Date: Thu, 04 Jun 2009 15:05:27 +0000 From: Jim Ray Subject: [IGSREPORT-17462] Wk 1532 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4a27e2b7.GhXurso7zlOs99gO%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 04 Jun 08:05:49 PDT 2009 Message Number 17462 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1532 (May 17, 2009 - May 23, 2009) Contacts: J. Ray (jim.ray@noaa.gov), J. Griffiths (jake.griffiths@noaa.gov) COMBINATION STRATEGY: --------------------- Starting with GPS week 860, the IGS Final orbit combination is done directly in the ITRF without any alignment to the Bulletin B EOP series. Each centre satellite clock corrections are first transformed to a common reference. One of the following two methods can be used (the REMARKS section of this report gives which method is used): [1] For each centre, a clock offset and a drift are estimated with respect to the broadcast clock corrections using only non-SA satellites; [2] A chosen reference centre is aligned to the broadcast clock corrections using all satellites. All other centres are then aligned to that reference centre. The offsets and drifts are used to align each centre satellite clock corrections to GPS time. Ephemerides and clock corrections are then combined as weighted averages computed over all centres. Each centre is given a position weight and a clock weight. The position weights are computed from each centre's absolute deviation to the unweighted average orbit after the estimation of a 7-parameter Helmert transformation. The clock weights are either computed from [1] the absolute deviation of the initial alignment to broadcast clock for the non-SA satellites, or [2] from the absolute deviation of centre's aligned clock corrections with respect to the unweighted mean. Finally, a 7-parameter Helmert transformation and clock offset and drift are estimated for each centre with respect to the combined solutions and parameters and RMS of fit reported. All the above estimations are performed using the L1-norm robust scheme. Each centre ephemerides are also evaluated individually and independently from the orbit combination by using week long arcs. The Earth Orientation Parameters (EOP) used in this evaluation are those submitted by the respective centres. The IGS combined orbits/clocks and all centres providing both orbit and clock solutions are further evaluated by an independent point positioning (navigation) program that uses both phase and pseudorange data. This is primarily intended for testing clock solution precision as well as the orbit/clock consistency. Like the clock solutions broadcast in the navigation message, the combined satellite clocks are corrected for the periodical relativistic correction (see e.g. GPS interface Control document ICD-GPS-200, p.73): -2*(X.V)/c [distance unit], where X and V are the inertial sv state and velocity vectors and c is the speed of light. Also for compatibility, no satellite L1/L2 delay calibration should be applied. SOFTWARE: --------- The weighted average software used was originally developed by T. Springer and G. Beutler in 1993. The GPS long arc orbit analysis software used here for individual centre ephemeris evaluation was developed by Beutler et al. at the Astronomical Institute of the University of Bern (AIUB). For more details on the orbit combination and complete references for both software see: Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS Analysis Centers, Bulletin Geodesique, 69, pp 200-222. Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination and Evaluation, Appendix I of the Analysis Coordinator Report, International GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94. Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report, International GPS Service for Geodynamics (IGS) 1995 Annual Report, pp. 45-76. Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report, International GPS Service for Geodynamics (IGS) 1996 Annual Report, pp. 55-100. PRODUCTS GENERATED: ------------------- The resulting average ephemeris and clocks are output to daily files in SP3 format. The satellite accuracy codes displayed in the header are based on the weighted RMS for each satellite. Note that each file contains all the satellites that appear in any of the centre ephemeris files. If a satellite or centre was excluded from combination, a note in the REMARKS section of this report will identify the exclusion and the reason. The resulting x and y earth rotation parameters (ERP) associated with the IGS ephemeris files and their rates (xrt, yrt) are computed using a weighted average of all available centres (weights are those from the orbit combination). Pole rate combination uses only centres providing estimated pole rates. Starting with GPS wk 0894, IGS LOD combinations were implemented in the Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to the last non-predicted day of Bulletin A. AC LOD biases are removed and the new AC bias-free LODs are used to compute a weighted IGS LOD which in turn is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC values are printed in the IGS Final erp file. The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are: igs1532[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1532[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1532[0-6].cls IGS GPS clock combination summary report. igs15327.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15327.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Duplicate entries can arise due to separate combination runs for the 30-s clocks ACs (listed first) and the 5-min clock ACs (listed second). Day | Centre | PRN/STA list ----+--------+--------------- 0 | ALL | 1 1 0 | COD | 8 9 25 27 8 9 25 27 MATE 0 | EMR | KHAJ MIZU 0 | ESA | 9 25 27 0 | GFZ | 31 UNSA 0 | GRG | USNO 0 | JPL | HARB NLIB 0 | MIT | 5 5 COCO HOB2 1 | ALL | 1 1 1 | COD | 9 25 27 9 25 27 1 | EMR | WTZR WTZR 1 | ESA | 9 25 27 1 | GFZ | 9 31 GOLD HARB 1 | GRG | NLIB NOVM POTS 1 | MIT | 5 8 5 8 USNO BOR1 FLIN HOB2 USNO 2 | ALL | 1 1 30 2 | COD | 9 25 27 9 25 27 2 | EMR | CHUR MIZU WTZR 2 | ESA | 9 25 27 UNSA 2 | GFZ | 9 31 ALGO CHUR FAA1 2 | GRG | NLIB 2 | JPL | 8 2 | MIT | 8 11 30 8 11 HOB2 IRKT 3 | ALL | 1 5 1 5 3 | COD | 9 25 27 9 25 27 HOFN RCMN 3 | EMR | FAIR WTZR 3 | ESA | 8 9 25 27 3 | GFZ | 9 21 31 CHUR FAA1 FAIR ULAB 3 | GRG | NLIB 3 | JPL | DAV1 HARB UNSA 3 | MIT | 10 10 COCO HOB2 4 | COD | 25 27 25 27 MDO1 4 | EMR | 9 MIZU WTZR 4 | ESA | 8 9 25 27 4 | GFZ | CHUR MATE UNSA 4 | GRG | NLIB 4 | JPL | MDO1 4 | MIT | 5 5 COCO HOB2 KERG SANT 4 | NGS | 1 5 | ALL | 1 1 5 | COD | 9 25 27 9 25 27 5 | EMR | MIZU WTZR 5 | ESA | 8 9 25 27 5 | GFZ | IRKT UNSA 5 | GRG | 8 9 25 27 BAKO CAS1 GOLD GUAM HOFN KHAJ LHAZ MANA 5 | GRG | NLIB PIE1 SCUB 5 | MIT | 5 5 BREW BREW PIE1 6 | COD | 9 25 27 9 25 27 6 | EMR | MIZU 6 | ESA | 8 9 25 27 6 | GFZ | 7 CHUR IRKT KOUR MDO1 OHI2 6 | GRG | KHAJ MKEA NOVM ZECK 6 | MIT | 5 5 HOB2 NISU 6 | NGS | 1 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 ----+------------+---------- G03 | 2009_05_19 | 2009034 6. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G01 | | | | 2 | | | | 7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447. 8. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .8 .4 -.6 -20 -33 -8 .10 EMR | 2.4 -13.2 -4.1 76 -14 101 .35 ESA | 2.0 -8.2 10.3 -8 -4 79 .10 GFZ | .0 .4 1.6 9 2 9 -.20 GRG | 6.3 -1.8 -2.9 15 -2 -7 .04 JPL | 2.3 -2.4 -4.0 2 -14 3 .31 MIT | 4.4 -13.1 8.4 -23 27 -4 .06 NGS | 8.5 -5.9 6.0 -57 -98 24 .08 SIO | -.8 -9.4 .2 -151 23 11 .49 9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 11. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five parts. The first, Table 1, summarizes all statistics for the week. It contains means and standard deviations over the week of satellite ephemeris and clock correction transformation parameters for each centre (table 1.1532.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1532.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 2.1532.[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 3.1532.[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 5.1532.0-6). 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 1532 summary. (May 17, 2009 - May 23, 2009) Table 1.1532.a GPS week: 1532 MJD: 54968.000-54974.000 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 235| 0 0 -1 3 11 0 -.17 9 8 | -611 52 15 72 | 0 0 1 14 13 13 .03 | 342 468 emr 78| -3 -2 0 -135 57 17 .35 19 19 | -139434 -541 17 95 | 0 1 1 19 22 17 .03 | 379475 1088 esa 125| 0 0 0 -37 -45 59 .37 10 9 | 222 -879 20 106 | 1 0 2 18 29 45 .03 | 1039 1727 gfz 191| 0 0 1 -62 -49 -61 .01 11 11 | -58 98 20 95 | 0 1 0 12 33 67 .03 | 214 346 grg 107| 4 0 -5 -90 -15 -68 1.00 43 37 | 4442 -29872 140 14936 | 1 1 3 24 34 56 .05 | 38743 109798 igr n/a| -1 0 -1 -36 -38 -9 .07 6 6 | 18709 -850 19 64 | 0 0 0 13 18 33 .02 | 2248 1003 jpl 103| 1 0 -2 -42 -26 -1 .47 20 18 | 2132 -657 18 93 | 1 1 1 15 12 18 .04 | 1845 982 mit 274| 0 0 0 9 -83 -16 -.31 12 10 | -14473 -691 18 145 | 0 0 1 18 30 21 .03 | 1042 1736 ngs 225| 0 1 0 84 163 -7 -.30 11 8 | 85148 -37993 2384 4060 | 0 0 1 26 26 27 .03 | 132827 75293 sio 249| -2 1 4 285 -63 15 -.01 25 23 | --- --- --- --- | 1 1 1 22 26 14 .03 | --- --- Table 1.1532.b GPS week : 1532 MJD: 54968.000-54974.000 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 | 14 15 18 17 16 14 13 | 2 | 6 5 5 6 5 6 6 | 3 | 3 4 0 4 4 4 5 | 4 | 5 5 4 5 4 4 4 | 5 | 9 9 8 20 13 11 10 | 6 | 4 4 4 4 4 4 5 | 7 | 4 4 4 5 5 5 5 | 8 | 9 9 8 8 8 7 6 | 9 | 5 5 5 6 8 8 6 | 10 | 6 5 4 4 5 4 4 | 11 | 4 5 4 5 4 4 4 | 12 | 5 5 5 5 6 6 5 | 13 | 5 4 5 5 5 5 6 | 14 | 6 5 5 5 6 6 6 | 15 | 6 6 5 6 5 6 5 | 16 | 5 5 5 5 6 5 6 | 17 | 5 5 5 5 5 6 6 | 18 | 5 5 5 5 5 5 5 | 19 | 5 5 4 6 5 5 5 | 20 | 5 5 5 5 5 5 5 | 21 | 4 4 4 5 4 5 5 | 22 | 5 5 5 5 5 5 5 | 23 | 5 5 5 5 5 5 6 | 24 | 5 4 4 4 4 4 5 | 25 | 5 5 5 6 6 6 6 | 26 | 4 4 4 4 4 4 4 | 27 | 6 6 6 6 5 5 5 | 28 | 5 5 5 5 5 5 6 | 29 | 5 5 4 4 5 5 5 | 30 | 5 4 4 4 4 4 3 | 31 | 6 5 5 6 6 5 5 | 32 | 5 5 4 8 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 2.1532.0 GPS week: 1532 Day: 0 MJD: 54968.000 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 235| 0 0 -1 11 4 -20 -.16 10 9 | -955 443 15 71 | -6 4 | emr 78| -3 -2 0 -135 27 19 .33 19 19 | 5309 595 15 88 | -32 -70 | esa 125| 1 0 1 -34 -20 128 .42 10 10 | 1332 -2169 21 115 | 40 13 | gfz 191| 0 0 1 -71 -27 -161 .06 11 11 | 223 -313 21 117 | -6 -32 | grg 107| 3 -1 -1 -51 -5 -85 1.00 41 37 | -153 367 75 221 | 69 -36 | igr n/a| 0 0 0 -11 -30 -4 .11 6 7 | 21785 -184 24 67 | 5 -19 | jpl 103| 1 0 -3 -49 -27 -2 .50 20 20 | 4378 243 17 96 | -5 7 | mit 274| 0 0 0 2 -98 -3 -.28 11 9 | -15739 1443 18 123 | -2 12 | ngs 225| 0 0 0 96 147 17 -.33 11 7 | -116 14004 3239 4491 | -33 -35 | sio 249| -3 3 2 271 -56 13 -.01 28 28 | --- --- --- --- | -144 -70 | Table 2.1532.1 GPS week: 1532 Day: 1 MJD: 54969.000 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 235| 2 -1 0 4 22 2 -.13 9 8 | -665 -219 16 67 | -3 -5 | emr 78| -5 -2 0 -154 89 10 .39 20 20 | 5602 125 16 91 | -27 -145 | esa 125| 0 0 1 -58 -79 110 .32 10 10 | -788 441 21 110 | 56 37 | gfz 191| 0 0 1 -61 -14 -110 .01 9 9 | -172 -263 21 92 | 11 -37 | grg 107| 6 0 -5 -78 -24 -19 1.06 40 37 | -4 122 84 211 | 80 12 | igr n/a| -1 1 -1 -39 -15 -49 .09 5 5 | 21336 -685 18 53 | 21 -59 | jpl 103| 0 0 -3 -51 -27 -31 .52 20 19 | 4400 -370 19 87 | -10 -29 | mit 274| 0 0 0 22 -89 -12 -.27 10 8 | -15213 747 18 138 | -13 13 | ngs 225| 0 1 0 91 159 17 -.32 12 7 | 269341 -145757 2146 4096 | -51 -5 | sio 249| -3 1 3 316 -77 8 .04 26 23 | --- --- --- --- | -152 -61 | Table 2.1532.2 GPS week: 1532 Day: 2 MJD: 54970.000 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 235| 0 -1 -2 17 32 -8 -.17 8 7 | -532 -23 14 72 | -25 -48 | emr 78| -3 0 0 -151 69 15 .35 19 19 | 4999 -2388 17 92 | -29 -109 | esa 125| 0 0 1 -53 -40 67 .35 8 8 | -559 -1655 19 109 | 54 47 | gfz 191| 0 2 2 -53 -70 -111 -.02 11 11 | -364 561 21 87 | 5 -23 | grg 107| 3 -1 -7 -97 23 -32 .92 42 36 | -498 756 100 237 | 18 -36 | igr n/a| -1 1 0 -25 -22 -17 .07 6 5 | 19963 -2609 20 72 | 16 13 | jpl 103| 2 -2 -1 -63 -17 10 .50 20 19 | 3439 -2339 17 101 | -1 15 | mit 274| 1 0 -2 19 -111 14 -.31 10 8 | -14190 -2033 18 170 | -9 6 | ngs 225| 0 2 1 99 208 -34 -.30 11 7 | 7797 3931 1990 3449 | -29 -59 | sio 249| -3 1 3 301 -91 36 .02 27 24 | --- --- --- --- | -145 -59 | Table 2.1532.3 GPS week: 1532 Day: 3 MJD: 54971.000 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 235| 1 -1 -2 4 5 -6 -.15 10 8 | -829 462 15 63 | -35 -9 | emr 78| -3 -2 0 -128 74 8 .36 18 18 | 2630 -1735 17 93 | -62 -147 | esa 125| -1 1 0 -32 -79 5 .35 12 12 | -131 -1448 20 108 | 25 7 | gfz 191| 0 0 0 -66 -4 -11 .03 11 11 | -104 -26 19 92 | -1 -34 | grg 107| 4 0 -2 -123 -74 -186 1.03 62 39 | -139 -235 86 248 | 27 18 | igr n/a| 0 1 -1 -45 -43 -35 .08 5 5 | 17337 -1911 18 54 | -21 -51 | jpl 103| 1 0 0 -35 -54 18 .47 20 18 | 872 -1743 18 100 | -15 2 | mit 274| 0 -1 1 -2 -97 -7 -.29 12 10 | -12854 -2923 19 153 | 0 17 | ngs 225| 1 2 1 76 165 24 -.28 11 9 | 7072 8080 1962 3773 | -63 1 | sio 249| -3 1 3 259 -44 8 -.00 25 23 | --- --- --- --- | -122 -59 | Table 2.1532.4 GPS week: 1532 Day: 4 MJD: 54972.000 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 235| 0 0 -3 -19 18 5 -.16 9 9 | -138 -467 16 82 | 0 -43 | emr 78| -4 -2 2 -114 58 55 .36 20 20 | -999999 -248 17 91 | -82 -92 | esa 125| -1 0 0 -11 -59 38 .39 10 9 | 1383 -3250 20 103 | -11 8 | gfz 191| 0 -1 2 -43 -70 -3 .01 10 10 | 228 -41 20 93 | 12 -5 | grg 107| 5 0 -4 -94 20 -54 1.03 39 37 | 192 -152 88 208 | 73 -47 | igr n/a| 0 0 0 -47 -32 49 .04 6 6 | 17070 -287 19 61 | -34 6 | jpl 103| 3 1 -1 -43 -23 -18 .44 19 16 | 693 -177 18 94 | -19 22 | mit 274| 0 0 1 7 -83 -33 -.35 14 11 | -13541 -2441 18 145 | 9 -1 | ngs 225| 0 1 1 51 183 -28 -.26 10 7 | 11864 2266 1840 3742 | 31 -25 | sio 249| 0 1 4 298 -88 6 .00 24 23 | --- --- --- --- | -156 -49 | Table 2.1532.5 GPS week: 1532 Day: 5 MJD: 54973.000 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 235| 0 -1 -2 19 -7 8 -.21 9 8 | -190 -484 16 83 | -33 25 | emr 78| -3 -3 -1 -108 50 15 .32 18 18 | 2863 -87 23 106 | -58 -101 | esa 125| -1 1 2 -53 0 31 .36 9 9 | 1193 1727 19 103 | 11 -25 | gfz 191| -1 0 1 -83 -67 -45 -.03 11 11 | -112 441 20 97 | 2 14 | grg 107| 1 -1 -9 -75 -40 -60 .96 36 36 | 81583 -273116 117 93426 | 8 6 | igr n/a| -1 0 -1 -39 -57 19 .06 5 5 | 16930 -244 20 76 | 17 -19 | jpl 103| 0 0 -2 -12 -17 0 .44 19 18 | 697 -272 20 89 | -45 8 | mit 274| 1 0 1 -18 -82 -17 -.32 13 12 | -14412 -45 18 151 | 8 2 | ngs 225| 0 2 -1 122 153 -10 -.31 12 9 | 10777 1820 2477 4175 | -24 -7 | sio 249| 0 1 5 258 -71 36 -.06 24 21 | --- --- --- --- | -166 -37 | Table 2.1532.6 GPS week: 1532 Day: 6 MJD: 54974.000 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 235| 1 0 0 -12 2 20 -.19 8 8 | -968 652 18 68 | 26 22 | emr 78| -3 -2 2 -155 33 0 .31 19 19 | 2556 -49 19 104 | -19 -67 | esa 125| -1 0 -3 -17 -39 33 .38 9 9 | -874 198 20 100 | -24 -4 | gfz 191| 0 1 1 -56 -92 16 .01 14 14 | -110 330 20 89 | 39 52 | grg 107| 4 1 -8 -112 -10 -38 .97 39 37 | -49884 63150 435 10006 | 46 90 | igr n/a| 0 0 -1 -46 -64 -27 .05 6 6 | 16548 -32 20 66 | 33 -10 | jpl 103| 0 0 -2 -44 -19 14 .40 20 17 | 451 59 21 84 | 11 -15 | mit 274| 0 -1 3 37 -18 -53 -.33 14 13 | -15363 412 20 139 | 0 -17 | ngs 225| 0 2 0 51 125 -39 -.32 10 8 | 289307 -150295 3039 4696 | 41 -2 | sio 249| 0 0 6 291 -16 -1 -.04 24 22 | --- --- --- --- | -156 -50 | 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 3.1532.0 GPS week: 1532 Day: 0 MJD: 54968.000 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 | 21 --- --- --- --- 44 --- 17 21 --- 14 | 125 --- --- --- --- 136 --- 129 132 --- 125 2 | 11 23 12 16 35 5 23 9 9 25 5 | 29 34 32 27 40 28 35 30 31 33 29 X3 | 4 12 7 9 20 7 --- 4 6 21 3 | 9 11 9 9 7 10 --- 10 10 3 9 4 | 9 17 11 11 26 6 15 10 9 31 4 | 19 29 28 24 33 22 29 19 20 45 21 X5 | 20 16 --- --- --- 20 --- 10 13 --- 8 | 22 24 --- --- --- 22 --- 21 23 --- 20 6 | 6 11 8 14 28 7 13 4 5 22 3 | 25 30 25 30 40 27 25 25 27 26 25 7E | 6 15 9 10 21 10 24 7 7 18 4 | 13 24 21 18 30 15 23 12 16 18 15 8E | 22 27 15 13 49 9 24 16 36 23 8 | 37 47 45 42 55 36 46 44 56 43 40 9E | 13 19 8 10 100 6 21 14 9 27 5 | 49 51 49 51 59 49 47 55 54 52 50 10 | 15 17 11 11 36 5 15 17 8 33 5 | 88 92 87 96 63 91 90 87 95 85 88 11 | 8 16 8 9 48 5 16 6 8 22 4 | 15 23 17 20 42 15 21 18 18 19 17 12 | 12 19 12 10 39 6 22 12 5 35 5 | 18 33 25 21 37 21 32 25 22 29 21 13 | 6 20 10 10 46 7 24 10 9 22 4 | 19 31 28 25 52 21 34 20 18 17 21 14 | 7 25 11 16 31 8 20 10 11 24 5 | 19 33 27 31 35 25 28 21 25 24 22 15 | 10 21 12 8 51 5 26 14 7 27 5 | 20 30 27 22 47 20 27 25 20 23 20 16 | 11 22 8 13 26 4 26 9 8 29 5 | 29 37 28 25 37 25 37 26 28 25 27 17 | 7 12 8 8 36 8 18 5 7 45 4 | 28 35 35 30 39 31 38 30 31 32 31 18 | 9 22 10 14 26 6 23 7 7 22 5 | 30 40 34 31 49 31 37 29 33 38 32 19 | 8 15 11 12 28 9 20 6 6 34 4 | 33 34 26 28 34 30 37 34 33 30 31 20 | 10 20 10 14 43 7 20 7 8 27 5 | 16 30 24 21 44 20 26 20 20 25 19 21 | 7 20 6 8 28 4 20 6 7 24 4 | 22 34 27 22 62 24 33 24 25 25 24 22 | 8 21 9 11 31 7 21 8 7 18 4 | 18 32 26 22 39 22 28 17 20 21 20 23 | 7 21 10 13 34 5 24 7 8 33 5 | 18 30 27 22 43 21 33 18 20 27 20 24 | 9 17 7 11 28 6 15 12 7 29 4 | 18 26 19 17 23 17 26 18 19 23 17 25E | 10 19 9 13 52 6 18 9 9 22 4 | 24 40 30 30 44 27 39 29 26 29 27 26 | 9 13 7 5 27 6 13 8 7 16 3 | 26 30 28 26 31 24 26 25 26 21 26 27E | 13 21 10 9 66 6 22 22 13 28 6 | 37 42 38 36 47 37 45 49 41 45 39 28 | 7 18 15 11 43 7 23 8 9 26 5 | 23 33 30 22 47 23 36 19 20 21 23 29 | 8 16 9 8 26 8 17 11 9 41 5 | 25 32 28 25 40 24 36 28 26 38 26 30 | 10 12 12 10 27 6 14 11 7 30 4 | 29 34 40 36 47 35 32 31 31 30 32 31E | 11 28 10 10 17 7 24 15 12 25 6 | 15 35 22 18 28 20 26 20 23 19 18 32 | 8 19 9 12 41 4 15 6 10 30 4 | 50 49 48 53 45 48 48 50 49 46 48 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 19 10 11 41 6 20 11 11 28 |T 29 35 31 29 41 31 35 31 32 30 30 WRMS | 9 19 10 11 37 7 20 9 7 28 |NE 29 33 30 28 40 31 34 30 31 29 30 MEDI | 9 19 10 11 31 6 20 9 8 26 |MD 23 33 28 25 40 24 33 25 25 26 24 Table 3.1532.1 GPS week: 1532 Day: 1 MJD: 54969.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 22 --- --- --- 1534 33 --- 15 24 --- 15 | 133 --- --- --- 17 124 --- 129 127 --- 126 2 | 7 20 10 12 32 4 19 8 11 24 4 | 27 30 26 25 44 26 31 27 26 31 25 X3 | 4 --- 7 11 --- 10 --- 6 4 --- 3 | 6 --- 8 5 --- 4 --- 8 11 --- 7 4 | 7 21 10 10 23 4 12 10 7 28 4 | 13 22 19 15 29 15 22 16 13 37 14 X5 | 10 22 --- --- --- 19 --- 12 17 --- 8 | 21 18 --- --- --- 15 --- 16 24 --- 18 6 | 6 14 8 12 32 7 13 7 7 21 3 | 20 21 20 22 31 21 19 21 21 20 19 7E | 5 16 8 8 22 7 22 6 15 16 4 | 11 20 13 12 24 12 21 7 17 12 10 8E | 21 30 13 10 34 7 26 17 41 22 9 | 30 36 39 36 43 36 40 38 60 35 34 9E | 12 20 12 11 101 8 21 12 7 24 5 | 49 48 51 48 49 48 42 52 51 44 48 10 | 14 17 9 9 31 4 13 8 11 22 4 | 40 39 38 34 51 35 37 32 35 38 35 11 | 8 17 12 9 45 4 17 9 9 25 4 | 17 23 20 18 32 16 20 19 19 19 16 12 | 12 24 9 7 42 5 21 10 9 27 5 | 15 27 20 16 34 14 24 19 19 22 16 13 | 6 19 8 8 47 4 22 8 8 21 4 | 15 29 19 18 47 18 27 15 16 17 15 14 | 6 25 10 11 36 5 23 9 9 24 5 | 12 27 20 19 35 15 23 12 13 18 13 15 | 7 23 12 14 37 5 22 16 10 20 5 | 12 30 18 18 36 17 23 21 19 26 14 16 | 9 23 7 8 32 6 26 12 7 26 5 | 27 40 30 31 40 30 39 29 32 30 29 17 | 7 13 9 7 24 5 16 9 9 44 4 | 21 26 23 22 36 23 27 20 20 28 20 18 | 8 27 11 10 28 4 26 9 6 25 5 | 20 35 26 21 40 22 28 20 22 26 20 19 | 8 14 12 12 34 7 17 7 5 33 4 | 29 30 26 25 41 27 31 30 30 28 27 20 | 7 20 11 8 33 6 19 12 6 23 4 | 12 29 17 14 31 14 21 14 14 18 12 21 | 6 20 10 8 29 3 18 7 9 27 4 | 16 27 14 11 70 15 24 16 15 22 13 22 | 7 20 13 5 35 4 24 9 6 20 4 | 12 25 20 14 37 13 22 9 15 16 13 23 | 6 22 14 8 34 4 24 7 6 33 5 | 18 28 22 18 33 18 25 15 19 28 16 24 | 8 18 9 7 21 4 14 10 8 29 4 | 13 23 14 16 21 13 20 19 15 17 13 25E | 11 19 8 11 60 6 17 12 14 17 4 | 16 28 20 22 33 18 29 19 21 22 18 26 | 8 11 9 7 23 5 11 8 10 17 3 | 17 20 17 16 27 15 18 17 19 16 15 27E | 12 22 9 10 66 8 21 21 14 24 6 | 31 43 37 35 46 35 44 39 39 36 35 28 | 6 21 12 9 33 5 22 7 8 23 4 | 23 38 28 23 45 26 36 23 25 23 24 29 | 10 14 8 11 35 5 16 8 11 36 4 | 19 21 15 15 31 17 22 20 19 22 15 30 | 8 12 8 7 36 5 12 6 9 27 3 | 26 26 34 29 44 26 26 28 30 31 28 31E | 10 23 5 9 29 7 24 15 9 22 5 | 14 30 18 16 32 15 26 12 21 20 15 32 | 8 15 9 7 29 3 14 6 14 28 4 | 66 64 65 66 67 67 66 69 64 65 65 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 10 9 40 5 20 10 12 26 |T 25 30 24 22 38 25 28 25 27 26 24 WRMS | 8 20 10 9 37 5 19 8 7 23 |NE 25 29 23 21 38 24 27 25 26 26 24 MEDI | 8 20 9 9 33 5 19 9 9 24 |MD 18 28 20 18 36 18 26 19 20 23 16 Table 3.1532.2 GPS week: 1532 Day: 2 MJD: 54970.000 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 | 23 --- --- --- --- 30 --- 30 19 --- 17 | 122 --- --- --- --- 128 --- 131 129 --- 123 2 | 9 19 9 14 30 4 20 8 7 25 4 | 25 29 29 22 42 22 31 25 25 24 24 X3 | 3 --- --- --- --- 21 --- --- --- --- 0 | 17 --- --- --- --- 27 --- --- --- --- 19 4 | 7 18 9 11 20 5 13 12 8 23 4 | 13 27 19 17 30 16 25 15 20 32 16 X5 | 10 17 --- --- --- 28 --- 12 18 --- 8 | 14 26 --- --- --- 19 --- 20 23 --- 17 6 | 7 12 6 14 20 7 12 5 11 19 3 | 17 23 26 28 18 25 21 17 28 19 21 7E | 5 13 8 11 25 6 24 7 12 15 4 | 7 15 15 14 28 9 20 12 14 15 9 8E | 18 30 8 14 57 10 28 17 32 24 7 | 20 30 25 27 35 28 30 26 49 22 23 9E | 13 18 10 12 109 7 19 15 7 28 5 | 51 49 51 58 48 51 46 59 56 51 52 10 | 5 17 6 12 28 5 14 9 8 20 3 | 29 36 35 31 34 30 35 29 31 32 31 11 | 6 20 6 8 46 4 16 6 6 22 3 | 19 25 18 21 38 18 20 19 23 23 19 12 | 11 22 9 11 41 6 23 11 10 26 5 | 15 30 23 17 35 18 28 18 18 20 18 13 | 6 21 7 12 41 3 25 7 7 22 4 | 10 24 17 17 44 12 26 13 15 11 12 14 | 6 21 7 15 34 5 25 8 8 23 4 | 13 28 21 23 36 19 25 18 19 19 17 15 | 7 18 9 11 33 6 22 12 14 27 5 | 10 23 13 15 35 11 22 17 19 18 10 16 | 10 20 9 7 39 5 26 10 8 26 5 | 24 35 28 28 42 24 35 23 26 28 25 17 | 5 13 6 10 38 7 15 5 9 45 4 | 23 30 27 28 42 26 32 25 23 26 24 18 | 8 24 9 15 33 5 25 9 10 28 5 | 15 29 19 16 36 16 26 17 17 22 16 19 | 6 15 8 11 20 7 17 6 10 32 4 | 22 23 20 20 23 20 25 22 26 27 21 20 | 7 22 8 12 28 7 21 8 9 21 4 | 12 29 15 16 31 14 22 17 16 19 14 21 | 6 19 7 7 77 3 19 6 7 27 4 | 18 29 21 14 73 17 26 18 22 20 19 22 | 7 20 8 14 36 3 26 7 8 22 4 | 13 27 20 16 40 15 27 13 19 18 15 23 | 6 21 9 12 31 4 27 8 10 35 5 | 12 24 16 16 33 12 25 15 18 30 12 24 | 8 15 6 7 19 4 14 9 9 28 4 | 13 21 12 13 23 12 21 14 18 16 12 25E | 8 21 7 12 54 5 17 17 13 19 5 | 14 25 17 19 35 16 27 22 22 18 16 26 | 6 11 6 8 22 3 11 7 10 25 3 | 21 23 22 21 26 19 22 22 26 24 21 27E | 11 18 9 11 60 5 20 19 12 28 5 | 31 38 36 31 45 31 43 30 31 34 31 28 | 5 20 13 10 31 5 22 9 14 30 5 | 21 36 25 21 48 22 36 19 21 17 20 29 | 5 14 7 10 34 5 15 6 7 35 4 | 20 24 22 19 37 19 26 22 24 28 21 30 | 8 12 5 8 34 7 14 6 7 24 3 | 24 25 32 30 44 26 23 26 32 26 27 31E | 8 20 8 11 19 6 26 13 10 26 5 | 19 34 25 20 37 21 30 25 27 19 22 32 | 7 17 7 7 22 6 18 6 9 29 4 | 50 52 55 51 59 50 52 54 60 53 53 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 8 11 42 6 20 10 11 27 |T 22 28 24 23 37 24 28 25 28 24 24 WRMS | 7 19 8 11 36 5 19 8 7 24 |NE 22 28 23 21 37 24 27 25 27 24 24 MEDI | 7 18 8 11 33 5 20 8 9 26 |MD 18 27 22 20 36 19 26 20 23 22 19 Table 3.1532.3 GPS week: 1532 Day: 3 MJD: 54971.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 25 --- --- --- --- 31 --- 11 29 --- 16 | 152 --- --- --- --- 157 --- 145 153 --- 147 2 | 7 20 12 17 35 3 24 9 12 21 5 | 27 31 25 25 38 26 35 24 33 27 26 X3 | 7 10 10 9 33 5 --- 9 6 15 3 | 11 20 25 23 24 16 --- 15 18 21 16 4 | 7 14 8 11 25 5 15 10 12 25 4 | 12 21 19 18 28 16 21 15 17 31 14 X5 | 25 --- --- --- --- 65 --- 16 38 --- 20 | 12 --- --- --- --- 65 --- 19 57 --- 24 6 | 7 10 8 13 30 5 11 6 9 13 3 | 20 26 23 27 32 25 25 24 29 18 23 7E | 6 15 12 11 23 5 21 11 10 16 4 | 9 17 16 15 25 12 19 16 13 17 10 8E | 19 26 14 14 54 9 26 19 28 19 8 | 19 27 29 31 37 27 31 28 48 24 25 9E | 14 18 14 12 86 5 22 16 12 22 5 | 55 55 56 58 66 55 49 69 63 52 57 10 | 7 16 13 9 23 4 14 9 10 19 4 | 32 33 31 31 35 31 32 26 33 31 29 11 | 7 17 9 10 42 5 17 10 8 25 4 | 18 25 13 17 35 14 24 20 19 22 17 12 | 10 23 14 9 43 5 22 9 8 26 5 | 19 33 24 23 39 18 29 22 25 28 20 13 | 7 18 14 8 45 3 25 8 7 19 4 | 11 26 19 14 49 14 26 14 15 18 12 14 | 9 20 12 11 46 5 24 9 11 23 5 | 16 28 24 24 37 21 26 20 24 21 18 15 | 8 23 12 9 36 2 24 11 12 23 5 | 18 31 18 20 38 16 24 20 19 19 17 16 | 8 21 12 11 33 4 24 11 9 25 5 | 34 41 35 37 48 34 43 35 40 35 35 17 | 7 12 12 10 33 8 15 8 13 43 5 | 31 35 34 34 40 32 36 29 40 27 32 18 | 10 23 11 11 59 4 23 10 8 22 5 | 21 35 32 23 58 24 32 22 25 29 23 19 | 7 14 23 11 27 7 17 7 9 31 5 | 32 32 33 32 34 30 36 33 34 29 31 20 | 7 15 8 12 42 4 19 20 6 18 5 | 11 26 17 14 39 14 22 23 16 19 14 21 | 7 18 10 9 253 3 19 8 11 25 4 | 18 28 18 18 177 19 27 20 21 22 18 22 | 8 19 10 7 37 4 24 8 11 18 4 | 12 28 26 18 41 15 27 14 18 18 16 23 | 6 19 10 11 37 3 24 12 7 32 5 | 14 27 21 16 37 17 25 18 20 27 15 24 | 7 15 8 10 31 3 14 10 7 24 4 | 11 22 13 16 34 12 19 17 15 19 12 25E | 11 20 12 17 56 4 20 15 12 17 5 | 16 25 16 22 37 15 27 20 17 19 15 26 | 5 12 13 6 31 5 12 9 10 17 4 | 9 14 18 12 24 9 14 13 18 11 11 27E | 9 18 14 12 60 4 22 14 12 22 5 | 40 45 42 43 59 40 52 39 44 43 40 28 | 6 23 15 13 44 7 21 9 8 18 5 | 29 40 39 31 43 27 42 29 30 26 30 29 | 5 11 13 6 36 5 15 8 7 30 4 | 27 26 24 27 36 23 30 27 27 26 25 30 | 7 10 10 8 18 3 11 9 6 20 3 | 24 27 30 25 41 25 24 26 26 24 25 31E | 6 20 13 12 30 6 24 15 11 20 5 | 15 30 26 22 38 20 30 24 25 22 19 32 | 25 19 10 9 46 3 19 29 9 49 8 | 130 132 136 136 123 132 136 139 138 144 135 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 12 11 62 5 20 12 11 25 |T 28 32 29 28 46 31 33 31 35 28 29 WRMS | 8 18 12 11 39 5 18 10 9 23 |NE 28 32 29 27 47 32 32 31 35 28 30 MEDI | 7 18 12 11 36 5 21 10 10 22 |MD 18 28 24 23 38 21 27 22 25 24 20 Table 3.1532.4 GPS week: 1532 Day: 4 MJD: 54972.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 22 --- --- --- --- 21 --- 16 27 --- 16 | 141 --- --- --- --- 145 --- 139 140 --- 137 2 | 10 24 9 13 30 4 21 10 9 22 5 | 23 34 24 20 35 23 32 23 25 27 23 3 | 8 12 8 8 22 5 7 9 9 18 3 | 21 23 22 20 26 22 10 17 17 18 23 4 | 7 19 5 8 23 7 10 8 10 17 3 | 17 29 20 18 31 21 24 15 17 32 17 X5 | 15 28 --- --- --- 27 --- 16 27 --- 12 | 18 25 --- --- --- 27 --- 17 33 --- 16 6 | 8 13 9 8 27 6 8 9 7 14 3 | 23 30 24 26 33 23 23 22 26 19 24 7E | 6 15 8 12 26 6 19 17 9 15 4 | 12 22 15 15 28 12 23 20 17 19 13 8E | 19 26 15 12 60 6 23 20 29 24 8 | 23 37 26 27 35 27 32 30 45 29 27 9E | 17 22 16 14 67 9 23 33 16 31 8 | 81 81 78 80 90 78 72 77 79 70 75 10 | 9 20 9 9 24 5 14 12 10 17 4 | 20 27 20 22 26 20 21 19 28 27 19 11 | 10 20 8 9 46 8 16 10 8 18 4 | 16 29 15 20 38 20 22 20 24 18 18 12 | 13 24 15 10 44 5 23 9 13 25 6 | 17 31 28 19 35 22 29 19 31 18 22 13 | 6 21 11 12 38 3 23 13 6 18 5 | 12 28 16 12 49 11 29 18 12 12 12 14 | 8 23 11 15 35 6 23 10 7 24 5 | 15 31 23 25 39 21 28 18 21 19 19 15 | 9 23 12 9 34 4 23 11 11 20 5 | 19 32 19 20 35 17 27 19 19 17 18 16 | 9 21 8 7 31 5 24 18 10 29 5 | 19 30 23 20 37 20 32 18 25 20 22 17 | 6 11 9 9 23 9 12 11 11 46 5 | 27 32 31 27 37 30 35 27 33 21 28 18 | 10 23 10 10 51 3 23 11 6 19 5 | 19 32 25 21 30 19 28 22 21 23 22 19 | 8 16 9 11 27 8 15 7 8 30 4 | 31 34 23 24 29 28 31 28 29 26 27 20 | 8 19 11 12 40 6 20 13 9 20 5 | 12 29 20 19 42 14 21 19 19 22 16 21 | 8 22 7 8 42 5 15 9 6 24 4 | 19 33 24 15 69 19 29 22 24 22 21 22 | 10 20 9 8 35 4 23 11 8 16 4 | 15 32 24 19 40 17 28 19 17 18 18 23 | 4 22 9 12 43 6 23 11 5 34 5 | 12 28 15 14 43 12 25 15 14 27 11 24 | 10 15 7 7 29 4 14 10 7 26 4 | 14 23 20 16 31 16 23 21 22 22 17 25E | 10 26 11 10 58 5 18 25 13 20 6 | 18 33 21 20 35 17 32 33 23 24 20 26 | 6 16 10 7 26 4 11 11 8 14 3 | 13 22 14 14 22 14 18 14 17 13 14 27E | 9 17 13 9 64 4 18 9 9 20 4 | 29 38 35 32 44 32 42 31 33 33 33 28 | 6 23 11 9 36 7 22 8 11 23 5 | 20 35 23 17 42 22 36 17 22 19 21 29 | 8 15 11 13 37 8 14 9 10 32 5 | 21 27 26 19 37 22 30 21 30 20 23 30 | 7 11 8 8 17 4 11 6 5 20 3 | 18 23 21 20 28 21 19 21 22 21 19 31E | 8 23 6 12 29 7 22 21 12 18 5 | 11 28 17 13 36 15 25 22 24 18 15 32 | 11 17 9 10 41 7 17 9 10 25 4 | 59 60 59 63 48 57 55 56 49 55 53 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 10 10 39 6 19 14 10 24 |T 25 32 25 23 38 27 29 27 29 24 26 WRMS | 9 20 9 10 37 6 16 11 7 23 |NE 24 30 23 21 36 26 27 25 28 22 25 MEDI | 8 20 9 9 35 6 18 11 9 20 |MD 19 30 23 20 35 21 28 20 24 21 20 Table 3.1532.5 GPS week: 1532 Day: 5 MJD: 54973.000 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 --- --- --- --- 29 --- 22 20 --- 13 | 125 --- --- --- --- 115 --- 115 125 --- 119 2 | 8 26 10 13 31 6 25 12 11 20 5 | 23 37 27 27 36 25 32 25 23 24 24 3 | 6 10 6 8 20 5 8 9 6 23 3 | 17 19 21 23 25 19 11 15 14 20 20 4 | 7 16 9 10 28 4 15 9 8 20 4 | 13 21 21 17 30 13 23 14 13 26 15 X5 | 13 34 19 --- --- 26 --- 14 26 --- 10 | 18 23 23 --- --- 27 --- 16 36 --- 20 6 | 5 11 8 12 25 5 9 10 9 24 4 | 20 24 23 29 35 20 21 21 21 20 22 7E | 6 14 7 13 27 7 22 16 15 19 5 | 10 17 11 14 28 11 20 21 18 22 11 8E | 16 25 10 14 55 6 22 17 20 24 6 | 21 32 29 33 38 26 34 35 30 32 26 9E | 18 21 14 13 50 7 24 29 17 25 7 | 56 56 57 60 48 58 53 74 64 63 59 10 | 7 15 6 9 23 7 14 12 12 20 4 | 31 38 34 36 40 32 36 35 33 34 33 11 | 9 18 8 10 58 6 17 11 9 16 4 | 15 23 12 16 39 12 19 18 19 19 14 12 | 10 24 10 12 31 6 24 11 13 29 5 | 15 31 22 20 31 15 29 16 21 21 18 13 | 6 19 9 12 39 5 24 13 7 16 4 | 13 25 17 14 46 11 26 21 21 13 14 14 | 9 21 10 14 32 5 24 14 12 17 5 | 16 30 24 23 41 20 27 21 21 19 19 15 | 10 22 14 13 36 3 20 12 12 18 5 | 14 24 14 19 30 10 22 17 16 16 12 16 | 10 21 7 10 33 4 25 15 8 25 5 | 29 40 32 29 52 28 37 27 30 36 29 17 | 7 11 7 7 30 7 14 14 15 44 5 | 28 34 33 31 33 28 34 30 36 21 29 18 | 10 27 11 11 30 2 19 11 7 21 5 | 35 42 41 35 41 34 38 35 35 35 36 19 | 5 13 8 12 28 6 14 9 8 31 4 | 20 24 21 21 28 20 23 22 24 21 20 20 | 8 15 9 11 36 6 21 16 13 13 4 | 15 24 17 18 38 14 19 21 14 18 13 21 | 9 16 9 9 26 4 16 10 11 22 4 | 17 26 18 13 46 15 22 21 23 17 17 22 | 7 22 9 11 28 3 22 13 9 17 4 | 15 28 23 16 41 17 24 19 15 17 16 23 | 6 18 9 14 43 5 25 13 8 31 5 | 12 23 16 14 36 12 24 17 19 29 13 24 | 9 14 10 7 31 4 16 11 10 22 4 | 14 23 17 14 26 13 23 16 19 20 15 25E | 9 18 10 13 58 6 19 20 16 21 5 | 17 25 22 21 35 17 29 32 26 23 20 26 | 6 13 8 6 23 4 10 10 9 11 3 | 13 17 12 12 23 10 13 16 16 12 12 27E | 10 19 10 9 49 4 19 10 12 20 4 | 36 44 36 38 49 36 46 34 37 35 37 28 | 7 22 7 11 37 5 23 12 13 24 5 | 21 39 26 26 45 22 37 19 23 16 22 29 | 7 10 7 8 38 6 16 10 14 34 4 | 22 24 24 17 33 18 23 18 22 26 20 30 | 9 13 8 7 16 3 13 7 11 20 4 | 19 22 24 22 26 20 21 23 30 22 22 31E | 7 17 7 11 38 6 23 13 13 23 5 | 12 26 21 14 34 14 23 16 20 23 16 32 | 8 20 10 10 34 5 18 9 14 32 5 | 91 96 94 93 94 93 95 94 93 94 92 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 9 11 36 5 19 13 12 24 |T 25 30 26 25 38 25 29 28 29 26 26 WRMS | 8 18 9 11 36 5 18 12 9 21 |NE 25 30 25 24 38 25 28 27 29 24 26 MEDI | 8 18 9 11 31 5 19 12 12 21 |MD 17 25 23 21 36 19 24 21 22 21 20 Table 3.1532.6 GPS week: 1532 Day: 6 MJD: 54974.000 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 | 16 --- --- --- --- 15 --- 19 19 --- 12 | 129 --- --- --- --- 134 --- 132 132 --- 128 2 | 9 23 8 19 43 6 25 16 11 21 5 | 30 37 31 27 47 29 41 28 28 32 28 3 | 8 14 7 18 29 4 10 10 8 28 4 | 18 23 21 29 19 22 11 15 14 19 22 4 | 6 17 7 13 27 3 12 9 9 21 4 | 19 24 23 21 28 20 24 16 15 32 18 X5 | 15 21 27 --- --- 18 --- 18 17 --- 10 | 16 22 19 --- --- 24 --- 18 26 --- 17 6 | 8 16 6 22 21 5 12 10 12 23 5 | 29 39 34 48 44 34 32 33 32 26 33 7E | 7 18 9 15 28 8 22 17 14 14 5 | 23 26 21 25 27 22 29 27 21 25 21 8E | 12 21 12 11 83 8 21 19 13 22 5 | 28 38 36 41 66 32 41 44 39 38 34 9E | 14 22 11 11 57 6 26 23 11 23 6 | 67 64 66 65 76 63 56 72 70 64 64 10 | 7 15 6 11 22 4 14 10 12 20 4 | 32 36 33 33 43 31 35 34 33 35 32 11 | 7 16 6 10 57 8 19 12 8 22 4 | 19 26 17 21 46 17 20 21 22 24 18 12 | 8 26 9 11 28 5 21 13 9 28 5 | 19 38 20 20 36 21 33 19 25 25 20 13 | 7 21 13 16 46 9 26 15 12 17 5 | 20 31 32 23 43 27 30 25 24 22 21 14 | 10 23 12 19 36 5 24 12 8 20 5 | 19 34 31 31 37 22 29 23 20 24 22 15 | 8 23 11 12 40 4 23 10 12 17 5 | 14 25 18 14 33 11 23 17 18 14 13 16 | 9 20 10 14 37 4 29 16 8 25 5 | 24 38 30 30 47 28 40 29 29 31 27 17 | 8 14 6 9 25 9 13 18 11 47 5 | 34 38 39 32 39 34 42 39 32 27 33 18 | 10 27 10 15 37 4 21 11 5 19 5 | 24 37 26 24 34 25 33 25 24 29 23 19 | 7 16 8 20 21 8 18 10 10 32 5 | 35 37 33 36 34 31 40 33 33 31 32 20 | 9 17 7 13 29 7 21 15 8 14 4 | 18 29 25 24 30 19 23 23 22 21 19 21 | 8 19 10 10 24 5 16 10 11 27 4 | 26 33 25 20 44 22 32 27 28 28 24 22 | 8 21 10 16 29 8 24 15 7 16 5 | 18 29 26 21 35 20 27 20 17 21 17 23 | 7 21 11 15 41 7 27 14 7 32 5 | 18 29 29 23 36 19 29 23 23 34 20 24 | 8 15 9 9 23 4 13 12 10 27 4 | 15 21 18 19 27 16 19 21 22 24 17 25E | 8 17 10 15 55 5 22 22 17 18 5 | 27 29 26 27 35 27 36 34 31 29 26 26 | 6 16 8 7 23 4 12 10 10 17 3 | 13 20 15 13 21 12 15 19 18 16 13 27E | 8 20 10 11 59 4 18 9 10 21 4 | 44 53 43 41 54 43 53 42 49 46 44 28 | 7 25 7 13 37 7 22 17 11 23 5 | 19 39 24 23 43 21 35 22 21 16 20 29 | 6 11 9 14 38 9 13 13 11 35 4 | 33 34 35 29 46 30 37 32 34 30 32 30 | 7 8 6 10 18 4 10 10 7 16 3 | 25 26 28 27 32 23 23 29 26 26 25 31E | 7 20 9 12 52 7 20 13 11 25 5 | 15 27 21 15 54 16 25 19 19 26 17 32 | 8 16 7 13 30 5 16 14 10 27 4 | 70 73 73 74 81 71 72 69 75 76 72 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 9 14 39 6 20 14 10 24 |T 29 34 29 29 41 30 32 32 31 29 29 WRMS | 8 19 9 14 37 6 17 13 8 22 |NE 28 32 28 27 38 29 31 30 30 27 28 MEDI | 8 19 9 13 30 5 20 13 10 22 |MD 23 33 26 25 37 23 32 25 25 26 22 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 4.1532 GPS week: 1532 MJD: 54968.0-54974.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3040 |U 7 7 20 |U 7 10 27 |U 7 7 16 | emr | emr 2914 | 9 9 24 | 8 11 34 |U 10 10 18 | esa | esa 2893 | 8 7 21 |U 6 9 28 | 7 7 14 | gfz | gfz 2843 |U 11 8 23 |U 7 8 29 | 7 6 14 | grg | grg 2866 | 9 8 23 |U 9 14 36 | 11 9 25 | igr | igr 2882 | 8 7 22 | 7 9 29 | 7 6 15 | igs | igs 2918 | 8 7 21 | 8 9 29 | 7 6 14 | jpl | jpl 2800 | 8 7 25 |U 7 8 25 |U 12 9 20 | mit | mit 3058 |U 7 7 20 |U 9 14 37 |U 9 10 34 | 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 5.1532.0 GPS week: 1532 Day: 0 MJD: 54968.0 CENT| CLK EPO | TOW2 | WILL | ----+----------+-------------------+-------------------+ cod | cod 3018 | 11 12 48 | 9 11 20 | emr | emr 2955 | 13 16 63 | 11 14 22 | esa | esa 2880 | 12 13 55 | 9 11 18 | gfz | gfz 2856 | 9 7 53 | 8 9 17 | grg | grg 2880 | 12 14 53 | 12 13 27 | igr | igr 2863 | 12 11 54 | 8 11 18 | igs | igs 2946 | 12 11 56 | 8 11 18 | jpl | jpl 2761 | 7 8 26 | 34 20 43 | mit | mit 3072 | 13 18 69 | 8 10 20 | Table 5.1532.1 GPS week: 1532 Day: 1 MJD: 54969.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3019 | 7 10 26 | 9 9 22 | 9 8 17 | emr | emr 2854 | 10 13 31 | 9 10 35 | 14 11 20 | esa | esa 2880 | 8 12 29 | 6 8 21 | 9 8 17 | gfz | gfz 2857 | 8 10 30 | 7 7 24 | 9 8 16 | grg | grg 2880 | 9 11 30 | 9 9 30 | ---- ---- ---- | igr | igr 2852 | 8 11 29 | 7 7 24 | 9 7 17 | igs | igs 2946 | 8 11 28 | 7 7 24 | 8 7 15 | jpl | jpl 2759 | 9 11 32 | 9 8 29 | 10 8 18 | mit | mit 3072 | 8 12 27 | 6 9 25 | 13 14 49 | Table 5.1532.2 GPS week: 1532 Day: 2 MJD: 54970.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3032 | 8 7 18 | 7 13 30 | 6 8 20 | emr | emr 2864 | 10 9 23 | 8 16 35 | 10 9 19 | esa | esa 2784 | 8 6 19 | 6 9 26 | 7 7 14 | gfz | gfz 2760 | 8 6 17 | 7 8 29 | 7 7 13 | grg | grg 2784 | 8 7 17 | 8 15 43 | 11 7 20 | igr | igr 2820 | 9 7 22 | 7 12 31 | 7 7 15 | igs | igs 2762 | 8 6 21 | 8 12 36 | 7 6 15 | jpl | jpl 2759 | 11 7 28 | 6 11 24 | 8 8 16 | mit | mit 2976 | 7 6 21 | 6 13 29 | 7 9 14 | Table 5.1532.3 GPS week: 1532 Day: 3 MJD: 54971.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3047 | 8 5 19 | 8 11 26 | 6 5 15 | emr | emr 2864 | 8 5 23 | 10 11 31 | 9 8 17 | esa | esa 2880 | 8 5 21 | 8 11 26 | 6 5 15 | gfz | gfz 2857 | 28 13 34 | 11 12 30 | 6 4 16 | grg | grg 2880 | 16 8 30 | 9 18 31 | 12 13 28 | igr | igr 2836 | 8 5 24 | 9 12 25 | 6 5 16 | igs | igs 2866 | 8 5 20 | 9 12 24 | 5 4 14 | jpl | jpl 2759 | 9 6 26 | 9 10 29 | 9 7 17 | mit | mit 3072 | 7 6 20 | 13 29 35 | 7 15 28 | Table 5.1532.4 GPS week: 1532 Day: 4 MJD: 54972.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3052 | 7 5 20 | 5 7 20 | 6 5 12 | emr | emr 2953 | 9 12 25 | 5 10 28 | 8 10 18 | esa | esa 2880 | 8 7 20 | 4 5 19 | 7 6 14 | gfz | gfz 2857 | 8 6 22 | 5 7 23 | 6 5 12 | grg | grg 2880 | 9 8 25 | 12 22 51 | 11 8 27 | igr | igr 2969 | 8 7 19 | 5 9 22 | 7 6 15 | igs | igs 2976 | 8 7 20 | 4 7 24 | 6 5 13 | jpl | jpl 2851 | 8 6 21 | 5 7 22 | 7 8 16 | mit | mit 3072 | 6 5 18 | 4 8 22 | 6 6 13 | Table 5.1532.5 GPS week: 1532 Day: 5 MJD: 54973.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3050 | 6 9 19 | 6 8 27 | 6 5 15 | emr | emr 2957 | 8 11 24 | 7 9 25 | 8 9 15 | esa | esa 2976 | 6 9 19 | 5 9 29 | 7 5 12 | gfz | gfz 2858 | 6 9 21 | 6 10 27 | 7 4 12 | grg | grg 2880 | 7 9 18 | 7 11 22 | 10 8 24 | igr | igr 2952 | 7 9 20 | 6 9 26 | 6 5 12 | igs | igs 2959 | 7 9 19 | 8 7 29 | 6 4 11 | jpl | jpl 2855 | 6 9 21 | 6 8 24 | 8 9 15 | mit | mit 3072 | 7 9 20 | 10 14 46 | 7 5 14 | Table 5.1532.6 GPS week: 1532 Day: 6 MJD: 54974.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3065 | 8 5 16 | 5 9 16 | 5 4 12 | emr | emr 2956 | 9 8 21 | 6 7 22 | 10 8 19 | esa | esa 2976 | 8 6 17 | 4 5 17 | 6 4 12 | gfz | gfz 2858 | 8 5 16 | 5 7 18 | 6 5 12 | grg | grg 2880 | 8 7 19 | 7 9 25 | 9 7 22 | igr | igr 2886 | 7 5 17 | 6 7 22 | 7 4 12 | igs | igs 2972 | 8 5 17 | 5 6 13 | 6 5 13 | jpl | jpl 2858 | 8 6 19 | 5 6 22 | 8 7 16 | mit | mit 3072 | 8 5 14 | 8 5 30 | 15 14 101 | 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 6.1532 GPS week: 1532 MJD: 54968.500-54974.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -7 -1 11 -101 2 | 2 11 | 29 17 82 89 6 | 2 emr uuuuu | 89 33 -30 130 -16 | 37 43 | 30 19 140 76 6 | 8 esa uuuuu | -27 -33 -24 20 12 | 9 17 | 25 33 142 120 6 | 2 gfz uuuuu | -6 -20 42 -114 -1 | 25 29 | 30 12 51 60 3 | 4 grg xxxxx | -16 -57 -15 -87 -3 | -2 24 | 46 28 57 118 45 | 4 igr xxxxx | 5 -17 -22 27 -4 | 4 16 | 24 22 64 81 10 | 4 irf xxxxx | -15 -12 35 -50 -1 | -5 15 | 4 8 56 38 5 | 4 jpl uuuuu | -16 0 -5 -15 -19 | 6 21 | 18 13 163 126 7 | 6 mit uuuuu | -20 -11 74 -70 -12 | 11 21 | 15 14 118 62 6 | 5 ngs uuuuu | 4 7 -54 36 5 | 2 12 | 23 36 130 68 7 | 2 sio uuxuu | 40 137 -538 193 0 | 69 71 | 10 18 149 44 4 | 4 Table 7.1532.0 GPS week: 1532 Day: 0 MJD: 54968.500 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 -5 126 -68 5 | 3 10 emr uuuuu | 53 21 -164 91 -20 | 44 47 esa uuuuu | -30 -51 118 -57 15 | 6 16 gfz uuuuu | 15 -5 96 -65 -5 | 28 32 grg xxxxx | 19 -80 2 -35 -51 | -2 17 igr xxxxx | 2 -16 -31 99 -1 | 0 21 irf xxxxx | -17 -11 -46 -29 -4 | -3 14 jpl uuuuu | -24 -6 179 -2 -9 | 10 20 mit uuuuu | -29 -9 -106 -72 -12 | 15 21 ngs uuuuu | 18 22 -68 95 1 | 3 13 sio uuxuu | 53 133 -604 179 0 | 73 74 Table 7.1532.1 GPS week: 1532 Day: 1 MJD: 54969.500 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 | -12 -7 -91 35 12 | 2 9 emr uuuuu | 128 17 -164 243 -9 | 42 46 esa uuuuu | -54 -66 4 -137 19 | 8 16 gfz uuuuu | 20 -21 -39 -34 0 | 26 30 grg xxxxx | -29 -90 19 46 18 | -8 25 igr xxxxx | 42 -31 -37 132 9 | 2 19 irf xxxxx | -17 -10 -1 -34 0 | -4 14 jpl uuuuu | 12 0 61 130 -16 | 10 20 mit uuuuu | -30 3 5 -131 -8 | 14 21 ngs uuuuu | -12 41 81 107 -1 | 1 12 sio uuxuu | 44 142 -659 126 2 | 72 73 Table 7.1532.2 GPS week: 1532 Day: 2 MJD: 54970.500 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 | 36 23 40 -54 -3 | 5 10 emr uuuuu | 97 27 -84 65 -22 | 44 47 esa uuuuu | -59 -56 -27 -111 15 | 12 19 gfz uuuuu | 11 -7 27 -58 0 | 28 31 grg xxxxx | 24 -20 -16 60 35 | -7 25 igr xxxxx | -25 -18 -76 -3 5 | 7 16 irf xxxxx | -12 -2 -13 10 -7 | -2 13 jpl uuuuu | -27 -1 18 24 -12 | 11 19 mit uuuuu | -18 7 -23 25 -17 | 16 21 ngs uuuuu | 47 27 75 76 5 | 3 11 sio uuxuu | 47 143 -745 223 -6 | 72 73 Table 7.1532.3 GPS week: 1532 Day: 3 MJD: 54971.500 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 | -12 11 62 -76 7 | 4 12 emr uuuuu | 126 38 -11 35 -16 | 40 46 esa uuuuu | -28 -49 -210 162 1 | 13 19 gfz uuuuu | 13 -23 91 -151 3 | 27 31 grg xxxxx | -39 -51 57 -243 44 | -4 24 igr xxxxx | 30 -3 81 -62 -2 | 8 15 irf xxxxx | -21 -24 51 -85 -1 | -3 16 jpl uuuuu | -23 -9 -7 -207 -22 | 9 21 mit uuuuu | -38 -24 113 -82 -12 | 14 22 ngs uuuuu | -22 39 0 83 11 | 2 12 sio uuxuu | 38 98 -483 227 5 | 70 72 Table 7.1532.4 GPS week: 1532 Day: 4 MJD: 54972.500 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 | 30 -10 -78 -217 -4 | 2 11 emr uuuuu | 79 72 3 176 -22 | 35 42 esa uuuuu | -21 1 -205 130 4 | 9 15 gfz uuuuu | -8 -22 47 -145 -5 | 24 28 grg xxxxx | 34 -83 14 -78 17 | -2 25 igr xxxxx | -19 24 -9 90 -19 | 6 15 irf xxxxx | -13 -10 87 -72 -7 | -6 16 jpl uuuuu | -35 9 105 -26 -29 | 5 22 mit uuuuu | -12 -19 158 -75 -23 | 10 21 ngs uuuuu | 12 -41 -16 -53 16 | 1 12 sio uuxuu | 36 146 -564 195 -6 | 68 70 Table 7.1532.5 GPS week: 1532 Day: 5 MJD: 54973.500 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 | -41 12 58 -207 1 | 2 11 emr uuuuu | 85 37 -40 196 -15 | 32 38 esa uuuuu | 9 -32 153 78 13 | 10 16 gfz uuuuu | -30 -23 77 -182 -2 | 24 27 grg xxxxx | -22 -29 -105 -157 -5 | 4 25 igr xxxxx | 3 -38 -110 5 -14 | 4 13 irf xxxxx | -16 -21 106 -101 5 | -7 16 jpl uuuuu | -24 24 -327 120 -19 | 1 21 mit uuuuu | -18 -29 228 -150 -6 | 7 20 ngs uuuuu | -9 3 -268 -20 5 | 2 14 sio uuxuu | 21 145 -340 150 3 | 67 69 Table 7.1532.6 GPS week: 1532 Day: 6 MJD: 54974.500 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 | -30 -28 -44 -122 -3 | -2 14 emr uuuuu | 59 17 248 106 -6 | 24 32 esa uuuuu | -4 22 1 73 15 | 7 14 gfz uuuuu | -60 -41 -4 -166 2 | 18 22 grg xxxxx | -98 -48 -76 -200 -76 | 1 27 igr xxxxx | 2 -35 28 -74 -10 | -2 17 irf xxxxx | -8 -2 59 -36 4 | -12 18 jpl uuuuu | 7 -13 -68 -146 -25 | -5 25 mit uuuuu | 9 -2 141 -8 -5 | 1 19 ngs uuuuu | -6 -43 -182 -33 -3 | -2 14 sio uuxuu | 42 154 -370 250 -1 | 62 64