[IGSREPORT-31081] Wk 2430 IGS Final Orbits
acc
acc at igs.org
Fri Aug 21 06:28:49 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2430 (Aug 02, 2026 - Aug 08, 2026)
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_20262140000_07D_01D_SUM.SUM Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, ESA, GFZ, GRG and JPL.
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 | 20 HOB2 BSHM CUSV CZTG HOB2
0 | EMR | FAIR POLV TID1 YEL2 BADG FAIR POLV TID1 YEL2
0 | ESA | 20 CHTI HOB2 MAW1 CHTI FTNA HOB2 MAW1 POLV PTBB TUVA
0 | GFZ | 20 21 9 20 21 ACRG AREQ ARHT ASCG BADG BAKE BRAZ
0 | GFZ | BRFT BSHM CCJ2 CHAN CHPI CHTI CHUR CKIS CMUM COCO
0 | GFZ | CPVG CRO1 DAEJ DAV1 DGAR DJIG DRAO DUMG FAIR FALK
0 | GFZ | FTNA GAMB GMSD GODE GUAM HERS HOB2 HOFN HRAO IISC
0 | GFZ | IRKJ ISPA KAT1 KERG KIRI KIT3 KOKB KOKV LAUT LPGS
0 | GFZ | MAC1 MAJU MATE MAW1 MCIL MIZU MKEA MONP NIUM NKLG
0 | GFZ | NLIB NRC1 NYA2 OUS2 PDEL PIE1 POHN POL2 POTS POVE
0 | GFZ | PTVL QAQ1 REUN RIO2 ROTH SANT SCOR SEYG SGOC SGPO
0 | GFZ | STHL STJO STR1 SUTH SYOG TASH THU2 TONG TOW2 TUVA
0 | GFZ | TWTF UNSA VOIM WHIT WSRT WTZR WUH2 YELL ZAMB ZECK
0 | GFZ | CHTI HOB2 ONSA POHN
0 | GRG | CZTG
0 | JGX | POHN THU2 YEL2 BAKE BSHM MAC1 SAMO SCOR THU2 YEL2
0 | JPL | 1 18 FAIR MAW1 POHN TUVA CZTG FAIR
0 | MIT | GMSD JOZE MEDI NOT1 NRC1 NYAL SFER SVTL TLSE VACS
0 | MIT | WGTN GMSD JOZE MEDI NOT1 NRC1 NYAL SFER SVTL TLSE
0 | MIT | VACS WGTN
1 | COD | ULAB ULAB
1 | EMR | BSHM CHUR FAIR NAUR TID1 WHIT YEL2 BSHM CHUR FAIR
1 | EMR | TID1 WHIT YEL2
1 | ESA | BADG FALK GAMB FALK GAMB MGUE PTBB
1 | GFZ | 16 16 BADG CHUR GAMB KIT3 ONSA POHN GAMB KIT3 ONSA
1 | GFZ | POHN
1 | JGX | BADG BAKE IQAL NAUR POHN QAQ1 STJ3 SYOG THU2 TRO1
1 | JGX | ULAB YEL2 BAKE IQAL MAC1 NAUR POHN QAQ1 STJ3 SYOG
1 | JGX | THU2 TRO1 ULAB YEL2
1 | JPL | CZTG GAMB MONP POHN CZTG FTNA GAMB MONP
1 | MIT | BRST DUND GMSD HARB LAMA MCM4 MEDI MQZG NOT1 NYAL
1 | MIT | SVTL VACS WGTN ZIM2 BRST DUND GMSD HARB LAMA MCM4
1 | MIT | MEDI MQZG NOT1 NYAL SVTL VACS WGTN ZIM2
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
----+--------+--------+-------------
0 | COD | ~17:40 | ~ 0.15 ns
0 | ESA | ~07:20 | ~ -0.25 ns
0 | GFZ | ~12:00 | ~ 0.11 ns
1 | COD | ~05:00 | ~ -0.14 ns
1 | ESA | ~18:45 | ~ 0.24 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
----+--------+---------------
3 | COD | 30
3 | EMR | 30
3 | GRG | 30
3 | JPL | 30
3 | SIO | 18
4 | MIT | 18
4 | SIO | 18
6 | ESA | 20
6 | MIT | 11
6 | SIO | 11
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G30 | 4 | 4 | 4 | 4 | 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 27-Nov-2022 (GPS Week 2238, day 0, MJD 59910), 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 lomg filename formats.
For more information see IGSMAIL #8238, #8256, #8274 and #8282.
Starting 02-Feb-2025 (GPS Week 2352, day 0, MJD 60708), all IGS products
are based on the IGS realization of the first yearly update of ITRF2020
called ITRF2020-u2023. This IGS realization is called IGb20.
For more information see IGSMAIL #8543.
Starting 11-Jan-2026 (GPS Week 2401, day 0, MJD 61051), all IGS products
are based on the IGS realization of the second yearly update of ITRF2020
called ITRF2020-u2024. This IGS realization is called IGc20.
For more information see IGSMAIL #8634.
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 | 1.2 -.1 .8 -1 4 14 .00
EMR | 0 | 5.8 -4.3 -15.5 -6 17 -2 -.07
ESA | 0 | .5 .2 -.4 5 15 -1 -.79
GFZ | 0 | .9 .1 .1 -26 22 -6 .15
GRG | 0 | -.1 .2 -1.2 14 -2 6 -.01
JGX | 0 | -.5 .8 -1.1 11 13 9 -.22
JPL | 0 | 1.9 -3.8 -11.3 -11 0 -8 .20
MIT | 0 | 2.3 -2.5 13.9 -10 -6 -28 .02
NGS | 0 | 4.9 -3.6 4.0 17 19 -4 -.15
SIO | 0 | 2.4 -.1 -6.7 29 -13 41 -.01
COD | 1 | 1.3 .0 .9 -3 9 6 -.03
EMR | 1 | 7.2 -3.6 -9.8 -3 9 0 .02
ESA | 1 | -.3 -1.2 -.8 -26 38 -22 -.87
GFZ | 1 | .3 .2 .5 -12 -9 -12 .16
GRG | 1 | .1 .1 -1.3 11 -8 -1 .06
JGX | 1 | -.4 1.0 -.9 7 -1 12 -.18
JPL | 1 | -.3 -2.0 -12.9 -1 -7 -5 .04
MIT | 1 | 2.3 -1.3 11.6 -4 -10 -24 .09
NGS | 1 | 4.7 -.8 9.8 13 26 -15 .01
SIO | 1 | 1.6 -2.5 -4.8 53 -77 71 .14
COD | 2 | 1.3 .2 .9 -1 2 9 -.01
EMR | 2 | 6.2 -4.3 -12.1 -4 10 1 -.13
ESA | 2 | -.3 .3 -.2 15 6 10 -.90
GFZ | 2 | .1 .7 .3 -5 -2 2 .11
GRG | 2 | -.5 -.4 -.9 8 6 4 .07
JGX | 2 | -.4 1.0 -.8 24 2 21 -.24
JPL | 2 | -1.3 -5.4 -12.5 7 -1 2 .03
MIT | 2 | 1.4 -2.3 10.6 -2 0 -8 .05
NGS | 2 | 9.9 -6.0 16.2 29 56 -20 .12
SIO | 2 | 1.2 .0 -4.1 -51 -101 65 .18
COD | 3 | 1.2 -.1 .8 -5 0 8 .00
EMR | 3 | 4.8 -3.3 -12.7 -3 16 -7 -.16
ESA | 3 | .4 -.2 -.7 21 10 2 -.94
GFZ | 3 | .7 .9 .6 -16 20 -6 .19
GRG | 3 | -.6 .3 -1.0 3 0 -8 .02
JGX | 3 | -.2 .5 -.4 8 15 9 -.23
JPL | 3 | -1.4 -3.3 -10.8 5 12 -3 .08
MIT | 3 | .3 1.1 10.6 -5 -11 -10 .04
NGS | 3 | 8.4 -1.4 14.5 10 61 -16 -.17
SIO | 3 | -3.4 4.1 .6 -32 -14 32 .19
COD | 4 | 1.2 -.3 1.1 -7 1 10 .04
EMR | 4 | 5.4 -2.5 -7.9 -5 12 -6 -.21
ESA | 4 | .5 .3 -.8 23 24 10 -.86
GFZ | 4 | -.2 .4 .0 -9 -3 -12 .06
GRG | 4 | .1 -.1 -1.1 4 5 2 .00
JGX | 4 | -.2 1.1 -.9 3 19 8 -.29
JPL | 4 | .3 .3 -7.6 6 3 -15 .05
MIT | 4 | 1.7 -1.4 10.7 5 -14 -12 -.01
NGS | 4 | 8.1 -.4 6.3 8 34 -2 -.06
SIO | 4 | .6 -1.2 -1.8 -34 -23 58 .14
COD | 5 | .8 .0 .9 -10 -2 4 -.03
EMR | 5 | 7.3 4.4 -6.9 -3 12 -5 -.19
ESA | 5 | .7 -.5 -.6 22 9 3 -.99
GFZ | 5 | .6 -.6 .3 3 -11 -3 -.03
GRG | 5 | .3 .1 -.8 0 7 -10 .0
JGX | 5 | -.4 1.1 -1.1 18 5 21 -.39
JPL | 5 | 2.1 -2.0 -4.3 6 -19 -1 .15
MIT | 5 | 1.5 -.4 9.2 0 -3 -4 .01
NGS | 5 | 4.7 2.2 -.9 -6 16 19 -.08
SIO | 5 | 1.1 -.0 -4.7 -67 -33 37 .27
COD | 6 | 1.0 .1 1.0 -5 -3 10 -.04
EMR | 6 | 11.8 3.9 -9.6 -10 16 -9 -.22
ESA | 6 | .1 -.1 -.8 17 9 2 -.94
GFZ | 6 | .1 .1 .2 -2 3 -9 -.08
GRG | 6 | -.3 .3 -1.4 2 12 -7 .02
JGX | 6 | -.5 1.1 -1.6 7 0 29 -.39
JPL | 6 | 1.2 1.4 -7.5 5 -2 -1 -.03
MIT | 6 | -1.8 1.1 4.6 2 -1 -12 -.18
NGS | 6 | 4.1 1.8 3.3 16 29 -6 -.44
SIO | 6 | -4.3 2.4 -10.3 -19 68 23 -.17
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
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 1.2430.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2430.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 2.2430.[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 3.2430.[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 5.2430.0-6). 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 2430 summary. (Aug 02, 2026 - Aug 08, 2026)
Table 1.2430.a GPS week: 2430 MJD: 61254.000-61260.000
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 935| 0 0 2 5 1 8 -.00 7 6 | 3695 -2810 1 101
| 0 0 0 9 11 11 .01 | 4074 2998
emr 107| 0 2 -4 -6 13 12 -.01 9 9 | 2538 -2952 1 129
| 1 3 2 3 9 7 .03 | 28023 27204
esa 187| 0 0 -2 0 9 -4 -.04 10 10 | -14311 -24083 1 199
| 0 0 0 7 4 9 .01 | 12020 19304
gfz 148| 0 0 -2 10 10 4 .03 10 10 | -33763 -46882 3 348
| 0 0 1 14 15 6 .02 | 23838 33974
grg 126| 1 0 5 -18 7 -1 .07 9 9 | 353 -15196 2 135
| 0 0 1 13 10 5 .01 | 19369 27879
jgx n/a| 0 0 -2 14 -17 -1 -.02 5 5 | 4506 3908 2 64
| 0 0 0 4 7 12 .02 | 4675 3469
jpl 120| 0 0 -1 -8 -1 14 -.00 10 10 | -1960 5150 2 76
| 0 2 1 10 5 11 .01 | 3255 5976
mit 360| 0 0 0 -3 0 -69 .04 11 7 | 11358 -15120 9 313
| 0 0 0 24 18 43 .01 | 10375 17831
ngs 259| 0 0 5 9 2 3 -.06 11 10 | 33685 -42697 172 873
| 0 1 4 15 19 13 .03 | 73959 141540
sio 357| 0 0 2 -14 7 45 .03 12 8 | 0 0 0 0
| 0 0 1 11 13 19 .01 | 0 0
Table 1.2430.b GPS week : 2430 MJD: 61254.000-61260.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 4 3 4 4 4 5 5 |
2 | 4 4 3 3 3 3 3 |
3 | 2 2 2 2 2 2 2 |
4 | 3 3 3 3 3 3 3 |
5 | 3 3 2 3 3 0 3 |
6 | 3 4 4 4 4 4 5 |
7 | 3 3 3 3 3 3 3 |
8 | 2 3 2 2 2 2 2 |
9 | 3 3 3 3 3 3 3 |
10 | 2 2 2 2 2 2 2 |
11 | 3 4 4 5 5 6 6 |
12 | 2 2 2 2 2 2 2 |
13 | 3 3 3 3 3 3 6 |
14 | 3 3 3 3 3 3 3 |
15 | 3 3 3 3 3 3 3 |
16 | 2 2 2 2 2 2 2 |
17 | 2 2 3 2 2 3 3 |
18 | 5 5 7 8 6 8 5 |
19 | 2 2 2 2 2 2 3 |
20 | 5 5 5 5 5 5 4 |
21 | 3 3 3 3 3 3 3 |
22 | 2 2 2 2 2 2 2 |
23 | 3 3 2 3 2 2 3 |
24 | 3 3 3 3 3 2 3 |
25 | 3 3 3 3 3 3 3 |
26 | 2 2 2 2 2 2 2 |
27 | 2 2 2 3 2 2 2 |
28 | 3 3 3 3 3 3 3 |
29 | 2 2 2 2 2 2 3 |
30 | 3 3 3 17 3 3 3 |
31 | 2 2 2 2 3 3 2 |
32 | 3 3 3 3 2 2 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 2.2430.0 GPS week: 2430 Day: 0 MJD: 61254.000
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 941| 0 0 2 6 -10 4 -.01 7 7 | -633 -134 5 136
emr 111| 0 1 -7 -6 3 0 .01 9 9 | 195 -216 7 108
esa 188| 0 0 -2 0 8 -12 -.03 9 9 | -1022 -50 6 209
gfz 148| 0 0 0 -14 21 -2 .04 10 10 | -161 186 11 123
grg 128| 1 -1 6 -15 7 2 .09 10 10 | 22 118 9 148
jgx n/a| 0 0 0 19 -8 -16 -.04 5 5 | 12 148 8 68
jpl 120| -1 0 -2 -19 1 3 .01 10 10 | -3509 -314 9 77
mit 360| 0 0 0 24 -6 -18 .05 8 6 | -1696 5674 35 1137
ngs 266| 0 -1 3 -8 4 10 -.07 10 9 | -635 -134 594 935
sio 359| 0 0 1 -27 -4 36 .05 9 9 | --- --- --- ---
Table 2.2430.1 GPS week: 2430 Day: 1 MJD: 61255.000
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 938| 0 0 1 0 18 -1 .01 6 6 | -776 -18 6 137
emr 107| 0 0 -6 -5 3 7 .02 9 9 | 31668 -63466 6 96
esa 188| 0 0 -2 15 15 -13 -.03 9 9 | -1256 126 6 207
gfz 149| 0 0 -3 31 6 5 -.00 11 11 | -25 -305 11 94
grg 125| 1 0 8 4 2 -2 .07 10 9 | 0 -54 9 129
jgx n/a| 0 0 -1 17 -21 -10 -.03 5 5 | -59 -79 8 72
jpl 120| 0 0 -2 5 3 9 -.02 10 10 | -4196 14 9 82
mit 360| 0 0 0 -42 8 -47 .05 8 6 | -2272 6230 34 644
ngs 261| 0 -1 8 -4 -17 8 -.03 9 9 | -779 -3 614 1020
sio 359| 0 0 0 -11 13 69 .03 10 9 | --- --- --- ---
Table 2.2430.2 GPS week: 2430 Day: 2 MJD: 61256.000
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 933| 0 0 2 13 10 10 -.01 7 7 | 9125 -618 0 87
emr 107| 0 -1 -5 -13 8 9 -.00 8 8 | -56790 7142 0 246
esa 187| 0 0 -2 -5 2 -9 -.05 9 9 | -26800 -19650 0 196
gfz 149| 0 0 -3 15 1 -1 .01 10 11 | -54580 -46180 0 460
grg 124| 1 0 6 -15 -7 2 .06 10 8 | -9703 -6604 0 118
jgx n/a| 0 0 -2 10 -21 -7 -.01 5 5 | 9298 4293 0 65
jpl 120| 0 0 -2 -11 -5 8 .01 10 10 | -2071 8380 0 69
mit 360| 0 0 0 -4 20 -54 .03 9 6 | 6516 -9468 0 73
ngs 254| 0 0 10 24 7 -11 -.06 11 10 | 10310 -50020 0 1033
sio 356| 0 0 1 -24 18 70 .04 11 9 | 0 0 0 0
Table 2.2430.3 GPS week: 2430 Day: 3 MJD: 61257.000
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 933| 0 0 2 -8 -4 30 .00 7 6 | 4424 -4790 0 94
emr 108| 0 0 -4 -2 16 20 -.00 9 9 | 8393 4708 0 115
esa 187| -1 1 -1 -1 10 0 -.05 10 10 | -10810 -51640 0 195
gfz 149| 1 0 -3 19 35 -3 .04 10 10 | -35760 -83300 0 450
grg 127| 0 0 4 -17 2 3 .06 9 7 | -10030 -20700 0 140
jgx n/a| 0 0 -3 14 -7 5 -.03 4 4 | 2677 9331 0 63
jpl 120| 0 0 -3 -12 -3 21 .02 11 11 | -5300 12450 0 78
mit 360| 0 0 1 -20 -29 -84 .04 11 7 | 21320 -38710 0 71
ngs 256| 0 1 8 18 38 -14 -.07 13 11 | -341 -8743 0 778
sio 356| 0 0 6 4 12 24 .01 14 8 | 0 0 0 0
Table 2.2430.4 GPS week: 2430 Day: 4 MJD: 61258.000
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 933| 0 0 1 12 -12 6 -.01 6 6 | 3123 -4424 0 77
emr 106| 0 1 -4 -2 15 12 .03 9 9 | 5071 11670 0 116
esa 187| 0 0 -3 4 14 2 -.04 9 10 | -9354 -34550 0 205
gfz 148| 0 0 0 11 18 14 .03 10 10 | -44080 -60590 0 429
grg 125| 1 0 4 -21 18 1 .05 9 9 | 1647 -1491 0 157
jgx n/a| 0 0 -2 6 -11 -4 -.01 4 4 | 9250 4755 0 61
jpl 120| -1 -1 -2 8 -2 7 .01 10 10 | -1042 -879 0 79
mit 360| -1 0 1 -16 -10 -70 .02 13 7 | 18060 -12260 0 92
ngs 255| 0 0 4 6 -13 -3 -.09 10 9 | 16610 117600 0 673
sio 354| 0 0 2 -9 24 55 .04 15 9 | 0 0 0 0
Table 2.2430.5 GPS week: 2430 Day: 5 MJD: 61259.000
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 934| 0 0 2 15 8 -3 .01 7 6 | 1741 -1734 0 85
emr 106| 1 6 0 -10 18 10 -.05 10 10 | 16299 3667 0 115
esa 187| 0 0 -1 -3 3 -10 -.02 9 10 | -19220 -37590 0 201
gfz 148| 0 -1 -2 1 -9 5 .05 9 9 | -53450 -64089 0 437
grg 127| 1 0 4 -39 7 -12 .08 9 9 | 40630 -76180 0 137
jgx n/a| 0 0 -1 16 -23 2 .00 5 5 | 688 6832 0 58
jpl 120| -1 -1 0 -15 -11 13 -.01 10 10 | 4680 3762 0 73
mit 360| -1 0 1 10 21 -54 .03 13 7 | 16379 -23340 0 88
ngs 259| 0 0 -2 32 9 18 -.08 12 11 | 200700 -341000 0 772
sio 358| 0 -1 1 -22 -4 24 .02 13 7 | 0 0 0 0
Table 2.2430.6 GPS week: 2430 Day: 6 MJD: 61260.000
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 936| 0 -1 2 -1 3 11 -.00 6 6 | 8866 -7957 0 89
emr 106| 2 6 0 -7 28 23 -.05 10 10 | 12930 15830 0 108
esa 187| 0 -1 -1 -7 9 12 -.06 15 10 | -31720 -25230 0 182
gfz 149| 0 -1 -4 7 1 11 .03 10 9 | -48290 -73900 0 443
grg 129| 1 -1 2 -24 23 -3 .07 9 9 | -20090 -1461 0 120
jgx n/a| 0 0 -2 15 -26 23 .00 5 5 | 9676 2078 0 60
jpl 120| 0 4 0 -12 4 37 -.01 11 11 | -2287 12640 0 77
mit 360| -1 -1 1 23 2 -156 .03 13 7 | 21200 -33970 0 84
ngs 263| 0 0 5 -4 -12 18 -.03 12 11 | 9931 -16580 0 904
sio 360| 0 0 1 -9 -10 38 .03 14 7 | 0 0 0 0
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 3.2430.0 GPS week: 2430 Day: 0 MJD: 61254.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 6 9 10 --- 9 4 20 6 16 14 3 | 29 29 29 --- 30 30 30 29 33 32 29
2E | 5 8 6 9 14 7 8 13 19 15 3 | 36 37 35 37 43 38 35 34 47 33 36
3 | 5 9 7 5 10 4 5 7 9 9 2 | 35 36 37 35 35 34 35 36 35 36 35
4 | 8 8 10 7 14 4 13 7 12 8 3 | 54 58 61 60 54 58 61 59 54 59 57
5 | 7 9 8 9 8 4 9 7 8 8 2 | 21 20 19 22 16 15 19 20 22 22 20
6E | 6 12 7 9 15 6 10 7 8 9 3 | 56 56 56 56 60 56 55 63 55 60 57
7 | 9 6 10 13 15 6 7 7 12 8 3 | 38 35 31 34 30 33 33 37 33 34 33
8 | 5 6 7 7 8 4 6 8 8 11 2 | 21 23 24 22 20 18 22 22 21 27 21
9 | 7 10 7 19 17 4 8 6 8 6 3 | 33 35 37 34 34 34 34 36 34 35 33
10 | 5 8 6 9 6 3 8 6 7 6 2 | 34 33 36 34 36 34 35 34 34 34 34
11E | 7 8 8 10 13 7 17 8 15 9 3 | 29 29 28 30 30 28 29 32 34 34 28
12 | 4 6 6 6 6 4 7 4 7 8 2 | 44 44 47 47 40 44 47 44 44 43 44
X13 | 5 7 10 14 5 --- 7 7 10 9 3 | 84 83 81 81 82 --- 83 83 83 82 82
14 | 4 16 5 9 7 4 15 6 6 7 2 | 54 56 52 53 55 53 55 53 54 52 53
15 | 9 8 11 8 9 6 8 8 8 10 2 | 25 24 22 23 24 23 23 24 23 22 22
16 | 4 7 8 8 4 4 8 5 5 11 2 | 22 20 25 27 21 21 21 24 21 28 22
17 | 4 7 8 7 8 4 6 7 9 7 2 | 43 44 43 44 43 42 43 44 45 44 43
18E | 11 9 12 16 13 4 21 15 15 18 4 | 54 53 53 50 54 53 53 58 55 59 53
19 | 6 6 6 6 8 4 5 8 9 6 2 | 34 36 35 33 35 34 36 33 35 34 34
20 | 18 15 29 18 14 5 21 6 14 12 5 | 56 59 61 54 56 57 61 58 56 56 56
21 | 6 9 8 5 10 5 11 11 9 7 2 | 37 38 38 38 37 36 38 36 39 39 37
22 | 3 5 7 6 7 4 4 4 7 6 1 | 23 24 23 24 23 21 24 24 24 23 23
23 | 7 7 8 7 9 4 9 7 12 7 2 | 26 30 28 30 31 30 29 31 30 31 29
24 | 8 8 6 11 8 4 7 7 8 7 2 | 34 34 32 32 39 33 32 33 34 34 33
25 | 4 13 8 10 6 5 14 5 8 9 2 | 22 31 30 26 22 23 33 26 25 23 25
26 | 5 7 7 6 4 4 9 6 6 6 2 | 36 40 41 39 36 36 43 39 33 37 37
27 | 6 8 7 7 7 3 6 8 7 13 2 | 19 20 21 20 19 17 19 17 19 22 18
28 | 6 8 7 10 9 5 12 6 10 8 2 | 55 53 52 54 58 55 55 59 56 56 55
29 | 7 6 8 8 7 5 7 5 7 10 2 | 39 38 37 35 35 35 36 37 36 38 36
30 | 6 7 6 14 18 4 7 7 8 9 3 | 624 624 626 623 637 456 624 621 627 624 624
31 | 4 7 10 6 8 5 9 6 4 9 2 | 27 27 25 30 29 25 28 29 26 27 26
32 | 8 11 5 9 7 5 8 8 7 11 2 | 29 34 33 31 29 30 31 28 30 26 29
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 9 10 10 5 10 8 10 9 |T 55 56 56 56 56 48 56 56 56 56 55
WRMS | 7 9 9 10 10 5 10 6 9 9 |NE 58 59 59 58 58 49 59 58 58 58 57
MEDI | 6 8 7 9 8 4 8 7 8 9 |MD 34 35 35 34 35 34 35 34 34 34 34
Table 3.2430.1 GPS week: 2430 Day: 1 MJD: 61255.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1E | 6 7 9 --- 11 4 17 10 13 10 3 | 18 18 18 --- 19 18 21 20 19 22 18
2E | 7 8 8 11 12 8 7 16 11 18 3 | 25 25 22 20 27 24 24 27 24 26 23
3 | 5 8 5 7 8 5 7 5 9 8 2 | 21 22 24 20 20 19 23 22 22 23 21
4 | 8 6 11 9 13 4 14 7 11 7 3 | 40 40 42 45 39 41 42 42 38 40 40
5 | 6 9 8 7 9 5 8 6 8 6 2 | 18 14 13 17 17 14 14 17 19 20 16
6E | 4 11 6 22 13 6 8 11 10 14 3 | 45 47 46 52 46 44 45 47 44 46 45
7 | 7 7 11 12 14 5 7 5 9 7 2 | 31 29 25 32 25 27 27 30 25 29 27
8 | 5 5 7 8 8 5 6 10 8 9 2 | 20 23 23 21 19 17 21 25 23 27 20
9 | 7 9 6 9 14 3 8 5 8 7 2 | 25 23 26 26 26 23 24 25 25 26 23
10 | 4 8 7 7 6 3 7 5 8 7 2 | 18 18 21 17 18 16 19 18 17 19 17
11E | 7 8 9 10 13 7 16 12 14 18 3 | 21 22 21 21 23 21 24 24 22 26 20
12 | 5 6 5 5 6 5 7 4 6 8 2 | 27 28 28 27 23 25 27 27 24 27 26
X13 | 6 6 12 9 7 --- 8 8 9 11 3 | 68 66 65 68 65 --- 67 68 66 68 67
14 | 2 16 7 13 6 5 14 7 8 10 3 | 41 42 38 40 41 40 41 41 37 42 39
15 | 7 10 11 8 9 7 9 9 9 13 3 | 22 17 15 20 20 17 18 22 22 23 18
16 | 4 6 7 9 5 4 7 4 7 8 2 | 14 13 16 16 15 13 11 18 15 22 14
17 | 3 6 7 9 8 4 7 6 7 11 2 | 33 34 30 34 33 32 35 35 34 36 33
18E | 9 9 12 17 12 5 20 20 15 22 4 | 38 39 38 40 40 37 41 42 39 43 37
19 | 5 4 6 8 7 4 5 4 7 9 2 | 29 30 28 29 30 29 31 32 31 30 29
20 | 16 17 29 15 13 7 21 8 17 11 5 | 42 43 45 41 41 43 44 44 41 43 42
21 | 6 8 7 7 8 5 12 8 9 9 2 | 18 18 15 17 21 19 20 19 13 19 17
22 | 4 5 7 8 7 5 4 6 9 8 2 | 20 20 21 22 18 17 21 20 19 22 19
23 | 5 7 8 8 8 4 9 7 10 9 2 | 10 15 11 15 17 14 14 16 12 17 12
24 | 6 9 7 14 8 3 8 8 7 8 2 | 32 32 32 32 35 32 32 32 34 33 32
25 | 5 12 6 8 6 6 14 6 10 9 2 | 21 28 24 20 21 20 29 22 23 23 22
26 | 6 8 6 7 5 4 9 6 8 8 2 | 28 32 30 29 26 26 32 31 26 33 28
27 | 6 7 7 7 7 5 8 7 8 10 2 | 17 21 19 16 16 14 19 18 19 22 17
28 | 7 7 8 16 11 6 16 6 12 8 3 | 42 40 42 43 46 43 43 45 41 45 42
29 | 5 6 7 7 7 6 6 5 6 7 2 | 31 31 28 27 28 27 28 32 32 33 29
30 | 6 7 5 18 16 4 7 6 7 7 2 | 720 720 722 719 738 492 721 718 723 721 720
31 | 5 7 10 7 8 4 6 8 8 7 2 | 24 22 15 24 23 20 22 24 21 25 21
32 | 6 10 7 5 7 4 8 7 10 12 2 | 23 25 26 22 23 22 23 22 25 22 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 9 9 11 10 5 10 8 9 10 |T 49 49 49 50 49 40 50 50 49 51 48
WRMS | 6 9 9 11 9 5 10 6 9 9 |NE 53 53 52 53 53 42 53 54 52 55 52
MEDI | 6 7 7 8 8 5 8 7 9 9 |MD 25 25 25 26 23 23 24 25 24 26 23
Table 3.2430.2 GPS week: 2430 Day: 2 MJD: 61256.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 7 8 10 --- 12 4 18 8 15 13 3 | 29 27 27 --- 31 28 29 29 31 29 28
2 | 9 7 7 12 10 6 6 11 14 11 3 | 31 30 30 29 33 30 31 31 31 29 29
3 | 5 7 5 9 8 4 6 5 11 7 2 | 32 36 34 35 31 33 34 33 36 34 33
4 | 8 7 10 8 13 4 12 7 12 9 3 | 38 43 44 47 43 42 44 45 41 45 42
5 | 6 7 8 8 7 4 8 5 7 8 2 | 25 24 23 26 21 19 23 26 27 30 25
6 | 7 8 6 20 15 7 8 10 10 11 3 | 55 56 54 58 55 53 55 61 54 59 55
7 | 6 7 10 10 12 4 8 6 11 6 2 | 27 27 23 28 29 25 25 29 26 29 25
8 | 6 6 7 7 6 3 7 7 11 8 2 | 20 24 24 21 22 20 22 23 22 23 21
9 | 8 9 6 15 12 3 6 5 7 7 2 | 31 32 33 35 32 30 32 32 32 35 31
10 | 6 7 6 7 5 4 7 4 11 7 2 | 36 35 36 33 36 35 36 33 34 35 35
11 | 10 8 9 11 13 6 15 19 14 20 4 | 33 31 31 28 31 30 33 33 33 35 30
12 | 5 5 5 6 4 4 6 6 7 10 2 | 34 35 35 37 32 32 36 33 33 32 33
X13 | 7 5 10 10 5 --- 8 8 9 14 3 | 59 61 58 64 60 --- 61 62 59 62 60
14 | 5 14 6 10 8 5 14 8 7 7 2 | 34 35 34 35 37 35 35 39 36 36 34
15 | 9 8 10 9 9 6 8 9 7 11 2 | 29 27 26 27 28 27 28 29 30 31 27
16 | 4 7 7 7 5 3 8 4 9 8 2 | 25 25 26 26 24 25 23 25 25 28 25
17 | 4 6 8 10 16 4 6 7 10 7 2 | 36 38 36 41 35 36 38 37 39 36 36
18 | 10 14 17 16 12 9 26 28 29 33 6 | 45 42 43 40 46 44 46 45 42 48 42
19 | 5 5 6 9 7 4 4 4 8 6 2 | 27 26 26 25 27 26 27 28 30 28 26
20 | 14 15 28 17 13 5 18 9 15 13 5 | 36 36 38 35 37 35 38 39 36 40 35
21 | 8 9 7 8 8 5 11 9 8 8 2 | 25 24 23 26 27 25 25 27 24 30 25
22 | 6 5 7 8 6 4 4 7 8 8 2 | 22 24 25 24 23 21 24 25 26 27 23
23 | 6 6 7 6 8 3 9 6 10 9 2 | 25 26 24 26 28 26 27 26 23 28 25
24 | 6 8 7 8 11 4 8 6 5 10 2 | 36 36 36 36 39 34 35 37 36 37 36
25 | 5 11 6 8 5 7 12 7 9 11 2 | 21 30 26 23 22 19 31 22 19 23 22
26 | 6 8 6 5 5 4 8 5 7 8 2 | 28 34 32 31 27 28 34 30 26 31 29
27 | 6 6 7 8 7 3 6 5 10 8 2 | 21 23 24 19 21 21 22 20 25 23 21
28 | 7 8 8 9 10 6 14 7 13 9 3 | 37 37 36 38 41 37 38 38 33 39 37
29 | 6 6 7 8 12 5 6 6 7 10 2 | 49 47 49 51 48 49 48 49 50 49 48
30 | 7 7 6 13 13 3 6 9 10 9 2 | 527 525 523 524 538 334 525 527 526 526 525
31 | 6 5 10 8 7 5 6 6 9 7 2 | 30 29 27 32 30 30 29 30 28 32 29
32 | 7 9 7 5 7 4 7 6 11 9 2 | 29 32 32 31 31 30 30 28 29 31 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 8 9 10 10 5 10 9 11 11 |T 47 48 48 49 48 40 48 49 48 50 47
WRMS | 7 8 9 11 8 5 10 6 10 9 |NE 49 50 50 50 50 41 50 50 50 51 49
MEDI | 6 7 7 8 8 4 8 7 10 9 |MD 31 32 32 32 31 30 32 31 31 32 30
Table 3.2430.3 GPS week: 2430 Day: 3 MJD: 61257.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 8 9 12 --- 9 4 18 9 21 13 3 | 23 22 23 --- 24 23 23 25 31 27 23
2 | 5 7 7 9 8 5 8 8 18 10 2 | 32 30 32 34 37 31 30 33 44 32 32
3 | 5 7 8 8 7 3 5 5 11 13 2 | 24 25 25 24 24 22 25 22 27 25 23
4 | 8 6 11 8 12 4 13 4 13 10 2 | 29 34 38 34 37 34 39 34 28 36 33
5 | 8 8 9 8 7 5 9 5 9 7 2 | 21 17 15 19 20 18 17 20 21 20 18
6 | 8 11 8 19 17 4 8 6 10 12 3 | 32 28 34 31 34 27 28 32 30 37 30
7 | 5 7 12 12 14 5 9 8 9 14 3 | 23 24 18 27 30 22 23 23 21 22 22
8 | 4 6 9 9 7 3 6 7 9 5 2 | 16 18 22 18 16 14 18 16 20 15 16
9 | 8 7 8 7 13 4 7 7 11 19 3 | 21 21 22 19 23 19 21 19 20 26 19
10 | 4 9 6 9 6 3 7 5 8 6 2 | 25 26 28 24 26 24 26 24 26 24 24
11 | 9 9 10 12 12 7 19 18 15 23 4 | 26 25 28 24 27 25 25 32 30 37 25
12 | 3 6 8 5 5 3 5 6 7 6 1 | 37 39 42 38 35 37 40 37 36 32 37
X13 | 5 6 9 11 5 --- 6 6 8 5 2 | 29 33 29 39 31 --- 33 34 29 29 31
14 | 4 14 8 7 8 5 13 7 9 11 2 | 24 21 19 24 26 24 24 27 23 30 23
15 | 8 9 11 10 8 6 10 8 11 12 3 | 22 20 17 20 21 19 20 21 21 23 19
16 | 5 7 7 7 5 2 8 5 13 9 2 | 18 16 20 21 18 17 16 19 20 20 17
17 | 5 6 6 11 6 3 5 6 9 9 2 | 29 33 30 36 30 30 31 30 31 31 30
18 | 10 15 18 17 8 8 26 43 33 53 7 | 37 40 39 38 39 37 41 53 50 60 38
19 | 6 4 7 10 7 4 5 6 9 7 2 | 22 23 23 26 24 23 23 25 25 25 23
20 | 13 15 28 17 11 5 20 10 15 13 4 | 22 26 23 22 27 22 26 25 24 27 22
21 | 6 9 9 8 9 5 10 6 11 11 2 | 20 21 21 21 23 21 21 22 21 25 20
22 | 4 7 7 8 6 3 4 7 9 9 2 | 18 22 19 21 18 19 21 21 20 22 19
23 | 6 7 8 6 8 4 9 7 13 9 2 | 18 20 18 20 22 22 19 21 21 21 19
24 | 7 8 7 8 15 4 9 7 11 5 2 | 58 59 58 58 61 59 60 60 63 61 59
25 | 5 11 8 8 5 4 12 5 10 6 2 | 19 30 27 22 20 19 30 20 21 19 21
26 | 5 8 7 7 5 3 9 5 8 7 2 | 30 32 32 28 27 28 35 29 27 26 29
27 | 5 8 9 8 7 2 6 7 9 11 2 | 17 19 23 16 17 15 19 16 22 17 16
28 | 7 7 8 10 9 4 14 5 12 9 2 | 19 20 20 21 25 19 24 23 19 25 20
29 | 5 5 7 5 5 4 6 5 12 6 2 | 36 33 33 33 35 34 34 32 36 32 33
X30 | 75 85 26 33 276 --- 87 36 28 40 16 | 9999 9999 9999 9999 9999 --- 9999 9999 9999 9999 9999
31 | 6 6 10 9 7 3 7 7 9 10 2 | 24 25 20 26 26 22 24 24 23 24 23
32 | 6 12 8 7 6 3 7 5 12 8 2 | 22 28 26 21 24 22 24 22 28 22 22
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 9 10 10 9 4 11 11 13 14 |T 25 26 26 26 27 24 27 27 27 28 25
WRMS | 6 9 10 10 7 4 11 7 11 8 |NE 24 26 25 26 26 24 26 25 25 26 24
MEDI | 6 7 8 8 7 4 8 6 11 9 |MD 23 25 23 24 26 22 24 24 25 25 23
Table 3.2430.4 GPS week: 2430 Day: 4 MJD: 61258.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 10 8 9 --- 11 6 18 12 14 15 4 | 28 27 26 --- 28 26 28 29 27 27 26
2 | 8 6 7 11 10 7 7 11 11 12 3 | 36 36 35 39 39 35 34 38 36 37 36
3 | 5 8 7 11 7 5 6 6 7 6 2 | 27 28 28 29 27 26 27 26 28 26 26
4 | 7 6 11 6 12 4 12 6 10 9 2 | 38 42 45 41 43 40 42 43 40 44 41
X5 | 6 8 8 6 --- --- 8 7 8 11 3 | 25 23 21 23 --- --- 22 25 25 28 23
6 | 10 12 6 18 19 4 8 8 12 7 3 | 36 37 33 34 38 33 33 36 34 34 34
7 | 6 9 11 12 12 4 8 8 10 7 2 | 46 46 42 44 46 43 42 46 40 46 44
8 | 4 6 6 7 7 4 7 8 9 7 2 | 35 39 37 35 35 34 36 37 37 36 35
9 | 6 7 8 6 12 4 8 6 9 6 2 | 24 24 25 24 28 21 23 23 24 25 23
10 | 4 8 7 9 5 3 7 4 7 7 2 | 26 25 27 25 25 26 27 25 25 25 25
11 | 10 11 12 15 12 7 18 28 13 24 5 | 26 27 27 28 29 28 28 35 26 34 27
12 | 5 6 6 6 5 4 5 5 7 10 2 | 50 48 51 49 46 49 50 48 50 45 48
X13 | 7 7 9 10 5 --- 6 6 10 12 3 | 80 79 78 83 79 --- 80 81 81 79 79
14 | 4 14 6 7 8 5 13 7 6 7 2 | 52 53 52 56 55 53 55 55 51 54 53
15 | 8 8 10 6 7 6 8 9 11 12 2 | 27 23 20 25 26 26 24 27 26 26 24
16 | 4 8 7 7 4 3 8 5 9 6 2 | 24 24 25 24 24 23 23 27 25 26 24
17 | 4 7 7 6 6 3 6 6 5 5 1 | 50 49 49 54 48 49 51 51 51 51 50
18 | 8 12 14 18 20 6 24 51 29 61 6 | 49 50 49 53 58 51 49 67 60 73 51
19 | 6 6 6 10 7 3 6 6 8 5 2 | 42 40 41 45 42 41 42 44 39 43 41
20 | 13 14 26 14 12 4 19 12 11 12 4 | 42 44 44 43 45 43 46 45 41 45 43
21 | 6 10 7 6 8 5 10 7 9 9 2 | 25 28 25 29 30 28 28 28 26 28 26
22 | 4 6 7 5 8 3 3 6 5 6 1 | 45 45 46 49 47 46 47 47 42 47 46
23 | 5 6 8 5 7 3 8 6 11 8 2 | 22 24 21 27 25 25 24 26 22 26 24
24 | 9 7 6 6 7 5 9 8 11 8 2 | 97 98 99 99 100 97 99 100 99 100 98
25 | 5 10 7 9 4 5 12 8 7 13 2 | 32 38 36 29 32 33 39 33 35 32 33
26 | 5 8 6 8 5 4 9 5 5 8 2 | 45 47 46 42 42 42 48 46 46 44 44
27 | 5 8 7 7 6 4 6 6 10 6 2 | 31 34 32 30 29 28 32 31 31 30 30
28 | 7 8 8 11 8 5 13 6 9 10 2 | 34 35 33 36 36 34 37 36 35 37 34
29 | 4 5 7 7 5 5 6 5 7 10 2 | 63 61 62 61 60 62 63 63 63 61 62
30 | 6 8 6 10 14 4 7 10 6 6 2 | 432 431 435 432 435 725 431 429 436 432 433
31 | 5 7 11 8 8 4 7 8 8 9 2 | 27 30 25 30 28 26 28 31 31 28 27
32 | 6 10 7 9 7 5 7 5 6 10 2 | 27 32 30 26 28 26 29 27 29 28 27
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 9 9 10 9 4 10 13 10 15 |T 51 52 51 53 53 60 52 53 51 53 51
WRMS | 6 9 10 10 9 4 10 7 9 9 |NE 54 55 54 55 56 65 55 55 54 55 54
MEDI | 6 8 7 8 7 4 8 6 9 8 |MD 35 37 35 36 38 34 36 36 35 36 34
Table 3.2430.5 GPS week: 2430 Day: 5 MJD: 61259.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 10 9 9 --- 11 7 16 17 14 22 4 | 38 38 38 --- 39 38 37 38 39 40 37
2 | 6 8 8 8 9 7 6 16 10 13 3 | 27 29 27 30 28 27 28 29 32 29 27
3 | 5 7 6 6 7 4 6 7 12 4 2 | 42 45 43 43 41 42 42 43 41 42 42
4 | 7 7 11 8 12 4 12 6 11 9 3 | 51 52 54 55 54 52 53 52 52 54 52
X5 | 1 --- --- --- --- --- --- --- --- --- 0 | 49 --- --- --- --- --- --- --- --- --- 43
6 | 6 20 6 10 13 5 8 10 19 9 3 | 70 74 71 73 72 68 68 73 76 73 70
7 | 7 9 11 11 14 5 10 11 14 7 3 | 35 34 31 36 36 32 34 35 32 37 32
8 | 4 7 6 6 7 4 5 7 10 7 2 | 33 35 36 34 35 34 35 33 36 34 34
9 | 8 10 7 8 13 3 7 7 10 10 2 | 46 48 48 46 50 45 47 45 46 47 46
10 | 4 8 6 7 5 4 6 6 6 7 2 | 43 42 44 41 44 42 45 41 44 45 42
11 | 11 13 12 19 13 7 19 38 16 30 6 | 41 42 41 40 40 39 41 47 42 48 39
12 | 4 7 5 6 5 4 5 4 8 5 1 | 37 37 37 37 34 34 36 34 38 37 35
X13 | 7 7 10 13 6 --- 7 5 10 6 3 | 56 58 54 56 55 --- 56 58 54 59 55
14 | 6 14 6 9 7 5 12 9 12 10 3 | 34 36 34 33 34 35 34 38 32 40 34
15 | 8 9 9 10 8 6 8 10 13 8 3 | 43 41 41 40 41 42 42 39 41 40 40
16 | 4 7 6 10 5 2 6 6 13 6 2 | 47 49 49 44 46 47 48 45 52 48 47
17 | 5 9 8 9 9 3 6 8 9 14 2 | 39 42 39 41 41 39 40 39 42 42 39
18 | 11 16 18 17 11 10 29 38 26 43 7 | 111 115 113 110 112 110 114 111 112 112 111
19 | 5 9 6 8 9 4 4 7 11 6 2 | 39 40 38 39 39 38 38 39 39 38 38
20 | 13 13 26 17 11 4 16 12 14 7 4 | 52 55 59 52 55 55 56 54 53 56 53
21 | 7 11 7 7 7 4 10 8 11 8 2 | 36 38 37 41 39 39 38 36 36 42 37
22 | 5 6 6 8 7 3 3 8 14 6 2 | 31 31 32 32 29 29 31 31 29 34 30
23 | 6 7 6 6 7 4 8 7 9 8 2 | 34 35 34 35 38 36 37 35 37 40 35
24 | 7 9 6 7 7 4 7 6 10 8 2 | 51 52 49 50 54 51 51 54 56 56 52
25 | 4 10 8 9 5 5 11 8 10 9 2 | 36 41 39 34 34 34 41 35 39 35 36
26 | 5 8 5 5 5 3 7 6 11 6 2 | 38 41 40 35 36 38 41 39 43 41 38
27 | 4 8 7 6 6 3 5 7 10 9 2 | 39 41 42 37 38 38 40 35 43 38 38
28 | 6 7 8 8 9 6 14 7 10 9 2 | 60 62 61 62 62 62 63 61 61 64 61
29 | 6 6 6 7 7 5 6 6 7 10 2 | 40 39 40 38 39 39 39 39 40 41 39
30 | 6 8 7 11 16 3 8 16 9 12 3 | 547 546 548 547 554 332 547 551 548 550 548
31 | 6 8 11 9 8 4 8 11 14 8 2 | 48 47 45 47 46 47 47 46 49 48 46
32 | 5 10 6 6 6 4 7 5 8 9 2 | 40 42 42 39 38 39 41 36 43 40 39
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 10 9 9 9 5 10 13 12 13 |T 60 62 61 61 61 53 61 61 62 62 59
WRMS | 6 10 10 9 9 5 10 7 11 7 |NE 60 62 62 61 62 52 62 61 62 63 60
MEDI | 6 8 7 8 7 4 7 7 11 8 |MD 40 42 41 40 40 39 41 39 42 42 39
Table 3.2430.6 GPS week: 2430 Day: 6 MJD: 61260.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg jgx jpl mit ngs sio IGS | cod emr esa gfz grg jgx jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
X1 | 11 10 10 --- 15 7 17 17 17 18 4 | 28 25 26 --- 29 28 26 32 26 32 26
2 | 8 9 7 7 10 6 9 11 9 11 3 | 30 29 29 27 31 30 29 30 32 30 28
3 | 5 7 5 7 6 3 7 4 7 9 2 | 34 35 36 35 35 34 36 34 34 35 34
4 | 9 8 9 10 12 3 13 6 11 9 3 | 51 49 56 54 51 53 55 53 56 55 52
5 | 7 10 8 9 7 6 9 7 8 8 2 | 19 15 11 18 16 15 16 15 16 15 15
6 | 9 21 7 19 14 7 20 14 19 13 4 | 58 65 59 60 58 58 66 64 51 61 58
7 | 5 11 10 11 12 5 12 8 11 8 3 | 23 26 20 26 28 23 25 25 28 26 23
8 | 4 8 7 5 8 4 7 5 10 4 2 | 17 19 21 16 17 16 20 16 19 19 17
9 | 7 10 6 5 12 3 9 7 10 6 2 | 35 32 34 32 34 33 34 36 39 35 33
10 | 3 11 6 9 6 4 7 4 4 7 2 | 33 33 34 32 34 33 33 33 32 33 32
11 | 10 10 10 13 11 5 16 56 37 59 5 | 29 28 27 28 28 26 29 52 43 58 27
12 | 4 7 7 6 6 3 7 4 8 7 2 | 45 45 47 46 41 43 48 43 40 38 43
X13 | 10 8 34 16 8 --- 10 8 8 7 5 | 70 73 72 70 70 --- 72 71 68 68 69
14 | 5 13 6 7 7 5 11 8 11 8 2 | 46 45 43 42 47 44 46 49 49 44 45
15 | 6 12 10 8 7 7 9 9 11 12 3 | 27 26 22 25 26 23 25 25 25 24 23
16 | 4 9 7 9 6 3 7 4 8 6 2 | 30 34 32 29 28 30 31 30 34 33 30
17 | 5 8 7 7 9 4 7 7 11 10 2 | 31 34 31 33 31 32 33 36 36 35 32
18 | 11 9 9 21 13 5 19 25 19 10 4 | 131 129 129 129 132 131 130 135 133 137 130
19 | 5 9 6 10 9 4 7 5 12 7 2 | 22 22 21 23 21 22 23 25 24 23 22
20 | 10 18 75 13 9 7 21 10 13 8 4 | 55 55 70 55 56 55 57 58 56 54 55
21 | 6 11 7 8 8 7 12 6 10 8 2 | 30 31 29 33 34 31 31 31 32 32 30
22 | 5 6 7 6 7 2 5 8 11 10 2 | 15 18 18 16 15 16 19 20 18 20 16
23 | 6 10 7 5 8 5 9 6 9 13 2 | 20 25 20 22 25 23 22 23 20 26 21
24 | 6 11 5 5 8 5 10 7 9 7 2 | 30 33 28 26 32 28 32 30 33 27 29
25 | 5 11 9 7 6 5 13 7 9 9 2 | 24 30 29 24 23 23 32 26 24 23 25
26 | 5 11 6 7 5 4 8 5 6 7 2 | 33 36 35 34 31 32 38 34 30 33 33
27 | 4 9 6 6 7 3 7 5 6 6 2 | 21 24 24 19 19 21 24 21 22 23 21
28 | 7 8 7 8 9 6 17 6 12 9 3 | 60 60 59 59 64 60 61 65 59 63 60
29 | 6 7 7 8 7 6 8 6 10 7 2 | 37 35 36 37 36 35 36 39 39 35 36
30 | 7 8 8 11 18 3 8 12 9 6 3 | 382 379 379 383 378 269 380 386 380 385 381
31 | 5 7 11 8 7 4 8 5 8 4 2 | 30 32 26 32 31 29 30 30 30 30 29
32 | 4 12 6 7 7 4 7 8 8 8 2 | 30 35 32 30 32 30 31 31 31 30 30
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 10 15 10 9 5 11 13 12 14 |T 47 48 47 48 47 42 49 49 48 49 47
WRMS | 6 10 10 9 9 5 11 7 11 7 |NE 46 47 46 46 46 40 47 47 47 46 45
MEDI | 6 9 7 8 8 5 9 7 10 8 |MD 30 33 31 32 31 30 32 32 32 33 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 4.2430 GPS week: 2430 MJD: 61254.0-61260.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 12 12 27 |U 7 15 33 |U 9 11 31 |
emr | emr 3044 |U 14 19 35 |U 9 14 36 | 10 16 37 |
esa | esa 3058 | 10 12 30 | 6 13 25 | 8 9 30 |
gfz | gfz 2962 | 9 11 27 | 7 12 27 | 7 8 25 |
grg | grg 3044 |U 11 13 32 |U 6 16 35 | 9 10 30 |
igs | igs 3058 | 9 12 25 | 6 13 26 | 7 9 26 |
jgx | jgx 2934 |U 9 11 28 |U 6 13 28 |U 7 9 24 |
jpl | jpl 3058 | 13 17 42 | 9 15 37 | 12 17 41 |
mit | mit 3058 |U 11 12 28 |U 7 15 34 |U 9 9 29 |
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 5.2430.0 GPS week: 2430 Day: 0 MJD: 61254.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 10 19 | 5 13 33 | 11 14 28 |
emr | emr 3072 | 12 17 32 | 7 12 32 | 13 22 35 |
esa | esa 3072 | 12 13 28 | 6 13 27 | 10 13 29 |
gfz | gfz 2976 | 8 10 24 | 6 13 28 | 10 13 28 |
grg | grg 3072 | 10 12 29 | 6 18 36 | 10 12 33 |
igs | igs 3072 | 8 11 24 | 5 13 27 | 9 13 26 |
jgx | jgx 2976 | 7 10 24 | 6 13 30 | 8 12 26 |
jpl | jpl 3072 | 13 15 43 | 8 15 31 | 13 20 39 |
mit | mit 3072 | 9 11 24 | 6 14 34 | 9 11 30 |
Table 5.2430.1 GPS week: 2430 Day: 1 MJD: 61255.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 13 14 25 | 7 12 27 | 8 11 32 |
emr | emr 3072 | 16 20 38 | 8 15 33 | 11 18 38 |
esa | esa 3072 | 15 16 30 | 7 13 26 | 9 11 33 |
gfz | gfz 2976 | 12 16 27 | 8 11 29 | 7 6 28 |
grg | grg 3072 | 14 17 34 | 7 17 36 | 9 8 34 |
igs | igs 3072 | 13 15 27 | 6 13 27 | 7 9 30 |
jgx | jgx 2976 | 11 15 29 | 6 13 29 | 7 7 29 |
jpl | jpl 3072 | 16 18 44 | 8 15 34 | 13 19 44 |
mit | mit 3072 | 13 14 29 | 7 13 34 | 9 8 35 |
Table 5.2430.2 GPS week: 2430 Day: 2 MJD: 61256.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 9 28 | 5 13 25 | 8 9 28 |
emr | emr 3072 | 12 16 35 | 7 13 26 | 9 16 35 |
esa | esa 3072 | 12 13 31 | 5 12 19 | 8 8 28 |
gfz | gfz 2976 | 9 12 27 | 8 12 28 | 6 6 27 |
grg | grg 3072 | 11 12 31 | 6 17 36 | 8 10 31 |
igs | igs 3072 | 9 10 27 | 5 12 24 | 6 9 26 |
jgx | jgx 2976 | 8 10 27 | 5 12 27 | 6 7 24 |
jpl | jpl 3072 | 13 15 39 | 6 13 26 | 10 17 40 |
mit | mit 3072 | 8 10 27 | 6 14 33 | 7 9 27 |
Table 5.2430.3 GPS week: 2430 Day: 3 MJD: 61257.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 18 23 50 | 11 25 51 | 11 16 54 |
emr | emr 3072 | 21 29 56 | 14 19 66 | 8 14 42 |
esa | esa 3072 | 9 15 36 | 6 14 26 | 7 9 33 |
gfz | gfz 2976 | 8 11 32 | 6 12 28 | 7 9 22 |
grg | grg 3072 | 10 13 31 | 6 15 30 | 10 11 27 |
igs | igs 3072 | 8 13 30 | 5 13 28 | 7 10 29 |
jgx | jgx 2880 | 9 10 33 | 6 12 26 | 7 9 20 |
jpl | jpl 3072 | 21 27 64 | 15 26 76 | 8 15 45 |
mit | mit 3072 | 8 12 31 | 6 17 34 | 9 12 33 |
Table 5.2430.4 GPS week: 2430 Day: 4 MJD: 61258.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 10 9 23 | 5 14 33 | 7 8 25 |
emr | emr 3072 | 12 15 36 | 8 13 32 | 11 13 32 |
esa | esa 3072 | 8 9 30 | 5 12 25 | 9 9 28 |
gfz | gfz 2976 | 8 10 28 | 6 12 27 | 7 7 22 |
grg | grg 2976 | 11 10 37 | 6 17 36 | 10 8 30 |
igs | igs 3072 | 8 9 28 | 5 13 27 | 7 9 22 |
jgx | jgx 2880 | 9 10 32 | 5 13 28 | 8 9 22 |
jpl | jpl 3072 | 10 15 39 | 7 13 28 | 12 15 39 |
mit | mit 3072 | 10 10 31 | 6 19 34 | 9 8 26 |
Table 5.2430.5 GPS week: 2430 Day: 5 MJD: 61259.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 2976 | 10 12 20 | 7 13 23 | 7 7 26 |
emr | emr 2880 | 13 16 26 | 9 13 32 | 11 17 44 |
esa | esa 2976 | 9 12 28 | 7 14 23 | 7 8 31 |
gfz | gfz 2880 | 8 10 23 | 6 12 22 | 7 7 24 |
grg | grg 2976 | ---- ---- ---- | ---- ---- ---- | ---- ---- ---- |
igs | igs 2976 | 9 12 19 | 6 13 20 | 6 7 26 |
jgx | jgx 2880 | 9 12 23 | 6 13 22 | 6 7 25 |
jpl | jpl 2976 | 11 16 35 | 8 13 32 | 11 14 45 |
mit | mit 2976 | 15 16 28 | 7 16 26 | 8 8 31 |
Table 5.2430.6 GPS week: 2430 Day: 6 MJD: 61260.0
CENT| CLK EPO | BRUX | TOW2 | WILL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3072 | 11 11 22 | 7 13 39 | 8 9 21 |
emr | emr 3072 | 14 17 25 | 10 14 35 | 9 14 32 |
esa | esa 3072 | 8 11 24 | 9 12 32 | 9 7 28 |
gfz | gfz 2976 | 9 11 25 | 6 11 29 | 7 8 23 |
grg | grg 3072 | 13 13 33 | 8 13 39 | 9 10 26 |
igs | igs 3072 | 10 12 21 | 8 11 31 | 7 8 20 |
jgx | jgx 2976 | 10 10 25 | 7 12 33 | 7 9 22 |
jpl | jpl 3072 | 10 15 29 | 9 13 33 | 14 17 39 |
mit | mit 3072 | 14 14 30 | 12 14 44 | 8 10 22 |
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 6.2430 GPS week: 2430 MJD: 61254.500-61260.500
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 -7 15 -44 2 | -2 25
| 18 10 47 58 3 | 3
emr uuuuu | -22 23 -35 -68 -3 | -21 32
| 14 18 68 57 15 | 3
esa uuuuu | -14 -10 35 -2 0 | -2 27
| 9 5 25 44 5 | 2
gfz uuuuu | -15 -12 -3 41 -1 | 1 26
| 21 20 142 52 4 | 3
grg uuuuu | 0 21 -13 -14 0 | 7 27
| 11 8 34 50 2 | 3
irf xxxxx | -5 5 10 -14 -3 | 3 27
| 6 3 6 16 2 | 3
jgx uuuuu | 27 -8 -25 71 2 | 2 26
| 6 6 27 24 4 | 3
jpl uuuuu | -10 2 29 -61 -5 | -4 24
| 11 11 39 57 9 | 4
mit uuuuu | -8 4 24 -109 1 | 22 32
| 15 12 53 83 3 | 3
ngs uuuuu | 19 1 -10 161 4 | 9 29
| 39 33 97 56 5 | 3
sio xxxxx | 41 57 -67 -10 3 | 29 40
| 73 60 99 53 5 | 3
Table 7.2430.0 GPS week: 2430 Day: 0 MJD: 61254.500
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 -15 33 -152 3 | 1 22
emr uuuuu | -34 12 -54 -101 3 | -18 28
esa uuuuu | -3 -2 23 64 7 | -2 24
gfz uuuuu | -39 16 18 -38 0 | 5 23
grg uuuuu | 16 16 -49 27 -2 | 9 24
irf xxxxx | -13 5 12 -13 -4 | 6 23
jgx uuuuu | 25 -16 -49 64 -2 | 6 23
jpl uuuuu | -28 -6 42 -137 -6 | 3 20
mit uuuuu | -27 -7 87 36 0 | 25 32
ngs uuuuu | 75 48 -35 205 2 | 11 27
sio xxxxx | -1 -20 -24 -67 7 | 27 37
Table 7.2430.1 GPS week: 2430 Day: 1 MJD: 61255.500
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 | -32 -2 69 -78 2 | 0 22
emr uuuuu | -21 15 -56 -56 7 | -19 29
esa uuuuu | -19 -18 15 -19 3 | -2 24
gfz uuuuu | 11 5 -272 125 -1 | 4 23
grg uuuuu | -7 8 9 -108 -2 | 8 24
irf xxxxx | 0 0 15 -3 -5 | 5 24
jgx uuuuu | 28 -1 -29 66 -2 | 4 24
jpl uuuuu | -12 -13 25 -36 -8 | 1 21
mit uuuuu | -3 -12 79 -70 -1 | 23 31
ngs uuuuu | 56 34 74 207 6 | 10 27
sio xxxxx | 125 -31 -149 -26 -2 | 28 38
Table 7.2430.2 GPS week: 2430 Day: 2 MJD: 61256.500
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 -12 -11 -16 6 | -4 25
emr uuuuu | -30 24 -43 -99 -18 | -22 32
esa uuuuu | 0 -5 16 -17 6 | -4 26
gfz uuuuu | 2 -21 78 20 -1 | 0 25
grg uuuuu | 4 21 -55 17 3 | 5 26
irf xxxxx | 3 7 13 9 1 | 1 26
jgx uuuuu | 24 -12 -7 52 7 | 0 26
jpl uuuuu | 1 4 18 -53 -16 | -4 25
mit uuuuu | 0 20 37 -91 0 | 20 31
ngs uuuuu | 5 -10 -31 223 8 | 8 28
sio xxxxx | 126 122 -103 -74 1 | 27 38
Table 7.2430.3 GPS week: 2430 Day: 3 MJD: 61257.500
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 | 11 6 -14 -50 0 | -6 23
emr uuuuu | -16 17 -84 -136 20 | -25 33
esa uuuuu | -16 -12 64 -78 -7 | -5 26
gfz uuuuu | -41 -40 61 90 -9 | -2 24
grg uuuuu | 11 24 -22 17 -1 | 3 25
irf xxxxx | -2 5 17 -37 -3 | 0 25
jgx uuuuu | 22 -9 -13 124 0 | -1 24
jpl uuuuu | 3 11 22 -67 10 | -7 25
mit uuuuu | 1 18 16 -99 1 | 18 29
ngs uuuuu | -37 -29 20 108 -5 | 6 26
sio xxxxx | 36 79 -45 63 -1 | 27 38
Table 7.2430.4 GPS week: 2430 Day: 4 MJD: 61258.500
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 -7 80 -9 4 | -6 24
emr uuuuu | -32 24 -63 -88 3 | -24 32
esa uuuuu | -21 -13 8 14 0 | -5 27
gfz uuuuu | -30 -33 161 24 -1 | -4 25
grg uuuuu | -10 25 -19 3 0 | 3 25
irf xxxxx | -2 8 8 -14 -1 | 0 25
jgx uuuuu | 21 2 -34 65 5 | -2 25
jpl uuuuu | -6 4 16 -95 -15 | -8 25
mit uuuuu | 11 6 41 -144 -1 | 18 29
ngs uuuuu | 3 -4 -194 176 7 | 6 27
sio xxxxx | 33 80 -127 34 5 | 28 38
Table 7.2430.5 GPS week: 2430 Day: 5 MJD: 61259.500
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 | -16 -21 -47 27 -3 | 0 29
emr uuuuu | 6 60 -64 -37 -14 | -18 33
esa uuuuu | -17 -13 66 22 -2 | 1 31
gfz uuuuu | -5 -4 34 30 0 | 1 30
grg uuuuu | -11 33 41 -57 1 | 9 31
irf xxxxx | -4 6 0 -31 -4 | 5 31
jgx uuuuu | 29 -11 18 53 7 | 5 31
jpl uuuuu | -8 18 -23 -86 1 | -5 27
mit uuuuu | -9 3 -33 -168 3 | 24 37
ngs uuuuu | -6 -44 -8 133 7 | 12 34
sio xxxxx | 51 107 129 29 4 | 34 46
Table 7.2430.6 GPS week: 2430 Day: 6 MJD: 61260.500
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 4 -6 -28 0 | -1 30
emr uuuuu | -27 6 117 39 -19 | -20 36
esa uuuuu | -22 -10 52 2 -4 | 0 32
gfz uuuuu | -5 -9 -103 37 5 | 1 31
grg uuuuu | -1 22 7 5 3 | 8 32
irf xxxxx | -14 1 7 -10 -3 | 4 32
jgx uuuuu | 40 -6 -63 73 3 | 4 31
jpl uuuuu | -17 -5 105 46 -1 | -5 28
mit uuuuu | -31 -1 -55 -224 7 | 23 37
ngs uuuuu | 37 12 107 76 3 | 13 34
sio xxxxx | -86 60 -148 -30 12 | 33 46
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