Close Conjunction of INTELSAT 1002 and MEV-2
Event Overview
On June 15, 2026, at 10:17 UTC, a close approach event is anticipated between INTELSAT 1002 (NORAD ID: 28358) and MEV-2 (NORAD ID: 46113). The predicted minimum separation distance is approximately 0.00 km, indicating a potential collision risk. This conjunction is classified as high-severity due to the proximity of the two satellites.
Significance of the Conjunction
Conjunction events of this nature are critical due to the potential for collision, which could generate space debris. Space debris poses a significant threat to operational satellites and future space missions. INTELSAT 1002 is a geostationary communications satellite, while MEV-2 is a servicing vehicle designed to extend the life of satellites. A collision could disrupt communications services and satellite servicing operations.
Technical Context
The close approach of these two satellites highlights the challenges of space traffic management in an increasingly crowded orbit. As of now, there are 17,929 active satellites in orbit, with a total of 28,422 catalogued objects, including debris. The debris environment currently tracks 8,614 debris objects. Orbital Radar's Debris Map (/debris-map) can provide a visual representation of these objects and their potential impact zones.
Monitoring and Mitigation
Operators of both INTELSAT 1002 and MEV-2 will be closely monitoring the situation using ground-based radar and satellite tracking systems. Manoeuvres may be planned to mitigate the risk of collision. The Orbital Radar Anomaly Panel provides updates on any unexpected satellite behaviours that could affect conjunction predictions.
Future Considerations
This event underscores the importance of international cooperation in space traffic management and the development of technologies to prevent collisions. As satellite launches continue to increase, the need for effective debris mitigation strategies becomes more pressing. The Orbital Radar Re-entry Tracker (/reentry-tracker) can be used to monitor objects that may re-enter Earth's atmosphere, reducing the long-term debris population.
