USA 40 R/B DEB
NORAD 23351
Debris
MEO
1989-061X
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MEO · NORAD 23351
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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
513 km
Apogee
4340 km
Inclination
57.0°
Period
137.0 min
Mean Motion
10.50897178 rev/day
TLE Epoch
2026-06-12 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,427 km
Orbital Velocity24,232 km/h
Velocity6.73 km/s
Orbital Period2 hours 17 minutes
Orbits / Day10.51
Eccentricity0.2175
Semi-Major Axis8,798 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1989-08-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
1989-061X
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
USA 40 R/B DEB is a tracked piece of space debris attributed to United States, launched on 1989-08-08 from Cape Canaveral, Florida. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 513 km and 4,340 km with an inclination of 57.0°. It travels at approximately 24,232 km/h (6.73 km/s), completing one full orbit every 2 hours 17 minutes — that’s roughly 10.51 orbits per day. Its orbital eccentricity of 0.2175 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, USA 40 R/B 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
USA 40 R/B DEB orbits at an average altitude of 2,427 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 USA 40 R/B DEB’s average altitude, there are currently 0 active payloads and 6 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 57.0°, USA 40 R/B DEB passes over latitudes between 57.0°N and 57.0°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 12,262 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
USA 40 R/B DEB orbits in Medium Earth Orbit (MEO) at altitudes between 513 km (perigee) and 4,340 km (apogee), with an average altitude of approximately 2,427 km. It completes one orbit every 2 hours 17 minutes, travelling at approximately 24,232 km/h (15,057 mph).
USA 40 R/B DEB (NORAD ID 23351) 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.
USA 40 R/B DEB was launched on 1989-08-08 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks USA 40 R/B DEB (NORAD ID 23351) 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.
USA 40 R/B DEB travels at approximately 24,232 km/h (15,057 mph) — roughly 6.73 km/s. It completes 10.51 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 21 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 6.73 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 USA 40 R/B DEB. Read more about debris statistics and the Kessler syndrome.