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

.2482ā€‰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