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AVUM R/B

NORAD 40698 Rocket Body LEO 2015-028B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
358 km
Apogee
526 km
Inclination
98.6°
Period
93.4 min
Mean Motion
15.41438370 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude442 km
Orbital Velocity27,536 km/h
Velocity7.65 km/s
Orbital Period93 minutes
Orbits / Day15.41
Eccentricity0.0123
Semi-Major Axis6,813 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
2015-06-23
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2015-028B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
AVUM R/B is a spent rocket body associated with France, launched on 2015-06-23 from Guiana Space Centre, Kourou on the Sentinel-2A launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 358 km and 526 km with an inclination of 98.6°. It travels at approximately 27,536 km/h (7.65 km/s), completing one full orbit every 93 minutes — that’s roughly 15.41 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 ~1–3 years. Spent rocket bodies like AVUM 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
AVUM R/B orbits at an average altitude of 442 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 AVUM R/B’s average altitude, there are currently 7,782 active payloads and 151 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 44.5% of all active satellites. With an inclination of 98.6°, AVUM R/B passes over latitudes between 98.6°N and 98.6°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 12 share a similar altitude band with AVUM 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
AVUM R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 442 km altitude. Its 98.6° 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 93 minutes, travelling at 27,536 km/h.
AVUM R/B (NORAD ID 40698) 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.
AVUM R/B was launched on 2015-06-23 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks AVUM R/B (NORAD ID 40698) 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.
AVUM R/B travels at approximately 27,536 km/h (17,110 mph) — roughly 7.65 km/s. It completes 15.41 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.