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ARIANE 40 R/B

NORAD 20443 Rocket Body LEO 1990-005H
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
752 km
Apogee
765 km
Inclination
98.3°
Period
100.0 min
Mean Motion
14.39931482 rev/day
TLE Epoch
2026-06-25 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude759 km
Orbital Velocity26,918 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.40
Eccentricity0.0009
Semi-Major Axis7,130 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1990-01-22
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1990-005H
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ARIANE 40 R/B is a spent rocket body associated with France, launched on 1990-01-22 from Guiana Space Centre, Kourou on the SPOT 2 launch. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 752 km and 765 km with an inclination of 98.3°. It travels at approximately 26,918 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.40 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Spent rocket bodies like ARIANE 40 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 40 R/B orbits at an average altitude of 759 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of ARIANE 40 R/B’s average altitude, there are currently 358 active payloads and 2,034 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179. With an inclination of 98.3°, ARIANE 40 R/B passes over latitudes between 98.3°N and 98.3°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. France operates approximately 115 active satellites in total, of which 5 share a similar altitude band with ARIANE 40 R/B.
🔗 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 40 R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 759 km altitude. Its 98.3° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 100 minutes, travelling at 26,918 km/h.
ARIANE 40 R/B (NORAD ID 20443) 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 40 R/B was launched on 1990-01-22 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks ARIANE 40 R/B (NORAD ID 20443) 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 40 R/B travels at approximately 26,918 km/h (16,726 mph) — roughly 7.48 km/s. It completes 14.40 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.