Date: Thu, 06 Nov 2008 13:49:04 +0000 From: Jim Ray Subject: [IGSREPORT-16806] Wk 1502 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4912f5d0.3GttkB3Zg8+Z89B5%igs.acc@noaa.gov> Content-type: text/plain; charset=us-ascii Content-transfer-encoding: 7bit User-Agent: nail 11.25 7/29/05 Sender: owner-igsreport Precedence: bulk ****************************************************************************** IGS Electronic Report 06 Nov 05:49:07 PST 2008 Message Number 16806 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1502 (Oct 19, 2008 - Oct 25, 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: igs1502[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1502[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1502[0-6].cls IGS GPS clock combination summary report. igs15027.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15027.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 | EMR | 21 MIZU 0 | ESA | 19 NRIL 0 | GFZ | 7 11 21 BAN2 HARB TOW2 0 | JPL | ZWE2 0 | MIT | SANT TOW2 1 | COD | DAEJ DRAO 1 | EMR | DAEJ 1 | ESA | RAMO 1 | GFZ | 7 11 BAN2 1 | MIT | DAEJ 2 | COD | FAA1 2 | EMR | MIZU 2 | GFZ | 7 29 LHAZ 2 | JPL | 4 3 | COD | 4 TOW2 3 | EMR | MIZU 3 | GFZ | 4 7 11 29 DAV1 3 | JPL | 4 3 | MIT | TOW2 4 | COD | 4 TWTF 4 | EMR | DAEJ MIZU 4 | ESA | 4 29 PIMO RAMO TOW2 4 | GFZ | 2 7 11 29 DAEJ TWTF 4 | JPL | HARB TOW2 TWTF ZWE2 4 | MIT | DAEJ TOW2 YELL 5 | COD | 4 5 | EMR | MIZU 5 | ESA | 4 29 TOW2 5 | GFZ | 7 29 BAN2 DAV1 5 | JPL | 21 24 HARB ZWE2 5 | MIT | 14 19 24 TOW2 6 | COD | 4 BOR1 6 | EMR | HARB MIZU 6 | ESA | 4 29 6 | GFZ | 4 7 29 ALGO BAN2 DAV1 TOW2 6 | JPL | HARB 6 | MIT | 24 ALGO BOR1 TOW2 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 | .2 .3 .7 -13 -10 -7 -.15 EMR | 8.9 -5.0 3.8 132 62 133 .13 ESA | 4.0 2.5 10.8 24 -27 16 -.15 GFZ | .8 .7 1.6 12 -33 11 -.38 GRG | 4.1 2.9 -1.1 -17 -15 -6 -.12 JPL | .0 10.0 1.1 25 -2 27 -.06 MIT | 5.9 3.7 6.4 4 -8 -4 -.17 NGS | 6.5 -.5 1.2 4 -96 33 .03 SIO | 10.6 3.5 -2.0 66 -192 20 .18 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 1.1502.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1502.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 2.1502.[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 3.1502.[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 5.1502.0-6). 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 1502 summary. (Oct 19, 2008 - Oct 25, 2008) Table 1.1502.a GPS week: 1502 MJD: 54758.000-54764.000 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 240| 0 1 3 63 -44 -25 -.16 10 9 | -560 362 14 113 | 0 0 1 6 19 16 .03 | 453 503 emr 71| -1 -3 0 -235 -212 10 .47 16 16 | -2760 366 17 223 | 1 1 1 17 23 14 .04 | 2487 2195 esa 124| 0 -1 0 7 15 14 .26 11 11 | -1258 1713 21 117 | 0 1 1 15 19 18 .03 | 923 1751 gfz 196| 0 1 -1 27 7 -12 -.05 15 15 | 159 -140 23 131 | 0 0 1 12 18 44 .05 | 191 234 grg 83| 1 1 -1 93 -32 32 1.12 34 32 | -564 344 97 364 | 1 1 2 22 28 50 .04 | 454 503 igr n/a| 0 0 0 41 -58 -22 .05 5 5 | -34208 1188 23 75 | 0 0 0 10 6 11 .02 | 4483 2292 jpl 127| 0 0 -3 -4 -54 49 .52 15 14 | -896 416 20 107 | 0 1 1 14 10 23 .04 | 2733 2135 mit 252| 0 1 0 70 -44 8 -.36 13 12 | -75 -43 20 141 | 0 1 0 28 42 16 .01 | 353 472 ngs 234| 0 0 -1 22 136 -30 -.38 11 9 | -574 357 2345 3940 | 0 0 0 29 48 21 .04 | 440 486 sio 108| 0 0 0 -76 334 -19 .06 24 23 | --- --- --- --- | 0 1 1 20 24 12 .04 | --- --- Table 1.1502.b GPS week : 1502 MJD: 54758.000-54764.000 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 | --- --- --- --- 0 0 0 | 2 | 5 5 5 5 5 5 5 | 3 | 5 5 5 5 4 4 4 | 4 | 6 7 7 6 6 6 8 | 5 | 5 4 5 4 5 4 5 | 6 | 4 4 5 4 4 4 4 | 7 | 5 5 5 5 5 5 5 | 8 | 4 5 4 5 5 5 5 | 9 | 5 5 5 5 5 6 6 | 10 | 3 4 4 4 4 4 4 | 11 | 6 5 5 5 5 5 5 | 12 | 5 5 5 5 5 5 5 | 13 | 5 5 5 5 5 5 5 | 14 | 6 6 6 5 5 5 5 | 15 | 5 6 5 5 6 6 6 | 16 | 5 5 5 5 5 6 6 | 17 | 6 6 6 6 6 6 6 | 18 | 7 6 6 6 6 5 6 | 19 | 6 6 6 6 6 6 6 | 20 | 6 6 6 6 5 6 6 | 21 | 5 6 5 5 6 5 5 | 22 | 7 6 6 6 6 6 6 | 23 | 6 6 6 6 6 6 6 | 24 | 6 6 6 6 6 6 7 | 25 | 4 5 5 5 5 5 5 | 26 | 4 4 4 4 5 4 5 | 27 | 5 5 5 6 5 5 5 | 28 | 6 6 6 6 6 6 6 | 29 | 6 6 6 6 7 6 6 | 30 | 4 4 4 4 5 5 5 | 31 | 6 5 5 5 5 5 5 | 32 | 5 5 5 5 5 5 5 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1502.0 GPS week: 1502 Day: 0 MJD: 54758.000 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 240| 0 1 4 56 -46 -25 -.17 11 10 | -131 254 15 133 | -6 30 | emr 71| 0 -2 0 -247 -189 3 .49 17 17 | -5442 -216 18 233 | -2 54 | esa 124| 0 0 0 30 0 -12 .22 11 12 | -984 675 23 120 | 0 7 | gfz 196| 0 0 -2 45 4 51 -.09 14 14 | 174 -215 26 147 | -1 19 | grg 83| 0 2 -2 122 -12 -43 1.09 32 31 | -147 256 91 386 | -21 84 | igr n/a| 0 0 0 53 -51 -35 .07 5 5 | -39498 285 24 80 | -35 23 | jpl 127| -1 -2 -4 -8 -52 29 .53 16 16 | -3845 -281 24 124 | -25 -24 | mit 252| 1 1 1 36 -24 14 -.34 12 11 | -52 -367 19 129 | -10 -15 | ngs 234| 0 0 -1 18 124 -50 -.33 11 9 | -183 310 2720 4225 | 0 11 | sio 108| 0 -1 2 -75 354 -8 .04 24 22 | --- --- --- --- | 34 -186 | Table 2.1502.1 GPS week: 1502 Day: 1 MJD: 54759.000 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 240| 0 0 4 63 -44 -5 -.14 10 10 | -1084 843 13 116 | 13 39 | emr 71| 0 -4 -1 -243 -216 35 .51 17 17 | -4816 117 18 245 | -20 89 | esa 124| 1 0 0 12 6 5 .26 12 12 | -1815 2111 20 104 | 37 24 | gfz 196| 0 0 -1 34 0 -35 -.11 15 15 | 226 -383 23 142 | -8 46 | grg 83| 2 2 -1 124 14 52 1.08 36 33 | -1096 837 96 396 | 16 105 | igr n/a| 0 0 0 45 -57 -37 .06 5 5 | -38449 1135 22 62 | -43 51 | jpl 127| 0 -1 -5 -10 -60 50 .55 15 15 | -3320 260 21 105 | -39 37 | mit 252| 0 2 0 70 -6 29 -.36 12 12 | -133 -206 23 125 | -20 -18 | ngs 234| -1 0 -1 11 94 -43 -.35 11 8 | -1096 837 2169 3807 | 32 42 | sio 108| 0 -2 1 -58 368 -27 .00 24 24 | --- --- --- --- | 21 -187 | Table 2.1502.2 GPS week: 1502 Day: 2 MJD: 54760.000 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 240| 0 1 3 56 -73 -27 -.12 10 9 | -577 373 14 74 | 19 41 | emr 71| 0 -5 1 -264 -194 -5 .47 17 17 | -4853 1786 19 171 | 48 45 | esa 124| 1 -1 -1 21 -9 39 .26 12 12 | 158 -937 20 114 | 24 10 | gfz 196| 0 0 -3 34 2 -6 .03 15 15 | -132 283 22 122 | 2 13 | grg 83| 0 3 -2 68 -25 26 1.12 36 33 | -594 373 104 365 | 47 76 | igr n/a| 1 0 -1 23 -51 -22 .05 5 5 | -37547 2911 22 78 | -10 34 | jpl 127| -1 1 -2 -12 -37 97 .57 16 15 | -3055 1814 17 99 | 7 -74 | mit 252| 0 2 0 110 -26 10 -.36 12 10 | -600 634 21 119 | -28 -30 | ngs 234| 1 0 0 -17 131 -58 -.36 11 9 | -594 373 2338 3698 | 65 17 | sio 108| 0 0 0 -53 339 -39 .07 23 24 | --- --- --- --- | 32 -162 | Table 2.1502.3 GPS week: 1502 Day: 3 MJD: 54761.000 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 240| 1 1 2 59 -47 -22 -.11 10 9 | 204 -558 15 107 | -18 18 | emr 71| -4 -2 -3 -230 -188 9 .49 16 16 | -2960 3542 19 196 | -9 38 | esa 124| 1 -1 0 9 39 25 .28 10 11 | -2108 4205 23 133 | 55 -22 | gfz 196| 1 2 2 13 1 -43 -.08 15 15 | 313 -31 24 125 | -2 16 | grg 83| 0 1 -2 68 -67 -8 1.17 36 35 | 209 -582 100 293 | 13 20 | igr n/a| 0 0 0 50 -52 -11 .03 6 5 | -34514 4581 21 69 | -29 39 | jpl 127| 0 0 -3 20 -70 51 .52 15 14 | -1265 3491 22 114 | 8 59 | mit 252| 0 1 0 60 -103 15 -.37 11 11 | -34 425 18 117 | -20 18 | ngs 234| -1 0 0 33 203 -19 -.47 13 10 | 178 -535 2428 4309 | -3 -52 | sio 108| 1 0 -1 -103 303 -20 .05 24 23 | --- --- --- --- | 42 -171 | Table 2.1502.4 GPS week: 1502 Day: 4 MJD: 54762.000 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 240| 0 1 2 70 -56 -6 -.16 10 9 | -707 128 13 117 | -9 53 | emr 71| -3 -5 0 -226 -215 22 .49 15 15 | -780 32 16 243 | -6 39 | esa 124| 1 -1 1 -12 12 4 .22 10 10 | -1077 1076 20 108 | 25 -48 | gfz 196| 0 1 -1 17 19 -77 -.04 14 14 | 79 -155 21 125 | 26 5 | grg 83| 2 2 -1 93 -62 26 1.09 34 31 | -711 104 92 339 | -26 -20 | igr n/a| 0 0 0 35 -62 -15 .08 5 5 | -31201 1189 21 67 | -10 35 | jpl 127| 0 0 -2 0 -55 27 .47 14 13 | 1142 425 20 99 | 0 7 | mit 252| 1 1 0 75 -57 14 -.38 13 12 | 44 -256 17 150 | -15 -10 | ngs 234| -1 0 -1 30 160 1 -.38 11 9 | -723 108 2112 3689 | -1 -59 | sio 108| 1 2 -1 -71 307 -2 .08 24 21 | --- --- --- --- | 30 -154 | Table 2.1502.5 GPS week: 1502 Day: 5 MJD: 54763.000 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 240| 1 1 1 72 -15 -51 -.20 10 9 | -667 553 16 125 | -20 -26 | emr 71| -2 -3 0 -220 -250 5 .40 15 15 | 1282 -3631 19 250 | -6 89 | esa 124| 1 0 2 -9 41 30 .26 10 9 | -524 1316 20 126 | 48 -16 | gfz 196| 0 0 0 15 -19 -5 -.03 15 15 | 442 -404 25 134 | 9 20 | grg 83| 1 0 3 88 -32 112 1.13 32 29 | -660 510 98 454 | -71 -18 | igr n/a| 0 0 -1 43 -68 -11 .04 5 5 | -27971 -2838 29 113 | 5 34 | jpl 127| 0 0 -1 3 -53 46 .46 14 13 | 3472 -3504 20 100 | 1 47 | mit 252| 0 0 0 37 -96 0 -.36 14 13 | 556 -707 24 198 | 4 4 | ngs 234| -1 0 -2 76 178 -28 -.41 11 9 | -648 495 2478 3897 | -115 -22 | sio 108| 0 1 -1 -104 323 -11 .06 25 20 | --- --- --- --- | 21 -175 | Table 2.1502.6 GPS week: 1502 Day: 6 MJD: 54764.000 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 240| 1 0 1 67 -24 -36 -.20 10 9 | -959 945 12 120 | 8 16 | emr 71| -1 -2 1 -212 -233 -1 .45 15 15 | -1751 934 15 228 | -24 65 | esa 124| 0 -2 0 2 18 8 .30 13 12 | -2456 3549 21 114 | 43 -17 | gfz 196| 0 1 -1 34 40 29 -.05 15 15 | 15 -76 24 127 | -12 2 | grg 83| 3 -1 0 89 -41 63 1.19 34 33 | -954 916 98 318 | 112 141 | igr n/a| 0 0 1 37 -62 -27 .05 5 5 | -30276 1053 22 62 | 14 4 | jpl 127| 0 0 0 -24 -48 45 .53 15 14 | 595 711 20 113 | 44 14 | mit 252| 1 0 0 99 2 -24 -.35 16 15 | -311 171 21 150 | -13 -37 | ngs 234| -1 0 0 2 62 -11 -.37 10 7 | -957 915 2170 3961 | -57 65 | sio 108| 0 1 -2 -69 346 -25 .14 28 25 | --- --- --- --- | 58 -145 | 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 3.1502.0 GPS week: 1502 Day: 0 MJD: 54758.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 11 20 9 10 40 4 19 15 9 16 5 | 20 32 19 25 41 --- 27 16 25 29 21 3 | 14 15 9 10 32 4 14 10 11 26 5 | 18 27 26 23 24 --- 25 18 26 34 23 4E | 14 18 10 15 30 4 15 11 17 36 6 | 55 59 56 61 63 --- 59 53 63 43 56 5 | 8 11 7 12 23 7 7 18 11 25 4 | 17 28 25 24 32 --- 28 27 24 17 22 6 | 8 15 11 9 35 5 15 8 9 23 4 | 15 26 24 22 21 --- 25 19 19 25 19 7 | 10 15 11 15 30 6 14 12 8 20 4 | 16 30 20 26 40 --- 27 15 16 16 18 8 | 10 11 6 12 18 5 10 8 7 24 4 | 9 19 10 17 26 --- 17 11 12 24 10 9 | 10 16 10 11 20 5 11 9 9 23 4 | 29 39 27 33 40 --- 35 28 29 38 29 10 | 6 9 7 8 15 4 7 9 7 18 3 | 25 28 26 23 31 --- 26 28 26 19 23 11E | 12 20 12 13 35 4 19 13 15 14 5 | 52 67 56 56 54 --- 60 50 55 63 55 12 | 7 9 9 13 29 6 14 16 13 35 5 | 20 32 26 25 37 --- 27 24 25 26 23 13 | 12 16 11 14 35 4 18 13 9 11 5 | 13 32 20 25 48 --- 31 14 20 16 18 14 | 8 15 14 16 25 5 22 14 10 15 5 | 15 30 16 25 38 --- 28 18 19 15 17 15 | 10 12 11 15 18 5 17 9 11 25 5 | 12 22 15 21 31 --- 23 12 16 18 12 16 | 10 13 11 14 41 5 15 10 11 35 5 | 19 27 22 26 25 --- 25 21 19 17 20 17 | 12 19 11 20 26 6 18 13 13 25 6 | 12 32 14 30 37 --- 29 15 17 20 16 18 | 12 22 16 16 28 4 25 20 13 20 6 | 23 38 28 31 39 --- 33 25 26 23 24 19 | 11 24 16 17 34 5 18 13 12 21 6 | 17 39 17 30 38 --- 34 15 16 21 20 20 | 12 23 15 19 45 4 22 11 11 19 6 | 22 33 26 25 46 --- 30 25 19 24 21 21E | 10 19 14 10 44 5 19 14 12 16 5 | 24 37 24 30 38 --- 35 28 29 32 27 22 | 8 24 15 20 39 5 24 16 11 20 6 | 21 40 29 27 35 --- 28 26 24 24 22 23 | 11 27 16 12 34 4 21 11 11 18 6 | 12 39 22 25 44 --- 33 15 21 23 19 24 | 21 16 8 18 36 5 13 16 11 29 6 | 51 60 52 57 69 --- 57 62 58 61 55 25 | 9 13 8 12 35 5 13 12 11 17 4 | 15 26 15 19 34 --- 26 16 13 26 15 26 | 9 14 8 12 19 4 9 9 8 18 4 | 13 27 19 20 28 --- 23 17 19 16 15 27 | 14 14 7 11 16 4 12 7 10 20 4 | 39 49 39 44 51 --- 46 44 43 40 41 28 | 10 12 9 13 53 8 14 12 12 42 5 | 27 35 29 28 37 --- 32 31 29 42 27 29 | 11 17 14 18 41 6 19 12 17 20 5 | 17 30 16 31 47 --- 24 17 20 19 19 30 | 8 15 7 14 28 5 7 9 9 27 4 | 31 35 38 36 31 --- 35 36 36 28 34 31 | 10 20 14 15 38 4 14 9 15 18 5 | 14 25 13 22 43 --- 21 13 17 18 13 32 | 9 19 10 9 24 5 16 10 13 32 5 | 29 38 34 31 40 --- 35 28 36 53 31 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 17 11 14 32 5 16 12 11 24 |T 22 34 25 29 38 --- 31 24 26 28 24 WRMS | 10 17 12 14 31 5 16 11 9 22 |NE 19 31 22 26 36 --- 28 21 22 24 21 MEDI | 10 16 11 13 32 5 15 12 11 20 |MD 19 32 24 26 38 --- 28 21 24 24 21 Table 3.1502.1 GPS week: 1502 Day: 1 MJD: 54759.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 9 20 12 12 33 3 17 16 10 18 5 | 21 34 23 28 46 --- 29 22 30 28 24 3 | 8 15 10 9 33 4 13 10 8 28 4 | 19 30 23 20 23 --- 25 24 23 22 20 4E | 11 21 14 14 43 7 17 16 22 31 6 | 32 42 34 39 39 --- 39 36 41 42 34 5 | 7 11 7 13 44 4 10 9 9 24 4 | 13 23 19 23 34 --- 21 18 20 17 17 6 | 8 13 11 9 29 4 12 10 7 26 4 | 13 24 20 19 21 --- 21 21 16 18 15 7 | 9 19 12 15 30 5 15 15 10 22 5 | 14 31 20 25 43 --- 26 16 19 19 17 8 | 9 13 7 12 20 5 11 11 10 26 4 | 14 25 16 18 22 --- 18 15 18 26 14 9 | 9 17 6 12 21 4 13 12 11 23 4 | 31 41 31 32 37 --- 38 31 36 41 33 10 | 7 11 9 6 44 4 10 8 9 24 3 | 25 28 28 24 30 --- 24 26 28 30 25 11E | 10 17 14 12 24 6 17 14 9 13 5 | 52 60 55 54 50 --- 55 53 51 55 53 12 | 7 12 6 12 32 6 14 9 12 33 4 | 14 28 18 22 28 --- 24 16 20 23 17 13 | 10 19 12 16 31 3 16 13 9 10 5 | 11 34 17 23 45 --- 29 16 17 17 16 14 | 8 18 11 20 35 6 18 14 13 17 5 | 16 29 17 25 34 --- 26 16 20 16 16 15 | 13 20 14 16 24 4 17 11 10 24 5 | 15 31 18 22 32 --- 26 14 16 23 16 16 | 9 13 11 12 37 5 13 9 9 36 5 | 12 23 18 22 26 --- 21 16 13 14 14 17 | 12 17 15 19 30 5 17 13 11 22 5 | 17 33 20 32 33 --- 32 22 24 26 21 18 | 9 20 15 17 33 5 21 17 10 22 6 | 19 35 25 29 34 --- 31 21 22 22 21 19 | 10 22 14 21 36 5 20 12 11 20 6 | 14 35 15 27 40 --- 30 15 10 18 15 20 | 12 19 13 20 41 5 19 14 7 16 5 | 18 35 22 25 34 --- 30 19 15 18 18 21E | 12 21 15 10 47 6 19 11 11 17 5 | 21 32 19 23 42 --- 30 21 28 26 21 22 | 8 17 16 20 56 5 18 13 9 17 5 | 16 31 23 27 44 --- 27 18 19 19 17 23 | 11 24 15 15 29 6 19 11 14 16 5 | 11 38 19 22 38 --- 29 14 16 19 16 24E | 17 19 8 19 43 7 12 19 13 25 6 | 73 83 76 81 90 --- 78 80 82 80 77 25 | 10 13 11 14 38 4 10 11 12 20 4 | 16 26 20 23 42 --- 26 17 18 28 17 26 | 8 12 9 11 26 3 8 11 7 21 4 | 18 28 19 19 27 --- 22 16 19 20 17 27 | 13 13 8 12 16 5 12 8 9 20 4 | 56 60 58 62 69 --- 62 58 61 62 58 28 | 8 12 9 11 66 7 14 12 12 41 5 | 18 30 21 23 43 --- 29 23 16 37 19 29 | 10 19 13 19 48 5 18 12 13 19 5 | 15 30 15 27 44 --- 25 16 15 17 15 30 | 8 15 7 17 31 5 11 8 9 21 4 | 38 41 44 43 37 --- 42 39 42 38 40 31 | 7 19 17 17 35 6 13 11 10 19 5 | 13 29 17 23 38 --- 23 15 14 19 15 32 | 9 16 10 11 29 4 12 8 5 31 4 | 19 26 20 18 30 --- 20 20 16 41 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 17 12 15 36 5 15 12 11 24 |T 22 34 25 29 38 --- 30 24 25 28 23 WRMS | 10 17 12 15 33 5 15 12 8 24 |NE 18 31 22 25 35 --- 27 20 21 25 20 MEDI | 9 17 11 14 33 5 14 11 10 22 |MD 17 31 20 24 37 --- 27 19 19 23 17 Table 3.1502.2 GPS week: 1502 Day: 2 MJD: 54760.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 10 21 12 13 47 3 16 14 12 16 5 | 19 30 22 24 43 --- 28 20 23 25 22 3 | 10 15 11 9 34 2 14 9 13 26 4 | 16 24 23 20 27 --- 20 22 27 23 19 4E | 12 19 20 13 69 6 17 14 21 22 6 | 28 37 39 32 59 --- 40 28 39 40 33 5 | 9 13 11 11 19 7 10 10 9 28 4 | 18 23 24 24 31 --- 24 20 19 22 19 6 | 8 13 11 10 28 4 14 10 11 22 4 | 11 24 20 15 23 --- 19 18 19 23 15 7 | 10 19 12 15 32 7 16 11 8 17 5 | 13 29 17 23 41 --- 26 12 13 14 14 8 | 9 12 6 12 18 5 14 10 7 24 4 | 9 20 11 17 23 --- 19 11 13 24 10 9 | 10 18 10 12 17 4 14 10 9 21 4 | 18 34 25 23 29 --- 30 21 24 31 23 10 | 8 11 6 6 38 5 13 9 9 18 3 | 23 28 21 21 22 --- 24 24 27 21 22 11E | 11 18 11 14 63 7 20 12 12 12 5 | 33 38 34 35 82 --- 37 35 33 31 30 12 | 7 11 7 13 22 6 10 9 10 34 4 | 18 27 22 23 33 --- 24 18 20 25 19 13 | 9 18 11 14 36 6 17 13 8 11 4 | 13 30 17 24 49 --- 29 17 16 18 16 14 | 9 17 16 21 32 6 19 12 10 13 5 | 12 26 22 28 35 --- 25 14 17 18 15 15 | 10 17 13 14 28 5 17 13 12 20 5 | 13 26 18 23 32 --- 24 13 20 17 15 16 | 10 14 13 11 30 6 14 9 9 35 5 | 16 23 17 20 24 --- 21 17 14 15 14 17 | 12 17 13 20 32 5 18 10 10 24 5 | 11 32 17 27 33 --- 34 14 16 14 16 18 | 8 19 13 18 33 7 21 15 9 20 5 | 17 34 24 29 34 --- 32 20 21 22 21 19 | 10 19 17 20 26 6 22 13 11 19 6 | 18 35 17 29 34 --- 34 14 19 19 19 20 | 11 19 14 19 57 6 17 13 10 17 5 | 20 35 29 25 40 --- 30 23 18 22 21 21E | 10 17 14 13 29 5 20 12 11 17 5 | 25 31 23 30 42 --- 31 26 29 31 25 22 | 7 14 18 23 39 6 23 11 12 17 5 | 20 30 27 28 38 --- 30 20 24 21 21 23 | 10 22 13 14 34 5 21 12 9 17 5 | 12 35 18 23 37 --- 30 16 17 23 17 24E | 14 23 11 17 33 7 16 17 14 25 6 | 48 51 46 54 59 --- 50 56 56 53 49 25 | 10 15 9 17 29 5 12 13 9 20 4 | 15 23 18 21 37 --- 27 15 13 28 15 26 | 8 13 10 12 25 4 11 12 10 16 4 | 12 24 16 17 28 --- 22 14 18 13 13 27 | 11 14 7 12 22 4 14 10 9 20 4 | 36 40 39 41 44 --- 41 37 32 33 35 28 | 7 11 10 12 55 6 13 10 10 44 5 | 22 32 28 24 33 --- 31 26 22 36 24 29 | 10 18 14 21 30 5 17 15 13 20 5 | 15 30 15 28 37 --- 23 17 19 17 17 30 | 7 13 6 15 22 5 9 9 7 23 4 | 30 32 33 31 35 --- 32 34 36 35 31 31 | 9 17 13 16 39 7 13 8 10 21 4 | 14 25 16 21 38 --- 24 14 17 23 15 32 | 7 17 10 9 31 5 15 7 10 32 4 | 19 26 24 19 25 --- 22 20 20 42 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 17 12 15 36 5 16 12 11 23 |T 19 30 23 25 37 --- 28 21 22 25 20 WRMS | 9 17 12 15 33 5 15 10 9 24 |NE 16 28 21 24 33 --- 26 18 20 23 18 MEDI | 10 17 11 14 32 5 16 11 10 20 |MD 18 30 22 24 35 --- 28 20 20 23 19 Table 3.1502.3 GPS week: 1502 Day: 3 MJD: 54761.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 9 18 11 13 56 5 16 14 11 15 5 | 20 30 21 24 53 --- 27 15 27 23 21 3 | 8 13 10 12 37 5 9 8 13 28 4 | 17 26 22 18 27 --- 24 16 26 32 20 4E | 13 18 11 15 57 7 15 15 24 21 6 | 44 48 51 44 76 --- 46 47 54 49 46 5 | 6 12 7 12 25 5 9 8 10 27 4 | 18 25 20 22 31 --- 25 21 18 19 19 6 | 6 13 10 11 33 6 9 9 12 19 4 | 15 23 21 18 24 --- 23 18 18 22 16 7 | 9 21 12 14 35 7 13 12 10 17 5 | 19 34 19 27 40 --- 26 17 23 17 19 8 | 10 13 8 14 18 3 10 10 9 27 4 | 17 24 18 23 25 --- 20 17 19 30 16 9 | 10 20 9 11 19 6 13 11 13 22 5 | 28 42 30 35 37 --- 35 31 37 38 32 10 | 8 9 5 8 31 4 9 8 8 20 3 | 17 24 18 19 23 --- 18 18 25 13 18 11E | 12 14 12 14 31 5 20 10 13 17 5 | 77 81 80 81 91 --- 82 77 77 79 78 12 | 7 11 8 12 29 6 14 12 10 35 5 | 22 30 25 24 33 --- 26 22 21 24 21 13 | 10 18 9 17 42 5 16 16 11 13 5 | 15 30 17 23 50 --- 26 16 20 17 17 14 | 9 18 10 20 29 5 15 11 13 11 5 | 17 30 23 29 31 --- 26 19 23 19 20 15 | 8 15 10 15 26 5 14 11 15 21 5 | 14 26 17 25 32 --- 23 13 21 19 16 16 | 9 13 8 12 44 6 12 10 14 39 5 | 18 25 22 21 33 --- 23 20 26 21 18 17 | 10 16 14 20 40 6 20 10 12 23 5 | 16 30 19 31 42 --- 32 16 25 18 19 18 | 8 17 15 19 30 7 18 12 10 20 5 | 22 34 30 33 36 --- 33 23 29 27 26 19 | 9 19 13 20 35 6 18 12 13 19 5 | 17 35 16 31 39 --- 34 17 17 15 19 20 | 12 18 13 20 42 5 18 14 11 15 5 | 22 33 26 28 39 --- 29 25 19 22 22 21E | 11 13 11 10 39 7 22 11 13 16 5 | 25 31 27 30 36 --- 33 26 36 34 27 22 | 9 17 14 21 32 7 18 11 11 15 5 | 21 32 29 30 35 --- 30 23 27 21 24 23 | 11 21 12 16 30 5 17 14 14 20 5 | 14 33 19 23 35 --- 27 15 23 21 17 24E | 15 24 11 16 41 6 12 14 14 24 6 | 51 57 51 55 53 --- 53 56 59 57 53 25 | 9 14 8 16 34 4 12 13 13 17 4 | 21 25 21 29 36 --- 30 19 25 30 22 26 | 8 12 7 15 23 5 8 11 14 17 4 | 17 27 19 24 26 --- 21 16 22 15 17 27 | 14 13 6 13 31 6 14 12 12 36 5 | 105 107 106 111 109 --- 111 110 106 114 107 28 | 8 11 10 13 63 8 13 10 12 45 5 | 24 34 26 24 38 --- 32 26 21 39 24 29 | 10 16 12 21 32 6 20 14 13 22 6 | 17 30 21 34 42 --- 28 22 24 23 22 30 | 6 11 9 15 20 4 8 9 9 26 4 | 26 28 30 27 34 --- 29 27 25 28 25 31 | 7 18 11 17 37 7 13 9 13 14 4 | 16 28 22 26 43 --- 27 16 23 21 19 32 | 9 18 10 13 24 6 17 8 10 31 5 | 15 25 20 16 25 --- 20 13 17 40 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 16 10 15 36 6 15 11 13 24 |T 25 35 28 31 41 --- 32 26 30 30 26 WRMS | 9 16 11 15 35 5 14 11 10 23 |NE 21 32 25 28 37 --- 29 22 26 27 23 MEDI | 9 16 10 15 32 6 14 11 12 20 |MD 18 30 22 27 36 --- 27 19 24 23 20 Table 3.1502.4 GPS week: 1502 Day: 4 MJD: 54762.000 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 | 6 --- --- --- --- 9670 --- --- --- --- 0 | 13 --- --- --- --- --- --- --- --- --- 14 2E | 9 20 13 12 40 6 13 14 11 17 5 | 17 29 19 20 42 --- 24 13 18 22 18 3 | 7 12 7 9 27 4 10 10 7 19 3 | 15 22 19 16 25 --- 20 19 20 22 16 4E | 12 18 9 15 64 6 14 13 23 21 6 | 28 33 31 35 56 --- 35 29 37 39 29 5 | 10 9 9 11 23 5 8 10 10 30 4 | 14 24 22 23 27 --- 22 19 15 22 17 6 | 8 11 8 10 30 4 10 11 8 13 3 | 15 21 16 14 25 --- 19 15 16 19 14 7 | 8 17 11 13 39 6 12 13 10 17 4 | 15 30 22 24 40 --- 25 16 16 16 18 8 | 9 12 7 12 10 4 11 13 9 25 4 | 12 24 18 19 24 --- 19 16 15 30 15 9 | 11 16 11 12 16 5 12 14 10 22 5 | 31 44 38 39 45 --- 41 36 33 48 35 10 | 7 12 7 9 26 4 6 10 11 20 3 | 18 23 17 19 22 --- 18 19 23 11 18 11E | 13 14 12 13 32 3 20 9 9 15 5 | 34 49 41 36 53 --- 46 38 40 43 40 12 | 10 10 9 11 29 7 12 15 7 36 5 | 18 30 21 22 29 --- 25 20 17 23 19 13 | 9 17 10 16 34 5 15 17 10 12 5 | 12 30 19 23 49 --- 27 16 13 17 15 14 | 8 16 10 21 31 6 15 12 10 12 5 | 14 27 14 27 34 --- 22 17 18 16 16 15 | 9 14 14 14 24 5 18 16 12 21 5 | 13 28 19 24 34 --- 26 14 24 18 17 16 | 10 11 9 12 38 5 14 11 9 39 5 | 18 25 19 22 29 --- 24 21 21 18 18 17 | 11 18 11 17 25 5 19 14 10 26 5 | 13 29 18 24 33 --- 28 19 14 25 15 18 | 8 17 14 18 28 7 19 14 13 21 5 | 16 30 22 28 33 --- 29 15 22 16 19 19 | 9 18 13 19 35 5 19 14 10 19 5 | 15 32 16 31 38 --- 31 13 17 13 18 20 | 12 15 10 19 39 5 16 14 12 15 5 | 18 31 24 26 41 --- 29 20 21 21 20 21E | 12 21 12 9 48 6 20 16 15 26 6 | 32 42 31 36 36 --- 38 33 39 35 33 22 | 9 15 14 21 31 7 19 13 10 17 5 | 18 28 23 26 35 --- 26 20 17 17 19 23 | 10 20 13 15 30 6 18 17 12 21 5 | 12 32 20 24 41 --- 30 17 13 23 16 24E | 14 22 11 17 43 6 12 15 15 24 5 | 28 36 27 36 35 --- 30 38 37 33 31 25 | 9 14 6 17 45 4 12 16 10 19 4 | 18 26 21 25 37 --- 28 20 19 29 20 26 | 6 12 9 14 14 4 11 15 9 19 4 | 14 28 21 23 29 --- 21 21 23 17 18 27 | 13 13 7 13 24 6 13 14 11 22 4 | 36 52 45 46 52 --- 46 45 47 53 45 28 | 7 8 11 13 45 6 12 10 12 48 5 | 23 30 25 24 29 --- 29 26 23 41 23 X29 | 12 21 13 20 43 7 --- 14 14 23 6 | 21 33 22 34 48 --- --- 24 23 31 23 30 | 8 10 9 16 24 5 8 12 9 31 4 | 20 22 23 28 35 --- 21 24 18 28 19 31 | 8 20 12 13 36 6 14 13 9 13 4 | 15 29 17 23 43 --- 24 18 18 18 17 32 | 8 17 9 12 32 5 12 6 11 31 4 | 12 24 18 13 29 --- 19 13 17 40 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 15 10 14 34 5 14 13 11 24 |T 18 30 22 26 36 --- 27 21 22 25 20 WRMS | 9 15 10 14 31 5 13 12 9 21 |NE 17 29 21 24 34 --- 25 20 20 24 19 MEDI | 9 15 10 13 31 5 13 14 10 21 |MD 16 29 21 24 35 --- 26 19 19 22 18 Table 3.1502.5 GPS week: 1502 Day: 5 MJD: 54763.000 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 | 6 --- --- --- --- >>>> --- --- --- --- 0 | 11 --- --- --- --- --- --- --- --- --- 11 2E | 12 18 12 11 33 5 14 14 12 20 5 | 15 26 19 19 39 --- 23 17 20 26 18 3 | 7 12 6 8 19 3 9 14 9 20 3 | 16 24 22 18 24 --- 22 17 24 25 18 4E | 13 17 10 14 57 7 14 12 25 21 6 | 45 47 50 49 49 --- 49 43 46 49 45 5 | 6 10 6 13 19 5 7 11 8 30 4 | 17 24 22 23 23 --- 25 22 19 19 19 6 | 5 12 5 6 15 5 9 13 10 18 3 | 16 25 18 16 24 --- 20 17 21 23 16 7 | 10 20 8 14 39 5 13 11 11 15 4 | 13 34 21 25 39 --- 24 16 17 14 17 8 | 11 13 9 14 15 5 13 14 9 26 4 | 12 22 17 19 25 --- 16 17 14 29 12 9 | 18 17 10 11 39 6 10 17 11 27 5 | 63 70 71 70 59 --- 70 75 66 79 67 10 | 8 10 6 7 30 4 7 12 12 19 3 | 16 25 20 19 26 --- 18 21 26 13 18 11E | 12 13 8 15 42 3 17 10 10 16 4 | 52 55 56 58 65 --- 55 55 54 54 54 12 | 9 11 8 14 29 6 11 15 9 39 5 | 18 28 25 26 32 --- 26 23 21 23 20 13 | 10 19 9 15 27 4 17 14 12 11 5 | 13 32 18 23 41 --- 27 17 16 18 15 14 | 7 13 11 18 42 6 16 13 9 12 4 | 13 23 17 22 36 --- 22 17 17 18 14 15 | 10 18 15 15 20 6 18 14 12 21 5 | 11 29 19 24 31 --- 26 15 21 20 15 16 | 10 13 10 11 32 6 13 15 10 38 5 | 18 25 23 20 25 --- 22 22 18 18 17 17 | 10 19 12 19 23 5 18 13 10 27 5 | 23 36 27 30 40 --- 34 26 22 24 23 18 | 7 16 13 19 28 5 18 13 9 22 5 | 18 35 23 28 37 --- 32 20 23 22 22 19 | 9 18 11 19 28 5 18 16 11 21 5 | 16 35 22 30 39 --- 32 16 22 20 20 20 | 12 17 11 20 33 4 19 12 11 20 5 | 17 33 24 26 38 --- 28 19 22 21 20 21E | 9 14 13 13 40 7 16 12 11 19 5 | 28 34 31 31 43 --- 34 28 32 30 28 22 | 8 13 11 23 28 6 17 16 10 16 5 | 15 29 20 25 35 --- 27 23 19 17 18 23 | 10 19 14 15 19 6 20 13 12 19 5 | 15 33 23 25 39 --- 29 19 20 23 18 24E | 17 18 16 18 45 6 12 18 15 24 6 | 46 47 44 49 50 --- 44 51 50 47 45 25 | 9 13 9 16 50 5 11 15 8 19 4 | 16 19 20 21 35 --- 24 19 20 28 17 26 | 7 11 6 13 24 5 8 15 8 19 4 | 14 25 18 21 24 --- 19 23 20 18 16 27 | 11 15 9 13 25 6 13 13 8 21 4 | 63 68 61 63 67 --- 66 64 65 68 63 28 | 8 11 10 11 33 6 11 10 12 51 5 | 15 27 22 23 37 --- 27 20 20 37 18 X29 | 9 19 11 21 40 7 --- 13 11 --- 6 | 32 40 33 46 39 --- --- 29 36 --- 34 30 | 6 10 5 19 28 5 8 12 8 37 4 | 21 24 21 29 26 --- 24 26 21 32 20 31 | 9 18 10 15 33 6 15 16 8 16 5 | 11 26 15 18 39 --- 24 18 11 15 12 32 | 8 15 6 12 30 3 16 7 11 34 5 | 13 21 19 15 28 --- 19 14 16 41 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 15 10 15 32 5 14 14 11 25 |T 22 32 27 29 37 --- 30 26 26 29 23 WRMS | 9 15 9 15 29 5 13 13 9 20 |NE 19 31 24 27 34 --- 28 23 23 26 21 MEDI | 9 15 10 14 30 5 13 13 10 20 |MD 16 29 22 25 37 --- 26 20 21 23 18 Table 3.1502.6 GPS week: 1502 Day: 6 MJD: 54764.000 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 --- --- --- --- 77 --- --- --- --- 0 | 10 --- --- --- --- --- --- --- --- --- 14 2E | 11 13 11 10 61 6 15 15 10 18 4 | 21 31 24 24 48 --- 31 19 24 31 24 3 | 6 13 8 9 19 4 14 10 6 32 4 | 22 30 26 20 31 --- 26 22 25 28 21 4E | 12 18 32 17 47 7 14 18 24 29 8 | 53 61 50 56 52 --- 61 56 60 66 55 5 | 8 10 6 14 23 4 9 18 7 29 4 | 21 32 25 28 28 --- 31 27 24 26 24 6 | 6 11 9 9 20 4 13 10 7 30 4 | 22 28 27 18 32 --- 25 24 23 30 21 7 | 8 17 13 13 30 6 13 12 9 21 4 | 19 38 25 26 40 --- 30 19 23 21 22 8 | 12 14 8 14 18 5 14 15 8 28 5 | 16 27 16 16 23 --- 21 19 15 32 14 9 | 16 18 9 12 31 5 15 21 11 23 5 | 47 61 51 52 45 --- 55 46 51 55 50 10 | 6 11 9 7 19 2 9 14 9 25 4 | 22 33 26 21 29 --- 23 26 25 17 23 11E | 10 13 11 11 27 5 19 11 7 16 4 | 56 58 55 55 66 --- 59 52 52 57 53 12 | 8 10 5 11 33 6 12 16 9 40 5 | 24 36 29 29 36 --- 32 29 30 34 27 13 | 10 17 13 16 33 6 12 17 9 12 5 | 20 38 21 25 50 --- 30 16 20 17 20 14 | 9 14 11 19 42 6 18 15 10 19 5 | 20 33 19 27 38 --- 29 22 21 28 20 15 | 10 17 11 17 29 5 19 17 10 22 5 | 21 34 18 27 32 --- 30 18 22 24 20 16 | 11 16 10 11 23 6 16 16 9 37 5 | 25 35 30 27 31 --- 29 30 26 22 25 17 | 11 17 17 19 24 6 15 13 11 30 6 | 22 44 30 37 45 --- 45 27 33 36 31 18 | 9 18 15 19 29 6 19 12 10 22 5 | 27 42 31 34 41 --- 40 29 29 31 29 19 | 10 16 14 21 25 6 20 15 11 26 6 | 22 39 24 34 44 --- 38 20 27 19 25 20 | 11 16 14 22 35 6 16 14 9 24 5 | 25 40 34 31 44 --- 35 28 27 32 27 21E | 10 18 14 12 37 5 20 12 10 23 5 | 24 37 23 27 36 --- 33 27 29 38 26 22 | 11 15 13 20 38 7 17 15 11 21 5 | 29 40 32 34 46 --- 35 32 28 33 29 23 | 10 21 16 14 37 5 16 15 11 19 5 | 16 37 21 22 40 --- 28 14 20 20 17 24E | 15 17 15 13 46 6 15 26 15 26 6 | 52 53 48 54 53 --- 51 53 53 50 49 25 | 7 13 12 14 41 5 12 19 8 19 4 | 19 29 21 21 36 --- 27 20 18 31 19 26 | 7 13 7 13 31 4 10 18 8 25 4 | 20 32 24 22 27 --- 23 27 25 24 22 27 | 10 16 9 15 19 5 14 17 8 22 5 | 50 52 50 48 54 --- 55 51 44 55 47 28 | 10 11 9 13 45 5 14 13 9 50 5 | 29 40 33 31 36 --- 38 33 30 43 31 X29 | 13 20 12 19 58 6 --- 10 11 22 6 | 40 46 41 50 53 --- --- 45 40 51 40 30 | 8 8 6 18 42 4 8 14 7 43 5 | 29 32 31 34 32 --- 32 35 30 43 29 31 | 10 20 9 14 32 6 16 17 10 20 5 | 17 33 18 23 49 --- 26 24 23 20 20 32 | 8 16 10 10 42 4 12 6 6 35 4 | 15 26 23 13 35 --- 21 16 19 42 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 15 12 15 34 5 15 15 10 28 |T 26 38 29 31 40 --- 34 29 29 34 27 WRMS | 9 15 12 15 33 5 14 15 7 25 |NE 24 36 27 28 38 --- 32 26 26 31 25 MEDI | 10 16 11 14 32 5 14 15 9 24 |MD 22 37 26 27 40 --- 31 27 26 31 24 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1502 GPS week: 1502 MJD: 54758.0-54764.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3009 |U 8 7 21 |U 10 10 20 | emr | emr 2968 | 11 9 25 | 11 10 23 | esa | esa 2976 | 8 8 23 | 11 10 21 | gfz | gfz 2957 |U 9 8 25 | 13 11 23 | igr | igr 2970 | 9 8 23 | 12 11 24 | igs | igs 2968 | 9 8 24 | 10 10 21 | jpl | jpl 2928 |U 10 9 27 |U 12 12 24 | mit | mit 2976 |U 8 8 22 |U 10 10 21 | 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 5.1502.0 GPS week: 1502 Day: 0 MJD: 54758.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 2976 | 6 8 15 | 8 11 16 | emr | emr 2974 | 9 7 18 | 8 10 17 | esa | esa 2976 | 6 8 22 | 8 10 17 | gfz | gfz 2961 | 6 6 20 | 10 11 16 | igr | igr 2976 | 6 7 19 | 8 10 16 | igs | igs 2976 | 6 7 19 | 8 9 17 | jpl | jpl 2974 | 6 6 19 | 8 9 15 | mit | mit 2976 | 6 7 17 | 8 8 18 | Table 5.1502.1 GPS week: 1502 Day: 1 MJD: 54759.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 2976 | 7 8 26 | 9 8 19 | emr | emr 2972 | 11 9 24 | 9 10 25 | esa | esa 2976 | 8 10 28 | 9 8 22 | gfz | gfz 2960 | 9 9 29 | 12 11 25 | igr | igr 2976 | 9 9 30 | 9 8 22 | igs | igs 2976 | 8 9 27 | 9 9 22 | jpl | jpl 2972 | 8 10 28 | 10 9 24 | mit | mit 2976 | 7 9 25 | 11 10 26 | Table 5.1502.2 GPS week: 1502 Day: 2 MJD: 54760.0 CENT| CLK EPO | WILL | ----+----------+-------------------+ cod | cod 2976 | 16 14 19 | emr | emr 2970 | 15 12 21 | esa | esa 2976 | 17 14 21 | gfz | gfz 2955 | 17 15 20 | igr | igr 2971 | 15 13 18 | igs | igs 2976 | 16 14 18 | jpl | jpl 2969 | 17 13 18 | mit | mit 2976 | 12 12 20 | Table 5.1502.3 GPS week: 1502 Day: 3 MJD: 54761.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 2976 | 8 7 22 | 9 10 22 | emr | emr 2968 | 8 7 21 | 13 11 30 | esa | esa 2976 | 7 7 19 | 11 11 25 | gfz | gfz 2956 | 7 6 19 | 15 11 30 | igr | igr 2976 | 7 5 19 | 11 9 26 | igs | igs 2948 | 8 6 19 | 11 10 24 | jpl | jpl 2967 | 8 7 20 | 12 12 26 | mit | mit 2976 | 7 8 20 | 13 12 22 | Table 5.1502.4 GPS week: 1502 Day: 4 MJD: 54762.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3037 | 5 6 19 | 10 9 17 | emr | emr 2968 | 8 9 29 | 12 12 22 | esa | esa 2976 | 7 7 22 | 11 10 19 | gfz | gfz 2958 | 8 8 25 | 15 10 24 | igr | igr 2974 | 6 6 22 | 10 9 19 | igs | igs 2972 | 7 7 25 | 11 10 19 | jpl | jpl 2872 | 7 6 28 | 14 15 29 | mit | mit 2976 | 8 8 25 | 11 11 20 | Table 5.1502.5 GPS week: 1502 Day: 5 MJD: 54763.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3066 | 15 9 28 | 7 8 17 | emr | emr 2962 | 17 14 39 | 11 10 26 | esa | esa 2976 | 16 9 29 | 8 8 18 | gfz | gfz 2951 | 15 11 40 | 11 8 18 | igr | igr 2950 | 21 16 30 | 19 22 39 | igs | igs 2958 | 16 11 35 | 9 11 24 | jpl | jpl 2870 | 21 15 47 | 11 12 25 | mit | mit 2976 | 16 10 28 | 8 8 18 | Table 5.1502.6 GPS week: 1502 Day: 6 MJD: 54764.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3062 | 6 6 18 | 9 8 28 | emr | emr 2968 | 9 10 21 | 10 7 24 | esa | esa 2976 | 6 8 19 | 10 8 26 | gfz | gfz 2958 | 8 7 19 | 12 9 29 | igr | igr 2970 | 6 7 19 | 9 8 25 | igs | igs 2972 | 7 7 17 | 9 8 22 | jpl | jpl 2872 | 7 9 19 | 12 11 29 | mit | mit 2976 | 6 8 18 | 9 7 24 | 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 6.1502 GPS week: 1502 MJD: 54758.500-54764.500 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 | -13 4 14 22 4 | 11 21 | 29 12 48 100 3 | 2 emr uuuuu | -48 5 48 -88 7 | 44 50 | 17 18 118 174 6 | 2 esa uuuuu | 20 -31 0 29 -4 | 18 28 | 18 22 60 67 8 | 4 gfz uuuuu | -6 1 -13 33 5 | 7 20 | 10 16 66 43 4 | 3 grg xxxxx | -44 -7 9 -65 -7 | -2 29 | 55 55 119 90 27 | 5 igr xxxxx | -20 18 45 20 5 | -9 22 | 17 25 44 84 3 | 2 irf xxxxx | 12 3 -68 27 6 | -8 21 | 12 9 32 50 7 | 2 jpl uuuuu | 2 3 44 16 3 | 10 24 | 45 28 80 109 8 | 3 mit uuuuu | 24 17 -215 -4 7 | 7 22 | 25 19 59 127 7 | 2 ngs uuuuu | 11 14 115 -24 -10 | 3 15 | 39 51 57 134 9 | 2 sio xuuuu | 180 -31 -1 23 2 | 31 37 | 24 16 80 135 12 | 3 Table 7.1502.0 GPS week: 1502 Day: 0 MJD: 54758.500 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 2 18 69 5 | 9 19 emr uuuuu | -43 -2 -1 -243 -4 | 47 53 esa uuuuu | 4 -4 2 -26 -14 | 23 31 gfz uuuuu | -8 -3 -43 54 7 | 5 18 grg xxxxx | -73 17 -4 -105 -58 | 6 35 igr xxxxx | -12 31 83 -22 4 | -8 21 irf xxxxx | 11 -4 -12 -57 -7 | -7 20 jpl uuuuu | 35 21 -36 8 -2 | 7 22 mit uuuuu | 26 6 -130 -176 -5 | 7 22 ngs uuuuu | 0 -4 178 196 1 | 3 14 sio xuuuu | 197 -38 -32 82 -22 | 36 41 Table 7.1502.1 GPS week: 1502 Day: 1 MJD: 54759.500 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 -9 -30 36 4 | 9 19 emr uuuuu | -55 24 161 -53 14 | 45 50 esa uuuuu | 10 -33 6 -22 -9 | 21 30 gfz uuuuu | -12 12 7 68 -1 | 5 18 grg xxxxx | -71 -12 -73 39 -23 | 2 38 igr xxxxx | -17 47 19 65 2 | -9 21 irf xxxxx | 34 4 -41 -28 2 | -9 21 jpl uuuuu | -3 43 60 85 13 | 8 22 mit uuuuu | 52 24 -184 -187 3 | 6 21 ngs uuuuu | -8 -28 30 37 -7 | 4 14 sio xuuuu | 221 -17 38 80 -2 | 32 38 Table 7.1502.2 GPS week: 1502 Day: 2 MJD: 54760.500 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 | -35 1 -22 -16 0 | 11 21 emr uuuuu | -39 -28 220 38 6 | 45 51 esa uuuuu | -4 -4 -109 75 -16 | 21 29 gfz uuuuu | -7 18 -3 4 3 | 7 19 grg xxxxx | -70 -27 142 -111 19 | 1 37 igr xxxxx | -28 30 97 139 5 | -9 21 irf xxxxx | 6 20 -58 53 4 | -8 21 jpl uuuuu | 80 13 163 200 11 | 10 24 mit uuuuu | 36 48 -235 -4 5 | 7 22 ngs uuuuu | -11 -45 138 -177 -5 | 5 14 sio xuuuu | 168 -12 -93 -49 3 | 31 37 Table 7.1502.3 GPS week: 1502 Day: 3 MJD: 54761.500 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 22 4 -75 9 | 9 20 emr uuuuu | -30 13 42 150 15 | 41 47 esa uuuuu | 30 -51 37 -24 -1 | 16 27 gfz uuuuu | -8 6 -57 1 10 | 5 19 grg xxxxx | -12 -9 -15 -5 -3 | -8 23 igr xxxxx | -31 33 1 55 1 | -11 22 irf xxxxx | 8 4 -87 75 13 | -10 22 jpl uuuuu | -51 -4 -44 21 9 | 9 24 mit uuuuu | -10 24 -198 40 16 | 5 21 ngs uuuuu | 60 7 181 -6 -27 | 3 15 sio xuuuu | 179 -38 103 -102 13 | 28 34 Table 7.1502.4 GPS week: 1502 Day: 4 MJD: 54762.500 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 | -57 13 -23 -19 0 | 11 22 emr uuuuu | -43 10 -13 5 8 | 42 48 esa uuuuu | 44 -21 85 104 -1 | 15 26 gfz uuuuu | -9 -22 -2 -37 6 | 6 20 grg xxxxx | 16 30 57 -48 3 | -7 22 igr xxxxx | -39 14 30 60 9 | -10 22 irf xxxxx | -4 4 -89 49 10 | -9 22 jpl uuuuu | -11 4 131 14 -2 | 11 25 mit uuuuu | 6 19 -266 102 10 | 7 23 ngs uuuuu | 55 5 92 -189 -10 | 1 16 sio xuuuu | 150 -26 -93 88 7 | 29 35 Table 7.1502.5 GPS week: 1502 Day: 5 MJD: 54763.500 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 | 33 10 105 -60 2 | 11 22 emr uuuuu | -82 -4 62 -166 8 | 43 49 esa uuuuu | 23 -58 6 119 6 | 14 25 gfz uuuuu | -13 -19 -104 71 9 | 8 22 grg xxxxx | 25 61 -189 -1 19 | -7 22 igr xxxxx | -27 -15 -6 -104 6 | -9 23 irf xxxxx | 7 -10 -95 65 11 | -8 23 jpl uuuuu | -40 -11 -5 -77 -9 | 12 26 mit uuuuu | 3 -14 -185 86 12 | 7 24 ngs uuuuu | 29 105 60 34 -14 | 1 16 sio xuuuu | 182 -31 -17 -166 9 | 29 35 Table 7.1502.6 GPS week: 1502 Day: 6 MJD: 54764.500 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 | 2 -9 45 218 5 | 14 22 emr uuuuu | -47 23 -138 -351 4 | 47 52 esa uuuuu | 35 -44 -29 -22 2 | 17 26 gfz uuuuu | 16 11 108 68 4 | 12 22 grg xxxxx | -123 -113 146 -227 -6 | -3 22 igr xxxxx | 14 -15 93 -56 5 | -5 20 irf xxxxx | 18 -1 -97 28 7 | -4 21 jpl uuuuu | 4 -45 42 -140 -1 | 16 24 mit uuuuu | 55 12 -308 109 7 | 11 25 ngs uuuuu | -47 56 126 -67 -8 | 3 14 sio xuuuu | 163 -59 88 229 8 | 32 37