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?