ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 14929.5437 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 69.2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2.013 ET - UTC (sec) : 68.18 UT1 - UTC (sec) : 0.00 Maneuvers contained within the current ephemeris are as follows: IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP ------------------------------------------------------------------------ 087/06:36:30.000 0.0 0.0 0.0 N/A 0.0 0.0 224.3 000/00:00:00.000 0.0 0.0 216.6 090/20:25:00.000 0.0 0.0 0.0 N/A 0.0 0.0 224.2 000/00:00:00.000 0.0 0.0 216.7 094/11:01:35.000 0.0 0.0 0.0 N/A 0.0 0.0 223.9 000/00:00:00.000 0.0 0.0 216.9 094/14:24:50.000 0.0 0.0 0.0 N/A 0.0 0.0 224.0 000/00:00:00.000 0.0 0.0 216.9 097/20:12:00.000 0.0 0.0 0.0 N/A 0.0 0.0 223.9 000/00:00:00.000 0.0 0.0 216.9 Coasting Arc #1 (Orbit 224) --------------------------------------- Vector Time (GMT): 2019/084/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4541754.57 A = 6793413.21 meter Y = -4833571.21 meter E = .0015898 Z = 1434553.63 I = 51.97770 XDOT = 2654.114481 Wp = 118.20257 YDOT = -4232.791722 meter/sec RA = 56.51944 deg ZDOT = -5817.480433 TA = 46.23111 MA = 46.09966 Ha = 224.405 n.mi Hp = 216.641 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -14900769.58 X = -4494334.93 Y = -15858173.26 feet Y = -4884095.04 meter Z = 4706540.78 Z = 1412606.96 XDOT = 8707.724674 XDOT = 2729.507662 YDOT = -13887.111949 feet/sec YDOT = -4202.690428 meter/sec ZDOT = -19086.221894 ZDOT = -5804.404286 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -15415972.06 X = -4698788.28 Y = -15387744.62 feet Y = -4690184.56 meter Z = 4607736.96 Z = 1404438.23 XDOT = 7278.775470 XDOT = 2218.570763 YDOT = -13031.229690 feet/sec YDOT = -3971.918810 meter/sec ZDOT = -19026.582768 ZDOT = -5799.302428 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19084.53496800 .00016717 00000-0 10270-3 0 9004 2 25544 51.6387 57.0811 0002084 112.5331 247.6042 15.52439279 2255 Satellite: ISS Catalog Number: 25544 Epoch time: 19084.53496800 = yrday.fracday Element set: 900 Inclination: 51.6387 deg RA of node: 57.0811 deg Eccentricity: .0002084 Arg of perigee: 112.5331 deg Mean anomaly: 247.6042 deg Mean motion: 15.52439279 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 225 Checksum: 293 Coasting Arc #2 (Orbit 239) --------------------------------------- Vector Time (GMT): 2019/085/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4404817.89 A = 6794159.76 meter Y = 5157153.54 meter E = .0012237 Z = -314710.76 I = 51.96183 XDOT = -3418.562267 Wp = 52.83059 YDOT = 3277.372064 meter/sec RA = 51.57924 deg ZDOT = 6026.643492 TA = 303.79545 MA = 303.91192 Ha = 224.378 n.mi Hp = 216.589 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14451502.28 X = 4348350.46 Y = 16919795.07 feet Y = 5206095.55 meter Z = -1032515.63 Z = -293451.25 XDOT = -11215.755470 XDOT = -3484.230797 YDOT = 10752.533018 feet/sec YDOT = 3238.776478 meter/sec ZDOT = 19772.452403 ZDOT = 6009.877709 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15256222.06 X = 4650096.48 Y = 16203747.55 feet Y = 4938902.25 meter Z = -936870.12 Z = -285558.01 XDOT = -9635.164625 XDOT = -2936.798178 YDOT = 10175.410114 feet/sec YDOT = 3101.465003 meter/sec ZDOT = 19696.211782 ZDOT = 6003.405351 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19085.50055288 .00016717 00000-0 10270-3 0 9014 2 25544 51.6394 52.2806 0002183 118.8369 241.3002 15.52455349 2404 Satellite: ISS Catalog Number: 25544 Epoch time: 19085.50055288 = yrday.fracday Element set: 901 Inclination: 51.6394 deg RA of node: 52.2806 deg Eccentricity: .0002183 Arg of perigee: 118.8369 deg Mean anomaly: 241.3002 deg Mean motion: 15.52455349 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 240 Checksum: 292 Coasting Arc #3 (Orbit 255) --------------------------------------- Vector Time (GMT): 2019/086/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4108070.67 A = 6793901.28 meter Y = -5335473.52 meter E = .0011904 Z = -864296.27 I = 51.93992 XDOT = 4236.920431 Wp = 136.54920 YDOT = -2306.524823 meter/sec RA = 46.63758 deg ZDOT = -5956.803757 TA = 52.75575 MA = 52.64722 Ha = 224.320 n.mi Hp = 216.660 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13477922.14 X = -4043904.31 Y = -17504834.37 feet Y = -5381054.10 meter Z = -2835617.67 Z = -884095.57 XDOT = 13900.657581 XDOT = 4291.332524 YDOT = -7567.338657 feet/sec YDOT = -2258.840679 meter/sec ZDOT = -19543.319414 ZDOT = -5936.090166 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14573613.87 X = -4442037.51 Y = -16588269.89 feet Y = -5056104.66 meter Z = -2924623.03 Z = -891425.10 XDOT = 12297.051521 XDOT = 3748.141304 YDOT = -7406.497104 feet/sec YDOT = -2257.500317 meter/sec ZDOT = -19449.316451 ZDOT = -5928.151654 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19086.53050777 .00016717 00000-0 10270-3 0 9027 2 25544 51.6400 47.1588 0002017 116.9830 243.1528 15.52440774 2566 Satellite: ISS Catalog Number: 25544 Epoch time: 19086.53050777 = yrday.fracday Element set: 902 Inclination: 51.6400 deg RA of node: 47.1588 deg Eccentricity: .0002017 Arg of perigee: 116.9830 deg Mean anomaly: 243.1528 deg Mean motion: 15.52440774 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 256 Checksum: 297 Coasting Arc #4 (Orbit 267) --------------------------------------- Vector Time (GMT): 2019/087/06:36:30.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3280199.52 A = 6791942.79 meter Y = -5486196.06 meter E = .0008010 Z = -2291651.68 I = 51.91720 XDOT = 5308.893968 Wp = 131.66515 YDOT = -904.622611 meter/sec RA = 42.80849 deg ZDOT = -5450.780275 TA = 73.72356 MA = 73.63547 Ha = 224.338 n.mi Hp = 216.598 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -10761809.44 X = -3207476.01 Y = -17999330.91 feet Y = -5522471.04 meter Z = -7518542.25 Z = -2307408.67 XDOT = 17417.631128 XDOT = 5345.091887 YDOT = -2967.921953 feet/sec YDOT = -845.052728 meter/sec ZDOT = -17883.137386 ZDOT = -5424.903819 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14967419.25 X = 4562069.39 Y = -14652675.69 feet Y = -4466135.55 meter Z = -7589228.50 Z = -2313196.85 XDOT = 5951.148115 XDOT = 1813.909945 YDOT = 15251.310434 feet/sec YDOT = 4648.599420 meter/sec ZDOT = -17765.927489 ZDOT = -5415.054699 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19087.30297294 .00016717 00000-0 10270-3 0 9031 2 25544 51.6418 43.3181 0002228 123.7957 236.3407 15.52450731 2689 Satellite: ISS Catalog Number: 25544 Epoch time: 19087.30297294 = yrday.fracday Element set: 903 Inclination: 51.6418 deg RA of node: 43.3181 deg Eccentricity: .0002228 Arg of perigee: 123.7957 deg Mean anomaly: 236.3407 deg Mean motion: 15.52450731 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 268 Checksum: 304 Coasting Arc #5 (Orbit 283) --------------------------------------- Vector Time (GMT): 2019/088/06:36:30.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2672617.26 A = 6789745.85 meter Y = 5315944.51 meter E = .0014597 Z = 3258983.52 I = 51.88329 XDOT = -6001.019917 Wp = 92.51230 YDOT = 78.911931 meter/sec RA = 37.85813 deg ZDOT = 4773.536447 TA = 305.12038 MA = 305.25711 Ha = 224.396 n.mi Hp = 216.619 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 8768429.32 X = 2597144.00 Y = 17440762.82 feet Y = 5345409.77 meter Z = 10692203.16 Z = 3271782.39 XDOT = -19688.385556 XDOT = -6024.643352 YDOT = 258.897412 feet/sec YDOT = 11.672513 meter/sec ZDOT = 15661.208815 ZDOT = 4744.328571 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14681413.53 X = -4474894.84 Y = 12817676.60 feet Y = 3906827.83 meter Z = 10749513.12 Z = 3276451.60 XDOT = -4313.023045 XDOT = -1314.609424 YDOT = -18015.644236 feet/sec YDOT = -5491.168363 meter/sec ZDOT = 15529.020000 ZDOT = 4733.245296 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19088.33292610 .00016717 00000-0 10270-3 0 9043 2 25544 51.6407 38.1967 0002289 123.5309 236.6062 15.52424371 2846 Satellite: ISS Catalog Number: 25544 Epoch time: 19088.33292610 = yrday.fracday Element set: 904 Inclination: 51.6407 deg RA of node: 38.1967 deg Eccentricity: .0002289 Arg of perigee: 123.5309 deg Mean anomaly: 236.6062 deg Mean motion: 15.52424371 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 284 Checksum: 303 Coasting Arc #6 (Orbit 298) --------------------------------------- Vector Time (GMT): 2019/089/06:36:30.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1888499.29 A = 6787011.22 meter Y = -5067003.96 meter E = .0008819 Z = -4109901.46 I = 51.84943 XDOT = 6587.487554 Wp = 82.54275 YDOT = 661.426660 meter/sec RA = 32.90180 deg ZDOT = -3848.365453 TA = 147.76347 MA = 147.70954 Ha = 224.282 n.mi Hp = 216.632 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6195863.81 X = -1811734.81 Y = -16624028.75 feet Y = -5087693.54 meter Z = -13483928.66 Z = -4118888.21 XDOT = 21612.491974 XDOT = 6598.294764 YDOT = 2170.034974 feet/sec YDOT = 735.152724 meter/sec ZDOT = -12625.870910 ZDOT = -3816.339980 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14369429.68 X = 4379802.17 Y = -10352973.11 feet Y = -3155586.21 meter Z = -13524009.41 Z = -4122118.07 XDOT = 2992.874430 XDOT = 912.228126 YDOT = 20432.372990 feet/sec YDOT = 6227.787287 meter/sec ZDOT = -12481.022926 ZDOT = -3804.215788 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19089.29850224 .00016717 00000-0 10270-3 0 9051 2 25544 51.6425 33.3959 0002160 129.2726 230.8617 15.52457293 2995 Satellite: ISS Catalog Number: 25544 Epoch time: 19089.29850224 = yrday.fracday Element set: 905 Inclination: 51.6425 deg RA of node: 33.3959 deg Eccentricity: .0002160 Arg of perigee: 129.2726 deg Mean anomaly: 230.8617 deg Mean motion: 15.52457293 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 299 Checksum: 320 Coasting Arc #7 (Orbit 314) --------------------------------------- Vector Time (GMT): 2019/090/06:36:30.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1007397.11 A = 6784698.14 meter Y = 4749350.32 meter E = .0009890 Z = 4734063.69 I = 51.81129 XDOT = -7039.389362 Wp = 119.68928 YDOT = -1271.665269 meter/sec RA = 27.93848 deg ZDOT = 2764.625566 TA = 302.96274 MA = 303.05779 Ha = 224.306 n.mi Hp = 216.663 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 3305108.62 X = 931218.40 Y = 15581858.01 feet Y = 4760190.17 meter Z = 15531705.03 Z = 4738771.81 XDOT = -23095.109457 XDOT = -7038.074960 YDOT = -4172.130148 feet/sec YDOT = -1350.377078 meter/sec ZDOT = 9070.293852 ZDOT = 2730.434448 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14019948.40 X = -4273280.27 Y = 7517582.57 feet Y = 2291359.17 meter Z = 15552456.47 Z = 4740388.73 XDOT = -2066.177637 XDOT = -629.770944 YDOT = -22360.033449 feet/sec YDOT = -6815.338195 meter/sec ZDOT = 8915.725819 ZDOT = 2717.513230 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19090.32844957 .00016717 00000-0 10270-3 0 9064 2 25544 51.6408 28.2743 0002210 129.2828 230.8520 15.52447281 3157 Satellite: ISS Catalog Number: 25544 Epoch time: 19090.32844957 = yrday.fracday Element set: 906 Inclination: 51.6408 deg RA of node: 28.2743 deg Eccentricity: .0002210 Arg of perigee: 129.2828 deg Mean anomaly: 230.8520 deg Mean motion: 15.52447281 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 315 Checksum: 295 Coasting Arc #8 (Orbit 323) --------------------------------------- Vector Time (GMT): 2019/090/20:25:00.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3540834.86 A = 6789077.94 meter Y = 4649794.19 meter E = .0013803 Z = 3444516.51 I = 51.80622 XDOT = -6025.684438 Wp = 97.57050 YDOT = 1171.261799 meter/sec RA = 25.08591 deg ZDOT = 4595.545384 TA = 302.67340 MA = 302.80646 Ha = 224.158 n.mi Hp = 216.732 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11616912.28 X = 3471844.97 Y = 15255230.29 feet Y = 4689004.84 meter Z = 11300907.17 Z = 3461548.44 XDOT = -19769.305900 XDOT = -6060.656404 YDOT = 3842.722437 feet/sec YDOT = 1103.683236 meter/sec ZDOT = 15077.248634 ZDOT = 4566.190074 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 2863369.21 X = 872754.94 Y = -18914025.65 feet Y = -5764995.02 meter Z = 11377431.84 Z = 3467841.22 XDOT = 15245.912551 XDOT = 4646.954145 YDOT = 11331.925490 feet/sec YDOT = 3453.970889 meter/sec ZDOT = 14944.283186 ZDOT = 4555.017515 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19090.90779416 .00016717 00000-0 10270-3 0 9076 2 25544 51.6380 25.3904 0002199 141.3621 218.7688 15.52465867 3245 Satellite: ISS Catalog Number: 25544 Epoch time: 19090.90779416 = yrday.fracday Element set: 907 Inclination: 51.6380 deg RA of node: 25.3904 deg Eccentricity: .0002199 Arg of perigee: 141.3621 deg Mean anomaly: 218.7688 deg Mean motion: 15.52465867 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 324 Checksum: 325 Coasting Arc #9 (Orbit 338) --------------------------------------- Vector Time (GMT): 2019/091/20:25:00.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2688811.49 A = 6786427.67 meter Y = -4557597.41 meter E = .0009246 Z = -4257759.86 I = 51.76878 XDOT = 6719.260874 Wp = 82.19739 YDOT = -580.996194 meter/sec RA = 20.12370 deg ZDOT = -3626.883353 TA = 150.74735 MA = 150.69554 Ha = 224.182 n.mi Hp = 216.678 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -8821560.02 X = -2616965.61 Y = -14952747.41 feet Y = -4587264.29 meter Z = -13969028.41 Z = -4270646.06 XDOT = 22044.819139 XDOT = 6742.875620 YDOT = -1906.155491 feet/sec YDOT = -505.725035 meter/sec ZDOT = -11899.223599 ZDOT = -3594.186512 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -4323395.34 X = -1317770.90 Y = 16765902.66 feet Y = 5110247.13 meter Z = -14026799.05 Z = -4275368.35 XDOT = -15837.010486 XDOT = -4827.120796 YDOT = -13900.144951 feet/sec YDOT = -4236.764181 meter/sec ZDOT = -11751.218394 ZDOT = -3581.771367 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19091.87336756 .00016717 00000-0 10270-3 0 9080 2 25544 51.6399 20.5897 0002187 140.2414 219.8898 15.52471235 3395 Satellite: ISS Catalog Number: 25544 Epoch time: 19091.87336756 = yrday.fracday Element set: 908 Inclination: 51.6399 deg RA of node: 20.5897 deg Eccentricity: .0002187 Arg of perigee: 140.2414 deg Mean anomaly: 219.8898 deg Mean motion: 15.52471235 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 339 Checksum: 339 Coasting Arc #10 (Orbit 354) --------------------------------------- Vector Time (GMT): 2019/092/20:25:00.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1733433.42 A = 6784170.01 meter Y = 4423890.58 meter E = .0009021 Z = 4838227.18 I = 51.72963 XDOT = -7246.344866 Wp = 125.84882 YDOT = 87.336712 meter/sec RA = 15.15343 deg ZDOT = 2507.917576 TA = 299.48869 MA = 299.57864 Ha = 224.074 n.mi Hp = 216.807 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5687117.52 X = 1660334.06 Y = 14514076.71 feet Y = 4442866.85 meter Z = 15873448.75 Z = 4846469.49 XDOT = -23774.097331 XDOT = -7258.964954 YDOT = 286.537770 feet/sec YDOT = 6.232719 meter/sec ZDOT = 8228.076037 ZDOT = 2472.687029 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 6004709.54 X = 1830235.47 Y = -14344911.50 feet Y = -4372329.02 meter Z = 15910219.39 Z = 4849434.87 XDOT = 16367.007813 XDOT = 4988.663981 YDOT = 15830.902402 feet/sec YDOT = 4825.259052 meter/sec ZDOT = 8068.679113 ZDOT = 2459.333394 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19092.90330781 .00016717 00000-0 10270-3 0 9098 2 25544 51.6399 15.4675 0002144 147.3129 212.8156 15.52476547 3555 Satellite: ISS Catalog Number: 25544 Epoch time: 19092.90330781 = yrday.fracday Element set: 909 Inclination: 51.6399 deg RA of node: 15.4675 deg Eccentricity: .0002144 Arg of perigee: 147.3129 deg Mean anomaly: 212.8156 deg Mean motion: 15.52476547 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 355 Checksum: 317 Coasting Arc #11 (Orbit 369) --------------------------------------- Vector Time (GMT): 2019/093/20:25:00.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -661210.52 A = 6782649.07 meter Y = -4303430.68 meter E = .0015182 Z = -5213945.37 I = 51.69253 XDOT = 7543.687998 Wp = 88.11284 YDOT = 351.652968 meter/sec RA = 10.17959 deg ZDOT = -1249.562433 TA = 169.89521 MA = 169.86466 Ha = 224.154 n.mi Hp = 216.747 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -2169325.84 X = -587712.74 Y = -14118867.06 feet Y = -4310414.43 meter Z = -17106119.97 Z = -5216978.29 XDOT = 24749.632541 XDOT = 7545.264734 YDOT = 1153.717086 feet/sec YDOT = 436.020444 meter/sec ZDOT = -4099.614280 ZDOT = -1212.914247 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8077637.67 X = -2462063.96 Y = 11762137.36 feet Y = 3585099.47 meter Z = -17119334.58 Z = -5217973.18 XDOT = -16550.563235 XDOT = -5044.611674 YDOT = -17078.989521 feet/sec YDOT = -5205.676006 meter/sec ZDOT = -3933.871703 ZDOT = -1199.044095 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19093.86887551 .00016717 00000-0 10270-3 0 9108 2 25544 51.6404 10.6678 0002254 146.6071 213.5223 15.52475899 3701 Satellite: ISS Catalog Number: 25544 Epoch time: 19093.86887551 = yrday.fracday Element set: 910 Inclination: 51.6404 deg RA of node: 10.6678 deg Eccentricity: .0002254 Arg of perigee: 146.6071 deg Mean anomaly: 213.5223 deg Mean motion: 15.52475899 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 370 Checksum: 313 Coasting Arc #12 (Orbit 379) --------------------------------------- Vector Time (GMT): 2019/094/11:01:35.000 Vector Time (MET): N/A Weight (LBS) : 914819.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2662528.43 A = 6784622.56 meter Y = 4087354.18 meter E = .0009363 Z = 4710905.03 I = 51.68042 XDOT = -7015.051605 Wp = 122.45430 YDOT = 1341.414161 meter/sec RA = 7.17016 deg ZDOT = 2791.974463 TA = 299.84981 MA = 299.94283 Ha = 223.922 n.mi Hp = 216.872 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 8735329.48 X = 2593741.57 Y = 13409954.65 feet Y = 4116744.35 meter Z = 15455725.17 Z = 4723671.10 XDOT = -23015.261170 XDOT = -7043.092200 YDOT = 4400.965094 feet/sec YDOT = 1262.810469 meter/sec ZDOT = 9160.021203 ZDOT = 2757.829645 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 7914789.21 X = 2412427.75 Y = 13846138.40 feet Y = 4220302.99 meter Z = 15512990.31 Z = 4728359.45 XDOT = -22265.863817 XDOT = -6786.635291 YDOT = 2605.372474 feet/sec YDOT = 794.117530 meter/sec ZDOT = 9005.413595 ZDOT = 2744.850064 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19094.51258494 .00016717 00000-0 10270-3 0 9110 2 25544 51.6414 7.4711 0001790 148.5925 211.5334 15.52490258 3805 Satellite: ISS Catalog Number: 25544 Epoch time: 19094.51258494 = yrday.fracday Element set: 911 Inclination: 51.6414 deg RA of node: 7.4711 deg Eccentricity: .0001790 Arg of perigee: 148.5925 deg Mean anomaly: 211.5334 deg Mean motion: 15.52490258 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 380 Checksum: 299 Coasting Arc #13 (Orbit 381) --------------------------------------- Vector Time (GMT): 2019/094/14:24:50.000 Vector Time (MET): N/A Weight (LBS) : 929253.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4844613.39 A = 6787505.97 meter Y = 2607491.19 meter E = .0011834 Z = 3965331.57 I = 51.68675 XDOT = -5329.323870 Wp = 86.79318 YDOT = -3787.861616 meter/sec RA = 6.42349 deg ZDOT = -4009.295105 TA = 45.03150 MA = 44.93561 Ha = 224.042 n.mi Hp = 216.896 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15894400.89 X = -4892672.47 Y = 8554761.11 feet Y = 2553047.05 meter Z = 13009618.01 Z = 3941681.18 XDOT = -17484.658367 XDOT = -5267.095854 YDOT = -12427.367506 feet/sec YDOT = -3847.110352 meter/sec ZDOT = -13153.855332 ZDOT = -4035.031472 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -4354285.77 X = -1327186.30 Y = 17596478.89 feet Y = 5363406.77 meter Z = 12902333.29 Z = 3932631.19 XDOT = -19598.077471 XDOT = -5973.494013 YDOT = 4906.915119 feet/sec YDOT = 1495.627728 meter/sec ZDOT = -13269.823251 ZDOT = -4044.642127 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19094.64132621 .00016717 00000-0 10270-3 0 9128 2 25544 51.6430 6.8319 0001592 145.7392 214.3863 15.52503217 3827 Satellite: ISS Catalog Number: 25544 Epoch time: 19094.64132621 = yrday.fracday Element set: 912 Inclination: 51.6430 deg RA of node: 6.8319 deg Eccentricity: .0001592 Arg of perigee: 145.7392 deg Mean anomaly: 214.3863 deg Mean motion: 15.52503217 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 382 Checksum: 289 Coasting Arc #14 (Orbit 396) --------------------------------------- Vector Time (GMT): 2019/095/14:24:50.000 Vector Time (MET): N/A Weight (LBS) : 929253.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 5574550.60 A = 6790164.16 meter Y = -2319461.98 meter E = .0004970 Z = -3110921.07 I = 51.66207 XDOT = 4370.784250 Wp = 90.41385 YDOT = 3970.352548 meter/sec RA = 1.45438 deg ZDOT = 4878.607569 TA = 233.85852 MA = 233.90452 Ha = 223.931 n.mi Hp = 217.098 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 18289208.00 X = 5615184.40 Y = -7609783.40 feet Y = -2256896.58 meter Z = -10206433.95 Z = -3083742.88 XDOT = 14339.843341 XDOT = 4302.364064 YDOT = 13026.091036 feet/sec YDOT = 4018.847663 meter/sec ZDOT = 16005.930343 ZDOT = 4899.672749 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 6324616.76 X = 1927743.19 Y = -18838863.23 feet Y = -5742085.51 meter Z = -10083237.66 Z = -3073370.84 XDOT = 17798.107259 XDOT = 5424.863093 YDOT = -2630.547258 feet/sec YDOT = -801.790804 meter/sec ZDOT = 16100.736444 ZDOT = 4907.504468 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19095.60688965 .00016717 00000-0 10270-3 0 9133 2 25544 51.6429 2.0306 0001540 154.9556 205.1670 15.52467757 3974 Satellite: ISS Catalog Number: 25544 Epoch time: 19095.60688965 = yrday.fracday Element set: 913 Inclination: 51.6429 deg RA of node: 2.0306 deg Eccentricity: .0001540 Arg of perigee: 154.9556 deg Mean anomaly: 205.1670 deg Mean motion: 15.52467757 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 397 Checksum: 321 Coasting Arc #15 (Orbit 412) --------------------------------------- Vector Time (GMT): 2019/096/14:24:50.000 Vector Time (MET): N/A Weight (LBS) : 929253.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6135395.70 A = 6792369.19 meter Y = 2021677.19 meter E = .0015112 Z = 2074370.91 I = 51.63640 XDOT = -3260.376219 Wp = 114.64539 YDOT = -4189.275079 meter/sec RA = 356.48745 deg ZDOT = -5534.867180 TA = 42.40452 MA = 42.28784 Ha = 223.946 n.mi Hp = 217.011 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20129250.98 X = -6167622.92 Y = 6632799.19 feet Y = 1952886.90 meter Z = 6805678.83 Z = 2044488.69 XDOT = -10696.772373 XDOT = -3186.402645 YDOT = -13744.340810 feet/sec YDOT = -4225.321780 meter/sec ZDOT = -18159.013059 ZDOT = -5550.524977 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7917505.10 X = -2413255.55 Y = 19705792.12 feet Y = 6006325.44 meter Z = 6670300.19 Z = 2033107.50 XDOT = -15888.987350 XDOT = -4842.963344 YDOT = -184.508994 feet/sec YDOT = -56.238341 meter/sec ZDOT = -18229.327990 ZDOT = -5556.299171 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19096.63682025 .00016717 00000-0 10270-3 0 9149 2 25544 51.6430 356.9090 0001544 152.8370 207.2862 15.52483545 4130 Satellite: ISS Catalog Number: 25544 Epoch time: 19096.63682025 = yrday.fracday Element set: 914 Inclination: 51.6430 deg RA of node: 356.9090 deg Eccentricity: .0001544 Arg of perigee: 152.8370 deg Mean anomaly: 207.2862 deg Mean motion: 15.52483545 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 413 Checksum: 303 Coasting Arc #16 (Orbit 427) --------------------------------------- Vector Time (GMT): 2019/097/14:24:50.000 Vector Time (MET): N/A Weight (LBS) : 929253.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6489706.79 A = 6793778.61 meter Y = -1745950.76 meter E = .0009268 Z = -971752.95 I = 51.60600 XDOT = 2068.265942 Wp = 46.60290 YDOT = 4423.653763 meter/sec RA = 351.52148 deg ZDOT = 5906.277979 TA = 302.87634 MA = 302.96550 Ha = 223.887 n.mi Hp = 217.061 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21291688.95 X = 6513468.48 Y = -5728184.91 feet Y = -1673245.53 meter Z = -3188165.85 Z = -940170.15 XDOT = 6785.649417 XDOT = 1989.955883 YDOT = 14513.299747 feet/sec YDOT = 4446.345135 meter/sec ZDOT = 19377.552424 ZDOT = 5916.134440 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8997428.38 X = 2742416.17 Y = -20151573.68 feet Y = -6142199.66 meter Z = -3045140.89 Z = -928158.94 XDOT = 13991.809874 XDOT = 4264.703650 YDOT = 3333.962159 feet/sec YDOT = 1016.191666 meter/sec ZDOT = 19421.597959 ZDOT = 5919.703058 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19097.60237765 .00016717 00000-0 10270-3 0 9155 2 25544 51.6411 352.1075 0001508 159.1609 200.9604 15.52472372 4281 Satellite: ISS Catalog Number: 25544 Epoch time: 19097.60237765 = yrday.fracday Element set: 915 Inclination: 51.6411 deg RA of node: 352.1075 deg Eccentricity: .0001508 Arg of perigee: 159.1609 deg Mean anomaly: 200.9604 deg Mean motion: 15.52472372 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 428 Checksum: 300 Coasting Arc #17 (Orbit 431) --------------------------------------- Vector Time (GMT): 2019/097/20:12:00.000 Vector Time (MET): N/A Weight (LBS) : 929253.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2093883.89 A = 6782623.74 meter Y = -3832165.63 meter E = .0014569 Z = -5202496.83 I = 51.56076 XDOT = 7211.727331 Wp = 88.55297 YDOT = -2239.083018 meter/sec RA = 350.33725 deg ZDOT = -1255.930441 TA = 169.37157 MA = 169.34074 Ha = 223.939 n.mi Hp = 216.893 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6869697.79 X = -2025604.72 Y = -12572721.88 feet Y = -3855199.49 meter Z = -17068559.16 Z = -5212502.17 XDOT = 23660.522739 XDOT = 7242.330095 YDOT = -7346.072894 feet/sec YDOT = -2158.265411 meter/sec ZDOT = -4120.506695 ZDOT = -1220.823630 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -3411635.77 X = -1039866.58 Y = 13859866.07 feet Y = 4224487.18 meter Z = -17113347.10 Z = -5216148.20 XDOT = -21494.614454 XDOT = -6551.558485 YDOT = -10171.494605 feet/sec YDOT = -3100.271556 meter/sec ZDOT = -3961.490405 ZDOT = -1207.462275 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19097.85986093 .00016717 00000-0 10270-3 0 9168 2 25544 51.6408 350.8234 0002122 162.3810 197.7416 15.52486651 4326 Satellite: ISS Catalog Number: 25544 Epoch time: 19097.85986093 = yrday.fracday Element set: 916 Inclination: 51.6408 deg RA of node: 350.8234 deg Eccentricity: .0002122 Arg of perigee: 162.3810 deg Mean anomaly: 197.7416 deg Mean motion: 15.52486651 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 432 Checksum: 318 Coasting Arc #18 (Orbit 447) --------------------------------------- Vector Time (GMT): 2019/098/20:12:00.000 Vector Time (MET): N/A Weight (LBS) : 929253.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1008945.65 A = 6782096.32 meter Y = 4096065.51 meter E = .0003348 Z = 5307995.65 I = 51.52711 XDOT = -7429.708049 Wp = 121.89230 YDOT = 1898.050003 meter/sec RA = 345.34777 deg ZDOT = -54.149912 TA = 328.61450 MA = 328.63447 Ha = 223.796 n.mi Hp = 217.044 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 3310189.15 X = 937283.65 Y = 13438535.12 feet Y = 4106947.81 meter Z = 17414683.90 Z = 5312722.55 XDOT = -24375.682577 XDOT = -7450.117357 YDOT = 6227.198172 feet/sec YDOT = 1814.851690 meter/sec ZDOT = -177.657191 ZDOT = -90.290801 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 6426212.33 X = 1958709.52 Y = -12228144.43 feet Y = -3727138.42 meter Z = 17435569.18 Z = 5314361.49 XDOT = 21571.257441 XDOT = 6574.919268 YDOT = 10857.599596 feet/sec YDOT = 3309.396357 meter/sec ZDOT = -341.298128 ZDOT = -104.027669 The mean element set is posted at the UTC for which position is just north of the next ascending node relative to the above vector time TWO LINE MEAN ELEMENT SET ISS 1 25544U 98067A 19098.88978613 .00016717 00000-0 10270-3 0 9172 2 25544 51.6414 345.7012 0002042 168.5136 191.6062 15.52499215 4487 Satellite: ISS Catalog Number: 25544 Epoch time: 19098.88978613 = yrday.fracday Element set: 917 Inclination: 51.6414 deg RA of node: 345.7012 deg Eccentricity: .0002042 Arg of perigee: 168.5136 deg Mean anomaly: 191.6062 deg Mean motion: 15.52499215 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 448 Checksum: 323