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At a given time, satellite are: inert position and velocity ectors in a geocentric equatorial frame of an earth F=-24291 +4555.1Ĵ+4577.0 K (km) v=-4.7689 Î-5.6113 J+3.0535 K (km/s) a) find the classical orbital elements b) determine the period and semimajor axis of the orbit

At a given time, satellite are: inert position and velocity ectors in a geocentric equatorial frame of an earth F=-24291 +4555.1Ĵ+4577.0 K (km) v=-4.7689 Î-5.6113 J+3.0535 K (km/s) a) find the classical orbital elements b) determine the period and semimajor axis of the orbit

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At a given time, the inertial position and velocity vectors in a geocentric equatorial frame of an earth satellite are: 7 = -24291 +4555.1Ĵ+4577.0 K (km) V=4.7689 Î-5.6113 J+3.0535 K (km/s) a) find the classical orbital elements b) determine the period and semimajor axis of the orbit
Transcribed Image Text:At a given time, the inertial position and velocity vectors in a geocentric equatorial frame of an earth satellite are: 7 = -24291 +4555.1Ĵ+4577.0 K (km) V=4.7689 Î-5.6113 J+3.0535 K (km/s) a) find the classical orbital elements b) determine the period and semimajor axis of the orbit
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