DELTA 1 DEB
NORAD 19512
Debris
LEO
1973-086HF
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LEO · NORAD 19512
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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
1503 km
Apogee
1551 km
Inclination
102.4°
Period
116.6 min
Mean Motion
12.35224487 rev/day
TLE Epoch
2026-06-15 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,527 km
Orbital Velocity25,575 km/h
Velocity7.10 km/s
Orbital Period117 minutes
Orbits / Day12.35
Eccentricity0.0030
Semi-Major Axis7,898 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1973-11-06
Launch Site
Vandenberg SFB, California
Int'l Designator
1973-086HF
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
DELTA 1 DEB is a tracked piece of space debris attributed to United States, launched on 1973-11-06 from Vandenberg SFB, California. After more than 53 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 1,503 km and 1,551 km with an inclination of 102.4°. It travels at approximately 25,575 km/h (7.10 km/s), completing one full orbit every 117 minutes — that’s roughly 12.35 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 1,527 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of DELTA 1 DEB’s average altitude, there are currently 159 active payloads and 255 tracked debris or rocket body fragments. With an inclination of 102.4°, DELTA 1 DEB passes over latitudes between 102.4°N and 102.4°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 12,261 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 Low Earth Orbit (LEO) at altitudes between 1,503 km (perigee) and 1,551 km (apogee), with an average altitude of approximately 1,527 km. It completes one orbit every 117 minutes, travelling at approximately 25,575 km/h (15,891 mph).
DELTA 1 DEB (NORAD ID 19512) 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 1973-11-06 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB (NORAD ID 19512) 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 25,575 km/h (15,891 mph) — roughly 7.10 km/s. It completes 12.35 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 7.10 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.