DELTA 1 DEB
NORAD 14528
Debris
LEO
1977-065FP
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LEO · NORAD 14528
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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
1233 km
Apogee
1725 km
Inclination
28.1°
Period
115.5 min
Mean Motion
12.46610104 rev/day
TLE Epoch
2026-06-19 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,479 km
Orbital Velocity25,653 km/h
Velocity7.13 km/s
Orbital Period116 minutes
Orbits / Day12.47
Eccentricity0.0313
Semi-Major Axis7,850 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1977-07-14
Launch Site
Cape Canaveral, Florida
Int'l Designator
1977-065FP
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 1977-07-14 from Cape Canaveral, Florida on the GMS launch. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 1,233 km and 1,725 km with an inclination of 28.1°. It travels at approximately 25,653 km/h (7.13 km/s), completing one full orbit every 116 minutes — that’s roughly 12.47 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 1,479 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 303 active payloads and 256 tracked debris or rocket body fragments. With an inclination of 28.1°, DELTA 1 DEB passes over latitudes between 28.1°N and 28.1°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. 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 Low Earth Orbit (LEO) at altitudes between 1,233 km (perigee) and 1,725 km (apogee), with an average altitude of approximately 1,479 km. It completes one orbit every 116 minutes, travelling at approximately 25,653 km/h (15,940 mph).
DELTA 1 DEB (NORAD ID 14528) 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 1977-07-14 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. 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 14528) 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 25,653 km/h (15,940 mph) — roughly 7.13 km/s. It completes 12.47 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 7.13 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.