NEONSAT-1
NORAD 59587
Payload
LEO
2024-077A
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LEO · NORAD 59587
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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
437 km
Apogee
446 km
Inclination
97.3°
Period
93.4 min
Mean Motion
15.41728730 rev/day
TLE Epoch
2026-11-02 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude442 km
Orbital Velocity27,537 km/h
Velocity7.65 km/s
Orbital Period93 minutes
Orbits / Day15.42
Eccentricity0.0007
Semi-Major Axis6,813 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇰🇷 KAIST (South Korea)
Launch Date
2024-04-23
Launch Site
Rocket Lab Launch Complex 1, New Zealand
Int'l Designator
2024-077A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
NEONSAT-1 is an active satellite operated by KAIST (South Korea), launched on 2024-04-23 from Rocket Lab Launch Complex 1, New Zealand on the Neonsat-1 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 437 km and 446 km with an inclination of 97.3°. It travels at approximately 27,537 km/h (7.65 km/s), completing one full orbit every 93 minutes — that’s roughly 15.42 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 ~1–3 years. Orbital Radar tracks NEONSAT-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
NEONSAT-1 orbits at an average altitude of 442 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 NEONSAT-1’s average altitude, there are currently 10,451 active payloads and 140 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 55.1% of all active satellites. With an inclination of 97.3°, NEONSAT-1 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. South Korea operates approximately 65 active satellites in total, of which 6 share a similar altitude band with NEONSAT-1.
❓ Frequently Asked Questions
NEONSAT-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 442 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 93 minutes, travelling at 27,537 km/h.
NEONSAT-1 is operated by KAIST (South Korea). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59587. You can track NEONSAT-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
NEONSAT-1 was launched on 2024-04-23 from Rocket Lab Launch Complex 1, New Zealand. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks NEONSAT-1 (NORAD ID 59587) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
NEONSAT-1 travels at approximately 27,537 km/h (17,111 mph) — roughly 7.65 km/s. It completes 15.42 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.