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LVM3 R/B

NORAD 66310 Rocket Body MEO 2025-249A
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
124 km
Apogee
17957 km
Inclination
21.5°
Period
317.6 min
Mean Motion
7.20967326 rev/day
TLE Epoch
2026-06-26 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,041 km
Orbital Velocity18,308 km/h
Velocity5.09 km/s
Orbital Period5 hours 18 minutes
Orbits / Day7.21
Eccentricity0.5786
Semi-Major Axis15,412 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2025-11-02
Launch Site
SRI
Int'l Designator
2025-249A
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
LVM3 R/B is a spent rocket body associated with India, launched on 2025-11-02 from SRI on the GSAT-7R launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Medium Earth Orbit (MEO) at altitudes between 124 km and 17,957 km with an inclination of 21.5°. It travels at approximately 18,308 km/h (5.09 km/s), completing one full orbit every 5 hours 18 minutes — that’s roughly 7.21 orbits per day. Its orbital eccentricity of 0.5786 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like LVM3 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
LVM3 R/B orbits at an average altitude of 9,041 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 LVM3 R/B’s average altitude, there are currently 2 active payloads and 10 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 21.5°, LVM3 R/B passes over latitudes between 21.5°N and 21.5°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.
🔗 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
LVM3 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 124 km (perigee) and 17,957 km (apogee), with an average altitude of approximately 9,041 km. It completes one orbit every 5 hours 18 minutes, travelling at approximately 18,308 km/h (11,376 mph).
LVM3 R/B (NORAD ID 66310) 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.
LVM3 R/B was launched on 2025-11-02 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 LVM3 R/B (NORAD ID 66310) 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.
LVM3 R/B travels at approximately 18,308 km/h (11,376 mph) — roughly 5.09 km/s. It completes 7.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 14 sunrises and sunsets every 24 hours.