PEGASUS R/B

PEGASUS R/B is a spent rocket body associated with United States, launched on 1993-02-09 from Cape Canaveral Space Force Station, United States on the Orbcomm OXP launch. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 668 km and 730 km with an inclination of 25.0°. It travels at approximately 27,031 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.58 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Spent rocket bodies like PEGASUS R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.

PEGASUS R/B orbits at an average altitude of 699 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of PEGASUS R/B’s average altitude, there are currently 295 active payloads and 1,573 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 25.0°, PEGASUS R/B passes over latitudes between 25.0°N and 25.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 13,200 active satellites in total, of which 82 share a similar altitude band with PEGASUS R/B.