ARIANE 5 R/B
NORAD 35757
Rocket Body
MEO
2009-044C
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MEO · NORAD 35757
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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
254 km
Apogee
31866 km
Inclination
1.7°
Period
557.5 min
Mean Motion
2.58305938 rev/day
TLE Epoch
2026-10-14 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude16,060 km
Orbital Velocity15,176 km/h
Velocity4.22 km/s
Orbital Period9 hours 17 minutes
Orbits / Day2.58
Eccentricity0.7046
Semi-Major Axis22,431 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
2009-08-21
Launch Site
Guiana Space Centre, French Guiana
Int'l Designator
2009-044C
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 2009-08-21 from Guiana Space Centre, French Guiana on the JCSAT 12 launch. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 254 km and 31,866 km with an inclination of 1.7°. It travels at approximately 15,176 km/h (4.22 km/s), completing one full orbit every 9 hours 17 minutes — that’s roughly 2.58 orbits per day. Its orbital eccentricity of 0.7046 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 16,060 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 1.7°, ARIANE 5 R/B passes over latitudes between 1.7°N and 1.7°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. France operates approximately 120 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 254 km (perigee) and 31,866 km (apogee), with an average altitude of approximately 16,060 km. It completes one orbit every 9 hours 17 minutes, travelling at approximately 15,176 km/h (9,430 mph).
ARIANE 5 R/B (NORAD ID 35757) 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 2009-08-21 from Guiana Space Centre, French Guiana. 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 35757) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 15,176 km/h (9,430 mph) — roughly 4.22 km/s. It completes 2.58 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.