Date: Thu, 26 Mar 2009 12:29:16 +0000 From: Jim Ray Subject: [IGSREPORT-17244] Wk 1522 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <49cb751c.QBlQYamqJlihT0F8%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 26 Mar 05:29:39 PDT 2009 Message Number 17244 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1522 (Mar 08, 2009 - Mar 14, 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: igs1522[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1522[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1522[0-6].cls IGS GPS clock combination summary report. igs15227.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15227.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Day | Centre | PRN/STA list ----+--------+--------------- 0 | COD | 3 6 3 6 0 | EMR | YELL HARB YELL 0 | ESA | 3 6 26 0 | GFZ | 7 29 FAA1 HARB KERG 0 | GRG | NLIB 0 | JPL | 3 0 | MIT | 26 26 1 | COD | 3 6 26 3 6 26 RCMN 1 | EMR | DAEJ 1 | ESA | 3 4 6 26 DAEJ DARW 1 | GFZ | 3 7 8 17 19 29 GLPS GUAT IRKT MBAR SCUB SSIA YKRO 1 | GFZ | YSSK 1 | GRG | PIE1 1 | JPL | 9 26 AREQ DAV1 1 | MIT | 4 9 24 4 24 2 | COD | 3 6 26 3 6 2 | EMR | MIZU 2 | ESA | 6 26 30 DAV1 2 | GFZ | 7 8 30 2 | GRG | KHAJ PIE1 2 | JPL | 3 30 2 | MIT | 12 12 3 | COD | 6 26 6 26 3 | EMR | DAEJ MIZU 3 | ESA | 3 6 26 3 | GFZ | 3 7 19 29 DAEJ FAA1 3 | GRG | NLIB 3 | JPL | 3 26 CHPI MATE 3 | MIT | 4 3 4 KOUR KOUR 4 | COD | 6 26 6 26 4 | EMR | IRKT MIZU 4 | ESA | 26 QAQ1 4 | GFZ | 7 13 19 29 MAL2 REYK VESL 4 | GRG | NLIB NOVM 4 | JPL | 3 6 4 | MIT | DARW 5 | COD | 6 26 6 26 5 | EMR | YELL MIZU YELL 5 | ESA | 6 26 YELL 5 | GFZ | 6 7 15 17 26 29 DAEJ HOLM REYK 5 | GRG | NLIB NOVM 5 | JPL | 26 YELL 6 | COD | 26 26 NRIL 6 | EMR | DAEJ 6 | ESA | KARR 6 | GFZ | 7 15 19 26 29 ARTU DAEJ HARB 6 | GRG | NLIB 6 | JPL | 6 21 6 | MIT | 6 6 CAS1 HARB TLSE 5. The following orbit solutions were excluded from the combination because they were biasing the weighted average (generally indicated by long arc RMS). They were still used for statistics computation. Day | Centre | PRN list ----+--------+--------------- 1 | ESA | 4 6. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447. 7. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .4 .3 .6 -19 -15 -8 .05 EMR | 11.4 -3.4 -1.8 91 50 50 .23 ESA | 7.4 3.4 3.3 38 -70 23 .04 GFZ | .7 .5 1.4 22 -7 26 -.23 GRG | 3.5 1.4 -6.5 13 -20 8 .11 JPL | 4.5 6.1 6.3 -5 -8 29 .53 MIT | 7.1 -4.6 1.6 -17 28 -7 .01 NGS | 8.6 -2.7 .9 -43 -128 15 .15 SIO | 4.4 -1.8 11.0 -44 -27 -7 .41 8. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 9. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 10. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five parts. The first, Table 1, summarizes all statistics for the week. It contains means and standard deviations over the week of satellite ephemeris and clock correction transformation parameters for each centre (table 1.1522.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1522.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 2.1522.[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 3.1522.[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 5.1522.0-6). 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 1522 summary. (Mar 08, 2009 - Mar 14, 2009) Table 1.1522.a GPS week: 1522 MJD: 54898.000-54904.000 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 1 35 -5 -26 -.17 8 7 | -315 -318 13 113 | 0 0 1 9 13 13 .02 | 476 546 emr 72| 0 2 5 -215 -129 -61 .46 18 18 | -156 398 18 179 | 1 1 1 22 24 24 .02 | 1318 1816 esa 122| 0 0 -2 -77 2 11 .29 14 9 | 221 -734 20 138 | 0 0 0 32 23 17 .04 | 423 897 gfz 198| 0 -1 -4 -24 -49 101 -.08 12 12 | 118 36 24 148 | 1 1 1 22 18 55 .02 | 288 815 grg 118| 2 1 -8 -50 0 -10 1.07 38 34 | 29 -247 83 235 | 1 1 2 20 19 59 .04 | 195 442 igr n/a| 0 0 0 -5 -34 -10 .02 5 5 | -2609 254 20 72 | 0 0 1 14 19 31 .01 | 1332 1914 jpl 133| 0 0 4 -7 0 -21 .54 18 17 | 584 674 20 112 | 1 1 1 17 10 24 .08 | 1422 1749 mit 259| 0 -1 -1 53 -99 -13 -.29 12 10 | 39 -215 21 143 | 0 0 1 39 22 14 .03 | 192 441 ngs 222| 0 0 0 101 205 3 -.33 11 9 | -334 -284 2138 3768 | 0 0 1 41 38 29 .07 | 556 632 sio 259| -1 0 4 80 6 4 .01 19 18 | --- --- --- --- | 1 2 0 38 25 26 .03 | --- --- Table 1.1522.b GPS week : 1522 MJD: 54898.000-54904.000 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: mm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------+------------------------------------+------------------------------------------ 2 | 5 5 5 5 5 5 5 | 3 | 6 7 7 7 7 7 6 | 4 | 3 4 6 4 4 4 3 | 5 | 4 4 4 4 4 3 3 | 6 | 6 6 6 7 6 7 6 | 7 | 6 6 5 5 5 5 5 | 8 | 3 3 3 4 4 4 4 | 9 | 3 3 4 3 4 4 4 | 10 | 4 4 3 4 3 4 4 | 11 | 5 4 4 4 4 5 4 | 12 | 5 5 5 6 5 5 5 | 13 | 4 5 5 5 5 5 5 | 14 | 5 5 5 5 5 5 5 | 15 | 6 5 6 5 6 5 5 | 16 | 6 6 6 6 7 6 6 | 17 | 5 5 5 5 5 5 5 | 18 | 6 6 6 6 6 5 5 | 19 | 6 6 6 6 6 5 5 | 20 | 5 5 5 5 5 5 5 | 21 | 5 6 5 5 5 5 5 | 22 | 6 5 5 5 6 5 5 | 23 | 5 6 6 6 6 6 6 | 24 | 4 4 4 3 4 4 3 | 25 | 4 4 4 4 5 5 4 | 26 | 6 6 6 5 5 5 5 | 27 | 4 3 3 3 4 3 4 | 28 | 5 4 6 6 5 5 5 | 29 | 5 5 5 5 5 5 6 | 30 | 4 4 4 3 4 3 3 | 31 | 5 5 6 5 5 5 6 | 32 | 5 5 5 5 5 5 5 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1522.0 GPS week: 1522 Day: 0 MJD: 54898.000 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 38 -6 -10 -.16 9 8 | -202 -255 15 91 | 34 11 | emr 72| -1 2 4 -188 -121 -84 .49 17 17 | 1216 -1875 21 145 | 39 -17 | esa 122| 0 0 -2 -95 -22 12 .36 9 9 | 839 -2623 18 121 | 54 61 | gfz 198| 0 0 -5 -51 -43 78 -.08 11 11 | 485 -810 26 152 | 1 31 | grg 118| 3 0 -6 -57 20 -28 1.04 40 36 | 304 -980 77 235 | 61 64 | igr n/a| 0 0 -3 -6 -54 -35 .01 6 5 | -763 -2317 22 70 | 2 42 | jpl 133| 0 0 6 11 -1 18 .63 19 17 | 1077 -1516 22 108 | -13 0 | mit 259| -1 0 -1 86 -92 -18 -.34 13 11 | 322 -952 22 112 | -8 -6 | ngs 222| 1 0 -2 94 215 -14 -.41 11 8 | -246 -168 1921 3937 | -39 47 | sio 259| -3 -3 5 99 17 12 .06 22 20 | --- --- --- --- | -5 -11 | Table 2.1522.1 GPS week: 1522 Day: 1 MJD: 54899.000 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 1 2 37 -23 -47 -.14 8 7 | 229 -801 13 113 | 1 -31 | emr 72| 0 0 4 -212 -114 -96 .48 18 18 | -763 -1192 18 186 | 48 -52 | esa 122| 1 -1 -2 -103 -5 1 .28 41 11 | 551 -98 21 152 | 37 73 | gfz 198| 0 -2 -6 -41 -72 173 -.07 12 12 | 336 -418 25 149 | -34 11 | grg 118| 3 2 -4 -53 -13 -44 1.12 43 37 | 174 -649 97 235 | -1 31 | igr n/a| 0 1 -1 -4 -50 -53 .03 5 5 | -2923 -1250 24 74 | -7 -1 | jpl 133| -1 0 5 9 -6 -39 .64 19 17 | -370 -629 21 119 | 19 15 | mit 259| 0 0 -2 0 -118 -10 -.27 12 9 | 234 -710 22 128 | 36 3 | ngs 222| 1 1 -1 134 223 3 -.25 9 7 | 370 -957 2238 3976 | -125 -23 | sio 259| -3 0 3 42 -6 34 -.04 20 18 | --- --- --- --- | -5 2 | Table 2.1522.2 GPS week: 1522 Day: 2 MJD: 54900.000 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 1 33 -19 -20 -.16 8 7 | -447 40 20 160 | 6 11 | emr 72| 1 0 5 -195 -93 -46 .46 18 18 | -1011 -1085 20 215 | 37 -60 | esa 122| 0 0 -3 -64 -30 8 .30 12 11 | 117 -368 24 136 | 22 76 | gfz 198| 0 -1 -3 -16 -41 163 -.07 13 13 | 12 39 30 152 | -41 7 | grg 118| 0 2 -9 -48 -4 95 1.06 38 33 | -180 235 85 239 | 7 7 | igr n/a| -1 0 0 10 -21 -16 .01 5 5 | -3330 -1230 22 69 | -67 -27 | jpl 133| -2 0 3 0 4 -7 .61 19 17 | -177 -837 21 112 | -34 -73 | mit 259| 0 -1 -2 9 -105 -7 -.26 12 10 | -119 201 25 182 | 24 12 | ngs 222| 0 0 0 103 232 -49 -.23 11 8 | -455 13 2202 3336 | -5 -29 | sio 259| 0 0 3 48 3 21 -.01 18 17 | --- --- --- --- | -6 7 | Table 2.1522.3 GPS week: 1522 Day: 3 MJD: 54901.000 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 34 1 -25 -.18 9 8 | 86 -637 14 106 | 48 -31 | emr 72| 0 1 4 -213 -119 -41 .49 18 18 | -1496 1585 19 194 | 60 6 | esa 122| 0 1 -1 -122 10 23 .31 9 9 | 230 -442 20 143 | 82 47 | gfz 198| 0 -2 -5 15 -78 12 -.06 13 13 | 360 -230 21 147 | -23 13 | grg 118| 0 2 -12 -25 20 -79 1.09 36 32 | 206 -87 80 242 | 17 -50 | igr n/a| 0 0 0 -6 0 42 .00 5 5 | -3973 1415 20 76 | 1 -23 | jpl 133| -2 0 2 -28 18 -18 .52 18 16 | -418 1386 21 109 | 0 -29 | mit 259| 0 -2 -1 69 -114 4 -.28 12 10 | 100 79 18 120 | -4 5 | ngs 222| 0 0 0 117 246 22 -.38 12 11 | 66 -596 2350 3818 | -31 -89 | sio 259| -2 0 4 125 -17 18 .02 17 16 | --- --- --- --- | -36 26 | Table 2.1522.4 GPS week: 1522 Day: 4 MJD: 54902.000 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 1 53 -9 -26 -.17 9 8 | -908 103 10 108 | -9 13 | emr 72| 0 3 6 -207 -148 -68 .44 18 18 | -921 1266 15 181 | 73 2 | esa 122| 1 0 -3 -86 34 -19 .23 9 9 | -532 55 20 143 | 85 14 | gfz 198| 2 -1 -5 -33 -44 112 -.09 12 12 | -341 1763 24 151 | -21 37 | grg 118| 3 2 -9 -31 -33 16 1.05 35 32 | -42 -382 80 222 | -38 101 | igr n/a| 0 1 0 1 -47 10 .01 5 5 | -3589 1150 19 75 | 5 3 | jpl 133| 0 -2 3 0 -8 -23 .49 17 17 | -363 1673 20 131 | 6 -86 | mit 259| 0 -1 0 35 -52 -4 -.27 13 12 | -171 -189 25 142 | -21 -1 | ngs 222| 0 0 0 160 145 45 -.35 13 11 | -1124 432 2039 3895 | -7 131 | sio 259| 0 2 5 32 59 -11 -.01 19 17 | --- --- --- --- | -25 23 | Table 2.1522.5 GPS week: 1522 Day: 5 MJD: 54903.000 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 21 7 -13 -.19 9 7 | -3 -1096 13 108 | 99 -29 | emr 72| 0 3 7 -245 -166 -62 .45 19 19 | -212 3120 16 157 | 113 12 | esa 122| 0 0 -3 -40 23 17 .27 7 6 | 137 -857 18 134 | 26 51 | gfz 198| 0 0 -6 -12 -32 105 -.13 12 12 | 31 -43 22 143 | 15 14 | grg 118| 3 2 -6 -89 8 22 1.02 37 37 | -162 42 85 249 | 135 26 | igr n/a| 0 0 0 -34 -33 -16 .03 6 5 | -2990 3152 19 67 | 71 -22 | jpl 133| 1 0 4 -34 0 -24 .42 19 19 | 855 3473 19 96 | 52 -3 | mit 259| 0 -1 0 102 -112 -41 -.28 12 11 | -139 11 19 140 | 10 -7 | ngs 222| 0 0 1 49 158 10 -.31 11 10 | 34 -1142 1892 3655 | -77 43 | sio 259| -1 1 4 114 -9 -45 .00 19 19 | --- --- --- --- | -22 28 | Table 2.1522.6 GPS week: 1522 Day: 6 MJD: 54904.000 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 1 -1 31 13 -41 -.18 8 7 | -966 420 11 105 | 36 -11 | emr 72| -1 4 6 -247 -145 -27 .45 19 19 | 2093 967 17 181 | 93 21 | esa 122| 0 0 -2 -33 4 34 .30 8 8 | 205 -811 19 141 | 48 69 | gfz 198| 0 -1 -2 -28 -35 69 -.08 12 12 | -54 -46 22 148 | -16 8 | grg 118| 2 2 -8 -47 1 -52 1.08 35 32 | -96 92 83 223 | 89 -30 | igr n/a| 0 0 0 0 -33 -2 .03 6 5 | -695 862 20 76 | -5 -6 | jpl 133| -2 0 2 -11 -10 -60 .49 18 17 | 3488 1170 20 109 | -8 -7 | mit 259| 0 -1 0 72 -101 -13 -.29 11 10 | 49 52 22 182 | -5 -7 | ngs 222| 1 -1 1 52 219 9 -.35 12 9 | -983 424 2329 3762 | 43 -33 | sio 259| 0 1 4 103 0 4 .03 21 19 | --- --- --- --- | -58 33 | 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 3.1522.0 GPS week: 1522 Day: 0 MJD: 54898.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 10 23 10 12 30 5 23 6 9 26 5 | 18 32 21 22 32 19 28 20 22 26 18 3E | 14 17 13 10 52 6 17 19 16 25 6 | 100 105 102 102 111 104 102 110 110 103 104 4 | 6 9 7 6 25 5 11 9 6 19 3 | 26 31 67 33 32 32 27 34 29 32 29 5 | 9 10 6 11 20 5 9 14 7 20 4 | 21 27 25 25 30 22 25 27 22 28 22 6E | 10 17 11 12 63 6 17 19 15 22 5 | 41 41 40 40 39 41 37 51 49 39 41 7 | 12 24 8 15 25 9 22 17 10 24 5 | 23 38 27 29 42 24 31 23 22 30 23 8 | 7 12 8 8 22 5 13 5 6 12 3 | 24 30 24 23 31 22 29 23 24 23 23 9 | 6 10 6 7 22 4 10 4 9 19 3 | 23 26 24 20 37 22 26 21 21 20 21 10 | 7 13 9 7 39 3 11 7 9 19 3 | 26 29 35 32 25 30 25 28 31 25 28 11 | 7 19 7 9 83 6 19 18 11 20 5 | 27 34 27 27 70 27 34 29 29 24 24 12 | 10 17 7 11 33 5 19 9 8 29 4 | 25 32 20 20 41 24 33 23 28 23 22 13E | 6 15 6 12 29 6 17 10 10 9 4 | 24 34 29 30 34 26 29 25 28 28 26 14E | 9 19 8 11 29 5 23 11 11 24 5 | 32 46 36 37 48 35 43 29 36 31 34 15E | 9 23 11 15 51 6 24 12 12 24 5 | 18 34 25 23 26 20 30 20 24 26 21 16 | 8 22 9 12 27 5 26 13 9 30 5 | 31 38 31 32 40 31 41 30 30 30 30 17E | 6 15 7 9 35 7 24 10 13 20 4 | 24 33 24 25 36 24 29 29 31 24 25 18 | 10 21 9 15 33 5 24 8 14 31 5 | 27 36 34 40 37 31 35 32 34 34 31 19E | 8 24 13 13 43 6 29 17 12 14 6 | 40 50 42 43 40 42 48 43 52 43 42 20 | 10 19 8 10 39 5 19 11 11 30 5 | 34 39 38 39 46 36 38 35 40 37 35 21 | 8 20 12 9 58 5 25 11 12 19 5 | 21 31 28 27 50 23 34 22 30 19 23 22 | 9 19 11 13 48 5 22 12 13 26 5 | 38 44 44 47 44 40 43 41 44 39 40 23E | 8 20 8 14 41 5 24 8 10 21 5 | 19 30 21 24 37 19 30 23 24 23 20 24 | 8 11 7 8 32 3 11 11 10 11 3 | 26 35 32 36 32 31 30 30 37 30 31 25 | 8 12 7 9 22 6 11 11 9 25 4 | 19 27 23 18 35 19 27 18 15 39 19 26E | 16 15 10 15 54 6 17 24 13 24 6 | 55 58 55 49 61 53 62 61 55 61 54 27 | 6 11 9 8 31 6 12 11 9 11 3 | 20 27 18 18 34 21 24 20 24 21 19 28 | 5 18 11 9 39 7 19 11 12 24 4 | 32 42 28 32 51 32 38 34 34 33 31 29E | 9 19 8 9 41 5 24 13 9 13 4 | 16 25 19 17 43 17 23 23 20 19 16 30 | 7 11 7 7 32 7 10 14 8 20 3 | 32 36 35 34 32 30 32 36 30 33 32 31 | 7 19 9 14 29 6 23 13 10 16 5 | 25 35 29 34 42 26 33 27 27 26 26 32 | 8 18 9 11 25 4 20 12 10 30 5 | 17 21 21 27 25 18 20 23 25 20 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 17 9 11 40 6 19 13 11 22 |T 29 36 33 32 41 30 35 31 33 31 29 WRMS | 8 17 9 11 36 5 17 11 8 20 |NE 25 32 30 29 38 26 31 27 28 28 25 MEDI | 8 18 8 11 33 5 19 11 10 21 |MD 25 34 28 30 37 26 31 28 29 28 26 Table 3.1522.1 GPS week: 1522 Day: 1 MJD: 54899.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 22 13 16 34 4 23 7 8 23 5 | 14 25 18 21 28 14 23 19 17 22 14 3E | 15 18 15 14 74 8 16 23 16 28 6 | 89 89 86 85 89 90 89 94 91 89 87 4 | 7 12 222 12 33 8 8 6 9 18 4 | 16 18 149 22 28 18 19 21 19 23 17 5 | 6 12 11 13 24 4 11 11 4 13 3 | 15 18 23 20 28 15 18 17 14 16 15 6E | 12 17 14 12 75 6 16 18 15 22 5 | 38 33 32 38 36 37 30 48 42 30 35 7 | 9 22 10 14 32 6 21 13 12 24 5 | 17 29 20 16 36 15 27 15 15 22 14 8 | 7 14 9 5 28 3 10 7 8 14 3 | 22 23 25 20 29 21 29 20 18 21 20 9 | 6 11 8 9 20 5 9 5 6 17 3 | 19 19 17 14 31 17 20 16 16 12 15 10 | 5 16 8 9 40 4 10 7 6 17 3 | 18 24 22 23 24 19 18 21 20 16 18 11 | 8 17 11 9 85 5 18 11 7 14 4 | 25 32 28 30 58 26 31 30 27 28 27 12 | 7 20 13 13 25 3 21 9 6 30 5 | 21 31 21 18 37 20 27 20 19 28 18 13E | 9 14 11 13 39 5 16 11 11 12 4 | 19 24 20 23 35 20 25 22 25 24 19 14E | 8 16 10 10 30 6 19 13 9 13 4 | 30 31 30 30 35 29 32 30 35 29 29 15E | 8 21 9 12 41 4 22 8 8 22 4 | 16 23 14 16 31 14 22 20 17 26 14 16 | 7 24 9 11 22 6 27 12 7 24 5 | 29 39 28 25 47 31 41 31 29 33 29 17E | 7 16 11 10 38 5 22 8 12 19 4 | 30 35 28 29 48 30 33 34 33 34 29 18 | 9 20 11 17 37 4 23 7 10 25 5 | 17 29 25 29 32 20 28 20 23 20 20 19E | 9 18 10 10 37 5 27 19 11 10 5 | 32 34 30 30 58 32 36 36 36 33 31 20 | 6 17 10 11 40 7 21 10 11 25 5 | 31 35 33 35 36 32 35 36 37 35 33 21 | 6 24 17 12 71 5 26 9 9 18 5 | 18 32 23 25 54 18 31 17 26 17 20 22 | 8 17 12 14 68 4 19 10 7 20 4 | 25 33 29 33 44 25 31 26 30 25 26 23E | 8 24 15 17 38 6 24 12 10 13 5 | 17 28 23 25 37 17 27 22 23 18 18 24 | 5 11 10 15 31 3 11 9 5 14 3 | 19 26 23 31 22 21 20 20 27 21 22 25 | 6 13 10 7 24 5 11 7 7 27 4 | 15 19 19 13 29 15 23 15 14 35 15 26E | 14 18 10 14 66 9 16 17 13 22 5 | 42 55 47 42 62 43 55 41 43 52 43 27 | 4 11 7 8 26 4 10 11 6 10 3 | 18 25 20 20 31 19 25 16 18 18 18 28 | 6 17 10 8 37 4 16 10 8 20 4 | 28 39 30 26 41 28 38 29 27 28 27 29E | 7 18 10 15 30 4 23 11 8 17 4 | 13 22 14 14 25 12 21 18 16 18 12 30 | 5 12 11 12 23 5 10 12 6 17 4 | 23 24 27 24 28 21 23 24 22 18 22 31 | 9 20 9 16 28 6 22 8 8 18 5 | 19 30 23 24 42 20 30 19 21 20 19 32 | 6 18 9 14 19 6 18 16 11 19 5 | 12 15 14 18 22 14 15 17 22 15 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 41 12 43 5 19 12 9 20 |T 24 30 30 26 38 24 29 26 26 26 23 WRMS | 7 18 11 12 37 5 17 9 7 18 |NE 20 26 29 23 34 20 26 21 21 22 20 MEDI | 7 17 10 12 34 5 18 10 8 18 |MD 19 29 23 24 35 20 27 21 23 23 20 Table 3.1522.2 GPS week: 1522 Day: 2 MJD: 54900.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 22 13 15 24 4 24 9 7 21 5 | 18 27 19 18 28 17 26 22 21 26 17 3E | 18 24 16 13 65 5 15 22 16 25 7 | 57 66 64 63 60 59 58 56 62 64 58 4 | 12 13 30 9 29 4 10 8 10 15 5 | 17 23 69 23 36 20 22 23 23 23 20 5 | 8 9 9 12 20 5 10 7 7 13 3 | 17 18 25 24 31 18 17 19 22 16 19 6E | 13 21 15 12 60 6 15 18 14 19 6 | 34 30 32 33 21 31 27 40 42 26 31 7 | 7 23 7 14 35 3 22 9 11 21 5 | 18 30 17 21 38 17 28 16 21 25 17 8 | 4 15 6 8 17 2 10 5 7 13 3 | 19 23 21 20 30 19 26 20 19 18 18 9 | 7 11 7 10 28 4 10 13 10 13 3 | 16 20 21 22 39 19 21 21 22 16 17 10 | 5 12 11 8 26 5 11 7 7 11 3 | 19 18 24 23 23 20 21 24 23 20 20 11 | 6 16 9 10 80 7 15 9 12 14 4 | 18 27 18 19 56 21 28 23 25 21 18 12 | 10 18 8 14 23 6 19 8 9 27 5 | 23 31 28 29 43 22 34 28 24 33 25 13E | 5 17 13 16 35 5 18 13 9 13 4 | 23 27 24 26 31 23 26 26 32 26 24 14E | 10 18 10 11 31 5 21 13 12 15 5 | 34 36 30 29 34 31 34 29 36 29 31 15E | 11 20 12 17 37 4 24 11 13 16 5 | 13 23 19 21 29 13 23 20 23 23 16 16 | 7 19 12 14 26 3 26 13 11 21 5 | 20 33 20 27 41 22 34 19 24 24 21 17E | 6 16 13 11 28 6 24 17 12 14 5 | 21 27 23 25 36 19 28 24 31 19 21 18 | 10 18 13 17 33 6 22 8 8 25 5 | 22 30 26 35 33 26 31 27 28 27 25 19E | 8 19 13 12 29 5 24 26 13 14 6 | 19 24 18 21 23 20 24 33 31 23 21 20 | 7 18 11 10 36 6 20 10 13 24 5 | 26 32 30 31 34 27 31 29 31 26 26 21 | 7 20 15 14 54 5 24 9 10 17 5 | 23 28 27 26 42 21 29 22 20 20 20 22 | 8 18 11 16 53 5 20 11 10 21 5 | 37 39 36 44 37 36 36 36 37 35 35 23E | 7 24 14 22 42 6 26 16 11 16 6 | 19 25 17 27 37 16 26 21 27 21 17 24 | 5 12 8 11 22 4 11 9 11 12 3 | 22 27 26 28 26 24 24 24 29 23 24 25 | 5 13 7 9 26 4 13 9 8 26 4 | 14 20 16 14 30 14 22 15 17 33 15 26E | 11 16 11 15 61 9 15 15 15 23 5 | 38 49 40 41 62 38 52 35 34 50 38 27 | 6 14 7 7 20 4 11 7 9 10 3 | 14 26 21 20 30 19 24 16 18 19 17 28 | 7 24 11 10 40 3 20 12 15 20 5 | 23 38 25 24 49 23 36 23 26 21 23 29E | 8 22 10 12 29 5 23 11 8 17 5 | 12 24 14 13 25 11 19 17 21 18 12 30 | 7 9 9 11 19 6 11 9 9 14 3 | 22 27 29 27 41 24 22 25 25 21 23 31 | 7 20 16 19 32 6 25 11 11 16 5 | 21 31 25 32 46 22 32 21 24 21 22 32 | 6 16 11 17 19 6 18 13 9 20 5 | 13 18 20 25 23 14 14 20 23 13 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 12 13 38 5 19 12 11 18 |T 22 28 26 26 35 22 28 24 27 25 22 WRMS | 7 18 11 13 33 5 17 10 8 17 |NE 20 26 25 25 36 21 26 22 23 22 20 MEDI | 7 18 11 12 29 5 19 11 10 16 |MD 20 27 24 25 34 21 26 23 24 23 21 Table 3.1522.3 GPS week: 1522 Day: 3 MJD: 54901.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 7 23 9 16 30 4 21 10 11 20 5 | 21 32 22 29 32 18 30 23 23 24 21 3E | 18 19 12 15 57 5 16 22 16 25 6 | 98 98 97 94 87 94 98 96 98 99 95 4 | 6 12 8 14 33 5 10 8 12 13 3 | 20 25 41 30 28 22 27 25 24 26 22 5 | 6 10 7 10 17 5 10 8 13 12 3 | 18 21 25 25 24 18 20 23 21 16 19 6E | 15 18 14 15 67 5 17 22 13 24 6 | 37 36 37 35 31 34 35 46 41 38 35 7 | 8 21 8 18 33 5 20 9 10 20 5 | 17 27 23 28 38 17 27 15 19 25 19 8 | 7 14 7 8 20 5 9 7 10 13 3 | 17 25 23 20 27 20 24 21 19 21 19 9 | 5 11 5 8 17 4 8 10 12 11 3 | 18 20 21 19 27 17 18 19 20 19 17 10 | 8 11 8 8 27 5 9 6 13 10 3 | 24 25 28 32 21 26 24 28 34 22 26 11 | 6 15 7 9 67 6 14 10 9 16 4 | 30 35 29 36 54 26 32 31 34 34 30 12 | 9 19 14 13 34 7 19 11 14 22 5 | 28 32 31 24 39 26 32 27 28 27 26 13E | 8 15 8 21 28 5 16 13 13 10 4 | 18 27 19 29 34 15 24 23 22 24 18 14E | 9 17 7 12 23 3 16 13 11 14 4 | 26 32 29 33 43 27 29 29 31 26 28 15E | 11 24 7 13 34 6 20 15 12 15 5 | 11 27 16 21 36 14 22 22 20 23 16 16 | 8 22 11 16 25 5 25 11 17 23 6 | 32 39 33 29 35 33 43 33 33 34 32 17E | 7 18 10 9 33 6 22 11 12 8 4 | 26 35 30 27 42 29 33 30 34 29 29 18 | 10 19 9 15 32 4 21 8 13 24 5 | 22 33 30 36 37 25 32 30 28 29 27 19E | 12 17 10 11 35 3 23 26 12 13 6 | 28 32 28 28 32 28 32 37 34 30 28 20 | 7 18 11 12 32 5 20 11 9 23 5 | 40 41 45 47 49 39 41 42 45 40 41 21 | 9 22 13 11 35 4 21 10 10 18 5 | 25 35 26 31 41 24 33 23 26 20 24 22 | 8 17 8 10 43 4 19 11 13 23 5 | 30 39 36 40 42 32 39 36 32 32 33 23E | 6 22 13 23 29 6 28 13 15 13 6 | 17 28 19 31 43 14 28 22 28 20 18 24 | 5 12 5 10 26 6 8 7 12 12 3 | 21 27 25 31 27 25 24 24 31 26 25 25 | 9 14 7 10 28 4 9 11 8 25 4 | 15 19 19 21 33 14 22 17 20 34 17 26E | 9 19 8 9 75 7 15 11 10 22 4 | 49 63 51 46 64 50 59 48 49 57 50 27 | 5 10 6 4 22 6 9 8 9 10 2 | 18 24 23 18 28 20 21 19 17 25 19 28 | 7 25 10 8 35 5 19 10 20 18 5 | 22 39 28 21 44 25 35 24 24 24 23 29E | 8 16 10 11 15 5 23 10 12 12 4 | 18 23 22 19 20 18 23 21 25 20 19 30 | 6 8 6 10 18 3 8 8 12 14 3 | 28 29 32 32 31 28 28 29 29 23 27 31 | 7 21 12 16 32 6 20 9 13 17 5 | 26 37 26 31 38 24 32 25 28 26 26 32 | 8 17 10 14 24 4 17 8 10 19 4 | 16 19 23 25 32 15 15 21 19 18 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 9 13 36 5 18 12 12 17 |T 26 33 30 31 37 26 31 29 30 29 27 WRMS | 8 18 9 13 32 5 16 10 11 16 |NE 23 29 28 28 34 23 28 25 26 25 24 MEDI | 8 17 8 11 32 5 17 10 12 16 |MD 22 32 28 29 35 25 29 25 28 26 25 Table 3.1522.4 GPS week: 1522 Day: 4 MJD: 54902.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 21 7 13 22 5 19 9 14 21 5 | 18 29 21 21 29 18 27 23 25 25 18 3E | 17 19 11 12 45 6 14 22 21 31 7 | 90 87 85 86 96 88 87 94 93 81 87 4 | 7 10 8 12 31 3 9 9 11 14 3 | 17 23 27 22 24 19 24 18 22 24 18 5 | 9 11 9 12 15 4 12 9 9 13 4 | 21 22 22 24 25 20 23 23 26 19 19 6E | 12 19 11 12 55 4 15 20 16 25 6 | 40 38 33 38 42 37 37 47 44 36 36 7 | 7 21 11 12 36 6 21 10 12 18 5 | 17 31 23 18 39 16 27 15 22 20 17 8 | 8 13 7 9 23 4 11 5 12 13 3 | 19 22 22 21 28 18 23 21 22 22 19 9 | 8 10 10 10 15 4 7 12 13 15 4 | 19 21 19 23 29 19 24 21 27 20 18 10 | 6 11 8 9 21 6 9 7 10 14 3 | 21 23 25 26 32 22 23 24 27 19 22 11 | 6 16 10 10 63 4 15 10 8 15 4 | 19 29 24 20 39 20 25 20 27 25 19 12 | 10 16 9 13 28 7 21 12 12 24 5 | 20 26 21 20 35 18 30 23 27 24 19 13E | 9 18 11 19 27 4 20 13 14 12 5 | 23 30 23 31 33 23 29 27 35 24 23 14E | 10 15 9 13 30 5 16 13 13 17 4 | 16 27 20 23 31 20 23 24 27 31 19 15E | 10 20 10 18 36 5 21 15 16 16 5 | 14 25 20 31 37 18 25 23 27 26 19 16 | 7 22 10 16 27 5 22 19 25 22 6 | 18 29 19 20 29 18 30 28 21 23 18 17E | 6 16 9 9 30 4 22 13 11 7 4 | 15 26 18 19 37 17 27 20 18 16 15 18 | 10 21 11 17 34 4 21 12 13 25 5 | 20 30 29 35 33 23 32 27 25 25 24 19E | 10 19 10 14 41 5 21 20 12 14 5 | 27 34 23 30 40 28 32 32 33 26 26 20 | 6 20 8 13 43 6 21 13 12 23 5 | 26 34 30 32 40 25 31 31 29 27 26 21 | 8 21 11 10 37 4 23 12 11 17 5 | 14 28 17 18 42 14 28 15 22 12 14 22 | 11 20 11 12 50 4 19 12 11 24 5 | 25 35 31 35 35 27 34 31 30 31 28 23E | 8 26 11 18 25 4 27 14 15 16 6 | 17 31 17 20 35 15 28 20 26 15 15 24 | 6 11 10 9 20 6 9 12 14 13 4 | 17 21 19 20 22 17 22 20 23 19 17 25 | 8 18 10 13 26 5 9 10 12 26 5 | 15 30 20 18 29 15 23 21 23 32 16 26E | 10 15 9 10 56 7 15 12 12 21 4 | 46 54 55 48 62 47 59 44 49 56 49 27 | 7 12 8 6 23 5 10 9 11 12 3 | 16 20 20 18 28 17 23 17 23 20 16 28 | 6 18 8 8 43 5 18 12 13 19 4 | 16 32 23 18 48 19 31 18 18 14 17 29E | 7 19 8 11 26 5 22 12 8 15 4 | 18 26 22 17 30 17 26 20 25 21 18 30 | 7 11 7 9 24 5 10 11 11 13 3 | 27 29 30 27 26 27 29 30 31 26 27 31 | 8 20 7 14 30 6 20 13 12 21 5 | 22 27 23 21 40 18 28 18 23 19 18 32 | 8 18 9 15 29 5 18 11 10 18 4 | 17 23 23 25 34 17 21 23 18 13 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 17 9 12 35 5 17 13 13 19 |T 22 30 25 26 36 23 30 26 28 25 23 WRMS | 8 17 9 12 32 5 17 12 11 17 |NE 19 26 23 22 32 19 26 22 24 21 19 MEDI | 8 18 9 12 30 5 18 12 12 17 |MD 19 29 23 22 34 19 27 23 26 24 19 Table 3.1522.5 GPS week: 1522 Day: 5 MJD: 54903.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 9 26 5 12 24 6 20 9 12 19 4 | 19 31 18 20 26 16 23 21 26 21 18 3E | 30 23 9 14 48 14 19 19 15 19 7 | 127 128 130 127 134 133 127 129 137 132 129 4 | 5 14 5 10 25 4 14 8 8 16 3 | 14 23 35 21 25 16 19 17 23 21 18 5 | 5 14 4 10 18 5 14 10 8 12 3 | 14 18 17 20 28 17 18 20 20 15 16 6E | 15 22 8 15 62 7 17 21 18 30 6 | 43 39 39 43 35 37 36 47 46 36 39 7 | 5 21 6 15 33 4 21 10 10 18 4 | 13 30 16 19 37 14 24 14 25 19 15 8 | 8 16 5 8 17 3 11 6 10 14 3 | 21 32 23 24 31 23 30 24 30 21 23 9 | 7 12 6 8 19 5 9 10 10 16 3 | 14 21 15 17 27 15 16 16 21 19 14 10 | 6 13 6 10 20 4 11 7 9 18 3 | 19 18 20 27 20 19 17 20 26 18 20 11 | 8 17 9 11 80 6 18 10 12 17 4 | 21 30 23 29 51 21 25 22 27 26 22 12 | 9 19 6 13 36 5 20 11 8 23 4 | 17 28 20 20 40 18 26 20 22 18 18 13E | 5 18 7 13 32 6 22 18 11 11 4 | 16 25 15 20 29 17 25 24 24 21 16 14E | 9 19 8 10 28 4 23 11 9 20 4 | 16 27 17 22 29 16 23 20 25 26 18 15E | 12 22 5 22 31 4 21 10 12 15 5 | 10 24 17 30 31 15 18 19 26 21 16 16 | 7 23 6 14 25 5 28 14 11 28 5 | 23 31 21 21 36 23 32 19 33 21 22 17E | 6 16 7 9 23 5 23 15 12 9 4 | 20 28 25 22 34 20 29 19 25 21 21 18 | 10 21 5 14 42 5 23 9 10 26 5 | 21 33 26 31 35 23 31 26 26 25 24 19E | 9 21 8 13 33 7 20 17 13 14 5 | 23 33 25 26 36 25 30 22 27 24 23 20 | 5 18 7 13 42 5 23 14 12 23 5 | 28 36 30 33 39 26 30 28 28 29 27 21 | 8 22 9 11 41 6 24 11 8 17 4 | 21 30 22 27 37 22 29 23 28 23 23 22 | 10 17 5 12 50 5 20 11 8 21 4 | 25 35 28 33 31 24 31 29 26 27 26 23E | 5 26 8 15 23 5 30 15 14 16 5 | 21 32 22 23 32 18 28 23 26 23 20 24 | 6 15 6 7 38 4 14 9 7 13 3 | 20 27 25 28 30 22 23 21 30 23 24 25 | 8 18 5 11 20 5 13 17 12 27 4 | 11 26 15 16 27 13 22 19 25 30 15 26E | 7 16 6 8 53 5 15 11 11 27 4 | 40 50 45 45 64 42 52 39 45 58 44 27 | 8 13 5 6 18 6 8 8 9 16 3 | 20 30 23 24 29 25 26 23 33 29 24 28 | 6 19 6 13 40 5 19 10 9 21 4 | 19 37 23 25 45 23 34 19 30 19 22 29E | 7 22 8 12 44 7 24 9 7 11 4 | 16 23 15 16 34 12 23 16 20 16 14 30 | 6 11 4 8 24 5 12 9 8 14 3 | 21 24 24 22 29 22 24 25 24 20 22 31 | 7 20 7 12 39 5 24 10 7 17 4 | 20 33 21 24 43 21 28 19 26 24 21 32 | 6 16 5 14 29 6 18 13 12 20 4 | 11 19 16 19 27 14 13 21 16 15 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 7 12 37 6 19 12 11 19 |T 23 32 26 28 37 24 29 25 30 27 24 WRMS | 7 19 6 12 37 5 19 11 10 19 |NE 18 28 21 23 33 19 24 21 25 22 20 MEDI | 7 18 6 12 32 5 20 10 10 17 |MD 20 30 22 24 32 21 26 21 26 21 21 Table 3.1522.6 GPS week: 1522 Day: 6 MJD: 54904.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 6 23 6 13 26 3 19 8 8 18 4 | 20 32 22 25 32 20 27 21 23 25 20 3E | 12 19 5 11 47 7 14 11 16 40 5 | 148 150 147 149 169 145 149 150 149 150 147 4 | 6 12 9 8 24 5 11 9 8 12 3 | 20 25 32 26 28 20 27 23 23 25 22 5 | 5 14 5 8 16 6 10 8 10 11 3 | 23 24 27 26 26 22 22 27 28 26 24 6E | 14 21 8 12 66 5 17 19 18 29 6 | 48 45 43 46 51 45 45 53 55 47 45 7 | 7 21 8 16 29 5 21 12 9 18 5 | 20 32 25 30 40 21 28 18 27 25 22 8 | 6 13 5 10 20 6 9 15 14 12 4 | 19 28 21 23 37 21 27 27 22 23 21 9 | 6 14 7 7 20 5 9 9 10 15 3 | 20 26 19 20 29 18 21 18 24 19 18 10 | 7 15 7 11 31 6 10 8 10 22 4 | 25 26 32 35 20 28 24 28 30 24 27 11 | 8 15 7 10 66 5 15 9 15 16 4 | 22 28 23 27 54 20 25 25 26 27 23 12 | 7 19 6 10 26 8 19 9 13 24 4 | 22 31 23 21 39 21 32 22 26 21 21 13E | 6 18 9 16 33 5 20 14 10 14 4 | 17 31 17 24 36 19 27 26 26 26 20 14E | 7 21 7 10 28 4 20 10 11 26 4 | 17 27 21 20 26 17 23 21 20 27 17 15E | 10 23 8 12 40 5 23 10 16 18 5 | 12 28 17 19 30 15 26 21 22 24 16 16 | 6 21 8 11 33 5 22 11 15 34 5 | 22 32 23 19 39 22 32 21 22 31 21 17E | 9 20 8 8 28 4 23 8 14 9 4 | 18 30 22 24 40 19 30 20 26 19 20 18 | 8 20 9 13 32 5 20 8 8 27 5 | 25 34 30 38 33 27 32 31 25 32 28 19E | 10 18 9 12 34 6 19 9 12 16 4 | 37 42 34 41 48 38 38 39 44 40 37 20 | 5 18 6 13 40 6 19 10 9 26 4 | 33 39 36 43 36 33 35 41 33 32 34 21 | 7 23 10 7 48 6 23 12 11 19 5 | 18 31 22 25 44 18 28 23 21 20 20 22 | 6 19 8 12 54 5 20 12 9 23 4 | 31 39 37 43 33 32 34 37 31 35 34 23E | 7 25 9 17 23 5 26 12 11 16 5 | 26 38 29 34 33 26 36 29 32 28 26 24 | 5 12 6 7 34 5 9 9 8 11 3 | 23 28 30 32 22 25 25 27 28 26 27 25 | 7 15 5 8 20 6 8 15 11 25 4 | 15 24 20 19 31 16 19 19 23 32 17 26E | 7 16 5 13 50 6 16 9 12 28 4 | 61 70 64 61 68 61 72 59 59 71 62 27 | 8 15 5 7 20 6 10 8 10 18 3 | 18 31 24 25 29 21 27 22 19 28 22 28 | 6 22 9 11 32 5 18 8 12 21 4 | 18 35 22 21 47 19 31 17 21 22 18 29E | 8 24 12 15 26 7 23 14 11 14 5 | 17 29 19 19 26 16 24 23 23 20 18 30 | 4 13 8 7 25 5 11 7 11 15 3 | 35 34 39 35 31 31 31 35 36 35 34 31 | 8 25 9 18 31 6 23 10 15 18 5 | 25 32 27 31 39 22 29 22 24 26 23 32 | 8 15 8 13 24 6 17 16 9 18 4 | 17 22 24 29 29 18 18 27 19 20 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 8 12 35 6 18 11 12 21 |T 28 36 31 33 40 28 33 31 31 32 29 WRMS | 7 19 8 12 32 5 17 10 9 19 |NE 22 30 26 28 34 22 27 25 25 26 23 MEDI | 7 19 8 11 31 5 19 10 11 18 |MD 22 31 24 26 33 21 28 25 26 26 22 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 4.1522 GPS week: 1522 MJD: 54898.0-54904.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2975 |U 7 6 20 |U 10 11 37 |U 7 6 14 | emr | emr 2964 | 9 10 28 | 12 12 40 | 10 7 17 | esa | esa 2976 | 8 8 21 |U 10 11 38 | 8 5 15 | gfz | gfz 2928 |U 10 9 24 |U 14 16 48 | 9 7 20 | grg | grg 2976 | 8 7 22 |U 10 12 45 | 11 7 21 | igr | igr 2962 | 8 7 22 | 10 11 37 | 8 5 13 | igs | igs 2946 | 8 7 24 | 11 11 37 | 7 6 15 | jpl | jpl 2961 |U 8 8 23 |U 11 12 39 |U 10 7 17 | mit | mit 2976 |U 8 7 24 |U 13 12 48 |U 9 7 19 | 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 5.1522.0 GPS week: 1522 Day: 0 MJD: 54898.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 9 6 24 | 13 9 45 | 7 4 15 | emr | emr 2964 | 11 11 35 | 17 13 45 | 11 6 16 | esa | esa 2976 | 10 6 24 | 12 8 44 | 7 3 15 | gfz | gfz 2937 | 13 12 32 | 17 18 62 | 8 7 24 | grg | grg 2976 | 8 5 25 | 14 13 57 | 12 5 18 | igr | igr 2954 | 9 6 25 | 13 8 43 | 7 6 13 | igs | igs 2938 | 9 7 26 | 14 9 44 | 8 7 16 | jpl | jpl 2963 | 9 8 26 | 16 14 50 | 10 6 15 | mit | mit 2976 | 10 7 26 | 16 12 59 | 9 6 21 | Table 5.1522.1 GPS week: 1522 Day: 1 MJD: 54899.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 9 20 | 8 14 44 | 7 8 16 | emr | emr 2964 | 9 14 31 | 15 14 48 | 10 9 16 | esa | esa 2976 | 8 10 18 | 8 14 45 | 8 7 17 | gfz | gfz 2936 | 12 11 21 | 15 20 56 | 12 10 21 | grg | grg 2976 | 8 9 20 | 11 17 56 | 11 8 18 | igr | igr 2969 | 9 11 26 | 8 14 48 | 7 6 15 | igs | igs 2938 | 8 10 27 | 13 14 48 | 8 7 15 | jpl | jpl 2960 | 8 11 25 | 13 14 44 | 10 9 16 | mit | mit 2976 | 8 11 29 | 18 18 70 | 10 8 16 | Table 5.1522.2 GPS week: 1522 Day: 2 MJD: 54900.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 6 6 22 | 13 14 47 | 8 8 16 | emr | emr 2964 | 7 6 19 | 13 14 50 | 10 9 15 | esa | esa 2976 | 11 14 23 | 12 14 44 | 9 9 16 | gfz | gfz 2936 | 9 7 19 | 14 14 45 | 9 8 18 | grg | grg 2976 | 6 6 21 | 13 15 49 | 10 8 19 | igr | igr 2962 | 6 6 18 | 11 14 46 | 8 7 15 | igs | igs 2960 | 6 6 21 | 11 13 45 | 8 7 15 | jpl | jpl 2962 | 7 6 22 | 10 14 45 | 10 9 18 | mit | mit 2976 | 7 6 19 | 15 15 69 | 11 9 24 | Table 5.1522.3 GPS week: 1522 Day: 3 MJD: 54901.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2975 | 6 7 12 | 5 7 21 | 8 5 12 | emr | emr 2963 | 9 10 22 | 10 10 33 | 10 7 11 | esa | esa 2976 | 7 7 14 | 5 7 23 | 8 4 14 | gfz | gfz 2938 | 10 8 20 | 16 13 32 | 8 7 19 | grg | grg 2976 | 7 7 14 | 7 11 30 | 9 6 15 | igr | igr 2957 | 8 7 16 | 6 6 20 | 6 3 10 | igs | igs 2928 | 7 7 18 | 8 7 26 | 6 5 14 | jpl | jpl 2958 | 7 7 17 | 9 9 39 | 10 7 12 | mit | mit 2976 | 8 7 22 | 9 7 41 | 8 6 18 | Table 5.1522.4 GPS week: 1522 Day: 4 MJD: 54902.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 6 7 24 | 7 13 29 | 7 5 14 | emr | emr 2964 | 11 10 35 | 10 11 31 | 9 6 22 | esa | esa 2976 | 6 7 26 | 7 15 30 | 6 5 17 | gfz | gfz 2935 | 11 10 33 | 11 19 43 | 7 6 21 | grg | grg 2976 | 7 8 27 | 7 11 36 | 10 9 30 | igr | igr 2954 | 7 7 27 | 7 15 24 | 7 5 13 | igs | igs 2969 | 9 8 33 | 8 14 27 | 6 6 15 | jpl | jpl 2962 | 7 8 28 | 10 11 31 | 8 5 17 | mit | mit 2976 | 10 7 31 | 10 12 35 | 8 8 23 | Table 5.1522.5 GPS week: 1522 Day: 5 MJD: 54903.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 5 18 | 11 8 38 | 10 6 10 | emr | emr 2964 | 9 9 25 | 9 10 34 | 12 7 21 | esa | esa 2976 | 8 6 22 | 10 8 38 | 10 6 14 | gfz | gfz 2937 | 8 7 20 | 12 12 50 | 11 7 20 | grg | grg 2976 | 10 8 23 | 10 8 41 | 12 9 25 | igr | igr 2970 | 9 6 21 | 10 8 38 | 10 6 13 | igs | igs 2936 | 8 7 21 | 8 8 28 | 10 6 13 | jpl | jpl 2963 | 8 8 21 | 8 10 28 | 12 6 16 | mit | mit 2976 | 8 7 21 | 10 9 26 | 10 7 16 | Table 5.1522.6 GPS week: 1522 Day: 6 MJD: 54904.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 5 5 18 | 15 11 36 | 6 4 14 | emr | emr 2968 | 8 10 27 | 13 12 39 | 10 6 22 | esa | esa 2976 | 7 6 23 | 13 10 42 | 7 4 13 | gfz | gfz 2877 | 7 6 22 | 15 16 50 | 8 4 18 | grg | grg 2976 | 8 8 23 | 11 11 45 | 10 5 24 | igr | igr 2971 | 6 5 20 | 13 9 38 | 7 4 14 | igs | igs 2956 | 6 6 21 | 14 10 39 | 6 4 15 | jpl | jpl 2964 | 8 7 22 | 10 10 33 | 9 5 23 | mit | mit 2976 | 7 8 23 | 10 11 34 | 7 6 17 | 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 6.1522 GPS week: 1522 MJD: 54898.500-54904.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 22 -23 58 13 -4 | 3 21 | 22 35 76 92 10 | 2 emr uuuuu | 25 -58 130 161 2 | 35 43 | 27 24 98 87 15 | 4 esa uuuuu | -43 -43 82 -192 -6 | 8 30 | 28 21 110 89 10 | 8 gfz uuuuu | -4 25 7 -44 6 | 6 23 | 11 18 62 87 6 | 2 grg xxxxx | -8 -31 38 20 -22 | 2 42 | 46 58 88 101 61 | 5 igr xxxxx | 18 8 25 -21 -12 | 2 22 | 20 39 68 106 8 | 7 irf xxxxx | 13 8 -9 36 -7 | 3 22 | 12 11 19 35 12 | 6 jpl uuuuu | 39 5 -10 72 0 | -10 28 | 38 30 100 185 17 | 3 mit uuuuu | 13 3 -24 177 -13 | 18 31 | 19 30 52 33 15 | 6 ngs uuuuu | 6 42 -97 -104 0 | -4 13 | 64 46 102 126 8 | 1 sio uuuuu | -3 30 -114 135 1 | 28 35 | 20 29 125 95 15 | 4 Table 7.1522.0 GPS week: 1522 Day: 0 MJD: 54898.500 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 -28 132 -78 14 | 2 19 emr uuuuu | 41 -33 -2 90 -8 | 38 45 esa uuuuu | -37 -48 184 -147 7 | 16 34 gfz uuuuu | -7 5 91 -112 8 | 3 22 grg xxxxx | -40 -55 40 -27 -122 | 11 32 igr xxxxx | -18 4 103 -87 -15 | 10 22 irf xxxxx | 24 6 -28 43 -14 | 8 21 jpl uuuuu | 24 19 -21 204 31 | -13 26 mit uuuuu | 30 14 -109 184 -20 | 24 32 ngs uuuuu | -23 45 -71 -64 -7 | -5 13 sio uuuuu | 35 11 -330 47 -6 | 32 37 Table 7.1522.1 GPS week: 1522 Day: 1 MJD: 54899.500 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 | 37 -14 81 -83 -10 | 6 21 emr uuuuu | 58 -61 29 156 -23 | 41 47 esa uuuuu | -67 -50 110 -238 -23 | 18 35 gfz uuuuu | -5 21 29 -172 -4 | 6 23 grg xxxxx | -25 -12 66 -61 8 | -1 43 igr xxxxx | 7 -6 35 -220 -27 | 9 21 irf xxxxx | 6 -13 -19 -24 -28 | 9 22 jpl uuuuu | -9 -32 -103 173 7 | -8 27 mit uuuuu | 3 -49 -70 168 -38 | 26 33 ngs uuuuu | 29 112 46 5 13 | -4 13 sio uuuuu | 4 -8 -179 21 -24 | 33 38 Table 7.1522.2 GPS week: 1522 Day: 2 MJD: 54900.500 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 -4 -14 68 -6 | 5 21 emr uuuuu | 57 -35 78 214 -9 | 38 45 esa uuuuu | -79 -20 22 -293 -15 | 14 34 gfz uuuuu | -10 43 22 -54 3 | 6 23 grg xxxxx | -10 -5 84 21 10 | -1 43 igr xxxxx | 24 69 105 -34 -13 | 6 22 irf xxxxx | -3 2 10 17 -17 | 6 22 jpl uuuuu | 70 36 44 285 3 | -7 27 mit uuuuu | -15 -22 -10 192 -27 | 23 33 ngs uuuuu | 26 7 -82 -207 7 | -2 13 sio uuuuu | -10 8 -17 104 -13 | 30 36 Table 7.1522.3 GPS week: 1522 Day: 3 MJD: 54901.500 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 | 30 -36 81 -67 2 | 4 22 emr uuuuu | -7 -48 152 159 15 | 35 44 esa uuuuu | -48 -70 150 -219 -3 | 8 33 gfz uuuuu | -14 35 -29 -59 15 | 7 22 grg xxxxx | 49 -5 -28 56 32 | -1 43 igr xxxxx | 22 11 -61 51 -12 | 3 24 irf xxxxx | -1 12 -36 18 1 | 2 24 jpl uuuuu | 28 12 -47 135 0 | -8 28 mit uuuuu | -6 16 -44 115 -6 | 18 33 ngs uuuuu | 88 43 -91 -22 -7 | -3 13 sio uuuuu | -27 48 -189 89 12 | 25 34 Table 7.1522.4 GPS week: 1522 Day: 4 MJD: 54902.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 8 27 112 85 -2 | 3 22 emr uuuuu | 19 -55 201 81 13 | 34 42 esa uuuuu | 7 -67 211 -261 -3 | 3 27 gfz uuuuu | -16 39 -99 25 11 | 8 23 grg xxxxx | -80 56 -100 -9 11 | -1 44 igr xxxxx | 18 13 17 55 -9 | -1 22 irf xxxxx | 21 18 -4 66 4 | 0 23 jpl uuuuu | 107 12 -117 -83 -7 | -8 28 mit uuuuu | 22 39 33 165 -2 | 16 31 ngs uuuuu | -110 25 -294 53 -4 | -4 13 sio uuuuu | -2 43 -40 265 13 | 25 33 Table 7.1522.5 GPS week: 1522 Day: 5 MJD: 54903.500 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 | 55 -89 -78 150 -13 | 3 22 emr uuuuu | 14 -103 264 104 14 | 32 40 esa uuuuu | -25 -16 -74 -30 -3 | 0 25 gfz uuuuu | 12 -5 -19 93 5 | 7 23 grg xxxxx | 0 -125 180 -65 4 | 3 43 igr xxxxx | 48 -61 41 2 -2 | -4 20 irf xxxxx | 26 10 -3 61 2 | -2 21 jpl uuuuu | 29 -42 178 -249 -22 | -11 28 mit uuuuu | 33 0 27 223 -3 | 13 28 ngs uuuuu | -17 87 -63 -249 1 | -4 13 sio uuuuu | -2 32 -70 239 13 | 25 33 Table 7.1522.6 GPS week: 1522 Day: 6 MJD: 54904.500 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 | 26 -17 93 17 -15 | 0 23 emr uuuuu | -6 -74 189 327 11 | 30 38 esa uuuuu | -54 -29 -31 -155 -3 | -2 25 gfz uuuuu | 7 35 54 -25 5 | 6 22 grg xxxxx | 45 -70 24 226 -97 | 3 43 igr xxxxx | 21 24 -62 87 -7 | -7 20 irf xxxxx | 15 19 15 75 2 | -5 21 jpl uuuuu | 22 27 -2 37 -13 | -16 31 mit uuuuu | 22 24 3 192 3 | 8 24 ngs uuuuu | 48 -24 -124 -243 -3 | -6 14 sio uuuuu | -18 77 29 181 10 | 24 31