OPS 4682 DEB
NORAD 14049
Debris
LEO
1965-027L
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LEO · NORAD 14049
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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
1252 km
Apogee
1314 km
Inclination
90.2°
Period
111.2 min
Mean Motion
12.94600982 rev/day
TLE Epoch
2026-06-20 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,283 km
Orbital Velocity25,979 km/h
Velocity7.22 km/s
Orbital Period111 minutes
Orbits / Day12.95
Eccentricity0.0041
Semi-Major Axis7,654 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
1965-027L
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 1,252 km and 1,314 km with an inclination of 90.2°. It travels at approximately 25,979 km/h (7.22 km/s), completing one full orbit every 111 minutes — that’s roughly 12.95 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 1,283 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 13 active payloads and 282 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 90.2°, OPS 4682 DEB passes over latitudes between 90.2°N and 90.2°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 12,358 active satellites in total, of which 4 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 1,252 km (perigee) and 1,314 km (apogee), with an average altitude of approximately 1,283 km. It completes one orbit every 111 minutes, travelling at approximately 25,979 km/h (16,143 mph).
OPS 4682 DEB (NORAD ID 14049) 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 14049) 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 25,979 km/h (16,143 mph) — roughly 7.22 km/s. It completes 12.95 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 7.22 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.