Date: Thu, 14 Jan 2010 12:56:13 +0000 From: Jim Ray Subject: [IGSREPORT-18189] Wk 1564 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4b4f146d.iIyEksursdPxUOW4%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 14 Jan 04:56:37 PST 2010 Message Number 18189 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1564 (Dec 27, 2009 - Jan 02, 2010) 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: igs1564[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1564[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1564[0-6].cls IGS GPS clock combination summary report. igs15647.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15647.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 | 30 30 0 | EMR | 25 12 16 25 WTZR 0 | ESA | 30 0 | GFZ | 32 ADE1 ALGO ALIC ALRT AMC2 AREQ BAKO BOR1 BRFT BRUS 0 | GFZ | CAS1 CEDU CHAT CHPI CHUR COCO CONZ CRO1 DAEJ DGAR 0 | GFZ | EIL1 FAA1 FAIR GLPS GODE GRAZ GUAM HARB HOFN HOLM 0 | GFZ | HRAO HRM1 HYDE IRKT ISPA KARR KIRU KOUR LPGS MAC1 0 | GFZ | MAL2 MAS1 MCM4 NICO NRC1 NRMD NTUS NYAL ONSA PDEL 0 | GFZ | PIE1 PIMO PRDS QAQ1 RABT RAMO RIOP SANT SFER SHAO 0 | GFZ | SSIA STJO SUTH SYOG TEHN THU3 TIDB TLSE TOW2 TRO1 0 | GFZ | TSKB TWTF UNSA USUD WAB2 WHIT WSRT WTZR YAKT YELL 0 | GFZ | YKRO YSSK 0 | GRG | ONSA 0 | JPL | 16 32 DGAR SYOG 0 | MIT | SYOG SYOG 0 | NGS | 1 1 | ALL | 1 1 1 | COD | 30 30 HARB NRIL 1 | EMR | HARB WTZR 1 | ESA | 30 1 | GFZ | 6 12 16 23 24 31 ALGO AUCK BOGT CHAT CHUR CONZ DAEJ 1 | GFZ | EIL1 GODE GRAZ GUAM GUAT HARB HOB2 HRAO KIRU MAC1 1 | GFZ | MCM4 METS NRC1 NYAL PETP PRDS PRE1 QAQ1 SHAO STJO 1 | GFZ | THU3 TLSE TOW2 TRO1 VILL WSRT WTZR YAKT YELL YKRO 1 | GFZ | ZIMM 1 | GRG | ONSA 1 | JPL | 32 DAEJ DGAR 1 | MIT | 25 25 HARB 2 | ESA | 30 2 | GFZ | 6 16 AREQ AUCK BRFT CAS1 CEDU CHPI COCO DARW FAA1 2 | GFZ | GUAM GUAT HARB HOLM HRAO ISPA KARR KIRU MAS1 METS 2 | GFZ | OUS2 PERT SUTH SUTM TOW2 YAKT YELL ZIMM 2 | GRG | ONSA YAKT 2 | JPL | 32 DGAR 2 | NGS | 1 3 | COD | MATE 3 | EMR | WTZR WTZR 3 | ESA | 21 3 | GFZ | 16 28 30 ASPA BRFT BRUS CHPI COCO CONZ CRO1 EIL1 3 | GFZ | FAA1 GUAM GUAT HARB HYDE MAS1 MCM4 MDO1 METS NRMD 3 | GFZ | NYAL PRDS RAMO SANT SUTH TOW2 VILL WHIT YAKT YELL 3 | GRG | ONSA 3 | JPL | 32 DGAR 3 | MIT | 1 25 1 25 30 HARB SHAO 4 | ALL | 1 4 | EMR | 25 25 WTZR WTZR 4 | ESA | FAA1 4 | GFZ | 5 16 28 30 32 ALGO ALIC AREQ CHAT CHPI COCO DAV1 4 | GFZ | DGAR GUAM GUAT HARB HOB2 IRKT ISPA KARR KERG MAC1 4 | GFZ | MAS1 MAW1 MCM4 MDO1 NRMD NTUS OUS2 PERT PRE1 RIOP 4 | GFZ | SANT SYOG TLSE TOW2 TSKB TWTF YAKT YAR2 YELL 4 | GRG | ALGO ONSA 4 | JPL | 30 DGAR 4 | MIT | 1 30 KHAJ 4 | NGS | 1 5 | ALL | 1 1 5 | COD | 30 30 5 | EMR | WTZR WTZR 5 | ESA | 25 26 5 | GFZ | 5 6 9 10 16 26 27 30 AMC2 AREQ AUCK BUE1 CAS1 CHPI 5 | GFZ | CHUR CRO1 DAEJ DARW DGAR EIL1 FAA1 FLIN GUAM GUAT 5 | GFZ | HRM1 ISPA MAS1 MDO1 MIZU PERT PIE1 PIMO PRDS QIKI 5 | GFZ | RIOP SFER STJO SUWN SYOG THU3 TSKB TWTF YAKT YAR2 5 | GFZ | YELL 5 | GRG | ONSA 5 | JPL | 30 32 DGAR HARB 5 | MIT | 23 25 26 10 23 25 26 6 | ALL | 1 1 6 | COD | 30 30 6 | EMR | 25 WTZR WTZR 6 | ESA | 30 6 | GFZ | 12 16 18 19 ALGO ALIC AUCK BRUS CHAT CHPI DARW DAV1 6 | GFZ | DGAR FAA1 GUAM HARB HOB2 HRAO KARR KERG MATE MAW1 6 | GFZ | MCM4 MIZU NRC1 NTUS NYAL ONSA PERT PRDS QIKI RAMO 6 | GFZ | RIOP SANT THU3 TIDB TLSE TOW2 TSKB WAB2 YAKT YAR2 6 | GRG | ONSA 6 | JPL | 32 DGAR 6 | MIT | HARB 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 | .0 .9 .6 -20 -3 -23 .06 EMR | 7.9 -2.3 4.9 27 -15 33 .43 ESA | 7.4 .2 -4.7 33 -93 4 .11 GFZ | .2 1.2 1.0 17 -18 -7 .07 GRG | .8 4.5 2.5 8 33 137 .81 JPL | 4.3 .9 14.1 6 -45 -38 .24 MIT | 1.6 .1 -13.6 -9 1 -34 .15 NGS | 11.8 -3.7 -8.6 -48 -196 13 .18 SIO | 1.3 2.0 1.9 46 5 48 .32 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 1.1564.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1564.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 2.1564.[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 3.1564.[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 5.1564.0-6). 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 1564 summary. (Dec 27, 2009 - Jan 02, 2010) Table 1.1564.a GPS week: 1564 MJD: 55192.000-55198.000 Mean and standard deviations of transformation parameters to the combined IGS orbit. WRMS - orbit RMS weighted by the SP3 header accuracy codes. STA - Mean number of stations in the daily solutions. CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 237| 0 0 2 37 -86 -11 -.17 8 7 | -394 150 16 65 | 0 0 0 13 20 26 .02 | 327 499 emr 104| 1 -1 6 -56 -63 -14 .50 18 18 | 161 -414 23 91 | 2 0 2 25 23 8 .04 | 2748 1317 esa 138| 0 0 -3 -71 37 -6 .27 8 8 | -912 1546 19 121 | 1 1 1 13 30 26 .02 | 1233 2239 gfz 192| 0 -1 -5 -30 -57 9 -.12 9 9 | 136 218 35 145 | 0 0 1 46 24 9 .03 | 501 1530 grg 106| -2 0 1 -45 -214 -16 1.12 27 23 | -19 31 57 232 | 1 1 1 25 21 18 .04 | 255 713 igr n/a| 0 0 -2 5 -85 -49 .03 5 5 | 4758 -332 20 68 | 0 0 1 20 11 24 .02 | 2526 1320 jpl 125| 0 0 10 -15 -1 -1 .60 17 16 | 2794 -248 20 96 | 1 1 1 21 9 38 .02 | 2279 1283 mit 264| -2 0 -3 28 -109 0 -.31 13 11 | -15436 525 21 118 | 0 1 1 37 26 13 .02 | 597 1786 ngs 212| 0 0 -3 95 303 -14 -.16 10 8 | 8950 1501 2591 15375 | 0 0 0 30 17 21 .03 | 6166 3166 sio 255| -1 1 10 -88 -135 62 -.16 19 18 | --- --- --- --- | 1 1 0 31 24 18 .04 | --- --- Table 1.1564.b GPS week : 1564 MJD: 55192.000-55198.000 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 | 14 13 17 11 9 9 7 | 2 | 5 5 4 4 5 4 4 | 3 | 4 5 4 4 4 5 6 | 4 | 5 5 4 4 4 4 4 | 5 | 5 5 4 5 4 3 4 | 6 | 4 4 4 4 5 5 6 | 7 | 5 5 5 4 4 4 5 | 8 | 5 5 4 4 4 4 4 | 9 | 3 4 4 3 4 4 4 | 10 | 5 5 4 5 5 4 5 | 11 | 4 4 4 4 5 4 4 | 12 | 5 5 4 4 4 5 4 | 13 | 4 4 4 4 4 4 4 | 14 | 4 4 4 4 4 4 4 | 15 | 5 5 5 4 5 5 5 | 16 | 6 7 6 5 5 5 6 | 17 | 5 5 5 5 5 5 5 | 18 | 4 4 4 4 5 5 5 | 19 | 5 6 6 6 6 5 5 | 20 | 4 4 5 4 5 5 5 | 21 | 4 4 4 4 4 4 5 | 22 | 4 4 4 4 4 4 4 | 23 | 4 5 5 5 6 5 5 | 24 | 4 3 3 3 4 4 4 | 25 | 8 8 8 9 9 8 8 | 26 | 3 3 3 3 4 4 4 | 27 | 4 4 4 3 4 4 4 | 28 | 4 5 5 5 5 5 5 | 29 | 5 5 4 5 5 5 5 | 30 | 6 6 5 5 6 7 8 | 31 | 4 4 4 4 5 4 4 | 32 | 6 6 5 5 6 5 5 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1564.0 GPS week: 1564 Day: 0 MJD: 55192.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 237| 1 0 3 38 -80 3 -.14 9 8 | -125 -160 21 55 | 17 -1 | emr 104| 1 0 6 -106 -56 -18 .48 19 19 | 2674 372 51 135 | 45 -2 | esa 138| 0 0 -2 -86 13 -9 .27 8 8 | 866 -1043 23 115 | -28 25 | gfz 192| 0 -2 -6 -10 -91 4 -.09 9 9 | 996 -256 47 204 | -21 -31 | grg 106| -1 0 4 -33 -184 -28 1.09 26 21 | -12 -7 62 205 | 56 32 | igr n/a| 0 0 0 17 -68 -95 .00 5 5 | 7138 343 25 78 | -18 -12 | jpl 125| -1 1 9 -24 5 -46 .59 16 15 | 4785 567 35 95 | 44 -31 | mit 264| -1 0 -4 73 -115 -2 -.34 12 11 | -16537 4129 30 109 | -10 20 | ngs 212| 0 1 -3 86 304 -21 -.21 9 7 | 10363 5380 2376 3852 | 16 -3 | sio 255| -2 0 10 -52 -131 68 -.14 19 18 | --- --- --- --- | -17 39 | Table 2.1564.1 GPS week: 1564 Day: 1 MJD: 55193.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 237| 0 1 2 39 -64 -56 -.18 8 7 | -897 404 15 66 | 17 6 | emr 104| 0 0 4 -57 -37 -6 .44 18 18 | 2692 -1093 17 88 | 8 -33 | esa 138| 1 0 -3 -47 -13 -29 .28 9 8 | -778 450 17 112 | -37 13 | gfz 192| 0 -1 -7 -45 -51 20 -.07 11 11 | -657 1777 31 117 | -3 -58 | grg 106| -1 1 0 -50 -214 -43 1.06 27 23 | -77 -639 51 246 | 48 79 | igr n/a| 0 0 -3 18 -83 -50 .05 6 6 | 7093 -1146 17 69 | -20 -18 | jpl 125| 0 -1 9 0 3 26 .61 16 15 | 5008 -1213 18 95 | 21 -16 | mit 264| -3 0 -4 28 -120 6 -.34 12 11 | -15081 -1564 15 122 | -8 34 | ngs 212| 0 0 -2 85 320 14 -.15 9 7 | 15121 -3623 2266 3090 | 14 1 | sio 255| -3 0 11 -95 -148 76 -.19 19 16 | --- --- --- --- | -13 54 | Table 2.1564.2 GPS week: 1564 Day: 2 MJD: 55194.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 237| 1 0 2 32 -58 22 -.16 7 7 | -305 290 21 70 | 9 -1 | emr 104| -1 0 6 -46 -43 -9 .52 18 18 | 2081 -71 19 86 | -4 -30 | esa 138| 1 1 -5 -76 66 -42 .32 8 8 | -640 1817 19 125 | -7 -6 | gfz 192| 0 -1 -4 -12 -48 8 -.10 9 9 | -57 563 37 143 | -9 -55 | grg 106| -1 1 0 -33 -209 -6 1.11 27 22 | 183 -117 55 241 | 23 129 | igr n/a| 0 0 -3 1 -84 -32 .06 5 5 | 6472 -36 19 73 | -75 -15 | jpl 125| 0 -1 12 -23 4 -46 .61 17 16 | 4279 124 18 86 | 17 -4 | mit 264| -2 0 -3 54 -121 15 -.33 11 10 | -14878 -80 24 144 | -12 22 | ngs 212| 0 0 -4 77 296 -30 -.15 11 9 | 12812 2813 1958 3638 | 55 2 | sio 255| -1 0 9 -65 -139 70 -.18 17 16 | --- --- --- --- | -34 58 | Table 2.1564.3 GPS week: 1564 Day: 3 MJD: 55195.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 237| 0 0 2 18 -89 0 -.15 7 7 | -473 -137 16 75 | 6 11 | emr 104| 5 -2 3 -34 -79 -8 .50 17 17 | 1683 -3018 20 83 | -17 5 | esa 138| 0 0 -1 -67 69 16 .25 8 9 | -3328 5951 19 126 | -59 1 | gfz 192| -1 0 -4 0 -40 -2 -.13 8 8 | -69 44 30 124 | 5 -40 | grg 106| -2 1 0 -59 -222 -15 1.11 27 23 | 360 -580 58 221 | 66 113 | igr n/a| 0 0 -3 -28 -73 -49 .02 5 5 | 6138 -2889 19 60 | -25 -8 | jpl 125| 1 -2 7 0 -3 -18 .59 15 14 | 4129 -2710 19 98 | 6 -11 | mit 264| -2 0 -2 2 -135 8 -.31 12 12 | -15190 -365 20 137 | 8 12 | ngs 212| 0 0 -4 95 302 -45 -.16 9 7 | 563 -809 5067 84721 | -13 -6 | sio 255| 0 1 10 -112 -170 77 -.17 17 18 | --- --- --- --- | -5 65 | Table 2.1564.4 GPS week: 1564 Day: 4 MJD: 55196.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 237| 0 0 1 37 -94 -23 -.21 7 7 | -760 1104 15 80 | 40 18 | emr 104| 0 -1 5 -70 -72 -30 .49 19 19 | -1347 -125 18 95 | 1 -10 | esa 138| 0 0 -2 -85 57 -11 .26 9 9 | -940 2399 21 125 | -17 38 | gfz 192| 0 -1 -6 -6 -47 -1 -.14 11 11 | 193 -2001 32 152 | -21 -39 | grg 106| -3 0 1 -38 -192 -9 1.20 27 24 | -466 1506 59 214 | 44 137 | igr n/a| 0 0 -3 -10 -94 -64 .01 4 4 | 3315 173 23 67 | -62 -4 | jpl 125| 2 0 9 -48 8 58 .60 18 18 | 1574 350 20 117 | -16 -9 | mit 264| -1 0 -2 31 -113 0 -.29 13 12 | -14987 1133 19 118 | -19 7 | ngs 212| 0 1 -3 95 328 13 -.10 11 8 | 12333 4619 2437 4521 | 0 -83 | sio 255| 0 0 11 -79 -141 69 -.20 19 19 | --- --- --- --- | -19 49 | Table 2.1564.5 GPS week: 1564 Day: 5 MJD: 55197.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 237| 0 1 2 61 -114 -26 -.15 7 7 | -124 -80 12 50 | -29 17 | emr 104| 0 -2 7 -41 -50 -7 .56 19 19 | -3275 -40 19 70 | 1 -35 | esa 138| 1 -1 -4 -69 28 34 .25 9 8 | -754 251 19 127 | -30 35 | gfz 192| 0 -1 -3 -131 -90 21 -.12 9 9 | 372 -1012 36 144 | -47 -7 | grg 106| -4 -1 0 -11 -229 -27 1.13 28 22 | -92 -107 60 265 | 23 146 | igr n/a| 0 0 -2 31 -95 -23 .04 5 5 | 1618 32 23 70 | -12 -6 | jpl 125| 0 -1 9 14 -14 3 .63 17 16 | -67 124 18 84 | 8 -53 | mit 264| -2 2 -1 -40 -110 -19 -.29 13 11 | -15916 29 20 103 | 1 5 | ngs 212| 0 1 -3 161 297 -15 -.16 8 6 | -212 144 2064 3906 | -17 -5 | sio 255| -1 1 12 -142 -128 46 -.13 20 20 | --- --- --- --- | -1 21 | Table 2.1564.6 GPS week: 1564 Day: 6 MJD: 55198.000 CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps] --------+----------------------------------------------------+------------------------------ cod 237| 0 0 1 33 -105 1 -.19 8 8 | -80 -369 17 59 | 50 40 | emr 104| 1 -1 9 -38 -103 -20 .51 18 18 | -3377 1072 18 80 | -3 51 | esa 138| 2 -1 -4 -66 39 0 .25 8 8 | -813 1000 18 122 | -30 10 | gfz 192| 0 0 -5 -9 -30 14 -.17 8 8 | 178 2411 34 132 | -29 -14 | grg 106| -3 0 2 -91 -247 13 1.13 29 23 | -32 163 58 237 | 131 172 | igr n/a| -1 1 1 7 -98 -30 .00 6 6 | 1533 1193 19 64 | -22 7 | jpl 125| 0 0 12 -27 -15 10 .56 17 15 | -149 1016 17 100 | 69 21 | mit 264| -3 1 -2 47 -53 -17 -.30 15 12 | -15468 393 20 99 | -6 11 | ngs 212| 0 0 -3 67 275 -13 -.17 10 9 | 11672 1989 1973 3901 | -44 -16 | sio 255| -2 3 10 -71 -89 27 -.10 21 17 | --- --- --- --- | 3 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 3.1564.0 GPS week: 1564 Day: 0 MJD: 55192.000 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 | 19 --- --- --- --- 24 --- 21 17 --- 13 | 21 --- --- --- --- 25 --- 24 27 --- 22 2 | 7 15 6 8 36 6 16 14 10 26 4 | 31 38 36 34 47 32 41 30 32 34 32 3 | 7 16 5 6 35 5 11 10 11 18 3 | 21 23 26 22 29 21 23 21 26 23 21 4 | 6 10 8 7 17 5 10 16 11 30 4 | 27 27 31 31 33 30 26 26 31 27 26 5 | 7 21 7 9 32 4 15 17 7 15 4 | 22 37 25 17 45 23 32 22 25 25 22 6 | 6 17 6 7 25 4 10 10 10 19 3 | 29 25 31 30 30 27 28 30 29 29 28 7 | 7 21 9 9 27 4 18 10 7 21 4 | 21 31 25 21 35 22 29 21 26 27 22 8 | 8 15 10 8 17 5 11 16 9 22 4 | 15 22 16 13 21 13 18 21 17 24 14 9 | 8 15 6 6 19 4 12 10 6 12 3 | 17 22 20 11 24 14 22 15 19 13 16 10 | 12 15 8 8 30 5 14 15 10 20 4 | 15 23 20 17 27 15 22 22 23 24 16 11 | 7 16 8 6 20 6 13 7 10 24 4 | 46 52 50 48 56 47 50 48 45 39 45 12E | 12 23 7 12 23 5 21 11 9 14 5 | 12 25 16 15 27 11 22 13 17 18 13 13 | 8 17 6 9 26 6 16 10 10 12 4 | 11 24 18 13 39 13 22 14 22 15 14 14 | 8 23 7 8 27 5 16 6 7 16 4 | 11 26 18 13 33 12 21 12 16 14 13 15 | 7 22 9 8 26 4 19 15 9 13 4 | 14 25 23 13 41 14 23 15 20 16 15 16E | 8 36 11 12 54 5 23 14 9 14 5 | 17 36 21 23 45 18 30 20 26 21 20 17 | 8 18 7 8 22 5 19 7 9 23 4 | 24 26 25 24 31 22 26 25 29 24 24 18 | 6 23 9 9 20 5 19 10 6 12 4 | 18 31 18 15 29 17 30 17 26 21 20 19 | 8 18 7 8 21 5 17 18 12 24 5 | 21 31 24 19 37 18 32 21 22 20 18 20 | 8 21 7 6 22 6 14 10 8 14 3 | 15 31 18 17 33 18 26 20 22 27 18 21 | 6 15 5 8 19 4 12 9 5 20 3 | 22 27 24 26 29 23 28 22 26 21 23 22 | 6 13 8 9 29 6 15 10 6 10 3 | 12 18 14 11 32 12 21 15 18 16 14 23 | 9 22 8 11 21 7 15 9 8 12 4 | 10 25 19 13 33 12 22 14 23 18 14 X24 | 6 13 7 --- 18 4 7 8 5 --- 3 | 30 33 37 --- 37 34 33 31 34 --- 32 X25 | 11 14 11 --- --- 13 --- 17 --- --- 7 | 18 25 25 --- --- 20 --- 20 --- --- 20 26 | 8 12 7 8 19 4 11 6 8 12 3 | 13 17 15 14 22 11 21 14 19 15 14 27 | 7 16 4 8 18 4 10 11 7 12 3 | 14 23 18 12 29 12 21 15 18 15 15 28E | 8 16 9 7 17 4 16 13 9 19 4 | 17 27 25 22 35 20 27 20 27 20 20 29 | 10 19 6 7 28 5 18 12 9 23 4 | 19 27 23 24 31 20 28 21 20 16 20 30E | 11 20 11 10 21 6 15 18 11 26 5 | 36 32 33 35 23 31 28 37 38 24 32 31 | 7 17 8 9 33 5 16 8 10 18 4 | 18 25 18 21 38 16 25 19 22 21 18 32 | 18 26 9 16 21 7 17 15 8 26 6 | 72 78 73 75 78 67 75 67 65 81 69 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 8 9 26 5 15 12 9 19 |T 21 29 25 22 34 21 28 22 26 23 22 WRMS | 8 19 8 9 21 5 15 11 7 18 |NE 21 29 25 22 35 21 28 22 25 24 22 MEDI | 8 17 7 8 22 5 15 10 9 18 |MD 18 26 23 19 33 18 26 21 25 21 20 Table 3.1564.1 GPS week: 1564 Day: 1 MJD: 55193.000 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 | 20 --- --- --- --- 29 --- 14 20 --- 13 | 19 --- --- --- --- 50 --- 32 44 --- 30 2 | 8 12 9 13 39 4 15 13 11 26 4 | 22 31 30 33 42 27 34 24 26 26 25 3 | 7 18 8 8 28 5 12 17 11 16 4 | 19 28 23 23 31 24 29 32 27 29 22 4 | 5 12 11 10 24 5 11 14 10 27 4 | 20 26 28 30 31 27 26 22 30 24 23 5 | 7 22 8 12 32 7 17 15 8 15 4 | 20 35 23 22 44 22 33 24 24 24 21 6 | 6 21 6 11 28 6 11 12 10 17 4 | 21 29 23 24 33 24 29 31 28 31 23 7 | 5 19 10 13 27 6 20 10 9 21 4 | 17 27 20 23 38 19 28 17 23 18 17 8 | 6 15 11 9 21 7 14 17 11 20 4 | 13 18 17 17 26 14 20 19 24 18 13 9 | 9 15 8 8 18 5 11 10 7 14 3 | 17 24 20 18 30 17 25 16 21 18 17 10 | 11 17 7 10 30 6 14 15 10 22 4 | 16 27 19 19 31 18 27 25 26 27 18 11 | 5 15 4 9 17 6 12 11 8 22 3 | 26 42 29 32 45 31 42 28 33 26 29 12E | 8 23 9 6 23 4 23 9 9 13 4 | 9 25 19 17 27 15 26 16 19 18 16 13 | 5 18 9 10 32 5 16 10 8 13 4 | 13 26 17 18 46 16 25 16 20 14 14 14 | 9 19 8 9 25 4 17 7 6 15 4 | 12 22 15 16 33 14 25 16 20 16 15 15 | 7 20 9 7 30 7 18 14 10 12 4 | 18 26 23 20 46 19 27 18 25 18 18 16E | 8 30 8 26 59 7 24 14 11 19 6 | 23 41 27 34 50 27 38 27 35 31 27 17 | 8 17 12 10 23 5 18 8 7 22 4 | 17 26 26 22 29 20 26 22 24 21 20 18 | 5 18 6 11 25 6 19 8 8 12 4 | 15 26 17 15 31 16 27 16 23 17 17 19 | 8 22 10 9 23 3 21 24 14 27 6 | 19 34 26 21 37 24 36 25 32 25 22 20 | 5 19 7 10 20 5 12 11 9 13 3 | 12 28 16 18 32 15 23 16 17 21 15 21 | 5 14 6 9 20 9 15 7 8 20 3 | 15 24 20 17 26 16 26 15 20 14 16 22 | 6 13 5 10 31 8 16 9 7 9 3 | 13 21 14 17 35 15 23 16 21 16 15 23 | 8 22 11 14 26 7 16 12 8 12 4 | 13 31 21 19 39 17 27 14 22 17 16 24 | 5 12 5 5 18 5 7 9 7 19 3 | 23 28 30 31 34 27 30 24 31 23 26 X25 | 9 16 13 --- --- 11 --- 16 --- --- 7 | 18 23 19 --- --- 17 --- 18 --- --- 16 26 | 7 13 9 10 20 5 12 5 6 12 3 | 11 19 15 16 24 13 23 15 20 15 14 27 | 8 17 9 9 19 4 10 11 6 15 3 | 18 28 23 22 32 20 27 19 24 20 20 28E | 7 18 10 13 22 5 15 14 8 20 4 | 22 31 29 29 34 26 31 29 33 29 27 29 | 8 18 8 9 25 7 21 13 11 24 5 | 15 24 18 18 30 14 29 15 19 15 16 30E | 11 21 8 12 15 7 19 16 14 24 5 | 30 31 26 31 18 28 25 32 35 19 27 31 | 7 16 9 8 31 6 16 5 9 15 3 | 16 25 19 18 37 18 30 19 23 19 18 32 | 14 24 11 13 23 7 20 11 10 27 5 | 29 37 29 32 36 30 40 27 27 37 28 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 9 11 27 6 16 12 9 19 |T 17 27 21 22 34 21 28 21 25 21 20 WRMS | 7 18 8 11 23 6 15 11 7 16 |NE 17 27 21 21 34 19 28 20 24 21 19 MEDI | 7 18 9 10 24 6 16 11 9 17 |MD 17 27 21 20 33 19 27 19 24 19 18 Table 3.1564.2 GPS week: 1564 Day: 2 MJD: 55194.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 18 --- --- --- --- 45 --- 16 37 --- 17 | 38 --- --- --- --- 54 --- 41 52 --- 39 2 | 7 13 5 8 37 4 14 9 12 24 4 | 21 27 25 25 37 23 29 21 21 24 22 3 | 7 17 6 7 29 6 13 10 13 14 4 | 15 19 20 19 30 15 20 22 20 19 17 4 | 5 10 9 8 25 6 10 10 11 20 3 | 19 22 27 22 33 23 21 21 28 18 21 5 | 7 21 6 8 37 6 19 11 8 15 4 | 18 32 18 18 39 16 32 19 22 21 18 6 | 6 16 6 7 25 4 11 9 14 14 3 | 21 19 20 22 29 19 20 24 25 22 20 7 | 8 19 11 8 26 5 19 10 10 17 4 | 16 26 21 20 37 17 26 16 20 15 16 8 | 4 14 9 8 20 5 14 11 11 15 4 | 12 17 10 13 22 10 17 14 17 16 10 9 | 7 14 8 8 16 2 10 8 7 13 3 | 13 21 16 11 28 13 21 12 18 13 12 10 | 10 14 6 10 33 6 14 12 11 17 4 | 11 20 14 16 21 12 20 22 20 22 14 11 | 6 15 6 7 19 3 14 9 12 22 4 | 35 43 39 38 50 36 43 36 39 33 36 12E | 8 21 8 8 18 3 22 9 7 11 4 | 11 27 17 15 25 15 24 16 17 17 13 13 | 7 19 9 7 31 7 17 9 8 9 3 | 12 25 15 16 44 14 23 12 15 11 11 14 | 10 20 7 6 26 4 16 7 9 14 4 | 14 22 15 11 34 13 22 13 20 13 13 15 | 6 22 8 7 27 3 17 15 14 13 4 | 10 22 17 12 40 11 20 15 18 12 11 16E | 8 27 9 22 56 5 24 15 11 15 6 | 19 34 23 29 51 21 32 23 25 25 22 17 | 7 15 11 10 23 3 19 8 13 22 4 | 21 24 22 19 32 22 24 24 27 20 20 18 | 6 22 6 8 28 4 21 7 10 12 4 | 14 31 15 13 32 13 29 16 25 18 17 19 | 9 23 9 8 23 3 23 21 11 26 6 | 15 29 21 18 33 17 31 23 20 21 16 20 | 5 22 9 12 21 6 13 14 10 13 4 | 11 29 16 19 33 14 22 20 17 21 13 21 | 7 12 10 10 21 6 17 6 10 21 4 | 16 23 23 17 28 16 26 15 25 13 17 22 | 7 18 4 6 30 6 19 8 8 10 3 | 14 26 15 14 38 13 26 14 24 15 16 23 | 7 24 9 10 27 8 18 14 9 12 4 | 10 26 17 14 36 12 23 12 17 15 11 24 | 5 12 6 8 20 2 8 8 8 18 3 | 27 30 33 20 37 29 29 25 30 15 27 X25 | 11 16 13 --- --- 10 --- 13 --- --- 7 | 19 21 21 --- --- 16 --- 17 --- --- 15 26 | 7 12 6 6 17 3 12 6 8 12 3 | 10 17 14 13 24 12 21 13 21 13 13 27 | 7 15 9 8 20 3 9 7 8 13 3 | 12 21 14 12 28 12 19 9 18 11 12 28E | 6 15 10 8 21 3 17 14 16 17 4 | 16 23 19 18 32 19 22 21 23 21 17 29 | 6 15 6 11 24 4 18 9 9 22 4 | 16 23 18 20 31 16 26 15 19 13 16 30E | 11 22 9 12 18 5 19 11 13 24 5 | 32 29 28 35 20 28 23 32 36 22 29 31 | 5 17 8 9 30 6 18 8 8 16 4 | 12 23 16 15 36 13 25 14 21 14 14 32 | 10 23 11 11 24 5 19 11 11 25 5 | 15 25 22 22 29 16 28 19 21 29 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 18 8 9 27 5 17 11 11 17 |T 17 25 19 18 32 18 24 19 23 18 17 WRMS | 7 18 8 9 22 5 16 10 9 16 |NE 15 24 19 17 33 16 24 17 21 17 16 MEDI | 7 17 8 8 24 5 17 9 10 15 |MD 15 24 18 18 32 16 23 17 21 17 16 Table 3.1564.3 GPS week: 1564 Day: 3 MJD: 55195.000 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 30 --- --- --- 22 --- 15 22 --- 11 | 58 30 --- --- --- 56 --- 50 49 --- 53 2 | 6 13 5 5 42 4 12 10 8 24 3 | 30 35 36 31 43 32 37 33 34 35 32 3 | 6 11 8 6 27 4 12 11 10 18 3 | 23 22 22 26 31 22 24 21 31 21 23 4 | 6 12 7 7 20 5 8 12 10 19 3 | 25 29 29 28 32 26 25 24 25 24 24 5 | 6 17 12 10 35 5 15 12 11 15 4 | 28 33 29 28 43 26 35 27 32 30 27 6 | 6 12 8 7 21 3 11 10 9 18 3 | 26 24 23 27 30 25 26 26 34 24 26 7 | 6 18 9 9 26 4 16 12 9 15 4 | 17 29 21 21 36 18 28 23 22 18 19 8 | 5 13 8 6 18 5 13 12 10 14 3 | 12 20 12 15 23 12 20 18 18 17 12 9 | 8 14 4 8 18 3 11 7 5 14 3 | 18 25 23 18 30 17 24 17 23 18 19 10 | 12 23 11 8 34 6 18 15 11 15 5 | 17 28 18 22 30 20 26 24 25 25 18 11 | 4 15 7 5 19 5 13 14 9 23 4 | 40 48 41 43 51 43 45 42 41 38 40 12E | 6 21 8 9 22 4 20 11 8 11 4 | 14 26 21 19 32 16 24 18 19 19 16 13 | 6 20 11 7 25 6 17 10 5 11 4 | 16 30 21 19 41 16 27 17 21 17 17 14 | 8 18 7 7 25 3 16 10 6 14 3 | 16 25 21 19 32 17 26 16 24 17 19 15 | 9 18 11 8 25 4 14 14 8 14 4 | 21 26 21 20 43 18 25 20 24 19 19 16E | 6 25 10 12 43 5 23 14 10 15 5 | 18 28 23 25 38 19 29 20 27 19 22 17 | 7 18 8 11 23 5 19 8 12 24 4 | 22 26 25 25 31 22 26 24 24 22 22 18 | 5 18 7 8 21 3 16 11 8 15 4 | 19 29 22 19 35 18 28 24 23 25 21 19 | 9 19 8 6 26 4 20 23 12 24 5 | 21 31 22 22 39 22 33 27 29 24 22 20 | 7 19 9 6 24 5 13 16 6 15 4 | 18 31 20 21 38 18 25 22 20 27 18 21 | 5 13 7 8 19 3 13 7 8 23 3 | 22 28 25 26 28 23 29 23 29 21 24 22 | 6 13 7 7 32 4 16 9 8 12 3 | 20 23 20 22 40 20 26 20 24 22 21 23 | 8 24 11 10 21 6 15 18 7 16 5 | 16 31 20 19 37 16 26 18 22 20 16 24 | 5 12 6 8 20 2 6 10 6 17 3 | 26 30 33 28 35 30 32 27 34 18 29 X25 | 9 18 15 --- --- 8 --- 22 --- --- 9 | 17 26 22 --- --- 15 --- 20 --- --- 18 26 | 6 15 8 6 16 3 12 7 8 12 3 | 14 24 21 17 24 15 23 18 24 19 18 27 | 7 15 6 8 19 3 11 7 8 14 3 | 19 27 25 21 32 21 26 19 27 21 21 28E | 6 14 8 11 52 4 17 14 12 16 4 | 21 28 21 19 46 21 29 22 26 24 21 29 | 8 17 10 9 24 5 17 11 9 22 4 | 17 27 23 20 31 18 27 17 19 11 18 30E | 9 21 9 9 21 6 19 11 11 22 5 | 34 31 31 35 21 30 28 38 35 28 31 31 | 7 18 9 7 32 6 15 11 12 15 4 | 20 28 20 20 36 18 29 21 23 19 20 32 | 10 25 12 9 16 8 19 9 10 23 5 | 25 33 23 27 34 25 34 24 29 35 25 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 17 8 8 27 5 15 12 9 17 |T 22 28 23 23 34 22 28 23 27 22 22 WRMS | 7 17 9 8 23 5 14 12 7 18 |NE 20 28 23 23 34 21 28 22 26 22 21 MEDI | 6 18 8 8 23 4 15 11 9 15 |MD 20 28 22 21 34 20 26 22 25 21 21 Table 3.1564.4 GPS week: 1564 Day: 4 MJD: 55196.000 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 | 9 24 --- --- --- 13 --- 14 15 --- 8 | 36 25 --- --- --- 31 --- 41 33 --- 38 2 | 8 14 6 13 40 4 17 11 9 26 4 | 25 34 32 32 47 30 35 31 30 32 29 3 | 8 16 9 10 26 5 15 7 10 21 4 | 21 24 21 19 28 19 23 17 25 21 20 4 | 7 12 11 10 25 3 12 13 10 16 4 | 22 27 26 31 36 26 24 23 28 22 24 5 | 7 17 10 12 42 4 15 8 13 13 4 | 22 34 27 20 53 24 31 23 27 26 23 6 | 7 15 9 11 20 6 13 14 12 23 4 | 27 27 27 25 31 25 24 27 26 26 25 7 | 6 21 8 9 25 3 20 9 9 17 4 | 15 26 19 17 34 16 26 19 19 13 16 8 | 5 14 5 8 21 4 13 12 9 13 3 | 14 18 11 17 23 13 18 16 15 12 11 9 | 9 18 6 8 15 3 15 9 8 15 3 | 20 26 22 17 29 19 23 18 18 19 17 10 | 10 20 8 9 38 3 17 12 13 14 4 | 16 28 20 19 37 19 23 22 23 24 17 11 | 6 17 8 6 24 4 19 14 10 25 4 | 33 45 40 35 48 35 43 37 37 34 35 12E | 6 19 6 11 18 6 24 10 11 10 4 | 12 23 17 16 24 16 22 15 14 17 12 13 | 6 18 10 12 24 4 18 11 7 14 4 | 13 26 18 19 41 14 25 14 12 14 13 14 | 8 17 6 10 20 4 20 13 6 13 4 | 22 28 24 24 36 24 31 22 22 20 22 15 | 7 21 9 9 24 3 19 12 10 15 4 | 18 27 29 26 41 23 25 18 22 19 21 16E | 5 23 9 14 51 6 25 15 11 18 5 | 13 25 18 15 41 15 25 15 19 18 14 17 | 7 20 7 12 23 4 22 9 17 24 5 | 21 24 20 23 30 21 27 21 25 20 20 18 | 7 21 10 9 22 4 20 15 7 17 4 | 17 30 21 18 35 17 29 26 21 26 21 19 | 8 23 9 10 27 4 24 19 11 26 5 | 20 34 28 21 36 18 34 16 24 15 20 20 | 5 23 11 12 24 5 20 17 7 19 5 | 14 32 21 20 34 15 25 18 17 22 16 21 | 5 14 8 9 19 4 16 10 8 25 4 | 21 28 25 24 29 22 28 24 25 19 23 22 | 6 17 10 7 33 5 16 9 6 12 3 | 18 23 18 17 40 16 25 18 23 19 19 23 | 7 26 11 14 22 6 17 20 12 20 5 | 16 33 24 18 34 16 23 17 15 17 15 24 | 6 13 7 7 18 5 9 12 9 16 3 | 25 28 31 26 33 28 27 26 27 20 26 X25 | 12 20 17 --- --- 8 --- 17 --- --- 9 | 16 20 22 --- --- 13 --- 16 --- --- 13 26 | 6 16 6 12 18 5 14 10 8 12 3 | 14 21 18 21 23 13 22 17 17 14 16 27 | 9 20 7 9 16 3 13 10 10 14 4 | 20 28 23 21 32 20 22 20 21 20 19 28E | 7 12 7 14 28 3 21 13 11 17 4 | 17 27 22 26 32 17 25 17 24 18 19 29 | 9 17 9 9 26 3 22 9 11 22 4 | 15 23 20 19 30 17 24 14 20 14 15 30E | 11 22 11 11 21 6 20 16 14 24 5 | 34 32 32 34 19 32 28 43 38 27 31 31 | 8 19 13 13 31 4 23 16 10 19 5 | 14 24 19 20 35 15 29 22 22 21 16 32 | 8 25 9 14 17 4 22 13 14 24 5 | 21 34 26 26 34 21 32 17 30 32 23 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 19 9 11 27 4 18 13 11 19 |T 19 27 23 22 34 20 26 21 23 20 20 WRMS | 7 19 9 11 24 4 18 12 8 19 |NE 19 27 23 22 34 19 26 20 22 20 19 MEDI | 7 18 9 10 24 4 18 12 10 17 |MD 18 27 22 20 34 19 25 18 23 20 19 Table 3.1564.5 GPS week: 1564 Day: 5 MJD: 55197.000 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 | 12 18 --- --- --- 21 --- 17 --- 16 8 | 45 22 --- --- --- 41 --- 47 --- 16 45 2 | 5 16 8 10 41 4 16 12 5 25 4 | 21 28 25 24 40 23 28 24 25 27 23 3 | 8 16 10 9 36 3 12 17 6 38 5 | 21 25 23 16 32 19 22 21 25 30 21 4 | 7 16 9 8 22 5 10 12 5 14 3 | 19 25 20 22 30 21 20 18 24 18 19 5 | 7 18 7 6 41 5 16 7 4 12 3 | 21 30 22 20 40 19 28 21 21 23 20 6 | 6 14 11 9 31 3 10 15 7 33 4 | 26 28 28 20 28 25 25 28 29 35 27 7 | 7 20 8 10 25 5 19 8 7 20 4 | 18 29 20 20 36 17 29 20 23 14 18 8 | 6 15 5 11 19 4 13 8 9 14 3 | 14 20 14 19 26 15 21 15 21 13 13 9 | 7 18 5 7 15 4 12 11 7 13 3 | 17 27 18 15 31 18 23 19 22 17 17 10 | 10 23 4 7 38 4 15 11 5 13 4 | 15 26 18 18 27 17 21 24 20 25 16 11 | 4 15 7 6 20 4 14 9 9 28 4 | 30 43 33 31 47 31 39 29 35 29 31 12E | 8 24 9 11 22 6 24 11 8 11 4 | 11 25 17 16 27 11 23 15 18 16 12 13 | 5 17 8 12 29 6 16 10 9 15 4 | 14 25 15 17 43 14 25 12 20 13 14 14 | 6 24 9 9 27 3 17 11 6 13 4 | 16 27 18 20 35 19 24 18 25 20 19 15 | 7 22 12 6 26 4 19 11 9 18 4 | 20 31 23 20 43 21 29 19 25 23 20 16E | 6 24 8 13 56 5 24 13 8 21 5 | 20 30 22 18 45 21 28 22 30 29 22 17 | 9 19 8 10 24 4 21 8 7 23 4 | 19 24 17 16 27 18 22 18 26 16 17 18 | 7 21 7 7 24 5 18 18 6 18 4 | 19 28 20 17 35 19 27 31 32 26 24 19 | 6 21 10 7 23 4 23 8 7 27 4 | 21 31 25 15 35 20 33 15 25 19 21 20 | 7 24 11 9 25 6 17 13 7 17 4 | 16 33 16 13 36 18 27 21 27 23 19 21 | 6 15 7 12 20 4 14 13 8 26 4 | 17 23 21 21 26 19 25 23 26 19 20 22 | 7 16 11 8 29 4 18 10 6 14 4 | 20 21 21 19 37 20 26 24 30 23 23 23 | 9 23 11 11 24 8 19 18 9 18 5 | 15 30 21 12 36 16 24 17 23 15 16 24 | 6 14 8 10 18 7 6 12 10 15 3 | 23 29 30 17 34 28 29 25 31 19 26 X25 | 10 19 9 --- --- 16 --- 17 --- --- 7 | 15 23 17 --- --- 17 --- 16 --- --- 14 26 | 7 16 7 9 15 4 12 13 7 21 4 | 14 20 20 18 26 15 20 21 27 20 19 27 | 6 19 5 7 16 4 10 11 8 13 3 | 19 31 23 18 34 21 26 23 26 21 21 28E | 6 14 8 12 24 4 18 15 9 19 4 | 21 29 26 25 32 25 28 24 28 24 23 X29 | 7 20 13 --- 29 4 18 9 8 --- 5 | 13 23 19 --- 29 12 22 12 17 --- 14 30E | 12 26 14 8 27 8 20 24 15 22 6 | 34 33 31 36 29 31 28 51 38 27 32 31 | 5 22 8 9 36 8 20 12 9 16 4 | 19 28 19 18 40 20 28 23 27 20 21 32 | 10 22 11 9 20 6 20 8 8 24 4 | 21 31 26 25 32 25 31 24 36 32 25 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 19 9 9 28 5 17 13 8 20 |T 19 27 21 19 33 20 26 22 26 21 21 WRMS | 7 19 8 9 22 5 16 11 6 20 |NE 18 27 21 18 34 19 25 20 25 21 19 MEDI | 7 19 8 9 24 4 17 11 7 18 |MD 19 28 21 18 34 19 26 21 25 20 20 Table 3.1564.6 GPS week: 1564 Day: 6 MJD: 55198.000 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 | 9 19 --- --- --- 22 --- 17 16 14 7 | 39 20 --- --- --- 32 --- 47 51 16 42 2 | 8 14 7 8 39 7 14 11 12 24 4 | 37 38 35 34 45 35 40 37 37 39 35 3 | 11 12 8 7 33 7 13 27 12 42 6 | 22 21 24 22 27 21 22 29 22 36 22 4 | 8 14 6 8 25 6 10 13 7 18 3 | 29 30 30 30 35 29 26 27 30 22 27 5 | 6 19 6 7 43 4 19 9 10 12 4 | 26 35 25 22 41 25 35 26 27 29 25 6 | 7 12 7 10 27 6 12 24 12 39 5 | 31 30 32 34 31 33 28 35 33 37 31 7 | 10 19 10 8 28 4 19 10 10 23 4 | 18 31 26 23 41 21 30 19 20 22 19 8 | 7 16 6 6 28 6 12 8 12 15 3 | 16 24 20 19 31 15 23 17 15 22 15 9 | 7 19 5 7 18 5 11 13 8 13 3 | 16 25 16 16 26 13 21 14 17 11 14 10 | 11 25 7 8 40 3 15 11 8 16 4 | 14 30 16 18 23 15 20 22 19 26 15 11 | 5 12 7 7 22 5 12 8 10 29 4 | 48 56 53 52 60 49 54 51 50 42 50 12E | 7 22 6 7 19 5 22 10 8 13 4 | 10 22 14 12 27 11 20 12 15 16 10 13 | 6 17 8 5 32 8 16 10 11 15 4 | 16 28 20 18 46 16 24 15 19 19 16 14 | 8 19 6 5 25 2 13 9 8 12 3 | 19 27 21 21 37 18 25 21 23 22 21 15 | 8 21 6 12 28 6 17 9 14 17 4 | 19 26 19 20 41 17 24 16 19 17 17 16E | 8 16 10 13 47 4 24 17 10 23 5 | 17 26 21 19 44 18 27 20 22 22 18 17 | 11 18 8 10 27 7 22 8 10 25 5 | 26 27 23 24 30 24 28 26 26 26 22 18 | 8 19 7 8 30 5 18 16 8 18 4 | 20 33 21 22 37 21 34 32 26 33 25 19 | 5 17 9 6 29 6 19 9 11 26 4 | 16 28 22 16 33 19 30 16 17 19 17 20 | 6 21 7 9 25 6 18 14 8 20 4 | 15 33 16 15 34 14 29 19 18 24 16 21 | 6 12 8 7 23 6 13 16 7 29 4 | 26 31 29 31 36 27 32 32 28 28 27 22 | 7 15 10 4 35 5 14 12 6 14 3 | 20 26 16 18 39 17 26 28 22 27 20 23 | 10 21 10 6 31 7 19 17 10 16 4 | 15 28 19 11 38 11 23 16 16 13 13 24 | 8 11 7 7 24 4 7 14 11 14 3 | 29 32 34 28 40 32 32 29 31 20 30 X25 | 11 16 8 --- --- 9 --- 19 --- --- 7 | 13 24 21 --- --- 17 --- 19 --- --- 13 26 | 6 14 6 5 18 5 16 10 11 10 3 | 15 22 18 18 28 14 25 21 17 16 17 27 | 6 19 5 8 18 5 11 15 9 12 3 | 15 24 17 17 28 14 20 17 19 14 15 28E | 9 17 10 9 35 7 21 17 12 15 5 | 15 25 22 17 29 17 24 19 21 20 16 X29 | 7 23 7 7 26 6 20 10 9 --- 4 | 19 28 21 21 32 19 27 18 22 --- 18 30E | 14 23 15 13 20 8 21 37 19 20 7 | 35 34 32 37 20 35 29 61 46 33 35 31 | 7 17 6 10 30 7 18 14 8 14 4 | 15 24 15 17 37 13 25 19 18 17 16 32 | 9 20 10 8 19 5 19 11 9 22 4 | 26 32 23 26 31 23 33 29 24 34 24 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 8 8 29 6 17 15 10 21 |T 21 28 23 22 34 21 27 25 24 24 21 WRMS | 8 18 8 8 23 6 15 12 9 17 |NE 21 29 23 22 35 21 28 24 23 24 21 MEDI | 8 17 7 7 27 6 16 12 10 16 |MD 19 28 21 20 34 18 26 21 22 22 18 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 4.1564 GPS week: 1564 MJD: 55192.0-55198.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3059 |U 8 8 18 |U 12 13 36 |U 7 7 12 | emr | emr 3018 | 13 12 29 |U 13 13 42 | 9 9 20 | esa | esa 2976 | 9 9 19 |U 12 12 35 | 8 8 13 | gfz | gfz 2798 |U 17 17 37 |U 16 15 50 | 15 18 31 | grg | grg 2880 | 11 9 26 |U 75 37 109 | 12 13 18 | igr | igr 2977 | 9 9 21 | 12 13 38 | 7 8 13 | igs | igs 2994 | 9 9 21 | 12 13 37 | 7 7 12 | jpl | jpl 2874 |U 9 9 21 |U 12 13 37 |U 8 6 16 | mit | mit 3072 |U 9 8 20 |U 13 13 38 |U 8 8 15 | 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 5.1564.0 GPS week: 1564 Day: 0 MJD: 55192.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3054 | 8 10 20 | 14 13 44 | 6 5 11 | emr | emr 2955 | 10 13 28 | 13 12 48 | 8 7 21 | esa | esa 2976 | 9 10 23 | 14 12 47 | 7 7 13 | gfz | gfz 2734 | 17 25 38 | 16 14 57 | 15 17 32 | grg | grg 2880 | 9 11 19 | 16 15 47 | 10 11 15 | igr | igr 2963 | 13 14 25 | 15 14 58 | 8 10 23 | igs | igs 2993 | 10 13 27 | 15 13 46 | 8 6 12 | jpl | jpl 2876 | 11 12 21 | 14 14 46 | 8 5 14 | mit | mit 3072 | 9 9 24 | 16 12 43 | 8 7 14 | Table 5.1564.1 GPS week: 1564 Day: 1 MJD: 55193.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3059 | 6 7 19 | 11 16 35 | 5 7 13 | emr | emr 2965 | 8 7 22 | 12 14 32 | 7 6 20 | esa | esa 2976 | 6 6 16 | 12 14 28 | 7 7 11 | gfz | gfz 2826 | 9 10 19 | 13 16 30 | 11 11 29 | grg | grg 2880 | 9 8 22 | 14 15 32 | 11 14 20 | igr | igr 2962 | 6 8 19 | 10 13 27 | 6 6 12 | igs | igs 2972 | 6 7 16 | 10 14 29 | 5 6 10 | jpl | jpl 2876 | 8 8 21 | 11 14 33 | 7 5 13 | mit | mit 3072 | 6 9 16 | 11 15 35 | 7 8 11 | Table 5.1564.2 GPS week: 1564 Day: 2 MJD: 55194.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3057 | 9 6 16 | 13 12 35 | 6 7 11 | emr | emr 2965 | 17 14 38 | 14 13 45 | 10 8 17 | esa | esa 2976 | 8 7 17 | 12 12 33 | 8 9 10 | gfz | gfz 2833 | 31 16 83 | 15 22 47 | 14 16 24 | grg | grg 2880 | 16 6 53 | 16 17 43 | 14 14 17 | igr | igr 2965 | 9 7 18 | 12 13 37 | 7 8 8 | igs | igs 3042 | 9 8 19 | 12 12 41 | 7 8 9 | jpl | jpl 2871 | 10 6 22 | 12 13 33 | 9 7 15 | mit | mit 3072 | 12 8 25 | 12 11 51 | 8 10 11 | Table 5.1564.3 GPS week: 1564 Day: 3 MJD: 55195.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3067 | 7 7 15 | 22 18 55 | 8 8 14 | emr | emr 3068 | 9 11 21 | 23 20 65 | 8 8 15 | esa | esa 2976 | 16 9 19 | 22 17 56 | 8 9 15 | gfz | gfz 2825 | 14 15 25 | 23 16 58 | 10 14 26 | grg | grg 2880 | 9 7 17 | 22 16 53 | 10 13 18 | igr | igr 2971 | 7 7 14 | 21 17 53 | 6 6 11 | igs | igs 3063 | 10 8 22 | 22 18 55 | 7 8 12 | jpl | jpl 2873 | 8 8 18 | 21 17 57 | 8 7 17 | mit | mit 3072 | 10 7 20 | 22 19 55 | 7 7 17 | Table 5.1564.4 GPS week: 1564 Day: 4 MJD: 55196.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3064 | 8 11 19 | 7 8 26 | 7 6 13 | emr | emr 3062 | 13 15 29 | 8 7 32 | 12 12 21 | esa | esa 2976 | 10 13 22 | 7 7 26 | 9 10 15 | gfz | gfz 2820 | 14 17 26 | 10 10 34 | 12 17 23 | grg | grg 2880 | 9 11 20 | 10 10 36 | 13 11 17 | igr | igr 2971 | 11 13 28 | 8 9 28 | 9 9 12 | igs | igs 3016 | 8 12 18 | 7 7 26 | 8 9 13 | jpl | jpl 2873 | 10 13 21 | 8 10 31 | 10 7 18 | mit | mit 3072 | 10 10 22 | 8 8 26 | 9 9 16 | Table 5.1564.5 GPS week: 1564 Day: 5 MJD: 55197.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3062 | 8 6 19 | 9 13 32 | 8 8 12 | emr | emr 3052 | 17 10 41 | 12 12 40 | 10 9 22 | esa | esa 2976 | 8 7 17 | 8 12 33 | 8 9 13 | gfz | gfz 2723 | 20 22 40 | 17 17 77 | 26 27 49 | grg | grg 2880 | 12 9 31 | 439 171 511 | 14 17 23 | igr | igr 3055 | 8 6 20 | 10 13 34 | 7 7 13 | igs | igs 2907 | 12 7 26 | 9 13 39 | 8 9 13 | jpl | jpl 2874 | 9 7 22 | 8 12 37 | 9 6 16 | mit | mit 3072 | 8 5 17 | 10 13 33 | 8 6 22 | Table 5.1564.6 GPS week: 1564 Day: 6 MJD: 55198.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3052 | 7 8 20 | 9 13 22 | 8 6 12 | emr | emr 3060 | 13 13 25 | 10 13 32 | 11 10 24 | esa | esa 2976 | 8 9 19 | 8 11 23 | 8 8 16 | gfz | gfz 2825 | 14 11 26 | 15 14 49 | 20 24 34 | grg | grg 2880 | 11 11 24 | 10 14 40 | 12 13 15 | igr | igr 2952 | 8 9 20 | 9 14 26 | 8 8 15 | igs | igs 2969 | 8 8 19 | 9 13 23 | 7 7 14 | jpl | jpl 2876 | 9 9 20 | 9 14 26 | 9 6 16 | mit | mit 3072 | 8 7 19 | 10 14 25 | 8 8 16 | 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 6.1564 GPS week: 1564 MJD: 55192.500-55198.500 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 | -15 -25 -1 40 2 | 2 20 | 13 26 54 98 5 | 2 emr uuuuu | 6 -13 19 144 -1 | 34 38 | 28 17 85 85 12 | 3 esa uuuuu | -18 21 72 25 1 | -17 26 | 18 15 83 96 18 | 4 gfz uuuuu | 33 9 49 -49 3 | 0 20 | 17 15 38 40 7 | 3 grg --xxx | -- -- 478 -144 14 | 13 19 | -- -- 76 171 22 | 2 igr xxxxx | 6 24 37 -36 2 | -5 16 | 8 28 58 84 12 | 3 irf xxxxx | -2 -9 -8 18 -2 | 3 18 | 5 7 20 47 5 | 3 jpl uuuuu | 13 -30 -43 57 6 | 16 23 | 23 28 54 120 7 | 1 mit uuuuu | -18 -2 -180 64 -4 | 8 21 | 11 13 66 121 12 | 4 ngs uuuuu | 14 -11 82 -74 3 | -6 15 | 28 25 63 135 8 | 1 sio uuuuu | -45 3 -89 -176 -12 | 16 26 | 22 19 125 47 13 | 3 Table 7.1564.0 GPS week: 1564 Day: 0 MJD: 55192.500 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 -19 -58 -64 -7 | 2 21 emr uuuuu | 4 -47 103 72 -5 | 37 40 esa uuuuu | -23 26 53 3 -17 | -12 22 gfz uuuuu | 33 19 -17 -56 7 | -5 22 grg --xxx | -- -- 386 128 33 | 11 18 igr xxxxx | 14 16 10 -113 -4 | -2 15 irf xxxxx | 2 -2 -21 92 4 | 0 19 jpl uuuuu | 33 -46 -39 102 -1 | 16 23 mit uuuuu | -18 8 -186 198 7 | 2 22 ngs uuuuu | 5 -18 71 -146 1 | -8 17 sio uuuuu | -37 15 46 -128 2 | 13 25 Table 7.1564.1 GPS week: 1564 Day: 1 MJD: 55193.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -7 -22 -50 71 -1 | 1 21 emr uuuuu | 32 -13 65 94 -20 | 36 40 esa uuuuu | -14 32 -63 24 -26 | -13 24 gfz uuuuu | 57 -2 20 -78 6 | -3 21 grg --xxx | -- -- 460 -173 -15 | 12 20 igr xxxxx | 17 15 155 -175 -15 | -3 15 irf xxxxx | -1 -5 -5 48 3 | 1 19 jpl uuuuu | 15 -26 -56 -54 10 | 14 22 mit uuuuu | -35 3 -65 183 10 | 4 21 ngs uuuuu | -2 -19 93 -90 0 | -7 16 sio uuuuu | -55 8 45 -116 2 | 14 25 Table 7.1564.2 GPS week: 1564 Day: 2 MJD: 55194.500 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 -7 -53 19 4 | 2 21 emr uuuuu | 25 6 33 122 -10 | 35 39 esa uuuuu | 1 9 9 112 -4 | -15 26 gfz uuuuu | 50 11 42 -8 9 | 0 20 grg --xxx | -- -- 406 -251 -3 | 12 20 igr xxxxx | 10 77 -21 -6 -9 | -3 16 irf xxxxx | -5 2 -17 51 -1 | 4 18 jpl uuuuu | -1 -15 -94 -79 15 | 16 23 mit uuuuu | -27 14 -145 163 2 | 8 21 ngs uuuuu | -7 -53 169 -270 -8 | -6 15 sio uuuuu | -63 36 -37 -168 -5 | 17 26 Table 7.1564.3 GPS week: 1564 Day: 3 MJD: 55195.500 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 | -14 -19 73 -10 5 | 3 20 emr uuuuu | -8 4 -135 106 1 | 34 38 esa uuuuu | -4 46 133 131 6 | -17 27 gfz uuuuu | 37 -18 78 -74 2 | 2 19 grg --xxx | -- -- 537 -73 8 | 9 17 igr xxxxx | 5 12 11 -8 5 | -5 17 irf xxxxx | -3 -13 5 -2 2 | 5 18 jpl uuuuu | 8 -19 -89 -13 4 | 16 24 mit uuuuu | -15 -21 -152 78 2 | 10 20 ngs uuuuu | 3 0 30 -80 -4 | -6 15 sio uuuuu | -68 -8 -25 -190 -8 | 18 26 Table 7.1564.4 GPS week: 1564 Day: 4 MJD: 55196.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -27 -54 14 -5 0 | 6 20 emr uuuuu | 1 -15 -51 257 -1 | 35 39 esa uuuuu | -47 3 134 73 4 | -17 27 gfz uuuuu | 30 7 79 -91 -10 | 6 18 grg --xxx | -- -- 531 -199 37 | 13 18 igr xxxxx | -5 48 65 -6 6 | -4 17 irf xxxxx | -9 -14 1 -1 -9 | 8 17 jpl uuuuu | 0 2 -27 256 11 | 18 25 mit uuuuu | -16 5 -268 -20 -14 | 14 20 ngs uuuuu | 74 -14 155 -129 16 | -4 14 sio uuuuu | -58 5 -226 -254 -25 | 21 26 Table 7.1564.5 GPS week: 1564 Day: 5 MJD: 55197.500 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 11 57 31 8 | 1 19 emr uuuuu | 34 -19 89 274 13 | 29 33 esa uuuuu | -36 12 175 -156 19 | -23 29 gfz uuuuu | 6 29 92 -54 -2 | 0 18 grg --xxx | -- -- 435 -34 1 | 15 19 igr xxxxx | 5 -6 30 83 15 | -8 16 irf xxxxx | -1 -18 19 -44 -6 | 3 17 jpl uuuuu | 52 -26 -59 147 7 | 15 23 mit uuuuu | -6 -19 -220 -78 -14 | 9 20 ngs uuuuu | 4 -1 -6 141 6 | -7 14 sio uuuuu | -22 -17 -235 -211 -24 | 15 26 Table 7.1564.6 GPS week: 1564 Day: 6 MJD: 55198.500 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 | -34 -65 11 240 8 | 1 19 emr uuuuu | -45 -12 31 83 15 | 29 33 esa uuuuu | -4 15 60 -12 26 | -22 28 gfz uuuuu | 20 14 50 19 7 | -2 19 grg --xxx | -- -- 591 -408 39 | 15 19 igr xxxxx | -1 7 11 -24 16 | -8 16 irf xxxxx | 6 -15 -41 -16 -8 | 2 18 jpl uuuuu | -15 -84 65 40 -7 | 16 23 mit uuuuu | -5 -9 -222 -74 -19 | 7 21 ngs uuuuu | 22 29 64 54 7 | -7 15 sio uuuuu | -10 -18 -192 -167 -28 | 12 26