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THOR BURNER 2 R/B

NORAD 4332 Rocket Body LEO 1970-012B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
743 km
Apogee
827 km
Inclination
98.8°
Period
100.5 min
Mean Motion
14.32054656 rev/day
TLE Epoch
2026-09-16 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude785 km
Orbital Velocity26,868 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.32
Eccentricity0.0059
Semi-Major Axis7,156 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1970-02-11
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1970-012B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
THOR BURNER 2 R/B is a spent rocket body associated with United States, launched on 1970-02-11 from Vandenberg Space Force Base, United States on the DAPP Block 5A F-1 launch. After more than 56 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 743 km and 827 km with an inclination of 98.8°. It travels at approximately 26,868 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.32 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. Spent rocket bodies like THOR BURNER 2 R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
THOR BURNER 2 R/B orbits at an average altitude of 785 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 2 R/B’s average altitude, there are currently 449 active payloads and 2,420 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 98.8°, THOR BURNER 2 R/B passes over latitudes between 98.8°N and 98.8°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 13,206 active satellites in total, of which 187 share a similar altitude band with THOR BURNER 2 R/B.
🔗 Spent Rocket Body

This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.

❓ Frequently Asked Questions
THOR BURNER 2 R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 785 km altitude. Its 98.8° 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 101 minutes, travelling at 26,868 km/h.
THOR BURNER 2 R/B (NORAD ID 4332) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
THOR BURNER 2 R/B was launched on 1970-02-11 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks THOR BURNER 2 R/B (NORAD ID 4332) 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 2 R/B travels at approximately 26,868 km/h (16,695 mph) — roughly 7.46 km/s. It completes 14.32 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.