From igs.acc at noaa.gov Thu Dec 16 06:43:41 2010 From: igs.acc at noaa.gov (Jim Ray) Date: Thu, 16 Dec 2010 14:43:41 +0000 Subject: [IGSREPORT-19263] Wk 1612 IGS Final Orbits Message-ID: <4d0a259d.6WZ7HTMsk4HTrLLG%igs.acc@noaa.gov> Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1612 (Nov 28, 2010 - Dec 04, 2010) Contacts: J. Ray (jim.ray at noaa.gov), J. Griffiths (jake.griffiths at 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 (as part of the separate SINEX combination since GPS week 1051; weighted according to the orbit combination before that time). 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: igs1612[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1612[0-6].clk IGS GPS satellite and station clocks in clock RINEX format. igs1612[0-6].cls IGS GPS clock combination summary report. igs16127.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs16127.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 1582, a new solution from CNES/GRGS (GRG) is included with weight except for the clock and LOD combinations. 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 | DAV1 DGAR 0 | EMR | 10 32 10 32 WTZR WTZR 0 | ESA | 22 22 KOKB SUTH UNSA 0 | GFZ | 5 10 18 20 22 CAS1 DGAR KERG OHI2 0 | GRG | DGAR 0 | JPL | 32 0 | MIT | 10 32 10 19 32 MAW1 IRKJ MAW1 1 | COD | 10 32 10 DGAR GLSV XMIS 1 | EMR | WTZR WTZR 1 | ESA | 10 22 32 10 22 32 AUCK SUTH UNSA 1 | GFZ | 5 10 18 20 22 DGAR 1 | GRG | DGAR 1 | JPL | 22 32 1 | MIT | GUAT 2 | COD | 10 WROC DGAR SOFI WROC WTZR 2 | EMR | 32 10 32 WTZR 2 | ESA | 10 22 22 WTZR CAS1 KERG SUTH UNSA 2 | GFZ | 5 10 18 20 22 32 ARTU DGAR IRKT MDVJ NYA1 PETS 2 | GRG | ADIS DGAR 2 | JPL | 22 32 2 | MIT | 32 10 32 BOR1 KOUR 3 | ALL | 1 1 3 | COD | BRMU BRMU DGAR 3 | EMR | 10 10 32 HARB WTZR HARB WTZR 3 | ESA | CAS1 MATE SUTH 3 | GFZ | 5 10 18 20 22 32 CAS1 MDVJ NURK RAMO 3 | GRG | ADIS AMC2 BRMU DGAR 3 | JPL | 22 32 POTS WILL 3 | MIT | 10 10 32 ALGO ALGO KELY 4 | COD | 10 10 DGAR 4 | EMR | 32 32 WTZR HARB WTZR 4 | ESA | 10 10 SUTH 4 | GFZ | 1 5 10 18 22 28 32 CRO1 DGAR MDVJ RIOP UNSA YKRO 4 | GRG | DGAR FAA1 4 | JPL | 22 32 4 | MIT | 32 32 5 | ALL | 1 5 | EMR | 10 21 32 10 21 32 WTZR WTZR 5 | ESA | SUTH UNSA 5 | GFZ | 5 10 18 20 22 28 30 32 BRFT DGAR KERG MDVJ RAMO 5 | GRG | ADIS DGAR FAA1 POTS 5 | JPL | 32 5 | MIT | 10 21 32 10 21 32 MAW1 6 | ALL | 1 6 | COD | 10 DGAR 6 | EMR | 32 32 WTZR WTZR 6 | ESA | 10 SUTH UNSA 6 | GFZ | 5 10 18 20 22 ARTU DGAR MDVJ RAMO 6 | GRG | ADIS DGAR 6 | JPL | 22 32 6 | MIT | 32 32 5. 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. 6. Small rotations were applied to all the AC orbit and ERP values in order to align them to the IGS05 frame. These rotations were estimated in the IGS SINEX combination process, performed by the IGS Reference Frame Coordinator at the Institut Geographique National (IGN), and are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX frame. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .6 1.5 .4 -1 -16 -25 .09 EMR | -1.4 5.0 -.6 34 13 68 .40 ESA | 1.1 6.7 -5.6 116 -7 -55 -.03 GFZ | .2 1.7 -.3 23 -29 -30 .37 GRG | -.9 7.5 -5.1 52 70 -87 .60 JPL | -2.2 5.3 12.4 70 -30 2 .50 MIT | -.6 4.6 -9.1 10 -13 -40 .29 NGS | 1.8 3.4 -5.7 59 -77 3 .09 SIO | 2.2 4.1 -8.5 51 -72 -1 .54 7. 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. 8. 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 IGN. 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. 9. 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 1.1612.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1612.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 2.1612.[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 3.1612.[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 5.1612.0-6). 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 1612 summary. (Nov 28, 2010 - Dec 04, 2010) Table 1.1612.a GPS week: 1612 MJD: 55528.000-55534.000 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 233| 0 0 3 78 -7 -12 -.22 8 8 | -212 -150 16 73 | 0 0 1 11 20 19 .01 | 259 329 emr 90| -1 0 4 16 -42 15 .39 19 19 | -1387 -429 14 94 | 1 1 1 16 19 14 .02 | 1451 1448 esa 148| 0 0 -1 -84 -79 -49 .23 9 9 | 373 66 13 114 | 1 0 1 34 30 20 .03 | 662 1870 gfz 190| 0 0 -2 19 0 -1 -.21 10 9 | 83 25 19 97 | 0 0 1 50 68 12 .03 | 291 518 grg 133| 0 2 -8 -22 -199 -31 .67 16 15 | 72 -54 47 238 | 1 0 2 30 24 18 .04 | 281 596 igr n/a| 0 0 0 72 7 25 -.04 5 5 | 8472 -580 15 79 | 0 0 0 21 19 16 .02 | 1725 1479 jpl 122| 0 0 8 -67 41 -24 .51 17 16 | 1376 -413 16 99 | 0 1 1 14 19 19 .05 | 1433 1517 mit 260| 1 0 -4 79 3 29 -.38 15 13 | -32 59 20 131 | 1 1 1 35 20 10 .02 | 268 532 ngs 214| 0 0 0 -28 137 46 -.25 10 8 | -169 -214 2267 3655 | 0 0 1 29 36 15 .03 | 373 497 sio 259| 0 2 5 -18 91 5 -.08 19 18 | --- --- --- --- | 0 1 0 35 26 7 .03 | --- --- Table 1.1612.b GPS week : 1612 MJD: 55528.000-55534.000 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 | 46 0 31 23 22 23 12 | 2 | 7 6 6 6 6 6 6 | 3 | 5 4 4 4 4 4 4 | 4 | 5 5 4 4 4 4 3 | 5 | 5 5 5 4 5 4 4 | 6 | 4 4 4 3 3 4 4 | 7 | 5 5 5 5 5 5 4 | 8 | 5 5 5 5 4 4 4 | 9 | 5 5 4 5 4 4 4 | 10 | 8 7 6 5 5 4 5 | 11 | 4 4 4 4 4 4 4 | 12 | 5 6 5 5 6 5 5 | 13 | 5 5 5 5 5 4 5 | 14 | 4 5 4 4 4 5 4 | 15 | 5 5 5 5 5 5 5 | 16 | 5 5 5 5 5 5 5 | 17 | 5 5 5 5 5 5 5 | 18 | 5 5 5 5 5 4 4 | 19 | 4 4 4 4 4 5 5 | 20 | 5 4 4 5 4 4 4 | 21 | 5 5 4 5 4 4 4 | 22 | 5 5 4 4 5 4 4 | 23 | 5 5 5 5 5 5 5 | 24 | 3 3 3 3 3 4 4 | 25 | 5 5 5 5 5 5 5 | 26 | 4 4 3 3 4 4 4 | 27 | 5 5 4 4 4 4 4 | 28 | 5 4 4 4 4 4 4 | 29 | 5 5 5 5 5 4 4 | 30 | 5 4 4 4 5 5 5 | 31 | 4 5 5 5 4 5 5 | 32 | 6 6 6 6 6 6 7 | 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 2.1612.0 GPS week: 1612 Day: 0 MJD: 55528.000 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 233| -1 0 3 84 -37 -30 -.23 9 9 | -166 -289 16 76 | -13 63 | emr 90| -3 0 3 23 -55 32 .43 18 18 | -133 -220 15 98 | -2 -6 | esa 148| 2 0 0 -45 -105 -40 .23 10 10 | 262 637 12 111 | -28 79 | gfz 190| 0 -1 -2 -44 54 -1 -.22 10 8 | 387 -480 20 91 | -74 63 | grg 133| 1 2 -10 13 -239 -50 .65 17 15 | 212 -643 58 263 | -22 106 | igr n/a| 0 0 0 112 5 17 -.03 5 5 | 9955 -159 17 89 | -68 17 | jpl 122| 0 0 6 -59 29 -29 .50 17 16 | 2611 -290 18 95 | 37 -7 | mit 260| 0 1 -2 40 23 22 -.39 19 15 | 73 -434 23 153 | 18 -42 | ngs 214| -1 1 0 12 124 53 -.25 10 8 | -53 -440 2173 3538 | -116 -18 | sio 259| 0 0 5 -47 135 7 -.14 23 18 | --- --- --- --- | 3 14 | Table 2.1612.1 GPS week: 1612 Day: 1 MJD: 55529.000 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 233| 0 0 3 93 -18 -16 -.22 9 9 | -355 282 18 77 | 26 48 | emr 90| -3 -2 6 0 -60 9 .41 19 19 | -57 997 13 99 | 2 -19 | esa 148| 1 0 0 -140 -97 -39 .30 10 10 | -120 3477 15 112 | 34 72 | gfz 190| -2 0 -4 73 33 20 -.18 11 10 | 18 143 20 97 | -48 25 | grg 133| -1 1 -8 -51 -213 -30 .62 16 14 | -332 1011 44 228 | 97 36 | igr n/a| 0 0 1 57 15 33 -.06 5 5 | 10214 854 18 69 | -43 -5 | jpl 122| 0 1 8 -82 20 0 .46 17 15 | 2706 992 16 91 | 21 8 | mit 260| 3 0 -5 121 3 21 -.41 17 14 | -435 961 21 140 | -16 -29 | ngs 214| 0 0 -2 -44 131 27 -.28 10 8 | -349 234 2186 3791 | 39 -60 | sio 259| 1 0 4 21 81 0 -.09 20 18 | --- --- --- --- | -24 16 | Table 2.1612.2 GPS week: 1612 Day: 2 MJD: 55530.000 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 233| 0 0 0 71 9 15 -.22 8 7 | -649 238 15 78 | 5 20 | emr 90| -2 -2 2 23 -35 1 .36 19 19 | -81 -1942 13 113 | -17 -8 | esa 148| 1 0 0 -93 -62 -37 .22 8 8 | 1010 259 11 109 | 10 71 | gfz 190| 0 0 -2 69 -25 -1 -.22 10 8 | -273 299 18 100 | -27 32 | grg 133| 1 2 -7 -33 -197 -31 .64 15 14 | 102 -504 38 212 | 82 31 | igr n/a| 0 0 1 61 5 7 -.04 6 5 | 9990 -2168 15 83 | -32 23 | jpl 122| 0 0 7 -61 57 -12 .45 17 16 | 2630 -1964 16 104 | -17 10 | mit 260| 2 1 -5 112 2 15 -.39 17 14 | 90 -461 23 121 | -20 -32 | ngs 214| -1 0 0 -70 129 20 -.26 9 7 | -800 459 2258 3479 | 106 15 | sio 259| 1 2 4 2 82 -2 -.08 19 16 | --- --- --- --- | -22 7 | Table 2.1612.3 GPS week: 1612 Day: 3 MJD: 55531.000 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 233| 0 -1 2 70 1 -42 -.22 8 8 | -13 -426 13 70 | 35 5 | emr 90| -3 0 4 -12 -48 31 .37 18 18 | -802 -2615 12 106 | 24 -9 | esa 148| 1 0 -2 -50 -60 -30 .19 8 8 | 615 675 12 123 | 25 53 | gfz 190| 0 -1 -1 22 13 -15 -.21 12 11 | 202 -209 20 102 | -47 19 | grg 133| 0 3 -5 -26 -173 -19 .65 15 14 | 367 -406 45 264 | 34 15 | igr n/a| 0 0 1 70 6 19 -.07 4 4 | 9091 -2908 15 81 | -28 38 | jpl 122| 2 0 8 -69 41 -2 .48 17 16 | 1808 -2698 15 117 | 36 -10 | mit 260| 0 0 -5 100 -12 32 -.40 15 13 | 250 -238 21 183 | -15 -33 | ngs 214| -1 0 0 -43 129 51 -.30 10 8 | 191 -738 2261 3556 | 47 51 | sio 259| 0 2 5 5 81 18 -.07 18 17 | --- --- --- --- | -25 3 | Table 2.1612.4 GPS week: 1612 Day: 4 MJD: 55532.000 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 233| 0 -1 2 83 -30 -2 -.20 8 7 | -347 2 17 66 | -15 77 | emr 90| 0 0 3 20 -61 -7 .38 19 19 | -3483 1418 14 85 | -23 -44 | esa 148| 0 0 -2 -60 -124 -92 .23 10 10 | -452 -922 14 111 | 0 71 | gfz 190| 0 0 -2 -26 90 -2 -.23 10 9 | -238 926 20 98 | -32 -39 | grg 133| 0 2 -6 -26 -215 -5 .70 17 15 | -279 472 50 274 | 39 18 | igr n/a| 0 0 0 85 -17 42 -.04 5 5 | 6206 1121 16 71 | -67 -7 | jpl 122| 0 0 8 -43 15 -32 .58 17 16 | -915 1604 19 101 | -4 -112 | mit 260| 0 0 -4 63 32 34 -.37 15 13 | -379 581 19 115 | 5 -31 | ngs 214| 0 0 0 -27 79 56 -.23 9 7 | -337 -9 2471 3685 | -18 69 | sio 259| -1 2 4 -30 120 1 -.03 18 19 | --- --- --- --- | -18 -3 | Table 2.1612.5 GPS week: 1612 Day: 5 MJD: 55533.000 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 233| 0 0 3 59 13 -17 -.22 8 8 | -88 -287 18 78 | 24 12 | emr 90| 1 0 2 29 -21 19 .39 18 18 | -2672 -412 16 79 | -43 -19 | esa 148| -1 0 -1 -107 -62 -59 .20 9 8 | 1385 -2307 15 105 | -8 45 | gfz 190| -1 -1 0 63 -70 6 -.26 11 10 | 1 105 18 94 | -44 -39 | grg 133| 1 1 -8 -57 -175 -23 .72 16 15 | 80 -33 38 212 | 95 -51 | igr n/a| 0 0 0 72 44 49 -.05 6 6 | 6837 -341 15 83 | -42 -39 | jpl 122| 0 0 9 -88 59 -48 .57 19 18 | 166 -48 16 94 | -22 -10 | mit 260| 0 -1 -3 86 3 47 -.36 13 11 | -5 78 19 100 | -12 -16 | ngs 214| 0 0 -2 -29 178 53 -.21 11 8 | -154 -119 2240 4013 | 12 -47 | sio 259| 0 3 4 0 74 11 -.08 19 18 | --- --- --- --- | -30 26 | Table 2.1612.6 GPS week: 1612 Day: 6 MJD: 55534.000 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 233| 0 0 5 85 9 2 -.21 9 8 | 131 -572 15 71 | -15 8 | emr 90| 0 0 5 30 -14 20 .40 18 18 | -2482 -234 17 84 | -35 -35 | esa 148| 0 0 -3 -93 -40 -47 .21 10 9 | -86 -1353 16 127 | 1 31 | gfz 190| -1 0 -3 -18 -99 -15 -.17 8 7 | 486 -606 20 98 | -43 -56 | grg 133| 1 2 -12 24 -185 -58 .68 16 15 | 355 -275 56 215 | -11 -35 | igr n/a| 0 0 0 45 -4 8 -.02 7 6 | 7013 -460 15 81 | -33 -47 | jpl 122| 1 -1 12 -66 63 -47 .52 18 16 | 628 -488 17 92 | 17 -20 | mit 260| 1 0 -3 29 -26 32 -.34 13 9 | 177 -68 16 109 | -14 -11 | ngs 214| -1 0 0 6 188 60 -.20 9 8 | 316 -889 2285 3524 | 6 24 | sio 259| 1 4 6 -77 63 1 -.08 20 17 | --- --- --- --- | -15 10 | 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 3.1612.0 GPS week: 1612 Day: 0 MJD: 55528.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 43 --- --- 49 --- 114 --- --- --- --- 46 | 50 --- --- 36 --- 61 --- --- --- --- 40 2 | 9 23 12 9 10 5 21 34 10 41 6 | 19 33 23 20 27 19 33 33 21 43 21 3 | 8 11 10 7 14 6 12 16 12 32 4 | 22 30 29 24 35 24 30 22 21 21 24 4 | 9 12 7 4 10 6 10 21 13 31 4 | 34 31 38 35 41 33 32 34 36 42 34 5E | 8 22 9 10 11 4 22 14 11 33 5 | 21 29 23 26 31 20 28 19 25 28 22 6 | 9 10 9 8 14 6 11 16 9 25 4 | 20 29 28 24 35 24 27 23 21 23 23 7 | 8 21 18 13 18 4 19 12 7 17 5 | 18 33 33 21 31 20 29 22 18 20 21 8 | 10 20 11 9 14 5 14 30 9 22 5 | 23 35 28 22 30 23 33 29 26 26 24 9 | 13 17 9 8 14 5 14 17 11 20 4 | 18 27 18 16 24 18 22 25 17 20 16 10E | 16 16 16 12 15 5 17 44 19 37 7 | 44 54 50 45 62 46 57 54 46 56 47 11 | 6 16 8 8 14 4 15 13 9 26 4 | 27 35 31 33 39 29 30 31 30 30 27 12 | 9 25 10 10 20 5 24 15 12 15 5 | 23 36 30 21 36 25 34 28 23 29 23 13 | 7 20 8 7 22 3 21 14 10 14 4 | 22 35 23 20 38 20 33 20 21 17 21 14 | 6 19 10 8 15 4 20 14 8 17 4 | 20 33 25 19 34 22 30 19 22 19 21 15 | 9 23 10 6 18 5 21 13 9 17 4 | 21 32 26 20 32 20 30 24 21 21 21 16 | 10 28 10 11 19 5 23 13 11 17 5 | 31 40 29 23 39 26 38 25 22 25 27 17 | 9 13 12 19 18 4 13 12 15 25 5 | 23 32 30 39 29 26 29 23 32 20 26 18E | 7 18 11 9 26 5 20 13 8 13 4 | 20 27 27 25 25 23 26 23 27 25 22 19 | 8 13 9 9 11 5 13 8 11 28 4 | 18 21 23 19 23 18 17 20 19 20 17 20E | 8 18 8 9 18 3 17 20 8 13 4 | 18 26 21 15 30 17 23 22 18 20 16 21 | 9 18 10 14 13 6 23 15 8 23 5 | 22 35 27 24 33 23 38 19 23 19 22 22E | 8 14 8 9 23 4 20 18 10 12 4 | 30 30 33 27 35 29 31 25 33 30 29 23 | 7 24 9 9 20 6 22 16 10 17 5 | 21 37 24 18 30 19 31 20 17 17 19 24 | 8 10 10 6 14 3 6 12 8 14 3 | 23 27 28 24 30 25 24 32 24 24 23 X25 | 11 19 8 6 18 7 --- 11 14 --- 5 | 39 50 40 37 45 39 --- 35 40 --- 38 26 | 8 15 8 5 10 5 9 14 7 15 3 | 14 25 17 14 21 13 19 19 13 14 14 27 | 10 16 8 15 16 6 11 18 8 21 4 | 14 24 16 23 20 14 18 19 16 20 13 28 | 8 13 9 8 20 5 16 12 10 23 4 | 20 31 24 21 35 22 32 21 25 25 21 X29 | 8 17 10 8 16 4 16 22 10 --- 4 | 19 22 23 23 22 18 23 25 23 --- 19 30 | 7 18 12 9 13 4 15 20 8 20 4 | 27 32 27 25 34 26 35 29 26 39 26 31 | 8 15 14 7 20 4 17 12 10 13 4 | 17 27 26 19 35 19 26 21 19 21 19 32E | 11 22 9 10 23 5 14 27 12 20 5 | 42 43 46 40 47 40 46 56 45 44 42 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 10 10 17 5 17 19 10 23 |T 24 32 27 24 33 25 30 26 24 26 24 WRMS | 9 18 10 8 15 5 16 15 8 18 |NE 23 31 26 23 31 24 28 24 23 24 23 MEDI | 8 18 10 9 16 5 16 15 10 20 |MD 21 32 27 23 33 23 30 23 23 23 22 Table 3.1612.1 GPS week: 1612 Day: 1 MJD: 55529.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 7 --- --- --- --- 73 --- --- --- --- 0 | 43 --- --- --- --- 42 --- --- --- --- 53 2 | 11 21 11 12 9 5 25 27 10 36 6 | 11 27 20 19 21 14 30 21 13 36 16 3 | 6 12 10 8 13 7 10 10 12 26 4 | 19 23 21 22 25 19 26 18 24 20 20 4 | 11 13 8 7 9 4 10 16 13 28 4 | 20 20 25 22 27 22 23 23 21 33 22 5E | 6 20 8 9 10 4 22 20 6 18 4 | 16 25 19 19 28 16 28 18 16 13 17 6 | 7 11 11 7 12 6 9 12 8 18 3 | 16 22 20 18 25 17 24 17 16 17 17 7 | 9 23 14 14 20 6 16 16 9 17 5 | 16 28 16 14 25 15 22 19 15 21 13 8 | 10 19 10 11 14 4 14 24 8 19 5 | 16 26 18 21 19 18 24 30 20 27 18 9 | 13 17 7 10 13 6 14 19 12 15 4 | 15 25 15 17 19 13 20 19 18 16 14 10E | 12 18 15 11 25 5 17 33 15 26 6 | 35 46 42 38 64 38 51 44 38 44 40 11 | 7 16 8 9 14 4 15 11 8 24 4 | 17 26 19 20 25 18 23 22 21 20 16 12 | 12 29 11 11 15 5 24 17 10 16 5 | 19 36 20 19 30 20 32 22 22 25 19 13 | 7 22 11 9 23 5 19 15 11 13 5 | 14 28 18 15 36 15 27 14 15 11 15 14 | 5 20 11 10 18 4 18 15 9 17 4 | 17 30 24 20 31 19 30 17 17 20 20 15 | 7 24 10 7 24 4 22 15 10 16 5 | 15 31 17 20 32 18 28 17 21 16 18 16 | 7 28 9 10 18 5 21 12 8 20 5 | 21 35 22 19 31 20 32 17 20 19 21 17 | 10 13 9 24 16 4 12 10 9 22 5 | 12 24 25 36 22 21 21 17 19 18 20 18E | 9 15 13 11 12 4 21 16 10 13 4 | 19 24 24 23 25 18 26 17 19 18 19 19 | 5 12 8 9 11 6 15 7 12 29 4 | 10 15 14 13 14 12 15 13 16 13 10 20E | 8 16 6 10 14 5 15 15 6 14 4 | 19 26 19 19 27 17 24 21 21 22 19 21 | 8 19 12 10 12 5 19 14 8 25 4 | 15 29 23 15 27 16 30 14 14 15 17 22E | 8 11 11 11 16 7 21 18 10 13 4 | 29 30 29 28 34 29 31 28 27 28 27 23 | 7 26 10 11 20 6 21 16 9 18 5 | 14 32 16 15 27 14 28 16 13 12 13 24 | 8 10 7 10 13 3 8 9 6 11 3 | 17 16 17 19 21 16 14 22 18 15 15 X25 | 13 19 7 10 15 5 --- 13 8 --- 4 | 31 43 34 32 40 34 --- 26 33 --- 32 26 | 7 12 9 9 9 4 12 15 6 11 3 | 14 23 19 20 23 17 20 15 17 17 17 27 | 10 17 9 11 13 5 14 17 13 16 4 | 12 26 16 17 22 14 18 17 18 19 14 28 | 8 16 10 8 18 4 16 12 6 19 4 | 14 26 18 15 32 14 22 18 15 18 16 X29 | 7 14 10 11 13 5 13 25 7 --- 4 | 16 20 16 11 14 15 19 18 18 --- 15 30 | 6 20 11 9 13 6 14 15 8 16 4 | 20 34 23 24 27 21 30 20 22 32 23 31 | 7 14 12 9 22 6 17 10 11 12 4 | 13 25 16 15 31 13 22 14 15 13 14 32E | 12 30 11 16 21 5 17 24 14 20 6 | 23 30 23 25 29 23 20 32 28 16 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 19 10 11 16 5 17 17 10 20 |T 18 27 20 20 27 19 25 20 19 20 19 WRMS | 9 19 10 10 14 5 15 14 8 18 |NE 17 26 19 19 25 18 24 18 18 19 18 MEDI | 8 17 10 10 14 5 16 15 9 18 |MD 16 26 19 19 27 17 24 18 18 18 17 Table 3.1612.2 GPS week: 1612 Day: 2 MJD: 55530.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 43 --- --- --- --- 43 --- 59 30 --- 30 | 42 --- --- --- --- 56 --- 25 36 --- 29 2 | 8 19 5 8 11 5 22 27 11 37 5 | 12 26 20 17 22 16 30 20 15 36 17 3 | 7 11 5 7 13 6 12 12 11 23 3 | 19 24 23 18 26 21 28 20 21 19 19 4 | 8 12 5 4 8 3 12 15 7 24 3 | 25 24 28 26 32 26 26 27 25 34 27 5E | 8 21 7 9 18 4 19 24 9 11 4 | 18 25 18 21 26 18 25 27 18 18 17 6 | 6 11 6 8 10 6 10 13 9 17 3 | 17 23 20 16 25 20 25 21 19 19 17 7 | 9 24 9 13 20 6 16 15 6 16 4 | 12 30 15 19 24 17 24 19 17 22 14 8 | 9 19 7 9 11 5 13 28 10 17 4 | 14 26 17 17 20 20 22 34 21 27 18 9 | 8 16 7 16 13 7 14 17 6 16 4 | 16 25 20 25 19 20 25 20 19 20 19 10E | 11 19 7 12 17 5 16 27 15 20 5 | 34 47 41 37 56 38 51 41 38 42 39 11 | 7 18 8 8 11 5 15 12 8 20 4 | 25 30 24 25 29 24 25 28 28 24 23 12 | 8 27 10 7 14 5 25 16 9 17 5 | 18 35 24 21 31 24 33 27 25 28 22 13 | 6 24 9 14 21 5 19 11 11 13 4 | 14 30 17 23 35 15 28 16 17 16 16 14 | 5 21 9 8 14 5 20 12 6 16 4 | 16 30 22 18 29 19 29 17 18 20 19 15 | 6 22 7 6 21 6 22 14 6 16 4 | 17 29 23 19 33 18 27 21 18 19 20 16 | 7 28 7 8 17 6 21 14 7 18 4 | 22 37 26 21 35 23 33 21 24 22 24 17 | 6 11 8 20 13 5 12 11 8 21 4 | 16 21 24 28 21 19 21 20 16 17 20 18E | 8 18 10 8 22 6 23 12 10 10 4 | 12 22 20 19 18 18 26 16 23 18 16 19 | 6 11 6 6 10 5 14 11 12 30 4 | 15 17 16 15 15 14 16 19 19 17 13 20E | 7 19 10 10 10 4 14 16 10 12 4 | 15 23 19 17 21 14 18 18 19 18 16 21 | 8 17 6 10 12 4 19 14 11 23 4 | 14 28 20 18 24 19 31 15 21 21 17 22E | 6 12 8 10 18 6 21 15 7 13 4 | 21 25 23 20 22 23 28 24 29 21 21 23 | 7 27 11 9 18 6 21 14 8 16 4 | 15 33 19 15 28 15 28 17 18 16 15 24 | 8 8 7 8 8 7 9 10 7 10 3 | 22 22 21 21 23 21 20 24 21 21 20 X25 | 15 23 9 7 16 5 --- 15 9 --- 5 | 33 46 38 36 47 38 --- 35 39 --- 36 26 | 7 13 5 7 11 6 9 14 7 11 3 | 13 18 18 16 19 13 20 19 17 18 16 27 | 6 16 6 8 12 5 14 15 6 17 3 | 12 24 18 17 21 17 20 20 16 24 16 28 | 7 20 6 7 18 4 19 12 8 17 4 | 13 30 19 16 32 16 28 18 16 19 17 X29 | 5 14 7 11 12 6 15 25 10 --- 4 | 15 20 16 18 17 16 20 26 22 --- 16 30 | 5 15 9 10 15 5 16 16 12 16 4 | 18 28 24 24 30 21 28 21 22 30 23 31 | 8 20 7 7 17 5 18 11 16 12 4 | 14 26 20 15 30 15 23 16 18 17 16 32E | 14 23 12 12 21 9 17 29 11 25 6 | 28 29 28 32 26 28 24 46 34 23 26 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 8 10 15 6 17 17 9 19 |T 18 27 21 20 26 21 26 23 22 22 20 WRMS | 7 19 8 8 14 5 16 14 7 16 |NE 18 27 21 20 26 20 25 21 21 22 19 MEDI | 7 19 7 8 14 5 16 14 9 17 |MD 16 26 20 19 26 19 25 20 19 20 18 Table 3.1612.3 GPS week: 1612 Day: 3 MJD: 55531.000 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 | 55 57 --- 48 --- 43 --- 33 31 --- 23 | 38 21 --- 39 --- 46 --- 26 38 --- 29 2 | 10 16 9 16 9 5 22 23 11 33 5 | 19 27 21 28 25 18 31 24 19 37 21 3 | 7 12 5 9 12 5 12 9 9 21 3 | 22 29 28 23 31 24 30 25 23 22 24 4 | 6 12 6 10 9 4 9 18 15 22 4 | 30 29 32 32 35 29 29 34 32 34 30 5E | 8 19 6 12 9 4 20 12 10 10 4 | 24 28 26 31 29 25 26 28 27 29 26 6 | 7 10 5 10 10 5 10 10 8 16 3 | 20 26 27 22 31 21 26 24 21 21 22 7 | 11 17 10 12 19 6 19 12 9 16 4 | 19 27 24 23 26 19 25 21 19 23 18 8 | 8 18 6 11 11 5 14 22 11 16 4 | 20 25 21 19 23 19 25 30 21 25 20 9 | 11 15 6 17 11 4 13 15 11 18 4 | 18 20 15 21 19 14 20 20 16 18 15 10E | 12 18 8 14 21 4 14 18 14 14 5 | 39 51 45 40 61 42 54 40 42 43 43 11 | 7 16 7 10 12 4 15 12 9 18 3 | 26 31 31 30 34 26 27 30 29 24 25 12 | 8 26 10 16 16 4 23 15 8 17 5 | 26 37 25 25 34 25 35 32 25 32 25 13 | 6 20 10 11 20 5 20 10 12 13 4 | 23 30 23 21 34 19 30 21 23 18 21 14 | 4 21 8 10 14 4 18 10 6 18 4 | 21 30 21 20 30 20 28 19 20 20 20 15 | 7 24 7 7 17 4 23 14 8 19 4 | 19 30 21 21 34 19 29 25 23 21 21 16 | 5 25 7 11 17 3 23 15 10 16 4 | 28 40 25 25 37 25 39 29 26 26 27 17 | 8 12 6 23 11 5 15 10 11 20 4 | 18 25 21 32 24 20 22 20 21 18 21 18E | 7 17 10 11 18 4 23 11 10 11 4 | 20 23 20 21 20 19 23 20 21 20 18 19 | 7 11 5 8 11 5 15 13 8 28 4 | 18 18 20 19 20 16 17 22 20 19 16 20E | 8 15 10 10 19 2 15 18 9 10 4 | 22 30 24 23 28 21 26 30 22 25 22 21 | 7 20 9 12 13 4 21 12 8 23 4 | 19 27 20 19 28 18 31 17 14 19 17 22E | 7 16 8 8 13 3 21 11 10 11 4 | 30 30 28 29 31 30 31 29 28 29 28 23 | 8 25 11 13 19 5 20 17 9 15 5 | 21 33 24 20 26 18 28 22 20 16 18 24 | 8 12 6 9 12 3 9 12 9 11 3 | 26 28 29 28 31 25 23 31 28 24 25 X25 | 10 21 8 14 18 4 --- 14 9 --- 5 | 39 50 39 40 48 40 --- 40 41 --- 40 26 | 6 10 5 11 9 5 9 13 8 12 3 | 17 21 18 18 22 16 18 21 19 18 17 27 | 7 18 6 15 11 3 11 15 10 19 4 | 18 25 19 22 21 17 22 21 18 23 17 28 | 6 16 5 10 17 3 16 11 10 16 4 | 22 33 23 21 37 22 32 24 24 23 23 X29 | 7 15 10 10 12 5 17 19 11 --- 4 | 20 18 20 22 19 18 21 23 25 --- 18 30 | 7 23 9 9 14 4 16 14 7 18 4 | 25 32 24 28 33 23 30 23 20 33 24 31 | 11 20 8 12 18 4 18 10 10 15 4 | 16 25 17 17 31 14 24 16 16 17 14 32E | 16 27 8 14 19 5 21 26 11 19 6 | 28 33 29 34 30 30 28 42 32 22 28 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 8 12 15 4 17 15 10 18 |T 23 29 24 25 30 23 27 25 24 24 22 WRMS | 8 18 8 11 14 4 16 13 8 17 |NE 22 28 23 24 29 21 26 24 23 23 21 MEDI | 7 17 8 11 13 4 16 13 10 16 |MD 21 28 24 23 30 20 27 24 22 23 21 Table 3.1612.4 GPS week: 1612 Day: 4 MJD: 55532.000 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 | 29 --- --- 51 --- 48 --- 28 36 --- 21 | 23 --- --- 44 --- 45 --- 29 49 --- 25 2 | 7 21 13 8 10 6 20 21 10 35 5 | 15 30 22 18 24 17 31 18 18 35 17 3 | 6 14 8 7 11 5 12 9 7 20 3 | 15 24 20 15 26 16 26 15 18 13 16 4 | 6 12 9 5 10 3 9 13 8 19 3 | 28 28 35 27 32 29 29 28 30 28 28 5E | 8 23 12 10 15 4 18 17 12 17 5 | 22 32 29 26 34 25 29 28 25 26 23 6 | 6 12 6 8 11 6 9 11 5 15 3 | 15 24 22 16 27 16 27 16 16 14 16 7 | 11 22 11 12 20 3 15 11 4 16 4 | 14 29 24 18 32 16 28 17 16 18 15 8 | 8 17 7 7 14 4 15 17 7 14 4 | 15 27 19 17 24 14 28 19 16 17 15 9 | 8 14 10 8 12 5 12 14 9 18 4 | 16 23 15 17 24 13 23 20 16 16 14 10E | 12 22 10 14 19 6 21 16 9 11 5 | 37 51 48 39 58 40 54 36 36 39 40 11 | 5 19 6 8 13 4 13 14 6 18 3 | 22 27 24 26 27 20 25 28 22 19 20 12 | 10 29 15 10 20 3 24 12 8 19 5 | 17 36 22 22 35 20 33 22 18 23 19 13 | 6 23 11 9 22 4 19 10 10 15 4 | 22 35 25 20 39 23 36 21 18 20 21 14 | 9 20 9 7 13 5 19 10 10 21 4 | 18 33 23 19 32 21 32 22 21 25 21 15 | 8 24 12 8 23 5 20 17 10 18 5 | 19 32 24 22 40 17 31 20 18 22 20 16 | 6 27 8 10 21 4 22 13 8 19 4 | 26 38 26 21 39 22 37 22 26 22 25 17 | 9 12 10 23 14 5 16 13 8 21 5 | 16 23 25 32 22 18 26 17 15 18 18 18E | 7 17 13 10 22 6 20 12 10 9 4 | 22 26 27 22 27 20 27 23 23 21 20 19 | 5 14 7 8 12 5 15 15 9 29 4 | 12 21 17 14 18 12 21 19 12 16 11 20E | 6 17 8 7 14 4 14 14 5 13 3 | 17 27 20 17 24 16 21 20 17 18 15 21 | 6 18 12 9 10 5 18 13 6 24 4 | 19 28 24 17 27 16 31 16 21 19 18 22E | 8 11 11 14 16 5 21 15 11 9 4 | 22 25 26 21 30 21 29 22 22 22 20 23 | 9 26 9 8 18 5 18 17 9 17 4 | 23 36 25 19 28 21 33 21 15 17 19 24 | 6 12 7 9 11 3 6 14 8 11 3 | 19 24 24 24 23 21 25 28 21 19 19 X25 | 8 21 10 11 20 6 --- 16 9 --- 5 | 37 45 35 37 46 37 --- 35 35 --- 35 26 | 8 13 10 10 10 6 10 14 10 14 3 | 16 26 21 22 26 16 26 17 16 19 17 27 | 7 17 8 8 10 5 11 14 9 20 4 | 10 24 12 12 19 9 19 15 13 19 10 28 | 6 16 8 7 19 3 14 11 10 18 4 | 18 32 24 18 36 20 30 18 25 20 20 X29 | 6 16 8 10 13 6 17 21 9 --- 4 | 16 20 19 21 21 16 19 21 19 --- 16 30 | 4 16 12 9 25 5 18 20 10 18 5 | 22 29 26 23 34 21 36 24 19 33 22 31 | 8 21 9 9 23 4 16 11 8 15 4 | 13 28 23 12 30 13 27 19 14 19 14 32E | 13 25 12 12 25 6 18 24 12 18 6 | 24 34 31 28 31 25 30 34 30 25 25 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 19 10 10 17 5 17 15 9 18 |T 19 29 24 22 30 20 28 22 21 21 19 WRMS | 7 19 10 9 15 5 16 13 7 19 |NE 18 28 23 21 29 19 28 21 20 20 18 MEDI | 7 17 10 9 14 5 16 14 9 18 |MD 18 28 24 21 28 20 28 21 18 19 19 Table 3.1612.5 GPS week: 1612 Day: 5 MJD: 55533.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 18 --- --- 29 --- 168 --- --- --- --- 23 | 46 --- --- 32 --- 100 --- --- --- --- 32 2 | 13 17 9 12 11 6 23 21 12 36 6 | 12 22 20 17 21 16 30 17 16 39 16 3 | 6 14 7 9 15 7 14 9 11 21 3 | 20 25 24 23 27 20 29 20 20 18 21 4 | 7 11 7 10 13 6 15 8 11 16 3 | 23 27 32 30 34 31 31 26 34 27 28 5E | 5 23 8 11 19 6 19 9 8 14 4 | 14 23 18 18 24 15 23 14 14 14 13 6 | 8 13 6 8 9 8 14 11 11 18 3 | 16 21 20 17 24 16 26 17 17 18 17 7 | 8 22 10 10 19 7 20 8 9 14 4 | 16 26 19 20 26 16 24 18 21 22 16 8 | 9 18 7 12 11 5 17 13 8 15 4 | 19 26 21 20 21 19 24 21 21 22 18 9 | 9 17 8 9 12 6 15 11 13 17 4 | 14 23 15 15 13 15 22 20 22 19 15 10E | 11 19 7 10 17 6 13 10 10 20 4 | 33 45 39 33 50 37 48 32 35 40 36 11 | 6 18 8 10 14 5 19 14 11 17 4 | 20 23 22 25 23 19 22 29 25 19 20 12 | 8 23 7 10 17 5 25 10 10 19 4 | 16 30 22 19 29 18 31 22 18 23 20 13 | 5 22 9 9 22 6 18 9 8 14 4 | 18 30 19 22 34 19 28 17 22 16 19 14 | 6 21 12 8 14 5 22 12 10 21 4 | 18 28 22 16 27 17 28 18 18 21 17 15 | 8 21 9 12 16 6 24 15 13 19 5 | 16 25 17 16 25 16 28 21 20 20 15 16 | 7 31 12 10 22 6 23 11 11 15 5 | 22 34 22 17 35 21 31 19 25 21 20 17 | 8 12 7 21 15 6 18 8 9 19 4 | 23 24 25 31 27 24 28 24 27 26 24 18E | 8 14 9 12 18 5 21 8 9 14 4 | 25 31 32 25 33 28 37 27 26 29 27 19 | 6 16 4 9 9 7 19 13 11 31 4 | 12 18 15 14 12 12 17 18 14 18 12 20E | 6 14 6 8 11 4 14 10 11 16 3 | 12 20 13 16 16 11 21 18 17 17 14 21 | 7 15 11 9 12 5 20 9 8 25 4 | 17 27 22 14 23 17 33 14 21 23 18 22E | 7 16 11 10 15 6 21 15 7 13 4 | 21 23 23 22 24 19 24 21 19 18 17 23 | 7 25 11 10 20 8 21 18 12 16 5 | 17 31 18 18 26 17 28 22 20 15 16 24 | 8 11 5 12 12 4 9 15 11 12 3 | 16 18 17 26 20 17 17 25 19 18 18 X25 | 12 19 8 11 16 7 --- 14 9 --- 5 | 30 34 30 29 37 27 --- 25 25 --- 28 26 | 8 11 8 10 10 5 10 14 12 14 3 | 19 23 20 21 22 19 21 20 20 19 18 27 | 9 19 6 10 11 4 15 13 15 19 4 | 15 25 15 15 14 15 21 18 24 22 15 28 | 8 17 7 10 22 5 20 7 9 17 4 | 17 27 21 17 35 18 28 16 21 20 19 X29 | 8 13 7 7 14 6 19 14 8 --- 4 | 20 24 23 25 21 21 24 26 24 --- 22 30 | 7 18 13 8 20 6 19 17 12 19 5 | 21 30 31 25 34 23 32 27 20 33 24 31 | 8 17 8 12 18 6 23 14 13 14 4 | 14 25 19 18 28 15 27 18 16 19 15 32E | 14 23 11 10 23 8 18 21 15 18 5 | 21 26 27 28 21 25 21 36 28 20 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 8 18 9 11 16 6 19 13 11 19 |T 19 26 22 21 26 21 26 21 21 21 19 WRMS | 8 18 8 10 15 6 18 11 8 18 |NE 19 25 21 20 25 21 26 20 21 21 19 MEDI | 8 17 8 10 15 6 19 12 11 17 |MD 18 25 21 20 25 18 27 20 21 20 18 Table 3.1612.6 GPS week: 1612 Day: 6 MJD: 55534.000 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 --- --- 16 --- 48 --- 15 26 --- 11 | 41 --- --- 32 --- 60 --- 21 28 --- 30 2 | 12 17 12 9 14 9 22 26 11 39 6 | 19 28 24 21 21 18 33 25 24 45 21 3 | 7 12 10 6 15 6 11 9 9 29 4 | 29 32 30 24 34 27 36 29 33 36 29 4 | 6 11 7 7 11 5 11 7 9 15 3 | 31 31 36 34 37 33 31 31 38 32 33 5E | 8 20 12 8 14 8 18 8 5 15 4 | 17 26 21 21 23 17 23 18 25 21 18 6 | 7 12 10 6 12 7 12 11 12 23 4 | 24 27 26 20 30 24 31 25 29 29 24 7 | 10 18 10 8 19 4 19 6 7 18 4 | 22 24 19 18 22 15 24 17 20 22 16 8 | 11 17 9 9 13 6 16 12 12 12 4 | 22 26 19 18 19 17 27 23 26 22 20 9 | 8 15 6 8 16 6 15 8 10 17 3 | 15 19 14 19 15 11 19 16 18 16 12 10E | 12 18 9 9 22 10 16 10 9 25 4 | 40 50 45 38 59 43 55 39 42 47 42 11 | 6 20 7 7 12 5 16 17 7 18 4 | 29 32 36 34 36 29 28 37 34 29 30 12 | 7 25 11 9 19 5 24 8 7 19 4 | 24 37 25 22 32 24 36 24 28 28 23 13 | 7 20 10 8 21 5 20 10 10 13 4 | 19 30 23 18 33 18 30 20 24 15 19 14 | 9 16 9 6 17 8 18 14 7 21 4 | 24 29 23 18 31 21 30 22 27 23 22 15 | 8 22 11 6 19 7 22 16 9 20 4 | 18 31 25 25 34 21 31 23 27 24 22 16 | 8 31 13 7 15 6 20 9 12 18 5 | 30 42 30 23 34 26 38 26 34 29 28 17 | 9 16 9 20 14 6 18 8 8 18 4 | 20 24 24 30 25 21 25 26 26 26 22 18E | 9 18 10 8 18 5 19 8 10 13 4 | 34 32 30 27 24 28 33 26 38 24 28 19 | 7 16 6 7 10 5 19 16 12 29 4 | 21 20 21 18 20 17 20 23 24 20 18 20E | 7 14 6 6 11 5 16 12 8 14 3 | 15 21 19 22 19 15 21 21 19 17 16 21 | 7 17 11 6 9 6 21 7 6 27 4 | 21 26 19 16 21 17 31 15 22 26 17 22E | 9 11 9 7 18 7 19 12 9 13 4 | 26 25 23 22 26 21 28 23 29 21 22 23 | 9 25 11 9 19 6 20 19 10 18 5 | 19 34 21 18 27 17 29 27 23 16 18 24 | 7 13 8 5 12 6 9 17 7 14 3 | 26 26 32 29 32 26 22 33 31 27 27 X25 | 7 17 12 12 14 5 --- 15 10 --- 5 | 42 48 42 45 45 42 --- 40 43 --- 41 26 | 9 12 9 9 15 8 11 8 9 14 3 | 19 21 21 20 22 15 22 19 25 17 18 27 | 8 15 6 9 14 6 12 9 11 20 4 | 15 20 16 19 17 12 16 16 19 22 13 28 | 8 19 6 10 20 5 19 5 10 16 4 | 22 32 22 20 34 23 31 19 27 25 22 X29 | 7 14 8 7 13 6 19 12 10 --- 4 | 24 26 24 31 21 24 24 27 30 --- 24 30 | 8 16 11 10 16 6 17 20 11 20 4 | 24 30 27 29 30 24 32 29 30 34 26 31 | 8 20 11 7 21 6 21 15 8 15 4 | 16 26 21 16 29 16 26 21 24 18 17 32E | 23 25 14 8 24 11 20 23 10 16 6 | 22 27 23 24 20 24 23 39 32 26 22 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 9 18 10 8 16 7 18 13 9 20 |T 24 29 25 24 28 23 28 25 28 25 23 WRMS | 8 18 9 7 15 6 16 9 8 17 |NE 23 28 24 23 28 23 28 24 27 25 22 MEDI | 8 17 10 8 15 6 18 11 9 18 |MD 22 27 23 22 27 21 28 23 27 24 22 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1612 GPS week: 1612 MJD: 55528.0-55534.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3030 |U 7 6 17 |U 9 10 30 |U 24 17 58 | emr | emr 2979 |U 12 10 30 |U 10 11 33 | 23 15 63 | esa | esa 2975 | 7 7 17 |U 8 10 29 | 21 14 54 | gfz | gfz 3025 |U 14 12 24 |U 15 24 70 |U 25 19 62 | grg | grg 2975 | 7 7 18 |U 9 14 33 | 23 17 57 | igr | igr 2944 | 7 7 18 | 9 11 30 | 22 15 57 | igs | igs 2934 | 8 9 17 | 9 10 30 | 22 16 57 | jpl | jpl 2866 |U 13 10 25 | 10 12 37 |U 19 13 50 | mit | mit 3030 |U 19 13 28 |U 9 10 29 |U 23 15 57 | 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 5.1612.0 GPS week: 1612 Day: 0 MJD: 55528.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3021 | 7 6 22 | 10 12 33 | 7 7 15 | emr | emr 2968 | 17 7 28 | 12 12 39 | 9 6 29 | esa | esa 2976 | 7 7 18 | 9 11 33 | 6 7 20 | gfz | gfz 3045 | 15 9 24 | 20 25 61 | 9 9 21 | grg | grg 2976 | 7 7 17 | 11 13 40 | 10 13 24 | igr | igr 2980 | 6 7 17 | 10 12 39 | 7 7 20 | igs | igs 2931 | 6 6 16 | 10 11 34 | 8 7 18 | jpl | jpl 2870 | 16 6 25 | 12 14 45 | 8 6 25 | mit | mit 2976 | 11 5 23 | 10 10 36 | 7 8 24 | Table 5.1612.1 GPS week: 1612 Day: 1 MJD: 55529.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3022 | 7 6 18 | 10 10 39 | 5 4 14 | emr | emr 2967 | 12 9 19 | 11 11 45 | 7 7 21 | esa | esa 2976 | 7 7 17 | 9 9 44 | 11 7 26 | gfz | gfz 2962 | 8 11 18 | 18 26 99 | 5 7 17 | grg | grg 2973 | 7 8 18 | 9 13 33 | 8 10 18 | igr | igr 2955 | 7 8 17 | 10 10 42 | 6 8 18 | igs | igs 2960 | 14 13 15 | 10 10 50 | 6 5 17 | jpl | jpl 2868 | 15 7 24 | 11 13 54 | 7 6 21 | mit | mit 2976 | 18 8 29 | 10 12 40 | 5 8 17 | Table 5.1612.2 GPS week: 1612 Day: 2 MJD: 55530.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3024 | 7 6 20 | 11 13 30 | 6 5 14 | emr | emr 2968 | 7 5 23 | 12 16 31 | 7 6 20 | esa | esa 2976 | 7 7 20 | 9 13 23 | 6 5 15 | gfz | gfz 2968 | 8 7 17 | 18 27 90 | 9 3 18 | grg | grg 2976 | 7 6 19 | 9 12 27 | 7 6 20 | igr | igr 2868 | 7 6 21 | 10 16 26 | 8 4 18 | igs | igs 2944 | 6 7 20 | 10 13 24 | 6 5 13 | jpl | jpl 2867 | 6 7 19 | 11 16 36 | 6 6 17 | mit | mit 3072 | 19 7 33 | 10 15 27 | 7 6 17 | Table 5.1612.3 GPS week: 1612 Day: 3 MJD: 55531.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3034 | 6 7 13 | 9 8 23 | 63 55 144 | emr | emr 3049 | 10 9 53 | 8 7 29 | 46 44 130 | esa | esa 2976 | 6 6 13 | 7 7 21 | 38 35 104 | gfz | gfz 3045 | 11 10 38 | 13 25 82 | 68 65 150 | grg | grg 2975 | 7 7 18 | 7 9 27 | 50 42 115 | igr | igr 3002 | 6 7 15 | 8 6 22 | 47 44 122 | igs | igs 2895 | 7 8 15 | 7 7 18 | 52 48 125 | jpl | jpl 2860 | 9 8 26 | 7 7 28 | 55 52 143 | mit | mit 3072 | 20 20 45 | 8 7 21 | 53 27 108 | Table 5.1612.4 GPS week: 1612 Day: 4 MJD: 55532.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3032 | 6 6 13 | 8 13 31 | 73 36 189 | emr | emr 2968 | 11 11 27 | 9 15 31 | 73 33 194 | esa | esa 2976 | 7 5 17 | 8 13 31 | 73 33 180 | gfz | gfz 3055 | 17 12 23 | 14 25 59 | 72 39 182 | grg | grg 2976 | 8 5 16 | 9 19 34 | 73 29 184 | igr | igr 2954 | 8 7 18 | 8 14 26 | 72 30 185 | igs | igs 2947 | 12 13 16 | 8 14 31 | 73 34 188 | jpl | jpl 2863 | 12 13 22 | 9 19 34 | 42 12 102 | mit | mit 3072 | 21 14 20 | 8 12 27 | 74 38 190 | Table 5.1612.5 GPS week: 1612 Day: 5 MJD: 55533.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3044 | 7 9 18 | 7 7 26 | 6 7 13 | emr | emr 2968 | 14 16 35 | 8 8 28 | 9 7 23 | esa | esa 2976 | 7 9 18 | 6 7 24 | 6 8 17 | gfz | gfz 3046 | 18 21 29 | 12 20 63 | 6 7 20 | grg | grg 2975 | 8 9 19 | 7 10 32 | 6 9 21 | igr | igr 2855 | 8 11 23 | 9 8 25 | 8 7 15 | igs | igs 2932 | 6 8 17 | 7 7 23 | 7 7 17 | jpl | jpl 2871 | 14 17 33 | 7 7 30 | 8 8 19 | mit | mit 2976 | 23 22 30 | 7 8 31 | 7 7 21 | Table 5.1612.6 GPS week: 1612 Day: 6 MJD: 55534.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 3034 | 7 5 16 | 11 8 27 | 7 6 20 | emr | emr 2968 | 16 13 22 | 12 7 26 | 8 5 24 | esa | esa 2972 | 7 6 17 | 9 9 26 | 7 6 20 | gfz | gfz 3054 | 18 15 21 | 14 21 36 | 8 6 22 | grg | grg 2976 | 9 5 19 | 11 21 40 | 7 8 22 | igr | igr 2998 | 8 6 17 | 9 9 29 | 6 5 21 | igs | igs 2935 | 10 8 18 | 10 7 27 | 6 6 20 | jpl | jpl 2864 | 19 13 26 | 9 8 30 | 7 5 25 | mit | mit 3072 | 19 15 19 | 10 7 26 | 7 8 25 | 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 6.1612 GPS week: 1612 MJD: 55528.500-55534.500 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 | -25 -10 -52 73 5 | 0 13 | 30 17 100 82 6 | 4 emr uuuuu | 28 10 -138 10 -4 | 44 47 | 12 26 115 145 9 | 2 esa uuuuu | -52 -8 179 -210 5 | -8 16 | 13 9 112 52 4 | 4 gfz uuuuu | 8 42 -11 -103 -1 | -3 15 | 32 14 84 45 6 | 2 grg uuuux | -9 -48 43 8 -3 | 4 16 | 39 37 108 112 32 | 3 igr xxxxx | 11 41 74 45 3 | 1 14 | 18 14 109 61 7 | 4 irf xxxxx | 8 -3 -45 91 -4 | 3 14 | 16 19 52 62 5 | 2 jpl uuuuu | 29 -13 -17 154 3 | 10 17 | 41 35 135 83 14 | 4 mit uuuuu | 36 4 -276 222 -1 | 21 26 | 26 32 111 114 6 | 2 ngs uuuuu | 4 -14 56 27 -2 | -2 10 | 48 51 80 133 2 | 2 sio uuuuu | -2 15 -12 152 5 | 31 36 | 21 29 53 97 8 | 6 Table 7.1612.0 GPS week: 1612 Day: 0 MJD: 55528.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -36 -24 -36 171 3 | -6 13 emr uuuuu | 33 -35 69 -157 8 | 41 43 esa uuuuu | -52 -9 207 -231 9 | -13 19 gfz uuuuu | -36 37 0 -108 -3 | -4 14 grg uuuux | -79 -15 -4 -201 -20 | 7 19 igr xxxxx | 10 31 84 7 7 | -4 14 irf xxxxx | 27 -37 -73 112 2 | 1 14 jpl uuuuu | 34 -74 -96 84 6 | 3 17 mit uuuuu | 69 -55 -362 270 4 | 18 23 ngs uuuuu | 45 79 25 215 -6 | -4 10 sio uuuuu | 13 -40 43 224 12 | 22 29 Table 7.1612.1 GPS week: 1612 Day: 1 MJD: 55529.500 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 | -43 -12 -194 146 12 | -4 12 emr uuuuu | 24 12 -118 -186 9 | 42 45 esa uuuuu | -67 -20 194 -220 10 | -13 19 gfz uuuuu | -20 62 45 -172 3 | -5 14 grg uuuux | -31 -83 -84 -44 -26 | 3 17 igr xxxxx | 10 57 141 -21 -7 | -3 14 irf xxxxx | 5 14 -93 123 2 | 1 14 jpl uuuuu | -3 -7 128 81 -21 | 6 17 mit uuuuu | 34 30 -396 291 6 | 18 23 ngs uuuuu | 65 -25 40 155 0 | -4 10 sio uuuuu | -11 38 -28 223 14 | 24 31 Table 7.1612.2 GPS week: 1612 Day: 2 MJD: 55530.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 4 12 -20 52 5 | 0 13 emr uuuuu | 32 34 -218 5 -8 | 45 48 esa uuuuu | -47 7 71 -161 7 | -9 17 gfz uuuuu | -8 44 -4 -77 2 | -2 14 grg uuuux | -7 -65 108 132 -5 | 0 16 igr xxxxx | 1 49 157 36 11 | -1 12 irf xxxxx | 24 17 -47 129 -3 | 3 14 jpl uuuuu | 14 34 57 182 -8 | 8 16 mit uuuuu | 56 37 -294 277 0 | 21 26 ngs uuuuu | 9 -89 126 -131 -1 | -2 10 sio uuuuu | 17 39 -65 185 8 | 30 35 Table 7.1612.3 GPS week: 1612 Day: 3 MJD: 55531.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | 15 -22 -48 64 9 | 3 13 emr uuuuu | 29 -11 -136 49 -6 | 47 49 esa uuuuu | -33 -12 135 -215 5 | -5 15 gfz uuuuu | 1 60 -72 -127 2 | -1 15 grg uuuux | 5 -21 103 16 -5 | 3 15 igr xxxxx | -18 41 12 21 7 | 3 13 irf xxxxx | 20 13 -71 117 0 | 5 15 jpl uuuuu | 30 -23 -155 218 0 | 11 16 mit uuuuu | 53 28 -319 255 6 | 24 28 ngs uuuuu | -31 -34 198 -22 -4 | 0 9 sio uuuuu | 17 38 -60 202 9 | 35 38 Table 7.1612.4 GPS week: 1612 Day: 4 MJD: 55532.500 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 | -74 6 -43 121 4 | 3 14 emr uuuuu | 47 14 -295 -2 -8 | 46 48 esa uuuuu | -68 -9 226 -264 0 | -5 15 gfz uuuuu | 42 23 136 -134 -11 | -2 14 grg uuuux | -15 -48 75 26 43 | 2 14 igr xxxxx | 10 58 126 11 7 | 4 14 irf xxxxx | 3 -9 -81 143 -9 | 5 13 jpl uuuuu | 115 -5 -55 57 24 | 12 17 mit uuuuu | 34 -14 -315 317 -5 | 23 27 ngs uuuuu | -66 9 -2 38 -1 | 0 9 sio uuuuu | 6 9 -57 205 2 | 36 39 Table 7.1612.5 GPS week: 1612 Day: 5 MJD: 55533.500 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 | -23 -31 -146 29 -5 | 3 14 emr uuuuu | 8 36 -85 206 -16 | 46 48 esa uuuuu | -56 1 42 -119 1 | -5 15 gfz uuuuu | 28 37 -117 -51 -5 | -4 17 grg uuuux | 40 -102 198 1 36 | 5 15 igr xxxxx | 28 35 142 130 -5 | 5 13 irf xxxxx | -11 -7 -5 35 -10 | 4 15 jpl uuuuu | -1 15 168 169 12 | 14 17 mit uuuuu | 5 5 -154 145 -9 | 24 27 ngs uuuuu | 36 -19 41 -135 0 | -1 12 sio uuuuu | -37 23 28 24 -4 | 37 39 Table 7.1612.6 GPS week: 1612 Day: 6 MJD: 55534.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod xxxxx | -18 2 121 -71 7 | 1 14 emr uuuuu | 25 22 -185 151 -6 | 44 46 esa uuuuu | -41 -14 379 -258 3 | -6 16 gfz uuuuu | 46 30 -61 -54 5 | -7 18 grg uuuux | 25 -2 -95 122 -43 | 7 17 igr xxxxx | 37 20 -146 132 -2 | 3 14 irf xxxxx | -10 -13 53 -25 -9 | 1 15 jpl uuuuu | 10 -30 -166 283 5 | 13 17 mit uuuuu | 1 1 -93 -5 -8 | 21 26 ngs uuuuu | -34 -19 -36 66 -4 | -4 12 sio uuuuu | -20 2 58 0 -5 | 35 38