ATLAS F DEB
NORAD 29197
Debris
MEO
1978-047C
CONNECTING…
MEO · NORAD 29197
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
478 km
Apogee
2068 km
Inclination
63.6°
Period
111.0 min
Mean Motion
12.97225138 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,273 km
Orbital Velocity25,996 km/h
Velocity7.22 km/s
Orbital Period111 minutes
Orbits / Day12.97
Eccentricity0.1040
Semi-Major Axis7,644 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 Medium Earth Orbit (MEO) at altitudes between 478 km and 2,068 km with an inclination of 63.6°. It travels at approximately 25,996 km/h (7.22 km/s), completing one full orbit every 111 minutes — that’s roughly 12.97 orbits per day. Its orbital eccentricity of 0.1040 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 1,273 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of ATLAS F DEB’s average altitude, there are currently 10 active payloads and 276 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0013, ONEWEB-0036. This is a relatively sparse altitude band, containing less than 1% of all active satellites. 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 12,358 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 Medium Earth Orbit (MEO) at altitudes between 478 km (perigee) and 2,068 km (apogee), with an average altitude of approximately 1,273 km. It completes one orbit every 111 minutes, travelling at approximately 25,996 km/h (16,153 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 25,996 km/h (16,153 mph) — roughly 7.22 km/s. It completes 12.97 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 7.22 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.