CZ-4 DEB
NORAD 26436
Debris
LEO
1999-057KH
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LEO · NORAD 26436
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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
732 km
Apogee
1806 km
Inclination
99.5°
Period
110.9 min
Mean Motion
12.98196403 rev/day
TLE Epoch
2026-06-20 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,269 km
Orbital Velocity26,003 km/h
Velocity7.22 km/s
Orbital Period111 minutes
Orbits / Day12.98
Eccentricity0.0703
Semi-Major Axis7,640 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
1999-10-14
Launch Site
Taiyuan, China
Int'l Designator
1999-057KH
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 732 km and 1,806 km with an inclination of 99.5°. It travels at approximately 26,003 km/h (7.22 km/s), completing one full orbit every 111 minutes — that’s roughly 12.98 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of 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 1,269 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of CZ-4 DEB’s average altitude, there are currently 66 active payloads and 280 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0013, ONEWEB-0017, ONEWEB-0020. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 99.5°, CZ-4 DEB passes over latitudes between 99.5°N and 99.5°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.
🔗 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 732 km (perigee) and 1,806 km (apogee), with an average altitude of approximately 1,269 km. It completes one orbit every 111 minutes, travelling at approximately 26,003 km/h (16,158 mph).
CZ-4 DEB (NORAD ID 26436) 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-4 DEB (NORAD ID 26436) 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 26,003 km/h (16,158 mph) — roughly 7.22 km/s. It completes 12.98 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 7.22 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.