Date: Thu, 27 Nov 2008 15:42:43 +0000 From: Jim Ray Subject: [IGSREPORT-16872] Wk 1505 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <492ebff3.cRBMRsHS1IS8KVns%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 27 Nov 07:42:46 PST 2008 Message Number 16872 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1505 (Nov 09, 2008 - Nov 15, 2008) 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: igs1505[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1505[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1505[0-6].cls IGS GPS clock combination summary report. igs15057.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15057.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 | ESA | 24 YELL 0 | GFZ | 7 29 0 | MIT | 7 8 9 1 | COD | 9 DAEJ PTBB RCMN WROC 1 | EMR | DAEJ 1 | GFZ | 7 BAN2 1 | MIT | DAEJ NNOR 2 | COD | 9 2 | ESA | 8 9 25 SCH2 2 | GFZ | 7 9 2 | JPL | ZWE2 2 | MIT | 30 3 | ESA | 10 RAMO 3 | GFZ | 7 29 BAN2 FAA1 ONSA 4 | COD | MCM4 SYDN THU3 4 | EMR | MIZU 4 | ESA | DARW 4 | GFZ | 7 29 DAV1 THU3 4 | MIT | 9 HOB2 5 | COD | 8 9 24 25 5 | EMR | 4 KERG 5 | ESA | 4 8 9 24 25 5 | GFZ | 4 7 24 29 5 | GRG | 27 5 | JPL | 4 5 | MIT | 27 6 | COD | 9 24 25 27 BOR1 6 | ESA | 9 25 27 6 | GFZ | 7 13 29 KOUC NRMD 6 | JPL | 8 27 ZWE2 6 | MIT | BOR1 SYDN 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 ----+--------+--------------- 3 | ESA | 10 5 | MIT | 1 6. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G04 | 2 | | | | | | | 7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447. 8. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .4 .4 .3 -25 -21 -7 -.04 EMR | 12.1 -6.3 9.1 38 16 93 .01 ESA | 5.1 5.1 7.9 38 -42 38 .0 GFZ | .6 .7 1.4 20 -26 16 -.24 GRG | 1.1 .9 2.1 -14 -11 4 -.17 JPL | 3.3 5.6 12.8 -21 -3 14 .21 MIT | 7.0 2.1 7.5 13 -15 3 -.07 NGS | 6.2 .8 .7 22 -93 25 .0 SIO | 10.0 .3 7.5 1 -140 19 .25 9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 11. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five parts. The first, Table 1, summarizes all statistics for the week. It contains means and standard deviations over the week of satellite ephemeris and clock correction transformation parameters for each centre (table 1.1505.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1505.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 2.1505.[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 3.1505.[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 5.1505.0-6). 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 1505 summary. (Nov 09, 2008 - Nov 15, 2008) Table 1.1505.a GPS week: 1505 MJD: 54779.000-54785.000 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 244| 0 0 0 65 -29 -37 -.27 11 10 | -501 405 39 124 | 0 0 1 6 16 19 .04 | 261 429 emr 72| -1 -3 4 -69 -107 -2 .44 19 19 | -626 424 22 187 | 1 2 0 25 24 31 .05 | 2600 1377 esa 124| 1 -1 -2 -47 22 10 .21 14 11 | -680 970 31 121 | 0 0 1 16 10 14 .03 | 1025 1657 gfz 203| 0 1 1 -30 -32 66 -.10 16 16 | 91 -74 26 119 | 0 1 1 25 23 63 .04 | 281 822 grg 83| 0 0 7 38 -31 -28 1.15 45 42 | -66283 65255 1709 143169 | 0 2 2 21 34 44 .07 | 174268 172472 igr n/a| 0 0 -1 18 -55 -40 .05 6 5 | -25845 1341 26 84 | 0 0 0 11 11 10 .03 | 4573 1562 jpl 136| 0 -1 0 41 -60 22 .49 15 14 | 937 406 23 105 | 1 1 1 10 12 28 .04 | 2401 1402 mit 264| 0 0 -1 -3 -30 2 -.35 15 14 | -255 87 24 149 | 0 1 0 39 44 7 .04 | 285 316 ngs 225| 0 0 0 -31 152 -24 -.33 12 10 | 58597 1909 2015 3668 | 0 1 1 39 36 33 .09 | 192256 38415 sio 111| 0 2 0 109 37 -56 .13 23 21 | --- --- --- --- | 1 1 1 19 40 34 .04 | --- --- Table 1.1505.b GPS week : 1505 MJD: 54779.000-54785.000 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 | 0 0 0 0 0 46 0 | 2 | 5 6 6 6 6 5 6 | 3 | 4 4 4 5 5 4 5 | 4 | 6 5 6 5 6 6 7 | 5 | 4 4 4 5 5 5 4 | 6 | 4 5 5 5 5 4 4 | 7 | 5 5 6 6 6 5 5 | 8 | 6 7 6 6 6 6 5 | 9 | 7 7 7 7 8 9 10 | 10 | 4 4 4 5 4 4 4 | 11 | 5 5 5 5 6 5 5 | 12 | 5 6 6 6 6 6 5 | 13 | 5 6 6 6 6 6 6 | 14 | 6 6 6 6 6 6 6 | 15 | 6 6 6 6 6 5 5 | 16 | 6 6 7 7 8 7 6 | 17 | 6 5 6 6 6 5 5 | 18 | 6 6 6 6 5 6 6 | 19 | 6 6 6 6 6 6 6 | 20 | 5 5 5 5 6 6 5 | 21 | 6 5 5 5 6 5 6 | 22 | 6 6 6 6 6 6 6 | 23 | 6 6 6 6 6 6 6 | 24 | 6 7 6 6 6 6 7 | 25 | 6 6 6 6 6 5 6 | 26 | 4 5 4 5 5 4 4 | 27 | 5 6 5 6 7 18 6 | 28 | 6 6 6 7 7 6 6 | 29 | 6 6 6 5 5 5 5 | 30 | 4 5 5 5 5 5 4 | 31 | 6 6 7 6 7 6 6 | 32 | 6 6 6 6 6 6 6 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1505.0 GPS week: 1505 Day: 0 MJD: 54779.000 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 244| 0 0 1 65 -37 -20 -.24 11 10 | -519 232 46 129 | -21 1 | emr 72| 1 -1 4 -87 -103 -15 .50 17 17 | -4868 974 23 178 | 5 47 | esa 124| 0 0 -1 -64 20 21 .21 12 12 | -218 846 34 127 | -8 -7 | gfz 203| 0 2 4 -35 -16 148 -.07 16 16 | -287 458 29 127 | -3 -18 | grg 83| 0 -1 4 36 37 -58 1.24 47 45 | -528 207 105 335 | -2 -60 | igr n/a| 0 0 -1 19 -64 -55 .12 6 6 | -33141 1900 29 86 | -38 9 | jpl 136| -2 -1 -1 42 -70 48 .54 15 15 | -3168 1251 25 102 | -4 68 | mit 264| 0 0 0 -1 -84 -1 -.40 14 14 | -636 273 24 139 | 23 1 | ngs 225| 0 -1 -2 -2 185 -74 -.29 10 8 | -77303 72221 2451 3895 | -2 -99 | sio 111| 0 0 -2 133 -22 -120 .21 23 19 | --- --- --- --- | -25 -26 | Table 2.1505.1 GPS week: 1505 Day: 1 MJD: 54780.000 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 244| 0 1 1 78 -30 -46 -.28 11 10 | -377 96 45 132 | -44 33 | emr 72| -1 -1 4 -95 -90 40 .46 17 17 | -3699 2243 21 205 | 27 45 | esa 124| 0 0 -3 -57 5 37 .23 11 11 | -1598 1280 36 121 | -5 -42 | gfz 203| 1 0 2 -56 -23 20 -.12 17 17 | 452 -1818 28 123 | -15 20 | grg 83| 0 3 7 49 -34 -3 1.14 46 40 | -391 71 108 355 | -23 71 | igr n/a| 0 0 -1 13 -52 -29 .06 5 5 | -31091 3466 25 71 | -26 4 | jpl 136| -1 0 0 36 -58 -9 .54 14 14 | -1669 2355 26 122 | -30 -10 | mit 264| 0 -1 -1 10 21 -4 -.41 16 16 | -242 -30 24 164 | 24 -24 | ngs 225| -1 0 -3 10 117 -7 -.44 12 10 | -386 66 1989 3377 | 14 -9 | sio 111| 0 0 0 109 54 -73 .18 22 21 | --- --- --- --- | 0 -12 | Table 2.1505.2 GPS week: 1505 Day: 2 MJD: 54781.000 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 244| -1 0 0 54 -13 -27 -.25 12 10 | -946 1073 45 149 | -2 -17 | emr 72| 0 -1 3 -100 -110 27 .49 18 18 | -109 2086 22 198 | 19 56 | esa 124| 1 -3 -4 -53 35 5 .19 12 12 | -2183 4025 33 112 | -5 -26 | gfz 203| 1 3 1 8 -22 -28 -.09 15 15 | -42 374 26 116 | -40 7 | grg 83| 0 1 8 -3 -57 -44 1.09 46 41 | -944 1025 111 405 | 43 16 | igr n/a| 0 1 0 4 -43 -42 .06 5 5 | -26249 3257 29 70 | -53 -1 | jpl 136| 0 -2 2 28 -42 68 .52 15 15 | 1891 1951 27 105 | -16 2 | mit 264| 0 -1 -2 68 -73 -2 -.35 14 14 | -45 407 24 163 | -2 0 | ngs 225| 0 2 0 -65 164 -26 -.40 13 10 | -937 1028 2091 3957 | 54 -139 | sio 111| 0 1 0 131 11 -50 .12 22 21 | --- --- --- --- | 14 -31 | Table 2.1505.3 GPS week: 1505 Day: 3 MJD: 54782.000 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 244| 0 1 0 64 -4 -54 -.31 11 10 | -184 615 49 143 | -58 -11 | emr 72| -4 -4 3 -68 -87 2 .38 18 18 | 1032 -424 27 205 | 20 52 | esa 124| 1 -1 -1 -23 17 0 .17 31 12 | 926 -1050 40 148 | -7 16 | gfz 203| 0 1 0 -57 -57 80 -.12 16 16 | 36 178 30 123 | -35 45 | grg 83| 1 -3 8 62 -29 -75 1.15 43 43 | -199 574 117 383 | -101 -30 | igr n/a| 0 0 -1 26 -40 -32 .02 6 5 | -23903 497 27 94 | -30 40 | jpl 136| 0 -1 1 48 -53 28 .46 15 14 | 2802 -878 29 111 | 41 45 | mit 264| 0 0 -3 -64 -64 3 -.37 15 15 | 162 -330 31 159 | 41 -21 | ngs 225| 0 1 0 18 214 -46 -.19 14 13 | -199 575 2049 3285 | -17 -125 | sio 111| 1 3 0 96 16 -27 .10 23 22 | --- --- --- --- | -33 -46 | Table 2.1505.4 GPS week: 1505 Day: 4 MJD: 54783.000 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 244| 0 0 0 67 -50 -54 -.31 11 9 | -261 -265 46 118 | -30 49 | emr 72| -2 -7 3 -35 -89 -7 .46 20 20 | 1411 94 22 165 | -30 39 | esa 124| 2 0 -1 -55 34 11 .19 11 11 | -853 767 37 128 | -27 -28 | gfz 203| 0 1 2 -45 -7 19 -.15 16 16 | 422 -199 27 110 | -9 35 | grg 83| 0 0 5 28 -67 -33 1.22 43 42 | 83 -1893 105 394 | -10 101 | igr n/a| 0 0 0 8 -56 -30 .04 5 5 | -22529 770 26 97 | -50 32 | jpl 136| 0 -2 0 58 -56 20 .50 15 14 | 2834 -302 20 89 | -64 14 | mit 264| 0 1 -2 -13 -28 8 -.30 17 17 | -125 -153 25 144 | 22 -41 | ngs 225| 0 0 -1 -41 137 35 -.39 15 13 | -277 -331 1631 3457 | -60 31 | sio 111| 0 4 0 83 73 -66 .11 23 21 | --- --- --- --- | -12 -61 | Table 2.1505.5 GPS week: 1505 Day: 5 MJD: 54784.000 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 244| 0 0 -1 66 -45 -52 -.28 11 9 | -691 581 19 89 | -22 38 | emr 72| -3 -4 4 -46 -114 -11 .42 20 20 | 1685 -748 20 160 | -5 74 | esa 124| 0 -2 -2 -52 25 -7 .25 11 11 | -63 -633 20 105 | -12 5 | gfz 203| 0 0 0 -24 -72 115 -.05 17 17 | 209 -111 23 129 | -36 60 | grg 83| 0 0 7 51 -48 59 1.04 44 39 | -461486 456380 11309 999999 | 51 119 | igr n/a| 0 -1 -1 19 -68 -47 .04 6 5 | -21603 -94 24 92 | -55 48 | jpl 136| 1 0 0 43 -60 0 .46 15 14 | 2634 -723 20 117 | -38 68 | mit 264| 0 2 0 -10 8 15 -.32 14 13 | -329 -80 22 132 | 15 -45 | ngs 225| 1 0 2 -67 121 -27 -.29 12 9 | 489728 -60518 2068 4189 | 105 21 | sio 111| 1 4 -1 119 94 -19 .10 23 20 | --- --- --- --- | -17 -71 | Table 2.1505.6 GPS week: 1505 Day: 6 MJD: 54785.000 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 244| 0 0 -2 63 -23 -7 -.20 11 9 | -532 503 23 110 | -19 27 | emr 72| -1 -1 3 -50 -156 -56 .40 20 20 | 165 -1254 21 199 | 4 136 | esa 124| 1 -1 0 -24 19 7 .23 12 11 | -774 1560 23 112 | -46 -18 | gfz 203| 1 0 1 -3 -30 111 -.07 17 17 | -147 597 23 110 | -54 35 | grg 83| 1 0 11 45 -19 -42 1.14 47 41 | -519 425 110 312 | 12 19 | igr n/a| 0 0 -1 37 -66 -47 .05 6 6 | -22403 -408 24 84 | -76 46 | jpl 136| -1 2 1 34 -82 -2 .43 16 16 | 1240 -807 20 94 | -47 -2 | mit 264| -1 1 0 -9 7 -1 -.30 15 13 | -576 525 22 144 | 23 -57 | ngs 225| 0 -1 0 -70 126 -22 -.28 11 9 | -447 325 1830 3518 | 114 39 | sio 111| -2 3 0 94 38 -40 .12 24 23 | --- --- --- --- | -7 -38 | 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 3.1505.0 GPS week: 1505 Day: 0 MJD: 54779.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 6 --- --- --- --- 188 --- --- --- --- 0 | 61 --- --- --- --- 136 --- --- --- --- 59 2E | 10 18 13 13 62 4 18 13 9 23 5 | 25 30 29 32 57 24 32 19 25 21 25 3 | 8 11 8 11 50 5 10 8 8 18 3 | 30 29 31 31 39 30 34 31 28 35 29 4E | 17 15 19 12 54 5 17 21 9 12 6 | 129 133 133 132 160 129 136 131 130 131 132 5 | 8 10 10 12 43 4 11 12 8 18 4 | 28 28 29 30 25 27 34 31 30 22 28 6 | 7 13 7 12 28 5 8 8 7 15 3 | 29 32 35 32 30 31 37 28 26 34 30 7E | 12 20 11 14 32 5 15 12 9 18 5 | 18 28 22 26 38 20 30 16 21 17 20 8E | 12 21 12 17 42 8 15 14 9 30 6 | 53 59 56 57 69 55 59 53 52 65 54 9E | 20 18 12 14 77 8 18 19 10 33 6 | 56 55 54 60 47 52 53 51 56 42 52 10 | 8 10 8 12 26 5 8 12 10 13 4 | 20 24 27 25 29 19 24 19 23 23 22 11 | 13 17 8 18 61 6 12 13 7 23 5 | 18 22 15 27 56 18 20 23 22 25 18 12 | 11 16 14 15 34 7 16 14 10 24 5 | 27 26 26 29 37 24 28 29 28 25 25 13 | 12 18 11 20 53 5 16 13 8 17 5 | 23 32 24 28 48 23 32 25 27 23 24 14 | 6 14 16 21 53 6 13 17 12 21 5 | 20 28 27 28 41 22 29 22 23 30 22 15 | 10 18 15 19 38 8 22 13 12 23 6 | 19 30 26 29 38 25 30 20 24 17 22 16 | 12 16 12 16 82 6 17 13 14 35 6 | 26 34 30 32 74 28 36 24 25 32 26 17 | 10 18 12 19 60 10 17 10 11 26 5 | 28 41 34 39 69 33 44 25 31 33 32 18 | 9 21 15 21 30 7 18 14 14 18 6 | 23 36 26 38 39 30 35 22 25 31 26 19 | 11 18 10 20 34 8 16 13 11 28 5 | 16 30 16 31 43 19 31 16 19 24 19 20 | 9 18 12 18 36 5 18 12 9 17 5 | 16 31 20 29 39 21 29 17 20 21 20 21E | 10 25 13 15 30 5 14 13 11 14 5 | 18 32 17 27 39 20 28 20 21 21 20 22 | 10 18 14 19 34 6 16 15 11 16 5 | 22 36 26 35 46 26 36 23 25 31 26 23 | 13 20 15 17 29 5 18 13 9 19 5 | 20 33 25 27 34 22 32 23 24 27 22 24E | 18 15 13 14 78 6 16 18 13 22 6 | 39 42 39 46 63 38 44 43 42 44 40 25E | 14 26 10 14 67 6 15 17 14 18 6 | 16 31 18 22 25 18 26 23 25 19 19 26 | 10 13 9 13 27 7 10 10 11 15 4 | 19 25 25 26 32 23 24 22 26 21 22 27E | 13 16 9 18 53 5 11 12 11 22 5 | 33 33 34 38 47 32 31 34 36 19 33 28 | 9 17 14 16 33 5 19 11 11 39 6 | 33 40 36 32 40 31 40 33 30 27 33 29 | 9 17 10 16 38 8 18 11 9 33 5 | 20 29 19 31 47 20 32 20 15 28 20 30 | 9 11 10 19 26 3 9 10 8 19 4 | 35 31 38 35 34 34 36 38 36 32 34 31E | 8 24 16 17 32 8 18 14 9 21 6 | 16 31 22 28 57 20 31 15 19 22 20 32 | 11 17 12 15 25 5 18 17 8 32 6 | 18 21 25 23 24 17 23 19 20 38 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 17 12 16 47 6 15 14 10 23 |T 29 35 31 35 47 33 36 29 30 31 31 WRMS | 10 17 12 16 45 6 15 14 8 19 |NE 25 30 26 30 41 29 31 24 25 27 26 MEDI | 10 17 12 16 38 6 16 13 10 21 |MD 23 31 26 31 40 24 32 23 25 27 25 Table 3.1505.1 GPS week: 1505 Day: 1 MJD: 54780.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 7 --- --- --- --- 46 --- --- --- --- 0 | 28 --- --- --- --- 47 --- --- --- --- 28 2E | 10 18 11 13 50 5 18 15 13 23 5 | 17 30 24 20 42 20 25 28 18 27 19 3 | 6 12 9 13 36 4 11 9 10 19 4 | 33 38 38 37 41 37 39 35 33 39 35 4E | 12 14 9 13 43 6 11 14 12 15 4 | 113 118 119 117 122 116 119 115 116 119 116 5 | 7 12 7 15 39 4 7 14 10 14 4 | 21 28 26 24 22 26 25 29 27 28 24 6 | 7 15 9 12 30 5 12 9 13 18 4 | 20 32 28 25 31 25 30 19 20 27 22 7E | 11 19 13 15 24 5 13 13 10 16 5 | 15 26 20 21 32 18 21 18 15 19 16 8E | 15 21 12 22 51 5 18 17 15 32 6 | 71 68 73 66 76 69 66 70 69 79 68 9E | 27 20 9 14 58 8 15 14 12 27 6 | 49 50 45 52 35 48 47 49 50 41 46 10 | 6 10 8 10 24 4 7 14 16 12 4 | 12 22 23 19 27 14 18 15 18 19 14 11 | 11 13 11 19 81 5 10 14 12 19 5 | 18 23 16 27 51 18 21 24 24 24 18 12 | 12 15 9 17 46 5 14 19 11 23 5 | 18 27 24 29 33 23 28 24 26 23 21 13 | 11 18 14 20 49 7 15 17 13 17 5 | 17 34 22 28 47 20 26 18 16 21 18 14 | 9 18 9 22 47 5 17 22 14 18 6 | 20 37 25 25 43 24 30 26 26 25 23 15 | 11 16 13 20 30 5 18 17 10 22 5 | 17 27 21 27 40 20 28 19 13 20 17 16 | 13 17 11 16 54 7 15 17 11 32 6 | 19 28 24 24 40 22 29 23 20 23 20 17 | 9 15 11 18 52 5 15 12 13 22 5 | 27 41 33 31 53 30 38 25 27 27 28 18 | 11 21 10 17 29 6 17 14 13 23 5 | 21 35 28 32 48 26 34 25 27 30 25 19 | 8 16 12 20 28 5 16 16 12 26 5 | 13 29 18 26 35 18 28 15 17 22 16 20 | 9 15 14 18 41 4 14 15 8 17 5 | 14 29 18 26 40 18 24 16 19 21 16 21E | 11 19 11 13 26 4 12 14 11 17 5 | 17 27 20 25 36 19 23 21 22 19 19 22 | 12 16 12 19 32 6 16 19 11 19 5 | 23 35 28 31 52 26 32 28 29 30 26 23 | 11 21 15 16 29 7 15 17 14 20 6 | 14 35 21 24 38 19 26 18 18 21 16 24E | 19 19 12 17 64 7 18 22 17 19 6 | 37 41 38 43 51 38 37 36 44 35 36 25E | 13 25 9 13 73 8 12 21 13 18 6 | 15 30 14 17 34 16 23 24 20 21 15 26 | 7 14 8 14 19 3 9 14 13 16 4 | 14 28 20 22 29 21 22 21 21 21 17 27E | 11 14 10 14 53 6 13 17 13 28 5 | 35 37 35 37 40 35 28 38 42 27 34 28 | 10 16 11 19 37 5 16 11 13 36 6 | 28 37 33 33 36 29 35 29 28 28 29 29 | 10 16 9 14 47 6 17 14 11 27 5 | 17 26 17 23 35 19 25 18 23 24 17 30 | 9 13 7 19 29 4 9 14 11 17 4 | 24 28 26 26 28 27 24 31 28 30 24 31E | 8 21 13 13 76 5 18 19 14 27 6 | 19 27 21 21 79 20 28 21 23 25 19 32 | 9 18 12 20 32 4 16 11 8 31 5 | 14 22 19 19 27 14 24 18 14 40 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 17 11 17 46 5 14 16 12 22 |T 25 35 29 31 43 28 32 28 28 30 26 WRMS | 10 17 11 17 40 5 14 16 10 21 |NE 19 30 24 26 37 23 27 22 22 25 21 MEDI | 10 16 11 16 41 5 15 14 12 19 |MD 19 30 24 26 40 22 28 24 23 25 20 Table 3.1505.2 GPS week: 1505 Day: 2 MJD: 54781.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 17 --- --- --- --- 0 | 40 --- --- --- --- 39 --- --- --- --- 38 2E | 9 18 14 12 49 7 19 13 12 24 5 | 20 32 28 29 40 23 28 24 19 22 23 3 | 8 12 9 10 33 3 12 10 13 18 4 | 30 37 39 35 32 35 39 28 31 37 33 4E | 14 23 12 11 28 6 12 12 13 18 5 | 72 81 72 75 80 76 79 78 73 77 75 5 | 6 12 7 14 31 4 11 13 11 17 4 | 22 24 23 24 20 22 22 28 25 24 22 6 | 6 14 9 12 30 3 12 12 14 16 4 | 22 30 33 30 28 26 29 25 23 29 26 7E | 13 23 13 13 29 4 16 13 10 18 5 | 22 35 28 30 33 27 27 26 29 24 25 8E | 15 16 10 15 65 5 17 16 13 26 5 | 54 56 55 55 54 53 51 50 52 56 52 9E | 26 18 11 12 80 8 15 12 17 29 6 | 41 41 35 43 46 38 36 41 45 30 37 10 | 8 10 8 10 14 4 8 13 10 15 3 | 16 24 24 22 26 20 22 20 21 20 19 11 | 11 15 14 16 51 4 11 13 12 15 5 | 26 29 21 30 38 23 22 27 25 26 22 12 | 9 14 12 15 46 5 14 14 12 25 5 | 25 28 26 29 39 25 26 27 31 25 25 13 | 11 16 14 20 46 6 15 15 11 18 5 | 23 32 25 28 41 24 28 22 23 22 22 14 | 8 14 14 20 45 6 18 16 14 18 5 | 17 30 23 29 45 22 28 23 22 25 21 15 | 9 16 11 17 34 5 18 16 11 20 5 | 15 29 18 27 35 22 27 19 16 17 18 16 | 14 19 13 16 47 6 22 21 14 33 7 | 23 32 28 30 42 26 33 26 24 31 24 17 | 11 30 13 16 42 3 14 12 14 23 6 | 19 41 24 29 45 22 29 19 24 24 22 18 | 10 21 13 16 28 5 18 14 14 24 6 | 23 34 25 32 44 26 32 22 20 33 24 19 | 12 19 13 18 31 5 17 15 17 24 6 | 21 34 22 35 33 26 32 24 27 25 24 20 | 10 16 14 18 36 5 12 12 9 16 5 | 16 31 23 29 40 21 25 19 20 24 19 21E | 10 20 13 11 50 5 13 13 13 16 5 | 21 30 17 28 42 24 24 23 24 26 21 22 | 10 15 12 19 25 5 17 16 13 21 5 | 17 29 22 31 43 23 27 22 19 29 21 23 | 13 22 16 17 28 6 19 13 12 22 6 | 17 34 24 28 36 21 28 19 19 24 19 24E | 19 16 11 12 67 5 17 18 15 19 6 | 30 32 31 34 37 31 30 35 35 32 30 25E | 12 27 10 14 58 5 14 21 15 19 6 | 18 33 19 24 29 21 23 27 25 20 19 26 | 9 10 8 11 22 4 14 14 11 15 4 | 16 27 19 24 28 20 25 22 22 20 19 27E | 15 15 9 12 50 5 15 15 10 23 5 | 30 32 31 33 32 31 24 33 31 21 28 28 | 9 14 11 14 40 7 17 10 13 37 5 | 26 32 30 30 36 29 31 28 28 28 27 29 | 11 16 11 15 67 5 17 12 13 25 5 | 21 29 21 31 50 25 28 24 20 24 22 30 | 6 18 8 17 30 6 10 14 11 18 4 | 31 29 30 29 26 27 26 35 31 33 28 31E | 11 25 13 11 86 5 20 20 15 28 6 | 22 32 26 28 78 21 33 21 26 25 24 32 | 7 19 12 17 28 5 14 10 10 31 5 | 16 23 24 24 30 18 21 20 18 38 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 18 12 15 46 5 15 14 13 22 |T 25 33 27 31 39 27 30 27 27 28 26 WRMS | 10 18 12 15 41 5 15 14 10 21 |NE 21 30 24 28 36 24 27 23 23 26 23 MEDI | 10 16 12 15 40 5 15 13 13 20 |MD 22 32 25 29 38 24 28 24 24 25 23 Table 3.1505.3 GPS week: 1505 Day: 3 MJD: 54782.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 7 --- --- --- --- 51 --- --- --- --- 0 | 36 --- --- --- --- 39 --- --- --- --- 37 2E | 10 21 12 19 52 6 19 17 16 22 6 | 20 34 22 29 40 22 28 18 22 22 21 3 | 8 12 10 14 62 4 8 13 14 18 4 | 34 39 34 34 53 33 36 32 30 40 33 4E | 14 18 12 15 44 6 13 12 12 20 5 | 107 112 111 108 132 110 113 106 112 105 109 5 | 8 14 8 12 33 4 10 15 12 18 4 | 27 25 26 22 22 24 27 33 33 23 26 6 | 6 14 8 14 47 4 7 14 14 17 4 | 24 30 28 22 34 26 28 28 25 36 25 7E | 13 22 12 11 27 6 15 17 12 19 5 | 18 31 21 23 32 22 29 18 27 19 19 8E | 16 17 12 13 53 5 15 17 16 27 6 | 69 74 74 65 69 70 69 72 70 73 70 9E | 25 22 11 17 68 7 17 15 17 28 7 | 47 52 47 53 57 50 48 50 51 42 46 10 | 9 12 162 13 19 5 7 14 18 15 5 | 18 24 138 23 28 19 22 18 14 24 18 11 | 13 16 10 20 49 4 11 14 12 17 5 | 20 27 20 27 50 20 21 25 20 24 19 12 | 10 19 10 13 32 6 20 15 16 29 6 | 25 30 30 29 34 26 32 26 33 23 26 13 | 12 18 14 19 47 5 17 14 10 20 5 | 20 33 19 25 44 21 30 22 23 23 20 14 | 7 23 11 21 44 6 15 15 18 18 6 | 18 33 25 26 37 22 28 23 28 27 22 15 | 10 17 13 20 33 5 19 18 14 25 6 | 19 31 26 30 34 23 31 23 20 23 21 16 | 13 19 12 16 41 6 19 24 15 35 7 | 23 33 26 26 42 25 34 26 26 25 23 17 | 11 16 14 15 41 7 15 15 15 19 5 | 21 36 26 27 54 28 34 22 27 26 25 18 | 8 20 14 16 22 7 15 12 17 19 5 | 24 35 27 33 39 28 32 22 28 31 26 19 | 10 17 11 20 33 7 15 13 12 24 5 | 20 34 18 28 38 22 29 17 23 23 20 20 | 12 15 11 17 29 6 15 13 14 16 5 | 16 30 19 26 39 21 30 17 21 20 19 21E | 8 22 11 12 25 5 13 13 14 18 5 | 29 37 30 27 49 30 34 28 31 28 29 22 | 8 18 13 20 28 6 14 14 18 17 5 | 23 32 30 31 46 27 32 24 28 30 26 23 | 11 21 15 17 28 5 19 13 11 21 6 | 18 33 25 25 39 23 31 20 25 24 21 24E | 16 16 11 14 64 5 15 17 17 22 6 | 40 43 43 42 55 42 42 43 44 41 41 25E | 12 19 10 14 62 7 12 23 14 26 6 | 17 30 21 19 32 18 24 25 27 21 19 26 | 9 13 13 16 23 4 10 14 14 22 5 | 18 26 25 24 27 19 21 24 19 21 19 27E | 14 16 10 13 57 4 13 19 13 23 5 | 31 34 30 31 38 30 27 31 36 19 29 28 | 11 16 14 14 38 5 20 13 18 40 6 | 26 34 29 29 47 27 37 27 30 24 28 29 | 9 15 11 15 49 7 15 12 14 25 5 | 19 24 22 25 49 21 29 17 25 21 20 30 | 7 15 8 17 27 5 10 13 10 22 4 | 33 32 34 30 28 33 31 37 40 29 32 31E | 9 25 12 21 52 6 16 17 14 19 6 | 23 34 25 30 58 25 33 23 30 25 25 32 | 11 22 7 17 37 4 18 15 13 33 6 | 18 26 21 22 29 19 28 17 22 41 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 18 31 16 43 6 15 15 14 23 |T 28 36 34 31 44 30 34 29 31 30 29 WRMS | 10 18 12 16 43 5 14 15 13 22 |NE 22 30 30 26 38 24 29 23 25 26 23 MEDI | 10 17 11 16 41 5 15 14 14 21 |MD 23 33 26 27 39 25 31 24 27 24 25 Table 3.1505.4 GPS week: 1505 Day: 4 MJD: 54783.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 7 --- --- --- --- 31 --- --- --- --- 0 | 28 --- --- --- --- 28 --- --- --- --- 30 2E | 10 25 11 15 55 6 16 16 15 23 6 | 16 30 18 20 38 15 21 20 21 22 16 3 | 8 15 12 14 49 4 8 17 15 20 5 | 24 28 25 25 35 24 26 28 22 30 22 4E | 15 23 8 13 33 7 13 14 14 18 5 | 54 66 57 58 60 56 60 56 59 69 57 5 | 6 15 6 14 37 3 10 18 16 19 4 | 14 19 18 17 21 14 17 22 20 23 14 6 | 6 16 10 15 41 5 8 17 12 19 4 | 21 29 29 21 29 22 27 28 22 29 22 7E | 12 24 12 15 31 5 15 19 15 16 5 | 16 29 17 20 34 17 24 17 25 22 15 8E | 13 19 13 12 65 5 16 21 15 26 6 | 45 47 48 45 64 44 52 49 44 53 46 9E | 25 25 11 16 84 6 17 21 28 33 8 | 49 50 42 49 41 45 45 56 59 46 45 10 | 7 14 6 11 29 4 8 17 12 13 4 | 13 19 43 22 24 14 18 18 20 16 14 11 | 12 19 10 20 62 5 10 18 15 15 5 | 22 30 24 29 51 22 22 27 28 27 21 12 | 11 16 11 16 44 5 17 15 19 30 6 | 22 26 25 26 30 21 26 23 28 26 21 13 | 12 21 12 21 47 4 17 15 15 16 6 | 18 32 18 25 41 18 26 18 22 17 16 14 | 7 23 10 23 38 4 16 19 15 17 6 | 17 33 22 25 37 20 25 20 19 21 18 15 | 8 20 12 18 34 6 16 17 11 23 5 | 15 30 18 27 34 20 27 18 21 17 16 16 | 12 22 14 18 45 5 19 27 15 42 7 | 19 35 20 25 41 22 31 30 23 31 20 17 | 11 16 12 16 39 6 12 15 13 23 5 | 11 26 22 25 37 20 29 17 22 24 18 18 | 9 20 9 15 25 6 18 13 13 18 5 | 16 29 21 28 38 21 29 18 20 28 19 19 | 9 20 9 18 29 4 15 15 12 26 5 | 16 35 17 28 34 22 28 19 25 19 19 20 | 10 19 13 20 25 5 16 13 13 13 5 | 17 32 19 29 36 21 27 17 19 23 18 21E | 10 22 12 19 25 5 13 12 15 15 5 | 18 31 17 31 36 21 23 21 26 27 20 22 | 9 20 13 19 29 6 18 13 15 18 5 | 15 29 22 27 44 20 27 20 23 30 20 23 | 11 22 15 18 22 5 20 14 14 18 6 | 16 32 21 23 30 17 28 16 22 20 16 24E | 18 18 8 12 57 6 16 19 18 18 6 | 27 35 23 33 40 26 30 29 35 34 27 25E | 11 16 9 15 78 5 14 25 15 17 5 | 10 22 14 18 39 14 21 23 25 15 13 26 | 7 15 8 13 24 6 10 16 10 20 4 | 13 26 19 23 25 18 19 21 23 15 15 X27E | 13 19 11 15 63 6 --- 20 16 22 6 | 16 20 19 25 33 15 --- 25 37 22 16 28 | 12 17 10 17 28 6 18 16 13 40 6 | 21 28 23 26 35 22 31 22 25 26 21 29 | 8 16 9 14 42 7 16 14 15 25 5 | 13 23 11 22 39 15 21 12 17 17 13 30 | 6 16 5 15 37 4 11 18 13 23 4 | 22 25 23 17 23 21 22 29 26 25 21 31E | 9 31 13 15 32 6 19 19 17 22 6 | 15 33 25 21 49 18 27 18 24 23 19 32 | 9 26 11 16 33 7 18 18 12 31 6 | 18 31 18 21 25 18 25 17 17 41 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 20 11 16 43 5 15 17 15 23 |T 20 30 23 26 36 22 27 24 26 27 21 WRMS | 9 20 11 16 42 5 14 17 13 21 |NE 17 28 21 24 33 20 25 20 22 24 18 MEDI | 10 19 11 15 37 5 16 17 15 20 |MD 17 30 21 25 36 20 26 21 23 24 19 Table 3.1505.5 GPS week: 1505 Day: 5 MJD: 54784.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 43 --- --- --- --- 55 --- 504 49 --- 46 | 32 --- --- --- --- 53 --- 4 5 --- 44 2E | 7 22 10 16 50 5 13 10 10 21 5 | 20 33 27 31 33 24 25 24 21 27 23 3 | 7 13 12 12 43 4 8 12 7 18 4 | 33 40 37 38 39 37 41 32 35 38 35 4E | 15 22 11 15 60 7 17 12 13 14 5 | 109 110 115 114 122 111 113 115 113 117 112 5 | 7 15 7 15 46 5 9 12 10 22 4 | 22 24 23 21 28 21 22 26 24 25 21 6 | 5 16 12 12 28 4 9 10 8 14 4 | 21 28 27 26 30 24 28 22 23 27 22 7E | 12 22 11 15 25 6 17 11 8 14 5 | 15 26 15 21 27 16 22 15 15 20 14 8E | 13 25 11 17 60 5 14 16 12 23 6 | 59 60 62 57 68 60 59 60 63 59 58 9E | 27 22 19 19 90 7 18 29 20 32 8 | 55 55 49 56 46 54 52 71 59 57 53 10 | 7 14 9 11 27 6 9 13 11 10 4 | 11 19 23 18 23 12 16 13 16 13 12 11 | 13 16 12 22 51 4 11 14 10 16 5 | 19 28 24 31 37 23 21 26 23 25 21 12 | 10 19 10 18 42 6 15 11 14 33 5 | 23 26 25 27 30 22 25 21 23 23 20 13 | 11 20 12 20 43 5 18 13 11 15 5 | 20 33 21 26 40 23 29 18 20 16 18 14 | 9 21 12 19 45 6 17 14 10 15 5 | 15 34 22 27 38 20 25 22 22 22 19 15 | 7 19 10 17 27 6 16 15 10 22 5 | 15 29 21 27 33 21 29 20 17 18 18 16 | 10 21 14 17 44 6 19 17 12 37 6 | 15 29 22 23 33 19 27 19 17 19 16 17 | 11 13 10 19 24 5 15 12 10 20 5 | 16 27 24 28 32 23 30 18 24 25 21 18 | 9 23 10 16 24 8 19 14 13 25 5 | 15 30 17 26 35 20 28 17 19 30 16 19 | 9 20 13 17 30 5 14 12 11 28 5 | 17 34 19 29 32 23 30 18 19 22 19 20 | 10 20 10 26 28 5 15 11 13 12 5 | 16 29 19 30 33 21 24 14 17 18 17 21E | 10 22 10 17 34 7 12 12 9 20 5 | 17 31 17 27 34 19 22 24 21 32 19 22 | 9 18 13 19 23 8 16 11 18 18 5 | 14 29 20 25 46 18 28 18 24 27 18 23 | 10 23 13 23 21 5 20 12 13 20 6 | 19 34 23 25 36 21 28 16 17 18 17 24E | 16 21 11 13 59 5 18 17 10 20 6 | 39 47 39 45 50 42 41 46 45 44 41 25E | 11 20 9 13 69 6 15 17 12 16 5 | 12 24 12 17 28 13 20 19 19 16 11 26 | 7 14 7 13 26 5 9 13 8 19 4 | 12 24 18 18 25 16 18 19 18 14 14 X27E | 22 28 26 24 77 16 --- 31 72 --- 17 | 26 41 39 28 80 31 --- 29 82 --- 35 28 | 12 16 10 19 48 7 18 11 11 36 6 | 22 30 20 28 41 22 31 22 19 21 21 29 | 9 16 9 14 50 7 17 11 14 27 5 | 10 21 11 19 31 12 21 12 14 16 9 30 | 8 15 7 16 45 4 9 10 13 23 4 | 22 23 23 18 24 20 19 24 24 22 19 31E | 8 28 12 21 40 6 18 14 14 23 6 | 18 36 25 37 54 23 28 23 25 26 22 32 | 10 26 10 17 32 4 15 18 13 30 6 | 19 28 21 24 29 20 25 18 21 39 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 20 11 17 44 6 15 14 12 23 |T 24 34 27 31 39 27 30 26 28 29 25 WRMS | 9 20 11 17 39 5 14 13 9 20 |NE 18 28 21 25 33 22 25 19 20 22 19 MEDI | 10 20 11 17 43 6 15 12 11 20 |MD 19 29 23 27 33 21 27 20 21 23 19 Table 3.1505.6 GPS week: 1505 Day: 6 MJD: 54785.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 33 --- --- --- --- 0 | 43 --- --- --- --- 51 --- --- --- --- 41 2 | 7 21 10 13 52 5 16 15 11 29 5 | 24 39 30 31 47 26 28 29 24 33 26 3 | 6 13 10 12 47 5 11 9 9 28 4 | 32 35 36 35 46 34 35 30 31 43 33 4 | 12 31 10 23 61 7 15 13 12 27 6 | 88 95 84 92 115 86 88 88 95 75 87 5 | 8 11 7 15 37 7 12 9 11 20 4 | 25 24 28 24 26 24 29 31 29 34 26 6 | 5 15 10 12 27 5 11 9 8 24 4 | 28 30 34 30 32 30 30 28 30 36 29 7E | 10 24 11 9 20 5 17 12 10 13 5 | 18 31 21 24 32 21 28 17 26 20 19 8E | 11 21 9 13 66 5 16 13 9 23 5 | 80 81 81 80 85 80 77 83 83 79 80 9E | 23 21 21 18 95 11 16 45 23 28 9 | 44 54 52 55 66 55 56 71 66 53 51 10 | 6 15 6 14 26 4 10 13 12 8 4 | 15 21 22 22 23 15 19 16 18 16 14 11 | 9 18 10 19 57 5 15 12 10 14 5 | 20 26 19 28 51 19 22 23 22 24 19 12 | 9 15 11 16 40 7 16 9 9 31 5 | 27 29 29 30 35 25 28 25 29 31 25 13 | 10 23 14 21 42 5 18 13 11 15 5 | 20 31 24 26 39 20 27 19 24 18 19 14 | 9 18 13 26 44 6 21 16 9 14 6 | 20 31 26 27 39 21 28 27 23 20 21 15 | 7 19 11 17 22 6 17 13 8 21 5 | 19 28 22 25 42 21 29 22 17 18 18 16 | 10 21 11 17 51 6 19 13 10 36 6 | 21 31 25 28 53 24 32 22 24 26 22 17 | 9 16 10 14 60 4 16 11 13 22 5 | 18 25 20 27 52 20 29 21 21 25 19 18 | 9 19 13 16 18 7 19 14 11 25 5 | 26 35 24 34 35 27 32 23 28 30 25 19 | 10 19 12 17 26 6 16 12 10 27 5 | 21 33 21 32 38 24 32 20 24 31 23 20 | 9 24 11 18 32 6 15 10 9 13 5 | 20 30 23 31 41 23 30 21 18 25 21 21E | 19 23 18 16 52 6 13 14 8 17 6 | 31 35 32 30 35 29 28 30 36 34 30 22 | 9 18 15 20 24 7 18 13 10 18 5 | 22 31 24 32 41 23 28 22 24 26 22 23 | 9 27 14 20 29 6 18 13 9 20 6 | 18 32 25 25 43 19 31 18 20 20 19 24E | 21 25 12 19 61 5 20 19 12 19 7 | 65 61 60 63 52 59 56 60 65 55 59 25E | 9 21 12 15 80 4 16 17 13 16 5 | 14 24 15 20 29 15 22 21 24 16 14 26 | 7 16 7 14 20 4 10 13 9 20 4 | 15 23 18 20 33 16 21 21 16 13 15 X27E | 12 22 11 12 48 6 19 14 10 --- 5 | 32 36 30 35 43 29 33 35 51 --- 32 28 | 9 18 12 18 42 8 20 8 12 38 6 | 26 29 28 29 36 26 33 27 23 33 24 29 | 10 16 8 16 41 5 16 13 11 28 5 | 19 22 18 23 39 17 25 21 22 20 17 30 | 7 10 6 16 39 5 10 8 10 23 4 | 31 31 33 29 24 30 32 35 34 31 30 31E | 8 21 11 15 41 5 20 11 10 29 5 | 20 29 22 26 53 22 32 19 24 25 21 32 | 7 26 12 18 44 6 14 20 11 34 6 | 20 26 27 26 28 23 28 19 22 48 21 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 20 12 17 47 6 16 15 11 24 |T 28 35 30 33 43 29 33 30 32 31 28 WRMS | 9 20 11 17 41 6 16 13 9 23 |NE 23 28 25 27 37 24 28 23 23 27 22 MEDI | 9 19 11 16 42 6 16 13 10 22 |MD 21 31 25 29 39 24 29 23 24 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 4.1505 GPS week: 1505 MJD: 54779.0-54785.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3059 |U 8 7 24 |U 9 15 34 |U 8 8 17 | emr | emr 2950 | 15 13 33 | 16 20 55 | 8 7 23 | esa | esa 2976 | 9 9 26 |U 9 14 35 | 10 9 21 | gfz | gfz 2933 |U 17 11 35 |U 14 17 68 | 11 10 27 | igr | igr 2963 | 16 18 67 | 11 16 43 | 9 8 21 | igs | igs 2956 | 18 15 42 | 14 18 51 | 9 8 20 | jpl | jpl 2925 |U 12 10 33 |U 14 17 52 |U 9 8 23 | mit | mit 2989 |U 18 13 34 |U 15 21 53 |U 9 8 23 | 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 5.1505.0 GPS week: 1505 Day: 0 MJD: 54779.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3062 | 8 6 27 | 8 13 27 | 8 6 14 | emr | emr 2956 | 12 11 28 | 13 14 52 | 10 10 23 | esa | esa 2976 | 8 9 28 | 8 10 28 | 8 7 14 | gfz | gfz 2937 | 27 7 40 | 14 12 51 | 14 13 24 | igr | igr 2976 | 13 41 186 | 12 11 38 | 9 8 20 | igs | igs 2975 | 31 29 80 | 11 11 50 | 10 8 20 | jpl | jpl 2954 | 9 9 32 | 13 14 47 | 10 9 19 | mit | mit 2976 | 11 11 29 | 15 27 39 | 9 8 20 | Table 5.1505.1 GPS week: 1505 Day: 1 MJD: 54780.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3072 | 9 6 22 | 14 31 48 | 9 9 18 | emr | emr 2954 | 14 11 24 | 24 44 96 | 10 9 25 | esa | esa 2976 | 10 11 29 | 15 27 49 | 9 9 16 | gfz | gfz 2937 | 14 10 24 | 19 26 70 | 13 12 27 | igr | igr 2975 | 8 8 39 | 19 32 67 | 11 10 24 | igs | igs 2975 | 14 10 24 | 19 34 70 | 10 10 22 | jpl | jpl 2954 | 9 8 27 | 28 48 100 | 10 10 25 | mit | mit 2976 | 16 12 19 | 21 34 73 | 10 9 22 | Table 5.1505.2 GPS week: 1505 Day: 2 MJD: 54781.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3068 | 10 11 30 | 7 12 30 | 6 7 13 | emr | emr 2952 | 16 17 53 | 12 18 50 | 7 7 20 | esa | esa 2976 | 10 12 36 | 6 10 30 | 6 6 15 | gfz | gfz 2934 | 15 14 59 | 11 13 56 | 8 9 24 | igr | igr 2961 | 12 13 33 | 11 14 47 | 7 7 19 | igs | igs 2955 | 14 14 39 | 11 15 46 | 6 6 18 | jpl | jpl 2949 | 16 14 54 | 11 12 43 | 6 6 19 | mit | mit 2976 | 20 14 55 | 14 16 62 | 7 6 17 | Table 5.1505.3 GPS week: 1505 Day: 3 MJD: 54782.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3072 | 9 7 27 | ---- ---- ---- | 8 6 17 | emr | emr 2952 | 20 12 40 | ---- ---- ---- | 8 5 24 | esa | esa 2976 | 8 8 29 | ---- ---- ---- | 7 8 20 | gfz | gfz 2939 | 19 15 46 | ---- ---- ---- | 12 8 29 | igr | igr 2976 | 11 15 32 | ---- ---- ---- | 11 7 23 | igs | igs 2972 | 13 19 49 | ---- ---- ---- | 11 8 24 | jpl | jpl 2950 | 12 9 37 | ---- ---- ---- | 9 8 26 | mit | mit 2976 | 19 18 37 | ---- ---- ---- | 9 8 16 | Table 5.1505.4 GPS week: 1505 Day: 4 MJD: 54783.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3048 | 6 7 20 | 8 12 42 | 8 6 24 | emr | emr 2952 | 15 13 28 | 14 18 63 | 8 9 27 | esa | esa 2976 | 7 6 20 | 8 13 44 | 7 5 23 | gfz | gfz 2936 | 14 9 23 | 12 20 64 | 11 9 31 | igr | igr 2972 | 12 14 89 | 10 15 53 | 8 6 22 | igs | igs 2974 | 13 10 31 | 11 16 59 | 9 7 22 | jpl | jpl 2860 | 13 12 32 | 12 12 56 | 9 7 26 | mit | mit 2976 | 14 14 28 | 17 19 71 | 7 7 26 | Table 5.1505.5 GPS week: 1505 Day: 5 MJD: 54784.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3038 | 10 9 20 | 7 9 26 | 9 11 14 | emr | emr 2933 | 18 15 29 | 16 12 39 | 8 8 21 | esa | esa 2976 | 12 10 21 | 8 10 28 | 23 23 41 | gfz | gfz 2913 | 14 12 29 | 13 12 50 | 10 10 28 | igr | igr 2931 | 35 23 65 | 10 11 27 | 10 11 20 | igs | igs 2887 | 22 12 33 | 14 11 39 | 7 8 17 | jpl | jpl 2859 | 13 9 26 | 11 8 31 | 8 9 20 | mit | mit 3072 | 21 14 39 | 14 12 38 | 9 9 35 | Table 5.1505.6 GPS week: 1505 Day: 6 MJD: 54785.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3055 | 7 6 20 | 8 11 33 | 9 9 15 | emr | emr 2955 | 12 9 30 | 14 13 31 | 8 5 24 | esa | esa 2976 | 8 10 17 | 7 12 31 | 8 7 19 | gfz | gfz 2941 | 15 7 29 | 13 19 117 | 11 8 24 | igr | igr 2952 | 21 10 29 | 8 11 28 | 9 6 19 | igs | igs 2958 | 20 8 35 | 15 20 42 | 9 9 18 | jpl | jpl 2954 | 13 10 24 | 11 12 33 | 11 9 29 | mit | mit 2976 | 24 10 32 | 11 16 35 | 10 8 22 | 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 6.1505 GPS week: 1505 MJD: 54779.500-54785.500 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 | -20 27 22 -91 -1 | 8 16 | 20 21 128 98 8 | 2 emr uuuuu | -67 -7 -112 -232 -7 | 56 57 | 28 13 143 176 15 | 4 esa uuuuu | 12 15 27 44 -1 | 17 21 | 20 17 96 46 5 | 3 gfz uuuuu | -29 26 34 -3 3 | 9 16 | 17 27 108 64 7 | 2 grg xxxxx | -36 3 46 -88 -8 | 2 33 | 61 51 100 146 16 | 3 igr xxxxx | -28 46 28 -43 0 | 2 13 | 10 21 63 64 9 | 3 irf xxxxx | -3 -1 -21 44 -1 | -1 13 | 14 12 22 26 2 | 2 jpl uuuuu | -29 22 39 4 -7 | 21 24 | 32 31 128 111 10 | 2 mit uuuuu | 24 -22 -187 244 4 | 15 21 | 35 18 72 80 8 | 2 ngs uuuuu | 38 -31 153 -121 -1 | 9 34 | 68 56 162 130 23 | 2 sio uuxxu | 38 10 22 -99 -4 | 32 35 | 31 20 163 142 7 | 2 Table 7.1505.0 GPS week: 1505 Day: 0 MJD: 54779.500 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 21 48 -224 -9 | 8 15 emr uuuuu | -59 -5 -86 -70 11 | 51 52 esa uuuuu | -5 8 183 34 6 | 13 17 gfz uuuuu | 6 3 40 -57 1 | 8 14 grg xxxxx | 48 2 22 36 -34 | 3 30 igr xxxxx | -21 38 -56 -114 14 | -2 10 irf xxxxx | -12 0 14 10 -1 | -2 11 jpl uuuuu | -80 4 -30 3 -12 | 24 27 mit uuuuu | -13 -23 -82 174 -4 | 14 18 ngs uuuuu | 87 2 -39 -86 7 | 7 34 sio uuxxu | 14 25 38 -294 -2 | 35 38 Table 7.1505.1 GPS week: 1505 Day: 1 MJD: 54780.500 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 | -41 46 65 13 -5 | 7 15 emr uuuuu | -53 -25 78 -127 4 | 53 54 esa uuuuu | 34 7 85 -33 2 | 13 18 gfz uuuuu | -28 17 72 5 3 | 7 13 grg xxxxx | -79 25 -146 -226 -15 | 0 33 igr xxxxx | -12 28 86 -121 0 | -1 9 irf xxxxx | -8 2 -15 80 1 | -3 12 jpl uuuuu | 2 32 6 -68 -9 | 21 25 mit uuuuu | 16 -22 -179 390 5 | 11 16 ngs uuuuu | 1 -12 -68 -116 -31 | 9 33 sio uuxxu | 4 2 64 -21 0 | 32 35 Table 7.1505.2 GPS week: 1505 Day: 2 MJD: 54781.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -5 5 -196 -146 2 | 7 16 emr uuuuu | -78 -16 -120 -105 5 | 55 57 esa uuuuu | 4 8 21 30 -2 | 16 21 gfz uuuuu | -29 43 -137 -20 3 | 8 16 grg xxxxx | -38 -40 132 -59 19 | -2 32 igr xxxxx | -21 56 -4 46 11 | 1 11 irf xxxxx | -22 3 -35 40 2 | -2 14 jpl uuuuu | -24 19 210 71 -15 | 21 25 mit uuuuu | -22 5 -157 234 10 | 13 19 ngs uuuuu | 117 -51 153 -225 -15 | 8 33 sio uuxxu | 9 -11 -229 -64 1 | 31 35 Table 7.1505.3 GPS week: 1505 Day: 3 MJD: 54782.500 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 62 188 -166 -10 | 10 19 emr uuuuu | -55 -16 -62 -165 -12 | 60 61 esa uuuuu | -19 11 -102 59 -7 | 19 24 gfz uuuuu | -48 39 147 -70 -7 | 11 19 grg xxxxx | 27 105 10 -107 -11 | 4 34 igr xxxxx | -43 34 67 -64 -6 | 5 15 irf xxxxx | -3 4 -7 67 -1 | 1 15 jpl uuuuu | -48 -37 -55 201 -5 | 22 26 mit uuuuu | 18 -37 -135 272 10 | 15 23 ngs uuuuu | 122 21 246 -352 29 | 10 33 sio uuxxu | 43 37 284 -224 -4 | 32 36 Table 7.1505.4 GPS week: 1505 Day: 4 MJD: 54783.500 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 | -50 2 120 -73 -1 | 11 18 emr uuuuu | -40 2 -330 -225 -11 | 61 62 esa uuuuu | 27 -1 63 93 -4 | 21 24 gfz uuuuu | -36 -19 162 -34 -5 | 12 19 grg xxxxx | -102 -18 79 -322 -10 | 6 33 igr xxxxx | -33 22 93 11 -7 | 6 15 irf xxxxx | -1 -28 -28 48 0 | 2 14 jpl uuuuu | -15 36 -134 -123 12 | 22 26 mit uuuuu | 40 -50 -293 286 14 | 18 24 ngs uuuuu | -32 32 392 -83 -25 | 13 35 sio uuxxu | 60 -16 99 -22 1 | 34 37 Table 7.1505.5 GPS week: 1505 Day: 5 MJD: 54784.500 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 | -20 30 16 -89 0 | 8 15 emr uuuuu | -56 13 -267 -371 -23 | 57 59 esa uuuuu | 13 20 10 22 -6 | 17 21 gfz uuuuu | -42 44 15 115 10 | 8 16 grg xxxxx | -101 -43 69 -38 -6 | 3 34 igr xxxxx | -30 63 61 -57 -7 | 3 14 irf xxxxx | 18 8 -20 54 -5 | -1 13 jpl uuuuu | -50 46 93 -85 -4 | 19 22 mit uuuuu | 63 -7 -205 160 -3 | 16 22 ngs uuuuu | -3 -97 220 38 12 | 7 35 sio uuxxu | 89 25 13 -184 -15 | 31 34 Table 7.1505.6 GPS week: 1505 Day: 6 MJD: 54785.500 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 | -16 24 -86 49 13 | 6 14 emr uuuuu | -125 1 1 -560 -27 | 54 57 esa uuuuu | 29 51 -72 104 5 | 17 21 gfz uuuuu | -24 59 -63 39 14 | 8 16 grg xxxxx | -8 -7 156 99 3 | 1 34 igr xxxxx | -35 81 -49 3 -7 | 1 15 irf xxxxx | 11 5 -56 12 -3 | -2 14 jpl uuuuu | 13 52 184 34 -19 | 17 20 mit uuuuu | 68 -18 -257 194 -5 | 16 22 ngs uuuuu | -28 -109 168 -21 17 | 7 35 sio uuxxu | 49 12 -117 119 -12 | 29 33