Date: Thu, 13 Nov 2008 13:57:04 +0000 From: Jim Ray Subject: [IGSREPORT-16828] Wk 1503 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <491c3230.ajYpCBabagB3rLN+%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 13 Nov 05:57:06 PST 2008 Message Number 16828 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1503 (Oct 26, 2008 - Nov 01, 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: igs1503[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1503[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1503[0-6].cls IGS GPS clock combination summary report. igs15037.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs15037.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 | EMR | MCM4 MIZU 0 | ESA | 4 0 | GFZ | 2 7 BAN2 0 | JPL | FAA1 0 | MIT | 24 TOW2 1 | COD | 4 1 | EMR | DAEJ MIZU 1 | ESA | 4 1 | GFZ | 2 7 29 BAN2 DAEJ DAV1 1 | MIT | 22 24 BOR1 NRC1 SYDN 2 | ALL | 2 2 | COD | USNO 2 | EMR | MIZU 2 | ESA | 4 2 | GFZ | 7 BAN2 DAV1 FAA1 TOW2 2 | MIT | 24 HARB SYDN TOW2 USNO 3 | EMR | HARB MIZU YELL 3 | ESA | CHUR QAQ1 SCH2 3 | GFZ | 7 3 | JPL | 4 HARB 3 | MIT | 24 KHAJ 4 | COD | 4 4 | EMR | DAEJ MIZU 4 | ESA | 4 CHUR PERT ZECK 4 | GFZ | 7 BAN2 4 | MIT | 24 SYDN 5 | COD | 4 5 | EMR | MIZU 5 | ESA | 4 ALIC 5 | GFZ | 2 7 23 BAN2 FAA1 ONSA 5 | JPL | 4 ZWE2 5 | MIT | 24 NRC1 6 | COD | 4 25 6 | EMR | MIZU YAKT 6 | ESA | 4 25 6 | GFZ | 7 BAN2 NRC1 YAKT 6 | JPL | ZWE2 6 | MIT | 24 NRC1 SYDN 5. The following table lists all maneuvered satellites for this week. The solutions from COD and ESA, which modeled the maneuver, are used that day for combination. An associated accuracy code of 0 (unknown) is given if only one AC is left (no redundancy). For the long arc evaluation the arc is split into two parts at the given maneuver epoch. PRN | Date | Ref. NANU ----+------------+---------- G02 | 2008_10_28 | 2008136 G02 | 2008_10_29 | 2008136 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 .4 .8 -12 -13 -8 -.14 EMR | 9.8 -3.6 4.8 89 14 28 .06 ESA | 2.9 1.6 7.4 -1 -30 20 -.06 GFZ | .4 .8 1.7 17 -20 10 -.30 GRG | 3.8 .6 -1.4 -24 -35 10 -.12 JPL | -1.7 6.6 10.3 -21 -28 -21 -.01 MIT | 7.4 -.5 6.8 -1 -9 -10 -.16 NGS | 6.4 -1.5 1.7 -11 -95 34 -.07 SIO | 10.3 -2.5 -4.1 -66 -209 19 .26 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 1.1503.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1503.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 2.1503.[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 3.1503.[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 5.1503.0-6). 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 1503 summary. (Oct 26, 2008 - Nov 01, 2008) Table 1.1503.a GPS week: 1503 MJD: 54765.000-54771.000 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 240| 0 0 0 17 -55 -16 -.23 10 10 | -301 81 18 133 | 0 0 1 8 12 18 .02 | 417 598 emr 72| -2 -3 2 -146 -140 2 .40 17 17 | 836 -142 17 234 | 1 2 1 33 18 13 .04 | 1343 1390 esa 128| 1 0 0 -17 7 0 .21 11 11 | -1200 2177 22 123 | 0 1 1 12 10 18 .03 | 1015 1194 gfz 194| 0 1 0 -39 -46 28 -.08 17 17 | 261 -337 25 131 | 1 0 0 22 19 51 .03 | 213 280 grg 81| 0 -2 1 50 -18 39 1.11 41 38 | -313 71 109 345 | 1 3 1 42 43 57 .02 | 407 580 igr n/a| 0 0 0 6 -67 -21 .05 6 5 | -27861 -375 24 72 | 0 0 0 10 8 18 .02 | 1262 1485 jpl 131| -1 0 0 30 -22 18 .51 16 16 | 2807 -281 23 113 | 0 1 1 23 19 32 .04 | 1265 1399 mit 255| 0 -1 -1 21 -63 5 -.34 13 12 | 231 -486 21 159 | 0 0 0 47 39 17 .03 | 195 324 ngs 233| 0 0 0 23 129 -40 -.34 12 9 | -308 72 2288 3932 | 0 1 1 55 50 22 .04 | 408 581 sio 108| 0 2 -2 149 312 21 .26 24 23 | --- --- --- --- | 0 1 1 26 32 23 .03 | --- --- Table 1.1503.b GPS week : 1503 MJD: 54765.000-54771.000 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: mm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------+------------------------------------+------------------------------------------ 1 | 0 0 0 0 0 0 0 | 2 | 5 6 8 0 6 5 5 | 3 | 5 5 4 4 5 5 5 | 4 | 6 6 7 7 8 8 9 | 5 | 4 5 5 4 5 4 4 | 6 | 5 5 4 4 5 4 5 | 7 | 5 5 5 5 5 5 5 | 8 | 5 5 5 5 6 5 5 | 9 | 6 6 6 6 6 6 6 | 10 | 4 4 4 4 4 4 4 | 11 | 6 5 5 5 5 5 5 | 12 | 5 5 5 5 5 5 5 | 13 | 5 5 5 5 6 6 6 | 14 | 6 6 5 6 6 6 6 | 15 | 6 5 5 6 6 6 6 | 16 | 5 6 6 6 6 6 6 | 17 | 7 6 6 6 6 6 6 | 18 | 6 6 6 6 6 6 6 | 19 | 6 6 6 6 7 6 7 | 20 | 6 6 6 6 5 5 6 | 21 | 5 5 5 5 6 6 6 | 22 | 6 6 6 6 6 6 6 | 23 | 6 5 5 6 6 5 6 | 24 | 6 6 7 7 7 7 6 | 25 | 5 5 5 5 7 7 7 | 26 | 5 5 4 4 5 5 5 | 27 | 5 5 5 5 5 5 7 | 28 | 5 5 5 5 6 6 6 | 29 | 7 6 6 6 6 6 6 | 30 | 4 5 5 4 5 5 5 | 31 | 6 6 6 6 6 5 5 | 32 | 5 4 4 5 5 5 5 | Table 2: Daily transformation of each centre to the combined IGS orbit and clocks for each day of the week. The transformation displayed is the sum of a priori and estimated transformations. WRMS - RMS weighted by the centres SP3 header accuracy codes. STA - Number of stations in the daily solutions. Table 2.1503.0 GPS week: 1503 Day: 0 MJD: 54765.000 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 240| 1 0 0 28 -33 -21 -.23 10 9 | -140 -189 28 156 | -34 14 | emr 72| 0 -1 0 -188 -159 10 .48 16 16 | -200 -1336 19 222 | 21 139 | esa 128| 0 -2 2 -20 17 -14 .28 12 12 | -1294 915 23 117 | 61 -19 | gfz 194| 0 1 0 -22 -33 61 -.07 17 17 | 410 -493 26 125 | 18 1 | grg 81| 2 -2 3 137 16 -35 1.13 36 34 | -160 -190 94 308 | 3 80 | igr n/a| 0 0 1 -5 -55 -32 .07 6 6 | -28595 -1382 25 73 | -22 11 | jpl 131| -2 1 -2 47 11 56 .49 15 14 | 2026 -1272 25 127 | 6 38 | mit 255| 0 0 -1 62 -29 -2 -.39 13 12 | 423 -772 25 169 | -28 -27 | ngs 233| 0 0 2 -43 54 -43 -.39 12 9 | -123 -246 2108 3406 | 58 51 | sio 108| 0 1 -3 170 367 -3 .27 24 24 | --- --- --- --- | -72 -122 | Table 2.1503.1 GPS week: 1503 Day: 1 MJD: 54766.000 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 240| 0 0 0 17 -47 -2 -.25 10 9 | 254 -351 13 116 | 11 18 | emr 72| -3 0 3 -179 -150 -11 .40 16 16 | -1331 1987 14 211 | 5 111 | esa 128| 1 -1 0 -24 0 -17 .19 11 11 | -793 1843 21 122 | 20 -14 | gfz 194| 1 2 0 -25 -49 122 -.11 16 16 | 497 -708 23 132 | 30 38 | grg 81| 2 0 1 60 16 141 1.09 38 37 | 246 -373 93 297 | 63 44 | igr n/a| 0 0 0 8 -57 -33 .04 5 5 | -29844 1836 21 73 | -62 12 | jpl 131| 0 1 -1 56 -3 15 .49 16 15 | 674 1879 20 116 | -21 -19 | mit 255| 0 -2 -2 80 -30 -13 -.35 14 13 | 41 -372 16 151 | -16 -24 | ngs 233| 1 0 -1 -40 79 -70 -.31 12 9 | 245 -372 2416 3876 | 64 6 | sio 108| 0 0 -1 190 331 2 .26 22 25 | --- --- --- --- | -51 -111 | Table 2.1503.2 GPS week: 1503 Day: 2 MJD: 54767.000 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 240| 0 1 2 11 -61 -46 -.20 10 9 | 57 -602 21 143 | -35 33 | emr 72| -2 -2 1 -110 -152 15 .40 18 18 | 394 928 20 260 | -45 84 | esa 128| 0 0 0 -22 21 20 .20 9 10 | -520 1837 22 125 | 23 -57 | gfz 194| 1 1 -1 -56 -13 29 -.09 17 17 | 249 -435 27 123 | 34 -23 | grg 81| 1 0 3 14 15 28 1.12 37 38 | -12 -502 105 289 | -26 -66 | igr n/a| 0 0 0 27 -69 5 .05 6 6 | -28176 800 26 65 | -54 -7 | jpl 131| -2 0 0 45 -32 -11 .51 17 16 | 2616 712 24 120 | -3 32 | mit 255| 0 -1 -1 -32 -107 12 -.32 12 11 | 148 -337 23 165 | 28 17 | ngs 233| 1 1 0 71 160 -27 -.29 11 7 | -15 -494 2520 4425 | -123 -65 | sio 108| 0 3 -3 126 265 29 .31 23 23 | --- --- --- --- | -72 -114 | Table 2.1503.3 GPS week: 1503 Day: 3 MJD: 54768.000 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 240| 0 0 1 8 -57 13 -.24 10 10 | -865 1056 24 153 | -31 40 | emr 72| -5 -2 4 -105 -140 -10 .37 19 19 | 1539 469 17 244 | -95 101 | esa 128| 0 0 -1 -7 2 5 .21 11 11 | -1576 2964 27 132 | 17 6 | gfz 194| 0 0 0 -60 -66 4 -.07 16 16 | 74 -65 26 130 | 33 24 | grg 81| -2 0 2 38 1 9 1.10 39 36 | -878 1046 121 472 | -61 -21 | igr n/a| 0 0 0 1 -77 -44 .07 5 5 | -27117 623 24 65 | -19 41 | jpl 131| 0 0 0 10 -35 59 .58 15 15 | 3390 657 26 105 | 5 21 | mit 255| 1 -1 0 -39 -102 -15 -.35 11 11 | 239 -500 26 193 | 28 18 | ngs 233| 1 0 1 94 198 -65 -.33 12 9 | -879 1047 2209 3630 | -65 -112 | sio 108| 2 4 -2 121 321 1 .29 22 23 | --- --- --- --- | -87 -141 | Table 2.1503.4 GPS week: 1503 Day: 4 MJD: 54769.000 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 240| 0 0 0 9 -62 -14 -.23 10 9 | -209 -24 15 113 | 19 42 | emr 72| -3 -6 3 -121 -102 -4 .36 18 18 | 2774 -1408 19 239 | -47 55 | esa 128| 2 0 -1 -37 0 0 .19 12 11 | 368 635 22 129 | 30 -21 | gfz 194| 0 1 -1 -22 -45 2 -.04 17 17 | 509 -489 26 139 | 38 31 | grg 81| -1 -8 1 10 -40 81 1.13 48 40 | -204 -53 110 385 | 57 25 | igr n/a| 0 0 0 4 -66 -25 .03 6 6 | -25764 -1687 25 74 | -5 16 | jpl 131| 0 0 0 5 -35 26 .53 17 17 | 4779 -1474 24 128 | 15 55 | mit 255| 0 -1 0 43 -42 9 -.33 13 13 | 556 -872 19 152 | 10 -24 | ngs 233| 0 0 0 23 128 -45 -.38 14 10 | -202 -38 2300 4059 | -38 -42 | sio 108| 0 2 0 166 304 16 .24 24 22 | --- --- --- --- | -91 -112 | Table 2.1503.5 GPS week: 1503 Day: 5 MJD: 54770.000 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 240| 0 1 0 23 -70 -20 -.23 12 11 | -793 744 17 114 | -22 -8 | emr 72| -2 -5 5 -155 -133 -6 .39 17 17 | 1100 75 19 231 | 6 76 | esa 128| 1 0 -2 0 14 -18 .20 10 10 | -2822 3767 22 121 | 52 11 | gfz 194| -2 1 0 -71 -69 18 -.12 17 17 | 103 -283 27 144 | 59 0 | grg 81| 1 -4 0 46 -39 10 1.11 45 39 | -793 716 122 315 | -46 -43 | igr n/a| 0 0 0 5 -74 -21 .05 5 5 | -27641 -663 23 76 | -10 24 | jpl 131| -1 0 1 1 -21 9 .48 17 16 | 3192 -537 24 94 | 26 -56 | mit 255| 2 -1 0 -3 -108 32 -.29 13 12 | 182 -647 18 142 | 7 6 | ngs 233| 0 2 0 67 165 -22 -.32 11 9 | -788 717 2280 4013 | -107 -54 | sio 108| 1 2 0 138 285 56 .24 25 22 | --- --- --- --- | -102 -124 | Table 2.1503.6 GPS week: 1503 Day: 6 MJD: 54771.000 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 240| 0 0 0 26 -54 -26 -.24 11 10 | -416 -66 14 136 | 13 23 | emr 72| -1 -4 2 -166 -145 23 .42 18 18 | 1576 -1714 17 233 | 3 113 | esa 128| 1 1 -2 -7 -5 26 .23 11 11 | -1767 3280 23 115 | 48 -5 | gfz 194| 0 2 -1 -14 -47 -42 -.07 18 18 | -9 111 25 130 | 42 22 | grg 81| 0 0 0 42 -98 41 1.12 46 43 | -390 -144 120 352 | 11 25 | igr n/a| 0 0 0 0 -70 0 .04 6 6 | -27892 -2154 27 78 | -16 26 | jpl 131| -2 -3 1 45 -39 -26 .50 18 17 | 2977 -1937 23 102 | -74 -60 | mit 255| 0 -1 0 40 -26 18 -.32 15 12 | 29 96 20 144 | -6 -20 | ngs 233| 0 1 2 -7 118 -10 -.36 12 8 | -396 -109 2185 4121 | -45 -71 | sio 108| 0 4 -4 130 312 47 .25 26 23 | --- --- --- --- | -75 -114 | 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 3.1503.0 GPS week: 1503 Day: 0 MJD: 54765.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 4 --- --- --- --- >>>> --- --- --- --- 0 | 26 --- --- --- --- --- --- --- --- --- 27 2E | 11 17 13 10 45 6 15 14 11 18 5 | 13 22 12 17 28 --- 15 13 12 18 13 3 | 11 14 9 12 26 6 13 9 9 32 5 | 21 22 20 15 25 --- 23 22 13 25 16 4E | 13 20 13 12 43 7 13 11 22 20 6 | 30 44 35 40 52 --- 43 32 37 36 33 5 | 9 12 8 14 28 4 9 10 9 17 4 | 18 22 18 19 17 --- 22 26 19 15 18 6 | 5 13 8 14 28 7 13 13 9 29 4 | 17 24 21 11 25 --- 23 24 12 27 16 7 | 9 18 13 18 36 6 13 11 9 24 5 | 12 31 22 23 40 --- 23 13 14 18 14 8 | 8 15 7 15 19 5 13 11 8 33 5 | 15 25 19 22 29 --- 24 17 15 40 16 9 | 12 21 9 12 31 4 15 18 9 26 5 | 20 34 21 23 44 --- 26 20 19 35 19 10 | 6 12 8 8 30 5 10 11 11 21 4 | 26 29 26 28 28 --- 25 24 29 32 25 11E | 8 14 17 16 29 6 17 11 14 19 5 | 23 27 20 28 24 --- 25 23 25 21 20 12 | 8 13 9 15 47 5 13 14 8 20 4 | 20 23 21 22 33 --- 23 26 22 18 19 13 | 8 16 12 18 40 5 19 11 13 14 5 | 18 33 19 29 49 --- 29 17 19 18 18 14 | 6 15 16 23 34 4 17 11 15 23 5 | 22 30 21 32 43 --- 33 22 20 19 21 15 | 10 16 11 18 31 4 18 18 11 20 5 | 22 34 23 31 30 --- 33 20 28 19 23 16 | 9 12 12 15 35 7 14 11 11 36 5 | 17 23 21 20 33 --- 23 22 16 20 16 17 | 12 21 13 22 33 6 15 13 21 29 6 | 17 39 25 37 52 --- 37 21 32 20 24 18 | 9 20 15 22 28 6 20 13 9 23 6 | 15 35 22 31 35 --- 33 21 18 20 19 19 | 9 17 13 26 31 8 20 13 11 26 6 | 28 36 22 42 41 --- 37 25 29 29 27 20 | 10 17 15 23 36 4 17 12 11 20 5 | 18 27 23 24 34 --- 22 19 20 18 17 21E | 8 12 14 12 44 11 20 12 11 18 5 | 18 26 25 20 49 --- 28 19 17 24 18 22 | 10 17 16 24 33 6 17 12 10 19 5 | 19 33 26 28 37 --- 29 24 21 17 21 23 | 9 19 15 17 29 5 20 11 16 15 5 | 19 34 20 27 38 --- 28 17 20 20 18 24E | 16 15 13 17 46 7 16 15 18 20 6 | 60 60 60 62 64 --- 62 61 63 59 59 25 | 9 16 9 13 52 6 13 14 7 25 4 | 60 66 59 64 86 --- 70 60 59 68 61 26 | 9 12 7 13 20 5 10 16 8 23 4 | 24 33 26 26 31 --- 25 23 25 27 23 27E | 8 18 8 13 21 6 14 10 8 27 4 | 17 31 22 21 34 --- 22 20 17 35 18 28 | 8 11 10 13 54 7 14 13 14 35 5 | 26 32 30 25 43 --- 33 29 26 19 26 29 | 12 19 17 22 58 8 19 13 11 36 6 | 19 35 19 34 63 --- 35 20 20 34 21 30 | 9 9 7 18 30 4 8 14 7 21 4 | 28 31 31 31 29 --- 32 35 27 25 28 31 | 10 22 15 16 31 6 13 13 9 26 5 | 14 33 22 24 42 --- 25 20 15 17 17 32 | 9 17 11 14 28 5 11 9 8 18 4 | 20 23 21 22 33 --- 20 18 20 20 18 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 16 12 17 36 6 15 13 12 24 |T 22 32 24 28 39 --- 29 24 23 26 22 WRMS | 9 16 12 17 34 6 14 12 9 24 |NE 20 30 22 26 36 --- 27 21 20 23 20 MEDI | 9 16 12 15 31 6 14 12 11 23 |MD 19 31 22 26 35 --- 26 22 20 20 19 Table 3.1503.1 GPS week: 1503 Day: 1 MJD: 54766.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 27 --- --- --- --- 0 | 35 --- --- --- --- --- --- --- --- --- 35 X2E | 8 15 12 14 47 7 --- 14 14 18 5 | 14 22 19 16 31 --- --- 14 15 19 18 3 | 6 16 10 13 37 6 12 12 12 24 4 | 23 27 28 22 31 --- 25 23 23 29 24 4E | 13 17 12 12 50 7 15 13 24 19 6 | 20 33 26 32 51 --- 35 24 34 34 25 5 | 10 9 8 15 35 4 12 15 11 20 4 | 14 19 14 15 23 --- 20 20 18 18 15 6 | 6 16 8 9 23 5 12 13 12 21 4 | 13 22 18 12 24 --- 20 19 17 22 15 7 | 10 20 11 17 38 4 14 12 10 18 5 | 10 28 15 21 43 --- 21 11 12 15 11 8 | 9 14 8 14 16 5 13 15 8 32 5 | 19 28 24 24 23 --- 23 20 22 38 20 9 | 11 19 8 14 19 6 19 20 13 25 6 | 14 26 18 20 33 --- 28 18 18 33 16 10 | 7 11 10 7 34 4 9 10 12 17 4 | 29 37 32 28 27 --- 31 31 31 27 30 11E | 7 13 12 15 32 5 16 10 8 17 4 | 19 27 20 23 29 --- 25 24 24 22 20 12 | 11 14 9 12 39 7 15 16 12 23 5 | 14 22 15 17 27 --- 20 18 19 17 15 13 | 8 15 14 19 33 4 18 12 10 12 5 | 14 30 17 28 46 --- 26 15 19 18 16 14 | 7 16 13 19 42 5 18 16 11 19 5 | 16 28 21 25 40 --- 28 17 17 23 17 15 | 8 14 11 17 24 5 19 18 11 17 5 | 22 32 20 30 32 --- 31 20 20 21 21 16 | 9 14 11 13 44 6 15 14 13 34 5 | 14 26 19 19 32 --- 23 16 12 20 15 17 | 10 22 10 19 33 6 19 13 10 25 5 | 15 36 27 28 46 --- 37 17 18 18 21 18 | 10 19 15 22 39 5 20 13 11 20 6 | 14 34 23 27 36 --- 29 16 21 19 19 19 | 10 19 11 22 30 7 21 15 12 25 6 | 23 34 24 33 32 --- 34 24 23 23 24 20 | 10 17 13 21 36 4 17 12 9 18 5 | 16 29 22 26 37 --- 25 17 17 14 18 21E | 10 15 12 11 78 6 20 14 14 16 5 | 12 24 18 17 53 --- 20 15 19 20 14 22 | 11 14 11 22 30 6 18 16 12 20 5 | 15 32 21 26 39 --- 29 19 20 20 19 23 | 9 17 14 18 26 6 18 13 12 15 5 | 13 30 19 23 37 --- 25 15 19 21 16 24E | 14 17 9 19 48 8 15 17 17 17 6 | 54 58 54 60 54 --- 55 56 60 55 55 25 | 10 15 11 14 48 4 14 15 9 24 5 | 47 55 46 57 75 --- 59 47 48 55 50 26 | 8 13 7 14 24 4 10 17 8 19 4 | 17 29 19 21 26 --- 20 20 17 20 17 27E | 11 15 10 13 36 5 16 14 9 25 5 | 11 26 17 20 35 --- 25 16 17 33 16 28 | 8 11 9 12 39 6 14 11 8 35 5 | 19 28 23 22 35 --- 29 21 22 15 21 29 | 13 22 13 19 50 7 20 13 12 28 6 | 14 32 16 29 47 --- 30 17 19 31 18 30 | 11 9 9 20 31 5 10 13 9 21 4 | 21 23 21 25 28 --- 26 27 22 31 22 31 | 9 26 10 15 38 5 18 18 12 26 6 | 12 34 17 20 39 --- 27 13 13 19 14 32 | 6 17 11 14 30 4 13 7 7 18 4 | 21 28 27 25 42 --- 25 23 24 23 23 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 16 11 16 38 5 16 14 12 22 |T 19 30 22 25 37 --- 28 21 21 24 21 WRMS | 9 16 11 16 37 5 15 13 9 25 |NE 17 28 20 23 34 --- 26 19 19 22 19 MEDI | 9 15 11 15 36 5 15 14 11 20 |MD 15 28 20 24 35 --- 26 19 19 21 18 Table 3.1503.2 GPS week: 1503 Day: 2 MJD: 54767.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 13 --- --- --- --- 0 | 24 --- --- --- --- --- --- --- --- --- 26 X2E | 9 --- 7 --- --- 9 --- --- --- --- 8 | 16 --- 17 --- --- --- --- --- --- --- 17 3 | 7 15 5 11 30 3 12 10 10 25 4 | 29 32 32 28 41 --- 33 27 29 38 29 4E | 17 21 13 12 49 6 21 12 23 33 7 | 29 40 34 35 65 --- 45 30 37 37 32 5 | 9 11 8 16 22 4 11 11 6 25 4 | 17 24 23 24 27 --- 25 27 24 25 22 6 | 5 17 4 11 22 3 12 10 11 22 4 | 15 24 22 16 29 --- 25 19 21 29 19 7 | 8 21 8 12 47 6 17 12 9 19 4 | 15 27 17 21 46 --- 24 15 20 21 18 8 | 9 14 7 14 34 6 15 12 8 29 4 | 18 25 22 26 34 --- 23 22 23 36 21 9 | 12 22 9 13 29 5 18 15 16 26 6 | 16 31 21 23 39 --- 27 23 28 39 22 10 | 9 12 5 10 31 6 11 8 10 11 3 | 14 20 18 19 32 --- 20 17 17 23 17 11E | 9 20 11 14 49 4 19 12 7 19 5 | 18 29 22 27 37 --- 27 22 24 21 21 12 | 11 12 10 15 40 6 14 10 8 27 4 | 22 29 26 28 32 --- 26 26 27 21 25 13 | 8 20 11 18 29 5 17 12 8 14 5 | 17 31 21 24 44 --- 30 21 24 26 21 14 | 8 19 11 20 37 6 19 11 9 18 5 | 18 30 23 27 38 --- 29 18 21 25 21 15 | 10 19 9 18 23 8 20 15 10 17 5 | 16 30 23 31 32 --- 30 18 25 18 22 16 | 8 18 9 12 43 5 15 15 12 36 5 | 19 29 23 23 36 --- 26 19 20 24 21 17 | 10 22 12 20 30 7 21 10 14 23 6 | 19 39 26 29 41 --- 36 19 22 21 23 18 | 7 20 12 22 30 5 20 12 8 18 5 | 15 31 20 29 37 --- 28 15 19 18 18 19 | 8 20 10 24 40 8 22 12 10 22 5 | 27 40 25 39 47 --- 40 21 30 23 28 20 | 11 18 12 23 39 5 18 11 8 15 5 | 18 27 20 24 31 --- 27 17 16 15 17 21E | 7 20 10 16 31 5 18 16 12 13 5 | 22 29 25 24 40 --- 25 21 20 25 22 22 | 10 19 11 24 23 7 21 14 10 19 5 | 15 30 22 27 38 --- 28 21 19 21 20 23 | 7 21 12 16 29 5 19 10 8 17 5 | 16 33 22 24 35 --- 29 19 22 26 21 24E | 17 23 11 18 51 7 19 15 23 16 6 | 32 39 31 40 49 --- 36 33 46 38 34 25 | 8 16 9 16 61 5 13 14 8 25 4 | 52 56 51 59 77 --- 60 55 55 62 55 26 | 8 13 6 15 25 5 12 14 10 16 4 | 14 25 21 23 30 --- 20 20 22 23 19 27E | 9 17 9 23 53 6 16 13 9 20 5 | 18 25 23 29 41 --- 27 21 24 37 23 28 | 8 13 8 12 41 5 18 12 13 37 5 | 23 33 28 23 30 --- 32 28 30 21 27 29 | 13 21 11 20 42 8 23 11 11 23 6 | 18 34 24 33 43 --- 38 22 21 30 24 30 | 9 17 6 18 30 3 10 11 5 21 4 | 22 27 23 28 29 --- 25 28 25 29 25 31 | 9 23 10 15 38 5 17 14 10 33 5 | 16 29 20 20 41 --- 28 16 14 28 18 32 | 7 19 8 12 35 4 15 6 5 19 4 | 18 22 20 16 29 --- 19 18 18 25 16 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 9 17 37 6 17 12 11 23 |T 20 30 24 27 39 --- 29 22 24 27 23 WRMS | 9 18 10 17 38 6 16 11 7 23 |NE 18 29 22 25 35 --- 27 20 22 25 21 MEDI | 9 19 9 16 34 5 17 12 10 20 |MD 18 29 23 26 37 --- 27 21 22 25 21 Table 3.1503.3 GPS week: 1503 Day: 3 MJD: 54768.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 28 --- --- --- --- 0 | 38 --- --- --- --- --- --- --- --- --- 40 X2E | 5 --- --- --- --- 13 --- --- --- --- 0 | 22 --- --- --- --- --- --- --- --- --- 24 3 | 7 14 8 11 38 4 11 9 8 28 4 | 18 21 24 19 34 --- 25 24 19 28 20 4E | 13 20 14 16 92 7 15 9 23 41 7 | 24 35 31 37 66 --- 40 25 32 34 27 5 | 9 12 9 13 31 4 9 8 9 19 4 | 20 27 25 23 35 --- 25 27 27 27 24 6 | 5 13 8 12 29 2 13 10 8 21 4 | 15 22 22 13 27 --- 23 19 17 30 17 7 | 12 21 12 13 48 5 14 10 11 17 5 | 12 26 15 19 47 --- 22 11 14 14 13 8 | 11 17 8 15 28 5 11 11 12 29 5 | 28 34 29 33 37 --- 33 30 29 44 29 9 | 14 23 8 12 23 5 15 14 10 25 5 | 16 28 19 19 28 --- 24 16 17 34 17 10 | 12 12 9 8 37 4 7 8 12 16 4 | 36 37 38 36 34 --- 39 35 37 33 36 11E | 11 17 11 15 41 4 15 9 8 10 4 | 17 25 17 25 37 --- 23 20 21 16 17 12 | 10 14 11 12 23 7 13 11 8 24 4 | 19 27 22 21 33 --- 25 24 21 22 21 13 | 11 21 13 17 30 4 15 12 12 11 5 | 14 31 15 27 45 --- 30 19 22 22 18 14 | 7 22 13 21 37 6 18 10 13 14 5 | 17 31 21 27 41 --- 29 15 21 22 19 15 | 10 21 10 17 24 6 18 12 11 19 5 | 18 34 21 29 34 --- 31 17 21 19 20 16 | 9 17 8 14 36 4 14 19 12 33 5 | 16 25 22 18 31 --- 27 23 17 23 18 17 | 9 22 13 20 30 7 18 11 12 24 5 | 20 37 25 26 46 --- 37 18 21 21 22 18 | 9 19 14 19 28 5 21 12 11 15 5 | 16 31 22 25 42 --- 31 17 20 19 18 19 | 10 21 13 23 35 8 20 13 12 26 6 | 25 39 27 42 45 --- 42 28 26 20 27 20 | 13 20 11 19 43 4 20 12 10 13 5 | 15 30 17 24 41 --- 29 15 14 13 15 21E | 9 20 9 13 39 4 18 12 11 12 5 | 23 31 29 25 49 --- 31 23 25 25 24 22 | 10 20 16 23 32 5 19 11 12 21 6 | 18 29 26 25 37 --- 30 20 18 23 19 23 | 12 24 14 16 29 5 19 10 11 16 5 | 14 34 18 26 39 --- 31 17 23 21 19 24E | 15 25 11 17 42 6 13 15 22 19 6 | 51 55 52 52 65 --- 55 50 54 56 51 25E | 12 23 10 16 61 5 12 10 9 27 5 | 83 87 83 91 117 --- 89 83 82 93 84 26 | 9 13 6 14 19 6 9 11 11 19 4 | 16 22 20 19 25 --- 20 17 20 22 16 27E | 11 17 10 15 35 5 13 10 12 24 5 | 15 23 21 23 37 --- 23 17 18 33 18 28 | 8 14 10 11 45 5 13 11 11 36 5 | 25 30 28 27 34 --- 34 27 26 24 26 29 | 13 22 14 19 37 7 22 9 13 23 6 | 24 40 29 40 42 --- 42 26 32 27 29 30 | 8 14 8 17 28 4 9 8 8 20 4 | 24 28 32 30 32 --- 25 30 27 31 27 31 | 6 26 11 17 33 4 14 14 10 19 5 | 13 31 16 19 44 --- 25 13 14 20 15 32 | 9 20 10 12 40 3 14 8 9 17 4 | 31 34 33 33 34 --- 36 31 35 35 31 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 19 11 16 39 5 15 11 12 22 |T 23 32 26 29 41 --- 32 24 25 28 25 WRMS | 10 19 11 16 36 5 15 11 9 23 |NE 20 30 23 25 36 --- 29 21 22 24 22 MEDI | 10 20 10 15 35 5 14 11 11 19 |MD 18 31 22 25 37 --- 30 20 21 23 20 Table 3.1503.4 GPS week: 1503 Day: 4 MJD: 54769.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 54 --- --- --- --- 0 | 42 --- --- --- --- --- --- --- --- --- 44 2E | 10 16 11 13 52 7 21 15 16 13 5 | 17 26 18 19 30 --- 27 17 22 18 21 3 | 7 13 10 15 56 4 12 11 10 36 5 | 18 25 26 21 41 --- 25 17 22 42 21 4E | 17 20 26 15 151 7 23 10 21 22 7 | 26 37 45 35 137 --- 40 24 37 35 30 5 | 8 13 7 15 34 6 10 11 9 28 4 | 16 23 20 19 26 --- 19 21 17 23 17 6 | 7 12 10 13 44 5 12 13 11 26 4 | 12 23 21 17 35 --- 20 17 15 30 16 7 | 12 17 9 13 45 8 19 14 12 17 5 | 11 28 17 19 42 --- 24 11 21 16 14 8 | 14 15 12 15 34 5 13 13 11 42 6 | 62 65 68 67 58 --- 69 67 63 71 65 9 | 11 22 7 12 26 6 15 15 14 26 5 | 12 28 17 17 34 --- 23 15 20 34 15 10 | 6 10 8 9 52 7 11 11 12 18 4 | 19 27 18 23 30 --- 22 19 24 25 20 11E | 8 15 11 18 60 5 14 12 9 12 4 | 20 30 22 28 49 --- 27 18 26 20 21 12 | 10 11 9 15 32 9 14 10 8 31 5 | 19 25 22 23 28 --- 21 19 19 21 18 13 | 10 18 13 21 48 7 19 17 16 12 6 | 14 31 14 23 56 --- 27 19 20 19 16 14 | 7 20 13 24 38 5 21 13 16 16 6 | 11 33 18 27 40 --- 29 13 19 17 16 15 | 7 16 15 18 27 5 17 13 13 22 5 | 15 28 15 28 30 --- 26 15 19 18 17 16 | 12 14 15 14 40 6 18 17 13 33 6 | 13 24 19 20 31 --- 22 20 12 17 12 17 | 10 23 13 20 53 5 19 13 15 24 6 | 15 40 26 27 54 --- 37 17 26 22 22 18 | 10 22 14 21 35 4 20 12 12 17 6 | 11 30 18 25 38 --- 29 13 13 18 14 19 | 11 20 13 25 41 5 21 14 15 26 6 | 21 36 19 36 47 --- 37 17 25 20 22 20 | 10 16 10 20 37 5 17 11 12 13 5 | 17 29 19 23 42 --- 27 16 19 15 16 21E | 9 24 14 15 27 5 20 9 15 14 5 | 15 26 18 19 35 --- 23 17 18 19 15 22 | 9 17 14 23 43 4 19 13 13 21 6 | 14 29 24 24 38 --- 28 17 15 20 17 23 | 10 22 14 19 25 5 21 15 12 19 6 | 11 32 14 22 36 --- 26 14 17 22 14 24E | 16 22 8 16 42 6 17 15 29 17 7 | 25 33 24 30 40 --- 30 28 43 27 26 25E | 17 22 18 22 48 8 18 15 15 23 7 | 52 60 53 62 69 --- 64 52 55 55 54 26 | 9 15 10 14 22 6 11 12 13 23 4 | 12 26 16 20 26 --- 20 17 21 20 16 27E | 10 15 8 17 41 5 15 14 10 24 5 | 14 27 19 23 39 --- 25 16 21 32 17 28 | 10 12 10 13 44 6 20 11 12 36 5 | 23 27 26 22 34 --- 28 19 24 16 21 29 | 9 16 15 20 43 9 21 11 16 23 6 | 14 28 18 28 44 --- 30 14 21 20 18 30 | 8 15 5 21 26 5 11 11 7 28 5 | 23 26 26 31 29 --- 26 26 24 24 23 31 | 8 22 12 17 36 5 14 14 13 15 5 | 13 29 17 20 44 --- 24 14 16 17 14 32 | 7 21 7 14 26 5 12 10 14 18 4 | 18 24 16 20 25 --- 21 17 16 19 15 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 10 18 12 17 48 6 17 13 14 24 |T 19 30 23 26 42 --- 28 20 23 24 21 WRMS | 9 18 11 17 40 6 17 13 10 22 |NE 18 29 21 25 37 --- 27 18 21 23 20 MEDI | 10 16 11 16 41 5 17 13 13 22 |MD 15 28 19 23 38 --- 26 17 21 20 17 Table 3.1503.5 GPS week: 1503 Day: 5 MJD: 54770.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 37 --- --- --- --- 0 | 34 --- --- --- --- --- --- --- --- --- 36 2E | 12 14 9 15 48 4 23 15 8 14 5 | 26 28 25 23 44 --- 26 16 23 16 28 3 | 8 11 8 14 49 5 11 12 8 29 4 | 12 22 19 14 34 --- 18 16 15 37 15 4E | 18 21 11 14 85 9 19 30 17 28 7 | 20 33 26 29 57 --- 39 34 28 37 24 5 | 7 13 7 15 44 3 7 11 7 27 4 | 14 21 17 16 41 --- 15 19 22 22 16 6 | 8 15 8 12 37 5 11 13 8 22 4 | 15 27 21 15 33 --- 20 21 15 31 17 7 | 13 20 10 15 60 6 15 11 9 17 5 | 12 30 18 22 56 --- 24 15 18 16 16 8 | 11 16 8 15 22 5 13 12 10 31 5 | 38 45 38 41 36 --- 38 38 46 51 39 9 | 16 21 10 13 41 6 15 14 12 24 5 | 15 27 21 18 49 --- 20 16 21 34 17 10 | 9 8 6 8 33 4 9 10 11 13 3 | 25 27 27 25 34 --- 27 24 23 24 25 11E | 11 14 13 21 38 3 18 8 9 16 5 | 16 25 18 32 39 --- 24 17 21 16 17 12 | 7 13 7 14 38 5 12 11 8 31 4 | 17 24 20 20 38 --- 22 17 19 21 18 13 | 11 19 13 22 37 6 19 15 9 18 5 | 16 31 19 28 46 --- 31 22 21 22 19 14 | 7 19 11 21 34 4 18 15 11 19 5 | 15 31 20 24 39 --- 26 16 20 20 19 15 | 19 20 11 18 24 5 18 13 11 23 6 | 23 31 25 29 32 --- 26 15 23 15 22 16 | 10 13 9 16 26 5 16 15 10 33 5 | 17 26 25 23 38 --- 26 19 18 16 20 17 | 12 16 10 20 55 4 19 10 9 26 5 | 15 34 22 28 52 --- 38 17 20 28 22 18 | 9 18 11 19 28 5 24 14 12 20 5 | 17 30 21 27 39 --- 31 14 23 18 20 19 | 11 20 12 22 51 6 21 13 8 32 6 | 19 36 19 34 53 --- 38 16 20 28 21 20 | 11 17 10 21 65 5 18 12 7 18 5 | 14 27 15 23 55 --- 24 14 13 14 14 21E | 12 18 15 12 35 6 19 17 10 14 5 | 26 31 35 29 47 --- 28 25 27 26 26 22 | 11 19 11 22 27 5 22 14 11 25 6 | 14 29 21 26 37 --- 28 15 23 19 19 23 | 12 20 13 17 35 5 18 11 8 17 5 | 13 32 21 24 42 --- 28 16 16 21 17 24E | 16 18 12 14 39 5 19 12 24 14 6 | 56 56 59 61 59 --- 60 51 66 61 57 25E | 22 17 11 21 58 7 22 15 12 45 7 | 69 72 69 77 85 --- 80 65 65 81 69 26 | 15 13 7 14 22 5 10 12 9 22 4 | 18 25 19 21 28 --- 18 15 18 16 16 27E | 11 18 8 13 44 4 16 13 9 24 5 | 18 28 23 27 48 --- 26 23 27 35 23 28 | 10 14 13 16 50 5 16 9 9 38 5 | 16 28 22 18 36 --- 30 14 16 17 18 29 | 11 20 12 22 64 5 19 11 11 28 6 | 15 34 20 32 56 --- 30 21 23 26 22 30 | 6 16 6 18 32 5 10 11 9 29 4 | 21 23 22 21 46 --- 22 21 22 23 20 31 | 8 20 10 19 52 5 13 10 11 25 5 | 10 27 16 18 45 --- 22 10 14 21 14 32 | 8 20 10 14 43 3 15 8 9 27 5 | 29 35 32 30 46 --- 32 27 32 31 29 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 17 10 17 45 5 17 13 11 25 |T 21 31 25 27 44 --- 29 21 24 27 23 WRMS | 11 17 10 17 39 5 16 12 9 22 |NE 18 29 21 24 42 --- 26 18 20 23 20 MEDI | 11 18 10 16 39 5 18 12 9 24 |MD 17 29 21 25 44 --- 26 17 21 22 20 Table 3.1503.6 GPS week: 1503 Day: 6 MJD: 54771.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- X1 | 5 --- --- --- --- 32 --- --- --- --- 0 | 31 --- --- --- --- --- --- --- --- --- 31 2E | 8 15 12 13 67 5 21 14 11 13 5 | 23 21 16 16 39 --- 22 14 12 16 24 3 | 7 16 8 14 33 5 11 12 7 35 5 | 14 22 20 21 29 --- 20 20 15 36 15 4E | 16 22 9 17 72 8 38 40 16 30 9 | 25 40 30 36 69 --- 54 38 28 38 28 5 | 8 12 7 15 28 7 8 10 6 24 4 | 18 23 19 19 19 --- 23 23 20 22 18 6 | 6 16 9 15 26 5 12 13 8 29 4 | 19 27 24 19 32 --- 26 23 21 41 21 7 | 12 23 8 13 52 6 16 11 12 18 5 | 13 32 17 18 49 --- 25 13 21 20 15 8 | 9 15 7 17 35 5 12 14 12 32 5 | 41 44 45 41 52 --- 46 45 38 54 41 9 | 14 20 12 10 79 5 16 15 14 22 5 | 18 26 17 19 60 --- 28 16 15 34 15 10 | 10 12 6 10 44 7 10 12 11 15 4 | 22 30 25 25 33 --- 27 23 25 22 23 11E | 13 18 12 18 50 7 15 12 9 12 5 | 23 34 26 28 57 --- 30 21 31 19 23 12 | 8 14 9 15 36 6 16 11 10 34 5 | 20 29 24 22 27 --- 24 22 22 29 21 13 | 13 18 12 21 31 6 18 16 15 13 6 | 12 28 13 25 40 --- 27 18 19 21 14 14 | 9 18 14 24 46 7 19 13 13 15 5 | 12 28 19 26 38 --- 29 20 18 21 16 15 | 7 19 11 16 32 6 20 14 12 17 5 | 18 27 17 28 33 --- 29 16 19 20 17 16 | 9 17 10 18 28 6 18 11 10 38 5 | 14 26 24 27 31 --- 26 15 16 16 18 17 | 13 21 13 23 52 6 20 12 10 27 6 | 15 40 21 27 53 --- 40 16 21 25 20 18 | 10 22 14 19 35 5 20 12 13 23 6 | 14 29 20 25 44 --- 28 14 16 28 15 19 | 9 20 13 30 30 7 21 15 13 36 7 | 21 40 21 43 48 --- 41 18 27 30 25 20 | 10 17 12 23 47 4 18 13 11 14 5 | 17 28 18 26 47 --- 27 18 19 18 16 21E | 14 16 14 13 31 5 18 14 13 12 5 | 19 25 27 19 45 --- 27 23 18 26 19 22 | 10 15 13 23 32 6 24 12 11 20 6 | 15 30 24 25 40 --- 28 19 16 24 18 23 | 11 22 14 18 30 4 22 12 11 23 6 | 12 33 17 25 43 --- 30 16 19 26 15 24E | 13 19 9 17 35 7 17 21 19 16 6 | 57 64 62 61 70 --- 66 66 69 66 62 25E | 20 21 12 22 85 6 20 16 13 32 7 | 76 79 75 82 98 --- 84 73 76 79 75 26 | 8 12 7 13 33 5 11 13 14 18 4 | 10 22 14 18 31 --- 20 16 19 18 12 27E | 15 20 9 19 51 6 16 20 11 33 6 | 27 36 27 34 52 --- 34 29 19 32 25 28 | 10 14 7 16 48 5 16 9 8 44 5 | 29 31 31 26 41 --- 32 26 31 30 27 29 | 11 19 12 18 48 5 23 13 12 26 6 | 19 32 22 34 55 --- 35 21 21 24 21 30 | 7 10 5 20 36 6 10 12 7 31 4 | 28 31 31 32 27 --- 31 33 31 33 28 31 | 9 17 10 15 52 8 14 12 11 28 5 | 15 28 17 20 46 --- 27 11 13 25 14 32 | 8 19 11 13 41 3 18 13 7 22 5 | 29 36 31 27 40 --- 38 28 30 44 28 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 18 11 18 46 6 18 15 12 26 |T 22 32 25 28 44 --- 33 24 24 30 23 WRMS | 10 18 11 18 43 6 17 12 8 23 |NE 19 30 22 25 39 --- 29 20 21 27 20 MEDI | 10 18 11 17 36 6 18 13 11 23 |MD 19 30 22 26 43 --- 28 20 20 26 20 Table 4: Precise Navigation Summary. Weekly station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. See Table 5 for the daily summary. CLK - Satellite clocks used. EPO - Mean number of satellite clock epochs available in the daily solutions. Units: mm. Table 4.1503 GPS week: 1503 MJD: 54765.0-54771.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3056 |U 10 9 30 |U 16 15 38 | emr | emr 2939 | 11 9 28 | 9 8 22 | esa | esa 2948 | 9 9 27 | 8 7 18 | gfz | gfz 2928 |U 10 9 27 | 10 7 23 | igr | igr 2953 | 10 11 27 | 7 7 19 | igs | igs 2943 | 9 8 25 | 7 7 18 | jpl | jpl 2923 |U 12 12 39 |U 8 8 20 | mit | mit 2948 |U 10 10 30 |U 9 8 19 | 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 5.1503.0 GPS week: 1503 Day: 0 MJD: 54765.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3072 | 10 6 22 | 7 7 16 | emr | emr 2968 | 11 7 31 | 8 7 16 | esa | esa 2976 | 9 8 26 | 7 7 15 | gfz | gfz 2958 | 11 9 28 | 10 7 18 | igr | igr 2972 | 11 9 29 | 7 7 14 | igs | igs 2976 | 10 7 25 | 7 7 13 | jpl | jpl 2966 | 11 9 27 | 7 7 15 | mit | mit 2976 | 11 8 31 | 8 8 18 | Table 5.1503.1 GPS week: 1503 Day: 1 MJD: 54766.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3069 | 10 14 31 | 8 5 18 | emr | emr 2968 | 10 11 32 | 10 7 25 | esa | esa 2976 | 10 19 34 | 8 5 17 | gfz | gfz 2956 | 11 18 38 | 11 7 25 | igr | igr 2972 | 10 15 38 | 8 5 20 | igs | igs 2972 | 9 13 34 | 7 6 19 | jpl | jpl 2871 | 14 16 40 | 8 9 22 | mit | mit 2976 | 10 14 43 | 7 5 19 | Table 5.1503.2 GPS week: 1503 Day: 2 MJD: 54767.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 2976 | 16 17 76 | 63 59 157 | emr | emr 2872 | 12 9 27 | 10 8 20 | esa | esa 2880 | 9 6 25 | 8 8 15 | gfz | gfz 2863 | 9 7 24 | 10 8 23 | igs | igs 2878 | 7 5 22 | 8 7 16 | jpl | jpl 2872 | 8 10 23 | 8 7 19 | mit | mit 2880 | 7 5 22 | 9 6 18 | Table 5.1503.3 GPS week: 1503 Day: 3 MJD: 54768.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3065 | 9 7 20 | 6 7 17 | emr | emr 2872 | 12 10 25 | 8 9 23 | esa | esa 2880 | 10 8 26 | 6 8 21 | gfz | gfz 2864 | 10 8 26 | 10 9 24 | igr | igr 2875 | 11 11 25 | 6 6 19 | igs | igs 2880 | 10 9 25 | 6 7 19 | jpl | jpl 2870 | 11 10 24 | 7 7 20 | mit | mit 2880 | 11 12 30 | 6 7 18 | Table 5.1503.4 GPS week: 1503 Day: 4 MJD: 54769.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3071 | 8 6 24 | 10 8 20 | emr | emr 2968 | 10 8 27 | 10 9 29 | esa | esa 2976 | 9 7 28 | 10 7 21 | gfz | gfz 2953 | 10 8 29 | 11 7 27 | igr | igr 2964 | 8 9 28 | 9 8 24 | igs | igs 2961 | 8 6 26 | 9 8 22 | jpl | jpl 2965 | 8 7 26 | 9 8 26 | mit | mit 2976 | 9 7 26 | 10 8 22 | Table 5.1503.5 GPS week: 1503 Day: 5 MJD: 54770.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3072 | 8 10 20 | 8 9 22 | emr | emr 2964 | 9 8 33 | 10 7 25 | esa | esa 2976 | 8 8 21 | 8 7 20 | gfz | gfz 2952 | 11 10 29 | 7 5 24 | igr | igr 2952 | 9 16 21 | 7 6 20 | igs | igs 2970 | 7 9 20 | 7 6 19 | jpl | jpl 2957 | 21 23 109 | 7 6 21 | mit | mit 2976 | 13 12 31 | 9 7 21 | Table 5.1503.6 GPS week: 1503 Day: 6 MJD: 54771.0 CENT| CLK EPO | BRUS | WILL | ----+----------+-------------------+-------------------+ cod | cod 3069 | 8 5 20 | 7 6 15 | emr | emr 2964 | 12 8 25 | 8 9 20 | esa | esa 2976 | 9 6 27 | 9 8 21 | gfz | gfz 2952 | 9 6 19 | 9 7 21 | igr | igr 2971 | 11 8 22 | 7 8 19 | igs | igs 2970 | 13 9 26 | 8 8 19 | jpl | jpl 2964 | 13 10 25 | 9 10 21 | mit | mit 2976 | 12 11 26 | 12 12 20 | 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 6.1503 GPS week: 1503 MJD: 54765.500-54771.500 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 | -24 7 25 -10 -7 | 16 23 | 19 21 65 109 6 | 1 emr uuuuu | -98 17 -176 -94 -6 | 52 56 | 24 35 163 173 4 | 3 esa uuuuu | 13 -40 82 62 -7 | 18 25 | 25 18 52 41 8 | 1 gfz uuuuu | -14 -41 -1 16 -2 | 16 24 | 21 20 81 78 6 | 3 grg xxxxx | -7 -4 39 -29 -1 | -3 16 | 43 40 129 91 14 | 5 igr xxxxx | -19 23 33 22 -1 | 0 17 | 19 26 56 33 4 | 4 irf xxxxx | -1 -4 -42 30 0 | 3 18 | 11 12 23 25 4 | 5 jpl uuuuu | -3 2 81 1 7 | 20 26 | 42 36 126 153 12 | 5 mit uuuuu | 7 -8 -193 78 3 | 19 27 | 28 32 68 40 5 | 6 ngs uuuuu | 40 32 102 -77 1 | 2 13 | 46 63 118 80 6 | 1 sio uuuuu | 119 74 36 3 10 | 42 46 | 15 16 54 131 3 | 8 Table 7.1503.0 GPS week: 1503 Day: 0 MJD: 54765.500 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 | 3 41 24 91 -3 | 14 23 emr uuuuu | -122 -14 10 -299 2 | 47 52 esa uuuuu | 36 -54 129 79 8 | 15 23 gfz uuuuu | 16 -11 -128 104 7 | 12 23 grg xxxxx | -63 4 -103 -128 -23 | -5 23 igr xxxxx | 6 29 136 4 6 | -6 21 irf xxxxx | 17 7 -49 28 4 | -4 22 jpl uuuuu | -21 1 202 -127 -12 | 15 23 mit uuuuu | 44 35 -233 43 4 | 10 25 ngs uuuuu | -34 -51 -18 -20 -3 | 1 13 sio uuuuu | 139 79 46 81 11 | 31 38 Table 7.1503.1 GPS week: 1503 Day: 1 MJD: 54766.500 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 | -12 1 -80 2 -17 | 15 24 emr uuuuu | -105 7 9 -269 -8 | 49 55 esa uuuuu | 20 -8 38 113 -12 | 18 26 gfz uuuuu | -32 -18 -30 67 -8 | 14 25 grg xxxxx | -38 -51 124 5 5 | -8 22 igr xxxxx | -6 74 -8 17 0 | -3 22 irf xxxxx | 6 12 -89 80 -3 | -2 22 jpl uuuuu | 25 33 135 65 3 | 15 23 mit uuuuu | 30 28 -318 97 0 | 13 27 ngs uuuuu | 0 -52 248 -136 9 | 1 13 sio uuuuu | 117 63 -30 79 11 | 35 41 Table 7.1503.2 GPS week: 1503 Day: 2 MJD: 54767.500 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 | -44 13 -40 -124 -12 | 15 24 emr uuuuu | -95 23 -294 104 -8 | 51 56 esa uuuuu | 46 -45 131 102 -12 | 17 26 gfz uuuuu | 12 -56 65 -100 -6 | 14 25 grg xxxxx | 55 4 123 91 12 | -7 21 igr xxxxx | -4 32 24 3 0 | -2 21 irf xxxxx | -11 -22 -21 9 0 | -1 21 jpl uuuuu | -43 -19 150 250 9 | 15 23 mit uuuuu | -28 -50 -177 74 9 | 15 27 ngs uuuuu | 54 101 70 -143 3 | 1 13 sio uuuuu | 103 50 30 -150 8 | 37 43 Table 7.1503.3 GPS week: 1503 Day: 3 MJD: 54768.500 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 | -41 15 112 -32 -4 | 17 23 emr uuuuu | -102 79 -431 77 -9 | 55 57 esa uuuuu | -7 -33 152 4 -9 | 18 26 gfz uuuuu | -25 -49 6 52 -1 | 17 23 grg xxxxx | 20 45 -106 -116 -10 | -4 18 igr xxxxx | -42 3 -38 3 -1 | 2 14 irf xxxxx | -1 -16 -34 8 0 | 4 15 jpl uuuuu | -22 -21 -5 -74 19 | 19 23 mit uuuuu | -19 -44 -135 47 3 | 20 25 ngs uuuuu | 111 49 43 -69 -3 | 2 13 sio uuuuu | 140 71 116 69 14 | 42 45 Table 7.1503.4 GPS week: 1503 Day: 4 MJD: 54769.500 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 | -39 -19 51 -3 -8 | 18 24 emr uuuuu | -52 47 -265 22 -9 | 56 59 esa uuuuu | 24 -30 35 66 -5 | 19 26 gfz uuuuu | -28 -38 31 -48 4 | 19 24 grg xxxxx | -22 -57 193 -62 5 | 1 10 igr xxxxx | -13 5 33 95 -8 | 4 15 irf xxxxx | 3 0 -36 10 4 | 7 16 jpl uuuuu | -52 -15 143 2 24 | 24 28 mit uuuuu | 27 -10 -210 71 10 | 24 28 ngs uuuuu | 45 38 219 -133 -6 | 3 14 sio uuuuu | 115 91 -31 -22 13 | 48 50 Table 7.1503.5 GPS week: 1503 Day: 5 MJD: 54770.500 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 15 46 -157 -3 | 15 22 emr uuuuu | -88 -13 -139 -48 -4 | 53 55 esa uuuuu | -23 -59 43 56 -16 | 17 25 gfz uuuuu | -12 -66 112 -42 -9 | 18 24 grg xxxxx | 31 39 -80 86 13 | 1 10 igr xxxxx | -36 3 20 6 -5 | 2 15 irf xxxxx | -12 -7 -24 38 -7 | 6 16 jpl uuuuu | 44 -33 113 97 1 | 24 28 mit uuuuu | -18 -14 -121 56 -3 | 24 27 ngs uuuuu | 42 100 -43 74 9 | 0 13 sio uuuuu | 112 95 42 -194 4 | 48 50 Table 7.1503.6 GPS week: 1503 Day: 6 MJD: 54771.500 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 | -33 -17 63 150 -2 | 17 23 emr uuuuu | -123 -7 -120 -246 -8 | 55 56 esa uuuuu | -5 -52 50 15 -2 | 19 24 gfz uuuuu | -32 -46 -63 81 -1 | 20 24 grg xxxxx | -35 -15 125 -80 -11 | 3 11 igr xxxxx | -36 12 65 27 -2 | 4 13 irf xxxxx | -10 -4 -39 36 -1 | 8 14 jpl uuuuu | 50 70 -166 -205 3 | 27 30 mit uuuuu | 10 2 -157 160 1 | 27 28 ngs uuuuu | 61 41 195 -110 1 | 3 12 sio uuuuu | 104 71 80 157 9 | 52 53