ZQ-2E DEB
NORAD 69631
Debris
LEO
2026-128F
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LEO · NORAD 69631
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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
340 km
Apogee
432 km
Inclination
54.5°
Period
92.3 min
Mean Motion
15.60722305 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude386 km
Orbital Velocity27,650 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.61
Eccentricity0.0068
Semi-Major Axis6,757 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-09
Launch Site
Jiuquan, China
Int'l Designator
2026-128F
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 340 km and 432 km with an inclination of 54.5°. It travels at approximately 27,650 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.61 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. 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 386 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 1,281 active payloads and 70 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 7.3% of all active satellites. 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 37 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 340 km (perigee) and 432 km (apogee), with an average altitude of approximately 386 km. It completes one orbit every 92 minutes, travelling at approximately 27,650 km/h (17,181 mph).
ZQ-2E DEB (NORAD ID 69631) 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks ZQ-2E DEB (NORAD ID 69631) 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 27,650 km/h (17,181 mph) — roughly 7.68 km/s. It completes 15.61 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 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 7.68 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.