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: 8 hours ago
TLE from 8 hours ago
0 A-SEANSAT-PG1
1 57197U 23091AH 26256.92854183 .00017092 00000-0 43290-3 0 9995
2 57197 97.4996 328.5479 0007928 117.7572 242.4478 15.39771284178351Epoch: 2026-09-13T22:17Z
TLE epoch observation values (Epoch: 2026-09-13T22:17:06.014Z)
Latitude
-0.00004°
Longitude
1.35669°
Altitude
452.406 km
Speed
7.64 km/s
True Right ascension
21h 54m 11s
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
22:40:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.137 km
Perigee altitude
438.32 km
Semi-major axis
6,821.866 km
Eccentricity
0.00079
Inclination
97.4996°
RAAN
328.5479°
Arg. of periapsis
117.7572°
True anomaly
242.36729°
Mean anomaly
242.4478°
Eccentric anomaly
242.40754°
Mean motion
3.85202 °/min
Orbital period
93.46 mins
BSTAR
0.0004329
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-14 17:33:12.025Z | 20.073° NNE | 2026-09-14 17:36:12.025Z | 77.422° E | 56.596° | 2026-09-14 17:39:12.025Z | 179.375° S |
| 4 mins | 2026-09-15 05:37:12.025Z | 225.051° WSW | 2026-09-15 05:39:12.025Z | 275.422° WNW | 22.245° | 2026-09-15 05:41:12.025Z | 314.692° NW |
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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