ATLAS F DEB
NORAD 29197
Debris
LEO
1978-047C
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LEO · NORAD 29197
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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
501 km
Apogee
1950 km
Inclination
63.6°
Period
110.0 min
Mean Motion
13.09639370 rev/day
TLE Epoch
2026-08-05 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,226 km
Orbital Velocity26,077 km/h
Velocity7.24 km/s
Orbital Period110 minutes
Orbits / Day13.10
Eccentricity0.0954
Semi-Major Axis7,597 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1978-05-13
Launch Site
Vandenberg SFB, California
Int'l Designator
1978-047C
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ATLAS F DEB is a tracked piece of space debris attributed to United States, launched on 1978-05-13 from Vandenberg SFB, California on the Navstar GPS SVN 2 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 501 km and 1,950 km with an inclination of 63.6°. It travels at approximately 26,077 km/h (7.24 km/s), completing one full orbit every 110 minutes — that’s roughly 13.10 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, ATLAS F 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
ATLAS F DEB orbits at an average altitude of 1,226 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 ATLAS F DEB’s average altitude, there are currently 666 active payloads and 301 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. With an inclination of 63.6°, ATLAS F DEB passes over latitudes between 63.6°N and 63.6°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 12,672 active satellites in total, of which 2 share a similar altitude band with ATLAS F 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
ATLAS F DEB orbits in Low Earth Orbit (LEO) at altitudes between 501 km (perigee) and 1,950 km (apogee), with an average altitude of approximately 1,226 km. It completes one orbit every 110 minutes, travelling at approximately 26,077 km/h (16,204 mph).
ATLAS F DEB (NORAD ID 29197) 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.
ATLAS F DEB was launched on 1978-05-13 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 ATLAS F DEB (NORAD ID 29197) 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.
ATLAS F DEB travels at approximately 26,077 km/h (16,204 mph) — roughly 7.24 km/s. It completes 13.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.24 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 ATLAS F DEB. Read more about debris statistics and the Kessler syndrome.