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JIELONG 3 R/B

NORAD 58507 Rocket Body LEO 2023-190C
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
336 km
Apogee
659 km
Inclination
86.6°
Period
94.6 min
Mean Motion
15.22841602 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude498 km
Orbital Velocity27,425 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.23
Eccentricity0.0235
Semi-Major Axis6,869 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2023-12-05
Launch Site
SCSLA
Int'l Designator
2023-190C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
JIELONG 3 R/B is a spent rocket body associated with China, launched on 2023-12-05 from SCSLA on the WHJSW 03 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 336 km and 659 km with an inclination of 86.6°. It travels at approximately 27,425 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.23 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Spent rocket bodies like JIELONG 3 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
JIELONG 3 R/B orbits at an average altitude of 498 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 JIELONG 3 R/B’s average altitude, there are currently 9,215 active payloads and 237 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 52.7% of all active satellites. With an inclination of 86.6°, JIELONG 3 R/B passes over latitudes between 86.6°N and 86.6°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 192 share a similar altitude band with JIELONG 3 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
JIELONG 3 R/B orbits in Low Earth Orbit (LEO) at altitudes between 336 km (perigee) and 659 km (apogee), with an average altitude of approximately 498 km. It completes one orbit every 95 minutes, travelling at approximately 27,425 km/h (17,041 mph).
JIELONG 3 R/B (NORAD ID 58507) 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.
JIELONG 3 R/B was launched on 2023-12-05 from SCSLA. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks JIELONG 3 R/B (NORAD ID 58507) 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.
JIELONG 3 R/B travels at approximately 27,425 km/h (17,041 mph) — roughly 7.62 km/s. It completes 15.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.