Date: Thu, 07 Jan 2010 13:37:57 +0000 From: Jim Ray Subject: [IGSREPORT-18164] Wk 1563 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4b45e3b5.qtgzs06ncjB2nQgo%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 07 Jan 05:38:21 PST 2010 Message Number 18164 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1563 (Dec 20, 2009 - Dec 26, 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: igs1563[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1563[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1563[0-6].cls IGS GPS clock combination summary report. igs15637.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15637.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 | ALL | 1 0 | COD | 32 0 | EMR | WTZR WTZR 0 | ESA | 25 32 UNSA 0 | GFZ | 10 18 30 32 ALGO ALIC AREQ AUCK CHPI CHUR COCO CRO1 0 | GFZ | DAEJ DAV1 FAA1 FLIN GUAT HARB MAC1 MCM4 NRC1 NRMD 0 | GFZ | PIMO PRDS RIOP SFER SHAO STJO TIXI TSKB YAKT YELL 0 | GFZ | YKRO YSSK 0 | GRG | ONSA 0 | JPL | 10 32 DGAR GUAT 0 | MIT | 10 25 30 10 25 32 HARB 1 | COD | 30 32 30 1 | EMR | WTZR 1 | ESA | 10 30 32 FAA1 1 | GFZ | 6 16 ALGO ALRT ASPA BOR1 BRUS COCO DAEJ EIL1 GUAT 1 | GFZ | HOLM HRM1 KARR KIRU MDO1 MIZU NRMD PERT SANT TIXI 1 | GFZ | WHIT WSRT YAKT 1 | GRG | ONSA 1 | JPL | 32 DGAR 2 | ALL | 1 1 2 | COD | 30 32 30 32 HARB 2 | EMR | HARB WTZR WTZR 2 | ESA | 30 32 UNSA 2 | GFZ | 6 18 ALGO ALIC AREQ ARTU BOR1 BRUS CEDU DAV1 DGAR 2 | GFZ | FAIR GRAZ HRAO HRM1 HYDE KARR PERT PETP PRE1 SANT 2 | GFZ | STJO SYOG TIXI VILL WHIT YELL YKRO 2 | GRG | ONSA 2 | JPL | 32 DGAR 2 | MIT | 25 25 HARB IRKT TOW2 3 | ALL | 1 1 3 | COD | 30 32 32 GUAT 3 | EMR | HARB WTZR 3 | ESA | 32 BAN2 UNSA 3 | GFZ | 7 8 19 22 ALIC AREQ ASPA BAKO BOGT CAS1 CEDU CHPI 3 | GFZ | COCO CONZ DARW DGAR FAA1 GLPS GUAT HOLM KARR KOUR 3 | GFZ | LPGS MDO1 MIZU NRMD PERT PRE1 RIOP SANT SFER TIDB 3 | GFZ | WHIT YAR2 YSSK 3 | GRG | ONSA 3 | JPL | 30 32 3 | MIT | 25 21 25 30 KHAJ 4 | ALL | 1 1 4 | COD | 30 32 32 HARB 4 | EMR | HARB 4 | ESA | 32 FAA1 4 | GFZ | 4 7 16 22 31 ALGO ALRT BOR1 BRUS CEDU CHUR COCO CONZ 4 | GFZ | CRO1 DGAR GLPS GRAZ GUAT HARB HRAO HYDE KARR KOUR 4 | GFZ | MAC1 MCM4 MDO1 METS NRC1 PRE1 RIOP SANT SSIA SUTH 4 | GFZ | SUTM SYOG TOW2 UNSA VESL WSRT YAKT YKRO 4 | GRG | ONSA 4 | JPL | 30 32 DGAR 4 | MIT | 30 HARB 5 | ALL | 1 5 | COD | 30 32 30 32 HARB 5 | EMR | HARB WTZR WTZR 5 | ESA | 21 32 UNSA 5 | GFZ | 5 16 ALGO ALIC AMC2 AREQ BJFS CHPI CHUR DGAR FAA1 5 | GFZ | GODE GUAM HARB HOLM HRAO HYDE IRKT ISPA MAL2 NRIL 5 | GFZ | PERT QAQ1 SANT SHAO STJO SUTH SUTM SYOG YAKT YAR2 5 | GRG | ONSA 5 | JPL | 30 32 DGAR GUAT 5 | MIT | 21 25 GUAT HARB 6 | COD | HARB SUTH 6 | EMR | HARB 6 | GFZ | 16 30 32 ALGO AREQ BJFS BOGT BOR1 BRFT BUE1 CHPI 6 | GFZ | CONZ DAEJ DGAR EIL1 FAA1 HARB HOB2 HOLM KARR KERG 6 | GFZ | KIRU KOUR MAL2 MCM4 MDO1 NRMD PETP PRE1 RESO REUN 6 | GFZ | RIOP SANT SHAO SSIA THU3 TSKB UNSA WTZR YAKT YKRO 6 | GRG | ALGO ONSA 6 | JPL | 30 32 DGAR 6 | MIT | 25 30 25 30 HARB KHAJ 6 | NGS | 1 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 ----+--------+--------+------------- 5 | GFZ | ~20:50 | ~ 1.65 ns 6. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G10 | 2 | | | | | | | PRN G32 | 2 | | | | | | | 7. 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. 8. 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 | .0 1.1 .4 -18 -3 -23 -.02 EMR | 8.4 -.5 2.0 35 1 12 .39 ESA | 7.9 4.5 -8.1 96 -56 75 .19 GFZ | .1 1.3 .7 24 -13 -9 -.07 GRG | 3.4 5.1 -3.8 15 37 -11 .72 JPL | 7.2 1.7 18.6 -14 -18 -66 .29 MIT | 3.0 .0 -11.1 0 3 -29 .06 NGS | 8.6 -1.8 -8.4 -29 -141 -3 .01 SIO | 5.7 .3 6.8 -4 -58 -15 .35 9. 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. 10. 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. 11. 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 1.1563.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1563.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 2.1563.[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 3.1563.[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 5.1563.0-6). 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 1563 summary. (Dec 20, 2009 - Dec 26, 2009) Table 1.1563.a GPS week: 1563 MJD: 55185.000-55191.000 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 239| 0 0 2 45 -56 -8 -.14 9 8 | -502 46 17 65 | 0 0 1 12 8 34 .02 | 522 813 emr 91| 1 -1 4 -58 -74 -8 .47 18 18 | -943 671 17 97 | 2 1 1 22 18 34 .03 | 1834 1059 esa 126| 1 0 -2 -143 21 14 .29 8 8 | -1224 1275 18 110 | 0 0 1 15 10 31 .02 | 883 1449 gfz 195| 0 0 -8 -33 -39 7 -.13 12 12 | 158 -717 33 140 | 1 1 1 29 49 18 .03 | 630 2319 grg 109| 0 0 -7 -63 -204 -17 1.10 26 22 | -33 -167 59 250 | 0 1 2 23 29 22 .04 | 294 566 igr n/a| 0 0 -2 13 -53 -29 .05 5 5 | 3774 585 19 68 | 0 0 0 14 23 10 .04 | 1824 997 jpl 114| 0 0 11 32 -29 0 .55 17 16 | 2341 504 18 85 | 1 1 2 10 17 26 .02 | 1446 812 mit 259| -1 0 -3 42 -83 0 -.32 10 8 | -15239 -42 22 144 | 0 0 0 16 10 10 .02 | 935 1997 ngs 213| 0 0 -2 97 206 -12 -.17 10 8 | 12821 2654 2150 3920 | 0 0 1 10 22 13 .02 | 3560 4035 sio 256| 0 1 12 25 22 -11 -.06 20 17 | --- --- --- --- | 1 0 1 18 15 11 .02 | --- --- Table 1.1563.b GPS week : 1563 MJD: 55185.000-55191.000 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 | 11 8 8 8 10 12 12 | 2 | 4 5 5 5 5 5 4 | 3 | 4 4 4 4 4 5 4 | 4 | 4 4 5 5 5 5 5 | 5 | 4 5 5 4 4 4 5 | 6 | 4 3 4 4 5 5 5 | 7 | 4 4 5 4 5 5 4 | 8 | 4 4 5 4 4 4 4 | 9 | 3 3 4 4 3 4 4 | 10 | 6 5 8 9 6 5 5 | 11 | 4 4 4 4 4 4 4 | 12 | 5 6 5 5 5 5 5 | 13 | 4 3 4 4 4 4 4 | 14 | 4 4 4 4 4 4 5 | 15 | 5 4 4 4 5 5 5 | 16 | 6 6 6 6 6 7 7 | 17 | 4 5 5 4 4 5 5 | 18 | 5 5 5 5 5 4 4 | 19 | 5 5 5 5 5 5 5 | 20 | 7 5 4 4 4 4 4 | 21 | 4 4 4 4 4 4 4 | 22 | 4 4 4 5 6 4 4 | 23 | 4 4 5 4 5 5 5 | 24 | 0 0 9 4 3 4 3 | 25 | 7 7 7 8 8 8 6 | 26 | 4 3 4 3 3 4 3 | 27 | 3 4 4 4 3 4 4 | 28 | 3 3 5 4 4 5 4 | 29 | 4 5 5 6 5 6 5 | 30 | 6 6 6 6 6 8 6 | 31 | 5 4 4 5 4 4 4 | 32 | 7 6 6 6 7 6 6 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1563.0 GPS week: 1563 Day: 0 MJD: 55185.000 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 239| 0 0 1 55 -57 21 -.13 9 8 | -1646 1697 15 66 | 6 -7 | emr 91| 2 -2 5 -17 -79 46 .49 19 19 | -1179 -747 19 93 | -32 -19 | esa 126| 0 0 -2 -125 11 -7 .25 7 7 | -2678 3389 16 102 | 3 -9 | gfz 195| -1 -2 -6 -70 -82 32 -.18 10 10 | -640 682 33 124 | -18 -86 | grg 109| -1 1 -10 -23 -174 -23 1.10 24 22 | -586 669 74 481 | 45 6 | igr n/a| 0 0 -1 31 -49 -40 .03 5 5 | 3406 -589 19 62 | -32 -24 | jpl 114| 0 0 11 41 -41 -16 .56 18 17 | 2316 -435 16 74 | 12 34 | mit 259| -1 0 -3 30 -103 2 -.29 12 9 | -16508 391 23 141 | -16 30 | ngs 213| 0 0 0 97 210 -22 -.15 8 6 | 15209 79 1903 3707 | 16 -4 | sio 256| 0 1 12 14 17 -22 -.03 21 19 | --- --- --- --- | -34 -8 | Table 2.1563.1 GPS week: 1563 Day: 1 MJD: 55186.000 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 239| 0 0 3 63 -50 -26 -.12 10 8 | -217 -815 29 90 | 6 8 | emr 91| 2 -2 5 -46 -58 14 .43 19 19 | -2483 -424 19 102 | -5 -34 | esa 126| 0 0 -4 -165 13 29 .30 7 7 | -1577 984 19 109 | 0 15 | gfz 195| 0 0 -5 -31 -100 3 -.12 10 10 | 420 -3423 41 150 | -23 -58 | grg 109| 0 1 -8 -90 -202 -31 1.02 27 24 | -147 -673 58 217 | 151 84 | igr n/a| 0 0 -1 25 -27 -34 .10 5 5 | 2336 -592 20 74 | -19 -14 | jpl 114| 0 0 14 33 -40 13 .54 17 16 | 1058 -442 21 88 | 36 19 | mit 259| -1 0 -3 42 -75 -9 -.33 9 8 | -15728 -1505 24 148 | -11 24 | ngs 213| 0 0 -1 112 220 0 -.20 8 7 | 16996 -2748 2289 4085 | -22 1 | sio 256| 0 1 11 17 43 -14 -.06 19 17 | --- --- --- --- | -38 -15 | Table 2.1563.2 GPS week: 1563 Day: 2 MJD: 55187.000 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 239| 1 1 0 44 -43 34 -.12 9 7 | -130 -28 23 71 | 34 -6 | emr 91| 2 -2 3 -57 -42 16 .51 18 18 | -2447 1043 18 94 | -7 -18 | esa 126| 1 0 0 -164 10 -27 .32 9 9 | -667 1597 22 113 | 7 -14 | gfz 195| 0 0 -9 -56 -45 -4 -.16 12 12 | 479 -1145 36 168 | 4 -62 | grg 109| 0 -2 -5 -56 -164 2 1.12 23 18 | 130 -139 54 214 | 53 74 | igr n/a| 1 0 0 9 -57 -28 .08 5 5 | 2303 791 23 64 | 8 22 | jpl 114| -2 0 14 28 -21 -38 .53 17 16 | 1143 901 20 93 | -35 -201 | mit 259| -1 0 -4 40 -93 10 -.30 9 7 | -15157 103 25 143 | -9 42 | ngs 213| 0 0 -2 107 239 -8 -.17 11 9 | 10904 3603 2121 3925 | -41 29 | sio 256| -1 0 10 52 37 1 -.04 21 15 | --- --- --- --- | -52 -14 | Table 2.1563.3 GPS week: 1563 Day: 3 MJD: 55188.000 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 239| 0 0 2 37 -64 -48 -.13 10 8 | -202 -522 13 55 | 35 27 | emr 91| 2 0 5 -78 -91 -23 .45 18 17 | -1995 483 18 105 | 26 16 | esa 126| 1 0 -1 -135 30 -17 .31 9 9 | -1742 2604 18 117 | 7 -20 | gfz 195| -2 2 -8 -22 -36 33 -.09 14 14 | 231 -396 29 128 | -25 -23 | grg 109| -1 1 -9 -55 -202 6 1.10 24 20 | 307 -741 53 193 | 11 121 | igr n/a| -1 0 -2 5 -89 -23 .05 6 6 | 2624 570 18 67 | -44 14 | jpl 114| 0 1 9 26 -36 28 .57 16 16 | 1459 382 18 83 | 19 21 | mit 259| 0 0 -2 23 -77 16 -.32 10 8 | -13741 -2843 21 145 | -6 25 | ngs 213| -1 0 -2 89 183 9 -.17 9 7 | 13316 2499 2236 4030 | -8 28 | sio 256| 0 0 12 20 24 6 -.05 21 17 | --- --- --- --- | -46 -12 | Table 2.1563.4 GPS week: 1563 Day: 4 MJD: 55189.000 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 239| 1 0 5 29 -69 -6 -.16 10 8 | -402 165 17 59 | 50 44 | emr 91| 0 -1 6 -53 -88 -41 .46 17 17 | -1186 1598 17 111 | -1 9 | esa 126| 1 0 -3 -134 20 40 .27 9 8 | -1376 1310 18 118 | 7 12 | gfz 195| 0 -2 -7 -55 56 -12 -.11 13 13 | 1028 -3170 31 123 | 32 -73 | grg 109| 0 0 -7 -54 -206 7 1.10 23 18 | -98 262 61 191 | 28 142 | igr n/a| 0 0 -2 -10 -76 -22 .07 5 5 | 3588 1587 19 73 | -8 -9 | jpl 114| 0 0 8 33 -49 30 .57 15 15 | 2248 1235 18 94 | 20 39 | mit 259| -1 0 -3 69 -76 -9 -.33 9 7 | -14501 1776 21 157 | -18 14 | ngs 213| 0 0 -4 83 174 -28 -.18 10 8 | 15778 130 2091 3795 | 24 86 | sio 256| -1 3 12 51 20 -20 -.07 18 16 | --- --- --- --- | -57 1 | Table 2.1563.5 GPS week: 1563 Day: 5 MJD: 55190.000 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 239| 1 1 3 35 -53 -50 -.18 9 8 | -402 -336 13 56 | 4 37 | emr 91| 1 -2 4 -84 -92 -28 .48 18 18 | -49 2241 16 85 | 37 21 | esa 126| 0 0 -2 -141 38 54 .28 9 9 | -309 -586 17 105 | -17 -6 | gfz 195| 0 0 -9 13 -34 9 -.11 12 12 | -729 3365 31 117 | -3 -42 | grg 109| 0 0 -8 -72 -235 -49 1.14 29 23 | 205 -739 66 242 | 108 169 | igr n/a| 0 0 -3 5 -29 -12 -.01 5 5 | 4747 2028 18 67 | -34 0 | jpl 114| -1 -1 10 14 -12 7 .57 16 16 | 2938 1682 16 86 | 8 -11 | mit 259| -1 0 -2 60 -74 -4 -.35 12 11 | -15049 -1196 22 125 | -15 21 | ngs 213| 0 0 -4 88 204 -15 -.17 11 9 | 6837 9441 2178 3845 | 50 -16 | sio 256| -1 2 14 22 12 -7 -.08 19 18 | --- --- --- --- | -44 29 | Table 2.1563.6 GPS week: 1563 Day: 6 MJD: 55191.000 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 239| 1 0 0 53 -58 17 -.14 7 7 | -517 167 14 61 | -13 6 | emr 91| -3 -2 2 -69 -71 -41 .46 19 19 | 2737 508 15 93 | 25 -25 | esa 126| 1 0 0 -140 26 26 .29 8 7 | -222 -372 17 111 | -23 17 | gfz 195| 1 -1 -7 -10 -36 -7 -.11 12 12 | 323 -933 31 170 | 27 -64 | grg 109| 0 0 -3 -88 -246 -31 1.13 31 27 | -46 189 50 212 | 166 162 | igr n/a| 0 0 -1 25 -44 -42 .05 5 5 | 7420 303 16 69 | -40 -30 | jpl 114| 0 -1 7 47 -3 -22 .54 18 17 | 5227 206 17 78 | 6 28 | mit 259| -1 0 -2 32 -83 -2 -.34 11 9 | -15992 2978 20 155 | 3 9 | ngs 213| 0 0 -3 105 210 -21 -.17 10 9 | 10709 5580 2232 4054 | -19 -8 | sio 256| -1 1 14 2 -1 -21 -.05 18 17 | --- --- --- --- | -26 16 | 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 3.1563.0 GPS week: 1563 Day: 0 MJD: 55185.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 17 26 --- --- --- 11 --- 16 16 --- 10 | 23 34 --- --- --- 22 --- 25 26 --- 24 2 | 8 18 6 7 27 4 21 10 7 23 4 | 23 30 21 23 36 21 34 26 25 25 23 3 | 7 12 8 9 27 5 14 12 7 19 3 | 21 24 25 27 27 22 23 22 24 22 23 4 | 8 15 7 8 16 5 11 8 8 32 4 | 29 26 29 33 37 30 25 26 29 37 27 5E | 7 18 6 11 22 5 18 9 10 17 4 | 29 32 27 37 36 28 28 30 26 31 28 6 | 6 11 6 9 30 5 13 10 6 18 3 | 26 27 31 33 36 28 29 29 31 30 29 7 | 4 23 8 9 24 5 18 7 7 10 3 | 22 34 23 25 44 21 30 20 25 18 21 8 | 8 21 8 9 13 3 14 11 8 12 4 | 13 26 15 16 27 13 24 18 16 15 14 9 | 8 15 6 7 16 4 13 9 4 13 3 | 18 23 16 17 27 16 22 17 20 16 16 10E | 15 20 7 14 26 7 19 14 10 30 5 | 102 101 101 103 107 102 103 101 97 101 99 11 | 6 20 6 11 20 5 19 8 8 21 4 | 35 42 36 36 48 34 38 35 41 29 36 12 | 9 24 8 7 25 3 22 7 7 17 4 | 53 59 60 55 61 54 58 53 54 56 56 13 | 5 21 5 7 26 5 17 6 6 10 3 | 21 33 26 28 50 21 30 19 23 17 21 14 | 8 21 7 5 25 4 19 9 7 15 4 | 16 27 19 16 37 17 26 18 22 19 18 15 | 7 25 8 9 25 5 22 8 7 18 4 | 18 30 19 19 37 16 25 18 16 22 17 16 | 7 26 11 10 51 6 19 16 8 36 5 | 28 37 26 31 45 27 33 32 31 40 29 17 | 8 16 6 14 22 4 20 7 5 24 4 | 20 28 24 31 35 21 32 23 26 24 22 18E | 7 23 6 16 22 5 21 9 7 16 4 | 26 35 29 28 42 27 38 27 29 29 28 19 | 7 15 9 9 20 5 17 13 8 26 4 | 22 27 23 25 29 21 28 23 24 22 21 20E | 10 21 11 22 17 6 15 30 8 16 6 | 35 44 43 48 45 41 39 39 44 36 39 21 | 6 15 5 8 23 5 19 10 5 21 3 | 29 41 30 26 44 28 44 26 29 25 29 22E | 7 15 5 11 17 7 18 8 8 12 3 | 21 25 22 22 31 22 33 24 27 26 23 23 | 7 23 5 7 21 5 17 11 5 12 3 | 25 34 27 26 45 23 31 20 24 19 22 X24 | 5 --- --- --- --- 23 --- --- --- --- 0 | 30 --- --- --- --- 34 --- --- --- --- 33 X25 | 8 18 12 --- --- 11 --- 12 --- --- 7 | 18 24 18 --- --- 15 --- 16 --- --- 15 26 | 11 12 6 8 18 4 12 10 6 11 3 | 19 30 23 22 33 21 30 21 22 20 21 27 | 7 14 6 6 15 4 12 9 5 12 3 | 19 23 17 19 27 16 21 20 22 18 17 28 | 7 13 4 7 24 3 15 6 8 16 3 | 38 43 41 42 57 39 42 37 42 35 39 29 | 9 14 8 7 22 5 19 7 7 29 4 | 23 28 30 23 36 24 32 22 24 19 25 30E | 12 23 10 11 23 5 23 10 16 34 6 | 102 104 99 100 111 102 103 98 105 117 101 31 | 10 18 7 8 35 3 18 19 10 16 5 | 21 28 22 20 44 17 29 22 20 19 20 32E | 19 25 7 17 17 7 21 19 10 30 6 | 128 132 130 126 135 125 134 124 131 125 129 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 7 10 24 5 18 12 8 21 |T 32 39 35 36 47 32 40 33 35 34 33 WRMS | 8 19 7 10 22 5 17 9 6 19 |NE 22 29 23 24 36 21 29 22 24 21 22 MEDI | 7 18 7 9 22 5 18 10 7 17 |MD 23 30 26 27 37 22 31 24 26 25 23 Table 3.1563.1 GPS week: 1563 Day: 1 MJD: 55186.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 11 27 --- --- --- 13 --- 11 9 --- 7 | 22 30 --- --- --- 21 --- 22 24 --- 21 2 | 7 15 9 7 33 5 18 11 9 24 4 | 15 23 19 15 29 14 25 18 17 15 14 3 | 5 16 6 8 29 4 12 9 10 20 3 | 17 20 22 24 29 19 20 18 20 18 18 4 | 8 9 7 8 20 5 9 10 9 33 4 | 15 19 24 20 26 18 19 19 18 33 18 5E | 7 23 7 14 17 6 18 8 9 19 4 | 23 30 29 35 34 23 25 23 27 23 24 6 | 5 13 6 7 31 4 11 7 10 17 3 | 20 22 27 24 35 24 25 22 25 26 23 7 | 5 26 7 11 26 4 16 8 7 10 4 | 17 32 23 21 40 18 28 16 20 15 18 8 | 7 20 5 8 15 4 14 11 9 12 4 | 12 24 21 17 30 15 24 17 19 16 15 9 | 9 15 5 5 20 3 14 8 6 13 3 | 13 21 19 17 23 14 21 14 17 14 14 10E | 14 18 8 9 28 5 18 11 10 17 4 | 98 100 99 100 109 99 97 102 99 112 100 11 | 6 20 5 6 18 4 16 6 5 21 3 | 24 36 30 28 41 28 33 28 29 26 26 12 | 22 22 8 7 29 8 23 9 9 23 5 | 99 105 104 107 113 104 112 108 103 103 103 13 | 4 21 6 7 30 3 14 5 8 9 3 | 17 29 22 18 49 18 28 15 18 15 17 14 | 9 23 6 9 30 5 21 8 7 15 4 | 15 26 23 18 35 18 29 16 24 14 18 15 | 8 22 7 6 27 4 21 7 6 21 4 | 12 28 20 16 36 15 24 14 17 14 14 16 | 11 25 9 14 55 6 23 14 8 31 5 | 44 50 45 46 64 46 48 47 47 48 44 17 | 9 13 9 18 23 5 19 7 7 23 4 | 16 26 25 33 31 20 28 19 19 22 21 18E | 8 23 8 11 27 6 18 7 8 19 4 | 25 34 29 30 32 27 33 24 31 24 26 19 | 9 18 6 10 24 5 15 11 9 26 4 | 14 20 16 17 24 15 20 19 18 18 14 20 | 17 21 8 11 21 5 14 16 7 11 5 | 50 58 51 53 58 51 55 51 48 56 49 21 | 6 14 8 8 27 5 16 7 8 22 3 | 20 32 29 22 39 23 34 19 22 18 22 22E | 9 14 6 8 27 5 19 5 7 11 3 | 19 23 21 20 27 19 29 20 24 17 20 23 | 9 25 6 11 25 4 15 6 6 11 4 | 17 31 24 21 39 20 29 19 21 19 20 X24 | 5 --- --- --- --- 151 --- --- --- --- 0 | 24 --- --- --- --- 132 --- --- --- --- 25 X25 | 12 18 12 --- --- 20 --- 10 --- --- 7 | 14 22 29 --- --- 18 --- 16 --- --- 19 26 | 10 10 5 9 21 4 10 7 7 10 3 | 17 22 26 22 29 21 27 21 26 19 21 27 | 6 15 7 7 22 3 14 10 7 13 3 | 11 21 20 19 24 15 19 13 16 16 14 28 | 4 15 7 7 25 5 14 5 6 16 3 | 30 37 35 33 48 31 33 31 31 32 31 29 | 8 18 7 10 20 8 20 9 8 27 4 | 18 32 26 22 33 24 32 21 22 18 21 30E | 13 19 10 23 21 7 21 9 14 23 6 | 78 82 84 82 82 80 80 77 78 85 79 31 | 9 20 8 9 39 5 17 11 7 14 4 | 16 27 20 19 41 17 26 18 25 16 18 32E | 22 26 6 14 23 6 18 12 10 16 5 | 117 124 125 119 126 121 125 120 123 124 121 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 19 7 10 27 5 17 9 8 19 |T 29 38 36 35 45 35 38 31 34 33 31 WRMS | 8 19 7 10 24 5 16 8 7 17 |NE 16 25 23 20 33 24 25 18 20 18 18 MEDI | 8 19 7 9 25 5 16 9 8 17 |MD 17 29 25 22 35 20 28 19 24 19 21 Table 3.1563.2 GPS week: 1563 Day: 2 MJD: 55187.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 11 26 --- --- --- 16 --- 11 11 --- 8 | 17 28 --- --- --- 22 --- 21 20 --- 18 2 | 8 14 9 7 33 4 18 12 7 24 4 | 18 24 22 21 35 20 32 22 24 21 20 3 | 6 10 7 9 27 5 12 8 10 19 3 | 21 25 24 26 30 23 28 26 24 23 22 4 | 8 11 9 7 20 4 10 12 10 30 4 | 18 21 23 24 30 22 23 19 27 28 19 5E | 7 19 9 15 16 5 16 8 10 20 4 | 24 31 30 38 33 24 32 28 28 27 26 6 | 5 10 8 9 29 6 12 9 8 19 3 | 20 24 21 27 32 23 28 25 25 24 22 7 | 6 17 11 13 24 4 19 6 18 11 4 | 16 26 20 22 37 17 30 17 30 15 17 8 | 9 17 10 9 12 6 15 11 14 12 4 | 11 23 17 17 28 16 27 20 24 17 14 9 | 7 16 8 8 15 4 13 8 8 13 3 | 13 24 21 18 24 16 26 15 16 15 15 10E | 17 28 14 19 29 7 18 13 14 56 8 | 78 81 75 76 87 73 80 68 67 62 70 11 | 6 15 7 10 17 5 15 6 10 20 4 | 24 30 24 25 33 25 30 27 30 20 23 12E | 17 20 11 10 20 3 23 8 9 16 5 | 51 59 62 56 66 59 65 56 57 57 56 13 | 4 18 7 9 26 4 16 6 12 10 3 | 14 27 20 17 44 15 27 14 25 13 15 14 | 7 19 8 5 24 4 17 6 8 11 3 | 13 24 20 14 36 16 27 16 19 14 15 15 | 6 20 9 8 23 5 18 7 8 18 4 | 12 26 18 16 34 15 27 15 17 18 13 16E | 9 27 10 23 41 4 21 9 8 13 5 | 53 60 55 60 59 53 54 51 59 56 55 17 | 9 15 10 14 20 6 19 7 13 22 4 | 16 28 26 28 34 21 30 20 21 21 20 18E | 6 19 8 14 16 6 18 7 11 17 4 | 26 35 31 34 39 31 39 30 30 29 29 19 | 8 14 7 7 20 6 17 8 12 26 4 | 19 24 20 21 25 17 28 23 22 20 18 20 | 7 19 7 11 22 5 15 8 10 20 4 | 35 38 37 35 34 35 36 32 39 31 33 21 | 6 17 8 10 19 5 19 8 9 21 4 | 19 33 25 21 36 22 39 19 22 19 21 22E | 7 15 6 16 21 5 19 6 9 8 4 | 23 29 26 29 36 26 37 28 29 28 26 23 | 9 23 8 15 22 3 16 7 11 14 4 | 13 30 18 17 35 15 25 17 24 14 15 X24 | 13 35 14 --- --- 10 --- 10 20 --- 8 | 23 36 24 --- --- 39 --- 21 23 --- 26 X25 | 11 15 11 --- --- 11 --- 10 --- --- 6 | 13 21 17 --- --- 17 --- 14 --- --- 12 26 | 7 10 7 9 14 3 11 8 11 12 3 | 16 21 17 18 28 18 26 21 25 21 18 27 | 7 18 9 11 16 4 11 9 8 13 4 | 11 24 20 19 25 15 23 15 16 16 14 28 | 13 16 13 10 19 6 16 7 13 14 4 | 64 73 69 70 73 69 70 67 72 66 67 29 | 8 15 11 9 21 5 19 10 10 28 4 | 15 24 24 22 28 18 32 19 21 18 17 30E | 10 20 9 23 18 9 19 12 13 25 5 | 48 58 54 58 59 51 61 47 49 63 50 31 | 7 15 10 9 30 6 16 8 6 12 3 | 15 25 21 19 39 16 31 18 20 17 17 32E | 14 27 13 14 20 7 17 12 15 29 6 | 57 63 60 62 59 63 66 62 66 58 60 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 9 12 23 5 17 9 11 21 |T 25 34 30 31 39 28 37 27 31 28 26 WRMS | 7 18 9 12 18 5 16 7 9 15 |NE 16 25 21 20 32 19 28 19 22 18 17 MEDI | 7 17 9 10 20 5 17 8 10 18 |MD 18 27 24 24 35 22 30 21 25 21 20 Table 3.1563.3 GPS week: 1563 Day: 3 MJD: 55188.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 14 21 --- --- --- 19 --- 10 11 --- 7 | 20 26 --- --- --- 24 --- 20 25 --- 20 2 | 9 12 9 12 31 6 18 14 9 26 5 | 25 26 23 21 34 21 29 26 20 25 22 3 | 7 10 9 10 25 6 11 6 6 20 3 | 25 24 25 28 33 24 26 25 25 25 24 4 | 8 12 12 9 22 7 14 14 9 30 5 | 26 27 27 29 38 28 28 26 28 35 25 5 | 8 17 8 12 23 5 15 6 8 15 4 | 60 60 61 67 67 59 58 59 64 61 60 6 | 6 11 7 12 27 5 12 9 8 21 3 | 25 25 25 27 33 26 29 27 24 30 25 7 | 8 17 9 11 26 5 15 6 9 12 4 | 22 28 22 19 39 17 26 18 22 17 19 8 | 7 18 10 11 17 5 14 12 8 12 4 | 18 22 19 12 28 14 23 19 17 16 14 9 | 10 14 8 10 16 5 10 5 7 12 3 | 20 21 18 19 25 16 20 17 17 16 15 10E | 25 24 13 28 33 10 19 21 11 54 9 | 78 89 82 85 89 83 88 90 88 106 84 11 | 4 17 6 10 17 4 16 6 6 18 3 | 33 35 30 35 41 31 31 31 33 24 29 12E | 11 21 9 20 21 6 23 6 8 14 5 | 37 41 39 33 42 37 39 33 37 35 35 13 | 4 17 10 9 28 5 18 6 9 10 3 | 19 28 22 18 45 17 26 15 16 15 16 14 | 10 18 9 9 27 5 18 5 7 13 4 | 16 25 19 16 36 16 29 15 21 14 16 15 | 6 21 8 12 24 7 17 8 5 15 4 | 17 25 16 12 36 14 22 14 14 14 13 16E | 9 25 9 20 45 5 20 10 10 16 5 | 41 45 41 46 55 39 46 36 42 38 40 17 | 9 15 7 16 19 6 17 7 8 20 4 | 21 28 26 31 34 23 29 21 21 23 21 18E | 7 20 7 13 18 5 19 8 8 20 4 | 24 31 27 26 30 22 27 21 27 22 23 19 | 8 15 11 10 19 5 17 9 6 26 4 | 20 26 23 25 28 23 26 23 21 21 20 20 | 5 16 7 8 19 7 14 6 8 16 3 | 25 29 25 22 32 21 24 23 22 26 21 21 | 7 14 8 9 25 7 16 7 10 22 4 | 25 35 28 26 38 27 34 21 26 20 24 22E | 13 13 10 29 20 8 18 8 7 11 5 | 36 44 46 51 48 43 47 42 48 40 42 23 | 6 22 8 9 22 6 19 9 6 12 4 | 19 32 21 18 37 16 28 16 17 15 16 X24 | 6 14 9 --- 17 6 --- 5 7 --- 4 | 26 18 15 --- 18 32 --- 15 15 --- 25 X25 | 12 14 18 --- --- 7 --- 12 --- --- 8 | 19 21 27 --- --- 18 --- 15 --- --- 16 26 | 7 10 8 10 17 5 11 6 8 10 3 | 23 27 25 21 30 23 28 23 27 22 23 27 | 7 16 8 11 16 4 10 7 7 13 3 | 17 22 16 18 24 17 18 16 18 17 14 28E | 11 15 11 10 18 5 16 7 11 11 4 | 33 40 38 36 41 38 40 36 36 39 35 29 | 10 17 11 12 23 8 19 15 7 28 5 | 21 29 24 22 31 24 30 25 24 21 21 30E | 13 18 13 13 19 7 16 16 15 28 6 | 73 75 75 71 78 74 74 73 74 79 72 31 | 9 18 9 11 34 7 20 7 10 12 4 | 20 30 21 18 42 19 31 19 23 17 19 32E | 13 32 9 13 24 7 16 11 15 31 6 | 97 100 98 96 97 94 100 94 97 100 96 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 9 14 24 6 16 10 9 21 |T 30 35 32 32 41 30 36 29 31 32 29 WRMS | 8 17 9 14 20 6 16 8 7 17 |NE 21 26 22 21 33 21 27 20 21 20 19 MEDI | 8 17 9 11 22 6 16 7 8 16 |MD 24 28 25 26 36 23 29 23 24 23 22 Table 3.1563.4 GPS week: 1563 Day: 4 MJD: 55189.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 15 --- --- --- --- 17 --- 11 15 --- 9 | 24 --- --- --- --- 27 --- 19 27 --- 22 2 | 7 11 6 10 35 6 15 13 11 25 4 | 21 28 22 24 35 23 29 28 23 25 22 3 | 8 12 7 9 27 4 10 6 14 22 4 | 20 22 21 25 35 21 21 23 22 23 20 4 | 9 12 6 8 20 6 10 14 13 28 4 | 25 28 29 28 33 29 25 29 34 34 27 5 | 6 17 8 10 24 4 14 5 7 14 3 | 33 36 32 37 49 32 33 33 37 31 33 6 | 8 12 9 10 26 3 10 9 15 22 4 | 19 23 23 27 34 23 24 26 23 28 22 7 | 7 20 11 11 26 5 20 6 7 14 4 | 20 32 26 24 42 23 30 22 22 20 21 8 | 7 15 8 10 15 4 13 12 8 10 4 | 15 24 20 18 29 16 21 20 20 16 16 9 | 7 13 8 8 14 4 12 6 6 11 3 | 16 21 16 17 25 14 20 16 19 15 15 10 | 17 15 6 28 22 6 16 12 11 14 6 | 82 90 87 85 93 86 93 90 93 80 86 11 | 6 16 9 7 16 4 13 6 7 19 3 | 29 38 30 34 40 31 34 31 31 29 29 12E | 6 22 7 18 18 4 18 9 8 12 4 | 30 36 31 34 40 30 33 29 30 30 29 13 | 7 18 9 8 28 6 19 5 9 10 4 | 18 32 23 21 48 21 29 19 19 16 19 14 | 9 19 9 6 25 2 16 6 7 11 3 | 15 23 20 16 37 14 25 17 20 17 15 15 | 7 20 8 7 24 4 22 10 9 15 4 | 16 25 20 17 38 17 25 19 24 21 17 16E | 10 26 10 26 43 6 20 10 12 14 6 | 31 39 27 35 52 29 33 29 29 29 28 17 | 9 14 9 12 21 5 17 5 7 19 4 | 18 32 26 31 36 25 29 21 25 23 23 18 | 19 22 9 12 21 6 17 6 12 15 5 | 36 50 45 48 50 44 46 44 53 38 43 19 | 6 16 11 8 20 4 17 8 11 25 4 | 17 24 18 21 27 18 23 23 25 20 18 20 | 5 19 7 9 18 5 12 7 10 13 3 | 21 31 22 23 30 21 26 24 23 26 21 21 | 5 12 7 6 21 4 14 6 9 22 3 | 25 36 29 26 40 27 37 24 28 23 26 22 | 30 13 8 13 24 7 14 7 10 13 5 | 51 66 66 66 71 63 64 66 70 62 62 23 | 7 22 11 10 21 6 19 8 8 14 4 | 16 29 22 18 37 17 26 18 20 17 17 X24 | 5 10 6 --- 15 4 6 5 8 --- 3 | 23 17 21 --- 18 28 9 20 25 --- 25 X25 | 10 16 14 --- --- 14 --- 15 --- --- 8 | 21 27 29 --- --- 28 --- 22 --- --- 21 26 | 7 12 8 7 15 2 12 8 7 11 3 | 16 23 20 16 30 16 27 17 21 16 17 27 | 7 14 7 8 15 3 12 6 8 13 3 | 15 21 15 18 26 14 19 17 20 18 15 28E | 8 13 8 12 19 5 14 6 7 10 3 | 24 32 26 27 33 28 28 26 30 27 25 29 | 10 14 8 11 19 8 17 15 8 28 5 | 21 25 28 25 35 20 27 26 23 20 22 30E | 12 19 10 11 22 4 16 17 12 27 5 | 40 44 44 43 54 42 47 45 43 45 41 31 | 7 17 9 6 32 5 16 6 5 13 3 | 16 28 21 19 40 20 28 20 23 17 18 32E | 14 32 10 24 23 5 16 13 19 32 7 | 74 78 72 78 79 73 74 72 69 81 72 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 17 9 13 23 5 15 9 10 18 |T 26 34 30 31 41 28 32 29 31 29 27 WRMS | 8 17 8 13 18 5 15 7 8 16 |NE 19 26 22 22 34 21 25 21 23 20 20 MEDI | 7 16 8 10 21 5 15 7 9 14 |MD 21 29 26 25 37 23 28 23 25 23 22 Table 3.1563.5 GPS week: 1563 Day: 5 MJD: 55190.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 16 28 --- --- --- 30 --- 10 28 --- 12 | 22 25 --- --- --- 43 --- 20 38 --- 20 2 | 8 14 9 11 42 5 16 15 13 25 5 | 17 21 16 19 30 16 23 24 16 19 16 3 | 9 14 10 9 39 5 11 9 12 25 4 | 19 24 22 25 40 21 20 21 17 25 19 4 | 7 13 9 9 24 5 10 19 8 27 4 | 21 22 27 26 32 21 21 22 22 28 21 5 | 8 17 6 11 30 5 15 10 9 21 4 | 25 31 27 31 39 25 28 24 27 30 26 6 | 8 15 9 10 41 5 11 12 12 25 4 | 13 21 20 22 41 19 18 21 15 28 16 7 | 8 20 11 11 23 4 16 11 11 16 4 | 19 30 25 25 41 20 28 20 23 18 20 8 | 9 16 9 9 20 4 12 15 9 13 4 | 14 22 15 15 29 13 22 15 16 12 12 9 | 8 16 6 9 16 4 14 8 16 14 4 | 18 24 16 17 24 16 21 19 20 16 16 10 | 14 20 8 11 49 7 17 13 11 16 5 | 61 66 64 64 86 62 70 61 62 65 63 11 | 8 14 7 7 18 5 15 9 8 18 3 | 26 32 30 31 36 30 28 28 30 23 26 12E | 8 20 8 8 29 4 21 8 10 13 4 | 21 30 28 25 37 25 30 25 22 25 23 13 | 6 16 7 9 28 4 16 9 9 12 3 | 18 31 23 23 49 20 29 18 23 17 19 14 | 8 19 7 9 31 6 19 7 10 12 4 | 14 23 17 15 37 15 22 13 16 15 13 15 | 7 25 10 12 25 4 19 13 12 15 5 | 19 29 22 21 40 18 25 15 19 18 17 16E | 7 29 13 17 47 7 22 25 11 16 6 | 22 35 21 25 45 22 29 32 28 27 23 17 | 9 14 6 13 21 7 16 7 14 20 4 | 15 27 24 28 36 20 28 16 24 20 20 18 | 6 19 6 10 28 5 16 7 9 12 3 | 15 26 15 14 34 14 23 12 17 13 13 19 | 5 16 12 10 24 5 17 15 10 25 5 | 17 23 24 21 23 18 22 26 20 22 18 20 | 7 22 7 8 22 4 14 8 7 11 4 | 27 37 27 30 32 27 30 29 29 29 27 21 | 7 18 6 7 24 6 16 10 10 23 4 | 21 37 25 19 42 24 35 18 24 20 22 22 | 9 14 8 8 38 5 17 8 10 10 4 | 22 25 23 25 42 23 26 19 25 19 20 23 | 9 21 8 9 22 5 16 14 6 15 4 | 19 30 23 21 36 19 27 19 23 17 19 X24 | 5 13 7 --- 20 3 7 8 12 --- 3 | 19 16 14 --- 16 26 10 16 20 --- 21 X25 | 12 16 10 --- --- 9 --- 14 --- --- 7 | 20 22 20 --- --- 18 --- 19 --- --- 16 26 | 6 13 7 11 22 3 12 7 11 11 3 | 22 27 23 23 32 22 27 22 24 22 22 27 | 7 17 6 10 17 4 13 8 15 14 4 | 17 26 18 21 26 18 21 21 21 20 17 28E | 8 13 12 12 21 4 15 12 13 21 4 | 19 31 26 29 31 24 26 23 25 27 23 29 | 9 15 9 8 27 6 21 19 10 27 5 | 19 24 22 20 32 22 26 28 25 23 21 30E | 13 20 10 35 27 4 21 19 17 28 7 | 64 63 70 77 69 67 64 66 68 71 66 31 | 7 14 8 10 34 4 16 11 12 11 4 | 15 25 18 19 39 15 24 15 18 15 15 32E | 17 29 10 18 21 6 16 9 15 24 6 | 107 109 105 103 111 106 107 102 106 110 105 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 9 12 29 5 16 12 11 19 |T 24 31 27 28 40 26 30 25 27 27 24 WRMS | 8 18 9 12 23 5 16 11 9 18 |NE 18 25 21 21 34 19 23 19 20 19 18 MEDI | 8 16 8 10 24 5 16 10 11 16 |MD 19 26 23 23 36 21 26 21 23 22 20 Table 3.1563.6 GPS week: 1563 Day: 6 MJD: 55191.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 17 --- --- --- --- 26 --- 12 21 --- 12 | 23 --- --- --- --- 39 --- 20 36 --- 23 2 | 7 14 6 11 46 4 17 11 10 24 4 | 28 29 26 21 38 23 34 29 26 26 25 3 | 8 17 8 8 32 6 13 8 7 29 4 | 25 23 26 28 36 23 27 27 27 35 25 4 | 6 13 10 10 28 6 10 15 10 26 4 | 29 27 36 33 39 33 30 30 35 34 31 5 | 4 20 6 14 30 5 14 10 11 21 4 | 32 31 31 33 42 29 29 35 32 39 31 6 | 7 16 9 9 29 5 13 11 8 27 4 | 25 24 27 31 38 26 30 31 27 36 27 7 | 6 19 9 14 29 5 18 8 10 15 4 | 27 31 24 22 38 22 32 24 26 21 24 8 | 5 17 8 9 26 5 13 11 8 11 3 | 18 20 17 13 26 13 22 19 18 14 15 9 | 8 14 7 8 22 4 11 7 12 15 3 | 17 21 18 17 24 15 20 15 23 13 15 10 | 12 20 7 12 36 6 16 13 9 15 4 | 73 78 77 71 91 76 81 74 76 78 75 11 | 5 18 6 9 21 4 17 9 8 19 4 | 41 42 40 43 48 42 36 43 43 32 39 12E | 8 23 8 12 28 3 23 10 10 14 4 | 42 44 45 40 45 40 47 39 41 45 41 13 | 6 17 5 11 35 6 17 8 7 13 3 | 22 28 21 19 42 19 28 19 19 17 19 14 | 6 23 9 7 31 4 21 8 13 12 4 | 18 27 22 17 35 16 29 17 23 18 19 15 | 6 22 7 8 31 6 22 12 9 14 4 | 19 27 19 17 37 16 24 22 23 19 18 16E | 8 28 10 25 59 9 27 30 10 16 7 | 39 44 36 39 56 33 43 37 35 38 34 17 | 6 15 6 15 26 3 24 5 10 20 4 | 22 24 26 29 35 23 29 20 26 23 22 18 | 5 19 6 11 28 2 21 6 7 13 3 | 25 33 27 31 41 28 33 26 32 25 27 19 | 5 17 7 8 26 3 19 13 8 25 4 | 26 28 24 30 33 25 26 31 28 28 25 20 | 5 19 7 8 24 6 17 9 8 10 3 | 23 32 23 23 31 23 29 27 24 26 23 21 | 5 13 7 10 --- 5 14 7 9 23 3 | 26 34 31 28 --- 25 37 23 25 23 26 22 | 6 13 5 8 37 4 16 9 8 12 3 | 29 35 34 35 51 33 34 33 38 31 32 23 | 8 23 7 13 31 6 19 11 8 14 4 | 21 34 21 21 34 19 30 24 25 21 21 X24 | 4 11 5 --- 27 4 11 8 8 --- 3 | 29 16 19 --- 18 30 13 20 20 --- 29 X25 | 8 16 10 --- --- 10 --- 11 --- --- 6 | 25 30 25 --- --- 23 --- 21 --- --- 23 26 | 5 13 7 8 27 2 13 5 9 13 3 | 23 28 27 25 27 23 31 23 27 25 25 27 | 6 17 8 9 22 4 11 7 11 17 3 | 19 23 22 21 26 18 24 17 27 17 19 28E | 6 19 9 10 26 4 21 8 10 10 4 | 27 31 25 27 33 26 31 27 28 31 25 29 | 8 15 6 11 28 6 21 19 8 27 5 | 25 30 28 31 35 25 32 27 27 27 25 30E | 12 17 8 21 27 6 18 14 11 22 5 | 77 75 77 81 77 76 73 73 79 80 76 31 | 5 19 6 8 35 6 18 10 10 13 4 | 19 31 21 21 41 20 30 17 22 17 19 32E | 13 28 10 19 27 5 20 9 11 15 5 | 132 135 129 135 138 129 137 133 132 131 131 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 19 8 12 31 5 18 11 10 18 |T 32 35 33 33 43 31 36 31 34 33 31 WRMS | 7 19 7 12 27 5 17 9 9 17 |NE 24 27 24 24 34 22 28 23 25 23 23 MEDI | 6 17 7 10 28 5 17 9 9 15 |MD 25 30 26 28 38 25 30 26 27 26 25 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 4.1563 GPS week: 1563 MJD: 55185.0-55191.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3055 |U 7 6 20 |U 10 12 34 |U 9 8 15 | emr | emr 2997 | 11 8 31 |U 11 12 39 | 9 7 18 | esa | esa 2948 | 11 8 25 |U 11 12 35 | 9 8 15 | gfz | gfz 2729 |U 13 16 70 |U 14 18 44 | 13 13 28 | grg | grg 2825 | 12 10 29 |U 14 15 39 | 13 11 20 | igr | igr 2961 | 9 7 24 | 12 15 42 | 7 7 16 | igs | igs 2932 | 8 7 23 | 12 15 36 | 8 6 15 | jpl | jpl 2814 | 11 7 32 |U 12 14 37 |U 9 7 18 | mit | mit 3044 |U 10 8 29 |U 12 13 35 |U 8 8 17 | 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 5.1563.0 GPS week: 1563 Day: 0 MJD: 55185.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3060 | 9 8 22 | 10 11 25 | 10 7 17 | emr | emr 2966 | 12 6 30 | 10 11 28 | 11 9 16 | esa | esa 2880 | 10 7 23 | 10 13 31 | 10 8 15 | gfz | gfz 2736 | 12 11 27 | 12 15 45 | 16 15 23 | grg | grg 2784 | 11 10 28 | 15 17 31 | 16 14 17 | igr | igr 3010 | 13 13 24 | 10 13 29 | 9 7 15 | igs | igs 2845 | 10 8 23 | 9 12 26 | 12 6 18 | jpl | jpl 2771 | 11 8 24 | 9 13 29 | 10 7 15 | mit | mit 2976 | 16 9 59 | 14 12 27 | 11 7 19 | Table 5.1563.1 GPS week: 1563 Day: 1 MJD: 55186.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3065 | 8 7 15 | 9 13 29 | 8 7 10 | emr | emr 2959 | 11 9 24 | 11 11 37 | 8 9 19 | esa | esa 2880 | 9 7 15 | 8 11 32 | 7 4 12 | gfz | gfz 2726 | 30 49 230 | 14 20 47 | 16 9 38 | grg | grg 2784 | 9 9 16 | 12 14 35 | 11 7 21 | igr | igr 2923 | 10 7 21 | 18 27 44 | 6 5 20 | igs | igs 2860 | 10 10 29 | 22 29 44 | 7 6 18 | jpl | jpl 2769 | 10 8 25 | 12 11 32 | 9 7 18 | mit | mit 2976 | 11 7 25 | 11 15 31 | 7 6 23 | Table 5.1563.2 GPS week: 1563 Day: 2 MJD: 55187.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3032 | 7 7 25 | 7 9 27 | 12 10 20 | emr | emr 3043 | 13 9 50 | 9 10 36 | 7 7 17 | esa | esa 2976 | 9 7 44 | 6 10 27 | 9 10 16 | gfz | gfz 2732 | 10 12 126 | 11 13 46 | 12 14 26 | grg | grg 2784 | 12 8 43 | 9 8 34 | 12 10 19 | igr | igr 2969 | 10 6 41 | 8 11 31 | 6 9 15 | igs | igs 2945 | 8 9 26 | 7 11 30 | 6 7 14 | jpl | jpl 2774 | 10 7 65 | 8 11 34 | 8 6 15 | mit | mit 3072 | 9 9 31 | 8 11 28 | 10 9 19 | Table 5.1563.3 GPS week: 1563 Day: 3 MJD: 55188.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3059 | 6 6 18 | 8 10 31 | 10 11 21 | emr | emr 3054 | 12 8 31 | 8 10 39 | 11 9 24 | esa | esa 2976 | 8 8 20 | 8 10 30 | 11 12 19 | gfz | gfz 2713 | 10 9 25 | 14 18 42 | 14 15 24 | grg | grg 2880 | 8 5 23 | 11 11 39 | 16 15 27 | igr | igr 2969 | 7 7 20 | 8 11 50 | 8 10 19 | igs | igs 2964 | 7 7 20 | 8 9 32 | 9 10 19 | jpl | jpl 2771 | 11 7 24 | 10 13 34 | 12 10 26 | mit | mit 3072 | 8 6 21 | 9 10 30 | 8 10 16 | Table 5.1563.4 GPS week: 1563 Day: 4 MJD: 55189.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3070 | 7 6 19 | 9 13 42 | 8 7 15 | emr | emr 2949 | 10 9 27 | 11 10 43 | 9 4 13 | esa | esa 2976 | 7 6 21 | 10 11 42 | 9 8 14 | gfz | gfz 2731 | 8 12 34 | 13 28 39 | 12 15 30 | grg | grg 2880 | 8 9 23 | 12 15 39 | 12 8 14 | igr | igr 2930 | 7 6 23 | 12 11 62 | 6 4 15 | igs | igs 2968 | 7 6 24 | 11 11 41 | 7 5 14 | jpl | jpl 2871 | 11 5 29 | 11 11 40 | 8 4 19 | mit | mit 3072 | 7 9 19 | 11 12 40 | 8 8 19 | Table 5.1563.5 GPS week: 1563 Day: 5 MJD: 55190.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3047 | 6 6 19 | 10 12 31 | 7 6 11 | emr | emr 3051 | 9 8 26 | 11 12 43 | 8 5 17 | esa | esa 2976 | 24 15 36 | 12 12 34 | 8 6 12 | gfz | gfz 2743 | 11 9 24 | 16 14 45 | 13 11 28 | grg | grg 2880 | 27 27 42 | 14 16 38 | 13 11 19 | igr | igr 2974 | 8 6 21 | 11 11 30 | 7 5 11 | igs | igs 2955 | 8 6 19 | 12 11 35 | 8 6 12 | jpl | jpl 2870 | 11 7 29 | 11 14 42 | 7 6 20 | mit | mit 3072 | 12 10 32 | 13 12 38 | 9 8 13 | Table 5.1563.6 GPS week: 1563 Day: 6 MJD: 55191.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3055 | 7 4 19 | 19 20 51 | 6 7 12 | emr | emr 2963 | 10 9 28 | 19 21 48 | 7 6 17 | esa | esa 2976 | 8 5 17 | 18 19 51 | 7 8 14 | gfz | gfz 2728 | 11 9 23 | 20 22 44 | 12 11 25 | grg | grg 2784 | 10 6 27 | 21 24 57 | 12 10 21 | igr | igr 2956 | 8 4 16 | 19 19 49 | 6 6 14 | igs | igs 2991 | 7 5 18 | 18 19 47 | 6 5 11 | jpl | jpl 2876 | 10 6 25 | 19 22 49 | 7 6 18 | mit | mit 3072 | 7 5 18 | 19 22 48 | 7 6 13 | 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 6.1563 GPS week: 1563 MJD: 55185.500-55191.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -18 -22 14 55 0 | 0 16 | 13 23 40 52 7 | 3 emr uuuuu | 5 -11 -117 -127 -6 | 39 42 | 19 22 112 79 9 | 2 esa uuuuu | -1 -2 98 168 -15 | -2 19 | 16 15 41 70 12 | 6 gfz uuuuu | 56 -4 67 27 10 | -13 23 | 21 22 51 48 8 | 6 grg --xxx | -- -- 336 47 -8 | 10 18 | -- -- 273 270 18 | 1 igr xxxxx | 4 20 58 -74 -7 | 1 13 | 23 22 21 65 8 | 3 irf xxxxx | -2 -5 1 32 4 | -3 16 | 11 6 17 33 3 | 3 jpl uuuuu | 8 -14 30 13 -13 | 22 27 | 78 20 66 45 6 | 4 mit uuuuu | -26 6 -73 21 10 | -4 17 | 20 11 39 69 7 | 4 ngs uuuuu | -19 -5 -84 -132 1 | -10 15 | 30 26 119 95 4 | 2 sio uuuuu | -2 38 60 -134 6 | 10 19 | 19 13 30 68 9 | 2 Table 7.1563.0 GPS week: 1563 Day: 0 MJD: 55185.500 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 -11 20 89 4 | -4 12 emr uuuuu | 9 27 -273 -1 6 | 36 38 esa uuuuu | -1 -8 20 148 1 | -2 19 gfz uuuuu | 76 13 44 21 11 | -22 25 grg --xxx | -- -- 49 158 -19 | 12 18 igr xxxxx | 14 27 59 18 7 | -3 12 irf xxxxx | -10 -5 -25 -20 -1 | -6 12 jpl uuuuu | -44 -17 13 54 -3 | 20 27 mit uuuuu | -40 11 -140 -64 -1 | -7 14 ngs uuuuu | -6 -21 131 -137 5 | -13 15 sio uuuuu | -2 29 54 -30 -10 | 9 16 Table 7.1563.1 GPS week: 1563 Day: 1 MJD: 55186.500 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 | -9 -16 34 132 8 | -3 12 emr uuuuu | 33 -5 -282 -35 0 | 37 39 esa uuuuu | -16 -10 102 200 -4 | 0 15 gfz uuuuu | 57 13 -12 8 19 | -21 24 grg --xxx | -- -- 373 335 -20 | 8 18 igr xxxxx | 13 9 27 -132 -2 | -1 10 irf xxxxx | -1 -10 25 -1 5 | -7 13 jpl uuuuu | -20 -46 67 13 -15 | 21 26 mit uuuuu | -25 1 -42 -42 6 | -9 15 ngs uuuuu | -2 12 -36 -124 -6 | -13 15 sio uuuuu | 14 28 114 -213 1 | 6 16 Table 7.1563.2 GPS week: 1563 Day: 2 MJD: 55187.500 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 | -13 -49 -42 74 2 | 1 18 emr uuuuu | -1 -8 -68 -134 0 | 40 44 esa uuuuu | -5 -22 146 44 -25 | 5 19 gfz uuuuu | 43 -19 134 120 21 | -15 24 grg --xxx | -- -- 189 216 -11 | 9 19 igr xxxxx | -41 -23 50 -92 -7 | 4 14 irf xxxxx | -19 -15 7 34 4 | -2 17 jpl uuuuu | 182 20 -24 23 -19 | 26 30 mit uuuuu | -61 -6 -58 -16 10 | -5 19 ngs uuuuu | -48 26 -183 14 5 | -10 16 sio uuuuu | -5 37 76 -199 5 | 9 21 Table 7.1563.3 GPS week: 1563 Day: 3 MJD: 55188.500 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 | -19 -39 63 72 3 | 0 17 emr uuuuu | -8 -30 -82 -207 -4 | 39 42 esa uuuuu | 28 -11 133 276 -27 | 2 17 gfz uuuuu | 31 21 45 -27 7 | -13 25 grg --xxx | -- -- 131 154 -13 | 11 18 igr xxxxx | -6 40 62 -130 -16 | 3 14 irf xxxxx | 8 -4 -5 34 8 | -3 17 jpl uuuuu | -13 -23 -35 13 -8 | 24 29 mit uuuuu | -17 2 -99 7 18 | -5 18 ngs uuuuu | -20 4 -8 -113 -2 | -9 16 sio uuuuu | 20 42 71 -133 17 | 8 18 Table 7.1563.4 GPS week: 1563 Day: 4 MJD: 55189.500 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 -46 27 32 -1 | 4 17 emr uuuuu | 6 5 -58 -155 -11 | 42 45 esa uuuuu | 3 -3 82 161 -24 | 0 18 gfz uuuuu | 88 -28 112 41 8 | -8 21 grg --xxx | -- -- 207 -44 -4 | 9 17 igr xxxxx | 24 12 97 -132 -8 | 4 13 irf xxxxx | 15 4 -3 76 5 | 1 17 jpl uuuuu | -24 -16 94 -82 -20 | 26 30 mit uuuuu | 1 22 -79 43 14 | 0 19 ngs uuuuu | -71 -20 -128 -74 5 | -7 15 sio uuuuu | 14 61 40 -172 11 | 12 22 Table 7.1563.5 GPS week: 1563 Day: 5 MJD: 55190.500 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 | -40 -2 38 -16 -15 | 4 17 emr uuuuu | -24 -35 -10 -190 -12 | 41 44 esa uuuuu | 3 19 90 189 -20 | -5 20 gfz uuuuu | 39 5 43 34 -4 | -6 19 grg --xxx | -- -- 619 4 30 | 10 17 igr xxxxx | -3 36 57 4 -11 | 3 14 irf xxxxx | -3 2 -13 64 5 | 1 17 jpl uuuuu | 8 -6 127 23 -15 | 22 28 mit uuuuu | -24 17 -71 103 15 | 1 19 ngs uuuuu | 13 -48 -172 -287 4 | -7 14 sio uuuuu | -32 46 21 -67 12 | 12 22 Table 7.1563.6 GPS week: 1563 Day: 6 MJD: 55191.500 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 | -9 9 -40 3 2 | -1 20 emr uuuuu | 22 -29 -44 -169 -18 | 37 41 esa uuuuu | -20 19 112 156 -6 | -12 24 gfz uuuuu | 61 -31 103 -11 10 | -9 22 grg --xxx | -- -- 786 -494 -18 | 10 17 igr xxxxx | 27 36 52 -57 -11 | -2 17 irf xxxxx | -3 -4 19 38 2 | -2 18 jpl uuuuu | -31 -10 -33 47 -11 | 15 23 mit uuuuu | -12 -7 -19 115 5 | -1 19 ngs uuuuu | 5 15 -189 -203 -1 | -10 17 sio uuuuu | -19 22 45 -123 5 | 10 21