Skip to content
Home Library Satellite Directory IRIDIUM 33 DEB

IRIDIUM 33 DEB

NORAD 34648 Debris LEO 1997-051JZ
CONNECTING… LEO · NORAD 34648
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
717 km
Apogee
969 km
Inclination
86.4°
Period
101.8 min
Mean Motion
14.14817176 rev/day
TLE Epoch
2026-06-26 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude843 km
Orbital Velocity26,760 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.15
Eccentricity0.0175
Semi-Major Axis7,214 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Iridium Communications (United States)
Launch Date
1997-09-14
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1997-051JZ
Object Type
Debris
RCS Size
Medium (0.1–1 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 717 km and 969 km with an inclination of 86.4°. It travels at approximately 26,760 km/h (7.43 km/s), completing one full orbit every 102 minutes — that’s roughly 14.15 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 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 843 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of IRIDIUM 33 DEB’s average altitude, there are currently 238 active payloads and 2,143 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 86.4°, IRIDIUM 33 DEB passes over latitudes between 86.4°N and 86.4°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 47 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 717 km (perigee) and 969 km (apogee), with an average altitude of approximately 843 km. It completes one orbit every 102 minutes, travelling at approximately 26,760 km/h (16,628 mph).
IRIDIUM 33 DEB (NORAD ID 34648) 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks IRIDIUM 33 DEB (NORAD ID 34648) 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 26,760 km/h (16,628 mph) — roughly 7.43 km/s. It completes 14.15 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.43 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.