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NSWPhysicsQuick questions

Module 5: Advanced Mechanics

Quick questions on Orbital motion and satellites explained: HSC Physics Module 5

8short Q&A pairs drawn directly from our worked dot-point answer. For full context and worked exam questions, read the parent dot-point page.

What is common orbits used in HSC?
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Low Earth Orbit (LEO). Altitude 200 to 2000 km. Periods 90 to 130 minutes. Used by the ISS, Earth-observation satellites, and Starlink. High orbital speed (about 7 to 8 km/s).
What is atmospheric drag?
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In low orbits (below about 400400 km), residual atmosphere creates drag, slowly reducing orbital energy. Satellites must boost periodically (the ISS does this every few months) or eventually re-enter.
What is low Earth Orbit?
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Altitude 200 to 2000 km. Periods 90 to 130 minutes. Used by the ISS, Earth-observation satellites, and Starlink. High orbital speed (about 7 to 8 km/s).
What is geostationary Earth Orbit?
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Altitude about 35 800 km (radius 4.22×1074.22 \times 10^7 m). Period exactly one sidereal day (about 23 h 56 min). The satellite sits over a fixed equatorial point.
What is medium Earth Orbit?
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Altitude 2 000 to 35 800 km. Used by GPS satellites (about 20 200 km altitude, 12-hour period).
What is q1?
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Define "geostationary orbit" and state its altitude above Earth's surface. [2 marks]
What is q2?
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A satellite is in a circular orbit of radius 9.0×106 m9.0 \times 10^6 \text{ m} about Earth. Calculate its orbital speed and period. [4 marks]
What is q3?
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Two satellites orbit Earth: A at r=7000 kmr = 7000 \text{ km} and B at r=14000 kmr = 14000 \text{ km}. (a) Identify which is faster and by what factor. (b) Find the ratio of orbital periods TB/TAT_B / T_A.

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