PEGASUS DEB
NORAD 39314
Debris
LEO
1994-029AEZ
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LEO · NORAD 39314
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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
541 km
Apogee
763 km
Inclination
81.7°
Period
97.8 min
Mean Motion
14.72978769 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude652 km
Orbital Velocity27,121 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.73
Eccentricity0.0158
Semi-Major Axis7,023 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1994-05-19
Launch Site
Vandenberg SFB, California
Int'l Designator
1994-029AEZ
Object Type
Debris
RCS Size
Small (<0.1 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 on the STEP 2 launch. With over 32 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 541 km and 763 km with an inclination of 81.7°. It travels at approximately 27,121 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.73 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 652 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of PEGASUS DEB’s average altitude, there are currently 697 active payloads and 1,045 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA. With an inclination of 81.7°, PEGASUS DEB passes over latitudes between 81.7°N and 81.7°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 12,358 active satellites in total, of which 298 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 541 km (perigee) and 763 km (apogee), with an average altitude of approximately 652 km. It completes one orbit every 98 minutes, travelling at approximately 27,121 km/h (16,852 mph).
PEGASUS DEB (NORAD ID 39314) 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks PEGASUS DEB (NORAD ID 39314) 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 27,121 km/h (16,852 mph) — roughly 7.53 km/s. It completes 14.73 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.53 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.