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OPS 9442 (DSCS 2-12) DEB

NORAD 59992 Debris GEO 1978-113H
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35318 km
Apogee
37362 km
Inclination
8.3°
Period
1464.5 min
Mean Motion
0.98330143 rev/day
TLE Epoch
2026-06-19 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,340 km
Orbital Velocity10,998 km/h
Velocity3.05 km/s
Orbital Period24.4 hours
Orbits / Day0.98
Eccentricity0.0239
Semi-Major Axis42,711 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1978-12-14
Launch Site
Cape Canaveral, Florida
Int'l Designator
1978-113H
Object Type
Debris
RCS Size
Unknown
📖 About This Object
OPS 9442 (DSCS 2-12) DEB is a tracked piece of space debris attributed to United States, launched on 1978-12-14 from Cape Canaveral, Florida on the DSCS II C-11 launch. With over 48 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,318 km and 37,362 km with an inclination of 8.3°. It travels at approximately 10,998 km/h (3.05 km/s), completing one full orbit every 24.4 hours — that’s roughly 0.98 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. As orbital debris, OPS 9442 (DSCS 2-12) 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 9442 (DSCS 2-12) DEB occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 8.3°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of OPS 9442 (DSCS 2-12) DEB’s average altitude, there are currently 43 active payloads and 10 tracked debris or rocket body fragments. United States operates approximately 12,358 active satellites in total, of which 11 share a similar altitude band with OPS 9442 (DSCS 2-12) 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 9442 (DSCS 2-12) DEB orbits at approximately 36,340 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 10,998 km/h — it just keeps pace with the ground below. With an inclination of 8.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
OPS 9442 (DSCS 2-12) DEB (NORAD ID 59992) 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 9442 (DSCS 2-12) DEB was launched on 1978-12-14 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 9442 (DSCS 2-12) DEB (NORAD ID 59992) 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 9442 (DSCS 2-12) DEB travels at approximately 10,998 km/h (6,834 mph) — roughly 3.05 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.
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 3.05 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 9442 (DSCS 2-12) DEB. Read more about debris statistics and the Kessler syndrome.