CZ-4C DEB
NORAD 43425
Debris
LEO
2015-040D
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LEO · NORAD 43425
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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
1067 km
Apogee
1283 km
Inclination
100.2°
Period
108.9 min
Mean Motion
13.22605936 rev/day
TLE Epoch
2026-06-16 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,175 km
Orbital Velocity26,165 km/h
Velocity7.27 km/s
Orbital Period109 minutes
Orbits / Day13.23
Eccentricity0.0143
Semi-Major Axis7,546 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2015-08-27
Launch Site
Taiyuan, China
Int'l Designator
2015-040D
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 2015-08-27 from Taiyuan, China on the YG-27 launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 1,067 km and 1,283 km with an inclination of 100.2°. It travels at approximately 26,165 km/h (7.27 km/s), completing one full orbit every 109 minutes — that’s roughly 13.23 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 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 1,175 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of CZ-4C DEB’s average altitude, there are currently 840 active payloads and 251 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. With an inclination of 100.2°, CZ-4C DEB passes over latitudes between 100.2°N and 100.2°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 1,217 active satellites in total, of which 174 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 1,067 km (perigee) and 1,283 km (apogee), with an average altitude of approximately 1,175 km. It completes one orbit every 109 minutes, travelling at approximately 26,165 km/h (16,258 mph).
CZ-4C DEB (NORAD ID 43425) 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 2015-08-27 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4C DEB (NORAD ID 43425) 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 26,165 km/h (16,258 mph) — roughly 7.27 km/s. It completes 13.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.27 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.