[IGSREPORT-29926] Wk 2316 IGS Final Orbits
acc
acc at igs.org
Mon Jun 17 07:59:21 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2316 (May 26, 2024 - Jun 01, 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_20241470000_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 | ALL | 07
0 | COD | ASCG CPVG JFNG MATE MAYG SCUB TONG MATE
0 | GFZ | POHN JFNG POHN
0 | GRG | SVTL NKLG SVTL
0 | MIT | BJFS KITG KOKV KOUG MADR METG MOBS REYK SFER TIDB
0 | MIT | TOW2 VNDP WTZZ YEBE BJFS KITG KOKV KOUG MADR METG
0 | MIT | MOBS REYK SFER TIDB TOW2 VNDP WTZZ YEBE
1 | ALL | 07
1 | COD | DAV1 NYA2 THTG
1 | GFZ | POHN POHN TASH
1 | GRG | DAV1 NYA2 OUS2 SVTL DAV1 NYA2 OUS2 SVTL VOIM WIND
1 | MIT | FTNA GAMG MARS PARC REDU SFER YEBE FTNA GAMG MARS
1 | MIT | PARC REDU SFER YEBE
2 | ALL | 07
2 | COD | 20 ASCG CPVG DAV1 IISC MADR SCUB SVTL IISC MADR
2 | ESA | AREQ AREQ JFNG THTG
2 | GFZ | 5 LAUT LAUT SCUB
2 | GRG | AREQ CPVG JFNG THTG AREQ JFNG
2 | MIT | CHTI MEDI NRC1 SFER STR1 TRO1 CHTI MEDI NRC1 SFER
2 | MIT | STR1 TRO1
3 | ALL | 07
3 | COD | THTG THTG
3 | GFZ | PTVL PTVL
3 | GRG | JFNG SCUB JFNG SCUB
3 | MIT | DARW FLIN FLRS MAR6 MCM4 METG MOBS PTVL SFER TRO1
3 | MIT | VNDP YEBE DARW FLIN FLRS MAR6 MCM4 METG MOBS PTVL
3 | MIT | SFER TRO1 VNDP YEBE
4 | ALL | 07
4 | COD | AREQ BJFS PTVL SCUB IRKJ PTVL
4 | GFZ | AREQ HERS POHN HERS POHN
4 | GRG | 8 8 CZTG SVTL BJFS CZTG SVTL
4 | MIT | AREQ CHTI DAEJ HERS HOLB KERG MEDI NYA1 POHN STJ3
4 | MIT | VNDP YEBE CHTI DAEJ HERS HOLB KERG MEDI NYA1 POHN
4 | MIT | STJ3 VNDP YEBE
5 | ALL | 07
5 | COD | DRAO LPGS NNOR SCUB NNOR
5 | GFZ | HERS IRKJ POHN BRUX HERS IRKJ SCUB
5 | GRG | 21 CZTG JFNG CZTG JFNG LPGS
5 | MIT | DRAO GLPS HERS KERG MEDI VNDP YEBE DRAO GLPS HERS
5 | MIT | KERG MEDI VNDP YEBE
6 | ALL | 07
6 | COD | AREQ ASCG IISC MAYG IISC
6 | ESA | JFNG AREQ JFNG VILL
6 | GFZ | AREQ IRKJ SEYG AREQ HERS IRKJ SEYG
6 | GRG | 21 21 CPVG CZTG JFNG CPVG CZTG JFNG
6 | MIT | BRAZ CHTI DAEJ DARW HRAG MAJU MCM4 MEDI NIUM NOT1
6 | MIT | STR1 TLSE VNDP WILL YAR3 YEBE BRAZ CHTI DAEJ DARW
6 | MIT | HERS HRAG MAJU MCM4 MEDI NIUM NOT1 STR1 TLSE VNDP
6 | MIT | WILL YAR3 YEBE
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
1 | COD | ~15:55 | ~ 0.13 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 | 8
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G08 | 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 | -.0 -.5 -.3 -16 -1 -11 -.17
EMR | 0 | 11.4 -1.1 -3.5 -3 0 -11 .07
ESA | 0 | -.4 .5 1.0 -20 -18 14 -.51
GFZ | 0 | .7 -.1 -.3 -2 6 14 .19
GRG | 0 | 1.2 .3 -.4 4 -23 15 -.01
JGX | 0 | 4.5 -3.4 -1.6 1 -29 37 -.19
JPL | 0 | 6.2 .3 -4.7 24 29 -59 .38
MIT | 0 | 1.6 -1.4 8.8 -23 -9 15 .04
NGS | 0 | 8.5 .1 10.7 -38 -5 -1 -.14
SIO | 0 | 1.2 1.5 -10.2 -31 -12 48 .10
COD | 1 | .1 -.2 -.3 -12 0 -17 -.20
EMR | 1 | 8.8 -.9 -1.4 3 20 -35 -.12
ESA | 1 | .1 .2 .6 -9 -17 12 -.57
GFZ | 1 | -.3 .1 -.2 -16 -14 7 .20
GRG | 1 | 1.4 -.1 -.2 -1 -16 10 -.05
JGX | 1 | 7.2 -2.4 -2.4 13 -36 53 -.11
JPL | 1 | 9.7 -3.1 -6.5 -2 26 -103 .64
MIT | 1 | 3.8 -.5 11.1 -25 -23 7 .07
NGS | 1 | 8.6 5.5 3.6 -3 -18 8 -.14
SIO | 1 | 1.6 7.3 -6.2 31 37 20 .12
COD | 2 | .6 -.3 -.3 2 -10 -19 -.16
EMR | 2 | 7.0 -3.5 -1.4 -9 -5 -2 .10
ESA | 2 | .4 -.0 -.6 -3 -25 10 -.47
GFZ | 2 | -.2 -.0 -.7 14 -5 -10 .13
GRG | 2 | .6 .5 -.1 9 5 -9 -.15
JGX | 2 | 8.2 -3.5 1.3 0 -34 53 .04
JPL | 2 | 1.7 -2.7 -5.0 8 45 -74 .69
MIT | 2 | 5.7 -1.1 11.2 3 8 -19 -.00
NGS | 2 | 7.6 .4 2.6 -8 -14 0 -.13
SIO | 2 | 2.4 .1 1.5 48 -24 35 .06
COD | 3 | .5 -.5 -.3 12 -26 -16 -.17
EMR | 3 | 5.1 -9.0 -1.0 -3 -8 6 .03
ESA | 3 | .2 -.0 .7 -2 -12 13 -.70
GFZ | 3 | .3 -.1 -.1 1 -6 -8 -.16
GRG | 3 | .4 .1 .1 7 -5 -3 -.19
JGX | 3 | 4.7 -9.9 1.3 -6 -19 98 -.25
JPL | 3 | -1.2 -3.3 -.2 -12 44 -44 .22
MIT | 3 | .6 -4.5 14.0 16 15 0 -.27
NGS | 3 | 2.8 -6.2 2.6 -32 8 4 -.09
SIO | 3 | -.9 .5 -5.9 -20 23 19 -.15
COD | 4 | .3 -.1 .7 6 -15 -15 -.13
EMR | 4 | 8.1 -3.5 -3.4 4 -28 31 .05
ESA | 4 | .4 .2 .1 -10 -18 21 -.58
GFZ | 4 | -.1 -.1 -1.0 7 -8 -12 .11
GRG | 4 | .4 -.1 -.4 12 -11 2 .07
JGX | 4 | -.0 -5.7 -.3 4 -17 80 .16
JPL | 4 | .9 -6.1 -6.3 2 27 -67 .80
MIT | 4 | -.3 -1.1 10.7 -1 4 -4 .09
NGS | 4 | 1.3 .4 -11.3 20 -25 -19 -.06
SIO | 4 | -2.6 -5.0 -2.6 -19 29 59 .14
COD | 5 | .6 -.3 .2 7 -15 -12 -.10
EMR | 5 | 11.9 -6.7 -.9 17 -43 19 .03
ESA | 5 | .0 .7 .9 -12 -12 6 -.43
GFZ | 5 | .1 -.6 -.9 -4 -16 -14 .36
GRG | 5 | .8 .1 -.4 16 -9 -6 .21
JGX | 5 | 5.9 -8.0 -1.5 -8 -43 97 -.18
JPL | 5 | 6.4 -5.0 -2.5 -10 50 -77 .86
MIT | 5 | -.7 -2.2 9.1 16 28 2 .12
NGS | 5 | -1.2 -2.3 -1.8 -22 25 -21 .07
SIO | 5 | -4.2 -1.4 -4.6 -30 16 55 .28
COD | 6 | .4 -.3 .2 0 -6 -10 -.09
EMR | 6 | 9.9 -3.8 -2.6 3 -21 28 .04
ESA | 6 | .6 .6 .9 -8 -11 9 -.55
GFZ | 6 | -.3 -.2 -1.1 3 -8 -1 .41
GRG | 6 | .1 -.3 -.3 11 -3 10 .01
JGX | 6 | 9.7 -11.2 -1.3 -10 -55 119 -.20
JPL | 6 | 6.7 -1.0 -7.9 34 23 -29 .74
MIT | 6 | 3.3 -2.4 10.6 28 2 22 .15
NGS | 6 | 6.8 -2.8 1.2 -36 -37 16 -.04
SIO | 6 | .7 -.3 -8.2 21 -19 40 .18
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 1.2316.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2316.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 2.2316.[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 3.2316.[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 5.2316.0-6). 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 2316 summary. (May 26, 2024 - Jun 01, 2024)
Table 1.2316.a GPS week: 2316 MJD: 60456.000-60462.000
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 806| -1 -1 -1 10 0 9 -.02 7 6 | -644 275 5 95
| 0 0 0 9 11 16 .01 | 101 386
emr 93| 0 0 4 -1 11 24 .04 11 10 | -1431 -54 59 119
| 1 0 1 14 16 13 .03 | 523 756
esa 150| 0 0 4 -1 -4 7 -.05 9 9 | -1649 1239 4 75
| 0 0 0 10 12 14 .01 | 183 155
gfz 116| 0 -1 0 38 -1 -14 .08 10 9 | -54 20 9 98
| 0 1 1 17 13 9 .04 | 161 280
grg 113| 2 0 4 6 -3 0 .04 15 8 | 14 -42 9 130
| 1 0 2 12 10 7 .04 | 107 176
igr n/a| 0 0 0 3 13 10 .01 4 4 | 1591 738 10 83
| 0 0 0 11 8 11 .01 | 1404 610
jgx n/a| 0 0 -1 25 -3 38 -.02 12 12 | -29 30 34 100
| 0 0 1 13 15 32 .02 | 85 138
jpl n/a| -1 0 0 18 -24 4 .16 27 27 | -1996 -18 84 199
| 1 1 1 17 19 28 .02 | 472 653
mit 384| -1 1 -6 -14 -8 -37 .01 8 7 | 5393 -6891 40 70
| 0 0 0 26 19 25 .01 | 1493 397
ngs 275| 0 0 1 -16 7 0 -.08 11 9 | -642 267 540 796
| 0 0 4 13 28 13 .03 | 104 389
sio 326| -1 0 -2 -34 -5 0 .01 10 8 | --- --- --- ---
| 1 0 1 9 18 18 .01 | --- ---
Table 1.2316.b GPS week : 2316 MJD: 60456.000-60462.000
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 | 7 8 7 7 7 6 7 |
2 | 4 4 3 3 4 3 3 |
3 | 4 4 4 4 4 4 4 |
4 | 3 2 3 3 3 3 3 |
5 | 3 4 4 3 4 3 3 |
6 | 3 3 3 3 3 2 3 |
7 | 16 3 3 3 3 3 2 |
8 | 3 3 3 3 12 4 3 |
9 | 3 3 3 2 2 2 2 |
10 | 4 3 3 3 3 4 3 |
11 | 3 3 3 3 3 3 3 |
12 | 4 3 3 4 4 3 4 |
13 | 3 3 3 3 3 3 3 |
14 | 4 4 4 4 4 4 3 |
15 | 3 3 3 3 3 3 3 |
16 | 4 4 4 4 5 0 4 |
17 | 4 3 3 3 3 3 3 |
18 | 4 3 3 3 4 4 3 |
19 | 4 4 3 3 3 3 3 |
20 | 4 4 6 5 5 4 3 |
21 | 4 4 3 3 4 5 3 |
22 | 3 4 3 3 3 3 3 |
23 | 4 4 4 4 4 5 4 |
24 | 3 3 3 3 3 3 3 |
25 | 4 3 3 3 3 3 3 |
26 | 3 3 3 4 4 4 3 |
27 | 3 3 3 3 3 3 3 |
28 | 3 3 4 3 4 4 4 |
29 | 4 4 3 4 3 4 4 |
30 | 3 3 3 3 3 3 2 |
31 | 3 3 3 3 3 3 3 |
32 | 3 3 3 3 3 3 2 |
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 2.2316.0 GPS week: 2316 Day: 0 MJD: 60456.000
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 814| -1 0 -2 18 17 11 -.03 7 7 | -722 -5 5 93
emr 94| 0 1 3 9 -2 3 .03 11 11 | -1500 -443 66 120
esa 150| 0 0 2 -8 -4 0 -.04 9 9 | -1537 1132 5 80
gfz 123| 0 -2 0 38 4 -23 .10 9 9 | 43 -55 9 85
grg 116| 0 -1 0 3 -13 7 .03 9 8 | 155 -189 8 127
igr n/a| 0 0 0 24 10 -8 .01 4 4 | -131 264 10 79
jgx n/a| 0 0 -2 23 2 15 -.05 10 10 | 71 -57 28 100
jpl n/a| -2 0 0 30 -20 10 .13 27 27 | -1230 -610 85 163
mit 384| 0 1 -6 -12 -20 -29 -.01 9 8 | 3676 -7378 44 68
ngs 282| 0 0 9 -30 29 4 -.07 11 10 | -724 -11 507 742
sio 345| 0 0 -2 -46 -23 14 -.00 11 10 | --- --- --- ---
Table 2.2316.1 GPS week: 2316 Day: 1 MJD: 60457.000
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 813| -1 -1 -1 5 -3 -14 -.02 6 6 | -635 192 5 100
emr 94| 0 2 4 15 -7 19 .01 11 11 | -1879 -144 49 139
esa 150| 0 0 4 4 14 -15 -.04 9 9 | -1756 1458 5 76
gfz 123| 0 -2 1 33 -2 -20 .04 8 8 | -96 64 9 108
grg 118| 1 0 3 3 8 8 .10 10 8 | -142 227 8 148
igr n/a| 0 0 0 5 19 4 .01 4 3 | 215 1064 11 94
jgx n/a| 0 0 0 22 2 52 -.05 11 11 | -167 291 32 104
jpl n/a| 0 -1 0 27 -26 -34 .16 27 27 | -1760 -84 86 206
mit 384| -1 0 -7 -31 -23 1 .02 8 7 | 4023 -6579 42 80
ngs 283| 0 0 2 -15 7 14 -.07 10 9 | -636 189 563 777
sio 341| 0 0 -2 -20 5 -9 .03 10 8 | --- --- --- ---
Table 2.2316.2 GPS week: 2316 Day: 2 MJD: 60458.000
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| 0 0 -2 3 8 2 -.02 7 7 | -520 -81 6 94
emr 90| 0 0 3 -9 19 36 .06 10 10 | -852 -969 65 102
esa 150| 0 0 4 0 -11 5 -.06 9 9 | -1430 994 5 73
gfz 118| -1 -3 1 47 4 -22 .02 9 9 | -158 200 8 102
grg 116| 2 0 3 16 2 -8 .08 9 9 | 49 5 9 110
igr n/a| 0 0 0 5 7 9 .02 4 3 | 1172 -32 10 81
jgx n/a| 1 0 0 3 0 58 -.01 13 13 | 37 11 31 103
jpl n/a| -2 0 0 30 -6 -9 .16 26 26 | -1928 -697 84 197
mit 384| 0 0 -7 -26 0 -35 .02 8 7 | 4778 -7270 43 73
ngs 278| 0 0 3 2 8 14 -.04 10 8 | -509 -100 495 777
sio 335| 0 1 -1 -30 -33 -11 -.00 10 8 | --- --- --- ---
Table 2.2316.3 GPS week: 2316 Day: 3 MJD: 60459.000
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 807| 0 -1 -1 10 7 23 -.02 6 6 | -514 -173 5 89
emr 94| 0 0 5 -5 12 17 .07 10 10 | -1096 -377 64 128
esa 150| 0 -1 4 -6 9 14 -.05 9 9 | -1516 1152 4 79
gfz 115| 0 -1 -1 9 12 4 .11 9 9 | 145 -286 11 104
grg 114| 3 0 5 -1 5 -4 -.00 9 8 | 100 -220 10 148
igr n/a| 0 0 0 -10 25 29 .02 4 4 | 1245 462 9 72
jgx n/a| 0 0 0 20 11 80 -.01 14 14 | 8 -84 39 111
jpl n/a| -1 2 2 0 2 45 .17 26 26 | -2615 -449 82 211
mit 384| -1 1 -6 22 -28 -63 .01 8 7 | 5046 -7167 44 77
ngs 276| 1 0 1 -20 -27 -1 -.09 11 9 | -512 -181 508 835
sio 325| -1 1 -3 -24 -12 -28 .02 9 7 | --- --- --- ---
Table 2.2316.4 GPS week: 2316 Day: 4 MJD: 60460.000
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 800| 0 -1 -1 6 -15 35 -.01 8 7 | -716 586 6 106
emr 96| 2 0 5 10 39 23 .04 12 11 | -781 -187 57 110
esa 150| -1 0 4 15 -5 23 -.06 9 9 | -1567 1286 5 80
gfz 112| 0 0 3 66 11 -11 .10 12 10 | -84 31 10 97
grg 111| 3 0 4 12 1 3 .02 49 9 | 39 -204 9 115
igr n/a| 0 0 2 5 22 15 .01 4 4 | 1946 604 11 71
jgx n/a| 1 -1 0 47 11 59 -.01 14 14 | -10 -76 36 99
jpl n/a| -1 0 0 16 -25 -9 .16 27 27 | -2398 16 85 231
mit 384| -1 1 -6 -57 -19 -72 .02 8 6 | 5567 -6661 40 67
ngs 270| 0 0 -3 -10 -19 -9 -.13 13 10 | -713 578 497 766
sio 317| -2 0 -2 -44 3 1 .01 12 9 | --- --- --- ---
Table 2.2316.5 GPS week: 2316 Day: 5 MJD: 60461.000
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 797| -1 -1 -1 27 -13 0 -.00 7 6 | -778 804 6 93
emr 97| 2 1 4 -24 18 47 .05 10 9 | -1855 320 61 122
esa 150| -1 0 5 -15 -17 23 -.05 9 8 | -1805 1323 5 75
gfz 110| -2 0 0 31 -22 -10 .09 10 10 | 91 -312 9 99
grg 111| 3 0 6 -14 -19 -10 .01 10 8 | 10 -54 9 126
igr n/a| 0 0 0 -7 3 11 -.01 4 4 | 2904 996 11 84
jgx n/a| 1 0 -2 29 -29 2 .01 11 11 | -25 -12 35 92
jpl n/a| 0 0 0 -10 -43 -10 .21 27 27 | -2292 661 83 202
mit 384| -1 1 -6 7 14 -41 .02 8 7 | 6829 -6880 37 65
ngs 270| 1 0 -1 -6 56 -21 -.10 11 10 | -779 802 596 818
sio 309| 0 1 -4 -39 0 20 .00 9 7 | --- --- --- ---
Table 2.2316.6 GPS week: 2316 Day: 6 MJD: 60462.000
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 800| -1 0 -1 2 2 9 -.01 6 6 | -624 602 5 92
emr 87| 0 0 3 -5 1 24 -.01 10 10 | -2055 1422 55 113
esa 150| 0 -1 5 0 -16 -1 -.07 8 8 | -1935 1330 4 68
gfz 111| 0 -1 0 40 -16 -19 .11 9 9 | -323 499 9 93
grg 109| 3 -1 7 22 -9 4 .02 10 9 | -112 138 10 139
igr n/a| 0 0 0 1 4 10 .01 4 4 | 3789 1810 9 106
jgx n/a| 0 0 -2 28 -19 -2 -.03 10 10 | -123 143 43 92
jpl n/a| 0 0 0 37 -53 35 .17 28 28 | -1752 1031 88 188
mit 384| 0 0 -5 -5 18 -19 .01 7 6 | 7834 -6307 34 65
ngs 266| 2 0 0 -35 -1 -3 -.09 11 10 | -623 595 616 858
sio 311| -1 0 -4 -38 18 17 -.00 8 7 | --- --- --- ---
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 3.2316.0 GPS week: 2316 Day: 0 MJD: 60456.000
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 --- --- --- 12 13 --- --- 8 --- --- 7 | 35 --- --- --- 32 34 --- --- 33 --- --- 33
2 | 11 11 5 8 10 5 8 11 15 12 12 3 | 19 18 19 18 22 18 19 18 20 22 22 18
3E | 7 13 11 10 11 4 13 12 7 14 15 4 | 23 23 27 22 25 21 24 24 22 22 22 22
4 | 8 11 4 7 6 2 8 45 6 9 9 2 | 63 61 62 63 60 61 60 73 59 63 60 61
5E | 6 11 7 9 6 1 10 11 5 10 8 2 | 36 41 41 34 39 39 41 41 40 43 41 39
6 | 5 13 8 9 10 2 7 10 9 8 9 3 | 24 24 26 25 23 23 20 26 21 24 23 22
X7 | 14 --- --- --- 17 14 --- 44 --- --- --- 15 | 39 --- --- --- 43 34 --- 43 --- --- --- 40
8 | 6 10 9 8 8 2 6 9 7 13 9 3 | 591 595 593 590 609 592 594 593 592 591 594 592
9 | 5 9 7 8 6 3 5 9 7 8 10 2 | 23 26 24 22 22 23 22 27 20 23 23 22
10E | 8 12 10 14 14 5 11 8 7 7 10 3 | 30 29 30 35 33 30 28 30 28 29 30 29
11 | 7 12 6 10 7 2 9 63 7 10 7 3 | 31 33 34 37 36 33 33 45 35 33 34 33
12E | 7 12 8 13 7 5 12 11 11 11 10 3 | 71 70 69 73 73 72 69 73 76 73 76 72
13 | 5 11 7 8 5 3 7 11 7 6 8 2 | 26 33 26 27 27 27 27 34 28 27 28 26
14 | 7 9 21 7 10 5 9 60 12 14 6 4 | 42 47 56 47 44 47 46 60 41 49 45 45
15 | 7 8 5 8 6 3 12 8 8 11 13 3 | 59 55 54 59 54 54 60 57 55 50 52 55
16E | 8 10 8 9 10 3 16 9 7 12 9 3 | 24 19 19 22 24 22 19 18 22 20 20 21
17 | 12 10 8 8 7 5 9 10 10 9 11 3 | 34 26 26 31 27 28 28 28 35 31 37 30
18 | 8 13 9 6 7 4 13 60 8 13 11 3 | 45 44 42 43 45 42 42 52 42 40 44 42
19 | 6 11 7 9 8 3 17 9 10 9 11 3 | 28 27 29 31 27 30 30 28 34 33 33 29
20E | 7 8 9 12 12 4 10 11 14 10 16 4 | 101 103 100 99 104 101 101 100 108 103 108 102
21 | 10 11 5 8 9 3 9 11 10 12 12 3 | 18 18 16 16 23 15 18 17 18 19 20 16
22E | 5 9 7 9 7 3 8 6 9 9 10 2 | 40 38 41 41 38 40 42 40 41 41 44 40
23E | 8 10 17 11 12 3 10 56 10 15 15 4 | 30 33 43 39 35 33 34 44 35 29 37 34
24 | 10 11 9 7 7 3 9 12 8 10 11 3 | 28 32 26 34 27 30 25 36 27 32 32 28
25 | 6 16 10 11 10 4 7 13 12 10 8 3 | 27 29 29 29 30 27 24 30 27 29 26 26
26 | 7 11 7 10 11 3 9 10 8 13 9 3 | 27 20 22 25 23 22 21 22 25 21 22 21
27 | 6 9 8 11 6 3 7 10 8 14 12 3 | 20 19 22 23 21 19 17 22 19 22 19 19
28 | 7 16 5 6 9 3 9 52 12 8 10 3 | 38 40 37 41 43 39 40 59 39 39 40 39
29 | 7 14 8 10 8 5 17 12 10 10 12 3 | 31 27 27 33 33 30 32 29 29 32 31 29
30 | 4 11 8 6 6 3 10 9 6 8 8 2 | 19 24 19 20 18 19 17 25 17 21 18 18
31 | 6 10 8 9 6 3 10 10 9 13 6 3 | 38 37 38 34 32 35 36 41 40 34 35 36
32 | 4 10 8 7 8 3 8 10 7 9 13 3 | 32 34 32 32 30 32 31 34 30 33 33 31
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 11 9 9 9 4 10 27 9 11 11 |T 52 54 54 54 53 52 53 57 53 54 54 52
WRMS | 7 11 9 9 8 4 10 27 8 10 10 |NE 55 57 57 58 56 54 56 60 55 57 57 54
MEDI | 7 11 8 9 8 3 9 11 8 10 10 |MD 31 32 29 33 32 30 30 34 33 32 33 30
Table 3.2316.1 GPS week: 2316 Day: 1 MJD: 60457.000
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 --- --- --- 16 14 --- --- 9 --- --- 8 | 50 --- --- --- 42 45 --- --- 41 --- --- 45
2 | 8 9 7 10 9 5 8 11 11 12 17 3 | 29 27 28 28 30 28 28 29 26 29 34 27
3E | 7 12 11 8 11 3 10 12 9 15 15 3 | 26 24 29 26 27 25 23 25 24 25 27 24
4 | 7 9 4 4 6 3 9 48 5 5 9 2 | 59 58 59 59 57 58 55 61 56 59 58 58
5E | 5 10 8 7 18 3 13 10 6 14 7 3 | 21 22 24 23 23 23 24 22 23 31 24 22
6 | 4 9 8 8 6 2 9 9 7 9 5 2 | 33 32 35 33 32 32 31 34 31 31 33 32
X7 | 7 10 5 7 5 7 --- 10 7 9 --- 3 | 31 38 36 38 32 31 --- 36 36 37 --- 31
8 | 4 10 8 10 10 2 8 9 8 10 7 3 | 461 465 463 459 475 462 465 463 464 462 463 462
9 | 4 9 7 5 5 3 8 10 6 8 9 2 | 32 32 31 30 30 31 28 33 28 29 31 29
10E | 5 11 9 8 10 2 9 8 7 8 11 3 | 25 24 27 23 25 24 25 25 24 26 26 24
11 | 7 13 8 7 7 2 11 62 8 10 5 3 | 34 34 35 34 36 33 34 39 32 33 32 33
12E | 6 10 10 7 9 3 13 11 8 9 8 3 | 61 59 58 62 64 61 59 62 65 65 63 61
13 | 5 12 7 8 6 3 9 10 7 8 8 2 | 37 40 36 35 35 35 34 42 36 34 34 35
14 | 8 9 19 7 10 4 10 61 9 11 6 3 | 45 47 53 49 47 47 46 54 44 45 47 46
15 | 7 8 5 9 5 4 12 8 7 10 12 3 | 46 42 43 46 44 43 43 46 42 40 40 43
16E | 6 11 8 9 7 6 18 8 8 14 9 3 | 33 28 32 34 32 34 32 27 31 34 33 32
17 | 8 10 7 7 7 4 13 8 8 10 8 3 | 30 30 26 30 28 29 29 32 32 30 31 29
18 | 6 11 9 7 7 3 9 58 6 11 9 3 | 43 43 42 44 43 41 42 47 40 41 42 42
19 | 4 11 6 8 8 6 18 8 12 8 8 3 | 33 32 32 34 32 33 34 33 37 35 35 33
20E | 8 9 9 10 14 6 10 11 16 11 18 4 | 72 76 74 75 75 74 74 73 76 69 77 73
21 | 7 10 7 10 9 4 11 9 8 12 13 3 | 29 28 27 30 29 27 27 28 24 29 30 27
22E | 6 10 7 9 23 4 10 7 10 11 8 4 | 36 36 36 35 38 36 37 34 38 39 37 36
23E | 7 9 20 11 9 3 10 57 9 13 10 4 | 22 21 31 26 25 22 22 29 22 22 25 22
24 | 7 12 8 6 7 4 9 13 8 8 7 2 | 29 32 29 29 28 29 27 36 27 29 28 28
25 | 6 16 10 8 9 3 8 13 10 7 6 3 | 41 39 40 37 41 37 34 40 37 39 37 38
26 | 6 11 9 6 9 3 10 11 9 11 9 3 | 37 33 38 38 34 36 33 31 34 36 37 35
27 | 5 10 7 8 9 3 8 9 6 10 6 2 | 33 28 33 31 31 31 28 31 27 32 27 30
28 | 5 19 4 6 9 3 11 52 10 10 10 3 | 35 37 35 34 36 34 35 47 35 35 36 34
29 | 7 11 8 12 7 4 16 12 6 11 9 3 | 37 33 34 38 37 34 34 36 34 37 34 35
30 | 4 11 7 8 4 3 11 10 6 9 6 2 | 31 31 30 30 29 30 28 34 26 29 30 29
31 | 5 10 6 7 7 3 11 8 10 9 11 3 | 30 30 30 28 26 28 27 33 30 31 31 28
32 | 4 12 8 5 7 2 10 11 7 6 9 2 | 41 39 42 42 39 40 39 40 37 39 39 39
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 11 9 8 10 4 11 27 8 10 10 |T 50 49 50 50 50 49 49 51 48 50 50 48
WRMS | 6 11 9 8 8 3 11 27 7 9 8 |NE 54 54 54 54 53 53 53 56 52 53 54 52
MEDI | 6 10 8 8 8 3 10 10 8 10 9 |MD 33 33 35 34 32 33 33 34 34 34 34 33
Table 3.2316.2 GPS week: 2316 Day: 2 MJD: 60458.000
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 --- --- --- 12 10 --- --- 8 --- --- 7 | 25 --- --- --- 25 24 --- --- 26 --- --- 24
2 | 8 8 7 11 9 4 11 10 7 12 8 3 | 18 18 16 19 19 17 21 19 21 20 21 17
3E | 7 11 12 17 7 3 13 10 8 9 10 3 | 23 28 27 29 24 23 27 25 25 26 24 24
4 | 6 11 6 6 5 2 12 45 4 7 6 2 | 38 36 40 42 40 38 40 50 38 37 40 38
5E | 5 10 9 8 22 2 14 11 6 10 8 4 | 33 36 37 32 27 34 38 37 38 38 38 34
6 | 4 10 9 10 5 2 11 8 7 8 7 2 | 17 20 21 21 18 19 20 22 18 17 17 17
X7 | 4 9 5 12 7 5 --- 8 6 5 8 2 | 27 20 17 17 25 25 --- 27 19 19 26 26
8 | 6 10 9 10 12 3 11 11 6 13 9 3 | 654 654 655 652 679 653 655 655 654 656 652 654
9 | 6 9 7 6 6 2 9 11 6 6 6 2 | 15 22 16 17 16 15 18 20 15 15 14 15
10E | 6 10 9 9 7 2 12 9 5 8 8 2 | 31 30 30 34 32 30 29 31 31 32 31 30
11 | 8 10 9 12 7 3 11 60 7 9 5 3 | 16 19 20 21 22 18 22 27 20 17 19 18
12E | 6 10 10 8 8 4 15 13 9 9 10 3 | 72 74 71 72 75 72 73 75 78 77 76 74
13 | 7 9 6 10 5 4 10 11 7 5 10 2 | 19 23 17 17 19 19 21 25 20 19 23 18
14 | 8 8 19 7 9 5 11 61 10 11 9 3 | 33 38 43 36 38 37 34 50 35 38 34 35
15 | 7 7 6 9 5 4 13 9 7 8 9 2 | 38 34 33 39 34 34 36 38 36 32 32 34
16E | 6 10 8 11 9 2 21 10 8 10 8 3 | 24 20 22 25 25 24 23 20 26 24 25 24
17 | 7 8 6 9 8 5 15 10 7 7 6 2 | 22 24 18 25 22 23 26 25 27 23 27 22
18 | 8 13 8 10 8 3 13 59 5 10 12 3 | 22 25 22 25 24 22 24 33 23 23 23 22
19 | 7 10 7 9 8 5 19 8 9 8 7 3 | 22 25 22 26 24 23 27 24 26 23 26 23
20E | 9 14 9 9 17 9 9 15 20 15 34 6 | 49 51 50 49 53 50 50 52 45 49 50 47
21 | 7 8 9 10 10 3 12 10 7 11 10 3 | 16 19 16 18 17 15 19 20 19 19 18 16
22E | 6 7 7 7 6 3 11 9 8 8 7 2 | 34 34 33 31 34 35 36 34 35 34 36 33
23E | 7 9 21 10 8 3 12 55 8 15 10 4 | 26 27 36 31 33 29 30 35 29 31 28 28
24 | 7 11 9 6 6 4 11 13 5 7 9 2 | 22 26 23 22 21 23 23 29 23 25 24 22
25 | 6 14 10 8 8 3 10 13 9 8 7 3 | 19 23 21 19 22 19 18 24 18 21 19 18
26 | 6 11 9 10 9 4 12 10 9 12 10 3 | 24 20 23 24 25 22 22 23 27 20 26 22
27 | 7 10 7 7 8 2 10 11 6 10 7 2 | 21 21 22 19 20 20 21 22 19 22 22 19
28 | 8 19 4 8 9 3 10 53 8 8 10 3 | 39 43 41 42 41 41 43 52 42 42 44 40
29 | 6 8 7 9 8 3 17 9 6 11 8 3 | 19 18 17 23 19 19 20 20 21 22 21 19
30 | 4 11 7 6 6 3 11 11 5 8 4 2 | 19 25 20 19 17 19 19 25 18 23 18 18
31 | 5 9 6 7 6 3 11 9 9 11 9 3 | 34 36 34 34 31 34 34 38 38 35 36 34
32 | 4 8 9 7 7 2 12 9 6 6 7 2 | 24 27 24 24 24 23 25 30 25 22 25 23
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 10 9 9 9 4 13 26 8 10 10 |T 46 48 47 48 48 46 49 51 47 48 48 46
WRMS | 7 10 9 9 9 3 13 26 7 8 8 |NE 50 52 51 52 51 50 54 56 51 51 52 49
MEDI | 6 10 8 9 8 3 11 11 7 9 8 |MD 24 25 23 25 24 23 25 27 26 23 26 23
Table 3.2316.3 GPS week: 2316 Day: 3 MJD: 60459.000
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 14 --- --- 10 --- --- 6 | 32 --- --- --- 29 30 --- --- 27 --- --- 28
2 | 7 8 5 10 12 5 11 9 9 13 7 3 | 17 19 17 19 19 18 20 18 18 19 19 17
3E | 6 13 11 13 9 3 18 10 8 9 11 3 | 20 22 24 20 21 19 22 20 18 16 20 18
4 | 7 10 4 6 6 2 13 46 5 10 7 2 | 26 26 27 28 30 26 29 42 28 22 28 26
5E | 6 9 9 9 7 3 15 10 7 9 7 3 | 25 25 26 25 29 25 30 29 25 28 24 25
6 | 3 10 8 8 10 2 11 9 4 11 6 2 | 23 24 23 23 21 22 24 26 19 20 20 21
X7 | 6 8 5 12 5 5 --- 7 5 12 6 3 | 28 29 25 31 29 32 --- 35 27 32 18 31
8 | 5 8 8 9 13 2 10 11 7 12 6 3 | 345 345 345 347 357 345 346 346 344 345 345 345
9 | 4 9 6 8 5 2 9 9 4 7 8 2 | 19 24 19 17 16 18 21 23 18 18 19 18
10E | 5 9 10 13 8 4 12 9 7 8 12 3 | 27 26 27 28 27 26 27 28 24 25 28 25
11 | 7 12 9 8 7 3 11 59 6 15 8 3 | 22 23 26 28 25 24 26 36 26 20 27 24
12 | 5 9 10 7 15 4 18 11 7 12 7 3 | 53 53 53 57 58 54 54 54 54 57 54 54
13 | 5 9 6 9 5 4 12 9 8 4 8 2 | 21 27 20 20 22 22 25 29 23 21 22 21
14 | 8 7 19 9 10 6 10 63 7 10 9 3 | 33 38 43 38 37 38 36 51 32 36 33 35
15 | 7 8 6 9 5 3 18 8 7 8 9 3 | 46 42 42 49 41 44 47 45 42 42 41 43
16E | 7 9 8 13 7 4 19 12 12 8 10 3 | 34 30 32 34 31 34 29 31 35 31 36 34
17 | 6 8 8 9 8 5 13 10 9 9 10 3 | 24 25 20 27 24 24 27 26 26 24 29 24
18 | 7 13 8 5 9 4 14 55 6 10 12 3 | 25 27 27 28 27 27 28 40 26 24 27 25
19 | 6 11 7 10 10 4 19 11 6 8 10 3 | 24 24 22 28 26 24 29 25 26 23 29 24
20E | 10 12 7 8 16 5 16 13 13 26 15 5 | 54 56 57 58 57 54 54 53 54 58 60 55
21 | 6 7 6 9 12 4 12 9 9 13 8 3 | 16 20 16 19 19 16 19 18 17 19 18 16
22E | 5 7 8 9 9 5 12 8 8 8 11 3 | 46 43 43 46 43 45 47 43 44 45 44 44
23E | 8 10 18 9 10 5 14 52 10 11 13 4 | 24 26 34 30 26 26 27 33 25 24 29 26
24 | 5 10 8 12 5 6 13 13 9 11 9 3 | 23 28 25 33 24 27 26 32 23 26 25 24
25 | 3 13 9 8 8 3 10 11 9 11 7 3 | 25 26 26 25 26 24 25 29 23 27 25 24
26 | 6 13 8 10 12 3 11 12 9 10 10 3 | 26 23 24 26 23 24 24 24 25 20 26 23
27 | 6 9 7 8 9 3 9 9 7 12 6 2 | 22 21 22 21 22 20 21 23 19 21 21 20
28 | 5 21 4 9 8 4 12 53 7 7 9 3 | 23 29 26 28 25 25 29 46 24 24 28 24
29 | 6 10 8 7 8 3 21 9 6 15 9 3 | 21 18 19 25 23 22 27 23 21 22 22 20
30 | 4 11 8 6 7 3 11 10 6 5 8 2 | 23 30 22 25 19 24 25 29 20 23 21 22
31 | 4 9 6 7 5 3 11 8 7 6 7 2 | 37 35 36 36 31 35 34 37 36 33 35 34
32 | 5 5 8 7 6 3 12 9 9 11 6 2 | 23 25 24 27 22 24 26 30 22 20 22 22
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 10 9 9 9 4 14 26 8 11 9 |T 37 39 38 40 38 38 40 42 37 37 38 37
WRMS | 6 10 9 9 8 4 14 26 7 9 7 |NE 38 40 38 41 39 38 41 44 38 38 39 37
MEDI | 6 9 8 9 8 4 12 10 7 10 8 |MD 24 26 26 28 26 25 27 30 25 24 27 24
Table 3.2316.4 GPS week: 2316 Day: 4 MJD: 60460.000
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 --- --- --- 13 16 --- --- 9 --- --- 7 | 24 --- --- --- 24 25 --- --- 23 --- --- 22
2 | 8 7 5 14 10 4 12 13 8 21 9 3 | 15 17 14 18 17 15 20 18 20 23 18 15
3E | 5 12 12 14 9 3 13 11 6 13 16 3 | 17 19 22 15 17 16 17 20 17 15 21 16
4 | 6 10 6 7 7 3 12 46 5 10 11 2 | 40 39 42 43 39 41 43 51 40 42 45 41
5E | 5 8 10 11 13 3 16 8 7 15 9 3 | 23 24 25 22 23 23 26 24 26 27 27 23
6 | 5 8 9 9 8 2 10 9 3 10 9 2 | 20 20 22 19 18 18 19 23 17 18 19 18
X7 | 5 6 4 10 5 3 --- 8 5 8 11 2 | 29 28 27 30 30 28 --- 32 28 29 23 29
8 | 25 35 19 43 267 12 39 35 23 28 38 11 | 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999 9999
9 | 3 8 7 6 5 2 8 10 5 8 10 2 | 18 22 18 18 17 18 21 22 17 18 21 17
10E | 6 9 10 9 9 4 18 10 6 10 9 3 | 23 23 23 28 22 23 29 23 21 21 25 22
11 | 7 11 7 7 6 3 10 61 4 12 9 2 | 18 22 21 21 20 18 21 28 21 17 20 19
12 | 6 12 9 9 13 4 15 11 7 11 9 3 | 54 52 52 57 54 55 53 55 57 61 57 55
13 | 6 11 6 11 5 4 11 10 7 8 13 3 | 19 26 18 20 18 19 23 27 19 18 20 18
14 | 8 8 18 8 9 6 9 64 6 12 8 3 | 35 41 46 43 40 41 37 52 36 34 37 38
15 | 6 7 5 7 7 4 14 8 7 9 9 2 | 39 37 35 38 35 35 40 40 36 39 37 37
16 | 8 9 5 17 23 4 22 10 10 12 16 5 | 35 33 30 35 44 33 37 30 33 33 34 33
17 | 6 7 6 11 9 3 12 10 7 11 6 3 | 24 25 22 28 25 24 24 25 28 25 27 24
18 | 7 13 9 9 8 3 13 57 5 11 14 3 | 25 28 25 29 27 23 27 36 26 22 26 25
19 | 5 10 7 9 11 4 16 11 5 10 9 3 | 22 26 25 27 26 24 26 26 27 23 28 24
20E | 17 12 5 13 12 5 11 13 11 16 12 4 | 37 35 34 35 36 36 38 37 39 40 40 35
21 | 9 6 7 11 10 3 12 13 8 19 10 3 | 16 19 15 18 18 15 20 21 20 23 18 15
22 | 6 6 8 5 8 5 10 9 6 13 7 2 | 59 60 60 59 58 59 60 60 59 59 60 59
23E | 8 9 20 12 12 4 14 52 7 14 13 4 | 21 21 27 22 20 21 21 27 20 21 23 20
24 | 7 11 8 10 7 4 12 11 5 7 8 3 | 19 27 20 28 18 22 20 29 19 20 20 19
25 | 7 13 9 9 8 3 8 11 7 10 8 3 | 23 26 24 24 26 22 21 25 21 22 20 21
26 | 9 9 8 9 13 3 10 11 10 10 13 3 | 26 23 22 21 22 21 25 22 25 23 27 22
27 | 7 9 6 8 11 2 9 11 5 13 15 3 | 21 21 20 17 19 18 21 20 19 20 23 18
28 | 6 21 6 7 8 4 11 48 5 8 9 3 | 38 43 40 41 40 41 43 51 40 42 41 39
29 | 6 7 6 10 8 4 20 11 6 13 9 3 | 24 22 21 26 24 22 27 22 21 25 22 22
30 | 3 12 8 6 4 2 10 10 4 8 7 2 | 16 27 18 19 16 19 18 24 16 18 18 17
31 | 6 8 5 6 7 3 11 11 6 11 5 2 | 35 37 34 34 31 33 33 41 36 33 33 33
32 | 5 5 9 7 7 2 13 10 6 8 7 2 | 27 25 24 26 24 24 27 27 24 26 24 24
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 8 12 9 12 49 4 14 27 8 13 12 |T 27 28 27 28 27 26 28 31 27 27 28 26
WRMS | 7 11 9 10 9 4 14 27 6 10 9 |NE 24 27 25 26 24 24 26 30 25 25 25 24
MEDI | 6 9 7 9 8 3 12 11 6 11 9 |MD 24 26 24 26 24 23 26 27 24 23 24 22
Table 3.2316.5 GPS week: 2316 Day: 5 MJD: 60461.000
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 --- --- --- 10 10 --- --- 10 --- --- 6 | 32 --- --- --- 29 26 --- --- 28 --- --- 29
2 | 6 8 5 10 10 4 11 12 8 15 9 3 | 17 18 16 18 19 16 20 18 19 19 19 16
3E | 7 11 13 15 10 3 13 10 5 13 10 3 | 17 18 22 17 18 15 17 20 16 17 18 16
4 | 7 10 5 9 7 3 7 47 4 12 7 2 | 44 47 47 44 44 44 46 51 46 43 44 44
5E | 8 7 9 9 6 3 13 8 7 10 10 3 | 24 28 27 24 28 25 30 27 27 25 27 26
6 | 4 7 8 7 9 2 7 7 4 10 5 2 | 21 25 25 22 22 21 19 26 21 21 21 21
X7 | 6 8 5 10 6 4 --- 8 6 11 7 2 | 31 32 30 32 34 32 --- 37 31 30 28 33
8 | 7 12 8 16 12 5 10 11 11 13 8 3 | 404 411 406 402 394 406 413 402 410 407 408 407
9 | 5 7 7 9 5 2 7 7 6 8 6 2 | 23 29 26 23 24 24 22 29 25 26 24 24
10E | 6 9 11 13 8 4 10 11 8 14 11 3 | 20 19 21 20 22 17 20 19 19 22 20 18
11 | 7 11 8 6 7 4 9 63 5 9 9 2 | 19 25 24 25 25 22 24 25 25 20 26 23
12 | 4 9 8 8 13 4 15 11 7 8 10 3 | 45 44 42 48 44 45 42 48 49 44 50 45
13 | 5 9 7 8 4 3 11 8 8 7 8 2 | 24 30 25 26 25 24 23 29 27 23 25 24
14 | 8 9 17 12 11 3 7 59 8 11 11 4 | 38 42 47 45 40 41 40 52 39 38 37 40
15 | 6 8 5 8 7 3 15 8 8 7 8 3 | 30 35 30 34 30 31 34 33 30 33 33 31
X16 | 2 --- --- --- --- 14 --- --- --- --- --- 0 | 39 --- --- --- --- 41 --- --- --- --- --- 38
17 | 6 7 6 8 8 3 11 9 8 13 8 3 | 25 26 21 24 25 23 24 26 28 22 28 24
18 | 7 12 9 8 9 4 12 59 7 12 11 3 | 26 30 27 26 30 26 28 32 28 26 26 26
19 | 6 7 6 11 10 4 15 7 6 10 10 3 | 25 27 26 24 28 25 28 26 28 25 30 26
20E | 15 8 6 14 8 5 11 9 10 10 9 3 | 47 48 48 48 46 46 47 44 49 46 49 47
21 | 6 8 5 9 29 5 12 11 10 16 11 4 | 16 19 14 19 32 15 19 19 17 19 18 16
22 | 5 7 6 11 12 5 8 8 7 12 9 3 | 27 28 29 28 28 27 27 28 27 26 29 27
23E | 10 9 21 13 11 4 12 54 12 15 13 4 | 17 21 26 17 21 18 21 26 21 21 21 18
24 | 7 10 8 9 7 3 8 10 6 7 7 2 | 18 28 21 26 17 20 17 29 19 20 20 19
25 | 5 11 10 10 7 4 8 12 8 10 9 3 | 29 33 32 30 32 29 27 29 31 32 32 30
26 | 7 12 8 10 11 4 8 11 10 14 10 3 | 28 25 26 26 26 25 25 27 26 26 25 24
27 | 7 9 7 9 10 3 8 12 8 9 6 3 | 22 21 23 20 21 19 20 22 21 20 21 20
28 | 5 21 5 11 8 4 7 50 7 12 7 3 | 31 32 32 34 33 31 33 42 32 36 34 31
29 | 6 8 7 9 8 4 19 10 8 11 9 3 | 29 27 26 31 31 28 27 30 27 28 25 27
30 | 5 12 7 9 4 3 6 10 7 10 9 2 | 16 25 19 20 18 18 17 27 18 17 20 17
31 | 5 7 6 7 6 3 8 6 6 12 7 2 | 32 31 30 34 28 32 31 35 31 30 33 30
32 | 5 7 9 8 6 3 11 8 9 9 6 2 | 29 32 30 32 27 28 30 32 29 27 28 28
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 7 10 9 10 10 4 11 27 8 11 9 |T 38 41 40 40 40 38 40 43 40 39 40 38
WRMS | 6 9 8 10 8 4 11 27 7 10 7 |NE 42 45 43 44 43 41 43 46 43 42 43 42
MEDI | 6 9 7 9 8 4 10 10 8 11 9 |MD 26 28 26 26 28 25 27 29 27 26 26 26
Table 3.2316.6 GPS week: 2316 Day: 6 MJD: 60462.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS | cod emr esa gfz grg igr jgx jpl mit ngs sio IGS
------+-------------------------------------------------------------+--------------------------------------------------------------
X1 | 8 --- --- --- 11 9 --- --- 10 --- --- 6 | 26 --- --- --- 27 28 --- --- 25 --- --- 24
2 | 6 9 5 8 11 3 9 15 6 10 6 2 | 22 24 24 24 25 23 25 23 25 23 25 22
3E | 6 12 13 11 10 4 10 18 8 15 8 3 | 30 34 36 30 32 29 34 37 30 30 30 30
4 | 5 9 5 8 7 3 8 49 5 11 7 2 | 60 60 62 62 59 60 62 73 60 61 59 60
5E | 8 6 8 6 6 3 11 16 5 10 7 2 | 47 54 53 48 49 51 56 56 52 52 52 50
6 | 5 9 8 6 10 3 7 13 5 7 6 2 | 27 26 28 25 25 25 25 30 24 24 26 25
X7 | 4 6 5 6 8 5 --- 9 5 9 7 2 | 41 38 37 40 43 41 --- 45 37 40 29 42
8 | 7 9 8 6 12 3 6 14 5 13 7 2 | 490 490 491 490 497 491 493 490 489 488 491 490
9 | 3 8 7 6 6 2 6 13 6 9 7 2 | 27 31 29 29 27 27 29 32 28 30 28 28
10E | 5 10 10 16 7 4 8 17 5 15 8 3 | 38 37 39 41 42 39 40 40 36 41 38 38
11 | 6 11 7 7 9 2 10 64 5 10 5 2 | 34 36 37 35 37 34 37 47 35 33 37 35
12 | 6 7 8 10 14 5 15 19 7 10 10 3 | 58 58 57 60 61 59 59 62 61 62 62 59
13 | 5 10 7 8 6 3 9 11 6 6 9 2 | 23 30 22 25 27 25 28 31 28 26 30 25
14 | 7 8 17 7 11 4 7 64 6 10 8 3 | 40 45 51 46 42 43 39 62 39 40 39 42
15 | 6 7 6 8 7 3 15 12 7 10 11 3 | 54 53 52 57 50 53 59 56 52 53 53 53
16 | 6 8 6 17 18 5 18 15 10 11 9 4 | 12 10 11 15 13 12 12 14 11 12 12 11
17 | 5 7 5 7 10 5 5 14 8 11 10 2 | 28 27 25 29 28 26 28 29 32 26 34 28
18 | 7 11 8 8 10 3 12 55 7 10 8 3 | 41 42 39 40 42 40 42 48 40 39 39 39
19 | 5 10 6 8 11 4 11 15 6 8 8 2 | 27 28 28 28 31 28 31 29 32 26 32 28
20E | 5 8 5 11 7 5 7 16 7 12 9 2 | 58 63 61 61 63 61 63 65 61 64 60 60
21 | 6 9 6 10 12 4 10 15 8 10 8 3 | 20 25 21 24 26 21 22 23 22 24 22 21
22 | 5 7 6 7 10 4 7 13 6 10 7 2 | 39 39 39 40 40 40 39 40 40 37 40 39
23E | 9 8 21 10 11 4 11 52 10 13 11 4 | 40 44 50 44 44 44 50 52 44 45 45 43
24 | 7 11 6 13 11 5 8 13 8 9 6 3 | 26 33 28 36 26 28 27 36 27 28 27 27
25 | 4 13 9 9 7 4 10 17 8 6 8 3 | 25 26 26 24 27 25 24 28 24 24 23 24
26 | 5 11 8 9 11 4 7 15 8 13 10 3 | 25 23 22 24 26 24 22 28 25 23 25 22
27 | 5 11 6 7 8 2 6 16 8 13 5 2 | 23 24 25 23 25 23 24 25 26 23 25 23
28 | 5 22 4 10 6 4 8 49 5 13 9 3 | 40 39 40 43 45 40 41 57 40 45 42 40
29 | 6 8 7 11 9 4 20 14 9 12 8 3 | 27 25 24 31 30 28 31 26 28 29 26 27
30 | 4 12 7 6 5 3 6 13 5 9 4 2 | 23 30 25 26 22 23 25 32 22 23 22 23
31 | 5 9 6 6 6 3 9 12 5 12 7 2 | 45 45 44 46 41 44 47 52 45 39 43 43
32 | 4 8 8 6 6 4 7 16 6 11 5 2 | 34 37 31 36 33 33 35 39 33 35 34 33
------+-------------------------------------------------------------+--------------------------------------------------------------
RMS | 6 10 8 9 10 4 10 28 7 11 8 |T 48 50 50 51 50 49 51 55 49 49 50 48
WRMS | 6 10 8 9 9 4 10 28 6 10 7 |NE 51 53 52 54 52 51 54 58 51 52 52 51
MEDI | 5 9 7 8 9 4 8 15 6 10 8 |MD 30 36 36 36 32 29 34 39 32 33 34 30
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 4.2316 GPS week: 2316 MJD: 60456.0-60462.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3050 |U 10 11 30 |U 8 15 38 |U 10 12 34 |
emr | emr 2907 |U 13 17 30 |U 11 18 40 | 13 15 42 |
esa | esa 2948 | 12 14 29 |U 9 17 44 |U 13 13 41 |
gfz | gfz 2947 |U 9 11 33 |U 9 12 36 | 10 12 40 |
grg | grg 3051 |U 9 12 35 |U 9 12 39 | 11 14 40 |
igr | igr 2948 | 9 11 28 | 8 13 36 | 10 13 34 |
igs | igs 2955 | 9 10 29 | 8 12 37 | 9 12 35 |
jgx | jgx 2866 |U 9 11 35 | 10 13 36 | 10 13 34 |
jpl | jpl 2962 | 17 17 35 | 11 19 46 | 15 18 48 |
mit | mit 3044 |U 9 12 32 |U 10 12 40 |U 11 13 35 |
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 5.2316.0 GPS week: 2316 Day: 0 MJD: 60456.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3022 | 13 15 32 | 8 18 41 | 9 12 33 |
emr | emr 2879 | 14 19 32 | 12 22 43 | 20 20 52 |
esa | esa 2880 | 12 15 28 | 9 19 44 | 12 8 38 |
gfz | gfz 2880 | 12 14 38 | 11 17 39 | 8 9 42 |
grg | grg 3022 | 13 15 39 | 8 15 40 | 9 13 38 |
igr | igr 2880 | 11 13 30 | 10 17 36 | 8 9 34 |
igs | igs 2926 | 11 14 31 | 8 16 37 | 8 9 34 |
jgx | jgx 2880 | 12 15 37 | 10 18 38 | 8 9 33 |
jpl | jpl 2976 | 16 16 34 | 11 24 52 | 16 10 43 |
mit | mit 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
Table 5.2316.1 GPS week: 2316 Day: 1 MJD: 60457.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 7 8 32 | 9 12 43 | 8 10 30 |
emr | emr 2880 | 11 17 28 | 12 16 36 | 11 15 35 |
esa | esa 2976 | 10 13 25 | 9 14 50 | 11 9 35 |
gfz | gfz 2975 | 7 11 38 | 11 11 39 | 9 9 37 |
grg | grg 3072 | 7 10 36 | 10 11 39 | 10 10 36 |
igr | igr 2976 | 6 9 30 | 9 11 41 | 8 9 31 |
igs | igs 2976 | 6 9 31 | 8 10 41 | 8 9 32 |
jgx | jgx 2880 | 7 10 38 | 12 12 41 | 8 10 31 |
jpl | jpl 2976 | 14 14 33 | 10 17 45 | 16 16 41 |
mit | mit 3072 | 7 10 31 | 11 12 44 | 8 9 33 |
Table 5.2316.2 GPS week: 2316 Day: 2 MJD: 60458.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 8 9 27 | 9 16 41 | 9 13 42 |
emr | emr 2880 | 13 19 33 | 10 19 47 | 9 16 47 |
esa | esa 2976 | 11 15 30 | 9 15 46 | 11 18 57 |
gfz | gfz 2972 | 7 9 25 | 9 14 37 | 10 20 59 |
grg | grg 3072 | 7 8 30 | 10 13 41 | 12 20 57 |
igr | igr 2976 | 8 10 25 | 9 14 38 | 11 20 52 |
igs | igs 2976 | 7 9 25 | 9 13 38 | 11 20 52 |
jgx | jgx 2880 | 8 9 29 | 13 15 35 | 11 19 51 |
jpl | jpl 2976 | 14 19 38 | 11 19 50 | 13 26 71 |
mit | mit 3072 | 7 13 28 | 11 15 40 | 13 19 53 |
Table 5.2316.3 GPS week: 2316 Day: 3 MJD: 60459.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3070 | 11 11 35 | ---- ---- ---- | 15 24 38 |
emr | emr 2880 | 11 12 33 | ---- ---- ---- | 15 21 51 |
esa | esa 2976 | 13 14 34 | ---- ---- ---- | 16 22 49 |
gfz | gfz 2971 | 10 12 38 | ---- ---- ---- | 17 25 46 |
grg | grg 3072 | 10 13 39 | ---- ---- ---- | 19 27 47 |
igr | igr 2976 | 9 11 33 | ---- ---- ---- | 16 24 41 |
igs | igs 2976 | 9 11 33 | ---- ---- ---- | 15 24 41 |
jgx | jgx 2880 | 10 12 39 | ---- ---- ---- | 16 24 41 |
jpl | jpl 2976 | 15 15 37 | ---- ---- ---- | 19 23 54 |
mit | mit 3072 | 10 13 35 | ---- ---- ---- | 18 26 40 |
Table 5.2316.4 GPS week: 2316 Day: 4 MJD: 60460.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3071 | 7 8 36 | ---- ---- ---- | 9 11 32 |
emr | emr 2976 | 10 17 31 | ---- ---- ---- | 13 14 45 |
esa | esa 2976 | 10 13 31 | ---- ---- ---- | 12 8 38 |
gfz | gfz 2976 | 6 10 32 | ---- ---- ---- | 7 7 34 |
grg | grg 3072 | 8 12 38 | ---- ---- ---- | 9 8 31 |
igr | igr 2976 | 7 12 31 | ---- ---- ---- | 8 8 27 |
igs | igs 2976 | 6 9 33 | ---- ---- ---- | 7 8 30 |
jgx | jgx 2880 | 9 14 40 | ---- ---- ---- | 10 13 29 |
jpl | jpl 2976 | 17 18 35 | ---- ---- ---- | 14 20 47 |
mit | mit 3072 | 6 10 42 | ---- ---- ---- | 9 8 33 |
Table 5.2316.5 GPS week: 2316 Day: 5 MJD: 60461.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 16 16 28 | 8 15 30 | 16 9 38 |
emr | emr 2880 | 17 17 25 | 11 17 33 | 11 11 33 |
esa | esa 2880 | 19 17 26 | 9 19 35 | 13 12 34 |
gfz | gfz 2880 | 12 11 32 | 8 9 31 | 8 7 33 |
grg | grg 2975 | 12 13 34 | 10 10 30 | 9 7 36 |
igr | igr 2880 | 13 12 28 | 7 11 28 | 8 9 28 |
igs | igs 2880 | 13 11 27 | 8 11 30 | 7 8 28 |
jgx | jgx 2784 | 11 11 35 | 8 9 31 | 8 9 27 |
jpl | jpl 2880 | 24 20 33 | 12 20 35 | 15 14 41 |
mit | mit 2976 | 13 15 34 | 8 12 37 | 9 5 30 |
Table 5.2316.6 GPS week: 2316 Day: 6 MJD: 60462.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 8 24 | 8 12 37 | 8 10 26 |
emr | emr 2976 | 12 16 28 | 11 17 42 | 14 11 30 |
esa | esa 2976 | 12 13 26 | 9 17 44 | 13 10 34 |
gfz | gfz 2976 | 8 10 28 | 9 11 35 | 10 9 31 |
grg | grg 3072 | 9 11 27 | 9 13 43 | 11 11 36 |
igr | igr 2976 | 9 9 22 | 7 10 39 | 10 10 27 |
igs | igs 2976 | 9 9 23 | 8 11 37 | 9 9 26 |
jgx | jgx 2880 | 8 8 29 | 9 11 34 | 9 9 26 |
jpl | jpl 2976 | 19 21 34 | 10 15 48 | 14 17 40 |
mit | mit 3072 | 8 12 24 | 9 10 38 | 10 8 24 |
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 6.2316 GPS week: 2316 MJD: 60456.500-60462.500
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 -12 16 -9 2 | -6 22
| 13 13 53 49 7 | 4
emr uuuuu | -7 15 54 66 -3 | -4 25
| 24 8 73 44 10 | 3
esa uuuuu | 8 -7 55 -22 1 | 2 21
| 9 9 39 30 1 | 3
gfz uuuuu | -6 -40 80 -75 2 | 6 23
| 14 21 114 114 5 | 3
grg uuuuu | -7 9 -4 -19 -3 | 10 24
| 9 11 20 61 4 | 3
igr xxxxx | -19 0 9 -23 5 | -6 20
| 7 14 69 43 4 | 2
irf xxxxx | 0 13 0 22 1 | -1 22
| 7 7 29 9 3 | 2
jgx uuuuu | -8 -26 35 22 0 | 7 23
| 9 9 32 39 4 | 3
mit uuuuu | 26 25 -24 62 3 | 7 22
| 16 20 64 30 5 | 2
ngs uuuuu | -7 45 -267 -21 0 | 7 23
| 44 28 171 159 7 | 4
sio xxxxx | 0 51 -79 -19 -6 | 11 27
| 33 25 63 42 8 | 3
Table 7.2316.0 GPS week: 2316 Day: 0 MJD: 60456.500
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 -17 -53 63 -3 | -2 22
emr uuuuu | 30 0 83 61 -2 | -3 29
esa uuuuu | 16 3 80 28 0 | 5 23
gfz uuuuu | -10 -51 48 -134 5 | 8 24
grg uuuuu | -9 2 3 -95 -3 | 13 25
igr xxxxx | -7 -30 93 -20 3 | -5 20
irf xxxxx | 11 19 14 14 1 | -1 23
jgx uuuuu | -13 -35 38 -7 -4 | 10 23
mit uuuuu | 47 57 -55 88 6 | 7 24
ngs uuuuu | -71 40 -125 -11 1 | 10 25
sio xxxxx | 33 92 -120 -32 -2 | 12 30
Table 7.2316.1 GPS week: 2316 Day: 1 MJD: 60457.500
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 -11 27 -41 -4 | 1 22
emr uuuuu | 18 15 -32 28 13 | 0 29
esa uuuuu | -9 -7 37 -17 0 | 8 24
gfz uuuuu | 1 -18 -57 -1 -6 | 12 25
grg uuuuu | -23 1 -23 -37 -1 | 16 27
igr xxxxx | -16 -3 80 45 5 | -2 20
irf xxxxx | -3 12 47 26 0 | 3 23
jgx uuuuu | -17 -32 94 42 -3 | 14 24
mit uuuuu | 44 44 50 85 9 | 11 26
ngs uuuuu | -40 12 -133 -36 -2 | 14 26
sio xxxxx | -49 40 -128 61 1 | 14 30
Table 7.2316.2 GPS week: 2316 Day: 2 MJD: 60458.500
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 | -18 0 -47 0 -7 | -6 25
emr uuuuu | -8 22 56 42 6 | -4 30
esa uuuuu | 15 -3 -11 -19 0 | 2 25
gfz uuuuu | 2 -44 69 -14 -3 | 5 27
grg uuuuu | -9 -4 9 28 3 | 11 27
igr xxxxx | -15 -4 61 -39 12 | -7 24
irf xxxxx | -8 5 19 10 2 | -2 26
jgx uuuuu | -6 -12 20 42 -5 | 8 25
mit uuuuu | 23 23 55 16 6 | 6 26
ngs uuuuu | -5 8 -136 -88 0 | 7 26
sio xxxxx | 25 21 -129 -72 -1 | 10 30
Table 7.2316.3 GPS week: 2316 Day: 3 MJD: 60459.500
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 -29 18 -92 1 | -11 25
emr uuuuu | -12 11 113 78 -2 | -8 28
esa uuuuu | 2 -9 28 -22 1 | -2 23
gfz uuuuu | 9 -4 -68 125 5 | 1 25
grg uuuuu | 0 20 -18 89 -9 | 7 24
igr xxxxx | -22 5 -30 17 4 | -10 23
irf xxxxx | -3 10 4 17 8 | -5 25
jgx uuuuu | -13 -27 19 -5 0 | 4 23
mit uuuuu | 3 6 16 76 6 | 3 24
ngs uuuuu | 46 54 -130 -231 -2 | 3 23
sio xxxxx | -17 54 -1 -36 -2 | 9 28
Table 7.2316.4 GPS week: 2316 Day: 4 MJD: 60460.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 12 4 97 -1 10 | -8 22
emr uuuuu | -38 20 -13 148 -5 | -3 20
esa uuuuu | 8 -25 72 -32 2 | 2 19
gfz uuuuu | -33 -52 189 -156 5 | 5 21
grg uuuuu | -12 10 -31 -61 -5 | 9 22
igr xxxxx | -24 6 -24 -62 8 | -6 19
irf xxxxx | 3 7 -19 33 0 | 0 20
jgx uuuuu | -12 -33 57 92 1 | 6 21
mit uuuuu | 22 6 -47 89 4 | 7 20
ngs uuuuu | 28 77 -465 -150 -12 | 6 21
sio xxxxx | -34 66 -59 -34 -6 | 13 25
Table 7.2316.5 GPS week: 2316 Day: 5 MJD: 60461.500
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 -28 16 -14 8 | -7 21
emr uuuuu | -20 13 170 83 -10 | -3 20
esa uuuuu | 15 0 106 -19 1 | 2 19
gfz uuuuu | -2 -52 186 -190 2 | 6 21
grg uuuuu | 6 27 16 -41 -4 | 9 23
igr xxxxx | -29 15 -26 -26 7 | -5 18
irf xxxxx | 5 26 -29 29 -2 | 0 20
jgx uuuuu | 10 -28 -1 -20 2 | 6 21
mit uuuuu | 11 32 -94 51 -2 | 8 20
ngs uuuuu | -40 44 -479 163 5 | 4 22
sio xxxxx | 6 61 14 4 -21 | 12 26
Table 7.2316.6 GPS week: 2316 Day: 6 MJD: 60462.500
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 | -22 -3 53 22 9 | -8 21
emr uuuuu | -23 24 1 18 -19 | -6 16
esa uuuuu | 8 -11 76 -74 3 | 0 17
gfz uuuuu | -7 -61 193 -154 4 | 5 20
grg uuuuu | -5 5 19 -17 -3 | 6 18
igr xxxxx | -18 7 -92 -80 0 | -6 17
irf xxxxx | -7 11 -34 23 -3 | -2 18
jgx uuuuu | -3 -18 22 9 8 | 4 18
mit uuuuu | 28 9 -91 29 -4 | 7 18
ngs uuuuu | 31 76 -400 207 10 | 2 19
sio xxxxx | 33 25 -128 -28 -13 | 7 19
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