Skip to content
Home › Library › Satellite Directory › CZ-3A DEB

CZ-3A DEB

NORAD 35552 Debris MEO 2007-003L
CONNECTING… MEO · NORAD 35552
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
375 km
Apogee
39465 km
Inclination
26.5°
Period
707.4 min
Mean Motion
2.03578829 rev/day
TLE Epoch
2026-11-02 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,920 km
Orbital Velocity14,017 km/h
Velocity3.89 km/s
Orbital Period11 hours 47 minutes
Orbits / Day2.04
Eccentricity0.7434
Semi-Major Axis26,291 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2007-02-02
Launch Site
Xichang Satellite Launch Center, China
Int'l Designator
2007-003L
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 Satellite Launch Center, 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 375 km and 39,465 km with an inclination of 26.5°. It travels at approximately 14,017 km/h (3.89 km/s), completing one full orbit every 11 hours 47 minutes — that’s roughly 2.04 orbits per day. Its orbital eccentricity of 0.7434 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 19,920 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 5 active payloads and 30 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 26.5°, CZ-3A DEB passes over latitudes between 26.5°N and 26.5°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 1,340 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 375 km (perigee) and 39,465 km (apogee), with an average altitude of approximately 19,920 km. It completes one orbit every 11 hours 47 minutes, travelling at approximately 14,017 km/h (8,710 mph).
CZ-3A DEB (NORAD ID 35552) 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 Satellite Launch Center, 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 35552) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 14,017 km/h (8,710 mph) — roughly 3.89 km/s. It completes 2.04 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 3.89 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.