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ZQ-2E DEB

NORAD 69632 Debris LEO 2026-128G
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
237 km
Apogee
353 km
Inclination
54.5°
Period
90.4 min
Mean Motion
15.95974975 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude295 km
Orbital Velocity27,838 km/h
Velocity7.73 km/s
Orbital Period90 minutes
Orbits / Day15.96
Eccentricity0.0087
Semi-Major Axis6,666 km
Est. Orbital LifetimeWeeks to months
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-09
Launch Site
Jiuquan, China
Int'l Designator
2026-128G
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ZQ-2E DEB is a tracked piece of space debris attributed to China, launched on 2026-06-09 from Jiuquan, China on the Qianfan DTC1/ZYD-02 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 237 km and 353 km with an inclination of 54.5°. It travels at approximately 27,838 km/h (7.73 km/s), completing one full orbit every 90 minutes — that’s roughly 15.96 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is weeks to months. As orbital debris, ZQ-2E 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
ZQ-2E DEB orbits at an average altitude of 295 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of ZQ-2E DEB’s average altitude, there are currently 363 active payloads and 12 tracked debris or rocket body fragments — notable neighbours include STARLINK-1067, STARLINK-1068, STARLINK-1171. With an inclination of 54.5°, ZQ-2E DEB passes over latitudes between 54.5°N and 54.5°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,218 active satellites in total, of which 9 share a similar altitude band with ZQ-2E 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
ZQ-2E DEB orbits in Low Earth Orbit (LEO) at altitudes between 237 km (perigee) and 353 km (apogee), with an average altitude of approximately 295 km. It completes one orbit every 90 minutes, travelling at approximately 27,838 km/h (17,298 mph).
ZQ-2E DEB (NORAD ID 69632) 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.
ZQ-2E DEB was launched on 2026-06-09 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: weeks to months. View the full satellite launch log.
Yes — Orbital Radar tracks ZQ-2E DEB (NORAD ID 69632) 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.
ZQ-2E DEB travels at approximately 27,838 km/h (17,298 mph) — roughly 7.73 km/s. It completes 15.96 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 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 7.73 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 ZQ-2E DEB. Read more about debris statistics and the Kessler syndrome.