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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 11 hours ago
TLE from 11 hours ago
0 A-SEANSAT-PG1
1 57197U 23091AH 25304.83733703 .00018711 00000-0 68217-3 0 9997
2 57197 97.5414 5.6188 0009215 161.1602 198.9980 15.28181548129732Epoch: 2025-10-31T20:05Z
TLE epoch observation values (Epoch: 2025-10-31T20:05:45.919Z)
Latitude
-0.00001°
Longitude
23.80143°
Altitude
490.325 km
Speed
7.616 km/s
True Right ascension
00h 22m 28s
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
02:42:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.527 km
Perigee altitude
471.891 km
Semi-major axis
6,856.346 km
Eccentricity
0.00092
Inclination
97.5414°
RAAN
5.6188°
Arg. of periapsis
161.1602°
True anomaly
198.96366°
Mean anomaly
198.998°
Eccentric anomaly
198.98083°
Mean motion
3.823 °/min
Orbital period
94.17 mins
BSTAR
0.00068217
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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 | 2025-11-01 17:04:48.002Z | 11.293° NNE | 2025-11-01 17:07:48.002Z | 0.524° NNE | 44.082° | 2025-11-01 17:10:48.002Z | 194.4° SSW |
| 4 mins | 2025-11-02 03:40:48.002Z | 118.591° SE | 2025-11-02 03:42:48.002Z | 62.636° ENE | 26.606° | 2025-11-02 03:44:48.002Z | 17.744° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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