@orbinauts/engine - v0.1.2
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@orbinauts/engine - v0.1.2
Classes
ElementsError
EphemerisError
PassesNotDefinedError
PropagationError
Interfaces
AltitudeRangeKm
Apsides
BodyState
Culmination
Elements
Ephemeris
GroundPoint
GroundVelocity
Interval
Observer
Omm
OrbitPhase
Pass
PassEvent
Peak
Position
Propagator
Sampling
SpherePoint
StateVector
TrackPoint
TrackSample
VisiblePassOptions
VisibleRule
VisibleWindow
Window
WindowEdge
Type Aliases
OmmField
OrbitName
Source
VisibleRuleOptions
WindowReason
Variables
DAY_MS
EARTH_MEAN_RADIUS_KM
GEOSTATIONARY_MAX_ECCENTRICITY
GEOSTATIONARY_MAX_INCLINATION_DEGREES
GEOSTATIONARY_MEAN_MOTION
GEOSTATIONARY_MEAN_MOTION_BAND
GEOSYNCHRONOUS_MEAN_MOTION_WINDOW
HIGHLY_ELLIPTICAL_MIN_ECCENTRICITY
IN_VIEW_MIN_ELEVATION
LOW_EARTH_ORBIT_KM
NIGHT_SUN_ALTITUDE
OMM_FIELDS
ORBIT_NAMES
SIDEREAL_DAY_SECONDS
STANDARD_MAGNITUDE_RANGE_KM
VISIBLE_FAINTEST_MAGNITUDE
VISIBLE_MIN_ELEVATION
VISIBLE_RULE
WGS84_E2
WGS84_EQUATORIAL_KM
WGS84_POLAR_KM
Functions
applySourceRule
apsides
brightestPossibleMagnitude
centralAngle
circularPeriodSeconds
course
destinationPoint
ephemerisCovers
ephemerisInterval
findPasses
findVisiblePasses
footprint
footprintAngleDegrees
footprintRadiusKm
greatCircleKm
groundTrack
groundTrackByDistance
initialBearingDegrees
interpolate
isEphemeris
isGeostationary
isInView
isNakedEye
isOrbitName
isSunlit
latitudeBandDegrees
longestPassSeconds
lookAngles
nextLightChange
nightsOver
orbitalPeriodSeconds
orbitalSpeed
orbitClass
orbitPhase
parseEphemeris
positionAt
predictedMagnitude
propagate
propagator
radiiOfCurvatureKm
readElements
readTwoLineElements
semiMajorAxisKm
separationDegrees
sourceAge
speedAt
subsolarPoint
sunAltitude
toDegrees
toRadians
wrapAzimuth
wrapLongitude
Settings
Member Visibility
Protected
Inherited
External
Theme
OS
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On This Page
Classes
Elements
Error
Ephemeris
Error
Passes
Not
Defined
Error
Propagation
Error
Interfaces
Altitude
Range
Km
Apsides
Body
State
Culmination
Elements
Ephemeris
Ground
Point
Ground
Velocity
Interval
Observer
Omm
Orbit
Phase
Pass
Pass
Event
Peak
Position
Propagator
Sampling
Sphere
Point
State
Vector
Track
Point
Track
Sample
Visible
Pass
Options
Visible
Rule
Visible
Window
Window
Window
Edge
Type Aliases
Omm
Field
Orbit
Name
Source
Visible
Rule
Options
Window
Reason
Variables
DAY_
MS
EARTH_
MEAN_
RADIUS_
KM
GEOSTATIONARY_
MAX_
ECCENTRICITY
GEOSTATIONARY_
MAX_
INCLINATION_
DEGREES
GEOSTATIONARY_
MEAN_
MOTION
GEOSTATIONARY_
MEAN_
MOTION_
BAND
GEOSYNCHRONOUS_
MEAN_
MOTION_
WINDOW
HIGHLY_
ELLIPTICAL_
MIN_
ECCENTRICITY
IN_
VIEW_
MIN_
ELEVATION
LOW_
EARTH_
ORBIT_
KM
NIGHT_
SUN_
ALTITUDE
OMM_
FIELDS
ORBIT_
NAMES
SIDEREAL_
DAY_
SECONDS
STANDARD_
MAGNITUDE_
RANGE_
KM
VISIBLE_
FAINTEST_
MAGNITUDE
VISIBLE_
MIN_
ELEVATION
VISIBLE_
RULE
WGS84_
E2
WGS84_
EQUATORIAL_
KM
WGS84_
POLAR_
KM
Functions
apply
Source
Rule
apsides
brightest
Possible
Magnitude
central
Angle
circular
Period
Seconds
course
destination
Point
ephemeris
Covers
ephemeris
Interval
find
Passes
find
Visible
Passes
footprint
footprint
Angle
Degrees
footprint
Radius
Km
great
Circle
Km
ground
Track
ground
Track
By
Distance
initial
Bearing
Degrees
interpolate
is
Ephemeris
is
Geostationary
is
In
View
is
Naked
Eye
is
Orbit
Name
is
Sunlit
latitude
Band
Degrees
longest
Pass
Seconds
look
Angles
next
Light
Change
nights
Over
orbital
Period
Seconds
orbital
Speed
orbit
Class
orbit
Phase
parse
Ephemeris
position
At
predicted
Magnitude
propagate
propagator
radii
Of
Curvature
Km
read
Elements
read
Two
Line
Elements
semi
Major
Axis
Km
separation
Degrees
source
Age
speed
At
subsolar
Point
sun
Altitude
to
Degrees
to
Radians
wrap
Azimuth
wrap
Longitude
@orbinauts/engine - v0.1.2
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