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OV1-19 R/B

NORAD 3827 Rocket Body MEO 1969-025E
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
485 km
Apogee
5333 km
Inclination
104.7°
Period
148.4 min
Mean Motion
9.70043430 rev/day
TLE Epoch
2026-09-16 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,909 km
Orbital Velocity23,594 km/h
Velocity6.55 km/s
Orbital Period2 hours 28 minutes
Orbits / Day9.70
Eccentricity0.2612
Semi-Major Axis9,280 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1969-03-18
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1969-025E
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
OV1-19 R/B is a spent rocket body associated with United States, launched on 1969-03-18 from Vandenberg Space Force Base, United States on the OV1-17S launch. After more than 57 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 485 km and 5,333 km with an inclination of 104.7°. It travels at approximately 23,594 km/h (6.55 km/s), completing one full orbit every 2 hours 28 minutes — that’s roughly 9.70 orbits per day. Its orbital eccentricity of 0.2612 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like OV1-19 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
OV1-19 R/B orbits at an average altitude of 2,909 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 OV1-19 R/B’s average altitude, there are currently 0 active payloads and 3 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 104.7°, OV1-19 R/B passes over latitudes between 104.7°N and 104.7°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
OV1-19 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 485 km (perigee) and 5,333 km (apogee), with an average altitude of approximately 2,909 km. It completes one orbit every 2 hours 28 minutes, travelling at approximately 23,594 km/h (14,660 mph).
OV1-19 R/B (NORAD ID 3827) 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.
OV1-19 R/B was launched on 1969-03-18 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 OV1-19 R/B (NORAD ID 3827) 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.
OV1-19 R/B travels at approximately 23,594 km/h (14,660 mph) — roughly 6.55 km/s. It completes 9.70 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 19 sunrises and sunsets every 24 hours.