USA 40 R/B
NORAD 20344
Rocket Body
MEO
1989-061D
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MEO · NORAD 20344
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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
486 km
Apogee
8075 km
Inclination
57.0°
Period
182.5 min
Mean Motion
7.88975196 rev/day
TLE Epoch
2026-06-25 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude4,281 km
Orbital Velocity22,022 km/h
Velocity6.12 km/s
Orbital Period3 hours 3 minutes
Orbits / Day7.89
Eccentricity0.3562
Semi-Major Axis10,652 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
1989-061D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
USA 40 R/B is a spent rocket body associated with 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 486 km and 8,075 km with an inclination of 57.0°. It travels at approximately 22,022 km/h (6.12 km/s), completing one full orbit every 3 hours 3 minutes — that’s roughly 7.89 orbits per day. Its orbital eccentricity of 0.3562 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like USA 40 R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
USA 40 R/B orbits at an average altitude of 4,281 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’s average altitude, there are currently 0 active payloads and 2 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 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.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
USA 40 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 486 km (perigee) and 8,075 km (apogee), with an average altitude of approximately 4,281 km. It completes one orbit every 3 hours 3 minutes, travelling at approximately 22,022 km/h (13,684 mph).
USA 40 R/B (NORAD ID 20344) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
USA 40 R/B 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 (NORAD ID 20344) 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 travels at approximately 22,022 km/h (13,684 mph) — roughly 6.12 km/s. It completes 7.89 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 16 sunrises and sunsets every 24 hours.