OV1-5 DEB
NORAD 5361
Debris
LEO
1966-025F
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LEO · NORAD 5361
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
687 km
Apogee
715 km
Inclination
144.6°
Period
98.8 min
Mean Motion
14.57493524 rev/day
TLE Epoch
2026-09-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude701 km
Orbital Velocity27,027 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.57
Eccentricity0.0020
Semi-Major Axis7,072 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-03-30
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-025F
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OV1-5 DEB is a tracked piece of space debris attributed to United States, launched on 1966-03-30 from Vandenberg Space Force Base, United States on the OV1-4S 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 687 km and 715 km with an inclination of 144.6°. It travels at approximately 27,027 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.57 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, OV1-5 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
OV1-5 DEB orbits at an average altitude of 701 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 OV1-5 DEB’s average altitude, there are currently 293 active payloads and 1,585 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 144.6°, OV1-5 DEB passes over latitudes between 144.6°N and 144.6°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 13,196 active satellites in total, of which 81 share a similar altitude band with OV1-5 DEB.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
OV1-5 DEB orbits in Low Earth Orbit (LEO) at altitudes between 687 km (perigee) and 715 km (apogee), with an average altitude of approximately 701 km. It completes one orbit every 99 minutes, travelling at approximately 27,027 km/h (16,794 mph).
OV1-5 DEB (NORAD ID 5361) is a piece of tracked orbital debris attributed to United States. It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
OV1-5 DEB was launched on 1966-03-30 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks OV1-5 DEB (NORAD ID 5361) 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.
OV1-5 DEB travels at approximately 27,027 km/h (16,794 mph) — roughly 7.51 km/s. It completes 14.57 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.51 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like OV1-5 DEB. Read more about debris statistics and the Kessler syndrome.