TLV R/B
NORAD 58501
Rocket Body
LEO
2023-188B
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LEO · NORAD 58501
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
402 km
Apogee
550 km
Inclination
46.9°
Period
94.1 min
Mean Motion
15.29902407 rev/day
TLE Epoch
2026-06-25 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude476 km
Orbital Velocity27,468 km/h
Velocity7.63 km/s
Orbital Period94 minutes
Orbits / Day15.30
Eccentricity0.0108
Semi-Major Axis6,847 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇰🇷 South Korea
Launch Date
2023-12-04
Launch Site
JJSLA
Int'l Designator
2023-188B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
TLV R/B is a spent rocket body associated with South Korea, launched on 2023-12-04 from JJSLA on the S-STEP launch. It orbits in Low Earth Orbit (LEO) at altitudes between 402 km and 550 km with an inclination of 46.9°. It travels at approximately 27,468 km/h (7.63 km/s), completing one full orbit every 94 minutes — that’s roughly 15.30 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Spent rocket bodies like TLV 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
TLV R/B orbits at an average altitude of 476 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of TLV R/B’s average altitude, there are currently 8,225 active payloads and 209 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 47% of all active satellites. With an inclination of 46.9°, TLV R/B passes over latitudes between 46.9°N and 46.9°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. South Korea operates approximately 51 active satellites in total, of which 11 share a similar altitude band with TLV 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
TLV R/B orbits in Low Earth Orbit (LEO) at altitudes between 402 km (perigee) and 550 km (apogee), with an average altitude of approximately 476 km. It completes one orbit every 94 minutes, travelling at approximately 27,468 km/h (17,068 mph).
TLV R/B (NORAD ID 58501) 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.
TLV R/B was launched on 2023-12-04 from JJSLA. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks TLV R/B (NORAD ID 58501) 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.
TLV R/B travels at approximately 27,468 km/h (17,068 mph) — roughly 7.63 km/s. It completes 15.30 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.