Space Debris Catalog
Comprehensive catalog of tracked orbital debris, major fragmentation events, remediation programs, and cascade risk assessment.
// Orbital Debris Overview
// Major Debris Events
// Debris by Orbit
// Top Contributors
// Active Remediation Programs
ClearSpace-1
ESA / ClearSpace SA
Mission to capture and deorbit a Vega Secondary Payload Adapter (VESPA) upper stage using a four-armed robotic capture mechanism.
ADRAS-J
Astroscale (JAXA contract)
Active Debris Removal by Astroscale-Japan. Performing proximity inspection of a Japanese H-2A upper stage rocket body to demonstrate rendezvous and characterization capabilities.
ELSA-d
Astroscale
End-of-Life Services by Astroscale demonstration. Successfully demonstrated magnetic capture and release of a client satellite in orbit using a servicer spacecraft.
RemoveDEBRIS
University of Surrey / SSC
Demonstrated multiple debris capture technologies in orbit including a net capture, a harpoon capture, and a vision-based navigation system for approaching debris.
CRD2
JAXA
Commercial Removal of Debris Demonstration Phase 2. Developing technologies for large-scale debris removal targeting spent rocket upper stages in critical orbital regions.
// Kessler Syndrome Risk Assessment
The current rate of debris generation, combined with mega-constellation deployments, is approaching thresholds where cascading collisions become statistically significant in critical orbital bands.
Peak debris concentration zone. Includes fragments from 2007 China ASAT test and 2009 Iridium-Cosmos collision.
Sun-synchronous orbit region with significant debris and active satellite population overlap.
Mega-constellation deployment zone. Starlink, OneWeb, and others are rapidly increasing object density here.
Without active debris removal, models predict the onset of cascading collisions in the 800-1,000 km band within 50-100 years.
Removing 5-10 large objects per year from critical bands could stabilize the environment and significantly extend the cascade timeline.
The “critical density” threshold for LEO is estimated at ~1 collision every 5 years generating enough fragments to sustain a chain reaction.