Geostationary
      Satellites
    
      A geostationary (Earth) satellite is a satellite that rotates
      around Earth in a certain orbit such that it is always positioned
      above the same point on the Earth’s surface.  Hence from the
      point of view of an observer standing at that point, the
      geostationary satellite appears to be always ‘stationary’ above
      him/her (but actually, both observer and satellite are rotating at
      the same angular speed). In order for a satellite to be moving in
      such a geostationary orbit, there are certain conditions to
      meet: 
    
    Characteristics
      of Geostationary satellites
    
      - placed vertically above the equator
 
      - same direction sense as the rotation of the Earth (determine
        through axis of rotation)
 
      - same orbital period of Planet, in our case, Earth orbital
        period of  approximately 24 hrs
 
    
    Determination
      of height above Earth surface for geostationary orbit radius.
    Analyzing the
      free body diagram of a satellite traveling in a geostationary
      oribt, we know the force on the satellite is assumed to be only
      due to Earth's gravitational pull,  the period is
      approximately 24 hours = (24)(60)(60) = 86400 s
    
    
    r = 4.23x107 m which is r =
      3.59x107 +
      6.37x106 m
    which is why
      Earth's geostationary satellites must be placed in an orbit
      at a fixed distance (around 35 700 km) from the Earth’s surface,
      in order to rotate with the same period as Earth. 
    Advantages
      of geostationary satellites:
    
    
      - A geostationary satellite is ideal for telecommunication
        purposes since it remains ‘stationary’ above the same spot on
        the Earth’s surface at all times. The distance between the
        satellite and the transmitting station on Earth is kept
        relatively constant and a clear line of ‘vision’ between the
        transmitter and the receiver allows continuous and uninterrupted
        signal transmission.
 
      - Since it is always at the same relative position above the
        Earth’s surface, there is no need to keep adjusting the
        direction of the satellite dish to receive signals from the
        geostationary satellite.
 
      - As geostationary satellites are positioned at a high altitude
        (a distance of 3.57 × 107 m away from the
        surface of the Earth), it can view a large section of the Earth
        and scan the same area frequently. Hence, they are ideal for
        meteorological applications and remote imaging.
 
    
    Disadvantages
      of geostationary satellites:
    
    
      - As geostationary satellites are positioned at such a high
        altitude, the resolution of the images may not be as good as
        those captured by the lower orbiting satellites (example shown
        is polar orbits at R=1.133Rearth with orbital period
        of 2 hours).
 
      - Because of its high altitude, there may be a delay in the
        reception of the signals resulting in a lag time for live
        international broadcast or video conferencing.
 
      
The
        transmitting stations in countries positioned at latitudes
        higher than 60 degrees may not be able to receive strong signals
        from geostationary satellites, as the signals would have to pass
        through a large amount of atmosphere. This is true for countries
        beyond the 60 degrees latitude ‘belt’, both on north and south
        sides. 
    
    
      Besides geostationary satellites which are placed at a large
      distance from Earth, there are other types of satellite which
      orbit at lower altitudes from Earth, like the polar orbit
      satellites as shown below.
      
    Satellites in polar orbits rotate around
      the Earth over the poles, in a constant plane perpendicular to the
      equator. Polar satellites have much lower altitudes (about 850km
      or R=1.133Rearth with
      orbital period of 2 hour) which serve to provide more detailed
      information about the weather and cloud formation. However
      satellites in this type of orbit can view only a narrow strip of
      Earth's surface on each orbit. Strips of images must be "stitched
      together," to produce a larger view. 
    Example
    Determine the typical orbital radius of
      a geostationary satellite around Earth. (Given:  mass of
      Earth = 6.0 x 1024 kg)
    
    Answer
    The orbital period for geostationary
      satellite = period of rotation of Earth = 24 hours
    Thus, T = 24 hr x 60 min x 60 sec = 8.64
      x 104 s
    assuming that only the gravitational
      force acts on the satellite moving in an ideal circular motion
      acceleration
    
    
    
    r = 4.23x107 m 
    Would
      a geostationary satellite that orbit around planet Mars be at the
      same distance r (= 4.2 x 107 m), be r = 4.23x107 m ? Why?
    
    referring the data from https://en.wikipedia.org/wiki/Mars, MMars = 6.4185×1023 kg,
      Sidereal rotation period T =1.025957 day.
    
    r =2.04x107 m,
      thus it is different due to the different planet mass and rotation
      period
    
    Example 
      (J2000/1/8)
    Which quantity is not necessarily the
      same for satellites that are in geostationary orbits around the
      Earth?
    
    A    angular
      velocity           
      C    kinetic energy
    B    centripetal
      acceleration       
      D    orbital period
    
    Answer C: Kinetic energy is dependent on
      the satellite's mass and velocity. Hence different satellites of
      different masses may have different kinetic energies.
    the rest of choice must be same.
    
    Example
    A spacecraft was launched from Earth
      into a circular orbit around Earth that was maintained at an
      almost constant height of 189 km from the Earth's surface. 
      Assuming the gravitational field strength in this orbit is 9.4 N
      kg-1, and the radius of the Earth is 6 370 km.
    a)  Calculate the speed of the
      spacecraft in this orbit.
    b)  Find the time to complete one
      orbit.
    c)  Comment whether this spacecraft
      is in a geostationary orbit
    
    since the condition for circular motion
      is assumed to be true, we can use the circular motion equation
      while also assuming only the Earth's gravitational field acts on
      spacecraft.
    
    rearranging to get
    
    substituting 
    
    
    7.85x103 m/s
      = v
    
    b) since 
    and 
    substituting
    
    T = 5249 = 5.25x103 s
    c) since the spacecraft does not
      satisfied just one of the condition (eg. T not 24 hours), it is
      safe to conclude i cannot be geostationary.
    
      - placed vertically above the equator
 
      - same direction sense as the rotation of the Earth (determine
        through axis of rotation)
 
      - same orbital period of Planet, in our case, Earth orbital
        period of  approximately 24 hrs
 
    
    Java
      3D Model
    http://iwant2study.org/lookangejss/02_newtonianmechanics_7gravity/ejs/ejs_model_EarthAndSatelite.jar
    Model
    https://dl.dropboxusercontent.com/u/44365627/lookangEJSworkspace/export/ejss_model_gravity10/gravity10_Simulation.xhtml
    Geostationary
      Satellite around Earth Model
     This
      Geostationary Satellite around Earth Model is a simple angular
      velocity model that uses the Java3D implementation for realistic
      visualization of satellite objects in geostationary orbits at
      three different locations namely (near Singapore, near Africa and
      America . Students can explore the meaning of geostationary
      orbits, cases of non-geostationary orbits and even non-gravity
      physics orbit . 
    Geostationary
      Satellites
    The term
      Geo-stationary implies a satellite fixed about a position above
      the earth. This is possible because such satellites have the same
      period as the Earth’s rotation 1 (T = 24 hours) 2 same rotational
      sense as the earth's rotation spin 3 is directly above the equator
      in other words the plane of rotation of the satellite must be in
      the plane of the Equator Therefore, it appears stationary. 
    Application
    Example of
      geostationary satellites are GMS1, GEOS, METEOSAT etc. Most of
      these satellites are used for commercial and military
      purposes 
    Main
      Simulation View
    The simulation
      has a Earth and a Satellite object  Menu Drop Down Allows for
      selecting what motion of Satellite is simulated.
    
      - Geostationary near sg
 
      - Geostationary near Africa
 
      - Geostationary near America
 
      - Non-geostationary due to direction
 
      - circular motion r=3*Re, T =7.30 hr
 
      - circular motion r=10.5*Re, T = 48 hr
 
      - Non-Geostationary generally
 
      - Unlikely Orbits
 
    
    Checkboxes
    
      - show:equator Plane, for visualizing the Earth's rotating
        equator plane
 
      - Geo stationary, for visualizing a geostationary object (RED)
        for comparative observation with the other modes.
 
      - Show text: 35 700 km fixed position of object relative to
        planet earth.
 
      - Axes earth: show spin axes of the rotation of earth in GREEN
 
      - Axes satellite: show spin axes of the rotation of satellite in
        MAGENTA
 
      - Force: pair of action reaction force of equal magnitude,
        opposite direction and on different bodies. (Newton's 3rd
        Law)  
 
    
    Buttons
    
      - Play
 
      - Step Forward
 
      - Reset
 
    
    have their usual meaning.