Skip to content
Home › Library › Satellite Directory › ARIANE 2 R/B

ARIANE 2 R/B

NORAD 19622 Rocket Body MEO 1988-098B
CONNECTING… MEO · NORAD 19622
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
360 km
Apogee
19542 km
Inclination
3.8°
Period
346.1 min
Mean Motion
4.16074337 rev/day
TLE Epoch
2026-10-15 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,951 km
Orbital Velocity17,790 km/h
Velocity4.94 km/s
Orbital Period5 hours 46 minutes
Orbits / Day4.16
Eccentricity0.5876
Semi-Major Axis16,322 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1988-10-28
Launch Site
Guiana Space Centre, French Guiana
Int'l Designator
1988-098B
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 1988-10-28 from Guiana Space Centre, French Guiana on the TDF 1 launch. With over 38 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 360 km and 19,542 km with an inclination of 3.8°. It travels at approximately 17,790 km/h (4.94 km/s), completing one full orbit every 5 hours 46 minutes — that’s roughly 4.16 orbits per day. Its orbital eccentricity of 0.5876 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 9,951 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 2 active payloads and 4 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 3.8°, ARIANE 2 R/B passes over latitudes between 3.8°N and 3.8°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 2 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 360 km (perigee) and 19,542 km (apogee), with an average altitude of approximately 9,951 km. It completes one orbit every 5 hours 46 minutes, travelling at approximately 17,790 km/h (11,054 mph).
ARIANE 2 R/B (NORAD ID 19622) 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 1988-10-28 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 2 R/B (NORAD ID 19622) 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 2 R/B travels at approximately 17,790 km/h (11,054 mph) — roughly 4.94 km/s. It completes 4.16 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 8 sunrises and sunsets every 24 hours.