Date: Thu, 01 Oct 2009 11:40:54 +0000 From: Jim Ray Subject: [IGSREPORT-17853] Wk 1549 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4ac49546.G9/8K6u/oVmPlJ6j%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 01 Oct 04:41:17 PDT 2009 Message Number 17853 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1549 (Sep 13, 2009 - Sep 19, 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: igs1549[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1549[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1549[0-6].cls IGS GPS clock combination summary report. igs15497.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15497.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 | EMR | WTZR WTZR 0 | ESA | HYDE UNSA 0 | GFZ | 1 17 19 FAA1 HARB VILL 0 | GRG | ONSA TWTF 0 | JPL | 5 32 0 | MIT | 24 HARB TWTF 0 | NGS | 1 1 | ALL | 1 1 | COD | MAW1 MDVJ MIZU TWTF 1 | EMR | HARB TWTF WTZR 1 | ESA | NLIB UNSA 1 | GFZ | 17 19 29 CAS1 DARW FAA1 KARR THTI TRO1 TWTF 1 | GRG | USNO 1 | JPL | 5 32 1 | MIT | BOR1 2 | COD | 24 MDVJ 2 | EMR | WTZR 2 | ESA | STJO 2 | GFZ | 19 24 FAA1 KIRU QAQ1 2 | GRG | TWTF USNO 2 | JPL | 5 32 MDVJ 2 | MIT | TWTF 2 | NGS | 1 3 | ALL | 1 3 | COD | TWTF 3 | EMR | HARB HARB NYAL WTZR 3 | ESA | ALIC UNSA 3 | GFZ | 1 8 ONSA STJO VILL 3 | GRG | TWTF USNO 3 | JPL | 5 32 BOGT 3 | MIT | 29 TWTF ALIC NYA1 OUS2 TWTF 3 | NGS | 1 4 | ALL | 1 4 | COD | 21 4 | ESA | 24 UNSA YELL 4 | GFZ | 24 29 FAA1 HOFN HRM1 MAS1 WSRT 4 | GRG | USNO 4 | JPL | 5 32 4 | MIT | 9 24 9 24 IRKJ MIZU 5 | COD | WROC JOZ2 WHIT WROC 5 | ESA | SCH2 UNSA 5 | GFZ | 1 19 FAA1 HARB HRM1 WSRT ZIMM 5 | GRG | NLIB TWTF 5 | JPL | 5 21 32 5 | MIT | 24 IRKJ TWTF 5 | NGS | 1 6 | ALL | 1 6 | ESA | UNSA 6 | GFZ | 19 24 CHUR FAA1 KIRU KIT3 6 | GRG | ONSA 6 | JPL | 5 32 6 | MIT | 24 24 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 ----+--------+--------+------------- 3 | MIT | ~00:00 | ~ -0.55 ns 6. The following table lists all maneuvered satellites for this week. The solutions from COD and ESA, which modeled the maneuver, are used that day for combination. An associated accuracy code of 0 (unknown) is given if only one AC is left (no redundancy). For the long arc evaluation the arc is split into two parts at the given maneuver epoch. PRN | Date | Ref. NANU ----+------------+---------- G23 | 2009_09_18 | 2009071 7. The following orbit solutions were excluded from the combination because they were biasing the weighted average (generally indicated by long arc RMS). They were still used for statistics computation. Day | Centre | PRN list ----+--------+--------------- 0 | SIO | 6 8. 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. 9. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .4 .7 1.7 -5 4 -13 -.41 EMR | .8 4.0 -5.0 68 4 21 .04 ESA | 1.0 2.8 3.7 70 -14 39 -.09 GFZ | .2 .3 1.0 11 -13 6 -.27 GRG | 4.3 3.1 .8 7 2 1 .06 JPL | -2.5 7.0 -4.1 22 -29 5 .10 MIT | 2.0 -3.0 2.2 7 0 -12 -.37 NGS | 2.9 .0 1.5 3 -23 -10 -.25 SIO | .6 -.6 -9.0 -15 -36 -29 -.02 10. 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. 11. 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. 12. 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 1.1549.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1549.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 2.1549.[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 3.1549.[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 5.1549.0-6). 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 1549 summary. (Sep 13, 2009 - Sep 19, 2009) Table 1.1549.a GPS week: 1549 MJD: 55087.000-55093.000 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 227| 1 0 1 43 -34 -2 -.17 8 8 | -268 -435 16 69 | 0 0 1 9 22 17 .03 | 219 601 emr 76| -1 1 -3 -122 -17 1 .55 19 19 | 2084 -456 15 82 | 1 1 2 29 26 13 .04 | 756 1109 esa 128| 0 0 1 -102 34 -7 .37 9 9 | -1082 517 19 121 | 0 0 1 11 16 19 .04 | 597 1729 gfz 184| 0 0 -1 34 -62 -13 -.17 11 11 | 161 -428 23 110 | 0 0 1 40 59 13 .03 | 183 519 grg 112| 4 1 -1 43 -11 41 1.10 35 36 | 189 -433 76 223 | 1 1 3 18 19 46 .03 | 234 655 igr n/a| 0 0 1 38 -15 -35 .07 5 5 | -9224 -556 18 65 | 0 0 0 12 14 23 .03 | 1119 1279 jpl 123| 1 0 -4 -13 36 33 .61 18 18 | 2643 -486 17 84 | 1 1 1 18 19 31 .04 | 848 1220 mit 264| 0 -1 -1 35 -29 -1 -.28 10 9 | -15290 -448 21 128 | 0 0 0 6 27 7 .03 | 487 389 ngs 218| -1 0 0 22 40 16 -.30 9 7 | -113372 180562 2031 3718 | 0 0 0 22 46 16 .03 | 336587 477064 sio 253| 0 0 4 84 66 -5 .05 21 20 | --- --- --- --- | 0 0 1 12 32 13 .05 | --- --- Table 1.1549.b GPS week : 1549 MJD: 55087.000-55093.000 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 | 9 10 11 11 12 15 11 | 2 | 5 5 5 5 4 5 5 | 3 | 5 4 4 4 4 4 5 | 4 | 4 4 4 4 4 4 4 | 5 | 5 5 6 5 5 6 5 | 6 | 7 6 5 5 4 4 4 | 7 | 5 4 4 5 4 5 5 | 8 | 4 4 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 6 6 | 13 | 5 5 4 4 4 4 4 | 14 | 4 4 4 4 4 4 4 | 15 | 6 6 6 6 6 6 6 | 16 | 5 6 6 6 6 6 5 | 17 | 5 5 5 4 5 6 5 | 18 | 5 5 5 5 4 5 5 | 19 | 6 5 5 5 5 5 5 | 20 | 4 5 5 4 4 5 4 | 21 | 5 5 5 5 5 5 5 | 22 | 4 5 4 5 5 5 5 | 23 | 5 5 5 5 5 10 4 | 24 | 7 7 7 9 8 8 8 | 25 | 4 3 3 4 4 4 4 | 26 | 6 6 5 5 5 5 5 | 27 | 4 4 4 4 4 4 4 | 28 | 5 5 4 5 5 5 5 | 29 | 4 4 5 5 5 5 5 | 30 | 4 3 3 3 4 4 4 | 31 | 5 5 5 5 5 5 4 | 32 | 4 4 4 4 4 4 3 | 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 2.1549.0 GPS week: 1549 Day: 0 MJD: 55087.000 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 227| 0 0 0 61 -56 2 -.18 8 7 | -211 60 16 69 | 16 18 | emr 76| -3 1 -7 -106 -36 8 .55 19 19 | 1947 1707 18 82 | 8 -43 | esa 128| 1 -1 2 -99 42 -8 .41 8 8 | -1604 1347 21 119 | 86 7 | gfz 184| 0 0 0 -7 -13 -1 -.17 12 12 | -71 296 25 112 | -18 37 | grg 112| 1 2 -1 43 -39 64 1.16 33 34 | -16 204 79 239 | 14 58 | igr n/a| 0 0 1 48 -33 -19 .10 5 5 | -9345 2053 19 61 | 6 4 | jpl 123| 3 -1 -6 10 40 46 .59 18 18 | 2037 2027 18 77 | -2 7 | mit 264| 0 -1 -1 40 -16 3 -.34 12 12 | -14945 -341 23 116 | -23 0 | ngs 218| -1 2 1 15 -2 -13 -.35 10 8 | -876675 1262429 2290 4093 | 48 29 | sio 253| -1 1 3 108 97 16 -.05 26 21 | --- --- --- --- | -84 -76 | Table 2.1549.1 GPS week: 1549 Day: 1 MJD: 55088.000 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 227| 0 0 2 48 -55 -5 -.16 9 8 | -71 -1739 17 61 | 14 -21 | emr 76| -2 2 -7 -134 -19 0 .55 20 20 | 3602 -1768 17 70 | 36 -60 | esa 128| 1 -1 0 -86 52 2 .36 9 9 | -493 -3033 20 118 | 28 -31 | gfz 184| 0 0 0 53 9 -4 -.14 11 11 | 492 -1305 25 111 | -32 7 | grg 112| 6 2 1 11 -20 98 1.09 32 33 | 541 -1598 71 224 | 67 42 | igr n/a| 0 0 2 27 -20 -50 .09 5 5 | -7281 -1895 19 60 | 6 -12 | jpl 123| 0 0 -7 -41 47 6 .59 18 18 | 4147 -1783 18 81 | 46 -115 | mit 264| 0 0 0 26 -60 -8 -.29 10 9 | -15326 -956 17 98 | -5 10 | ngs 218| -1 0 1 11 15 21 -.30 8 6 | 15140 -4324 2260 3752 | 3 39 | sio 253| 1 0 3 80 42 -19 .02 20 19 | --- --- --- --- | -54 -65 | Table 2.1549.2 GPS week: 1549 Day: 2 MJD: 55089.000 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 227| 0 0 2 35 -61 -21 -.16 8 7 | -161 -468 22 81 | -5 44 | emr 76| -3 3 -4 -161 -60 -4 .60 20 20 | 2556 -735 16 73 | 42 0 | esa 128| 2 0 2 -88 47 6 .43 9 9 | -47 -46 21 131 | 35 2 | gfz 184| -1 1 -3 93 -6 -17 -.18 12 12 | 4 -55 26 112 | -28 35 | grg 112| 3 0 3 46 -34 32 1.09 34 35 | 163 75 78 212 | 73 96 | igr n/a| 0 0 1 16 -37 -35 .08 5 5 | -8120 -1077 20 69 | -34 10 | jpl 123| 0 0 -4 -35 -3 38 .66 18 18 | 3554 -954 18 86 | -1 -54 | mit 264| 0 -2 0 45 22 -5 -.30 10 9 | -15606 -203 25 142 | -16 -8 | ngs 218| -1 0 0 -16 -21 31 -.30 7 5 | 12388 533 1921 3454 | 39 31 | sio 253| 0 0 5 90 127 -20 .02 20 21 | --- --- --- --- | -52 -89 | Table 2.1549.3 GPS week: 1549 Day: 3 MJD: 55090.000 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 227| 0 1 0 39 -8 19 -.13 8 8 | -122 -335 18 70 | 26 -15 | emr 76| 0 0 -3 -124 -10 -3 .59 19 19 | 1595 -236 16 87 | 15 1 | esa 128| 0 0 4 -109 37 -50 .39 9 9 | -1394 1696 18 115 | 41 31 | gfz 184| 0 0 -1 27 -71 -25 -.17 10 10 | 168 -276 23 118 | 1 0 | grg 112| 4 0 -2 55 -5 87 1.05 34 36 | 434 -658 77 208 | 52 -13 | igr n/a| 0 0 0 35 1 -61 .11 5 5 | -9485 -810 18 64 | -16 -4 | jpl 123| 2 0 -4 -3 39 90 .64 19 19 | 2346 -575 17 75 | 34 25 | mit 264| 0 0 -2 36 -33 -8 -.26 8 7 | -15545 -348 22 129 | -12 3 | ngs 218| -2 0 1 26 40 22 -.31 8 6 | 12215 3480 1833 3232 | -12 -31 | sio 253| 0 0 2 82 43 -2 .05 19 21 | --- --- --- --- | -64 -67 | Table 2.1549.4 GPS week: 1549 Day: 4 MJD: 55091.000 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 227| 0 1 1 41 -15 -28 -.15 8 8 | -717 -84 13 56 | 41 17 | emr 76| -1 1 -1 -126 -4 -1 .57 19 19 | 1744 -868 16 89 | 28 -45 | esa 128| 0 0 1 -110 33 0 .34 10 9 | -1519 1629 19 122 | 58 40 | gfz 184| 0 0 -1 -7 -119 5 -.16 9 9 | 165 -313 23 106 | -11 3 | grg 112| 5 0 -5 30 8 -20 1.13 37 40 | 236 -899 75 226 | 35 -17 | igr n/a| 0 0 1 44 -3 -56 .06 5 4 | -9922 -1025 18 65 | -17 -13 | jpl 123| 1 -2 -4 -10 58 39 .66 18 18 | 2197 -893 19 90 | 27 -21 | mit 264| 0 0 -1 36 -26 10 -.26 10 9 | -14749 -819 22 152 | -11 -6 | ngs 218| 0 0 0 40 59 2 -.26 8 7 | 13105 1863 2104 3521 | -59 4 | sio 253| 0 0 5 82 52 4 .10 19 20 | --- --- --- --- | -48 -71 | Table 2.1549.5 GPS week: 1549 Day: 5 MJD: 55092.000 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 227| 1 0 3 31 -17 9 -.19 8 8 | -369 -336 16 82 | 28 2 | emr 76| -1 0 0 -136 24 26 .52 18 18 | 1636 -1201 12 80 | 17 -60 | esa 128| 0 0 -1 -112 8 -5 .38 10 10 | -1485 1792 16 119 | 16 41 | gfz 184| 0 0 -4 74 -143 -16 -.12 11 11 | 108 -551 22 111 | -55 -4 | grg 112| 2 2 -5 48 6 -14 1.10 37 39 | 76 -215 66 226 | 37 -21 | igr n/a| 0 0 0 41 -6 4 .03 5 5 | -10127 -1151 15 68 | -67 6 | jpl 123| 2 0 -2 -7 32 -8 .54 17 17 | 2172 -1121 16 92 | 1 88 | mit 264| 0 -1 0 32 -39 0 -.28 11 9 | -16067 178 20 123 | 5 -7 | ngs 218| 0 0 0 24 105 14 -.32 9 8 | 14922 84 1823 3426 | 57 -20 | sio 253| 0 0 7 76 53 -5 .11 21 20 | --- --- --- --- | -44 -66 | Table 2.1549.6 GPS week: 1549 Day: 6 MJD: 55093.000 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 227| 2 2 1 46 -30 5 -.22 9 9 | -225 -149 15 65 | 11 -1 | emr 76| 0 3 -2 -65 -16 -18 .49 17 17 | 1510 -95 16 95 | -28 -19 | esa 128| 0 0 2 -113 16 0 .30 8 8 | -1032 238 18 124 | 31 47 | gfz 184| 0 0 -3 7 -93 -31 -.22 9 9 | 262 -793 21 103 | -43 -6 | grg 112| 5 0 -2 71 4 39 1.10 39 35 | -106 60 88 227 | -12 -15 | igr n/a| 0 0 1 54 -10 -27 .05 5 5 | -10293 8 17 69 | -69 13 | jpl 123| 0 0 -4 -4 35 22 .58 17 17 | 2050 -107 16 91 | 30 56 | mit 264| -1 0 -2 32 -52 -2 -.24 12 11 | -14798 -652 18 139 | -4 -16 | ngs 218| 0 0 0 54 87 34 -.29 9 6 | 15301 -129 1991 4553 | -15 29 | sio 253| 0 0 6 71 48 -9 .08 20 20 | --- --- --- --- | -29 -76 | 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 3.1549.0 GPS week: 1549 Day: 0 MJD: 55087.000 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 --- --- 19 --- 19 --- 14 15 --- 9 | 19 --- --- 25 --- 25 --- 17 30 --- 21 2 | 6 22 8 13 41 6 21 17 6 21 5 | 22 32 22 22 54 21 30 23 22 26 22 3 | 9 20 9 13 21 5 14 13 10 24 4 | 17 21 17 24 20 16 17 22 22 22 16 4 | 5 13 7 12 33 4 10 10 9 24 4 | 13 19 15 16 33 12 16 13 13 27 12 5 | 8 20 6 9 24 4 18 17 9 30 5 | 27 27 24 27 30 23 29 29 26 26 23 6E | 21 24 9 16 37 9 20 19 11 82 7 | 91 109 104 104 107 99 106 95 97 67 98 7 | 6 23 7 14 28 5 20 9 15 13 4 | 18 33 23 24 40 22 31 17 16 17 18 8 | 6 15 9 10 23 4 10 10 12 16 4 | 13 22 15 18 28 14 20 15 15 22 14 9 | 7 19 11 11 32 6 11 12 6 20 4 | 10 24 20 16 25 13 19 17 15 21 14 10 | 5 17 9 8 27 4 10 9 7 20 3 | 21 27 27 25 17 23 19 23 23 22 21 11 | 6 17 7 13 36 4 16 15 9 18 4 | 16 36 24 21 54 20 26 22 17 18 19 12 | 6 17 10 9 26 5 16 12 7 34 4 | 22 34 26 24 43 24 35 23 23 32 24 13E | 6 23 7 10 26 4 21 11 10 11 4 | 73 74 75 76 86 76 72 78 73 76 74 14 | 4 14 6 10 33 8 19 11 7 14 3 | 20 24 21 21 24 17 27 22 25 20 22 15 | 10 25 11 11 22 4 22 17 13 12 5 | 14 25 17 16 28 14 24 19 18 18 13 16 | 7 20 8 15 25 8 23 12 7 30 5 | 16 29 20 16 35 16 30 16 16 25 15 17E | 10 22 5 14 25 5 25 12 9 12 5 | 38 36 33 37 39 35 37 35 36 36 33 18 | 6 19 6 14 28 4 20 16 9 21 4 | 16 28 22 25 33 17 26 20 20 14 18 19E | 7 28 10 16 34 4 26 12 9 25 5 | 23 35 21 22 29 21 30 19 24 34 21 20 | 7 17 5 14 49 4 19 9 8 21 4 | 21 30 26 30 40 25 26 24 23 23 22 21 | 6 20 6 11 39 3 24 10 11 22 4 | 18 37 23 18 43 21 36 22 20 27 21 22 | 7 17 8 12 44 5 19 9 6 22 4 | 25 32 26 32 39 25 30 29 29 23 26 23 | 7 26 9 11 48 4 23 12 9 15 5 | 8 28 16 14 40 12 22 13 10 13 10 X24 | 14 20 10 17 59 10 --- 11 20 --- 7 | 16 18 18 22 320 18 --- 12 20 --- 13 X25 | 6 14 7 10 --- 5 --- 8 8 15 3 | 10 21 19 16 --- 15 --- 13 14 19 13 26E | 12 21 9 15 30 5 13 14 10 31 5 | 52 53 48 49 69 48 51 51 48 58 49 27 | 10 19 9 12 43 7 12 10 9 16 4 | 10 24 17 17 27 14 17 17 17 21 14 28 | 8 19 7 12 41 6 20 9 12 23 4 | 14 31 18 20 41 19 29 19 17 25 17 29E | 6 13 10 12 26 5 16 9 11 16 4 | 14 21 17 21 30 15 19 14 18 17 15 30 | 5 12 5 8 21 4 8 12 6 21 3 | 24 27 25 24 32 22 26 27 22 24 23 31 | 5 18 8 11 44 5 20 13 12 19 4 | 14 26 17 18 39 15 24 14 16 14 14 32 | 6 14 7 13 25 3 17 8 9 16 4 | 22 29 29 29 31 24 24 23 21 24 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 8 12 33 5 18 12 10 26 |T 23 32 26 27 49 24 30 25 25 27 23 WRMS | 7 19 8 12 34 5 18 12 8 21 |NE 17 27 21 21 47 19 25 19 19 21 18 MEDI | 6 19 8 12 30 5 19 12 9 20 |MD 18 28 22 22 35 20 26 20 20 23 19 Table 3.1549.1 GPS week: 1549 Day: 1 MJD: 55088.000 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 | 20 --- --- 18 --- 15 --- 13 16 --- 10 | 18 --- --- 27 --- 21 --- 13 19 --- 16 2 | 7 22 6 10 42 6 18 19 6 21 5 | 15 29 18 18 44 16 25 20 18 20 17 3 | 10 15 7 12 20 5 14 11 6 24 4 | 20 21 17 23 16 16 19 21 22 17 16 4 | 6 15 7 8 34 4 9 9 7 24 3 | 13 25 16 17 28 14 21 13 18 28 14 5 | 6 20 8 10 25 7 19 17 10 30 5 | 25 23 20 23 25 18 25 25 25 21 21 6 | 21 18 11 12 27 5 16 11 8 28 5 | 85 101 100 94 109 94 99 90 95 84 91 7 | 8 21 7 12 33 4 19 7 7 13 4 | 17 31 21 24 39 19 28 18 17 16 19 8 | 7 13 8 7 23 3 10 9 9 16 3 | 10 21 15 12 27 11 18 10 14 16 11 9 | 7 20 5 8 32 6 11 8 8 16 3 | 10 25 13 12 29 11 16 14 17 18 11 10 | 5 14 9 7 23 6 11 10 9 18 3 | 16 17 20 18 24 18 16 16 20 16 16 11 | 6 17 10 11 32 5 15 12 6 19 4 | 11 28 16 11 45 12 23 15 12 12 10 12 | 7 17 11 11 27 5 18 8 7 31 4 | 22 32 23 23 39 22 32 25 27 31 23 13E | 7 25 8 11 36 4 21 9 7 13 4 | 108 105 106 109 112 105 104 105 104 105 105 14 | 6 16 10 8 23 6 20 8 6 14 4 | 14 20 18 15 25 15 22 13 20 14 14 15 | 13 27 8 9 25 6 24 16 15 10 5 | 16 29 20 21 27 19 26 21 28 19 19 16 | 8 20 11 13 32 5 24 12 10 28 5 | 11 24 18 13 34 12 27 15 13 17 11 17E | 7 23 9 15 29 5 23 7 10 13 4 | 29 42 33 36 38 32 36 33 33 35 32 18 | 8 18 8 14 30 4 21 10 10 19 4 | 13 27 21 22 35 15 28 17 19 12 16 19E | 7 27 9 12 37 5 20 10 6 23 5 | 15 34 18 17 30 13 25 15 17 23 16 20 | 8 19 9 13 55 3 20 7 7 19 4 | 16 25 22 23 28 19 25 16 19 18 17 21 | 8 21 7 11 29 5 28 7 11 19 5 | 16 33 21 17 44 18 32 17 19 22 17 22 | 9 17 9 10 46 3 21 8 6 20 4 | 19 31 24 23 37 21 29 21 23 19 20 23 | 7 26 8 12 45 4 23 8 5 16 4 | 9 28 16 14 40 12 21 14 11 14 11 X24 | 11 22 10 17 --- 18 --- 13 16 --- 6 | 14 17 23 19 --- 17 --- 13 29 --- 15 25 | 7 13 9 8 --- 4 9 6 5 15 3 | 10 21 17 15 --- 12 22 10 10 16 11 26E | 17 20 12 10 30 6 11 15 10 30 5 | 47 45 41 39 55 42 45 38 42 50 39 27 | 9 25 6 10 36 7 13 7 9 13 4 | 12 28 11 11 24 11 17 13 19 16 11 28 | 9 21 8 10 41 6 20 9 10 22 4 | 14 32 21 17 35 17 29 21 17 22 17 29E | 6 14 7 16 21 6 20 7 9 15 4 | 15 19 16 20 31 16 20 18 20 18 15 30 | 7 13 6 7 21 5 10 8 6 17 3 | 16 23 21 14 28 14 20 18 15 18 16 31 | 8 21 12 12 31 3 20 9 9 17 4 | 14 27 17 15 45 13 25 13 13 16 13 32 | 6 17 11 9 27 2 14 6 7 13 3 | 18 21 18 20 28 16 17 18 18 17 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 20 9 11 32 5 18 10 8 20 |T 21 31 25 24 38 22 29 22 24 25 21 WRMS | 8 20 9 11 33 5 18 9 6 19 |NE 15 25 18 18 32 15 23 16 18 17 15 MEDI | 7 20 8 11 30 5 19 9 8 18 |MD 15 27 20 18 34 16 25 17 19 18 16 Table 3.1549.2 GPS week: 1549 Day: 2 MJD: 55089.000 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 | 20 --- --- 17 --- 16 --- 13 23 --- 11 | 13 --- --- 29 --- 23 --- 18 29 --- 17 2 | 8 21 7 14 42 9 20 17 6 22 5 | 20 32 26 23 45 24 30 22 22 23 21 3 | 8 16 9 9 24 4 14 7 4 23 3 | 20 23 19 21 19 19 19 24 21 21 19 4 | 7 15 7 8 30 5 10 8 6 25 3 | 13 22 15 16 25 15 22 12 14 27 13 5 | 6 23 9 9 33 4 20 16 11 33 5 | 32 35 27 33 32 29 32 34 35 30 30 6 | 8 19 11 9 17 6 16 7 6 28 4 | 46 48 47 51 47 47 50 46 46 31 45 7 | 8 20 6 15 29 3 18 5 9 14 4 | 17 30 21 22 37 19 28 15 15 18 17 8 | 8 15 7 8 28 4 10 6 8 13 3 | 14 26 20 14 27 16 23 15 15 21 15 9 | 8 20 6 8 34 5 12 10 8 12 3 | 14 29 17 22 27 19 25 20 24 22 19 10 | 5 18 12 5 31 4 12 9 8 20 4 | 20 25 21 20 15 21 21 21 22 18 19 11 | 6 17 7 14 35 3 13 8 5 17 3 | 11 28 21 19 46 16 23 16 16 11 15 12 | 7 19 10 13 34 5 19 8 6 31 4 | 23 39 23 32 38 27 37 29 32 28 26 13 | 5 23 6 9 30 5 17 7 9 12 3 | 74 77 76 73 83 75 76 76 72 75 74 14 | 5 15 9 6 30 5 19 7 6 14 3 | 14 21 15 13 28 14 24 13 16 14 13 15 | 12 25 11 8 38 4 24 21 8 13 5 | 15 31 19 20 30 19 30 20 21 19 17 16 | 8 23 9 16 29 5 26 12 10 27 5 | 12 27 18 18 34 13 29 15 16 17 13 17E | 9 21 8 14 28 5 21 10 6 11 4 | 18 31 22 25 27 21 28 24 18 21 20 18 | 6 21 8 14 29 4 20 8 5 22 4 | 15 33 20 21 35 19 30 18 18 14 18 19E | 8 24 10 17 36 4 20 9 7 22 5 | 17 31 18 25 34 17 25 16 17 26 17 20 | 8 21 8 12 59 4 21 7 8 22 4 | 16 29 25 26 37 20 26 17 17 19 18 21 | 7 22 10 11 29 5 23 6 6 19 4 | 17 35 24 22 38 21 35 19 22 23 21 22 | 8 19 7 10 36 5 19 11 5 20 4 | 21 34 26 24 36 24 32 25 20 22 22 23 | 8 29 10 11 39 3 23 8 8 16 5 | 9 29 18 16 45 13 23 13 13 11 12 X24 | 12 22 12 15 36 12 --- 14 16 --- 6 | 10 27 23 25 277 16 --- 13 31 --- 17 25 | 7 15 6 10 --- 3 12 5 7 15 3 | 14 22 17 13 --- 16 22 15 13 19 13 26 | 12 22 10 12 27 5 13 11 9 30 5 | 59 67 63 63 74 61 65 64 61 66 61 27 | 8 20 6 9 36 3 13 11 7 10 3 | 14 28 15 20 25 19 25 18 22 20 17 28 | 8 19 7 9 41 5 18 8 7 21 4 | 19 31 23 20 37 21 32 18 20 25 20 29E | 6 19 9 25 24 5 21 7 10 14 5 | 20 29 17 38 32 20 25 22 20 22 19 30 | 6 12 7 8 26 4 9 9 5 18 3 | 19 28 24 26 27 21 27 26 25 18 22 31 | 5 24 10 13 42 4 19 9 9 17 4 | 15 28 14 21 41 15 25 14 19 15 15 32 | 9 14 9 10 33 3 18 10 8 15 4 | 22 25 23 23 28 20 25 23 18 20 19 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 20 9 12 34 5 18 10 7 20 |T 20 32 24 26 44 23 30 23 24 23 22 WRMS | 7 20 9 12 35 5 18 9 5 21 |NE 16 28 20 21 43 19 27 19 20 19 18 MEDI | 8 20 9 10 31 4 18 8 7 18 |MD 17 29 21 22 34 19 26 18 20 21 18 Table 3.1549.3 GPS week: 1549 Day: 3 MJD: 55090.000 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 | 21 --- --- 16 --- 21 --- 12 20 --- 10 | 19 --- --- 33 --- 28 --- 24 31 --- 22 2 | 9 20 10 7 47 8 22 12 10 19 4 | 21 32 24 23 52 25 31 23 28 26 23 3 | 8 14 10 7 19 4 16 5 9 27 4 | 19 18 20 20 18 17 20 21 20 20 17 4 | 9 14 7 7 29 5 11 5 7 22 3 | 14 22 18 17 32 14 18 15 13 26 14 5 | 6 22 8 10 35 8 20 10 8 32 5 | 20 26 23 26 32 19 23 22 27 21 21 6 | 7 16 10 7 23 4 18 6 10 33 4 | 40 45 44 41 42 41 46 42 39 44 41 7 | 9 20 12 13 32 5 19 7 6 14 4 | 21 33 27 27 42 24 29 24 20 22 23 8 | 8 16 7 9 27 3 12 7 8 12 3 | 15 28 23 19 24 19 22 19 18 24 18 9 | 7 16 9 7 34 7 15 7 7 11 3 | 19 30 26 25 34 23 24 21 23 21 21 10 | 8 16 9 8 36 6 10 9 8 20 3 | 18 28 28 26 19 22 19 21 27 19 23 11 | 6 14 6 12 38 4 15 7 5 16 3 | 20 31 26 22 54 22 27 22 19 18 21 12 | 11 17 10 9 32 7 18 10 9 31 5 | 28 39 31 32 42 31 35 35 32 34 30 13 | 9 20 6 9 27 5 22 6 6 12 4 | 48 52 56 52 57 51 50 52 51 50 50 14 | 8 16 9 6 38 5 21 6 12 13 4 | 19 26 26 19 37 22 26 23 27 21 21 15 | 13 22 14 11 38 5 26 13 9 11 5 | 19 32 34 28 30 25 31 26 30 25 25 16 | 7 21 10 14 35 5 24 11 12 28 5 | 20 30 27 19 35 20 33 23 23 25 21 17E | 10 20 7 10 23 4 18 8 8 10 4 | 51 52 48 53 57 51 51 51 49 50 50 18 | 6 21 8 11 22 6 23 7 7 18 4 | 15 30 24 24 33 21 29 21 20 16 20 19E | 8 24 11 12 34 4 23 8 5 21 4 | 18 29 22 20 40 19 28 19 19 27 18 20 | 6 18 8 15 64 5 21 5 6 17 4 | 23 30 30 28 41 25 26 21 26 19 23 21 | 8 25 9 14 33 6 27 7 8 15 5 | 24 42 32 24 37 30 41 29 28 30 27 22 | 9 19 7 8 28 4 21 14 6 18 4 | 20 31 25 26 36 24 30 30 26 25 24 23 | 8 25 8 12 34 3 23 6 7 16 4 | 12 27 20 12 45 16 23 14 13 15 14 X24 | 13 16 15 27 53 12 --- 10 27 --- 8 | 25 26 26 38 362 27 --- 22 43 --- 26 25 | 10 13 8 9 --- 2 15 5 4 13 3 | 14 22 21 15 --- 19 24 16 13 20 16 26 | 11 17 10 11 36 4 13 12 11 28 5 | 37 40 40 39 56 38 36 41 38 47 37 27 | 7 19 7 9 42 5 16 7 5 9 3 | 16 30 23 22 35 21 23 18 21 19 19 28 | 7 21 6 8 42 5 21 8 9 21 4 | 20 34 25 23 43 23 33 25 23 23 22 29E | 10 20 10 14 25 4 20 9 10 16 4 | 29 33 27 30 37 26 27 28 24 27 25 30 | 9 12 7 7 26 5 10 6 6 18 3 | 22 29 28 28 28 25 25 29 27 22 25 31 | 5 30 9 12 39 5 22 7 10 17 5 | 17 34 24 23 47 21 30 20 20 23 19 32 | 7 13 8 10 29 4 18 4 6 12 3 | 15 18 20 21 24 17 16 15 20 15 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 9 10 34 5 19 8 8 19 |T 22 31 28 26 49 25 29 25 26 25 24 WRMS | 8 19 9 10 36 5 19 7 6 21 |NE 19 29 25 24 50 22 26 22 24 21 21 MEDI | 8 19 9 10 34 5 19 7 8 17 |MD 20 30 26 24 37 23 27 22 24 23 22 Table 3.1549.4 GPS week: 1549 Day: 4 MJD: 55091.000 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 --- --- 19 --- 26 --- 18 23 --- 11 | 19 --- --- 28 --- 33 --- 20 31 --- 17 2 | 8 20 10 7 46 5 17 7 7 21 4 | 19 27 22 17 49 18 26 18 21 22 18 3 | 7 16 8 10 18 4 12 8 8 21 4 | 22 19 16 23 18 18 15 22 22 14 17 4 | 7 15 9 6 25 4 11 6 9 23 3 | 15 21 16 16 24 12 19 15 14 24 12 5 | 8 21 9 12 34 5 19 11 8 31 5 | 25 26 26 28 26 21 24 24 27 22 23 6 | 7 19 7 8 24 4 15 9 8 23 4 | 35 40 39 37 40 35 39 35 36 32 36 7 | 8 20 11 9 37 2 17 6 9 13 4 | 16 27 23 19 36 16 28 14 15 14 15 8 | 8 12 7 7 33 3 11 7 8 10 3 | 19 26 20 22 26 21 26 21 17 25 19 9 | 8 23 10 7 47 5 15 12 7 11 4 | 17 23 20 20 27 16 23 18 17 18 15 10 | 5 15 8 7 30 4 14 9 10 20 3 | 15 19 18 18 20 16 17 17 19 13 14 11 | 9 16 8 11 34 2 14 6 6 17 3 | 15 30 24 17 49 17 26 17 18 10 17 12 | 12 17 9 8 29 6 17 12 7 33 5 | 19 27 18 21 37 17 28 20 19 20 16 13 | 9 19 7 6 54 4 20 7 11 10 4 | 29 36 34 30 59 31 37 32 30 32 30 14 | 8 19 9 7 33 4 18 11 5 15 4 | 11 23 16 13 37 12 19 18 15 14 13 15 | 13 24 12 10 40 6 26 18 9 12 5 | 13 28 19 20 28 15 26 24 21 20 16 16 | 9 24 17 13 21 4 24 7 11 26 5 | 17 30 18 17 34 17 30 18 22 17 17 17 | 7 21 8 13 24 4 23 9 8 11 4 | 31 34 32 35 37 29 33 34 30 36 30 18 | 7 17 6 12 25 4 19 8 8 22 4 | 12 24 20 18 33 13 26 13 19 12 14 19E | 8 23 11 13 21 5 21 8 9 24 5 | 20 33 24 25 31 23 30 20 25 27 21 20 | 6 15 10 10 71 4 18 7 10 20 4 | 17 25 26 21 46 19 24 17 23 12 18 21 | 8 21 9 11 33 10 24 12 6 19 4 | 18 33 23 17 41 20 33 22 22 23 20 22 | 9 17 7 8 37 4 18 16 8 19 4 | 15 25 20 20 33 15 25 26 20 19 17 X23 | 7 26 10 8 128 4 --- 10 6 15 4 | 13 28 24 12 95 12 --- 14 17 14 13 X24 | 17 20 16 22 42 15 --- 11 14 --- 7 | 14 25 21 31 573 20 --- 10 29 --- 16 25 | 8 17 7 7 --- 4 12 8 9 10 3 | 17 28 22 16 --- 17 23 16 17 19 16 26 | 12 18 8 7 31 5 12 13 9 27 4 | 26 30 24 26 48 23 30 26 24 38 24 27 | 8 23 11 7 56 4 16 12 6 11 4 | 15 27 19 23 35 16 24 17 20 18 17 28 | 6 21 8 9 51 6 20 8 10 24 4 | 16 30 23 22 41 19 32 20 18 23 18 29 | 9 19 12 11 21 6 19 7 8 17 4 | 28 33 34 38 45 31 32 34 33 33 31 30 | 9 16 7 7 18 5 9 10 8 18 3 | 17 21 20 21 30 16 21 21 21 13 16 31 | 7 27 14 11 43 3 24 8 9 14 5 | 17 29 18 18 50 14 27 15 17 13 14 32 | 8 16 9 7 37 3 15 4 8 15 3 | 13 15 17 18 27 13 13 15 16 14 13 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 9 37 5 18 10 8 19 |T 18 27 22 22 55 19 26 20 21 20 18 WRMS | 8 19 9 9 40 4 18 9 7 20 |NE 16 25 20 20 60 17 24 18 20 16 16 MEDI | 8 19 9 8 33 4 17 8 8 18 |MD 17 27 21 20 36 17 26 18 20 19 17 Table 3.1549.5 GPS week: 1549 Day: 5 MJD: 55092.000 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 | 21 --- --- 13 --- 35 --- 21 37 --- 14 | 15 --- --- 30 --- 42 --- 19 44 --- 20 2 | 6 18 10 10 39 6 19 8 10 25 4 | 16 25 17 15 39 18 27 20 24 25 17 3 | 8 16 9 11 19 4 12 8 9 21 4 | 20 16 18 18 12 17 17 22 24 13 16 4M | 7 14 8 9 32 4 11 9 11 22 4 | 17 23 19 16 31 17 27 21 20 32 17 5 | 6 21 10 14 38 5 19 9 12 33 5 | 24 30 23 26 25 24 25 25 31 22 23 6 | 8 17 8 12 23 3 14 8 7 24 4 | 33 39 37 37 39 35 40 35 35 33 34 7 | 9 21 12 13 31 3 18 7 9 14 4 | 16 30 23 21 38 20 28 17 16 16 17 8 | 7 13 8 12 25 5 10 8 7 10 3 | 13 21 18 17 25 17 22 15 18 19 15 9 | 10 18 10 8 40 3 13 9 9 10 4 | 17 25 22 20 25 19 21 19 22 18 18 10 | 7 14 10 9 36 6 10 8 9 21 4 | 15 24 21 18 16 20 18 18 23 17 17 11 | 8 16 8 11 33 5 14 7 8 18 4 | 13 31 26 19 48 18 26 19 20 14 18 12 | 10 17 10 9 29 5 20 12 11 36 5 | 20 30 22 22 34 20 30 26 25 28 20 13 | 6 15 6 9 46 6 16 10 8 10 3 | 34 40 37 36 55 37 41 37 37 37 35 14 | 6 22 7 8 32 5 17 13 7 16 4 | 9 26 16 12 36 12 21 18 16 14 11 15 | 12 20 12 10 40 4 23 19 11 17 5 | 16 27 19 22 28 17 27 26 18 24 17 16 | 8 21 14 14 29 4 23 12 11 25 5 | 17 28 20 18 34 16 31 18 23 17 16 17 | 12 20 10 11 40 4 18 13 7 34 5 | 74 73 74 73 93 70 76 74 74 80 73 18 | 5 18 9 10 29 3 19 8 7 24 4 | 11 25 19 13 33 15 28 14 15 14 13 19E | 7 25 8 13 17 4 18 9 9 20 4 | 20 30 23 20 25 19 26 19 22 23 20 20 | 8 20 10 10 75 5 16 8 9 20 4 | 15 27 22 18 54 17 25 18 21 11 16 21 | 7 19 13 10 29 5 22 11 9 18 5 | 18 32 26 21 39 20 32 22 21 20 20 22 | 8 16 11 8 47 5 16 19 9 19 5 | 15 25 17 14 40 16 26 25 18 21 14 X23 | 7 --- 12 --- --- 14 --- --- --- --- 9 | 7 --- 37 --- --- 16 --- --- --- --- 8 X24 | 12 21 13 25 2883 10 --- 15 16 --- 7 | 17 28 24 35 590 23 --- 15 36 --- 20 25 | 6 13 9 12 --- 5 12 11 9 11 3 | 19 26 24 17 --- 20 26 21 20 22 19 26 | 10 17 10 10 35 4 12 12 9 27 4 | 29 34 29 28 45 29 35 30 29 40 28 27 | 10 18 12 6 42 3 15 9 9 10 4 | 9 22 19 15 23 11 18 13 17 12 11 28 | 8 20 7 12 58 6 18 7 7 25 4 | 15 27 22 23 38 17 27 18 17 23 15 29 | 8 22 10 10 29 5 21 12 9 17 4 | 19 28 21 21 36 19 26 18 25 19 18 30 | 6 14 8 7 24 5 11 9 8 20 3 | 16 19 21 21 33 19 22 21 24 18 18 31 | 6 24 10 13 31 5 21 10 9 13 4 | 13 26 18 18 37 14 25 21 17 14 14 32 | 8 15 16 11 44 6 14 7 8 14 4 | 11 16 20 18 32 13 18 13 16 11 11 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 10 11 37 5 17 10 9 21 |T 18 28 24 22 55 21 27 22 24 22 19 WRMS | 8 18 10 11 39 5 17 9 8 20 |NE 15 25 21 19 58 18 24 19 21 17 16 MEDI | 8 18 10 10 33 5 16 9 9 20 |MD 16 27 22 20 36 18 26 19 22 19 17 Table 3.1549.6 GPS week: 1549 Day: 6 MJD: 55093.000 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 --- --- 10 --- 22 --- 19 22 --- 10 | 22 --- --- 33 --- 37 --- 27 36 --- 25 2 | 9 21 9 9 45 6 19 11 9 25 5 | 23 32 23 21 57 23 31 26 23 30 23 3 | 9 15 8 10 22 4 12 15 8 21 4 | 20 17 21 23 19 19 20 25 23 22 18 4 | 8 13 6 9 32 4 10 10 9 22 4 | 14 25 18 19 31 14 22 15 17 29 15 5 | 7 17 9 11 49 5 19 13 7 30 5 | 25 26 21 30 35 22 24 30 26 25 23 6 | 10 17 9 8 25 3 13 12 8 21 4 | 33 36 33 34 39 32 37 33 33 28 31 7 | 9 23 12 11 26 3 18 9 13 14 5 | 13 29 22 19 36 16 26 17 17 17 16 8 | 7 11 6 9 23 5 10 11 9 13 3 | 15 21 19 20 23 17 20 21 18 22 16 9 | 9 16 7 9 31 6 13 13 6 12 3 | 21 27 25 31 27 23 25 28 25 27 24 10 | 6 13 7 6 44 5 10 9 6 20 3 | 18 24 19 21 21 20 18 24 23 22 19 11 | 8 14 8 7 37 5 16 9 9 18 4 | 18 25 20 17 48 17 26 21 19 15 17 12 | 13 17 9 10 33 6 17 14 11 39 5 | 22 33 26 31 38 25 34 30 31 36 25 13 | 7 15 6 8 42 5 17 13 11 11 4 | 41 46 46 40 58 43 43 44 41 43 42 14 | 8 17 8 8 24 5 20 12 6 15 4 | 13 25 17 11 34 13 22 20 17 16 13 15 | 10 20 10 10 24 5 28 19 10 15 5 | 20 35 29 31 31 27 38 30 29 31 27 16 | 9 17 12 8 25 5 19 10 9 26 4 | 21 31 23 16 36 22 36 22 26 26 21 17 | 7 22 10 10 41 6 19 8 11 12 4 | 50 56 52 53 63 51 52 50 49 46 50 18 | 7 19 7 11 25 4 21 11 10 25 5 | 14 28 24 23 32 18 28 20 20 18 18 19 | 12 28 8 9 34 5 19 9 8 20 5 | 35 39 30 26 43 30 37 32 36 42 31 20 | 9 17 6 10 94 4 16 9 11 19 4 | 18 24 24 25 63 21 24 23 20 17 19 21 | 9 19 9 12 29 4 24 10 10 19 5 | 22 36 26 20 39 22 40 27 29 26 24 22 | 10 17 4 9 30 5 20 17 9 20 4 | 20 31 24 25 33 23 28 29 25 24 22 X23 | 7 --- 6 8 83 4 --- 12 9 15 4 | 9 --- 6 5 12 8 --- 7 7 8 8 X24 | 18 17 11 20 --- 14 --- 10 21 --- 7 | 17 23 25 30 --- 22 --- 23 39 --- 24 25 | 7 11 5 5 --- 4 10 15 11 12 3 | 16 22 21 19 --- 19 22 21 19 21 18 26 | 11 14 6 12 28 4 10 11 9 28 4 | 31 37 31 33 41 32 34 33 32 43 31 27 | 9 15 8 10 34 5 15 10 5 10 3 | 14 23 20 24 26 18 22 23 18 22 18 28 | 7 17 6 11 74 5 20 8 10 28 4 | 18 30 22 25 53 20 32 20 19 30 19 29 | 8 21 10 9 28 6 18 13 11 18 5 | 21 30 18 24 26 21 23 24 23 21 20 30 | 11 11 8 7 25 4 8 11 8 22 4 | 24 28 27 31 38 25 29 32 32 23 26 31 | 8 20 10 7 33 5 18 12 6 14 4 | 16 25 15 16 41 14 25 22 19 17 15 32 | 8 13 6 6 43 4 13 8 6 13 3 | 12 13 16 15 38 12 18 13 13 13 11 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 17 8 9 39 5 17 12 9 20 |T 21 29 23 24 37 22 28 25 25 25 22 WRMS | 9 17 8 9 35 5 17 11 6 20 |NE 18 26 21 22 35 20 26 23 22 22 19 MEDI | 9 17 8 9 32 5 17 11 9 19 |MD 20 28 23 24 36 21 26 24 23 23 20 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 4.1549 GPS week: 1549 MJD: 55087.0-55093.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3063 |U 6 8 20 |U 6 9 26 |U 9 10 21 | emr | emr 2946 | 9 9 24 |U 7 9 25 | 9 9 26 | esa | esa 2962 | 7 8 23 |U 6 8 25 | 9 9 21 | gfz | gfz 3045 |U 7 8 23 |U 8 9 28 | 8 9 21 | grg | grg 2838 | 8 8 24 |U 8 12 33 | 11 11 24 | igr | igr 2978 | 7 8 22 | 6 8 25 | 9 9 21 | igs | igs 2964 | 7 8 22 | 6 7 24 | 9 9 21 | jpl | jpl 2822 | 9 9 26 |U 7 7 25 |U 9 9 26 | mit | mit 3058 |U 9 11 38 |U 7 8 27 |U 10 10 23 | Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit positions and satellite clock corrections at 15 min intervals. Each line gives the daily station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. CLK - Satellite clocks used. EPO - Number of satellite clock epochs available for that day. Units: mm. Table 5.1549.0 GPS week: 1549 Day: 0 MJD: 55087.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3060 | 6 5 17 | 4 8 27 | 11 13 20 | emr | emr 2975 | 8 8 22 | 7 7 22 | 10 9 28 | esa | esa 2976 | 7 7 19 | 5 6 22 | 11 13 24 | gfz | gfz 3048 | 7 8 21 | 9 10 30 | 11 12 24 | grg | grg 2880 | 7 6 18 | 9 21 73 | ---- ---- ---- | igr | igr 3000 | 6 6 17 | 5 7 23 | 10 12 23 | igs | igs 3008 | 6 6 17 | 5 5 22 | 10 11 22 | jpl | jpl 2783 | 7 8 20 | 5 6 22 | 9 11 24 | mit | mit 3072 | 23 26 131 | 6 6 27 | 12 12 24 | Table 5.1549.1 GPS week: 1549 Day: 1 MJD: 55088.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3061 | 5 5 21 | 6 7 19 | 6 10 21 | emr | emr 2974 | 7 6 23 | 7 9 22 | 8 10 26 | esa | esa 2976 | 6 5 27 | 5 7 21 | 7 9 22 | gfz | gfz 3049 | 6 5 24 | 9 10 25 | 7 10 23 | grg | grg 2784 | 8 6 24 | 6 10 19 | 14 18 33 | igr | igr 2970 | 6 5 24 | 5 6 19 | 6 8 20 | igs | igs 2976 | 5 5 23 | 5 6 19 | 6 9 22 | jpl | jpl 2879 | 7 8 24 | 5 6 19 | 9 12 30 | mit | mit 3072 | 5 5 24 | 6 6 21 | 8 10 23 | Table 5.1549.2 GPS week: 1549 Day: 2 MJD: 55089.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3056 | 7 12 26 | 7 8 26 | 6 8 18 | emr | emr 2974 | 9 11 31 | 5 8 27 | 6 7 26 | esa | esa 2976 | 8 11 33 | 5 7 25 | 6 6 20 | gfz | gfz 3060 | 7 11 30 | 6 8 32 | 5 7 19 | grg | grg 2880 | 7 9 31 | 6 9 27 | 8 7 22 | igr | igr 3005 | 7 10 31 | 5 7 26 | 5 6 19 | igs | igs 3042 | 7 11 32 | 5 6 24 | 6 7 19 | jpl | jpl 2872 | 7 8 27 | 5 7 25 | 5 5 18 | mit | mit 3072 | 7 13 34 | 6 6 27 | 7 8 17 | Table 5.1549.3 GPS week: 1549 Day: 3 MJD: 55090.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3063 | 7 6 21 | 7 9 22 | 9 15 20 | emr | emr 2976 | 8 9 19 | 8 8 22 | 9 12 20 | esa | esa 2976 | 7 8 22 | 7 6 21 | 8 12 18 | gfz | gfz 3055 | 8 7 22 | 9 8 28 | 8 14 18 | grg | grg 2880 | 8 8 25 | 10 12 28 | 11 14 27 | igr | igr 2976 | 7 9 20 | 8 7 22 | 8 11 19 | igs | igs 3025 | 6 7 20 | 7 7 20 | 8 12 17 | jpl | jpl 2880 | 8 7 23 | 9 7 24 | 9 11 25 | mit | mit 3072 | 7 7 22 | 8 8 20 | 11 11 22 | Table 5.1549.4 GPS week: 1549 Day: 4 MJD: 55091.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3066 | 6 5 15 | 10 12 49 | 9 8 20 | emr | emr 2967 | 10 8 18 | 8 13 39 | 9 8 23 | esa | esa 2976 | 6 5 17 | 10 11 47 | 8 7 16 | gfz | gfz 3065 | 6 7 24 | 8 11 36 | 7 7 13 | grg | grg 2880 | 7 5 14 | 11 14 42 | 10 8 17 | igr | igr 2994 | 6 5 17 | 10 11 46 | 8 7 16 | igs | igs 2939 | 6 5 17 | 9 11 45 | 8 8 19 | jpl | jpl 2779 | 8 6 16 | 10 11 43 | 9 8 24 | mit | mit 3072 | 6 4 15 | 12 11 46 | 10 9 21 | Table 5.1549.5 GPS week: 1549 Day: 5 MJD: 55092.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3065 | 8 9 20 | 6 8 21 | 9 9 24 | emr | emr 2878 | 10 12 27 | 8 8 22 | 12 10 34 | esa | esa 2880 | 8 8 24 | 6 9 23 | 10 8 26 | gfz | gfz 2972 | 8 9 24 | 7 9 24 | 10 9 24 | grg | grg 2784 | 9 7 27 | 6 7 20 | ---- ---- ---- | igr | igr 2905 | 8 9 25 | 6 9 22 | 11 9 26 | igs | igs 2805 | 8 9 24 | 6 8 22 | 10 9 26 | jpl | jpl 2781 | 20 11 37 | 7 6 21 | 11 9 32 | mit | mit 2976 | 8 9 22 | 7 11 24 | 10 11 27 | Table 5.1549.6 GPS week: 1549 Day: 6 MJD: 55093.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3072 | 7 12 19 | 5 9 19 | 12 8 22 | emr | emr 2878 | 9 11 32 | 6 9 23 | 12 7 25 | esa | esa 2976 | 8 12 18 | 4 7 16 | 12 7 22 | gfz | gfz 3068 | 7 12 17 | 5 9 19 | 11 6 23 | grg | grg 2784 | 9 17 27 | 5 9 24 | 13 8 24 | igr | igr 2999 | 7 12 19 | 4 6 19 | 11 7 21 | igs | igs 2954 | 7 12 18 | 4 7 17 | 12 7 22 | jpl | jpl 2784 | 9 14 33 | 5 7 19 | 12 7 25 | mit | mit 3072 | 7 13 17 | 5 8 23 | 12 7 26 | 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 6.1549 GPS week: 1549 MJD: 55087.500-55093.500 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 -14 -9 -124 -6 | 5 12 | 20 20 126 64 7 | 2 emr uuuuu | 32 -12 286 -66 8 | 53 54 | 25 22 71 115 9 | 4 esa uuuuu | -20 -38 -76 133 6 | 20 23 | 23 20 123 122 9 | 1 gfz uuuuu | -11 31 -36 -122 -3 | -5 11 | 20 21 56 77 4 | 2 grg xxxxx | -19 -33 12 -133 -6 | 0 25 | 49 30 90 76 38 | 4 igr xxxxx | -1 32 -13 -6 9 | -8 11 | 6 28 37 50 8 | 4 irf xxxxx | -1 5 -51 -35 4 | -8 12 | 8 9 21 36 2 | 1 jpl uuuuu | 1 -15 92 -10 -1 | 16 21 | 63 26 68 119 9 | 3 mit uuuuu | 3 14 -159 -108 -1 | 8 12 | 16 16 78 80 2 | 1 ngs uuuuu | -12 -4 65 39 0 | 8 14 | 29 35 80 101 5 | 2 sio uuuuu | 72 58 14 141 12 | 29 31 | 14 25 77 51 6 | 3 Table 7.1549.0 GPS week: 1549 Day: 0 MJD: 55087.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -13 5 -68 -44 4 | 2 14 emr uuuuu | 48 13 332 -35 8 | 49 50 esa uuuuu | -2 -65 33 22 0 | 21 23 gfz uuuuu | -32 39 -57 -216 -3 | -7 14 grg xxxxx | -53 7 -122 -152 -71 | 9 16 igr xxxxx | 1 15 -21 -42 15 | -13 15 irf xxxxx | 5 21 -89 -56 4 | -9 13 jpl uuuuu | -2 23 11 199 3 | 13 20 mit uuuuu | 5 44 -286 -176 0 | 9 14 ngs uuuuu | -24 -27 75 97 -4 | 8 15 sio uuuuu | 81 105 -49 196 17 | 27 29 Table 7.1549.1 GPS week: 1549 Day: 1 MJD: 55088.500 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 -10 -55 -156 0 | 3 14 emr uuuuu | 44 -32 324 -22 4 | 48 49 esa uuuuu | 15 -24 102 166 -10 | 20 23 gfz uuuuu | -23 36 -124 -163 5 | -6 14 grg xxxxx | -58 -63 -52 -229 1 | 1 26 igr xxxxx | -4 -2 -20 -57 15 | -12 15 irf xxxxx | -16 4 -72 -98 2 | -10 13 jpl uuuuu | 99 -42 20 -66 -1 | 12 19 mit uuuuu | -26 9 -188 -253 -2 | 8 13 ngs uuuuu | -55 1 -1 180 -2 | 8 15 sio uuuuu | 49 58 63 78 14 | 26 28 Table 7.1549.2 GPS week: 1549 Day: 2 MJD: 55089.500 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 | -44 14 -149 -138 -2 | 4 13 emr uuuuu | 0 -33 257 -317 17 | 48 49 esa uuuuu | -2 -26 -30 262 8 | 18 22 gfz uuuuu | -35 37 -77 -169 -7 | -5 12 grg xxxxx | -96 -64 -50 -208 -23 | 0 26 igr xxxxx | -10 43 -7 -57 0 | -9 12 irf xxxxx | 0 9 -45 -29 5 | -10 13 jpl uuuuu | 54 10 115 -153 9 | 13 19 mit uuuuu | 8 25 -126 -95 -1 | 7 12 ngs uuuuu | -31 -30 22 51 -3 | 9 15 sio uuuuu | 89 61 78 202 17 | 26 28 Table 7.1549.3 GPS week: 1549 Day: 3 MJD: 55090.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 12 -24 -142 -230 -3 | 7 14 emr uuuuu | -4 -13 338 -78 22 | 52 54 esa uuuuu | -34 -39 -141 208 12 | 19 23 gfz uuuuu | -3 1 -30 -38 -3 | -3 11 grg xxxxx | 10 -50 21 -138 14 | -4 25 igr xxxxx | 1 18 -78 23 21 | -8 11 irf xxxxx | -3 2 -38 -10 3 | -8 13 jpl uuuuu | -28 -32 172 -35 6 | 17 23 mit uuuuu | -6 14 -68 -71 -3 | 7 13 ngs uuuuu | 28 14 -12 -87 -4 | 9 15 sio uuuuu | 64 66 109 133 13 | 28 31 Table 7.1549.4 GPS week: 1549 Day: 4 MJD: 55091.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -20 -46 154 -60 -13 | 9 13 emr uuuuu | 42 -33 352 -27 8 | 57 58 esa uuuuu | -43 -63 -209 216 7 | 21 25 gfz uuuuu | -6 6 35 -16 -5 | -2 9 grg xxxxx | 14 -40 126 -117 44 | -5 24 igr xxxxx | 10 12 42 -21 5 | -4 8 irf xxxxx | -3 -5 -45 -2 7 | -6 11 jpl uuuuu | 18 -32 154 -95 -2 | 20 23 mit uuuuu | 3 6 -94 -86 2 | 9 13 ngs uuuuu | -7 54 20 -82 4 | 9 15 sio uuuuu | 68 43 42 133 18 | 32 34 Table 7.1549.5 GPS week: 1549 Day: 5 MJD: 55092.500 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 -22 63 -95 -11 | 5 10 emr uuuuu | 61 -11 244 27 0 | 57 58 esa uuuuu | -40 -10 -230 135 19 | 19 22 gfz uuuuu | 5 61 -30 -174 -1 | -5 8 grg xxxxx | 22 -31 101 -85 24 | -2 27 igr xxxxx | -5 73 -18 56 0 | -4 8 irf xxxxx | 1 6 -36 -50 5 | -7 10 jpl uuuuu | -87 5 137 -15 -19 | 19 22 mit uuuuu | 8 1 -125 -45 -1 | 7 10 ngs uuuuu | 21 -51 186 -6 3 | 6 11 sio uuuuu | 67 50 -64 168 6 | 32 35 Table 7.1549.6 GPS week: 1549 Day: 6 MJD: 55093.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 12 -17 134 -147 -14 | 2 9 emr uuuuu | 30 22 155 -11 -5 | 58 59 esa uuuuu | -36 -37 -60 -82 3 | 21 24 gfz uuuuu | 17 37 27 -77 -5 | -6 9 grg xxxxx | 26 6 56 -3 -27 | 0 27 igr xxxxx | -2 63 12 56 7 | -3 7 irf xxxxx | 11 -6 -35 -1 2 | -7 10 jpl uuuuu | -45 -36 34 91 -6 | 16 19 mit uuuuu | 27 -2 -228 -28 -2 | 6 9 ngs uuuuu | -18 9 163 116 8 | 5 9 sio uuuuu | 87 23 -84 78 2 | 34 36