SLS DEB
NORAD 55905
Debris
LEO
2022-156E
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LEO · NORAD 55905
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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
361 km
Apogee
1664 km
Inclination
30.5°
Period
105.4 min
Mean Motion
13.66276551 rev/day
TLE Epoch
2026-06-20 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,013 km
Orbital Velocity26,451 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.66
Eccentricity0.0882
Semi-Major Axis7,384 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2022-11-16
Launch Site
Cape Canaveral, Florida
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, Florida on the Artemis I launch. It orbits in Low Earth Orbit (LEO) at altitudes between 361 km and 1,664 km with an inclination of 30.5°. It travels at approximately 26,451 km/h (7.35 km/s), completing one full orbit every 105 minutes — that’s roughly 13.66 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 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 1,013 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 192 active payloads and 777 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 12,358 active satellites in total, of which 29 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 361 km (perigee) and 1,664 km (apogee), with an average altitude of approximately 1,013 km. It completes one orbit every 105 minutes, travelling at approximately 26,451 km/h (16,436 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, Florida, 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: ~500–1,000 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 26,451 km/h (16,436 mph) — roughly 7.35 km/s. It completes 13.66 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.35 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.