In astrodynamics, any given pair of [[apsis|apsides]] can predict the [[semi-major axis]] and eccentricity of any orbit. Specifically, for periapsis q and apoapsis Q:
In astrodynamics, any given pair of [[apsis|apsides]] can predict the [[semi-major axis]] and eccentricity of any orbit. Specifically, for periapsis q and apoapsis Q:
−
a = (Q + q)/2
+
<math>a = (Q + q)/2</math>
−
''e'' = (Q - q)/(Q + q)
+
<math>e = (Q - q)/(Q + q)</math>
or
or
−
''e'' = 1 - 2/((Q/q) + 1)
+
<math>e = 1 - 2/((Q/q) + 1)</math>
By the same token, a and ''e'' can predict Q and q.
By the same token, a and ''e'' can predict Q and q.
−
Q/q = (1+e)/(1-e)
+
<math>Q/q = (1+e)/(1-e)</math>
and
and
−
Q + q = 2a
+
<math>Q + q = 2a</math>
Therefore
Therefore
−
Q - q(1+e)/(1-e) = 0
+
<math>Q - q(1+e)/(1-e) = 0</math>
and
and
−
Q + q = 2a.
+
<math>Q + q = 2a</math>
Subtracting the first equation from the second yields
Subtracting the first equation from the second yields
−
q(1 + (1+e)/(1-e)) = 2a
+
<math>q(1 + (1+e)/(1-e)) = 2a</math>
From the above:
From the above:
−
q = a(1-e)
+
<math>q = a(1-e)</math>
and
and
−
Q = a(1+e).
+
<math>Q = a(1+e)</math>
For ''e'' = 0, Q = q = a = r, the orbital radius, as one would expect.
For ''e'' = 0, Q = q = a = r, the orbital radius, as one would expect.