ARIANE 2 R/B
NORAD 19920
Rocket Body
MEO
1989-027B
CONNECTING…
MEO · NORAD 19920
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
358 km
Apogee
15203 km
Inclination
4.0°
Period
279.4 min
Mean Motion
5.15305501 rev/day
TLE Epoch
2026-06-25 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,781 km
Orbital Velocity19,106 km/h
Velocity5.31 km/s
Orbital Period4 hours 39 minutes
Orbits / Day5.15
Eccentricity0.5245
Semi-Major Axis14,152 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1989-04-02
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1989-027B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ARIANE 2 R/B is a spent rocket body associated with France, launched on 1989-04-02 from Guiana Space Centre, Kourou on the Tele-X launch. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 358 km and 15,203 km with an inclination of 4.0°. It travels at approximately 19,106 km/h (5.31 km/s), completing one full orbit every 4 hours 39 minutes — that’s roughly 5.15 orbits per day. Its orbital eccentricity of 0.5245 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like ARIANE 2 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 2 R/B orbits at an average altitude of 7,781 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 2 R/B’s average altitude, there are currently 0 active payloads and 5 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 4.0°, ARIANE 2 R/B passes over latitudes between 4.0°N and 4.0°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 2 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 358 km (perigee) and 15,203 km (apogee), with an average altitude of approximately 7,781 km. It completes one orbit every 4 hours 39 minutes, travelling at approximately 19,106 km/h (11,872 mph).
ARIANE 2 R/B (NORAD ID 19920) 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 2 R/B was launched on 1989-04-02 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 2 R/B (NORAD ID 19920) 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 2 R/B travels at approximately 19,106 km/h (11,872 mph) — roughly 5.31 km/s. It completes 5.15 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 10 sunrises and sunsets every 24 hours.