IRIDIUM 914
NORAD 24836
Payload
LEO
1997-030A
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LEO · NORAD 24836
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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
752 km
Apogee
757 km
Inclination
86.4°
Period
99.9 min
Mean Motion
14.41239469 rev/day
TLE Epoch
2026-06-19 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude755 km
Orbital Velocity26,925 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.41
Eccentricity0.0004
Semi-Major Axis7,126 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 Iridium Communications (United States)
Launch Date
1997-06-18
Launch Site
Baikonur, Kazakhstan
Int'l Designator
1997-030A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
iridium
📖 About This Object
IRIDIUM 914 is an active satellite operated by Iridium Communications (United States), launched on 1997-06-18 from Baikonur, Kazakhstan. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 752 km and 757 km with an inclination of 86.4°. It travels at approximately 26,925 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.41 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. 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 914 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 914 orbits at an average altitude of 755 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 914’s average altitude, there are currently 355 active payloads and 1,995 tracked debris or rocket body fragments. With an inclination of 86.4°, IRIDIUM 914 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 147 share a similar altitude band with IRIDIUM 914.
🔗 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 914 orbits in Low Earth Orbit (LEO) at altitudes between 752 km (perigee) and 757 km (apogee), with an average altitude of approximately 755 km. It completes one orbit every 100 minutes, travelling at approximately 26,925 km/h (16,731 mph).
IRIDIUM 914 is operated by Iridium Communications (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24836. You can track IRIDIUM 914 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRIDIUM 914 was launched on 1997-06-18 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks IRIDIUM 914 (NORAD ID 24836) 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 914 travels at approximately 26,925 km/h (16,731 mph) — roughly 7.48 km/s. It completes 14.41 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
IRIDIUM 914 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.