KOMPSAT 2
NORAD 29268
Payload
LEO
2006-031A
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LEO · NORAD 29268
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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
667 km
Apogee
689 km
Inclination
97.8°
Period
98.3 min
Mean Motion
14.64660259 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude678 km
Orbital Velocity27,071 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.65
Eccentricity0.0016
Semi-Major Axis7,049 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇰🇷 Korea Aerospace Research Institute (KARI) (South Korea)
Launch Date
2006-07-28
Launch Site
PKMTR
Int'l Designator
2006-031A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
KOMPSAT 2 is an active satellite operated by Korea Aerospace Research Institute (KARI) (South Korea), launched on 2006-07-28 from PKMTR. With over 20 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 667 km and 689 km with an inclination of 97.8°. It travels at approximately 27,071 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.65 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 ~10–25 years. Orbital Radar tracks KOMPSAT 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
KOMPSAT 2 orbits at an average altitude of 678 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 KOMPSAT 2’s average altitude, there are currently 521 active payloads and 1,255 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 97.8°, KOMPSAT 2 passes over latitudes between 97.8°N and 97.8°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 12 share a similar altitude band with KOMPSAT 2.
❓ Frequently Asked Questions
KOMPSAT 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 678 km altitude. Its 97.8° 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 98 minutes, travelling at 27,071 km/h.
KOMPSAT 2 is operated by Korea Aerospace Research Institute (KARI) (South Korea). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 29268. You can track KOMPSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
KOMPSAT 2 was launched on 2006-07-28 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks KOMPSAT 2 (NORAD ID 29268) 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.
KOMPSAT 2 travels at approximately 27,071 km/h (16,821 mph) — roughly 7.52 km/s. It completes 14.65 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.