Date: Thu, 23 Oct 2008 12:24:02 +0000 From: Jim Ray Subject: [IGSREPORT-16744] Wk 1500 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <49006ce2.xh3+rWYzdwzTw2ob%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 23 Oct 05:24:06 PDT 2008 Message Number 16744 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1500 (Oct 05, 2008 - Oct 11, 2008) Contacts: J. Ray (jim.ray@noaa.gov), J. Griffiths (jake.griffiths@noaa.gov) COMBINATION STRATEGY: --------------------- Starting with GPS week 860, the IGS Final orbit combination is done directly in the ITRF without any alignment to the Bulletin B EOP series. Each centre satellite clock corrections are first transformed to a common reference. One of the following two methods can be used (the REMARKS section of this report gives which method is used): [1] For each centre, a clock offset and a drift are estimated with respect to the broadcast clock corrections using only non-SA satellites; [2] A chosen reference centre is aligned to the broadcast clock corrections using all satellites. All other centres are then aligned to that reference centre. The offsets and drifts are used to align each centre satellite clock corrections to GPS time. Ephemerides and clock corrections are then combined as weighted averages computed over all centres. Each centre is given a position weight and a clock weight. The position weights are computed from each centre's absolute deviation to the unweighted average orbit after the estimation of a 7-parameter Helmert transformation. The clock weights are either computed from [1] the absolute deviation of the initial alignment to broadcast clock for the non-SA satellites, or [2] from the absolute deviation of centre's aligned clock corrections with respect to the unweighted mean. Finally, a 7-parameter Helmert transformation and clock offset and drift are estimated for each centre with respect to the combined solutions and parameters and RMS of fit reported. All the above estimations are performed using the L1-norm robust scheme. Each centre ephemerides are also evaluated individually and independently from the orbit combination by using week long arcs. The Earth Orientation Parameters (EOP) used in this evaluation are those submitted by the respective centres. The IGS combined orbits/clocks and all centres providing both orbit and clock solutions are further evaluated by an independent point positioning (navigation) program that uses both phase and pseudorange data. This is primarily intended for testing clock solution precision as well as the orbit/clock consistency. Like the clock solutions broadcast in the navigation message, the combined satellite clocks are corrected for the periodical relativistic correction (see e.g. GPS interface Control document ICD-GPS-200, p.73): -2*(X.V)/c [distance unit], where X and V are the inertial sv state and velocity vectors and c is the speed of light. Also for compatibility, no satellite L1/L2 delay calibration should be applied. SOFTWARE: --------- The weighted average software used was originally developed by T. Springer and G. Beutler in 1993. The GPS long arc orbit analysis software used here for individual centre ephemeris evaluation was developed by Beutler et al. at the Astronomical Institute of the University of Bern (AIUB). For more details on the orbit combination and complete references for both software see: Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS Analysis Centers, Bulletin Geodesique, 69, pp 200-222. Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination and Evaluation, Appendix I of the Analysis Coordinator Report, International GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94. Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report, International GPS Service for Geodynamics (IGS) 1995 Annual Report, pp. 45-76. Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report, International GPS Service for Geodynamics (IGS) 1996 Annual Report, pp. 55-100. PRODUCTS GENERATED: ------------------- The resulting average ephemeris and clocks are output to daily files in SP3 format. The satellite accuracy codes displayed in the header are based on the weighted RMS for each satellite. Note that each file contains all the satellites that appear in any of the centre ephemeris files. If a satellite or centre was excluded from combination, a note in the REMARKS section of this report will identify the exclusion and the reason. The resulting x and y earth rotation parameters (ERP) associated with the IGS ephemeris files and their rates (xrt, yrt) are computed using a weighted average of all available centres (weights are those from the orbit combination). Pole rate combination uses only centres providing estimated pole rates. Starting with GPS wk 0894, IGS LOD combinations were implemented in the Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated using Bulletin A most recent 3 weeks (21 days), i.e. up to 5 days prior to the last non-predicted day of Bulletin A. AC LOD biases are removed and the new AC bias-free LODs are used to compute a weighted IGS LOD which in turn is integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC values are printed in the IGS Final erp file. The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are: igs1500[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1500[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1500[0-6].cls IGS GPS clock combination summary report. igs15007.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15007.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Day | Centre | PRN/STA list ----+--------+--------------- 0 | COD | ALGO MCM4 0 | EMR | DAEJ THU3 0 | ESA | 4 0 | GFZ | 7 0 | MIT | 28 30 1 | COD | BOR1 FAA1 1 | EMR | MIZU 1 | ESA | 10 1 | GFZ | 7 10 1 | JPL | 10 2 | COD | WROC 2 | EMR | 13 2 | ESA | 5 ONSA 2 | GFZ | 5 7 29 BAN2 2 | JPL | BOGT 2 | MIT | DARW 3 | EMR | MIZU 3 | GFZ | 7 BAN2 3 | GRG | 26 3 | MIT | 4 19 4 | ESA | DAEJ DARW 4 | GFZ | 7 BAN2 DAEJ 4 | MIT | DARW 5 | ALL | 1 5 | EMR | MIZU 5 | GFZ | 7 YSSK 5 | JPL | NTUS 5 | MIT | 9 6 | ALL | 1 6 | EMR | KIRU MIZU 6 | ESA | 21 CHUR 6 | GFZ | 7 21 6 | MIT | 21 5. 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. 6. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .1 .0 .8 -16 -11 5 -.10 EMR | 10.5 -3.6 -2.0 69 -7 56 -.11 ESA | 5.5 3.7 6.7 41 -63 -5 -.15 GFZ | .9 .6 1.4 16 -29 12 -.35 GRG | 5.3 6.8 1.6 -4 -23 -6 -.15 JPL | .1 6.3 -1.7 1 11 -7 .07 MIT | 4.3 .6 5.0 9 -7 -7 -.17 NGS | 5.4 -.5 -.4 -1 -93 15 .09 SIO | 5.7 2.3 2.9 47 -90 9 .07 7. 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. 8. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 9. 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 1.1500.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1500.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 2.1500.[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 3.1500.[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 5.1500.0-6). 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 1500 summary. (Oct 05, 2008 - Oct 11, 2008) Table 1.1500.a GPS week: 1500 MJD: 54744.000-54750.000 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 238| 1 0 1 59 -54 -3 -.16 10 9 | -614 384 19 139 | 0 1 1 5 6 11 .03 | 480 857 emr 76| 0 0 0 -106 -45 5 .49 16 16 | 350 -5 18 217 | 1 1 1 16 12 17 .04 | 1925 1648 esa 125| 2 0 1 -50 40 -17 .29 11 10 | -817 897 22 124 | 0 1 1 15 14 21 .04 | 728 1434 gfz 193| 0 0 -5 -7 -17 57 -.08 14 14 | 236 -73 24 126 | 0 0 0 23 13 49 .03 | 299 527 grg 82| 1 4 0 30 -37 62 1.10 33 31 | -630 1040 90 143148 | 1 1 2 23 24 61 .04 | 492 1873 igr n/a| 0 0 0 28 -70 -13 .07 5 5 | -29925 -166 23 69 | 0 0 1 10 11 12 .03 | 1784 1780 jpl 115| -1 0 -4 28 -85 25 .52 15 14 | 2948 5 22 102 | 1 0 1 19 10 30 .02 | 2012 1606 mit 255| 0 0 0 28 -53 11 -.34 14 13 | -96 201 23 148 | 1 1 1 25 34 40 .09 | 447 1014 ngs 230| 0 0 1 31 102 -42 -.38 10 8 | -110950 605180 2549 4136 | 0 0 1 32 16 21 .01 | 291801 1600364 sio 106| -2 -1 2 -58 138 -6 -.03 21 20 | --- --- --- --- | 0 0 1 36 23 19 .04 | --- --- Table 1.1500.b GPS week : 1500 MJD: 54744.000-54750.000 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 16 10 10 0 12 14 | 2 | 6 6 6 6 5 5 6 | 3 | 5 5 5 5 5 4 4 | 4 | 5 4 5 5 4 5 5 | 5 | 7 6 7 4 4 4 4 | 6 | 5 5 5 5 5 4 5 | 7 | 5 5 6 5 5 5 5 | 8 | 4 4 4 4 4 4 4 | 9 | 4 5 4 4 4 4 4 | 10 | 4 4 4 4 3 4 4 | 11 | 5 5 6 5 5 5 6 | 12 | 6 6 5 5 5 5 5 | 13 | 6 5 6 5 4 5 5 | 14 | 5 5 5 5 5 5 5 | 15 | 6 6 5 6 5 6 6 | 16 | 6 6 6 5 5 5 5 | 17 | 6 6 6 6 5 6 6 | 18 | 6 6 6 6 6 6 6 | 19 | 6 6 6 6 5 5 6 | 20 | 6 5 6 6 5 5 6 | 21 | 6 6 5 5 5 6 6 | 22 | 6 6 5 5 5 5 6 | 23 | 6 6 5 5 5 6 6 | 24 | 5 5 5 5 5 5 5 | 25 | 4 4 4 4 4 4 4 | 26 | 6 5 4 6 4 4 4 | 27 | 4 4 4 4 3 4 4 | 28 | 6 6 6 6 6 6 6 | 29 | 5 5 5 5 5 5 5 | 30 | 5 4 4 4 4 4 4 | 31 | 6 6 6 5 5 5 5 | 32 | 5 5 5 4 3 4 4 | 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 2.1500.0 GPS week: 1500 Day: 0 MJD: 54744.000 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 238| 1 0 1 63 -50 -1 -.23 10 10 | -1150 1404 17 140 | 12 17 | emr 76| 1 0 -2 -120 -52 0 .40 16 16 | -3133 1849 25 344 | -16 53 | esa 125| 0 0 0 -17 38 -13 .22 11 11 | -519 -335 25 138 | 12 5 | gfz 193| 0 1 -5 24 -17 76 -.14 15 15 | 474 -850 25 120 | -24 -15 | grg 82| 0 5 -4 23 -28 27 1.05 35 32 | -1173 1412 97 312 | 5 40 | igr n/a| 0 0 0 44 -64 -35 .05 5 4 | -33151 1837 25 64 | -60 41 | jpl 115| 0 -1 -2 49 -74 10 .49 14 14 | -262 1596 24 98 | -95 37 | mit 255| 0 0 1 34 -83 26 -.20 20 19 | -380 679 26 157 | -33 22 | ngs 230| 0 0 1 -15 91 -58 -.37 10 8 | -1103 1209 2946 4326 | 58 45 | sio 106| -3 -1 2 -73 147 0 -.08 20 17 | --- --- --- --- | 61 -106 | Table 2.1500.1 GPS week: 1500 Day: 1 MJD: 54745.000 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 238| 1 0 2 56 -62 8 -.17 9 9 | 257 -1091 29 234 | -6 52 | emr 76| 2 1 2 -109 -36 -18 .48 16 16 | -1069 422 19 264 | -23 -1 | esa 125| 2 0 0 -47 47 -63 .25 12 11 | -856 448 27 123 | 23 -16 | gfz 193| 0 1 -6 5 -7 51 -.09 13 13 | 27 310 25 131 | 8 4 | grg 82| 2 3 -1 25 -53 73 1.13 33 31 | 274 -1092 96 338 | 10 30 | igr n/a| 0 0 0 34 -71 -4 .04 5 5 | -31153 278 27 78 | -47 23 | jpl 115| -1 0 -5 46 -91 2 .53 16 16 | 1408 123 25 121 | -50 2 | mit 255| 0 1 1 31 -36 88 -.22 16 16 | 402 -1479 26 220 | -21 -6 | ngs 230| -1 0 0 16 94 -35 -.40 11 9 | -297 125 2461 4177 | 9 2 | sio 106| -2 0 3 -87 130 -30 -.05 21 20 | --- --- --- --- | 46 -89 | Table 2.1500.2 GPS week: 1500 Day: 2 MJD: 54746.000 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 238| 1 0 3 63 -58 2 -.16 10 10 | -270 -233 23 122 | -3 22 | emr 76| 0 -1 2 -85 -34 -7 .49 16 16 | 82 -808 15 140 | -58 23 | esa 125| 2 0 -1 -57 67 -11 .30 11 11 | 455 -990 21 107 | 32 15 | gfz 193| 0 0 -6 -11 -22 132 -.08 14 14 | 721 -434 22 120 | -13 10 | grg 82| 3 3 3 6 -34 -47 1.08 35 32 | -290 -205 93 369 | -17 24 | igr n/a| 0 0 0 38 -74 -13 .08 6 5 | -30163 -934 21 71 | -44 56 | jpl 115| -1 0 -5 8 -90 -2 .51 15 15 | 2159 -895 19 93 | -30 2 | mit 255| 0 0 2 18 -84 -29 -.42 15 15 | -356 816 21 104 | -20 27 | ngs 230| -1 1 1 63 88 -38 -.38 10 9 | -22 -603 3086 4179 | -78 -19 | sio 106| -1 -2 3 -93 171 -34 -.06 20 20 | --- --- --- --- | 39 -109 | Table 2.1500.3 GPS week: 1500 Day: 3 MJD: 54747.000 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 238| 1 0 0 55 -61 -2 -.16 10 10 | -771 239 21 122 | -14 41 | emr 76| 1 -1 -1 -88 -53 25 .52 16 16 | 666 2269 17 155 | -43 5 | esa 125| 1 -2 3 -45 29 -2 .27 10 10 | -586 920 22 116 | 19 -10 | gfz 193| 0 0 -5 -40 0 57 -.08 14 14 | 83 77 24 122 | 2 -1 | grg 82| 2 2 1 6 -72 98 1.06 34 31 | -829 4826 88 999999 | -53 28 | igr n/a| 0 0 2 22 -90 -8 .04 6 5 | -29698 2405 23 60 | -16 -1 | jpl 115| -3 -1 -5 41 -99 53 .52 15 15 | 2776 2579 23 99 | -50 1 | mit 255| 0 0 1 -14 0 -16 -.41 14 14 | -559 761 22 127 | 8 -25 | ngs 230| 0 1 2 76 95 -58 -.36 10 8 | -772693 4234466 2584 4490 | -32 63 | sio 106| -2 0 3 -82 126 4 -.03 20 20 | --- --- --- --- | 25 -52 | Table 2.1500.4 GPS week: 1500 Day: 4 MJD: 54748.000 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 238| 1 2 2 51 -48 2 -.14 9 9 | -1028 375 17 118 | 40 -5 | emr 76| 2 0 1 -96 -28 14 .52 16 16 | 2187 -1983 16 185 | -52 26 | esa 125| 3 0 0 -61 24 -24 .34 9 9 | -917 1433 21 111 | 18 -2 | gfz 193| 0 0 -5 9 -38 60 -.04 15 15 | 204 -246 24 135 | -13 4 | grg 82| 0 5 4 27 -15 143 1.08 31 29 | -1034 363 87 329 | -10 -19 | igr n/a| 0 0 1 20 -54 3 .11 5 5 | -28087 -1886 23 75 | -49 38 | jpl 115| -1 -1 -6 4 -69 4 .53 15 15 | 4698 -1466 22 111 | -35 13 | mit 255| -1 0 0 44 -93 -6 -.36 9 9 | 218 -721 23 150 | -20 22 | ngs 230| -1 0 1 34 132 -18 -.37 9 7 | -1041 390 2120 3593 | -4 -16 | sio 106| -3 0 3 -55 109 -7 -.01 20 20 | --- --- --- --- | 43 -67 | Table 2.1500.5 GPS week: 1500 Day: 5 MJD: 54749.000 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 238| 0 1 0 61 -53 -25 -.14 9 9 | -567 1134 15 110 | -13 18 | emr 76| 0 0 0 -120 -54 26 .52 16 16 | 1892 -61 17 199 | -2 13 | esa 125| 2 -1 3 -57 42 0 .32 11 10 | -1769 3460 19 132 | 70 -30 | gfz 193| 0 0 -4 -34 -8 55 -.08 15 15 | 323 -152 24 126 | 0 -4 | grg 82| 1 4 1 62 -56 94 1.10 30 30 | -578 1131 86 366 | -33 27 | igr n/a| 0 0 1 17 -71 -24 .10 5 5 | -28252 -584 22 74 | -29 16 | jpl 115| 0 0 -4 36 -87 31 .55 14 13 | 5063 -78 18 91 | -38 4 | mit 255| -1 0 0 16 -29 28 -.36 10 9 | -487 1428 24 162 | -18 -13 | ngs 230| -1 0 0 43 99 -71 -.37 10 7 | -49 -404 2204 4194 | -14 35 | sio 106| -1 0 2 -14 118 18 -.01 21 20 | --- --- --- --- | -11 -47 | Table 2.1500.6 GPS week: 1500 Day: 6 MJD: 54750.000 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 238| 2 3 2 65 -46 -10 -.16 10 10 | -772 861 15 127 | 8 5 | emr 76| -1 -1 0 -125 -62 -3 .48 16 16 | 1829 -1725 20 234 | -3 41 | esa 125| 2 -1 3 -62 34 -5 .32 11 11 | -1531 1349 23 142 | 19 7 | gfz 193| 0 1 -5 -9 -28 -34 -.06 14 14 | -179 783 25 130 | 19 9 | grg 82| 3 3 0 64 -2 47 1.17 34 30 | -782 849 88 325 | 94 9 | igr n/a| 0 1 0 21 -65 -12 .10 5 5 | -28972 -2280 23 64 | -17 40 | jpl 115| -4 -1 -3 10 -86 79 .52 14 14 | 4800 -1822 24 102 | 12 23 | mit 255| 1 -1 -1 67 -49 -8 -.39 11 10 | 486 -76 22 120 | -36 -7 | ngs 230| 0 0 0 0 117 -15 -.38 9 8 | -1446 1081 2446 3994 | 50 59 | sio 106| 0 -1 0 0 163 5 .02 23 21 | --- --- --- --- | 6 -72 | 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 3.1500.0 GPS week: 1500 Day: 0 MJD: 54744.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 14 --- --- --- --- 27 --- 37 16 --- 14 | 32 --- --- --- --- 35 --- 44 24 --- 28 2 | 11 20 17 15 41 6 15 16 12 19 5 | 24 38 27 32 56 27 34 26 23 29 26 3 | 7 17 7 15 22 3 12 19 10 26 5 | 16 30 24 22 33 20 29 25 18 38 21 4 | 9 14 9 12 25 5 8 20 9 23 4 | 39 47 40 42 59 39 45 35 38 51 40 X5 | 8 --- 9 18 --- 9 --- 26 14 --- 7 | 17 --- 27 24 --- 23 --- 31 18 --- 21 6 | 9 18 9 13 24 3 13 18 11 24 5 | 14 34 23 22 33 19 30 24 16 34 20 7 | 12 16 12 16 28 6 15 18 8 16 5 | 17 27 17 25 38 17 26 22 17 13 16 8 | 11 13 6 10 17 4 9 18 7 14 4 | 14 21 16 21 22 16 21 23 19 14 16 9 | 8 13 10 11 25 4 10 23 7 17 4 | 11 20 15 17 28 15 22 24 16 13 13 10 | 7 13 8 9 37 4 7 19 8 14 3 | 15 22 20 15 28 17 18 23 15 12 15 11 | 8 16 11 20 63 5 11 15 9 15 5 | 19 32 21 26 43 21 27 23 22 31 22 12 | 10 14 9 14 39 5 13 27 12 27 5 | 18 31 25 27 39 26 31 34 24 25 22 13 | 15 13 9 14 32 5 18 25 9 15 5 | 33 34 32 34 46 31 33 29 28 24 29 14 | 8 15 12 16 50 4 15 20 14 9 5 | 9 24 14 20 48 13 20 19 13 12 11 15 | 12 18 14 13 39 5 17 22 13 16 5 | 10 25 17 22 33 17 26 23 20 14 16 16 | 13 16 10 15 26 5 14 15 10 34 6 | 21 34 25 27 34 24 31 24 24 25 24 17 | 13 16 11 14 33 5 17 21 8 24 5 | 22 41 28 34 36 30 39 27 30 33 29 18 | 9 21 16 16 28 6 19 20 11 22 6 | 13 33 23 26 33 20 28 19 18 14 18 19 | 9 25 15 13 36 4 19 20 13 19 6 | 20 45 23 25 38 24 34 27 18 24 24 20 | 11 15 12 20 57 4 16 15 13 19 5 | 18 32 26 24 47 21 28 21 19 21 19 21 | 11 19 16 15 32 5 17 21 10 15 5 | 17 36 20 32 45 25 34 27 27 27 23 22 | 11 16 15 18 29 6 16 23 11 18 5 | 19 29 25 23 32 18 26 28 17 19 19 23 | 13 20 12 12 49 4 18 22 9 17 5 | 9 33 17 18 37 16 29 24 15 16 15 24 | 8 14 8 16 28 4 10 21 8 20 4 | 23 30 26 27 32 25 29 32 29 31 25 25 | 9 11 8 12 29 4 9 20 9 11 4 | 11 20 19 18 26 12 21 21 15 15 14 26E | 14 16 10 19 30 4 11 23 9 26 5 | 42 48 54 56 68 49 51 51 45 50 46 27 | 10 14 5 11 14 4 8 18 8 14 4 | 18 22 18 22 22 18 23 27 21 18 18 28 | 9 15 9 14 49 6 13 17 10 37 5 | 21 34 24 29 42 26 32 26 23 36 23 29 | 9 19 12 12 22 6 12 20 14 19 5 | 22 32 23 28 42 25 29 32 23 34 23 30 | 8 11 7 13 37 4 8 23 8 20 4 | 30 30 33 31 53 29 31 42 28 24 29 31 | 9 15 15 20 36 6 14 22 13 17 5 | 20 33 24 27 47 24 30 23 22 27 22 32 | 10 13 9 9 27 3 13 21 9 11 4 | 11 24 21 18 29 18 21 20 20 22 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 16 11 15 35 5 14 20 10 20 |T 19 31 24 26 38 23 29 27 22 24 21 WRMS | 10 16 11 15 32 4 14 19 8 17 |NE 18 30 23 25 37 21 28 26 21 23 20 MEDI | 9 15 10 14 30 5 13 20 10 18 |MD 18 32 23 25 37 21 29 25 20 24 21 Table 3.1500.1 GPS week: 1500 Day: 1 MJD: 54745.000 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 | 20 --- --- --- --- 25 --- 23 23 --- 15 | 29 --- --- --- --- 31 --- 41 52 --- 37 2 | 10 18 15 15 31 5 17 12 11 23 5 | 18 31 17 26 45 21 29 24 20 24 20 3 | 7 16 8 14 24 4 13 16 8 22 4 | 10 24 15 18 30 13 21 21 12 30 14 4 | 7 14 7 11 22 4 11 13 10 24 4 | 45 49 45 46 66 47 48 46 50 54 46 X5 | 8 --- 9 14 --- 7 --- 17 11 --- 5 | 14 --- 21 23 --- 18 --- 26 22 --- 18 6 | 9 16 8 12 31 4 13 14 9 22 4 | 8 23 17 18 30 14 22 20 16 27 14 7 | 8 17 12 16 27 7 15 15 11 19 5 | 12 29 20 24 35 16 26 19 14 16 15 8 | 8 12 6 9 18 3 11 15 7 13 3 | 22 23 23 25 26 21 25 26 22 22 21 9 | 8 13 10 10 25 5 12 18 11 16 4 | 17 27 21 19 24 20 23 30 20 23 18 10 | 7 10 6 9 35 6 10 15 8 12 3 | 13 19 17 10 29 14 14 21 18 11 13 11 | 5 16 12 18 57 4 18 14 13 14 5 | 18 25 22 24 45 22 25 29 23 20 19 12 | 9 14 12 13 31 9 13 21 12 28 5 | 14 27 20 23 28 21 25 26 19 21 17 X13 | 9 17 9 14 32 6 --- 16 10 11 5 | 12 28 16 20 35 16 --- 24 17 19 16 14 | 8 16 13 14 30 5 20 17 12 13 5 | 12 24 15 19 31 15 22 23 15 11 14 15 | 12 19 14 13 42 4 21 18 10 13 5 | 10 24 17 19 38 14 24 22 15 12 14 16 | 10 17 13 14 38 7 15 13 14 41 6 | 14 26 16 23 34 18 25 20 18 29 16 17 | 10 16 11 14 26 6 20 20 13 19 5 | 19 28 17 25 27 20 27 23 24 21 18 18 | 9 20 20 19 21 6 21 17 9 22 6 | 12 30 22 24 37 17 28 18 13 13 14 19 | 9 24 14 13 34 5 19 16 10 19 5 | 14 37 17 19 38 17 28 23 13 19 16 20 | 10 16 13 19 47 5 17 12 10 17 5 | 11 31 20 22 36 17 27 17 15 17 14 21 | 11 20 15 12 26 4 19 19 11 19 5 | 13 29 18 24 42 18 26 21 21 22 17 22 | 9 18 16 18 34 7 20 19 10 17 5 | 15 29 21 22 33 17 24 24 16 15 15 23 | 11 22 12 11 48 5 20 18 13 18 5 | 9 34 17 20 36 17 28 21 19 18 15 24 | 7 15 9 15 29 4 13 17 11 20 4 | 25 32 29 31 33 26 30 28 25 33 26 25 | 8 15 9 13 31 5 9 16 10 13 4 | 16 27 23 24 30 18 24 25 16 22 18 26 | 11 14 7 11 44 4 11 19 9 21 4 | 25 30 26 28 51 27 27 34 29 31 26 27 | 9 15 7 9 17 4 10 16 8 16 4 | 21 27 24 25 26 21 28 24 23 27 21 28 | 8 14 12 14 44 8 16 15 10 39 5 | 13 22 15 22 33 15 22 18 17 34 13 29 | 8 18 13 12 27 4 15 18 10 18 5 | 19 30 19 28 37 22 26 26 21 27 21 30 | 6 11 9 11 31 4 8 17 9 19 4 | 20 21 23 22 39 18 20 27 20 19 19 31 | 9 18 14 16 36 6 18 16 11 20 5 | 16 29 13 23 35 18 26 22 16 19 16 32 | 8 12 11 7 20 4 16 15 11 14 4 | 9 17 15 14 24 14 21 19 16 20 12 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 16 12 13 33 5 16 16 10 21 |T 16 27 20 22 35 19 25 24 20 22 18 WRMS | 9 16 11 13 31 5 16 16 9 20 |NE 15 27 19 22 34 18 25 23 19 22 17 MEDI | 9 16 12 13 31 5 15 16 10 19 |MD 14 27 19 23 34 18 25 23 18 21 16 Table 3.1500.2 GPS week: 1500 Day: 2 MJD: 54746.000 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 | 12 --- --- --- --- 29 --- 17 15 --- 10 | 28 --- --- --- --- 41 --- 28 30 --- 25 2 | 9 19 12 14 33 5 17 21 10 19 5 | 19 34 24 28 45 23 29 23 24 24 22 3 | 10 12 11 13 26 6 12 13 12 27 5 | 14 23 21 20 26 15 21 21 18 32 16 4 | 8 13 11 12 32 6 11 16 10 21 4 | 30 28 27 30 34 26 25 31 25 29 25 X5 | 11 25 16 12 --- 11 --- 17 9 --- 6 | 18 24 33 26 --- 24 --- 21 20 --- 22 6 | 10 14 10 12 21 5 14 12 13 25 5 | 11 21 17 18 21 12 22 21 15 27 13 7 | 10 19 13 17 28 6 17 16 10 19 5 | 14 31 18 26 37 18 25 23 15 15 16 8 | 10 11 8 11 24 5 11 15 9 14 4 | 13 18 22 20 22 15 20 26 15 13 16 9 | 9 13 12 11 23 6 12 9 8 14 4 | 14 20 17 17 25 14 23 16 11 15 12 10 | 9 12 5 7 26 4 10 13 8 15 3 | 15 17 13 12 23 12 15 18 14 16 12 11E | 9 14 11 19 36 7 17 19 11 17 5 | 30 38 32 33 53 32 36 37 32 35 31 12 | 10 13 10 11 37 7 11 13 11 29 5 | 16 25 20 20 36 19 24 19 19 18 16 X13 | 9 19 10 14 33 6 --- 14 9 --- 5 | 20 29 25 27 44 22 --- 27 21 --- 22 14 | 8 15 15 16 36 6 18 11 12 14 5 | 11 23 16 19 33 14 21 18 16 14 13 15 | 13 19 11 11 32 3 18 19 8 12 5 | 11 25 17 22 35 17 27 19 21 18 15 16 | 12 14 10 12 35 7 16 14 13 34 5 | 15 25 18 22 34 19 26 20 20 22 16 17 | 13 17 13 16 26 6 18 17 11 21 5 | 22 32 21 31 29 23 30 30 25 33 24 18 | 8 19 13 17 30 6 20 18 9 22 5 | 11 29 17 24 34 18 27 18 14 13 14 19 | 11 21 14 13 29 6 16 17 11 17 5 | 15 33 18 23 39 18 27 21 22 22 18 20 | 11 17 13 20 49 4 17 16 9 16 5 | 17 31 23 25 38 19 27 25 18 16 18 21 | 11 18 10 13 76 6 19 16 10 16 5 | 15 32 25 29 48 22 31 24 24 24 22 22 | 10 14 12 20 46 6 18 13 10 16 5 | 15 25 18 22 36 16 23 18 15 14 14 23 | 10 18 14 12 37 6 19 13 9 21 5 | 10 29 18 20 33 14 25 19 14 20 15 24 | 8 17 10 16 27 6 13 17 8 18 5 | 14 29 18 22 34 18 27 22 15 27 17 25 | 8 15 8 12 37 4 8 13 8 12 4 | 18 29 25 22 30 19 20 25 17 19 19 26 | 8 15 8 11 40 5 11 10 10 17 4 | 19 24 17 20 48 18 27 16 21 25 17 27 | 8 12 6 12 21 5 9 12 11 14 4 | 15 21 20 21 26 16 19 25 15 17 16 28 | 12 12 10 16 33 7 13 21 12 36 6 | 16 23 20 25 26 17 23 30 19 33 17 29 | 7 19 12 12 38 7 15 17 13 17 5 | 16 28 16 21 44 18 21 24 18 21 16 30 | 8 10 8 11 23 5 8 12 8 17 3 | 23 24 27 27 35 24 27 25 24 19 22 31 | 8 16 15 18 39 7 16 14 12 24 5 | 16 28 20 23 39 18 25 20 18 28 17 32 | 7 17 12 8 27 4 16 12 12 11 4 | 11 19 17 15 24 12 19 21 15 14 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 16 11 14 35 6 15 15 10 20 |T 16 26 20 22 34 19 24 22 19 21 17 WRMS | 10 16 11 14 32 5 15 15 9 20 |NE 15 26 20 22 33 18 24 22 18 20 17 MEDI | 9 15 11 12 32 6 16 14 10 17 |MD 15 25 20 22 34 18 25 21 18 20 16 Table 3.1500.3 GPS week: 1500 Day: 3 MJD: 54747.000 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 | 12 --- --- --- --- 22 --- 15 13 --- 9 | 18 --- --- --- --- 18 --- 22 24 --- 16 2 | 8 17 10 15 38 6 15 23 9 22 5 | 19 31 24 30 43 23 30 22 26 26 22 3 | 6 14 9 13 18 4 12 9 9 26 4 | 19 26 23 24 32 22 28 25 26 32 22 4 | 8 10 10 15 29 6 14 13 7 26 4 | 73 74 74 76 70 72 74 73 79 78 75 X5 | 6 11 6 12 28 6 --- 9 6 18 3 | 14 18 18 20 28 17 --- 15 17 11 15 6 | 9 13 8 12 24 4 13 10 7 25 4 | 15 23 17 20 24 15 25 22 18 28 16 7 | 9 16 9 17 30 6 14 15 11 19 5 | 12 27 17 23 36 17 23 18 16 12 14 8 | 12 12 8 11 20 5 11 13 8 16 4 | 21 26 23 24 28 20 25 22 21 22 19 9 | 10 15 10 10 33 5 11 12 9 16 4 | 15 25 20 17 25 17 26 13 14 24 14 10 | 6 12 6 7 31 5 10 16 11 18 4 | 16 19 20 16 29 19 17 18 25 19 16 11E | 10 15 9 17 32 5 15 14 9 16 4 | 15 27 19 23 51 19 28 20 16 25 17 12 | 10 15 10 12 37 7 13 12 10 29 5 | 20 34 25 27 43 27 33 22 24 24 22 13 | 10 17 9 13 34 4 18 14 9 12 4 | 17 26 21 23 46 19 31 22 19 24 18 14 | 9 17 13 15 41 6 17 14 9 10 5 | 10 22 14 19 38 12 21 16 16 12 11 15 | 18 21 13 15 42 7 20 18 14 14 6 | 19 26 19 23 38 18 28 17 20 15 16 16 | 10 13 10 12 37 5 14 12 10 34 5 | 18 27 19 26 35 22 26 25 24 23 20 17 | 14 18 12 15 21 8 20 16 9 16 5 | 19 31 20 31 30 25 29 26 28 21 22 18 | 10 16 14 16 38 6 18 15 10 21 5 | 15 27 19 24 37 17 27 17 15 14 14 19 | 10 25 10 15 27 5 18 15 13 17 5 | 16 35 22 23 36 22 29 21 22 20 19 20 | 9 19 14 18 38 4 19 14 12 18 5 | 16 30 23 23 35 20 27 21 18 17 17 21 | 11 21 13 13 58 4 17 11 11 14 5 | 21 37 22 28 44 23 32 26 28 27 24 22 | 8 16 13 19 56 5 17 12 9 17 5 | 16 27 23 23 39 18 24 20 20 15 16 23 | 9 22 12 9 35 6 20 15 9 18 5 | 10 29 16 17 33 14 25 14 15 17 13 24 | 8 16 10 13 34 5 11 15 13 19 4 | 32 41 38 34 47 34 40 37 39 39 35 25 | 7 15 8 11 26 5 10 12 7 11 3 | 13 25 17 18 30 14 21 17 15 17 14 X26 | 11 19 9 14 112 9 --- 15 12 --- 6 | 17 28 26 28 104 26 --- 26 28 --- 21 27 | 13 13 7 11 16 4 10 12 8 14 4 | 14 22 17 19 26 14 21 18 17 18 14 28 | 11 14 8 14 37 9 14 23 8 38 6 | 21 26 19 24 28 21 24 29 21 33 18 29 | 8 17 15 14 33 7 14 14 12 16 5 | 25 32 28 33 46 29 33 29 33 33 28 30 | 6 10 8 11 27 4 8 11 7 17 3 | 23 27 23 22 37 22 28 22 24 18 21 31 | 9 17 10 16 33 7 13 14 11 26 5 | 13 25 14 22 38 17 23 18 15 22 13 32 | 6 14 10 7 26 5 14 14 8 16 4 | 11 18 18 12 24 14 17 19 14 21 11 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 16 10 14 34 6 15 14 10 20 |T 18 28 22 24 38 21 28 22 23 23 19 WRMS | 10 16 10 14 31 5 15 14 8 20 |NE 19 28 22 24 36 21 28 22 23 23 19 MEDI | 9 16 10 13 33 5 14 14 9 17 |MD 16 27 20 23 36 19 27 21 20 21 17 Table 3.1500.4 GPS week: 1500 Day: 4 MJD: 54748.000 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 | 5 --- --- --- --- 96 --- --- --- --- 0 | 16 --- --- --- --- 79 --- --- --- --- 18 2 | 8 16 11 15 40 6 17 16 11 22 5 | 20 29 24 25 49 22 32 17 24 23 21 3 | 10 14 10 16 19 4 14 6 8 26 4 | 15 28 25 23 28 21 25 19 24 36 21 4 | 7 13 7 13 18 5 10 8 11 23 4 | 26 30 24 32 40 29 30 27 34 36 27 5 | 7 12 6 9 24 4 9 9 8 21 3 | 12 16 18 17 29 14 10 14 12 13 12 6 | 10 15 9 15 21 4 14 6 6 25 4 | 11 27 20 20 31 16 20 15 20 32 17 7 | 9 17 11 19 29 6 15 11 9 18 5 | 14 28 17 24 35 16 25 12 14 12 14 8 | 9 14 7 12 17 4 10 6 6 13 3 | 14 24 17 19 21 15 20 15 16 16 15 9 | 9 17 7 10 29 5 12 7 9 17 4 | 12 22 14 17 31 16 23 15 18 24 14 10 | 7 11 5 7 34 5 8 7 7 18 3 | 13 23 18 16 21 16 20 14 20 17 16 11E | 9 20 9 16 35 5 16 11 8 17 4 | 23 35 26 27 44 24 28 21 25 23 23 12 | 9 13 8 12 32 4 13 9 8 30 4 | 17 28 21 25 37 20 28 16 17 21 17 13 | 10 13 9 13 46 5 18 9 7 11 4 | 17 29 22 21 46 20 29 16 19 18 18 14 | 10 17 11 18 29 5 18 9 7 13 4 | 13 27 20 26 32 16 24 18 22 14 18 15 | 12 19 10 14 30 5 19 11 8 12 5 | 13 29 22 25 36 20 31 19 18 20 19 16 | 10 12 10 14 25 5 14 9 11 31 5 | 17 28 18 23 31 20 25 17 20 24 18 17 | 10 17 10 16 30 7 18 10 8 15 4 | 17 28 15 27 31 21 27 18 24 21 19 18 | 8 20 10 17 25 7 20 13 10 23 5 | 14 30 17 25 33 19 28 15 19 17 16 19 | 9 23 11 16 29 4 19 10 10 17 5 | 16 37 20 25 34 20 28 16 20 20 18 20 | 9 16 10 20 40 6 19 10 9 17 5 | 15 31 23 23 32 20 26 17 18 15 17 21 | 8 19 11 16 28 6 20 10 9 20 5 | 19 30 19 27 43 21 32 17 25 24 21 22 | 8 15 12 21 47 6 18 12 10 17 5 | 15 26 17 23 38 17 24 19 21 15 16 23 | 12 22 11 10 32 5 21 12 10 14 5 | 9 33 17 20 34 18 30 12 16 17 15 24 | 7 19 6 17 34 6 12 9 10 20 4 | 27 36 29 29 41 30 34 30 31 37 29 25 | 8 13 7 13 23 3 10 6 8 10 3 | 11 23 16 19 27 14 21 11 16 15 14 26 | 8 14 6 13 39 5 12 8 9 17 4 | 14 29 20 25 58 19 29 16 18 22 18 27 | 7 13 7 11 18 4 10 6 7 11 3 | 13 23 16 18 22 15 22 12 16 14 14 28 | 8 20 11 14 33 7 14 12 7 35 5 | 17 30 18 23 26 17 25 20 18 33 17 29 | 8 20 10 17 32 8 16 10 10 19 5 | 21 34 19 31 42 25 31 24 22 28 23 30 | 8 12 6 13 29 4 8 8 6 19 3 | 18 21 22 19 36 19 24 20 19 17 17 31 | 7 19 12 18 33 6 15 11 8 21 5 | 12 29 15 22 37 16 24 13 15 19 14 32 | 6 12 9 8 25 4 13 5 6 11 3 | 10 19 18 14 24 14 18 11 13 12 12 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 16 9 15 31 5 15 9 9 20 |T 15 27 19 22 34 20 25 16 19 21 17 WRMS | 9 16 9 15 29 5 15 9 7 20 |NE 15 27 19 22 33 18 25 16 19 21 17 MEDI | 8 16 10 14 29 5 14 9 8 18 |MD 15 28 19 23 34 19 25 16 19 20 17 Table 3.1500.5 GPS week: 1500 Day: 5 MJD: 54749.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 13 --- --- --- --- 27 --- 17 16 --- 11 | 21 --- --- --- --- 43 --- 26 37 --- 24 2 | 10 17 11 15 33 5 13 18 10 21 5 | 15 27 17 21 40 17 24 17 22 19 16 3 | 7 15 8 12 17 4 12 8 8 28 4 | 14 19 18 19 25 14 20 19 16 28 14 4 | 10 15 9 12 21 4 10 8 9 28 4 | 47 47 46 48 48 45 44 45 47 50 45 5 | 11 10 6 11 23 5 6 7 6 21 3 | 14 20 19 19 20 17 17 16 16 16 15 6 | 9 14 7 12 20 3 10 6 8 25 4 | 13 21 16 19 23 13 19 17 19 28 14 7 | 7 16 12 18 30 6 15 10 13 19 5 | 17 30 26 27 37 23 29 16 24 13 20 8 | 10 12 6 13 20 4 9 5 7 16 3 | 21 24 23 21 24 22 24 20 22 23 20 9 | 8 18 9 12 21 6 11 11 7 16 4 | 17 27 18 18 27 17 24 18 17 23 16 10 | 6 12 7 7 35 5 9 10 7 21 3 | 14 22 18 16 21 15 20 11 18 12 14 11E | 8 19 11 14 35 5 12 9 9 16 4 | 13 28 18 18 40 16 22 15 15 18 15 12 | 11 13 7 12 26 5 11 7 8 29 4 | 15 28 23 23 31 20 27 17 18 21 17 13 | 10 15 9 15 40 5 15 9 12 12 4 | 14 25 19 21 43 17 23 14 22 17 16 14 | 10 14 13 19 41 6 17 9 8 11 4 | 11 24 15 24 37 16 23 19 17 15 15 15 | 14 19 13 15 29 6 17 14 11 13 5 | 13 25 16 23 38 16 24 19 14 18 14 16 | 10 13 10 13 33 5 15 11 10 35 5 | 13 23 16 22 27 15 22 16 17 20 14 17 | 11 24 17 19 22 7 19 11 11 19 6 | 17 32 21 28 23 20 25 24 25 18 19 18 | 8 16 14 20 26 6 20 13 8 24 5 | 12 28 16 24 32 15 29 16 14 17 14 19 | 8 23 12 15 18 5 16 11 10 20 5 | 11 32 17 21 36 15 25 14 13 15 13 20 | 10 18 14 19 42 4 19 10 8 18 5 | 13 29 23 23 35 17 26 15 15 14 15 21 | 9 22 15 12 36 5 18 10 14 20 5 | 14 32 17 21 40 19 29 16 25 21 17 22 | 9 14 13 23 33 4 17 12 7 16 5 | 11 22 17 24 33 14 23 17 14 13 12 23 | 12 21 13 12 33 5 20 11 12 16 5 | 8 30 18 20 35 16 26 12 18 17 14 24 | 10 15 8 18 34 6 11 6 15 20 4 | 24 35 27 30 32 26 35 23 23 36 25 25 | 7 15 8 14 27 4 10 7 9 11 3 | 17 25 20 22 27 18 26 19 20 19 18 26 | 9 13 8 15 32 8 11 8 10 21 4 | 16 27 19 23 34 21 25 18 19 24 17 27 | 10 13 7 13 27 4 9 5 8 14 3 | 22 26 23 24 22 22 25 22 25 22 22 28 | 9 15 14 15 33 6 14 9 11 38 5 | 15 23 25 21 25 15 23 19 15 32 15 29 | 9 22 12 16 25 5 15 9 9 20 5 | 19 34 20 28 38 22 29 21 23 27 21 30 | 9 10 6 14 32 4 7 6 7 20 3 | 20 24 23 24 36 22 27 21 22 21 21 31 | 11 18 12 18 36 6 17 10 9 21 5 | 11 26 17 20 37 13 25 13 15 20 13 32 | 9 15 10 9 30 3 16 6 7 14 4 | 10 20 17 13 28 12 18 10 10 12 10 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 16 11 15 30 5 14 10 10 21 |T 16 26 20 22 32 19 25 18 19 20 17 WRMS | 9 16 10 15 30 5 13 9 7 20 |NE 15 26 20 22 31 18 25 18 19 20 17 MEDI | 9 15 10 14 30 5 14 9 9 20 |MD 14 26 18 22 33 17 25 17 18 19 15 Table 3.1500.6 GPS week: 1500 Day: 6 MJD: 54750.000 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 | 20 --- --- --- --- 18 --- 16 20 --- 13 | 17 --- --- --- --- 34 --- 26 34 --- 23 2 | 10 17 12 14 33 5 15 18 14 29 5 | 21 35 22 29 41 24 31 19 27 35 23 3 | 9 13 8 11 18 4 10 6 7 29 4 | 12 26 17 16 26 13 22 17 13 34 14 4 | 9 13 9 13 37 7 12 10 10 27 4 | 32 35 35 36 33 34 36 33 36 35 33 5 | 10 10 6 11 44 5 6 7 8 28 4 | 16 21 25 22 40 20 13 22 19 18 19 6 | 11 13 8 11 16 4 12 7 8 30 4 | 15 23 12 16 21 12 19 14 15 29 12 7 | 10 15 12 17 28 6 14 12 11 25 5 | 18 29 21 25 37 20 24 12 22 13 18 8 | 10 12 6 11 17 4 12 6 7 17 3 | 13 23 18 19 27 16 22 15 17 16 15 9 | 10 14 10 12 21 6 11 11 9 19 4 | 13 23 19 18 27 16 25 16 13 19 14 10 | 8 12 8 7 32 5 10 8 10 23 3 | 19 30 29 18 21 23 25 19 29 28 23 11E | 12 18 13 15 39 5 14 19 9 22 5 | 17 34 22 27 46 21 27 21 18 29 19 12 | 10 13 9 11 33 6 11 7 9 34 4 | 21 33 28 29 44 26 33 26 24 25 24 13 | 9 16 9 15 35 4 16 11 8 18 4 | 12 26 19 23 45 17 26 14 16 19 16 14 | 12 16 12 17 28 7 16 14 8 12 5 | 14 28 17 24 34 17 27 21 20 17 18 15 | 12 20 13 12 31 4 17 16 14 13 5 | 22 37 28 30 39 26 36 23 29 25 26 16 | 12 12 12 13 32 6 13 9 11 36 5 | 25 31 22 30 37 27 31 24 26 24 24 17 | 12 18 14 15 26 6 18 13 11 19 5 | 21 33 22 32 26 25 32 25 29 25 24 18 | 11 17 14 17 34 6 19 13 9 24 5 | 15 37 25 28 35 21 32 20 19 23 21 19 | 11 23 14 15 24 6 16 11 10 17 5 | 20 43 20 26 38 23 34 20 21 19 22 20 | 10 18 13 20 52 6 18 10 9 17 5 | 18 31 25 21 42 19 25 21 13 17 16 21 | 11 23 11 12 33 8 17 13 12 21 5 | 18 42 21 26 35 21 35 20 26 26 23 22 | 13 15 14 20 61 6 18 15 8 17 5 | 17 30 21 25 48 18 29 25 17 20 19 23 | 11 22 16 12 37 4 17 11 9 17 5 | 8 31 18 21 32 16 28 13 17 19 15 24 | 9 17 7 17 32 7 10 10 8 24 4 | 19 33 22 27 28 21 32 19 21 30 22 25 | 8 13 6 12 22 4 10 8 7 14 3 | 12 22 16 17 28 14 20 16 15 20 14 26 | 9 13 7 14 29 3 10 10 9 23 4 | 21 35 27 28 37 25 32 23 26 29 25 27 | 9 15 6 12 20 3 9 9 8 12 3 | 12 27 18 19 25 16 22 17 17 19 16 28 | 9 15 12 15 30 6 16 10 11 38 5 | 23 31 23 26 29 21 26 24 23 37 22 29 | 8 18 14 16 25 7 17 11 12 20 5 | 27 40 26 39 52 32 40 27 29 36 30 30 | 9 10 6 13 51 5 7 7 5 26 3 | 27 29 32 29 65 28 31 29 30 26 27 31 | 10 18 11 17 40 6 13 11 8 19 5 | 15 28 18 25 40 18 27 20 16 21 18 32 | 8 11 14 8 33 5 14 5 6 16 3 | 10 20 22 12 25 13 22 14 15 13 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 16 11 14 34 5 14 11 9 23 |T 17 30 22 24 35 21 27 20 21 24 20 WRMS | 10 16 11 14 30 5 14 10 8 21 |NE 17 30 22 24 35 20 27 20 21 23 20 MEDI | 10 15 11 13 32 6 14 10 9 21 |MD 17 31 22 25 35 21 27 20 20 24 19 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 4.1500 GPS week: 1500 MJD: 54744.0-54750.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3063 |U 8 9 22 |U 0 0 0 |U 8 8 14 | emr | emr 2946 | 9 12 25 | 0 0 0 | 11 10 21 | esa | esa 2976 | 8 9 23 |U 0 0 0 | 8 7 15 | gfz | gfz 2968 |U 9 10 26 |U 0 0 0 | 11 10 19 | igr | igr 2972 | 8 9 23 | 0 0 0 | 8 7 15 | igs | igs 3003 | 8 9 23 | 0 0 0 | 8 9 15 | jpl | jpl 2879 |U 9 10 26 |U 0 0 0 |U 10 7 19 | mit | mit 3058 |U 8 10 26 |U 0 0 0 |U 14 13 20 | 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 5.1500.0 GPS week: 1500 Day: 0 MJD: 54744.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3072 | 6 7 24 | ---- ---- ---- | 10 7 14 | emr | emr 2880 | 10 9 29 | ---- ---- ---- | 13 9 26 | esa | esa 2976 | 6 7 25 | ---- ---- ---- | 10 7 14 | gfz | gfz 2968 | 8 8 31 | ---- ---- ---- | 13 9 20 | igr | igr 2976 | 7 7 27 | ---- ---- ---- | 11 6 16 | igs | igs 3059 | 8 7 26 | ---- ---- ---- | 11 16 19 | jpl | jpl 2879 | 8 7 27 | ---- ---- ---- | 13 8 22 | mit | mit 3072 | 7 6 25 | ---- ---- ---- | 10 7 17 | Table 5.1500.1 GPS week: 1500 Day: 1 MJD: 54745.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3072 | 6 10 22 | ---- ---- ---- | 7 8 15 | emr | emr 2880 | 9 17 28 | ---- ---- ---- | 10 10 26 | esa | esa 2976 | 6 10 21 | ---- ---- ---- | 8 6 16 | gfz | gfz 2976 | 7 14 26 | ---- ---- ---- | 9 7 22 | igr | igr 2976 | 7 11 23 | ---- ---- ---- | 8 6 17 | igs | igs 2965 | 6 11 23 | ---- ---- ---- | 8 7 17 | jpl | jpl 2784 | 9 13 29 | ---- ---- ---- | 9 6 21 | mit | mit 3072 | 6 9 24 | ---- ---- ---- | 8 8 20 | Table 5.1500.2 GPS week: 1500 Day: 2 MJD: 54746.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3039 | 9 9 21 | ---- ---- ---- | 8 10 13 | emr | emr 2970 | 10 11 23 | ---- ---- ---- | 12 11 22 | esa | esa 2976 | 8 8 21 | ---- ---- ---- | 8 8 13 | gfz | gfz 2971 | 9 11 26 | ---- ---- ---- | 11 9 15 | igr | igr 2970 | 9 8 21 | ---- ---- ---- | 10 9 16 | igs | igs 3024 | 8 8 21 | ---- ---- ---- | 9 9 15 | jpl | jpl 2784 | 10 10 24 | ---- ---- ---- | 11 8 21 | mit | mit 3072 | 8 7 21 | ---- ---- ---- | 10 9 19 | Table 5.1500.3 GPS week: 1500 Day: 3 MJD: 54747.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3056 | 12 15 30 | ---- ---- ---- | 10 11 12 | emr | emr 2964 | 13 15 31 | ---- ---- ---- | 11 11 18 | esa | esa 2976 | 12 15 33 | ---- ---- ---- | ---- ---- ---- | gfz | gfz 2944 | 13 14 33 | ---- ---- ---- | 11 13 19 | igr | igr 2959 | 12 13 31 | ---- ---- ---- | 8 8 14 | igs | igs 3047 | 11 14 32 | ---- ---- ---- | 9 11 12 | jpl | jpl 2783 | 13 15 36 | ---- ---- ---- | 9 9 17 | mit | mit 3072 | 13 19 42 | ---- ---- ---- | ---- ---- ---- | Table 5.1500.4 GPS week: 1500 Day: 4 MJD: 54748.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3067 | 8 11 20 | ---- ---- ---- | 8 6 12 | emr | emr 2976 | 8 13 20 | ---- ---- ---- | 10 9 19 | esa | esa 2976 | 7 8 20 | ---- ---- ---- | 8 6 14 | gfz | gfz 2972 | 8 9 21 | ---- ---- ---- | 12 9 20 | igr | igr 2976 | 7 9 19 | ---- ---- ---- | 8 6 13 | igs | igs 2976 | 7 10 20 | ---- ---- ---- | 9 6 14 | jpl | jpl 2976 | 9 9 22 | ---- ---- ---- | 9 5 17 | mit | mit 2976 | 8 15 28 | ---- ---- ---- | 8 6 17 | Table 5.1500.5 GPS week: 1500 Day: 5 MJD: 54749.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3069 | 7 6 18 | ---- ---- ---- | 7 7 11 | emr | emr 2976 | 8 12 18 | ---- ---- ---- | 8 9 17 | esa | esa 2976 | 7 6 19 | ---- ---- ---- | 8 8 13 | gfz | gfz 2974 | 8 9 18 | ---- ---- ---- | 10 12 16 | igr | igr 2976 | 7 7 18 | ---- ---- ---- | 7 7 11 | igs | igs 2976 | 6 7 17 | ---- ---- ---- | 7 7 11 | jpl | jpl 2976 | 8 10 20 | ---- ---- ---- | 9 8 15 | mit | mit 3072 | 8 7 21 | ---- ---- ---- | 13 10 17 | Table 5.1500.6 GPS week: 1500 Day: 6 MJD: 54750.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3072 | 7 5 18 | ---- ---- ---- | 7 10 19 | emr | emr 2976 | 8 6 22 | ---- ---- ---- | 10 9 20 | esa | esa 2976 | 8 6 23 | ---- ---- ---- | 7 9 17 | gfz | gfz 2972 | 8 5 23 | ---- ---- ---- | 10 11 21 | igr | igr 2976 | 8 5 23 | ---- ---- ---- | 7 8 17 | igs | igs 2976 | 7 5 20 | ---- ---- ---- | 7 8 17 | jpl | jpl 2976 | 9 6 24 | ---- ---- ---- | 8 10 22 | mit | mit 3072 | 6 5 19 | ---- ---- ---- | 35 39 33 | 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 6.1500 GPS week: 1500 MJD: 54744.500-54750.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -15 -7 -40 10 6 | 9 13 | 21 18 73 89 6 | 4 emr uuuuu | -16 24 156 41 6 | 62 62 | 17 17 76 70 5 | 2 esa uuuuu | 11 -31 154 -9 1 | 26 28 | 14 23 91 84 9 | 1 gfz uuuuu | 6 -1 -47 25 -2 | 12 14 | 12 13 26 56 4 | 1 grg xxxxx | -13 -3 -21 -2 10 | -4 15 | 18 40 68 64 42 | 4 igr xxxxx | -24 34 1 38 -1 | 3 10 | 20 18 38 64 5 | 1 irf xxxxx | 7 -4 -13 25 -3 | 1 10 | 7 9 42 29 6 | 1 jpl uuuuu | -5 37 -82 86 -2 | 15 20 | 11 30 78 168 7 | 2 mit uuuuu | 4 16 -68 -100 -6 | 19 22 | 23 21 79 64 5 | 1 ngs uuuuu | -17 -2 -46 -34 -3 | 5 13 | 30 39 91 52 6 | 1 sio uuuuu | 84 -34 -43 21 -2 | 49 50 | 27 29 59 58 8 | 1 Table 7.1500.0 GPS week: 1500 Day: 0 MJD: 54744.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -3 -13 -101 44 6 | 4 10 emr uuuuu | -39 15 214 -89 -3 | 60 60 esa uuuuu | 9 -13 59 -35 -12 | 29 29 gfz uuuuu | 29 23 -72 -18 -6 | 14 16 grg xxxxx | -26 -6 74 13 -9 | 2 15 igr xxxxx | -27 59 24 21 -4 | 3 8 irf xxxxx | 14 -1 -94 26 -12 | 3 9 jpl uuuuu | -23 94 -110 183 10 | 12 17 mit uuuuu | -8 32 -211 -120 -12 | 20 22 ngs uuuuu | -31 -59 148 -55 -3 | 7 11 sio uuuuu | 120 -62 -31 28 -16 | 51 52 Table 7.1500.1 GPS week: 1500 Day: 1 MJD: 54745.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -49 4 -23 -40 17 | 5 11 emr uuuuu | 4 21 288 72 12 | 59 59 esa uuuuu | 19 -25 197 -21 -6 | 27 28 gfz uuuuu | -1 -10 -76 -32 1 | 12 14 grg xxxxx | -27 -12 -92 -89 -10 | 1 16 igr xxxxx | -20 45 19 72 -9 | 3 8 irf xxxxx | 3 -2 -30 -10 -6 | 2 9 jpl uuuuu | 1 48 -160 202 -2 | 14 18 mit uuuuu | 9 19 -100 -130 -8 | 19 21 ngs uuuuu | 1 -11 -92 -7 -14 | 6 11 sio uuuuu | 92 -48 -26 13 -7 | 49 50 Table 7.1500.2 GPS week: 1500 Day: 2 MJD: 54746.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -19 -16 29 -122 10 | 7 11 emr uuuuu | -20 39 69 101 7 | 59 60 esa uuuuu | -12 -51 203 175 -2 | 25 27 gfz uuuuu | -7 -6 -16 39 -3 | 11 13 grg xxxxx | -21 -2 27 64 -4 | -2 17 igr xxxxx | -53 25 3 20 5 | 1 10 irf xxxxx | 3 -19 -20 12 -6 | 1 10 jpl uuuuu | 1 11 -131 240 -8 | 14 18 mit uuuuu | -24 1 -59 -210 -10 | 18 21 ngs uuuuu | 22 59 -127 -110 -3 | 4 13 sio uuuuu | 112 -58 -10 -91 -7 | 47 49 Table 7.1500.3 GPS week: 1500 Day: 3 MJD: 54747.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -30 2 -2 67 3 | 10 13 emr uuuuu | 6 31 143 80 5 | 61 62 esa uuuuu | 21 -31 6 -3 -5 | 26 27 gfz uuuuu | 12 -14 -26 -39 -4 | 12 14 grg xxxxx | -17 41 -32 -50 -27 | -5 12 igr xxxxx | 12 4 52 -88 0 | 3 11 irf xxxxx | 11 -12 34 -3 -5 | 1 10 jpl uuuuu | 10 38 33 -144 3 | 16 19 mit uuuuu | 36 -20 47 -47 -10 | 19 22 ngs uuuuu | -52 20 -96 22 4 | 5 13 sio uuuuu | 63 -37 -41 59 -2 | 48 49 Table 7.1500.4 GPS week: 1500 Day: 4 MJD: 54748.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 5 -41 -69 -55 8 | 12 16 emr uuuuu | -26 51 150 102 9 | 64 65 esa uuuuu | 2 -19 171 -54 11 | 26 28 gfz uuuuu | -4 12 -25 99 1 | 12 16 grg xxxxx | 19 9 1 82 -3 | -7 13 igr xxxxx | -38 48 -68 79 5 | 5 13 irf xxxxx | 0 -1 1 68 2 | 2 11 jpl uuuuu | -13 34 -103 231 -9 | 19 22 mit uuuuu | -22 19 -36 -66 -1 | 20 23 ngs uuuuu | 16 3 -39 -75 -7 | 7 15 sio uuuuu | 67 -44 -67 -6 6 | 50 51 Table 7.1500.5 GPS week: 1500 Day: 5 MJD: 54749.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -17 10 42 148 4 | 12 16 emr uuuuu | -12 -1 81 -7 6 | 63 64 esa uuuuu | 31 -73 172 -48 9 | 25 27 gfz uuuuu | 5 -3 -72 43 -6 | 10 13 grg xxxxx | -26 30 -122 -50 22 | -9 14 igr xxxxx | -15 26 -21 51 2 | 4 12 irf xxxxx | 1 -3 -3 54 3 | 0 10 jpl uuuuu | -3 35 -126 -121 0 | 17 21 mit uuuuu | 14 15 -30 -14 0 | 18 21 ngs uuuuu | -34 11 -77 -43 0 | 4 14 sio uuuuu | 48 8 31 55 7 | 48 50 Table 7.1500.6 GPS week: 1500 Day: 6 MJD: 54750.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 10 3 -158 26 -3 | 14 16 emr uuuuu | -26 14 146 29 7 | 64 65 esa uuuuu | 8 -8 273 -76 11 | 26 28 gfz uuuuu | 6 -8 -41 84 2 | 10 13 grg xxxxx | 6 -83 -4 16 100 | -8 15 igr xxxxx | -25 28 2 111 -4 | 4 12 irf xxxxx | 15 11 21 31 1 | 1 10 jpl uuuuu | -8 -1 26 15 -7 | 17 21 mit uuuuu | 22 47 -87 -111 -3 | 18 21 ngs uuuuu | -44 -39 -37 32 1 | 3 14 sio uuuuu | 87 5 -157 87 1 | 50 51