ZQ-2E R/B
NORAD 69537
Rocket Body
LEO
2026-128C
CONNECTING…
LEO · NORAD 69537
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
332 km
Apogee
422 km
Inclination
54.5°
Period
92.1 min
Mean Motion
15.63624910 rev/day
TLE Epoch
2026-06-25 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude377 km
Orbital Velocity27,668 km/h
Velocity7.69 km/s
Orbital Period92 minutes
Orbits / Day15.64
Eccentricity0.0067
Semi-Major Axis6,748 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/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 332 km and 422 km with an inclination of 54.5°. It travels at approximately 27,668 km/h (7.69 km/s), completing one full orbit every 92 minutes — that’s roughly 15.64 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 377 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 1,360 active payloads and 61 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 7.8% 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 1,221 active satellites in total, of which 35 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 332 km (perigee) and 422 km (apogee), with an average altitude of approximately 377 km. It completes one orbit every 92 minutes, travelling at approximately 27,668 km/h (17,192 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 27,668 km/h (17,192 mph) — roughly 7.69 km/s. It completes 15.64 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.