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(Q6380)
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Revision as of 08:20, 7 April 2023 by
Fire
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Created claim:
has quality
(P14)
:
true anomaly
(Q6449)
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Statements
subclass of
trajectory
0 references
part of
celestial mechanics
0 references
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}}
0 references
has list
list of orbits
0 references
has quality
orbital inclination
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eccentricity
0 references
longitude of the ascending node
0 references
argument of periapsis
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orbital period
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periapsis
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apoapsis
0 references
ground track
0 references
semi-major axis
0 references
mean anomaly
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longitude of the periapsis
0 references
semi-minor axis
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true anomaly
0 references
Sitelinks
⧼wikibase-sitelinks-mywikigroup⧽
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