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SEEDS II (CO-66)

NORAD 32791 Payload LEO 2008-021J ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
477 km
Apogee
478 km
Inclination
97.8°
Period
94.2 min
Mean Motion
15.29438589 rev/day
TLE Epoch
2026-03-17 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude478 km
Orbital Velocity27,465 km/h
Velocity7.63 km/s
Orbital Period94 minutes
Orbits / Day15.29
Eccentricity0.0001
Semi-Major Axis6,849 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2008-04-28
Launch Site
SRI
Int'l Designator
2008-021J
Object Type
Payload
RCS Size
Small (<0.1 m²)
🔗 Constellation / Groups
cubesatamateur
📖 About This Object
SEEDS II (CO-66) is an active satellite operated by Japan, launched on 2008-04-28 from SRI. After 18 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 477 km and 478 km with an inclination of 97.8°. It travels at approximately 27,465 km/h (7.63 km/s), completing one full orbit every 94 minutes — that’s roughly 15.29 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 Cubesat constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks SEEDS II (CO-66) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SEEDS II (CO-66) 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
SEEDS II (CO-66) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 478 km altitude. Its 97.8° 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 94 minutes, travelling at 27,465 km/h.
SEEDS II (CO-66) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 32791. You can track SEEDS II (CO-66) in real time on Orbital Radar’s live tracker.
SEEDS II (CO-66) was launched on 2008-04-28 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years.
Yes — Orbital Radar tracks SEEDS II (CO-66) (NORAD ID 32791) 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.
SEEDS II (CO-66) travels at approximately 27,465 km/h (17,066 mph) — roughly 7.63 km/s. It completes 15.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.
SEEDS II (CO-66) is a member of the Cubesat constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Cubesat satellites on Orbital Radar’s live tracker.