Date: Thu, 29 Apr 2010 11:26:41 +0000 From: Jim Ray Subject: [IGSREPORT-18526] Wk 1579 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4bd96cf1.4TML8exSz1v/wNGm%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 29 Apr 04:27:00 PDT 2010 Message Number 18526 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1579 (Apr 11, 2010 - Apr 17, 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: igs1579[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1579[0-6].clk IGS GPS satellite and station clocks in clock RINEX format. igs1579[0-6].cls IGS GPS clock combination summary report. igs15797.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15797.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 0 | COD | 4 4 27 0 | EMR | 21 24 21 24 WTZR 0 | ESA | 4 4 27 DGAR 0 | GFZ | 13 21 KARR MATE NTUS PERT SUTH YAR2 0 | GRG | DGAR WTZR 0 | JPL | 4 24 0 | MIT | 9 24 9 24 PERT SHAO 0 | NGS | 1 1 | ALL | 1 1 | COD | BRAZ DGAR 1 | EMR | 4 8 24 27 4 8 24 27 HARB WTZR HARB WTZR 1 | ESA | DGAR 1 | GFZ | 8 BAKE GUAT METS MIZU SCUB SUTH UNSA 1 | GRG | DGAR ONSA 1 | JPL | 4 24 27 HARB 1 | MIT | 4 24 27 4 24 27 IRKJ 1 | NGS | 1 2 | ALL | 1 1 2 | COD | CAS1 DGAR KOUR 2 | EMR | 4 9 24 27 4 9 24 27 WTZR MATE ONSA WTZR 2 | ESA | CAS1 DGAR UNSA 2 | GFZ | HARB IRKT KOUR MDVJ ONSA SUTH 2 | GRG | DGAR WTZR 2 | JPL | 4 9 24 27 2 | MIT | 4 10 11 23 24 27 4 11 21 23 24 27 28 WTZR CAS1 HARB 2 | MIT | NYA1 TRO1 3 | ALL | 1 3 | COD | DGAR 3 | EMR | 4 4 WTZR 3 | ESA | DGAR 3 | GFZ | SUTH 3 | GRG | DGAR ONSA 3 | JPL | 4 3 | MIT | 4 4 3 | NGS | 1 4 | EMR | 4 4 WTZR 4 | ESA | METS YELL DGAR METS YELL 4 | GFZ | 21 CRO1 RIOP SUTH UNSA 4 | GRG | DGAR ONSA 4 | JPL | 4 8 AREQ 4 | MIT | 4 21 4 21 YELL YELL 4 | NGS | 1 5 | COD | ARTU DGAR PDEL 5 | EMR | 4 4 WTZR 5 | ESA | DGAR 5 | GFZ | 27 SUTH UNSA 5 | GRG | DGAR SPT0 ULAB 5 | JPL | 4 9 27 5 | MIT | 4 8 10 24 26 27 4 8 24 26 27 HARB HARB PDEL 5 | NGS | 1 6 | ALL | 1 1 6 | EMR | 4 4 WTZR WTZR 6 | ESA | DGAR 6 | GFZ | SFER SUTH 6 | GRG | DGAR SPT0 ULAB 6 | JPL | 4 9 24 27 6 | MIT | 4 8 24 4 8 24 DAEJ MAW1 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 | | | | 4 | | | | 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 | .4 .9 .6 -15 -8 -6 .0 EMR | 3.5 -2.2 2.6 13 7 -6 .20 ESA | 2.7 2.0 -1.8 51 14 -54 .17 GFZ | -1.2 .9 .3 -12 42 -88 .29 GRG | 1.0 8.9 6.5 16 41 44 .73 JPL | 1.4 1.2 .6 -1 -26 -3 .50 MIT | 8.3 -7.3 6.2 -8 24 -34 -.01 NGS | 2.2 -7.9 -3.8 -127 -61 38 .20 SIO | 6.7 1.7 -7.7 -27 251 -590 .31 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 1.1579.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1579.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 2.1579.[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 3.1579.[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 5.1579.0-6). 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 1579 summary. (Apr 11, 2010 - Apr 17, 2010) Table 1.1579.a GPS week: 1579 MJD: 55297.000-55303.000 Mean and standard deviations of transformation parameters to the combined IGS orbit. WRMS - orbit RMS weighted by the SP3 header accuracy codes. STA - Mean number of stations in the daily solutions. CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 242| 0 0 0 1 18 11 -.24 10 8 | -406 -262 21 72 | 0 0 0 13 15 15 .01 | 381 484 emr 87| 0 -1 1 -47 15 11 .43 20 20 | -106 -436 21 93 | 2 1 1 17 22 20 .02 | 1857 1045 esa 131| 1 1 -1 -133 -43 -38 .24 9 9 | -113 -708 16 91 | 0 0 1 15 14 18 .03 | 1075 1497 gfz 197| 0 0 2 -16 -101 4 -.09 12 12 | 105 101 22 103 | 0 0 2 38 56 12 .03 | 388 500 grg 107| -1 1 2 -76 -49 44 .87 25 23 | -119 131 67 213 | 2 0 2 67 31 7 .04 | 261 466 igr n/a| 0 0 0 -22 13 6 .01 6 5 | 5362 -1297 19 67 | 0 0 0 18 22 17 .03 | 3495 1135 jpl 122| -1 1 -1 -37 51 59 .47 21 21 | 1725 -418 20 120 | 1 0 2 18 15 48 .03 | 1569 1130 mit 271| 1 -2 0 -8 -32 0 -.27 14 12 | -14896 731 27 170 | 0 0 1 21 19 8 .02 | 1830 1363 ngs 214| 0 -1 0 246 126 -8 -.20 15 8 | 14366 -1878 1991 3620 | 1 1 1 26 29 8 .02 | 2242 2808 sio 261| 0 3 6 49 -503 -576 -.09 22 22 | --- --- --- --- | 1 0 1 19 24 10 .04 | --- --- Table 1.1579.b GPS week : 1579 MJD: 55297.000-55303.000 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 | 18 16 12 21 14 14 11 | 2 | 5 5 5 6 6 6 6 | 3 | 4 4 4 4 4 4 4 | 4 | 7 7 6 6 7 6 6 | 5 | 5 5 5 5 6 5 5 | 6 | 4 4 4 4 4 4 4 | 7 | 5 5 5 5 6 5 5 | 8 | 6 6 7 7 7 8 8 | 9 | 18 16 8 7 7 7 7 | 10 | 4 4 3 3 4 4 4 | 11 | 5 5 5 5 5 4 5 | 12 | 5 5 5 5 5 6 5 | 13 | 5 6 6 6 6 5 5 | 14 | 5 5 6 7 5 6 6 | 15 | 6 5 5 5 6 5 6 | 16 | 5 5 5 5 6 5 6 | 17 | 5 5 5 5 5 5 5 | 18 | 6 6 6 6 6 6 6 | 19 | 6 5 6 6 6 5 5 | 20 | 6 6 6 6 6 6 6 | 21 | 6 5 6 5 5 5 5 | 22 | 5 5 5 5 5 5 5 | 23 | 5 6 6 6 6 5 6 | 24 | 8 9 12 12 14 15 12 | 26 | 4 3 4 4 4 4 4 | 27 | 9 6 6 7 6 6 7 | 28 | 5 5 5 6 5 5 6 | 29 | 5 5 5 6 6 6 5 | 30 | 4 4 4 4 4 4 4 | 31 | 5 5 5 6 6 6 5 | 32 | 4 5 5 5 5 5 6 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1579.0 GPS week: 1579 Day: 0 MJD: 55297.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 242| 0 0 0 -2 5 8 -.23 8 8 | -279 -476 20 82 | 11 6 | emr 87| -6 0 0 -68 44 37 .45 22 21 | 2668 -99 12 82 | -5 -46 | esa 131| 2 1 0 -152 -38 -38 .22 8 8 | -208 -2244 11 91 | 60 31 | gfz 197| 1 0 0 33 -134 1 -.13 12 12 | 329 -373 21 87 | -42 49 | grg 107| 1 0 5 -149 -74 52 .91 26 25 | -128 253 64 206 | 151 20 | igr n/a| 0 0 0 -27 13 20 .05 8 7 | 10693 -977 22 68 | -10 12 | jpl 122| -2 2 -3 -37 66 -2 .49 21 20 | 3952 199 17 114 | 11 4 | mit 271| 1 -2 0 1 -29 16 -.26 14 13 | -13492 1375 25 174 | -14 15 | ngs 214| -1 -2 1 233 133 -4 -.20 13 8 | 14430 -4994 1907 3519 | 27 28 | sio 261| 0 2 6 50 -475 -562 -.02 25 24 | --- --- --- --- | -120 263 | Table 2.1579.1 GPS week: 1579 Day: 1 MJD: 55298.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 242| 0 0 0 5 9 11 -.24 8 7 | -1173 778 20 80 | 33 31 | emr 87| 0 0 5 -63 17 -12 .44 19 19 | 2076 -1328 16 98 | -11 -58 | esa 131| 2 1 0 -127 -29 -34 .28 10 9 | 957 -2496 11 72 | 48 8 | gfz 197| 0 0 -1 -25 -145 9 -.05 12 12 | -707 1111 22 100 | -17 21 | grg 107| 1 0 2 -88 -5 35 .90 24 22 | -665 941 57 201 | 28 -161 | igr n/a| 0 0 0 -45 14 27 .04 6 5 | 9226 -2512 18 62 | -21 -28 | jpl 122| -1 0 2 -62 35 55 .47 21 21 | 3687 -1382 19 116 | 27 -30 | mit 271| 0 -3 0 12 -56 0 -.27 13 12 | -13801 2184 23 158 | -10 30 | ngs 214| -1 0 -2 213 150 -6 -.17 12 7 | 12276 659 1852 3845 | 46 20 | sio 261| 0 2 7 73 -501 -572 -.06 23 23 | --- --- --- --- | -128 262 | Table 2.1579.2 GPS week: 1579 Day: 2 MJD: 55299.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 242| 0 0 0 19 45 28 -.24 8 7 | -371 -522 21 64 | 49 8 | emr 87| 1 -2 2 -41 12 -6 .44 20 20 | 169 -319 19 93 | -25 -8 | esa 131| 1 1 -1 -141 -46 -27 .28 10 9 | 1429 201 12 80 | 68 86 | gfz 197| 0 0 1 -59 -169 5 -.08 11 11 | 413 -80 22 97 | -32 52 | grg 107| -2 0 6 -20 -28 55 .90 26 22 | -120 193 83 240 | -46 -95 | igr n/a| 0 0 -1 -26 47 0 .02 6 5 | 6284 -1425 18 69 | -1 24 | jpl 122| 0 1 -2 -55 46 47 .50 21 21 | 1922 -323 17 118 | 40 7 | mit 271| 1 -2 -1 23 -14 -3 -.26 14 12 | -11864 -2069 29 191 | -16 18 | ngs 214| -3 0 0 258 149 -20 -.20 15 8 | 10472 2967 1854 3817 | 28 14 | sio 261| 1 3 4 67 -478 -570 -.08 22 23 | --- --- --- --- | -110 256 | Table 2.1579.3 GPS week: 1579 Day: 3 MJD: 55300.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 242| 0 1 -1 10 7 5 -.27 10 9 | -113 -420 25 86 | 55 19 | emr 87| 0 -3 -1 -33 -12 38 .44 19 19 | -1018 -432 30 101 | -60 -8 | esa 131| 1 1 0 -139 -29 -65 .23 9 9 | -1830 1604 22 102 | 27 65 | gfz 197| 0 0 4 -68 -44 22 -.08 12 12 | 319 -17 23 97 | -61 46 | grg 107| 0 1 2 -28 -58 44 .82 23 22 | -130 228 57 197 | -47 -65 | igr n/a| 0 0 0 -24 5 20 -.00 5 5 | 4206 -1116 19 71 | -22 -5 | jpl 122| -2 1 -2 -8 40 62 .48 22 22 | 846 -67 25 127 | -21 -34 | mit 271| 1 0 -1 -31 -27 -5 -.32 15 13 | -16193 1024 35 193 | 0 24 | ngs 214| 1 0 -1 293 89 -1 -.18 16 9 | 16315 -2742 2210 3816 | 48 9 | sio 261| -1 2 4 47 -514 -590 -.10 21 20 | --- --- --- --- | -123 274 | Table 2.1579.4 GPS week: 1579 Day: 4 MJD: 55301.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 242| 0 0 0 1 16 30 -.25 11 10 | -25 -641 22 66 | 21 29 | emr 87| 0 0 2 -19 0 7 .44 19 19 | -2382 1222 29 93 | -66 -31 | esa 131| 1 1 -1 -140 -70 -29 .24 10 10 | -4 -1700 23 95 | 2 55 | gfz 197| 0 0 3 7 -42 -18 -.13 13 13 | -31 301 27 151 | -92 33 | grg 107| -1 2 0 -94 -71 44 .84 25 24 | 53 -155 76 206 | 32 -30 | igr n/a| 0 0 0 -26 -19 -18 -.01 6 5 | 2405 529 21 63 | -38 -3 | jpl 122| -2 0 -1 -43 53 34 .46 21 21 | -11 1267 26 134 | 9 -31 | mit 271| 0 -1 0 -29 -7 3 -.25 12 11 | -16484 1310 29 154 | -1 12 | ngs 214| -1 0 0 252 86 -11 -.23 16 10 | 15394 -1833 2063 3268 | 87 57 | sio 261| -1 4 7 33 -500 -588 -.14 21 21 | --- --- --- --- | -113 279 | Table 2.1579.5 GPS week: 1579 Day: 5 MJD: 55302.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 242| -1 0 -1 -25 35 -17 -.23 11 9 | -311 -423 24 68 | 47 -28 | emr 87| 0 -1 1 -55 45 16 .41 19 19 | -932 -18 22 99 | -38 -32 | esa 131| 1 2 -1 -128 -36 -59 .24 9 9 | -699 103 20 101 | 16 31 | gfz 197| 0 0 3 17 -135 6 -.06 10 10 | 303 84 21 102 | -71 32 | grg 107| -3 1 2 -165 -18 42 .84 26 25 | 33 57 65 234 | 132 -97 | igr n/a| 0 0 -1 -19 32 9 -.03 5 5 | 3088 -721 21 74 | -28 -4 | jpl 122| 1 0 0 -33 78 157 .45 20 20 | 1377 -363 19 118 | 38 15 | mit 271| 0 -1 0 -9 -59 0 -.28 14 12 | -16099 231 21 155 | -6 23 | ngs 214| 1 -1 0 224 157 1 -.21 16 6 | 16691 -2891 2016 3710 | 82 -91 | sio 261| -2 4 6 52 -548 -569 -.14 20 22 | --- --- --- --- | -99 291 | Table 2.1579.6 GPS week: 1579 Day: 6 MJD: 55303.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 242| 0 0 1 4 7 11 -.24 10 9 | -575 -132 20 63 | 24 29 | emr 87| 1 0 2 -51 -2 -1 .38 20 20 | -1325 -2083 25 88 | -22 -18 | esa 131| 1 3 -2 -105 -50 -12 .22 9 8 | -442 -426 19 98 | 39 67 | gfz 197| -1 0 2 -21 -38 2 -.10 12 12 | 109 -315 21 91 | -35 51 | grg 107| -4 2 2 11 -89 38 .90 27 22 | 122 -598 68 207 | -105 22 | igr n/a| 0 0 -1 14 -1 -13 -.02 6 5 | 1637 -2859 19 64 | -16 -17 | jpl 122| 0 2 -1 -20 41 62 .42 22 21 | 305 -2258 19 118 | 2 -16 | mit 271| 1 -3 0 -24 -31 -7 -.25 13 12 | -16341 1067 29 169 | -18 14 | ngs 214| -1 -3 0 249 119 -18 -.23 15 9 | 14984 -4313 2036 3366 | 18 -23 | sio 261| -2 4 7 18 -509 -579 -.10 22 23 | --- --- --- --- | -90 284 | 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 3.1579.0 GPS week: 1579 Day: 0 MJD: 55297.000 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 --- --- --- --- 28 --- 19 35 --- 18 | 98 --- --- --- --- 105 --- 98 109 --- 102 2E | 9 19 6 10 --- 6 29 10 6 22 5 | 28 35 29 29 --- 26 34 24 25 29 27 3 | 8 16 6 8 15 7 15 8 12 17 4 | 20 26 25 23 28 22 22 23 24 26 21 4E | 12 15 12 16 21 6 19 23 17 22 6 | 21 29 24 21 32 23 29 25 25 22 22 5 | 8 19 7 15 29 8 23 14 11 22 5 | 24 32 22 29 37 22 31 25 28 26 23 6 | 7 16 6 8 16 7 16 9 7 17 3 | 20 23 26 25 28 22 19 24 24 26 22 7E | 6 20 8 12 18 6 20 9 11 14 4 | 15 25 14 14 24 15 21 15 27 16 15 8E | 12 27 7 13 25 8 19 19 15 17 6 | 21 34 19 24 24 20 23 21 28 19 20 X9E | 25 --- 19 --- 28 21 --- 34 --- --- 18 | 15 --- 45 --- 33 37 --- 38 --- --- 29 10 | 7 14 4 15 17 6 11 15 8 22 4 | 27 28 33 29 38 30 33 27 35 31 28 11E | 6 20 8 12 19 8 18 16 10 26 5 | 19 31 25 22 38 24 28 25 27 18 22 12 | 9 19 8 8 22 9 18 11 10 32 4 | 13 26 17 17 29 14 22 18 14 21 14 13 | 6 20 7 11 41 9 24 9 7 19 4 | 13 26 17 15 45 13 28 17 17 13 13 14 | 8 25 9 10 25 8 23 12 10 22 5 | 17 31 22 20 40 20 29 23 21 16 19 15 | 6 18 9 11 34 11 25 19 14 36 5 | 13 26 22 19 36 16 27 24 23 28 16 16 | 11 21 6 9 24 6 23 14 10 28 5 | 13 27 19 18 31 15 28 19 14 22 15 17 | 8 21 11 12 28 8 22 11 12 36 5 | 21 33 18 22 37 23 36 23 22 33 21 18 | 8 25 8 13 31 6 25 15 9 29 5 | 20 38 27 26 41 24 35 28 25 30 23 19 | 9 29 9 10 26 10 27 10 16 26 6 | 29 41 25 23 36 28 40 28 29 30 27 20 | 7 23 11 12 34 9 24 17 8 37 5 | 20 28 24 27 33 20 27 25 24 23 21 21E | 7 23 9 11 25 5 25 16 12 23 5 | 39 41 33 38 37 35 39 38 34 39 35 22 | 6 23 8 8 31 8 26 16 9 31 5 | 21 35 25 23 43 23 35 28 24 32 22 23 | 7 23 7 13 38 9 26 12 9 24 5 | 16 27 15 18 41 14 27 18 19 13 13 24E | 15 18 14 16 19 15 19 24 33 26 8 | 135 130 135 135 126 137 127 134 144 131 134 26 | 6 15 6 7 25 6 12 15 8 19 3 | 10 18 14 8 20 10 15 18 15 11 10 27E | 9 54 10 18 21 12 17 13 23 17 8 | 13 48 16 18 27 14 23 14 25 14 14 28 | 5 20 10 11 28 8 21 16 10 32 5 | 18 32 28 25 35 21 32 24 16 23 21 29 | 8 19 8 10 22 6 23 10 11 --- 5 | 29 38 26 27 36 30 40 32 32 --- 28 30 | 7 14 6 8 16 6 12 12 9 21 3 | 27 26 27 26 30 24 23 28 26 23 26 31E | 6 25 6 9 24 8 23 10 10 24 5 | 29 47 33 28 46 33 43 33 27 33 31 32 | 7 18 5 11 21 6 17 10 8 24 4 | 19 20 21 25 26 18 18 24 22 15 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 22 8 12 26 8 21 14 13 25 |T 26 34 27 26 37 28 32 30 30 27 27 WRMS | 8 21 8 12 25 7 20 13 8 24 |NE 23 29 22 22 34 24 28 27 26 23 24 MEDI | 8 20 8 11 25 8 22 14 10 23 |MD 20 31 24 23 36 22 28 24 25 23 22 Table 3.1579.1 GPS week: 1579 Day: 1 MJD: 55298.000 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 --- --- --- --- 29 --- 18 29 --- 15 | 95 --- --- --- --- 104 --- 100 105 --- 101 2E | 7 18 7 9 18 4 24 12 8 17 4 | 25 28 26 24 28 21 27 25 25 23 22 3 | 6 10 8 10 13 4 13 8 10 18 3 | 15 23 22 19 27 16 22 16 27 22 17 4E | 10 23 14 19 17 7 18 15 19 19 6 | 24 33 25 27 35 22 27 25 29 19 21 5 | 6 19 8 14 26 5 22 14 11 22 5 | 30 36 30 36 42 28 35 32 31 30 29 6 | 6 12 7 10 13 4 14 9 9 16 3 | 15 22 21 20 28 15 20 17 25 21 16 7E | 7 18 7 13 18 4 19 7 7 13 4 | 16 23 17 18 25 14 20 14 22 13 15 8E | 14 24 12 12 14 6 15 19 10 19 6 | 21 31 21 24 22 21 22 20 28 17 20 X9E | 21 --- 20 --- 24 15 --- 26 --- --- 15 | 14 --- 37 --- 37 24 --- 34 --- --- 23 10 | 7 13 4 10 20 3 13 11 7 21 3 | 19 23 25 26 30 24 26 24 27 26 22 11E | 7 18 8 8 38 6 16 13 10 22 4 | 14 26 20 17 37 17 22 21 22 13 16 12 | 7 20 9 12 21 5 19 13 9 31 5 | 13 27 17 19 29 15 23 17 17 16 13 13 | 8 20 11 15 37 5 26 12 8 20 5 | 15 25 18 20 41 15 26 16 20 10 14 14 | 7 16 10 11 28 5 23 15 12 18 5 | 15 24 20 20 38 16 26 17 20 14 15 15 | 7 21 8 14 30 6 24 15 10 31 5 | 16 28 19 22 36 18 26 21 22 25 16 16 | 7 21 8 9 22 5 25 15 8 28 5 | 12 24 17 12 33 10 27 13 19 15 12 17 | 7 17 11 13 25 4 23 8 12 34 5 | 16 25 15 19 31 15 28 14 18 29 14 18 | 9 22 11 15 28 5 26 14 10 27 5 | 16 30 20 26 34 17 28 18 22 24 17 19 | 7 22 10 11 23 6 25 10 9 25 5 | 23 31 21 20 30 19 31 24 30 25 21 20 | 9 24 12 11 31 4 24 16 12 28 6 | 19 29 21 25 32 18 26 23 28 19 19 21E | 7 19 9 11 19 4 27 12 9 22 5 | 32 32 27 30 37 28 34 31 32 34 28 22 | 5 18 11 8 32 6 22 14 11 29 5 | 17 29 23 19 38 16 27 20 22 23 17 23 | 8 22 9 12 31 5 27 14 6 24 5 | 19 25 19 22 40 16 27 19 23 13 17 24E | 10 18 23 15 21 15 21 21 37 30 9 | 88 81 87 81 77 84 79 83 91 76 83 26 | 4 13 5 7 18 4 12 11 5 18 3 | 11 16 13 14 21 9 17 15 18 12 11 27E | 7 19 11 14 32 6 15 11 19 9 5 | 11 26 15 14 35 12 22 14 29 10 11 28 | 5 20 10 10 24 5 24 13 8 30 5 | 15 28 18 14 32 14 28 19 21 19 15 29 | 6 19 8 11 22 4 22 16 10 --- 5 | 20 26 16 16 26 17 26 22 26 --- 17 30 | 6 12 7 9 17 5 14 13 7 21 3 | 20 18 20 18 23 17 16 21 24 16 18 31E | 6 22 12 10 19 5 17 11 8 17 4 | 36 48 42 38 47 41 45 40 41 43 38 32 | 9 16 11 10 21 7 20 11 11 23 4 | 16 19 21 23 24 15 17 23 21 17 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 12 24 6 21 13 12 23 |T 23 28 23 23 33 23 27 25 29 22 23 WRMS | 7 19 9 12 22 5 21 12 7 23 |NE 20 25 19 20 31 20 25 23 26 19 20 MEDI | 7 19 9 11 22 5 22 13 10 22 |MD 16 26 20 20 32 17 26 21 24 19 17 Table 3.1579.2 GPS week: 1579 Day: 2 MJD: 55299.000 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 --- --- --- --- 18 --- 22 14 --- 11 | 99 --- --- --- --- 102 --- 98 103 --- 99 2E | 7 18 9 10 22 4 24 17 11 19 5 | 25 30 28 22 28 22 28 22 29 23 22 3 | 8 11 8 10 14 4 15 8 9 16 4 | 15 20 25 22 30 18 20 15 26 22 18 4E | 10 17 11 16 20 4 16 15 22 23 6 | 20 28 21 20 34 17 26 21 31 20 18 5 | 7 19 10 11 30 10 22 10 6 22 5 | 22 31 28 22 39 22 31 26 27 24 21 6 | 7 12 9 9 14 3 15 8 8 14 4 | 15 18 24 23 30 16 18 15 26 19 18 7E | 5 24 8 12 14 6 20 9 10 14 5 | 25 29 22 25 27 23 27 24 32 22 23 8E | 15 23 9 16 20 8 16 20 16 20 6 | 22 30 22 25 22 21 24 21 35 19 21 X9E | 12 36 14 --- 28 11 17 16 19 18 8 | 16 43 31 --- 46 24 31 32 34 17 23 10 | 6 11 6 8 22 4 10 9 7 19 3 | 17 17 21 18 28 16 20 18 23 22 16 11E | 7 18 7 10 39 7 17 11 13 19 4 | 15 25 21 19 42 21 23 24 27 20 18 12 | 8 21 7 10 21 5 22 16 10 30 5 | 11 27 18 22 29 16 26 19 19 18 15 13 | 8 22 10 13 43 7 27 12 9 18 5 | 15 25 21 16 43 13 25 17 23 10 13 14 | 8 20 12 11 29 8 24 19 13 17 6 | 16 24 20 22 35 19 29 22 27 17 18 15 | 8 19 10 8 29 4 21 12 8 30 5 | 16 27 22 19 36 17 27 21 21 22 17 16 | 8 21 8 11 19 6 22 14 7 24 5 | 14 24 18 20 33 15 26 19 17 16 13 17 | 6 22 10 11 26 5 24 10 10 35 5 | 17 31 14 19 33 16 32 16 18 28 15 18 | 7 23 10 11 29 4 23 12 10 27 5 | 16 32 20 23 35 17 29 19 24 24 17 19 | 8 22 11 11 23 8 27 9 13 25 5 | 20 28 15 13 26 16 30 21 23 21 16 20 | 6 25 10 13 51 6 25 14 9 24 5 | 19 29 24 22 46 18 25 25 24 21 18 21E | 8 20 9 6 21 4 25 13 18 12 5 | 25 27 24 24 29 22 30 24 31 22 22 22 | 6 22 8 9 32 4 24 12 9 21 5 | 16 28 20 19 37 17 29 22 26 22 18 23 | 9 25 11 12 31 6 30 14 11 24 6 | 16 26 21 14 36 12 27 16 23 12 13 24E | 16 23 25 16 21 12 26 29 53 22 11 | 115 110 110 111 104 115 112 113 134 109 112 26 | 6 12 8 8 17 4 11 12 8 16 3 | 14 14 16 13 23 12 18 15 18 13 11 27E | 7 21 12 16 23 6 16 11 22 13 6 | 12 26 19 15 33 14 23 17 31 11 12 28 | 7 21 7 8 27 6 24 13 10 29 5 | 13 25 17 16 32 12 26 16 19 15 13 29 | 6 20 10 7 19 6 23 15 10 --- 5 | 22 29 19 21 26 21 31 27 28 --- 21 30 | 7 13 6 7 15 4 13 15 10 19 4 | 22 18 24 23 24 19 16 23 26 19 19 31E | 8 21 9 10 23 5 20 17 10 14 5 | 31 37 31 22 40 28 30 24 35 22 27 32 | 8 21 7 14 18 4 19 13 8 23 5 | 15 17 20 22 21 14 16 20 22 13 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 20 10 11 26 6 21 14 15 22 |T 23 29 24 23 34 23 28 26 31 22 23 WRMS | 7 20 9 11 22 5 21 12 8 23 |NE 20 24 20 19 32 20 25 23 26 18 20 MEDI | 8 21 9 11 22 6 22 13 10 20 |MD 16 27 21 22 33 17 26 21 26 20 18 Table 3.1579.3 GPS week: 1579 Day: 3 MJD: 55300.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 27 --- --- --- --- 37 --- 37 26 --- 21 | 122 --- --- --- --- 127 --- 131 128 --- 129 2E | 8 21 9 10 20 2 24 18 11 14 5 | 17 30 19 21 33 20 29 22 24 23 18 3 | 8 11 6 11 11 6 13 9 10 15 4 | 19 25 27 26 29 23 24 20 31 24 23 4E | 14 15 11 13 19 7 15 18 23 20 6 | 21 27 20 21 31 26 28 26 38 19 21 5 | 12 16 8 10 28 5 20 10 10 13 5 | 30 37 26 31 42 30 37 29 36 29 29 6 | 9 11 5 9 10 6 14 8 9 13 3 | 19 26 28 28 30 23 22 21 31 24 24 7E | 7 21 9 13 16 3 22 11 11 15 5 | 29 31 23 22 32 25 32 25 37 24 26 8E | 18 23 9 18 17 9 17 19 17 20 7 | 23 31 22 29 24 21 28 23 35 20 23 X9E | 10 18 11 --- 23 7 16 23 16 14 6 | 17 28 25 --- 41 19 29 27 30 14 21 10 | 7 10 6 6 18 4 11 10 8 17 3 | 20 20 24 18 31 20 23 20 30 25 21 11E | 6 13 8 12 19 4 14 20 10 19 4 | 19 23 20 18 26 19 23 29 25 18 19 12 | 9 22 8 8 22 3 22 16 8 29 5 | 16 26 17 21 30 14 24 16 20 17 14 13 | 8 20 6 13 34 6 26 13 12 16 5 | 17 27 14 18 41 17 29 18 26 12 16 X14 | 13 29 9 12 29 8 --- 20 12 --- 7 | 15 32 25 25 34 22 --- 20 27 --- 18 15 | 11 18 7 9 29 6 21 14 7 27 5 | 17 26 21 22 34 23 26 20 22 26 18 16 | 11 18 9 9 22 6 23 15 9 25 5 | 14 24 20 19 33 15 25 18 22 15 15 17 | 6 18 14 11 26 4 23 11 10 34 5 | 19 32 17 17 38 21 34 18 25 29 18 18 | 9 21 9 12 28 4 26 13 10 25 5 | 17 30 21 21 35 17 32 18 25 23 18 19 | 8 22 12 14 23 7 29 10 11 26 6 | 27 35 18 22 30 23 36 25 32 25 23 20 | 9 24 8 13 34 5 25 12 11 18 5 | 22 33 23 28 31 21 29 25 24 20 22 21E | 6 21 8 8 19 6 24 13 10 13 5 | 29 33 29 30 32 29 32 28 34 28 28 22 | 7 19 9 9 38 6 26 13 8 18 5 | 20 30 23 22 39 18 30 20 27 18 20 23 | 9 26 9 13 36 5 30 10 11 21 6 | 17 31 19 24 43 20 31 21 29 18 19 24E | 23 24 20 16 16 11 25 26 58 32 12 | 94 88 95 94 90 91 86 91 113 93 92 26 | 7 12 7 8 17 3 13 13 9 15 3 | 11 17 16 8 22 11 19 14 22 13 13 27E | 8 17 10 25 21 7 14 13 20 11 6 | 13 21 20 25 30 11 21 13 29 13 13 28 | 8 24 13 10 23 5 23 12 13 29 5 | 18 29 25 24 36 20 29 21 24 19 20 29 | 12 21 10 8 22 4 26 14 10 --- 5 | 28 34 22 24 38 25 40 28 33 --- 27 30 | 7 16 5 9 15 3 15 15 7 16 4 | 24 19 24 23 26 20 19 23 27 21 20 31E | 7 20 9 8 20 3 20 24 12 18 5 | 37 46 42 41 45 40 48 44 38 47 39 32 | 10 18 6 12 20 5 21 16 8 19 5 | 20 22 19 23 23 19 18 27 24 17 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 19 9 12 23 5 22 15 16 21 |T 26 30 24 25 34 26 30 28 34 24 26 WRMS | 9 19 9 12 22 5 22 13 9 20 |NE 24 27 21 22 33 25 27 26 31 20 25 MEDI | 9 19 9 11 21 5 22 13 10 18 |MD 19 29 22 23 32 21 29 22 29 20 20 Table 3.1579.4 GPS week: 1579 Day: 4 MJD: 55301.000 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 --- --- --- --- 33 --- 20 25 --- 14 | 108 --- --- --- --- 114 --- 105 106 --- 108 2E | 8 21 9 13 21 6 23 16 6 17 5 | 14 30 19 18 27 16 25 18 22 22 16 3 | 10 11 8 12 13 3 13 10 10 16 4 | 14 24 22 26 28 20 23 17 27 25 19 4E | 11 17 13 16 20 6 14 14 24 16 6 | 18 31 25 25 30 24 28 24 34 25 22 5 | 11 19 9 14 32 6 27 9 9 19 5 | 23 35 24 28 41 25 36 23 29 25 24 6 | 9 13 6 11 12 3 13 10 10 16 4 | 12 23 20 24 24 18 19 16 26 23 17 7E | 9 22 11 13 28 6 22 9 8 15 5 | 21 29 22 25 35 24 30 21 32 20 21 8E | 19 23 11 16 19 6 18 18 20 19 7 | 20 31 24 28 24 23 27 22 39 22 23 X9E | 13 18 17 --- 23 8 15 17 14 19 7 | 17 28 32 --- 40 21 29 27 31 16 22 10 | 8 14 9 12 17 5 14 11 7 20 4 | 19 25 30 26 32 24 28 20 27 26 23 11 | 11 13 7 14 29 4 14 14 12 17 5 | 13 23 17 19 30 17 21 24 25 20 17 12 | 10 20 8 10 20 7 22 12 8 30 5 | 13 24 15 17 28 12 25 16 22 15 13 13 | 8 18 9 13 44 8 25 14 7 20 5 | 16 26 20 21 49 17 30 21 30 16 18 X14 | 7 18 8 14 28 7 --- 12 12 --- 5 | 18 28 24 27 36 20 --- 19 28 --- 20 15 | 10 20 9 13 26 4 27 10 11 27 5 | 13 26 21 22 33 19 29 20 25 23 17 16 | 10 19 9 10 21 5 23 15 8 26 5 | 11 23 19 17 34 15 27 19 19 20 14 17 | 7 19 13 13 28 3 22 8 10 35 5 | 16 33 21 20 38 22 35 19 23 29 19 18 | 10 22 13 11 29 3 25 13 9 24 6 | 18 32 22 21 37 19 31 19 27 24 19 19 | 9 21 13 13 22 3 24 10 12 26 5 | 24 32 19 24 33 22 36 21 28 23 21 20 | 9 24 11 16 31 7 24 13 11 18 6 | 17 31 22 24 29 20 29 24 21 18 19 21E | 7 18 7 10 23 8 23 11 9 14 4 | 18 30 20 21 37 24 29 21 27 25 20 22 | 8 17 8 9 31 5 21 12 10 18 5 | 22 30 26 21 38 21 29 22 26 22 21 23 | 10 21 9 15 33 7 25 9 7 22 5 | 18 27 20 20 38 18 29 19 27 17 19 24E | 23 33 20 24 28 11 35 20 61 28 13 | 89 70 77 83 82 75 72 75 110 80 80 26 | 6 12 9 9 16 3 12 10 7 17 3 | 12 15 14 11 20 11 16 14 23 16 11 27E | 12 17 11 15 20 8 13 11 21 14 6 | 13 23 22 18 28 17 24 14 34 13 14 28 | 7 21 10 12 22 4 24 10 9 30 5 | 20 29 24 22 35 21 30 23 28 20 21 29 | 15 19 6 12 23 7 26 14 15 --- 6 | 25 31 20 21 36 24 37 28 34 --- 25 30 | 7 13 6 7 14 5 15 10 10 18 4 | 20 21 22 21 22 18 20 21 27 21 19 31E | 7 22 11 10 19 6 21 15 10 11 5 | 22 36 25 20 41 23 31 27 28 28 23 32 | 11 18 9 14 20 7 16 13 11 20 5 | 20 24 26 25 23 21 25 28 25 18 23 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 19 10 13 25 6 21 12 16 21 |T 22 29 23 23 34 24 29 25 32 23 24 WRMS | 10 19 10 13 24 5 21 11 10 21 |NE 21 26 21 21 32 23 28 24 29 21 23 MEDI | 10 19 9 13 22 6 22 12 10 19 |MD 18 28 22 21 33 21 29 21 27 22 20 Table 3.1579.5 GPS week: 1579 Day: 5 MJD: 55302.000 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 --- --- --- --- 19 --- 23 23 --- 14 | 95 --- --- --- --- 101 --- 106 99 --- 102 2E | 10 24 9 9 19 4 21 15 6 14 5 | 12 30 20 14 20 13 22 13 18 17 14 3 | 10 13 7 9 15 3 11 7 5 16 3 | 16 24 19 18 25 16 23 16 23 23 18 4E | 12 17 10 12 14 4 14 13 22 16 6 | 14 23 16 16 24 14 24 15 30 15 14 5 | 9 19 9 9 28 5 23 13 8 14 5 | 23 30 24 22 36 21 30 22 26 19 21 6 | 10 13 7 8 17 4 13 7 5 16 3 | 18 25 22 19 26 17 22 19 24 25 20 7E | 8 20 10 10 25 6 18 11 9 11 4 | 21 29 20 22 32 21 30 20 28 20 21 8E | 20 24 10 17 22 5 17 19 20 20 7 | 18 29 20 24 22 21 23 16 33 17 19 X9E | 11 20 10 --- 23 6 16 21 13 16 6 | 14 29 25 --- 42 20 31 26 28 14 20 10 | 8 12 9 5 17 3 11 11 8 17 3 | 17 20 23 16 30 18 25 18 20 23 18 11 | 8 14 8 7 32 7 14 10 9 16 4 | 14 23 18 20 37 18 26 24 22 17 17 12 | 10 22 10 11 21 6 22 12 10 30 5 | 13 25 20 20 27 13 26 18 13 10 14 13 | 8 16 6 9 36 5 22 9 10 17 4 | 11 24 16 14 41 11 26 13 21 12 12 14 | 10 20 10 14 28 5 25 13 9 18 5 | 14 24 19 24 34 16 28 16 21 16 16 15 | 8 21 9 8 28 5 23 12 8 28 5 | 13 26 18 14 33 15 25 19 18 21 13 16 | 10 18 11 7 25 5 24 14 8 26 5 | 17 23 18 13 30 15 28 17 18 14 15 17 | 8 16 7 10 26 4 20 12 11 36 4 | 17 26 18 17 34 16 30 18 23 31 17 18 | 8 24 9 12 31 3 25 10 9 24 5 | 21 35 24 27 40 23 34 21 26 29 22 19 | 8 17 12 10 27 5 24 8 9 25 5 | 18 23 15 16 30 16 26 18 22 17 14 20 | 9 23 9 10 33 5 22 14 8 19 5 | 16 25 18 22 28 15 24 21 16 15 15 21E | 11 17 7 10 29 5 20 13 11 14 5 | 21 25 21 17 31 15 24 18 22 17 17 22 | 9 19 8 10 38 5 23 10 9 17 5 | 16 29 24 24 41 20 30 17 22 17 19 23 | 9 19 7 10 35 3 28 10 11 20 5 | 15 25 17 16 41 13 28 18 23 15 15 24E | 31 30 20 14 36 11 32 35 69 22 15 | 111 107 109 110 106 109 107 109 135 110 108 26 | 6 16 6 8 20 5 10 15 6 16 4 | 12 17 13 12 23 12 17 18 18 15 10 27E | 10 18 10 15 24 5 15 12 19 12 5 | 10 22 15 20 30 14 24 13 30 10 13 28 | 8 20 8 8 25 6 22 12 11 29 5 | 12 24 17 16 32 14 28 17 18 16 13 29 | 17 18 10 11 21 6 23 12 8 --- 5 | 24 27 20 21 27 21 33 22 27 --- 21 30 | 7 15 6 9 14 4 10 7 9 20 3 | 19 16 22 22 19 16 19 19 21 16 18 31E | 8 20 10 9 20 5 19 21 12 13 5 | 22 30 22 20 36 22 28 21 25 21 20 32 | 11 22 7 10 23 4 18 18 5 18 5 | 13 19 19 17 23 13 16 24 19 13 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 19 9 10 26 5 20 14 16 20 |T 21 27 22 21 33 22 28 24 28 20 22 WRMS | 9 19 9 10 25 5 20 12 6 22 |NE 20 24 19 18 31 20 25 22 24 18 20 MEDI | 9 19 9 10 25 5 20 12 9 17 |MD 16 25 19 19 30 16 26 18 22 17 17 Table 3.1579.6 GPS week: 1579 Day: 6 MJD: 55303.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 9 --- --- --- --- 21 --- 17 17 --- 10 | 106 --- --- --- --- 111 --- 104 108 --- 107 2E | 7 24 7 12 24 3 24 15 10 13 5 | 18 30 21 15 27 19 26 20 21 20 18 3 | 9 12 6 12 14 5 13 9 9 16 4 | 18 28 23 27 29 20 23 21 24 28 21 4E | 12 17 9 14 23 6 15 15 21 17 6 | 19 27 21 19 28 23 26 23 33 25 20 5 | 8 19 8 14 28 7 22 10 6 18 5 | 26 37 29 28 42 28 34 29 30 28 27 6 | 8 13 7 11 13 5 15 9 9 17 4 | 20 29 28 29 30 23 24 25 26 32 25 7E | 10 22 9 12 16 4 20 9 10 13 5 | 22 29 20 19 26 21 28 22 31 22 21 8E | 19 22 8 19 14 6 17 19 23 23 7 | 25 33 28 34 20 28 27 23 42 24 27 X9E | 11 21 12 --- 20 8 17 17 14 14 6 | 15 28 23 --- 42 19 26 24 24 13 18 10 | 9 13 7 8 18 5 11 9 7 16 3 | 22 26 29 27 31 26 28 24 28 29 25 11 | 12 19 8 9 32 8 17 14 9 18 5 | 14 25 17 18 32 15 19 23 21 20 16 12 | 8 22 9 14 23 5 23 11 7 31 5 | 15 27 17 25 32 15 23 21 16 17 16 13 | 8 18 7 9 37 4 23 12 9 20 4 | 21 27 21 21 39 20 29 24 28 20 21 14 | 8 20 10 14 29 6 28 11 13 21 5 | 18 25 22 24 32 18 26 19 23 15 18 15 | 9 23 7 10 25 4 28 13 9 26 5 | 13 25 18 20 31 14 26 23 17 23 15 16 | 10 22 10 10 24 7 25 17 10 26 5 | 14 24 19 19 32 13 27 22 16 19 16 17 | 10 19 9 12 28 5 20 11 14 39 5 | 20 32 22 19 36 21 35 22 23 38 21 18 | 8 23 8 10 24 5 26 13 10 24 5 | 22 33 24 22 35 22 31 25 22 30 21 19 | 8 20 8 13 27 8 28 9 7 25 5 | 26 33 23 22 39 24 39 23 30 25 24 20 | 9 22 9 9 33 6 26 14 13 20 5 | 18 27 23 24 30 18 24 26 20 19 19 21E | 7 17 8 8 44 3 22 9 12 16 4 | 25 25 23 21 40 22 27 24 28 23 22 22 | 7 19 7 8 34 6 27 11 9 17 5 | 21 30 25 23 39 20 27 25 23 23 21 23 | 9 22 8 10 35 5 30 15 8 24 5 | 17 29 20 20 38 16 29 20 21 16 17 24E | 24 26 14 19 22 18 25 29 54 25 11 | 108 103 103 108 100 104 98 106 131 104 106 26 | 6 16 8 11 17 5 15 13 8 18 4 | 13 17 13 13 20 12 17 18 18 13 12 27E | 12 19 11 18 32 6 16 9 24 12 6 | 12 22 14 16 37 12 23 13 30 14 12 28 | 12 29 8 13 26 3 24 13 13 31 6 | 22 33 25 31 37 25 29 29 32 25 25 29 | 12 19 10 11 24 5 22 9 11 --- 5 | 32 38 30 29 38 32 41 32 36 --- 31 30 | 7 14 7 8 18 5 12 7 10 22 3 | 25 25 28 30 29 23 20 28 26 21 24 31E | 7 18 8 13 43 7 23 14 6 11 5 | 17 27 21 16 32 19 26 18 23 16 18 32 | 10 18 9 9 27 7 18 21 11 20 5 | 19 23 25 24 23 20 21 32 24 18 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 20 9 12 27 6 22 13 15 22 |T 25 30 25 25 34 25 29 28 31 24 26 WRMS | 9 20 8 12 22 5 21 12 9 23 |NE 24 28 23 23 33 24 27 28 28 23 25 MEDI | 9 19 8 11 24 5 22 13 10 20 |MD 20 27 23 22 32 20 26 23 24 22 21 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1579 GPS week: 1579 MJD: 55297.0-55303.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2964 |U 8 7 22 |U 9 10 22 |U 8 8 20 | emr | emr 2832 | 12 10 32 |U 10 11 28 | 12 10 25 | esa | esa 2880 | 9 8 27 |U 9 10 25 | 10 8 19 | gfz | gfz 2766 |U 14 8 36 |U 9 11 27 |U 8 7 19 | grg | grg 2866 | 10 9 26 |U 10 12 29 | 11 8 24 | igr | igr 2891 | 9 7 26 | 9 11 24 | 10 7 19 | igs | igs 2879 | 9 8 25 | 9 11 25 | 9 8 20 | jpl | jpl 2804 |U 11 11 29 | 10 11 30 |U 11 8 21 | mit | mit 2976 |U 10 8 28 |U 9 11 25 |U 11 8 28 | Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit positions and satellite clock corrections at 15 min intervals. Each line gives the daily station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. CLK - Satellite clocks used. EPO - Number of satellite clock epochs available for that day. Units: mm. Table 5.1579.0 GPS week: 1579 Day: 0 MJD: 55297.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2960 | 8 7 21 | 7 9 22 | 9 10 24 | emr | emr 2769 | 9 6 24 | 9 10 24 | 11 8 24 | esa | esa 2880 | 8 6 21 | 8 7 22 | 9 8 19 | gfz | gfz 2768 | 8 5 20 | 9 8 29 | 6 5 17 | grg | grg 2784 | 10 8 25 | 6 9 25 | 10 7 22 | igr | igr 2803 | 7 5 20 | 8 13 20 | 8 5 18 | igs | igs 2853 | 8 5 22 | 9 13 33 | 9 8 19 | jpl | jpl 2768 | 8 6 24 | 8 8 24 | 13 9 22 | mit | mit 2976 | 7 6 20 | 8 9 26 | 10 7 26 | Table 5.1579.1 GPS week: 1579 Day: 1 MJD: 55298.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 6 6 23 | 7 7 15 | 8 7 18 | emr | emr 2767 | 8 10 34 | 8 8 21 | 9 9 21 | esa | esa 2880 | 9 9 35 | 7 8 17 | 9 8 19 | gfz | gfz 2768 | 9 10 44 | 6 9 19 | 6 5 22 | grg | grg 2880 | 8 9 27 | 9 9 26 | 8 7 21 | igr | igr 2880 | 8 9 35 | 6 9 18 | 7 7 17 | igs | igs 2818 | 7 8 25 | 6 8 17 | 8 8 19 | jpl | jpl 2768 | 8 9 28 | 8 9 20 | 8 7 21 | mit | mit 2976 | 16 10 38 | 7 9 18 | 9 7 22 | Table 5.1579.2 GPS week: 1579 Day: 2 MJD: 55299.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2968 | 8 6 16 | 14 12 23 | 8 6 15 | emr | emr 2860 | 8 8 25 | 15 11 39 | 12 7 22 | esa | esa 2880 | 9 7 28 | 13 12 34 | 9 6 18 | gfz | gfz 2768 | 8 6 24 | 14 13 40 | 8 6 17 | grg | grg 2880 | 8 7 21 | 16 13 40 | 11 7 22 | igr | igr 2936 | 9 7 21 | 14 12 29 | 9 6 16 | igs | igs 2870 | 9 7 23 | 14 12 32 | 8 6 18 | jpl | jpl 2852 | 10 8 22 | 15 12 35 | 9 6 19 | mit | mit 2976 | 11 9 28 | 16 12 36 | 11 6 18 | Table 5.1579.3 GPS week: 1579 Day: 3 MJD: 55300.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2963 | 8 7 20 | 6 8 21 | 8 7 19 | emr | emr 2851 | 8 11 23 | 8 9 24 | 13 13 31 | esa | esa 2880 | 9 8 21 | 7 7 21 | 10 10 21 | gfz | gfz 2759 | 8 8 21 | 6 8 20 | 9 9 22 | grg | grg 2880 | 9 9 26 | 6 9 23 | 14 11 29 | igr | igr 2898 | 9 7 21 | 7 7 21 | 11 10 23 | igs | igs 2909 | 8 8 20 | 6 7 21 | 9 8 21 | jpl | jpl 2763 | 10 14 32 | 8 9 33 | 11 12 26 | mit | mit 2976 | 8 8 21 | 7 8 20 | 10 9 22 | Table 5.1579.4 GPS week: 1579 Day: 4 MJD: 55301.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2967 | 10 11 25 | 9 12 32 | 8 7 21 | emr | emr 2858 | 26 15 64 | 9 10 36 | 13 13 29 | esa | esa 2880 | 15 12 43 | 10 11 34 | 10 9 18 | gfz | gfz 2767 | 47 18 100 | 11 13 35 | 7 7 15 | grg | grg 2880 | 15 13 39 | 20 15 36 | 10 9 22 | igr | igr 2941 | 15 10 42 | 10 11 35 | 9 7 20 | igs | igs 2909 | 15 12 40 | 10 10 35 | 10 8 19 | jpl | jpl 2763 | 19 21 49 | 11 11 53 | 12 11 23 | mit | mit 2976 | 14 11 40 | 11 11 32 | 14 10 57 | Table 5.1579.5 GPS week: 1579 Day: 5 MJD: 55302.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2956 | 9 7 16 | 10 14 20 | 10 9 23 | emr | emr 2860 | 10 8 19 | 10 17 18 | 12 12 26 | esa | esa 2880 | 8 8 17 | 10 14 20 | 10 9 20 | gfz | gfz 2769 | 8 6 18 | 10 15 21 | 10 9 22 | grg | grg 2880 | 9 10 21 | 8 15 19 | 12 9 22 | igr | igr 2943 | 8 8 17 | 10 16 20 | 13 9 22 | igs | igs 2918 | 8 8 19 | 9 15 16 | 10 10 22 | jpl | jpl 2857 | 9 9 20 | 9 16 19 | 8 8 20 | mit | mit 2976 | 8 7 22 | 10 14 15 | 10 10 23 | Table 5.1579.6 GPS week: 1579 Day: 6 MJD: 55303.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2960 | 9 8 32 | 8 11 24 | 9 7 20 | emr | emr 2860 | 13 10 33 | 8 13 32 | 14 10 21 | esa | esa 2880 | 8 6 25 | 7 10 25 | 12 9 21 | gfz | gfz 2769 | 8 6 24 | 7 11 28 | 10 7 19 | grg | grg 2880 | 8 7 23 | 8 14 31 | 11 9 30 | igr | igr 2842 | 7 6 24 | 7 12 27 | 10 8 20 | igs | igs 2878 | 8 7 25 | 7 10 25 | 10 9 20 | jpl | jpl 2860 | 10 7 31 | 8 12 29 | 12 7 18 | mit | mit 2976 | 7 6 26 | 8 12 28 | 14 10 26 | 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 6.1579 GPS week: 1579 MJD: 55297.500-55303.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 6 -29 71 7 -5 | 8 15 | 20 20 97 101 8 | 2 emr uuuuu | 48 38 -22 191 -5 | 60 63 | 14 15 112 60 4 | 3 esa uuuuu | -30 -32 -4 -177 -1 | 15 21 | 17 17 76 16 4 | 1 gfz uuuuu | -21 55 -17 -48 -4 | 30 32 | 9 19 51 29 7 | 1 grg --xxx | -- -- 32 -165 -5 | 14 18 | -- -- 259 149 14 | 1 igr xxxxx | 22 25 -49 -24 -4 | 4 14 | 14 9 55 56 7 | 2 irf xxxxx | 19 5 33 30 6 | -4 16 | 13 9 91 47 6 | 2 jpl uuuuu | 31 -10 46 26 -2 | 22 28 | 26 17 118 77 8 | 1 mit uuuuu | 0 15 189 55 7 | 2 17 | 17 15 135 89 9 | 3 ngs uuuuu | 17 -43 -154 105 -3 | 9 15 | 41 33 81 82 4 | 1 sio xxxxx | -254 117 -272 -26 1 | 38 41 | 22 18 152 113 8 | 1 Table 7.1579.0 GPS week: 1579 Day: 0 MJD: 55297.500 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 | 15 2 9 -120 10 | 6 11 emr uuuuu | 67 18 97 216 -2 | 63 64 esa uuuuu | -10 -47 70 -162 -1 | 16 21 gfz uuuuu | -28 55 -40 -65 4 | 28 30 grg --xxx | -- -- 455 -324 -11 | 15 18 igr xxxxx | 9 23 -67 59 -2 | 4 14 irf xxxxx | 21 13 -132 -46 -2 | -2 13 jpl uuuuu | 17 2 146 23 11 | 20 25 mit uuuuu | 6 27 -50 -60 -4 | 7 16 ngs uuuuu | -7 -14 -143 206 -1 | 7 14 sio xxxxx | -242 133 -543 -200 -4 | 39 41 Table 7.1579.1 GPS week: 1579 Day: 1 MJD: 55298.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -26 -16 -23 -82 -5 | 10 14 emr uuuuu | 63 28 33 166 -15 | 65 66 esa uuuuu | -3 -31 -15 -165 3 | 17 22 gfz uuuuu | -16 34 -23 -47 4 | 30 32 grg --xxx | -- -- -20 -223 -3 | 15 18 igr xxxxx | 33 38 -120 -61 1 | 6 13 irf xxxxx | 5 17 -38 -9 -2 | -2 12 jpl uuuuu | 35 -10 135 153 0 | 24 28 mit uuuuu | -25 27 73 -7 -4 | 5 15 ngs uuuuu | -15 -29 -102 61 3 | 9 14 sio xxxxx | -257 145 -340 -175 -8 | 39 41 Table 7.1579.2 GPS week: 1579 Day: 2 MJD: 55299.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 28 -36 22 -38 -3 | 9 15 emr uuuuu | 44 38 32 82 -5 | 63 65 esa uuuuu | -50 -55 -30 -177 1 | 16 22 gfz uuuuu | -16 45 -53 -28 0 | 31 32 grg --xxx | -- -- -113 -200 22 | 13 18 igr xxxxx | 12 14 -92 -33 0 | 5 14 irf xxxxx | 36 13 19 89 5 | -5 15 jpl uuuuu | 29 -27 43 -80 5 | 23 28 mit uuuuu | 18 29 194 172 6 | 2 16 ngs uuuuu | 22 -15 -127 98 -5 | 10 13 sio xxxxx | -220 123 -346 35 -3 | 38 41 Table 7.1579.3 GPS week: 1579 Day: 3 MJD: 55300.500 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 | 8 -61 89 66 -7 | 7 15 emr uuuuu | 35 54 -198 162 -4 | 59 62 esa uuuuu | -38 -33 130 -184 -8 | 14 20 gfz uuuuu | -19 55 -84 -30 -9 | 29 32 grg --xxx | -- -- 14 -322 -22 | 12 17 igr xxxxx | 32 16 46 -11 -18 | 4 14 irf xxxxx | 27 -6 116 53 6 | -8 15 jpl uuuuu | 61 15 -161 -27 -4 | 21 27 mit uuuuu | 3 -6 349 123 7 | -1 14 ngs uuuuu | 18 -54 -150 100 0 | 8 13 sio xxxxx | -247 117 -187 13 -2 | 36 39 Table 7.1579.4 GPS week: 1579 Day: 4 MJD: 55301.500 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 -27 49 173 -8 | 10 19 emr uuuuu | 56 60 -78 264 -5 | 60 64 esa uuuuu | -30 -8 -44 -188 3 | 15 23 gfz uuuuu | -8 86 74 -19 -8 | 31 34 grg --xxx | -- -- 217 -131 -9 | 14 18 igr xxxxx | 28 32 -42 -117 4 | 3 14 irf xxxxx | 25 -6 82 73 10 | -5 19 jpl uuuuu | 56 -15 175 -19 -11 | 23 30 mit uuuuu | 13 -5 254 131 13 | 1 18 ngs uuuuu | -32 -93 -315 -26 -8 | 10 18 sio xxxxx | -254 107 -251 49 5 | 38 42 Table 7.1579.5 GPS week: 1579 Day: 5 MJD: 55302.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 27 -44 80 -16 -15 | 9 17 emr uuuuu | 31 41 -123 230 -5 | 58 60 esa uuuuu | -32 -13 -72 -202 0 | 14 20 gfz uuuuu | -33 74 0 -45 -6 | 31 34 grg --xxx | -- -- 46 -37 2 | 15 19 igr xxxxx | 3 31 -57 -23 -6 | 3 13 irf xxxxx | -1 3 103 26 11 | -5 19 jpl uuuuu | -16 -35 -10 75 -9 | 21 28 mit uuuuu | -24 9 271 53 13 | 2 19 ngs uuuuu | 90 -79 -56 90 -5 | 10 17 sio xxxxx | -292 102 -106 13 9 | 37 41 Table 7.1579.6 GPS week: 1579 Day: 6 MJD: 55303.500 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 -22 273 69 -6 | 6 18 emr uuuuu | 40 24 84 219 -2 | 55 58 esa uuuuu | -45 -37 -70 -160 -2 | 13 20 gfz uuuuu | -29 37 8 -104 -13 | 28 31 grg --xxx | -- -- -375 83 -15 | 15 19 igr xxxxx | 39 18 -11 17 -8 | 1 14 irf xxxxx | 22 2 83 22 14 | -5 19 jpl uuuuu | 38 0 -4 58 -7 | 20 28 mit uuuuu | 8 20 234 -29 18 | 2 19 ngs uuuuu | 45 -16 -185 208 -6 | 8 17 sio xxxxx | -262 92 -132 80 14 | 36 40