Date: Thu, 19 Feb 2009 12:58:46 +0000 From: Jim Ray Subject: [IGSREPORT-17131] Wk 1517 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <499d5786.ifhdnK6H5YYvQukd%igs.acc@noaa.gov> Content-type: text/plain; charset=us-ascii Content-transfer-encoding: 7bit User-Agent: nail 11.25 7/29/05 Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 19 Feb 04:58:54 PST 2009 Message Number 17131 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1517 (Feb 01, 2009 - Feb 07, 2009) Contacts: J. Ray (jim.ray@noaa.gov), J. Griffiths (jake.griffiths@noaa.gov) 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: igs1517[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1517[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1517[0-6].cls IGS GPS clock combination summary report. igs15177.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15177.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, 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. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and 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 | YELL 0 | EMR | DAEJ DAEJ MIZU 0 | GFZ | 7 15 29 AUCK DAEJ HARB 0 | GRG | NLIB RABT 0 | MIT | HARB 1 | EMR | HARB HARB MIZU WTZR 1 | ESA | AREQ PETP 1 | GFZ | 7 15 29 DAEJ ONSA SCH2 1 | GRG | NLIB 1 | JPL | AREQ HARB 1 | MIT | WTZR 2 | EMR | 21 HARB HARB MATE MIZU WTZR 2 | GFZ | 7 15 21 29 IRKT KERG THTI WTZR 2 | GRG | NLIB 2 | JPL | HARB ZWE2 2 | MIT | DAEJ MDVJ SANT 3 | COD | YELL 3 | EMR | SYOG YELL DAEJ SYOG WTZR YELL 3 | ESA | MAL2 YELL 3 | GFZ | 7 13 29 TIXI 3 | GRG | NLIB 3 | MIT | 2 OUS2 WTZR 4 | EMR | IENG MCM4 MIZU 4 | ESA | YELL 4 | GFZ | 7 15 29 FAA1 VESL 4 | GRG | NLIB 4 | MIT | 10 MAW1 5 | EMR | MIZU WTZR 5 | ESA | 30 5 | GFZ | 7 13 15 29 30 HARB 5 | GRG | NLIB 5 | JPL | 30 5 | MIT | 10 10 WTZR ALIC DARW HARB WTZR 6 | ALL | 25 6 | EMR | HARB 6 | ESA | 23 UNSA 6 | GFZ | 7 15 23 FAA1 6 | GRG | NLIB 6 | JPL | 23 HARB 6 | MIT | 25 ALIC BAKO BOR1 BRAZ HYDE OUS2 5. New clock offsets and drifts were estimated for centres showing reference clock resets. Note that only the largest clock offset and drift are output to the summary file. However, the clock combination and the listed RMS include all the clock segments. In summary, the following clock shifts/resets were noticed and accounted for: Day | Centre | Time | Jump ----+--------+--------+------------- 3 | MIT | ~00:00 | ~ -0.43 ns 6. 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. 7. 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 | .4 .1 1.4 -16 -4 -7 -.10 EMR | 13.2 -9.7 -15.2 129 -6 46 .23 ESA | 8.0 2.2 -3.1 3 -104 23 .14 GFZ | 1.2 .3 1.7 13 -34 6 -.42 GRG | 2.8 -1.4 -10.4 -21 -9 6 .13 JPL | 5.8 3.3 -1.3 -19 -39 11 .01 MIT | 7.0 -3.7 -14.8 -17 -2 -6 -.12 NGS | 6.8 -2.8 -.9 -39 -107 10 .03 SIO | 1.5 -5.1 -12.4 -83 -64 10 .24 8. 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. 9. 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. 10. 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 1.1517.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1517.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 2.1517.[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 3.1517.[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 5.1517.0-6). 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 1517 summary. (Feb 01, 2009 - Feb 07, 2009) Table 1.1517.a GPS week: 1517 MJD: 54863.000-54869.000 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 235| 0 0 3 7 -56 -19 -.12 9 8 | -66 -651 14 109 | 0 0 1 6 17 13 .03 | 183 368 emr 75| 0 0 2 -269 -79 -59 .49 19 19 | 756 -86 19 178 | 1 1 0 46 23 14 .04 | 1623 827 esa 128| 1 0 0 -25 37 -2 .30 9 9 | 124 -925 20 123 | 0 0 2 30 48 19 .01 | 370 1024 gfz 193| 0 0 -3 -38 -6 55 -.16 9 9 | 354 -244 21 132 | 0 0 1 12 16 44 .03 | 476 828 grg 78| 0 0 10 21 -48 28 1.07 40 38 | 132 -437 208 322 | 1 2 3 20 31 97 .09 | 304 671 igr n/a| 0 0 1 -4 -59 -18 .05 5 5 | 9304 -320 20 90 | 0 0 0 10 17 29 .03 | 1901 920 jpl 127| 0 1 4 12 15 18 .53 18 17 | 2525 -195 18 104 | 1 1 1 12 28 28 .02 | 1608 930 mit 260| 0 -1 -7 54 -104 -1 -.31 13 12 | 38 -489 24 194 | 1 0 1 30 34 14 .02 | 400 1042 ngs 217| 0 0 2 89 133 -32 -.30 10 8 | -101 -604 2331 4053 | 0 0 1 43 66 19 .05 | 220 394 sio 258| 1 3 -2 160 50 5 .02 23 22 | --- --- --- --- | 0 1 2 20 38 21 .03 | --- --- Table 1.1517.b GPS week : 1517 MJD: 54863.000-54869.000 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 ------+------------------------------------+------------------------------------------ 2 | 5 5 5 6 5 6 6 | 3 | 4 5 4 5 5 5 5 | 4 | 4 4 4 4 4 5 4 | 5 | 4 5 5 4 4 4 4 | 6 | 4 5 4 4 5 5 5 | 7 | 6 5 5 5 5 5 5 | 8 | 4 5 4 4 4 4 4 | 9 | 3 4 4 4 4 3 4 | 10 | 4 5 4 4 4 5 4 | 11 | 5 5 4 4 5 5 5 | 12 | 5 5 5 5 5 5 5 | 13 | 4 5 4 4 4 4 5 | 14 | 6 5 4 4 5 4 5 | 15 | 6 5 5 5 5 6 6 | 16 | 7 5 5 5 5 6 6 | 17 | 5 5 5 5 5 5 5 | 18 | 5 5 4 5 5 5 5 | 19 | 6 6 5 5 5 5 6 | 20 | 5 5 5 5 5 5 6 | 21 | 4 4 4 4 5 5 5 | 22 | 5 5 5 4 5 4 5 | 23 | 5 5 5 5 5 5 5 | 24 | 4 4 3 4 4 4 4 | 25 | 5 5 4 4 4 4 5 | 26 | 5 6 6 6 6 7 8 | 27 | 5 5 5 4 4 5 5 | 28 | 4 4 4 4 4 5 4 | 29 | 6 6 5 5 5 5 6 | 30 | 5 5 4 4 4 4 4 | 31 | 5 6 5 5 5 5 5 | 32 | 5 5 4 4 5 5 5 | 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 2.1517.0 GPS week: 1517 Day: 0 MJD: 54863.000 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 235| 0 0 1 3 -81 -24 -.12 9 8 | -18 -1017 12 107 | 74 -10 | emr 75| 1 0 3 -325 -105 -67 .51 19 19 | 2481 -1035 16 138 | 148 43 | esa 128| 2 1 0 -9 122 -2 .31 10 9 | 7 -826 22 118 | 3 -79 | gfz 193| -1 0 0 -28 -29 116 -.20 9 9 | 1279 -1992 22 118 | 34 -20 | grg 78| 0 3 12 7 -13 -112 .95 39 39 | 711 -1545 80 192 | 68 58 | igr n/a| 0 0 2 -10 -67 -21 .02 5 5 | 11683 -1478 19 78 | 25 -7 | jpl 127| 0 2 2 15 50 7 .53 17 15 | 4330 -1441 18 101 | 58 -26 | mit 260| 2 0 -5 70 -70 -19 -.30 13 13 | 816 -1567 23 184 | -9 13 | ngs 217| 0 0 2 56 35 -59 -.29 10 8 | -43 -1005 2333 4031 | 22 111 | sio 516| 0 1 -4 192 84 -31 .04 22 23 | --- --- --- --- | -101 -72 | Table 2.1517.1 GPS week: 1517 Day: 1 MJD: 54864.000 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 235| 0 0 1 7 -75 -14 -.14 10 9 | -439 -481 13 107 | 42 10 | emr 75| 0 2 3 -314 -114 -69 .49 19 19 | 2093 -598 21 180 | 145 30 | esa 128| 1 1 1 9 77 -5 .30 8 8 | -498 -881 21 125 | -24 -46 | gfz 193| 0 0 -3 -31 -10 80 -.13 10 10 | -86 -13 23 137 | 41 -2 | grg 78| -1 1 13 35 -93 190 .96 39 37 | -128 -153 244 347 | 82 48 | igr n/a| 0 1 1 -10 -54 -31 .01 5 5 | 10784 -852 24 77 | 14 -65 | jpl 127| -2 0 6 9 31 -2 .51 18 17 | 3586 -536 19 115 | 56 -55 | mit 260| 2 -2 -5 85 -53 3 -.33 12 11 | -264 -42 21 122 | -20 1 | ngs 217| 1 0 0 47 49 -40 -.39 11 9 | -565 -294 2599 4536 | 76 110 | sio 516| 0 2 -3 173 90 3 .03 22 24 | --- --- --- --- | -80 -79 | Table 2.1517.2 GPS week: 1517 Day: 2 MJD: 54865.000 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 235| 0 0 1 10 -54 -15 -.08 9 8 | -155 -275 11 94 | 51 -83 | emr 75| 1 2 1 -305 -76 -76 .53 20 20 | 1889 -785 17 183 | 135 -3 | esa 128| 1 0 4 12 47 -23 .29 8 8 | 210 -813 21 131 | -5 6 | gfz 193| -1 0 -3 -37 -8 47 -.17 8 8 | 174 267 20 124 | 47 -70 | grg 78| 1 0 11 28 -43 3 1.07 41 39 | 355 -1122 233 341 | 87 -66 | igr n/a| 0 0 1 2 -28 -38 .08 6 6 | 10386 -961 20 79 | -2 -66 | jpl 127| -1 1 4 18 28 7 .53 19 18 | 3468 -732 18 116 | 67 -17 | mit 260| 1 0 -8 82 -157 16 -.30 11 11 | 301 -851 19 128 | -27 27 | ngs 217| -1 0 2 31 166 -7 -.31 9 6 | -174 -257 2372 4331 | 9 -9 | sio 516| 1 2 -4 164 -17 1 -.01 21 19 | --- --- --- --- | -49 -53 | Table 2.1517.3 GPS week: 1517 Day: 3 MJD: 54866.000 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 235| 0 0 3 12 -47 -15 -.11 8 8 | -27 -703 13 108 | 40 -22 | emr 75| 0 2 2 -268 -73 -70 .52 19 19 | 966 1174 18 198 | 80 8 | esa 128| 0 1 2 -40 -7 -30 .29 9 9 | 312 -880 20 116 | 44 31 | gfz 193| 0 0 -3 -36 17 78 -.14 8 8 | 245 -193 22 129 | 30 -76 | grg 78| 2 1 12 -6 -75 52 1.11 41 38 | 121 17 234 356 | 68 -17 | igr n/a| -1 0 1 -2 -54 -59 .05 6 6 | 9315 1278 19 84 | 30 -18 | jpl 127| 0 1 4 18 -18 36 .52 18 18 | 2738 1500 19 86 | 72 13 | mit 260| 1 -1 -7 66 -110 -21 -.32 12 11 | 57 256 20 133 | -28 15 | ngs 217| 0 0 0 94 170 -27 -.25 10 8 | -50 -688 2351 3977 | -19 50 | sio 516| 0 5 -2 145 38 -9 .02 23 22 | --- --- --- --- | -41 -38 | Table 2.1517.4 GPS week: 1517 Day: 4 MJD: 54867.000 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 235| 0 0 3 17 -31 -36 -.08 8 8 | 113 -651 14 95 | 38 -65 | emr 75| 1 0 2 -209 -80 -41 .54 19 19 | 664 -340 19 189 | 19 33 | esa 128| 1 0 1 -67 24 16 .31 10 9 | 713 165 20 118 | 74 29 | gfz 193| 0 0 -4 -48 -16 40 -.11 8 8 | 697 462 22 117 | 34 -55 | grg 78| -1 -1 6 54 -43 -39 1.12 40 37 | 9 164 251 397 | 33 -34 | igr n/a| 0 0 2 14 -62 10 .10 6 5 | 9193 -323 22 101 | -1 60 | jpl 127| -1 0 4 16 -21 -13 .52 17 16 | 2706 -188 18 95 | 9 -29 | mit 260| 0 -1 -7 20 -111 12 -.28 11 10 | -153 554 32 178 | -24 21 | ngs 217| 0 0 3 126 213 -18 -.33 10 8 | 92 -630 1971 3578 | -80 -11 | sio 516| 2 4 -2 138 30 23 .05 23 22 | --- --- --- --- | -50 -43 | Table 2.1517.5 GPS week: 1517 Day: 5 MJD: 54868.000 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 235| 0 0 5 -2 -52 3 -.15 9 9 | 13 -216 16 121 | 55 -26 | emr 75| 0 -1 2 -224 -58 -40 .41 19 19 | -938 223 23 180 | 5 -3 | esa 128| 0 0 -2 -43 0 20 .29 8 8 | 172 -3055 19 117 | 59 30 | gfz 193| 0 -1 -2 -60 13 -25 -.20 9 9 | 20 207 19 108 | 37 -50 | grg 78| 0 -2 6 4 -65 93 1.18 42 39 | -119 148 209 306 | 37 24 | igr n/a| 0 0 2 -17 -85 26 .04 5 4 | 7571 -289 20 80 | 33 33 | jpl 127| 0 3 2 24 3 20 .50 17 16 | 1251 -361 17 78 | 43 -55 | mit 260| -1 -1 -8 45 -129 3 -.33 15 13 | -245 352 21 160 | -37 23 | ngs 217| 0 0 2 136 168 -17 -.30 11 9 | 7 -161 2340 3668 | 22 -27 | sio 516| 0 4 0 167 49 30 -.01 23 21 | --- --- --- --- | -75 -62 | Table 2.1517.6 GPS week: 1517 Day: 6 MJD: 54869.000 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 235| 0 0 5 1 -55 -35 -.14 9 9 | 45 -1214 19 133 | 36 -31 | emr 75| -1 0 3 -237 -48 -52 .47 22 22 | -1860 757 22 183 | 10 -18 | esa 128| 1 -1 -3 -37 -4 7 .28 9 9 | -46 -190 21 136 | 49 29 | gfz 193| -1 0 -2 -25 -12 48 -.18 8 8 | 153 -447 22 195 | 9 -20 | grg 78| 0 1 9 23 -7 9 1.15 38 37 | -22 -570 211 319 | 41 -7 | igr n/a| 0 0 1 -8 -60 -12 .07 5 5 | 6198 383 22 133 | 1 5 | jpl 127| 1 0 3 -13 36 70 .56 18 16 | -399 388 20 137 | 18 -108 | mit 260| -1 0 -8 7 -101 -7 -.29 16 15 | -245 -2125 35 457 | -20 10 | ngs 217| -1 0 3 132 132 -54 -.23 11 8 | 26 -1197 2353 4250 | -21 28 | sio 516| 1 2 1 137 79 22 -.00 25 21 | --- --- --- --- | -64 -83 | 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 3.1517.0 GPS week: 1517 Day: 0 MJD: 54863.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 7 10 10 8 56 6 10 9 9 38 4 | 26 31 29 34 40 30 28 26 29 29 28 3 | 8 15 8 8 26 6 11 13 10 18 4 | 26 29 25 27 33 26 28 30 26 31 25 4 | 7 10 8 6 34 6 10 9 10 24 3 | 35 41 36 39 31 39 36 35 40 34 36 5 | 11 18 10 7 30 5 11 15 8 17 4 | 22 34 25 25 32 24 29 24 23 28 23 6 | 8 14 10 6 27 5 12 10 12 19 4 | 28 37 30 26 45 27 38 25 22 42 28 7 | 9 25 9 17 39 5 20 14 8 17 5 | 26 40 29 34 43 28 34 27 29 29 28 8 | 9 14 7 8 34 4 8 13 9 22 4 | 31 35 31 30 44 32 31 32 28 38 29 9 | 6 13 8 5 25 4 8 12 8 11 3 | 24 27 24 24 29 23 27 25 23 22 23 10 | 7 21 7 7 25 5 11 11 12 22 4 | 21 36 26 26 28 24 29 23 21 25 23 11 | 8 19 7 5 55 6 16 18 8 17 4 | 44 50 42 45 41 43 48 52 44 38 43 12E | 8 25 13 11 44 6 17 16 6 15 5 | 20 35 22 21 40 21 29 22 19 25 20 13 | 7 15 8 6 29 2 13 14 8 23 4 | 30 35 32 31 37 32 35 30 33 33 30 14 | 20 20 12 15 41 10 17 10 6 18 5 | 37 58 49 54 62 43 53 49 47 48 49 15E | 7 22 12 12 30 5 23 17 8 27 5 | 24 35 28 27 38 26 32 20 28 31 25 16E | 9 26 13 14 37 4 25 21 12 31 6 | 27 35 31 36 59 29 36 35 26 22 26 17 | 8 18 10 16 45 4 19 11 12 15 5 | 23 35 28 25 47 26 32 20 27 23 23 18 | 7 21 10 6 34 4 19 11 11 21 4 | 24 37 28 25 43 26 38 23 23 26 25 19 | 9 23 13 8 25 5 25 16 11 17 5 | 28 41 32 23 51 28 40 23 26 22 26 20 | 6 19 10 9 50 3 21 12 11 27 5 | 24 31 27 26 45 23 32 23 25 29 23 21 | 7 13 9 5 56 5 14 7 7 27 4 | 27 31 28 33 34 27 27 33 27 37 29 22 | 8 17 9 6 60 5 19 15 10 17 4 | 25 39 29 26 66 27 38 27 24 28 27 23E | 8 21 9 13 40 3 22 15 11 13 5 | 24 31 25 26 43 23 32 25 29 28 24 24 | 7 14 7 4 37 4 8 9 9 21 3 | 29 35 34 37 21 31 31 35 31 32 31 25 | 9 17 9 10 31 5 12 17 7 27 4 | 23 28 25 22 32 23 27 25 26 35 23 26 | 12 17 12 9 45 5 13 13 12 29 5 | 126 127 122 124 132 123 126 123 122 139 124 27 | 10 18 7 7 26 4 9 10 13 33 4 | 27 36 28 27 35 29 31 27 30 47 27 28E | 7 15 10 6 38 4 17 15 11 13 4 | 23 30 26 23 43 24 27 26 22 22 22 29 | 11 25 14 7 31 3 23 12 8 21 5 | 24 34 20 23 44 22 33 21 21 23 20 30 | 9 22 7 6 39 6 15 15 9 19 4 | 22 34 23 24 38 23 29 23 22 24 21 31 | 8 23 13 9 36 4 23 12 10 23 5 | 26 34 37 34 41 30 35 29 31 31 28 32 | 8 17 11 6 47 6 17 12 12 15 4 | 22 27 26 23 30 22 29 23 24 23 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 10 9 39 5 17 13 10 22 |T 29 38 32 32 43 30 36 31 30 33 30 WRMS | 8 19 9 9 39 5 15 13 8 23 |NE 26 34 28 28 38 27 32 27 27 30 26 MEDI | 8 18 10 7 37 5 16 13 10 21 |MD 26 35 28 26 41 27 32 26 26 29 26 Table 3.1517.1 GPS week: 1517 Day: 1 MJD: 54864.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 12 7 13 50 4 16 10 8 37 5 | 19 25 25 26 30 22 21 17 14 22 19 3 | 9 20 9 11 26 7 15 14 12 17 4 | 24 30 26 24 21 25 24 29 21 21 22 4 | 8 10 5 10 54 5 9 9 10 27 4 | 21 23 27 23 28 26 23 21 26 30 22 5 | 10 16 7 10 39 5 12 14 12 17 4 | 25 34 28 28 35 28 29 31 29 32 27 6 | 8 16 9 9 34 6 14 12 13 18 4 | 19 33 23 17 42 22 30 17 20 37 21 7 | 8 24 6 12 40 5 23 10 9 16 4 | 19 32 20 26 32 21 28 18 19 20 18 8 | 14 13 9 9 24 6 10 10 10 22 4 | 27 28 28 29 40 27 27 27 24 36 26 9 | 7 12 10 8 32 5 11 12 13 12 4 | 20 23 24 20 31 23 23 20 20 27 19 10 | 11 13 9 8 39 5 13 14 12 19 4 | 12 24 21 17 36 18 23 19 18 21 16 11 | 8 19 9 8 60 5 19 16 13 16 4 | 28 37 30 31 37 31 34 35 36 25 29 12 | 5 28 9 14 39 5 17 11 9 14 5 | 19 36 21 20 38 21 26 22 22 27 20 13 | 17 16 7 10 31 4 18 11 9 25 5 | 41 46 43 45 56 45 49 44 44 41 42 14E | 11 19 7 12 27 4 23 9 10 18 5 | 20 30 21 23 36 21 30 25 30 21 22 15E | 9 19 11 9 32 6 19 12 12 22 5 | 22 30 25 20 35 24 31 16 17 26 20 16 | 9 26 8 11 49 5 24 14 9 18 5 | 19 33 26 21 60 23 31 24 23 27 22 17 | 11 19 8 8 38 6 20 11 12 17 4 | 14 26 20 13 33 16 24 13 17 12 13 18 | 8 21 7 8 32 5 21 9 9 19 4 | 10 30 16 12 33 14 28 13 18 17 13 19 | 6 24 11 13 25 5 27 14 13 18 5 | 19 34 27 22 48 23 36 17 18 18 20 20 | 5 20 9 7 50 5 25 11 11 26 5 | 15 26 16 16 39 16 27 15 17 21 14 21 | 8 13 5 6 45 6 13 10 9 27 4 | 19 24 19 24 25 19 21 27 16 27 19 22 | 9 21 6 7 44 5 20 13 9 14 4 | 13 33 19 16 46 18 30 21 19 21 16 23E | 7 25 8 10 40 4 21 10 6 14 4 | 21 31 19 19 42 20 28 20 20 23 19 24 | 8 9 9 7 40 4 8 9 9 20 3 | 18 22 21 23 17 19 17 21 17 22 20 25 | 8 16 7 7 40 5 11 13 11 27 4 | 19 22 23 20 23 20 21 20 21 32 18 26 | 14 16 11 11 42 4 13 14 12 37 5 | 108 109 109 111 125 111 108 114 113 113 109 27 | 10 13 8 9 26 5 9 12 10 33 4 | 15 22 18 17 43 17 21 20 16 41 16 28 | 9 18 8 9 30 6 16 12 10 10 4 | 19 28 20 18 40 20 24 23 20 19 18 29 | 11 25 9 9 28 6 28 15 10 21 5 | 18 32 19 15 34 20 33 20 21 22 17 30 | 10 17 6 7 38 7 17 15 9 20 4 | 16 28 21 17 34 18 26 23 18 26 17 31 | 12 24 12 19 37 6 26 13 10 21 6 | 15 32 32 33 43 23 31 19 26 19 22 32 | 8 18 12 6 42 5 18 11 13 17 4 | 13 22 15 14 25 14 23 15 13 16 12 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 19 8 10 39 5 18 12 11 22 |T 22 31 25 24 38 24 29 24 24 27 22 WRMS | 9 19 8 10 37 5 17 11 9 24 |NE 18 27 22 21 33 20 26 20 20 24 18 MEDI | 9 18 8 9 39 5 17 12 10 19 |MD 19 30 21 20 36 21 27 20 20 23 19 Table 3.1517.2 GPS week: 1517 Day: 2 MJD: 54865.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 11 8 9 43 8 21 10 7 34 4 | 20 27 25 27 24 23 24 23 25 30 24 3 | 9 17 8 9 17 6 13 11 8 22 4 | 42 44 46 46 36 44 42 48 51 45 45 4 | 8 11 8 6 37 5 16 10 12 25 4 | 24 31 27 30 26 27 26 28 37 30 28 5 | 8 16 8 8 23 7 15 15 11 18 4 | 20 28 24 21 28 20 27 23 22 27 20 6 | 8 16 7 8 29 6 14 9 10 19 4 | 21 34 28 28 34 26 32 24 26 37 27 7 | 9 23 7 10 27 5 21 10 7 15 4 | 23 31 26 24 38 23 30 22 27 25 23 8 | 12 14 8 3 26 6 12 11 7 25 4 | 35 39 39 39 43 36 36 38 37 45 37 9 | 5 13 9 5 42 5 14 9 13 11 3 | 19 24 25 21 35 19 22 21 20 18 20 10 | 9 16 8 6 31 5 12 13 5 21 4 | 18 28 23 23 34 21 22 22 24 22 22 11 | 7 19 7 6 56 7 20 14 8 18 4 | 37 46 36 40 44 36 39 44 39 32 38 12 | 7 30 8 9 43 8 24 12 12 14 5 | 18 34 22 19 39 21 29 24 26 20 21 13E | 16 16 8 7 52 5 16 10 6 18 4 | 59 67 67 65 97 62 63 63 62 71 62 14E | 7 22 6 6 52 5 20 8 10 16 4 | 27 39 30 31 58 31 34 31 33 30 32 15E | 10 23 10 9 31 6 20 10 11 22 5 | 23 35 26 26 44 23 32 22 27 27 26 16 | 8 25 7 8 43 7 18 15 10 15 4 | 18 29 20 22 48 18 25 21 23 23 21 17 | 9 21 8 7 37 7 26 13 14 21 5 | 21 34 25 24 40 22 29 22 27 28 23 18 | 7 22 7 6 29 7 22 7 11 17 4 | 20 36 25 20 33 23 34 20 28 22 24 19 | 8 28 8 9 28 5 28 13 9 14 5 | 21 38 26 25 48 26 37 23 29 24 25 20 | 7 23 9 9 54 6 27 11 11 27 5 | 21 31 25 23 48 20 30 21 22 25 22 21 | 7 15 7 11 89 6 14 9 10 25 4 | 24 28 24 34 51 25 26 31 30 36 28 22 | 9 21 7 7 41 6 23 8 14 12 4 | 19 36 24 23 46 22 33 20 31 23 24 23E | 9 23 9 9 46 4 25 11 4 12 4 | 15 29 24 21 42 18 26 18 22 22 20 24 | 7 10 5 6 49 5 11 11 6 17 3 | 24 29 26 33 24 27 26 29 30 32 29 25 | 7 17 9 4 31 6 12 13 6 28 4 | 20 23 25 20 25 21 21 21 25 34 21 26E | 11 17 8 10 36 5 15 13 11 44 5 | 64 64 65 70 80 65 64 69 74 54 66 27 | 10 17 8 6 30 5 9 12 6 34 4 | 24 32 27 25 38 24 28 25 28 43 27 28 | 9 20 9 6 39 6 18 12 8 11 4 | 23 35 29 27 42 26 29 27 30 26 27 29 | 9 24 8 8 26 6 25 14 8 17 5 | 22 31 20 22 33 22 32 24 25 24 22 30 | 9 20 6 7 26 5 18 14 11 16 4 | 19 29 23 21 29 22 28 22 25 25 21 31 | 9 24 8 8 45 5 23 12 10 19 4 | 23 36 34 30 44 29 35 24 34 27 29 32 | 8 18 8 6 46 6 16 11 8 17 4 | 18 25 22 20 43 19 24 20 20 22 21 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 8 8 41 6 19 11 9 21 |T 25 34 29 29 41 27 31 28 30 30 28 WRMS | 8 20 8 8 39 6 18 11 6 19 |NE 23 32 27 26 36 25 29 25 28 29 26 MEDI | 8 19 8 7 37 6 18 11 10 18 |MD 21 32 25 25 40 23 29 23 27 27 24 Table 3.1517.3 GPS week: 1517 Day: 3 MJD: 54866.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 10 11 10 15 43 6 17 10 10 40 5 | 19 28 26 33 30 24 23 23 31 28 25 3 | 10 18 7 9 27 4 14 16 10 16 4 | 43 39 37 40 49 37 39 44 41 40 38 4 | 6 11 9 7 37 6 14 9 8 27 4 | 26 33 29 31 30 29 27 29 36 28 29 5 | 8 15 8 6 18 5 15 13 10 17 4 | 23 31 26 26 27 25 27 25 30 26 24 6 | 7 20 8 6 27 4 15 14 11 18 4 | 19 34 22 17 37 20 28 18 22 32 20 7 | 9 25 9 13 26 5 25 7 9 18 5 | 21 34 25 31 40 23 31 24 30 25 24 8 | 8 13 7 6 19 5 8 11 9 24 3 | 25 30 26 27 40 29 26 28 32 31 26 9 | 6 14 10 6 43 6 13 9 12 11 3 | 25 26 25 21 28 22 25 21 26 18 22 10 | 9 15 7 10 29 4 9 13 5 23 4 | 13 23 20 24 24 18 20 20 22 23 19 11 | 7 17 7 5 59 6 21 15 9 17 4 | 34 40 35 35 38 33 38 41 38 32 34 12 | 8 22 10 8 38 5 23 12 9 16 4 | 22 36 25 22 43 24 31 24 27 26 24 13E | 7 17 7 6 42 5 18 10 9 21 4 | 51 55 52 52 78 50 59 52 51 52 51 14E | 7 25 9 6 35 7 20 8 8 14 4 | 24 37 29 29 41 25 35 27 34 32 29 15E | 9 21 10 12 32 7 19 14 11 27 5 | 40 47 42 44 56 41 47 41 40 50 41 16 | 8 25 8 8 32 5 22 15 14 19 5 | 13 26 15 13 32 15 24 19 19 21 14 17 | 8 21 8 8 42 7 25 12 9 27 5 | 16 32 20 18 33 19 28 17 25 18 17 18 | 7 22 9 6 36 4 22 10 9 19 4 | 20 35 20 22 32 22 32 19 27 21 22 19 | 7 23 7 7 27 7 29 14 10 20 5 | 21 33 24 17 41 21 37 16 26 17 20 20 | 7 21 8 8 55 6 26 11 11 27 5 | 17 29 18 18 47 17 29 18 23 27 17 21 | 5 15 7 8 105 5 11 9 10 26 4 | 26 28 25 29 68 24 22 31 31 29 27 22 | 7 21 8 5 42 5 20 8 11 14 4 | 19 35 21 21 52 20 30 20 25 23 22 23E | 9 19 9 10 39 5 21 9 10 11 4 | 25 33 26 27 42 24 32 27 30 28 26 24 | 7 12 9 7 39 4 10 9 9 20 3 | 25 32 28 33 16 27 28 31 36 30 30 25 | 7 15 7 5 37 5 11 9 10 27 3 | 22 29 20 24 32 22 26 23 31 35 23 26E | 14 19 11 11 33 5 14 13 10 46 6 | 105 103 102 105 89 104 100 107 110 108 104 27 | 10 15 7 6 28 6 9 8 8 35 4 | 18 25 18 21 27 20 20 19 22 40 18 28 | 7 15 9 6 44 6 15 15 11 12 4 | 19 26 19 19 48 19 22 23 27 20 18 29 | 9 24 8 9 33 7 23 14 15 19 5 | 21 34 21 19 45 21 31 24 28 23 21 30 | 10 18 9 5 28 6 15 13 11 18 4 | 16 27 21 16 34 19 24 19 22 21 17 31 | 8 23 11 7 38 6 23 13 8 17 4 | 26 33 31 25 39 26 30 28 29 29 26 32 | 8 20 9 5 40 6 17 9 12 19 4 | 15 26 20 16 34 16 23 17 27 23 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 9 8 41 6 18 12 10 23 |T 26 34 28 28 41 26 32 28 32 30 27 WRMS | 8 19 9 8 38 6 18 11 8 22 |NE 22 31 24 24 36 23 28 24 28 26 23 MEDI | 8 19 8 7 37 5 17 11 10 19 |MD 22 33 25 24 39 23 28 24 29 28 24 Table 3.1517.4 GPS week: 1517 Day: 4 MJD: 54867.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 9 10 9 10 52 5 16 8 12 41 5 | 12 25 23 23 28 19 20 19 23 26 19 3 | 11 14 9 9 21 10 13 12 12 33 5 | 108 112 111 113 107 111 109 118 114 116 112 4 | 8 12 7 8 49 5 11 8 12 34 4 | 17 25 20 25 21 21 23 22 25 27 21 5 | 10 12 7 6 23 4 10 10 9 19 3 | 19 30 20 22 23 23 24 26 29 25 23 6 | 8 15 12 10 29 5 12 15 10 20 4 | 17 29 24 19 33 19 30 17 21 34 19 7 | 7 24 8 9 39 3 18 10 10 20 4 | 15 30 22 17 37 17 25 21 24 16 17 8 | 10 13 8 6 16 4 9 10 6 25 3 | 17 23 19 19 25 17 20 16 20 24 17 9 | 6 13 10 7 36 4 11 6 10 16 3 | 18 25 23 19 22 19 21 19 26 16 21 10 | 8 13 5 7 38 5 9 13 7 14 3 | 9 21 15 14 31 14 17 20 15 19 13 11 | 6 17 9 5 78 9 18 14 13 17 4 | 26 34 24 30 39 26 35 36 29 29 27 12 | 7 29 9 11 30 4 20 8 6 16 4 | 14 36 19 16 32 18 26 20 22 23 18 13E | 6 18 7 9 26 5 17 9 9 26 4 | 32 35 31 30 42 33 38 33 38 29 32 14E | 8 24 9 9 48 5 18 8 12 20 4 | 16 31 18 17 48 21 27 20 28 20 20 15E | 6 21 10 13 33 7 20 6 10 23 4 | 26 29 28 24 48 25 30 26 32 33 27 16 | 6 23 10 8 21 4 22 14 12 17 5 | 12 29 20 13 29 17 27 19 20 20 16 17 | 10 19 9 9 38 6 20 9 8 18 4 | 17 29 17 16 37 15 26 18 20 14 15 18 | 8 22 11 7 33 5 26 7 13 20 5 | 16 30 17 16 34 18 30 15 25 17 18 19 | 6 27 11 9 32 6 26 15 9 16 5 | 17 36 23 18 44 20 36 18 21 18 18 20 | 6 20 12 8 61 7 20 14 9 28 5 | 14 26 19 19 48 17 26 18 13 25 13 21 | 7 13 15 8 69 6 14 10 11 29 4 | 20 24 21 23 31 18 19 26 23 27 20 22 | 8 21 11 7 43 5 22 7 12 16 4 | 13 30 14 14 42 18 28 13 23 17 16 23E | 7 23 10 10 35 7 21 10 9 16 4 | 18 28 17 19 37 20 27 20 24 17 18 24 | 7 11 12 5 42 5 10 10 9 24 3 | 24 29 34 29 20 28 26 32 34 33 29 25 | 6 18 9 4 34 4 10 7 8 32 4 | 15 23 18 13 25 18 19 17 24 27 16 26E | 15 22 14 11 34 5 19 12 15 29 6 | 69 69 64 71 58 68 69 72 68 73 67 27 | 10 14 7 5 38 4 9 10 7 34 4 | 13 22 16 16 29 16 20 14 20 37 15 28 | 8 15 6 8 36 5 16 10 8 14 3 | 17 21 15 17 29 16 21 18 21 17 15 29 | 11 22 13 7 29 6 24 11 9 18 5 | 19 35 29 22 35 22 32 25 25 26 23 30 | 10 18 6 5 30 4 14 10 10 17 4 | 12 26 14 15 32 15 22 19 22 18 15 31 | 8 21 8 7 36 5 23 15 11 17 5 | 21 33 21 20 40 23 30 21 30 20 23 32 | 9 20 10 6 35 6 17 12 9 20 4 | 14 23 15 14 26 15 23 15 17 18 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 8 40 6 17 11 10 23 |T 21 32 24 23 36 24 29 25 28 27 23 WRMS | 8 19 9 8 37 5 16 10 8 22 |NE 20 31 24 23 35 23 28 24 27 27 22 MEDI | 8 18 9 8 35 5 17 10 10 20 |MD 17 29 20 19 33 19 26 20 24 24 18 Table 3.1517.5 GPS week: 1517 Day: 5 MJD: 54868.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 11 15 8 20 84 6 14 13 14 41 6 | 15 25 26 33 45 21 22 21 21 27 20 3 | 11 16 7 10 26 7 14 20 11 20 4 | 87 90 88 94 84 88 91 86 82 87 87 4 | 10 10 9 13 89 5 8 14 13 30 4 | 18 22 22 25 50 19 19 25 22 31 19 5 | 10 14 8 8 18 4 9 12 12 21 4 | 21 30 23 27 28 22 26 28 25 32 23 6 | 6 16 8 9 37 4 13 21 12 20 4 | 18 25 20 16 33 15 29 17 21 32 17 7 | 8 24 6 10 34 4 22 16 13 15 5 | 20 31 19 24 31 18 27 26 27 21 19 8 | 8 13 6 4 20 4 8 12 11 25 3 | 17 20 17 16 29 16 18 19 21 25 14 9 | 8 11 8 6 37 5 9 9 9 14 3 | 19 24 21 20 26 18 21 19 21 22 19 10 | 10 12 7 8 31 5 9 18 15 17 4 | 9 17 14 16 27 9 19 18 19 18 11 11 | 8 21 6 6 68 6 18 17 11 20 4 | 26 37 24 31 42 26 38 35 27 31 26 12 | 8 23 9 8 27 3 19 13 10 16 4 | 18 34 23 25 38 20 27 25 22 27 21 13E | 6 20 6 7 40 3 19 11 11 18 4 | 28 36 30 30 44 28 34 25 31 26 29 14E | 8 21 8 6 33 3 17 10 10 16 4 | 17 26 22 22 41 19 26 19 26 20 21 15E | 9 27 10 13 45 4 22 13 15 23 5 | 18 32 21 20 44 18 29 17 16 25 17 16 | 7 30 8 11 20 5 24 22 10 21 6 | 11 31 14 12 32 9 25 22 12 19 10 17 | 9 20 6 8 34 5 17 14 10 20 4 | 17 29 16 18 29 13 24 14 18 13 14 18 | 7 22 5 7 25 4 23 10 8 24 4 | 15 27 15 15 28 13 27 16 22 17 15 19 | 6 26 11 9 35 5 25 15 10 18 5 | 21 35 25 20 48 20 34 17 22 16 19 20 | 7 21 8 10 52 6 21 16 10 27 5 | 15 28 17 19 42 14 28 19 17 27 14 21 | 6 16 4 9 55 5 15 10 12 31 4 | 21 23 23 24 23 20 20 25 28 26 21 22 | 10 20 6 7 43 3 19 8 11 14 4 | 14 27 17 13 42 13 26 13 22 18 15 23E | 9 27 9 11 45 5 20 11 10 12 5 | 18 33 24 24 36 18 29 21 24 21 20 24 | 7 11 8 9 33 4 10 13 11 25 4 | 21 24 26 28 25 22 23 28 29 26 22 25 | 8 13 6 7 39 3 11 13 10 31 4 | 19 22 19 19 25 16 22 19 25 34 17 26E | 15 21 11 12 38 6 18 20 20 36 6 | 92 84 86 91 81 88 85 95 99 79 88 27 | 10 13 7 6 31 3 9 11 10 35 4 | 16 21 16 16 27 15 20 15 16 38 14 28 | 9 19 7 8 34 5 14 17 12 13 4 | 16 23 14 14 32 13 18 14 18 16 11 29 | 11 22 10 10 22 5 23 13 9 18 5 | 21 31 22 24 36 20 28 24 24 25 21 30 | 9 18 6 8 18 3 12 14 8 20 4 | 15 28 19 18 27 17 22 20 16 25 16 31 | 9 20 6 8 43 4 21 20 10 14 4 | 21 29 21 16 39 16 29 25 18 20 17 32 | 8 20 9 7 39 3 17 14 10 19 4 | 14 22 14 15 25 10 23 15 16 22 12 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 8 9 42 5 17 15 11 23 |T 22 31 24 25 37 21 29 25 26 27 22 WRMS | 9 19 8 9 39 4 16 13 9 21 |NE 20 29 22 23 35 20 27 23 24 27 20 MEDI | 8 20 8 8 35 4 17 13 11 20 |MD 18 28 21 20 33 18 26 20 22 25 19 Table 3.1517.6 GPS week: 1517 Day: 6 MJD: 54869.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 10 13 9 12 59 3 17 11 14 40 5 | 17 25 25 29 36 23 25 26 25 33 21 3 | 8 18 7 7 19 5 14 24 8 17 4 | 83 80 81 79 84 80 84 85 83 86 81 4 | 9 15 6 7 55 5 12 12 12 21 4 | 24 29 27 33 29 26 22 30 31 29 26 5 | 9 15 10 7 18 4 11 13 10 25 4 | 22 31 23 26 33 22 27 28 24 25 21 6 | 8 17 12 8 28 4 15 26 9 21 5 | 19 31 22 23 33 20 31 24 21 34 21 7 | 11 24 8 8 41 6 20 16 14 19 5 | 25 32 26 31 36 25 30 31 29 24 25 8 | 10 17 8 6 19 6 12 11 9 28 4 | 26 30 27 30 34 28 29 26 29 31 26 9 | 7 15 6 8 42 2 10 11 9 16 3 | 23 25 21 23 29 22 26 21 21 19 20 10 | 10 16 9 7 24 4 9 13 6 16 3 | 15 25 21 22 26 18 24 22 17 23 18 11 | 7 22 8 3 55 5 17 17 12 24 4 | 37 45 40 41 48 37 43 47 39 37 39 12 | 6 25 11 11 26 4 17 14 9 18 4 | 17 35 18 20 40 18 28 25 19 25 18 13E | 7 24 8 5 26 5 19 14 8 20 4 | 34 41 34 35 37 31 39 34 35 34 32 14E | 9 25 10 6 36 5 19 11 11 18 4 | 24 36 27 30 42 27 33 29 33 29 29 15E | 8 22 15 9 28 4 19 18 10 29 5 | 19 31 27 20 34 21 28 18 19 27 19 16 | 9 31 9 8 30 5 26 23 10 22 6 | 17 40 18 19 29 19 33 26 20 26 20 17 | 13 24 8 7 35 4 19 14 13 20 5 | 25 34 24 23 36 22 33 21 23 20 22 18 | 9 25 8 8 28 5 26 13 9 25 5 | 21 35 18 24 35 21 35 22 25 25 22 19 | 7 27 9 9 32 8 25 15 13 21 5 | 23 39 25 24 46 23 38 19 25 19 22 20 | 6 27 9 8 46 5 22 17 11 28 5 | 21 36 24 23 49 19 31 22 21 31 21 21 | 8 17 7 11 68 7 19 12 13 35 5 | 28 29 30 36 35 27 23 37 31 38 30 22 | 11 22 7 7 38 3 23 12 10 18 4 | 19 28 23 23 44 19 33 23 23 26 21 23E | 8 34 8 9 51 5 22 13 9 13 5 | 22 37 25 25 41 21 32 23 26 27 23 24 | 7 13 6 9 34 4 9 14 10 24 4 | 30 34 35 40 33 34 34 38 39 32 36 25 | 9 19 7 5 44 6 13 13 11 37 4 | 25 24 23 23 30 21 25 22 23 42 21 26E | 17 26 16 12 47 5 21 23 18 51 7 | 103 99 101 106 110 102 100 107 108 112 102 27 | 11 17 5 6 19 4 11 13 7 36 4 | 21 28 21 24 31 21 25 18 22 39 21 28 | 10 19 8 7 39 5 12 16 9 16 4 | 20 25 16 18 37 16 21 20 23 21 17 29 | 11 28 9 9 26 5 24 15 14 21 5 | 25 35 20 24 35 23 34 25 31 25 23 30 | 9 18 9 5 23 4 14 14 11 21 4 | 16 29 18 19 33 16 24 24 18 21 16 31 | 7 22 8 7 49 8 24 19 13 17 5 | 22 31 25 25 42 20 31 26 27 22 23 32 | 7 21 10 4 38 4 19 13 11 19 4 | 17 26 23 18 30 16 24 17 24 24 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 22 9 8 38 5 18 16 11 25 |T 27 35 28 30 39 27 33 30 30 32 27 WRMS | 9 22 9 8 37 5 16 15 8 21 |NE 25 33 27 28 37 25 31 28 28 30 25 MEDI | 9 22 8 7 35 5 19 14 10 21 |MD 22 31 24 24 35 22 31 25 25 27 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 4.1517 GPS week: 1517 MJD: 54863.0-54869.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 |U 6 7 18 |U 18 28 64 |U 7 6 16 | emr | emr 2974 | 8 9 23 | 19 30 66 | 9 7 18 | esa | esa 2976 | 7 8 20 |U 18 29 65 | 7 6 17 | gfz | gfz 2957 |U 8 12 25 |U 18 25 63 | 9 8 22 | grg | grg 2976 | 21 22 54 |U 36 43 165 | 19 18 40 | igr | igr 2976 | 7 8 19 | 18 28 63 | 7 6 16 | igs | igs 2965 | 7 8 20 | 18 29 63 | 7 6 17 | jpl | jpl 2973 |U 7 9 22 |U 17 30 63 |U 8 6 16 | mit | mit 2976 |U 8 8 18 |U 19 30 68 |U 8 7 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 5.1517.0 GPS week: 1517 Day: 0 MJD: 54863.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 7 14 | 23 16 60 | 7 9 18 | emr | emr 2976 | 7 10 21 | 23 17 63 | 12 11 22 | esa | esa 2976 | 8 9 15 | 21 17 60 | 7 9 17 | gfz | gfz 2957 | 7 9 20 | 25 20 65 | 11 10 26 | grg | grg 2976 | 10 12 30 | 23 18 66 | 15 15 19 | igr | igr 2976 | 8 8 14 | 21 16 60 | 6 7 17 | igs | igs 2976 | 7 8 14 | 22 17 60 | 8 8 17 | jpl | jpl 2976 | 7 10 20 | 22 17 63 | 10 9 19 | mit | mit 2976 | 6 9 12 | 22 18 58 | 8 7 16 | Table 5.1517.1 GPS week: 1517 Day: 1 MJD: 54864.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 8 18 | 22 19 66 | 6 5 16 | emr | emr 2976 | 7 9 21 | 23 25 69 | 8 7 18 | esa | esa 2976 | 6 6 18 | 21 20 63 | 6 5 16 | gfz | gfz 2952 | 10 12 28 | 22 21 73 | 10 7 24 | grg | grg 2976 | 26 19 80 | 36 49 149 | 23 19 41 | igr | igr 2976 | 6 6 19 | 22 21 64 | 6 5 15 | igs | igs 2976 | 7 6 18 | 22 21 63 | 6 5 14 | jpl | jpl 2975 | 6 7 21 | 22 20 66 | 7 6 14 | mit | mit 2976 | 6 5 16 | 21 23 65 | 7 5 17 | Table 5.1517.2 GPS week: 1517 Day: 2 MJD: 54865.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 12 25 | 40 119 193 | 6 7 16 | emr | emr 2976 | 9 11 27 | 40 116 184 | 9 8 18 | esa | esa 2976 | 8 13 28 | 40 120 202 | 7 7 18 | gfz | gfz 2963 | 9 16 28 | 34 87 139 | 10 8 20 | grg | grg 2976 | 21 22 44 | 45 56 370 | 16 12 37 | igr | igr 2976 | 7 13 28 | 38 116 187 | 7 5 16 | igs | igs 2976 | 7 12 26 | 38 117 188 | 6 5 15 | jpl | jpl 2975 | 8 11 26 | 32 118 179 | 6 5 15 | mit | mit 2976 | 7 12 22 | 40 114 195 | 6 7 16 | Table 5.1517.3 GPS week: 1517 Day: 3 MJD: 54866.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 6 6 18 | 7 9 24 | 7 5 15 | emr | emr 2976 | 8 8 23 | 10 9 25 | 8 6 16 | esa | esa 2976 | 7 7 21 | 7 8 23 | 7 4 14 | gfz | gfz 2958 | 8 10 26 | 11 12 28 | 8 8 23 | grg | grg 2976 | 21 29 67 | 27 53 152 | 21 28 55 | igr | igr 2976 | 7 7 18 | 7 8 23 | 6 5 15 | igs | igs 2976 | 7 6 21 | 7 8 23 | 7 5 14 | jpl | jpl 2976 | 7 7 20 | 8 7 23 | 7 6 15 | mit | mit 2976 | 9 7 24 | 9 8 26 | 7 6 16 | Table 5.1517.4 GPS week: 1517 Day: 4 MJD: 54867.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 6 7 20 | 11 9 34 | 7 5 14 | emr | emr 2973 | 8 9 24 | 11 9 41 | 10 7 17 | esa | esa 2976 | 8 9 25 | 10 10 35 | 7 6 16 | gfz | gfz 2957 | 8 15 30 | 11 10 40 | 11 8 18 | grg | grg 2976 | 18 22 40 | 32 39 132 | 20 20 45 | igr | igr 2976 | 6 8 23 | 10 10 35 | 7 5 14 | igs | igs 2976 | 6 8 24 | 10 9 36 | 7 5 15 | jpl | jpl 2971 | 7 12 26 | 9 12 37 | 9 6 14 | mit | mit 2976 | 8 8 26 | 10 10 40 | 8 7 17 | Table 5.1517.5 GPS week: 1517 Day: 5 MJD: 54868.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 6 5 17 | 11 11 41 | 6 5 21 | emr | emr 2972 | 10 6 22 | 13 15 42 | 8 5 22 | esa | esa 2976 | 7 6 17 | 12 14 41 | 7 7 24 | gfz | gfz 2957 | 8 11 21 | 14 13 49 | 9 6 24 | grg | grg 2976 | 25 21 39 | 48 44 141 | 18 15 33 | igr | igr 2976 | 7 5 17 | 13 13 42 | 6 4 22 | igs | igs 2914 | 8 7 20 | 13 16 39 | 7 5 23 | jpl | jpl 2972 | 7 7 19 | 13 16 40 | 8 4 20 | mit | mit 2976 | 9 6 16 | 17 20 59 | 8 8 25 | Table 5.1517.6 GPS week: 1517 Day: 6 MJD: 54869.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 6 9 18 | 14 16 31 | 6 6 14 | emr | emr 2972 | 7 12 24 | 14 19 38 | 9 6 15 | esa | esa 2976 | 7 9 16 | 13 18 31 | 7 8 15 | gfz | gfz 2958 | 8 15 19 | 13 15 45 | 9 8 18 | grg | grg 2976 | 28 29 78 | 38 44 144 | 18 15 46 | igr | igr 2976 | 6 7 14 | 14 16 34 | 7 7 16 | igs | igs 2965 | 7 12 19 | 13 16 30 | 6 7 20 | jpl | jpl 2972 | 6 11 20 | 13 20 34 | 7 5 15 | mit | mit 2976 | 7 8 13 | 14 15 34 | 10 10 31 | 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 6.1517 GPS week: 1517 MJD: 54863.500-54869.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 25 -31 38 131 -4 | -2 24 | 27 11 125 69 6 | 4 emr uuuuu | -20 -60 -1 289 -6 | 39 45 | 19 60 187 91 10 | 8 esa uuuuu | -7 -11 38 -26 6 | 0 24 | 49 44 174 135 6 | 8 gfz uuuuu | 35 -16 10 69 -3 | -7 24 | 26 10 120 41 5 | 5 grg xxxxx | -8 -42 40 137 1 | -3 31 | 41 17 102 101 45 | 4 igr xxxxx | 1 3 20 81 3 | 7 23 | 48 12 103 95 6 | 7 irf xxxxx | -7 17 -71 -15 1 | 1 23 | 7 9 54 40 6 | 7 jpl uuuuu | 33 -29 83 239 -4 | -16 32 | 37 17 182 83 11 | 4 mit uuuuu | -23 41 -224 -208 5 | 0 25 | 15 12 107 73 6 | 8 ngs uuuuu | -43 16 74 -155 -11 | -3 22 | 51 41 72 80 17 | 2 sio uuxxu | 54 83 112 2 7 | 6 27 | 20 27 86 59 10 | 10 Table 7.1517.0 GPS week: 1517 Day: 0 MJD: 54863.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 10 -50 8 110 -14 | -7 22 emr uuuuu | -43 -124 149 227 0 | 25 33 esa uuuuu | 79 21 346 57 12 | -13 20 gfz uuuuu | 20 -10 -115 70 -8 | -15 24 grg xxxxx | -58 -44 -161 91 1 | -7 34 igr xxxxx | 7 -1 107 22 -8 | -4 18 irf xxxxx | 0 24 -119 -81 7 | -11 20 jpl uuuuu | 26 -34 -201 150 -16 | -19 33 mit uuuuu | -13 33 -286 -285 8 | -13 22 ngs uuuuu | -111 2 26 -114 -27 | -6 22 sio uuxxu | 72 125 100 -61 14 | -9 19 Table 7.1517.1 GPS week: 1517 Day: 1 MJD: 54864.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -9 -16 -129 157 -4 | -4 23 emr uuuuu | -29 -119 124 241 12 | 32 40 esa uuuuu | 47 50 110 143 6 | -6 23 gfz uuuuu | 3 -15 -168 26 2 | -12 25 grg xxxxx | -47 -56 40 -23 -39 | -4 36 igr xxxxx | 66 12 138 -12 4 | 1 20 irf xxxxx | 1 26 -125 4 7 | -5 24 jpl uuuuu | 56 -30 135 215 0 | -16 32 mit uuuuu | 0 46 -325 -152 13 | -7 25 ngs uuuuu | -109 -50 181 -328 -32 | -2 21 sio uuxxu | 80 106 37 48 17 | -3 25 Table 7.1517.2 GPS week: 1517 Day: 2 MJD: 54865.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 66 -31 -116 40 -1 | -2 23 emr uuuuu | -14 -115 185 276 -3 | 38 44 esa uuuuu | -23 25 -20 -31 10 | -2 22 gfz uuuuu | 53 -27 -14 52 -1 | -9 23 grg xxxxx | 49 -67 -7 190 -26 | -6 37 igr xxxxx | 49 22 66 234 5 | 5 20 irf xxxxx | -17 20 -117 -32 2 | -1 22 jpl uuuuu | 0 -47 312 264 -8 | -14 32 mit uuuuu | -44 47 -317 -212 7 | -3 24 ngs uuuuu | -8 11 84 -84 -19 | -3 22 sio uuxxu | 36 69 -11 -72 12 | 3 25 Table 7.1517.3 GPS week: 1517 Day: 3 MJD: 54866.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 21 -20 75 155 -10 | 3 25 emr uuuuu | -9 -60 117 283 -12 | 45 50 esa uuuuu | -32 -24 -105 -92 13 | 4 26 gfz uuuuu | 75 -10 67 58 -6 | -3 23 grg xxxxx | 16 -48 93 68 8 | -7 37 igr xxxxx | 17 -10 -34 166 6 | 11 24 irf xxxxx | -1 20 -53 35 -1 | 6 24 jpl uuuuu | -14 -52 295 248 -7 | -10 31 mit uuuuu | -16 48 -189 -121 1 | 4 26 ngs uuuuu | -51 39 -7 -131 -3 | 0 22 sio uuxxu | 37 61 152 69 7 | 11 28 Table 7.1517.4 GPS week: 1517 Day: 4 MJD: 54867.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 57 -35 136 49 1 | 1 25 emr uuuuu | -41 -16 -104 205 -9 | 44 49 esa uuuuu | -37 -71 -187 29 0 | 5 26 gfz uuuuu | 47 -31 53 61 5 | -5 24 grg xxxxx | 26 -30 52 245 -20 | 1 24 igr xxxxx | -68 4 -169 103 11 | 11 25 irf xxxxx | -8 3 16 21 3 | 6 24 jpl uuuuu | 21 -6 57 168 -11 | -13 32 mit uuuuu | -29 27 -21 -138 10 | 5 25 ngs uuuuu | 3 83 162 -157 -11 | -1 22 sio uuxxu | 35 53 257 64 10 | 12 29 Table 7.1517.5 GPS week: 1517 Day: 5 MJD: 54868.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 12 -33 207 230 -3 | 2 25 emr uuuuu | -11 17 -212 313 -18 | 46 50 esa uuuuu | -44 -37 3 -3 5 | 8 27 gfz uuuuu | 36 -15 184 64 -8 | -2 24 grg xxxxx | -38 -15 142 134 -13 | 3 22 igr xxxxx | -47 -11 36 -21 6 | 15 27 irf xxxxx | -14 22 -25 -43 -5 | 9 24 jpl uuuuu | 41 -21 -18 227 -1 | -15 32 mit uuuuu | -37 59 -176 -306 0 | 9 27 ngs uuuuu | 13 0 25 -146 7 | -1 22 sio uuxxu | 48 97 112 -31 0 | 16 30 Table 7.1517.6 GPS week: 1517 Day: 6 MJD: 54869.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 22 -30 88 178 1 | -3 24 emr uuuuu | 9 -4 -263 478 -13 | 41 47 esa uuuuu | -38 -43 119 -282 -5 | 6 26 gfz uuuuu | 11 -3 62 156 -6 | -7 24 grg xxxxx | -2 -35 118 254 97 | 1 24 igr xxxxx | -14 5 -7 77 -4 | 13 25 irf xxxxx | -9 6 -71 -7 -8 | 6 24 jpl uuuuu | 99 -12 0 403 17 | -21 32 mit uuuuu | -19 26 -254 -242 -5 | 7 26 ngs uuuuu | -37 27 46 -124 11 | -5 20 sio uuxxu | 74 70 137 -1 -11 | 14 30