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GOSAT 2 (IBUKI 1)

NORAD 43672 Payload LEO 2018-084B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
615 km
Apogee
617 km
Inclination
97.9°
Period
97.0 min
Mean Motion
14.84244285 rev/day
TLE Epoch
2026-03-16 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude616 km
Orbital Velocity27,191 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.84
Eccentricity0.0001
Semi-Major Axis6,987 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2018-10-29
Launch Site
TNSTA
Int'l Designator
2018-084B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
GOSAT 2 (IBUKI 1) is an active satellite operated by Japan, launched on 2018-10-29 from TNSTA. It orbits in Low Earth Orbit (LEO) at altitudes between 615 km and 617 km with an inclination of 97.9°. It travels at approximately 27,191 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.84 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 GOSAT 2 (IBUKI 1) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
GOSAT 2 (IBUKI 1) 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
GOSAT 2 (IBUKI 1) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 616 km altitude. Its 97.9° 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 27,191 km/h.
GOSAT 2 (IBUKI 1) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43672. You can track GOSAT 2 (IBUKI 1) in real time on Orbital Radar’s live tracker.
GOSAT 2 (IBUKI 1) was launched on 2018-10-29 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years.
Yes — Orbital Radar tracks GOSAT 2 (IBUKI 1) (NORAD ID 43672) 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.
GOSAT 2 (IBUKI 1) travels at approximately 27,191 km/h (16,896 mph) — roughly 7.55 km/s. It completes 14.84 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.