SCOUT B DEB
NORAD 29170
Debris
MEO
1965-063U
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MEO · NORAD 29170
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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
1119 km
Apogee
2329 km
Inclination
69.2°
Period
121.0 min
Mean Motion
11.90414974 rev/day
TLE Epoch
2026-06-14 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,724 km
Orbital Velocity25,262 km/h
Velocity7.02 km/s
Orbital Period2 hours 1 minutes
Orbits / Day11.90
Eccentricity0.0747
Semi-Major Axis8,095 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-08-10
Launch Site
Wallops Island, Virginia
Int'l Designator
1965-063U
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 1965-08-10 from Wallops Island, Virginia on the Secor Type I S/N 2 launch. After more than 61 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 1,119 km and 2,329 km with an inclination of 69.2°. It travels at approximately 25,262 km/h (7.02 km/s), completing one full orbit every 2 hours 1 minutes — that’s roughly 11.90 orbits per day. 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 1,724 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 14 active payloads and 49 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 69.2°, SCOUT B DEB passes over latitudes between 69.2°N and 69.2°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,358 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 1,119 km (perigee) and 2,329 km (apogee), with an average altitude of approximately 1,724 km. It completes one orbit every 2 hours 1 minutes, travelling at approximately 25,262 km/h (15,697 mph).
SCOUT B DEB (NORAD ID 29170) 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 1965-08-10 from Wallops Island, Virginia. 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 29170) 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 25,262 km/h (15,697 mph) — roughly 7.02 km/s. It completes 11.90 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 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 7.02 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.