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ZQ-2E R/B

NORAD 69537 Rocket Body LEO 2026-128C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
325 km
Apogee
410 km
Inclination
54.5°
Period
91.9 min
Mean Motion
15.67093353 rev/day
TLE Epoch
2026-07-28 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude368 km
Orbital Velocity27,688 km/h
Velocity7.69 km/s
Orbital Period92 minutes
Orbits / Day15.67
Eccentricity0.0063
Semi-Major Axis6,739 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-09
Launch Site
Jiuquan, China
Int'l Designator
2026-128C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ZQ-2E R/B is a spent rocket body associated with China, launched on 2026-06-09 from Jiuquan, China on the Qianfan DTC1 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 325 km and 410 km with an inclination of 54.5°. It travels at approximately 27,688 km/h (7.69 km/s), completing one full orbit every 92 minutes — that’s roughly 15.67 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Spent rocket bodies like ZQ-2E R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
ZQ-2E R/B orbits at an average altitude of 368 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 R/B’s average altitude, there are currently 1,130 active payloads and 55 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 6.4% of all active satellites. With an inclination of 54.5°, ZQ-2E R/B 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 1,247 active satellites in total, of which 25 share a similar altitude band with ZQ-2E R/B.
🔗 Spent Rocket Body

This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.

❓ Frequently Asked Questions
ZQ-2E R/B orbits in Low Earth Orbit (LEO) at altitudes between 325 km (perigee) and 410 km (apogee), with an average altitude of approximately 368 km. It completes one orbit every 92 minutes, travelling at approximately 27,688 km/h (17,204 mph).
ZQ-2E R/B (NORAD ID 69537) is a spent rocket body — the upper stage of a launch vehicle attributed to China. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
ZQ-2E R/B 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 R/B (NORAD ID 69537) 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 R/B travels at approximately 27,688 km/h (17,204 mph) — roughly 7.69 km/s. It completes 15.67 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.