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SLS DEB

NORAD 55905 Debris LEO 2022-156E
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
360 km
Apogee
1564 km
Inclination
30.5°
Period
104.3 min
Mean Motion
13.80727546 rev/day
TLE Epoch
2026-09-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude962 km
Orbital Velocity26,542 km/h
Velocity7.37 km/s
Orbital Period104 minutes
Orbits / Day13.81
Eccentricity0.0821
Semi-Major Axis7,333 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2022-11-16
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
2022-156E
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SLS DEB is a tracked piece of space debris attributed to United States, launched on 2022-11-16 from Cape Canaveral Space Force Station, United States on the Artemis I launch. It orbits in Low Earth Orbit (LEO) at altitudes between 360 km and 1,564 km with an inclination of 30.5°. It travels at approximately 26,542 km/h (7.37 km/s), completing one full orbit every 104 minutes — that’s roughly 13.81 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, SLS 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
SLS DEB orbits at an average altitude of 962 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of SLS DEB’s average altitude, there are currently 378 active payloads and 1,237 tracked debris or rocket body fragments. With an inclination of 30.5°, SLS DEB passes over latitudes between 30.5°N and 30.5°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 13,196 active satellites in total, of which 132 share a similar altitude band with SLS 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
SLS DEB orbits in Low Earth Orbit (LEO) at altitudes between 360 km (perigee) and 1,564 km (apogee), with an average altitude of approximately 962 km. It completes one orbit every 104 minutes, travelling at approximately 26,542 km/h (16,492 mph).
SLS DEB (NORAD ID 55905) 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.
SLS DEB was launched on 2022-11-16 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks SLS DEB (NORAD ID 55905) 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.
SLS DEB travels at approximately 26,542 km/h (16,492 mph) — roughly 7.37 km/s. It completes 13.81 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.37 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 SLS DEB. Read more about debris statistics and the Kessler syndrome.