Date: Thu, 10 Jul 2008 12:23:37 +0000 From: Jim Ray Subject: [IGSREPORT-16417] Wk 1485 IGS Final Orbits To: igsreport@igscb.jpl.nasa.gov Message-id: <4875ff49.Ah9651gUT7tm3Zn+%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 10 Jul 05:23:49 PDT 2008 Message Number 16417 ****************************************************************************** Author: AC Coordinator / NOAA NGS sum-file Version 2.0 Final IGS Orbit Combination - Week 1485 (Jun 22, 2008 - Jun 28, 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: igs1485[0-6].sp3 IGS GPS ephemeris files in SP3 format. igs1485[0-6].clk IGS GPS satellite and station clocks in SP3 format. igs1485[0-6].cls IGS GPS clock combination summary report. igs14857.erp Earth Rotation Parameters (ERP) and their rates as well as Universal Time (UT1-UTC) and Length Of Day (LOD) associated with IGS ephemerides. igs14857.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 | ALL | 32 0 | COD | 10 BOR1 SYDN 0 | ESA | 10 NRIL 0 | GFZ | 7 8 18 20 29 1 | COD | 10 AREQ CHUR HYDE NRC1 PERT 1 | EMR | 32 1 | ESA | 10 NRC1 1 | GFZ | 7 8 18 20 29 32 BJFS DAEJ HYDE LHAZ 1 | JPL | AREQ 1 | MIT | SYDN 2 | COD | 10 BOR1 CEDU NRIL 2 | EMR | WTZR 2 | ESA | 10 2 | GFZ | 7 29 32 NLIB 2 | JPL | 32 2 | MIT | 32 DARW NLIB SYDN WTZR 3 | COD | 10 CEDU NRMD 3 | ESA | 10 32 KOUR MAS1 SSIA 3 | GFZ | 7 20 29 32 KOUR MAS1 3 | JPL | 32 3 | MIT | 32 DARW 4 | COD | CEDU TOW2 4 | EMR | PERT 4 | ESA | 10 4 | GFZ | 7 24 29 32 FAA1 MAS1 VESL 4 | JPL | 32 4 | MIT | 10 19 32 NISU 5 | COD | 22 NRIL 5 | EMR | SPT0 5 | ESA | 32 ALIC 5 | GFZ | 7 21 22 29 BJFS DAEJ VESL 5 | JPL | 10 22 5 | MIT | 32 DAEJ KOUR SPT0 SYDN TSKB 6 | COD | ALGO YELL 6 | EMR | SUWN YELL 6 | ESA | 32 PERT 6 | GFZ | 7 22 29 32 6 | JPL | 10 6 | MIT | 32 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 ----+------------+---------- G08 | 2008_06_26 | 2008060 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 | .6 .2 .2 -16 -15 -9 -.14 EMR | 2.5 -1.7 -3.3 70 -63 39 .01 ESA | 1.2 -3.1 10.6 5 12 39 -.05 GFZ | .9 .1 1.0 -7 -26 -9 -.32 GRG | 7.5 -1.6 1.1 -49 -11 -3 -.25 JPL | -3.1 -5.6 .0 -26 -8 -8 -.09 MIT | 4.3 -5.8 9.5 -13 -5 -9 -.05 NGS | 7.1 -.5 3.5 -6 -87 16 .07 SIO | -2.5 -4.5 -.6 -80 38 4 .19 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 1.1485.a). It also displays the computed satellite position sigmas for the combined orbits (table 1.1485.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 2.1485.[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 3.1485.[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 5.1485.0-6). 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 1485 summary. (Jun 22, 2008 - Jun 28, 2008) Table 1.1485.a GPS week: 1485 MJD: 54639.000-54645.000 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 205| 1 0 1 28 -34 -17 -.15 12 12 | -419 -300 18 87 | 0 0 1 4 11 22 .03 | 213 310 emr 70| 0 -1 0 -144 126 -6 .26 16 16 | 884 -956 19 130 | 1 2 1 13 12 22 .02 | 2151 1031 esa 120| 0 -1 4 -45 -88 -5 .31 9 9 | -10100 -138 18 105 | 0 1 1 12 10 22 .06 | 1325 1750 gfz 184| 0 0 -2 2 -8 87 -.13 13 13 | -12 89 22 142 | 1 0 1 24 17 87 .04 | 331 712 grg 78| 3 2 -8 48 -11 13 .99 37 34 | -421 -341 100 8042 | 1 1 3 13 31 12 .03 | 216 312 igr n/a| 0 1 0 0 -33 -38 .05 6 5 | -12266 -1038 21 81 | 0 0 0 7 9 15 .03 | 2538 1151 jpl 125| 0 1 -5 51 -30 29 .47 16 16 | 3291 -1081 18 90 | 1 2 1 15 13 13 .03 | 2470 1087 mit 265| 0 -1 1 11 -44 -5 -.29 11 10 | -31 -265 18 101 | 0 0 1 14 25 18 .04 | 278 583 ngs 228| 0 1 -2 23 159 -62 -.28 11 9 | -384 -312 2091 3852 | 1 0 0 28 28 22 .04 | 184 314 sio 107| -2 1 1 147 -119 -3 -.03 22 20 | --- --- --- --- | 0 1 1 20 23 14 .07 | --- --- Table 1.1485.b GPS week : 1485 MJD: 54639.000-54645.000 Satellite position sigmas for the combined orbits (coded in the IGS SP3 orbit files). "E" flags eclipsing satellites. Units: mm. Day of GPS week PRN | 0 1 2 3 4 5 6 | Remarks ------+------------------------------------+------------------------------------------ 2 | 6 6 6 6 6 6 6 | 3 | 4 3 3 4 3 3 6 | 4 | 4 4 4 4 4 4 4 | 5 | 4 5 4 5 6 5 4 | 6 | 3 3 3 4 4 3 4 | 7 | 5 4 4 5 5 5 6 | 8 | 6 6 6 6 0 5 5 | 9 | 5 5 5 5 5 5 5 | 10 | 5 5 5 6 7 8 7 | 11 | 6 6 5 5 5 5 5 | 12 | 6 6 6 6 6 6 6 | 13 | 5 5 5 5 6 6 6 | 14 | 5 6 5 5 5 5 5 | 15 | 6 6 6 6 5 5 6 | 16 | 6 5 5 5 5 5 5 | 17 | 6 5 5 6 6 6 6 | 18 | 5 5 5 5 5 4 4 | 19 | 4 4 4 4 4 4 4 | 20 | 6 6 6 6 5 5 5 | 21 | 6 6 6 6 6 6 7 | 22 | 4 5 5 5 5 5 5 | 23 | 5 5 5 5 6 6 6 | 24 | 4 4 4 4 3 4 4 | 25 | 5 5 5 5 5 5 5 | 26 | 5 5 5 5 5 5 5 | 27 | 5 5 5 5 4 5 4 | 28 | 5 6 5 5 6 6 6 | 29 | 5 5 5 7 5 5 5 | 30 | 4 4 4 4 4 5 5 | 31 | 5 5 5 5 5 5 5 | 32 | 9 7 6 6 6 6 6 | 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 2.1485.0 GPS week: 1485 Day: 0 MJD: 54639.000 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 205| 1 0 -1 25 -40 -23 -.19 12 12 | -557 -368 14 68 | -8 42 | emr 70| 0 -1 1 -148 137 12 .27 18 18 | 3755 -1417 18 116 | -28 -78 | esa 120| 0 0 3 -57 -90 27 .27 10 10 | -10054 -545 18 105 | -6 38 | gfz 184| 1 2 -1 42 -26 -29 -.12 13 13 | 176 -75 23 170 | -3 23 | grg 78| 2 0 -4 30 -38 5 1.01 37 31 | -567 -418 95 207 | 32 17 | igr n/a| 0 1 0 1 -35 -21 .08 5 5 | -8600 -1576 21 77 | -37 10 | jpl 125| 0 0 -4 55 -21 47 .45 15 15 | 6542 -1292 19 91 | -43 -17 | mit 265| 0 -3 2 14 -20 17 -.26 12 11 | 102 -248 16 87 | 20 -28 | ngs 228| -1 0 -2 9 150 -66 -.34 11 9 | -464 -529 2171 3854 | 18 -54 | sio 107| -2 0 1 138 -140 7 .08 23 19 | --- --- --- --- | -10 95 | Table 2.1485.1 GPS week: 1485 Day: 1 MJD: 54640.000 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 205| 2 0 1 30 -28 -29 -.16 14 14 | -290 -450 16 87 | 9 2 | emr 70| 0 -2 0 -137 109 -1 .21 16 16 | 2442 -1222 17 106 | -27 -32 | esa 120| 1 0 2 -32 -78 -18 .24 8 8 | -7942 -2842 19 116 | 9 34 | gfz 184| 1 0 -4 -8 -17 114 -.19 13 13 | -237 401 22 126 | 37 27 | grg 78| 5 2 -9 46 38 9 .96 40 35 | -299 -477 109 231 | 25 -5 | igr n/a| 1 0 0 -10 -25 -65 .06 5 5 | -9981 -1773 22 79 | 0 24 | jpl 125| -1 0 -2 70 -10 29 .44 14 14 | 5460 -1437 18 97 | -15 -36 | mit 265| 0 -1 2 17 -78 -8 -.26 11 9 | -80 178 20 151 | 11 -3 | ngs 228| -1 1 -2 -1 178 -76 -.25 10 9 | -311 -450 2015 4249 | 23 -56 | sio 107| -2 1 1 156 -117 -14 .03 22 21 | --- --- --- --- | -48 57 | Table 2.1485.2 GPS week: 1485 Day: 2 MJD: 54641.000 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 205| 1 0 0 25 -45 -8 -.15 13 12 | -599 340 20 89 | -3 23 | emr 70| -1 1 0 -137 118 -17 .24 15 15 | 1095 549 19 127 | -12 -87 | esa 120| 0 -1 3 -26 -110 12 .28 10 9 | -11341 903 18 102 | 20 5 | gfz 184| 0 1 -1 -9 17 98 -.15 13 13 | -249 251 23 128 | 32 12 | grg 78| 2 3 -6 46 -29 20 .95 37 34 | -604 311 103 219 | -10 40 | igr n/a| 0 0 1 -5 -39 -34 .06 5 4 | -11948 -16 20 86 | 11 -1 | jpl 125| -1 0 -4 54 -42 28 .46 15 15 | 3685 264 17 75 | -35 -9 | mit 265| 0 0 1 -4 -39 1 -.24 12 11 | -434 409 17 89 | 12 -29 | ngs 228| 0 0 -2 14 143 -80 -.27 9 8 | -592 308 2279 4179 | 71 44 | sio 107| -2 1 1 152 -119 -3 -.02 20 19 | --- --- --- --- | -61 87 | Table 2.1485.3 GPS week: 1485 Day: 3 MJD: 54642.000 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 205| 0 0 2 26 -35 -1 -.18 13 12 | -673 -210 19 83 | -9 10 | emr 70| -1 -3 1 -132 120 11 .26 15 15 | 2052 -2351 20 103 | -49 -56 | esa 120| 1 -1 3 -40 -80 -15 .28 9 9 | -9782 -98 19 88 | 33 16 | gfz 184| 2 0 -3 30 3 49 -.16 14 14 | 157 -420 21 123 | 6 17 | grg 78| 2 4 -13 68 -37 0 1.00 36 34 | -666 -267 92 207 | 44 -32 | igr n/a| 0 1 -1 2 -18 -48 .02 6 5 | -11546 -2606 22 75 | -35 3 | jpl 125| 0 1 -4 20 -49 22 .52 16 16 | 4369 -2742 19 92 | -6 -15 | mit 265| 0 -1 0 39 -65 6 -.30 11 11 | 296 -929 15 63 | -12 -11 | ngs 228| 0 1 -3 -12 184 -77 -.25 10 10 | -482 -292 2101 3854 | 97 -14 | sio 107| -3 2 0 178 -148 22 -.06 22 20 | --- --- --- --- | -64 90 | Table 2.1485.4 GPS week: 1485 Day: 4 MJD: 54643.000 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 205| 1 0 1 36 -36 -50 -.15 11 11 | -493 -500 19 97 | -17 1 | emr 70| 1 0 -1 -172 123 -50 .27 15 15 | 670 -1833 21 150 | 32 -60 | esa 120| 0 -1 5 -53 -81 -41 .36 10 10 | -12098 2911 19 111 | 36 13 | gfz 184| 0 0 -1 -28 -18 255 -.14 14 14 | -136 468 27 174 | 29 31 | grg 78| 3 2 -10 62 -18 15 1.01 37 36 | -502 -526 110 230 | -33 -25 | igr n/a| 0 1 0 11 -39 -41 .01 6 6 | -13197 -1697 23 92 | 37 20 | jpl 125| 1 -1 -5 64 -32 6 .51 16 16 | 2653 -1968 18 93 | -14 -1 | mit 265| 0 0 0 0 -62 -36 -.32 12 11 | -161 145 23 123 | 23 5 | ngs 228| 0 1 -2 65 177 -37 -.29 11 8 | -545 -196 1777 3440 | -93 -158 | sio 107| -1 1 3 111 -117 -16 -.14 22 20 | --- --- --- --- | -47 66 | Table 2.1485.5 GPS week: 1485 Day: 5 MJD: 54644.000 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 205| 1 0 2 24 -44 -28 -.10 11 10 | -208 -311 17 85 | 7 38 | emr 70| 0 0 1 -149 147 5 .28 18 18 | -2023 -257 20 155 | -47 -91 | esa 120| 0 -3 3 -48 -92 -3 .35 9 9 | -9775 -638 18 107 | -19 15 | gfz 184| 0 0 0 -6 3 49 -.09 13 13 | -373 1114 24 156 | 20 34 | grg 78| 5 3 -8 36 -22 37 .99 37 35 | -203 -364 100 216 | 8 71 | igr n/a| 0 0 -1 -4 -47 -38 .06 6 6 | -15574 -47 22 89 | 11 31 | jpl 125| -1 5 -7 46 -19 26 .43 19 19 | -33 -233 20 97 | -27 -36 | mit 265| 0 0 0 8 -6 4 -.31 11 10 | -245 -259 17 85 | 26 3 | ngs 228| -1 0 -3 41 105 -24 -.26 11 8 | -192 -360 2133 3718 | -64 59 | sio 107| -1 2 0 143 -72 -2 -.03 21 21 | --- --- --- --- | -9 33 | Table 2.1485.6 GPS week: 1485 Day: 6 MJD: 54645.000 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 205| 0 0 0 29 -11 18 -.12 13 12 | -116 -604 22 101 | -8 -11 | emr 70| 2 -3 1 -135 126 -2 .27 17 17 | -1798 -161 24 157 | -36 -40 | esa 120| 0 -3 6 -59 -85 1 .41 9 9 | -9713 -663 18 112 | 29 15 | gfz 184| 0 0 0 0 -24 70 -.09 13 13 | 572 -1112 20 118 | 12 16 | grg 78| 4 0 -5 49 25 7 1.02 36 33 | -109 -649 94 54988 | -6 -28 | igr n/a| 0 1 0 3 -30 -18 .09 6 5 | -15019 448 23 70 | -18 17 | jpl 125| -1 3 -8 46 -35 45 .46 16 16 | 365 -162 19 91 | -34 -16 | mit 265| -1 0 0 4 -36 -23 -.35 11 10 | 305 -1151 20 110 | 25 -5 | ngs 228| 0 2 0 48 180 -72 -.33 11 9 | -106 -667 2164 3674 | 58 28 | sio 107| -2 0 0 154 -118 -19 -.09 22 21 | --- --- --- --- | -66 35 | 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 3.1485.0 GPS week: 1485 Day: 0 MJD: 54639.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 11 19 13 16 52 7 19 13 10 31 6 | 25 30 21 29 37 23 29 23 24 27 21 3 | 10 8 8 9 20 3 7 8 9 22 3 | 15 20 20 19 28 18 18 15 18 9 15 4 | 6 11 9 6 47 4 7 7 11 14 3 | 21 28 24 24 19 23 24 27 25 30 23 5 | 11 11 7 15 24 4 11 14 9 14 4 | 29 37 35 37 46 34 41 32 29 41 33 6 | 6 8 7 7 21 4 7 8 9 19 3 | 17 19 19 19 21 19 16 21 21 18 17 7 | 16 18 11 12 68 7 13 13 9 19 5 | 28 34 26 28 73 24 29 17 22 23 22 8E | 11 26 10 16 32 5 16 14 10 15 5 | 22 36 23 31 35 22 30 24 22 26 23 9 | 9 14 11 15 30 5 16 16 10 20 5 | 19 27 22 28 25 20 29 21 20 28 20 10E | 12 15 9 10 58 4 12 10 14 16 4 | 28 32 23 30 23 26 26 25 33 21 25 11 | 10 19 11 18 55 6 14 16 10 18 5 | 33 44 38 34 47 33 44 36 29 31 33 12 | 21 18 10 14 25 6 17 17 8 26 6 | 23 35 23 29 38 24 33 21 25 23 23 13 | 8 16 12 14 48 5 20 11 8 15 5 | 14 28 21 25 50 19 30 16 12 13 16 14 | 10 15 11 16 33 4 16 10 11 20 5 | 19 25 23 22 34 18 24 18 19 19 17 15 | 15 17 11 16 26 5 17 13 14 24 5 | 17 29 21 19 29 18 25 20 21 23 17 16 | 11 17 14 16 32 8 17 12 11 22 5 | 19 32 17 27 29 22 30 17 21 27 20 17 | 11 14 11 10 60 8 11 8 13 47 5 | 26 29 29 30 62 23 21 29 29 48 25 18E | 13 15 7 8 35 5 20 13 6 18 4 | 21 23 18 19 41 18 26 19 20 27 18 19 | 9 9 8 5 32 2 11 7 9 19 3 | 23 27 26 21 29 22 20 23 24 26 22 20E | 10 14 13 10 35 5 16 23 9 28 5 | 21 28 22 26 26 21 26 32 24 38 23 21 | 13 18 10 16 37 7 20 10 10 32 5 | 20 33 21 33 45 26 32 17 23 28 22 22E | 9 16 8 10 24 5 16 13 8 11 4 | 11 22 15 17 24 13 21 13 15 16 12 23 | 9 18 13 13 28 5 18 10 9 22 5 | 14 31 20 23 45 18 28 14 15 15 16 24 | 9 10 7 7 24 4 10 13 11 14 3 | 24 26 28 21 28 26 26 25 27 22 24 25 | 13 14 8 12 22 3 14 12 9 20 4 | 12 26 17 19 29 16 28 16 16 25 15 26 | 7 9 7 10 26 4 8 11 12 34 4 | 13 17 15 19 29 14 16 18 24 32 14 27 | 17 17 8 12 29 3 13 11 7 27 5 | 10 25 15 21 30 14 25 16 11 30 13 28 | 10 16 13 15 33 5 17 10 13 18 5 | 24 29 20 34 49 24 34 23 25 23 24 29 | 16 11 5 9 30 7 11 11 11 25 4 | 28 29 30 20 30 28 23 27 27 33 26 30 | 12 11 7 13 26 4 12 9 12 15 4 | 15 23 17 21 33 17 24 15 13 20 15 31 | 10 14 10 12 38 3 15 7 14 13 4 | 11 21 12 18 39 12 22 10 13 14 11 32E | 16 57 8 19 43 7 18 19 15 32 9 | 58 78 62 61 69 61 64 61 58 79 59 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 18 10 13 37 5 15 12 11 23 |T 21 29 23 25 36 22 27 22 22 26 21 WRMS | 12 18 10 13 31 5 15 11 9 19 |NE 19 28 22 24 36 21 26 20 21 25 20 MEDI | 11 15 10 12 32 5 15 11 10 20 |MD 21 28 21 24 33 22 26 21 22 26 21 Table 3.1485.1 GPS week: 1485 Day: 1 MJD: 54640.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 13 21 10 17 37 8 17 13 9 29 5 | 21 30 14 25 27 20 22 19 21 25 17 3 | 8 10 7 8 30 4 6 7 8 17 3 | 12 16 14 14 22 13 15 11 15 11 12 4 | 11 15 6 7 31 4 9 9 9 15 3 | 14 23 14 13 16 14 17 19 19 23 14 5 | 13 11 6 15 24 5 11 15 7 17 4 | 31 41 38 35 44 34 41 31 29 41 34 6 | 8 10 7 9 25 4 6 8 9 16 3 | 17 17 11 12 14 14 11 16 14 15 12 7 | 13 15 8 13 51 6 10 7 8 14 4 | 17 21 16 18 51 15 21 12 11 15 13 8E | 22 24 10 14 102 8 17 14 11 18 6 | 54 55 50 60 118 58 33 51 58 52 55 9 | 15 16 7 15 24 7 19 13 9 15 5 | 19 29 21 30 31 20 28 21 23 26 22 10E | 15 14 9 13 52 5 16 12 15 14 5 | 21 22 18 18 21 18 20 19 23 16 16 11 | 30 14 7 18 55 8 14 11 9 18 5 | 38 32 28 29 45 26 38 29 24 21 26 12 | 21 15 11 15 28 6 18 17 8 26 6 | 19 31 18 28 32 18 30 19 20 22 19 13 | 8 15 12 17 50 6 14 9 8 16 4 | 13 28 18 24 52 18 29 14 14 10 15 14 | 13 20 8 18 39 4 16 8 15 18 5 | 18 32 19 28 33 22 27 17 23 22 20 15 | 15 17 9 16 32 5 19 12 11 20 5 | 17 27 15 21 35 16 24 18 16 18 15 16 | 13 16 9 16 29 5 14 10 11 23 5 | 20 30 18 25 32 22 25 19 26 27 20 17 | 11 14 6 9 54 5 9 7 8 45 5 | 13 21 15 14 40 14 17 17 19 44 15 18E | 10 14 7 8 29 6 22 12 10 19 4 | 16 23 20 22 30 18 24 19 23 30 19 19 | 7 10 6 7 41 4 9 6 12 19 3 | 16 18 18 18 21 15 18 14 18 17 15 20E | 12 20 10 11 35 8 16 19 9 20 5 | 19 32 23 22 32 23 22 21 23 23 20 21 | 16 18 11 18 32 6 21 9 11 31 6 | 14 30 15 25 36 18 29 13 14 22 14 22E | 9 12 8 9 27 5 20 11 11 13 4 | 10 17 10 15 27 12 21 12 17 17 11 23 | 11 19 12 15 29 6 13 8 9 23 5 | 18 34 20 26 41 20 27 18 17 21 18 24 | 10 11 6 8 29 4 10 11 8 13 3 | 19 24 21 21 26 20 22 20 24 20 20 25 | 14 19 9 12 25 4 11 11 8 19 4 | 15 28 20 24 31 17 27 17 18 24 18 26 | 15 10 7 11 22 4 11 8 12 34 5 | 18 14 13 16 26 12 13 14 20 31 12 27 | 16 17 9 11 31 5 13 11 10 21 4 | 11 26 16 19 32 14 24 12 15 18 14 28 | 16 17 11 18 34 6 15 10 13 19 5 | 24 31 27 30 44 24 30 19 22 21 23 29 | 17 14 5 10 43 5 11 12 10 25 4 | 29 27 26 23 33 23 19 21 26 29 24 30 | 12 13 6 11 31 5 11 11 8 17 4 | 13 25 18 22 33 16 23 15 15 21 17 31 | 14 20 8 14 28 5 14 6 10 12 4 | 13 33 18 24 38 20 24 15 15 18 18 32E | 16 24 11 15 51 4 18 19 16 41 7 | 88 92 91 92 100 91 94 91 92 108 91 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 14 16 8 13 40 5 14 11 10 22 |T 21 29 22 25 37 22 26 21 23 26 21 WRMS | 14 16 8 13 35 5 14 9 9 21 |NE 18 26 18 22 33 18 24 17 19 22 17 MEDI | 13 15 8 13 31 5 14 11 9 19 |MD 18 28 18 23 32 18 24 18 20 22 18 Table 3.1485.2 GPS week: 1485 Day: 2 MJD: 54641.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 11 17 11 16 50 6 17 11 9 28 5 | 24 27 16 27 34 20 27 22 23 28 19 3 | 5 8 5 11 27 3 7 8 8 16 3 | 12 17 16 16 21 15 13 13 21 15 13 4 | 9 11 8 6 32 3 10 10 8 16 3 | 18 23 15 18 25 19 21 23 22 24 18 5 | 10 12 9 15 29 4 10 12 10 14 4 | 49 52 55 52 63 51 57 50 48 53 51 6 | 6 8 6 9 26 4 9 8 9 15 3 | 11 11 14 12 19 12 12 14 19 13 11 7 | 16 13 10 14 49 5 13 6 6 13 4 | 23 23 19 23 47 18 24 16 17 20 16 X8 | 18 21 8 12 42 6 --- 14 8 21 5 | 37 35 45 45 51 42 --- 46 37 28 41 9 | 13 17 7 13 22 6 17 15 10 15 5 | 16 27 17 26 23 20 26 25 21 22 18 10E | 15 14 10 11 59 3 17 11 17 15 5 | 15 27 17 19 32 17 22 20 25 16 17 11 | 17 14 9 20 49 7 15 10 9 17 5 | 28 32 29 29 37 24 32 26 27 27 25 12 | 19 17 14 14 35 6 19 17 9 24 6 | 20 28 17 24 33 16 28 18 18 21 16 13 | 8 15 13 16 46 5 16 10 10 13 4 | 13 28 23 22 49 18 29 15 16 12 15 14 | 10 15 11 17 37 5 17 10 10 15 5 | 15 26 19 22 35 16 24 14 17 18 14 15 | 17 21 11 14 36 7 16 14 9 20 5 | 19 32 15 22 34 16 23 17 19 16 15 16 | 10 17 10 15 33 4 18 12 9 21 5 | 15 27 16 27 34 18 28 15 24 22 17 17 | 12 13 10 13 53 6 11 7 6 41 5 | 22 24 24 30 48 20 20 23 22 41 21 18E | 9 12 9 9 28 3 21 12 9 17 4 | 15 17 16 15 30 16 18 16 20 20 13 19 | 11 7 7 6 41 5 12 7 8 18 3 | 21 21 18 19 28 20 15 20 28 23 19 20E | 13 15 11 12 30 8 18 23 9 17 5 | 19 23 18 24 19 17 28 31 23 31 20 21 | 11 17 10 18 45 6 20 10 9 27 5 | 18 29 20 27 43 22 32 16 21 18 17 22E | 9 18 9 10 21 4 19 16 12 12 5 | 12 23 14 15 29 13 21 14 18 15 11 23 | 11 16 13 15 34 6 13 10 10 20 5 | 18 28 22 22 37 20 26 18 16 21 16 24 | 10 12 8 8 27 4 9 8 8 12 3 | 19 25 20 21 20 22 19 22 24 20 20 25 | 10 17 10 11 18 3 13 12 6 19 4 | 13 25 20 18 28 17 27 19 15 24 15 26 | 13 12 7 9 19 3 10 10 9 35 5 | 14 18 12 17 25 12 16 15 23 32 13 27 | 16 19 9 15 26 4 13 12 10 20 5 | 12 28 21 23 33 16 26 17 17 23 16 28 | 13 16 10 15 29 6 18 12 10 17 5 | 20 31 19 24 46 20 31 15 20 16 19 29 | 19 9 7 10 29 5 10 12 7 24 4 | 16 22 18 17 22 16 18 18 18 23 17 30 | 10 14 8 13 24 4 11 11 10 15 4 | 14 22 15 20 29 15 21 13 16 19 13 31 | 12 16 11 12 33 5 17 7 8 13 4 | 10 23 14 17 42 14 24 10 17 12 11 32E | 16 23 10 17 68 7 15 15 10 26 6 | 75 82 78 77 63 76 80 71 70 81 75 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 12 15 10 13 37 5 15 12 9 20 |T 20 27 22 24 34 21 26 21 23 24 20 WRMS | 12 15 9 13 34 4 15 11 8 18 |NE 18 25 19 23 34 19 24 18 21 22 17 MEDI | 11 15 10 13 33 5 15 11 9 17 |MD 18 26 18 22 33 18 24 18 21 21 17 Table 3.1485.3 GPS week: 1485 Day: 3 MJD: 54642.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 15 19 11 17 41 7 19 12 11 29 6 | 23 34 21 31 33 25 29 25 25 31 23 3 | 6 10 6 10 37 4 11 9 12 20 4 | 20 29 25 27 31 23 26 20 27 21 23 4 | 9 8 8 7 32 3 11 10 9 21 3 | 22 29 21 23 20 23 26 26 23 37 23 5 | 19 12 7 15 25 6 15 11 7 12 4 | 30 36 33 39 39 34 39 31 38 38 33 6 | 7 10 6 9 27 4 11 8 15 18 4 | 18 22 18 18 23 18 19 16 26 16 18 7 | 17 14 11 14 38 5 12 9 13 15 5 | 20 28 17 25 48 19 24 17 20 20 18 X8 | 10 --- 6 15 --- 6 --- 13 9 --- 5 | 33 --- 34 41 --- 33 --- 32 36 --- 34 9 | 16 14 9 15 23 6 17 12 9 13 5 | 24 33 33 38 31 30 32 28 34 27 30 10E | 14 18 11 13 55 7 15 12 20 27 6 | 20 32 26 25 29 24 29 24 32 28 23 11 | 10 13 8 18 48 7 18 9 10 14 4 | 35 38 33 36 42 30 36 28 28 27 30 12 | 20 18 10 14 30 6 17 15 10 24 6 | 22 35 28 33 36 26 33 26 30 27 26 13 | 9 16 12 14 45 6 18 12 8 15 5 | 17 32 22 25 51 21 30 17 21 17 19 14 | 11 17 10 18 42 7 21 12 9 13 5 | 17 31 24 27 37 22 28 20 24 23 21 15 | 17 18 10 19 25 7 17 14 10 23 5 | 15 33 22 26 32 23 26 23 27 23 21 16 | 11 19 11 14 43 7 17 10 12 23 5 | 19 37 19 32 33 27 31 22 31 28 25 17 | 12 13 12 12 32 7 13 10 10 43 5 | 21 29 18 25 31 18 20 20 21 39 19 18E | 6 11 7 10 29 5 21 11 10 17 4 | 19 23 22 22 26 22 25 17 27 29 20 19 | 7 10 8 7 40 5 14 10 11 20 4 | 25 31 26 29 27 24 26 23 22 24 24 X20E | 19 18 9 13 39 8 --- 14 10 19 5 | 23 32 22 22 39 22 --- 22 24 23 21 21 | 12 15 10 18 38 7 19 12 10 27 5 | 18 32 15 29 41 22 31 14 23 25 19 22E | 10 16 10 9 12 6 19 16 8 10 4 | 15 23 15 20 18 14 22 14 19 17 14 23 | 10 16 11 14 30 6 18 13 9 23 5 | 19 32 19 26 42 20 29 19 20 19 19 24 | 11 9 6 7 28 4 12 7 10 14 3 | 28 31 31 32 35 33 35 29 37 29 31 25 | 10 18 10 13 26 5 11 12 10 21 4 | 20 32 22 29 32 22 28 20 24 24 22 26 | 15 11 6 13 19 5 12 10 10 36 5 | 14 22 18 22 25 17 19 17 21 33 15 27 | 15 17 9 12 27 5 12 13 9 20 5 | 13 30 19 24 30 18 26 12 17 15 16 28 | 10 17 10 19 31 7 16 14 8 18 5 | 18 31 22 29 45 23 30 18 20 20 21 X29 | 34 12 8 9 31 8 --- 12 9 24 6 | 41 33 31 30 28 26 --- 28 31 30 29 30 | 12 12 6 13 28 5 14 9 8 13 4 | 19 28 25 28 37 22 26 22 28 24 23 31 | 15 17 10 14 27 7 19 10 8 14 5 | 18 33 16 26 38 21 31 17 22 20 20 32E | 12 22 11 19 79 6 17 11 10 26 5 | 88 96 89 90 97 88 92 85 87 97 89 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 13 15 9 14 36 6 16 11 10 22 |T 23 32 25 29 35 25 30 23 27 27 24 WRMS | 12 15 9 14 34 5 16 11 10 20 |NE 21 31 23 28 34 23 28 21 25 25 22 MEDI | 12 15 10 14 31 6 16 12 10 20 |MD 20 32 22 27 33 23 28 22 25 24 22 Table 3.1485.4 GPS week: 1485 Day: 4 MJD: 54643.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 11 18 11 17 46 7 18 10 11 31 5 | 26 32 23 33 29 25 30 25 30 32 25 3 | 7 8 7 10 19 4 9 7 7 17 3 | 10 16 18 22 17 13 16 14 12 14 14 4 | 9 10 6 10 43 6 10 11 12 24 4 | 17 24 19 25 23 19 22 21 18 29 19 5 | 18 16 9 16 26 8 12 16 10 27 5 | 120 128 127 122 127 124 131 126 121 130 124 6 | 6 10 9 9 17 4 8 9 8 18 3 | 16 18 15 23 15 18 14 20 19 22 17 7 | 15 15 12 17 40 7 16 10 8 12 5 | 21 20 18 24 48 17 24 17 16 17 15 X8 | 5 --- --- --- --- 42 --- --- --- --- 0 | 11 --- --- --- --- 21 --- --- --- --- 13 9 | 12 17 7 14 21 5 17 11 12 15 5 | 10 23 15 28 19 16 23 18 21 16 16 10E | 13 21 14 11 36 6 17 15 27 20 6 | 30 35 29 36 37 28 31 26 39 27 28 11 | 8 13 10 18 58 7 15 7 10 19 4 | 24 32 31 32 43 25 34 25 28 23 25 12 | 17 14 12 18 33 5 17 15 9 24 5 | 27 32 23 33 36 24 31 24 25 26 23 13 | 9 18 14 18 44 7 22 14 11 13 5 | 11 29 19 25 48 17 31 17 12 12 14 14 | 9 17 10 20 36 5 18 10 11 16 5 | 13 26 17 27 30 16 25 17 16 18 15 15 | 11 16 9 16 28 7 17 13 13 22 5 | 13 26 17 25 30 16 22 18 20 18 15 16 | 10 18 11 15 35 5 17 13 10 20 5 | 15 28 15 30 28 19 24 20 17 29 19 17 | 11 14 14 13 39 8 14 13 13 44 6 | 17 23 19 22 30 13 15 18 12 38 15 18E | 7 13 9 11 15 5 20 14 7 15 4 | 24 28 23 26 24 25 28 30 22 29 24 19 | 9 7 8 9 37 5 11 9 9 20 3 | 13 18 16 25 19 14 16 16 18 16 15 20E | 11 18 11 9 51 6 19 11 10 13 4 | 15 23 12 20 29 12 23 15 14 16 13 21 | 11 17 10 18 43 8 19 12 9 26 5 | 14 26 12 26 45 18 28 10 12 22 14 22E | 8 14 9 12 19 5 19 15 8 15 4 | 14 19 13 21 17 15 21 17 17 18 14 23 | 11 17 12 15 32 9 18 16 9 19 5 | 11 28 16 26 42 18 26 18 15 17 14 24 | 8 10 6 8 40 6 8 6 8 13 3 | 15 17 18 20 25 18 20 17 17 19 16 25 | 10 17 10 15 27 5 13 11 8 22 4 | 12 27 16 26 31 16 25 17 13 21 16 26 | 11 10 9 13 26 6 10 9 12 39 5 | 13 15 14 26 31 13 13 14 21 32 13 27 | 11 16 9 14 31 5 13 11 7 14 4 | 8 21 17 23 33 13 24 12 9 14 12 28 | 11 15 10 22 31 7 18 18 10 18 5 | 16 29 17 31 46 23 32 21 15 26 19 29 | 19 12 8 10 34 4 13 9 8 25 5 | 14 18 21 21 21 16 21 14 15 18 14 30 | 11 14 8 13 35 4 12 10 10 15 4 | 11 20 16 24 38 14 21 13 13 19 13 31 | 12 20 8 15 26 6 20 10 9 16 5 | 12 30 14 27 37 16 26 10 11 16 15 32E | 9 23 9 16 84 6 18 11 7 30 5 | 56 65 61 65 60 59 63 59 58 71 60 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 15 10 14 37 6 16 12 11 22 |T 20 29 23 30 35 22 28 22 22 26 21 WRMS | 11 15 10 14 36 6 16 11 8 20 |NE 19 28 22 29 35 21 27 21 21 25 20 MEDI | 11 15 9 14 34 6 17 11 9 19 |MD 14 26 17 26 30 17 24 17 17 19 15 Table 3.1485.5 GPS week: 1485 Day: 5 MJD: 54644.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 11 20 13 17 48 8 23 13 11 32 6 | 19 28 17 26 32 21 27 25 27 35 20 3 | 7 11 6 10 18 5 11 4 6 17 3 | 14 21 22 19 19 17 24 18 20 16 17 4 | 11 15 7 7 40 4 16 7 11 14 4 | 18 21 17 19 25 15 19 19 19 22 15 5 | 14 14 7 14 27 5 16 10 11 14 4 | 104 111 110 104 107 106 110 105 104 110 105 6 | 7 12 7 9 22 4 10 6 7 16 3 | 12 17 15 13 20 12 15 18 14 13 12 7 | 10 19 10 12 41 4 17 13 10 13 4 | 20 29 19 20 49 16 23 22 14 20 16 8 | 11 22 9 14 25 7 19 11 11 19 5 | 9 23 12 15 20 13 17 8 8 9 11 9 | 11 17 9 13 20 5 18 9 11 16 4 | 16 30 21 25 29 20 26 22 25 22 19 10E | 15 20 14 14 49 8 20 14 33 21 7 | 37 42 38 35 32 37 37 36 49 33 34 11 | 8 16 9 16 60 8 22 7 9 19 4 | 25 29 25 27 40 20 31 22 22 24 21 12 | 22 19 10 13 31 7 20 14 9 25 6 | 23 35 24 26 37 22 30 24 23 26 21 13 | 8 23 11 15 45 7 25 15 11 13 5 | 11 31 20 20 48 17 30 19 16 14 14 14 | 9 22 8 17 28 6 16 9 7 16 4 | 14 29 18 23 31 16 24 17 13 21 14 15 | 9 19 10 16 32 6 18 11 9 22 5 | 11 28 15 22 32 15 22 16 18 15 12 16 | 8 22 9 15 36 7 20 11 7 20 5 | 16 31 18 24 25 20 26 17 19 24 17 17 | 12 12 10 10 28 6 17 12 8 44 5 | 17 21 18 16 28 14 19 20 20 39 15 18E | 10 15 9 9 15 5 23 9 7 11 4 | 26 31 29 27 35 26 28 28 29 35 27 19 | 8 10 9 6 40 5 14 6 6 18 3 | 19 23 24 17 17 17 20 23 24 19 19 20E | 8 17 10 8 52 5 22 10 11 16 4 | 14 25 18 19 34 15 24 20 21 21 15 21 | 11 19 10 18 36 7 20 11 9 29 5 | 13 32 16 25 37 15 28 13 15 22 13 22E | 11 13 8 14 19 6 19 13 7 10 4 | 12 22 18 22 20 17 24 20 22 23 17 23 | 10 24 12 13 28 9 23 16 11 19 5 | 16 34 22 22 40 17 31 21 19 21 17 24 | 8 14 8 8 33 7 11 4 8 14 3 | 21 30 23 19 24 24 22 24 28 23 22 25 | 8 14 6 15 23 3 16 11 12 20 4 | 14 24 19 20 28 14 23 19 15 22 15 26 | 10 13 8 12 26 4 13 9 10 36 5 | 18 21 17 23 30 17 22 19 20 34 16 27 | 8 15 7 13 24 4 18 10 12 10 4 | 9 22 18 19 30 12 23 13 14 11 11 28 | 9 21 10 18 29 7 24 15 11 18 5 | 16 31 20 27 44 21 33 15 18 16 17 29 | 11 15 8 12 35 7 13 7 11 25 4 | 26 26 25 18 25 20 20 22 23 23 20 30 | 11 17 7 12 29 5 17 8 9 17 4 | 15 25 19 21 36 16 24 18 20 23 16 31 | 11 25 9 13 31 5 21 8 13 15 5 | 9 29 13 16 38 14 27 10 19 16 11 32E | 9 24 9 15 93 5 20 12 11 29 5 | 67 70 67 62 77 67 71 65 67 82 66 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 11 18 9 13 37 6 19 11 11 21 |T 21 31 24 25 35 22 29 23 24 26 21 WRMS | 10 18 9 13 35 6 19 10 8 21 |NE 19 30 23 24 34 20 27 22 22 25 19 MEDI | 10 17 9 13 31 6 18 10 10 18 |MD 16 29 19 22 32 17 24 20 20 22 17 Table 3.1485.6 GPS week: 1485 Day: 6 MJD: 54645.000 Weighted Average Orbit Dynamics (7 days) PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS ------+--------------------------------------------------------+--------------------------------------------------------- 2 | 12 19 10 17 41 7 18 14 11 30 5 | 24 32 22 31 38 25 31 28 30 34 24 3 | 34 12 9 9 25 6 9 6 11 21 6 | 19 25 24 20 21 19 19 18 26 16 17 4 | 10 13 6 7 40 4 12 5 7 16 3 | 21 25 21 19 20 19 22 22 22 26 19 5 | 10 14 7 15 26 3 13 8 9 14 4 | 103 103 102 105 100 104 106 105 109 106 104 6 | 9 10 9 8 27 2 8 5 8 19 3 | 14 25 26 22 28 20 21 23 26 17 20 7 | 17 17 11 14 39 9 16 20 11 12 5 | 24 28 20 25 43 18 23 23 24 20 18 8 | 10 15 8 12 28 5 14 9 9 22 4 | 9 18 7 14 15 11 15 9 13 11 12 9 | 10 16 8 13 22 6 16 8 10 18 4 | 13 29 17 26 22 21 24 23 23 17 18 10E | 19 17 14 13 39 5 18 13 32 13 7 | 56 57 54 58 58 54 54 57 69 54 56 11 | 7 15 10 15 55 5 21 9 10 20 5 | 33 40 36 33 39 30 36 31 29 34 31 12 | 18 18 9 13 32 6 19 10 9 24 5 | 26 38 26 32 36 29 35 30 35 30 28 13 | 11 18 12 16 45 8 20 18 10 16 5 | 12 28 20 21 48 17 28 20 17 14 15 14 | 9 18 9 15 38 5 16 11 8 19 4 | 17 29 23 27 42 20 25 21 21 22 19 15 | 11 22 10 15 28 6 21 14 14 18 5 | 14 31 13 21 34 15 24 17 22 14 13 16 | 11 18 10 15 33 5 13 9 11 20 5 | 22 37 28 34 37 28 35 26 30 30 27 17 | 11 13 9 8 41 5 14 9 9 43 5 | 18 25 24 19 41 17 19 20 21 38 17 18E | 7 16 7 11 31 5 18 10 9 17 4 | 39 42 39 38 36 39 40 42 43 38 39 19 | 11 10 12 6 37 4 11 6 7 25 4 | 21 28 28 21 21 19 22 23 26 17 22 20E | 7 17 7 11 30 5 19 9 10 17 4 | 13 24 14 18 21 15 22 16 23 21 14 21 | 13 29 10 18 33 9 20 13 11 28 6 | 16 32 18 26 43 20 30 15 24 23 15 22E | 7 14 9 10 22 6 20 13 9 17 4 | 21 23 22 21 30 19 25 21 25 24 19 23 | 12 17 12 14 28 8 17 15 12 21 5 | 17 31 21 23 34 19 27 18 17 23 16 24 | 13 14 7 7 34 4 16 7 9 15 4 | 25 30 26 24 21 27 25 26 32 29 25 25 | 11 12 9 13 26 4 13 11 10 25 4 | 14 20 17 18 24 13 21 15 18 23 12 26 | 9 13 7 12 19 6 12 10 11 38 5 | 21 23 16 22 37 15 19 19 29 39 18 27 | 10 14 9 11 26 5 15 11 9 11 4 | 9 21 15 16 27 12 21 12 15 13 10 28 | 8 24 10 17 18 6 19 13 11 18 5 | 25 39 25 34 46 27 38 21 28 20 25 29 | 15 12 9 9 26 6 14 6 10 27 4 | 22 28 24 20 25 20 20 17 27 26 20 30 | 19 16 8 14 42 6 16 9 10 18 5 | 20 27 19 21 41 18 27 16 27 21 18 31 | 8 24 11 11 27 5 16 10 12 16 5 | 18 38 24 23 38 21 29 15 25 20 20 32E | 9 25 9 18 89 4 19 10 8 29 5 | 63 67 65 58 66 61 62 62 58 76 61 ------+--------------------------------------------------------+--------------------------------------------------------- RMS | 13 17 9 13 36 6 16 11 11 22 |T 24 33 26 28 36 25 30 26 30 28 24 WRMS | 12 17 9 13 33 5 16 10 9 21 |NE 22 32 25 27 36 23 29 24 28 26 22 MEDI | 11 16 9 13 31 5 16 10 10 19 |MD 21 29 23 23 36 20 25 21 26 23 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 4.1485 GPS week: 1485 MJD: 54639.0-54645.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2975 |U 11 12 29 |U 5 9 20 |U 7 7 17 | emr | emr 2940 | 13 11 32 |U 8 8 36 | 9 9 23 | esa | esa 2962 | 11 10 29 |U 5 7 19 | 7 8 18 | gfz | gfz 2940 |U 11 10 29 |U 11 11 42 |U 7 7 18 | igr | igr 2950 | 11 10 29 | 6 8 23 | 7 7 17 | igs | igs 2928 | 11 10 28 | 6 8 24 | 7 7 17 | jpl | jpl 2899 |U 12 12 31 |U 6 9 29 |U 7 8 20 | mit | mit 2962 |U 11 13 29 |U 9 14 40 |U 8 9 23 | Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit positions and satellite clock corrections at 15 min intervals. Each line gives the daily station RMS w.r.t. the estimated coordinates for the Latitude, Longitude and Height components. CLK - Satellite clocks used. EPO - Number of satellite clock epochs available for that day. Units: mm. Table 5.1485.0 GPS week: 1485 Day: 0 MJD: 54639.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 16 12 39 | 5 7 16 | 7 7 21 | emr | emr 2966 | 18 14 35 | 9 7 41 | 10 11 26 | esa | esa 2976 | 15 11 38 | 4 5 19 | 9 9 23 | gfz | gfz 2947 | 16 11 37 | 20 13 50 | 8 8 19 | igr | igr 2962 | 16 11 36 | 6 5 18 | 8 8 21 | igs | igs 2878 | 15 11 34 | 5 7 21 | 8 8 20 | jpl | jpl 2966 | 17 12 39 | 5 10 25 | 8 9 23 | mit | mit 2976 | 15 11 34 | 7 11 35 | 8 8 23 | Table 5.1485.1 GPS week: 1485 Day: 1 MJD: 54640.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 10 9 23 | 6 9 19 | 7 6 16 | emr | emr 2968 | 14 9 28 | 7 8 32 | 8 6 24 | esa | esa 2976 | 10 8 29 | 5 6 22 | 6 6 18 | gfz | gfz 2953 | 12 8 30 | 12 10 32 | 6 5 17 | igr | igr 2953 | 10 7 27 | 5 7 23 | 5 5 17 | igs | igs 2972 | 10 8 26 | 6 8 26 | 6 5 16 | jpl | jpl 2968 | 11 8 28 | 5 8 29 | 6 6 19 | mit | mit 2976 | 9 8 23 | 9 14 47 | 8 8 22 | Table 5.1485.2 GPS week: 1485 Day: 2 MJD: 54641.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 8 9 25 | 4 8 19 | 6 7 15 | emr | emr 2968 | 12 9 35 | 11 8 48 | 8 9 18 | esa | esa 2976 | 8 8 27 | 4 7 21 | 7 8 15 | gfz | gfz 2956 | 9 8 30 | 9 10 39 | 7 6 15 | igr | igr 2963 | 8 8 28 | 5 7 22 | 7 7 13 | igs | igs 2968 | 9 8 28 | 5 7 24 | 6 7 15 | jpl | jpl 2872 | 10 11 33 | 5 7 24 | 6 6 16 | mit | mit 2976 | 9 25 41 | 7 11 35 | 8 8 19 | Table 5.1485.3 GPS week: 1485 Day: 3 MJD: 54642.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 14 17 31 | 5 13 20 | 7 7 17 | emr | emr 2872 | 13 15 28 | 10 9 47 | 7 11 26 | esa | esa 2976 | 12 15 29 | 5 9 19 | 7 9 17 | gfz | gfz 2956 | 11 11 23 | 11 14 48 | 7 7 15 | igr | igr 2969 | 11 12 25 | 8 11 29 | 5 8 15 | igs | igs 2915 | 13 15 30 | 7 13 28 | 6 8 16 | jpl | jpl 2680 | 14 18 27 | 7 11 48 | 7 10 21 | mit | mit 2976 | 14 14 30 | 11 18 41 | 9 9 20 | Table 5.1485.4 GPS week: 1485 Day: 4 MJD: 54643.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2973 | 8 12 27 | 4 6 21 | 7 7 16 | emr | emr 2872 | 13 10 34 | 7 12 37 | 9 10 25 | esa | esa 2880 | 9 10 26 | 4 6 14 | 8 7 18 | gfz | gfz 2861 | 11 11 26 | 11 16 46 | 7 8 24 | igr | igr 2855 | 10 11 26 | 7 15 29 | 7 7 18 | igs | igs 2876 | 11 10 25 | 5 10 28 | 7 8 20 | jpl | jpl 2872 | 12 12 31 | 5 10 32 | 7 9 22 | mit | mit 2880 | 11 8 26 | 13 22 36 | 8 13 37 | Table 5.1485.5 GPS week: 1485 Day: 5 MJD: 54644.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 11 15 35 | 8 11 28 | 8 7 17 | emr | emr 2968 | 14 11 38 | 7 6 28 | 11 9 25 | esa | esa 2976 | 11 13 35 | 7 10 23 | 8 9 20 | gfz | gfz 2956 | 12 13 32 | 8 10 36 | 9 8 18 | igr | igr 2976 | 12 13 35 | 6 8 19 | 9 8 17 | igs | igs 2964 | 12 11 33 | 6 6 20 | 9 8 20 | jpl | jpl 2968 | 13 12 38 | 6 8 24 | 9 10 20 | mit | mit 2976 | 11 13 32 | 7 10 30 | 9 8 22 | Table 5.1485.6 GPS week: 1485 Day: 6 MJD: 54645.0 CENT| CLK EPO | BRUS | TOW2 | WILL | ----+----------+-------------------+-------------------+-------------------+ cod | cod 2976 | 8 9 21 | 5 7 16 | 6 7 14 | emr | emr 2968 | 10 11 25 | 7 7 20 | 9 5 21 | esa | esa 2976 | 8 8 20 | 4 6 19 | 6 6 16 | gfz | gfz 2957 | 9 9 22 | 10 7 39 | 8 7 18 | igr | igr 2976 | 11 10 23 | 4 6 17 | 7 5 16 | igs | igs 2925 | 8 10 21 | 5 5 21 | 7 6 15 | jpl | jpl 2968 | 9 9 23 | 7 10 24 | 7 6 19 | mit | mit 2976 | 8 8 18 | 10 9 57 | 6 6 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 6.1485 GPS week: 1485 MJD: 54639.500-54645.500 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 7 22 -141 0 | 2 10 | 18 14 68 89 4 | 1 emr uuuuu | 63 26 81 141 -13 | 9 15 | 29 31 153 50 7 | 2 esa uuuuu | -20 -12 -20 -12 4 | -1 11 | 17 17 79 71 5 | 1 gfz uuuuu | -23 -17 8 -83 0 | -7 12 | 15 16 45 45 3 | 1 grg xxxxx | -6 -6 38 -136 -11 | 0 36 | 33 27 94 108 45 | 3 igr xxxxx | -15 7 16 -26 2 | -3 11 | 15 31 33 34 4 | 2 irf xxxxx | 0 2 -32 11 0 | -3 13 | 11 10 49 22 6 | 3 jpl uuuux | 18 27 135 48 -17 | 5 15 | 22 16 110 70 25 | 3 mit uuuuu | 10 -13 -150 71 -4 | 6 17 | 19 20 128 69 14 | 4 ngs uuuuu | 21 -13 3 49 13 | -5 15 | 65 62 106 89 9 | 2 sio uuuuu | -66 46 33 -125 -16 | 41 44 | 31 33 168 76 8 | 3 Table 7.1485.0 GPS week: 1485 Day: 0 MJD: 54639.500 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 | -43 3 6 -84 -3 | 1 9 emr uuuuu | 77 23 -168 141 0 | 9 15 esa uuuuu | -39 1 11 20 0 | -2 10 gfz uuuuu | -24 -2 -9 -129 -3 | -7 12 grg xxxxx | -18 -37 106 -252 -102 | 6 28 igr xxxxx | -11 32 20 -87 9 | -6 9 irf xxxxx | -1 -5 13 47 9 | -8 14 jpl uuuux | 16 38 41 71 1 | 4 12 mit uuuuu | 27 -25 -52 139 17 | -1 16 ngs uuuuu | 53 -23 49 -88 -1 | -7 14 sio uuuuu | -96 5 182 -41 -5 | 40 43 Table 7.1485.1 GPS week: 1485 Day: 1 MJD: 54640.500 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 -3 153 -282 -7 | 2 9 emr uuuuu | 30 33 20 54 -12 | 11 16 esa uuuuu | -36 -3 -105 10 0 | -2 10 gfz uuuuu | -29 -31 34 -100 0 | -8 12 grg xxxxx | 3 -19 92 -71 7 | -3 39 igr xxxxx | -26 6 43 -22 2 | -5 11 irf xxxxx | -2 6 -53 11 7 | -6 14 jpl uuuux | 34 21 166 135 1 | 5 13 mit uuuuu | 1 -5 -160 -6 11 | 2 18 ngs uuuuu | 54 -17 62 199 20 | -8 14 sio uuuuu | -59 54 -28 -212 -7 | 41 43 Table 7.1485.2 GPS week: 1485 Day: 2 MJD: 54641.500 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 | -18 16 61 -1 1 | 1 9 emr uuuuu | 92 25 12 172 -16 | 9 15 esa uuuuu | 0 -7 -18 -144 0 | -2 10 gfz uuuuu | -7 -19 52 -65 1 | -9 12 grg xxxxx | -35 23 72 -189 -14 | -3 39 igr xxxxx | 6 2 59 -34 1 | -5 10 irf xxxxx | 5 13 -72 -10 -1 | -5 14 jpl uuuux | 14 48 165 110 -15 | 5 13 mit uuuuu | 34 1 -257 80 0 | 4 18 ngs uuuuu | -39 -58 -38 -2 12 | -7 14 sio uuuuu | -82 74 223 -78 -16 | 42 44 Table 7.1485.3 GPS week: 1485 Day: 3 MJD: 54642.500 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 | -10 19 -23 -184 -1 | 4 10 emr uuuuu | 56 59 82 122 -12 | 12 15 esa uuuuu | -16 -23 18 81 1 | 0 11 gfz uuuuu | -17 4 -22 1 -2 | -6 12 grg xxxxx | 32 -34 127 -112 26 | 2 37 igr xxxxx | -3 45 -2 -23 5 | -1 10 irf xxxxx | 0 10 -48 21 -6 | -1 12 jpl uuuux | 15 16 265 21 -1 | 7 13 mit uuuuu | 11 22 -253 -22 -7 | 9 17 ngs uuuuu | 14 -87 107 22 25 | -5 16 sio uuuuu | -90 74 -184 -116 -21 | 45 46 Table 7.1485.4 GPS week: 1485 Day: 4 MJD: 54643.500 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 | -22 12 24 -170 1 | 2 11 emr uuuuu | 39 -37 125 190 -10 | 8 15 esa uuuuu | -34 -41 103 -5 8 | -2 12 gfz uuuuu | -52 -34 7 -96 -6 | -7 13 grg xxxxx | 4 28 -151 -2 17 | 0 35 igr xxxxx | -41 -42 -26 11 -2 | -3 11 irf xxxxx | -21 -5 -100 22 -3 | -2 14 jpl uuuux | -20 9 -62 81 -2 | 6 13 mit uuuuu | -26 -28 -296 52 -10 | 8 18 ngs uuuuu | 137 88 3 97 14 | -5 16 sio uuuuu | -87 42 211 -234 -13 | 41 44 Table 7.1485.5 GPS week: 1485 Day: 5 MJD: 54644.500 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 -19 -7 -98 5 | 2 11 emr uuuuu | 105 35 174 198 -22 | 8 15 esa uuuuu | -1 7 -132 -53 4 | 0 12 gfz uuuuu | -20 -32 59 -64 1 | -6 13 grg xxxxx | -57 -20 17 -285 19 | 1 36 igr xxxxx | -17 -23 38 -38 -3 | -2 11 irf xxxxx | 14 -12 -2 -20 -3 | 0 12 jpl uuuux | 50 15 155 -48 -59 | 7 14 mit uuuuu | 11 -38 -78 90 -13 | 10 17 ngs uuuuu | -45 52 54 53 19 | -3 16 sio uuuuu | -19 -3 -88 -50 -23 | 41 44 Table 7.1485.6 GPS week: 1485 Day: 6 MJD: 54645.500 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 17 -56 -165 5 | 1 11 emr uuuuu | 44 45 324 114 -20 | 4 18 esa uuuuu | -11 -20 -18 11 12 | 0 12 gfz uuuuu | -12 -3 -66 -128 5 | -8 14 grg xxxxx | 32 15 6 -43 -31 | 0 36 igr xxxxx | -13 27 -22 15 2 | -3 13 irf xxxxx | 4 9 36 9 -6 | -2 14 jpl uuuux | 20 43 214 -31 -43 | -1 26 mit uuuuu | 9 -16 50 163 -25 | 8 18 ngs uuuuu | -24 -49 -212 64 5 | -2 15 sio uuuuu | -31 75 -84 -145 -27 | 37 41