Orbital Control Simulator: Cislunar & Earth Constellation Mechanics

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Mission Scenarios SOURCE GROUNDED

Explore how orbital regimes (LEO to Cislunar) dictate space control, sensor dwell times, and delta-v thruster budgets.

Target Telemetry ACTIVE TRACK

Flatellite Alpha-01 LEO RADAR

ALTITUDE (AP / PE) 550 km / 548 km

ORBITAL VELOCITY 7.59 km/s

ORBITAL PERIOD 95.6 min

ECCENTRICITY 0.0002

REMAINING Δv 2,850 m/s

SENSOR FOOTPRINT 2,200 km

Orbital Thruster Burns Δv ENGINE

Burn Magnitude Impulse: 150 m/s

Flight Telemetry Log EVENT BUS

[00:00:00] Constellation simulation initialized in LEO band.

[00:00:01] All 6 tracking radar nodes synched. Global coverage: 78.4%.