Index

A

altitude_from_radius() (in module orbital.utilities) angular_momentum() (in module orbital.utilities)

apply_maneuver() (orbital.elements.KeplerianElements method)

C

change_apocenter_by() (orbital.maneuver.Maneuver class method) change_inclination_by() (orbital.maneuver.Maneuver class method) change_pericenter_by() (orbital.maneuver.Maneuver class method) ChangeApocenterBy (class in orbital.maneuver)

ChangeInclinationBy (class in orbital.maneuver) ChangePericenterBy (class in orbital.maneuver) Circularise (class in orbital.maneuver)

E

E (orbital.elements.KeplerianElements attribute) eccentric_anomaly_from_mean() (in module orbital.utilities) eccentric_anomaly_from_true() (in module orbital.utilities)

eccentricity_vector() (in module orbital.utilities) elements_for_apsides() (in module orbital.utilities) epoch (orbital.elements.KeplerianElements attribute)

F

f (orbital.elements.KeplerianElements attribute) from_state_vector() (orbital.elements.KeplerianElements class method)

from_tle() (orbital.elements.KeplerianElements class method)

H

hohmann_transfer_to_altitude() (orbital.maneuver.Maneuver class method)

hohmann_transfer_to_radius() (orbital.maneuver.Maneuver class method)

K

KeplerianElements (class in orbital.elements)

M

M (orbital.elements.KeplerianElements attribute) Maneuver (class in orbital.maneuver)

mean_anomaly_from_eccentric() (in module orbital.utilities) mean_anomaly_from_true() (in module orbital.utilities)

N

n (orbital.elements.KeplerianElements attribute)

node_vector() (in module orbital.utilities)

O

orbit_radius() (in module orbital.utilities) orbital.bodies (module) orbital.elements (module)

orbital.maneuver (module), [1] orbital.plotting (module) orbital.utilities (module)

P

plot() (in module orbital.plotting) plot2d() (in module orbital.plotting) plot3d() (in module orbital.plotting) Plotter2D (class in orbital.plotting) Plotter3D (class in orbital.plotting)

position (orbital.utilities.StateVector attribute) propagate_anomaly_by() (orbital.elements.KeplerianElements method) propagate_anomaly_to() (orbital.elements.KeplerianElements method) PropagateAnomalyBy (class in orbital.maneuver) PropagateAnomalyTo (class in orbital.maneuver)

R

r (orbital.elements.KeplerianElements attribute)

radius_from_altitude() (in module orbital.utilities)

S

set_apocenter_altitude_to() (orbital.maneuver.Maneuver class method) set_apocenter_radius_to() (orbital.maneuver.Maneuver class method) set_inclination_to() (orbital.maneuver.Maneuver class method) set_pericenter_altitude_to() (orbital.maneuver.Maneuver class method) set_pericenter_radius_to() (orbital.maneuver.Maneuver class method) SetApocenterAltitudeTo (class in orbital.maneuver) SetApocenterRadiusTo (class in orbital.maneuver)

SetInclinationTo (class in orbital.maneuver) SetPericenterAltitudeTo (class in orbital.maneuver) SetPericenterHere (class in orbital.maneuver) SetPericenterRadiusTo (class in orbital.maneuver) specific_orbital_energy() (in module orbital.utilities) StateVector (class in orbital.utilities)

T

T (orbital.elements.KeplerianElements attribute) t (orbital.elements.KeplerianElements attribute)

true_anomaly_from_eccentric() (in module orbital.utilities) true_anomaly_from_mean() (in module orbital.utilities)

U

U (orbital.elements.KeplerianElements attribute) UVW (orbital.elements.KeplerianElements attribute)

uvw_from_elements() (in module orbital.utilities)

V

V (orbital.elements.KeplerianElements attribute) v (orbital.elements.KeplerianElements attribute)

velocity (orbital.utilities.StateVector attribute)

W

W (orbital.elements.KeplerianElements attribute) with_altitude() (orbital.elements.KeplerianElements class method) with_apside_altitudes() (orbital.elements.KeplerianElements class method)

with_apside_radii() (orbital.elements.KeplerianElements class method) with_period() (orbital.elements.KeplerianElements class method)