SNUSAT-2, 43782
Orbit data source: Space-Track
SNUSAT-2, 43782 is a payload satellite owned by SNU (KR) in SSO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets 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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43782 intel report (Beta)
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SNUSAT-2 radio frequencies
SNUSAT-2 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 10 hours ago |
| Origin | |
| Manufacturer | SNU |
| Mission | Operational Amateur Technology |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | 4 kg wet, 4 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, 0.3 m |
| Radar Cross Section | 0.035 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 SNUSAT-2
1 43782U 18099AA 24361.09483433 .00014913 00000-0 91078-3 0 9997
2 43782 97.4889 53.3473 0013372 11.5152 348.6381 15.10312667331481Epoch: 2024-12-26T02:16Z
Definitive object data (Epoch: 2024-12-26T02:16:33.686Z)
| Latitude | 0.00001° |
| Longitude | -75.87222° |
| Altitude | 529.256 km |
| Speed | 7.603 km/s |
| True Right ascension | 03h 33m 23s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 48.03446° |
| Longitude | 112.89894° |
| Altitude | 547.585 km |
| Speed | 7.59 km/s |
| Apparent Right ascension | 20h 06m 30s |
| Apparent Declination | 11° 30' 31" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:45:16 |
| Azimuth | 57.143° ENE |
| Elevation | -17.841° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 541.469 km |
| Perigee altitude | 522.987 km |
| Semi-major axis | 6,910.365 km |
| Eccentricity | 0.0013372 |
| Inclination | 97.4889° |
| RAAN | 53.3473° |
| Arg. of periapsis | 11.5152° |
| True anomaly | 348.60786° |
| Mean anomaly | 348.6381° |
| Eccentric anomaly | 348.62299° |
| Mean motion | 3.77826 °/min |
| BSTAR | 0.00091078 |
| Orbital period | 95.28 mins |
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Other satellites on launch #99 in the year 2018 (2018-12-03 UTC)
SNUSAT-2 Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-26 17:09:45.996Z | 337.918° N | 2024-12-26 17:11:45.996Z | 285.59° WNW | 29.174° | 2024-12-26 17:14:45.996Z | 225.839° WSW |
| 5 mins | 2024-12-27 03:51:45.996Z | 176.067° S | 2024-12-27 03:53:45.996Z | 292.123° WNW | 43.954° | 2024-12-27 03:56:45.996Z | 344.126° N |
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