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OPS 7684 DEB

NORAD 3618 Debris LEO 1968-112D
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1373 km
Apogee
1507 km
Inclination
80.5°
Period
114.7 min
Mean Motion
12.55911492 rev/day
TLE Epoch
2026-09-17 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,440 km
Orbital Velocity25,717 km/h
Velocity7.14 km/s
Orbital Period115 minutes
Orbits / Day12.56
Eccentricity0.0086
Semi-Major Axis7,811 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1968-12-12
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1968-112D
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 7684 DEB is a tracked piece of space debris attributed to United States, launched on 1968-12-12 from Vandenberg Space Force Base, United States on the CORONA J-50 launch. After more than 58 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 1,373 km and 1,507 km with an inclination of 80.5°. It travels at approximately 25,717 km/h (7.14 km/s), completing one full orbit every 115 minutes — that’s roughly 12.56 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. As orbital debris, OPS 7684 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 7684 DEB orbits at an average altitude of 1,440 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 7684 DEB’s average altitude, there are currently 507 active payloads and 312 tracked debris or rocket body fragments. With an inclination of 80.5°, OPS 7684 DEB passes over latitudes between 80.5°N and 80.5°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 13,198 active satellites in total, of which 18 share a similar altitude band with OPS 7684 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 7684 DEB orbits in Low Earth Orbit (LEO) at altitudes between 1,373 km (perigee) and 1,507 km (apogee), with an average altitude of approximately 1,440 km. It completes one orbit every 115 minutes, travelling at approximately 25,717 km/h (15,980 mph).
OPS 7684 DEB (NORAD ID 3618) 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 7684 DEB was launched on 1968-12-12 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 7684 DEB (NORAD ID 3618) 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 7684 DEB travels at approximately 25,717 km/h (15,980 mph) — roughly 7.14 km/s. It completes 12.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 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 7.14 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 7684 DEB. Read more about debris statistics and the Kessler syndrome.