Date: Thu, 05 Feb 2009 13:38:52 +0000 From: Jim Ray Subject: [IGSREPORT-17087] Wk 1515 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <498aebec.mNpgW91KdJCP3UZM%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 05 Feb 05:38:54 PST 2009 Message Number 17087 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1515 (Jan 18, 2009 - Jan 24, 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: igs1515[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1515[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1515[0-6].cls IGS GPS clock combination summary report. igs15157.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15157.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Day | Centre | PRN/STA list ----+--------+--------------- 0 | EMR | 28 MIZU 0 | ESA | 28 MAS1 0 | GFZ | 7 12 29 CHUR DAEJ FAA1 0 | GRG | NLIB 0 | JPL | 5 12 28 30 HARB 0 | MIT | 5 30 WTZR 1 | EMR | MAS1 MIZU 1 | ESA | 29 UNSA 1 | GFZ | 7 12 28 29 IRKT 1 | GRG | NLIB 1 | JPL | 5 29 30 1 | MIT | 16 2 | EMR | HARB MIZU 2 | GFZ | 7 12 28 29 ALIC KOUR 2 | GRG | NLIB 2 | JPL | 30 ALIC HARB 2 | MIT | 5 25 30 BOR1 ONSA 3 | EMR | DAEJ HARB MIZU THU3 YELL 3 | ESA | YAKT 3 | GFZ | 7 12 28 29 CONZ YAKT 3 | GRG | NLIB 3 | JPL | 30 HARB MCM4 THU3 3 | MIT | 5 30 KOUR 4 | EMR | MIZU 4 | ESA | UNSA 4 | GFZ | 7 12 28 29 DAEJ 4 | GRG | NLIB 4 | JPL | 30 4 | MIT | 2 5 29 30 KHAJ OUS2 5 | COD | GUAT SUWN 5 | EMR | MIZU 5 | ESA | SCH2 UNSA 5 | GFZ | 7 12 28 29 BOR1 IRKT 5 | GRG | NLIB 5 | JPL | 5 30 5 | MIT | 5 30 STJO 6 | EMR | DAEJ HARB WTZR 6 | GFZ | 7 12 29 DAEJ FAA1 THTI UNSA WTZR 6 | GRG | NLIB 6 | JPL | HARB TIDB 6 | MIT | 5 30 WTZR 5. New clock offsets and drifts were estimated for centres showing reference clock resets. Note that only the largest clock offset and drift are output to the summary file. However, the clock combination and the listed RMS include all the clock segments. In summary, the following clock shifts/resets were noticed and accounted for: Day | Centre | Time | Jump ----+--------+--------+------------- 1 | MIT | ~00:00 | ~ -0.40 ns 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 | .3 -.1 .9 -22 -14 -13 -.01 EMR | 8.9 -8.2 -16.5 159 31 4 .39 ESA | 4.1 -.7 -5.5 -38 -87 55 .13 GFZ | 1.4 .5 1.6 24 -34 2 -.22 GRG | 4.3 -5.2 -14.6 -55 -8 16 .04 JPL | 5.8 2.5 6.1 -13 -44 19 .21 MIT | .8 -2.2 -3.0 -21 9 7 -.05 NGS | 4.1 -2.4 -6.2 -31 -108 25 .06 SIO | -1.8 -7.0 7.9 -123 76 8 .06 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 1.1515.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1515.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 2.1515.[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 3.1515.[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 5.1515.0-6). 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 1515 summary. (Jan 18, 2009 - Jan 24, 2009) Table 1.1515.a GPS week: 1515 MJD: 54849.000-54855.000 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 21 -21 -4 -.10 8 8 | -255 -280 13 94 | 0 0 1 10 17 26 .03 | 674 939 emr 74| 1 0 4 -319 -92 -62 .44 18 18 | 50 464 20 182 | 1 1 0 18 26 12 .05 | 737 749 esa 134| 0 0 -2 41 57 25 .32 9 9 | -138 -675 19 111 | 1 0 1 27 25 15 .03 | 1165 1745 gfz 193| 0 0 -2 -76 15 -2 -.13 9 9 | 166 -86 20 115 | 0 0 1 19 10 44 .04 | 281 579 grg 79| 3 -2 -2 77 -61 16 1.17 37 34 | -163 149 93 226 | 1 2 2 38 21 69 .08 | 377 701 igr n/a| 0 0 0 -2 -39 -16 .05 5 5 | 9417 545 19 88 | 0 0 0 18 18 21 .02 | 773 810 jpl 122| 0 0 6 2 58 -1 .57 17 16 | 1106 472 18 100 | 0 1 1 24 14 61 .03 | 728 820 mit 264| 0 1 0 32 -97 18 -.27 11 10 | -241 180 21 137 | 0 0 1 32 40 13 .02 | 304 526 ngs 213| -1 0 1 65 141 -38 -.30 12 8 | -314 -221 2444 4139 | 0 0 1 21 52 17 .04 | 636 878 sio 256| 0 1 2 210 -225 44 -.24 22 20 | --- --- --- --- | 1 1 1 49 50 18 .03 | --- --- Table 1.1515.b GPS week : 1515 MJD: 54849.000-54855.000 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 ------+------------------------------------+------------------------------------------ 2 | 5 5 4 4 5 4 4 | 3 | 4 4 4 3 5 6 5 | 4 | 5 4 4 4 4 4 4 | 5 | 6 6 6 6 6 6 6 | 6 | 4 4 3 4 5 6 5 | 7 | 5 5 5 5 5 5 6 | 8 | 4 3 4 3 4 3 4 | 9 | 3 3 4 3 4 4 4 | 10 | 5 4 4 4 4 5 4 | 11 | 4 5 5 5 5 5 5 | 12 | 5 5 5 5 5 5 5 | 13 | 4 4 4 4 4 4 4 | 14 | 5 5 5 5 5 5 5 | 15 | 5 4 5 5 5 5 5 | 16 | 5 5 5 5 6 5 6 | 17 | 4 5 6 5 5 5 5 | 18 | 4 5 5 5 5 5 5 | 19 | 5 6 5 5 6 5 5 | 20 | 5 5 5 5 5 5 5 | 21 | 4 4 4 4 4 4 4 | 22 | 4 4 4 5 5 4 4 | 23 | 5 5 5 5 5 5 5 | 24 | 4 4 4 4 4 4 4 | 25 | 4 4 4 4 5 4 4 | 26 | 4 4 4 4 4 5 7 | 27 | 5 4 4 4 4 4 4 | 28 | 4 4 4 3 4 4 4 | 29 | 5 5 5 5 6 5 6 | 30 | 8 8 7 7 7 7 7 | 31 | 4 5 5 5 6 5 5 | 32 | 5 5 5 5 5 4 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 2.1515.0 GPS week: 1515 Day: 0 MJD: 54849.000 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 31 -15 -36 -.13 9 8 | -321 -581 16 108 | -4 -20 | emr 74| 2 0 4 -300 -76 -48 .39 18 18 | 161 -149 18 173 | 35 -24 | esa 134| 0 0 0 73 40 10 .29 7 7 | 494 -2732 21 110 | -47 -3 | gfz 193| 0 0 -1 -103 28 68 -.15 8 8 | 391 -749 24 113 | 36 -33 | grg 79| 5 0 -5 73 -83 -117 1.06 36 32 | 59 -863 84 247 | 9 0 | igr n/a| 0 0 0 1 -32 -61 .02 5 5 | 8892 98 19 82 | -25 -9 | jpl 122| 0 0 7 32 70 -114 .52 18 16 | 1009 -204 19 92 | -38 -152 | mit 264| 0 0 -2 26 -137 13 -.26 12 11 | -8 -615 23 113 | 14 23 | ngs 213| -2 0 -1 57 156 -27 -.22 14 9 | -477 -467 2710 4507 | 60 -7 | sio 256| 0 0 0 212 -270 17 -.29 22 20 | --- --- --- --- | -110 125 | Table 2.1515.1 GPS week: 1515 Day: 1 MJD: 54850.000 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 1 25 -15 6 -.07 8 8 | -677 742 15 114 | 19 1 | emr 74| 1 1 4 -321 -80 -57 .49 18 18 | 127 1810 18 168 | 63 -7 | esa 134| 2 0 -4 66 38 25 .35 9 9 | -872 1220 20 109 | -60 20 | gfz 193| 0 0 -1 -69 19 3 -.06 8 8 | -141 872 19 114 | 41 -20 | grg 79| 4 -2 -3 82 -51 2 1.12 37 35 | -498 797 82 210 | 24 58 | igr n/a| 1 0 0 15 -20 -7 .07 5 5 | 9117 2053 21 104 | -22 -6 | jpl 122| 0 1 6 -22 43 -21 .63 18 17 | 936 1950 20 105 | 61 -76 | mit 264| 0 0 -1 17 -87 22 -.27 9 8 | -716 387 25 319 | 25 18 | ngs 213| -2 -1 1 56 171 -55 -.34 13 8 | -693 744 2469 3802 | 40 40 | sio 256| -1 0 1 187 -215 28 -.25 21 21 | --- --- --- --- | -92 107 | Table 2.1515.2 GPS week: 1515 Day: 2 MJD: 54851.000 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 4 -1 -4 -.09 9 8 | -125 -292 12 93 | 63 -47 | emr 74| 3 2 4 -338 -56 -71 .40 19 19 | 1447 243 19 221 | 71 -48 | esa 134| 0 -1 -3 16 25 38 .35 8 8 | -393 501 20 106 | 12 10 | gfz 193| 0 0 0 -57 6 1 -.14 8 8 | -11 431 23 125 | 31 -23 | grg 79| 4 -5 0 44 -69 90 1.11 39 36 | -449 1014 110 249 | 24 21 | igr n/a| 0 0 0 -21 -28 -24 .03 6 6 | 10750 428 18 82 | -29 59 | jpl 122| 0 0 5 -17 74 -27 .59 17 16 | 2324 333 19 111 | -9 -78 | mit 264| 0 0 -1 60 -125 28 -.26 9 9 | -455 1037 23 131 | -21 25 | ngs 213| -1 0 3 46 213 -58 -.34 13 9 | -204 -176 2559 4049 | 37 13 | sio 256| 0 1 1 257 -262 37 -.22 21 20 | --- --- --- --- | -116 125 | Table 2.1515.3 GPS week: 1515 Day: 3 MJD: 54852.000 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 24 -20 8 -.10 8 8 | 1084 -2092 12 82 | 9 -12 | emr 74| 3 0 4 -309 -92 -68 .39 19 19 | 288 0 21 196 | 62 -13 | esa 134| 0 0 -3 28 66 0 .35 7 7 | 1280 -2514 18 124 | 21 -35 | gfz 193| -1 0 -4 -95 22 -43 -.10 9 9 | 624 -490 20 118 | 17 -8 | grg 79| 2 -6 -3 53 -58 14 1.17 37 34 | 262 -147 93 200 | -54 80 | igr n/a| 1 0 0 13 -62 -7 .05 5 5 | 10011 198 20 101 | -32 66 | jpl 122| 0 1 7 18 36 24 .57 17 16 | 1519 295 20 93 | 9 19 | mit 264| 0 1 1 -3 -97 37 -.30 9 8 | 107 85 18 118 | -3 23 | ngs 213| 0 0 1 101 143 -34 -.30 12 8 | 955 -1915 2359 4116 | -61 48 | sio 256| 0 2 2 155 -221 46 -.23 20 17 | --- --- --- --- | -81 127 | Table 2.1515.4 GPS week: 1515 Day: 4 MJD: 54853.000 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 1 9 -10 0 -.11 9 8 | -740 69 15 84 | 84 -50 | emr 74| 1 1 4 -338 -107 -47 .45 18 18 | -256 -333 20 140 | 72 36 | esa 134| 1 0 -2 15 99 25 .30 11 10 | -274 209 18 112 | 18 -69 | gfz 193| -1 -1 -3 -63 22 -26 -.13 10 10 | 202 -447 21 113 | 49 -24 | grg 79| 2 -3 -1 45 -57 4 1.28 34 33 | 317 -462 87 237 | 80 100 | igr n/a| 1 0 -1 -32 -41 -16 .04 6 5 | 9691 -550 19 77 | 49 48 | jpl 122| 0 1 5 -19 69 13 .56 17 15 | 1368 -595 18 98 | 36 -7 | mit 264| 0 1 -1 62 -110 -3 -.25 11 10 | 15 -175 20 89 | -13 24 | ngs 213| 0 0 0 76 142 -10 -.33 13 9 | -749 72 2453 4442 | 6 27 | sio 256| 1 2 2 249 -255 62 -.25 20 19 | --- --- --- --- | -110 147 | Table 2.1515.5 GPS week: 1515 Day: 5 MJD: 54854.000 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 30 -51 -41 -.08 9 8 | -937 583 11 74 | 11 39 | emr 74| 0 0 5 -296 -141 -82 .46 18 18 | -716 828 22 179 | 65 48 | esa 134| 2 0 -4 70 75 37 .27 10 10 | -2135 861 19 113 | -32 -40 | gfz 193| 0 0 -3 -92 3 34 -.16 9 9 | -125 105 19 113 | 37 32 | grg 79| 2 0 -4 156 -86 29 1.26 36 36 | -608 680 97 218 | 6 195 | igr n/a| 0 0 0 1 -67 -1 .07 5 4 | 8924 716 19 92 | -6 55 | jpl 122| 0 0 5 30 51 38 .58 17 15 | 526 634 16 92 | 20 22 | mit 264| 0 1 0 -5 -13 9 -.23 12 11 | -446 497 21 98 | 1 -7 | ngs 213| -2 0 2 79 45 -30 -.29 11 8 | -945 585 2547 4669 | 0 115 | sio 256| 1 1 3 143 -121 71 -.20 21 22 | --- --- --- --- | -69 112 | Table 2.1515.6 GPS week: 1515 Day: 6 MJD: 54855.000 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 2 23 -37 33 -.15 9 8 | -69 -389 14 103 | 75 -32 | emr 74| 0 -2 2 -335 -94 -65 .48 18 18 | -695 850 23 198 | 84 -17 | esa 134| -1 0 -1 19 54 41 .33 9 9 | 928 -2273 23 104 | -21 -9 | gfz 193| 0 0 -3 -55 2 -57 -.19 9 9 | 222 -330 20 113 | 47 -24 | grg 79| 4 0 3 87 -21 89 1.16 39 35 | -227 27 99 224 | 45 19 | igr n/a| 0 0 -2 5 -23 1 .06 5 5 | 8534 875 19 81 | -8 -51 | jpl 122| 0 -1 4 -2 61 78 .58 17 16 | 62 894 20 115 | 66 -21 | mit 264| 0 2 0 71 -110 20 -.28 16 13 | -187 44 22 94 | -14 6 | ngs 213| 0 0 0 37 116 -53 -.26 10 7 | -85 -390 2015 3391 | 38 22 | sio 256| 0 2 5 265 -234 51 -.25 25 22 | --- --- --- --- | -81 143 | 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 3.1515.0 GPS week: 1515 Day: 0 MJD: 54849.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 6 13 7 13 42 8 15 10 10 38 5 | 38 43 45 48 45 42 40 39 45 34 42 3 | 7 14 5 5 39 4 13 10 10 22 3 | 20 29 25 22 41 22 29 24 19 28 22 4 | 6 11 8 10 34 8 8 12 9 36 4 | 39 46 44 49 41 42 41 35 39 30 41 5E | 14 23 7 8 45 5 15 15 33 20 6 | 28 41 33 33 59 32 38 38 53 35 33 6 | 6 12 6 6 32 4 11 9 10 19 3 | 22 28 26 25 31 23 27 23 23 27 23 7 | 9 17 7 9 32 5 18 11 5 33 4 | 23 33 23 25 41 23 31 24 23 38 22 8 | 8 13 8 7 20 5 10 13 7 21 3 | 20 29 24 24 31 22 28 24 24 23 22 9 | 8 14 4 7 37 4 11 10 9 13 3 | 21 28 23 23 31 22 22 24 25 22 21 10 | 10 15 9 9 22 7 13 17 11 25 4 | 19 31 23 26 31 21 28 24 23 28 21 11 | 6 19 6 7 52 5 16 14 9 24 4 | 45 54 47 45 46 43 47 46 43 36 44 12E | 11 17 7 10 41 6 27 10 9 17 4 | 20 26 24 28 41 21 23 25 26 30 23 13 | 5 16 5 11 27 4 15 12 7 14 3 | 23 32 25 24 49 24 31 26 23 24 24 14 | 8 23 8 8 47 4 19 7 11 21 4 | 26 33 30 30 57 25 31 27 27 29 27 15 | 6 24 9 8 39 5 21 8 10 26 4 | 22 36 26 24 41 24 33 25 29 31 25 16E | 7 22 7 8 35 6 29 14 10 13 5 | 32 35 33 38 40 33 34 39 34 35 33 17 | 6 18 6 7 46 4 21 10 10 21 4 | 26 38 31 25 47 31 38 26 36 23 29 18 | 8 20 6 6 29 4 20 11 12 19 4 | 29 42 30 28 44 30 40 29 34 30 30 19 | 7 23 7 6 27 3 24 16 10 24 5 | 23 37 23 22 41 21 38 21 21 21 21 20 | 8 25 6 7 37 4 19 11 12 21 4 | 20 35 22 20 41 19 30 21 23 29 21 21 | 5 15 4 6 40 3 14 7 11 22 3 | 34 45 37 37 46 38 40 39 41 34 38 22 | 9 16 7 6 41 3 18 11 10 13 4 | 22 32 26 26 47 23 33 23 29 28 25 23 | 9 19 10 11 29 5 21 13 10 17 4 | 20 29 25 21 39 20 30 22 22 24 21 24 | 7 11 4 9 32 6 8 9 10 27 3 | 27 34 30 31 31 28 29 27 32 27 29 25 | 7 13 7 6 28 4 13 14 9 24 4 | 21 25 21 20 28 20 25 21 23 27 20 26 | 8 20 9 7 30 4 13 10 13 16 4 | 20 32 21 24 32 21 28 24 25 25 22 27 | 8 16 8 6 22 5 12 21 11 29 5 | 21 30 24 25 31 23 27 24 27 29 22 28E | 9 16 7 7 22 4 23 11 11 10 4 | 27 35 24 27 36 24 33 23 27 27 25 29 | 10 22 11 9 39 6 25 13 11 21 5 | 26 35 25 30 42 24 36 30 32 23 27 30E | 20 23 11 10 53 7 21 16 44 20 8 | 78 75 75 72 69 77 73 71 91 80 74 31 | 4 19 9 7 40 6 20 11 8 20 4 | 19 29 24 21 44 19 29 22 24 24 21 32 | 11 23 9 9 35 5 17 12 13 17 5 | 21 31 25 24 30 22 27 23 28 21 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 7 8 36 5 18 12 14 22 |T 26 35 29 29 41 27 33 28 31 29 28 WRMS | 8 18 7 8 32 5 16 11 9 20 |NE 24 34 27 27 39 25 32 26 28 27 26 MEDI | 8 17 7 7 35 5 17 11 10 21 |MD 23 33 25 25 41 23 31 24 27 28 24 Table 3.1515.1 GPS week: 1515 Day: 1 MJD: 54850.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 6 14 9 12 40 8 18 10 11 28 4 | 20 26 27 27 31 22 27 18 21 18 21 3 | 10 16 8 7 31 4 13 6 10 16 3 | 23 33 31 30 34 27 30 27 23 28 27 4 | 6 9 9 10 44 8 11 9 7 32 4 | 27 30 31 27 31 25 28 24 26 30 25 5E | 13 22 7 11 21 6 18 12 28 20 6 | 29 41 33 31 40 33 41 34 50 32 32 6 | 8 13 9 6 38 4 11 5 12 14 3 | 19 26 27 26 28 23 25 23 22 24 22 7 | 7 20 6 11 30 5 20 8 9 28 4 | 19 30 21 22 34 17 29 20 20 38 19 8 | 7 12 11 7 18 4 9 7 6 16 3 | 17 22 18 16 29 15 21 19 18 23 17 9 | 5 13 7 7 42 6 12 7 9 15 3 | 13 21 20 16 32 16 18 12 23 14 15 10 | 8 12 8 8 32 5 10 12 8 24 4 | 15 23 19 15 31 16 24 20 16 25 15 11 | 6 19 6 9 39 5 20 9 10 26 4 | 29 41 29 33 39 29 38 31 29 25 29 12E | 7 21 9 10 28 5 26 6 13 19 4 | 18 29 21 25 32 21 25 20 24 26 20 13 | 6 16 7 8 39 3 16 10 11 16 4 | 15 25 18 17 46 14 25 15 19 14 15 14 | 9 24 8 7 38 6 21 5 15 23 4 | 25 35 24 24 39 26 33 23 27 22 24 15 | 6 18 9 7 32 6 21 6 10 24 4 | 17 24 21 17 38 16 26 15 15 27 16 16E | 7 23 8 7 40 4 27 9 13 16 4 | 18 29 21 20 29 19 29 23 24 20 19 17 | 9 17 13 8 43 5 22 7 9 21 4 | 15 27 19 17 34 16 28 19 19 20 15 18 | 11 23 7 9 26 3 20 8 12 18 4 | 19 32 19 19 27 19 30 17 22 21 18 19 | 7 25 11 6 42 5 26 15 11 23 5 | 17 33 20 18 42 16 30 20 18 21 17 20 | 6 23 8 9 37 4 19 9 7 21 4 | 18 31 19 17 33 17 25 19 21 23 17 21 | 7 16 9 7 52 5 13 5 10 19 3 | 20 29 27 22 26 22 26 20 24 19 21 22 | 10 20 7 6 35 5 17 7 11 19 4 | 23 30 18 20 31 20 28 19 28 15 20 23 | 8 21 8 10 31 3 20 8 10 17 4 | 14 25 18 15 37 13 25 16 20 18 14 24 | 6 10 9 7 45 3 9 8 14 22 3 | 18 22 23 20 23 18 19 14 23 21 18 25 | 6 13 9 5 27 5 13 7 8 23 3 | 19 23 24 21 30 18 21 19 24 24 20 26 | 8 16 7 6 26 5 11 7 8 17 3 | 20 29 24 20 35 20 26 19 19 20 19 27 | 6 13 8 6 21 5 9 8 6 24 3 | 17 23 20 17 34 17 22 20 20 25 18 28E | 8 18 9 8 39 5 25 8 5 12 4 | 15 28 21 16 41 15 26 17 21 17 16 29 | 7 20 13 6 43 5 22 11 11 25 5 | 24 32 26 26 39 25 32 25 27 26 24 30E | 15 23 10 11 50 8 21 15 40 18 7 | 71 74 73 71 59 70 72 73 87 72 71 31 | 8 21 9 8 37 7 22 9 17 23 5 | 19 32 25 21 42 19 32 15 26 14 19 32 | 11 22 12 9 40 4 18 9 5 23 4 | 17 25 18 17 23 16 25 19 21 16 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 9 8 37 5 18 9 13 21 |T 20 30 24 22 34 21 28 21 25 23 21 WRMS | 8 18 9 8 35 5 17 8 8 21 |NE 19 28 22 20 33 19 26 19 21 21 19 MEDI | 7 18 9 8 38 5 18 8 10 21 |MD 19 29 21 20 34 19 26 19 22 22 19 Table 3.1515.2 GPS week: 1515 Day: 2 MJD: 54851.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 5 13 9 8 36 9 15 11 11 26 4 | 25 32 32 27 34 27 30 26 31 25 27 3 | 7 16 6 7 40 5 12 11 13 12 3 | 28 26 28 25 36 24 27 29 30 32 26 4 | 5 11 6 9 47 5 9 11 11 27 4 | 28 36 34 34 33 30 33 28 34 24 30 5E | 12 21 9 7 27 5 17 11 26 20 5 | 29 35 30 28 52 32 36 34 51 35 30 6 | 6 14 4 7 38 5 10 8 14 9 3 | 23 22 24 23 27 19 24 21 25 25 21 7 | 9 21 11 9 29 5 19 8 7 32 5 | 22 32 20 23 36 23 30 23 24 42 21 8 | 9 12 7 8 24 4 9 7 8 18 3 | 20 25 19 21 28 22 23 20 27 24 20 9 | 5 20 5 6 31 5 14 9 8 16 3 | 17 28 20 20 31 19 22 20 23 20 18 10 | 11 13 8 6 22 7 10 8 9 25 4 | 17 25 23 20 27 21 25 21 27 27 20 11 | 6 21 7 7 38 4 13 11 11 27 4 | 39 46 39 37 55 35 38 38 34 29 35 12E | 8 24 8 12 27 5 27 9 9 17 5 | 20 30 22 25 37 21 26 23 31 29 21 13 | 7 19 5 7 31 6 13 9 10 16 3 | 20 28 20 21 43 21 26 21 23 20 19 14 | 8 24 8 8 24 4 18 8 11 21 4 | 24 33 25 24 40 24 33 21 29 23 24 15 | 6 20 9 11 34 7 24 8 13 29 5 | 21 33 26 19 36 22 33 23 26 33 22 16E | 10 23 8 8 36 7 25 8 14 13 5 | 17 27 23 24 33 19 25 22 26 19 19 X17 | 10 19 14 --- 34 7 21 12 9 --- 6 | 24 30 24 --- 34 24 31 25 30 --- 23 18 | 11 23 6 9 28 4 23 8 12 16 4 | 24 35 22 25 39 26 36 23 32 27 25 19 | 6 24 9 7 40 8 22 15 10 23 5 | 21 34 21 21 44 23 33 22 25 22 20 20 | 8 24 6 8 40 5 20 11 9 22 4 | 20 30 19 22 38 19 29 19 22 24 19 21 | 7 14 5 6 69 3 16 8 9 20 3 | 28 34 29 28 44 30 32 30 34 29 29 22 | 11 17 8 7 38 4 16 7 8 17 4 | 29 37 27 29 46 30 36 26 33 31 29 23 | 8 25 9 8 30 5 17 8 9 18 4 | 19 28 21 21 35 19 24 19 22 22 18 24 | 6 10 7 5 51 6 12 9 11 21 3 | 25 29 26 25 30 27 29 23 32 25 26 25 | 7 14 8 8 36 6 12 10 8 23 4 | 23 25 23 24 32 23 27 23 24 28 22 26 | 7 16 7 7 33 7 11 8 9 25 3 | 21 30 23 22 32 20 30 21 21 24 21 27 | 9 14 6 8 21 4 9 7 9 23 3 | 20 24 18 22 29 21 22 20 27 27 20 28E | 8 17 11 9 32 7 20 8 12 11 4 | 19 28 19 22 37 21 27 22 28 23 20 29 | 11 25 8 6 43 8 24 10 9 26 5 | 29 40 29 31 44 31 37 33 39 32 31 30E | 16 23 11 9 84 7 20 12 36 20 7 | 42 43 38 38 53 40 46 44 64 46 40 31 | 10 23 12 8 35 6 24 11 10 18 5 | 20 32 28 26 43 23 34 21 30 20 23 32 | 10 24 12 8 38 4 15 10 11 21 4 | 19 30 23 23 25 20 26 20 25 19 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 8 8 39 6 17 9 13 21 |T 23 31 25 25 37 24 30 24 29 26 23 WRMS | 8 19 8 8 36 6 16 9 9 20 |NE 23 30 24 24 36 23 29 23 28 26 23 MEDI | 8 20 8 8 35 5 16 9 10 20 |MD 22 30 23 24 36 23 30 23 28 25 22 Table 3.1515.3 GPS week: 1515 Day: 3 MJD: 54852.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 5 12 8 9 26 6 14 11 10 24 4 | 28 31 32 31 36 27 29 27 28 23 27 3 | 8 15 3 9 33 5 10 6 10 13 3 | 42 44 41 40 60 42 45 44 42 48 42 4 | 5 10 8 10 41 5 8 11 11 27 4 | 30 35 34 35 55 30 30 27 33 24 30 5E | 10 19 8 9 32 8 16 11 24 23 5 | 32 40 35 34 46 35 41 36 46 35 34 6 | 7 14 4 10 40 5 11 7 12 10 3 | 22 26 25 27 36 24 25 24 19 27 23 7 | 6 22 9 11 35 5 19 11 8 29 5 | 21 34 26 24 39 21 28 25 23 34 21 8 | 7 10 8 7 20 4 10 6 8 14 3 | 16 23 22 20 31 17 22 18 19 20 17 9 | 6 12 6 7 27 5 11 7 7 12 3 | 16 21 18 21 34 17 20 20 18 16 17 10 | 9 12 5 7 26 6 9 9 8 24 3 | 16 22 18 20 33 14 21 17 20 25 16 11 | 6 19 6 9 40 5 15 10 13 27 4 | 42 48 44 44 51 43 43 42 45 32 41 12E | 7 24 5 11 35 6 24 8 10 17 4 | 20 30 21 25 33 23 25 25 28 29 22 13 | 6 16 4 11 32 5 14 8 9 14 3 | 19 27 20 20 47 16 22 19 19 18 18 14 | 5 24 7 9 30 4 16 9 11 23 4 | 21 30 26 21 35 23 28 22 27 25 22 15 | 6 22 8 9 37 5 22 7 7 32 4 | 22 30 24 24 40 21 30 21 23 34 22 16E | 7 24 6 9 45 7 28 10 12 14 5 | 20 30 24 24 38 21 31 21 23 24 21 17 | 10 21 8 13 26 5 21 7 7 21 4 | 20 33 24 26 36 21 31 23 23 26 21 18 | 11 22 8 9 28 3 22 8 13 16 4 | 22 32 23 20 38 23 34 23 31 23 22 19 | 6 25 9 6 31 6 23 14 10 22 5 | 21 35 22 19 43 20 34 22 20 22 19 20 | 6 23 6 12 32 4 18 12 10 23 4 | 23 32 22 24 34 19 29 22 23 27 21 21 | 8 12 7 6 76 4 13 7 9 17 3 | 26 32 32 31 53 27 29 30 31 29 29 22 | 13 19 10 8 38 4 19 7 12 16 4 | 35 41 29 37 46 35 40 35 43 39 35 23 | 9 23 6 11 22 4 18 10 9 16 4 | 21 30 24 20 36 17 25 19 22 23 19 24 | 7 11 10 10 32 6 10 8 11 16 3 | 26 29 29 33 22 28 28 26 35 25 28 25 | 5 14 7 7 23 6 9 11 6 23 3 | 20 26 25 19 26 19 22 22 22 28 20 26 | 10 16 7 9 25 5 12 8 9 20 4 | 26 33 28 29 35 25 33 27 26 25 26 27 | 6 13 7 6 17 4 10 7 8 23 3 | 16 25 22 19 28 18 21 18 21 24 18 28E | 6 13 6 7 45 5 18 8 8 11 3 | 21 26 21 21 33 19 24 22 21 18 19 29 | 7 21 11 7 53 6 23 13 15 22 5 | 25 31 22 24 44 23 30 26 28 20 22 30E | 13 22 11 10 71 6 18 14 34 23 6 | 81 82 82 77 84 81 82 82 92 83 81 31 | 6 25 7 7 27 6 22 11 11 21 4 | 19 32 22 22 39 20 30 23 28 23 21 32 | 9 24 9 9 35 6 18 7 12 20 4 | 20 29 21 23 28 17 25 19 23 20 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 7 9 37 5 17 9 12 20 |T 25 32 27 27 39 25 30 26 29 28 25 WRMS | 8 19 7 9 34 5 16 8 8 16 |NE 23 31 25 25 38 23 29 24 26 26 23 MEDI | 7 19 7 9 32 5 16 8 10 21 |MD 21 31 24 24 36 21 29 23 23 25 22 Table 3.1515.4 GPS week: 1515 Day: 4 MJD: 54853.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 7 13 8 15 31 5 12 13 9 21 4 | 25 30 31 37 32 27 28 29 27 25 28 3 | 8 13 16 6 42 9 11 9 16 17 4 | 30 38 39 34 36 28 35 34 26 34 33 4 | 9 11 6 12 48 5 7 13 11 22 4 | 23 33 33 36 54 29 29 28 27 24 27 5E | 12 20 12 11 40 7 14 10 23 23 5 | 25 37 31 30 56 27 36 27 37 30 28 6 | 6 11 14 5 33 6 13 12 17 16 4 | 19 24 22 22 27 18 23 22 24 21 20 7 | 8 19 10 8 31 5 19 12 11 28 5 | 17 30 18 17 39 14 25 22 21 30 16 8 | 9 9 9 6 18 4 10 7 7 15 3 | 13 19 15 14 27 12 18 15 16 15 12 9 | 8 13 9 8 27 4 8 9 8 15 3 | 13 21 20 18 24 15 18 16 16 15 15 10 | 9 13 8 7 36 6 10 12 9 24 4 | 14 22 17 19 35 17 20 20 18 28 15 11 | 9 19 9 10 47 6 14 13 12 25 5 | 37 47 40 42 39 36 40 39 33 30 36 12E | 9 21 10 15 28 6 21 10 8 17 5 | 17 27 18 23 36 18 22 22 19 28 19 13 | 6 17 10 11 29 6 15 8 7 15 4 | 15 26 23 12 43 14 22 17 12 19 14 14 | 8 18 11 10 22 4 17 15 16 15 5 | 15 25 20 16 40 16 24 19 23 12 16 15 | 5 21 11 9 34 5 21 9 11 34 5 | 15 26 17 16 40 14 23 16 14 32 14 16E | 7 28 11 16 39 7 27 11 13 12 6 | 21 35 25 30 31 20 32 23 21 26 24 17 | 10 19 9 11 29 3 19 12 10 20 5 | 17 31 15 18 36 15 28 20 21 21 16 18 | 12 19 7 10 30 4 24 9 14 18 5 | 19 29 19 18 35 17 30 18 23 23 18 19 | 8 25 10 8 29 9 22 16 10 21 5 | 17 34 21 17 39 16 31 25 16 26 18 20 | 6 22 7 13 35 3 17 9 12 23 5 | 17 28 15 17 32 12 23 16 14 21 12 21 | 9 10 9 8 54 4 15 7 10 19 4 | 22 29 28 26 31 25 27 27 29 25 25 22 | 9 15 10 10 37 3 20 10 11 19 4 | 32 34 34 32 45 30 36 26 34 28 29 23 | 6 24 12 12 23 5 18 12 8 16 5 | 14 28 20 12 32 13 21 14 14 16 12 24 | 8 10 10 6 35 5 9 12 11 13 3 | 25 29 28 27 33 25 26 27 29 25 25 25 | 6 14 12 11 16 6 10 12 10 29 4 | 16 21 19 16 23 14 17 17 18 23 14 26 | 9 17 10 9 21 5 10 9 10 19 4 | 25 32 28 28 33 23 28 24 23 23 23 27 | 8 10 10 7 17 3 8 7 8 24 3 | 14 19 17 13 28 12 17 16 16 23 13 28E | 7 13 8 7 31 4 19 9 8 12 3 | 19 28 21 21 27 19 27 23 19 15 20 29 | 8 23 15 10 39 7 23 10 15 22 5 | 24 36 25 27 34 23 31 27 26 29 25 30E | 15 19 16 12 57 10 16 17 34 23 7 | 54 60 58 54 69 55 59 52 68 54 55 31 | 9 24 10 10 31 5 24 14 15 14 5 | 14 32 19 18 40 15 30 14 18 14 15 32 | 9 18 12 10 27 6 20 7 8 17 4 | 19 25 14 19 29 14 25 19 13 19 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 11 10 34 6 17 11 13 20 |T 20 30 24 23 36 20 27 23 23 24 21 WRMS | 8 18 10 10 33 5 15 10 9 19 |NE 19 28 22 21 34 19 25 21 21 23 19 MEDI | 8 18 10 10 31 5 16 10 11 19 |MD 19 29 21 19 35 17 27 22 21 24 18 Table 3.1515.5 GPS week: 1515 Day: 5 MJD: 54854.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 7 12 8 10 34 7 12 9 10 22 4 | 20 26 24 23 31 20 22 20 23 18 20 3 | 11 16 13 9 52 6 11 28 12 29 6 | 45 52 46 41 68 42 52 52 38 54 44 4 | 7 8 6 9 34 4 6 8 10 21 3 | 22 27 25 28 25 23 23 23 23 19 22 5E | 9 22 10 11 33 7 15 13 21 22 5 | 33 42 35 31 56 31 40 35 40 35 33 6 | 8 9 12 9 47 5 10 27 10 23 5 | 21 26 23 21 39 19 27 27 13 28 19 7 | 8 23 11 11 35 4 19 15 8 27 5 | 17 33 19 24 38 17 27 27 20 30 18 8 | 9 10 10 6 27 3 9 7 6 14 3 | 16 22 18 18 30 16 18 19 18 15 15 9 | 11 13 8 9 34 4 12 8 9 14 3 | 14 22 16 20 25 15 17 17 19 15 15 10 | 11 17 9 10 27 4 9 11 7 28 4 | 13 27 14 20 25 15 20 16 16 26 13 11 | 7 17 10 6 27 6 16 10 9 33 4 | 33 42 41 35 53 33 39 32 33 24 33 12E | 9 24 10 12 32 3 20 8 7 18 5 | 17 32 21 23 36 18 21 24 23 26 20 13 | 5 17 8 8 33 3 17 9 7 13 3 | 16 29 18 14 43 15 23 14 17 14 15 14 | 9 20 9 9 39 5 17 9 9 18 4 | 15 25 24 21 45 19 24 22 17 19 18 15 | 7 20 13 10 48 6 19 7 9 34 5 | 13 27 20 17 44 16 22 13 16 30 14 16E | 6 21 11 8 44 4 25 10 12 20 5 | 24 34 30 24 47 25 32 24 19 23 24 17 | 8 21 9 11 26 3 21 8 12 18 5 | 20 31 20 20 30 20 29 25 21 23 19 18 | 11 17 11 9 34 3 22 11 9 18 5 | 16 28 20 17 35 17 29 21 22 23 18 19 | 7 24 10 7 34 4 23 12 10 20 5 | 18 34 21 17 42 17 31 20 14 17 18 20 | 6 26 10 9 49 4 20 10 10 22 5 | 17 30 21 18 40 14 25 17 17 19 16 21 | 8 13 8 8 44 3 15 7 12 19 4 | 18 25 21 24 26 19 23 24 21 19 20 22 | 10 13 10 8 35 3 18 11 8 16 4 | 27 30 24 22 42 25 32 24 28 29 24 23 | 6 22 8 10 28 3 18 16 9 16 4 | 15 28 18 12 32 12 21 13 15 13 12 24 | 7 11 10 9 36 4 8 10 13 13 3 | 16 25 22 25 38 18 17 20 21 19 18 25 | 6 14 7 3 26 4 11 9 8 23 3 | 14 22 15 14 26 12 17 15 14 19 13 26 | 13 18 12 10 40 4 11 12 9 21 4 | 26 33 25 29 48 26 30 27 28 25 25 27 | 10 11 7 7 19 2 10 10 7 23 3 | 16 25 20 19 28 18 19 19 19 22 16 28E | 8 13 9 10 29 4 21 8 7 9 4 | 15 22 17 18 31 15 21 17 17 16 14 29 | 7 21 10 8 40 6 23 10 13 20 5 | 22 34 23 27 28 20 27 23 27 34 23 30E | 12 24 13 11 42 9 15 19 30 23 7 | 95 101 95 95 87 95 99 98 104 99 97 31 | 9 22 10 7 39 5 22 15 11 19 5 | 13 32 16 14 41 14 27 17 17 19 14 32 | 8 17 11 7 35 5 17 9 9 19 4 | 17 25 19 19 25 16 24 18 19 17 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 10 9 36 5 17 12 11 21 |T 22 31 24 24 38 22 28 24 23 25 22 WRMS | 8 18 10 9 36 4 15 11 8 22 |NE 19 29 22 21 36 19 25 21 20 22 19 MEDI | 8 17 10 9 34 4 17 10 9 20 |MD 17 28 21 21 38 18 24 21 19 22 18 Table 3.1515.6 GPS week: 1515 Day: 6 MJD: 54855.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 13 6 9 53 6 14 11 8 22 3 | 33 39 37 37 44 35 34 35 39 33 35 3 | 6 19 6 9 32 4 15 18 7 29 4 | 24 34 30 25 44 26 32 28 26 34 27 4 | 9 9 4 9 39 4 10 14 8 19 3 | 32 35 36 37 44 34 33 31 33 27 32 5E | 11 23 12 11 36 6 14 18 19 27 6 | 41 53 40 43 63 42 48 42 47 37 40 6 | 5 20 10 10 50 4 11 23 11 26 5 | 22 30 26 24 39 22 24 28 25 32 24 7 | 19 23 8 11 32 6 21 17 9 31 6 | 26 34 25 25 41 22 29 32 24 33 23 8 | 9 11 6 6 21 7 10 10 9 21 3 | 20 25 22 20 28 20 24 23 21 23 20 9 | 7 17 7 8 34 5 12 12 5 16 3 | 20 30 20 23 30 20 23 22 19 18 20 10 | 9 15 7 7 21 4 9 10 8 27 4 | 18 28 20 21 33 20 23 23 21 31 20 11 | 7 17 6 5 48 5 13 14 11 35 4 | 45 54 49 49 46 47 49 48 44 38 46 12E | 10 22 6 13 46 6 22 13 9 21 5 | 20 29 23 25 26 21 24 25 20 29 20 13 | 5 20 7 5 35 4 14 11 8 20 3 | 21 33 24 22 48 21 26 21 19 21 21 14 | 6 19 9 11 32 4 18 14 9 17 4 | 23 33 26 24 43 23 31 26 26 24 26 15 | 5 22 10 9 37 7 20 12 9 35 5 | 24 32 25 24 40 22 30 22 21 37 23 16E | 8 25 11 12 50 4 24 12 13 24 5 | 20 29 24 22 45 20 28 21 20 25 19 17 | 9 21 9 9 23 4 24 12 12 22 5 | 27 36 27 23 34 24 32 29 24 33 25 18 | 8 18 7 11 35 4 23 14 7 23 4 | 25 31 26 22 37 24 36 28 28 31 25 19 | 8 22 11 7 32 5 24 13 9 20 5 | 24 33 21 21 48 21 34 24 23 21 20 20 | 7 22 10 9 42 4 24 16 9 22 5 | 23 34 21 19 39 19 30 21 21 27 21 21 | 8 14 9 7 85 3 15 11 8 23 4 | 33 38 37 36 57 32 35 36 32 34 34 22 | 8 16 8 10 37 6 19 14 6 20 4 | 26 38 28 29 51 29 37 31 31 37 30 23 | 6 22 11 6 34 5 18 15 9 22 4 | 23 35 26 23 44 23 29 23 23 24 23 24 | 6 10 8 6 35 6 10 14 10 17 3 | 28 31 33 35 36 29 29 31 29 30 30 25 | 6 14 7 5 18 6 10 10 7 31 3 | 24 27 21 22 28 22 26 24 24 32 21 26 | 13 17 8 9 46 7 15 39 12 48 7 | 70 78 77 72 50 67 74 85 63 80 71 27 | 8 12 7 5 17 5 9 10 9 27 3 | 20 25 21 20 30 20 23 21 22 26 21 28E | 8 12 5 7 26 5 16 11 6 17 3 | 22 24 19 17 27 19 21 20 18 17 17 X29 | 7 24 15 7 45 5 23 13 9 --- 5 | 30 42 28 32 48 29 37 33 27 --- 29 30E | 14 24 13 11 24 6 18 22 24 24 6 | 89 91 87 88 82 87 92 91 94 89 86 31 | 8 20 9 5 37 4 20 16 8 18 4 | 20 32 24 21 40 18 30 21 21 18 21 32 | 6 16 14 8 32 5 17 13 8 20 4 | 22 27 24 21 27 20 27 24 21 25 21 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 9 9 39 5 17 16 10 25 |T 28 36 30 29 41 28 33 31 29 32 28 WRMS | 8 18 9 9 35 5 16 13 7 22 |NE 27 35 29 27 40 26 32 29 27 30 27 MEDI | 8 19 8 9 35 5 16 13 9 22 |MD 24 33 26 24 41 22 30 26 24 30 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 4.1515 GPS week: 1515 MJD: 54849.0-54855.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 |U 9 7 22 |U 12 13 38 |U 14 14 30 | emr | emr 2968 | 15 14 32 | 13 15 43 | 15 13 29 | esa | esa 2976 | 13 11 25 |U 12 15 40 | 13 13 28 | gfz | gfz 2929 |U 12 11 34 |U 13 15 45 | 15 16 40 | grg | grg 62 | 32 24 77 |U 70 46 144 | 11 17 84 | igr | igr 2974 | 11 10 25 | 12 14 39 | 14 13 29 | igs | igs 2968 | 12 9 26 | 12 14 38 | 14 14 30 | jpl | jpl 2968 |U 21 17 36 |U 13 16 39 | 15 13 28 | mit | mit 2976 |U 16 16 36 |U 14 20 44 |U 14 14 31 | 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 5.1515.0 GPS week: 1515 Day: 0 MJD: 54849.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 9 9 26 | 20 27 68 | 14 14 24 | emr | emr 2968 | 15 16 33 | 23 32 78 | 13 10 26 | esa | esa 2976 | 16 14 30 | 20 30 71 | 12 12 25 | gfz | gfz 2957 | 15 9 35 | 21 31 74 | 14 15 30 | grg | grg 62 | 11 17 80 | 117 70 456 | 10 22 106 | igr | igr 2974 | 13 14 30 | 19 29 68 | 12 12 23 | igs | igs 2934 | 14 13 31 | 20 30 67 | 13 15 29 | jpl | jpl 2968 | 23 24 33 | 22 35 74 | 15 12 26 | mit | mit 2976 | 14 14 36 | 22 36 80 | 14 15 32 | Table 5.1515.1 GPS week: 1515 Day: 1 MJD: 54850.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 11 8 27 | 11 9 28 | 16 17 37 | emr | emr 2968 | 21 15 41 | 12 10 37 | 15 14 27 | esa | esa 2976 | 16 12 30 | 10 10 26 | 15 15 32 | gfz | gfz 2860 | 14 31 58 | 14 11 43 | 18 19 48 | grg | grg 62 | 85 35 79 | 88 82 343 | 7 12 114 | igr | igr 2972 | 12 9 28 | 11 11 30 | 15 14 31 | igs | igs 2971 | 17 12 30 | 11 11 30 | 16 16 35 | jpl | jpl 2968 | 42 25 69 | 12 14 32 | 17 15 34 | mit | mit 2976 | 14 34 71 | 16 28 39 | 15 14 37 | Table 5.1515.2 GPS week: 1515 Day: 2 MJD: 54851.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 8 7 20 | 12 13 50 | 15 17 30 | emr | emr 2968 | 12 12 25 | 14 14 44 | 12 11 22 | esa | esa 2976 | 11 9 23 | 10 14 50 | 13 13 24 | gfz | gfz 2862 | 12 11 28 | 16 17 61 | 14 15 36 | grg | grg 62 | 19 37 218 | 93 50 9 | 10 16 64 | igr | igr 2975 | 10 8 22 | 12 14 49 | 13 13 25 | igs | igs 2975 | 11 10 22 | 12 13 48 | 14 15 27 | jpl | jpl 2968 | 10 12 23 | 12 13 45 | 13 12 24 | mit | mit 2976 | 9 8 30 | 13 15 44 | 13 15 26 | Table 5.1515.3 GPS week: 1515 Day: 3 MJD: 54852.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 10 7 18 | 8 9 34 | 14 14 33 | emr | emr 2968 | 17 16 27 | 11 11 38 | 14 12 24 | esa | esa 2976 | 13 12 19 | 8 10 30 | 13 12 28 | gfz | gfz 2957 | 12 6 31 | 7 10 39 | 15 15 41 | grg | grg 62 | 42 34 44 | 82 14 62 | 4 10 80 | igr | igr 2976 | 13 12 21 | 8 9 31 | 14 12 32 | igs | igs 2975 | 11 9 19 | 8 11 32 | 13 13 31 | jpl | jpl 2968 | 27 19 41 | 8 14 30 | 15 13 26 | mit | mit 2976 | 20 8 27 | 8 15 32 | 12 12 25 | Table 5.1515.4 GPS week: 1515 Day: 4 MJD: 54853.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 8 7 26 | 15 14 41 | 14 15 31 | emr | emr 2968 | 14 14 36 | 16 14 38 | 24 19 42 | esa | esa 2976 | 11 9 28 | 17 17 43 | 14 14 29 | gfz | gfz 2956 | 10 6 34 | 17 14 41 | 17 18 45 | grg | grg 62 | 33 30 5 | 49 72 33 | 12 21 43 | igr | igr 2975 | 10 9 28 | 16 15 41 | 16 15 33 | igs | igs 2975 | 11 8 33 | 16 14 40 | 14 15 31 | jpl | jpl 2968 | 20 16 38 | 18 14 41 | 14 13 27 | mit | mit 2976 | 22 16 28 | 17 19 46 | 17 19 42 | Table 5.1515.5 GPS week: 1515 Day: 5 MJD: 54854.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 10 7 25 | 9 8 28 | 13 13 29 | emr | emr 2968 | 16 14 30 | 10 11 36 | 15 13 32 | esa | esa 2976 | 13 10 27 | 10 10 35 | 14 14 32 | gfz | gfz 2956 | 14 8 33 | 10 11 28 | 16 16 43 | grg | grg 62 | 6 0 54 | 45 14 62 | 14 18 75 | igr | igr 2976 | 12 10 27 | 10 9 31 | 14 14 32 | igs | igs 2976 | 13 9 26 | 10 9 31 | 14 13 31 | jpl | jpl 2968 | 13 11 25 | 10 11 34 | 16 14 36 | mit | mit 2976 | 25 19 38 | 11 10 35 | 13 13 29 | Table 5.1515.6 GPS week: 1515 Day: 6 MJD: 54855.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 4 16 | 8 10 20 | 12 11 23 | emr | emr 2968 | 13 11 28 | 9 12 28 | 14 13 29 | esa | esa 2976 | 10 8 21 | 8 13 26 | 12 13 26 | gfz | gfz 2959 | 9 7 20 | 8 14 29 | 13 15 34 | grg | grg 62 | 27 15 62 | 14 23 45 | 17 18 109 | igr | igr 2976 | 9 7 23 | 7 10 24 | 12 12 26 | igs | igs 2976 | 9 6 20 | 7 11 22 | 12 13 26 | jpl | jpl 2968 | 12 8 25 | 8 13 20 | 14 13 26 | mit | mit 2976 | 9 9 22 | 8 16 30 | 12 14 27 | 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 6.1515 GPS week: 1515 MJD: 54849.500-54855.500 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 | 23 -28 72 70 7 | -2 20 | 23 30 114 68 5 | 3 emr uuuuu | 9 -55 3 149 -7 | 28 34 | 26 10 97 90 5 | 4 esa uuuuu | 24 25 89 10 8 | -15 27 | 39 35 171 64 13 | 3 gfz uuuuu | 20 -28 38 46 1 | 2 19 | 10 7 70 66 5 | 4 grg xxxxx | -62 -10 120 61 11 | 10 83 | 54 35 100 48 56 | 14 igr xxxxx | -17 20 75 61 6 | -11 18 | 41 25 92 72 15 | 2 irf xxxxx | 6 9 -40 13 0 | -1 18 | 14 8 23 59 3 | 3 jpl uuuuu | 48 -12 -5 113 -3 | -2 26 | 53 31 136 68 9 | 6 mit uuuuu | -10 11 -183 -135 1 | 4 20 | 24 20 79 128 11 | 3 ngs uuuuu | -31 -8 48 -88 -2 | -1 23 | 26 38 116 94 16 | 6 sio uuxxu | -121 103 60 -370 -5 | 8 23 | 24 19 147 111 9 | 3 Table 7.1515.0 GPS week: 1515 Day: 0 MJD: 54849.500 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 4 110 -1 -2 | -5 16 emr uuuuu | 10 -35 -172 56 -9 | 27 33 esa uuuuu | -11 47 136 58 -16 | -14 21 gfz uuuuu | 19 -36 82 24 0 | -2 17 grg xxxxx | -14 -9 201 24 91 | 16 119 igr xxxxx | -5 25 84 8 -6 | -11 18 irf xxxxx | -14 0 -67 58 2 | -3 13 jpl uuuuu | 138 38 -61 75 -16 | 1 24 mit uuuuu | -37 -14 -242 15 13 | -1 15 ngs uuuuu | -7 -60 31 -251 4 | 3 22 sio uuxxu | -139 110 115 -367 2 | 4 19 Table 7.1515.1 GPS week: 1515 Day: 1 MJD: 54850.500 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 67 64 7 | -5 16 emr uuuuu | 15 -49 23 145 -14 | 27 33 esa uuuuu | -12 74 -121 -27 6 | -16 24 gfz uuuuu | 28 -27 86 -50 3 | -1 16 grg xxxxx | -50 -10 56 54 -85 | 29 122 igr xxxxx | 14 36 51 111 -21 | -11 18 irf xxxxx | 8 14 -13 49 4 | -3 13 jpl uuuuu | 84 -47 196 119 -7 | 1 25 mit uuuuu | -10 -11 -88 -2 10 | 0 14 ngs uuuuu | -32 -26 37 -42 -27 | 3 22 sio uuxxu | -99 106 246 -369 4 | 4 19 Table 7.1515.2 GPS week: 1515 Day: 2 MJD: 54851.500 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 | 47 -55 98 -37 7 | 2 21 emr uuuuu | 48 -63 -15 304 -8 | 31 37 esa uuuuu | -10 -4 -70 -9 -1 | -12 26 gfz uuuuu | 23 -23 -1 60 5 | 5 21 grg xxxxx | -21 -16 196 30 -31 | 28 122 igr xxxxx | -59 37 -50 165 12 | -9 18 irf xxxxx | 0 8 -24 52 1 | 2 19 jpl uuuuu | 78 17 66 219 -9 | 4 27 mit uuuuu | -25 29 -119 -189 10 | 5 22 ngs uuuuu | -13 -29 248 -128 -9 | 5 23 sio uuxxu | -125 124 117 -484 3 | 10 25 Table 7.1515.3 GPS week: 1515 Day: 3 MJD: 54852.500 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 | 22 -9 207 100 7 | 1 22 emr uuuuu | 23 -62 10 213 -13 | 31 37 esa uuuuu | 45 -21 -41 49 19 | -14 28 gfz uuuuu | 18 -17 134 36 5 | 5 21 grg xxxxx | -70 54 85 43 32 | -9 62 igr xxxxx | -56 32 15 1 5 | -9 18 irf xxxxx | 10 0 -18 23 -1 | 2 20 jpl uuuuu | -9 -9 -156 84 -4 | 1 29 mit uuuuu | -13 3 -102 -138 2 | 6 22 ngs uuuuu | -38 61 141 -108 -12 | 2 25 sio uuxxu | -117 81 200 -315 -3 | 10 24 Table 7.1515.4 GPS week: 1515 Day: 4 MJD: 54853.500 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 | 54 -70 150 111 14 | 0 21 emr uuuuu | -32 -58 -1 97 -5 | 30 37 esa uuuuu | 73 -4 311 95 8 | -15 28 gfz uuuuu | 28 -35 56 113 4 | 5 21 grg xxxxx | -96 -66 98 20 31 | 4 53 igr xxxxx | -44 -35 82 106 10 | -10 18 irf xxxxx | 4 14 -47 -3 -2 | 2 20 jpl uuuuu | 11 -22 -115 12 1 | -3 27 mit uuuuu | -20 27 -201 -168 -1 | 7 22 ngs uuuuu | -23 8 -112 -120 -3 | -1 23 sio uuxxu | -143 124 -81 -348 -7 | 12 25 Table 7.1515.5 GPS week: 1515 Day: 5 MJD: 54854.500 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 -5 24 98 10 | 0 22 emr uuuuu | -17 -59 21 56 -3 | 27 35 esa uuuuu | 71 38 276 -5 16 | -16 29 gfz uuuuu | -1 -31 -21 -6 -4 | 3 21 grg xxxxx | -164 0 -40 148 6 | 5 53 igr xxxxx | -24 12 93 -37 19 | -11 19 irf xxxxx | 31 6 -37 25 -2 | 0 20 jpl uuuuu | 9 -14 -96 106 8 | -7 27 mit uuuuu | 38 5 -238 -97 -7 | 7 22 ngs uuuuu | -84 6 12 13 9 | -6 24 sio uuxxu | -81 75 -35 -186 -12 | 12 25 Table 7.1515.6 GPS week: 1515 Day: 6 MJD: 54855.500 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 | 33 -54 -151 156 7 | -5 20 emr uuuuu | 18 -63 159 169 1 | 20 28 esa uuuuu | 10 42 134 -96 22 | -19 30 gfz uuuuu | 25 -26 -66 142 -7 | -3 20 grg xxxxx | -18 -24 248 103 34 | 0 52 igr xxxxx | 52 29 251 68 20 | -15 19 irf xxxxx | 1 21 -70 -112 -5 | -4 21 jpl uuuuu | 22 -45 132 176 8 | -13 25 mit uuuuu | -5 35 -287 -365 -18 | 3 23 ngs uuuuu | -21 -17 -21 16 21 | -12 21 sio uuxxu | -142 102 -141 -521 -20 | 7 25