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CZ-4C DEB

NORAD 38304 Debris LEO 2010-009H
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1005 km
Apogee
1486 km
Inclination
63.3°
Period
110.4 min
Mean Motion
13.04248129 rev/day
TLE Epoch
2026-06-15 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,246 km
Orbital Velocity26,043 km/h
Velocity7.23 km/s
Orbital Period110 minutes
Orbits / Day13.04
Eccentricity0.0316
Semi-Major Axis7,617 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2010-03-05
Launch Site
Jiuquan, China
Int'l Designator
2010-009H
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 2010-03-05 from Jiuquan, China on the yaogan weixing jiuhao launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 1,005 km and 1,486 km with an inclination of 63.3°. It travels at approximately 26,043 km/h (7.23 km/s), completing one full orbit every 110 minutes — that’s roughly 13.04 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 1,246 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 405 active payloads and 296 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. With an inclination of 63.3°, CZ-4C DEB passes over latitudes between 63.3°N and 63.3°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 5 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 1,005 km (perigee) and 1,486 km (apogee), with an average altitude of approximately 1,246 km. It completes one orbit every 110 minutes, travelling at approximately 26,043 km/h (16,182 mph).
CZ-4C DEB (NORAD ID 38304) 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 2010-03-05 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C DEB (NORAD ID 38304) 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 26,043 km/h (16,182 mph) — roughly 7.23 km/s. It completes 13.04 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 7.23 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.