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PSLV R/B

NORAD 33406 Rocket Body MEO 2008-052B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
250 km
Apogee
18815 km
Inclination
17.8°
Period
332.9 min
Mean Motion
4.32581498 rev/day
TLE Epoch
2026-06-24 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,533 km
Orbital Velocity18,023 km/h
Velocity5.01 km/s
Orbital Period5 hours 33 minutes
Orbits / Day4.33
Eccentricity0.5837
Semi-Major Axis15,904 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2008-10-22
Launch Site
SRI
Int'l Designator
2008-052B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
PSLV R/B is a spent rocket body associated with India, launched on 2008-10-22 from SRI on the Chandrayaan-1 launch. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 250 km and 18,815 km with an inclination of 17.8°. It travels at approximately 18,023 km/h (5.01 km/s), completing one full orbit every 5 hours 33 minutes — that’s roughly 4.33 orbits per day. Its orbital eccentricity of 0.5837 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like PSLV 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
PSLV R/B orbits at an average altitude of 9,533 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of PSLV R/B’s average altitude, there are currently 0 active payloads and 9 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 17.8°, PSLV R/B passes over latitudes between 17.8°N and 17.8°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. India operates approximately 108 active satellites in total.
🔗 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
PSLV R/B orbits in Medium Earth Orbit (MEO) at altitudes between 250 km (perigee) and 18,815 km (apogee), with an average altitude of approximately 9,533 km. It completes one orbit every 5 hours 33 minutes, travelling at approximately 18,023 km/h (11,199 mph).
PSLV R/B (NORAD ID 33406) is a spent rocket body — the upper stage of a launch vehicle attributed to India. 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.
PSLV R/B was launched on 2008-10-22 from SRI. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks PSLV R/B (NORAD ID 33406) 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.
PSLV R/B travels at approximately 18,023 km/h (11,199 mph) — roughly 5.01 km/s. It completes 4.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 9 sunrises and sunsets every 24 hours.