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IRIDIUM 33 DEB

NORAD 35915 Debris LEO 1997-051TY
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
604 km
Apogee
617 km
Inclination
86.3°
Period
96.9 min
Mean Motion
14.86078662 rev/day
TLE Epoch
2026-06-23 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude611 km
Orbital Velocity27,202 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.86
Eccentricity0.0009
Semi-Major Axis6,982 km
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Iridium Communications (United States)
Launch Date
1997-09-14
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1997-051TY
Object Type
Debris
RCS Size
Small (<0.1 m²)
📖 About This Object
IRIDIUM 33 DEB is a tracked piece of space debris attributed to United States, launched on 1997-09-14 from Baikonur, Kazakhstan on the Iridium SV029 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 604 km and 617 km with an inclination of 86.3°. It travels at approximately 27,202 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.86 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. As orbital debris, IRIDIUM 33 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 33 DEB orbits at an average altitude of 611 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 33 DEB’s average altitude, there are currently 1,599 active payloads and 714 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 9.1% of all active satellites. With an inclination of 86.3°, IRIDIUM 33 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 12,413 active satellites in total, of which 1,089 share a similar altitude band with IRIDIUM 33 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 33 DEB orbits in Low Earth Orbit (LEO) at altitudes between 604 km (perigee) and 617 km (apogee), with an average altitude of approximately 611 km. It completes one orbit every 97 minutes, travelling at approximately 27,202 km/h (16,902 mph).
IRIDIUM 33 DEB (NORAD ID 35915) 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 33 DEB was launched on 1997-09-14 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks IRIDIUM 33 DEB (NORAD ID 35915) 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 33 DEB travels at approximately 27,202 km/h (16,902 mph) — roughly 7.56 km/s. It completes 14.86 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 7.56 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 33 DEB. Read more about debris statistics and the Kessler syndrome.