DELTA 1 DEB
NORAD 8544
Debris
MEO
1972-058GT
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MEO · NORAD 8544
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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
715 km
Apogee
2014 km
Inclination
97.4°
Period
113.0 min
Mean Motion
12.74270702 rev/day
TLE Epoch
2026-09-18 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,365 km
Orbital Velocity25,842 km/h
Velocity7.18 km/s
Orbital Period113 minutes
Orbits / Day12.74
Eccentricity0.0840
Semi-Major Axis7,736 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1972-07-23
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1972-058GT
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 1972-07-23 from Vandenberg Space Force Base, United States on the ERTS A launch. After more than 54 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 715 km and 2,014 km with an inclination of 97.4°. It travels at approximately 25,842 km/h (7.18 km/s), completing one full orbit every 113 minutes — that’s roughly 12.74 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. 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 1,365 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 184 active payloads and 250 tracked debris or rocket body fragments. With an inclination of 97.4°, DELTA 1 DEB passes over latitudes between 97.4°N and 97.4°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, of which 12 share a similar altitude band with DELTA 1 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
DELTA 1 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 715 km (perigee) and 2,014 km (apogee), with an average altitude of approximately 1,365 km. It completes one orbit every 113 minutes, travelling at approximately 25,842 km/h (16,058 mph).
DELTA 1 DEB (NORAD ID 8544) 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 1972-07-23 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB (NORAD ID 8544) 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 25,842 km/h (16,058 mph) — roughly 7.18 km/s. It completes 12.74 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.18 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.