OPS 4682 DEB
NORAD 38433
Debris
LEO
1965-027EN
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LEO · NORAD 38433
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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
1190 km
Apogee
1238 km
Inclination
90.3°
Period
109.7 min
Mean Motion
13.12280088 rev/day
TLE Epoch
2026-07-18 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,214 km
Orbital Velocity26,097 km/h
Velocity7.25 km/s
Orbital Period110 minutes
Orbits / Day13.12
Eccentricity0.0032
Semi-Major Axis7,585 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-04-03
Launch Site
Vandenberg SFB, California
Int'l Designator
1965-027EN
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 4682 DEB is a tracked piece of space debris attributed to United States, launched on 1965-04-03 from Vandenberg SFB, California on the SNAP-10A FS-4 launch. After more than 61 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 1,190 km and 1,238 km with an inclination of 90.3°. It travels at approximately 26,097 km/h (7.25 km/s), completing one full orbit every 110 minutes — that’s roughly 13.12 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, OPS 4682 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
OPS 4682 DEB orbits at an average altitude of 1,214 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of OPS 4682 DEB’s average altitude, there are currently 732 active payloads and 236 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. With an inclination of 90.3°, OPS 4682 DEB passes over latitudes between 90.3°N and 90.3°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 12,554 active satellites in total, of which 5 share a similar altitude band with OPS 4682 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
OPS 4682 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,190 km (perigee) and 1,238 km (apogee), with an average altitude of approximately 1,214 km. It completes one orbit every 110 minutes, travelling at approximately 26,097 km/h (16,216 mph).
OPS 4682 DEB (NORAD ID 38433) 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.
OPS 4682 DEB was launched on 1965-04-03 from Vandenberg SFB, California, 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 4682 DEB (NORAD ID 38433) 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.
OPS 4682 DEB travels at approximately 26,097 km/h (16,216 mph) — roughly 7.25 km/s. It completes 13.12 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 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 7.25 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 OPS 4682 DEB. Read more about debris statistics and the Kessler syndrome.