Date: Thu, 18 Jun 2009 11:45:57 +0000 From: Jim Ray Subject: [IGSREPORT-17499] Wk 1534 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4a3a28f5.nrqC5VwyoIrgSwGs%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 Jun 04:46:19 PDT 2009 Message Number 17499 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1534 (May 31, 2009 - Jun 06, 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: igs1534[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1534[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1534[0-6].cls IGS GPS clock combination summary report. igs15347.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15347.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 | ALL | 1 1 0 | COD | 8 9 10 27 8 9 10 27 0 | ESA | 8 9 10 0 | GFZ | 32 CHUR OHI2 0 | GRG | NLIB 0 | JPL | 27 32 0 | MIT | 5 32 5 32 1 | ALL | 1 1 1 | COD | 8 9 10 27 8 9 10 27 MATE 1 | EMR | 21 21 MIZU WTZR 1 | ESA | 8 9 10 27 32 MIZU 1 | GFZ | 32 AMC2 ANKR CHUR EIL1 PRDS TSKB UNSA 1 | GRG | NLIB 1 | JPL | 32 1 | MIT | 32 32 2 | COD | 8 9 8 9 10 MIZU 2 | EMR | 27 27 WTZR 2 | ESA | 8 9 10 SEY1 2 | GRG | NLIB 2 | JPL | 27 32 HARB 2 | MIT | 5 32 5 32 HOB2 2 | NGS | 1 3 | COD | 8 10 8 10 YAR2 3 | EMR | 5 9 5 9 3 | ESA | 8 10 DAV1 MIZU UNSA 3 | GFZ | 20 32 IRKT 3 | GRG | PIE1 3 | JPL | 9 32 3 | MIT | 29 32 13 29 32 DAV1 3 | NGS | 1 4 | COD | 8 8 CHUR 4 | EMR | MIZU WTZR 4 | ESA | 8 10 32 CHUR MAS1 MIZU 4 | GFZ | 18 31 CHUR GUAT IRKT UNSA 4 | GRG | NLIB 4 | MIT | 5 10 32 5 10 19 32 4 | NGS | 1 5 | ALL | 5 1 5 5 | COD | 8 10 8 10 5 | EMR | 32 32 MIZU 5 | ESA | 8 10 32 MIZU NRC1 UNSA 5 | GFZ | BAN2 CHUR FAA1 5 | GRG | NLIB 5 | JPL | HARB 5 | MIT | SYOG FLIN SYOG 6 | ALL | 1 1 6 | COD | 8 10 8 10 6 | EMR | 32 32 MIZU WTZR 6 | ESA | 8 10 MIZU UNSA 6 | GFZ | BRAZ IRKT 6 | GRG | KHAJ NLIB 6 | JPL | MDVJ 6 | MIT | 5 19 5 19 BRAZ 5. New clock offsets and drifts were estimated for centres showing reference clock resets. Note that only the largest clock offset and drift are output to the summary file. However, the clock combination and the listed RMS include all the clock segments. In summary, the following clock shifts/resets were noticed and accounted for: Day | Centre | Time | Jump ----+--------+--------+------------- 2 | GFZ | ~21:15 | ~ -0.75 ns 6. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G09 | | | | 1 | | | | 7. 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. 8. 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 | .2 .4 .1 -12 -17 0 .12 EMR | 6.6 -18.5 -4.7 -9 35 13 .19 ESA | .7 -4.5 19.0 -20 33 80 .15 GFZ | .1 .3 1.2 10 -4 4 -.08 GRG | 8.1 -1.1 -.1 -4 -18 13 .12 JPL | 3.2 -1.9 -.6 6 -2 -10 .25 MIT | 3.1 -8.8 11.9 -19 33 -10 .08 NGS | 10.0 -9.2 7.6 -103 -107 30 .04 SIO | -2.1 -4.3 -4.0 -63 16 -15 .45 9. 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. 10. 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. 11. 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 1.1534.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1534.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 2.1534.[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 3.1534.[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 5.1534.0-6). 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 1534 summary. (May 31, 2009 - Jun 06, 2009) Table 1.1534.a GPS week: 1534 MJD: 54982.000-54988.000 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 231| 0 0 0 -24 0 -25 -.14 8 8 | -315 -401 16 80 | 0 0 0 13 13 25 .02 | 198 339 emr 79| 0 1 -1 -22 -80 -44 .30 18 18 | 2780 -555 17 94 | 1 1 1 35 6 19 .03 | 1391 1332 esa 126| -1 1 0 -43 -71 46 .39 10 9 | 234 -1789 18 106 | 1 0 1 14 21 17 .03 | 656 831 gfz 187| 0 0 1 -80 -16 201 -.01 11 11 | -428539 34358 24 144 | 0 1 0 14 16 86 .08 | 534551 43481 grg 104| 2 0 -10 -73 35 -31 1.00 37 35 | 28 -167 90 222 | 1 1 1 32 18 54 .05 | 182 446 igr n/a| 0 0 0 -46 -10 -71 .07 5 5 | 17889 -443 20 69 | 0 0 1 14 8 15 .05 | 1229 1308 jpl 127| 1 1 -4 -64 -27 -9 .46 18 16 | 907 -444 17 98 | 1 0 1 11 14 31 .05 | 1083 1203 mit 260| 0 -1 1 4 -69 -58 -.28 10 9 | -14849 -505 20 153 | 0 0 1 33 23 18 .02 | 667 829 ngs 215| 0 0 0 144 203 -71 -.31 9 7 | -241037 368340 1975 3783 | 1 0 0 23 47 19 .03 | 422051 507958 sio 255| -3 0 1 97 -35 -64 .17 22 20 | --- --- --- --- | 1 0 2 39 36 13 .03 | --- --- Table 1.1534.b GPS week : 1534 MJD: 54982.000-54988.000 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 | 16 22 18 15 20 18 19 | 2 | 5 5 5 5 5 5 4 | 3 | 4 4 4 3 3 4 4 | 4 | 3 4 4 3 3 3 4 | 5 | 12 0 9 9 11 12 9 | 6 | 4 4 4 3 4 4 4 | 7 | 4 5 5 5 6 5 5 | 8 | 6 5 5 5 5 5 6 | 9 | 5 5 6 7 6 4 4 | 10 | 5 5 5 5 5 4 5 | 11 | 4 5 4 4 4 4 5 | 12 | 5 5 6 5 5 5 5 | 13 | 5 5 5 6 5 5 5 | 14 | 5 5 5 5 4 5 5 | 15 | 6 7 6 6 5 4 5 | 16 | 5 5 5 5 5 5 5 | 17 | 5 4 5 4 4 4 5 | 18 | 5 5 5 5 5 5 5 | 19 | 5 5 6 5 5 5 5 | 20 | 5 5 5 5 4 4 4 | 21 | 4 5 5 5 4 4 5 | 22 | 4 5 5 4 4 5 5 | 23 | 5 6 6 5 5 6 5 | 24 | 3 4 3 3 3 3 3 | 25 | 7 7 5 5 5 4 5 | 26 | 3 4 4 4 3 3 4 | 27 | 5 5 6 6 5 4 4 | 28 | 5 5 6 5 5 5 5 | 29 | 5 5 5 5 5 5 5 | 30 | 4 4 4 3 3 4 4 | 31 | 6 6 5 5 4 4 4 | 32 | 6 6 6 7 5 5 5 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1534.0 GPS week: 1534 Day: 0 MJD: 54982.000 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 231| 1 0 0 -25 -25 -66 -.16 9 8 | -89 -1060 17 77 | -3 28 | emr 79| -3 2 3 -50 -88 -13 .30 19 19 | 3730 1690 17 100 | 23 0 | esa 126| 0 0 2 -33 -79 31 .38 9 8 | 990 -2475 19 115 | 48 42 | gfz 187| -1 0 0 -89 5 236 .01 11 11 | -333 506 26 116 | 47 -7 | grg 104| 4 -1 -9 -81 20 15 .95 37 32 | -308 629 88 214 | 36 53 | igr n/a| 0 0 0 -35 -8 -68 .11 6 5 | 18805 1451 20 71 | 36 -13 | jpl 127| 1 2 -3 -76 -15 -37 .40 19 17 | 1692 1402 18 106 | 31 -18 | mit 260| 0 -2 0 -35 -49 -65 -.27 11 11 | -15229 80 21 176 | -2 -21 | ngs 215| 1 -1 -1 177 155 -51 -.34 8 6 | 316334 -163696 2286 4354 | 29 22 | sio 255| -3 1 -1 54 -12 -66 .13 23 20 | --- --- --- --- | -72 -22 | Table 2.1534.1 GPS week: 1534 Day: 1 MJD: 54983.000 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 231| 0 0 1 -49 -3 -17 -.13 9 8 | -568 -299 17 68 | 76 30 | emr 79| 0 3 0 -72 -69 -43 .31 20 20 | 4872 -1447 15 93 | 27 -33 | esa 126| 1 0 1 -50 -69 26 .36 10 10 | -260 -2293 18 106 | 60 31 | gfz 187| 0 1 0 -88 -28 318 .00 14 14 | 19 -307 29 116 | 91 21 | grg 104| 3 3 -10 -105 31 -3 1.02 38 34 | 189 -576 96 216 | 130 1 | igr n/a| 0 0 0 -68 -5 -69 .10 7 6 | 19623 -1550 20 59 | 21 -61 | jpl 127| 3 0 -4 -81 -14 -45 .46 19 17 | 2358 -1533 16 89 | 20 27 | mit 260| 0 -2 0 71 -66 -69 -.27 11 10 | -14592 -790 20 131 | -5 -16 | ngs 215| 0 0 0 109 162 -63 -.31 9 9 | 11517 3285 1936 3894 | 27 -10 | sio 255| -5 0 -2 170 -6 -55 .18 23 22 | --- --- --- --- | -91 -25 | Table 2.1534.2 GPS week: 1534 Day: 2 MJD: 54984.000 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 231| 0 -1 0 -17 -5 -45 -.16 9 9 | -153 -519 18 79 | -17 -19 | emr 79| 2 0 -2 -32 -73 -62 .30 19 19 | 3985 -2475 17 88 | -1 -48 | esa 126| -1 2 2 -32 -52 61 .41 11 11 | 916 -3033 18 95 | 35 -12 | gfz 187| -1 0 0 -101 -1 298 .10 12 12 | -999999 81807 23 93 | 48 -14 | grg 104| 2 1 -10 -17 58 -75 1.03 40 38 | 173 -135 83 221 | 41 -4 | igr n/a| 0 0 1 -36 -18 -102 .09 5 4 | 18546 -2273 19 68 | -1 -13 | jpl 127| 3 2 -5 -55 -19 -37 .43 18 16 | 1243 -2077 17 87 | 21 9 | mit 260| 1 -1 0 -7 -105 -84 -.31 10 10 | -14791 -118 19 158 | 0 3 | ngs 215| -1 0 0 160 195 -82 -.34 9 8 | 5769 10044 1880 4190 | 66 66 | sio 255| -2 0 1 63 -42 -83 .17 21 20 | --- --- --- --- | -70 -18 | Table 2.1534.3 GPS week: 1534 Day: 3 MJD: 54985.000 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 231| 0 0 0 -23 1 -25 -.13 8 7 | -494 -296 16 98 | 6 -1 | emr 79| 0 2 0 -19 -81 -67 .31 19 18 | 1570 -1241 19 108 | -13 -15 | esa 126| -1 0 -2 -24 -49 47 .43 10 10 | 454 -1140 18 105 | 10 41 | gfz 187| 0 0 1 -84 -40 183 -.03 11 11 | -999999 80071 24 281 | 61 27 | grg 104| 5 0 -12 -107 30 -56 .94 38 37 | 178 -591 99 239 | 86 52 | igr n/a| 0 -1 0 -40 -25 -49 .01 6 5 | 16490 -1192 21 82 | 16 -3 | jpl 127| 1 1 -3 -56 -22 -14 .49 18 16 | -530 -1070 16 102 | -16 21 | mit 260| 0 -1 2 0 -34 -57 -.28 10 9 | -14916 -2056 20 174 | 15 -13 | ngs 215| 0 0 0 128 155 -66 -.33 10 8 | 10171 6134 2289 4105 | 62 6 | sio 255| -1 1 3 94 16 -78 .20 22 20 | --- --- --- --- | -76 -40 | Table 2.1534.4 GPS week: 1534 Day: 4 MJD: 54986.000 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 231| 1 0 0 -16 16 -25 -.14 8 7 | -95 -261 16 89 | 17 -31 | emr 79| 0 -1 -2 -32 -81 -24 .29 18 18 | 1416 -98 18 91 | -17 -31 | esa 126| -4 1 1 -67 -103 67 .41 10 10 | 574 -1630 18 98 | 42 80 | gfz 187| 0 -1 0 -68 -4 89 .06 11 11 | 56 -285 22 107 | 54 -12 | grg 104| 1 0 -10 -65 63 -74 .97 36 36 | 47 -422 95 218 | 70 -55 | igr n/a| 0 1 -2 -45 -10 -69 .11 5 5 | 16316 -261 21 71 | 3 -25 | jpl 127| 0 1 -3 -57 -30 16 .47 17 15 | -420 -307 17 112 | -9 19 | mit 260| 0 0 2 5 -89 -25 -.32 8 7 | -15906 446 18 149 | 12 -3 | ngs 215| 1 1 -1 134 255 -47 -.27 10 7 | -682022 909389 1868 3093 | 51 -84 | sio 255| -2 0 3 119 -50 -44 .18 20 19 | --- --- --- --- | -93 -18 | Table 2.1534.5 GPS week: 1534 Day: 5 MJD: 54987.000 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 231| 1 0 0 -8 5 -14 -.12 8 7 | -406 -423 14 75 | -13 -24 | emr 79| 1 0 -1 24 -83 -53 .34 17 17 | 1660 -419 16 94 | -67 -7 | esa 126| -2 1 -1 -50 -92 63 .39 9 9 | -599 -1224 21 121 | 69 74 | gfz 187| 0 0 1 -69 -21 128 -.10 9 9 | 481 -1904 25 200 | 14 -17 | grg 104| 0 -1 -12 -49 23 -83 1.08 36 33 | 26 -277 93 231 | 6 -33 | igr n/a| 0 0 -1 -33 -3 -71 .07 4 4 | 17329 32 21 74 | 7 -13 | jpl 127| 1 0 -5 -53 -33 25 .56 18 16 | 578 25 20 106 | -33 24 | mit 260| 0 -1 2 -17 -73 -49 -.28 9 8 | -14819 -204 19 176 | 19 -17 | ngs 215| 1 0 0 164 262 -87 -.29 9 7 | -678338 909818 1954 3305 | -4 -104 | sio 255| -4 0 4 75 -81 -61 .19 20 20 | --- --- --- --- | -73 21 | Table 2.1534.6 GPS week: 1534 Day: 6 MJD: 54988.000 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 231| 0 -1 0 -33 9 14 -.17 8 7 | -401 47 17 75 | 15 -24 | emr 79| 1 1 -2 23 -86 -47 .25 17 17 | 2230 100 18 86 | -65 -20 | esa 126| -1 1 -1 -49 -53 27 .36 9 8 | -437 -734 19 104 | 62 52 | gfz 187| 0 1 1 -60 -22 157 -.09 11 11 | -999999 80620 25 100 | 44 -11 | grg 104| 2 0 -9 -89 18 56 .99 36 34 | -107 203 82 218 | 83 10 | igr n/a| 0 0 -1 -64 -5 -67 .01 5 5 | 18114 691 20 62 | 59 -18 | jpl 127| 1 1 -5 -69 -55 24 .44 18 16 | 1434 452 17 89 | -10 54 | mit 260| 1 -2 2 13 -68 -56 -.27 10 9 | -13694 -899 25 112 | 13 -26 | ngs 215| 0 0 0 140 238 -101 -.29 10 7 | -670691 903410 1613 3545 | 11 -52 | sio 255| -4 1 3 104 -72 -62 .13 22 22 | --- --- --- --- | -76 17 | 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 3.1534.0 GPS week: 1534 Day: 0 MJD: 54982.000 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 | 25 --- --- --- --- 33 --- 14 24 --- 15 | 35 --- --- --- --- 38 --- 30 32 --- 30 2 | 9 21 9 10 33 7 23 13 9 21 5 | 20 27 16 20 28 16 25 17 23 23 17 3 | 5 8 9 11 21 7 8 10 7 17 3 | 25 28 23 29 24 24 22 32 29 24 26 4 | 8 15 6 7 25 4 11 11 5 14 3 | 20 32 23 23 27 22 25 26 23 28 22 X5 | 26 18 --- --- --- 31 --- 17 19 --- 12 | 25 19 --- --- --- 160 --- 15 14 --- 17 6 | 8 9 7 9 29 6 10 10 7 23 3 | 37 45 42 46 38 41 41 42 35 45 40 7E | 11 15 7 13 53 4 17 8 8 17 4 | 21 27 27 22 55 22 29 25 25 29 22 8E | 10 25 11 10 80 4 24 12 9 21 5 | 31 39 28 26 48 26 39 27 31 28 27 9E | 8 17 8 13 42 5 18 13 8 13 4 | 43 48 48 47 52 44 47 44 47 46 44 10E | 10 18 7 11 50 6 16 10 10 28 4 | 35 40 36 35 62 36 36 38 43 45 36 11 | 10 16 12 9 51 4 18 9 4 17 4 | 28 32 31 27 38 27 26 29 32 28 27 12 | 9 20 7 9 26 7 21 10 6 21 4 | 18 33 22 22 35 22 31 25 24 26 22 13 | 7 16 8 12 46 4 21 8 8 28 4 | 14 28 21 25 48 20 29 23 22 24 19 14 | 6 21 8 11 39 5 25 10 7 17 4 | 17 29 26 26 38 20 28 23 21 21 20 15 | 8 25 8 12 29 8 22 20 11 27 6 | 19 35 23 23 35 20 29 25 25 25 20 16 | 9 18 8 10 33 4 28 13 7 25 5 | 19 32 23 22 39 22 37 20 24 22 21 17 | 8 17 12 8 21 6 14 15 12 24 5 | 29 39 34 30 39 31 29 33 36 34 30 18E | 11 20 7 15 31 7 23 13 8 15 5 | 19 29 22 21 30 19 27 23 24 25 20 19 | 8 10 6 13 23 7 15 8 7 39 4 | 31 30 31 29 31 30 29 33 35 35 30 20E | 8 24 11 8 28 5 18 12 11 19 5 | 12 29 18 15 25 15 23 16 19 20 15 21 | 7 21 8 8 26 4 19 10 8 20 4 | 14 30 18 14 37 16 26 19 22 21 16 22E | 8 16 6 8 27 3 24 12 10 10 4 | 13 26 20 17 31 18 26 17 25 20 17 23 | 8 17 10 13 34 7 22 10 8 32 5 | 11 27 17 19 36 15 27 18 17 25 13 24 | 9 14 5 5 26 5 13 6 6 12 3 | 15 22 17 16 24 16 18 20 20 18 16 25E | 18 27 11 17 35 8 23 14 9 35 6 | 107 116 111 115 115 111 118 108 109 117 110 26 | 6 15 6 6 38 5 11 8 7 17 3 | 21 28 24 23 53 21 28 24 26 32 23 27E | 10 22 7 13 51 5 18 13 9 17 4 | 122 127 122 126 109 125 124 117 128 121 123 28 | 8 17 9 14 38 7 20 17 11 21 5 | 18 32 23 22 46 22 32 20 20 21 19 29 | 8 13 9 11 30 6 15 9 7 40 5 | 21 27 27 27 26 23 22 26 27 36 23 30 | 8 9 9 6 20 6 11 7 7 25 3 | 23 28 28 24 36 24 25 25 24 24 23 31E | 11 27 12 18 33 3 24 11 7 23 5 | 16 34 20 18 44 18 31 19 21 21 18 32E | 14 32 11 18 27 5 17 11 8 19 5 | 102 106 101 106 104 103 107 99 109 104 104 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 9 11 37 6 19 11 8 23 |T 30 39 34 33 45 36 37 33 34 36 31 WRMS | 8 19 8 11 32 5 17 11 6 20 |NE 21 30 24 24 35 30 27 25 25 26 22 MEDI | 8 17 8 11 31 5 18 11 8 21 |MD 21 30 23 23 38 22 29 25 25 25 22 Table 3.1534.1 GPS week: 1534 Day: 1 MJD: 54983.000 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 | 32 --- --- --- --- 54 --- 15 38 --- 21 | 28 --- --- --- --- 51 --- 36 48 --- 33 2 | 6 21 10 13 37 6 23 10 11 20 5 | 21 28 18 21 34 20 27 19 24 22 19 3 | 7 12 9 13 30 7 8 10 5 17 3 | 20 29 17 26 20 21 23 26 24 21 22 4 | 6 15 8 10 31 6 15 11 8 15 4 | 17 25 21 17 31 23 23 20 20 23 19 X5 | 3 --- --- --- --- 705 --- --- --- --- 0 | 25 --- --- --- --- 605 --- --- --- --- 29 6 | 8 13 6 13 23 6 9 9 6 20 3 | 21 31 25 29 26 26 28 26 26 29 24 7E | 11 19 9 18 23 3 17 12 8 19 5 | 19 31 24 29 39 23 28 25 23 24 21 8E | 12 23 13 11 56 7 19 12 8 17 5 | 26 35 31 28 47 26 35 29 30 29 27 9E | 11 20 11 15 54 6 24 9 11 16 5 | 40 45 45 42 51 41 43 44 48 40 42 10E | 14 19 10 16 80 5 14 10 12 22 5 | 38 40 37 42 49 39 37 39 42 40 37 11 | 10 19 10 12 57 9 16 8 10 18 4 | 22 30 23 25 31 24 24 24 26 27 22 12 | 8 20 10 8 29 6 21 12 8 22 4 | 22 34 28 22 34 25 32 26 27 25 25 13 | 7 18 9 16 44 7 22 10 9 26 5 | 17 30 23 27 43 22 31 23 20 24 20 14 | 8 20 12 11 40 7 23 10 8 17 4 | 16 30 25 24 43 22 29 21 22 23 21 15 | 8 26 12 14 40 6 23 18 15 30 6 | 17 30 24 18 34 20 27 26 27 26 20 16 | 8 22 8 14 32 5 26 13 7 23 5 | 20 34 21 24 36 21 34 23 23 25 21 17 | 9 11 7 9 25 7 11 10 7 25 4 | 15 23 22 16 25 21 20 19 21 24 17 18E | 12 17 10 16 30 4 22 14 6 15 5 | 33 40 36 34 40 34 39 35 33 35 33 19 | 8 12 6 18 22 11 17 9 6 39 5 | 23 27 20 28 26 22 22 28 28 27 23 20E | 7 22 10 16 30 7 20 10 8 16 4 | 12 28 20 19 26 16 23 17 17 18 14 21 | 6 20 12 12 31 4 21 11 7 21 4 | 17 27 16 13 31 14 27 19 21 21 16 22E | 10 18 10 11 31 4 22 11 6 10 4 | 16 28 23 20 35 18 27 19 16 19 17 23 | 8 19 12 15 29 7 23 10 8 33 5 | 15 30 20 21 36 18 29 20 17 30 17 24 | 8 14 8 12 22 3 10 7 7 11 3 | 16 23 20 16 18 17 17 22 21 17 18 25E | 15 29 12 28 27 11 20 14 10 30 7 | 60 64 54 67 63 57 65 56 62 60 58 26 | 7 16 9 10 24 5 14 8 10 20 4 | 15 25 18 17 28 19 25 20 22 25 17 27E | 11 23 12 11 46 7 21 9 11 19 5 | 109 112 115 113 114 110 114 109 114 111 112 28 | 9 19 10 13 40 9 21 10 8 22 4 | 18 30 20 18 40 20 31 15 18 20 17 29 | 7 12 7 12 30 7 12 7 5 41 4 | 14 18 13 16 20 14 18 17 17 27 13 30 | 7 13 6 7 19 5 13 8 8 19 3 | 19 21 18 16 25 18 19 20 21 21 17 31E | 7 26 10 16 28 7 18 16 11 21 5 | 15 34 16 17 38 17 26 24 18 26 16 32E | 12 32 13 16 49 9 16 9 10 22 5 | 85 91 88 85 78 88 86 86 83 89 84 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 10 14 38 7 19 11 9 23 |T 26 35 29 29 38 47 33 30 30 31 27 WRMS | 8 20 10 14 34 6 17 10 9 22 |NE 18 27 20 20 30 49 25 22 23 24 20 MEDI | 8 19 10 13 30 7 19 10 8 20 |MD 19 30 22 22 34 22 27 24 23 25 21 Table 3.1534.2 GPS week: 1534 Day: 2 MJD: 54984.000 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 | 27 --- --- --- --- 31 --- 13 29 --- 17 | 26 --- --- --- --- 27 --- 25 34 --- 22 2 | 8 19 15 9 39 4 25 7 10 19 5 | 17 26 15 17 36 13 25 16 25 16 15 3 | 8 10 8 13 42 4 7 8 8 16 3 | 19 23 23 29 19 21 20 26 25 21 21 4 | 7 14 8 8 24 5 12 13 7 13 3 | 17 22 21 22 31 19 21 19 23 24 18 X5 | 17 19 --- --- --- 25 --- 14 13 --- 9 | 22 22 --- --- --- 98 --- 15 24 --- 14 6 | 7 12 8 13 29 4 7 8 7 19 3 | 23 28 30 32 23 25 26 25 26 29 24 7E | 10 15 11 14 26 7 19 11 6 14 4 | 16 26 19 20 31 20 23 24 23 22 16 8E | 10 22 11 12 73 7 19 12 8 16 5 | 13 24 19 18 47 16 24 20 26 20 16 9E | 15 24 13 13 64 8 22 14 9 17 5 | 71 75 73 71 76 75 75 77 76 78 73 10E | 11 17 8 12 82 4 15 10 9 22 4 | 27 30 26 27 41 27 24 30 32 23 25 11 | 8 17 11 10 61 6 17 8 9 15 4 | 22 29 21 30 35 22 24 24 27 27 22 12 | 12 22 15 9 28 6 22 14 8 20 5 | 15 33 18 23 39 18 30 18 22 20 17 13 | 8 18 14 12 50 3 22 12 8 23 5 | 8 24 19 24 43 13 25 22 19 19 14 14 | 8 20 10 11 36 4 21 9 10 15 4 | 15 28 26 28 33 20 27 23 26 22 20 15 | 9 23 11 10 29 5 20 15 12 21 5 | 17 23 14 23 31 15 24 24 24 22 17 16 | 9 20 10 11 35 3 23 8 12 23 5 | 16 30 21 25 37 19 31 17 24 20 18 17 | 9 13 11 11 29 6 10 7 15 23 4 | 19 24 24 23 36 22 19 21 30 25 19 18E | 10 19 6 18 26 3 20 9 9 14 4 | 15 25 22 28 37 19 26 18 30 26 20 19 | 11 13 8 19 29 4 13 9 11 37 5 | 19 21 27 34 25 23 21 24 28 29 21 20E | 6 19 12 16 21 4 18 9 8 17 4 | 10 21 16 23 25 11 17 15 20 15 11 21 | 6 19 13 11 34 3 20 11 9 18 4 | 13 23 16 16 38 12 25 17 27 18 15 22E | 8 16 8 12 29 5 21 12 8 10 4 | 20 30 26 28 34 26 30 27 28 28 24 23 | 8 20 15 13 25 5 24 8 7 31 5 | 11 25 18 24 35 13 25 18 19 28 14 24 | 7 13 7 7 22 5 10 9 8 11 3 | 14 18 13 16 17 15 13 20 25 16 15 25 | 12 19 12 12 32 8 16 9 7 27 5 | 63 70 65 67 70 62 71 63 65 66 64 26 | 7 15 7 8 23 4 10 9 9 19 3 | 13 18 15 19 28 15 19 17 25 23 15 27E | 10 31 13 13 54 5 21 13 9 25 6 | 90 94 89 95 100 89 91 86 89 88 89 28 | 9 24 15 17 38 7 20 9 12 18 5 | 15 29 23 21 42 16 27 13 23 14 14 29 | 7 10 8 12 34 4 13 9 8 40 5 | 16 15 21 23 21 18 16 21 26 28 18 30 | 7 12 11 6 20 2 13 9 8 15 3 | 15 16 21 17 28 17 16 18 25 18 15 31E | 6 26 12 14 32 4 18 8 11 16 5 | 19 34 22 24 38 17 24 19 23 22 18 32E | 12 35 13 12 37 4 18 11 13 24 6 | 51 64 51 50 43 49 44 48 43 52 47 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 11 12 40 5 18 10 9 21 |T 23 31 27 29 37 27 29 26 30 28 24 WRMS | 9 19 11 12 38 4 16 10 8 20 |NE 16 23 20 23 31 21 22 20 25 22 17 MEDI | 8 19 11 12 32 4 18 9 9 18 |MD 17 25 21 24 35 19 24 21 25 22 18 Table 3.1534.3 GPS week: 1534 Day: 3 MJD: 54985.000 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 | 22 --- --- --- --- 30 --- 17 22 --- 14 | 25 --- --- --- --- 37 --- 29 33 --- 25 2 | 6 21 10 9 29 9 21 8 9 19 4 | 19 26 17 17 28 21 27 17 25 21 18 3 | 7 8 9 6 36 6 8 8 9 18 3 | 24 29 21 27 20 25 24 28 28 23 24 4 | 6 14 9 7 23 8 9 7 7 12 3 | 21 22 21 19 28 21 25 21 18 26 19 X5 | 19 15 --- --- --- 21 --- 12 12 --- 8 | 24 16 --- --- --- 53 --- 15 19 --- 15 6 | 6 10 8 5 23 5 7 7 8 21 3 | 24 34 31 30 27 29 27 28 26 31 27 7E | 10 18 7 12 29 5 17 16 8 15 4 | 26 33 23 28 29 26 29 28 30 28 25 8E | 9 18 11 10 58 5 19 10 11 19 4 | 18 28 22 23 37 17 30 19 22 22 19 9E | 11 23 14 11 57 7 23 23 12 35 6 | 127 126 130 132 138 125 126 120 125 118 125 10E | 12 15 12 12 92 8 13 9 12 19 4 | 42 39 44 39 56 39 37 42 40 40 39 11 | 5 19 11 6 59 5 17 6 8 16 4 | 26 34 23 28 39 28 29 29 29 31 26 12 | 10 21 9 8 31 8 21 11 7 18 4 | 22 34 28 23 48 23 33 25 25 22 23 13 | 8 23 9 11 56 5 24 19 9 23 5 | 18 32 19 22 42 18 30 27 19 23 18 14 | 7 22 12 12 37 3 21 9 8 15 4 | 19 33 29 26 35 21 28 23 17 20 21 15 | 7 24 11 8 29 4 22 13 16 20 5 | 18 29 26 20 31 21 27 22 30 17 20 16 | 8 20 11 9 31 7 23 7 10 24 5 | 19 33 22 20 45 18 30 18 20 20 19 17 | 8 9 11 9 38 8 10 7 11 22 4 | 24 27 25 25 42 26 26 27 29 29 24 18E | 9 15 9 19 21 3 21 7 9 13 4 | 28 34 32 34 38 29 34 30 27 34 29 19 | 6 10 10 7 22 6 13 7 10 40 4 | 26 27 24 27 28 26 26 29 33 32 26 20E | 5 15 13 11 29 4 17 9 10 17 4 | 14 21 22 16 28 16 21 14 16 19 14 21 | 6 20 9 10 32 4 21 11 9 17 4 | 13 26 13 14 39 13 24 18 18 18 13 22E | 9 18 9 10 33 3 22 8 6 9 4 | 11 27 23 20 31 17 26 15 16 19 15 23 | 7 22 9 12 40 6 23 11 8 31 5 | 15 28 18 19 38 15 25 18 16 28 14 24 | 7 11 5 7 28 4 10 7 8 12 3 | 15 22 18 19 16 17 17 23 20 20 17 25 | 8 19 9 9 31 5 19 11 8 26 4 | 64 67 60 64 56 60 69 64 61 68 62 26 | 7 15 8 7 20 5 9 7 10 17 3 | 13 19 19 17 29 15 19 16 23 22 15 27E | 16 23 11 15 33 4 20 10 9 28 6 | 92 96 90 91 95 92 93 92 96 98 92 28 | 8 22 7 9 36 5 19 7 12 18 4 | 15 31 19 17 44 15 29 16 19 17 16 29 | 8 11 9 10 25 5 13 8 8 39 4 | 18 20 18 21 24 18 19 23 20 29 18 30 | 7 11 8 6 13 4 10 7 8 14 3 | 12 17 16 16 22 16 15 19 16 20 13 31E | 8 26 8 12 28 5 19 9 11 12 4 | 21 38 26 26 35 22 31 25 21 25 22 32E | 10 35 12 20 29 5 19 11 13 25 6 | 77 83 78 83 67 76 77 78 81 78 77 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 11 38 6 18 10 10 22 |T 29 36 31 32 41 31 35 31 31 33 29 WRMS | 7 18 10 11 37 5 16 9 8 20 |NE 19 26 21 21 32 22 25 22 23 23 19 MEDI | 8 18 9 9 31 5 19 9 9 18 |MD 21 29 23 23 35 21 27 23 23 23 20 Table 3.1534.4 GPS week: 1534 Day: 4 MJD: 54986.000 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 | 31 --- --- --- --- 26 --- 13 36 --- 20 | 27 --- --- --- --- 31 --- 17 34 --- 21 2 | 7 23 10 11 31 5 23 8 9 19 4 | 17 29 19 17 25 15 28 17 21 20 16 3 | 6 11 6 8 37 5 9 6 8 20 3 | 18 22 20 21 20 18 20 26 21 21 20 4 | 6 15 10 7 22 4 9 6 9 9 3 | 19 23 27 22 28 18 23 17 17 25 19 X5 | 23 22 --- --- --- 26 --- 10 16 --- 10 | 22 17 --- --- --- 39 --- 14 22 --- 13 6 | 6 13 6 7 36 6 9 7 10 21 3 | 22 28 28 27 28 26 25 27 24 28 24 7E | 8 17 12 22 37 6 18 17 15 17 6 | 22 26 28 35 47 25 26 32 31 33 25 8E | 9 17 11 8 56 4 19 9 11 17 4 | 22 27 24 23 40 22 31 18 23 24 20 9E | 13 26 10 15 24 6 20 10 12 21 5 | 87 91 84 85 100 87 88 90 88 90 87 10E | 11 17 12 9 73 5 14 8 12 18 4 | 21 24 23 20 33 19 23 24 29 18 21 11 | 6 17 11 10 64 3 18 6 7 17 4 | 23 28 26 23 38 22 25 27 30 30 24 12 | 7 25 8 8 25 4 21 8 6 18 4 | 16 37 24 19 33 21 32 20 23 19 21 13 | 8 19 12 11 38 4 24 12 9 19 5 | 13 26 20 18 45 16 29 23 20 17 16 14 | 7 20 12 7 39 4 18 9 10 14 4 | 14 30 26 22 36 20 28 20 20 17 18 15 | 4 22 8 12 28 4 20 8 12 17 4 | 15 27 19 24 30 18 25 17 22 15 17 16 | 8 20 8 9 40 7 22 9 12 20 4 | 15 28 19 16 35 18 28 17 23 17 17 17 | 7 11 10 11 28 6 11 7 14 25 4 | 22 26 27 27 36 23 23 23 24 26 22 18E | 9 19 11 16 25 4 19 8 5 13 4 | 17 25 19 17 31 17 25 16 15 21 13 19 | 7 11 10 15 18 6 15 6 12 40 5 | 21 25 25 26 31 21 23 25 26 26 22 20E | 4 16 10 6 35 6 19 8 6 16 3 | 10 20 15 12 30 11 19 13 13 15 9 21 | 6 19 11 8 24 4 20 8 8 17 4 | 13 24 17 13 32 13 25 16 20 16 14 22E | 10 15 11 8 40 4 19 8 7 10 4 | 13 23 21 22 35 16 25 15 20 19 16 23 | 6 18 10 9 29 6 23 8 9 31 5 | 12 26 16 15 32 12 26 14 15 26 12 24 | 8 12 8 5 29 4 9 6 9 12 3 | 14 17 16 12 17 13 15 18 24 16 15 25 | 8 20 9 8 25 4 16 8 9 25 4 | 42 48 42 41 52 40 48 40 39 48 40 26 | 6 14 10 7 24 2 12 5 6 17 3 | 16 21 21 21 32 16 22 17 22 24 18 27 | 11 18 7 14 30 4 17 8 10 17 4 | 66 80 75 85 88 74 80 75 78 77 76 28 | 7 22 10 9 34 6 20 8 13 17 4 | 15 30 21 18 43 19 28 13 25 17 16 29 | 8 12 13 13 27 6 13 9 7 39 5 | 17 18 20 21 25 16 18 21 22 29 17 30 | 4 11 7 5 19 3 9 8 5 15 2 | 12 14 16 12 25 12 16 16 15 21 12 31E | 6 17 10 8 36 4 16 7 7 13 3 | 10 23 17 10 35 9 21 11 16 12 10 32E | 11 29 10 11 46 6 15 9 10 25 5 | 45 51 47 48 50 47 50 51 51 49 48 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 10 11 36 5 17 8 10 20 |T 22 30 26 25 37 24 29 24 27 27 23 WRMS | 7 18 10 11 36 5 15 7 7 19 |NE 17 24 21 19 31 19 24 19 22 21 17 MEDI | 7 17 10 9 30 4 18 8 9 17 |MD 17 26 21 21 33 18 25 18 22 21 18 Table 3.1534.5 GPS week: 1534 Day: 5 MJD: 54987.000 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 | 26 --- --- --- --- 25 --- 11 31 --- 17 | 28 --- --- --- --- 31 --- 28 41 --- 29 2 | 7 21 10 9 35 4 24 7 10 20 4 | 17 28 15 17 33 13 27 15 20 18 15 3 | 6 11 7 8 28 5 8 9 8 23 3 | 18 19 16 17 13 17 17 21 26 19 18 4 | 4 9 8 8 22 4 11 4 9 10 3 | 16 18 14 18 31 16 21 15 17 23 15 X5 | 17 --- --- --- --- 20 --- 17 13 --- 11 | 15 --- --- --- --- 26 --- 19 17 --- 12 6 | 4 11 8 5 33 4 7 7 12 23 3 | 20 27 27 21 27 23 24 20 23 30 21 7E | 8 16 8 15 34 5 19 11 9 13 4 | 28 30 24 29 32 25 31 29 28 30 26 8E | 12 16 10 11 58 5 19 8 9 14 4 | 25 27 26 27 40 24 32 25 28 24 25 9 | 11 17 9 8 33 4 18 6 9 15 4 | 86 91 90 87 98 85 88 86 94 83 88 10E | 10 13 7 9 55 7 15 6 8 15 3 | 36 37 41 40 54 37 36 40 39 35 38 11 | 8 14 9 9 67 4 17 9 6 19 4 | 22 24 19 26 35 20 23 23 24 26 21 12 | 7 22 8 7 31 4 23 10 7 18 4 | 21 32 26 22 42 23 31 23 24 18 23 13 | 8 19 6 10 43 3 23 13 4 18 4 | 11 25 18 15 46 13 28 19 17 13 14 14 | 6 18 12 8 36 4 20 10 12 14 4 | 14 29 23 19 37 18 26 16 21 14 18 15 | 7 22 7 10 24 3 20 9 9 15 4 | 18 28 19 20 33 17 27 18 23 16 18 16 | 6 18 8 11 40 6 21 7 11 21 4 | 14 31 24 17 45 18 28 15 17 19 17 17 | 10 10 11 6 28 4 12 6 14 24 4 | 18 23 19 20 30 16 20 18 23 21 17 18E | 9 19 10 10 20 4 22 9 8 13 4 | 24 31 29 25 37 25 31 28 28 28 26 19 | 7 11 8 4 40 5 11 8 12 43 5 | 18 20 17 17 29 15 18 18 25 27 16 20E | 6 16 7 11 35 5 20 8 9 11 4 | 10 19 11 15 32 9 18 12 13 13 8 21 | 8 17 8 8 25 5 22 9 7 18 4 | 15 22 17 14 29 13 25 16 22 16 16 22E | 10 17 11 11 27 3 22 10 9 9 4 | 10 25 17 17 29 13 22 10 16 15 12 23 | 8 23 9 11 33 4 25 10 7 33 5 | 10 28 17 17 37 12 25 15 14 27 12 24 | 7 12 6 6 29 3 10 10 6 14 3 | 14 17 14 11 18 12 14 18 19 15 14 25 | 7 19 6 8 37 3 16 9 8 27 4 | 36 44 35 38 51 36 44 37 37 42 36 26 | 5 12 10 4 19 4 11 6 8 17 3 | 14 17 17 13 25 15 20 15 17 25 15 27 | 8 21 8 7 28 5 17 5 8 21 4 | 53 62 60 57 75 57 64 54 61 55 57 28 | 8 18 15 7 37 4 18 8 10 15 4 | 14 28 19 16 43 15 27 13 19 16 15 29 | 7 12 8 8 25 6 14 11 7 39 4 | 13 15 16 12 23 12 13 15 18 27 13 30 | 6 13 8 6 26 3 11 10 8 15 3 | 9 15 15 12 32 11 13 15 18 20 12 31E | 9 17 9 12 23 4 17 9 10 13 4 | 15 26 25 21 33 19 23 19 21 22 18 32E | 10 28 9 9 47 6 19 8 8 22 5 | 79 83 80 80 82 78 78 81 81 80 80 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 17 9 9 36 4 18 9 9 20 |T 23 30 26 25 39 23 29 24 27 27 23 WRMS | 7 17 9 9 33 4 16 8 7 20 |NE 16 23 18 17 32 16 22 17 21 20 16 MEDI | 8 17 8 8 33 4 18 9 9 17 |MD 17 27 19 18 33 17 25 18 22 22 17 Table 3.1534.6 GPS week: 1534 Day: 6 MJD: 54988.000 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 | 30 --- --- --- --- 26 --- 13 34 --- 19 | 27 --- --- --- --- 22 --- 20 32 --- 22 2 | 7 19 8 11 29 6 19 6 7 21 4 | 16 26 15 17 27 15 27 15 18 18 14 3 | 6 11 8 8 35 4 8 9 8 24 3 | 28 36 34 34 18 32 31 35 33 30 31 4 | 6 10 9 13 27 8 9 11 10 15 3 | 19 26 20 23 29 21 24 24 20 27 20 X5 | 14 22 --- --- --- 34 --- 13 15 --- 9 | 11 18 --- --- --- 45 --- 15 23 --- 11 6 | 5 12 7 8 31 4 8 8 8 27 3 | 31 41 41 37 28 35 34 39 34 38 35 7E | 9 16 9 20 33 4 18 12 12 14 5 | 23 30 22 28 32 24 29 28 25 28 23 8E | 17 19 13 18 65 8 21 9 10 17 5 | 31 37 36 43 50 35 35 35 37 41 34 9 | 8 14 9 12 35 6 19 9 9 19 4 | 82 85 83 79 85 82 90 81 87 78 82 10E | 11 13 9 11 77 4 16 9 9 22 4 | 46 45 44 50 42 45 42 51 45 55 45 11 | 9 19 11 8 63 3 20 6 8 20 4 | 29 40 30 31 45 29 30 29 29 34 28 12 | 9 22 11 10 30 4 22 10 10 20 5 | 26 41 33 29 39 27 42 27 27 30 29 13 | 7 16 6 15 39 3 24 11 9 24 5 | 15 28 20 24 38 20 28 22 20 21 17 14 | 7 18 10 13 27 4 21 8 11 14 4 | 16 28 27 29 36 24 28 22 24 17 21 15 | 6 25 12 9 30 5 22 9 13 18 5 | 15 30 22 18 31 14 25 18 24 15 16 16 | 6 19 8 8 29 3 23 9 8 25 4 | 18 33 27 20 39 20 34 17 22 20 20 17 | 9 9 9 15 21 7 11 11 18 24 5 | 32 37 38 35 40 33 32 33 35 32 32 18E | 9 17 8 13 21 6 19 8 9 16 4 | 21 26 28 23 31 24 28 20 26 31 23 19 | 7 10 7 8 47 4 15 8 12 42 4 | 29 33 32 33 40 30 28 32 33 37 30 20E | 5 14 7 11 32 4 17 7 6 12 3 | 9 18 11 13 26 9 17 11 12 13 8 21 | 9 19 7 8 25 6 21 11 9 19 4 | 16 25 16 13 35 13 27 18 24 20 16 22E | 11 18 9 14 33 5 20 13 7 12 5 | 17 29 25 24 29 22 27 22 26 26 21 23 | 7 17 8 12 29 4 25 8 11 34 5 | 14 26 19 20 33 17 25 19 19 29 15 24 | 8 13 6 7 23 6 8 10 7 13 3 | 18 21 17 16 18 15 18 23 20 21 17 25 | 7 21 6 9 31 5 15 9 11 27 4 | 67 68 63 68 70 63 68 65 63 68 64 26 | 6 12 9 4 25 4 11 6 9 21 3 | 15 16 17 15 27 16 20 17 21 22 15 27 | 7 15 7 9 25 6 17 8 9 20 4 | 68 74 73 70 79 69 80 68 73 73 71 28 | 7 17 12 9 32 6 19 12 15 14 4 | 14 25 17 18 44 17 27 17 23 15 15 29 | 6 12 8 8 35 6 13 13 8 38 4 | 22 22 22 26 36 22 22 27 26 35 22 30 | 6 11 6 7 18 5 12 10 11 17 3 | 13 14 16 17 23 14 15 19 20 23 14 31E | 5 20 6 12 32 5 16 11 9 16 4 | 13 28 17 15 31 12 24 16 15 18 14 32E | 10 26 7 13 38 7 19 8 8 27 5 | 107 103 107 109 95 102 101 105 103 97 104 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 17 9 11 36 5 18 10 10 22 |T 28 35 32 32 39 30 35 30 32 33 29 WRMS | 7 17 8 11 34 5 16 9 7 22 |NE 20 28 24 23 32 22 27 23 25 25 20 MEDI | 7 17 8 10 31 5 18 9 9 20 |MD 19 29 25 24 35 22 28 22 25 28 21 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 4.1534 GPS week: 1534 MJD: 54982.0-54988.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3048 |U 8 7 21 |U 6 8 24 |U 8 9 20 | emr | emr 2928 | 12 11 27 | 10 10 42 |U 8 9 21 | esa | esa 2880 | 8 8 22 |U 5 8 24 | 7 9 19 | gfz | gfz 2842 |U 16 22 37 |U 16 19 56 | 14 15 32 | grg | grg 2880 | 9 9 25 |U 8 8 29 | 12 10 28 | igr | igr 2855 | 8 7 22 | 7 11 26 | 8 8 20 | igs | igs 2924 | 8 7 22 | 7 10 31 | 7 8 18 | jpl | jpl 2862 | 9 8 24 |U 10 11 52 |U 8 8 19 | mit | mit 3058 |U 8 8 22 |U 12 19 49 |U 10 13 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 5.1534.0 GPS week: 1534 Day: 0 MJD: 54982.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3055 | 7 6 15 | 6 9 23 | 10 9 18 | emr | emr 2949 | 9 7 24 | 8 10 30 | 9 9 14 | esa | esa 2880 | 7 5 17 | 5 8 22 | 8 9 20 | gfz | gfz 2837 | 7 6 22 | 14 16 40 | 8 9 21 | grg | grg 2880 | 8 8 19 | 6 9 31 | 10 9 25 | igr | igr 2810 | 7 5 18 | 5 11 22 | 9 8 17 | igs | igs 2936 | 7 5 19 | 8 13 28 | 8 9 17 | jpl | jpl 2859 | 8 6 20 | 14 12 77 | 9 9 16 | mit | mit 3072 | 8 6 18 | 11 13 43 | 11 10 21 | Table 5.1534.1 GPS week: 1534 Day: 1 MJD: 54983.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3053 | 12 11 31 | 8 10 23 | 7 6 17 | emr | emr 2860 | 13 14 34 | 8 8 24 | 8 8 22 | esa | esa 2880 | 12 12 28 | 7 9 23 | 6 6 18 | gfz | gfz 2837 | 12 12 32 | 12 10 40 | 9 10 30 | grg | grg 2880 | 12 11 33 | 9 8 21 | 11 7 25 | igr | igr 2896 | 11 11 28 | 7 8 23 | 7 6 20 | igs | igs 2832 | 12 12 30 | 7 7 22 | 6 5 16 | jpl | jpl 2858 | 12 12 29 | 12 11 57 | 6 4 18 | mit | mit 2976 | 11 11 28 | 10 17 50 | 7 6 18 | Table 5.1534.2 GPS week: 1534 Day: 2 MJD: 54984.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3044 | 8 7 19 | 5 8 22 | 5 6 14 | emr | emr 2959 | 11 10 23 | 8 10 34 | 7 9 20 | esa | esa 2880 | 8 8 23 | 4 6 24 | 5 7 13 | gfz | gfz 2839 | 8 8 26 | 12 12 44 | 5 5 12 | grg | grg 2880 | 8 7 24 | 7 7 30 | 9 8 26 | igr | igr 2822 | 8 6 20 | 6 10 25 | 5 7 12 | igs | igs 2974 | 8 7 20 | 5 8 23 | 6 7 13 | jpl | jpl 2861 | 9 8 21 | 12 11 65 | 6 7 15 | mit | mit 3072 | 8 7 19 | 11 23 44 | 11 21 22 | Table 5.1534.3 GPS week: 1534 Day: 3 MJD: 54985.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3059 | 7 10 17 | 6 12 20 | 8 9 26 | emr | emr 2954 | 13 15 24 | 9 12 31 | 8 11 24 | esa | esa 2880 | 8 11 18 | 6 8 25 | 7 9 22 | gfz | gfz 2842 | 66 105 103 | 40 53 143 | 55 53 100 | grg | grg 2880 | 8 13 22 | 9 11 27 | 11 13 27 | igr | igr 2840 | 7 11 18 | 7 10 24 | 7 8 24 | igs | igs 3002 | 7 11 19 | 7 14 24 | 7 8 21 | jpl | jpl 2865 | 9 13 21 | 11 14 57 | 7 10 22 | mit | mit 3072 | 7 10 18 | 11 14 59 | 10 11 35 | Table 5.1534.4 GPS week: 1534 Day: 4 MJD: 54986.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3035 | 8 4 19 | 5 7 29 | 9 13 23 | emr | emr 2958 | 13 11 32 | 7 8 31 | 11 8 20 | esa | esa 2880 | 9 6 23 | 5 5 24 | 8 10 21 | gfz | gfz 2847 | 8 5 28 | 13 12 39 | 8 11 18 | grg | grg 2880 | 11 9 24 | 9 7 35 | 13 10 33 | igr | igr 2871 | 10 6 26 | 6 9 25 | 10 10 24 | igs | igs 2955 | 8 4 22 | 9 7 46 | 9 9 20 | jpl | jpl 2867 | 9 6 26 | 10 9 48 | 8 7 19 | mit | mit 3072 | 10 8 30 | 14 31 61 | 11 14 28 | Table 5.1534.5 GPS week: 1534 Day: 5 MJD: 54987.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3045 | 8 7 20 | 5 7 26 | 8 12 25 | emr | emr 2868 | 10 8 22 | 13 14 75 | 8 11 28 | esa | esa 2880 | 6 7 19 | 6 8 31 | 8 12 22 | gfz | gfz 2844 | 7 9 23 | 12 15 45 | 9 11 22 | grg | grg 2880 | 7 8 23 | 8 10 34 | 14 16 30 | igr | igr 2870 | 7 6 18 | 8 13 31 | 8 11 23 | igs | igs 2865 | 7 6 19 | 9 10 51 | 7 10 21 | jpl | jpl 2863 | 8 7 20 | 7 11 31 | 8 11 25 | mit | mit 3072 | 6 5 18 | 11 18 42 | 12 16 41 | Table 5.1534.6 GPS week: 1534 Day: 6 MJD: 54988.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3049 | 7 7 24 | 5 7 23 | 9 8 20 | emr | emr 2954 | 13 9 28 | 14 12 67 | 8 8 21 | esa | esa 2880 | 8 6 24 | 5 8 21 | 9 8 19 | gfz | gfz 2848 | 7 6 24 | 12 13 41 | 9 7 19 | grg | grg 2880 | 11 9 28 | 8 7 25 | 13 8 28 | igr | igr 2881 | 8 7 25 | 10 14 32 | 9 9 22 | igs | igs 2907 | 8 6 24 | 7 11 27 | 8 7 18 | jpl | jpl 2867 | 10 8 29 | 7 10 27 | 9 8 20 | mit | mit 3072 | 7 6 25 | 12 14 45 | 9 13 31 | Table 6: Earth Orientation Parameters weekly summary. Weekly mean and standard deviation of Centre ERP, ERP rates and LOD differences with respect to IGS combined values. See Table 7 for the daily summaries. Xpole,Xrt: x pole and x pole rate Ypole,Yrt: y pole and y pole rate LOD : Length Of Day AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A AC LOD BIAS RMS: RMS of AC LOD BIAS FLAG: "u" (used), "x" (excluded), "-" (no submission) for Xpole, Ypole, Xrt, Yrt and LOD Table 6.1534 GPS week: 1534 MJD: 54982.500-54988.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 7 8 51 -87 9 | -2 22 | 22 29 93 133 5 | 3 emr uuuuu | 23 36 172 5 -18 | 25 43 | 19 31 105 63 4 | 6 esa uuuuu | -43 -27 -7 110 3 | 1 16 | 36 24 148 179 3 | 1 gfz uuuuu | 3 -32 55 -88 0 | 22 31 | 15 17 36 67 9 | 2 grg xxxxx | -3 -45 12 -98 0 | 4 29 | 34 37 80 61 26 | 7 igr xxxxx | 22 -1 6 2 9 | -4 19 | 19 23 49 62 7 | 3 irf xxxxx | 1 19 25 -4 -2 | -5 27 | 7 8 13 17 6 | 2 jpl uuuuu | -19 19 34 20 1 | -5 31 | 25 18 107 98 9 | 3 mit uuuuu | 14 12 -66 9 -10 | 4 32 | 12 16 70 76 7 | 4 ngs uuuuu | 23 -15 14 6 3 | 3 18 | 54 22 75 83 4 | 2 sio uuuuu | 13 98 -222 -164 -22 | 54 63 | 28 14 131 55 9 | 8 Table 7.1534.0 GPS week: 1534 Day: 0 MJD: 54982.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -22 27 119 99 8 | -6 22 emr uuuuu | 6 1 86 23 -17 | 27 45 esa uuuuu | -36 -24 146 133 1 | 1 15 gfz uuuuu | 13 -23 2 55 10 | 18 27 grg xxxxx | -47 -12 103 -27 -6 | -4 41 igr xxxxx | 19 -12 29 -63 4 | -10 22 irf xxxxx | 6 24 13 -13 -7 | -6 27 jpl uuuuu | 24 -7 123 -21 0 | -10 35 mit uuuuu | 27 26 -132 -105 -14 | 4 32 ngs uuuuu | -16 -5 -23 -18 4 | 0 19 sio uuuuu | 28 96 -341 -238 -31 | 62 69 Table 7.1534.1 GPS week: 1534 Day: 1 MJD: 54983.500 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 -49 39 -39 15 | -4 24 emr uuuuu | 34 0 216 -48 -15 | 29 46 esa uuuuu | -30 -33 108 248 0 | 2 16 gfz uuuuu | -20 -64 82 -140 7 | 20 31 grg xxxxx | 0 -103 98 -86 24 | -5 41 igr xxxxx | 62 6 95 40 13 | -8 23 irf xxxxx | 1 27 20 3 -7 | -4 28 jpl uuuuu | -26 7 159 -39 3 | -6 35 mit uuuuu | 17 32 -132 -3 -15 | 7 33 ngs uuuuu | 11 0 -60 -48 8 | 0 20 sio uuuuu | 26 118 -385 -179 -30 | 61 68 Table 7.1534.2 GPS week: 1534 Day: 2 MJD: 54984.500 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 42 75 -270 4 | -1 22 emr uuuuu | 54 26 244 -91 -23 | 31 46 esa uuuuu | 18 -10 132 183 9 | 2 16 gfz uuuuu | 20 -23 47 -121 5 | 23 32 grg xxxxx | 10 -16 -92 -202 35 | -1 40 igr xxxxx | 19 26 -1 -44 3 | -4 19 irf xxxxx | 6 25 16 -31 -9 | -2 27 jpl uuuuu | -3 4 -63 -9 -7 | -3 32 mit uuuuu | 3 25 -92 -20 -18 | 8 32 ngs uuuuu | -60 -41 -28 59 2 | 2 19 sio uuuuu | 24 95 -276 -160 -31 | 59 67 Table 7.1534.3 GPS week: 1534 Day: 3 MJD: 54985.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 10 14 -14 2 13 | -1 22 emr uuuuu | 24 33 142 -27 -23 | 29 46 esa uuuuu | -32 10 36 347 0 | 0 17 gfz uuuuu | -18 -41 50 -133 2 | 23 32 grg xxxxx | -43 -66 -59 -98 0 | 10 24 igr xxxxx | 12 4 27 -40 6 | -3 18 irf xxxxx | 9 20 16 8 2 | -3 28 jpl uuuuu | -12 36 -97 -54 -5 | -1 29 mit uuuuu | 22 5 -127 32 -5 | 7 33 ngs uuuuu | 3 -42 130 -145 7 | 3 18 sio uuuuu | 49 96 -274 -152 -18 | 56 66 Table 7.1534.4 GPS week: 1534 Day: 4 MJD: 54986.500 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 | 24 4 -104 -249 4 | 1 21 emr uuuuu | 24 38 344 27 -20 | 27 46 esa uuuuu | -87 -21 -194 105 4 | 0 17 gfz uuuuu | 5 -33 25 -75 -5 | 25 32 grg xxxxx | 48 -49 52 -40 0 | 6 22 igr xxxxx | 18 18 -27 98 3 | -2 17 irf xxxxx | -7 21 41 -18 0 | -3 28 jpl uuuuu | -26 30 140 107 -3 | -2 30 mit uuuuu | -4 9 18 -45 -11 | 6 33 ngs uuuuu | 77 -30 -28 39 5 | 4 17 sio uuuuu | 11 114 -159 -220 -20 | 53 64 Table 7.1534.5 GPS week: 1534 Day: 5 MJD: 54987.500 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 | 14 19 185 -44 12 | 0 20 emr uuuuu | -3 73 29 82 -18 | 21 40 esa uuuuu | -84 -63 -89 -158 5 | 0 17 gfz uuuuu | 7 -8 109 -102 -15 | 23 31 grg xxxxx | 23 0 -54 -80 -9 | 10 20 igr xxxxx | 3 -1 -35 56 12 | -3 17 irf xxxxx | -10 6 45 20 4 | -6 26 jpl uuuuu | -34 39 -48 203 19 | -7 26 mit uuuuu | 7 -13 12 96 -4 | 1 30 ngs uuuuu | 94 10 -4 57 -3 | 5 18 sio uuuuu | -31 79 -62 -79 -12 | 46 57 Table 7.1534.6 GPS week: 1534 Day: 6 MJD: 54988.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 23 -2 56 -106 5 | 1 20 emr uuuuu | 19 78 142 70 -11 | 14 35 esa uuuuu | -53 -49 -188 -89 4 | 2 16 gfz uuuuu | 10 -31 68 -98 -5 | 20 29 grg xxxxx | -11 -70 38 -151 -46 | 12 18 igr xxxxx | 17 -46 -47 -34 22 | -1 16 irf xxxxx | -1 13 27 3 6 | -8 26 jpl uuuuu | -55 23 24 -50 1 | -7 26 mit uuuuu | 25 0 -8 109 0 | -3 28 ngs uuuuu | 51 2 111 100 1 | 4 18 sio uuuuu | -18 89 -58 -120 -13 | 41 51