Skip to content
Home Library Satellite Directory CZ-4C DEB

CZ-4C DEB

NORAD 54702 Debris LEO 2022-169D
CONNECTING… LEO · NORAD 54702
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
778 km
Apogee
789 km
Inclination
60.0°
Period
100.5 min
Mean Motion
14.32378111 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
Eccentricity0.0008
Semi-Major Axis7,155 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2022-12-12
Launch Site
Jiuquan, China
Int'l Designator
2022-169D
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
CZ-4C DEB is a tracked piece of space debris attributed to China, launched on 2022-12-12 from Jiuquan, China on the Shiyan 20A/20B launch. It orbits in Low Earth Orbit (LEO) at altitudes between 778 km and 789 km with an inclination of 60.0°. 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. 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 ~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 2,214 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 60.0°, CZ-4C DEB passes over latitudes between 60.0°N and 60.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,217 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 778 km (perigee) and 789 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 54702) 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 2022-12-12 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. 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 54702) 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.