DELTA 1 DEB
NORAD 720
Debris
LEO
1963-054C
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LEO · NORAD 720
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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
647 km
Apogee
799 km
Inclination
58.5°
Period
99.3 min
Mean Motion
14.50767557 rev/day
TLE Epoch
2026-09-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude723 km
Orbital Velocity26,985 km/h
Velocity7.50 km/s
Orbital Period99 minutes
Orbits / Day14.51
Eccentricity0.0107
Semi-Major Axis7,094 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1963-12-21
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1963-054C
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 1963-12-21 from Vandenberg Space Force Base, United States on the Tiros H launch. After more than 63 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 647 km and 799 km with an inclination of 58.5°. It travels at approximately 26,985 km/h (7.50 km/s), completing one full orbit every 99 minutes — that’s roughly 14.51 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 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 723 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of DELTA 1 DEB’s average altitude, there are currently 325 active payloads and 1,858 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 58.5°, DELTA 1 DEB passes over latitudes between 58.5°N and 58.5°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 13,196 active satellites in total, of which 105 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 647 km (perigee) and 799 km (apogee), with an average altitude of approximately 723 km. It completes one orbit every 99 minutes, travelling at approximately 26,985 km/h (16,768 mph).
DELTA 1 DEB (NORAD ID 720) 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 1963-12-21 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 DEB (NORAD ID 720) 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 26,985 km/h (16,768 mph) — roughly 7.50 km/s. It completes 14.51 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.50 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.