Eccentricity vector
From Wikipedia, the free encyclopedia
In astrodynamics the eccentricity vector of a conic section orbit is the vector pointing towards the periapsis and with magnitude equal to the orbit's scalar eccentricity. The magnitude is unitless.
The eccentricity vector
can be calculated from the orbital state vectors
and
at any time (the result is constant):
where:
is velocity vector of the orbital state vectors,
is position vector of the orbital state vectors,
is standard gravitational parameter.
Alternatively it can also be computed from orbital angular momentum vector
:
where:
is orbital velocity vector,
is orbital angular momentum vector,
is orbital position vector,
is standard gravitational parameter.
Since
is defined as
, it can be shown by the vector triple product identity that this formula is equivalent to the one above.

