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
407 km
Apogee
485 km
Inclination
81.9°
Period
93.5 min
Mean Motion
15.40210316 rev/day
TLE Epoch
2026-06-20 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude446 km
Orbital Velocity27,528 km/h
Velocity7.65 km/s
Orbital Period94 minutes
Orbits / Day15.40
Eccentricity0.0057
Semi-Major Axis6,817 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1994-05-19
Launch Site
Vandenberg SFB, California
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 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 407 km and 485 km with an inclination of 81.9°. It travels at approximately 27,528 km/h (7.65 km/s), completing one full orbit every 94 minutes — that’s roughly 15.40 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 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 446 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of PEGASUS DEB’s average altitude, there are currently 7,684 active payloads and 159 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 44.1% 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 12,358 active satellites in total, of which 7,344 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 407 km (perigee) and 485 km (apogee), with an average altitude of approximately 446 km. It completes one orbit every 94 minutes, travelling at approximately 27,528 km/h (17,105 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 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks PEGASUS DEB (NORAD ID 39307) 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 27,528 km/h (17,105 mph) — roughly 7.65 km/s. It completes 15.40 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 7.65 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.