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PSLV R/B

NORAD 62257 Rocket Body HEO 2024-233B
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🛰️ Orbital Parameters
Perigee
1046 km
Apogee
60825 km
Inclination
60.0°
Period
1195.5 min
Mean Motion
1.20449649 rev/day
TLE Epoch
2026-10-14 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude30,936 km
Orbital Velocity11,767 km/h
Velocity3.27 km/s
Orbital Period19 hours 56 minutes
Orbits / Day1.20
Eccentricity0.8012
Semi-Major Axis37,307 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2024-12-05
Launch Site
Satish Dhawan Space Centre, India
Int'l Designator
2024-233B
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 2024-12-05 from Satish Dhawan Space Centre, India on the PROBA-3 launch. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 1,046 km and 60,825 km with an inclination of 60.0°. It travels at approximately 11,767 km/h (3.27 km/s), completing one full orbit every 19 hours 56 minutes — that’s roughly 1.20 orbits per day. Its orbital eccentricity of 0.8012 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 follows a Highly Elliptical Orbit, sweeping between 1,046 km (perigee) and 60,825 km (apogee). It spends most of its 19 hours 56 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. With an inclination of 60.0°, PSLV R/B passes over latitudes between 60.0°N and 60.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. India operates approximately 106 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 follows a Highly Elliptical Orbit, swinging between 1,046 km (perigee) and 60,825 km (apogee). It spends most of its 19 hours 56 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
PSLV R/B (NORAD ID 62257) 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 2024-12-05 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks PSLV R/B (NORAD ID 62257) 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’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 11,767 km/h (3.27 km/s), completing one revolution every 19 hours 56 minutes. Learn more about highly elliptical orbits.