WebNov 29, 2016 · E = 1 2 v 2 − μ r = − μ 2 a, Which can be rewritten to a = − μ r r v 2 − 2 μ Where a is the semi major axis, μ = G ( M + m), v is the velocity and M, m are the … WebDec 31, 2015 · Explanation: The formulas for Aphelion and Perihelion are, Ra = a ( 1 + e) and Rp = a ( 1 - e ) if you divide the above equations you can get the eccentricity of the …
Lecture 13: Binary Star Systems - University of Alberta
WebJul 13, 1995 · Semi-major axis (Saturnian Radii) Orbital Period* (days) Rotation Period (days) Inclination (degrees) Eccentricity : Major Satellites : Mimas (SI) 185.52: 3.0783: 0.9424218: S: 1.53: ... the rotation period is the same as the orbital period C indicates chaotic rotation Saturn Surpasses Jupiter After The Discovery Of 20 New Moons... WebDec 15, 2024 · Use Kepler’s Third Law to find its orbital period from its semi-major axis. The Law states that the square of the period is equal to the cube of the semi-major axis. In order for the units to be correct, the … life cycle of a pig worksheet
Calculating specific orbital energy, semi-major axis, and orbital ...
WebNov 29, 2016 · E = 1 2 v 2 − μ r = − μ 2 a, Which can be rewritten to a = − μ r r v 2 − 2 μ Where a is the semi major axis, μ = G ( M + m), v is the velocity and M, m are the bigger and smaller masses, respectively. WebApr 10, 2024 · Question: Phobos orbits Mars with an average distance of about 9500 km from the center of the planet around a rotational period of about 8 hr. Estimate the mass of Mars. Solution: Given that semi-major axis a = 9500 km = 9.5 x 10 6 m Planet periord T = 8 hrs = 28800 sec Kepler's equation is a³/T² = 4 * π²/ [G * (M + m)] WebJan 1, 2016 · Explanation: The formulas for Aphelion and Perihelion are, Ra = a ( 1 + e) and Rp = a ( 1 - e ) if you divide the above equations you can get the eccentricity of the orbit e, Place the obtained value of e in one of the above given equations to … life cycle of a pine tree diagram