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OPS 0856 DEB

NORAD 24676 Debris MEO 1966-077Q
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1345 km
Apogee
5376 km
Inclination
88.4°
Period
159.4 min
Mean Motion
9.03304033 rev/day
TLE Epoch
2026-09-17 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,361 km
Orbital Velocity23,040 km/h
Velocity6.40 km/s
Orbital Period2 hours 39 minutes
Orbits / Day9.03
Eccentricity0.2071
Semi-Major Axis9,732 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1966-08-19
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-077Q
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 0856 DEB is a tracked piece of space debris attributed to United States, launched on 1966-08-19 from Vandenberg Space Force Base, United States on the Midas RTS-I F2 launch. After more than 60 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,345 km and 5,376 km with an inclination of 88.4°. It travels at approximately 23,040 km/h (6.40 km/s), completing one full orbit every 2 hours 39 minutes — that’s roughly 9.03 orbits per day. Its orbital eccentricity of 0.2071 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, OPS 0856 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 0856 DEB orbits at an average altitude of 3,361 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of OPS 0856 DEB’s average altitude, there are currently 1 active payload and 4 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 88.4°, OPS 0856 DEB passes over latitudes between 88.4°N and 88.4°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.
🔗 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 0856 DEB orbits in Medium Earth Orbit (MEO) at altitudes between 1,345 km (perigee) and 5,376 km (apogee), with an average altitude of approximately 3,361 km. It completes one orbit every 2 hours 39 minutes, travelling at approximately 23,040 km/h (14,316 mph).
OPS 0856 DEB (NORAD ID 24676) 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 0856 DEB was launched on 1966-08-19 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 0856 DEB (NORAD ID 24676) 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 0856 DEB travels at approximately 23,040 km/h (14,316 mph) — roughly 6.40 km/s. It completes 9.03 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 18 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 6.40 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 0856 DEB. Read more about debris statistics and the Kessler syndrome.