CZ-4B DEB
NORAD 40532
Debris
LEO
2013-057E
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LEO · NORAD 40532
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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
574 km
Apogee
834 km
Inclination
74.9°
Period
98.9 min
Mean Motion
14.56672395 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude704 km
Orbital Velocity27,021 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.57
Eccentricity0.0184
Semi-Major Axis7,075 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2013-10-25
Launch Site
Jiuquan, China
Int'l Designator
2013-057E
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
CZ-4B DEB is a tracked piece of space debris attributed to China, launched on 2013-10-25 from Jiuquan, China on the SJ-16 launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 574 km and 834 km with an inclination of 74.9°. It travels at approximately 27,021 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.57 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 704 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of CZ-4B DEB’s average altitude, there are currently 265 active payloads and 1,482 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 74.9°, CZ-4B DEB passes over latitudes between 74.9°N and 74.9°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 61 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 574 km (perigee) and 834 km (apogee), with an average altitude of approximately 704 km. It completes one orbit every 99 minutes, travelling at approximately 27,021 km/h (16,790 mph).
CZ-4B DEB (NORAD ID 40532) 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 2013-10-25 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4B DEB (NORAD ID 40532) 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 27,021 km/h (16,790 mph) — roughly 7.51 km/s. It completes 14.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.51 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.