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This deck focuses on Motion Of Orbiting Satellites, giving you a quick way to review the definitions, rules, and examples that matter most for AP Physics 1.
Study Motion Of Orbiting Satellites in AP Physics 1 with focused flashcards that help you recognize the idea, recall the key rule, and apply it in practice-style prompts.
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What happens to a satellite's speed as it approaches perigee?
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Speed increases. Conservation of energy: closer orbit means higher speed.
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This deck focuses on Motion Of Orbiting Satellites, giving you a quick way to review the definitions, rules, and examples that matter most for AP Physics 1.
Work through these flashcards in short sessions. Try to answer each prompt before flipping the card, then revisit any cards you miss until the explanation feels automatic.
Answer: Speed increases. Conservation of energy: closer orbit means higher speed.
Answer: v=T2πr. Circumference divided by period gives orbital speed.
Answer: Planets orbit in ellipses with the Sun at one focus. Describes the elliptical shape of planetary orbits.
Answer: Orbital period remains unchanged. Period depends only on orbital radius, not satellite mass.
Answer: Orbital velocity. The speed needed to maintain circular orbital motion.
Answer: Fc=rmv2. Force needed to keep a satellite in circular motion.
Answer: Higher eccentricity means more elongated orbit. Eccentricity measures how much orbit deviates from circular.
Answer: Longest radius from center to edge of ellipse. Half the longest diameter of the elliptical orbit.
Answer: Towards the center of the orbit. Centripetal force always points toward the center.
Answer: Gravitational force. Gravity provides the centripetal acceleration for orbital motion.
Answer: U=−rGMm. Negative because it's a bound system below zero reference.
Answer: They are equal: Fg=Fc. Gravitational force provides the centripetal force for orbit.
Answer: Orbit with a period equal to Earth's rotation period. Satellite appears stationary relative to Earth's surface.
Answer: T2 is proportional to r3. Period squared varies with radius cubed.
Answer: Period increases. Kepler's third law: larger orbits have longer periods.
Answer: Gravitational constant. The universal gravitational constant in Newton's law.
Answer: v=T2πr. Circumference divided by period gives orbital speed.
Answer: Force increases by a factor of 4. Force varies as 1/r2, so halving r quadruples force.
Answer: Towards the center of the orbit. Centripetal force always points toward the center.
Answer: T2 is proportional to r3. Period squared varies with radius cubed.
Answer: N m²/kg². Derived from F=Gr2m1m2 dimensional analysis.
Answer: A line from a planet to the Sun sweeps equal areas in equal times. Conservation of angular momentum causes varying speeds.
Answer: T2=GM4π2r3. Derived from setting gravitational and centripetal forces equal.
Answer: Orbital speed decreases. Larger radius requires smaller speed for stable orbit.
Answer: A line from a planet to the Sun sweeps equal areas in equal times. Conservation of angular momentum causes varying speeds.
Answer: Perigee. The closest approach point in an elliptical orbit.
Answer: Atmospheric drag. Air resistance gradually slows down low-altitude satellites.
Answer: Gravitational constant. The universal gravitational constant in Newton's law.
Answer: Elliptical. Most satellite orbits are elliptical, not perfectly circular.
Answer: Gravitational force. Gravity provides the centripetal acceleration for orbital motion.
Answer: Fc=rmv2. Force needed to keep a satellite in circular motion.
Answer: Balance of gravitational and centripetal forces. Gravitational force must equal required centripetal force.
Answer: Planets orbit in ellipses with the Sun at one focus. Describes the elliptical shape of planetary orbits.
Answer: Atmospheric drag. Air resistance gradually slows down low-altitude satellites.
Answer: Orbit. The curved path a satellite follows around a body.
Answer: Geostationary remains fixed above a point; polar passes over poles. Different orbital planes and periods serve different purposes.
Answer: F=Gr2m1m2. Newton's law of universal gravitation for any two masses.
Answer: Higher eccentricity means more elongated orbit. Eccentricity measures how much orbit deviates from circular.
Answer: Orbital speed decreases. Higher altitude means larger radius and slower speed.
Answer: Orbital speed. Constant radius and period give constant speed.
Answer: Gravitational force decreases. Gravitational force decreases with distance squared.
Answer: Apogee. The farthest point in an elliptical orbit.
Answer: They are equal: Fg=Fc. Gravitational force provides the centripetal force for orbit.
Answer: N m²/kg². Derived from F=Gr2m1m2 dimensional analysis.
Answer: Force increases by a factor of 4. Force varies as 1/r2, so halving r quadruples force.
Answer: Force increases by a factor of 4. Force is proportional to the product of both masses.
Answer: Period increases. Kepler's third law: larger orbits have longer periods.
Answer: Seconds (s). Period is a time measurement.
Answer: Orbit with a period equal to Earth's rotation period. Satellite appears stationary relative to Earth's surface.
Answer: Gravitational force. Gravity provides the centripetal acceleration for curved motion.
Answer: Gravitational force. Gravity provides the centripetal acceleration for curved motion.
Answer: F=Gr2m1m2. Newton's law of universal gravitation for any two masses.