The period T of a satellite is proportional to the square root of the orbital radius r (T ∝ √r).

The time period T of a satellite is related to the orbital radius r by T ∝ r^(3/2), according to Kepler's third law.

The period T of a satellite is proportional to the square root of the orbital radius r, as given by T = 2π√(r^3/GM).

A geosynchronous satellite typically has a circular orbit to maintain a constant position relative to the Earth's surface.

The gravitational force depends on the masses of the objects and the distance between them, but not on the speed of the satellite.

The gravitational force depends on the masses and the distance, but not on the speed of the satellite.

The gravitational force on a satellite depends on its mass, the mass of the Earth, and the distance from the center of the Earth, but not on the speed of the satellite.

The mass of the satellite does not affect the orbital period; it is determined by the height of the orbit and the mass of the Earth.

The mass of the satellite does not affect its orbital speed; it is determined by the mass of the Earth and the radius of the orbit.

A polar orbiting satellite passes over the poles, allowing it to cover the entire surface of the Earth over time.

A satellite in a stable orbit does experience a net force (gravitational force), but it is in free fall, moving with constant speed along a curved path.

Escape velocity is independent of the mass of the object, but it depends on the mass and radius of the Earth.

The period of a satellite in a low Earth orbit is shorter than that of a satellite in a high Earth orbit due to the stronger gravitational pull.

A satellite in a low Earth orbit has a shorter orbital period compared to a geostationary satellite due to its closer proximity to Earth.

A satellite in a low Earth orbit has a very high orbital speed due to the proximity to the Earth and the gravitational pull.

A polar orbit allows a satellite to pass over the entire surface of the Earth as the Earth rotates beneath it.

Weather satellites typically use polar orbits to cover the entire surface of the Earth as the planet rotates beneath them.

Geostationary satellites have an orbital period equal to the Earth's rotation period, which is 24 hours.

Geostationary satellites have a period equal to the Earth's rotation period and remain in the same position relative to the Earth.

A satellite in a stable orbit is acted upon by gravitational force, which provides the necessary centripetal force to keep it in orbit.

A polar orbit allows a satellite to pass over the entire surface of the Earth as the Earth rotates beneath it.

A polar orbit allows a satellite to pass over the entire surface of the Earth as the Earth rotates beneath it.

A sun-synchronous orbit allows a satellite to pass over the same point on the Earth's surface at the same local solar time every day, as it is synchronized with the Earth's position relative to the Sun.

Geostationary satellites are ideal for monitoring weather patterns as they provide a constant view of the same area.

Geostationary orbits are ideal for weather monitoring as they provide a constant view of the same area of the Earth.