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A-SEANSAT-PG1

NORAD 57197 Payload LEO 2023-091AH ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
449 km
Apogee
460 km
Inclination
97.5°
Period
93.7 min
Mean Motion
15.37038994 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude455 km
Orbital Velocity27,511 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.37
Eccentricity0.0008
Semi-Major Axis6,826 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
Malaysia
Launch Date
2023-06-27
Launch Site
Vostochny, Russia
Int'l Designator
2023-091AH
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
A-SEANSAT-PG1 is an active satellite operated by Malaysia, launched on 2023-06-27 from Vostochny, Russia. It orbits in Low Earth Orbit (LEO) at altitudes between 449 km and 460 km with an inclination of 97.5°. It travels at approximately 27,511 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 A-SEANSAT-PG1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
A-SEANSAT-PG1 orbits at an average altitude of 455 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 A-SEANSAT-PG1’s average altitude, there are currently 7,842 active payloads and 167 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 97.5°, A-SEANSAT-PG1 passes over latitudes between 97.5°N and 97.5°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. Malaysia operates approximately 9 active satellites in total.
❓ Frequently Asked Questions
A-SEANSAT-PG1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 455 km altitude. Its 97.5° 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 27,511 km/h.
A-SEANSAT-PG1 is operated by Malaysia. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 57197. You can track A-SEANSAT-PG1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
A-SEANSAT-PG1 was launched on 2023-06-27 from Vostochny, Russia. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks A-SEANSAT-PG1 (NORAD ID 57197) 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.
A-SEANSAT-PG1 travels at approximately 27,511 km/h (17,094 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.