What affects the speed of satellites?

Answer 1

The speed of a satellite in its orbit depends only on its distance from Earth (or other parent body, e.g., Jupiter). For a circular orbit, this velocity is given by balancing gravitational and centripetal acceleration:

v^2/r = GM/r^2

or

v = sqrt(GM/r),

where G is the gravitational constant, M the mass of the planet, and r the distance from the center of mass. Some satellites have elliptical orbits, in which case their speed is greatest at closest approach ("periapse") and slowest at the furthest point in the orbit ("apoapse").

Drag is an extremely slow process for most satellites in Earth orbit.

Answer 2

Satellites in low Earth orbit and the Space Station and Shuttle are affected by a very thin portion of the atmosphere to a much greater extent than a satellites in geosynchronous orbits which are many many times farther out in space. Low Earth orbit is up to 1240 miles whereas geosynchronous orbit is 22,400 Miles.

Answer 3

Theoretically, nothing, because they travel through vacuum. However, the vacuum of space is not perfect, so there is some drag which slows satellites down ever so slowly, so that eventually their orbits decay and they disintegrate upon entry into the atmosphere.

Answer 4

Gravity

Answer 5

The speed depends on the distance from the planet.

Answer 6

I guess the nature of this question is related to satilitte TV, Internet, etc... Weather mostly..

Answer 7

Gravity, mostly.

Answer 8

The speed of a satellite is what determines its orbit.

The biggest threat to the speed of a satellite is friction from the atmosphere, which extends in some trace form beyond most of our satellites. Gravity is what keeps it in orbit.

A satellite is in free fall, as it falls around the earth. It doesn't hit the earth because it is traveling fast enough to not hit, but it is not traveling fast enough to escape the gravity of the earth. The range here is quite wide and allows satellites to be put at various orbits.

The most important orbit is a geocentric orbit because that keeps a satellite in the same place with respect to the revolution of the earth. This is how we position our GPS satellites so we can use them to determine our position; they are at a fixed point (relative to the earth).

The odd thing about a satellite orbit is that if you go higher you will slow down, because of gravity. To speed up you only have to move to a lower orbit. However, the faster you are going the higher orbit you can reach.

According to Wikipedia: http://en.wikipedia.org/wiki/Satellite#Orbit_types
“Orbit types
Centric Classifications
Galacto-centric Orbit - An orbit about the center of a galaxy. Earth's sun follows this type of orbit about the galactic center of the Milky Way.
Heliocentric Orbit - An orbit around the Sun. In our Solar System, all planets, comets, and asteroids are in such orbits, as are many artificial satellites and pieces of space debris. Moons by contrast are not in a heliocentric orbit but rather orbit their parent planet.
Geocentric Orbit - An orbit around the planet Earth, such as the Moon or artificial satellites. Currently there are approximately 2465 artificial satellites orbiting the Earth.
Areocentric Orbit - An orbit around the planet Mars, such as moons or artificial satellites.
Altitude Classifications
Low Earth Orbit (LEO) - Geocentric orbits ranging in altitude from 0 - 2,000 km (0 - 1,240 miles)
Medium Earth Orbit (MEO) - Geocentric orbits ranging in altitude from 2,000 km (1,240 miles) - to just below geosynchronous orbit at 35,786 km (22,240 miles). Also known as an intermediate circular orbit.
High Earth Orbit (HEO) - Geocentric orbits above the altitude of geosynchronous orbit 35,786 km (22,240 miles).
Inclination Classifications
Inclined Orbit - An orbit whose inclination in reference to the equatorial plane is not 0.
Polar Orbit - An orbit that passes above or nearly above both poles of the planet on each revolution. Therefore it has an inclination of (or very close to) 90 degrees.
Polar sun synchronous orbit - A nearly polar orbit that passes the equator at the same local time on every pass. Useful for image taking satellites because shadows will be the same on every pass.
Eccentricity Classifications
Circular Orbit - An orbit that has an eccentricity of 0 and whose path traces a circle.
Hohmann transfer orbit - An orbital maneuver that moves a spacecraft from one circular orbit to another using two engine impulses. This maneuver was named after Walter Hohmann.
Elliptic Orbit - An orbit with an eccentricity greater than 0 and less than 1 whose orbit traces the path of an ellipse.
Geosynchronous Transfer Orbit - An elliptic orbit where the perigee is at the altitude of a Low Earth Orbit (LEO) and the apogee at the altitude of a geosynchronous orbit.
Geostationary Transfer Orbit - An elliptic orbit where the perigee is at the altitude of a Low Earth Orbit (LEO) and the apogee at the altitude of a geostationary orbit.
Molniya Orbit - A highly elliptic orbit with inclination of 63.4° and orbital period of ½ of a sidereal day (roughly 12 hours). Such a satellite spends most of its time over a designated area of the planet.
Tundra Orbit - A highly elliptic orbit with inclination of 63.4° and orbital period of one sidereal day (roughly 24 hours). Such a satellite spends most of its time over a designated area of the planet.
Hyperbolic orbit - An orbit with the eccentricity greater than 1. Such an orbit also has a velocity in excess of the escape velocity and as such, will escape the gravitational pull of the planet and continue to travel infinitely.
Parabolic Orbit - An orbit with the eccentricity equal to 1. Such an orbit also has a velocity equal to the escape velocity and therefore will escape the gravitational pull of the planet and travel until its velocity relative to the planet is 0. If the speed of such an orbit is increased it will become a hyperbolic orbit.
Escape Orbit (EO) - A high-speed parabolic orbit where the object has escape velocity and is moving away from the planet.
Capture Orbit - A high-speed parabolic orbit where the object has escape velocity and is moving toward the planet.
Synchronous Classifications
Synchronous Orbit - An orbit where the satellite has an orbital period equal to the average rotational period (earth's is: 23 hours, 56 minutes, 4.091 seconds) of the body being orbited and in the same direction of rotation as that body. To a ground observer such a satellite would trace an analemma (figure 8) in the sky.
Semi-Synchronous Orbit (SSO) - An orbit with an altitude of approximately 20,200 km (12544.2 miles) and an orbital period of approximately 12 hours
Geosynchronous Orbit (GEO) - Orbits with an altitude of approximately 35,786 km (22,240 miles). Such a satellite would trace an analemma (figure 8) in the sky.
Geostationary orbit (GSO): A geosynchronous orbit with an inclination of zero. To an observer on the ground this satellite would appear as a fixed point in the sky.
Clarke Orbit - Another name for a geostationary orbit. Named after the writer Arthur C. Clarke.
Supersynchronous orbit - A disposal / storage orbit above GSO/GEO. Satellites will drift west. Also a synonym for Disposal Orbit.
Subsynchronous orbit - A drift orbit close to but below GSO/GEO. Satellites will drift east.
Graveyard Orbit - An orbit a few hundred kilometers above geosynchronous that satellites are moved into at the end of their operation.
Disposal Orbit - A synonym for graveyard orbit.
Junk Orbit - A synonym for graveyard orbit.
Areosynchronous Orbit - A synchronous orbit around the planet Mars with an orbital period equal in length to Mars' sidereal day, 24.6229 hours.
Areostationary Orbit (ASO) - A circular areosynchronous orbit on the equatorial plane and about 17,000 km(10557 miles) above the surface. To an observer on the ground this satellite would appear as a fixed point in the sky.
Heliosynchronous Orbit - An heliocentric orbit about the Sun where the satellite's orbital period matches the Sun's period of rotation. These orbits occur at a radius of 24.360 Gm (0.1628 AU) around the Sun, a little less than half of the orbital radius of Mercury.
Special Classifications
Sun-synchronous Orbit - An orbit which combines altitude and inclination in such a way that the satellite passes over any given point of the planets's surface at the same local solar time. Such an orbit can place a satellite in constant sunlight and is useful for imaging, spy, and weather satellites.
Moon Orbit - The orbital characteristics of earth's moon. Average altitude of 384,403 kilometres (238,857 mi), elliptical-inclined orbit.
Pseudo-Orbit Classifications
Horseshoe Orbit - An orbit that appears to a ground observer to be orbiting a certain planet but is actually in co-orbit with the planet. See asteroids 3753 (Cruithne) and 2002 AA29.
Exo-orbit - A maneuver where a spacecraft approaches the height of orbit but lacks the velocity to sustain it.
Orbital Spaceflight - A synonym for Exo-orbit.
Lunar transfer orbit (LTO) -
Prograde Orbit - An orbit with an inclination of less than 90°. Or rather, an orbit that is in the same direction as the rotation of the primary.
Retrograde orbit - An orbit with an inclination of more than 90°. Or rather, an orbit counter to the direction of rotation of the planet. Apart from those in Sun-synchronous orbit, few satellites are launched into retrograde orbit because the quantity of fuel required to launch them is much greater than for a prograde orbit. This is because when the rocket starts out on the ground, it already has an eastward component of velocity equal to the rotational velocity of the planet at its launch latitude.

Satellites can also orbit Lagrangian Points.