ZQ-2E R/B
NORAD 69095
Rocket Body
LEO
2026-105A
CONNECTING…
LEO · NORAD 69095
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
178 km
Apogee
410 km
Inclination
88.9°
Period
90.4 min
Mean Motion
15.92463544 rev/day
TLE Epoch
2026-11-12 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude294 km
Orbital Velocity27,840 km/h
Velocity7.73 km/s
Orbital Period90 minutes
Orbits / Day15.92
Eccentricity0.0174
Semi-Major Axis6,665 km
Est. Orbital LifetimeWeeks to months
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-05-13
Launch Site
Jiuquan Satellite Launch Center, 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 Satellite Launch Center, 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 178 km and 410 km with an inclination of 88.9°. It travels at approximately 27,840 km/h (7.73 km/s), completing one full orbit every 90 minutes — that’s roughly 15.92 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is weeks to months. 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 294 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 209 active payloads and 22 tracked debris or rocket body fragments — notable neighbours include STARLINK-1020, STARLINK-1043, STARLINK-1046. With an inclination of 88.9°, ZQ-2E R/B passes over latitudes between 88.9°N and 88.9°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 1,695 active satellites in total, of which 14 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 178 km (perigee) and 410 km (apogee), with an average altitude of approximately 294 km. It completes one orbit every 90 minutes, travelling at approximately 27,840 km/h (17,299 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 Satellite Launch Center, 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 R/B (NORAD ID 69095) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 27,840 km/h (17,299 mph) — roughly 7.73 km/s. It completes 15.92 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.