ARIANE 40 R/B
NORAD 22830
Rocket Body
LEO
1993-061H
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
775 km
Apogee
789 km
Inclination
98.5°
Period
100.5 min
Mean Motion
14.32911069 rev/day
TLE Epoch
2026-06-25 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude782 km
Orbital Velocity26,874 km/h
Velocity7.46 km/s
Orbital Period100 minutes
Orbits / Day14.33
Eccentricity0.0010
Semi-Major Axis7,153 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1993-09-26
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1993-061H
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 1993-09-26 from Guiana Space Centre, Kourou on the SPOT 3 launch. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 775 km and 789 km with an inclination of 98.5°. It travels at approximately 26,874 km/h (7.46 km/s), completing one full orbit every 100 minutes — that’s roughly 14.33 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. 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 782 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 420 active payloads and 2,226 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.5°, ARIANE 40 R/B passes over latitudes between 98.5°N and 98.5°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 3 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 782 km altitude. Its 98.5° 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 26,874 km/h.
ARIANE 40 R/B (NORAD ID 22830) 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 1993-09-26 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 22830) 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 26,874 km/h (16,699 mph) — roughly 7.46 km/s. It completes 14.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.