Question:

A satellite revolves very near to the earth surface. Its speed should be around

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First cosmic velocity (orbital) \(\approx 7.9\ \mathrm{km/s}\); second cosmic velocity (escape) \(\approx 11.2\ \mathrm{km/s}\).
Updated On: Apr 7, 2026
  • 5 km/s
  • 8 km/s
  • 2 km/s
  • 11 km/s
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The Correct Option is B

Solution and Explanation

Step 1: Understanding the Concept:
Orbital speed for a near-Earth satellite is the first cosmic velocity.
Step 2: Detailed Explanation:
Orbital speed ≈ 7.9 km/s, rounded ≈ 8 km/s.
Step 3: Final Answer:
Speed is about 8 km/s.
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