ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 13747.6664 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 69.0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.995 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 ------------------------------------------------------------------------ 141/12:15:00.000 0.0 0.0 0.0 N/A 0.0 0.0 223.6 000/00:00:00.000 0.0 0.0 216.8 143/14:00:00.000 0.0 0.0 0.0 N/A 0.0 0.0 223.5 000/00:00:00.000 0.0 0.0 216.7 143/16:03:00.458 -2.1 7.1 7.1 N/A 6.7 -0.7 223.7 000/00:20:00.916 -1.1 -0.1 221.4 143/19:55:00.000 0.0 0.0 0.0 N/A 0.0 0.0 223.9 000/00:00:00.000 0.0 0.0 221.4 143/21:05:00.000 0.0 0.0 0.0 N/A 0.0 0.0 223.6 000/00:00:00.000 0.0 0.0 221.5 144/08:35:00.000 0.0 0.0 0.0 N/A 0.0 0.0 223.7 000/00:00:00.000 0.0 0.0 221.3 147/06:36:00.000 0.0 0.0 0.0 N/A 0.0 0.0 224.0 000/00:00:00.000 0.0 0.0 221.5 Coasting Arc #1 (Orbit 1094) --------------------------------------- Vector Time (GMT): 2019/140/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 965984.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4500860.51 A = 6793164.43 meter Y = -5009324.62 meter E = .0012689 Z = 851116.91 I = 51.91103 XDOT = 4053.927296 Wp = 118.48361 YDOT = 2620.125413 meter/sec RA = 137.62458 deg ZDOT = -5955.543086 TA = 52.34940 MA = 52.23434 Ha = 223.458 n.mi Hp = 216.777 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14766602.73 X = 4552407.38 Y = -16434792.05 feet Y = -4958704.74 meter Z = 2792378.33 Z = 873105.28 XDOT = 13300.286404 XDOT = 4053.256131 YDOT = 8596.211986 feet/sec YDOT = 2665.456271 meter/sec ZDOT = -19539.183353 ZDOT = -5935.851645 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -5739698.45 X = -1749460.09 Y = -21322330.31 feet Y = -6499046.28 meter Z = 2892475.45 Z = 881626.52 XDOT = 12972.015203 XDOT = 3953.870234 YDOT = -6156.774328 feet/sec YDOT = -1876.584815 meter/sec ZDOT = -19450.129954 ZDOT = -5928.399610 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 19140.53392535 .00016717 00000-0 10270-3 0 9007 2 25544 51.6365 138.5791 0001834 8.4894 351.6288 15.52697407 10955 Satellite: ISS Catalog Number: 25544 Epoch time: 19140.53392535 = yrday.fracday Element set: 900 Inclination: 51.6365 deg RA of node: 138.5791 deg Eccentricity: .0001834 Arg of perigee: 8.4894 deg Mean anomaly: 351.6288 deg Mean motion: 15.52697407 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1095 Checksum: 326 Coasting Arc #2 (Orbit 1110) --------------------------------------- Vector Time (GMT): 2019/141/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 965984.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4803182.47 A = 6793299.58 meter Y = 4779441.24 meter E = .0014039 Z = 371587.84 I = 51.93636 XDOT = -3100.514434 Wp = 45.39277 YDOT = -3594.228616 meter/sec RA = 132.68073 deg ZDOT = 6022.266602 TA = 318.59525 MA = 318.70157 Ha = 223.393 n.mi Hp = 216.699 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15758472.67 X = -4858075.55 Y = 15680581.48 feet Y = 4725421.71 meter Z = 1219120.22 Z = 348122.88 XDOT = -10172.291451 XDOT = -3089.345421 YDOT = -11792.088634 feet/sec YDOT = -3628.839115 meter/sec ZDOT = 19758.092525 ZDOT = 6007.231947 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 4926025.65 X = 1501452.62 Y = 21683942.41 feet Y = 6609265.65 meter Z = 1112323.44 Z = 339036.19 XDOT = -13880.449430 XDOT = -4230.760986 YDOT = 2119.264428 feet/sec YDOT = 645.951798 meter/sec ZDOT = 19690.228134 ZDOT = 6001.581535 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 19141.56370928 .00016717 00000-0 10270-3 0 9014 2 25544 51.6371 133.4571 0001596 14.1894 345.9302 15.52748083 11110 Satellite: ISS Catalog Number: 25544 Epoch time: 19141.56370928 = yrday.fracday Element set: 901 Inclination: 51.6371 deg RA of node: 133.4571 deg Eccentricity: .0001596 Arg of perigee: 14.1894 deg Mean anomaly: 345.9302 deg Mean motion: 15.52748083 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1111 Checksum: 298 Coasting Arc #3 (Orbit 1110) --------------------------------------- Vector Time (GMT): 2019/141/12:15:00.000 Vector Time (MET): N/A Weight (LBS) : 965984.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4858835.81 A = 6784172.57 meter Y = -192444.46 meter E = .0007591 Z = 4725139.10 I = 51.90514 XDOT = 2986.712128 Wp = 103.32391 YDOT = -6484.773787 meter/sec RA = 132.64618 deg ZDOT = 2801.631188 TA = 318.99139 MA = 319.04845 Ha = 223.616 n.mi Hp = 216.813 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15941062.36 X = -4879275.04 Y = -631379.48 feet Y = -246894.30 meter Z = 15502424.86 Z = 4701486.79 XDOT = 9798.924306 XDOT = 3045.395838 YDOT = -21275.504550 feet/sec YDOT = -6451.046545 meter/sec ZDOT = 9191.703372 ZDOT = 2816.281303 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8157917.96 X = -2486533.40 Y = 13830310.82 feet Y = 4215478.74 meter Z = 15395199.34 Z = 4692456.76 XDOT = -13112.239620 XDOT = -3996.610636 YDOT = -18060.795389 feet/sec YDOT = -5504.930434 meter/sec ZDOT = 9258.677333 ZDOT = 2822.044851 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 19141.56371164 .00016717 00000-0 10270-3 0 9028 2 25544 51.6367 133.4566 0001864 7.9665 352.1516 15.52692196 11113 Satellite: ISS Catalog Number: 25544 Epoch time: 19141.56371164 = yrday.fracday Element set: 902 Inclination: 51.6367 deg RA of node: 133.4566 deg Eccentricity: .0001864 Arg of perigee: 7.9665 deg Mean anomaly: 352.1516 deg Mean motion: 15.52692196 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1111 Checksum: 305 Coasting Arc #4 (Orbit 1125) --------------------------------------- Vector Time (GMT): 2019/142/12:15:00.000 Vector Time (MET): N/A Weight (LBS) : 965984.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4236752.40 A = 6782324.55 meter Y = 1156196.32 meter E = .0014611 Z = -5181437.96 I = 51.92056 XDOT = -3614.041682 Wp = 72.02377 YDOT = 6582.701869 meter/sec RA = 127.68285 deg ZDOT = -1485.300756 TA = 183.70065 MA = 183.71147 Ha = 223.554 n.mi Hp = 216.872 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13900106.30 X = 4248677.29 Y = 3793295.02 feet Y = 1203642.04 meter Z = -16999468.37 Z = -5160828.16 XDOT = -11857.092132 XDOT = -3680.167920 YDOT = 21596.790908 feet/sec YDOT = 6541.917594 meter/sec ZDOT = -4873.033975 ZDOT = -1503.016228 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9797042.54 X = 2986138.57 Y = -10713795.43 feet Y = -3265564.85 meter Z = -16906108.71 Z = -5152981.94 XDOT = 12986.862056 XDOT = 3958.395555 YDOT = 19697.734897 feet/sec YDOT = 6003.869597 meter/sec ZDOT = -4953.937591 ZDOT = -1509.960178 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 19142.52913523 .00016717 00000-0 10270-3 0 9037 2 25544 51.6366 128.6541 0001924 14.3169 345.8037 15.52684051 11263 Satellite: ISS Catalog Number: 25544 Epoch time: 19142.52913523 = yrday.fracday Element set: 903 Inclination: 51.6366 deg RA of node: 128.6541 deg Eccentricity: .0001924 Arg of perigee: 14.3169 deg Mean anomaly: 345.8037 deg Mean motion: 15.52684051 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1126 Checksum: 294 Coasting Arc #5 (Orbit 1141) --------------------------------------- Vector Time (GMT): 2019/143/12:15:00.000 Vector Time (MET): N/A Weight (LBS) : 965984.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3572820.65 A = 6781561.56 meter Y = -2170695.54 meter E = .0003313 Z = 5337197.83 I = 51.93770 XDOT = 4082.480168 Wp = 61.22622 YDOT = -6491.225209 meter/sec RA = 122.71873 deg ZDOT = 94.347157 TA = 27.88734 MA = 27.86959 Ha = 223.684 n.mi Hp = 216.736 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11721852.52 X = -3574206.98 Y = -7121704.54 feet Y = -2210657.76 meter Z = 17510491.57 Z = 5319838.71 XDOT = 13393.963807 XDOT = 4154.305194 YDOT = -21296.670634 feet/sec YDOT = -6445.170472 meter/sec ZDOT = 309.537916 ZDOT = 114.351987 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -11630753.22 X = -3545053.58 Y = 7455894.83 feet Y = 2272556.75 meter Z = 17431954.25 Z = 5313259.66 XDOT = -12609.944259 XDOT = -3843.511010 YDOT = -20596.298667 feet/sec YDOT = -6277.751834 meter/sec ZDOT = 400.837192 ZDOT = 122.175176 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 19143.55891967 .00016717 00000-0 10270-3 0 9049 2 25544 51.6367 123.5318 0001914 14.6109 345.5098 15.52683577 11420 Satellite: ISS Catalog Number: 25544 Epoch time: 19143.55891967 = yrday.fracday Element set: 904 Inclination: 51.6367 deg RA of node: 123.5318 deg Eccentricity: .0001914 Arg of perigee: 14.6109 deg Mean anomaly: 345.5098 deg Mean motion: 15.52683577 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1142 Checksum: 323 Coasting Arc #6 (Orbit 1142) --------------------------------------- Vector Time (GMT): 2019/143/14:00:00.000 Vector Time (MET): N/A Weight (LBS) : 965984.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 248497.31 A = 6787855.97 meter Y = -5718390.77 meter E = .0012603 Z = 3640692.14 I = 51.96183 XDOT = 5716.766923 Wp = 77.29918 YDOT = -2572.697332 meter/sec RA = 122.33159 deg ZDOT = -4415.561294 TA = 59.74527 MA = 59.62058 Ha = 223.525 n.mi Hp = 216.721 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 815279.88 X = 294739.01 Y = -18761124.58 feet Y = -5715353.81 meter Z = 11944528.03 Z = 3642010.83 XDOT = 18755.796993 XDOT = 5766.559073 YDOT = -8440.608044 feet/sec YDOT = -2508.489473 meter/sec ZDOT = -14486.749652 ZDOT = -4387.670701 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -18760412.11 X = -5718173.61 Y = -732428.65 feet Y = -223244.25 meter Z = 11951013.03 Z = 3642668.77 XDOT = -8497.721992 XDOT = -2590.105663 YDOT = -17483.304135 feet/sec YDOT = -5328.911100 meter/sec ZDOT = -14360.029835 ZDOT = -4376.937094 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 19143.62328100 .00016717 00000-0 10270-3 0 9052 2 25544 51.6382 123.2119 0002013 12.4497 347.6704 15.52703955 11431 Satellite: ISS Catalog Number: 25544 Epoch time: 19143.62328100 = yrday.fracday Element set: 905 Inclination: 51.6382 deg RA of node: 123.2119 deg Eccentricity: .0002013 Arg of perigee: 12.4497 deg Mean anomaly: 347.6704 deg Mean motion: 15.52703955 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1143 Checksum: 277 Coasting Arc #7 (Orbit 1143) --------------------------------------- Vector Time (GMT): 2019/143/16:13:00.916 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1824494.96 A = 6787897.58 meter Y = 4332542.99 meter E = .0006751 Z = -4902836.89 I = 51.94968 XDOT = -5309.323068 Wp = 118.82482 YDOT = 4964.296937 meter/sec RA = 121.87951 deg ZDOT = 2410.436080 TA = 174.73920 MA = 174.73210 Ha = 223.699 n.mi Hp = 221.420 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5985875.86 X = 1799726.94 Y = 14214379.89 feet Y = 4352807.90 meter Z = -16085422.87 Z = -4894033.76 XDOT = -17419.038936 XDOT = -5376.149237 YDOT = 16287.063443 feet/sec YDOT = 4904.550416 meter/sec ZDOT = 7908.254857 ZDOT = 2384.483636 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8522052.88 X = 2597521.72 Y = -12904436.41 feet Y = -3933272.22 meter Z = -16045880.15 Z = -4890784.27 XDOT = 22269.886252 XDOT = 6787.861330 YDOT = 5017.751921 feet/sec YDOT = 1529.410785 meter/sec ZDOT = 7790.112326 ZDOT = 2374.426237 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 19143.68764930 .00016717 00000-0 10270-3 0 9064 2 25544 51.6393 122.8904 0005473 273.0040 87.0485 15.51153202 11447 Satellite: ISS Catalog Number: 25544 Epoch time: 19143.68764930 = yrday.fracday Element set: 906 Inclination: 51.6393 deg RA of node: 122.8904 deg Eccentricity: .0005473 Arg of perigee: 273.0040 deg Mean anomaly: 87.0485 deg Mean motion: 15.51153202 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1144 Checksum: 295 Coasting Arc #8 (Orbit 1146) --------------------------------------- Vector Time (GMT): 2019/143/19:55:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4369236.85 A = 6786926.08 meter Y = -582957.98 meter E = .0002871 Z = 5162541.98 I = 51.94903 XDOT = 2780.025364 Wp = 212.60110 YDOT = -6966.374956 meter/sec RA = 121.14982 deg ZDOT = 1564.233289 TA = 222.36181 MA = 222.38398 Ha = 223.860 n.mi Hp = 221.429 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -14334766.56 X = -4387470.12 Y = -1912591.81 feet Y = -631920.44 meter Z = 16937473.68 Z = 5141273.46 XDOT = 9120.818124 XDOT = 2850.120548 YDOT = -22855.560878 feet/sec YDOT = -6934.895035 meter/sec ZDOT = 5131.998979 ZDOT = 1577.907017 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14412551.43 X = 4392945.68 Y = 2162986.65 feet Y = 659278.33 meter Z = 16841063.03 Z = 5133156.01 XDOT = -9325.458144 XDOT = -2842.399642 YDOT = 21642.375649 feet/sec YDOT = 6596.596098 meter/sec ZDOT = 5194.632485 ZDOT = 1583.323982 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 19143.88092548 .00016717 00000-0 10270-3 0 9076 2 25544 51.6395 121.9318 0005561 274.1616 85.8899 15.51130054 11475 Satellite: ISS Catalog Number: 25544 Epoch time: 19143.88092548 = yrday.fracday Element set: 907 Inclination: 51.6395 deg RA of node: 121.9318 deg Eccentricity: .0005561 Arg of perigee: 274.1616 deg Mean anomaly: 85.8899 deg Mean motion: 15.51130054 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1147 Checksum: 325 Coasting Arc #9 (Orbit 1146) --------------------------------------- Vector Time (GMT): 2019/143/21:05:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2557753.43 A = 6797337.67 meter Y = 6168582.92 meter E = .0007408 Z = -1242321.68 I = 51.98307 XDOT = -4852.634720 Wp = 358.63984 YDOT = -830.696371 meter/sec RA = 120.88349 deg ZDOT = 5872.614707 TA = 347.93618 MA = 347.95391 Ha = 223.602 n.mi Hp = 221.470 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -8391579.50 X = -2620507.67 Y = 20238132.93 feet Y = 6139629.60 meter Z = -4075858.53 Z = -1254897.96 XDOT = -15920.717585 XDOT = -4871.510929 YDOT = -2725.381795 feet/sec YDOT = -885.068203 meter/sec ZDOT = 19267.108618 ZDOT = 5848.996429 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 2253066.30 X = 686734.61 Y = -21781909.47 feet Y = -6639126.01 meter Z = -4133444.80 Z = -1259873.97 XDOT = 14572.319930 XDOT = 4441.643115 YDOT = -2124.605977 feet/sec YDOT = -647.579902 meter/sec ZDOT = 19160.062019 ZDOT = 5839.986903 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 19143.88092423 .00016717 00000-0 10270-3 0 9089 2 25544 51.6377 121.9301 0005735 273.0604 86.9891 15.51146889 11472 Satellite: ISS Catalog Number: 25544 Epoch time: 19143.88092423 = yrday.fracday Element set: 908 Inclination: 51.6377 deg RA of node: 121.9301 deg Eccentricity: .0005735 Arg of perigee: 273.0604 deg Mean anomaly: 86.9891 deg Mean motion: 15.51146889 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1147 Checksum: 325 Coasting Arc #10 (Orbit 1154) --------------------------------------- Vector Time (GMT): 2019/144/08:35:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 473009.66 A = 6793771.55 meter Y = -6005303.65 meter E = .0007607 Z = 3133964.14 I = 51.98066 XDOT = 5504.543490 Wp = 95.25027 YDOT = -2123.741273 meter/sec RA = 118.50448 deg ZDOT = -4890.804191 TA = 48.88700 MA = 48.82135 Ha = 223.733 n.mi Hp = 221.260 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 1551868.96 X = 524904.45 Y = -19702439.78 feet Y = -5999724.33 meter Z = 10282034.58 Z = 3136387.18 XDOT = 18059.525886 XDOT = 5551.639495 YDOT = -6967.655095 feet/sec YDOT = -2061.921706 meter/sec ZDOT = -16045.945507 ZDOT = -4863.951013 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -1796563.59 X = -547592.58 Y = -19675609.64 feet Y = -5997125.82 meter Z = 10293561.61 Z = 3137477.58 XDOT = 15328.978853 XDOT = 4672.272754 YDOT = -9746.817584 feet/sec YDOT = -2970.829999 meter/sec ZDOT = -15923.957411 ZDOT = -4853.622219 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 19144.39632949 .00016717 00000-0 10270-3 0 9090 2 25544 51.6389 119.3729 0005308 274.4884 85.5661 15.51174559 11555 Satellite: ISS Catalog Number: 25544 Epoch time: 19144.39632949 = yrday.fracday Element set: 909 Inclination: 51.6389 deg RA of node: 119.3729 deg Eccentricity: .0005308 Arg of perigee: 274.4884 deg Mean anomaly: 85.5661 deg Mean motion: 15.51174559 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1155 Checksum: 349 Coasting Arc #11 (Orbit 1169) --------------------------------------- Vector Time (GMT): 2019/145/08:35:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -588627.99 A = 6795186.99 meter Y = 6278896.08 meter E = .0004245 Z = -2522955.07 I = 52.00192 XDOT = -5257.143379 Wp = 344.50632 YDOT = 1646.229126 meter/sec RA = 113.56805 deg ZDOT = 5325.434171 TA = 347.37164 MA = 347.38227 Ha = 223.804 n.mi Hp = 221.219 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -1931194.18 X = -646541.53 Y = 20600052.74 feet Y = 6271990.07 meter Z = -8277411.64 Z = -2525954.41 XDOT = -17247.845732 XDOT = -5301.029271 YDOT = 5401.014192 feet/sec YDOT = 1587.194129 meter/sec ZDOT = 17471.896886 ZDOT = 5299.790507 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1912278.92 X = 582862.62 Y = 20596115.77 feet Y = 6277696.09 meter Z = -8291588.03 Z = -2527276.03 XDOT = -14586.490594 XDOT = -4445.962333 YDOT = 8338.732450 feet/sec YDOT = 2541.645651 meter/sec ZDOT = 17355.424078 ZDOT = 5289.933259 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 19145.36271214 .00016717 00000-0 10270-3 0 9104 2 25544 51.6403 114.5770 0005230 277.8952 82.1606 15.51188979 11702 Satellite: ISS Catalog Number: 25544 Epoch time: 19145.36271214 = yrday.fracday Element set: 910 Inclination: 51.6403 deg RA of node: 114.5770 deg Eccentricity: .0005230 Arg of perigee: 277.8952 deg Mean anomaly: 82.1606 deg Mean motion: 15.51188979 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1170 Checksum: 300 Coasting Arc #12 (Orbit 1185) --------------------------------------- Vector Time (GMT): 2019/146/08:35:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 666822.62 A = 6796505.42 meter Y = -6500669.76 meter E = .0008846 Z = 1850978.84 I = 52.01630 XDOT = 5040.549843 Wp = 120.20379 YDOT = -1100.910912 meter/sec RA = 108.63452 deg ZDOT = -5666.463367 TA = 39.56759 MA = 39.50305 Ha = 223.961 n.mi Hp = 221.236 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 2187738.25 X = 730474.37 Y = -21327656.70 feet Y = -6492857.15 meter Z = 6072765.22 Z = 1854372.02 XDOT = 16537.237019 XDOT = 5080.010479 YDOT = -3611.912441 feet/sec YDOT = -1044.322796 meter/sec ZDOT = -18590.759077 ZDOT = -5641.882494 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -2145389.23 X = -653914.64 Y = -21327398.43 feet Y = -6500591.04 meter Z = 6088759.94 Z = 1855854.03 XDOT = 14052.413107 XDOT = 4283.175515 YDOT = -6703.979585 feet/sec YDOT = -2043.372978 meter/sec ZDOT = -18479.146751 ZDOT = -5632.443930 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 19146.39351949 .00016717 00000-0 10270-3 0 9113 2 25544 51.6383 109.4616 0005230 282.9344 77.1222 15.51164269 11864 Satellite: ISS Catalog Number: 25544 Epoch time: 19146.39351949 = yrday.fracday Element set: 911 Inclination: 51.6383 deg RA of node: 109.4616 deg Eccentricity: .0005230 Arg of perigee: 282.9344 deg Mean anomaly: 77.1222 deg Mean motion: 15.51164269 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1186 Checksum: 311 Coasting Arc #13 (Orbit 1199) --------------------------------------- Vector Time (GMT): 2019/147/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4379436.64 A = 6788073.51 meter Y = -1773007.45 meter E = .0007678 Z = -4880897.46 I = 51.99803 XDOT = 170.432050 Wp = 50.37179 YDOT = 7243.823209 meter/sec RA = 104.13938 deg ZDOT = -2476.256033 TA = 195.38695 MA = 195.41030 Ha = 224.012 n.mi Hp = 221.458 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14368230.43 X = 4422646.17 Y = -5816953.58 feet Y = -1723791.52 meter Z = -16013443.13 Z = -4859518.94 XDOT = 559.160268 XDOT = 101.445194 YDOT = 23765.824176 feet/sec YDOT = 7245.343573 meter/sec ZDOT = -8124.199583 ZDOT = -2475.595099 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15551782.31 X = 4740183.25 Y = -1235796.70 feet Y = -376670.83 meter Z = -15916288.16 Z = -4851284.63 XDOT = -6592.643531 XDOT = -2009.437748 YDOT = 21732.555488 feet/sec YDOT = 6624.082913 meter/sec ZDOT = -8121.883167 ZDOT = -2475.549989 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 19147.29547563 .00016717 00000-0 10270-3 0 9123 2 25544 51.6395 104.9845 0005387 284.7476 75.3078 15.51149502 12009 Satellite: ISS Catalog Number: 25544 Epoch time: 19147.29547563 = yrday.fracday Element set: 912 Inclination: 51.6395 deg RA of node: 104.9845 deg Eccentricity: .0005387 Arg of perigee: 284.7476 deg Mean anomaly: 75.3078 deg Mean motion: 15.51149502 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1200 Checksum: 326 Coasting Arc #14 (Orbit 1215) --------------------------------------- Vector Time (GMT): 2019/148/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4263514.54 A = 6786942.71 meter Y = 1251006.02 meter E = .0001340 Z = 5131228.54 I = 52.00127 XDOT = -139.493795 Wp = 213.83379 YDOT = -7469.554743 meter/sec RA = 99.19658 deg ZDOT = 1704.322065 TA = 219.76711 MA = 219.77693 Ha = 224.355 n.mi Hp = 221.210 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13987908.59 X = -4302111.56 Y = 4104350.47 feet Y = 1203112.22 meter Z = 16834739.31 Z = 5110424.22 XDOT = -457.656807 XDOT = -64.235429 YDOT = -24506.413200 feet/sec YDOT = -7470.693993 meter/sec ZDOT = 5591.607824 ZDOT = 1703.826681 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -14686019.64 X = -4476298.79 Y = -34401.36 feet Y = -10485.54 meter Z = 16740232.10 Z = 5102422.75 XDOT = 6428.156244 XDOT = 1959.302023 YDOT = -22581.507392 feet/sec YDOT = -6882.843453 meter/sec ZDOT = 5590.078249 ZDOT = 1703.855850 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 19148.32627907 .00016717 00000-0 10270-3 0 9130 2 25544 51.6392 99.8685 0005328 290.4687 69.5892 15.51168711 12162 Satellite: ISS Catalog Number: 25544 Epoch time: 19148.32627907 = yrday.fracday Element set: 913 Inclination: 51.6392 deg RA of node: 99.8685 deg Eccentricity: .0005328 Arg of perigee: 290.4687 deg Mean anomaly: 69.5892 deg Mean motion: 15.51168711 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1216 Checksum: 346 Coasting Arc #15 (Orbit 1230) --------------------------------------- Vector Time (GMT): 2019/149/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4198735.35 A = 6786293.82 meter Y = -704242.01 meter E = .0010163 Z = -5293321.02 I = 52.00443 XDOT = 138.736936 Wp = 67.24988 YDOT = 7602.182680 meter/sec RA = 94.25352 deg ZDOT = -898.926529 TA = 194.16777 MA = 194.19630 Ha = 224.387 n.mi Hp = 221.385 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13775378.44 X = 4232010.55 Y = -2310505.28 feet Y = -657102.36 meter Z = -17366538.77 Z = -5272844.19 XDOT = 455.173674 XDOT = 58.083371 YDOT = 24941.544225 feet/sec YDOT = 7603.283238 meter/sec ZDOT = -2949.234020 ZDOT = -898.447916 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14007156.29 X = 4269381.24 Y = 1455904.29 feet Y = 443759.63 meter Z = -17273565.65 Z = -5264982.81 XDOT = -6051.648327 XDOT = -1844.542410 YDOT = 23152.483844 feet/sec YDOT = 7056.877076 meter/sec ZDOT = -2947.810046 ZDOT = -898.492502 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 19149.29265615 .00016717 00000-0 10270-3 0 9142 2 25544 51.6405 95.0728 0005419 293.9485 66.1098 15.51155316 12313 Satellite: ISS Catalog Number: 25544 Epoch time: 19149.29265615 = yrday.fracday Element set: 914 Inclination: 51.6405 deg RA of node: 95.0728 deg Eccentricity: .0005419 Arg of perigee: 293.9485 deg Mean anomaly: 66.1098 deg Mean motion: 15.51155316 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1231 Checksum: 319 Coasting Arc #16 (Orbit 1246) --------------------------------------- Vector Time (GMT): 2019/150/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4176904.02 A = 6785988.70 meter Y = 131730.06 meter E = .0003274 Z = 5348451.66 I = 52.00320 XDOT = -150.020235 Wp = 317.32036 YDOT = -7660.619016 meter/sec RA = 89.30972 deg ZDOT = 73.885548 TA = 131.99249 MA = 131.96460 Ha = 224.669 n.mi Hp = 221.057 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13703753.35 X = -4204046.74 Y = 432185.22 feet Y = 84868.78 meter Z = 17547413.59 Z = 5328095.68 XDOT = -492.192372 XDOT = -64.704756 YDOT = -25133.264488 feet/sec YDOT = -7661.819625 meter/sec ZDOT = 242.406655 ZDOT = 73.363381 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13494931.08 X = -4113254.99 Y = -3016567.85 feet Y = -919449.88 meter Z = 17455042.75 Z = 5320297.03 XDOT = 5550.556893 XDOT = 1691.809741 YDOT = -23482.748544 feet/sec YDOT = -7157.541756 meter/sec ZDOT = 240.809823 ZDOT = 73.398834 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 19150.32345772 .00016717 00000-0 10270-3 0 9152 2 25544 51.6387 89.9568 0005293 299.0226 61.0394 15.51166870 12473 Satellite: ISS Catalog Number: 25544 Epoch time: 19150.32345772 = yrday.fracday Element set: 915 Inclination: 51.6387 deg RA of node: 89.9568 deg Eccentricity: .0005293 Arg of perigee: 299.0226 deg Mean anomaly: 61.0394 deg Mean motion: 15.51166870 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1247 Checksum: 329 Coasting Arc #17 (Orbit 1261) --------------------------------------- Vector Time (GMT): 2019/151/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4211991.59 A = 6786219.11 meter Y = 428357.53 meter E = .0009894 Z = -5311903.35 I = 52.00345 XDOT = 164.697210 Wp = 81.75307 YDOT = 7618.327696 meter/sec RA = 84.36652 deg ZDOT = 747.510590 TA = 195.34837 MA = 195.37840 Ha = 224.736 n.mi Hp = 221.264 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 13818870.06 X = 4232691.18 Y = 1405372.47 feet Y = 475575.23 meter Z = -17427504.42 Z = -5291392.46 XDOT = 540.345176 XDOT = 75.863612 YDOT = 24994.513438 feet/sec YDOT = 7619.672682 meter/sec ZDOT = 2452.462565 ZDOT = 748.095628 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13229832.73 X = 4032453.02 Y = 4597961.09 feet Y = 1401458.54 meter Z = -17334486.77 Z = -5283551.57 XDOT = -4952.136484 XDOT = -1509.411200 YDOT = 23469.905875 feet/sec YDOT = 7153.627311 meter/sec ZDOT = 2454.328103 ZDOT = 748.079206 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 19151.28983241 .00016717 00000-0 10270-3 0 9168 2 25544 51.6399 85.1614 0005506 301.5440 58.5173 15.51151988 12627 Satellite: ISS Catalog Number: 25544 Epoch time: 19151.28983241 = yrday.fracday Element set: 916 Inclination: 51.6399 deg RA of node: 85.1614 deg Eccentricity: .0005506 Arg of perigee: 301.5440 deg Mean anomaly: 58.5173 deg Mean motion: 15.51151988 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1262 Checksum: 309 Coasting Arc #18 (Orbit 1277) --------------------------------------- Vector Time (GMT): 2019/152/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4290751.01 A = 6786773.97 meter Y = -992947.27 meter E = .0006067 Z = 5165441.08 I = 52.00080 XDOT = -156.170244 Wp = 356.27462 YDOT = -7498.935754 meter/sec RA = 79.42248 deg ZDOT = -1565.452856 TA = 108.78499 MA = 108.71916 Ha = 224.940 n.mi Hp = 220.908 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -14077267.09 X = -4304419.93 Y = -3257701.03 feet Y = -1041006.50 meter Z = 16946985.17 Z = 5144564.57 XDOT = -512.369568 XDOT = -64.699178 YDOT = -24602.807592 feet/sec YDOT = -7500.170525 meter/sec ZDOT = -5136.000184 ZDOT = -1565.990213 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13157600.93 X = -4010436.76 Y = -6233586.07 feet Y = -1899997.03 meter Z = 16852368.19 Z = 5136601.82 XDOT = 4372.438041 XDOT = 1332.719115 YDOT = -23170.263318 feet/sec YDOT = -7062.296259 meter/sec ZDOT = -5137.639938 ZDOT = -1565.952653 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 19152.32062961 .00016717 00000-0 10270-3 0 9172 2 25544 51.6395 80.0450 0005453 306.9611 53.1040 15.51176843 12783 Satellite: ISS Catalog Number: 25544 Epoch time: 19152.32062961 = yrday.fracday Element set: 917 Inclination: 51.6395 deg RA of node: 80.0450 deg Eccentricity: .0005453 Arg of perigee: 306.9611 deg Mean anomaly: 53.1040 deg Mean motion: 15.51176843 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1278 Checksum: 289 Coasting Arc #19 (Orbit 1292) --------------------------------------- Vector Time (GMT): 2019/153/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4419110.77 A = 6787855.94 meter Y = 1508046.03 meter E = .0007293 Z = -4932914.23 I = 51.99658 XDOT = 124.240695 Wp = 88.81715 YDOT = 7289.684857 meter/sec RA = 74.48059 deg ZDOT = 2342.968092 TA = 204.01313 MA = 204.04715 Ha = 225.141 n.mi Hp = 220.991 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 14498394.90 X = 4425880.66 Y = 4947657.58 feet Y = 1557502.17 meter Z = -16184101.80 Z = -4911430.85 XDOT = 407.613829 XDOT = 31.335111 YDOT = 23916.288902 feet/sec YDOT = 7290.554403 meter/sec ZDOT = 7686.903190 ZDOT = 2343.346998 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13335436.41 X = 4064641.02 Y = 7745276.05 feet Y = 2360760.14 meter Z = -16086788.25 Z = -4903253.06 XDOT = -3829.752963 XDOT = -1167.308703 YDOT = 22539.876482 feet/sec YDOT = 6870.154352 meter/sec ZDOT = 7687.824696 ZDOT = 2343.248967 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 19153.28700116 .00016717 00000-0 10270-3 0 9180 2 25544 51.6391 75.2500 0005546 310.9446 49.1224 15.51149356 12930 Satellite: ISS Catalog Number: 25544 Epoch time: 19153.28700116 = yrday.fracday Element set: 918 Inclination: 51.6391 deg RA of node: 75.2500 deg Eccentricity: .0005546 Arg of perigee: 310.9446 deg Mean anomaly: 49.1224 deg Mean motion: 15.51149356 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1293 Checksum: 294 Coasting Arc #20 (Orbit 1308) --------------------------------------- Vector Time (GMT): 2019/154/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 965071.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4579957.13 A = 6789102.19 meter Y = -2005540.15 meter E = .0008314 Z = 4593228.56 I = 51.99012 XDOT = -38.292148 Wp = 27.76727 YDOT = -7011.183352 meter/sec RA = 69.53844 deg ZDOT = -3090.069844 TA = 93.06808 MA = 92.97294 Ha = 225.191 n.mi Hp = 220.743 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -15026106.06 X = -4579501.87 Y = -6579856.13 feet Y = -2056754.63 meter Z = 15069647.49 Z = 4570981.31 XDOT = -125.630407 XDOT = 55.121795 YDOT = -23002.570051 feet/sec YDOT = -7011.088749 meter/sec ZDOT = -10138.024421 ZDOT = -3090.030105 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13682117.97 X = -4170309.56 Y = -9214313.67 feet Y = -2808522.81 meter Z = 14968925.05 Z = 4562528.35 XDOT = 3445.253022 XDOT = 1050.113121 YDOT = -21634.176094 feet/sec YDOT = -6594.096874 meter/sec ZDOT = -10137.056789 ZDOT = -3089.774909 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 19154.31779590 .00016717 00000-0 10270-3 0 9198 2 25544 51.6381 70.1342 0005660 314.0909 45.9775 15.51186402 13099 Satellite: ISS Catalog Number: 25544 Epoch time: 19154.31779590 = yrday.fracday Element set: 919 Inclination: 51.6381 deg RA of node: 70.1342 deg Eccentricity: .0005660 Arg of perigee: 314.0909 deg Mean anomaly: 45.9775 deg Mean motion: 15.51186402 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1309 Checksum: 311 Coasting Arc #21 (Orbit 1323) --------------------------------------- Vector Time (GMT): 2019/155/06:36:00.000 Vector Time (MET): N/A Weight (LBS) : 945394.7 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 4770745.97 A = 6790705.22 meter Y = 2424441.84 meter E = .0003922 Z = -4182238.44 I = 51.98325 XDOT = -91.893369 Wp = 63.76432 YDOT = 6669.824077 meter/sec RA = 64.59780 deg ZDOT = 3766.086696 TA = 244.82771 MA = 244.86840 Ha = 225.462 n.mi Hp = 220.681 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 15652053.70 X = 4763595.78 Y = 7954205.52 feet Y = 2477752.43 meter Z = -13721254.72 Z = -4159080.65 XDOT = -301.487431 XDOT = -184.764148 YDOT = 21882.624924 feet/sec YDOT = 6668.276518 meter/sec ZDOT = 12355.927480 ZDOT = 3765.415927 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 14220981.93 X = 4334555.29 Y = 10434795.67 feet Y = 3180525.72 meter Z = -13616450.12 Z = -4150294.00 XDOT = -3218.115338 XDOT = -980.881555 YDOT = 20485.108572 feet/sec YDOT = 6243.861093 meter/sec ZDOT = 12352.117519 ZDOT = 3764.925420 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 19155.28416503 .00016717 00000-0 10270-3 0 9209 2 25544 51.6388 65.3388 0005614 319.1622 40.9108 15.51156773 13249 Satellite: ISS Catalog Number: 25544 Epoch time: 19155.28416503 = yrday.fracday Element set: 920 Inclination: 51.6388 deg RA of node: 65.3388 deg Eccentricity: .0005614 Arg of perigee: 319.1622 deg Mean anomaly: 40.9108 deg Mean motion: 15.51156773 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1324 Checksum: 302