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EYESAT A

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
14.30942876 rev/day
TLE Epoch
2026-06-19 17:00:00 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)
📖 About This Object
EYESAT A 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks EYESAT A 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 orbits at an average altitude of 789 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 EYESAT A’s average altitude, there are currently 418 active payloads and 2,234 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, EYESAT A passes over latitudes between 98.7°N and 98.7°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 155 share a similar altitude band with EYESAT A.
❓ Frequently Asked Questions
EYESAT A 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 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22825. You can track EYESAT A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EYESAT A 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. View the full satellite launch log.
Yes — Orbital Radar tracks EYESAT A (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. You can also browse the satellite directory to find other tracked objects.
EYESAT A 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.