| Display title | Orbital state vectors |
| Default sort key | Orbital state vectors |
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| Page ID | 188838 |
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| Page creator | imported>NBrush |
| Date of page creation | 21:18, 6 February 2024 |
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Description | Content |
Article description: (description)
This attribute controls the content of the description and og:description elements. | In astrodynamics and celestial dynamics, the orbital state vectors (sometimes state vectors) of an orbit are
Cartesian vectors of position ($ \mathbf {r} $) and velocity ($ \mathbf {v} $) that together with their time (epoch) ($ t $) uniquely determine the trajectory of the orbiting body in space. |
