IRIDIUM 47 DEB
NORAD 40251
Debris
LEO
1997-082L
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LEO · NORAD 40251
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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
693 km
Apogee
866 km
Inclination
86.3°
Period
100.4 min
Mean Motion
14.33640293 rev/day
TLE Epoch
2026-06-19 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude780 km
Orbital Velocity26,878 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.34
Eccentricity0.0121
Semi-Major Axis7,151 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Iridium Communications (United States)
Launch Date
1997-12-20
Launch Site
Vandenberg SFB, California
Int'l Designator
1997-082L
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
IRIDIUM 47 DEB is a tracked piece of space debris attributed to United States, launched on 1997-12-20 from Vandenberg SFB, California on the Iridium MS-6 launch. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 693 km and 866 km with an inclination of 86.3°. It travels at approximately 26,878 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.34 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. As orbital debris, IRIDIUM 47 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
IRIDIUM 47 DEB orbits at an average altitude of 780 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of IRIDIUM 47 DEB’s average altitude, there are currently 410 active payloads and 2,164 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 86.3°, IRIDIUM 47 DEB passes over latitudes between 86.3°N and 86.3°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 12,358 active satellites in total, of which 154 share a similar altitude band with IRIDIUM 47 DEB.
🔗 Iridium NEXT Constellation
This satellite is part of the Iridium NEXT constellation, a fleet of 66 operational cross-linked LEO satellites (plus spares) providing global voice, data and IoT connectivity. Iridium operates at approximately 780 km altitude across six polar orbital planes, ensuring coverage over the entire Earth surface including oceans and polar regions. The second-generation NEXT satellites replaced the original constellation between 2017–2019 and support Iridium Certus broadband and the Aireon ADS-B aircraft tracking payload.
❓ Frequently Asked Questions
IRIDIUM 47 DEB orbits in Low Earth Orbit (LEO) at altitudes between 693 km (perigee) and 866 km (apogee), with an average altitude of approximately 780 km. It completes one orbit every 100 minutes, travelling at approximately 26,878 km/h (16,701 mph).
IRIDIUM 47 DEB (NORAD ID 40251) 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.
IRIDIUM 47 DEB was launched on 1997-12-20 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks IRIDIUM 47 DEB (NORAD ID 40251) 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.
IRIDIUM 47 DEB travels at approximately 26,878 km/h (16,701 mph) — roughly 7.47 km/s. It completes 14.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 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 7.47 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 IRIDIUM 47 DEB. Read more about debris statistics and the Kessler syndrome.