SCOUT B DEB
NORAD 2800
Debris
MEO
1966-070D
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MEO · NORAD 2800
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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
401 km
Apogee
2571 km
Inclination
81.4°
Period
115.7 min
Mean Motion
12.44809218 rev/day
TLE Epoch
2026-11-03 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,486 km
Orbital Velocity25,641 km/h
Velocity7.12 km/s
Orbital Period116 minutes
Orbits / Day12.45
Eccentricity0.1381
Semi-Major Axis7,857 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-08-04
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-070D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SCOUT B DEB is a tracked piece of space debris attributed to United States, launched on 1966-08-04 from Vandenberg Space Force Base, United States on the OV3-3 launch. After more than 60 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 401 km and 2,571 km with an inclination of 81.4°. It travels at approximately 25,641 km/h (7.12 km/s), completing one full orbit every 116 minutes — that’s roughly 12.45 orbits per day. Its orbital eccentricity of 0.1381 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, SCOUT B DEB 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
SCOUT B DEB orbits at an average altitude of 1,486 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of SCOUT B DEB’s average altitude, there are currently 404 active payloads and 405 tracked debris or rocket body fragments. With an inclination of 81.4°, SCOUT B DEB passes over latitudes between 81.4°N and 81.4°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. United States operates approximately 13,342 active satellites in total, of which 14 share a similar altitude band with SCOUT B DEB.
🔗 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
SCOUT B DEB orbits in Medium Earth Orbit (MEO) at altitudes between 401 km (perigee) and 2,571 km (apogee), with an average altitude of approximately 1,486 km. It completes one orbit every 116 minutes, travelling at approximately 25,641 km/h (15,933 mph).
SCOUT B DEB (NORAD ID 2800) is a piece of tracked orbital debris attributed to United States. 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.
SCOUT B DEB was launched on 1966-08-04 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks SCOUT B DEB (NORAD ID 2800) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
SCOUT B DEB travels at approximately 25,641 km/h (15,933 mph) — roughly 7.12 km/s. It completes 12.45 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.12 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 SCOUT B DEB. Read more about debris statistics and the Kessler syndrome.