Added satellite pass start and orbit tracks

Starting to move all sat data to SatelliteTrack

src/satellite/SatelliteTrack.java

 package satellite;
 
+import java.util.ArrayList;
+import java.util.Date;
+
+import predict4java.*;
+
 public class SatelliteTrack {
 	
-	public void getTLE(){
+	private String name;
+	private Satellite satellite;
+	private SatPassTime satPassTime;
+	private Boolean isVisible;
+	private ArrayList<satPosition> dayOrbit;
+	private ArrayList<satPosition> singleOrbit;
+	private ArrayList<satPosition> doubleOrbit;
+	private ArrayList<satPosition> tripleOrbit;
+	
+	public SatelliteTrack(String name, String[] tleData){
+		TLE tle = new TLE(tleData);
+		this.name = name;
+		this.satellite = SatelliteFactory.createSatellite(tle);
+		
+		this.satellite.calculateSatelliteVectors(new Date());
+		this.dayOrbit = getDayOrbit(this.satellite);
+		this.singleOrbit = getSingleOrbit(this.satellite);
+		this.doubleOrbit = getDoubleOrbit(this.satellite);
+		this.tripleOrbit = getTripleOrbit(this.satellite);
 		
 	}
 	
-	public void getConstillation(){
-		
+	public TLE getTLE(){
+		return this.satellite.getTLE();
+	}
+	
+	public String getConstillation(){
+		return "TBD";
 	}
 	
+	public Boolean isVisible(){
+		return isVisible;
+	}
+	
+	public ArrayList<satPosition> getDayOrbit(){
+		return dayOrbit;
+	}
+	
+	public ArrayList<satPosition> getSingleOrbit(){
+		return singleOrbit;
+	}
+	
+	public ArrayList<satPosition> getDoubleOrbit(){
+		return doubleOrbit;
+	}
 	
+	public ArrayList<satPosition> getTripleOrbit(){
+		return tripleOrbit;
+	}
+	
+	public Date getNextPassStart(GroundStationPosition gpos){
+		SatPassTime satPassTime = null;
+		Date pass = new Date(0);
+		if(!this.satellite.willBeSeen(gpos)){
+			return pass;
+		}else{
+			PassPredictor nextPass = null;
+			try {
+				nextPass = new PassPredictor(this.satellite.getTLE(),gpos);
+			} catch (IllegalArgumentException | SatNotFoundException e) {
+				// TODO Auto-generated catch block
+				e.printStackTrace();
+			}
+			try {
+				satPassTime = nextPass.nextSatPass(new Date());
+				return satPassTime.getStartTime();
+			} catch (SatNotFoundException e) {
+				// TODO Auto-generated catch block
+				e.printStackTrace();
+			}
+		}
+		return pass;
+	}
+	
+	private void updateSatPassTime(){
+		//TODO move sat pass data from getNextPass
+	}
+	
+	private 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;
+	}
+
+	private 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;
+	}
+	
+	private 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;
+	}
+
+	private 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;
+	}
 
 }