From IGS.ACC at noaa.gov Thu Jul 9 04:50:41 2009 From: IGS.ACC at noaa.gov (Jim Ray) Date: Thu, 09 Jul 2009 11:50:41 +0000 Subject: [IGSREPORT-17573] Wk 1537 IGS Final Orbits Message-ID: <4a55d991.r/2yvVkYVtRlD/Vp%igs.acc@noaa.gov> ****************************************************************************** IGS Electronic Report 09 Jul 04:51:04 PDT 2009 Message Number 17573 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1537 (Jun 21, 2009 - Jun 27, 2009) Contacts: J. Ray (jim.ray at noaa.gov), J. Griffiths (jake.griffiths at 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: igs1537[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1537[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1537[0-6].cls IGS GPS clock combination summary report. igs15377.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15377.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Duplicate entries can arise due to separate combination runs for the 30-s clocks ACs (listed first) and the 5-min clock ACs (listed second). Day | Centre | PRN/STA list ----+--------+--------------- 0 | COD | YELL YELL 0 | EMR | 10 32 10 32 MIZU WTZR 0 | ESA | MIZU 0 | GFZ | 32 BAN2 FAA1 0 | GRG | ONSA TWTF 0 | JPL | 10 UNSA 0 | MIT | 19 19 DRAO HOB2 1 | ALL | 1 1 1 | COD | MATE 1 | EMR | 10 32 10 32 WTZR 1 | ESA | SSIA 1 | GFZ | 7 15 32 AUCK CHUR FAA1 UNSA 1 | GRG | ONSA 1 | JPL | 10 32 FLIN 1 | MIT | FLIN OUS2 SYOG 2 | ALL | 1 1 32 2 | COD | SCH2 SCH2 2 | EMR | 10 10 MIZU 2 | ESA | UNSA 2 | GFZ | 7 15 HARB 2 | GRG | ONSA 2 | JPL | 10 2 | MIT | MATE 3 | EMR | 10 32 10 32 MIZU WTZR 3 | GFZ | 7 15 32 AUCK CHUR FAA1 UNSA 3 | GRG | ONSA 3 | JPL | 10 3 | MIT | HOB2 4 | EMR | 32 32 MIZU WTZR 4 | GFZ | 7 15 32 AUCK CHUR 4 | GRG | ONSA 4 | JPL | 10 4 | MIT | 15 29 15 29 AMC2 HYDE 4 | NGS | 1 5 | ALL | 1 1 25 5 | COD | MATE 5 | EMR | 32 32 WTZR 5 | ESA | 32 5 | GFZ | 7 15 AUCK BOR1 CHUR GRAZ HYDE KIRU MATE NYA1 ONSA 5 | GRG | DAV1 ONSA TWTF 5 | JPL | 32 DAV1 KERG 5 | MIT | BUE1 KERG TWTF 6 | EMR | 32 32 MIZU WTZR 6 | ESA | 26 32 UNSA 6 | GFZ | 7 15 26 32 AUCK CHUR HOFN 6 | GRG | ONSA TWTF 6 | JPL | 10 32 HARB 6 | MIT | 12 19 25 26 12 19 25 26 HOB2 6 | NGS | 1 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 | .8 .6 .4 -19 -23 -13 -.07 EMR | 10.7 -7.7 -12.1 58 29 69 -.20 ESA | 5.7 -1.9 10.8 -3 -25 9 .11 GFZ | .4 .7 1.0 0 -4 1 -.21 GRG | 9.0 -1.8 1.6 -32 -13 -3 .07 JPL | 4.2 -2.1 -11.1 -3 -1 3 .13 MIT | 6.8 -3.6 5.9 1 18 -28 -.25 NGS | 12.5 -7.8 4.3 -93 -149 -11 -.10 SIO | 3.4 -4.3 -19.9 -67 -138 10 .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 1.1537.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1537.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 2.1537.[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 3.1537.[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 5.1537.0-6). 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 1537 summary. (Jun 21, 2009 - Jun 27, 2009) Table 1.1537.a GPS week: 1537 MJD: 55003.000-55009.000 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 236| 0 0 0 -13 -10 -20 -.13 9 8 | -229 -623 16 75 | 0 0 1 12 16 22 .02 | 323 480 emr 76| 2 0 -5 -121 -84 -10 .38 18 18 | 2753 -664 20 110 | 1 2 2 26 28 20 .03 | 1386 1287 esa 126| 1 0 3 -34 -21 -24 .32 9 9 | -1970 1065 19 115 | 0 0 1 9 14 21 .02 | 1362 2220 gfz 192| 0 0 4 -35 -60 82 -.12 10 10 | 1 74 23 129 | 0 0 1 14 18 39 .03 | 303 451 grg 108| 3 0 -1 -10 9 -27 1.05 37 35 | 73 -228 84 212 | 1 2 3 15 21 88 .07 | 159 335 igr n/a| 0 0 0 -17 -55 -19 .04 5 5 | 22802 -501 20 71 | 0 0 0 13 20 37 .02 | 1637 1515 jpl 129| 0 0 -10 -39 -55 23 .56 17 16 | 2702 -650 17 97 | 0 0 2 15 17 18 .04 | 1885 1435 mit 260| 0 0 0 -20 -98 -21 -.21 10 10 | -10968 305 21 160 | 1 0 1 32 21 14 .02 | 7402 816 ngs 218| 0 0 0 165 240 -26 -.26 12 9 | 6308 5039 2207 3723 | 1 0 2 33 29 15 .04 | 5099 5352 sio 260| -3 1 1 137 210 -19 -.16 18 18 | --- --- --- --- | 0 0 1 28 24 19 .03 | --- --- Table 1.1537.b GPS week : 1537 MJD: 55003.000-55009.000 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 13 16 0 10 16 16 | 2 | 6 6 5 6 5 5 6 | 3 | 4 3 3 3 3 4 5 | 4 | 4 4 3 4 4 3 4 | 6 | 4 3 3 3 3 4 5 | 7 | 5 5 5 4 5 4 5 | 8 | 5 4 4 4 5 5 6 | 9 | 4 4 4 4 4 4 5 | 10 | 6 5 5 6 6 6 7 | 11 | 5 5 4 4 4 4 4 | 12 | 5 6 5 5 5 5 7 | 13 | 5 5 5 4 5 4 5 | 14 | 4 5 5 5 4 4 5 | 15 | 5 5 5 5 5 5 5 | 16 | 5 5 5 5 5 5 5 | 17 | 6 6 6 5 5 6 6 | 18 | 5 5 4 4 5 4 5 | 19 | 4 5 4 4 4 4 5 | 20 | 4 5 4 5 4 4 5 | 21 | 5 5 4 4 5 4 5 | 22 | 4 4 4 3 4 3 4 | 23 | 5 5 5 5 5 5 6 | 24 | 4 4 4 4 4 3 4 | 25 | 4 4 5 5 5 6 7 | 26 | 4 4 4 4 4 4 4 | 27 | 4 4 4 4 4 4 4 | 28 | 5 4 4 4 5 5 6 | 29 | 6 6 5 5 6 6 5 | 30 | 5 5 5 5 6 5 7 | 31 | 5 5 5 4 5 4 5 | 32 | 6 5 5 6 5 7 6 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1537.0 GPS week: 1537 Day: 0 MJD: 55003.000 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 236| 1 0 0 0 -27 -5 -.13 7 7 | -353 -548 18 59 | 16 -6 | emr 76| 1 0 -3 -134 -117 7 .35 17 17 | 4599 -284 19 84 | -1 -19 | esa 126| 0 -1 1 -44 -24 4 .34 10 10 | -3474 4054 21 104 | -9 41 | gfz 192| 0 0 5 -44 -91 53 -.09 9 9 | -29 -98 22 88 | 10 3 | grg 108| 3 0 -6 3 2 -84 1.11 35 32 | 3 2 81 223 | -57 38 | igr n/a| -1 0 0 -11 -75 17 .02 5 5 | 24853 -126 21 61 | -40 36 | jpl 129| -1 0 -11 -55 -71 2 .58 16 15 | 5276 -310 15 78 | 80 46 | mit 260| 0 0 1 -20 -84 -16 -.21 13 13 | -63 47 27 132 | 9 28 | ngs 218| 0 0 0 174 266 -33 -.30 11 7 | -334 -609 2374 3862 | 56 -24 | sio 260| -2 1 0 127 197 -10 -.12 17 16 | --- --- --- --- | -93 -100 | Table 2.1537.1 GPS week: 1537 Day: 1 MJD: 55004.000 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 236| 0 0 0 1 -25 1 -.15 8 8 | 4 -778 12 59 | 27 23 | emr 76| 3 -1 -2 -154 -113 -5 .41 16 16 | 4700 -2123 18 91 | 35 -16 | esa 126| 0 -1 1 -47 5 -59 .32 9 9 | -1493 1915 20 117 | -2 -13 | gfz 192| 0 0 4 -37 -61 134 -.14 9 9 | -11 492 23 129 | 30 33 | grg 108| 3 -3 0 -36 -8 -13 1.01 39 37 | 67 422 89 209 | 2 73 | igr n/a| 0 0 0 -14 -77 -14 .02 6 6 | 25232 -2323 20 64 | -22 27 | jpl 129| 0 0 -7 -56 -82 38 .58 16 15 | 5263 -2310 18 107 | 20 40 | mit 260| -2 0 0 15 -62 -42 -.24 12 12 | -15348 939 20 154 | 11 33 | ngs 218| 0 0 -2 152 202 -53 -.31 13 9 | 13335 330 2308 3828 | 11 8 | sio 260| -3 1 0 161 254 -50 -.15 18 18 | --- --- --- --- | -98 -117 | Table 2.1537.2 GPS week: 1537 Day: 2 MJD: 55005.000 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 236| 0 0 1 -25 -9 6 -.14 8 7 | 300 -1213 15 96 | 48 -4 | emr 76| 4 -3 -4 -141 -106 -5 .37 17 17 | 2936 -2384 21 132 | 32 -14 | esa 126| 1 0 1 -36 -18 -33 .32 9 9 | -1889 -421 20 127 | 30 11 | gfz 192| 0 0 2 -30 -61 48 -.11 10 10 | 390 -359 23 165 | 16 10 | grg 108| 3 1 0 -3 26 121 .95 36 36 | 274 -469 77 203 | 21 23 | igr n/a| 0 0 -1 -35 -44 -25 .04 5 5 | 23057 -2532 21 78 | -5 -15 | jpl 129| 0 0 -8 -46 -56 25 .61 17 16 | 3145 -2596 18 105 | -3 -34 | mit 260| -1 0 1 9 -98 -7 -.20 10 10 | -15139 1678 21 224 | 3 27 | ngs 218| 0 0 -2 111 202 -26 -.26 11 7 | 5358 10446 2458 3760 | 69 -8 | sio 260| -3 2 1 164 212 -10 -.15 17 19 | --- --- --- --- | -107 -106 | Table 2.1537.3 GPS week: 1537 Day: 3 MJD: 55006.000 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 236| 0 0 -1 -24 5 -20 -.12 8 8 | -85 -1130 20 69 | 43 10 | emr 76| 1 0 -6 -104 -57 17 .42 18 18 | 1585 139 21 113 | -18 -51 | esa 126| 1 0 6 -23 -36 -29 .31 9 9 | -3175 706 20 122 | 25 23 | gfz 192| 0 0 5 -57 -36 79 -.12 10 10 | 9 -36 24 117 | 34 -12 | grg 108| 5 3 -1 -13 44 -21 1.13 38 34 | -12 -282 86 221 | -3 8 | igr n/a| 0 0 0 -29 -23 -36 .08 5 5 | 21417 -26 19 76 | -3 -12 | jpl 129| 0 1 -13 -39 -30 0 .58 17 16 | 1501 -212 17 88 | -34 -3 | mit 260| 0 0 0 -6 -126 -10 -.19 8 7 | -209 118 21 140 | 2 49 | ngs 218| 0 -1 0 152 260 -33 -.27 12 8 | -106 -1134 2128 3801 | 13 -69 | sio 260| -4 1 1 142 180 -20 -.11 17 19 | --- --- --- --- | -103 -95 | Table 2.1537.4 GPS week: 1537 Day: 4 MJD: 55007.000 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 236| 0 0 -1 -24 13 -46 -.11 9 9 | -307 -637 19 91 | 64 -10 | emr 76| 2 2 -6 -128 -45 -33 .38 19 19 | 1798 110 27 152 | 16 -34 | esa 126| 0 -1 3 -35 -37 -34 .33 9 9 | -1214 544 22 113 | 0 36 | gfz 192| 1 0 3 -42 -75 103 -.10 9 9 | -58 442 26 137 | 39 11 | grg 108| 0 0 0 -8 5 -88 1.04 37 35 | 318 -412 87 211 | 0 -10 | igr n/a| 0 0 0 -9 -43 -1 .05 5 5 | 21324 505 22 85 | -48 6 | jpl 129| 1 0 -12 -33 -40 53 .55 16 15 | 1051 321 19 105 | 18 79 | mit 260| 0 -1 0 -13 -117 -34 -.21 8 7 | -15652 -690 22 180 | 21 41 | ngs 218| 0 0 0 160 273 -9 -.22 12 9 | 10051 7056 1869 3764 | -54 -68 | sio 260| -3 1 2 158 190 -4 -.19 18 19 | --- --- --- --- | -96 -106 | Table 2.1537.5 GPS week: 1537 Day: 5 MJD: 55008.000 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 236| 0 0 -1 -19 -6 -33 -.10 9 9 | -621 -177 15 80 | 28 27 | emr 76| 1 1 -7 -109 -78 -13 .39 20 18 | 2232 -1224 20 119 | -10 -17 | esa 126| 2 0 4 -20 -13 -4 .33 8 8 | 407 -2519 17 112 | 21 36 | gfz 192| 0 0 3 -14 -45 34 -.12 9 9 | -568 624 22 143 | -8 28 | grg 108| 1 0 2 -24 12 37 1.01 38 36 | -80 -539 87 213 | -45 57 | igr n/a| 0 0 0 -22 -49 15 .03 5 5 | 22025 -726 19 72 | -32 6 | jpl 129| 0 1 -11 -29 -56 23 .53 17 16 | 1529 -921 16 104 | 31 50 | mit 260| 0 -1 0 -53 -107 -8 -.22 10 8 | -15358 -459 17 154 | 26 32 | ngs 218| -2 0 2 187 236 -6 -.23 12 9 | 7145 11158 2251 3806 | -66 -66 | sio 260| -3 1 1 124 205 2 -.17 19 18 | --- --- --- --- | -91 -112 | Table 2.1537.6 GPS week: 1537 Day: 6 MJD: 55009.000 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 236| 0 0 0 -2 -24 -47 -.16 11 9 | -544 120 17 72 | 37 31 | emr 76| 4 2 -8 -77 -69 -41 .33 19 19 | 1426 1112 18 81 | -53 -10 | esa 126| 1 0 3 -32 -25 -12 .29 9 9 | -2957 3179 18 110 | 30 77 | gfz 192| 0 0 6 -23 -51 127 -.16 11 11 | 274 -543 23 124 | -12 46 | grg 108| 4 -1 -4 6 -19 -141 1.11 37 36 | -55 -318 86 208 | -54 65 | igr n/a| -1 0 1 3 -75 -91 .04 5 5 | 21708 1716 20 67 | -43 48 | jpl 129| -1 0 -10 -14 -53 20 .49 17 16 | 1151 1472 17 96 | 6 25 | mit 260| 1 -1 0 -73 -92 -33 -.23 12 10 | -15009 507 22 136 | 23 15 | ngs 218| -1 0 3 221 243 -24 -.24 15 15 | 8712 8030 2063 3240 | -171 -57 | sio 260| -3 0 0 84 229 -39 -.18 20 19 | --- --- --- --- | -85 -124 | 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 3.1537.0 GPS week: 1537 Day: 0 MJD: 55003.000 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 | 2 --- --- --- --- 35 --- --- --- --- 0 | 38 --- --- --- --- 29 --- --- --- --- 36 2 | 9 18 9 7 33 7 18 10 12 34 5 | 30 35 28 26 37 29 36 30 32 36 28 3 | 8 9 8 7 50 4 8 12 13 17 4 | 31 35 35 35 41 35 34 35 35 38 33 4 | 7 14 7 9 32 5 8 8 16 12 3 | 30 32 29 32 28 28 25 32 32 33 30 6 | 6 9 7 6 52 4 11 11 10 14 3 | 32 33 34 35 38 36 32 36 39 35 33 7 | 6 18 11 13 36 6 13 16 10 16 4 | 27 33 28 27 55 26 31 30 29 30 26 8 | 8 17 8 7 18 7 16 19 8 11 4 | 22 27 25 24 31 23 28 24 28 22 22 9 | 7 17 9 9 22 5 15 10 7 9 3 | 24 32 33 25 37 28 33 26 32 26 27 10E | 10 19 13 12 43 4 16 12 25 14 5 | 22 27 26 21 40 20 30 26 32 27 22 11 | 8 16 8 14 57 6 20 14 11 21 5 | 35 48 43 43 49 41 52 36 38 33 38 12 | 7 27 10 9 33 6 21 11 10 13 5 | 27 41 31 23 32 28 37 28 31 25 27 13 | 8 15 12 9 34 6 21 18 9 16 5 | 25 32 28 27 45 26 35 28 32 29 26 14 | 8 22 11 7 27 4 14 11 9 14 4 | 29 39 36 32 43 33 38 34 39 37 34 15 | 6 23 13 9 36 5 17 14 8 16 4 | 29 38 32 27 47 31 35 30 35 32 29 16 | 7 15 9 9 35 5 22 12 9 12 4 | 22 32 31 23 34 26 36 24 33 25 25 17 | 11 15 9 20 21 9 14 15 14 22 5 | 29 31 31 39 37 31 33 32 33 37 29 18E | 7 18 11 9 27 4 21 12 8 13 4 | 18 28 28 18 27 21 31 23 29 25 21 19 | 6 10 8 8 47 3 15 14 13 17 4 | 31 35 39 32 46 33 40 29 30 37 32 20E | 5 15 10 11 38 5 16 11 7 11 4 | 24 31 30 24 37 25 33 24 26 21 24 21 | 7 17 13 8 43 6 18 14 11 19 4 | 20 28 26 20 48 22 32 27 28 25 22 22E | 6 13 9 6 32 4 15 12 8 8 3 | 23 29 28 24 31 26 33 27 35 27 27 23 | 6 17 9 10 36 6 20 13 9 18 4 | 27 34 32 29 50 29 37 26 35 29 28 24 | 7 13 10 5 32 4 9 13 8 12 3 | 34 33 43 32 36 35 35 38 37 31 35 25 | 7 14 8 7 19 5 13 15 4 22 4 | 28 36 31 29 357 30 27 31 32 36 30 26 | 6 12 10 6 22 5 11 12 8 9 3 | 28 29 34 26 34 29 35 28 36 29 29 27 | 7 17 9 7 27 4 13 9 7 11 3 | 26 31 33 26 45 28 32 27 29 28 27 28 | 10 18 15 9 32 8 19 15 11 13 5 | 23 30 24 22 43 22 30 27 29 23 22 29 | 8 17 15 8 39 6 17 15 10 32 5 | 29 37 40 33 38 34 39 34 33 47 33 30 | 6 16 9 8 36 7 14 12 10 26 4 | 22 31 31 23 42 26 32 27 28 42 25 31 | 7 18 11 7 28 6 14 14 15 17 4 | 24 33 32 28 47 30 34 30 38 34 28 X32E | 8 20 8 11 45 9 --- 18 19 12 5 | 32 35 35 36 56 34 --- 35 41 35 33 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 17 10 9 35 5 16 13 11 17 |T 27 33 31 28 51 28 33 29 32 31 28 WRMS | 7 17 10 9 32 5 15 13 7 16 |NE 27 32 32 27 39 29 33 30 33 31 28 MEDI | 7 17 9 8 33 5 15 12 10 14 |MD 27 32 31 27 40 29 33 28 32 30 28 Table 3.1537.1 GPS week: 1537 Day: 1 MJD: 55004.000 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 | 18 --- --- --- --- 20 --- 16 19 --- 13 | 32 --- --- --- --- 26 --- 25 23 --- 28 2 | 8 16 8 8 38 6 18 8 18 32 5 | 17 22 22 18 27 20 24 19 25 31 17 3 | 6 9 4 6 51 5 10 10 10 16 3 | 32 34 29 32 47 33 32 32 34 34 31 4 | 8 10 7 5 50 4 11 8 16 9 3 | 21 22 25 23 27 22 17 21 23 24 20 6 | 6 9 6 5 34 4 11 10 9 14 3 | 27 28 22 28 28 26 22 28 32 24 26 7M | 6 17 9 11 52 6 16 12 14 15 4 | 26 33 28 24 52 26 32 25 29 21 24 8 | 7 16 5 7 25 7 15 15 13 11 4 | 14 23 19 15 28 17 22 19 22 17 15 9 | 6 17 9 7 17 6 14 9 9 11 3 | 20 29 23 22 34 21 29 23 23 23 21 10E | 10 19 10 9 60 7 14 14 21 16 5 | 16 28 23 25 35 24 27 19 31 23 19 11M | 7 12 7 8 41 5 17 13 13 21 4 | 26 38 31 29 44 30 38 28 32 18 27 12 | 10 27 13 14 48 9 23 10 11 19 5 | 24 37 28 27 32 25 33 25 32 22 24 13M | 8 13 11 8 40 8 19 13 8 15 4 | 19 30 23 17 41 21 30 18 18 17 17 14M | 7 22 13 9 33 4 18 15 12 20 5 | 23 34 29 22 36 22 29 22 24 28 22 15 | 7 18 8 16 35 5 18 13 12 16 5 | 20 30 23 22 36 23 29 22 21 24 20 16 | 7 22 10 9 44 6 22 11 13 12 4 | 18 33 21 18 29 19 28 16 26 15 18 17 | 11 14 12 18 39 5 16 17 19 22 6 | 22 24 23 26 36 19 26 23 24 26 19 18E | 8 20 11 9 23 4 21 9 8 12 4 | 21 30 28 20 26 20 27 23 24 23 21 19M | 7 11 7 7 48 5 14 19 12 24 4 | 20 28 27 22 35 23 29 23 18 30 21 20E | 8 19 11 9 36 5 16 11 10 12 4 | 21 33 24 20 33 21 30 16 19 14 19 21 | 7 15 12 9 39 5 19 12 9 20 4 | 17 24 18 18 40 16 27 19 24 17 17 22E | 7 16 8 9 26 5 14 10 8 12 3 | 19 26 23 18 34 17 22 21 21 19 18 23M | 7 17 10 10 46 6 22 12 12 19 5 | 24 37 28 24 39 26 34 25 27 24 24 24 | 6 16 9 6 29 5 12 13 12 12 4 | 22 24 27 25 27 23 27 24 28 19 22 25M | 9 14 7 8 25 7 15 10 11 22 4 | 30 40 37 30 465 34 33 31 32 34 31 26 | 7 11 12 7 26 4 13 14 9 9 3 | 19 22 25 20 30 20 24 25 22 23 20 27 | 5 16 7 8 24 6 13 8 10 11 3 | 20 28 22 25 33 22 28 23 24 22 21 28 | 7 15 8 8 39 8 17 11 15 12 4 | 19 26 23 18 34 21 24 24 32 21 20 29 | 11 15 9 11 29 6 18 13 9 34 5 | 21 27 25 28 28 24 28 25 27 39 23 30 | 9 16 9 9 38 4 14 14 9 26 4 | 23 32 28 24 40 24 30 25 25 35 24 31 | 9 17 12 9 42 4 15 11 11 16 4 | 18 31 20 17 48 17 26 18 21 20 17 32E | 9 21 6 10 52 6 17 15 23 13 5 | 27 39 29 29 31 30 24 29 45 25 28 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 16 9 9 39 6 16 12 13 18 |T 21 29 25 22 49 22 27 23 26 23 21 WRMS | 8 16 9 9 37 6 15 12 9 18 |NE 20 27 23 22 33 21 26 22 25 24 20 MEDI | 7 16 9 9 38 5 16 12 12 15 |MD 21 29 24 22 34 22 28 23 24 23 21 Table 3.1537.2 GPS week: 1537 Day: 2 MJD: 55005.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 25 --- --- --- --- 14 --- 20 21 --- 16 | 38 --- --- --- --- 34 --- 27 28 --- 29 2 | 7 20 8 9 39 6 19 11 10 31 5 | 31 36 32 35 43 32 35 35 33 43 32 3 | 7 11 8 6 44 4 10 9 5 15 3 | 40 41 38 41 42 39 34 38 39 36 39 4 | 6 12 8 9 54 4 9 10 7 11 3 | 31 34 36 36 30 34 33 37 28 38 33 6 | 6 9 9 5 29 4 9 10 5 14 3 | 39 39 37 40 37 39 34 40 38 37 38 7 | 6 16 10 18 32 5 18 10 12 14 5 | 33 39 37 38 58 35 38 35 36 36 34 8M | 7 16 7 8 29 8 16 9 11 11 3 | 24 29 29 29 33 28 32 28 30 27 26 9 | 9 19 11 9 23 5 14 9 7 9 4 | 25 34 31 31 37 27 33 28 29 29 28 10E | 11 18 9 10 52 4 15 13 18 13 5 | 27 32 31 31 32 29 33 30 36 31 28 11M | 7 15 8 8 45 3 18 8 9 21 4 | 33 44 38 39 42 37 42 35 39 37 36 12 | 10 26 11 11 29 6 20 9 11 13 5 | 26 41 30 32 33 30 35 30 32 32 29 13 | 5 15 10 11 38 5 23 11 11 12 4 | 28 36 34 29 43 29 41 29 27 29 29 14 | 8 26 11 6 30 4 20 9 11 14 4 | 28 44 32 33 39 32 35 30 34 33 31 15 | 6 17 13 9 42 4 17 10 11 15 4 | 28 34 34 32 41 30 34 30 29 33 29 16 | 7 19 10 9 58 4 24 8 8 13 4 | 25 37 28 32 32 28 36 25 26 26 26 17M | 11 18 9 22 26 5 16 14 14 21 6 | 30 35 32 44 37 34 33 34 38 40 33 18E | 7 20 11 9 23 4 20 8 9 8 4 | 27 37 33 30 30 30 35 29 34 28 30 19 | 5 13 10 8 49 5 14 9 7 18 3 | 27 34 35 27 44 30 34 27 28 31 29 20E | 9 17 10 12 31 5 13 10 11 12 4 | 28 34 30 30 34 27 33 25 27 25 26 21 | 6 15 8 7 38 4 20 10 8 19 4 | 24 30 27 29 37 27 32 28 30 27 26 22E | 9 14 9 6 28 5 15 8 11 7 3 | 28 37 30 34 30 32 33 32 36 30 31 23 | 7 18 8 10 39 4 21 10 10 18 4 | 31 40 34 31 43 30 40 29 28 30 29 24 | 7 16 7 5 25 1 11 9 11 12 3 | 31 30 33 31 35 30 31 32 35 31 31 25 | 6 14 10 8 25 3 17 13 9 22 4 | 36 44 43 40 625 38 36 40 40 40 38 26 | 6 12 10 6 27 4 11 12 8 10 3 | 27 31 33 32 31 28 31 32 30 32 30 27 | 6 16 7 8 26 4 12 7 8 12 3 | 26 30 30 30 38 27 32 28 31 29 28 28 | 7 15 11 10 35 5 17 10 9 11 4 | 28 33 27 28 38 28 32 31 32 30 28 29 | 8 14 9 6 30 5 17 8 13 32 5 | 28 32 35 32 27 30 32 28 31 38 30 30 | 9 18 7 12 27 6 16 9 12 30 5 | 28 37 33 33 42 32 37 29 29 43 30 31 | 11 17 9 11 39 4 13 11 13 14 4 | 26 32 30 35 49 31 31 29 36 30 29 32E | 11 24 7 8 38 4 16 13 19 12 5 | 30 39 35 35 28 32 23 30 40 31 31 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 17 9 10 36 5 17 10 11 17 |T 29 35 32 33 57 31 34 30 32 32 30 WRMS | 7 17 9 10 36 5 16 10 7 19 |NE 29 33 32 33 36 30 32 31 31 32 30 MEDI | 7 16 9 9 31 4 16 10 11 13 |MD 28 35 33 32 37 30 33 30 32 31 30 Table 3.1537.3 GPS week: 1537 Day: 3 MJD: 55006.000 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 | 2 --- --- --- --- 37 --- --- --- --- 0 | 31 --- --- --- --- 34 --- --- --- --- 32 2 | 8 20 10 9 33 5 19 10 15 32 5 | 24 28 23 20 27 21 27 26 29 32 23 3 | 6 11 7 6 45 3 10 4 8 15 3 | 35 33 38 37 50 36 36 37 36 37 35 4 | 8 14 7 10 62 6 10 9 15 11 4 | 27 25 28 29 37 24 21 28 31 28 26 6 | 6 10 6 6 35 4 13 5 7 15 3 | 27 25 28 27 22 26 22 27 30 23 25 7 | 5 16 7 16 29 4 14 7 12 13 4 | 23 26 25 26 49 22 28 21 25 20 21 8 | 8 19 7 9 20 5 19 6 11 10 4 | 18 27 22 22 31 18 27 18 27 17 19 9 | 8 17 7 8 22 4 14 9 9 12 3 | 19 28 19 21 28 19 27 17 22 18 19 10E | 13 22 12 12 57 4 16 10 21 16 5 | 19 28 24 23 32 20 26 21 22 24 18 11 | 7 14 10 9 75 5 17 5 13 18 4 | 29 36 37 37 50 32 39 29 26 31 30 12 | 11 26 8 9 28 7 18 7 9 13 4 | 26 37 21 21 29 22 30 25 25 20 23 13 | 6 16 7 8 32 5 20 8 10 11 3 | 20 29 25 22 46 21 30 21 25 22 21 14 | 8 20 13 8 23 4 17 7 13 13 4 | 26 35 31 31 33 28 33 26 35 28 29 15 | 5 17 10 13 35 5 22 9 14 15 4 | 20 30 23 24 45 22 31 20 23 24 21 16 | 7 23 10 11 45 4 24 7 12 16 4 | 22 36 22 20 38 22 35 18 29 19 21 17 | 8 20 11 14 25 5 18 8 11 21 5 | 24 29 24 33 36 25 27 24 27 28 24 18E | 7 20 9 9 22 5 17 5 10 8 3 | 22 28 24 21 36 20 28 20 28 20 21 19 | 7 14 11 8 46 6 17 6 10 20 4 | 26 30 29 25 48 26 32 25 31 29 26 20E | 7 20 14 12 24 5 17 5 13 12 4 | 22 29 28 23 35 23 29 21 23 19 22 21 | 9 19 9 8 44 4 21 4 6 19 4 | 20 25 19 21 35 19 29 19 25 18 19 22E | 9 16 7 5 31 5 14 5 10 8 3 | 25 28 23 23 35 23 28 22 31 21 24 23 | 6 21 11 11 28 4 22 7 6 20 4 | 19 31 26 21 46 21 30 19 23 22 20 24 | 8 14 10 6 28 4 11 8 9 11 3 | 28 27 33 30 32 29 28 25 29 24 27 25 | 7 15 8 7 17 5 16 11 12 22 4 | 28 35 27 30 818 30 33 23 31 30 27 26 | 6 14 10 9 28 5 12 11 7 8 3 | 21 20 17 20 34 20 25 18 20 16 18 27 | 7 22 6 7 23 4 13 7 9 12 3 | 20 32 20 22 35 20 25 17 21 19 19 28 | 9 17 9 9 52 4 20 7 9 14 4 | 20 26 17 19 43 17 24 19 24 15 18 29 | 7 17 14 8 38 7 21 8 11 31 5 | 21 28 26 24 37 25 32 19 22 31 21 30 | 8 21 7 12 38 5 17 7 12 29 5 | 28 33 29 32 42 28 30 27 32 39 28 31 | 8 21 8 9 34 5 16 7 11 12 4 | 20 31 25 22 43 22 28 21 26 23 21 32E | 11 26 10 11 57 5 15 11 26 10 5 | 25 28 25 28 44 22 19 22 31 22 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 9 10 38 5 17 8 12 17 |T 23 29 25 25 63 23 28 22 26 23 23 WRMS | 8 18 9 10 34 5 16 7 8 19 |NE 23 28 24 24 36 23 27 22 26 23 22 MEDI | 7 17 9 9 32 5 17 7 11 13 |MD 23 28 25 23 36 22 28 21 26 22 22 Table 3.1537.4 GPS week: 1537 Day: 4 MJD: 55007.000 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 --- --- --- --- 15 --- 10 17 --- 9 | 25 --- --- --- --- 33 --- 20 30 --- 21 2 | 9 17 9 7 41 6 17 10 14 33 5 | 19 25 19 20 25 23 28 23 25 33 20 3 | 7 14 7 6 28 5 9 5 9 18 3 | 23 21 19 26 27 21 19 21 24 18 20 4 | 10 15 7 7 46 5 10 6 13 12 3 | 22 25 22 24 29 24 19 26 28 30 24 6 | 7 12 6 6 29 5 10 7 6 17 3 | 24 20 21 28 17 22 19 25 28 22 23 7 | 9 19 9 13 40 4 14 9 12 14 4 | 23 32 27 27 45 24 31 28 32 29 25 8 | 9 18 6 8 21 5 16 13 12 13 4 | 15 26 20 20 28 20 24 25 22 25 19 9 | 9 17 9 10 20 3 14 8 13 13 4 | 10 23 15 15 25 15 24 14 18 20 13 10E | 13 23 10 12 44 6 16 12 19 18 5 | 17 28 22 24 45 23 27 21 26 24 19 11 | 7 16 8 8 63 5 16 5 11 18 4 | 22 31 28 27 36 23 34 21 23 24 23 12 | 13 26 9 9 51 6 20 9 6 15 4 | 25 35 24 22 33 24 32 29 30 27 25 13 | 5 19 9 7 29 6 26 11 10 12 4 | 12 30 17 18 40 17 31 18 18 19 16 14 | 9 19 11 6 33 4 14 6 9 10 3 | 16 26 20 20 38 17 24 15 21 19 17 15 | 5 20 10 9 29 5 21 8 12 15 4 | 11 27 17 20 32 16 27 14 18 22 14 16 | 7 22 9 9 44 4 24 7 14 17 4 | 16 28 17 16 27 18 31 16 22 18 17 17 | 10 18 10 14 18 5 21 11 13 22 5 | 18 24 21 26 24 17 21 22 22 27 19 18E | 9 26 10 9 31 3 17 8 11 8 4 | 27 39 28 28 30 27 36 28 29 27 28 19 | 7 14 8 7 38 6 15 8 8 22 4 | 30 30 28 31 36 26 32 26 30 28 28 20E | 8 21 7 9 28 4 11 4 12 11 3 | 17 28 21 19 35 18 26 17 26 18 18 21 | 9 18 7 10 56 3 19 6 11 21 4 | 20 26 19 18 57 18 29 20 24 19 20 22E | 10 14 10 7 27 4 14 4 8 6 3 | 15 21 19 17 26 14 24 13 18 13 15 23 | 7 22 8 9 34 4 19 7 8 20 4 | 13 30 19 18 38 15 29 14 18 21 15 24 | 11 17 8 5 35 3 11 8 7 10 3 | 20 22 24 20 28 20 23 20 23 20 21 X25 | 10 17 6 9 4979 6 --- 12 13 25 5 | 22 29 26 25 9999 25 --- 25 28 35 23 26 | 8 13 11 8 24 2 11 10 10 8 3 | 10 18 17 13 26 13 20 15 17 15 13 27 | 9 18 9 9 22 4 12 7 13 14 4 | 13 23 13 17 26 15 22 13 20 18 13 28 | 9 18 10 7 41 5 21 7 11 19 4 | 20 28 21 25 34 21 28 23 25 29 22 29 | 12 17 14 10 42 5 18 11 7 31 5 | 18 27 24 22 35 22 28 21 25 33 22 30E | 12 20 11 11 43 5 18 8 11 33 5 | 39 50 44 41 61 41 49 42 40 54 42 31 | 11 21 9 8 45 7 15 7 19 12 4 | 12 28 19 17 48 16 25 15 24 16 15 32E | 11 20 6 9 37 7 16 11 24 10 5 | 18 17 16 19 33 18 18 19 37 16 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 9 9 37 5 16 8 12 18 |T 19 27 21 22 33 20 26 20 24 23 20 WRMS | 9 19 9 9 35 5 15 7 9 19 |NE 17 24 19 20 31 18 24 19 22 22 18 MEDI | 9 18 9 9 35 5 16 8 11 15 |MD 18 27 20 20 33 20 27 21 24 22 20 Table 3.1537.5 GPS week: 1537 Day: 5 MJD: 55008.000 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 | 29 --- --- --- --- 15 --- 17 16 --- 15 | 33 --- --- --- --- 28 --- 26 30 --- 25 2 | 9 16 6 7 40 3 19 10 16 34 5 | 11 19 11 15 28 11 20 16 17 29 12 3 | 10 12 7 7 30 5 10 7 7 22 3 | 24 21 24 22 24 21 23 28 26 24 23 4 | 8 11 7 5 45 5 10 7 10 14 3 | 20 20 23 23 18 19 17 23 22 27 21 6 | 10 10 7 6 28 5 10 8 7 19 3 | 16 12 17 18 24 14 13 22 17 18 16 7 | 7 16 10 14 40 5 15 7 11 15 4 | 22 29 27 23 40 20 28 23 26 19 22 8 | 8 16 7 11 27 4 17 20 14 13 5 | 16 24 18 19 23 15 23 28 25 20 18 9 | 8 19 5 10 18 4 15 6 11 14 4 | 10 22 15 18 28 12 19 14 20 16 13 10E | 14 19 12 11 53 6 19 13 20 20 5 | 11 25 21 23 46 19 23 21 25 27 17 11 | 7 13 8 8 65 3 17 4 10 20 4 | 17 31 26 25 37 22 33 18 21 21 20 12 | 11 26 11 11 47 6 17 9 12 17 5 | 17 31 17 16 33 15 25 21 18 23 17 13 | 5 17 9 7 33 6 21 7 11 11 4 | 14 29 18 19 40 15 29 17 19 20 16 14 | 7 21 9 5 26 5 19 5 14 10 4 | 18 30 22 20 29 17 26 19 19 21 19 15 | 10 16 10 10 35 6 19 9 14 15 4 | 13 24 17 16 38 14 23 11 15 18 12 16 | 8 24 8 9 60 6 22 5 14 22 5 | 13 26 19 12 33 14 27 13 19 15 14 17 | 12 20 8 17 31 5 26 16 14 22 6 | 16 22 16 28 33 14 24 24 18 25 18 18E | 8 21 8 8 29 3 18 6 12 10 4 | 22 34 27 25 32 20 32 24 24 22 23 19 | 8 14 7 8 36 3 15 10 8 24 4 | 24 29 23 23 27 24 29 24 26 27 23 20E | 7 20 11 13 36 4 14 8 11 11 4 | 14 25 20 18 34 15 24 15 18 13 15 21 | 9 17 6 6 28 3 18 7 10 21 4 | 15 22 15 15 25 11 25 14 17 16 14 22E | 10 15 6 4 33 4 13 4 10 7 3 | 14 20 15 14 30 9 21 14 17 12 13 23 | 6 21 11 9 33 4 21 11 10 20 4 | 13 29 16 15 36 13 26 12 16 21 13 24 | 8 12 6 6 32 4 9 7 9 13 3 | 18 21 24 17 26 18 21 18 19 15 18 X25 | 9 21 13 12 --- 8 --- 8 12 --- 5 | 18 29 24 19 --- 17 --- 16 25 --- 18 26 | 7 13 9 7 24 4 14 9 13 7 3 | 8 15 14 9 25 8 17 14 11 12 9 27 | 8 17 6 7 20 4 12 6 8 16 3 | 11 21 14 15 30 12 19 11 20 14 12 28 | 8 18 9 7 42 7 24 14 11 18 5 | 17 23 16 19 34 14 25 22 23 24 18 29 | 12 18 12 9 31 5 18 13 9 30 5 | 13 21 18 15 27 14 22 14 15 27 14 30E | 12 22 9 8 43 5 19 9 12 31 5 | 31 37 32 31 44 32 37 34 31 48 32 31 | 10 21 8 8 37 5 17 6 12 12 4 | 9 25 16 14 38 9 23 11 14 10 11 32E | 10 47 9 9 56 5 18 14 22 14 6 | 20 50 17 21 34 19 18 19 38 19 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 8 9 38 5 17 10 12 18 |T 16 25 19 18 31 16 23 18 21 20 17 WRMS | 9 18 8 9 36 5 16 8 9 18 |NE 14 20 17 16 28 13 21 16 18 18 14 MEDI | 8 17 8 8 33 5 17 8 11 16 |MD 16 24 18 18 32 15 23 18 19 20 17 Table 3.1537.6 GPS week: 1537 Day: 6 MJD: 55009.000 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 | 18 --- --- --- --- 20 --- 15 33 --- 15 | 45 --- --- --- --- 61 --- 51 67 --- 51 2 | 9 14 8 5 32 4 16 11 14 37 5 | 25 25 23 25 27 23 28 28 27 40 24 3 | 11 13 9 12 50 6 11 11 15 22 4 | 27 24 26 31 31 25 21 32 26 28 26 4 | 9 13 9 6 40 5 11 9 19 17 4 | 29 28 30 30 25 26 21 30 28 34 27 6 | 10 13 8 12 40 7 12 13 15 20 4 | 27 23 28 34 23 26 22 35 27 30 27 7 | 6 19 11 12 40 3 19 6 18 14 5 | 23 30 24 24 54 22 32 21 23 23 23 8 | 8 16 7 9 30 3 13 25 17 13 5 | 20 27 21 26 30 20 26 27 21 22 21 9 | 12 17 7 9 25 5 13 9 16 14 4 | 22 25 23 23 31 18 27 23 25 23 22 10E | 17 23 9 9 49 5 17 15 28 22 6 | 25 27 25 21 46 21 25 26 25 28 21 11 | 9 14 7 9 62 5 16 8 12 20 4 | 28 34 33 36 43 30 35 29 29 32 29 12E | 24 26 9 11 40 10 23 13 15 16 6 | 42 47 35 34 55 29 42 30 36 29 34 13 | 5 16 12 12 31 4 22 8 16 12 5 | 23 29 25 25 44 21 33 21 22 20 22 14 | 9 23 11 8 25 5 17 7 19 10 4 | 26 36 30 30 44 27 33 26 28 28 28 15 | 8 19 9 14 37 4 16 11 16 16 5 | 22 28 22 24 41 21 28 20 22 25 20 16 | 7 24 7 14 38 6 22 8 13 20 5 | 18 32 18 19 31 16 29 16 20 16 17 17 | 12 22 10 15 25 5 20 21 12 22 6 | 25 31 28 37 32 25 31 32 29 33 27 18E | 9 20 12 10 27 5 19 11 12 13 5 | 26 32 34 26 42 24 34 24 28 24 26 19 | 8 15 7 11 35 4 16 11 13 26 5 | 45 45 45 44 54 42 48 41 44 41 44 20E | 12 22 10 12 34 7 13 7 14 22 5 | 21 32 24 23 35 22 29 22 23 24 22 21 | 8 18 6 9 33 6 19 8 11 21 4 | 21 26 18 20 43 17 30 19 20 16 17 22E | 10 14 7 8 41 4 13 9 10 10 3 | 21 26 23 24 44 20 30 20 24 19 21 23 | 8 21 13 17 25 3 24 12 11 20 5 | 21 32 26 25 38 20 33 23 26 24 22 24 | 10 15 7 5 27 4 10 11 10 14 3 | 28 25 29 29 34 26 24 27 28 24 26 X25 | 11 18 14 17 --- 16 --- 10 16 --- 6 | 23 27 23 31 --- 26 --- 21 27 --- 23 26 | 8 13 10 7 23 3 10 10 14 9 4 | 21 22 21 21 24 16 23 20 19 20 19 27 | 8 13 8 8 33 4 12 6 14 15 3 | 23 23 23 24 31 20 25 21 23 24 22 28 | 7 20 10 10 26 5 22 18 19 20 5 | 20 27 21 20 29 15 26 22 19 20 18 29 | 10 18 8 10 39 6 17 14 7 29 5 | 23 32 26 25 43 23 31 22 25 32 24 30E | 13 22 10 11 50 5 18 12 17 39 6 | 51 55 48 47 64 46 56 49 46 55 48 31 | 10 21 8 14 38 5 18 8 15 12 5 | 21 31 21 24 44 18 30 18 25 19 20 32E | 13 28 8 12 54 6 17 14 20 17 6 | 27 34 26 29 43 25 18 25 37 22 25 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 19 9 11 37 5 17 12 15 20 |T 26 30 26 27 38 24 30 26 28 26 25 WRMS | 9 19 9 11 36 5 16 10 15 19 |NE 23 26 23 24 32 20 26 23 23 25 22 MEDI | 9 18 9 10 35 5 17 11 15 17 |MD 23 28 25 25 41 23 29 24 26 24 23 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1537 GPS week: 1537 MJD: 55003.0-55009.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 |U 8 8 22 |U 8 15 40 |U 7 7 18 | emr | emr 2870 | 11 11 31 | 17 21 96 |U 7 9 22 | esa | esa 2880 | 8 8 27 |U 8 14 36 | 7 6 18 | gfz | gfz 2859 |U 9 8 28 |U 15 25 80 | 8 7 18 | grg | grg 2852 | 10 10 25 |U 10 16 40 | 9 8 23 | igr | igr 2871 | 8 8 23 | 7 15 39 | 7 7 17 | igs | igs 2848 | 9 9 24 | 8 14 44 | 7 7 17 | jpl | jpl 2816 |U 9 9 25 |U 9 18 48 |U 7 7 19 | mit | mit 2948 |U 8 9 25 |U 16 32 97 |U 8 8 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 5.1537.0 GPS week: 1537 Day: 0 MJD: 55003.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2966 | 7 8 17 | 6 9 27 | 5 6 21 | emr | emr 2872 | 12 10 19 | 15 13 93 | 7 8 22 | esa | esa 2880 | 8 8 19 | 6 8 29 | 5 5 21 | gfz | gfz 2861 | 8 9 19 | 14 23 68 | 5 5 19 | grg | grg 2880 | 9 12 24 | 9 8 37 | 7 6 22 | igr | igr 2879 | 7 9 17 | 5 11 30 | 5 5 19 | igs | igs 2876 | 8 9 16 | 7 10 36 | 5 5 20 | jpl | jpl 2780 | 9 10 21 | 6 10 29 | 6 6 21 | mit | mit 2880 | 10 14 31 | 11 16 78 | 10 9 18 | Table 5.1537.1 GPS week: 1537 Day: 1 MJD: 55004.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2962 | 7 8 21 | 6 12 26 | 5 6 15 | emr | emr 2872 | 11 10 32 | 14 14 103 | 6 9 20 | esa | esa 2880 | 8 8 24 | 6 8 27 | 6 6 16 | gfz | gfz 2860 | 8 8 23 | 14 22 77 | 6 8 16 | grg | grg 2880 | 9 9 22 | 8 11 40 | 7 9 22 | igr | igr 2875 | 8 9 22 | 5 10 32 | 5 7 15 | igs | igs 2874 | 8 8 22 | 5 9 30 | 5 6 15 | jpl | jpl 2870 | 8 8 24 | 8 12 49 | 5 8 18 | mit | mit 2976 | 9 8 24 | 16 21 107 | 7 6 20 | Table 5.1537.2 GPS week: 1537 Day: 2 MJD: 55005.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2943 | 7 5 17 | 7 12 29 | 8 7 19 | emr | emr 2872 | 11 9 24 | 15 20 91 | 8 9 19 | esa | esa 2880 | 7 5 18 | 5 10 21 | 9 7 18 | gfz | gfz 2860 | 8 6 24 | 12 19 66 | 8 7 16 | grg | grg 2880 | 9 9 18 | 9 15 40 | 10 9 22 | igr | igr 2876 | 8 5 18 | 6 14 32 | 8 7 15 | igs | igs 2783 | 7 5 16 | 6 13 31 | 7 7 14 | jpl | jpl 2871 | 8 6 18 | 6 15 33 | 8 8 17 | mit | mit 2976 | 7 5 16 | 11 17 66 | 8 7 16 | Table 5.1537.3 GPS week: 1537 Day: 3 MJD: 55006.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2930 | 7 7 17 | 5 7 41 | 10 7 23 | emr | emr 2872 | 10 11 19 | 15 13 97 | 7 10 26 | esa | esa 2880 | 9 8 27 | 5 8 34 | 8 7 22 | gfz | gfz 2860 | 7 6 19 | 14 16 89 | 9 7 20 | grg | grg 2880 | 8 7 22 | 8 12 47 | 10 7 24 | igr | igr 2878 | 7 7 17 | 4 8 43 | 9 7 20 | igs | igs 2878 | 9 8 30 | 5 9 43 | 9 7 21 | jpl | jpl 2872 | 7 9 20 | 9 12 57 | 8 8 20 | mit | mit 2880 | 7 5 21 | 12 14 81 | 9 7 21 | Table 5.1537.4 GPS week: 1537 Day: 4 MJD: 55007.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2964 | 7 7 23 | 6 10 27 | 6 7 16 | emr | emr 2872 | 10 13 31 | 15 15 97 | 8 9 21 | esa | esa 2880 | 7 7 24 | 5 8 23 | 6 7 18 | gfz | gfz 2860 | 7 9 26 | 15 22 78 | 7 7 19 | igr | igr 2878 | 7 7 23 | 6 10 34 | 6 8 17 | igs | igs 2923 | 7 7 25 | 6 11 38 | 6 8 17 | jpl | jpl 2776 | 9 8 30 | 8 13 35 | 6 7 19 | mit | mit 2976 | 8 7 26 | 11 13 64 | 8 11 22 | Table 5.1537.5 GPS week: 1537 Day: 5 MJD: 55008.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 | 10 12 32 | 25 43 103 | 8 6 17 | emr | emr 2868 | 15 13 43 | 28 44 106 | 9 8 25 | esa | esa 2880 | 12 12 36 | 23 43 90 | 8 7 18 | gfz | gfz 2855 | 12 11 37 | 24 41 104 | 10 7 19 | grg | grg 2784 | 13 12 39 | 16 34 48 | 10 8 25 | igr | igr 2835 | 11 13 37 | 15 36 66 | 9 7 19 | igs | igs 2775 | 11 12 35 | 18 35 106 | 9 7 19 | jpl | jpl 2774 | 13 13 40 | 21 49 84 | 8 7 23 | mit | mit 2976 | 11 10 34 | 36 109 207 | 11 11 22 | Table 5.1537.6 GPS week: 1537 Day: 6 MJD: 55009.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2953 | 8 11 24 | 6 13 27 | 7 8 16 | emr | emr 2868 | 12 13 49 | 15 26 83 | 7 11 24 | esa | esa 2880 | 9 10 44 | 6 12 26 | 7 8 16 | gfz | gfz 2857 | 9 10 47 | 14 31 79 | 7 7 16 | grg | grg 2784 | 10 10 26 | 10 16 30 | 9 8 26 | igr | igr 2879 | 9 10 28 | 7 17 33 | 7 8 15 | igs | igs 2831 | 10 13 26 | 6 10 27 | 7 8 16 | jpl | jpl 2771 | 8 11 25 | 8 18 51 | 8 9 16 | mit | mit 2976 | 7 12 25 | 14 32 79 | 7 7 20 | 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 6.1537 GPS week: 1537 MJD: 55003.500-55009.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -8 -37 122 -68 -2 | -2 27 | 15 21 117 54 6 | 5 emr uuuxx | 25 0 -54 360 31 | -14 43 | 12 22 135 105 18 | 12 esa uuuux | -28 -13 -146 21 -6 | -17 29 | 24 24 105 112 37 | 3 gfz uuuuu | -15 -15 60 -47 -8 | 7 26 | 14 17 84 51 5 | 3 grg xxxxx | -34 20 109 -51 4 | -4 26 | 28 27 92 63 44 | 2 igr xxxxx | -12 28 -34 -29 5 | -8 27 | 19 17 71 78 10 | 3 irf xxxxx | 2 0 11 25 4 | -7 27 | 7 12 31 40 5 | 5 jpl uuuuu | -27 -17 53 -40 6 | -6 30 | 33 34 90 132 13 | 7 mit uuuuu | -30 -13 120 23 10 | -2 31 | 16 20 147 40 11 | 5 ngs uuuxu | 43 21 4 176 -3 | 0 23 | 35 72 151 283 14 | 3 sio uuuuu | 111 96 -49 53 4 | 5 30 | 16 18 121 61 13 | 3 Table 7.1537.0 GPS week: 1537 Day: 0 MJD: 55003.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 7 -5 118 -70 2 | -8 23 emr uuuxx | 20 12 14 271 23 | -30 37 esa uuuux | -40 20 -208 101 -30 | -14 28 gfz uuuuu | -2 1 52 -49 -9 | 6 21 grg xxxxx | -37 68 11 -16 23 | -3 26 igr xxxxx | -35 51 -129 -111 -1 | -11 23 irf xxxxx | 1 11 73 19 -2 | -12 23 jpl uuuuu | -45 -69 38 -35 26 | -16 25 mit uuuuu | -27 2 315 -10 1 | -8 25 ngs uuuxu | 25 -45 -190 102 -3 | -1 17 sio uuuuu | 101 104 99 -31 -6 | 4 26 Table 7.1537.1 GPS week: 1537 Day: 1 MJD: 55004.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -21 -21 18 -25 5 | -9 22 emr uuuxx | 18 -29 164 209 51 | -31 37 esa uuuux | 15 8 -75 107 -48 | -19 30 gfz uuuuu | -31 -24 -91 -32 -12 | 3 18 grg xxxxx | -71 4 37 -80 -66 | -2 27 igr xxxxx | -25 28 -70 -129 0 | -14 22 irf xxxxx | 2 6 20 7 6 | -15 22 jpl uuuuu | -38 -14 -96 -227 12 | -14 26 mit uuuuu | -31 -5 236 16 16 | -11 23 ngs uuuxu | -6 -5 -74 277 -9 | -3 16 sio uuuuu | 119 104 20 43 8 | -2 19 Table 7.1537.2 GPS week: 1537 Day: 2 MJD: 55005.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -3 -34 -74 -128 -6 | 1 27 emr uuuxx | 7 -18 64 275 48 | -18 45 esa uuuux | -18 -16 -163 135 -43 | -15 26 gfz uuuuu | -17 -2 8 -71 -12 | 10 25 grg xxxxx | -30 -7 -9 -122 -34 | -2 27 igr xxxxx | 8 19 79 -90 -2 | -8 27 irf xxxxx | -7 14 8 -26 6 | -7 27 jpl uuuuu | 27 17 74 -182 14 | -4 30 mit uuuuu | -34 11 174 16 21 | -3 32 ngs uuuxu | 1 -55 -130 -187 -19 | 4 23 sio uuuuu | 99 121 81 21 16 | 5 30 Table 7.1537.3 GPS week: 1537 Day: 3 MJD: 55006.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -18 -43 126 -109 -9 | 6 27 emr uuuxx | 43 18 -120 413 43 | -9 46 esa uuuux | -31 -25 -242 75 -7 | -14 24 gfz uuuuu | 4 -34 54 -104 -15 | 13 26 grg xxxxx | -16 3 187 -69 35 | -6 27 igr xxxxx | 4 3 4 25 2 | -4 26 irf xxxxx | -8 0 4 -6 12 | -2 27 jpl uuuuu | -5 34 212 -55 8 | 2 31 mit uuuuu | -57 -2 151 12 26 | 3 34 ngs uuuxu | 61 -13 -44 -91 -14 | 6 23 sio uuuuu | 87 103 -70 78 20 | 8 33 Table 7.1537.4 GPS week: 1537 Day: 4 MJD: 55007.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 16 -64 256 -103 -9 | 1 31 emr uuuxx | 40 -16 -152 467 31 | -8 46 esa uuuux | -30 0 -281 -24 5 | -20 32 gfz uuuuu | -5 -39 137 -76 -6 | 7 30 grg xxxxx | 16 0 194 -62 -4 | -5 26 igr xxxxx | 0 48 0 65 0 | -7 30 irf xxxxx | 6 0 4 32 5 | -6 29 jpl uuuuu | -73 -18 68 -4 -5 | -2 33 mit uuuuu | -35 -21 104 57 11 | 0 34 ngs uuuxu | 74 54 109 262 -5 | 0 28 sio uuuuu | 112 96 -82 76 8 | 5 33 Table 7.1537.5 GPS week: 1537 Day: 5 MJD: 55008.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -21 -33 205 -67 5 | -1 30 emr uuuxx | 23 5 -192 446 19 | -4 47 esa uuuux | -30 -26 -57 -152 36 | -21 32 gfz uuuuu | -22 3 112 -51 -2 | 7 30 grg xxxxx | -51 40 178 -81 9 | -5 26 igr xxxxx | 0 27 -25 15 14 | -8 30 irf xxxxx | 6 -5 -18 51 2 | -5 29 jpl uuuuu | -44 -36 37 89 -10 | -3 33 mit uuuuu | -26 -31 -50 93 1 | 1 35 ngs uuuxu | 72 61 210 193 12 | -2 28 sio uuuuu | 118 86 -191 163 -5 | 6 33 Table 7.1537.6 GPS week: 1537 Day: 6 MJD: 55009.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -18 -59 207 26 -6 | 0 31 emr uuuxx | 23 31 -158 440 3 | 1 47 esa uuuux | -64 -52 2 -98 43 | -18 33 gfz uuuuu | -33 -10 147 57 -2 | 6 30 grg xxxxx | -52 32 167 74 66 | -5 26 igr xxxxx | -35 21 -98 23 25 | -7 30 irf xxxxx | 13 -22 -17 95 -3 | -4 29 jpl uuuuu | -12 -28 41 136 -6 | -3 33 mit uuuuu | -2 -45 -92 -22 -4 | 2 35 ngs uuuxu | 70 149 145 679 20 | 0 29 sio uuuuu | 137 63 -201 20 -16 | 7 34