Keplerian orbital elements

E157395

Keplerian orbital elements are a set of parameters that uniquely describe the size, shape, and orientation of an orbit and the position of an orbiting body along that path.

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Label Occurrences
Keplerian orbital elements canonical 1

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Statements (49)

Predicate Object
instanceOf astronomical concept
orbital elements
advantage provide intuitive geometric interpretation of orbits
appliesTo bound orbits
elliptical orbits
hyperbolic orbits
parabolic orbits
unbound orbits
assumes Newtonian celestial mechanics
surface form: Newtonian gravity

two-body problem
canBeExpressedAs mean orbital elements
osculating orbital elements
component argument of periapsis
eccentricity
inclination
longitude of ascending node
mean anomaly
mean motion
orbital period
semi-major axis
time of periapsis passage
true anomaly
contrastedWith Cartesian state vectors
coordinateSystemType osculating elements
definesReferenceDirection reference direction in the reference plane
definesReferencePlane fundamental reference plane
dependsOn standard gravitational parameter of central body
describes orientation of an orbit
position of an orbiting body along its orbit
shape of an orbit
size of an orbit
domain orbital mechanics
frame typically defined in an inertial reference frame
hasLimitation do not remain constant under perturbations
less accurate over long time spans with strong perturbations
mathematicalNature set of six independent parameters
namedAfter Johannes Kepler
relatedTo Kepler’s laws of planetary motion
surface form: Kepler's laws of planetary motion
standardizedIn Two-Line Element set format
usedBy astronomers
mission planners
space engineers
usedIn astrodynamics
celestial mechanics
orbit prediction
satellite tracking
spacecraft orbit determination
usedToCompute position vector in inertial space
velocity vector in inertial space

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Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

Gauss’s planetary equations appliesTo Keplerian orbital elements