Research Article
Optimal Trajectory Determination and Mission Design for Asteroid/Deep-Space Exploration via Multibody Gravity Assist Maneuvers
Table 5
Orbital characteristics of Hylonome.
| Element | Value | Uncertainty () | Units |
| | .2482 | ā | ā | | 25.1017 | 0.0016667 | au | | 18.8690 | 0.00028158 | au | | 4.1442 | | deg | Node | 178.0727 | 0.00055742 | deg | Peri | 6.5554 | 0.0045953 | deg | | 60.5576 | 0.0086221 | deg | | 2449873.32 (1995-Jun-04.82286853) | 0.33896 | JED | Period | 45936.0887346103 125.77 | 4.575 0.01253 | d yr | | .007836 | | deg/d | | 31.3343 | 0.0020805 | au |
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