ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 14262.1813 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 71.2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.940 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 ------------------------------------------------------------------------ 146/12:07:22.200 0.0 0.0 0.0 N/A -0.0 -0.0 228.5 000/00:12:03.600 0.0 0.0 222.2 148/20:33:33.000 0.0 0.0 0.0 N/A 0.0 0.0 228.5 000/00:00:00.000 0.0 0.0 222.2 149/04:45:00.000 0.0 0.0 0.0 N/A 0.0 0.0 228.6 000/00:00:00.000 0.0 0.0 222.2 149/15:39:55.000 0.0 0.0 0.0 N/A 0.0 0.0 228.5 000/00:00:00.000 0.0 0.0 222.2 152/12:36:00.000 0.0 0.0 0.0 N/A 0.0 0.0 228.7 000/00:00:00.000 0.0 0.0 222.0 160/04:50:00.000 0.0 0.0 0.0 N/A 0.0 0.0 229.1 000/00:00:00.000 0.0 0.0 221.7 Coasting Arc #1 (Orbit 2848) --------------------------------------- Vector Time (GMT): 2020/146/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 918884.5 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2889874.51 A = 6794559.08 meter Y = 4146263.08 meter E = .0008863 Z = -4549652.35 I = 52.01546 XDOT = -3558.870999 Wp = 100.43334 YDOT = 5977.020061 meter/sec RA = 99.78665 deg ZDOT = 3190.246072 TA = 201.47895 MA = 201.51616 Ha = 228.508 n.mi Hp = 222.348 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 9481215.58 X = 2865394.76 Y = 13603225.32 feet Y = 4178443.61 meter Z = -14926680.95 Z = -4535673.11 XDOT = -11676.085955 XDOT = -3640.939819 YDOT = 19609.645868 feet/sec YDOT = 5936.762816 meter/sec ZDOT = 10466.686589 ZDOT = 3172.760012 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16485077.08 X = 5024651.49 Y = -2256772.27 feet Y = -687864.19 meter Z = -14862577.33 Z = -4530113.57 XDOT = 11850.386685 XDOT = 3611.997862 YDOT = 18245.111353 feet/sec YDOT = 5561.109940 meter/sec ZDOT = 10385.912307 ZDOT = 3165.626071 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 20146.51043290 .00016717 00000-0 10270-3 0 9004 2 25544 51.6406 100.7144 0001800 349.1600 10.9511 15.49370393 28497 Satellite: ISS Catalog Number: 25544 Epoch time: 20146.51043290 = yrday.fracday Element set: 900 Inclination: 51.6406 deg RA of node: 100.7144 deg Eccentricity: .0001800 Arg of perigee: 349.1600 deg Mean anomaly: 10.9511 deg Mean motion: 15.49370393 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2849 Checksum: 265 Coasting Arc #2 (Orbit 2848) --------------------------------------- Vector Time (GMT): 2020/146/12:13:24.000 Vector Time (MET): N/A Weight (LBS) : 953907.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -701260.56 A = 6802998.96 meter Y = 6735841.02 meter E = .0011985 Z = -577568.87 I = 52.04380 XDOT = -4756.359817 Wp = 34.69622 YDOT = 13.772283 meter/sec RA = 99.75811 deg ZDOT = 6006.255110 TA = 319.11688 MA = 319.20671 Ha = 228.479 n.mi Hp = 222.228 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -2300723.61 X = -773725.09 Y = 22099215.96 feet Y = 6727593.95 meter Z = -1894911.00 Z = -581150.21 XDOT = -15604.855044 XDOT = -4785.335498 YDOT = 45.184656 feet/sec YDOT = -39.579749 meter/sec ZDOT = 19705.561386 ZDOT = 5983.080014 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 19256206.59 X = 5869291.77 Y = 11081655.95 feet Y = 3377688.73 meter Z = -1911745.70 Z = -582700.09 XDOT = -5553.452079 XDOT = -1692.692194 YDOT = 12991.496985 feet/sec YDOT = 3959.808281 meter/sec ZDOT = 19598.924930 ZDOT = 5973.752319 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 20146.51043288 .00016717 00000-0 10270-3 0 9012 2 25544 51.6406 100.7145 0001739 350.4977 9.6140 15.49388265 28491 Satellite: ISS Catalog Number: 25544 Epoch time: 20146.51043288 = yrday.fracday Element set: 901 Inclination: 51.6406 deg RA of node: 100.7145 deg Eccentricity: .0001739 Arg of perigee: 350.4977 deg Mean anomaly: 9.6140 deg Mean motion: 15.49388265 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2849 Checksum: 307 Coasting Arc #3 (Orbit 2864) --------------------------------------- Vector Time (GMT): 2020/147/12:13:24.000 Vector Time (MET): N/A Weight (LBS) : 953907.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 240217.86 A = 6803092.67 meter Y = -6780518.15 meter E = .0011549 Z = 426130.12 I = 52.04946 XDOT = 4730.741475 Wp = 124.45933 YDOT = -217.667071 meter/sec RA = 94.83664 deg ZDOT = -6020.727335 TA = 50.98127 MA = 50.87850 Ha = 228.508 n.mi Hp = 222.226 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 788116.33 X = 313951.87 Y = -22245794.47 feet Y = -6777419.67 meter Z = 1398064.69 Z = 427474.94 XDOT = 15520.805365 XDOT = 4762.069237 YDOT = -714.130811 feet/sec YDOT = -164.588367 meter/sec ZDOT = -19753.042439 ZDOT = -5997.671111 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20169169.59 X = -6147562.89 Y = -9417149.50 feet Y = -2870347.17 meter Z = 1404626.96 Z = 428130.30 XDOT = 4777.859810 XDOT = 1456.291670 YDOT = -13216.807430 feet/sec YDOT = -4028.482905 meter/sec ZDOT = -19646.932111 ZDOT = -5988.384907 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 20147.54241826 .00016717 00000-0 10270-3 0 9025 2 25544 51.6415 95.6070 0001774 352.3114 7.8008 15.49379051 28657 Satellite: ISS Catalog Number: 25544 Epoch time: 20147.54241826 = yrday.fracday Element set: 902 Inclination: 51.6415 deg RA of node: 95.6070 deg Eccentricity: .0001774 Arg of perigee: 352.3114 deg Mean anomaly: 7.8008 deg Mean motion: 15.49379051 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2865 Checksum: 296 Coasting Arc #4 (Orbit 2879) --------------------------------------- Vector Time (GMT): 2020/148/12:13:24.000 Vector Time (MET): N/A Weight (LBS) : 953907.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 251524.14 A = 6803096.90 meter Y = 6784787.01 meter E = .0012691 Z = -309656.41 I = 52.05143 XDOT = -4703.414238 Wp = 36.96813 YDOT = 443.375401 meter/sec RA = 89.91521 deg ZDOT = 6032.082295 TA = 319.71962 MA = 319.81358 Ha = 228.529 n.mi Hp = 222.181 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 825210.44 X = 177140.08 Y = 22259799.89 feet Y = 6787183.87 meter Z = -1015933.11 Z = -308614.18 XDOT = -15431.149076 XDOT = -4737.323010 YDOT = 1454.643705 feet/sec YDOT = 390.587913 meter/sec ZDOT = 19790.296244 ZDOT = 6009.152672 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 20945544.48 X = 6384201.96 Y = 7581079.66 feet Y = 2310713.08 meter Z = -1011524.16 Z = -308312.57 XDOT = -3938.345258 XDOT = -1200.407635 YDOT = 13447.015885 feet/sec YDOT = 4098.650442 meter/sec ZDOT = 19684.747180 ZDOT = 5999.910941 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 20148.50990252 .00016717 00000-0 10270-3 0 9037 2 25544 51.6417 90.8191 0001788 354.3512 5.7618 15.49390270 28806 Satellite: ISS Catalog Number: 25544 Epoch time: 20148.50990252 = yrday.fracday Element set: 903 Inclination: 51.6417 deg RA of node: 90.8191 deg Eccentricity: .0001788 Arg of perigee: 354.3512 deg Mean anomaly: 5.7618 deg Mean motion: 15.49390270 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2880 Checksum: 307 Coasting Arc #5 (Orbit 2885) --------------------------------------- Vector Time (GMT): 2020/148/20:33:33.000 Vector Time (MET): N/A Weight (LBS) : 953907.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3083515.96 A = 6797274.51 meter Y = -4746944.28 meter E = .0011636 Z = 3755767.29 I = 52.03018 XDOT = 3184.651135 Wp = 76.55949 YDOT = -5483.136797 meter/sec RA = 88.17932 deg ZDOT = -4301.754022 TA = 58.90773 MA = 58.79359 Ha = 228.524 n.mi Hp = 222.241 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -10116522.17 X = -3048448.38 Y = -15573964.18 feet Y = -4781230.86 meter Z = 12322071.15 Z = 3740873.23 XDOT = 10448.330497 XDOT = 3266.623933 YDOT = -17989.293953 feet/sec YDOT = -5447.064755 meter/sec ZDOT = -14113.366215 ZDOT = -4286.086011 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13518508.89 X = 4120441.51 Y = 12799223.14 feet Y = 3901203.21 meter Z = 12253800.35 Z = 3734958.35 XDOT = -5174.880094 XDOT = -1577.303453 YDOT = 18951.894138 feet/sec YDOT = 5776.537333 meter/sec ZDOT = -14040.942766 ZDOT = -4279.679355 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 20148.89689468 .00016717 00000-0 10270-3 0 9044 2 25544 51.6400 88.9000 0001552 350.3688 9.7432 15.49384063 28861 Satellite: ISS Catalog Number: 25544 Epoch time: 20148.89689468 = yrday.fracday Element set: 904 Inclination: 51.6400 deg RA of node: 88.9000 deg Eccentricity: .0001552 Arg of perigee: 350.3688 deg Mean anomaly: 9.7432 deg Mean motion: 15.49384063 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2886 Checksum: 329 Coasting Arc #6 (Orbit 2890) --------------------------------------- Vector Time (GMT): 2020/149/04:45:00.000 Vector Time (MET): N/A Weight (LBS) : 953907.1 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3424456.97 A = 6794135.53 meter Y = -3586466.27 meter E = .0010891 Z = -4655231.62 I = 52.02236 XDOT = 2731.266477 Wp = 62.15332 YDOT = 6490.755674 meter/sec RA = 86.54889 deg ZDOT = -2991.826359 TA = 178.10843 MA = 178.10431 Ha = 228.556 n.mi Hp = 222.235 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11235095.06 X = 3486919.79 Y = -11766621.63 feet Y = -3547821.61 meter Z = -15273069.62 Z = -4638445.81 XDOT = 8960.848023 XDOT = 2673.014472 YDOT = 21295.130164 feet/sec YDOT = 6520.973378 meter/sec ZDOT = -9815.703276 ZDOT = -2978.699479 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 16324519.36 X = 4975713.50 Y = -742272.37 feet Y = -226244.62 meter Z = -15195607.94 Z = -4631621.30 XDOT = -8148.749160 XDOT = -2483.738744 YDOT = 20475.963468 feet/sec YDOT = 6241.073665 meter/sec ZDOT = -9755.668588 ZDOT = -2973.527786 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 20149.21938957 .00016717 00000-0 10270-3 0 9052 2 25544 51.6431 87.3066 0001595 359.6128 .5021 15.49383675 28915 Satellite: ISS Catalog Number: 25544 Epoch time: 20149.21938957 = yrday.fracday Element set: 905 Inclination: 51.6431 deg RA of node: 87.3066 deg Eccentricity: .0001595 Arg of perigee: 359.6128 deg Mean anomaly: .5021 deg Mean motion: 15.49383675 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2891 Checksum: 321 Coasting Arc #7 (Orbit 2897) --------------------------------------- Vector Time (GMT): 2020/149/15:39:55.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3952090.34 A = 6791572.19 meter Y = -1734265.44 meter E = .0014449 Z = -5256571.32 I = 52.01410 XDOT = 1662.795802 Wp = 73.23091 YDOT = 7373.070355 meter/sec RA = 84.29978 deg ZDOT = -1181.030567 TA = 185.46516 MA = 185.48094 Ha = 228.516 n.mi Hp = 222.244 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12966175.67 X = 3996723.02 Y = -5689847.24 feet Y = -1689820.06 meter Z = -17245968.90 Z = -5237265.51 XDOT = 5455.366804 XDOT = 1585.961111 YDOT = 24189.863369 feet/sec YDOT = 7391.235476 meter/sec ZDOT = -3874.772201 ZDOT = -1173.138962 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -11575416.21 X = -3528186.86 Y = -8340630.30 feet Y = -2542224.11 meter Z = -17157014.37 Z = -5229457.98 XDOT = 17387.365052 XDOT = 5299.668868 YDOT = -16224.786995 feet/sec YDOT = -4945.315076 meter/sec ZDOT = -3838.887915 ZDOT = -1170.093037 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 20149.67088053 .00016717 00000-0 10270-3 0 9066 2 25544 51.6442 85.0740 0001957 356.7746 3.3392 15.49414510 28989 Satellite: ISS Catalog Number: 25544 Epoch time: 20149.67088053 = yrday.fracday Element set: 906 Inclination: 51.6442 deg RA of node: 85.0740 deg Eccentricity: .0001957 Arg of perigee: 356.7746 deg Mean anomaly: 3.3392 deg Mean motion: 15.49414510 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2898 Checksum: 319 Coasting Arc #8 (Orbit 2913) --------------------------------------- Vector Time (GMT): 2020/150/15:39:55.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3833331.39 A = 6791512.11 meter Y = 1899084.64 meter E = .0003154 Z = 5272106.00 I = 52.00853 XDOT = -2183.876654 Wp = 90.85231 YDOT = -7272.857605 meter/sec RA = 79.37532 deg ZDOT = 1031.315979 TA = 349.31227 MA = 349.31897 Ha = 228.761 n.mi Hp = 222.074 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12576546.55 X = -3879891.42 Y = 6230592.64 feet Y = 1855956.64 meter Z = 17296935.71 Z = 5253372.37 XDOT = -7164.949653 XDOT = -2107.396620 YDOT = -23861.081382 feet/sec YDOT = -7296.851764 meter/sec ZDOT = 3383.582607 ZDOT = 1020.892477 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 11972657.45 X = 3649265.99 Y = 7524927.84 feet Y = 2293598.01 meter Z = 17210599.27 Z = 5245790.66 XDOT = -15974.229044 XDOT = -4868.945013 YDOT = 17781.672720 feet/sec YDOT = 5419.853845 meter/sec ZDOT = 3336.050235 ZDOT = 1016.828112 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 20150.70286133 .00016717 00000-0 10270-3 0 9072 2 25544 51.6435 79.9662 0001894 2.3710 357.7449 15.49392457 29144 Satellite: ISS Catalog Number: 25544 Epoch time: 20150.70286133 = yrday.fracday Element set: 907 Inclination: 51.6435 deg RA of node: 79.9662 deg Eccentricity: .0001894 Arg of perigee: 2.3710 deg Mean anomaly: 357.7449 deg Mean motion: 15.49392457 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2914 Checksum: 320 Coasting Arc #9 (Orbit 2928) --------------------------------------- Vector Time (GMT): 2020/151/15:39:55.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3725093.87 A = 6791367.59 meter Y = -2065957.70 meter E = .0014870 Z = -5302329.77 I = 52.00036 XDOT = 2689.744462 Wp = 75.69881 YDOT = 7107.262304 meter/sec RA = 74.45019 deg ZDOT = -878.060369 TA = 185.91686 MA = 185.93444 Ha = 228.581 n.mi Hp = 222.174 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12221436.60 X = 3773674.85 Y = -6778076.44 feet Y = -2024028.87 meter Z = -17396095.05 Z = -5284116.94 XDOT = 8824.620939 XDOT = 2614.334151 YDOT = 23317.789711 feet/sec YDOT = 7136.919385 meter/sec ZDOT = -2880.775488 ZDOT = -865.177081 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -12369678.90 X = -3770278.13 Y = -6723894.36 feet Y = -2049443.00 meter Z = -17312141.52 Z = -5276740.74 XDOT = 14357.603851 XDOT = 4376.197654 YDOT = -19134.660074 feet/sec YDOT = -5832.244391 meter/sec ZDOT = -2821.923849 ZDOT = -860.122389 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 20151.67034205 .00016717 00000-0 10270-3 0 9081 2 25544 51.6430 75.1776 0001969 1.9303 358.1854 15.49413342 29297 Satellite: ISS Catalog Number: 25544 Epoch time: 20151.67034205 = yrday.fracday Element set: 908 Inclination: 51.6430 deg RA of node: 75.1776 deg Eccentricity: .0001969 Arg of perigee: 1.9303 deg Mean anomaly: 358.1854 deg Mean motion: 15.49413342 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2929 Checksum: 302 Coasting Arc #10 (Orbit 2942) --------------------------------------- Vector Time (GMT): 2020/152/12:36:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3942327.12 A = 6791047.42 meter Y = 1391871.96 meter E = .0003231 Z = 5349372.14 I = 51.99118 XDOT = -2583.917138 Wp = 51.65637 YDOT = -7214.389109 meter/sec RA = 70.14733 deg ZDOT = -25.172616 TA = 38.59405 MA = 38.57096 Ha = 228.716 n.mi Hp = 221.987 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12934144.10 X = -3983582.72 Y = 4566509.06 feet Y = 1347554.88 meter Z = 17550433.52 Z = 5330121.72 XDOT = -8477.418432 XDOT = -2502.929379 YDOT = -23669.255606 feet/sec YDOT = -7242.831477 meter/sec ZDOT = -82.587323 ZDOT = -37.528286 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 1650666.96 X = 503123.29 Y = 13730460.88 feet Y = 4185044.48 meter Z = 17461745.26 Z = 5322339.96 XDOT = -23937.793464 XDOT = -7296.239448 YDOT = 3062.766006 feet/sec YDOT = 933.531079 meter/sec ZDOT = -138.991037 ZDOT = -42.364468 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 20152.57332332 .00016717 00000-0 10270-3 0 9094 2 25544 51.6434 70.7082 0001915 3.9610 356.1555 15.49434558 29430 Satellite: ISS Catalog Number: 25544 Epoch time: 20152.57332332 = yrday.fracday Element set: 909 Inclination: 51.6434 deg RA of node: 70.7082 deg Eccentricity: .0001915 Arg of perigee: 3.9610 deg Mean anomaly: 356.1555 deg Mean motion: 15.49434558 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2943 Checksum: 298 Coasting Arc #11 (Orbit 2957) --------------------------------------- Vector Time (GMT): 2020/153/12:36:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3885946.87 A = 6791126.99 meter Y = -1572988.27 meter E = .0015324 Z = -5355806.04 I = 51.97990 XDOT = 3077.685885 Wp = 83.84458 YDOT = 7000.873640 meter/sec RA = 65.22082 deg ZDOT = 178.933036 TA = 187.84489 MA = 187.86889 Ha = 228.711 n.mi Hp = 222.038 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12749169.53 X = 3929263.33 Y = -5160722.67 feet Y = -1529290.13 meter Z = -17571542.11 Z = -5336824.42 XDOT = 10097.394637 XDOT = 2998.302135 YDOT = 22968.745538 feet/sec YDOT = 7034.846636 meter/sec ZDOT = 587.050644 ZDOT = 193.691209 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -2505678.05 X = -763730.67 Y = -13636790.95 feet Y = -4156493.88 meter Z = -17484078.02 Z = -5329146.98 XDOT = 23520.373777 XDOT = 7169.009927 YDOT = -5152.285385 feet/sec YDOT = -1570.416585 meter/sec ZDOT = 654.508009 ZDOT = 199.494041 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 20153.54080201 .00016717 00000-0 10270-3 0 9109 2 25544 51.6446 65.9195 0002034 12.2919 347.8281 15.49415880 29588 Satellite: ISS Catalog Number: 25544 Epoch time: 20153.54080201 = yrday.fracday Element set: 910 Inclination: 51.6446 deg RA of node: 65.9195 deg Eccentricity: .0002034 Arg of perigee: 12.2919 deg Mean anomaly: 347.8281 deg Mean motion: 15.49415880 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2958 Checksum: 301 Coasting Arc #12 (Orbit 2973) --------------------------------------- Vector Time (GMT): 2020/154/12:36:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3817524.40 A = 6791078.99 meter Y = 1736794.88 meter E = .0003967 Z = 5338849.60 I = 51.96452 XDOT = -3561.240704 Wp = 47.38391 YDOT = -6777.156614 meter/sec RA = 60.29411 deg ZDOT = -338.984404 TA = 45.85191 MA = 45.81929 Ha = 228.816 n.mi Hp = 221.868 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12524686.34 X = -3862595.40 Y = 5698145.94 feet Y = 1693852.01 meter Z = 17515910.77 Z = 5320196.06 XDOT = -11683.860576 XDOT = -3483.545234 YDOT = -22234.765795 feet/sec YDOT = -6816.546483 meter/sec ZDOT = -1112.153556 ZDOT = -356.095762 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 3309189.57 X = 1008640.98 Y = 13468113.97 feet Y = 4105081.14 meter Z = 17429943.65 Z = 5312646.82 XDOT = -23002.860688 XDOT = -7011.271938 YDOT = 7204.381325 feet/sec YDOT = 2195.895428 meter/sec ZDOT = -1190.436204 ZDOT = -362.844955 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 20154.57277630 .00016717 00000-0 10270-3 0 9118 2 25544 51.6443 60.8122 0001995 12.6931 347.4269 15.49438452 29742 Satellite: ISS Catalog Number: 25544 Epoch time: 20154.57277630 = yrday.fracday Element set: 911 Inclination: 51.6443 deg RA of node: 60.8122 deg Eccentricity: .0001995 Arg of perigee: 12.6931 deg Mean anomaly: 347.4269 deg Mean motion: 15.49438452 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2974 Checksum: 314 Coasting Arc #13 (Orbit 2988) --------------------------------------- Vector Time (GMT): 2020/155/12:36:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3752880.36 A = 6791189.45 meter Y = -1918724.59 meter E = .0015220 Z = -5337941.63 I = 51.94747 XDOT = 4016.024688 Wp = 86.26773 YDOT = 6492.048964 meter/sec RA = 55.36645 deg ZDOT = 492.099615 TA = 188.40545 MA = 188.43097 Ha = 228.735 n.mi Hp = 221.989 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12312599.60 X = 3799986.21 Y = -6295028.17 feet Y = -1876493.10 meter Z = -17512931.84 Z = -5319597.19 XDOT = 13175.934017 XDOT = 3940.739817 YDOT = 21299.373240 feet/sec YDOT = 6536.538000 meter/sec ZDOT = 1614.500048 ZDOT = 511.426182 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -4164024.01 X = -1269194.52 Y = -13298234.84 feet Y = -4053301.98 meter Z = -17428371.24 Z = -5312167.56 XDOT = 22206.027415 XDOT = 6768.397156 YDOT = -9175.786450 feet/sec YDOT = -2796.779710 meter/sec ZDOT = 1702.977018 ZDOT = 519.067395 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 20155.54025356 .00016717 00000-0 10270-3 0 9123 2 25544 51.6448 56.0244 0002017 15.3179 344.8032 15.49420344 29895 Satellite: ISS Catalog Number: 25544 Epoch time: 20155.54025356 = yrday.fracday Element set: 912 Inclination: 51.6448 deg RA of node: 56.0244 deg Eccentricity: .0002017 Arg of perigee: 15.3179 deg Mean anomaly: 344.8032 deg Mean motion: 15.49420344 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2989 Checksum: 292 Coasting Arc #14 (Orbit 3004) --------------------------------------- Vector Time (GMT): 2020/156/12:36:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3679011.95 A = 6791177.98 meter Y = 2080987.82 meter E = .0004608 Z = 5313011.36 I = 51.92842 XDOT = -4456.970395 Wp = 44.58426 YDOT = -6199.559359 meter/sec RA = 50.43717 deg ZDOT = -654.476607 TA = 51.66437 MA = 51.62297 Ha = 228.833 n.mi Hp = 221.825 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -12070249.18 X = -3727816.65 Y = 6827387.87 feet Y = 2039572.75 meter Z = 17431139.63 Z = 5295021.72 XDOT = -14622.606284 XDOT = -4384.134714 YDOT = -20339.761677 feet/sec YDOT = -6248.993018 meter/sec ZDOT = -2147.232961 ZDOT = -675.951216 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 4954534.95 X = 1510142.25 Y = 13062981.02 feet Y = 3981596.61 meter Z = 17348195.29 Z = 5287729.92 XDOT = -21320.609679 XDOT = -6498.521830 YDOT = 11084.232419 feet/sec YDOT = 3378.474041 meter/sec ZDOT = -2245.597850 ZDOT = -684.458225 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 20156.57222510 .00016717 00000-0 10270-3 0 9139 2 25544 51.6456 50.9169 0001990 15.7573 344.3639 15.49442796 30057 Satellite: ISS Catalog Number: 25544 Epoch time: 20156.57222510 = yrday.fracday Element set: 913 Inclination: 51.6456 deg RA of node: 50.9169 deg Eccentricity: .0001990 Arg of perigee: 15.7573 deg Mean anomaly: 344.3639 deg Mean motion: 15.49442796 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3005 Checksum: 310 Coasting Arc #15 (Orbit 3019) --------------------------------------- Vector Time (GMT): 2020/157/12:36:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3605128.07 A = 6791315.14 meter Y = -2264003.83 meter E = .0015131 Z = -5304440.68 I = 51.90597 XDOT = 4860.536062 Wp = 88.27934 YDOT = 5851.447704 meter/sec RA = 45.50628 deg ZDOT = 808.391358 TA = 189.42330 MA = 189.45172 Ha = 228.808 n.mi Hp = 221.889 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11827847.99 X = 3655943.08 Y = -7427834.07 feet Y = -2223403.60 meter Z = -17403020.60 Z = -5286805.20 XDOT = 15946.640624 XDOT = 4790.815448 YDOT = 19197.663071 feet/sec YDOT = 5905.411694 meter/sec ZDOT = 2652.202618 ZDOT = 831.833936 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -5805483.09 X = -1769511.24 Y = -12813717.94 feet Y = -3905621.23 meter Z = -17321686.74 Z = -5279650.12 XDOT = 20178.737011 XDOT = 6150.479041 YDOT = -12861.988900 feet/sec YDOT = -3920.334217 meter/sec ZDOT = 2759.635004 ZDOT = 841.136749 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 20157.53969837 .00016717 00000-0 10270-3 0 9147 2 25544 51.6453 46.1285 0002133 20.6040 339.5196 15.49426741 30207 Satellite: ISS Catalog Number: 25544 Epoch time: 20157.53969837 = yrday.fracday Element set: 914 Inclination: 51.6453 deg RA of node: 46.1285 deg Eccentricity: .0002133 Arg of perigee: 20.6040 deg Mean anomaly: 339.5196 deg Mean motion: 15.49426741 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3020 Checksum: 298 Coasting Arc #16 (Orbit 3035) --------------------------------------- Vector Time (GMT): 2020/158/12:36:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -3524345.89 A = 6791375.54 meter Y = 2426894.50 meter E = .0005472 Z = 5270911.24 I = 51.88111 XDOT = -5248.194455 Wp = 44.97962 YDOT = -5499.066676 meter/sec RA = 40.57412 deg ZDOT = -972.825434 TA = 54.33134 MA = 54.28041 Ha = 228.933 n.mi Hp = 221.729 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -11562814.60 X = -3576825.40 Y = 7962252.28 feet Y = 2387188.25 meter Z = 17293015.87 Z = 5253664.28 XDOT = -17218.485745 XDOT = -5181.586749 YDOT = -18041.557336 feet/sec YDOT = -5557.383097 meter/sec ZDOT = -3191.684495 ZDOT = -998.158578 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 6586160.78 X = 2007461.81 Y = 12508561.02 feet Y = 3812609.40 meter Z = 17213451.95 Z = 5246660.16 XDOT = -18964.656344 XDOT = -5780.427254 YDOT = 14557.420570 feet/sec YDOT = 4437.101790 meter/sec ZDOT = -3307.833379 ZDOT = -1008.227614 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 20158.57166748 .00016717 00000-0 10270-3 0 9153 2 25544 51.6445 41.0211 0002083 23.3917 336.7327 15.49437661 30363 Satellite: ISS Catalog Number: 25544 Epoch time: 20158.57166748 = yrday.fracday Element set: 915 Inclination: 51.6445 deg RA of node: 41.0211 deg Eccentricity: .0002083 Arg of perigee: 23.3917 deg Mean anomaly: 336.7327 deg Mean motion: 15.49437661 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3036 Checksum: 300 Coasting Arc #17 (Orbit 3050) --------------------------------------- Vector Time (GMT): 2020/159/12:36:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3437294.31 A = 6791528.11 meter Y = -2613757.43 meter E = .0014880 Z = -5254844.43 I = 51.85456 XDOT = 5592.244878 Wp = 90.72103 YDOT = 5097.019119 meter/sec RA = 35.63977 deg ZDOT = 1125.312688 TA = 190.04471 MA = 190.07448 Ha = 228.854 n.mi Hp = 221.822 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 11277212.31 X = 3491791.67 Y = -8575319.64 feet Y = -2575013.36 meter Z = -17240303.25 Z = -5238015.58 XDOT = 18347.260099 XDOT = 5529.366749 YDOT = 16722.503672 feet/sec YDOT = 5159.203776 meter/sec ZDOT = 3691.970762 ZDOT = 1152.325946 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7438121.30 X = -2267139.37 Y = -12167895.01 feet Y = -3708774.40 meter Z = -17162644.41 Z = -5231174.02 XDOT = 17523.468607 XDOT = 5341.153231 YDOT = -16082.209945 feet/sec YDOT = -4901.857591 meter/sec ZDOT = 3815.875793 ZDOT = 1163.078942 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 20159.53913921 .00016717 00000-0 10270-3 0 9164 2 25544 51.6439 36.2325 0002106 25.7314 334.3941 15.49426941 30513 Satellite: ISS Catalog Number: 25544 Epoch time: 20159.53913921 = yrday.fracday Element set: 916 Inclination: 51.6439 deg RA of node: 36.2325 deg Eccentricity: .0002106 Arg of perigee: 25.7314 deg Mean anomaly: 334.3941 deg Mean motion: 15.49426941 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3051 Checksum: 291 Coasting Arc #18 (Orbit 3061) --------------------------------------- Vector Time (GMT): 2020/160/04:50:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2842517.57 A = 6791281.17 meter Y = 3137908.83 meter E = .0004951 Z = 5306871.95 I = 51.83185 XDOT = -6171.099180 Wp = 51.01506 YDOT = -4498.843242 meter/sec RA = 32.30485 deg ZDOT = -641.856605 TA = 45.12019 MA = 45.08000 Ha = 229.058 n.mi Hp = 221.658 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -9325845.04 X = -2903172.98 Y = 10294976.46 feet Y = 3105781.56 meter Z = 17410997.20 Z = 5292917.47 XDOT = -20246.388385 XDOT = -6117.215371 YDOT = -14759.984389 feet/sec YDOT = -4567.551452 meter/sec ZDOT = -2105.828757 ZDOT = -671.703309 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13422958.21 X = -4091317.66 Y = 3875966.42 feet Y = 1181394.56 meter Z = 17346522.04 Z = 5287219.92 XDOT = -9310.304367 XDOT = -2837.780771 YDOT = -22154.558397 feet/sec YDOT = -6752.709399 meter/sec ZDOT = -2242.818002 ZDOT = -683.610927 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 20160.24861767 .00016717 00000-0 10270-3 0 9175 2 25544 51.6409 32.7196 0002088 33.6699 326.4584 15.49407739 30621 Satellite: ISS Catalog Number: 25544 Epoch time: 20160.24861767 = yrday.fracday Element set: 917 Inclination: 51.6409 deg RA of node: 32.7196 deg Eccentricity: .0002088 Arg of perigee: 33.6699 deg Mean anomaly: 326.4584 deg Mean motion: 15.49407739 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3062 Checksum: 330 Coasting Arc #19 (Orbit 3076) --------------------------------------- Vector Time (GMT): 2020/161/04:50:00.000 Vector Time (MET): N/A Weight (LBS) : 980162.0 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2718185.57 A = 6791403.09 meter Y = -3287201.38 meter E = .0015683 Z = -5298311.04 I = 51.80358 XDOT = 6443.644369 Wp = 89.07041 YDOT = 4043.601805 meter/sec RA = 27.36740 deg ZDOT = 799.320456 TA = 188.55721 MA = 188.58398 Ha = 229.023 n.mi Hp = 221.700 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 8917931.66 X = 2780477.97 Y = -10784781.43 feet Y = -3256455.41 meter Z = -17382910.24 Z = -5284956.57 XDOT = 21140.565514 XDOT = 6394.066098 YDOT = 13266.410123 feet/sec YDOT = 4115.381865 meter/sec ZDOT = 2622.442442 ZDOT = 830.501260 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13249941.89 X = 4038582.29 Y = -4735212.94 feet Y = -1443292.90 meter Z = -17321183.05 Z = -5279496.59 XDOT = 11167.812292 XDOT = 3403.949187 YDOT = 21160.662797 feet/sec YDOT = 6449.770021 meter/sec ZDOT = 2765.603024 ZDOT = 842.955802 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 20161.21608553 .00016717 00000-0 10270-3 0 9186 2 25544 51.6415 27.9310 0002203 36.5304 323.5996 15.49397635 30770 Satellite: ISS Catalog Number: 25544 Epoch time: 20161.21608553 = yrday.fracday Element set: 918 Inclination: 51.6415 deg RA of node: 27.9310 deg Eccentricity: .0002203 Arg of perigee: 36.5304 deg Mean anomaly: 323.5996 deg Mean motion: 15.49397635 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3077 Checksum: 300