SCOUT B DEB
NORAD 29168
Debris
LEO
1965-063S
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LEO · NORAD 29168
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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
1150 km
Apogee
1720 km
Inclination
69.3°
Period
114.6 min
Mean Motion
12.57036110 rev/day
TLE Epoch
2026-06-20 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,435 km
Orbital Velocity25,725 km/h
Velocity7.15 km/s
Orbital Period115 minutes
Orbits / Day12.57
Eccentricity0.0365
Semi-Major Axis7,806 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
1965-063S
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 Low Earth Orbit (LEO) at altitudes between 1,150 km and 1,720 km with an inclination of 69.3°. It travels at approximately 25,725 km/h (7.15 km/s), completing one full orbit every 115 minutes — that’s roughly 12.57 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 1,435 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of SCOUT B DEB’s average altitude, there are currently 357 active payloads and 178 tracked debris or rocket body fragments. With an inclination of 69.3°, SCOUT B DEB passes over latitudes between 69.3°N and 69.3°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 Low Earth Orbit (LEO) at altitudes between 1,150 km (perigee) and 1,720 km (apogee), with an average altitude of approximately 1,435 km. It completes one orbit every 115 minutes, travelling at approximately 25,725 km/h (15,985 mph).
SCOUT B DEB (NORAD ID 29168) 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 29168) 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 25,725 km/h (15,985 mph) — roughly 7.15 km/s. It completes 12.57 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 7.15 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.