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OV1-14 R/B

NORAD 3177 Rocket Body MEO 1968-026C
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Longitude
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🛰️ Orbital Parameters
Perigee
539 km
Apogee
9832 km
Inclination
100.0°
Period
206.3 min
Mean Motion
6.98189118 rev/day
TLE Epoch
2026-09-15 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude5,186 km
Orbital Velocity21,143 km/h
Velocity5.87 km/s
Orbital Period3 hours 26 minutes
Orbits / Day6.98
Eccentricity0.4021
Semi-Major Axis11,557 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
1968-026C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
OV1-14 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 539 km and 9,832 km with an inclination of 100.0°. It travels at approximately 21,143 km/h (5.87 km/s), completing one full orbit every 3 hours 26 minutes — that’s roughly 6.98 orbits per day. Its orbital eccentricity of 0.4021 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like OV1-14 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
OV1-14 R/B orbits at an average altitude of 5,186 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 OV1-14 R/B’s average altitude, there are currently 1 active payload and 4 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°, OV1-14 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
OV1-14 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 539 km (perigee) and 9,832 km (apogee), with an average altitude of approximately 5,186 km. It completes one orbit every 3 hours 26 minutes, travelling at approximately 21,143 km/h (13,137 mph).
OV1-14 R/B (NORAD ID 3177) 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.
OV1-14 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 OV1-14 R/B (NORAD ID 3177) 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.
OV1-14 R/B travels at approximately 21,143 km/h (13,137 mph) — roughly 5.87 km/s. It completes 6.98 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 14 sunrises and sunsets every 24 hours.