Orbital Cleanup Command Center

Mission planning sandbox inspired by ADRAS-J operations and ESA Zero Debris ambitions through 2030.

Launch-rate growth assumption (2026→2030): 6%

Removal missions per year: 3

Campaign mode: Balanced

ADRAS-J close-proximity debris RPO demonstrated, including a reported 15 m stand-off milestone (late 2024).
ADRAS-J2 style modeled as stronger capture efficiency for derelict rocket bodies.
Zero Debris planning objective framed here as conjunction-pressure reduction by 2030.

References: Astroscale ADRAS-J update, ESA Zero Debris, ESA Space Environment Report 2025.

Risk score = congestion(altitude shell) × mass term × cross-section × instability factor × launch growth pressure. Removal value = risk × campaign capture confidence.

Explorable 3D Orbit Viewer

Orange = active high-risk derelict object. Green = selected for removal campaign.

Modeled conjunction pressure (before)0.0

Modeled conjunction pressure (after)0.0

Risk buy-down by 20300%

Objects removed by campaign0

Before campaign conjunction map

After campaign conjunction map

Launch-rate Scenario Through 2030

Projected total conjunction pressure by year (with vs without cleanup campaign).

Priority Ranking — Risk Reduced per Mission

#	Target	Type	Altitude (km)	Inclination (°)	Base risk	Removal value	Status