Skip to content
Home › Library › Satellite Directory › CHOLLIMA-1 R/B

CHOLLIMA-1 R/B

NORAD 58401 Rocket Body LEO 2023-179B
CONNECTING… LEO · NORAD 58401
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
343 km
Apogee
362 km
Inclination
97.3°
Period
91.6 min
Mean Motion
15.72088763 rev/day
TLE Epoch
2026-10-14 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude353 km
Orbital Velocity27,719 km/h
Velocity7.70 km/s
Orbital Period92 minutes
Orbits / Day15.72
Eccentricity0.0014
Semi-Major Axis6,724 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
North Korea
Launch Date
2023-11-21
Launch Site
Sohae / Tonghae, North Korea
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 Sohae / Tonghae, North Korea on the Manligyeong-1 F3 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 343 km and 362 km with an inclination of 97.3°. It travels at approximately 27,719 km/h (7.70 km/s), completing one full orbit every 92 minutes — that’s roughly 15.72 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 353 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 1,034 active payloads and 39 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 5.5% 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 353 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 27,719 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 Sohae / Tonghae, North Korea. 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) 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.
CHOLLIMA-1 R/B travels at approximately 27,719 km/h (17,224 mph) — roughly 7.70 km/s. It completes 15.72 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.