TEN-KOH
NORAD 43677
Payload
LEO
2018-084G
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LEO · NORAD 43677
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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
550 km
Apogee
566 km
Inclination
98.1°
Period
95.8 min
Mean Motion
15.02949767 rev/day
TLE Epoch
2026-06-19 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude558 km
Orbital Velocity27,305 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.03
Eccentricity0.0012
Semi-Major Axis6,929 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Kyushu Institute of Technology (KIT) (Japan)
Launch Date
2018-10-29
Launch Site
TNSTA
Int'l Designator
2018-084G
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TEN-KOH is an active satellite operated by Kyushu Institute of Technology (KIT) (Japan), launched on 2018-10-29 from TNSTA. It orbits in Low Earth Orbit (LEO) at altitudes between 550 km and 566 km with an inclination of 98.1°. It travels at approximately 27,305 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.03 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks TEN-KOH in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TEN-KOH orbits at an average altitude of 558 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 TEN-KOH’s average altitude, there are currently 3,274 active payloads and 407 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 18.8% of all active satellites. With an inclination of 98.1°, TEN-KOH 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 40 share a similar altitude band with TEN-KOH.
❓ Frequently Asked Questions
TEN-KOH is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 558 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 96 minutes, travelling at 27,305 km/h.
TEN-KOH is operated by Kyushu Institute of Technology (KIT) (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43677. You can track TEN-KOH in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TEN-KOH was launched on 2018-10-29 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks TEN-KOH (NORAD ID 43677) 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.
TEN-KOH travels at approximately 27,305 km/h (16,966 mph) — roughly 7.58 km/s. It completes 15.03 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.