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THORAD DELTA 1 DEB

NORAD 8405 Debris MEO 1974-089CH
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1417 km
Apogee
2596 km
Inclination
102.7°
Period
127.3 min
Mean Motion
11.30719119 rev/day
TLE Epoch
2026-09-16 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,007 km
Orbital Velocity24,832 km/h
Velocity6.90 km/s
Orbital Period2 hours 7 minutes
Orbits / Day11.31
Eccentricity0.0704
Semi-Major Axis8,378 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1974-11-15
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1974-089CH
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
THORAD DELTA 1 DEB is a tracked piece of space debris attributed to United States, launched on 1974-11-15 from Vandenberg Space Force Base, United States on the ITOS G launch. After more than 52 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,417 km and 2,596 km with an inclination of 102.7°. It travels at approximately 24,832 km/h (6.90 km/s), completing one full orbit every 2 hours 7 minutes — that’s roughly 11.31 orbits per day. As orbital debris, THORAD DELTA 1 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
THORAD DELTA 1 DEB orbits at an average altitude of 2,007 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of THORAD DELTA 1 DEB’s average altitude, there are currently 9 active payloads and 33 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 102.7°, THORAD DELTA 1 DEB passes over latitudes between 102.7°N and 102.7°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 13,196 active satellites in total.
🔗 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
THORAD DELTA 1 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 1,417 km (perigee) and 2,596 km (apogee), with an average altitude of approximately 2,007 km. It completes one orbit every 2 hours 7 minutes, travelling at approximately 24,832 km/h (15,430 mph).
THORAD DELTA 1 DEB (NORAD ID 8405) 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.
THORAD DELTA 1 DEB was launched on 1974-11-15 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks THORAD DELTA 1 DEB (NORAD ID 8405) 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.
THORAD DELTA 1 DEB travels at approximately 24,832 km/h (15,430 mph) — roughly 6.90 km/s. It completes 11.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 23 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 6.90 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 THORAD DELTA 1 DEB. Read more about debris statistics and the Kessler syndrome.