HIBARI
NORAD 49400
Payload
LEO
2021-102F
● Active
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LEO · NORAD 49400
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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
463 km
Apogee
479 km
Inclination
97.3°
Period
94.0 min
Mean Motion
15.31761296 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude471 km
Orbital Velocity27,478 km/h
Velocity7.63 km/s
Orbital Period94 minutes
Orbits / Day15.32
Eccentricity0.0012
Semi-Major Axis6,842 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Tokyo Institute of Technology (Japan)
Launch Date
2021-11-09
Launch Site
Uchinoura, Japan
Int'l Designator
2021-102F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
HIBARI is an active satellite operated by Tokyo Institute of Technology (Japan), launched on 2021-11-09 from Uchinoura, Japan. It orbits in Low Earth Orbit (LEO) at altitudes between 463 km and 479 km with an inclination of 97.3°. It travels at approximately 27,478 km/h (7.63 km/s), completing one full orbit every 94 minutes — that’s roughly 15.32 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 ~1–3 years. Orbital Radar tracks HIBARI in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HIBARI orbits at an average altitude of 471 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 HIBARI’s average altitude, there are currently 7,923 active payloads and 196 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 45.5% of all active satellites. With an inclination of 97.3°, HIBARI passes over latitudes between 97.3°N and 97.3°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 25 share a similar altitude band with HIBARI.
❓ Frequently Asked Questions
HIBARI is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 471 km altitude. Its 97.3° 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 27,478 km/h.
HIBARI is operated by Tokyo Institute of Technology (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 49400. You can track HIBARI in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HIBARI was launched on 2021-11-09 from Uchinoura, Japan. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks HIBARI (NORAD ID 49400) 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.
HIBARI travels at approximately 27,478 km/h (17,074 mph) — roughly 7.63 km/s. It completes 15.32 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.