ATLAS CENTAUR DEB
NORAD 43342
Debris
GEO
2018-036D
CONNECTING…
GEO · NORAD 43342
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
35139 km
Apogee
35302 km
Inclination
7.1°
Period
1407.3 min
Mean Motion
1.02326582 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,221 km
Orbital Velocity11,145 km/h
Velocity3.10 km/s
Orbital Period23 hours 27 minutes
Orbits / Day1.02
Eccentricity0.0020
Semi-Major Axis41,592 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2018-04-14
Launch Site
Cape Canaveral, Florida
Int'l Designator
2018-036D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ATLAS CENTAUR DEB is a tracked piece of space debris attributed to United States, launched on 2018-04-14 from Cape Canaveral, Florida on the CBAS/EAGLE launch. It orbits in Geostationary Orbit (GEO) at altitudes between 35,139 km and 35,302 km with an inclination of 7.1°. It travels at approximately 11,145 km/h (3.10 km/s), completing one full orbit every 23 hours 27 minutes — that’s roughly 1.02 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. As orbital debris, ATLAS CENTAUR 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 CENTAUR DEB occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 7.1°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of ATLAS CENTAUR DEB’s average altitude, there are currently 2 active payloads and 8 tracked debris or rocket body fragments. United States operates approximately 12,358 active satellites in total.
🔗 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 CENTAUR DEB orbits at approximately 35,221 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,145 km/h — it just keeps pace with the ground below. With an inclination of 7.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ATLAS CENTAUR DEB (NORAD ID 43342) 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 CENTAUR DEB was launched on 2018-04-14 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. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS CENTAUR DEB (NORAD ID 43342) 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 CENTAUR DEB travels at approximately 11,145 km/h (6,925 mph) — roughly 3.10 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.
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 3.10 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 CENTAUR DEB. Read more about debris statistics and the Kessler syndrome.