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GEOSAT

NORAD 15595 Payload LEO 1985-021A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
758 km
Apogee
760 km
Inclination
108.0°
Period
100.0 min
Mean Motion
14.39967314 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude759 km
Orbital Velocity26,917 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.40
Eccentricity0.0001
Semi-Major Axis7,130 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1985-03-13
Launch Site
Vandenberg SFB, California
Int'l Designator
1985-021A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GEOSAT is an active satellite operated by United States, launched on 1985-03-13 from Vandenberg SFB, California. With over 41 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 758 km and 760 km with an inclination of 108.0°. It travels at approximately 26,917 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.40 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks GEOSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GEOSAT orbits at an average altitude of 759 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 GEOSAT’s average altitude, there are currently 357 active payloads and 2,015 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179. With an inclination of 108.0°, GEOSAT passes over latitudes between 108.0°N and 108.0°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 12,360 active satellites in total, of which 148 share a similar altitude band with GEOSAT.
❓ Frequently Asked Questions
GEOSAT orbits in Low Earth Orbit (LEO) at altitudes between 758 km (perigee) and 760 km (apogee), with an average altitude of approximately 759 km. It completes one orbit every 100 minutes, travelling at approximately 26,917 km/h (16,725 mph).
GEOSAT is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 15595. You can track GEOSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
GEOSAT was launched on 1985-03-13 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 GEOSAT (NORAD ID 15595) 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.
GEOSAT travels at approximately 26,917 km/h (16,725 mph) — roughly 7.48 km/s. It completes 14.40 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.