Date: Fri, 08 Feb 2008 13:31:56 +0100 To: igsreport@igscb.jpl.nasa.gov Subject: [IGSREPORT-15925] Wk 1463 IGS Final Orbits User-Agent: Heirloom mailx 12.3 7/15/07 Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: 7bit Message-Id: <20080208123156.C06F250984@kg20.gfz-potsdam.de> From: igsacc@gfz-potsdam.de (Gerd Gendt3) Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 08 Feb 04:32:05 PST 2008 Message Number 15925 ****************************************************************************** Author: AC Coordinator / GFZ Potsdam sum-file Version 2.0 Final IGS Orbit Combination - Week 1463 (Jan 20, 2008 - Jan 26, 2008) Contacts: G. Gendt (gendt@gfz-potsdam.de), Th. Nischan ( nisn@gfz-potsdam.de) 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. 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, no satellite L1/L2 delay calibration should be 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. 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: igs1463[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1463[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1463[0-6].cls IGS GPS clock combination summary report. igs14637.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14637.sum Complete report. REMARKS concerning the IGS 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 | ONSA 0 | ESA | 10 19 0 | GFZ | 16 1 | COD | BRAZ YELL 1 | EMR | ONSA 1 | ESA | 5 10 19 29 30 32 DAEJ YELL 1 | GFZ | 29 2 | COD | MCM4 2 | EMR | GODE ONSA 2 | ESA | 10 19 29 30 AREQ 2 | GFZ | 2 29 KERG 2 | JPL | AREQ 3 | ESA | 10 19 29 30 3 | GFZ | CEDU 4 | COD | MCM4 4 | EMR | ONSA 4 | ESA | 10 19 MAS1 4 | GFZ | MAS1 NISU 5 | COD | BRAZ YELL 5 | EMR | ONSA 5 | ESA | 5 10 17 19 29 30 CHUR HOLM 5 | GFZ | 5 29 6 | COD | BRAZ 6 | EMR | ONSA SPT0 WTZR 6 | ESA | 10 17 19 29 30 31 6 | GFZ | 29 6 | JPL | 5 5. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) 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. 6. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. 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 IGS05.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 | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .0 .5 .0 -16 9 -7 .17 EMR | 1.8 9.6 .1 -21 50 4 .27 ESA | 6.5 9.3 -5.6 31 -62 62 .82 GFZ | .7 .0 -.2 -6 -22 10 .06 JPL | -1.4 6.2 14.3 17 9 -18 .43 MIT | .6 6.6 -8.7 -13 12 -2 .03 NGS | 4.0 -2.3 -3.3 -45 -77 27 -.69 SIO | -1.1 9.8 12.7 115 -1 0 .66 7. 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 navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 8. Starting on 27-Feb-2000 (GPS Week 1051-0; 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. 9. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five 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 1.1463.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1463.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 2.1463.[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 3.1463.[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 and final part, Table 5, is similar to Table 4 and contains daily precise navigation statistics (tables 5.1463.0-6). 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 1463 summary. (Jan 20, 2008 - Jan 26, 2008) Table 1.1463.a GPS week: 1463 MJD: 54485.000-54491.000 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 169| 1 0 -3 20 -31 -9 -.33 11 10 | -326 -296 40 79 | 0 0 1 16 18 34 .03 | 513 828 emr 66| 1 2 1 40 -134 -6 .32 15 15 | 4977 -263 49 88 | 2 1 1 8 35 13 .04 | 1877 2200 esa 106| 2 0 -3 -2 76 9 .13 14 14 | -7814 -267 36 159 | 1 2 2 44 87 17 .03 | 2225 2156 gfz 164| -1 1 0 1 25 -10 -.15 12 12 | 16 148 29 100 | 0 0 1 26 23 30 .08 | 315 582 igr n/a| 0 -1 -3 -12 -19 -7 -.03 7 7 | 12708 45 31 84 | 0 0 0 11 23 19 .03 | 2567 2561 jpl 116| 0 -3 7 -44 -39 -7 .45 13 13 | 7590 -128 32 77 | 0 1 0 19 23 20 .04 | 2079 2364 ngs 184| -2 0 0 67 119 11 -.34 14 11 | -284 -344 2473 4234 | 1 0 1 28 44 28 .05 | 447 684 sio 86| 0 0 -3 -253 -46 14 .07 26 25 | --- --- --- --- | 2 0 1 44 30 34 .03 | --- --- Table 1.1463.b GPS week : 1463 MJD: 54485.000-54491.000 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 | 6 5 6 5 6 6 6 | 2 | 6 6 6 7 6 6 6 | 3 | 5 5 5 6 6 5 5 | 4 | 5 6 5 6 5 5 4 | 5E | 6 6 6 7 8 7 8 | 6 | 5 5 5 5 5 4 4 | 8 | 6 5 5 5 5 5 5 | 9 | 5 5 5 5 5 5 4 | 10E | 9 9 8 7 7 7 6 | 11 | 7 6 5 6 6 6 6 | 12E | 6 7 7 7 6 6 7 | 13 | 6 6 6 6 6 6 5 | 14 | 7 6 6 7 6 6 6 | 15 | 6 7 6 6 7 7 6 | 16E | 7 6 6 7 7 6 6 | 17 | 6 6 7 7 7 7 6 | 18E | 6 6 7 6 5 6 6 | 19 | 8 6 6 6 6 6 6 | 20 | 6 5 6 6 6 5 6 | 21 | 6 6 6 6 6 6 6 | 22E | 7 5 6 6 5 6 5 | 23 | 6 6 6 7 6 5 6 | 24 | 5 5 5 4 5 5 5 | 25 | 5 4 4 5 4 4 4 | 26 | 5 6 6 6 6 6 6 | 27 | 6 5 5 5 5 5 5 | 28E | 6 7 7 6 6 6 6 | 29 | 8 8 8 8 7 8 8 | 30E | 7 6 7 7 7 7 7 | 31 | 7 6 7 6 7 6 6 | 32E | 16 16 18 19 15 13 17 | 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. Table 2.1463.0 GPS week: 1463 Day: 0 MJD: 54485.000 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 169| 0 0 -4 11 -25 42 -.32 11 10 | 500 -2049 41 90 | 22 27 | emr 66| -1 1 2 41 -145 -21 .32 15 15 | 2916 1140 49 93 | 2 28 | esa 106| 4 4 -1 -9 72 -10 .10 16 16 | -3151 -3794 40 199 | 77 9 | gfz 164| -1 1 -2 34 59 -10 -.30 14 14 | 385 -474 34 130 | -11 -23 | igr n/a| 1 -2 -2 -1 14 -23 -.06 8 8 | 8915 1788 41 123 | -15 -66 | jpl 116| 0 -3 8 -55 -40 -11 .50 12 12 | 5163 1312 34 83 | 40 -27 | ngs 184| -1 0 -1 55 100 -6 -.31 14 13 | 413 -1835 2548 4725 | 45 84 | sio 86| -3 0 -3 -195 -32 -56 .05 30 26 | --- --- --- --- | 125 46 | Table 2.1463.1 GPS week: 1463 Day: 1 MJD: 54486.000 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 169| 2 0 -4 21 -18 -52 -.36 11 10 | -835 553 42 75 | -7 18 | emr 66| 1 1 1 48 -84 -8 .28 15 15 | 3910 1767 51 84 | -23 -26 | esa 106| 1 1 0 0 -49 39 .09 12 12 | -9123 236 32 145 | -28 -9 | gfz 164| -3 1 0 0 25 24 -.21 13 13 | 211 -474 30 89 | -22 -30 | igr n/a| 0 0 -3 -3 8 -23 -.08 7 7 | 10686 2510 29 62 | -28 -10 | jpl 116| 0 -2 7 -46 10 8 .47 12 12 | 6125 2024 30 68 | 6 -67 | ngs 184| -3 0 -1 71 182 -19 -.29 14 12 | -524 75 2551 4221 | 57 -7 | sio 86| 1 0 -2 -304 -50 11 .09 27 25 | --- --- --- --- | 152 40 | Table 2.1463.2 GPS week: 1463 Day: 2 MJD: 54487.000 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 169| 1 0 -3 31 -52 12 -.37 12 11 | -1045 -24 42 82 | -65 11 | emr 66| -1 2 1 41 -103 0 .34 15 15 | 5492 1685 55 95 | 23 -38 | esa 106| 3 1 -4 -61 23 -3 .10 14 14 | -9075 770 35 160 | -16 -65 | gfz 164| 0 1 -1 -19 34 -44 -.18 13 13 | -198 31 31 101 | -12 -44 | igr n/a| 1 -1 -4 -14 -29 8 -.03 7 7 | 13016 2253 32 74 | 34 -18 | jpl 116| 0 -4 6 -13 -41 -10 .46 12 12 | 7871 1860 36 85 | 20 -1 | ngs 184| -2 0 0 117 154 27 -.39 14 11 | -1042 36 2545 3936 | -32 44 | sio 86| -1 -1 -2 -288 -52 22 .11 25 24 | --- --- --- --- | 118 5 | Table 2.1463.3 GPS week: 1463 Day: 3 MJD: 54488.000 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 169| 0 0 -1 -4 -40 -15 -.33 11 11 | -274 -432 45 90 | 23 9 | emr 66| 0 0 -1 50 -119 -18 .30 14 14 | 6519 1124 50 92 | -32 3 | esa 106| 3 0 -5 61 64 6 .13 14 14 | -6777 -2293 40 150 | -2 -13 | gfz 164| 0 0 1 31 17 24 -.11 11 11 | -47 -81 28 104 | 9 -28 | igr n/a| 0 -1 -4 -34 -26 -35 -.02 7 7 | 14602 1514 28 69 | 7 3 | jpl 116| 0 -4 7 -75 -41 -14 .47 14 14 | 9121 1546 34 76 | 26 8 | ngs 184| -1 0 1 30 148 -7 -.28 14 11 | -249 -449 2384 4478 | 70 32 | sio 86| -1 1 -2 -264 -18 16 .10 26 24 | --- --- --- --- | 157 -8 | Table 2.1463.4 GPS week: 1463 Day: 4 MJD: 54489.000 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 169| 0 0 -3 46 -56 -25 -.35 11 10 | -194 120 41 79 | -2 6 | emr 66| 3 5 1 40 -139 3 .33 15 15 | 6902 -1986 51 87 | 38 6 | esa 106| 2 -1 -4 -55 237 5 .17 14 14 | -9295 2579 40 177 | 6 5 | gfz 164| 0 0 2 -39 -18 -17 -.06 12 12 | -2 1124 29 116 | 61 -30 | igr n/a| 0 -1 -1 -6 -55 2 -.03 7 7 | 15357 -1766 33 99 | 40 -1 | jpl 116| 0 -4 6 -27 -57 1 .40 13 13 | 9844 -1746 33 77 | 45 -8 | ngs 184| -4 0 0 88 113 37 -.40 15 11 | -206 97 2289 4224 | -9 76 | sio 86| -1 0 -5 -200 -104 39 .07 28 26 | --- --- --- --- | 107 22 | Table 2.1463.5 GPS week: 1463 Day: 5 MJD: 54490.000 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 169| 0 0 -2 18 -9 14 -.31 11 10 | -418 -128 38 74 | 8 1 | emr 66| 3 1 0 39 -153 -16 .31 15 15 | 6678 -3666 45 81 | -12 46 | esa 106| 0 0 -3 28 81 27 .17 12 12 | -8751 1104 33 147 | -34 -26 | gfz 164| -1 1 1 -7 35 3 -.09 12 12 | 293 619 27 81 | 11 -24 | igr n/a| 0 -1 -2 -18 -27 17 -.00 6 6 | 15417 -3860 27 69 | -21 -1 | jpl 116| 1 -2 7 -45 -55 -46 .40 14 14 | 9782 -3834 33 78 | 7 -37 | ngs 184| -2 0 0 61 65 -4 -.38 13 11 | -367 -197 2696 4300 | -83 132 | sio 86| 1 0 -2 -288 -13 13 .04 25 23 | --- --- --- --- | 190 41 | Table 2.1463.6 GPS week: 1463 Day: 6 MJD: 54491.000 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 169| 1 0 -2 15 -20 -44 -.29 11 10 | -21 -117 37 69 | 31 -22 | emr 66| 1 1 2 24 -192 16 .40 17 17 | 2423 -1908 48 86 | 35 55 | esa 106| 1 -1 -7 17 109 4 .13 12 12 | -8531 -472 35 141 | 36 -38 | gfz 164| -1 1 1 9 24 -53 -.11 12 12 | -530 297 26 83 | 35 -50 | igr n/a| 0 -1 -3 -7 -23 0 .02 6 6 | 10968 -2123 29 93 | 0 -51 | jpl 116| -1 -2 8 -47 -53 17 .43 13 13 | 5224 -2063 30 77 | 49 -16 | ngs 184| 0 0 -1 47 68 56 -.35 13 10 | -18 -138 2301 3758 | -78 84 | sio 86| 2 0 -3 -235 -51 51 .05 25 25 | --- --- --- --- | 187 63 | 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 3.1463.0 GPS week: 1463 Day: 0 MJD: 54485.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl ngs sio IGS | cod emr esa gfz igr jpl ngs sio IGS ------+----------------------------------------------+----------------------------------------------- 1 | 8 12 17 13 9 9 12 29 5 | 26 34 24 32 28 35 26 42 29 2 | 11 11 11 15 7 9 12 45 6 | 44 46 46 49 42 45 47 44 44 3 | 10 11 12 9 13 7 14 34 5 | 25 30 30 27 28 25 26 35 25 4 | 8 12 11 13 9 8 11 32 5 | 39 41 40 37 42 36 40 43 38 5E | 12 15 10 14 8 13 14 31 6 | 40 40 36 42 40 36 44 46 39 6 | 7 9 10 13 6 9 13 24 4 | 33 36 36 33 38 32 39 38 34 8 | 8 11 14 11 5 9 17 31 5 | 24 27 21 31 26 27 26 28 24 9 | 10 12 14 13 6 9 13 20 5 | 24 30 26 28 24 27 21 28 24 10E | 21 18 23 20 7 14 18 55 9 | 79 81 74 77 80 80 83 86 78 11 | 10 15 16 11 8 17 18 30 6 | 46 55 44 47 44 48 41 44 44 12E | 13 16 15 9 5 15 11 26 6 | 36 42 30 40 36 43 38 33 37 13 | 10 16 14 15 7 10 15 25 5 | 19 34 22 28 25 29 22 23 22 14 | 13 20 19 14 8 13 15 14 6 | 21 34 24 26 24 27 24 24 22 15 | 10 17 16 12 6 12 13 20 5 | 20 33 24 29 22 26 23 23 22 16E | 11 14 19 16 5 16 13 32 6 | 18 31 22 28 21 32 22 27 22 17 | 13 17 13 13 8 16 15 23 6 | 28 32 26 35 27 34 30 29 27 18E | 11 16 12 18 6 18 14 21 6 | 31 37 30 38 31 36 32 32 30 19 | 12 16 34 11 8 13 17 29 7 | 25 32 45 31 26 35 27 23 27 20 | 10 19 15 9 10 14 15 24 6 | 19 32 19 23 24 27 21 29 21 21 | 11 13 14 13 5 14 12 32 6 | 37 44 39 42 37 43 38 40 38 22E | 13 13 18 27 9 15 11 17 6 | 23 29 26 38 28 27 28 25 23 23 | 11 20 14 11 6 13 15 25 6 | 20 39 22 30 26 33 20 31 25 24 | 7 11 11 12 8 9 14 20 4 | 34 38 34 34 35 31 37 32 34 X25 | 8 10 13 10 9 7 15 --- 4 | 23 25 22 29 27 28 24 --- 24 26 | 8 10 13 12 8 9 15 31 5 | 21 28 26 27 22 29 17 43 23 27 | 8 10 12 12 6 9 15 39 5 | 25 26 22 32 27 28 25 26 25 28E | 12 15 17 11 10 14 17 28 6 | 27 35 31 32 29 36 29 39 29 X29 | 17 17 18 12 8 20 17 --- 7 | 43 54 45 47 50 55 46 --- 46 30E | 12 16 14 13 7 14 20 30 6 | 53 55 49 56 53 47 57 55 50 31 | 13 15 16 15 8 15 12 36 6 | 20 35 21 30 26 33 24 41 24 X32E | 17 32 29 --- 45 --- 33 --- 16 | 71 79 69 --- 71 --- 75 --- 71 ------+----------------------------------------------+----------------------------------------------- RMS | 11 15 16 14 8 12 14 30 |T 32 39 33 35 34 35 33 36 32 WRMS | 10 15 16 14 8 12 13 26 |NE 28 35 29 33 30 33 29 33 29 MEDI | 11 15 14 13 8 13 15 29 |MD 26 35 30 32 28 33 28 32 27 Table 3.1463.1 GPS week: 1463 Day: 1 MJD: 54486.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl ngs sio IGS | cod emr esa gfz igr jpl ngs sio IGS ------+----------------------------------------------+----------------------------------------------- 1 | 7 10 13 13 5 7 12 24 4 | 27 32 35 37 30 33 31 42 31 2 | 11 10 13 14 4 9 11 44 6 | 36 44 40 40 39 43 36 46 38 3 | 8 12 10 9 4 8 13 32 5 | 18 23 21 22 19 21 23 34 18 4 | 7 10 10 14 6 10 11 37 5 | 23 30 25 25 28 26 27 35 25 5E | 12 16 11 13 10 14 16 33 6 | 24 27 22 26 24 21 31 31 22 6 | 8 10 9 10 8 11 11 30 4 | 21 23 22 23 24 23 31 32 22 8 | 9 11 9 12 5 9 14 20 4 | 13 18 17 21 17 23 21 25 16 9 | 12 13 12 11 5 9 12 25 5 | 18 22 20 23 20 23 20 27 17 10E | 20 36 18 18 9 14 17 34 9 | 47 68 52 57 52 58 54 74 52 11 | 10 17 15 10 14 14 13 33 6 | 30 46 30 36 31 41 28 33 32 X12E | 15 13 --- 9 4 16 13 26 6 | 48 53 --- 52 49 55 54 46 50 13 | 9 17 14 16 8 9 12 22 5 | 14 32 24 27 23 28 22 22 21 14 | 14 17 13 16 7 12 20 14 6 | 18 30 21 28 23 25 28 25 21 15 | 11 17 15 15 5 14 20 25 6 | 15 29 24 24 20 24 20 22 18 16E | 10 13 13 8 6 16 13 29 5 | 23 34 25 28 27 35 34 34 27 17 | 14 14 11 15 11 14 15 21 6 | 15 24 14 24 20 25 25 22 16 18E | 13 16 13 10 8 17 14 20 6 | 42 54 55 54 50 53 52 52 49 19 | 11 14 14 13 7 14 14 34 6 | 19 34 27 31 25 34 28 33 25 20 | 10 17 10 11 7 11 13 25 5 | 13 27 13 17 15 21 19 23 14 21 | 11 13 11 13 5 13 11 29 5 | 26 37 32 33 31 35 32 37 30 22E | 12 14 11 12 10 12 16 17 5 | 24 32 27 32 23 26 31 26 25 23 | 10 18 12 11 6 14 16 21 5 | 16 35 22 26 24 31 25 24 22 24 | 6 9 7 15 5 10 12 23 4 | 23 24 23 23 25 22 30 31 24 25 | 7 10 10 11 6 8 12 15 4 | 14 21 23 24 18 24 21 23 19 26 | 8 12 10 13 6 11 18 31 5 | 18 28 26 26 20 26 20 41 22 27 | 7 8 10 12 6 9 14 26 4 | 14 20 22 21 17 23 21 29 18 28E | 14 17 14 14 5 16 19 27 6 | 20 35 31 25 22 35 30 39 25 X29 | 16 18 15 13 9 20 19 --- 7 | 54 64 56 57 56 65 56 --- 57 30E | 14 16 13 12 8 16 14 28 6 | 44 43 40 43 41 35 47 49 40 31 | 12 18 11 17 8 10 12 25 5 | 19 33 21 28 24 29 26 27 22 X32E | 10 37 29 --- 23 --- 31 --- 15 | 45 69 54 --- 60 --- 58 --- 51 ------+----------------------------------------------+----------------------------------------------- RMS | 11 15 12 13 7 12 14 27 |T 25 35 28 31 28 32 31 33 28 WRMS | 10 15 12 13 7 12 12 25 |NE 21 30 25 28 24 29 26 30 24 MEDI | 11 14 12 13 6 12 14 26 |MD 21 32 24 26 24 26 28 32 24 Table 3.1463.2 GPS week: 1463 Day: 2 MJD: 54487.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl ngs sio IGS | cod emr esa gfz igr jpl ngs sio IGS ------+----------------------------------------------+----------------------------------------------- 1 | 10 15 12 14 6 9 14 24 5 | 25 33 21 28 24 29 34 35 26 2 | 9 13 15 10 4 11 13 39 6 | 35 36 38 38 35 37 34 50 34 3 | 9 14 11 10 7 8 9 26 4 | 22 32 23 22 22 24 26 28 22 4 | 9 12 14 11 6 8 11 24 5 | 26 31 35 26 30 29 32 32 28 5E | 13 15 13 11 7 14 18 27 6 | 25 27 20 24 24 22 34 29 22 6 | 6 11 12 11 9 9 11 30 5 | 21 28 25 25 26 26 30 35 24 8 | 11 13 10 12 6 9 13 26 5 | 12 19 12 20 14 20 16 26 13 9 | 8 13 11 10 4 10 9 20 4 | 17 22 17 19 16 22 20 12 16 10 | 19 16 18 22 8 13 17 25 7 | 91 98 93 97 97 103 102 99 95 11 | 8 13 12 9 8 15 11 22 5 | 33 43 29 33 34 39 33 33 32 X12E | 15 15 --- 8 8 14 12 28 6 | 31 31 --- 32 32 35 33 43 31 13 | 13 16 14 18 6 12 14 20 6 | 13 33 17 22 20 28 20 19 17 14 | 14 19 14 15 7 10 16 18 6 | 19 32 21 25 22 27 28 19 22 15 | 13 19 14 13 7 14 14 22 6 | 12 29 15 20 15 22 18 20 14 16E | 9 14 17 12 7 17 19 20 6 | 16 31 21 26 21 30 31 24 21 17 | 14 16 18 14 6 17 13 24 6 | 18 28 22 26 20 27 24 24 18 18E | 24 17 15 13 8 15 17 19 7 | 106 118 111 123 108 114 118 120 115 19 | 12 14 16 12 7 13 11 27 6 | 17 31 26 27 20 30 20 21 21 20 | 12 18 13 10 6 12 14 27 6 | 11 30 15 18 18 25 23 24 16 21 | 12 16 15 13 5 14 12 29 6 | 35 40 33 37 34 38 33 42 33 22E | 12 14 14 13 7 12 16 25 6 | 28 33 26 33 27 30 32 29 29 23 | 12 19 13 11 7 13 17 18 6 | 14 36 18 22 21 28 23 24 19 24 | 7 12 12 14 6 9 10 10 4 | 25 32 26 31 29 26 35 27 28 25 | 9 9 9 11 6 8 9 18 4 | 15 21 17 22 17 24 19 20 17 26 | 11 15 10 11 7 10 13 32 5 | 18 25 16 21 19 26 18 45 19 27 | 9 8 11 13 7 8 11 24 4 | 12 20 15 22 16 22 19 30 15 28E | 14 19 13 15 8 16 16 29 6 | 28 35 31 26 28 32 29 41 27 X29 | 14 18 17 14 13 18 19 --- 7 | 78 87 80 82 80 87 82 --- 81 30E | 16 16 19 12 8 17 13 25 6 | 44 44 39 45 40 35 49 44 40 31 | 12 15 14 15 5 14 14 32 6 | 16 31 14 24 19 28 27 30 19 X32E | 20 32 30 --- 36 --- 42 --- 18 | 68 72 79 --- 81 --- 81 --- 74 ------+----------------------------------------------+----------------------------------------------- RMS | 12 15 14 13 7 12 14 25 |T 30 38 31 33 32 35 36 35 31 WRMS | 11 15 14 13 7 12 10 24 |NE 25 35 27 30 28 33 31 31 27 MEDI | 12 15 14 12 7 12 13 25 |MD 22 32 22 26 24 28 30 29 22 Table 3.1463.3 GPS week: 1463 Day: 3 MJD: 54488.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl ngs sio IGS | cod emr esa gfz igr jpl ngs sio IGS ------+----------------------------------------------+----------------------------------------------- 1 | 8 15 13 13 5 10 12 25 5 | 32 41 36 40 36 41 37 40 36 2 | 14 13 14 12 8 12 19 39 6 | 42 45 39 42 43 44 42 40 40 3 | 8 16 12 7 8 12 15 40 6 | 18 25 30 21 25 20 28 34 21 4 | 11 10 13 14 8 11 17 27 5 | 30 30 27 27 32 26 38 34 28 5E | 13 18 11 10 9 17 23 27 6 | 29 33 27 32 30 29 41 39 30 6 | 7 8 11 7 5 12 8 29 4 | 23 30 31 25 27 25 27 34 25 8 | 9 9 12 10 7 11 14 16 4 | 15 19 17 19 18 22 19 24 15 9 | 8 13 11 9 3 9 11 25 4 | 19 26 17 22 19 24 21 19 18 10 | 14 21 14 13 4 15 14 22 6 | 58 61 58 62 60 66 59 65 59 11 | 10 14 15 10 12 18 15 20 5 | 36 47 44 37 39 43 37 38 38 X12E | 18 14 --- 6 8 19 14 28 7 | 53 58 --- 53 54 58 57 47 53 13 | 12 16 17 14 10 13 13 23 6 | 16 34 25 25 26 30 23 21 21 14 | 11 19 16 12 6 16 15 28 6 | 20 31 20 26 24 30 25 29 22 15 | 13 18 16 12 5 13 13 21 6 | 18 31 20 24 21 25 21 19 19 16E | 10 15 25 9 5 16 16 25 6 | 18 28 32 23 22 30 28 26 21 17 | 17 16 20 14 8 19 13 23 7 | 17 27 20 26 18 29 20 16 18 18 | 10 14 14 8 10 18 15 22 5 | 64 67 64 64 63 61 66 58 62 19 | 10 11 19 11 5 15 15 30 6 | 16 25 21 24 19 26 23 20 18 20 | 12 17 13 11 7 13 16 22 5 | 12 27 13 19 17 24 15 26 15 21 | 8 13 13 12 7 13 13 26 5 | 33 40 31 33 33 38 35 29 33 22 | 17 16 14 9 4 14 13 14 5 | 26 37 36 34 33 33 35 31 31 23 | 15 18 13 9 9 16 15 29 6 | 16 37 25 26 25 33 20 37 23 24 | 8 11 10 10 5 11 10 16 4 | 28 33 33 29 33 30 34 39 30 25 | 8 6 13 10 5 11 11 21 4 | 13 22 19 19 17 24 18 22 16 26 | 11 12 9 12 6 9 15 33 5 | 20 27 24 28 24 27 22 45 23 27 | 7 7 13 9 5 10 12 22 4 | 15 21 18 20 18 24 19 27 17 28E | 11 14 15 10 10 20 17 23 6 | 40 48 42 36 41 46 38 58 40 X29 | 15 17 16 12 12 21 19 --- 7 | 120 129 127 123 123 128 122 --- 123 30E | 16 15 13 12 9 18 11 32 6 | 43 43 38 47 41 36 48 55 42 31 | 11 15 15 15 8 16 17 19 6 | 18 32 19 27 24 31 27 25 21 X32E | 32 38 20 --- 32 --- 37 --- 19 | 48 78 68 --- 65 --- 70 --- 60 ------+----------------------------------------------+----------------------------------------------- RMS | 11 14 14 11 7 14 14 26 |T 30 39 34 34 34 36 35 34 32 WRMS | 11 14 14 11 7 14 11 24 |NE 29 37 32 33 32 36 33 32 30 MEDI | 11 15 13 10 7 13 15 25 |MD 23 33 27 27 27 30 28 34 25 Table 3.1463.4 GPS week: 1463 Day: 4 MJD: 54489.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl ngs sio IGS | cod emr esa gfz igr jpl ngs sio IGS ------+----------------------------------------------+----------------------------------------------- 1 | 10 23 12 14 7 11 13 25 6 | 17 34 28 27 22 30 26 31 24 2 | 11 13 15 11 7 11 15 39 6 | 29 31 38 31 31 32 37 25 30 3 | 8 13 10 7 5 12 11 41 5 | 17 23 21 16 20 18 22 30 17 4 | 7 9 15 11 8 8 14 24 5 | 27 27 37 24 28 26 32 32 26 5E | 16 17 14 12 7 15 29 25 7 | 23 27 25 25 25 24 42 32 22 6 | 5 10 15 9 5 9 11 28 4 | 29 30 34 29 29 29 34 42 30 8 | 7 11 13 11 5 10 11 20 4 | 12 19 20 18 18 20 19 20 14 9 | 8 13 11 9 5 8 12 25 4 | 16 22 24 22 18 21 23 21 17 10 | 11 24 15 16 8 15 16 30 7 | 35 55 44 41 34 43 40 54 39 11 | 8 12 13 11 10 15 12 30 5 | 35 44 41 37 34 39 35 34 35 12E | 14 16 16 8 7 17 15 22 6 | 20 32 31 21 22 32 30 21 23 13 | 10 15 14 15 7 10 11 25 5 | 13 32 28 22 21 28 16 21 18 14 | 12 19 16 15 7 13 17 20 6 | 15 29 26 24 20 24 23 22 19 15 | 15 18 16 14 6 14 18 24 6 | 15 31 25 25 20 24 28 19 18 16E | 9 15 17 12 6 18 19 26 6 | 13 23 24 22 18 25 29 25 17 17 | 13 17 19 15 8 15 13 22 6 | 18 26 29 26 18 27 24 22 18 18 | 10 15 13 10 9 12 14 18 5 | 37 42 45 38 38 39 35 37 37 19 | 11 12 19 12 7 14 12 27 6 | 15 25 24 23 17 26 19 18 17 20 | 10 16 14 11 5 15 16 23 5 | 9 25 25 17 13 24 21 19 13 21 | 10 14 12 11 5 13 11 35 5 | 24 34 33 30 27 32 30 30 28 22 | 12 14 10 10 6 13 11 16 5 | 26 31 31 28 24 27 27 25 25 23 | 11 16 13 11 5 12 13 34 6 | 13 32 29 22 20 28 20 37 19 24 | 9 11 10 14 5 10 9 32 5 | 23 28 32 28 27 22 32 33 25 25 | 7 9 13 10 5 9 10 18 4 | 14 22 26 19 17 21 21 24 17 26 | 11 13 11 10 5 13 14 38 6 | 15 25 25 21 16 24 20 48 18 27 | 6 11 14 11 6 9 13 27 5 | 14 21 23 20 16 20 20 25 16 28E | 10 12 17 10 6 15 13 29 5 | 16 28 25 21 21 28 23 36 19 X29 | 13 17 20 12 13 19 16 --- 7 | 94 99 95 98 99 101 97 --- 96 30E | 20 16 15 15 8 15 16 29 7 | 45 42 42 42 42 35 51 53 41 31 | 10 17 17 15 12 13 19 28 6 | 13 29 24 23 19 26 25 25 17 X32E | 24 30 18 --- 21 --- 30 --- 15 | 85 93 88 --- 93 --- 96 --- 87 ------+----------------------------------------------+----------------------------------------------- RMS | 11 15 14 12 7 13 15 28 |T 25 34 33 28 27 29 32 29 27 WRMS | 10 15 14 12 7 13 11 26 |NE 23 32 32 28 25 30 29 28 25 MEDI | 10 15 14 11 7 13 13 26 |MD 17 29 28 24 21 26 27 25 19 Table 3.1463.5 GPS week: 1463 Day: 5 MJD: 54490.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl ngs sio IGS | cod emr esa gfz igr jpl ngs sio IGS ------+----------------------------------------------+----------------------------------------------- 1 | 10 19 10 12 6 11 12 22 5 | 25 36 28 30 26 30 28 33 26 2 | 10 12 13 13 6 16 12 24 5 | 28 31 29 30 28 33 30 25 26 3 | 6 12 8 7 6 10 14 33 5 | 20 23 22 18 19 24 25 29 20 4 | 7 11 10 13 8 9 13 17 4 | 23 24 25 22 22 23 24 29 21 5E | 13 18 16 11 6 17 26 22 7 | 24 28 23 24 24 25 41 35 23 6 | 6 11 10 6 6 11 9 17 4 | 36 39 35 37 38 43 43 41 38 8 | 8 12 11 11 5 11 14 21 5 | 14 24 16 19 18 24 22 29 17 9 | 8 10 10 9 5 10 10 26 4 | 13 22 19 20 16 20 19 22 16 10 | 13 18 13 14 6 17 14 42 7 | 33 43 32 41 36 44 36 54 35 11 | 7 13 10 10 8 15 11 36 5 | 28 42 31 32 31 39 28 25 30 12E | 14 15 14 10 7 16 12 21 5 | 24 31 21 27 25 33 23 28 25 13 | 12 15 11 17 7 14 12 19 5 | 12 33 18 24 21 29 17 19 18 14 | 12 17 13 12 6 10 12 21 5 | 13 26 17 22 18 23 23 22 16 15 | 15 20 18 12 6 15 13 30 6 | 10 29 21 20 17 24 26 22 15 16E | 13 14 16 10 6 19 15 19 6 | 15 28 28 24 20 29 23 21 20 17 | 12 19 15 15 7 17 14 22 6 | 14 29 11 22 15 24 18 15 12 18 | 11 19 12 10 7 15 11 19 5 | 25 36 30 28 27 31 30 33 27 19 | 11 14 14 14 5 16 16 29 6 | 11 28 17 23 17 28 18 20 16 20 | 11 16 11 9 5 15 11 21 5 | 7 26 13 17 14 25 13 19 12 21 | 9 12 13 12 5 13 13 29 5 | 23 29 25 26 23 29 23 32 22 22 | 12 16 10 10 6 13 14 20 5 | 15 25 21 19 18 23 22 22 17 23 | 12 17 11 10 6 12 12 19 5 | 15 35 21 23 21 30 20 23 20 24 | 7 12 9 13 4 9 11 20 4 | 22 27 27 25 23 27 28 26 23 25 | 7 10 9 10 4 9 11 20 4 | 15 22 19 18 19 25 19 27 18 26 | 13 12 12 10 6 13 12 35 6 | 15 24 23 26 20 25 21 46 21 27 | 7 12 10 10 4 11 11 23 4 | 15 24 20 21 19 25 17 34 18 28E | 10 15 15 13 5 15 14 24 6 | 28 45 31 32 31 37 32 47 32 X29 | 15 19 16 12 13 21 18 --- 7 | 115 129 119 120 124 132 125 --- 122 30E | 17 16 13 10 6 18 16 25 6 | 44 45 36 44 40 36 51 49 40 31 | 13 17 14 16 8 14 14 21 6 | 13 29 15 23 18 27 20 18 15 X32E | 18 25 22 --- 29 --- 25 --- 13 | 71 76 75 --- 91 --- 92 --- 76 ------+----------------------------------------------+----------------------------------------------- RMS | 11 15 12 12 6 14 13 25 |T 24 35 28 28 28 32 30 29 27 WRMS | 10 15 12 12 6 14 11 23 |NE 22 33 26 28 25 32 27 27 24 MEDI | 11 15 12 11 6 14 13 22 |MD 20 29 23 24 21 27 23 27 21 Table 3.1463.6 GPS week: 1463 Day: 6 MJD: 54491.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz igr jpl ngs sio IGS | cod emr esa gfz igr jpl ngs sio IGS ------+----------------------------------------------+----------------------------------------------- 1 | 9 26 12 14 7 9 15 23 6 | 17 31 24 26 21 26 29 30 22 2 | 11 15 13 10 6 15 10 24 5 | 36 39 38 38 36 39 35 38 35 3 | 8 17 9 5 8 9 12 30 5 | 20 28 25 22 25 23 27 23 22 4 | 8 12 10 13 5 8 10 15 4 | 37 36 39 33 39 35 41 39 36 5E | 17 23 14 14 8 17 26 22 7 | 36 38 34 36 33 32 50 42 33 6 | 8 12 12 7 7 11 10 17 4 | 30 34 33 29 33 32 34 26 30 8 | 8 12 7 10 5 9 8 29 4 | 18 21 19 21 21 21 23 28 18 9 | 9 14 8 9 6 6 8 16 4 | 19 21 19 21 19 20 20 13 18 10 | 12 18 10 16 5 12 11 36 6 | 54 63 55 61 57 60 54 67 56 11 | 8 14 13 9 10 16 13 27 5 | 46 57 49 47 46 48 45 38 46 12E | 14 15 14 9 6 22 17 21 6 | 28 32 24 31 31 36 42 22 30 13 | 9 17 15 13 5 9 9 17 5 | 16 33 22 23 22 28 18 21 19 14 | 11 22 14 14 8 11 11 22 5 | 16 29 20 25 21 24 23 23 19 15 | 15 19 15 15 6 12 13 23 6 | 15 31 20 24 19 22 23 19 17 16E | 11 16 14 9 3 19 13 21 5 | 18 28 22 23 21 32 23 16 21 17 | 12 16 14 15 6 14 12 23 6 | 18 30 22 28 20 26 17 22 18 18 | 10 17 11 10 5 14 13 25 5 | 37 45 42 37 39 40 37 45 38 19 | 11 15 15 13 6 11 13 28 6 | 15 30 22 28 21 30 20 16 19 20 | 9 18 16 11 5 16 14 20 5 | 11 27 16 21 18 26 16 18 14 21 | 10 16 12 11 4 14 11 28 5 | 31 39 32 33 32 35 32 36 31 22 | 10 17 11 11 6 10 9 26 5 | 22 31 23 23 22 24 24 32 21 23 | 10 16 14 10 5 11 13 26 5 | 14 32 21 23 19 26 18 21 18 24 | 9 16 10 12 4 9 9 29 5 | 35 39 40 35 37 34 38 48 36 25 | 7 13 8 10 4 9 7 21 4 | 18 21 21 21 22 21 21 23 19 26 | 12 17 10 11 6 11 14 34 6 | 18 28 21 21 18 23 21 43 19 27 | 7 13 6 11 5 10 12 30 5 | 19 23 22 23 23 22 24 32 20 28E | 11 17 16 9 10 14 17 23 6 | 37 43 35 37 36 39 37 42 36 X29 | 16 20 19 14 14 22 16 --- 8 | 113 122 122 110 113 122 112 --- 115 30E | 17 21 15 14 8 15 19 31 7 | 45 42 38 41 40 36 52 55 41 31 | 13 22 14 14 7 14 15 18 6 | 14 30 15 24 19 26 19 19 16 X32 | 28 24 26 --- 33 --- 37 --- 17 | 80 85 79 --- 66 --- 72 --- 76 ------+----------------------------------------------+----------------------------------------------- RMS | 11 17 12 12 6 13 13 25 |T 30 38 32 32 31 33 33 30 30 WRMS | 10 17 12 12 6 13 10 25 |NE 29 38 33 31 31 33 32 30 30 MEDI | 10 17 13 11 6 11 13 23 |MD 20 32 24 26 23 28 27 28 22 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 4.1463 GPS week: 1463 MJD: 54485.0-54491.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ igs | igs 2965 | 12 9 29 | 13 15 59 | 8 10 20 | 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 5.1463.0 GPS week: 1463 Day: 0 MJD: 54485.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ igs | igs 2969 | 12 9 34 | 22 28 147 | 7 9 23 | Table 5.1463.1 GPS week: 1463 Day: 1 MJD: 54486.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ igs | igs 2951 | 13 9 34 | 19 16 63 | 9 12 19 | Table 5.1463.2 GPS week: 1463 Day: 2 MJD: 54487.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ igs | igs 2965 | 11 10 32 | 11 10 41 | 6 7 18 | Table 5.1463.3 GPS week: 1463 Day: 3 MJD: 54488.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ igs | igs 2972 | 8 6 21 | 12 16 52 | 8 11 24 | Table 5.1463.4 GPS week: 1463 Day: 4 MJD: 54489.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ igs | igs 2970 | 17 12 33 | 9 9 34 | 8 8 18 | Table 5.1463.5 GPS week: 1463 Day: 5 MJD: 54490.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ igs | igs 2958 | 10 9 22 | 12 14 42 | 9 11 17 | Table 5.1463.6 GPS week: 1463 Day: 6 MJD: 54491.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ igs | igs 2974 | 10 9 27 | 8 10 31 | 9 11 23 | 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 : 21-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 6.1463 GPS week: 1463 MJD: 54485.500-54491.500 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 13 -15 -16 1 | -3 18 | 20 23 74 74 8 | 3 emr uuuuu | -9 10 33 -134 -10 | 53 57 | 27 29 149 121 15 | 4 esa uuuux | 21 9 -72 2 -32 | 27 45 | 22 27 117 52 18 | 12 gfz uuuuu | 34 4 36 10 6 | 0 19 | 11 26 29 67 14 | 3 igr xxxxx | 22 12 67 3 3 | 1 18 | 33 30 61 80 9 | 2 irf xxxxx | 1 15 -19 23 -5 | 3 19 | 13 17 46 51 11 | 3 jpl uuuuu | 23 -13 -9 83 -12 | 21 30 | 27 10 117 62 11 | 2 ngs uuuuu | -62 19 59 39 3 | -4 12 | 35 60 98 65 10 | 2 sio uuuuu | -28 -133 -30 -20 -1 | 2 17 | 24 39 69 105 8 | 3 Table 7.1463.0 GPS week: 1463 Day: 0 MJD: 54485.500 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 11 -50 24 -10 | 0 16 emr uuuuu | -12 31 -181 -172 -23 | 60 61 esa uuuux | 7 -44 113 35 -50 | 46 52 gfz uuuuu | 39 44 9 98 -18 | 1 16 igr xxxxx | 82 48 -62 74 -4 | 4 18 irf xxxxx | 16 33 -41 90 -18 | 9 16 jpl uuuuu | 43 -7 81 -39 5 | 24 32 ngs uuuuu | -68 -12 50 64 19 | -4 13 sio uuuuu | -30 -92 -50 -71 1 | 6 18 Table 7.1463.1 GPS week: 1463 Day: 1 MJD: 54486.500 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 | -34 10 -50 -68 -8 | -3 20 emr uuuuu | 10 26 -49 -10 -27 | 57 60 esa uuuux | -7 31 -72 32 -56 | 39 52 gfz uuuuu | 14 25 40 -84 -4 | -1 20 igr xxxxx | -6 31 76 109 -11 | 2 19 irf xxxxx | -16 3 -60 96 -14 | 5 20 jpl uuuuu | 51 -3 67 85 -4 | 22 31 ngs uuuuu | -9 -54 72 77 13 | -6 14 sio uuuuu | -56 -149 53 -27 -10 | 4 19 Table 7.1463.2 GPS week: 1463 Day: 2 MJD: 54487.500 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 | -24 57 35 -9 8 | -7 20 emr uuuuu | 25 -31 -52 -53 -21 | 53 58 esa uuuux | 52 8 -32 -61 -41 | 32 50 gfz uuuuu | 31 4 -10 -19 1 | -3 19 igr xxxxx | 5 -42 97 -124 6 | -1 19 irf xxxxx | -13 -8 -75 6 -13 | 2 20 jpl uuuuu | -12 -28 -76 80 -6 | 20 30 ngs uuuuu | -57 24 124 66 1 | -6 14 sio uuuuu | -18 -126 25 -61 -4 | 1 18 Table 7.1463.3 GPS week: 1463 Day: 3 MJD: 54488.500 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 | -9 1 -146 -42 1 | -6 20 emr uuuuu | -3 56 45 -54 -13 | 51 56 esa uuuux | 13 26 -225 -14 -29 | 26 46 gfz uuuuu | 28 15 40 -55 12 | -3 19 igr xxxxx | -3 17 58 53 0 | -1 19 irf xxxxx | 0 24 13 -7 -9 | 1 19 jpl uuuuu | -8 -2 177 131 -16 | 20 30 ngs uuuuu | -32 -46 213 53 5 | -5 14 sio uuuuu | 8 -133 -118 66 -10 | -1 16 Table 7.1463.4 GPS week: 1463 Day: 4 MJD: 54489.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 2 29 78 -128 8 | -5 19 emr uuuuu | 2 -11 72 -77 -4 | 49 54 esa uuuux | 3 21 -202 82 -14 | 20 42 gfz uuuuu | 38 -34 37 16 23 | -3 19 igr xxxxx | 9 -13 123 -27 1 | 0 18 irf xxxxx | 8 27 -40 -31 1 | 0 19 jpl uuuuu | 16 -18 -73 113 -25 | 20 30 ngs uuuuu | -68 36 63 110 -8 | -3 12 sio uuuuu | -14 -80 -38 -190 0 | -1 17 Table 7.1463.5 GPS week: 1463 Day: 5 MJD: 54490.500 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 | 13 -12 17 104 9 | 0 17 emr uuuuu | -32 8 104 -217 7 | 51 56 esa uuuux | 40 30 4 1 -15 | 18 42 gfz uuuuu | 38 -15 74 45 17 | 3 20 igr xxxxx | 15 17 71 -24 13 | 3 16 irf xxxxx | 14 -4 37 23 5 | 2 19 jpl uuuuu | 51 -11 -121 61 -22 | 23 29 ngs uuuuu | -118 79 -97 -77 -5 | -1 8 sio uuuuu | -27 -194 33 10 5 | 3 14 Table 7.1463.6 GPS week: 1463 Day: 6 MJD: 54491.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 22 -4 12 10 0 | -1 16 emr uuuuu | -55 -8 290 -353 10 | 49 53 esa uuuux | 38 -9 -88 -60 -16 | 10 32 gfz uuuuu | 50 -8 60 72 12 | 4 21 igr xxxxx | 51 27 104 -41 13 | 3 16 irf xxxxx | 0 27 35 -16 11 | 1 17 jpl uuuuu | 16 -22 -118 151 -15 | 19 26 ngs uuuuu | -84 105 -13 -21 -3 | -3 7 sio uuuuu | -63 -160 -114 136 12 | 2 14