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ZK-2 R/B

NORAD 101282 Rocket Body LEO 2026-248U
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🛰️ Orbital Parameters
Perigee
529 km
Apogee
791 km
Inclination
89.0°
Period
97.9 min
Mean Motion
14.70367312 rev/day
TLE Epoch
2026-11-07 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude660 km
Orbital Velocity27,106 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.70
Eccentricity0.0186
Semi-Major Axis7,031 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-11-03
Launch Site
Jiuquan Satellite Launch Center, China
Int'l Designator
2026-248U
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
ZK-2 R/B is a spent rocket body associated with China, launched on 2026-11-03 from Jiuquan Satellite Launch Center, China on the Qianfan Jigui 21 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 529 km and 791 km with an inclination of 89.0°. It travels at approximately 27,106 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.70 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Spent rocket bodies like ZK-2 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
ZK-2 R/B orbits at an average altitude of 660 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of ZK-2 R/B’s average altitude, there are currently 864 active payloads and 1,216 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 89.0°, ZK-2 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 1,684 active satellites in total, of which 140 share a similar altitude band with ZK-2 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
ZK-2 R/B orbits in Low Earth Orbit (LEO) at altitudes between 529 km (perigee) and 791 km (apogee), with an average altitude of approximately 660 km. It completes one orbit every 98 minutes, travelling at approximately 27,106 km/h (16,843 mph).
ZK-2 R/B (NORAD ID 101282) 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.
ZK-2 R/B was launched on 2026-11-03 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks ZK-2 R/B (NORAD ID 101282) 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.
ZK-2 R/B travels at approximately 27,106 km/h (16,843 mph) — roughly 7.53 km/s. It completes 14.70 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.