IUS DEB
NORAD 43361
Debris
MEO
1999-040J
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MEO · NORAD 43361
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
1267 km
Apogee
8626 km
Inclination
27.8°
Period
199.9 min
Mean Motion
7.20378261 rev/day
TLE Epoch
2026-09-16 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude4,947 km
Orbital Velocity21,365 km/h
Velocity5.93 km/s
Orbital Period3 hours 20 minutes
Orbits / Day7.20
Eccentricity0.3251
Semi-Major Axis11,318 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1999-07-23
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1999-040J
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 Space Force Station, United States 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 1,267 km and 8,626 km with an inclination of 27.8°. It travels at approximately 21,365 km/h (5.93 km/s), completing one full orbit every 3 hours 20 minutes — that’s roughly 7.20 orbits per day. Its orbital eccentricity of 0.3251 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 4,947 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 1 active payload and 6 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 27.8°, IUS DEB passes over latitudes between 27.8°N and 27.8°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 13,199 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 1,267 km (perigee) and 8,626 km (apogee), with an average altitude of approximately 4,947 km. It completes one orbit every 3 hours 20 minutes, travelling at approximately 21,365 km/h (13,275 mph).
IUS DEB (NORAD ID 43361) 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 Space Force Station, United States, 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 43361) 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 21,365 km/h (13,275 mph) — roughly 5.93 km/s. It completes 7.20 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 5.93 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.