Physics
Gravitation and Orbital Mechanics
522 Questions
Gravitation and orbital mechanics focus on planetary motion, elliptical orbits, and satellite deployment. Questions examine astrodynamics fundamentals, including geostationary orbits and perturbation theory. These topics are highly relevant for civil services and specialized technical examinations.
Planetary orbitsSatellite dynamicsGeostationary orbitsPerturbation theoryOrbital eccentricity
Gravitation and Orbital Mechanics Questions
What is the parameter that describes the shape of an orbit?
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Eccentricity
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Semi-major axis
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Inclination
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Argument of periapsis
A
Correct answer
Explanation
Eccentricity is a dimensionless parameter that describes the shape of an orbit. It is defined as the ratio of the distance between the focus and the center of the ellipse to the semi-major axis.
What is the parameter that describes the size of an orbit?
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Eccentricity
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Semi-major axis
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Inclination
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Argument of periapsis
B
Correct answer
Explanation
The semi-major axis is the average distance between an orbiting body and the body it is orbiting.
What is the parameter that describes the orientation of an orbit in space?
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Eccentricity
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Semi-major axis
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Inclination
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Argument of periapsis
C
Correct answer
Explanation
Inclination is the angle between the orbital plane of an object and the reference plane.
What is the parameter that describes the position of an object in its orbit at a given time?
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True anomaly
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Mean anomaly
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Eccentric anomaly
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Argument of periapsis
A
Correct answer
Explanation
True anomaly is the angle between the periapsis and the current position of an object in its orbit.
What is the parameter that describes the average position of an object in its orbit?
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True anomaly
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Mean anomaly
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Eccentric anomaly
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Argument of periapsis
B
Correct answer
Explanation
Mean anomaly is the angle between the periapsis and the current position of an object in its orbit, averaged over time.
What is the parameter that describes the eccentric anomaly of an object in its orbit?
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True anomaly
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Mean anomaly
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Eccentric anomaly
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Argument of periapsis
C
Correct answer
Explanation
Eccentric anomaly is the angle between the periapsis and the current position of an object in its orbit, as seen from the center of the ellipse.
What is the parameter that describes the time it takes for an object to complete one orbit?
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Orbital period
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Sidereal period
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Synodic period
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Anomalistic period
A
Correct answer
Explanation
Orbital period is the time it takes for an object to complete one orbit around another object.
What is the parameter that describes the time it takes for an object to return to the same position in the sky as seen from Earth?
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Orbital period
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Sidereal period
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Synodic period
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Anomalistic period
B
Correct answer
Explanation
Sidereal period is the time it takes for an object to return to the same position in the sky as seen from Earth.
What is the parameter that describes the time it takes for an object to return to the same position relative to the Sun as seen from Earth?
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Orbital period
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Sidereal period
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Synodic period
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Anomalistic period
C
Correct answer
Explanation
Synodic period is the time it takes for an object to return to the same position relative to the Sun as seen from Earth.
What is the parameter that describes the time it takes for an object to return to the same perigee?
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Orbital period
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Sidereal period
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Synodic period
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Anomalistic period
D
Correct answer
Explanation
Anomalistic period is the time it takes for an object to return to the same perigee.
What is the parameter that describes the rate at which the eccentric anomaly changes?
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Mean motion
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True motion
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Eccentric motion
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Anomalistic motion
C
Correct answer
Explanation
Eccentric motion is the rate at which the eccentric anomaly changes.
What are the three main types of satellite orbits?
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Geostationary, polar, and sun-synchronous.
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Low Earth orbit, medium Earth orbit, and high Earth orbit.
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Circular, elliptical, and parabolic.
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Prograde, retrograde, and polar.
A
Correct answer
Explanation
The three main types of satellite orbits are geostationary, polar, and sun-synchronous.
What is the difference between a geostationary and a polar orbit?
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Geostationary satellites orbit the Earth at a constant altitude, while polar satellites orbit the Earth at a varying altitude.
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Geostationary satellites orbit the Earth at a constant speed, while polar satellites orbit the Earth at a varying speed.
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Geostationary satellites orbit the Earth in a circular orbit, while polar satellites orbit the Earth in an elliptical orbit.
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Geostationary satellites orbit the Earth in a prograde orbit, while polar satellites orbit the Earth in a retrograde orbit.
A
Correct answer
Explanation
Geostationary satellites orbit the Earth at a constant altitude of 35,786 kilometers, while polar satellites orbit the Earth at a varying altitude of 800 to 1,000 kilometers.
What is the difference between a sun-synchronous and a non-sun-synchronous orbit?
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Sun-synchronous satellites orbit the Earth in a way that keeps them in constant sunlight, while non-sun-synchronous satellites orbit the Earth in a way that takes them through both sunlight and darkness.
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Sun-synchronous satellites orbit the Earth at a constant altitude, while non-sun-synchronous satellites orbit the Earth at a varying altitude.
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Sun-synchronous satellites orbit the Earth at a constant speed, while non-sun-synchronous satellites orbit the Earth at a varying speed.
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Sun-synchronous satellites orbit the Earth in a circular orbit, while non-sun-synchronous satellites orbit the Earth in an elliptical orbit.
A
Correct answer
Explanation
Sun-synchronous satellites orbit the Earth in a way that keeps them in constant sunlight, while non-sun-synchronous satellites orbit the Earth in a way that takes them through both sunlight and darkness.
What is the term used to describe the process by which an exoplanet's orbit becomes more elliptical over time?
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Orbital eccentricity
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Orbital precession
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Orbital resonance
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Orbital decay
A
Correct answer
Explanation
Orbital eccentricity is the term used to describe the process by which an exoplanet's orbit becomes more elliptical over time.