CZ-10B DEB
NORAD 69973
Debris
LEO
2026-158B
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LEO · NORAD 69973
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
804 km
Apogee
813 km
Inclination
50.0°
Period
101.1 min
Mean Motion
14.24917183 rev/day
TLE Epoch
2026-08-25 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude809 km
Orbital Velocity26,824 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.25
Eccentricity0.0006
Semi-Major Axis7,180 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-07-10
Launch Site
Wenchang, China
Int'l Designator
2026-158B
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
CZ-10B DEB is a tracked piece of space debris attributed to China, launched on 2026-07-10 from Wenchang, China on the CX-26 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 804 km and 813 km with an inclination of 50.0°. It travels at approximately 26,824 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.25 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, CZ-10B 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-10B DEB orbits at an average altitude of 809 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-10B DEB’s average altitude, there are currently 428 active payloads and 2,324 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 50.0°, CZ-10B DEB passes over latitudes between 50.0°N and 50.0°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 1,275 active satellites in total, of which 99 share a similar altitude band with CZ-10B 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-10B DEB orbits in Low Earth Orbit (LEO) at altitudes between 804 km (perigee) and 813 km (apogee), with an average altitude of approximately 809 km. It completes one orbit every 101 minutes, travelling at approximately 26,824 km/h (16,668 mph).
CZ-10B DEB (NORAD ID 69973) 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-10B DEB was launched on 2026-07-10 from Wenchang, China, China’s newest coastal launch facility on Hainan Island, used for heavy-lift Long March 5 missions. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-10B DEB (NORAD ID 69973) 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-10B DEB travels at approximately 26,824 km/h (16,668 mph) — roughly 7.45 km/s. It completes 14.25 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.45 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-10B DEB. Read more about debris statistics and the Kessler syndrome.