Date: Thu, 18 Sep 2008 12:55:24 +0000 From: Jim Ray Subject: [IGSREPORT-16636] Wk 1495 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <48d24fbc.zMt8C4gijbWTmrYY%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 18 Sep 05:55:26 PDT 2008 Message Number 16636 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1495 (Aug 31, 2008 - Sep 06, 2008) 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: igs1495[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1495[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1495[0-6].cls IGS GPS clock combination summary report. igs14957.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14957.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. Day | Centre | PRN/STA list ----+--------+--------------- 0 | COD | 3 26 NRIL 0 | EMR | 4 MIZU TWTF 0 | ESA | 25 TWTF 0 | GFZ | 3 4 7 29 BAN2 0 | JPL | 6 26 0 | MIT | 6 MAS1 1 | COD | 26 BRUS NRIL 1 | ESA | 25 26 BOGT 1 | GFZ | 7 29 HARB 1 | MIT | 5 SYDN 2 | COD | 26 CEDU IENG RAMO 2 | EMR | MIZU 2 | ESA | 26 DARW 2 | GFZ | 7 29 HARB SUTM 2 | JPL | 26 2 | MIT | SYDN 3 | COD | 26 BRUS NRIL 3 | EMR | MIZU 3 | ESA | 26 3 | GFZ | 7 29 WES2 3 | JPL | 26 SCUB 3 | MIT | 5 25 DARW SYDN 4 | COD | 6 26 4 | EMR | 4 NNOR 4 | ESA | 6 26 CHUR SCH2 YELL 4 | GFZ | 7 26 29 BAN2 DARW 4 | JPL | 4 4 | MIT | KOUC 5 | COD | 3 6 26 5 | EMR | HARB MIZU 5 | ESA | 3 6 26 5 | GFZ | 7 26 29 5 | JPL | HARB 5 | MIT | 5 18 25 ALGO BAKO DARW 6 | COD | 3 23 26 BRUS IENG 6 | EMR | MIZU 6 | ESA | 3 6 26 6 | GFZ | 7 23 26 29 BAN2 BJFS HARB ONSA 6 | MIT | 25 DARW MAR6 ONSA 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 ----+--------+--------+------------- 0 | ESA | ~22:30 | ~ 0.36 ns 6. Velocity changes were estimated to alleviate the effects of modeling problems, experienced by all centres,in the Long Arc (LA) process. Velocity changes per day and affected satellites: Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 | --------+----+----+----+----+----+----+----+ PRN G19 | | | | | | 2 | | 7. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) all IGS products, including the IGS combined orbits, are based on the IGS realization of the ITRF2005 reference frame (IGS05). For more information see IGSMAIL #5447. 8. Small rotations were applied to the all AC orbit and ERP values in order to align them to the IGS05. These rotations were estimated in the process of the IGS SINEX combination, performed at NRCan by Remi Ferland, are based on the common stations between the individual AC SINEX solutions and the IGS05.snx SINEX. The estimated 7 transformations, from which only the 3 rotations are applied to the orbit and ERP values, are: | DX DY DZ RX RY RZ SCL Centre | [mm] [mm] [mm] [uas] [uas] [uas] [ppb] -------+--------------------------------------------------- COD | .3 .3 .5 -11 -9 -2 -.41 EMR | 1.3 1.2 -11.5 46 -9 40 -.45 ESA | 1.1 4.5 2.8 49 7 21 -.41 GFZ | 1.0 .2 2.2 8 -30 5 -.82 GRG | 4.6 5.4 6.3 -18 -25 -14 -.24 JPL | -5.5 2.1 -6.5 2 4 -2 -.34 MIT | 3.6 .5 1.9 18 -11 -10 -.34 NGS | 3.3 3.2 .6 47 -44 -14 -.31 SIO | -.4 .2 -8.0 -3 -10 -15 -.10 9. Starting on 22-Oct-2000 (GPS Week 1085-0; mjd=51839) all IGS clock products are based on the new clock combination scheme which uses the clock RINEX files as input if available, otherwise SP3 clocks are used. The navigation solution is still based on the SP3 clocks but this will soon adopt the clock RINEX files as well. 10. Starting on 27-Feb-2000 (GPS Week 1051-0; MJD 51601) the IGS final products are aligned to the IGS reference frame products (station coordinates and ERPs as generated by NRCan. For more information see IGSMAIL #2750. Because of this change in alignment Table 2 has been enhanced with one additional line per AC. This additional line shows the X- and Y-rotations which were applied to each of the AC orbits prior to the orbit combination. These rotations are based on the difference between the individual AC ERP estimates and the IGS reference frame ERP product. The total rotation of the individual AC orbits w.r.t. the IGS combined orbit is the sum of the values in the two lines of Table 2 plus the reference frame rotation. 11. Starting on 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) the absolute antenna model is introduced (IGSMAIL #5272). The antenna phase center offsets and phase center variations are given in the file: ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx ORBIT COMBINATION AND EVALUATION STATISTICS: -------------------------------------------- Most combination statistics are with respect to the combined orbits and consist of five parts. The first, Table 1, summarizes all statistics for the week. It contains means and standard deviations over the week of satellite ephemeris and clock correction transformation parameters for each centre (table 1.1495.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1495.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 2.1495.[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 3.1495.[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 5.1495.0-6). 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 1495 summary. (Aug 31, 2008 - Sep 06, 2008) Table 1.1495.a GPS week: 1495 MJD: 54709.000-54715.000 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 217| 0 0 1 62 -24 -11 -.24 11 9 | -388 -27 24 102 | 0 1 1 7 11 19 .02 | 877 1230 emr 75| 0 -1 -2 -91 6 12 .35 15 15 | 887 -275 20 124 | 0 2 2 15 27 22 .03 | 1681 1790 esa 115| 0 0 2 -49 -57 -14 .26 11 11 | -8721 -17 21 124 | 0 0 1 11 21 10 .02 | 1253 1265 gfz 200| -1 0 -5 30 39 15 -.08 16 16 | 354 -12 26 130 | 0 0 1 24 10 66 .04 | 313 535 grg 80| 0 2 -3 52 23 -42 .95 39 33 | -373 -94 105 215 | 1 2 1 19 13 60 .05 | 876 1225 igr n/a| 0 0 0 46 -15 -20 .05 6 6 | 11367 -1457 25 75 | 0 0 1 4 7 14 .01 | 1155 1780 jpl 127| 1 0 -2 28 -27 12 .50 16 16 | 2032 -253 20 98 | 0 0 1 18 27 30 .04 | 1769 1802 mit 255| 1 -1 0 13 -10 23 -.23 14 12 | 117 -394 25 113 | 0 1 1 25 36 11 .03 | 733 1384 ngs 226| 0 0 0 -44 82 -31 -.33 12 8 | -400 -193 2817 4757 | 0 0 1 23 19 11 .04 | 401 585 sio 110| -1 1 5 48 -16 -5 .01 18 17 | --- --- --- --- | 1 1 1 22 31 16 .02 | --- --- Table 1.1495.b GPS week : 1495 MJD: 54709.000-54715.000 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 ------+------------------------------------+------------------------------------------ 2 | 6 6 6 6 6 6 6 | 3 | 8 5 6 6 6 6 8 | 4 | 6 4 6 5 5 5 4 | 5 | 7 7 8 7 8 7 6 | 6 | 6 6 7 7 6 6 6 | 7 | 6 5 6 6 6 7 6 | 8 | 5 7 4 3 3 4 4 | 9 | 4 4 4 4 4 4 4 | 10 | 5 5 4 3 4 4 4 | 11 | 5 5 7 8 5 5 5 | 12 | 6 5 6 5 5 6 6 | 13 | 5 5 5 5 5 6 5 | 14 | 5 4 5 5 4 4 4 | 15 | 6 6 6 6 7 6 6 | 16 | 7 7 7 6 6 6 6 | 17 | 6 5 6 5 5 5 5 | 18 | 6 6 6 6 6 6 6 | 19 | 6 6 5 6 7 9 6 | 20 | 6 6 5 5 5 5 5 | 21 | 6 6 6 6 6 6 6 | 22 | 6 5 6 5 5 5 5 | 23 | 6 6 6 6 6 6 6 | 24 | 4 4 4 4 4 3 4 | 25 | 7 6 6 6 7 7 8 | 26 | 6 7 8 5 5 5 5 | 27 | 5 4 4 3 3 4 4 | 28 | 6 6 6 6 6 6 5 | 29 | 6 6 6 6 5 5 5 | 30 | 4 4 4 4 4 4 3 | 31 | 7 6 6 6 6 6 5 | 32 | 4 4 3 4 4 4 4 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1495.0 GPS week: 1495 Day: 0 MJD: 54709.000 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 217| 1 1 1 56 -6 -42 -.26 13 11 | -811 19 16 98 | 49 -10 | emr 75| 0 1 -3 -97 30 -14 .39 15 15 | -569 -2566 18 124 | 21 -22 | esa 115| 0 -1 3 -59 -57 -15 .27 13 13 | -8261 -628 19 128 | 19 30 | gfz 200| 0 0 -4 36 22 127 -.09 15 15 | 610 -594 27 127 | -8 -8 | grg 80| -2 0 -4 30 11 -136 .98 47 35 | -793 -53 130 236 | 12 -43 | igr n/a| 0 0 2 45 -10 -36 .05 6 6 | 13505 -3573 29 70 | -40 12 | jpl 127| 1 0 -2 -10 -18 -4 .53 15 15 | 962 -2459 17 82 | 57 16 | mit 255| 1 -2 -2 56 -52 27 -.23 14 13 | -605 223 21 107 | 5 4 | ngs 226| 0 0 2 -48 91 -51 -.30 12 9 | -276 -528 2602 3636 | -55 -24 | sio 110| -3 0 4 71 -56 -38 .03 20 17 | --- --- --- --- | -27 44 | Table 2.1495.1 GPS week: 1495 Day: 1 MJD: 54710.000 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 217| 0 0 2 65 -37 12 -.25 10 9 | -32 -969 24 105 | 12 43 | emr 75| 0 0 -1 -75 25 -13 .36 15 15 | -949 -1066 20 108 | 41 -38 | esa 115| 1 0 4 -65 -70 -21 .23 12 11 | -6173 -1320 20 125 | 35 12 | gfz 200| -1 1 -5 -1 39 42 -.10 15 15 | 447 -47 29 142 | -22 4 | grg 80| 2 1 -2 39 28 -64 .88 37 35 | -41 -1001 106 221 | -24 24 | igr n/a| 1 1 0 43 -13 -31 .05 6 6 | 12042 -2390 24 72 | -10 -4 | jpl 127| 1 0 -2 43 -22 19 .48 15 15 | 604 -1503 21 85 | 26 -10 | mit 255| 1 -2 -1 -18 25 0 -.20 16 14 | 603 -1915 34 153 | 21 -27 | ngs 226| 0 0 -2 -2 60 -40 -.27 11 7 | -34 -998 2850 5245 | -68 -96 | sio 110| -1 0 5 65 -55 -10 .04 21 17 | --- --- --- --- | -27 65 | Table 2.1495.2 GPS week: 1495 Day: 2 MJD: 54711.000 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 217| 0 0 2 54 -18 -35 -.22 11 9 | -1191 1522 32 117 | 46 21 | emr 75| 1 -1 -2 -109 33 -1 .32 16 16 | -817 2331 22 133 | 33 -21 | esa 115| 2 0 0 -47 -91 -5 .31 12 12 | -9464 277 25 117 | 26 20 | gfz 200| 0 0 -3 53 34 24 -.01 15 15 | 132 86 26 127 | -42 -4 | grg 80| 0 4 -3 52 35 59 .88 42 34 | -1182 1467 110 224 | 35 -26 | igr n/a| 1 0 0 43 -1 -31 .07 7 6 | 10450 837 24 59 | -35 3 | jpl 127| 0 0 -2 23 6 29 .44 17 17 | -174 1876 23 108 | -4 -37 | mit 255| 0 -1 0 25 -23 25 -.23 13 12 | -495 1238 27 103 | -9 11 | ngs 226| 0 0 0 -74 97 -23 -.31 14 10 | -612 -151 2513 5116 | -7 1 | sio 110| -2 0 7 58 -29 4 -.00 18 17 | --- --- --- --- | 12 29 | Table 2.1495.3 GPS week: 1495 Day: 3 MJD: 54712.000 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 217| 0 1 2 57 -31 -7 -.22 10 9 | 46 -897 31 97 | 0 40 | emr 75| 0 -1 -5 -107 12 17 .36 16 16 | 1645 -1858 30 139 | 50 -32 | esa 115| 0 -1 2 -35 -53 -18 .25 10 9 | -8695 -1536 25 125 | 30 -11 | gfz 200| -1 1 -5 27 39 50 -.13 16 16 | 446 51 27 121 | -20 -16 | grg 80| 0 1 -4 74 0 -10 .98 35 30 | 55 -935 93 231 | -1 -42 | igr n/a| 0 0 0 41 -23 1 .03 6 5 | 11800 -2961 26 78 | -21 12 | jpl 127| 1 0 0 31 -5 -37 .49 15 15 | 2207 -1727 21 92 | 12 -23 | mit 255| 1 -1 0 -1 -64 16 -.20 14 13 | 436 -759 31 105 | 10 23 | ngs 226| 0 0 -1 -38 116 -19 -.39 12 8 | -215 -702 2779 4090 | -70 -124 | sio 110| 0 0 6 55 -7 6 .02 16 15 | --- --- --- --- | -13 20 | Table 2.1495.4 GPS week: 1495 Day: 4 MJD: 54713.000 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 217| 0 0 0 61 -34 -3 -.25 10 8 | 1120 -1378 27 104 | -14 39 | emr 75| 1 -2 -2 -78 5 38 .36 15 15 | 1221 1630 23 135 | -10 13 | esa 115| 0 0 3 -39 -65 -5 .26 10 9 | -8972 181 25 133 | 13 52 | gfz 200| -1 1 -5 20 43 -38 -.07 16 16 | 743 -599 28 130 | -34 13 | grg 80| 0 2 -2 68 29 -71 1.01 40 34 | 1140 -1452 99 212 | -19 10 | igr n/a| 0 0 0 52 -23 -14 .04 6 5 | 10370 872 27 91 | -68 32 | jpl 127| 1 -1 -1 30 -23 1 .49 16 16 | 2057 2114 21 92 | -9 -11 | mit 255| 1 0 0 0 20 28 -.25 13 11 | 1245 -2194 28 116 | -5 -18 | ngs 226| 2 0 1 -34 71 -27 -.34 11 7 | 88 97 2597 4808 | 0 -7 | sio 110| 0 2 3 44 23 -8 .00 17 17 | --- --- --- --- | 19 -4 | Table 2.1495.5 GPS week: 1495 Day: 5 MJD: 54714.000 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 217| 0 0 0 68 -27 -1 -.25 11 9 | -1485 1754 17 92 | -1 33 | emr 75| 1 -4 0 -100 -27 23 .36 15 15 | 2483 257 17 119 | 14 31 | esa 115| 0 0 1 -56 -38 -32 .26 11 11 | -9817 2076 18 118 | -10 24 | gfz 200| -2 0 -4 68 55 -35 -.07 16 16 | -196 998 26 132 | -33 -26 | grg 80| 3 6 0 72 23 -36 .98 35 30 | -1465 1675 100 207 | -12 28 | igr n/a| 0 0 0 44 -18 -5 .06 6 6 | 10899 -890 24 72 | -40 15 | jpl 127| 0 0 -3 34 -56 60 .54 16 16 | 3756 538 19 91 | 20 25 | mit 255| 1 0 0 31 2 29 -.26 14 12 | -702 1257 17 94 | -6 -23 | ngs 226| 1 0 0 -69 65 -34 -.31 11 7 | -1027 673 2849 5162 | 62 38 | sio 110| 0 4 4 41 12 7 .00 18 16 | --- --- --- --- | 44 6 | Table 2.1495.6 GPS week: 1495 Day: 6 MJD: 54715.000 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 217| 0 -1 0 74 -15 -2 -.25 12 9 | -369 -245 21 107 | -28 31 | emr 75| 0 0 0 -71 -32 36 .32 15 15 | 3199 -657 16 112 | -27 24 | esa 115| 1 -1 1 -40 -27 -2 .27 11 10 | -9671 830 18 122 | -7 7 | gfz 200| -1 0 -7 9 44 -62 -.11 15 15 | 300 17 25 134 | -27 -17 | grg 80| 0 0 -4 28 38 -36 .96 35 30 | -328 -359 98 179 | -35 -29 | igr n/a| 0 0 0 51 -14 -25 .05 6 6 | 10505 -2097 25 87 | -57 6 | jpl 127| 1 -1 -3 45 -73 20 .55 15 15 | 4814 -612 18 142 | -2 30 | mit 255| 1 0 1 1 19 35 -.27 13 12 | 337 -609 23 114 | 4 -22 | ngs 226| 1 0 1 -43 76 -25 -.35 12 9 | -730 257 3531 5244 | 27 16 | sio 110| 0 2 5 4 -4 1 .00 18 17 | --- --- --- --- | 26 29 | 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 3.1495.0 GPS week: 1495 Day: 0 MJD: 54709.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 12 13 19 66 5 11 13 11 34 5 | 18 26 25 28 55 22 26 23 21 32 20 3E | 36 19 17 15 68 8 13 13 23 18 8 | 50 44 41 35 44 36 40 34 41 48 37 4 | 8 14 12 14 29 5 8 13 8 34 5 | 26 36 34 29 29 31 32 32 28 42 29 X5 | 11 16 14 15 --- 6 --- 14 18 --- 6 | 19 27 25 26 --- 22 --- 22 23 --- 20 6E | 15 17 17 15 33 8 13 13 19 18 6 | 52 59 56 57 55 53 63 60 53 56 54 7M | 12 15 17 21 24 5 14 9 9 20 5 | 24 38 35 37 37 32 29 28 30 26 29 8M | 9 11 13 10 31 7 8 12 11 30 5 | 33 37 36 33 39 33 33 40 35 39 34 9 | 9 9 6 9 48 4 11 12 8 13 3 | 22 24 24 22 31 23 23 28 22 24 21 10 | 8 12 12 11 36 4 7 12 8 22 4 | 23 27 30 20 26 25 25 25 29 26 25 11 | 11 12 10 21 46 4 14 7 7 15 4 | 37 43 45 36 49 38 37 36 35 33 36 12 | 12 17 17 16 39 7 15 13 11 19 5 | 27 38 22 34 52 29 36 23 25 23 26 13E | 9 13 14 14 18 4 14 13 9 13 4 | 17 29 24 24 31 20 26 20 22 18 19 14E | 9 14 9 10 22 6 18 19 8 11 5 | 11 22 18 17 26 16 23 20 20 17 16 15E | 11 17 14 12 99 6 23 18 11 22 6 | 41 45 42 45 79 42 46 49 42 38 42 16 | 16 24 16 17 35 7 21 12 14 23 6 | 27 46 35 40 37 34 44 27 30 30 32 17E | 11 14 14 14 68 8 14 21 12 19 5 | 21 27 18 25 32 22 26 28 26 30 21 18 | 13 15 14 18 33 6 19 13 11 28 6 | 18 33 23 31 38 24 34 21 24 22 22 19 | 17 19 13 15 54 7 16 14 12 15 5 | 48 66 65 61 60 59 61 54 60 60 59 20 | 9 15 17 18 29 4 15 11 13 20 5 | 20 29 29 30 36 25 30 22 26 26 22 21 | 11 15 11 16 60 5 18 18 11 18 5 | 22 36 30 32 48 30 36 27 26 27 27 22 | 11 15 13 18 25 5 16 14 13 18 5 | 17 29 23 29 34 22 30 22 24 20 20 23E | 11 17 15 9 25 5 20 14 11 13 5 | 15 26 21 17 35 18 26 20 21 19 17 24M | 9 10 7 12 29 4 8 10 10 16 4 | 26 28 28 23 31 27 23 27 30 26 25 X25 | 8 13 20 15 --- 8 --- 15 17 --- 6 | 18 26 32 27 --- 23 --- 18 25 --- 21 26E | 15 17 14 17 65 8 14 20 16 20 6 | 47 55 54 53 68 52 56 60 49 65 52 27M | 8 11 13 10 23 6 7 8 11 23 4 | 19 29 29 24 36 24 28 20 24 21 23 28 | 9 16 16 18 29 8 14 12 15 25 6 | 22 37 27 37 46 27 35 25 21 31 25 29E | 25 18 14 12 89 5 18 13 8 15 6 | 68 81 77 84 124 74 79 78 75 83 77 30 | 9 14 8 12 36 5 12 13 7 17 4 | 16 28 21 24 30 19 26 22 18 18 18 31 | 11 19 12 21 27 7 19 20 15 19 6 | 17 33 26 27 31 22 29 26 21 18 20 32 | 5 12 10 9 23 6 10 11 7 9 3 | 17 20 21 21 22 20 22 16 17 20 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 13 15 13 15 46 6 15 14 12 20 |T 27 36 32 33 43 30 35 30 30 32 29 WRMS | 11 15 13 15 35 6 15 13 9 17 |NE 21 31 27 29 37 25 31 24 24 26 23 MEDI | 11 15 14 15 33 6 14 13 11 19 |MD 22 33 29 29 37 25 30 26 26 26 25 Table 3.1495.1 GPS week: 1495 Day: 1 MJD: 54710.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 12 10 21 38 6 12 13 8 32 5 | 16 25 21 29 33 20 24 18 19 30 18 3E | 12 12 10 14 64 7 13 8 20 14 5 | 19 30 27 27 35 25 33 22 26 28 22 4 | 8 11 7 12 23 4 8 10 9 24 4 | 21 27 28 26 29 24 27 24 23 33 23 X5 | 12 16 11 19 --- 10 --- 17 14 --- 6 | 25 29 27 35 --- 25 --- 25 28 --- 25 6E | 17 15 12 14 50 7 13 15 19 16 6 | 40 46 45 45 53 44 47 46 46 48 43 7 | 11 13 14 21 34 7 16 13 8 17 5 | 23 30 22 28 33 26 27 21 24 19 22 8 | 7 13 14 10 36 10 14 27 10 50 7 | 66 67 70 69 53 66 70 72 70 81 67 9 | 8 9 9 9 43 5 9 18 9 10 4 | 17 20 21 21 27 21 20 22 23 22 18 10 | 9 11 10 12 28 4 7 12 6 26 4 | 19 27 27 23 34 21 23 23 26 28 22 X11 | 10 16 10 23 51 9 --- 7 8 12 5 | 25 36 30 25 44 28 --- 22 23 21 23 12 | 9 15 12 18 37 7 18 16 8 17 5 | 24 29 18 30 36 23 31 19 19 22 20 13E | 9 20 12 9 23 6 11 14 10 10 4 | 11 29 17 18 30 16 23 19 22 16 16 14E | 7 12 9 9 23 5 17 15 8 10 4 | 12 23 15 17 20 15 24 16 12 14 13 15E | 10 14 16 12 22 6 23 22 12 21 6 | 30 35 32 32 45 32 36 36 31 33 30 16 | 14 22 15 19 33 6 23 14 14 22 6 | 18 38 25 32 34 26 37 22 24 20 24 17E | 7 13 10 13 24 7 14 21 13 12 5 | 20 29 18 23 27 21 29 30 23 28 22 18 | 11 16 13 21 30 7 17 12 11 27 6 | 15 32 19 30 36 22 30 18 17 16 18 19 | 14 19 14 14 73 6 17 13 12 27 6 | 67 75 73 69 84 68 74 71 67 72 69 20 | 11 15 13 21 29 7 15 12 11 18 5 | 13 25 18 24 30 17 25 14 14 18 13 21 | 11 13 12 18 24 6 18 16 10 19 5 | 15 26 23 24 36 21 30 21 20 20 19 22 | 11 13 13 21 27 6 14 12 11 16 5 | 13 26 18 28 31 19 28 19 20 16 16 23E | 9 19 13 9 26 5 19 20 11 13 5 | 11 28 17 14 37 15 26 17 19 18 14 24 | 8 12 7 12 35 6 10 8 9 19 4 | 24 24 25 23 19 24 21 25 27 31 23 X25 | 7 15 13 15 --- 10 --- 13 17 --- 6 | 14 22 19 17 --- 16 --- 17 26 --- 15 26E | 15 20 13 15 65 9 17 26 13 25 6 | 69 70 70 69 86 71 74 70 61 76 67 27 | 5 10 9 9 25 6 9 10 6 16 3 | 14 21 20 16 27 18 22 16 19 16 16 28 | 7 14 14 19 30 7 12 13 12 27 5 | 17 28 20 26 41 20 25 20 21 28 17 29E | 13 26 12 11 32 5 20 13 9 16 5 | 44 53 42 50 49 43 51 42 42 41 43 30 | 6 10 7 11 32 7 12 15 7 14 3 | 16 19 17 21 24 17 23 23 18 23 16 31 | 11 15 10 20 30 5 18 20 12 19 6 | 13 25 18 21 35 16 27 18 15 16 14 32 | 7 12 5 8 22 6 10 10 11 9 3 | 12 16 15 13 23 15 17 13 16 14 11 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 15 12 15 37 6 15 16 11 21 |T 23 32 27 29 37 26 33 27 27 29 25 WRMS | 9 15 11 15 35 6 15 14 7 17 |NE 17 26 21 25 32 20 26 19 20 21 18 MEDI | 9 14 12 14 30 6 14 13 11 17 |MD 18 28 21 26 34 21 27 22 23 22 20 Table 3.1495.2 GPS week: 1495 Day: 2 MJD: 54711.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 16 10 18 33 6 16 12 11 31 5 | 18 26 20 26 33 20 25 17 20 28 18 3E | 11 13 12 12 63 5 15 9 24 14 5 | 18 31 27 29 43 26 34 23 34 28 24 4 | 9 28 11 15 33 11 14 15 16 18 6 | 23 41 26 21 26 30 31 29 27 34 25 X5 | 10 30 13 16 --- 9 --- 15 12 --- 7 | 16 31 24 23 --- 21 --- 21 20 --- 16 6E | 15 18 13 13 53 7 17 16 25 14 6 | 33 43 38 38 46 39 50 41 46 45 39 7 | 10 14 15 22 37 6 18 10 14 15 5 | 25 33 28 27 33 28 27 26 34 23 26 8 | 9 13 10 10 27 4 9 9 11 19 4 | 29 37 34 31 42 32 36 35 36 36 32 9 | 8 11 9 9 37 7 12 12 9 12 4 | 19 24 27 20 28 24 23 26 22 23 21 10 | 6 12 9 13 44 5 11 11 9 15 4 | 17 18 21 14 27 16 21 21 21 21 17 X11 | 11 19 11 25 74 9 --- 8 11 --- 6 | 27 39 33 32 49 31 --- 29 27 --- 28 12 | 9 20 15 17 37 6 21 11 10 17 5 | 22 31 14 30 40 20 30 19 17 20 18 13E | 8 15 12 9 33 4 18 12 14 11 4 | 15 30 20 20 31 21 28 21 30 17 20 14E | 7 11 11 10 26 6 18 14 9 12 4 | 12 23 21 18 28 17 23 19 18 18 16 15E | 13 17 16 14 34 6 23 18 16 19 6 | 33 42 30 33 33 34 42 34 46 35 35 16 | 13 21 15 19 40 9 25 15 13 21 6 | 24 40 28 37 38 31 42 25 26 26 27 17E | 8 19 12 12 29 6 18 19 15 20 5 | 18 29 19 22 25 20 28 21 21 23 17 18 | 9 19 15 19 31 6 19 13 13 26 6 | 16 32 19 28 36 19 31 18 18 16 18 19E | 12 15 13 15 97 8 18 11 11 14 5 | 42 56 50 50 100 49 51 48 48 51 48 20 | 9 14 9 19 31 7 15 9 9 17 4 | 16 27 20 27 36 21 27 16 21 22 18 21 | 10 14 11 18 28 6 20 16 10 18 5 | 19 33 25 29 37 25 32 24 22 23 23 22 | 11 16 14 19 34 6 17 12 12 16 5 | 16 29 19 27 37 19 29 21 24 16 19 23E | 9 19 14 11 20 6 20 17 14 13 5 | 16 31 21 20 32 21 29 22 29 19 19 24 | 7 12 6 15 39 6 10 11 7 19 4 | 28 29 26 28 31 28 23 31 30 27 27 X25 | 9 15 14 13 --- 13 --- 10 12 --- 5 | 15 29 28 27 --- 24 --- 19 27 --- 21 26E | 30 17 16 16 91 12 18 23 17 23 8 | 78 84 81 79 67 74 83 85 80 86 80 27 | 7 11 9 9 21 4 9 6 11 13 3 | 17 26 23 19 27 22 23 21 26 19 21 28 | 8 16 16 21 26 7 13 11 17 24 6 | 17 32 21 31 42 23 27 20 26 29 20 X29E | 12 22 9 13 25 7 --- 12 11 15 5 | 31 41 36 37 34 34 --- 35 37 36 34 30 | 7 12 8 12 14 5 13 14 7 13 4 | 15 19 21 18 25 17 19 19 15 18 15 31 | 9 15 10 23 36 7 20 17 12 15 5 | 15 28 22 25 38 20 28 22 17 18 17 32 | 5 12 6 8 18 7 9 9 9 10 3 | 16 22 18 18 23 20 18 17 23 21 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 16 12 15 42 7 17 13 14 18 |T 22 33 27 28 37 26 31 26 28 27 25 WRMS | 9 16 12 15 34 6 17 12 10 17 |NE 18 29 22 25 34 22 27 21 21 22 19 MEDI | 9 15 12 15 33 6 17 12 12 15 |MD 18 31 24 27 34 23 28 22 26 23 21 Table 3.1495.3 GPS week: 1495 Day: 3 MJD: 54712.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 7 16 9 19 33 6 14 14 11 31 5 | 17 24 22 23 32 17 23 17 15 26 16 3E | 12 13 7 15 57 4 14 9 25 14 5 | 17 31 25 26 35 24 32 22 39 27 24 4 | 6 13 7 17 40 6 8 18 10 16 4 | 25 26 28 23 31 24 29 29 20 29 24 X5 | 13 15 7 18 --- 5 --- 15 18 --- 6 | 21 32 26 31 --- 22 --- 24 26 --- 23 6E | 14 23 10 14 46 5 15 17 26 16 6 | 40 50 47 50 63 46 53 51 56 48 46 7 | 11 14 12 21 29 6 19 11 11 16 5 | 25 36 32 32 38 27 30 29 26 26 28 8 | 6 9 5 9 14 5 8 9 7 14 3 | 42 41 41 39 52 40 38 43 45 41 41 9 | 7 12 6 8 30 5 7 11 10 11 3 | 19 22 20 19 25 19 20 24 23 20 20 10 | 5 10 6 10 36 5 7 13 6 12 3 | 26 23 24 22 28 23 25 25 23 26 23 X11 | 28 17 10 26 50 8 --- 10 13 20 8 | 44 33 33 31 45 28 --- 30 31 38 31 12 | 8 15 12 19 35 6 19 12 10 18 5 | 23 31 23 34 42 25 36 21 23 21 23 13E | 9 12 11 12 24 4 15 15 11 12 4 | 18 24 22 25 32 19 28 23 17 22 19 14E | 9 13 9 10 28 5 16 17 7 12 4 | 17 22 18 19 32 17 23 19 18 18 16 15E | 10 18 12 13 35 6 22 22 12 16 6 | 40 47 43 45 36 45 51 44 47 42 44 16 | 11 22 13 19 33 6 20 14 13 19 6 | 26 42 32 39 34 32 43 28 33 26 32 17E | 12 22 10 13 30 4 17 13 12 13 5 | 17 31 17 22 32 19 25 20 23 21 18 18 | 10 18 11 20 27 6 20 14 11 24 6 | 19 31 21 30 36 23 31 19 22 18 20 19E | 14 20 12 13 39 8 17 15 12 20 5 | 70 71 72 70 79 71 73 71 71 74 70 20 | 10 14 11 22 29 5 14 12 12 16 5 | 18 26 19 29 37 18 27 18 21 25 19 21 | 10 18 11 19 28 8 18 13 10 19 5 | 18 30 27 26 34 24 32 22 19 22 21 22 | 9 15 12 20 33 5 15 12 10 15 5 | 19 28 20 27 37 19 29 22 20 18 19 23E | 10 19 13 14 13 5 21 20 14 14 6 | 18 28 22 21 32 18 30 23 19 18 18 24 | 6 11 7 14 22 5 8 13 9 12 3 | 28 27 29 22 29 28 28 32 30 28 26 X25 | 10 13 13 11 --- 10 --- 12 14 --- 5 | 21 28 24 21 --- 24 --- 19 29 --- 22 26E | 13 15 9 14 92 9 18 14 15 13 5 | 80 83 83 80 99 82 90 83 77 84 81 27 | 6 10 6 9 15 4 10 8 6 12 3 | 16 25 20 16 25 18 26 17 19 15 18 28 | 10 16 12 21 26 6 15 12 10 25 5 | 17 27 22 32 45 21 30 17 18 29 18 29E | 12 21 12 12 18 5 19 13 12 13 5 | 24 34 19 25 24 22 31 25 26 29 24 30 | 5 12 6 10 22 4 11 11 7 10 3 | 15 24 17 18 26 16 23 18 18 16 16 31 | 10 15 9 27 28 5 15 16 9 14 5 | 17 30 23 27 34 20 28 24 19 21 19 32 | 7 13 6 12 21 4 13 10 9 7 3 | 14 18 18 20 21 16 22 16 18 19 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 16 10 16 35 6 15 14 12 16 |T 26 33 28 30 38 27 34 28 28 29 26 WRMS | 9 16 9 16 30 5 15 13 8 15 |NE 21 27 23 26 33 21 28 21 22 23 21 MEDI | 10 15 10 14 29 5 15 13 11 14 |MD 19 30 23 26 34 23 29 23 23 26 22 Table 3.1495.4 GPS week: 1495 Day: 4 MJD: 54713.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 7 13 11 20 47 7 15 14 15 32 6 | 16 25 21 25 39 19 23 17 19 24 16 3E | 10 15 9 17 63 5 15 8 24 21 5 | 16 32 22 25 38 21 31 21 32 30 21 4 | 7 11 10 14 89 7 8 18 7 16 4 | 24 26 28 21 57 22 25 26 18 23 22 X5 | 16 21 20 17 --- 12 --- 15 15 --- 7 | 10 30 30 27 --- 23 --- 15 30 --- 18 6E | 13 14 10 16 63 4 14 13 22 19 5 | 29 42 36 41 45 34 46 40 38 42 35 X7 | 9 15 10 25 30 8 --- 10 6 17 5 | 20 28 20 26 35 20 --- 19 15 17 17 8 | 7 9 4 10 17 5 9 8 6 15 3 | 24 27 24 22 27 22 26 29 24 26 24 9 | 7 13 7 8 27 4 9 11 8 10 3 | 19 24 22 23 33 23 24 26 25 24 22 10 | 6 8 7 14 35 5 7 13 10 14 3 | 18 21 21 16 25 19 19 21 19 17 17 11 | 10 15 11 23 56 6 19 7 7 13 5 | 32 35 36 28 41 27 38 28 25 27 28 12 | 7 17 11 19 38 6 19 12 11 17 5 | 20 31 19 31 44 22 31 18 16 19 19 13E | 9 16 9 11 24 7 16 19 9 12 5 | 12 24 16 16 30 15 23 18 15 16 13 14E | 5 11 9 13 33 5 17 12 11 10 4 | 12 20 15 19 31 14 21 14 14 13 12 15E | 10 16 16 13 25 6 23 23 13 18 6 | 30 37 36 33 43 32 37 40 33 32 32 16 | 10 23 12 20 39 7 24 12 12 20 6 | 20 39 21 32 33 25 39 22 23 23 24 17E | 7 17 9 14 34 5 14 11 10 14 4 | 25 30 21 24 27 21 24 25 27 25 22 18 | 10 18 10 22 29 7 18 13 11 24 5 | 16 31 20 32 36 21 31 17 17 11 18 19E | 26 21 10 15 30 8 21 12 10 28 7 | 69 82 75 75 60 75 78 79 76 86 75 20 | 9 15 11 20 28 5 17 11 9 16 5 | 16 24 20 25 29 16 25 17 17 19 15 21 | 9 16 11 19 28 7 18 14 13 17 5 | 14 32 23 26 36 21 30 19 20 18 18 22 | 9 15 11 22 29 6 16 13 7 16 5 | 15 28 21 27 33 19 28 22 16 17 17 23E | 10 19 13 13 15 6 23 20 12 13 6 | 12 24 16 17 28 15 26 21 19 17 13 24 | 9 13 6 12 30 5 10 9 8 13 3 | 35 35 33 35 31 33 31 36 35 35 33 X25 | 10 20 12 12 --- 16 --- 15 17 --- 6 | 12 29 20 18 --- 20 --- 18 17 --- 14 26E | 11 15 11 12 81 6 17 10 12 13 4 | 42 50 49 48 54 45 55 44 42 51 45 27 | 7 11 7 10 16 5 9 7 4 14 3 | 11 22 17 14 26 14 20 15 13 14 13 28 | 9 16 11 19 34 6 15 9 11 26 5 | 18 31 21 30 47 22 32 17 23 31 20 29E | 11 22 10 11 23 5 18 12 9 17 5 | 25 39 29 30 31 26 32 28 31 32 27 30 | 5 12 7 11 19 5 10 10 9 12 3 | 16 22 19 21 29 17 18 19 18 19 16 31 | 7 16 12 23 35 5 17 13 12 18 5 | 16 28 23 23 33 19 27 19 15 17 16 32 | 5 14 7 9 22 4 13 11 8 8 3 | 11 16 14 11 19 11 16 14 15 15 11 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 15 10 16 40 6 16 13 11 17 |T 21 31 25 27 35 23 30 24 24 25 22 WRMS | 8 15 9 16 34 5 16 11 7 17 |NE 17 27 22 24 35 20 27 19 19 20 18 MEDI | 9 15 10 14 30 6 16 12 10 16 |MD 18 29 21 25 33 21 27 21 19 23 18 Table 3.1495.5 GPS week: 1495 Day: 5 MJD: 54714.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 7 15 11 22 22 7 14 14 10 31 6 | 14 23 16 23 29 16 22 14 15 24 13 3E | 13 14 10 14 52 5 15 10 23 14 5 | 19 28 23 22 33 21 30 19 32 23 20 4 | 6 11 7 16 25 5 7 19 7 16 4 | 18 26 21 19 32 21 21 25 21 20 19 X5 | 12 12 17 15 --- 10 --- 13 23 --- 7 | 20 26 23 19 --- 27 --- 21 33 --- 19 6E | 12 15 14 14 47 5 17 13 23 17 6 | 37 51 46 41 50 44 54 48 50 49 44 X7 | 12 19 13 24 38 9 --- 14 9 --- 6 | 45 50 48 50 45 47 --- 47 48 --- 46 8 | 10 12 8 13 24 5 7 6 7 13 3 | 33 33 34 31 43 29 30 33 31 34 32 9 | 8 10 8 9 27 5 8 11 9 14 3 | 17 18 21 17 21 19 19 19 20 18 16 10 | 8 9 9 15 32 5 9 13 7 8 3 | 21 27 25 21 28 21 24 24 23 21 22 11 | 9 14 12 24 54 6 16 9 8 12 5 | 20 27 24 25 40 21 29 19 20 22 19 12 | 8 17 14 19 37 8 18 13 10 16 5 | 20 29 18 28 41 21 29 17 18 18 18 13E | 10 15 12 12 18 8 16 26 12 17 5 | 12 21 18 16 30 14 22 23 13 24 13 14E | 6 11 10 10 26 3 16 13 10 9 4 | 15 20 18 17 26 15 21 14 14 16 14 15E | 13 15 12 14 28 6 23 14 10 15 5 | 41 46 44 46 39 46 55 49 47 43 45 16 | 12 21 13 21 32 8 20 11 11 20 6 | 21 37 23 32 33 25 36 23 26 24 25 17E | 10 15 10 13 28 6 18 9 9 11 4 | 22 27 22 23 30 21 28 22 23 23 21 18 | 9 17 13 19 29 7 19 14 10 25 5 | 16 32 22 29 34 21 33 17 16 15 18 19E | 28 23 14 18 48 13 23 13 12 42 8 | 95 114 110 111 112 108 110 108 111 118 108 20 | 11 16 11 20 24 7 17 13 8 18 5 | 13 26 15 24 27 16 25 13 14 21 13 21 | 10 17 11 17 25 7 19 13 10 18 5 | 15 32 22 24 35 20 31 16 16 18 18 22 | 9 14 12 20 36 6 17 11 9 16 5 | 15 27 18 25 36 18 27 19 16 14 16 23E | 11 19 14 11 20 7 23 24 13 14 6 | 12 23 18 15 29 12 24 18 14 16 11 24 | 5 12 9 11 25 5 8 8 4 12 3 | 23 26 29 26 29 24 23 25 25 22 24 X25 | 9 20 11 12 --- 14 --- 15 23 --- 7 | 12 31 17 22 --- 17 --- 15 24 --- 14 26E | 12 13 10 13 90 5 15 12 14 18 5 | 58 57 60 59 66 59 67 59 55 63 58 27 | 8 12 9 11 19 4 6 7 5 13 3 | 13 19 18 14 26 14 20 14 13 17 14 28 | 11 18 12 22 35 7 14 13 9 24 5 | 13 29 20 29 49 19 29 13 15 24 17 29E | 9 19 13 11 24 5 16 13 10 14 5 | 24 35 20 27 24 24 31 25 27 28 24 30 | 5 12 8 10 20 5 8 11 9 11 3 | 10 22 17 13 23 13 17 14 13 12 12 31 | 9 15 12 25 31 7 13 14 9 17 5 | 14 28 21 23 34 19 27 17 13 19 16 32 | 6 13 10 9 19 7 12 12 8 9 3 | 11 15 13 12 23 13 16 13 17 16 11 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 15 11 16 35 6 16 14 11 18 |T 23 32 27 28 36 25 32 25 26 27 24 WRMS | 9 15 11 16 30 6 16 12 7 16 |NE 15 26 19 22 32 19 25 17 18 19 16 MEDI | 9 15 11 14 28 6 16 13 10 15 |MD 18 27 21 24 33 21 27 19 20 21 18 Table 3.1495.6 GPS week: 1495 Day: 6 MJD: 54715.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 8 17 10 19 21 5 14 13 11 33 6 | 16 27 21 26 36 19 24 18 20 30 17 3E | 36 16 12 14 55 8 15 13 27 18 8 | 31 36 28 32 37 28 37 24 38 31 26 4 | 6 10 8 12 44 6 8 13 10 13 3 | 26 31 32 27 31 29 30 31 26 27 27 X5 | 10 18 8 12 --- 8 --- 11 14 --- 5 | 19 30 24 26 --- 25 --- 30 35 --- 24 6E | 12 14 10 14 53 8 16 16 22 20 6 | 44 55 52 56 63 53 59 55 55 62 52 X7 | 9 16 13 22 40 7 --- 11 11 15 5 | 34 38 33 36 33 30 --- 32 33 30 31 8 | 7 13 9 10 24 4 9 8 10 12 3 | 28 31 35 31 39 31 32 34 32 36 31 9 | 7 11 8 11 25 4 8 10 10 12 3 | 22 25 27 24 19 25 23 28 25 22 23 10 | 9 10 9 12 39 3 8 14 9 10 4 | 23 25 30 19 28 24 28 28 22 20 23 11 | 9 13 9 24 47 6 14 9 12 16 5 | 31 36 33 26 42 28 33 30 26 29 27 12 | 7 19 12 18 41 7 18 12 14 17 5 | 21 30 17 31 49 24 32 19 19 22 20 13E | 9 14 11 15 20 6 15 22 9 12 5 | 11 23 16 17 24 15 24 25 16 19 14 14E | 8 11 8 13 31 5 17 14 7 11 4 | 15 19 18 18 26 17 23 19 19 17 15 15E | 11 17 14 14 36 5 24 14 10 18 5 | 41 49 40 47 67 44 51 40 45 44 43 16 | 13 20 12 18 25 9 18 12 15 22 6 | 30 42 29 39 37 32 41 30 32 32 32 17E | 8 15 11 12 32 8 15 11 9 12 4 | 20 28 21 23 40 23 26 22 24 22 21 18 | 9 16 12 20 26 7 18 15 9 24 5 | 20 32 23 29 37 22 32 21 17 14 20 19E | 13 14 14 15 29 8 15 14 13 27 5 | 83 84 84 83 84 86 88 86 86 83 83 20 | 9 14 11 20 25 5 15 12 9 22 5 | 17 27 20 26 30 18 25 17 17 22 17 21 | 11 17 14 20 22 9 18 11 12 18 5 | 17 32 27 27 37 23 31 20 18 21 20 22 | 9 16 12 19 33 6 16 13 10 16 5 | 19 30 21 27 36 20 29 22 16 18 19 23E | 15 17 11 11 32 7 22 24 11 12 6 | 16 25 17 16 33 17 27 25 24 18 16 24 | 6 12 7 13 23 5 10 8 6 19 3 | 22 26 25 19 20 24 22 25 26 26 22 X25 | 9 29 15 13 --- 9 --- 20 12 --- 7 | 15 32 22 22 --- 19 --- 18 19 --- 16 26E | 12 13 11 12 86 5 17 12 12 22 5 | 63 64 64 65 65 62 68 62 60 64 63 27 | 10 11 8 11 20 5 7 9 9 12 3 | 15 21 21 16 25 15 22 18 13 18 16 28 | 9 14 11 21 27 6 16 11 10 23 5 | 17 29 21 32 47 23 31 18 19 28 20 29E | 14 20 10 9 24 6 19 10 10 16 5 | 49 54 48 53 32 52 53 53 58 58 51 30 | 6 12 5 10 21 6 9 9 7 13 3 | 18 25 21 21 26 19 22 23 19 17 18 31 | 8 14 10 21 28 6 13 14 10 18 5 | 21 31 23 24 35 23 29 23 24 22 21 32 | 6 12 9 9 18 6 11 10 11 15 4 | 12 14 14 11 19 12 14 14 13 15 10 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 15 11 15 35 6 15 13 12 18 |T 26 33 29 30 37 28 34 29 28 29 27 WRMS | 9 15 10 15 30 6 15 12 9 17 |NE 20 29 23 25 33 22 28 22 21 22 20 MEDI | 9 14 11 14 28 6 15 12 10 16 |MD 21 30 24 26 36 24 29 25 24 22 21 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 4.1495 GPS week: 1495 MJD: 54709.0-54715.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2973 |U 9 10 24 |U 5 9 25 |U 8 8 16 | emr | emr 2959 | 12 12 37 | 8 10 36 | 9 9 21 | esa | esa 2976 | 9 11 27 |U 5 7 23 | 9 7 17 | gfz | gfz 2937 |U 11 12 34 |U 12 12 30 |U 9 10 19 | igr | igr 2948 | 10 11 28 | 6 8 23 | 11 8 17 | igs | igs 2966 | 9 11 29 | 6 8 23 | 8 7 17 | jpl | jpl 2676 |U 10 11 32 |U 7 9 31 |U 9 8 20 | mit | mit 2976 |U 12 11 30 |U 7 12 28 |U 10 10 21 | 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 5.1495.0 GPS week: 1495 Day: 0 MJD: 54709.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2972 | 10 11 24 | 5 10 24 | 8 8 19 | emr | emr 2963 | 11 9 38 | 6 8 38 | 9 9 21 | esa | esa 2976 | 10 10 30 | 4 7 22 | 8 7 19 | gfz | gfz 2945 | 12 11 31 | 11 9 24 | 9 9 22 | igr | igr 2962 | 10 9 27 | 4 4 18 | 9 8 17 | igs | igs 2969 | 10 10 27 | 6 7 19 | 8 8 18 | jpl | jpl 2772 | 10 10 27 | 6 7 28 | 8 9 18 | mit | mit 2976 | 9 10 26 | 7 10 25 | 10 7 23 | Table 5.1495.1 GPS week: 1495 Day: 1 MJD: 54710.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2975 | 8 7 25 | 5 9 25 | 8 7 16 | emr | emr 2962 | 10 10 36 | 6 7 30 | 10 10 23 | esa | esa 2976 | 8 9 27 | 5 7 26 | 9 7 16 | gfz | gfz 2940 | 11 10 33 | 10 9 28 | 9 9 19 | igr | igr 2969 | 10 7 26 | 7 7 29 | 10 8 15 | igs | igs 2973 | 9 8 24 | 4 6 23 | 9 7 16 | jpl | jpl 2676 | 11 12 34 | 8 9 30 | 11 8 19 | mit | mit 2976 | 20 11 26 | 8 13 31 | 11 12 17 | Table 5.1495.2 GPS week: 1495 Day: 2 MJD: 54711.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2970 | 9 9 30 | 6 8 26 | 8 6 13 | emr | emr 2955 | 14 13 44 | 7 8 36 | 9 8 20 | esa | esa 2976 | 9 8 31 | 6 8 23 | 9 7 18 | gfz | gfz 2935 | 11 9 37 | 11 19 33 | 8 8 20 | igr | igr 2966 | 10 9 33 | 6 9 26 | 7 7 14 | igs | igs 2964 | 10 10 33 | 6 8 22 | 7 6 15 | jpl | jpl 2580 | 11 9 41 | 10 6 37 | 10 5 21 | mit | mit 2976 | 9 9 33 | 7 11 26 | 8 6 17 | Table 5.1495.3 GPS week: 1495 Day: 3 MJD: 54712.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 10 13 25 | 5 9 24 | 7 7 15 | emr | emr 2960 | 12 13 35 | 7 10 27 | 7 7 20 | esa | esa 2976 | 10 16 27 | 6 10 26 | 8 6 17 | gfz | gfz 2938 | 13 17 36 | 14 14 31 | 7 8 16 | igr | igr 2976 | 11 14 29 | 7 10 23 | 6 6 14 | igs | igs 2969 | 10 15 29 | 7 11 24 | 6 6 16 | jpl | jpl 2676 | 11 16 28 | 6 9 27 | 9 8 23 | mit | mit 2976 | 16 17 39 | 9 18 29 | 9 13 22 | Table 5.1495.4 GPS week: 1495 Day: 4 MJD: 54713.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 8 21 | 4 11 26 | 7 10 18 | emr | emr 2963 | 11 11 32 | 15 11 58 | 10 10 20 | esa | esa 2976 | 7 9 21 | 4 7 23 | 10 9 20 | gfz | gfz 2940 | 10 9 31 | 12 12 26 | 11 12 21 | igr | igr 2854 | 8 11 28 | 6 10 22 | 25 11 19 | igs | igs 2964 | 7 10 25 | 4 6 24 | 9 8 19 | jpl | jpl 2676 | 9 6 26 | 6 7 33 | 9 9 20 | mit | mit 2976 | 8 6 29 | 6 10 27 | 11 8 21 | Table 5.1495.5 GPS week: 1495 Day: 5 MJD: 54714.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2968 | 9 14 19 | 6 7 25 | 7 8 15 | emr | emr 2957 | 11 18 27 | 8 16 29 | 10 10 21 | esa | esa 2976 | 9 18 29 | 6 6 21 | 8 8 14 | gfz | gfz 2930 | 10 16 29 | 15 14 38 | 10 11 17 | igr | igr 2950 | 9 16 24 | 6 7 24 | 10 9 20 | igs | igs 2958 | 9 17 24 | 7 15 22 | 7 8 15 | jpl | jpl 2676 | 9 15 23 | 10 17 27 | 7 7 18 | mit | mit 2976 | 9 14 25 | 6 7 28 | 7 6 19 | Table 5.1495.6 GPS week: 1495 Day: 6 MJD: 54715.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 12 10 25 | 6 8 23 | 8 8 15 | emr | emr 2959 | 14 9 48 | 8 6 33 | 8 10 20 | esa | esa 2976 | 11 9 26 | 6 7 21 | 9 8 16 | gfz | gfz 2936 | 12 10 44 | 12 10 27 | 9 13 18 | igr | igr 2959 | 11 9 30 | 6 7 23 | 9 9 18 | igs | igs 2966 | 11 9 38 | 5 6 24 | 7 8 19 | jpl | jpl 2676 | 11 10 43 | 6 8 32 | 8 9 20 | mit | mit 2976 | 11 10 35 | 7 15 27 | 13 14 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 6.1495 GPS week: 1495 MJD: 54709.500-54715.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -25 -6 -6 -11 -5 | 3 14 | 23 25 42 65 7 | 1 emr uuuuu | 10 -15 118 -26 -6 | 37 40 | 18 25 73 123 5 | 3 esa uuuuu | -16 -12 154 -41 -6 | 31 34 | 15 19 73 104 5 | 1 gfz uuuuu | 11 29 5 34 13 | 13 24 | 19 13 47 46 9 | 7 grg xxxxx | 14 9 -16 9 -19 | 6 36 | 29 20 52 72 20 | 2 igr xxxxx | -8 42 9 42 0 | 6 16 | 12 18 60 69 3 | 2 irf xxxxx | 3 3 -45 20 -2 | 5 17 | 12 7 25 33 5 | 3 jpl uuuuu | 5 -11 -31 -37 -2 | 19 24 | 22 20 99 30 16 | 1 mit uuuuu | 11 0 -244 -18 4 | 14 22 | 28 14 50 82 5 | 5 ngs uuuuu | 31 19 -11 102 -2 | 13 22 | 49 50 61 61 9 | 2 sio uuuuu | -24 -2 -1 -33 2 | 53 56 | 31 28 47 83 5 | 6 Table 7.1495.0 GPS week: 1495 Day: 0 MJD: 54709.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | 11 -41 -3 -130 -17 | 4 15 emr uuuuu | 23 -13 119 81 0 | 32 36 esa uuuuu | -29 -11 89 11 -4 | 29 33 gfz uuuuu | 9 16 49 -1 19 | 4 16 grg xxxxx | 44 -4 -65 -22 -30 | 6 39 igr xxxxx | -11 48 36 102 1 | 4 14 irf xxxxx | 1 8 -38 79 3 | 0 15 jpl uuuuu | -15 -49 38 -5 -4 | 19 22 mit uuuuu | -3 3 -187 61 7 | 7 16 ngs uuuuu | 25 63 -53 76 -8 | 11 19 sio uuuuu | -43 35 -1 -154 7 | 44 48 Table 7.1495.1 GPS week: 1495 Day: 1 MJD: 54710.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -52 -10 -10 -3 -8 | 2 14 emr uuuuu | 29 -39 75 59 -8 | 34 38 esa uuuuu | -21 -33 176 -74 -10 | 30 33 gfz uuuuu | -13 24 -17 13 18 | 6 20 grg xxxxx | -33 26 30 -123 -27 | 6 39 igr xxxxx | -5 12 30 -93 1 | 5 16 irf xxxxx | -9 2 -74 11 1 | 2 17 jpl uuuuu | 1 -24 -29 -83 -25 | 21 25 mit uuuuu | 18 -19 -316 73 7 | 9 20 ngs uuuuu | 87 70 30 54 13 | 10 19 sio uuuuu | -74 29 42 -63 4 | 47 52 Table 7.1495.2 GPS week: 1495 Day: 2 MJD: 54711.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -17 -37 -45 55 -8 | 3 14 emr uuuuu | 25 -24 180 18 0 | 36 40 esa uuuuu | -16 -17 237 -258 3 | 30 34 gfz uuuuu | 8 51 -31 40 27 | 9 24 grg xxxxx | 30 -26 -11 86 -12 | 2 37 igr xxxxx | 1 44 -5 121 3 | 5 17 irf xxxxx | 4 9 -32 2 3 | 4 19 jpl uuuuu | 41 13 97 -65 -17 | 20 24 mit uuuuu | -7 18 -224 -58 9 | 12 23 ngs uuuuu | 3 16 -131 209 1 | 12 22 sio uuuuu | -25 -3 -30 96 4 | 50 55 Table 7.1495.3 GPS week: 1495 Day: 3 MJD: 54712.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -55 0 -8 -7 2 | 2 15 emr uuuuu | 17 -50 106 90 -6 | 38 41 esa uuuuu | -4 -30 47 46 -7 | 31 35 gfz uuuuu | 1 20 12 2 8 | 12 26 grg xxxxx | 27 1 22 14 12 | 6 34 igr xxxxx | -27 21 -17 54 2 | 5 17 irf xxxxx | -15 0 -82 -23 -2 | 6 18 jpl uuuuu | 8 -12 -7 -14 -7 | 19 24 mit uuuuu | -38 -10 -228 -155 7 | 14 23 ngs uuuuu | 109 70 14 75 -8 | 13 22 sio uuuuu | -35 13 62 -83 7 | 53 57 Table 7.1495.4 GPS week: 1495 Day: 4 MJD: 54713.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -25 9 70 21 -5 | 3 14 emr uuuuu | 1 5 -9 -80 -11 | 40 42 esa uuuuu | -38 -18 111 -25 -6 | 33 35 gfz uuuuu | 1 29 -5 37 15 | 16 25 grg xxxxx | 4 14 -107 68 -20 | 6 34 igr xxxxx | -18 63 -102 41 -1 | 8 16 irf xxxxx | 14 -5 -46 3 -4 | 8 16 jpl uuuuu | 25 4 3 -35 -2 | 19 24 mit uuuuu | 32 0 -277 -68 1 | 18 23 ngs uuuuu | 21 -5 28 112 5 | 13 22 sio uuuuu | 18 -24 20 9 1 | 57 59 Table 7.1495.5 GPS week: 1495 Day: 5 MJD: 54714.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -17 12 -60 49 -3 | 2 13 emr uuuuu | -15 -3 213 -108 -12 | 39 41 esa uuuuu | -8 21 230 -26 -10 | 32 34 gfz uuuuu | 42 44 82 15 9 | 19 29 grg xxxxx | -12 23 25 -20 -3 | 7 34 igr xxxxx | 1 51 88 53 0 | 8 16 irf xxxxx | 16 11 -23 28 -7 | 8 17 jpl uuuuu | -9 -9 -111 -8 20 | 18 23 mit uuuuu | 39 17 -287 -11 -1 | 19 25 ngs uuuuu | -22 -51 -4 35 -5 | 15 24 sio uuuuu | 10 -33 -74 27 -3 | 59 61 Table 7.1495.6 GPS week: 1495 Day: 6 MJD: 54715.500 AC LOD AC LOD CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS | [uas] [uas] [uas/d] [uas/d] [us]| [us] [us] ------------+----------------------------------------+------------------ cod uuuuu | -19 23 14 -60 1 | 3 12 emr uuuuu | -12 22 141 -244 -6 | 40 42 esa uuuuu | 5 2 191 37 -7 | 33 34 gfz uuuuu | 29 22 -53 131 -2 | 23 30 grg xxxxx | 41 30 -4 60 -51 | 8 34 igr xxxxx | 6 52 36 16 -6 | 9 16 irf xxxxx | 12 -5 -17 37 -8 | 10 16 jpl uuuuu | -18 -3 -205 -51 17 | 21 25 mit uuuuu | 34 -9 -188 32 -3 | 22 25 ngs uuuuu | -4 -32 37 155 -11 | 14 24 sio uuuuu | -17 -31 -25 -61 -7 | 61 62