KKS-1 (KISEKI)
NORAD 33499
Payload
LEO
2009-002H
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LEO · NORAD 33499
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
615 km
Apogee
624 km
Inclination
98.1°
Period
97.1 min
Mean Motion
14.83128488 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude620 km
Orbital Velocity27,184 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.83
Eccentricity0.0006
Semi-Major Axis6,991 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Tokyo Metropolitan College of Industrial Technology (Japan)
Launch Date
2009-01-23
Launch Site
TNSTA
Int'l Designator
2009-002H
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
KKS-1 (KISEKI) is an active satellite operated by Tokyo Metropolitan College of Industrial Technology (Japan), launched on 2009-01-23 from TNSTA. After 17 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 615 km and 624 km with an inclination of 98.1°. It travels at approximately 27,184 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.83 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 ~10–25 years. Orbital Radar tracks KKS-1 (KISEKI) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
KKS-1 (KISEKI) orbits at an average altitude of 620 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 KKS-1 (KISEKI)’s average altitude, there are currently 1,540 active payloads and 771 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3090, STARLINK-3077. This makes it one of the more crowded altitude bands, containing roughly 8.8% of all active satellites. With an inclination of 98.1°, KKS-1 (KISEKI) passes over latitudes between 98.1°N and 98.1°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. Japan operates approximately 189 active satellites in total, of which 33 share a similar altitude band with KKS-1 (KISEKI).
❓ Frequently Asked Questions
KKS-1 (KISEKI) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 620 km altitude. Its 98.1° 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 97 minutes, travelling at 27,184 km/h.
KKS-1 (KISEKI) is operated by Tokyo Metropolitan College of Industrial Technology (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 33499. You can track KKS-1 (KISEKI) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
KKS-1 (KISEKI) was launched on 2009-01-23 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks KKS-1 (KISEKI) (NORAD ID 33499) 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.
KKS-1 (KISEKI) travels at approximately 27,184 km/h (16,892 mph) — roughly 7.55 km/s. It completes 14.83 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.