Tundra orbit

From Wikipedia, the free encyclopedia

Tundra orbit is a type of highly elliptical orbit with an inclination of 63.4° and orbital period of one sidereal day (almost 24 hours). A satellite placed in this orbit spends most of its time over a chosen area of the Earth, a phenomenon known as apogee dwell.

These are conceptually similar to Molniya orbits which have the same inclination but half the period (about 12 hours).

[edit] References

Sample Mission Analysis from the Danish Space Research Institute (see page 8).

[edit] See also

List of orbits

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