OV1-20/OV1-21 AKM
NORAD 5395
Rocket Body
LEO
1971-067K
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LEO · NORAD 5395
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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
710 km
Apogee
791 km
Inclination
87.6°
Period
99.8 min
Mean Motion
14.42512365 rev/day
TLE Epoch
2026-09-16 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude751 km
Orbital Velocity26,933 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.43
Eccentricity0.0057
Semi-Major Axis7,122 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1971-08-07
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1971-067K
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
OV1-20/OV1-21 AKM is a spent rocket body associated with United States, launched on 1971-08-07 from Vandenberg Space Force Base, United States on the OAR-901 launch. After more than 55 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 710 km and 791 km with an inclination of 87.6°. It travels at approximately 26,933 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.43 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Spent rocket bodies like OV1-20/OV1-21 AKM 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
OV1-20/OV1-21 AKM orbits at an average altitude of 751 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of OV1-20/OV1-21 AKM’s average altitude, there are currently 412 active payloads and 2,112 tracked debris or rocket body fragments — notable neighbours include LANDSAT 9. With an inclination of 87.6°, OV1-20/OV1-21 AKM passes over latitudes between 87.6°N and 87.6°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,206 active satellites in total, of which 183 share a similar altitude band with OV1-20/OV1-21 AKM.
🔗 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
OV1-20/OV1-21 AKM orbits in Low Earth Orbit (LEO) at altitudes between 710 km (perigee) and 791 km (apogee), with an average altitude of approximately 751 km. It completes one orbit every 100 minutes, travelling at approximately 26,933 km/h (16,735 mph).
OV1-20/OV1-21 AKM (NORAD ID 5395) 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.
OV1-20/OV1-21 AKM was launched on 1971-08-07 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks OV1-20/OV1-21 AKM (NORAD ID 5395) 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.
OV1-20/OV1-21 AKM travels at approximately 26,933 km/h (16,735 mph) — roughly 7.48 km/s. It completes 14.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.