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AVUM DEB (ADAPTOR)

NORAD 39162 Debris LEO 2013-021D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
642 km
Apogee
760 km
Inclination
98.8°
Period
98.8 min
Mean Motion
14.57515605 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude701 km
Orbital Velocity27,027 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.58
Eccentricity0.0083
Semi-Major Axis7,072 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
2013-05-07
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2013-021D
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
AVUM DEB (ADAPTOR) is a tracked piece of space debris attributed to ESA (European Space Agency), launched on 2013-05-07 from Guiana Space Centre, Kourou on the PROBA-V launch. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 642 km and 760 km with an inclination of 98.8°. It travels at approximately 27,027 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.58 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. As orbital debris, AVUM DEB (ADAPTOR) poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
AVUM DEB (ADAPTOR) orbits at an average altitude of 701 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 DEB (ADAPTOR)’s average altitude, there are currently 273 active payloads and 1,469 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.8°, AVUM DEB (ADAPTOR) passes over latitudes between 98.8°N and 98.8°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. ESA (European Space Agency) operates approximately 93 active satellites in total, of which 8 share a similar altitude band with AVUM DEB (ADAPTOR).
🔗 Tracked Space Debris

This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.

❓ Frequently Asked Questions
AVUM DEB (ADAPTOR) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 701 km altitude. Its 98.8° 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 99 minutes, travelling at 27,027 km/h.
AVUM DEB (ADAPTOR) (NORAD ID 39162) is a piece of tracked orbital debris attributed to ESA (European Space Agency). It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
AVUM DEB (ADAPTOR) was launched on 2013-05-07 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 AVUM DEB (ADAPTOR) (NORAD ID 39162) 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 DEB (ADAPTOR) travels at approximately 27,027 km/h (16,794 mph) — roughly 7.51 km/s. It completes 14.58 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.51 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like AVUM DEB (ADAPTOR). Read more about debris statistics and the Kessler syndrome.