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OV1-5 DEB

NORAD 5599 Debris LEO 1966-025G
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
493 km
Apogee
511 km
Inclination
144.6°
Period
94.7 min
Mean Motion
15.21404247 rev/day
TLE Epoch
2026-09-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude502 km
Orbital Velocity27,416 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.21
Eccentricity0.0013
Semi-Major Axis6,873 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-03-30
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-025G
Object Type
Debris
RCS Size
Small (<0.1 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 493 km and 511 km with an inclination of 144.6°. It travels at approximately 27,416 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.21 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 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 502 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of OV1-5 DEB’s average altitude, there are currently 10,287 active payloads and 241 tracked debris or rocket body fragments — notable neighbours include STARLINK-1039, STARLINK-1184, STARLINK-1231. This makes it one of the more crowded altitude bands, containing roughly 55% of all active satellites. 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 9,645 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 493 km (perigee) and 511 km (apogee), with an average altitude of approximately 502 km. It completes one orbit every 95 minutes, travelling at approximately 27,416 km/h (17,035 mph).
OV1-5 DEB (NORAD ID 5599) 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks OV1-5 DEB (NORAD ID 5599) 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 27,416 km/h (17,035 mph) — roughly 7.62 km/s. It completes 15.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 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 7.62 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.