A-SEANSAT-PG1, 57197
Orbit data source: Space-Track
A-SEANSAT-PG1, 57197 is a payload satellite owned by ANGKASA-X (MY) in SSO that was launched on Tue, 27 Jun 2023 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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57197 intel report (Beta)
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Identifier
Orbit
Country
MY / MALARelated business
Manufacturer
ANGKASA-X
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 A-SEANSAT-PG1
1 57197U 23091AH 26155.24859823 .00020753 00000-0 58361-3 0 9997
2 57197 97.5082 224.5583 0008626 122.8984 237.3090 15.36490364162720Epoch: 2026-06-04T05:57Z
TLE epoch observation values (Epoch: 2026-06-04T05:57:58.887Z)
Latitude
-0.00008°
Longitude
-117.63264°
Altitude
462.796 km
Speed
7.633 km/s
True Right ascension
14h 58m 13s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:43:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.339 km
Perigee altitude
447.553 km
Semi-major axis
6,831.583 km
Eccentricity
0.00086
Inclination
97.5082°
RAAN
224.5583°
Arg. of periapsis
122.8984°
True anomaly
237.22586°
Mean anomaly
237.309°
Eccentric anomaly
237.26742°
Mean motion
3.8438 °/min
Orbital period
93.66 mins
BSTAR
0.00058361
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Other satellites on launch #91 in the year 2023 (2023-06-27 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.A-SEANSAT-PG1 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-06 17:54:42.945Z | 353.955° N | 2026-06-06 17:57:42.945Z | 278.098° WNW | 31.841° | 2026-06-06 17:59:42.945Z | 224.673° SW |
| 5 mins | 2026-06-07 04:26:42.945Z | 144.416° SSE | 2026-06-07 04:28:42.945Z | 65.263° ENE | 38.82° | 2026-06-07 04:31:42.945Z | 358.126° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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