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PSLV R/B

NORAD 40548 Rocket Body MEO 2015-018B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
253 km
Apogee
17903 km
Inclination
19.0°
Period
318.7 min
Mean Motion
4.51808894 rev/day
TLE Epoch
2026-08-30 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,078 km
Orbital Velocity18,286 km/h
Velocity5.08 km/s
Orbital Period5 hours 19 minutes
Orbits / Day4.52
Eccentricity0.5712
Semi-Major Axis15,449 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2015-03-28
Launch Site
SRI
Int'l Designator
2015-018B
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 2015-03-28 from SRI on the IRNSS-1D launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 253 km and 17,903 km with an inclination of 19.0°. It travels at approximately 18,286 km/h (5.08 km/s), completing one full orbit every 5 hours 19 minutes — that’s roughly 4.52 orbits per day. Its orbital eccentricity of 0.5712 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 9,078 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 11 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 19.0°, PSLV R/B passes over latitudes between 19.0°N and 19.0°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. India operates approximately 107 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 253 km (perigee) and 17,903 km (apogee), with an average altitude of approximately 9,078 km. It completes one orbit every 5 hours 19 minutes, travelling at approximately 18,286 km/h (11,362 mph).
PSLV R/B (NORAD ID 40548) 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 2015-03-28 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 40548) 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 18,286 km/h (11,362 mph) — roughly 5.08 km/s. It completes 4.52 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 9 sunrises and sunsets every 24 hours.