H-2 R/B(2)

H-2 R/B(2) is a spent rocket body associated with Japan, launched on 1995-03-18 from Tanegashima Space Center, Japan on the SFU launch. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 260 km and 24,273 km with an inclination of 25.1°. It travels at approximately 16,649 km/h (4.62 km/s), completing one full orbit every 7 hours 2 minutes — that’s roughly 3.41 orbits per day. Its orbital eccentricity of 0.6442 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like H-2 R/B(2) are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.

H-2 R/B(2) orbits at an average altitude of 12,267 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 H-2 R/B(2)’s average altitude, there are currently 0 active payloads and 3 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 25.1°, H-2 R/B(2) passes over latitudes between 25.1°N and 25.1°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. Japan operates approximately 208 active satellites in total.