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IUS DEB

NORAD 43367 Debris MEO 1999-040Q
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
806 km
Apogee
9499 km
Inclination
28.1°
Period
205.4 min
Mean Motion
7.01198043 rev/day
TLE Epoch
2026-06-13 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude5,153 km
Orbital Velocity21,173 km/h
Velocity5.88 km/s
Orbital Period3 hours 25 minutes
Orbits / Day7.01
Eccentricity0.3772
Semi-Major Axis11,524 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1999-07-23
Launch Site
Cape Canaveral, Florida
Int'l Designator
1999-040Q
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
IUS DEB is a tracked piece of space debris attributed to United States, launched on 1999-07-23 from Cape Canaveral, Florida on the OV-102 IUS deploy launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 806 km and 9,499 km with an inclination of 28.1°. It travels at approximately 21,173 km/h (5.88 km/s), completing one full orbit every 3 hours 25 minutes — that’s roughly 7.01 orbits per day. Its orbital eccentricity of 0.3772 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, IUS 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
IUS DEB orbits at an average altitude of 5,153 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 IUS DEB’s average altitude, there are currently 0 active payloads and 2 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 28.1°, IUS DEB passes over latitudes between 28.1°N and 28.1°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 12,358 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
IUS DEB orbits in Medium Earth Orbit (MEO) at altitudes between 806 km (perigee) and 9,499 km (apogee), with an average altitude of approximately 5,153 km. It completes one orbit every 3 hours 25 minutes, travelling at approximately 21,173 km/h (13,156 mph).
IUS DEB (NORAD ID 43367) 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.
IUS DEB was launched on 1999-07-23 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. 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 IUS DEB (NORAD ID 43367) 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.
IUS DEB travels at approximately 21,173 km/h (13,156 mph) — roughly 5.88 km/s. It completes 7.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 14 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 5.88 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 IUS DEB. Read more about debris statistics and the Kessler syndrome.