Date: Thu, 16 Jul 2009 12:39:02 +0000 From: Jim Ray Subject: [IGSREPORT-17594] Wk 1538 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4a5f1f66.TnVzuHZ9l2Uo+xfU%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 16 Jul 05:39:24 PDT 2009 Message Number 17594 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1538 (Jun 28, 2009 - Jul 04, 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: igs1538[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1538[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1538[0-6].cls IGS GPS clock combination summary report. igs15387.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15387.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 | EMR | 32 32 WTZR 0 | GFZ | 7 15 32 AUCK BOR1 CHUR FAA1 NANO 0 | GRG | ONSA 0 | JPL | 32 UNSA 0 | MIT | HOB2 1 | ALL | 1 1 1 | EMR | MIZU 1 | ESA | 32 YELL 1 | GFZ | 7 15 32 AUCK 1 | GRG | ONSA 1 | JPL | 32 1 | MIT | 25 25 YELL YELL 2 | ALL | 1 1 2 | EMR | 32 32 MIZU 2 | ESA | 27 HOFN 2 | GFZ | 7 15 21 27 29 ALIC AREQ AUCK BAN2 BRAZ CHUR DARW 2 | GFZ | HARB HOB2 MAW1 TOW2 UNSA WTZR YAR2 2 | GRG | BRAZ DAV1 ONSA 2 | JPL | 27 30 2 | MIT | 27 30 27 30 3 | ALL | 1 3 | COD | NANO 3 | EMR | 32 32 YAR2 3 | ESA | DAV1 UNSA 3 | GFZ | 7 15 29 BAN2 3 | GRG | DAV1 ONSA 3 | JPL | 30 IRKJ 3 | MIT | 15 17 19 15 17 CEDU 3 | NGS | 1 4 | ALL | 1 1 4 | COD | 30 30 4 | EMR | 32 32 MIZU 4 | ESA | UNSA 4 | GFZ | 7 15 16 29 ALIC BAN2 CHUR DARW TOW2 4 | GRG | DAV1 IRKJ ONSA 4 | JPL | 30 32 5 | ALL | 1 5 | COD | 30 30 5 | EMR | 32 32 WTZR AREQ HARB WTZR 5 | ESA | 30 5 | GFZ | 7 12 15 29 30 ALIC BAN2 CHUR DARW MAW1 TOW2 UNSA 5 | GRG | DAV1 MCM4 ONSA 5 | JPL | 32 DAV1 5 | MIT | 1 KHAJ 6 | COD | 1 30 1 30 6 | EMR | WTZR MIZU WTZR 6 | ESA | 1 30 6 | GFZ | 7 15 29 32 ALIC BAN2 CAS1 CHAT CHUR DARW HOFN MAW1 6 | GFZ | TOW2 UNSA 6 | GRG | MCM4 ONSA TWTF 6 | JPL | 32 6 | MIT | HRAO 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 | .6 .6 .6 -15 -23 -7 -.22 EMR | 12.4 -10.9 -6.5 62 6 51 -.31 ESA | 5.5 -.4 9.9 9 -34 23 -.07 GFZ | .1 1.1 1.8 17 0 5 -.41 GRG | 5.7 .0 1.4 -19 -6 14 .05 JPL | 4.4 -7.1 -3.0 8 1 3 .03 MIT | 5.8 -9.4 14.3 0 34 -29 -.28 NGS | 9.6 -8.3 12.5 -75 -73 7 -.33 SIO | 3.8 -7.0 -4.0 -114 -77 -4 -.03 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 1.1538.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1538.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 2.1538.[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 3.1538.[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 5.1538.0-6). 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 1538 summary. (Jun 28, 2009 - Jul 04, 2009) Table 1.1538.a GPS week: 1538 MJD: 55010.000-55016.000 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 236| 0 0 0 3 15 -34 -.11 8 7 | -232 -923 16 69 | 0 0 1 13 8 24 .02 | 603 782 emr 76| 3 -1 -4 -147 -14 -20 .39 17 17 | 3894 -698 17 103 | 1 1 2 25 23 17 .04 | 1135 1456 esa 123| 0 0 1 -41 -2 0 .35 9 8 | -1251 1023 19 142 | 1 0 1 17 43 9 .02 | 1042 1322 gfz 191| 1 0 3 -63 -41 113 -.10 10 10 | 227 -87 24 185 | 0 1 1 10 11 73 .03 | 287 413 grg 109| 1 0 -4 -2 14 -76 1.06 33 30 | 128 -186 81 205 | 1 1 2 35 19 67 .10 | 434 610 igr n/a| -1 0 -1 -9 -31 -50 .04 5 5 | 25351 -444 19 86 | 0 0 0 18 10 25 .01 | 1068 1472 jpl 130| 0 2 -11 -49 -30 16 .56 17 16 | 3768 -788 17 93 | 0 0 1 22 10 41 .04 | 1193 1463 mit 259| 0 -1 1 -20 -109 -35 -.26 10 9 | -9501 3193 22 170 | 0 1 0 28 19 27 .02 | 9324 8890 ngs 211| -1 0 1 148 125 -44 -.30 12 9 | 8020 -4153 2093 3722 | 0 1 1 35 39 13 .05 | 8036 7679 sio 261| -2 0 1 234 132 -23 -.22 18 18 | --- --- --- --- | 0 1 1 41 33 24 .03 | --- --- Table 1.1538.b GPS week : 1538 MJD: 55010.000-55016.000 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 | 0 17 16 14 10 13 12 | 2 | 5 4 4 4 4 5 5 | 3 | 4 4 4 4 4 4 4 | 4 | 4 4 4 3 3 4 4 | 6 | 4 3 4 4 3 3 4 | 7 | 5 5 5 5 4 4 5 | 8 | 5 4 4 3 3 3 4 | 9 | 5 4 4 5 4 4 5 | 10 | 7 7 5 5 5 5 5 | 11 | 4 4 5 4 4 4 4 | 12 | 6 5 6 5 6 6 5 | 13 | 5 5 5 5 5 4 4 | 14 | 5 4 5 4 4 4 4 | 15 | 5 5 5 5 5 5 6 | 16 | 5 5 5 4 4 4 4 | 17 | 6 5 6 6 6 6 5 | 18 | 5 5 5 4 4 5 5 | 19 | 5 5 5 5 4 4 4 | 20 | 4 5 5 4 4 5 4 | 21 | 5 4 4 4 4 4 4 | 22 | 5 4 4 4 4 3 4 | 23 | 6 5 5 5 5 5 5 | 24 | 4 4 3 4 3 4 4 | 25 | 9 8 7 7 4 4 4 | 26 | 4 4 4 3 3 4 4 | 27 | 4 4 4 4 4 4 4 | 28 | 5 5 4 5 4 4 5 | 29 | 5 5 5 5 5 6 5 | 30 | 6 5 6 6 6 6 6 | 31 | 5 5 5 4 5 4 4 | 32 | 6 6 6 6 6 5 7 | 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 2.1538.0 GPS week: 1538 Day: 0 MJD: 55010.000 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 236| 0 0 0 -1 3 -63 -.09 10 8 | -320 -637 22 77 | 38 16 | emr 76| 2 0 -6 -123 -7 -45 .35 18 18 | 3834 -827 17 90 | -13 -78 | esa 123| 1 0 0 -65 19 -9 .33 9 8 | -468 -1056 20 112 | 63 22 | gfz 191| 0 1 3 -70 -55 209 -.16 10 10 | 410 -471 26 117 | 25 25 | grg 109| 1 2 -1 0 3 -222 1.02 32 30 | 44 -137 78 220 | -26 33 | igr n/a| 0 0 0 -4 -43 -74 .06 5 5 | 24606 -250 20 63 | -46 5 | jpl 130| 0 3 -11 -72 -30 -63 .47 17 17 | 3802 -538 18 83 | 24 -18 | mit 259| -1 -3 2 -20 -101 -66 -.23 12 11 | -27 -104 24 146 | 4 30 | ngs 211| -2 -1 1 216 108 -31 -.30 14 12 | -240 -679 2060 3496 | -108 46 | sio 261| -2 -1 0 239 181 -56 -.21 20 18 | --- --- --- --- | -132 -79 | Table 2.1538.1 GPS week: 1538 Day: 1 MJD: 55011.000 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 236| 0 0 -2 10 8 -47 -.14 9 8 | -50 -751 20 71 | -24 12 | emr 76| 1 0 -6 -133 -18 -31 .35 17 17 | 3606 257 16 112 | 9 -50 | esa 123| 0 1 4 -13 5 14 .33 8 7 | -2395 2880 18 139 | 1 2 | gfz 191| 2 0 6 -46 -41 132 -.09 10 10 | -150 544 23 149 | 7 29 | grg 109| 2 0 -5 42 4 -64 .95 33 31 | -108 352 77 209 | -58 29 | igr n/a| -1 0 -1 -25 -40 -41 .04 6 5 | 25045 527 19 78 | 2 -28 | jpl 130| 0 0 -12 -61 -13 30 .54 18 18 | 4039 234 17 98 | 21 10 | mit 259| 0 -1 0 -61 -79 -47 -.26 11 10 | -15036 -356 22 193 | 17 29 | ngs 211| 0 -1 0 165 100 -54 -.33 12 9 | 16008 -669 2438 3818 | -62 -59 | sio 261| -2 -1 -1 190 160 -20 -.23 19 19 | --- --- --- --- | -108 -47 | Table 2.1538.2 GPS week: 1538 Day: 2 MJD: 55012.000 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 236| 1 0 0 -10 10 -51 -.10 8 7 | 45 -1086 15 72 | 70 -33 | emr 76| 2 0 0 -187 -48 -40 .34 17 17 | 4087 31 17 101 | 54 -4 | esa 123| 0 0 0 -48 28 0 .37 9 9 | -2030 1950 18 144 | 28 -5 | gfz 191| 0 0 1 -58 -42 205 -.08 11 11 | 291 -386 24 178 | 64 -13 | grg 109| 3 -2 -3 -46 55 -31 .93 35 34 | 163 -122 83 194 | 48 -16 | igr n/a| -1 0 0 -23 -10 -82 .04 6 6 | 25836 -4 21 100 | -31 -61 | jpl 130| 0 3 -9 -73 -19 30 .54 17 16 | 4459 -372 16 100 | 49 1 | mit 259| 0 0 2 21 -123 -76 -.29 11 10 | -15500 594 21 164 | -3 39 | ngs 211| 0 -2 0 124 93 -43 -.35 11 9 | 8223 -175 2006 3816 | -48 -39 | sio 261| -2 0 0 305 132 -50 -.27 18 18 | --- --- --- --- | -132 -55 | Table 2.1538.3 GPS week: 1538 Day: 3 MJD: 55013.000 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 236| 0 0 -2 29 12 -44 -.10 8 8 | -280 -1500 21 88 | -27 -7 | emr 76| 4 -1 -3 -169 -37 -3 .42 18 18 | 5040 -2108 19 104 | 47 -42 | esa 123| 0 0 2 -24 54 -5 .37 8 8 | -899 -112 21 171 | 19 -2 | gfz 191| 0 0 3 -63 -50 99 -.14 9 9 | 560 -494 25 226 | 9 -4 | grg 109| 0 0 -1 48 11 -40 1.05 35 32 | 618 -1187 80 212 | -59 11 | igr n/a| -1 0 -2 26 -34 -70 .04 5 5 | 26457 -2251 21 72 | -74 -30 | jpl 130| 0 1 -11 -9 -33 57 .59 17 16 | 4907 -2523 17 101 | -30 7 | mit 259| 0 0 1 -45 -101 -22 -.27 9 8 | -15286 -805 34 247 | 16 35 | ngs 211| -2 0 0 138 90 -57 -.27 12 10 | 13296 -2941 2178 3694 | -60 -10 | sio 261| -1 0 2 210 135 -31 -.23 17 17 | --- --- --- --- | -122 -47 | Table 2.1538.4 GPS week: 1538 Day: 4 MJD: 55014.000 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 236| 0 0 -1 -3 27 6 -.11 7 7 | -1502 612 11 52 | 49 -37 | emr 76| 5 -4 -4 -145 -12 -10 .45 17 17 | 3532 -65 17 122 | 29 -35 | esa 123| 0 0 2 -45 -34 -10 .35 7 7 | -1914 927 20 147 | -10 41 | gfz 191| 0 0 2 -81 -49 72 -.09 10 10 | -144 377 25 232 | 42 -8 | grg 109| 2 -1 -7 -30 16 -56 1.11 33 29 | -510 285 90 200 | 55 13 | igr n/a| -1 0 0 -19 -33 -41 .05 5 5 | 24838 149 19 91 | -31 -24 | jpl 130| 0 1 -11 -50 -30 11 .57 17 16 | 3121 -235 16 93 | 33 24 | mit 259| 0 0 0 1 -109 -14 -.25 10 9 | -21288 23324 20 167 | 12 16 | ngs 211| -1 0 4 104 127 -58 -.34 10 8 | 18355 -21446 1994 3770 | 23 -10 | sio 261| -1 0 2 272 127 -5 -.23 17 17 | --- --- --- --- | -144 -53 | Table 2.1538.5 GPS week: 1538 Day: 5 MJD: 55015.000 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 236| 1 0 -1 -7 23 -13 -.10 7 7 | 301 -1727 13 70 | 26 -5 | emr 76| 3 -1 -3 -155 8 -11 .38 18 18 | 5308 -3159 17 93 | 25 -68 | esa 123| 0 0 2 -39 -75 0 .33 9 9 | 564 827 20 151 | 13 81 | gfz 191| 2 1 2 -61 -22 53 -.08 9 9 | 474 -169 23 213 | 36 -20 | grg 109| 0 -2 -8 -17 14 -91 1.23 30 28 | 749 -843 80 203 | 9 -9 | igr n/a| 0 0 -2 -21 -30 -31 .03 5 5 | 26836 -2657 20 101 | -42 -10 | jpl 130| 0 2 -12 -41 -43 -5 .61 17 17 | 4632 -3059 18 84 | 23 58 | mit 259| 0 0 1 -8 -106 -14 -.25 9 8 | 705 -633 20 143 | 14 20 | ngs 211| 0 -1 4 137 159 -35 -.24 11 8 | 291 -1749 1913 3814 | -68 -54 | sio 261| -3 0 2 225 114 -8 -.17 17 16 | --- --- --- --- | -122 -45 | Table 2.1538.6 GPS week: 1538 Day: 6 MJD: 55016.000 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 236| 0 0 0 8 20 -29 -.14 8 7 | 182 -1374 14 56 | 26 -46 | emr 76| 3 -1 -3 -118 14 -2 .42 17 17 | 1852 982 20 104 | -5 -78 | esa 123| -1 0 1 -51 -17 9 .38 10 10 | -1620 1748 21 136 | 10 53 | gfz 191| 1 -1 3 -64 -31 21 -.09 10 10 | 149 -14 22 185 | 23 -30 | grg 109| -1 0 -6 -14 -1 -31 1.09 31 29 | -55 348 85 203 | -43 -59 | igr n/a| 0 0 -1 2 -25 -15 .04 5 5 | 23841 1376 19 98 | -56 -25 | jpl 130| 1 2 -11 -35 -42 56 .55 17 16 | 1416 973 18 92 | -26 20 | mit 259| 0 0 0 -33 -141 -8 -.27 10 10 | -79 331 19 134 | 17 29 | ngs 211| 0 1 1 150 198 -26 -.24 12 8 | 207 -1413 2067 3648 | -63 -145 | sio 261| 0 0 4 200 75 10 -.20 19 19 | --- --- --- --- | -122 -31 | 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 3.1538.0 GPS week: 1538 Day: 0 MJD: 55010.000 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 | 4 --- --- --- --- 35 --- --- --- --- 0 | 43 --- --- --- --- 26 --- --- --- --- 42 2 | 9 17 8 5 33 7 15 11 14 30 5 | 21 26 21 21 34 20 26 21 26 22 21 3 | 8 12 8 9 34 3 10 8 11 18 3 | 30 34 28 35 23 32 30 33 36 29 31 4 | 8 13 8 6 33 5 12 12 13 18 4 | 33 32 30 33 26 28 29 33 26 31 30 6 | 8 12 9 7 29 3 10 7 12 14 3 | 32 34 36 37 35 34 31 33 36 36 34 7 | 9 18 8 13 41 4 18 13 18 18 5 | 20 29 20 25 53 21 29 17 23 22 19 8 | 9 16 7 9 28 4 16 12 15 20 4 | 16 25 20 18 29 18 26 18 20 16 17 9 | 8 16 7 6 23 5 15 14 13 21 4 | 16 24 16 17 26 16 25 18 20 21 16 10E | 24 19 12 12 32 9 17 21 24 23 7 | 119 110 111 109 111 108 114 105 103 106 109 11 | 7 11 8 8 37 3 16 9 11 18 4 | 33 41 41 37 36 35 38 34 37 32 35 12E | 19 30 8 9 31 9 21 11 12 14 5 | 33 41 27 31 37 27 33 30 31 35 29 13 | 8 17 11 7 30 3 22 9 15 19 4 | 20 32 25 22 46 20 29 23 20 24 21 14 | 6 20 8 11 27 5 18 11 12 16 4 | 20 31 25 25 35 21 26 22 23 24 22 15 | 6 16 7 13 31 8 18 11 10 17 4 | 18 25 18 21 34 17 24 18 18 21 17 16 | 10 21 8 11 36 6 21 7 12 17 4 | 28 32 28 23 40 27 33 27 34 34 26 17 | 13 19 10 21 30 4 21 14 14 25 6 | 23 32 26 25 39 20 33 22 23 25 21 18E | 7 20 9 10 22 3 18 12 10 15 4 | 26 34 32 31 43 29 32 30 31 27 28 19 | 7 14 9 8 30 3 18 15 14 25 5 | 24 29 25 26 35 25 31 25 27 24 24 20 | 9 15 10 8 34 4 14 7 9 17 4 | 30 29 32 26 38 28 32 27 32 24 28 21 | 5 17 7 9 37 6 16 9 13 25 4 | 21 27 24 23 38 20 27 23 26 29 21 22E | 9 18 6 11 24 4 18 10 10 16 4 | 32 37 37 37 44 33 36 32 33 32 33 23 | 10 21 10 12 28 3 23 10 15 21 5 | 20 36 29 23 38 21 31 25 27 25 23 24 | 8 14 7 7 28 6 11 9 10 18 3 | 29 25 28 32 23 26 19 32 31 34 28 X25 | 14 23 22 20 --- 16 --- 14 29 --- 9 | 16 29 25 32 --- 26 --- 20 37 --- 21 26 | 6 13 8 9 16 4 13 12 10 13 3 | 15 20 17 16 25 15 23 17 20 17 15 27 | 7 19 9 9 21 5 14 9 13 16 4 | 14 26 17 17 27 14 23 15 17 19 14 28 | 10 17 15 11 29 5 19 10 11 19 5 | 26 32 31 29 44 29 33 29 33 36 28 29 | 9 17 9 10 35 7 22 9 9 29 5 | 23 31 28 25 37 25 33 24 27 30 24 30E | 11 21 9 10 38 6 18 13 22 15 5 | 44 47 38 42 52 38 46 34 48 40 40 31 | 9 20 10 9 55 5 18 11 15 16 5 | 16 30 23 23 51 22 28 17 28 18 19 32E | 14 22 7 12 43 6 20 16 20 21 6 | 104 106 104 105 97 105 106 105 107 104 104 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 9 10 32 5 17 12 14 20 |T 30 36 32 32 41 29 35 30 33 32 30 WRMS | 8 18 8 10 30 5 17 11 12 18 |NE 22 29 25 25 34 22 28 23 26 24 22 MEDI | 9 17 8 9 31 5 18 11 13 18 |MD 24 31 27 25 37 26 31 25 27 27 24 Table 3.1538.1 GPS week: 1538 Day: 1 MJD: 55011.000 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 | 19 --- --- --- --- 23 --- 22 29 --- 16 | 26 --- --- --- --- 27 --- 20 29 --- 15 2 | 6 14 5 7 29 4 16 5 9 29 4 | 13 17 14 15 28 14 21 13 16 15 12 3 | 7 10 8 11 34 5 12 15 8 18 4 | 24 21 28 31 17 23 19 26 26 21 25 4 | 7 13 5 7 29 5 10 9 10 16 3 | 24 29 29 24 29 24 26 25 22 26 24 6 | 7 12 7 8 31 5 10 8 7 13 3 | 24 24 30 31 36 26 27 24 26 27 26 7 | 8 17 8 14 42 7 20 9 10 19 4 | 15 26 17 18 44 18 27 18 19 23 15 8 | 6 16 6 10 26 4 15 8 12 18 4 | 15 24 18 14 26 18 23 18 16 20 15 9 | 8 16 6 8 27 5 15 9 13 22 4 | 16 24 21 14 26 18 25 19 23 21 17 10E | 24 21 14 12 26 11 16 18 19 23 7 | 63 70 66 66 73 69 69 75 74 71 66 11 | 8 11 6 12 24 6 13 10 10 19 4 | 21 28 29 27 36 24 29 20 24 20 23 12E | 10 27 8 8 20 5 23 12 8 15 5 | 17 32 19 21 28 19 25 21 20 25 18 13 | 7 16 8 8 37 4 23 11 12 15 4 | 19 29 22 17 41 20 29 19 21 20 18 14 | 9 21 9 8 30 6 16 10 10 16 4 | 15 30 22 18 37 17 24 17 18 21 17 15 | 7 17 8 11 34 6 16 12 13 21 4 | 17 23 21 19 30 15 24 17 22 15 16 16E | 6 20 6 12 41 4 25 7 8 13 4 | 15 25 16 17 31 14 24 16 14 21 14 17 | 11 16 7 15 30 6 23 9 13 24 5 | 18 29 22 19 40 19 31 16 19 18 17 18E | 8 22 8 11 20 6 20 9 9 16 4 | 22 35 28 25 35 26 31 24 26 27 25 19 | 6 15 9 12 40 4 22 16 9 22 5 | 17 26 27 17 37 20 32 16 15 19 18 20 | 8 19 10 8 35 6 13 10 16 16 4 | 20 27 26 17 36 22 25 19 22 22 19 21 | 6 16 7 8 38 4 18 8 10 23 4 | 18 27 22 18 38 20 29 21 21 20 19 22E | 7 13 6 7 32 5 14 7 9 16 3 | 23 31 34 27 48 28 31 26 28 27 27 23 | 9 21 9 11 31 5 24 14 11 18 5 | 21 33 26 21 36 22 33 20 21 25 21 24 | 5 13 6 6 34 3 11 7 12 20 3 | 19 22 24 25 25 22 20 24 23 24 22 X25 | 11 31 11 12 --- 14 --- 11 27 --- 7 | 16 28 26 14 --- 19 --- 18 32 --- 16 26 | 7 13 9 6 15 4 11 8 10 12 3 | 13 19 18 12 22 14 20 13 17 14 14 27 | 5 16 7 7 32 4 13 8 14 19 4 | 12 23 17 11 35 15 22 13 19 17 13 28E | 9 16 9 9 33 8 19 16 13 19 5 | 25 33 26 25 38 28 32 31 28 35 26 29 | 8 16 8 11 29 5 23 11 12 27 5 | 13 23 20 15 23 16 25 18 16 21 14 30E | 9 18 7 14 33 6 19 13 22 16 5 | 35 38 34 40 31 34 36 32 40 32 34 31 | 10 21 7 13 50 4 20 10 11 15 4 | 12 29 18 15 42 15 31 12 12 16 13 32E | 12 19 7 12 53 6 22 17 23 23 6 | 78 83 81 82 83 81 80 82 90 83 81 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 17 8 10 33 6 18 11 12 19 |T 22 30 26 23 36 24 30 23 25 25 22 WRMS | 8 17 7 10 31 5 18 10 9 19 |NE 17 25 22 18 32 19 25 18 20 20 17 MEDI | 8 16 7 10 32 5 16 10 11 18 |MD 18 27 22 18 36 20 27 19 22 21 18 Table 3.1538.2 GPS week: 1538 Day: 2 MJD: 55012.000 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 --- --- --- --- 23 --- 19 24 --- 15 | 34 --- --- --- --- 32 --- 16 27 --- 23 2 | 5 14 5 8 28 6 16 8 11 27 4 | 14 18 14 15 28 13 20 14 15 17 12 3 | 5 14 8 9 31 7 10 9 8 18 3 | 28 31 24 27 27 30 26 33 33 27 28 4 | 7 12 5 8 42 6 11 9 10 13 3 | 21 26 24 21 26 21 20 24 20 27 21 6 | 5 14 6 8 32 6 9 9 8 18 3 | 22 31 27 28 32 29 28 26 26 30 25 7 | 7 18 10 13 51 6 15 11 9 19 4 | 10 24 15 15 48 13 21 12 9 17 10 8 | 7 18 8 7 33 4 16 6 10 15 3 | 10 23 18 13 30 16 22 13 12 14 13 9 | 8 15 7 6 19 5 13 11 11 23 4 | 14 22 20 14 31 16 23 15 21 19 15 10E | 13 17 10 11 25 7 12 12 11 21 5 | 83 83 82 78 90 81 85 82 82 81 81 11 | 8 12 12 16 40 5 14 11 10 17 4 | 23 34 27 31 30 26 32 25 28 23 25 12E | 10 26 13 12 24 6 22 14 7 13 5 | 20 33 21 25 37 21 27 21 22 26 20 13 | 9 18 9 10 29 5 20 16 9 15 4 | 16 29 19 18 37 19 25 19 16 18 15 14 | 7 22 10 10 30 6 18 12 10 15 4 | 14 30 23 21 37 18 25 18 18 21 18 15 | 7 19 9 14 28 4 18 13 9 18 4 | 14 27 17 16 34 15 22 17 15 16 13 16E | 7 15 11 14 35 5 22 7 11 15 4 | 19 26 27 21 38 22 30 23 26 25 22 17 | 10 19 9 18 29 7 23 13 16 25 6 | 16 32 24 20 34 20 31 15 26 18 17 18E | 10 21 8 14 44 5 19 9 9 14 4 | 24 32 29 25 45 21 31 23 23 26 23 19 | 8 17 9 9 38 6 19 14 9 22 4 | 16 26 22 18 30 21 26 17 19 16 17 20 | 6 17 11 12 42 7 16 13 10 18 4 | 17 22 21 16 35 18 22 16 16 22 14 21 | 6 16 7 9 26 5 18 8 8 20 4 | 16 24 17 12 27 17 24 20 16 18 16 22E | 6 15 6 10 42 5 13 8 10 14 3 | 22 27 28 24 46 24 29 23 26 22 24 23 | 9 21 10 11 29 6 21 13 12 22 5 | 16 32 22 19 30 17 28 19 20 25 17 24 | 6 13 5 6 29 5 11 7 8 17 3 | 21 24 21 18 18 22 17 26 22 25 21 X25 | 13 18 11 12 --- 17 --- 16 22 --- 7 | 14 22 16 18 --- 24 --- 17 31 --- 14 26 | 5 14 7 9 21 5 11 10 10 11 3 | 13 19 16 15 27 15 22 17 17 18 14 27 | 7 15 9 8 23 4 13 11 13 19 4 | 13 22 18 12 35 14 23 13 19 16 14 28E | 11 16 7 8 33 5 20 10 8 10 4 | 21 31 26 26 38 27 32 25 26 29 25 29 | 9 15 8 8 35 6 22 9 11 24 4 | 15 25 19 20 31 18 25 19 17 21 16 30E | 11 22 9 13 55 8 19 14 22 14 5 | 27 36 26 34 28 29 32 25 35 25 27 31 | 10 20 8 9 40 9 17 9 12 14 4 | 13 31 22 18 45 19 28 14 16 19 17 32E | 11 17 11 12 55 6 20 17 19 20 5 | 82 80 76 80 93 79 81 85 82 83 79 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 17 9 11 35 6 17 11 11 18 |T 22 30 25 23 37 24 29 23 25 25 22 WRMS | 7 17 9 11 34 6 16 10 9 18 |NE 16 26 20 18 32 19 24 18 19 20 16 MEDI | 8 17 9 10 32 6 17 11 10 18 |MD 16 27 22 19 34 21 26 19 21 22 17 Table 3.1538.3 GPS week: 1538 Day: 3 MJD: 55013.000 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 | 24 --- --- --- --- 15 --- 14 21 --- 14 | 40 --- --- --- --- 30 --- 23 31 --- 30 2 | 5 13 7 6 30 5 17 7 14 27 4 | 21 25 22 23 34 22 26 22 26 22 21 3 | 8 15 5 7 34 4 12 5 13 16 3 | 27 32 31 34 25 33 26 32 40 30 30 4 | 6 11 7 4 38 5 12 7 12 13 3 | 31 33 31 30 27 29 29 31 31 29 30 6 | 7 15 6 5 33 5 11 6 13 12 3 | 40 39 44 41 40 40 37 40 43 42 41 7 | 8 17 6 15 39 6 17 10 10 13 4 | 24 30 22 25 51 25 30 20 27 23 22 8 | 5 15 6 7 31 4 15 6 7 11 3 | 23 27 22 24 34 22 26 21 21 21 21 9 | 9 16 7 7 17 6 16 10 12 21 4 | 24 27 24 21 33 23 26 20 26 23 21 10 | 11 23 9 10 37 5 14 8 14 20 5 | 62 64 58 61 80 59 65 58 58 60 59 11 | 7 12 7 10 41 7 15 7 13 15 4 | 34 37 35 35 31 35 34 33 35 32 32 12E | 9 27 11 10 32 5 23 10 10 14 5 | 29 38 30 31 30 30 33 28 31 31 28 13 | 6 17 8 8 30 5 20 15 12 11 4 | 23 32 26 24 42 24 31 25 27 26 23 14 | 8 20 6 8 22 5 16 8 10 13 4 | 25 33 28 26 39 26 30 22 27 25 24 15 | 7 20 8 15 34 5 22 11 10 17 5 | 20 26 22 21 39 19 26 21 19 21 19 16E | 8 14 7 12 47 5 23 7 10 9 4 | 26 30 26 26 36 24 30 24 29 26 25 17 | 9 18 12 17 28 5 22 9 10 26 5 | 23 33 28 24 34 21 33 21 24 24 22 18 | 9 20 9 8 28 4 17 7 8 13 4 | 62 70 69 69 62 67 67 64 66 66 65 19 | 9 17 7 8 31 4 18 10 11 19 4 | 25 32 29 27 36 25 28 22 28 22 25 20 | 8 19 8 8 41 6 15 8 10 17 4 | 25 31 27 29 38 25 29 23 24 29 24 21 | 7 14 8 5 29 5 19 8 9 20 4 | 26 27 27 26 33 26 32 27 33 28 26 22 | 12 15 5 6 51 5 13 5 5 11 3 | 48 59 56 59 76 56 56 55 52 55 54 23 | 7 20 8 11 32 5 21 10 12 19 4 | 25 34 29 25 44 25 32 25 26 30 24 24 | 5 14 9 6 28 6 11 5 11 17 3 | 27 27 30 30 24 27 23 30 32 32 28 X25 | 12 23 18 13 --- 18 --- 11 15 --- 6 | 19 28 28 20 --- 26 --- 20 20 --- 19 26 | 9 14 6 5 21 7 12 9 9 9 3 | 23 24 24 22 31 23 26 21 25 23 22 27 | 7 20 7 8 38 4 14 8 12 17 4 | 20 27 23 21 38 21 24 18 23 22 19 28E | 12 20 10 9 35 6 20 13 8 15 4 | 32 39 34 34 46 34 38 33 37 36 33 29 | 6 16 11 8 35 6 20 12 13 25 5 | 24 31 26 27 33 24 32 24 24 26 24 30E | 11 17 11 11 51 6 19 13 25 13 5 | 37 38 35 33 47 34 37 35 43 34 34 31 | 8 20 7 10 37 6 17 8 12 16 4 | 19 33 23 24 42 22 31 19 24 19 21 32E | 12 26 11 12 37 7 19 12 20 19 5 | 128 132 126 128 131 128 130 130 132 132 129 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 8 9 35 5 17 9 12 17 |T 32 37 34 34 43 33 36 31 34 34 32 WRMS | 8 18 8 9 32 5 16 8 10 17 |NE 24 30 27 26 35 25 29 24 27 26 24 MEDI | 8 17 7 8 34 5 17 8 12 16 |MD 25 32 28 26 38 26 31 24 28 28 25 Table 3.1538.4 GPS week: 1538 Day: 4 MJD: 55014.000 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 | 12 --- --- --- --- 23 --- 16 15 --- 10 | 29 --- --- --- --- 35 --- 23 30 --- 28 2 | 7 16 7 5 27 5 16 9 8 26 4 | 16 25 23 20 34 19 26 19 20 21 19 3 | 4 13 5 9 41 4 11 13 7 19 3 | 41 40 41 42 37 41 38 47 45 44 42 4 | 7 8 4 8 56 5 9 9 10 14 3 | 29 33 33 34 33 28 30 29 29 28 29 6 | 3 13 3 8 33 4 11 5 7 11 2 | 26 33 32 32 39 29 31 28 29 32 29 7 | 6 18 8 13 37 7 16 11 8 14 4 | 17 26 24 19 52 20 28 23 22 23 20 8 | 6 15 6 9 20 4 16 6 8 12 3 | 17 27 23 22 30 20 27 20 21 18 19 9 | 7 16 6 7 16 4 13 11 8 21 4 | 17 26 19 20 28 16 23 19 21 20 18 10 | 11 21 8 11 29 6 13 9 9 20 4 | 45 50 48 50 59 46 47 46 44 50 45 11 | 7 11 9 6 27 5 17 7 8 13 3 | 26 36 36 32 39 29 33 28 31 30 29 12E | 10 31 9 14 31 5 23 12 10 13 5 | 21 38 24 25 27 20 30 22 23 25 22 13 | 6 17 6 8 32 5 21 17 8 16 4 | 18 28 24 26 43 22 30 28 20 24 21 14 | 7 20 7 8 21 4 15 9 7 12 3 | 18 34 26 26 39 22 31 23 26 26 23 15 | 7 22 10 13 28 8 21 16 9 18 5 | 18 29 22 27 39 20 28 23 23 26 20 16E | 6 14 6 12 33 4 26 7 8 12 4 | 19 25 18 19 37 17 31 20 20 23 19 17 | 10 17 8 19 36 7 22 13 15 25 5 | 19 34 27 23 43 20 34 24 27 19 21 18 | 8 19 8 9 18 3 17 11 8 13 4 | 49 57 56 54 62 50 58 52 52 54 52 19 | 6 16 6 6 34 3 19 12 8 19 4 | 20 29 24 26 37 23 28 23 21 21 22 20 | 5 22 7 10 27 4 15 6 10 18 4 | 19 32 27 23 35 24 30 22 25 25 22 21 | 7 12 6 9 23 4 17 6 9 20 3 | 21 26 19 21 32 19 27 21 24 22 20 22 | 6 17 8 7 45 4 13 7 6 13 3 | 29 37 36 35 52 32 36 31 33 32 32 23 | 8 22 6 10 28 5 19 9 6 21 4 | 18 36 23 26 36 21 28 23 21 28 21 24 | 5 11 5 6 21 4 9 5 9 15 3 | 23 27 24 26 25 24 21 26 26 25 24 X25 | 8 11 9 5 --- 5 --- 6 6 23 4 | 18 24 23 20 --- 18 --- 20 21 11 19 26 | 6 13 7 8 13 4 13 11 7 9 3 | 16 23 19 19 27 16 24 20 20 17 17 27 | 6 16 6 5 17 3 14 10 10 16 3 | 16 24 20 19 30 16 23 18 20 19 17 28E | 7 14 7 9 24 7 18 11 10 12 4 | 20 27 23 22 32 20 29 26 27 27 22 29 | 5 14 8 6 33 6 21 9 10 27 4 | 17 27 21 17 30 18 31 17 19 19 18 30E | 11 19 7 8 57 6 19 13 25 13 5 | 27 30 25 30 35 28 30 26 42 26 27 31 | 7 20 8 14 40 5 19 9 12 13 4 | 17 31 22 26 42 20 30 19 20 21 19 32E | 11 19 13 13 52 6 17 13 21 19 5 | 97 101 103 99 110 102 100 99 104 95 99 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 17 7 10 33 5 17 10 10 17 |T 25 33 29 29 40 26 33 27 29 28 26 WRMS | 7 17 7 10 29 5 16 9 8 17 |NE 20 29 25 24 35 22 28 23 24 23 22 MEDI | 7 16 7 8 29 5 17 9 8 15 |MD 19 29 24 26 37 21 30 23 24 25 22 Table 3.1538.5 GPS week: 1538 Day: 5 MJD: 55015.000 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 | 16 62 25 --- --- 18 --- 13 16 --- 12 | 23 58 27 --- --- 30 --- 23 30 --- 24 2 | 8 14 9 7 25 4 18 7 12 28 4 | 12 20 13 15 28 13 23 14 19 15 13 3 | 7 12 5 10 34 7 11 7 11 15 3 | 37 34 35 37 34 38 35 41 45 38 37 4 | 8 12 6 6 40 5 12 8 10 14 3 | 21 20 19 17 25 18 21 19 20 22 18 6 | 5 12 6 9 25 4 11 6 9 12 3 | 19 23 23 22 30 22 25 19 26 25 21 7 | 7 20 8 14 28 9 14 8 6 18 4 | 17 27 19 23 44 19 24 17 21 23 18 8 | 5 12 8 7 19 5 16 7 8 9 3 | 16 22 17 18 26 16 23 15 19 15 16 9 | 7 16 8 5 26 5 14 10 13 19 4 | 13 17 14 15 26 13 20 17 19 19 14 10 | 8 19 10 10 26 5 14 9 14 19 4 | 31 38 35 35 35 31 36 34 29 36 31 11 | 8 12 11 8 25 4 14 7 6 12 3 | 24 30 30 28 34 23 29 23 26 26 24 12E | 12 29 11 9 38 5 23 13 11 11 5 | 20 32 21 24 28 19 27 23 22 27 20 13 | 6 17 8 7 30 4 17 12 7 18 4 | 15 26 22 20 37 18 25 20 18 20 17 14 | 6 21 9 6 23 5 19 7 8 12 4 | 15 29 18 16 37 15 27 14 18 17 16 15 | 8 19 12 12 23 5 21 16 10 22 5 | 13 22 15 14 29 12 21 20 16 25 13 16E | 7 14 10 11 29 5 20 6 9 10 4 | 17 21 18 15 36 13 24 17 19 17 16 17 | 10 17 13 15 31 9 23 11 17 24 5 | 12 24 19 19 35 13 28 14 18 18 13 18 | 6 21 8 10 27 2 19 11 11 14 4 | 31 35 32 33 50 30 37 31 35 31 31 19 | 7 17 7 9 35 5 17 10 11 19 4 | 15 24 18 18 38 16 25 16 21 14 16 20 | 5 29 14 11 26 5 19 5 7 18 4 | 19 31 24 22 32 17 26 19 19 23 19 21 | 8 16 9 9 28 5 18 7 9 22 4 | 18 22 18 18 27 16 25 19 24 20 18 22 | 4 15 7 5 21 4 13 8 8 12 3 | 21 26 27 25 41 23 29 21 24 22 22 23 | 6 26 11 9 25 4 20 6 9 22 4 | 15 35 21 19 30 17 26 19 21 26 17 24 | 5 12 9 7 28 4 12 8 9 14 3 | 21 23 21 26 16 20 16 25 25 22 22 25 | 6 13 7 8 --- 5 15 6 4 18 3 | 13 22 19 17 --- 16 12 15 18 14 15 26 | 7 14 8 6 18 2 12 11 9 10 3 | 11 17 12 11 23 12 19 16 15 13 11 27 | 5 14 9 5 14 4 13 9 12 14 3 | 10 15 13 12 25 10 19 14 17 14 11 28E | 7 16 9 9 26 4 23 9 10 11 4 | 24 29 22 26 40 25 31 26 32 28 25 29 | 8 16 16 8 36 5 24 12 9 29 5 | 14 23 22 16 27 16 27 16 18 17 15 30E | 9 18 8 10 55 5 20 15 27 13 5 | 25 27 22 25 30 21 25 19 40 20 23 31 | 7 19 11 8 29 3 17 7 13 14 4 | 14 27 17 18 40 14 25 11 20 14 14 32E | 10 20 11 11 40 10 14 14 16 22 5 | 147 151 147 145 156 150 150 147 147 151 147 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 18 9 9 30 5 17 9 11 17 |T 22 30 25 24 36 23 29 24 27 25 23 WRMS | 7 18 9 9 28 5 17 8 8 16 |NE 16 24 19 19 30 17 23 18 21 20 17 MEDI | 7 16 9 9 27 5 17 8 10 14 |MD 17 26 21 19 32 17 25 19 21 20 18 Table 3.1538.6 GPS week: 1538 Day: 6 MJD: 55016.000 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 34 34 --- --- 18 --- 15 17 --- 11 | 34 29 31 --- --- 39 --- 34 35 --- 35 2 | 8 16 11 8 24 6 17 8 13 28 4 | 22 24 25 22 29 22 28 22 23 24 22 3 | 9 15 8 10 26 5 10 13 11 16 4 | 33 31 34 37 32 33 31 36 33 32 32 4 | 9 10 10 6 29 6 8 11 14 16 4 | 34 34 39 35 29 33 30 35 37 38 35 6 | 7 14 8 10 22 4 10 10 12 12 3 | 33 31 33 37 33 32 32 35 35 35 34 7 | 6 19 8 20 21 9 16 9 9 28 5 | 25 33 24 22 36 27 30 28 27 40 23 8 | 5 16 12 7 20 5 14 7 13 15 4 | 22 29 26 26 25 24 27 26 24 28 24 9 | 9 16 10 7 22 6 14 12 12 20 4 | 22 24 24 20 26 21 24 25 27 24 23 10 | 10 17 14 15 19 5 14 8 9 19 4 | 56 58 51 55 59 53 57 53 55 56 53 11 | 6 13 10 7 35 4 14 6 11 13 3 | 37 38 42 37 34 35 36 35 36 35 36 12E | 10 25 11 10 33 5 21 13 7 14 5 | 29 39 27 28 31 29 34 29 31 32 29 13 | 5 15 8 9 32 5 17 11 8 22 4 | 23 33 27 28 42 25 30 26 25 31 25 14 | 6 19 10 6 26 3 13 6 11 11 3 | 21 29 27 23 38 22 27 20 24 23 22 15 | 8 18 11 20 23 8 20 17 12 23 6 | 21 26 21 25 35 19 27 26 25 31 22 16E | 7 16 8 9 46 5 23 9 8 12 4 | 25 32 26 25 40 27 36 27 26 31 26 17 | 7 21 14 9 41 7 22 10 12 23 5 | 25 30 28 30 39 24 33 25 29 30 26 18 | 8 17 9 11 21 4 17 11 8 17 4 | 37 43 46 42 50 42 43 42 43 43 41 19 | 7 17 7 10 26 3 18 9 8 19 4 | 25 29 28 27 35 25 33 25 24 21 25 20 | 4 19 8 11 26 4 15 6 10 17 4 | 23 30 26 26 38 25 30 25 28 31 25 21 | 7 13 6 6 24 5 19 7 9 25 4 | 32 30 30 28 39 30 36 33 34 35 32 22 | 8 14 7 8 33 5 12 7 5 16 3 | 35 39 41 38 49 37 38 35 40 33 37 23 | 6 22 12 11 30 5 18 8 8 24 4 | 23 35 26 26 34 25 31 28 28 34 24 24 | 6 13 11 5 30 5 13 9 10 16 3 | 32 30 30 33 26 30 25 35 35 34 32 25 | 6 14 11 7 --- 4 14 6 6 19 3 | 23 28 23 26 --- 25 12 27 24 13 23 26 | 8 14 9 6 21 3 12 11 9 12 3 | 20 21 23 20 32 19 25 24 25 23 21 27 | 5 16 10 6 21 5 12 11 14 15 4 | 20 21 24 19 27 19 23 22 25 22 21 28E | 10 18 10 11 34 4 26 10 12 18 5 | 43 44 44 48 45 44 49 46 48 55 46 29 | 8 18 10 9 41 6 21 10 10 32 5 | 26 30 24 24 38 24 31 26 26 24 25 30E | 10 19 11 9 49 6 21 13 30 13 6 | 30 31 27 29 31 29 30 24 45 25 28 31 | 6 17 11 10 41 5 14 6 15 14 4 | 21 31 23 23 46 22 31 19 23 20 22 32E | 9 27 13 15 39 10 18 20 17 26 6 | 142 138 139 138 139 136 144 144 138 142 141 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 17 10 10 31 5 17 10 12 19 |T 32 35 33 33 39 32 35 33 34 34 32 WRMS | 7 17 10 10 29 5 16 10 8 19 |NE 25 29 27 27 33 25 28 27 28 28 26 MEDI | 7 17 10 9 26 5 15 10 11 17 |MD 25 31 27 27 35 27 31 27 28 31 26 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 4.1538 GPS week: 1538 MJD: 55010.0-55016.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2957 |U 9 9 27 |U 7 11 25 |U 8 8 20 | emr | emr 2897 | 10 9 32 | 14 18 76 |U 9 10 21 | esa | esa 2907 | 9 9 30 |U 6 11 23 | 8 7 18 | gfz | gfz 2855 |U 8 8 24 |U 9 24 56 | 8 8 19 | grg | grg 2784 | 10 9 27 |U 10 18 36 | 8 10 22 | igr | igr 2879 | 10 10 29 | 6 11 26 | 8 8 18 | igs | igs 2871 | 9 9 24 | 7 9 30 | 8 8 18 | jpl | jpl 2802 | 11 9 35 |U 7 14 38 |U 7 8 19 | mit | mit 2962 |U 9 9 31 |U 10 41 83 |U 9 10 20 | Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit positions and satellite clock corrections at 15 min intervals. Each line gives the daily station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. CLK - Satellite clocks used. EPO - Number of satellite clock epochs available for that day. Units: mm. Table 5.1538.0 GPS week: 1538 Day: 0 MJD: 55010.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2969 | 10 12 22 | 6 15 28 | 11 14 26 | emr | emr 2868 | 11 9 27 | 16 22 98 | 9 10 19 | esa | esa 2880 | 11 11 24 | 5 10 28 | 8 8 19 | gfz | gfz 2857 | 10 9 21 | 10 17 77 | 8 8 22 | grg | grg 2784 | 10 7 25 | 10 13 35 | 7 9 21 | igr | igr 2877 | 11 11 25 | 5 10 28 | 8 10 18 | igs | igs 2834 | 10 10 22 | 5 8 32 | 10 12 24 | jpl | jpl 2772 | 12 9 23 | 6 10 32 | 8 8 19 | mit | mit 2880 | 10 8 21 | 15 19 92 | 9 9 21 | Table 5.1538.1 GPS week: 1538 Day: 1 MJD: 55011.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2975 | 10 7 39 | 7 10 31 | 9 7 17 | emr | emr 2868 | 11 8 52 | 13 24 73 | 8 6 16 | esa | esa 2880 | 11 9 40 | 5 9 24 | 7 5 16 | gfz | gfz 2849 | 10 8 37 | 15 19 102 | 8 5 16 | grg | grg 2784 | 10 7 36 | 8 24 36 | 9 9 17 | igr | igr 2878 | 11 9 42 | 5 8 29 | 8 5 16 | igs | igs 2878 | 9 8 34 | 9 10 63 | 8 5 15 | jpl | jpl 2772 | 16 11 75 | 6 11 33 | 8 6 15 | mit | mit 2976 | 11 11 55 | 12 13 80 | 8 5 17 | Table 5.1538.2 GPS week: 1538 Day: 2 MJD: 55012.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2917 | 9 13 27 | 8 10 27 | 7 7 15 | emr | emr 2872 | 13 12 36 | 18 23 87 | 8 10 19 | esa | esa 2880 | 10 12 30 | 6 12 24 | 7 6 15 | gfz | gfz 2848 | 9 11 23 | 12 85 115 | 8 8 17 | grg | grg 2784 | 10 11 28 | 10 22 32 | 8 10 12 | igr | igr 2876 | 10 13 29 | 10 22 32 | 7 7 17 | igs | igs 2834 | 10 13 26 | 8 11 26 | 7 8 14 | jpl | jpl 2772 | 12 13 31 | 6 25 39 | 8 8 18 | mit | mit 2976 | 9 13 37 | 11 212 293 | 9 11 16 | Table 5.1538.3 GPS week: 1538 Day: 3 MJD: 55013.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2949 | 10 10 39 | 8 13 21 | 7 6 15 | emr | emr 2872 | 12 9 28 | 13 12 82 | 8 8 18 | esa | esa 2880 | 12 11 47 | 6 14 21 | 6 4 17 | gfz | gfz 2852 | 8 8 24 | 7 15 24 | 6 5 16 | grg | grg 2784 | 10 10 32 | 9 12 36 | 6 6 21 | igr | igr 2867 | 11 11 44 | 6 15 23 | 6 7 16 | igs | igs 2912 | 8 9 24 | 7 12 21 | 6 5 14 | jpl | jpl 2775 | 10 9 26 | 7 10 26 | 6 6 16 | mit | mit 2976 | 13 14 40 | 8 12 26 | 13 14 23 | Table 5.1538.4 GPS week: 1538 Day: 4 MJD: 55014.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2973 | 7 6 20 | 8 12 17 | 7 8 18 | emr | emr 2872 | 9 8 24 | 15 20 83 | 9 10 23 | esa | esa 2880 | 7 5 25 | 8 11 17 | 6 7 16 | gfz | gfz 2861 | 7 6 20 | 9 14 22 | 7 7 20 | grg | grg 2784 | 10 7 20 | 10 16 39 | 8 9 27 | igr | igr 2880 | 7 6 22 | 8 11 17 | 6 7 17 | igs | igs 2871 | 7 6 22 | 7 10 20 | 6 7 16 | jpl | jpl 2776 | 8 6 25 | 13 25 62 | 8 8 20 | mit | mit 2976 | 8 6 26 | 9 12 36 | 7 9 22 | Table 5.1538.5 GPS week: 1538 Day: 5 MJD: 55015.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2944 | 9 9 23 | 6 8 29 | 8 6 20 | emr | emr 2960 | 10 11 28 | 15 15 78 | 10 8 21 | esa | esa 2976 | 9 10 24 | 5 6 25 | 10 8 20 | gfz | gfz 2861 | 9 9 23 | 5 8 26 | 9 8 21 | grg | grg 2784 | 10 12 26 | 8 12 44 | 10 10 19 | igr | igr 2872 | 9 11 22 | 5 5 30 | 9 7 19 | igs | igs 2863 | 8 9 21 | 6 6 26 | 9 7 19 | jpl | jpl 2874 | 11 10 47 | 8 13 42 | 8 7 16 | mit | mit 2976 | 9 9 21 | 6 6 24 | 10 7 19 | Table 5.1538.6 GPS week: 1538 Day: 6 MJD: 55016.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2974 | 7 7 17 | 5 10 25 | 8 10 28 | emr | emr 2970 | 9 8 31 | 8 13 29 | 8 14 31 | esa | esa 2976 | 6 6 19 | 5 13 25 | 8 11 26 | gfz | gfz 2861 | 6 6 19 | 7 12 30 | 8 12 25 | grg | grg 2784 | 9 7 24 | 12 27 32 | 10 17 36 | igr | igr 2905 | 7 6 16 | 5 5 24 | 8 13 26 | igs | igs 2911 | 6 6 17 | 5 7 26 | 7 12 25 | jpl | jpl 2876 | 8 8 20 | 5 8 33 | 7 12 29 | mit | mit 2976 | 6 6 16 | 5 13 31 | 7 11 22 | 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 6.1538 GPS week: 1538 MJD: 55010.500-55016.500 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 | 11 -26 10 -10 -3 | -1 26 | 21 31 81 97 4 | 5 emr uuuuu | 48 -24 92 189 -8 | 12 37 | 28 22 93 118 5 | 9 esa uuuuu | -30 -21 -30 -25 12 | -8 27 | 34 24 155 70 14 | 9 gfz uuuuu | 0 -33 -4 -22 1 | 6 27 | 19 14 69 74 8 | 5 grg xxxxx | -3 7 -3 30 -7 | 4 25 | 24 42 131 64 33 | 3 igr xxxxx | 22 37 -45 -8 7 | 2 24 | 18 23 79 66 4 | 7 irf xxxxx | -3 -3 -26 -35 -1 | -3 25 | 9 7 31 22 6 | 5 jpl uuuuu | -18 -17 68 5 2 | 0 29 | 26 24 122 89 7 | 5 mit uuuuu | -31 -14 -76 -212 -10 | 2 29 | 14 14 59 60 9 | 5 ngs uuuuu | 36 52 -41 232 -1 | 2 23 | 51 37 109 113 3 | 4 sio uuuxu | 48 123 127 -362 -5 | 6 30 | 22 18 103 103 8 | 5 Table 7.1538.0 GPS week: 1538 Day: 0 MJD: 55010.500 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 -40 92 51 6 | -4 28 emr uuuuu | 85 11 34 237 0 | 0 46 esa uuuuu | -15 -65 97 -127 25 | -18 31 gfz uuuuu | -18 -27 50 -7 2 | 2 26 grg xxxxx | -26 24 116 -15 45 | -2 30 igr xxxxx | 2 44 -109 -113 12 | -7 27 irf xxxxx | 7 -2 -36 -41 -6 | -7 29 jpl uuuuu | 25 -26 33 100 -10 | -6 33 mit uuuuu | -23 -6 -100 -312 -18 | -1 35 ngs uuuuu | -39 106 -185 442 1 | -2 24 sio uuuxu | 86 130 45 -503 -8 | 2 34 Table 7.1538.1 GPS week: 1538 Day: 1 MJD: 55011.500 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 | -16 15 50 71 -1 | -5 28 emr uuuuu | 46 -18 -62 257 -10 | 4 44 esa uuuuu | -6 -10 76 -95 9 | -18 31 gfz uuuuu | -33 -16 11 -44 14 | 0 26 grg xxxxx | -33 49 -127 87 -33 | 3 32 igr xxxxx | 24 -11 41 -27 5 | -5 26 irf xxxxx | -4 -9 9 -32 -10 | -7 29 jpl uuuuu | -14 -30 -102 60 0 | -5 32 mit uuuuu | -33 -26 -12 -196 -21 | -1 35 ngs uuuuu | 55 53 -105 288 4 | -3 24 sio uuuxu | 43 99 161 -423 -18 | 2 34 Table 7.1538.2 GPS week: 1538 Day: 2 MJD: 55012.500 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 | 26 -62 -93 62 -4 | -2 29 emr uuuuu | -3 -46 201 82 -1 | 10 42 esa uuuuu | -2 -20 128 -26 13 | -16 31 gfz uuuuu | 6 -56 -23 94 7 | 4 29 grg xxxxx | 9 -40 23 136 -37 | 1 32 igr xxxxx | 54 39 80 102 7 | -1 27 irf xxxxx | -7 8 -86 -21 -3 | -5 29 jpl uuuuu | -8 -41 104 9 5 | -1 32 mit uuuuu | -46 11 -188 -255 -14 | 2 34 ngs uuuuu | 32 56 -86 164 -5 | 1 25 sio uuuxu | 48 140 -57 -412 -7 | 5 34 Table 7.1538.3 GPS week: 1538 Day: 3 MJD: 55013.500 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 | 5 19 -84 25 -5 | 5 25 emr uuuuu | 40 -55 197 24 -12 | 21 36 esa uuuuu | 0 -27 33 -11 28 | -8 27 gfz uuuuu | 2 -17 -141 -38 -5 | 11 28 grg xxxxx | -13 51 -222 60 -16 | 7 23 igr xxxxx | 28 66 -92 29 2 | 8 23 irf xxxxx | -2 -8 -34 -6 -1 | 3 24 jpl uuuuu | -9 22 -43 2 -1 | 7 29 mit uuuuu | -37 -24 -55 -143 -13 | 9 29 ngs uuuuu | 8 52 14 282 -1 | 7 23 sio uuuxu | 45 114 212 -208 -4 | 12 31 Table 7.1538.4 GPS week: 1538 Day: 4 MJD: 55014.500 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 | 42 -44 -44 13 -2 | 5 25 emr uuuuu | 40 -24 59 102 -10 | 22 36 esa uuuuu | -36 15 -78 89 15 | -2 25 gfz uuuuu | 13 -37 -12 9 -1 | 12 28 grg xxxxx | -8 -50 89 -24 21 | 3 22 igr xxxxx | 29 36 -63 7 11 | 10 23 irf xxxxx | 5 5 -17 -46 0 | 4 24 jpl uuuuu | -19 -28 181 -138 4 | 6 29 mit uuuuu | -11 -7 -86 -226 -7 | 9 29 ngs uuuuu | 15 -18 41 121 -4 | 8 23 sio uuuxu | 58 149 106 -345 -4 | 13 31 Table 7.1538.5 GPS week: 1538 Day: 5 MJD: 55015.500 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 | 6 -30 83 -125 -7 | 1 25 emr uuuuu | 69 -29 100 289 -14 | 16 33 esa uuuuu | -80 -17 -186 0 4 | 1 22 gfz uuuuu | 21 -40 75 -154 -2 | 8 28 grg xxxxx | 10 -13 125 -21 10 | 7 18 igr xxxxx | 11 38 -40 -11 8 | 8 23 irf xxxxx | 1 -4 -18 -22 6 | 0 24 jpl uuuuu | -57 -27 247 86 6 | 2 28 mit uuuuu | -19 -18 -67 -143 0 | 3 28 ngs uuuuu | 55 64 -102 166 -1 | 4 23 sio uuuxu | 46 118 227 -251 1 | 8 29 Table 7.1538.6 GPS week: 1538 Day: 6 MJD: 55016.500 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 -38 67 -170 -7 | -6 20 emr uuuuu | 57 -7 112 330 -8 | 7 20 esa uuuuu | -74 -22 -278 -7 -13 | 1 22 gfz uuuuu | 9 -35 10 -14 -9 | 3 23 grg xxxxx | 38 31 -24 -15 -39 | 6 18 igr xxxxx | 4 44 -135 -44 4 | 4 18 irf xxxxx | -21 -12 -3 -75 6 | -6 17 jpl uuuuu | -41 14 56 -85 13 | -5 19 mit uuuuu | -50 -29 -21 -211 2 | -4 16 ngs uuuuu | 124 51 134 162 0 | 0 19 sio uuuxu | 10 110 194 -393 6 | 0 17