H-2A DEB

H-2A DEB is a tracked piece of space debris attributed to Japan, launched on 2002-02-04 from TNSTA on the MDS-1 launch. With over 24 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 340 km and 33,132 km with an inclination of 28.3°. It travels at approximately 14,952 km/h (4.15 km/s), completing one full orbit every 9 hours 43 minutes — that’s roughly 2.47 orbits per day. Its orbital eccentricity of 0.7096 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, H-2A DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.

H-2A DEB orbits at an average altitude of 16,736 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-2A DEB’s average altitude, there are currently 0 active payloads and 7 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 28.3°, H-2A DEB passes over latitudes between 28.3°N and 28.3°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 189 active satellites in total.