Solution: The total radius of the orbit is the sum of the planet's radius and the satellite's orbital radius: $ 6,000 + 10,000 = 16,000 $ km. The circumference $ C $ is calculated as $ C = 2\pi \times 16,000 = 32,000\pi $ km.

Fri, 01 May 2026 04:56:05 +0000

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