CZ-2F DEB
NORAD 53364
Debris
LEO
2022-093H
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LEO · NORAD 53364
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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
447 km
Apogee
545 km
Inclination
50.0°
Period
94.5 min
Mean Motion
15.23222999 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude496 km
Orbital Velocity27,428 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.23
Eccentricity0.0071
Semi-Major Axis6,867 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2022-08-04
Launch Site
Jiuquan, China
Int'l Designator
2022-093H
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CZ-2F DEB is a tracked piece of space debris attributed to China, launched on 2022-08-04 from Jiuquan, China on the CSSHQ launch. It orbits in Low Earth Orbit (LEO) at altitudes between 447 km and 545 km with an inclination of 50.0°. It travels at approximately 27,428 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.23 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. As orbital debris, CZ-2F 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-2F DEB orbits at an average altitude of 496 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of CZ-2F DEB’s average altitude, there are currently 9,231 active payloads and 235 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 52.8% of all active satellites. With an inclination of 50.0°, CZ-2F DEB passes over latitudes between 50.0°N and 50.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,221 active satellites in total, of which 192 share a similar altitude band with CZ-2F 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-2F DEB orbits in Low Earth Orbit (LEO) at altitudes between 447 km (perigee) and 545 km (apogee), with an average altitude of approximately 496 km. It completes one orbit every 95 minutes, travelling at approximately 27,428 km/h (17,043 mph).
CZ-2F DEB (NORAD ID 53364) 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-2F DEB was launched on 2022-08-04 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-2F DEB (NORAD ID 53364) 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-2F DEB travels at approximately 27,428 km/h (17,043 mph) — roughly 7.62 km/s. It completes 15.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 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 7.62 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-2F DEB. Read more about debris statistics and the Kessler syndrome.