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ARIANE 5 R/B

NORAD 37607 Rocket Body MEO 2011-022C
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Longitude
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🛰️ Orbital Parameters
Perigee
145 km
Apogee
16469 km
Inclination
2.4°
Period
295.2 min
Mean Motion
4.88213507 rev/day
TLE Epoch
2026-06-26 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude8,307 km
Orbital Velocity18,760 km/h
Velocity5.21 km/s
Orbital Period4 hours 55 minutes
Orbits / Day4.88
Eccentricity0.5561
Semi-Major Axis14,678 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
2011-05-20
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2011-022C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ARIANE 5 R/B is a spent rocket body associated with France, launched on 2011-05-20 from Guiana Space Centre, Kourou on the INSAT-4G launch. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 145 km and 16,469 km with an inclination of 2.4°. It travels at approximately 18,760 km/h (5.21 km/s), completing one full orbit every 4 hours 55 minutes — that’s roughly 4.88 orbits per day. Its orbital eccentricity of 0.5561 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like ARIANE 5 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
ARIANE 5 R/B orbits at an average altitude of 8,307 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. With an inclination of 2.4°, ARIANE 5 R/B passes over latitudes between 2.4°N and 2.4°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. France operates approximately 115 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
ARIANE 5 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 145 km (perigee) and 16,469 km (apogee), with an average altitude of approximately 8,307 km. It completes one orbit every 4 hours 55 minutes, travelling at approximately 18,760 km/h (11,657 mph).
ARIANE 5 R/B (NORAD ID 37607) is a spent rocket body — the upper stage of a launch vehicle attributed to France. 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.
ARIANE 5 R/B was launched on 2011-05-20 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. 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 ARIANE 5 R/B (NORAD ID 37607) 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.
ARIANE 5 R/B travels at approximately 18,760 km/h (11,657 mph) — roughly 5.21 km/s. It completes 4.88 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 10 sunrises and sunsets every 24 hours.