This is the question. but, i know how to create the two-line element set. i just need to know how to find the type of orbit this satellite is in.
determine the orbit of the following spacecraft by developing a two-line element set.
satellite name: amusat 1
satellite catalog number: 27230u
international designator: 02007a
first derivative of the mean motion/2: .1428
second derivative of the mean motion/6: -0
ballistic coefficient: 46512-4
element type: 0
element set number: 15
number of revolutions: 33
epoch time: 02046.6232174
mean anomaly: 5.2502
argument of perigee: 82.0871
right ascension of the ascending node: 227.8983
eccentricity: 0.8135719
inclination: 87.8691
mean motion: 1.26429138
what type of orbit is this satellite in?
what type of orbit is this satellite in, based on the following two-line element set? and why?
1 27230u 02007a 02046.6232174 .1428 -0 46512-4 0 15
2 27230 87.8691 227.8983 0.8135719 82.0871 5.2502 1.26429138