DELTA 1 DEB
NORAD 10306
Debris
LEO
1977-065DC
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LEO · NORAD 10306
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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
524 km
Apogee
1488 km
Inclination
29.1°
Period
105.3 min
Mean Motion
13.68165123 rev/day
TLE Epoch
2026-06-19 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,006 km
Orbital Velocity26,463 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.68
Eccentricity0.0653
Semi-Major Axis7,377 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1977-07-14
Launch Site
Cape Canaveral, Florida
Int'l Designator
1977-065DC
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 524 km and 1,488 km with an inclination of 29.1°. It travels at approximately 26,463 km/h (7.35 km/s), completing one full orbit every 105 minutes — that’s roughly 13.68 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 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 1,006 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of DELTA 1 DEB’s average altitude, there are currently 207 active payloads and 839 tracked debris or rocket body fragments. With an inclination of 29.1°, DELTA 1 DEB passes over latitudes between 29.1°N and 29.1°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, of which 37 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 Low Earth Orbit (LEO) at altitudes between 524 km (perigee) and 1,488 km (apogee), with an average altitude of approximately 1,006 km. It completes one orbit every 105 minutes, travelling at approximately 26,463 km/h (16,443 mph).
DELTA 1 DEB (NORAD ID 10306) 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB (NORAD ID 10306) 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 26,463 km/h (16,443 mph) — roughly 7.35 km/s. It completes 13.68 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.35 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.