PEGASUS DEB
NORAD 39307
Debris
LEO
1994-029AES
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LEO · NORAD 39307
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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
335 km
Apogee
377 km
Inclination
81.9°
Period
91.7 min
Mean Motion
15.71136647 rev/day
TLE Epoch
2026-11-03 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude356 km
Orbital Velocity27,712 km/h
Velocity7.70 km/s
Orbital Period92 minutes
Orbits / Day15.71
Eccentricity0.0031
Semi-Major Axis6,727 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1994-05-19
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1994-029AES
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 Space Force Base, United States 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 335 km and 377 km with an inclination of 81.9°. It travels at approximately 27,712 km/h (7.70 km/s), completing one full orbit every 92 minutes — that’s roughly 15.71 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. 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 356 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of PEGASUS DEB’s average altitude, there are currently 1,164 active payloads and 40 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 5.9% of all active satellites. With an inclination of 81.9°, PEGASUS DEB passes over latitudes between 81.9°N and 81.9°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 13,350 active satellites in total, of which 1,028 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 335 km (perigee) and 377 km (apogee), with an average altitude of approximately 356 km. It completes one orbit every 92 minutes, travelling at approximately 27,712 km/h (17,219 mph).
PEGASUS DEB (NORAD ID 39307) 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 Space Force Base, United States, 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks PEGASUS DEB (NORAD ID 39307) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 27,712 km/h (17,219 mph) — roughly 7.70 km/s. It completes 15.71 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 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 7.70 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.