IRIDIUM 920
NORAD 24871
Payload
LEO
1997-034C
● Active
CONNECTING…
LEO · NORAD 24871
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
745 km
Apogee
759 km
Inclination
86.4°
Period
99.9 min
Mean Motion
14.41896279 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude752 km
Orbital Velocity26,930 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.42
Eccentricity0.0010
Semi-Major Axis7,123 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Iridium Communications (United States)
Launch Date
1997-07-09
Launch Site
Vandenberg SFB, California
Int'l Designator
1997-034C
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
iridium
📖 About This Object
IRIDIUM 920 is an active satellite operated by Iridium Communications (United States), launched on 1997-07-09 from Vandenberg SFB, California. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 745 km and 759 km with an inclination of 86.4°. It travels at approximately 26,930 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.42 orbits per day. It is part of the Iridium constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks IRIDIUM 920 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IRIDIUM 920 orbits at an average altitude of 752 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 920’s average altitude, there are currently 357 active payloads and 1,962 tracked debris or rocket body fragments — notable neighbours include LANDSAT 9. With an inclination of 86.4°, IRIDIUM 920 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 12,339 active satellites in total, of which 149 share a similar altitude band with IRIDIUM 920.
🔗 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 920 orbits in Low Earth Orbit (LEO) at altitudes between 745 km (perigee) and 759 km (apogee), with an average altitude of approximately 752 km. It completes one orbit every 100 minutes, travelling at approximately 26,930 km/h (16,734 mph).
IRIDIUM 920 is operated by Iridium Communications (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24871. You can track IRIDIUM 920 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRIDIUM 920 was launched on 1997-07-09 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 920 (NORAD ID 24871) 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 920 travels at approximately 26,930 km/h (16,734 mph) — roughly 7.48 km/s. It completes 14.42 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
IRIDIUM 920 is a member of the Iridium constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Iridium satellites on Orbital Radar’s live tracker.