Orbit


Orbital Elements

perihelion time
use format YYYY or YYYY MM or YYYY MM DD
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perihelion
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eccentricity
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semi-major axis
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aphelion
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argument of perihelion
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ascending node
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inclination
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Data

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Type of Orbital Solution

Please provide a valid state.

Orbital Elements

time interval to previous/next perihelion
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perihelion distance
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aphelion distance
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Swarm

no. of returning VCs in the swarm
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no. of escaping VCs in the swarm
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% of VCs with q < 10
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% of VCs with 10 < q < 20
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% of VCs with q > 20
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