Date: Thu, 18 Dec 2008 12:40:46 +0000 From: Jim Ray Subject: [IGSREPORT-16935] Wk 1508 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <494a44ce.zht06Dxc6Hh3wX37%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 18 Dec 04:40:49 PST 2008 Message Number 16935 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1508 (Nov 30, 2008 - Dec 06, 2008) 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: igs1508[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1508[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1508[0-6].cls IGS GPS clock combination summary report. igs15087.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15087.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Day | Centre | PRN/STA list ----+--------+--------------- 0 | COD | PDEL RCMN 0 | EMR | DAEJ MATE MIZU 0 | ESA | 27 AREQ 0 | GFZ | 7 29 31 DAEJ DARW GUAT HARB ISPA 0 | MIT | PDEL 1 | COD | 9 RCMN WROC 1 | ESA | 8 9 27 1 | GFZ | 7 8 9 31 ADE1 HOB2 IRKT MCM4 1 | MIT | DARW KHAJ 2 | COD | 9 2 | EMR | DAEJ SCH2 2 | ESA | 9 27 2 | GFZ | 7 9 13 IRKT PIE1 2 | JPL | MCM4 SCH2 2 | MIT | DARW HARB SCH2 3 | COD | MAS1 WROC WTZR 3 | EMR | MIZU 3 | ESA | WTZR 3 | GFZ | 7 TOW2 3 | MIT | 12 20 BOR1 HARB TOW2 4 | GFZ | 7 FAA1 GOLD 4 | JPL | 9 4 | MIT | 32 5 | EMR | MATE WHIT 5 | GFZ | 7 5 | JPL | 8 5 | MIT | 5 14 32 KHAJ 6 | EMR | FAIR YELL 6 | ESA | CHUR 6 | GFZ | 7 6 | JPL | 9 ZWE2 6 | MIT | 26 BOR1 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 | .3 .0 .7 -26 -21 -10 .04 EMR | 6.8 2.6 -.8 123 27 17 -.03 ESA | 5.4 5.3 .2 44 -89 24 -.02 GFZ | 1.0 .6 1.6 12 -35 8 -.22 GRG | 5.0 2.0 -.4 -9 -25 12 -.09 JPL | -.7 1.7 10.6 17 -14 14 .20 MIT | 4.3 -1.3 -3.0 7 -5 -4 -.17 NGS | 5.5 -10.0 -3.6 -130 -115 88 .04 SIO | 2.3 -.5 .6 -8 -38 -11 -.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 1.1508.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1508.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 2.1508.[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 3.1508.[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 5.1508.0-6). 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 1508 summary. (Nov 30, 2008 - Dec 06, 2008) Table 1.1508.a GPS week: 1508 MJD: 54800.000-54806.000 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 243| 0 0 1 42 -16 -44 -.16 11 10 | -524 370 30 155 | 0 1 1 6 10 27 .01 | 579 857 emr 73| -1 0 5 -253 -134 -26 .48 19 19 | 875 599 23 243 | 1 1 1 23 23 23 .02 | 2355 1066 esa 135| 1 -1 -1 -75 13 -6 .33 10 10 | -799 -296 27 111 | 0 0 1 18 21 20 .03 | 859 772 gfz 198| 1 0 -3 -35 11 125 -.13 9 9 | 6 12 29 135 | 0 0 1 14 11 55 .05 | 304 632 grg 82| 2 3 11 47 -19 -20 1.14 46 43 | -527 351 112 382 | 2 1 3 25 26 60 .05 | 577 858 igr n/a| 0 -1 1 -3 -57 -49 .10 7 7 | -4060 2191 30 76 | 0 0 1 11 7 21 .03 | 5757 1048 jpl 135| -2 0 3 -32 -22 -12 .54 19 17 | 2103 629 29 121 | 1 1 1 6 25 29 .03 | 2094 996 mit 272| 0 0 -1 -29 -78 -19 -.31 13 11 | -188 -71 28 182 | 0 0 1 29 32 12 .02 | 304 672 ngs 236| 0 -1 1 259 141 -52 -.23 12 9 | -498 298 2258 3916 | 0 0 1 26 35 18 .04 | 578 857 sio 109| -1 2 0 7 8 -28 -.18 24 22 | --- --- --- --- | 1 0 1 13 22 17 .03 | --- --- Table 1.1508.b GPS week : 1508 MJD: 54800.000-54806.000 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 0 0 --- 0 0 0 | 2 | 5 6 6 5 6 6 6 | 3 | 7 7 7 7 8 7 7 | 4 | 4 4 4 4 5 4 4 | 5 | 4 4 4 4 4 4 5 | 6 | 4 4 4 4 4 4 4 | 7 | 5 4 4 4 5 4 5 | 8 | 6 6 8 7 7 6 7 | 9 | 6 6 6 6 7 7 7 | 10 | 5 5 5 5 5 5 5 | 11 | 5 5 5 5 5 5 4 | 12 | 5 6 6 6 6 6 6 | 13 | 5 5 5 5 5 5 5 | 14 | 6 6 5 5 5 5 6 | 15 | 5 5 5 6 6 5 6 | 16 | 7 6 6 6 6 6 7 | 17 | 5 5 4 4 5 5 5 | 18 | 5 5 6 6 6 6 6 | 19 | 5 4 4 4 4 4 4 | 20 | 7 5 5 5 5 5 5 | 21 | 4 4 4 5 6 5 5 | 22 | 5 5 4 6 5 4 5 | 23 | 6 6 6 6 6 6 6 | 24 | 5 5 5 4 4 5 4 | 25 | 8 7 8 7 6 6 6 | 26 | 4 4 4 4 8 4 5 | 27 | 5 5 6 5 6 6 6 | 28 | 6 6 6 6 6 6 6 | 29 | 5 4 4 5 4 4 5 | 30 | 4 4 4 4 4 4 5 | 31 | 5 5 5 5 5 5 5 | 32 | 5 5 5 5 5 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 2.1508.0 GPS week: 1508 Day: 0 MJD: 54800.000 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 243| 0 0 1 36 -17 -51 -.15 12 11 | 365 -1154 33 155 | -11 -24 | emr 73| 0 -3 3 -222 -114 0 .50 19 19 | -1256 -658 23 268 | 22 -14 | esa 135| 2 0 0 -67 27 -4 .34 11 11 | 84 -809 28 112 | -10 -5 | gfz 198| 1 0 -5 -32 9 122 -.06 11 11 | 208 -543 26 117 | -15 -16 | grg 82| 3 5 16 57 -2 -78 1.19 48 44 | 357 -1175 116 440 | 27 2 | igr n/a| 0 -1 0 21 -57 -19 .12 8 7 | -11167 846 33 80 | -57 -24 | jpl 135| -2 0 2 -21 -25 2 .59 20 19 | 24 -770 26 129 | -5 -68 | mit 272| 0 1 0 -43 -65 -21 -.30 12 9 | 101 -688 20 157 | 12 17 | ngs 236| 0 -1 1 258 141 -46 -.23 12 9 | 365 -1194 2299 3841 | -1 20 | sio 109| -3 3 1 -8 17 -31 -.20 24 21 | --- --- --- --- | 14 -42 | Table 2.1508.1 GPS week: 1508 Day: 1 MJD: 54801.000 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 243| 0 0 -1 37 -32 -24 -.16 10 9 | -720 640 26 137 | 9 -25 | emr 73| -1 0 3 -235 -118 -30 .51 18 18 | -1561 224 22 245 | 5 9 | esa 135| 1 -2 0 -66 27 -14 .32 10 10 | -515 -1619 23 109 | 5 7 | gfz 198| 1 0 -1 -38 20 143 -.17 10 10 | -99 21 27 149 | -15 -34 | grg 82| 3 3 17 -2 -47 -8 1.17 46 42 | -714 602 108 344 | 51 -30 | igr n/a| 0 0 1 -2 -59 -43 .10 7 6 | -9924 2043 29 72 | -14 -9 | jpl 135| -2 0 3 -35 -67 -32 .55 18 17 | -306 515 27 119 | -30 -4 | mit 272| -1 1 -1 -6 -79 -37 -.28 13 11 | -61 -438 22 162 | -14 6 | ngs 236| 0 0 0 242 178 -48 -.22 13 9 | -705 593 2318 3741 | 12 -18 | sio 109| -1 2 0 -14 -18 -52 -.23 23 23 | --- --- --- --- | 22 -22 | Table 2.1508.2 GPS week: 1508 Day: 2 MJD: 54802.000 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 243| 0 0 0 48 -6 -85 -.16 10 9 | -557 525 26 129 | -4 -47 | emr 73| 0 0 4 -260 -117 -61 .48 18 18 | -1218 796 24 251 | 59 -9 | esa 135| 1 -2 0 -65 43 -39 .36 11 10 | 360 -366 26 106 | 11 12 | gfz 198| 0 0 -5 -48 -9 234 -.17 10 10 | 388 -721 27 137 | -14 -24 | grg 82| 0 4 11 81 -11 -80 1.10 44 40 | -562 501 106 406 | 25 -46 | igr n/a| 0 -1 0 -9 -67 -74 .13 7 6 | -7372 2389 28 77 | -2 11 | jpl 135| -1 0 5 -33 -43 -28 .53 18 16 | 535 966 30 120 | 25 -44 | mit 272| 0 0 0 -22 -99 -28 -.29 11 10 | 83 -892 25 170 | 9 -3 | ngs 236| 0 -1 0 243 181 -49 -.17 12 9 | -478 346 2068 3639 | 24 5 | sio 109| 0 2 0 8 -7 -39 -.19 23 21 | --- --- --- --- | -18 -19 | Table 2.1508.3 GPS week: 1508 Day: 3 MJD: 54803.000 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 243| 0 0 2 39 -9 -57 -.14 13 12 | -1586 1742 31 164 | 16 -50 | emr 73| -1 1 6 -267 -121 -20 .50 18 18 | 362 2612 24 235 | 50 -6 | esa 135| 0 -2 0 -69 15 -20 .37 9 9 | -833 190 30 122 | 1 8 | gfz 198| 1 0 -4 -5 10 128 -.20 8 8 | -491 911 31 155 | -27 -40 | grg 82| 3 6 8 46 -21 45 1.07 48 42 | -1590 1729 120 388 | 36 26 | igr n/a| 1 0 0 -11 -55 -51 .14 8 7 | -4370 4122 33 80 | -24 12 | jpl 135| -2 1 2 -35 -11 0 .58 19 17 | 1969 2436 31 123 | -9 -82 | mit 272| 0 1 0 -26 -107 -11 -.31 12 11 | -770 963 24 163 | -7 4 | ngs 236| 0 0 1 239 145 -61 -.24 12 9 | -1574 1705 2519 4409 | 62 50 | sio 109| -1 2 -1 10 0 -38 -.13 24 22 | --- --- --- --- | -3 -18 | Table 2.1508.4 GPS week: 1508 Day: 4 MJD: 54804.000 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 243| 0 2 3 53 -17 0 -.14 12 11 | -361 182 35 168 | 3 6 | emr 73| -3 0 6 -272 -175 -38 .48 20 20 | 2478 1179 26 230 | 67 65 | esa 135| 0 -1 -3 -114 -9 3 .34 10 10 | -1581 63 25 100 | 40 23 | gfz 198| 1 -1 -1 -46 21 107 -.13 8 8 | 227 -370 29 129 | 9 5 | grg 82| 6 3 8 45 -30 68 1.19 45 42 | -350 160 109 384 | 27 56 | igr n/a| 0 -1 0 -7 -50 -61 .07 7 7 | -946 2699 27 65 | -26 -13 | jpl 135| -3 0 3 -24 -14 -15 .52 19 18 | 3443 978 27 115 | -40 -164 | mit 272| 0 0 -2 15 -12 -16 -.33 16 13 | -162 -228 40 263 | -28 -44 | ngs 236| 0 -1 0 240 75 -87 -.21 11 9 | -285 92 2427 3862 | 4 114 | sio 109| 0 2 0 13 45 -2 -.18 25 26 | --- --- --- --- | 7 -16 | Table 2.1508.5 GPS week: 1508 Day: 5 MJD: 54805.000 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 243| 0 2 1 44 -5 -62 -.16 11 10 | -396 145 33 181 | -15 -64 | emr 73| -1 0 6 -283 -159 -41 .45 18 18 | 3472 106 25 222 | 56 42 | esa 135| 0 0 -3 -61 8 19 .30 9 9 | -1073 -333 30 112 | -8 21 | gfz 198| 1 0 -2 -38 7 77 -.09 9 9 | -238 786 33 128 | -36 -33 | grg 82| 0 2 9 46 26 -15 1.13 45 48 | -404 131 108 397 | -32 2 | igr n/a| 0 0 0 -12 -44 -71 .07 7 7 | 1566 1830 33 73 | -27 -8 | jpl 135| -1 2 3 -41 7 40 .50 19 19 | 4262 238 33 128 | 31 -83 | mit 272| 0 0 -1 -41 -104 -24 -.33 14 12 | -389 370 35 174 | 19 -3 | ngs 236| 0 -2 1 289 137 -39 -.24 13 9 | -386 81 2176 3965 | -28 17 | sio 109| 0 1 0 23 27 -21 -.19 24 22 | --- --- --- --- | -18 -38 | Table 2.1508.6 GPS week: 1508 Day: 6 MJD: 54806.000 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 243| 0 0 1 38 -27 -32 -.18 12 11 | -413 514 28 153 | -9 -35 | emr 73| -4 1 7 -231 -138 2 .46 19 19 | 3849 -60 23 256 | -12 16 | esa 135| 2 0 -4 -84 -16 13 .29 10 9 | -2039 799 28 119 | 21 7 | gfz 198| 0 0 -1 -39 20 66 -.12 9 9 | 53 3 31 131 | -37 -43 | grg 82| 2 1 11 56 -49 -73 1.16 49 47 | -426 510 117 320 | -15 8 | igr n/a| 0 0 3 -4 -65 -24 .11 7 7 | 3789 1412 31 85 | -29 -9 | jpl 135| 0 2 4 -33 -2 -50 .53 18 16 | 4796 46 31 115 | 27 -34 | mit 272| 1 0 -5 -77 -79 1 -.33 16 14 | -123 413 33 185 | 33 -17 | ngs 236| 0 0 4 306 132 -31 -.30 12 9 | -427 465 2002 3960 | -40 32 | sio 109| -1 2 -3 17 -4 -10 -.18 25 22 | --- --- --- --- | -40 -9 | 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 3.1508.0 GPS week: 1508 Day: 0 MJD: 54800.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 4 --- --- --- --- 44 --- --- --- --- 0 | 19 --- --- --- --- 9999 --- --- --- --- 22 2 | 11 20 10 12 38 8 23 9 11 24 5 | 23 36 26 14 41 26 38 26 24 24 22 3 | 9 12 10 6 58 8 16 9 12 69 7 | 24 28 26 22 36 26 30 23 27 67 23 4 | 11 15 10 7 29 6 10 7 8 28 4 | 12 20 19 18 27 16 16 16 17 22 13 5 | 12 10 8 7 24 4 9 7 9 22 3 | 20 21 17 14 26 15 20 15 16 27 14 6 | 8 13 9 6 73 6 17 6 12 19 4 | 25 28 29 25 49 29 31 25 31 25 27 7E | 10 23 10 13 45 7 20 9 11 12 5 | 14 27 18 16 41 16 25 14 15 17 13 8E | 15 15 16 13 75 7 20 12 24 18 6 | 24 30 29 21 48 25 29 22 29 25 21 9E | 15 21 11 12 69 7 18 13 18 18 5 | 31 31 27 23 46 24 30 24 32 28 23 10 | 14 17 8 8 42 7 12 15 11 17 4 | 28 40 31 31 45 30 36 33 32 30 30 11 | 8 20 10 8 47 8 20 7 9 26 4 | 20 39 27 25 60 26 38 22 23 22 23 12 | 14 19 14 9 34 10 22 12 10 20 5 | 25 32 26 21 47 24 34 21 21 19 20 13 | 10 25 9 10 47 9 24 8 12 15 5 | 15 35 18 17 49 21 31 16 18 13 16 14 | 11 23 11 10 48 9 25 11 11 23 5 | 18 29 24 25 35 20 28 19 21 25 19 15 | 8 24 12 11 28 9 20 7 11 24 5 | 14 29 20 16 39 17 29 16 15 21 15 16 | 13 29 13 7 49 9 29 25 14 24 7 | 21 37 22 18 57 24 35 27 23 25 19 17 | 10 14 9 13 78 10 15 4 9 26 4 | 33 39 35 39 74 36 38 35 34 32 34 18 | 8 22 14 11 69 9 23 10 9 20 5 | 27 37 36 33 52 30 35 30 34 29 31 19 | 12 13 9 11 49 11 22 9 13 24 5 | 30 33 34 32 42 32 36 28 30 31 30 20 | 23 27 9 12 36 6 21 17 9 15 6 | 79 82 76 82 85 76 84 79 83 81 80 21 | 9 15 9 9 36 8 16 10 6 13 4 | 20 29 21 23 48 23 29 20 26 20 21 22 | 9 20 13 9 40 8 21 8 16 20 5 | 16 20 22 18 43 14 19 19 20 21 15 23 | 9 29 8 14 30 9 30 9 8 17 5 | 15 39 21 20 40 21 34 15 18 19 16 24 | 9 18 7 11 41 5 15 10 10 23 4 | 13 29 19 18 31 18 30 17 25 32 19 25E | 20 21 15 16 37 6 20 27 19 19 7 | 26 33 30 28 39 29 37 44 34 32 29 26 | 8 12 8 10 22 6 10 7 8 20 3 | 16 28 24 19 31 19 25 17 19 24 18 27E | 16 17 9 10 73 7 19 8 18 19 5 | 28 33 29 28 40 29 29 26 34 29 26 28 | 7 26 12 12 49 12 25 14 14 31 6 | 22 33 22 25 39 22 32 32 23 31 20 29 | 11 11 7 9 31 4 13 7 11 29 4 | 38 43 42 39 40 40 42 37 40 38 38 30 | 12 9 8 7 26 4 8 8 11 17 3 | 26 25 24 20 24 21 22 18 19 25 20 31E | 8 19 15 16 49 6 23 8 9 14 5 | 23 30 24 25 44 23 30 19 23 22 22 32 | 12 21 13 5 49 6 23 13 11 20 5 | 17 27 27 23 32 23 36 25 27 26 21 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 19 11 11 48 8 20 12 12 24 |T 23 32 27 25 43 25 32 25 26 28 23 WRMS | 11 19 11 11 44 7 19 9 9 21 |NE 21 31 24 22 41 23 31 22 23 27 21 MEDI | 10 19 10 10 45 7 20 9 11 20 |MD 22 31 26 23 41 24 31 22 24 25 21 Table 3.1508.1 GPS week: 1508 Day: 1 MJD: 54801.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 4 --- --- --- --- 37 --- --- --- --- 0 | 26 --- --- --- --- 9999 --- --- --- --- 30 2 | 10 21 13 13 39 10 22 12 11 24 5 | 15 28 17 12 32 18 27 20 22 23 16 3 | 8 10 7 5 41 7 13 9 12 66 6 | 13 20 19 15 32 16 20 14 23 59 16 4 | 10 14 12 8 34 5 10 9 9 21 4 | 11 19 16 15 27 13 14 17 19 23 14 5 | 8 10 9 10 32 4 9 10 12 23 4 | 10 21 18 16 28 16 20 16 16 25 15 6 | 6 10 10 10 41 6 12 10 12 21 4 | 17 18 18 15 27 17 18 17 24 16 16 7E | 10 20 8 10 32 6 16 9 5 13 4 | 13 25 19 18 31 15 25 13 17 18 15 8E | 15 17 16 9 57 6 16 13 24 20 6 | 24 29 23 28 34 25 30 26 33 28 23 9E | 12 19 8 13 69 8 19 13 19 16 5 | 17 24 17 20 33 18 22 14 33 18 16 10 | 11 15 11 8 38 8 12 18 9 15 4 | 25 36 31 30 38 28 35 27 28 30 28 11 | 6 18 10 12 67 6 20 10 10 21 4 | 15 33 21 20 59 20 34 16 16 17 17 12 | 10 20 15 9 48 9 24 13 11 20 5 | 14 32 22 17 42 21 33 16 17 15 17 13 | 10 20 10 14 47 9 22 7 7 18 5 | 14 32 20 25 46 20 31 16 18 16 17 14 | 13 20 13 12 46 9 25 12 11 24 5 | 14 32 23 25 33 21 29 19 26 27 20 15 | 8 20 9 10 33 9 22 11 13 25 5 | 10 26 18 11 34 15 26 13 18 13 12 16 | 12 24 10 9 34 10 25 20 14 25 6 | 16 33 17 17 34 20 32 16 24 20 17 17 | 6 13 11 9 84 6 17 7 11 23 4 | 15 21 15 15 54 16 21 17 18 20 14 18 | 6 20 10 11 55 6 22 9 12 19 5 | 24 35 31 27 39 28 34 26 33 28 28 19 | 10 13 7 5 43 7 13 11 10 23 4 | 19 26 21 20 29 22 24 17 25 22 20 20E | 6 20 9 12 36 7 17 10 10 12 4 | 40 47 41 41 57 39 47 45 43 44 43 21 | 10 16 10 8 42 7 18 9 10 12 4 | 16 26 16 20 47 19 25 18 23 20 18 22 | 7 18 8 10 40 7 20 10 13 16 4 | 15 25 16 16 35 16 21 16 30 18 18 23 | 8 27 10 15 29 8 26 11 11 18 5 | 12 34 20 21 40 19 32 11 15 16 14 24 | 6 16 9 8 37 4 14 14 10 22 4 | 14 26 20 16 26 17 26 18 24 30 19 25E | 19 18 14 14 43 6 17 28 19 20 7 | 26 35 29 27 39 28 36 37 36 29 27 26 | 8 10 7 7 23 6 12 12 12 15 3 | 12 24 18 16 34 17 20 14 21 22 14 27E | 15 17 9 9 84 6 16 8 19 18 5 | 21 26 18 23 43 20 24 19 29 23 18 28 | 8 22 8 11 43 9 23 16 13 28 5 | 18 28 18 22 35 20 27 29 25 30 19 29 | 9 9 10 5 36 5 12 8 13 26 4 | 21 28 27 25 36 24 27 24 25 24 25 30 | 8 12 7 9 28 5 10 10 6 20 3 | 15 24 18 17 24 17 18 16 20 20 16 31E | 9 19 13 8 32 7 22 15 11 9 5 | 27 39 33 32 41 31 35 30 30 24 29 32 | 8 20 11 8 53 6 19 18 8 14 5 | 14 23 20 18 46 17 28 19 19 21 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 10 10 46 7 18 13 13 23 |T 17 28 21 20 37 20 27 19 24 23 19 WRMS | 9 18 10 10 42 6 17 11 9 23 |NE 15 26 19 18 36 18 25 17 20 22 17 MEDI | 8 18 10 9 41 7 17 11 11 20 |MD 15 26 19 20 35 19 27 17 24 22 17 Table 3.1508.2 GPS week: 1508 Day: 2 MJD: 54802.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 6 --- --- --- --- 24 --- --- --- --- 0 | 25 --- --- --- --- 9999 --- --- --- --- 28 2 | 11 27 10 14 35 9 22 9 11 18 5 | 16 34 17 18 34 19 28 18 20 19 17 3 | 9 10 7 10 46 6 16 8 9 66 6 | 24 28 28 32 29 27 31 28 28 60 27 4 | 9 12 6 9 25 5 10 6 9 27 4 | 12 16 13 21 19 13 16 16 20 22 14 5 | 8 12 9 8 23 6 10 8 11 21 3 | 14 20 19 18 26 15 18 15 22 24 16 6 | 5 9 8 12 51 4 12 7 9 20 3 | 18 19 21 24 29 18 21 20 24 22 20 7E | 10 19 9 10 39 7 17 9 9 12 4 | 17 28 21 19 30 19 26 18 19 19 18 8E | 16 18 29 11 63 5 17 17 29 23 7 | 19 24 32 22 44 19 26 21 35 20 18 9E | 13 19 11 9 62 9 16 13 23 14 5 | 19 26 21 22 33 23 21 17 37 23 20 10 | 11 14 8 11 62 9 14 15 7 15 4 | 32 38 36 38 70 34 39 35 34 37 34 11 | 7 14 8 12 73 7 19 10 11 23 4 | 19 35 24 30 64 25 35 22 20 21 23 12 | 13 18 14 9 43 10 24 12 9 20 5 | 17 30 24 21 42 22 33 20 21 18 20 13 | 9 21 12 11 35 8 20 7 6 17 4 | 14 33 21 24 47 21 32 15 21 17 18 14 | 11 17 9 10 41 10 22 10 7 21 4 | 15 28 24 27 33 20 27 19 27 24 21 15 | 9 22 7 10 34 10 22 9 9 26 5 | 12 28 20 22 37 19 26 13 19 15 16 16 | 9 25 10 11 39 8 24 12 12 25 5 | 18 31 19 20 41 21 30 18 26 23 19 17 | 8 13 7 11 85 7 11 8 9 21 4 | 22 27 24 30 66 24 25 25 28 25 24 18 | 16 22 11 10 50 6 23 9 9 21 5 | 42 54 55 52 71 49 55 51 50 50 50 19 | 9 11 7 7 34 5 10 7 8 20 3 | 19 26 25 25 30 21 27 21 28 22 23 20E | 7 20 12 9 40 7 21 10 8 11 4 | 26 39 28 33 47 33 38 29 34 34 30 21 | 10 16 8 6 35 10 18 9 10 14 4 | 15 27 16 20 44 20 26 15 24 18 17 22 | 7 15 8 9 24 7 17 7 9 14 3 | 17 23 19 18 32 17 20 17 26 19 19 23 | 8 27 12 12 24 7 26 10 8 18 5 | 13 36 22 20 38 21 33 14 21 17 17 24 | 8 17 11 8 34 5 13 13 9 22 4 | 10 23 18 17 30 13 22 13 24 27 15 25E | 18 20 15 13 43 7 18 26 23 22 7 | 18 31 25 24 43 22 34 30 33 19 20 26 | 8 14 8 9 22 6 10 9 12 20 4 | 29 35 32 34 39 29 31 30 31 27 30 27E | 15 17 9 10 52 5 17 9 20 19 5 | 19 26 23 26 42 20 23 21 32 25 21 28 | 8 21 7 12 45 10 21 16 14 27 5 | 16 28 18 24 39 19 27 25 26 26 19 29 | 9 10 8 6 42 5 11 8 9 26 4 | 26 30 34 30 33 28 28 26 30 27 29 30 | 9 11 8 8 32 4 9 8 11 19 3 | 17 19 22 22 25 18 17 14 26 20 18 31E | 8 18 12 10 33 7 20 10 11 14 4 | 17 29 26 25 35 21 27 20 25 23 21 32 | 8 19 13 5 27 7 20 15 9 12 4 | 18 27 20 21 37 18 31 22 22 23 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 11 10 44 7 18 11 12 23 |T 19 28 24 25 39 22 28 21 26 24 21 WRMS | 9 18 10 10 40 6 16 10 9 21 |NE 17 27 21 23 37 20 26 19 24 23 20 MEDI | 9 17 9 10 39 7 17 9 9 20 |MD 18 28 22 24 37 21 27 20 26 23 20 Table 3.1508.3 GPS week: 1508 Day: 3 MJD: 54803.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 13 21 8 11 41 9 20 11 6 17 4 | 22 34 22 15 38 23 30 20 27 19 19 3 | 10 12 9 5 43 7 14 8 9 67 6 | 31 30 32 29 29 28 32 26 31 61 27 4 | 9 13 7 8 33 7 10 10 12 21 4 | 17 21 15 18 20 18 21 18 21 19 15 5 | 15 16 8 4 22 5 10 11 6 21 4 | 22 24 17 12 23 15 21 13 17 23 14 6 | 8 8 9 5 62 4 10 9 9 21 3 | 26 24 24 25 40 23 25 25 30 21 24 7E | 9 19 10 8 31 8 17 10 9 11 4 | 25 30 24 26 38 24 30 23 23 27 23 8E | 13 19 15 8 87 7 18 15 29 29 6 | 22 30 24 22 44 24 26 31 39 34 23 9E | 21 21 9 9 71 8 16 18 20 17 6 | 37 31 30 25 40 27 29 26 39 29 27 10 | 15 17 6 7 47 8 17 15 11 18 4 | 38 52 43 41 62 41 48 41 41 39 41 11 | 10 13 8 9 66 10 20 10 11 23 4 | 20 35 24 22 54 24 34 21 23 18 21 12 | 18 20 12 6 40 11 25 14 8 21 5 | 29 32 27 21 42 25 36 21 22 19 22 13 | 10 23 12 9 41 10 23 8 11 18 5 | 15 33 19 14 46 18 32 13 21 14 14 14 | 16 18 8 8 49 11 25 8 9 26 5 | 17 30 20 18 33 21 29 16 25 22 18 15 | 13 23 8 10 31 11 25 10 9 26 5 | 20 30 20 20 40 19 28 17 23 20 18 16 | 11 24 11 8 43 10 27 9 11 25 5 | 20 35 21 18 48 22 31 18 23 25 19 17 | 9 16 8 9 90 8 14 12 8 21 4 | 31 33 28 30 68 32 32 32 34 32 29 18E | 18 21 8 14 40 7 26 13 10 31 6 | 54 62 60 64 75 62 66 63 62 68 60 19 | 9 10 9 6 51 7 12 8 7 23 3 | 28 29 27 28 39 27 29 27 29 30 26 20E | 10 22 11 7 42 8 22 11 10 12 4 | 19 33 24 21 44 24 32 20 23 22 20 21 | 14 19 8 6 37 8 19 11 10 14 4 | 19 31 22 19 46 23 29 20 24 19 20 22E | 12 21 10 13 31 7 20 13 15 18 5 | 16 24 19 22 40 20 20 24 29 20 18 23 | 10 29 10 11 28 11 28 11 11 17 5 | 15 38 19 18 40 19 33 12 20 15 15 24 | 10 16 7 6 35 5 13 13 9 22 4 | 15 27 22 17 31 18 26 18 23 31 19 25E | 16 20 14 13 35 8 18 23 17 19 6 | 25 32 29 25 46 26 35 38 33 26 26 26 | 11 12 6 6 21 6 14 11 8 19 4 | 29 34 29 27 34 30 32 25 34 24 29 27E | 14 17 9 7 68 6 18 10 20 19 5 | 25 29 22 26 40 25 27 28 33 31 23 28 | 9 21 8 10 47 11 23 17 11 27 5 | 20 31 19 23 37 22 28 30 25 26 20 29 | 12 10 6 5 45 6 14 10 13 30 4 | 32 39 35 31 40 37 38 33 36 31 33 30 | 12 10 7 5 36 5 12 11 7 16 3 | 22 21 21 18 31 19 22 17 20 21 17 31E | 11 18 9 9 38 7 22 8 13 8 4 | 29 40 32 28 46 30 37 30 29 29 29 32 | 10 19 9 6 30 7 21 17 8 13 4 | 18 30 23 23 42 22 33 22 25 25 21 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 13 18 9 8 48 8 19 12 12 24 |T 24 32 25 24 41 25 31 24 28 27 23 WRMS | 12 18 9 8 42 7 17 11 9 22 |NE 22 30 23 21 39 23 29 21 25 24 20 MEDI | 11 19 9 8 41 8 18 11 10 21 |MD 22 31 24 22 40 24 30 23 25 25 21 Table 3.1508.4 GPS week: 1508 Day: 4 MJD: 54804.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 4 --- --- --- --- 150 --- --- --- --- 0 | 50 --- --- --- --- 9999 --- --- --- --- 48 2 | 14 28 12 11 49 7 25 16 8 18 6 | 26 40 23 22 32 27 41 24 26 25 23 3 | 10 12 9 9 43 8 14 23 9 69 7 | 45 52 50 47 40 47 52 55 52 63 48 4 | 13 14 11 8 23 6 12 14 10 24 4 | 18 22 22 20 29 20 23 20 21 24 17 5 | 10 16 9 8 24 6 12 15 7 19 4 | 16 29 22 17 27 18 26 16 16 25 16 6 | 9 11 10 5 48 6 13 12 8 19 3 | 22 31 30 27 25 26 33 28 29 25 26 7E | 9 25 9 10 32 7 16 8 6 10 4 | 18 34 27 25 42 23 34 20 22 22 21 8E | 13 16 21 9 59 8 16 15 24 22 6 | 18 29 25 22 27 24 30 23 34 23 20 9E | 18 22 11 10 71 8 19 23 21 15 6 | 26 33 31 28 41 27 35 30 36 31 26 10E | 12 19 10 10 48 7 20 18 10 20 5 | 47 52 52 52 58 48 55 47 53 48 48 11 | 9 15 9 8 69 7 20 12 12 19 4 | 23 37 31 25 61 27 40 26 27 23 26 12 | 15 22 10 8 45 8 26 17 8 19 5 | 20 35 28 25 51 25 39 25 25 24 23 13 | 9 22 13 10 43 5 20 10 6 16 4 | 19 36 24 22 49 23 36 21 21 18 19 14 | 13 19 8 7 54 8 25 13 7 25 5 | 16 31 23 22 37 21 32 19 25 25 20 15 | 12 24 9 8 38 8 25 13 10 32 5 | 19 34 29 24 46 23 34 24 24 24 22 16 | 13 27 7 6 32 7 21 12 9 29 5 | 19 37 24 21 36 22 33 21 28 26 21 17 | 10 12 11 8 52 6 15 14 11 21 4 | 29 33 30 27 42 26 33 28 26 28 26 18E | 11 24 8 11 35 7 24 13 7 28 5 | 45 48 44 41 61 43 49 47 46 42 43 19 | 10 11 7 5 60 6 13 10 8 26 4 | 26 33 31 28 42 28 35 27 32 30 28 20E | 8 22 10 8 40 6 19 11 8 10 4 | 19 34 27 22 44 23 32 21 23 23 21 21 | 13 41 8 6 39 6 20 12 9 17 6 | 20 49 20 21 51 24 34 22 23 25 21 22E | 8 17 8 9 25 9 21 17 11 13 4 | 23 28 22 27 33 24 28 26 30 27 24 23 | 8 28 13 10 32 7 21 11 10 18 5 | 22 42 31 26 44 27 38 23 24 20 23 24 | 11 15 8 6 32 5 13 12 8 24 4 | 17 27 22 21 31 20 31 22 23 33 21 25E | 17 18 12 10 40 5 15 23 16 20 6 | 23 31 27 24 42 25 34 36 29 31 24 26 | 13 17 8 10 47 9 17 45 12 40 8 | 77 83 82 82 77 78 85 87 79 69 79 27E | 16 20 10 9 65 7 16 12 18 22 5 | 22 33 24 29 30 28 30 30 36 32 25 28 | 9 21 10 12 45 5 27 14 12 26 5 | 18 33 19 20 39 21 37 28 21 29 18 29 | 11 12 9 6 35 7 16 8 8 26 4 | 28 34 35 28 38 30 35 29 30 28 29 30 | 11 12 9 7 33 4 13 13 6 15 3 | 21 29 24 20 26 20 29 19 18 22 18 31E | 8 22 9 7 36 7 20 15 8 10 4 | 23 37 27 24 49 26 36 22 23 20 23 32 | 11 18 12 6 32 7 23 15 8 11 4 | 23 34 32 26 33 26 38 26 26 28 25 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 20 10 8 45 7 19 16 11 25 |T 26 36 30 27 41 28 37 28 29 29 27 WRMS | 11 20 10 8 42 7 18 13 9 26 |NE 26 37 30 27 40 27 37 28 28 29 27 MEDI | 11 19 9 8 40 7 19 13 9 20 |MD 22 34 27 25 41 25 34 25 26 25 23 Table 3.1508.5 GPS week: 1508 Day: 5 MJD: 54805.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 30 --- --- --- --- 0 | 20 --- --- --- --- 9999 --- --- --- --- 21 2 | 13 23 10 12 42 9 22 25 10 21 6 | 20 31 13 11 33 18 28 22 19 20 14 3 | 8 10 8 5 32 7 16 8 13 68 6 | 31 35 36 35 34 32 36 35 33 75 34 4 | 10 11 9 7 25 8 9 15 9 24 4 | 10 14 10 14 18 11 13 18 18 20 9 5 | 9 14 8 5 22 4 15 11 5 20 4 | 12 24 16 12 22 14 20 11 13 21 11 6 | 6 8 7 5 40 5 15 8 13 21 3 | 17 19 20 20 20 16 20 18 21 15 17 7E | 5 22 10 8 47 7 17 10 9 11 4 | 15 25 20 22 50 18 24 18 21 18 17 8E | 14 19 14 7 72 6 20 14 25 21 6 | 18 28 17 18 40 17 21 21 34 22 16 9E | 19 19 11 12 64 7 21 23 22 19 6 | 26 25 26 22 39 21 26 25 39 27 22 10E | 12 16 8 9 49 6 16 14 13 17 4 | 39 43 38 39 53 37 45 36 35 40 36 11 | 9 19 8 8 62 8 19 11 13 23 4 | 17 35 24 21 58 21 33 18 22 17 19 12 | 13 22 10 8 27 9 27 18 9 19 5 | 16 27 17 15 38 15 31 16 18 15 14 13 | 10 23 10 9 37 8 20 11 11 17 5 | 14 31 17 18 43 17 29 13 21 10 14 14 | 10 20 9 9 56 9 26 12 12 26 5 | 11 27 15 17 33 16 27 14 24 24 15 15 | 10 20 11 8 45 9 24 12 10 19 5 | 26 30 22 24 53 22 31 23 22 23 20 16 | 10 28 9 9 43 8 26 15 13 31 6 | 16 34 17 18 39 18 31 17 24 26 16 17 | 9 12 8 11 53 12 19 14 12 23 5 | 19 20 17 18 25 16 20 23 18 16 15 18E | 7 23 10 13 33 6 24 12 9 36 6 | 72 82 73 76 95 75 80 74 75 68 75 19 | 9 10 5 6 77 6 14 8 8 22 3 | 17 21 18 19 49 16 20 16 18 15 16 20E | 6 21 10 10 46 5 16 16 16 15 5 | 17 28 20 17 50 19 27 23 27 21 19 21 | 11 17 7 8 33 7 21 16 10 18 5 | 16 26 14 16 45 17 28 21 18 19 15 22E | 6 14 10 7 28 8 18 14 11 15 4 | 21 26 17 21 34 23 25 26 29 21 22 23 | 11 28 9 14 36 8 22 13 11 19 5 | 17 36 24 23 47 22 31 16 23 15 18 24 | 10 13 9 9 39 6 15 13 7 24 4 | 9 21 15 13 27 13 24 13 17 27 12 25E | 14 19 11 10 45 6 17 24 16 15 6 | 24 34 27 21 36 25 34 36 28 24 23 26 | 11 12 8 6 44 5 15 13 9 16 4 | 63 63 63 63 85 63 67 66 67 72 63 27E | 17 17 9 9 67 6 20 15 19 20 5 | 18 25 16 20 35 17 19 27 30 26 16 28 | 11 21 10 11 40 8 24 14 14 25 5 | 17 29 17 20 32 18 27 27 23 30 15 29 | 12 9 8 8 26 5 12 8 11 27 4 | 20 26 26 21 29 24 24 19 21 17 21 30 | 9 13 8 7 25 6 13 10 9 16 3 | 17 22 17 17 25 16 21 14 16 18 14 31E | 7 23 7 10 32 8 21 10 12 10 4 | 24 35 24 25 42 23 31 26 24 26 23 32 | 11 21 12 7 46 8 17 18 14 16 5 | 23 29 24 22 39 22 31 28 30 26 23 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 18 9 9 45 7 19 14 13 24 |T 21 30 23 23 40 22 29 24 26 26 21 WRMS | 10 18 9 9 48 7 19 12 9 22 |NE 19 28 21 20 37 20 28 21 23 24 18 MEDI | 10 19 9 8 42 7 19 13 11 20 |MD 17 28 18 20 39 18 27 21 23 21 17 Table 3.1508.6 GPS week: 1508 Day: 6 MJD: 54806.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 4 --- --- --- --- 54 --- --- --- --- 0 | 38 --- --- --- --- 9999 --- --- --- --- 42 2 | 14 25 11 12 51 10 22 21 11 18 6 | 28 39 25 19 41 31 36 30 30 27 25 3 | 7 10 6 8 23 6 13 10 11 69 6 | 35 34 35 36 33 35 34 36 35 81 33 4 | 11 13 8 6 36 7 9 14 6 18 3 | 17 20 20 21 24 20 17 25 28 23 19 5 | 14 13 10 7 22 4 11 16 8 21 4 | 17 21 17 12 32 14 19 17 18 24 14 6 | 8 10 7 8 21 4 11 10 10 21 3 | 29 29 30 28 33 28 29 31 30 29 27 7E | 7 24 9 9 25 8 17 10 8 9 4 | 26 36 25 28 38 28 30 28 26 29 26 8E | 14 18 17 10 72 8 17 14 26 21 6 | 23 28 24 24 28 25 26 24 36 23 21 9E | 21 21 8 12 60 9 16 32 21 14 7 | 36 36 35 34 34 33 34 33 45 36 33 10E | 12 17 8 6 44 7 17 15 11 19 4 | 56 58 58 55 68 57 60 55 60 54 56 11 | 7 19 8 8 70 8 15 13 9 20 4 | 22 36 30 22 67 27 35 23 27 20 24 12 | 16 23 10 8 24 10 24 19 9 19 6 | 27 35 27 27 37 29 35 29 27 30 25 13 | 9 21 11 9 43 7 19 11 7 18 4 | 21 34 25 22 49 23 29 19 22 19 20 14 | 13 18 10 10 65 9 25 16 15 25 6 | 19 29 22 23 37 22 29 23 32 25 20 15 | 11 23 9 7 42 8 26 17 10 20 5 | 22 32 24 23 40 23 34 23 27 26 24 16 | 12 28 10 9 50 8 24 17 7 43 6 | 22 39 22 23 49 26 32 25 28 40 23 17 | 10 12 10 15 99 9 13 15 13 24 5 | 39 39 36 39 79 36 36 41 41 35 37 18E | 8 27 11 11 40 6 21 13 10 27 5 | 29 39 31 29 54 32 36 31 35 38 29 19 | 8 13 4 6 80 6 11 10 8 26 3 | 34 36 31 33 64 32 30 33 34 35 31 20E | 6 19 10 7 55 7 19 15 9 17 4 | 26 37 34 30 65 29 35 28 29 35 28 21 | 12 18 8 9 41 8 19 14 9 17 4 | 26 35 24 27 60 29 36 26 31 28 27 22E | 6 22 10 9 35 5 19 17 12 17 5 | 21 30 19 24 39 22 26 26 25 28 21 23 | 10 27 11 11 34 9 22 13 9 21 5 | 20 36 25 22 43 25 30 20 27 19 21 24 | 10 13 8 8 42 4 11 14 6 24 4 | 16 26 20 17 28 19 26 20 26 31 20 25E | 13 16 13 13 30 7 16 22 17 26 6 | 30 37 34 29 40 30 38 36 33 35 29 26 | 8 15 8 7 35 4 14 18 10 17 4 | 55 58 58 58 63 57 60 55 61 56 59 27E | 16 18 9 10 78 7 15 14 21 24 5 | 30 35 28 34 28 33 31 36 42 37 30 28 | 12 23 10 13 45 9 20 14 12 27 5 | 24 32 23 28 39 24 30 33 28 34 23 29 | 9 8 9 9 30 4 12 11 12 30 4 | 42 47 46 42 58 45 48 43 45 46 44 30 | 13 13 11 8 19 7 11 18 12 15 4 | 29 26 30 23 35 23 26 28 28 28 25 31E | 9 19 10 9 41 9 21 11 9 12 4 | 22 35 28 25 38 28 32 24 31 24 24 32 | 26 22 13 10 39 10 18 18 10 27 6 | 53 52 50 50 59 45 56 40 52 45 49 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 19 10 9 49 7 18 16 12 25 |T 29 35 30 29 45 30 34 30 33 33 29 WRMS | 11 19 9 9 47 7 16 14 9 22 |NE 28 35 29 28 46 29 33 29 32 33 28 MEDI | 10 18 10 9 41 7 17 14 10 21 |MD 26 35 28 27 40 28 32 28 30 30 25 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 4.1508 GPS week: 1508 MJD: 54800.0-54806.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3054 |U 8 8 20 |U 32 33 78 |U 10 10 24 | emr | emr 2958 | 12 12 28 | 33 32 79 | 11 21 36 | esa | esa 2976 | 9 10 23 |U 32 33 77 | 9 10 21 | gfz | gfz 2943 |U 9 8 24 |U 32 35 94 | 14 13 37 | igr | igr 2975 | 9 10 25 | 32 32 79 | 9 11 25 | igs | igs 2970 | 10 9 24 | 32 32 78 | 10 15 30 | jpl | jpl 2957 |U 22 24 37 |U 32 33 77 |U 13 20 37 | mit | mit 2976 |U 10 8 24 |U 38 41 88 |U 10 15 28 | 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 5.1508.0 GPS week: 1508 Day: 0 MJD: 54800.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3072 | 10 13 22 | 14 22 52 | 11 8 23 | emr | emr 2960 | 13 10 22 | 17 21 54 | 10 17 34 | esa | esa 2976 | 11 14 23 | 15 19 52 | 6 7 18 | gfz | gfz 2951 | 11 8 20 | 16 20 58 | 11 8 23 | igr | igr 2973 | 11 14 24 | 16 19 54 | 8 9 22 | igs | igs 2973 | 12 9 19 | 15 20 52 | 10 13 30 | jpl | jpl 2960 | 17 15 33 | 16 20 49 | 11 13 31 | mit | mit 2976 | 14 7 26 | 17 21 54 | 9 11 25 | Table 5.1508.1 GPS week: 1508 Day: 1 MJD: 54801.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3067 | 8 13 20 | 19 15 81 | 9 10 25 | emr | emr 2960 | 14 12 26 | 19 18 69 | 11 17 30 | esa | esa 2976 | 9 9 18 | 16 19 69 | 8 8 18 | gfz | gfz 2949 | 8 8 21 | 18 20 106 | 13 10 37 | igr | igr 2976 | 9 11 24 | 18 15 76 | 10 11 23 | igs | igs 2969 | 10 9 21 | 18 16 74 | 9 17 31 | jpl | jpl 2959 | 19 21 33 | 17 13 76 | 14 19 33 | mit | mit 2976 | 8 7 20 | 18 17 72 | 9 13 22 | Table 5.1508.2 GPS week: 1508 Day: 2 MJD: 54802.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3061 | 6 8 18 | 10 12 38 | 10 13 22 | emr | emr 2960 | 8 10 24 | 13 13 38 | 10 25 32 | esa | esa 2976 | 7 9 18 | 9 12 36 | 9 11 17 | gfz | gfz 2949 | 7 9 21 | 10 15 51 | 15 19 40 | igr | igr 2976 | 7 10 21 | 10 14 37 | 9 14 24 | igs | igs 2955 | 6 7 18 | 9 12 38 | 9 15 22 | jpl | jpl 2959 | 25 29 36 | 9 15 34 | 18 28 42 | mit | mit 2976 | 8 7 15 | 9 12 35 | 9 18 22 | Table 5.1508.3 GPS week: 1508 Day: 3 MJD: 54803.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 9 5 21 | 155 149 285 | 8 9 22 | emr | emr 2960 | 12 12 30 | 157 142 290 | 9 18 31 | esa | esa 2976 | 10 8 23 | 156 149 288 | 7 9 21 | gfz | gfz 2949 | 11 7 25 | 155 153 292 | 11 10 32 | igr | igr 2976 | 11 10 25 | 155 146 289 | 7 9 22 | igs | igs 2974 | 11 10 27 | 155 146 288 | 7 11 24 | jpl | jpl 2958 | 17 22 35 | 156 148 287 | 13 18 35 | mit | mit 2976 | 11 9 20 | 155 146 283 | 9 13 24 | Table 5.1508.4 GPS week: 1508 Day: 4 MJD: 54804.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3061 | 8 5 18 | 10 12 34 | 8 7 19 | emr | emr 2960 | 9 9 33 | 12 12 33 | 12 20 37 | esa | esa 2976 | 7 5 24 | 9 11 32 | 8 8 18 | gfz | gfz 2936 | 9 8 22 | 9 13 51 | 15 11 33 | igr | igr 2973 | 8 7 25 | 8 11 32 | 8 8 19 | igs | igs 2970 | 11 10 30 | 9 12 33 | 9 16 31 | jpl | jpl 2959 | 25 30 37 | 10 11 37 | 11 18 33 | mit | mit 2976 | 15 10 27 | 40 63 84 | 10 15 30 | Table 5.1508.5 GPS week: 1508 Day: 5 MJD: 54805.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3072 | 9 8 21 | 9 12 31 | 10 8 20 | emr | emr 2955 | 18 18 33 | 9 13 39 | 14 22 37 | esa | esa 2976 | 13 12 30 | 10 13 36 | 10 9 22 | gfz | gfz 2933 | 9 9 33 | 9 13 55 | 15 13 40 | igr | igr 2976 | 13 12 30 | 11 14 37 | 11 10 21 | igs | igs 2976 | 10 10 29 | 9 14 33 | 12 13 27 | jpl | jpl 2954 | 28 23 51 | 10 13 29 | 14 19 38 | mit | mit 2976 | 11 10 34 | 16 20 47 | 14 16 31 | Table 5.1508.6 GPS week: 1508 Day: 6 MJD: 54806.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3070 | 6 6 18 | 7 7 26 | 12 15 36 | emr | emr 2956 | 10 14 31 | 7 8 29 | 13 27 50 | esa | esa 2976 | 8 9 25 | 7 8 28 | 14 16 37 | gfz | gfz 2935 | 10 10 28 | 8 11 48 | 18 18 52 | igr | igr 2976 | 8 7 24 | 7 8 28 | 12 15 41 | igs | igs 2976 | 8 7 24 | 7 8 29 | 14 18 44 | jpl | jpl 2955 | 21 28 36 | 6 10 30 | 13 25 51 | mit | mit 2976 | 7 9 23 | 9 12 41 | 13 22 43 | 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 6.1508 GPS week: 1508 MJD: 54800.500-54806.500 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 | 29 4 5 238 0 | -2 16 | 18 11 55 58 8 | 1 emr uuuuu | -19 -33 -59 45 6 | 36 40 | 24 25 90 67 7 | 1 esa uuuuu | -15 -7 176 -195 -1 | 2 17 | 8 16 58 29 3 | 2 gfz uuuuu | 22 21 26 124 0 | -4 19 | 11 12 47 42 8 | 4 grg xxxxx | -7 -15 -39 229 -7 | -2 20 | 29 27 91 72 24 | 4 igr xxxxx | 1 28 46 69 0 | -5 15 | 17 16 78 72 10 | 2 irf xxxxx | -5 2 -24 -9 -2 | -9 19 | 7 8 36 29 11 | 4 jpl uuuuu | 64 2 -117 284 1 | 8 18 | 57 32 97 82 12 | 3 mit uuuuu | 1 -1 -188 -157 -11 | 8 20 | 26 26 109 40 12 | 6 ngs uuuuu | -36 -3 23 32 1 | 4 20 | 36 29 70 87 10 | 1 sio uuxxx | 19 7 1 246 -24 | 2 23 | 13 21 125 55 19 | 11 Table 7.1508.0 GPS week: 1508 Day: 0 MJD: 54800.500 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 | 17 11 -36 265 4 | -2 15 emr uuuuu | 7 -22 -190 94 -3 | 38 42 esa uuuuu | -2 10 59 -166 -6 | 4 18 gfz uuuuu | 9 15 17 183 -8 | 2 22 grg xxxxx | -9 -27 -28 196 -45 | 4 22 igr xxxxx | 17 57 -23 110 -10 | -2 15 irf xxxxx | -7 0 7 13 -18 | -3 19 jpl uuuuu | 61 5 -90 221 17 | 3 12 mit uuuuu | -24 -12 -40 -85 -26 | 17 25 ngs uuuuu | -27 1 121 -102 -13 | 5 21 sio uuxxx | 35 -14 -79 222 -53 | 20 30 Table 7.1508.1 GPS week: 1508 Day: 1 MJD: 54801.500 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 -12 -68 220 -2 | -2 15 emr uuuuu | -18 -8 -177 113 5 | 37 40 esa uuuuu | -16 -8 195 -223 -1 | 3 16 gfz uuuuu | 25 12 -38 92 -3 | -1 19 grg xxxxx | 21 -54 24 228 -6 | 1 23 igr xxxxx | 0 11 -38 132 -1 | -3 14 irf xxxxx | -9 -3 -4 0 -15 | -5 17 jpl uuuuu | -5 27 -1 296 16 | 5 17 mit uuuuu | -15 11 -131 -149 -27 | 15 23 ngs uuuuu | 9 -15 66 41 3 | 3 19 sio uuxxx | 13 -25 -23 292 -46 | 13 25 Table 7.1508.2 GPS week: 1508 Day: 2 MJD: 54802.500 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 | 38 16 14 211 4 | -1 15 emr uuuuu | 0 -47 18 87 -2 | 37 40 esa uuuuu | -21 1 193 -214 1 | 3 16 gfz uuuuu | 15 26 74 148 -6 | -2 18 grg xxxxx | 37 -13 -168 238 5 | -1 22 igr xxxxx | -20 14 42 53 -12 | -4 14 irf xxxxx | -9 12 15 -2 -3 | -8 18 jpl uuuuu | 35 -13 -138 224 -4 | 9 19 mit uuuuu | -6 3 -111 -156 -13 | 11 21 ngs uuuuu | -14 -12 -91 52 20 | 4 19 sio uuxxx | 10 30 -60 203 -26 | 6 23 Table 7.1508.3 GPS week: 1508 Day: 3 MJD: 54803.500 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 | 43 -9 12 341 14 | -2 15 emr uuuuu | -1 -43 -31 76 6 | 35 38 esa uuuuu | -15 6 178 -183 2 | 1 16 gfz uuuuu | 33 34 10 137 -4 | -5 19 grg xxxxx | -33 -29 -77 298 -33 | 0 22 igr xxxxx | -19 31 35 170 -6 | -6 16 irf xxxxx | -7 7 -13 -2 3 | -10 19 jpl uuuuu | 75 16 -308 285 5 | 9 19 mit uuuuu | -11 14 -138 -166 -6 | 8 20 ngs uuuuu | -57 -55 71 3 -1 | 5 20 sio uuxxx | 11 10 10 345 -15 | -1 22 Table 7.1508.4 GPS week: 1508 Day: 4 MJD: 54804.500 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 7 44 259 -5 | -1 17 emr uuuuu | -53 -57 43 11 13 | 35 39 esa uuuuu | -11 -30 247 -227 0 | 1 16 gfz uuuuu | 7 1 -23 152 4 | -7 18 grg xxxxx | -44 -17 -95 294 8 | -6 18 igr xxxxx | 25 36 202 40 15 | -7 16 irf xxxxx | 12 10 -36 23 5 | -11 18 jpl uuuuu | 176 50 -130 442 -4 | 11 21 mit uuuuu | 56 38 -297 -188 -6 | 6 17 ngs uuuuu | -102 6 17 -39 5 | 6 21 sio uuxxx | 28 3 80 217 -9 | -4 19 Table 7.1508.5 GPS week: 1508 Day: 5 MJD: 54805.500 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 | 58 10 -27 158 -9 | -3 18 emr uuuuu | -48 -61 -29 -73 11 | 35 38 esa uuuuu | -27 3 155 -150 2 | -1 17 gfz uuuuu | 27 31 75 94 13 | -9 19 grg xxxxx | -8 27 -47 262 -4 | -7 18 igr xxxxx | 2 22 37 5 5 | -8 16 irf xxxxx | -6 -5 -62 -48 6 | -13 20 jpl uuuuu | 77 -36 -44 316 -12 | 10 21 mit uuuuu | -3 -24 -291 -212 -3 | 1 16 ngs uuuuu | -23 23 -11 128 -4 | 4 20 sio uuxxx | 32 13 -154 255 -9 | -9 21 Table 7.1508.6 GPS week: 1508 Day: 6 MJD: 54806.500 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 | 28 2 96 212 -3 | -3 18 emr uuuuu | -23 5 -52 4 15 | 38 41 esa uuuuu | -14 -28 203 -203 -2 | 0 16 gfz uuuuu | 36 30 66 63 6 | -7 18 grg xxxxx | -15 8 116 89 26 | -7 18 igr xxxxx | 2 22 63 -30 8 | -6 15 irf xxxxx | -7 -7 -79 -50 8 | -12 19 jpl uuuuu | 27 -34 -107 204 -9 | 11 20 mit uuuuu | 10 -40 -310 -144 3 | 1 16 ngs uuuuu | -39 33 -11 143 -5 | 3 20 sio uuxxx | 2 33 231 191 -5 | -11 21