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CZ-4C DEB

NORAD 45483 Debris LEO 2018-034L
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
891 km
Apogee
1295 km
Inclination
63.4°
Period
107.1 min
Mean Motion
13.44341462 rev/day
TLE Epoch
2026-06-16 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,093 km
Orbital Velocity26,308 km/h
Velocity7.31 km/s
Orbital Period107 minutes
Orbits / Day13.44
Eccentricity0.0271
Semi-Major Axis7,464 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2018-04-10
Launch Site
Jiuquan, China
Int'l Designator
2018-034L
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
CZ-4C DEB is a tracked piece of space debris attributed to China, launched on 2018-04-10 from Jiuquan, China on the YG-31-01 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 891 km and 1,295 km with an inclination of 63.4°. It travels at approximately 26,308 km/h (7.31 km/s), completing one full orbit every 107 minutes — that’s roughly 13.44 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, CZ-4C 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.
🌍 Orbit Context
CZ-4C DEB orbits at an average altitude of 1,093 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of CZ-4C DEB’s average altitude, there are currently 181 active payloads and 393 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 63.4°, CZ-4C DEB passes over latitudes between 63.4°N and 63.4°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,218 active satellites in total, of which 159 share a similar altitude band with CZ-4C DEB.
🔗 Tracked Space Debris

This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.

❓ Frequently Asked Questions
CZ-4C DEB orbits in Low Earth Orbit (LEO) at altitudes between 891 km (perigee) and 1,295 km (apogee), with an average altitude of approximately 1,093 km. It completes one orbit every 107 minutes, travelling at approximately 26,308 km/h (16,347 mph).
CZ-4C DEB (NORAD ID 45483) is a piece of tracked orbital debris attributed to China. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
CZ-4C DEB was launched on 2018-04-10 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C DEB (NORAD ID 45483) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
CZ-4C DEB travels at approximately 26,308 km/h (16,347 mph) — roughly 7.31 km/s. It completes 13.44 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.31 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like CZ-4C DEB. Read more about debris statistics and the Kessler syndrome.