Graphic Visualization
Tabulated Results
Column heading descriptions
| |
Unique object identifier | |
Full name of object | |
H magnitude for asteroids, M2 nuclear magnitude for comets[more] | |
Known or estimated range of diameters[more] | |
Orbit knowledge uncertainty (0-9)[more] | |
Departure date from Earth | |
Arrival date at destination | |
Flyby date of object | |
Departure date from destination | |
Return date to Earth | |
Time spent at destination | |
Total mission duration | |
Energy required for Earth departure[more] | |
Declination of the launching asymptote[more] | |
Change in velocity required for Earth departure from 200 km LEO[more] | |
Change in velocity required for all maneuvers after Earth departure[more] | |
Total change in velocity required[more] | |
Relative speed of spacecraft and object at closest approach | |
Relative speed of spacecraft to Earth at reentry | |
Trajectory itinerary[more] | |
See the user guide for more documentation. |