Delivered-To: igsreport@igscb.jpl.nasa.gov To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-11498] Wk 1276 IGS Final Orbits Message-Id: <20040709074627.779834F738@kg20.gfz-potsdam.de> Date: Fri, 9 Jul 2004 09:46:27 +0200 (CEST) From: igsacc@gfz-potsdam.de (Gerd Gendt.) Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 09 Jul 00:47:25 PDT 2004 Message Number 11498 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam Final IGS Orbit Combination - Week 1276 (Jun 20, 2004 - Jun 26, 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 (IGS12767.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: IGS12760-6.SP3 IGS GPS ephemeris files for days 0-6, week 1276 in SP3 format. IGS12767.ERP Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. IGS12767.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 | COD | 4 SANT 0 | ESA | 4 ALGO AUCK ZWEN 0 | GFZ | BAN2 LPGS 0 | JPL | SANT 1 | EMR | 15 1 | ESA | 4 ALGO AUCK MCM4 MIZU NNOR 1 | GFZ | BAN2 LPGS 1 | JPL | MCM4 1 | MIT | GUAM IISC 2 | COD | 4 24 2 | EMR | 15 17 2 | ESA | 4 ALGO PERT 2 | GFZ | LPGS RIOG 2 | JPL | 4 BOGT TNML 2 | MIT | BOGT RIOG UNSA 3 | COD | 4 17 BOGT 3 | EMR | 15 3 | ESA | 4 17 24 3 | GFZ | BAN2 LPGS MCM4 3 | JPL | ASC1 FORT SANT YSSK 3 | MIT | BOGT DRAO KIT3 PIMO SANT 4 | COD | 4 JAB1 4 | EMR | 15 4 | ESA | 4 ALGO MIZU 4 | GFZ | BAN2 LPGS MCM4 4 | JPL | TNML 4 | MIT | 24 ARTU RIOG 5 | COD | 4 17 5 | ESA | 4 15 17 24 ALGO BOGT LPGS MIZU PIMO YELL 5 | GFZ | BAN2 MCM4 5 | JPL | ASC1 BOGT 5 | MIT | BOGT CRO1 PIMO SANT SCUB 6 | COD | 4 15 6 | ESA | 4 15 17 24 BOGT PIMO 6 | GFZ | LPGS MCM4 VESL 6 | JPL | BOGT SANT 6 | MIT | 10 17 BOGT CEDU CRO1 RIOG SANT WSRT YSSK 5. The following table lists all maneuvered satellites for this week. The solutions from COD and ESA, which modeled the maneuver, are used that day for combination. An associated accuracy code of 0 (unknown) is given if only one AC is left (no redundancy). For the long arc evaluation the arc is split into two parts at the given maneuver epoch. PRN | Day | Date | Ref. NANU ----+-----+------------+----------- 07 | 5 | 2004_06_25 | 2004077 6. The following orbit solutions were excluded from the combination because they were biasing the weighted average (generally indicated by long arc RMS). They were still used for statistics computation. Day | Centre | PRN list ----+--------+--------------- 0 | NGS | ALL (high Transformation - See Table 2) 1 | NGS | ALL (high Transformation - See Table 2) 2 | NGS | ALL (high Transformation - See Table 2) 3 | NGS | ALL (high Transformation - See Table 2) 4 | NGS | ALL (high Transformation - See Table 2) 5 | ESA | 7 5 | NGS | ALL (high Transformation - See Table 2) 6 | NGS | ALL (high Transformation - See Table 2) 7. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 --------+----+----+----+----+----+----+----- PRN 24 | 3 | 2 | 2 | 2 | | | 8. 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. 9. 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 | +0.77 +0.18 +1.69 -0.01 -0.01 +0.01 +2.86 EMR | -1.21 -0.08 +1.27 -0.02 -0.02 -0.01 +3.64 ESA | -0.30 +1.05 -1.89 -0.00 -0.04 +0.02 +2.53 GFZ | -0.05 +0.05 -0.25 +0.02 +0.00 +0.00 +1.69 JPL | -0.52 +0.45 +0.21 +0.12 -0.05 +0.08 +1.19 MIT | -0.23 +0.31 -0.53 +0.13 -0.02 -0.04 +3.91 NGS | -2.14 -0.32 +6.33 -0.29 +0.43 -0.15 +2.69 SIO | +0.27 -0.20 +2.36 -0.08 +0.08 +0.00 +2.57 10.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. 11.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. 12.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 (IGS12767.SUM). Table 1: Week 1276 summary. (Jun 20, 2004 - Jun 26, 2004) Table 1.1276.a GPS week: 1276 MJD: 53176.000-53182.000 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 165|0.00 0.00 0.00 0.04 -0.02 -0.02 -0.3 0.02 0.01 | 0.1 -0.5 0.04 |0.00 0.00 0.00 0.02 0.01 0.04 0.0 | 0.1 0.4 emr 40 |0.00 0.00 0.00 0.06 0.03 -0.01 0.4 0.02 0.02 | 209.1 33.5 0.04 |0.00 0.00 0.00 0.02 0.03 0.03 0.0 | 72.1 2.2 esa 72 |0.00 0.00-0.01 0.02 0.03 -0.03 0.3 0.03 0.03 | 208.3 33.5 0.06 |0.00 0.00 0.00 0.05 0.07 0.07 0.1 | 72.1 2.4 gfz 166|0.00 0.00 0.00 0.00 0.00 0.08 -0.2 0.01 0.01 | 0.1 0.0 0.03 |0.00 0.00 0.00 0.03 0.02 0.03 0.0 | 0.3 0.5 igr n/a|0.00 0.00 0.00 0.02 -0.04 -0.01 -0.1 0.01 0.01 | 14.6 0.3 0.04 |0.00 0.00 0.00 0.01 0.02 0.03 0.1 | 2.3 3.0 jpl 80 |0.00 0.00 0.00 -0.21 0.08 -0.03 0.3 0.04 0.04 | 6.4 1.1 0.03 |0.01 0.00 0.00 0.02 0.03 0.02 0.1 | 2.9 2.5 mit 148|-.01 0.00 0.00 -0.17 -0.03 -0.04 0.1 0.03 0.03 | 2.3 0.2 0.04 |0.00 0.00 0.00 0.02 0.03 0.03 0.1 | 0.5 1.0 ngs 84 |-.01 0.00 0.03 0.70 -0.95 0.13 -0.1 0.06 0.05 | 0.0 -0.1 2.93 |0.01 0.00 0.00 0.07 0.04 0.09 0.1 | 0.3 0.4 sio 143|0.00 0.00-0.02 0.22 -0.27 -0.03 0.3 0.05 0.05 | 0.0 0.0 0.00 |0.00 0.00 0.00 0.13 0.07 0.06 0.1 | 0.0 0.0 Table 1.1276.b GPS week : 1276 MJD: 53176.000-53182.000 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 ------|-----------------------------|------------------------------------------ 1E | 1 1 1 1 1 1 1 | 3 | 1 1 1 1 1 1 1 | 4E | 1 1 2 1 1 1 1 | 5 | 1 1 1 1 1 1 1 | 6 | 1 1 1 1 1 1 1 | 7 | 1 1 1 1 1 0 1 | 8 | 1 1 1 1 1 1 1 | 9 | 1 1 1 1 1 1 1 | 10 | 1 1 1 1 1 1 1 | 11E | 1 1 1 1 1 1 1 | 13 | 1 1 1 1 1 1 1 | 14 | 1 1 1 1 1 1 1 | 15E | 1 1 1 1 1 1 1 | 16 | 1 1 1 1 1 1 1 | 17E | 1 1 1 1 1 1 1 | 18 | 1 1 1 1 1 1 1 | 19 | 1 1 1 1 1 1 1 | 20 | 1 1 1 1 1 1 1 | 21E | 1 1 1 1 1 1 1 | 22 | 1 1 1 1 1 1 1 | 24E | 1 7 1 1 1 1 1 | 25 | 1 1 1 1 1 1 1 | 26 | 1 1 1 1 1 1 1 | 27 | 1 1 1 1 1 1 1 | 28 | 1 1 1 1 1 2 1 | 29 | 1 1 1 1 1 1 1 | 30 | 1 1 1 1 1 1 1 | 31 | 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 2.1276.0 GPS week: 1276 Day: 0 MJD: 53176.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 165|0.00 0.00 0.00 0.02 -0.03 -0.07 -0.3 0.02 0.02 | -0.1 0.1 0.04 | 0.05 -0.01 | emr 40 |0.00 0.00 0.00 0.08 -0.01 -0.01 0.3 0.01 0.01 | 107.6 36.8 0.05 | -0.02 0.02 | esa 72 |0.00 0.00-0.01 -0.01 0.14 -0.02 0.3 0.03 0.03 | 106.4 36.8 0.06 | -0.04 -0.10 | gfz 162|0.00 0.00 0.00 0.00 -0.02 0.11 -0.2 0.01 0.01 | 0.1 0.2 0.03 | -0.08 -0.04 | igr n/a|0.00 0.00 0.00 0.01 -0.01 -0.03 -0.1 0.01 0.01 | 10.6 4.7 0.03 | -0.04 -0.02 | jpl 80 |0.01 0.00-0.01 -0.20 0.05 -0.05 0.2 0.03 0.03 | 0.9 4.7 0.03 | 0.02 0.00 | mit 147|-.01 0.01 0.00 -0.21 -0.01 -0.07 0.2 0.03 0.03 | 1.4 2.1 0.04 | 0.15 0.02 | ngs 84 |-.02-0.01 0.03 0.68 -0.93 0.12 -0.1 0.06 0.06 | -0.1 0.3 2.96 | -0.24 0.15 | sio 146|0.00 0.00-0.01 0.46 -0.40 0.05 0.1 0.07 0.07 | 0.0 0.0 0.00 | -0.14 0.13 | Table 2.1276.1 GPS week: 1276 Day: 1 MJD: 53177.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 165|0.00 0.00 0.00 0.02 -0.04 -0.02 -0.3 0.02 0.01 | 0.1 -0.7 0.04 | 0.06 0.01 | emr 40 |0.00 0.00 0.00 0.07 0.00 -0.03 0.4 0.02 0.02 | 142.9 34.1 0.04 | 0.03 -0.06 | esa 72 |0.00 0.00-0.01 0.10 0.03 0.04 0.3 0.03 0.03 | 142.0 33.9 0.05 | 0.00 -0.08 | gfz 159|0.00 0.00 0.00 -0.04 0.05 0.08 -0.2 0.01 0.01 | -0.1 0.1 0.03 | -0.01 -0.07 | igr n/a|0.00 0.00 0.00 0.03 -0.05 -0.05 -0.1 0.01 0.01 | 14.0 2.3 0.04 | -0.03 -0.08 | jpl 80 |0.01 0.00-0.01 -0.17 0.11 -0.04 0.2 0.04 0.04 | 4.5 2.4 0.03 | 0.00 -0.09 | mit 147|-.01 0.00 0.00 -0.17 -0.02 -0.08 0.2 0.03 0.03 | 2.2 -0.1 0.05 | 0.13 0.01 | ngs 84 |-.02 0.00 0.02 0.74 -0.96 0.22 -0.1 0.07 0.06 | -0.1 0.0 2.80 | -0.38 0.14 | sio 147|0.00 0.00-0.01 0.31 -0.33 -0.02 0.3 0.05 0.04 | 0.0 0.0 0.00 | -0.10 0.07 | Table 2.1276.2 GPS week: 1276 Day: 2 MJD: 53178.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 165|0.00 0.00 0.00 0.02 -0.01 -0.05 -0.3 0.01 0.01 | 0.0 -0.3 0.04 | 0.06 -0.01 | emr 40 |0.00 0.00 0.00 0.03 0.03 -0.01 0.4 0.02 0.02 | 176.9 33.3 0.04 | -0.03 0.00 | esa 72 |0.00 0.00 0.00 0.04 0.05 0.00 0.3 0.03 0.03 | 176.2 34.9 0.05 | -0.03 -0.06 | gfz 166|0.00 0.00 0.00 0.03 0.00 0.08 -0.2 0.01 0.01 | 0.3 -0.1 0.03 | -0.08 -0.03 | igr n/a|0.00 0.00 0.00 0.01 -0.07 0.02 -0.1 0.01 0.01 | 16.2 0.9 0.04 | -0.03 -0.01 | jpl 80 |0.01 0.00-0.01 -0.23 0.06 0.00 0.4 0.04 0.04 | 7.0 1.3 0.03 | -0.02 0.02 | mit 148|-.01 0.01 0.00 -0.17 -0.05 -0.05 0.2 0.03 0.03 | 2.5 0.3 0.04 | 0.10 0.03 | ngs 84 |-.02 0.00 0.02 0.72 -0.98 0.25 -0.1 0.06 0.05 | 0.3 -0.4 3.22 | -0.34 0.28 | sio 148|0.00 0.00-0.02 0.17 -0.23 -0.04 0.2 0.05 0.04 | 0.0 0.0 0.00 | -0.11 0.14 | Table 2.1276.3 GPS week: 1276 Day: 3 MJD: 53179.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 165|0.00 0.00 0.00 0.06 0.00 0.00 -0.3 0.01 0.01 | 0.2 -0.8 0.04 | 0.08 -0.03 | emr 40 |0.00 0.00 0.00 0.06 0.04 0.02 0.4 0.01 0.01 | 208.8 35.4 0.04 | 0.07 -0.04 | esa 72 |0.00 0.00-0.01 0.03 -0.05 -0.11 0.2 0.03 0.03 | 207.9 35.3 0.06 | -0.02 -0.06 | gfz 173|0.00 0.00 0.00 -0.04 0.02 0.03 -0.2 0.01 0.01 | 0.3 -0.6 0.04 | 0.00 -0.07 | igr n/a|0.00 0.00-0.01 0.02 -0.05 0.02 -0.1 0.01 0.01 | 15.7 2.0 0.03 | 0.03 -0.05 | jpl 80 |0.00 0.00 0.00 -0.20 0.08 0.00 0.3 0.04 0.04 | 7.0 2.2 0.04 | 0.07 -0.06 | mit 148|-.01 0.00 0.00 -0.15 -0.04 -0.01 0.1 0.03 0.03 | 2.4 -0.1 0.04 | 0.11 0.05 | ngs 84 |-.01 0.00 0.03 0.71 -0.97 0.19 0.0 0.06 0.05 | 0.0 -0.2 2.85 | -0.23 0.35 | sio 143|0.00 0.00-0.01 0.15 -0.28 -0.01 0.3 0.05 0.04 | 0.0 0.0 0.00 | -0.09 0.14 | Table 2.1276.4 GPS week: 1276 Day: 4 MJD: 53180.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 165|0.00 0.00 0.00 0.04 -0.03 0.01 -0.3 0.02 0.02 | 0.2 -0.6 0.04 | 0.08 -0.01 | emr 40 |0.00 0.00 0.00 0.04 0.05 -0.06 0.4 0.02 0.02 | 243.4 32.9 0.05 | 0.01 -0.06 | esa 72 |0.00 0.00-0.01 -0.04 0.08 0.01 0.2 0.04 0.03 | 243.0 32.1 0.06 | 0.05 -0.07 | gfz 170|0.00 0.00 0.00 0.04 -0.01 0.10 -0.2 0.02 0.01 | -0.2 0.5 0.03 | -0.10 -0.04 | igr n/a|0.00 0.00 0.00 0.02 -0.04 -0.06 -0.1 0.01 0.01 | 16.9 -0.8 0.04 | -0.07 -0.05 | jpl 80 |0.00 0.00 0.00 -0.21 0.04 -0.04 0.3 0.03 0.03 | 7.9 1.6 0.04 | -0.02 -0.03 | mit 148|-.01 0.00 0.00 -0.15 -0.05 -0.07 0.1 0.03 0.03 | 2.3 0.7 0.05 | 0.08 0.05 | ngs 84 |0.00 0.00 0.03 0.59 -1.01 0.01 -0.1 0.06 0.05 | -0.3 0.7 2.82 | -0.19 0.28 | sio 145|0.00 0.00-0.02 0.18 -0.29 -0.08 0.4 0.05 0.05 | 0.0 0.0 0.00 | -0.15 0.15 | Table 2.1276.5 GPS week: 1276 Day: 5 MJD: 53181.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 165|0.00 0.00 0.01 0.05 -0.01 -0.05 -0.4 0.02 0.02 | 0.2 -0.8 0.04 | 0.09 0.00 | emr 40 |0.00 0.00 0.00 0.04 0.04 0.01 0.4 0.02 0.02 | 276.5 30.2 0.04 | 0.07 -0.01 | esa 72 |0.00 0.00-0.01 -0.02 0.01 0.00 0.3 0.03 0.03 | 275.5 29.9 0.06 | -0.01 -0.06 | gfz 164|0.00 0.00 0.00 0.02 0.01 0.05 -0.2 0.02 0.01 | 0.3 -0.6 0.03 | -0.04 -0.04 | igr n/a|0.00 0.00 0.00 0.03 -0.04 -0.01 -0.2 0.02 0.02 | 16.2 -4.0 0.03 | -0.01 -0.05 | jpl 80 |0.00 0.00 0.00 -0.25 0.10 -0.02 0.2 0.04 0.04 | 9.7 -2.7 0.03 | 0.05 -0.04 | mit 148|-.01 0.00 0.00 -0.17 -0.05 0.00 0.0 0.03 0.03 | 3.1 -1.4 0.05 | 0.09 0.06 | ngs 84 |-.01 0.00 0.02 0.66 -0.89 0.09 -0.2 0.07 0.05 | 0.5 -0.6 3.10 | -0.33 0.07 | sio 140|0.00 0.00-0.02 0.20 -0.20 0.01 0.4 0.05 0.05 | 0.0 0.0 0.00 | -0.10 0.10 | Table 2.1276.6 GPS week: 1276 Day: 6 MJD: 53182.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT RMS --------|------------------------------------------------|--------------------- cod 165|0.00 0.00 0.00 0.06 -0.02 0.03 -0.3 0.01 0.01 | -0.1 0.0 0.04 | 0.09 0.00 | emr 40 |0.00 0.00 0.00 0.06 0.05 -0.01 0.4 0.02 0.02 | 307.6 31.7 0.03 | 0.09 -0.05 | esa 72 |0.00 0.00-0.01 0.01 -0.04 -0.17 0.2 0.03 0.03 | 306.9 31.6 0.06 | 0.00 -0.07 | gfz 165|0.00 0.00 0.00 0.02 -0.02 0.11 -0.2 0.01 0.01 | -0.3 0.5 0.04 | -0.07 -0.01 | igr n/a|0.00 0.00 0.00 0.05 -0.04 0.02 0.0 0.01 0.01 | 12.9 -2.8 0.04 | -0.01 -0.02 | jpl 80 |0.00 0.00 0.00 -0.20 0.10 -0.06 0.2 0.03 0.03 | 7.9 -1.5 0.03 | 0.05 -0.04 | mit 148|-.01 0.00 0.00 -0.15 0.01 -0.03 0.1 0.03 0.03 | 2.3 0.2 0.04 | 0.12 0.00 | ngs 84 |-.01 0.00 0.03 0.81 -0.92 0.05 0.1 0.06 0.05 | 0.1 -0.1 2.76 | -0.43 0.24 | sio 132|0.00 0.00-0.02 0.07 -0.19 -0.12 0.3 0.05 0.04 | 0.0 0.0 0.00 | -0.09 0.10 | 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","MD" stands for median of the centre's satellite RMS. Units: cm. Table 3.1276.0 GPS week: 1276 Day: 0 MJD: 53176.000 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 ------|------------------------------------------|------------------------------------------ 1E | 2 2 4 2 1 2 4 7 7 1 | 9 10 10 9 9 9 8 11 11 9 3 | 2 2 2 1 1 2 2 7 6 1 | 5 5 5 5 5 5 6 8 10 5 4E | 2 1 4 2 1 2 3 4 6 1 | 5 5 5 5 4 5 4 6 6 4 5 | 1 1 2 1 1 2 2 6 5 1 | 6 5 6 4 5 5 6 6 7 5 6 | 2 1 2 1 1 2 2 8 7 1 | 4 4 5 3 4 4 5 8 8 4 7 | 2 1 2 1 1 1 2 6 4 1 | 3 4 4 3 3 3 4 8 5 3 8 | 2 1 3 1 1 2 3 6 6 1 | 4 5 5 4 4 4 6 8 7 4 9 | 1 1 2 1 1 2 3 7 6 1 | 3 3 5 3 4 3 5 6 6 3 10 | 1 1 3 1 1 1 3 6 6 1 | 4 4 4 3 4 3 5 7 7 4 11E | 1 1 4 2 2 5 2 8 6 1 | 3 3 5 3 3 3 3 6 6 3 13 | 1 1 4 1 1 6 5 7 6 1 | 3 4 5 3 4 4 4 8 6 3 14 | 2 1 3 1 2 5 3 9 5 1 | 2 3 2 2 3 3 2 6 5 2 15E | 2 1 3 1 1 2 3 6 5 1 | 5 5 4 5 4 4 4 7 5 4 16 | 1 1 3 1 1 4 4 7 6 1 | 4 5 4 4 4 6 4 7 5 4 17E | 1 1 3 1 1 1 3 5 6 1 | 5 5 6 5 5 5 4 7 7 5 18 | 1 1 3 1 2 5 4 6 8 1 | 3 3 4 3 3 4 4 5 5 3 X19 | 2 2 5 1 2 --- 4 7 8 1 | 4 5 6 4 5 --- 7 5 7 4 20 | 1 1 3 1 1 5 3 5 7 1 | 3 4 4 3 3 4 3 6 5 3 21E | 1 2 3 1 1 5 2 6 6 1 | 3 4 3 4 4 4 4 7 5 3 22 | 2 2 4 2 2 5 5 9 7 1 | 3 4 5 4 4 5 5 7 8 4 X24E | 2 2 3 1 1 1 3 5 --- 1 | 23 23 24 23 32 31 32 32 --- 32 25 | 2 1 3 1 1 2 2 5 4 1 | 3 3 4 3 3 3 3 6 5 3 26 | 3 1 3 1 1 1 4 6 7 1 | 3 3 3 3 3 3 4 6 6 3 27 | 1 1 3 1 1 2 2 7 7 1 | 3 4 5 4 4 3 4 7 6 3 28 | 2 2 2 1 1 6 5 6 12 1 | 2 3 3 2 2 3 5 6 12 2 29 | 1 1 2 1 1 1 3 6 7 1 | 3 3 3 3 3 3 5 6 6 3 30 | 1 1 2 1 1 2 2 4 6 1 | 5 3 3 4 4 4 4 4 4 4 31 | 1 1 3 1 1 2 3 6 8 1 | 4 4 5 3 3 3 4 6 8 4 ------|------------------------------------------|------------------------------------------ RMS | 2 1 3 1 1 3 3 6 7 |T 5 6 6 5 7 7 7 9 6 7 WRMS | 2 1 3 1 1 3 3 6 7 |NE 3 3 4 3 3 3 4 6 6 3 MEDI | 2 1 3 1 1 2 3 6 6 |MD 4 4 5 4 4 4 4 7 6 4 Table 3.1276.1 GPS week: 1276 Day: 1 MJD: 53177.000 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 ------|------------------------------------------|------------------------------------------ 1E | 3 2 3 2 2 2 3 7 5 1 | 7 8 7 8 8 8 8 10 9 7 3 | 2 2 3 1 1 2 2 7 6 1 | 4 5 5 4 4 4 5 7 8 4 X4E | 2 2 2 2 1 --- 3 7 2 1 | 4 4 4 4 3 --- 3 7 4 3 5 | 1 1 2 1 1 2 2 5 4 1 | 4 4 5 3 4 4 4 6 6 4 6 | 1 1 2 1 1 2 1 8 4 1 | 3 3 4 3 4 4 4 7 7 3 7 | 1 2 2 1 1 2 2 9 2 1 | 3 4 4 3 3 3 3 9 4 3 8 | 2 2 2 1 1 2 2 5 4 1 | 3 4 5 3 4 4 5 7 5 3 9 | 2 1 3 1 1 2 3 7 2 1 | 3 3 4 3 3 4 4 6 5 3 10 | 1 2 2 1 1 1 2 7 3 1 | 3 3 4 3 3 3 4 7 6 3 11E | 1 1 3 1 1 5 2 7 5 1 | 3 4 4 3 4 3 3 8 5 3 13 | 1 2 3 1 1 5 3 8 4 1 | 3 4 4 3 3 3 4 7 5 3 14 | 2 1 3 1 1 4 3 8 6 1 | 3 3 3 2 3 3 4 6 5 2 15E | 2 2 3 3 1 2 3 7 3 1 | 5 5 5 5 5 5 4 6 5 4 16 | 1 2 3 1 1 4 3 6 5 1 | 6 7 6 6 6 6 6 8 6 6 17E | 1 2 4 1 2 2 4 6 3 1 | 5 5 7 5 6 5 6 7 6 5 18 | 1 2 2 1 1 6 4 6 5 1 | 3 3 3 2 3 4 4 5 4 2 19 | 2 2 4 1 2 5 5 5 6 1 | 3 5 5 4 4 4 6 6 6 3 20 | 1 1 2 1 1 5 2 6 4 1 | 3 4 4 3 3 3 3 5 5 3 21E | 1 1 3 1 1 5 2 6 5 1 | 3 4 4 3 3 4 3 7 5 3 22 | 2 2 3 1 2 5 5 7 7 1 | 3 4 4 3 3 4 4 6 6 3 X24E | --- --- --- --- 14 8 6 7 --- 7 | --- --- --- --- 18 14 18 16 --- 15 X25 | 1 1 3 1 1 --- 2 8 2 1 | 3 3 5 3 3 --- 3 6 4 3 26 | 1 1 2 1 1 2 4 6 4 1 | 3 3 3 2 3 3 4 6 5 2 27 | 2 2 3 1 1 2 3 9 6 1 | 3 4 4 3 4 3 4 6 5 3 28 | 2 3 2 2 1 5 4 6 10 1 | 2 5 3 2 3 3 5 6 10 3 29 | 1 1 3 1 1 2 3 7 4 1 | 2 3 4 2 3 3 5 6 5 3 30 | 1 1 2 1 1 2 2 5 2 1 | 3 3 4 3 3 3 3 5 4 3 31 | 1 2 2 1 1 2 3 4 4 1 | 3 4 4 3 3 3 3 5 5 3 ------|------------------------------------------|------------------------------------------ RMS | 2 2 3 1 1 4 3 7 5 |T 3 4 4 3 5 4 5 7 5 4 WRMS | 1 2 3 1 1 4 3 6 4 |NE 3 4 4 3 3 3 4 6 5 3 MEDI | 1 2 3 1 1 2 3 7 4 |MD 3 4 4 3 3 4 4 6 5 3 Table 3.1276.2 GPS week: 1276 Day: 2 MJD: 53178.000 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 --- 3 5 4 1 | 6 6 7 5 6 --- 7 7 7 6 3 | 2 2 3 1 1 2 3 4 5 1 | 4 5 5 4 4 4 5 7 8 4 4E | 1 2 4 2 2 14 3 4 3 2 | 4 4 4 4 4 10 4 4 5 4 5 | 1 1 2 1 1 2 2 6 4 1 | 5 4 5 4 4 4 4 8 7 4 6 | 2 2 2 1 1 2 2 8 5 1 | 3 4 4 3 3 3 5 6 7 3 7 | 1 2 1 1 1 2 2 7 3 1 | 3 3 4 3 3 3 3 6 4 3 8 | 1 2 2 1 1 2 3 5 4 1 | 4 3 4 4 4 4 5 6 5 3 X9 | 1 1 2 1 1 --- 3 8 3 1 | 3 3 5 3 3 --- 4 5 5 3 10 | 1 2 3 1 1 2 2 5 2 1 | 3 4 4 3 3 3 4 6 5 3 11E | 2 1 4 2 2 5 2 6 5 1 | 3 3 5 3 4 3 4 7 5 3 13 | 1 2 2 1 1 5 3 6 4 1 | 3 3 4 3 3 3 5 6 4 3 14 | 1 2 2 1 1 4 4 10 6 1 | 2 3 3 3 3 3 4 6 3 2 15E | 2 2 3 3 1 2 3 5 3 1 | 5 4 5 5 5 4 4 6 5 4 16 | 1 2 3 1 1 3 3 5 4 1 | 5 6 4 5 4 5 5 7 7 5 X17E | 1 2 3 1 2 --- 2 4 3 1 | 5 5 5 5 5 --- 5 6 5 5 18 | 1 1 3 1 1 5 3 5 5 1 | 3 3 4 3 3 4 3 5 4 3 19 | 2 2 4 1 2 6 5 6 6 1 | 3 5 6 4 4 4 7 5 4 4 20 | 1 1 2 1 1 5 2 5 4 1 | 3 3 4 3 3 4 3 7 3 3 21E | 1 1 4 1 1 5 2 5 5 1 | 3 3 3 3 3 3 3 7 4 3 22 | 1 2 3 1 1 5 4 9 7 1 | 3 3 4 3 3 4 4 7 6 2 X24E | 1 1 3 2 2 2 3 7 --- 1 | 8 8 7 8 13 11 11 12 --- 11 25 | 1 1 2 1 1 3 2 5 2 1 | 3 3 4 3 3 3 3 5 4 3 26 | 1 1 2 1 1 1 3 6 4 1 | 3 3 3 3 3 3 4 6 5 3 27 | 1 1 2 2 1 3 3 7 4 1 | 3 3 4 4 3 3 4 5 4 3 28 | 1 2 3 2 1 5 4 4 9 1 | 3 4 3 2 3 2 5 5 9 3 29 | 1 1 2 1 1 1 3 6 4 1 | 2 3 3 3 3 3 4 6 5 3 30 | 1 2 2 1 1 2 2 5 3 1 | 4 3 5 3 3 3 3 5 4 3 31 | 1 1 2 1 1 2 4 5 4 1 | 3 3 4 3 3 3 4 6 5 3 ------|------------------------------------------|------------------------------------------ RMS | 1 2 3 1 1 4 3 6 5 |T 3 4 4 3 4 4 4 6 5 4 WRMS | 1 2 3 1 1 4 3 5 4 |NE 3 3 4 3 3 3 4 5 5 3 MEDI | 1 2 3 1 1 3 3 5 4 |MD 3 3 4 3 3 3 4 6 5 3 Table 3.1276.3 GPS week: 1276 Day: 3 MJD: 53179.000 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 1 1 3 2 6 4 1 | 5 5 5 5 5 6 6 7 7 5 3 | 2 2 2 1 1 2 2 5 6 1 | 5 5 5 4 4 5 6 7 8 4 4E | 1 1 3 2 1 2 3 4 2 1 | 4 4 5 4 4 6 4 5 4 4 5 | 1 1 2 1 1 2 2 5 4 1 | 5 5 6 5 5 4 5 6 7 5 6 | 1 1 2 1 1 2 3 8 6 1 | 4 4 5 4 4 4 5 7 7 4 7 | 1 2 2 1 1 1 2 8 3 1 | 3 3 3 2 3 3 3 8 4 2 8 | 1 1 2 1 1 2 3 4 4 1 | 4 4 4 3 4 3 5 6 5 4 9 | 2 1 3 1 1 2 3 6 3 1 | 4 4 5 3 4 4 4 6 4 3 10 | 1 1 2 1 1 1 2 3 3 1 | 4 4 4 3 3 3 4 5 5 3 11E | 1 1 3 1 1 6 2 6 6 1 | 3 4 3 4 3 3 3 6 6 3 13 | 1 1 3 2 1 5 4 6 4 1 | 3 4 4 3 3 4 6 7 5 3 14 | 1 2 3 1 1 4 4 7 6 1 | 3 3 4 3 3 3 4 5 3 2 X15E | 1 3 4 3 2 --- 3 6 3 1 | 4 5 5 5 5 --- 4 6 4 4 16 | 1 2 4 1 1 4 3 7 4 1 | 6 7 6 7 6 7 7 10 6 6 17E | 2 1 3 2 2 2 3 5 3 1 | 5 5 5 5 5 5 5 7 5 4 18 | 1 1 4 1 1 5 3 5 6 1 | 3 4 4 3 3 4 3 4 4 3 19 | 2 2 5 2 1 6 4 4 6 1 | 4 6 5 5 5 4 6 5 4 4 20 | 1 2 3 1 1 5 2 7 4 1 | 3 3 4 3 3 4 4 6 5 3 21E | 1 1 4 1 1 5 3 7 4 1 | 3 3 4 3 3 3 4 7 4 3 22 | 1 2 4 1 1 5 4 8 8 1 | 3 4 5 4 3 4 5 7 6 3 X24E | 1 1 3 2 2 2 3 5 --- 1 | 9 9 9 9 12 12 12 14 --- 12 25 | 1 1 3 1 1 2 2 4 2 1 | 3 4 5 3 3 3 3 4 3 3 26 | 1 1 3 1 1 1 3 4 3 1 | 3 3 4 3 3 3 4 6 5 3 27 | 1 1 3 1 1 2 2 6 4 1 | 3 4 4 3 4 3 4 6 4 3 28 | 2 2 4 1 1 5 5 5 9 1 | 3 4 4 3 3 3 5 6 8 3 29 | 1 1 3 1 1 1 3 3 4 1 | 3 3 4 3 3 3 4 5 5 3 30 | 1 1 2 1 1 2 2 5 3 1 | 4 4 4 4 4 3 4 7 4 3 31 | 1 1 2 1 1 2 3 4 4 1 | 4 4 5 3 3 3 4 6 5 3 ------|------------------------------------------|------------------------------------------ RMS | 1 1 3 1 1 4 3 6 5 |T 4 4 4 4 4 4 5 6 5 4 WRMS | 1 1 3 1 1 4 3 5 4 |NE 3 4 4 3 3 3 4 6 4 3 MEDI | 1 1 3 1 1 2 3 5 4 |MD 4 4 5 3 4 4 4 6 5 3 Table 3.1276.4 GPS week: 1276 Day: 4 MJD: 53180.000 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 1 1 2 3 6 4 1 | 4 5 4 3 4 4 5 6 6 4 3 | 2 3 4 1 1 2 2 9 5 1 | 4 4 6 4 4 4 5 7 7 4 4E | 1 1 3 2 1 2 3 4 3 1 | 4 4 5 4 4 4 4 5 4 3 5 | 1 1 2 1 1 2 2 5 4 1 | 4 4 5 4 4 4 5 6 7 4 6 | 2 3 2 2 1 2 3 8 6 1 | 4 4 4 3 3 3 5 8 7 3 7 | 1 2 2 2 1 1 2 4 3 1 | 3 3 3 2 2 3 4 4 4 3 8 | 1 2 3 1 1 2 2 6 5 1 | 3 3 4 3 2 3 4 6 5 3 9 | 2 2 3 1 1 2 3 6 3 1 | 3 4 5 2 3 3 4 5 4 3 10 | 1 2 3 1 1 1 2 4 3 1 | 3 4 3 3 3 3 4 6 5 3 11E | 1 2 2 1 1 5 2 12 6 1 | 2 3 3 3 3 2 3 11 6 2 13 | 1 2 3 2 1 6 4 5 5 1 | 3 3 4 2 3 3 5 6 5 2 14 | 1 2 2 2 2 4 4 10 6 1 | 2 3 3 3 3 3 4 4 3 2 15E | 2 2 3 4 2 2 3 5 4 1 | 4 4 5 5 4 4 3 6 4 4 16 | 1 1 9 2 1 4 3 9 4 1 | 3 2 8 2 2 3 3 7 4 2 17E | 2 2 3 2 1 2 2 5 3 1 | 5 5 5 5 5 5 5 6 5 5 18 | 1 1 4 1 2 5 3 5 5 1 | 3 3 4 3 3 3 3 4 3 3 19 | 2 3 6 2 2 5 4 6 6 1 | 3 5 6 3 4 3 4 5 4 3 20 | 1 2 4 1 1 5 2 5 5 1 | 3 3 5 2 3 3 3 6 4 2 21E | 1 2 2 1 1 5 3 8 3 1 | 2 3 3 2 3 2 4 5 3 2 22 | 2 2 3 2 2 5 5 8 8 1 | 3 3 5 3 3 4 6 7 6 3 X24E | 2 2 3 3 1 2 3 6 --- 1 | 12 12 11 12 14 14 15 17 --- 14 25 | 2 2 2 1 1 1 3 7 2 1 | 3 4 3 3 3 3 3 6 3 2 26 | 1 1 2 1 1 2 3 4 4 1 | 3 4 4 2 3 3 4 4 5 3 27 | 1 2 3 1 1 2 2 5 5 1 | 3 4 4 2 2 2 4 5 3 3 28 | 2 2 3 2 1 6 5 6 9 1 | 3 3 2 2 3 2 5 6 9 2 29 | 1 1 2 1 2 2 3 4 5 1 | 3 4 4 3 3 3 4 5 5 3 30 | 1 2 3 1 1 2 2 4 3 1 | 4 3 4 3 3 3 3 4 3 3 31 | 2 2 3 1 1 2 3 5 4 1 | 4 4 4 3 3 3 4 5 5 3 ------|------------------------------------------|------------------------------------------ RMS | 2 2 4 2 1 3 3 6 5 |T 3 4 4 3 4 4 4 6 5 3 WRMS | 2 2 3 1 1 3 3 5 5 |NE 3 3 4 2 2 2 4 5 4 2 MEDI | 1 2 3 1 1 2 3 6 4 |MD 3 4 4 3 3 3 4 6 5 3 Table 3.1276.5 GPS week: 1276 Day: 5 MJD: 53181.000 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 1 2 2 4 5 5 1 | 5 5 4 4 5 4 6 6 6 4 3 | 2 1 2 1 2 2 3 16 5 1 | 4 5 5 4 4 4 5 12 7 4 4E | 1 2 6 2 2 2 3 4 3 1 | 4 4 6 3 3 4 4 5 5 3 5 | 1 1 4 1 1 2 2 5 3 1 | 4 4 6 3 4 3 4 6 5 4 6 | 2 2 3 1 1 2 3 8 6 1 | 4 4 5 3 3 3 6 7 8 3 X7 | 1 --- >>> --- --- --- --- --- --- 0 | 3 --- 0 --- --- --- --- --- --- 3 8 | 1 1 3 1 1 2 3 4 4 1 | 3 3 4 3 3 3 3 5 5 3 9 | 2 1 4 1 1 2 2 8 3 1 | 3 4 5 3 3 3 4 4 4 3 10 | 1 1 3 1 1 1 2 5 3 1 | 3 3 4 3 3 3 3 5 4 3 11E | 2 2 4 2 2 6 2 11 7 1 | 3 4 5 3 4 3 3 11 6 3 13 | 1 2 3 2 2 5 5 6 4 1 | 3 4 4 3 3 3 6 6 4 3 14 | 1 2 2 1 1 4 4 10 6 1 | 3 3 3 2 3 3 4 6 4 2 15E | 3 2 2 5 2 3 4 6 6 1 | 5 4 4 6 4 4 4 6 5 4 16 | 2 1 3 1 2 4 2 6 4 1 | 5 5 5 5 4 5 5 6 5 5 17E | 2 2 3 2 1 2 4 4 3 1 | 5 5 5 5 5 5 5 7 5 5 18 | 1 1 4 1 2 5 3 7 5 1 | 3 3 3 2 2 3 3 5 3 3 19 | 2 2 4 2 2 6 5 9 5 1 | 4 4 5 4 4 4 5 8 3 3 20 | 1 2 2 1 1 5 3 8 4 1 | 3 4 4 2 3 3 4 8 3 2 21E | 2 2 3 2 1 5 3 7 4 1 | 3 3 3 3 3 2 3 7 3 3 22 | 2 2 4 2 2 5 5 5 9 1 | 3 4 5 3 3 4 6 6 7 3 X24E | 2 2 4 3 2 2 3 5 --- 1 | 12 13 12 12 16 16 16 17 --- 16 X25 | 2 2 3 1 1 --- 2 5 3 1 | 3 3 3 3 3 --- 3 3 3 3 26 | 1 1 3 1 1 2 4 7 4 1 | 3 3 4 3 3 3 4 7 5 3 27 | 1 2 3 2 1 2 3 5 4 1 | 3 4 3 3 3 2 3 4 4 3 28 | 2 2 4 2 2 5 5 6 9 2 | 4 4 4 3 4 3 7 7 11 4 29 | 1 1 3 1 1 2 3 7 5 1 | 3 3 4 3 3 3 4 6 5 3 30 | 1 1 4 1 1 2 2 5 3 1 | 4 4 3 3 3 3 3 6 4 3 31 | 2 2 2 1 2 2 3 5 4 1 | 3 3 3 3 3 3 4 5 4 3 ------|------------------------------------------|------------------------------------------ RMS | 2 2 3 2 2 4 3 7 5 |T 4 4 4 4 4 4 5 7 5 4 WRMS | 2 2 3 1 2 4 3 5 5 |NE 3 3 3 3 3 3 4 6 5 3 MEDI | 2 2 3 1 1 2 3 6 4 |MD 3 4 4 3 3 3 4 6 5 3 Table 3.1276.6 GPS week: 1276 Day: 6 MJD: 53182.000 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 1 1 2 2 6 5 1 | 5 6 6 4 5 5 5 7 7 5 3 | 2 2 2 1 1 1 3 6 5 1 | 6 5 7 5 5 5 6 8 8 5 4E | 2 1 3 2 2 2 4 6 3 1 | 5 5 5 4 5 5 4 7 5 4 5 | 1 2 2 1 1 2 2 7 5 1 | 6 6 6 5 5 5 6 8 8 5 6 | 2 2 2 1 1 2 3 8 7 1 | 5 5 6 4 5 4 7 10 9 5 7 | 1 2 2 1 2 1 3 5 3 1 | 3 2 2 1 2 2 1 2 1 2 8 | 1 2 3 1 1 1 2 3 5 1 | 4 4 4 3 4 4 4 6 5 4 9 | 2 1 2 1 1 2 3 9 3 1 | 3 4 5 3 3 3 4 4 5 3 10 | 1 1 3 1 1 1 2 5 3 1 | 4 4 4 3 3 4 4 5 5 3 11E | 1 2 4 1 1 6 3 8 8 1 | 3 4 4 3 3 3 3 8 7 3 13 | 1 2 3 2 1 6 4 7 6 1 | 3 4 4 2 3 4 5 6 4 3 14 | 2 2 2 2 1 4 4 5 7 1 | 3 4 3 2 3 3 5 3 4 2 15E | 2 3 5 4 2 2 3 6 4 1 | 5 5 6 6 5 4 4 7 5 4 16 | 1 1 2 1 1 4 3 7 4 1 | 5 5 4 4 4 4 6 8 7 4 17E | 2 2 3 2 2 2 3 6 4 1 | 6 6 5 5 5 5 6 6 5 5 18 | 1 2 4 1 2 5 3 7 6 1 | 3 4 3 3 3 4 4 5 3 3 19 | 2 3 4 2 2 5 4 6 6 1 | 4 7 5 4 5 4 6 6 4 4 20 | 1 2 2 1 1 5 2 7 5 1 | 4 4 4 3 3 4 4 8 4 3 21E | 1 1 2 1 2 5 3 4 4 1 | 3 3 3 2 3 3 4 5 4 2 22 | 2 2 3 1 2 5 4 5 8 1 | 3 4 4 3 3 4 5 5 7 3 X24E | 2 2 3 3 2 2 2 5 --- 1 | 13 13 13 13 17 18 18 20 --- 17 25 | 2 1 2 1 1 2 3 6 4 1 | 4 4 3 3 3 4 3 4 4 3 26 | 1 1 2 1 1 2 3 5 4 1 | 3 3 4 3 3 3 4 6 5 3 27 | 1 2 3 1 1 2 2 8 6 1 | 4 4 4 3 3 3 4 6 4 3 28 | 2 2 3 2 1 5 5 5 9 1 | 4 5 3 3 4 3 7 8 11 4 29 | 1 1 2 1 1 1 3 4 4 1 | 3 3 4 3 3 3 5 7 4 3 30 | 1 1 3 1 1 2 2 4 3 1 | 5 4 4 4 4 3 5 5 4 4 31 | 1 2 2 1 1 1 5 4 4 1 | 4 4 4 4 4 4 6 6 7 4 ------|------------------------------------------|------------------------------------------ RMS | 1 2 3 1 1 3 3 6 5 |T 4 5 5 4 4 5 5 7 5 4 WRMS | 1 2 3 1 1 3 3 5 4 |NE 3 4 3 3 3 3 4 6 5 3 MEDI | 1 2 3 1 1 2 3 6 5 |MD 4 4 4 3 4 4 5 6 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 4.1276 GPS week: 1276 MJD: 53176.0-53182.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----|----------|----------------|----------------|----------------| cod | cod 2674 |U 4 6 7 |U 2 5 6 |U 4 4 8 | emr | emr 2644 | 4 6 8 | 4 5 16 | 4 4 8 | esa | esa 2666 | 4 6 9 |U 2 5 9 | 4 4 12 | gfz | gfz 2635 |U 4 6 8 |U 3 5 11 |U 4 4 8 | igr | igr 2604 | 4 6 8 | 3 5 9 | 4 4 8 | igs | igs 2665 | 4 6 8 | 2 5 9 | 4 4 8 | jpl | jpl 2541 | 4 6 10 |U 3 5 9 | 5 4 10 | mit | mit 2688 |U 4 6 8 |U 3 5 10 |U 4 4 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 5.1276.0 GPS week: 1276 Day: 0 MJD: 53176.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----|----------|----------------|----------------|----------------| cod | cod 2688 | 4 4 7 | 1 4 5 | 3 2 7 | emr | emr 2672 | 4 5 8 | 3 4 10 | 4 3 7 | esa | esa 2688 | 4 5 7 | 2 5 8 | 4 4 13 | gfz | gfz 2654 | 4 5 8 | 3 4 12 | 4 3 8 | igr | igr 2574 | 5 6 11 | 3 5 9 | 4 4 8 | igs | igs 2684 | 4 5 8 | 2 4 10 | 4 3 8 | jpl | jpl 2569 | 5 6 10 | 3 5 10 | 4 3 8 | mit | mit 2688 | 4 5 8 | 3 5 11 | 3 5 8 | Table 5.1276.1 GPS week: 1276 Day: 1 MJD: 53177.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----|----------|----------------|----------------|----------------| cod | cod 2592 | 4 5 7 | 1 4 6 | 4 4 8 | emr | emr 2580 | 5 5 9 | 3 4 7 | 4 6 9 | esa | esa 2592 | 4 4 9 | 2 5 9 | 4 4 12 | gfz | gfz 2568 | 5 5 8 | 2 5 11 | 4 5 8 | igr | igr 2576 | 3 5 7 | 2 5 8 | 4 4 9 | igs | igs 2681 | 3 5 8 | 2 4 9 | 4 5 9 | jpl | jpl 2484 | 5 6 10 | 3 5 7 | 6 4 12 | mit | mit 2688 | 4 5 7 | 3 4 11 | 3 4 8 | Table 5.1276.2 GPS week: 1276 Day: 2 MJD: 53178.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----|----------|----------------|----------------|----------------| cod | cod 2688 | 4 6 7 | 1 4 6 | 4 3 8 | emr | emr 2672 | 4 6 9 | 9 6 37 | 4 3 6 | esa | esa 2688 | 4 6 9 | 3 5 8 | 4 3 8 | gfz | gfz 2664 | 4 6 8 | 3 5 11 | 4 3 6 | igr | igr 2572 | 3 5 9 | 3 4 10 | 3 3 5 | igs | igs 2670 | 3 6 9 | 2 4 11 | 4 3 6 | jpl | jpl 2388 | 4 6 11 | 2 5 13 | 5 2 10 | mit | mit 2688 | 4 5 9 | 3 5 11 | 3 3 6 | Table 5.1276.3 GPS week: 1276 Day: 3 MJD: 53179.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----|----------|----------------|----------------|----------------| cod | cod 2688 | 4 5 7 | 2 5 6 | 4 2 8 | emr | emr 2672 | 4 5 9 | 3 5 11 | 3 3 8 | esa | esa 2688 | 4 5 9 | 3 5 8 | 4 3 10 | gfz | gfz 2665 | 4 6 9 | 3 5 10 | 4 3 8 | igr | igr 2577 | 4 6 9 | 3 5 10 | 4 4 9 | igs | igs 2682 | 4 5 9 | 2 4 9 | 4 3 8 | jpl | jpl 2545 | 4 5 9 | 3 4 7 | 5 4 8 | mit | mit 2688 | 4 5 9 | 3 5 10 | 3 3 8 | Table 5.1276.4 GPS week: 1276 Day: 4 MJD: 53180.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----|----------|----------------|----------------|----------------| cod | cod 2688 | 4 5 7 | 2 5 6 | 4 3 9 | emr | emr 2671 | 4 5 8 | 3 5 8 | 4 3 10 | esa | esa 2688 | 4 6 9 | 3 5 9 | 4 3 12 | gfz | gfz 2664 | 4 5 8 | 3 5 9 | 4 3 9 | igr | igr 2674 | 4 5 8 | 3 5 7 | 4 3 9 | igs | igs 2685 | 4 5 8 | 2 5 9 | 4 3 9 | jpl | jpl 2662 | 4 6 10 | 3 5 8 | 5 4 11 | mit | mit 2688 | 4 5 8 | 3 5 10 | 4 3 10 | Table 5.1276.5 GPS week: 1276 Day: 5 MJD: 53181.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----|----------|----------------|----------------|----------------| cod | cod 2688 | 4 8 9 | 3 7 10 | 4 3 7 | emr | emr 2573 | 4 8 8 | 4 5 7 | 5 4 7 | esa | esa 2630 | 5 8 10 | 2 5 11 | 5 6 9 | gfz | gfz 2568 | 4 8 8 | 3 5 11 | 4 4 7 | igr | igr 2575 | 4 7 8 | 3 5 8 | 4 4 7 | igs | igs 2581 | 4 7 8 | 3 5 8 | 4 4 7 | jpl | jpl 2474 | 5 9 10 | 3 6 7 | 5 4 9 | mit | mit 2688 | 4 8 8 | 4 6 8 | 4 4 6 | Table 5.1276.6 GPS week: 1276 Day: 6 MJD: 53182.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----|----------|----------------|----------------|----------------| cod | cod 2684 | 3 5 5 | 1 5 6 | 3 6 9 | emr | emr 2671 | 3 6 6 | 3 5 8 | 3 4 10 | esa | esa 2687 | 3 7 6 | 2 5 7 | 3 6 15 | gfz | gfz 2663 | 3 6 5 | 3 4 11 | 2 4 11 | igr | igr 2678 | 4 7 6 | 3 5 8 | 2 5 10 | igs | igs 2672 | 3 6 5 | 3 5 8 | 3 5 10 | jpl | jpl 2667 | 3 7 7 | 2 5 9 | 3 5 13 | mit | mit 0 | 0 0 0 | 0 0 0 | 0 0 0 | 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 6.1276 GPS week: 1276 MJD: 53176.500-53182.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | -1 -6 0 -12 -2 | -19 29 | 2 2 4 8 8 | 6 emr uuuuu | 1 -1 2 19 4 | 25 35 | 2 3 10 13 11 | 5 esa uuuuu | 5 3 0 -12 -5 | 19 27 | 2 3 6 11 17 | 5 gfz uuuuu | 2 7 2 2 0 | 10 27 | 1 3 5 5 6 | 7 igr xxxxx | 2 4 -1 -11 1 | -4 23 | 2 2 9 9 7 | 5 irf xxxxx | -2 2 0 -10 0 | 0 21 | 1 2 6 7 8 | 7 jpl uuuuu | 2 0 -14 16 10 | -2 28 | 2 2 9 5 20 | 10 mit uuuuu | -5 -9 0 -10 -5 | 32 37 | 2 3 8 9 8 | 4 ngs xxxxx | -23 32 0 -6 -33 | -36 48 | 10 10 38 15 44 | 10 sio uuuuu | -14 13 1 -14 -7 | 37 40 | 3 2 10 10 7 | 3 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 7.1276.0 GPS week: 1276 Day: 0 MJD: 53176.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | 0 -5 5 -12 10 | -26 31 emr uuuuu | -3 1 -17 16 -13 | 22 31 esa uuuuu | 9 4 12 -4 -25 | 13 21 gfz uuuuu | 2 7 5 -5 9 | 2 22 igr xxxxx | 1 4 -7 -4 8 | -11 23 irf xxxxx | -1 0 13 -1 16 | -10 18 jpl uuuuu | -1 -2 -6 21 22 | -15 25 mit uuuuu | -3 -16 5 -7 6 | 27 32 ngs xxxxx | -16 23 56 22 51 | -50 60 sio uuuuu | -14 14 13 -4 2 | 32 35 Table 7.1276.1 GPS week: 1276 Day: 1 MJD: 53177.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | -5 -4 2 1 2 | -24 30 emr uuuuu | 2 0 1 1 4 | 21 30 esa uuuuu | 4 2 -6 -13 10 | 12 20 gfz uuuuu | 3 4 1 0 -1 | 6 23 igr xxxxx | 4 5 7 -23 -13 | -8 23 irf xxxxx | -4 3 -1 -8 6 | -7 18 jpl uuuuu | 5 3 -18 16 -14 | -9 24 mit uuuuu | -5 -10 7 3 0 | 29 34 ngs xxxxx | -18 41 -44 -2 -7 | -40 54 sio uuuuu | -10 12 0 -19 -10 | 34 37 Table 7.1276.2 GPS week: 1276 Day: 2 MJD: 53178.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | 0 -7 -3 -17 -15 | -21 31 emr uuuuu | 0 2 9 21 -8 | 22 32 esa uuuuu | 5 2 -3 5 -3 | 17 28 gfz uuuuu | 2 7 9 1 -11 | 8 27 igr xxxxx | 0 2 -14 -8 1 | -8 23 irf xxxxx | 0 -1 -4 -7 -6 | -3 22 jpl uuuuu | -2 1 -21 8 37 | -9 24 mit uuuuu | -3 -11 -15 -12 -18 | 30 37 ngs xxxxx | -29 33 10 -21 -27 | -30 42 sio uuuuu | -15 10 -6 0 -17 | 35 39 Table 7.1276.3 GPS week: 1276 Day: 3 MJD: 53179.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | 0 -3 0 -5 1 | -21 31 emr uuuuu | 1 -3 2 14 7 | 22 32 esa uuuuu | 3 6 -4 -27 -17 | 18 30 gfz uuuuu | 4 5 6 5 3 | 8 26 igr xxxxx | 2 2 -3 -22 4 | -7 24 irf xxxxx | -3 4 -5 -14 -2 | -1 23 jpl uuuuu | 3 -3 -24 17 13 | -5 30 mit uuuuu | -8 -6 3 -11 0 | 30 36 ngs xxxxx | -38 27 -30 -21 -73 | -24 35 sio uuuuu | -17 13 -11 -21 -11 | 35 38 Table 7.1276.4 GPS week: 1276 Day: 4 MJD: 53180.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | -1 -8 -7 -13 -8 | -15 27 emr uuuuu | 4 0 11 11 12 | 27 38 esa uuuuu | 5 -4 1 -4 -22 | 23 31 gfz uuuuu | 2 10 -2 6 6 | 13 29 igr xxxxx | 3 7 -1 -2 4 | 0 23 irf xxxxx | -2 0 3 -6 -4 | 5 23 jpl uuuuu | 1 2 0 12 23 | 3 30 mit uuuuu | -7 -8 -6 -4 -13 | 34 40 ngs xxxxx | -30 19 40 -3 -55 | -28 40 sio uuuuu | -17 15 16 -10 1 | 39 42 Table 7.1276.5 GPS week: 1276 Day: 5 MJD: 53181.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | -1 -6 1 -21 -7 | -13 26 emr uuuuu | 0 -4 -1 43 15 | 30 40 esa uuuuu | 5 5 -4 -17 -1 | 23 31 gfz uuuuu | 3 8 2 -2 -2 | 17 30 igr xxxxx | 4 4 14 -10 -5 | 2 22 irf xxxxx | -1 3 -3 -24 -2 | 7 22 jpl uuuuu | 3 -2 -8 21 9 | 8 31 mit uuuuu | -7 -6 6 -28 -8 | 35 41 ngs xxxxx | -8 36 -1 -2 -65 | -37 47 sio uuuuu | -11 13 -2 -24 -2 | 41 43 Table 7.1276.6 GPS week: 1276 Day: 6 MJD: 53182.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS ------------------------------------------------------------------------ cod uuuuu | -2 -6 -1 -17 3 | -12 24 emr uuuuu | 3 -6 11 28 11 | 34 42 esa uuuuu | 5 4 6 -23 19 | 24 31 gfz uuuuu | -1 10 -5 10 -1 | 20 29 igr xxxxx | 0 4 -5 -4 5 | 3 22 irf xxxxx | -2 3 -1 -9 -6 | 9 21 jpl uuuuu | 2 -1 -19 15 -19 | 13 30 mit uuuuu | -2 -9 2 -13 -3 | 36 41 ngs xxxxx | -26 46 -33 -17 -58 | -46 57 sio uuuuu | -12 13 -3 -22 -10 | 41 43