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OV1-9 R/B

NORAD 2622 Rocket Body MEO 1966-111D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
476 km
Apogee
4386 km
Inclination
99.1°
Period
137.1 min
Mean Motion
10.50063849 rev/day
TLE Epoch
2026-09-16 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,431 km
Orbital Velocity24,226 km/h
Velocity6.73 km/s
Orbital Period2 hours 17 minutes
Orbits / Day10.50
Eccentricity0.2221
Semi-Major Axis8,802 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-12-11
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-111D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
OV1-9 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 Medium Earth Orbit (MEO) at altitudes between 476 km and 4,386 km with an inclination of 99.1°. It travels at approximately 24,226 km/h (6.73 km/s), completing one full orbit every 2 hours 17 minutes — that’s roughly 10.50 orbits per day. Its orbital eccentricity of 0.2221 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like OV1-9 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
OV1-9 R/B orbits at an average altitude of 2,431 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 OV1-9 R/B’s average altitude, there are currently 0 active payloads and 9 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 99.1°, OV1-9 R/B passes over latitudes between 99.1°N and 99.1°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.
🔗 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
OV1-9 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 476 km (perigee) and 4,386 km (apogee), with an average altitude of approximately 2,431 km. It completes one orbit every 2 hours 17 minutes, travelling at approximately 24,226 km/h (15,053 mph).
OV1-9 R/B (NORAD ID 2622) 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.
OV1-9 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks OV1-9 R/B (NORAD ID 2622) 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.
OV1-9 R/B travels at approximately 24,226 km/h (15,053 mph) — roughly 6.73 km/s. It completes 10.50 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 21 sunrises and sunsets every 24 hours.