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: 13 hours ago
TLE from 13 hours ago
0 A-SEANSAT-PG1
1 57197U 23091AH 26105.92080828 .00009570 00000-0 28535-3 0 9992
2 57197 97.5126 174.2661 0005989 303.6315 56.4356 15.34863039155158Epoch: 2026-04-15T22:05Z
TLE epoch observation values (Epoch: 2026-04-15T22:05:57.835Z)
Latitude
-0.00002°
Longitude
-1.30065°
Altitude
462.171 km
Speed
7.637 km/s
True Right ascension
11h 37m 03s
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
18:04:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.372 km
Perigee altitude
454.184 km
Semi-major axis
6,836.415 km
Eccentricity
0.0006
Inclination
97.5126°
RAAN
174.2661°
Arg. of periapsis
303.6315°
True anomaly
56.49281°
Mean anomaly
56.4356°
Eccentric anomaly
56.4642°
Mean motion
3.83973 °/min
Orbital period
93.76 mins
BSTAR
0.00028535
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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 | 2026-04-16 17:25:43.793Z | 10.434° NNE | 2026-04-16 17:28:43.793Z | 340.234° N | 44.408° | 2026-04-16 17:31:43.793Z | 195.629° SSW |
| 4 mins | 2026-04-17 03:58:43.793Z | 119.584° SE | 2026-04-17 04:00:43.793Z | 68.214° E | 24.965° | 2026-04-17 04:02:43.793Z | 20.857° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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