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CHOLLIMA-1 R/B

NORAD 58401 Rocket Body LEO 2023-179B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
365 km
Apogee
388 km
Inclination
97.3°
Period
92.1 min
Mean Motion
15.63937645 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude377 km
Orbital Velocity27,669 km/h
Velocity7.69 km/s
Orbital Period92 minutes
Orbits / Day15.64
Eccentricity0.0017
Semi-Major Axis6,748 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
North Korea
Launch Date
2023-11-21
Launch Site
YUN
Int'l Designator
2023-179B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CHOLLIMA-1 R/B is a spent rocket body associated with North Korea, launched on 2023-11-21 from YUN on the Manligyeong-1 F3 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 365 km and 388 km with an inclination of 97.3°. It travels at approximately 27,669 km/h (7.69 km/s), completing one full orbit every 92 minutes — that’s roughly 15.64 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 CHOLLIMA-1 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
CHOLLIMA-1 R/B orbits at an average altitude of 377 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 CHOLLIMA-1 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 97.3°, CHOLLIMA-1 R/B passes over latitudes between 97.3°N and 97.3°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.
🔗 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
CHOLLIMA-1 R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 377 km altitude. Its 97.3° 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 27,669 km/h.
CHOLLIMA-1 R/B (NORAD ID 58401) is a spent rocket body — the upper stage of a launch vehicle attributed to North 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.
CHOLLIMA-1 R/B was launched on 2023-11-21 from YUN. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks CHOLLIMA-1 R/B (NORAD ID 58401) 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.
CHOLLIMA-1 R/B travels at approximately 27,669 km/h (17,193 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.