SNUSAT-2
NORAD 43782
Payload
LEO
2018-099AA
● Active
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LEO · NORAD 43782
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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
494 km
Apogee
506 km
Inclination
97.4°
Period
94.6 min
Mean Motion
15.21860979 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude500 km
Orbital Velocity27,420 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.22
Eccentricity0.0009
Semi-Major Axis6,871 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇰🇷 South Korea
Launch Date
2018-12-03
Launch Site
Vandenberg SFB, California
Int'l Designator
2018-099AA
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SNUSAT-2 is an active satellite operated by South Korea, launched on 2018-12-03 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 494 km and 506 km with an inclination of 97.4°. It travels at approximately 27,420 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.22 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 ~3–10 years. Orbital Radar tracks SNUSAT-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
SNUSAT-2 orbits at an average altitude of 500 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 SNUSAT-2’s average altitude, there are currently 9,610 active payloads and 240 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 55.2% of all active satellites. With an inclination of 97.4°, SNUSAT-2 passes over latitudes between 97.4°N and 97.4°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. South Korea operates approximately 51 active satellites in total, of which 13 share a similar altitude band with SNUSAT-2.
❓ Frequently Asked Questions
SNUSAT-2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 500 km altitude. Its 97.4° 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 95 minutes, travelling at 27,420 km/h.
SNUSAT-2 is operated by South Korea. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43782. You can track SNUSAT-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SNUSAT-2 was launched on 2018-12-03 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks SNUSAT-2 (NORAD ID 43782) 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.
SNUSAT-2 travels at approximately 27,420 km/h (17,038 mph) — roughly 7.62 km/s. It completes 15.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.