CZ-3B DEB

CZ-3B DEB is a tracked piece of space debris attributed to China, launched on 2010-09-04 from Xichang, China on the zhongxing liu A weixing launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 653 km and 43,408 km with an inclination of 29.8°. It travels at approximately 13,487 km/h (3.75 km/s), completing one full orbit every 13 hours 14 minutes — that’s roughly 1.81 orbits per day. Its orbital eccentricity of 0.7527 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, CZ-3B 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.

CZ-3B DEB follows a Highly Elliptical Orbit, sweeping between 653 km (perigee) and 43,408 km (apogee). It spends most of its 13 hours 14 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of CZ-3B DEB’s average altitude, there are currently 0 active payloads and 13 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 29.8°, CZ-3B DEB passes over latitudes between 29.8°N and 29.8°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. China operates approximately 1,218 active satellites in total.