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CZ-3C DEB

NORAD 40194 Debris MEO 2012-008D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
2739 km
Apogee
35539 km
Inclination
20.9°
Period
676.1 min
Mean Motion
2.12990500 rev/day
TLE Epoch
2026-09-16 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,139 km
Orbital Velocity14,230 km/h
Velocity3.95 km/s
Orbital Period11 hours 16 minutes
Orbits / Day2.13
Eccentricity0.6429
Semi-Major Axis25,510 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2012-02-24
Launch Site
Xichang Satellite Launch Center, China
Int'l Designator
2012-008D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CZ-3C DEB is a tracked piece of space debris attributed to China, launched on 2012-02-24 from Xichang Satellite Launch Center, China on the di shiyi ke beidou d.w. launch. After 14 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,739 km and 35,539 km with an inclination of 20.9°. It travels at approximately 14,230 km/h (3.95 km/s), completing one full orbit every 11 hours 16 minutes — that’s roughly 2.13 orbits per day. Its orbital eccentricity of 0.6429 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, CZ-3C 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-3C DEB orbits at an average altitude of 19,139 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of CZ-3C DEB’s average altitude, there are currently 121 active payloads and 32 tracked debris or rocket body fragments — notable neighbours include COSMOS 1414 (GLONASS), COSMOS 1490 (GLONASS), COSMOS 1492 (GLONASS). With an inclination of 20.9°, CZ-3C DEB passes over latitudes between 20.9°N and 20.9°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,288 active satellites in total.
🔗 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-3C DEB orbits in Medium Earth Orbit (MEO) at altitudes between 2,739 km (perigee) and 35,539 km (apogee), with an average altitude of approximately 19,139 km. It completes one orbit every 11 hours 16 minutes, travelling at approximately 14,230 km/h (8,842 mph).
CZ-3C DEB (NORAD ID 40194) 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-3C DEB was launched on 2012-02-24 from Xichang Satellite Launch Center, China. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-3C DEB (NORAD ID 40194) 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-3C DEB travels at approximately 14,230 km/h (8,842 mph) — roughly 3.95 km/s. It completes 2.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 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 3.95 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-3C DEB. Read more about debris statistics and the Kessler syndrome.