PSLV R/B
NORAD 46915
Rocket Body
LEO
2020-081L
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LEO · NORAD 46915
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
436 km
Apogee
466 km
Inclination
36.8°
Period
93.6 min
Mean Motion
15.38284764 rev/day
TLE Epoch
2026-06-25 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude451 km
Orbital Velocity27,518 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.38
Eccentricity0.0022
Semi-Major Axis6,822 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2020-11-07
Launch Site
SRI
Int'l Designator
2020-081L
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 2020-11-07 from SRI on the PSLV Rideshare 17 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 436 km and 466 km with an inclination of 36.8°. It travels at approximately 27,518 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.38 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 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 451 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 PSLV R/B’s average altitude, there are currently 7,929 active payloads and 160 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 45.3% of all active satellites. With an inclination of 36.8°, PSLV R/B passes over latitudes between 36.8°N and 36.8°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. India operates approximately 108 active satellites in total, of which 4 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 orbits in Low Earth Orbit (LEO) at altitudes between 436 km (perigee) and 466 km (apogee), with an average altitude of approximately 451 km. It completes one orbit every 94 minutes, travelling at approximately 27,518 km/h (17,099 mph).
PSLV R/B (NORAD ID 46915) 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 2020-11-07 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks PSLV R/B (NORAD ID 46915) 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 27,518 km/h (17,099 mph) — roughly 7.64 km/s. It completes 15.38 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.