Create Matlab code that:

Convert from the topocentric horizon coordinate system (azimuth, elevation, range) to the geocentric equatorial coordinates

Solve Lambert's problem from the two position vector and the time between them

Present the orbital parameter of the orbit

The Inputs of the problem will be:

Observation 1: Azimuth Angle 1, Elevation Angle 1, Range, Date (30/4/2021 23:00:00 for example)

Observation 2: Azimuth Angle 2, Elevation Angle 2, Range, Date (30/4/2021 23:45:00 for example)

Observation site: Longitude, Latitude, Heigh