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(Q6380)
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Statements
subclass of
trajectory
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part of
celestial mechanics
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defining formula
−
G
m
1
m
2
r
2
=
m
2
A
2
{\displaystyle -{\frac {Gm_{1}m_{2}}{r^{2}}}=m_{2}A_{2}}
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has list
list of orbits
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has quality
orbital inclination
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eccentricity
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longitude of the ascending node
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argument of periapsis
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orbital period
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periapsis
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apoapsis
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ground track
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semi-major axis
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mean anomaly
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longitude of the periapsis
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semi-minor axis
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true anomaly
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eccentric anomaly
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mean longitude
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true longitude
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mean motion
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orbital speed
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Wikidata property
orbit diagram
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type of orbit
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Sitelinks
⧼wikibase-sitelinks-mywikigroup⧽
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