Determine the orbit of the following spacecraft by


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: .00001428

Second derivative of the mean motion/6: 00000-0

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?

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Physics: Determine the orbit of the following spacecraft by
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