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CZ-3C DEB

NORAD 40170 Debris MEO 2010-057Y
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
694 km
Apogee
35932 km
Inclination
19.9°
Period
643.5 min
Mean Motion
2.23767840 rev/day
TLE Epoch
2026-06-18 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude18,313 km
Orbital Velocity14,467 km/h
Velocity4.02 km/s
Orbital Period10 hours 44 minutes
Orbits / Day2.24
Eccentricity0.7138
Semi-Major Axis24,684 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2010-10-31
Launch Site
Xichang, China
Int'l Designator
2010-057Y
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 2010-10-31 from Xichang, China on the di liu ke beidou daohang launch. After 16 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 694 km and 35,932 km with an inclination of 19.9°. It travels at approximately 14,467 km/h (4.02 km/s), completing one full orbit every 10 hours 44 minutes — that’s roughly 2.24 orbits per day. Its orbital eccentricity of 0.7138 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 18,313 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 1 active payload and 26 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 19.9°, CZ-3C DEB passes over latitudes between 19.9°N and 19.9°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. China operates approximately 1,218 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 694 km (perigee) and 35,932 km (apogee), with an average altitude of approximately 18,313 km. It completes one orbit every 10 hours 44 minutes, travelling at approximately 14,467 km/h (8,989 mph).
CZ-3C DEB (NORAD ID 40170) 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 2010-10-31 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-3C DEB (NORAD ID 40170) 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 14,467 km/h (8,989 mph) — roughly 4.02 km/s. It completes 2.24 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 4.02 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.