ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 16466.6302 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 70.2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.865 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 ------------------------------------------------------------------------ 089/03:30:00.000 0.0 0.0 0.0 N/A 0.0 0.0 230.9 000/00:00:00.000 0.0 0.0 221.3 093/12:44:33.314 1.5 1.5 1.5 N/A -0.0 0.0 231.0 000/00:07:06.628 -0.2 -0.0 222.0 096/03:42:00.000 0.0 0.0 0.0 N/A 0.0 0.0 231.1 000/00:00:00.000 0.0 0.0 221.8 097/14:00:43.000 0.0 0.0 0.0 N/A 0.0 0.0 230.9 000/00:00:00.000 0.0 0.0 222.0 100/06:00:00.000 0.0 0.0 0.0 N/A 0.0 0.0 231.0 000/00:00:00.000 0.0 0.0 222.0 100/08:05:06.000 0.0 0.0 0.0 N/A 0.0 0.0 230.8 000/00:00:00.000 0.0 0.0 221.9 100/14:16:50.000 0.0 0.0 0.0 N/A 0.0 0.0 230.9 000/00:00:00.000 0.0 0.0 222.0 Coasting Arc #1 (Orbit 1934) --------------------------------------- Vector Time (GMT): 2020/087/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 939740.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2379380.55 A = 6792533.25 meter Y = 3457858.90 meter E = .0007412 Z = 5334741.74 I = 51.83086 XDOT = -6429.693633 Wp = 64.30776 YDOT = -4170.445973 meter/sec RA = 32.02071 deg ZDOT = -161.250515 TA = 27.24490 MA = 27.20604 Ha = 231.008 n.mi Hp = 221.233 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -7806366.63 X = -2443783.77 Y = 11344681.44 feet Y = 3430891.32 meter Z = 17502433.53 Z = 5323026.87 XDOT = -21094.795383 XDOT = -6381.797339 YDOT = -13682.565527 feet/sec YDOT = -4242.079589 meter/sec ZDOT = -529.037122 ZDOT = -192.366930 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7014518.55 X = -2138025.25 Y = 11930009.61 feet Y = 3636266.93 meter Z = 17448430.77 Z = 5318281.70 XDOT = -21225.160498 XDOT = -6469.428920 YDOT = -11481.741988 feet/sec YDOT = -3499.634958 meter/sec ZDOT = -671.525558 ZDOT = -204.680990 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 20087.54807131 .00016717 00000-0 10270-3 0 9003 2 25544 51.6426 32.4250 0005074 57.3311 302.8328 15.48930609 19357 Satellite: ISS Catalog Number: 25544 Epoch time: 20087.54807131 = yrday.fracday Element set: 900 Inclination: 51.6426 deg RA of node: 32.4250 deg Eccentricity: .0005074 Arg of perigee: 57.3311 deg Mean anomaly: 302.8328 deg Mean motion: 15.48930609 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1935 Checksum: 284 Coasting Arc #2 (Orbit 1949) --------------------------------------- Vector Time (GMT): 2020/088/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 939740.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2049076.16 A = 6792597.89 meter Y = -3677819.46 meter E = .0019328 Z = -5347071.41 I = 51.80180 XDOT = 6757.481125 Wp = 83.42484 YDOT = 3574.342404 meter/sec RA = 27.08829 deg ZDOT = 133.632541 TA = 187.83441 MA = 187.86465 Ha = 230.950 n.mi Hp = 221.282 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 6722690.82 X = 2116023.53 Y = -12066336.81 feet Y = -3654531.26 meter Z = -17542885.20 Z = -5336954.89 XDOT = 22170.213665 XDOT = 6716.360428 YDOT = 11726.845156 feet/sec YDOT = 3649.679452 meter/sec ZDOT = 438.426971 ZDOT = 166.357848 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 5661079.96 X = 1725497.17 Y = -12664087.19 feet Y = -3860013.77 meter Z = -17496198.06 Z = -5332841.17 XDOT = 22259.486716 XDOT = 6784.691551 YDOT = 9149.270340 feet/sec YDOT = 2788.697600 meter/sec ZDOT = 588.323380 ZDOT = 179.320966 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 20088.51584914 .00016717 00000-0 10270-3 0 9013 2 25544 51.6426 27.6385 0005031 61.2618 298.9037 15.48913846 19502 Satellite: ISS Catalog Number: 25544 Epoch time: 20088.51584914 = yrday.fracday Element set: 901 Inclination: 51.6426 deg RA of node: 27.6385 deg Eccentricity: .0005031 Arg of perigee: 61.2618 deg Mean anomaly: 298.9037 deg Mean motion: 15.48913846 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1950 Checksum: 319 Coasting Arc #3 (Orbit 1959) --------------------------------------- Vector Time (GMT): 2020/089/03:30:00.000 Vector Time (MET): N/A Weight (LBS) : 939740.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2227996.95 A = 6792721.18 meter Y = -3601066.56 meter E = .0018997 Z = -5327591.23 I = 51.78325 XDOT = 6801.709948 Wp = 87.01036 YDOT = 3454.680784 meter/sec RA = 23.89798 deg ZDOT = 511.901580 TA = 187.86308 MA = 187.89290 Ha = 230.905 n.mi Hp = 221.340 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 7309701.28 X = 2293978.12 Y = -11814522.84 feet Y = -3575782.88 meter Z = -17478973.84 Z = -5316607.97 XDOT = 22315.321353 XDOT = 6760.086628 YDOT = 11334.254542 feet/sec YDOT = 3530.509639 meter/sec ZDOT = 1679.467126 ZDOT = 544.840568 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 6215457.02 X = 1894471.30 Y = 12496046.80 feet Y = 3808795.06 meter Z = -17428313.67 Z = -5312150.01 XDOT = -20382.937219 XDOT = -6212.719264 YDOT = 12679.467325 feet/sec YDOT = 3864.701641 meter/sec ZDOT = 1830.342592 ZDOT = 557.888422 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 20089.16103214 .00016717 00000-0 10270-3 0 9026 2 25544 51.6433 24.4471 0004767 65.9697 294.1952 15.48902988 19604 Satellite: ISS Catalog Number: 25544 Epoch time: 20089.16103214 = yrday.fracday Element set: 902 Inclination: 51.6433 deg RA of node: 24.4471 deg Eccentricity: .0004767 Arg of perigee: 65.9697 deg Mean anomaly: 294.1952 deg Mean motion: 15.48902988 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1960 Checksum: 324 Coasting Arc #4 (Orbit 1975) --------------------------------------- Vector Time (GMT): 2020/090/03:30:00.000 Vector Time (MET): N/A Weight (LBS) : 939740.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1891939.88 A = 6792559.52 meter Y = 3777952.66 meter E = .0007619 Z = 5312604.23 I = 51.75271 XDOT = -7097.918028 Wp = 67.93842 YDOT = -2852.248539 meter/sec RA = 18.96238 deg ZDOT = -496.048094 TA = 26.80766 MA = 26.76830 Ha = 230.940 n.mi Hp = 221.159 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6207151.82 X = -1959851.18 Y = 12394857.82 feet Y = 3756416.12 meter Z = 17429803.91 Z = 5303248.80 XDOT = -23287.132639 XDOT = -7063.086280 YDOT = -9357.770796 feet/sec YDOT = -2931.427766 meter/sec ZDOT = -1627.454376 ZDOT = -530.442488 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7488250.87 X = -2282418.87 Y = -11729946.92 feet Y = -3575287.82 meter Z = 17386596.64 Z = 5299434.65 XDOT = 18997.323871 XDOT = 5790.384316 YDOT = -14789.904538 feet/sec YDOT = -4507.962903 meter/sec ZDOT = -1785.038789 ZDOT = -544.079823 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 20090.19332297 .00016717 00000-0 10270-3 0 9037 2 25544 51.6439 19.3416 0004800 69.1166 291.0497 15.48950351 19761 Satellite: ISS Catalog Number: 25544 Epoch time: 20090.19332297 = yrday.fracday Element set: 903 Inclination: 51.6439 deg RA of node: 19.3416 deg Eccentricity: .0004800 Arg of perigee: 69.1166 deg Mean anomaly: 291.0497 deg Mean motion: 15.48950351 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1976 Checksum: 312 Coasting Arc #5 (Orbit 1990) --------------------------------------- Vector Time (GMT): 2020/091/03:30:00.000 Vector Time (MET): N/A Weight (LBS) : 939740.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1536320.46 A = 6792698.70 meter Y = -3948603.83 meter E = .0019382 Z = -5326057.23 I = 51.72024 XDOT = 7304.483470 Wp = 88.00477 YDOT = 2208.393436 meter/sec RA = 14.02454 deg ZDOT = 471.902975 TA = 186.49233 MA = 186.51748 Ha = 231.006 n.mi Hp = 221.182 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5040421.45 X = 1606231.74 Y = -12954736.98 feet Y = -3931032.83 meter Z = -17473941.05 Z = -5318424.47 XDOT = 23964.840782 XDOT = 7276.953438 YDOT = 7245.385288 feet/sec YDOT = 2289.923444 meter/sec ZDOT = 1548.238106 ZDOT = 507.318477 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8749621.37 X = 2666884.59 Y = 10858556.92 feet Y = 3309688.15 meter Z = -17438622.12 Z = -5315292.02 XDOT = -17287.480427 XDOT = -5269.224034 YDOT = 16665.702083 feet/sec YDOT = 5079.705995 meter/sec ZDOT = 1710.545184 ZDOT = 521.374172 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 20091.16109611 .00016717 00000-0 10270-3 0 9048 2 25544 51.6436 14.5552 0004970 71.9270 288.2421 15.48906343 19915 Satellite: ISS Catalog Number: 25544 Epoch time: 20091.16109611 = yrday.fracday Element set: 904 Inclination: 51.6436 deg RA of node: 14.5552 deg Eccentricity: .0004970 Arg of perigee: 71.9270 deg Mean anomaly: 288.2421 deg Mean motion: 15.48906343 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 1991 Checksum: 297 Coasting Arc #6 (Orbit 2006) --------------------------------------- Vector Time (GMT): 2020/092/03:30:00.000 Vector Time (MET): N/A Weight (LBS) : 939740.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1174436.73 A = 6792551.70 meter Y = 4061308.93 meter E = .0007736 Z = 5310255.84 I = 51.68660 XDOT = -7490.715537 Wp = 72.89288 YDOT = -1564.051829 meter/sec RA = 9.08501 deg ZDOT = -457.706633 TA = 21.48749 MA = 21.45504 Ha = 231.013 n.mi Hp = 221.043 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3853138.88 X = -1245558.37 Y = 13324504.37 feet Y = 4047777.97 meter Z = 17422099.23 Z = 5304378.09 XDOT = -24575.838377 XDOT = -7470.445848 YDOT = -5131.403637 feet/sec YDOT = -1647.705008 meter/sec ZDOT = -1501.662183 ZDOT = -494.044310 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -9825840.57 X = -2994916.21 Y = -9838275.31 feet Y = -2998706.31 meter Z = 17394822.03 Z = 5301941.76 XDOT = 15493.840159 XDOT = 4722.522480 YDOT = -18439.954544 feet/sec YDOT = -5620.498145 meter/sec ZDOT = -1668.240446 ZDOT = -508.479688 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 20092.19338426 .00016717 00000-0 10270-3 0 9051 2 25544 51.6428 9.4502 0004980 76.2031 283.9673 15.48948725 20078 Satellite: ISS Catalog Number: 25544 Epoch time: 20092.19338426 = yrday.fracday Element set: 905 Inclination: 51.6428 deg RA of node: 9.4502 deg Eccentricity: .0004980 Arg of perigee: 76.2031 deg Mean anomaly: 283.9673 deg Mean motion: 15.48948725 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2007 Checksum: 313 Coasting Arc #7 (Orbit 2021) --------------------------------------- Vector Time (GMT): 2020/093/03:30:00.000 Vector Time (MET): N/A Weight (LBS) : 939740.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 797480.96 A = 6792670.35 meter Y = -4164542.16 meter E = .0019568 Z = -5323641.38 I = 51.65424 XDOT = 7580.254920 Wp = 89.59157 YDOT = 895.300213 meter/sec RA = 4.14211 deg ZDOT = 436.680905 TA = 184.57583 MA = 184.59374 Ha = 231.029 n.mi Hp = 221.093 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 2616407.36 X = 869849.93 Y = -13663196.07 feet Y = -4155219.62 meter Z = -17466015.01 Z = -5319591.70 XDOT = 24869.602757 XDOT = 7567.558894 YDOT = 2937.336656 feet/sec YDOT = 979.997033 meter/sec ZDOT = 1432.680136 ZDOT = 473.471800 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 10864210.49 X = 3311411.36 Y = 8726811.54 feet Y = 2659932.16 meter Z = -17447116.82 Z = -5317881.21 XDOT = -13431.669243 XDOT = -4093.972785 YDOT = 19912.926467 feet/sec YDOT = 6069.459987 meter/sec ZDOT = 1601.381047 ZDOT = 488.100943 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 20093.16115430 .00016717 00000-0 10270-3 0 9068 2 25544 51.6438 4.6632 0004983 79.1781 280.9930 15.48912334 20224 Satellite: ISS Catalog Number: 25544 Epoch time: 20093.16115430 = yrday.fracday Element set: 906 Inclination: 51.6438 deg RA of node: 4.6632 deg Eccentricity: .0004983 Arg of perigee: 79.1781 deg Mean anomaly: 280.9930 deg Mean motion: 15.48912334 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2022 Checksum: 296 Coasting Arc #8 (Orbit 2027) --------------------------------------- Vector Time (GMT): 2020/093/12:48:06.628 Vector Time (MET): N/A Weight (LBS) : 939584.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 965428.07 A = 6793518.01 meter Y = -4159502.89 meter E = .0018059 Z = -5299476.68 I = 51.64292 XDOT = 7565.025934 Wp = 91.31265 YDOT = 855.179671 meter/sec RA = 2.22536 deg ZDOT = 708.623198 TA = 185.46497 MA = 185.48471 Ha = 230.952 n.mi Hp = 221.973 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 3167414.92 X = 1037610.79 Y = -13646663.04 feet Y = -4148303.30 meter Z = -17386734.51 Z = -5294611.63 XDOT = 24819.638892 XDOT = 7551.458750 YDOT = 2805.707582 feet/sec YDOT = 939.701326 meter/sec ZDOT = 2324.879260 ZDOT = 745.337954 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -2176375.20 X = -663359.16 Y = -13867731.65 feet Y = -4226884.61 meter Z = -17364097.33 Z = -5292576.87 XDOT = 22983.203694 XDOT = 7005.280486 YDOT = -6721.810686 feet/sec YDOT = -2048.807897 meter/sec ZDOT = 2493.230800 ZDOT = 759.936748 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 20093.54826209 .00016717 00000-0 10270-3 0 9074 2 25544 51.6451 2.7504 0003712 75.7633 284.3929 15.48660634 20288 Satellite: ISS Catalog Number: 25544 Epoch time: 20093.54826209 = yrday.fracday Element set: 907 Inclination: 51.6451 deg RA of node: 2.7504 deg Eccentricity: .0003712 Arg of perigee: 75.7633 deg Mean anomaly: 284.3929 deg Mean motion: 15.48660634 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2028 Checksum: 306 Coasting Arc #9 (Orbit 2043) --------------------------------------- Vector Time (GMT): 2020/094/12:48:06.628 Vector Time (MET): N/A Weight (LBS) : 939584.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -468161.96 A = 6793364.42 meter Y = 4222751.60 meter E = .0006574 Z = 5295608.07 I = 51.60956 XDOT = -7641.161565 Wp = 71.89647 YDOT = -104.814924 meter/sec RA = 357.28272 deg ZDOT = -589.342235 TA = 23.74856 MA = 23.71823 Ha = 230.921 n.mi Hp = 221.918 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -1535964.45 X = -541070.05 Y = 13854171.90 feet Y = 4217108.81 meter Z = 17374042.23 Z = 5293156.72 XDOT = -25069.427708 XDOT = -7636.558925 YDOT = -343.880983 feet/sec YDOT = -190.238112 meter/sec ZDOT = -1933.537518 ZDOT = -626.448523 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 3993996.80 X = 1217370.22 Y = 13369631.12 feet Y = 4075063.57 meter Z = 17362475.70 Z = 5292082.59 XDOT = -22149.928193 XDOT = -6751.298113 YDOT = 9360.090783 feet/sec YDOT = 2852.955671 meter/sec ZDOT = -2103.733268 ZDOT = -641.217900 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 20094.58073802 .00016717 00000-0 10270-3 0 9083 2 25544 51.6455 357.6459 0003659 78.7517 281.4044 15.48688518 20442 Satellite: ISS Catalog Number: 25544 Epoch time: 20094.58073802 = yrday.fracday Element set: 908 Inclination: 51.6455 deg RA of node: 357.6459 deg Eccentricity: .0003659 Arg of perigee: 78.7517 deg Mean anomaly: 281.4044 deg Mean motion: 15.48688518 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2044 Checksum: 339 Coasting Arc #10 (Orbit 2058) --------------------------------------- Vector Time (GMT): 2020/095/12:48:06.628 Vector Time (MET): N/A Weight (LBS) : 939584.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -41192.05 A = 6793395.44 meter Y = -4249544.42 meter E = .0018372 Z = -5315948.58 I = 51.57533 XDOT = 7603.951221 Wp = 90.92703 YDOT = -652.013738 meter/sec RA = 352.33819 deg ZDOT = 463.396490 TA = 183.50345 MA = 183.51633 Ha = 230.972 n.mi Hp = 221.887 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -135144.51 X = 32152.29 Y = -13942074.87 feet Y = -4249595.26 meter Z = -17440776.19 Z = -5315970.30 XDOT = 24947.346524 XDOT = 7608.426196 YDOT = -2139.152685 feet/sec YDOT = -566.955900 meter/sec ZDOT = 1520.329690 ZDOT = 500.344090 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -5780820.01 X = -1761993.94 Y = -12688164.57 feet Y = -3867352.56 meter Z = -17440555.89 Z = -5315881.44 XDOT = 20894.808309 XDOT = 6368.737573 YDOT = -11837.639920 feet/sec YDOT = -3608.112647 meter/sec ZDOT = 1689.842778 ZDOT = 515.064079 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 20095.54868513 .00016717 00000-0 10270-3 0 9092 2 25544 51.6449 352.8610 0003754 81.3647 278.7928 15.48667408 20592 Satellite: ISS Catalog Number: 25544 Epoch time: 20095.54868513 = yrday.fracday Element set: 909 Inclination: 51.6449 deg RA of node: 352.8610 deg Eccentricity: .0003754 Arg of perigee: 81.3647 deg Mean anomaly: 278.7928 deg Mean motion: 15.48667408 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2059 Checksum: 348 Coasting Arc #11 (Orbit 2068) --------------------------------------- Vector Time (GMT): 2020/096/03:42:00.000 Vector Time (MET): N/A Weight (LBS) : 939584.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4403070.64 A = 6799907.85 meter Y = 3730257.54 meter E = .0016071 Z = 3583728.42 I = 51.57419 XDOT = -5733.715195 Wp = 86.74891 YDOT = -2491.051135 meter/sec RA = 349.24479 deg ZDOT = -4433.597373 TA = 50.92001 MA = 50.77716 Ha = 231.128 n.mi Hp = 221.821 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -14445769.82 X = -4461863.81 Y = 12238377.75 feet Y = 3680690.79 meter Z = 11757639.17 Z = 3562197.14 XDOT = -18811.401560 XDOT = -5683.897672 YDOT = -8172.739945 feet/sec YDOT = -2554.891382 meter/sec ZDOT = -14545.923139 ZDOT = -4461.328126 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -6066972.15 X = -1849213.11 Y = -17999135.48 feet Y = -5486136.50 meter Z = 11658610.77 Z = 3553544.56 XDOT = 13147.784483 XDOT = 4007.444710 YDOT = -13974.643282 feet/sec YDOT = -4259.471272 meter/sec ZDOT = -14672.920825 ZDOT = -4472.306267 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 20096.19398170 .00016717 00000-0 10270-3 0 9103 2 25544 51.6427 349.6698 0003989 86.3821 273.7784 15.48674788 20692 Satellite: ISS Catalog Number: 25544 Epoch time: 20096.19398170 = yrday.fracday Element set: 910 Inclination: 51.6427 deg RA of node: 349.6698 deg Eccentricity: .0003989 Arg of perigee: 86.3821 deg Mean anomaly: 273.7784 deg Mean motion: 15.48674788 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2069 Checksum: 369 Coasting Arc #12 (Orbit 2083) --------------------------------------- Vector Time (GMT): 2020/097/03:42:00.000 Vector Time (MET): N/A Weight (LBS) : 939584.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3944257.30 A = 6799675.97 meter Y = -4146253.35 meter E = .0009354 Z = -3681253.35 I = 51.54125 XDOT = 6017.169028 Wp = 94.64729 YDOT = 1883.932063 meter/sec RA = 344.29569 deg ZDOT = 4333.955868 TA = 221.65180 MA = 221.72307 Ha = 231.074 n.mi Hp = 221.929 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12940476.71 X = 4008210.14 Y = -13603193.40 feet Y = -4101788.61 meter Z = -12077602.86 Z = -3661938.07 XDOT = 19741.368201 XDOT = 5974.603343 YDOT = 6180.879472 feet/sec YDOT = 1950.982722 meter/sec ZDOT = 14219.015314 ZDOT = 4363.081239 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 8180545.44 X = 2493430.25 Y = 16962327.72 feet Y = 5170117.49 meter Z = -11988720.25 Z = -3654161.93 XDOT = -11434.090779 XDOT = -3485.110869 YDOT = 15637.944197 feet/sec YDOT = 4766.445391 meter/sec ZDOT = 14352.444203 ZDOT = 4374.624993 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 20097.16192608 .00016717 00000-0 10270-3 0 9110 2 25544 51.6434 344.8851 0003894 89.6199 270.5397 15.48652741 20844 Satellite: ISS Catalog Number: 25544 Epoch time: 20097.16192608 = yrday.fracday Element set: 911 Inclination: 51.6434 deg RA of node: 344.8851 deg Eccentricity: .0003894 Arg of perigee: 89.6199 deg Mean anomaly: 270.5397 deg Mean motion: 15.48652741 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2084 Checksum: 338 Coasting Arc #13 (Orbit 2090) --------------------------------------- Vector Time (GMT): 2020/097/14:00:43.000 Vector Time (MET): N/A Weight (LBS) : 915571.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6598700.92 A = 6804637.81 meter Y = 1076725.01 meter E = .0011355 Z = -1248264.72 I = 51.54439 XDOT = 286.259056 Wp = 127.48306 YDOT = -4955.098617 meter/sec RA = 342.20584 deg ZDOT = -5830.690427 TA = 66.07106 MA = 65.95217 Ha = 230.901 n.mi Hp = 222.021 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -21649281.22 X = -6604187.40 Y = 3532562.37 feet Y = 1002902.84 meter Z = -4095356.69 Z = -1280331.99 XDOT = 939.170130 XDOT = 369.969264 YDOT = -16256.885227 feet/sec YDOT = -4951.429972 meter/sec ZDOT = -19129.561770 ZDOT = -5829.096104 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -12914989.67 X = -3936488.85 Y = 17695950.52 feet Y = 5393725.72 meter Z = -4242487.20 Z = -1293110.10 XDOT = -9363.530160 XDOT = -2854.003993 YDOT = -11385.243608 feet/sec YDOT = -3470.222252 meter/sec ZDOT = -19121.889536 ZDOT = -5828.351931 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 20097.61363271 .00016717 00000-0 10270-3 0 9127 2 25544 51.6438 342.6522 0003498 89.5949 270.5601 15.48634627 20910 Satellite: ISS Catalog Number: 25544 Epoch time: 20097.61363271 = yrday.fracday Element set: 912 Inclination: 51.6438 deg RA of node: 342.6522 deg Eccentricity: .0003498 Arg of perigee: 89.5949 deg Mean anomaly: 270.5601 deg Mean motion: 15.48634627 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2091 Checksum: 321 Coasting Arc #14 (Orbit 2106) --------------------------------------- Vector Time (GMT): 2020/098/14:00:43.000 Vector Time (MET): N/A Weight (LBS) : 915571.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6472739.36 A = 6804647.20 meter Y = -1748557.62 meter E = .0016704 Z = 1119935.68 I = 51.51225 XDOT = 305.734500 Wp = 64.23967 YDOT = 4924.850374 meter/sec RA = 337.25096 deg ZDOT = 5860.943119 TA = 307.91096 MA = 308.06186 Ha = 230.877 n.mi Hp = 221.905 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21236021.51 X = 6486371.15 Y = -5736737.60 feet Y = -1676098.51 meter Z = 3674329.67 Z = 1151411.12 XDOT = 1003.065945 XDOT = 222.171416 YDOT = 16157.645583 feet/sec YDOT = 4927.802664 meter/sec ZDOT = 19228.816006 ZDOT = 5862.224816 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 10747062.69 X = 3275704.71 Y = -19164995.14 feet Y = -5841490.52 meter Z = 3818778.79 Z = 1163963.78 XDOT = 10754.789064 XDOT = 3278.059707 YDOT = 9902.017115 feet/sec YDOT = 3018.134817 meter/sec ZDOT = 19234.338441 ZDOT = 5862.626357 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 20098.64610188 .00016717 00000-0 10270-3 0 9134 2 25544 51.6428 337.5468 0003566 92.4992 267.6566 15.48680018 21078 Satellite: ISS Catalog Number: 25544 Epoch time: 20098.64610188 = yrday.fracday Element set: 913 Inclination: 51.6428 deg RA of node: 337.5468 deg Eccentricity: .0003566 Arg of perigee: 92.4992 deg Mean anomaly: 267.6566 deg Mean motion: 15.48680018 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2107 Checksum: 336 Coasting Arc #15 (Orbit 2121) --------------------------------------- Vector Time (GMT): 2020/099/14:00:43.000 Vector Time (MET): N/A Weight (LBS) : 915571.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6290382.41 A = 6804808.13 meter Y = 2365691.65 meter E = .0012248 Z = -1042728.77 I = 51.48056 XDOT = -853.317618 Wp = 128.94490 YDOT = -4835.338201 meter/sec RA = 332.29540 deg ZDOT = -5876.600008 TA = 62.35613 MA = 62.23185 Ha = 230.910 n.mi Hp = 221.976 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -20637737.56 X = -6311303.73 Y = 7761455.54 feet Y = 2295231.05 meter Z = -3421026.15 Z = -1073336.29 XDOT = -2799.598483 XDOT = -770.638581 YDOT = -15863.970476 feet/sec YDOT = -4844.418819 meter/sec ZDOT = -19280.183754 ZDOT = -5880.543904 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -8535319.53 X = -2601565.39 Y = 20305754.88 feet Y = 6189194.09 meter Z = -3561525.38 Z = -1085552.94 XDOT = -11875.150141 XDOT = -3619.545763 YDOT = -8346.419325 feet/sec YDOT = -2543.988610 meter/sec ZDOT = -19297.920603 ZDOT = -5882.006200 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 20099.61404299 .00016717 00000-0 10270-3 0 9147 2 25544 51.6414 332.7616 0003591 95.5921 264.5638 15.48647697 21228 Satellite: ISS Catalog Number: 25544 Epoch time: 20099.61404299 = yrday.fracday Element set: 914 Inclination: 51.6414 deg RA of node: 332.7616 deg Eccentricity: .0003591 Arg of perigee: 95.5921 deg Mean anomaly: 264.5638 deg Mean motion: 15.48647697 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2122 Checksum: 329 Coasting Arc #16 (Orbit 2131) --------------------------------------- Vector Time (GMT): 2020/100/06:00:00.000 Vector Time (MET): N/A Weight (LBS) : 915571.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1820946.12 A = 6797888.77 meter Y = -5020450.65 meter E = .0011518 Z = -4217698.70 I = 51.43668 XDOT = 6693.092486 Wp = 105.17732 YDOT = -633.098138 meter/sec RA = 328.95879 deg ZDOT = 3648.686420 TA = 202.38956 MA = 202.43988 Ha = 231.007 n.mi Hp = 221.975 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5974232.67 X = 1897438.36 Y = -16471294.78 feet Y = -4999660.13 meter Z = -13837594.15 Z = -4208667.02 XDOT = 21958.964850 XDOT = 6681.951089 YDOT = -2077.093627 feet/sec YDOT = -558.313260 meter/sec ZDOT = 11970.755972 ZDOT = 3681.172208 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 17527208.94 X = 5342293.29 Y = 972637.62 feet Y = 296459.95 meter Z = -13795830.61 Z = -4204969.17 XDOT = 8469.532091 XDOT = 2581.513381 YDOT = 19029.157818 feet/sec YDOT = 5800.087303 meter/sec ZDOT = 12119.734899 ZDOT = 3694.095197 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 20100.25933742 .00016717 00000-0 10270-3 0 9151 2 25544 51.6404 329.5714 0003726 96.9838 263.1736 15.48643895 21323 Satellite: ISS Catalog Number: 25544 Epoch time: 20100.25933742 = yrday.fracday Element set: 915 Inclination: 51.6404 deg RA of node: 329.5714 deg Eccentricity: .0003726 Arg of perigee: 96.9838 deg Mean anomaly: 263.1736 deg Mean motion: 15.48643895 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2132 Checksum: 318 Coasting Arc #17 (Orbit 2133) --------------------------------------- Vector Time (GMT): 2020/100/08:05:06.000 Vector Time (MET): N/A Weight (LBS) : 915571.4 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3869179.65 A = 6794274.18 meter Y = 2360876.27 meter E = .0008766 Z = 5055419.54 I = 51.42448 XDOT = -5471.027220 Wp = 113.76818 YDOT = 5048.389851 meter/sec RA = 328.56831 deg ZDOT = 1823.694817 TA = 318.47915 MA = 318.54571 Ha = 230.753 n.mi Hp = 221.913 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12694158.96 X = 3817935.43 Y = 7745657.07 feet Y = 2403858.00 meter Z = 16586022.10 Z = 5074090.10 XDOT = -17949.564370 XDOT = -5535.931763 YDOT = 16562.958830 feet/sec YDOT = 4986.846148 meter/sec ZDOT = 5983.250711 ZDOT = 1796.960414 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 4266934.64 X = 1300561.68 Y = 14145282.13 feet Y = 4311481.99 meter Z = 16671450.64 Z = 5081458.15 XDOT = -23417.968718 XDOT = -7137.796865 YDOT = 134.144045 feet/sec YDOT = 40.887105 meter/sec ZDOT = 5860.326306 ZDOT = 1786.227458 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 20100.38839500 .00016717 00000-0 10270-3 0 9163 2 25544 51.6420 328.9341 0003608 98.8413 261.3145 15.48693770 21342 Satellite: ISS Catalog Number: 25544 Epoch time: 20100.38839500 = yrday.fracday Element set: 916 Inclination: 51.6420 deg RA of node: 328.9341 deg Eccentricity: .0003608 Arg of perigee: 98.8413 deg Mean anomaly: 261.3145 deg Mean motion: 15.48693770 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2134 Checksum: 299 Coasting Arc #18 (Orbit 2137) --------------------------------------- Vector Time (GMT): 2020/100/14:16:50.000 Vector Time (MET): N/A Weight (LBS) : 931488.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 3906085.93 A = 6794457.50 meter Y = 2289406.94 meter E = .0008758 Z = 5060159.42 I = 51.41515 XDOT = -5370.868168 Wp = 113.96407 YDOT = 5161.305210 meter/sec RA = 327.28614 deg ZDOT = 1804.793909 TA = 318.47032 MA = 318.53683 Ha = 230.870 n.mi Hp = 222.016 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 12815242.54 X = 3855615.12 Y = 7511177.61 feet Y = 2332805.66 meter Z = 16601572.91 Z = 5079011.18 XDOT = -17620.958558 XDOT = -5436.951002 YDOT = 16933.416042 feet/sec YDOT = 5100.874953 meter/sec ZDOT = 5921.239859 ZDOT = 1778.543203 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 13777521.73 X = 4199388.62 Y = -5287388.93 feet Y = -1611596.15 meter Z = 16687835.90 Z = 5086452.38 XDOT = 1913.330580 XDOT = 583.183161 YDOT = 23354.490042 feet/sec YDOT = 7118.448565 meter/sec ZDOT = 5800.527528 ZDOT = 1768.000791 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 20100.64651300 .00016717 00000-0 10270-3 0 9173 2 25544 51.6401 327.6559 0003634 99.4808 260.6753 15.48624055 21383 Satellite: ISS Catalog Number: 25544 Epoch time: 20100.64651300 = yrday.fracday Element set: 917 Inclination: 51.6401 deg RA of node: 327.6559 deg Eccentricity: .0003634 Arg of perigee: 99.4808 deg Mean anomaly: 260.6753 deg Mean motion: 15.48624055 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2138 Checksum: 300 Coasting Arc #19 (Orbit 2152) --------------------------------------- Vector Time (GMT): 2020/101/14:16:50.000 Vector Time (MET): N/A Weight (LBS) : 931488.8 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -4175919.84 A = 6794472.39 meter Y = -1861758.00 meter E = .0016340 Z = -5040732.01 I = 51.38755 XDOT = 4807.240125 Wp = 81.68046 YDOT = -5633.797184 meter/sec RA = 322.32638 deg ZDOT = -1904.691887 TA = 169.74814 MA = 169.71478 Ha = 230.923 n.mi Hp = 221.809 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -13700524.42 X = -4130305.45 Y = -6108129.92 feet Y = -1908201.20 meter Z = -16537834.67 Z = -5060906.40 XDOT = 15771.785186 XDOT = 4879.133645 YDOT = -18483.586563 feet/sec YDOT = -5579.637277 meter/sec ZDOT = -6248.989131 ZDOT = -1881.165131 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -13108398.42 X = -3995439.84 Y = 7079572.74 feet Y = 2157853.77 meter Z = -16630187.51 Z = -5068881.15 XDOT = -4554.745552 XDOT = -1388.286444 YDOT = -22835.261024 feet/sec YDOT = -6960.187560 meter/sec ZDOT = -6140.739016 ZDOT = -1871.697252 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 20101.61444970 .00016717 00000-0 10270-3 0 9185 2 25544 51.6397 322.8691 0003671 104.0942 256.0616 15.48665346 21536 Satellite: ISS Catalog Number: 25544 Epoch time: 20101.61444970 = yrday.fracday Element set: 918 Inclination: 51.6397 deg RA of node: 322.8691 deg Eccentricity: .0003671 Arg of perigee: 104.0942 deg Mean anomaly: 256.0616 deg Mean motion: 15.48665346 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 2153 Checksum: 305