Delivered-To: igsreport@igscb.jpl.nasa.gov To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-11221] Wk 1263 IGS Final Orbits - with MIT Message-Id: <20040414180510.529E14F738@kg20.gfz-potsdam.de> Date: Wed, 14 Apr 2004 20:05:10 +0200 (CEST) From: igsacc@gfz-potsdam.de (Gerd Gendt.) Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 14 Apr 11:05:43 PDT 2004 Message Number 11221 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam Final IGS Orbit Combination - Week 1263 (Mar 21, 2004 - Mar 27, 2004) Contacts: G. Gendt (gendt@gfz-potsdam.de), Th. Nischan (nisn@gfz-potsdam.de) COMBINATION STRATEGY: For a complete description of combination strategy, please refer to the report posted on CDDIS (IGS12637.SUM). 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. 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 (weights are those from the orbit combination). Pole rate combination uses only centres providing estimated pole rates. 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 3 weeks (21 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: IGS12630-6.SP3 IGS GPS ephemeris files for days 0-6, week 1263 in SP3 format. IGS12637.ERP Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. IGS12637.SUM Complete report. REMARKS on IGS Final Orbit Combination: 1. The centres used in the clock combination are COD, EMR, ESA, GFZ and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid ("IGR") orbits/clocks are included in the combination for statistics 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. Day | Centre | PRN/STA list ----+--------+--------------- 0 | EMR | TRO1 YELL 0 | ESA | ALGO AUCK PIMO TIXI YELL 0 | GFZ | BAN2 0 | JPL | SEY1 0 | MIT | BAN2 CRO1 FAIR JPLM KARR MAS1 NKLG SFER 1 | JPL | ALL 1 | EMR | TRO1 1 | ESA | 6 ALGO AUCK GODE 1 | GFZ | BAN2 LPGS MALI MCM4 YELL 1 | MIT | BOR1 DAV1 GODE NRIL SFER 2 | COD | 10 2 | EMR | TRO1 2 | ESA | 6 10 ALGO AUCK CRO1 FORT LPGS 2 | GFZ | LPGS MALI 2 | MIT | FORT JPLM KARR LPGS MALI MCM4 SANT 3 | COD | 10 SANT 3 | EMR | TRO1 3 | ESA | 6 10 ALGO AUCK LPGS YELL 3 | GFZ | BAN2 LPGS STJO 3 | JPL | ASC1 CRO1 SEY1 YELL 3 | MIT | CRO1 STJO TOW2 4 | COD | 10 SCH2 4 | EMR | TRO1 4 | ESA | 6 10 15 AUCK CEDU FORT PIMO 4 | GFZ | 15 RIOG 4 | JPL | FORT 4 | MIT | 15 NKLG NLIB RIOG SCH2 5 | COD | FAIR NRIL 5 | EMR | FORT TRO1 5 | ESA | 6 ALGO AUCK FORT PERT YELL 5 | GFZ | ASC1 BAN2 MALI 5 | JPL | SEY1 5 | MIT | FAIR KIT3 MAD2 NRIL SFER 6 | COD | 10 6 | EMR | TRO1 YELL 6 | ESA | 6 ALGO AUCK FORT RIOG 6 | GFZ | BAN2 FORT LPGS MALI SYOG WES2 6 | JPL | FAIR SEY1 TRO1 YELL 6 | MIT | CAGZ FAIR SANT SFER SYOG 5. 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 19 | | | | | 2 | 2 | 2 PRN 29 | | | 1 | | | | PRN 05 | | | | 2 | | | 6. Starting on 11-Jan-2004 (GPS Week 1253, day 0, MJD 53015) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2000 reference frame (IGb00). For more information see IGSMAIL #4748. 7. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGb00. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS03P33_RS99.snx SINEX. 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 | (cm) (cm) (cm) (mas) (mas) (mas) (ppb) -------+--------------------------------------------------- COD | +0.86 +0.49 +0.42 +0.00 +0.04 +0.01 +2.22 EMR | +0.06 -0.09 -0.05 -0.01 -0.03 -0.00 +3.46 ESA | +0.04 +0.66 +0.04 +0.01 -0.01 +0.01 +2.46 GFZ | -0.16 +0.24 -0.10 +0.01 +0.01 +0.03 +1.85 JPL | -0.44 +0.37 +0.56 +0.09 -0.02 +0.07 +1.07 MIT | +0.09 -0.28 +0.67 +0.07 -0.01 -0.09 +4.28 NGS | -0.24 +0.09 -1.93 +0.09 -0.03 +0.00 +2.53 SIO | +0.62 -0.74 +3.79 -0.06 -0.03 +0.12 +2.65 8. Starting on 22-Oct-2000 (GPS Week 1085, day 0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 9. Starting on 27-Feb-2000 (GPS Week 1051, day 0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs) as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 10.Starting on 29-Nov-1998 (GPS Week 986, day 0; MJD 51146) all IGS clock products reflect the use of the following antenna phase center offsets (satellite fixed reference frame): Block II/IIA: 0.279 0.000 1.023 X, Y, Z in meters Block IIR : 0.000 0.000 0.000 X, Y, Z in meters ORBIT COMBINATION AND EVALUATION STATISTICS: For a complete description of tables and statistics, please refer to the report posted on CDDIS (IGS12637.SUM). Table 1: Week 1263 summary. (Mar 21, 2004 - Mar 27, 2004) Table 1.1263.a GPS week: 1263 MJD: 53085.000-53091.000 Mean and standard deviations of transformation parameters. WRMS - orbit RMS weighted by the SP3 header accuracy codes. STA - Mean number of stations in the daily solutions. Units: meters, mas, ppb, nano-sec, nano-sec/day. CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 169|0.00 0.00 0.00 0.02 -0.07 -0.02 -0.4 0.02 0.02 | -0.1 0.4 0.05 |0.00 0.00 0.00 0.01 0.01 0.05 0.0 | 0.5 1.3 emr 40 |0.00 0.00 0.00 0.05 0.08 0.10 0.2 0.02 0.02 | 2428.9 27.0 0.03 |0.00 0.00 0.00 0.03 0.04 0.16 0.0 | 58.4 2.6 esa 73 |0.00 0.00 0.00 0.07 0.05 -0.01 0.2 0.03 0.03 | 2403.4 28.0 0.06 |0.00 0.00 0.00 0.06 0.05 0.09 0.0 | 48.5 2.4 gfz 170|0.00 0.00 0.00 0.02 -0.02 0.08 -0.3 0.02 0.02 | 0.2 -0.2 0.03 |0.00 0.00 0.00 0.02 0.03 0.08 0.0 | 0.2 0.4 igr n/a|0.00 0.00 0.00 -0.01 0.00 -0.02 -0.2 0.01 0.01 | -2.2 0.6 0.04 |0.00 0.00 0.00 0.01 0.01 0.03 0.0 | 3.0 2.7 jpl 80 |0.00 0.00 0.00 -0.18 0.06 -0.03 0.2 0.03 0.03 | -2.2 0.1 0.03 |0.00 0.00 0.00 0.04 0.02 0.02 0.1 | 2.4 2.5 mit 148|0.00 0.00 0.00 -0.09 -0.05 -0.11 0.2 0.03 0.02 | -1.3 0.3 0.04 |0.00 0.00 0.00 0.01 0.04 0.02 0.0 | 2.0 0.7 ngs 80 |0.00 0.00-0.01 -0.01 -0.01 -0.22 -0.1 0.07 0.06 | 0.0 0.1 3.25 |0.00 0.00 0.00 0.07 0.16 0.09 0.1 | 0.4 0.5 sio 154|0.00 0.00-0.01 0.18 0.07 -0.03 0.5 0.05 0.05 | 0.0 0.0 0.00 |0.00 0.00 0.00 0.08 0.08 0.06 0.1 | 0.0 0.0 Table 1.1263.b GPS week : 1263 MJD: 53085.000-53091.000 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: cm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------|-----------------------------|------------------------------------------ 1 | 1 1 1 1 1 1 1 | 3E | 2 1 1 1 1 1 1 | 4 | 1 1 1 1 1 1 1 | 5E | 1 1 1 1 1 1 1 | 6E | 1 1 1 1 1 1 1 | 7 | 1 1 1 1 1 1 1 | 8 | 1 1 1 1 1 1 1 | 9 | 1 1 1 1 1 1 1 | 10E | 1 1 1 1 1 1 1 | 11 | 1 1 1 1 1 1 1 | 13 | 1 1 1 1 1 1 1 | 14 | 1 1 1 1 1 1 1 | 15 | 1 1 1 1 1 1 1 | 16E | 1 1 1 1 1 1 1 | 17 | 1 1 1 1 1 1 1 | 18E | 1 1 1 1 1 1 1 | 19 | --- --- --- --- 0 0 0 | 20E | 1 1 1 1 1 1 1 | 21 | 1 1 1 1 1 1 1 | 22E | 1 1 1 1 1 1 1 | 24 | 1 1 1 1 1 1 1 | 25E | 1 1 1 1 1 1 1 | 26 | 1 1 1 1 1 1 1 | 27 | 1 1 1 1 1 1 1 | 28E | 1 1 1 1 1 1 1 | 29 | 1 1 1 1 1 1 1 | 30E | 1 2 1 1 1 1 1 | 31E | 1 1 1 1 1 1 1 | 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 sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Units: meters, mas, ppb, nano-sec, nano-sec/day. Table 2.1263.0 GPS week: 1263 Day: 0 MJD: 53085.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 169|0.00 0.00 0.00 0.02 -0.09 -0.09 -0.5 0.02 0.02 | 0.0 0.0 0.05 | 0.01 0.02 | emr 40 |0.00 0.00 0.00 0.01 0.06 0.30 0.2 0.02 0.02 | 2351.0 25.0 0.03 | 0.05 -0.05 | esa 73 |0.00 0.00 0.00 0.05 0.05 -0.03 0.2 0.03 0.03 | 2352.0 26.9 0.06 | -0.04 0.04 | gfz 171|0.00 0.00 0.00 0.03 -0.02 -0.04 -0.2 0.02 0.02 | 0.3 -0.1 0.03 | -0.04 0.00 | igr n/a|0.00 0.00 0.00 -0.03 0.00 -0.07 -0.1 0.01 0.01 | -2.0 -2.1 0.03 | 0.02 0.01 | jpl 80 |0.00 0.00 0.00 -0.15 0.03 -0.05 0.2 0.03 0.03 | -1.1 -2.3 0.03 | 0.02 0.05 | mit 147|0.00 0.00 0.00 -0.10 -0.05 -0.14 0.2 0.04 0.02 | -5.4 0.2 0.04 | 0.13 0.03 | ngs 80 |0.01 0.00-0.02 0.04 0.09 -0.11 -0.1 0.06 0.05 | 0.3 0.0 2.50 | -0.33 -0.13 | sio 151|0.00 0.00-0.01 0.31 0.23 0.06 0.5 0.05 0.05 | 0.0 0.0 0.00 | -0.07 -0.07 | Table 2.1263.1 GPS week: 1263 Day: 1 MJD: 53086.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 169|0.00 0.00 0.00 0.02 -0.09 -0.07 -0.5 0.02 0.02 | -0.4 -0.5 0.05 | 0.02 0.01 | emr 40 |0.00 0.00 0.00 0.06 0.10 0.36 0.2 0.02 0.02 | 2374.2 27.5 0.04 | 0.08 -0.10 | esa 73 |0.00 0.00 0.00 0.07 -0.02 -0.19 0.2 0.03 0.03 | 2339.7 28.5 0.06 | -0.07 -0.05 | gfz 176|0.00 0.00 0.00 0.01 -0.01 0.01 -0.2 0.02 0.02 | 0.1 0.2 0.03 | -0.03 -0.01 | igr n/a|0.00 0.00 0.00 -0.01 0.00 0.00 -0.1 0.01 0.01 | -4.2 -0.1 0.04 | 0.03 -0.05 | jpl 79 |0.00 0.01 0.00 -0.12 0.05 -0.05 0.2 0.03 0.03 | 0.0 0.0 0.00 | -0.03 -0.02 | mit 147|0.00 0.00 0.00 -0.09 -0.02 -0.12 0.2 0.03 0.02 | -1.7 1.0 0.03 | 0.11 0.04 | ngs 80 |0.01 0.00-0.01 -0.07 0.07 -0.13 0.0 0.06 0.05 | -0.7 -0.4 3.30 | -0.16 -0.14 | sio 154|0.00 0.00-0.01 0.21 0.11 0.02 0.4 0.04 0.04 | 0.0 0.0 0.00 | -0.02 -0.04 | Table 2.1263.2 GPS week: 1263 Day: 2 MJD: 53087.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 169|0.00 0.00 0.00 0.05 -0.06 0.03 -0.5 0.02 0.02 | -0.8 2.8 0.05 | 0.01 -0.01 | emr 40 |0.00 0.00 0.00 0.03 0.07 0.01 0.2 0.02 0.02 | 2400.3 24.8 0.04 | 0.06 -0.07 | esa 73 |0.00 0.00 0.00 0.10 0.12 0.01 0.2 0.03 0.03 | 2401.7 26.0 0.06 | -0.06 -0.03 | gfz 172|0.00 0.00 0.00 0.05 -0.03 0.06 -0.3 0.02 0.02 | 0.4 -0.9 0.02 | -0.07 0.01 | igr n/a|0.00 0.00 0.00 0.01 0.01 -0.01 -0.2 0.01 0.01 | -4.0 -2.5 0.04 | 0.01 -0.05 | jpl 80 |-.01 0.00 0.00 -0.22 0.04 0.02 0.3 0.03 0.03 | -3.9 -3.0 0.04 | 0.05 0.04 | mit 148|0.00 0.00 0.00 -0.10 -0.11 -0.10 0.2 0.02 0.02 | 0.8 -0.6 0.04 | 0.12 0.07 | ngs 80 |0.00-0.01-0.01 -0.10 0.13 -0.22 0.0 0.07 0.05 | 0.5 -0.2 3.69 | -0.12 -0.21 | sio 155|0.00 0.00-0.01 0.11 0.02 -0.04 0.5 0.04 0.03 | 0.0 0.0 0.00 | -0.03 0.02 | Table 2.1263.3 GPS week: 1263 Day: 3 MJD: 53088.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 169|0.00 0.00 0.00 0.03 -0.06 -0.02 -0.5 0.01 0.01 | -0.4 1.4 0.04 | 0.04 -0.03 | emr 40 |0.00 0.00 0.00 0.06 0.15 0.03 0.2 0.02 0.02 | 2426.4 29.8 0.03 | 0.06 -0.12 | esa 73 |0.00 0.00 0.00 0.00 -0.01 0.00 0.3 0.03 0.03 | 2394.1 29.8 0.06 | -0.08 -0.03 | gfz 170|0.00 0.00 0.00 0.03 0.00 0.12 -0.2 0.02 0.02 | -0.1 0.0 0.03 | -0.06 -0.01 | igr n/a|0.00 0.00 0.00 0.00 0.00 0.01 -0.2 0.01 0.01 | -5.5 2.5 0.04 | 0.06 -0.06 | jpl 80 |0.00 0.00 0.00 -0.17 0.07 -0.02 0.3 0.03 0.03 | -5.9 2.0 0.03 | 0.01 -0.02 | mit 148|0.00 0.00 0.00 -0.11 -0.09 -0.10 0.2 0.03 0.02 | -0.4 0.7 0.04 | 0.16 0.06 | ngs 80 |0.00-0.01-0.01 -0.01 0.08 -0.22 -0.2 0.06 0.05 | -0.2 1.1 3.39 | -0.18 -0.17 | sio 156|0.00 0.00 0.00 0.19 0.01 -0.02 0.6 0.05 0.04 | 0.0 0.0 0.00 | -0.06 0.08 | Table 2.1263.4 GPS week: 1263 Day: 4 MJD: 53089.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 169|0.00 0.00 0.00 0.00 -0.07 0.02 -0.5 0.02 0.02 | 0.0 0.3 0.05 | 0.04 0.00 | emr 40 |0.00 0.00 0.00 0.07 0.11 0.00 0.3 0.02 0.02 | 2454.2 31.0 0.04 | 0.01 -0.10 | esa 73 |0.00 0.00 0.00 0.09 0.06 0.03 0.2 0.03 0.03 | 2414.1 32.3 0.06 | -0.14 -0.06 | gfz 167|0.00 0.00 0.00 0.03 -0.08 0.14 -0.3 0.02 0.02 | 0.1 -0.5 0.03 | -0.08 0.01 | igr n/a|0.00 0.00 0.00 -0.01 0.03 0.00 -0.2 0.01 0.01 | -3.3 4.9 0.04 | -0.03 -0.06 | jpl 80 |0.00 0.00 0.00 -0.19 0.09 -0.05 0.2 0.03 0.03 | -4.1 4.1 0.03 | 0.03 0.00 | mit 148|0.00 0.00 0.00 -0.09 -0.07 -0.08 0.2 0.02 0.02 | -0.9 0.7 0.04 | 0.11 0.05 | ngs 80 |0.00 0.00-0.01 -0.05 -0.02 -0.36 -0.3 0.06 0.05 | -0.1 0.4 3.58 | -0.20 -0.12 | sio 153|0.00 0.00-0.01 0.16 0.06 -0.06 0.5 0.05 0.05 | 0.0 0.0 0.00 | -0.05 0.00 | Table 2.1263.5 GPS week: 1263 Day: 5 MJD: 53090.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 169|0.00 0.00 0.00 0.03 -0.07 -0.02 -0.4 0.01 0.01 | 0.1 -0.5 0.04 | 0.03 -0.01 | emr 40 |0.00 0.00 0.00 0.08 0.07 0.02 0.2 0.02 0.02 | 2485.4 24.4 0.03 | 0.07 -0.07 | esa 73 |0.00 0.00 0.00 0.02 0.04 -0.01 0.1 0.03 0.03 | 2443.9 25.5 0.06 | -0.09 -0.07 | gfz 165|0.00 0.00 0.00 0.00 -0.03 0.14 -0.3 0.02 0.02 | 0.4 -0.5 0.03 | -0.01 0.01 | igr n/a|0.00 0.00 0.00 0.01 -0.01 -0.02 -0.1 0.01 0.01 | 1.6 -0.4 0.04 | -0.01 0.00 | jpl 80 |0.00 0.01 0.00 -0.22 0.07 -0.02 0.2 0.03 0.03 | 0.1 -1.2 0.03 | 0.05 0.01 | mit 147|0.00 0.00 0.00 -0.08 -0.03 -0.10 0.2 0.03 0.02 | 0.2 -0.8 0.04 | 0.11 0.05 | ngs 80 |0.00-0.01-0.01 0.09 -0.11 -0.21 -0.2 0.07 0.06 | 0.4 -0.4 2.94 | -0.43 -0.09 | sio 153|0.00 0.00-0.01 0.20 0.10 -0.02 0.6 0.05 0.05 | 0.0 0.0 0.00 | -0.06 -0.02 | Table 2.1263.6 GPS week: 1263 Day: 6 MJD: 53091.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 169|0.00 0.00 0.00 0.02 -0.05 0.00 -0.4 0.01 0.01 | 0.8 -0.9 0.04 | 0.05 -0.04 | emr 40 |0.00 0.00 0.00 0.06 0.03 -0.01 0.3 0.02 0.02 | 2510.9 26.7 0.03 | 0.02 -0.03 | esa 73 |0.00 0.00 0.00 0.16 0.12 0.13 0.2 0.04 0.03 | 2478.1 26.5 0.06 | -0.04 -0.06 | gfz 170|0.00-0.01 0.00 -0.01 0.00 0.15 -0.2 0.02 0.02 | -0.1 0.1 0.03 | -0.01 -0.01 | igr n/a|0.00 0.00 0.00 -0.01 0.00 -0.03 -0.1 0.01 0.01 | 2.1 2.2 0.03 | 0.04 -0.02 | jpl 80 |0.00 0.00 0.00 -0.18 0.04 -0.04 0.2 0.03 0.03 | -0.1 1.3 0.03 | -0.03 0.02 | mit 148|0.00 0.00 0.00 -0.09 0.01 -0.14 0.2 0.03 0.02 | -1.5 0.6 0.04 | 0.08 -0.01 | ngs 80 |0.00 0.00-0.02 0.03 -0.33 -0.28 -0.2 0.08 0.07 | -0.1 0.1 3.17 | -0.24 0.42 | sio 153|0.00 0.00 0.00 0.07 -0.02 -0.11 0.6 0.05 0.05 | 0.0 0.0 0.00 | -0.04 -0.04 | 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. "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","MD" stands for median of the centre's satellite RMS. Units: cm. Table 3.1263.0 GPS week: 1263 Day: 0 MJD: 53085.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------|------------------------------------------|------------------------------------------ 1 | 1 2 3 2 1 2 1 5 4 1 | 2 3 4 2 3 3 3 6 6 3 3E | 3 3 6 3 2 3 11 16 9 2 | 3 4 5 3 3 4 10 12 10 4 4 | 1 2 3 2 1 2 3 7 3 1 | 2 3 4 3 2 3 4 6 5 2 5E | 1 2 2 2 1 2 4 6 4 1 | 5 5 5 6 5 5 6 9 6 5 6E | 3 3 3 2 1 3 5 5 5 1 | 4 7 4 4 4 4 8 7 9 5 7 | 2 2 3 2 1 2 3 4 3 1 | 3 3 4 3 3 4 5 5 5 3 8 | 2 3 4 2 1 1 1 5 6 1 | 6 5 7 5 5 5 6 6 9 5 9 | 1 2 2 1 1 2 3 5 3 1 | 5 5 5 4 5 5 6 6 5 5 10E | 1 2 3 3 1 1 2 5 5 1 | 3 3 3 4 3 3 4 5 4 3 11 | 2 2 3 2 1 4 2 6 7 1 | 2 4 4 3 3 3 3 6 6 2 13 | 1 2 4 2 1 6 3 4 6 1 | 3 4 5 3 3 3 4 5 5 3 14 | 2 2 2 2 2 5 2 7 5 1 | 2 3 3 2 3 3 4 8 6 2 15 | 2 2 3 2 1 3 3 5 3 1 | 4 3 5 3 3 3 5 7 5 3 16E | 1 2 3 2 1 5 2 5 6 1 | 2 2 3 2 2 2 2 6 3 2 17 | 1 2 3 2 1 1 2 4 6 1 | 3 3 4 2 3 3 4 6 6 3 18E | 1 2 3 2 1 4 3 5 5 1 | 2 3 4 2 2 2 3 4 3 2 20E | 1 1 2 2 1 4 2 6 3 1 | 2 3 3 2 2 3 3 6 4 2 21 | 2 2 3 2 2 5 3 6 6 1 | 3 4 4 3 4 3 4 7 6 3 22E | 1 1 4 1 1 3 2 8 5 1 | 3 4 6 3 3 3 3 7 4 3 24 | 2 2 3 2 1 1 2 5 8 1 | 3 4 4 3 3 3 5 6 8 3 25E | 1 2 2 1 2 2 2 6 4 1 | 5 5 6 4 5 5 5 7 8 5 26 | 1 2 4 2 1 2 2 7 3 1 | 3 3 4 2 2 3 4 5 5 3 27 | 2 3 4 2 1 2 2 6 7 1 | 5 5 7 4 5 5 5 7 10 5 28E | 1 1 3 3 1 4 2 8 6 1 | 2 3 3 2 2 2 3 8 4 2 29 | 2 2 3 2 1 2 2 7 3 1 | 4 5 5 4 4 5 5 5 6 4 30E | 2 3 3 2 2 2 6 5 4 1 | 6 8 7 8 7 7 9 9 8 7 31E | 2 1 4 2 1 1 4 6 5 1 | 3 3 5 3 3 3 6 5 5 3 ------|------------------------------------------|------------------------------------------ RMS | 2 2 3 2 1 3 4 6 5 |T 3 4 4 3 3 3 5 6 6 3 WRMS | 2 2 3 2 1 3 2 5 5 |NE 3 3 4 2 3 3 4 6 6 3 MEDI | 1 2 3 2 1 2 2 6 5 |MD 3 4 4 3 3 3 4 6 6 3 Table 3.1263.1 GPS week: 1263 Day: 1 MJD: 53086.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------|------------------------------------------|------------------------------------------ 1 | 1 2 3 2 1 3 1 5 5 1 | 3 3 4 2 3 3 3 5 6 3 3 | 2 2 3 1 1 1 2 5 4 1 | 3 3 4 3 3 3 4 5 5 3 4 | 2 3 4 2 1 2 3 4 3 1 | 3 3 3 3 3 2 5 4 4 3 5E | 1 2 4 2 1 2 4 7 3 1 | 5 7 6 6 6 5 7 8 6 6 6 | 3 3 3 2 1 3 4 7 5 1 | 4 5 5 4 4 4 8 9 9 4 7 | 2 3 4 2 1 2 2 5 4 1 | 3 4 4 3 3 3 4 5 5 3 8 | 2 2 4 2 1 2 1 6 6 1 | 5 4 6 4 4 4 4 7 8 4 X9 | 1 2 2 1 2 --- 2 6 2 1 | 3 4 4 3 3 --- 4 7 4 3 10E | 1 2 3 3 1 1 3 5 3 1 | 2 3 3 3 2 2 2 5 3 2 11 | 2 3 3 2 2 5 2 7 7 1 | 3 4 4 3 3 4 4 8 6 3 13 | 1 2 4 2 1 7 3 4 5 1 | 2 4 4 3 3 6 4 6 4 2 14 | 1 2 3 2 2 5 3 4 6 1 | 3 4 3 3 3 3 4 5 6 3 15 | 2 2 4 1 1 3 2 7 2 1 | 4 4 4 3 3 4 4 7 4 3 16E | 1 1 2 2 1 5 2 5 4 1 | 3 4 3 3 3 3 3 5 3 2 17 | 1 2 4 2 1 1 2 6 4 1 | 2 3 4 3 3 2 3 6 4 2 18E | 1 2 2 2 1 4 2 7 4 1 | 3 4 3 4 3 3 4 6 4 3 20E | 1 2 3 1 1 5 2 5 4 1 | 2 3 3 2 2 3 3 5 4 2 21 | 1 2 3 2 2 6 3 5 6 1 | 2 4 5 3 3 4 3 6 5 2 22E | 1 2 3 2 1 4 2 6 4 1 | 3 4 3 3 3 3 3 6 4 3 24 | 2 1 2 2 1 2 2 7 5 1 | 3 4 4 3 3 3 4 8 6 3 25 | 1 2 3 2 2 2 2 6 4 1 | 4 5 4 3 3 4 4 6 5 3 26 | 2 2 2 2 1 1 2 7 3 1 | 3 4 3 2 2 2 4 6 4 2 27 | 2 2 4 2 1 1 1 5 7 1 | 5 5 6 4 4 4 5 7 9 4 28E | 1 2 4 2 2 4 2 5 6 1 | 4 4 5 3 3 3 4 6 5 3 29 | 2 2 5 2 1 2 3 6 3 1 | 5 5 4 4 4 4 5 8 6 4 30E | 2 6 6 3 2 3 5 10 3 2 | 7 10 8 8 8 8 10 13 10 8 31 | 2 2 4 2 1 1 4 6 4 1 | 3 3 5 3 3 4 5 5 4 3 ------|------------------------------------------|------------------------------------------ RMS | 2 2 3 2 1 3 3 6 4 |T 3 4 4 3 3 3 4 6 5 3 WRMS | 2 2 3 2 1 3 2 5 4 |NE 3 4 4 3 3 3 4 6 5 2 MEDI | 1 2 3 2 1 3 2 6 4 |MD 3 4 4 3 3 3 4 6 5 3 Table 3.1263.2 GPS week: 1263 Day: 2 MJD: 53087.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------|------------------------------------------|------------------------------------------ 1 | 1 2 2 2 1 2 2 7 5 1 | 3 3 4 2 3 3 3 7 6 2 3 | 2 2 3 2 1 1 2 6 3 1 | 3 4 4 3 3 3 4 6 5 3 4 | 1 2 2 1 1 2 2 5 3 1 | 3 3 4 3 2 3 4 4 3 3 5E | 2 2 2 2 1 2 4 8 3 1 | 5 6 6 6 5 5 6 7 5 5 6 | 2 3 4 2 1 3 4 13 4 1 | 3 3 5 4 3 3 7 13 7 4 7 | 2 2 3 2 1 2 2 5 3 1 | 3 4 4 3 3 3 5 5 4 3 8 | 2 3 3 2 1 2 2 7 6 1 | 5 4 6 4 4 4 5 7 9 5 9 | 1 2 2 1 1 2 2 5 2 1 | 4 5 5 4 4 5 5 6 5 4 10E | 2 2 3 2 1 1 2 4 4 1 | 2 3 2 2 2 2 3 4 3 2 11 | 2 3 3 2 1 5 2 5 6 1 | 3 4 5 3 3 3 4 6 6 3 13 | 1 2 4 2 2 6 3 5 6 1 | 3 4 5 4 4 4 4 6 5 3 14 | 2 2 2 1 2 5 2 7 6 1 | 2 3 2 2 2 3 4 7 6 2 15 | 2 2 3 2 1 3 2 9 3 1 | 3 3 3 3 3 2 3 8 4 2 16E | 2 1 2 2 1 5 2 4 5 1 | 3 3 3 3 2 3 2 4 3 2 17 | 1 2 2 2 1 1 2 7 3 1 | 3 3 4 2 3 3 4 7 4 3 18E | 1 2 2 2 1 5 2 8 3 1 | 3 4 4 3 3 3 3 5 3 3 20E | 1 2 3 2 1 5 2 5 3 1 | 3 3 4 3 3 3 3 5 3 3 21 | 1 2 3 2 1 5 3 6 7 1 | 3 3 4 3 3 3 4 5 6 3 22E | 1 2 3 1 1 5 2 7 4 1 | 3 4 5 3 3 4 3 6 4 3 24 | 2 1 2 2 1 1 2 7 4 1 | 6 6 6 6 5 5 6 6 6 5 25 | 1 2 2 2 2 2 2 7 5 1 | 4 5 5 4 4 4 4 7 6 4 26 | 1 1 3 2 1 2 3 7 2 1 | 3 4 3 2 3 3 4 5 5 3 27 | 2 2 3 2 1 2 2 6 7 1 | 4 5 6 4 4 5 5 9 10 5 28E | 1 2 3 2 1 5 2 5 6 1 | 3 3 3 2 3 2 3 5 4 2 29 | 2 2 4 2 2 2 3 7 3 1 | 5 5 5 4 4 5 5 6 5 4 30E | 2 3 3 2 2 3 5 6 3 1 | 6 7 7 7 7 7 9 10 9 7 31 | 2 2 3 2 1 1 2 5 4 1 | 3 4 5 3 3 3 5 5 4 3 ------|------------------------------------------|------------------------------------------ RMS | 2 2 3 2 1 3 2 7 4 |T 3 4 4 3 3 3 4 6 5 3 WRMS | 2 2 3 2 1 3 2 5 3 |NE 3 4 4 3 3 3 4 6 5 3 MEDI | 2 2 3 2 1 2 2 6 4 |MD 3 4 4 3 3 3 4 6 5 3 Table 3.1263.3 GPS week: 1263 Day: 3 MJD: 53088.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------|------------------------------------------|------------------------------------------ 1 | 1 1 2 2 1 2 1 6 6 1 | 3 3 3 3 3 4 4 4 7 3 3 | 1 1 3 2 1 1 1 7 4 1 | 4 4 6 3 4 4 5 6 5 3 4 | 1 2 2 1 1 2 3 5 3 1 | 2 2 3 2 2 2 4 5 3 2 5E | 2 2 3 2 1 2 6 7 3 1 | 6 6 7 7 7 7 10 10 7 7 6 | 2 2 3 2 2 4 4 9 5 1 | 4 4 4 4 5 3 7 11 8 4 7 | 1 2 3 3 1 2 2 5 5 1 | 3 3 3 3 3 4 4 5 5 3 8 | 2 2 3 2 1 2 1 5 6 1 | 5 5 5 4 4 5 5 5 8 4 9 | 1 2 2 1 1 2 2 5 4 1 | 4 5 5 4 4 4 5 6 5 4 10E | 1 1 3 2 1 1 4 7 4 1 | 3 3 4 4 3 3 3 6 3 3 11 | 2 3 2 2 1 4 2 5 8 1 | 3 4 4 3 3 3 4 6 7 3 13 | 1 2 4 2 1 6 3 6 6 1 | 3 4 4 2 3 3 4 6 6 2 14 | 1 2 3 1 2 5 2 7 7 1 | 2 4 3 2 3 3 4 7 5 2 15 | 2 1 2 2 1 2 2 9 2 1 | 3 3 4 3 3 3 4 8 4 3 16E | 1 2 4 1 2 7 2 5 5 1 | 3 4 4 3 3 5 4 4 5 3 17 | 2 5 3 2 1 2 2 6 2 1 | 3 4 3 3 3 3 3 6 3 2 18E | 1 2 4 1 2 5 2 7 5 1 | 2 3 4 3 2 3 3 5 3 2 20E | 1 2 2 2 1 4 2 6 4 1 | 3 4 3 4 3 3 4 5 5 3 21 | 1 2 3 2 2 6 3 6 6 1 | 3 4 3 3 3 3 4 5 5 2 22E | 2 2 4 1 1 4 2 7 5 1 | 3 4 5 3 3 3 3 7 5 3 24 | 2 2 2 2 1 2 2 6 4 1 | 5 5 5 5 5 5 5 8 6 4 25 | 1 2 2 1 1 2 2 5 4 1 | 4 4 4 4 4 4 4 7 7 4 26 | 1 1 4 2 1 2 2 6 3 1 | 3 3 4 2 3 3 4 6 4 3 27 | 1 2 3 2 1 2 2 5 8 1 | 5 5 6 4 4 5 5 6 9 5 28E | 1 2 5 2 2 5 2 5 6 1 | 4 4 5 4 4 4 4 5 6 3 29 | 2 2 4 2 1 2 7 6 3 1 | 8 9 8 9 8 9 8 10 10 8 30E | 2 3 4 2 2 2 4 5 3 1 | 8 9 9 10 8 9 9 10 10 9 31 | 1 2 4 1 1 1 3 6 5 1 | 3 4 5 3 3 3 4 5 5 3 ------|------------------------------------------|------------------------------------------ RMS | 1 2 3 2 1 3 3 6 5 |T 4 4 4 4 4 4 5 6 6 3 WRMS | 1 2 3 2 1 3 2 5 4 |NE 4 4 4 4 4 4 4 6 6 3 MEDI | 1 2 3 2 1 2 2 6 5 |MD 3 4 4 3 3 3 4 6 5 3 Table 3.1263.4 GPS week: 1263 Day: 4 MJD: 53089.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------|------------------------------------------|------------------------------------------ 1 | 1 2 2 2 1 2 2 6 5 1 | 3 4 4 2 2 3 3 4 6 3 3 | 2 1 2 2 1 2 2 6 3 1 | 4 4 4 3 4 4 5 6 5 4 4 | 2 1 3 2 1 1 2 4 3 1 | 2 3 3 3 2 3 4 4 4 3 5E | 2 2 2 1 2 2 2 5 3 1 | 5 6 6 5 6 6 5 8 6 5 6 | 2 3 3 2 1 3 3 8 5 1 | 4 4 5 4 4 4 7 10 8 4 7 | 1 2 3 1 1 2 2 4 4 1 | 4 4 4 4 3 4 5 5 5 4 8 | 2 2 3 2 1 2 2 5 7 1 | 4 5 5 3 4 4 5 6 9 4 9 | 2 2 2 1 1 2 2 4 3 1 | 4 5 5 4 4 5 5 5 5 4 10E | 2 1 3 1 2 2 3 5 2 1 | 3 3 3 3 3 3 3 4 3 3 11 | 2 2 3 2 1 5 2 6 8 1 | 3 4 4 3 3 4 4 6 7 3 13 | 2 2 4 2 1 6 3 6 6 1 | 3 3 5 3 3 3 4 5 5 3 14 | 2 2 3 1 2 5 3 6 6 1 | 3 3 3 2 3 3 4 6 5 2 15 | 2 1 2 2 1 2 2 8 3 1 | 3 3 4 3 3 3 3 7 4 3 16E | 2 2 4 2 1 6 2 5 5 1 | 3 4 5 3 3 3 3 5 5 3 17 | 2 2 2 2 2 1 2 5 2 1 | 3 3 3 3 3 3 4 6 4 3 18E | 2 2 3 2 1 5 3 8 4 1 | 3 3 4 3 3 3 3 5 3 2 X19 | 1 --- --- --- --- --- --- --- --- 0 | 14 --- --- --- --- --- --- --- --- 14 20E | 1 2 3 2 1 4 2 5 4 1 | 3 3 3 2 3 3 3 6 5 3 21 | 2 2 3 2 1 6 3 4 6 1 | 3 4 4 3 3 4 4 4 4 3 22E | 1 2 3 2 1 4 2 8 4 1 | 3 4 3 3 3 4 3 8 5 3 24 | 2 2 2 2 2 2 2 5 4 1 | 4 4 4 3 3 4 5 7 5 4 25 | 2 2 2 2 1 2 2 5 4 1 | 4 4 5 3 3 4 4 5 6 4 26 | 2 1 2 2 2 1 3 8 3 1 | 3 3 4 2 3 3 5 6 5 3 27 | 2 2 3 2 1 2 2 4 7 1 | 4 4 5 4 4 5 5 7 10 4 28E | 1 2 3 2 1 5 2 5 7 1 | 3 3 3 3 3 3 3 3 6 3 29 | 2 1 3 2 1 2 2 7 3 1 | 6 6 5 6 5 6 5 8 7 5 30E | 3 2 4 2 1 2 3 4 3 1 | 7 8 8 8 8 8 9 9 9 8 31 | 2 1 5 2 1 1 2 4 5 1 | 3 4 5 3 4 4 4 5 5 3 ------|------------------------------------------|------------------------------------------ RMS | 2 2 3 2 1 3 2 6 5 |T 4 4 4 3 3 4 4 6 5 4 WRMS | 2 2 3 2 1 3 2 5 5 |NE 5 3 4 3 3 3 4 6 5 5 MEDI | 2 2 3 2 1 2 2 5 4 |MD 3 4 4 3 3 4 4 6 5 3 Table 3.1263.5 GPS week: 1263 Day: 5 MJD: 53090.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------|------------------------------------------|------------------------------------------ X1 | 1 1 3 1 1 --- 2 6 5 1 | 3 3 3 2 3 --- 4 5 6 2 3 | 1 2 3 2 2 2 2 8 3 1 | 3 4 4 2 3 3 4 6 5 3 4 | 1 1 3 2 1 2 2 7 3 1 | 2 3 3 2 2 2 3 6 4 2 5E | 1 1 3 2 1 2 5 7 3 1 | 7 7 8 7 7 7 9 11 8 7 6 | 2 2 3 2 1 3 3 7 5 1 | 2 4 4 4 3 4 6 8 8 4 7 | 1 2 3 1 1 2 3 6 4 1 | 2 3 2 3 2 3 4 5 5 2 8 | 2 2 2 2 1 2 2 4 7 1 | 4 4 4 3 4 3 5 5 9 4 9 | 1 2 1 2 1 2 3 7 2 1 | 4 5 4 3 4 4 5 6 4 4 10E | 2 1 3 2 1 1 3 7 4 1 | 3 3 3 3 2 2 3 5 4 2 11 | 2 2 3 2 1 4 2 9 9 1 | 3 4 4 3 3 3 3 7 7 3 13 | 1 2 6 1 1 6 3 6 6 1 | 3 3 6 3 3 3 3 4 5 2 14 | 1 2 3 1 1 5 3 7 6 1 | 2 4 3 3 3 3 4 6 5 2 15 | 2 1 4 2 1 2 2 10 3 1 | 3 3 4 3 2 2 3 6 4 2 16E | 1 1 5 2 2 5 2 8 4 1 | 3 4 4 3 2 3 4 6 3 2 17 | 1 1 2 2 2 1 2 6 2 1 | 2 3 3 2 2 3 3 7 3 2 X18E | 1 2 4 1 1 --- 2 6 5 1 | 4 5 4 4 4 --- 4 5 4 3 X19 | 1 --- --- --- --- --- --- --- --- 0 | 11 --- --- --- --- --- --- --- --- 11 20E | 1 1 4 1 1 4 2 7 5 1 | 3 3 4 3 2 3 3 6 5 2 21 | 1 2 3 2 1 5 3 5 6 1 | 3 4 4 3 3 3 3 6 4 2 22E | 1 2 6 2 1 4 2 11 6 1 | 3 4 6 3 3 4 4 8 5 3 24 | 2 1 2 2 1 1 2 8 5 1 | 4 5 4 4 4 4 6 11 7 5 25 | 1 1 2 1 1 3 2 7 5 1 | 4 4 4 3 3 4 4 6 5 4 26 | 2 2 3 2 1 1 2 7 3 1 | 2 3 3 3 2 3 4 4 5 2 27 | 2 2 2 2 1 2 2 5 8 1 | 4 5 4 4 4 4 5 5 10 4 28E | 1 1 3 2 1 5 2 6 7 1 | 3 3 3 3 3 3 3 6 6 3 29 | 2 1 3 2 1 2 3 8 3 1 | 5 6 5 5 5 5 6 7 6 5 30E | 2 2 3 2 1 3 3 6 3 1 | 8 9 8 9 8 8 10 11 10 9 31 | 2 2 7 1 1 2 2 8 3 1 | 3 3 5 2 3 2 3 7 4 2 ------|------------------------------------------|------------------------------------------ RMS | 1 2 3 2 1 3 3 7 5 |T 4 4 4 3 3 3 4 6 5 4 WRMS | 1 2 3 2 1 3 2 6 5 |NE 4 4 4 3 3 3 4 6 5 4 MEDI | 1 2 3 2 1 2 2 7 5 |MD 3 4 4 3 3 3 4 6 5 3 Table 3.1263.6 GPS week: 1263 Day: 6 MJD: 53091.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl mit ngs sio IGS | cod emr esa gfz igr jpl mit ngs sio IGS ------|------------------------------------------|------------------------------------------ 1 | 1 1 3 2 1 2 2 8 5 1 | 4 4 5 4 4 4 5 4 6 4 3 | 1 1 3 1 2 2 2 7 3 1 | 4 5 5 3 4 4 5 6 5 4 4 | 1 2 3 2 1 2 2 7 3 1 | 3 4 4 3 2 2 3 7 3 3 5 | 2 2 6 2 1 2 5 9 3 1 | 7 8 8 8 8 7 8 10 8 7 6 | 2 2 3 2 2 3 4 7 4 1 | 4 5 6 4 4 3 7 6 7 4 7 | 1 2 3 2 1 1 3 10 3 1 | 4 4 4 3 4 4 5 9 5 4 8 | 1 2 3 2 1 2 2 7 6 1 | 5 5 7 4 5 5 6 6 10 5 9 | 1 2 3 1 1 2 2 8 2 1 | 6 5 6 4 5 5 6 6 5 5 10E | 1 1 3 2 1 1 3 9 2 1 | 4 4 4 4 3 3 3 6 3 3 11 | 2 2 3 2 1 4 2 7 9 1 | 3 5 5 3 3 3 4 7 8 3 13 | 1 2 4 2 1 5 3 6 6 1 | 3 4 5 3 4 3 4 5 6 3 14 | 1 2 3 1 1 5 3 8 7 1 | 3 4 3 3 3 3 4 6 6 3 15 | 1 1 3 1 1 3 2 7 3 1 | 4 4 3 3 3 3 3 6 4 3 16E | 1 1 3 1 2 6 2 9 5 1 | 3 3 4 3 2 3 3 7 4 2 17 | 1 2 3 2 1 2 2 8 3 1 | 3 3 5 3 3 3 4 8 4 3 X18E | 1 1 3 1 1 --- 2 7 5 1 | 2 3 4 2 2 --- 2 6 2 2 X19 | 1 --- --- --- --- --- --- --- --- 0 | 14 --- --- --- --- --- --- --- --- 14 20E | 1 1 3 1 1 4 2 7 5 1 | 3 4 4 3 3 3 4 6 5 3 21 | 1 2 3 2 1 6 3 7 7 1 | 3 4 4 3 4 3 4 7 5 3 X22E | 2 2 6 1 1 --- 3 11 4 1 | 3 3 6 3 3 --- 3 8 5 2 24 | 1 2 3 2 1 2 2 9 5 1 | 6 5 6 5 5 5 5 9 6 5 25 | 1 2 3 1 1 2 3 5 4 1 | 5 4 6 4 4 4 5 8 7 4 26 | 1 2 3 2 1 2 2 11 3 1 | 3 4 4 2 3 3 4 6 5 3 27 | 1 2 3 2 1 2 2 7 7 1 | 5 5 6 4 5 5 5 7 11 5 28E | 1 2 5 3 1 5 2 6 6 1 | 3 3 5 3 3 3 3 7 5 3 29 | 2 2 4 2 1 2 6 10 3 1 | 6 6 7 7 6 7 6 9 8 6 30E | 2 2 2 2 2 3 3 9 3 1 | 11 11 12 12 11 11 12 14 12 11 31 | 2 1 8 2 2 2 2 7 6 1 | 4 4 8 3 4 3 5 6 5 4 ------|------------------------------------------|------------------------------------------ RMS | 1 2 4 2 1 3 3 8 5 |T 5 4 5 4 4 4 5 7 6 5 WRMS | 1 2 3 2 1 3 2 7 5 |NE 5 4 5 3 4 3 4 7 6 5 MEDI | 1 2 3 2 1 2 2 7 4 |MD 4 4 5 3 4 3 4 7 5 4 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. U - Station Used in centre's solution (at least one day). Units: centimetres. Table 4.1263 GPS week: 1263 MJD: 53085.0-53091.0 CENT| CLK EPO | BRUS | TOW2 | ----|----------|----------------|----------------| cod | cod 2620 |U 1 2 4 |U 1 2 5 | emr | emr 2581 | 2 2 6 | 2 2 8 | esa | esa 2592 | 3 2 6 |U 2 2 8 | gfz | gfz 2561 |U 2 2 5 |U 2 3 7 | igr | igr 2589 | 2 2 5 | 2 2 7 | igs | igs 2590 | 2 2 5 | 2 2 7 | jpl | jpl 2499 | 3 3 6 |U 2 3 8 | mit | mit 2592 |U 3 3 7 |U 3 3 8 | 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: centimetres. Table 5.1263.0 GPS week: 1263 Day: 0 MJD: 53085.0 CENT| CLK EPO | BRUS | TOW2 | ----|----------|----------------|----------------| cod | cod 2592 | 1 2 4 | 1 2 5 | emr | emr 2580 | 3 3 8 | 2 3 9 | esa | esa 2592 | 3 4 8 | 2 2 8 | gfz | gfz 2561 | 2 4 7 | 2 2 7 | igr | igr 2587 | 2 3 6 | 2 2 8 | igs | igs 2592 | 2 3 7 | 2 2 8 | jpl | jpl 2578 | 4 4 9 | 2 3 9 | mit | mit 2592 | 5 4 12 | 3 2 8 | Table 5.1263.1 GPS week: 1263 Day: 1 MJD: 53086.0 CENT| CLK EPO | BRUS | TOW2 | ----|----------|----------------|----------------| cod | cod 2590 | 1 2 4 | 1 2 4 | emr | emr 2580 | 2 3 6 | 2 2 9 | esa | esa 2592 | 2 2 6 | 2 2 10 | gfz | gfz 2561 | 2 2 4 | 2 3 9 | igr | igr 2583 | 2 2 5 | 2 2 8 | igs | igs 2592 | 2 2 4 | 2 2 8 | jpl | jpl 2563 | 3 2 4 | 2 3 9 | mit | mit 2592 | 2 3 7 | 3 2 11 | Table 5.1263.2 GPS week: 1263 Day: 2 MJD: 53087.0 CENT| CLK EPO | BRUS | TOW2 | ----|----------|----------------|----------------| cod | cod 2590 | 1 2 4 | 1 2 4 | emr | emr 2580 | 1 2 4 | 2 3 9 | esa | esa 2592 | 3 3 6 | 2 2 9 | gfz | gfz 2560 | 1 2 4 | 2 3 8 | igr | igr 2592 | 2 3 5 | 2 3 9 | igs | igs 2588 | 1 2 4 | 2 3 8 | jpl | jpl 2563 | 2 3 4 | 2 3 9 | mit | mit 2592 | 2 2 6 | 2 3 10 | Table 5.1263.3 GPS week: 1263 Day: 3 MJD: 53088.0 CENT| CLK EPO | BRUS | TOW2 | ----|----------|----------------|----------------| cod | cod 2592 | 1 2 4 | 1 2 4 | emr | emr 2580 | 2 2 5 | 2 2 7 | esa | esa 2592 | 3 2 7 | 2 2 7 | gfz | gfz 2561 | 2 2 4 | 2 2 6 | igr | igr 2592 | 2 2 5 | 2 2 5 | igs | igs 2588 | 2 2 4 | 2 2 6 | jpl | jpl 2564 | 2 3 5 | 2 2 7 | mit | mit 2592 | 4 2 6 | 3 3 8 | Table 5.1263.4 GPS week: 1263 Day: 4 MJD: 53089.0 CENT| CLK EPO | BRUS | TOW2 | ----|----------|----------------|----------------| cod | cod 2602 | 1 2 4 | 1 2 7 | emr | emr 2579 | 2 2 5 | 2 3 9 | esa | esa 2591 | 3 2 5 | 2 2 9 | gfz | gfz 2560 | 2 2 4 | 2 3 8 | igr | igr 2585 | 2 2 6 | 2 2 8 | igs | igs 2588 | 2 2 4 | 2 3 8 | jpl | jpl 2557 | 2 3 6 | 2 3 10 | mit | mit 2592 | 2 2 5 | 2 3 9 | Table 5.1263.5 GPS week: 1263 Day: 5 MJD: 53090.0 CENT| CLK EPO | BRUS | TOW2 | ----|----------|----------------|----------------| cod | cod 2686 | 1 2 4 | 1 1 4 | emr | emr 2584 | 2 2 5 | 2 2 7 | esa | esa 2592 | 3 2 7 | 2 2 7 | gfz | gfz 2562 | 2 2 5 | 2 2 6 | igr | igr 2592 | 2 2 5 | 2 2 5 | igs | igs 2592 | 2 2 5 | 2 2 6 | jpl | jpl 2387 | 4 4 9 | 2 3 7 | mit | mit 2592 | 2 3 6 | 2 3 6 | Table 5.1263.6 GPS week: 1263 Day: 6 MJD: 53091.0 CENT| CLK EPO | BRUS | TOW2 | ----|----------|----------------|----------------| cod | cod 2688 | 1 2 3 | 1 1 4 | emr | emr 2584 | 2 2 4 | 2 2 6 | esa | esa 2592 | 2 2 5 | 2 2 8 | gfz | gfz 2564 | 2 2 4 | 2 2 6 | igr | igr 2592 | 2 2 4 | 2 2 6 | igs | igs 2592 | 1 2 4 | 2 2 6 | jpl | jpl 2344 | 2 1 4 | 2 2 6 | mit | mit 2592 | 2 2 3 | 2 2 6 | 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 (10**-5") Ypole,Yrt: y pole and y pole rate (10**-5"/day) LOD: Length Of Day (us) AC LOD BIAS: 21-day mean LOD bias with respect to Bulletin A (us) AC LOD BIAS RMS: RMS of AC LOD BIAS (us) FLAG: "u" (used), "x" (excluded), "-" (no submission) for Xpole, Ypole, Xrt, Yrt and LOD Table 6.1263 GPS week: 1263 MJD: 53085.500-53091.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | 0 -1 -2 -4 -2 | -20 25 | 2 2 4 4 9 | 2 emr uuuuu | 6 -3 14 10 10 | -24 28 | 3 2 5 6 8 | 4 esa uuuuu | 2 9 -1 -2 -14 | 78 80 | 3 3 8 7 10 | 4 gfz uuuuu | -1 6 -3 -3 -4 | 12 22 | 1 2 7 3 9 | 6 igr xxxxx | 2 0 -2 -12 -7 | -7 15 | 3 3 8 9 10 | 4 irf xxxxx | -1 2 -3 -2 0 | -9 21 | 1 1 4 4 4 | 6 jpl uuuuu | -2 0 -6 2 -3 | 29 33 | 2 3 11 9 14 | 2 mit uuuuu | -5 -10 -3 0 0 | 32 35 | 2 2 10 7 5 | 3 ngs xxxxx | 5 25 -17 -10 51 | -36 64 | 22 11 33 38 46 | 20 sio uuuuu | 0 6 -7 -8 -1 | 19 23 | 5 2 16 10 5 | 4 Table 7: Earth Orientation Parameters daily summary. Daily Centre ERP, ERP Rates and LOD differences with respect to IGS combined values. Xpole,Xrt: x pole and x pole rate (10**-5") Ypole,Yrt: y pole and y pole rate (10**-5"/day) LOD: Length Of Day (us) AC LOD BIAS: 21-day mean LOD bias with respect to Bulletin A (us) AC LOD BIAS RMS: RMS of AC LOD BIAS (us) FLAG: "u" (used), "x" (excluded), "-" (no submission) for Xpole, Ypole, Xrt, Yrt and LOD Table 7.1263.0 GPS week: 1263 Day: 0 MJD: 53085.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | -2 0 1 -9 7 | -18 22 emr uuuuu | 5 -3 20 19 3 | -20 26 esa uuuuu | -3 6 15 1 -14 | 85 86 gfz uuuuu | 1 6 -12 -4 -20 | 24 33 igr xxxxx | 0 0 -7 -12 -1 | 0 14 irf xxxxx | 1 2 0 -1 -7 | 3 28 jpl uuuuu | -4 0 -20 4 1 | 31 35 mit uuuuu | -2 -11 -9 -4 0 | 37 39 ngs xxxxx | 13 35 1 -19 100 | -66 74 sio uuuuu | 8 9 -5 -12 2 | 26 31 Table 7.1263.1 GPS week: 1263 Day: 1 MJD: 53086.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | -2 -1 -1 1 13 | -22 24 emr uuuuu | 8 -6 10 10 -1 | -26 28 esa uuuuu | 3 9 -2 0 0 | 80 82 gfz uuuuu | -1 5 2 -7 -13 | 16 26 igr xxxxx | 3 -1 12 -18 0 | -4 13 irf xxxxx | -2 2 -2 -3 -5 | -5 23 jpl uuuuu | 0 5 -8 -6 9 | 29 33 mit uuuuu | -5 -9 6 6 -4 | 33 35 ngs xxxxx | 13 18 -1 -20 89 | -55 69 sio uuuuu | 2 4 -26 -13 -6 | 22 27 Table 7.1263.2 GPS week: 1263 Day: 2 MJD: 53087.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | 1 0 -4 0 -7 | -22 24 emr uuuuu | 8 -5 14 4 17 | -28 29 esa uuuuu | 3 8 -10 -4 -19 | 80 82 gfz uuuuu | -1 8 2 0 -7 | 11 19 igr xxxxx | 5 1 -3 -17 -15 | -6 12 irf xxxxx | 0 1 -2 5 1 | -10 20 jpl uuuuu | -4 -3 12 9 14 | 29 33 mit uuuuu | -7 -10 -16 -6 -10 | 32 34 ngs xxxxx | 21 14 6 10 94 | -43 63 sio uuuuu | -2 4 17 0 5 | 19 23 Table 7.1263.3 GPS week: 1263 Day: 3 MJD: 53088.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | 1 -2 -4 -4 -4 | -24 26 emr uuuuu | 10 -4 6 2 4 | -28 29 esa uuuuu | 0 10 -3 9 -21 | 78 80 gfz uuuuu | -1 8 6 1 6 | 6 14 igr xxxxx | 3 -4 -12 0 -18 | -10 16 irf xxxxx | -2 2 -9 -1 1 | -15 17 jpl uuuuu | -1 1 -8 -3 -3 | 26 28 mit uuuuu | -8 -14 8 2 4 | 28 30 ngs xxxxx | 14 20 -27 3 32 | -31 60 sio uuuuu | -10 8 -24 -7 -8 | 15 16 Table 7.1263.4 GPS week: 1263 Day: 4 MJD: 53089.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | -1 -4 -8 -3 -5 | -20 26 emr uuuuu | 8 -1 19 10 19 | -23 29 esa uuuuu | 4 13 2 -4 -11 | 77 79 gfz uuuuu | -3 7 -1 -4 -4 | 9 21 igr xxxxx | 4 3 -3 -7 -15 | -9 16 irf xxxxx | -2 0 0 -7 5 | -12 20 jpl uuuuu | -2 -3 0 5 -4 | 30 34 mit uuuuu | -6 -11 -15 0 0 | 31 36 ngs xxxxx | 11 20 11 -4 42 | -25 62 sio uuuuu | -2 4 7 -10 -1 | 18 22 Table 7.1263.5 GPS week: 1263 Day: 5 MJD: 53090.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | 0 0 3 -4 -8 | -19 25 emr uuuuu | 6 -4 18 11 16 | -21 28 esa uuuuu | 6 12 -5 -14 -29 | 76 78 gfz uuuuu | -2 3 -12 -1 4 | 9 21 igr xxxxx | -1 4 -4 -4 -6 | -11 17 irf xxxxx | -1 3 -10 -1 3 | -11 20 jpl uuuuu | -3 -2 -17 15 -26 | 31 35 mit uuuuu | -6 -9 4 -9 4 | 31 36 ngs xxxxx | 8 46 -24 40 28 | -18 61 sio uuuuu | 1 9 -16 7 3 | 18 23 Table 7.1263.6 GPS week: 1263 Day: 6 MJD: 53091.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | 2 -4 -2 -6 -10 | -19 26 emr uuuuu | 1 0 14 11 13 | -19 26 esa uuuuu | 3 6 -4 0 -2 | 72 75 gfz uuuuu | -2 3 -5 -1 2 | 10 21 igr xxxxx | -1 -2 4 -26 10 | -12 19 irf xxxxx | -2 2 0 -4 2 | -10 19 jpl uuuuu | -4 5 -5 -9 -15 | 29 35 mit uuuuu | -1 -6 -2 12 5 | 30 35 ngs xxxxx | -44 25 -84 -84 -26 | -12 57 sio uuuuu | 1 6 -1 -23 0 | 18 22