Date: Thu, 13 Aug 2009 12:06:33 +0000 From: Jim Ray Subject: [IGSREPORT-17683] Wk 1542 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4a8401c9./kQJ/a/F8jFDP9VR%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 13 Aug 05:06:56 PDT 2009 Message Number 17683 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1542 (Jul 26, 2009 - Aug 01, 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: igs1542[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1542[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1542[0-6].cls IGS GPS clock combination summary report. igs15427.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15427.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Duplicate entries can arise due to separate combination runs for the 30-s clocks ACs (listed first) and the 5-min clock ACs (listed second). Day | Centre | PRN/STA list ----+--------+--------------- 0 | ALL | 1 1 0 | COD | 30 30 DAV1 0 | EMR | WTZR 0 | ESA | 18 30 0 | GFZ | 12 23 ADE1 AUCK BRUS CEDU HOB2 NYA1 PERT 0 | GRG | DAV1 ONSA 0 | JPL | 32 0 | MIT | 18 18 HRAO 1 | ALL | 1 1 | COD | WTZR 1 | EMR | MIZU WTZR 1 | ESA | BHR1 1 | GFZ | 23 ONSA 1 | GRG | ONSA 1 | JPL | 32 1 | MIT | 4 18 4 18 BOR1 IRKJ STJO 2 | ALL | 1 1 2 | COD | WTZR 2 | EMR | KERG WTZR 2 | ESA | WHIT 2 | GFZ | KIRU SCH2 VESL VILL 2 | GRG | USNO 2 | JPL | 32 2 | MIT | 10 15 16 18 10 15 16 18 ALGO TWTF 3 | ALL | 1 3 | COD | WTZR 3 | EMR | MIZU WTZR 3 | GFZ | 12 14 16 23 28 ANKR BRFT FAA1 KIRU WHIT YELL 3 | GRG | USNO 3 | JPL | 32 UNSA 3 | MIT | 18 18 BOR1 IRKJ SYDN 3 | NGS | 1 4 | ALL | 1 1 4 | COD | 26 26 WTZR 4 | EMR | MIZU 4 | ESA | 26 4 | GFZ | 18 23 CAS1 FLIN NICO NYA1 UNSA WTZR 4 | GRG | AMC2 4 | JPL | 32 4 | MIT | 18 19 18 19 NICO WTZR 5 | ALL | 1 1 5 | COD | 26 26 ALBH MATE 5 | EMR | ALBH YELL CHUR MIZU WTZR YELL 5 | GFZ | 8 13 14 15 23 26 CAS1 CHUR DAV1 MAW1 NTUS RCMN SUTH 5 | GFZ | SUTM VESL 5 | GRG | DAV1 USNO 5 | JPL | 32 DAV1 5 | MIT | 18 18 SYDN 6 | COD | 26 26 WTZR 6 | EMR | MIZU WTZR 6 | ESA | 26 UNSA 6 | GFZ | 15 18 23 CAS1 HARB 6 | GRG | 1 DAV1 IRKJ TWTF USNO 6 | JPL | 32 DAV1 6 | MIT | 18 18 IRKJ SYDN TWTF 6 | NGS | 1 5. New clock offsets and drifts were estimated for centres showing reference clock resets. Note that only the largest clock offset and drift are output to the summary file. However, the clock combination and the listed RMS include all the clock segments. In summary, the following clock shifts/resets were noticed and accounted for: Day | Centre | Time | Jump ----+--------+--------+------------- 2 | GFZ | ~16:55 | ~ -0.31 ns 3 | GFZ | ~11:55 | ~ -0.35 ns 6. The following table lists all maneuvered satellites for this week. The solutions from COD and ESA, which modeled the maneuver, are used that day for combination. An associated accuracy code of 0 (unknown) is given if only one AC is left (no redundancy). For the long arc evaluation the arc is split into two parts at the given maneuver epoch. PRN | Date | Ref. NANU ----+------------+---------- G20 | 2009_07_30 | 2009042 G20 | 2009_07_30 | 2009043 G20 | 2009_07_30 | 2009050 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 | .6 .3 1.3 -15 -13 -20 -.49 EMR | 9.7 -6.0 -13.4 103 -6 34 -.11 ESA | -1.9 1.9 -3.4 6 -27 2 -.06 GFZ | .1 .8 1.2 19 -30 4 -.22 GRG | 3.0 -.5 7.5 10 19 122 -.03 JPL | -4.5 -1.9 2.8 3 23 -7 .02 MIT | 3.6 -5.2 2.7 5 8 0 -.30 NGS | 6.2 -3.8 5.1 -21 -44 -8 -.40 SIO | -.7 -3.8 -21.0 -75 -59 5 .07 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 1.1542.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1542.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 2.1542.[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 3.1542.[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 5.1542.0-6). 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 1542 summary. (Jul 26, 2009 - Aug 01, 2009) Table 1.1542.a GPS week: 1542 MJD: 55038.000-55044.000 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 236| 0 0 0 49 -1 -10 -.12 8 7 | -285 -350 15 68 | 0 0 1 11 9 13 .03 | 317 368 emr 75| 3 0 -3 -247 -30 -17 .43 18 18 | 2069 -231 17 96 | 1 2 1 27 25 17 .02 | 595 1599 esa 127| 0 1 5 -36 -13 14 .39 10 10 | -1172 984 18 112 | 0 1 2 23 18 17 .03 | 1103 1478 gfz 189| 1 0 0 -53 4 -14 -.11 11 11 | 45 274 24 113 | 0 0 0 43 56 13 .03 | 387 627 grg 110| 3 0 0 -25 -26 13 1.07 34 32 | -7108 1060 78 229 | 1 1 1 19 25 75 .08 | 6875 1530 igr n/a| 0 0 0 10 -13 -47 .08 5 5 | 27342 -880 19 70 | 0 0 0 11 16 22 .03 | 1922 1807 jpl 127| 0 1 -3 -1 -68 31 .58 16 15 | 1124 -307 17 100 | 1 1 1 19 14 33 .04 | 883 1849 mit 286| 0 0 0 0 -43 10 -.25 10 9 | -15002 -781 20 151 | 0 0 0 17 14 15 .02 | 746 928 ngs 226| -1 0 0 87 81 2 -.29 11 9 | -8225 31494 2135 3770 | 1 1 1 43 38 20 .03 | 63346 88958 sio 254| -4 2 1 164 83 -19 -.06 20 20 | --- --- --- --- | 1 1 2 27 14 6 .04 | --- --- Table 1.1542.b GPS week : 1542 MJD: 55038.000-55044.000 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 | 18 11 11 10 9 7 14 | 2 | 5 5 5 4 4 4 4 | 3 | 4 4 4 4 4 4 4 | 4 | 5 5 5 5 5 4 4 | 6 | 4 4 4 4 4 4 4 | 7 | 5 5 5 5 5 4 4 | 8 | 5 4 4 4 4 4 4 | 9 | 4 4 4 4 4 4 3 | 10 | 4 4 4 4 3 3 3 | 11 | 6 5 4 4 4 4 5 | 12 | 7 5 5 6 4 4 4 | 13 | 5 5 5 4 5 4 4 | 14 | 6 6 4 4 5 4 4 | 15 | 5 5 5 5 4 5 5 | 16 | 6 6 6 6 6 5 5 | 17 | 5 5 5 5 5 4 4 | 18 | 16 6 6 6 5 5 5 | 19 | 6 5 5 4 4 4 4 | 20 | 6 6 5 5 0 5 5 | 21 | 5 5 5 5 5 5 5 | 22 | 4 4 4 4 4 4 4 | 23 | 6 6 5 5 5 5 5 | 24 | 4 4 4 4 4 4 4 | 25 | 4 4 4 3 3 4 3 | 26 | 5 5 5 6 6 5 5 | 27 | 4 4 4 4 3 4 4 | 28 | 5 5 6 5 5 5 4 | 29 | 6 6 5 5 5 5 5 | 30 | 6 8 5 5 4 5 5 | 31 | 5 6 5 5 5 5 5 | 32 | 5 5 5 5 5 4 4 | 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 2.1542.0 GPS week: 1542 Day: 0 MJD: 55038.000 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 236| 0 0 -1 38 -18 2 -.17 9 8 | 19 -789 14 64 | 29 17 | emr 75| 1 3 -2 -216 -66 -18 .39 16 16 | 1785 277 16 89 | 35 19 | esa 127| -1 0 9 3 16 19 .33 12 12 | 532 1182 15 100 | 19 32 | gfz 189| 2 0 1 -26 73 -31 -.11 11 11 | -293 38 22 103 | -11 -32 | grg 110| 4 0 2 -59 -30 14 1.05 35 35 | 129 -110 72 216 | 56 28 | igr n/a| -1 0 1 9 -19 -45 .03 6 6 | 29219 -561 19 73 | 11 -3 | jpl 127| 0 0 -3 -14 -81 25 .55 16 14 | 1450 -109 15 88 | 5 37 | mit 286| -1 0 -1 -10 -53 27 -.28 12 11 | -15744 295 20 162 | 16 0 | ngs 226| -2 0 1 142 63 37 -.29 16 13 | -151803 233089 2076 3862 | -133 4 | sio 254| -3 1 -2 128 75 -20 -.11 20 19 | --- --- --- --- | -79 -52 | Table 2.1542.1 GPS week: 1542 Day: 1 MJD: 55039.000 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 236| 0 0 -1 45 -4 -15 -.16 9 8 | -726 245 21 80 | 31 6 | emr 75| 3 2 0 -223 -4 -29 .42 18 18 | 2316 -1809 15 102 | 68 0 | esa 127| 0 2 7 -58 -6 36 .40 11 11 | -2278 3055 21 119 | 60 52 | gfz 189| 1 -1 0 -96 -44 0 -.16 10 10 | 283 -684 28 137 | 19 -23 | grg 110| 3 0 -1 -21 4 -14 1.02 35 33 | 774 -1680 77 223 | -15 -47 | igr n/a| 0 0 0 24 14 -41 .04 5 5 | 29111 -2653 20 65 | -17 -43 | jpl 127| 0 1 -3 25 -60 81 .54 19 17 | 1755 -2175 18 90 | 34 -15 | mit 286| 0 0 0 21 -49 -15 -.23 12 10 | -14091 -2204 17 142 | 4 -6 | ngs 226| -2 -2 -1 138 141 -11 -.25 14 13 | 14298 1280 2505 3824 | -110 -64 | sio 254| -5 0 0 185 79 -24 -.05 20 20 | --- --- --- --- | -113 -51 | Table 2.1542.2 GPS week: 1542 Day: 2 MJD: 55040.000 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 236| 1 0 0 73 0 -36 -.11 8 8 | -559 -344 15 68 | -17 23 | emr 75| 5 1 -2 -248 -29 13 .42 19 19 | 3081 -1449 19 102 | 61 -11 | esa 127| -1 1 5 -59 -13 9 .39 10 10 | -2057 707 16 103 | 28 48 | gfz 189| 0 0 -1 -101 -54 4 -.16 11 11 | -385 1235 23 108 | 3 -40 | grg 110| 4 1 0 0 -56 -14 1.13 33 30 | -221 717 86 237 | -17 -34 | igr n/a| 0 1 1 7 -13 -63 .11 6 6 | 29200 -2011 19 77 | 31 -33 | jpl 127| 2 2 0 11 -78 -4 .60 17 15 | 2347 -1429 16 94 | -1 -26 | mit 286| 0 -1 -1 -20 -51 21 -.22 10 9 | -14255 -367 20 150 | 8 2 | ngs 226| -2 -1 0 102 115 9 -.26 10 8 | 11693 1899 2266 3749 | -69 -135 | sio 254| -3 1 0 143 100 -23 -.00 19 18 | --- --- --- --- | -105 -45 | Table 2.1542.3 GPS week: 1542 Day: 3 MJD: 55041.000 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 236| 0 0 -1 43 3 -2 -.13 8 7 | -405 -121 18 75 | 42 -30 | emr 75| 3 -2 -4 -300 -2 -43 .44 19 19 | 2483 -1506 17 82 | 76 -39 | esa 127| -1 2 4 -48 0 39 .41 9 9 | -2372 2758 17 100 | 15 6 | gfz 189| 2 -1 0 20 -33 -23 -.09 11 11 | 74 238 23 91 | -7 -45 | grg 110| 0 -2 1 -34 -23 65 .96 31 28 | -12059 1940 78 249 | 89 -48 | igr n/a| 0 0 0 -10 3 -44 .09 6 5 | 27780 -2581 17 64 | 32 -68 | jpl 127| 2 0 -3 -30 -59 36 .56 16 14 | 1564 -2012 16 111 | 65 9 | mit 286| 0 -1 0 16 -60 9 -.26 10 9 | -15594 -108 22 129 | 4 -9 | ngs 226| -1 0 1 18 98 -20 -.30 9 7 | 17534 -7234 2048 3267 | 19 -12 | sio 254| -4 3 3 207 68 -26 -.08 20 19 | --- --- --- --- | -123 -44 | Table 2.1542.4 GPS week: 1542 Day: 4 MJD: 55042.000 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 236| 0 0 1 57 2 2 -.11 7 6 | -385 -242 13 70 | -14 11 | emr 75| 6 2 -2 -243 -56 -9 .45 18 18 | 1454 73 16 90 | 46 25 | esa 127| -1 0 1 -43 -24 0 .39 9 9 | -978 -501 19 113 | 26 37 | gfz 189| 1 -1 -1 -76 46 -16 -.10 13 13 | -49 -50 26 124 | -18 -23 | grg 110| 3 -3 0 -15 -22 139 1.05 32 35 | -12880 2701 81 236 | -61 26 | igr n/a| 0 0 0 20 -31 -43 .10 5 5 | 25629 -454 20 74 | -50 -4 | jpl 127| 0 3 -2 15 -77 1 .61 18 16 | -80 208 19 108 | -51 -19 | mit 286| 0 -1 0 -17 -19 24 -.25 8 7 | -15742 -1105 23 153 | 6 -21 | ngs 226| -1 -1 0 70 32 -13 -.33 10 8 | 16025 8 1707 3560 | -44 17 | sio 254| -3 4 2 178 98 -7 -.04 20 19 | --- --- --- --- | -110 -47 | Table 2.1542.5 GPS week: 1542 Day: 5 MJD: 55043.000 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 236| 0 0 0 44 -8 -4 -.09 7 7 | 139 -798 13 68 | 5 -1 | emr 75| 3 -2 -4 -251 -41 -21 .45 17 17 | 1445 -38 18 107 | 30 5 | esa 127| 0 0 2 -16 -29 4 .41 10 10 | -732 -772 19 124 | 29 21 | gfz 189| 1 0 0 -57 69 -7 -.08 9 9 | -79 265 24 112 | -34 -20 | grg 110| 5 0 -3 -13 -60 7 1.07 35 35 | -12499 2136 82 225 | -31 54 | igr n/a| 0 0 0 15 -26 -83 .08 5 5 | 25345 -463 20 67 | -41 -24 | jpl 127| 0 1 -4 -15 -79 8 .59 16 14 | 285 158 20 115 | 13 66 | mit 286| 0 -1 0 17 -29 -2 -.26 8 7 | -14334 -1756 18 154 | 5 -15 | ngs 226| 0 0 1 64 45 13 -.33 10 9 | 17340 -4460 2204 3872 | -69 36 | sio 254| -5 2 2 163 97 -19 -.09 21 22 | --- --- --- --- | -90 -52 | Table 2.1542.6 GPS week: 1542 Day: 6 MJD: 55044.000 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 236| 0 0 0 43 12 -17 -.09 6 6 | -84 -403 13 57 | -5 -20 | emr 75| 2 -2 -6 -246 -14 -12 .46 17 17 | 1925 2829 18 102 | 8 -7 | esa 127| 0 -1 5 -30 -38 -6 .42 11 11 | -320 459 19 130 | 8 59 | gfz 189| 1 0 0 -39 -26 -22 -.08 10 10 | 767 876 26 118 | -29 -28 | grg 110| 3 -1 0 -36 4 -103 1.20 34 31 | -13005 1717 75 223 | -10 7 | igr n/a| -1 0 0 8 -23 -9 .11 4 4 | 25113 2560 19 74 | -52 3 | jpl 127| 0 0 -4 -3 -42 70 .64 15 13 | 547 3206 19 94 | -19 -42 | mit 286| 0 0 0 -4 -36 7 -.25 9 8 | -15257 -224 23 169 | 15 -15 | ngs 226| 0 0 0 77 70 0 -.29 8 7 | 17333 -4124 2143 4256 | -45 -14 | sio 254| -6 3 3 145 67 -15 -.09 23 21 | --- --- --- --- | -85 -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 3.1542.0 GPS week: 1542 Day: 0 MJD: 55038.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 23 --- --- --- 2923 31 --- 16 36 --- 17 | 30 --- --- --- 9999 39 --- 35 40 --- 32 2 | 7 13 10 8 56 7 11 11 19 25 4 | 22 29 32 27 32 27 26 32 32 29 26 3 | 4 10 10 8 32 6 9 12 12 23 4 | 12 23 18 17 26 13 22 12 14 27 14 4 | 8 11 8 6 39 8 9 11 18 31 4 | 32 42 40 37 28 38 39 42 40 37 36 6 | 5 9 8 9 27 7 9 10 12 20 3 | 12 25 21 18 26 15 24 12 16 22 15 7 | 7 15 15 9 31 5 18 10 12 21 5 | 15 27 20 20 35 16 27 17 15 15 15 8 | 9 11 12 7 23 4 9 15 14 22 4 | 14 22 21 18 33 18 22 24 22 23 18 9 | 8 9 10 6 31 5 10 9 20 16 4 | 21 27 28 25 24 23 25 28 33 18 24 10 | 8 11 11 13 25 5 9 11 17 13 4 | 19 26 28 27 22 23 24 27 31 28 24 11 | 10 11 14 10 37 7 16 21 15 19 5 | 40 46 51 44 39 42 41 46 41 36 42 12E | 11 18 15 25 30 5 19 11 20 20 6 | 18 27 18 36 34 19 25 20 27 30 19 13 | 6 17 14 7 25 6 17 15 16 13 4 | 23 33 27 30 36 26 29 28 27 23 25 14 | 19 16 11 10 39 8 17 16 17 14 6 | 44 56 49 46 48 46 53 46 41 50 46 15E | 7 15 13 13 51 7 16 11 15 18 5 | 13 25 20 23 41 19 21 21 25 21 17 16E | 9 25 14 15 20 5 20 14 15 18 6 | 21 36 22 25 30 20 31 19 21 22 20 17 | 9 16 12 9 33 6 19 10 13 17 4 | 17 33 23 21 49 20 35 17 16 21 19 X18 | 32 36 44 --- 49 20 --- 20 18 --- 16 | 27 39 40 --- 46 20 --- 17 20 --- 15 19 | 9 19 10 8 39 6 20 20 15 20 5 | 16 30 19 18 36 17 30 21 21 22 17 X20 | 8 19 15 --- 33 9 20 13 13 13 5 | 11 24 15 --- 30 11 19 10 12 11 10 X21 | 6 10 12 --- 27 6 11 9 13 30 5 | 23 31 31 --- 26 27 26 30 32 31 27 22 | 7 15 9 8 28 4 15 9 12 13 4 | 12 27 18 18 38 14 25 14 13 12 15 23E | 8 24 16 8 28 6 26 10 12 12 5 | 17 35 21 22 27 20 34 20 18 23 20 24 | 7 10 7 8 53 5 8 11 17 21 4 | 26 35 32 32 31 32 28 35 38 23 30 25 | 6 11 13 8 --- 3 10 7 11 22 4 | 14 20 17 20 --- 16 17 18 15 20 14 26 | 8 18 12 10 33 6 13 9 11 16 4 | 90 94 92 91 94 91 87 94 94 91 91 27 | 7 10 12 7 33 4 9 10 20 15 4 | 19 26 24 21 25 22 24 26 28 18 21 28E | 9 14 13 12 25 6 15 8 16 14 4 | 23 29 22 26 31 24 30 25 28 30 23 29 | 8 19 11 11 36 6 23 13 17 22 5 | 18 32 22 20 31 19 33 20 21 25 20 30E | 11 26 13 13 49 8 21 15 20 21 6 | 69 70 66 66 71 64 70 68 65 72 67 31 | 6 20 13 9 28 6 21 11 16 22 5 | 14 29 20 22 37 14 28 15 14 18 15 32 | 9 14 9 11 26 8 15 15 16 28 5 | 12 21 18 20 23 15 21 17 16 30 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 16 12 11 35 6 16 12 16 20 |T 24 33 29 29 36 26 31 27 28 28 25 WRMS | 8 16 12 11 35 6 14 11 13 19 |NE 18 29 25 23 31 21 26 22 23 23 20 MEDI | 8 15 12 9 32 6 15 11 16 20 |MD 19 29 22 23 32 20 27 21 25 23 20 Table 3.1542.1 GPS week: 1542 Day: 1 MJD: 55039.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 21 --- --- 21 --- 17 --- 14 17 --- 11 | 29 --- --- 44 --- 38 --- 31 28 --- 27 2 | 10 13 15 9 44 6 13 10 17 27 5 | 12 25 28 19 21 15 17 15 20 20 15 3 | 8 11 11 8 31 5 12 10 13 21 4 | 13 22 19 19 23 14 21 15 20 27 16 4 | 9 14 10 9 38 4 12 11 16 31 5 | 18 30 27 22 23 20 24 24 23 27 20 6 | 8 9 7 7 23 5 11 10 12 18 3 | 14 21 21 15 26 15 22 13 19 21 15 7 | 5 18 13 9 39 3 19 10 14 22 5 | 11 25 20 15 34 13 23 14 19 15 13 8 | 6 11 15 5 25 3 11 10 13 22 4 | 9 15 21 11 28 11 18 14 13 19 11 9 | 6 13 9 8 30 5 13 7 14 17 4 | 13 18 19 11 27 12 17 14 16 8 12 10 | 7 14 8 7 28 6 11 10 16 11 4 | 14 21 16 14 24 10 17 17 13 19 13 11 | 10 14 7 6 65 6 17 15 11 18 4 | 27 30 27 23 30 23 30 29 21 22 24 12E | 9 17 10 12 29 4 22 11 11 22 5 | 18 27 20 19 32 16 24 18 18 26 17 13 | 8 20 12 7 26 5 20 18 15 13 5 | 20 28 22 24 33 20 23 26 23 21 21 14E | 14 20 11 14 41 6 20 12 13 15 5 | 23 33 33 28 39 27 33 31 28 30 26 15E | 6 17 12 14 39 5 19 12 14 15 5 | 13 23 18 19 37 9 21 11 13 16 11 16E | 7 30 10 17 25 6 26 13 14 16 6 | 23 36 24 24 24 20 32 22 29 23 22 17 | 9 17 11 10 45 6 22 7 13 20 5 | 17 34 24 20 41 16 32 16 17 19 18 X18 | 10 24 9 --- 56 8 --- 10 13 18 6 | 14 29 19 --- 48 17 --- 15 14 16 13 19 | 8 17 12 7 45 5 23 18 13 20 5 | 15 28 21 16 36 16 30 20 21 19 16 X20 | 9 21 10 --- 26 5 22 12 15 14 5 | 16 22 14 --- 22 11 21 14 14 11 11 X21 | 9 9 9 --- 24 6 14 10 14 30 5 | 15 23 20 --- 22 19 21 21 24 18 18 22 | 8 17 9 7 29 4 20 8 10 13 4 | 12 24 14 12 35 12 26 10 11 10 11 23E | 9 27 12 15 30 6 29 12 14 14 6 | 16 31 19 20 33 14 28 17 21 16 15 24 | 8 9 7 8 32 6 14 11 14 21 4 | 17 23 18 23 14 21 18 24 25 16 19 25 | 5 11 11 7 --- 5 12 7 14 21 4 | 11 17 17 11 --- 9 14 13 16 18 11 26 | 13 22 11 7 32 4 16 10 10 17 5 | 95 95 95 96 109 94 94 95 95 98 95 27 | 7 13 9 9 34 5 14 9 15 15 4 | 14 17 17 11 30 10 17 14 14 10 11 28E | 7 11 14 11 25 6 17 8 13 17 4 | 20 27 27 22 43 23 23 23 24 21 22 29 | 11 22 13 11 32 6 26 8 14 20 5 | 16 29 18 12 26 14 30 16 17 20 14 30E | 17 32 11 12 40 6 23 21 15 38 7 | 39 51 37 43 47 36 49 37 35 48 37 31 | 7 20 11 13 27 6 26 11 20 20 5 | 14 27 14 14 36 14 30 16 25 19 14 32 | 11 15 9 10 25 7 21 12 13 27 5 | 18 20 17 17 22 14 21 16 18 29 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 11 10 35 5 19 12 14 20 |T 19 28 23 22 33 19 26 21 22 22 19 WRMS | 8 18 11 10 33 5 17 10 13 20 |NE 14 23 19 15 28 14 22 16 18 18 14 MEDI | 8 17 11 9 31 6 19 10 14 18 |MD 16 25 20 19 30 15 23 16 20 19 15 Table 3.1542.2 GPS week: 1542 Day: 2 MJD: 55040.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 21 --- --- 21 --- 21 --- 12 18 --- 10 | 27 --- --- 30 --- 28 --- 27 24 --- 26 2 | 7 17 8 10 36 6 11 9 12 27 4 | 25 37 31 26 24 25 28 29 29 29 27 3 | 8 14 8 10 30 7 12 8 10 21 4 | 16 22 19 19 31 14 20 16 17 30 16 4 | 9 19 11 7 27 7 10 8 15 33 5 | 30 43 34 33 34 34 34 33 39 33 32 6 | 7 14 6 7 22 10 12 7 9 16 3 | 17 26 20 18 30 19 25 16 19 27 18 7 | 6 18 14 10 30 5 21 11 10 18 4 | 17 30 21 22 35 18 27 20 19 20 17 8 | 6 14 14 6 22 3 10 9 7 19 4 | 15 23 21 21 29 15 17 22 15 22 16 9 | 7 15 11 9 32 4 9 6 10 19 4 | 18 25 22 19 31 16 20 20 22 14 19 10 | 6 18 12 10 14 5 10 8 11 11 4 | 19 29 23 20 23 18 22 21 20 19 18 11 | 9 15 8 6 73 6 15 9 7 16 3 | 32 38 34 34 36 33 34 34 34 28 32 12E | 10 21 8 13 25 5 16 7 9 19 4 | 18 31 18 24 34 17 23 19 19 23 19 13 | 12 20 9 9 30 7 19 18 10 13 5 | 28 35 34 32 45 32 36 35 33 30 31 14E | 8 17 10 9 36 7 17 10 9 14 4 | 24 29 26 26 29 26 30 23 24 25 23 15E | 8 21 13 22 31 4 19 7 9 15 5 | 13 27 22 33 30 19 22 20 20 20 17 16E | 8 32 13 13 41 6 25 10 10 15 5 | 20 37 23 23 42 20 30 23 21 26 22 17 | 10 22 8 9 38 4 18 7 13 19 4 | 19 36 24 21 52 20 30 19 24 24 20 X18 | 9 20 12 --- 37 5 21 12 9 18 5 | 19 29 19 --- 37 16 24 17 17 18 17 19 | 7 18 8 7 31 7 21 12 9 20 4 | 19 32 26 18 41 19 28 21 23 21 20 X20 | 8 24 13 --- 24 6 17 10 9 13 5 | 13 27 14 --- 23 14 19 14 13 15 12 X21 | 7 14 10 --- 31 4 14 7 12 30 5 | 23 30 32 --- 25 24 25 27 22 28 25 22 | 6 17 9 8 26 3 19 7 6 13 3 | 14 28 18 19 36 14 26 15 15 17 16 23E | 8 23 9 15 23 5 26 11 10 13 5 | 19 31 21 19 32 19 31 22 23 24 21 24 | 7 14 9 13 31 5 11 9 10 19 4 | 25 32 33 30 19 26 24 30 30 25 28 25 | 6 12 8 7 --- 4 8 8 8 19 3 | 16 23 17 20 --- 15 18 20 18 21 16 26E | 13 23 10 9 38 3 17 10 7 16 4 | 75 83 77 76 97 78 84 78 77 88 78 27 | 8 18 11 9 33 3 10 9 11 17 4 | 15 24 23 19 29 15 20 20 19 13 17 28E | 11 14 11 26 29 4 15 10 11 15 5 | 22 31 27 39 34 23 26 25 29 28 24 29 | 9 23 13 11 31 5 24 8 8 20 5 | 18 32 21 18 33 18 29 20 21 20 19 30 | 10 23 11 10 33 7 15 14 9 18 5 | 60 73 61 62 67 60 68 63 62 61 61 31 | 8 21 9 10 33 6 20 9 10 21 4 | 17 31 22 24 43 19 29 20 18 20 18 32 | 8 17 8 12 26 6 18 8 7 27 4 | 15 22 17 18 22 16 23 17 18 32 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 11 33 6 17 10 10 19 |T 22 33 26 27 35 23 29 25 25 26 23 WRMS | 8 19 10 11 30 6 15 9 8 18 |NE 19 29 23 22 31 19 24 21 21 22 19 MEDI | 8 18 10 10 31 5 16 9 10 18 |MD 19 30 22 22 33 19 26 21 21 24 19 Table 3.1542.3 GPS week: 1542 Day: 3 MJD: 55041.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1E | 21 --- --- 18 81 19 --- 15 13 --- 10 | 57 --- --- 52 792 52 --- 56 47 --- 55 2 | 6 16 10 9 24 4 11 9 8 29 4 | 20 34 32 28 31 25 24 28 29 28 27 3 | 7 14 13 10 30 6 10 11 7 22 4 | 10 24 21 14 26 14 20 14 14 26 14 4 | 7 18 9 10 16 6 9 9 6 36 4 | 27 41 34 35 45 31 32 31 33 35 31 6 | 6 12 10 10 22 5 9 8 9 17 3 | 12 25 21 15 26 15 21 12 17 21 15 7 | 7 19 10 11 29 5 18 11 8 18 4 | 15 30 18 17 36 14 25 16 16 17 15 8 | 6 16 7 10 27 3 8 11 8 19 3 | 14 27 17 18 35 14 18 18 17 18 15 9 | 7 19 10 7 27 4 9 7 9 19 3 | 20 26 23 16 23 18 22 18 24 11 20 10 | 7 15 10 7 17 4 9 7 8 15 3 | 15 29 23 18 24 19 21 21 22 25 19 11 | 8 17 10 6 48 8 15 9 7 15 3 | 37 42 39 36 28 37 39 39 39 33 37 12E | 11 18 9 22 29 5 18 12 10 23 5 | 23 32 24 35 32 19 23 22 21 23 22 13E | 6 17 8 11 30 5 17 12 12 11 4 | 35 44 37 41 39 36 41 39 42 40 38 14E | 5 20 6 15 35 6 15 10 10 13 4 | 16 25 22 22 34 15 23 17 19 20 17 15E | 6 21 10 12 35 5 18 9 11 19 4 | 11 25 16 18 33 12 19 14 15 21 12 16E | 10 27 12 18 31 6 24 13 10 16 5 | 14 33 17 20 28 15 27 15 17 19 15 17 | 9 24 9 8 39 6 20 11 11 17 4 | 17 37 25 18 48 18 30 18 20 19 19 X18 | 6 22 13 --- 32 6 23 11 10 17 5 | 19 32 20 --- 36 18 28 16 24 17 19 19 | 7 18 7 9 33 5 17 11 7 18 4 | 14 31 23 18 36 18 27 16 17 18 17 X20 | 7 25 11 --- 30 7 --- 10 9 14 5 | 11 28 15 --- 25 11 --- 9 11 11 9 X21 | 7 15 11 --- 23 5 14 8 8 30 5 | 21 29 28 --- 32 21 22 25 24 24 23 22 | 6 16 10 7 29 6 18 9 11 14 4 | 15 29 20 19 38 18 28 15 21 17 18 23E | 7 21 9 10 33 5 25 13 8 12 4 | 18 33 21 23 44 19 31 18 21 21 19 24 | 7 17 7 11 22 5 9 10 8 19 3 | 21 33 28 28 31 24 20 27 31 20 25 25 | 6 11 6 7 --- 5 8 7 7 21 3 | 12 20 16 18 --- 11 16 15 14 17 13 26E | 13 25 11 11 32 7 18 7 12 35 5 | 144 151 148 144 167 147 152 145 149 148 146 27 | 7 17 8 10 39 6 10 8 11 15 3 | 17 24 20 15 30 17 20 16 22 10 17 28E | 10 15 10 14 29 7 16 9 8 16 4 | 19 28 23 20 29 21 26 21 28 24 21 29 | 8 25 12 12 27 7 27 7 8 21 5 | 18 39 24 16 28 19 34 20 21 20 20 30 | 8 24 9 7 31 5 15 13 6 22 4 | 59 69 66 61 62 60 65 61 60 60 62 31 | 8 27 8 9 33 10 19 11 9 22 5 | 17 36 22 19 38 17 28 17 18 17 17 32 | 7 16 10 8 31 4 17 11 7 27 4 | 10 24 18 17 23 13 20 13 15 29 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 9 11 31 6 16 10 9 20 |T 24 36 28 28 63 25 31 26 28 26 26 WRMS | 7 19 9 11 28 5 14 9 7 19 |NE 17 30 23 20 31 18 24 19 21 20 19 MEDI | 7 18 10 10 30 5 16 10 8 18 |MD 17 30 22 19 32 18 25 18 21 20 19 Table 3.1542.4 GPS week: 1542 Day: 4 MJD: 55042.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 16 --- --- 14 66 21 --- 13 14 --- 8 | 50 --- --- 41 324 47 --- 34 37 --- 40 2 | 5 14 9 9 33 4 14 7 9 28 4 | 19 26 25 20 21 18 23 19 17 19 18 3 | 7 17 8 9 26 6 15 7 9 21 4 | 13 24 18 15 22 15 24 14 19 26 15 4 | 8 15 6 9 20 5 9 7 13 36 4 | 26 33 26 25 28 24 29 23 29 27 24 6 | 6 14 7 10 28 5 14 5 9 15 3 | 15 27 24 14 27 19 27 14 21 24 18 7 | 5 19 10 13 31 4 21 9 8 18 4 | 14 31 20 21 39 15 27 19 13 18 16 8 | 5 13 11 10 18 5 11 11 8 18 3 | 16 22 20 21 29 16 22 24 19 20 18 9 | 5 15 7 10 22 3 9 5 11 18 3 | 14 20 19 18 23 16 19 16 20 7 15 10 | 5 15 4 10 23 3 10 6 5 12 3 | 14 22 14 14 22 13 21 15 13 17 13 11 | 8 18 9 6 59 7 18 6 10 16 4 | 33 36 34 27 30 28 32 33 32 29 30 12 | 5 19 9 12 27 4 17 5 9 18 4 | 28 29 33 29 37 28 29 29 28 26 28 13E | 7 20 8 11 28 6 19 13 9 13 4 | 22 36 24 29 31 26 33 26 26 27 24 14E | 6 17 8 25 30 4 15 8 8 13 4 | 12 21 17 30 29 13 24 13 12 14 12 15E | 5 19 9 14 35 4 21 8 7 16 4 | 12 22 17 19 31 13 22 14 15 23 12 16E | 10 27 9 17 33 4 26 9 12 23 5 | 27 38 33 34 38 31 33 30 30 33 28 17 | 8 24 9 6 35 7 21 8 11 17 4 | 16 35 23 21 44 20 34 18 19 16 18 X18 | 6 22 10 --- 38 5 21 6 10 16 4 | 14 29 16 --- 38 15 26 14 17 14 15 19 | 7 18 9 10 32 5 22 6 8 18 4 | 14 29 25 18 37 17 27 14 16 19 16 X20 | 4 --- --- --- --- 25 --- --- --- --- 0 | 7 --- --- --- --- 25 --- --- --- --- 8 X21 | 7 12 6 --- 37 4 13 6 11 30 4 | 18 22 21 --- 45 15 21 21 20 18 18 22 | 6 19 9 11 34 4 20 5 8 13 4 | 14 27 19 13 36 16 30 15 18 15 15 23E | 7 19 15 13 40 6 24 10 9 14 5 | 17 31 26 23 35 19 33 21 19 24 20 24 | 6 14 6 12 32 2 10 5 9 21 3 | 19 22 19 25 29 17 17 22 22 16 19 25 | 4 12 9 10 --- 6 9 4 6 22 3 | 13 20 18 19 --- 14 19 17 15 21 14 26E | 12 23 10 31 50 5 19 6 15 23 6 | 90 98 91 98 97 92 94 93 90 103 91 27 | 5 14 8 8 24 6 10 6 9 15 3 | 11 16 14 15 30 13 18 14 15 14 12 28E | 8 18 13 13 33 4 19 6 9 12 4 | 16 30 26 23 36 18 28 21 21 22 20 29 | 6 23 10 11 27 4 27 6 6 20 4 | 19 31 19 15 26 18 32 18 18 17 17 30 | 7 18 6 10 32 3 15 11 9 23 4 | 37 46 41 40 58 38 47 38 40 44 40 31 | 10 22 7 10 26 5 21 10 13 23 5 | 15 31 21 16 37 18 30 17 23 17 16 32 | 7 17 8 11 34 7 18 7 11 27 4 | 10 21 18 15 26 11 22 15 16 29 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 18 9 13 32 5 18 8 10 20 |T 20 30 24 24 45 22 29 22 23 24 21 WRMS | 6 18 9 13 35 5 16 7 8 19 |NE 15 26 20 18 31 17 25 18 19 19 16 MEDI | 6 18 9 10 32 5 18 6 9 18 |MD 16 29 21 21 31 18 27 18 19 20 18 Table 3.1542.5 GPS week: 1542 Day: 5 MJD: 55043.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 14 --- --- 11 55 7 --- 7 17 --- 7 | 29 --- --- 28 332 32 --- 29 28 --- 29 2 | 5 14 8 9 49 6 11 7 10 29 4 | 14 22 18 19 28 15 19 16 19 15 15 3 | 9 16 11 10 27 4 10 6 8 23 4 | 15 21 19 17 25 15 21 17 16 31 16 4 | 7 12 7 7 33 5 8 7 8 37 4 | 18 28 20 21 28 19 25 18 20 25 18 6 | 8 14 9 8 29 4 10 6 8 18 3 | 12 23 17 14 26 14 22 12 12 24 12 7 | 6 14 11 9 36 5 16 8 8 20 4 | 15 25 21 19 34 16 25 17 15 20 16 8 | 6 11 10 9 16 3 8 9 9 18 3 | 13 21 17 16 25 14 17 16 15 17 13 9 | 5 13 8 8 28 4 10 6 11 16 3 | 14 18 15 12 22 15 17 18 16 10 13 10 | 7 13 7 3 30 4 8 6 8 16 3 | 14 20 16 14 30 16 19 14 16 15 13 11 | 8 14 12 9 68 3 17 8 10 19 4 | 34 35 37 36 34 33 36 34 32 31 32 12 | 7 17 10 9 24 4 18 7 12 17 4 | 18 26 24 21 28 20 22 19 17 18 17 13E | 6 15 10 9 35 4 18 7 9 13 4 | 15 21 18 15 39 14 20 15 16 15 13 14E | 6 14 10 14 27 4 16 6 12 14 4 | 14 21 20 20 36 14 22 16 16 17 14 15E | 6 20 13 18 29 7 21 9 5 23 5 | 12 24 18 24 29 16 20 15 14 32 12 16 | 10 26 14 11 34 4 19 9 8 18 5 | 20 28 22 20 41 18 27 21 20 19 19 17 | 6 20 10 8 30 7 18 11 6 17 4 | 13 30 18 15 39 14 28 19 13 14 15 X18 | 7 18 11 --- 35 5 20 7 10 16 4 | 13 24 16 --- 37 11 26 11 16 11 12 19 | 7 18 9 10 32 5 18 8 10 20 4 | 14 27 23 14 34 16 28 13 15 14 14 X20 | 6 21 11 --- 93 6 --- 5 13 17 5 | 8 21 13 --- 49 10 --- 11 8 11 8 X21 | 6 13 11 --- 27 4 14 8 10 31 5 | 17 23 24 --- 27 17 20 19 19 14 16 22 | 6 15 10 9 38 4 17 6 9 13 3 | 11 22 15 14 38 12 26 13 14 12 12 23E | 7 20 12 11 25 4 23 8 11 18 5 | 8 23 17 16 28 11 25 13 13 14 10 24 | 5 12 8 8 23 4 9 7 9 22 3 | 17 18 18 18 21 15 14 19 20 15 16 25 | 6 10 9 7 --- 5 8 5 10 24 3 | 11 17 15 15 --- 13 14 15 15 19 12 26E | 11 19 9 8 64 5 19 8 9 14 4 | 138 146 138 138 152 141 144 138 138 139 139 27 | 6 13 10 10 36 5 10 10 15 15 4 | 15 19 17 15 28 15 17 19 19 19 14 28E | 13 14 9 11 27 7 15 10 11 15 4 | 23 28 27 21 35 25 29 25 25 26 22 29 | 8 24 13 5 25 5 24 9 6 19 5 | 15 32 18 17 30 16 31 15 18 14 16 30 | 6 23 7 7 22 3 15 11 9 22 4 | 43 54 44 42 48 42 50 44 44 47 43 31 | 7 21 11 7 22 3 22 7 13 23 4 | 14 28 21 16 36 15 30 14 17 15 15 32 | 6 13 9 8 35 6 13 6 14 29 4 | 11 20 15 12 25 13 19 17 16 30 12 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 17 10 9 35 5 16 8 10 21 |T 20 28 24 23 46 21 28 22 22 23 20 WRMS | 7 17 10 9 35 5 14 7 9 22 |NE 14 23 18 16 30 15 22 16 16 17 14 MEDI | 6 14 10 9 30 4 16 7 10 18 |MD 14 23 18 17 30 15 22 17 16 17 15 Table 3.1542.6 GPS week: 1542 Day: 6 MJD: 55044.000 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 | 30 --- --- 18 75 18 --- 20 20 --- 13 | 45 --- --- 37 382 43 --- 33 37 --- 39 2 | 5 12 12 9 31 5 10 6 8 31 4 | 21 29 28 22 23 23 22 26 24 24 23 3 | 8 16 10 11 28 5 13 8 8 25 4 | 13 20 18 17 24 16 25 18 16 29 15 4 | 5 12 9 9 16 4 8 8 8 42 4 | 29 38 32 30 30 30 32 31 31 41 30 6 | 7 15 10 10 24 3 10 5 6 19 3 | 13 21 20 15 26 16 23 15 18 23 15 7 | 6 18 10 11 41 4 17 8 6 21 4 | 18 30 19 22 35 17 27 20 18 25 18 8 | 5 12 10 11 16 3 8 9 9 18 3 | 19 23 18 22 22 18 22 22 17 20 17 9 | 5 14 10 11 31 3 9 5 7 15 3 | 15 24 17 15 27 16 20 18 21 10 16 10 | 6 13 9 6 22 5 9 5 8 13 3 | 16 21 18 15 22 16 20 18 14 16 15 11 | 6 18 10 9 60 6 15 16 11 23 4 | 48 43 47 43 33 45 41 55 50 44 46 12 | 6 19 12 12 59 3 17 7 8 18 4 | 20 29 23 26 69 19 21 21 19 21 19 13E | 7 15 12 13 33 4 13 6 7 16 3 | 12 25 15 17 32 13 22 12 15 17 12 14E | 5 16 13 15 29 4 16 5 11 15 4 | 17 26 19 21 35 18 26 18 22 22 18 15E | 5 25 10 12 30 5 21 12 9 32 5 | 11 27 13 14 27 10 21 15 13 32 10 16 | 7 22 12 9 33 4 20 13 8 19 4 | 26 36 33 29 56 27 31 29 28 26 27 17 | 7 20 12 9 25 5 17 10 6 21 4 | 16 33 17 14 42 16 30 14 15 22 15 X18 | 7 19 16 --- 35 6 20 8 9 17 5 | 15 29 20 --- 39 17 26 16 20 15 17 19 | 5 19 11 9 41 4 17 10 6 20 4 | 17 31 22 17 42 19 30 16 19 19 18 X20 | 6 20 11 --- 30 5 18 7 9 14 4 | 7 19 10 --- 31 9 16 8 8 9 6 X21 | 7 13 11 --- 27 6 13 9 8 31 4 | 25 27 31 --- 27 27 25 30 29 26 26 22 | 6 14 13 10 36 5 15 8 10 14 4 | 17 25 21 17 40 18 27 20 22 19 19 23E | 7 21 17 12 25 3 23 8 9 19 5 | 12 27 18 12 29 13 27 14 17 20 12 24 | 6 12 11 10 28 4 9 11 7 25 3 | 26 28 29 32 21 28 23 31 29 24 28 25 | 4 13 7 5 --- 4 7 7 7 23 3 | 15 22 15 19 --- 15 18 18 16 19 14 26E | 9 21 11 10 61 6 18 7 12 29 5 | 136 139 135 136 153 136 142 136 134 148 137 27 | 5 13 10 10 43 4 10 7 9 18 3 | 20 22 21 17 41 19 23 21 23 16 19 28 | 7 16 9 10 24 5 15 8 7 21 4 | 17 21 18 17 28 16 23 16 21 26 16 29 | 7 25 11 9 27 4 22 9 9 20 5 | 21 37 18 17 33 19 33 21 23 21 21 30 | 7 22 11 10 20 3 17 9 9 21 4 | 54 59 52 52 57 52 60 54 53 56 53 31 | 7 21 10 11 23 6 19 9 9 26 4 | 17 31 25 22 38 19 29 19 17 22 18 32 | 7 13 10 9 23 3 15 7 10 29 4 | 13 17 17 15 26 14 21 15 20 30 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 6 17 11 10 34 4 15 9 8 23 |T 24 31 26 26 49 24 30 25 26 28 24 WRMS | 6 17 11 10 31 4 13 8 7 21 |NE 19 27 22 20 31 19 25 21 21 22 19 MEDI | 6 16 11 10 29 4 15 8 8 20 |MD 17 27 19 17 32 18 25 19 20 22 18 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1542 GPS week: 1542 MJD: 55038.0-55044.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2965 |U 8 8 23 |U 8 17 31 |U 8 8 20 | emr | emr 2863 | 10 12 30 | 9 15 38 |U 9 9 24 | esa | esa 2866 | 8 8 26 |U 7 16 32 | 8 8 20 | gfz | gfz 2647 |U 15 15 38 |U 36 77 354 | 9 10 25 | grg | grg 2838 | 9 11 29 |U 9 20 43 | 10 11 26 | igr | igr 2878 | 8 9 26 | 8 14 32 | 8 8 21 | igs | igs 2880 | 8 9 26 | 7 14 32 | 8 8 20 | jpl | jpl 2807 | 9 11 29 |U 8 15 60 |U 9 8 23 | mit | mit 2962 |U 13 14 36 |U 7 13 33 |U 11 11 26 | 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 5.1542.0 GPS week: 1542 Day: 0 MJD: 55038.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2949 | 8 11 15 | 10 11 34 | 8 8 19 | emr | emr 2871 | 10 17 20 | 9 9 38 | 8 9 26 | esa | esa 2879 | 8 11 17 | 8 15 33 | 8 8 22 | gfz | gfz 2567 | 11 20 33 | 108 257 1311 | 8 10 27 | grg | grg 2880 | 9 14 20 | 10 13 34 | ---- ---- ---- | igr | igr 2822 | 8 10 16 | 10 13 31 | 7 8 23 | igs | igs 2841 | 8 11 15 | 8 9 30 | 8 8 21 | jpl | jpl 2778 | 9 14 20 | 8 9 38 | 7 7 22 | mit | mit 2976 | 7 8 15 | 8 9 30 | 9 9 21 | Table 5.1542.1 GPS week: 1542 Day: 1 MJD: 55039.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2972 | 9 10 27 | 9 35 46 | 7 6 20 | emr | emr 2880 | 9 11 30 | 12 15 69 | 8 8 25 | esa | esa 2880 | 9 9 30 | 9 19 56 | 7 6 22 | gfz | gfz 2653 | 15 16 39 | 22 50 248 | 9 7 29 | grg | grg 2784 | 10 12 34 | 8 17 53 | 10 9 27 | igr | igr 2880 | 9 9 33 | 10 19 59 | 6 6 21 | igs | igs 2880 | 9 10 29 | 9 20 58 | 7 6 22 | jpl | jpl 2783 | 11 11 30 | 13 31 176 | 9 7 25 | mit | mit 2976 | 8 10 29 | 8 14 49 | 7 6 21 | Table 5.1542.2 GPS week: 1542 Day: 2 MJD: 55040.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2957 | 6 6 23 | 8 19 29 | 7 7 21 | emr | emr 2880 | 8 10 30 | 7 21 30 | 10 8 28 | esa | esa 2880 | 8 6 26 | 6 21 27 | 7 5 21 | gfz | gfz 2657 | 13 15 43 | 19 33 98 | 9 9 25 | grg | grg 2784 | 9 10 36 | 11 26 40 | 9 6 25 | igr | igr 2880 | 7 6 24 | 8 19 26 | 8 6 21 | igs | igs 2880 | 8 7 26 | 7 18 27 | 7 6 21 | jpl | jpl 2879 | 8 9 27 | 6 19 33 | 8 6 26 | mit | mit 2976 | 20 14 50 | 7 17 30 | 24 17 54 | Table 5.1542.3 GPS week: 1542 Day: 3 MJD: 55041.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2965 | 9 10 28 | 8 16 30 | 10 12 22 | emr | emr 2880 | 10 13 35 | 9 24 32 | 10 14 21 | esa | esa 2879 | 9 10 30 | 8 22 30 | 10 11 21 | gfz | gfz 2667 | 31 15 48 | 16 28 86 | 11 15 25 | grg | grg 2880 | 10 10 32 | 12 31 47 | 11 15 27 | igr | igr 2905 | 9 10 29 | 8 15 27 | 10 11 20 | igs | igs 2955 | 9 10 31 | 8 17 26 | 10 12 20 | jpl | jpl 2784 | 10 12 32 | 8 11 34 | 10 11 22 | mit | mit 2976 | 16 11 51 | 8 17 37 | 11 13 25 | Table 5.1542.4 GPS week: 1542 Day: 4 MJD: 55042.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2975 | 9 10 23 | ---- ---- ---- | 8 8 18 | emr | emr 2780 | 11 16 37 | ---- ---- ---- | 11 8 19 | esa | esa 2784 | 9 10 29 | ---- ---- ---- | 8 9 18 | gfz | gfz 2657 | 13 15 35 | ---- ---- ---- | 9 14 21 | grg | grg 2784 | 11 18 29 | ---- ---- ---- | 10 11 23 | igr | igr 2842 | 10 13 32 | ---- ---- ---- | 9 8 17 | igs | igs 2780 | 10 13 32 | ---- ---- ---- | 9 7 17 | jpl | jpl 2780 | 11 16 37 | ---- ---- ---- | 9 8 18 | mit | mit 2880 | 12 17 41 | ---- ---- ---- | 10 8 16 | Table 5.1542.5 GPS week: 1542 Day: 5 MJD: 55043.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2971 | 8 4 23 | ---- ---- ---- | 8 8 15 | emr | emr 2876 | 10 9 24 | ---- ---- ---- | 10 7 19 | esa | esa 2880 | 9 5 24 | ---- ---- ---- | 7 8 13 | gfz | gfz 2663 | 11 10 25 | ---- ---- ---- | 8 7 20 | grg | grg 2880 | 11 6 22 | ---- ---- ---- | 11 14 26 | igr | igr 2899 | 8 5 21 | ---- ---- ---- | 7 6 12 | igs | igs 2878 | 8 4 23 | ---- ---- ---- | 7 7 13 | jpl | jpl 2774 | 10 9 26 | ---- ---- ---- | 9 8 19 | mit | mit 2976 | 18 30 40 | ---- ---- ---- | 8 8 15 | Table 5.1542.6 GPS week: 1542 Day: 6 MJD: 55044.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2972 | 8 6 25 | 5 5 18 | 7 10 24 | emr | emr 2876 | 9 11 30 | 7 8 19 | 10 11 33 | esa | esa 2880 | 8 6 26 | 5 6 17 | 8 10 28 | gfz | gfz 2669 | 12 12 42 | 13 16 27 | 8 11 28 | grg | grg 2880 | 7 9 33 | 8 13 41 | 9 13 28 | igr | igr 2918 | 7 6 27 | 6 5 17 | 8 12 29 | igs | igs 2947 | 8 7 26 | 5 6 17 | 9 12 29 | jpl | jpl 2874 | 8 8 31 | 6 7 20 | 8 11 29 | mit | mit 2976 | 7 5 29 | 6 6 19 | 9 13 30 | 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 6.1542 GPS week: 1542 MJD: 55038.500-55044.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -9 -17 -23 103 7 | -5 14 | 24 18 80 88 7 | 1 emr uuxuu | -7 -54 385 -61 -3 | 21 34 | 17 16 128 44 6 | 4 esa uuuuu | -45 -34 69 -227 -2 | 22 32 | 25 17 108 71 17 | 1 gfz uuuuu | 22 4 70 -21 -6 | 19 25 | 9 15 32 91 8 | 2 grg xxxxx | -7 -9 -81 121 11 | 2 22 | 31 47 112 99 15 | 6 igr xxxxx | 16 5 71 94 -5 | 5 15 | 23 32 28 105 6 | 2 irf xxxxx | -9 -7 6 -7 -4 | 2 20 | 13 10 19 47 11 | 2 jpl uuuuu | -10 -14 103 189 5 | 0 18 | 32 30 84 99 6 | 2 mit uuuuu | 1 -16 -106 -87 -5 | 7 24 | 19 14 33 141 12 | 2 ngs uuuuu | 15 57 -71 245 1 | 11 17 | 47 46 78 178 11 | 3 sio uuuuu | 38 93 -35 87 -9 | 14 28 | 16 25 75 81 13 | 3 Table 7.1542.0 GPS week: 1542 Day: 0 MJD: 55038.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -15 -42 -25 209 -1 | -6 15 emr uuxuu | -17 -48 200 -107 -11 | 14 35 esa uuuuu | -30 -32 -35 -315 26 | 21 30 gfz uuuuu | 34 -2 86 131 5 | 18 23 grg xxxxx | -26 -69 -3 204 36 | -8 21 igr xxxxx | 5 -24 70 226 3 | 5 12 irf xxxxx | 2 -13 -27 -52 -22 | 4 20 jpl uuuuu | -35 -18 223 234 -2 | -1 18 mit uuuuu | 2 -29 -60 -252 -23 | 7 25 ngs uuuuu | -2 120 -213 484 8 | 7 13 sio uuuuu | 54 66 -65 -2 -30 | 14 30 Table 7.1542.1 GPS week: 1542 Day: 1 MJD: 55039.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -18 -30 78 33 -3 | -6 14 emr uuxuu | -12 -67 234 -107 -8 | 17 36 esa uuuuu | -64 -59 51 -249 13 | 22 32 gfz uuuuu | 11 -18 100 -26 -10 | 20 26 grg xxxxx | 35 16 100 206 20 | -3 26 igr xxxxx | 31 18 51 36 1 | 6 14 irf xxxxx | -12 1 -7 -49 -16 | 3 20 jpl uuuuu | 3 -33 186 336 0 | 1 19 mit uuuuu | -6 -3 -110 -221 -20 | 7 25 ngs uuuuu | 52 111 -104 497 17 | 9 16 sio uuuuu | 39 114 -154 -3 -23 | 14 30 Table 7.1542.2 GPS week: 1542 Day: 2 MJD: 55040.500 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 | -54 8 84 243 10 | -5 13 emr uuxuu | -20 -70 508 -32 -4 | 21 34 esa uuuuu | -79 -37 56 -162 -7 | 25 34 gfz uuuuu | 9 -12 99 -82 -8 | 21 26 grg xxxxx | 3 8 -124 41 5 | 1 25 igr xxxxx | 2 -40 74 49 -2 | 7 14 irf xxxxx | -31 -9 9 -29 -3 | 4 19 jpl uuuuu | -5 -8 53 267 2 | 3 17 mit uuuuu | -33 -17 -106 -133 -1 | 8 24 ngs uuuuu | 104 60 -38 202 8 | 13 17 sio uuuuu | 14 96 -30 69 -8 | 16 29 Table 7.1542.3 GPS week: 1542 Day: 3 MJD: 55041.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 15 -31 -134 90 14 | -6 14 emr uuxuu | 24 -65 544 -4 0 | 23 33 esa uuuuu | -21 -4 240 -148 -22 | 22 33 gfz uuuuu | 30 18 57 37 5 | 20 26 grg xxxxx | 33 -78 -220 213 -14 | 3 22 igr xxxxx | 53 -21 44 246 -7 | 6 15 irf xxxxx | -15 11 5 -34 -2 | 3 20 jpl uuuuu | -24 -54 31 125 2 | 1 18 mit uuuuu | -6 7 -169 -128 0 | 8 24 ngs uuuuu | -3 -8 -87 137 5 | 13 17 sio uuuuu | 29 134 -97 38 -7 | 16 29 Table 7.1542.4 GPS week: 1542 Day: 4 MJD: 55042.500 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 | -12 2 -21 79 12 | -4 15 emr uuxuu | -26 -58 411 -92 0 | 26 34 esa uuuuu | -38 -38 130 -193 -11 | 21 33 gfz uuuuu | 22 6 73 23 -6 | 21 27 grg xxxxx | -27 49 -199 172 7 | 6 21 igr xxxxx | 3 38 105 106 -8 | 5 15 irf xxxxx | -1 -12 32 1 3 | 3 20 jpl uuuuu | 18 39 4 174 11 | 1 18 mit uuuuu | 20 -18 -113 -48 5 | 9 25 ngs uuuuu | -18 32 -58 157 -9 | 14 19 sio uuuuu | 46 98 48 161 1 | 16 28 Table 7.1542.5 GPS week: 1542 Day: 5 MJD: 55043.500 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 -19 -67 59 14 | -3 15 emr uuxuu | 2 -44 383 -71 7 | 25 34 esa uuuuu | -14 -43 -83 -197 -13 | 22 33 gfz uuuuu | 27 20 65 -107 -9 | 19 26 grg xxxxx | -47 17 -46 -22 17 | 6 20 igr xxxxx | 31 27 111 -27 -7 | 4 16 irf xxxxx | 7 -14 10 45 6 | 2 20 jpl uuuuu | -59 -27 149 35 12 | -1 18 mit uuuuu | 22 -19 -95 23 7 | 8 25 ngs uuuuu | -29 55 42 214 -12 | 13 19 sio uuuuu | 59 76 5 166 5 | 13 27 Table 7.1542.6 GPS week: 1542 Day: 6 MJD: 55044.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 10 -11 -74 10 5 | -5 15 emr uuxuu | -3 -24 414 -14 -2 | 22 31 esa uuuuu | -69 -24 121 -323 1 | 21 33 gfz uuuuu | 18 13 9 -122 -18 | 15 25 grg xxxxx | -17 -6 -79 37 9 | 7 20 igr xxxxx | -13 36 44 23 -15 | 1 17 irf xxxxx | -10 -16 19 69 4 | -2 19 jpl uuuuu | 32 3 72 154 12 | -4 16 mit uuuuu | 5 -31 -89 152 0 | 4 22 ngs uuuuu | 4 29 -41 26 -7 | 10 20 sio uuuuu | 28 69 46 181 2 | 9 24