Question

What is orbital speed of low orbit satellite?

Answer 1

Answer:

The mean orbital velocity needed to maintain a stable low Earth orbit is about 7.8 km/s (28,000 km/h; 17,000 mph), but reduces with increased orbital altitude. Calculated for circular orbit of 200 km (120 mi) it is 7.79 km/s (28,000 km/h; 17,400 mph), and for 1,500 km (930 mi) it is 7.12 km/s (25,600 km/h; 15,900 mph).

Explanation:

Hope this helps. Please mark me as the brainliest. Have a good day.

Answer 2

Answer:

Hii Buddy ur answer

Explanation:

The mean orbital velocity needed to maintain a stable low Earth orbit is about 7.8 km/s , but reduces with increased orbital altitude. Calculated for circular orbit of 200 km (120 mi) it is 7.79 km/s, and for 1,500 km (930 mi) it is 7.12 km/s (25,600 km/h; 15,900 mph).

Hope it helps you✌

Mark me plz...

#Saranya ❤️