@Shazwan@scott23192 ketinggian orbit satelit, specifically Transporter-9:
https://t.co/Tq5ax3bLbc
58300 kemungkinan besar ION SCV-013:
https://t.co/sNMRckUeLM
https://t.co/PrYWXQsy68
SpaceANT-D naik ION SCV-013 sebelum deploy:
https://t.co/zsktjopjdH
https://t.co/h3hnt1UJBh
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@DutchSpace not a python code, but this is in space-track documentation:
Using semi-major axis "a", eccentricity "e", and the Earth's radius in km,
apogee = (a * (1 + e))- 6378.135
perigee = (a * (1 - e))- 6378.135
https://t.co/fHJvTKOyDH