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LVM3 CUS R/B

NORAD 67233 Rocket Body LEO 2025-309B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
492 km
Apogee
507 km
Inclination
52.9°
Period
94.6 min
Mean Motion
15.22028407 rev/day
TLE Epoch
2026-06-25 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude500 km
Orbital Velocity27,421 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.22
Eccentricity0.0011
Semi-Major Axis6,871 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2025-12-24
Launch Site
SRI
Int'l Designator
2025-309B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
LVM3 CUS R/B is a spent rocket body associated with India, launched on 2025-12-24 from SRI on the BlueBird Block-2 FM1 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 492 km and 507 km with an inclination of 52.9°. It travels at approximately 27,421 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.22 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Spent rocket bodies like LVM3 CUS 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 CUS R/B orbits at an average altitude of 500 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 LVM3 CUS R/B’s average altitude, there are currently 9,674 active payloads and 240 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 55.3% of all active satellites. With an inclination of 52.9°, LVM3 CUS R/B passes over latitudes between 52.9°N and 52.9°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. India operates approximately 108 active satellites in total, of which 11 share a similar altitude band with LVM3 CUS 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
LVM3 CUS R/B orbits in Low Earth Orbit (LEO) at altitudes between 492 km (perigee) and 507 km (apogee), with an average altitude of approximately 500 km. It completes one orbit every 95 minutes, travelling at approximately 27,421 km/h (17,038 mph).
LVM3 CUS R/B (NORAD ID 67233) 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 CUS R/B was launched on 2025-12-24 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks LVM3 CUS R/B (NORAD ID 67233) 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 CUS R/B travels at approximately 27,421 km/h (17,038 mph) — roughly 7.62 km/s. It completes 15.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.