CZ-4B DEB
NORAD 46471
Debris
LEO
2020-066C
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LEO · NORAD 46471
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
906 km
Apogee
955 km
Inclination
66.1°
Period
103.6 min
Mean Motion
13.89468980 rev/day
TLE Epoch
2026-06-20 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude931 km
Orbital Velocity26,599 km/h
Velocity7.39 km/s
Orbital Period104 minutes
Orbits / Day13.89
Eccentricity0.0034
Semi-Major Axis7,302 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2020-09-21
Launch Site
Jiuquan, China
Int'l Designator
2020-066C
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CZ-4B DEB is a tracked piece of space debris attributed to China, launched on 2020-09-21 from Jiuquan, China on the HY-2C launch. It orbits in Low Earth Orbit (LEO) at altitudes between 906 km and 955 km with an inclination of 66.1°. It travels at approximately 26,599 km/h (7.39 km/s), completing one full orbit every 104 minutes — that’s roughly 13.89 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, CZ-4B 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-4B DEB orbits at an average altitude of 931 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-4B DEB’s average altitude, there are currently 278 active payloads and 1,143 tracked debris or rocket body fragments. With an inclination of 66.1°, CZ-4B DEB passes over latitudes between 66.1°N and 66.1°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 83 share a similar altitude band with CZ-4B 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-4B DEB orbits in Low Earth Orbit (LEO) at altitudes between 906 km (perigee) and 955 km (apogee), with an average altitude of approximately 931 km. It completes one orbit every 104 minutes, travelling at approximately 26,599 km/h (16,528 mph).
CZ-4B DEB (NORAD ID 46471) 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-4B DEB was launched on 2020-09-21 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4B DEB (NORAD ID 46471) 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-4B DEB travels at approximately 26,599 km/h (16,528 mph) — roughly 7.39 km/s. It completes 13.89 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.39 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-4B DEB. Read more about debris statistics and the Kessler syndrome.