OV1-13 R/B
NORAD 3212
Rocket Body
MEO
1968-026D
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
602 km
Apogee
9120 km
Inclination
100.0°
Period
197.6 min
Mean Motion
7.28625425 rev/day
TLE Epoch
2026-09-15 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude4,861 km
Orbital Velocity21,446 km/h
Velocity5.96 km/s
Orbital Period3 hours 18 minutes
Orbits / Day7.29
Eccentricity0.3792
Semi-Major Axis11,232 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1968-04-06
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1968-026D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
OV1-13 R/B is a spent rocket body associated with United States, launched on 1968-04-06 from Vandenberg Space Force Base, United States on the OV1-13 launch. After more than 58 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 602 km and 9,120 km with an inclination of 100.0°. It travels at approximately 21,446 km/h (5.96 km/s), completing one full orbit every 3 hours 18 minutes — that’s roughly 7.29 orbits per day. Its orbital eccentricity of 0.3792 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like OV1-13 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
OV1-13 R/B orbits at an average altitude of 4,861 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 OV1-13 R/B’s average altitude, there are currently 1 active payload and 5 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 100.0°, OV1-13 R/B passes over latitudes between 100.0°N and 100.0°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
OV1-13 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 602 km (perigee) and 9,120 km (apogee), with an average altitude of approximately 4,861 km. It completes one orbit every 3 hours 18 minutes, travelling at approximately 21,446 km/h (13,326 mph).
OV1-13 R/B (NORAD ID 3212) 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.
OV1-13 R/B was launched on 1968-04-06 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 OV1-13 R/B (NORAD ID 3212) 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.
OV1-13 R/B travels at approximately 21,446 km/h (13,326 mph) — roughly 5.96 km/s. It completes 7.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 15 sunrises and sunsets every 24 hours.