Date: Thu, 22 Apr 2010 12:22:05 +0000 From: Jim Ray Subject: [IGSREPORT-18497] Wk 1578 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4bd03f6d.eni1R0sdp9yYjSCj%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 22 Apr 05:22:18 PDT 2010 Message Number 18497 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1578 (Apr 04, 2010 - Apr 10, 2010) 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 (as part of the separate SINEX combination since GPS week 1051; weighted according to the orbit combination before that time). 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: igs1578[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1578[0-6].clk IGS GPS satellite and station clocks in clock RINEX format. igs1578[0-6].cls IGS GPS clock combination summary report. igs15787.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15787.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Duplicate entries can arise due to separate combination runs for the 30-s clocks ACs (listed first) and the 5-min clock ACs (listed second). Day | Centre | PRN/STA list ----+--------+--------------- 0 | COD | YELL YELL 0 | EMR | WTZR WTZR 0 | ESA | UNSA 0 | GFZ | 4 ALIC CAS1 0 | GRG | ONSA 0 | JPL | DGAR 0 | NGS | 1 1 | COD | SCH2 WHIT EIL1 WHIT 1 | EMR | 4 4 SCH2 1 | ESA | CAS1 SCH2 WHIT 1 | GFZ | ADE1 CAS1 YAR2 1 | JPL | 4 1 | MIT | 4 4 NNOR NTUS YELL HRAO IRKT NNOR NTUS SCH2 YELL 1 | NGS | 1 2 | ALL | 1 1 2 | COD | SUTM 2 | EMR | 4 4 SYOG CHUR SYOG YAKT YELL 2 | ESA | CHUR CHUR MAW1 QAQ1 YELL 2 | GFZ | 5 ARTU MCM4 RIO2 2 | GRG | ONSA ULAB YAKT 2 | JPL | 4 27 DGAR YAKT 2 | MIT | 4 27 28 4 27 28 3 | COD | XMIS 3 | EMR | 4 24 4 24 WTZR WTZR 3 | GFZ | 5 21 AUCK BOR1 HARB TSKB 3 | GRG | ONSA 3 | JPL | 4 24 DGAR 3 | MIT | 4 24 27 29 4 24 27 29 BOR1 CHUR EIL1 3 | NGS | 1 4 | ALL | 1 1 4 | COD | ARTU MCM4 4 | EMR | 4 4 WTZR YELL 4 | ESA | YELL YELL 4 | GFZ | BOR1 4 | GRG | ONSA 4 | JPL | 4 24 27 DGAR 4 | MIT | 4 24 27 4 24 27 BOR1 5 | ALL | 1 5 | EMR | 4 24 4 24 WTZR 5 | ESA | MATE 5 | GFZ | 4 5 7 8 11 13 17 19 24 28 DGAR NICO NTUS PERT TOW2 5 | GFZ | TSKB 5 | GRG | NRC1 5 | JPL | 4 24 DGAR 5 | MIT | 4 24 4 24 NICO USNO DARW NICO USNO 5 | NGS | 1 6 | EMR | 4 4 24 WTZR HARB MDO1 6 | ESA | RAMO UNSA 6 | GFZ | REUN TSKB 6 | GRG | WTZR 6 | JPL | 4 24 27 DGAR 6 | MIT | 4 9 24 4 24 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 ----+--------+--------+------------- 1 | ESA | ~23:55 | ~ -0.19 ns 6. 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 ----+------------+---------- G02 | 2010_04_09 | 2010067 7. The following orbit solutions were excluded from the combination because they were biasing the weighted average (generally indicated by long arc RMS). They were still used for statistics computation. Day | Centre | PRN list ----+--------+--------------- 0 | SIO | ALL (high Transformation - See Table 2) 1 | SIO | ALL (high Transformation - See Table 2) 2 | SIO | ALL (high Transformation - See Table 2) 3 | SIO | ALL (high Transformation - See Table 2) 4 | SIO | ALL (high Transformation - See Table 2) 5 | SIO | ALL (high Transformation - See Table 2) 5 | GFZ | 23 6 | SIO | ALL (high Transformation - See Table 2) 8. 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 G04 | 2 | | | | | | | 9. 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. 10. Small rotations were applied to all the AC orbit and ERP values in order to align them to the IGS05 frame. These rotations were estimated in the IGS SINEX combination process, performed by the IGS Reference Frame Coordinator at the Institut Geographique National (IGN), and are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX frame. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .5 1.3 .9 -27 -1 -29 -.02 EMR | 11.4 4.8 8.7 -2 36 16 .22 ESA | 5.7 4.6 -1.9 81 -19 -66 .11 GFZ | -1.1 .8 1.2 -12 50 -80 .0 GRG | 4.8 8.5 11.9 30 59 -89 .65 JPL | 8.7 5.0 6.5 21 0 16 .24 MIT | 8.3 -.8 7.1 -4 16 -38 -.18 NGS | 5.8 -4.5 3.3 -75 -87 29 .02 SIO | 10.2 2.4 -8.8 -13 184 -597 .13 11. 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. 12. 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 IGN. 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. 13. 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 1.1578.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1578.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 2.1578.[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 3.1578.[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 5.1578.0-6). 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 1578 summary. (Apr 04, 2010 - Apr 10, 2010) Table 1.1578.a GPS week: 1578 MJD: 55290.000-55296.000 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 247| 0 0 1 34 -11 3 -.20 9 8 | -509 -57 22 77 | 0 0 1 7 18 25 .03 | 324 570 emr 86| 1 1 2 -3 -44 19 .48 20 20 | 498 1189 21 92 | 1 2 2 35 18 21 .03 | 2967 1641 esa 140| 2 1 -2 -163 -20 -47 .28 9 9 | -186 -788 16 91 | 1 0 1 23 30 13 .04 | 1022 2104 gfz 199| 0 0 -2 39 -79 -11 -.08 23 23 | 79 41 26 103 | 2 2 1 67 71 8 .04 | 366 649 grg 105| 0 1 2 -82 -115 19 .92 27 23 | 12 -25 79 223 | 1 1 2 22 29 9 .04 | 275 451 igr n/a| -1 0 -1 7 4 13 .04 6 6 | 12107 405 20 66 | 0 0 0 19 25 22 .04 | 1718 1724 jpl 131| -2 0 -1 -77 -2 60 .50 21 21 | 2494 993 19 112 | 1 1 1 12 13 13 .03 | 2354 1405 mit 259| 0 -1 0 1 -49 15 -.37 12 11 | -14449 1507 24 152 | 1 1 1 17 42 16 .02 | 1320 155 ngs 213| -1 -1 1 150 143 4 -.18 11 8 | 14569 -4315 2046 3609 | 0 1 0 30 35 13 .03 | 1445 2143 sio 260| 0 1 4 21 -370 -557 -.21 21 18 | --- --- --- --- | 1 1 1 21 29 13 .03 | --- --- Table 1.1578.b GPS week : 1578 MJD: 55290.000-55296.000 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 | 15 20 16 15 9 15 12 | 2 | 5 5 5 7 6 6 8 | 3 | 5 4 5 4 4 5 4 | 4 | 5 6 7 9 6 6 7 | 5 | 5 5 6 6 6 8 6 | 6 | 4 4 5 4 4 7 4 | 7 | 5 5 6 5 5 5 5 | 8 | 5 5 5 5 6 8 6 | 9 | --- --- --- --- --- 0 14 | 10 | 4 5 5 4 4 4 6 | 11 | 5 6 5 5 5 8 5 | 12 | 5 5 5 5 5 6 5 | 13 | 5 5 5 5 5 7 5 | 14 | 6 5 6 6 6 6 5 | 15 | 5 5 6 5 5 7 6 | 16 | 6 5 5 5 5 6 5 | 17 | 6 6 6 5 5 8 6 | 18 | 5 5 5 6 6 6 6 | 19 | 6 6 6 6 6 8 5 | 20 | 6 5 6 5 6 7 6 | 21 | 5 5 5 5 5 5 5 | 22 | 5 5 5 5 5 6 5 | 23 | 6 5 6 5 5 6 5 | 24 | 5 5 5 5 5 9 7 | 26 | 4 4 4 4 4 3 3 | 27 | 6 6 6 6 6 8 6 | 28 | 5 5 6 5 5 9 6 | 29 | 5 6 5 6 5 5 5 | 30 | 4 4 4 4 4 6 4 | 31 | 7 5 5 5 6 6 5 | 32 | 5 5 5 5 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 2.1578.0 GPS week: 1578 Day: 0 MJD: 55290.000 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 247| 0 1 1 35 11 36 -.24 9 8 | -683 407 26 85 | 8 -50 | emr 86| 0 0 0 49 -33 -13 .47 20 20 | -3852 2286 29 99 | -81 -107 | esa 140| 2 1 0 -131 36 -53 .30 8 7 | -457 618 18 87 | 8 -25 | gfz 199| -1 0 0 -66 -196 0 -.12 13 13 | 61 -12 26 101 | -71 -52 | grg 105| 0 2 5 -111 -142 33 .90 27 24 | -453 933 83 208 | 89 9 | igr n/a| -1 0 -1 12 47 15 -.02 6 6 | 9230 1975 21 69 | -51 -54 | jpl 131| 0 -2 0 -82 13 63 .51 22 22 | -1370 2332 22 108 | 61 -70 | mit 259| 0 -3 -1 2 -136 -15 -.38 12 12 | -15676 1375 29 151 | 8 59 | ngs 213| 0 -1 0 199 200 4 -.21 11 8 | 15583 -4522 1776 3689 | -51 -5 | sio 260| 0 1 4 2 -429 -580 -.23 22 20 | --- --- --- --- | -65 207 | Table 2.1578.1 GPS week: 1578 Day: 1 MJD: 55291.000 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 247| 0 1 2 47 2 37 -.17 9 8 | 72 -873 21 75 | 9 -8 | emr 86| 0 2 1 15 -23 22 .50 21 21 | -2356 1639 24 87 | -62 -63 | esa 140| 0 2 -2 -138 -2 -61 .33 8 8 | -2079 2632 20 93 | 9 58 | gfz 199| -1 0 -3 -45 -126 -19 -.14 12 12 | 673 -635 30 108 | -72 5 | grg 105| 0 2 3 -85 -87 29 .93 28 22 | 348 -402 101 238 | 76 1 | igr n/a| 0 0 -1 19 18 19 .03 5 5 | 10657 1288 21 69 | -30 0 | jpl 131| -2 1 0 -90 11 34 .51 21 21 | 417 1422 19 106 | 39 -38 | mit 259| 2 -2 0 -28 -71 13 -.38 11 10 | -14970 1529 30 134 | 10 42 | ngs 213| 0 -3 1 186 158 2 -.21 10 7 | 15969 -7600 2099 3963 | 24 14 | sio 260| 2 2 6 -5 -366 -558 -.22 21 19 | --- --- --- --- | -84 193 | Table 2.1578.2 GPS week: 1578 Day: 2 MJD: 55292.000 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 247| 0 0 1 40 -22 4 -.18 9 9 | -554 5 20 79 | 28 1 | emr 86| 0 2 2 -1 -67 1 .47 19 19 | -538 1178 20 81 | -38 -35 | esa 140| 0 0 -2 -161 -19 -56 .29 9 8 | -901 573 20 104 | 54 77 | gfz 199| 0 -1 -1 61 17 -19 -.07 14 14 | 283 -423 28 113 | -60 37 | grg 105| -1 0 4 -50 -129 22 .84 29 25 | 5 -204 79 211 | -12 117 | igr n/a| 0 0 -2 15 -17 -10 .01 7 7 | 12222 574 20 64 | -7 10 | jpl 131| -1 -1 0 -75 -2 63 .45 20 20 | 2040 940 21 129 | 55 12 | mit 259| 1 -2 0 22 -26 28 -.37 11 10 | -15145 1757 27 169 | -9 19 | ngs 213| -1 0 1 124 111 7 -.17 12 8 | 15088 -5005 2397 3565 | 47 163 | sio 260| 1 3 4 53 -341 -540 -.24 21 17 | --- --- --- --- | -94 198 | Table 2.1578.3 GPS week: 1578 Day: 3 MJD: 55293.000 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 247| 0 0 3 31 -3 -7 -.19 9 8 | -625 185 21 71 | 55 7 | emr 86| 0 3 1 -56 -73 8 .52 20 20 | 223 3365 22 101 | 5 -24 | esa 140| 1 1 -4 -159 -31 -42 .30 8 8 | 436 -2479 14 83 | 45 55 | gfz 199| 0 0 -4 94 -7 -2 -.08 14 14 | 5 244 26 98 | -28 32 | grg 105| -2 2 0 -67 -108 18 .94 25 24 | -97 129 79 241 | 24 77 | igr n/a| -1 0 -1 22 -24 -14 .05 5 5 | 12433 2285 19 76 | -2 20 | jpl 131| -1 0 -1 -85 -11 79 .49 21 21 | 2540 2742 19 132 | 44 41 | mit 259| 0 -1 0 18 -16 35 -.41 12 10 | -14728 1464 23 139 | -17 10 | ngs 213| -1 -1 2 131 88 -12 -.12 11 7 | 14982 -4643 2029 3762 | 48 165 | sio 260| 0 2 5 47 -354 -542 -.25 21 16 | --- --- --- --- | -92 199 | Table 2.1578.4 GPS week: 1578 Day: 4 MJD: 55294.000 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 247| -1 1 0 33 -3 -9 -.16 9 8 | -431 -179 22 72 | 33 14 | emr 86| 1 0 0 -44 -33 30 .49 20 20 | 2926 1836 23 116 | -4 -47 | esa 140| 3 0 0 -194 -40 -60 .23 10 10 | 649 -2051 15 89 | 59 89 | gfz 199| 0 0 0 97 -65 -6 -.03 11 11 | -13 -21 22 88 | -56 29 | grg 105| 0 3 0 -77 -129 14 .99 26 25 | 339 -253 73 236 | 6 61 | igr n/a| -2 -1 0 -17 18 27 .07 5 5 | 14122 569 17 71 | -32 7 | jpl 131| -2 0 -3 -73 0 54 .56 21 21 | 4662 1122 17 102 | 34 2 | mit 259| 0 0 -1 -4 -37 17 -.35 11 11 | -14263 1585 18 147 | -13 18 | ngs 213| -1 -2 2 125 140 25 -.18 10 7 | 14414 -3063 1870 3830 | 94 112 | sio 260| -2 0 2 16 -353 -554 -.18 19 16 | --- --- --- --- | -81 192 | Table 2.1578.5 GPS week: 1578 Day: 5 MJD: 55295.000 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 247| 0 1 0 24 -21 -30 -.22 9 8 | -979 728 26 99 | 51 13 | emr 86| 4 -1 5 9 -34 31 .43 18 18 | 3864 -1224 15 86 | -53 -64 | esa 140| 3 0 -1 -178 -61 -31 .22 9 9 | 442 -1582 18 100 | 44 91 | gfz 199| -5 6 -2 75 -101 -15 -.08 82 82 | -551 1360 34 116 | -21 51 | grg 105| 2 0 1 -111 -66 5 .92 25 22 | 7 -174 67 225 | 47 -12 | igr n/a| 0 0 0 25 0 4 .01 6 6 | 13884 -2189 20 56 | -49 11 | jpl 131| -4 0 -1 -51 -4 60 .51 21 21 | 4998 -1222 18 98 | 4 -3 | mit 259| 0 -1 0 9 -26 14 -.36 11 10 | -14746 1277 22 161 | -15 16 | ngs 213| -2 -2 0 155 149 15 -.17 11 9 | 11559 -534 2106 3140 | -18 87 | sio 260| -1 0 1 21 -365 -566 -.16 22 20 | --- --- --- --- | -85 189 | Table 2.1578.6 GPS week: 1578 Day: 6 MJD: 55296.000 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 247| 0 0 0 28 -42 -4 -.21 8 8 | -369 -674 19 60 | 32 28 | emr 86| 1 0 6 0 -41 51 .46 19 19 | 3219 -757 16 77 | -28 -64 | esa 140| 2 0 -4 -181 -26 -27 .27 10 9 | 603 -3228 13 86 | 29 84 | gfz 199| 1 -1 0 59 -74 -18 -.08 14 13 | 98 -222 21 99 | -40 53 | grg 105| -1 0 4 -70 -144 14 .92 26 23 | -65 -207 74 208 | 25 59 | igr n/a| -2 0 0 -22 -14 49 .10 7 7 | 12207 -1663 22 58 | 14 10 | jpl 131| -3 -1 0 -80 -26 71 .48 19 18 | 4175 -380 17 110 | 33 21 | mit 259| 0 1 1 -5 -28 10 -.36 14 12 | -11620 1562 23 164 | -11 19 | ngs 213| -1 -2 1 132 155 -12 -.19 10 7 | 14388 -4841 2046 3317 | 37 50 | sio 260| -1 2 3 11 -385 -560 -.20 21 18 | --- --- --- --- | -82 203 | 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 3.1578.0 GPS week: 1578 Day: 0 MJD: 55290.000 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 | 15 --- --- --- --- 23 --- 18 29 --- 15 | 31 --- --- --- --- 34 --- 35 45 --- 33 2E | 9 20 7 9 23 4 26 16 12 14 5 | 15 25 17 22 25 16 24 19 21 16 16 3 | 8 15 6 12 17 7 15 16 8 17 4 | 25 27 33 30 31 26 26 33 35 30 27 4E | 12 18 6 13 28 7 17 10 16 24 5 | 119 124 119 120 129 122 126 122 118 125 120 5 | 9 21 7 16 26 6 23 10 11 23 5 | 26 36 30 40 42 27 35 30 34 26 29 6 | 8 15 7 11 18 4 16 12 6 17 4 | 33 36 40 39 37 34 35 40 39 40 35 7E | 10 15 8 16 20 4 17 13 12 20 5 | 51 49 53 50 54 51 52 52 60 50 52 8 | 14 14 10 14 17 4 13 5 11 22 4 | 36 36 38 36 40 35 37 40 47 39 38 10 | 6 11 4 13 17 6 12 16 9 15 4 | 29 24 26 29 19 28 23 37 36 24 29 11E | 9 18 8 15 35 9 22 8 10 15 5 | 15 32 25 27 41 20 30 22 25 23 21 12 | 8 24 8 9 23 6 18 10 9 28 4 | 26 32 32 28 44 29 32 29 31 26 29 13 | 7 16 5 15 44 4 21 10 6 10 4 | 17 28 20 20 51 19 32 21 21 16 18 14 | 8 24 7 15 25 4 26 10 11 21 5 | 20 28 24 30 39 20 28 21 24 20 22 15 | 8 22 10 12 29 4 25 8 12 21 5 | 20 34 31 29 42 26 35 23 30 20 25 16 | 10 21 6 12 27 5 27 13 12 30 5 | 20 25 24 21 29 17 28 21 25 21 19 17 | 9 23 9 12 31 9 28 19 12 25 6 | 30 31 26 33 32 30 35 23 30 24 25 18 | 6 20 9 11 25 4 28 9 8 25 5 | 22 31 26 29 34 23 32 25 24 27 23 19 | 8 28 10 16 25 8 31 10 10 20 6 | 18 37 19 20 38 19 40 18 28 18 21 20 | 6 22 7 17 36 6 25 15 11 21 5 | 29 40 35 40 44 32 40 37 31 32 32 21E | 9 17 7 11 24 6 24 7 11 18 4 | 17 23 21 18 35 18 25 16 25 23 18 22 | 6 19 7 12 28 5 29 14 9 28 5 | 25 29 28 31 36 24 28 27 29 31 25 23 | 9 23 7 13 42 5 25 14 8 17 5 | 17 31 21 23 42 18 32 20 19 14 18 24E | 12 17 9 12 23 5 14 12 10 23 5 | 106 103 104 108 100 106 104 110 111 100 106 26 | 6 17 6 7 26 5 14 10 8 17 3 | 23 23 27 26 28 24 24 25 26 18 24 27E | 10 23 10 12 19 9 18 10 21 18 6 | 29 34 37 40 38 31 34 34 40 33 32 28 | 7 21 8 14 47 7 21 12 9 39 5 | 24 30 30 37 45 26 26 29 31 26 27 29 | 10 22 8 15 22 5 24 9 10 --- 5 | 25 38 31 32 41 28 34 27 31 --- 28 30 | 5 17 5 7 18 5 14 9 12 19 3 | 47 44 52 41 56 45 44 51 50 48 48 31E | 16 25 7 12 22 9 25 18 11 15 6 | 50 59 54 52 54 52 54 44 56 52 51 32 | 10 20 5 16 25 6 16 18 9 24 5 | 12 19 20 24 31 15 22 20 19 19 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 8 13 27 6 22 12 11 22 |T 31 38 35 37 44 33 38 35 38 33 33 WRMS | 8 20 7 13 24 6 22 12 8 20 |NE 24 31 28 30 38 25 31 28 30 25 26 MEDI | 9 20 7 12 25 5 22 10 10 20 |MD 25 32 30 30 40 26 32 27 31 26 27 Table 3.1578.1 GPS week: 1578 Day: 1 MJD: 55291.000 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 --- --- --- --- 32 --- 20 35 --- 20 | 30 --- --- --- --- 36 --- 26 34 --- 25 2E | 9 23 6 11 49 4 22 11 8 14 5 | 14 27 18 19 52 17 22 18 25 18 17 3 | 8 17 6 11 13 5 13 14 8 14 4 | 18 24 23 21 29 21 23 25 26 22 20 4E | 12 17 10 9 23 7 20 10 21 19 6 | 136 143 142 139 148 141 145 141 139 149 140 5 | 10 22 8 13 28 6 24 11 7 30 5 | 27 40 30 34 43 28 37 24 28 23 27 6 | 8 19 6 10 14 4 13 12 8 16 4 | 30 35 37 39 39 34 33 36 36 33 34 7E | 9 21 11 13 17 5 17 12 8 13 5 | 25 34 26 26 31 25 31 28 30 25 25 8 | 11 17 9 12 12 5 12 13 11 22 4 | 32 37 34 31 39 31 35 34 32 36 32 10 | 8 15 6 10 18 5 13 19 12 17 5 | 28 28 24 29 20 27 25 33 33 28 27 11E | 11 20 10 17 26 5 17 17 8 11 5 | 16 29 24 25 39 21 28 26 28 24 21 12 | 8 22 8 11 25 6 19 9 10 27 4 | 18 31 25 23 40 20 29 17 22 17 20 13 | 7 21 8 12 35 7 22 9 5 10 4 | 14 30 21 17 44 16 30 17 20 15 17 14 | 10 24 8 14 37 4 26 8 7 16 5 | 18 25 18 22 39 16 25 16 21 16 16 15 | 11 21 8 10 31 4 26 12 9 18 5 | 19 34 26 31 39 25 32 24 24 25 22 16 | 9 22 8 12 23 4 22 15 7 34 5 | 14 25 19 20 31 14 25 16 18 17 13 17 | 9 26 12 16 33 5 29 9 11 26 6 | 26 27 16 30 28 21 27 22 25 23 20 18 | 6 23 8 11 26 4 25 8 5 23 5 | 26 36 31 26 40 27 36 24 32 30 27 19 | 7 27 8 13 23 7 28 9 9 19 5 | 14 34 20 22 33 16 32 16 20 14 17 20 | 5 24 7 14 33 6 26 11 10 19 5 | 30 40 35 32 46 30 40 33 37 31 33 21E | 12 18 5 10 53 2 21 8 8 12 4 | 23 27 23 23 52 20 27 20 25 19 20 22 | 7 21 9 12 28 6 26 11 8 25 5 | 22 31 26 24 38 22 30 23 29 29 22 23 | 7 27 6 12 42 6 26 9 7 18 5 | 17 32 21 18 46 17 30 16 20 15 17 24E | 11 21 7 12 26 5 13 11 8 22 4 | 100 96 99 107 87 99 93 102 100 96 99 26 | 7 16 6 7 24 5 14 8 9 14 3 | 15 21 18 18 23 16 19 19 20 12 16 27E | 10 25 13 12 17 6 17 9 20 --- 6 | 16 27 28 23 28 19 26 19 28 --- 18 28 | 7 24 9 13 24 6 21 8 8 39 5 | 21 29 23 25 35 20 28 22 26 28 21 29 | 16 21 8 15 23 4 25 9 12 --- 6 | 39 43 37 36 45 36 35 34 40 --- 36 30 | 7 14 7 9 16 3 15 8 10 19 3 | 35 36 38 33 45 34 38 37 38 35 35 31E | 6 22 7 9 20 7 22 12 8 11 4 | 22 33 27 29 30 24 28 21 31 21 24 32 | 9 20 6 13 26 4 18 17 6 19 5 | 12 21 17 20 24 13 21 25 18 20 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 21 8 12 28 5 21 11 10 21 |T 28 37 31 32 42 29 35 30 33 30 29 WRMS | 8 21 8 12 22 5 21 10 7 19 |NE 22 31 25 26 36 23 29 24 27 22 22 MEDI | 9 21 8 12 25 5 21 11 8 19 |MD 22 31 25 25 39 21 30 24 28 23 21 Table 3.1578.2 GPS week: 1578 Day: 2 MJD: 55292.000 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 | 18 --- --- --- --- 30 --- 14 31 --- 15 | 24 --- --- --- --- 34 --- 25 35 --- 25 2E | 11 14 10 9 48 5 23 14 10 13 5 | 12 22 15 16 47 15 22 15 20 16 14 3 | 8 13 9 10 18 9 15 11 15 13 4 | 20 26 29 27 29 22 23 27 28 25 23 4E | 16 25 11 14 31 8 19 15 25 44 7 | 130 131 132 129 142 131 135 121 135 120 128 5 | 9 21 8 18 34 7 21 9 10 27 5 | 25 38 29 35 38 29 34 24 29 23 26 6 | 9 12 8 10 18 7 16 10 16 10 4 | 22 25 31 27 31 25 25 31 31 28 26 7E | 6 20 10 14 25 8 20 19 14 20 5 | 31 41 35 30 39 31 38 34 30 31 32 8 | 13 17 8 16 18 6 13 14 7 24 5 | 31 37 30 33 36 27 33 28 26 36 29 10 | 8 10 5 19 21 8 13 13 9 19 4 | 30 27 25 31 20 28 23 33 31 27 27 11E | 7 16 10 18 20 7 15 15 12 14 5 | 19 31 20 32 37 21 30 25 25 26 21 12 | 9 21 10 14 25 6 19 11 9 28 5 | 21 33 24 30 39 22 30 21 23 18 22 13 | 8 18 6 15 56 9 26 9 9 13 5 | 20 33 24 21 53 22 32 17 19 16 19 14 | 9 25 10 15 24 6 23 11 12 18 6 | 20 27 26 26 35 19 25 19 24 19 19 15 | 8 23 8 10 34 7 22 13 12 18 5 | 21 31 26 21 35 23 26 20 19 18 21 16 | 9 19 5 10 23 9 22 10 15 31 5 | 19 26 21 19 30 16 24 18 26 18 18 17 | 9 21 9 16 31 5 24 8 10 28 5 | 26 26 18 20 24 22 27 22 24 22 19 18 | 8 22 10 10 26 5 24 9 9 22 5 | 22 33 26 26 37 22 31 20 19 22 22 19 | 7 24 11 14 24 6 28 9 15 17 6 | 14 29 13 20 33 14 31 13 20 15 14 20 | 7 21 9 18 37 7 25 12 6 20 5 | 28 38 36 35 46 31 38 31 33 27 31 21E | 9 17 8 11 24 7 21 9 6 9 4 | 12 23 16 13 30 11 20 12 19 12 12 22 | 6 20 10 12 28 6 26 9 11 22 5 | 25 30 28 26 36 24 29 24 24 25 24 23 | 8 21 9 15 42 9 26 9 8 19 5 | 22 32 23 23 42 21 29 16 19 16 19 24E | 10 21 6 13 22 5 13 11 7 22 4 | 90 82 86 89 71 87 83 92 90 79 88 26 | 6 13 7 7 23 5 14 8 8 13 3 | 23 23 26 21 26 22 21 25 22 17 22 27E | 9 23 8 10 25 9 16 9 23 18 5 | 23 32 29 28 37 26 29 26 33 27 24 X28 | 9 24 8 17 26 7 --- 9 14 --- 6 | 21 33 28 29 38 23 --- 24 28 --- 24 29 | 11 20 9 15 26 7 21 8 10 --- 5 | 30 37 34 35 36 32 29 34 37 --- 32 30 | 5 13 6 9 18 7 11 9 10 20 3 | 29 36 34 36 43 31 36 30 30 25 32 31E | 5 17 8 9 21 5 20 10 11 12 4 | 32 39 34 29 40 34 37 30 44 31 33 32 | 9 17 5 18 22 8 16 13 10 17 5 | 18 23 19 21 25 18 22 24 22 19 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 9 14 29 7 20 11 12 21 |T 28 36 31 32 40 29 34 29 32 28 28 WRMS | 9 19 8 14 25 7 20 10 8 17 |NE 22 30 26 26 34 23 28 23 25 21 23 MEDI | 9 20 8 14 25 7 20 10 10 19 |MD 22 32 26 27 37 23 29 24 26 23 23 Table 3.1578.3 GPS week: 1578 Day: 3 MJD: 55293.000 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 | 14 --- --- --- --- 29 --- 16 29 --- 14 | 21 --- --- --- --- 33 --- 27 35 --- 21 2E | 10 21 12 12 20 5 27 22 10 13 6 | 19 31 24 16 23 19 28 16 18 19 19 3 | 6 15 7 11 15 5 14 9 8 11 3 | 21 24 25 28 27 22 20 28 27 27 22 4E | 20 21 15 17 29 6 20 23 26 47 8 | 143 154 150 148 161 147 156 153 142 167 148 5 | 10 21 8 17 27 6 23 13 13 22 5 | 25 40 31 38 41 29 35 28 35 30 28 6 | 6 16 7 12 17 5 18 10 8 8 4 | 32 32 35 39 33 33 28 38 36 36 33 7E | 7 19 8 17 18 7 20 11 9 14 5 | 35 44 41 36 46 39 44 37 38 35 37 8 | 13 16 7 16 12 6 14 15 9 26 5 | 35 42 41 37 41 36 40 42 37 38 37 10 | 7 14 5 15 16 4 11 7 8 12 3 | 29 26 25 30 17 26 23 33 31 23 27 11E | 8 21 9 12 20 5 20 11 8 16 4 | 19 31 24 26 32 21 28 21 24 24 22 12 | 9 20 9 16 22 4 21 9 11 26 5 | 23 30 23 27 36 23 29 25 26 21 23 13 | 8 17 6 13 46 4 24 9 7 13 4 | 16 32 26 17 49 18 28 17 19 13 19 14 | 9 28 8 15 22 4 25 9 8 15 5 | 15 30 24 26 34 20 30 22 18 20 19 15 | 8 22 7 16 27 5 23 13 10 17 5 | 19 29 27 28 36 23 28 24 20 21 21 16 | 5 22 7 9 24 6 23 13 10 30 5 | 17 26 24 21 30 17 27 21 22 20 17 17 | 6 19 10 15 29 4 24 7 11 27 5 | 24 24 16 22 26 19 25 21 22 24 19 18 | 7 25 10 15 28 5 27 10 8 21 5 | 18 34 24 26 36 22 33 21 22 22 21 19 | 7 24 11 14 25 6 28 9 9 19 5 | 14 31 15 19 33 16 31 14 21 17 15 20 | 5 25 8 16 34 7 25 10 9 18 5 | 28 42 36 34 45 30 40 32 28 29 31 21E | 10 20 6 12 32 6 23 9 13 10 5 | 15 29 22 18 40 16 28 17 26 19 18 22 | 7 23 9 13 31 6 23 11 7 18 5 | 19 32 24 24 37 21 29 24 22 24 21 23 | 7 21 9 13 38 4 26 8 8 18 5 | 16 29 24 20 39 18 27 15 17 14 17 24E | 9 18 8 14 18 5 14 10 15 20 5 | 104 101 103 108 97 104 100 108 104 99 103 26 | 5 15 8 10 21 4 14 8 9 13 3 | 18 23 23 20 29 19 21 21 18 16 18 27E | 9 25 9 11 23 6 16 11 18 17 5 | 24 31 32 35 39 27 31 27 34 24 26 28 | 8 20 7 18 27 5 22 10 8 37 5 | 20 32 24 29 32 20 26 24 21 25 21 X29 | 8 23 9 11 30 7 --- 19 13 --- 6 | 80 88 83 79 77 79 --- 77 81 --- 80 30 | 7 14 9 8 17 5 12 11 5 19 4 | 40 43 41 39 48 39 41 44 39 40 39 31E | 6 22 8 7 19 5 17 9 11 11 4 | 30 42 34 36 40 34 39 31 34 31 32 32 | 7 20 7 16 18 5 18 12 9 14 5 | 12 21 17 19 25 13 21 17 18 15 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 8 14 25 5 21 12 11 21 |T 31 40 35 36 43 32 37 34 34 31 32 WRMS | 8 20 8 14 24 5 21 10 7 16 |NE 24 33 28 29 36 25 28 27 27 23 25 MEDI | 7 21 8 14 23 5 21 10 9 17 |MD 21 31 25 28 36 22 28 24 26 24 21 Table 3.1578.4 GPS week: 1578 Day: 4 MJD: 55294.000 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 | 9 --- --- --- --- 15 --- 16 13 --- 9 | 23 --- --- --- --- 32 --- 25 34 --- 25 2E | 10 17 10 8 --- 5 25 18 10 12 5 | 12 24 16 15 --- 11 24 15 19 14 12 3 | 6 14 7 8 22 4 13 10 8 12 3 | 15 24 24 24 32 19 19 21 25 21 19 4E | 11 20 10 11 27 9 18 9 18 16 5 | 112 119 117 118 131 114 123 112 112 118 114 5 | 14 18 10 13 28 7 21 12 7 18 5 | 29 34 28 40 42 25 35 27 30 25 26 6 | 6 16 10 10 21 4 16 10 7 8 4 | 21 27 28 30 33 22 19 26 28 24 23 7E | 8 18 10 14 17 6 18 9 8 11 4 | 27 35 23 24 36 25 33 26 27 25 24 8 | 14 21 9 13 18 5 14 16 10 25 5 | 33 45 39 37 38 35 40 39 38 38 35 10 | 9 9 6 7 17 5 10 13 8 14 3 | 32 33 32 30 24 32 27 41 37 30 33 11E | 8 17 10 10 20 7 17 11 9 17 4 | 24 35 30 42 39 27 33 29 31 31 26 12 | 11 19 9 14 23 5 20 9 9 26 5 | 19 29 28 32 38 24 30 22 28 17 24 13 | 5 19 10 10 39 4 24 9 10 13 5 | 15 28 21 22 44 16 29 14 23 11 16 14 | 8 26 9 17 25 4 25 9 9 16 5 | 17 28 15 24 33 15 25 17 21 15 15 15 | 7 18 8 11 33 6 20 11 11 17 4 | 15 27 21 24 39 18 26 21 22 18 17 16 | 9 21 8 10 25 4 24 12 10 29 5 | 16 24 20 24 33 16 26 21 23 19 16 17 | 6 18 10 12 28 7 24 13 6 30 5 | 21 21 14 27 25 17 23 23 22 27 17 18 | 6 25 12 13 29 4 26 10 7 23 5 | 16 32 24 22 38 18 31 20 21 20 19 19 | 6 25 14 13 39 5 28 8 7 20 5 | 11 27 13 24 42 10 30 10 20 13 10 20 | 7 24 12 12 31 6 27 13 7 17 5 | 21 35 28 27 40 23 36 24 24 22 23 21E | 10 17 9 10 25 3 23 8 8 16 4 | 12 27 25 19 33 16 25 15 18 20 17 22 | 6 21 10 11 32 4 24 12 6 18 5 | 17 26 21 22 37 17 25 23 22 22 18 23 | 8 23 9 12 41 5 27 8 10 17 5 | 14 29 21 34 41 15 28 15 21 13 15 24E | 11 17 11 11 21 4 14 6 12 23 4 | 91 82 88 84 79 89 84 92 95 81 88 26 | 8 13 6 8 23 4 12 9 7 14 3 | 13 21 14 16 26 14 19 15 19 12 13 27E | 9 22 10 11 23 7 13 15 20 20 6 | 16 26 21 25 33 18 22 21 30 20 16 28 | 8 19 11 10 25 4 21 16 6 38 5 | 18 26 20 35 30 18 25 22 22 22 17 29 | 9 23 11 11 26 4 24 9 10 --- 5 | 37 38 30 33 40 31 51 35 32 --- 32 30 | 6 13 9 7 14 3 12 9 8 18 3 | 31 34 39 42 42 32 34 32 37 27 34 31E | 9 32 9 10 24 4 24 8 9 11 5 | 22 39 18 26 36 20 31 23 25 21 20 32 | 8 21 8 15 20 6 19 13 9 14 5 | 15 21 16 23 25 15 20 23 22 18 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 10 11 26 5 21 11 10 19 |T 25 34 28 32 40 26 33 28 30 26 26 WRMS | 8 20 10 11 25 5 21 11 7 16 |NE 19 28 22 27 35 20 27 22 25 19 20 MEDI | 8 19 10 11 25 5 21 10 9 17 |MD 18 28 23 26 37 18 28 23 24 21 19 Table 3.1578.5 GPS week: 1578 Day: 5 MJD: 55295.000 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 | 15 --- --- --- --- 23 --- 16 29 --- 15 | 20 --- --- --- --- 32 --- 19 34 --- 20 X2E | 4 --- --- 16 --- 33 --- --- --- --- 6 | 10 --- --- 16 --- 14 --- --- --- --- 6 3 | 8 13 7 45 12 6 13 8 11 14 4 | 16 25 23 47 22 19 20 20 23 22 19 4E | 10 21 10 33 25 8 17 13 19 23 6 | 92 99 93 93 109 93 100 89 89 98 92 5 | 10 20 8 107 28 10 24 12 9 24 8 | 28 34 27 106 41 25 34 31 33 27 28 6 | 8 14 6 105 14 6 14 6 11 9 6 | 27 31 31 105 26 28 26 30 33 29 29 7E | 7 16 12 47 12 8 19 8 8 11 5 | 25 31 25 53 30 22 32 23 29 23 25 8 | 15 19 8 113 27 7 13 10 10 22 8 | 59 65 63 105 72 59 67 64 62 69 61 X9E | 4 --- --- --- --- --- --- --- --- --- 0 | 79 --- --- --- --- --- --- --- --- --- 76 10 | 7 11 6 28 17 6 12 16 7 13 4 | 32 33 30 30 22 32 26 44 30 30 31 11E | 8 18 9 114 18 4 18 11 11 17 7 | 26 33 29 117 37 24 29 31 27 29 28 12 | 10 19 8 55 19 6 20 12 9 25 6 | 18 29 21 54 35 20 30 21 21 20 20 13 | 7 18 10 86 37 5 24 11 9 14 7 | 15 29 22 77 45 15 29 14 14 11 15 14 | 9 19 11 35 25 4 24 10 13 16 6 | 15 24 17 33 33 14 25 16 19 16 14 15 | 9 22 9 67 27 8 22 12 11 20 6 | 21 29 24 63 37 19 29 26 22 20 20 16 | 8 18 7 72 20 6 21 11 9 29 6 | 15 25 18 70 33 15 27 19 18 16 17 17 | 7 21 11 96 27 4 26 13 13 29 7 | 21 23 13 85 24 16 24 23 23 26 17 18 | 9 21 8 40 31 5 24 14 7 27 5 | 16 30 19 40 35 16 29 19 19 19 17 19 | 7 21 14 103 23 9 27 7 10 21 8 | 16 26 17 95 30 12 31 16 21 17 16 20 | 8 21 14 78 30 5 26 12 10 18 7 | 24 38 27 79 45 24 36 27 28 19 26 21E | 9 16 5 25 26 5 21 9 9 45 4 | 13 24 18 20 34 14 25 15 19 46 15 22 | 7 20 8 30 29 6 23 15 8 22 5 | 17 27 16 33 34 15 25 20 21 22 15 23 | 7 21 12 159 38 6 27 9 10 18 6 | 13 27 21 135 42 14 26 14 15 13 13 24E | 13 15 12 143 24 8 15 13 11 30 9 | 108 102 103 184 93 106 102 111 110 102 107 26 | 6 12 6 20 23 5 12 6 6 14 3 | 16 20 20 21 25 15 20 18 20 15 16 27E | 9 21 11 98 17 6 14 13 22 16 8 | 14 25 22 85 31 16 22 19 26 18 16 28 | 7 20 10 123 23 8 22 13 8 38 8 | 12 29 17 105 31 17 24 20 20 22 15 29 | 8 18 8 28 25 4 26 9 10 --- 5 | 49 51 48 63 47 49 40 51 53 --- 50 30 | 8 13 7 69 15 5 15 13 8 17 5 | 32 39 39 57 46 34 39 35 37 32 35 31E | 5 17 9 64 30 5 21 9 7 12 5 | 18 28 17 54 36 17 26 23 21 20 18 32 | 8 16 11 33 18 5 19 6 10 16 5 | 19 21 16 37 29 16 21 20 24 19 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 9 82 25 6 21 11 11 22 |T 28 35 29 71 40 27 34 30 31 29 28 WRMS | 8 18 9 82 22 6 21 10 9 20 |NE 21 29 23 66 34 21 28 23 25 20 21 MEDI | 8 18 9 67 24 6 21 11 10 18 |MD 19 29 22 63 34 17 27 21 23 22 19 Table 3.1578.6 GPS week: 1578 Day: 6 MJD: 55296.000 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 | 13 --- --- --- --- 26 --- 20 17 --- 11 | 29 --- --- --- --- 24 --- 38 21 --- 28 X2E | 12 --- 11 11 3315 7 30 27 8 15 7 | 10 --- 4 6 115 10 19 5 6 6 6 3 | 7 14 7 10 17 5 12 11 9 15 4 | 17 24 24 31 25 20 19 27 27 27 21 4E | 12 18 13 15 38 8 18 20 16 25 6 | 112 120 119 114 143 115 123 113 109 122 114 5 | 7 23 9 18 27 8 24 11 9 22 5 | 27 37 28 36 40 28 35 28 26 31 27 6 | 7 16 7 10 18 5 13 8 8 10 3 | 28 29 33 51 29 28 26 35 34 33 30 7E | 6 18 12 18 21 7 20 8 8 11 5 | 38 44 41 40 49 40 43 38 39 36 38 8E | 14 21 10 19 27 7 14 21 9 28 6 | 41 53 44 56 55 45 51 46 43 49 43 X9E | 16 --- 18 --- --- 17 --- 28 --- --- 14 | 52 --- 5 --- --- 11 --- 6 --- --- 45 10 | 6 15 9 12 19 5 12 27 9 13 5 | 31 29 31 36 25 30 27 38 34 27 29 11E | 7 18 9 14 23 10 16 12 9 18 4 | 32 41 37 50 45 34 41 40 34 46 35 12 | 9 19 9 11 20 7 17 13 8 25 4 | 19 31 26 32 39 23 31 25 21 20 22 13 | 8 17 9 13 42 7 21 11 6 13 4 | 16 27 20 33 45 16 27 16 16 11 15 14 | 8 20 8 12 27 6 19 12 10 20 5 | 21 27 25 28 35 20 28 23 20 23 21 15 | 11 23 11 20 30 7 22 12 9 21 6 | 18 28 27 31 35 23 26 26 22 18 20 16 | 8 19 9 14 24 5 21 14 8 32 5 | 17 23 19 27 29 16 24 19 21 17 15 17 | 8 19 15 14 29 7 22 14 11 27 5 | 24 26 19 39 26 20 24 24 25 26 20 18 | 7 22 8 14 28 9 23 14 9 31 5 | 22 33 26 34 40 23 36 28 27 23 24 19 | 7 23 13 11 23 9 25 10 6 24 5 | 15 28 16 32 30 16 31 18 20 22 15 20 | 8 21 10 11 32 9 26 16 9 17 5 | 23 38 30 37 45 25 35 29 28 20 26 21E | 6 18 8 12 20 9 22 15 8 10 5 | 16 24 20 17 32 15 26 17 17 16 15 22 | 7 19 10 11 31 9 21 17 11 25 5 | 22 30 27 33 37 21 30 30 27 27 23 23 | 8 19 10 12 35 6 24 12 8 18 5 | 17 27 21 49 38 19 26 17 20 15 16 24E | 11 16 15 19 15 8 18 21 17 23 6 | 123 120 125 145 110 121 118 127 121 118 122 26 | 6 12 6 9 17 7 9 5 7 15 3 | 17 17 19 20 23 15 20 18 19 12 16 27E | 9 20 11 17 15 6 14 13 21 17 6 | 26 30 35 31 40 27 30 27 35 25 27 28 | 6 20 10 15 26 7 20 18 8 41 5 | 20 29 27 42 34 23 26 28 25 30 23 29 | 8 19 10 11 23 8 21 9 9 --- 4 | 35 38 35 39 33 35 31 36 38 --- 34 30 | 7 12 8 7 15 5 9 19 7 16 4 | 38 45 45 40 51 40 45 47 38 40 42 31E | 7 17 6 9 27 10 21 11 10 11 4 | 37 46 39 30 46 42 46 38 41 39 38 32 | 8 17 9 10 18 4 19 11 7 15 4 | 12 20 19 16 24 14 19 21 17 16 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 14 26 7 19 14 10 21 |T 30 38 32 40 45 30 36 33 32 31 31 WRMS | 8 19 9 13 23 7 18 12 7 18 |NE 22 29 25 34 34 22 28 27 25 23 22 MEDI | 8 19 9 12 24 7 20 13 9 18 |MD 23 29 27 34 38 23 30 28 26 25 24 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 4.1578 GPS week: 1578 MJD: 55290.0-55296.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2868 |U 9 7 20 |U 9 11 25 |U 8 7 19 | emr | emr 2741 | 10 9 29 |U 9 11 29 | 13 10 26 | esa | esa 2783 | 9 8 23 |U 9 10 27 | 8 8 19 | gfz | gfz 2754 |U 8 7 22 |U 9 12 31 |U 8 7 21 | grg | grg 2756 | 18 11 32 |U 10 14 42 | 11 9 26 | igr | igr 2820 | 8 8 24 | 10 13 30 | 9 8 20 | igs | igs 2783 | 9 8 22 | 9 10 28 | 8 8 20 | jpl | jpl 2729 |U 14 9 36 | 9 14 29 |U 12 8 22 | mit | mit 2880 |U 8 8 23 |U 10 12 27 |U 9 9 22 | 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 5.1578.0 GPS week: 1578 Day: 0 MJD: 55290.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2872 | 10 7 22 | 10 9 22 | 8 7 13 | emr | emr 2772 | 11 7 27 | 10 9 20 | 10 8 27 | esa | esa 2784 | 12 11 29 | 10 9 23 | 7 7 15 | gfz | gfz 2770 | 9 6 18 | 11 10 23 | 7 7 17 | grg | grg 2784 | 10 10 22 | 11 16 44 | 8 8 27 | igr | igr 2848 | 10 6 18 | 11 10 22 | 7 7 17 | igs | igs 2840 | 12 10 22 | 11 9 25 | 7 7 17 | jpl | jpl 2770 | 11 10 28 | 11 12 21 | 9 7 21 | mit | mit 2880 | 9 8 20 | 11 10 22 | 9 8 16 | Table 5.1578.1 GPS week: 1578 Day: 1 MJD: 55291.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2865 | 8 7 23 | 12 10 37 | 6 6 15 | emr | emr 2772 | 10 11 32 | 14 9 33 | 14 10 26 | esa | esa 2784 | 9 8 24 | 12 10 35 | 7 7 14 | gfz | gfz 2769 | 7 6 21 | 12 13 49 | 7 6 15 | grg | grg 2784 | 12 11 39 | 11 12 33 | 11 9 29 | igr | igr 2768 | 9 9 32 | 12 10 34 | 7 6 14 | igs | igs 2795 | 9 10 22 | 12 9 37 | 7 6 13 | jpl | jpl 2771 | 9 9 30 | 13 9 37 | 9 7 17 | mit | mit 2880 | 9 9 25 | 12 9 37 | 7 6 20 | Table 5.1578.2 GPS week: 1578 Day: 2 MJD: 55292.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2863 | 6 7 20 | 10 17 32 | 9 9 19 | emr | emr 2765 | 8 9 38 | 10 11 35 | 13 11 20 | esa | esa 2784 | 7 6 31 | 10 15 35 | 10 10 22 | gfz | gfz 2763 | 7 5 30 | 10 14 34 | 10 8 20 | grg | grg 2784 | 10 8 36 | 12 22 50 | 11 11 22 | igr | igr 2831 | 7 6 32 | 11 18 45 | 10 8 20 | igs | igs 2776 | 7 6 32 | 9 13 31 | 10 10 19 | jpl | jpl 2673 | 9 6 31 | 10 29 41 | 29 10 27 | mit | mit 2880 | 7 6 34 | 11 17 30 | 10 10 20 | Table 5.1578.3 GPS week: 1578 Day: 3 MJD: 55293.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2864 | 9 8 19 | 8 9 26 | 6 6 18 | emr | emr 2762 | 11 12 27 | 11 10 32 | 8 7 24 | esa | esa 2784 | 9 9 23 | 8 7 25 | 7 7 19 | gfz | gfz 2764 | 9 8 21 | 9 9 29 | 7 7 21 | grg | grg 2784 | 9 10 30 | 11 9 26 | 7 7 21 | igr | igr 2840 | 8 8 19 | 8 8 27 | 7 6 17 | igs | igs 2811 | 9 8 21 | 8 8 24 | 7 7 17 | jpl | jpl 2676 | 14 12 45 | 10 10 29 | 6 7 20 | mit | mit 2880 | 8 7 22 | 8 8 28 | 8 8 18 | Table 5.1578.4 GPS week: 1578 Day: 4 MJD: 55294.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2875 | 8 6 23 | 7 13 20 | 7 5 23 | emr | emr 2770 | 8 7 25 | 8 18 22 | 16 12 24 | esa | esa 2784 | 8 6 21 | 8 15 19 | 10 6 19 | gfz | gfz 2773 | 8 6 23 | 9 17 21 | 9 6 20 | grg | grg 2688 | 10 9 31 | 12 23 23 | 12 9 22 | igr | igr 2830 | 8 7 27 | 11 28 22 | 10 7 20 | igs | igs 2781 | 8 6 21 | 9 15 21 | 9 7 19 | jpl | jpl 2768 | 9 8 25 | 9 18 22 | 10 6 18 | mit | mit 2880 | 8 6 19 | 10 24 20 | 9 6 20 | Table 5.1578.5 GPS week: 1578 Day: 5 MJD: 55295.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2783 | 17 9 21 | 6 9 22 | 10 6 25 | emr | emr 2674 | 13 10 28 | 7 10 30 | 18 14 34 | esa | esa 2688 | 9 11 19 | 6 7 27 | 10 9 26 | gfz | gfz 2677 | 12 9 24 | 7 13 41 | 11 6 35 | grg | grg 2688 | 8 9 21 | 7 7 37 | 14 9 37 | igr | igr 2694 | 9 11 21 | 7 8 29 | 12 11 30 | igs | igs 2715 | 10 10 23 | 6 8 27 | 10 7 31 | jpl | jpl 2676 | 8 8 19 | 6 8 30 | 13 11 32 | mit | mit 2784 | 12 10 24 | 8 9 31 | 15 13 36 | Table 5.1578.6 GPS week: 1578 Day: 6 MJD: 55296.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2959 | 8 8 13 | 7 12 20 | 8 9 20 | emr | emr 2676 | 10 10 24 | 7 10 29 | 13 10 26 | esa | esa 2879 | 8 7 18 | 7 9 24 | 8 11 19 | gfz | gfz 2768 | 7 6 14 | 8 8 23 | 9 10 21 | grg | grg 2784 | 65 22 44 | 9 10 83 | 11 11 28 | igr | igr 2932 | 7 7 16 | 8 10 27 | 8 10 21 | igs | igs 2766 | 8 8 16 | 7 10 30 | 10 11 23 | jpl | jpl 2771 | 40 9 74 | 6 10 28 | 9 9 21 | mit | mit 2976 | 7 8 19 | 7 10 25 | 9 10 22 | Table 6: Earth Orientation Parameters weekly summary. Weekly mean and standard deviation of Centre ERP, ERP rates and LOD differences with respect to IGS combined values. See Table 7 for the daily summaries. Xpole,Xrt: x pole and x pole rate Ypole,Yrt: y pole and y pole rate LOD : Length Of Day AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A AC LOD BIAS RMS: RMS of AC LOD BIAS FLAG: "u" (used), "x" (excluded), "-" (no submission) for Xpole, Ypole, Xrt, Yrt and LOD Table 6.1578 GPS week: 1578 MJD: 55290.500-55296.500 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 | 33 -25 59 57 1 | 6 15 | 16 16 92 72 6 | 3 emr uuuuu | 91 43 23 288 3 | 58 61 | 9 17 110 89 10 | 7 esa uuuuu | -28 -30 75 -150 -6 | 19 24 | 23 12 115 39 7 | 3 gfz uuuuu | 11 55 -25 -76 6 | 23 28 | 18 21 49 66 7 | 7 grg --xxx | -- -- 22 -209 -2 | 13 16 | -- -- 147 179 21 | 2 igr xxxxx | 33 28 88 -6 -2 | 6 16 | 9 20 74 81 3 | 2 irf xxxxx | 34 6 -73 14 -16 | 7 18 | 28 15 49 31 5 | 3 jpl uuuuu | 39 -33 96 115 0 | 18 27 | 16 25 71 119 11 | 5 mit uuuuu | 7 12 -64 7 -19 | 15 24 | 45 25 79 59 6 | 3 ngs uuuuu | -50 -20 -49 8 6 | 2 14 | 45 33 113 110 5 | 5 sio xxxxx | -164 89 -131 45 -1 | 39 42 | 31 23 56 40 4 | 4 Table 7.1578.0 GPS week: 1578 Day: 0 MJD: 55290.500 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 -27 83 20 -9 | 3 14 emr uuuuu | 85 62 -188 378 14 | 47 50 esa uuuuu | 3 -27 -21 -135 -5 | 14 22 gfz uuuuu | 30 52 19 -31 6 | 12 21 grg --xxx | -- -- 236 66 -22 | 15 19 igr xxxxx | 32 32 0 -32 2 | 3 17 irf xxxxx | -22 -19 -88 12 -14 | 5 19 jpl uuuuu | 48 -80 90 261 2 | 12 25 mit uuuuu | -81 -27 -11 42 -16 | 14 24 ngs uuuuu | -17 32 88 -128 3 | -5 13 sio xxxxx | -229 46 -186 69 1 | 34 38 Table 7.1578.1 GPS week: 1578 Day: 1 MJD: 55291.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 26 -12 152 86 -3 | 3 15 emr uuuuu | 81 59 -23 425 19 | 50 55 esa uuuuu | -40 -12 -19 -150 5 | 16 23 gfz uuuuu | 13 69 -64 -90 2 | 15 24 grg --xxx | -- -- -40 -143 -31 | 14 18 igr xxxxx | 18 27 50 -108 -4 | 3 17 irf xxxxx | 18 -3 -61 10 -16 | 6 20 jpl uuuuu | 56 -42 57 232 6 | 13 26 mit uuuuu | -24 -13 -15 49 -19 | 15 25 ngs uuuuu | 4 -27 64 -71 1 | -3 15 sio xxxxx | -175 81 -141 23 3 | 35 39 Table 7.1578.2 GPS week: 1578 Day: 2 MJD: 55292.500 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 | 55 -15 193 148 4 | 5 16 emr uuuuu | 91 51 96 216 9 | 55 60 esa uuuuu | -21 -41 -1 -84 -8 | 18 26 gfz uuuuu | 19 73 -12 -103 18 | 19 28 grg --xxx | -- -- 104 -459 -17 | 13 17 igr xxxxx | 46 20 236 -90 -1 | 4 18 irf xxxxx | 56 13 -71 56 -17 | 7 20 jpl uuuuu | 44 -42 154 115 -10 | 16 29 mit uuuuu | 37 22 -64 88 -20 | 16 25 ngs uuuuu | -107 -34 -55 -99 7 | -1 16 sio xxxxx | -142 107 -68 72 3 | 37 42 Table 7.1578.3 GPS week: 1578 Day: 3 MJD: 55293.500 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 | 50 -35 -52 63 2 | 7 16 emr uuuuu | 81 15 147 288 -8 | 60 63 esa uuuuu | 2 -25 43 -180 -4 | 20 25 gfz uuuuu | 25 48 -14 -43 12 | 25 29 grg --xxx | -- -- 64 -173 12 | 9 13 igr xxxxx | 37 22 120 -33 -3 | 7 17 irf xxxxx | 57 20 -147 43 -24 | 9 18 jpl uuuuu | 16 -24 167 184 -17 | 19 28 mit uuuuu | 47 37 -207 17 -28 | 18 25 ngs uuuuu | -108 -28 7 15 12 | 2 14 sio xxxxx | -142 112 -182 98 -8 | 40 43 Table 7.1578.4 GPS week: 1578 Day: 4 MJD: 55294.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 34 -8 -43 132 0 | 9 16 emr uuuuu | 95 29 62 185 -6 | 63 65 esa uuuuu | -41 -34 273 -191 -8 | 22 26 gfz uuuuu | 19 81 -21 32 3 | 29 31 grg --xxx | -- -- 54 -136 21 | 11 14 igr xxxxx | 41 57 79 99 2 | 9 16 irf xxxxx | 48 25 -97 -1 -17 | 9 18 jpl uuuuu | 46 -9 79 80 18 | 22 27 mit uuuuu | 30 38 -130 -48 -19 | 18 24 ngs uuuuu | -64 -69 -194 82 3 | 6 13 sio xxxxx | -144 106 -169 31 -1 | 43 45 Table 7.1578.5 GPS week: 1578 Day: 5 MJD: 55295.500 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 | 27 -55 55 -49 3 | 9 16 emr uuuuu | 104 49 -6 219 -4 | 65 66 esa uuuuu | -51 -48 195 -187 -17 | 22 26 gfz uuuuu | -11 17 28 -140 -3 | 30 32 grg --xxx | -- -- -20 -419 6 | 13 17 igr xxxxx | 29 45 55 75 -6 | 9 16 irf xxxxx | 40 -4 16 -40 -17 | 8 18 jpl uuuuu | 43 -8 -32 -31 1 | 25 29 mit uuuuu | 24 11 19 -78 -21 | 17 24 ngs uuuuu | -47 14 -195 161 12 | 7 14 sio xxxxx | -149 81 -44 -26 -6 | 44 46 Table 7.1578.6 GPS week: 1578 Day: 6 MJD: 55296.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 9 -23 24 -2 9 | 6 11 emr uuuuu | 101 37 76 304 0 | 63 65 esa uuuuu | -47 -20 53 -123 -3 | 17 22 gfz uuuuu | -16 49 -113 -156 4 | 28 30 grg --xxx | -- -- -241 -197 17 | 13 17 igr xxxxx | 27 -5 76 48 -4 | 4 13 irf xxxxx | 37 9 -65 19 -7 | 2 14 jpl uuuuu | 16 -24 157 -35 1 | 23 28 mit uuuuu | 18 20 -39 -20 -8 | 10 19 ngs uuuuu | -13 -28 -61 95 4 | 7 13 sio xxxxx | -166 91 -126 51 -2 | 41 42