deviation of semi-major axis












3














If I calculate the semi-major axis of Molniya-1T with
$a = sqrt[3]{dfrac{GM}{n^2}}$ with $n=3.18683728text{ }d^{-1}$
, I get another apoapsis ($a=19505.7$ km) as noted at heavens above :




apogee height: 25659 km



perigee height: 595 km




which is $a=frac{25659+595}{2}=13127$ km.



This is my approach in octave/matlab:



# computes the Semi major axis a from n with constant GM
# @params:
# GM constant (cubic km per square second)
# n: mean motion (revs/day)
# @return:
# a: semi major axis (km)

function a = getSemiMajorAxis(GM,n)
n = n*2*pi/(24*60*60); #conversion (revs/day) --> (rad/s)
a = (GM/(power(n,2))).^(1./3);
endfunction

getSemiMajorAxis(398600.44,3.18683728) # test with Molniya-1T


So, what is the origin of the deviation? Isn't apogee the same as apoapsis basically?










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    3














    If I calculate the semi-major axis of Molniya-1T with
    $a = sqrt[3]{dfrac{GM}{n^2}}$ with $n=3.18683728text{ }d^{-1}$
    , I get another apoapsis ($a=19505.7$ km) as noted at heavens above :




    apogee height: 25659 km



    perigee height: 595 km




    which is $a=frac{25659+595}{2}=13127$ km.



    This is my approach in octave/matlab:



    # computes the Semi major axis a from n with constant GM
    # @params:
    # GM constant (cubic km per square second)
    # n: mean motion (revs/day)
    # @return:
    # a: semi major axis (km)

    function a = getSemiMajorAxis(GM,n)
    n = n*2*pi/(24*60*60); #conversion (revs/day) --> (rad/s)
    a = (GM/(power(n,2))).^(1./3);
    endfunction

    getSemiMajorAxis(398600.44,3.18683728) # test with Molniya-1T


    So, what is the origin of the deviation? Isn't apogee the same as apoapsis basically?










    share|improve this question









    New contributor




    sequoia is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
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      3












      3








      3







      If I calculate the semi-major axis of Molniya-1T with
      $a = sqrt[3]{dfrac{GM}{n^2}}$ with $n=3.18683728text{ }d^{-1}$
      , I get another apoapsis ($a=19505.7$ km) as noted at heavens above :




      apogee height: 25659 km



      perigee height: 595 km




      which is $a=frac{25659+595}{2}=13127$ km.



      This is my approach in octave/matlab:



      # computes the Semi major axis a from n with constant GM
      # @params:
      # GM constant (cubic km per square second)
      # n: mean motion (revs/day)
      # @return:
      # a: semi major axis (km)

      function a = getSemiMajorAxis(GM,n)
      n = n*2*pi/(24*60*60); #conversion (revs/day) --> (rad/s)
      a = (GM/(power(n,2))).^(1./3);
      endfunction

      getSemiMajorAxis(398600.44,3.18683728) # test with Molniya-1T


      So, what is the origin of the deviation? Isn't apogee the same as apoapsis basically?










      share|improve this question









      New contributor




      sequoia is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
      Check out our Code of Conduct.











      If I calculate the semi-major axis of Molniya-1T with
      $a = sqrt[3]{dfrac{GM}{n^2}}$ with $n=3.18683728text{ }d^{-1}$
      , I get another apoapsis ($a=19505.7$ km) as noted at heavens above :




      apogee height: 25659 km



      perigee height: 595 km




      which is $a=frac{25659+595}{2}=13127$ km.



      This is my approach in octave/matlab:



      # computes the Semi major axis a from n with constant GM
      # @params:
      # GM constant (cubic km per square second)
      # n: mean motion (revs/day)
      # @return:
      # a: semi major axis (km)

      function a = getSemiMajorAxis(GM,n)
      n = n*2*pi/(24*60*60); #conversion (revs/day) --> (rad/s)
      a = (GM/(power(n,2))).^(1./3);
      endfunction

      getSemiMajorAxis(398600.44,3.18683728) # test with Molniya-1T


      So, what is the origin of the deviation? Isn't apogee the same as apoapsis basically?







      orbital-mechanics orbit orbital-elements






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      edited 1 hour ago





















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      asked 2 hours ago









      sequoia

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          Ok, that's embarrassing:



          You just have to add earth's radii of about 6378 to the a calculated from the apogee/perigee.






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            Ok, that's embarrassing:



            You just have to add earth's radii of about 6378 to the a calculated from the apogee/perigee.






            share|improve this answer








            New contributor




            sequoia is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
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              2














              Ok, that's embarrassing:



              You just have to add earth's radii of about 6378 to the a calculated from the apogee/perigee.






              share|improve this answer








              New contributor




              sequoia is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
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                2












                2








                2






                Ok, that's embarrassing:



                You just have to add earth's radii of about 6378 to the a calculated from the apogee/perigee.






                share|improve this answer








                New contributor




                sequoia is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
                Check out our Code of Conduct.









                Ok, that's embarrassing:



                You just have to add earth's radii of about 6378 to the a calculated from the apogee/perigee.







                share|improve this answer








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                sequoia is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
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                answered 1 hour ago









                sequoia

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