ZQ-2E R/B
NORAD 69095
Rocket Body
LEO
2026-105A
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LEO · NORAD 69095
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
206 km
Apogee
813 km
Inclination
89.0°
Period
94.8 min
Mean Motion
15.19054012 rev/day
TLE Epoch
2026-06-26 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude510 km
Orbital Velocity27,401 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.19
Eccentricity0.0441
Semi-Major Axis6,881 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-05-13
Launch Site
Jiuquan, China
Int'l Designator
2026-105A
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 2026-05-13 from Jiuquan, China on the Dummy sat 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 206 km and 813 km with an inclination of 89.0°. It travels at approximately 27,401 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.19 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. 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 510 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 ZQ-2E R/B’s average altitude, there are currently 9,590 active payloads and 262 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 54.8% of all active satellites. With an inclination of 89.0°, ZQ-2E R/B passes over latitudes between 89.0°N and 89.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,221 active satellites in total, of which 220 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 206 km (perigee) and 813 km (apogee), with an average altitude of approximately 510 km. It completes one orbit every 95 minutes, travelling at approximately 27,401 km/h (17,026 mph).
ZQ-2E R/B (NORAD ID 69095) 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 2026-05-13 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks ZQ-2E R/B (NORAD ID 69095) 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 27,401 km/h (17,026 mph) — roughly 7.61 km/s. It completes 15.19 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.