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EYESAT A (AO-27)

NORAD 22825 Payload LEO 1993-061C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
782 km
Apogee
795 km
Inclination
98.7°
Period
100.6 min
Mean Motion
14.30915625 rev/day
TLE Epoch
2026-03-17 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude789 km
Orbital Velocity26,861 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.31
Eccentricity0.0009
Semi-Major Axis7,160 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1993-09-26
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1993-061C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
🔗 Constellation / Groups
amateur
📖 About This Object
EYESAT A (AO-27) is an active satellite operated by United States, launched on 1993-09-26 from Guiana Space Centre, Kourou. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 782 km and 795 km with an inclination of 98.7°. It travels at approximately 26,861 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.31 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. It is part of the Amateur constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks EYESAT A (AO-27) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
EYESAT A (AO-27) 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
EYESAT A (AO-27) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 789 km altitude. Its 98.7° 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 101 minutes, travelling at 26,861 km/h.
EYESAT A (AO-27) is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22825. You can track EYESAT A (AO-27) in real time on Orbital Radar’s live tracker.
EYESAT A (AO-27) was launched on 1993-09-26 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years.
Yes — Orbital Radar tracks EYESAT A (AO-27) (NORAD ID 22825) 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.
EYESAT A (AO-27) travels at approximately 26,861 km/h (16,691 mph) — roughly 7.46 km/s. It completes 14.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
EYESAT A (AO-27) is a member of the Amateur constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Amateur satellites on Orbital Radar’s live tracker.