public class LEOSatellite extends AbstractSatellite
ASTRONOMICAL_UNIT, CK4, EARTH_GRAVITATIONAL_CONSTANT, EARTH_RADIUS, EARTH_ROTATIONS_PER_SIDERIAL_DAY, EARTH_ROTATIONS_RADIANS_PER_SIDERIAL_DAY, MFACTOR, PERIGEE_156_KM, QOMS2T, RHO, S, SOLAR_RADIUS, SOLAR_RADIUS_KM, SPEED_OF_LIGHTCK2, DEG2RAD, EARTH_RADIUS_KM, EPSILON, J2_HARMONIC, J3_HARMONIC, J4_HARMONIC, TWO_PI, TWO_THIRDS, XKE| Constructor and Description |
|---|
LEOSatellite(TLE tle)
Creates a Low Earth Orbit Satellite.
|
| Modifier and Type | Method and Description |
|---|---|
protected void |
calculateSGP4(double tsince) |
calculatePhase, calculatePositionAndVelocity, calculateSatelliteGroundTrack, calculateSatelliteVectors, calculateSatPosForGroundStation, converge, getEclipseDepth, getPosition, getQoms24, getS4, getTLE, invert, julianDateOfYear, magnitude, mod2PI, setPerigee, sqr, willBeSeenpublic LEOSatellite(TLE tle)
tle - the three line elementsCopyright © 2014–2019. All rights reserved.