From IGS.ACC at noaa.gov Thu Jan 22 04:54:19 2009 From: IGS.ACC at noaa.gov (Jim Ray) Date: Thu, 22 Jan 2009 12:54:19 +0000 Subject: [IGSREPORT-17039] Wk 1513 IGS Final Orbits Message-ID: <49786c7b.eHfXiOBR5tfT519L%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 22 Jan 04:54:22 PST 2009 Message Number 17039 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1513 (Jan 04, 2009 - Jan 10, 2009) Contacts: J. Ray (jim.ray at noaa.gov), J. Griffiths (jake.griffiths at 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: igs1513[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1513[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1513[0-6].cls IGS GPS clock combination summary report. igs15137.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15137.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 | 5 10 30 0 | EMR | KHAJ MIZU 0 | ESA | 5 10 30 0 | GFZ | 7 18 29 30 32 FAA1 0 | JPL | 32 ZWE2 0 | MIT | 32 ALIC 1 | COD | 5 30 1 | ESA | 5 30 1 | GFZ | 7 18 29 32 DAEJ FAA1 TIDB 1 | JPL | 32 ZWE2 1 | MIT | 32 DAEJ HRAO 2 | COD | 5 30 2 | EMR | MIZU NYAL 2 | ESA | 5 30 ALGO 2 | GFZ | 5 7 16 21 29 32 ALGO PETP 2 | JPL | 5 32 NYAL 2 | MIT | 21 32 REUN 3 | COD | 5 30 3 | EMR | MIZU THU3 3 | ESA | 5 30 3 | GFZ | 7 29 32 GUAT TWTF 3 | JPL | 5 32 BOR1 THU3 3 | MIT | 7 11 15 26 32 BOR1 DAEJ HRAO 4 | ALL | 15 4 | COD | 5 30 4 | EMR | KHAJ MIZU YELL 4 | ESA | 5 9 30 32 AREQ SCH2 4 | GFZ | 7 29 32 IRKT 4 | JPL | 30 AREQ YELL 4 | MIT | 2 3 11 32 DARW 5 | COD | 5 30 5 | EMR | DAEJ MIZU YELL 5 | ESA | 5 30 UNSA 5 | GFZ | 7 29 FAA1 ONSA PETP RAMO 5 | JPL | ZWE2 6 | COD | 5 30 NISU 6 | EMR | MIZU SUTM 6 | ESA | 5 30 6 | GFZ | 7 12 29 DAEJ IRKT 6 | JPL | 5 6 | MIT | 7 DAEJ DARW 5. The following table lists all maneuvered satellites for this week. The solutions from COD and ESA, which modeled the maneuver, are used that day for combination. An associated accuracy code of 0 (unknown) is given if only one AC is left (no redundancy). For the long arc evaluation the arc is split into two parts at the given maneuver epoch. PRN | Date | Ref. NANU ----+------------+---------- G15 | 2009_01_08 | 2009002 G15 | 2009_01_09 | 2009002 6. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447. 7. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | -.2 .3 .7 -25 -16 -17 .14 EMR | 6.9 4.7 -4.7 131 -35 -4 .59 ESA | 1.3 7.3 -5.4 49 -59 26 .19 GFZ | .8 .1 1.8 13 -24 17 -.06 GRG | 1.9 2.3 -6.5 -17 -9 2 .08 JPL | .4 2.4 11.5 19 -21 17 .39 MIT | -1.2 1.2 -19.5 -4 -5 -10 .08 NGS | 6.5 -2.1 -9.6 -28 -165 31 .08 SIO | -1.0 4.9 8.8 84 69 -1 .19 8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 10. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five parts. The first, Table 1, summarizes all statistics for the week. It contains means and standard deviations over the week of satellite ephemeris and clock correction transformation parameters for each centre (table 1.1513.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1513.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 2.1513.[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 3.1513.[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 5.1513.0-6). 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 1513 summary. (Jan 04, 2009 - Jan 10, 2009) Table 1.1513.a GPS week: 1513 MJD: 54835.000-54841.000 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 242| 0 0 3 76 -42 -30 -.17 9 8 | -159 -513 12 87 | 0 0 1 14 10 21 .02 | 343 558 emr 76| 1 0 5 -226 -3 -44 .43 19 19 | 1939 -312 18 157 | 1 2 1 31 37 17 .05 | 1441 2531 esa 139| 0 -1 -1 -36 10 -15 .27 9 9 | 153 -251 18 108 | 0 0 2 22 37 12 .02 | 766 1806 gfz 195| 0 0 -6 -10 -36 140 -.13 10 10 | 291 -289 22 124 | 0 0 1 18 15 72 .03 | 262 331 grg 81| 1 -1 0 69 -74 -92 1.19 41 40 | -153 -554 105 381 | 1 3 5 28 48 67 .12 | 345 559 igr n/a| 0 0 0 18 -67 -44 .05 5 5 | 16877 -1570 20 81 | 0 0 0 11 32 20 .06 | 3218 2427 jpl 138| 0 0 8 -21 -35 -13 .54 17 16 | 3046 -333 19 97 | 2 1 1 11 25 25 .03 | 1356 2330 mit 276| -1 1 -5 51 -97 -14 -.30 13 12 | -19 -105 24 142 | 0 1 1 33 47 18 .01 | 644 878 ngs 229| 0 0 0 94 274 -61 -.25 11 9 | -138 -540 2284 3908 | 0 0 0 26 60 28 .04 | 366 604 sio 254| 0 0 4 -147 -248 -8 .03 23 21 | --- --- --- --- | 1 1 2 30 41 12 .02 | --- --- Table 1.1513.b GPS week : 1513 MJD: 54835.000-54841.000 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 --- --- --- --- | 2 | 5 5 5 5 5 5 4 | 3 | 5 4 4 4 4 4 5 | 4 | 5 5 5 4 4 5 4 | 5 | 5 5 5 5 5 5 6 | 6 | 4 3 4 4 4 4 5 | 7 | 5 5 5 5 5 5 5 | 8 | 6 5 4 4 4 4 4 | 9 | 4 4 4 4 6 4 4 | 10 | 6 7 6 5 5 5 5 | 11 | 5 5 4 5 5 5 5 | 12 | 6 5 5 5 5 5 5 | 13 | 4 4 4 5 4 4 4 | 14 | 5 6 5 5 5 5 5 | 15 | 6 5 5 5 6 0 6 | 16 | 8 6 6 6 6 6 6 | 17 | 6 5 6 5 6 6 6 | 18 | 6 6 7 5 5 5 5 | 19 | 5 5 5 6 6 6 5 | 20 | 5 4 4 5 5 5 5 | 21 | 5 5 5 4 5 5 5 | 22 | 5 5 5 5 4 5 5 | 23 | 5 5 5 5 5 5 6 | 24 | 3 3 3 3 4 4 4 | 25 | 4 4 4 4 4 5 5 | 26 | 5 5 4 4 5 5 4 | 27 | 6 5 5 5 4 4 4 | 28 | 5 5 4 5 5 5 5 | 29 | 5 5 5 5 6 5 5 | 30 | 6 5 6 6 6 6 6 | 31 | 6 5 5 5 5 5 5 | 32 | 6 6 6 6 7 8 6 | 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 2.1513.0 GPS week: 1513 Day: 0 MJD: 54835.000 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 242| 0 1 2 81 -41 -29 -.16 10 9 | 13 -449 13 98 | 38 -30 | emr 76| 1 0 9 -264 25 -60 .44 20 19 | 1962 -63 19 204 | 65 -59 | esa 139| 1 -1 0 -65 -41 -23 .26 10 10 | -54 466 20 101 | 47 8 | gfz 195| 0 0 -6 -30 -42 226 -.10 14 13 | 321 -539 25 123 | 54 -53 | grg 81| 1 -6 9 70 -139 -73 1.27 45 43 | 8 -497 111 416 | 32 -138 | igr n/a| 0 0 0 26 -38 -56 .12 7 7 | 19752 -719 21 69 | -53 -34 | jpl 138| -2 1 7 -25 -47 2 .49 18 18 | 2012 238 22 99 | -10 -2 | mit 276| 0 0 -4 94 -195 -8 -.29 12 10 | 46 -360 22 125 | -11 33 | ngs 229| 0 0 0 100 394 -80 -.23 10 8 | 65 -520 2343 4029 | -30 -186 | sio 254| 0 0 3 -117 -328 -25 .04 25 20 | --- --- --- --- | 41 147 | Table 2.1513.1 GPS week: 1513 Day: 1 MJD: 54836.000 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 242| 0 0 2 95 -55 -50 -.12 10 8 | 349 -1177 12 83 | -26 10 | emr 76| 1 4 6 -262 -10 -42 .49 19 19 | 3231 -2186 18 141 | 78 -14 | esa 139| 0 0 -2 -45 -26 -32 .30 9 9 | -789 2474 18 116 | 8 -6 | gfz 195| 1 0 -3 -35 -14 214 -.15 10 10 | 407 -89 22 126 | 29 -33 | grg 81| 1 -1 5 99 -146 -55 1.20 41 41 | 360 -1217 107 529 | -39 21 | igr n/a| 0 0 1 26 -122 -51 .14 6 6 | 20526 -3034 19 69 | -22 34 | jpl 138| 0 0 8 -10 -76 -47 .53 16 16 | 3851 -1829 19 105 | -43 -24 | mit 276| -1 0 -4 27 -85 -34 -.29 13 11 | 478 -450 21 126 | 9 7 | ngs 229| 0 0 0 130 286 -67 -.25 10 8 | 415 -1344 2600 4159 | -73 -21 | sio 254| -2 0 2 -176 -232 -28 .04 24 23 | --- --- --- --- | 49 136 | Table 2.1513.2 GPS week: 1513 Day: 2 MJD: 54837.000 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 242| 1 0 3 83 -50 -37 -.18 10 8 | -385 -611 16 96 | 16 22 | emr 76| -1 1 4 -251 -34 -69 .42 19 19 | 308 2522 16 136 | 51 18 | esa 139| 0 0 0 -51 23 -25 .26 9 9 | 724 -2208 17 106 | 18 -29 | gfz 195| 0 0 -5 9 -23 200 -.14 10 10 | -91 -74 21 123 | 15 -3 | grg 81| 0 -2 -3 41 -38 -133 1.08 42 40 | -379 -659 104 356 | 86 57 | igr n/a| 0 -1 1 -1 -98 -40 .04 5 4 | 17090 1107 18 95 | 21 9 | jpl 138| 1 1 7 -35 -47 -36 .57 16 15 | 1899 2432 17 95 | -13 4 | mit 276| -1 1 -5 94 -75 -28 -.32 12 11 | -895 722 27 132 | -9 11 | ngs 229| 1 0 0 52 227 -61 -.25 10 9 | -409 -492 1975 3581 | 35 -16 | sio 254| 0 0 2 -103 -210 -5 .01 22 21 | --- --- --- --- | 42 109 | Table 2.1513.3 GPS week: 1513 Day: 3 MJD: 54838.000 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 242| 0 0 5 88 -22 -50 -.16 10 9 | -372 -383 11 75 | -47 11 | emr 76| 0 0 7 -216 -48 -44 .46 19 19 | 2421 1549 19 145 | 41 44 | esa 139| 1 0 -4 -47 51 -12 .28 9 9 | 761 -479 19 97 | -4 -31 | gfz 195| 0 0 -6 11 -36 106 -.08 9 9 | 285 -243 22 124 | -15 2 | grg 81| 2 -5 -5 95 -54 -119 1.12 41 39 | -365 -418 107 362 | 13 -1 | igr n/a| 1 0 0 28 -35 -16 .05 5 5 | 17771 -12 21 73 | -34 -31 | jpl 138| 2 0 9 -2 -38 6 .52 16 15 | 4010 1253 20 100 | -22 23 | mit 276| -1 1 -5 52 -109 14 -.31 12 11 | 13 -139 30 160 | 0 -2 | ngs 229| 0 0 0 88 264 -76 -.34 11 9 | -342 -457 2009 3765 | 72 -41 | sio 254| -1 0 5 -164 -258 0 .02 21 20 | --- --- --- --- | 49 118 | Table 2.1513.4 GPS week: 1513 Day: 4 MJD: 54839.000 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 242| 0 0 6 55 -36 11 -.17 9 8 | -298 -160 11 103 | 23 22 | emr 76| 2 2 3 -194 -37 -17 .41 20 20 | 3323 -2611 17 165 | 33 47 | esa 139| 0 -1 -4 -29 56 -7 .24 10 10 | 221 -735 19 113 | -7 -14 | gfz 195| 0 -2 -6 -3 -29 113 -.12 10 10 | 663 -760 22 127 | 14 7 | grg 81| -1 2 -1 35 -25 24 1.08 40 39 | -283 -198 109 307 | 21 59 | igr n/a| 0 0 0 27 -57 -44 .00 5 5 | 17092 -4105 22 104 | 1 28 | jpl 138| 3 -1 9 -28 -29 -32 .54 16 16 | 4520 -2622 19 105 | 48 34 | mit 276| 0 2 -6 60 -59 -23 -.32 12 11 | 715 -1229 26 157 | 12 -31 | ngs 229| -1 0 0 101 238 -98 -.22 13 11 | -299 -63 2242 3687 | 47 58 | sio 254| 0 0 8 -131 -220 0 .02 21 20 | --- --- --- --- | 23 107 | Table 2.1513.5 GPS week: 1513 Day: 5 MJD: 54840.000 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 242| 0 0 4 62 -46 -41 -.19 9 8 | 176 -1200 14 83 | 2 47 | emr 76| 1 1 3 -196 34 -40 .45 21 21 | 2713 -3680 20 169 | 14 -26 | esa 139| 0 -1 0 0 12 4 .28 8 8 | 1076 -2541 20 117 | -29 -14 | gfz 195| 0 -1 -6 -13 -46 69 -.15 9 9 | 460 -519 24 127 | 18 38 | grg 81| 3 2 -2 47 -61 -107 1.21 39 40 | 184 -1240 97 390 | 21 63 | igr n/a| 0 0 0 13 -61 -79 -.01 6 5 | 15063 -4934 22 73 | 12 10 | jpl 138| -1 -2 10 -29 -11 -8 .56 18 18 | 3990 -3546 22 94 | 8 -66 | mit 276| -2 2 -6 10 -53 -25 -.30 15 14 | 395 -655 24 158 | 28 -38 | ngs 229| 0 0 -1 113 217 -24 -.24 12 10 | 194 -1258 2362 4027 | -25 26 | sio 254| 0 3 7 -185 -220 -4 .04 24 22 | --- --- --- --- | 38 108 | Table 2.1513.6 GPS week: 1513 Day: 6 MJD: 54841.000 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 242| 1 0 1 68 -42 -18 -.20 8 7 | -598 384 11 72 | -6 25 | emr 76| 2 -3 5 -200 43 -35 .34 18 18 | -382 2284 19 140 | 18 -36 | esa 139| 0 -2 2 -13 -5 -8 .25 8 8 | -868 1260 17 107 | -22 -8 | gfz 195| -1 0 -8 -14 -59 51 -.17 10 10 | -2 195 22 121 | 7 40 | grg 81| 4 -1 1 98 -54 -186 1.40 40 40 | -601 345 105 310 | 17 -14 | igr n/a| 0 0 0 12 -54 -23 -.00 5 5 | 10845 701 19 88 | 29 12 | jpl 138| -1 1 7 -17 0 21 .55 17 16 | 1044 1741 18 84 | 40 -23 | mit 276| 0 3 -7 22 -103 5 -.30 14 14 | -890 1375 24 137 | 15 -26 | ngs 229| 0 0 0 71 292 -22 -.20 11 9 | -595 350 2463 4111 | 36 -29 | sio 254| -1 1 5 -152 -267 2 .07 24 23 | --- --- --- --- | 38 103 | 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 3.1513.0 GPS week: 1513 Day: 0 MJD: 54835.000 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 | 32 --- --- --- --- 41 --- --- --- --- 36 2 | 8 19 9 14 40 8 20 12 11 29 5 | 27 39 29 33 47 30 39 24 33 28 31 3 | 11 15 6 12 59 5 13 15 10 21 4 | 29 32 34 35 39 30 33 28 29 26 30 4 | 8 15 9 11 49 7 12 13 7 39 5 | 35 39 39 40 27 38 36 31 42 36 38 5E | 12 17 8 12 69 8 18 13 11 24 5 | 35 34 32 37 29 33 30 37 41 25 36 6 | 8 16 6 9 50 5 12 8 8 20 3 | 40 42 44 47 43 43 46 37 46 48 44 7 | 9 18 9 16 30 5 15 10 9 27 5 | 18 29 16 23 42 21 27 16 25 26 21 8 | 10 16 11 13 22 6 15 19 11 23 5 | 20 27 20 21 35 19 26 21 22 25 20 9 | 9 14 10 7 32 7 15 11 10 17 4 | 23 26 22 20 24 23 25 23 29 27 25 10E | 15 19 11 16 32 8 18 18 10 30 6 | 86 88 90 84 94 89 91 88 92 99 90 11 | 5 17 11 11 81 7 19 11 6 33 5 | 38 40 36 41 55 34 35 37 35 34 35 12E | 9 24 11 20 35 6 25 10 11 16 5 | 24 32 28 31 33 29 32 30 31 29 30 13 | 6 18 8 8 36 6 14 9 9 25 4 | 17 29 20 18 49 20 27 14 21 21 21 14 | 10 24 13 10 44 9 20 9 10 21 5 | 19 32 25 20 41 21 27 21 29 24 25 15 | 9 24 11 8 22 6 22 10 14 29 5 | 22 30 23 18 32 22 27 16 22 18 24 16E | 12 33 11 43 48 6 24 11 11 18 8 | 17 31 21 48 41 19 27 13 21 25 22 17 | 9 18 11 18 58 6 18 8 10 41 5 | 32 39 36 42 43 33 39 31 40 51 37 18E | 11 22 12 20 50 8 22 8 7 24 5 | 28 39 32 34 33 28 35 31 33 32 32 19 | 8 15 10 11 47 5 18 12 12 27 5 | 18 30 19 17 38 20 28 21 23 18 19 20 | 9 21 12 10 36 6 15 7 10 14 4 | 19 29 18 18 29 19 25 16 26 23 21 21 | 11 17 8 9 62 5 18 6 9 30 4 | 27 35 24 26 60 26 34 22 30 22 28 22E | 11 18 10 15 34 7 20 11 8 20 5 | 23 32 22 29 30 22 30 26 28 30 26 23 | 10 21 8 12 31 6 17 13 11 15 4 | 20 31 23 20 41 22 31 20 27 24 25 24 | 7 11 7 4 60 5 12 8 7 17 3 | 33 32 35 31 35 33 31 34 39 29 36 25 | 8 14 8 10 33 7 12 11 8 20 4 | 20 24 17 17 28 20 25 18 25 21 22 26 | 9 15 10 8 16 7 13 10 11 36 5 | 23 30 23 23 30 24 28 19 30 38 26 27 | 12 14 12 12 20 6 15 20 11 25 5 | 21 24 20 19 30 20 24 20 23 25 20 28E | 11 19 12 9 40 4 20 9 11 13 4 | 15 29 22 18 48 21 29 17 24 23 22 29 | 11 21 10 9 29 8 19 14 9 26 5 | 31 32 29 29 37 28 31 36 33 34 32 30E | 13 20 8 12 66 7 19 18 10 20 5 | 47 45 46 50 53 45 47 53 51 38 48 31 | 12 30 14 8 29 6 22 8 12 24 5 | 21 37 29 23 43 24 27 21 30 26 25 32E | 16 24 11 14 57 12 20 11 12 23 5 | 72 81 71 71 100 72 79 71 72 76 74 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 20 10 14 45 7 18 12 10 25 |T 29 36 30 31 42 30 34 28 33 32 31 WRMS | 9 19 10 13 43 7 18 10 8 20 |NE 25 32 26 26 38 26 30 23 29 28 27 MEDI | 9 18 10 11 40 6 18 11 10 24 |MD 23 32 25 29 39 24 30 23 30 26 26 Table 3.1513.1 GPS week: 1513 Day: 1 MJD: 54836.000 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 | 7 --- --- --- --- 26 --- --- --- --- 0 | 20 --- --- --- --- 35 --- --- --- --- 20 2 | 8 18 11 8 37 7 17 13 13 27 5 | 18 34 25 24 40 23 30 19 23 23 22 3 | 9 13 8 5 47 6 9 9 9 18 3 | 25 32 33 29 36 31 34 26 31 27 28 4 | 10 14 9 7 56 7 10 14 8 29 4 | 24 29 31 24 36 25 25 25 27 34 25 5E | 12 19 9 8 47 7 17 11 9 23 4 | 31 28 28 31 24 27 25 33 37 19 29 6 | 6 14 7 5 40 5 9 9 8 16 3 | 33 40 40 36 41 36 41 32 35 38 35 7 | 7 17 6 15 32 6 16 10 10 25 4 | 17 27 17 23 39 19 24 15 22 26 17 8 | 8 16 11 8 20 5 11 22 11 22 5 | 20 28 22 20 35 20 24 29 25 30 22 9 | 9 14 6 8 38 4 12 9 6 18 3 | 17 22 22 19 31 19 21 21 22 29 18 10E | 18 35 9 14 34 5 21 17 14 31 7 | 55 75 60 58 66 59 67 60 60 79 59 11 | 5 18 8 11 50 8 15 12 8 34 4 | 26 37 26 26 33 24 30 26 29 22 25 12E | 10 20 11 7 22 7 20 9 8 14 4 | 21 28 23 22 35 23 25 22 25 28 21 13 | 6 17 8 10 34 7 16 11 9 15 4 | 14 26 17 18 45 16 23 12 17 16 15 14 | 9 27 13 7 27 4 20 10 10 28 5 | 21 33 24 23 44 22 28 19 25 21 22 15 | 10 24 10 8 24 6 21 13 10 22 5 | 11 25 16 13 33 11 19 12 18 16 12 16E | 9 30 9 18 37 5 22 12 7 19 5 | 16 33 18 21 35 17 26 14 23 22 17 17 | 10 19 11 16 53 5 17 10 8 33 5 | 18 33 24 28 38 20 27 22 24 33 21 18E | 13 25 10 19 38 7 22 9 10 20 5 | 44 55 54 58 58 51 51 54 53 52 51 19 | 6 14 7 9 38 6 17 14 13 24 4 | 21 30 24 24 40 25 31 21 29 23 23 20 | 6 15 8 8 44 7 16 11 10 16 4 | 13 23 14 13 43 16 23 16 23 16 14 21 | 9 16 7 7 67 5 18 8 13 27 4 | 17 27 18 20 49 18 24 18 19 22 17 22E | 11 16 8 13 35 5 13 9 10 25 4 | 32 36 33 35 47 31 31 30 38 27 33 23 | 10 22 8 14 27 6 16 13 9 12 4 | 14 30 17 19 39 17 23 13 17 17 14 24 | 6 12 8 5 59 6 9 8 7 20 3 | 21 24 29 26 26 22 21 24 24 25 24 25 | 7 15 10 5 24 4 11 10 8 13 3 | 16 22 19 17 25 16 21 17 16 17 15 26 | 11 13 10 10 22 5 9 12 13 34 5 | 24 32 27 31 45 27 32 26 29 45 27 27 | 8 14 8 8 22 5 10 23 9 25 5 | 19 24 19 17 31 18 22 28 23 30 20 28E | 6 19 10 9 39 6 16 12 13 12 4 | 14 29 23 17 50 19 25 18 23 23 19 29 | 10 17 8 6 29 9 19 18 7 27 5 | 22 23 21 22 27 22 25 24 27 28 22 30E | 15 19 9 13 69 5 17 15 10 21 5 | 43 45 42 47 60 42 43 45 49 47 44 31 | 8 22 12 7 30 6 18 9 11 25 4 | 20 31 24 20 47 21 27 19 26 22 21 32E | 13 25 10 12 51 8 17 14 7 28 5 | 60 64 63 64 79 62 64 62 67 67 63 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 19 9 10 41 6 16 13 10 24 |T 23 33 27 27 41 26 30 25 29 29 25 WRMS | 8 19 9 10 41 6 16 11 8 23 |NE 19 28 23 22 37 21 26 21 24 25 20 MEDI | 9 17 9 8 37 6 16 11 9 23 |MD 20 30 24 23 39 22 25 22 25 26 22 Table 3.1513.2 GPS week: 1513 Day: 2 MJD: 54837.000 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 | 7 --- --- --- --- 72 --- --- --- --- 0 | 44 --- --- --- --- 34 --- --- --- --- 48 2 | 7 12 9 9 36 5 16 13 11 25 4 | 18 32 23 26 36 22 33 19 23 25 23 3 | 7 13 10 5 35 6 11 8 14 17 4 | 25 33 37 31 38 29 37 26 27 28 29 4 | 10 12 9 8 48 4 9 15 10 31 4 | 23 29 26 28 30 27 26 27 29 36 25 5E | 12 19 8 9 70 4 17 12 12 23 5 | 29 31 24 31 33 26 24 31 33 18 26 6 | 7 12 8 6 27 5 9 9 12 15 3 | 25 33 35 30 41 29 35 27 25 33 28 7 | 5 19 10 13 25 5 17 15 6 26 5 | 16 30 19 22 34 16 25 12 16 27 16 8 | 8 13 11 9 26 4 12 15 8 21 4 | 14 25 19 15 23 15 22 23 17 29 17 9 | 9 14 6 6 30 4 11 11 9 15 3 | 11 22 18 13 30 15 22 16 12 21 14 10 | 14 22 10 16 38 6 19 13 12 17 5 | 74 85 78 78 84 77 83 80 78 85 78 11 | 7 16 6 8 42 4 13 9 7 24 4 | 28 39 29 34 32 30 35 31 31 28 30 12E | 10 20 8 9 33 5 20 11 11 14 4 | 16 24 22 19 37 18 25 18 24 18 19 13 | 5 17 9 8 27 3 15 12 8 17 4 | 18 31 21 18 41 19 27 17 15 17 17 14 | 10 30 8 9 28 4 16 10 7 25 5 | 12 32 16 15 37 13 24 13 18 17 14 15 | 8 18 8 9 28 5 21 13 8 23 4 | 11 24 17 14 32 12 22 14 14 17 13 16E | 8 29 11 15 35 5 22 15 11 18 5 | 10 31 17 18 31 13 25 14 15 18 13 17 | 10 16 12 17 40 5 17 8 14 28 5 | 18 30 21 23 35 19 26 20 17 25 18 18E | 26 25 12 13 45 8 21 10 10 22 6 | 92 115 111 110 108 98 110 107 104 105 107 19 | 8 18 10 7 41 4 18 14 12 26 5 | 19 33 26 20 44 22 31 18 20 18 20 20 | 7 21 6 9 38 4 16 10 13 14 4 | 15 33 16 16 29 19 26 18 18 19 16 21 | 7 16 6 8 66 4 16 10 11 27 4 | 13 24 16 16 47 15 24 15 19 18 15 22E | 12 20 12 8 42 4 13 9 8 29 4 | 45 51 49 46 48 44 47 46 46 41 46 23 | 8 20 9 12 26 4 19 12 9 12 4 | 17 31 23 22 39 20 27 15 17 18 18 24 | 5 11 5 6 50 3 8 10 9 19 3 | 26 26 27 26 22 25 23 26 28 25 26 25 | 7 15 11 7 33 4 11 15 9 15 4 | 16 23 20 14 27 15 22 13 15 16 13 26 | 5 14 7 8 23 5 10 10 8 32 4 | 14 25 17 15 37 13 22 15 13 35 15 27 | 8 12 10 8 18 3 12 15 7 26 4 | 14 24 20 15 25 16 21 22 16 31 17 28E | 9 17 7 8 30 4 14 10 9 12 4 | 14 30 21 16 39 17 27 18 17 15 17 29 | 7 21 9 8 34 6 18 18 8 27 5 | 21 28 19 22 35 22 27 27 24 28 22 30E | 14 19 11 12 82 5 18 20 15 21 6 | 32 35 29 33 31 30 31 34 38 35 31 31 | 8 24 11 6 41 5 17 7 9 23 4 | 14 31 19 15 54 15 26 15 17 19 15 32E | 16 26 14 14 73 5 15 12 9 26 6 | 48 53 53 52 63 50 51 55 55 53 51 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 19 9 10 42 5 16 12 10 22 |T 24 35 28 27 40 26 32 26 27 29 26 WRMS | 8 19 9 10 40 4 15 11 9 21 |NE 18 29 22 20 34 20 26 19 19 24 20 MEDI | 8 18 9 8 35 4 16 12 9 23 |MD 18 31 21 22 36 19 26 19 19 25 18 Table 3.1513.3 GPS week: 1513 Day: 3 MJD: 54838.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 14 12 8 44 3 16 13 14 20 4 | 24 34 29 32 46 26 33 22 31 27 27 3 | 8 13 7 5 49 5 10 10 11 17 3 | 23 31 32 27 37 27 32 24 24 28 26 4 | 8 13 11 6 50 4 9 12 12 21 4 | 30 35 38 35 35 32 29 30 31 29 32 5E | 11 20 9 8 70 5 16 11 10 23 4 | 31 31 25 33 32 28 26 33 36 20 29 6 | 7 13 4 7 47 3 10 8 10 19 3 | 29 36 36 35 39 32 36 30 35 40 33 7 | 6 16 11 13 29 6 17 13 13 26 5 | 18 27 20 20 35 16 25 17 23 28 17 8 | 9 14 10 7 16 4 12 13 11 21 4 | 24 27 23 21 32 19 23 22 26 31 21 9 | 9 14 7 6 36 5 12 12 8 18 3 | 18 28 24 19 30 19 25 20 27 26 21 10 | 13 17 7 13 34 5 17 12 9 18 4 | 77 84 78 79 85 77 83 76 77 78 78 11 | 6 17 9 8 54 3 13 9 16 23 4 | 34 39 39 34 32 32 35 34 32 25 33 12E | 9 19 10 7 31 3 22 10 11 13 4 | 17 23 23 21 37 16 24 15 22 19 18 13 | 8 17 7 10 29 5 17 12 15 18 4 | 17 28 16 19 42 16 25 14 22 16 16 14 | 14 25 8 6 25 2 17 9 10 21 5 | 19 28 19 21 42 16 24 18 24 19 19 X15 | 8 22 7 9 27 6 --- 16 9 22 5 | 14 23 15 11 34 9 --- 14 18 14 11 16E | 10 27 10 15 31 4 26 15 10 18 6 | 21 37 26 31 38 23 33 19 23 25 23 17 | 9 15 11 15 46 4 18 7 11 27 5 | 23 30 25 28 38 23 30 24 23 34 24 18 | 9 21 7 10 51 7 20 9 12 19 4 | 60 63 66 68 80 64 61 64 69 66 64 19 | 7 19 10 5 42 5 20 19 16 27 5 | 20 31 23 21 39 20 31 22 24 21 19 20 | 7 24 9 8 38 2 15 12 9 18 4 | 15 31 15 20 30 15 23 20 21 24 15 21 | 8 16 6 7 39 3 15 8 7 25 4 | 21 30 21 24 34 19 25 20 24 21 20 22 | 18 18 7 6 33 6 16 8 10 20 4 | 31 38 37 38 35 36 34 36 43 32 35 23 | 9 21 9 10 30 6 18 16 10 11 4 | 16 30 22 21 41 17 27 21 20 22 18 24 | 6 11 8 6 43 3 9 9 6 17 3 | 26 28 34 30 40 27 26 28 31 26 29 25 | 8 12 9 7 28 5 11 14 12 15 4 | 19 23 20 17 28 18 23 20 22 20 17 26 | 7 16 6 7 29 3 8 11 10 26 4 | 22 30 21 23 35 20 24 18 25 34 20 27 | 9 13 11 6 18 3 13 15 11 20 4 | 23 26 21 20 30 19 21 21 27 29 20 28E | 6 22 10 14 26 3 17 9 7 11 4 | 16 29 23 20 39 16 24 16 18 21 17 29 | 8 17 6 9 31 6 19 15 9 28 5 | 27 29 26 33 34 26 32 31 33 31 29 30E | 15 19 8 11 75 6 17 19 10 24 5 | 51 48 48 52 55 46 48 53 51 50 49 31 | 9 22 10 8 29 6 17 6 11 20 4 | 21 31 20 23 42 18 29 19 29 19 21 32E | 16 33 10 11 61 6 19 13 14 22 6 | 70 75 68 71 82 68 73 67 63 77 68 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 19 9 9 41 5 16 12 11 21 |T 27 34 30 30 41 27 32 28 31 30 28 WRMS | 9 19 9 9 39 5 15 11 9 20 |NE 21 29 24 24 36 21 27 22 26 25 22 MEDI | 8 17 9 8 34 5 16 12 10 20 |MD 23 30 24 24 37 20 27 22 26 26 21 Table 3.1513.4 GPS week: 1513 Day: 4 MJD: 54839.000 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 | 6 14 10 8 56 4 14 14 15 19 4 | 24 32 28 28 52 27 34 28 27 27 26 3 | 7 13 9 8 39 5 14 10 12 22 4 | 30 34 37 35 35 33 38 33 36 37 33 4 | 8 16 7 5 41 6 8 12 11 17 3 | 22 30 33 29 25 29 27 27 34 25 27 5E | 13 20 6 11 70 5 16 14 13 22 5 | 33 33 29 39 31 32 29 39 38 27 32 6 | 6 15 10 9 36 4 12 12 12 17 4 | 29 34 33 33 42 32 38 31 35 38 31 7 | 7 20 9 10 26 5 15 11 9 26 4 | 19 31 20 26 34 20 29 22 25 29 20 8 | 9 13 14 8 15 5 12 11 11 18 4 | 18 23 23 21 22 20 25 22 22 25 18 9 | 8 17 19 8 35 5 13 16 18 23 5 | 17 25 26 18 29 20 23 23 27 26 18 10 | 11 20 8 12 30 5 16 12 10 17 4 | 55 64 57 60 57 57 62 56 58 54 57 11 | 7 21 8 8 53 3 14 9 13 24 4 | 30 39 34 32 33 30 34 35 30 28 30 12E | 9 22 8 13 33 3 23 9 13 19 5 | 19 30 28 29 46 22 30 23 29 24 23 13 | 8 19 12 8 30 5 13 10 11 15 4 | 19 30 22 21 43 20 29 19 23 22 20 14 | 11 25 12 7 36 4 19 12 13 19 5 | 18 28 26 21 42 18 27 22 27 23 20 X15 | 5 --- 6 --- --- 39 --- --- --- --- 6 | 17 --- 20 --- --- 138 --- --- --- --- 15 16E | 9 31 12 16 26 4 26 12 12 17 6 | 18 31 23 25 32 21 31 22 32 25 21 17 | 12 17 11 17 38 7 18 9 14 29 5 | 19 30 22 34 33 21 32 24 31 33 23 18 | 8 24 7 11 49 6 20 11 12 19 5 | 37 45 45 43 61 42 43 40 48 39 41 19 | 7 20 9 7 32 5 20 18 14 30 5 | 20 32 24 23 36 23 34 26 30 23 22 20 | 6 27 7 10 44 4 14 11 11 21 4 | 18 35 20 24 32 19 27 25 26 26 20 21 | 7 17 6 7 30 4 17 8 14 26 4 | 19 27 20 18 27 19 29 20 26 19 19 22 | 10 21 9 5 30 6 16 8 10 16 4 | 25 32 31 28 32 29 31 31 35 28 28 23 | 8 25 12 9 29 5 16 15 12 14 5 | 18 31 24 23 35 20 28 19 25 22 19 24 | 5 14 4 6 39 3 9 9 14 17 3 | 23 23 26 26 33 24 23 24 34 25 24 25 | 8 13 11 8 38 6 12 14 10 18 4 | 17 22 18 18 30 17 25 19 21 21 16 26 | 7 18 8 9 36 4 10 10 13 25 4 | 17 26 20 23 35 19 28 20 24 36 20 27 | 6 13 13 8 22 6 11 11 9 20 4 | 17 23 24 20 24 21 24 22 22 26 19 28E | 8 20 11 11 37 5 17 10 12 12 4 | 17 32 26 21 46 21 29 22 29 26 21 29 | 8 20 16 9 38 5 19 12 16 29 5 | 24 30 30 26 30 24 28 27 28 30 25 30E | 14 19 10 13 64 5 18 18 19 18 6 | 29 33 31 35 28 29 33 36 39 27 30 31 | 8 22 7 9 34 7 19 9 13 25 4 | 22 31 22 20 41 20 30 19 28 27 20 32E | 21 32 14 15 61 7 19 9 11 28 6 | 89 90 84 83 86 84 88 85 80 91 85 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 10 10 40 5 16 12 13 21 |T 25 33 29 29 37 30 32 28 32 30 26 WRMS | 8 20 10 10 39 5 16 11 11 20 |NE 20 29 25 24 33 27 29 24 27 27 22 MEDI | 8 20 9 9 36 5 16 11 12 19 |MD 19 31 26 26 33 22 29 24 29 26 22 Table 3.1513.5 GPS week: 1513 Day: 5 MJD: 54840.000 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 | 5 14 11 8 44 7 21 13 14 21 4 | 18 29 24 23 36 22 31 22 24 25 22 3 | 11 15 6 6 40 3 12 11 10 21 4 | 23 27 28 24 44 24 31 21 25 28 24 4 | 6 19 10 8 30 5 13 15 12 20 4 | 25 32 32 29 28 27 29 29 30 25 28 5E | 10 21 7 10 81 5 18 16 15 24 5 | 32 33 28 33 24 31 31 44 39 33 32 6 | 8 16 7 6 34 5 11 16 11 18 4 | 23 30 29 26 36 26 31 25 29 31 25 7 | 7 20 8 10 26 6 17 15 11 28 5 | 17 26 21 22 34 17 24 17 20 25 16 8 | 8 13 7 6 15 5 13 16 8 21 4 | 20 23 20 19 26 19 24 23 21 25 18 9 | 8 15 7 7 32 5 16 10 10 17 4 | 15 25 18 18 39 18 20 19 21 20 16 10 | 10 22 8 10 33 6 17 13 8 17 4 | 45 52 49 49 49 48 52 47 47 51 47 11 | 8 20 9 5 57 3 17 16 14 30 5 | 23 33 26 23 29 24 30 29 20 25 21 12E | 10 25 10 7 34 8 25 11 12 21 5 | 20 29 28 23 35 23 32 22 24 28 23 13 | 6 21 9 7 37 7 16 12 11 16 4 | 14 27 18 13 50 15 28 13 16 16 13 14 | 10 27 7 7 28 5 20 12 10 19 4 | 13 25 18 15 37 11 23 16 12 17 13 X15 | 6 --- --- --- --- 12 --- --- --- --- 0 | 8 --- --- --- --- 11 --- --- --- --- 8 16E | 10 25 7 11 31 6 28 13 19 21 5 | 12 26 18 15 29 12 27 15 24 19 14 17 | 8 22 14 15 35 5 23 11 12 38 6 | 22 31 24 24 33 19 32 24 24 33 21 18 | 9 27 6 9 44 5 24 13 11 20 5 | 23 35 29 29 36 27 30 29 31 30 26 19 | 8 22 9 5 34 4 21 23 13 28 5 | 15 29 20 17 44 15 30 25 17 20 15 20 | 6 23 9 10 40 4 14 20 9 27 5 | 19 34 25 22 29 22 30 25 24 27 20 21 | 8 19 5 5 41 5 21 9 11 28 4 | 17 24 19 16 26 16 26 17 20 21 16 22 | 11 20 7 6 40 4 17 10 11 20 4 | 18 27 22 19 31 19 20 21 24 25 19 23 | 8 26 9 9 27 7 20 19 12 15 5 | 15 31 18 15 38 16 29 16 17 21 14 24 | 5 14 6 8 36 4 12 10 11 18 3 | 20 24 25 22 20 23 20 22 30 20 22 25 | 8 16 6 6 31 6 16 19 15 22 4 | 18 22 20 13 22 17 26 17 22 21 15 26 | 7 18 9 9 29 5 12 14 10 28 4 | 19 25 21 23 32 18 26 19 21 34 19 27 | 7 13 8 6 17 5 12 16 8 22 4 | 19 23 20 17 29 19 24 22 22 25 18 28E | 9 23 10 10 23 5 21 15 11 19 5 | 14 29 20 17 34 15 27 17 12 28 15 29 | 7 23 8 6 45 5 21 12 14 32 5 | 21 28 21 23 34 21 28 24 28 33 22 30E | 13 20 7 12 75 6 20 18 12 22 5 | 50 49 48 53 45 47 46 49 54 47 48 31 | 8 24 8 7 26 5 20 9 17 30 5 | 14 30 17 15 44 14 29 17 21 25 15 32E | 20 28 12 21 39 11 19 27 13 31 7 | 79 85 79 87 97 75 84 91 83 88 81 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 21 8 9 39 6 18 15 12 24 |T 22 31 26 24 36 22 30 25 26 28 22 WRMS | 8 21 8 9 40 5 18 14 10 22 |NE 18 27 22 19 33 18 27 21 22 24 18 MEDI | 8 20 8 7 34 5 17 13 11 21 |MD 19 29 21 22 34 19 29 22 24 25 19 Table 3.1513.6 GPS week: 1513 Day: 6 MJD: 54841.000 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 | 6 14 6 9 48 4 15 14 9 21 4 | 28 35 31 29 55 29 37 32 30 34 30 3 | 9 14 9 9 23 6 13 12 11 27 4 | 24 30 32 33 44 27 32 30 29 29 29 4 | 5 10 5 4 25 5 9 15 11 18 3 | 32 33 34 35 37 32 29 32 29 27 31 5E | 12 19 8 12 61 6 18 23 21 25 6 | 35 36 31 36 22 34 28 51 47 32 34 6 | 6 12 12 9 24 6 13 22 10 17 4 | 28 32 34 36 41 30 33 36 33 34 32 7 | 8 17 10 9 40 5 20 13 10 28 5 | 17 29 22 20 43 18 28 23 19 27 18 8 | 5 17 9 11 43 4 12 15 9 21 4 | 22 30 20 20 40 20 23 25 25 25 21 9 | 6 13 5 6 39 4 12 11 7 17 3 | 20 28 23 21 29 21 25 23 23 25 21 10 | 8 21 8 8 42 5 16 13 9 20 4 | 72 78 75 73 92 75 78 73 73 73 73 11 | 7 17 7 14 44 6 16 15 13 33 5 | 39 46 42 44 49 38 40 41 36 31 38 12E | 9 23 8 10 35 6 24 11 12 15 5 | 19 31 25 23 50 21 30 26 27 24 22 13 | 7 17 7 9 29 6 14 13 9 17 4 | 17 31 23 19 39 18 24 19 15 23 18 14 | 10 23 7 8 40 4 19 14 10 20 5 | 20 30 22 22 48 21 29 21 28 21 21 X15 | 7 25 8 7 28 7 --- 16 12 --- 5 | 8 22 6 8 22 12 --- 5 8 --- 10 16E | 8 19 9 16 38 5 24 15 12 25 5 | 19 31 25 29 44 23 32 22 30 31 23 17 | 8 21 9 13 32 6 21 11 12 38 5 | 30 33 31 29 40 28 34 33 32 44 29 18 | 9 20 8 10 42 4 21 12 11 20 4 | 43 47 46 48 69 45 43 43 52 40 45 19 | 6 20 9 9 43 3 23 18 11 25 5 | 20 32 22 18 44 20 34 23 25 19 20 20 | 7 23 7 11 38 6 13 12 10 26 4 | 19 34 21 21 42 21 25 25 23 30 21 21 | 9 17 5 6 35 4 15 10 9 31 4 | 25 28 25 25 38 24 27 25 27 27 24 22 | 8 16 7 7 35 3 18 13 9 27 4 | 29 34 29 33 48 32 32 29 42 32 31 23 | 8 22 10 13 38 6 19 20 12 16 5 | 19 34 26 19 35 19 27 23 20 25 20 24 | 4 14 7 8 39 4 9 11 9 24 3 | 30 31 36 33 29 32 31 32 39 34 33 25 | 7 14 7 7 40 5 13 17 12 26 4 | 17 26 19 15 32 17 21 20 20 26 16 26 | 7 12 9 7 34 5 12 14 11 28 4 | 23 24 22 22 32 21 28 18 25 33 21 27 | 5 15 8 8 37 5 12 14 10 19 4 | 21 27 19 18 37 20 22 23 24 24 20 28E | 7 20 8 14 46 4 17 15 11 23 5 | 18 31 23 21 57 20 28 21 26 33 20 29 | 6 21 7 8 30 5 20 11 13 30 5 | 33 38 33 37 36 35 37 37 37 42 35 30E | 14 20 8 12 62 6 19 13 16 22 5 | 68 63 62 65 54 59 59 65 65 61 63 31 | 8 22 9 8 24 7 20 12 8 28 5 | 22 34 25 23 40 21 31 20 26 24 23 32 | 11 20 10 20 54 9 18 13 11 25 5 | 88 89 88 89 97 84 86 88 88 87 88 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 8 10 40 5 17 14 11 24 |T 29 36 31 31 44 29 34 31 33 33 30 WRMS | 7 18 8 10 40 5 16 14 9 23 |NE 23 31 25 24 38 23 29 25 26 28 24 MEDI | 7 19 8 9 38 5 16 13 11 24 |MD 23 32 25 25 41 23 30 25 28 30 23 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 4.1513 GPS week: 1513 MJD: 54835.0-54841.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3012 |U 7 8 18 |U 11 14 45 |U 12 10 25 | emr | emr 2937 | 14 11 31 | 13 16 49 | 13 9 30 | esa | esa 2948 | 8 9 22 |U 11 13 42 | 13 11 24 | gfz | gfz 2920 |U 13 11 32 |U 13 19 47 | 14 14 31 | igr | igr 2925 | 10 10 24 | 11 14 46 | 12 10 26 | igs | igs 2927 | 11 10 27 | 12 17 42 | 12 10 25 | jpl | jpl 2909 |U 19 13 35 |U 12 15 43 | 12 8 29 | mit | mit 2948 |U 11 10 29 |U 14 17 46 |U 12 10 27 | 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 5.1513.0 GPS week: 1513 Day: 0 MJD: 54835.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3062 | 7 9 24 | ---- ---- ---- | 13 11 25 | emr | emr 2960 | 18 15 42 | ---- ---- ---- | 11 8 26 | esa | esa 2976 | 9 12 27 | ---- ---- ---- | 12 12 26 | gfz | gfz 2941 | 17 16 40 | ---- ---- ---- | 15 15 38 | igr | igr 2943 | 17 17 37 | ---- ---- ---- | 11 10 28 | igs | igs 2928 | 17 16 39 | ---- ---- ---- | 10 10 27 | jpl | jpl 2960 | 17 16 43 | ---- ---- ---- | 11 8 34 | mit | mit 2976 | 16 15 39 | ---- ---- ---- | 10 8 31 | Table 5.1513.1 GPS week: 1513 Day: 1 MJD: 54836.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3070 | 9 10 19 | ---- ---- ---- | 13 9 18 | emr | emr 2962 | 14 10 27 | ---- ---- ---- | 13 10 26 | esa | esa 2976 | 10 11 24 | ---- ---- ---- | 12 10 20 | gfz | gfz 2942 | 13 10 26 | ---- ---- ---- | 13 14 29 | igr | igr 2958 | 11 11 28 | ---- ---- ---- | 12 8 20 | igs | igs 2970 | 10 10 20 | ---- ---- ---- | 12 8 21 | jpl | jpl 2962 | 12 10 27 | ---- ---- ---- | 11 8 22 | mit | mit 2976 | 9 9 24 | ---- ---- ---- | 11 8 22 | Table 5.1513.2 GPS week: 1513 Day: 2 MJD: 54837.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3051 | 6 8 17 | ---- ---- ---- | 12 8 22 | emr | emr 2964 | 9 11 30 | ---- ---- ---- | 12 7 31 | esa | esa 2976 | 7 7 22 | ---- ---- ---- | 12 9 21 | gfz | gfz 2941 | 8 13 26 | ---- ---- ---- | 14 15 33 | igr | igr 2952 | 7 8 17 | ---- ---- ---- | 11 8 22 | igs | igs 2953 | 9 9 27 | ---- ---- ---- | 12 8 24 | jpl | jpl 2963 | 13 11 25 | ---- ---- ---- | 12 8 30 | mit | mit 2976 | 8 11 28 | ---- ---- ---- | 11 7 27 | Table 5.1513.3 GPS week: 1513 Day: 3 MJD: 54838.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 9 10 16 | ---- ---- ---- | 11 7 24 | emr | emr 2964 | 11 8 23 | ---- ---- ---- | 13 7 32 | esa | esa 2976 | 9 8 15 | ---- ---- ---- | 13 8 24 | gfz | gfz 2952 | 11 12 24 | ---- ---- ---- | 13 9 29 | igr | igr 2907 | 9 10 21 | ---- ---- ---- | 11 6 27 | igs | igs 2959 | 8 9 20 | ---- ---- ---- | 11 7 24 | jpl | jpl 2866 | 21 15 26 | ---- ---- ---- | 12 6 29 | mit | mit 2976 | 11 13 29 | ---- ---- ---- | 12 8 25 | Table 5.1513.4 GPS week: 1513 Day: 4 MJD: 54839.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 6 6 22 | 13 15 37 | 14 14 33 | emr | emr 2870 | 20 10 25 | 14 18 37 | 14 12 30 | esa | esa 2880 | 8 7 25 | 14 14 38 | 15 15 29 | gfz | gfz 2858 | 17 10 24 | 14 22 35 | 17 17 35 | igr | igr 2919 | 6 7 21 | 13 13 38 | 14 14 29 | igs | igs 2847 | 16 10 26 | 13 18 34 | 14 14 30 | jpl | jpl 2869 | 35 15 37 | 13 15 36 | 13 9 35 | mit | mit 2880 | 16 10 23 | 15 19 41 | 15 13 37 | Table 5.1513.5 GPS week: 1513 Day: 5 MJD: 54840.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 5 7 14 | 9 12 43 | 13 11 23 | emr | emr 2872 | 14 10 31 | 12 15 50 | 12 11 32 | esa | esa 2880 | 8 10 20 | 9 12 43 | 13 13 25 | gfz | gfz 2859 | 13 12 42 | 12 21 53 | 15 16 29 | igr | igr 2847 | 8 10 23 | 10 15 47 | 12 13 28 | igs | igs 2873 | 9 9 28 | 11 17 42 | 11 11 24 | jpl | jpl 2872 | 16 10 32 | 11 16 44 | 13 10 27 | mit | mit 2880 | 8 10 29 | 12 19 43 | 12 14 27 | Table 5.1513.6 GPS week: 1513 Day: 6 MJD: 54841.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 5 5 13 | 12 15 56 | 14 12 27 | emr | emr 2968 | 9 11 41 | 13 15 60 | 13 12 31 | esa | esa 2976 | 6 7 20 | 10 13 44 | 14 12 25 | gfz | gfz 2952 | 11 8 41 | 13 15 54 | 14 13 26 | igr | igr 2953 | 10 6 25 | 11 14 52 | 12 9 26 | igs | igs 2965 | 8 7 32 | 11 15 51 | 12 11 25 | jpl | jpl 2872 | 17 13 56 | 10 15 50 | 14 10 28 | mit | mit 2976 | 9 6 33 | 14 15 54 | 12 10 24 | 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 6.1513 GPS week: 1513 MJD: 54835.500-54841.500 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 | -19 11 69 -62 -4 | 0 17 | 14 26 122 96 8 | 3 emr uuxuu | 0 -32 -186 35 -14 | 40 44 | 30 26 295 49 5 | 4 esa uuuuu | 9 10 -25 -5 -16 | 4 21 | 27 24 143 77 16 | 4 gfz uuuuu | -4 -6 85 -45 2 | -3 16 | 26 23 92 76 6 | 6 grg xxxxx | -11 -10 48 -37 43 | 11 26 | 57 32 135 129 134 | 4 igr xxxxx | -8 18 82 -13 -17 | 17 26 | 21 31 66 76 5 | 4 irf xxxxx | -4 11 -17 27 -7 | 10 17 | 16 8 40 24 3 | 3 jpl uuuux | 4 10 40 -9 -10 | 12 30 | 34 30 136 98 20 | 6 mit uuuuu | 3 5 -171 153 2 | 6 17 | 39 19 121 80 7 | 5 ngs uuuuu | 26 2 85 -112 3 | 3 17 | 62 47 73 69 11 | 2 sio uuxxu | -122 -29 39 -81 -2 | 12 19 | 31 15 93 151 9 | 5 Table 7.1513.0 GPS week: 1513 Day: 0 MJD: 54835.500 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 -21 146 -196 -15 | -1 16 emr uuxuu | 23 -48 153 7 -22 | 42 45 esa uuuuu | -44 -30 -276 51 -18 | 3 25 gfz uuuuu | 17 -37 249 -200 13 | -12 22 grg xxxxx | 102 -15 292 181 31 | 3 32 igr xxxxx | -2 70 156 48 -19 | 15 26 irf xxxxx | -36 17 -31 31 -5 | 6 16 jpl uuuux | -34 27 325 54 -44 | 18 31 mit uuuuu | -69 28 -133 189 -2 | -1 14 ngs uuuuu | 150 47 49 -108 4 | 0 17 sio uuxxu | -183 -24 50 10 2 | 6 13 Table 7.1513.1 GPS week: 1513 Day: 1 MJD: 54836.500 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 25 240 -41 -8 | -2 18 emr uuxuu | 7 -79 167 -24 -16 | 39 44 esa uuuuu | -1 -9 -133 -12 -23 | 3 25 gfz uuuuu | 26 -30 94 50 4 | -9 19 grg xxxxx | -28 38 -62 -199 -16 | 10 28 igr xxxxx | -41 21 24 -95 -15 | 15 26 irf xxxxx | -7 -1 33 47 -4 | 5 17 jpl uuuux | 17 42 -93 -62 -23 | 14 33 mit uuuuu | -14 -10 6 248 5 | -2 15 ngs uuuuu | 14 72 90 -201 -4 | 0 17 sio uuxxu | -143 -50 217 73 5 | 5 14 Table 7.1513.2 GPS week: 1513 Day: 2 MJD: 54837.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -21 1 -138 54 -8 | 1 17 emr uuxuu | -17 -34 -81 42 -10 | 42 45 esa uuuuu | 30 -1 86 -1 -40 | 7 22 gfz uuuuu | 4 2 7 -53 2 | -3 12 grg xxxxx | -56 -69 44 -20 -10 | 14 27 igr xxxxx | -8 -4 57 -5 -9 | 19 25 irf xxxxx | 1 17 -25 62 -9 | 10 16 jpl uuuux | -3 30 35 -130 -5 | 15 33 mit uuuuu | -10 26 -184 244 3 | 4 13 ngs uuuuu | 17 -18 47 -105 9 | 4 16 sio uuxxu | -108 -25 27 68 5 | 10 16 Table 7.1513.3 GPS week: 1513 Day: 3 MJD: 54838.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -11 58 15 -187 -3 | 3 18 emr uuxuu | -44 -30 -119 -20 -5 | 44 47 esa uuuuu | 31 15 78 134 -30 | 8 22 gfz uuuuu | -2 26 -23 -35 6 | 1 13 grg xxxxx | 1 -2 -21 -144 -20 | 12 24 igr xxxxx | 31 45 36 -109 -14 | 22 28 irf xxxxx | 0 11 29 11 -4 | 13 18 jpl uuuux | -23 33 8 -121 -9 | 15 34 mit uuuuu | 2 11 -77 87 14 | 8 17 ngs uuuuu | 41 -61 3 -132 -18 | 7 20 sio uuxxu | -118 -38 44 -85 9 | 14 20 Table 7.1513.4 GPS week: 1513 Day: 4 MJD: 54839.500 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 -3 94 18 -3 | 2 17 emr uuxuu | -31 -13 -536 78 -15 | 43 46 esa uuuuu | 30 27 84 -45 -2 | 6 21 gfz uuuuu | 9 6 151 -37 -2 | 2 15 grg xxxxx | -43 -1 -2 10 -35 | 16 23 igr xxxxx | -12 19 31 21 -26 | 22 28 irf xxxxx | 16 20 -25 40 -7 | 13 18 jpl uuuux | -18 -28 -48 27 -12 | 12 29 mit uuuuu | 47 8 -237 167 2 | 10 20 ngs uuuuu | -42 -27 40 -184 6 | 3 16 sio uuxxu | -91 -3 23 -73 -6 | 16 24 Table 7.1513.5 GPS week: 1513 Day: 5 MJD: 54840.500 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 | -46 0 125 -56 -3 | -1 17 emr uuxuu | 27 -12 -520 68 -15 | 38 42 esa uuuuu | 15 31 -85 -74 2 | 2 18 gfz uuuuu | -37 -16 58 -13 -8 | 2 15 grg xxxxx | -62 -19 167 -119 7 | 12 25 igr xxxxx | -9 -10 190 -48 -20 | 18 27 irf xxxxx | 1 2 -17 3 -6 | 11 18 jpl uuuux | 67 -6 66 32 13 | 6 26 mit uuuuu | 39 -26 -195 93 3 | 10 20 ngs uuuuu | -25 27 205 -17 10 | 2 15 sio uuxxu | -107 -36 15 -324 -8 | 16 24 Table 7.1513.6 GPS week: 1513 Day: 6 MJD: 54841.500 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 18 5 -25 11 | -4 18 emr uuxuu | 33 -6 -367 98 -13 | 33 38 esa uuuuu | 5 34 71 -85 0 | -3 16 gfz uuuuu | -43 5 61 -25 0 | 0 17 grg xxxxx | 11 -5 -80 32 343 | 10 24 igr xxxxx | -15 -17 83 99 -17 | 11 24 irf xxxxx | -3 12 -85 -2 -11 | 9 18 jpl uuuux | 20 -28 -11 136 12 | 1 21 mit uuuuu | 23 -3 -373 47 -8 | 10 21 ngs uuuuu | 26 -24 160 -34 13 | 2 15 sio uuxxu | -106 -26 -101 -234 -17 | 14 24