Index

A

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

apocenter_altitude (orbital.elements.KeplerianElements property) apocenter_radius (orbital.elements.KeplerianElements property) 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)

E

E (orbital.elements.KeplerianElements property) 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 property)

F

f (orbital.elements.KeplerianElements property)

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 property) Maneuver (class in orbital.maneuver) mean_anomaly_from_eccentric() (in module orbital.utilities) mean_anomaly_from_true() (in module orbital.utilities) module orbital.bodies orbital.elements orbital.maneuver orbital.plotting orbital.utilities

N

n (orbital.elements.KeplerianElements property)

node_vector() (in module orbital.utilities)

O

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

orbital.plotting module orbital.utilities module OrbitalWarning

P

pericenter_altitude (orbital.elements.KeplerianElements property) pericenter_radius (orbital.elements.KeplerianElements property) 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 (class in orbital.utilities) position (orbital.utilities.StateVector attribute) propagate_anomaly_by() (orbital.elements.KeplerianElements method) propagate_anomaly_to() (orbital.elements.KeplerianElements method)

R

r (orbital.elements.KeplerianElements property)

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) specific_orbital_energy() (in module orbital.utilities) StateVector (class in orbital.utilities)

T

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

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

U

U (orbital.elements.KeplerianElements property)

UVW (orbital.elements.KeplerianElements property) uvw_from_elements() (in module orbital.utilities)

V

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

Velocity (class in orbital.utilities) velocity (orbital.utilities.StateVector attribute)

W

W (orbital.elements.KeplerianElements property) 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)