CZ-4C DEB
NORAD 43627
Debris
LEO
2013-065D
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LEO · NORAD 43627
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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
693 km
Apogee
874 km
Inclination
100.6°
Period
100.5 min
Mean Motion
14.32496114 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude784 km
Orbital Velocity26,871 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.32
Eccentricity0.0126
Semi-Major Axis7,155 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2013-11-20
Launch Site
Taiyuan, China
Int'l Designator
2013-065D
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 2013-11-20 from Taiyuan, China on the yaogan weixing 19 launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 693 km and 874 km with an inclination of 100.6°. It travels at approximately 26,871 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.32 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 784 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of CZ-4C DEB’s average altitude, there are currently 412 active payloads and 2,215 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 100.6°, CZ-4C DEB passes over latitudes between 100.6°N and 100.6°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,218 active satellites in total, of which 80 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 693 km (perigee) and 874 km (apogee), with an average altitude of approximately 784 km. It completes one orbit every 101 minutes, travelling at approximately 26,871 km/h (16,697 mph).
CZ-4C DEB (NORAD ID 43627) 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 2013-11-20 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C DEB (NORAD ID 43627) 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 26,871 km/h (16,697 mph) — roughly 7.46 km/s. It completes 14.32 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.46 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.