 28 30 25 38 28 30 30 28 27 28 28
31 | 9 8 8 9 11 3 17 14 5 12 9 3 | 24 23 18 25 27 22 28 23 22 22 26 22
32 | 8 14 9 8 9 4 17 14 6 11 8 3 | 34 34 36 33 36 35 36 37 34 37 35 34
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 9 10 10 9 12 4 15 26 5 10 8 |T 34 34 35 35 36 34 37 36 34 34 35 33
WRMS | 8 10 10 9 11 4 15 26 5 10 8 |NE 33 34 34 34 35 33 35 36 33 33 34 32
MEDI | 8 9 9 9 10 4 14 11 5 10 8 |MD 23 27 26 27 24 24 29 27 24 26 26 23
Table 3.2328.2 GPS week: 2328 Day: 2 MJD: 60542.000
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 | 18 --- --- --- 8 9 --- --- 8 --- --- 8 | 28 --- --- --- 20 20 --- --- 21 --- --- 22
2E | 10 10 8 9 8 4 11 12 7 9 10 3 | 19 21 25 27 25 22 24 24 26 23 28 23
3 | 6 8 12 8 8 3 11 10 5 7 6 2 | 32 32 33 32 32 30 34 33 30 29 29 30
4 | 12 8 25 8 14 2 10 59 5 10 5 4 | 27 32 33 32 35 30 33 35 31 31 30 30
5 | 6 9 6 7 8 3 12 10 3 9 6 2 | 30 29 29 33 28 30 32 33 30 30 31 30
6 | 12 12 9 7 19 3 14 12 5 11 5 3 | 53 55 55 51 53 53 58 54 53 53 52 52
7 | 8 8 8 9 15 4 13 10 7 7 8 3 | 35 32 30 32 36 33 34 34 35 37 35 33
8 | 6 8 8 8 8 3 8 9 5 7 7 2 | 33 36 34 34 34 34 33 37 32 31 32 32
9 | 8 11 10 7 19 4 10 13 4 11 5 3 | 39 34 36 37 43 36 35 38 35 36 35 35
10 | 5 9 10 10 5 3 14 14 5 6 7 2 | 32 30 33 32 30 31 32 36 32 33 33 31
11 | 8 9 19 9 13 4 13 62 7 12 6 3 | 38 38 45 38 42 39 40 48 37 40 39 38
12 | 6 9 7 8 7 4 21 13 5 9 10 3 | 22 19 21 21 22 21 26 22 19 24 20 19
13E | 10 10 11 9 8 4 15 12 6 9 7 3 | 59 62 59 58 59 58 61 59 60 59 60 59
14 | 5 17 6 6 7 3 10 49 7 6 6 3 | 35 36 36 36 39 35 38 48 39 39 40 37
15 | 7 11 12 7 9 6 15 13 6 9 9 3 | 43 32 31 41 38 35 34 37 40 38 42 38
16 | 6 8 6 7 7 3 22 9 4 8 8 3 | 22 23 24 26 23 22 23 23 23 21 25 22
17 | 12 6 8 10 13 3 12 9 4 8 5 3 | 27 27 26 24 30 25 27 27 26 28 29 26
18 | 8 9 21 14 11 5 12 51 8 12 6 4 | 96 100 104 97 100 99 101 104 96 98 98 98
19 | 8 5 7 12 12 3 16 9 5 8 6 3 | 30 29 31 26 30 28 34 28 29 31 32 29
20 | 8 9 6 6 8 3 13 11 3 13 7 2 | 22 22 24 25 22 23 26 23 22 27 26 22
21E | 8 8 10 11 8 5 16 12 6 8 8 3 | 22 28 31 27 29 26 29 32 28 29 28 27
22 | 6 6 7 7 8 2 11 6 4 6 6 2 | 24 26 26 24 26 24 26 28 25 29 28 25
23 | 6 8 12 9 8 3 12 49 4 10 6 2 | 17 19 19 23 21 18 23 16 20 21 22 19
24 | 6 9 8 9 9 3 9 18 6 7 6 2 | 326 325 326 328 336 328 327 328 327 326 327 327
25 | 6 11 8 14 5 5 12 15 6 11 9 3 | 27 34 33 37 28 30 26 34 26 29 28 28
26 | 31 11 11 10 5 5 12 13 8 9 8 5 | 30 28 26 23 21 22 23 31 23 23 25 21
27 | 7 8 7 9 8 2 12 9 5 10 7 2 | 32 34 34 35 32 32 33 35 32 30 30 31
28 | 6 11 12 9 10 2 14 56 5 10 6 3 | 52 46 52 47 55 49 48 65 50 48 52 50
29 | 6 8 8 11 11 4 14 9 4 8 4 2 | 37 37 39 39 37 37 39 36 38 39 40 38
30 | 7 8 10 8 15 3 10 10 6 9 5 3 | 34 32 31 31 37 32 33 32 32 34 32 32
31 | 8 8 8 8 8 3 14 11 5 9 7 3 | 27 27 23 30 27 27 27 30 26 25 30 26
32 | 8 12 9 7 7 4 16 13 7 10 6 3 | 39 37 38 39 37 38 35 39 38 37 39 37
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 9 9 11 9 10 4 13 26 6 9 7 |T 43 43 44 44 44 42 44 46 43 44 45 42
WRMS | 8 9 10 9 10 4 13 26 6 8 7 |NE 42 42 42 43 43 41 43 45 41 43 43 41
MEDI | 7 9 8 9 8 3 12 12 5 9 6 |MD 32 32 33 32 32 30 33 34 31 31 32 30
Table 3.2328.3 GPS week: 2328 Day: 3 MJD: 60543.000
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 | 16 --- --- --- 7 29 --- --- 4 19 6 5 | 22 --- --- --- 18 29 --- --- 19 30 20 21
2E | 11 8 9 11 11 4 8 10 11 7 11 3 | 26 24 27 30 25 27 27 27 30 28 32 27
3 | 7 7 12 7 9 2 7 9 7 7 7 2 | 34 32 34 31 32 32 33 34 33 31 32 32
4 | 11 8 24 7 17 4 7 58 5 11 5 4 | 16 22 28 21 26 20 21 31 20 16 21 19
5 | 6 8 8 6 9 4 7 11 6 9 10 2 | 31 28 32 32 31 31 32 33 30 34 31 31
6 | 13 11 8 8 10 3 9 12 6 10 6 3 | 82 86 84 84 82 83 85 84 79 88 85 83
7 | 8 6 8 10 16 3 10 9 9 11 6 3 | 31 31 29 33 35 31 32 32 32 33 31 31
8 | 6 8 9 6 11 4 6 11 7 6 7 2 | 36 38 38 38 35 37 38 39 35 38 40 37
9 | 8 11 9 7 22 3 6 12 3 10 6 3 | 31 26 29 25 35 28 27 30 27 28 28 27
10 | 6 8 10 7 6 3 9 12 6 10 8 2 | 34 32 35 36 33 34 32 36 33 37 33 33
11 | 8 9 18 4 13 4 12 58 6 9 6 3 | 42 45 51 46 47 45 42 57 41 46 46 44
12 | 6 8 7 4 9 4 18 13 5 6 7 2 | 19 16 18 18 19 18 20 20 19 19 17 18
13 | 10 9 9 9 10 4 12 11 6 7 8 3 | 49 48 47 46 46 46 46 51 47 46 46 46
14 | 6 17 7 7 6 2 8 50 8 8 8 3 | 34 32 34 38 36 35 36 50 36 39 36 35
15 | 10 8 8 12 9 6 11 12 8 14 12 3 | 39 30 30 29 34 31 30 33 37 35 36 33
16 | 6 6 7 8 9 3 19 9 6 7 8 3 | 26 28 29 32 27 28 23 27 28 28 27 27
17 | 5 5 7 8 13 3 8 9 5 8 8 2 | 30 28 28 29 29 29 29 30 29 34 29 29
18 | 7 9 19 9 10 4 9 49 9 10 6 3 | 117 116 119 117 115 116 113 118 114 118 116 116
19 | 6 7 6 11 14 3 15 9 6 8 7 3 | 31 32 33 30 29 31 35 29 31 36 32 31
20 | 6 9 6 7 10 3 10 11 4 13 8 3 | 23 22 24 26 23 24 25 26 22 25 23 23
21E | 12 7 9 9 10 5 13 9 8 7 6 3 | 28 29 32 28 27 29 29 31 32 32 34 29
22 | 6 7 7 8 8 3 6 5 5 9 7 2 | 28 29 30 34 28 30 29 30 31 38 31 31
23 | 7 8 12 7 8 3 10 49 4 14 7 3 | 16 20 19 24 22 19 21 19 20 22 22 20
24 | 11 11 8 7 10 4 8 14 5 10 8 3 | 188 188 188 188 195 188 188 184 187 185 186 187
25 | 5 11 9 8 6 5 9 15 5 11 7 2 | 31 38 33 36 32 33 29 36 33 33 32 32
26 | 9 9 6 8 6 3 6 12 4 7 7 2 | 25 28 25 23 23 24 22 28 24 24 24 23
27 | 6 8 7 8 9 3 7 10 5 8 6 2 | 38 38 39 41 36 38 38 40 37 37 38 38
28 | 7 10 11 6 10 4 9 57 6 9 9 3 | 38 33 41 37 44 37 34 58 39 33 43 38
29 | 6 7 6 8 11 4 14 13 5 9 7 3 | 38 40 39 38 39 37 42 40 39 41 39 39
30 | 6 7 10 7 16 3 7 8 7 10 6 3 | 35 33 32 31 38 33 33 34 32 35 32 32
31 | 6 8 7 5 10 3 12 11 5 11 9 3 | 29 26 24 28 27 26 25 27 28 26 30 27
32 | 9 10 9 7 7 3 9 14 7 9 7 3 | 33 31 34 32 33 32 29 33 34 31 35 32
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 9 10 8 11 4 10 25 6 9 8 |T 40 40 41 41 40 40 40 43 39 41 40 39
WRMS | 7 9 10 8 10 4 10 26 6 9 7 |NE 36 36 37 37 36 35 36 39 35 37 36 35
MEDI | 7 8 8 7 10 3 9 12 6 9 7 |MD 31 31 32 32 32 31 32 33 32 33 32 31
Table 3.2328.4 GPS week: 2328 Day: 4 MJD: 60544.000
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 | 10 --- --- --- 11 12 --- --- 5 --- --- 6 | 24 --- --- --- 18 21 --- --- 19 --- --- 20
2E | 8 6 9 8 11 3 7 9 7 10 9 3 | 23 22 25 23 21 23 23 25 26 25 28 23
3 | 7 9 12 8 8 3 4 9 6 9 12 3 | 24 24 25 22 22 22 21 29 23 22 27 22
4 | 10 10 22 6 16 3 5 60 5 12 5 3 | 29 33 35 30 35 31 31 40 32 30 32 30
5 | 6 7 5 8 10 2 8 11 5 11 6 2 | 20 18 18 21 18 18 17 20 19 20 21 18
6E | 10 12 9 11 15 3 8 12 8 13 6 3 | 82 84 87 81 81 82 84 79 86 82 83 83
7 | 7 6 10 9 14 4 10 8 10 8 6 3 | 29 28 25 28 28 26 29 29 30 26 27 27
8 | 6 7 9 9 8 4 4 9 6 8 8 2 | 28 29 28 28 29 28 30 31 28 28 30 28
9 | 8 12 8 6 20 2 5 11 5 12 5 3 | 34 29 33 30 35 31 30 33 31 32 29 30
10 | 5 8 10 5 8 3 6 11 5 9 6 2 | 20 21 23 22 20 21 21 25 21 19 22 20
11 | 6 8 17 6 13 3 10 63 8 9 9 3 | 33 35 42 37 41 37 35 44 34 35 41 36
12 | 5 8 8 5 10 2 11 12 4 8 8 2 | 22 20 21 20 20 21 21 24 20 22 19 19
13 | 10 8 10 10 16 4 12 13 6 7 9 3 | 47 47 44 44 47 44 43 47 46 45 47 45
14 | 6 16 8 9 6 3 6 51 7 7 8 3 | 32 32 33 37 32 31 31 43 35 29 32 31
15 | 9 9 8 7 12 3 9 11 6 10 8 3 | 36 28 27 30 28 30 28 32 33 32 31 30
16 | 5 7 7 9 8 2 18 8 5 8 8 3 | 18 17 20 23 20 19 16 17 19 20 20 18
17 | 5 7 6 8 12 2 6 7 7 8 5 2 | 22 25 21 28 26 24 23 26 25 26 25 24
18E | 8 7 20 11 9 2 6 52 11 14 7 3 | 102 99 102 96 98 99 99 104 99 99 100 99
19 | 6 7 6 7 13 3 10 9 10 9 6 3 | 22 23 22 26 23 23 22 20 26 22 27 23
20 | 5 7 5 6 10 3 6 11 4 8 6 2 | 15 15 16 17 15 15 15 17 15 15 18 15
21E | 7 8 11 13 12 7 12 12 8 12 13 3 | 37 40 40 38 44 39 40 41 38 40 40 38
22 | 4 6 7 7 7 2 7 6 5 6 6 2 | 21 23 23 26 19 20 20 24 22 20 20 21
23 | 6 7 10 4 11 2 6 50 4 10 6 2 | 11 15 15 15 17 13 14 18 15 11 17 13
24 | 22 25 12 11 139 7 30 31 10 13 18 7 | 526 526 525 523 551 527 527 526 526 522 527 526
25 | 6 12 10 8 8 3 8 14 5 10 8 3 | 24 32 27 22 26 23 23 33 24 21 24 24
26 | 6 11 6 7 6 2 7 14 5 9 6 2 | 17 24 22 19 20 19 18 26 19 19 18 18
27 | 6 9 8 6 8 3 6 9 5 9 8 2 | 28 29 29 26 28 28 30 30 28 30 32 28
28 | 7 8 13 11 9 3 8 55 6 13 5 3 | 49 47 53 48 53 50 49 61 48 53 50 49
29 | 6 8 7 8 10 3 10 12 7 14 5 3 | 29 30 29 32 30 29 30 30 29 32 32 30
30 | 6 8 12 9 16 3 6 10 7 6 6 3 | 26 25 26 24 29 24 26 26 25 22 24 24
31 | 7 7 8 7 10 2 9 15 6 12 7 2 | 24 24 21 27 24 24 25 26 25 24 26 24
32 | 6 13 9 7 11 3 7 14 6 12 8 3 | 30 30 33 33 29 30 28 32 31 32 33 30
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 10 10 8 27 3 10 27 7 10 8 |T 46 47 48 47 47 46 46 50 46 46 48 45
WRMS | 7 10 9 9 11 3 10 27 6 9 6 |NE 44 45 46 46 45 44 45 48 44 45 46 43
MEDI | 6 8 9 8 10 3 7 12 6 9 7 |MD 26 28 27 28 28 24 28 30 26 26 28 24
Table 3.2328.5 GPS week: 2328 Day: 5 MJD: 60545.000
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 --- --- --- 8 16 --- --- 5 13 6 4 | 22 --- --- --- 19 19 --- --- 19 20 15 19
2E | 12 9 8 12 12 4 11 10 10 18 16 4 | 25 25 28 27 24 26 25 27 28 35 33 26
3 | 9 8 11 10 9 4 8 9 6 9 7 3 | 22 25 28 25 23 23 22 30 23 24 24 23
4 | 12 9 20 12 15 5 9 57 5 12 7 4 | 37 39 37 37 42 37 40 44 37 36 36 37
5 | 8 8 5 15 8 3 10 11 5 6 7 2 | 22 21 21 27 21 22 22 24 20 22 24 21
6E | 9 13 8 13 12 4 10 11 5 10 5 3 | 82 86 86 89 85 86 87 86 84 87 88 85
7 | 7 6 8 13 12 3 11 7 6 8 5 3 | 32 30 27 30 29 30 31 32 27 32 29 29
8 | 6 8 9 11 8 4 11 11 6 10 9 3 | 25 29 28 27 28 26 32 30 25 26 29 26
9 | 8 12 8 15 17 4 9 11 5 10 6 3 | 38 34 36 34 39 35 37 38 35 36 35 35
10 | 4 8 10 14 6 3 8 13 6 5 6 2 | 23 27 26 27 23 24 25 28 22 24 26 24
11 | 8 8 18 11 10 4 12 61 7 11 6 3 | 31 33 36 34 35 32 31 40 34 30 34 32
12 | 6 7 6 15 7 3 14 13 5 9 6 2 | 24 25 25 22 25 26 26 26 23 28 27 25
13 | 8 9 10 11 15 4 15 13 7 9 7 3 | 49 50 48 51 57 48 49 53 49 47 48 49
14 | 6 16 8 15 5 3 8 49 6 8 6 3 | 33 36 33 30 35 34 36 39 32 35 37 33
15 | 8 10 10 15 10 4 13 12 7 8 9 3 | 39 35 33 36 34 35 33 37 36 37 39 35
16 | 5 6 7 13 7 3 22 12 6 10 7 3 | 21 21 23 23 21 22 20 19 21 22 23 21
17 | 5 7 8 16 11 3 9 7 6 7 6 2 | 26 29 26 25 28 26 28 29 26 30 27 26
18E | 8 9 19 17 11 3 14 47 8 12 8 4 | 133 137 138 139 136 135 133 137 131 136 135 135
19 | 6 7 6 13 12 4 13 8 7 6 4 2 | 22 24 24 22 22 22 25 22 22 24 23 22
20 | 7 9 5 12 9 3 11 11 4 10 7 2 | 18 19 21 26 20 20 21 22 19 22 24 19
21E | 17 8 10 11 23 4 13 12 10 18 9 4 | 32 36 38 34 31 34 35 37 37 45 37 34
22 | 5 6 8 14 7 2 10 7 5 6 6 2 | 20 24 22 20 19 21 21 23 20 22 23 20
23 | 6 7 9 14 6 2 11 48 6 8 7 2 | 20 24 21 28 24 22 23 21 21 21 24 21
24 | 8 9 9 15 10 3 11 15 5 7 9 3 | 290 289 290 295 290 289 284 292 292 289 293 290
25 | 5 12 10 13 4 3 13 16 7 9 7 3 | 26 32 29 26 24 26 25 31 24 24 25 25
26 | 7 9 7 13 5 2 11 14 6 7 7 2 | 23 28 27 23 23 25 25 30 22 24 26 24
27 | 6 8 9 13 7 4 10 11 6 11 8 3 | 24 27 28 28 27 26 31 29 25 26 28 26
28 | 8 10 12 13 8 3 11 53 7 11 8 3 | 56 51 57 49 56 54 57 63 54 55 54 54
29 | 7 8 7 11 8 3 15 12 7 10 7 3 | 25 25 24 26 26 24 27 28 25 26 26 24
30 | 5 7 11 16 13 3 8 9 5 6 5 3 | 28 28 27 24 30 26 28 29 24 25 26 26
31 | 7 7 8 14 9 3 14 14 7 9 9 3 | 26 25 21 30 26 25 25 26 26 25 27 25
32 | 7 12 9 11 8 4 9 13 6 10 6 3 | 34 34 35 37 34 34 35 34 32 32 34 33
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 9 10 13 11 3 12 25 6 10 7 |T 41 43 43 43 42 41 43 45 41 42 43 41
WRMS | 7 9 10 13 9 3 12 25 6 8 7 |NE 37 39 38 39 38 37 39 41 36 37 38 37
MEDI | 7 8 9 13 9 3 11 12 6 9 7 |MD 26 29 28 28 27 26 28 30 25 26 27 26
Table 3.2328.6 GPS week: 2328 Day: 6 MJD: 60546.000
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 | 10 --- --- --- 7 10 --- --- 6 --- --- 5 | 21 --- --- --- 20 23 --- --- 21 --- --- 19
2E | 9 9 11 13 9 4 13 12 7 14 12 3 | 21 21 24 32 23 22 26 20 25 25 33 24
3 | 7 8 11 7 9 2 10 10 6 11 8 3 | 30 31 29 28 30 28 28 31 26 28 31 28
4 | 12 9 21 7 14 3 10 60 4 11 7 4 | 60 65 64 61 65 62 64 72 59 62 64 61
5 | 9 9 6 9 7 4 12 11 4 10 8 3 | 31 26 26 30 26 27 28 29 28 28 30 27
6E | 9 12 8 9 12 4 15 11 6 8 6 3 | 79 82 80 81 79 79 84 80 77 81 78 79
7 | 8 8 7 8 15 4 14 7 7 7 6 3 | 38 34 31 36 36 34 36 35 35 34 34 34
8 | 6 8 10 8 6 3 13 8 7 8 7 2 | 35 39 38 37 37 38 45 40 34 35 37 36
9 | 8 11 7 9 17 3 10 12 4 11 4 3 | 52 48 51 52 53 50 52 53 47 47 49 49
10 | 5 9 10 9 6 3 10 14 5 6 7 2 | 28 28 29 32 27 29 29 32 29 28 30 28
11E | 10 8 16 8 9 3 14 62 8 12 7 3 | 58 59 66 60 60 59 55 70 56 61 59 58
12 | 6 7 6 7 5 3 15 13 5 9 6 2 | 24 25 23 22 23 24 27 25 24 25 25 23
13 | 11 8 9 7 11 3 16 12 6 8 9 3 | 58 57 56 57 58 56 56 60 55 53 54 55
14 | 5 15 7 6 6 3 9 53 7 7 7 2 | 48 49 46 47 48 48 50 64 49 49 48 47
15 | 9 9 9 7 9 4 13 12 9 10 11 3 | 41 33 33 38 34 35 34 38 38 34 37 35
16 | 6 6 6 8 6 3 24 10 5 12 7 3 | 29 26 27 29 29 28 26 27 27 31 29 27
17 | 9 8 7 10 12 2 12 10 5 8 9 3 | 30 29 27 31 29 27 32 28 26 31 27 27
18E | 8 10 20 11 11 4 13 52 6 18 6 4 | 144 145 148 144 144 145 143 147 143 144 143 143
19 | 10 8 6 8 11 3 15 11 7 10 4 3 | 33 31 32 34 32 32 37 32 33 34 34 32
20 | 10 9 6 7 9 5 13 11 5 10 11 3 | 22 21 20 22 19 20 23 23 19 18 25 20
21E | 11 8 12 12 18 4 15 8 6 16 7 4 | 42 39 39 49 42 40 45 41 41 41 41 41
22 | 7 6 6 9 8 3 12 7 5 6 10 2 | 30 30 29 33 30 30 32 34 31 32 33 30
23 | 7 7 10 5 9 2 10 47 5 11 3 2 | 19 22 20 23 23 20 22 20 23 22 22 21
24 | 7 10 9 12 15 4 11 16 7 14 7 3 | 306 303 304 307 309 304 303 303 306 303 306 305
25 | 6 12 9 8 5 3 15 15 6 14 6 3 | 32 39 34 33 33 32 32 36 32 29 33 32
26 | 6 12 6 6 5 3 13 12 5 11 6 2 | 22 27 27 23 25 24 24 28 24 26 26 24
27 | 6 7 9 9 7 3 12 12 5 12 7 2 | 37 40 39 38 37 38 43 41 34 36 37 37
28 | 9 12 14 9 9 4 12 58 5 12 8 3 | 82 77 82 79 82 80 85 93 79 78 80 80
29 | 9 6 7 8 7 4 17 14 8 11 8 3 | 44 44 43 44 44 43 49 47 43 44 45 44
30 | 6 9 10 7 16 3 10 9 7 7 6 3 | 42 40 40 41 44 40 42 41 39 35 39 39
31 | 6 8 6 8 8 2 14 12 5 15 6 3 | 32 30 27 33 34 30 36 32 30 31 34 31
32 | 8 14 9 6 8 3 12 15 9 15 7 3 | 43 43 44 43 42 43 46 46 43 44 42 42
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 9 10 8 10 3 13 26 6 11 7 |T 50 51 50 52 50 49 52 53 49 50 51 49
WRMS | 8 9 9 9 9 3 13 26 6 9 6 |NE 46 47 46 47 46 45 49 50 45 46 47 45
MEDI | 8 9 9 8 9 3 13 12 6 11 7 |MD 35 39 34 37 34 34 37 38 34 34 37 34
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 4.2328 GPS week: 2328 MJD: 60540.0-60546.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 |U 12 13 30 |U 8 11 26 |U 11 12 33 |
emr | emr 2975 |U 15 20 37 |U 8 12 35 | 13 13 36 |
esa | esa 2976 | 13 19 38 |U 8 14 39 |U 14 12 32 |
gfz | gfz 2975 |U 10 14 29 |U 8 13 25 | 10 9 29 |
grg | grg 3070 |U 11 15 32 |U 7 14 33 | 12 12 30 |
igr | igr 2976 | 10 14 31 | 7 12 27 | 11 10 29 |
igs | igs 2948 | 11 14 30 | 7 12 26 | 10 10 30 |
jgx | jgx 2976 |U 12 13 32 |U 8 12 27 | 10 10 30 |
jpl | jpl 2976 | 17 23 44 | 10 16 41 | 15 14 42 |
mit | mit 3072 |U 12 12 35 |U 8 12 27 |U 278 107 306 |
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 5.2328.0 GPS week: 2328 Day: 0 MJD: 60540.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 13 33 | 7 9 24 | 13 12 29 |
emr | emr 2976 | 14 17 43 | 11 11 40 | 13 13 33 |
esa | esa 2976 | 13 20 46 | 7 13 42 | 13 12 28 |
gfz | gfz 2976 | 11 18 38 | 7 12 21 | 10 6 25 |
grg | grg 3072 | 10 17 35 | 6 12 31 | 11 8 29 |
igr | igr 2976 | 10 17 40 | 7 11 25 | 12 10 26 |
igs | igs 2976 | 10 15 38 | 7 10 24 | 11 9 26 |
jgx | jgx 2976 | 10 14 39 | 7 7 23 | 12 8 32 |
jpl | jpl 2976 | 16 24 56 | 9 16 46 | 16 11 35 |
mit | mit 3072 | 11 12 40 | 7 9 25 | 1466 193 1593 |
Table 5.2328.1 GPS week: 2328 Day: 1 MJD: 60541.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 9 12 22 | 9 8 24 | 13 13 29 |
emr | emr 2976 | 9 12 21 | 7 10 32 | 14 16 39 |
esa | esa 2976 | 11 15 29 | 10 11 35 | 15 13 37 |
gfz | gfz 2976 | 7 8 20 | 9 11 24 | 11 11 28 |
grg | grg 3068 | 7 10 22 | 9 11 29 | 13 15 30 |
igr | igr 2976 | 7 9 20 | 9 9 26 | 12 13 29 |
igs | igs 2880 | 6 8 18 | 10 10 24 | 12 16 32 |
jgx | jgx 2976 | 6 11 20 | 9 7 30 | 13 12 32 |
jpl | jpl 2976 | 13 20 29 | 12 12 38 | 16 13 44 |
mit | mit 3072 | 9 6 22 | 11 9 33 | 152 182 148 |
Table 5.2328.2 GPS week: 2328 Day: 2 MJD: 60542.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 16 18 39 | 8 11 26 | 13 13 36 |
emr | emr 2976 | 17 25 40 | 8 12 38 | 14 13 36 |
esa | esa 2976 | 17 25 39 | 9 15 43 | 15 13 35 |
gfz | gfz 2976 | 17 18 36 | 8 15 32 | 11 8 28 |
grg | grg 3072 | 17 19 42 | 7 16 37 | 13 11 36 |
igr | igr 2976 | 16 19 37 | 8 13 31 | 11 11 31 |
igs | igs 2880 | 17 20 40 | 7 13 29 | 11 11 33 |
jgx | jgx 2976 | 17 16 36 | 9 9 31 | 11 10 35 |
jpl | jpl 2976 | 18 28 40 | 10 18 46 | 15 14 43 |
mit | mit 3072 | 17 17 42 | 10 13 28 | 12 10 30 |
Table 5.2328.3 GPS week: 2328 Day: 3 MJD: 60543.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 12 15 21 | 8 11 22 | 12 11 32 |
emr | emr 2972 | 11 20 33 | 7 13 27 | 13 8 35 |
esa | esa 2976 | 11 24 32 | 7 15 35 | 15 9 31 |
gfz | gfz 2973 | 7 15 19 | 7 15 22 | 8 8 25 |
grg | grg 3065 | 9 14 24 | 7 14 28 | 10 9 29 |
igr | igr 2976 | 8 16 21 | 7 14 21 | 11 9 29 |
igs | igs 2976 | 8 15 20 | 7 12 22 | 10 8 28 |
jgx | jgx 2976 | 9 14 21 | 7 11 23 | 10 8 31 |
jpl | jpl 2976 | 11 22 32 | 9 17 34 | 17 12 40 |
mit | mit 3072 | 10 15 28 | 8 14 24 | 14 8 34 |
Table 5.2328.4 GPS week: 2328 Day: 4 MJD: 60544.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 8 20 | 9 13 18 | 10 13 30 |
emr | emr 2976 | 26 24 41 | 7 12 30 | 11 15 35 |
esa | esa 2976 | 13 13 31 | 10 15 34 | 13 13 29 |
gfz | gfz 2976 | 8 9 23 | 10 14 26 | 9 9 26 |
grg | grg 3072 | 8 10 24 | 10 16 33 | 9 10 29 |
igr | igr 2976 | 9 9 23 | 9 14 25 | 9 10 28 |
igs | igs 2976 | 10 9 23 | 9 14 23 | 8 10 27 |
jgx | jgx 2976 | 16 10 31 | 9 15 27 | 9 10 26 |
jpl | jpl 2976 | 23 20 51 | 11 15 39 | 13 18 41 |
mit | mit 3072 | 9 9 27 | 10 13 21 | 285 338 278 |
Table 5.2328.5 GPS week: 2328 Day: 5 MJD: 60545.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 13 12 42 | 8 11 30 | 11 10 39 |
emr | emr 2976 | 16 19 50 | 7 10 43 | 13 12 34 |
esa | esa 2976 | 17 16 47 | 8 13 43 | 15 11 33 |
gfz | gfz 2976 | 13 13 39 | 8 12 23 | 9 10 33 |
grg | grg 3071 | 14 15 42 | 6 14 32 | 15 20 32 |
igr | igr 2976 | 14 13 42 | 7 12 29 | 11 9 33 |
igs | igs 2976 | 14 13 41 | 6 12 27 | 10 9 33 |
jgx | jgx 2976 | 15 13 42 | 6 14 28 | 9 9 30 |
jpl | jpl 2976 | 19 21 56 | 10 15 45 | 14 13 46 |
mit | mit 3072 | 14 12 44 | 9 13 24 | 11 9 32 |
Table 5.2328.6 GPS week: 2328 Day: 6 MJD: 60546.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 13 32 | 8 12 36 | 9 11 33 |
emr | emr 2976 | 15 24 33 | 7 14 37 | 10 13 39 |
esa | esa 2976 | 13 21 38 | 6 15 40 | 13 12 34 |
gfz | gfz 2974 | 10 15 30 | 6 14 27 | 14 13 42 |
grg | grg 3072 | 10 17 35 | 7 16 39 | 10 12 28 |
igr | igr 2976 | 10 16 32 | 6 14 31 | 9 11 29 |
igs | igs 2976 | 9 16 31 | 6 13 30 | 9 10 28 |
jgx | jgx 2976 | 10 14 31 | 7 17 31 | 8 10 24 |
jpl | jpl 2976 | 16 25 46 | 9 18 40 | 12 17 45 |
mit | mit 3072 | 14 16 40 | 7 12 30 | 11 8 26 |
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 6.2328 GPS week: 2328 MJD: 60540.500-60546.500
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 -12 41 -26 0 | -2 22
| 17 14 38 41 5 | 2
emr uuuuu | -26 -5 -31 -25 -3 | -9 29
| 10 16 44 63 7 | 2
esa uuuuu | 12 4 52 95 10 | 16 31
| 13 10 40 57 8 | 4
gfz uuuuu | -23 -49 102 -2 -1 | 1 22
| 20 17 82 115 5 | 2
grg uuuuu | -17 -6 23 -56 1 | 4 22
| 17 12 40 95 3 | 2
igr xxxxx | -19 -6 13 3 1 | 8 24
| 9 11 46 46 5 | 1
irf xxxxx | -9 5 -3 3 -4 | 2 22
| 9 7 12 14 1 | 2
jgx uuuuu | -5 -2 -20 -43 -1 | 13 25
| 12 10 26 45 4 | 2
mit uuuuu | 28 28 -38 -6 -4 | 22 31
| 16 15 17 29 2 | 2
ngs uuuuu | 16 31 -143 67 -2 | 7 23
| 21 17 71 116 6 | 2
sio xxxxx | -28 -1 -96 -48 3 | 27 36
| 58 48 88 33 8 | 2
Table 7.2328.0 GPS week: 2328 Day: 0 MJD: 60540.500
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 | -41 12 15 -78 0 | -3 28
emr uuuuu | -30 3 -99 -142 6 | -12 35
esa uuuuu | 32 -3 2 151 8 | 10 32
gfz uuuuu | -2 -44 238 208 3 | 0 27
grg uuuuu | -9 1 9 -152 1 | 2 27
igr xxxxx | -17 9 -9 26 0 | 6 28
irf xxxxx | 4 0 1 -10 -4 | 2 27
jgx uuuuu | 10 11 12 -11 -3 | 13 30
mit uuuuu | 27 -3 -54 -5 -1 | 22 34
ngs uuuuu | 4 36 -141 -11 -11 | 8 29
sio xxxxx | -119 -41 -134 -88 3 | 23 36
Table 7.2328.1 GPS week: 2328 Day: 1 MJD: 60541.500
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 | -20 4 87 -77 -2 | 0 27
emr uuuuu | -36 -36 18 -65 -7 | -7 31
esa uuuuu | 8 -6 25 103 12 | 15 33
gfz uuuuu | -12 -66 115 90 5 | 3 26
grg uuuuu | -14 -10 -27 -62 2 | 6 27
igr xxxxx | -36 -13 -43 -44 8 | 7 27
irf xxxxx | -22 -3 2 2 -6 | 5 27
jgx uuuuu | -10 5 -45 13 -5 | 16 30
mit uuuuu | 35 38 -61 0 -3 | 25 35
ngs uuuuu | 8 40 -141 -7 -3 | 10 29
sio xxxxx | -87 -75 -247 -74 12 | 27 37
Table 7.2328.2 GPS week: 2328 Day: 2 MJD: 60542.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -4 -19 -10 16 -7 | -3 24
emr uuuuu | -23 9 -17 53 -4 | -9 31
esa uuuuu | 11 -1 99 104 17 | 13 30
gfz uuuuu | -21 -75 141 -96 6 | 0 23
grg uuuuu | -42 -26 -23 -114 3 | 2 23
igr xxxxx | -22 -25 62 -63 2 | 8 26
irf xxxxx | 0 0 12 25 -2 | 1 23
jgx uuuuu | -13 3 14 9 -6 | 12 26
mit uuuuu | 52 32 -12 44 -3 | 21 31
ngs uuuuu | -14 50 -168 -53 -4 | 6 24
sio xxxxx | 57 12 -5 -39 11 | 25 35
Table 7.2328.3 GPS week: 2328 Day: 3 MJD: 60543.500
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 -25 35 -29 -1 | 0 23
emr uuuuu | -21 -15 -54 -25 -15 | -7 29
esa uuuuu | 7 21 112 120 14 | 18 32
gfz uuuuu | -47 -40 53 -56 -1 | 4 22
grg uuuuu | -14 -15 84 -57 4 | 6 23
igr xxxxx | -9 1 80 58 6 | 9 26
irf xxxxx | -12 17 -1 5 -6 | 4 23
jgx uuuuu | -8 -7 -7 -81 3 | 14 27
mit uuuuu | 45 35 -45 -31 -5 | 24 33
ngs uuuuu | 24 34 -150 196 1 | 9 24
sio xxxxx | -4 71 -36 -62 6 | 29 37
Table 7.2328.4 GPS week: 2328 Day: 4 MJD: 60544.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 10 -12 14 -16 1 | -4 21
emr uuuuu | -8 1 24 21 0 | -11 30
esa uuuuu | 27 6 47 148 15 | 16 30
gfz uuuuu | -47 -47 35 -119 -5 | 0 21
grg uuuuu | -38 -1 44 -150 2 | 3 21
igr xxxxx | -11 -8 20 45 1 | 7 23
irf xxxxx | -8 2 -27 13 -3 | -1 20
jgx uuuuu | -6 -12 -32 -68 3 | 11 23
mit uuuuu | 8 37 -40 -2 -6 | 20 29
ngs uuuuu | 53 28 -70 228 -5 | 5 20
sio xxxxx | -11 7 -68 -24 3 | 26 35
Table 7.2328.5 GPS week: 2328 Day: 5 MJD: 60545.500
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 -23 71 -29 2 | -2 19
emr uuuuu | -24 -7 -24 -9 1 | -8 27
esa uuuuu | -3 13 29 46 9 | 21 30
gfz uuuuu | -32 -24 -7 -7 -9 | 2 19
grg uuuuu | 3 10 31 83 -2 | 6 18
igr xxxxx | -17 -4 16 16 -5 | 10 22
irf xxxxx | -17 9 -6 3 -3 | 1 18
jgx uuuuu | -18 2 -31 -69 1 | 13 23
mit uuuuu | 17 17 -26 0 -5 | 22 29
ngs uuuuu | 24 -4 -59 -18 8 | 6 20
sio xxxxx | -9 33 -21 -60 0 | 29 35
Table 7.2328.6 GPS week: 2328 Day: 6 MJD: 60546.500
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 -21 78 30 10 | -5 15
emr uuuuu | -38 7 -62 -7 0 | -12 22
esa uuuuu | 2 -1 53 -6 -6 | 20 28
gfz uuuuu | -2 -50 136 -32 -3 | 0 15
grg uuuuu | -4 -2 42 61 -5 | 4 15
igr xxxxx | -22 -6 -32 -20 -6 | 8 18
irf xxxxx | -11 5 -1 -16 -3 | -1 14
jgx uuuuu | 12 -18 -51 -94 1 | 11 17
mit uuuuu | 15 36 -25 -49 -5 | 19 24
ngs uuuuu | 16 31 -275 132 2 | 5 15
sio xxxxx | -22 -18 -158 10 -11 | 28 34
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