Areosynchronous orbit

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Areosynchronous orbits are class of synchronous orbits for artificial satellites around the planet Mars. As with all synchronous orbits, an areosynchronous orbit has an orbital period equal in length to Mars' sidereal day. A satellite in areosynchronous orbit does not necessarily maintain a fixed position in the sky as seen by an observer on the surface of Mars, however such a satellite will return to the same apparent position every Martian day.

An areosynchronous orbit that is equatorial (in the same plane as the equator of Mars), circular, and prograde (rotating about Mars' axis in the same direction as the planet's surface) is known as an areostationary orbit (ASO). To an observer on the surface of Mars, the position of a satellite in ASO would appear to be fixed in a constant position in the sky. The ASO is analogous to a geostationary orbit (GSO) about Earth.

Although no satellites currently occupy areosynchronous or areostationary orbits, some scientists foresee a future telecommunications network for the exploration of Mars.

List of orbits

Mars Network - Marsats - NASA site devoted to future communications infrastructure for Mars exploration

v • d • e Orbits

Orbit types by characteristics:	Box orbit \| Circular orbit \| Ecliptic orbit \| Elliptic orbit \| Highly Elliptical Orbit \| Graveyard orbit \| Hyperbolic trajectory \| Inclined orbit \| Osculating orbit \| Parabolic trajectory \| Capture orbit \| Escape orbit \| Semi-synchronous orbit \| Subsynchronous orbit \| Synchronous orbit
Earth-centered orbits:	Geosynchronous orbit \| Geostationary orbit \| Sun-synchronous orbit \| Low Earth orbit \| Medium Earth Orbit \| Molniya orbit \| Near equatorial orbit \| Orbit of the Moon \| Polar orbit \| Polar sun synchronous orbit \| Tundra orbit
Orbits about other bodies:	Areosynchronous orbit \| Areostationary orbit \| Lunar orbit \| Heliocentric orbit \| Heliosynchronous orbit

Orbital elements:	Inclination ( $i\,\!$ ) \| Longitude of the ascending node ( $\Omega\,\!$ ) \| Eccentricity ( $e\,\!$ ) \| Argument of periapsis ( $\omega\,\!$ ) \| Semimajor axis ( $a\,\!$ ) \| Mean anomaly at epoch ( $M_o\,\!$ )
Other orbital parameters:	True anomaly ( $v\,$ ) \| Semi-major axis ( $a\,$ ) \| Semi-minor axis ( $b\,$ ) \| Linear eccentricity ( $\epsilon\,$ ) \| Eccentric anomaly ( $E\,$ ) \| Mean longitude ( $L\,$ ) \| True longitude ( $l\,$ ) \| Orbital period ( $T\,$ )
Orbital maneuvers:	Bi-elliptic transfer \| Geostationary transfer orbit \| Gravitational slingshot \| Hohmann transfer orbit \| Orbital inclination change \| Orbit phasing \| Space rendezvous

Other orbital mechanics topics:	Apsis \| Celestial coordinate system \| Delta-v budget \| Epoch \| Ephemeris \| Equatorial coordinate system \| Ground track \| Interplanetary Transport Network \| Kepler's laws of planetary motion \| Lagrangian point \| List of orbits \| n-body problem \| Orbit equation \| Orbital state vectors \| Retrograde and direct motion \| Specific orbital energy \| Specific relative angular momentum