Date: Thu, 23 Jul 2009 12:40:23 +0000 From: Jim Ray Subject: [IGSREPORT-17617] Wk 1539 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4a685a37.3uHIgfWY8Tb2mUbm%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 23 Jul 05:40:48 PDT 2009 Message Number 17617 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1539 (Jul 05, 2009 - Jul 11, 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: igs1539[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1539[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1539[0-6].cls IGS GPS clock combination summary report. igs15397.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15397.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. Duplicate entries can arise due to separate combination runs for the 30-s clocks ACs (listed first) and the 5-min clock ACs (listed second). Day | Centre | PRN/STA list ----+--------+--------------- 0 | COD | 30 30 HRAO MATE 0 | EMR | WTZR MIZU WTZR 0 | ESA | 1 30 UNSA 0 | GFZ | 30 CHUR 0 | GRG | ONSA 0 | JPL | 32 0 | MIT | 1 1 1 | COD | 30 30 1 | EMR | WTZR 1 | ESA | 1 21 BARH UNSA 1 | GFZ | 21 FAA1 1 | GRG | IRKJ ONSA 1 | JPL | 30 1 | MIT | 1 15 1 15 2 | COD | STR2 2 | EMR | MIZU TWTF WTZR 2 | ESA | KHAJ UNSA 2 | GFZ | 28 CAS1 CHUR FAA1 2 | GRG | IRKJ MANA TWTF USNO 2 | JPL | 32 2 | MIT | 1 1 HRAO SYDN 3 | COD | 30 30 RCMN YELL 3 | EMR | WTZR WTZR 3 | GFZ | ALIC ANKR CHUR KERG TOW2 3 | GRG | IRKJ KHAJ ONSA 3 | JPL | 32 NLIB 3 | MIT | 1 1 YELL 3 | NGS | 1 4 | COD | 30 30 STR2 4 | EMR | WTZR MIZU SCH2 WTZR 4 | ESA | 21 TWTF UNSA 4 | GFZ | CAS1 FLIN MAS1 4 | GRG | KHAJ ONSA 4 | JPL | 32 4 | MIT | 1 19 1 19 NISU TWTF 4 | NGS | 1 5 | COD | ANKR NYA1 YELL 5 | EMR | WTZR MIZU WTZR 5 | GFZ | 12 ALIC CAS1 GODE UNSA YELL 5 | GRG | ONSA 5 | JPL | 32 5 | MIT | 1 30 1 30 TWTF TWTF 5 | NGS | 1 6 | EMR | MIZU WTZR 6 | ESA | IRKJ KERG 6 | GFZ | 12 16 FAA1 NYA1 UNSA 6 | GRG | IRKJ ONSA POTS 6 | JPL | 30 32 6 | MIT | 15 29 30 15 19 29 30 HARB KHAJ 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 | .5 .3 .7 -17 -19 -6 -.23 EMR | 4.0 -8.9 -6.2 65 21 45 -.22 ESA | 7.9 -5.7 3.5 -33 -83 22 -.01 GFZ | .0 .8 1.2 20 -4 9 -.09 GRG | 5.4 -.6 2.0 -22 -2 11 .15 JPL | 2.9 -5.0 -5.5 -10 -12 -2 .02 MIT | 5.5 -6.3 10.3 -3 25 3 -.37 NGS | 9.1 -9.3 7.8 -118 -91 4 -.28 SIO | 1.8 -5.6 -20.6 -100 -98 -16 .05 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 1.1539.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1539.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 2.1539.[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 3.1539.[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 5.1539.0-6). 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 1539 summary. (Jul 05, 2009 - Jul 11, 2009) Table 1.1539.a GPS week: 1539 MJD: 55017.000-55023.000 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 0 -15 -3 -5 -.16 7 7 | -244 -560 15 72 | 0 0 1 13 23 9 .03 | 318 605 emr 78| 0 -1 -2 -166 -71 -4 .44 16 16 | 2524 -4 20 108 | 2 1 1 21 27 17 .03 | 1546 1634 esa 129| 0 0 1 -8 58 27 .34 9 8 | -1304 799 18 102 | 0 0 1 7 19 16 .03 | 1077 1660 gfz 188| 0 0 1 -84 -40 -39 -.10 9 9 | 56 -153 23 100 | 0 0 1 22 47 6 .02 | 216 492 grg 106| 1 0 -3 -10 5 0 1.08 32 29 | 1428671 -20 74 214 | 1 1 1 10 26 62 .04 | 3779600 782 igr n/a| 0 1 -1 -24 -21 -36 .05 5 5 | 26905 574 17 59 | 0 0 0 12 39 21 .02 | 2745 1600 jpl 129| 0 0 -8 -32 -21 30 .59 17 16 | 1943 -17 16 95 | 1 0 0 17 18 18 .04 | 1401 1546 mit 261| 0 0 2 -36 -125 13 -.25 9 8 | -5936 -3407 19 134 | 0 0 1 20 21 10 .01 | 9036 8358 ngs 218| 0 0 0 223 138 -10 -.27 12 8 | 4521 4666 2059 3709 | 0 0 1 17 41 18 .02 | 7783 8607 sio 258| -1 2 -2 165 134 -8 -.04 17 17 | --- --- --- --- | 1 0 1 17 27 9 .04 | --- --- Table 1.1539.b GPS week : 1539 MJD: 55017.000-55023.000 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 | 8 13 7 10 12 8 0 | 2 | 5 5 5 5 5 5 5 | 3 | 4 3 3 3 4 3 4 | 4 | 5 4 4 4 4 4 5 | 6 | 3 3 3 3 3 3 4 | 7 | 4 4 4 5 5 4 4 | 8 | 4 4 4 3 4 4 3 | 9 | 4 4 3 4 4 4 4 | 10 | 5 4 5 4 4 4 4 | 11 | 5 4 4 4 4 4 4 | 12 | 5 5 5 5 5 5 4 | 13 | 4 4 4 4 4 4 4 | 14 | 4 5 4 4 3 4 4 | 15 | 5 5 5 5 5 5 5 | 16 | 4 4 4 5 5 4 4 | 17 | 6 5 5 5 5 5 5 | 18 | 4 4 4 4 5 4 5 | 19 | 5 4 4 5 5 5 5 | 20 | 5 4 4 4 4 4 4 | 21 | 4 4 4 4 4 4 4 | 22 | 4 3 3 3 4 4 4 | 23 | 5 4 4 4 5 5 5 | 24 | 4 4 3 3 3 3 3 | 25 | 4 4 4 4 4 4 4 | 26 | 4 3 3 3 3 4 3 | 27 | 4 3 3 3 4 4 4 | 28 | 5 4 4 4 4 4 5 | 29 | 5 5 5 5 5 5 5 | 30 | 7 7 7 7 7 7 7 | 31 | 4 4 4 4 4 4 4 | 32 | 5 5 5 5 4 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 2.1539.0 GPS week: 1539 Day: 0 MJD: 55017.000 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 0 -17 1 3 -.11 7 7 | 145 -1281 16 69 | 30 -6 | emr 78| 1 -2 -1 -148 -35 -4 .49 16 16 | 2611 -2185 21 121 | 5 -44 | esa 129| 0 0 1 2 45 58 .39 11 11 | 415 -1900 21 105 | 14 47 | gfz 188| 2 0 0 -103 -88 -32 -.14 9 9 | 377 -736 24 110 | -18 -61 | grg 106| 1 2 -3 -21 15 17 1.09 33 30 | 764 -1366 73 198 | 36 -4 | igr n/a| 0 0 -1 -44 -34 -5 .07 5 5 | 25051 -1815 20 59 | -16 -27 | jpl 129| 0 0 -9 -54 -23 11 .62 17 16 | 2077 -2301 18 92 | -7 7 | mit 261| 0 0 1 -17 -95 -3 -.25 10 9 | 467 -970 20 141 | 8 46 | ngs 218| 0 0 1 205 162 -22 -.26 11 8 | 125 -1240 1957 3934 | -50 -41 | sio 258| -2 2 -2 176 170 -18 .02 18 16 | --- --- --- --- | -116 -82 | Table 2.1539.1 GPS week: 1539 Day: 1 MJD: 55018.000 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 0 -2 10 -21 -.14 7 7 | -489 -133 20 82 | 24 -43 | emr 78| 3 -1 -2 -151 -43 18 .43 16 16 | 1362 -651 25 117 | 22 -59 | esa 129| 0 0 2 0 81 32 .33 10 10 | -1679 2058 19 103 | 35 34 | gfz 188| 1 0 0 -111 -72 -32 -.07 8 8 | -165 126 24 87 | -7 -75 | grg 106| -1 1 -3 -12 27 -40 1.14 30 28 | -166 260 74 204 | -33 -47 | igr n/a| 0 0 -1 0 -30 -58 .05 5 4 | 24198 -75 18 53 | -44 -34 | jpl 129| 0 0 -9 -27 -20 32 .61 16 15 | 786 -554 17 106 | 0 -41 | mit 261| 0 0 1 -27 -119 13 -.24 8 7 | -285 269 26 126 | 14 41 | ngs 218| 0 0 1 236 170 7 -.28 13 9 | -476 -170 1864 3567 | -95 -35 | sio 258| -2 2 -1 179 134 1 .01 16 16 | --- --- --- --- | -123 -73 | Table 2.1539.2 GPS week: 1539 Day: 2 MJD: 55019.000 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 0 -16 31 7 -.16 7 7 | -651 -78 17 80 | 16 -47 | emr 78| 3 0 -2 -139 -64 -35 .42 16 16 | 905 489 22 111 | -2 -27 | esa 129| 0 0 0 -7 30 20 .32 7 7 | -1527 1821 16 93 | 3 31 | gfz 188| 1 0 2 -103 -71 -40 -.10 10 10 | 127 -580 21 101 | 9 -79 | grg 106| 1 0 -2 -10 32 -62 1.10 32 28 | -173 901 80 211 | -17 -68 | igr n/a| 0 2 0 -29 59 -55 .04 5 4 | 24589 1133 16 54 | -35 -79 | jpl 129| 0 0 -8 -31 7 36 .62 16 15 | 427 488 15 96 | -7 2 | mit 261| -1 0 2 -53 -145 6 -.26 8 7 | 4743 -22308 18 124 | 15 49 | ngs 218| 0 0 0 240 181 6 -.28 11 8 | -5485 23279 2025 3908 | -23 -88 | sio 258| -2 2 -3 160 108 -21 -.03 16 17 | --- --- --- --- | -116 -62 | Table 2.1539.3 GPS week: 1539 Day: 3 MJD: 55020.000 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 0 -34 2 -6 -.21 8 8 | 78 -530 18 76 | 43 -23 | emr 78| 1 -1 -1 -175 -73 5 .42 16 16 | 1360 1112 23 130 | 41 -25 | esa 129| 0 0 0 -17 62 6 .30 8 8 | -2094 2085 19 109 | 25 34 | gfz 188| 0 0 0 -72 -70 -49 -.09 9 9 | -119 281 25 110 | 3 -46 | grg 106| 2 1 -5 -20 19 107 1.03 33 30 | 9999999 -21 76 221 | 19 -47 | igr n/a| 0 1 -1 -24 -15 -37 .05 5 5 | 25827 1645 17 62 | -27 -41 | jpl 129| 1 0 -7 -32 -12 65 .62 16 15 | 1112 866 15 93 | 25 -6 | mit 261| 0 0 4 -6 -124 28 -.27 9 8 | -15375 -466 19 120 | -1 25 | ngs 218| 0 0 -1 242 167 -15 -.26 14 11 | 12886 2957 2091 3569 | -69 14 | sio 258| -2 2 0 194 131 0 -.08 15 16 | --- --- --- --- | -119 -85 | Table 2.1539.4 GPS week: 1539 Day: 4 MJD: 55021.000 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 0 -9 -24 -8 -.16 7 7 | -514 276 16 76 | 26 16 | emr 78| 0 -4 -5 -168 -92 6 .46 17 17 | 2350 2317 20 89 | 0 -42 | esa 129| 0 0 1 -16 52 27 .34 8 8 | -427 -277 18 107 | 35 6 | gfz 188| 0 1 2 -88 15 -44 -.12 9 9 | -19 32 22 104 | 14 -43 | grg 106| 1 0 -4 6 -28 47 1.07 30 29 | -152 330 74 243 | 0 45 | igr n/a| 0 1 0 -24 -52 -8 .03 4 4 | 27438 2712 19 57 | -29 -33 | jpl 129| 0 0 -7 -17 -34 22 .61 16 15 | 1651 2059 15 91 | -29 -38 | mit 261| 0 0 4 -43 -116 18 -.25 8 8 | -15798 281 17 121 | -1 30 | ngs 218| 0 0 0 227 93 -30 -.27 12 8 | 11914 5910 1852 3421 | -48 2 | sio 258| -2 2 -1 151 143 1 -.04 16 19 | --- --- --- --- | -111 -81 | Table 2.1539.5 GPS week: 1539 Day: 5 MJD: 55022.000 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 -2 -28 -12 -5 -.16 7 6 | -9 -1153 12 64 | 63 -14 | emr 78| -1 -1 -2 -201 -77 -5 .45 18 18 | 5191 -1853 19 90 | 26 -22 | esa 129| 1 0 4 -8 85 26 .36 8 7 | -986 -471 18 96 | -4 -13 | gfz 188| 0 0 3 -54 -19 -35 -.07 9 9 | 304 -659 21 91 | -15 -61 | grg 106| 2 -2 -3 -16 7 -15 1.08 33 30 | 445 -752 72 200 | 36 -16 | igr n/a| 0 2 -1 -24 -18 -51 .05 5 5 | 30850 -1005 16 62 | -15 -48 | jpl 129| 1 0 -9 -56 -16 36 .55 18 17 | 4345 -1623 18 90 | 19 4 | mit 261| 0 0 1 -40 -161 24 -.25 9 8 | -15092 -1144 19 139 | 5 38 | ngs 218| -1 0 0 205 118 -31 -.25 11 7 | 12969 2964 2289 3548 | -6 14 | sio 258| 0 3 -4 151 91 -11 -.08 18 16 | --- --- --- --- | -109 -76 | Table 2.1539.6 GPS week: 1539 Day: 6 MJD: 55023.000 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 2 -38 -6 -.17 7 7 | -274 -1023 11 60 | 26 28 | emr 78| -1 0 -4 -181 -115 -13 .42 16 16 | 3895 741 16 98 | 35 -1 | esa 129| 1 1 3 -9 52 17 .35 8 7 | -2830 2281 19 104 | 13 34 | gfz 188| 0 0 2 -60 26 -40 -.10 9 9 | -110 459 24 100 | -58 -63 | grg 106| 3 0 -2 -1 -32 -58 1.06 31 30 | -20 503 75 225 | 1 15 | igr n/a| 0 0 0 -20 -56 -35 .01 5 5 | 30384 1424 17 67 | -30 -13 | jpl 129| 0 1 -9 -10 -51 11 .51 18 17 | 3204 941 20 103 | 53 73 | mit 261| 0 0 3 -63 -114 8 -.24 10 9 | -212 485 19 169 | 14 9 | ngs 218| -1 0 0 206 77 11 -.31 12 7 | -282 -1034 2337 4022 | -124 46 | sio 258| 0 1 -3 145 162 -7 -.07 20 17 | --- --- --- --- | -100 -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 3.1539.0 GPS week: 1539 Day: 0 MJD: 55017.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 10 26 19 --- --- 15 --- 11 13 --- 7 | 28 26 16 --- --- 27 --- 21 22 --- 25 2 | 7 13 10 7 26 5 17 7 13 33 4 | 26 27 23 27 33 23 27 24 24 29 23 3 | 5 13 9 8 32 5 11 11 6 15 3 | 22 25 27 24 32 22 23 23 30 30 24 4 | 8 10 7 10 30 5 11 13 14 21 4 | 32 31 27 35 18 27 23 31 31 34 29 6 | 4 12 10 7 29 3 11 8 7 12 3 | 22 23 27 24 28 22 22 26 26 27 23 7 | 5 16 9 11 38 5 17 8 6 17 4 | 16 28 18 26 36 17 25 17 19 16 17 8 | 5 13 11 9 23 5 14 9 9 15 3 | 14 19 18 22 19 14 18 13 19 16 15 9 | 6 17 10 6 28 7 14 9 9 17 4 | 11 20 15 16 26 10 20 13 14 19 11 10 | 10 17 13 11 18 6 15 11 11 19 4 | 15 25 20 20 26 14 24 15 15 25 14 11 | 6 12 13 10 53 5 15 6 11 29 4 | 39 49 49 46 38 42 47 41 38 32 41 12E | 10 22 13 9 25 8 25 9 7 13 5 | 12 23 19 17 32 15 23 16 15 13 14 13 | 5 13 10 7 30 2 18 9 8 13 3 | 21 31 24 25 38 22 28 22 22 18 21 14 | 7 19 12 7 26 4 17 7 13 13 4 | 14 28 20 17 38 15 23 17 18 20 16 15 | 8 17 11 9 32 5 20 15 10 18 4 | 18 25 16 19 37 16 24 19 19 20 15 16E | 5 17 12 9 31 4 22 7 8 12 4 | 16 27 23 18 32 17 27 17 16 20 16 17 | 11 15 12 17 31 4 20 20 13 19 6 | 19 27 22 26 37 18 28 19 24 18 18 18 | 5 17 7 8 26 4 15 5 9 14 3 | 16 25 18 17 31 15 24 18 21 17 17 19 | 7 14 13 7 32 4 22 9 8 32 5 | 20 33 28 24 39 24 38 21 22 29 22 20 | 5 16 17 10 22 4 18 7 11 12 4 | 17 25 20 24 35 18 27 16 21 16 16 21 | 5 11 10 8 27 5 17 7 9 23 4 | 27 26 27 27 34 23 28 25 24 27 24 22 | 6 14 10 8 26 5 10 9 9 10 3 | 11 17 17 14 29 11 19 16 19 14 13 23 | 7 22 14 8 30 3 17 8 8 15 4 | 19 36 26 25 34 21 27 21 22 17 20 24 | 5 11 9 8 28 4 11 7 6 19 3 | 24 26 28 26 24 23 23 27 24 25 24 25 | 6 11 11 6 --- 3 12 8 9 21 3 | 14 24 18 23 --- 16 22 17 22 25 16 26 | 7 12 11 8 18 3 14 7 10 12 3 | 10 16 16 17 27 13 18 17 13 18 12 27 | 4 14 10 5 37 4 13 7 10 14 3 | 9 16 12 11 29 8 18 9 14 16 9 28E | 9 14 12 14 23 5 22 10 11 13 4 | 11 19 17 17 27 12 19 13 17 16 12 29 | 8 21 11 9 25 5 23 9 7 20 4 | 15 32 24 19 33 20 34 19 19 21 19 30E | 11 16 10 13 66 6 21 14 32 15 6 | 38 44 43 41 61 41 52 38 56 43 41 31 | 6 20 12 11 39 6 17 7 11 13 4 | 13 29 20 16 46 13 26 12 16 15 14 32 | 10 20 15 13 47 6 17 10 13 13 5 | 19 31 21 26 48 18 29 20 23 21 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 16 11 9 33 5 17 10 11 18 |T 18 26 22 22 33 19 26 20 22 21 19 WRMS | 7 16 11 9 30 5 16 9 8 16 |NE 18 26 22 22 32 18 25 19 21 21 18 MEDI | 6 15 11 8 29 5 17 9 9 15 |MD 17 26 20 23 33 18 24 19 21 20 17 Table 3.1539.1 GPS week: 1539 Day: 1 MJD: 55018.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 23 50 23 --- --- 16 --- 17 18 --- 12 | 24 40 19 --- --- 21 --- 14 23 --- 22 2 | 7 13 10 7 25 4 13 8 14 32 4 | 15 19 17 16 22 13 17 14 18 21 13 3 | 5 13 9 7 33 4 10 5 11 13 3 | 20 25 23 18 27 19 25 19 23 26 21 4 | 7 10 8 9 40 5 7 10 19 19 4 | 21 20 18 24 18 19 15 20 21 27 19 6 | 4 13 7 7 27 4 11 6 10 10 3 | 20 24 23 18 25 20 24 21 23 24 21 7 | 6 18 10 12 30 3 16 5 10 14 4 | 17 27 21 17 38 15 25 15 19 16 16 8 | 5 14 11 4 19 3 14 6 17 11 3 | 12 18 16 13 22 9 17 12 20 12 12 9 | 6 16 7 11 21 6 12 9 12 16 4 | 12 22 17 16 28 10 18 11 16 20 14 10 | 11 17 10 10 19 5 14 8 15 11 4 | 13 26 19 19 27 12 21 16 20 20 14 11 | 7 14 9 7 39 4 14 6 11 27 4 | 27 36 34 30 39 29 40 28 25 19 28 12E | 10 24 10 8 33 5 24 8 9 11 4 | 17 28 20 17 40 17 24 17 23 17 18 13 | 5 13 10 11 32 2 18 9 12 11 4 | 16 24 23 19 43 16 25 20 19 16 17 14 | 8 20 11 6 21 7 18 9 16 13 4 | 12 28 22 14 36 15 22 20 22 21 18 15 | 7 20 11 9 29 4 21 11 10 16 4 | 14 26 18 17 33 13 22 16 18 20 14 16E | 7 18 9 8 29 5 20 7 11 8 4 | 17 26 22 14 23 13 22 17 22 16 18 17 | 7 13 11 10 37 7 20 12 10 16 4 | 12 20 14 15 28 10 24 13 17 16 11 18 | 6 18 7 9 26 3 17 5 11 13 4 | 13 20 19 8 31 11 19 14 20 16 14 19 | 6 16 10 7 32 2 18 8 9 24 4 | 18 29 26 22 35 20 33 19 18 27 21 20 | 7 23 13 7 20 4 17 7 9 13 4 | 14 30 20 15 36 16 25 15 17 13 15 21 | 6 14 6 10 27 5 17 5 11 22 4 | 13 19 16 15 29 12 18 12 17 16 13 22 | 7 15 6 9 27 4 12 5 11 9 3 | 11 16 16 11 27 9 17 15 19 15 13 23 | 5 19 10 8 25 2 19 8 7 15 4 | 12 29 21 14 34 14 26 16 16 15 15 24 | 5 13 9 7 43 5 13 6 8 15 3 | 17 18 23 18 27 15 18 19 22 18 18 25 | 7 15 10 8 --- 3 11 6 10 20 4 | 14 27 23 16 --- 16 23 17 21 26 17 26 | 7 12 8 8 19 4 12 7 10 10 3 | 12 15 18 10 25 9 18 14 16 13 13 27 | 4 13 7 6 20 5 12 5 8 13 3 | 11 17 15 11 27 9 18 10 16 16 12 28E | 10 14 10 8 22 4 21 8 13 10 4 | 20 21 21 24 24 20 24 21 26 21 20 29 | 8 20 14 8 28 6 23 10 9 19 5 | 14 31 25 15 31 16 31 16 20 21 18 30E | 10 18 11 8 46 6 19 15 40 12 6 | 41 48 46 44 66 43 53 36 64 44 42 31 | 7 19 10 9 37 7 14 6 12 12 4 | 13 27 18 15 41 14 24 12 20 13 14 32 | 11 17 12 9 38 4 19 8 12 11 4 | 16 26 20 23 42 16 29 17 19 20 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 16 10 8 30 5 16 8 13 16 |T 16 25 21 17 31 15 23 16 21 19 17 WRMS | 7 16 10 8 28 4 15 7 9 16 |NE 14 23 20 16 30 14 22 16 19 18 16 MEDI | 7 16 10 8 28 4 16 8 11 13 |MD 14 26 20 16 29 15 23 16 20 18 17 Table 3.1539.2 GPS week: 1539 Day: 2 MJD: 55019.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 10 26 --- --- --- 21 --- 7 9 --- 7 | 23 32 --- --- --- 29 --- 14 18 --- 19 2 | 5 14 5 10 25 5 15 9 11 32 4 | 17 20 19 19 24 17 20 16 19 23 17 3 | 5 9 5 7 29 4 10 5 7 12 2 | 18 25 21 20 31 19 26 16 24 27 20 4 | 7 11 5 11 35 5 10 9 13 18 3 | 26 25 24 23 20 23 19 25 27 30 24 6 | 4 8 5 8 24 3 11 4 9 10 2 | 18 22 23 23 23 21 23 20 29 21 23 7 | 6 17 7 12 37 3 16 9 9 15 4 | 13 24 17 18 43 12 25 13 17 14 13 8 | 4 14 7 8 22 3 13 7 12 11 3 | 12 20 16 15 23 11 19 12 16 13 13 9 | 5 12 5 7 20 4 12 7 8 15 3 | 10 19 14 16 25 13 21 12 17 21 14 10 | 11 16 13 16 17 4 13 8 9 13 4 | 12 22 22 24 26 15 21 17 17 23 14 11 | 6 12 8 9 34 5 13 5 9 26 4 | 27 41 38 35 41 34 42 32 31 25 32 12E | 11 23 10 11 56 3 22 11 10 11 5 | 12 26 20 15 44 14 22 12 13 14 13 13 | 5 14 7 10 42 4 15 9 11 12 3 | 15 26 20 21 46 15 24 17 22 14 16 14 | 7 19 8 7 32 5 17 7 10 12 3 | 14 27 17 13 37 14 22 16 21 18 16 15 | 7 18 9 13 32 4 18 11 8 18 4 | 13 25 16 22 36 15 23 19 20 24 15 16E | 6 16 6 12 31 4 20 6 12 11 4 | 17 25 20 21 29 19 26 18 27 20 20 17 | 8 16 7 15 46 7 18 11 11 17 4 | 16 22 17 19 41 17 25 16 19 18 16 18 | 6 18 6 8 29 5 17 5 7 13 3 | 14 23 18 11 33 15 23 14 19 15 16 19 | 6 13 7 7 32 3 18 8 9 21 4 | 20 29 26 21 39 21 34 18 24 22 22 20 | 6 21 9 10 24 5 13 7 11 12 4 | 14 23 18 16 37 14 22 15 24 14 15 21 | 6 12 5 9 28 5 14 6 8 22 3 | 19 21 17 16 34 16 22 15 18 21 17 22 | 6 13 5 7 24 4 11 4 8 9 2 | 12 18 16 12 27 15 19 15 19 15 14 23 | 7 20 8 9 30 4 17 7 7 15 4 | 14 30 19 18 37 15 26 16 20 13 16 24 | 4 11 4 6 29 6 12 5 7 15 2 | 21 23 24 23 21 22 22 22 24 20 22 25 | 7 13 6 8 --- 3 11 8 8 21 3 | 10 24 18 15 --- 13 23 13 20 24 14 26 | 6 12 6 8 16 4 11 8 8 9 3 | 10 15 15 11 25 12 19 14 15 15 13 27 | 5 14 4 9 20 3 12 6 8 13 3 | 10 19 15 17 27 12 19 11 19 19 13 28E | 6 14 8 10 26 4 19 9 12 9 4 | 15 21 17 17 23 16 21 16 17 16 14 29 | 8 21 8 8 31 6 23 7 8 19 4 | 15 29 23 16 31 19 31 16 18 20 18 30E | 9 18 11 12 39 6 20 14 36 11 6 | 36 44 39 36 53 38 50 33 54 38 38 31 | 6 17 7 13 39 4 18 5 9 14 4 | 13 23 16 15 42 12 25 9 18 10 13 32 | 11 20 10 11 36 5 18 8 15 12 4 | 16 28 18 19 34 18 27 17 27 19 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 16 7 10 32 5 16 8 11 16 |T 16 24 20 18 32 17 24 16 21 19 17 WRMS | 7 16 7 10 28 4 15 7 8 17 |NE 15 23 19 18 32 16 23 16 20 19 17 MEDI | 6 14 7 9 30 4 15 7 9 13 |MD 15 24 18 18 33 15 23 16 19 19 16 Table 3.1539.3 GPS week: 1539 Day: 3 MJD: 55020.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 17 28 --- --- --- 17 --- 13 15 --- 10 | 20 27 --- --- --- 25 --- 13 24 --- 19 2 | 7 12 6 7 30 7 13 9 14 31 4 | 21 24 23 23 26 23 23 20 23 26 21 3 | 5 12 6 9 34 7 10 6 11 15 3 | 20 24 25 19 28 20 27 20 28 28 22 4 | 8 11 6 7 45 6 9 8 16 16 3 | 26 26 22 24 18 23 21 29 30 33 25 6 | 5 11 6 9 23 5 10 6 12 12 3 | 21 22 25 21 22 22 22 24 27 25 22 7 | 8 18 10 13 35 6 15 10 11 15 4 | 12 28 18 20 41 17 25 17 20 17 15 8 | 5 12 7 6 16 3 11 9 10 10 3 | 10 18 18 17 24 14 18 15 15 13 13 9 | 9 12 5 6 22 4 11 8 11 16 3 | 14 19 18 18 27 17 23 16 20 23 16 10 | 11 13 10 9 23 5 10 8 11 10 3 | 11 24 20 23 27 17 22 18 14 21 15 11 | 6 12 5 11 30 6 12 6 12 25 4 | 37 42 40 39 39 37 44 37 31 32 36 12E | 10 21 10 11 46 4 24 9 11 9 4 | 13 23 18 16 43 14 24 11 19 12 14 13 | 7 17 7 9 27 5 15 8 10 11 3 | 16 31 25 23 39 19 25 20 19 19 19 14 | 8 19 8 4 36 5 17 6 10 10 3 | 14 27 22 15 39 15 22 16 23 19 17 15 | 7 18 9 11 30 5 19 11 11 18 4 | 16 28 21 25 34 20 23 18 20 26 18 16E | 7 17 9 10 50 4 24 9 14 9 4 | 15 27 24 22 43 20 28 17 25 19 19 17 | 8 17 9 12 67 6 16 10 13 16 4 | 14 24 19 21 59 16 25 18 22 19 16 18 | 7 18 5 9 24 4 19 8 12 12 4 | 14 23 20 13 33 15 26 17 25 16 17 19 | 8 17 8 8 28 5 20 10 13 23 4 | 20 30 29 24 35 23 35 19 26 22 23 20 | 7 20 11 9 20 5 16 6 13 10 4 | 14 22 21 18 40 17 23 16 22 16 15 21 | 7 12 7 7 43 3 15 6 12 23 4 | 19 23 22 20 47 19 22 19 22 22 20 22 | 7 12 4 8 26 4 13 6 11 8 3 | 12 17 16 13 30 12 20 15 20 14 14 23 | 8 22 9 8 27 6 16 6 10 15 4 | 14 32 25 20 35 18 27 17 19 16 17 24 | 6 11 6 6 22 5 11 8 9 14 3 | 19 19 22 22 24 18 18 21 21 20 20 25 | 7 12 6 10 --- 3 10 10 10 21 4 | 12 25 19 22 --- 19 25 18 23 27 17 26 | 7 13 6 5 17 3 12 7 12 6 3 | 10 15 17 11 25 12 18 15 17 14 12 27 | 7 11 6 6 24 2 10 8 10 13 3 | 14 20 17 19 27 15 20 14 21 20 15 28E | 7 15 7 9 20 5 19 10 14 6 4 | 16 21 17 20 33 17 24 18 23 17 17 29 | 10 20 10 9 34 6 23 10 13 19 5 | 13 28 22 17 36 18 32 16 22 21 18 30E | 8 18 11 10 33 6 20 15 39 9 6 | 35 44 43 37 56 37 48 28 57 34 36 31 | 7 20 10 11 33 4 16 8 9 11 4 | 18 29 24 17 40 16 28 12 21 16 17 32 | 11 19 9 13 24 3 18 9 19 7 4 | 16 30 19 24 34 19 27 19 27 20 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 16 8 9 33 5 16 9 14 15 |T 16 25 22 20 34 19 25 18 23 20 18 WRMS | 8 16 8 9 30 5 15 8 11 16 |NE 16 25 21 20 33 18 24 18 22 20 18 MEDI | 7 17 7 9 28 5 15 8 12 12 |MD 15 24 21 20 34 18 24 18 22 20 17 Table 3.1539.4 GPS week: 1539 Day: 4 MJD: 55021.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 21 26 --- --- --- 12 --- 19 14 --- 11 | 26 27 --- --- --- 13 --- 19 19 --- 16 2 | 6 14 6 6 32 4 14 9 13 33 4 | 21 25 21 19 28 19 22 21 19 24 19 3 | 7 14 10 7 27 4 11 7 8 15 3 | 18 22 22 20 27 16 25 17 20 26 20 4 | 7 15 6 7 52 4 10 6 13 17 3 | 24 28 24 26 22 23 22 27 24 33 24 6 | 6 13 8 5 23 2 9 5 9 11 3 | 17 23 18 17 23 17 23 19 19 21 18 7 | 8 19 9 11 36 5 17 8 9 18 4 | 10 29 19 16 41 14 25 17 17 19 14 8 | 6 15 7 7 25 3 14 10 9 11 3 | 13 22 19 14 22 15 22 18 19 15 14 9 | 9 15 6 4 18 4 12 9 10 16 3 | 11 24 16 17 26 13 21 15 20 21 14 10 | 8 16 5 10 19 3 12 7 14 9 3 | 13 27 18 17 28 16 26 18 19 19 15 11 | 7 12 6 10 47 4 14 6 10 26 4 | 31 41 37 34 37 34 43 34 31 29 32 12E | 11 22 9 10 33 5 24 11 9 9 4 | 13 26 18 20 34 18 23 16 17 17 16 13 | 6 16 9 11 28 5 18 6 8 14 4 | 16 27 24 18 40 18 25 20 18 21 17 14 | 7 14 8 6 30 4 13 5 6 10 3 | 13 24 17 16 37 13 20 15 21 17 15 15 | 8 18 9 11 31 6 16 9 9 23 4 | 12 26 18 19 34 16 22 15 18 28 14 16E | 7 15 9 12 41 3 23 10 14 12 4 | 18 21 21 21 36 17 22 22 28 23 19 17 | 8 18 8 12 44 3 20 10 12 17 4 | 13 24 16 19 36 14 24 17 17 18 14 18 | 6 22 10 12 26 5 17 10 10 13 4 | 11 27 15 13 31 11 22 13 17 14 12 19 | 8 15 8 7 30 4 18 10 10 25 4 | 18 30 25 19 37 20 34 20 21 21 21 20 | 7 17 10 7 29 5 13 5 9 12 3 | 14 27 19 12 41 15 22 14 18 14 14 21 | 5 16 5 6 28 4 12 6 12 23 3 | 18 23 18 18 35 17 20 18 22 21 17 22 | 7 15 9 9 23 3 11 7 7 9 3 | 10 19 13 10 31 7 17 11 17 10 10 23 | 7 23 13 10 20 5 20 7 8 16 4 | 13 31 25 15 35 15 27 16 15 14 15 24 | 6 12 4 7 24 4 10 8 4 14 3 | 19 22 22 19 33 19 23 20 21 19 20 25 | 7 15 8 8 --- 3 12 9 7 21 4 | 14 27 18 15 --- 17 24 18 19 26 15 26 | 7 13 8 7 15 2 11 8 8 6 3 | 9 15 13 9 25 8 16 12 13 10 8 27 | 8 14 6 5 21 4 11 8 12 13 3 | 9 22 13 16 29 11 21 11 18 18 12 28E | 7 18 8 10 23 3 18 9 11 9 4 | 14 20 12 12 22 13 21 13 20 12 12 29 | 9 20 8 9 33 7 23 8 10 19 4 | 12 26 18 15 39 16 29 12 15 19 14 30E | 10 21 10 10 27 7 20 13 36 15 6 | 32 41 39 34 46 33 45 27 51 32 33 31 | 7 20 6 12 37 6 17 7 12 13 4 | 10 26 13 16 40 10 24 7 17 8 11 32 | 10 17 6 12 23 4 17 9 11 11 4 | 22 31 20 21 39 18 28 19 23 22 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 17 8 9 30 4 16 8 12 16 |T 15 25 19 17 32 16 24 17 20 19 16 WRMS | 7 17 8 9 29 4 15 8 8 19 |NE 15 25 19 17 32 15 24 17 19 19 16 MEDI | 7 16 8 9 28 4 14 8 10 14 |MD 14 26 18 17 34 16 23 17 19 19 15 Table 3.1539.5 GPS week: 1539 Day: 5 MJD: 55022.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 10 24 --- --- --- 14 --- 13 16 --- 8 | 24 26 --- --- --- 23 --- 15 25 --- 23 2 | 6 16 5 6 25 4 17 8 9 34 4 | 15 24 19 18 22 15 20 17 20 25 16 3 | 5 13 5 6 25 6 9 9 11 16 3 | 17 26 24 19 35 20 25 17 20 31 19 4 | 5 13 4 7 41 4 10 6 11 21 3 | 19 24 21 26 14 20 17 24 22 34 21 6 | 5 12 6 5 24 5 11 9 11 14 3 | 17 23 18 22 26 18 21 19 21 20 17 7 | 7 20 8 11 35 4 17 8 7 21 4 | 9 26 16 13 40 13 24 12 15 17 10 8 | 7 17 7 6 19 3 16 11 9 11 3 | 9 22 15 15 21 12 19 13 17 14 12 9 | 7 14 5 7 23 5 14 8 6 19 3 | 11 19 14 14 27 10 20 11 15 20 12 10 | 7 15 8 9 20 5 13 9 12 11 3 | 12 21 16 17 23 15 23 21 15 19 14 11 | 9 13 9 8 54 7 15 7 9 29 4 | 24 41 38 34 38 32 39 30 28 23 30 12E | 11 26 8 11 43 3 27 12 8 10 5 | 19 29 25 22 44 23 25 21 22 20 21 13 | 6 17 6 8 35 4 18 7 7 15 3 | 14 27 19 19 41 16 25 17 15 20 15 14 | 6 20 6 9 28 5 16 5 10 10 3 | 11 27 16 15 36 12 19 13 20 16 14 15 | 6 20 12 14 34 5 19 10 10 21 5 | 13 24 18 21 33 14 22 15 16 26 13 16E | 7 15 8 7 44 4 23 9 11 11 4 | 17 23 23 21 44 18 25 20 26 22 20 17 | 7 19 10 10 29 6 22 13 11 18 4 | 14 24 18 18 31 13 24 18 19 20 15 18 | 5 22 9 7 32 5 20 9 10 14 4 | 10 25 18 10 37 11 24 13 18 14 13 19 | 7 17 7 7 27 4 20 9 13 31 4 | 17 31 25 19 37 20 34 16 24 24 20 20 | 6 18 11 8 19 6 17 7 11 12 4 | 12 19 18 15 33 13 20 13 20 14 13 21 | 5 16 6 9 74 4 17 6 10 23 4 | 15 21 14 12 73 12 21 16 17 18 14 22 | 5 15 8 9 29 5 12 8 8 11 3 | 10 19 15 12 33 9 17 13 18 15 12 23 | 7 24 11 10 25 5 21 7 10 17 4 | 10 31 21 12 33 12 26 13 14 12 12 24 | 4 14 4 7 19 4 10 7 6 17 3 | 15 20 17 19 23 16 16 16 19 16 16 25 | 6 16 5 5 --- 3 12 7 7 25 3 | 12 23 16 14 --- 14 20 14 19 27 14 26 | 5 17 8 9 18 4 12 9 8 6 3 | 5 15 14 8 25 7 17 11 14 10 8 27 | 5 14 7 9 19 4 14 8 8 17 3 | 10 19 13 14 30 11 21 11 16 17 11 28E | 5 18 8 9 31 5 23 11 9 9 4 | 12 22 15 17 35 15 22 16 18 17 15 29 | 10 22 6 10 26 5 23 7 9 21 4 | 11 26 20 17 32 16 27 14 16 19 15 30E | 8 22 14 9 42 7 24 16 30 14 6 | 35 42 44 36 49 37 48 34 51 33 37 31 | 5 22 6 12 37 5 20 5 7 11 4 | 10 27 14 13 37 8 24 8 17 10 11 32 | 10 19 9 13 22 5 18 9 11 12 4 | 17 29 19 24 34 18 26 18 22 21 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 18 8 9 33 5 18 9 11 18 |T 14 25 19 17 34 15 23 16 19 19 16 WRMS | 6 18 7 9 30 5 17 8 7 16 |NE 13 24 18 16 32 14 22 15 18 19 14 MEDI | 6 17 7 9 28 5 17 8 10 15 |MD 13 24 18 17 33 15 22 16 19 19 15 Table 3.1539.6 GPS week: 1539 Day: 6 MJD: 55023.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 3 --- --- --- --- 20 --- --- --- --- 0 | 31 --- --- --- --- 30 --- --- --- --- 35 2 | 5 12 6 8 32 4 14 8 12 34 4 | 27 27 29 30 37 28 29 29 30 35 27 3 | 7 14 5 7 30 5 13 14 8 24 4 | 21 25 23 20 33 20 26 23 21 33 22 4 | 8 10 5 6 33 5 8 8 20 27 4 | 33 34 34 35 21 32 29 37 33 47 33 6 | 6 13 6 7 30 5 12 9 9 18 3 | 27 24 28 31 32 26 25 33 27 34 28 7 | 6 16 9 13 31 7 18 8 7 22 4 | 11 26 17 12 39 12 27 11 12 17 12 8 | 6 14 6 6 25 4 13 10 7 12 3 | 12 23 15 15 27 13 21 15 14 13 13 9 | 7 14 6 10 20 4 14 7 11 19 3 | 14 21 17 16 25 15 22 13 21 20 15 10 | 8 15 7 13 21 7 15 9 13 13 4 | 13 27 17 22 27 19 23 23 22 19 16 11 | 7 11 9 7 51 5 15 8 8 31 4 | 43 51 49 47 41 44 51 46 43 40 44 12E | 9 20 7 9 29 5 23 7 10 12 4 | 15 24 20 17 39 15 25 16 18 17 15 13 | 5 14 10 10 32 3 23 11 8 13 4 | 17 25 24 19 48 17 30 18 18 18 18 14 | 5 17 5 8 26 4 20 8 7 11 3 | 16 26 19 17 34 17 25 18 20 19 18 15 | 8 13 8 13 29 4 20 10 8 20 4 | 17 25 20 23 32 20 22 18 24 27 17 16E | 5 18 6 9 39 5 23 9 10 12 4 | 8 20 13 14 32 9 21 13 16 14 10 17 | 7 18 12 13 39 4 23 17 12 19 5 | 15 27 20 19 39 17 27 22 18 22 16 18 | 5 20 9 10 28 5 20 14 10 15 4 | 15 26 17 12 36 14 27 19 16 16 15 19 | 6 17 7 8 39 6 21 8 6 39 5 | 17 31 24 18 38 20 35 16 19 30 19 20 | 6 20 10 8 24 6 18 10 10 12 4 | 14 23 16 14 40 15 26 15 18 16 14 21 | 7 15 6 7 38 5 16 7 8 27 4 | 24 28 21 21 41 21 27 22 20 24 21 22 | 7 12 8 8 28 4 14 11 6 10 3 | 10 19 15 11 34 9 20 16 13 13 11 23 | 6 21 8 9 25 3 26 12 10 16 4 | 13 29 20 15 36 15 29 17 17 15 15 24 | 6 12 4 6 22 6 12 8 7 19 3 | 23 26 25 26 26 23 21 25 26 24 24 25 | 6 14 10 9 --- 4 13 7 8 23 4 | 13 27 22 16 --- 15 24 14 20 27 17 26 | 5 14 8 7 16 2 14 9 7 11 3 | 11 15 17 9 24 9 20 12 11 15 11 27 | 6 11 7 10 21 3 14 8 10 17 3 | 14 22 16 17 26 16 23 13 21 18 14 28E | 7 17 7 10 25 6 27 13 13 14 4 | 8 18 11 11 28 9 24 14 16 15 10 29 | 11 24 7 7 30 5 23 10 11 21 5 | 15 34 22 17 40 20 35 17 21 22 18 30E | 11 21 9 12 55 7 23 14 36 9 6 | 36 40 39 35 54 33 48 32 41 30 33 31 | 8 19 7 11 25 6 21 7 11 12 4 | 13 24 15 14 34 11 26 10 18 12 12 32 | 10 19 6 12 16 5 18 12 13 14 4 | 18 26 19 20 33 17 28 18 22 23 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 16 8 9 31 5 18 10 12 19 |T 18 26 21 19 34 18 27 19 21 22 19 WRMS | 7 16 7 9 30 5 17 9 7 17 |NE 17 26 21 19 33 18 26 20 20 23 18 MEDI | 6 15 7 9 29 5 18 9 10 16 |MD 15 26 20 17 34 17 26 17 20 19 17 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 4.1539 GPS week: 1539 MJD: 55017.0-55023.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2961 |U 9 9 23 |U 28 30 87 |U 10 9 20 | emr | emr 2957 | 11 11 29 | 31 33 92 |U 10 13 22 | esa | esa 2907 | 9 10 25 |U 27 30 85 | 10 9 20 | gfz | gfz 2865 |U 9 9 23 |U 29 35 92 | 10 9 21 | grg | grg 2784 | 9 10 26 |U 32 31 94 | 10 12 24 | igr | igr 2882 | 9 10 24 | 28 28 86 | 17 13 24 | igs | igs 2917 | 9 9 24 | 27 29 86 | 17 13 23 | jpl | jpl 2875 | 10 10 26 |U 29 28 89 |U 11 10 21 | mit | mit 2962 |U 16 12 36 |U 34 32 91 |U 14 14 32 | 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 5.1539.0 GPS week: 1539 Day: 0 MJD: 55017.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2939 | 9 15 32 | 5 13 28 | 6 6 19 | emr | emr 2971 | 11 15 35 | 8 24 36 | 6 7 20 | esa | esa 2976 | 9 14 33 | 5 16 26 | 7 5 17 | gfz | gfz 2867 | 9 14 32 | 6 25 32 | 7 6 21 | grg | grg 2784 | 11 16 36 | 7 11 34 | 6 8 22 | igr | igr 2876 | 9 14 33 | 5 16 28 | 7 6 19 | igs | igs 2908 | 9 14 31 | 5 14 28 | 6 6 20 | jpl | jpl 2876 | 10 16 37 | 6 14 38 | 6 6 19 | mit | mit 2976 | 9 14 32 | 9 18 44 | 10 9 31 | Table 5.1539.1 GPS week: 1539 Day: 1 MJD: 55018.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2964 | 11 11 24 | 153 123 435 | 28 26 24 | emr | emr 2972 | 14 13 32 | 158 130 433 | 20 32 22 | esa | esa 2976 | 12 11 27 | 150 123 433 | 30 30 23 | gfz | gfz 2867 | 11 10 25 | 154 130 439 | 27 27 22 | grg | grg 2784 | 12 12 24 | 159 125 431 | 23 33 25 | igr | igr 2902 | 12 12 27 | 152 124 435 | 78 52 48 | igs | igs 2897 | 11 12 27 | 152 125 436 | 79 52 48 | jpl | jpl 2874 | 12 13 27 | 160 131 441 | 36 29 30 | mit | mit 2976 | 16 18 50 | 153 125 438 | 36 33 35 | Table 5.1539.2 GPS week: 1539 Day: 2 MJD: 55019.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2971 | 11 9 25 | 7 18 23 | 7 4 14 | emr | emr 2971 | 11 11 36 | 10 16 29 | 8 9 16 | esa | esa 2880 | 10 8 29 | 9 16 21 | 7 4 15 | gfz | gfz 2866 | 10 8 27 | 9 22 32 | 7 4 16 | grg | grg 2784 | 10 8 32 | 10 16 30 | 8 6 18 | igr | igr 2879 | 11 9 30 | 8 14 23 | 6 4 14 | igs | igs 2916 | 11 9 29 | 8 16 23 | 7 4 13 | jpl | jpl 2875 | 11 9 33 | 8 15 27 | 7 5 13 | mit | mit 2976 | 11 8 27 | 8 11 26 | 7 4 18 | Table 5.1539.3 GPS week: 1539 Day: 3 MJD: 55020.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2966 | 7 7 20 | 11 15 39 | 7 7 14 | emr | emr 2970 | 9 10 26 | 14 13 59 | 9 12 20 | esa | esa 2880 | 7 9 19 | 10 12 35 | 7 7 13 | gfz | gfz 2864 | 7 8 20 | 10 13 40 | 8 7 14 | grg | grg 2784 | 7 9 26 | 12 21 42 | 8 9 21 | igr | igr 2880 | 7 9 20 | 10 13 37 | 8 7 13 | igs | igs 2942 | 7 8 20 | 10 12 37 | 8 7 14 | jpl | jpl 2876 | 8 9 22 | 11 14 45 | 7 8 18 | mit | mit 2976 | 11 14 32 | 10 12 35 | 10 13 32 | Table 5.1539.4 GPS week: 1539 Day: 4 MJD: 55021.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2969 | 9 7 22 | 5 11 31 | 8 7 23 | emr | emr 2970 | 10 8 26 | 8 10 28 | 10 9 24 | esa | esa 2880 | 9 8 23 | 5 11 28 | 8 8 24 | gfz | gfz 2864 | 9 6 21 | 7 14 33 | 8 8 26 | grg | grg 2784 | 9 8 25 | 6 9 35 | 10 11 26 | igr | igr 2880 | 9 7 21 | 5 8 26 | 8 9 23 | igs | igs 2954 | 9 6 21 | 5 8 27 | 8 8 23 | jpl | jpl 2874 | 10 7 24 | 6 7 29 | 8 8 22 | mit | mit 2976 | 46 16 67 | 10 14 36 | 11 12 26 | Table 5.1539.5 GPS week: 1539 Day: 5 MJD: 55022.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2969 | 6 5 17 | 8 20 29 | 8 6 24 | emr | emr 2971 | 9 7 21 | 10 20 31 | 9 9 27 | esa | esa 2880 | 6 5 19 | 6 19 24 | 8 7 24 | gfz | gfz 2865 | 6 4 15 | 10 25 36 | 8 7 25 | grg | grg 2784 | 7 7 18 | 18 23 48 | 9 10 32 | igr | igr 2880 | 7 5 16 | 8 13 25 | 8 7 24 | igs | igs 2927 | 6 4 16 | 7 15 25 | 8 7 24 | jpl | jpl 2876 | 8 6 20 | 7 9 21 | 7 8 27 | mit | mit 2976 | 6 4 17 | 5 8 22 | 10 10 30 | Table 5.1539.6 GPS week: 1539 Day: 6 MJD: 55023.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2951 | 8 11 24 | 6 11 25 | 6 6 24 | emr | emr 2876 | 9 12 25 | 8 17 25 | 8 12 22 | esa | esa 2880 | 8 12 25 | 6 14 27 | 6 5 22 | gfz | gfz 2864 | 8 11 24 | 6 16 31 | 6 6 24 | grg | grg 2784 | 8 11 24 | 8 12 38 | 7 6 24 | igr | igr 2879 | 8 12 25 | 7 11 26 | 7 6 24 | igs | igs 2879 | 9 13 27 | 6 10 23 | 6 6 22 | jpl | jpl 2876 | 9 12 21 | 7 8 25 | 6 7 18 | mit | mit 2880 | 9 11 28 | 42 35 37 | 18 17 50 | 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 6.1539 GPS week: 1539 MJD: 55017.500-55023.500 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 | 2 -45 115 -34 -7 | -2 15 | 24 15 83 63 4 | 2 emr uuuuu | 21 -31 43 230 6 | 12 22 | 12 19 57 93 5 | 5 esa uuuuu | -35 -30 -80 -27 -7 | 5 14 | 21 16 150 57 11 | 1 gfz uuuuu | 51 -2 50 43 -3 | 9 20 | 14 19 36 50 2 | 3 grg xxxxx | 7 -18 148 -29 -1 | -1 16 | 38 27 63 57 28 | 4 igr xxxxx | 29 16 -9 20 -7 | 11 17 | 19 12 85 41 7 | 2 irf xxxxx | -10 -12 6 -13 2 | 3 16 | 8 6 16 22 6 | 5 jpl uuuuu | -10 -20 180 -62 2 | 8 21 | 31 30 56 56 14 | 7 mit uuuuu | -44 -20 -46 -102 9 | 3 18 | 21 11 100 30 7 | 6 ngs uuuuu | 2 47 -100 79 -8 | 3 14 | 40 37 94 92 6 | 2 sio uuuuu | 67 101 61 -84 10 | 11 23 | 14 12 123 37 9 | 8 Table 7.1539.0 GPS week: 1539 Day: 0 MJD: 55017.500 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 | -7 -48 9 -46 -3 | -3 17 emr uuuuu | 31 -23 17 275 8 | 7 20 esa uuuuu | -60 -32 -339 -94 -12 | 5 15 gfz uuuuu | 48 0 -9 14 -3 | 6 20 grg xxxxx | -9 -54 154 67 -25 | 4 20 igr xxxxx | 14 -2 -73 1 -4 | 8 15 irf xxxxx | -13 -18 17 -6 3 | -3 16 jpl uuuuu | -20 -11 138 -49 3 | -1 18 mit uuuuu | -59 -26 86 -62 9 | -4 16 ngs uuuuu | 28 32 27 38 -10 | 4 15 sio uuuuu | 69 98 160 -93 13 | 2 17 Table 7.1539.1 GPS week: 1539 Day: 1 MJD: 55018.500 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 -37 81 -88 -7 | -2 18 emr uuuuu | 38 -35 56 222 1 | 8 21 esa uuuuu | -55 -48 -240 -14 -14 | 7 15 gfz uuuuu | 54 -6 81 0 1 | 8 21 grg xxxxx | 26 20 33 -44 -9 | 4 20 igr xxxxx | 13 31 -131 -30 -5 | 11 17 irf xxxxx | -21 -13 -15 -22 5 | -2 17 jpl uuuuu | 20 -13 214 -138 14 | 1 20 mit uuuuu | -62 -27 -5 -103 12 | -3 17 ngs uuuuu | 14 82 -80 268 -15 | 5 15 sio uuuuu | 52 110 104 -154 17 | 3 20 Table 7.1539.2 GPS week: 1539 Day: 2 MJD: 55019.500 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 | 34 -24 75 81 -10 | -4 18 emr uuuuu | 14 -6 -58 184 9 | 6 19 esa uuuuu | -44 -11 -64 20 -14 | 4 13 gfz uuuuu | 66 -17 18 91 -5 | 7 21 grg xxxxx | 55 9 217 -24 -31 | 2 20 igr xxxxx | 66 27 -20 42 -20 | 10 16 irf xxxxx | -13 -8 28 -6 8 | -3 17 jpl uuuuu | -15 -1 185 -133 11 | 3 20 mit uuuuu | -62 -23 62 -77 15 | -4 17 ngs uuuuu | 75 15 -213 13 -14 | 2 15 sio uuuuu | 49 108 206 -84 21 | 4 20 Table 7.1539.3 GPS week: 1539 Day: 3 MJD: 55020.500 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 | 18 -50 251 -74 -12 | 0 14 emr uuuuu | 20 -48 48 297 14 | 12 21 esa uuuuu | -39 -32 42 -113 -17 | 5 14 gfz uuuuu | 41 -10 39 126 -2 | 11 21 grg xxxxx | 42 -26 137 19 -13 | -2 17 igr xxxxx | 36 20 -56 57 0 | 12 16 irf xxxxx | -5 -7 12 10 1 | 4 15 jpl uuuuu | 1 -32 104 -53 14 | 10 20 mit uuuuu | -30 -6 -101 -123 11 | 3 18 ngs uuuuu | -19 62 -128 89 -6 | 4 15 sio uuuuu | 80 112 45 -58 9 | 12 22 Table 7.1539.4 GPS week: 1539 Day: 4 MJD: 55021.500 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 | -30 -35 190 -2 -7 | 1 14 emr uuuuu | 28 -9 49 345 5 | 16 25 esa uuuuu | -20 -44 12 -40 -5 | 6 14 gfz uuuuu | 29 -23 78 -4 -5 | 14 22 grg xxxxx | -59 -9 201 -104 15 | -6 11 igr xxxxx | 19 20 95 31 0 | 15 19 irf xxxxx | -14 -9 8 13 5 | 8 16 jpl uuuuu | 24 20 135 20 2 | 16 23 mit uuuuu | -44 -8 -63 -79 14 | 8 19 ngs uuuuu | -16 39 -219 -12 -10 | 6 16 sio uuuuu | 67 102 116 -36 15 | 17 25 Table 7.1539.5 GPS week: 1539 Day: 5 MJD: 55022.500 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 | 3 -71 65 -101 -6 | -2 13 emr uuuuu | 11 -34 136 230 3 | 16 25 esa uuuuu | 2 -4 -8 35 8 | 4 13 gfz uuuuu | 50 7 58 19 -4 | 11 19 grg xxxxx | 5 -44 184 -47 1 | -5 11 igr xxxxx | 37 7 38 69 -12 | 13 18 irf xxxxx | -11 -8 7 -44 -2 | 8 16 jpl uuuuu | -15 -27 262 -53 -16 | 16 23 mit uuuuu | -49 -13 -107 -132 7 | 10 20 ngs uuuuu | -25 -2 -76 62 -6 | 2 14 sio uuuuu | 65 101 -83 -99 2 | 19 27 Table 7.1539.6 GPS week: 1539 Day: 6 MJD: 55023.500 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 | -23 -50 132 -10 -2 | -4 12 emr uuuuu | 6 -59 53 58 -1 | 15 24 esa uuuuu | -29 -37 36 13 8 | 3 12 gfz uuuuu | 68 34 85 52 -2 | 8 15 grg xxxxx | -10 -25 107 -68 52 | -4 11 igr xxxxx | 18 6 86 -31 -10 | 11 14 irf xxxxx | 5 -24 -15 -36 -9 | 7 15 jpl uuuuu | -68 -77 220 -28 -18 | 13 21 mit uuuuu | -4 -38 -195 -137 -5 | 10 20 ngs uuuuu | -41 100 -9 92 2 | 0 11 sio uuuuu | 88 76 -122 -68 -4 | 20 27