Longitude of the periapsis
This article may be confusing or unclear to readers. Please help us clarify the article; suggestions may be found on the talk page. (July 2009)
In celestial mechanics, the longitude of the periapsis (symbolized ϖ) of an orbiting body is the longitude (measured from the point of the vernal equinox) at which the periapsis (closest approach to the central body) would occur if the body's inclination were zero. For...
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Rabu, 30 April 2014
Parameters - Argument Of Periapsis
Argument of periapsis
The argument of periapsis (also called argument of perifocus or argument of pericenter), symbolized as ω, is one of the orbital elements of an orbiting body. Specifically, ω is the angle between the orbit's periapsis (the point of closest approach to the central point) and the orbit's ascending node (the point where the body crosses the plane of reference from South to North). The angle is measured in the orbital plane...
Parameters - Longitude Of The Asending Node
Longitude of the ascending node
This article may be confusing or unclear to readers. Please help us clarify the article; suggestions may be found on the talk page. (July 2009)
The longitude of the ascending node.
The longitude of the ascending node (☊ or Ω) is one of the orbital elements used to specify the orbit of an object in space. It is the angle from a reference direction, called the origin of longitude, to the direction...
Paramaters - Azimuth
Azimuth
The azimuth is the angle formed between a reference direction (North)
and a line from the observer to a point of interest projected on the
same plane as the reference direction
An azimuth (i/ˈæzɪməθ/) is an angular measurement in a spherical coordinate system. The vector from an observer (origin) to a point of interest is projected perpendicularly onto a reference plane; the angle between the projected vector and a reference vector...
Parameters - Horizontal Coordinate System
Horizontal coordinate system
Azimuth is measured from the north point (sometimes from the south
point) of the horizon around to the east; altitude is the angle above
the horizon.
The horizontal coordinate system is a celestial coordinate system that uses the observer's local horizon as the fundamental plane. This coordinate system divides the sky into the upper hemisphere where objects are visible, and the lower hemisphere where objects...
Parameters - Orbital inclination Change
Orbital inclination change
Orbital inclination change is an orbital maneuver aimed at changing the inclination of an orbiting body's orbit.
This maneuver is also known as an orbital plane change as the plane of
the orbit is tipped. This maneuver requires a change in the orbital
velocity vector (delta v) at the orbital nodes
(i.e. the point where the initial and desired orbits intersect, the
line of orbital nodes is defined by the intersection of the two orbital
planes).
In general, inclination changes can take a very large amount of...
Parameters - Orbital Inclination
Orbital inclination
Fig. 1: One view of inclination i (green) and other orbital parameters
Inclination in general is the angle between a reference plane and another plane or axis of direction.
&nb...
Parameters - Eccentricity
Orbital eccentricity
An elliptic Kepler orbit with an eccentricity of 0.7 (red ellipse), a
parabolic Kepler orbit (green) and a hyperbolic Kepler orbit with an
eccentricity of 1.3 (blue outer line)
The orbital eccentricity of an astronomical object is a
parameter that determines the amount by which its orbit around another
body deviates from a perfect circle. A value of 0 is a circular orbit, values between 0 and 1 form an elliptical...
Parameters - Apsis
Apsis
"Apogee", "Aphelion", "Perigee" and "Perihelion" redirect here. For the literary journal, see Perigee: Publication for the Arts. For Edenbridge's Album, see Aphelion (album). For the architectural term, see Apse. For other uses, see Apogee (disambiguation) and Perihelion (disambiguation).
Apsides 1) Apoapsis; 2) Periapsis; 3)
Focus
An apsis (Greek ἁψίς, gen. ἁψίδος), plural apsides (/ˈæpsɨdiːz/; Greek: ἁψίδες), is a point of greatest...
Parameters - Semi-minor Axis
Semi-minor axis
The semi-major (in red*) and semi-minor axis (in blue*) of an ellipse.
(* on some browsers)
In geometry, the semi-minor axis (also semiminor axis) is a line segment associated with most conic sections (that is, with ellipses and hyperbolas) that is at right angles with the semi-major axis and has one end at the center of the conic section. It is one of the axes of symmetry for the curve: in an ellipse, the shorter one;...
Parameters - Semi-major Axis
Semi-major axis
The semi-major and semi-minor axis of an ellipse
In geometry, the major axis of an ellipse is the longest diameter: a line (line segment) that runs through the center and both foci, with ends at the widest points of the shape. The semi-major axis is one half of the major axis, and thus runs from the centre, through a focus,
and to the edge of the ellipse; essentially, it is the radius of an
orbit at the orbit's two most...
Orbit - Geostationary Orbit
Geostationary orbit
Geostationary orbits (top view). To an observer on the rotating Earth,
both satellites appear stationary in the sky at their respective
locations.
Geostationary orbits (side view)
A 5 × 6 degree view of a part of the geostationary belt, showing several
geostationary satellites. Those with inclination 0 degrees form a
diagonal belt across the image; a few objects with small inclinations to
the Equator...
Orbit - Aerosynchronous Orbit
Areosynchronous orbit
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's 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.
The orbital altitude
required to maintain an areosynchonous orbit is...
Orbit - Circular Orbit
Circular orbit
A circular orbit is depicted in the top-left quadrant of this diagram, where the gravitational potential well
of the central mass shows potential energy, and the kinetic energy of
the orbital speed is shown in red. The height of the kinetic energy
remains constant throughout the constant speed circular orbit.
For other meanings of the term "orbit", see orbit (disambiguation)
A circular orbit is the orbit at a fixed...
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