ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 17659.2714 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 69.6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.922 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 ------------------------------------------------------------------------ 016/05:25:00.000 0.0 0.0 0.0 N/A 0.0 0.0 220.8 000/00:00:00.000 0.0 0.0 216.2 018/18:05:10.698 3.0 3.2 3.2 N/A 0.8 0.0 220.9 000/00:08:17.397 -0.6 -0.0 218.0 020/01:03:00.000 0.0 0.0 0.0 N/A 0.0 0.0 221.0 000/00:00:00.000 0.0 0.0 217.9 025/12:55:30.000 0.0 0.0 0.0 N/A 0.0 0.0 221.6 000/00:00:00.000 0.0 0.0 217.5 026/08:59:00.000 0.0 0.0 0.0 N/A 0.0 0.0 221.8 000/00:00:00.000 0.0 0.0 217.4 Coasting Arc #1 (Orbit 3136) --------------------------------------- Vector Time (GMT): 2019/014/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 928709.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2829696.45 A = 6787626.57 meter Y = -5628335.52 meter E = .0003091 Z = -2524477.48 I = 51.92620 XDOT = 5505.483972 Wp = 146.58238 YDOT = -385.072906 meter/sec RA = 45.01300 deg ZDOT = -5318.198167 TA = 61.61581 MA = 61.58465 Ha = 220.719 n.mi Hp = 216.074 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -9283781.02 X = -2754286.09 Y = -18465667.70 feet Y = -5659557.42 meter Z = -8282406.43 Z = -2538040.02 XDOT = 18062.611458 XDOT = 5535.213467 YDOT = -1263.362551 feet/sec YDOT = -323.340344 meter/sec ZDOT = -17448.156715 ZDOT = -5291.382574 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13452162.09 X = 4100219.01 Y = -15658974.03 feet Y = -4772855.28 meter Z = -8342877.04 Z = -2542908.92 XDOT = 7063.413020 XDOT = 2152.928288 YDOT = 15289.851465 feet/sec YDOT = 4660.346727 meter/sec ZDOT = -17327.048985 ZDOT = -5281.284531 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 19014.52708432 .00016717 00000-0 10270-3 0 9003 2 25544 51.6422 45.5300 0002452 287.2155 72.8729 15.53770861 31374 Satellite: ISS Catalog Number: 25544 Epoch time: 19014.52708432 = yrday.fracday Element set: 900 Inclination: 51.6422 deg RA of node: 45.5300 deg Eccentricity: .0002452 Arg of perigee: 287.2155 deg Mean anomaly: 72.8729 deg Mean motion: 15.53770861 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3137 Checksum: 291 Coasting Arc #2 (Orbit 3152) --------------------------------------- Vector Time (GMT): 2019/015/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 928709.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1735385.68 A = 6784308.64 meter Y = 5345456.63 meter E = .0009272 Z = 3792576.05 I = 51.88865 XDOT = -6317.419207 Wp = 92.76245 YDOT = -964.724541 meter/sec RA = 40.05289 deg ZDOT = 4241.062848 TA = 312.54859 MA = 312.62682 Ha = 220.859 n.mi Hp = 216.036 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5693522.56 X = 1657060.17 Y = 17537587.36 feet Y = 5364424.80 meter Z = 12442834.81 Z = 3800815.88 XDOT = -20726.440969 XDOT = -6326.762490 YDOT = -3165.106762 feet/sec YDOT = -1035.422762 meter/sec ZDOT = 13914.248189 ZDOT = 4210.352606 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13789876.04 X = -4203154.22 Y = 12203015.80 feet Y = 3719479.22 meter Z = 12479304.14 Z = 3803691.90 XDOT = -4605.049008 XDOT = -1403.618938 YDOT = -19322.838392 feet/sec YDOT = -5889.601142 meter/sec ZDOT = 13775.747544 ZDOT = 4198.847851 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 19015.55616275 .00016717 00000-0 10270-3 0 9011 2 25544 51.6402 40.4028 0002312 294.1684 65.9227 15.53745097 31539 Satellite: ISS Catalog Number: 25544 Epoch time: 19015.55616275 = yrday.fracday Element set: 901 Inclination: 51.6402 deg RA of node: 40.4028 deg Eccentricity: .0002312 Arg of perigee: 294.1684 deg Mean anomaly: 65.9227 deg Mean motion: 15.53745097 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3153 Checksum: 294 Coasting Arc #3 (Orbit 3163) --------------------------------------- Vector Time (GMT): 2019/016/05:25:00.000 Vector Time (MET): N/A Weight (LBS) : 928709.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5936183.90 A = 6787015.53 meter Y = -1566921.04 meter E = .0010879 Z = 2881736.78 I = 51.87942 XDOT = -975.177622 Wp = 98.20537 YDOT = -5666.323504 meter/sec RA = 36.39803 deg ZDOT = -5074.986258 TA = 49.10465 MA = 49.01047 Ha = 220.802 n.mi Hp = 216.189 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19475668.98 X = -5932218.78 Y = -5140817.07 feet Y = -1633281.59 meter Z = 9454517.00 Z = 2852910.69 XDOT = -3199.401648 XDOT = -887.091372 YDOT = -18590.300210 feet/sec YDOT = -5676.735795 meter/sec ZDOT = -16650.217381 ZDOT = -5079.509679 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 20200160.38 X = 6157008.88 Y = -350365.99 feet Y = -106791.55 meter Z = 9324609.29 Z = 2842140.91 XDOT = 7988.070137 XDOT = 2434.763778 YDOT = 15584.615103 feet/sec YDOT = 4750.190683 meter/sec ZDOT = -16669.858994 ZDOT = -5080.973021 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 19016.26365308 .00016717 00000-0 10270-3 0 9029 2 25544 51.6410 36.8752 0002482 283.3022 76.7854 15.53747168 31644 Satellite: ISS Catalog Number: 25544 Epoch time: 19016.26365308 = yrday.fracday Element set: 902 Inclination: 51.6410 deg RA of node: 36.8752 deg Eccentricity: .0002482 Arg of perigee: 283.3022 deg Mean anomaly: 76.7854 deg Mean motion: 15.53747168 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3164 Checksum: 307 Coasting Arc #4 (Orbit 3178) --------------------------------------- Vector Time (GMT): 2019/017/05:25:00.000 Vector Time (MET): N/A Weight (LBS) : 928709.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6163261.66 A = 6789600.00 meter Y = 2448057.32 meter E = .0008332 Z = -1434397.95 I = 51.86204 XDOT = -624.072454 Wp = 20.10035 YDOT = 4964.754004 meter/sec RA = 31.44094 deg ZDOT = 5809.373304 TA = 324.30761 MA = 324.36329 Ha = 220.841 n.mi Hp = 216.138 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 20220674.74 X = 6142396.20 Y = 8031684.12 feet Y = 2516862.65 meter Z = -4706030.02 Z = -1404509.78 XDOT = -2047.481803 XDOT = -707.761897 YDOT = 16288.563005 feet/sec YDOT = 4957.306791 meter/sec ZDOT = 19059.623701 ZDOT = 5806.138942 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -21705992.01 X = -6615986.36 Y = -1866025.05 feet Y = -568764.43 meter Z = -4571456.75 Z = -1393380.02 XDOT = -2739.427061 XDOT = -834.977368 YDOT = -14644.144467 feet/sec YDOT = -4463.535234 meter/sec ZDOT = 19044.335112 ZDOT = 5804.713342 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 19017.22841008 .00016717 00000-0 10270-3 0 9033 2 25544 51.6423 32.0688 0002536 292.9444 67.1441 15.53751354 31792 Satellite: ISS Catalog Number: 25544 Epoch time: 19017.22841008 = yrday.fracday Element set: 903 Inclination: 51.6423 deg RA of node: 32.0688 deg Eccentricity: .0002536 Arg of perigee: 292.9444 deg Mean anomaly: 67.1441 deg Mean motion: 15.53751354 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3179 Checksum: 299 Coasting Arc #5 (Orbit 3194) --------------------------------------- Vector Time (GMT): 2019/018/05:25:00.000 Vector Time (MET): N/A Weight (LBS) : 928709.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6011679.70 A = 6790369.24 meter Y = -3142412.48 meter E = .0009430 Z = -167195.90 I = 51.83495 XDOT = 2322.870056 Wp = 141.26601 YDOT = -4133.385208 meter/sec RA = 26.48690 deg ZDOT = -6025.324510 TA = 40.52991 MA = 40.45972 Ha = 220.793 n.mi Hp = 216.078 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -19723358.59 X = -5975281.42 Y = -10309752.24 feet Y = -3209435.74 meter Z = -548542.98 Z = -196310.04 XDOT = 7620.964751 XDOT = 2398.185518 YDOT = -13560.975091 feet/sec YDOT = -4106.987556 meter/sec ZDOT = -19768.125034 ZDOT = -6013.858450 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21920578.10 X = 6681392.20 Y = 3824823.40 feet Y = 1165806.17 meter Z = -679519.52 Z = -207117.55 XDOT = -2982.363790 XDOT = -909.024483 YDOT = 13679.275511 feet/sec YDOT = 4169.443176 meter/sec ZDOT = -19715.790181 ZDOT = -6009.372847 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 19018.25748341 .00016717 00000-0 10270-3 0 9044 2 25544 51.6414 26.9420 0002471 294.9208 65.1687 15.53764139 31959 Satellite: ISS Catalog Number: 25544 Epoch time: 19018.25748341 = yrday.fracday Element set: 904 Inclination: 51.6414 deg RA of node: 26.9420 deg Eccentricity: .0002471 Arg of perigee: 294.9208 deg Mean anomaly: 65.1687 deg Mean motion: 15.53764139 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3195 Checksum: 317 Coasting Arc #6 (Orbit 3202) --------------------------------------- Vector Time (GMT): 2019/018/18:09:19.397 Vector Time (MET): N/A Weight (LBS) : 928366.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1978710.32 A = 6780178.40 meter Y = -3711628.21 meter E = .0010205 Z = -5326606.75 I = 51.77926 XDOT = 6910.898202 Wp = 86.86691 YDOT = 3291.485180 meter/sec RA = 23.84784 deg ZDOT = 274.698500 TA = 185.74362 MA = 185.75534 Ha = 220.947 n.mi Hp = 217.951 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 6491831.76 X = 2045941.14 Y = -12177257.90 feet Y = -3689124.43 meter Z = -17475743.95 Z = -5316832.12 XDOT = 22673.550533 XDOT = 6872.243943 YDOT = 10798.835894 feet/sec YDOT = 3368.551498 meter/sec ZDOT = 901.241799 ZDOT = 308.175143 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -198942.88 X = -60637.79 Y = -13854538.50 feet Y = -4222863.34 meter Z = -17431101.53 Z = -5312999.75 XDOT = 24041.484986 XDOT = 7327.844624 YDOT = -1664.524446 feet/sec YDOT = -507.347051 meter/sec ZDOT = 1051.886530 ZDOT = 320.615014 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 19018.77202257 .00016717 00000-0 10270-3 0 9053 2 25544 51.6414 24.3821 0004744 283.7239 76.3385 15.53170510 32034 Satellite: ISS Catalog Number: 25544 Epoch time: 19018.77202257 = yrday.fracday Element set: 905 Inclination: 51.6414 deg RA of node: 24.3821 deg Eccentricity: .0004744 Arg of perigee: 283.7239 deg Mean anomaly: 76.3385 deg Mean motion: 15.53170510 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3203 Checksum: 291 Coasting Arc #7 (Orbit 3218) --------------------------------------- Vector Time (GMT): 2019/019/18:09:19.397 Vector Time (MET): N/A Weight (LBS) : 928366.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3247629.22 A = 6781237.02 meter Y = 3116494.70 meter E = .0004618 Z = 5073430.95 I = 51.75198 XDOT = -6443.508778 Wp = 358.22806 YDOT = -3727.145510 meter/sec RA = 18.86814 deg ZDOT = -1830.686914 TA = 109.50062 MA = 109.45073 Ha = 221.058 n.mi Hp = 217.907 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -10654951.51 X = -3306880.86 Y = 10224720.15 feet Y = 3079845.62 meter Z = 16645114.67 Z = 5057511.87 XDOT = -21140.120663 XDOT = -6392.459589 YDOT = -12228.167683 feet/sec YDOT = -3798.915683 meter/sec ZDOT = -6006.190662 ZDOT = -1861.862946 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -4137512.10 X = -1261113.69 Y = 14260272.40 feet Y = 4346531.03 meter Z = 16572819.95 Z = 5051395.52 XDOT = -23347.045175 XDOT = -7116.179369 YDOT = 386.241740 feet/sec YDOT = 117.726482 meter/sec ZDOT = -6146.386608 ZDOT = -1873.418638 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 19019.80149679 .00016717 00000-0 10270-3 0 9067 2 25544 51.6413 19.2582 0004951 287.3682 72.6929 15.53193896 32194 Satellite: ISS Catalog Number: 25544 Epoch time: 19019.80149679 = yrday.fracday Element set: 906 Inclination: 51.6413 deg RA of node: 19.2582 deg Eccentricity: .0004951 Arg of perigee: 287.3682 deg Mean anomaly: 72.6929 deg Mean motion: 15.53193896 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3219 Checksum: 345 Coasting Arc #8 (Orbit 3222) --------------------------------------- Vector Time (GMT): 2019/020/01:03:00.000 Vector Time (MET): N/A Weight (LBS) : 928366.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1820716.88 A = 6780253.91 meter Y = -3816708.92 meter E = .0010188 Z = -5308756.95 I = 51.73723 XDOT = 7154.952543 Wp = 89.82382 YDOT = 2683.196869 meter/sec RA = 17.44620 deg ZDOT = 525.726351 TA = 185.18580 MA = 185.19636 Ha = 220.985 n.mi Hp = 217.886 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5973480.57 X = 1889047.58 Y = -12522010.91 feet Y = -3795965.79 meter Z = -17417181.61 Z = -5299747.20 XDOT = 23474.253749 XDOT = 7121.862876 YDOT = 8803.139334 feet/sec YDOT = 2763.023459 meter/sec ZDOT = 1724.823987 ZDOT = 560.401693 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13239044.54 X = -4035260.78 Y = 4317942.42 feet Y = 1316108.85 meter Z = -17375975.24 Z = -5296197.25 XDOT = -9649.252720 XDOT = -2941.092229 YDOT = -22027.834444 feet/sec YDOT = -6714.083939 meter/sec ZDOT = 1880.961847 ZDOT = 573.317171 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 19020.05886592 .00016717 00000-0 10270-3 0 9079 2 25544 51.6391 17.9724 0004596 283.7195 76.3446 15.53170504 32237 Satellite: ISS Catalog Number: 25544 Epoch time: 19020.05886592 = yrday.fracday Element set: 907 Inclination: 51.6391 deg RA of node: 17.9724 deg Eccentricity: .0004596 Arg of perigee: 283.7195 deg Mean anomaly: 76.3446 deg Mean motion: 15.53170504 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3223 Checksum: 320 Coasting Arc #9 (Orbit 3238) --------------------------------------- Vector Time (GMT): 2019/021/01:03:00.000 Vector Time (MET): N/A Weight (LBS) : 928366.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3133093.51 A = 6781742.52 meter Y = 3348126.14 meter E = .0004819 Z = 4997336.25 I = 51.70928 XDOT = -6675.471755 Wp = 10.30574 YDOT = -3149.235811 meter/sec RA = 12.46214 deg ZDOT = -2070.332732 TA = 99.84792 MA = 99.79350 Ha = 221.258 n.mi Hp = 217.835 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -10279178.18 X = -3194574.03 Y = 10984665.80 feet Y = 3312745.51 meter Z = 16395460.13 Z = 4981968.20 XDOT = -21901.154051 XDOT = -6629.703706 YDOT = -10332.138487 feet/sec YDOT = -3223.629498 meter/sec ZDOT = -6792.430223 ZDOT = -2102.647995 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15114072.59 X = 4606769.33 Y = -417587.45 feet Y = -127280.65 meter Z = 16325621.90 Z = 4976049.55 XDOT = 8110.038362 XDOT = 2471.939693 YDOT = 21660.760474 feet/sec YDOT = 6602.199792 meter/sec ZDOT = -6937.848359 ZDOT = -2114.656180 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 19021.08833941 .00016717 00000-0 10270-3 0 9084 2 25544 51.6386 12.8464 0004509 287.8517 72.2143 15.53130165 32398 Satellite: ISS Catalog Number: 25544 Epoch time: 19021.08833941 = yrday.fracday Element set: 908 Inclination: 51.6386 deg RA of node: 12.8464 deg Eccentricity: .0004509 Arg of perigee: 287.8517 deg Mean anomaly: 72.2143 deg Mean motion: 15.53130165 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3239 Checksum: 306 Coasting Arc #10 (Orbit 3253) --------------------------------------- Vector Time (GMT): 2019/022/01:03:00.000 Vector Time (MET): N/A Weight (LBS) : 928366.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4324456.33 A = 6784229.01 meter Y = -2900794.42 meter E = .0003976 Z = -4352625.85 I = 51.68592 XDOT = 5852.664258 Wp = 108.79321 YDOT = 3529.308393 meter/sec RA = 7.48243 deg ZDOT = 3464.030130 TA = 196.38349 MA = 196.39634 Ha = 221.253 n.mi Hp = 217.885 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14187848.84 X = 4377714.47 Y = -9517042.06 feet Y = -2852137.29 meter Z = -14280268.55 Z = -4331490.68 XDOT = 19201.654390 XDOT = 5795.937703 YDOT = 11579.095779 feet/sec YDOT = 3594.439579 meter/sec ZDOT = 11364.928249 ZDOT = 3492.321814 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -16884341.14 X = -5146347.18 Y = -3084659.83 feet Y = -940204.31 meter Z = -14184467.29 Z = -4323425.63 XDOT = -5926.114396 XDOT = -1806.279668 YDOT = -20387.472132 feet/sec YDOT = -6214.101506 meter/sec ZDOT = 11492.130727 ZDOT = 3502.801445 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 19022.05346789 .00016717 00000-0 10270-3 0 9092 2 25544 51.6394 8.0428 0004585 291.4174 68.6488 15.53161727 32544 Satellite: ISS Catalog Number: 25544 Epoch time: 19022.05346789 = yrday.fracday Element set: 909 Inclination: 51.6394 deg RA of node: 8.0428 deg Eccentricity: .0004585 Arg of perigee: 291.4174 deg Mean anomaly: 68.6488 deg Mean motion: 15.53161727 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3254 Checksum: 330 Coasting Arc #11 (Orbit 3269) --------------------------------------- Vector Time (GMT): 2019/023/01:03:00.000 Vector Time (MET): N/A Weight (LBS) : 928366.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -5338626.77 A = 6787398.38 meter Y = 2452548.81 meter E = .0008477 Z = 3393595.34 I = 51.66343 XDOT = -4728.357610 Wp = 78.08431 YDOT = -3871.168335 meter/sec RA = 2.50588 deg ZDOT = -4629.215342 TA = 62.29682 MA = 62.21084 Ha = 221.350 n.mi Hp = 217.803 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -17515179.68 X = -5382138.81 Y = 8046419.98 feet Y = 2392605.18 meter Z = 11133842.99 Z = 3367557.43 XDOT = -15512.984284 XDOT = -4662.232189 YDOT = -12700.683514 feet/sec YDOT = -3923.674269 meter/sec ZDOT = -15187.714378 ZDOT = -4652.022775 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 18347077.79 X = 5592189.31 Y = 6125494.48 feet Y = 1867050.72 meter Z = 11015984.17 Z = 3357671.97 XDOT = 3038.838668 XDOT = 926.238026 YDOT = 18464.125266 feet/sec YDOT = 5627.865381 meter/sec ZDOT = -15290.114605 ZDOT = -4660.426932 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 19023.08293871 .00016717 00000-0 10270-3 0 9101 2 25544 51.6395 2.9178 0004617 294.2978 65.7692 15.53151143 32703 Satellite: ISS Catalog Number: 25544 Epoch time: 19023.08293871 = yrday.fracday Element set: 910 Inclination: 51.6395 deg RA of node: 2.9178 deg Eccentricity: .0004617 Arg of perigee: 294.2978 deg Mean anomaly: 65.7692 deg Mean motion: 15.53151143 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3270 Checksum: 318 Coasting Arc #12 (Orbit 3284) --------------------------------------- Vector Time (GMT): 2019/024/01:03:00.000 Vector Time (MET): N/A Weight (LBS) : 928366.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6088239.54 A = 6790110.59 meter Y = -2017584.53 meter E = .0006900 Z = -2216023.52 I = 51.64120 XDOT = 3373.938490 Wp = .63998 YDOT = 4184.843322 meter/sec RA = 357.53442 deg ZDOT = 5466.265841 TA = 334.74862 MA = 334.78233 Ha = 221.514 n.mi Hp = 217.720 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 19974539.17 X = 6121112.18 Y = -6619371.80 feet Y = -1949317.78 meter Z = -7270418.37 Z = -2186370.08 XDOT = 11069.352000 XDOT = 3300.340257 YDOT = 13729.800925 feet/sec YDOT = 4222.161540 meter/sec ZDOT = 17933.943048 ZDOT = 5482.475985 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -19300214.19 X = -5882705.28 Y = -8498943.71 feet Y = -2590478.04 meter Z = -7136313.45 Z = -2175148.34 XDOT = 450.035474 XDOT = 137.170812 YDOT = -16122.151433 feet/sec YDOT = -4914.031757 meter/sec ZDOT = 18006.523706 ZDOT = 5488.388426 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 19024.04806487 .00016717 00000-0 10270-3 0 9112 2 25544 51.6412 358.1137 0004659 299.7091 60.3597 15.53169889 32853 Satellite: ISS Catalog Number: 25544 Epoch time: 19024.04806487 = yrday.fracday Element set: 911 Inclination: 51.6412 deg RA of node: 358.1137 deg Eccentricity: .0004659 Arg of perigee: 299.7091 deg Mean anomaly: 60.3597 deg Mean motion: 15.53169889 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3285 Checksum: 339 Coasting Arc #13 (Orbit 3300) --------------------------------------- Vector Time (GMT): 2019/025/01:03:00.000 Vector Time (MET): N/A Weight (LBS) : 928366.9 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6552033.19 A = 6791807.87 meter Y = 1546519.23 meter E = .0008710 Z = 865714.30 I = 51.61316 XDOT = -1848.950872 Wp = 127.16501 YDOT = -4494.801544 meter/sec RA = 352.56636 deg ZDOT = -5927.973487 TA = 43.47023 MA = 43.40160 Ha = 221.549 n.mi Hp = 217.631 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -21496171.88 X = -6573044.91 Y = 5073881.98 feet Y = 1473132.35 meter Z = 2840270.01 Z = 833836.64 XDOT = -6066.111785 XDOT = -1769.757163 YDOT = -14746.724226 feet/sec YDOT = -4515.035093 meter/sec ZDOT = -19448.731913 ZDOT = -5936.762384 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 19552596.24 X = 5959631.34 Y = 10311317.77 feet Y = 3142889.66 meter Z = 2696205.38 Z = 821803.40 XDOT = -4463.623998 XDOT = -1360.512595 YDOT = 13592.238051 feet/sec YDOT = 4142.914158 meter/sec ZDOT = -19487.779015 ZDOT = -5939.875044 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 19025.07753157 .00016717 00000-0 10270-3 0 9122 2 25544 51.6405 352.9896 0004656 303.5351 56.5356 15.53177678 33013 Satellite: ISS Catalog Number: 25544 Epoch time: 19025.07753157 = yrday.fracday Element set: 912 Inclination: 51.6405 deg RA of node: 352.9896 deg Eccentricity: .0004656 Arg of perigee: 303.5351 deg Mean anomaly: 56.5356 deg Mean motion: 15.53177678 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3301 Checksum: 319 Coasting Arc #14 (Orbit 3308) --------------------------------------- Vector Time (GMT): 2019/025/12:55:30.000 Vector Time (MET): N/A Weight (LBS) : 913933.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4060136.58 A = 6783115.20 meter Y = 2960978.54 meter E = .0003984 Z = 4552865.75 I = 51.56783 XDOT = -6055.953289 Wp = 94.17228 YDOT = 3544.102569 meter/sec RA = 350.13646 deg ZDOT = 3093.009432 TA = 324.82304 MA = 324.84933 Ha = 221.599 n.mi Hp = 217.517 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13320658.07 X = 4004609.48 Y = 9714496.52 feet Y = 3006071.43 meter Z = 14937223.60 Z = 4572453.06 XDOT = -19868.613152 XDOT = -6110.158171 YDOT = 11627.633100 feet/sec YDOT = 3476.077655 meter/sec ZDOT = 10147.668739 ZDOT = 3063.460765 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 3193825.03 X = 973477.87 Y = 16092689.00 feet Y = 4905051.61 meter Z = 15025207.66 Z = 4579683.29 XDOT = -21383.990261 XDOT = -6517.840231 YDOT = -5113.615911 feet/sec YDOT = -1558.630130 meter/sec ZDOT = 10013.848294 ZDOT = 3052.220960 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 19025.59226340 .00016717 00000-0 10270-3 0 9139 2 25544 51.6400 350.4317 0004980 309.1721 50.8988 15.53207744 33096 Satellite: ISS Catalog Number: 25544 Epoch time: 19025.59226340 = yrday.fracday Element set: 913 Inclination: 51.6400 deg RA of node: 350.4317 deg Eccentricity: .0004980 Arg of perigee: 309.1721 deg Mean anomaly: 50.8988 deg Mean motion: 15.53207744 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3309 Checksum: 299 Coasting Arc #15 (Orbit 3321) --------------------------------------- Vector Time (GMT): 2019/026/08:59:00.000 Vector Time (MET): N/A Weight (LBS) : 913933.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4592363.79 A = 6783957.71 meter Y = 2422975.74 meter E = .0005360 Z = 4361162.40 I = 51.54198 XDOT = -5452.809776 Wp = 87.45205 YDOT = 4165.489121 meter/sec RA = 345.97313 deg ZDOT = 3424.212794 TA = 327.76632 MA = 327.79906 Ha = 221.794 n.mi Hp = 217.436 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 15066810.34 X = 4543744.34 Y = 7949395.49 feet Y = 2474058.98 meter Z = 14308275.59 Z = 4383351.88 XDOT = -17889.795853 XDOT = -5515.616828 YDOT = 13666.302890 feet/sec YDOT = 4104.160880 meter/sec ZDOT = 11234.293943 ZDOT = 3397.572928 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -10606641.65 X = -3232904.38 Y = 13222522.19 feet Y = 4030224.76 meter Z = 14408069.70 Z = 4391579.64 XDOT = -9107.163589 XDOT = -2775.863462 YDOT = -19427.520206 feet/sec YDOT = -5921.508159 meter/sec ZDOT = 11113.525881 ZDOT = 3387.402689 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 19026.42870485 .00016717 00000-0 10270-3 0 9148 2 25544 51.6390 346.2679 0004860 313.5493 46.5255 15.53164039 33223 Satellite: ISS Catalog Number: 25544 Epoch time: 19026.42870485 = yrday.fracday Element set: 914 Inclination: 51.6390 deg RA of node: 346.2679 deg Eccentricity: .0004860 Arg of perigee: 313.5493 deg Mean anomaly: 46.5255 deg Mean motion: 15.53164039 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3322 Checksum: 315 Coasting Arc #16 (Orbit 3336) --------------------------------------- Vector Time (GMT): 2019/027/08:59:00.000 Vector Time (MET): N/A Weight (LBS) : 913933.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3453483.88 A = 6781419.20 meter Y = -3019730.07 meter E = .0011479 Z = -5004320.10 I = 51.50199 XDOT = 6298.732230 Wp = 53.15425 YDOT = -3863.732097 meter/sec RA = 340.98049 deg ZDOT = -2011.753922 TA = 197.21423 MA = 197.25319 Ha = 222.025 n.mi Hp = 217.151 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11330327.67 X = -3395151.87 Y = -9907250.89 feet Y = -3058023.21 meter Z = -16418373.03 Z = -5020953.90 XDOT = 20665.131989 XDOT = 6351.241285 YDOT = -12676.286408 feet/sec YDOT = -3793.001698 meter/sec ZDOT = -6600.242527 ZDOT = -1981.029916 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 11670180.98 X = 3557071.16 Y = -9374447.78 feet Y = -2857331.68 meter Z = -16493014.37 Z = -5027070.78 XDOT = 8291.698191 XDOT = 2527.309609 YDOT = 21709.967819 feet/sec YDOT = 6617.198191 meter/sec ZDOT = -6461.100172 ZDOT = -1969.343333 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 19027.39382636 .00016717 00000-0 10270-3 0 9152 2 25544 51.6394 341.4639 0004780 318.2479 41.8308 15.53175743 33374 Satellite: ISS Catalog Number: 25544 Epoch time: 19027.39382636 = yrday.fracday Element set: 915 Inclination: 51.6394 deg RA of node: 341.4639 deg Eccentricity: .0004780 Arg of perigee: 318.2479 deg Mean anomaly: 41.8308 deg Mean motion: 15.53175743 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3337 Checksum: 330 Coasting Arc #17 (Orbit 3352) --------------------------------------- Vector Time (GMT): 2019/028/08:59:00.000 Vector Time (MET): N/A Weight (LBS) : 913933.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2188289.78 A = 6780191.07 meter Y = 3635818.79 meter E = .0003094 Z = 5288322.67 I = 51.46553 XDOT = -6833.149168 Wp = 349.22462 YDOT = 3446.840031 meter/sec RA = 335.98074 deg ZDOT = 460.791105 TA = 96.38658 MA = 96.35134 Ha = 222.125 n.mi Hp = 217.208 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7179428.40 X = 2121782.98 Y = 11928539.34 feet Y = 3659917.87 meter Z = 17350139.99 Z = 5298790.92 XDOT = -22418.468399 XDOT = -6873.423092 YDOT = 11308.530287 feet/sec YDOT = 3370.201805 meter/sec ZDOT = 1511.781840 ZDOT = 427.500859 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -12869319.53 X = -3922568.59 Y = 5156625.93 feet Y = 1571739.58 meter Z = 17396879.73 Z = 5302568.94 XDOT = -7371.153172 XDOT = -2246.727487 YDOT = -22954.745743 feet/sec YDOT = -6996.606503 meter/sec ZDOT = 1361.129030 ZDOT = 414.872128 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 19028.42328729 .00016717 00000-0 10270-3 0 9161 2 25544 51.6382 336.3390 0004944 321.7154 38.3647 15.53171978 33530 Satellite: ISS Catalog Number: 25544 Epoch time: 19028.42328729 = yrday.fracday Element set: 916 Inclination: 51.6382 deg RA of node: 336.3390 deg Eccentricity: .0004944 Arg of perigee: 321.7154 deg Mean anomaly: 38.3647 deg Mean motion: 15.53171978 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3353 Checksum: 325 Coasting Arc #18 (Orbit 3367) --------------------------------------- Vector Time (GMT): 2019/029/08:59:00.000 Vector Time (MET): N/A Weight (LBS) : 913933.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -914478.66 A = 6780614.68 meter Y = -4247390.75 meter E = .0011339 Z = -5215137.31 I = 51.43666 XDOT = 7011.476078 Wp = 79.92519 YDOT = -2873.526272 meter/sec RA = 330.97857 deg ZDOT = 1114.847045 TA = 200.78033 MA = 200.82646 Ha = 222.289 n.mi Hp = 217.060 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3000258.08 X = -841583.27 Y = -13935009.03 feet Y = -4257209.39 meter Z = -17110030.54 Z = -5219402.49 XDOT = 23003.530441 XDOT = 7037.672318 YDOT = -9427.579631 feet/sec YDOT = -2794.972610 meter/sec ZDOT = 3657.634661 ZDOT = 1148.969283 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14199072.00 X = 4327877.15 Y = -965912.05 feet Y = -294409.99 meter Z = -17128705.10 Z = -5220829.32 XDOT = 6147.930116 XDOT = 1873.889099 YDOT = 23010.811451 feet/sec YDOT = 7013.695330 meter/sec ZDOT = 3811.954469 ZDOT = 1161.883722 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 19029.38840601 .00016717 00000-0 10270-3 0 9176 2 25544 51.6380 331.5353 0004968 325.4799 34.6030 15.53162305 33681 Satellite: ISS Catalog Number: 25544 Epoch time: 19029.38840601 = yrday.fracday Element set: 917 Inclination: 51.6380 deg RA of node: 331.5353 deg Eccentricity: .0004968 Arg of perigee: 325.4799 deg Mean anomaly: 34.6030 deg Mean motion: 15.53162305 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3368 Checksum: 311