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SCOUT G-1 DEB

NORAD 15951 Debris LEO 1985-066E
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
809 km
Apogee
963 km
Inclination
89.9°
Period
102.7 min
Mean Motion
14.02288250 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude886 km
Orbital Velocity26,680 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.02
Eccentricity0.0106
Semi-Major Axis7,257 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1985-08-03
Launch Site
Vandenberg SFB, California
Int'l Designator
1985-066E
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SCOUT G-1 DEB is a tracked piece of space debris attributed to United States, launched on 1985-08-03 from Vandenberg SFB, California on the NNS O-24 launch. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 809 km and 963 km with an inclination of 89.9°. It travels at approximately 26,680 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.02 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, SCOUT G-1 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 G-1 DEB orbits at an average altitude of 886 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of SCOUT G-1 DEB’s average altitude, there are currently 170 active payloads and 1,584 tracked debris or rocket body fragments. With an inclination of 89.9°, SCOUT G-1 DEB passes over latitudes between 89.9°N and 89.9°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 12,413 active satellites in total, of which 31 share a similar altitude band with SCOUT G-1 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 G-1 DEB orbits in Low Earth Orbit (LEO) at altitudes between 809 km (perigee) and 963 km (apogee), with an average altitude of approximately 886 km. It completes one orbit every 103 minutes, travelling at approximately 26,680 km/h (16,578 mph).
SCOUT G-1 DEB (NORAD ID 15951) 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 G-1 DEB was launched on 1985-08-03 from Vandenberg SFB, California, 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks SCOUT G-1 DEB (NORAD ID 15951) 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 G-1 DEB travels at approximately 26,680 km/h (16,578 mph) — roughly 7.41 km/s. It completes 14.02 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.41 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 G-1 DEB. Read more about debris statistics and the Kessler syndrome.