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IRAS

NORAD 13777 Payload LEO 1983-004A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
878 km
Apogee
904 km
Inclination
99.1°
Period
102.8 min
Mean Motion
14.00921964 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude891 km
Orbital Velocity26,671 km/h
Velocity7.41 km/s
Orbital Period103 minutes
Orbits / Day14.01
Eccentricity0.0018
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 878 km and 904 km with an inclination of 99.1°. It travels at approximately 26,671 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 orbits at an average altitude of 891 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of IRAS’s average altitude, there are currently 201 active payloads and 1,490 tracked debris or rocket body fragments. With an inclination of 99.1°, IRAS passes over latitudes between 99.1°N and 99.1°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 32 share a similar altitude band with IRAS.
❓ Frequently Asked Questions
IRAS is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 891 km altitude. Its 99.1° 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 26,671 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 or browse all operators in the operator directory.
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. View the full satellite launch log.
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. You can also browse the satellite directory to find other tracked objects.
IRAS travels at approximately 26,671 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.