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GSLV R/B

NORAD 65054 Rocket Body LEO 2025-163B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
724 km
Apogee
742 km
Inclination
98.4°
Period
99.5 min
Mean Motion
14.47845768 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude733 km
Orbital Velocity26,966 km/h
Velocity7.49 km/s
Orbital Period99 minutes
Orbits / Day14.48
Eccentricity0.0013
Semi-Major Axis7,104 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2025-07-30
Launch Site
SRI
Int'l Designator
2025-163B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
GSLV R/B is a spent rocket body associated with India, launched on 2025-07-30 from SRI on the NISAR launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 724 km and 742 km with an inclination of 98.4°. It travels at approximately 26,966 km/h (7.49 km/s), completing one full orbit every 99 minutes — that’s roughly 14.48 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 ~25–100 years. Spent rocket bodies like GSLV 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
GSLV R/B orbits at an average altitude of 733 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 GSLV R/B’s average altitude, there are currently 359 active payloads and 1,871 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.4°, GSLV R/B passes over latitudes between 98.4°N and 98.4°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 108 active satellites in total, of which 7 share a similar altitude band with GSLV 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
GSLV R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 733 km altitude. Its 98.4° 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 99 minutes, travelling at 26,966 km/h.
GSLV R/B (NORAD ID 65054) 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.
GSLV R/B was launched on 2025-07-30 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks GSLV R/B (NORAD ID 65054) 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.
GSLV R/B travels at approximately 26,966 km/h (16,756 mph) — roughly 7.49 km/s. It completes 14.48 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.