Date: Thu, 17 Sep 2009 11:38:33 +0000 From: Jim Ray Subject: [IGSREPORT-17804] Wk 1547 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4ab21fb9.DwfukWUi+FLKn0FJ%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 17 Sep 04:38:57 PDT 2009 Message Number 17804 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1547 (Aug 30, 2009 - Sep 05, 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: igs1547[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1547[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1547[0-6].cls IGS GPS clock combination summary report. igs15477.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15477.sum Complete report. REMARKS concerning the IGS Orbit Combination: --------------------------------------------- 1. The centres used in the clock combination are COD, EMR, ESA, GFZ, MIT, and JPL. The other centres are excluded because they either provide broadcast clocks (NGS) or clock corrections are not provided (SIO). The clock information not used is still compared to combination for completeness. The value of 999999.999999 microseconds, according to the sp3 format convention, is used to signify that no clock solution is available and therefore must not be used. 2. Rapid (IGR) orbits/clocks are included in the combination for statistics only. Starting week 1478, a new solution from CNES/GRGS (GRG) is included for evaluation and statistics only. 3. The following centre clock solutions, which provide broadcast clock corrections, were excluded from the combination but kept in the combination statistics: -> Centre: NGS 4. The following clock solutions were excluded from the combination because they were biasing the combined clock solutions (clock shifts/outliers) but were kept for the RMS computation. Duplicate entries can arise due to separate combination runs for the 30-s clocks ACs (listed first) and the 5-min clock ACs (listed second). Day | Centre | PRN/STA list ----+--------+--------------- 0 | ALL | 1 0 | COD | 3 6 26 3 6 26 AREQ HARB SCH2 0 | EMR | 5 5 WTZR WTZR 0 | ESA | 3 26 CHUR 0 | GFZ | 14 19 21 25 26 FAA1 KIRU MAS1 NANO NYA1 TRO1 UNSA 0 | GRG | ONSA 0 | JPL | 5 6 32 AREQ 0 | MIT | MIZU MIZU TLSE 1 | ALL | 1 1 | COD | 6 26 6 26 1 | EMR | 5 3 5 WTZR WTZR 1 | ESA | 3 6 26 1 | GFZ | 14 CHUR HARB MIZU TSKB UNSA 1 | GRG | ONSA 1 | JPL | 5 32 1 | MIT | 22 22 25 HARB 2 | ALL | 1 3 2 | COD | 3 6 26 6 26 VESL 2 | EMR | 5 5 HARB WTZR HARB WTZR 2 | ESA | 6 26 UNSA 2 | GFZ | 6 14 17 19 32 ANKR AUCK BAKO DARW FAA1 HOB2 MCM4 2 | GFZ | NRMD TOW2 TWTF USUD 2 | GRG | TWTF USNO 2 | JPL | 5 32 HARB 3 | ALL | 1 1 3 | COD | 3 6 3 6 NANO 3 | EMR | 5 5 HARB WTZR WTZR 3 | ESA | 3 6 UNSA 3 | GFZ | 6 14 17 ALGO GUAT KIRU NLIB PRDS QAQ1 SCH2 VILL WHIT 3 | GRG | USNO 3 | JPL | 5 32 VESL 3 | MIT | 25 25 TWTF 4 | COD | 6 6 MIZU MIZU TIDB 4 | EMR | 5 21 5 21 WTZR AREQ WTZR 4 | ESA | 6 UNSA ZWE2 4 | GFZ | 1 3 6 14 17 23 26 29 FAA1 HARB MIZU NLIB OHI2 THTI 4 | GRG | ONSA 4 | JPL | 6 GODE MDVJ VESL 4 | MIT | 3 25 26 3 25 26 4 | NGS | 1 5 | ALL | 1 1 6 5 | COD | 3 25 3 25 DAV1 HARB 5 | EMR | 5 5 WTZR WTZR 5 | ESA | 3 32 TWTF 5 | GFZ | 3 17 19 23 29 FAA1 HARB REUN WSRT 5 | GRG | PIE1 5 | JPL | 26 5 | MIT | 26 26 TWTF MAW1 TWTF 6 | ALL | 1 1 6 | COD | 3 6 3 6 6 | EMR | HARB WTZR HARB TWTF WTZR 6 | ESA | 3 6 UNSA ZWE2 6 | GFZ | 3 14 17 19 22 29 ALIC AUCK BRAZ CHAT DAV1 FAA1 HOB2 6 | GFZ | KERG MAC1 MCM4 NTUS ONSA SANT TOW2 6 | GRG | USNO 6 | JPL | 3 26 6 | MIT | 25 26 25 26 TWTF 5. 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 ----+------------+---------- G26 | 2009_09_02 | 2009059 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 G03 | 2 | 1 | | | | | | PRN G06 | | | | | | | 1 | 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 | .3 .6 1.1 -8 -2 -9 -.29 EMR | 3.6 2.9 -12.3 82 -15 41 .30 ESA | 3.1 2.4 2.4 37 -60 22 .09 GFZ | -.1 .9 1.3 13 -6 0 -.14 GRG | 5.1 .1 6.3 -8 -9 21 .06 JPL | -3.9 3.9 -6.9 28 0 -21 .12 MIT | 1.2 -6.5 9.1 9 4 -11 -.26 NGS | 3.1 1.4 3.4 14 -18 -18 -.14 SIO | -.8 -3.4 -9.5 -73 -26 -5 .15 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 1.1547.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1547.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 2.1547.[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 3.1547.[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 5.1547.0-6). 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 1547 summary. (Aug 30, 2009 - Sep 05, 2009) Table 1.1547.a GPS week: 1547 MJD: 55073.000-55079.000 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 228| 0 0 -1 42 -14 10 -.18 8 7 | -521 160 13 59 | 0 0 0 13 15 15 .02 | 349 502 emr 81| 0 0 -6 -177 4 -4 .54 18 18 | 1637 -264 17 78 | 1 2 1 23 36 13 .03 | 1140 1207 esa 138| 0 0 1 -63 118 -20 .34 9 9 | -1566 1037 18 120 | 0 1 1 18 27 15 .03 | 1197 1228 gfz 186| 0 0 3 16 -58 -9 -.16 11 11 | -13 -104 25 114 | 1 1 1 33 62 11 .04 | 329 704 grg 110| 2 0 0 36 6 21 1.06 39 35 | -8 75 77 223 | 2 0 1 19 18 71 .06 | 243 520 igr n/a| 0 0 0 28 -18 -60 .08 6 5 | -7057 -689 21 69 | 0 0 0 16 15 57 .05 | 2074 1532 jpl 142| 2 0 -8 -22 -20 21 .63 19 18 | 983 -184 18 96 | 1 0 1 12 29 33 .09 | 1221 1354 mit 257| 0 -1 1 17 -68 4 -.21 10 9 | -14659 -526 19 123 | 0 0 1 6 23 9 .03 | 877 929 ngs 220| 0 1 1 2 0 0 -.33 11 8 | -713791 1758709 2291 15946 | 1 0 1 27 40 18 .03 | 757233 1313302 sio 256| -1 0 4 184 17 27 -.04 20 17 | --- --- --- --- | 1 0 1 17 25 8 .02 | --- --- Table 1.1547.b GPS week : 1547 MJD: 55073.000-55079.000 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 | 13 12 12 11 11 11 12 | 2 | 5 5 5 5 5 5 5 | 3 | 5 6 9 7 6 6 7 | 4 | 4 4 4 4 4 4 4 | 5 | 8 7 6 6 7 6 6 | 6 | 6 6 7 6 6 9 7 | 7 | 5 4 5 5 4 5 5 | 8 | 3 4 3 3 3 3 4 | 9 | 4 3 3 3 4 4 4 | 10 | 4 3 4 4 3 4 4 | 11 | 3 4 4 4 4 4 4 | 12 | 5 5 5 6 6 5 5 | 13 | 4 4 4 7 5 4 5 | 14 | 4 4 4 4 4 4 4 | 15 | 5 5 5 5 5 5 5 | 16 | 6 5 5 6 6 6 6 | 17 | 4 5 4 5 5 5 5 | 18 | 5 5 5 5 5 5 5 | 19 | 5 4 5 5 5 5 6 | 20 | 5 5 5 5 5 5 5 | 21 | 5 5 5 5 5 5 5 | 22 | 4 4 4 5 5 5 5 | 23 | 5 5 5 5 5 4 5 | 24 | 3 3 4 4 4 3 4 | 25 | 10 7 8 9 8 9 11 | 26 | 6 5 6 0 9 6 6 | 27 | 4 3 4 3 4 4 4 | 28 | 4 5 5 5 5 5 5 | 29 | 5 5 5 6 5 5 5 | 30 | 3 3 3 4 3 3 3 | 31 | 5 5 5 5 5 5 5 | 32 | 4 4 4 4 4 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 2.1547.0 GPS week: 1547 Day: 0 MJD: 55073.000 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 228| 0 0 -2 47 9 23 -.16 8 7 | -430 -149 13 49 | -12 -78 | emr 81| 0 -2 -5 -179 17 -14 .58 18 18 | 3344 -1160 18 78 | 19 -55 | esa 138| 0 -1 0 -60 96 -10 .30 9 9 | -1303 497 18 113 | 39 -19 | gfz 186| 1 0 1 -7 -58 3 -.13 10 10 | 597 -1279 26 102 | -38 -71 | grg 110| 1 0 -1 11 15 45 1.10 40 35 | 239 -597 81 223 | 63 -52 | igr n/a| 1 0 0 16 -6 -33 .09 6 5 | -3402 -2187 18 74 | 13 -33 | jpl 142| 1 0 -10 -40 4 3 .68 19 18 | 2750 -1362 17 95 | 15 -94 | mit 257| 0 0 3 19 -99 6 -.25 10 9 | -13917 -1786 23 113 | -18 39 | ngs 220| 0 1 3 26 19 -34 -.34 10 7 | 1003452 -999999 2411 3928 | -21 23 | sio 256| -4 0 4 197 -17 44 -.05 21 18 | --- --- --- --- | -90 -10 | Table 2.1547.1 GPS week: 1547 Day: 1 MJD: 55074.000 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 228| 0 0 -2 61 -17 -17 -.16 8 7 | -973 672 16 67 | 5 -8 | emr 81| 0 3 -7 -169 1 20 .53 18 18 | 2352 -1053 19 82 | 33 -15 | esa 138| 1 -2 2 -83 111 5 .35 8 8 | -2744 1750 17 117 | 32 -18 | gfz 186| 1 0 3 -19 -75 -8 -.13 10 10 | -412 534 26 105 | -33 -25 | grg 110| 2 0 1 39 -25 -80 1.03 41 35 | -401 659 81 248 | 5 -21 | igr n/a| 0 0 0 45 -14 -16 .06 6 5 | -5477 -1941 19 62 | -26 -30 | jpl 142| 3 0 -10 -18 -44 79 .66 19 19 | 1501 -1192 18 86 | 28 40 | mit 257| 0 -1 2 23 -40 -6 -.24 9 8 | -15035 293 19 107 | -8 31 | ngs 220| -1 1 2 20 10 -5 -.39 11 7 | -999999 3312655 2119 87974 | -44 -27 | sio 256| -2 1 2 201 36 24 -.04 20 19 | --- --- --- --- | -80 -4 | Table 2.1547.2 GPS week: 1547 Day: 2 MJD: 55075.000 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 228| 0 0 0 49 -17 11 -.17 8 7 | -899 530 11 48 | 5 -37 | emr 81| 1 -1 -7 -183 -28 -6 .57 19 19 | 1142 -874 16 73 | 65 16 | esa 138| 0 0 0 -91 155 -32 .38 9 9 | -2901 712 18 112 | 35 -42 | gfz 186| -1 0 4 -5 -27 1 -.21 11 11 | -275 35 23 107 | -68 -23 | grg 110| 3 1 0 64 14 14 .97 39 35 | -197 -22 73 220 | 40 -14 | igr n/a| 0 0 0 31 -20 -10 .13 5 5 | -7421 -1397 18 60 | 28 -15 | jpl 142| 3 1 -9 -33 -28 44 .72 20 19 | 247 -697 18 83 | 71 -11 | mit 257| 0 0 2 18 -84 -7 -.24 9 9 | -15936 229 21 128 | -7 42 | ngs 220| -2 0 1 18 -9 6 -.33 10 8 | -999999 2009107 2095 3547 | -47 9 | sio 256| -1 1 2 195 9 27 -.06 22 16 | --- --- --- --- | -86 -4 | Table 2.1547.3 GPS week: 1547 Day: 3 MJD: 55076.000 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 228| 0 0 -1 33 -38 16 -.17 8 7 | -730 784 15 63 | 32 11 | emr 81| 0 0 -7 -204 -36 -5 .55 19 19 | 1473 -400 19 82 | 60 21 | esa 138| 1 0 0 -58 145 -17 .33 10 10 | -1814 2314 21 122 | 7 -48 | gfz 186| 0 1 5 55 18 -16 -.14 13 13 | 130 -662 29 127 | -35 -17 | grg 110| 0 0 1 17 -16 90 1.12 40 40 | -129 805 76 206 | 90 57 | igr n/a| 0 0 0 4 -41 -49 .09 6 5 | -7628 -731 21 67 | 24 9 | jpl 142| -1 -1 -9 -28 -52 2 .70 20 19 | 777 -346 20 92 | -11 24 | mit 257| 0 -1 2 25 -39 0 -.20 11 9 | -15298 236 21 127 | -4 15 | ngs 220| -1 0 3 -9 -65 -4 -.34 11 7 | -999999 2065291 1992 3873 | -7 69 | sio 256| 0 0 3 199 53 22 -.06 20 17 | --- --- --- --- | -81 -22 | Table 2.1547.4 GPS week: 1547 Day: 4 MJD: 55077.000 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 228| 0 0 0 25 -24 2 -.18 7 7 | -294 15 15 72 | 13 -16 | emr 81| -2 1 -7 -196 -19 -15 .52 19 19 | 986 -1117 16 71 | 45 -3 | esa 138| 1 0 3 -37 133 -35 .37 10 10 | -2123 2612 21 117 | -37 -64 | gfz 186| 0 -1 3 48 0 2 -.15 12 12 | -163 446 25 103 | -18 -9 | grg 110| 0 0 -1 55 16 31 1.10 39 33 | 41 80 75 224 | 52 28 | igr n/a| 0 0 0 17 -38 -36 .11 5 5 | -8521 -1224 21 74 | -31 9 | jpl 142| 2 1 -10 -9 -45 7 .65 19 19 | 196 -884 21 106 | -48 -36 | mit 257| 0 -2 1 10 -55 19 -.17 10 9 | -14208 -1771 17 123 | -8 34 | ngs 220| 0 1 0 -45 -35 3 -.32 11 9 | -999999 1841531 2352 3904 | 18 34 | sio 256| 0 0 4 167 37 29 -.02 18 18 | --- --- --- --- | -67 -18 | Table 2.1547.5 GPS week: 1547 Day: 5 MJD: 55078.000 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 228| 0 0 -2 30 -5 28 -.17 8 7 | -264 -184 12 70 | 9 -56 | emr 81| -1 -1 -5 -175 28 5 .52 18 18 | -155 2016 15 87 | 32 -27 | esa 138| 0 -1 1 -49 106 -33 .35 9 8 | -459 139 20 141 | 4 -16 | gfz 186| 0 0 4 50 -102 -25 -.16 12 12 | 74 -394 22 110 | -65 -2 | grg 110| 3 0 0 37 22 113 1.09 39 36 | 142 -466 84 218 | 35 -60 | igr n/a| 0 0 0 36 -9 -109 .09 6 5 | -9767 2148 24 72 | -53 -48 | jpl 142| 3 1 -6 -13 5 -20 .56 18 18 | -742 2462 18 102 | -10 -28 | mit 257| 0 0 0 6 -81 4 -.19 10 8 | -13375 -765 17 133 | -2 35 | ngs 220| 0 1 0 -20 23 4 -.28 12 9 | -999999 2051578 2496 4029 | -46 -20 | sio 256| 0 0 5 168 12 26 -.02 19 16 | --- --- --- --- | -66 -14 | Table 2.1547.6 GPS week: 1547 Day: 6 MJD: 55079.000 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 228| 1 -1 -1 52 -6 6 -.22 9 8 | -58 -542 11 50 | -10 -37 | emr 81| 1 0 -2 -131 68 -15 .49 19 19 | 2321 737 16 75 | -9 -70 | esa 138| 0 -1 2 -63 79 -22 .32 8 7 | 376 -759 17 124 | 37 -4 | gfz 186| 0 1 0 -8 -163 -21 -.22 11 11 | -44 586 26 150 | -83 30 | grg 110| 5 -1 -1 29 16 -61 1.03 36 29 | 248 66 71 226 | -1 -57 | igr n/a| 0 0 0 47 -1 -167 -.03 6 6 | -7183 509 26 79 | 5 -47 | jpl 142| 1 0 -6 -11 16 32 .47 20 18 | 2157 726 19 111 | 20 -19 | mit 257| 0 -1 0 16 -81 12 -.20 11 9 | -14850 -120 21 131 | -15 28 | ngs 220| 0 2 0 26 58 26 -.31 13 10 | -999999 2030801 2573 4368 | -77 -36 | sio 256| -2 1 6 160 -5 15 -.05 21 16 | --- --- --- --- | -66 -6 | 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 3.1547.0 GPS week: 1547 Day: 0 MJD: 55073.000 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 | 24 --- --- 26 --- 24 --- 17 21 --- 12 | 15 --- --- 23 --- 22 --- 19 21 --- 15 2 | 7 19 8 9 39 5 22 11 6 27 4 | 18 30 22 22 48 18 32 20 17 29 19 3E | 10 16 8 8 109 6 18 16 17 24 5 | 94 101 99 93 108 96 103 102 94 100 97 4 | 5 11 5 9 36 6 12 9 9 23 3 | 33 34 34 39 23 35 29 37 37 35 33 5 | 28 25 9 13 37 20 26 16 9 33 7 | 103 97 98 98 89 99 67 99 100 105 99 6E | 11 20 10 12 37 8 21 18 14 32 6 | 74 71 69 71 53 68 63 68 73 68 70 7 | 9 18 11 12 31 5 17 6 10 15 4 | 18 29 27 24 40 22 28 19 16 19 20 8 | 7 11 6 8 21 3 10 6 8 10 3 | 14 23 20 16 22 15 22 16 18 13 16 9 | 6 13 7 7 31 3 12 12 6 22 3 | 22 24 24 19 33 20 27 18 22 16 21 10 | 5 19 7 7 41 6 9 9 8 22 3 | 23 30 27 30 23 24 24 29 25 29 25 11 | 4 14 6 9 57 5 17 6 8 14 3 | 30 39 37 28 61 31 40 30 31 29 31 12 | 6 20 11 14 34 6 21 9 8 24 4 | 25 40 27 26 50 23 39 26 27 25 26 13E | 7 16 9 10 23 7 21 10 5 14 4 | 14 28 20 20 35 15 28 12 15 16 15 14E | 5 12 8 7 29 6 20 8 11 13 3 | 25 33 28 30 34 27 35 29 26 28 28 15E | 7 21 11 10 37 5 21 11 6 10 4 | 21 29 26 20 39 20 25 24 20 23 20 16 | 6 21 12 18 30 5 26 9 10 34 5 | 18 32 20 15 39 17 34 20 22 26 20 17E | 8 13 8 8 28 5 23 10 9 18 4 | 69 74 71 66 76 67 73 65 64 65 68 18 | 6 20 7 10 27 7 21 10 8 26 4 | 18 29 24 26 35 22 30 23 22 18 21 19E | 5 19 10 10 27 5 22 9 9 15 4 | 26 34 33 26 42 27 32 24 25 27 26 20 | 6 14 10 10 39 4 18 6 9 28 4 | 26 31 37 32 35 28 29 29 28 27 28 21 | 9 21 9 13 31 7 23 8 8 20 5 | 25 38 33 26 45 27 39 25 26 25 27 22 | 5 16 8 8 35 6 20 7 7 21 4 | 25 30 32 33 33 29 29 28 32 20 28 23E | 7 22 10 9 38 5 20 12 9 15 4 | 16 29 23 15 33 17 26 20 18 22 17 24 | 5 15 7 11 24 4 11 5 6 17 3 | 27 31 37 37 40 30 28 32 33 30 31 X25 | 12 30 28 21 --- 9 --- 13 25 --- 9 | 26 48 44 26 --- 26 --- 23 19 --- 27 26E | 10 24 10 8 49 5 15 13 20 25 5 | 9 24 12 13 17 8 15 17 22 16 9 27 | 6 14 7 6 31 4 11 10 7 20 3 | 27 31 30 24 40 26 32 24 28 20 27 28 | 6 20 6 9 41 5 19 10 9 21 4 | 12 29 16 16 45 13 27 11 14 19 12 29E | 7 17 10 15 52 6 24 11 9 13 4 | 61 61 64 63 71 61 64 58 59 59 60 30 | 5 14 6 6 23 5 11 8 8 12 3 | 18 25 22 20 27 16 24 18 19 16 18 31 | 5 20 10 16 34 4 20 10 10 17 4 | 17 29 22 26 38 17 26 19 18 17 19 32 | 6 14 8 10 27 5 17 10 13 18 4 | 18 25 27 21 23 18 20 22 20 19 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 9 10 40 6 19 10 10 21 |T 30 38 35 32 43 30 36 31 31 32 31 WRMS | 7 18 9 10 35 5 18 9 7 18 |NE 25 34 31 28 39 26 31 26 27 26 26 MEDI | 6 18 8 10 34 5 20 10 9 20 |MD 23 31 27 26 39 23 29 24 22 25 25 Table 3.1547.1 GPS week: 1547 Day: 1 MJD: 55074.000 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 | 19 --- --- 23 --- 27 --- 11 27 --- 11 | 17 --- --- 28 --- 25 --- 20 26 --- 18 2 | 6 21 10 6 42 6 25 12 7 25 5 | 18 32 28 19 37 21 34 21 20 30 21 3E | 13 17 6 14 108 5 19 13 20 20 5 | 109 116 115 107 125 111 119 117 111 121 113 4 | 6 12 6 7 22 5 14 10 5 22 3 | 28 28 28 33 23 30 24 32 32 30 28 5 | 22 26 9 11 34 19 27 14 11 31 7 | 68 61 61 61 53 62 50 66 65 68 63 6E | 11 17 10 15 69 8 18 20 16 34 6 | 61 58 56 59 42 56 60 53 59 57 56 7 | 6 15 6 8 32 5 19 5 8 16 3 | 14 27 21 20 38 17 30 16 14 15 16 8 | 8 12 7 9 24 4 11 7 11 11 3 | 11 21 19 15 22 14 23 15 11 12 13 9 | 7 12 4 10 42 2 13 10 6 14 3 | 19 24 23 19 33 20 23 26 27 26 21 10 | 4 12 5 7 26 4 11 7 10 18 3 | 19 24 24 25 23 23 21 26 25 21 22 11 | 5 14 8 10 48 4 17 7 9 17 3 | 22 36 32 26 53 28 40 25 26 22 26 12 | 6 19 10 12 33 5 23 7 9 24 4 | 22 36 28 27 39 26 36 27 28 27 25 13E | 6 21 9 9 24 4 23 6 9 13 4 | 15 29 24 18 37 18 29 15 15 19 17 14E | 5 12 8 10 29 3 17 7 6 13 3 | 21 25 26 19 32 20 27 21 19 20 20 15E | 7 23 8 8 41 4 26 9 11 11 4 | 20 27 26 24 42 20 26 25 29 25 23 16 | 6 20 10 17 33 6 22 7 13 30 5 | 14 28 19 12 35 14 31 18 15 24 15 17E | 8 15 5 8 22 4 23 16 11 11 4 | 52 58 57 52 62 54 59 57 53 58 54 18 | 6 18 7 11 36 3 21 10 6 24 4 | 15 28 23 21 33 19 30 20 18 16 18 19E | 6 16 8 11 30 6 24 8 11 15 4 | 20 30 27 25 31 23 31 20 21 23 21 20 | 7 17 9 11 40 4 18 8 10 26 4 | 16 27 26 23 31 20 28 18 22 17 18 21 | 6 23 7 12 31 3 23 6 9 23 4 | 25 40 29 29 47 26 40 25 25 27 26 22 | 5 19 8 8 44 3 19 6 7 19 4 | 18 29 25 23 31 20 29 22 21 17 20 23E | 7 22 9 11 30 4 21 9 9 16 4 | 12 28 22 18 30 16 25 15 20 14 15 24 | 4 14 5 9 25 3 11 5 9 17 3 | 26 29 31 31 30 27 27 28 31 27 28 X25 | 12 23 10 17 --- 5 --- 11 26 --- 7 | 18 30 26 41 --- 21 --- 23 35 --- 23 26E | 9 22 10 10 47 3 14 9 21 22 5 | 8 23 15 13 15 11 14 16 25 16 12 27 | 7 15 4 7 42 3 11 8 5 12 3 | 23 28 26 25 34 24 26 27 31 28 25 28 | 7 17 7 9 35 5 22 11 11 22 4 | 14 25 15 12 37 14 28 11 14 16 11 29E | 6 17 9 12 54 5 25 9 8 14 4 | 43 47 48 45 42 44 46 41 42 43 43 30 | 4 14 5 7 22 2 11 6 8 12 3 | 14 24 19 16 25 15 23 15 18 15 15 31 | 7 22 11 11 31 5 18 7 14 18 4 | 16 31 21 20 36 16 29 16 21 16 17 32 | 7 13 11 9 29 4 18 7 11 16 4 | 13 21 23 16 21 16 22 17 18 13 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 8 10 41 6 19 9 11 20 |T 25 34 31 28 37 27 34 27 29 28 26 WRMS | 7 18 8 10 35 5 19 8 7 19 |NE 20 29 26 24 34 22 29 23 24 23 22 MEDI | 6 17 8 10 33 4 19 8 9 17 |MD 18 28 26 23 34 20 29 21 25 22 21 Table 3.1547.2 GPS week: 1547 Day: 2 MJD: 55075.000 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 | 19 --- --- 23 --- 35 --- 15 28 --- 12 | 13 --- --- 24 --- 35 --- 15 27 --- 15 2 | 7 20 8 10 50 4 24 10 10 27 5 | 13 25 19 18 43 13 28 16 17 22 14 3E | 15 22 12 14 71 8 22 18 20 64 8 | 84 97 91 85 103 89 100 93 89 94 88 4 | 5 14 5 11 30 4 11 7 8 22 3 | 29 27 32 34 22 29 25 33 31 31 29 5 | 13 24 8 14 49 10 26 13 11 30 6 | 95 84 88 94 71 87 70 92 91 97 91 6E | 11 16 16 11 86 7 19 18 14 39 6 | 62 58 58 59 48 55 53 55 60 63 57 7 | 7 20 13 12 27 4 19 5 11 15 4 | 14 26 28 22 36 17 29 16 12 15 17 8 | 5 12 7 5 25 3 10 5 6 8 2 | 10 21 18 13 21 11 18 12 10 10 12 9 | 6 18 6 7 33 4 12 7 6 12 3 | 15 22 17 17 31 14 20 18 16 18 15 10 | 5 15 5 12 21 5 12 10 11 15 3 | 20 24 23 29 18 21 19 25 24 22 22 11 | 6 13 5 8 48 4 16 8 9 13 3 | 22 32 29 21 47 23 34 22 22 20 23 12 | 9 23 10 15 34 4 23 7 9 23 5 | 18 32 19 22 38 18 33 20 20 19 17 13E | 7 21 9 9 25 5 19 8 7 11 4 | 13 28 22 16 35 19 27 15 13 19 16 14E | 6 15 10 9 26 4 19 9 6 10 3 | 19 27 29 23 33 19 27 25 23 23 23 15E | 7 25 9 13 37 6 25 8 9 9 4 | 17 30 25 27 32 20 25 22 22 19 20 16 | 5 21 7 17 26 5 24 6 11 28 5 | 14 30 22 12 33 15 31 15 20 22 17 17E | 9 14 7 8 19 5 24 10 9 7 4 | 47 50 49 46 46 48 50 46 48 47 46 18 | 7 21 9 13 39 5 22 13 9 23 5 | 16 30 26 26 34 17 31 20 18 14 18 19E | 7 21 11 9 20 5 22 10 6 16 4 | 20 33 37 29 33 26 31 22 22 25 25 20 | 6 16 9 14 38 5 19 6 12 25 4 | 20 28 24 25 30 24 28 21 24 20 20 21 | 7 22 9 12 35 4 27 9 10 17 5 | 25 40 29 26 48 25 41 23 22 26 25 22 | 7 17 7 7 52 5 22 6 7 17 4 | 18 27 27 26 35 20 30 22 23 16 21 23E | 6 25 8 11 24 5 20 9 11 14 4 | 14 29 20 17 28 16 24 17 15 16 14 24 | 5 15 10 11 29 4 12 6 10 17 3 | 26 29 38 34 27 26 29 29 29 29 29 X25 | 9 24 29 9 --- 10 --- 12 18 --- 8 | 11 26 29 21 --- 20 --- 19 21 --- 16 X26E | 9 20 10 9 --- 6 --- 9 19 23 5 | 9 20 12 15 --- 10 --- 18 25 15 12 27 | 7 23 6 6 44 5 12 7 9 9 3 | 16 28 19 19 33 14 19 19 17 19 16 28 | 7 20 8 13 27 5 21 8 11 20 4 | 12 28 19 13 35 13 28 11 15 15 11 29E | 8 20 11 16 35 6 29 12 10 13 5 | 42 44 45 46 54 44 43 44 42 43 42 30 | 5 16 8 8 22 4 9 6 9 13 3 | 15 22 22 17 25 16 22 16 18 14 16 31 | 6 24 10 14 34 6 23 10 14 17 5 | 16 31 22 21 40 16 29 18 13 18 16 32 | 6 12 6 10 23 4 17 6 12 14 3 | 12 18 18 14 21 13 19 15 16 12 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 9 11 39 5 20 9 10 22 |T 24 33 30 28 37 26 33 26 27 27 25 WRMS | 7 19 9 11 35 5 19 9 8 16 |NE 20 30 27 24 34 22 29 22 23 22 21 MEDI | 7 20 9 11 33 5 20 8 10 16 |MD 16 28 25 22 34 19 29 20 22 19 17 Table 3.1547.3 GPS week: 1547 Day: 3 MJD: 55076.000 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 --- --- 24 --- 26 --- 13 24 --- 10 | 16 --- --- 24 --- 28 --- 22 32 --- 17 2 | 8 18 11 9 46 5 24 8 6 24 4 | 16 29 23 20 42 20 29 21 21 25 19 3E | 13 17 14 12 74 8 19 14 20 40 7 | 97 112 108 97 110 100 109 106 98 102 102 4 | 7 12 7 13 45 5 13 8 8 23 4 | 48 47 45 52 37 47 45 48 47 49 46 5 | 15 21 10 19 45 13 26 11 10 29 6 | 79 76 73 75 60 78 56 82 79 81 77 6E | 11 16 13 13 106 7 17 16 19 33 6 | 58 54 55 63 57 56 53 55 61 61 57 7 | 8 20 12 13 29 5 18 6 8 15 4 | 17 31 29 24 39 21 31 19 16 17 20 8 | 7 12 8 9 18 5 11 6 5 10 3 | 16 25 23 17 21 20 25 18 19 14 18 9 | 6 14 4 7 30 3 9 10 7 11 3 | 19 25 20 24 21 21 26 24 23 21 21 10 | 5 12 9 8 27 4 10 9 9 14 3 | 23 29 29 31 18 25 25 30 31 28 26 11 | 7 12 10 11 48 4 17 5 8 11 3 | 24 34 30 28 50 25 36 26 23 25 26 12 | 7 22 13 12 27 5 22 13 10 23 5 | 22 34 22 23 37 22 33 23 21 21 20 13E | 10 21 9 15 28 11 20 28 17 20 6 | 13 28 20 17 39 17 28 32 21 30 16 14E | 7 16 10 12 24 4 22 8 8 11 4 | 11 23 20 18 34 15 26 17 14 14 14 15E | 8 30 9 11 34 3 22 11 8 12 5 | 25 34 23 26 36 24 31 25 25 27 24 16 | 6 21 11 17 26 5 24 10 21 26 6 | 16 31 17 14 34 16 35 19 20 23 17 17E | 8 15 10 13 25 6 24 8 12 18 4 | 83 85 83 78 86 85 88 81 87 80 83 18 | 7 20 10 11 38 4 22 7 10 24 4 | 19 31 28 26 35 22 33 21 23 17 21 19E | 6 18 10 8 25 5 26 10 9 19 4 | 26 38 34 28 39 28 36 28 27 31 29 20 | 6 17 13 16 45 4 22 9 9 25 5 | 22 29 29 32 33 25 30 24 27 23 23 21 | 7 23 7 13 30 4 26 11 13 20 5 | 26 42 34 28 49 29 42 30 29 28 29 22 | 9 18 8 10 45 7 22 9 8 19 4 | 22 30 30 30 33 25 31 26 26 20 24 23E | 7 23 8 15 29 5 20 11 13 13 5 | 12 29 20 16 31 16 27 15 18 18 15 24 | 8 17 7 11 26 4 11 7 11 16 4 | 32 33 39 36 36 35 34 34 36 34 33 X25 | 15 23 19 16 --- 10 --- 17 31 --- 9 | 20 36 34 26 --- 23 --- 21 35 --- 21 X26E | 4 --- --- --- --- 67 --- --- --- --- 0 | 42 --- --- --- --- 42 --- --- --- --- 49 27 | 7 16 5 6 41 3 10 9 8 8 3 | 22 30 22 27 27 25 30 27 28 24 24 28 | 8 19 11 16 24 8 20 8 6 21 4 | 15 29 22 18 34 18 29 14 14 18 15 29E | 13 21 11 15 28 7 29 11 8 14 5 | 53 54 56 63 63 56 62 59 54 60 55 30 | 5 18 7 10 16 4 11 8 8 14 3 | 17 26 23 20 25 18 28 21 21 17 19 31 | 6 23 10 16 33 8 21 9 16 15 5 | 16 29 22 23 37 16 28 17 16 16 16 32 | 4 12 9 11 25 4 16 9 9 13 3 | 15 21 18 18 21 17 20 18 14 17 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 13 40 6 20 11 11 20 |T 29 38 34 32 40 31 38 32 32 32 30 WRMS | 7 19 10 13 40 5 19 9 7 17 |NE 23 33 29 28 34 26 32 26 27 25 24 MEDI | 7 18 10 12 29 5 20 9 9 18 |MD 22 31 28 26 36 24 31 24 25 24 21 Table 3.1547.4 GPS week: 1547 Day: 4 MJD: 55077.000 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 | 18 --- --- 16 --- 21 --- 20 17 --- 10 | 17 --- --- 20 --- 19 --- 15 19 --- 14 2 | 6 22 13 9 40 4 23 7 7 25 5 | 12 28 19 13 37 13 27 14 13 23 12 3E | 11 15 15 16 56 6 19 16 16 32 6 | 85 98 94 85 101 90 100 95 86 93 90 4 | 6 13 9 9 28 6 11 11 7 20 4 | 38 36 41 40 36 35 34 42 35 40 38 5 | 14 34 11 12 37 8 23 9 11 30 6 | 85 85 79 83 64 79 67 81 86 87 82 6E | 10 15 13 16 112 6 21 16 17 29 6 | 61 57 58 62 51 57 55 54 61 58 57 7 | 6 21 11 13 24 5 18 6 10 13 4 | 16 28 23 23 39 20 29 15 18 14 16 8 | 6 14 6 9 17 4 9 7 9 9 3 | 14 23 20 17 25 17 21 15 19 13 15 9 | 7 13 9 13 30 4 10 12 7 11 3 | 18 23 20 14 29 16 24 22 22 18 17 10 | 4 10 8 8 22 5 11 9 8 17 3 | 19 24 27 23 19 22 26 26 22 23 21 11 | 6 14 6 11 51 4 16 7 9 12 3 | 24 34 28 25 55 25 38 23 23 22 24 12 | 8 20 14 15 22 6 22 11 11 22 5 | 14 30 22 18 35 14 30 16 15 14 14 13E | 6 22 10 10 33 5 17 14 9 14 4 | 13 27 16 13 42 15 25 23 13 22 14 14E | 8 14 12 9 35 5 22 10 9 11 4 | 13 24 20 13 39 14 24 16 15 14 13 15E | 8 24 9 12 28 6 25 12 9 10 5 | 23 31 20 21 27 19 31 24 23 22 21 16 | 5 24 10 12 30 7 24 10 20 26 6 | 15 31 17 15 33 13 29 16 15 20 15 17E | 7 17 11 13 23 5 24 8 11 15 4 | 62 66 63 66 71 63 65 63 64 70 64 18 | 6 19 9 14 27 6 20 8 10 23 4 | 18 31 23 22 34 19 31 17 17 14 17 19E | 6 19 13 8 33 3 24 10 11 9 4 | 24 31 31 24 33 26 29 26 24 27 25 20 | 7 17 12 10 58 6 15 7 11 25 4 | 24 28 29 29 37 23 28 25 22 23 23 21 | 7 20 11 11 34 6 23 8 14 18 5 | 19 37 28 18 50 24 37 23 20 24 22 22 | 6 18 9 11 31 7 19 13 11 19 4 | 18 28 20 24 31 20 27 27 19 20 19 23E | 5 24 9 11 29 5 17 11 13 13 4 | 12 26 17 12 31 12 24 12 12 15 12 24 | 8 17 9 11 28 5 11 5 10 14 3 | 23 28 30 29 31 28 27 23 27 27 25 X25 | 10 21 31 19 --- 21 --- 17 18 22 8 | 13 32 45 24 --- 22 --- 15 12 6 17 X26E | 27 21 22 18 --- 15 --- 13 22 24 9 | 27 20 21 18 --- 23 --- 21 34 16 28 27 | 7 12 10 16 36 2 11 11 8 8 4 | 18 22 19 13 32 14 24 21 21 18 17 28 | 6 21 9 11 27 7 19 7 8 21 4 | 12 27 19 13 35 14 29 12 16 19 12 29E | 5 21 10 11 28 6 27 6 7 9 4 | 69 70 72 69 65 66 69 67 66 67 68 30 | 5 14 7 6 18 3 10 8 7 14 3 | 17 23 20 18 28 17 23 19 21 14 17 31 | 5 23 10 14 27 5 18 9 15 16 4 | 16 30 18 21 33 14 26 14 14 14 14 32 | 6 13 8 10 37 5 13 7 9 12 3 | 15 19 20 17 28 14 20 15 14 15 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 19 10 12 39 5 19 10 11 18 |T 26 35 31 28 40 27 35 28 27 28 26 WRMS | 7 19 10 12 33 5 19 9 9 18 |NE 21 30 27 23 35 21 29 22 22 22 21 MEDI | 6 19 10 11 30 5 19 9 10 16 |MD 18 28 22 21 35 19 29 21 20 20 17 Table 3.1547.5 GPS week: 1547 Day: 5 MJD: 55078.000 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 | 18 --- --- 16 --- 37 --- 13 25 --- 10 | 19 --- --- 16 --- 34 --- 12 19 --- 12 2 | 7 17 11 11 44 5 20 7 12 25 4 | 10 22 18 15 37 11 21 11 13 24 12 3E | 9 17 11 15 66 6 16 18 18 18 5 | 104 113 112 107 122 108 117 114 103 106 108 4 | 6 12 8 10 35 5 11 9 12 19 4 | 34 37 37 37 38 37 37 36 36 43 35 X5 | 11 21 8 14 31 7 --- 10 10 31 5 | 67 59 58 62 49 61 --- 64 69 68 63 6E | 17 21 14 14 82 10 19 22 28 42 8 | 122 118 113 120 107 113 114 116 122 116 116 7 | 6 22 11 17 25 5 19 7 12 13 4 | 14 27 22 23 40 17 26 15 17 14 15 8 | 6 14 7 11 23 4 10 9 8 8 3 | 10 22 16 17 31 14 19 15 15 10 12 9 | 9 13 7 12 27 4 12 9 6 12 3 | 15 19 15 14 29 13 20 14 16 13 13 10 | 6 13 7 11 25 2 9 9 9 20 3 | 15 23 22 22 23 18 18 21 21 23 18 11 | 6 14 5 12 53 6 15 7 11 12 3 | 16 31 26 20 59 22 32 16 20 17 20 12 | 7 22 11 12 29 7 18 10 7 23 5 | 19 32 22 15 36 16 28 16 19 18 16 13E | 5 17 7 10 28 6 18 8 10 8 3 | 10 22 19 12 41 13 24 9 12 14 12 14E | 6 16 10 10 36 6 19 8 8 12 4 | 14 26 19 21 39 17 25 19 18 20 17 15E | 10 24 10 11 45 4 24 11 9 10 5 | 16 29 19 20 31 16 27 19 23 19 18 16 | 6 22 7 18 42 8 24 6 11 27 5 | 11 28 13 8 36 11 28 11 13 18 11 17E | 8 14 8 11 21 5 25 10 9 10 4 | 71 75 72 70 79 73 75 70 73 69 71 18 | 7 21 8 17 24 6 22 11 9 23 5 | 13 28 16 21 35 15 28 17 17 13 15 19E | 10 17 11 13 32 5 26 13 14 8 5 | 29 35 33 25 34 29 36 26 26 26 28 20 | 5 18 9 15 54 5 17 6 9 26 4 | 16 26 24 20 33 17 25 18 18 19 17 21 | 7 22 8 11 33 7 23 8 9 17 4 | 24 38 30 23 48 26 39 25 26 27 26 22 | 7 19 8 12 35 6 19 10 10 20 4 | 17 27 18 21 29 19 26 23 22 20 18 23E | 6 22 6 12 33 5 16 7 10 13 4 | 9 25 17 11 34 11 21 10 15 13 11 24 | 5 14 9 9 29 5 11 5 7 14 3 | 23 26 27 24 31 26 28 22 28 26 24 X25 | 11 26 20 22 --- 22 --- 21 21 --- 8 | 21 33 32 28 --- 19 --- 21 27 --- 20 26E | 14 22 10 9 68 9 15 10 25 20 6 | 23 27 20 18 22 20 15 22 30 26 24 27 | 8 17 10 13 26 4 11 10 7 9 4 | 20 27 23 18 32 18 22 19 22 18 19 28 | 9 17 7 15 27 4 20 7 9 24 4 | 9 25 16 17 34 13 26 12 14 18 11 29E | 7 19 10 12 27 7 24 7 9 12 4 | 38 38 38 40 46 36 37 38 33 36 35 30 | 5 14 8 7 19 4 9 7 6 14 3 | 11 18 18 15 30 12 19 15 16 11 13 31 | 5 23 8 12 33 7 20 9 10 15 4 | 14 29 17 17 33 13 26 18 17 12 14 X32 | 6 16 10 12 32 6 --- 7 10 16 4 | 14 19 17 18 25 14 --- 16 17 18 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 9 12 39 6 18 10 12 18 |T 26 35 30 28 42 27 34 27 29 29 26 WRMS | 7 18 8 12 36 5 18 8 9 16 |NE 18 28 23 21 35 20 26 19 21 21 19 MEDI | 7 17 8 12 32 6 18 9 10 15 |MD 16 27 22 20 34 17 26 18 19 19 17 Table 3.1547.6 GPS week: 1547 Day: 6 MJD: 55079.000 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 | 18 --- --- 29 --- 17 --- 16 13 --- 11 | 23 --- --- 26 --- 22 --- 20 18 --- 19 2 | 7 18 9 8 47 6 22 8 11 28 5 | 20 27 23 19 42 17 32 21 22 29 20 3E | 9 17 9 15 64 7 17 24 17 45 7 | 133 144 141 133 145 134 144 150 130 145 139 4 | 5 11 7 7 20 5 11 14 12 20 4 | 33 36 37 41 31 36 34 39 35 44 36 X5 | 11 20 5 11 39 6 --- 9 9 32 5 | 91 90 85 90 75 88 --- 88 90 96 88 6E | 13 18 10 16 32 6 18 17 25 31 6 | 58 54 56 60 47 57 51 46 60 52 53 7 | 8 23 8 12 33 5 20 11 8 13 4 | 18 31 25 24 39 21 28 22 19 19 21 8 | 6 16 7 12 17 5 9 9 9 10 3 | 16 27 23 22 25 17 22 21 17 17 18 9 | 10 15 8 7 37 6 13 10 12 12 4 | 23 27 29 29 26 22 27 33 31 30 27 10 | 7 12 5 10 22 4 9 9 9 28 4 | 28 32 34 32 19 27 28 37 30 41 31 11 | 5 16 5 10 48 4 17 6 11 15 3 | 26 33 31 25 53 27 35 25 31 28 28 12 | 10 20 8 10 33 6 22 9 9 25 5 | 22 33 26 24 36 21 35 26 23 27 23 13E | 7 24 7 8 24 7 18 12 13 9 4 | 13 34 21 15 35 16 27 16 15 19 16 14E | 8 18 5 10 26 6 20 9 8 11 4 | 16 27 19 18 33 16 25 17 19 17 16 15E | 10 20 7 10 31 7 24 12 9 11 4 | 18 31 23 24 29 16 30 22 22 23 21 16 | 8 25 8 19 22 5 27 10 13 29 6 | 20 35 22 17 42 17 36 21 22 30 21 17E | 8 17 8 13 27 7 24 11 10 12 4 | 72 74 71 68 81 73 76 73 74 76 72 18 | 7 20 8 13 40 6 22 11 9 25 5 | 21 31 29 30 37 22 33 27 25 20 24 19E | 10 19 13 9 46 5 30 17 12 13 5 | 41 41 49 46 45 41 41 46 45 44 43 20 | 7 19 8 11 54 8 17 7 10 28 4 | 27 30 32 31 39 28 30 27 26 30 27 21 | 9 25 6 10 37 7 25 8 10 17 5 | 25 37 30 25 51 23 39 25 25 26 26 22 | 8 17 6 11 43 6 20 11 12 23 4 | 23 30 27 33 35 26 29 28 31 23 25 23E | 7 22 8 10 32 7 22 12 15 14 5 | 15 30 21 15 30 16 29 16 21 20 17 24 | 7 17 5 9 35 5 13 5 9 13 3 | 29 32 34 35 31 30 31 31 33 32 31 X25 | 20 41 21 23 --- 19 --- 21 26 --- 10 | 22 47 44 38 --- 29 --- 24 37 --- 30 26E | 16 20 10 9 39 7 14 9 27 20 6 | 17 18 13 18 19 15 14 21 36 17 17 27 | 11 17 7 8 39 7 13 11 11 9 4 | 24 31 31 33 26 25 30 37 35 33 30 28 | 8 21 8 13 25 6 20 7 9 26 5 | 14 29 20 17 39 15 28 16 18 25 16 29E | 8 19 7 11 27 9 23 9 13 10 4 | 66 68 66 70 71 68 67 66 65 66 66 30 | 7 13 5 8 17 8 10 8 8 13 3 | 20 21 22 22 30 17 23 24 24 18 21 31 | 5 23 7 10 46 6 24 8 12 15 4 | 21 27 21 23 47 15 27 21 18 17 19 X32 | 5 18 6 9 36 4 --- 8 13 15 4 | 19 24 24 22 29 18 --- 20 21 23 21 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 8 11 36 6 20 11 13 21 |T 31 39 36 35 42 31 37 34 34 36 33 WRMS | 8 19 7 11 29 6 18 9 10 16 |NE 25 33 30 29 37 25 30 28 28 30 27 MEDI | 8 19 7 10 33 6 20 9 11 15 |MD 22 31 29 25 36 22 30 25 25 27 24 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 4.1547 GPS week: 1547 MJD: 55073.0-55079.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3039 |U 8 10 25 |U 6 8 24 |U 10 9 21 | emr | emr 2948 | 12 13 33 |U 8 9 30 | 10 9 25 | esa | esa 2962 | 9 11 27 |U 7 7 24 | 10 8 21 | gfz | gfz 3015 |U 9 12 27 |U 23 26 56 | 12 11 40 | grg | grg 2838 | 9 11 28 |U 8 13 34 | 10 9 21 | igr | igr 2904 | 9 12 28 | 7 9 28 | 10 8 20 | igs | igs 2931 | 9 12 30 | 7 9 28 | 10 8 21 | jpl | jpl 2771 |U 10 14 30 |U 8 8 32 |U 10 8 22 | mit | mit 3058 |U 10 14 29 |U 9 10 30 |U 13 10 24 | 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 5.1547.0 GPS week: 1547 Day: 0 MJD: 55073.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3066 | 6 6 19 | 8 11 40 | 7 8 16 | emr | emr 2957 | 10 13 27 | 11 14 43 | 9 7 24 | esa | esa 2976 | 6 7 20 | 8 8 35 | 8 7 19 | gfz | gfz 3031 | 8 9 25 | 18 18 92 | 8 6 19 | grg | grg 2880 | 7 6 19 | 11 31 65 | 7 5 19 | igr | igr 2849 | 7 9 27 | 13 14 50 | 8 7 17 | igs | igs 2957 | 7 11 23 | 11 15 43 | 7 5 18 | jpl | jpl 2866 | 8 12 24 | 10 12 40 | 7 5 18 | mit | mit 3072 | 7 12 25 | 10 12 34 | 9 17 19 | Table 5.1547.1 GPS week: 1547 Day: 1 MJD: 55074.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3061 | 7 8 27 | 5 5 24 | 9 9 21 | emr | emr 2959 | 9 11 34 | 8 8 29 | 10 11 27 | esa | esa 2976 | 8 9 31 | 6 6 23 | 8 9 22 | gfz | gfz 3033 | 8 9 30 | 12 16 51 | 9 9 21 | grg | grg 2880 | 8 6 30 | 7 8 29 | 9 8 24 | igr | igr 2868 | 8 10 27 | 5 8 26 | 9 10 22 | igs | igs 3025 | 8 11 41 | 6 8 28 | 9 9 22 | jpl | jpl 2865 | 8 12 30 | 7 7 25 | 10 10 28 | mit | mit 3072 | 8 12 32 | 6 8 27 | 10 9 26 | Table 5.1547.2 GPS week: 1547 Day: 2 MJD: 55075.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3049 | 12 19 37 | 6 8 20 | 11 7 24 | emr | emr 2963 | 14 19 53 | 7 10 26 | 11 9 20 | esa | esa 2976 | 11 15 39 | 6 8 22 | 9 6 15 | gfz | gfz 3032 | 12 18 37 | 13 17 51 | 10 7 14 | grg | grg 2784 | 13 20 44 | 7 9 29 | 9 10 17 | igr | igr 2861 | 11 20 52 | 5 9 24 | 10 7 15 | igs | igs 2870 | 12 18 50 | 5 9 23 | 10 8 16 | jpl | jpl 2771 | 14 21 46 | 6 6 25 | 9 6 16 | mit | mit 3072 | 12 20 39 | 7 10 33 | 11 7 17 | Table 5.1547.3 GPS week: 1547 Day: 3 MJD: 55076.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3068 | 7 11 23 | 6 8 26 | 15 10 18 | emr | emr 2872 | 9 12 22 | 8 9 33 | 14 7 22 | esa | esa 2880 | 8 14 27 | 7 9 28 | 13 8 22 | gfz | gfz 2932 | 8 13 24 | 13 13 47 | 16 12 26 | grg | grg 2784 | 8 11 22 | 8 8 31 | 13 10 23 | igr | igr 2859 | 7 13 22 | 7 11 29 | 14 9 21 | igs | igs 2868 | 8 14 23 | 7 10 30 | 15 9 21 | jpl | jpl 2775 | 9 14 24 | 8 9 32 | 13 7 22 | mit | mit 2976 | 8 15 23 | 10 11 33 | 16 10 21 | Table 5.1547.4 GPS week: 1547 Day: 4 MJD: 55077.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3033 | 11 15 27 | 5 6 21 | 11 13 31 | emr | emr 2964 | 23 20 38 | 8 8 26 | 12 13 36 | esa | esa 2976 | 12 16 29 | 6 8 23 | 11 10 30 | gfz | gfz 3035 | 11 17 30 | 82 97 64 | 26 23 167 | grg | grg 2784 | 13 14 31 | 7 8 27 | 12 13 30 | igr | igr 2949 | 12 16 29 | 5 7 21 | 11 11 31 | igs | igs 2978 | 12 15 29 | 6 6 23 | 11 12 34 | jpl | jpl 2776 | 14 18 30 | 8 7 34 | 12 11 27 | mit | mit 3072 | 11 14 31 | 7 9 29 | 23 13 41 | Table 5.1547.5 GPS week: 1547 Day: 5 MJD: 55078.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2975 | 7 7 24 | 5 9 14 | 8 7 20 | emr | emr 2964 | 10 10 30 | 7 7 20 | 9 8 25 | esa | esa 2976 | 8 9 26 | 5 6 16 | 9 6 19 | gfz | gfz 3031 | 8 7 23 | 11 12 43 | 8 5 17 | grg | grg 2880 | 7 8 31 | 9 12 28 | 8 7 20 | igr | igr 2975 | 8 8 26 | 6 6 18 | 8 6 17 | igs | igs 2870 | 7 8 25 | 6 6 19 | 8 7 19 | jpl | jpl 2672 | 10 11 29 | 10 7 37 | 10 9 24 | mit | mit 3072 | 13 12 34 | 7 6 21 | 11 6 21 | Table 5.1547.6 GPS week: 1547 Day: 6 MJD: 55079.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3021 | 7 8 17 | 6 8 22 | 9 10 20 | emr | emr 2957 | 9 8 29 | 7 7 34 | 8 5 21 | esa | esa 2976 | 8 9 19 | 9 6 25 | 9 8 19 | gfz | gfz 3011 | 8 9 21 | 13 12 47 | 9 13 16 | grg | grg 2880 | 9 9 23 | 10 14 31 | 10 8 18 | igr | igr 2970 | 8 9 17 | 9 8 30 | 8 9 20 | igs | igs 2954 | 8 8 21 | 8 7 28 | 9 9 18 | jpl | jpl 2672 | 9 11 26 | 10 10 31 | 9 7 19 | mit | mit 3072 | 8 10 20 | 12 10 32 | 11 11 23 | 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 6.1547 GPS week: 1547 MJD: 55073.500-55079.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 27 -18 -47 -44 0 | 2 19 | 25 14 71 41 9 | 3 emr uuuuu | 14 -47 254 155 17 | 44 49 | 30 22 57 117 19 | 9 esa uuuuu | 25 -29 -61 78 -1 | 31 38 | 25 27 86 139 9 | 4 gfz uuuuu | 12 36 -46 -53 -14 | 12 24 | 28 21 37 116 2 | 7 grg xxxxx | 12 -53 -30 0 9 | -4 17 | 41 29 81 95 19 | 4 igr xxxxx | 17 -6 -26 31 -12 | 9 22 | 21 28 52 54 8 | 4 irf xxxxx | -5 -12 -57 -15 0 | 4 17 | 7 6 17 18 8 | 2 jpl uuuux | 13 -21 3 -30 -9 | 48 52 | 38 36 31 180 28 | 4 mit uuuuu | -37 -3 -117 -56 7 | 19 26 | 14 8 65 60 11 | 3 ngs uuuuu | -12 20 52 -91 -6 | 10 20 | 36 29 102 105 11 | 7 sio uuuuu | 6 64 158 106 5 | 46 49 | 11 16 115 75 13 | 4 Table 7.1547.0 GPS week: 1547 Day: 0 MJD: 55073.500 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 | 61 4 13 -54 6 | 2 22 emr uuuuu | 38 -27 218 210 28 | 36 43 esa uuuuu | 2 -47 -164 -15 -19 | 38 44 gfz uuuuu | 54 30 -21 99 -14 | 21 31 grg xxxxx | 35 -71 136 186 -2 | 3 20 igr xxxxx | 16 -21 -14 124 -3 | 15 27 irf xxxxx | -17 -8 -62 -25 3 | 7 21 jpl uuuux | 77 -23 52 -61 14 | 46 51 mit uuuuu | -56 10 -63 -109 11 | 18 27 ngs uuuuu | -40 13 25 -71 -8 | 20 27 sio uuuuu | -7 82 266 115 15 | 44 49 Table 7.1547.1 GPS week: 1547 Day: 1 MJD: 55074.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 4 -12 -92 -46 7 | -1 23 emr uuuuu | 11 -40 335 139 30 | 33 40 esa uuuuu | 14 -39 -112 -17 -4 | 31 40 gfz uuuuu | 21 26 -27 32 -12 | 15 28 grg xxxxx | 17 -12 -51 -81 -16 | -2 21 igr xxxxx | 26 19 -74 28 -11 | 10 25 irf xxxxx | -4 -7 -41 11 5 | 2 19 jpl uuuux | -44 -35 -9 -75 9 | 44 49 mit uuuuu | -35 1 -85 1 12 | 14 24 ngs uuuuu | 23 37 -34 -144 -19 | 16 26 sio uuuuu | 0 73 316 236 14 | 40 45 Table 7.1547.2 GPS week: 1547 Day: 2 MJD: 55075.500 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 | 36 -13 -15 -1 7 | 0 23 emr uuuuu | -17 -73 316 54 34 | 36 43 esa uuuuu | 41 -43 -29 120 2 | 30 39 gfz uuuuu | 22 60 -103 38 -13 | 13 27 grg xxxxx | 13 -48 -110 1 -11 | -6 20 igr xxxxx | 14 -36 -73 6 -7 | 8 25 irf xxxxx | -1 -8 -48 -18 6 | 1 18 jpl uuuux | 10 -79 -31 -90 24 | 46 51 mit uuuuu | -43 -1 -26 -93 14 | 15 24 ngs uuuuu | -10 39 -96 -74 -18 | 12 24 sio uuuuu | 3 78 249 69 16 | 41 46 Table 7.1547.3 GPS week: 1547 Day: 3 MJD: 55076.500 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 -39 -76 -21 -5 | 6 18 emr uuuuu | -15 -67 243 -2 23 | 45 50 esa uuuuu | 54 -14 93 259 -1 | 34 41 gfz uuuuu | 23 28 -95 -47 -11 | 15 26 grg xxxxx | -51 -97 -30 -113 12 | -4 19 igr xxxxx | -3 -31 34 -30 -5 | 13 21 irf xxxxx | 6 -7 -84 -7 4 | 6 17 jpl uuuux | -18 4 -3 -304 2 | 53 56 mit uuuuu | -9 -3 -206 31 15 | 20 26 ngs uuuuu | -63 0 28 -211 -10 | 12 24 sio uuuuu | 28 74 116 139 8 | 48 50 Table 7.1547.4 GPS week: 1547 Day: 4 MJD: 55077.500 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 -27 -98 -79 3 | 5 18 emr uuuuu | -3 -59 269 91 23 | 50 55 esa uuuuu | 58 23 -11 265 7 | 31 38 gfz uuuuu | 3 4 -36 -111 -14 | 11 23 grg xxxxx | -34 -66 -58 2 31 | -8 12 igr xxxxx | -15 17 51 6 -12 | 11 20 irf xxxxx | -6 -14 -70 -23 5 | 6 17 jpl uuuux | 30 34 -17 -85 -21 | 53 56 mit uuuuu | -40 -6 -181 -29 14 | 21 28 ngs uuuuu | -40 -32 89 -213 -3 | 8 19 sio uuuuu | 12 53 49 114 9 | 49 52 Table 7.1547.5 GPS week: 1547 Day: 5 MJD: 55078.500 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 -29 -129 1 -4 | 1 14 emr uuuuu | 21 -52 225 281 1 | 52 56 esa uuuuu | 10 -24 -122 15 7 | 27 33 gfz uuuuu | -4 45 -33 -211 -16 | 5 17 grg xxxxx | 54 -55 -6 -5 24 | -7 13 igr xxxxx | 42 33 -36 84 -23 | 6 16 irf xxxxx | -6 -20 -57 -42 -4 | 3 15 jpl uuuux | 22 -10 41 218 -42 | 48 52 mit uuuuu | -41 -18 -146 -132 0 | 20 26 ngs uuuuu | 14 26 191 35 6 | 2 11 sio uuuuu | 8 46 50 -9 -4 | 48 51 Table 7.1547.6 GPS week: 1547 Day: 6 MJD: 55079.500 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 | 31 -12 68 -110 -16 | 1 15 emr uuuuu | 64 -13 173 309 -18 | 54 57 esa uuuuu | -2 -59 -84 -78 1 | 26 31 gfz uuuuu | -36 61 -9 -173 -19 | 1 18 grg xxxxx | 51 -21 -92 9 28 | -5 12 igr xxxxx | 41 -27 -68 -2 -21 | 2 18 irf xxxxx | -6 -22 -34 2 -16 | 3 15 jpl uuuux | 13 -42 -11 189 -48 | 44 51 mit uuuuu | -34 -7 -114 -64 -13 | 21 26 ngs uuuuu | 30 55 160 40 9 | 1 10 sio uuuuu | 0 44 64 76 -20 | 49 51