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Template
:
Orbits
Language
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Change
v
t
e
Gravitational
orbits
Types
General
Box
Capture
Circular
Elliptical
/
Highly elliptical
Escape
Horseshoe
Hyperbolic trajectory
Inclined
/
Non-inclined
Kepler
Lagrange point
Osculating
Parabolic trajectory
Parking
Prograde / Retrograde
Synchronous
semi
sub
Transfer orbit
Geocentric
Geosynchronous
Geostationary
Geostationary transfer
Graveyard
High Earth
Low Earth
Medium Earth
Molniya
Near-equatorial
Orbit of the Moon
Polar
Sun-synchronous
Transatmospheric
Tundra
Very low Earth
About
other points
Mars
Areocentric
Areosynchronous
Areostationary
Lagrange points
Distant retrograde
Halo
Lissajous
Libration
Lunar
Sun
Heliocentric
Earth's orbit
Mars cycler
Heliosynchronous
Other
Lunar cycler
Parameters
Shape
Size
e
Eccentricity
a
Semi-major axis
b
Semi-minor axis
Q
,
q
Apsides
Orientation
i
Inclination
Ω
Longitude of the ascending node
ω
Argument of periapsis
ϖ
Longitude of the periapsis
Position
M
Mean anomaly
ν
,
θ
,
f
True anomaly
E
Eccentric anomaly
L
Mean longitude
l
True longitude
Variation
T
Orbital period
n
Mean motion
v
Orbital speed
t
0
Epoch
Maneuvers
Bi-elliptic transfer
Collision avoidance (spacecraft)
Delta-v
Delta-v budget
Gravity assist
Gravity turn
Hohmann transfer
Inclination change
Low-energy transfer
Oberth effect
Phasing
Rocket equation
Rendezvous
Trans-lunar injection
Transposition, docking, and extraction
Orbital
mechanics
Astronomical coordinate systems
Characteristic energy
Escape velocity
Ephemeris
Equatorial coordinate system
Ground track
Hill sphere
Interplanetary Transport Network
Kepler's laws of planetary motion
Lagrangian point
n
-body problem
Orbit equation
Orbital state vectors
Perturbation
Retrograde and prograde motion
Specific orbital energy
Specific angular momentum
Two-line elements
List of orbits
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