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KSLV-II R/B

NORAD 100969 Rocket Body LEO 2026-229Q
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🛰️ Orbital Parameters
Perigee
525 km
Apogee
574 km
Inclination
97.7°
Period
95.7 min
Mean Motion
15.05536108 rev/day
TLE Epoch
2026-10-08 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude550 km
Orbital Velocity27,321 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.06
Eccentricity0.0035
Semi-Major Axis6,921 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇰🇷 South Korea
Launch Date
2026-10-07
Launch Site
Naro Space Center, South Korea
Int'l Designator
2026-229Q
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
KSLV-II R/B is a spent rocket body associated with South Korea, launched on 2026-10-07 from Naro Space Center, South Korea on the NeonSat 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 525 km and 574 km with an inclination of 97.7°. It travels at approximately 27,321 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.06 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 ~3–10 years. Spent rocket bodies like KSLV-II 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
KSLV-II R/B orbits at an average altitude of 550 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 KSLV-II R/B’s average altitude, there are currently 1,519 active payloads and 403 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 8.1% of all active satellites. With an inclination of 97.7°, KSLV-II R/B passes over latitudes between 97.7°N and 97.7°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. South Korea operates approximately 58 active satellites in total, of which 20 share a similar altitude band with KSLV-II 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
KSLV-II R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 550 km altitude. Its 97.7° 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 96 minutes, travelling at 27,321 km/h.
KSLV-II R/B (NORAD ID 100969) is a spent rocket body — the upper stage of a launch vehicle attributed to South Korea. 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.
KSLV-II R/B was launched on 2026-10-07 from Naro Space Center, South Korea. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks KSLV-II R/B (NORAD ID 100969) 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.
KSLV-II R/B travels at approximately 27,321 km/h (16,977 mph) — roughly 7.59 km/s. It completes 15.06 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.