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GSLV R/B

NORAD 56760 Rocket Body MEO 2023-076B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
206 km
Apogee
24164 km
Inclination
19.3°
Period
419.5 min
Mean Motion
3.43323547 rev/day
TLE Epoch
2026-07-16 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude12,185 km
Orbital Velocity16,685 km/h
Velocity4.63 km/s
Orbital Period6 hours 60 minutes
Orbits / Day3.43
Eccentricity0.6456
Semi-Major Axis18,556 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2023-05-29
Launch Site
SRI
Int'l Designator
2023-076B
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 2023-05-29 from SRI on the IRNSS-1J launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 206 km and 24,164 km with an inclination of 19.3°. It travels at approximately 16,685 km/h (4.63 km/s), completing one full orbit every 6 hours 60 minutes — that’s roughly 3.43 orbits per day. Its orbital eccentricity of 0.6456 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 12,185 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of GSLV R/B’s average altitude, there are currently 1 active payload and 3 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 19.3°, GSLV R/B passes over latitudes between 19.3°N and 19.3°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. India operates approximately 109 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
GSLV R/B orbits in Medium Earth Orbit (MEO) at altitudes between 206 km (perigee) and 24,164 km (apogee), with an average altitude of approximately 12,185 km. It completes one orbit every 6 hours 60 minutes, travelling at approximately 16,685 km/h (10,368 mph).
GSLV R/B (NORAD ID 56760) 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 2023-05-29 from SRI. 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 GSLV R/B (NORAD ID 56760) 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 16,685 km/h (10,368 mph) — roughly 4.63 km/s. It completes 3.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 7 sunrises and sunsets every 24 hours.