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OSCAR 30 DEB

NORAD 21878 Debris LEO 1985-066H
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
957 km
Apogee
1174 km
Inclination
90.2°
Period
106.5 min
Mean Motion
13.51939680 rev/day
TLE Epoch
2026-06-26 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,066 km
Orbital Velocity26,356 km/h
Velocity7.32 km/s
Orbital Period107 minutes
Orbits / Day13.52
Eccentricity0.0146
Semi-Major Axis7,437 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1985-08-03
Launch Site
Vandenberg SFB, California
Int'l Designator
1985-066H
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OSCAR 30 DEB is a tracked piece of space debris attributed to United States, launched on 1985-08-03 from Vandenberg SFB, California on the NNS O-24 launch. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 957 km and 1,174 km with an inclination of 90.2°. It travels at approximately 26,356 km/h (7.32 km/s), completing one full orbit every 107 minutes — that’s roughly 13.52 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. As orbital debris, OSCAR 30 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
OSCAR 30 DEB orbits at an average altitude of 1,066 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of OSCAR 30 DEB’s average altitude, there are currently 187 active payloads and 437 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 90.2°, OSCAR 30 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 12,413 active satellites in total, of which 14 share a similar altitude band with OSCAR 30 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
OSCAR 30 DEB orbits in Low Earth Orbit (LEO) at altitudes between 957 km (perigee) and 1,174 km (apogee), with an average altitude of approximately 1,066 km. It completes one orbit every 107 minutes, travelling at approximately 26,356 km/h (16,377 mph).
OSCAR 30 DEB (NORAD ID 21878) 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.
OSCAR 30 DEB was launched on 1985-08-03 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks OSCAR 30 DEB (NORAD ID 21878) 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.
OSCAR 30 DEB travels at approximately 26,356 km/h (16,377 mph) — roughly 7.32 km/s. It completes 13.52 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 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 7.32 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 OSCAR 30 DEB. Read more about debris statistics and the Kessler syndrome.