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.

All labels observed (1)

Label Occurrences
Keplerian orbital elements canonical 2

How this entity was disambiguated

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 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 ⓘ
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 ⓘ

How these facts were elicited

Referenced by (2)

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

Gauss’s planetary equations → appliesTo → Keplerian orbital elements ⓘ
Delaunay variables → basedOn → Keplerian orbital elements ⓘ