ARIANE 42L+3 R/B
NORAD 23687
Rocket Body
MEO
1995-055B
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MEO · NORAD 23687
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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
463 km
Apogee
36375 km
Inclination
4.9°
Period
647.7 min
Mean Motion
2.22332353 rev/day
TLE Epoch
2026-06-26 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude18,419 km
Orbital Velocity14,436 km/h
Velocity4.01 km/s
Orbital Period10 hours 48 minutes
Orbits / Day2.22
Eccentricity0.7243
Semi-Major Axis24,790 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1995-10-19
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1995-055B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ARIANE 42L+3 R/B is a spent rocket body associated with France, launched on 1995-10-19 from Guiana Space Centre, Kourou on the Astra 1E launch. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 463 km and 36,375 km with an inclination of 4.9°. It travels at approximately 14,436 km/h (4.01 km/s), completing one full orbit every 10 hours 48 minutes — that’s roughly 2.22 orbits per day. Its orbital eccentricity of 0.7243 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like ARIANE 42L+3 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 42L+3 R/B orbits at an average altitude of 18,419 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 ARIANE 42L+3 R/B’s average altitude, there are currently 0 active payloads and 21 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 4.9°, ARIANE 42L+3 R/B passes over latitudes between 4.9°N and 4.9°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 42L+3 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 463 km (perigee) and 36,375 km (apogee), with an average altitude of approximately 18,419 km. It completes one orbit every 10 hours 48 minutes, travelling at approximately 14,436 km/h (8,970 mph).
ARIANE 42L+3 R/B (NORAD ID 23687) 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 42L+3 R/B was launched on 1995-10-19 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 42L+3 R/B (NORAD ID 23687) 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 42L+3 R/B travels at approximately 14,436 km/h (8,970 mph) — roughly 4.01 km/s. It completes 2.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.