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USA 40 R/B DEB

NORAD 23159 Debris MEO 1989-061N
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
441 km
Apogee
2961 km
Inclination
57.0°
Period
120.5 min
Mean Motion
11.95452141 rev/day
TLE Epoch
2026-06-25 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,701 km
Orbital Velocity25,298 km/h
Velocity7.03 km/s
Orbital Period2 hours
Orbits / Day11.95
Eccentricity0.1561
Semi-Major Axis8,072 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1989-08-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
1989-061N
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 on the OV-102 Medium deploy launch. With over 37 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 441 km and 2,961 km with an inclination of 57.0°. It travels at approximately 25,298 km/h (7.03 km/s), completing one full orbit every 2 hours — that’s roughly 11.95 orbits per day. Its orbital eccentricity of 0.1561 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, 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 1,701 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 16 active payloads and 58 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 12,413 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 441 km (perigee) and 2,961 km (apogee), with an average altitude of approximately 1,701 km. It completes one orbit every 2 hours, travelling at approximately 25,298 km/h (15,719 mph).
USA 40 R/B DEB (NORAD ID 23159) 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks USA 40 R/B DEB (NORAD ID 23159) 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 25,298 km/h (15,719 mph) — roughly 7.03 km/s. It completes 11.95 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 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 7.03 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.