NEONSAT-1, 59587
Orbit data source: Space-Track
NEONSAT-1, 59587 is a payload satellite owned by KAIST (KR) in SSO that was launched on Tue, 23 Apr 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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59587 intel report (Beta)
NEONSAT-1 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 5 hours ago |
| Origin | |
| Manufacturer | KAIST/SATRHW |
| Mission | Operational spacecraft |
| Bus & Motor | NEONSAT, Unknown motor |
| Mass | ~100 kg wet, ~100 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 5 hours ago
0 NEONSAT-1
1 59587U 24077A 24330.10073169 .00017185 00000-0 72890-3 0 9994
2 59587 97.4003 46.7195 0011844 255.1099 104.8826 15.23116162 32664Epoch: 2024-11-25T02:25Z
Definitive object data (Epoch: 2024-11-25T02:25:03.218Z)
| Latitude | -0.00003° |
| Longitude | -54.0738° |
| Altitude | 501.643 km |
| Speed | 7.612 km/s |
| True Right ascension | 03h 06m 52s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 65.57294° |
| Longitude | -70.39016° |
| Altitude | 515.844 km |
| Speed | 7.607 km/s |
| Apparent Right ascension | 19h 02m 08s |
| Apparent Declination | 33° 23' 33" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 04:44:49 |
| Azimuth | 331.427° NNW |
| Elevation | -10.118° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 501.548 km |
| Perigee altitude | 485.271 km |
| Semi-major axis | 6,871.546 km |
| Eccentricity | 0.0011844 |
| Inclination | 97.4003° |
| RAAN | 46.7195° |
| Arg. of periapsis | 255.1099° |
| True anomaly | 105.01372° |
| Mean anomaly | 104.8826° |
| Eccentric anomaly | 104.94816° |
| Mean motion | 3.81032 °/min |
| BSTAR | 0.0007289 |
| Orbital period | 94.48 mins |
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Other satellites on launch #77 in the year 2024 (2024-04-23 UTC)
| NEONSAT-1, 59587 |
| ACS 3, 59588 |
| ELECTRON R/B, 59589 (Decayed) |
| ELECTRON KICK STAGE R/B, 59590 |
NEONSAT-1 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 | 2024-11-25 18:45:21.122Z | 339.227° N | 2024-11-25 18:47:21.122Z | 289.011° WNW | 27.67° | 2024-11-25 18:50:21.122Z | 226.515° WSW |
| 6 mins | 2024-11-26 05:21:21.122Z | 166.553° S | 2024-11-26 05:24:21.122Z | 350.26° N | 42.517° | 2024-11-26 05:27:21.122Z | 348.414° N |
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