Date: Thu, 21 May 2009 11:55:21 +0000 From: Jim Ray Subject: [IGSREPORT-17418] Wk 1530 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4a154129.gwzfkwvVT9vYi+73%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 21 May 04:55:44 PDT 2009 Message Number 17418 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1530 (May 03, 2009 - May 09, 2009) 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: igs1530[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1530[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1530[0-6].cls IGS GPS clock combination summary report. igs15307.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15307.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 | 4 9 27 4 0 | EMR | WTZR MIZU WTZR 0 | ESA | DAEJ 0 | GFZ | 7 29 LPGS MATE SUTM UNSA 0 | GRG | PIE1 0 | JPL | 4 MDVJ NLIB 0 | MIT | 5 24 5 NLIB 1 | ALL | 1 1 1 | COD | MKEA 1 | EMR | MIZU 1 | GFZ | 7 29 CHUR DAV1 FAA1 1 | GRG | DAV1 NLIB NOVM 1 | JPL | 4 1 | MIT | 5 8 10 5 8 10 MATE 2 | EMR | MIZU 2 | GFZ | 7 29 FAA1 HYDE 2 | GRG | NLIB POTS 2 | MIT | 8 10 20 29 30 8 10 20 29 30 2 | NGS | 1 3 | ALL | 1 1 3 | COD | 9 27 9 27 RCMN 3 | EMR | KHAJ MIZU 3 | ESA | 9 27 GUAT 3 | GFZ | 7 29 ALIC AUCK CHUR NICO ONSA 3 | GRG | NLIB 3 | JPL | UNSA 3 | MIT | 5 8 5 8 GUAT 4 | ALL | 1 1 4 | COD | 27 27 4 | EMR | MIZU SCH2 4 | ESA | 27 4 | GFZ | 7 29 CHUR DAEJ NICO 4 | GRG | KERG NLIB POTS 4 | JPL | 25 HARB ZWE2 4 | MIT | 5 8 5 8 5 | COD | 27 NLIB 5 | EMR | SYOG KHAJ MIZU YELL 5 | ESA | 5 9 27 REYK 5 | GFZ | 7 29 CHUR FAA1 MAW1 5 | GRG | KHAJ PIE1 5 | JPL | 8 24 25 5 | MIT | 5 8 5 8 HOB2 5 | NGS | 1 6 | ALL | 1 1 6 | COD | 9 27 6 | EMR | ALBH ALBH MIZU 6 | ESA | 5 9 27 HOLM 6 | GFZ | 7 29 CHUR FAA1 OHI2 6 | GRG | NLIB NOVM TWTF 6 | JPL | 8 6 | MIT | 5 8 5 8 25 CHUR 5. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G24 | 2 | | | | | | 1 | 6. 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. 7. 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 .1 .5 -19 -5 -13 -.02 EMR | 11.7 -9.0 -17.5 50 -36 69 .29 ESA | 3.7 -1.8 -4.5 -24 -77 18 -.14 GFZ | .4 .8 .9 28 -20 13 -.23 GRG | 4.8 -2.3 -1.9 -5 -18 35 -.03 JPL | 3.9 -2.5 -7.4 13 -19 2 .39 MIT | 8.2 -13.1 -6.1 -4 15 -19 -.04 NGS | 9.5 -8.0 -2.2 -107 -148 19 .04 SIO | 2.8 -1.2 -18.9 -7 -103 -10 .29 8. 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. 9. 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. 10. 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 1.1530.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1530.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 2.1530.[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 3.1530.[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 5.1530.0-6). 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 1530 summary. (May 03, 2009 - May 09, 2009) Table 1.1530.a GPS week: 1530 MJD: 54954.000-54960.000 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 237| 0 0 0 4 -59 -16 -.15 9 8 | -476 -12 25 76 | 0 0 0 7 16 25 .03 | 381 590 emr 77| -1 -1 1 -103 48 -7 .43 21 21 | -141220 -442 23 100 | 1 1 1 25 11 13 .03 | 378688 1420 esa 123| 1 0 0 -33 -15 18 .30 10 10 | -96 -1324 22 139 | 0 0 1 26 17 21 .03 | 930 1721 gfz 194| 1 0 3 -78 -26 51 -.04 11 11 | 301 -263 24 166 | 0 1 1 18 9 54 .02 | 232 285 grg 111| 0 0 0 -38 10 -19 1.00 37 34 | 86 -138 87 218 | 1 1 2 30 15 57 .03 | 389 530 igr n/a| 0 0 0 -39 -66 -4 .06 6 6 | 16813 445 21 66 | 0 0 0 22 19 23 .02 | 2650 1353 jpl 131| 0 0 -2 -54 -11 8 .50 20 19 | 1392 -225 21 94 | 1 0 1 16 14 32 .02 | 1448 1359 mit 260| 0 0 -4 -17 -108 -37 -.26 12 10 | -12778 706 23 130 | 1 0 1 14 27 12 .02 | 6098 3394 ngs 226| 0 0 0 214 197 1 -.32 13 8 | 17492 79616 2316 4098 | 1 1 2 35 30 21 .02 | 48315 140111 sio 253| -2 2 4 -10 122 -33 -.06 25 22 | --- --- --- --- | 1 1 1 25 20 21 .01 | --- --- Table 1.1530.b GPS week : 1530 MJD: 54954.000-54960.000 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 16 18 19 12 12 16 | 2 | 6 5 6 6 6 6 6 | 3 | 4 4 3 4 3 4 4 | 4 | 7 7 7 8 6 6 6 | 5 | 7 6 7 8 6 7 7 | 6 | 4 5 4 4 4 4 5 | 7 | 4 5 5 5 5 5 5 | 8 | 6 6 6 7 6 7 7 | 9 | 5 5 5 5 5 5 5 | 10 | 4 4 4 4 4 4 4 | 11 | 5 5 5 4 5 4 4 | 12 | 6 6 5 6 6 6 6 | 13 | 5 5 5 5 5 5 5 | 14 | 5 5 5 5 5 5 5 | 15 | 5 6 6 6 6 6 5 | 16 | 5 6 5 6 5 5 6 | 17 | 5 6 5 5 5 6 6 | 18 | 5 5 5 5 5 6 5 | 19 | 6 6 5 6 6 5 5 | 20 | 5 6 5 5 5 5 4 | 21 | 5 5 4 4 5 6 5 | 22 | 5 5 5 5 5 5 5 | 23 | 5 7 5 5 5 5 5 | 24 | 7 11 8 7 7 7 8 | 25 | 7 7 7 7 6 6 6 | 26 | 4 4 4 4 4 5 4 | 27 | 5 6 6 6 6 7 7 | 28 | 5 5 5 5 6 6 6 | 29 | 6 6 6 5 5 5 5 | 30 | 4 4 4 4 4 4 4 | 31 | 5 4 5 5 5 6 6 | 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 2.1530.0 GPS week: 1530 Day: 0 MJD: 54954.000 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 237| 0 -1 0 -6 -41 -26 -.15 9 8 | -525 -99 29 75 | 69 -30 | emr 77| 0 -1 1 -92 49 -12 .45 21 21 | 3223 -2718 29 86 | -10 -92 | esa 123| 2 0 -1 -48 -38 11 .32 10 10 | 234 -2795 23 126 | 75 44 | gfz 194| 1 0 1 -93 -20 68 -.01 10 10 | 585 -583 27 173 | 48 -42 | grg 111| 1 0 0 -99 18 -15 .95 38 36 | 836 -1095 90 203 | 151 -36 | igr n/a| 0 0 1 -51 -45 -12 .06 6 6 | 15038 -1589 22 60 | 43 -47 | jpl 131| 0 1 -4 -84 -20 -23 .50 21 20 | 1783 -2429 22 88 | 15 -42 | mit 260| -1 0 -3 4 -134 -35 -.24 12 10 | 521 -762 25 105 | 6 13 | ngs 226| 0 1 3 221 220 0 -.33 12 7 | -530 -157 2340 4290 | -59 -43 | sio 253| -4 2 2 15 113 -15 -.05 26 24 | --- --- --- --- | 19 -112 | Table 2.1530.1 GPS week: 1530 Day: 1 MJD: 54955.000 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 237| 0 0 0 7 -67 -34 -.12 10 9 | -782 -126 32 85 | 8 -47 | emr 77| -3 0 0 -104 53 5 .44 23 23 | 1266 -1211 27 94 | 3 -134 | esa 123| 0 0 0 -59 -16 56 .36 12 11 | -378 -248 24 150 | 116 35 | gfz 194| 2 1 4 -106 -27 -24 -.03 12 12 | 248 -44 24 159 | 26 -44 | grg 111| 0 1 1 -12 6 -95 1.02 40 32 | -196 160 87 212 | 21 -52 | igr n/a| 0 0 0 -21 -53 36 .08 7 7 | 14222 67 24 67 | 5 -47 | jpl 131| 0 0 -4 -47 -2 -2 .49 20 19 | 190 -680 24 93 | 9 -59 | mit 260| -1 0 -3 -35 -135 -17 -.28 12 10 | -15521 146 32 141 | 2 9 | ngs 226| 0 0 2 263 231 43 -.35 14 8 | 119903 351793 1914 3909 | -108 -48 | sio 253| 0 2 4 -35 83 -1 -.05 25 23 | --- --- --- --- | 23 -79 | Table 2.1530.2 GPS week: 1530 Day: 2 MJD: 54956.000 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 237| 0 0 0 0 -89 2 -.12 9 8 | -920 957 32 103 | 35 16 | emr 77| 0 0 0 -117 40 -4 .47 23 23 | 409 -525 27 91 | -1 -125 | esa 123| 1 0 -1 -67 7 -1 .32 10 10 | 1271 -2925 29 156 | 72 -14 | gfz 194| 1 -1 2 -84 -32 106 -.01 11 11 | 582 -586 28 166 | 24 -7 | grg 111| -1 0 2 -49 -20 72 1.01 35 29 | 225 -423 92 227 | 89 68 | igr n/a| 0 0 0 -48 -99 -12 .07 6 6 | 14595 701 23 65 | 67 9 | jpl 131| 1 0 -3 -53 -23 4 .47 20 19 | -92 105 22 90 | 11 -29 | mit 260| -1 0 -3 -14 -59 -59 -.25 11 10 | -15589 557 28 157 | 12 -2 | ngs 226| 0 0 1 245 152 -14 -.32 13 8 | 8877 4739 2531 4105 | -95 56 | sio 253| 0 0 6 -39 137 -62 -.06 25 23 | --- --- --- --- | 49 -84 | Table 2.1530.3 GPS week: 1530 Day: 3 MJD: 54957.000 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 237| 0 0 0 7 -60 -49 -.15 11 8 | -36 -770 19 56 | 17 -17 | emr 77| -2 -2 1 -114 68 -12 .43 20 20 | 175 1290 20 91 | 13 -116 | esa 123| 0 0 0 -13 -10 4 .27 9 8 | 809 -3030 18 131 | 73 28 | gfz 194| 1 1 2 -64 -35 114 -.04 10 10 | 68 -301 22 171 | 27 -48 | grg 111| 0 -1 -2 -13 23 -78 .97 35 33 | -299 283 81 202 | 89 13 | igr n/a| 0 0 0 -39 -50 -38 .05 6 6 | 15375 2180 19 70 | 12 -39 | jpl 131| -1 0 -3 -44 8 12 .47 19 19 | -86 1401 20 92 | 2 -13 | mit 260| 0 0 -5 -25 -107 -37 -.27 12 10 | -16913 6987 19 108 | 6 22 | ngs 226| 1 0 2 207 192 -11 -.33 14 9 | -36417 195365 1960 3911 | -43 -45 | sio 253| -1 1 6 -3 134 -55 -.07 24 20 | --- --- --- --- | 28 -118 | Table 2.1530.4 GPS week: 1530 Day: 4 MJD: 54958.000 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 237| 0 0 0 5 -50 -11 -.16 9 8 | -524 200 22 70 | 27 -19 | emr 77| -3 0 0 -129 54 14 .41 21 21 | -999999 1229 23 109 | 23 -105 | esa 123| 1 0 0 4 -34 11 .28 8 8 | -521 -639 20 140 | 77 53 | gfz 194| 1 0 5 -81 -33 79 -.07 11 11 | 215 175 26 177 | 24 -36 | grg 111| -2 0 -2 -36 19 5 .98 37 35 | -98 467 89 266 | 87 -22 | igr n/a| 0 0 0 -80 -70 -11 .03 6 6 | 17907 2103 21 67 | 8 6 | jpl 131| 0 0 -3 -69 3 -15 .49 20 20 | 1621 1424 19 92 | 31 -17 | mit 260| 0 -1 -5 -2 -122 -41 -.28 12 10 | -16077 2669 23 143 | 1 22 | ngs 226| 0 0 0 166 226 -20 -.30 13 9 | 11073 3451 3051 4483 | -30 -64 | sio 253| -1 1 6 27 115 -23 -.05 24 20 | --- --- --- --- | 17 -137 | Table 2.1530.5 GPS week: 1530 Day: 5 MJD: 54959.000 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 237| 0 0 -2 16 -68 -24 -.18 9 8 | 115 -619 25 73 | -11 15 | emr 77| 0 -4 2 -113 39 -29 .40 20 20 | 3620 -1084 19 108 | -12 -83 | esa 123| 0 1 2 -15 -15 41 .28 10 10 | -639 -1227 21 139 | 59 38 | gfz 194| 1 0 3 -59 -8 11 -.06 11 11 | 405 -394 23 165 | -13 -40 | grg 111| 3 -1 -2 -36 23 11 1.00 37 35 | 250 -348 84 213 | 70 24 | igr n/a| 0 0 0 -17 -83 3 .05 6 6 | 20435 -423 22 71 | -22 4 | jpl 131| 0 -1 0 -38 -17 75 .52 20 19 | 3529 -924 21 100 | -6 -36 | mit 260| 0 -1 -4 -16 -86 -34 -.26 13 11 | -11738 -3896 22 146 | 4 36 | ngs 226| -1 0 -1 173 163 11 -.30 14 8 | 14905 -8832 1925 3666 | 39 -96 | sio 253| -2 5 3 -14 134 -30 -.07 25 22 | --- --- --- --- | 41 -109 | Table 2.1530.6 GPS week: 1530 Day: 6 MJD: 54960.000 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 237| 1 0 0 4 -42 27 -.18 8 7 | -663 372 18 73 | -15 -34 | emr 77| -1 -3 3 -53 36 -10 .41 20 20 | 2766 -81 22 124 | -59 -90 | esa 123| 1 0 1 -37 1 4 .28 10 10 | -1453 1592 19 137 | 95 32 | gfz 194| 0 1 1 -57 -30 6 -.03 10 10 | 4 -108 20 157 | 11 -32 | grg 111| 0 -1 0 -21 2 -36 1.04 40 37 | -113 -12 88 204 | 8 22 | igr n/a| 0 0 0 -21 -66 6 .07 6 7 | 20125 76 20 66 | 4 20 | jpl 131| -1 0 -1 -42 -28 9 .52 20 19 | 2802 -477 20 108 | -10 -21 | mit 260| 0 0 -2 -29 -113 -35 -.24 13 11 | -14132 -758 17 114 | 7 22 | ngs 226| -1 -2 -3 223 197 0 -.31 14 10 | 4633 10957 2494 4327 | -40 47 | sio 253| -4 3 2 -26 140 -41 -.08 27 21 | --- --- --- --- | 28 -138 | 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 3.1530.0 GPS week: 1530 Day: 0 MJD: 54954.000 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 | 3 --- --- --- --- 33 --- --- --- --- 0 | 42 --- --- --- --- 49 --- --- --- --- 41 2E | 8 29 11 11 31 5 22 13 8 26 5 | 24 35 28 27 36 24 27 22 24 23 24 3 | 6 13 7 8 36 5 14 8 7 17 3 | 42 44 43 45 37 44 42 43 44 40 44 4E | 12 29 10 9 58 6 20 18 21 26 6 | 109 112 108 111 119 111 110 116 115 117 111 X5 | 10 25 13 --- --- 14 --- 8 16 --- 7 | 25 24 24 --- --- 23 --- 24 41 --- 27 6 | 7 14 6 10 31 6 18 11 8 14 4 | 26 26 28 32 31 27 23 27 28 28 27 7E | 8 19 10 9 32 4 21 9 7 16 4 | 31 37 34 34 42 30 35 30 30 31 32 8E | 15 25 12 7 19 7 18 16 17 21 6 | 32 41 34 34 41 34 36 34 48 37 35 9E | 8 21 7 8 72 4 21 10 13 15 4 | 19 28 26 23 44 20 30 21 26 21 22 10 | 6 17 10 7 13 5 12 13 8 22 4 | 14 18 13 16 21 13 16 17 16 20 14 11 | 8 17 10 11 50 7 17 13 8 21 4 | 15 17 16 17 44 13 17 17 19 20 17 12 | 7 24 10 9 25 6 22 8 10 41 5 | 26 33 29 28 41 26 30 25 30 46 28 13 | 6 21 13 8 56 5 23 9 10 25 4 | 20 34 33 25 55 22 32 20 27 18 25 14 | 7 25 11 10 32 5 22 7 7 18 4 | 21 31 28 30 35 25 30 25 24 22 25 15 | 8 22 13 8 32 7 26 10 8 25 5 | 21 31 25 27 36 20 28 26 23 29 23 16 | 7 21 9 10 36 6 24 13 10 27 5 | 24 35 31 30 32 28 33 26 32 27 29 17 | 7 16 8 10 39 7 21 11 7 38 5 | 17 26 20 16 43 18 31 19 21 27 19 18 | 8 24 7 11 38 3 27 10 7 21 5 | 18 31 22 26 37 19 30 21 21 26 22 19 | 7 22 10 10 28 9 24 12 7 35 5 | 23 32 20 19 32 20 33 24 25 28 23 20 | 9 21 12 11 32 7 24 13 6 29 5 | 19 26 25 23 39 17 24 23 19 24 21 21E | 8 20 9 9 43 2 18 9 11 20 4 | 24 38 25 20 38 24 34 23 24 29 25 22 | 7 23 8 11 53 4 28 10 6 17 4 | 19 30 25 27 40 21 27 26 21 23 23 23 | 8 22 11 9 41 4 23 10 9 29 5 | 51 58 56 56 78 51 60 54 53 52 55 24E | 19 22 13 13 29 5 18 15 28 32 7 | 140 152 152 139 157 144 152 147 134 141 143 25E | 14 22 17 10 28 9 20 22 24 22 7 | 49 62 57 55 66 51 62 60 59 56 55 26 | 8 17 9 7 24 6 16 10 7 19 4 | 20 27 21 23 32 16 25 20 20 17 21 27E | 8 19 8 7 49 4 19 12 21 18 5 | 23 29 23 22 40 20 28 27 31 28 24 28 | 7 21 13 10 30 6 21 9 12 34 5 | 24 37 27 29 44 26 34 26 26 25 26 29 | 10 21 8 9 28 7 19 10 9 50 5 | 18 32 22 20 35 19 33 25 22 45 22 30 | 6 16 6 7 20 6 14 5 9 26 3 | 36 30 38 38 43 35 29 33 38 36 37 31E | 6 18 9 10 34 6 21 9 10 25 4 | 16 25 22 21 36 17 22 15 22 25 20 32 | 8 20 9 15 38 6 18 11 10 25 5 | 17 19 27 25 42 17 17 18 22 14 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 21 10 10 38 6 21 12 12 26 |T 31 38 34 34 47 32 37 33 35 35 33 WRMS | 8 21 10 10 36 6 20 10 7 24 |NE 24 30 27 27 39 24 29 25 27 28 26 MEDI | 8 21 10 9 32 6 21 10 9 25 |MD 23 31 27 27 40 23 30 25 26 27 25 Table 3.1530.1 GPS week: 1530 Day: 1 MJD: 54955.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 19 --- --- --- --- 31 --- 28 19 --- 16 | 36 --- --- --- --- 53 --- 32 34 --- 38 2E | 8 25 11 11 35 5 23 12 10 22 5 | 26 38 34 31 40 32 33 34 31 36 31 3 | 7 15 10 14 26 8 12 9 7 17 4 | 38 34 41 41 41 37 35 35 36 33 36 4E | 12 29 15 10 44 7 19 15 23 28 6 | 75 75 72 76 76 73 76 74 81 78 74 X5 | 7 24 15 --- --- 13 --- 8 11 --- 6 | 13 24 21 --- --- 22 --- 15 24 --- 17 6 | 9 17 10 14 27 9 13 9 8 16 4 | 19 21 26 27 28 22 21 18 18 25 20 7E | 7 20 12 13 24 6 23 9 10 12 4 | 31 38 33 27 38 33 37 35 40 34 32 8E | 16 23 12 12 28 6 16 12 20 16 6 | 32 41 36 41 51 33 39 36 42 39 36 9E | 7 21 10 7 61 6 20 10 14 13 4 | 15 27 22 13 35 18 27 19 21 20 16 10 | 7 20 12 11 21 9 12 9 6 21 4 | 15 21 19 20 19 16 16 18 18 24 16 11 | 8 20 12 10 51 8 17 14 7 19 4 | 12 22 20 19 43 15 19 20 23 23 19 12 | 8 22 11 11 26 6 22 8 10 39 5 | 16 28 24 19 29 20 26 19 24 42 21 13 | 9 25 10 10 44 7 23 10 10 19 5 | 18 33 22 16 42 20 29 20 22 17 18 14 | 10 26 10 13 34 6 22 9 10 17 5 | 16 32 26 25 34 20 28 21 23 23 21 15 | 10 21 11 13 32 5 24 12 8 33 5 | 16 26 23 23 34 17 25 23 17 32 17 16 | 10 25 8 10 34 7 24 12 10 26 5 | 17 26 20 18 30 16 27 15 17 18 17 17 | 7 20 13 12 31 3 23 9 10 33 5 | 11 26 15 13 32 12 25 12 16 20 13 18 | 9 29 10 12 41 8 23 10 7 19 5 | 16 36 24 21 37 22 29 22 20 24 21 19 | 11 27 13 15 32 12 24 10 9 34 6 | 15 26 17 15 25 14 25 18 25 22 18 20 | 14 26 14 10 36 8 25 14 8 25 6 | 15 30 23 20 34 17 26 22 25 23 19 21E | 7 21 10 13 73 8 17 8 10 15 4 | 20 33 25 17 72 21 31 19 23 23 22 22 | 10 22 10 11 47 5 23 11 9 13 5 | 16 30 25 25 36 21 29 22 20 21 22 23 | 12 29 13 14 85 8 24 21 11 32 7 | 113 112 108 112 84 104 110 109 106 108 107 24E | 22 24 16 18 25 11 21 21 41 56 10 | 112 121 119 104 131 114 124 119 121 114 115 25E | 14 24 16 13 31 9 23 21 21 17 7 | 43 55 51 47 63 49 55 56 54 46 48 26 | 7 19 11 7 20 5 14 8 10 19 4 | 13 24 20 15 25 16 21 18 18 15 15 27E | 7 21 8 9 53 7 19 13 21 18 5 | 23 28 24 20 28 21 26 27 32 32 22 28 | 7 20 11 10 34 4 21 7 8 29 5 | 19 30 25 21 47 20 30 19 22 20 20 29 | 13 22 13 15 28 10 20 9 13 38 6 | 16 27 23 10 28 17 26 19 20 33 18 30 | 8 17 10 9 24 6 13 6 7 24 4 | 22 25 28 25 35 25 21 23 27 29 25 31E | 7 19 9 12 30 5 16 9 9 16 4 | 14 25 19 16 29 17 21 15 20 21 16 32 | 10 21 14 11 34 7 21 8 7 22 5 | 13 18 21 14 28 13 15 16 20 18 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 23 12 12 40 7 20 12 14 25 |T 27 36 32 29 42 29 35 30 32 33 29 WRMS | 9 23 11 12 32 7 19 10 8 23 |NE 22 31 27 24 35 24 29 24 26 28 24 MEDI | 9 22 11 11 32 7 21 10 10 19 |MD 16 28 24 20 35 20 27 20 23 24 20 Table 3.1530.2 GPS week: 1530 Day: 2 MJD: 54956.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 20 --- --- --- --- 27 --- 30 26 --- 18 | 38 --- --- --- --- 29 --- 26 39 --- 35 2E | 7 25 10 14 26 8 22 14 14 28 5 | 18 30 21 23 32 21 27 21 21 24 18 3 | 4 14 6 9 21 4 11 6 6 14 3 | 27 29 30 31 28 28 27 24 22 24 25 4E | 11 31 11 12 33 8 19 18 23 35 7 | 102 110 106 108 114 105 109 108 111 104 106 X5 | 12 22 9 --- --- 17 --- 9 20 --- 7 | 17 26 22 --- --- 22 --- 19 30 --- 18 6 | 6 17 6 12 21 5 12 7 5 13 3 | 20 23 23 26 28 20 20 22 20 23 20 7E | 8 22 11 13 24 5 21 8 9 13 4 | 20 28 18 20 28 20 23 20 26 19 19 8E | 13 24 15 9 43 6 16 10 22 21 6 | 20 35 26 30 42 26 29 24 32 22 23 9E | 7 19 10 8 78 6 19 9 15 17 4 | 14 27 22 18 36 17 27 20 18 24 16 10 | 6 18 8 9 15 5 11 8 10 19 3 | 13 20 18 14 22 14 16 19 18 22 13 11 | 9 26 11 9 46 6 17 11 10 17 4 | 16 25 17 15 40 15 22 21 19 27 16 12 | 8 23 9 7 25 6 22 8 7 40 5 | 18 31 23 22 34 23 28 22 24 41 21 13 | 8 24 10 9 38 7 24 12 6 22 5 | 18 32 22 17 41 17 27 21 17 23 17 14 | 9 27 10 17 39 6 24 8 10 15 5 | 20 36 29 32 39 24 31 25 23 22 24 15 | 8 22 8 12 32 6 24 13 9 31 5 | 17 27 24 24 34 18 26 25 16 31 18 16 | 6 24 8 12 43 6 22 12 7 25 5 | 17 28 24 21 35 19 26 21 19 24 18 17 | 8 19 9 13 21 6 18 11 10 36 5 | 14 26 18 17 28 17 27 18 18 25 14 18 | 10 31 7 14 35 4 24 8 6 17 5 | 15 38 23 24 36 20 28 22 20 20 19 19 | 7 25 10 8 27 8 24 9 8 30 5 | 21 32 19 19 28 20 33 26 24 26 21 20 | 10 24 12 11 36 7 22 14 7 21 5 | 18 32 25 20 33 17 25 25 21 25 19 21E | 7 20 9 9 22 4 13 5 7 18 3 | 19 32 23 19 37 20 27 20 19 26 20 22 | 7 25 11 11 50 5 25 9 7 14 4 | 18 33 26 26 36 21 27 25 20 21 21 23 | 8 25 9 10 29 9 24 9 7 24 5 | 44 51 46 46 56 44 51 49 53 46 48 24E | 20 21 14 17 29 5 19 15 29 42 8 | 107 114 110 102 123 106 118 111 110 114 109 25E | 13 21 16 9 27 10 21 20 18 19 6 | 41 48 46 44 59 45 49 52 48 45 44 26 | 7 17 8 7 17 4 13 10 9 26 4 | 14 24 21 18 24 16 22 20 18 23 17 27E | 7 21 8 10 61 8 16 13 25 19 5 | 20 27 20 19 30 19 23 25 30 28 18 28 | 7 25 13 10 28 5 22 8 8 30 5 | 22 36 29 30 43 23 31 26 23 26 23 29 | 9 19 8 16 29 7 20 8 11 40 5 | 16 25 17 19 27 17 26 23 18 37 17 30 | 6 15 9 8 17 5 13 8 11 25 4 | 25 25 27 24 35 25 23 26 26 31 24 31E | 9 21 8 11 39 7 21 8 7 15 4 | 13 29 18 19 46 16 19 15 17 19 14 32 | 8 21 11 11 27 5 20 8 10 24 4 | 16 23 23 21 31 17 19 21 22 20 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 23 10 11 35 6 20 11 13 25 |T 25 35 29 28 40 26 32 29 29 32 26 WRMS | 8 23 10 11 29 6 19 10 8 23 |NE 20 29 24 23 33 21 26 23 23 26 21 MEDI | 8 22 9 10 29 6 20 9 9 21 |MD 18 29 23 21 35 20 27 22 21 24 19 Table 3.1530.3 GPS week: 1530 Day: 3 MJD: 54957.000 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 | 21 --- --- --- --- 30 --- 20 38 --- 19 | 62 --- --- --- --- 60 --- 39 32 --- 49 2E | 8 22 11 11 20 4 21 11 14 27 5 | 20 27 23 23 26 22 25 20 19 24 19 3 | 5 13 8 10 36 7 12 10 13 17 4 | 40 43 46 49 43 45 43 45 46 38 45 4E | 31 22 12 13 29 7 14 17 24 33 8 | 122 114 109 114 116 112 114 112 107 120 112 X5 | 14 25 14 --- --- 13 --- 12 17 --- 7 | 15 31 29 --- --- 27 --- 19 26 --- 21 6 | 6 14 7 12 32 7 14 8 12 13 4 | 21 26 29 33 26 27 21 24 26 25 26 7E | 9 21 9 13 25 6 21 11 11 14 4 | 28 37 30 28 37 29 32 27 34 38 29 8E | 17 23 12 11 35 6 18 13 26 23 6 | 41 49 44 45 51 43 50 42 50 43 43 9E | 7 19 6 10 53 5 18 10 17 13 4 | 13 25 20 14 31 16 27 17 21 17 14 10 | 10 18 9 7 23 4 13 10 7 22 4 | 16 19 20 19 19 16 20 21 14 28 16 11 | 9 20 8 10 49 6 14 11 6 15 4 | 13 21 12 15 46 11 16 17 13 18 12 12 | 10 23 7 6 46 7 21 10 11 38 5 | 19 29 24 22 49 21 26 21 21 41 21 13 | 8 21 8 10 35 6 24 9 11 19 4 | 18 30 25 21 46 18 28 24 19 21 20 14 | 6 22 9 10 51 6 23 11 11 17 5 | 20 32 23 26 41 24 31 26 19 26 22 15 | 9 21 8 12 29 7 23 13 7 33 5 | 21 27 24 23 35 18 26 25 19 30 20 16 | 9 22 8 12 39 5 24 14 10 27 5 | 22 28 28 32 31 25 29 27 26 22 25 17 | 8 20 11 9 21 7 19 8 14 32 5 | 16 25 14 15 34 18 28 18 20 23 16 18 | 8 24 9 9 26 5 23 10 8 16 4 | 15 32 22 18 38 18 29 20 14 19 17 19 | 7 28 8 10 33 9 24 11 11 30 5 | 19 31 19 17 29 18 29 20 20 24 18 20 | 10 22 11 10 31 7 22 12 8 20 5 | 17 28 19 23 31 17 23 25 20 22 19 21E | 6 20 8 10 23 5 14 7 11 18 4 | 20 29 23 18 40 20 26 22 19 24 20 22 | 7 23 9 7 51 7 23 11 7 13 4 | 16 29 24 21 39 18 27 24 15 18 19 23 | 8 22 7 10 30 6 21 10 10 23 4 | 65 68 65 68 67 65 69 69 63 67 65 24E | 18 20 9 16 30 8 17 14 28 36 7 | 116 120 119 108 125 115 123 116 116 112 115 25E | 14 22 13 10 28 8 22 21 18 23 6 | 55 65 62 57 69 60 63 64 64 65 59 26 | 7 15 8 9 19 7 13 9 8 16 3 | 15 23 17 18 29 14 20 19 13 15 17 27E | 8 20 9 9 52 6 19 15 28 19 6 | 20 25 20 18 27 18 24 22 32 20 18 28 | 7 21 8 10 40 5 24 11 11 26 5 | 19 31 21 21 41 21 32 21 19 21 18 29 | 10 16 9 9 25 10 18 10 12 34 5 | 13 24 15 14 26 16 28 20 19 27 16 30 | 5 13 6 6 31 6 12 7 10 24 3 | 29 27 35 35 42 30 24 29 33 34 31 31E | 9 16 9 10 36 7 21 16 14 15 5 | 21 30 23 22 38 21 26 24 24 27 21 32 | 10 17 9 11 36 6 18 8 9 24 4 | 15 19 17 18 27 14 17 19 14 16 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 20 9 10 35 6 19 12 14 24 |T 30 36 32 31 43 31 35 32 31 34 30 WRMS | 8 20 8 10 33 6 19 10 9 20 |NE 23 29 25 25 36 24 28 26 23 26 23 MEDI | 8 21 9 10 31 6 19 11 11 22 |MD 20 29 23 22 38 21 27 24 20 24 20 Table 3.1530.4 GPS week: 1530 Day: 4 MJD: 54958.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 17 --- --- --- --- 19 --- 17 15 --- 12 | 28 --- --- --- --- 33 --- 18 26 --- 26 2 | 8 27 10 13 30 6 22 10 15 21 5 | 26 37 30 38 33 30 33 30 28 27 29 3 | 5 12 6 9 31 4 13 8 7 18 3 | 24 28 28 29 28 27 27 27 28 24 28 4E | 18 24 11 15 26 13 15 17 13 29 6 | 141 142 143 147 151 143 148 143 146 143 143 X5 | 8 23 8 --- --- 17 --- 11 13 --- 6 | 14 23 17 --- --- 18 --- 16 21 --- 15 6 | 5 12 7 11 43 5 13 9 7 14 3 | 19 25 26 26 45 22 21 22 26 24 23 7E | 8 21 10 13 32 5 23 10 9 17 4 | 16 25 22 19 38 19 26 20 20 13 18 8E | 15 24 9 9 29 8 20 12 26 24 6 | 31 40 36 36 47 32 33 38 43 42 33 9E | 7 18 10 7 54 5 18 11 13 16 4 | 13 26 22 14 30 17 26 17 19 21 15 10 | 6 21 8 7 23 5 14 8 11 19 4 | 11 15 18 11 20 14 15 17 18 25 13 11 | 7 20 9 11 46 5 18 10 10 19 4 | 14 23 17 15 44 15 18 18 16 20 15 12 | 9 23 9 9 46 7 23 9 10 38 5 | 18 27 19 18 44 17 26 16 21 38 18 13 | 9 22 7 9 45 6 26 9 7 25 4 | 16 30 21 17 45 16 28 22 17 18 17 14 | 7 22 9 14 47 5 22 8 10 20 4 | 19 30 25 27 40 22 29 22 19 21 21 15 | 9 25 7 12 30 3 25 10 13 27 5 | 16 28 20 23 33 18 25 23 21 28 18 16 | 8 21 8 9 30 7 24 15 7 26 5 | 17 29 22 20 30 18 27 22 25 23 21 17 | 8 18 8 10 34 7 22 11 11 33 5 | 13 24 13 14 42 18 30 17 17 21 14 18 | 9 25 6 15 34 4 22 10 11 17 5 | 12 31 21 20 38 17 27 18 20 19 18 19 | 7 23 11 9 28 6 25 11 12 31 5 | 20 31 17 17 29 19 29 22 23 23 20 20 | 9 25 9 10 43 5 23 15 10 21 5 | 16 31 19 18 33 18 23 24 21 23 18 21E | 10 19 8 10 27 4 13 9 12 19 4 | 25 29 27 21 45 23 28 23 26 25 24 22 | 9 23 8 10 49 5 24 11 12 14 5 | 14 28 23 22 38 19 26 21 20 19 19 23 | 8 24 8 12 39 6 24 9 6 25 5 | 35 41 37 35 34 35 40 38 35 42 34 24E | 16 23 7 14 36 6 17 13 23 30 6 | 122 129 124 119 133 124 133 125 123 124 123 25E | 12 22 10 10 35 8 21 21 16 27 6 | 44 52 48 48 60 47 56 51 48 46 47 26 | 7 18 9 7 21 5 14 11 9 17 4 | 13 24 17 14 25 15 20 19 16 15 15 27E | 9 19 11 7 60 7 17 16 30 18 6 | 19 27 19 18 23 18 24 23 32 21 18 28 | 7 23 7 11 40 5 24 12 14 27 5 | 19 32 26 25 40 21 31 25 24 23 20 29 | 9 20 9 10 24 9 19 11 11 35 5 | 17 27 23 16 27 16 30 23 17 31 19 30 | 5 13 5 8 32 4 15 8 9 23 3 | 22 20 23 24 43 22 19 19 25 28 22 31E | 8 19 8 11 21 7 18 13 14 17 4 | 14 30 20 20 34 20 27 24 22 27 19 32 | 8 14 9 10 32 5 20 11 7 26 4 | 16 20 21 19 25 16 19 20 17 17 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 21 8 11 37 6 20 12 13 24 |T 26 35 30 29 43 28 34 30 30 32 28 WRMS | 8 21 8 11 35 6 20 10 9 20 |NE 17 27 21 20 35 19 25 21 21 24 19 MEDI | 8 22 8 10 32 5 20 11 11 21 |MD 17 28 22 20 38 19 27 22 21 23 19 Table 3.1530.5 GPS week: 1530 Day: 5 MJD: 54959.000 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 --- --- --- --- 14 --- 14 19 --- 12 | 43 --- --- --- --- 37 --- 22 25 --- 38 2 | 6 23 12 12 45 4 23 13 13 20 5 | 22 30 23 21 40 23 29 24 31 23 22 3 | 5 13 9 9 23 5 10 9 15 21 4 | 32 38 38 38 44 33 33 29 32 32 33 4 | 8 20 8 13 37 7 13 17 14 34 5 | 66 78 74 70 82 71 78 75 72 74 71 X5 | 9 21 11 --- --- 8 --- 12 19 --- 7 | 14 21 22 --- --- 16 --- 17 20 --- 14 6 | 5 15 9 10 32 5 10 13 14 15 4 | 17 27 25 25 33 20 20 19 24 24 21 7E | 6 21 10 13 20 3 23 14 12 15 5 | 32 35 32 34 34 31 37 34 34 32 31 8E | 18 28 9 14 47 7 18 14 27 19 7 | 59 69 62 68 84 63 62 64 72 66 63 9E | 9 20 8 10 53 6 19 13 13 20 5 | 13 24 19 18 38 16 27 15 26 20 15 10 | 7 17 8 7 17 6 13 10 10 21 4 | 9 12 11 12 19 9 11 14 15 20 7 11 | 7 15 10 9 42 5 12 8 11 21 4 | 13 18 12 12 42 10 17 14 17 21 10 12 | 8 23 11 10 32 5 25 8 10 42 6 | 13 28 16 18 34 15 27 15 14 36 14 13 | 7 19 9 11 39 5 23 10 11 19 5 | 16 25 20 19 45 16 29 19 19 14 15 14 | 8 19 9 11 51 4 20 10 10 21 4 | 19 28 23 24 38 21 28 21 17 22 19 15 | 12 24 11 14 32 5 25 8 14 26 6 | 16 26 21 22 37 17 23 21 26 31 18 16 | 8 20 11 10 33 7 21 15 11 25 5 | 20 30 24 25 38 21 27 22 22 24 22 17 | 7 19 9 12 40 8 19 13 14 33 5 | 15 26 22 15 50 18 27 21 21 23 16 18 | 9 27 10 15 35 5 24 11 12 20 5 | 15 35 20 20 37 18 29 20 25 17 18 19 | 7 21 11 11 29 8 21 12 12 29 5 | 15 24 11 13 29 13 22 17 19 23 12 20 | 7 21 6 11 38 7 23 14 5 21 5 | 15 27 16 20 36 15 23 23 17 20 15 21 | 17 20 12 11 29 5 14 8 15 30 5 | 54 57 57 53 56 51 57 54 61 42 55 22 | 7 23 12 11 43 6 23 14 9 13 5 | 14 30 22 21 35 18 24 24 20 19 18 23 | 8 21 7 12 35 4 24 11 8 28 5 | 49 55 45 51 58 49 52 51 50 52 48 24E | 15 22 11 13 33 7 16 16 18 40 6 | 131 137 134 127 143 127 140 137 126 132 131 25E | 11 19 12 10 56 8 21 19 13 22 5 | 57 62 59 59 67 59 65 64 63 60 58 26 | 7 18 11 10 26 5 15 10 13 16 4 | 13 21 13 17 27 12 19 17 21 15 13 27E | 10 21 10 11 54 5 19 16 33 17 6 | 16 24 15 17 32 14 24 22 38 24 15 28 | 7 24 9 16 39 7 26 13 11 29 6 | 15 33 18 24 38 17 30 21 20 21 16 29 | 9 16 8 15 31 7 19 9 7 30 5 | 16 21 16 19 28 15 24 20 23 31 17 30 | 5 14 7 8 24 4 15 6 9 22 3 | 18 19 24 21 35 17 17 17 19 26 19 31E | 8 16 11 10 19 8 20 24 14 18 5 | 13 23 19 16 29 13 22 21 20 29 15 32 | 11 14 10 8 31 3 18 10 8 25 4 | 14 16 22 17 27 14 19 16 19 16 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 10 11 37 6 20 13 14 25 |T 27 35 30 30 44 27 34 30 32 32 27 WRMS | 8 20 10 11 35 6 19 11 8 22 |NE 18 26 21 21 36 19 25 20 22 24 18 MEDI | 8 20 10 11 33 5 19 12 12 21 |MD 16 27 22 21 37 17 27 21 22 24 18 Table 3.1530.6 GPS week: 1530 Day: 6 MJD: 54960.000 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 --- --- --- --- 26 --- 14 33 --- 15 | 43 --- --- --- --- 44 --- 24 30 --- 35 2 | 6 27 11 9 37 5 26 11 10 26 5 | 25 36 27 27 31 26 33 29 25 41 26 3 | 5 13 6 9 39 8 10 9 9 29 4 | 34 39 37 43 33 40 38 32 38 33 35 4 | 9 21 12 14 58 7 14 20 14 40 6 | 124 126 123 127 141 120 124 119 115 124 121 X5 | 11 26 9 --- --- 11 --- 12 16 --- 7 | 23 29 20 --- --- 20 --- 24 23 --- 20 6 | 7 15 8 12 26 8 10 16 10 19 4 | 26 31 33 36 37 31 25 30 34 30 29 7E | 5 20 7 14 24 6 23 13 12 16 5 | 27 34 31 26 34 31 33 32 36 34 29 8E | 17 29 9 9 49 9 22 16 31 24 7 | 30 40 30 32 37 32 34 33 49 34 30 9E | 7 19 8 9 59 4 19 13 13 17 4 | 18 25 23 20 35 19 26 21 28 17 19 10 | 6 17 11 6 26 6 12 9 15 21 4 | 13 14 13 12 17 13 13 16 21 18 12 11 | 5 18 12 8 52 4 16 6 10 23 4 | 13 19 16 15 50 12 18 16 18 24 12 12 | 9 23 9 8 32 7 25 8 11 40 5 | 23 31 26 24 41 22 31 22 26 42 24 13 | 7 17 10 10 33 4 25 10 9 15 4 | 21 28 25 23 41 21 28 24 29 21 21 14 | 7 23 11 12 38 3 22 9 11 29 5 | 24 35 28 32 41 27 30 26 28 33 26 15 | 9 19 9 10 40 5 23 10 13 24 5 | 18 27 21 23 33 20 25 23 26 26 20 16 | 7 23 11 9 32 5 26 13 15 24 5 | 23 34 33 30 35 26 32 27 32 29 26 17 | 6 19 11 10 47 8 19 16 15 35 5 | 20 26 19 20 41 21 32 25 26 32 20 18 | 8 27 9 10 32 5 24 8 8 13 5 | 18 31 20 20 31 18 28 22 21 20 18 19 | 8 22 8 11 32 7 18 12 11 32 5 | 27 32 22 20 37 22 30 26 25 31 23 20 | 7 14 11 7 29 7 21 10 9 18 4 | 19 24 22 19 32 17 19 23 21 17 18 21 | 7 18 10 8 30 5 17 8 12 23 4 | 35 37 33 33 30 33 34 34 33 40 32 22 | 6 26 11 9 58 6 23 12 10 17 5 | 24 35 27 27 40 22 30 28 26 23 24 23 | 8 18 11 9 30 6 24 12 9 27 5 | 43 48 46 46 58 44 50 42 45 47 44 24E | 16 23 8 14 28 9 16 18 17 65 7 | 131 139 135 130 140 135 142 136 128 127 131 25E | 12 25 10 10 46 8 25 20 13 24 6 | 46 52 50 44 60 46 55 48 48 50 45 26 | 5 15 11 8 23 4 13 9 12 16 4 | 16 21 19 16 22 16 20 21 27 17 18 27E | 9 20 11 10 63 6 19 17 37 19 7 | 25 29 23 22 33 22 28 26 44 30 23 28 | 7 21 10 11 43 4 23 15 14 29 5 | 23 35 27 29 50 25 30 28 29 23 25 29 | 8 18 9 11 27 7 20 10 10 33 5 | 26 31 29 24 36 26 36 32 31 41 28 30 | 4 13 7 7 17 8 14 5 8 23 3 | 31 29 33 33 41 31 26 27 36 34 30 31E | 10 18 9 10 56 7 21 18 16 22 5 | 17 26 24 21 49 19 23 23 31 30 19 32 | 10 17 11 8 40 6 17 12 11 23 4 | 20 21 25 17 26 18 18 24 19 18 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 20 10 10 40 6 20 13 14 27 |T 31 37 33 33 44 31 36 33 35 36 31 WRMS | 7 20 10 10 37 7 19 11 10 21 |NE 24 29 25 25 37 24 27 25 27 27 23 MEDI | 7 19 10 9 33 6 20 12 12 23 |MD 24 31 27 24 37 22 30 26 29 30 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 4.1530 GPS week: 1530 MJD: 54954.0-54960.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3046 |U 7 8 26 |U 9 11 67 |U 10 9 17 | emr | emr 2947 | 10 8 31 | 10 13 72 | 10 11 21 | esa | esa 2976 | 8 7 27 |U 11 10 36 | 8 7 16 | gfz | gfz 2844 |U 8 7 27 |U 13 13 72 | 13 11 20 | grg | grg 2880 | 8 8 24 |U 10 11 70 | 15 14 20 | igr | igr 2993 | 8 8 26 | 11 12 76 | 8 7 16 | igs | igs 2976 | 8 7 25 | 9 11 65 | 8 7 16 | jpl | jpl 2856 |U 8 7 27 |U 12 14 78 |U 13 11 20 | mit | mit 3058 |U 11 10 29 |U 12 17 86 |U 12 12 24 | 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 5.1530.0 GPS week: 1530 Day: 0 MJD: 54954.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3051 | 8 9 24 | 6 11 21 | 9 7 18 | emr | emr 2946 | 10 10 31 | 8 11 30 | 11 10 24 | esa | esa 2976 | 9 9 26 | 5 9 20 | 9 5 18 | gfz | gfz 2842 | 9 7 25 | 9 11 30 | 10 7 19 | grg | grg 2880 | 9 8 30 | 7 9 28 | 10 5 18 | igr | igr 3027 | 9 10 28 | 5 10 19 | 10 8 21 | igs | igs 2974 | 8 8 25 | 5 10 20 | 9 5 16 | jpl | jpl 2854 | 9 10 25 | 6 12 19 | 9 6 20 | mit | mit 2976 | 8 7 25 | 7 10 30 | 9 5 16 | Table 5.1530.1 GPS week: 1530 Day: 1 MJD: 54955.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3049 | 11 12 43 | 22 23 320 | 8 10 19 | emr | emr 2946 | 11 8 32 | 22 23 339 | 11 12 23 | esa | esa 2976 | 11 7 31 | 38 28 102 | 8 7 16 | gfz | gfz 2842 | 10 9 30 | 39 38 322 | 10 9 19 | grg | grg 2880 | 8 6 20 | 26 23 316 | 11 12 19 | igr | igr 2999 | 9 9 27 | 38 30 385 | 9 9 17 | igs | igs 2976 | 10 9 30 | 28 26 311 | 9 8 19 | jpl | jpl 2854 | 8 5 25 | 39 37 382 | 9 8 19 | mit | mit 3072 | 29 28 51 | 23 35 384 | 12 16 26 | Table 5.1530.2 GPS week: 1530 Day: 2 MJD: 54956.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3036 | 6 8 23 | 8 8 37 | 12 11 20 | emr | emr 2945 | 8 7 29 | 7 12 36 | 11 10 17 | esa | esa 2976 | 7 5 24 | 6 9 33 | 9 7 18 | gfz | gfz 2840 | 7 5 29 | 9 10 32 | 9 8 19 | grg | grg 2880 | 8 7 26 | 8 11 37 | 12 12 21 | igr | igr 3024 | 6 6 23 | 6 10 33 | 9 6 17 | igs | igs 3016 | 6 5 23 | 6 9 31 | 9 7 16 | jpl | jpl 2854 | 7 6 27 | 7 12 37 | 10 7 20 | mit | mit 3072 | 8 6 22 | 11 21 49 | 19 19 43 | Table 5.1530.3 GPS week: 1530 Day: 3 MJD: 54957.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3054 | 7 4 28 | 7 10 23 | 19 18 18 | emr | emr 2943 | 11 6 43 | 8 12 26 | 8 9 17 | esa | esa 2976 | 9 5 42 | 6 7 20 | 9 9 14 | gfz | gfz 2842 | 9 5 36 | 9 9 25 | 37 31 25 | grg | grg 2880 | 8 5 30 | 8 8 26 | 42 39 30 | igr | igr 2963 | 9 5 38 | 6 10 25 | 8 7 12 | igs | igs 2963 | 8 4 37 | 6 9 22 | 7 7 13 | jpl | jpl 2854 | 10 6 45 | 7 11 29 | 37 31 24 | mit | mit 3072 | 8 5 36 | 7 9 25 | 18 25 31 | Table 5.1530.4 GPS week: 1530 Day: 4 MJD: 54958.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3056 | 7 7 17 | 6 6 23 | 8 7 16 | emr | emr 2949 | 11 10 24 | 6 10 25 | 10 10 21 | esa | esa 2976 | 8 7 20 | 6 6 22 | 7 7 14 | gfz | gfz 2842 | 9 7 23 | 8 9 36 | 7 8 23 | grg | grg 2880 | 9 10 13 | 8 7 28 | 8 10 17 | igr | igr 2969 | 8 8 18 | 7 10 24 | 8 8 17 | igs | igs 2968 | 8 6 19 | 5 7 22 | 6 6 15 | jpl | jpl 2860 | 9 8 17 | 7 9 30 | 8 8 19 | mit | mit 3072 | 8 6 22 | 6 9 24 | 8 8 19 | Table 5.1530.5 GPS week: 1530 Day: 5 MJD: 54959.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3042 | 7 7 24 | 7 9 21 | 6 6 18 | emr | emr 2948 | 10 7 33 | 8 9 20 | 10 15 24 | esa | esa 2976 | 8 8 26 | 5 5 23 | 5 5 17 | gfz | gfz 2845 | 8 8 26 | 6 8 28 | 7 6 19 | grg | grg 2880 | 8 11 27 | 8 9 27 | 11 9 18 | igr | igr 3014 | 7 8 26 | 6 6 21 | 6 6 17 | igs | igs 2981 | 7 7 26 | 6 7 20 | 6 6 18 | jpl | jpl 2859 | 7 8 28 | 7 9 24 | 8 7 19 | mit | mit 3072 | 7 7 24 | 8 11 29 | 8 7 21 | Table 5.1530.6 GPS week: 1530 Day: 6 MJD: 54960.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3038 | 7 7 20 | 9 10 26 | 8 7 12 | emr | emr 2954 | 10 8 27 | 10 11 30 | 11 11 19 | esa | esa 2976 | 7 6 22 | 8 9 32 | 8 9 15 | gfz | gfz 2855 | 8 9 23 | 8 7 34 | 9 8 16 | grg | grg 2880 | 8 7 24 | 7 11 30 | 12 11 18 | igr | igr 2955 | 7 8 24 | 9 10 27 | 9 8 13 | igs | igs 2959 | 7 7 19 | 9 9 29 | 8 8 15 | jpl | jpl 2863 | 8 8 25 | 9 10 27 | 11 10 19 | mit | mit 3072 | 7 8 25 | 21 23 61 | 7 8 15 | 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 6.1530 GPS week: 1530 MJD: 54954.500-54960.500 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 -3 50 153 3 | 11 21 | 24 29 126 24 8 | 2 emr uuuxu | 87 22 67 574 -8 | 60 64 | 20 25 136 99 8 | 4 esa uuuuu | -51 -66 49 -234 -3 | 9 21 | 26 22 111 100 10 | 5 gfz uuuuu | 16 -6 18 88 3 | 30 35 | 10 20 77 44 5 | 1 grg xxxxx | -22 -58 85 203 2 | 5 30 | 37 46 154 123 15 | 3 igr xxxxx | -6 -1 -21 132 -11 | 1 18 | 24 33 92 77 11 | 5 irf xxxxx | -20 15 -3 37 -3 | 1 20 | 8 6 40 25 5 | 4 jpl uuuuu | 11 8 82 219 -10 | 13 26 | 13 14 130 74 8 | 5 mit uuuuu | -37 10 71 -19 -10 | 22 32 | 16 9 83 53 6 | 6 ngs uuuuu | 8 63 -133 78 7 | 9 18 | 50 44 120 66 8 | 1 sio uuuuu | 91 -14 -279 9 22 | 64 68 | 27 16 105 106 6 | 6 Table 7.1530.0 GPS week: 1530 Day: 0 MJD: 54954.500 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 -53 111 158 -6 | 11 20 emr uuuxu | 69 26 -128 555 -10 | 64 66 esa uuuuu | -67 -59 25 -280 -1 | 14 22 gfz uuuuu | 19 -32 69 135 3 | 31 35 grg xxxxx | 13 -135 420 296 -5 | 5 37 igr xxxxx | 24 -27 145 183 3 | 5 16 irf xxxxx | -23 16 -64 34 -12 | 7 19 jpl uuuuu | 19 1 344 226 -5 | 18 29 mit uuuuu | -36 10 -38 -23 -19 | 30 35 ngs uuuuu | 20 75 -25 75 5 | 10 17 sio uuuuu | 89 -3 -483 -19 24 | 55 59 Table 7.1530.1 GPS week: 1530 Day: 1 MJD: 54955.500 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 | 17 1 293 161 10 | 7 19 emr uuuxu | 104 6 103 671 -4 | 61 65 esa uuuuu | -65 -107 97 -353 -2 | 12 22 gfz uuuuu | 14 -17 131 77 -1 | 29 34 grg xxxxx | 22 -12 64 239 -5 | 1 37 igr xxxxx | 17 4 -49 141 -22 | 4 17 irf xxxxx | -30 9 -6 26 -7 | 3 21 jpl uuuuu | 29 0 -3 367 -19 | 14 27 mit uuuuu | -39 7 31 -27 -15 | 26 34 ngs uuuuu | 18 117 -213 118 10 | 7 16 sio uuuuu | 49 -14 -222 -51 23 | 56 60 Table 7.1530.2 GPS week: 1530 Day: 2 MJD: 54956.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -27 -28 52 173 15 | 10 22 emr uuuxu | 114 8 39 690 5 | 63 66 esa uuuuu | 3 -65 206 -266 -2 | 14 23 gfz uuuuu | -4 -17 65 87 4 | 31 36 grg xxxxx | -79 -82 81 13 15 | 2 38 igr xxxxx | -20 -60 50 -17 -2 | 4 17 irf xxxxx | -11 7 -16 40 -3 | 4 21 jpl uuuuu | 18 -4 8 189 -20 | 17 27 mit uuuuu | -9 -5 1 67 -13 | 26 35 ngs uuuuu | -67 102 -200 28 11 | 10 18 sio uuuuu | 73 -42 -315 -5 28 | 63 67 Table 7.1530.3 GPS week: 1530 Day: 3 MJD: 54957.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -6 3 -104 166 6 | 12 22 emr uuuxu | 93 7 70 619 -6 | 64 67 esa uuuuu | -51 -53 136 -178 -23 | 12 22 gfz uuuuu | 25 -7 -84 42 7 | 31 35 grg xxxxx | -36 -69 10 318 20 | 10 30 igr xxxxx | 16 8 -41 230 -10 | 4 17 irf xxxxx | -23 20 2 23 1 | 2 21 jpl uuuuu | -10 18 155 238 -11 | 15 27 mit uuuuu | -45 14 100 9 -5 | 24 33 ngs uuuuu | 22 63 -302 124 18 | 9 18 sio uuuuu | 95 -8 -208 -143 27 | 68 71 Table 7.1530.4 GPS week: 1530 Day: 4 MJD: 54958.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 1 -3 13 101 3 | 11 22 emr uuuxu | 87 1 239 478 -20 | 61 64 esa uuuuu | -71 -53 55 -47 -5 | 6 21 gfz uuuuu | 18 0 -6 147 10 | 29 35 grg xxxxx | 4 -63 60 55 -6 | 5 23 igr xxxxx | -24 16 -67 102 -28 | 1 17 irf xxxxx | -18 24 -27 5 -1 | -1 20 jpl uuuuu | -1 -7 73 130 -12 | 12 27 mit uuuuu | -40 23 49 -112 -9 | 20 31 ngs uuuuu | 46 54 -182 -47 9 | 9 17 sio uuuuu | 119 7 -281 4 18 | 68 71 Table 7.1530.5 GPS week: 1530 Day: 5 MJD: 54959.500 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 | -41 29 7 162 -4 | 11 22 emr uuuxu | 57 30 215 419 -13 | 57 61 esa uuuuu | -64 -41 -102 -217 7 | 4 20 gfz uuuuu | 14 31 -67 30 -4 | 29 34 grg xxxxx | -50 -52 -40 300 16 | 6 23 igr xxxxx | -30 40 -42 138 -12 | -4 18 irf xxxxx | -26 18 22 47 2 | -3 19 jpl uuuuu | 10 24 15 205 2 | 8 24 mit uuuuu | -62 14 176 -31 -4 | 17 27 ngs uuuuu | 70 -21 -6 131 -5 | 10 18 sio uuuuu | 83 -23 -292 89 22 | 69 72 Table 7.1530.6 GPS week: 1530 Day: 6 MJD: 54960.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 27 28 -25 149 -6 | 11 22 emr uuuxu | 83 72 -72 589 -10 | 54 59 esa uuuuu | -39 -82 -76 -296 5 | 4 20 gfz uuuuu | 25 2 20 98 1 | 28 34 grg xxxxx | -29 5 -2 201 -19 | 7 23 igr xxxxx | -27 9 -141 144 -2 | -8 21 irf xxxxx | -7 13 64 84 0 | -4 20 jpl uuuuu | 14 23 -17 176 -1 | 5 24 mit uuuuu | -29 6 176 -15 -3 | 14 27 ngs uuuuu | -54 53 -3 115 -3 | 9 19 sio uuuuu | 131 -15 -155 191 9 | 70 73