ARIANE 5 R/B
NORAD 25990
Rocket Body
HEO
1999-066B
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HEO · NORAD 25990
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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
18517 km
Apogee
94116 km
Inclination
71.4°
Period
2603.8 min
Mean Motion
0.55304365 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude56,317 km
Orbital Velocity9,078 km/h
Velocity2.52 km/s
Orbital Period43.4 hours
Orbits / Day0.55
Eccentricity0.6030
Semi-Major Axis62,688 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1999-12-10
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1999-066B
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 1999-12-10 from Guiana Space Centre, Kourou on the XMM launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 18,517 km and 94,116 km with an inclination of 71.4°. It travels at approximately 9,078 km/h (2.52 km/s), completing one full orbit every 43.4 hours — that’s roughly 0.55 orbits per day. Its orbital eccentricity of 0.6030 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. 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 18,517 km (perigee) and 94,116 km (apogee). It spends most of its 43.4 hours 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. With an inclination of 71.4°, ARIANE 5 R/B passes over latitudes between 71.4°N and 71.4°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. 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 5 R/B follows a Highly Elliptical Orbit, swinging between 18,517 km (perigee) and 94,116 km (apogee). It spends most of its 43.4 hours 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 25990) 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 1999-12-10 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. View the full satellite launch log.
Yes — Orbital Radar tracks ARIANE 5 R/B (NORAD ID 25990) 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 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 9,078 km/h (2.52 km/s), completing one revolution every 43.4 hours. Learn more about highly elliptical orbits.