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PEGASUS DEB

NORAD 24129 Debris LEO 1994-029GC
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Longitude
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🛰️ Orbital Parameters
Perigee
535 km
Apogee
1324 km
Inclination
81.5°
Period
103.6 min
Mean Motion
13.89679877 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude930 km
Orbital Velocity26,601 km/h
Velocity7.39 km/s
Orbital Period104 minutes
Orbits / Day13.90
Eccentricity0.0540
Semi-Major Axis7,301 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1994-05-19
Launch Site
Vandenberg SFB, California
Int'l Designator
1994-029GC
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PEGASUS DEB is a tracked piece of space debris attributed to United States, launched on 1994-05-19 from Vandenberg SFB, California. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 535 km and 1,324 km with an inclination of 81.5°. It travels at approximately 26,601 km/h (7.39 km/s), completing one full orbit every 104 minutes — that’s roughly 13.90 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, PEGASUS 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
PEGASUS DEB orbits at an average altitude of 930 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 PEGASUS DEB’s average altitude, there are currently 257 active payloads and 1,146 tracked debris or rocket body fragments. With an inclination of 81.5°, PEGASUS DEB passes over latitudes between 81.5°N and 81.5°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 12,339 active satellites in total, of which 87 share a similar altitude band with PEGASUS 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
PEGASUS DEB orbits in Low Earth Orbit (LEO) at altitudes between 535 km (perigee) and 1,324 km (apogee), with an average altitude of approximately 930 km. It completes one orbit every 104 minutes, travelling at approximately 26,601 km/h (16,529 mph).
PEGASUS DEB (NORAD ID 24129) 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.
PEGASUS DEB was launched on 1994-05-19 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 PEGASUS DEB (NORAD ID 24129) 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.
PEGASUS DEB travels at approximately 26,601 km/h (16,529 mph) — roughly 7.39 km/s. It completes 13.90 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 7.39 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 PEGASUS DEB. Read more about debris statistics and the Kessler syndrome.