ARIANE 5 R/B
NORAD 53766
Rocket Body
HEO
2022-110B
CONNECTING…
HEO · NORAD 53766
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
232 km
Apogee
42841 km
Inclination
4.3°
Period
773.6 min
Mean Motion
1.86149916 rev/day
TLE Epoch
2026-10-15 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude21,537 km
Orbital Velocity13,605 km/h
Velocity3.78 km/s
Orbital Period12 hours 54 minutes
Orbits / Day1.86
Eccentricity0.7634
Semi-Major Axis27,908 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
2022-09-07
Launch Site
Guiana Space Centre, French Guiana
Int'l Designator
2022-110B
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 2022-09-07 from Guiana Space Centre, French Guiana on the Eutelsat Konnect VHTS launch. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 232 km and 42,841 km with an inclination of 4.3°. It travels at approximately 13,605 km/h (3.78 km/s), completing one full orbit every 12 hours 54 minutes — that’s roughly 1.86 orbits per day. Its orbital eccentricity of 0.7634 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 follows a Highly Elliptical Orbit, sweeping between 232 km (perigee) and 42,841 km (apogee). It spends most of its 12 hours 54 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of ARIANE 5 R/B’s average altitude, there are currently 36 active payloads and 10 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 4.3°, ARIANE 5 R/B passes over latitudes between 4.3°N and 4.3°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 follows a Highly Elliptical Orbit, swinging between 232 km (perigee) and 42,841 km (apogee). It spends most of its 12 hours 54 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
ARIANE 5 R/B (NORAD ID 53766) 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 2022-09-07 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 53766) 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’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 13,605 km/h (3.78 km/s), completing one revolution every 12 hours 54 minutes. Learn more about highly elliptical orbits.