DELTA 1 DEB
NORAD 37643
Debris
LEO
1978-026JE
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LEO · NORAD 37643
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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
760 km
Apogee
821 km
Inclination
98.7°
Period
100.7 min
Mean Motion
14.30361001 rev/day
TLE Epoch
2026-10-21 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude791 km
Orbital Velocity26,858 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.30
Eccentricity0.0043
Semi-Major Axis7,162 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1978-03-05
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1978-026JE
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 1978-03-05 from Vandenberg Space Force Base, United States on the Landsat C launch. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 760 km and 821 km with an inclination of 98.7°. It travels at approximately 26,858 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.30 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. 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 791 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of DELTA 1 DEB’s average altitude, there are currently 437 active payloads and 2,459 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 98.7°, DELTA 1 DEB passes over latitudes between 98.7°N and 98.7°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 13,281 active satellites in total, of which 190 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 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 791 km altitude. Its 98.7° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 101 minutes, travelling at 26,858 km/h.
DELTA 1 DEB (NORAD ID 37643) 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 1978-03-05 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 37643) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 26,858 km/h (16,689 mph) — roughly 7.46 km/s. It completes 14.30 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 7.46 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.