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NEONSAT-1A

NORAD 67614 Payload LEO 2026-019A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
532 km
Apogee
550 km
Inclination
97.4°
Period
95.5 min
Mean Motion
15.08438238 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude541 km
Orbital Velocity27,338 km/h
Velocity7.59 km/s
Orbital Period95 minutes
Orbits / Day15.08
Eccentricity0.0013
Semi-Major Axis6,912 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇰🇷 South Korea
Launch Date
2026-01-30
Launch Site
RLLC
Int'l Designator
2026-019A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
NEONSAT-1A is an active satellite operated by South Korea, launched on 2026-01-30 from RLLC. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 532 km and 550 km with an inclination of 97.4°. It travels at approximately 27,338 km/h (7.59 km/s), completing one full orbit every 95 minutes — that’s roughly 15.08 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 ~3–10 years. Orbital Radar tracks NEONSAT-1A 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-1A orbits at an average altitude of 541 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-1A’s average altitude, there are currently 3,502 active payloads and 328 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 20.1% of all active satellites. With an inclination of 97.4°, NEONSAT-1A 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 16 share a similar altitude band with NEONSAT-1A.
❓ Frequently Asked Questions
NEONSAT-1A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 541 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 27,338 km/h.
NEONSAT-1A is operated by South Korea. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 67614. You can track NEONSAT-1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
NEONSAT-1A was launched on 2026-01-30 from RLLC. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks NEONSAT-1A (NORAD ID 67614) 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.
NEONSAT-1A travels at approximately 27,338 km/h (16,987 mph) — roughly 7.59 km/s. It completes 15.08 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.