GSLV R/B
NORAD 54149
Rocket Body
LEO
2022-138AN
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LEO · NORAD 54149
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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
559 km
Apogee
592 km
Inclination
87.4°
Period
96.2 min
Mean Motion
14.97293389 rev/day
TLE Epoch
2026-06-25 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude576 km
Orbital Velocity27,270 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day14.97
Eccentricity0.0024
Semi-Major Axis6,947 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2022-10-22
Launch Site
SRI
Int'l Designator
2022-138AN
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 2022-10-22 from SRI on the OneWeb L14 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 559 km and 592 km with an inclination of 87.4°. It travels at approximately 27,270 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 14.97 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 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 576 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 GSLV R/B’s average altitude, there are currently 2,965 active payloads and 512 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-2112, STARLINK-2722. This makes it one of the more crowded altitude bands, containing roughly 17% of all active satellites. With an inclination of 87.4°, GSLV R/B passes over latitudes between 87.4°N and 87.4°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 14 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 orbits in Low Earth Orbit (LEO) at altitudes between 559 km (perigee) and 592 km (apogee), with an average altitude of approximately 576 km. It completes one orbit every 96 minutes, travelling at approximately 27,270 km/h (16,945 mph).
GSLV R/B (NORAD ID 54149) 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 2022-10-22 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks GSLV R/B (NORAD ID 54149) 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 27,270 km/h (16,945 mph) — roughly 7.58 km/s. It completes 14.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.