orbit library

TLE and NORAD SGP4/SDP4/SGP8/SDP8 Implementation for Dart and Flutter.

Classes

KeplerianElements
The Keplerian Elements.
Orbit
Orbit data.
OrbitalState
RV Pair for satellite state.
OrbitPoint
An orbital point in time.
Pass
Satellite pass.
PassPoint
SGP4
SGP4 Calculator.
TwoLineElement
Represents a TLE record.

Functions

getMoonLocation(DateTime utcNow) → LatLng
Calculates the Moon position on a given UTC time.
getSunLocation(DateTime utcNow) → LatLng
Calculates the Sun position on a given UTC time.
getSunLookAngle(DateTime utc, LatLng observer, double altitude) → LookAngle
Calculates the look angles for the specified observer.

Exceptions / Errors

PropagationException
Propagation Exception.