DELTA 1 DEB
NORAD 14620
Debris
MEO
1981-070J
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MEO · NORAD 14620
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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
502 km
Apogee
21058 km
Inclination
90.7°
Period
372.8 min
Mean Motion
3.86273430 rev/day
TLE Epoch
2026-06-15 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude10,780 km
Orbital Velocity17,355 km/h
Velocity4.82 km/s
Orbital Period6 hours 13 minutes
Orbits / Day3.86
Eccentricity0.5993
Semi-Major Axis17,151 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1981-08-03
Launch Site
Vandenberg SFB, California
Int'l Designator
1981-070J
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DELTA 1 DEB is a tracked piece of space debris attributed to United States, launched on 1981-08-03 from Vandenberg SFB, California on the DE A launch. With over 45 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 502 km and 21,058 km with an inclination of 90.7°. It travels at approximately 17,355 km/h (4.82 km/s), completing one full orbit every 6 hours 13 minutes — that’s roughly 3.86 orbits per day. Its orbital eccentricity of 0.5993 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, 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
DELTA 1 DEB orbits at an average altitude of 10,780 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 DELTA 1 DEB’s average altitude, there are currently 1 active payload and 7 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 90.7°, DELTA 1 DEB passes over latitudes between 90.7°N and 90.7°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 12,358 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
DELTA 1 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 502 km (perigee) and 21,058 km (apogee), with an average altitude of approximately 10,780 km. It completes one orbit every 6 hours 13 minutes, travelling at approximately 17,355 km/h (10,784 mph).
DELTA 1 DEB (NORAD ID 14620) 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.
DELTA 1 DEB was launched on 1981-08-03 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB (NORAD ID 14620) 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.
DELTA 1 DEB travels at approximately 17,355 km/h (10,784 mph) — roughly 4.82 km/s. It completes 3.86 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 8 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 4.82 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 DELTA 1 DEB. Read more about debris statistics and the Kessler syndrome.