CZ-4 DEB
NORAD 26134
Debris
LEO
1999-057W
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LEO · NORAD 26134
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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
705 km
Apogee
1321 km
Inclination
99.0°
Period
105.4 min
Mean Motion
13.66261369 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,013 km
Orbital Velocity26,450 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.66
Eccentricity0.0417
Semi-Major Axis7,384 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
1999-10-14
Launch Site
Taiyuan, China
Int'l Designator
1999-057W
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CZ-4 DEB is a tracked piece of space debris attributed to China, launched on 1999-10-14 from Taiyuan, China on the ZY-1/CBERS 1 launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 705 km and 1,321 km with an inclination of 99.0°. It travels at approximately 26,450 km/h (7.35 km/s), completing one full orbit every 105 minutes — that’s roughly 13.66 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, CZ-4 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-4 DEB orbits at an average altitude of 1,013 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-4 DEB’s average altitude, there are currently 192 active payloads and 777 tracked debris or rocket body fragments. With an inclination of 99.0°, CZ-4 DEB passes over latitudes between 99.0°N and 99.0°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 20 share a similar altitude band with CZ-4 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-4 DEB orbits in Low Earth Orbit (LEO) at altitudes between 705 km (perigee) and 1,321 km (apogee), with an average altitude of approximately 1,013 km. It completes one orbit every 105 minutes, travelling at approximately 26,450 km/h (16,435 mph).
CZ-4 DEB (NORAD ID 26134) 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-4 DEB was launched on 1999-10-14 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-4 DEB (NORAD ID 26134) 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-4 DEB travels at approximately 26,450 km/h (16,435 mph) — roughly 7.35 km/s. It completes 13.66 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.35 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-4 DEB. Read more about debris statistics and the Kessler syndrome.