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Time of Deflection (D):
 days
ΔVA:  mm⁄s
ΔVC:  mm⁄s
ΔVN:  mm⁄s
TOF:  days
Near Earth Object Orbital Parameters
Semi-Major Axis:   AU
Eccentricity:  
Inclination:   °
Long. of Ascending Node:   °
Arg. of Perihelion:   °
True Anomaly:   °
Orbital Period:   years

About Orbital Parameters
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Time of Deflection (D):
ΔVA: 
 mm⁄s
ΔVC: 
 mm⁄s
ΔVN: 
 mm⁄s
Transfer Time (L to D):
Vehicle: 
# Launches:
Mass Delivered to Object: 
Simulated Near Earth Object (NEO)
View Orbital
Parameters
Diameter:   km
Density:   g⁄cm3
Beta: 
Mass:   kg
Object parameters
are only applicable in
Intercept Mode
Orbit Changes
ΔVA: ... mm⁄s
ΔVC: ... mm⁄s
ΔVN: ... mm⁄s
Total ΔV: ... mm⁄s
Period at D: ... d
Δ Period: ... s

B-Plane Values
ζ (zeta): ... Re
ξ (xi): ... Re
B magnitude: ... Re
Capture Rad.: ... Re
Perigee Dist.: ... Re
Miss Dist.: ... Re
V∞: ... km⁄s

Mission Values
Depart C3: ... (km⁄s)2
Arrival Vrel: ... km⁄s
Phase Angle: ... °

* Re = Earth Radii