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TEN-KOH 2

NORAD 68261 Payload LEO 2025-241B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
490 km
Apogee
498 km
Inclination
51.7°
Period
94.5 min
Mean Motion
15.23889978 rev/day
TLE Epoch
2026-06-15 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude494 km
Orbital Velocity27,432 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.24
Eccentricity0.0006
Semi-Major Axis6,865 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2025-10-26
Launch Site
TNSTA
Int'l Designator
2025-241B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TEN-KOH 2 is an active satellite operated by Japan, launched on 2025-10-26 from TNSTA. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 490 km and 498 km with an inclination of 51.7°. It travels at approximately 27,432 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.24 orbits per day. 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 ~1–3 years. Orbital Radar tracks TEN-KOH 2 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 2 orbits at an average altitude of 494 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of TEN-KOH 2’s average altitude, there are currently 9,156 active payloads and 238 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 52.6% of all active satellites. With an inclination of 51.7°, TEN-KOH 2 passes over latitudes between 51.7°N and 51.7°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Japan operates approximately 189 active satellites in total, of which 32 share a similar altitude band with TEN-KOH 2.
❓ Frequently Asked Questions
TEN-KOH 2 orbits in Low Earth Orbit (LEO) at altitudes between 490 km (perigee) and 498 km (apogee), with an average altitude of approximately 494 km. It completes one orbit every 95 minutes, travelling at approximately 27,432 km/h (17,045 mph).
TEN-KOH 2 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 68261. You can track TEN-KOH 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TEN-KOH 2 was launched on 2025-10-26 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks TEN-KOH 2 (NORAD ID 68261) 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 2 travels at approximately 27,432 km/h (17,045 mph) — roughly 7.62 km/s. It completes 15.24 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.