SCOUT B DEB
NORAD 2498
Debris
MEO
1966-052C
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MEO · NORAD 2498
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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
582 km
Apogee
4208 km
Inclination
40.6°
Period
136.3 min
Mean Motion
10.56494437 rev/day
TLE Epoch
2026-09-19 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,395 km
Orbital Velocity24,276 km/h
Velocity6.74 km/s
Orbital Period2 hours 16 minutes
Orbits / Day10.56
Eccentricity0.2068
Semi-Major Axis8,766 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-06-10
Launch Site
Wallops Flight Facility / MARS, United States
Int'l Designator
1966-052C
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 1966-06-10 from Wallops Flight Facility / MARS, United States on the OV3-4 PHASR 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 582 km and 4,208 km with an inclination of 40.6°. It travels at approximately 24,276 km/h (6.74 km/s), completing one full orbit every 2 hours 16 minutes — that’s roughly 10.56 orbits per day. Its orbital eccentricity of 0.2068 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 2,395 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 0 active payloads and 10 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 40.6°, SCOUT B DEB passes over latitudes between 40.6°N and 40.6°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 13,196 active satellites in total.
🔗 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 582 km (perigee) and 4,208 km (apogee), with an average altitude of approximately 2,395 km. It completes one orbit every 2 hours 16 minutes, travelling at approximately 24,276 km/h (15,084 mph).
SCOUT B DEB (NORAD ID 2498) 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 1966-06-10 from Wallops Flight Facility / MARS, United States. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks SCOUT B DEB (NORAD ID 2498) 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.
SCOUT B DEB travels at approximately 24,276 km/h (15,084 mph) — roughly 6.74 km/s. It completes 10.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 21 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 6.74 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.