PSLV R/B
NORAD 41385
Rocket Body
MEO
2016-015B
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MEO · NORAD 41385
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
254 km
Apogee
17411 km
Inclination
17.8°
Period
311.2 min
Mean Motion
4.62798682 rev/day
TLE Epoch
2026-06-26 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude8,833 km
Orbital Velocity18,433 km/h
Velocity5.12 km/s
Orbital Period5 hours 11 minutes
Orbits / Day4.63
Eccentricity0.5642
Semi-Major Axis15,204 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2016-03-10
Launch Site
SRI
Int'l Designator
2016-015B
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 2016-03-10 from SRI on the IRNSS-1F launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 254 km and 17,411 km with an inclination of 17.8°. It travels at approximately 18,433 km/h (5.12 km/s), completing one full orbit every 5 hours 11 minutes — that’s roughly 4.63 orbits per day. Its orbital eccentricity of 0.5642 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 8,833 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 2 active payloads and 10 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 254 km (perigee) and 17,411 km (apogee), with an average altitude of approximately 8,833 km. It completes one orbit every 5 hours 11 minutes, travelling at approximately 18,433 km/h (11,454 mph).
PSLV R/B (NORAD ID 41385) 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 2016-03-10 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 41385) 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 18,433 km/h (11,454 mph) — roughly 5.12 km/s. It completes 4.63 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 9 sunrises and sunsets every 24 hours.