Site Navigation
Categories:
Celestial mechanics
Orbits
Astrodynamics

Summary Of: Orbital elements

all sets of orbital elements contain exactly six parameters... The traditional orbital elements are the six... We see that the first three orbital elements are simply the... Evolution of the orbital elements takes place due to the... are equivalent to Keplerian orbital elements and each can be computed with each other... Also furnishes orbital elements for a large number of solar system objects...

Encyclodia Page On: Orbital elements

These Are Links To Other Documents
orbit | Newtonian laws of motion | inverse-square law | gravitational attraction | degrees of freedom | Cartesian coordinates | Kepler orbit | perturbations | relativity | Johannes Kepler | laws of planetary motion | Eccentricity | Semimajor axis | orbital plane | Inclination | Longitude of the ascending node | Argument of periapsis | Mean anomaly | epoch | orbital state vectors | direct computations | Eulerian angles | two-body | ellipse, a parabola, or a hyperbola | osculating | mean anomaly | epoch | mean anomaly | mean longitude | true anomaly | eccentric anomaly | period | apoapsis | periapsis | apogee | perigee | standard gravitational parameter | Fig. 1: Keplerian orbital parameters. | | orbital plane | ecliptic plane | line of nodes | Vernal Point | semi-major axis | periapsis | focal point | center of mass | orbital period | eccentricity | longitude of the ascending node | axis of rotation | center of mass | inclination | axis of rotation | line of nodes | argument of periapsis (perihelion) | axis of rotation | center of mass | true anomaly | axis of rotation | center of mass | Newtonian | planetary orbit | points | free space | real | time | gravitational | nonsphericity | atmospheric | drag | relativistic effects | radiation pressure | electromagnetic forces | Lagrange | Gauss | Delaunay | Poincaré | Hill | true anomaly | euler angles | ATAN2(y,x) | double precision | FORTRAN | Two-line elements | NASA | NORAD | SGP4 | SDP4 | Orbital state vectors | orbit | Ephemeris | Orbital state vectors | Proper orbital elements | Osculating orbit | NORAD | v | d | Orbits | Box | Capture | Circular | Elliptical | Highly elliptical | Escape | Graveyard | Hyperbolic trajectory | Inclined | Non-inclined | Osculating | Parabolic trajectory | Parking | Synchronous | semi | sub | Geocentric | Geosynchronous | Geostationary | Sun-synchronous | Low Earth | Medium Earth | Molniya | Near-equatorial | Orbit of the Moon | Polar | Tundra | Areosynchronous | Areostationary | Halo | Lissajous | Lunar | Heliocentric | Heliosynchronous | Inclination | Longitude of the ascending node | Eccentricity | Argument of periapsis | Semi-major axis | Mean anomaly | epoch | True anomaly | Semi-minor axis | Linear eccentricity | Eccentric anomaly | Mean longitude | True longitude | Orbital period | Maneuvers | Bi-elliptic transfer | Geostationary transfer | Gravity assist | Hohmann transfer | Inclination change | Phasing | Rendezvous | Transposition, docking, and extraction | orbital mechanics | Apsis | Celestial coordinate system | Delta-v budget | Epoch | Ephemeris | Equatorial coordinate system | Gravity turn | Ground track | Interplanetary Transport Network | Kepler's laws of planetary motion | Lagrangian point | Low energy transfers | n-body problem | Oberth effect | Orbit equation | Orbital speed | Orbital state vectors | Perturbation | Retrograde and direct motion | Specific orbital energy | Specific relative angular momentum | List of orbits | Categories | Celestial mechanics | Orbits | Astrodynamics |
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Orbital elements".