OV1-5 R/B
NORAD 2123
Rocket Body
LEO
1966-025C
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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
980 km
Apogee
1049 km
Inclination
144.6°
Period
105.4 min
Mean Motion
13.65907859 rev/day
TLE Epoch
2026-09-16 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,015 km
Orbital Velocity26,447 km/h
Velocity7.35 km/s
Orbital Period105 minutes
Orbits / Day13.66
Eccentricity0.0047
Semi-Major Axis7,386 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-03-30
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-025C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
OV1-5 R/B is a spent rocket body associated with United States, launched on 1966-03-30 from Vandenberg Space Force Base, United States on the OV1-4S launch. After more than 60 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 980 km and 1,049 km with an inclination of 144.6°. It travels at approximately 26,447 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. Spent rocket bodies like OV1-5 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
OV1-5 R/B orbits at an average altitude of 1,015 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 OV1-5 R/B’s average altitude, there are currently 263 active payloads and 984 tracked debris or rocket body fragments. With an inclination of 144.6°, OV1-5 R/B passes over latitudes between 144.6°N and 144.6°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 51 share a similar altitude band with OV1-5 R/B.
🔗 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
OV1-5 R/B orbits in Low Earth Orbit (LEO) at altitudes between 980 km (perigee) and 1,049 km (apogee), with an average altitude of approximately 1,015 km. It completes one orbit every 105 minutes, travelling at approximately 26,447 km/h (16,434 mph).
OV1-5 R/B (NORAD ID 2123) 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.
OV1-5 R/B was launched on 1966-03-30 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks OV1-5 R/B (NORAD ID 2123) 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.
OV1-5 R/B travels at approximately 26,447 km/h (16,434 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.