CONTECSAT-1
NORAD 59117
Payload
LEO
2024-043V
● Active
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LEO · NORAD 59117
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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
450 km
Apogee
462 km
Inclination
97.6°
Period
93.7 min
Mean Motion
15.36660535 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude456 km
Orbital Velocity27,508 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.37
Eccentricity0.0009
Semi-Major Axis6,827 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇰🇷 South Korea
Launch Date
2024-03-04
Launch Site
Vandenberg SFB, California
Int'l Designator
2024-043V
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CONTECSAT-1 is an active satellite operated by South Korea, launched on 2024-03-04 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 450 km and 462 km with an inclination of 97.6°. It travels at approximately 27,508 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.37 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 CONTECSAT-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
CONTECSAT-1 orbits at an average altitude of 456 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 CONTECSAT-1’s average altitude, there are currently 7,832 active payloads and 169 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 45% of all active satellites. With an inclination of 97.6°, CONTECSAT-1 passes over latitudes between 97.6°N and 97.6°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 11 share a similar altitude band with CONTECSAT-1.
❓ Frequently Asked Questions
CONTECSAT-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 456 km altitude. Its 97.6° 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 94 minutes, travelling at 27,508 km/h.
CONTECSAT-1 is operated by South Korea. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59117. You can track CONTECSAT-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CONTECSAT-1 was launched on 2024-03-04 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks CONTECSAT-1 (NORAD ID 59117) 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.
CONTECSAT-1 travels at approximately 27,508 km/h (17,093 mph) — roughly 7.64 km/s. It completes 15.37 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.