DELTA 2 R/B

DELTA 2 R/B is a spent rocket body associated with United States, launched on 1991-04-13 from Cape Canaveral, Florida on the ASC 2 launch. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 555 km and 2,327 km with an inclination of 24.0°. It travels at approximately 25,715 km/h (7.14 km/s), completing one full orbit every 115 minutes — that’s roughly 12.56 orbits per day. Its orbital eccentricity of 0.1134 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Spent rocket bodies like DELTA 2 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.

DELTA 2 R/B orbits at an average altitude of 1,441 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of DELTA 2 R/B’s average altitude, there are currently 380 active payloads and 194 tracked debris or rocket body fragments. With an inclination of 24.0°, DELTA 2 R/B passes over latitudes between 24.0°N and 24.0°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 12,413 active satellites in total.