PSLV R/B
NORAD 41791
Rocket Body
LEO
2016-059J
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LEO · NORAD 41791
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
653 km
Apogee
709 km
Inclination
97.8°
Period
98.4 min
Mean Motion
14.63746430 rev/day
TLE Epoch
2026-10-15 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude681 km
Orbital Velocity27,065 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.64
Eccentricity0.0040
Semi-Major Axis7,052 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2016-09-26
Launch Site
Satish Dhawan Space Centre, India
Int'l Designator
2016-059J
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 2016-09-26 from Satish Dhawan Space Centre, India on the PSLV Rideshare 08 launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 653 km and 709 km with an inclination of 97.8°. It travels at approximately 27,065 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.64 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. 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 681 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of PSLV R/B’s average altitude, there are currently 338 active payloads and 1,360 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 97.8°, PSLV R/B passes over latitudes between 97.8°N and 97.8°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. India operates approximately 101 active satellites in total, of which 7 share a similar altitude band with PSLV 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
PSLV R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 681 km altitude. Its 97.8° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 98 minutes, travelling at 27,065 km/h.
PSLV R/B (NORAD ID 41791) 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 2016-09-26 from Satish Dhawan Space Centre, India, India’s primary launch facility on a barrier island off the coast of Andhra Pradesh. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks PSLV R/B (NORAD ID 41791) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 27,065 km/h (16,818 mph) — roughly 7.52 km/s. It completes 14.64 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.