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PVSAT

NORAD 52894 Payload LEO 2022-065A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
688 km
Apogee
701 km
Inclination
98.2°
Period
98.7 min
Mean Motion
14.59544890 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude695 km
Orbital Velocity27,040 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.60
Eccentricity0.0009
Semi-Major Axis7,066 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇰🇷 Korean Aerospace Research Institute (KARI) (South Korea)
Launch Date
2022-06-21
Launch Site
Naro Space Center, South Korea
Int'l Designator
2022-065A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PVSAT is an active satellite operated by Korean Aerospace Research Institute (KARI) (South Korea), launched on 2022-06-21 from Naro Space Center, South Korea. It orbits in Low Earth Orbit (LEO) at altitudes between 688 km and 701 km with an inclination of 98.2°. It travels at approximately 27,040 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.60 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 ~10–25 years. Orbital Radar tracks PVSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PVSAT orbits at an average altitude of 695 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 PVSAT’s average altitude, there are currently 278 active payloads and 1,392 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.2°, PVSAT passes over latitudes between 98.2°N and 98.2°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 PVSAT.
❓ Frequently Asked Questions
PVSAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 695 km altitude. Its 98.2° 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 99 minutes, travelling at 27,040 km/h.
PVSAT is operated by Korean Aerospace Research Institute (KARI) (South Korea). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 52894. You can track PVSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PVSAT was launched on 2022-06-21 from Naro Space Center, South Korea. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks PVSAT (NORAD ID 52894) 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.
PVSAT travels at approximately 27,040 km/h (16,802 mph) — roughly 7.51 km/s. It completes 14.60 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.