Date: Thu, 24 Sep 2009 11:31:32 +0000 From: Jim Ray Subject: [IGSREPORT-17827] Wk 1548 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4abb5894.Pv9HwCb1JJz2Hgid%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 24 Sep 04:32:05 PDT 2009 Message Number 17827 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1548 (Sep 06, 2009 - Sep 12, 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: igs1548[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1548[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1548[0-6].cls IGS GPS clock combination summary report. igs15487.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15487.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 3 6 0 | EMR | WTZR 0 | ESA | 3 6 32 NLIB RABT UNSA ZWE2 0 | GFZ | 3 14 17 29 BOR1 FAA1 0 | GRG | ONSA TWTF 0 | JPL | 32 0 | MIT | 4 24 26 4 24 26 1 | ALL | 1 1 27 1 | COD | 3 6 3 6 STR2 UNBJ 1 | EMR | WTZR WTZR 1 | ESA | 3 6 KOKB UNSA 1 | GFZ | 3 5 14 17 19 29 CAS1 FAA1 GUAT MIZU SCH2 1 | GRG | ONSA WROC 1 | JPL | 32 MDVJ 1 | MIT | 25 26 30 26 30 WROC IRKJ IRKT OUS2 WROC 2 | COD | 3 6 3 6 2 | EMR | 25 25 WTZR WTZR 2 | ESA | 3 6 UNSA 2 | GFZ | 14 17 19 29 FAA1 FLIN GLSV NYA1 REUN TLSE 2 | GRG | ONSA 2 | JPL | 5 32 2 | MIT | MIZU 2 | NGS | 1 3 | COD | 3 6 3 6 WROC 3 | EMR | WTZR 3 | ESA | 3 6 CHUR UNSA 3 | GFZ | 6 19 29 FAA1 SFER TOW2 3 | GRG | ONSA 3 | JPL | 5 32 3 | MIT | BAKO BRAZ DARW HARB MAW1 3 | NGS | 1 4 | ALL | 1 1 4 | COD | 6 6 DARW MIZU DARW STR2 4 | EMR | WTZR 4 | ESA | 4 6 KERG UNSA 4 | GFZ | 6 14 17 19 25 29 EIL1 FAA1 HARB KOUC NYA1 SUTH TOW2 4 | GFZ | WHIT 4 | GRG | PIE1 4 | JPL | 5 32 4 | MIT | 25 4 25 MIZU 5 | ALL | 1 31 5 | COD | 6 6 DAV1 5 | EMR | TWTF TWTF WTZR 5 | ESA | UNSA 5 | GFZ | 14 17 25 EIL1 FAA1 KOUC MAC1 MIZU TLSE YELL 5 | GRG | NLIB 5 | JPL | 5 32 TWTF 5 | MIT | 21 21 BAKO IRKJ TWTF 6 | ALL | 1 6 | COD | 6 6 DRAO SCH2 6 | EMR | WTZR 6 | ESA | 4 25 SCH2 6 | GFZ | 10 17 19 25 FAA1 HOFN HOLM JPLM MAS1 PRDS SHAO TWTF 6 | GFZ | UNSA 6 | GRG | ONSA TWTF 6 | JPL | 5 6 32 MCM4 6 | MIT | 4 4 IRKT 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 | MIT | ~00:00 | ~ -0.60 ns 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 G06 | 4 | | | | | | | 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 .4 1.5 -11 5 -16 -.38 EMR | 1.6 2.1 -9.1 89 -8 70 .12 ESA | .0 .1 3.8 50 -21 44 -.05 GFZ | .0 .6 1.3 19 -6 2 -.27 GRG | 3.9 1.7 1.0 -1 -4 19 -.03 JPL | -3.5 3.9 -4.6 12 -19 -53 .01 MIT | 1.1 -4.7 3.1 10 4 -19 -.31 NGS | 3.0 -1.8 3.9 -19 -13 -8 -.32 SIO | -.1 -2.4 -17.8 -40 -71 56 .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 1.1548.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1548.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 2.1548.[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 3.1548.[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 5.1548.0-6). 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 1548 summary. (Sep 06, 2009 - Sep 12, 2009) Table 1.1548.a GPS week: 1548 MJD: 55080.000-55086.000 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 230| 1 0 0 46 -48 2 -.15 8 7 | -426 -32 15 63 | 0 0 0 13 14 15 .02 | 182 223 emr 79| -1 1 -4 -177 -10 -9 .49 18 18 | 1359 -444 16 73 | 1 0 2 23 15 6 .05 | 1605 933 esa 137| 0 -1 2 -83 54 -14 .32 9 9 | -1307 1172 18 114 | 0 1 1 21 14 18 .02 | 880 1970 gfz 187| 0 0 2 0 -12 -31 -.15 11 11 | 0 386 24 102 | 0 0 1 39 50 13 .03 | 385 712 grg 113| 1 -1 -1 41 -25 9 1.04 47 36 | 120339 -126787 81 233 | 2 2 1 35 23 52 .07 | 304581 297621 igr n/a| 0 0 1 27 -29 -41 .06 5 5 | -9237 -650 20 72 | 0 0 0 20 11 43 .04 | 2081 1044 jpl 121| 2 0 -5 6 27 0 .55 18 17 | 1247 -383 17 84 | 1 0 0 16 15 26 .05 | 1464 1005 mit 259| 0 0 -1 12 -55 1 -.27 11 10 | -15186 -630 19 119 | 0 1 0 23 26 8 .02 | 825 775 ngs 219| 0 1 0 67 -10 10 -.28 10 8 | -806223 2867976 2162 3761 | 0 0 1 28 34 23 .03 | 382792 3405281 sio 256| -2 1 0 86 124 60 -.06 19 18 | --- --- --- --- | 1 0 1 34 22 16 .02 | --- --- Table 1.1548.b GPS week : 1548 MJD: 55080.000-55086.000 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 | 11 13 11 11 10 12 10 | 2 | 5 5 5 5 5 5 5 | 3 | 5 5 5 5 6 5 5 | 4 | 3 3 3 4 4 4 3 | 5 | 0 7 6 6 6 5 5 | 6 | 7 6 5 5 5 5 5 | 7 | 5 5 5 5 5 5 5 | 8 | 4 3 3 4 3 4 4 | 9 | 4 4 4 4 4 4 4 | 10 | 4 4 4 4 4 4 4 | 11 | 4 4 4 4 4 4 4 | 12 | 5 5 5 5 5 5 5 | 13 | 5 4 4 5 5 4 4 | 14 | 4 4 4 4 4 4 6 | 15 | 5 6 5 6 5 5 5 | 16 | 6 6 5 5 5 6 6 | 17 | 5 5 4 5 4 5 5 | 18 | 5 5 5 5 5 5 5 | 19 | 5 5 5 5 5 6 6 | 20 | 4 4 4 5 5 5 5 | 21 | 5 5 4 5 5 5 5 | 22 | 5 5 4 4 5 5 5 | 23 | 5 4 4 5 5 5 5 | 24 | 4 4 4 3 4 5 5 | 25 | 7 6 5 7 9 7 7 | 26 | 6 6 6 6 5 6 6 | 27 | 4 4 4 4 4 4 4 | 28 | 6 5 4 5 5 5 5 | 29 | 4 5 4 5 5 5 5 | 30 | 3 3 3 3 4 4 4 | 31 | 4 5 5 5 5 5 5 | 32 | 4 4 4 4 4 4 5 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1548.0 GPS week: 1548 Day: 0 MJD: 55080.000 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 230| 1 0 0 49 -32 11 -.17 8 8 | -329 -100 14 65 | 3 -13 | emr 79| -2 0 -2 -134 15 -1 .45 17 17 | 3312 -608 16 72 | -38 -44 | esa 137| 0 0 0 -89 58 -51 .29 9 9 | -1937 2331 19 126 | 38 -11 | gfz 187| 0 0 1 -41 -68 -27 -.18 12 12 | -210 1192 23 100 | -65 22 | grg 113| 5 0 -1 56 -6 -11 1.11 107 38 | 31904 -90014 86 257 | 9 13 | igr n/a| 0 0 2 44 -25 -139 .05 5 5 | -6268 -1189 19 85 | -50 -22 | jpl 121| 0 0 -4 5 33 -28 .48 17 16 | 3248 -1016 20 96 | -23 -66 | mit 259| 0 -2 0 -4 -75 13 -.24 11 10 | -15231 -964 21 134 | 5 31 | ngs 219| 0 1 0 104 22 24 -.23 10 9 | -999999 1863956 2138 3653 | -55 -37 | sio 256| -3 0 1 91 112 77 -.06 20 18 | --- --- --- --- | -72 -73 | Table 2.1548.1 GPS week: 1548 Day: 1 MJD: 55081.000 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 230| 1 0 0 53 -44 -20 -.17 7 7 | -744 80 17 67 | -5 -12 | emr 79| -1 0 -5 -167 0 -13 .46 18 18 | 3849 -2154 17 68 | -4 -41 | esa 137| 0 -1 1 -77 73 -4 .35 8 8 | 140 -1723 15 111 | 20 -38 | gfz 187| 0 0 1 14 -23 -10 -.19 11 11 | -165 834 25 114 | -58 35 | grg 113| 2 -2 -1 59 -13 -56 1.05 38 37 | -271 686 74 253 | -6 41 | igr n/a| 0 0 2 31 -37 -16 -.02 5 5 | -6394 -2415 26 78 | -33 -4 | jpl 121| 3 0 -5 6 27 -8 .49 17 17 | 3376 -2168 17 92 | -8 -48 | mit 259| 0 0 -2 5 -48 1 -.27 11 10 | -13674 -1563 15 92 | -11 11 | ngs 219| 1 2 2 70 -52 16 -.27 12 9 | 11439 1304 2367 3703 | 63 13 | sio 256| -3 1 1 80 139 64 -.08 18 15 | --- --- --- --- | -70 -71 | Table 2.1548.2 GPS week: 1548 Day: 2 MJD: 55082.000 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 230| 1 0 -1 27 -34 18 -.13 8 7 | -582 235 13 61 | 25 -8 | emr 79| -3 2 -2 -205 -13 -7 .53 17 17 | 1160 -460 15 71 | 12 -38 | esa 137| 0 0 3 -88 56 -19 .32 8 8 | -1250 -118 18 114 | 39 -34 | gfz 187| 0 0 3 47 -19 -30 -.18 9 9 | -443 134 21 93 | -40 -2 | grg 113| 0 -1 0 3 -54 100 .99 39 36 | -526 355 87 219 | 80 7 | igr n/a| 0 0 1 -1 -27 -33 .11 5 5 | -9338 -542 24 67 | -4 -11 | jpl 121| 2 0 -7 -1 43 53 .60 19 18 | 689 -30 15 77 | 18 -19 | mit 259| 0 0 -1 28 -61 3 -.22 10 9 | -14768 -1292 20 128 | -20 12 | ngs 219| -1 0 0 46 10 -27 -.27 9 6 | -999999 2039880 2445 4002 | 15 5 | sio 256| -2 1 0 110 100 52 -.08 19 17 | --- --- --- --- | -81 -49 | Table 2.1548.3 GPS week: 1548 Day: 3 MJD: 55083.000 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 230| 1 -1 0 54 -43 -7 -.15 9 9 | -207 -454 15 56 | -25 4 | emr 79| -1 2 -3 -180 -35 -6 .43 19 19 | 454 -340 17 81 | 12 12 | esa 137| -1 -1 2 -63 43 2 .30 8 8 | -2734 4243 18 117 | 24 7 | gfz 187| 2 1 0 13 -72 -20 -.15 11 11 | -241 423 24 97 | -52 45 | grg 113| 2 -2 0 79 -33 11 .93 36 34 | -126 173 82 211 | 10 28 | igr n/a| 0 0 0 35 -14 -22 .04 5 5 | -10206 -557 18 65 | -50 -16 | jpl 121| 1 0 -5 26 28 4 .54 18 17 | 306 -11 16 74 | -32 23 | mit 259| 0 -1 0 -11 -40 9 -.28 11 11 | -15413 272 23 137 | -19 -5 | ngs 219| 0 1 0 62 28 -7 -.31 10 8 | -999999 2051425 1835 3768 | -3 -7 | sio 256| -1 1 2 54 135 68 -.04 19 18 | --- --- --- --- | -55 -74 | Table 2.1548.4 GPS week: 1548 Day: 4 MJD: 55084.000 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 230| 1 0 0 41 -57 16 -.13 8 7 | -391 -25 16 69 | 34 10 | emr 79| -2 2 -2 -202 -10 -8 .50 19 19 | -192 -429 15 81 | 44 -26 | esa 137| -1 -2 3 -105 55 -21 .33 10 10 | -1020 -115 19 116 | 45 -4 | gfz 187| 0 1 2 -44 2 -40 -.12 11 11 | 49 -218 24 96 | -30 37 | grg 113| 3 -3 -2 18 -33 21 1.01 38 36 | 146 -124 82 236 | 24 61 | igr n/a| 0 -1 0 30 -48 -36 .04 5 5 | -10942 -803 19 71 | -24 47 | jpl 121| 3 0 -5 15 13 -9 .57 19 18 | -8 -498 19 86 | 16 -1 | mit 259| 0 0 -2 31 -47 0 -.27 11 11 | -15914 -16 16 109 | -34 -11 | ngs 219| 0 1 0 85 -9 2 -.26 9 7 | -655011 -999999 2167 3804 | -26 -1 | sio 256| -1 1 -1 91 123 61 -.04 19 18 | --- --- --- --- | -70 -62 | Table 2.1548.5 GPS week: 1548 Day: 5 MJD: 55085.000 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 230| 1 0 1 67 -75 -11 -.17 8 7 | -432 136 15 64 | -33 46 | emr 79| 0 2 -7 -174 -19 -6 .54 18 18 | -76 1034 15 66 | 6 -28 | esa 137| 0 -2 1 -49 27 -9 .35 9 9 | -1161 1952 18 108 | 40 -23 | gfz 187| 0 1 3 -34 69 -38 -.14 10 10 | 673 1087 28 108 | -36 46 | grg 113| 1 0 -3 78 -48 -41 1.06 37 38 | 810539 -797428 82 237 | -26 110 | igr n/a| 0 0 2 52 -30 -22 .05 4 4 | -11314 1004 18 64 | -49 8 | jpl 121| 3 0 -4 18 3 -21 .55 18 18 | 7 1056 19 85 | 11 -12 | mit 259| 1 0 -1 -12 -15 0 -.29 10 10 | -16204 252 21 122 | -16 -10 | ngs 219| -1 1 0 85 -60 45 -.33 10 8 | -999999 7639373 2013 3852 | -56 62 | sio 256| 0 1 -1 36 159 72 -.09 20 17 | --- --- --- --- | -53 -63 | Table 2.1548.6 GPS week: 1548 Day: 6 MJD: 55086.000 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 230| 1 0 1 32 -51 13 -.13 8 7 | -299 -102 16 62 | 29 -19 | emr 79| 0 1 -6 -179 -7 -20 .53 20 20 | 1012 -154 17 72 | -2 -43 | esa 137| 0 -2 2 -107 65 2 .32 10 10 | -1192 1638 19 110 | 27 -26 | gfz 187| 0 0 3 45 27 -49 -.11 11 11 | 333 -744 29 110 | -53 18 | grg 113| -1 2 -1 -4 9 38 1.14 34 33 | 712 -1157 76 221 | 90 -2 | igr n/a| 0 0 1 2 -20 -23 .11 5 5 | -10201 -50 18 76 | -67 -18 | jpl 121| 4 0 -6 -24 45 6 .60 18 18 | 1112 -19 18 82 | 28 -11 | mit 259| 0 1 -1 47 -97 -12 -.29 11 11 | -15104 -1101 17 117 | -31 3 | ngs 219| 0 0 2 19 -8 19 -.30 9 7 | -999999 7479897 2170 3549 | 35 45 | sio 256| -1 3 -2 141 98 28 -.05 20 20 | --- --- --- --- | -83 -72 | 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 3.1548.0 GPS week: 1548 Day: 0 MJD: 55080.000 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 | 17 --- --- 29 --- 17 --- 17 12 --- 10 | 12 --- --- 33 --- 20 --- 22 22 --- 16 2 | 7 16 9 6 65 6 18 9 9 25 4 | 24 36 26 23 68 25 36 23 23 23 24 3E | 9 15 8 12 60 6 16 9 8 30 4 | 48 50 50 48 56 48 48 50 49 60 48 4 | 8 10 7 9 538 7 10 7 9 15 3 | 29 34 30 32 166 30 35 27 29 28 29 X5 | 4 --- --- --- 81 167 --- --- --- --- 0 | 90 --- --- --- 74 93 --- --- --- --- 88 6E | 14 16 11 17 52 7 19 25 16 32 7 | 113 121 119 112 124 115 127 111 112 128 115 7 | 7 18 11 13 39 4 18 9 10 17 4 | 22 30 27 27 43 20 30 18 22 23 22 8 | 7 11 8 9 31 5 8 12 10 12 3 | 13 21 16 20 23 12 18 14 18 12 13 9 | 8 15 9 13 40 4 10 15 8 12 4 | 15 23 17 21 28 14 20 15 16 19 14 10 | 6 12 7 7 28 6 8 12 10 19 3 | 20 25 28 28 28 25 23 24 23 21 23 11 | 7 14 6 15 43 4 17 11 8 13 4 | 13 21 13 16 46 10 20 15 14 12 12 12 | 10 18 10 11 32 6 19 14 8 26 5 | 13 27 15 15 32 11 26 18 14 17 12 13E | 9 20 9 8 31 7 19 10 12 14 4 | 38 44 35 33 54 36 41 37 38 39 36 14E | 7 17 9 9 27 4 20 8 8 10 4 | 17 24 20 20 35 17 26 15 17 17 16 15E | 9 20 7 11 42 4 23 15 12 11 5 | 44 46 48 48 60 44 45 50 43 45 45 16 | 7 21 11 15 27 3 25 7 10 28 5 | 18 32 19 14 43 16 34 15 20 19 17 17E | 7 19 9 12 37 4 22 9 10 23 5 | 29 38 30 34 38 27 35 28 28 23 28 18 | 8 20 8 16 34 4 20 12 7 23 5 | 19 30 20 30 32 19 28 23 22 21 19 19E | 7 23 8 13 21 5 26 11 9 12 5 | 18 26 21 21 30 15 24 18 17 16 16 20 | 6 15 8 9 57 5 15 7 10 23 4 | 23 27 26 26 36 23 22 24 25 19 23 21 | 9 21 9 17 33 5 22 5 7 18 5 | 23 36 21 20 44 19 37 21 20 20 21 22 | 11 18 6 16 39 6 20 10 7 22 5 | 22 33 26 35 35 26 32 27 27 24 24 23E | 7 20 10 9 28 5 17 9 10 18 4 | 38 44 37 34 39 36 42 38 37 40 36 24 | 6 12 7 11 48 3 9 12 8 20 3 | 16 21 19 23 24 16 15 16 20 20 16 X25 | 12 21 12 13 --- 12 --- 13 19 --- 6 | 14 28 17 23 --- 21 --- 19 30 --- 16 26E | 14 17 9 10 29 6 14 10 22 24 5 | 38 45 38 40 55 38 47 37 43 50 38 27 | 9 15 7 12 44 4 10 10 9 8 3 | 24 32 26 33 37 26 30 28 29 31 26 28 | 7 19 12 16 41 5 21 8 10 33 5 | 15 31 28 25 42 18 31 17 20 18 19 29E | 7 15 10 13 28 7 17 10 11 12 4 | 18 23 15 24 26 16 20 26 23 18 18 30 | 7 10 7 7 27 5 8 8 6 14 3 | 25 28 27 29 27 24 27 30 29 23 26 31 | 5 19 9 10 49 5 18 8 9 16 4 | 22 32 23 25 49 19 26 19 15 22 21 32 | 5 15 14 12 38 6 16 9 9 16 4 | 15 20 22 20 24 15 15 17 15 17 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 17 9 12 107 5 17 11 10 20 |T 27 34 28 30 47 27 33 27 27 28 27 WRMS | 8 17 9 12 38 5 16 10 9 18 |NE 22 28 22 24 45 22 26 20 21 20 22 MEDI | 7 17 9 12 38 5 18 10 9 18 |MD 22 30 26 26 38 20 30 23 23 21 21 Table 3.1548.1 GPS week: 1548 Day: 1 MJD: 55081.000 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 --- --- 28 --- 18 --- 21 24 --- 12 | 15 --- --- 33 --- 28 --- 22 36 --- 20 2 | 7 18 7 9 48 5 20 10 10 24 4 | 23 34 30 22 52 25 36 22 22 20 24 3E | 10 15 8 15 72 4 19 9 11 31 5 | 55 51 49 51 58 51 51 53 55 44 50 4 | 5 10 7 9 30 4 10 8 6 13 3 | 21 29 29 24 157 25 29 21 22 24 23 X5 | 12 18 7 26 43 11 --- 13 10 30 6 | 127 94 94 116 116 121 --- 94 98 91 125 6E | 11 14 10 12 51 5 16 21 14 24 5 | 143 152 150 147 158 146 153 139 143 154 146 7 | 8 21 11 12 32 5 18 10 12 15 4 | 17 31 25 24 34 20 28 17 19 21 18 8 | 6 13 6 8 26 5 10 9 11 9 3 | 16 22 18 18 22 16 19 17 18 15 15 9 | 5 15 8 11 48 5 10 12 13 14 4 | 13 25 20 18 29 17 20 19 16 21 16 10 | 6 9 6 8 43 6 10 12 11 16 3 | 16 22 18 19 24 21 18 19 23 17 17 11 | 6 15 8 14 39 5 14 10 8 13 4 | 11 24 15 15 41 12 22 12 13 14 11 12 | 9 18 7 12 40 5 18 13 11 24 4 | 13 28 19 16 39 15 27 18 20 16 14 13E | 8 15 7 8 31 6 18 9 8 18 4 | 42 48 48 45 47 47 49 43 45 46 44 14E | 6 19 9 10 35 4 18 9 8 9 4 | 22 32 27 24 38 26 29 21 27 24 23 15E | 11 23 10 10 40 9 23 18 13 12 5 | 31 44 37 35 49 36 39 36 31 29 33 16 | 7 23 8 15 27 5 22 10 17 26 5 | 15 36 22 19 40 19 33 16 23 15 19 17E | 7 20 8 14 19 5 23 8 13 10 4 | 28 32 29 30 36 30 31 28 31 27 27 18 | 7 20 9 15 25 6 20 15 12 23 5 | 17 32 23 26 30 21 29 21 24 21 20 19E | 7 21 10 12 31 6 23 10 12 11 4 | 14 26 23 24 42 21 23 17 13 19 17 20 | 6 16 7 11 59 5 14 8 9 22 4 | 14 22 16 18 32 17 21 13 20 15 14 21 | 7 24 8 11 30 4 22 6 15 16 5 | 17 35 24 20 38 23 31 19 26 24 20 22 | 7 20 9 11 44 6 19 13 10 21 4 | 19 34 26 26 35 27 32 30 27 27 24 23E | 5 20 8 9 36 5 16 11 11 18 4 | 36 44 40 41 42 41 41 38 41 41 38 24 | 5 15 7 11 26 3 10 10 12 19 4 | 13 22 18 19 20 16 14 17 15 21 15 X25 | 11 17 9 12 --- 14 --- 15 21 --- 6 | 20 24 21 25 --- 21 --- 22 30 --- 19 26E | 11 15 10 11 30 6 14 11 25 24 5 | 29 41 33 31 48 34 42 33 43 46 33 27 | 7 16 8 10 51 5 12 11 10 7 3 | 28 32 26 27 50 28 33 29 31 31 27 28 | 6 19 9 12 42 5 19 9 8 24 4 | 18 33 23 21 40 22 33 17 20 19 19 29E | 7 21 7 14 21 6 18 11 12 11 4 | 18 28 21 24 33 23 22 26 30 27 20 30 | 5 11 4 6 25 4 9 12 8 15 3 | 21 25 20 23 20 22 22 26 28 18 21 31 | 8 21 8 10 33 5 19 8 15 14 4 | 20 33 25 25 42 24 29 19 26 21 22 32 | 5 14 8 8 30 5 15 10 13 15 3 | 13 19 15 15 25 17 20 18 20 21 14 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 7 18 8 11 38 5 17 11 12 18 |T 28 37 31 31 47 31 33 29 32 30 29 WRMS | 7 18 8 11 37 5 17 10 9 15 |NE 22 31 25 25 44 25 26 23 26 23 23 MEDI | 7 18 8 11 33 5 18 10 11 16 |MD 18 32 24 24 39 23 29 21 26 21 20 Table 3.1548.2 GPS week: 1548 Day: 2 MJD: 55082.000 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 | 22 --- --- 18 --- 16 --- 15 17 --- 11 | 13 --- --- 26 --- 23 --- 19 31 --- 16 2 | 7 18 7 7 49 5 22 8 8 25 4 | 21 34 24 20 57 23 36 19 20 20 21 3E | 9 17 11 12 66 5 18 9 10 30 5 | 72 76 77 83 75 76 74 78 78 81 77 4 | 5 11 8 5 32 6 11 7 11 15 3 | 14 27 25 19 47 21 23 16 21 19 19 5 | 14 20 9 9 30 7 19 12 10 28 5 | 56 42 43 46 59 55 26 43 49 43 55 6E | 10 16 10 10 47 4 17 11 11 23 4 | 107 118 110 102 122 108 119 106 102 120 107 7 | 7 24 9 8 31 6 22 8 8 13 4 | 18 32 19 19 32 19 27 17 17 16 17 8 | 6 13 6 7 25 4 9 8 10 10 3 | 13 21 19 14 24 15 20 12 19 13 15 9 | 7 16 6 9 35 4 11 12 9 10 3 | 15 26 20 16 24 17 19 19 18 18 16 10 | 5 18 6 6 52 4 10 9 10 14 3 | 15 27 26 23 28 19 18 19 21 17 19 11 | 7 15 8 8 36 6 18 8 11 15 4 | 9 25 15 12 42 11 19 13 13 12 11 12 | 9 19 7 9 38 8 19 9 10 23 4 | 11 30 17 16 41 16 26 18 19 15 15 13E | 6 16 7 6 38 4 21 10 10 16 4 | 29 34 30 26 35 28 32 26 30 35 28 14E | 6 16 11 8 34 5 21 9 8 9 4 | 20 33 24 21 39 22 29 22 22 22 22 15E | 9 19 9 8 32 5 22 11 9 12 4 | 47 54 51 51 64 49 49 52 48 50 48 16 | 7 21 11 15 37 7 26 8 8 25 5 | 16 35 21 13 46 18 36 16 20 17 18 17E | 6 17 6 10 17 5 23 8 12 12 4 | 18 29 19 25 20 22 25 20 24 19 20 18 | 7 17 9 12 31 6 21 13 8 23 4 | 15 31 24 26 29 21 27 19 23 16 19 19E | 7 24 9 12 34 3 26 11 9 13 5 | 12 31 20 18 32 16 23 15 15 16 15 20 | 9 17 7 12 54 5 19 6 6 21 4 | 16 26 19 23 34 17 20 17 19 16 16 21 | 6 20 7 9 31 6 23 8 8 16 4 | 15 32 18 18 39 17 29 16 20 18 17 22 | 7 15 8 7 57 4 21 11 6 18 4 | 18 31 22 22 43 24 29 28 25 23 22 23E | 6 20 8 10 41 5 20 8 4 21 4 | 43 48 43 42 48 44 46 43 46 47 43 24 | 5 14 4 6 22 4 10 11 7 20 3 | 12 24 18 18 22 17 14 15 20 18 15 X25 | 8 19 10 11 --- 8 --- 10 12 --- 5 | 14 23 18 22 --- 17 --- 19 15 --- 15 26E | 13 18 13 9 29 5 13 11 20 25 5 | 31 43 37 32 59 35 42 33 42 46 34 27 | 9 18 7 8 41 4 12 10 9 11 3 | 17 27 20 21 39 19 24 18 22 20 18 28 | 5 17 6 8 51 4 18 9 11 23 4 | 13 28 18 14 45 16 26 11 15 15 13 29E | 6 14 8 11 20 4 18 13 9 14 4 | 22 25 21 24 22 20 19 28 26 27 22 30 | 6 10 6 6 21 6 8 9 7 16 3 | 22 25 24 23 24 22 22 28 30 20 23 31 | 6 20 11 12 38 5 22 10 8 15 4 | 18 32 23 22 44 21 30 18 20 20 19 32 | 9 15 10 9 44 6 20 9 7 16 4 | 9 19 18 16 33 14 16 15 12 18 12 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 17 8 9 39 5 19 10 9 19 |T 24 35 28 27 42 26 31 26 28 27 25 WRMS | 7 17 8 9 36 5 18 9 6 17 |NE 16 28 21 20 37 20 24 18 21 18 18 MEDI | 7 17 8 9 35 5 19 9 9 16 |MD 16 31 21 22 39 20 26 19 21 19 19 Table 3.1548.3 GPS week: 1548 Day: 3 MJD: 55083.000 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 | 23 --- --- 16 --- 18 --- 19 16 --- 11 | 24 --- --- 28 --- 25 --- 21 29 --- 21 2 | 8 21 10 8 44 6 25 9 9 27 5 | 22 36 27 23 55 23 37 20 20 22 22 3E | 10 19 8 12 55 4 18 12 9 27 5 | 114 115 117 118 116 117 112 116 114 120 115 4 | 5 13 7 8 35 4 10 10 10 17 3 | 23 31 27 19 59 19 26 21 22 22 22 5 | 13 21 8 12 24 6 19 12 16 27 5 | 96 51 49 52 85 87 24 48 47 49 93 6E | 8 17 6 11 48 3 17 10 8 29 4 | 109 116 110 108 118 110 119 106 108 115 110 7 | 8 25 9 13 33 5 21 10 11 14 5 | 19 32 26 24 32 20 28 20 21 25 21 8 | 6 15 10 12 25 4 9 11 10 9 3 | 19 28 23 24 25 20 24 21 25 20 20 9 | 8 15 8 13 46 6 12 10 11 9 4 | 18 26 19 18 33 18 24 19 22 20 17 10 | 4 11 8 9 29 4 8 10 12 15 3 | 22 25 28 22 22 21 21 21 16 22 20 11 | 10 18 8 13 43 5 16 8 10 14 4 | 15 29 22 19 43 15 21 15 16 17 15 12 | 11 17 7 10 33 5 19 11 10 22 4 | 13 26 16 16 37 14 26 16 16 13 13 13E | 9 20 7 8 33 7 18 17 13 24 5 | 43 49 43 42 46 44 46 44 43 48 42 14E | 8 19 8 10 26 4 20 10 9 10 4 | 26 36 28 30 42 27 33 22 31 26 26 15 | 16 22 8 10 26 9 21 17 10 15 5 | 46 56 55 49 55 50 52 53 53 50 50 16 | 8 22 10 11 30 7 21 10 11 25 5 | 19 35 23 18 42 20 34 18 21 19 19 17E | 8 22 8 12 30 5 21 8 9 7 4 | 24 36 26 24 42 23 29 25 27 23 24 18 | 8 17 9 13 30 5 21 15 8 28 5 | 18 28 23 26 30 19 29 21 24 22 20 19E | 9 21 7 13 37 5 22 13 10 15 5 | 16 30 22 26 33 21 24 17 15 20 17 20 | 13 19 6 9 49 5 17 7 12 21 4 | 22 28 25 26 32 23 22 22 27 19 21 21 | 7 24 8 12 26 4 24 9 7 26 5 | 18 34 19 16 37 17 34 18 24 23 18 22 | 6 19 7 10 40 4 18 11 6 20 4 | 20 31 25 28 38 25 30 27 25 23 23 23E | 8 25 8 10 42 6 18 12 9 21 5 | 78 79 74 78 73 76 80 75 75 80 76 24 | 4 11 6 6 24 3 10 9 7 18 3 | 14 19 18 15 22 14 16 16 18 19 14 X25 | 7 24 13 18 --- 8 --- 10 22 --- 7 | 19 31 21 28 --- 19 --- 21 32 --- 20 26E | 14 19 8 12 34 4 14 12 17 23 5 | 35 42 37 36 62 36 44 38 37 49 36 27 | 8 16 9 15 46 6 13 10 12 9 4 | 23 34 28 30 39 27 30 29 29 30 26 28 | 10 20 7 13 39 6 20 7 10 21 4 | 19 34 24 22 44 20 32 21 22 21 20 29E | 7 15 9 11 25 4 17 12 13 11 4 | 14 22 13 23 27 15 18 22 25 20 16 30 | 6 9 5 6 23 3 7 13 6 17 3 | 26 28 27 25 26 25 26 29 29 22 26 X31 | 8 19 9 9 31 6 --- 11 9 15 4 | 19 28 22 24 43 18 --- 19 21 18 20 32 | 11 18 7 8 28 4 17 10 9 14 4 | 19 25 26 20 26 20 21 23 24 21 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 8 11 36 5 18 11 10 19 |T 31 39 33 33 46 32 36 31 33 33 31 WRMS | 9 19 8 11 34 5 17 11 8 18 |NE 23 30 24 23 38 23 26 22 24 22 23 MEDI | 8 19 8 11 33 5 18 10 10 17 |MD 20 31 26 24 39 21 29 21 25 22 21 Table 3.1548.4 GPS week: 1548 Day: 4 MJD: 55084.000 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 --- --- 13 --- 14 --- 17 20 --- 9 | 20 --- --- 25 --- 20 --- 19 29 --- 18 2 | 6 24 10 7 40 6 22 11 10 25 5 | 23 36 24 24 52 25 35 21 20 22 22 3E | 9 18 7 20 50 4 17 12 9 32 5 | 110 107 105 110 123 106 111 113 114 109 109 4 | 7 14 6 6 48 5 10 12 6 14 3 | 21 30 22 22 49 20 29 19 20 21 20 5 | 11 22 12 12 32 7 21 14 12 28 5 | 63 43 40 47 61 62 35 46 47 46 61 6E | 10 15 7 10 48 5 18 8 10 33 5 | 108 118 116 116 124 112 119 113 110 131 114 7 | 8 25 13 10 29 4 22 9 12 12 5 | 16 33 24 24 34 16 29 17 17 18 18 8 | 6 15 5 9 26 4 11 9 8 7 3 | 15 19 13 15 20 13 17 14 14 14 11 9 | 7 18 12 11 43 5 13 9 7 9 4 | 12 25 17 17 30 13 17 18 13 15 13 10 | 5 14 10 8 32 4 10 11 12 15 4 | 14 23 24 22 23 18 17 18 20 19 17 11 | 8 16 8 13 38 4 16 11 8 16 4 | 11 27 16 17 44 11 21 11 15 13 11 12 | 8 17 10 11 29 4 19 10 8 25 4 | 15 25 16 13 34 12 25 15 11 13 11 13E | 10 21 7 9 35 5 20 12 11 14 4 | 29 36 30 27 44 28 37 25 29 26 26 14E | 7 20 10 9 26 5 19 10 6 11 4 | 18 24 23 19 31 17 26 16 15 17 16 15 | 7 22 10 10 36 6 23 13 8 16 4 | 24 32 29 29 37 25 30 25 24 24 24 16 | 8 23 10 16 31 4 23 10 7 25 5 | 21 37 21 19 47 21 36 19 18 17 19 17E | 7 16 8 11 30 6 23 8 8 9 4 | 16 30 21 26 30 19 26 23 23 24 21 18 | 7 20 11 14 34 5 23 16 8 23 5 | 14 27 24 26 33 15 28 20 17 16 17 19E | 9 24 9 14 31 4 25 11 9 15 5 | 13 27 18 22 30 16 22 13 16 16 14 20 | 9 16 10 10 62 5 18 9 9 23 4 | 22 26 27 23 35 22 21 20 24 18 20 21 | 5 22 7 12 28 4 26 8 7 16 4 | 14 31 18 16 38 12 31 13 15 17 13 22 | 6 18 10 9 50 5 21 10 7 20 4 | 19 29 26 25 35 21 29 23 21 18 20 23 | 7 23 10 10 46 5 19 12 7 22 4 | 104 104 108 108 121 104 102 105 103 101 104 24 | 5 14 8 8 36 5 12 11 9 19 3 | 14 19 17 17 24 14 16 15 19 17 14 X25 | 17 17 23 18 --- 12 --- 16 23 --- 8 | 17 20 28 22 --- 18 --- 14 31 --- 14 26E | 12 19 11 7 31 5 15 13 15 23 5 | 33 41 36 36 60 36 42 36 36 48 35 27 | 9 19 11 12 47 4 13 8 5 8 4 | 15 27 21 21 31 17 19 19 15 20 16 28 | 8 19 9 14 38 6 21 8 10 21 4 | 11 32 19 24 37 15 29 15 16 16 16 29E | 6 19 13 12 25 4 15 11 11 12 4 | 21 26 20 22 31 19 20 24 24 24 19 30 | 5 11 10 6 28 4 11 10 7 16 3 | 20 22 26 23 25 20 21 25 23 16 21 X31 | 7 22 9 9 40 5 --- 14 7 17 4 | 15 28 18 18 49 17 --- 18 14 17 14 32 | 8 15 9 8 44 4 17 12 7 17 4 | 13 20 24 18 28 16 17 19 19 17 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 11 38 5 19 11 9 19 |T 27 36 31 31 45 28 34 28 29 29 27 WRMS | 7 19 10 11 36 5 18 11 7 18 |NE 18 27 22 21 36 19 24 19 19 18 18 MEDI | 7 19 10 10 35 5 19 11 8 16 |MD 17 28 24 22 35 18 28 19 20 18 18 Table 3.1548.5 GPS week: 1548 Day: 5 MJD: 55085.000 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 | 12 --- --- 22 --- 17 --- 20 24 --- 11 | 15 --- --- 36 --- 30 --- 13 35 --- 21 2 | 7 23 8 7 36 4 20 11 9 23 4 | 19 34 24 20 49 20 32 19 16 17 19 3 | 9 17 9 8 41 5 15 11 10 23 4 | 125 124 123 124 132 123 124 125 125 121 124 4 | 6 14 10 6 26 3 10 9 10 10 3 | 19 25 21 19 54 19 25 19 18 20 18 5 | 9 18 6 14 28 4 18 11 11 28 5 | 62 28 26 33 51 53 27 32 35 30 59 6E | 9 15 6 10 60 4 17 10 10 32 4 | 106 114 114 109 114 109 114 107 106 127 110 7 | 6 22 8 10 32 4 19 11 11 14 4 | 15 30 16 21 34 16 25 17 16 17 15 8 | 6 15 7 9 20 4 8 10 10 9 3 | 10 25 13 15 24 12 18 15 13 12 11 9 | 8 15 8 7 37 3 10 10 8 12 3 | 14 25 20 13 29 16 22 20 18 19 16 10 | 7 13 7 10 26 2 8 9 8 17 3 | 15 19 19 19 19 16 16 14 19 19 14 11 | 5 17 7 9 35 3 15 11 11 18 4 | 9 23 11 12 39 7 19 10 12 14 7 12 | 9 17 8 12 29 3 19 10 11 26 5 | 18 29 17 16 32 16 28 16 19 14 15 13E | 8 19 7 6 36 4 18 11 9 17 4 | 38 44 39 38 46 39 42 39 40 42 38 14E | 9 17 11 8 27 5 20 10 7 12 4 | 26 32 30 28 40 26 32 26 29 26 26 15 | 9 19 9 11 32 3 21 11 10 14 4 | 21 28 25 23 35 21 27 21 24 24 21 16 | 8 23 12 13 24 5 23 11 15 27 5 | 17 33 21 14 35 17 33 13 20 14 15 17E | 7 17 9 13 33 5 25 9 11 8 4 | 19 26 18 25 35 18 27 20 22 21 18 18 | 7 16 6 15 27 4 21 12 9 27 5 | 14 27 18 24 30 15 27 20 20 19 16 19E | 8 25 12 12 34 5 26 10 10 15 5 | 13 28 22 17 32 15 25 13 15 15 14 20 | 7 17 9 9 64 4 16 10 11 25 4 | 17 26 21 22 33 21 23 21 27 16 19 21 | 6 21 9 12 40 4 26 8 9 20 5 | 14 31 21 21 37 17 32 20 23 22 18 22 | 7 18 9 9 56 4 19 11 7 21 4 | 17 32 23 22 38 20 29 20 19 18 18 23 | 6 22 7 9 47 4 17 11 7 22 4 | 32 41 35 38 56 34 37 36 34 40 34 X24 | 5 13 9 8 38 4 --- 13 12 21 4 | 12 18 13 18 25 10 --- 17 16 20 12 X25 | 12 17 12 16 --- 14 --- 15 18 --- 6 | 17 25 15 19 --- 14 --- 18 18 --- 14 26E | 13 19 13 10 28 5 13 13 13 24 5 | 30 38 36 32 56 32 41 31 31 45 31 27 | 9 13 8 9 34 4 9 10 7 11 3 | 22 30 27 21 34 23 30 25 20 26 23 28 | 8 18 6 11 45 5 19 8 11 24 4 | 14 31 22 20 37 17 29 16 20 20 17 29E | 7 12 12 17 37 5 18 13 12 12 4 | 24 22 23 29 41 23 25 27 27 26 23 30 | 7 9 8 7 21 4 8 9 9 20 3 | 18 25 17 22 19 19 20 22 26 14 18 X31 | 5 --- 7 7 33 10 --- --- --- --- 4 | 18 --- 22 20 38 20 --- --- --- --- 19 32 | 7 14 8 8 46 3 16 11 9 20 4 | 13 19 21 16 30 17 18 19 19 20 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 9 10 37 4 18 10 10 20 |T 25 34 28 28 42 26 33 26 28 28 26 WRMS | 7 18 9 10 38 4 18 10 8 17 |NE 17 26 19 20 34 18 25 18 20 18 18 MEDI | 7 17 8 9 34 4 18 11 10 20 |MD 17 28 21 21 35 19 27 20 20 20 18 Table 3.1548.6 GPS week: 1548 Day: 6 MJD: 55086.000 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 --- --- 21 --- 21 --- 19 17 --- 10 | 14 --- --- 32 --- 25 --- 19 29 --- 19 2 | 8 22 11 9 43 6 24 12 10 23 5 | 23 34 27 22 57 25 37 25 21 23 23 3 | 8 18 8 10 27 5 15 9 12 22 4 | 110 113 116 118 119 113 111 112 115 110 114 4 | 6 14 9 9 35 5 10 7 8 9 3 | 18 26 24 21 54 20 25 19 16 18 18 5 | 8 20 11 12 29 4 19 11 8 29 5 | 65 35 34 38 58 60 28 38 39 41 64 6E | 9 19 6 13 46 6 20 10 11 24 5 | 112 117 110 105 115 111 121 110 106 118 109 7 | 6 23 12 13 34 5 20 9 12 17 5 | 18 30 18 21 36 16 26 18 17 18 16 8 | 6 15 9 8 23 5 12 11 7 11 3 | 12 20 15 12 21 12 18 15 14 13 12 9 | 8 18 10 8 34 4 13 10 8 11 4 | 12 25 15 11 30 14 20 19 14 15 12 10 | 6 14 9 10 22 3 11 8 8 15 3 | 20 25 27 25 23 22 22 23 23 22 21 11 | 5 16 11 13 36 5 15 11 10 17 4 | 18 29 22 26 45 21 22 16 21 19 19 12 | 10 16 9 10 26 5 17 8 7 28 4 | 16 24 16 16 33 15 26 14 14 15 13 13E | 6 21 8 9 31 5 15 12 10 18 4 | 39 44 40 38 46 40 41 40 39 47 39 14E | 18 17 13 9 37 6 19 12 10 14 5 | 45 60 52 50 62 46 60 50 50 49 48 15 | 10 25 9 8 30 7 25 10 7 17 5 | 39 45 43 41 45 41 43 43 39 43 40 16 | 8 22 10 15 35 7 23 13 8 28 5 | 23 35 23 20 46 21 38 19 22 23 21 17E | 9 22 7 12 31 4 25 9 7 9 4 | 21 28 18 21 31 18 27 21 21 21 18 18 | 8 22 10 11 27 5 21 14 8 26 5 | 21 31 26 31 32 23 32 23 26 22 24 19E | 7 29 10 16 25 5 22 13 12 16 5 | 14 36 21 26 32 20 29 18 19 17 18 20 | 7 19 8 12 56 5 17 11 12 24 4 | 25 29 29 32 36 29 25 29 32 23 26 21 | 7 21 8 12 34 6 25 11 10 23 5 | 15 30 19 17 35 16 33 19 22 24 17 22 | 8 21 10 10 36 6 19 10 6 23 4 | 26 33 31 35 36 29 33 28 31 27 28 23 | 6 26 8 11 42 5 17 11 8 21 4 | 46 49 50 53 74 48 45 49 48 47 47 X24 | 7 19 8 11 32 5 --- 17 8 --- 5 | 14 22 18 19 25 15 --- 21 19 --- 16 X25 | 8 21 17 21 --- 13 --- 11 18 --- 7 | 13 20 18 17 --- 18 --- 15 18 --- 12 26E | 15 23 15 11 27 5 14 16 12 27 6 | 40 48 43 43 63 42 49 40 41 53 41 27 | 8 22 11 10 40 4 13 7 7 10 4 | 16 30 18 16 39 17 23 17 17 19 16 28 | 8 21 16 12 41 6 20 10 8 24 5 | 19 31 18 18 43 17 28 18 18 21 16 29E | 9 18 13 12 17 4 18 11 9 13 4 | 20 26 18 21 22 17 20 24 22 23 19 30 | 7 13 10 7 19 5 8 11 8 20 3 | 26 32 31 28 29 28 27 33 33 21 28 31 | 5 17 12 13 26 4 17 16 11 19 5 | 18 33 20 21 39 22 27 17 17 22 17 32 | 7 17 11 10 36 6 14 12 10 19 4 | 19 23 27 24 30 24 22 24 21 26 21 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 20 10 11 34 5 18 11 9 20 |T 29 37 31 31 45 30 36 30 30 32 29 WRMS | 7 20 10 11 33 5 18 11 7 20 |NE 20 28 22 22 37 22 26 21 22 21 20 MEDI | 8 20 10 11 32 5 17 11 8 19 |MD 20 31 24 24 36 22 28 21 22 23 19 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 4.1548 GPS week: 1548 MJD: 55080.0-55086.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3039 |U 10 11 30 |U 6 7 26 |U 9 8 20 | emr | emr 2932 | 12 12 31 |U 7 8 30 | 10 9 21 | esa | esa 2962 | 10 12 30 |U 6 7 25 | 9 8 19 | gfz | gfz 3021 |U 11 12 30 |U 12 11 40 | 10 9 20 | grg | grg 2880 | 11 12 33 |U 8 8 28 | 11 10 22 | igr | igr 2931 | 11 12 31 | 7 9 30 | 10 9 22 | igs | igs 2926 | 11 11 30 | 6 8 30 | 9 8 19 | jpl | jpl 2771 |U 10 12 34 |U 7 8 31 |U 9 8 20 | mit | mit 3044 |U 11 12 31 |U 7 9 32 |U 11 11 27 | 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 5.1548.0 GPS week: 1548 Day: 0 MJD: 55080.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2959 | 6 6 25 | 8 9 33 | 11 8 31 | emr | emr 2864 | 10 8 31 | 8 10 36 | 11 9 33 | esa | esa 2880 | 7 7 28 | 8 9 32 | 11 10 32 | gfz | gfz 2937 | 8 5 26 | 15 11 46 | 10 10 31 | grg | grg 2880 | 7 7 30 | 10 8 33 | 13 8 33 | igr | igr 2858 | 7 7 26 | 9 11 38 | 10 8 32 | igs | igs 2848 | 7 5 29 | 9 11 38 | 10 9 32 | jpl | jpl 2768 | 8 7 29 | 9 10 33 | 10 8 31 | mit | mit 2976 | 7 6 27 | 11 16 38 | 11 13 31 | Table 5.1548.1 GPS week: 1548 Day: 1 MJD: 55081.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3038 | 7 6 31 | 6 10 28 | 9 8 15 | emr | emr 2955 | 9 10 23 | 7 8 30 | 9 6 15 | esa | esa 2976 | 7 6 21 | 6 9 28 | 8 8 13 | gfz | gfz 3023 | 9 9 27 | 12 10 47 | 12 9 16 | grg | grg 2880 | 8 6 22 | 8 7 29 | 11 10 19 | igr | igr 2958 | 7 7 20 | 7 9 34 | 9 7 16 | igs | igs 2851 | 7 7 23 | 6 9 33 | 9 7 16 | jpl | jpl 2765 | 8 7 24 | 8 9 32 | 10 7 19 | mit | mit 3072 | 7 8 26 | 8 7 36 | 12 12 29 | Table 5.1548.2 GPS week: 1548 Day: 2 MJD: 55082.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3047 | 16 13 32 | 6 5 27 | 7 7 15 | emr | emr 2954 | 15 16 33 | 7 8 30 | 8 5 16 | esa | esa 2976 | 16 12 33 | 5 5 27 | 8 5 16 | gfz | gfz 3033 | 16 15 35 | 11 11 45 | 6 6 17 | grg | grg 2880 | 16 11 37 | 7 8 24 | 8 4 19 | igr | igr 2889 | 20 15 45 | 8 11 38 | 11 12 29 | igs | igs 3023 | 15 14 32 | 6 8 31 | 7 5 14 | jpl | jpl 2867 | 13 13 37 | 6 8 29 | 7 4 13 | mit | mit 3072 | 15 14 37 | 7 8 31 | 11 10 19 | Table 5.1548.3 GPS week: 1548 Day: 3 MJD: 55083.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3049 | 12 24 42 | 6 6 19 | 10 11 26 | emr | emr 2964 | 12 21 40 | 7 7 23 | 11 14 25 | esa | esa 2976 | 13 25 43 | 4 5 16 | 11 12 20 | gfz | gfz 3036 | 15 24 43 | 12 11 35 | 9 12 18 | grg | grg 2880 | 10 27 46 | 7 8 24 | 11 13 23 | igr | igr 2973 | 12 24 42 | 5 5 17 | 11 12 22 | igs | igs 3015 | 13 23 41 | 6 7 24 | 9 11 19 | jpl | jpl 2772 | 11 25 54 | 8 7 39 | 10 10 22 | mit | mit 3072 | 14 25 45 | 6 7 23 | 11 10 22 | Table 5.1548.4 GPS week: 1548 Day: 4 MJD: 55084.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3047 | 15 10 30 | 6 4 21 | 11 14 23 | emr | emr 2953 | 17 14 29 | 5 7 22 | 14 16 22 | esa | esa 2976 | 15 11 31 | 5 6 19 | 13 13 22 | gfz | gfz 3036 | 15 11 30 | 12 10 36 | 14 16 26 | grg | grg 2880 | 16 11 37 | 7 9 27 | 15 16 20 | igr | igr 2990 | 16 11 31 | 5 7 19 | 13 13 20 | igs | igs 2955 | 15 11 30 | 5 6 20 | 12 13 20 | jpl | jpl 2772 | 13 10 30 | 7 7 20 | 11 11 21 | mit | mit 3072 | 16 13 32 | 6 7 22 | 15 12 46 | Table 5.1548.5 GPS week: 1548 Day: 5 MJD: 55085.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3064 | 8 6 21 | 6 7 30 | 7 5 14 | emr | emr 2872 | 12 7 26 | 7 9 39 | 8 9 22 | esa | esa 2976 | 8 7 25 | 7 7 32 | 6 6 17 | gfz | gfz 3043 | 7 8 23 | 12 12 34 | 8 6 15 | grg | grg 2880 | 10 7 27 | 8 7 32 | 9 9 23 | igr | igr 2906 | 9 6 25 | 7 9 39 | 6 6 19 | igs | igs 2874 | 10 6 25 | 6 8 37 | 6 6 16 | jpl | jpl 2679 | 10 8 31 | 7 8 38 | 7 7 22 | mit | mit 2976 | 9 5 26 | 6 9 40 | 9 13 23 | Table 5.1548.6 GPS week: 1548 Day: 6 MJD: 55086.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3069 | 8 15 29 | 6 9 27 | 6 6 14 | emr | emr 2966 | 8 11 32 | 6 9 28 | 9 7 17 | esa | esa 2976 | 8 15 28 | 5 9 26 | 8 7 13 | gfz | gfz 3044 | 8 15 31 | 8 10 36 | 9 8 16 | grg | grg 2880 | 8 15 35 | 8 8 28 | 10 7 19 | igr | igr 2946 | 7 13 28 | 6 10 27 | 7 7 15 | igs | igs 2919 | 7 14 29 | 6 7 26 | 7 6 14 | jpl | jpl 2775 | 10 12 35 | 7 9 29 | 7 6 12 | mit | mit 3072 | 7 14 27 | 7 9 30 | 8 6 16 | Table 6: Earth Orientation Parameters weekly summary. Weekly mean and standard deviation of Centre ERP, ERP rates and LOD differences with respect to IGS combined values. See Table 7 for the daily summaries. Xpole,Xrt: x pole and x pole rate Ypole,Yrt: y pole and y pole rate LOD : Length Of Day AC LOD BIAS : 21-day mean LOD bias with respect to Bulletin A AC LOD BIAS RMS: RMS of AC LOD BIAS FLAG: "u" (used), "x" (excluded), "-" (no submission) for Xpole, Ypole, Xrt, Yrt and LOD Table 6.1548 GPS week: 1548 MJD: 55080.500-55086.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -7 -13 -7 37 5 | 1 14 | 18 25 83 33 5 | 3 emr uuuuu | 24 -14 202 30 -5 | 53 55 | 15 22 94 93 15 | 2 esa uuuuu | 12 -43 121 8 -7 | 24 28 | 14 13 92 119 7 | 2 gfz uuuuu | -35 38 -21 -133 0 | -4 15 | 14 12 78 43 7 | 2 grg xxxxx | -43 -35 -6 22 2 | 3 14 | 36 41 108 58 23 | 3 igr xxxxx | -4 30 15 9 -5 | -7 17 | 24 19 48 79 15 | 4 irf xxxxx | -6 -9 -42 -5 -9 | -2 14 | 9 7 20 21 9 | 3 jpl uuuux | 13 -11 -56 142 -14 | 29 41 | 22 19 89 54 20 | 8 mit uuuuu | -11 9 -287 -93 -12 | 18 23 | 23 18 78 58 8 | 3 ngs uuuuu | -18 -5 95 140 4 | 5 13 | 29 40 89 127 7 | 4 sio uuuuu | 60 60 -51 -138 -19 | 40 43 | 14 16 48 63 13 | 6 Table 7.1548.0 GPS week: 1548 Day: 0 MJD: 55080.500 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 -24 -14 -2 -6 | 1 14 emr uuuuu | 27 17 38 179 -19 | 57 58 esa uuuuu | -6 -59 20 -102 -12 | 26 32 gfz uuuuu | -39 44 -39 -203 -13 | 1 18 grg xxxxx | -30 -30 -94 0 30 | -2 14 igr xxxxx | 5 29 -67 -118 -19 | 1 19 irf xxxxx | -17 -21 -21 -25 -20 | 3 14 jpl uuuux | 49 2 -92 100 -49 | 41 50 mit uuuuu | -48 -26 -172 -105 -26 | 23 26 ngs uuuuu | 20 34 226 254 13 | 2 11 sio uuuuu | 56 51 -50 -106 -34 | 50 52 Table 7.1548.1 GPS week: 1548 Day: 1 MJD: 55081.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -3 1 60 49 3 | -2 13 emr uuuuu | 26 0 146 100 -25 | 54 56 esa uuuuu | 23 -24 110 132 -4 | 22 27 gfz uuuuu | -50 54 55 -145 -7 | -4 17 grg xxxxx | -56 2 -4 18 -17 | 1 16 igr xxxxx | -11 29 22 -63 -25 | -4 19 irf xxxxx | -15 -4 -28 -6 -16 | -2 15 jpl uuuux | 33 4 32 98 -36 | 36 49 mit uuuuu | -26 7 -285 -59 -19 | 18 24 ngs uuuuu | -28 -67 0 -123 7 | 1 9 sio uuuuu | 56 66 -35 -26 -34 | 44 48 Table 7.1548.2 GPS week: 1548 Day: 2 MJD: 55082.500 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 -28 -27 37 9 | -2 14 emr uuuuu | 25 -15 195 8 -16 | 53 55 esa uuuuu | 21 -42 33 174 -18 | 22 28 gfz uuuuu | -11 37 39 -138 3 | -6 15 grg xxxxx | -20 -83 72 -30 -22 | 3 16 igr xxxxx | -2 1 80 61 -13 | -8 15 irf xxxxx | -13 -3 -36 -28 -14 | -3 13 jpl uuuux | 6 -21 -4 120 -9 | 30 43 mit uuuuu | -25 17 -208 -157 -14 | 17 23 ngs uuuuu | -18 -18 18 105 10 | 3 13 sio uuuuu | 36 78 29 -174 -27 | 41 44 Table 7.1548.3 GPS week: 1548 Day: 3 MJD: 55083.500 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 | 1 13 103 -3 10 | 1 15 emr uuuuu | -7 -24 243 -57 -3 | 52 55 esa uuuuu | -2 -36 52 36 -12 | 24 28 gfz uuuuu | -40 40 46 -117 6 | -5 15 grg xxxxx | -23 -22 -63 97 -8 | 2 16 igr xxxxx | 21 38 26 46 -5 | -9 16 irf xxxxx | 5 -12 -33 -5 -7 | -3 14 jpl uuuux | -18 20 -29 142 -2 | 28 40 mit uuuuu | 10 7 -289 -96 -7 | 17 23 ngs uuuuu | 12 -9 49 144 2 | 6 15 sio uuuuu | 79 43 -33 -116 -14 | 39 43 Table 7.1548.4 GPS week: 1548 Day: 4 MJD: 55084.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -14 -42 33 46 6 | 4 15 emr uuuuu | 22 -52 302 7 0 | 54 56 esa uuuuu | 0 -53 212 -159 -3 | 26 29 gfz uuuuu | -41 22 -5 -58 6 | -3 14 grg xxxxx | -65 -32 15 92 0 | 5 14 igr xxxxx | -51 16 0 26 5 | -9 15 irf xxxxx | -4 -8 -51 -10 -8 | -2 13 jpl uuuux | -3 -24 -169 249 -6 | 28 40 mit uuuuu | 7 26 -333 -127 -11 | 19 24 ngs uuuuu | -3 18 56 244 1 | 9 15 sio uuuuu | 58 62 -87 -171 -16 | 39 42 Table 7.1548.5 GPS week: 1548 Day: 5 MJD: 55085.500 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 | -42 21 -49 92 6 | 4 15 emr uuuuu | 32 -18 182 -91 10 | 53 55 esa uuuuu | 27 -52 170 -14 5 | 25 28 gfz uuuuu | -42 24 -96 -142 4 | -3 14 grg xxxxx | -106 14 -143 35 -9 | 6 13 igr xxxxx | -4 37 -8 -10 5 | -9 16 irf xxxxx | 4 -12 -47 36 2 | -4 13 jpl uuuux | 16 -23 -169 116 -5 | 24 36 mit uuuuu | 14 4 -316 19 -4 | 16 22 ngs uuuuu | -58 44 202 177 -4 | 9 15 sio uuuuu | 67 41 -55 -154 -5 | 35 39 Table 7.1548.6 GPS week: 1548 Day: 6 MJD: 55086.500 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 | 17 -33 -152 37 9 | 3 14 emr uuuuu | 41 -2 306 63 15 | 51 52 esa uuuuu | 24 -31 251 -10 -4 | 24 26 gfz uuuuu | -20 49 -148 -128 5 | -5 14 grg xxxxx | 0 -94 178 -55 37 | 6 13 igr xxxxx | 16 63 55 118 18 | -11 16 irf xxxxx | -2 -4 -81 4 2 | -6 13 jpl uuuux | 9 -32 40 172 6 | 17 27 mit uuuuu | -5 27 -406 -129 -3 | 13 19 ngs uuuuu | -47 -39 116 179 -4 | 9 15 sio uuuuu | 70 79 -126 -221 -3 | 31 34