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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 A-SEANSAT-PG1
1 57197U 23091AH 26207.57869534 .00018916 00000-0 50372-3 0 9993
2 57197 97.5065 278.0318 0005041 298.3663 61.7073 15.38229591170769Epoch: 2026-07-26T13:53Z
TLE epoch observation values (Epoch: 2026-07-26T13:53:19.277Z)
Latitude
-0.00003°
Longitude
125.42688°
Altitude
452.826 km
Speed
7.642 km/s
True Right ascension
18h 32m 07s
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
17:04:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
451.732 km
Perigee altitude
444.849 km
Semi-major axis
6,826.427 km
Eccentricity
0.0005
Inclination
97.5065°
RAAN
278.0318°
Arg. of periapsis
298.3663°
True anomaly
61.75818°
Mean anomaly
61.7073°
Eccentric anomaly
61.73274°
Mean motion
3.84816 °/min
Orbital period
93.55 mins
BSTAR
0.00050372
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-27 04:05:36.947Z | 112.046° ESE | 2026-07-27 04:07:36.947Z | 65.59° ENE | 20.553° | 2026-07-27 04:09:36.947Z | 23.864° NE |
| 4 mins | 2026-07-27 17:00:36.947Z | 52.53° ENE | 2026-07-27 17:02:36.947Z | 102.433° ESE | 22.48° | 2026-07-27 17:04:36.947Z | 146.249° SSE |
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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