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CZ-4C DEB

NORAD 38664 Debris LEO 2012-029F
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1108 km
Apogee
1317 km
Inclination
100.2°
Period
109.7 min
Mean Motion
13.12643607 rev/day
TLE Epoch
2026-06-23 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,213 km
Orbital Velocity26,100 km/h
Velocity7.25 km/s
Orbital Period110 minutes
Orbits / Day13.13
Eccentricity0.0138
Semi-Major Axis7,584 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2012-05-29
Launch Site
Taiyuan, China
Int'l Designator
2012-029F
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 2012-05-29 from Taiyuan, China on the yaogan weixing shiwuhao launch. After 14 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 1,108 km and 1,317 km with an inclination of 100.2°. It travels at approximately 26,100 km/h (7.25 km/s), completing one full orbit every 110 minutes — that’s roughly 13.13 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of 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 1,213 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of CZ-4C DEB’s average altitude, there are currently 732 active payloads and 230 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. With an inclination of 100.2°, CZ-4C DEB passes over latitudes between 100.2°N and 100.2°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,221 active satellites in total, of which 67 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 1,108 km (perigee) and 1,317 km (apogee), with an average altitude of approximately 1,213 km. It completes one orbit every 110 minutes, travelling at approximately 26,100 km/h (16,218 mph).
CZ-4C DEB (NORAD ID 38664) 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 2012-05-29 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C DEB (NORAD ID 38664) 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 26,100 km/h (16,218 mph) — roughly 7.25 km/s. It completes 13.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.25 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.