Date: Thu, 31 Dec 2009 13:01:40 +0000 From: Jim Ray Subject: [IGSREPORT-18143] Wk 1562 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4b3ca0b4.Qcv7/kwDfqsy4aAF%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 31 Dec 05:02:03 PST 2009 Message Number 18143 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1562 (Dec 13, 2009 - Dec 19, 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: igs1562[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1562[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1562[0-6].cls IGS GPS clock combination summary report. igs15627.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15627.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 | 32 32 0 | EMR | WTZR 0 | ESA | 32 0 | GFZ | 2 3 5 9 17 18 ALGO AREQ ARTU BOR1 BRAZ BRFT BRUS 0 | GFZ | CEDU CONZ DAEJ FAA1 HARB HOLM HRM1 HYDE ISPA KERG 0 | GFZ | KIT3 LPGS MAL2 MAS1 MAW1 MCM4 MDO1 METS NTUS ONSA 0 | GFZ | PETP PRDS PRE1 QAQ1 RABT REUN RIOP SANT SFER SUWN 0 | GFZ | TSKB WHIT WSRT YELL YKRO ZIMM 0 | GRG | WTZR 0 | JPL | 32 DGAR KARR 0 | MIT | 1 24 10 24 1 | COD | 10 32 10 32 ONSA 1 | EMR | WTZR 1 | ESA | 10 32 MAW1 MCM4 YELL 1 | GFZ | 3 5 7 11 15 18 20 22 ALGO ALIC AMC2 ARTU AUCK BAKO 1 | GFZ | BOGT BOR1 BRUS COCO DAV1 EIL1 GLPS GODE GUAM GUAT 1 | GFZ | HOB2 HOLM HYDE KIRU KIT3 MAC1 MAS1 MBAR MDO1 NICO 1 | GFZ | NTUS NYA1 NYAL ONSA PETP PIE1 QAQ1 RABT RIOP SANT 1 | GFZ | SHAO SUWN TEHN TWTF UNSA VESL VILL WAB2 WSRT YAKT 1 | GFZ | YELL YKRO YSSK ZIMM 1 | GRG | SPT0 1 | JPL | 32 DGAR 1 | MIT | PDEL 2 | COD | 1 10 1 10 2 | EMR | WTZR 2 | ESA | 10 32 2 | GFZ | 3 5 11 18 20 22 23 ADE1 BOGT BOR1 BUE1 CONZ CRO1 2 | GFZ | DAEJ DAV1 DUBO EIL1 FAIR GOLD GUAT HARB HOLM HRAO 2 | GFZ | KOUR MAL2 MAS1 MBAR MCM4 MDO1 MIZU NRMD NTUS NYA1 2 | GFZ | NYAL ONSA PIE1 PRE1 QAQ1 RABT RAMO REUN RIOP SANT 2 | GFZ | SFER SHAO SUWN UNSA YAKT YELL 2 | GRG | ONSA 2 | JPL | 32 DGAR RAMO 2 | MIT | 24 24 KERG OUS2 3 | COD | 32 10 32 NRIL 3 | EMR | 24 24 MCM4 3 | ESA | 10 32 3 | GFZ | 2 3 13 17 18 22 30 32 AMC2 AREQ ARTU BOR1 BRAZ BRUS 3 | GFZ | COCO CONZ DAV1 DGAR GODE GRAS GRAZ GUAT HARB HOLM 3 | GFZ | HYDE ISPA KERG KIRU MAL2 MDO1 METS PERT PIMO QAQ1 3 | GFZ | RAMO RIOP SANT SFER STJO THTI TIDB TIXI TLSE TOW2 3 | GFZ | TWTF USUD VILL WAB2 WHIT WTZR YAKT ZIMM 3 | GRG | ONSA 3 | JPL | 32 DGAR 3 | NGS | 1 4 | ALL | 1 4 | COD | 10 4 | EMR | WTZR 4 | ESA | 10 32 YELL 4 | GFZ | 5 18 32 ALIC AMC2 AUCK BRUS CAS1 CHAT CRO1 DAEJ DAV1 4 | GFZ | EIL1 GUAT HARB HRM1 HYDE KOUR MAC1 MAL2 MCM4 MDO1 4 | GFZ | ONSA PERT RESO RIOP SHAO SUTM THTI THU3 TOW2 VESL 4 | GFZ | WSRT WTZR YAKT YELL 4 | GRG | SPT0 4 | JPL | 32 DGAR 4 | MIT | 1 HARB KHAJ TLSE 5 | COD | 32 32 5 | EMR | WTZR WTZR 5 | ESA | 10 32 UNSA 5 | GFZ | 10 18 22 30 32 AMC2 AREQ ASPA AUCK BRFT BRUS CONZ 5 | GFZ | CRO1 DAV1 DGAR DUBO FAA1 GUAT HARB HOLM KERG MAC1 5 | GFZ | MDO1 NRMD NTUS ONSA PIE1 RAMO RIOP SANT SFER STJO 5 | GFZ | SYOG TIDB TOW2 WTZR YELL 5 | GRG | ONSA 5 | JPL | 32 DGAR 5 | MIT | 24 27 24 27 SYOG HARB SYOG 6 | COD | 32 GUAT 6 | EMR | 1 WTZR 6 | ESA | 32 FAA1 UNSA 6 | GFZ | 5 18 BOR1 BRFT BRUS CHAT CHPI DAEJ DAV1 DGAR EIL1 6 | GFZ | FLIN HOFN HRM1 MAC1 MAW1 METS MKEA NRIL PERT PETP 6 | GFZ | RAMO SANT SFER SYOG TEHN THU3 TIXI TOW2 TSKB VILL 6 | GFZ | WHIT YAKT YKRO YSSK 6 | GRG | ONSA 6 | JPL | 32 DGAR 6 | MIT | 24 24 SYOG HARB 6 | NGS | 1 5. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447. 6. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | -.2 1.6 -.3 -16 -5 -30 .25 EMR | 5.4 -2.7 5.9 53 -13 12 .49 ESA | 4.1 5.6 -10.2 91 -47 63 .41 GFZ | .3 1.3 1.1 20 -11 -7 .20 GRG | 3.0 13.8 -11.1 44 -7 -187 .85 JPL | 3.4 2.7 20.4 25 -48 -28 .41 MIT | 2.4 1.3 -5.6 14 -2 -23 .22 NGS | 4.8 1.1 -5.0 10 -82 -18 .26 SIO | 3.4 4.1 4.4 60 -21 8 .55 7. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 8. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 9. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five parts. The first, Table 1, summarizes all statistics for the week. It contains means and standard deviations over the week of satellite ephemeris and clock correction transformation parameters for each centre (table 1.1562.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1562.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 2.1562.[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 3.1562.[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 5.1562.0-6). 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 1562 summary. (Dec 13, 2009 - Dec 19, 2009) Table 1.1562.a GPS week: 1562 MJD: 55178.000-55184.000 Mean and standard deviations of transformation parameters to the combined IGS orbit. WRMS - orbit RMS weighted by the SP3 header accuracy codes. STA - Mean number of stations in the daily solutions. CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 240| 0 0 2 77 -38 -13 -.15 9 8 | -352 74 19 71 | 0 0 0 16 20 24 .03 | 370 637 emr 91| 0 -2 4 -46 -19 0 .46 18 18 | 1019 -263 28 115 | 1 1 2 26 38 15 .03 | 1173 1404 esa 125| 1 0 -3 -94 -24 6 .28 9 9 | -147 244 19 113 | 0 0 1 5 36 20 .03 | 949 1706 gfz 198| 0 -1 -3 15 -32 -16 -.15 11 11 | 162 -202 37 138 | 0 1 1 43 68 11 .03 | 575 1781 grg 110| -2 0 -13 -75 -69 -6 1.09 24 21 | 136 -63 63 222 | 1 1 1 23 40 17 .03 | 322 264 igr n/a| 0 0 -1 57 -33 -44 .05 5 5 | 5461 -247 23 73 | 0 0 0 27 25 25 .02 | 1170 1173 jpl 127| 0 0 7 -16 54 12 .60 17 16 | 3996 -125 23 95 | 1 0 1 19 9 21 .03 | 1135 1277 mit 261| 0 0 -3 25 -63 16 -.31 12 10 | -15244 -410 23 136 | 1 1 0 28 23 11 .02 | 739 872 ngs 222| 0 0 -2 29 122 10 -.16 9 7 | -121189 -66306 2601 15154 | 0 0 1 50 57 21 .02 | 235384 421910 sio 264| 0 2 9 -85 -32 -22 -.08 19 17 | --- --- --- --- | 1 1 1 23 25 6 .02 | --- --- Table 1.1562.b GPS week : 1562 MJD: 55178.000-55184.000 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 | 10 10 12 10 15 11 11 | 2 | 5 5 5 4 4 5 5 | 3 | 4 4 4 5 5 5 5 | 4 | 4 4 4 3 4 5 5 | 5 | 4 4 4 4 4 5 4 | 6 | 4 3 4 5 5 5 5 | 7 | 5 4 5 6 5 5 5 | 8 | 6 5 5 5 4 4 4 | 9 | 4 4 4 4 4 4 4 | 10 | 7 5 6 6 5 6 6 | 11 | 4 4 4 5 4 5 4 | 12 | 5 5 5 5 5 4 5 | 13 | 4 4 4 4 5 5 4 | 14 | 4 4 5 4 4 4 5 | 15 | 5 5 5 5 5 5 5 | 16 | 5 5 5 5 5 6 5 | 17 | 6 5 6 6 5 6 6 | 18 | 4 5 4 5 7 4 4 | 19 | 5 5 5 5 5 4 4 | 20 | 4 5 5 6 4 4 4 | 21 | 5 5 5 5 5 5 5 | 22 | 4 4 4 5 4 4 4 | 23 | 5 5 5 5 6 5 5 | 24 | 14 0 11 12 7 18 14 | 25 | 5 4 5 6 5 6 7 | 26 | 3 3 3 3 3 4 4 | 27 | 4 4 4 4 4 4 4 | 28 | 4 4 4 4 4 4 4 | 29 | 5 4 5 5 5 4 5 | 30 | 4 4 4 5 4 5 6 | 31 | 4 4 5 4 4 4 5 | 32 | 6 6 6 9 7 7 7 | 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 2.1562.0 GPS week: 1562 Day: 0 MJD: 55178.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 240| 0 1 1 55 -5 -9 -.14 8 8 | 121 -546 23 72 | 28 -28 | emr 91| 0 -1 7 -45 20 -18 .49 17 17 | 2925 -1444 51 132 | -43 -84 | esa 125| 1 0 -7 -94 -57 27 .27 11 10 | -194 396 24 123 | -20 35 | gfz 198| -1 -3 -4 53 -155 -31 -.17 11 11 | 1038 -2553 42 143 | -45 -47 | grg 110| -2 3 -13 -81 -29 -33 1.07 26 24 | 527 -221 67 229 | 79 -86 | igr n/a| 0 0 -2 74 11 -72 .03 5 5 | 7516 -975 24 78 | -88 -67 | jpl 127| -1 1 8 -28 56 29 .63 16 15 | 5697 -1063 38 115 | -9 -18 | mit 261| -2 -1 -2 17 -86 1 -.33 14 11 | -13796 -1553 28 124 | 4 22 | ngs 222| 1 0 -1 30 202 6 -.16 8 6 | -515247 -932772 1936 3113 | -3 -94 | sio 264| -2 0 11 -96 -60 -14 -.05 19 16 | --- --- --- --- | 14 65 | Table 2.1562.1 GPS week: 1562 Day: 1 MJD: 55179.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 240| 0 1 2 99 -14 -25 -.13 8 8 | -288 62 22 69 | -22 -30 | emr 91| 0 -1 7 -2 41 -9 .46 18 18 | 878 -785 52 133 | -56 -94 | esa 125| 0 0 -2 -89 -57 32 .27 8 8 | -652 993 22 113 | -15 -14 | gfz 198| 0 -1 -1 -47 -90 -9 -.13 11 11 | 120 -1131 41 140 | -22 -48 | grg 110| -2 0 -11 -60 -45 -16 1.08 25 22 | 89 306 66 253 | 85 -46 | igr n/a| 0 0 -1 99 -16 -50 .01 6 6 | 6120 -1062 34 85 | -83 -9 | jpl 127| 0 0 6 -3 60 3 .62 17 15 | 4125 -734 36 113 | 25 -30 | mit 261| -1 0 -3 -18 -64 18 -.33 10 9 | -14766 -1678 26 117 | 3 21 | ngs 222| 0 0 -4 105 200 -16 -.16 10 8 | 16032 -526 1859 3013 | -10 -74 | sio 264| 0 0 10 -111 -28 -30 -.07 18 16 | --- --- --- --- | 9 69 | Table 2.1562.2 GPS week: 1562 Day: 2 MJD: 55180.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 240| 0 0 2 65 -42 0 -.14 9 9 | -998 1354 13 68 | 23 9 | emr 91| 1 -3 4 -50 -21 1 .49 18 18 | -919 465 17 103 | -34 -56 | esa 125| 2 -1 -4 -102 -64 20 .35 10 10 | 226 -687 16 115 | -14 0 | gfz 198| -1 0 -4 -9 -25 -6 -.11 11 11 | -756 2896 30 116 | -20 -21 | grg 110| -3 0 -11 -74 -90 9 1.12 23 20 | -75 11 68 229 | 51 50 | igr n/a| 0 0 -2 44 -65 -54 .06 5 5 | 3815 111 19 63 | -31 -6 | jpl 127| -1 0 8 -51 42 -3 .64 17 16 | 2111 410 20 96 | 13 -65 | mit 261| 0 0 -3 42 -17 7 -.31 9 8 | -15393 -412 17 146 | -13 2 | ngs 222| 0 1 -2 59 123 -7 -.15 9 7 | -410557 478253 5299 83315 | 0 -51 | sio 264| 0 1 10 -83 4 -17 -.07 17 15 | --- --- --- --- | 9 52 | Table 2.1562.3 GPS week: 1562 Day: 3 MJD: 55181.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 240| 0 0 2 96 -40 14 -.13 9 9 | -529 269 14 61 | -17 -58 | emr 91| -1 -2 2 -23 -26 -11 .43 17 17 | 280 2218 18 116 | -42 -36 | esa 125| 1 0 -3 -99 -21 5 .26 10 9 | 326 -808 18 119 | -19 -6 | gfz 198| 0 -1 -1 -28 5 -14 -.18 13 13 | 695 -1508 35 136 | -12 -67 | grg 110| -4 0 -13 -37 -38 16 1.11 24 21 | -131 195 62 224 | 16 -36 | igr n/a| 0 0 -1 78 -33 -62 .08 5 4 | 4549 1874 25 77 | -46 -23 | jpl 127| 0 0 7 6 66 -17 .59 16 15 | 3087 2125 19 96 | -12 -101 | mit 261| 0 0 -3 -4 -81 17 -.31 13 9 | -15479 -115 22 165 | -1 7 | ngs 222| -1 0 -2 61 108 -2 -.15 9 7 | 15958 -2320 2197 3989 | 44 -22 | sio 264| -1 1 8 -112 -59 -26 -.11 19 14 | --- --- --- --- | -9 62 | Table 2.1562.4 GPS week: 1562 Day: 4 MJD: 55182.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 240| -1 1 2 82 -58 -56 -.17 10 10 | -437 -160 15 67 | 38 24 | emr 91| 1 -1 4 -76 -64 16 .41 18 18 | 1311 314 21 107 | 14 5 | esa 125| 1 -1 -2 -99 18 -11 .26 9 9 | -1846 3466 19 106 | -21 -15 | gfz 198| -1 -2 -5 46 7 0 -.11 10 10 | 101 927 34 130 | -18 -4 | grg 110| -1 2 -14 -67 -146 -18 1.14 23 21 | -278 -56 57 207 | 48 89 | igr n/a| 0 0 -1 42 -55 -16 .08 5 5 | 5330 388 21 73 | -11 11 | jpl 127| 0 1 8 -19 41 4 .57 17 16 | 4081 494 16 79 | 14 -48 | mit 261| 0 0 -1 45 -54 35 -.28 11 11 | -15979 150 19 124 | -18 -8 | ngs 222| 0 0 -3 9 64 27 -.17 9 6 | 14314 -1869 2376 4273 | 53 3 | sio 264| 0 4 9 -73 -10 -17 -.10 20 18 | --- --- --- --- | -10 58 | Table 2.1562.5 GPS week: 1562 Day: 5 MJD: 55183.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 240| 0 0 1 66 -54 6 -.19 9 8 | 20 -491 21 72 | 29 -3 | emr 91| 1 -3 4 -74 -57 0 .48 18 18 | 1445 -605 19 95 | 23 6 | esa 125| 0 0 -3 -89 16 -8 .28 9 9 | 1233 -1883 17 107 | -34 -29 | gfz 198| -1 -1 -5 57 44 -26 -.17 9 9 | 54 17 35 145 | 9 -34 | grg 110| -1 -1 -14 -101 -83 0 1.07 23 20 | 294 -213 63 216 | 115 28 | igr n/a| 0 0 -2 18 -31 -2 .04 5 5 | 5434 -402 25 72 | -4 9 | jpl 127| 1 0 8 -10 59 31 .56 18 17 | 4274 -324 17 91 | 31 -48 | mit 261| 0 1 -2 54 -77 10 -.29 13 12 | -15738 509 21 135 | -26 -8 | ngs 222| 0 0 0 -34 65 24 -.12 9 7 | 16937 -5051 2506 4472 | 145 20 | sio 264| 0 3 9 -45 -50 -29 -.08 18 18 | --- --- --- --- | -34 56 | Table 2.1562.6 GPS week: 1562 Day: 6 MJD: 55184.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 240| 0 0 2 77 -50 -23 -.18 9 8 | -354 34 30 92 | 25 -1 | emr 91| 0 -3 1 -51 -27 23 .45 19 19 | 1219 -2004 24 120 | 3 -20 | esa 125| 0 0 -3 -88 -2 -19 .27 8 8 | -123 235 19 111 | -46 -26 | gfz 198| 0 0 -3 38 -11 -25 -.14 11 11 | -112 -65 47 157 | 5 -54 | grg 110| 0 0 -14 -105 -54 -2 1.06 25 22 | 532 -467 58 200 | 111 13 | igr n/a| 0 0 -1 47 -43 -49 .03 5 5 | 5467 -1666 18 68 | -22 -42 | jpl 127| 0 0 5 -6 55 41 .61 17 16 | 4598 -1789 15 78 | 49 33 | mit 261| -1 1 -3 45 -62 21 -.28 13 12 | -15558 228 28 143 | -23 4 | ngs 222| 0 0 0 -24 93 43 -.19 9 8 | 14238 141 2040 3907 | 113 -11 | sio 264| -2 4 8 -76 -23 -20 -.09 21 21 | --- --- --- --- | -9 62 | 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 3.1562.0 GPS week: 1562 Day: 0 MJD: 55178.000 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 | 14 27 --- --- --- 15 --- 18 12 --- 9 | 23 30 --- --- --- 24 --- 25 18 --- 19 2 | 8 17 13 8 34 4 21 13 7 24 5 | 20 34 26 23 44 22 38 21 21 25 23 3 | 7 11 9 10 19 6 11 15 10 20 4 | 30 33 38 34 37 32 36 32 31 25 31 4 | 8 10 10 7 23 2 11 11 5 24 4 | 28 24 31 30 33 27 24 30 30 26 28 5E | 6 19 10 11 23 4 17 10 8 9 4 | 18 25 17 16 32 16 25 21 24 21 18 6 | 6 10 7 9 30 6 11 10 8 17 3 | 30 28 33 31 36 30 33 32 30 27 30 7 | 6 20 9 16 24 5 16 12 5 14 4 | 40 44 39 41 50 39 44 39 40 36 39 8 | 12 22 9 13 17 5 13 23 7 21 5 | 19 29 17 19 22 17 22 31 20 27 20 9 | 7 16 9 8 17 4 13 7 8 16 3 | 19 26 21 17 22 20 26 19 22 24 21 10E | 12 20 13 13 23 5 14 29 9 35 6 | 39 50 49 46 60 44 53 43 42 58 43 11 | 9 19 9 10 24 5 13 10 7 21 4 | 27 38 30 29 46 27 33 28 26 24 26 12 | 7 24 13 11 26 5 19 11 6 16 4 | 15 29 21 14 39 16 26 20 18 22 17 13 | 6 16 10 10 31 7 15 12 7 10 4 | 15 26 18 16 44 18 28 16 21 19 17 14 | 7 17 10 6 26 4 19 9 6 15 4 | 15 23 19 12 31 15 26 17 18 19 17 15 | 8 19 10 13 26 5 21 9 10 18 4 | 14 24 18 16 38 15 27 15 16 17 16 16 | 8 26 11 8 34 6 20 15 12 14 5 | 18 32 19 14 34 15 29 16 21 19 17 17 | 8 14 12 20 22 5 15 8 9 34 5 | 23 23 29 32 30 23 23 22 28 31 25 18E | 5 17 11 12 29 5 19 8 9 12 4 | 24 27 27 22 32 22 33 22 28 26 25 19 | 7 12 10 8 20 4 13 24 12 25 5 | 19 22 27 21 28 19 21 23 20 16 18 20E | 7 17 10 12 23 5 15 13 9 12 4 | 21 30 22 27 30 21 29 26 23 28 22 21 | 12 17 16 8 27 5 17 11 5 22 5 | 21 26 21 18 33 16 29 16 20 18 18 22E | 8 12 12 13 45 4 18 6 9 11 4 | 20 20 20 24 33 18 31 21 24 20 21 23 | 10 23 11 11 24 9 17 15 7 13 5 | 14 31 22 16 34 16 29 21 20 21 18 X24 | 20 26 --- --- --- 44 --- 15 30 --- 13 | 24 34 --- --- --- 46 --- 33 39 --- 30 X25 | 7 19 11 9 --- 5 12 16 8 --- 4 | 40 45 38 29 --- 39 38 37 30 --- 39 26 | 5 11 9 8 20 3 11 9 6 13 3 | 14 23 16 15 23 14 24 16 16 21 16 27 | 6 16 10 10 18 4 12 7 8 16 3 | 13 22 17 14 23 15 21 15 17 19 16 28 | 8 16 9 9 26 3 13 13 7 19 4 | 19 24 17 15 39 15 24 13 18 15 17 29 | 8 12 9 11 22 6 14 25 8 20 5 | 24 24 24 27 28 23 24 31 27 30 26 30 | 7 16 9 8 19 4 15 14 7 18 4 | 25 33 30 28 35 29 32 27 26 35 27 31 | 7 15 9 9 28 5 18 9 10 12 4 | 16 26 19 18 42 16 28 19 19 19 18 32E | 9 26 10 14 28 8 18 12 15 28 6 | 39 39 36 42 31 39 34 34 42 32 36 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 17 11 11 26 5 16 14 8 19 |T 22 29 25 23 34 23 29 24 24 24 23 WRMS | 8 17 10 11 24 5 15 11 6 16 |NE 19 26 21 19 34 20 26 20 23 22 20 MEDI | 7 17 10 10 24 5 15 12 8 17 |MD 20 27 22 21 33 20 28 22 22 24 21 Table 3.1562.1 GPS week: 1562 Day: 1 MJD: 55179.000 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 | 16 28 --- --- --- 23 --- 14 16 --- 10 | 17 31 --- --- --- 34 --- 23 27 --- 18 2 | 9 16 8 10 31 5 17 10 14 22 4 | 16 29 25 24 38 21 31 17 22 19 19 3 | 7 13 5 7 19 8 12 8 9 21 3 | 25 28 27 25 36 26 31 24 25 18 24 4 | 9 9 6 8 27 5 8 8 8 23 3 | 22 19 23 20 25 20 22 25 24 26 21 5E | 7 17 9 11 25 3 18 10 8 7 4 | 12 20 19 17 32 12 23 16 17 16 14 6 | 7 11 7 6 33 8 11 6 7 19 3 | 24 22 20 20 35 24 26 24 24 23 22 7 | 6 18 9 12 23 7 17 10 6 11 4 | 36 40 35 37 50 36 41 36 36 34 35 8 | 12 19 10 10 15 7 15 18 8 17 5 | 20 25 16 19 25 18 22 28 18 24 18 9 | 8 18 10 8 19 7 11 6 10 17 4 | 14 24 18 14 27 14 24 14 20 16 14 10E | 11 20 13 14 37 4 18 14 12 13 5 | 43 51 47 45 59 43 53 45 42 52 44 11 | 8 18 6 9 21 6 15 8 9 21 4 | 19 31 20 19 41 18 31 21 25 20 19 12 | 6 24 8 12 23 5 19 10 6 15 4 | 15 29 21 16 37 16 25 19 18 19 17 13 | 5 21 8 10 31 6 18 8 11 11 4 | 12 28 18 16 45 14 26 11 18 12 12 14 | 9 23 8 6 25 5 20 7 9 15 4 | 17 25 17 15 32 15 26 17 21 17 16 15 | 8 23 11 9 29 5 21 8 10 18 4 | 14 26 17 16 40 12 26 14 19 14 13 16 | 7 24 6 9 35 7 21 10 10 16 4 | 14 31 19 19 34 17 27 16 22 19 16 17 | 7 13 9 14 22 6 16 7 8 33 4 | 15 18 18 19 21 16 20 16 19 24 15 18E | 7 18 9 11 23 6 21 10 11 16 4 | 19 26 23 21 23 21 27 18 28 22 21 19 | 5 15 6 7 22 7 13 18 10 23 4 | 16 20 19 17 27 17 21 20 18 13 14 20E | 7 17 8 25 18 5 16 10 9 15 5 | 22 28 22 31 29 23 30 29 28 27 24 21 | 12 20 10 7 26 7 20 9 8 22 4 | 23 27 18 16 33 18 29 17 23 13 18 22E | 8 13 8 10 32 4 19 8 7 15 4 | 18 21 18 14 24 15 27 16 22 16 17 23 | 8 26 8 13 25 5 18 11 8 11 4 | 14 31 19 16 35 13 26 14 15 14 13 X24 | 6 --- --- --- --- 101 --- --- --- --- 0 | 19 --- --- --- --- 68 --- --- --- --- 23 X25 | 9 15 8 7 --- 5 15 10 8 --- 4 | 34 38 38 27 --- 34 33 32 23 --- 34 26 | 6 13 5 7 19 4 10 8 7 14 3 | 19 22 18 16 23 19 26 18 25 19 19 27 | 7 18 9 8 19 7 9 6 10 16 3 | 9 23 18 12 27 12 19 12 19 14 12 28 | 8 15 7 9 30 6 17 6 7 14 3 | 11 21 14 15 38 15 21 12 15 15 11 29 | 7 14 7 12 21 7 14 15 7 19 4 | 20 23 17 24 23 17 20 21 18 21 17 30 | 6 19 6 10 15 7 16 13 7 16 4 | 28 36 30 28 35 29 38 29 29 33 28 31 | 6 19 6 10 29 5 21 7 11 10 4 | 15 26 18 18 38 17 28 15 18 16 16 32E | 10 27 9 17 21 8 19 14 18 24 6 | 36 36 32 37 29 38 31 33 40 30 33 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 8 11 25 6 16 10 10 18 |T 19 27 22 21 33 22 27 21 23 20 19 WRMS | 8 18 8 11 22 6 15 9 8 16 |NE 15 24 18 17 32 19 24 15 19 17 15 MEDI | 7 18 8 10 23 6 17 10 9 16 |MD 18 26 19 19 33 18 26 18 22 19 18 Table 3.1562.2 GPS week: 1562 Day: 2 MJD: 55180.000 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 | 15 26 --- --- --- 13 --- 18 23 --- 11 | 16 33 --- --- --- 28 --- 24 38 --- 23 2 | 9 16 9 10 32 6 18 8 9 22 4 | 15 27 20 19 36 17 31 14 12 19 16 3 | 10 11 10 9 16 6 12 6 7 21 4 | 22 28 28 32 36 26 32 26 21 19 24 4 | 9 12 8 8 18 6 9 9 9 22 4 | 21 24 24 20 30 23 23 23 22 21 20 5E | 9 19 11 8 19 3 19 8 6 10 4 | 15 29 22 23 32 19 31 17 19 20 18 6 | 9 8 11 8 26 6 12 7 6 18 3 | 20 24 22 28 37 23 26 22 22 20 21 7 | 9 20 12 12 26 4 19 9 6 10 4 | 35 42 37 36 47 35 40 37 36 33 35 8 | 11 17 13 10 16 5 16 14 10 14 4 | 19 27 28 25 29 21 26 26 23 21 20 9 | 8 16 9 9 16 3 12 6 7 15 3 | 10 25 18 14 25 12 24 12 11 14 11 10E | 14 20 13 15 26 5 17 14 11 24 5 | 32 41 35 31 55 32 44 31 29 35 31 11 | 8 19 8 7 20 5 18 10 8 19 4 | 19 34 24 21 40 20 30 23 21 19 20 12 | 8 26 12 9 19 3 20 7 7 13 4 | 14 31 22 14 35 14 26 14 12 17 15 13 | 7 18 10 10 28 5 19 7 8 10 4 | 16 28 22 16 43 14 28 12 14 12 13 14 | 9 20 11 8 24 4 21 8 9 18 4 | 14 24 18 16 31 14 26 14 16 16 13 15 | 7 20 13 9 26 4 20 7 7 17 4 | 14 25 20 15 38 13 23 10 11 14 11 16 | 9 26 9 9 35 6 18 8 6 18 4 | 15 30 19 17 32 15 27 12 16 17 13 17 | 9 14 10 20 21 5 17 7 11 32 5 | 14 20 19 23 23 17 18 17 19 22 14 18E | 8 19 9 9 28 5 21 7 11 13 4 | 27 33 31 28 34 27 36 29 30 35 28 19 | 8 12 5 7 21 5 15 17 9 24 4 | 14 21 20 17 26 15 21 20 14 13 13 20E | 9 20 8 22 16 4 14 8 8 10 4 | 25 32 26 34 31 24 31 29 28 29 26 21 | 12 19 13 6 27 4 19 6 8 22 4 | 18 25 14 12 31 12 27 15 17 14 14 22E | 8 12 11 11 22 5 17 7 9 14 4 | 14 23 21 17 27 16 24 15 15 17 15 23 | 8 24 11 11 23 5 20 12 8 12 4 | 16 32 24 17 33 14 29 13 14 12 13 X24 | 8 20 --- --- --- 20 --- 14 27 --- 10 | 19 27 --- --- --- 26 --- 20 33 --- 20 X25 | 10 14 12 10 --- 3 15 10 8 --- 4 | 36 41 38 32 --- 36 38 37 30 --- 36 26 | 7 10 6 9 18 3 12 7 8 13 3 | 11 22 18 17 23 14 22 15 19 17 14 27 | 8 16 10 9 16 4 13 7 8 15 3 | 7 22 14 14 26 10 19 10 9 12 9 28 | 7 16 11 8 28 6 17 6 6 10 3 | 14 23 21 14 34 16 20 13 16 12 12 29 | 8 11 15 6 22 6 14 11 10 20 4 | 19 21 19 21 22 19 19 24 25 23 21 30 | 8 16 9 9 18 6 16 12 10 14 4 | 24 34 27 20 36 24 35 29 25 29 25 31 | 9 17 10 12 31 4 20 9 9 10 4 | 15 28 17 21 40 16 30 12 16 13 15 32E | 10 23 11 14 16 6 18 13 15 18 5 | 39 35 34 38 30 37 31 38 42 35 35 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 10 11 23 5 17 9 9 17 |T 19 28 23 21 33 20 27 20 21 20 19 WRMS | 9 18 10 11 20 5 16 8 7 15 |NE 15 25 19 17 31 16 24 14 16 15 14 MEDI | 9 17 10 9 22 5 17 8 8 15 |MD 16 27 22 20 32 17 27 17 19 19 16 Table 3.1562.3 GPS week: 1562 Day: 3 MJD: 55181.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- X1M | 16 --- --- --- --- 13 --- 12 11 --- 9 | 24 --- --- --- --- 23 --- 28 29 --- 25 2 | 8 15 7 8 23 4 17 8 7 22 4 | 19 30 21 24 36 21 33 20 23 27 22 3M | 8 11 14 14 19 4 12 11 6 25 4 | 25 29 23 24 39 26 31 27 27 32 25 4 | 8 11 6 8 16 5 7 6 7 19 3 | 22 22 23 19 33 21 18 23 21 20 20 5E | 6 16 8 12 18 5 18 9 9 10 4 | 16 25 16 16 33 17 26 19 17 19 16 6M | 8 10 13 14 28 4 11 13 4 23 4 | 26 24 24 21 37 26 27 30 27 35 25 7M | 12 25 14 15 27 8 18 16 11 21 6 | 60 62 59 61 68 59 60 59 62 55 59 8M | 12 16 6 12 11 5 14 15 10 16 4 | 36 40 36 37 41 35 38 36 38 34 34 9 | 8 17 7 13 14 3 12 7 7 15 3 | 14 24 17 15 25 14 22 13 18 16 14 10E | 12 20 10 19 23 5 15 14 11 22 5 | 40 52 42 46 58 41 50 39 43 51 42 11M | 12 19 9 11 23 4 16 14 8 20 5 | 23 37 25 26 43 25 32 28 32 23 25 12M | 8 23 8 16 23 4 19 11 8 17 5 | 15 28 18 17 38 14 25 15 20 20 15 13 | 7 18 8 10 27 5 17 7 7 11 3 | 15 26 16 17 41 16 25 11 18 15 13 14M | 10 19 9 8 24 3 18 8 6 12 4 | 17 28 21 21 33 20 27 18 25 19 21 15 | 8 21 9 13 23 3 22 7 8 19 4 | 14 27 20 20 37 16 24 12 16 16 14 16 | 7 23 10 11 40 5 17 8 7 20 4 | 12 28 17 14 34 14 25 12 16 19 14 17 | 8 13 8 21 21 6 18 8 10 32 5 | 16 20 17 23 22 14 20 18 16 26 15 18E | 9 17 8 12 25 6 19 10 9 14 4 | 34 39 35 34 43 36 42 32 41 36 36 19M | 11 11 7 9 23 4 13 15 8 24 4 | 18 24 18 18 34 19 24 23 19 16 16 20E | 12 18 9 17 21 7 13 28 8 17 6 | 36 40 34 34 42 31 38 41 31 35 32 21M | 14 14 10 13 27 5 18 9 7 26 5 | 23 26 21 22 34 18 28 20 20 21 19 22E | 9 14 10 18 34 4 19 7 7 12 4 | 30 31 27 30 42 28 36 29 33 26 29 23 | 9 24 8 12 22 4 18 12 9 13 4 | 15 31 18 17 32 16 26 17 20 16 15 X24 | 15 36 --- --- --- 40 --- 15 20 --- 12 | 21 44 --- --- --- 51 --- 25 43 --- 25 X25M | 16 18 13 11 --- 8 16 16 12 --- 6 | 55 55 55 49 --- 55 45 52 41 --- 54 26M | 8 10 7 8 21 3 10 6 7 12 3 | 16 22 18 19 27 19 24 19 21 22 20 27 | 8 18 5 14 13 2 11 8 8 14 4 | 8 21 14 18 23 11 17 10 16 14 11 28 | 10 18 10 8 31 3 18 5 7 12 4 | 15 25 15 13 39 13 23 14 16 15 14 29 | 5 12 14 10 22 5 16 12 7 22 4 | 21 25 22 22 28 20 24 22 26 23 21 30 | 7 19 8 9 16 4 16 9 9 23 4 | 43 52 46 43 51 46 52 49 51 52 47 31 | 7 16 8 9 29 5 16 9 9 10 4 | 14 28 17 19 42 18 29 16 23 17 18 32E | 14 24 18 13 17 7 16 37 25 20 8 | 48 46 41 44 39 45 43 56 55 44 44 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 17 10 13 24 5 16 13 9 19 |T 24 32 25 26 37 25 31 26 28 26 25 WRMS | 9 17 9 13 21 4 15 9 7 14 |NE 15 27 18 18 32 18 23 16 20 18 16 MEDI | 8 18 8 12 23 5 16 9 8 19 |MD 21 28 21 21 37 20 27 22 23 22 21 Table 3.1562.4 GPS week: 1562 Day: 4 MJD: 55182.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 12 58 --- --- --- 24 --- 17 15 --- 14 | 17 57 --- --- --- 30 --- 16 28 --- 20 2 | 9 15 8 9 25 5 17 10 7 22 4 | 16 29 25 21 36 20 31 18 20 25 21 3 | 10 11 10 9 20 4 12 15 8 26 4 | 21 26 26 22 41 25 30 25 27 20 23 4 | 10 9 9 6 15 6 10 13 7 19 3 | 23 22 29 24 32 23 19 25 26 17 23 5E | 7 19 8 8 22 4 17 8 6 11 3 | 14 26 18 16 28 15 25 16 16 17 15 6 | 9 13 12 11 31 5 11 16 6 24 4 | 18 21 20 21 43 22 24 24 24 21 20 7 | 16 19 12 13 26 4 20 10 10 13 5 | 39 45 42 41 52 39 43 38 38 33 37 8 | 12 17 8 10 16 6 14 12 6 15 4 | 28 32 28 30 31 28 29 37 28 32 29 9 | 9 15 8 10 12 4 13 10 8 17 4 | 13 23 17 14 26 12 21 13 13 13 13 10E | 14 18 8 13 24 6 16 13 8 13 4 | 29 35 36 30 51 32 41 28 27 36 30 11 | 9 19 5 6 19 5 15 13 6 22 4 | 23 35 26 23 44 25 32 28 26 25 24 12 | 9 24 6 9 22 5 20 10 8 16 4 | 16 31 24 18 36 18 28 16 19 18 19 13 | 5 20 10 10 26 5 20 13 9 13 4 | 16 28 20 15 40 17 27 13 17 11 14 14 | 10 20 8 8 25 5 17 6 8 16 4 | 15 25 19 17 33 13 22 13 14 15 14 15 | 6 25 7 8 26 4 21 11 8 19 4 | 17 30 21 13 39 15 24 16 13 19 14 16 | 11 26 10 10 34 3 18 12 8 22 5 | 15 31 19 15 32 15 25 13 11 20 14 17 | 10 15 6 13 21 5 18 8 8 33 5 | 14 19 16 17 23 13 19 17 14 22 14 18E | 14 23 10 17 25 5 23 12 11 38 6 | 74 72 69 71 72 67 72 67 66 79 69 19 | 9 14 9 7 25 4 14 15 9 25 4 | 16 22 18 16 33 15 21 21 17 17 15 20E | 7 18 7 11 16 4 14 8 7 14 3 | 27 35 24 26 32 26 31 30 30 29 26 21 | 14 17 10 9 26 4 21 10 11 28 5 | 20 25 18 18 30 15 28 15 16 18 13 22E | 8 13 7 10 22 4 21 7 9 14 4 | 26 24 24 23 31 20 30 20 23 20 22 23 | 8 22 11 14 22 4 20 18 9 17 5 | 17 30 22 17 35 16 28 18 18 13 15 X24 | 9 20 --- --- --- 27 --- 9 9 --- 6 | 23 36 --- --- --- 41 --- 24 34 --- 26 X25 | 14 14 13 10 --- 3 14 13 8 --- 5 | 39 44 48 39 --- 40 37 40 28 --- 39 26 | 9 12 6 8 18 3 9 9 5 13 3 | 15 20 16 16 24 13 21 17 16 15 15 27 | 9 18 8 10 12 3 12 10 9 17 4 | 11 24 14 15 27 11 19 14 12 15 11 28 | 10 17 9 7 25 4 17 6 5 12 3 | 14 24 20 13 36 13 22 16 15 19 14 29 | 7 14 12 8 23 7 17 12 5 23 4 | 19 27 28 27 24 23 25 21 22 24 22 30 | 7 17 6 9 18 5 17 13 7 16 4 | 26 34 28 28 34 26 35 23 26 26 26 31 | 8 16 12 8 28 5 20 9 7 12 4 | 14 25 16 17 38 15 26 12 12 11 13 32E | 20 27 10 16 27 8 17 15 19 17 6 | 52 58 53 56 51 54 51 48 53 49 51 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 9 10 23 5 17 11 9 20 |T 22 31 26 23 36 23 29 23 23 23 22 WRMS | 10 18 9 10 21 5 16 11 6 18 |NE 16 26 20 17 32 18 23 16 17 17 16 MEDI | 9 17 8 9 23 5 17 11 8 17 |MD 17 28 22 18 34 20 27 18 20 20 20 Table 3.1562.5 GPS week: 1562 Day: 5 MJD: 55183.000 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 | 16 25 --- --- --- 21 --- 18 20 --- 11 | 24 38 --- --- --- 30 --- 23 26 --- 23 2 | 8 14 9 8 28 5 17 12 11 23 4 | 15 27 25 20 36 19 28 19 17 26 19 3 | 7 12 11 9 31 5 13 20 7 26 5 | 22 27 23 19 38 23 31 26 22 26 22 4 | 10 14 10 7 19 4 10 18 10 22 4 | 22 24 24 26 28 24 18 27 24 17 22 5E | 8 19 10 10 32 5 18 13 10 10 4 | 16 29 22 20 43 17 27 25 19 24 19 6 | 7 13 10 8 32 6 14 21 9 24 5 | 16 20 16 13 34 15 23 23 16 21 15 7 | 8 24 11 10 24 6 20 11 9 13 4 | 48 52 45 47 52 46 48 48 49 43 46 8 | 10 19 8 10 14 7 15 11 9 13 4 | 30 40 32 33 36 29 34 34 29 32 31 9 | 8 18 6 6 12 2 14 10 9 14 3 | 15 26 17 11 28 14 22 14 15 16 14 10E | 14 16 12 15 25 5 20 17 10 15 5 | 43 50 48 46 64 45 51 44 44 49 45 11 | 7 16 6 7 21 3 17 13 13 20 4 | 18 34 24 19 40 21 29 22 25 22 20 12 | 7 23 8 7 22 4 19 12 5 14 4 | 13 29 21 14 37 15 23 16 14 17 15 13 | 6 20 9 7 27 5 21 12 10 13 4 | 16 31 20 16 44 17 28 18 16 16 16 14 | 9 19 8 5 27 5 17 8 6 14 4 | 12 21 20 14 33 13 21 15 13 17 14 15 | 9 22 8 8 24 6 20 13 13 18 5 | 17 28 24 17 41 16 25 19 20 20 17 16 | 11 23 14 9 35 7 22 15 6 24 5 | 14 31 19 14 31 13 27 13 14 18 13 17 | 9 17 11 18 20 4 21 11 9 30 5 | 17 22 19 20 20 14 20 18 14 20 14 18E | 7 16 9 10 15 5 20 7 6 18 4 | 59 61 61 58 63 61 63 57 56 61 58 19 | 7 12 8 6 22 4 16 9 6 25 4 | 13 20 17 13 28 13 22 13 14 12 13 20E | 7 18 9 10 14 5 17 12 7 10 4 | 25 35 27 28 33 27 33 31 29 30 27 21 | 12 15 9 8 25 6 20 11 9 26 5 | 17 25 16 14 32 13 27 17 18 16 14 22E | 7 14 8 8 20 5 20 9 5 12 3 | 18 27 23 19 29 20 26 21 19 25 21 23 | 5 26 10 9 --- 4 23 16 9 17 5 | 15 34 21 16 --- 17 30 18 16 16 16 X24 | 18 48 --- --- --- 19 --- 16 38 --- 17 | 23 60 --- --- --- 30 --- 24 39 --- 25 X25 | 9 17 11 11 --- 6 --- 12 --- --- 5 | 47 48 47 43 --- 47 --- 44 --- --- 45 26 | 9 11 8 6 16 4 10 11 7 11 3 | 15 22 23 16 27 18 24 20 18 16 17 27 | 7 17 6 6 13 3 13 11 8 15 3 | 10 24 13 11 26 10 19 15 15 17 11 28 | 7 15 8 6 27 3 19 9 12 10 4 | 12 25 15 12 36 12 21 17 14 18 13 29 | 6 12 9 9 20 5 16 9 5 24 4 | 18 24 22 25 22 19 22 21 18 24 21 30 | 15 16 10 8 21 5 18 13 8 15 4 | 47 59 54 52 62 52 56 51 53 53 52 31 | 6 17 9 9 31 4 20 10 5 13 4 | 13 27 20 16 39 15 25 16 15 16 15 32E | 12 26 16 15 17 7 20 27 18 17 7 | 49 51 43 50 41 47 48 55 55 48 47 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 9 9 23 5 18 13 9 18 |T 23 33 26 24 37 24 30 25 24 25 23 WRMS | 8 18 9 9 20 5 17 12 7 18 |NE 15 29 19 17 31 16 23 18 18 18 16 MEDI | 8 17 9 8 22 5 18 12 9 15 |MD 17 28 22 19 36 18 27 21 18 20 19 Table 3.1562.6 GPS week: 1562 Day: 6 MJD: 55184.000 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 | 11 28 --- --- --- 19 --- 20 20 --- 11 | 19 32 --- --- --- 27 --- 26 18 --- 18 2 | 8 17 8 8 29 5 18 11 10 22 4 | 17 30 26 21 38 21 32 19 21 27 21 3 | 7 11 10 7 26 5 11 23 8 27 5 | 25 33 34 29 44 29 34 30 26 28 28 4 | 9 13 7 9 23 7 10 22 12 25 5 | 29 28 31 33 37 30 26 37 29 21 28 5E | 7 17 5 9 15 3 18 13 8 17 4 | 20 30 27 22 32 22 27 24 22 31 23 6 | 6 12 6 4 29 4 12 20 8 25 4 | 24 26 27 26 39 26 28 31 26 26 25 7 | 7 26 9 15 22 5 19 11 8 19 5 | 45 50 46 46 47 44 48 44 43 39 44 8 | 8 15 9 12 16 5 13 13 8 17 4 | 26 34 31 35 37 30 31 30 30 27 27 9 | 8 14 6 8 15 5 12 12 7 19 3 | 21 25 22 21 29 20 25 22 18 21 18 10E | 15 18 11 17 31 4 14 16 9 25 5 | 42 48 44 47 51 43 50 43 45 52 42 11 | 7 16 6 10 22 4 15 11 10 24 4 | 28 37 34 30 48 29 35 33 30 28 29 12 | 8 24 9 8 27 6 22 15 9 14 5 | 16 34 21 17 38 18 31 22 20 21 19 13 | 4 21 8 10 26 5 17 11 10 17 4 | 19 31 25 22 45 22 28 17 19 18 20 14 | 8 22 8 8 26 4 18 11 8 18 4 | 18 29 22 17 36 16 26 20 20 22 19 15 | 7 23 7 14 25 5 22 12 9 24 5 | 19 27 22 16 38 17 26 19 20 23 17 16 | 7 29 7 11 40 3 16 13 10 22 5 | 22 37 23 16 34 19 29 18 19 21 20 17 | 8 16 8 17 23 8 19 10 11 33 5 | 24 24 23 23 28 20 22 22 22 26 20 18E | 7 19 7 8 20 5 21 7 7 16 4 | 48 48 47 49 44 47 47 45 48 50 46 19 | 5 12 11 7 22 5 15 8 8 27 4 | 18 26 26 20 29 19 25 19 20 19 19 20E | 5 20 8 15 21 6 15 10 7 17 4 | 25 31 27 26 31 24 27 29 26 31 25 21 | 8 17 6 9 27 6 18 13 4 27 4 | 19 27 20 18 35 16 31 17 18 20 18 22E | 8 14 7 10 26 5 20 10 8 13 4 | 25 26 21 26 28 22 29 27 29 28 23 23 | 6 25 11 8 --- 5 18 11 8 18 4 | 20 32 26 19 --- 21 28 19 22 19 20 X24 | 9 28 --- --- --- 25 --- 27 30 --- 13 | 31 48 --- --- --- 39 --- 34 51 --- 34 X25 | 9 13 15 --- --- 9 --- 13 --- --- 7 | 44 48 49 --- --- 44 --- 43 --- --- 45 26 | 11 11 7 7 20 5 12 12 9 13 4 | 19 24 20 19 23 17 25 24 25 20 20 27 | 7 15 8 9 20 4 13 12 9 18 4 | 12 21 14 14 28 11 19 15 15 17 12 28 | 7 14 8 11 27 6 14 9 10 11 3 | 18 27 19 17 37 17 23 19 18 21 17 29 | 5 12 8 10 20 4 16 13 13 23 4 | 25 25 26 29 30 25 28 25 31 27 26 30E | 19 23 12 13 23 10 22 10 9 21 6 | 37 44 42 39 45 36 47 34 37 41 39 31 | 5 20 10 8 31 4 20 13 12 15 4 | 15 29 19 16 39 14 30 16 21 19 18 32E | 16 27 8 19 22 8 20 17 17 17 6 | 66 61 62 63 59 59 57 55 63 60 62 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 8 11 25 5 17 13 9 21 |T 26 33 29 26 37 26 31 27 27 27 26 WRMS | 8 19 8 11 22 5 16 12 8 21 |NE 20 29 23 20 34 21 26 21 23 21 20 MEDI | 7 17 8 9 23 5 17 12 9 19 |MD 22 30 26 22 37 22 28 24 22 26 21 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 4.1562 GPS week: 1562 MJD: 55178.0-55184.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3052 |U 6 6 20 |U 11 12 37 |U 10 11 19 | emr | emr 3019 | 15 9 31 |U 12 11 37 | 10 11 22 | esa | esa 2880 | 7 7 21 |U 10 11 36 | 10 11 19 | gfz | gfz 2813 |U 16 13 36 |U 13 16 48 | 14 14 32 | grg | grg 2756 | 9 11 29 |U 11 12 37 | 13 15 26 | igr | igr 2925 | 13 15 31 | 11 13 40 | 11 11 25 | igs | igs 2923 | 11 8 24 | 11 12 41 | 10 11 21 | jpl | jpl 2842 | 12 8 31 |U 10 12 35 |U 10 10 19 | mit | mit 3058 |U 17 12 40 |U 11 12 38 |U 11 11 22 | 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 5.1562.0 GPS week: 1562 Day: 0 MJD: 55178.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3046 | 7 9 26 | 10 13 37 | 9 14 17 | emr | emr 3048 | 9 7 21 | 12 12 38 | 10 14 22 | esa | esa 2880 | 6 8 23 | 10 12 32 | 10 15 16 | gfz | gfz 2828 | 20 17 52 | 13 18 37 | 12 19 27 | grg | grg 2784 | 13 25 38 | 11 12 34 | 12 14 25 | igr | igr 2923 | 19 21 41 | 11 15 44 | 11 18 26 | igs | igs 2910 | 11 9 27 | 13 13 48 | 11 14 22 | jpl | jpl 2868 | 14 8 38 | 11 11 34 | 11 15 15 | mit | mit 3072 | 13 10 34 | 10 11 34 | 9 12 19 | Table 5.1562.1 GPS week: 1562 Day: 1 MJD: 55179.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3054 | 7 6 17 | 12 13 40 | 9 11 20 | emr | emr 2966 | 19 8 33 | 16 13 43 | 10 8 21 | esa | esa 2880 | 8 9 18 | 12 12 38 | 10 11 21 | gfz | gfz 2823 | 24 12 51 | 15 19 46 | 13 19 38 | grg | grg 2784 | 8 7 26 | 11 13 35 | 12 15 24 | igr | igr 2852 | 8 6 19 | 12 14 39 | 8 9 24 | igs | igs 2867 | 22 12 33 | 12 15 45 | 10 11 25 | jpl | jpl 2870 | 19 9 37 | 12 12 45 | 9 11 21 | mit | mit 2976 | 19 11 29 | 12 13 45 | 11 12 21 | Table 5.1562.2 GPS week: 1562 Day: 2 MJD: 55180.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3058 | 7 6 25 | 14 15 45 | 9 11 21 | emr | emr 3045 | 17 6 51 | 15 16 43 | 11 11 20 | esa | esa 2880 | 7 8 29 | 13 14 44 | 11 12 17 | gfz | gfz 2827 | 18 9 35 | 15 20 48 | 14 16 29 | grg | grg 2784 | 8 9 34 | 15 17 42 | 15 19 28 | igr | igr 2960 | 12 10 37 | 14 14 43 | 9 8 16 | igs | igs 3008 | 15 6 35 | 15 15 59 | 9 9 19 | jpl | jpl 2872 | 9 8 43 | 14 15 43 | 10 9 18 | mit | mit 3072 | 17 9 31 | 14 15 48 | 11 13 22 | Table 5.1562.3 GPS week: 1562 Day: 3 MJD: 55181.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3062 | 5 7 20 | 15 13 53 | 8 7 15 | emr | emr 2947 | 8 6 24 | 15 11 43 | 9 8 19 | esa | esa 2880 | 7 8 21 | 12 13 46 | 9 9 17 | gfz | gfz 2829 | 19 14 36 | 14 14 56 | 11 9 25 | grg | grg 2784 | 8 7 24 | ---- ---- ---- | 11 14 19 | igr | igr 2845 | 13 12 33 | 13 16 55 | 12 13 30 | igs | igs 2917 | 7 6 18 | 13 12 46 | 7 7 16 | jpl | jpl 2867 | 11 8 25 | 12 13 41 | 7 6 16 | mit | mit 3072 | 15 9 35 | 12 14 48 | 9 9 20 | Table 5.1562.4 GPS week: 1562 Day: 4 MJD: 55182.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3055 | 6 5 14 | 9 11 36 | 9 7 15 | emr | emr 3044 | 33 24 22 | 10 12 35 | 11 10 22 | esa | esa 2880 | 7 8 14 | 9 11 37 | 10 9 19 | gfz | gfz 2835 | 8 18 20 | 13 13 50 | 15 12 33 | grg | grg 2784 | 8 10 23 | 12 11 35 | 13 14 26 | igr | igr 2916 | 19 27 22 | 9 12 44 | 13 10 29 | igs | igs 2827 | 9 12 14 | 9 10 38 | 9 9 19 | jpl | jpl 2869 | 13 10 19 | 9 12 35 | 9 9 17 | mit | mit 3072 | 29 25 16 | 9 9 40 | 11 11 24 | Table 5.1562.5 GPS week: 1562 Day: 5 MJD: 55183.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3047 | 5 8 15 | 6 5 20 | 13 12 22 | emr | emr 3041 | 9 8 30 | 8 6 26 | 12 16 30 | esa | esa 2880 | 6 7 18 | 6 6 22 | 11 11 21 | gfz | gfz 2829 | 8 9 22 | 11 12 53 | 15 11 27 | grg | grg 2688 | 8 10 26 | 7 7 29 | 13 15 27 | igr | igr 3042 | 12 22 32 | 7 11 25 | 14 12 30 | igs | igs 2921 | 6 9 18 | 5 7 20 | 11 13 26 | jpl | jpl 2774 | 8 8 29 | 6 6 22 | 12 14 23 | mit | mit 3072 | 12 13 76 | 6 9 24 | 13 13 27 | Table 5.1562.6 GPS week: 1562 Day: 6 MJD: 55184.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3042 | 7 5 24 | 10 12 31 | 13 15 25 | emr | emr 3048 | 10 6 37 | 9 11 31 | 11 11 21 | esa | esa 2880 | 8 5 22 | 9 11 30 | 12 12 22 | gfz | gfz 2725 | 14 13 37 | 11 16 48 | 17 15 43 | grg | grg 2688 | 9 9 33 | 12 12 45 | 16 12 32 | igr | igr 2938 | 7 6 31 | 9 13 32 | 10 11 20 | igs | igs 3013 | 7 4 23 | 9 11 32 | 11 11 20 | jpl | jpl 2774 | 10 7 29 | 9 12 27 | 11 10 20 | mit | mit 3072 | 15 6 59 | 10 12 32 | 10 9 21 | 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 6.1562 GPS week: 1562 MJD: 55178.500-55184.500 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 | -4 -14 -27 83 -2 | 0 17 | 22 23 94 63 5 | 2 emr uuuuu | 24 20 -214 21 -5 | 44 47 | 33 21 67 60 8 | 3 esa uuuuu | -8 25 129 -32 11 | -6 24 | 28 24 152 142 14 | 6 gfz uuuuu | 23 15 77 50 -2 | -16 25 | 18 8 62 90 13 | 4 grg --xxx | -- -- 178 65 8 | 10 19 | -- -- 99 98 21 | 2 igr xxxxx | 2 41 70 34 8 | -4 17 | 25 24 61 43 2 | 3 irf xxxxx | -16 1 2 3 0 | -4 17 | 8 14 47 30 2 | 3 jpl uuuuu | 23 -15 -40 172 13 | 17 26 | 41 17 83 49 8 | 4 mit uuuuu | -22 11 -165 27 -6 | 0 18 | 20 25 135 112 3 | 3 ngs uuuuu | 16 -48 18 -46 1 | -10 16 | 35 47 80 96 6 | 1 sio uuuuu | -77 5 107 -204 -10 | 18 25 | 12 30 103 122 2 | 3 Table 7.1562.0 GPS week: 1562 Day: 0 MJD: 55178.500 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 -42 -22 -40 -9 | 3 19 emr uuuuu | 59 29 -214 71 -18 | 47 50 esa uuuuu | -60 6 -150 -180 30 | -15 27 gfz uuuuu | 22 31 64 -8 -21 | -10 21 grg --xxx | -- -- 207 9 28 | 10 23 igr xxxxx | 42 74 15 72 10 | -9 19 irf xxxxx | -25 -14 -25 42 3 | -7 19 jpl uuuuu | -7 -5 111 149 11 | 12 21 mit uuuuu | -47 -18 -104 224 -6 | -3 21 ngs uuuuu | 69 -11 103 -115 4 | -8 15 sio uuuuu | -90 -28 184 -30 -7 | 16 26 Table 7.1562.1 GPS week: 1562 Day: 1 MJD: 55179.500 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 13 173 99 -8 | 0 19 emr uuuuu | 70 47 -311 52 -14 | 45 49 esa uuuuu | -10 6 28 -170 23 | -13 26 gfz uuuuu | 24 13 121 23 -13 | -13 25 grg --xxx | -- -- 242 112 -24 | 13 24 igr xxxxx | -15 74 -30 51 5 | -8 19 irf xxxxx | -24 -9 57 -12 2 | -7 19 jpl uuuuu | 6 -34 -157 153 21 | 12 21 mit uuuuu | -45 -12 16 118 -4 | -3 21 ngs uuuuu | 50 1 -39 -13 -9 | -10 16 sio uuuuu | -93 -18 236 -92 -8 | 16 26 Table 7.1562.2 GPS week: 1562 Day: 2 MJD: 55180.500 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 | -29 -32 -24 94 1 | 0 18 emr uuuuu | 36 25 -212 41 -7 | 45 49 esa uuuuu | -20 5 189 -170 20 | -7 25 gfz uuuuu | 1 11 116 -8 -7 | -14 25 grg --xxx | -- -- 181 -38 -16 | 12 24 igr xxxxx | -14 22 125 -52 9 | -5 18 irf xxxxx | -20 -9 52 -41 0 | -3 17 jpl uuuuu | 45 -22 -82 178 25 | 15 25 mit uuuuu | -22 4 -73 5 -8 | 1 18 ngs uuuuu | 31 -9 -103 106 -3 | -10 16 sio uuuuu | -72 -18 180 -174 -13 | 19 26 Table 7.1562.3 GPS week: 1562 Day: 3 MJD: 55181.500 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 | 36 15 -79 117 -3 | 1 17 emr uuuuu | 14 40 -236 28 -3 | 44 49 esa uuuuu | -16 17 250 26 1 | -1 23 gfz uuuuu | 45 10 37 194 0 | -16 26 grg --xxx | -- -- 64 252 8 | 6 15 igr xxxxx | 1 44 67 40 8 | -2 17 irf xxxxx | -22 -2 32 27 -1 | -1 16 jpl uuuuu | 79 10 -80 196 8 | 18 28 mit uuuuu | -29 -1 -122 6 -7 | 2 17 ngs uuuuu | 0 -46 -26 -180 8 | -11 16 sio uuuuu | -84 7 54 -199 -12 | 20 26 Table 7.1562.4 GPS week: 1562 Day: 4 MJD: 55182.500 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 | -28 -35 -121 165 6 | 0 17 emr uuuuu | -9 -11 -92 81 4 | 42 46 esa uuuuu | 11 24 180 92 -10 | -1 23 gfz uuuuu | 0 21 2 -14 13 | -19 26 grg --xxx | -- -- 44 27 21 | 9 15 igr xxxxx | -15 14 64 14 8 | -1 17 irf xxxxx | -4 3 7 5 -1 | -1 16 jpl uuuuu | 44 -11 -24 91 17 | 19 29 mit uuuuu | 4 21 -203 -64 -3 | 2 17 ngs uuuuu | -7 -50 6 21 0 | -11 16 sio uuuuu | -62 13 121 -345 -9 | 20 26 Table 7.1562.5 GPS week: 1562 Day: 5 MJD: 55183.500 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 | -5 -6 -64 74 4 | 2 16 emr uuuuu | -14 0 -187 -79 1 | 44 48 esa uuuuu | 21 57 298 171 6 | 0 22 gfz uuuuu | 26 14 22 -5 7 | -17 24 grg --xxx | -- -- 177 -2 9 | 13 18 igr xxxxx | -17 27 137 43 7 | 1 17 irf xxxxx | -8 23 -50 23 -3 | 0 15 jpl uuuuu | 40 -8 -35 188 5 | 22 31 mit uuuuu | 0 49 -371 10 -11 | 2 17 ngs uuuuu | -28 -122 105 -108 5 | -9 13 sio uuuuu | -64 57 -55 -228 -12 | 20 26 Table 7.1562.6 GPS week: 1562 Day: 6 MJD: 55184.500 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 | -10 -12 -53 69 -1 | -3 13 emr uuuuu | 9 10 -249 -46 1 | 38 40 esa uuuuu | 15 59 108 3 6 | -4 22 gfz uuuuu | 43 8 173 166 9 | -22 26 grg --xxx | -- -- 330 91 28 | 11 17 igr xxxxx | 31 35 109 69 8 | -4 15 irf xxxxx | -11 13 -59 -26 2 | -6 13 jpl uuuuu | -44 -36 -12 251 7 | 18 28 mit uuuuu | -15 36 -302 -111 -5 | -5 14 ngs uuuuu | 0 -100 79 -35 3 | -13 15 sio uuuuu | -73 22 26 -361 -10 | 12 19