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). 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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59587 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SKORRelated business
Manufacturer
KAIST/SATRHW
Mission
Operational Civil Imaging
Bus & Motor
NEONSAT, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + Cyl + 4 Pan, 0.5 m
Radar Cross Section
0.625 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 NEONSAT-1
1 59587U 24077A 25289.22685153 .00014558 00000-0 47949-3 0 9991
2 59587 97.3707 8.7086 0011031 178.1553 181.9731 15.31525715 82302Epoch: 2025-10-16T05:26Z
TLE epoch observation values (Epoch: 2025-10-16T05:26:39.972Z)
Latitude
-0.00002°
Longitude
-97.94755°
Altitude
481.919 km
Speed
7.62 km/s
True Right ascension
00h 34m 50s
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
11:29:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.761 km
Perigee altitude
460.656 km
Semi-major axis
6,846.346 km
Eccentricity
0.0011
Inclination
97.3707°
RAAN
8.7086°
Arg. of periapsis
178.1553°
True anomaly
181.96875°
Mean anomaly
181.9731°
Eccentric anomaly
181.97093°
Mean motion
3.83138 °/min
Orbital period
93.96 mins
BSTAR
0.00047949
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Other satellites on launch #77 in the year 2024 (2024-04-23 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.NEONSAT-1 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 | 2025-10-16 18:32:42.597Z | 0.198° NNE | 2025-10-16 18:35:42.597Z | 280.226° WNW | 38.459° | 2025-10-16 18:38:42.597Z | 208.971° SW |
| 5 mins | 2025-10-17 05:06:42.597Z | 136.008° SSE | 2025-10-17 05:08:42.597Z | 74.505° E | 34.322° | 2025-10-17 05:11:42.597Z | 3.897° NNE |
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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