THOR BURNER 2A DEB
NORAD 29139
Debris
LEO
1974-015F
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LEO · NORAD 29139
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
730 km
Apogee
815 km
Inclination
99.1°
Period
100.3 min
Mean Motion
14.35728021 rev/day
TLE Epoch
2026-06-13 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude773 km
Orbital Velocity26,892 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.36
Eccentricity0.0059
Semi-Major Axis7,144 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1974-03-16
Launch Site
Vandenberg SFB, California
Int'l Designator
1974-015F
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
THOR BURNER 2A DEB is a tracked piece of space debris attributed to United States, launched on 1974-03-16 from Vandenberg SFB, California. After more than 52 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 730 km and 815 km with an inclination of 99.1°. It travels at approximately 26,892 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.36 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, THOR BURNER 2A 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
THOR BURNER 2A DEB orbits at an average altitude of 773 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of THOR BURNER 2A DEB’s average altitude, there are currently 401 active payloads and 2,117 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, ONEWEB-0455. With an inclination of 99.1°, THOR BURNER 2A DEB passes over latitudes between 99.1°N and 99.1°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 12,262 active satellites in total, of which 148 share a similar altitude band with THOR BURNER 2A 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
THOR BURNER 2A DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 773 km altitude. Its 99.1° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 100 minutes, travelling at 26,892 km/h.
THOR BURNER 2A DEB (NORAD ID 29139) 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.
THOR BURNER 2A DEB was launched on 1974-03-16 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks THOR BURNER 2A DEB (NORAD ID 29139) 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.
THOR BURNER 2A DEB travels at approximately 26,892 km/h (16,710 mph) — roughly 7.47 km/s. It completes 14.36 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 7.47 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 THOR BURNER 2A DEB. Read more about debris statistics and the Kessler syndrome.