Date: Thu, 06 May 2010 12:15:00 +0000 From: Jim Ray Subject: [IGSREPORT-18547] Wk 1580 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4be2b2c4.osVRBGXoDDGhmVSN%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 06 May 05:15:15 PDT 2010 Message Number 18547 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1580 (Apr 18, 2010 - Apr 24, 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: igs1580[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1580[0-6].clk IGS GPS satellite and station clocks in clock RINEX format. igs1580[0-6].cls IGS GPS clock combination summary report. igs15807.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15807.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 | DGAR 0 | EMR | WTZR 0 | ESA | DGAR 0 | GFZ | HARB SUTH UNSA 0 | GRG | CAS1 DGAR POTS WTZR 0 | JPL | 4 0 | MIT | 8 9 27 8 9 27 CAS1 CAS1 HARB 1 | ALL | 1 1 | COD | USNO ALGO BRAZ USNO 1 | EMR | 4 4 WTZR WTZR 1 | GFZ | BOR1 DGAR SUTH UNSA 1 | GRG | ONSA 1 | JPL | 4 21 BRUS 1 | MIT | 4 8 27 4 8 DAV1 ALGO DAV1 2 | COD | DAV1 DAV1 DGAR NRIL XMIS 2 | EMR | 4 4 YELL 2 | ESA | DGAR UNSA 2 | GFZ | SUTH 2 | GRG | DGAR ONSA 2 | JPL | 4 24 2 | MIT | 4 8 4 8 3 | COD | BRAZ DGAR WES2 3 | EMR | 4 9 27 4 9 27 ONSA WTZR METS 3 | ESA | DGAR OHI2 3 | GFZ | MATE METS MIZU NICO ONSA SUTH 3 | GRG | DGAR WTZR 3 | JPL | 4 9 27 UNSA 3 | MIT | 4 8 9 18 27 4 8 9 18 27 AUCK CAS1 HOB2 NNOR TOW2 3 | MIT | CAS1 4 | ALL | 1 1 4 | COD | XMIS 4 | EMR | 4 8 27 4 8 4 | ESA | MATE SCH2 SCH2 4 | GFZ | 27 DGAR MAW1 SUTH 4 | GRG | ONSA 4 | JPL | 4 8 27 4 | MIT | 8 26 8 26 MAW1 OUS2 5 | ALL | 1 1 5 | COD | DGAR UNBJ 5 | EMR | 4 8 9 27 4 8 9 27 WTZR 5 | ESA | DGAR 5 | GFZ | CHUR SUTH 5 | GRG | DGAR ONSA 5 | JPL | 4 8 9 27 5 | MIT | 8 9 24 27 8 9 24 27 USNO HARB USNO 6 | ALL | 1 1 6 | COD | DGAR MATE MDVJ 6 | EMR | 4 8 21 4 8 9 21 MIZU WTZR MIZU 6 | ESA | METS DGAR METS UNSA 6 | GFZ | SUTH 6 | GRG | DGAR ONSA POTS 6 | JPL | 4 8 21 27 6 | MIT | 8 9 21 8 9 21 26 KOUR MDVJ 5. 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) 6 | SIO | ALL (high Transformation - See Table 2) 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 | | | | | | 1 | 1 | 7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447. 8. Small rotations were applied to 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 | .0 .8 .5 -20 -3 -19 .0 EMR | 5.2 -.6 -.2 31 25 -2 .29 ESA | 6.3 1.6 -1.3 53 -34 -39 .08 GFZ | -1.0 .9 -.3 -19 30 -95 .32 GRG | 3.6 1.1 9.3 16 32 9 .29 JPL | 3.4 -.6 -3.1 22 -22 12 .48 MIT | 6.7 -4.1 .1 2 9 -27 -.03 NGS | 10.0 -6.3 -2.9 -97 -188 47 .18 SIO | 3.8 .2 -16.7 -65 338 -725 .25 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 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. 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 1.1580.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1580.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 2.1580.[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 3.1580.[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 5.1580.0-6). 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 1580 summary. (Apr 18, 2010 - Apr 24, 2010) Table 1.1580.a GPS week: 1580 MJD: 55304.000-55310.000 Mean and standard deviations of transformation parameters to the combined IGS orbit. WRMS - orbit RMS weighted by the SP3 header accuracy codes. STA - Mean number of stations in the daily solutions. CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 243| 0 0 0 10 -38 -16 -.21 10 8 | -414 -413 21 73 | 0 0 1 18 9 15 .01 | 343 643 emr 87| 0 0 0 -51 -88 17 .40 20 20 | -901 1106 20 96 | 1 1 1 19 19 21 .02 | 2579 1481 esa 142| 0 1 0 -113 -9 -20 .27 9 8 | -1274 856 18 100 | 0 0 1 15 25 21 .01 | 1724 2541 gfz 195| 0 0 3 24 -114 8 -.09 12 12 | 70 -18 22 96 | 0 0 1 38 41 5 .04 | 295 456 grg 123| -1 0 -1 -70 -70 -4 .63 19 17 | -98 -3 55 211 | 1 1 2 52 22 12 .05 | 302 616 igr n/a| 0 0 0 3 -48 14 .01 6 5 | 1269 1098 19 66 | 0 0 1 25 33 35 .03 | 2800 1671 jpl 117| -1 1 -3 -54 -15 65 .49 20 20 | 451 1182 20 119 | 1 0 1 18 12 21 .04 | 2676 1548 mit 269| -1 -1 -1 -18 -72 12 -.32 12 11 | -16275 721 26 161 | 0 0 1 15 22 13 .02 | 565 960 ngs 216| 1 -1 0 202 331 -5 -.23 15 8 | 6310 -2799 2128 3826 | 0 0 1 27 22 11 .02 | 8349 3322 sio 260| -2 2 5 145 -732 -692 -.26 22 22 | --- --- --- --- | 1 1 1 32 32 13 .02 | --- --- Table 1.1580.b GPS week : 1580 MJD: 55304.000-55310.000 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 14 13 16 22 19 23 | 2 | 6 6 5 5 5 5 7 | 3 | 5 4 4 4 4 4 5 | 4 | 6 6 6 6 6 6 9 | 5 | 5 5 5 5 6 5 5 | 6 | 5 4 4 4 5 4 4 | 7 | 5 6 5 5 6 5 6 | 8 | 7 7 7 7 9 9 9 | 9 | 7 6 6 6 6 6 7 | 10 | 4 4 4 4 3 4 4 | 11 | 5 5 4 4 5 5 5 | 12 | 5 5 5 5 6 5 6 | 13 | 5 5 5 4 5 5 5 | 14 | 6 5 5 5 6 6 5 | 15 | 6 6 5 5 5 5 6 | 16 | 6 5 6 6 6 6 6 | 17 | 6 5 5 5 5 5 5 | 18 | 5 6 5 7 6 6 6 | 19 | 6 5 6 6 5 5 6 | 20 | 6 5 5 6 6 6 6 | 21 | 5 6 4 5 5 5 5 | 22 | 5 5 4 5 5 5 5 | 23 | 6 5 6 5 7 5 5 | 24 | 10 10 9 9 9 10 9 | 26 | 4 4 3 4 4 4 4 | 27 | 6 7 7 7 8 8 6 | 28 | 6 6 6 5 6 6 6 | 29 | 5 5 5 5 6 5 5 | 30 | 4 3 4 4 4 4 4 | 31 | 4 5 5 5 5 5 5 | 32 | 6 5 5 5 6 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 2.1580.0 GPS week: 1580 Day: 0 MJD: 55304.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 243| 0 0 0 -18 -29 -33 -.21 9 9 | -53 -1301 20 69 | 34 -55 | emr 87| 2 -3 1 -79 -80 19 .38 20 20 | -3317 416 25 103 | -55 -22 | esa 142| 0 2 -2 -115 -55 -8 .27 10 9 | -2079 -1158 17 108 | 21 45 | gfz 195| 0 0 5 93 -52 7 -.09 11 11 | 249 -508 21 95 | -91 11 | grg 123| 0 0 -2 -145 -104 -3 .60 21 20 | 45 -668 55 201 | 187 20 | igr n/a| 0 0 0 -6 -19 18 -.00 6 6 | -1152 9 17 62 | -52 -20 | jpl 117| -1 2 -2 -76 3 56 .46 20 19 | -1824 145 22 120 | 17 -35 | mit 269| -1 -1 0 -9 -87 0 -.31 14 13 | -16710 1274 24 163 | -4 21 | ngs 216| 1 -1 -1 165 315 7 -.25 15 8 | 15895 -6817 2233 3494 | 72 -80 | sio 260| -3 3 7 140 -750 -698 -.27 22 23 | --- --- --- --- | -174 321 | Table 2.1580.1 GPS week: 1580 Day: 1 MJD: 55305.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 243| 0 0 0 8 -27 -8 -.22 10 9 | -718 168 23 76 | 43 -18 | emr 87| 1 1 0 -54 -86 -3 .38 20 20 | -2950 732 26 82 | -47 -12 | esa 142| 0 0 -1 -103 -29 -15 .29 9 8 | -409 -835 22 95 | 7 21 | gfz 195| 0 -1 3 38 -113 5 -.09 11 11 | -280 509 21 89 | -95 -8 | grg 123| -2 0 -3 -96 -46 -17 .63 19 18 | -19 168 58 210 | 88 -103 | igr n/a| 0 0 0 -30 0 21 -.01 5 5 | -1228 715 20 61 | -41 -26 | jpl 117| -1 1 -1 -55 -19 73 .47 20 19 | -1834 733 22 113 | -7 12 | mit 269| -1 -1 -1 -16 -84 3 -.31 12 11 | -16141 268 30 139 | 6 23 | ngs 216| 0 0 0 172 355 -5 -.24 14 7 | 14668 -3014 1813 3596 | 56 -8 | sio 260| -4 3 6 142 -725 -698 -.29 22 23 | --- --- --- --- | -172 326 | Table 2.1580.2 GPS week: 1580 Day: 2 MJD: 55306.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 243| 0 1 0 34 -39 -4 -.21 9 8 | -670 186 29 84 | -31 -16 | emr 87| 0 0 -1 -36 -93 8 .40 19 19 | -2582 796 24 86 | -69 -23 | esa 142| 0 1 0 -125 0 -23 .28 8 8 | 17 -838 24 96 | 27 14 | gfz 195| 0 0 5 -7 -179 18 -.05 11 11 | -48 130 24 91 | -99 0 | grg 123| -2 1 -1 -19 -44 -4 .65 19 17 | -403 569 55 210 | -5 -137 | igr n/a| 0 0 0 -7 -43 -1 .02 6 5 | -576 891 22 67 | -62 -21 | jpl 117| -3 0 -3 -25 -31 72 .51 21 21 | -1234 688 25 120 | -11 -138 | mit 269| -2 0 -2 -42 -70 7 -.31 11 10 | -16073 82 32 167 | 1 17 | ngs 216| 1 -2 0 220 345 -15 -.25 13 7 | -793 299 1960 3803 | -27 -52 | sio 260| -5 3 6 85 -711 -713 -.28 22 23 | --- --- --- --- | -165 328 | Table 2.1580.3 GPS week: 1580 Day: 3 MJD: 55307.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 243| 0 0 0 -10 -31 -1 -.19 9 8 | -43 -785 18 73 | 34 -67 | emr 87| -1 -2 -1 -38 -97 18 .39 19 19 | -2049 2461 15 94 | -70 -10 | esa 142| 1 2 0 -121 -3 -36 .28 9 9 | -3294 4068 15 85 | 15 -15 | gfz 195| 0 0 6 37 -133 11 -.13 12 12 | 611 -739 23 102 | -79 -36 | grg 123| -2 0 1 -109 -60 7 .58 17 16 | -13 -117 76 209 | 129 -107 | igr n/a| 0 0 0 34 -53 -57 .03 6 5 | 62 2588 19 63 | -44 -38 | jpl 117| 0 1 -2 -67 -17 53 .55 20 20 | -780 2300 20 113 | 39 -2 | mit 269| -2 0 -1 1 -91 21 -.32 11 11 | -16536 1721 24 147 | 3 28 | ngs 216| 0 0 -1 184 342 -13 -.23 14 8 | -68 -769 2125 3966 | -55 -56 | sio 260| -2 3 4 167 -753 -692 -.27 21 21 | --- --- --- --- | -185 343 | Table 2.1580.4 GPS week: 1580 Day: 4 MJD: 55308.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 243| 0 0 0 24 -48 -37 -.21 10 8 | -886 264 22 71 | 14 3 | emr 87| -1 0 -1 -31 -109 61 .40 21 21 | -606 3760 22 92 | -114 0 | esa 142| 0 1 0 -108 6 -50 .26 9 9 | -2930 3924 23 118 | 31 28 | gfz 195| 0 0 2 -2 -87 9 -.10 12 12 | -171 285 23 97 | -115 -12 | grg 123| 0 0 0 -58 -65 -4 .61 17 15 | -609 698 49 196 | 5 -63 | igr n/a| 0 0 0 34 -51 43 -.01 5 5 | 1638 4122 21 68 | -54 -10 | jpl 117| 0 1 -3 -70 -26 108 .52 20 20 | 525 4218 20 116 | 14 1 | mit 269| -1 -2 -2 -33 -54 38 -.31 12 11 | -17055 2055 31 159 | 5 14 | ngs 216| 1 0 3 228 320 -10 -.19 16 10 | 15110 -7994 2147 3924 | 97 -3 | sio 260| -1 1 5 143 -714 -669 -.26 21 19 | --- --- --- --- | -196 339 | Table 2.1580.5 GPS week: 1580 Day: 5 MJD: 55309.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 243| 0 0 1 20 -46 -3 -.22 10 9 | -352 -375 17 73 | 3 -6 | emr 87| -1 0 0 -76 -103 16 .42 20 20 | 3365 -458 15 105 | -67 -3 | esa 142| 0 1 -1 -85 -8 -25 .26 9 8 | 1510 -1687 13 97 | 45 34 | gfz 195| -1 0 1 -19 -93 0 -.04 12 12 | 20 287 21 97 | -87 6 | grg 123| -1 0 0 -72 -72 -24 .62 19 16 | 30 274 48 214 | 4 -55 | igr n/a| 0 0 2 18 -105 32 .06 6 5 | 5806 -255 19 73 | -22 27 | jpl 117| 0 2 -3 -53 -12 46 .46 19 19 | 4793 -36 17 112 | -20 -22 | mit 269| -1 -1 -1 -22 -30 8 -.35 11 10 | -15289 -512 22 193 | 1 8 | ngs 216| 2 -1 0 227 292 12 -.25 15 9 | -353 -410 2096 3895 | -54 -48 | sio 260| -1 0 5 147 -686 -694 -.23 23 21 | --- --- --- --- | -179 325 | Table 2.1580.6 GPS week: 1580 Day: 6 MJD: 55310.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 243| -1 0 3 13 -48 -29 -.22 12 8 | -182 -1048 18 70 | 46 -28 | emr 87| 0 0 0 -46 -50 2 .43 22 22 | 1830 40 17 110 | -68 -40 | esa 142| 1 1 1 -132 22 15 .26 8 7 | -1737 2523 14 103 | 32 26 | gfz 195| 0 0 1 33 -144 4 -.15 11 11 | 111 -92 21 101 | -79 15 | grg 123| 0 3 -4 7 -95 12 .72 21 19 | 281 -951 48 239 | -95 -40 | igr n/a| 0 0 0 -19 -65 45 -.01 6 6 | 4333 -383 21 74 | -63 13 | jpl 117| -2 1 -5 -35 -5 48 .43 21 20 | 3512 229 20 140 | 20 1 | mit 269| 0 -1 -2 -2 -89 6 -.34 14 13 | -16124 161 19 162 | -3 20 | ngs 216| 1 0 0 217 349 -16 -.23 15 9 | -289 -889 2528 4109 | -54 -110 | sio 260| 0 1 4 190 -782 -683 -.23 21 20 | --- --- --- --- | -181 333 | 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 3.1580.0 GPS week: 1580 Day: 0 MJD: 55304.000 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 --- --- --- --- 21 --- 20 24 --- 13 | 49 --- --- --- --- 40 --- 53 23 --- 48 2E | 7 25 11 10 26 4 21 19 8 17 5 | 20 33 20 19 25 19 29 26 20 24 20 3 | 7 16 9 10 17 8 12 12 13 15 4 | 11 22 21 20 21 12 15 14 20 16 14 4E | 11 17 8 12 21 4 15 18 23 26 6 | 49 49 47 48 42 48 46 44 54 46 46 5 | 8 20 7 11 22 5 22 14 8 17 5 | 15 28 18 18 27 16 30 16 19 19 16 6 | 7 14 10 10 16 5 15 11 14 18 4 | 15 21 24 21 22 15 18 17 22 24 17 7E | 8 25 7 11 24 3 20 11 9 13 5 | 23 32 23 25 26 21 30 21 29 22 23 8E | 17 19 8 19 18 7 17 16 25 17 7 | 28 34 31 42 34 31 35 31 46 31 33 X9E | 8 20 11 --- 21 6 17 19 15 19 6 | 15 29 20 --- 26 16 29 19 24 20 15 10 | 7 14 7 9 15 4 11 11 8 19 3 | 14 16 18 14 21 12 15 18 20 16 14 11 | 6 20 8 11 26 5 16 11 8 18 4 | 17 29 26 18 42 19 29 17 23 14 20 12 | 10 23 11 11 22 8 22 10 7 31 5 | 18 31 24 24 30 22 31 19 18 20 20 13 | 8 19 8 9 27 5 24 14 12 17 5 | 23 29 25 25 37 23 31 29 31 24 24 14 | 11 21 9 15 19 6 22 9 13 24 5 | 16 24 20 25 30 17 26 17 17 20 16 15 | 9 20 8 9 21 5 26 12 9 16 5 | 17 27 21 19 32 17 25 19 18 22 16 16 | 10 19 9 11 19 4 24 20 11 27 6 | 16 26 20 21 23 16 28 20 19 24 17 17 | 8 22 11 10 21 6 21 15 9 31 5 | 24 30 21 24 20 22 31 23 23 24 21 18 | 8 22 10 11 19 4 23 12 8 20 5 | 19 33 22 20 29 19 31 19 19 25 19 19 | 8 25 11 11 16 8 25 10 9 26 5 | 19 37 15 18 23 19 36 22 22 20 19 20 | 9 22 9 12 19 4 26 13 11 23 5 | 14 28 23 23 28 16 29 19 18 17 16 21E | 9 19 9 9 24 6 18 10 14 15 5 | 14 27 16 11 29 11 25 16 20 20 13 22 | 8 23 9 10 24 6 21 11 12 23 5 | 17 29 21 21 32 17 26 20 17 27 17 23 | 9 23 10 11 31 4 26 14 11 23 5 | 17 30 22 20 35 17 30 17 18 17 18 24E | 16 22 17 18 25 10 21 16 47 21 9 | 33 35 32 39 36 35 31 38 66 33 33 26 | 6 16 7 11 15 5 12 14 5 28 4 | 10 19 14 9 21 11 18 13 16 28 11 27E | 9 19 12 8 18 4 15 15 27 17 6 | 54 63 54 54 55 55 58 55 58 54 54 28 | 7 24 10 13 18 4 24 17 9 30 5 | 18 30 24 27 27 20 28 27 23 23 20 29 | 14 19 9 10 15 5 18 12 10 --- 5 | 21 32 20 16 21 19 34 21 23 --- 18 30 | 5 14 8 8 18 4 9 10 10 21 3 | 25 23 29 29 32 25 25 25 30 24 27 31E | 5 16 10 9 27 6 19 10 8 21 4 | 9 20 13 13 27 7 19 10 16 14 11 32 | 10 22 7 8 23 6 18 19 12 23 5 | 15 22 22 21 28 18 22 23 22 13 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 10 11 21 6 20 14 15 22 |T 21 29 23 23 29 21 28 23 25 23 21 WRMS | 9 20 9 11 20 6 19 13 8 23 |NE 18 26 21 20 27 18 26 21 20 20 19 MEDI | 8 20 9 11 21 5 20 13 11 21 |MD 17 29 21 21 28 19 29 20 22 22 19 Table 3.1580.1 GPS week: 1580 Day: 1 MJD: 55305.000 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 --- --- --- --- 31 --- 18 24 --- 14 | 44 --- --- --- --- 41 --- 42 35 --- 40 2E | 9 23 9 12 21 5 21 16 10 17 5 | 14 30 19 16 20 16 25 23 22 23 17 3 | 8 13 6 8 16 5 13 8 4 14 3 | 11 18 17 13 15 14 15 12 22 12 13 4E | 13 17 6 10 16 6 12 17 22 25 6 | 36 36 34 38 32 34 33 32 48 32 34 5 | 11 20 6 14 19 7 22 9 11 16 5 | 12 26 14 19 25 12 26 14 20 15 13 6 | 8 13 7 7 15 4 15 10 5 15 3 | 14 18 16 13 14 14 13 15 24 18 14 7E | 9 28 9 11 27 4 21 9 10 17 5 | 16 29 19 18 24 15 24 17 22 19 16 8E | 17 22 7 16 17 7 19 12 25 20 7 | 17 25 14 18 16 18 23 14 35 16 15 X9E | 8 19 8 --- 17 5 18 18 13 19 6 | 14 27 20 --- 23 15 28 19 30 15 17 10 | 8 13 7 9 18 4 12 10 10 15 4 | 19 25 20 25 24 21 19 24 22 26 19 11 | 10 14 8 11 19 4 16 11 10 16 4 | 17 24 25 18 37 18 28 16 29 13 20 12 | 9 21 9 9 18 4 22 10 11 32 5 | 14 26 20 21 26 17 29 14 19 15 17 13 | 9 18 9 8 24 4 25 11 10 19 5 | 18 27 22 18 38 18 30 19 28 17 19 14 | 7 21 9 12 13 4 23 10 9 24 5 | 15 25 18 19 26 15 27 17 22 17 16 15 | 12 24 9 14 25 6 24 8 14 17 6 | 14 27 16 20 30 15 25 16 28 21 14 16 | 8 20 9 10 16 5 23 16 8 25 5 | 15 22 15 15 17 15 25 14 24 18 15 17 | 8 20 8 11 15 4 21 14 7 31 5 | 20 25 13 23 15 16 24 20 22 21 16 18 | 6 22 10 14 17 4 25 10 11 22 5 | 19 33 26 24 31 19 32 21 27 26 23 19 | 9 22 10 10 16 6 26 9 6 28 5 | 15 27 16 15 18 17 29 17 24 12 16 20 | 9 25 7 8 18 4 23 13 9 21 5 | 12 27 19 18 28 13 26 15 23 13 14 21E | 12 15 23 10 23 7 16 9 12 17 6 | 16 22 28 12 31 10 23 13 22 15 14 22 | 6 17 8 9 23 5 22 11 9 26 4 | 16 26 18 19 29 15 25 19 25 24 18 23 | 9 21 8 7 24 4 26 12 7 24 5 | 19 31 22 18 36 19 30 20 24 21 19 24E | 18 21 15 16 20 6 20 13 44 23 9 | 34 34 32 35 32 34 32 33 62 33 32 26 | 6 15 6 12 17 3 13 11 8 29 4 | 11 20 14 12 22 11 20 13 23 26 13 27E | 11 21 11 15 21 4 18 16 24 19 6 | 47 50 48 48 45 47 51 55 56 50 48 28 | 9 25 9 13 19 5 25 12 12 31 5 | 13 28 17 21 23 14 24 20 23 19 15 29 | 9 16 9 9 18 5 22 11 7 --- 4 | 12 27 20 15 23 14 29 14 22 --- 15 30 | 5 14 6 7 11 3 11 8 7 19 3 | 22 23 23 21 23 22 23 24 30 22 23 31E | 6 19 8 9 26 5 20 11 8 22 4 | 13 23 13 13 22 11 22 14 21 13 13 32 | 13 17 6 9 17 4 16 13 8 19 4 | 18 25 25 27 21 21 23 30 19 27 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 20 9 11 19 5 20 12 14 22 |T 18 26 20 20 25 18 26 20 27 20 19 WRMS | 9 20 8 11 18 5 19 11 7 23 |NE 16 25 18 18 24 17 24 18 24 19 17 MEDI | 9 20 8 10 18 5 21 11 10 20 |MD 16 26 19 18 24 16 25 17 24 19 16 Table 3.1580.2 GPS week: 1580 Day: 2 MJD: 55306.000 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 | 10 --- --- --- --- 27 --- 15 --- 34 12 | 40 --- --- --- --- 42 --- 39 --- 53 40 2E | 7 21 8 10 27 6 25 11 7 18 5 | 22 32 21 23 33 21 33 24 27 24 22 3 | 7 13 5 12 21 4 13 7 9 15 3 | 11 18 16 18 19 13 17 13 24 13 15 4E | 11 18 10 11 19 5 14 15 20 26 5 | 31 32 27 27 32 30 32 26 40 24 28 5 | 10 15 7 10 19 6 25 10 8 19 4 | 16 26 19 18 25 16 30 16 29 20 19 6 | 7 15 6 9 19 4 13 8 11 15 4 | 14 19 18 16 19 14 17 16 26 18 17 7E | 7 22 11 9 22 4 27 7 12 22 5 | 23 33 30 23 26 24 37 24 31 24 25 8E | 16 23 8 17 18 8 18 12 24 24 7 | 28 34 32 35 30 31 37 30 45 31 30 X9E | 7 21 9 --- 19 6 17 14 11 19 5 | 15 27 18 --- 24 17 28 18 30 17 17 10 | 9 12 7 7 19 5 11 13 7 16 4 | 29 31 29 27 29 28 30 36 39 28 31 11 | 6 11 7 10 19 7 19 8 7 17 3 | 14 23 23 17 35 16 24 15 21 13 18 12 | 9 20 9 12 17 5 23 11 7 30 5 | 17 26 21 21 28 17 28 19 18 17 18 X13 | 7 20 6 7 20 7 --- 12 10 20 4 | 14 30 23 20 38 18 --- 18 22 14 18 14 | 8 21 9 11 15 5 23 10 5 22 5 | 16 26 21 19 26 16 28 16 21 20 18 15 | 8 21 8 10 23 5 25 14 6 17 5 | 14 25 18 15 31 14 26 17 22 20 14 16 | 9 24 7 9 20 7 23 17 7 25 5 | 16 26 19 17 17 15 23 17 27 18 18 17 | 9 18 10 9 13 3 19 10 6 30 4 | 17 25 18 18 17 16 29 18 21 20 15 18 | 8 18 9 8 16 5 24 8 8 20 4 | 16 27 23 19 30 16 32 18 27 23 20 19 | 8 23 10 13 16 9 28 9 8 27 5 | 17 32 15 16 18 16 34 20 26 15 19 20 | 8 20 8 10 18 5 25 12 10 21 5 | 12 24 18 21 28 14 30 16 18 13 15 21E | 9 18 7 8 13 5 18 6 8 13 4 | 19 28 25 13 30 17 32 18 27 19 21 22 | 8 16 9 8 24 4 20 7 8 20 4 | 17 26 23 20 34 16 26 19 22 25 20 23 | 9 20 6 10 17 4 32 12 6 23 5 | 15 27 18 16 28 14 32 17 17 15 14 24E | 19 17 11 23 19 9 21 15 40 23 9 | 32 34 30 37 29 33 29 32 53 30 29 26 | 6 13 4 7 16 4 12 10 6 27 3 | 12 16 17 12 22 13 20 13 22 25 15 27E | 10 19 10 19 20 7 16 13 24 20 6 | 35 37 31 28 34 31 38 38 46 40 34 28 | 8 28 7 13 19 5 22 10 9 33 5 | 15 36 21 24 25 17 28 21 26 21 19 29 | 9 16 6 9 21 6 23 11 12 --- 4 | 13 27 20 14 21 17 32 17 25 --- 17 30 | 7 12 7 8 12 6 15 7 7 19 3 | 15 18 23 25 25 20 19 17 21 17 18 31E | 6 17 7 13 22 6 22 8 7 20 4 | 10 22 15 14 20 11 21 13 22 16 13 32 | 10 18 11 10 14 4 21 9 10 21 5 | 15 20 19 17 21 15 21 20 24 17 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 8 11 19 6 21 11 13 22 |T 18 26 21 20 26 19 28 20 27 21 20 WRMS | 8 19 8 11 17 5 21 10 7 23 |NE 16 25 20 18 25 17 26 19 23 20 18 MEDI | 8 18 8 10 19 5 21 10 8 20 |MD 16 26 21 19 26 16 29 18 25 20 18 Table 3.1580.3 GPS week: 1580 Day: 3 MJD: 55307.000 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 --- --- --- --- 20 --- 17 --- 34 15 | 64 --- --- --- --- 63 --- 61 --- 54 64 2E | 6 21 10 13 18 4 21 10 8 18 5 | 19 28 16 19 25 18 27 23 25 23 19 3 | 8 15 9 14 16 5 13 7 11 12 4 | 12 20 17 21 19 14 16 16 18 15 15 4E | 11 19 11 18 16 5 13 14 20 26 6 | 36 39 36 40 36 38 39 39 45 37 37 5 | 6 18 9 12 17 4 22 14 6 25 5 | 13 27 17 15 23 13 28 18 17 18 15 6 | 8 14 9 11 15 5 12 10 8 13 4 | 15 17 17 21 19 15 14 19 18 20 16 7E | 7 19 12 10 18 5 22 9 11 18 5 | 16 27 23 16 24 19 28 17 22 19 18 8E | 15 22 10 17 18 6 18 12 30 24 7 | 26 31 25 31 33 23 30 28 40 29 25 X9E | 6 19 8 --- 21 6 19 13 12 19 5 | 16 28 24 --- 27 20 32 21 27 24 20 10 | 5 12 7 10 13 5 11 6 9 14 3 | 30 32 29 31 33 30 33 34 38 34 32 11 | 7 23 6 9 19 5 16 8 6 16 4 | 18 34 24 18 35 22 27 19 22 19 21 12 | 9 20 8 12 16 3 23 10 8 27 5 | 20 28 22 25 29 20 28 23 21 19 21 X13 | 8 20 7 7 24 5 --- 9 7 18 4 | 20 30 19 20 37 18 --- 18 19 19 17 14 | 8 19 9 13 13 4 22 8 10 19 5 | 17 28 22 22 27 17 29 18 23 20 19 15 | 10 23 8 10 22 4 23 9 10 15 5 | 12 28 17 15 28 14 27 18 19 18 14 16 | 10 22 7 19 17 8 24 16 8 24 6 | 18 27 20 30 19 20 29 21 22 21 20 17 | 9 16 11 10 13 4 20 9 12 33 5 | 18 23 15 15 14 15 25 17 20 23 14 X18 | 8 25 --- 12 22 10 --- 11 12 20 6 | 23 38 --- 28 36 22 --- 27 26 29 26 19 | 6 24 12 14 16 13 24 8 10 26 5 | 23 33 18 16 21 26 36 24 27 21 22 20 | 7 24 14 12 18 5 24 15 8 19 5 | 13 28 24 18 28 14 27 17 13 17 14 21E | 11 19 9 9 20 4 19 9 10 12 4 | 15 29 20 18 24 15 26 17 20 18 17 22 | 6 18 8 8 20 5 21 12 9 16 4 | 19 28 24 22 26 17 27 21 21 22 20 23 | 9 18 8 11 18 4 28 8 8 21 5 | 19 30 24 24 29 22 31 19 21 20 20 24E | 19 22 13 18 18 8 17 19 39 22 9 | 49 51 45 54 48 50 48 48 63 46 47 26 | 6 13 7 10 15 3 10 12 6 27 3 | 11 17 17 10 22 11 19 14 20 25 13 27E | 9 20 12 18 23 6 18 13 24 20 6 | 56 60 60 59 59 57 63 59 60 60 58 28 | 6 25 10 7 15 5 24 9 11 33 5 | 15 28 24 21 24 16 28 20 21 20 17 29 | 10 18 7 9 21 4 20 11 13 --- 5 | 14 29 20 15 19 17 30 18 26 --- 18 30 | 7 14 5 9 11 4 12 6 6 15 3 | 22 22 29 28 31 22 22 27 31 22 26 31E | 6 19 7 9 22 5 19 11 10 19 4 | 13 26 17 17 22 12 23 14 23 17 16 32 | 8 19 6 10 16 6 16 14 9 19 4 | 14 20 17 18 21 13 18 21 17 16 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 9 12 17 6 20 11 14 21 |T 21 29 23 23 27 22 28 24 26 24 23 WRMS | 8 19 9 12 16 5 20 11 8 21 |NE 19 27 20 20 25 20 26 22 21 22 20 MEDI | 8 19 9 11 18 5 19 10 10 19 |MD 18 28 22 21 26 18 28 20 22 20 19 Table 3.1580.4 GPS week: 1580 Day: 4 MJD: 55308.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 30 --- --- --- --- 40 --- 24 35 41 21 | 65 --- --- --- --- 81 --- 82 33 64 73 2E | 7 27 8 9 17 4 19 11 10 18 5 | 22 39 24 22 30 22 31 27 31 29 23 3 | 8 12 8 8 13 4 11 10 12 11 4 | 11 18 20 16 17 13 15 14 27 14 14 4E | 11 18 9 13 16 4 16 15 21 24 6 | 36 42 37 38 36 38 37 39 44 39 36 5 | 8 17 8 11 21 5 23 17 11 24 5 | 12 26 14 17 26 12 27 20 27 18 14 6 | 8 13 10 10 13 5 14 12 13 12 4 | 17 19 24 21 19 18 15 20 27 22 18 7E | 7 24 12 10 21 5 26 8 10 16 5 | 16 29 24 21 34 17 26 17 28 18 17 8E | 22 23 10 18 23 8 18 16 35 20 8 | 41 50 46 48 49 43 47 48 57 47 44 X9E | 8 18 8 --- 18 8 20 13 14 17 5 | 15 28 17 --- 25 18 30 19 32 21 16 10 | 6 11 5 8 15 4 12 8 9 17 3 | 19 25 19 23 22 20 19 23 22 19 18 11 | 8 21 6 11 19 5 20 10 9 18 4 | 19 30 26 18 35 20 30 22 31 16 21 12 | 10 23 10 13 14 5 23 10 10 27 5 | 16 32 18 28 27 22 29 19 22 17 18 13 | 8 22 7 9 19 7 27 10 10 18 5 | 17 34 18 19 36 20 36 19 27 17 18 14 | 10 23 10 16 13 5 29 10 13 18 6 | 15 27 21 22 26 17 30 20 27 20 17 15 | 8 18 10 7 19 6 24 9 9 16 4 | 14 26 20 17 30 15 28 21 23 19 16 16 | 9 22 8 9 13 3 24 14 12 22 5 | 14 23 15 19 21 16 28 18 20 20 14 17 | 7 19 9 12 14 4 20 8 11 38 4 | 20 27 17 19 19 18 26 21 30 31 17 18 | 9 24 11 9 19 6 23 12 14 19 5 | 16 32 25 21 28 18 33 17 24 19 16 19 | 9 17 8 11 13 6 22 10 12 24 5 | 17 29 16 17 16 18 31 19 29 15 17 20 | 7 29 11 10 20 7 24 13 11 18 6 | 12 28 24 20 28 13 26 19 26 14 15 21E | 11 18 11 9 14 4 19 11 14 15 5 | 20 26 18 13 23 12 25 16 23 14 15 22 | 8 18 9 10 23 5 20 11 13 16 5 | 17 28 22 23 31 16 28 20 24 21 19 X23 | 10 27 --- 11 24 8 --- 9 10 21 6 | 17 34 --- 22 36 18 --- 18 25 15 19 24E | 17 20 15 19 22 6 15 20 39 25 8 | 53 51 47 61 52 49 50 54 70 47 52 26 | 6 15 7 14 15 5 13 10 7 27 4 | 10 20 15 15 22 13 19 13 25 25 12 27E | 14 20 12 26 17 6 18 12 30 19 7 | 33 44 33 48 34 36 38 35 47 39 34 28 | 6 25 10 11 15 5 25 8 10 30 5 | 16 30 23 24 27 19 27 20 28 16 18 29 | 12 22 10 8 19 3 20 12 12 --- 5 | 12 30 22 18 22 16 30 18 25 --- 17 30 | 6 17 5 10 10 5 11 9 8 15 3 | 26 24 24 24 26 23 22 25 35 23 24 31E | 7 21 6 9 24 4 21 7 11 22 4 | 13 25 14 21 26 14 25 19 22 23 14 32 | 8 27 6 13 14 6 20 13 12 20 5 | 13 20 19 21 22 15 18 22 27 17 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 21 9 12 17 5 20 12 16 21 |T 20 29 22 24 28 22 28 24 30 23 21 WRMS | 8 21 9 12 15 5 20 11 10 19 |NE 17 26 20 20 25 20 25 22 26 21 19 MEDI | 8 20 9 10 17 5 20 11 12 19 |MD 17 28 21 21 26 18 28 20 27 19 17 Table 3.1580.5 GPS week: 1580 Day: 5 MJD: 55309.000 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 | 17 --- --- --- --- 62 --- 22 --- 43 19 | 100 --- --- --- --- 92 --- 101 --- 81 100 2E | 7 26 9 10 20 5 19 11 7 18 5 | 17 33 18 20 24 17 24 22 16 25 17 3 | 6 16 8 7 17 4 10 8 8 13 3 | 11 18 17 13 18 14 13 12 14 14 11 4E | 11 18 11 12 20 7 13 17 20 24 6 | 31 32 29 32 27 30 30 29 35 28 28 5 | 8 18 9 9 17 4 22 16 9 22 5 | 12 26 14 15 25 13 24 18 16 16 13 6 | 7 17 7 8 14 5 13 11 10 15 4 | 12 18 16 16 18 13 12 16 15 22 12 7E | 7 20 10 11 18 7 21 8 10 14 5 | 15 26 23 19 30 19 25 19 21 14 18 8E | 19 25 8 22 23 12 16 14 36 22 8 | 30 36 29 27 30 28 31 28 46 25 27 X9E | 8 20 8 --- 19 11 19 13 17 21 6 | 16 27 21 --- 27 19 30 19 24 21 16 10 | 4 14 6 7 13 5 10 7 13 17 3 | 24 30 24 23 27 26 25 27 27 25 23 11 | 9 18 7 8 22 4 15 12 9 20 4 | 16 29 25 18 39 19 28 23 21 16 19 12 | 12 21 7 8 16 5 21 12 9 30 5 | 16 29 20 21 27 19 28 20 18 18 17 13 | 6 20 9 12 35 5 26 8 7 19 5 | 19 30 23 21 47 23 34 20 21 16 19 14 | 11 24 8 11 13 5 21 10 11 22 5 | 16 30 21 20 27 17 27 19 19 17 17 15 | 8 18 6 9 20 6 25 11 16 18 5 | 15 26 15 20 28 15 27 21 19 16 14 16 | 10 21 8 10 15 4 23 15 10 21 5 | 14 21 13 16 20 14 25 16 17 16 12 17 | 7 18 9 12 10 4 21 8 9 37 4 | 16 22 14 18 15 14 24 18 18 29 14 18 | 9 23 9 12 18 4 24 11 11 18 5 | 20 34 22 27 34 24 30 25 22 24 23 19 | 7 20 11 9 15 6 25 10 9 26 5 | 17 26 19 14 16 17 28 21 19 18 16 20 | 12 22 13 11 19 4 23 15 7 20 6 | 13 26 23 20 28 17 27 22 19 15 16 21E | 11 20 8 10 14 6 17 8 12 17 5 | 16 27 17 13 23 12 23 16 15 15 14 22 | 8 21 9 7 23 3 21 10 13 18 5 | 15 29 19 20 31 16 26 17 17 19 16 X23 | 8 25 8 11 22 7 --- 12 7 22 5 | 22 29 25 21 32 23 --- 20 22 18 19 24E | 21 26 16 22 23 9 18 17 41 43 9 | 64 65 60 66 65 59 61 61 73 63 60 26 | 8 13 4 8 12 6 11 9 9 25 3 | 9 19 14 16 20 13 19 12 16 26 11 27E | 13 20 9 22 17 8 17 14 30 19 7 | 48 51 49 47 49 47 53 50 52 48 47 28 | 6 27 10 12 15 5 23 8 6 32 5 | 17 30 24 22 26 19 28 19 19 14 18 29 | 10 17 8 11 17 7 23 11 11 --- 5 | 16 27 18 12 22 18 31 16 16 --- 15 30 | 9 12 6 7 13 4 11 8 11 17 3 | 20 23 21 23 23 19 21 22 24 20 19 31E | 5 12 6 10 26 10 21 9 14 20 4 | 13 18 16 15 23 19 21 13 21 18 14 32 | 7 21 6 12 17 3 16 8 9 23 4 | 15 20 13 16 17 14 18 18 15 15 12 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 20 9 12 19 6 19 11 15 23 |T 22 28 22 21 27 22 27 24 23 23 21 WRMS | 9 20 8 12 16 5 19 10 9 21 |NE 19 25 19 18 25 20 24 22 18 21 19 MEDI | 8 20 8 10 17 5 21 11 10 20 |MD 16 27 20 20 27 19 27 20 19 18 17 Table 3.1580.6 GPS week: 1580 Day: 6 MJD: 55310.000 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 | 19 --- --- --- --- 30 --- 26 --- 38 22 | 117 --- --- --- --- 123 --- 118 --- 78 115 2E | 16 28 9 11 19 4 21 16 16 18 6 | 34 47 39 35 43 35 44 34 44 37 37 3 | 9 18 8 11 21 6 10 14 11 13 4 | 13 23 18 23 20 16 15 17 15 18 17 4E | 33 23 14 11 20 9 19 19 20 24 8 | 55 59 55 56 56 53 58 54 58 51 55 5 | 6 22 7 11 20 7 23 14 8 18 5 | 13 29 15 16 23 16 28 17 16 15 14 6 | 8 16 7 10 20 5 10 13 12 16 4 | 18 21 22 23 21 17 17 20 18 26 19 7E | 9 29 9 13 26 6 23 13 11 15 6 | 12 31 18 17 29 11 24 16 17 14 14 8E | 21 21 9 23 27 7 21 19 36 25 9 | 25 30 21 32 30 24 29 31 48 29 25 X9E | 8 20 7 --- 22 9 19 21 15 26 6 | 24 32 24 --- 29 23 35 28 28 29 24 10 | 5 18 5 7 16 3 14 12 10 16 4 | 21 26 23 21 24 20 30 24 26 22 24 11 | 8 20 7 8 22 5 19 16 14 18 5 | 20 32 26 18 40 21 31 26 23 19 22 12 | 12 26 6 7 16 7 24 15 9 31 5 | 23 29 24 24 29 22 29 26 23 23 23 13 | 7 21 6 9 23 6 26 10 9 20 5 | 22 35 26 21 43 20 36 28 23 18 24 14 | 9 22 6 13 15 6 23 14 10 24 5 | 24 35 31 33 35 29 36 31 31 32 29 15 | 6 22 9 7 18 6 27 15 11 18 5 | 18 31 25 24 29 22 30 25 22 21 20 16 | 10 23 8 11 16 5 24 17 8 21 5 | 19 26 18 24 21 18 29 21 20 20 19 17 | 9 18 8 11 19 5 20 8 10 32 4 | 26 30 22 23 29 24 34 24 27 29 24 18 | 8 27 7 11 22 5 25 13 11 19 5 | 23 40 26 25 35 24 35 25 25 20 26 19 | 7 24 11 9 20 9 24 12 13 24 5 | 27 40 24 21 27 26 38 29 30 26 27 20 | 10 29 8 11 23 5 22 15 12 18 6 | 14 29 26 23 30 16 22 26 22 15 19 21E | 10 20 7 7 24 6 21 9 16 16 5 | 18 29 19 14 27 16 29 18 17 18 17 22 | 7 21 6 8 25 5 23 12 10 18 4 | 19 31 26 23 38 19 29 25 23 20 22 23 | 7 22 7 10 16 4 27 10 8 22 5 | 19 30 20 20 30 17 28 23 20 17 18 24E | 20 25 11 17 25 10 19 20 33 21 8 | 52 47 46 60 49 47 51 55 64 55 50 26 | 9 15 6 8 15 6 11 13 10 25 4 | 15 21 19 16 21 16 22 16 19 28 16 27E | 9 17 9 11 23 7 18 17 27 21 6 | 52 52 50 52 57 49 53 52 55 52 50 28 | 9 29 10 10 20 4 29 12 13 30 6 | 19 33 26 24 30 19 31 24 24 20 19 29 | 7 17 7 8 22 6 21 13 14 --- 4 | 16 29 20 16 21 17 33 21 21 --- 19 30 | 7 17 5 7 11 4 16 6 14 16 4 | 31 26 32 35 33 31 25 31 35 30 31 31E | 6 16 9 7 32 5 21 13 10 16 4 | 25 30 27 26 36 25 27 28 28 28 26 32 | 8 20 4 19 13 6 17 11 12 27 5 | 16 18 18 24 22 16 17 22 21 18 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 22 8 11 21 6 21 14 15 21 |T 26 32 26 26 31 26 31 30 28 27 27 WRMS | 8 22 7 11 19 6 20 13 9 20 |NE 24 29 23 22 28 24 28 28 23 24 25 MEDI | 9 21 7 10 20 6 21 13 11 20 |MD 21 30 24 23 29 21 29 25 23 22 23 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1580 GPS week: 1580 MJD: 55304.0-55310.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2955 |U 7 7 19 |U 48 48 204 |U 9 8 19 | emr | emr 2854 | 10 10 31 |U 34 47 167 | 11 9 25 | esa | esa 2852 | 7 7 24 |U 41 48 212 | 10 9 20 | gfz | gfz 2763 |U 8 7 22 |U 47 49 197 |U 9 7 19 | grg | grg 2880 | 10 8 27 |U 13 15 69 | 9 8 25 | igr | igr 2876 | 8 7 26 | 16 50 206 | 9 8 19 | igs | igs 2880 | 7 7 22 | 48 49 199 | 10 9 20 | jpl | jpl 2786 |U 9 8 27 | 45 56 203 |U 10 8 24 | mit | mit 2976 |U 8 7 29 |U 44 43 222 |U 9 8 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 5.1580.0 GPS week: 1580 Day: 0 MJD: 55304.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2958 | 8 6 18 | 13 13 35 | 9 9 21 | emr | emr 2860 | 10 9 31 | 15 12 36 | 10 7 20 | esa | esa 2880 | 7 6 24 | 13 11 34 | 10 9 20 | gfz | gfz 2768 | 7 7 18 | 14 11 36 | 8 8 20 | grg | grg 2880 | 9 8 27 | 12 13 36 | 9 7 24 | igr | igr 2896 | 7 6 24 | 12 11 34 | 9 8 17 | igs | igs 2872 | 8 6 23 | 13 13 39 | 10 10 23 | jpl | jpl 2859 | 7 7 27 | 14 10 35 | 9 8 20 | mit | mit 2976 | 8 7 26 | 13 10 39 | 9 9 21 | Table 5.1580.1 GPS week: 1580 Day: 1 MJD: 55305.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2962 | 6 4 21 | 6 12 24 | 11 11 25 | emr | emr 2860 | 8 6 27 | 8 13 25 | 12 8 20 | esa | esa 2880 | 6 5 31 | 5 11 19 | 13 12 23 | gfz | gfz 2768 | 6 5 22 | 5 13 19 | 12 11 23 | grg | grg 2880 | 13 8 35 | ---- ---- ---- | ---- ---- ---- | igr | igr 2878 | 6 4 27 | 5 12 20 | 12 11 21 | igs | igs 2877 | 5 4 25 | 5 11 19 | 13 12 23 | jpl | jpl 2858 | 7 7 28 | 6 13 21 | 13 10 24 | mit | mit 2976 | 7 6 38 | 5 9 19 | 11 9 24 | Table 5.1580.2 GPS week: 1580 Day: 2 MJD: 55306.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2952 | 8 9 17 | 7 9 26 | 8 6 19 | emr | emr 2851 | 14 9 39 | 7 8 32 | 11 7 30 | esa | esa 2880 | 8 8 22 | 5 8 24 | 10 6 22 | gfz | gfz 2760 | 12 7 23 | 6 8 24 | 7 5 23 | grg | grg 2880 | 15 9 31 | 31 24 193 | 10 8 30 | igr | igr 2879 | 8 9 25 | 5 7 23 | 10 6 22 | igs | igs 2897 | 9 8 18 | 6 8 25 | 10 7 23 | jpl | jpl 2762 | 15 9 41 | 7 11 29 | 8 4 23 | mit | mit 2976 | 9 8 21 | 6 9 28 | 10 7 23 | Table 5.1580.3 GPS week: 1580 Day: 3 MJD: 55307.0 CENT| CLK EPO | TOW2 | WILL | ----+----------+-------------------+-------------------+ cod | cod 2961 | 6 7 31 | 10 9 15 | emr | emr 2849 | 5 8 30 | 11 9 23 | esa | esa 2784 | 5 8 28 | 10 7 15 | gfz | gfz 2757 | 5 9 28 | 10 8 15 | grg | grg 2880 | 7 10 41 | 9 6 21 | igr | igr 2895 | 5 9 27 | 9 8 15 | igs | igs 2911 | 5 8 27 | 10 8 16 | jpl | jpl 2668 | 6 8 24 | 7 6 20 | mit | mit 2976 | 6 7 22 | 9 7 17 | Table 5.1580.4 GPS week: 1580 Day: 4 MJD: 55308.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2933 | 6 6 17 | 291 270 1249 | 8 8 19 | emr | emr 2844 | 8 8 21 | 187 259 978 | 12 8 26 | esa | esa 2784 | 7 4 22 | 244 270 1315 | 8 10 23 | gfz | gfz 2751 | 7 7 25 | 289 272 1205 | 8 7 21 | grg | grg 2880 | 7 5 17 | ---- ---- ---- | 9 11 33 | igr | igr 2838 | 8 6 22 | 74 284 1276 | 9 7 21 | igs | igs 2856 | 8 5 19 | 292 278 1218 | 9 6 20 | jpl | jpl 2751 | 8 6 19 | 267 321 1235 | 9 9 21 | mit | mit 2976 | 7 5 34 | 265 243 1380 | 9 7 26 | Table 5.1580.5 GPS week: 1580 Day: 5 MJD: 55309.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2955 | 7 10 21 | 6 12 33 | 8 9 15 | emr | emr 2860 | 8 11 34 | 9 16 30 | 14 12 29 | esa | esa 2880 | 7 9 22 | 7 13 34 | 9 7 17 | gfz | gfz 2768 | 6 7 22 | 7 14 34 | 8 6 16 | grg | grg 2880 | 8 11 28 | 8 15 38 | 10 7 19 | igr | igr 2878 | 8 11 32 | 7 15 33 | 8 8 17 | igs | igs 2874 | 7 9 24 | 7 14 33 | 9 8 16 | jpl | jpl 2760 | 7 12 23 | 10 15 43 | 12 10 33 | mit | mit 2976 | 8 9 29 | 8 14 35 | 9 8 17 | Table 5.1580.6 GPS week: 1580 Day: 6 MJD: 55310.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2965 | 7 7 20 | 7 10 28 | 8 7 19 | emr | emr 2858 | 10 14 35 | 8 15 35 | 11 12 28 | esa | esa 2880 | 8 7 22 | 6 12 29 | 10 9 20 | gfz | gfz 2769 | 8 8 22 | 6 17 30 | 8 7 19 | grg | grg 2880 | 8 9 24 | 7 11 39 | 8 9 24 | igr | igr 2870 | 8 9 26 | 7 15 31 | 8 8 20 | igs | igs 2873 | 8 8 26 | 6 13 29 | 9 9 21 | jpl | jpl 2845 | 8 10 28 | 8 16 36 | 10 12 28 | mit | mit 2976 | 8 7 25 | 7 11 29 | 8 9 23 | 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 6.1580 GPS week: 1580 MJD: 55304.500-55310.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 23 -36 107 122 5 | 6 16 | 22 25 94 93 9 | 2 emr uuuxu | 12 54 -104 393 3 | 59 61 | 13 23 82 80 5 | 3 esa uuuuu | -26 -41 4 -95 2 | 17 22 | 15 17 65 76 3 | 3 gfz uuuuu | -1 76 17 80 -5 | 26 29 | 18 18 63 77 4 | 1 grg xxxxx | 65 -61 73 217 0 | 9 13 | 49 92 293 90 23 | 3 igr xxxxx | 7 32 -30 68 -2 | -2 12 | 22 17 56 59 11 | 1 irf xxxxx | -4 -16 13 -10 1 | 4 17 | 10 8 58 50 4 | 4 jpl uuuuu | 22 -23 77 139 7 | 25 30 | 47 21 75 65 11 | 3 mit uuuuu | -23 -17 87 -118 4 | 13 22 | 14 8 61 65 5 | 5 ngs uuuuu | 47 -21 -116 96 -4 | 6 16 | 33 60 151 87 5 | 1 sio xxxxx | -335 163 -456 133 15 | 48 52 | 14 14 82 82 5 | 7 Table 7.1580.0 GPS week: 1580 Day: 0 MJD: 55304.500 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 | 52 -39 105 147 -3 | 5 17 emr uuuxu | 19 50 -84 398 -4 | 56 58 esa uuuuu | -48 -26 28 -248 3 | 13 19 gfz uuuuu | -14 86 -11 151 -6 | 26 30 grg xxxxx | -23 -192 508 239 -18 | 14 18 igr xxxxx | 17 47 22 125 -17 | 0 13 irf xxxxx | -3 -5 31 -32 9 | -2 17 jpl uuuuu | 32 -22 149 125 3 | 22 28 mit uuuuu | -24 -1 131 -138 14 | 6 19 ngs uuuuu | 77 -77 -198 229 -11 | 7 16 sio xxxxx | -324 169 -447 67 23 | 39 42 Table 7.1580.1 GPS week: 1580 Day: 1 MJD: 55305.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 24 -54 31 159 -7 | 5 17 emr uuuxu | 18 36 1 375 2 | 56 58 esa uuuuu | -15 -18 -128 -128 8 | 14 20 gfz uuuuu | 14 84 -16 67 -9 | 26 29 grg xxxxx | 109 -99 46 258 -22 | 11 15 igr xxxxx | 32 30 -29 99 -16 | -2 12 irf xxxxx | 6 -11 -85 31 1 | 0 18 jpl uuuuu | -6 -4 125 240 3 | 21 26 mit uuuuu | -17 -17 -8 -61 6 | 8 21 ngs uuuuu | 14 -67 131 30 -8 | 6 16 sio xxxxx | -320 161 -578 200 17 | 41 45 Table 7.1580.2 GPS week: 1580 Day: 2 MJD: 55306.500 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 | -1 8 119 207 9 | 6 17 emr uuuxu | 6 46 -40 279 8 | 58 61 esa uuuuu | -31 -50 -15 -49 -1 | 18 23 gfz uuuuu | -17 76 -48 121 -1 | 27 30 grg xxxxx | 120 -18 -160 281 2 | 10 15 igr xxxxx | 4 39 -110 -16 -2 | -1 12 irf xxxxx | -17 -23 -29 6 1 | 4 18 jpl uuuuu | 121 -12 77 72 5 | 23 29 mit uuuuu | -34 -24 30 -97 6 | 12 22 ngs uuuuu | 35 4 22 25 -5 | 7 16 sio xxxxx | -345 142 -556 182 18 | 46 50 Table 7.1580.3 GPS week: 1580 Day: 3 MJD: 55307.500 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 | 52 -56 110 195 -1 | 6 17 emr uuuxu | -5 48 -181 399 6 | 58 61 esa uuuuu | 0 -37 46 -105 -1 | 18 23 gfz uuuuu | 21 57 -13 185 -9 | 26 30 grg xxxxx | 92 -151 213 233 -13 | 8 13 igr xxxxx | 23 22 1 106 -4 | -2 13 irf xxxxx | -15 -22 -8 -3 -3 | 4 17 jpl uuuuu | -13 -61 75 48 23 | 23 29 mit uuuuu | -43 -25 75 -111 -1 | 14 22 ngs uuuuu | 41 33 -67 62 -4 | 5 17 sio xxxxx | -358 163 -444 92 13 | 48 52 Table 7.1580.4 GPS week: 1580 Day: 4 MJD: 55308.500 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 | 4 -22 295 33 5 | 4 16 emr uuuxu | 7 106 -235 324 4 | 58 60 esa uuuuu | -21 -39 -4 -62 1 | 17 23 gfz uuuuu | 19 107 142 61 -9 | 24 27 grg xxxxx | 70 -13 202 171 -4 | 6 12 igr xxxxx | 17 46 -10 -5 3 | -3 13 irf xxxxx | 7 -8 85 -48 1 | 4 17 jpl uuuuu | 6 -22 25 171 16 | 24 30 mit uuuuu | -7 -13 136 -143 3 | 14 23 ngs uuuuu | 10 -105 -200 89 -4 | 4 16 sio xxxxx | -332 188 -360 50 15 | 50 54 Table 7.1580.5 GPS week: 1580 Day: 5 MJD: 55309.500 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 -25 97 161 20 | 7 15 emr uuuxu | 4 45 -71 521 10 | 61 63 esa uuuuu | -33 -67 41 -44 2 | 19 23 gfz uuuuu | -5 65 51 -24 2 | 24 28 grg xxxxx | 56 -26 112 35 7 | 8 12 igr xxxxx | -26 0 22 52 7 | -2 12 irf xxxxx | 1 -22 44 61 2 | 7 15 jpl uuuuu | 23 -2 150 171 8 | 28 33 mit uuuuu | -7 -23 87 -39 2 | 18 22 ngs uuuuu | 49 32 -300 29 -5 | 5 16 sio xxxxx | -324 157 -410 266 14 | 55 58 Table 7.1580.6 GPS week: 1580 Day: 6 MJD: 55310.500 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 -66 -4 -46 11 | 9 15 emr uuuxu | 33 48 -117 454 -3 | 63 64 esa uuuuu | -33 -52 63 -32 -1 | 20 24 gfz uuuuu | -22 59 16 -1 -5 | 24 28 grg xxxxx | 33 75 -412 302 47 | 6 10 igr xxxxx | -20 43 -106 118 13 | -1 11 irf xxxxx | -7 -20 54 -88 -4 | 9 14 jpl uuuuu | -8 -40 -58 144 -12 | 30 33 mit uuuuu | -27 -17 162 -236 -3 | 20 22 ngs uuuuu | 103 34 -201 210 6 | 5 16 sio xxxxx | -340 161 -393 77 8 | 59 60