ISS TRAJECTORY DATA Lift off time (UTC) : N/A Area (sq ft) : 16520.4497 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 68.6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.584 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 ------------------------------------------------------------------------ 317/14:50:00.000 0.0 0.0 0.0 N/A 0.0 0.0 225.3 000/00:00:00.000 0.0 0.0 223.6 Coasting Arc #1 (Orbit 3809) --------------------------------------- Vector Time (GMT): 2019/315/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6612352.48 A = 6801362.03 meter Y = -1500575.73 meter E = .0008091 Z = -458931.19 I = 51.60004 XDOT = 1449.107127 Wp = 7.83322 YDOT = 4562.232768 meter/sec RA = 350.28927 deg ZDOT = 5982.030275 TA = 347.22357 MA = 347.24406 Ha = 225.252 n.mi Hp = 223.538 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21694069.81 X = 6630870.20 Y = -4923148.73 feet Y = -1426528.19 meter Z = -1505679.74 Z = -426764.98 XDOT = 4754.288475 XDOT = 1368.924999 YDOT = 14967.955276 feet/sec YDOT = 4577.989306 meter/sec ZDOT = 19626.083579 ZDOT = 5988.875000 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -10368487.97 X = -3160315.13 Y = 19692257.63 feet Y = 6002200.12 meter Z = -1358887.97 Z = -414189.05 XDOT = -12942.925635 XDOT = -3945.003733 YDOT = -5463.433878 feet/sec YDOT = -1665.254646 meter/sec ZDOT = 19656.824114 ZDOT = 5991.399990 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 19315.50080136 .00016717 00000-0 10270-3 0 9009 2 25544 51.6432 350.8820 0006364 267.3689 92.6733 15.49972798 38102 Satellite: ISS Catalog Number: 25544 Epoch time: 19315.50080136 = yrday.fracday Element set: 900 Inclination: 51.6432 deg RA of node: 350.8820 deg Eccentricity: .0006364 Arg of perigee: 267.3689 deg Mean anomaly: 92.6733 deg Mean motion: 15.49972798 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3810 Checksum: 325 Coasting Arc #2 (Orbit 3825) --------------------------------------- Vector Time (GMT): 2019/316/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -6550473.00 A = 6801335.26 meter Y = 1805324.81 meter E = .0008759 Z = 110873.67 I = 51.56773 XDOT = -1361.713601 Wp = 163.08418 YDOT = -4565.501582 meter/sec RA = 345.33357 deg ZDOT = -6000.589812 TA = 15.72237 MA = 15.69519 Ha = 225.148 n.mi Hp = 223.497 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -21491053.14 X = -6570712.39 Y = 5922981.65 feet Y = 1731959.62 meter Z = 363758.76 Z = 79003.88 XDOT = -4467.564307 XDOT = -1281.411230 YDOT = -14978.679732 feet/sec YDOT = -4580.280019 meter/sec ZDOT = -19686.974450 ZDOT = -6007.009816 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 9123263.93 X = 2780770.85 Y = -20342020.52 feet Y = -6200247.85 meter Z = 218296.87 Z = 66536.89 XDOT = 12825.792422 XDOT = 3909.301530 YDOT = 5534.174455 feet/sec YDOT = 1686.816374 meter/sec ZDOT = -19715.774735 ZDOT = -6009.368139 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 19316.53237707 .00016717 00000-0 10270-3 0 9012 2 25544 51.6433 345.7717 0006330 270.5076 89.5349 15.50006661 38264 Satellite: ISS Catalog Number: 25544 Epoch time: 19316.53237707 = yrday.fracday Element set: 901 Inclination: 51.6433 deg RA of node: 345.7717 deg Eccentricity: .0006330 Arg of perigee: 270.5076 deg Mean anomaly: 89.5349 deg Mean motion: 15.50006661 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3826 Checksum: 310 Coasting Arc #3 (Orbit 3841) --------------------------------------- Vector Time (GMT): 2019/317/12:00:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 6455442.81 A = 6801357.88 meter Y = -2109381.59 meter E = .0009480 Z = 228121.92 I = 51.53481 XDOT = 1287.947667 Wp = 18.64040 YDOT = 4596.312902 meter/sec RA = 340.37552 deg ZDOT = 5993.993133 TA = 343.81696 MA = 343.84721 Ha = 225.305 n.mi Hp = 223.485 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 21179274.31 X = 6477442.62 Y = -6920543.27 feet Y = -2037069.28 meter Z = 748431.49 Z = 259534.27 XDOT = 4225.550089 XDOT = 1207.338299 YDOT = 15079.766739 feet/sec YDOT = 4610.264587 meter/sec ZDOT = 19665.331801 ZDOT = 6000.054153 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -7793102.32 X = -2375337.59 Y = 20868347.36 feet Y = 6360672.27 meter Z = 891831.87 Z = 271830.35 XDOT = -12820.140959 XDOT = -3907.578964 YDOT = -5636.239363 feet/sec YDOT = -1717.925758 meter/sec ZDOT = 19692.490096 ZDOT = 6002.270981 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 19317.56395313 .00016717 00000-0 10270-3 0 9025 2 25544 51.6426 340.6614 0006282 275.4802 84.5631 15.49989463 38428 Satellite: ISS Catalog Number: 25544 Epoch time: 19317.56395313 = yrday.fracday Element set: 902 Inclination: 51.6426 deg RA of node: 340.6614 deg Eccentricity: .0006282 Arg of perigee: 275.4802 deg Mean anomaly: 84.5631 deg Mean motion: 15.49989463 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3842 Checksum: 327 Coasting Arc #4 (Orbit 3842) --------------------------------------- Vector Time (GMT): 2019/317/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2101465.26 A = 6792841.26 meter Y = -4612075.60 meter E = .0003748 Z = -4526474.92 I = 51.49960 XDOT = 6981.075738 Wp = 134.88743 YDOT = 93.039020 meter/sec RA = 339.76470 deg ZDOT = 3145.255771 TA = 166.77514 MA = 166.76531 Ha = 225.340 n.mi Hp = 223.630 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 6894571.07 X = 2174870.38 Y = -15131481.63 feet Y = -4588164.83 meter Z = -14850639.49 Z = -4516088.47 XDOT = 22903.791792 XDOT = 6964.238149 YDOT = 305.246130 feet/sec YDOT = 171.012007 meter/sec ZDOT = 10319.080615 ZDOT = 3179.127315 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 15587480.81 X = 4751064.15 Y = 5911442.48 feet Y = 1801807.67 meter Z = -14802825.06 Z = -4511901.08 XDOT = 1734.249173 XDOT = 528.599148 YDOT = 21661.775648 feet/sec YDOT = 6602.509218 meter/sec ZDOT = 10473.464894 ZDOT = 3192.312100 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 19317.62842611 .00016717 00000-0 10270-3 0 9031 2 25544 51.6397 340.3424 0006379 276.0674 83.9750 15.49977217 38432 Satellite: ISS Catalog Number: 25544 Epoch time: 19317.62842611 = yrday.fracday Element set: 903 Inclination: 51.6397 deg RA of node: 340.3424 deg Eccentricity: .0006379 Arg of perigee: 276.0674 deg Mean anomaly: 83.9750 deg Mean motion: 15.49977217 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3843 Checksum: 337 Coasting Arc #5 (Orbit 3858) --------------------------------------- Vector Time (GMT): 2019/318/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -2094614.11 A = 6793474.57 meter Y = 4796780.99 meter E = .0004983 Z = 4330701.47 I = 51.47115 XDOT = -6826.566550 Wp = 35.15325 YDOT = 158.049381 meter/sec RA = 334.79917 deg ZDOT = -3470.851217 TA = 90.27100 MA = 90.21389 Ha = 225.480 n.mi Hp = 223.625 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6872093.52 X = -2169134.13 Y = 15737470.45 feet Y = 4772940.53 meter Z = 14208338.16 Z = 4320345.73 XDOT = -22396.871884 XDOT = -6810.966622 YDOT = 518.534714 feet/sec YDOT = 81.797391 meter/sec ZDOT = -11387.307141 ZDOT = -3503.975100 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -16288135.16 X = -4964623.60 Y = -5562665.44 feet Y = -1695500.43 meter Z = 14160647.05 Z = 4316165.22 XDOT = -2876.305118 XDOT = -876.697800 YDOT = -21000.599959 feet/sec YDOT = -6400.982868 meter/sec ZDOT = -11538.303664 ZDOT = -3516.874957 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 19318.65999985 .00016717 00000-0 10270-3 0 9043 2 25544 51.6399 335.2316 0006495 279.9380 80.1037 15.50008655 38599 Satellite: ISS Catalog Number: 25544 Epoch time: 19318.65999985 = yrday.fracday Element set: 904 Inclination: 51.6399 deg RA of node: 335.2316 deg Eccentricity: .0006495 Arg of perigee: 279.9380 deg Mean anomaly: 80.1037 deg Mean motion: 15.50008655 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3859 Checksum: 356 Coasting Arc #6 (Orbit 3873) --------------------------------------- Vector Time (GMT): 2019/319/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 2053600.79 A = 6794271.87 meter Y = -4995110.38 meter E = .0001105 Z = -4123574.47 I = 51.44476 XDOT = 6651.220114 Wp = 135.52300 YDOT = -383.926122 meter/sec RA = 329.83194 deg ZDOT = 3777.320170 TA = 173.57951 MA = 173.57809 Ha = 225.763 n.mi Hp = 223.676 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 6737535.40 X = 2129335.42 Y = -16388157.42 feet Y = -4971721.73 meter Z = -13528787.63 Z = -4113415.13 XDOT = 21821.588302 XDOT = 6636.670414 YDOT = -1259.600137 feet/sec YDOT = -309.629183 meter/sec ZDOT = 12392.782709 ZDOT = 3809.594667 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 17013912.68 X = 5185840.58 Y = 5075165.26 feet Y = 1546910.37 meter Z = -13481975.17 Z = -4109306.03 XDOT = 3898.042599 XDOT = 1188.123384 YDOT = 20245.440527 feet/sec YDOT = 6170.810273 meter/sec ZDOT = 12539.927370 ZDOT = 3822.169862 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 19319.62709836 .00016717 00000-0 10270-3 0 9056 2 25544 51.6408 330.4404 0006446 284.4317 75.6118 15.49987373 38749 Satellite: ISS Catalog Number: 25544 Epoch time: 19319.62709836 = yrday.fracday Element set: 905 Inclination: 51.6408 deg RA of node: 330.4404 deg Eccentricity: .0006446 Arg of perigee: 284.4317 deg Mean anomaly: 75.6118 deg Mean motion: 15.49987373 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3874 Checksum: 339 Coasting Arc #7 (Orbit 3889) --------------------------------------- Vector Time (GMT): 2019/320/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1997326.91 A = 6794980.58 meter Y = 5200207.61 meter E = .0006228 Z = 3889827.98 I = 51.41882 XDOT = -6460.975749 Wp = 52.41229 YDOT = 572.342677 meter/sec RA = 324.86337 deg ZDOT = -4074.476880 TA = 80.50194 MA = 80.43155 Ha = 225.977 n.mi Hp = 223.587 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -6552909.82 X = -2074223.66 Y = 17061048.58 feet Y = 5177441.75 meter Z = 12761902.83 Z = 3879939.28 XDOT = -21197.426998 XDOT = -6447.103757 YDOT = 1877.764687 feet/sec YDOT = 500.169445 meter/sec ZDOT = -13367.706298 ZDOT = -4105.828697 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -17743413.93 X = -5408192.57 Y = -4511420.78 feet Y = -1375081.05 meter Z = 12716308.99 Z = 3875930.98 XDOT = -4762.681397 XDOT = -1451.665290 YDOT = -19427.055530 feet/sec YDOT = -5921.366526 meter/sec ZDOT = -13510.662282 ZDOT = -4118.049864 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 19320.65866855 .00016717 00000-0 10270-3 0 9067 2 25544 51.6405 325.3298 0006521 288.9754 71.0690 15.50014194 38905 Satellite: ISS Catalog Number: 25544 Epoch time: 19320.65866855 = yrday.fracday Element set: 906 Inclination: 51.6405 deg RA of node: 325.3298 deg Eccentricity: .0006521 Arg of perigee: 288.9754 deg Mean anomaly: 71.0690 deg Mean motion: 15.50014194 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3890 Checksum: 326 Coasting Arc #8 (Orbit 3904) --------------------------------------- Vector Time (GMT): 2019/321/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1898045.42 A = 6795806.63 meter Y = -5408157.90 meter E = .0001813 Z = -3649192.17 I = 51.39456 XDOT = 6262.860660 Wp = 337.52274 YDOT = -735.536805 meter/sec RA = 319.89349 deg ZDOT = 4348.486715 TA = 339.06356 MA = 339.07098 Ha = 226.197 n.mi Hp = 223.587 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 6227183.14 X = 1976105.93 Y = -17743300.18 feet Y = -5386495.81 meter Z = -11972415.25 Z = -3639782.96 XDOT = 20547.443111 XDOT = 6249.497364 YDOT = -2413.178493 feet/sec YDOT = -665.576198 meter/sec ZDOT = 14266.688697 ZDOT = 4378.877227 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 18448018.72 X = 5622956.10 Y = 3782978.83 feet Y = 1153051.95 meter Z = -11928994.71 Z = -3635957.59 XDOT = 5504.413256 XDOT = 1677.745160 YDOT = 18572.315949 feet/sec YDOT = 5660.841901 meter/sec ZDOT = 14405.277281 ZDOT = 4390.728515 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 19321.62576530 .00016717 00000-0 10270-3 0 9074 2 25544 51.6404 320.5390 0006564 292.3692 67.6753 15.49990430 39053 Satellite: ISS Catalog Number: 25544 Epoch time: 19321.62576530 = yrday.fracday Element set: 907 Inclination: 51.6404 deg RA of node: 320.5390 deg Eccentricity: .0006564 Arg of perigee: 292.3692 deg Mean anomaly: 67.6753 deg Mean motion: 15.49990430 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3905 Checksum: 321 Coasting Arc #9 (Orbit 3920) --------------------------------------- Vector Time (GMT): 2019/322/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1785722.72 A = 6796516.87 meter Y = 5616969.84 meter E = .0007113 Z = 3381523.50 I = 51.37351 XDOT = -6056.682513 Wp = 67.00502 YDOT = 856.298673 meter/sec RA = 314.92225 deg ZDOT = -4610.313272 TA = 73.42706 MA = 73.34895 Ha = 226.362 n.mi Hp = 223.429 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -5858670.34 X = -1864826.31 Y = 18428378.73 feet Y = 5596558.06 meter Z = 11094237.20 Z = 3372657.35 XDOT = -19871.005620 XDOT = -6043.413187 YDOT = 2809.378848 feet/sec YDOT = 788.643127 meter/sec ZDOT = -15125.699710 ZDOT = -4639.702363 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -19128651.11 X = -5830412.86 Y = -2988461.79 feet Y = -910883.15 meter Z = 11053282.88 Z = 3369040.62 XDOT = -6073.281810 XDOT = -1851.136296 YDOT = -17694.160309 feet/sec YDOT = -5393.180062 meter/sec ZDOT = -15259.732742 ZDOT = -4651.166540 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 19322.65733379 .00016717 00000-0 10270-3 0 9085 2 25544 51.6416 315.4287 0006606 296.4091 63.6381 15.50018677 39216 Satellite: ISS Catalog Number: 25544 Epoch time: 19322.65733379 = yrday.fracday Element set: 908 Inclination: 51.6416 deg RA of node: 315.4287 deg Eccentricity: .0006606 Arg of perigee: 296.4091 deg Mean anomaly: 63.6381 deg Mean motion: 15.50018677 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3921 Checksum: 325 Coasting Arc #10 (Orbit 3935) --------------------------------------- Vector Time (GMT): 2019/323/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1628035.42 A = 6797299.58 meter Y = -5816954.78 meter E = .0004794 Z = -3110279.16 I = 51.35316 XDOT = 5854.936710 Wp = 342.71585 YDOT = -952.371176 meter/sec RA = 309.94951 deg ZDOT = 4848.407451 TA = 341.40036 MA = 341.41788 Ha = 226.577 n.mi Hp = 223.335 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 5341323.56 X = 1708069.44 Y = -19084497.31 feet Y = -5798301.26 meter Z = -10204327.96 Z = -3102176.65 XDOT = 19209.109941 XDOT = 5841.600179 YDOT = -3124.577348 feet/sec YDOT = -886.971986 meter/sec ZDOT = 15906.848593 ZDOT = 4876.816338 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 19732963.82 X = 6014607.37 Y = 2030124.76 feet Y = 618782.03 meter Z = -10166848.91 Z = -3098855.55 XDOT = 6525.990886 XDOT = 1989.122022 YDOT = 16834.957789 feet/sec YDOT = 5131.295134 meter/sec ZDOT = 16036.418821 ZDOT = 4887.900457 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 19323.62442667 .00016717 00000-0 10270-3 0 9091 2 25544 51.6416 310.6377 0006659 300.3842 59.6650 15.50001189 39360 Satellite: ISS Catalog Number: 25544 Epoch time: 19323.62442667 = yrday.fracday Element set: 909 Inclination: 51.6416 deg RA of node: 310.6377 deg Eccentricity: .0006659 Arg of perigee: 300.3842 deg Mean anomaly: 59.6650 deg Mean motion: 15.50001189 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3936 Checksum: 315 Coasting Arc #11 (Orbit 3951) --------------------------------------- Vector Time (GMT): 2019/324/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1460561.73 A = 6797990.21 meter Y = 6012325.48 meter E = .0007867 Z = 2811593.38 I = 51.33489 XDOT = -5653.098402 Wp = 79.18311 YDOT = 1003.899015 meter/sec RA = 304.97609 deg ZDOT = -5069.826418 TA = 68.82183 MA = 68.73779 Ha = 226.764 n.mi Hp = 223.114 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -4791869.18 X = -1541342.04 Y = 19725477.28 feet Y = 5995540.67 meter Z = 9224387.72 Z = 2804302.47 XDOT = -18546.910768 XDOT = -5639.277505 YDOT = 3293.631940 feet/sec YDOT = 940.759539 meter/sec ZDOT = -16633.288773 ZDOT = -5097.253712 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -20288726.38 X = -6184003.80 Y = -1022819.72 feet Y = -311755.45 meter Z = 9190604.72 Z = 2801296.32 XDOT = -6805.288675 XDOT = -2074.251988 YDOT = -15994.972425 feet/sec YDOT = -4875.267595 meter/sec ZDOT = -16758.384278 ZDOT = -5107.955528 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 19324.65599159 .00016717 00000-0 10270-3 0 9106 2 25544 51.6414 305.5275 0006632 305.0724 54.9804 15.50020059 39524 Satellite: ISS Catalog Number: 25544 Epoch time: 19324.65599159 = yrday.fracday Element set: 910 Inclination: 51.6414 deg RA of node: 305.5275 deg Eccentricity: .0006632 Arg of perigee: 305.0724 deg Mean anomaly: 54.9804 deg Mean motion: 15.50020059 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3952 Checksum: 304 Coasting Arc #12 (Orbit 3966) --------------------------------------- Vector Time (GMT): 2019/325/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 1246652.78 A = 6798682.03 meter Y = -6186610.25 meter E = .0007649 Z = -2515318.77 I = 51.31828 XDOT = 5468.053963 Wp = 350.38843 YDOT = -1037.394326 meter/sec RA = 300.00154 deg ZDOT = 5266.718959 TA = 341.29886 MA = 341.32695 Ha = 226.894 n.mi Hp = 223.022 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 4090068.17 X = 1327958.78 Y = -20297277.71 feet Y = -6172214.63 meter Z = -8252358.16 Z = -2509065.57 XDOT = 17939.809591 XDOT = 5453.664890 YDOT = -3403.524690 feet/sec YDOT = -976.327254 meter/sec ZDOT = 17279.261676 ZDOT = 5293.246082 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 20716368.28 X = 6314349.05 Y = -137518.48 feet Y = -41915.63 meter Z = -8223304.03 Z = -2506463.07 XDOT = 7001.414261 XDOT = 2134.031067 YDOT = 15224.468256 feet/sec YDOT = 4640.417924 meter/sec ZDOT = 17400.251272 ZDOT = 5303.596588 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 19325.62308272 .00016717 00000-0 10270-3 0 9119 2 25544 51.6408 300.7367 0006687 307.8743 52.1802 15.50007439 39678 Satellite: ISS Catalog Number: 25544 Epoch time: 19325.62308272 = yrday.fracday Element set: 911 Inclination: 51.6408 deg RA of node: 300.7367 deg Eccentricity: .0006687 Arg of perigee: 307.8743 deg Mean anomaly: 52.1802 deg Mean motion: 15.50007439 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3967 Checksum: 311 Coasting Arc #13 (Orbit 3982) --------------------------------------- Vector Time (GMT): 2019/326/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -1028551.35 A = 6799278.24 meter Y = 6351462.02 meter E = .0008065 Z = 2190856.66 I = 51.30578 XDOT = -5290.384147 Wp = 90.42648 YDOT = 1026.623801 meter/sec RA = 295.02577 deg ZDOT = -5442.573832 TA = 65.18134 MA = 65.09748 Ha = 227.065 n.mi Hp = 222.832 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -3374512.31 X = -1110140.95 Y = 20838129.99 feet Y = 6339503.79 meter Z = 7187849.94 Z = 2185662.21 XDOT = -17356.903370 XDOT = -5275.033511 YDOT = 3368.188325 feet/sec YDOT = 967.548921 meter/sec ZDOT = -17856.213358 ZDOT = -5468.235667 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -21076589.64 X = -6424144.52 Y = 1319127.12 feet Y = 402069.95 meter Z = 7163620.21 Z = 2183471.44 XDOT = -7036.505372 XDOT = -2144.726837 YDOT = -14511.060104 feet/sec YDOT = -4422.971120 meter/sec ZDOT = -17973.252539 ZDOT = -5478.247374 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 19326.65464452 .00016717 00000-0 10270-3 0 9127 2 25544 51.6419 295.6260 0006722 311.8405 48.2171 15.50023445 39832 Satellite: ISS Catalog Number: 25544 Epoch time: 19326.65464452 = yrday.fracday Element set: 912 Inclination: 51.6419 deg RA of node: 295.6260 deg Eccentricity: .0006722 Arg of perigee: 311.8405 deg Mean anomaly: 48.2171 deg Mean motion: 15.50023445 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3983 Checksum: 303 Coasting Arc #14 (Orbit 3997) --------------------------------------- Vector Time (GMT): 2019/327/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 768822.73 A = 6799830.95 meter Y = -6484444.59 meter E = .0010416 Z = -1872904.30 I = 51.29419 XDOT = 5139.562908 Wp = 358.71616 YDOT = -1004.049280 meter/sec RA = 290.04902 deg ZDOT = 5595.648908 TA = 340.59445 MA = 340.63408 Ha = 227.218 n.mi Hp = 222.654 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 2522384.27 X = 850374.25 Y = -21274424.51 feet Y = -6475391.04 meter Z = -6144699.15 Z = -1868971.67 XDOT = 16862.083033 XDOT = 5123.227367 YDOT = -3294.124935 feet/sec YDOT = -946.666550 meter/sec ZDOT = 18358.428176 ZDOT = 5620.575802 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21267924.46 X = 6482463.38 Y = -2620249.00 feet Y = -798651.89 meter Z = -6126220.10 Z = -1867271.89 XDOT = 7025.048580 XDOT = 2141.234807 YDOT = 13906.210400 feet/sec YDOT = 4238.612930 meter/sec ZDOT = 18472.111602 ZDOT = 5630.299616 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 19327.62173105 .00016717 00000-0 10270-3 0 9138 2 25544 51.6416 290.8346 0006765 315.9977 44.0635 15.50018250 39980 Satellite: ISS Catalog Number: 25544 Epoch time: 19327.62173105 = yrday.fracday Element set: 913 Inclination: 51.6416 deg RA of node: 290.8346 deg Eccentricity: .0006765 Arg of perigee: 315.9977 deg Mean anomaly: 44.0635 deg Mean motion: 15.50018250 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 3998 Checksum: 322 Coasting Arc #15 (Orbit 4013) --------------------------------------- Vector Time (GMT): 2019/328/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = -510795.57 A = 6800319.58 meter Y = 6604383.15 meter E = .0008026 Z = 1527256.25 I = 51.28597 XDOT = -5003.247200 Wp = 99.66528 YDOT = 941.831272 meter/sec RA = 285.07240 deg ZDOT = -5721.657623 TA = 63.60058 MA = 63.51822 Ha = 227.392 n.mi Hp = 222.465 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = -1675838.48 X = -592028.48 Y = 21667923.73 feet Y = 6598216.80 meter Z = 5010683.25 Z = 1524577.95 XDOT = -16414.853018 XDOT = -4985.613875 YDOT = 3089.997610 feet/sec YDOT = 885.980290 meter/sec ZDOT = -18771.842594 ZDOT = -5745.919235 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = -21380580.44 X = -6516800.92 Y = 3912272.61 feet Y = 1192460.69 meter Z = 4997919.85 Z = 1523365.97 XDOT = -6882.770665 XDOT = -2097.868499 YDOT = -13389.087044 feet/sec YDOT = -4080.993731 meter/sec ZDOT = -18882.486855 ZDOT = -5755.381993 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 19328.65328940 .00016717 00000-0 10270-3 0 9142 2 25544 51.6421 285.7242 0006710 319.8933 40.1722 15.50019711 40146 Satellite: ISS Catalog Number: 25544 Epoch time: 19328.65328940 = yrday.fracday Element set: 914 Inclination: 51.6421 deg RA of node: 285.7242 deg Eccentricity: .0006710 Arg of perigee: 319.8933 deg Mean anomaly: 40.1722 deg Mean motion: 15.50019711 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 4014 Checksum: 292 Coasting Arc #16 (Orbit 4028) --------------------------------------- Vector Time (GMT): 2019/329/14:50:00.000 Vector Time (MET): N/A Weight (LBS) : 932295.2 M50 Cartesian M50 Keplerian ----------------------------------- -------------------------------- X = 216948.39 A = 6800683.87 meter Y = -6683114.40 meter E = .0012757 Z = -1194703.37 I = 51.27985 XDOT = 4901.638493 Wp = 6.87394 YDOT = -879.159609 meter/sec RA = 280.09497 deg ZDOT = 5826.977140 TA = 340.09773 MA = 340.14745 Ha = 227.479 n.mi Hp = 222.327 M50 Cartesian J2K Cartesian ----------------------------------- -------------------------------- X = 711772.92 X = 297468.14 Y = -21926228.33 feet Y = -6680238.03 meter Z = -3919630.48 Z = -1193454.40 XDOT = 16081.491118 XDOT = 4882.800291 YDOT = -2884.381920 feet/sec YDOT = -824.451777 meter/sec ZDOT = 19117.379069 ZDOT = 5850.742236 TDR Cartesian TDR Cartesian ----------------------------------- -------------------------------- X = 21292942.31 X = 6490088.82 Y = -5284473.04 feet Y = -1610707.38 meter Z = -3913382.82 Z = -1192799.09 XDOT = 6749.192462 XDOT = 2057.153863 YDOT = 13003.282711 feet/sec YDOT = 3963.400570 meter/sec ZDOT = 19225.756171 ZDOT = 5860.010481 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 19329.62037406 .00016717 00000-0 10270-3 0 9155 2 25544 51.6423 280.9330 0006812 322.8911 37.1768 15.50025009 40295 Satellite: ISS Catalog Number: 25544 Epoch time: 19329.62037406 = yrday.fracday Element set: 915 Inclination: 51.6423 deg RA of node: 280.9330 deg Eccentricity: .0006812 Arg of perigee: 322.8911 deg Mean anomaly: 37.1768 deg Mean motion: 15.50025009 rev/day Decay rate: 1.67170E-04 rev/day^2 Epoch rev: 4029 Checksum: 294