Deleted satOrbit

Orbit propagation has been rolled into SatelliteTrack

src/satellite/satOrbit.java

-package satellite;
-
-import predict4java.*;
-import java.util.ArrayList;
-import java.util.Date;
-import satellite.satPosition;
-
-public class satOrbit {
-	
-	public static ArrayList<satPosition> getDayOrbit(Satellite trackedSat){
-		ArrayList<satPosition> dayOrbit	= new ArrayList<satPosition>();
-		Date now = new Date();
-		long timeNow = now.getTime();
-		for(int i = 0; i<8640;i++){						//10s of seconds in a day
-			Date increment = new Date(timeNow + i*10000);
-			trackedSat.calculateSatelliteVectors(increment);
-			dayOrbit.add(new satPosition(
-					trackedSat.calculateSatelliteGroundTrack().getLatitude(),
-					trackedSat.calculateSatelliteGroundTrack().getLongitude(),
-					trackedSat.calculateSatelliteGroundTrack().getAltitude(),
-					trackedSat.calculateSatelliteGroundTrack().getTime()));
-		}
-		System.out.println("Calculated 24hr Orbit for: " + trackedSat.getTLE().getName());
-		return dayOrbit;
-	}
-
-	public static ArrayList<satPosition> getSingleOrbit(Satellite trackedSat){
-		//Array to store orbit
-		ArrayList<satPosition> singleOrbit = new ArrayList<satPosition>();
-		Date now = new Date();
-		long timeNow = now.getTime();
-		trackedSat.calculateSatelliteVectors(now);
-		//Iterate through one orbit
-		double meanMotion = trackedSat.getTLE().getMeanmo();
-		double period = 8460/meanMotion;
-		for(int i = 0;i<period;i++){						//Seconds in a day
-			Date increment = new Date(timeNow  + i * 10000);
-			trackedSat.calculateSatelliteVectors(increment);
-			singleOrbit.add(new satPosition(
-					trackedSat.calculateSatelliteGroundTrack().getLatitude(),
-					trackedSat.calculateSatelliteGroundTrack().getLongitude(),
-					trackedSat.calculateSatelliteGroundTrack().getAltitude(),
-					trackedSat.calculateSatelliteGroundTrack().getTime()));
-		}		
-		System.out.println("Calculated Single Orbit for: " + trackedSat.getTLE().getName());
-		return singleOrbit;
-	}
-	
-	public static ArrayList<satPosition> getDoubleOrbit(Satellite trackedSat){
-		//Array to store orbit
-		ArrayList<satPosition> doubleOrbit = new ArrayList<satPosition>();
-		Date now = new Date();
-		long timeNow = now.getTime();
-		trackedSat.calculateSatelliteVectors(now);
-		//Iterate through two orbits
-		double meanMotion = trackedSat.getTLE().getMeanmo();
-		double period = 8460/meanMotion;
-		for(int i = 0;i<period*2;i++){						//Seconds in a day
-			Date increment = new Date(timeNow  + i * 10000);
-			trackedSat.calculateSatelliteVectors(increment);
-			doubleOrbit.add(new satPosition(
-					trackedSat.calculateSatelliteGroundTrack().getLatitude(),
-					trackedSat.calculateSatelliteGroundTrack().getLongitude(),
-					trackedSat.calculateSatelliteGroundTrack().getAltitude(),
-					trackedSat.calculateSatelliteGroundTrack().getTime()));
-		}		
-		System.out.println("Calculated Double Orbit for: " + trackedSat.getTLE().getName());
-		return doubleOrbit;
-	}
-
-	public static ArrayList<satPosition> getTripleOrbit(Satellite trackedSat){
-		//Array to store orbit
-		ArrayList<satPosition> tripleOrbit = new ArrayList<satPosition>();
-		Date now = new Date();
-		long timeNow = now.getTime();
-		trackedSat.calculateSatelliteVectors(now);
-		//Iterate through two orbits
-		double meanMotion = trackedSat.getTLE().getMeanmo();
-		double period = 8460/meanMotion;
-		for(int i = 0;i<period*3;i++){						//Seconds in a day
-			Date increment = new Date(timeNow  + i * 10000);
-			trackedSat.calculateSatelliteVectors(increment);
-			tripleOrbit.add(new satPosition(
-					trackedSat.calculateSatelliteGroundTrack().getLatitude(),
-					trackedSat.calculateSatelliteGroundTrack().getLongitude(),
-					trackedSat.calculateSatelliteGroundTrack().getAltitude(),
-					trackedSat.calculateSatelliteGroundTrack().getTime()));
-		}		
-		System.out.println("Calculated Triple Orbit for: " + trackedSat.getTLE().getName());
-		return tripleOrbit;
-	}
-
-}