This question is based on satellite so I thought to keep it under mechanical engineering section. It's a 2 part question and both the part are attached as an image. Thanks a lot. Consider a satellite is moving around the earth. The position and velocity vectorof the satellite are T = 7000- 20003–4000k (km) and T = 3i-63+5k (km/s),respectively in earth-centered Cartesian coordinate system. The eccentricityvector e of the orbit is (Assume the earth to be non-rotating)a) 0.2888å + 0.08523 – 0.3840kb) 0.1332i +0.1246j – 0.2698kc) 0.2888i – 0.08523; + 0.3840kd) 0.1332i – 0.1246j + 0.2698k Referring to Question 1, the true anomaly of the satellite's orbit isa) 23.42°b) 53.35°c) 33.32°d) 28.12°

Hello. Since your question has multiple parts, we will solve first question for you. If you want…

Consider a satellite is moving around the earth. The position and velocity vector of the satellite are 7 = 7000-20003-4000k (km) and T 31-6)+5k (km/s), respectively in earth-centered Cartesian coordinate system. The eccentricity vector e of the orbit is (Assume the earth to be non-rotating) a) 0.2888? + 0.085233- 0.3840k b) 0.1332i +0.1246j – 0.2698k c) 0.2888? – 0.08523; +0.3840k d) 0.1332 - 0.1246j + 0.2698k

Consider a satellite is moving around the earth. The position and velocity vector of the satellite are 7 = 7000-20003-4000k (km) and T 31-6)+5k (km/s), respectively in earth-centered Cartesian coordinate system. The eccentricity vector e of the orbit is (Assume the earth to be non-rotating) a) 0.2888? + 0.085233- 0.3840k b) 0.1332i +0.1246j – 0.2698k c) 0.2888? – 0.08523; +0.3840k d) 0.1332 - 0.1246j + 0.2698k

International Edition---engineering Mechanics: Statics, 4th Edition

4th Edition

ISBN:9781305501607

Author:Andrew Pytel And Jaan Kiusalaas

Publisher:Andrew Pytel And Jaan Kiusalaas

Chapter7: Dry Friction

Section: Chapter Questions

Problem 7.11P: Solve Prob. 7.10 assuming that the pick-up truck has front-wheel drive.

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