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: 7 hours ago
TLE from 7 hours ago
0 A-SEANSAT-PG1
1 57197U 23091AH 26162.80243669 .00017132 00000-0 47809-3 0 9994
2 57197 97.5088 232.2692 0008504 101.0156 259.2045 15.36773280163880Epoch: 2026-06-11T19:15Z
TLE epoch observation values (Epoch: 2026-06-11T19:15:30.530Z)
Latitude
0.00002°
Longitude
43.25098°
Altitude
459.862 km
Speed
7.636 km/s
True Right ascension
15h 29m 04s
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
12:54:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.415 km
Perigee altitude
446.798 km
Semi-major axis
6,830.743 km
Eccentricity
0.00085
Inclination
97.5088°
RAAN
232.2692°
Arg. of periapsis
101.0156°
True anomaly
259.1088°
Mean anomaly
259.2045°
Eccentric anomaly
259.15665°
Mean motion
3.84451 °/min
Orbital period
93.64 mins
BSTAR
0.00047809
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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 | 2026-06-12 04:45:30.862Z | 172.066° S | 2026-06-12 04:48:30.862Z | 260.234° W | 44.225° | 2026-06-12 04:51:30.862Z | 344.345° N |
| 5 mins | 2026-06-12 17:42:30.862Z | 359.308° N | 2026-06-12 17:44:30.862Z | 267.707° W | 41.549° | 2026-06-12 17:47:30.862Z | 203.287° SW |
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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