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OV1-10 R/B

NORAD 2621 Rocket Body LEO 1966-111C
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Altitude (km)
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
571 km
Apogee
652 km
Inclination
93.4°
Period
96.9 min
Mean Motion
14.85696062 rev/day
TLE Epoch
2026-09-16 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude612 km
Orbital Velocity27,200 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.86
Eccentricity0.0058
Semi-Major Axis6,983 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-12-11
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-111C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
OV1-10 R/B is a spent rocket body associated with United States, launched on 1966-12-11 from Vandenberg Space Force Base, United States on the OV1-9 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 571 km and 652 km with an inclination of 93.4°. It travels at approximately 27,200 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.86 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Spent rocket bodies like OV1-10 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
OV1-10 R/B orbits at an average altitude of 612 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 OV1-10 R/B’s average altitude, there are currently 1,594 active payloads and 772 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 8.5% of all active satellites. With an inclination of 93.4°, OV1-10 R/B passes over latitudes between 93.4°N and 93.4°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 1,042 share a similar altitude band with OV1-10 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
OV1-10 R/B orbits in Low Earth Orbit (LEO) at altitudes between 571 km (perigee) and 652 km (apogee), with an average altitude of approximately 612 km. It completes one orbit every 97 minutes, travelling at approximately 27,200 km/h (16,901 mph).
OV1-10 R/B (NORAD ID 2621) 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.
OV1-10 R/B was launched on 1966-12-11 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks OV1-10 R/B (NORAD ID 2621) 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.
OV1-10 R/B travels at approximately 27,200 km/h (16,901 mph) — roughly 7.56 km/s. It completes 14.86 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.