Date: Thu, 22 May 2008 14:21:50 +0000 From: Jim Ray Subject: [IGSREPORT-16259] Wk 1478 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4835817e.7bqNgsGInPRoRuzM%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 22 May 07:22:05 PDT 2008 Message Number 16259 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1478 (May 04, 2008 - May 10, 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: igs1478[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1478[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1478[0-6].cls IGS GPS clock combination summary report. igs14787.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14787.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 | 4 24 ALIC MALI SUWN 0 | EMR | 2 0 | ESA | 4 24 CHUR 0 | GFZ | 7 29 DAV1 YELL 0 | MIT | ALIC STR2 1 | COD | 24 IENG 1 | ESA | 4 24 CHUR MAS1 1 | GFZ | 7 21 29 FAA1 KERG KIRU MAS1 SFER 1 | MIT | 4 7 TIXI 2 | ALL | 24 25 2 | COD | BRUS CEDU MAW1 UNBJ YELL 2 | ESA | MAW1 2 | GFZ | 2 4 7 21 29 DAV1 2 | JPL | 4 2 | MIT | 4 3 | COD | 4 ARTU BRUS IENG NRMD 3 | EMR | SFER 3 | GFZ | 7 29 FAA1 KERG MAS1 SSIA 3 | MIT | 24 SYOG 4 | COD | 4 24 NRC1 4 | EMR | 18 4 | ESA | 4 24 4 | GFZ | 7 24 29 NRC1 4 | JPL | LHAZ 4 | MIT | 21 DAEJ NRC1 5 | COD | 4 BOR1 METS ONSA 5 | ESA | 4 5 | GFZ | 7 29 ONSA WTZR YAKT 5 | MIT | 24 28 NTUS 6 | COD | 4 BOR1 BRUS 6 | EMR | 32 6 | ESA | 4 6 | GFZ | 7 21 29 BAN2 COCO KARR 6 | MIT | 24 DAEJ 5. 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 G08 | | 2 | | | | | | PRN G18 | | | | | | | 1 | 6. 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. 7. 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 .5 -1.1 -5 -11 -13 .06 EMR | 5.1 -16.4 -1.7 43 -16 6 .45 ESA | .2 2.5 2.2 42 16 22 .04 GFZ | 1.0 .2 .3 6 -25 -2 -.22 GRG | 7.3 -.3 -5.0 -19 -34 5 -.07 JPL | -1.0 -8.9 .7 -24 3 -50 .31 MIT | 8.8 -8.1 2.6 -14 -2 -4 -.01 NGS | 7.9 -2.1 -2.6 -22 -132 23 -1.06 SIO | 8.3 -4.7 -18.6 -67 -238 48 .30 8. 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. 9. 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. 10. 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 1.1478.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1478.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 2.1478.[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 3.1478.[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 5.1478.0-6). 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 1478 summary. (May 04, 2008 - May 10, 2008) Table 1.1478.a GPS week: 1478 MJD: 54590.000-54596.000 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 206| 1 -1 0 -7 -35 -21 -.19 12 11 | -438 48 18 73 | 0 0 0 15 23 15 .01 | 564 834 emr 68| 1 -1 4 -111 -31 -27 .43 20 20 | 1646 -771 24 89 | 1 1 0 46 15 14 .06 | 1044 2077 esa 114| 0 2 1 -71 -145 -4 .29 16 15 | -8893 -540 22 115 | 1 1 2 37 34 22 .04 | 631 1224 gfz 183| 0 0 -3 -9 -28 64 -.14 15 15 | 100 -154 21 120 | 0 0 1 15 30 35 .02 | 563 692 grg 82| 1 0 0 -22 -2 0 1.00 43 33 | -426 1 154 28908 | 2 1 3 31 31 53 .06 | 564 834 igr n/a| 0 0 0 -7 -70 -3 .06 7 7 | 19248 -1628 21 82 | 0 1 0 8 18 12 .03 | 1850 1939 jpl 118| -1 -1 2 39 -68 9 .53 19 19 | 2463 -767 18 83 | 1 1 1 38 25 17 .07 | 1585 2030 mit 310| 0 0 0 8 -68 -22 -.25 14 13 | 88 -239 26 118 | 0 0 0 46 30 18 .02 | 539 579 ngs 208| -1 1 0 35 165 -23 -.33 18 12 | -378 -7 2316 4079 | 0 0 1 43 37 29 .05 | 549 812 sio 106| -2 0 0 157 406 40 .10 22 23 | --- --- --- --- | 1 1 1 16 35 27 .04 | --- --- Table 1.1478.b GPS week : 1478 MJD: 54590.000-54596.000 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 5 6 | 3 | 5 5 5 5 5 4 5 | 4 | 7 7 7 6 6 6 6 | 5 | 5 6 5 5 5 5 5 | 6 | 5 4 4 5 4 5 4 | 7 | 6 6 6 6 6 5 6 | 8 | 6 6 6 6 5 5 5 | 9 | 6 6 6 6 6 7 6 | 10 | 5 5 5 5 4 4 4 | 11 | 7 6 6 5 5 6 7 | 12 | 6 6 6 6 6 7 6 | 13 | 6 7 7 6 6 7 7 | 14 | 6 6 6 7 6 6 6 | 15 | 7 7 7 6 5 6 6 | 16 | 6 6 6 6 6 6 6 | 17 | 8 7 7 7 8 7 7 | 18 | 7 7 8 7 7 7 7 | 19 | 7 7 7 7 7 7 9 | 20 | 6 7 7 6 7 7 7 | 21 | 6 6 6 6 6 5 9 | 22 | 7 7 7 7 7 7 6 | 23 | 7 7 7 7 7 7 7 | 24 | 8 8 10 11 11 12 13 | 25 | 6 6 7 7 7 7 7 | 26 | 6 6 6 5 5 5 6 | 27 | 6 6 6 6 6 6 7 | 28 | 6 6 6 6 7 6 7 | 29 | 7 7 7 7 7 7 7 | 30 | 5 5 5 5 4 5 5 | 31 | 6 6 7 6 5 5 5 | 32 | 5 7 6 6 6 6 8 | 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 2.1478.0 GPS week: 1478 Day: 0 MJD: 54590.000 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 206| 1 0 -1 7 -59 -38 -.20 12 11 | 269 -1112 19 63 | 14 2 | emr 68| 3 -1 3 -141 -4 -22 .36 18 18 | 1691 104 23 84 | 57 -67 | esa 114| 0 0 -3 -57 -104 15 .32 17 16 | -8552 -1008 23 119 | -2 61 | gfz 183| 0 0 -1 -4 -83 17 -.14 14 14 | 842 -1066 21 120 | -1 19 | grg 82| 4 2 -2 13 9 50 1.00 42 29 | 293 -1182 97 658 | 6 17 | igr n/a| 0 1 -1 0 -81 -16 .01 6 6 | 22147 -1097 22 103 | -4 21 | jpl 118| 0 -2 4 3 -70 30 .42 16 16 | 3721 -181 18 79 | 43 13 | mit 310| 0 0 -1 -23 -66 -10 -.25 16 15 | 778 -684 33 130 | 37 66 | ngs 208| -1 2 0 63 165 -30 -.32 16 13 | 296 -1182 2472 3939 | -40 23 | sio 106| -2 -1 2 181 475 78 .15 24 23 | --- --- --- --- | -133 -300 | Table 2.1478.1 GPS week: 1478 Day: 1 MJD: 54591.000 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 206| 0 0 0 7 -53 -4 -.20 11 10 | -483 -86 17 64 | 15 14 | emr 68| 2 -3 5 -162 -47 -20 .51 23 23 | 1877 -767 26 94 | 86 8 | esa 114| 0 0 0 -28 -115 0 .28 17 16 | -9646 912 21 111 | 45 27 | gfz 183| 0 0 -1 -6 -47 29 -.16 15 15 | -93 20 21 124 | 4 11 | grg 82| 1 0 -6 17 -50 37 1.06 43 33 | -453 -161 117 667 | 43 28 | igr n/a| 0 0 0 -4 -78 -2 .06 7 7 | 21043 -1947 22 84 | 5 -2 | jpl 118| 0 0 1 11 -103 20 .52 18 18 | 1920 -762 16 74 | 34 35 | mit 310| -1 0 0 15 -19 -27 -.23 15 14 | -115 145 24 119 | -4 2 | ngs 208| -1 0 0 -1 156 -7 -.36 16 12 | -430 -204 2085 3970 | -12 15 | sio 106| -2 0 -1 162 411 33 .16 23 24 | --- --- --- --- | -98 -256 | Table 2.1478.2 GPS week: 1478 Day: 2 MJD: 54592.000 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 206| 2 -2 0 -11 2 -24 -.19 12 11 | -549 218 17 60 | 48 -47 | emr 68| 0 0 4 -159 -38 -21 .47 20 20 | 1108 -1252 22 86 | 67 20 | esa 114| 1 2 0 -56 -182 31 .28 15 14 | -8337 -1226 21 119 | 67 10 | gfz 183| -1 0 -1 15 -13 72 -.15 15 15 | -346 152 18 114 | -15 -8 | grg 82| 2 0 0 -66 24 -84 .95 45 42 | -548 158 111 657 | 72 -57 | igr n/a| 0 1 0 -18 -40 2 .05 7 7 | 19084 -1831 20 83 | -7 10 | jpl 118| -5 -2 1 6 -70 11 .53 19 19 | 996 -1202 17 89 | 26 50 | mit 310| 0 0 -1 91 -105 -44 -.26 14 13 | -125 -124 22 86 | -67 55 | ngs 208| 0 2 -1 -24 203 -23 -.40 18 12 | -295 225 2205 3963 | 85 38 | sio 106| -1 0 0 129 375 17 .07 22 26 | --- --- --- --- | -59 -242 | Table 2.1478.3 GPS week: 1478 Day: 3 MJD: 54593.000 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 206| 1 0 0 2 -25 -29 -.20 11 10 | -411 -30 21 61 | 26 -37 | emr 68| 1 -1 3 -118 -44 -33 .48 19 19 | 1164 -221 25 76 | 41 -23 | esa 114| 2 3 3 -67 -131 -29 .21 16 16 | -8818 -1299 23 96 | 48 -14 | gfz 183| 0 0 -4 -24 -8 100 -.10 14 14 | 466 -850 20 118 | -6 -20 | grg 82| 2 -1 4 -20 14 -37 1.01 39 34 | -422 -40 113 604 | 18 -38 | igr n/a| 0 0 1 1 -83 18 .11 7 7 | 18627 -945 21 84 | 8 -3 | jpl 118| -2 -1 1 94 -94 27 .54 19 19 | 2509 -158 20 85 | -24 -11 | mit 310| 0 -1 0 -37 -37 -49 -.23 14 13 | 346 -610 40 147 | 43 -2 | ngs 208| -2 1 0 48 137 14 -.36 21 15 | -423 -34 2261 4464 | -47 53 | sio 106| -1 0 0 155 366 18 .10 21 24 | --- --- --- --- | -104 -205 | Table 2.1478.4 GPS week: 1478 Day: 4 MJD: 54594.000 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 206| 1 -1 -1 -34 -14 -7 -.19 11 10 | -1478 1681 16 115 | 79 -25 | emr 68| 1 -1 2 -95 -40 -55 .44 20 20 | 106 2903 26 114 | -6 8 | esa 114| 0 3 4 -44 -181 -10 .27 15 14 | -9925 186 22 117 | 48 50 | gfz 183| 0 0 -5 -3 -36 63 -.14 15 15 | -793 981 22 131 | -7 -1 | grg 82| -1 0 0 -51 34 -31 .92 41 28 | -1459 1623 373 198573 | 62 -46 | igr n/a| 0 0 0 -17 -57 -21 .05 7 7 | 17023 1902 23 79 | -17 6 | jpl 118| 0 -2 2 19 -66 -10 .59 19 19 | 148 2932 20 95 | 10 -12 | mit 310| 0 0 0 41 -78 -19 -.25 12 11 | -675 680 16 104 | -4 38 | ngs 208| -1 0 -1 8 211 -5 -.26 17 12 | -1411 1540 2352 4207 | -67 -5 | sio 106| -2 1 0 154 396 32 .06 22 21 | --- --- --- --- | -94 -232 | Table 2.1478.5 GPS week: 1478 Day: 5 MJD: 54595.000 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 206| 0 0 0 -6 -42 -42 -.18 12 10 | -536 -64 20 79 | 54 -34 | emr 68| 0 -4 3 -47 -18 -10 .37 20 20 | 3488 -2629 21 82 | -43 -19 | esa 114| 0 2 1 -132 -181 -11 .34 14 14 | -8453 916 23 133 | 60 30 | gfz 183| 0 0 -4 -30 -19 52 -.14 14 14 | 101 114 21 121 | 16 -19 | grg 82| 0 0 1 -16 -13 57 .99 45 31 | -520 -94 127 612 | 2 -12 | igr n/a| 0 0 0 0 -60 0 .08 6 6 | 19439 -3344 21 74 | 26 10 | jpl 118| 0 0 1 82 -26 2 .63 21 21 | 4721 -2691 20 83 | -12 -95 | mit 310| 0 0 0 -31 -95 0 -.25 12 12 | -300 -46 25 128 | 21 30 | ngs 208| -1 1 -1 100 181 -38 -.34 19 11 | -516 -99 2300 4137 | 6 48 | sio 106| -2 1 2 172 411 81 .10 21 22 | --- --- --- --- | -113 -232 | Table 2.1478.6 GPS week: 1478 Day: 6 MJD: 54596.000 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 206| 2 -2 0 -15 -58 -7 -.16 13 11 | 116 -265 22 72 | 71 4 | emr 68| 0 0 5 -56 -27 -26 .36 23 21 | 2092 -3537 27 89 | -49 -28 | esa 114| 1 1 2 -112 -120 -29 .32 16 14 | -8522 -2266 22 113 | 68 58 | gfz 183| 0 -1 -3 -14 9 116 -.13 14 14 | 529 -435 25 116 | 11 -10 | grg 82| 0 3 -1 -32 -34 5 1.08 45 33 | 124 -294 143 590 | 100 91 | igr n/a| 0 -1 0 -12 -93 -6 .04 7 7 | 17374 -4134 22 72 | 26 21 | jpl 118| 0 1 2 56 -49 -12 .48 19 19 | 3228 -3308 19 78 | -53 -66 | mit 310| 0 -1 1 6 -75 -7 -.28 15 15 | 707 -1036 23 113 | 1 33 | ngs 208| -1 0 -1 58 104 -76 -.27 19 10 | 132 -298 2541 3876 | -128 -25 | sio 106| -5 1 1 147 405 23 .05 23 23 | --- --- --- --- | -80 -220 | 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 3.1478.0 GPS week: 1478 Day: 0 MJD: 54590.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 12 16 17 12 28 5 27 17 13 17 6 | 25 31 26 30 31 25 36 19 27 23 23 3 | 7 13 13 14 19 7 15 11 12 14 4 | 32 37 39 29 40 33 38 36 34 34 33 4E | 14 19 18 13 116 8 18 18 24 21 6 | 59 59 55 55 52 55 61 65 56 62 58 5 | 8 17 15 9 27 6 8 18 11 25 5 | 16 23 18 17 17 18 19 17 20 25 15 6 | 7 14 11 14 25 5 11 10 15 11 4 | 17 24 26 21 32 23 26 18 26 23 20 7 | 10 17 15 13 65 5 16 12 16 17 5 | 18 25 15 23 50 17 22 16 21 15 15 8 | 12 18 13 12 16 5 10 12 13 29 5 | 92 87 92 90 100 92 88 99 98 97 94 9 | 12 18 15 15 27 5 12 17 14 25 5 | 26 30 25 31 35 27 30 30 28 36 26 10 | 8 11 15 9 21 4 10 13 13 17 4 | 17 19 24 18 32 18 21 19 19 17 17 11E | 27 15 13 16 27 7 17 16 15 15 7 | 36 34 34 34 59 30 38 24 30 30 29 12 | 10 17 15 11 21 6 11 19 15 34 6 | 16 24 18 18 25 16 22 18 22 31 17 13 | 10 18 18 16 43 6 22 16 12 19 6 | 14 31 21 23 52 17 29 17 16 16 14 14 | 12 19 18 16 28 5 17 18 14 13 6 | 16 30 20 26 34 20 27 20 15 20 17 15 | 12 20 22 13 29 6 17 15 19 21 6 | 16 30 24 19 36 17 26 22 20 17 16 16 | 9 18 16 12 38 6 12 18 12 29 5 | 18 28 26 20 34 18 24 22 21 27 20 17 | 11 20 23 18 38 8 18 14 22 37 7 | 29 36 21 38 48 30 38 28 29 37 28 18 | 14 22 19 16 28 4 22 19 12 30 7 | 18 33 24 27 37 20 28 21 15 28 18 19 | 12 20 20 19 23 7 23 14 17 23 7 | 20 33 22 37 32 22 38 22 24 28 24 20 | 12 18 16 16 53 5 20 19 13 16 6 | 21 32 25 26 38 20 29 26 22 24 19 21E | 12 16 23 11 36 8 19 17 14 13 6 | 21 24 22 22 34 20 25 27 25 19 18 22 | 11 22 19 17 34 6 16 17 11 31 6 | 21 37 29 26 35 22 26 26 21 32 21 23 | 13 19 22 15 37 6 25 20 13 23 7 | 16 31 23 25 39 19 34 19 18 20 17 24E | 15 18 20 12 91 10 16 21 33 20 7 | 103 93 97 97 89 98 90 96 105 94 96 X25 | 12 21 14 11 30 6 14 --- 16 19 6 | 56 59 60 60 56 58 57 --- 58 56 56 26 | 12 14 16 13 15 5 11 12 15 27 5 | 15 21 20 22 27 15 22 13 18 24 14 27 | 13 19 10 13 33 4 12 11 16 23 5 | 27 37 26 36 39 30 37 31 35 31 30 28 | 9 14 14 13 41 7 15 18 14 28 5 | 18 26 21 18 46 15 21 22 18 16 15 29 | 10 18 17 17 37 6 14 14 13 40 6 | 37 42 33 48 51 39 43 40 42 61 40 30 | 7 16 15 9 21 5 6 14 9 19 4 | 25 33 27 25 36 27 25 27 29 26 25 31 | 11 21 13 14 40 6 14 17 14 18 5 | 15 30 18 22 38 17 25 16 19 18 17 32 | 6 14 17 10 --- 6 15 17 13 24 5 | 15 22 25 20 --- 16 24 18 16 32 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 18 17 14 42 6 16 16 16 24 |T 28 35 30 32 42 28 34 29 30 32 28 WRMS | 11 18 16 14 29 6 16 15 13 23 |NE 22 31 26 27 39 23 30 25 25 29 23 MEDI | 12 18 16 13 29 6 15 17 14 21 |MD 20 31 25 26 37 20 28 22 22 27 20 Table 3.1478.1 GPS week: 1478 Day: 1 MJD: 54591.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 14 19 16 10 24 5 30 10 13 11 6 | 12 20 16 13 27 11 27 16 18 17 11 3 | 7 14 16 12 27 8 11 13 13 10 4 | 37 42 43 39 46 37 38 38 40 36 37 4E | 14 26 18 17 100 9 23 12 22 18 7 | 44 48 45 44 57 45 44 43 47 41 41 5 | 6 19 15 13 29 6 13 17 12 25 5 | 13 21 18 16 23 13 17 19 22 25 14 X6 | 4 --- 11 11 26 8 11 10 15 10 4 | 12 --- 19 13 26 17 22 14 18 16 14 7 | 8 21 20 14 68 4 16 13 12 16 5 | 17 27 15 23 46 16 21 16 22 15 14 8 | 12 23 14 14 54 5 14 11 13 27 6 | 46 45 50 50 75 48 47 52 45 53 45 9 | 12 17 15 16 19 6 14 14 14 23 5 | 21 31 26 30 37 25 28 24 26 34 23 10 | 6 16 11 12 28 7 12 12 15 14 4 | 18 22 19 20 33 20 23 16 23 22 17 11E | 15 21 17 14 44 9 19 12 12 13 5 | 26 33 31 29 54 25 33 21 22 27 24 12 | 9 18 13 14 24 6 15 17 15 33 6 | 15 27 19 19 26 16 23 21 22 32 16 13 | 11 21 19 17 44 6 24 17 13 19 6 | 9 28 17 20 48 14 27 20 12 19 10 14 | 12 23 20 18 27 5 17 15 11 17 6 | 13 30 19 21 36 16 26 19 14 20 15 15 | 12 24 22 14 24 6 20 16 17 20 6 | 11 32 19 20 37 16 25 20 19 18 14 16 | 9 18 17 12 40 9 15 17 11 23 5 | 14 26 22 18 38 16 23 17 17 21 16 17 | 12 25 18 16 29 8 20 11 17 30 6 | 19 30 12 25 33 19 28 17 26 29 17 18 | 15 28 17 18 33 5 24 16 11 30 7 | 14 36 19 26 42 19 29 22 18 29 17 19 | 9 24 23 19 38 7 21 15 17 25 7 | 17 31 18 27 29 17 32 17 16 25 17 20 | 10 29 19 18 44 6 21 19 15 20 7 | 14 38 21 24 41 17 27 22 16 22 15 21E | 11 26 15 9 32 6 23 11 13 13 5 | 18 32 19 23 35 19 30 19 22 19 18 22 | 10 23 18 21 40 6 18 17 14 30 7 | 16 35 22 25 37 21 27 23 19 30 18 23 | 12 20 22 15 33 4 25 19 11 22 6 | 8 27 20 20 38 15 27 18 14 20 11 24E | 14 20 16 14 91 8 20 19 42 16 8 | 75 68 69 69 71 68 65 65 79 64 67 X25 | 13 21 13 13 46 5 16 --- 16 17 6 | 51 50 48 52 69 49 46 --- 55 47 49 26 | 9 19 18 13 17 5 13 13 13 21 5 | 12 24 20 19 25 12 23 15 14 24 14 27 | 15 22 13 13 43 5 15 12 17 22 6 | 21 35 27 34 38 27 34 28 30 31 26 28 | 10 20 14 13 47 8 20 13 13 25 5 | 13 21 15 18 41 12 21 18 18 14 11 29 | 10 22 15 17 23 8 19 15 17 39 7 | 24 34 21 33 27 25 30 28 33 48 27 30 | 8 18 13 11 18 6 12 13 10 19 4 | 21 23 22 22 20 20 20 23 27 23 20 31 | 8 25 13 15 46 6 15 17 15 23 6 | 13 31 17 20 41 16 24 19 17 19 14 32 | 9 38 17 11 --- 8 13 15 18 26 6 | 17 34 25 19 --- 18 26 19 19 37 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 23 17 15 43 7 18 15 16 23 |T 21 32 24 26 39 22 29 23 25 28 21 WRMS | 10 23 16 15 33 7 18 14 12 24 |NE 17 30 21 23 36 19 26 21 21 25 17 MEDI | 10 21 16 14 33 6 17 14 14 21 |MD 17 31 20 23 37 18 27 19 22 25 17 Table 3.1478.2 GPS week: 1478 Day: 2 MJD: 54592.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 12 15 16 13 38 6 25 14 18 15 6 | 15 24 19 20 32 18 26 17 26 22 17 3 | 9 13 14 12 49 6 21 12 16 12 5 | 27 33 37 28 42 29 32 26 28 26 27 4E | 15 25 16 14 51 5 18 13 26 21 7 | 36 44 33 37 38 32 41 41 33 40 35 5 | 5 16 12 11 43 6 12 13 10 24 5 | 16 22 17 19 31 18 19 18 28 27 18 6 | 6 15 11 9 56 6 11 8 10 10 3 | 18 25 22 19 42 22 26 19 28 16 19 7 | 11 21 18 16 79 6 17 12 17 16 6 | 19 25 17 24 61 19 24 18 27 14 16 8 | 13 22 12 13 25 7 13 11 20 23 6 | 43 45 42 44 46 43 43 43 48 44 42 9 | 10 19 14 17 31 8 14 14 13 25 5 | 22 35 24 31 34 25 33 27 28 36 26 10 | 8 14 11 11 36 6 11 13 14 13 4 | 12 20 16 15 33 15 20 13 20 17 13 11E | 20 18 15 17 51 6 17 11 14 14 6 | 23 31 31 30 54 26 36 24 25 22 24 12 | 9 17 12 16 28 7 14 14 13 32 6 | 16 26 17 19 27 18 25 20 28 35 20 13 | 12 20 19 17 48 10 24 16 15 19 6 | 14 30 26 24 58 18 31 21 22 22 17 14 | 13 21 16 19 31 8 20 16 11 12 6 | 17 38 19 27 47 24 34 25 24 20 22 15 | 14 28 20 16 24 4 19 12 17 18 6 | 25 36 24 23 40 23 28 22 28 18 21 16 | 8 18 13 12 29 8 20 11 10 24 5 | 22 29 24 27 31 24 30 25 24 26 24 17 | 10 19 20 18 32 7 19 13 16 31 6 | 21 30 16 27 39 22 30 23 30 30 21 18 | 17 28 15 19 58 5 25 15 12 30 7 | 20 40 20 31 61 24 35 24 28 27 23 19 | 11 21 21 18 30 8 20 14 18 23 6 | 18 33 21 32 41 24 35 18 22 25 22 20 | 10 19 18 19 53 9 22 17 15 20 6 | 18 33 27 26 46 23 33 27 24 24 21 21E | 15 23 16 10 33 5 23 13 9 14 6 | 19 26 16 20 41 18 30 22 26 19 19 22 | 11 22 17 19 45 7 22 15 14 28 6 | 17 36 25 25 40 23 30 26 26 32 22 23 | 13 21 21 19 44 8 24 15 15 22 7 | 16 30 26 26 47 21 32 18 24 19 18 24E | 14 24 17 12 97 9 23 20 53 17 9 | 76 73 72 73 69 72 70 73 89 71 71 X25E | 12 21 14 12 105 6 17 --- 18 18 6 | 35 35 30 38 85 33 38 --- 39 31 32 26 | 13 22 13 14 28 6 17 12 17 20 6 | 25 30 22 26 32 22 29 20 27 26 22 27 | 17 23 13 12 44 7 17 12 19 20 6 | 32 40 35 37 52 33 41 35 40 35 34 28 | 9 17 13 13 43 10 17 17 15 25 6 | 19 26 20 22 42 21 26 25 30 19 21 29 | 9 18 14 20 24 7 18 15 14 37 7 | 27 33 24 38 36 29 36 32 38 49 31 30 | 8 14 10 12 29 7 13 11 13 16 4 | 22 26 23 25 30 24 21 24 36 26 23 31 | 11 22 15 16 36 6 21 16 15 21 6 | 17 34 18 26 35 21 31 19 26 23 21 32 | 9 14 13 12 --- 6 19 17 16 26 6 | 13 27 22 18 --- 17 27 22 20 34 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 20 15 15 45 7 19 14 18 22 |T 23 32 25 28 43 25 32 25 30 28 24 WRMS | 11 20 14 15 42 7 19 13 12 26 |NE 20 30 22 25 41 22 29 22 27 26 21 MEDI | 11 20 15 14 38 7 19 13 15 20 |MD 19 31 23 26 41 23 31 23 28 26 22 Table 3.1478.3 GPS week: 1478 Day: 3 MJD: 54593.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 9 16 17 12 22 6 21 15 14 14 5 | 12 22 15 20 21 16 24 15 21 18 14 3 | 7 15 15 16 37 6 16 16 16 9 5 | 45 52 54 50 54 53 50 49 53 47 49 4E | 13 22 16 15 56 6 15 11 24 17 6 | 21 33 21 31 33 26 29 23 33 25 24 5 | 6 16 14 13 15 7 11 12 18 24 5 | 14 19 18 17 26 17 17 14 26 25 14 6 | 6 16 12 13 30 8 14 8 17 8 4 | 19 25 24 21 34 25 24 19 21 20 20 7 | 10 20 19 13 64 6 13 11 19 12 5 | 15 29 13 24 49 21 25 19 26 17 17 8 | 12 19 14 14 16 8 9 10 19 18 5 | 32 38 33 37 48 34 39 34 38 38 33 9 | 13 19 17 14 39 5 15 12 12 23 6 | 23 32 25 31 52 27 32 25 31 34 26 10 | 7 12 9 13 21 5 13 16 15 17 4 | 18 23 24 27 28 22 27 19 26 25 21 11E | 8 16 16 13 44 6 13 9 20 13 5 | 24 37 34 34 52 31 40 29 24 31 29 12 | 9 17 16 14 25 6 14 14 20 33 6 | 15 24 19 19 34 18 24 15 28 34 18 13 | 11 18 18 16 43 6 22 14 15 15 6 | 11 31 17 21 49 18 33 15 15 16 13 14 | 13 20 17 16 43 12 27 14 19 13 6 | 15 31 23 22 42 20 30 18 22 14 17 15 | 10 23 18 13 34 6 14 12 18 16 5 | 10 29 18 20 38 16 24 17 20 21 14 16 | 8 19 17 12 21 10 17 13 16 26 6 | 17 27 19 21 27 20 24 19 21 25 19 17 | 10 20 18 15 31 9 22 14 18 31 6 | 24 33 21 34 31 27 37 25 31 34 25 18 | 14 24 18 16 28 5 24 15 16 27 7 | 19 33 19 26 36 20 29 18 21 25 18 19 | 12 22 21 19 21 6 19 14 21 23 7 | 16 33 15 32 31 21 37 19 16 22 19 20 | 10 19 17 15 58 7 24 17 17 14 6 | 17 34 18 26 48 21 33 22 15 18 18 21E | 12 21 12 10 29 5 24 10 14 12 5 | 17 29 17 21 38 17 25 19 22 19 18 22 | 11 22 21 18 34 6 24 15 14 27 7 | 22 36 27 27 39 22 29 24 21 28 22 23 | 13 20 19 15 41 6 25 14 12 22 6 | 15 34 18 23 44 21 35 16 17 19 16 24E | 21 25 16 18 78 10 31 26 64 22 11 | 79 76 76 81 62 77 74 77 102 75 76 X25E | 13 23 16 11 46 6 13 --- 21 17 6 | 53 50 53 51 54 49 46 --- 57 46 50 26 | 8 18 12 12 25 4 13 12 16 18 5 | 12 22 16 21 26 15 27 16 20 23 15 27 | 13 21 14 14 56 6 12 9 21 20 5 | 42 49 44 51 67 47 50 47 51 49 46 28 | 12 14 14 15 32 10 19 14 14 24 6 | 22 30 25 28 43 24 28 27 26 23 22 29 | 11 18 14 19 33 8 17 15 19 38 7 | 31 40 32 45 48 33 39 32 39 50 35 30 | 7 13 13 12 39 7 10 13 13 16 4 | 25 24 23 21 51 25 21 20 31 24 22 31 | 11 20 13 12 41 7 24 16 17 21 6 | 15 31 14 21 38 16 27 16 24 20 17 32 | 10 17 14 10 --- 7 16 17 20 27 6 | 19 26 24 22 --- 22 27 24 23 37 20 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 19 16 14 39 7 19 14 21 21 |T 23 33 25 29 41 26 32 24 29 29 24 WRMS | 10 19 16 14 34 7 19 13 15 24 |NE 19 30 22 26 39 23 29 21 25 26 21 MEDI | 11 19 16 14 34 6 16 14 17 18 |MD 19 31 21 26 39 22 29 19 24 25 20 Table 3.1478.4 GPS week: 1478 Day: 4 MJD: 54594.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 9 19 13 12 26 6 22 13 17 13 5 | 16 30 22 22 25 21 27 20 27 24 18 3 | 8 13 11 12 28 8 13 13 15 10 4 | 26 37 33 30 36 36 37 34 40 32 32 4E | 12 19 14 17 70 6 18 10 25 18 6 | 18 30 23 26 24 23 23 23 35 22 21 5 | 7 17 11 11 19 6 13 10 12 25 5 | 14 22 18 16 18 19 16 15 30 24 16 6 | 8 13 9 13 20 7 11 6 9 8 3 | 18 28 27 22 32 25 25 20 21 20 21 7 | 9 22 15 16 66 7 17 12 13 11 5 | 16 30 15 24 42 17 22 17 19 15 15 8 | 10 18 9 14 22 6 12 10 11 18 4 | 24 31 26 32 40 28 27 32 29 30 26 9 | 13 24 12 15 31 6 17 13 11 20 5 | 23 34 22 33 50 26 35 26 27 30 25 10 | 7 17 12 12 22 5 11 9 14 9 4 | 14 23 24 21 28 20 25 18 23 16 18 11E | 8 17 15 15 56 7 16 9 11 14 5 | 29 38 36 32 65 31 39 30 35 31 31 12 | 9 19 13 13 22 6 16 11 12 34 6 | 14 25 19 17 26 19 22 16 28 34 17 13 | 11 21 14 19 34 7 23 13 12 18 6 | 13 34 21 23 47 21 33 19 20 19 16 14 | 12 19 20 19 33 6 24 11 10 14 6 | 16 29 23 25 43 20 27 16 26 16 18 15 | 11 23 14 13 26 6 14 10 15 14 5 | 13 34 20 22 39 20 29 15 24 22 18 16 | 8 19 18 15 27 10 18 10 12 25 5 | 18 30 23 26 33 24 28 22 23 29 22 17 | 11 22 21 18 29 7 24 13 18 37 7 | 19 33 21 31 31 24 34 24 30 33 22 18 | 15 29 17 18 31 6 23 12 14 29 7 | 17 37 18 26 42 21 28 17 28 25 18 19 | 10 20 20 21 22 10 21 13 16 22 6 | 16 32 19 32 35 24 35 19 26 22 20 20 | 9 16 19 18 63 8 24 17 16 16 6 | 16 32 22 24 48 23 33 23 25 22 18 21E | 15 24 14 11 34 6 20 8 12 13 5 | 16 29 22 19 35 20 25 19 23 17 17 22 | 12 19 17 18 32 6 23 11 13 26 6 | 20 35 26 28 36 24 30 23 27 26 22 23 | 10 19 16 19 47 8 24 17 12 19 6 | 12 30 17 22 45 19 34 16 17 19 14 24E | 21 35 21 19 67 14 30 20 59 21 11 | 85 80 82 81 74 76 76 82 101 81 80 X25E | 14 26 15 11 38 7 16 --- 15 18 6 | 27 35 29 33 38 32 31 --- 34 34 28 26 | 9 20 10 13 23 5 13 13 13 19 5 | 15 31 21 25 30 20 29 16 24 26 19 27E | 15 25 12 14 86 7 15 9 15 21 6 | 55 62 51 57 102 55 60 52 51 57 53 28 | 11 22 16 17 37 9 22 17 12 28 6 | 19 34 27 24 44 22 29 25 24 20 21 29 | 12 22 11 18 27 8 21 11 14 40 7 | 26 40 25 39 39 30 37 29 34 49 31 30 | 8 13 8 11 17 6 13 8 12 17 4 | 21 23 21 19 28 23 19 19 34 21 20 31 | 10 18 12 13 46 5 18 12 11 21 5 | 20 35 22 27 42 25 31 22 27 18 22 32 | 7 15 13 11 --- 7 16 19 18 26 6 | 14 21 20 21 --- 20 26 19 25 34 17 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 20 15 15 41 7 19 12 17 22 |T 21 33 25 28 40 26 31 24 30 28 23 WRMS | 10 20 14 15 28 7 19 11 12 21 |NE 17 30 22 25 36 22 28 20 26 24 20 MEDI | 10 19 14 15 31 7 18 11 13 19 |MD 18 32 22 25 38 23 29 20 27 24 20 Table 3.1478.5 GPS week: 1478 Day: 5 MJD: 54595.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 9 20 13 8 36 5 21 15 9 12 5 | 11 24 14 14 26 11 21 17 15 16 11 3 | 7 15 11 11 36 4 14 9 11 14 4 | 39 44 43 40 45 40 41 37 43 38 39 4E | 11 20 13 13 46 7 15 11 24 18 6 | 18 27 18 23 24 21 24 19 30 21 18 5 | 8 21 13 11 27 5 18 12 11 24 5 | 12 20 13 17 26 14 15 17 21 22 14 6 | 10 13 12 12 26 6 13 9 13 12 4 | 20 25 26 19 31 22 23 22 32 23 21 7 | 9 20 17 12 72 4 19 11 11 11 5 | 17 26 10 22 43 13 22 15 19 16 13 8 | 11 18 8 11 20 6 13 11 14 16 4 | 25 29 27 30 34 26 30 30 29 33 26 9 | 25 21 16 16 39 7 23 15 12 19 7 | 53 59 56 61 84 58 62 58 57 63 56 10 | 6 15 12 10 22 4 12 8 11 8 4 | 17 21 18 21 27 16 21 16 21 19 17 11E | 16 16 16 13 110 7 15 10 14 12 5 | 20 34 37 35 98 32 37 29 32 32 29 12 | 10 22 13 15 29 5 22 12 11 33 6 | 11 25 18 21 30 17 21 17 20 31 16 13 | 10 20 17 16 46 7 27 15 13 21 6 | 13 31 22 21 47 17 30 14 16 20 12 14 | 12 21 20 19 39 5 24 12 11 14 6 | 14 28 23 25 44 19 26 13 21 15 16 15 | 10 21 16 14 29 5 18 12 17 15 5 | 12 31 20 19 35 16 26 10 22 16 13 16 | 9 20 15 15 31 8 19 10 13 24 5 | 17 25 17 20 27 18 25 18 21 25 17 17 | 9 22 18 14 29 6 24 15 14 32 6 | 24 31 20 28 33 22 31 27 25 35 23 18 | 17 20 14 18 66 7 23 11 12 29 6 | 22 35 24 32 73 26 32 24 29 31 24 19 | 10 21 18 20 --- 10 23 15 17 23 6 | 15 35 21 29 --- 19 34 14 23 18 18 20 | 10 19 17 17 63 5 29 18 13 15 6 | 17 29 23 22 48 17 30 19 17 16 15 21E | 12 20 10 12 17 5 20 9 15 13 5 | 16 28 19 20 18 16 25 16 26 13 16 22 | 13 19 17 20 41 5 24 12 13 28 6 | 19 32 24 28 40 23 29 23 27 29 22 X23 | 10 24 15 19 49 7 --- 18 12 21 7 | 16 31 20 23 47 18 --- 18 14 19 13 24E | 20 30 17 15 64 8 30 17 73 21 12 | 103 101 94 104 85 97 96 99 120 107 100 X25E | 14 23 14 10 36 6 16 --- 19 18 6 | 50 48 45 47 55 48 44 --- 54 45 46 26 | 7 14 9 12 26 5 14 15 15 22 5 | 13 23 17 20 27 14 24 15 18 28 15 27E | 17 25 12 10 40 6 16 10 16 20 6 | 32 44 38 39 48 38 45 33 39 37 35 28 | 9 18 18 13 38 7 25 14 10 26 6 | 14 23 20 20 38 14 23 20 18 16 14 29 | 13 23 12 17 25 7 23 11 16 40 7 | 26 35 22 37 30 28 33 28 35 53 30 30 | 8 16 11 11 23 5 18 10 12 16 4 | 18 22 17 19 29 18 21 17 29 19 19 31 | 10 19 12 13 45 5 20 11 14 17 5 | 17 29 19 20 38 19 27 15 26 18 18 32 | 10 21 12 12 --- 6 23 12 12 26 5 | 15 23 21 19 --- 18 26 14 21 33 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 20 14 14 45 6 21 12 19 21 |T 23 32 26 28 42 25 31 23 29 29 23 WRMS | 10 20 14 14 31 6 21 12 11 22 |NE 17 28 21 24 37 19 26 19 23 24 18 MEDI | 10 20 14 13 36 6 20 12 13 19 |MD 17 29 21 22 38 19 26 18 25 23 18 Table 3.1478.6 GPS week: 1478 Day: 6 MJD: 54596.000 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 ------+--------------------------------------------------------+--------------------------------------------------------- 2E | 12 17 15 8 25 5 23 14 11 13 5 | 16 22 16 17 26 15 26 21 20 19 14 3 | 11 16 12 14 32 7 13 9 11 18 4 | 37 43 46 41 44 41 43 35 40 39 38 4E | 10 18 12 16 43 6 14 14 22 18 6 | 18 28 19 22 23 21 25 16 35 22 16 5 | 9 13 12 9 25 9 12 18 10 25 5 | 12 20 19 16 19 17 19 23 20 24 14 6 | 9 14 12 12 34 8 13 11 8 12 4 | 17 24 26 19 34 23 22 20 22 21 19 7 | 11 18 15 12 78 5 19 13 14 11 5 | 16 24 11 22 47 15 22 15 17 13 13 8 | 11 20 12 13 21 6 13 15 11 17 5 | 25 30 27 26 34 24 30 27 25 32 23 9E | 11 18 13 16 94 5 17 13 13 20 5 | 39 53 43 53 89 47 56 45 46 51 46 10 | 8 12 10 10 28 4 12 8 13 8 4 | 18 24 24 26 39 21 25 23 26 24 20 11 | 22 20 14 13 58 12 15 17 12 25 6 | 51 62 62 59 109 56 61 55 58 51 56 12 | 10 16 14 14 22 6 17 16 6 36 6 | 13 27 21 18 29 17 25 18 17 37 17 13 | 11 19 11 18 40 7 25 20 16 20 6 | 14 29 19 24 46 20 29 18 23 21 14 14 | 13 22 19 16 34 6 20 13 9 15 6 | 16 28 23 19 34 15 24 17 15 14 14 15 | 13 23 13 12 27 5 17 18 17 16 6 | 10 35 21 20 35 18 29 18 24 25 15 16 | 9 21 14 14 29 7 19 11 15 27 6 | 18 27 23 22 30 20 24 20 18 29 19 17 | 11 21 14 14 70 7 21 17 14 34 6 | 26 34 22 33 53 27 34 29 27 42 27 18 | 19 22 13 17 77 5 26 15 16 29 7 | 18 34 19 25 42 19 30 19 21 28 17 19 | 14 52 23 22 21 9 21 16 12 24 9 | 19 55 16 36 35 21 34 20 23 22 21 20 | 11 21 17 16 64 9 25 19 12 17 6 | 15 30 24 23 56 19 27 20 18 18 15 21E | 14 30 43 11 31 5 21 11 14 18 8 | 23 35 32 21 32 19 27 23 27 20 19 22 | 14 17 14 16 47 7 20 13 14 29 6 | 25 34 27 27 39 24 30 27 25 29 22 23 | 11 21 12 16 37 9 26 20 12 20 6 | 13 27 15 22 42 18 30 17 17 17 12 24E | 23 27 18 16 58 7 26 20 76 26 12 | 119 116 103 116 116 113 113 116 134 117 113 X25E | 15 24 16 12 33 7 14 --- 18 20 6 | 60 53 53 53 67 53 52 --- 59 50 53 26 | 11 14 11 13 20 5 13 15 12 26 5 | 10 23 17 21 27 12 24 16 20 27 12 27E | 21 28 14 14 30 8 16 21 17 25 7 | 70 65 60 68 80 64 67 70 66 67 64 28 | 11 22 16 12 30 10 23 13 14 28 6 | 22 29 25 24 44 20 27 28 26 21 20 29 | 13 22 13 15 23 8 21 10 13 42 7 | 37 41 33 47 46 37 44 41 39 63 40 30 | 9 13 12 10 25 9 12 11 11 17 4 | 25 28 29 22 41 28 25 24 32 23 24 31 | 9 17 10 12 50 5 17 13 10 17 5 | 16 26 15 20 36 18 25 16 20 16 16 32 | 11 46 10 13 --- 7 21 12 14 27 7 | 20 49 23 18 --- 18 24 20 20 33 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 13 23 16 14 45 7 19 15 19 23 |T 27 37 29 31 46 28 34 28 31 32 26 WRMS | 11 21 14 14 33 7 19 15 10 23 |NE 19 31 22 24 38 21 28 22 23 26 19 MEDI | 11 20 13 14 32 7 19 14 13 20 |MD 18 30 23 23 39 20 27 20 24 25 19 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1478 GPS week: 1478 MJD: 54590.0-54596.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 |U 8 8 26 |U 6 10 24 |U 7 7 16 | emr | emr 2951 | 12 10 31 |U 9 8 27 | 10 9 26 | esa | esa 2976 | 11 9 29 |U 9 12 24 |U 13 7 21 | gfz | gfz 2952 |U 10 8 25 |U 9 12 34 |U 8 7 21 | grg | grg 2866 | 0 0 0 |U 0 0 0 | 0 0 0 | igr | igr 2942 | 10 9 29 | 8 10 23 | 7 7 19 | igs | igs 2939 | 8 8 25 | 6 9 24 | 8 7 19 | jpl | jpl 2948 | 9 9 27 |U 7 11 28 |U 7 6 20 | mit | mit 2880 |U 19 15 39 |U 9 12 30 |U 10 8 22 | 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 5.1478.0 GPS week: 1478 Day: 0 MJD: 54590.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 8 21 | 7 16 38 | 7 8 13 | emr | emr 2968 | 17 17 27 | 9 14 43 | 10 9 27 | esa | esa 2976 | 18 11 34 | 10 15 40 | 13 4 15 | gfz | gfz 2957 | 16 11 31 | 11 19 53 | 8 7 19 | igr | igr 2947 | 11 11 30 | 8 15 37 | 8 6 18 | igs | igs 2969 | 10 8 29 | 8 14 41 | 10 8 18 | jpl | jpl 2968 | 9 8 30 | 8 16 43 | 8 6 19 | mit | mit 2880 | 11 10 30 | 11 18 54 | 14 13 36 | Table 5.1478.1 GPS week: 1478 Day: 1 MJD: 54591.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 13 12 33 | 6 9 20 | 6 6 14 | emr | emr 2872 | 8 12 26 | 8 8 16 | 9 9 23 | esa | esa 2976 | 7 13 28 | 9 15 21 | 15 6 15 | gfz | gfz 2956 | 8 13 20 | 7 8 29 | 7 6 15 | igr | igr 2951 | 14 12 33 | 12 12 21 | 7 5 13 | igs | igs 2962 | 5 11 20 | 6 10 20 | 7 7 14 | jpl | jpl 2968 | 7 12 21 | 6 9 19 | 6 5 14 | mit | mit 2880 | 10 11 27 | 7 10 25 | 16 9 14 | Table 5.1478.2 GPS week: 1478 Day: 2 MJD: 54592.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 6 27 | 5 5 20 | 7 7 19 | emr | emr 2968 | 8 6 24 | 8 7 24 | 12 10 30 | esa | esa 2976 | 10 7 26 | 9 12 20 | 15 10 24 | gfz | gfz 2952 | 7 6 20 | 7 9 30 | 8 7 23 | igr | igr 2845 | 7 7 25 | 5 6 21 | 8 7 21 | igs | igs 2779 | 7 7 22 | 4 7 19 | 8 8 21 | jpl | jpl 2968 | 6 6 20 | 5 6 21 | 8 7 22 | mit | mit 2880 | 6 5 25 | 6 8 23 | 7 7 19 | Table 5.1478.3 GPS week: 1478 Day: 3 MJD: 54593.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 7 5 19 | 8 21 25 | 6 5 15 | emr | emr 2966 | 10 8 25 | 8 7 26 | 9 11 26 | esa | esa 2976 | 12 7 29 | 12 18 24 | 13 8 22 | gfz | gfz 2953 | 10 6 28 | 11 17 36 | 7 7 21 | igr | igr 2943 | 8 7 23 | 10 17 24 | 7 8 18 | igs | igs 2972 | 8 7 23 | 5 13 24 | 9 9 21 | jpl | jpl 2966 | 8 6 20 | 8 19 29 | 7 9 20 | mit | mit 2880 | 11 8 28 | 11 23 29 | 9 6 21 | Table 5.1478.4 GPS week: 1478 Day: 4 MJD: 54594.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 8 6 38 | 7 7 20 | 6 6 14 | emr | emr 2963 | 16 11 61 | 11 7 25 | 9 9 24 | esa | esa 2976 | 10 8 39 | 10 9 21 | 11 8 20 | gfz | gfz 2953 | 11 8 41 | 7 9 21 | 8 6 19 | igr | igr 2970 | 12 9 45 | 7 8 19 | 7 7 17 | igs | igs 2954 | 9 6 40 | 7 8 20 | 7 7 16 | jpl | jpl 2944 | 15 11 53 | 8 10 30 | 7 5 18 | mit | mit 2880 | 79 57 119 | 9 8 23 | 9 10 21 | Table 5.1478.5 GPS week: 1478 Day: 5 MJD: 54595.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 8 9 22 | 5 6 18 | 7 6 16 | emr | emr 2962 | 11 10 29 | 8 7 22 | 9 7 25 | esa | esa 2976 | 10 8 28 | 6 9 20 | 11 6 21 | gfz | gfz 2948 | 8 7 20 | 7 8 27 | 8 6 21 | igr | igr 2968 | 8 8 23 | 6 6 15 | 7 6 20 | igs | igs 2971 | 9 9 23 | 5 6 17 | 7 5 19 | jpl | jpl 2866 | 9 9 22 | 6 9 24 | 6 5 22 | mit | mit 2880 | 7 8 22 | 8 6 25 | 8 5 20 | Table 5.1478.6 GPS week: 1478 Day: 6 MJD: 54596.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 8 8 20 | 7 6 24 | 8 9 22 | emr | emr 2960 | 11 8 26 | 10 7 29 | 10 11 27 | esa | esa 2976 | 11 7 21 | 8 8 25 | 10 9 26 | gfz | gfz 2945 | 10 7 18 | 11 15 44 | 11 11 30 | igr | igr 2971 | 9 7 21 | 9 7 27 | 8 9 28 | igs | igs 2971 | 9 7 19 | 8 6 26 | 7 9 25 | jpl | jpl 2960 | 10 10 24 | 8 8 29 | 7 7 28 | mit | mit 2880 | 10 7 22 | 8 10 28 | 8 9 24 | 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 6.1478 GPS week: 1478 MJD: 54590.500-54596.500 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 | 23 -38 -22 36 -5 | 7 15 | 21 29 65 61 4 | 1 emr uuxxu | 19 -16 276 512 8 | 59 61 | 31 50 421 59 16 | 4 esa uuuuu | -27 -41 16 -26 -7 | 8 15 | 24 24 68 73 14 | 2 gfz uuuuu | 9 6 -52 57 1 | 3 12 | 7 16 33 52 7 | 3 grg xxxxx | 7 -37 -14 18 -10 | 26 42 | 52 40 112 162 71 | 28 igr xxxxx | -4 1 -17 74 2 | -1 15 | 13 21 114 37 9 | 2 irf xxxxx | 5 6 18 92 8 | -4 15 | 11 8 104 55 10 | 4 jpl uuxxx | 17 3 -2 127 32 | 5 27 | 46 30 317 317 25 | 10 mit uuuuu | -27 2 210 -26 12 | 7 21 | 21 41 181 66 17 | 4 ngs uuuuu | -16 35 -170 -107 -1 | -9 15 | 33 58 120 163 13 | 1 sio xuuuu | 246 104 -22 35 16 | 35 39 | 40 23 77 74 16 | 6 Table 7.1478.0 GPS week: 1478 Day: 0 MJD: 54590.500 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 | 15 -10 7 -37 -12 | 9 16 emr uuxxu | 84 -53 324 526 -15 | 59 60 esa uuuuu | -44 6 47 -15 14 | 5 16 gfz uuuuu | -2 5 -32 -21 6 | 2 13 grg xxxxx | 0 -2 -136 -17 93 | 0 0 igr xxxxx | -4 8 32 109 -14 | 1 12 irf xxxxx | 17 4 49 54 -4 | -6 12 jpl uuxxx | 4 -39 197 -39 -6 | -2 16 mit uuuuu | -49 -33 316 -78 -18 | 8 17 ngs uuuuu | -6 44 -319 211 4 | -8 14 sio xuuuu | 317 137 5 -83 -2 | 32 35 Table 7.1478.1 GPS week: 1478 Day: 1 MJD: 54591.500 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 | 1 -6 -84 40 -6 | 6 16 emr uuxxu | 7 -77 759 413 14 | 53 55 esa uuuuu | -12 -36 -26 -58 -6 | 5 16 gfz uuuuu | 4 5 -70 54 6 | -1 11 grg xxxxx | -13 -34 92 -134 -68 | 78 78 igr xxxxx | 17 4 191 12 -4 | -3 14 irf xxxxx | 15 9 135 30 9 | -9 15 jpl uuxxx | -20 -25 355 -214 27 | -5 17 mit uuuuu | 13 13 366 -48 5 | 3 16 ngs uuuuu | 0 21 -110 -8 -11 | -9 15 sio xuuuu | 271 107 -116 -30 17 | 28 30 Table 7.1478.2 GPS week: 1478 Day: 2 MJD: 54592.500 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 | 59 -29 -53 -22 -8 | 7 15 emr uuxxu | -8 -48 676 506 15 | 55 57 esa uuuuu | 2 -48 36 24 -6 | 8 15 gfz uuuuu | 20 34 -103 33 5 | 2 10 grg xxxxx | 69 -53 70 189 -59 | 46 56 igr xxxxx | 2 26 -48 87 2 | -2 14 irf xxxxx | 12 19 74 150 14 | -7 12 jpl uuxxx | -38 -7 333 -140 45 | -1 18 mit uuuuu | -43 86 271 102 19 | 4 16 ngs uuuuu | -26 -66 -132 -185 -15 | -8 13 sio xuuuu | 254 78 -97 22 24 | 30 33 Table 7.1478.3 GPS week: 1478 Day: 3 MJD: 54593.500 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 -21 -34 60 -4 | 7 15 emr uuxxu | 11 -36 405 516 28 | 57 58 esa uuuuu | 2 -43 -120 -30 -30 | 9 14 gfz uuuuu | 8 11 -34 65 7 | 3 9 grg xxxxx | 26 -13 -127 -19 -67 | 25 47 igr xxxxx | -9 -3 2 89 11 | -3 14 irf xxxxx | -12 5 81 25 20 | -5 12 jpl uuxxx | -1 29 -56 -72 42 | 3 21 mit uuuuu | -10 -38 349 9 33 | 5 17 ngs uuuuu | -65 52 -251 -275 -17 | -9 15 sio xuuuu | 193 109 -26 70 37 | 32 35 Table 7.1478.4 GPS week: 1478 Day: 4 MJD: 54594.500 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 | 32 -74 -86 -10 -6 | 6 13 emr uuxxu | -1 11 343 526 22 | 59 63 esa uuuuu | -43 -43 76 57 -16 | 10 14 gfz uuuuu | 8 12 -63 51 2 | 4 12 grg xxxxx | 53 -57 34 107 -43 | 15 41 igr xxxxx | 1 22 -17 116 11 | -2 15 irf xxxxx | 7 5 42 138 16 | -2 16 jpl uuxxx | 19 -5 -50 311 61 | 7 30 mit uuuuu | -31 9 228 -23 28 | 8 23 ngs uuuuu | 12 72 -177 -124 7 | -10 15 sio xuuuu | 239 99 -29 76 27 | 36 43 Table 7.1478.5 GPS week: 1478 Day: 5 MJD: 54595.500 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 | 29 -44 99 102 -2 | 6 14 emr uuxxu | 14 53 -201 610 3 | 63 67 esa uuuuu | -35 -50 64 5 -2 | 10 14 gfz uuuuu | 14 -6 -63 62 -4 | 6 14 grg xxxxx | 7 8 -134 216 -13 | 9 37 igr xxxxx | -15 -16 -163 59 8 | 0 17 irf xxxxx | -5 10 -100 146 7 | 1 19 jpl uuxxx | 90 22 -457 551 53 | 14 40 mit uuuuu | -35 -11 75 -48 15 | 11 28 ngs uuuuu | -53 4 -245 -219 2 | -8 16 sio xuuuu | 227 123 -5 51 19 | 41 48 Table 7.1478.6 GPS week: 1478 Day: 6 MJD: 54596.500 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 | -4 -79 0 119 0 | 6 14 emr uuxxu | 28 41 -371 484 -8 | 63 68 esa uuuuu | -58 -76 34 -168 -2 | 9 14 gfz uuuuu | 10 -19 0 155 -13 | 6 14 grg xxxxx | -91 -108 102 -219 88 | 6 35 igr xxxxx | -21 -34 -116 43 -2 | 2 17 irf xxxxx | 0 -8 -152 104 -5 | 2 19 jpl uuxxx | 66 45 -338 492 5 | 21 44 mit uuuuu | -33 -9 -136 -96 2 | 13 28 ngs uuuuu | 25 120 46 -151 20 | -8 16 sio xuuuu | 220 72 118 140 -7 | 43 50