Skip to content
Home Library Satellite Directory IRIDIUM 47 DEB

IRIDIUM 47 DEB

NORAD 40254 Debris LEO 1997-082P
CONNECTING… LEO · NORAD 40254
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
593 km
Apogee
685 km
Inclination
86.0°
Period
97.5 min
Mean Motion
14.77031703 rev/day
TLE Epoch
2026-06-20 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude639 km
Orbital Velocity27,146 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.77
Eccentricity0.0066
Semi-Major Axis7,010 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Iridium Communications (United States)
Launch Date
1997-12-20
Launch Site
Vandenberg SFB, California
Int'l Designator
1997-082P
Object Type
Debris
RCS Size
Small (<0.1 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 593 km and 685 km with an inclination of 86.0°. It travels at approximately 27,146 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.77 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 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 639 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 755 active payloads and 913 tracked debris or rocket body fragments — notable neighbours include AQUA, ONEWEB-0050. With an inclination of 86.0°, IRIDIUM 47 DEB passes over latitudes between 86.0°N and 86.0°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 327 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 593 km (perigee) and 685 km (apogee), with an average altitude of approximately 639 km. It completes one orbit every 98 minutes, travelling at approximately 27,146 km/h (16,868 mph).
IRIDIUM 47 DEB (NORAD ID 40254) 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks IRIDIUM 47 DEB (NORAD ID 40254) 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 27,146 km/h (16,868 mph) — roughly 7.54 km/s. It completes 14.77 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 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 7.54 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.