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ZK-1A R/B

NORAD 64093 Rocket Body LEO 2025-108G
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
351 km
Apogee
440 km
Inclination
97.4°
Period
92.5 min
Mean Motion
15.57311788 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude396 km
Orbital Velocity27,631 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.57
Eccentricity0.0066
Semi-Major Axis6,767 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-05-21
Launch Site
Jiuquan, China
Int'l Designator
2025-108G
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ZK-1A R/B is a spent rocket body associated with China, launched on 2025-05-21 from Jiuquan, China on the Taijing 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 351 km and 440 km with an inclination of 97.4°. It travels at approximately 27,631 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.57 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Spent rocket bodies like ZK-1A 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-1A R/B orbits at an average altitude of 396 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of ZK-1A R/B’s average altitude, there are currently 1,286 active payloads and 88 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 7.4% of all active satellites. With an inclination of 97.4°, ZK-1A R/B passes over latitudes between 97.4°N and 97.4°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 41 share a similar altitude band with ZK-1A 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-1A R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 396 km altitude. Its 97.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 92 minutes, travelling at 27,631 km/h.
ZK-1A R/B (NORAD ID 64093) 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-1A R/B was launched on 2025-05-21 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 ZK-1A R/B (NORAD ID 64093) 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.
ZK-1A R/B travels at approximately 27,631 km/h (17,169 mph) — roughly 7.68 km/s. It completes 15.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.