I am trying to calculate the orbital elements of common low earth orbit communication satellites. The orbital
Fantastic news! We've Found the answer you've been seeking!
Question:
I am trying to calculate the orbital elements of common low earth orbit communication satellites. The orbital elements I am referring to are the 6 COES such as Eccentricity ,semi major axis ,Argument of Perigee, RAAN or Right ascension of the ascending node , True Anomaly and Inclination.
I only have low earth altitude of 1000 km and the orbit is not circular, I know the eccenctricty can be quite low
Also Please provide all calculations regarding questionn when required
Please provide all sources such as url for websites or articles, textbooks
Posted Date: