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In astrodynamics and celestial dynamics, the orbital state vectors (sometimes state vectors) of an orbit are Cartesian vectors of position ( r {\displaystyle \mathbf {r} } ) and velocity ( v {\displaystyle \mathbf {v} } ) that together with their time (epoch) ( t {\displaystyle t} ) uniquely determine the trajectory of the orbiting body in space.: 154
Art, Position and velocity vectors & Frame of reference
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state vectors orbit velocity vector position time trajectory orbital reference displaystyle mathbf used determine body frame defined inertial elements epoch
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| B1950 or J2000 are also commonly used.Many other reference frames can be used to meet various application requirements | instance of | so the reference frames defined by Earth's orientation at a standard astronomical epoch | 0.80 | text |
| including those centered on the Sun or on other planets or moons | instance of | so the reference frames defined by Earth's orientation at a standard astronomical epoch | 0.80 | text |
| the one defined by the barycenter | instance of | so the reference frames defined by Earth's orientation at a standard astronomical epoch | 0.80 | text |
| total angular momentum of the Solar System | instance of | so the reference frames defined by Earth's orientation at a standard astronomical epoch | 0.80 | text |
| drag or thrust are significant | instance of | If other forces | 0.80 | text |
| they must be added vectorially to those of gravity when performing the integration to determine future position | instance of | If other forces | 0.80 | text |
| velocity.For any object moving through space | instance of | If other forces | 0.80 | text |
| the velocity vector is tangent to the trajectory | instance of | If other forces | 0.80 | text |
| drag | instance of | time-varying forces | 0.80 | text |
| thrust | instance of | time-varying forces | 0.80 | text |
| gravitational perturbations from third bodies as well as the gravity of the primary body.The state vectors | instance of | time-varying forces | 0.80 | text |
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