IRAS
NORAD 13777
Payload
LEO
1983-004A
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LEO · NORAD 13777
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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
876 km
Apogee
905 km
Inclination
99.0°
Period
102.8 min
Mean Motion
14.00902493 rev/day
TLE Epoch
2026-05-08 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude891 km
Orbital Velocity26,672 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.01
Eccentricity0.0020
Semi-Major Axis7,262 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1983-01-26
Launch Site
Vandenberg SFB, California
Int'l Designator
1983-004A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
IRAS is an active satellite operated by United States, launched on 1983-01-26 from Vandenberg SFB, California. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 876 km and 905 km with an inclination of 99.0°. It travels at approximately 26,672 km/h (7.41 km/s), completing one full orbit every 103 minutes — that’s roughly 14.01 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks IRAS in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IRAS operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
❓ Frequently Asked Questions
IRAS is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 891 km altitude. Its 99.0° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 103 minutes, travelling at 26,672 km/h.
IRAS is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13777. You can track IRAS in real time on Orbital Radar’s live tracker.
IRAS was launched on 1983-01-26 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: ~100–500 years.
Yes — Orbital Radar tracks IRAS (NORAD ID 13777) 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.
IRAS travels at approximately 26,672 km/h (16,573 mph) — roughly 7.41 km/s. It completes 14.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.