CZ-3A DEB
NORAD 35557
Debris
MEO
2007-003R
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MEO · NORAD 35557
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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
372 km
Apogee
24152 km
Inclination
23.2°
Period
422.1 min
Mean Motion
3.41134874 rev/day
TLE Epoch
2026-06-20 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude12,262 km
Orbital Velocity16,651 km/h
Velocity4.63 km/s
Orbital Period7 hours 2 minutes
Orbits / Day3.41
Eccentricity0.6381
Semi-Major Axis18,633 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2007-02-02
Launch Site
Xichang, China
Int'l Designator
2007-003R
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CZ-3A DEB is a tracked piece of space debris attributed to China, launched on 2007-02-02 from Xichang, China on the di si ke beidou daohang launch. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 372 km and 24,152 km with an inclination of 23.2°. It travels at approximately 16,651 km/h (4.63 km/s), completing one full orbit every 7 hours 2 minutes — that’s roughly 3.41 orbits per day. Its orbital eccentricity of 0.6381 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, CZ-3A 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-3A DEB orbits at an average altitude of 12,262 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-3A DEB’s average altitude, there are currently 0 active payloads and 5 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 23.2°, CZ-3A DEB passes over latitudes between 23.2°N and 23.2°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 1,218 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-3A DEB orbits in Medium Earth Orbit (MEO) at altitudes between 372 km (perigee) and 24,152 km (apogee), with an average altitude of approximately 12,262 km. It completes one orbit every 7 hours 2 minutes, travelling at approximately 16,651 km/h (10,346 mph).
CZ-3A DEB (NORAD ID 35557) 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-3A DEB was launched on 2007-02-02 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-3A DEB (NORAD ID 35557) 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-3A DEB travels at approximately 16,651 km/h (10,346 mph) — roughly 4.63 km/s. It completes 3.41 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 7 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 4.63 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-3A DEB. Read more about debris statistics and the Kessler syndrome.